20050627000042005062700004EA 2005 6 27 SWIA200515090 120050530A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07720SW 7297 OVERHEAD EMERGENCY LIGHT IN CABIN INOPERATIVE. RELAMPED OVERHEAD FWD EMERGENCY LAMP. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050711000112005071100011CE 2005 7 11 DXTA200500818 120050704A3350 LIGHT CESSNA500 560CESSNA 2076750CE CABIN MALFUNCTIONED E DXTAK NONE N FALSE WARNING ININSP/MAINT 1 GL07341QS 5600341 EMERGENCY LIGHTS WILL NOT EXTINGUISH DUE TO A HARD LANDING. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20050627000012005062700001EA 2005 6 27 SWIA200515087 120050520A2597 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA FLAP SCEW INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07905SW 7437 FLAP SKEW DETECTION SYSTEM INOPERATIVE. REPLACED CONNECTOR 1J9CE IAW WDM 27-51-00. OPERATIONAL CHECK GOOD IAW MM 27-51-00. 2L72 4F RTA21EA 20050627001552005062700155NM 2005 6 27 QXEA200501064 120050617A5230 HANDLE BOMBDRDHC8 DHC8402 1390042NM PAX DOOR UNSECURE A QXEAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 NM09408QX 4050 SEA - ON FLIGHT 2438, RETURNED TO FIELD SEA-GEG, (MASTER WARNING) BAGGAGE DOOR LIGHT AND LOSS OF PRESSURIZATION AT 3000 FEET. INSPECTED AND FOUND LATCH HANDLE EXTENDED. OPENED DOOR AND INSPECTED. FOUND NO DEFECTS. RESET LATCH. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20081024 NM 2008 10 24 DL76G081358 120050630A5751 SKIN BOEING767 7673P6 1385105NM LT AILERON DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27156DL 25354 SPARE REMOVED FROM A/C 1506. LT OTBD AILERON UPPER SKIN, LOWER SKIN, CORE AND TAILING EDGE WEDGE DAMAGED AT WS 1025. A NEW SECTION OF CORE WAS INSTALLED, UPPER AND LOWER SKINS REPAIRED WITH REPAIR PLIES AND ADDED PLIES AND TRAILING EDGE WEDGE SPLICED IN. 2L72 4F RTA1NM 20050623000092005062300009EA 2005 6 23 MASA200500395 120050525A5210 HAND RAIL CNDAIRCL600 CL6002B19 1900309EA PAX DOOR OBSTRUCTED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07154SF 7154 ASH 2628 CLT. THE CREW REPORTED THAT THE PASSENGER DOOR WOULD NOT CLOSE IN THE DOOR FRAME. AFTER SEVERAL HOURS OF RIGGING, MAINTENANCE REMOVED THE DEBRIS FROM THE HAND RAILS. OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA21EA 20050623000022005062300002NM 2005 6 23 AALA20050385 120050611A3350 LIGHT BOEING777 777223 1385213NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW21774AN 29581 MIA - EMERGENCY LIGHT ASSEMBLY AT FIRST CLASS CLOSET IN FORWARD GALLEY BROKEN. REPLACED EMERGENCY LIGHT ASSEMBLY AT FIRST CLASS CLOSET IN FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20051003001152005100300115EU 2005 10 3 2005UALA01005 120050921A5313 STRINGER AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FR 55-57 CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29415UA 475 STR 42L HAS CORROSION BETWEEN FR 55 AND FR 57. 2L72 4F4 FRTA28NM E40NE 20050317000922005031700092NM 2005 3 17 2005UALA00206 120050302A5322 SHEAR TIE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29582UA 26702 AFT PIT STA 1440 SHEAR TIE CORRODED BETWEEN STR 29L AND 30L. A REPLACEMENT SHEAR TIE WAS FABRICATED AND INSTALLED. 2L72 4F4 FRTA2NM E17NE 20060210000072006021000007SO 2006 2 10 MASA200500619 120050807A3350 SWITCH EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL EMRG LIGHT SYS NOT CLOSED A MASAK NONE O OTHER NRNOT REPORTED 1 SW07853MJ 145464 ASH 2674 GSP. FIRST FLOOR EMERG PATH EXIT LIGHT WILL NOT ILLUMINATE. CONTRACT MX PLACED EMERG LIGHT SW TO ARM FOR CHARGING FOR 1 HOUR. OPS NML. NO OTHER DEFECTS NOTED. 2L72 4T4 FRTT00011ATTE6CH 20050929000012005092900001NM 2005 9 29 05FDEA02993 120050919A5230 WEB BOEING727 727200 138407ENM CARGO DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25268FE 21674 FWD CARGO DOOR INNER WEB CRACKED AT UPPER MIDDLE RIVNUT. REPAIRED FWD CARGO DOOR INNER WEB PER FED EX EA 7-5230-91364. 2L73 4F RTA3WE 20050801000822005080100082EA 2005 8 1 A6WA200540248 120050717A5246 DOOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUEL TANK DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31420AW 7640 RT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT FOR PANEL 640BB HAS FRETTING DAMAGE. 2 INCH LONG X .125 INCH WIDE. REPAIRED BY BLENDING AND TREATING DAMAGED AREA IAW REO. (K) 2L72 4F4 FRTA21EA E15NE 20060210000082006021000008SO 2006 2 10 MASA200500620 120050807A3350 SWITCH EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL EMRG LIGHT SYS NOT CLOSED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07853MJ 145464 ASH 2674 GSP ROW 12 D,F EMERG EXIT LIGHT WILL NOT ILLUMINATE. CONTRACT MX PLACED EMERG LIGHT SW TO ARM FOR CHARGING FOR 1 HOUR. OPS NML. NO OTHER DEFECTS NOTED. 2L72 4T4 FRTT00011ATTE6CH 20050705000092005070500009EU 2005 7 5 USAA050691 120050518A5315D5347209300000 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSLEAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19716UW 1055 PIT - FOUND FLOORBEAM CORRODED 3 FT BY 3 INCHES, FLOORBEAM AT -Y31 BETWEEN FRAME 67-70. REPLACED FLOORBEAM PER AIRBUS DWG D53471815 AND TR 51-40-01. (M) 2L72 4F RTA28NM 20060609001132006060900113CE 2006 6 9 DBCA122DA 120050515A3230 CONTROL UNIT CESSNA650 650 2076802CE MLG FAILED E DBCAO OTHER O OTHER NRNOT REPORTED 1 GL13605SA 2744 6500152 AFTER DEPARTING, THE LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO DEPARTURE, LANDING WAS UNEVENTFUL. RECEIVING SPECIAL FLIGHT PERMIT DATED 8 MAY 06 FROM FSDO SW01. FERRIED AIRCRAFT, LANDING GEAR CONTROL REPLACED. OPERATION CHECKED GOOD. (K) 2L72 4F A9NM 20050209001362005020900136NM 2005 2 9 MASA200500024 120050109A33501317 BULB DHAV DHC8 DHC8202 2809007NM EMERGENCY LIGHTSBURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07989HA 427 FLOOR PROXIMITY EMERGENCY ESCAPE PATH MARKING SYSTEM HAS A LIGHT THAT IS OUT. MAINTENANCE RELAMPED THE LIGHT. 2H72 4T RTA13NM 20050711000312005071100031NM 2005 7 11 WRLA2005125 120050622A5510 STRUCTURE DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C-04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098, FOUND CORROSION IN HST LT BARREL NUT HOLE NR 36. 2L73 4F4 FRTA22WE E24NE 20050302001652005030200165NM 2005 3 2 USAA050075 120050101A5320 STIFFENER BOEING737 7373B7 1384580NM MLG WW CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19522AU49282 23857 PIT - FOUND STIFFENER CRACKED .75 INCH, MAIN LANDING GEAR WHEEL WELL BS 663.75 AT LBL 6.15. REPLACED STIFFENER PER EA 75002 AND BOEING DWG 65-45402. (M) 2L72 4F RTA16WE 20050323001932005032300193WP 2005 3 23 AALA20050210 120050320A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217532A 49924 DTW - OVERHEAD EMERGENCY LIGHTS AT ROW 6 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT ROW 6. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050323001952005032300195WP 2005 3 23 AALA20050209 120050321A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217543A 53025 PHX - EMERGENCY LIGHTS AT OVERHEAD MID CABIN INOPERATIVE. REPLACED BATTERY CHARGER FOR EMERGENCY LIGHTS AT MID CABIN OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050323001972005032300197NM 2005 3 23 SWAA050764 120050313A53206517590 WEB BOEING737 7373L9 1384470NM COCKPIT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND FLOOR WEB CRACKED RT SIDE BETWEEN BS 188 & BS 196, WL 208. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050323001992005032300199NM 2005 3 23 SWAA050754 120050311A276065463607 MIXER BOX BOEING737 7373A4 1384585NM LT WING W/W FAULTY A SWAAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SW29679AA 23291 AIR TURNBACK IMMEDIATELY AFTER TAKEOFF, NOTED HEAVY ROLL TO LT, ACCOMPANIED BY CONSIDERABLE RUMBLING. REQUIRED 5 UNITS OF RUDDER TRIM & UNKNOWN AILERON TRIM AT 1/2 YOKE DEFLECTION TO LEVEL WINGS. REMOVED AND REPLACED SPOILER MIXER & NR 3 SPOILER ACTUATOR PER MM. 2L72 4F RTA16WE 20050323002012005032300201NM 2005 3 23 SWAA050765 120050312A33507003661 BALLAST BOEING737 7375H4 138449DNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29502SW 24179 DURING SCHEDULED SERVICE CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BALLAST ASSY PER MM. 2L72 4F RTA16WE 20050324000122005032400012EA 2005 3 24 QXEA200500189 120050124A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - RIGHT INBOARD SEAT RAIL, AT STATION X396, HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01, REO 670-53-00-060, REV B. AND HORIZON AIR EA R-53-266. 2L72 4F RTA21EA 20050324000292005032400029CE 2005 3 24 DELA200500003 120050214A750067469 GASKET LEAR 55 55LEAR 5170702CE BLEED AIR DUCT LEAKING E DELAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03903JC 081 RIGHT ENGINE FIRE WARNING ILLUMINATED IN FLIGHT AT FL250. AFM PROCEDURES FOLLOWED, THROTTLE RETARDED TO IDLE AND WARNING CEASED. THROTTLE SLOWLY RETURNED TO CRUISE POWER WITHOUT INCIDENT. MAINTENANCE FOUND LEAKING BLEED AIR PIPE GASKET NEAR PYLON FIRE DETECTION LOOP. GASKET WAS REPLACED AND GROUND RUN, LEAK CHECKS AND OPERATIONAL CHECKS SATISFACTORY. 2L72 4F A10CE 20050324000412005032400041NM 2005 3 24 WRLA2005027 120050216A5512 SKIN DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST LT BARREL NUT HOLE NR 21. 2L73 4F4 FRTA22WE E24NE 20050324000442005032400044SO 2005 3 24 C2XA05CL010 120050215A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714960 145100 CLE FLIGHT NR 2107, CREW REPORTED THAT THE GALLEY AND BULKHEAD EMERGENCY LIGHTS WERE INOP. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM, AND DID NOT FIND AND DEFECTS. SYSTEM OPERATIONALLY CHECKED GOOD. 2L72 4T RTT00011AT 20050324000622005032400062EU 2005 3 24 AWXA200500263 120050215A5315D5347209800000 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28647AW 762 MCN - MAJOR REPAIR - DURING 8-DAY CHECK, CORROSION WAS FOUND ON FLOORBEAM Y35 AT FS 64. MAINTENANCE REMOVED CORRODED FLOORBEAM Y35 AT FS 64; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-49-00. 2L72 4F RTA28NM 20050324000662005032400066WP 2005 3 24 05FDEA00485 120050310A5310AJC7207181 DOOR FRAME DOUG DC10 DC1030 3023501WP ZONE 100 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25311FE 46871 C/W EA8-5310-55459 FUSELAGE-MAIN FRAME-AFT ENTRY DOOR JAMB REPAIR (P/N AJC7207- 181). CLOSING ACTION 03/10/05 C/W EA8-5310-55459. ON NO. S00017. 2L73 4F A22WE 20050324000682005032400068NM 2005 3 24 WRLA2005020 120050131A5313 LONGERON DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11273 48519 DURING "C2" CHECK, FOUND CORROSION ON LONGERON L46L BETWEEN STA 5-73 AND STA 5-93. CUT AND REMOVED CORRODED SECTION BETWEEN STA 5-63 AND 5-103, CUT FRAME STA 5-73 TO STA 5-93 TO PROVIDE ACCESS FOR REMOVAL/INSTALLATION OF LONGERON L46L. FABRICATED NEW LONGERON SECTION FROM 1D0865T, 7150-T61511 EXTRUSION, FABRICATED LONGERON SPLICE FITTING FROM 7150-T61511 EXTRUSION PER MD11 SRM 53-10-00 VOL I. INSTALLED REPAIR PARTS. FABRICATED FRAME REPAIR PARTS AND HEATED THE REPAIR PARTS TO T6. CONDITION CHECK SATISFACTORY REF MD11 SRM 53-30-00 VOL I. 2L73 4F4 FRTA22WE E24NE 20050324000712005032400071CE 2005 3 24 2003793 120050214A5330 SKIN BEECH 1900 1900D 1154162CE FUSELAGE CORRODED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03179GL UE179 DURING ROUTINE STRUCTURAL INSPECTION, CORROSION WAS FOUND ON INSIDE SKIN NEAR MAIN PAX DOOR HANDLE DOUBLER APPROX 2" BY 2" AREA. AREA REPAIRED, AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA24CE 20050324000852005032400085NM 2005 3 24 2005UALA00245 120050314A2613 OVERHEAT LOOP BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE NR 1 ENGINE MALFUNCTIONED A UALAE ENGINE SHUTDOWN N FALSE WARNING DEDESCENT 1 WP29935UA 26663 SHUT DOWN NR 2 ENG DUE TO OVERHEAT INDICATION. CREW REPORTED NR 2 ENG OVERHEAT LIGHT CAME ON WITH NO ABNORMAL ENGINE INDICATION. OVERHEAT LIGHT STAYED ON AFTER THE CHECKLIST. CREW SHUT DOWN NR 2 ENGINE. OVERHEAT LIGHT WENT OUT. UPON ARRIVAL AT THE GATE BOTH A & B LOOPS TESTED NORMAL. FOUND LOWER FAN DETECTOR M1121, LOOPS A & B WITH LOW RESISTANCE. ALSO REPLACED UPPER FAN DETECTOR M1120, LOOP A. ENG OVERHEAT DETECTION SYSTEM TESTED NORMAL AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA16WE E2GL 20050324001162005032400116 2005 3 24 DJFA2005057 420050210A3425 DISPLAY BEECH MU300 400A 1155402CE COCKPIT MALFUNCTIONED E DJFAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA23792TA RK264 SHORTLY AFTER TAKEOFF CREW NOTICED AN INCREASING TREND OF A BURNING ELECTRICAL SMELL. AFTER APROXIMATELY 15 MINUTES THE NR 2 PRIMARY FLIGHT DISPLAY FAILED WITH A "DISPLAY TEMP" FLAG. THE APPROPRIATE CIRCUIT BREAKER WAS PULLED, AND AIRCRAFT RETURNED TO KAPA WITHOUT FURTHER INCIDENT. MAINTENANCE VERIFIED THE FAULT AND FOUND LOW AIR FLOW TO THE NR 2 PRIMARY FLIGHT DISPLAY. AFTER REMOVING AN INK PEN FROM THE COOLING FAN AIRFLOW WAS BACK TO A NORMAL STRONG FLOW. THE NR 2 PRIMARY FLIGHT DISPLAY WAS REINSTALLED, AND OPERATIONALLY CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4F RTA16SW 20050324001212005032400121CE 2005 3 24 20030802 120050226A5320 STRUCTURE BEECH 1900 1900D 1154162CE FUSELAGE DAMAGED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03150GL UE150 ON ROUTINE INSPECTION, A SMALL LIGHTNING HOLE FOUND ON BOTTOM SIDE OF FUSELAGE DIRECTLY IN FRONT OF AFT PRESS BULKHEAD AT FS 545.50. REPAIRED, AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA24CE 20050324001262005032400126NM 2005 3 24 P5CA0501322 120050212A5230 SKIN BOEING747 74746NF 13848BTNM CARGO DOOR DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 EA15451PA 30809 ON WALK AROUND FOUND PUNCTURE DAMAGE ON OUTERSKIN OF BULK CARGO DOOR. DAMAGE WAS .7500 ROUND IN DIAMETER 10 INCHES FROM FRONT EDGE, 6 INCHES FROM LOWER EDGE. REPAIRED PER SRM 52-00-01. COI 451-008 RAISED FOR INTERIM REPAIR. 2L74 4F RTA20WE 20050324001542005032400154EA 2005 3 24 QXEA200500194 120050123A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - RIGHT INBOARD SEAT RAIL, AT STATION X478 HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW CRJ700 SRM 51-21-00-001-001-A01, REO 670-53-00-060, REV B AND HORIZON AIR EA R -53-266. 2L72 4F RTA21EA 20050324001562005032400156NM 2005 3 24 WRLA2005080 120050226A5340 ANGLE DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE OVERWING TANK CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK INSPECTION, FOUND OVERWING TANK REAR SPAR LOWER CHORD REINFORCE ANGLE SURFACE CORROSION AT STA 1376 BETWEEN X=37.5 AND X=-37.5 (LENGTH = 57"). 2L73 4F4 FRTA22WE E24NE 20050324001612005032400161NM 2005 3 24 WRLA2005019 120050131A5347 SEAT TRACK DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11273 48519 DURING "C2" CHECK FOUND CABIN SEAT TRACK CORROSION BETWEEN STA 858 AND STA 873 X=27.5. CUT AND REMOVED CORRODED SECTION BETWEEN STA 832 AND 909 X=27.5, FABRICATED AND INSTALLED NEW SEAT TRACK SECTION AND SPLICE HAT. CONDITION CHECK SATISFACTORY REF MD11 SRM 53-70-00 FIG 1 REV 36 VOL I. 2L73 4F4 FRTA22WE E24NE 20050324001632005032400163NM 2005 3 24 ASMF200503009 120050312A71105930645509 NOSE COWL DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE RIGHT DAMAGED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23831LF10043 53050 716778 DURING TRANSIT CHECK, DETECTED DAMAGE IN RIGHT ENGINE NOSE COWLING BY FOREIGN OBJECT DAMAGE WITH LIP DENT DEPTH OF 0.150 PER 1 DIAMETER AT 03:00 POSITION. AIRCRAFT WAS SENT TO THE HANGAR AND NOSE COWLING WAS REPLACED IAW MM 71-10-01 PAGE 201, ALL CORRECT. 2L72 4F4 FRT E9NE 20050324001732005032400173SO 2005 3 24 C2XA05SH008 120050215A532014530644401 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO FUSLEAGE DAMAGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714940 145033 SHV - DURING C-CHECK, THE LT OMEGA BEAM AT FRAME 48 HAS DAMAGED SEAT TRACK SCREW HOLE. 2L72 4F RTT00011AT 20050324001772005032400177EA 2005 3 24 SWIA200514499 120050122A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07954SW 7815 FS 621 FLOOR SUPPORT ANGLE LBL 42 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. FLOOR SUPPORT ANGLE REPAIRED IAW CRJ REO 601R-53-61-117 REV B. 2L72 4F RTA21EA 20050324001802005032400180EA 2005 3 24 SWIA200514739 120050110A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07439SW 7578 FS 625 STRINGER 14, LT AND RT SIDE ANGLES CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED LT AND RT STRINGER 14 SIDE-ANGLES IAW CRJ 200 SRM 51-10-6 PG 3 PARA D & CRJ 200 SRM 51-42-06. 2L72 4F RTA21EA 20050324001822005032400182EA 2005 3 24 SWIA200514741 120050110A5340 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07439SW 7578 FS 280 BL RIGHT INBOARD ANGLE BRACKET CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ 200 SRM 51-42-06 PG 4 & 18 & 51-42-20 PG 3 & 16. 2L72 4F RTA21EA 20050324001852005032400185EA 2005 3 24 SWIA200514726 120050319A2741 SWITCH CNDAIRCL600 CL6002B19 1900309EA TRIM STUCK A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07978SW 7953 REMOVE AND REPLACE F/O'S TRIM SWITCH DUE TO COMPLAINT OF STICKING. REPLACED F/O TRIM SWITCH AS REQUIRED PER CRJ MM 27-41-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050324001872005032400187EA 2005 3 24 SWIA200514728 120050318A2741 SWITCH CNDAIRCL600 CL6002B19 1900309EA TRIM STUCK A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07927SW 7693 CAPTAIN`S TRIM SWITCH STICKS. REMOVED AND REPLACED CAPTAIN'S SIDE TRIM SWITCH IAW MM 27-41-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050324001982005032400198EU 2005 3 24 05FDEA00581 120050317A3040 CONTROLLER AIRBUS300 A300F4605R 3930327EU WINDOW TEMP MALFUNCTIONED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25660FE 759 AFTER TAKEOFF GOT RIGHT AND RIGHT LATERAL WINDOW HEAT FAULT. C/W ECAM AND RESET, FAULTED SECOND TIME AND REMAINED OFF FOR REMAINDER OF FLIGHT. NOTE: NO ECAM CHIME. REPLACED RIGHT WINDOW TEMP CONTROLLER, REF M/M 32-42-11. OPS CHECKS OK. MFG 6664157. 2L72 4F RTA35EU 20050324002002005032400200EU 2005 3 24 05FDEA00583 120050317A5347 SEAT TRACK AIRBUS310 A310222 3930315EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 MAIN DECK CARGO COMPT LEFT NR 3 SEAT TRACK, FR48, FR49.5, FR51.5, FR53.5, 4 EA AREAS OF CORROSION INSIDE SCALLOP HOLES AS MARKED. REMOVED AND REPLACED SEAT TRACK SECTION BETWEEN FRAME 50.5 TO 54 IAW A310-200 SRM 53-10-16. 2L72 4F RTA35EU 20050325000152005032500015NM 2005 3 25 UPS05444153 120050312A532269B028032 SHEAR TIE BOEING747 747121 1384871NM M/D CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE:C M/D - BS 1780 BETWEEN S10-11R FRAME ATTACH SHEAR TIE FOUND CRACKED, CRACK LENGTH .375 INCH. M/D - BS 1780 BETWEEN S10-11R FRAME ATTACH SHEAR TIE REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02. 2L74 4F A20WE 20050325000302005032500030EA 2005 3 25 SWIA200514746 120050307A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07442SW 7609 MAIN FUSELAGE FS 280 LBL 9.0 LOWER FLANGE CRACKED ON TRANSVERSE BEAM. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR IAW CRJ REO 601R-53-11-138 REV NC. 2L72 4F RTA21EA 20050325000322005032500032EA 2005 3 25 SWIA200514748 120050307A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07442SW 7609 FUSELAGE PULLEY INTERCOSTAL HAS A PREVIOUS REPAIRED CRACKED ANGLE FS 484.00 LBL 36.0. ITEM FOUND AT C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ REO 601R-53-41-059 REV A. 2L72 4F RTA21EA 20050325000432005032500043EA 2005 3 25 SWIA200514753 120050309A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07953SW 7813 LEFT FLOORBEAM ANGLE AT FS 621.00 IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. CRACKED FLOOR SUPPORT REPAIRED IAW CRJ REO 601R-53-61-117 REV B. 2L72 4F RTA21EA 20050325000462005032500046NM 2005 3 25 05FDEA00614 120050321A5710 STIFFENER BOEING727 727200 138407ENM FUEL CELL CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 RIGHT WING INTERNAL FUEL CELL UPPER STIFFENER NR 9 IS CRACKED AT WS 656.5. REPAIRED PER E.A. 7-5710-86251. 2L73 4F RTA3WE 20050325000502005032500050NM 2005 3 25 QXEA200500419 120050203A5730 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - LEFT WING PANEL 522BT BOTTOM SURFACE OF PANEL PITTING AND FRETTING CORROSION AROUND PANEL ATTACH HOLES. REPAIRED IAW RD 8/4-87-422. 2H72 4T RTA13NM 20050325000552005032500055EU 2005 3 25 05FDEA00603 120050318A5230 STRUCTURE AIRBUS310 A310222 3930315EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 CORROSION FOUND UNDER THE NR 9 LATCH ROLLER FOR FWD CARGO DOOR. COMPLIED WITH EA 6-5310-86132. 2L72 4F RTA35EU 20050325000672005032500067EU 2005 3 25 MALA050286 120050319A3030QR5OV SENSOR SAAB SF340 340B 7860101EU PITOT HEAT MALFUNCTIONED A MALAO OTHER J WARNING INDICATION CRCRUISE 1 GL15446XJ 340B446 LT PITOT HEAT ILLUMINATED INFLIGHT. CREW DECIDED TO RETURN TO MSP RATHER THAN BYPASS EAU TO RHI. REPLACED 5HG CURRENT SENSOR P/N ON/OFF QR5OV. LT PITOT HEAT CHECKS GOOD IAW SF340 MM CH 30. 2L72 4T RTA52EU 20050325000712005032500071NM 2005 3 25 QXEA200500427 120050129A5730 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - LEFTHAND WING, LEFTHAND FUEL PANEL REBATE AT 522AT HAS CORROSION AROUND SCREW HOLES, TOP SURFACE. REPAIRED IAW Q400 SRM SUB TASK 57-10-30-940-002. 2H72 4T RTA13NM 20050325000732005032500073WP 2005 3 25 DHL2005805521 120050308A534774529523 CARGO TRACK DOUG DC8 DC873F 302199FWP CARGO BAY DETERIORATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT NR 5 TRACK PLUG DETERIORATED AT STA 158.000. REMOVED DETERIORATED NR 5 TRACK PLUG IAW SRM 51-3-0 PG 1-2. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW TRACK PLUG IAW SRM 51-3-0 PG 1-2. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050325000772005032500077WP 2005 3 25 05FDEA00608 120050318A29101489951 SHUTOFF VALVE DOUG DC10 DC1030 3023501WP HYD SYSTEM LEAKING A FDEAJ DUMP FUEL K FLUID LOSS CLCLIMB 1 SO25302FE 46801 APPROXIMATELY 5 MINUTES AFTER TAKEOFF, MASTER CAUTION LIGHT ILLUMINATED AND OBSERVED BOTH LT & RT NR 2 EDP LIGHT ON, PRESSURE AND QUANTITY RAPIDLY WENT TO ZERO. FOUND 1-2 NONREVERSIBLE MOTOR PUMP SHUTOFF VALVE LEAKING FROM BACKUP RING. 2L73 4F A22WE 20050325001032005032500103EA 2005 3 25 COMA0560195 120050321A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS SYS ILLUMINATED A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01470CA 7650 FLIGHT 5393 FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20050325001212005032500121EU 2005 3 25 05FDEA00417 120050308A5347 SEAT TRACK AIRBUS310 A310222 3930315EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 MDCC NR 4 SEAT TRACK RT OF CENTER FROM FR 16 TO FR 19 CORRODED REF N00517. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-21. 2L72 4F RTA35EU 20050325001222005032500122EU 2005 3 25 05FDEA00418 120050308A5730 PANEL AIRBUS310 A310222 3930315EU RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 UPON REMOVAL OF LANDING AT RT WING HINGE PANEL ON L/E FOUND PANEL LANDING CRACKED REF N00915. REMOVED AND REPLACED PANEL LANDING IAW SRM 51-40-21 AND DRW A572-434548. 2L72 4F RTA35EU 20050325001242005032500124EU 2005 3 25 05FDEA00420 120050308A5347 SEAT TRACK AIRBUS310 A310222 3930315EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 MDC NR 4 SEAT TRACK RT OF CENTER AT FR19 ON I/B SPLICE HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED SPLICE ANGLE AT FR19 IAW SRM 51-40-21. 2L72 4F RTA35EU 20050325001262005032500126NM 2005 3 25 SWAA050781 120050314A53206546833 WEB BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29605SW 27956 DURING SCHEDULED D-CHECK, FOUND 2 EA FLOOR WEB CRACKS BETWEEN BS 188 TO BS 196, LBL 29 & RBL 29, WL 208. REMOVED AND REPLACED WEB SECTION PER SRM. 2L72 4F RTA16WE 20050325001352005032500135NM 2005 3 25 QXEA200500386 120050124A5340 STOP FITTING BOMBDRDHC8 DHC8401 1390041NM ZONE 200 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - AFT FUSELAGE - AFT ENTRY DOOR SURROUND STRUCTURE FORWARD STOP FITTING GOUGED AT STATION 668.900 AND STRINGER 19P. 2H72 4T RTA13NM 20050328000072005032800007SO 2005 3 28 SWIA200514764 120050207A5315 FLOORBEAM EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0758733 120197 RIGHT FLOOR SUPPORT ANGLE AT FRAME 44-47 IS CORRODED. ITEM FOUND AT C-CHECK INSPECTION. SUPPORT ANGLE REPLACED IAW EMB 120 SRM 57-40-02, 57-25-00, 51-23-00. 2L72 4T RTA31SO 20050328000122005032800012NM 2005 3 28 72300085 120050315A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1.5 X 18 INCH AREA OF CORROSION ON STRINGER. 2L73 4F4 FRTA3WE E2EA 20050328000142005032800014SO 2005 3 28 SWIA200514771 120050207A5347 SEAT TRACK EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0758733 120197 SEAT RAIL, LT OB CORRODED IN SEVERAL SPOTS AROUND THE SCREW HEADS. FR 15A AND FR32. (ITEM FOUND AT C-CHECK INSPECTION.) SEAT TRACK REPLACED IAW EMB 120 SRM 51-22-00, 51-25-00, 51-40-02. 2L72 4T4 TRTA31SO E20NE 20050328000202005032800020SO 2005 3 28 SWIA200514777 120050207A5347 SEAT TRACK EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0758733 120197 LT AFT SEAT TRACK AT YL 479.00 IS CORRODED. (ITEM FOUND AT C-CHECK INSPECTION.) INSTALLED SEAT TRACK IAW EMB 120 SRM 51-22-00, 51-40-02, 51-25-00. 2L72 4T4 TRTA31SO E20NE 20050328000522005032800052CE 2005 3 28 TZR2005F00001 120050304A3211509410 ATTACH FITTING CESSNA401 401A 207590DCE CONT O520 TSIO520E 17040SO MLG CRACKED E TZRAK NONE O OTHER ININSP/MAINT 1 SW05409TE8875 401A0118 THE LT AND RT MAIN LANDING GEAR HAD CRACKS ON THE BOSS AREA WHERE THE TORQUE LINKS ATTACH. THE CRACKS WERE ABOUT .2500 INCH LONG AND LACATED NEXT TO WHERE THE BOSS CONNECTS TO THE TUBE. (SW05200506155) (K) 1L72 3O3 O A7CE E8CE 20050328000542005032800054WP 2005 3 28 AALA20050192 120050303A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21297AA 49309 OVERHEAD EMERGENCY LIGHT AT ROW 20 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHT AT ROW 20. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F A6WE 20050328000552005032800055WP 2005 3 28 AALA20050193 120050313A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217535A 49989 ATL FORWARD ENTRY AND FORWARD GALLEY OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD LIGHTS AT FORWARD ENTRY AND FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F A6WE 20050328000572005032800057WP 2005 3 28 ASMF200503008 120050309A2910 SERVO VALVE DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE HYD SYSTEM LEAKING W ASMFK NONE K FLUID LOSS ININSP/MAINT 1 SW23753RA 49587 DURING TRANSIT CHECK WAS DETECTED HYDRAULIC LEAK IN THE DUAL SERVO VALVE OF LT WHEEL WELL . THE DUAL SERVO VALVE AND HYDRAULIC LINES WERE ADJUSTED IAW MM 32-43-03, TESTED CORRECT. 2L72 4F4 FRTA6WE E9NE 20050328000682005032800068CE 2005 3 28 2005F00039 120050308A531057111451 DOOR FRAME CESSNA414 414A 2075907CE CONT O520 TSIO520NB 17040SO FUSELAGE CRACKED D LZ2RK NONE O OTHER ININSP/MAINT 1 GL274057C3000 414A0848 LOWER DOOR FRAME CRACKING BY THE REAR HINGE. 1L72 3O3 O A7CE E8CE 20050328000802005032800080 2005 3 28 2005F00040 420050303A6122DCFS290D7 GOVERNOR CESSNA402 402B 207590PCE CONT O520 TSIO520E 17040SO RT ENGINE PROP SEIZED E DUFAO OTHER F FLT CONT AFFECTED CRCRUISE 1 GL273796C 1464 402B0803 WHILE IN CRUISE FLIGHT, THE RT ENGINE BEGAN TO LOSE RPM. THE PILOT PUSHED THE PROPELLER CONTROL LEVER ALL THE WAY FORWARD TO MAX RPM WITH NO CHANGE. THE PILOT DESCENDED AND MADE AN UNEVENTFUL LANDING. THE RT ENGINE QUIT ON ROLL OUT AND THE RT PROPELLER WENT INTO FEATHER. THE PROPELLER GOVERNOR WAS REMOVED AND APPEARED TO HAVE AN INTERNAL FAILURE. A SERVICEABLE GOVERNOR WAS INSTALLED AND OPS CHECKED OK. 1L72 3O3 O A7CE E8CE 20050328000812005032800081 2005 3 28 2005F00041 420050303A6122DCFS290D7 GOVERNOR CESSNA402 402B 207590PCE CONT O520 TSIO520E 17040SO ZONE 600 SEIZED E DUFAO OTHER R PARTIAL RPM/PWR LOSS CRCRUISE 1 GL273796C 1464 402B0803 WHILE IN CRUISE FLIGHT, THE RT ENGINE BEGAN TO LOSE RPM. THE PILOT PUSHED THE PROPELLER CONTROL LEVER ALL THE WAY FORWARD TO MAX RPM WITH NO CHANGE. THE PILOT DESCENDED AND MADE AN UNEVENTFUL LANDING. THE RT ENGINE QUIT ON ROLL OUT AND THE RT PROPELLER WENT INTO FEATHER. THE PROPELLER GOVERNOR WAS REMOVED AND APPEARED TO HAVE AN INTERNAL FAILURE. A SERVICABLE GOVERNOR WAS INSTALLED AND OPS CHECKED OK. 1L72 3O3 O A7CE E8CE 20050328000932005032800093CE 2005 3 28 HYI2005F00001 120050103A801199103971 RELAY CESSNA402 402C 207590RCE CONT O520 TSIO520* 17040SO RT STARTER STUCK E HYIAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 NE01812AN 402C0229 AIRCRAFT LOST ELECTRICAL POWER SHORTLY AFTER TAKEOFF. AIRCRAFT LANDED W/O INCIDENT. MECHANIC FOUND RT STRAT RELAY STUCK ON. REMOVED AND REPLACED LT AND RT RELAYS, RT STARTER. AIRCRAFT IS EQUIPPED WITH STAART WARNING LIGHT SYSTEM. MX DETERMINED THAT THE SYSTEM WORKED PROPERLY. PILOT MUST NOT HAVE NOTICED WARNING LIGHT. (K) 1L72 3O3 O A7CE E8CE 20050328001072005032800107NM 2005 3 28 ASMF200503016 120050319A2410 CSD DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE RIGHT OVERHEATED W ASMFA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW23861LF 49826 AIRCRAFT RETURNED, TEMPERATURE IN RT CSD INCREASED HIGHLY AFTER TAKE OFF AND BATTERIES CIRCUIT BREAKER POPPED OUT. RT CSD WAS SERVICED IAW MM 24-10-1, TESTED CORRECT. DURING OVERNIGHT SERVICE CSD FILTERS AND OIL WERE REPLACED IAW MM 24-10-01 AND CSD WAS SERVICED IAW MM 24-10-02. ADDITIONALLY, CIRCUIT BREAKER B1-146 WAS REPLACED AND BATTERIES CHARGER WAS TESTED IAW MM24-30-2, ALL CORRECT. 2L72 4F4 FRT E9NE 20050328001082005032800108CE 2005 3 28 IJA2005F00004 120050203A32305081029525 TORQUE LINK BEECH 90 C90 1152913CE PWA PT6 PT6* 52043EA RT MLG MISMANUFACTURED E IJAAK NONE O OTHER ININSP/MAINT 1 CE07403EM LJ1000 UPON INSTALLATION OF RT GEAR LEG AFTER O/H, IT WAS NOTED THAT THE TIRE EXTENDED 1 INCH FORE THAN THE LEFT GEAR. WHEN LANDING GEAR WAS RETRACTED THE RT TIRE HIT THE FWD PART OF THE WHEEL WELL. BECAUSE THIS AIRCRAFT IS FITTED WITH CLEVELAND WHEELS AND BRAKES THE RT BRAKE CONTACTED THE MAIN FUEL LINE IN THE WHEEL WELL. IT WAS DETERMINED THAT THE LOWER TORQUE LINK WAS EITHER MARKED OR MFG INCORRECTLY. (K) 1L72 3T3 T 3A20 E2NE 20050328001122005032800112SO 2005 3 28 X6PA200500001 120050115A1430 BOLT PIPER PA32 PA32300 7103212SO LYC O540 IO540* 41532EA SEAT BACK BROKEN E X6PAK NONE O OTHER ININSP/MAINT 1 SO33631BW 327340041 PILOT'S SEAT BACK ADJUST BOLTS BROKE, ALLOWING SEAT BACK TO RECLINE. 1L71 3O3 O A3SO 1E4 20050328001152005032800115NE 2005 3 28 ASMF200503014 220050314A720097980611 CONTROL VALVE BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE LT ENGINE FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23806AM6983 4275 26273 726731 AIRCRAFT RETURNED TO PLATFORM AFTER ENGINES STARTED WITH CROSSED FEEDING, EICAS MESSAGES R HYD R SUR PRESS, R ENG REV CONE, L ENG REV CONE, L ENG FIRE LOOP 2, EPR DET LOOP 2 INCHES AND (RT ENGINE EPR OUT OF SERVICE) WERE SHOWN AND PNEUMATIC AUXILIARY POWER UNIT FAIL. THE ENGINES WERE TURNED OFF AND FIM 71-00-00 FIGURE 110, SHEET 1, CODE 352-17 AND 352-15 PROCEDURES WERE PERFORMED AND ENGINES WERE RESTARTED IAW MM 71-00-00, TESTED CORRECT. DURING OVERNIGHT SERVICE, THE SURGE CONTROL VALVE OF AUXILIARY POWER UNIT WAS REPLACED IAW MM 49-53-01, TESTED CORRECT. 2L72 4F4 FRTA2NM E17NE 20050328001162005032800116CE 2005 3 28 AL200501485 120050228A5340680501A BRACKET CESSNA206 U206G 2073356CE CONT O520 IO520F 17032SO FLOW TRANSDUCER BROKEN B HJBRK NONE O OTHER ININSP/MAINT 1 AL055428U450 U20605290 DURING SCHEDULED INSPECTION, FOUND MOUNTING BRACKET FOR FUEL FLOW TRANSDUCER INSTALLED IAW STC NR SE443GL CRACKED ON ALL FLANGES WITH ONE FLANGE BROKEN OFF COMPLETELY. 1H71 3O3 O A4CE E5CE 20050328001192005032800119NM 2005 3 28 SWAA050894 120050323A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29355SW 25250 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727 E + 16, STR 24L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050328001202005032800120NM 2005 3 28 SWAA050895 120050323A55236959227 BUSHING BOEING737 7373H4 1384600NM RT ELEVATOR TAB WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29380SW 26587 DURING SCHEDULED C2 CHECK, RT ELEVATOR TAB FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR NR 1 TAB HINGE BOLT & BUSHING PER MM. 2L72 4F RTA16WE 20050328001212005032800121NM 2005 3 28 SWAA050896 120050323A3350101073 LENS BOEING737 7377H4 1384404NM R2 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29459WN 32497 R2 DOOR EMERGENCY EXIT LIGHT LENS FELL OFF. INSTALLED LENS ASSY PER MM. 2L72 4F RTA16WE 20050328001222005032800122NM 2005 3 28 SWAA050897 120050323A53306545769 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE BELLY SKIN CRACKED AT BS 378, LBL 2. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050328001232005032800123NM 2005 3 28 SWAA050898 120050323A53146545866 KEELBEAM BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND FUSELAGE KEEL BEAM CORRODED AT BS 723, BS 725, BS 529 & BS 500D + 6. REMOVED AND REPLACED KEEL BEAM PER SRM. 2L72 4F RTA16WE 20050328001242005032800124NM 2005 3 28 SWAA050899 120050323A33506574550 LIGHT BOEING737 7373Q8 1384670NM L2 DOOR BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER SRM. 2L72 4F RTA16WE 20050328001282005032800128NM 2005 3 28 UPS05444174 120050313A5347BAC15201566 SEAT TRACK BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE:C M/D - BS 1528-1532 RBL 75 SEAT TRACK LT FLANGE CORROSION. CORROSION BLEND OUT 0.045 X 1 X 1 INCH, EXCEED SRM 53-10-01 FIG 1 LIMIT. SEAT TRACK REPLACED AS PER SRM 51-10-01 PG 9 & INSTALLED AS PER SRM 51-30-02. 2L74 4F A20WE 20050328001292005032800129NM 2005 3 28 UPS05444175 120050313A5347BAC15201566 SEAT TRACK BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, M/D- BS 1920 - 2040 LBL 95 SEAT TRACK & FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.045 X 1 X 3 INCH, EXCEED SRM 53-10-01 FIG 1 LIMIT. SEAT TRACK REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050328001322005032800132SO 2005 3 28 CHQA200500062 120050324A3350RPS1B BATTERY PACK EMB 145 EMB145MP 3260216SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11974SK 145203 THE EMERGENCY EXIT LIGHTS ASSOCIATED WITH THE FORWARD BATTERY ARE INOP. REMOVED AND REPLACED THE FORWARD EMERGENCY BATTERY IAW EMB 135/145 J/C E33-50-04-720-001. OPS CHECK GOOD. 2L72 4F RTT00011AT 20050328001332005032800133 2005 3 28 CHQA200500060 420050322A34177014700626 ADC EMB 135 EMB135LR 3260305SO COCKPT FAILED A CHQAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 GL11834RP 145696 DESCENT FL360 APPROX 2-3,000 FPM, PILOTS NOTICED HIGH WIND NOISE, 5 SEC LATER CAPTAIN'S AIRSPEED INDICATOR ROSE 130 KTS TO 285 KTS. RECEIVED HIGH SPEED WARNING & SPS ADVANCE CAUTION MESSAGE. ACFT LEVELED OFF, AFTER LEVEL OFF BOTH AIRSPEED INDICATORS BEGAN WORKING NORMALLY AS COMPARED TO THE ISIS. DESCENT NORMAL UNTIL 13,000 FT, SMOKE BEGAN TO FILL COCKPIT FROM BEHIND AVIONIC PANELS. EMERGENCY DECLARED. SMOKE CLEARED WITHIN 5 MINUTES AND ACFT LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED ALL AVIONICS PANELS ON GLARESHIELD & WIRES ON WINDSHIELD, NO DEFECTS NOTED. A PITOT STATIC TEST WAS PERFORMED. SYS 2 FOUND TO BE LOOSING 12 FT PER MINUTE. REMOVED & REPLACED NR 2 ADC COMPUTER, OPS CHECK GOOD. 2L72 4F RTT00011AT 20050328001342005032800134SO 2005 3 28 CHQA200500061 120050322A2611FDS765A2 SMOKE DETECTOR EMB 145 EMB145LR 3260212SO CABIN MALFUNCTIONED A CHQAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL11971RP 145426 FLIGHT 3223 PHL-ABE - AFTER DEPARTURE AT APPROXIMATELY 500 FT MSL RECEIVED AN EICAS MESSAGE LAV SMOKE. THE FLIGHT ATTENDANT INVESTIGATED THE LAVATORY AND INFORMED THAT ALL WAS NORMAL IN THE LAVATORY WITH NO INDICATIONS OF FIRE OR SMOKE AT ALL. PHL OPERATIONS WAS NOTIFIED AND THE AIRCRAFT RETURNED TO THE FIELD NON-EMERGENCY LANDING. THE AIRCRAFT WAS VECTORED FOR A VISUAL APPROACH TO RUNWAY 27R AND LANDED UNEVENTFULLY. THE AIRCRAFT WAS FERRIED TO IND WHERE MAINTENANCE REMOVED AND REPLACED THE LAVATORY SMOKE DETECTOR. ENGINE RUNS WERE PERFORMED WITH NO DEFECTS NOTED IAW EMB 145 AMM 26-14-01. 2L72 4T RTT00011AT 20050328001352005032800135NM 2005 3 28 CALA0500082 120050317A3233651781914 ACTUATOR BOEING737 7373T0 1384582NM NLG INOPERATIVE A CALAO OTHER J WARNING INDICATION APAPPROACH 1 SW2712327 23457 CREW REPORTED THAT THE NOSE LANDING GEAR REQUIRED A MANUAL EXTENSION ON APPROACH TO DTW. EXTENSIVE TROUBLESHOOTING WAS PERFORMED. MAINTENANCE FOUND THAT THE NLG LOCK ACTUATOR WAS AT FAULT. THE NLG LOCK ACTUATOR WAS REMOVED AND REPLACED IAW MM 32-33-00. A FLIGHT EVALUATION WAS CONDUCTED AND THE GEAR WAS CYCLED SUCESSFULLY SEVERAL TIMES. 2L72 4F RTA16WE 20050328001372005032800137SO 2005 3 28 C2XA05IA049 120050321A3397375921 CONNECTOR EMB 145 EMB145XR 3260214SO EMERGENCY SIGN LOOSE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2734110 145658 IAH - FLIGHT 2339, DURING POSTFLIGHT INSPECTION THE CREW REPORTED THE EMERGENCY EXIT LIGHT IN THE EXIT ROW TO BE INOPERATIVE. MAINTENANCE RESECURED THE CONNECTOR TO THE EMERGENCY LIGHT, OPERATIONALLY CHECKED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THIS PART IS NOT SERIALIZED, AND TIMES ARE NOT AVAILABLE. 2L72 4F RT 20050328001382005032800138NM 2005 3 28 UPS05444178 120050314A5347BAC15201566 SEAT TRACK BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE:C M/D - BS 2040-2050 LBL 88 SEAT TRACK FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.045 X 1 X 5 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. SEAT TRACK REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050328001392005032800139NM 2005 3 28 UPS05444179 120050314A5347 SEAT TRACK BOEING747 747121 1384871NM FUSLEAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE:C M/D- BS 2040 - 2140 LBL 65 SEAT TRACK FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.050 X 1 X 10 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A. 2L74 4F A20WE 20050328001402005032800140NM 2005 3 28 UPS05444180 120050314A5315BAC1505101047 FLOORBEAM BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C M/D- BS 1500 RBL 83-89 FLOORBEAM UPPER CHORD LWR SURFACE CRACKED CRACK, LENGTH .375 INCH. FLOORBEAM REPAIRED AS PER SRM 51-40-04 FIG 1. 2L74 4F A20WE 20050328001432005032800143NM 2005 3 28 UPS05444183 120050313A5320 FLOOR SUPPORT BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE:C M/D- BS 1580 - 1600 LBL 118 FLOOR SUPPORT CORRODED. CORROSION BLEND OUT 0.035 X 1 X 3 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. FLOOR SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 2. 2L74 4F A20WE 20050328001442005032800144NM 2005 3 28 UPS05444184 120050313A5320HXC108663 FLOOR SUPPORT BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE:C M/D- STA 1500 RBL 117 FLOOR SUPPORT ANGLE CRACKED, LENGTH .75 INCH. FLOOR SUPPORT REPAIRED AS PER SRM 51-40-03 FIG 1. 2L74 4F A20WE 20050328001452005032800145NM 2005 3 28 UPS05444185 120050313A5320 WEB BOEING747 747121 1384871NM M/D CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE:C M/D- STA 1220 LBL 116-118 BELOW FLOOR SUPPORT WEB CRACKED, LENGTH 2 INCHES. FLOOR SUPPORT WEB REPAIRED AS PER SRM 51-40-02 FIG 1. 2L74 4F A20WE 20050328001472005032800147NE 2005 3 28 BA05007 220050322A752052G225 SOLENOID AIRBUS330 A330323 3930335EU PWA 4168 PW4168A NE RT ENGINE FAILED A USAAA UNSCHED LANDING GJ MULTIPLE FAILURE WARNING INDICATION CLCLIMB 1 EA19670UW 315 733501 AFTER TAKEOFF, CREW RECEIVED MULTIPLE ECAM WARNINGS: ENGINE NR 1 BLEED LOW TEMP, APU AFT FUEL PUMP, PACK NR 2 AIR INLET FLAP ACTUATOR FAIL, PACK 2 INLET PRESSURE SENSOR AND NAC COOL VALVE FAILURE. FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE RESET THE SDAC'S AND FWC'S AND PERFORMED AN ENGINE RUN. THE BLEED AND PACK PROBLEMS DID NOT RETURN. HOWEVER, THE PACK INLET PRESSURE SENSOR IS TARGETED FOR TROUBLESHOOTING. THE APU AFT FUEL PUMP PROBLEM COULD NOT BE DUPLICATED. MAINTENANCE REPLACED THE RIGHT TVBC AIR VALVE. SUBSEQUENTLY, THE AFT FUEL PUMP AND THE RIGHT PACK INLET FLAP ACTUATOR WERE REPLACED. 2L72 4F4 FRTA46NM 20050328001492005032800149NM 2005 3 28 UPS05244166 120050310A5347 CARGO TRACK BOEING727 72722C 138400FNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 INSPECTION TYPE:C CARGO TIE DOWN TRACK CRACKED AT BS 1030 RBL 14. REPAIR CARRIED OUT IAW SRM 53-10-5, 51-30-2, 51-20-1 & 53-10-5. 2L73 4F A3WE 20050328001512005032800151NM 2005 3 28 UPS05244168 120050308A5755 PANEL BOEING727 72722C 138400FNM NR 8 SPOILER DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 INSPECTION TYPE:C DELAMINATION ON NR 8 SPOILER AT I/B END. NR 8 SPOILER PANEL REPLACED IAW MM 27-62-01 AND SPOILER LINK REPLACED IAW MM 27-62-91. 2L73 4F A3WE 20050328001532005032800153NM 2005 3 28 UPS05444187 120050313A534065B386001427 STRINGER CLIP BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE:C M/D- BS 1960 LT STR 2L TIE CLIP CRACKED, LENGTH .375 INCH. TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9 & SRM 51-30-02. 2L74 4F A20WE 20050328001542005032800154NM 2005 3 28 UPS05444188 120050313A532265B071793 SHEAR TIE BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE:C M/D- BS 2160 L BETWEEN STR 13L & 14L SHEAR TIE CRACKED, LENGTH .25 INCH. SHEAR TIE REPLACED AS PER SRM 51-10-01 PG 9 & INSTALLED AS PER SRM 51-30-02. 2L74 4F A20WE 20050328001572005032800157NM 2005 3 28 UPS05444192 120050309A55327075T60080IN SKIN BOEING747 747121 1384871NM VERTICAL FIN CHAFED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE:C VERTICAL FIN RT LWR EDGE FWD SECTION FX SKIN CHAFING MARK FOUND WITH ONE LOCATION OF SKIN BLEND OUT EXCEED EO LIMIT. CHAFE BLEND OUT 0.029 INCH. SKIN REPAIRED AS PER SRM 53-30-03 FIG 1A AT STA 2360 TO 2394 STR 3R AREA. 2L74 4F A20WE 20050328001582005032800158NM 2005 3 28 UPS05444193 120050309A55327075T60080IN SKIN BOEING747 747121 1384871NM VERTICAL FIN CHAFED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE:C VERTICAL FIN LT LWR EDGE FWD SECTION FX SKIN CHAFING MARK FOUND WITH 2 LOCATIONS CHAFE BLEND OUT EXCEED EO LIMIT. CHAFE BLEND OUT DEPTH 0.025 & 0.022 INCH. SKIN REPAIRED AT BS 2310-2360 STR 3L AREA AS PER SRM 53-30-03 FIG 1 & BS 2360 - 2380 STR 3L AREA AS PER SRM 53-30-03 FIG 1A. 2L74 4F A20WE 20050328001592005032800159NM 2005 3 28 UPS05544194 120050324A3510 ELBOW BOEING757 75724APF 1384969NM COCKPIT OXYGEN LEAKING A IPXAK NONE O OTHER ININSP/MAINT 1 SO01403UP 23725 INSPECTION TYPE:N/A PER TECH ALERT H29535 FOUND CAPT'S SUPPLY HOSE ELBOW FITTING SLOW LEAK (ELBOW FITTING ATTACHED TO STOWAGE BOX) LIMNE CAPPED. REPLACED CAPT'S AND F/O`S ELBOW FITTING AND AS A PRECAUTION, R2 CAPTS AND F/O`S MASK AND MASK STOWAGE BOXES PER MM 35-11-51-4, LEAKS NOTED. 2L72 4F RTA2NM 20050328001602005032800160NM 2005 3 28 UPS05544196 120050222A5347 CARGO TRACK BOEING757 75724APF 1384969NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01439UP 25470 CORROSION AROUND ALL RT CARGO TIE DOWNS IN FWD CARGO BAY BS 620 820 RBL 25. BLENDED CORROSION IN 11 AREAS TO BE OUT OF LIMITS PER SRM 53-00-53-1 FIG 101. BLENDED AREAS BS 620-BS 820 RBL 25. 2L72 4F RTA2NM 20050328001622005032800162SO 2005 3 28 RAIA00503011 120050321A3097 CONNECTOR EMB 145 EMB145LR 3260212SO PITOT HEAT LOOSE A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03812HK 145373 ERI - AT 10 KTS ON TAKEOFF ROLL, PITOT 3 INOP MESSAGE ILLUMINATED. MAINTENANCE CLEANED AND SECURED PITOT 3 HEAT CONNECTOR AND OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050328001632005032800163 2005 3 28 BB05021 420050322A2565 LIGHT BOEING767 7672B7 1385107NM ESCAPE SLIDE INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19651US PA0199 24764 BFM DURING ANNUAL SLIDE INFLATION CHECK, THE EMERGENCY LIGHTS DID NOT ILLUMINATE. MAINTENANCE REPLACED THE SLIDE. FURTHER INFORMATION PENDING. 2L72 4F RTA1NM 20050328001652005032800165NE 2005 3 28 DXTA200500640 220050321A7200 ENGINE CESSNA560 560XL 2076702CE PWA 545 PW545A NE RIGHT MALFUNCTIONED E DXTAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 GL07670QS 5605170 PCEDB0371 AFTER APPLYING TAKEOFF POWER, RIGHT EEC REVERTED TO MANUAL MODE, ABORTED TAKEOFF. ITEM IS UNDER INVESTIGATION. 2L72 4F4 FRTA22CE E00059EN 20050328001672005032800167SO 2005 3 28 RAIA00503010 120050318A213122250N030301 CONTROLLER EMB 145 EMB145LR 3260212SO CABIN PRESSURE MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03817HK8845 39 145058 STL - AUTO PRESSURIZATION FAULT INDICATION. MAINTENANCE REMOVED AND REPLACED AUTO PRESSURE CONTROLLER. 2L72 4T RTT00011AT 20050328001682005032800168SO 2005 3 28 C2XA05SD017 120050323A335066903 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714558 145598 SDF - FWD FRONT EMERGENCY LIGHT STRIP INOP. REMOVED AND REPLACED EMERGENCY LIGHT STRIP, OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE. 2L72 4T RTT00011AT 20050328001692005032800169SO 2005 3 28 153303132005 120050313A32501159SCH4023 SHUTOFF VALVE GULSTMG1159 GIV 3980115SO NLG STEERING FAILED E N93AO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO13467QS114 1533 NWS FAILED PRIOR TO TAXI. 2L72 4F RTA12EA 20050328001712005032800171NM 2005 3 28 AALA20050212 120050320A3350 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21785AN 30005 DFW - FIRST CLASS SEAT EMERGENCY ESCAPE PATH LIGHT AT RIGHT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR FIRST CLASS SEAT EMERGENCY ESCAPE PATH LIGHT AT RT NR 1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20050328001732005032800173 2005 3 28 AALA20050213 420050322A2565 GIRT BAR DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21427AA 49339 DFW - THE GIRT BAR AT AFT GALLEY DOOR BECAME DISLODGED AND PIN CAME PARTIALLY OUT PREVENTING RESETTING SLIDE LANYARD. REPLACED SLIDE ASSEMBLY FOR AFT GALLEY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050328001742005032800174NM 2005 3 28 AALA20050215 120050323A3350 LIGHT BOEING767 767223 1385123NM CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21323AA 22324 LAX - LEFT HAND FORWARD GALLEY EMERGENCY ESCAPE PATH LIGHTING DIRECTIONAL ARROW SIGN INOPERATIVE. REPAIRED BROKEN WIRE AT SIGN ASSEMBLY FOR LEFT HAND FORWARD GALLEY EMERGENCY ESCAPE PATH LIGHTING DIRECTIONAL ARROW SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050328001762005032800176NM 2005 3 28 AALA20050217 120050228A5313 LONGERON BOEING767 767323 1385205NM FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21357AA 24038 AFW - RIGHT HAND UPPER LONGERON WEB AT STRINGER 12 RIGHT JUST FORWARD OF STATION 1809 CRACKED. CUT OUT DAMAGED WEB AT APPROXIMATELY STATION 1798 AND FABRICATED A REPAIR WEB FROM .032 7075T6 CLAD. DOUBLER FROM .040 7075T6 CLAD AND FILLER FROM 0.080 7075T6 AND MACHINE SPLICE. ALODINE AND PRIME ALL ALUMINUM SURFACES PER 767 SRM. INSTALLED WEB SPLICES WITH BMS595 SEALANT AND INSTALLED BACR15FTC7K6 AT ALL RIVET LOCATIONS AND BACB30VT OR BACB30NX AT ALL HIL OK LOCATIONS IN TRANSITION FIT. 2L72 4F RTA1NM 20050328001772005032800177NM 2005 3 28 AALA20050219 120050311A1430 FASTENER BOEING767 767323 1385205NM WING FUEL TANK CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21357AA 24038 AFW - SEVEN LOCK FASTENER COLLARS CRACKED INSIDE FUEL TANKS AT WING STATION 261.2 LEFT HAND 394.2 LEFT HAND, 308.1 RT, 798.2 RIGHT HAND. REPLACED SEVEN EACH LOCK FASTENER COLLARS. NO LOOSE OR LEAKING LOCK FASTENERS AFTER REPLACEMENT OF COLLARS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050328001802005032800180NM 2005 3 28 AALA20050214 120050323A3397 WIRE BOEING757 757223 1384957NM EMERGENCY LIGHT BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21601AN 27052 DFW - AFT LOWER RIGHT HAND LAVATORY EMERGENCY FLOOD LIGHT WITH ARROW IS INOPERATIVE. REPAIRED BREAKS IN FEED WIRES WITH ENVIRONMENTAL SPLICES FOR AFT LOWER RIGHT HAND LAVATORY FLOOD LIGHT WITH ARROWS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050328001842005032800184EU 2005 3 28 SA05031 120050320A5610NP1653115 WINDSHIELD AIRBUSA319 A319112 3930323EU COCKPIT CRACKED A USAAH DEACTIVATE SYST/CIRCUITS A FLAME/FIRE CRCRUISE 1 EA19744US13830 1287 PHL FLT 1174 EN ROUTE PVD TO PHL. DURING THE FLIGHT, THE CAPTAIN'S WINDSHIELD BEGAN TO ARC, AND THEN CRACK. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE CAPTAIN'S WINDSHIELD. OK FOR SERVICE. 2L72 4F RTA28NM 20050328001862005032800186EU 2005 3 28 SA05032 120050321A3230 PIN AIRBUSA319 A319112 3930323EU NLG INSTALLED A USAAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 EA19719US 1084 BOS FLT 2035 EN ROUTE BOS TO DCA. AFTER TAKEOFF, THE NOSE GEAR WOULD NOT RETRACT. FLIGHT RETURNED TO FIELD IN BOS AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED A NOSE GEAR PIN. OK FOR SERVICE. 2L72 4F RTA28NM 20050328001872005032800187NE 2005 3 28 IXXA0500025O 220050322A72009026M70G01 ENGINE DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C1 13802NE NR 3 FLAMED OUT A IXXAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SW11605AL385354668 46106 692502 ON CLIMB NR 3 ENG FLAMED OUT 32,000 FT, NO AUDIBLE/VISUAL ENG STALL OR VIBRATION. WEATHER VMC THROUGHOUT CLIMB. ENG FLAMED OUT N1 30%, N2 15% & OIL PRESSURE 3 PSI. GEN WENT OFF LINE, IGNITION NOT ON. FUEL CONFIG NORMAL, FUEL TEMP TANK -5C & FUEL PRESSURE AFTER FLAMEOUT 7 PSI ENG MOTORING 18% N2. ATTEMPTED RESTART AFTER RUNNING ABNORMAL ENGINE CHECKLIST. RECYCLED FIRE HANDLE, ATTEMPTED RESTART DESCENDING 21,000 FT, STARTER RESET & ALL 4 CROSSFEEDS IN POSITION. ENG RESTARTED 17,000, PARAMETERS NORMAL. LANDED WITH ALL 4 MOTORS RUNNING AND NO FURTHER PROBLEMS THROUGHOUT FLIGHT. MX PERFORMED CFM MM 71-00-00 FAULT 51, T/S TREE, PERFORMED POWER RUN. ENGINE INDICATIONS NORMAL, NO DEFECTS NOTED. 2L74 4F4 FRT4A25 E2GL 20050328001892005032800189SO 2005 3 28 139203172005 120050317A78301159PM4156143 LINK GULSTM GULSTMG1159 GIV 3980115SO THRUST REVERSER DAMAGED E N93AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO13492QS4814 0399 1392 RIGHT THRUST REVERSER UNLOCK LIGHT ILLUMINATED CLIMBING THRU 17,000 FEET. 2L72 4F RTA12EA 20050328001912005032800191SO 2005 3 28 SWIA200514755 120050322A2120 SMOKE EMB 120 EMB120ER 3260203SO CABIN DETECTED A SWIAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DEDESCENT 1 NM07236SW 120312 F/A REPORTED LIGHT SMOKE AND BURNING SMELL DURING DESCENT IN BOTH AUTO & LOW. RAN RIGHT AND LEFT PACKS ON GROUND FROM APU BLEED. NO SMOKE NOTED AT THIS TIME. 2L72 4T RTA31SO 20050328001922005032800192 2005 3 28 SWIA200514756 420050323A2216C818022 SERVO EMB 120 EMB120ER 3260203SO STICK SHAKER INOPERATIVE A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07288SW1127011270 120316 WHEN CAPTAIN'S STALL WARNING SYSTEM IS TESTED THE SHAKER DOES NOT ACTIVATE. REPLACED NR 1 STICK SHAKER SERVO. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050324001062005032400106EU 2005 3 24 SSHA099270 120050210A6320704A34412009 HOSE AEROSPAS355 AS355* EU OIL COOLER FAILED E SSHAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP133607P 1249 PILOT MADE A PRECAUTIONARY LANDING DUE TO ILLUMINATION OF THE MGB PRESSURE LIGHT, INSPECTION REVEALED THE MGB OIL COOLER LINE HAD BURST AT THE JOINT BETWEEN THE HOSE AND THE METAL CRIMPEND END. THE HOSE WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1G72 3U H11EU 20050324001172005032400117EA 2005 3 24 QXEA200500265 120050212A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - FUSELAGE EXTERIOR, CROWN STATION 773 AND STRINGER 2R HAS NICK ON FUSELAGE SKIN. REPAIRED IAW CRJ700 SRM 51-26-00-01-001-A01, 51-12-00-001-001-A01 AND SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050324001342005032400134NM 2005 3 24 TSAA0529012 120050307A2910 LINE BOEING737 7372T4 1384492NM HYD SYSTEM LEAKING A TSAAO OTHER KJ FLUID LOSS WARNING INDICATION LDLANDING 1 WP13808AL 23445 LOST A SYSTEM HYDRAULICS ON SHORT FINAL. MAINTENANCE MET THE AIRCRAFT ON THE RUNWAY. MAINTENANCE REPLACED THE NOSE GEAR DOWN ACTUATOR LINE PER AMM 32-3-11. SERVICED HYDRAULIC SYSTEM TO FULL. LEAK CHECK OKAY. REPLACED THE NR 1 AND NR 2 CASE DRAIN FILTERS, LEAK CHECK OK PER AMM 29-11-91. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A16WE 20050324001352005032400135NM 2005 3 24 F3LA200500007 120050308A5320 SILL BOEING737 7373L9 1384470NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03313FL 4372 26442 DURING C-4 CHECK INSPECTION, REPORTED R2 DOOR MOP SILL CORRODED. REPLACED R2 DOOR MOP SILL PER SRM 51-40-02. 2L72 4F RTA16WE 20050324001432005032400143SO 2005 3 24 C2XA05SH010 120050215A531114527703001 FRAME EMB 145 EMB145ER 3260211SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714940 145033 SHV - DURING C-CHECK, SEVERAL GOUGES FOUND ON LEFT HAND EMERGENCY EXIT DOOR LOWER INTERNAL FRAME. 2L72 4F RTT00011AT 20050324001552005032400155EA 2005 3 24 QXEA200500190 120050124A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - RIGHT INBOARD SEAT RAIL, AT STATION X418, HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW CRJ700 SRM 51-21-00-001-001-A01, REO 670-53-00-060, REV B. AND HORIZON AIR EA R-53-266. 2L72 4F RTA21EA 20050324001652005032400165NE 2005 3 24 ASMF200503010 220050313A732176960615 FUEL CONTROL DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE RIGHT FAILED W ASMFO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SW23753RA9120 2761 49587 718196 AFTER LANDING RIGHT ENGINE FREQUENCY WAS BELOW 390 AND BUS WAS OFF, THE RIGHT ENGINE WAS STARTED AND PARAMETERS WERE VERIFIED; N2 STABILIZED IN 40 PERCENT AND BUSS WAS OFF. N2 WAS ADJUSTED TO 56 PERCENT BUT RIGHT ENGINE DID NOT STABILIZED. AIRCRAFT WAS SENT TO THE HANGAR AND THE FUEL CONTROL UNIT AND RELAY R2-8 WERE REPLACED IAW MM 73-20-01 AND WDM 73-23-01 RESPECTIVELY. ENGINES TRIM AND OPERATIONAL CHECK WERE PERFORMED IAW MM 71-00-00 AND MPCM 71-00-00, ALL CORRECT. 2L72 4F4 FRTA6WE E9NE 20050324001692005032400169EA 2005 3 24 SWIA200514640 120050223A27604916405 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07924SW8400 8400 7681 DURING TAXI OUT, GOT SPOILERONS FAULT MESSAGE. REPLACED NR 2 SECU IAW MM 27-61-05, OPERATIONAL CHECKS GOOD. 2L72 4F RTA21EA 20050324001702005032400170EA 2005 3 24 SWIA200514641 120050224A2760C13045BA03 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA SPOILER MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CRCRUISE 1 NM07742SK 10197 "RUD LIMIT FAULT" STATUS MSG CAME ON DURING FLIGHT. REMOVED AND REPLACED SSCU NR 1 AND PERFORMED OPERATIONAL CHECK IN IAW AMM 27-61-05. 2L72 4F RTA21EA 20050324001712005032400171EA 2005 3 24 SWIA200514642 120050224A2750860D10018 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAP MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 NM07919SW6589 6589 7657 SELECTED FLAPS TO 8 DEGREES, THEN FLAPS FAIL CAUTION MESSAGE. REMOVED AND REPLACED FECU IAW CRJ 200 MM CHAPTER 27-51-05, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050325000062005032500006NM 2005 3 25 QXEA200500417 120050128A5730 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - LEFTHAND WING LEFTHAND PANEL 523AT BOTTOM SURFACE OF PANEL PITTING AND FRETTING CORROSION AROUND PANEL ATTACH HOLES. REPAIRED IAW RD 8/4-57-421. 2H72 4T RTA13NM 20050325000092005032500009NM 2005 3 25 CALA0500083 120050322A5313BAC1498156 STRINGER BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2759302 23353 INSPECTION FOUND SKIN BULGING AT STA 360 MINUS 6 INCHES TO 360 WITH CORROSION ON STRINGER 25L. REPAIRED STRINGER IAW ECRA 5311-01219. 2L72 4F RTA16WE 20050325000222005032500022EU 2005 3 25 05FDEA00587 120050317A5730A5724279520100 PANEL AIRBUS310 A310222 3930315EU RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 RIGHT WING T/E PANEL LANDING FOR ACCESS PANEL 675CB HAS 1.0 INCH CRACK. REMOVED AND REPLACED LANDING PLATE IAW SRM 51-72-10. 2L72 4F RTA35EU 20050325000592005032500059WP 2005 3 25 DHL2005805504 120050220A5531 FRAME DOUG DC8 DC873F 302199FWP VERTICAL STAB CRACKED A DHLAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SO01805DH80855 46125 VERTICAL STAB L/E FORMER CRACKED 1.000, STA ZFS 114.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE AND FABRICATED ANGLE DOUBLER (AL7075-T6 0.032) IAW SRM 55-2-0 PG 7-8 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED ANGLE DOUBLER IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. TORQUED IAW SRM 51-3-1 PG 2A TABLE II. 2L74 4F RT4A25 20050325000602005032500060WP 2005 3 25 DHL2005805505 120050223A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 LEFT OUTER WING INBOARD L/E UPPER FORMER CRACKED 0.500, XFS 678.750. REMOVED FASTENERS IAW SRM 51-1-20D PG 21. FABRICATED (2EA) ANGLE DOUBLERS (AL7075-T6 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLERS IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLERS WITH FASTENERS IAW SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. TORQUED IAW SRM 51-3-1 PG 2A. 2L74 4F RT4A25 20050325000642005032500064NM 2005 3 25 QXEA200500426 120050127A5730 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - LEFTHAND WING LEFTHAND FUEL TANK AT 521BT HAS CORROSION AROUND PANEL REBATE TOP SURFACE. REPAIRED IAW Q400 SRM 57-10-35-940-001. 2H72 4T RTA13NM 20050325000792005032500079WP 2005 3 25 05FDEA00610 120050321A5310 STRUCTURE DOUG DC10 DC1010 3022110WP FUSELAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25571FE 47830 DURING INSPECTION FOUND AT STA 1741 STRUCTURE X=-17; X= 17 WITH CORROSION AND RETAINER X= 17 WITH CORROSION. REMOVED CORROSION FROM AFFECTED AREA PER SRM 51-21-01. PERFORMED CHECK LIMITS; THE MATERIAL REMOVED IS WITHIN LIMITS PER SRM 53-00-01. PROTECTED AREA PER SRM 51-21-01. 2L73 4F A22WE 20050325000872005032500087NM 2005 3 25 QXEA200500429 120050127A5730 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 600 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - RIGHT WING FUEL PANEL AT 621AT LOWER SURFACE HAS AREA OF CORROSION, AROUND SCREW HOLES. REPAIRED IAW Q400 SRM SUB TASK 57-10-35-940-001. 2H72 4T RTA13NM 20050325000892005032500089EA 2005 3 25 SWIA200514733 120050319A3397 WIRE CNDAIRCL600 CL6002C10 1390015EA EMERGENCY SIGN DAMAGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07744SK 10200 EMERGENCY LIGHT EXIT SIGN ON AFT OF BULKHEAD SEPARATING 1ST CLASS & COACH (RT SIDE) IS INOPERATIVE. REPAIRED WIRES ON EMERGENCY LGIHT EXIT SIGN. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050325000952005032500095NM 2005 3 25 SWAA050873 120050321A56105893543129 WINDOW BOEING737 7373Q8 1384670NM COCKPIT ARCED A SWAAO OTHER O OTHER NRNOT REPORTED 1 SW29688SW 23254 ARCING OBSERVED ON L1 COCKPIT WINDOW IN TOP RT CORNER. WINDOW HEAT SWITCHED OFF. OUTER PANE L1 COCKPIT WINDOW CRACKED. REMOVED AND REPLACED L1 COCKPIT WINDOW AND HEAT CONTROLLER. 2L72 4F RTA16WE 20050325000972005032500097NM 2005 3 25 05FDEA00516 120050315A5322 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 CORROSION ON SHEAR TIE BS 950E, STR 26L. *S/D* REPAIRED PER SRM 53-10-4. 2L73 4F RTA3WE 20050325001012005032500101EA 2005 3 25 SWIA200514735 120050317A2740 SWITCH CNDAIRCL600 CL6002B19 1900309EA PITCH TRIM INOPERATIVE A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07907SW 7511 F/O TRIM MOSTLY INOPERATIVE. REPLACED F/O'S PITCH TRIM SWITCH IAW CRJ MM 27-41-05. OPERATIONAL CHECKS GOOD. 2L72 4F RTA21EA 20050325001022005032500102EA 2005 3 25 SWIA200514736 120050314A2711 TRIM SYSTEM CNDAIRCL600 CL6002C10 1390015EA AILERONS MALFUNCTIONED A SWIAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 NM07732SK 10194 AILERON TRIM RANAWAY DURING TAKEOFF ROLL. TAKEOFF CONFIG AILERON TRIM MOVES LWD. CLEANED TRIM SWITCHES & PANEL CONNECTOR. OHM'ED AND MEGGED WIRING BETWEEN AILERON TRIM ACTUATOR AND JB10. WIRING ALL OHM'ED OUT NORMAL. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050325001052005032500105 2005 3 25 SWAA050865 420050321A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29795SW 30606 R2 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. SLIDE DID NOT DEPLOY. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20050325001072005032500107 2005 3 25 SWAA050866 420050321A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29375SW 26583 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050325001082005032500108NM 2005 3 25 SWAA050867 120050321A3350101073 LENS BOEING737 7375H4 138449DNM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29512SW 24189 LT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20050325001092005032500109NM 2005 3 25 DHL2005781534 120050214A5330 SKIN BOEING727 727227 1384078NM FUSELAGE GOUGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A C-CHECK, 4 HAND FUSELAGE 4 E AREA IS GOUGED APPROX STA 720E (MARKED) STR 19L. REMOVED PREVIOUS AT LT/HAND FUSELAGE L/E AREA STA 720E STR 19L IAW B727 SRM 51-30-2. FABRICATED DOUBLER REPAIR MAT USED 2024T3 .071 PO 9001978 DIM 17 X 12 INCH AND 1 EA FILLER MAT USED 2024T3 .063 PO 9001684 DIM 10 X 17 INCH IAW B727 SRM 53-30-2 FIG 2 AND 53-30-3 FIG 14. ALODINED AND PRIMED AREA AND PARTS IAW 13 727 SRM 51-10-2. INSTALLED REPAIR IAW B727 SRM 53-30-3 FIG 14. THIS REPAIR IS CATEGORY-B. 2L73 4F A3WE 20050325001162005032500116NM 2005 3 25 05FDEA00511 120050314A5347AEA7579501 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25592FE 48550 MAIN DECK CARGO - SEAT TRACK CORRODED AT STA 1351 RT 76 INCHES. SEAT TRACK REPAIRED AS PER SRM 53-70-00 VOL 1 FIG 1, AT STA 1269 TO 1391. 2L73 4F RTA22WE 20050325001272005032500127NM 2005 3 25 SWAA050782 120050314A57546546486 WEDGE BOEING737 7373H4 1384600NM RT WING SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29607SW 27927 DURING SCHEDULED D-CHECK, FOUND RT WING, NR 4 L/E SLAT, INBOARD END T/E WEDGE DELAMINATED. REPAIRED WEDGE PER SRM. 2L72 4F RTA16WE 20050325001302005032500130NM 2005 3 25 SWAA050785 120050314A3350612825 BATTERY PACK BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29741SA 29277 DURING SCHEDULED MV2 CHECK, FOUND 2 EA EMERGENCY EXIT LIGHTS INOP IN CABIN & 1 EA EXTERIOR LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050328000092005032800009EA 2005 3 28 COMA0560201 120050323A301060059122223 SENSOR CNDAIRCL600 CL6002B19 1900309EA WING OVERHEAT MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01435CA 7473 FLIGHT 5060 RECEIVED A WING OVERHEAT WARNING DURING CRUISE FLIGHT. CREW DECLARED AN EMERGENCY AND RETURNED TO CVG. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED WING OVERHEAT SENSOR. 2L72 4F RTA21EA 20050328000292005032800029CE 2005 3 28 02021105 120050311A324006111800 BRAKE CESSNA208 208B 2073701CE PWA PT6 PT6A114 52043NE RT MLG UNSERVICEABLE E HSYAD RETURN TO BLOCK C F.O.D. TXTAXI/GRND HDL 1 NM05963FE 208B0080 WHILE TAXIING OUT TO PERFORM A FLIGHT TEST REQUIRED FOR UNRELATED MAINTENANCE (STALL WARNING), THE PILOT EXPERIENCED A LOSS OF ABILITY TO STEER THE AIRCRAFT TO THE RT. UPON INSPECTION OF AIRCRAFT BY MAINTENANCE, THE RT MAIN BRAKE CALIPER WAS FOUND TO BE HANGING OFF THE AIRCRAFT BY THE BRAKE LINE. MAINTENANCE FOUND THAT THE GUIDE PINS HAD BEEN SHEARED OFF. CAUSE UNDER INVESTIGATION. REMOVED ALL AFFECTED PARTS AND REPLACED WITH SERVICEABLE COMPONENTS. HIDDEN DAMAGE INSPECTION CARRIED OUT WITH NO FURTHER DAMAGE FOUND. ALL SYSTEMS AFFECTED, OPS CHECKED SATISFACTORILY. 1H71 3T3 T A37CE E4EA 20050328000592005032800059NM 2005 3 28 TZR2005F00000 120050104A3210400054001 TRUNNION PIPER PA60 PA60600 7106001NM LYC O540 IO540K1J5 41532EA HARTZLHCC3Y HCC3YR2 NE LT MLG CRACKED E TZRAK NONE O OTHER ININSP/MAINT 1 SW05604TE7533 600320118 LT MLG, TRUNION CRACKED AT TOP WHERE TUBE GOES INTO MOUNTING BOSS. (SW05200506154) (K) 1M72 3O3 ORTA17WE 1E4 5 CP25EA 20050328001412005032800141NM 2005 3 28 UPS05444181 120050313A5315BAC1505101045 FLOORBEAM BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE:C M/D- BS 1580 RBL 83-96 FLOORBEAM UPPER CHORD CORROSION. CORROSION BLEND OUT 0.060 X 2 X 2 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. M/D BS 1580 RBL 83-96 FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 1. 2L74 4F A20WE 20050328001502005032800150NM 2005 3 28 UPS05244167 120050309A5230 SKIN BOEING727 72722C 138400FNM FWD CARGO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 INSPECTION TYPE: C FWD CARGO DOOR CRACKED AT AFT UPPER FRAME BETWEEN LWR ATTACH BOLT FOR BALANCE MECHANISM. REPAIR CARRIED OUT IAW AAAE EO 2005-021-002. 2L73 4F A3WE 20050328001522005032800152NM 2005 3 28 UPS05244169 120050311A5740 FITTING BOEING727 72722C 138400FNM RT TRUNNION CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 INSPECTION TYPE:C EXTENSIVE CRACKING SROUND BOTH I/B B & C HOLES FOR A LARGE AREA OF THE RT TRUNNION FITTING ON RT REAR SPAR. REMOVED MLG FWD TRUNNION HOUSING ATTACHMENT FITTING ON REAR SPAR IAW SRM 51-30-2. REPAIR CARRIED OUT IAW SRM 51-30-2, DRAWING 65-19297 & AAA E EO 2005-021-001. 2L73 4F A3WE 20050328001722005032800172NM 2005 3 28 AALA20050211 120050320A3350 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21785AN 30005 DFW - EMERGENCY ESCAPE PATH LIGHT AT COACH R3 DOOR FORWARD AND AFT SEAL INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY ESCAPE PATH LIGHT AT COACH R3 DOOR FORWARD AND AFT SEAL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20050328001752005032800175NM 2005 3 28 AALA20050216 120050323A3350 REFLECTOR BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21385AM 27059 DFW - EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED LIGHT REFLECTOR ASSEMBLY FOR EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050328001782005032800178NM 2005 3 28 HNAA0500028 120050323A7797 WIRE DHAV DHC8 DHC8102 2809003NM SPEED SENSE DAMAGED A HNAAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 EA07907HA 011 RT AC BUSS LIGHT ILLUMINATED IN FLT WITH ASSOCIATED RT TRU, RIGHT ELEVATOR HEAT AND RIGHT STALL WARNING. REMOVED AND REPLACED CONNECTOR 2421-P6 AT A/C CONTACTOR BOX, REPLACED WIRES 2022B22, 2023B22, 2021B22, 2024B22, 10024G22, 10023G22, 10022G22, 10021M22, 20015G22, 20045C22, 20044C22, 20043C22, 2442-2009D2, 20011B22, 20010B22 NO FIX, PROBLEM RETURNED ON 25 MARCH 2005. R & R RT AC GENERATOR AND GCU NO FIX PROBLEM RETURNED 02 APRIL 2005. REPAIRED SPEED SENSE WIRES NEAR RT AC CONTACTOR BOX. OPS CHECK GOOD 2H72 4T RTA13NM 20050328001792005032800179NM 2005 3 28 BB05020 120050321A3397 WIRE BOEING767 767201 1385125NM EMERGENCY LIGHT DETACHED A USAAK NONE O OTHER ININSP/MAINT 1 EA19648US 23900 PHL FOUND A BROKEN WIRE FOR THE EMERGENCY FLOOR TRACK LIGHTING NEAR SEAT ROWS 22 AND 23. MAINTENANCE RE-ATTACHED THE WIRE TO THE HOUSING. 2L72 4F RTA1NM 20050328001852005032800185NM 2005 3 28 P5CA0501331 120050320A783019600263 DOOR BOEING747 747283B 1384867NM PWA JT9 JT9D70A 52054NE THRUST REVERSER MISSING A P5CAK NONE O OTHER ININSP/MAINT 1 EA15921FT 21575 688856 ON POST FLIGHT NR 3 ENGINE REVERSER PANEL MISSING. ACCOMPLISHED INTERIM REPAIR PER SRM 51-00-04 AND SRM 51-40-16, ALSO GMM 3-17-1. TRANSFERRED TO C/O ITEM 921-179. 2L74 4F4 F A20WE E3NE 20050328001942005032800194EA 2005 3 28 SWIA200514758 120050322A27508004301 DETECTOR CNDAIRCL600 CL6002B19 1900309EA UNIT-SKEW MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TOTAKEOFF 1 NM07463SW2891 2891 7820 AFTER T/O, THE GEAR AND FLAP INDICATORS REMAINED ILLUMINATED ON ED1 FOR APPROX 20 MINUTES. GEAR AND FLAPS INDICATED NORMAL (UP & 0 DEGREES). REPLACED SKEW DETECTOR UNIT IAW MM 27-51-15, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050328001962005032800196NM 2005 3 28 DHL2005745006 120050325A2120 SMOKE BOEING727 727224 1384076NM CABIN DETECTED A DHLAGB O2 MASK DEPLOYED EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO01745DH 20665 SMOKE IN COCKPIT BEGAN SHORTLY AFTER INITIAL DESCENT INTO SLC. COMPLETED SMOKE SOURCE I.D. EMERGENCY CHKLST & AIR CON SYS SMOKE EMERGENCY CHKLST. SMOKE BEGAN TO DISSIPATE AFTER ENG 1 & 2 BLEEDS REVERSED. RAN NR 1, 2 & 3 ENGINES WITH BLEEDS & PACKS ON, NO EVIDENCE OF SMOKE OR FIRE. RAN ENGINES AT ALL PWR SETTINGS AND MIX VALVES AT ALL SETTINGS TO DUPLICATESMOKE COND, NO SMOKE NOTED EXCEPT FOR SLIGHT CARBON ODOR. INSPECTED AIR COND BAY AND BOTH PACKS AND FOUND LH WATER SEPERATOR COALESCER BAG FILTER CONTAMINATED WITH OIL AND CARBON RESIDUE. R AND R LH WATER SEPERATOR FILTER AND RAN PACKS WITH ENG AND APU BLEED AIR, SYST CKS GD. MX 2L73 4F A3WE 20050328001982005032800198NM 2005 3 28 SWAA050880 120050322A3350BR2013 LIGHT BOEING737 7377H4 1384404NM FWD CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29402WN 29814 FWD CABIN EEPLS COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20050328001992005032800199SO 2005 3 28 SWIA200514770 120050207A5347 SEAT TRACK EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0758733 120197 RIGHT SEAT RAIL CORRODED IN SEVERAL SPOTS AROUND SCREW HEADS FROM FRAME 13A- FR.32 OUTBOARD SIDEWALL. ITEM FOUND AT C-CHECK INSPECTION. SEAT TRACK REPLACED IAW EMB 120 SRM 51-25-00, 51-22-00, 51-40-02. 2L72 4T RTA31SO 20050328002002005032800200NM 2005 3 28 SWAA050881 120050322A21216454051 FAN BOEING737 7373H4 1384600NM COCKPIT FAULTY A SWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW29602SW 27953 ELECTRICAL ODOR IN CABIN WHEN RECIRCULATING FAN ON. ODOR DISPENSES WHEN TURNED OFF. REMOVED AND REPLACED FAN PER MM. 2L72 4F RTA16WE 20050328002022005032800202NM 2005 3 28 SWAA050883 120050322A53116546533 FRAME BOEING737 7373H4 1384600NM FWD CARGO CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29395SW 27689 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 492, STR 24R. REPAIRED FRAME PER PAE ER. 2L72 4F RTA16WE 20050328002032005032800203NM 2005 3 28 SWAA050884 120050322A53116546539 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29607SW 27927 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, LBL 64, WL 202. REPAIRED FRAME PER PAE ER. 2L72 4F RTA16WE 20050328002052005032800205NM 2005 3 28 SWAA050886 120050322A55116573782 SPAR BOEING737 7373Q8 1384670NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND LT HORIZONTAL STAB, AFT SPAR, UPPER CHORD CORRODED AT STA 276.70. REPAIRED LT HORIZONTAL STAB PER SRM & SB. 2L72 4F RTA16WE 20050328002102005032800210NM 2005 3 28 SWAA050891 120050322A53306545765 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29691WN 23781 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D + 10, STR 14R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050328002152005032800215NM 2005 3 28 SWAA050874 120050322A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29355SW 25250 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050328002162005032800216NM 2005 3 28 SWAA050875 120050322A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29355SW 25250 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E + 6, STR 25R. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050328002172005032800217NM 2005 3 28 SWAA050876 120050322A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29355SW 25250 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 948.5, R2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050328002182005032800218NM 2005 3 28 SWAA050877 120050322A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29355SW 25250 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 948.5, L2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050328002192005032800219NM 2005 3 28 SWAA050878 120050322A57536546435 SKIN BOEING737 7373H4 1384600NM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29355SW 25250 DURING SCHEDULED C1 CHECK, FOUND LT WING INBOARD AFT FLAP T/E DELAMINATED. REPAIRED FLAP PER SRM. 2L72 4F RTA16WE 20050328002202005032800220NM 2005 3 28 SWAA050879 120050322A5310907822 FITTING BOEING737 7373H4 1384600NM L1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29625SW 27701 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR LOWER FUSELAGE HINGE BOX FITTING CRACKED. REMOVED AND REPLACED HINGE BOX FITTING PER SRM & SAM 326. 2L72 4F RTA16WE 20050328002212005032800221SO 2005 3 28 SWIA200514761 120050207A5347 SEAT TRACK EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0758733 120197 RIGHT OUTBOARD AFT SEAT TRACK CORRODED AT FR38 TO FR34 (SIDEWALL). ITEM FOUND AT C-CHECK INSPECTION. SEAT TRACK REPLACED IAW EMB 120 SRM 51-25-00, 51-22-00, 51-40-02. 2L72 4T RTA31SO 20050329000022005032900002WP 2005 3 29 ASAA0580132 120050227A532199365451 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 HV-CHECK, CABIN FLOOR PANEL HAS CORRODED FASTENERS. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050329000032005032900003WP 2005 3 29 ASAA0580133 120050227A5230 SKIN DOUG DC9 DC983 3022083WP CARGO DOOR BENT A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 HV-CHECK, FORWARD CARGO BAY DOOR IS BENT AROUND DOOR HANDLE. REMOVED DAMAGED SECTION. INSTALLED REPAIR SCUFF PLATE. (M) 2L72 4F RTA6WE 20050329000062005032900006WP 2005 3 29 ASAA0580136 120050227A5230 SKIN DOUG DC9 DC983 3022083WP CARGO DOOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 OKC - HV-CHECK, MID CARGO BAY DOOR IS DENTED. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050329000092005032900009WP 2005 3 29 ASAA0580130 120050227A53219936639501 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 OKC - HV-CHECK, CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050329000102005032900010WP 2005 3 29 ASAA0580131 120050227A532199366391 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 OKC - HV-CHECK, CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050329000112005032900011WP 2005 3 29 ASAA0580134 120050227A53305912494501 SKIN DOUG DC9 DC983 3022083WP FUSELAGE BENT A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 HV-CHECK, FORWARD CARGO BAY DOOR CUTOUT IS GOUGED FORWARD OF UPPER DOOR STOP. REMOVED DAMAGE, AND INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050329000142005032900014WP 2005 3 29 ASAA0580139 120050227A523059101573 SKIN DOUG DC9 DC983 3022083WP CARGO DOOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 OKC - HV-CHECK, AFT CARGO BAY DOOR IS DENTED. COLD-WORKED TO ORIGINAL CONTOUR, INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050329000282005032900028WP 2005 3 29 ASAA0580124 120050227A53219936537501 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 OKC - HV-CHK, CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050329000342005032900034WP 2005 3 29 ASAA0580140 120050227A523059101573 SKIN DOUG DC9 DC983 3022083WP AFT CARGO DOOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 OKC - HV-CHECK, AFT CARGO BAY DOOR IS DENTED. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050329000362005032900036EA 2005 3 29 A6WA200540101 120050316A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31413AW 7585 RIGHT INTERCOSTAL AT FS 484 AT RBL 36 CRACKED 1 INCH LONG. (M) PERFORMED A REPAIR AT FS484, RBL 36 BY CUTTING OUT DAMAGED AREA AND INSTALLING NEW ANGLE IAW REO. (K) 2L72 4F RTA21EA 20050329000392005032900039SO 2005 3 29 SIMA200506605 120050302A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21801AE 145469 DURING AN IMBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. PERFORMED A CUTOUT TO REMOVE THE CORROSION. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB-145/1142 REV 28 CHAPTERS 53-21-10 FIG 201. (M) 2L72 4F RTT00011AT 20050329000402005032900040CE 2005 3 29 S2YA05015 120050211A3297 WIRE BEECH 1900 1900D 1154162CE NLG CORRODED A S2YAO OTHER J WARNING INDICATION CLCLIMB 1 GL1392SK UE92 FLT 1851 - GRR-MKE - AFTER TAKEOFF, THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT AND THE INSTRANSIT LIGHTS REMAINED ILLUMINATED. THE CREW CONTINUED TO MKE WITH THE GEAR DOWN. MAINTENANCE INSPECTED THE SYSTEM AND FOUND A CORRODED JUMPER WIRE AT A325P1 IN THE NOSE WHEEL WELL. THE JUMPER WAS REPLACED AND THE GEAR OPERATIONALLY CHECKED GOOD. WITH NO FURTHER DISCREPANCIES NOTED THE A/C WAS RETURNED TO SERVICE. (M) 2L72 4T RTA24CE 20050329000412005032900041NE 2005 3 29 S2YA05014 220050210A751002ND362033 VALVE DORNERDO32 DO328300 NM PWA 306 PW306B NE ANTI ICE SYSTEM MALFUNCTIONED A S2YAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL13359SK 3202 APPROXIMATELY 80 KNOTS RECEIVED AN ENGINE ANTI-ICE OVERHEAT AND A SINGLE WARNING CHIME. CREW ABORTED TAKEOFF AND MESSAGE CLEARED DURING ROLLOUT. CREW UNABLE TO DUPLICATE THE PROBLEM AND THE A/C WAS CLEAR TO LAUNCH. DURING FLT 2265, MKE-BNA, THE SAME PROBLEM OCCURRED. THE CREW MADE AN AIR TURN BACK TO MKE. MAINTENANCE REPLACED THE BLEED AIR SHUTOFF VALVE AND WITH ALL OPERATIONAL CHECKS WERE GOOD THE A/C WAS RETURNED TO SERVICE. LATER THAT DAY BEFORE FLIGHT 2127 - CLE-MKE, THE SAME PROBLEM OCCURRED. THE CREW ABORTED THE TAKEOFF AND AGAIN THE MESSAGE CLEARED AND WAS UNABLE TO BE DUPLICATED. ON RETURN TO MKE, MAINTENANCE INSPECTED THE RIGHT ANTI-ICE VALVE AND CONNECTOR, ALL OPERATIONAL CHECK WERE GOOD. (M)2H72 4T4 FRTA55NM E35NE 20050329000422005032900042CE 2005 3 29 S2YA05019 120050225A2750 SWITCH BEECH 1900 1900D 1154162CE TE FLAPS MALFUNCTIONED A S2YAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL1385SK UE85 FLT 1071 - SDF-MKE - AFTER TAKEOFF, THE CREW WAS UNABLE TO RAISE THE FLAPS, PERFORMED AIR TURN BACK TO SDF. THE FLAPS WHERE RETRACTED USING THE BYPASS SWITCH AND THE SYSTEM WAS MEL'D. THE MEL WAS CLEAR BY ADJUSTING THE RT FLAP SAFETY SWITCH AND REPLACING THE FLAP SWITCH ARM ASSEMBLY. (M) 2L72 4T RTA24CE 20050329000432005032900043NM 2005 3 29 USAA050330 120050216A5322 SHEAR TIE BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19438US 24560 PIT - FOUND SHEAR TIE CRACKED .5 INCH, STRINGER 2R STATION 578. REMOVED AND REPLACED WITH NEW PART PER SRM 51-40-02. (M) 2L72 4F RTA16WE 20050329000442005032900044NM 2005 3 29 USAA050306 120050228A5754 SKIN BOEING737 7373B7 1384580NM NR 5 SLAT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19519AU50516 23705 CLT - FOUND NR 5 SLAT WITH 4 INCH CRACK, LOWER LE SKIN NR 5. INSTALLED REPAIR DOUBLER IAW SRM 57-43-01. (M) 2L72 4F RTA16WE 20050329000452005032900045NM 2005 3 29 USAA050303 120050223A5315 FLOORBEAM BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19442US40275 24841 CLT - FOUND FLOORBEAM CORRODED 10.9 INCHES BY 2 INCHES, STATION 328 ENTIRE T-CAP. INSTALLED T-CAP REPAIR PER SRM 53-10-51. (M) 2L72 4F RTA16WE 20050329000482005032900048NM 2005 3 29 USAA050331 120050216A5322 SHEAR TIE BOEING737 7374B7 1384702NM FUSLEAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19438US 24560 PIT - FOUND SHEAR TIE CRACKED .25 INCH, STRINGER 1 STATION 578. REMOVED AND REPLACED WITH NEW PART PR SRM 51-40-02. (M) 2L72 4F RTA16WE 20050329000492005032900049NM 2005 3 29 USAA050328 120050223A5320 CHANNEL BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19438US40959 24560 PIT - FOUND CARGO FLOOR CHANNEL AND SUPPORT ANGLE WITH CRACKS, APPROX .5 INCH CRACKS, FS 500G, RBBL 6. MANUFACTURED AND INSTALLED CARGO FLOOR CHANNEL AND SUPPORT ATTACH ANGLE PER SRM 53-00-53. (M) 2L72 4F RTA16WE 20050329000532005032900053NM 2005 3 29 USAA050335 120050223A53151137215 FLOORBEAM BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19438US40959 24560 PIT - FOUND FLOORBEAM CORRODED 8 INCHES, STATION 312. CORROSION LEVEL 1, TASK C53-107-01. REMOVED AND REPLACED PER SRM AND IPC 53-4200 FIG 2. (M) 2L72 4F RTA16WE 20050329000542005032900054NM 2005 3 29 USAA050324 120050220A5315BAC1505100296 FLOORBEAM BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19438US40959 24560 PIT - FOUND BEAM WITH CORROSION 48 INCH LONG SEVERAL AREAS, FS 312, UPPER CAP FLOORBEAM. CORROSION LEVEL 1, TASK C53-107-01. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 53-10-51, FIG 205. (M) 2L72 4F RTA16WE 20050329000552005032900055NM 2005 3 29 USAA050311 120050216A5320 CHANNEL BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU50570 23706 PIT - FOUND U-CHANNEL WITH 1 INCH CRACK, BS 747-767. FABRICATED AND INSTALLED NEW U-CHANNEL SUPPORT. (M) 2L72 4F RTA16WE 20050329000562005032900056NM 2005 3 29 USAA050334 120050219A53201138222 CHANNEL BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19438US40959 24560 PIT - FOUND ZEE CHANNEL CORRODED 1 INCH BY 12 INCH AREA, RIGHT SIDE ZEE CHANNEL STATION 294-362. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-10-02, 51-20-01, 51-40-00. (M) 2L72 4F RTA16WE 20050329000582005032900058NM 2005 3 29 USAA050329 120050220A5320 ANGLE BOEING737 7374B7 1384702NM FUSLEAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19438US40732 24560 PIT - FOUND ANGLE CRACKED .25 INCH, S14R TO S15R AT BS 360 ANGLE BETWEEN STRINGERS. CUTOUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-00-07 FIG 207. (M) 2L72 4F RTA16WE 20050329000602005032900060NM 2005 3 29 USAA050322 120050211A554265C2584151 SKIN BOEING737 7373B7 1384580NM RUDDER DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU50570 23706 PIT - FOUND EXT COMPOSITE SURF 4 INCH LONG BY .125 INCH SINGLE LAYER DAMAGE, RUDDER RT SIDE 64 INCHES FROM BOTTOM 34 INCHES FROM T/E. INSTALLED REPAIR PLYS, SEALED AND REFINISHED PER BOEING SRM 51-70-17, EA 79999. (M) 2L72 4F RTA16WE 20050329000622005032900062NM 2005 3 29 USAA050320 120050211A554265C2584151 SKIN BOEING737 7373B7 1384580NM RUDDER DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU 23706 PIT - FOUND EXT COMPOSITE SURF WITH 1 INCH SINGLE LAYER DAMAGE DELAMINATION, RUDDER RT SIDE 41 INCHES FROM BOTTOM, 8 INCH FROM T/E. INSTALLED REPAIR PLYS, SEALED AND REFINISHED PER BOEING SRM 51-70-17, EA 79999. (M) 2L72 4F RTA16WE 20050329000632005032900063NM 2005 3 29 USAA050310 120050217A5720 SUPPORT ANGLE BOEING737 7373B7 1384580NM RT WING CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU50570 23706 PIT - FOUND SUPPORT ANGLE CRACKED 1 INCH, TRAILING EDGE OF SUPPORT PANEL, RT WING JUST ABOVE INBOARD EDGE OF NR 5 FLAP. FABRICATED AND INSTALLED NEW SUPPORT ANGLE PER BOEING DWG 69-47542 AND SRM 57-51-02. (M) 2L72 4F RTA16WE 20050329000642005032900064NM 2005 3 29 USAA050309 120050218A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU50570 23706 PIT - FOUND SKIN CHAFED .013 INCH BY .011 INCH DEEP BY 20 INCHES LONG, BS 867-887 LT/RT SIDE OF SKIN UNDER DORSAL FIN. CUT AREA OUT, INSTALLED FILLER, DOUBLER AND TRIPLER AND CHAFED STRAPS PER SRM 53-60-01 FIG 201 PAGE 241. (M) 2L72 4F RTA16WE 20050329000652005032900065NM 2005 3 29 USAA050305 120050224A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19387US54352 22959 CLT - FOUND SKIN CRACKED 3.375 INCH STATION 883 STRINGER 25R. INSTALLED DOUBLER IAW SRM 53-00-01. (M) 2L72 4F RTA16WE 20050329000672005032900067NM 2005 3 29 USAA050307 120050222A575535759 SKIN BOEING737 7374B7 1384702NM NR 2 SPOILER CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19440US39212 24811 PIT - FOUND NR 2 SPOILER CRACKED .125 INCH, AND .5 INCH BY .5 INCH AREA DELAMINATED. REMOVED AND REPLACED PER M/M 27-61-11 AND 27-61-11 AND 27-61-51. (M) 2L72 4F RTA16WE 20050329000702005032900070NM 2005 3 29 S2YA05016 120050218A2421ALT3524 GENERATOR DORNERDO32 DO328300 NM AC SYSTEM INOPERATIVE A S2YAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL13355SK9994 3124 FLT 2380 - MKE-PIT - DURING TAKOFF ROLL, THE RIGHT ALTERNATOR FAILED AND ALONG WITH THAT THE WINDSHIELD HEAT FAILED AND THE RT AC VOLT FAILED, THE CREW ABORTED THE TAKEOFF. THE ALTERNATOR REMAINED FAIL THROUGH SEVERAL ATTEMPTS TO RESET SO THE CREW RETURNED THE A/C TO THE GATE. MAINTENANCE REPLACED THE RT AC GENERATOR (ALTERNATOR) AND WITH OPERATIONAL CHECK GOOD THE A/C WAS RETURNED TO SERVICE. (M) 2H72 4T RTA55NM 20050329000712005032900071NM 2005 3 29 S2YA05021 120050227A1420 CONNECTOR DORNERDO32 DO328300 NM SHUTOFF VALVE DIRTY A S2YAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL13351SK 3108 FLT 2297 - YYZ-MKE - TAKEOFF ROLL THE CREW GOT A RT BLEED SOV CAS MESSAGE, THEY CONSULTED WITH MX AND WHERE ABLE TO GET IT TO CLEAR. THE CREW ATTEMPTED TAKEOFF AGAIN BUT AGAIN RECEIVED A RT BLEED SOV CAS MESSAGE. THE A/C RETURNED TO THE GATE. OUTSTATION MX CLEANED THE CONNECTOR FO THE LOW PRESSURE PRSOV. WITH NO FURTHER DISCREPANCIES NOTED THE A/C WAS RETURNED TO SERVICE. (M) 2H72 4T RTA55NM 20050329000732005032900073NM 2005 3 29 S2YA05013 120050206A24218160121 GENERATOR DORNERDO32 DO328300 NM LEFT OVERHEATED A S2YAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL13359SK 3202 FLT 2380 - MKE-PIT - DURING FLIGHT, THE CREW NOTICED A LEFT GENERATOR OVERHEAT CAS MESSAGE, CONSULTED WITH MX BUT WAS UNABLE TO GET THE MESSAGE TO CLEAR. THE CREW MADE AN AIR TURN BACK TO MKE. MAINTENANCE INSPECTED THE A/C AND REPLACED THE LEFT GENERATOR, AFTER OPERATIONAL CHECKS WERE GOOD THE A/C WAS RETURNED TO SERVICE WITH NO OTHER DISCREPANCIES NOTED. (M) 2H72 4T RTA55NM 20050329000752005032900075EA 2005 3 29 A6WA200540092 120050309A3220 STRUT CNDAIRCL600 CL6002B19 1900309EA NLG UNDERSERVICED A A6WAO OTHER WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 GL31409AW 7447 NLG WOULD NOT RETRACT ON DEPARTURE. CYCLED GEAR AND COMPLIED WITH QRH. GEAR DISAGREE RED CAS. AMBER NWS CAS AND AMBER WOW INPUT CAS. SERVICED NLG STRUT IAW AMM 32-21-30. OPS GOOD IAW 32-33-00. (M) 2L72 4F RTA21EA 20050329000762005032900076EA 2005 3 29 A6WA200540093 120050311A5414 SKIN CNDAIRCL600 CL6002B19 1900309EA NACELLE DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31419AW 7633 DURING POST FLIGHT WALK AROUND, RIGHT ENGINE COWLING DISCOVERED POSSIBLY OPENED IN FLIGHT. DAMAGED NOTED. (M) REMOVED AND REPLACED DOOR INSTALL LOWER CORE COWL. OPS CHECK GOOD. (K) 2L72 4F RTA21EA 20050329000772005032900077SO 2005 3 29 SIMA200506606 120050302A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21801AE 145469 ABI - DURING AN IMBV INSPECTION, THE CENTER OMEGA BEAM AT FRAMES 23 AND 25 WERE FOUND CORRODED. BLENDED THE CORRODED AREAS TO REMOVED THE CORROSION AND PERFORMED NDT INSPECTION AND FABRICATED AN EXTERNAL DOUBLER FOR REPAIR. REPAIR DONE IAW EMB REPAIR DONE IAW EMB REPAIR STATEMENT IC2005-145/0976, PARA 3 DATED FEB 24, 2005. (M) 2L72 4F RTT00011AT 20050329000792005032900079SO 2005 3 29 SIMA200506802 120050308A335066367 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A SIMAK NONE O OTHER ININSP/MAINT 1 SW21636AE 145160 DFW - FLT 3358 - DURING POSTFLIGHT, CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHTS BETWEEN ROWS 7 THROUGH 10 APPEARS TO BE INOPERATIVE. MAINTENANCE REPLACED THE LIGHT STRIP IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20050329000812005032900081EA 2005 3 29 A6WA200540084 120050303A215032156222 RELIEF VALVE CNDAIRCL600 CL6002B19 1900309EA A/C PACK FAILED A A6WAO OTHER J WARNING INDICATION DEDESCENT 1 GL31438AW 7748 DURING DESCENT WITH POWER AT IDLE BOTH PACKS DROP OFF LINE. REMOVED AND REPLACED RT AND LT PRESSURE RELIEF VALVES IAW 21-51-43. (M) 2L72 4F RTA21EA 20050329000832005032900083NM 2005 3 29 S2YA05018 120050222A3246AHA22252 WHEEL DORNERDO32 DO328300 NM NLG VIBRATION A S2YAA UNSCHED LANDING E VIBRATION/BUFFET TOTAKEOFF 1 GL13355SK8404 718 3124 FLT 2265 - MKE-BNA - DURING TAKEOFF, THE CREW NOTICED A NOSEWHEEL VIBRATION JUST BEFORE TAKEOFF. THE CREW ELECTED TO CONTINUE WITH THE TAKEOFF AND CALLED MX IN THE AIR FOR A CONSULATION WHERE A DECISION WAS MADE TO PERFORM AN AIR TURN BACK TO MKE. MAINTENANCE REPLACED BOTH NOSE WHEEL ASSEMBLIES FOR TIRES BEING OUT OF ROUND AND THE A/C WAS RETURNED TO SERVICE. (M) 2H72 4T RTA55NM 20050329000842005032900084NM 2005 3 29 UIEA200500014 120050308A541465B940512 SKIN BOEING747 7472D7B 1384803NM NR 2 PYLON CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15527MC 22471 DURING INSPECTION, NR 2 PYLON, CRACK DAMAGE WAS FOUND AT PRE-COOLER EXHAUST CUTOUT LOWER AFT CORNER AT NACELLE STATION 248. THE NR 3 STIFFENER WAS REINFORCED WITH A NEW STEEL LOWER REPAIR ANGLE FROM NS 235 TO STA 254. THE RIB INSTALLATION AT NACELLE STATION 248 WAS MODIFIED TO ACCOMMODATE THE NEW STEEL LOWER REPAIR ANGLE INSTALLATION ON THE NR 3 STIFFENER. (M) 2L74 4F RTA20WE 20050329000852005032900085NM 2005 3 29 GAIA05012OP 120050302A311031892 SOCKET BOEING727 727224 1384076NM ANNUNCIATOR SMOKE A GAIAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW0769740 20668 FLT 754 - FWA-IND - DURING CLIMB FROM F/L 230 TO F/L 280. SMOKE WAS NOTICED COMING FROM THE FIRST OFFICERS INSTRUMENT PANEL. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO IND WHERE A LANDING WAS MADE WITHOUT INCIDENT. REMOVED AND REPLACED BELOW G/S PUSH TO TEST INHIBIT AND GPWS ANNUNCIATOR. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20050329000862005032900086NM 2005 3 29 UIEA200500017 120050308A542065B941001 CAP BOEING747 7472D7B 1384803NM STRUT CHAFED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15527MC 22471 DURING SCHEDULED MAINTENANCE, CHAFING MARK WAS FOUND ON THE LEFT SIDE OF THE SKIN ASSEMBLY AT NACELLE STATION 270. AFFECTED FASTENERS WERE REMOVED AND FASTENER HOLES WERE HFEC INSPECTED TO ENSURE CRACK AND DAMAGE FREE CONDITION. THE CHAFING DAMAGE WAS REMOVED BY BLENDING TO A SMOOTH CONTOUR. ENSURED MINIMUM MATERIAL REMOVED. THE BLENDED SURFACE WAS REFINISHED AND DESIGN TYPE OVERSIZE FASTENERS WERE INSTALLED PER SRM REQUIREMENTS. THE REPAIR CONFORMS TO DESIGN REQUIREMENTS. (M) 2L74 4F RTA20WE 20050329000892005032900089NM 2005 3 29 USAA050301 120050223A5315 FLOORBEAM BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19442US40275 24841 CLT - FOUND FLOORBEAM CORRODED 2 INCH BY 78 INCH AREA OF CORROSION, STATION 294 ENTIRE T-CAP. INSTALLED NEW SECTION OF FLOORBEAM PER SRM 53-10-51. (M) 2L72 4F RTA16WE 20050329000922005032900092NM 2005 3 29 S2YA05010 120050201A21504067B000004 SHUTOFF VALVE DORNERDO32 DO328300 NM LT A/C PACK FAILED A S2YAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL13356SK 3163 FLT 2265 - MKE-GRR - DURING TAKEOFF, THE CREW GOT A LEFT PACK INOPERATIVE CAS MESSAGE, CONSULTED WITH MAINTENANCE BUT WERE UNABLE TO GET THE MESSAGE TO CLEAR. THE A/C RETURNED TO THE GATE. MAINTENANCE REPLACED THE LEFT HIGH PRESSURE VALVE (PRSOV) BUT THE PROBLEM REMAINED. MAINTENANCE THEN REPLACED THE OXYGEN/ECS PANEL AND ALL OPERATIONAL CHECKS WERE GOOD. WITH NO FURTHER DISCREPANCIES NOTED THE A/C WAS RETURNED TO SERVICE. (M) 2H72 4T RTA55NM 20050329000932005032900093EA 2005 3 29 A6WA200540104 120050316A5313 RIB CNDAIRCL600 CL6002B19 1900309EA LT MLG WW CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31413AW 7585 LEFT MLG WHEEL WELL AT SS 48.30 FS 523.8 BATT RIB IS CRACKED 1.25 INCH LONG. (M) REPAIRED LT WING BATT RIB AT WS 53.60 IAW MFG REO. (K) 2L72 4F RTA21EA 20050329000942005032900094EA 2005 3 29 A6WA200540095 120050313A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE GOUGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31407AW 7424 FOUND SKIN GOUGED AT PANEL B2AL ATTACH SCREW AT 1 O'CLOCK POSITION. BLENDED AREA, PERFORMED EDDY CURRENT AND TREATED BARE MATERIAL. (M) 2L72 4F RTA21EA 20050329000982005032900098 2005 3 29 A6WA200540091 420050308A22106229815704 COMPUTER CNDAIRCL600 CL6002B19 1900309EA AUTOFLIGHT MALFUNCTIONED A A6WAO OTHER F FLT CONT AFFECTED CLCLIMB 1 GL31418AW 7618 RUDDER FLUTTER INFLIGHT, ALL CONDITIONS, AUTOPILOT ENGAGES. REMOVED AND REPLACED FCC NR 1 IAW 22-12-14. PERFORMED OPS TEST IAW AMM 22-11-00. OPS CHECK GOOD. AIRCRAFT CERTIFIED FOR RVSM. (M) 2L72 4F RTA21EA 20050329001002005032900100NM 2005 3 29 S2YA05020 120050227A2621335000121 FIRE BOTTLE DORNERDO32 DO328300 NM LEFT DISCHARGED A S2YAFA ACTIVATE FIRE EXT. UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL13356SK 3163 MKE-BDL - DURING TAKEOFF, THE CREW RECEIVED A FIRE BOTTLE DISCHARGE LIGHT INDICATION. THE CREW PERFORMED AN AIR TURN BACK TO MKE. MAINTENANCE REPLACED THE LEFT FIRE BOTTLE AND WITH OPERATIONAL CHECKS GOOD THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2H72 4T RTA55NM 20050329001022005032900102EA 2005 3 29 A6WA20050090 120050308A21707536893 COALESCER BAG CNDAIRCL600 CL6002B19 1900309EA RIGHT CONTAMINATED A A6WAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL31453AW 7838 SMOKE TOILET MESSAGE INFLIGHT. COMPLIED WITH QRH. FLIGHT ATTENDANT REPORTS HAZE IN CABIN. SMOKE NO LONGER PRESENT. RESET C/B, TESTED TOILET SMOKE DETECTORS, SYSTEM CHECK GOOD. TROUBLESHOT AND FOUND PACK NR 2 ACM DEFECTIVE. NR 2 ACM OIL CHECKED NORMAL. REPLACED RIGHT WATER SEPARATOR SOC GROUND RAN ECS PACK NR 2 AND ACM CHECKS NORMAL. NO SMOKE VISIBLE. (M) 2L72 4F RTA21EA 20050329001032005032900103NM 2005 3 29 S2YA05011 120050203A5280001A3221A500000 ROD DORNERDO32 DO328300 NM MLG DOOR SHEARED A S2YAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL13352SK 3111 FLT 2343 - MKE-CMH - AFTER TAKEOFF, THE CREW NOTICED A NOSE VIBRATION BELIEVING THAT THE GEAR DOOR MIGHT NOT BE FULLY CLOSE. THE CREW MADE AN AIR TURN BACK TO MKE. MAINTENANCE INSPECTED THE A/C AND REPLACED THE LEFT FORWARD NOSE LANDING GEAR DOOR SHEAR ROD. AFTER OPERATIONAL AND RIG CHECKS WERE GOOD THE A/C WAS RETURNED TO SERVICE WITH NO OTHER DISCREPANCIES NOTED. (M) 2H72 4T RTA55NM 20050329001072005032900107NM 2005 3 29 SWAA050900 120050326A53126546568 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29324SW 23414 DURING SCHEDULED C4 CHECK, FOUND 2 EA FUSELAGE CRACKS AT AFT PRESSURE BULKHEAD, BS 1016, STR 4L & BETWEEN STR 6R TO STR 7R. REPAIRED AFT PRESSURE BULKHEAD PER SWA EA. 2L72 4F RTA16WE 20050329001082005032900108NM 2005 3 29 SWAA050901 120050324A53306545776 SKIN BOEING737 7373H4 1384600NM FUSLAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29324SW 23414 DURING SCHEDULED C4 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS AT BS 908 & BS 920, STR 23L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050329001092005032900109NM 2005 3 29 SWAA050902 120050325A3350101331 LENS BOEING737 7377AD 1384502NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29798SW 28436 OVERWING CENTER AISLE EMERGENCY EXIT SIGN LENS MISSING. INSTALLED LENS COVER PER MM. 2L72 4F RTA16WE 20050329001102005032900110NM 2005 3 29 SWAA050903 120050324A57546573714 WEDGE BOEING737 7373H4 1384600NM RT WING SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29324SW 23414 DURING SCHEDULED C4 CHECK, FOUND RT WING NR 6 L/E SLAT T/E WEDGE DELAMINATED. REMOVED AND REPLACED SLAT PER MM. 2L72 4F RTA16WE 20050329001112005032900111NM 2005 3 29 SWAA050904 120050324A57536546486 WEDGE BOEING737 7373H4 1384600NM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29324SW 23414 DURING SCHEDULED C4 CHECK, FOUND RT WING INBOARDD MIDFLAP OUTBOARD T/E WEDGE DELAMINATED. REMOVED AND REPLACED WEDGE PER MM. 2L72 4F RTA16WE 20050329001122005032900112 2005 3 29 SWAA050905 420050324A25656970843 HOOK BOEING737 7377H4 1384404NM R1 DOOR GIRT BARLOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29420WN 29825 R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR STOW HOOK LOOSE. SECURED HOOK PER MM. 2L72 4F RTA16WE 20050329001132005032900113NM 2005 3 29 SWAA050906 120050324A335070036611 BALLAST BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29426WN 29830 DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BALLAST PER MM. 2L72 4F RTA16WE 20050330000372005033000037 2005 3 30 KBM2005F00010 420050211A34225050031904 GYRO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE COCKPIT INTERMITTENT E KBMAK NONE O OTHER ININSP/MAINT 1 WP19966SH 3787 DG INTERMITTENT IN FLIGHT, 2 KNOBS LOOSE, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050330001702005033000170 2005 3 30 S2YA05007 420050120A34577015327905 GPS DORNERDO32 DO328300 NM PWA 306 PW306B NE AUTO PILOT INOPERATIVE A S2YAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL13355SK113322628 3124 SHORTLY AFTER TAKEOFF, THE CREW DECLARED AN EMERGENCY DUE TO THE SMELL OF SMOKE ACCOMPANIED BY WITH THE LIGHT RESEMBLANCE OF SMOKE IN THE COCKPIT. THE CREW MADE AN AIR-TURN-BACK. MECHANIC REPLACED THE GPS-300 FLIGHT DIRECTOR AND AUTO PILOT CONTROL PANEL. OPERATIONAL CHECK REVEALED THE AUTO PILOT NOW DID NOT WORK WITH THE NEW PANEL. THE AUTO PILOT FUNCTION WAS MELED. ON 01/23/05 THE MEL WAS CLEARED BY REPLACING THE GPS-300 PANEL AGAIN. WITH NO FURTHER DISCREPANCIES NOTED THE AC WAS RETURNED TO SERVICE. (K) 2H72 4T4 FRTA55NM E35NE 20050330001822005033000182NM 2005 3 30 72300106 120050328A5340 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 6 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050330001862005033000186NM 2005 3 30 72300102 120050328A5340 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 6 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050330001902005033000190NM 2005 3 30 72300098 120050328A5340 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 3 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050330001932005033000193NM 2005 3 30 72300095 120050323A5340 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 3 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050330001952005033000195NM 2005 3 30 72300093 120050323A5340 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 3 X 1 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050330001962005033000196NM 2005 3 30 72300092 120050323A5340 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 4 X 1 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050330001992005033000199SO 2005 3 30 LR7A05036 120050306A5311 FRAME LKHEED382 382G 526414USO FUSELAGE MISDRILLED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2850 4763 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED / MIS-DRILLED FUSELAGE LINER HOLES AT FS 782E, WL 148, LBL 65. REPAIRED IAW LAC MEA 382-53-04-074 R1. 2H74 4T A1SO 20050330002042005033000204SO 2005 3 30 LR7A05031 120050306A5311 FRAME LKHEED382 382G 526414USO FUSELAGE MISDRILLED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2850 4763 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED / MIS-DRILLED FUSELAGE LINER HOLES AT FS 444, WL 148, RBL 65. REPAIRED IAW LAC MEA 382-53-04-074 R1. 2H74 4T A1SO 20050330002212005033000221SO 2005 3 30 LR7A05014 120050306A5310 BEAM LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2850 4763 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND CW REAR BEAM WEB CRACKED AT FS 597, WL 276, CWS 52L. REPAIRED IAW LAC MEA 382-57-05-025. 2H74 4T A1SO 20050330002312005033000231NM 2005 3 30 EIA2005041 120050222A5314 KEELBEAM BOEING747 747SR46 1384816NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09478EV 21033 KEEL BEAM RIGHT LOWER CHORD CORROSION BS 1335-1345 WL 100 RBL 10. CORROSION REMOVED PER SRM 53-10-01, REPAIR PARTS FABBED AND INSTALLED PER ECRA 478-51-173-1. 2L74 4F RTA20WE 20050331000112005033100011WP 2005 3 31 ASAA0580016 120050123A5320991555415 INTERCOSTAL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02964AS 53078 OKC - HV-CHECK, SEAT TRACK SUPPORT HAS CORRODED FASTENERS ON ATTACHING ANGLE INTERCOSTAL. REPLACED INTERCOSTAL. (M) 2L72 4F RTA6WE 20050331000332005033100033WP 2005 3 31 DHL2005805571 120050322A574037048412 FITTING DOUG DC8 DC873F 302199FWP NR 2 FUEL TANK CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 NR 2 MAIN TANK INTERIOR FITTING CRACKED 2.000 AT STA 740.000 S-51 (FWD PORT). REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9. TORQUED IAW SRM 51-3-1. REFER TO NR 028714 FOR LEAK CHECK. 2L74 4F RT4A25 20050331000362005033100036EU 2005 3 31 05FDEA00670 120050328A5347 SEAT TRACK AIRBUS310 A310222 3930315EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 MAIN CABIN FRAME 34 TO 37 SEAT TRACK YB77 HAS 2EA AREAS OF CORROSION NR 4 SEAT TRACK RT. REMOVED CORROSION IAW A310 SRM 51-74-10, OUT OF LIMITS IAW A310 SRM 53-10-16 FIG 101. FABBED NEW REPAIR SECTION OF SEAT TRACK IAW A310 SRM 53-10-16 FIG 208. REMOVED AND REINSTALLED SPICES AND SUPPORT BRACKET IAW A310-200 SRM 51-72-10. REMOVE BAD SECTION OF TRACK FROM FR33.5 TO 36.5 AND INSTALLED NEW REPAIR SECTION IAW A310-200 SRM 51-72-10 AND 53-10-16 FIG 208. 2L72 4F RTA35EU 20050331000432005033100043WP 2005 3 31 DHL2005805553 120050320A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME WORN, STA 700.000 L-8 L-9R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-04-05, EO AST 050217 DATE 03-03-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO AST050217, SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050331000562005033100056NM 2005 3 31 05FDEA00680 120050328A5347ABA7680505 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 MAIN DECK, SEAT TRACK LBL 107 CORRODED AT STA. REMOVED AND REPLACED AS IAW SRM 51-33-01 VOLUME II. 2L73 4F RTA22WE 20050331000682005033100068NM 2005 3 31 05FDEA00684 120050328A5347AEA75791 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 MAIN DECK, SEAT TRACK 47.5 CORRODED AT STA 1531. CARRIED OUT REPAIR IAW SRM 53-70-00 VOLUME I FIGURE 1. 2L73 4F RTA22WE 20050331000722005033100072NM 2005 3 31 05FDEA00688 120050328A5347AFA7795510 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 MAIN DECK, SEAT TRACK RBL 27.5 CORRODED AT STA 1691. REPAIRED IAW SRM 53-70-00 FIGURE 1 VOLUME I. 2L73 4F RTA22WE 20050331000772005033100077EA 2005 3 31 COMA0560206 120050326A3620356072310 SENSOR CNDAIRCL600 CL6002B19 1900309EA E/E BAY FAULTY A COMAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 SO01814CA 7387 FLIGHT 5138 RECEVIED A LEFT 14TH STAGE DUCT MESSAGE DURING CLIMBOUT OF CAE, CREW DECLARED AN EMERGENCY, LEFT ENGINE WAS SHUT DOWN AND RETURNED TO THE FIELD, AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE 14TH STAGE HEAT SENSING ELEMENT. 2L72 4F RTA21EA 20050331000782005033100078EA 2005 3 31 COMA0560207 120050326A3620356024310 SENSOR CNDAIRCL600 CL6002B19 1900309EA E/E BAY FAULTY A COMAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 SO01814CA 7387 FLIGHT 5138 RECEIVED A LEFT 14TH STAGE DUCT MESSAGE CLIMBOUT OF CAE, CREW DECLARED AN EMERGENCY, LEFT ENGINE WAS SHUT DOWN AND RETURNED TO THE FIELD, AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE 14TH STAGE HEAT SENSING ELEMENT. 2L72 4F RTA21EA 20050331000862005033100086WP 2005 3 31 DHL2005805632 120050320A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT INBOARD FLANGE Z-FRAME (1) HOLE MISDRILLED AT STA 340.000 L-8 L-9R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-04-05 EO AST 050217 DATE 03-03-05. PERFORMED NDT INSPECTION (DETAILED). NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO AST 050217 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050331001012005033100101SO 2005 3 31 SWIA200514791 120050325A5210 ROD END EMB 120 EMB120ER 3260203SO PAX DOOR OUT OF ADJUST A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07579SW 120347 MAIN CABIN DOOR VERY HARD TO OPEN & CLOSE. ADJUSTED 2 ROD ENDS AND LUBRICATED ALL MOVING PARTS AS NECESSARY. DOOR NOW OPERATIONALLY CHECKS GOOD. 2L72 4T RTA31SO 20050331001122005033100112SO 2005 3 31 SWIA200514796 120050314A2797 CONNECTOR EMB 120 EMB120ER 3260203SO TE FLAP CONTROL FAILED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07584SW 120352 FLAP CONTROL FAULT. REPLACED CONNECTOR ON LEFT AND RIGHT OUTBOARD ACTUATOR. OPERATIONAL CHECK GOOD IAW MM 27-50-00. 2L72 4T RTA31SO 20050401000012005040100001CE 2005 4 1 ZH92005F00000 120050323A3110BAS350352831 SWITCH LEAR 35 35A 5170602CE GARRTTTFE731TFE731* 01518WP INSTRUMENT PANELSHORTED E ZH9AO OTHER O OTHER NRNOT REPORTED 1 EA27326HG 501 WHILE RETURNING TO AIRPORT, THE COPILOTS ALTIMETER BREAKER POPPED, WHICH IN TURN DISABLED THE NR2 ALTIMETER/ADDU. THE AC LANDED 10 MINUTES LATER WITHOUT INCIDENT AND THE NR2 ALTIMETER FAILURE WAS REPORTED TO MAINTENANCE. WHEN THIS PROBLEM WAS INVESTIGATED IT WAS FOUND THAT BOTH ALTIMETER BREAKERS WERE POPPED AND BOTH ALTIMETER/ADDU WERE INOPERATIVE. THE PROBLEM WAS EVENTUALLY TRACED TO A SHORTED AIR DATA SWITCH PANEL WHICH WAS INSTALLED IN THE INSTRUMENT PANEL AS NEW DURING THE STC MODIFICATION. FAILURE OF THIS COMPONENT CAUSED BOTH ALTIMETERS, BOTH ADDUS, ALL MODE C TRANSPONDER INFO, AND THE AUTOPILOT TO BECOME INOPERATIVE. 2L72 4F4 F A10CE E6WE 20050401000032005040100003 2005 4 1 KBM2005F00043 420050312A34225040017901 GYRO SNIAS 350 AS350B2 8680813EU ALLSN 250C 250C20B 03013GL ATTITUDE MALFUNCTIONED A KBMAK NONE O OTHER ININSP/MAINT 1 WP19751H 729 3403 ATTITUDE INDICATOR WOULD NOT CAGE PROPERLY. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E4CE 20050401000152005040100015NM 2005 4 1 USAA050338 120050302A5340 ATTACH ANGLE BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19442US40275 24841 CLT - Q6 - ATTACH ANGLE, .250 INCH CRACK, STATION 578 BETWEEN STRINGERS 8R AND 9R. REPLACED ATTACH ANGLE WITH FABRICATED PART IAW DWG. 2L72 4F4 FRTA16WE E21EU 20050401000162005040100016NM 2005 4 1 USAA050342 120050307A5754 WEDGE BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU NR4 SLAT WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19519AU50516 23705 CLT - Q2 - NR 4 SLAT, 2 INCH X 2 INCH, WEAR. NR 4 SLAT T/E WEDGE LOWER SKIN IB. ACCOMPLISHED COMPOSITE REPAIR IAW EA. (K) 2L72 4F4 FRTA16WE E21EU 20050401000302005040100030NM 2005 4 1 USAA050357 120050222A552365C2638415A SKIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU LT ELEVATOR TAB DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19438US40959 24560 PIT - Q4 - EXT COMPOSITE SURFACE, .500 INCH AREA OF DELAMINATION, LT ELEVATOR TAB TOP IB CORNER. PREPARED DAMAGED AREA, INSTALLED REPAIR PLYS, HARDWARE, REFINISHED IAW SRM 55-20-01 AND 51-70-05. (K) 2L72 4F4 FRTA16WE E21EU 20050401000312005040100031NM 2005 4 1 USAA050359 120050218A5320 SUPPORT BRACKET BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19438US40959 24560 PIT - Q4 - BRACKETS, 1 INCH X 3 INCH CORROSION, 4 BRACKETS. CORROSION; LEVEL 1; TASK C53-107-02 THRESHOLD SUPPORT BRAKETS, FWD DOOR ENTRY FLOOR STRUCTURE. PARTS REPLACED IAW MFG DWG. (K) 2L72 4F4 FRTA16WE E21EU 20050401000982005040100098EA 2005 4 1 A6WA200540110 120050316A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT SIDE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31415AW 7593 FLOOR SUPPORT ANGLE AT FS 621 RT SIDE IS CRACKED 1 INCH. PERFORMED REPAIR TO RT FS621, FLOOR SUPPORT ANGLE IAW REO. (K) 2L72 4F4 FRTA21EA E15NE 20050401001042005040100104NM 2005 4 1 USAA050354 120050310A5743 SUPPORT FITTING BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU LT MLG CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19519AU50516 23705 CLT - Q2 - SUPPORT FITTING, .1250 INCH CRACK. LT WING MLG SUPPORT FITTING. ACCOMPLISHED REPAIR IAW TR 57-40-13. (K) 2L72 4F4 FRTA16WE E21EU 20050404000012005040400001CE 2005 4 4 VLI2005F00000 120050127A322026430623 SPRING CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE MCAULY3AF34C3GFR34C703 GL NLG CRACKED E VLIAK NONE O OTHER ININSP/MAINT 1 SO21335VL1922 208B0964 PCEPC0975 020393 PILOT REPORTED, NOSE GEAR COLLAPSED. DURING RUN-UP SPRING NOSE GEAR CRACKED. (SO21200503223) 1H71 3T3 T A37CE E4EA 5 CP60GL 20050404000032005040400003EU 2005 4 4 M7K2005F00000 120050316A2913704A44310027 PUMP UROCOPEC130 EC130B4 8680989EU TMECA ARRIELARRIEL2B NE HYDRAULIC SYS INOPERATIVE E M7KAK NONE O OTHER ININSP/MAINT 1 WP19804MH 3750 23072 DURING RUNUP, IT WAS NOTICED THAT HYDRAULIC PRESSURE WARNING FAILED TO EXTINGUISH UNTIL AIRCRAFT WAS RUN-UP ABOVE IDLE TO FLIGHT IDLE SPEED. SUBSEQUENT INVESTIGATION REVEALED NO FLUID RETURN TO THIS PUMPS RESERVOIR. REPLACEMENT OF THE PUMP CORRECTED THE PROBLEM. EXTERNALLY THE REMOVED PUMP APPEARED NORMAL. PUMP RETURNED TO MFG FOR INSPECTION. THIS IS A 2-PUMP HYDRAULIC SYSTEM. (K) 1G72 3U3 U H9EU E00054EN 20050404000072005040400007CE 2005 4 4 XRR2005F00000 120050211A56105042006930 WINDSHIELD BEECH 100 B100 1152919CE GARRTTTPE331TPE331* 01514WP COCKPIT CRACKED E XRRAK NONE O OTHER ININSP/MAINT 1 CE01564CA3902 BE58 INNER PANE OF CO-PILOTS WINDSHIELD CRACKED WHILE AT ALTITUDE. 1L72 4T3 T A14CE E2WE 20050404000082005040400008 2005 4 4 TVD2005F00000 420050215A3417 LINE PILATSPC12 PC12 7090550EU ADC DETERIORATED E TVDAO OTHER N FALSE WARNING CRCRUISE 1 NM01156SB3430 156 WHILE FLYING AT 170 KIAS, THE PILOT NOTED HE HAD TO REDUCE POWER TO MAINTAIN 170 KIAS. SHORTLY AFTER THAT THE AIRCRAFT`S (STICK SHAKER) ACTIVATED. INSPECTION REVEALED SEVERELY DETERIORATED PLASTIC TUBING FROM FWD PRESSURE BULKHEAD TO AIR DATA COMPUTER. LINES WERE REPLACED. (K) 1L71 3T RTA78EU 20050404000212005040400021EA 2005 4 4 A6WA200540107 120050317A5730 ACCESS PANEL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT WING CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31415AW 7593 RT LOWER WING PLANK FUEL TANK ACCESS PANEL CUT-OUT BETWEEN SS 50.54 AND WS 66.2 HAS MINOR FRETTING AND FAYING SURFACE LESS THAT .006 INCH DEEP. (K) BLEED MINOR FRETTING ON RT LOWER WING PLANK BETWEEN WS 50-54 AND 66.2 IAW REO. (K) 2L72 4F4 FRTA21EA E15NE 20050404000282005040400028CE 2005 4 4 LQY2005F00000 120050207A273058151036CR CONTROL CABLE CESSNA441 441 2076020CE GARRTTTPE331TPE331* 01514WP RT ELEVATOR FRAYED E LQYAK NONE O OTHER ININSP/MAINT 1 CE07258VB4000 4410258 RT AFT ELEVATOR CABLE WAS FRAYED THROUGH 4 OF THE 7 STRANDS - FAILURE WAS IMMINENT. THIS CABLE SHOWED NO SIGNS OF WEAR ON THE PREVIOUS INSPECTION 500 HOURS BEFORE AND IT ONLY TAKES A 20 DEGREE BEND AT THIS PULLEY. PROBABLY SHOULD BE INSPECTED EVERY 300 HOURS INSTEAD OF THE FACTORY INSPECTION SCHEDULE OF 600 HOURS. SUGGEST THAT CORROSION RESISTANT STAINLESS STEEL CABLES SEEM TO BE MORE BRITTLE THAN THE STANDARD STEEL CABLES. (K) 1L72 3T3 TRTA28CE E2WE 20050404000302005040400030EA 2005 4 4 A6WA200540106 120050317A5730 ACCESS PANEL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT WING CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31415AW 7593 LT LOWER WING PLANK FUEL TANK ACCESS PANEL CUT-OUT BETWEEN SS 0.00 AND WS 29.42 HAS MINOR FRETTING ON FAYING SURFACE LESS THAN .006 INCH DEEP. C/A PENDING (K) 2L72 4F4 FRTA21EA E15NE 20050404000312005040400031CE 2005 4 4 ALG2005F00016 120050114A6340206075545001 SENSOR CESSNASTC STC206C 1182107CE ALLSN 250C 250C30P 03013GL MAIN ROTOR CORRODED E ALGAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW032611 45417 JUST AFTER TAKEOFF, THE LOW ROTOR CAUTION LIGHT ILLUMINATED. 2 OR 3 SECONDS LATER, THE LOW ROTOR RPM HORN SOUNDED. ROTOR TACH INDICATIONS WERE NORMAL, PILOT RETURNED TO BASE. UPON LANDING, THE MECHANIC REMOVED AND REPLACED BOTH THE LOW ROTOR RPM AND ENGINE OUT SENSORS DUE TO CORROSION AND AC WAS OPS CHECKED AND RETURNED TO SERVICE. (K) 1H71 3O3 UNTA4CE E1GL 20050404000322005040400032NM 2005 4 4 GAIA05014ST 120050319A5753652163223 SKIN BOEING727 727243 138408DNM PWA JT8 JT8D7B 52053NE LT TE FLAP DELAMINATED A GAIAK NONE O OTHER ININSP/MAINT 1 SW071269Y 21269 DURING A-CHECK, NO FLIGHT, FWA: FOUND LT IB MID-FLAP OB T/E MISSING 6 INCHES OF SKIN. REMOVED AND REPLACED LT IB MID-FLAP AND AFT FLAPS ASSY. OPS CHECKED NORMAL IAW MM 27-51. AIRCRAFT WAS RETURNED TO SERVICE. (SW07200506017) (K) 2L73 4F4 FRTA3WE E2EA 20050404000412005040400041EA 2005 4 4 A6WA200540034 120050125A5712 RIB CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT WING CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31412AW 7582 MWC 60. RT WING STATION 53.6 BUTT RIB IS CRACKED .5000 INCH LONG IN UPPER AFT RADIUS. REPAIRED RT WING STATION 53.60 BATT RIB IAW MFG EO 601R-57-51-046, REV B. 2L72 4F4 FRTA21EA E15NE 20050404000422005040400042WP 2005 4 4 ASAA0580106 120050215A53219936651505 FLOOR PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE PAX CABIN PEELING A ASAAK NONE O OTHER ININSP/MAINT 1 NM02943AS 53018 OKC C-CHECK - PAX CABIN FLOOR PANEL PEELED. FIBERGLASS BOND REPAIRED. (K) 2L72 4F4 FRTA6WE E9NE 20050404000482005040400048CE 2005 4 4 MXI2005F00002 120050309A212166082672 MOTOR LEAR 35 35A 5170602CE GARRTTTFE731TFE731* 01518WP COCKPIT FAN FAILED E MXIAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 EA21804TF 404 THE COCKPIT FAN MOTOR FAILED AND CAUSED SMOKE TO COME OUT OF THE OVERHEAD AIR VENTS. AFTER REPLACEMENT IT WAS NOTED THE FAN MOTOR WAS VERY HARD TO TURN. THERE IS NO TIME CHANGE FOR THIS MOTOR LISTED IN CHAPTER 5. (EA21200504524) (K) 2L72 4F4 F A10CE E6WE 20050404000542005040400054CE 2005 4 4 AZN2005F00000 120050201A324016400806 BRAKE DISC CESSNA310 310R 2074245CE CONT O520 IO520* 17032SO LT BRAKES CRACKED E AZNAK NONE O OTHER ININSP/MAINT 1 GL131761G 310R1223 NOTICED NUMEROUS OF OUR MFG BRAKE DISC, PN 164-00806 BEING CRACKED. THE CRACKS BEGIN WHERE MFG NAME IS STAMPED ON THE BRAKE DISC. FOUND 3 CRACKS WHERE THE LETTER (P) IS STAMPED AND ONE CRACK WHERE THE LETTER (R) IS STAMPED. PROBABLE CAUSE IS THE STAMPING LOCATION SETS UP A STRESS POINT. RECOMMEND DIFFERENT STAMPING LOCATION TO PREVENT RECURRENCE. (K) 1L72 3O3 O 3A10 E5CE 20050404000662005040400066CE 2005 4 4 L1K2005F00000 120050209A3243054113922 MASTER CYLINDER CESSNA185 A185F 2072821CE CONT O520 IO520D 17032SO MCAULY2A34C D2A34C58 GL BRAKE SYSTEM CONTAMINATED E L1KCO OTHER O OTHER LDLANDING 1 AL01185MF5034 18503268 1588618D AC LANDING AT BELOW FREEZING TEMP, HAD BRAKES LOCKING UP (FROZE UP) ON LANDING. INSP AFTER INCIDENT FOUND DIRT AND DEBRIS ALONG WITH CONTAMINATED FLUID (WATER) IN BOTTOM OF BOTH RT AND LT BRAKE MASTER CYL PN 0541139-22 WHEN REMOVED. CYL BODIES SHOWED NO SIGN OF EVER BEING REMOVED. NEW AT FACTORY ON 1-31-1977 AND WITH TT 5034.0. REVIEW OF AC RECORDS SHOWED THAT CYL HAVE HAD SEAL REPLACED BEFORE WITH NO MENTION OF BODIES BEING REMOVED AND CLEANED IN 27 YEARS 11MONTHS IN SERVICE. NOTE: INNER PART OF CYL CAN BE REMOVED AND SEAL REPLACED WITHOUT REMOVING CYL BODY. PROB CAUSE: BRAKE CYLINDER CONTAMINATION. RECOMMEND: IF CYL SEALS ARE REPLACED, ENTIRE BODY SHOULD BE REMOVED AND CLEANED. (AL01200502421) 1H71 3O3 O 3A24 E5CE 5 CP3EA 20050404000672005040400067SO 2005 4 4 QTL2005F00000 220050204A741410357584 DISTRIBUTOR GEARCONT CESSNA182 182H 2072718CE CONT O470 O470R 17026SO MAGNETO FAILED E QTLAK NONE O OTHER ININSP/MAINT 1 NM051904X D279801DR 18256004 1309324R MAGNETO REMOVED FOR FAILURE, 24 TEETH MISSING ON DISTRIBUTOR GEAR. REPLACED WITH NEW GEAR NR 10-357586. (K) 1H71 3O3 ONT3A13 E273 20050404000682005040400068WP 2005 4 4 K2D2005F00000 120050128A6410HTC500P3100101 BLADE HUGHES369 369E 4470707WP ALLSN 250C 250C20B 03013GL TAIL ROTOR DAMAGED E K2DAA UNSCHED LANDING D INFLIGHT SEPARATION CRCRUISE 1 WP13142MK2379 0187E REF: K2DA320J TAIL ROTOR BLADE ABRASION STRIP AND TIP CAP DEPARTED BLADE ASSY, INFLIGHT. (WP13200506018) (K) 1G71 3U3 U H3WE E4CE 20050404000762005040400076EU 2005 4 4 YVB2005F00000 120050125A3260D228580001 PROXIMITY SWITCH AMD FALC50FALCON900 2700160EU NLG WARPED E YVBAO OTHER J WARNING INDICATION CLCLIMB 1 EA11990BB 42 (CNTRL NR 0501) DURING TAKEOFF, LANDING GEAR WOULD NOT COME UP (HANDLE WOULD). WHEN GEAR HANDLE WAS PUT DONW, 3 GREEN DOWN AND LOCK AND AUTO SLAT LIGHT ON THE GEAR HANDLE WAS LOCKED (GROUND MODE). AIRCRAFT JACKED, GEAR SWUNG NORMALLY IN HANGAR. FOUND NOSE GEAR PROX SWITCHES WEAK. REPAIRED PROXIMITY SWITCH AND TESTED IAW MM. OK, EVERYTHING DONE IAW MM. (EA11200502913) (EA11200502879) (K) 2L73 4F RTA46EU 20050404000852005040400085EU 2005 4 4 KBM2005F00036 120050304A6520350A33215300 BEARING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE TAIL ROTOR WORN E KBMAK NONE O OTHER ININSP/MAINT 1 WP19345SH4464 3345 LAMINATED BEARINGS, WORN. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050404001102005040400110EU 2005 4 4 KBM2005F00038 120050202A6520350A33215300 BEARING SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE TAIL ROTOR WORN E KBMAK NONE O OTHER ININSP/MAINT 1 WP191188P448 2347 LAMINATED BEARING, WORN. REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20050404001132005040400113WP 2005 4 4 DHL2005805582 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBOARD FLANGE (2EA) MISDRILLED HOLES AT STA 1260.00 L-10R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-07-05, EO AST 050201 DATED 02-17-05. PERFORMED DETAIL VISUAL INSPECTION, NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO AST 050201, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050404001182005040400118WP 2005 4 4 DHL2005805602 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBOARD FLANGE (2EA) MISDRILLED HOLES AT STA 1160.000 L-12R TO L-13R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-07-05, EO AST050201 DATED 02-17-05. PERFORMED DETAIL VISUAL INSPECTION NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO AST050201, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050404001202005040400120WP 2005 4 4 DHL2005805626 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME (2EA) MISDRILLED HOLES AT STA 702.000 L-9L TO L-10L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 02-25-05 EO AST 050203 DATED 02-18-05. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. PERFORMED DETAIL VISUAL INSPECTION NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD5-4) IAW EO AST050203 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050404001212005040400121WP 2005 4 4 DHL2005805531 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT INBOARD FLANGE Z-FRAME HOLES (3EA) MISDRILLED STA 100.000 L-11L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-05-05, EO AST 050205 DATE 02-21-05. CLEANED, TREATED AND PRIMED (AREA) MISDRILLED HOLES IAW SRM 51-1-8B. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD5-6) IAW EO AST 050205, SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050404001282005040400128WP 2005 4 4 DHL2005805614 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT Z-FRAME INBOARD FLANGE HOLES (2EA) MISDRILLED STA 1140.000 L-9L L-10L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-05-05 EO AST 050205 DATE 02-21-05. CLEANED, TREATED AND PRIMED (AREA) MISDRILLED HOLES IAW SRM 51-1-8B. PERFORMED DETAILED VISUAL INSPECTION NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD5-4) IAW EO AST 050205 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050404001292005040400129WP 2005 4 4 DHL2005805617 120050320A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT (8EA) MISDRILLED HOLES IN L-12R (STA 600.000 - 620.000). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-15-05 EO AST 050216 DATED 03-02-05. PERFORMED DETAIL VISUAL INSPECTION, NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO AST 050216 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050404001302005040400130WP 2005 4 4 DHL2005805619 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT INBOARD FLANGE J-FRAME HOLES (2EA) MISDRILLED AT STA 960.000 L-10L. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 02-25-05 EO AST 050203 DATE 02-18-05. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. PERFORMED DETAILED VISUAL INSPECTION, NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO AST 050203, SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050404001322005040400132WP 2005 4 4 DHL2005805563 120050320A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME MISDRILLED HOLE AT STA 702.000 L-11L TO L-12L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 02-25-05, EO AST 050202 DATED 02-17-05. PERFORMED DETAIL VISUAL INSPECTION NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLE WITH RIVET (MS20470AD) IAW EO AST050202, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050404001332005040400133WP 2005 4 4 DHL2005805565 120050321A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT L-12L HOLES (8EA) MISDRILLED BETWEEN FRAME STA 520.000 AND FRAME STA 540.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-15-05 EO AST 050216 DATE 03-02-05. PERFORMED DETAILED VISUAL INSPECTION NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO AST 050216, SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050404001342005040400134WP 2005 4 4 DHL2005805568 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME (2EA) MISDRILLED HOLES AT STA 440.000 L-10L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-05-05 EO AST 050205 DATED 02-21-05. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA AT STA 440.000 L-10L IAW SRM 51-1-8B. PERFORMED DETAIL VISUAL INSPECTION NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD5-6) IAW EO AST050205, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050404001362005040400136WP 2005 4 4 DHL2005805539 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBOARD FLANGE (01EA) HOLE MISDRILLED STA 620.000 L-12.5R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-07-05 EO AST050201 DATE 02-17-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLE WITH RIVET (MS20470AD) IAW EO AST 050201, SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050404001372005040400137WP 2005 4 4 DHL2005805581 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBOARD FLANGE (2EA) MISDRILLED HOLES, STA 1420.000 L-12R TO L-13R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-07-05, EO AST 050201 DATED 02-17-05. PERFORMED DETAIL VISUAL INSPECTION NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO AST 050201, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050404001402005040400140WP 2005 4 4 DHL2005805529 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBOARD FLANGE HOLES (2EA) MISDRILLED AT STA 1340.000 L-12L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-05-05 EO AST050205 DATE 02-21-05. CLEANED, TREATED AND PRIMED (AREA) MISDRILLED HOLES IAW SRM 51-1-8B. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO AST050205 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050404001422005040400142EU 2005 4 4 F3LA200500014 120050322A2121EVT3454H FAN AIRBUSA319 A319112 3930323EU CABIN INOPERATIVE A F3LAO OTHER EB VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM03916FR8118 4311 1876 FLIGHT CREW REPORTED VENT EXTRACT FAULT. NOTICED AIRCRAFT VIBRATION, FRONT RIGHTSIDE, AND SMELL OF ELECTRICAL SMOKE FRONT TO BACK OF AIRCRAFT. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE VERIFIED VENT EXTRACT FAN FAILURE AS CAUSE OF ODOR PER TSM 24-00-00-810-823 AND PLACARD PER MEL 21-26-02A. UPON ARRIVAL IN DEN, REPLACED VENT EXTRACT FAN PER MM 21-26-51-000-001 AND 21-26-51-400-001. PERFORMED TEST OF SYSTEM VIA MCDU PER MM 21-26-00-710-001. 2L72 4F RTA28NM 20050404001462005040400146NM 2005 4 4 2005UALA00257 120050321A2613 OVERHEAT LOOP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE NR 2 ENGINE MALFUNCTIONED A UALAEA ENGINE SHUTDOWN UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 WP29341UA 24245 RETURNED TO ORD DUE TO NR 2 ENGINE OVERHEATED AND SHUTDOWN. CREW REPORTED NR 2 ENGINE OVERHEAT INDICATION AT CLIMB. CREW SHUT DOWN NR 2 ENGINE PER QRC. PERFORMED TROUBLESHOOTING OF THE OVERHEAT DETECTION SYSTEM. FOUND NR 2 ENGINE CORE DETECTOR M1122, LOOPS A & B WITH LOW RESISTANCE SHORT TO GROUND. REMOVED AND REPLACED OVERHEAT DETECTOR CORE LOOPS A & B. ENGINE OVERHEAT DETECTION SYSTEM TESTED NORMAL. 2L72 4F4 FRTA16WE E2GL 20050404001482005040400148NM 2005 4 4 05FDEA00635 120050325A5312 BULKHEAD BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25272FE 22037 LOWER CHORD OF BS 950 CANTED BULKHEAD IS CORRODED, RBL 23. REPLACED BS 950 LOWER CHORD PER SRM 51-40-3 & 51-30-2. 2L73 4F RTA3WE 20050404001502005040400150NE 2005 4 4 2005UALA00259 220050323A7510 VALVE BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE LT ENGINE STUCK A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29218UA 30222 LEFT ENG ANTI-ICE VALVE STUCK CLOSED. MAINTENANCE REPLACED LH ENGINE ANTI-ICE VALVE. OP CHECKED OK AFTER REACTIVATING VALVE. 2L72 4F4 FRTT0001SE E46NE 20050404001522005040400152EU 2005 4 4 2005UALA00261 120050325A3610 DUCT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE BLEED AIR DISCONNECTED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29404UA 450 LT WING LEAK DISPLAYED ON UPPER ECAM. FOUND DUCT DISCONNECTED AT GROUND BLEED AIR CONNECTOR. RECONNECTED DUCT. 2L72 4F4 FRTA28NM E40NE 20050404001532005040400153NM 2005 4 4 2005UALA00262 120050324A5230 SKIN BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE CARGO DOOR DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29937UA 26668 DENT ON FWD SIDE OF FWD CARGO DOOR, MEASURES 1.25 WIDE, .157 DEEP. MAJOR REPAIR ACCOMPLISHED. CAUSED BY CONTACT WITH LOADER. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20050404001552005040400155EU 2005 4 4 05FDEA00637 120050325A5730A57350005201 SKIN AIRBUS310 A310203 3930313EU ZONE 600 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25401FE 191 PANEL LAND AT 650HB HAS 9 EA ELONGATED HOLES. REPAIRED 5 EA HOLES IAW A310-200 SRM 51-40-44 FIG 1. COMPLIED WITH EA 6-5710-87184 BY INSTALLING 4 EA REPAIR BUSHINGS FOR REMAINING 4 HOLES. 2L72 4F RTA35EU 20050401001012005040100101EA 2005 4 1 A6WA200540121 120050319A57112024T3 SPAR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT WING MISDRILLED A A6WAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL31413AW 7585 DUE TO HOLES SPACING ON RT LOWER WING SPAR AT WS 148, JOINT STRAP 601R100465-4 S/B CANNOT BE INSTALLED IAW SB 601R-57-037. REPAIRED RT WING SPAR AT WS 148, SHIFTED CUTLINE ON T/E RT WING AT WS 148. FABRICATED A NEW DOUBLE JOINT STRAP OUT OF 2024-T3.050 PO NR 46952/7 IAW BRAS 601R-57-6125. (K) 2L72 4F4 FRTA21EA E15NE 20050404000112005040400011NE 2005 4 4 KBM2005F00011 220050203A7532 BLEED VALVE SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE ENGINE STICKING E KBMAK NONE O OTHER ININSP/MAINT 1 WP191188P 2347 BLEED VALVE STICKS, REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20050404000152005040400015EA 2005 4 4 O2G2005F00004 120050314A2497OCDB9A023 CONTACTOR CNDAIRCL600 CL6002B16 1900305EA GE CF34 CF34* NE FUSELAGE FAILED E O2GAA UNSCHED LANDING G MULTIPLE FAILURE CRCRUISE 1 NE03601VH4858 2532 5043 NR1 THRU FAILED INFLIGHT CAUSING LOSS OF NR 1 DC BUSS AND UTILITY BUSS. REPLACED THE NR 1 LINE CONTACTOR AND NR1 TRU. 2L72 4F4 FRTA21EA E15NE 20050404000222005040400022EA 2005 4 4 A6WA200540117 120050320A5743601R572100621 BUSHING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT MLG MIGRATED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31415AW 7593 RT MLG AFT TRUNNION BUSHING IS MIGRATED 0.15 INCH. REMOVED BUSHING, REAMED BARE AND INSTALLED 1ST OVERSIZE BUSHING IAW MFG REO. (K) 2L72 4F4 FRTA21EA E15NE 20050404000872005040400087NE 2005 4 4 GAIA05013OP 220050303A7200C25455 AIR CLEANER BOEING727 727214 138407RNM PWA JT8 JT8D9 52048NE NR 1 ENGINE CRACKED A GAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07750US 21512 DURING CLIMBOUT THE LOWER AFT BODY OVERHEAT LIGHT CAME ON. THE AC RETURNED TO AIRPORT AND AN UNEVENTFUL LANDING WAS MADE. REMOVED AND REPLACED THE NR 1 ENGINE AIR CLEANER DUE TO CRACKED FLANGES. LEAK CHECK AND OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (SW07200503890) (K) 2L73 4F4 F A3WE E2EA 20050404000982005040400098 2005 4 4 KBM2005F00046 420050321A3422103002201 GYRO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE DIRECTIONAL MALFUNCTIONED E KBMAK NONE O OTHER ININSP/MAINT 1 WP19345SH226 3345 TUMBLES IN FLIGHT. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050404001062005040400106NM 2005 4 4 USAA050356 120050218A5340 ATTACH ANGLE BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19438US40959 24560 PIT - Q4 - ATTACH ANGLE, 1 INCH X 2 INCH WEAR AREA, BS 1288 AT S2R. FABRICATED NEW ANGLE IAW TYP REP 53-20-05A. (K) 2L72 4F4 FRTA16WE E21EU 20050404001092005040400109NM 2005 4 4 USAA050352 120050203A575465C26602224 SKIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU NR 5 SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19436US41648 24558 PIT - C5 - SLAT, 3 INCH LONG X 2.5 INCH WIDE - 2 AREAS, DELAMINATION. NR 5 SLAT TOP SURFACE IB AND OB T/E. INSTALED NEW CORE, TOP DOUBLERS, SEAL AND REFINISH IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050404001142005040400114WP 2005 4 4 DHL2005805613 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBOARD FLANGE (2EA) MISDRILLED HOLES STA 1320.000 L-13L L-12L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-05-05 EO AST 050205 DATED 02-21-05. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA AT STA 1320.000 L-12L IAW SRM 51-1-8B. PERFORMED DETAIL VISUAL INSPECTION NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO AST050205 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050404001232005040400123WP 2005 4 4 DHL2005805567 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME (2EA) MISDRILLED HOLES AT STA 540.000 L-12L TO L-13L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-05-05, EO AST 050205 DATED 02-21-05. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA AT STA 540.000 L-12L TO L-13L IAW SRM 51-1-8B. PERFORMED DETAIL VISUAL INSPECTTION NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD6-5) IAW EO AST 050205 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050404001262005040400126WP 2005 4 4 DHL2005805564 120050320A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME MISDRILLED HOLE AT STA 702.000 L-12L TO L-13L 1EA (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 02-25-05, EO AST 050202 DATED 02-17-05. PERFORMED DETAIL VISUAL INSPECTION NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLE WITH RIVET (MS20470AD) IAW EO AST050202, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050404001312005040400131WP 2005 4 4 DHL2005805623 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT Z-FRAME INBOARD FLANGE HOLES (2EA) MISDRILLED AT STA 1020.000 L-12 L-13L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-05-05 EO AST 050205 DATE 02-21-05. CLEANED, TREATED AND PRIMED AREA (MISDRILLED HOLES) IAW SRM 51-1-8B. PERFORMED DETAILED VISUAL INSPECTION NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD6-4) IAW EO AST 050205 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050404001432005040400143EU 2005 4 4 2005UALA00254 120050318A4990 SEPARATOR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE APU OIL SYSTEM WORN A UALAA UNSCHED LANDING KH FLUID LOSS ELECT. POWER LOSS-50 PC CRCRUISE 1 WP29442UA 780 AUTO SHUTDOWN OF APU WITH NR 2 ENG DRIVEN GENERATOR ALREADY INOPERATIVE. CONFIRMED NO EXTERNAL OIL LEAKAGE. GEARBOX MODULE 756407J, S/N SP-G 970369 WAS PARTIALLY DISASSEMBLED FOR INSPECTION AND REPLACEMENT OF THE BEARING TABS AND AIR-OIL SEPARATOR SEAL. AIR-OIL SEPARATOR LIP SEAL WAS WORN, ALLOWING OIL TO BLOW BY. 2L72 4F4 FRTA28NM E40NE 20050404001452005040400145NM 2005 4 4 2005UALA00256 120050318A5330147W4350 SKIN BOEING777 777222 1385219NM PWA PW4077PW4077 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29778UA35305 26940 FUSELAGE SKIN IS DENTED JUST FWD OF FUSELAGE STA 2108 AT STR 24R. *S/D* EXISTING DENT RE-EVALUATED AND REPAIRED AT BS 2108, STR 24R. REPAIR WAS ACCOMPLISHED BY UA-EVA-50137. 2L72 4F4 FRTT0001SE E46NE 20050404001542005040400154EU 2005 4 4 U30A200500002 120050312A2910D2901005201300 PIPE AIRBUS320 A320214 3930316EU ZONE 413 LEAKING A U30AA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA17264AV7663 7663 1867 CREW RECEIVED AN ECAM MESSAGE, GREEN HYD LOW PRESS. TURNED OFF PUMP & PTU. STATUS PG INDICATED LOW PRESS & NIL QTY. DIVERTED, DECLARED AN EMERGENCY. ECAM GENERATED APPROACH LIST INSTRUCTS TO TURN PTU BACK ON TO TRY TO RESTORE PRESSURE, PRESSURE RESTORED. CANCELED THE EMERGENCY. FLT CREW ELECTED TO MAKE AN OVERWEIGHT LANDING & LANDED AT LESS THAN 50 FPM VERTICAL SPEED. MAINTENANCE REPLACED A LEAKING (PINHOLE) GREEN HYD RETURN LINE IN THE NR 1 ENGINE PYLON. SERVICED THE GREEN HYD SYSTEM PER AMM 12-12-00, LEAK CK'D AND OP'S CK'D THE GREEN HYD SYSTEM OK PER AMM 29-11-06. THE OVERWEIGHT LANDING WAS FOUND TO BE WITHIN ALLOWABLE LIMITS PER AMM 05-51-11. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA28NM 20050404001642005040400164NM 2005 4 4 05FDEA00660 120050326A2612 WARNING LIGHT BOEING727 727200 138407ENM CARGO BAY SMOKE ILLUMINATED A FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25258FE 20940 LOWER CARGO SMOKE LIGHT ILLUMINATED ON T/O AT 70 KTS, RTO NO OTHER INDICATIONS LIGHT WENT OUT DURING DECELERATION. RELEASED FOR SERVICE PER MEL/CDL: 26-19-A CATEGORY: C EXPIRATION: 05APR05 MEL 26-19-A: SMOKE DETECTION IN THE FWD LOWER CARGO COMPARTMENT INOP. OHMED AND MEGGED WIRING TO THE FWD LIGHT L9109 TO THE CONTROL PANEL REF 727-200 WDM 26-23-00, ALL CKS GOOD. CHECKED THE LIGHT SOCKET, CHECKS GOOD. REMOVED AND REPLACED CSCP, OPS CKS GOOD PER 727-200 M/M 26-17-001-5. OK FOR SERVICE. 2L73 4F RTA3WE 20050404001672005040400167NM 2005 4 4 05FDEA00645 120050325A5347FXSEATRACK03 SEAT TRACK BOEING727 727200 138407ENM MAIN CABIN CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25271FE 22036 SEAT TRACK STA 344-480 RBL 45 IS CORRODED AND REQUIRES REPLACEMENT PER EO 7-5340-7- 5002. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2. 2L73 4F RTA3WE 20050404001752005040400175NM 2005 4 4 AWXA200500374 120050321A5730654783852 SKIN BOEING737 7373G7 1384595NM RT WING CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 MCN - MAJOR REPAIR - DURING C-16 CHECK A .375 INCH CRACK WAS FOUND IN PREVIOUS REPAIR OF RT WING SKIN AT INBOARD MID FLAP LEADING EDGE CUTOUT FOR FORE FLAP CONTROL ROD RS 176.0. MAINTENANCE REMOVED PREVIOUS REPAIR OF RT WING SKIN AT RS 176.0; FABRICATED A NEW SECTION OF REPLACEMENT SKIN AND REPAIR SPLICE PLATE; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-53-01 FIG 202. 2L72 4F RTA16WE 20050404001812005040400181CE 2005 4 4 DXTA200500628 120050312A3260 UPLOCK SWITCH CESSNA750 750 2076810CE MLG OUT OF ADJUST E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07936QS 7500036 UPON GEAR RETRACTION, HEARD THUMP GEAR UNLOCK LIGHT WOULD NOT EXTINGUISH. FOUND NOSE LANDING GEAR UPLOCK SWITCH OUT OF ADJUSTMENT. ADJUSTED NLG UPLOCK SWITCH IAW CE 750 MM 32-30-05. OPS CHECK GOOD IAW CE 750 MM CH 32-00-01. 2L72 4J RTT00007WI 20050404001842005040400184SO 2005 4 4 SWIA200514768 120050207A5340 FITTING EMB 120 EMB120ER 3260203SO FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0758733 120197 RIGHT SIDE FIN TO FUSELAGE FITTING IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. FIN TO FUSE ANGLE REPAIRED IAW EMB 120 SB 120-53-0074 & EMBRAER EST-504/96. 2L72 4T RTA31SO 20050404001862005040400186NM 2005 4 4 SWAA050740 120050310A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, BELOW STR 12R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050405000042005040500004WP 2005 4 5 ASAA0580098 120050215A53305936667501 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02943AS 53018 OKC - DURING C-CHECK, FOUND FUSELAGE SKIN DENTED. RECONTOURED DENTED DAMAGED AREA. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050405000052005040500005EU 2005 4 5 ASOA05192 120050205A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27633AS 344 DURING A C-CHECK IN YUL, THE INBOARD AND OUTBOARD SEAT TRACKS BETWEEN FRAME 28-29 RT WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE INBOARD AND OUTBOARD SEAT TRACKS BETWEEN FRAME 28-29 RT IAW SRM 53-00-00 FIG 434. (M) 2H72 4T RTA53EU 20050405000062005040500006EA 2005 4 5 ASOA05207 120050304A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27880AS 7606 DURING A C-CHECK IN MCN, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW ASA EO 600-53-0072B. (M) 2L72 4F RTA21EA 20050405000082005040500008WP 2005 4 5 ASAA0580115 120050226A532199365051 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 OKC - HV-CHECK, FOUND CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050405000472005040500047WP 2005 4 5 ASAA0580072 120050131A571299374639 RIB DOUG DC9 DC983 3022083WP RT WING CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - DURING C-CHECK, FOUND RIGHT WING LEADING EDGE RIB CRACKED. REPLACED DAMAGE. INSTALLED REPAIR ANGLE, SHIM, RADIUS, AND FILLER. (M) 2L72 4F RTA6WE 20050405000492005040500049WP 2005 4 5 ASAA0580050 120050131A532199365831 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - DURING C-CHECK, PAX CABIN FLOOR PANEL IS PUNCTURED AT TWO LOCATIONS. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050405000552005040500055WP 2005 4 5 ASAA0580063 120050131A5320993053857 WEB DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - DURING C-CHECK, LONGERON CUSP WEB CRACKED IN FORWARD CARGO BAY. REPLACED CUSP WEB. (M) 2L72 4F RTA6WE 20050405000792005040500079WP 2005 4 5 ASAA0580055 120050131A532199365821 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE BROKEN A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - DURING C-CHECK, PAX CABIN FLOOR PANEL HAS BROKEN INSERTS. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050405000902005040500090WP 2005 4 5 ASAA0580116 120050226A53219936651515 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 OKC - HV-CHECK, FOUND CABIN FLOOR PANEL IS WATER DAMAGED AND HAS CORRODED FASTENERS. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050405000972005040500097WP 2005 4 5 ASAA0580066 120050131A5320993053812 CUSP WEB DOUG DC9 DC983 3022083WP FUSLEAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - DURING C-CHECK, FOUND LONGERON CUSP WEB CORRODED IN MID CARGO BAY. REMOVED DAMAGED. INSTALLED FILLER AND REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050405001132005040500113EA 2005 4 5 QXEA200500467 120050307A5240 HANDLE CNDAIRCL600 CL6002C10 1390015EA ZONE 800 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - SERVICE DOOR INNER HANDLE HOUSING IS CRACKED. REPAIRED IAW CRJ700 SRM 52-41-00-801-A01, SRM 51-41-21-001-001-A01 AND SRM 52-41-00-710-801-A01. 2L72 4F RTA21EA 20050405001212005040500121EA 2005 4 5 VTZA200500026 120050328A5346601R536066 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA LT ENGINE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27657BR 7491 LT ENGINE SUPPORT BEAM IS CRACKED IN LOWER WEB AT .75 INCH. 2L72 4F RTA21EA 20050405001342005040500134EA 2005 4 5 QXEA200500460 120050310A5510 HINGE PIN CNDAIRCL600 CL6002C10 1390015EA ZONE 300 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - VERTICAL STABILIZER HINGE PIN FOR HORIZONTAL STABILIZER HAS EVIDENCE OF CORROSION COMING FROM BEARINGS. REPAIRED IAW REO 670-55-11-021 AND CRJ700 SRM 51-21-16. 2L72 4F RTA21EA 20050405001352005040500135EA 2005 4 5 QXEA200500458 120050304A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - LEFT HAND INBOARD SEAT RAIL AT STATION X663 HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01 AND HORIZON AIR EA R-53-083. 2L72 4F RTA21EA 20050405001542005040500154EU 2005 4 5 05FDEA00626 120050321A5315 FLOORBEAM AIRBUS310 A310 EU FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 FR 38 MDCC FLOORBEAM LT OF CTR AT 38 INCHES, AFTER REMOVAL OF CLS ADAPTER TO FACILITATE FRAME REPAIR, FASTENER HOLES FOUND TO BE OUT OF ROUND, FWD INBOARD HOLE ON CLS ADAPTOR AFT OUTBD, AND ALSO 2 DRILL STARTS. BLENDED OUT DRILL STARTS PER A310 SRM 51-73-10, NDT FOR CRACKS NONE FOUND PER A310 NTM 51-10-08, MEASURED DEPTH FOUND A .019 LOSS AND WITHIN LIMITS PER A310 SRM 53-10-15 FIG 101 SHEET 2, DRILLED 2 EA HOLES TO 2ND OVER 1/4 INCH HILOCKS AND ALL OTHER HOLE DRILLED TO .247 NOMENIAL 1/4" HILOCK IN CONJUCTION WITH N00681 FLOORBEAM REPAIR AND CLS ADAPTER REMOVAL AND REPLACEMENT PER A310 SRM SUPPLEMENT 53-10-15 FIG 201 SHEET 6A. 2L72 4F RTA35EU 20050405001662005040500166NM 2005 4 5 AALA20050229 120050329A3350PBS73 BATTERY PACK BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21378AN 25447 LAX - SEAT MOUNTED EMERGENCY LIGHTS AT SEATS 20 AND 21HJ INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS AT SEATS 20 AND 21HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050405001692005040500169WP 2005 4 5 AALA20050224 120050328A323039567851 LINK DOUG DC9 DC982 3022082WP MLG INOPERATIVE A AALAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SW21203AA 49145 STL INFLIGHT T1245/28MAR - AFTER TAKEOFF AND GEAR HANDLE RAISED AIRCRAFT BEGAN VIBRATING TOWARD NOSE AND BELOW OUR FEET. CYCLED GEAR DOWN. VIBRATION REDUCED BUT CONTINUED. RETURNED TO STL AND LANDED WITHOUT INCIDENT. REPLACED RIGHT NOSE GEAR DOOR ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050405001702005040500170NM 2005 4 5 AALA20050223 120050328A33970201875001 WIRE HARNESS BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21967AN 29545 LGA - EMERGENCY LIGHT AT SEATS 19DEF INOPERATIVE. REPLACED SEAT HARNESS AT 19DEF FOR EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20050405001902005040500190NM 2005 4 5 UPS05444209 120050313A534769B620491 CARGO TRACK BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 M/DECK BS 1940 AND 1960 LBL 80 INCH TIE DOWN FTG ATT PLATE FOUND CORRODED. CORROSION BLEND OUT 0.020 INCH BY 1 INCH BY 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT, M/D BS 1940 LBL 80 INCH TIE DOWN FTG REPLACED AS PER MM 20-51-01. 2L74 4F A20WE 20050405001962005040500196EU 2005 4 5 05FDEA00740 120050331A5410A5451526850600 GUSSET AIRBUS310 A310 EU ZONE 400 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 NR 1 PYLON OUTBD SIDE AT RIB 15 ANGLE HAS 3 SQ INCHES OF CORROSION. REMOVED AND REPLACED GUSSET IAW A310200 SRM 51-72-10. 2L72 4F RTA35EU 20050405002052005040500205NE 2005 4 5 MASA200500056 220050124A73214147T70P01 FUEL CONTROL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 2 ENGINE CONTAMINATED A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0727172137828004 7172 872268 ASH 9432 CLT TO CLT, RETURNED TO THE FIELD FOR THE NR 2 HYDRAULIC SYSTEM LOW PRESSURE AND QUANTITY. MX FOUND EVIDENCE OF HYD FLUID IN THE LT WING FUEL SYSTEM. MX TOOK FLUID SAMPLES FROM E1 AND E2 FUEL FILTER. FOUND DAMAGED LINE IN RT TANK. MX COULD NOT REPAIR REC'D TUBE ASSY FROM BOMBA. FUEL SAMPLE RESULTS WERE BEYOND ALLOWABLE LIMITS. NR 2 ENGINE FUEL CONTROL AND FUEL PUMP WERE CHANGED. FUEL PUMP P/N 6078T39P04 S/N REMOVED CGWT0595 (TT-21042 TC-17580 TSO-5546 CSO-2351 MFGR- GE). 2L72 4F4 FRTA21EA E15NE 20050406000042005040600004NM 2005 4 6 DHL2005782502 120050310A5330 SKIN BOEING727 727227 1384078NM DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 CREASE L/SIDE FUSELAGE SKIN STA 1148 STR 26L. REMOVED INTERCOSTAL IAW B727 SRM 51-30-2 CUT OUT DAMAGED AREA IAW B727 SRM 53-30-3 FIG 24. FAB FILLER SIZE 2" BY 19/16 USING 2024 T3 .100" PO NR 9001576 STRUCTURAL FILLER USING 2024 T3 .063 INCH PO NR 9002039 SIZE 13 1/2" BY 7 3/4" DOUBLER 11 1/8" BY 11 5/8" USING 2024 T3 .125" PO NR 9001673 IAW B727 SRM 53-30-3 FIG 24. TREATED AND PRIMED PARTS IAW B727 SRM 51-10-2. REINSTALLED INTERCOSTAL IAW B727 SRM 53-30-2 2L73 4F A3WE 20050406000062005040600006NM 2005 4 6 DHL2005782539 120050314A5730 SKIN BOEING727 727227 1384078NM RT WING DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 DENT ON RT WING L/E ABOVE NR 5 KFLAP (MARKED). CUT OUT DAMAGED AREA DIMENSIONS 1 1/2" BY 1/2" AND FABRICATED REPAIR DOUBLER MATERIAL USE 2024 T3 0.080 PO NR 9002012 DIMENSIONS 5 1/4" BY 5 1/4" IAW B727 SRM=57-30-4 FIG NR 1, PARTS TREATED AND PRIMED IAW B727 SRM=51-10-2. INSTALLED NEW DOUBLER IAW B727 SRM=57-30-4 FIG NR 1 SUBSTITUTED 2024 T3 FOR 2024 T4 IAW B727 SRM=51-20-1 FIG NR 2. 2L73 4F A3WE 20050406000112005040600011NM 2005 4 6 05FDEA00736 120050331A5322 SUPPORT BOEING727 727233 138408ANM SKIN CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25272FE 22037 LWR FUSELAGE, BS 740 R A/C BAY RBL 10, CORROSION EMANATING FROM LWR CHORD AND BULKHEAD. REPAIRED BS470 LOWER CHORD PER FED-EX EA 7-5310-86268. 2L73 4F RTA3WE 20050406000132005040600013NM 2005 4 6 05FDEA00723 120050331A5320ABA7681503 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 MAIN DECK, SEAT TRACK RBL 107 CORRODED AT STA 435. REMOVED AND REPLACED IAW SRM 51-33-01 VOLUME II. 2L73 4F RTA22WE 20050406000152005040600015NM 2005 4 6 UPS05444213 120050311A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 BS 2180 STR 25R FRAME FOUND CRACKED, CRACK LENGTH 1 INCH. FRAME REPAIRED AT BS 2180 STR 25R AREA AS PER HX RS R-53-62-35275 AND UPS EO B747-5310-21972A. 2L74 4F A20WE 20050406000172005040600017EA 2005 4 6 QXEA200500477 120050306A5730 ACCESS PANEL CNDAIRCL600 CL6002C10 1390015EA ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - LEFT HAND WING, FUEL PANEL 551BB REBATE IS CORRODED. REPAIRED IAW REO 670-57-00-010, CRJ700 SRM 51-24-11-001-001-A01, AND HORIZON AIR EA R-57-96. 2L72 4F RTA21EA 20050406000272005040600027NM 2005 4 6 72300068 120050114A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 GOUGED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 .1875 INCH DIAMETER GOUGE ON LOWER FLANGE OF SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050406000282005040600028NM 2005 4 6 72300069 120050205A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 1 INCH BY 4 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050406000422005040600042EA 2005 4 6 QXEA200500516 120050228A5320 FLOOR SUPPORT CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - FUSELAGE INTERIOR COCKPIT FLOOR SUPPORT ANGLE IS CORRODED AT FS 280. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01 AND SRM 51-23-00-001-001-A01. 2L72 4F RTA21EA 20050406000432005040600043EA 2005 4 6 QXEA200500479 120050306A5730 ACCESS PANEL CNDAIRCL600 CL6002C10 1390015EA ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - LEFT HAND, FUEL PANEL 551EB REBATE IS CORRODED. REPAIRED IAW CRJ700 SRM 51-24-11-001-001-A01, REO 670-57-00-010, AND HORIZON AIR EA R-57-96. 2L72 4F RTA21EA 20050406000442005040600044EA 2005 4 6 QXEA200500478 120050306A5730 ACCESS PANEL CNDAIRCL600 CL6002C10 1390015EA ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - LEFT HAND, FUEL PANEL 55100 REBATE IS CORRODED. REPAIRED IAW REO 670-57-00-010, CRJ700 SRM 51-24-11-001-001-A01, AND HORIZON AIR EA R-57-96. 2L72 4F RTA21EA 20050406000452005040600045EA 2005 4 6 QXEA200500480 120050303A5730 ACCESS PANEL CNDAIRCL600 CL6002C10 1390015EA ZONE 600 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - RIGHT HAND LOWER WING LEADING EDGE ACCESS PANEL 622DB FORWARD SECTION, SKIN HAS A SCRATCH AND CHAFE MARK. REPAIRED IAW CRJ700 SRM 57-41-01-101-001-A01, SRM 51-12-00-001-001-A01, AND SRM 51-25-16-001-001-A01. 2L72 4F RTA21EA 20050406000482005040600048EA 2005 4 6 QXEA200500468 120050303A5230 RETAINER CNDAIRCL600 CL6002C10 1390015EA ZONE 800 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - FORWARD CARGO DOOR SEAL RETAINER IS GOUGED AND BENT AT TWO CORNERS. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01 AND SRM 52-35-07-400-802-A01. 2L72 4F RTA21EA 20050406000492005040600049NM 2005 4 6 SB05041 120050329A335020121 CHARGER BOEING737 7374B7 1384702NM R1 DOOR INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19780AU 24997 CLT - FOUND FORWARD SERVICE DOOR EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REPLACED THE CHARGER AND BATTERY. 2L72 4F RTA16WE 20050406000512005040600051NM 2005 4 6 72300071 120050117A5322 ANGLE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 1 INCH BY 3 INCH AREA OF CORROSION ON REINFORCEMENT ANGLE. 2L73 4F4 FRTA3WE E2EA 20050406000532005040600053NM 2005 4 6 05FDEA00712 120050330A5347 CARGO TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25583FE 48421 MAIN DECK CARGO COMPARTMENT FLOOR TRACK AT STA 635, WL 47, FOUND WORN AT CROWN AREA. REPAIR TRACK AND SPLICE FABRICATED AS PER SRM 53-70-00 VOL I, FIG 1 & INSTALLED PER SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20050406000542005040600054NM 2005 4 6 05FDEA00713 120050330A5347 CARGO TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 MAIN DECK CARGO COMPARTMENT FLOOR TRACK AT STA 635, WL 8.5, FOUND CRACKED APPROXIMATELY 3 INCHES LONG. REPAIR TRACK AND SPLICE FABRICATED AS PER SRM 53-70-00 VOL I, FIG 1 & INSTALLED PER SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20050406000562005040600056NM 2005 4 6 QXEA200500523 120050330A27207G773 SWITCH DHAV DHC8 DHC8202 2809007NM ZONE 200 INOPERATIVE A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09357PH150 504 FLT NUMBER 2118, RETURNED TO FIELD. RUDDER FULL PRESSURE CAUTION ON TAKEOFF, NO OTHER CAUTION LIGHT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED RUD FULL PRESS SWITCHES. PERFORMED OPERATIONAL CHECK AND LEAK CHECK, ALL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050406000572005040600057EU 2005 4 6 05FDEA00737 120050331A5414 ACCESS PANEL AIRBUS310 A310 EU ZONE 400 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 NR 2 PYLON ACCESS PANEL NR 423EL HAS MODERATE CORROSION AROUND INTERIOR SIDE OF ALL FASTENER HOLES. REMOVED CORROSION IAW A310-200 SRM 51-74-10, VERIFIED THREE AREAS OUT OF LIMITS. VERIFIED REPAIR MATERIAL, FABBED THREE EA. REPAIR DOUBLERS AND FILLERS IAW A310-200 SRM 54- 52-51. CUT OUT DAMAGED AREAS IAW A310-200 SRM 54-52-51. APPLIED PROTECTIVE TREATMENT TO FABBED PARTS AND ACCESS PANEL IAW A310-200 SRM 51-21-10. INSTALLED THREE EACH REPAIR DOUBLER AND FILLERS IAW A310-200 SRM 54-52-51. 2L72 4F RTA35EU 20050406000592005040600059NM 2005 4 6 05FDEA00818 120050404A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT UPPER AFT SKIN PLANK NR 28L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82941. 2L73 4F RTA22WE 20050406000602005040600060NM 2005 4 6 05FDEA00819 120050404A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT UPPER FORWARD SKIN PLANK NR 3R BARREL NUT BORE FOUND EXCEEDED LIMITS. REWORK/REPAIR - 1-5510-7-5000 HAS BEEN COMPLIED WITH. 2L73 4F RTA22WE 20050406000612005040600061CE 2005 4 6 4519203142005 120050314A21306621000000073 VALVE LEAR 45 45LEAR 5170805CE CABIN PRESSURE MALFUNCTIONED E J7SAA UNSCHED LANDING BMJSMOKE/FUMES/ODORS/SPARKS OVER TEMP WARNING INDICATION CLCLIMB 1 SW05433FX 192 SMOKE IN CABIN AND COCKPIT WITH HIGH HEAT ALSO AN AMBER CABIN DUCT OVERHEAT CAS MESSAGE ILLUMINATED. CREW REPORTED IN A CLIMB AMBER ICAS (CAB DUCT OVHT) CAME UP. CREW REPORTED CABIN TEMP WAS SHOWING 91F. CREW SELECTED MANUAL TEMP CONTROL AND NO CHANGE. THE CABIN TEMP CONT CARROT RED X'ED. CREW REPORTED SMOKE STARTED TO COME INTO CABIN. AIRCRAFT RETURNED TO THE AIRPORT. CREW NOTICED NOW THE COCKPIT CONT CARROT RED X'ED AND CABIN CARROT WAS BACK NOW ON THE ICAS. FIRE DEPARTMENT MEASURED CABIN TEMP AND FOUND 114F AFTER THE DOOR HAD BEEN OPEN FOR SOME TIME. EMERGENCY PRESSURIZATION VALVES ARE NOT OPENING. REPLACED LT HIGH PRESSURE VALVE AND ECS CONTROLLER AND CABIN TEMP CONTROL VALVE. OPS CHECK NORMAL 2L72 4F RTT00008WI 20050406000622005040600062NM 2005 4 6 72300072 120050131A5311 FRAME BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 APPROX 2 INCH BY 3 INCH AREA OF CORROSION ON FRAME. 2L73 4F4 FRTA3WE E2EA 20050406000632005040600063NM 2005 4 6 72300073 120050117A5311 FRAME BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 1 INCH BY 3 INCH AREA OF CORROSION ON LOWER FRAME ANGLE. 2L73 4F4 FRTA3WE E2EA 20050406000712005040600071EU 2005 4 6 0500363232 120050321A2120 ODOR AIRBUS320 A320211 3930320EU CABIN DETECTED A NWAAG O2 MASK DEPLOYED B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 GL01332NW 319 DURING DESCENT INTO MEM, EXPERIENCED BURNING ODOR AND OBSERVED WHITE SMOKE IN COCKPIT. DECLARED AN EMERGENCY AND PROCEEDED TO MEM AND LANDED UNEVENTFULLY. INSPECTED ALL AVIONICS BAYS AND BEHIND CIRCUIT BREAKER PANELS, OVENS, AND COFFEEMAKERS WITH NO PROBLEMS FOUND AND NO ODOR PRESENT. RAN BOTH PACKS WITH NO SMOKE NOTED. PERFORMED TEST FLIGHT WITH NO SMOKE OR ODOR PRESENT. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA28NM 20050406000752005040600075EU 2005 4 6 05FDEA00741 120050331A5320A5461139920000 STRAP AIRBUS310 A310 EU ZONE 400 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 NR 1 PYLON OUTBD SIDE FWD OF PRECOOLER STRAP IS CRACKED. REMOVED AND REPLACED ANGLE IAW A310-200 SRM 51-72-10. 2L72 4F RTA35EU 20050406000822005040600082SW 2005 4 6 ALGA098989 120050112A6710406310405101 PITCH LINK BELL 407 407 1182206SW MAIN ROTOR WORN B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03404AL140 53479 SEVERE BINDING AND AXIAL PLAY BEYOND MAX. REPLACED BY FIELD MAINTENANCE. 1G71 3U O H2SW 20050406000842005040600084WP 2005 4 6 DHL2005802002 120050311A3297 WIRE DOUG DC8 DC873 302199CWP LT MLG DOOR BROKEN A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01802DH 46076 ON CLIMB OUT LEFT DOOR UNSAFE LIGHT ILLUMINATED. RAN APPROPRIATE PROCEDURE. AFTER PROCEDURE, LEFT AND RIGHT DOOR UNSAFE LIGHTS ILLUMINATED. FOUND BROKEN WIRE AT THE LEFT GEAR DOOR UP SWITCH, REPAIRED SAME ALSO FOUND CONNECTOR FULL OF DEICING FLUID CLEANED. SYSTEM CKD NORMAL IAW 32-60-0. 2L74 4F RT4A25 20050406000852005040600085NM 2005 4 6 TSAA0549007 120050204A492038007021 APU BOEING737 73776N 13844CHNM APU BAY DEFECTIVE A TSAAE ENGINE SHUTDOWN E VIBRATION/BUFFET CRCRUISE 1 WP13748AL 30050 FLT 446, HNL-LAS: APU EGT SPIKE 660 DEGREES THEN FLUCTUATING AT CRUISE; FLT ATTENDANT REPORTED LOW RUMBLING SOUND; APU CPS FREQ BLANK; AMPS=0, VOLTS=1. SHUTDOWN APU; FLIGHT ATTENDANT REPORTED RUMBLING SOUND STOPPED. DIVERTED TO OAK, UNEVENTFUL LANDING. REPLACED APU PER 737-700 MM 49-11-00-4 AND TASK 49-11-00-400-802. NO FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO VIBRATION NOTED ON SUBSEQUENT FLIGHT VERIFICATION. 2L72 4F RTA16WE 20050406000882005040600088NM 2005 4 6 QXEA200500227 120050217A3350 WIRE DHAV DHC8 DHC8202 2809007NM ZONE 200 EXPOSED A QXEAO OTHER O OTHER CRCRUISE 1 NM09056PH 502 SEA - ON FLIGHT 2042, EMERGENCY TRACK LIGHT WIRES EXPOSED AT ROW 1. MAINTENANCE REMOVED AND REPLACED FORWARD FLOOR TRACK LIGHTING. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050406000902005040600090NM 2005 4 6 P9RA20050072 120050315A3350S417N50918MI LIGHT BOEING757 757236 1384971NM AFT CABIN BURNED OUT A P9RAK NONE L NO TEST ININSP/MAINT 1 SO11958PG 24118 AIRCRAFT IN MAINTENANCE FLOOR EMERGENCY TRACK LIGHTS AFT CABIN INOPERATIVE. REPLACED FLOOR TRACK LIGHT ASSY PER MM. 2L72 4F RTA2NM 20050406000922005040600092NM 2005 4 6 P9RA20050073 120050316A33503071BPEGPL BULB BOEING757 757236 1384971NM EMERGENCY LIGHT BURNED OUT A P9RAK NONE L NO TEST ININSP/MAINT 1 SO11962PG 24119 AIRCRAFT IN MAINTENANCE, ROW 20 TO 23 EMERGENCY PATH LIGHTING INOPERATIVE. REPLACED BULBS PER MM. 2L72 4F RTA2NM 20050406000982005040600098NM 2005 4 6 05010 120050204A3600 DUCT BOEING747 7472B4B 138481BNM PWA JT9 JT9D7J 52054NE 8TH STAGE LOOSE A KCSAO OTHER MJ OVER TEMP WARNING INDICATION CRCRUISE 1 GL23713CK 21099 662450 AT FL 34.0, NR 2 ENG START VALVE LIGHT ILLUMINATED; FOLLOWED CHECKLIST. NR 2 THROTTLE SEIZED; RAN SEVERE DAMAGE CHECKLIST. ALL ENGINE INDICATIONS NORMAL. PERFORMED VISUAL INSPECTION TO ENGINE. FOUND 8TH STAGE BLEED DUCTS LOOSE AND START VALVE DAMAGED. INSTALLED SERVICEABLE 8TH STAGE DUCTS AND STARTER LEAK AND OP'S CHECK GOOD IAW B747 MM 71-00-00. 2L74 4F4 FRTA20WE E20EA 20050406001002005040600100NM 2005 4 6 72300001 120050202A5340 STRINGER CLIP BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 APPROX 1 INCH BY 2 INCH AREA OF CORROSION ON STRINGER SLIP. 2L73 4F4 FRTA3WE E2EA 20050406001092005040600109EU 2005 4 6 05FDEA00568 120050315A5410 RIB AIRBUS310 A310 EU NR 2 PYLON CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25419FE 345 NR 2 PYLON OTBD SIDE RIB 16A UPPER AREA BRACKET LWR AREA HAS AN AREA OF CORROSION EXTENDING UNDER FASTENERS. REMOVED AND REPLACED BRACKET IAW A310-200 SRM 51-72-10. REINSTALLED 3 NUTPLATES IAW A310 SRM 51-40-21. (SEE JPF) 2L72 4F RTA35EU 20050406001122005040600112EU 2005 4 6 ALGA099803 120050307A6230C622A1003102 SWASHPLATE UROCOPEC120 EC120B 8680987EU MAIN ROTOR DEBONDED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03512AL255 1148 DEBONDED, REPLACED WITH NEW PART IN FIELD. 1G72 3U NCR0001RD 20050406001152005040600115 2005 4 6 SA05035 420050328A2565 STRAP AIRBUSA319 A319112 3930323EU GIRT BAR LOOSE A USAAO OTHER J WARNING INDICATION CLCLIMB 1 EA19723UW 1109 MSP - FLT 910 EN ROUTE CLT TO MSP, AFTER TAKEOFF, THE AFT RIGHT DOOR SLIDE DISARM INDICATION CAME ON ECAM. THE CABIN CREW FOUND THAT THE SLIDE ARM HANDLE HAD COME OUT OF DETENT, AND WOULD NOT STAY DOWN. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE DOOR SLIDE GIRT BAR STRAP WAS LOOSE AND INTERFERING WITH THE ARMING DETENT. THE STRAP WAS SECURED. AN OPERATIONAL CHECK WAS PERFORMED ON ALL DOORS. ALL DOORS WERE FOUND OK. 2L72 4F RTA28NM 20050406001192005040600119NM 2005 4 6 ASAA0540031 120050118A5350654865790 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU RT FAIRING DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02755AS 25096 PAE - RT AFT WING -TO-BODY FAIRING FORMER HOLES ELONGATED. REMOVED AND INSTALLED NEW T-ANGLE IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050406001202005040600120NM 2005 4 6 ASAA0510014 120050307A53306545800594 DOUBLER BOEING737 7372Q8C 138448SNM PWA JT8 JT8D17 52049NE FUSELAGE SCRATCHED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02741AS 21959 OKC - LT FUSELAGE EXTERNAL DOUBLER HAS DEEP SCRATCHES BELOW L-1 DOOR CUTOUT AT FS 314, S20L. (MARKED) REMOVED DAMAGED DOUBLER, FABRICATED AND INSTALLED A REPLACMENT DOUBLER IAW AS EA AND AAR EA. (K) 2L72 4F4 F A16WE E2EA 20050406001212005040600121NM 2005 4 6 ASAA0540028 120050112A5320146A70272 SUPPORT BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU CARGO BAY CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02755AS 25096 PAE - CORROSION AFT CARGO BAY, ON FLOOR TO SIDEWALL SUPPORT RT FROM BS 867-887. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT. (K) 2L72 4F4 FRTA16WE E21EU 20050406001232005040600123NM 2005 4 6 ASAA0540032 120050118A5312651630095 BULKHEAD BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02755AS 25096 PAE - BS 178 AFT PRESSURE BULKHEAD SKIN GOUGED AT LBL 25 WL 206. REPAIRED IAW EA AND ER. (K) 2L72 4F4 FRTA16WE E21EU 20050406001242005040600124NM 2005 4 6 ASAA0540130 120050211A53206551629U501 SEAL DEPRESSOR BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FWD GALLEY DOOR CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02713AS 28896 PAE - FWD GALLEY DOOR CUTOUT FWD SIDE SEAL DEPRESSOR CRACKED ABOVE UPPER HINGE CUTOUT. REMOVED AND REPLACED. (K) 2L72 4F4 FRTA16WE E21EU 20050406001252005040600125NM 2005 4 6 ASAA0540128 120050209A5320655384421 FLOOR SUPPORT BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02713AS 30161 PAE - FLOOR SUPPORT DAMAGED FROM PREVIOUS PANEL REPAIR. SPLICED IN REPAIR. (K) 2L72 4F4 FRTA16WE E21EU 20050406001272005040600127NM 2005 4 6 ASAA0540029 120050113A523069366792 STOP FITTING BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU CARGO DOOR GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02755AS 25096 PAE - AFT CARGO BAY FWD CTR DOOR STOP FITTING HAS MECHANICAL DAMAGE. REPLACED IAW SOPM. (K) 2L72 4F4 FRTA16WE E21EU 20050406001292005040600129NM 2005 4 6 ASAA0540121 120050206A532065C264594 FLOOR SUPPORT BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - CORROSION ON NR 1 FLOOR SUPPORT STRAP AT BS 727D + 5 INCHES. REMOVED AND REPLACED NR 1 FLOOR SUPPORT STRAP. (K) 2L72 4F4 FRTA16WE E21EU 20050406001302005040600130NM 2005 4 6 ASAA0540097 120050204A5322654655055 SHEAR TIE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - AFT CARGO BAY CORROSION ON SHEAR TIE (FRAME) STA 787. REPAIRED IAW SRM, SHEAR TIE AT B-STA 787, LBL 12.5, RBL 13.8, WI 146. (K) 2L72 4F4 FRTA16WE E21EU 20050406001312005040600131NM 2005 4 6 ASAA0540074 120050130A532065C311861 FINGER DOUBLER BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02756AS 25097 PAE - FINGER DOUBLER ON AFT EDGE OF AFT CARGO DOOR CUTOUT IS DAMAGED. REMOVED AND REPLACED FINGER DOUBLER ON AFT EDGE OF AFT CARGO DOOR CUTOUT. (K) 2L72 4F4 FRTA16WE E21EU 20050406001332005040600133NM 2005 4 6 ASAA0540138 120050218A53206552878119 WEB BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02791AS 28886 PAE - AFTER ACCESSED LT AFT ENTRY MOPSILL WEB FOUND CORRODED. BLENDED OUT OF LIMITS, FABRICATED AND INSTALLED NEW WEB BELOW MOPSILL LT AFT ENTRY. (K) 2L72 4F4 FRTA16WE E21EU 20050406001392005040600139NM 2005 4 6 ASAA0510001 120050128A29106544510 HYDRAULIC LINE BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE HYDRAULIC SYS CRACKED A ASAAK NONE J WARNING INDICATION APAPPROACH 1 NM02730AS 22577 SEA - WHILE EXTENDING FLAPS TO NR5 POSITION, HYDRAULIC LOW-PRESSURE LIGHTS ILLUMINATED. QUANTITY WENT TO ZERO. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED (A) SYSTEM HYDRAULIC PRESSURE LINE. ACCOMPLISHED CONDITIONAL INSPECTIONS. RETURNED TO SERVICE. (K) 2L72 4F4 F A16WE E2EA 20050406001402005040600140NM 2005 4 6 ASAA0540142 120050223A2424948F4583 GCU BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU E/E BAY MALFUNCTIONED A ASAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 NM02774AS4385 385 25107 SEA - ATB SMOKE IN FLIGHT DECK THROUGH 1000 FT. COMING FROM G4 AND G5 AREA, BEHIND F/O AREA. TROUBLESHOT NR 2 ENG GCU. INSPECTED AREA NEAR P-6 C/B PANELS, EE COMPARTMENT, AND NR 2 ENGINE GENERATOR. REPLACED NR 2 GCU. ENGINE RUN, OPS CHECK NORMAL. GCU RECEIVED UNSERVICEABLE. INSP SHOWED INTERNAL PWR SUPPLY CIRCUIT OVERHEATED AND TRANSFORMER T901 AND DIODE CR909 HAD OVERHEATED AND BURNED. TRANSFORMER AND DIODES TO BE REPLACED. UNIT REQUIRES COMPLETE CLEANING TO REMOVE BURNED COMPONENTS AND RESIDUE. (K) 2L72 4F4 FRTA16WE E21EU 20050406001412005040600141NM 2005 4 6 ASAA0540099 120050204A5322654653120 SHEAR TIE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - FWD CARGO BAY CORROSION ON SHEAR TIE AT BSTA 500F, RBL 10, WL 148. REPAIRED SHEAR TIE AT B-STA 500F, RBL 10, WI 148 IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050411001622005041100162NM 2005 4 11 QXEA200500535 120050322A5420 STIFFENER BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09416QX 4083 PDX - AFT NACELLE, TOP DECK, OUTBOARD ANGLE/LONGITUDINAL STIFFENER CRACKED, 25 INCHES FORWARD FROM AFT END OF NACELLE. REPAIRED IAW SRM 51-42-05, PAGE 20D. 2H72 4T RTA13NM 20050411001812005041100181EU 2005 4 11 F3LA200500003 120050120A2150 DUCT AIRBUSA318 A318111 3940019EU WATER EXTRACTOR MISINSTALLED A F3LAO OTHER WB INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM03804FR 2051 ON ARRIVAL, CREW REPORTED FUMES IN COCKPIT. F/A REPORTED SMELL IN AFT CABIN. A/C RETURNED TO MDW & LANDED W/O INCIDENT. REMOVED BELLY FAIRINGS FOR ACCESS TO LT PACK. INSPECTED PACK DUCTING & FOUND VASELINE ON DUCT SEALS & JOINTS. REMOVED WATER EXTRACTOR SEALS & JOINTS, REMOVED VASELINE, & RENSTALLED WATER EXTRACTOR. REMOVED DUCT BETWEEN MAIN HEAT EXCHANGER & ACM. CLEANED SEALS & JOINTS & REMOVED VASELINE. REINSTALLED DUCT. REMOVED ANTI-ICE VALVE/PRIMARY HEAT EXCHANGER BYPASS DUCT. CLEANED VASELINE FROM SEALS & JOINTS. REINSTALLED DUCT. REMOVED REHEATER DUCTING. CLEANED RESIDUE FROM SEALS & DUCTS. REINSTALLED REHEATER DUCTING. PERFORMED OPS CHECK OF LT PACK USING APU BLEED. OPS TEST NORMAL. 2L72 4F RT 20050411001842005041100184CE 2005 4 11 2003788 120050207A5511 SPAR BEECH 1900 1900D 1154162CE HORIZONTAL STAB CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03100UX UE100 DURING ROUTINE STRUCTURAL "I" INSPECTION, FOUR CRACKS WERE IDENTIFIED EMANATING FROM THE DE-ICE HOLE ON THE HORIZONTAL CENTER MAIN SPAR CENTER WEB SKIN APPROX 1 INCH LONG EACH UNDER PANEL 332 ATC. REPAIR WAS MADE AND AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA24CE 20050411001902005041100190NM 2005 4 11 HNAA0500007 120050129A533085320251 SKIN PANEL DHAV DHC8 DHC8102 2809003NM FUSELAGE DEBONDED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07936HA 145 DURING BOND TESTING, FOUND WIDE SPREAD DISBOND ON SKIN PANEL AT STRS 27P & 28P FROM FRAME X325 TO X424. REMOVED AND REPLACED SKIN PANEL FROM X325 TO X 424. 2H72 4T RTA13NM 20050411001972005041100197SO 2005 4 11 C2XA05IA050 120050322A5610163500111 WINDSHIELD EMB 145 EMB145XR 3260214SO COCKPIT BURNED A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SW27171385004 5004 145727 IAH - FLIGHT 3229, THE CREW REPORTED THE NUMBER TWO PACK CAUSED A BURNING SMELL DURING DESCENT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NUMBER TWO PACK TO BE OPERATING NORMALLY, FURTHER INSPECTION REVEALED THE CAPTAINS WINDSHIELD TERMINAL BLOCK WAS BURNT. THE CAPTAINS WINDSHIELD WAS REMOVED AND REPLACED, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20050411002052005041100205EA 2005 4 11 QXEA200500471 120050302A5753 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 500 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - LEFT HAND INBOARD FLAP LOWER SURFACE HAS GRAVEL DAMAGE. REPAIRED IAW CRJ700 SRM 51-26-00-001-001-A01, SRM 51-25-01-001-001-A01, AND SRM 57-52-01-101-001-A01. 2L72 4F RTA21EA 20050412002242005041200224WP 2005 4 12 05FDEA00320 120050228A2550 PANEL DOUG DC10 DC1010F 3022111WP CARGO BAY CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568053 47807 COMPLY WITH EA8-2550-55440, EQUIP/FURNISHINGS LWR CARGO, REPAIR OF STA 1841 CENTER/AFT PARTITION. COMPLIED WITH EA8-2550-55440. 2L73 4F A22WE 20050412002262005041200226WP 2005 4 12 05FDEA00322 120050301A5753ARC1953 SKIN DOUG MD10 MD1010F 3022112WP T/E FLAP DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25361FE 48260 RIGHT OUTBOARD FLAP WEDGE TOP SKIN STATION XFO 560 TO 575 HAS 3 EACH PREVIOUS REPAIRS WITH TEMPORARY FASTENERS. REMOVED DAMAGED SKIN IAW DC10 SRM 51-35-01 VOL II, FABRICATED NEW SKIN IAW DAC DWG NR ARC1953. INSTALLED SKIN IAW DC 10 SRM 51-35-01 VIL II AND FEDEX EA 8-5710-83982, WINGS RIGHT OUTBOARD FLAP WEDGE, TOP SKIN REPAIR. REFERENCE NON-ROUTINE N00341. 2L73 4F RTA22WE 20050412002342005041200234WP 2005 4 12 GTIA050055 120050227A5753 SKIN DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE FLAP VANE DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 LT WING FLAP VANE NR 4 HAS DENT TOP SIDE. REMOVED DAMAGED SKIN AND CORE. FABRICATED NEW CORE AND DOUBLER, TREATED DOUBLER AND BONDED CORE IAW 57-50. (K) 2L72 4F4 F A6WE E9NE 20050412002372005041200237 2005 4 12 GTIA050072 420050314A3413 INDICATOR DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE COCKPIT INTERMITTENT A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23820NK 49126 F/O`S VSI INDICATOR GOES ON AND OFF, INTERMITTENT. TAIL SWAP WITH AC N819. REMOVED AND REPLACED VSI INDICATOR. (K) 2L72 4F4 F A6WE E9NE 20050412002382005041200238WP 2005 4 12 GTIA050050 120050303A5330 SKIN DOUG DC9 DC983 3022083WP PWA JT8 JT8D217C 52053NE FUSELAGE DAMAGED A GTIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL23802NK 53168 WHILE PUSHBACK FROM GATE, AIRCRAFT TUG WENT OVER 90 DEGREES AND HIT AIRCRAFT PUTTING HOLE ON THE RT SIDE OF AIRCRAFT APPROX FS 275. REPAIR AT RT FUSELAGE SKIN BETWEEN L22 AND L24, NOSE GEAR SUPPORT WEB HAS BEEN INSTALLED IAW EA, REV.A HAS BEEN ACCOMPLISHED. (K) 2L72 4F4 FRTA6WE E9NE 20050412002402005041200240WP 2005 4 12 GTIA050052 120050218A5320 STIFFENER DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 AFT CARGO COMPARTMENT, STA 1338, 27L-27R AFT SIDE OF FALSE BULKHEAD, LOWER STIFFENERS ARE CORRODED. REMOVED CORROSION AT STIFFENER STA 1338L, 29L. MATERIAL LOSS OUT OF LIMITS. REMOVED STIFFENER AT STA 1338L, 29L, LOCATED AND DRILLED NEW STIFFENER. INSTALLED STIFFENER AT STA 1338 IAW SRM. (K) 2L72 4F4 F A6WE E9NE 20050412002522005041200252WP 2005 4 12 GTIA050051 120050302A7711 GAUGE DOUG DC9 DC981 3022081WP PWA JT8 JT8D217C 52053NE COCKPIT DEFECTIVE A GTIAO OTHER O OTHER DEDESCENT 1 GL23811NK 48017 WINDOW POPS WHEN IT PRESSURIZES AND LT EPR GAUGE ERRATIC READING TOP TO BOTTOM SCALE IN IDLE IN DESCENT, AIRCRAFT TAIL SWAP WITH 819NK. PRESSURIZED AC NO POP - OK FOR CONTINUED SERVICE, REMOVED AND REPLACED NR1 EPR GAUGE. OPS CHECK NORMAL. (K) 2L72 4F4 F A6WE E9NE 20050412002532005041200253WP 2005 4 12 GTIA050076 120050326A2797 WIRE DOUG DC9 DC983 3022083WP PWA JT8 JT8D217A 52053NE RUDDER CONTROL BROKEN A GTIAK NONE P NO WARNING INDICATION ININSP/MAINT 1 GL23808NK 49504 UPON PREFLIGHT (COCKPIT SETUP) COULD NOT GET RUDDER CONTROL MANUAL LIGHT DURING TEST, AIRCRAFT TAIL SWAP TO 817NK. TROUBLESHOT DOWN TO BROKEN WIRE AT CANT. STA 1485, REPAIRED BROKEN WIRE IAW SRM. OPS CHECK, OK. (K) 2L72 4F4 FRTA6WE E9NE 20050412002542005041200254WP 2005 4 12 GTIA050044 120050220A5610 WINDSHIELD DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE COCKPIT CRACKED A GTIAK NONE O OTHER CRCRUISE 1 GL23820NK 49126 F/O WINDSHIELD CRACKED IN FLIGHT, OUTER PANE ONLY. AIRCRAFT TAIL SWAP WITH N835NK. REMOVED AND REPLACED WINDSHIELD. (K) 2L72 4F4 F A6WE E9NE 20050412002552005041200255WP 2005 4 12 GTIA050047 120050118A5315 FLOORBEAM DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 AFT PIT FS 1338 APB FWD SIDE LOTER T-CHORD CORRODED L28L TO L28R. REMOVED CORROSION OUT OF LIMITS, REMOVED T-CAP (CHORD) STA 1338, L28L TO L29L, DRILLED AND LOCATED NEW T-CAP STA 1338. OK TO TOP COAT AND INSTALL NEW T-CAP. (K) 2L72 4F4 F A6WE E9NE 20050412002702005041200270NM 2005 4 12 ASAA054069 120050130A5320654147327 WEB BOEING737 7374Q8 138447QNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - FOUND DAMAGED FLOOR SUPPORT SHEAR WEB AT BS 500E-500F RBL 36 WL 152. REMOVED, FABRICATED AND INSTALLED NEW SHEAR WEB. (M) 2L72 4F RTA16WE 20050412002792005041200279NM 2005 4 12 ASAA0540145 120050224A1430654587523 NUT BOEING737 7374Q8 138447QNM R1 DOOR MISSING A ASAAK NONE O OTHER ININSP/MAINT 1 NM02756AS 25097 PDX- FOUND R1 DOOR WOULD NOT OPEN. FOUND UPPER GEAR CONTROL ROD RETAINING NUT MISSING AND BOLT FELL OUT. SECURED UPPER CONTROL ROD BOLT AND RETAINING NUT. ALL RIG AND OPS CHECKS GOOD. 2L72 4F RTA16WE 20050412002832005041200283WP 2005 4 12 ASAA080137 120050227A52305910141129 SKIN DOUG DC9 DC983 3022083WP MID CARGO DOOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 OKC - FOUND HV CHECK, MID CARGO BAY DOOR IS DENTED. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050412002932005041200293NM 2005 4 12 ASAA0540060 120050126A5320654652837 SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - FORWARD CARGO BAY AREAS OF CORROSION ON FLOOR TO SIDEWALL SUPPORT BS 500G LBL 23 WL 156. PART WILL BE REPLACED ON MIG-5 4878962. (M) 2L72 4F RTA16WE 20050412002962005041200296NM 2005 4 12 ASAA0540058 120050125A5320654795134 RETAINER BOEING737 7374Q8 138447QNM AFT CARGO BAY GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - AFT CARGO BAY FLOOR RETAINER STRIP GOUGED. GOUGED OUT OF LIMITS. FABRICATED NEW AFT CARGO BAY FLOOR RETAINER STRIP IAW BOEING DWG 65-47951, AMM 51-40-02 PAGE 1 STEP 2. (M) 2L72 4F RTA16WE 20050412003102005041200310NM 2005 4 12 ASAA0540155 120050303A53206552878102 SILL BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02791AS 28886 PAE - FOUND CORROSION ON AFT ENTRY DOOR MOPSILL. REPLACED MOPSILL. (M) 2L72 4F RTA16WE 20050413000022005041300002EU 2005 4 13 ASOA05185 120050204A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27633AS 344 DURING A C-CHECK IN YUL, THE SEAT TRACKS BETWEEN FRAME 36 AND 39 LEFT/RIGHT WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS BETWEEN FRAME 36 AND 39 LT/RT IAW SRM 51-25-04. (M) 2H72 4T RTA53EU 20050413000032005041300003EU 2005 4 13 ASOA05184 120050204A5320S53371293201 SUPPORT AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27633AS 344 DURING A C-CHECK IN YUL, THE SUPPORT PLATE BETWEEN FRAME 13-17 LEFT WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SUPPORT PLATE BETWEEN FRAM 13-17 LEFT IAW SRM 53-31-00, 51-21-42 AND 51-25-01. (M) 2H72 4T RTA53EU 20050413000062005041300006EU 2005 4 13 ASOA05177 120050202A5714 ANGLE AEROSPATR72 ATR72212 8680945EU WINGBOX CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27633AS 344 DURING A C-CHECK IN YUL, THE ANGLE IN THE WING BOX AT FS 28 RT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE ANGLE IN THE WING BOX AT FS 28 RT IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20050413000082005041300008EA 2005 4 13 ASOA05246 120050318A33504871907191 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA CABIN DISCONNECTED A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27906EV 7642 DURING A GROUND INSPECTION IN ATL, THE EMERGENCY FLOOR LIGHT STRIP AT ROW 7 WAS FOUND TO BE INOPERATIVE. MAINTENANCE RESECURED THE PLUG (CONNECTORS) TO THE EMERGENCY FLOOR LIGHT STRIP AT ROW 7. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050413000092005041300009EA 2005 4 13 ASOA05253 120050321A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27902EV 7620 DURING A C-CHECK IN MCN, THE ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW ASA EO 600-53-0072B. (M) 2L72 4F RTA21EA 20050413000102005041300010EA 2005 4 13 ASOA05252 120050321A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27902EV 7620 DURING A C-CHECK IN MCN, THE OUTBOARD FS 280 LEFT CLIP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE OUTBOARD FS 280 LT CLIP. (M) 2L72 4F RTA21EA 20050413000122005041300012EA 2005 4 13 ASOA05247 120050318A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA EXTERIOR INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27849AS 7347 DURING HANGAR MAINTENANCE IN BTR, AN EXTERIOR EMERGENCY LIGHT ON THE RIGHT SIDE WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN AN EXTERIOR EMERGENCY LIGHT ON THE RIGHT SIDE. OPERATIONAL CHECKS GOOD. (M) 2L72 4F RTA21EA 20050413000132005041300013EA 2005 4 13 ASOA05254 120050321A5260601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27902EV 7620 DURING A C-CHECK IN MCJHN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE BOTTOM STEP ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20050413000142005041300014EU 2005 4 13 ASOA05183 120050204A5320S53371293200 CHANNEL AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27633AS 344 DURING A C-CHECK IN YUL, THE FORWARD CARGO FLOOR DRAIN CHANNEL BETWEEN FRAME 13-17 LEFT WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE PERFORMED A TEMPORARY REPAIR ON THE FORWARD CARGO FLOOR DRAIN CHANNEL BETWEEN FRAME 13-17 LEFT IAW ASA EO 72-53-0161. (M) 2H72 4T RTA53EU 20050413000152005041300015EU 2005 4 13 ASOA05180 120050204A5320 INTERCOSTAL AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27633AS 344 DURING A C-CHECK IN YUL, THE INTERCOSTAL BETWEEN FRAME 36-38 LEFT WAS FOUND TO BE CORRODED ON THE UPPER AND LOWER FLANGE BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTAL BETWEEN FRAME 36-38 LEFT IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20050413000172005041300017EA 2005 4 13 ASOA05173 120050302A5260601R3167017 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27844AS 7317 FLT 4287 - DURING A GROUND INSPECTION IN FWA, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050413000182005041300018EA 2005 4 13 ASOA05172 120050301A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27909EV 7658 FLT 4118 - DURING A GROUND INSPECTION IN MGM, THE NR 4 EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE NR 4 EMERGENCY CEILING LIGHT. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050413000192005041300019EA 2005 4 13 ASOA05171 120050228A5260601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27852AS 7369 DURING HANGAR MAINTENANCE IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED AT THE FORWARD SECTION. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20050413000202005041300020EA 2005 4 13 ASOA05170 120050228A5210 SKIN CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27852AS 7369 DURING HANGAR MAINTENANCE IN MCN, THE INTERNAL SKIN UNDER THE TOP STEP ON THE PASSENGER DOOR WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE INTERNAL SKIN UNDER THE TOP STEP ON THE PASSENGER DOOR IAW ASA EO 600-52-0043. (M) 2L72 4F RTA21EA 20050413000212005041300021EU 2005 4 13 ASOA05187 120050204A5315 FLOORBEAM AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27633AS 344 DURING A C-CHECK IN YUL, THE FLOORBEAMS AT FRAME 38/40 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANANCE REMOVED AND REPLACED THE FLOORBEAMS AT FRAME 38/40 IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20050413000222005041300022EU 2005 4 13 ASOA05186 120050204A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27633AS 344 DURING A C-CHECK IN YUL, THE SEAT TRACK BETWEEN FRAME 39 AND 40 RIGHT WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK BETWEEN FRAME 39 AND 40 RT IAW SRM 51-25-04. (M) 2H72 4T RTA53EU 20050413000232005041300023EU 2005 4 13 ASOA05189 120050205A5313 STRINGER AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27633AS 344 DURING A C-CHECK IN YUL THE FS 40, STRINGER 14R WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FS 40, STRINGER 14R IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20050413000242005041300024EU 2005 4 13 ASOA05188 120050204A5315 FLOORBEAM AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27633AS 344 DURING A C-CHECK IN YUL, THE FLOORBEAMS AT FS 36, STRINGER 14L AND 14R AND FRAME 39, STRINGER 14L AND 14R WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAMS AT FRAME 36, STRINGER 14L AND 14R IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20050413000252005041300025EU 2005 4 13 ASOA05182 120050204A5320S5367800821602 FLOOR SUPPORT AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27633AS 344 DURING A C-CHECK IN YUL, THE Z-FLOOR SUPPORT BETWEEN FRAME 39 AND 41 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE Z-FLOOR SUPPORT BETWEEN FRAME 39 AND 41 IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20050413000272005041300027EA 2005 4 13 ASOA05169 120050228A335014806990 CONNECTOR CNDAIRCL600 CL6002C10 1390015EA CABIN DISCONNECTED A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27750EV 10161 DURING AN A-CHECK IN BTR, THE THIRD FROM THE FRONT EMERGENCY CEILING LIGHT AS FOUND TO BE INOPERATIVE. MAINTENANCE FOUND THE CONNECTOR TO THE THIRD FROM THE FRONT EMERGENCY CEILING LIGHT DISCONNECTED AND RECONNECTED IT TO THE LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050413000282005041300028EA 2005 4 13 ASOA05167 120050228A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27880AS 7606 DURING A C-CHECK IN MCN, THE CLIP AT FS 625 LEFT PRESSURE BULKHEAD WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CLIP AT FS 625 LEFT PRESSURE BULKHEAD. (M) 2L72 4F RTA21EA 20050413000312005041300031EA 2005 4 13 ASOA05234 120050320A3350100865 POWER SUPPLY CNDAIRCL600 CL6002B19 1900309EA CABIN DISCHARGED A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27926EV3853 7843 FLT 4500 - DURING A GROUND INSPECTION IN ATL, LEFT EXTERIOR EMERGENCY LIGHT WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTS POWER SUPPLY UNIT AT ROW 8. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050413000322005041300032EA 2005 4 13 ASOA05233 120050314A3350 LIGHT CNDAIRCL600 CL6002C10 1390015EA CABIN MALFUNCTIONED A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27718EV 10095 FLT 4911 - DURING A GROUND INSPECTION IN SLC, THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE RESET CIRCUIT BREAKER P2U3. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050413000342005041300034EA 2005 4 13 ASOA05250 120050312A3260864202 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA RT MLG FAULTY A ASOAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27914EV 7752 FOLLOWING TAKEOFF FROM ATL-CHO, THE CREW BROUGHT THE GEAR HANDLE TO THE UP POSITION AND A FEW SECONDS LATER RECEIVED A GEAR UP DISAGREE WARNING WITH A WHITE INDICATION APPEARING ON THE RIGHT MAIN GEAR. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED TO ATL AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE UPLOCK PROXIMITY SENSOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050413000352005041300035EA 2005 4 13 ASOA05249 120050304A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA T/E FLAP MALFUNCTIONED A ASOAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO27853AS 7374 FLT 4563 - DURING FINAL APPROACH INTO XNA FROM ATL, THE CREW SELECTED THE FLAPS TO FIRTY FIVE DEGREES FROM THIRTY AND RECEIVED A FLAPS FAIL MESSAGE. THE AIRCRAFT PERFORMED A GO AROUND AND COMPLIED WITH THE QRH. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY IN XNA. MAINTENANCE REMOVED AND REPLACED THE BRAKE POSITION SENSOR UNIT, BPSU, AND THE POWER DRIVE UNIT. MAINTENANCE ALSO PERFORMED A TORQUE CHECK OF THE ACTUATORS. NO DEFECTS WERE NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050413000362005041300036EA 2005 4 13 ASOA05244 120050317A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27905EV 7632 DURING A C-CHECK IN MCN, THE FS 280 LT CLIPS INBOARD AND OUTBOARD AT LBL 9 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FS 280 LT CLIPS INBOARD AND OUTBOARD AT LBL 9. (M) 2L72 4F RTA21EA 20050413000392005041300039EA 2005 4 13 ASOA05240 120050316A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27905EV 7632 DURING A C-CHECK IN MCN, THE ENGINE SUPPORT BEAM AT BL 36.20 RT WAS FOUND TO BE CRACKED BEYOND LIMIT. MAINTENANCE IS REPAIRING THE ENGINE SUPPORT BEAM AT BL 36.20 RT IAW ASA EO 600-53-0070. (M) 2L72 4F RTA21EA 20050413000402005041300040EA 2005 4 13 ASOA05239 120050316A5320601R3501153 PLATE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27905EV 7632 DURING A C-CHECK IN MCN, THE CARGO FLOOR LANDING PLATE AT FS 589 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO FLOOR LANDING PLATE AT FS 589 IAW ASA EO 600-53-0117. (M) 2L72 4F RTA21EA 20050413000452005041300045EA 2005 4 13 ASOA05228 120050305A5315 FLOORBEAM CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27702EV 10035 DURING HANGAR MAINTENANCE IN CKB, THE FS 280 FLOOR TRANSVERSE BEAM WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FS 280 FLOOR TRANSVERSE BEAM IAW BOMBARDIER REO 670-53-11-047. (M) 2L72 4F RTA21EA 20050413000492005041300049EA 2005 4 13 ASOA05224 120050310A3234750006000 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A ASOAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO27847AS 7335 DURING APPROACH INTO ATL FROM EVV AFTER SELECTING GEAR DOWN THE CREW RECEIVED A GEAR DISAGREE WARNING MESSAGE. THE CREW EXECUTED A GO AROUND AND COMPLIED WITH THE QRH. THE CREW SELECTED THE GEAR HANDLE TO THE UP POSITION AND RECEIVED A GEAR DOWN INDICATION OF ALL GREEN AND NORMAL WITH THE ONLY EXCEPTION BEING THE NOSE GEAR DOOR REMAINING OPEN. AN EMERGENCY WAS DECLARED WITH EMERGENCY EQUIPMENT REQUESTED TO BE ON STANDBY AS A PRECAUTION. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE NOSE GEAR DOOR SELECTOR VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050413000502005041300050EA 2005 4 13 ASOA05242 120050316A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27925EV 7831 DURING A C-CHECK IN MCN, THE FS 621 LT/RT FLOOR SUPPORT ANGLES WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FS 621 LT/RT FLOOR SUPPORT ANGLES IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20050413000522005041300052EA 2005 4 13 ASOA05222 120050309A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27904EV 7628 DURING A C-CHECK IN MCN, THE INBOARD FS 280 LEFT/RIGHT CLIPS WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE INBOARD FS 280 LEFT/RIGHT CLIPS IAW CRJ-200 SRM 51-42-20. (M) 2L72 4F RTA21EA 20050413000532005041300053EA 2005 4 13 ASOA05226 120050311A7830 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A ASOAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27854AS 7382 FLT 4602 - DURING CRUISE FROM BTR-ATL, AT APPROXIMATELY 27,000 FEET, THE CREW RECEIVED A RIGHT REV ICON CAUTION MESSAGE FOLLOWED BY A REV UNLOCKED MESSAGE. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT DIVERTED TO MGM AND LANDED SAFELY. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF BOTH THRUST REVERSERS AND ALSO PERFORMED A VISUAL INSPECTION OF THE RIGHT ENGINE THRUST REVERSER AND HARDWARE. NO DEFECTS WERE NOTED. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050413000542005041300054EU 2005 4 13 ASOA05225 120050311A33503012000 POWER SUPPLY AEROSPATR72 ATR72212 8680945EU CABIN DISCHARGED A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27637AS 383 FLT 4733 - DURING A GROUND INSPECTION IN ATL, THE LEFT FORWARD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY 61LG. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20050413000552005041300055EA 2005 4 13 ASOA05221 120050309A5260601R319805 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR SEPARATED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27827AS 7212 DURING HANGAR MAINTENANCE IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND SEPARATING AT THE ATTACHMENT POINT STAY ROD. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20050413000592005041300059SO 2005 4 13 SIMA200507522 120050310A532013500437001 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21705AE 145184 SAW - DURING CPCP INSPECTION, FOUND CENTER OMEGA BEAM HAS CORROSION UNDER CROSS BEAM AT FRAME 25. REMOVED AND REPLACED OMEGA BEAM IAW EMB 135 SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050413000612005041300061SO 2005 4 13 SIMA200508201 120050321A335020131A BATTERY EMB 135 EMB135KL 3260302SO CABIN DISCHARGED A SIMAK NONE L NO TEST TXTAXI/GRND HDL 1 SW21801AE 145469 LAX - FLT 3195 - CREW REPORTED A ROW OF EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY BATTERY IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050413000622005041300062SO 2005 4 13 SIMA200507901 120050318A2150 A/C PACK EMB 145 EMB145LR 3260212SO A/C BAY MALFUNCTIONED A SIMAH DEACTIVATE SYST/CIRCUITS BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TXTAXI/GRND HDL 1 SW21646AE 145213 LBB - FLT 3390 - CREW REPORTED THE NR 2 PACK FAILED, WITH SMOKE PRESENT IN THE CABIN. THE LAVATORY SMOKE DETECTOR ACTIVATED, THE NR 2 PACK WAS DESELECTED AND THE CABIN SMOKE WENT AWAY WITH ONLY NR 1 RUNNING. PERFORMED OPERATIONAL CHECK OF NR 2 PACK WITH NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20050413000642005041300064SO 2005 4 13 SIMA200507504 120050313A532014525381003 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21652RS 145432 ABI - DURING INSPECTION OF AIRCRAFT, A PREVIOUS REPAIR ON THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. REMOVED THE CORRODED REPAIR. FABRICATED AN EXTERNAL ANGLE, FABRICATED A FILLER AND THREE SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 28, CHAPTER 53-21-10 FIG 201. (M) 2L72 4T RTT00011AT 20050413000662005041300066SO 2005 4 13 SIMA200507512 120050310A532014522178005 SILL EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21700LE 145156 ABI - DURING INSPECTION OF AIRCRAFT, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. REMIOVED 2L72 4F RTT00011AT 20050413000672005041300067SO 2005 4 13 SIMA200507503 120050303A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21801AE 145469 ABI - DURING INSPECTION AIRCRAFT, THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. PERFORMED A CUT OUT TO REMOVED THE CORROSION. FABRICATED A EXTERNAL DOUBLER, FILLER, SHIMS AND PLATE. REPAIR DONE IAW EMB 145 SRM, SRM EMB145/1142 REV 28, CHAPTER 53-21-10 FIG 201 AND EMB. REPAIR STATEMENT IC2005-145/0983 PARA 1 DATED FEB 23, 2005. (M) 2L72 4F RTT00011AT 20050413000692005041300069SO 2005 4 13 SIMA200508703 120050316A532014522178005 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21636AE11968 145160 THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED CENTER SILL AND INSTALLED NEW SERVICEABLE SILL IAW EMB SRM, SRM 145/1142 REV 28, CHAPTER 51-40-02, IC2003-145/0818 DATED MARCH 6, 2003 AND AEA ETN EM-53-013 DATED AUGUST 28, 2001. (M) 2L72 4T RTT00011AT 20050413000702005041300070SO 2005 4 13 SIMA200507508 120050306A531314533888001 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21655AE 145452 ABI - DURING INSPECTION OF AIRCRAFT, STRINGER 19R WAS FOUND CHAFED. BLENDED THE CHAFED AREA AND PERFORMED NDT INSPECTION. FABRICATED REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2005-145/1147 PARA 8 DATED MARCH 3, 2005. (M) 2L72 4T RTT00011AT 20050413000722005041300072SO 2005 4 13 SIMA200507509 120050304A532014522178005 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21655AE 145452 ABI - DURING INSPECTION OF THE AIRCRAFT, FOUND THE SERVICE DOOR CENTER SILL CORRODED. BLENDED THE CENTER SILL TO REMOVED THE CORROSION AND PERFORMED NDT INSPECTION. FABRICATED THREE REPAIR DOUBLERS, REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 28, CHAPTERS 53-21-02. (M) 2L72 4T RTT00011AT 20050413000742005041300074SO 2005 4 13 SIMA200507525 120050310A532013500436003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21705AE 145184 SAW - DURING CPCP INSPECTION FOUND, LEFT OMEGA HAS CORROSION UNDER CROSSBEAM AT FRAME 29. REMOVED AND REPLACED LEFT OMEGA BEAM AT FRAME 29 IAW EMB135 SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050413000752005041300075SO 2005 4 13 SIMA200507524 120050310A532013500436001 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21705AE 145184 SAW DURING CPCP INSPECTION, FOUND LEFT OMEGA BEAM HAS CORROSION UNDER CROSS BEAM AT FRAME 25. REMOVED AND REPLACED LEFT OMEGA BEAM AT FRAME 25 IAW EMB 135 SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050413000762005041300076SO 2005 4 13 SIMA200508704 120050319A532014525381003 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21636AE11968 145160 ABI - THE CENTER OMEGA BEAM AT FRAME 24 WAS FOUND TO BE CORRODED. PERFORMED A CUT OUT OF THE CENTER OMEGA BEAM TO REMOVE CORROSION. FABRICATED FILLER, TWO SHIMS AND DOUBLER. REPAIR DONE IAW EMB REPAIR STATEMENT IC2005-145/1180 PARA 2 DATED MARCH 15, 2005. (M) 2L72 4T RTT00011AT 20050413000782005041300078SO 2005 4 13 SIMA200507507 120050313A531314533888001 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21652RS 145432 DURING INSPECTION, 652 STRINGER 19R WAS FOUND TO BE CHAFED AT AFT FAIRING CUTOUT. BLENDED THE CHAFE AND PERFORMED EDDY CURRENT INSPECTION WITH NO CRACKS NOTED. FABRICATED A DOUBLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 28, CHAPTER 53-24-02. (M) 2L72 4T RTT00011AT 20050413000792005041300079SO 2005 4 13 SIMA200507505 120050313A531314533888001 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21652RS 145432 ABI - DURING INSPECTION STRINGER 19L WAS FOUND TO BE CHAFED AT AFT FAIRING CUTOUT. BLENDED THE CHAFE AND PERFORMED EDDY CURRENT INSPECTION WITH NO CRACKS NOTED. FABRICATED A DOUBLER, TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 28, CHAPTER 53-24-02. (M) 2L72 4T RTT00011AT 20050413000802005041300080SO 2005 4 13 SIMA200506607 120050305A335020131A BATTERY PACK EMB 135 EMB135LR 3260305SO CABIN DISCHARGED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21711PH 145235 BOS - FLT 4585 - CREW REPORTED AN EMERGENCY EXIT SIGN IN CABIN TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK POWER SUPPLY NR 5 IAW EMB 135 AMM 33-50-04. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050413000882005041300088SO 2005 4 13 SIMA200507521 120050308A5514KSC35762OV BUSHING EMB 135 EMB135LR 3260305SO HORIZ STAB WORN A SIMAK NONE O OTHER ININSP/MAINT 1 SW21705AE 145184 SAW - BUSHING AT HORIZONTAL STABILIZER HINGE POINTS HAVE PLAY. COMPLIED WITH EMB 135 SRM 55-10-02 FOR HORIZONTAL STABILIZER BUSHING RAI. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050413000892005041300089SO 2005 4 13 SIMA200507520 120050308A532014522459001 RAMP EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21705AE 145184 SAW - DURING CPCP INSPECTION, FOUND SUPPORT RAMP IN CENTER HAT SECTION IS CORRODED AT FRAME 20. INSTALLED NEW RAMP IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050413000902005041300090SO 2005 4 13 SIMA200507519 120050308A532013500469401 ANGLE EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21705AE 145184 SAW - DURING CPCP INSPECTION, FOUND Z-ANGLE AT FRAME 22A CORRODED. RAI'D ANGLE AT FRAME 22A IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050413000922005041300092EU 2005 4 13 USAA050382 120050303A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW 0337 BFM - FOUND THE SEAT TRACK CORRODED 6 AREAS, .150 INCH WIDE BY .67 INCH LONG BY .024 DEEP, BETWEEN FRAME 55-58, Y + -2462. REPLACED TRACK SECTION WITH REPAIR SPLICE PER SRM 53-00-15, FIG 204 SHEET 1. (M) 2L72 4F RTA46NM 20050413000942005041300094NM 2005 4 13 USAA050379 120050310A5315BAC14902905 FLOORBEAM BOEING767 767201 1385125NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19648US68950 23900 BFM - FOUND FLOORBEAM CORRODED 4 INCH BY 1 INCH BY .080 INCH AREA, STATION 303, RBL 20-24. REPAIRED FLOORBEAM T-CHORD PER SRM 53-00-51. (M) 2L72 4F RTA1NM 20050413000962005041300096EU 2005 4 13 USAA050012 120050101A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW 0315 BFM - FOUND SEAT TRACK CORRODED .640 INCH LONG BY .125 INCH WIDE BY .038 INCH DEEP AREA, Y+450. CORROSION LEVEL 2, TASK NR J7-200-2580C. REMOVED AND REPLACED SEAT TRACK PER SRM 53-00-15, 53-00-10, 51-42-11, 51-21-11, 51-42-11. (M) 2L72 4F RTA46NM 20050413000982005041300098EU 2005 4 13 USAA050011 120050101A21404E33572 ELEMENT AIRBUS330 A330323 3930335EU CABIN CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW22421 0315 BFM - FOUND HEATED FLOOR PANEL ELEMENT CORRODED BETWEEN FRAME 13A-16A, Y=1456-1959. CORROSION LEVEL 1, TASK NR J7-230-53101-002. FABRICATED REPLACEMENT SKIN PER EA 96114 REV A. (M) 2L72 4F RTA46NM 20050414000022005041400002NM 2005 4 14 UPS05444201 120050313A5347BAC15201566 SEAT TRACK BOEING747 747121 1384871NM FUSLEAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 BS 1564-1570 RBL 98 INCH SEAT TRACK LEFT FLANGE CORROSION. CORROSION BLEND OUT 0.035 INCH BY 1 INCH BY 3 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT, SEAT TRACK REPLACED AS PER SRM 51-10-01 P.9 2L74 4F A20WE 20050414000032005041400003NM 2005 4 14 UPS05444202 120050313A5347BAC15201890 SEAT TRACK BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 BS 1700-1707 LBL 11 INCH SEAT TRACK RT FLANGE CORROSION. CORROSION BLEND OUT 0.040 INCH BY 1 INCH BY 2 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT, SEAT TRACK REPLACED AS PER SRM 51-10-01 P.9. 2L74 4F A20WE 20050414000042005041400004NM 2005 4 14 UPS05444203 120050313A534069B621091 FITTING BOEING747 747121 1384871NM FUSLEAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 BS 1680 LBL 55 TIE DOWN FIG ATT PLATE FOUND CORRODED. CORROSION BLEND OUT 0.025 INCH BY 1 INCH BY 1 INCH OUT OF SRM 53-10-01 FIG 1 LIMIT, TIE DOWN FIG PLATE REPLACED AS PER MM 20-51-01. 2L74 4F A20WE 20050414000082005041400008 2005 4 14 UPS05844239 420050407A2565 BOTTLE DOUG DC8 DC873F 302199FWP ESCAPE SLIDE DISCHARGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 341 46094 ESCAPE SLIDE BOTTLE PRESSURE 2000 LBS. REMOVED AND REPLACED ESCAPE SLIDE. 2L74 4F RT4A25 20050414000112005041400011WP 2005 4 14 UPS05844245 120050324A534037558411 FITTING DOUG DC8 DC873F 302199FWP FUSLAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE: C2, AFT CARGO PIT STA 1200 LONGERON 34R BATHTUB FITTING CRACKED IN FWD AND AFT CORNERS. REMOVED AND REPLACED BATHTUB FITTING IAW DC-8 SRM 53-2-0 FIG 26 AND SRM 51-1-20D. 2L74 4F RT4A25 20050414000122005041400012WP 2005 4 14 UPS05844246 120050324A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE: C2, 60 COMPT, 6 INCHES CRACK IN L-17L STA 1770. REMOVED LONGERON 17L IAW DC-8 SRM 51-1-21. FABRICATED LONGERON IAW DC- 8 SRM 53-5-3 AND SRM 51-3-2. INSTALLED REPLACEMENT LONGERON IAW DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20050414000132005041400013WP 2005 4 14 UPS05844247 120050319A5510SE085500094 FITTING DOUG DC8 DC873F 302199FWP HORIZONTAL STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE: C2, CRACKED L-FITTING IN RT HORIZONTAL STAB L/E FWD SPAR AREA AT FUSELAGE. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-21 AND SRM 51-1-20D. 2L74 4F RT4A25 20050414000152005041400015WP 2005 4 14 UPS05844249 120050319A5712 RIB DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE: C2, LEFT L/E UPPER RIB CRACKED .5 INCH LONG AT STA 811. REPAIRED LT L/E UPPER RIB IAW DC-8 SRM 57-2-0 FIG 2 AND SRM 51-1 20D. 2L74 4F RT4A25 20050414000162005041400016WP 2005 4 14 UPS05844251 120050321A5531 RIB DOUG DC8 DC873F 302199FWP VERTICAL STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE: C2, VERTICAL FIN L/E HAS CRACKED RIB .75 INCH AT ACCESS PNL 51F. REPAIRED VERTICAL FIN RIB IAW DC-8 SRM 55-02-00 FIG 002 AND SRM 51-1-20D. 2L74 4F RT4A25 20050414000172005041400017WP 2005 4 14 UPS05844252 120050318A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE: C2, RIGHT WING L/E UPPER RIB CRACKED .5 INCH LONG AT STA XRS 727, VIEW FROM PANEL 518A. REPAIRED RIGHT WING L/E UPPER RIB AT STA XRS 727 IAW DC-8 SRM 57-2-0. 2L74 4F RT4A25 20050414000202005041400020WP 2005 4 14 UPS05844257 120050319A532056434037 ANGLE DOUG DC8 DC873F 302199FWP LT WING WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE: C2, ANGLE CRACKED AT UPPER WING SKIN, LEFT W/W, STA 940 AT GROUND SPOILER PULLYS O/B SIDE OF W/W, 27 INCHES BELOW CEILING. REMOVED CRACKED ANGLE IAW DC-8 SRM 51-1-21. FABRICATED REPLACEMENT ANGLE IAW DWG 5643403. INSTALLED REPLACEMENT ANGLE IAW DC-8 SRM 51-1-20D, 51-1-21, 51-3-0, & DWG 5643403. 2L74 4F RT4A25 20050414000212005041400021WP 2005 4 14 UPS05844259 120050322A53403755827U2 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE:C2 "A" PIT CARGO DOOR ENTRANCE L33R FWD CORNER BOTTOM BANANA FITTING HAS .400 INCH LONG CRACK. ROMOVED AND REPLACED BANANA FITTING IAW DC-8 SRM 51-1-20D & 51-1-21. 2L74 4F RT4A25 20050414000222005041400022WP 2005 4 14 UPS05844260 120050320A5511 RIB DOUG DC8 DC873F 302199FWP HORIZONAL STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE: C2, CRACKED LOWER RIB ON L/H HORIZONTAL LEADING EDGE 40 INCHES FROM IB END. STOPDRILLED CRACK IAW DC-8 SRM 55-2-0 FIG.2. REPAIRED CRACKED RIB IAW DC-8 SRM 55-3-1 FIG. 3, 55-2-0 FIG. 2, & 51-1-20D. 2L74 4F RT4A25 20050414000232005041400023WP 2005 4 14 UPS05844261 120050330A574037048411 FITTING DOUG DC8 DC873F 302199FWP WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE: C2, STRINGER END FITTING FWD INSIDE ACCESS PANEL 505E NR 3 MAIN CRACKED AT STRINGER 51. REMOVED AND REPLACED STRINGER 51 END FITTING IAW DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20050414000262005041400026WP 2005 4 14 UPS05844264 120050319A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE: C2, LONGERON 15L IS CRACKED AT F/S 1750 AT CANTED FRAME. REMOVED AND REPLACE LONGERON FROM F/S 1735 TO F/S 1765 IAW DC-8 SRM 53 -2-0 FIG. 10, & 51-1-21. 2L74 4F RT4A25 20050414000302005041400030NM 2005 4 14 ASMF200501008 120050115A80105938255501 DUCT DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE RT ENGINE DAMAGED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23583MD 49659 718260 DURING ENGINES STARTING, RT ENGINE DID NOT STARTED BECAUSE N1 WAS OUT OF SERVICE. DURING MAINTENANCE REVISION WAS DETECTED 8TH STAGE DUCT BROKEN. DUCT WAS REPLACED AND TESTS WERE PERFORMED IAW MM 71-00-01, ALL CORRECT. 2L72 4F4 FRT E9NE 20050414000312005041400031NE 2005 4 14 ASMF200501013 220050119A7230821501 COMPRESSOR WHEEL DOUG DC8 DC8* WP PWA JT8 JT8D219 52053NE LT ENGINE DAMAGED W ASMFK NONE CJ F.O.D. WARNING INDICATION ININSP/MAINT 1 SW23755RA10600 49727 725417 DURING TRANSIT CHECK WERE DETECTED 15 BLADES OF LEFT ENGINE DAMAGED BY FOD. ONE BLADE HAD 0.25 DEPTH AND 7.25 FORM THE BLEED ROOT. AIRCRAFT WAS SENT TO THE HANGAR AND BLADES WERE REWORKED IAW MM 72-33-22. BOROSCOPE INSPECTION WAS PERFORMED TO THE SIX AND SEVEN STAGES, BEING ALL CORRECT. DURING OVERNIGHT SERVICE, LEFT ENGINE C1 DISK WAS REPLACED IAW MM 72-33-02, ENGINE RUNNING TEST WAS PERFORMED IAW MM 71-00-00, ALL CORRECT. 2L74 4J4 FF 4A25 E9NE 20050414000322005041400032NM 2005 4 14 ASMF200501014 120050123A2150 A/C PACK BOEING757 7572Q8 1384972NM LEFT INOPERATIVE W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23803AM 26268 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF LT AIR CONDITIONING PACK WAS OUT OF SERVICE. AT PLATFORM, BOTH AIR CONDITIONING SYSTEMS WERE CHECKED BEING CORRECT. DURING CHECK, LT ENGINE BLEED AIR OFF LIGHT TURNED ON, LIGHT WAS DEFERRED IAW MM 36-11-1. AT MEX, B757 FIM PROCEDURE AND TESTS WERE PERFORMED IAW FIM 36-10-22 AND MM 36-11-09, ALL CORRECT. 2L72 4F RTA2NM 20050414000342005041400034NM 2005 4 14 ASMF200502002 120050205A2741160202100 CONTROL MODULE BOEING757 7572Q8 1384972NM STAB TRIM FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23803AM36028 26268 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF AFTER ENGINES STARTED, EICAS MESSAGES "STAB TRIM" WAS SHOWN. REPORT WAS DEFERRED IAW MEL 27-41-2. DURING TRANSIT CHECK AT MEX, LEFT STAB TRIM CONTROL MODULE WAS REPLACED IAW MM 27-41-05, TESTED CORRECT, DEFERRED REPORT WAS CLOSED. 2L72 4F RTA2NM 20050414000362005041400036NM 2005 4 14 ASMF200502004 120050206A2760 PROXIMITY SWITCH DOUG MD88 MD88 3023688NM SPOILERS MALFUNCTIONED W ASMFD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SW23160PL 49763 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF LIGHT SPOILER DEPLOYED ON. REPORT WAS DEFERRED IAW MEL 22-32-1. DURING TRANSIT SERVICE AT MEX, BITE WAS PERFORMED TO UNIT PROXIMITY SWITCH ELECTRONIC IAW MM 27-60-00, TESTED CORRECT, DEFERRED REPORT WAS CLOSED. 2L72 4F RTA6WE 20050414000382005041400038NM 2005 4 14 ASMF200502011 120050219A3260 PROXIMITY SWITCH BOEING737 73773A 1384606NM MLG MALFUNCTIONED W ASMFD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SW23908AM 30038 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF AFTER ENGINES STARTED, PSEU LIGHT TURNED ON. BITE WAS PERFORMED TO THE PROXIMITY SWITCH SHOWING 32-62005 AND 27-62004 FAIL CODES. F IM 32-61 PROCEDURE TASK 805 AND TASK 825 WAS PERFORMED IAW MM 32-61-00, TESTED CORRECT. THE ENGINES WERE STARTED, BEING CORRECT. DURING OVERNIGHT SERVICE, FIM 32-09 PROCEDURE TASK 801 WAS PERFORMED, WITHOUT ANY MAINTENANCE MALFUNCTION MESSAGE IN PSEU. 2L72 4F RTA16WE 20050414000422005041400042NE 2005 4 14 ASMF200503002 220050303A73217696068 FUEL CONTROL DOUG DC8 DC821 3021906WP PWA JT8 JT8D217A 52053NE RT ENGINE FAILED W ASMFD RETURN TO BLOCK RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SW23501AM363618673 49188 708438 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF RIGHT ENGINE WITHOUT ACCELERATION AND PARAMETERS WERE BELOW NORMAL IN IDLE. THE ACCELERATION CHAMBER WAS SERVICED AND FCU WAS LUBRICATED IAW MM 73-00-00, TESTED CORRECT. AIRCRAFT RETURNED TO PLATFORM AGAIN DUE TO THE FAIL CONTINUED. AIRCRAFT WAS SENT TO THE HANGAR AND THE RIGHT FCU WAS REPLACED IAW MM 73-20-01 AND TRIM WAS PERFORMED IAW MM 71-00-00, TESTED CORRECT. 2L74 4J4 F 4A25 E9NE 20050414000452005041400045NE 2005 4 14 ASMF200503015 220050315A7200 ENGINE BOEING737 73773A 1384606NM CFMINTCFM567CFM567B22 13802NE RIGHT MALFUNCTIONED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23906AM 29356 892112 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING RIGHT ENGINE STARTED, N1 WAS INCREASED SLOWLY AFTER EGT INDICATION. THE FAULT ISOLATION PROCEDURE 80-07, TASK 802 WAS PERFORMED AND THE RIGHT ENGINE WAS STARTED IAW MM 71-00-00, TESTED CORRECT. 2L72 4F4 FRTA16WE E00055EN 20050414000462005041400046NM 2005 4 14 ASMF200503022 120050330A21001305901 SELECTOR DOUG MD88 MD88 3023688NM CABIN AIR FAILED W ASMFA UNSCHED LANDING O OTHER CLCLIMB 1 SW23169PL28218 53175 AIRCRAFT RETURNED OF FLIGHT AS A CONSEQUENCE OF BOTH PRESSURIZATION CONTROLLERS WERE OUT OF SERVICE IN AUTOMATIC MODE AND OUT OF SERVICE IN MANUAL MODE WITH VALVE CLOSED AT 100 AND 200 FT OF CLIMB. AIRCRAFT WAS SENT TO THE HANGAR AND CABIN AIR SELECTOR AND CABIN PRESS CONTROL WERE REPLACED IAW MM 21-32-00, TESTED CORRECT. ADDITIONALLY, OUTFLOW VALVE ACTUATOR WAS REPLACED IAW MM 21-32-05, TESTED CORRECT. 2L72 4F RTA6WE 20050414000502005041400050WP 2005 4 14 ASMF200504006 120050408A24209008D093 GENERATOR DOUG DC8 DC821 3021906WP RIGHT FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23501AM11760 49188 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF YAW DAMPER AND ANTISKID LIGHTS TURNED ON. THE POWER RELAY GENERATOR AND AC CROSS TIE RELAY WERE REPLACED IAW MM 24-20-06 CORRECTING THE FAILURE, BUT DURING ENGINES RUNNING TEST WAS NOT POSSIBLE TO CROSS FEED FROM RIGHT GENERATOR TO LEFT GENERATOR. THE REPORT WAS DEFERRED BY MEL. DURING OVERNIGHT SERVICE, THE RELAY R2-83 WAS REPLACED IAW WDM 24-22-00 AND GENERATION TEST WAS PERFORMED IAW MM 24-20-00, ALL CORRECT. DEFERRED REPORT WAS CLOSED. 2L74 4J 4A25 20050414000522005041400052WP 2005 4 14 ASMF200504008 120050409A8011 STARTER DOUG DC9 DC987 3022087WP RT ENGINE MALFUNCTIONED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23755RA 49727 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING RIGHT ENGINE STARTED, THE A AND B IGNITION SYSTEM DID NOT HAVE ROTATION IN N1 AND N2. DURING REVISION, THE RIGHT ENGINE FAN WAS DETECTED JAMMED. THE STARTER WAS DEINSTALLED AND REINSTALLED IAW MM 80-10-01, ALL CORRECT. DURING OVERNIGHT SERVICE, THE RIGHT ENGINE WAS STARTED FOUR TIMES INSPECTING BY FREE ROTATION, BEING ALL CORRECT IAW MPCM 71-00-01. THE STARTER WAS CHECKED AND STARTER DRIVE GEAR SHAFT COUPPLING WAS REPLACED IAW MM 72-61-04 AND THE RIGHT CHIP DETECTORS WERE CHECKED IAW EO 987218, ALL CORRECT. 2L72 4F RTA6WE 20050414000532005041400053WP 2005 4 14 ASMF200504009 120050410A801138334211 STARTER DOUG DC9 DC987 3022087WP LEFT ENGINE FAILED W ASMFK NONE J WARNING INDICATION TXTAXI/GRND HDL 1 SW23214AM7495 49585 DURING ENGINES STARTING, CAPTAIN REPORTED THAT THERE WAS NOT LEFT ENGINE PARAMETERS INDICATION. THE PNEUMATIC PRESSURE AND STARTER VALVE OPENING WERE VERIFIED IAW MM 80-00-00, BEING CORRECT, SO IT WAS DETERMINED THE STARTER REPLACEMENT. THE LEFT ENGINE WAS STARTED IAW 80-10-01, TESTED CORRECT. 2L72 4F RTA6WE 20050414000722005041400072NM 2005 4 14 05FDEA00021 120050105A7810683L220G04 THRUST REVERSER DOUG MD11 MD11 3023602NM ZONE 400 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 NR 3 ENGINE, LT THRUST REVERSER, TRANSLATING COWL, UPPER TRACK, MOST AFT END FOUND WITH CRACKED. THRUST REVERSER P/N 683L220G04, S/N R591-090 NR 3 ENGINE, LT THRUST REVERSER REMOVED AND REPLACED PER AMM 78-33-01-4. THRUST REVERSER DOOR ADJUSTMENT AND CHECK CARRIED OUT PER AMM 78-33-01-700-807. FUCTIONAL TEST CARRIED OUT PER AMM 78-30-00-700-801. COMPLIED WITH ROUTINE WORKCARD NOS.: 78T3003-L AND 78T3903-L 2L73 4F RTA22WE 20050414000762005041400076EU 2005 4 14 05FDEA00035 120050106A5730 SKIN AIRBUS310 A310222 3930315EU RT WING DENTED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25454FE 278 ACCOMPLISH MAINTENANCE C-CHECK, NON-ROUTINE, RT WING - DENTS AND DEBONDS AT LOWER SKIN SURFACE OF T/E OF FLAP INBOARD. REPAIRED IAW AIRBUS REF: 001-57-01-2005-A1B AND IAW EA 6-5750-81828. PAINTED IAW SRM 51-75-10-8. 2L72 4F RTA35EU 20050414000772005041400077EU 2005 4 14 05FDEA00036 120050106A5712 RIB AIRBUS310 A310222 3930315EU LT WING CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25454FE 278 ACCOMPLISH MAINTENANCE C-CHECK, NON-ROUTINE, LT WING - CORROSION FOUND ON UPPER SURFACE STA 1659 RIB 27 TO STA 1713 RIB 28 INTERSECTION WITH STRINGER 12. REPAIRED IAW FAX REF 942-034715/005/2004 DATED 12/27/2004 AND FEDEX EA 6-5710-81827. PERFORMED NDT INSPECTION 51-10-08 PT6. PAINTED IAW SRM 51-75-10-8. 2L72 4F RTA35EU 20050414000792005041400079NM 2005 4 14 SB05002 120050108A323365448105 ACTUATOR BOEING737 737301 1384611NM MLG FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19558AU1507315073 23512 ON CLIMB-OUT FROM CLT, ENROUTE TO DCA, CREW RECEIVED A RT MLG RED LIGHT AFTER GEAR RETRACTION. ALL OTHER GEAR LIGHTS WERE EXTINGUISHED. A SHORT TIME LATER, THE RT MLG GREEN LIGHT ILLUMINATED ALONG WITH THE RED LIGHT. CREW ACCOMP QUICK REF HANDBOOK PROCEDURES AND EXTENDED THE GEAR. CREW RECEIVED NORMAL GEAR IND OF THREE GREEN GEAR LIGHTS AND NO RED LIGHTS. FLT RETURNED TO FIELD AT CLT AND LANDED W/O FURTHER INCIDENT. NO EMERG WAS DECLARED. MX R/R`D RT MLG DOWNLOCK ACT PER MM 32-32-51 AND THE DOWNLOCK AND UPLOCK SENSORS PER MM 32-61-21 AND 32-61-31. ALSO, R/R`D PRINTED CIRCUIT CARDS M981, M982 AND M986 FOR T/S PURPOSES. LUBRICATED GEAR AND PERFORMED OPS CHECK OF RT MLG SEVERAL TIMES. INDICATION AND OPS CHECK G2L72 4F RTA16WE 20050414000802005041400080EU 2005 4 14 05FDEA00052 120050107A2410735874D IDG AIRBUS300 A300B4605R 3930308EU NR 2 GENERATOR FAILED A FDEAC ABORTED TAKEOFF HJ ELECT. POWER LOSS-50 PC WARNING INDICATION TOTAKEOFF 1 SO25653FE 736 ON INITIAL T/O ROLL NR 2 GEN FAULTED. T/O WAS REJECTED AT 70 KTS ESTIMATED. GENERATOR WAS RESET, VOLTS AND FREQS APPEARED NORMAL. SECOND T/O WAS ATTEMPTED GENERATOR FAILED AGAIN ON INITIAL T/O ROLL, IDG 2 FAULT LIGHT WAS FLUCUATING ON AND OFF. RELEASED FOR SERVICE PER MEL/CDL: 24-11-01 CATEGORY: B EXPIRATION: 10JAN05. 2L72 4F RTA35EU 20050414000812005041400081 2005 4 14 EM05001 420050109A2230426000183 CONTROL UNIT EMB ERJ170ERJ170100 EU AUTOTHOTTLE MALFUNCTIONED A USAAO OTHER J WARNING INDICATION NRNOT REPORTED 1 EA19811 1242 000028 AUTO THROTTLE FAIL MESSAGE RECEIVED. MAINTENANCE REMOVED AND REPLACED THRUST CONTROL QUADRANT. CLEARED MEL. 2L74 4F RTA56NM 20050414000892005041400089NM 2005 4 14 2005UALA00072 120050115A5315 FLOORBEAM BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSLEAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29907UA 25007 FLOORBEAM AT STATION 947 HAS CORROSION FROM LBL 14 TO RBL 53. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. SPLICED IN NEW SECTION OF FLOOR BEAM. 2L72 4F4 FRTA16WE E2GL 20050414000902005041400090NM 2005 4 14 2005UALA00073 120050116A5315 FLOORBEAM BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29907UA 25007 STA 986 FLOORBEAM FWD FLANGE HAS CORROSION FROM RBL 16 TO RBL 41. DATA MAJOR CUT-OUT DAMAGE AND INSTALLED REPAIR ANGLE AND FILLER. 2L72 4F4 FRTA16WE E2GL 20050414000972005041400097CE 2005 4 14 DXTA200500571 120050201A2120 ODOR CESSNA750 750 2076810CE CABIN DETECTED E DXTAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 GL07901QS 7500102 CABIN AIR CONDITIONING HAS VERY STRONG ODOR, POSSIBLY DEICE FLUID FUMES. BOTH PAX COMPLAINED OF BURNING EYES AFTER 1+45 FLIGHT. ODOR IS SLIGHTLY LESS EVIDENT IN COCKPIT. REMOVED LT & RT COALESCER SOCKS, CLEANED AND REINSTALLED. RAN AIRCRAFT ON MAX HEAT AT MAX POWER FOR 1/2 HR, REMOVED LT & RT SOCKS, CLEANED AGAIN THEN REINSTALLED. AIR CONDITIONING SYSTEM OPS CHECK GOOD IAW CE 750 MM CH 21-00-00. 2L72 4J RTT00007WI 20050209001332005020900133WP 2005 2 9 DHL2004809530 120050121A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01809DH91189 46047 AFT ACCY COMPT L-34 CORRODED STA 1694. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. TRIMMED OUT CORRODED LONGERON SEGMENT IAW SRM 53-2-2 FIG 8. FABRICATED STANDARD LONGERON SPLICE (AL7075-T6510.100) IAW SRM 53-2-2 FIG 10, TR 53-153, NEW LONGERON SEGMENT (EXTRUSION 1415997) IAW SRM 53-5-3 PG 16. PERFORMED NDT INSPECTION TO STANDARD LONGERON SPLICE IAW NDT SPM PART 08-00-02/07, SRM 53-2-2. GENERAL NOTE ITEM 22 FIG 10 PG 2. CLEANED, TREATED AND PRIMED AREA AND REPAIRED PARTS IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES. INSTALLED REPAIRED PARTS WITH NEW FASTENERS IAW SRM 53-2-2 FIG 8, SRM 53-2-2 FIG 10, SRM 51-1-20D PG 9. TORQUED IAW SRM 51-3-1 PG 2A. 2L74 4F RT4A25 20050228000012005022800001SO 2005 2 28 MASA200500143 120050222A5210 BRACKET EMB 145 EMB145LR 3260212SO PAX DOOR LOOSE A MASAO OTHER O OTHER TXTAXI/GRND HDL 1 SW07826MJ 145214 ASH - CLT HAD A MAIN CABIN DOOR THAT WOULD NOT CLOSE. MAINTENANCE SECURED A BRACKET INSIDE THE DOOR ASSEMBLY. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050224001842005022400184EA 2005 2 24 SWIA200514536 120050212A5610 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAA UNSCHED LANDING O OTHER CLCLIMB 1 NM07453SW 7743 F/O'S WINDSHIELD CRACKED ON CLIMBOUT SIDE OF SLC. REPLACED WINDSHIELD. OPERATIONAL CHECK GOOD. P/N NP139321-12, S/N OFF 02273H6987. 2L72 4F RTA21EA 20050421000092005042100009NM 2005 4 21 AWXA200500170 120050206A2560 BATTERY BOEING737 73733A 1384673NM FLASHLIGHT DISCHARGED A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28164AW 23625 MAINTENANCE FOUND THE AFT GALLEY OUTBOARD EMERGENCY FLASHLIGHT INOPERATIVE. MX REMOVED AND REPLACED THE EMERGENCY FLASHLIGHT. OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050421000122005042100012NM 2005 4 21 2005UALA00133 120050203A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29598UA 28751 EXTERIOR FUSELAGE 2 FT AFT OF EE DOOR FROM STA 540 TO 580 IS DAMAGED. DAMAGE CAUSED BY IMPACT. TEMPORARY BLIND FASTENER REPAIR WAS INSTALLED. THIS REPAIR WAS REMOVED AND REPLACED WITH ANOTHER EXTERNAL DOUBLER REPAIR INSTALLED WITH PERMANENT SOLID FASTENERS. 2L72 4F4 FRTA2NM E17NE 20050421000142005042100014NM 2005 4 21 2005UALA00135 120050210A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29598UA 28751 EXTERIOR FUSELAGE SKIN AT STA 600 TO 620 BETWEEN STR 15L AND 18L HAS 8 EACH DENTS. PARTIAL SKIN REPLACEMENT ACCOMPLISHED. PARTIAL SKIN PANEL REMOVED AND NEW SECTION SPLICED IN USING SPLICE DOUBLERS AND TRIPLERS. 2L72 4F4 FRTA2NM E17NE 20050421000162005042100016NM 2005 4 21 BB05009 120050214A335020131A BATTERY PACK BOEING767 7672B7 1385107NM EMERGENCY LIGHT DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19653US 24894 MAINTENANCE REPORTED THE EMERGENCY LIGHT TRACK AT ROWS 1 THRU 3, RIGHT-HAND SIDE, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT TRACK BATTERY PACK. OPERATIONAL CHECK NORMAL. 2L72 4F RTA1NM 20050421000272005042100027NM 2005 4 21 WRLA2005045 120050216A5530 SKIN DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST RT BARREL NUT HOLE NR 29. (OPEN) 2L73 4F4 FRTA22WE E24NE 20050421000342005042100034NM 2005 4 21 UPS05443937 120050225A3510 LIGHT BOEING747 747121 1384871NM COCKPIT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 F/E O2 REG INOP. *S/D* REMOVED AND REPLACED 02 REG BACKGROUND LIGHTS INOP. FOUND WIRES BROKEN BEHIND FE'S OXY GEN REGULATOR. REPAIRED WIRES WITH REF TO BOEING STD WIRING PRAC MANUA L 20-10-13. LIGHTS OPERATED NORMAL AND PLACARD REMOVED. THIS CLEARS M297824. 2L74 4F A20WE 20050421000372005042100037NM 2005 4 21 SB05030 120050220A521069902913 SEAL BOEING737 7373B7 1384580NM L1 ENTRY DOOR BENT A USAAGB O2 MASK DEPLOYED EMER. DESCENT O OTHER CRCRUISE 1 EA19389US 23311 BWI - FLT428 - ENROUTE FROM CLT TO BWI, CREW REPORTED A LOSS OF CABIN PRESSURE AT FL270. CABIN CREW NOTED A NOISE AROUND THE FORWARD ENTRY DOOR. OXYGEN MASKS DEPLOYED. FLIGHT DESCENDED AND CONTINUED ONTO BWI WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE FORWARD ENTRY DOOR LOWER HINGE SEAL BENT. REPLACED SEAL AND ACCOMPLISHED HULL LEAK DOWN TEST PER MM 05-51-91. TEST WITHIN LIMITS. ACCOMPLISHED PRESSURIZATION CONTROL SYSTEM TEST PER MM 21-31-00. FOUND FORWARD OUTFLOW VALVE COMMANDED CLOSED AT ALL TIMES. REPLACED AFT OUTFLOW VALVE PER MM 21-31-11-4. OPERATIONAL CHECK NORMAL. REPLACED OXYGEN GENERATORS AND REPACKED ALL MASKS. AIRCRAFT OK FOR SERVICE. 2L72 4F RTA16WE 20050422000162005042200016NM 2005 4 22 2005UALA00149 120050213A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29578UA 26694 CREASE NEAR BELLY SKIN CENTERLINE AT BS 1420 (EXTERIOR). SKIN DOUBLER REPAIRS AND STRINGER REPAIRS WERE ACCOMPLISHED. 2L72 4F4 FRTA2NM E17NE 20050422000182005042200018NM 2005 4 22 2005UALA00151 120050213A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29578UA 26694 AFT PIT STA 1360 AT STR 26L FRAME INBD FLANGE IS DENTED. INSTALLED NESTED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20050422000202005042200020NM 2005 4 22 2005UALA00153 120050213A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29578UA 26694 AFT PIT STA 1620, FRAME IS DENTED AT STR 25L ON INBD FLANGE. INSTALLED NESTED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20050422000222005042200022NM 2005 4 22 2005UALA00156 120050213A5315 STIFFENER BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FLOORBEAM CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29652UA 25390 FLOORBEAM AT STA 246 HAS A CRACKED VERTICAL STIFFENER ON FWD FACE OF FLOORBEAM AT APPROX RBL 26.39. CRACKED STIFFENER WAS REPLACED. 2L72 4F4 FRTA1NM E24NE 20050422000242005042200024NM 2005 4 22 2005UALA00158 120050212A3350 CONNECTOR BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE AFT GALLEY DISCONNECTED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29340UA 24244 EEL STRIP AT AFT GALLEY INOPERATIVE. FOUND POWER SOCKET DISCONNECTED. CONNECTED SOCKET. 2L72 4F4 FRTA16WE E2GL 20050422000262005042200026NM 2005 4 22 2005UALA00160 120050215A383015800240 HOUSING BOEING777 777222 1385219NM PWA PW4077PW4077 NE LAVATORY TOILET BROKEN A UALAA UNSCHED LANDING O OTHER CLCLIMB 1 WP29769UA 26921 MALFUNCTIONING LAVATORY. FWD LAV AT DOOR 3L WASTE COMING UP FROM TOILET BOWL IN FLIGHT AT APPROX 3000 FEET. BLOCKAGE ON THE WASTE LINE DOWNSTREAM TO THE WASTE TANK CAUSED ALL THE LAVS ASSOCIATED TO THE WASTE TANK TO BE INOPERABLE. WITH LAV 3L FLUSH VALVE HOUSING BROKEN, WASTE FOUND A PATH TO OVERFLOW. BLOCKAGE WAS SUBSEQUENTLY REMOVED AND DOOR 3L TOILET ASSEMBLY WAS REPLACED. 2L72 4F4 FRTT0001SE E46NE 20050422000282005042200028NM 2005 4 22 2005UALA00162 120050216A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29581UA 26701 AFT CABIN FLOORBEAM HAS CORROSION UPPER CAP STA 1640, RBL 11 TO RBL 12. TYPICAL FLOOR BEAM CORROSION. DAMAGE WAS TRIMMED. NEW SECTION OF FLOOR BEAM WAS SPLICED IN USING SPLICE ANGLES. 2L72 4F4 FRTA2NM E17NE 20050422000322005042200032NM 2005 4 22 2005UALA00166 120050220A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29581UA 26701 CABIN STA 324 FLOORBEAM CORRODED BETWEEN RBL 38 AND RBL 44. TYPICAL FLOORBEAM CORROSION DAMAGE IN THE WET AREAS. FLOOR BEAM T-CAP WAS CUT AND REPAIRED USING ANGLES, FILLERS, AND A STRAP. 2L72 4F4 FRTA2NM E17NE 20050422000342005042200034NM 2005 4 22 2005UALA00169 120050220A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29581UA 26701 CABIN FLOORBEAM CORRODED AT BS 1640, RBL 42-57. DAMAGE CAUSED BY TYPICAL FLOORBEAM CORROSION. FLOORBEAM CAP REPAIRED WITH ANGLE AND FILLERS. 2L72 4F4 FRTA2NM E17NE 20050422000472005042200047EU 2005 4 22 2005UALA00185 120050223A5210 DOOR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE R1 NOISY A UALAA UNSCHED LANDING O OTHER CLCLIMB 1 WP29472UA 1435 RETURN TO FIELD DUE TO LOUD NOISE BY DOOR 1R. ON SECOND ATTEMPT LOUD BANGING DETECTED FROM DOORS 1R AND 1L. APPEARS TO BE NORMAL NOISES FROM FUSELAGE DURING TAKEOFF AND CLIMB. ENGINEERING FLIGHT TEST CREW SHOWED NOTHING ABNORMAL. 2L72 4F4 FRTA28NM E40NE 20050422000502005042200050NM 2005 4 22 05FDEA00348 120050303A534065453136 STRINGER CLIP BOEING727 727227 1384078NM FUSELAGE MISDRILLED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25481FE 21463 BONUS HOLES IN STRINGER CLIP AT BS 950C STR 7L. REPLACED PER SRM 51-30-2 2L73 4F A3WE 20050422000512005042200051NM 2005 4 22 05FDEA00349 120050303A534065453136 STRINGER CLIP BOEING727 727227 1384078NM FUSELAGE MISDRILLED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 BONUS HOLES IN STRINGER CLIP AT BS 950A STR 7L. REPLACED PER SRM 51-30-2 2L73 4F A3WE 20050422000532005042200053EA 2005 4 22 HNAA0500018 120050302A3150JV5 SWITCH DHAV DHC8 DHC8311 1386006EA WARNING SYSTEM INOPERATIVE A HNAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA07326EN 234 ON CLIMB-OUT, BETA WARNING HORN SOUNDED. ALL ENGINE PARAMETERS NORMAL. DEACTIVATED SYSTEM. R&R MICRO SWITCH ACTUATOR AT M/S 3151-S9 IN CENTRAL COLLUM. OPS CHECK GOOD. 2H72 4T RTA13NM 20050422000662005042200066NM 2005 4 22 05FDEA00408 120050307A5713ARB31422 STRINGER DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 RIGHT HAND WING, NR 3 FUEL TANK THRU ACCESS PANEL 635AT, STRINGER 13 FOUND CRACKED OF ABOUT 2.5 INCHES LONG. REPAIRED PER SRM 57-20-00 VOLUME I, FIGURE 10. EXISTING SPLICES AND FABRICATED REPAIR ANGLES INSTALLED PER SRM 51-33-01 VOLUME II. 2L73 4F RTA22WE 20050422000672005042200067EU 2005 4 22 WRNA20050005 120050308A3230C23005302 DAMPENER AIRBUS300 A300B4203 3930306EU LT MLG UNSERVICEABLE A WRNAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO05820SC 154 UPON LANDING GEAR RETRACTION LEFT DOOR AND UNSAFE RED LIGHTS ILLUMINATED. GEAR UP ABNORMAL INDICATION ACCOMPLISHED. AIRCRAFT DIVERTED TO MIAMI INT'L FOR UNSCHEDULED STOP. FOUND LEFT GEAR PITCH DAMPNER BROKEN AT CLEVIS END AND SYSTEM 1 AND SYSTEM 2 LEFT HAND SENSORS BAD. REMOVED AND REPLACED DAMPNER IAW 32-11-15 AND SYSTEM 1 & 2 SENSORS IAW 32-00, OP'S CHECK GOOD IAW 32-32-00. AIRCRAFT RETURNED TO SERVICE 2L72 4F RTA35EU 20050422000752005042200075NM 2005 4 22 05FDEA00433 120050308A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 FRAME IS DENTED ON I/B FLANGE AT BS 500 BETWEEN STR'S 23 LT AND 25 LT. REMOVED DAMAGE ON FRAME BS 500 BETWEEN STR 23L AND 25L. FABRICATED DOUBLER, MATERIAL 7075-T6 0.63", LOT #181795 IAW SRM 51-40-3, ALODINED, PRIMED, INSTALLED PER SRM 51-20-2, MM 51-20-151-7, SRM 51-30-2 2L73 4F RTA3WE 20050422000772005042200077NM 2005 4 22 05FDEA00434 120050308A5340 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE MISDRILLED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25481FE 21463 BONUS HOLES IN STRINGER CLIP AT BS 970 STRINGER 7R. REPLACED EPR SRM 51-30-2. 2L73 4F RTA3WE 20050425001732005042500173NM 2005 4 25 2005UALA00113 120050131A2133106120921 RELIEF VALVE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN PRESSURE OUT OF ADJUST A UALAA UNSCHED LANDING O OTHER CRCRUISE 1 WP29386UA 24661 FLIGHT DIVERTED TO CMH DUE TO LOSS OF CABIN PRESSURE. THE INBOARD SAFETY RELIEF VALVE FAILED OPERATIONAL TEST AND WAS REPLACED. THE CABIN PRESSURE CONTROLLER WAS ALSO REPLACED PRECAUTIONARY. 2L72 4F4 FRTA16WE E2GL 20050425001772005042500177NM 2005 4 25 2005UALA00168 120050220A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29581UA 26701 CABIN LT FLOORBEAM CORRODED FROM STA 680-740 LBL 60-LBL64. 2L72 4F4 FRTA2NM E17NE 20050425001872005042500187EA 2005 4 25 QXEA200500263 120050216A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 200 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - FUSELAGE EXTERIOR, STATION 310 AND STRINGER 15L HAS SCRATCHES ON FUSELAGE SKIN, FORWARD OF PASSENGER DOOR CUTOUT. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01 AND REO 670-53-21-073. 2L72 4F RTA21EA 20050425001982005042500198WP 2005 4 25 IXXA0500017O 120050305A2750 CABLE DOUG DC8 DC871F 302199DWP TE FLAPS LOOSE A IXXAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SW11829BX 45994 UPON APPROACH TO SCHEDULED LANDING AT KTOL, FLAP SELECTOR HANDLE WOULD ALLOW 5 DEGREES TO BE SELECTED AND STOP. AFTER STAYING IN HOLDING PATTERN FOR APPOX 15-20 MINUTES FLAPS OPERATED NORMALLY. AIRCRAFT MADE UNEVENTFUL LANDING IN KTOL. UPON INSPECTION MX NOTED CABLE HAD COME OFF PULLEY IN GYRO BAY. MX REPOSITIONED CABLE AND PERFORMED NUMEROUS, OPS CHECK OF FLAP SYSTEM. SYSTEM CHECKED NORMAL AND AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20050425002102005042500210NM 2005 4 25 05018 120050304A2150 DUCT BOEING747 747246F 1384850NM NR 1 ACM CONTAMINATED A KCSAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL23705CK 21034 AC SMOKE IN COCKPIT WAS TERMINATED. CK LIST QRH, PG 3 ACCOMPLISHED. CONTINUED FLIGHT WITH PACK NR 1 OFF. FOUND OIL CONTAMINATION IN NR 1 ACM DUCTING. CLEANED PER AMM 21-00-01. NO OIL ODOR NOTED AFTER CLEANUP. 2L74 4F RTA20WE 20050425002172005042500217NM 2005 4 25 UPS05444347 120050411A5320BAC15113790 STRAP BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 INSPECTION TYPE:C M/D BS 1680 BETWEEN STR 11-12R FRAME O/B CHORD ATT STRAP FOUND CRACK ( CRACK LENGTH .3125 INCH). M/D BS 1680 BETWEEN STR 5R TO STR 12R FRAME ATTACH STRAP REPLACED AS PER SRM 51-10-01 PG 9 2L74 4F RTA20WE 20050425002202005042500220NM 2005 4 25 UPS05644351 120050424A2560 SMOKE GOGGLES BOEING767 76734AF 1385212NM COCKPIT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01301UP 27239 INSPECTION TYPE:N/A F/O'S SMOKE GOGGLES CRACKED LENS. RR'D F/O'S SMOKE GOGGLES. OK FOR SERVICE. 2L72 4F RTA1NM 20050425002272005042500227WP 2005 4 25 UPS05844258 120050321A5531 RIB DOUG DC8 DC873F 302199FWP VERTICAL STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 C2 VER. FIN L/E HAS CRACKED RIB 3/4 INCH AT ACCESS PNL 51I. STOP DRILLED CRACK IAW DC-8 SRM 55-02-00. REPAIRED RIB IAW 55-02-00, 51 -1-20D, AND 51-3-0. 2L74 4F RT4A25 20050425002302005042500230NM 2005 4 25 UPS05544312 120050417A2560 SMOKE GOGGLES BOEING757 75724APF 1384969NM COCKPIT BROKEN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01432UP 25463 INSPECTION TYPE:N/A CAPTAINS SMOKE GOGGLES BROKE. REPLACED CAPTAINS SMOKE GOGGLES AS REQUIRED. 2L72 4F RTA2NM 20050425002352005042500235WP 2005 4 25 UPS05844296 120050408A5320 SPLICE DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 INSPECTION TYPE:C1 SPLICE FITTING CRACKED ON L31R AT STA 450. REMOVED AND REPLACED SPLICE FITTING IAW SRM 51-1-20D AND 51-1-21. 2L74 4F RT4A25 20050425002382005042500238WP 2005 4 25 AALA20050261 120050412A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21957U 49702 ATL - FORWARD ENTRY OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT B523 FOR FORWARD ENTRY OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050425002412005042500241NM 2005 4 25 AALA20050258 120050412A3350D71702001 BATTERY PACK BOEING777 777223 1385213NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21779AN 29955 ORD - SEAT MOUNTED EMERGENCY LIGHTS IN FORWARD SECTION IS INOPERATIVE. REPLACED BATTERY PACKS AT M33401 AND M33404 AND REPLACED SOCKETS AT SEAT 20C FOR SEAT MOUNTED EMERGENCY LIGHTS IN FORWARD SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20050425002462005042500246NM 2005 4 25 AALA20050243 120050405A3350 LIGHT BOEING777 777223 1385213NM CABIN DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21795AN 30257 MIA - EMERGENCY LIGHT MOUNTED ON FIRST CLASS CLOSET DOOR FRAME DAMAGED. REPLACED EMERGENCY LIGHT MOUNTED ON FIRST CLASS CLOSET DOOR FRAME. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20050425002562005042500256WP 2005 4 25 ABXA050088 120050407A5330991556173 DOUBLER DOUG DC9 DC941 302207NWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23973AX 47511 DURING ROUTINE LINE MAINTENANCE, FOUND THE FUSELAGE DOUBLER BETWEEN EXTERIOR SKIN AND JACK PAD FITTING AT STA 1072, LONGERON 30, CORRODED BEYOND LIMITS. REPLACED DOUBLER IAW DC-9 SRM 51-30-3 AND 51-30-2. 2L72 4F A6WE 20050425002582005042500258NM 2005 4 25 AWXA200500481 120050421A3397BMS13311122 WIRE BOEING737 7373G7 1384595NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28157AW 23779 PHX - EEL - DURING 4-DAY CHECK FOUND EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 13 LT INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRING SPLICE FOR EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 13 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050425002682005042500268NM 2005 4 25 AWXA200500465 120050328A532065317876 CHANNEL BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - DURING C-19 CHECK CORROSION WAS FOUND ON L-1 DOOR ENTRYWAY INNER CHORD UPPER CHANNEL BETWEEN BS 316 AND BS 341, LBL 62, WL 209. MAINTENANCE REMOVED CORRODED UPPER CHANNEL ON INNER CHORD FROM BS 316 TO BS 341 AT LBL 62; FABRICATED A NEW REPLACEMENT CHANNEL PER DWG 65-17688; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050425002722005042500272NM 2005 4 25 AWXA200500431 120050313A5320652072616 ATTACH ANGLE BOEING737 737375 13844BNNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 MCN - MAJOR REPAIR - DURING C-05 CHECK CORROSION WAS FOUND ON FORWARD CARGO COMPARTMENT THRESHOLD UPPER ATTACH ANGLE FOR INTERCOSTAL AT BS 474, STR 25 RT. MAINTENANCE REMOVED CORRODED ATTACH ANGLE AT BS 474, STR 25 RT; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 65-20726; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050425002732005042500273NM 2005 4 25 AWXA200500433 120050408A3397BR963280 WIRE BOEING737 7373S3 1384711NM CABIN BACKED OUT A AWXAK NONE BL SMOKE/FUMES/ODORS/SPARKS NO TEST ININSP/MAINT 1 WP28313AW 23712 PHX - EEL - DURING 4-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 2 LT INOPERATIVE. MAINTENANCE FOUND WIRE PULLED OUT OF RECEPTACLE WITH EVIDENCE OF ARCHING. REPLACED EMERGENCY ESCAPE PATH LIGHT WIRE HARNESS AT SEAT ROW 2 LT, OPERATIONAL WAS GOOD. 2L72 4F RTA16WE 20050426000082005042600008NM 2005 4 26 DHL2005781519 120050213A5320 INTERCOSTAL BOEING727 727227 1384078NM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A "C" CHECK, AFT CARGO CORROSION ON INTERCOSTAL STA 1150 TO 1166 O/B OF 26R. EVALUATED ANGLE FROM BS 1150 TO 1166 AND FOUND IT TO BE OUT OF LIMITS IAW 727 SRM 53-10-1 FIG 5. REMOVED ANGLE FROM BS 1150 TO 1166 IAW 727 SRM 51-30-2. FABRICATED ANGLE FROM 7075 T6 .050 PO NR 9001777 14 1/8 INCH BY 2 INCH IAW 727 SRM 53-10-2 FIG 5 AND 51-20-1. TREATED AND PRIMED ANGLE AND BARE METAL IAW 727 SRM 51-10-2. INSTALLED ANGLE IAW 727 SRM 51-30-2. 2L73 4F A3WE 20050426000122005042600012EU 2005 4 26 WRNA200500004 120050305A2830 VALVE AIRBUS300 A300B4203 3930306EU FUEL SYSTEM MALFUNCTIONED A WRNAJ DUMP FUEL O OTHER CRCRUISE 1 SO05501TR 53 UPON PERFORMING EMERGENCY PROCEDURES FOR A LOW SPEED AILERON FAULT, WHEN STARTING TO DUMP FUEL FOR A RETURN TO BASE LANDING, RT FUEL JETTISON VALVE MI CROSSHATCHED DURING FUEL JETTISON. DEFERRED JETTISON RT VALVE MI IAW MEL 28-31-01 CAT "C" EXPIRES 3-15-05. PLACARD INSTALLED UPDATE. 3-8-05 REMOVED AND REPLACED RT VLVE FUEL JETTISON MI INDICATOR, OPS CHECK GOOD I/A/W 28-00-00. CLEAR MEL, PLACARD REMOVED. A/C RETURNED TO SERVICE. 2L72 4F RTA35EU 20050426000232005042600023NM 2005 4 26 0500276730 120050222A5330 SKIN BOEING747 7472J9F 1384806NM FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01630US 21668 DURING SPECIAL VISIT, FOUND CRACKS IN FUSELAGE SKIN AT BS 341-342 BELOW S7R. REPAIRED PER EA 67-202958. 2L74 4F RTA20WE 20050426000252005042600025NM 2005 4 26 0500285521 120050202A5347 SEAT TRACK BOEING757 757251 1384970NM FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01521US 23209 DURING "H" CHECK, FOUND CORROSION ON SEAT TRACK AT BS 378 LBL 25. REPAIRED PER EA 55-202113. 2L72 4F RTA2NM 20050426000262005042600026EU 2005 4 26 05FDEA00421 120050308A5347 SEAT TRACK AIRBUS310 A310 EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 NR 4 SEAT TRACK LT OF CENTER FROM FS 16 TO FS 18 HAS CORROSION REF N00519. REMOVED AND REPLACED SEAT TRACK FROM FS 16 TO FS 18 IAW SRM 51-40-21 AND EA 6-5310-86038. 2L72 4F RTA35EU 20050426000272005042600027EU 2005 4 26 05FDEA00422 120050308A5522 SKIN AIRBUS310 A310 EU LT ELEVATOR DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 REPAIR FUSELAGE AT LT ELEVATOR T/E AFT FROM OB END HAS NO DATA REF N00806. REMOVED AND INSTALLED CORRECT REPAIR IAW EA 6-5100-87090 REF A310 SRM 55-21-11, REPAIR NR 5 G. 2L72 4F RTA35EU 20050426000282005042600028EU 2005 4 26 05FDEA00423 120050308A5730 SKIN AIRBUS310 A310 EU RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 RT WING T/E SKIN HAS A .4 CRACK ON IB CORNER OF CUTOUT FOR PANEL 681 AB REF N00265. REPAIRED SKIN IAW EA 6-5710-86028. 2L72 4F RTA35EU 20050426000292005042600029EU 2005 4 26 05FDEA00424 120050308A5280 DOOR AIRBUS310 A310 EU NLG DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 NOSE LANDING GEAR DOORS HAS STRUCTURAL DAMAGE REF N00748. REPAIRED RT GEAR DOORS IAW SRM 52-82-11 C1 FIG 201. 2L72 4F RTA35EU 20050426000302005042600030EU 2005 4 26 05FDEA00426 120050308A5712 RIB AIRBUS310 A310 EU RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 RT WING L/E UPPER SIDE OF PANEL LANDING, LANDING FOR PANEL HAS 2 EA CRACKS AT 11 IN I/B OF RIB 14 AND 11 IN O/B OF RIB 14 REF N00631. REMOVED AND REPLACED PANEL LANDING IAW SRM 51-40-21 AND DRW A57244165. 2L72 4F RTA35EU 20050426000342005042600034EU 2005 4 26 05FDEA00443 120050308A5753 FLAP TRACK AIRBUS310 A310 EU RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 RT WING FLAP O/B UPPER SURFACE AT NR 3 FLAP TRACK AND NR 4 FLAP TRACK HAS 2 EA AREAS OF NOTED CORROSION REF N00771. REMOVED CORR IAW SRM 51-74-10, FOUND IN LIMITS IAW SRM 57-53-12. 2L72 4F RTA35EU 20050426000352005042600035EU 2005 4 26 05FDEA00444 120050308A5347A5327828620600 ADAPTER AIRBUS310 A310 EU ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 MDCC ZONE 250, FR 55/58 BETWEEN LT SEAT TRACK 2 - 3, 1 EA, CLS ADAPTER BROKEN. REMOVED AND REPLACED CLS ADAPTER IAW A310-200 SRM 51-72-10. 2L72 4F RTA35EU 20050426000362005042600036EU 2005 4 26 05FDEA00445 120050308A5347A538131742000 ADAPTER AIRBUS310 A310 EU ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 MDCC ZONE 241, FR 39, BETWEEN NR 2 - 3 RT SEAT TRACK LCS ADAPTER HAS 1 AREA OF CORROSION INSIDE SCALLOP HOLE. REMOVED AND REPLACED CLS ADAPTER IAW A310-200 SRM 51-72-10. 2L72 4F RTA35EU 20050426000382005042600038EU 2005 4 26 05FDEA00448 120050308A5310 STRUCTURE AIRBUS310 A310 EU CARGO FLOOR CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25446FE 224 AFT PIT UNDER FLOOR FROM 12 INCH FWD OF FS 59 TO 3 INCHES FWD OF FS 59 STG44L HAS CORROSION. REMOVED CORROSION IAW A310-200 SRM 51-74-10. THE AREA WAS FOUND OUT OF LIMITS IAW A310-200 SRM 53-10-00. REPAIRED STRINGER IAW A310-200 SRM 53-10-14. TREATED, PRIMED AND TOPCOATED IAW A310-200 SRM 51-23-10. 2L72 4F RTA35EU 20050426000402005042600040EU 2005 4 26 05FDEA00450 120050308A5330 SKIN AIRBUS310 A310 EU FUSELAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25446FE 224 AFT PIT UNDER FLOOR 16 INCH FWD OF FS 54.1, STG 47R HAS CORROSION. REMOVED CORROSION IAW A310-200 SRM 51-74-10. AREA WAS OUT OF LIMITS IAW A310-200 SRM 53-10-00. REMOVED AND REPLACED DAMAGED AREA IAW A310-200 SRM 53-10-14. TREATED, PRIMED, TOPCOATED IAW A310-200 SRM 51-21-10. SEALED AREA IAW A310-200 SRM 51-76-00. 2L72 4F RTA35EU 20050426000422005042600042EU 2005 4 26 05FDEA00452 120050308A5322 SHEAR TIE AIRBUS310 A310 EU FUSELAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25446FE 224 BULK PIT UNDER FLOOR STG 55L FROM FS 65 TO FS 66 HAS CORROSION AND CORROSION. EXTENDS BETWEEN SPLICE ANGLE AND STG AND UNDER SHEAR TIE AT FS 66. REMOVED CORROSION IAW A310-200 SRM 51-74-10. STRINGER CORRODED BEYOND ALLOWABLE LIMITS AS PER A310-200 SRM 51-10-00. CUT AND REPAIRED STRINGER IAW A310-200 SRM 53-10-14. REMOVED AND REPLACED PRODUCTION SPLICE AT FRAME 65 IAW A310-200 SRM 51-72-10 AND 51-40-21. 2L72 4F RTA35EU 20050426000432005042600043EU 2005 4 26 05FDEA00453 120050308A5510 ANGLE AIRBUS310 A310 EU HORIZONTAL STAB CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25446FE 224 THS ACTUATOR STRUCTURAL HOUSING HAS APPROX 12 INCH OF CORROSION (10 EA. AREAS). REMOVED CORROSION IN 10 EA AREAS ON THS ACTUATOR STRUCTURAL HOUSING. ALL AREAS WERE WITHIN LIMITS EXCEPT AREA 10 WHICH WAS OUT OF LIMITS IAW A310-200 SRM 53-10-00. REMOVED L-ANGLE IAW A310-200 SRM 51-40-21 AND INSTALLED NEW L-ANGLE IAW A310-200 SRM 51-72-10 AND DRAWING NR A534-72550. 2L72 4F RTA35EU 20050426000442005042600044EU 2005 4 26 05FDEA00454 120050308A5347A5378193620200 ADAPTER AIRBUS310 A310 EU ZONE 200 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 MAIN CABIN FRAME 36, CLS ADAPTER -Y60 IS GOUGED, BETWEEN SEAT TRACK 3 - 4 LT. REMOVED AND REPLACED CLS ADAPTER IAW A310-200 SRM 51-72-10. 2L72 4F RTA35EU 20050426000452005042600045EU 2005 4 26 05FDEA00455 120050308A5347A5327541120300 ADAPTER AIRBUS310 A310 EU ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 MDCC ZONE 251 FS 60 BETWEEN RT SEAT TRACK NR 4 - 5, 1 - EA. CLS ADAPTER BROKEN. REMOVED AND REPLACED CLS ADAPTER IAW A310-200 SRM 51-72-10. 2L72 4F RTA35EU 20050426000462005042600046EU 2005 4 26 05FDEA00456 120050308A5751A5724279520000 PLATE AIRBUS310 A310 EU ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 LEFT WING LOWER AILERON ACCESS DOOR LANDING PLATE HAS CRACK IN IT. REMOVED CRACKED LANDING AND INSTALLED A NEW LANDING IAW A310-200 SRM 51-72-10. 2L72 4F RTA35EU 20050426000472005042600047EU 2005 4 26 05FDEA00457 120050308A5310A5381318420000 CROSSBEAM AIRBUS310 A310 EU ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 MDCC ZONE 250, FS 54.2 BETWEEN LT SEAT TRACK 4 -5, LATERAL STUCTURE HAS CORROSION AT SCREW HOLES. REMOVED AND REPLACED CROSS BEAM IAW A310-200 SRM 51-72-10. 2L72 4F RTA35EU 20050426000482005042600048EU 2005 4 26 05FDEA00458 120050308A5347A5381114620200 SEAT TRACK AIRBUS310 A310 EU ZONE 200 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 MDCC ZONE 250, FS 54.2 LT SEAT TRACK NR 3 HAS GOUGES ON SCALLOP HOLE 1 - EA AREA. REMOVED AND REPLACED SEAT TRACK FITTING IAW A310-200 SRM 51-72-10. 2L72 4F RTA35EU 20050426000492005042600049WP 2005 4 26 05FDEA00464 120050309A5712NRD60371 RIB DOUG DC10 DC1010 3022110WP ZONE 500 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25369FE 46607 COMPLY WITH EA 8-5710-55459, REWORK OF GOUGES IN WING LEADING EDGE RIB PN NRD6037-1. CLOSING ACTION ON 03/09/05. ON NR S00019. COMPLIED WITH EA 8-5710-55459. 2L73 4F A22WE 20050426000502005042600050CE 2005 4 26 DXTA200500618 120050308A2720 RUDDER CESSNA560 560XL 2076702CE HORIZONTAL STAB MALFUNCTIONED E DXTAA UNSCHED LANDING S AFFECT SYSTEMS CRCRUISE 1 GL07679QS 5605279 AIRCRAFT REQUIRES EXCESSIVE EFFORT FOR RUDDER CONTROL IN HIGH POWER SETTINGS ON GROUND AND INFLIGHT "AIRSPEED IS NOT AN ISSUE". FEELS AS IF YAW DAMPER IS ON, SUSPECT RUDDER BIAS SYSTEM. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20050426000512005042600051NM 2005 4 26 DXTA200500619 120050309A3231 DOOR GULSTM200 200 4500308NM MLG ICED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07703QS 060 RT MAIN GEAR WILL NOT LOCK UP. WHILE ACCOMPLISHING INCOMING INSP TO ACFT FOUND ICE TO BE FORMED ON I/B GEAR DOOR OF RT MLG. SUSPECT ICE BUILT UP TO CAUSE DOOR INTERFERANCE TO STRUCTURE AND NOT ALLOW DOOR TO FULLY UP AND LOCK. VERIFIED INTEGRITY OF SWITCHES. NO DEFECTS NOTED IAW G200 M/M 32-30-00. 2L72 4F RTA53NM 20050426000522005042600052CE 2005 4 26 DXTA200500617 120050307A3260 LANDING GEAR CESSNA750 750 2076810CE MAINS FALSE INDICATIONE DXTAO OTHER N FALSE WARNING APAPPROACH 1 GL07905QS 7500105 GEAR EXTENDED PREMATURELY. UPON MOVING THE GEAR HANDLE ONLY A SMALL AMOUNT BUT NOT FULLY OUT OF THE DETENT, IN THE UP POSITION THE GEAR STARTED EXTENDING. PLACED AIRCRAFT ON JACKS, CYCLED GEAR HANDLE SEVERAL TIMES. NO DISCREPANCIES NOTED AT THIS TIME. WORK DONE IAW 750 M/M CH 32-30-00. 2L72 4J RTT00007WI 20050426000532005042600053EU 2005 4 26 05FDEA00465 120050309A5347A5378193720000 ADAPTER AIRBUS310 A310 EU ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 MAIN CABIN AT FRAME 38 CLS ADAPTOR, -YE15 HAS 1EA AREA OF CORROSION (BETWEEN SEAT TRACK LAND 2 LT) 2L72 4F RTA35EU 20050426000542005042600054EU 2005 4 26 05FDEA00466 120050309A5542A5547156000000 PANEL AIRBUS310 A310 EU ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 CORROSION AROUND FASTERNER HOLES, LEFT AND RIGHT SIDE TOP OF RUDDER, PANEL 326AT REMOVED TO REPAIR STATIC WICK BASE N00238. 2L72 4F RTA35EU 20050426000552005042600055EU 2005 4 26 05FDEA00467 120050309A5347 SEAT TRACK AIRBUS310 A310 EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 MDCC RT NR 5 SEATRACK, FS 78 FS 78.5 HAS 2 AREAS OF CORROSION INSIDE SCALLOPED HOLES. REPLACED SEAT TRACK IAW A310-200 SRM51-72-10, FABRICATED NEW SEAT TRACK IAW DRAWING A53279232, REMOVED REINSTALLED FLOORBOARDS IAW A310 AMM 53-10-21. REMOVED, REINSTALLED GILL LINERS IAW A310 AMM 25-58-22-4, APPLIED DINATROL ON SEAT TRACK IAW A310-200 SRM 51-75- 10. 2L72 4F RTA35EU 20050426000562005042600056EU 2005 4 26 05FDEA00468 120050309A5347 SEAT TRACK AIRBUS310 A310 EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 MDCC SONE 252 RT NR 4 SEAT TRACK FS 68 FS 69.5 FS 70.5 HAS 3 AREAS OF CORROSION INSIDE SCALLOPED HOLES. REMOVED DAMAGED SEAT TRACK SECTION AND REPLACED WITH NEW SEAT TRACK SECTION FROM FRAME 69.5 TO FRAME 71.5 IAW A31-200 SRM 51-10-16 FIG 208 RT NR 4 RESTORED SURFACE PROTECTION IAW A310-200 SRM 51-23-00 AND SRM 51-21-10. APPLIED LUBRICANT RUST INHIBITOR TO REPAIR AREA IAW A3140-200 SRM 51-23-00. 2L72 4F RTA35EU 20050426000572005042600057EU 2005 4 26 05FDEA00469 120050309A5410 BRACKET AIRBUS310 A310 EU NR 1 PYLON CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 NR 1 PYLON OTBD SIDE UPPER AREA RIB 15A BRACKET ON LWR AREA HAS CORROSION EXTENDING UNDER FASTENERS FOR NUT PLATE. CORROSION REMOVED IAW A310 SRM 51-74-10, NDT MATERIAL THICKNESS AFTER THICKNESS IS OUT OF LIMITS. REMOVED AND REPLACED BRACKET AND 3EA NUTPLATES IAW A310 SRM 51-72-10 AND SRM 51-40-21. 2L72 4F RTA35EU 20050426000582005042600058EU 2005 4 26 05FDEA00470 120050309A5347 SEAT TRACK AIRBUS310 A310 EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 MDCC ZONE 252 RT NR 4 SEAT TRACK HAS AREA OF CORROSION INSIDE SCALLOPED HOLE (1- AREA ONLY) AT FRAME 64.5. REMOVED CORROSION IAW A310-200 SRM 51-74-10 FOUND CRACK, FABBED REPAIR SECTION AND SPLICED IAW A310-200 SRM 51-10-16 FIG 208 AND SRM 51-40-40. REMOVED OLD SECTION OF SEAT TRACK IAW A310-200 SRM 51-72-0 TREATED PRIMED AND TOP COATED NEW SECTION IAW A310-200 SRM 51-21-10 HEAT TREATED RIVETS IAW A310-200 SRM 51-25-00. INSTALLED SEAT TRACK SECTION IAW A310-200 SRM 53-10-16 FIG 208 AND SRM 51-40-20. 2L72 4F RTA35EU 20050426000592005042600059EU 2005 4 26 05FDEA00471 120050309A5540A5547155821300 BRACKET AIRBUS310 A310 EU ZONE 300 LIGHTNING STRIKEA FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 LIGHTNING STRIKE TO BRACKET TOP OF RUDDER RIGHT SIDE FOUND AFTER REMOVAL OF PANEL 326AT FOR STATIC WICK REPAIR NOO238. REMOVED AND REPLACED COUPLING IAW A310-200 SRM 51-40-21, TOPCOATED COUPLING IAW A310-200 SRM 51-75-10. 2L72 4F RTA35EU 20050426000602005042600060EU 2005 4 26 05FDEA00472 120050309A5330 SKIN AIRBUS310 A310 EU FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 REPAIR NEEDS EVALUATION FOR FAA APPROVED DATA AND MAJOR OR MINOR CLASSIFICATION. ITEM NR 8 ON LIST FUSELAGE, LT SIDE FR77 AT 3 O'CLOCK POSITION. REPAIRED DENT AREA IAW A310 SRM 53-10-12 FIG 112 AND 51-73-10 PARA. 7 FIG 4. TREATED BARE METAL IAW A310 SRM 51-21-10. 2L72 4F RTA35EU 20050426000612005042600061EU 2005 4 26 05FDEA00473 120050309A5320A5398675120400 STRAP AIRBUS310 A310 EU ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 REF. SNRM NR N00844 BETWEEN FR 86 AND FR 87 STG 34L (LT) INTERCOSTAL IS BENT ANGLE STRAP FOUND TO BE CRACKED REMOVED AND REPLACED WITH NEW ANGLE IAW A310 SRM 51-40-21. 2L72 4F RTA35EU 20050426000632005042600063EU 2005 4 26 05FDEA00475 120050309A5320 INTERCOSTAL AIRBUS310 A310 EU FUSELAGE BENT A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25419FE 345 BETWEEN FR 84 AND FR 85 STG 34L INTERCOSTAL IS BENT. INTERCOSTAL ANGLE HAS BEEN REMOVED AND REPLACED IAW A310-200 SRM 51-40-21. 2L72 4F RTA35EU 20050426000642005042600064EU 2005 4 26 05FDEA00476 120050309A5347 SEAT TRACK AIRBUS310 A310 EU FUSELAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25419FE 345 MDCC ZONE 241, RT SEAT TRACK NR 5, FR39.5, HAS 1-AREA OF CORROSION INSIDE SCALLOPED HOLE. REMOVED DAMAGED SEAT TRACK AND REPLACED WITH NEW SEAT TRACK P/N A53810820000IAW A310-200 SRM 51-72-10. 2L72 4F RTA35EU 20050426000652005042600065EU 2005 4 26 05FDEA00477 120050308A5330 SKIN AIRBUS310 A310 EU FUSELAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25446FE 224 BULK PIT UNDER FLOOR AREA FR69 STG48L HAS AN AREA THAT EXTEND 2" FWD OF FR 69 OF CORROSION EXTENDING UNDER SHEAR TIE. REMOVED SHEAR TIE AND STRINGER SECTION IAW A310-200 SRM 53-10-14. INSTALLED SHEAR TIE AND STRINGER SECTION IAW A310-200 SRM 53-10-14. 2L72 4F RTA35EU 20050426000662005042600066EU 2005 4 26 05FDEA00478 120050309A5347 SEAT TRACK AIRBUS310 A310 EU FUSLEAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25419FE 345 M DECK CARGO COMPT LT NR 4 SEAT TRACK, FR 48, FR 49, FR 50, FR 52.5, FR 53.5 CORROSION INSIDE SCALOPE HOLES 5-AREAS AS MARKED. REMOVED CORROSION IAW SRM 51-74-10. OUT OF LIMITS IAW A310 SRM 53-10-16 FIG 101. CUT AND REMOVED BAD SECTION OF SEAT TRACK FROM FR 49.5 TO FR 45.5 LT NR 4 IAW A310 SRM 53-10-10 FIG 205. FABBED NEW REPAIR SPLICES IAW SRM 53-10-16 FIG 205. 2L72 4F RTA35EU 20050426000672005042600067EU 2005 4 26 05FDEA00479 120050309A5347 ADAPTER AIRBUS310 A310 EU FUSELAGE CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25419FE 345 MDCC ZONE 241, BETWEEN RT SEAT TRACK 2-3 FR 43, 1-EA. CLS ADAPTER HAS CRACKED UNDERNEATH. REMOVED AND REPLACED CLS ADAPTER IAW A310 SRM 51-72-10. 2L72 4F RTA35EU 20050426000682005042600068EU 2005 4 26 05FDEA00480 120050309A5347 SEAT TRACK AIRBUS310 A310 EU FUSELAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25419FE 345 M DECK ZONE 240, LEFT NR 2 SEAT TRACK, FR47, FR51, FR51.5, FR52.5, FR53 AND FR54, CORROSION INSIDE SCALLOPED HOLES, 6-AREAS. BLENDED CORROSION PER A310 SRM 51-74-10 MEASURED MATERIAL LOSS AND FOUND ALL AREAS WITHIN LIMITS EXCEPT FOR AREAS AT FRS 51.5 AND 52.5 WERE OUT OF LIMITS PER A310 SRM 53-10-16 FIG 101, CUT OUT AND REMOVED DAMAGED SEAT TRACK SECTION FROM FRAMES 50.5 TO PRODUCTION END AT FRAME 54, FABRICATED SEAT TRACK SECTION AND SPLICES, DRILLED AND INSTALLED PER A310 SRM 53-10-16 PARA 5.D FIG 205, TREATED, PRIMED AND TOPCOATED PER A310 SRM 51-75-10. 2L72 4F RTA35EU 20050426000692005042600069NM 2005 4 26 F3LA200500009 120050308A5320 INTERCOSTAL BOEING737 7373L9 1384470NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03313FL 4372 26442 DURING C-4 CHECK INSPECTION, REPORTED INTERCOSTAL AT BS 950, RBL 20 TO RBL 40, CORRODED. FOUND TO BE OUT OF LIMITS PER SRM 53-60-51. REPLACED INTERCOSTAL PER SRM 51-40-05, 51-40-02, AND 53-60-51. 2L72 4F RTA16WE 20050426000702005042600070NM 2005 4 26 F3LA200500011 120050308A524069584321 ROLLER BOEING737 73736N 1384408NM GUIDE ARM WORN A F3LAK NONE O OTHER ININSP/MAINT 1 NM03306FL 3166 28563 MAINTENANCE REPORTED R1 DOOR HARD TO CLOSE. REPLACED GUIDE ARM ROLLER PER MM 52-61-20. ADJUSTED R1 DOOR PER MM 52-41-00. REMOVED AND REINSTALLED R1 DOOR SLIDE PER MM 25-61-35. REMOVED AND REINSTALLED R1 DOOR LINER PER MM 52-41-31. REMOVED AND REINSTALLED R1 DOOR PER MM 52-41-00. 2L72 4F RTA16WE 20050426000712005042600071NM 2005 4 26 DHL2005781523 120050211A5730 SKIN BOEING727 727227 1384078NM LT WING GOUGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A "C" CHECK, LT WING UPPER SURFACE GOUGED 1 INCH AFT OF NR 2 SLAT O/B SLAT HOOK RETAINER. REMOVED PAINT AT AFFECTED AREA IAW B727 B772 51-20-1. INSPECTED AREA USING C/3 ULTRSONIC THICKNESS GOUGE ORIGINAL THICKNESS OF 0.040 MATERIAL LOSS OF 0.0102 INCH, MAT REMAINING IS 0.0298 AREA FOUND TO BE OUT OF LIMITS IAW B727 SRM 57-20-01 FIG 1. REMOVED FASTENERS FOR ACCESS IAW B727 SRM 51-30-2. CUT OUT EXISTING FILLER STRIP DIMENSION 71/2 INCH BY 1 1/2 INCH IAW B727 SRM 57-30-4 FIG 9. FAB`D REPAIR AT SLAT HOOK MAT USED 0.038 CRESS AISI 301 1/2 HAND AND PO NR 9001628 DIM 7 1/2 BY 1 1/2 DIM OF THE DOUBLER 7 1/2 BY 4 1/2 IAW B727 SRM 57-30-4 FIG 9. PRIMED AREA AND PARTS IAW B727 SRM 51-10-2. INSTALLED REPAIR I2L73 4F A3WE 20050426000722005042600072NM 2005 4 26 DHL2005781524 120050218A5313 STRINGER BOEING727 727227 1384078NM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A "C" CHECK, STRINGER 30 AT STA 1175 CRACKED AND EXFOLIATED. REMOVED REINFORCEMENT ANGLE FOR ACCESS IAW B727 SRM 51-30-2 BS 1175 TO 1183 STR 30 EVALUATED STRINGER 30 AT BS 1175 TO 1183. NO CORROSION NOTED. EVALUATED REINFORCEMENT ANGLE FROM BS 1175 TO 1183 STR 30 FOUND OUT OF LIMITS. FABRICATED NEW REINFORCEMENT ANGLE MAT USED 7075-T6 .100 PO NR 9411586 SIZE 12 1/2 INCH BY 5 INCH 4 INCH IAW B727 SRM 53-10-2 51-20-1 AND 51-30-5 TREATED AND PRIMED AREA IAW B727 SRM 51-10-2. INSTALLED REINFORCMENT ANGLE AT STR 30 BS1175 TO 1183 IAW B727 SRM 51-30-2. 2L73 4F A3WE 20050426000732005042600073WP 2005 4 26 ABXA050057 120050216A531199115057 FRAME DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23966AX 47510 BOTH ENDS OF STRUCTURAL ANGLE LOCATED BENEATH CENTER WINDSHIELD ARE CRACKED. REPAIRED AREA IAW REA D953-51500MR AND DWG SR09530268. 2L72 4F A6WE 20050426000742005042600074WP 2005 4 26 ABXA050056 120050216A531199115055 FRAME DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23966AX 47510 STRUCTURAL ANGLE LOCATED BENEATH CAPTAIN'S WINDSHIELD WAS CRACKED AT INBOARD END. REPAIRED AREA IAW REA D953-51500MR AND IAW DWG SR09530268. 2L72 4F A6WE 20050426000752005042600075WP 2005 4 26 ABXA050058 120050216A531199115056 FRAME DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23966AX 47510 STRUCTURAL ANGLE LOCATED BENEATH FIRST OFFICER'S WINDOW CRACKED AT INBOARD END. REPAIRED AREA IAW REA D953-51500MR AND IAW DWG SR09530268. 2L72 4F A6WE 20050426000762005042600076WP 2005 4 26 ABXA050061 120050217A5311591236068 WINDOW FRAME DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23966AX 47510 CRACK INDICATIONS ON LOWER RIGHT WINDSHIELD ZEE. REMOVED AND REPLACED NEW ZEE ANGLE IAW DC-9 SRM 51-30-5 AND 51-30-8. 2L72 4F A6WE 20050426000772005042600077WP 2005 4 26 ABXA050062 120050217A5311591236067 WINDOW FRAME DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23966AX 47510 CRACK INDICATIONS ON LOWER LEFT WINDSHIELD ZEE. REMOVED AND INSTALLED NEW ZEE ANGLE IAW DC-9 SRM 51-30-5 AND 51-30-8. 2L72 4F A6WE 20050426000782005042600078WP 2005 4 26 ABXA050063 120050217A52305911424221 STOP DOUG DC9 DC941 302207NWP FWD CARGO DOOR CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23966AX 47510 FORWARD LOWER CARGO DOOR STOPS HAD EXTERNAL AND INTERNAL CORROSION. REPAIRED IAW REA D953-51511MR. 2L72 4F A6WE 20050426000792005042600079NM 2005 4 26 SB05038 120050304A2750 CIRCUIT BREAKER BOEING737 737301 1384611NM P6 PANEL TRIPPED A USAAO OTHER F FLT CONT AFFECTED CLCLIMB 1 EA19350US 23553 CLT - FLT406 - AFTER TAKEOFF FROM SRQ, CREW NOTED A SPLIT FLAP INDICATION ON FLAP POSITION INDICATOR. ON APPROACH TO CLT, FLAPS WOULD NOT EXTEND AS FLAPS WERE LOCKED OUT. CREW DECLARED AN EMERGENCY AND ACCOMPLISHED A ZERO FLAPS LANDING WITHOUT INCIDENT. MAINTENANCE FOUND FLAP POSITION INDICATOR CIRCUIT BREAKER TRIPPED JUST BEHIND FIRST OFFICER SEAT AT SHOULDER STRAP HEIGHT. RESET CIRCUIT BREAKER AND RAN FLAPS SEVERAL TIMES. ACCOMPLISHED A VISUAL INSPECTION OF FLAPS. ALL CHECK GOOD. ACCOMPLISHED FLAP ASYMMETRY SYSTEM CHECK PER MM 27-51-00. ALL CHECK GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F RTA16WE 20050426000802005042600080NM 2005 4 26 CALA0500072 120050308A531565C339503 FLOORBEAM BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717614 27327 INSPECTION FOUND CABIN FLOORBEAM CORRODED AT FASTENER HOLE OF FORWARD FLANGE OF UPPER CHORD, STA 986, LBL 43. A REPAIR WAS INSTALLED IAW ECRA 5321-01210. 2L72 4F RTA16WE 20050426000812005042600081NM 2005 4 26 CALA0500073 120050309A3350D71701100 BATTERY PACK BOEING737 737724 13844BYNM EMERGENCY LIGHT INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2713750 28941 THE LT EMERGENCY EXIT LIGHT BATTERY AT ROW 12 FAILED TEST. THE BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51-06. 2L72 4F RTA16WE 20050426000822005042600082NM 2005 4 26 CALA0500074 120050309A3350D71701100 BATTERY PACK BOEING737 737724 13844BYNM EMERGENCY LIGHT INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2713750 28941 THE LT EMERGENCY EXIT LIGHT BATTERY AT ROW 19 FAILED TEST. THE BATTERY PACK WAS REPLACED IAW MM 33-51-06. 2L72 4F RTA16WE 20050426000832005042600083NM 2005 4 26 CALA0500075 120050309A3350D71701100 BATTERY PACK BOEING737 737724 13844BYNM EMERGENCY EXIT INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2713750 28941 THE LT EMERGENCY EXIT LIGHT BATTERY AT AFT GALLEY OVERHEAD FAILED TEST. THE BATTERY PACK WAS REPLACED IAW MM 33-51-06. 2L72 4F RTA16WE 20050426000842005042600084NM 2005 4 26 TSAA0529013 120050308A2914 SEAL BOEING737 7372T4 1384492NM HYDRAULIC PUMP LEAKING A TSAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP13808AL 183824 23445 NON-ETOPS FLT 104, HNL-KOA: LOST A SYSTEM HYDRAULICS DURING CLIMB-OUT. RETURNED TO HNL. FLAPS WOULD NOT EXTEND TO 15 USING ALTERNATE FLAP SYSTEM. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE HYDRAULIC PUMP DUE TO INPUT SHAFT SEAL LEAKING PER AMM 29-11-31. OPS AND LEAK CHECK GOOD. MAINTENANCE REMOVED AND REPLACED THE FLAP ALTERNATE DRIVE UNIT. OPERATIONAL AND LEAK CHECK GOOD PER MM 27-51-241. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A16WE 20050426000852005042600085NM 2005 4 26 TSAA0529014 120050308A2914 SEAL BOEING737 7372T4 1384492NM HYDRAULIC PUMP LEAKING A TSAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP13808AL 6091 23445 NON-ETOPS FLT 104, HNL-KOA: LOST A SYSTEM HYDRAULICS DURING CLIMB-OUT. RETURNED TO HNL. FLAPS WOULD NOT EXTEND TO 15 USING ALTERNATE FLAP SYSTEM. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE HYDRAULIC PUMP DUE TO INPUT SHAFT SEAL LEAKING PER AMM 29-11-31. OPS AND LEAK CHECK GOOD. MAINTENANCE REMOVED AND REPLACED THE FLAP ALTERNATE DRIVE UNIT. OPERATIONAL AND LEAK CHECK GOOD PER MM 27-51-241. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A16WE 20050426000862005042600086NM 2005 4 26 TSAA0532015 120050309A3260B06002 CIRCUIT CARD BOEING737 737230 1384401NM PROXIMITY SYS FAILED A TSAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13818AL 22117 LANDING GEAR LEVER WOULD NOT GO TO UP POSITION AFTER TAKEOFF. NO GREEN OR RED GEAR LIGHTS ILLUMINATED. RETURNED TO HNL. MAINTENANCE INSPECTED AND LUBED THE TELEFLEX CABLE. MEASURED PROXIMITY SENSOR AND GAP WITHIN TOLERANCE. REPLACED PROXIMITY CARD AND SWUNG GEARS PER AMM 32-09-200. OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA16WE 20050426000882005042600088EA 2005 4 26 QXEA200500506 120050323A5534 FITTING CNDAIRCL600 CL6002C10 1390015EA VERTICAL STAB CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09613QX 10045 PDX - VERTICAL STAB REAR SPAR BACKUP FITTING HAS APPROXIMATELY 2 INCHES LONG HORIZONTAL CHAFE MARK ON WEB DIRECTLY ABOVE RUDDER TOP HINGE FITTING. REPAIRED IAW HORIZON AIR EA R-55-43 AND REO 670-55-31-003. 2L72 4F RTA21EA 20050426000902005042600090EA 2005 4 26 QXEA200500507 120050323A5542 PANEL CNDAIRCL600 CL6002C10 1390015EA RUDDER CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09613QX 10045 PDX - RUDDER TOP HINGE PANEL HAS .5 INCH LONG HORIZONTAL CHAFE MARK AT UPPER FORWARD END. REPAIRED IAW HORIZON AIR EA R-55-42 AND REO 670-55-41-005. 2L72 4F RTA21EA 20050426000932005042600093NM 2005 4 26 SWAA051026 120050410A5320BAC1518 STIFFENER BOEING737 7373H4 1384600NM MLG W/W CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED C4 CHECK, FOUND 2 EA VERTICAL STIFFENERS CRACKED AT BS 663, LBL 4 & RBL 4. REPAIRED STIFFENERS PER SWA EA. 2L72 4F RTA16WE 20050426000962005042600096NM 2005 4 26 SWAA051029 120050408A575565C2525121A SPOILER BOEING737 7373H4 1384600NM RT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED C4 CHECK, FOUND RT WING NR 6 SPOILER DELAMINATED. REMOVED AND REPLACED NR 6 SPOILER PER MM. 2L72 4F RTA16WE 20050601002022005060100202WP 2005 6 1 DHL2005807527 120050505A5315LS3983 FLOORBEAM DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01807DH86990 45990 MAIN CARGO COMPT FLOORBEAM (2EA) MISDRILLED HOLES AT STA 980.000 BETWEEN TRACK 3 AND 4 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 51-2-1 FIG 1 SHEET 7-12, TR NR 51-130. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. CUT OUT DAMAGED SECTION IAW SRM 51-2-1 FIG 1 SHEET 7. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED REPAIR ANGLE (EXTRUSION 7075-O P/N LS3983) AND FILLER (AL7075T6 0.125) IAW SRM 51-2-1 FIG 1 SHEET 7-12. HEAT TREATED REPAIR ANGLE IAW SRM 51-1-1 PG 1, 13, 17 DPS 7.001 REV BK. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SRM 51-2-1 FIG 1 SHEET 7, 12 SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050601002052005060100205NM 2005 6 1 05FDEA01349 120050517A3244 TIRE BOEING727 727233 138408ANM NLG DEFECTIVE A FDEAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 SO25220FE 20934 RTO DUE TO VIBRATION ON T/O ROLL. MINOR VIBRATION AT 60 KTS INCREASING IN INTENSIVE TO MODERATE VIBRATION AS SPEED INCREASED RTO AT 110 KTS. RTO AT 0815Z WITH 49 MIN COOL TIME. AFTER DEBRIEF WITH FLIGHT CREW IT WAS DETERMINED THAT VIBRATION WAS WORSE WHEN YOKE WAS PUSHED FWD. CHANGED BOTH NOSE GEAR TIRES. REMOVED AND REPLACED NOSE GEAR TIRE REF 727-200 MM 32-45-011-4. SWAP COMPONENT POSITIONS MPN: 65-72762-15 MSN: 388 TO POS: NRH MSN: A0117 TO POS: NLH. SWAPPED COMPONENTS DUE TO ERROR UPON INITIAL POSITION LOCATION. SWAPPED ON MAXI ENTRY ONLY. 2L73 4F RTA3WE 20050601002162005060100216NM 2005 6 1 ABXA050113 120050516A3350 LIGHT BOEING767 767281 1385109NM EXTERIOR INOPERATIVE A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23775AX 22790 L1 DOOR EMERGENCY EXTERIOR LIGHT WAS INOP. RELAMPED AND SEALED LENS TO L1 DOOR EMERGENCY LIGHT. OPS CHECKED GOOD. 2L72 4F RTA1NM 20050602000142005060200014NM 2005 6 2 AWXA200500569 120050517A5330 SKIN BOEING757 7572S7 1384962NM FUSELAGE DAMAGED A AWXAA UNSCHED LANDING O OTHER TOTAKEOFF 1 WP28904AW 23566 DURING ROTATION EN ROUTE FROM PHX TO EWR PILOTS SUSPECTED A BLOWN TIRE DURING ROTATION. ACFT CONTINUED & LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED ALL TIRES AND FOUND NO EVIDENCE OF DAMAGE. UPON FURTHER INSPECTION OF ACFT, MX FOUND DAMAGE TO AFT BELLY OF THE AIRCRAFT DUE TO AN APPARENT OVER ROTATION DURING TAKEOFF. MX REMOVED DAMAGED SKIN PANEL & REPLACED AFT SKIN PANEL FROM STA 1720 TO STA 1787 AND BLENDED AREAS FROM STA 1825 TO STA 1862 IAW AM WEST ENGINEERING REPAIR 19-5361-05147. MX ALSO REMOVED DAMAGED SHEAR TIE AT STA 1740 ON LOWER FLANGE BETWEEN STRINGER 29L TO STRINGER 29R. FABRICATED A NEW SHEAR TIE AND INSTALLED AT STA 1740 ON LOWER FLANGE BETWEEN STRINGER 29L TO STRINGER 29R IAW BOEING 757 2L72 4F RTA2NM 20050602000192005060200019WP 2005 6 2 UPS05844469 120050502A53204646163U501 SPLICE DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE:C3 "D" PIT BETWEEN STA 1340-1360 L30R SPLICE FITTING CRACKED. REMOVED AND REPLACED SPLICE FITTING IAW SRM 51-1-21 AND 51-1-20D. 2L74 4F RT4A25 20050602000252005060200025WP 2005 6 2 UPS05844476 120050427A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE:C3 FUSELAGE SKIN AT APROX STA 1723 RT L16 HAS CRACK APROX. 1/2 INCH LENGTH. CUT OUT DAMAGE AND INSTALLED DOUBLER, FINGER DOUBLER FILLER AND EXTERNAL DOUBLER IAW SRM 53-02-01-0 FIG 007. 2L74 4F RT4A25 20050602000282005060200028NM 2005 6 2 QXEA200500846 120050513A2760 SWITCH BOMBDRDHC8 DHC8401 1390041NM SPOILER FAULTY A QXEAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM09403QX 4037 GEG FLIGHT NR 2376 - DURING CLIMB THROUGH ABOUT 6000 FT AND 190 KIAS, THE 'SPLR OUTBD' CAUTION LIGHT ILLUMINATED. REDUCED TO 200 KIAS FOR CRUISE AS PER E/A CHECKLIST. LIGHT WENT OUT GOING THROUGH 185 KIAS APROACH. MAINTENANCE REPLACED "ROLL SPLR" OUTBOARD HYDRAULIC PSI SWITCH. LEAK AND OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050602000362005060200036EU 2005 6 2 MALA050422 120050518A3242AHA23322 BRAKE BAC 146 AVRO146RJ85A1500097EU RT MLG FAILED A MALAO OTHER O OTHER TXTAXI/GRND HDL 1 GL15530XJ E2364 DURING O/B TAXI FOR FLIGHT FELT SOME BINDING DURING VERY SLOW TAXI SPEED ALMOST AS IF THERE WAS 2 FLAT TIRES ON ONE SIDE. VISUAL INSPECTION NOTED NO FLATS. FELT AS IF BRAKE COULD BE BINDING. NOTED SLIGHTLY HIGHER TEMP ON RT INNER INDICATION. FOUND RIGHT I/B BRAKE FAILED. REMOVED AND REPLACED I/B BRAKE IAW JC 3240-501PN, AHA2332-2. S/N OFF XC-143 ON VK051. FOUND RIGHT I/B WHEEL ASSY DAMAGED. REMOVED AND REPLACED WHEEL ASSY IAW JC 3240-502, P/N AHA1489, S/N OFF XF116, S/N ON VE009. REMOVED AND REPLACED RIGHT IN BRAKE FAN DUE TO DAMAGE BLADE IAW 3240-501, P/N AHA3240-501. 2H74 4F RTA49EU 20050602000372005060200037EU 2005 6 2 MALA050421 120050426A3020 MODULE SAAB SF340 340B 7860101EU DEICE SYSTEM FAILED A MALAO OTHER O OTHER UKUNKNOWN 1 GL15427XJ 340B427 FLIGHT RETURNED TO DTW FOLLOWING FAILURE OF THE ENGINE AIR INTAKE ICE PROTECTION SYSTEM. REPLACED DEICE MODULE. 2L72 4T RTA52EU 20050602000672005060200067WP 2005 6 2 DHL2005807528 120050505A5315LS3983 FLOORBEAM DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH86990 45990 MAIN CARGO COMPT FLOORBEAM MISDRILLED HOLE AT STA 879.000 RBL 32 AND SHOWS CORROSION ON FLANGE. PERFORMED MAJOR REPAIR IAW SRM 51-2-1 FIG 1 SHEET 7-12 TR NR 51-130. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. OUT OF LIMITS IAW SRM 53-2-0 PG 2P. CUT OUT DAMAGED SECTION IAW SRM 51-2-1 FIG 1 SHEET 7. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED REPAIR ANGLE AND FILLER IAW SRM 51-2-1 FIG 1 SHEET 7-12. HEAT TREATED REPAIR ANGLE IAW SRM 51-1-1 PG 1, 13, 17 DPS 7.00-1 REV BK. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT IAW SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW SRM 51-2-1 FIG 1 SHEET 7-12, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. TORQUED IAW SRM 512L74 4F RT4A25 20050602000792005060200079CE 2005 6 2 GUU2005F00012 120050308A2120 ODOR BEECH 1900 1900D 1154162CE COCKPIT DETECTED A GUUAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO2987557 UE246 FLT 9191 - EYW/MCO - DURING FLIGHT, SMELLED SMOKE IN THE COCKPIT. DIVERTED TO RSW. LANDED WITHOUT INCIDENT. CLEANED CARBON FROM INTERNAL SCAVENGE PUMP SCREEN. OPERATIONAL CHECK OF OIL PRESSURE AND OIL TEMPERATURE SYSTEMS NORMAL. NO SMOKE NOTICED IN THE COCKPIT. (M) 2L72 4T RTA24CE 20050602000832005060200083SO 2005 6 2 C2XA05BT028 120050509A335078241 INVERTER EMB 145 EMB145LR 3260212SO CABIN FAILED A C2XAO OTHER O OTHER UKUNKNOWN 1 SW2714959 145091 BNA - MAINTENANCE FOUND THE EMERGENCY EXIT SIGN ABOVE FLIGHT ATTENDANTS SEAT IS NOT WORKING. REMOVED AND REPLACED NR 1 INVERTER IAW EMB AMM NR 33-50-11, OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050602000922005060200092EU 2005 6 2 KBM2005F00054 120050421A6730SC5084 SERVO SNIAS 350 AS350B2 8680813EU MAIN ROTOR LEAKING E KBMAO OTHER K FLUID LOSS NRNOT REPORTED 1 WP19751SH 3403 SERVO LEAKING. REMOVED AND REPLACED SERVO. (M) 1G71 3U H9EU 20050602000942005060200094EU 2005 6 2 KBM2005F00056 120050418A2130060018 BELT SNIAS 350 AS350B2 8680813EU CABIN PRESSURE BROKEN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH 2957 FOUND COMPRESSOR BELT BROKEN. AIRCRAFT MEL. (M) 1G71 3U H9EU 20050602001092005060200109NM 2005 6 2 AWXA200500583 120050429A532050794544 INTERCOSTAL BOEING737 7373B7 1384580NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28332AW 23384 MCN- MAJOR REPAIR- DURING C-18 CHECK, A CRACK WAS FOUND AT A L-1 DOOR INTERCOSTAL, ADJACENT TO THE UPPER L-1 DOOR HINGE. MAINTENANCE REMOVED AND INSTALLED NEW INTERCOSTAL IAW B737-300 SRM 51-40-02-0 (FIGURE 3, 4, 6, 7, 8, 10 AND 16) 2L72 4F RTA16WE 20050602001252005060200125NM 2005 6 2 EIA2005099 120050405A5315 FLOORBEAM BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 BS 600 UPPER DECK FLOOR BEAM UPPER CHORD HORIZONAL FLANGE FASTENER HOLE AT RBL 27 FOUND CRACKED APPROX .0030 INCH IN LENGTH RUNNING AFT. CRACKED FASTENER HOLE FURTHER OVERSIZED TO .31 INCH. FOUND CRACK FREE CONDITION. THE HOLE REPAIRED PER SB53A2452 PT 3 REPAIR TABLE II, FIGURE 14. 2L74 4F A20WE 20050602001342005060200134NM 2005 6 2 EIA2005110 120050513A5320 STRAP BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 M/D RT BS 800 FRAME STRAP BETWEEN STRINGER 25R AND 26R FRAME INNER CHORD STRAP FOUND CRACKED. RT BS 800 FRAME STRAP BETWEEN STRINGER 25R AND 26R, DOUBLER REPAIRED PER SRM 51-40-01, FIG 1. 2L74 4F A20WE 20050602001462005060200146NM 2005 6 2 EIA2005122 120050513A5712 RIB BOEING747 747212B 1384886NM LT WING CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 LT WING SURGE TANK WS 1516, RIB LOWER CHORD AT STRINGER 6 AREA FOUND CRACKED AS MARKED. LT WING SURGE TANK, WS 1516 RIB LOWER CHORD REPLACED AT STRINGER 6 AREA PER SRM 57-10-05, FIG 4. 2L74 4F A20WE 20050602001512005060200151NM 2005 6 2 ANCF200400047 120050416A2400 SMOKE DOUG MD80 MD83 3023681NM COCKPIT DETECTED W ANCFK NONE B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO23583AN 53183 IN BAQ WHEN EXTERNAL POWER WAS CONNECTED SMOKE CAME INTO COCKPIT FROM OVERHEAD PANEL. AS PER AMM 20-50-01 PAGE 201, GROUND ELECTRICAL 106 LINE WAS ISOLATED ON CONNECTOR P1-568 OF CABIN PRESS SELECTOR ELECTRICAL LINES WERE CHECKED BY CONDITIONS ON OVERHEAD PANEL WITH SATISFACTORY RESULTS. 2L72 4F RT 20050602001572005060200157NM 2005 6 2 DL767050267 120050512A3610361001794 SHUTOFF VALVE BOEING767 767232 1385132NM BLEED AIR SYS STICKS A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO27102DA 22214 WHEN POWER INITIALLY REDUCED TO START INITIAL DESCENT A SMELL DEVELOPED IN THE AIRCRAFT. REPLACED NR 1 HPSOV. 2L72 4F RTA1NM 20050602001652005060200165NM 2005 6 2 DL73S050276 120050517A7830 ACTUATOR BOEING737 737232 1384475NM PWA JT8 JT8D15 52051NE THRUST REVERSER STICKING A DALAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO27316DL 23088 709162 NR 2 ENGINE THRUST REVERSER UNLOCKED LIGHT ON DURING TAKEOFF ROLL. CLEANED LOWER ACTUATOR FOR STICKING. 2L72 4F4 FRTA16WE E2EA 20050602001772005060200177EU 2005 6 2 MALA050427 120050516A5330 SKIN BAC 146 AVRO146RJ85A1500097EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15519XJ E2344 DURING A C3 CHECK IN YYC 2 DENT ON RT FUSELAGE AT FR15 AND FR16 13.5 INCHES BELOW LAP JOINT. REPAIRED IAW SRM 517200. 2H74 4F RTA49EU 20050606000032005060600003EA 2005 6 6 QXEA200500940 220050518A7200312162701 ENGINE BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA NR 2 LEAKING A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 NM09409QX2899 1621 4051 PCEFA0184 PDX FLIGHT NR 2455 SMOKE IN COCKPIT AND CABIN. EMERGENCY DECLARED AFTER CHECKLIST RUN. LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NR 2 ENGINE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E00062EN 20050606000112005060600011WP 2005 6 6 UPS05844487 120050506A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE: C3, LONGERON 14L CRACKED AT STA 1746. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-2-2 FIG 11 AND 51-1-20D. 2L74 4F RT4A25 20050606000122005060600012WP 2005 6 6 UPS05844488 120050503A5712 RIB DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE: C3, LT WING L/E UPPER RIB CRACKED AT XFS 822.500 .5 INCH LONG. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2 -0, 57-2-0 FIG 2, 51-1-20D, 51-1-21 AND DWG 5769470. 2L74 4F RT4A25 20050606000132005060600013WP 2005 6 6 UPS05844489 120050505A5312 RIB DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE: C3, LT WING L/E LWR RIB CRACKED AT XFS 816. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-3-0, 51-1-21, 51-1-20D AND DWG 5769471. 2L74 4F RT4A25 20050606000142005060600014WP 2005 6 6 UPS05844490 120050505A5312 RIB DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE: C3, LEFT L/E LWR RIB CRACKED AT XFS 816. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-3-0, 51-1-21 AND 51-1-20D. 2L74 4F RT4A25 20050606000162005060600016WP 2005 6 6 UPS05844494 120050503A5712 RIB DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE: C3, LEFT WING L/E UPPER RIB CRACKED 1 INCH LONG AT XFS 828.500. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 53-2-0 FIG 1B, 57-2-0 FIG 2B, AND DWG'S 5769470-45, 576947U. 2L74 4F RT4A25 20050606000192005060600019WP 2005 6 6 UPS05844497 120050504A5712 RIB DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE: C3, LT WING L/E UPPER RIB CRACKED AT XFS 408. STOP DRILLED CRACK, FABRICATED AND INSTALLED 2 EA REPAIR DOUBLERS IAW SRM 57-2-0 FIG 2, 51-1-20D AND DWG 5770375. 2L74 4F RT4A25 20050606000222005060600022 2005 6 6 ABXA050120 420050519A2565 GIRT BAR BOEING767 767231 1385131NM PAX DOOR SLIDE CONTAMINATED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23702AX 22566 CREW REPORTED MAIN ENTRY DOOR SLIDE WOULD NOT ARM. CHECKED FOR DEBRIS IN GIRT BAR AREA. CLEARED AREA AND CYCLED DOOR. DOOR CHECKED GOOD. SLIDE ARMS AND DISARMS. 2L72 4F RTA1NM 20050606000252005060600025EA 2005 6 6 COMA0560305 120050510A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS UNRELIABLE A COMAO OTHER J WARNING INDICATION LDLANDING 1 SO01917CA141299478 7017 FLIGHT 5537 - FLAPS FAIL CAUTION. COULD NOT DUPLICATE REPLACED THE LT BPSU. 2L72 4F RTA21EA 20050606000282005060600028NM 2005 6 6 DHL2005741511 120050421A5330 SKIN BOEING727 7272Q9 138448MNM FUSELAGE CANNING A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 FUSELAGE NOSE BS 185, 7 O`CLOCK POS HAS SKIN OIL-CANNING. CUT OUT DAMAGED AREA 2 BY 2 INCHES. FABRICATED DOUBLER 2024-T3 .050 PO NR 9001873, (11 BY 7.5 INCHES) IAW B727 SRM 53-30-2 FIG 1, AN 53-30-3 FIG 1. TREATED AND PRIMED PARTS AN AREA IAW B727 SRM 51-10-2, INSTALLED DOUBLER REPAIR IAW B727 SRM 53-30-3 FIG 1. 2L73 4F RTA3WE 20050606000372005060600037EU 2005 6 6 YENA200531 120050520A2120 ODOR AIRBUS320 A320232 3930326EU IAE V2500 V2500A1 NE CABIN DETECTED A YENAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15543JB 1823 ELECTRICAL ODOR THROUGHOUT CABIN JUST PRIOR TO DESCENT. COULD ODOR ON FLIGHT DECK ALSO. TURNED OFF TV'S, BEGAN DESCENT, ODOR WENT AWAY. PERFORMED INSPECTION IAW TSM 24-00-00-810-823, 71-00-00-810-801 EXCEPT FOR STEP 3, AND 26-15-00-810-804. NO DEFECTS NOTED. REPLACED OZONE FILTERS IAW AMM 21-51-41-000-001, REPLACED RECIRCULATION FILTERS IAW AMM 21-21-41-000-001, NO EVIDENCE OF OIL, FUEL OR HYDRAULIC LEAK NOTED FROM ENGINES OR APU, RAN ENGINES, APU AND ALL PACKS. NO BURNING/ELECTRICAL ODOR NOTED. PERFORMED JB INFO NOTICE 2004-TO23TR NO EVIDENCE OF SYS BEING COMPROMISED, NO FAULTS FOUND. 2L72 4F4 FRTA28NM E311NE 20050606000442005060600044NM 2005 6 6 AALA20050338 120050518A3350 LIGHT BOEING757 757223 1384957NM ROW 18D INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21619AA 24577 SFO - WHITE EMERGENCY PATH LIGHT AT 18D INOPERATIVE. REPLACED EMERGENCY PATH LIGHT ASSEMBLY AT 18D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050606000462005060600046NM 2005 6 6 AWXA200500573 120050429A53206517684642 INTERCOSTAL BOEING737 7373B7 1384580NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28332AW 23384 MCN - MAJOR REPAIR - DURING C-18 CHECK A CRACK WAS FOUND AT S7L BS 294.5 INTERCOSTAL WEB. MAINTENANCE REMOVED AND REPLACED INTERCOSTAL WEB, AUX INTERCOSTAL, AND SHEAR TIE CLIP AT MS 294.5 STR 7LT IAW AWA ER 03-5300-05135-SS1. 2L72 4F RTA16WE 20050606000492005060600049NM 2005 6 6 AWXA200500586 120050519A2530 HEATING ELEMENT BOEING737 7373S3 1384711NM COFFEEMAKER SHORTED A AWXAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP28314AW 23733 LAS - AIR TURN BACK - FLT 797 - ON CLIMB-OUT FROM LAS EN ROUTE TO PDX FLIGHT ATTENDANT REPORTED SMOKE AND A LOUD POP FROM THE FWD COFFEEMAKER. MAINTENANCE DISCOVERED THE WATER HEATER ELEMENT SHORTED. MAINTENANCE REMOVED COFFEEMAKER AND COLLARED CIRCUIT BREAKER THEN PLACED ON MEL. TEAR DOWN REPORT ATTRIBUTES THE FAILURE OF THE COFFEEMAKER TO WATER BEING ABSORBED INTO THE MAGNESIUM OXIDE CORE OF ONE HEATER IN THIS UNIT. 2L72 4F RTA16WE 20050606000512005060600051NM 2005 6 6 AWXA200500589 120050429A5210 SKIN BOEING737 7373B7 1384580NM PAX DOOR BUCKLED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28332AW 868 23384 MCN - MAJOR REPAIR - DURING C-18 CHECK, THE SKIN WAS FOUND TO BE BUCKLED AT THE L1 DOOR UPPER HINGE CUTOUT. THE DAMAGE WAS LOCATED JUST BELOW THE HINGE, BS 319, STRINGER 10 LT. MAINTENANCE PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS PRESENT; FABRICATED A REPAIRED DOUBLER AND INSTALLED REPAIR IAW AMERICA WEST AIRLINES ENGINEERING REPAIR 03-5200-05138-SS7. 2L72 4F RTA16WE 20050606000542005060600054NM 2005 6 6 QXEA200500951 120050519A2612 FIRE LOOP DHAV DHC8 DHC8202 2809007NM NR 1 ENGINE MALFUNCTIONED A QXEAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 NM09359PH 514 SEA FLIGHT NR 2179, NR 1 ENGINE FIRE DETECTION "FAULT B" ILLUMINATED. MAINTENANCE REPLACED NR 1 ENGINE FIRE DETECTION LOOP B IAW PSW MM 72-01-30. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050606000562005060600056CE 2005 6 6 DXTA200500729 120050518A2710 TRIM SYSTEM CESSNA500 560CESSNA 2076750CE AILERONS MALFUNCTIONED E DXTAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 GL07825QS 5600655 AILERON TRIM APPEARS TO BE FREEZING UP IN FLIGHT AT FL 380 AT -28 C RAT. THE ROLL TRIM ANNUNCIATOR ILLUMINATED, WAS UNABLE TO MOVE THE AILERON TRIM KNOB UNTIL THE RAT WAS +10 C. THE RUDDER TRIM WAS MOVING FREELY AT -28 RAT BOTH OPERATE NORMALLY ON THE GROUND. LUBED AILERON TRIM ACTUATOR WITH SILICON GREASE (DC-33) PER M/M. INSPECTED TRIM WHEEL IN COCKPIT AND VISIBLE CABLES FOR BINDING OR SEIZED PULLIES. CHECKED TRIM RODS FROM ACTUATOR TO TRIM TAB FOR BINDING AND CORRECT INSTALLATION. NO DEFECTS NOTED. AILERON TRIM TAB, OPS CHECKS GOOD AT THIS TIME I/A/W CE 560 M/M CH 27-11-00 2L72 4F RTA22CE 20050606000822005060600082EU 2005 6 6 USAASA05058 120050531A335032145410 EPSU AIRBUSA319 A319112 3930323EU EMERGENCY LIGHTSFAULTY A USAAK NONE L NO TEST ININSP/MAINT 1 EA19109UW18662 1065 THE AFT LEFT EMERGENCY POWER SUPPLY UNIT FAILED THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE AFT POWER SUPPLY UNIT. 2L72 4F RTA28NM 20050606000832005060600083 2005 6 6 SA05055 420050523A2565 LANYARD AIRBUSA319 A319112 3930323EU ESCAPE SLIDE MISROUTED A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19716UW 1055 PIT - MAINTENANCE REPORTED THAT THE FORWARD, RIGHT SIDE DOOR EMERGENCY ESCAPE SLIDE ASSEMBLY MOORING LINE WAS FOUND INCORRECTLY ROUTED TO THE GIRT BAR ASSEMBLY. MAINTENANCE CORRECTLY ROUTED THE MOORING LINE. OK FOR SERVICE. 2L72 4F RTA28NM 20050606000842005060600084NM 2005 6 6 AALA20050342 120050519A33500201991004 LIGHT BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21661AA 25295 RNO FOUND WHITE EMERGENCY EXIT SEAT MOUNTED LIGHT ASSEMBLY INOPERATIVE AT SEAT 18D. PLACARDED ITEM PER MEL 33 16 AUTH 5 891 C. REPLACED LIGHT ASSEMBLY FOR WHITE EMERGENCY EXIT SEAT MOUNTED EGRESS LIGHT AT SEAT 18D. SYSTEM GROUND CHECKED NORMAL OPERATION. (SUPP CLOSED) 2L72 4F RTA2NM 20050606000862005060600086NM 2005 6 6 P5CA0501350 120050519A324426070812 WHEEL BOEING747 747230B 1384889NM MLG FAILED A P5CAJA DUMP FUEL UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 EA15508MC 21644 CREW REPORTED HEARING TWO LOUD BANGS AFTER TAKEOFF. FOUND NR 8 TIRE BLOWN AND PANEL 193E MISSING. REPLACED NR 7 & 8 WHEEL ASSY'S. 2L74 4F A20WE 20050606000992005060600099NM 2005 6 6 05FDEA01463 120050525A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 N01344 CREASE IN EXTERNAL SKIN AT BS 1124 STRINGER 20 LT, JUST BELOW SKIN LAP REPAIRED SKIN PER SRM 53-30-3 2L73 4F RTA3WE 20050606001032005060600103EU 2005 6 6 F3LA200500019 120050518A212120092455101 COOLING FAN AIRBUSA318 A318111 3940019EU E/E BAY INOPERATIVE A F3LAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM03806FR 3696 2218 FLIGHT CREW REPORTED LIVE TV SMOKE WARNING LIGHT DURING FLIGHT. INSPECTED LIVE TV RACK, FOUND COOLING FAN INOP (NO SMOKE PRESENT). REPLACED LTV COOLING FAN ASSY PER LTV AMM 44-25-00. OPS CHECK NORMAL. 2L72 4F RT 20050606001052005060600105EA 2005 6 6 QXEA200500875 120050505A5230 RETAINER CNDAIRCL600 CL6002C10 1390015EA ZONE 800 BENT A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FORWARD BAGGAGE DOOR SEAL RETAINER BENT AT FORWARD BOTTOM CORNER. REPAIRED IAW CRJ-7090 SRM 51-41-02-001-001-A01, 51-21-16-001-001-A01 AND 51-23-00-001-001-A01. 2L72 4F RTA21EA 20050607000042005060700004EA 2005 6 7 QXEA200500877 120050505A5410 COWL DOOR CNDAIRCL600 CL6002C10 1390015EA ZONE 400 WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - LEFT ENGINE LOWER FAN COWL DOOR INNER INBOARD SURFACE WORN BY TRAILING EDGE FLEX CABLE. REPAIRED IAW CRJ-700 SRM 51-12-00-001-001, 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050607000052005060700005EA 2005 6 7 QXEA200500878 120050505A5410 COWL DOOR CNDAIRCL600 CL6002C10 1390015EA ZONE 400 WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - LEFT ENGINE LOWER FAN COWL DOOR INNER INBOARD SURFACE WORN BY ELECTRICAL HARNESS. REPAIRED IAW CRJ-700 SRM 51-12-00-001-001-A01, 51-21-11-001-001-A01 AND 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050607000062005060700006EA 2005 6 7 QXEA200500879 120050503A7830 PLATE CNDAIRCL600 CL6002C10 1390015EA ZONE 400 WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - LEFT ENGINE TRANS COWL ALL LOWER RETAINER PLATES AND RAMPS WORN. REPAIRED IAW REO 67-78-33-0333. 2L72 4F RTA21EA 20050607000222005060700022NM 2005 6 7 DHL2005740529 120050327A5330 SKIN BOEING727 7272Q9 138448MNM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH21930 21930 DENT RT FUSELAGE SKIN 4 INCHES AFT OF STA 1342.4 STRINGER 22R. REMOVED FASTENERS FOR ACCESS IAW B727 SRM 51-30-2 CUTOUT DAMAGED AREA ON RT FUSELAGE STA 1342 STR 22R AND 23R SIZE 3 X .750 INCHES AND 1 X .500 INCHES IAW B727 SRM 54-30-3 FIG 7. FABRICATED DOUBLER REPAIR WITH 2024T3 .063 SIZE 16.750 X 10 INCHES PO 9002039 IAW B727 SRM 54-30-3 FIG 7 AND 54-30-2. TREATED AND PRIMED PART AND AREA IAW B727 SRM 51-10-2 AND INSTALLED DOUBLER REPAIR IAW B727 SRM 54-30-3 AND 51-30-2. 2L73 4F RTA3WE 20050607000232005060700023NM 2005 6 7 DHL2005740530 120050327A5330 SKIN BOEING727 7272Q9 138448MNM FUSELAGE LIGHTNING STRIKEA DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH21930 21930 2 RIVETS SHOWING SIGNS OF LIGHTNING STRIKE AFT OF STA 950B UNDERNEATH FUSELAGE SKIN STR 29R. CUT-OUT 6.750 X 3.125 INCHES SECTION OF LOWER FUSELAGE SKIN AT BS 950B+15 AT STR 29R DUE TO LIGHTNING STRIKE DAMAGED BEYOND ALLOWABLE LIMITS PER B727 SRM 53-30-1 FIG 1. FABRICATED REPAIR DOUBLER 11 X 22 INCHES FROM 2024T3 .090 PO NR 9002149 REPAIR TRIPLER 9 X 20.750 INCHES FROM 2024T3 .125 PO NR 9001873 AND FILLER FROM 2024T3 .090" PO NR 90022149 2 EACH 6.750 X 3.125 IAW BOEING SERVICE REQUEST ID NR 1-88767670. TREATED AND PRIMED DOUBLER TRIPLER AND FILLER AND AREA IAW B727 SRM 51-10-2. INSTALLED REPAIR DOUBLER TRIPLER AND SKIN FILLER ON FUSELAGE SKIN BS 950+15" AT STR 29R IAW BOEING SERVICE REQUEST ID NR 1-887676702L73 4F RTA3WE 20050607000292005060700029NM 2005 6 7 DHL2005740535 120050409A5314 KEELBEAM BOEING727 7272Q9 138448MNM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH46106 21930 REMOVED FASTENERS AS REQ AND PRIMED THE UPPER FLANGE OF THE KEELBEAM CHORD PER S/B 727-53-208 REV 1 FIG 3 DETAIL 2 AT LEFT SIDE BS 870. FABBED REPAIR DOUBLER FROM 15-5 PH .071 HEAT TREATED TO 170 TO 190 KSI PO NR 315722 DIM 8.625 BY 3.875 INCHES HFEC INSPECTED UPPER FLANGE OF THE KEELBEAM TRIM WITH NO CRACKS NOTED IAW B727 NDT MANUAL PT 6 51-00-00 FIG 23. TREATED AND PRIMED DOUBLER AND BARE METAL AT KEELBEAM LOWER CHORD ANGLE LT SIDE BS 870 IAW S/B 727-53-0208 REV 1 FIG 3 DETAIL 2. 2L73 4F RTA3WE 20050607000352005060700035NM 2005 6 7 DHL2005740543 120050405A5330 SKIN BOEING727 7272Q9 138448MNM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 REMOVED INBD FLOW CONTROL VALVE TO FOM S/M IAW B727 MM 21-58-21. REMOVED OUTBD FLOW CTL VLV TO FOM S/M REPAIR IAW B727 MM 21-58-31. REMOVED FASTENERS AT FUSE EXT SKIN BS 1223 BELOW STR 20L IAW B727 SRM 51-30-2, CUTOUT 4 EA DAMAGED AREAS DIM 3 3/8" BY 1 1/4", 7" BY 3", 2 3/8" BY 1 1/4", 2 3/8" BY 1 1/4" IAW B727 SRM 53-30-3 FIG 1. FABRICATED DOUBLER REPAIR MAT USED 2024T3 .067 P.O 9002149 DIM 47" BY 11" IAW B727 SRM 53-30-2 FIG 3 AND 53-30-3 FIG 1. INSTALLED DOUBLER REPAIR IAW B727 SRM 53-30-2 FIG 3 AND 53-30-3 FIG 1, LATE ENTRY, ALODINED AND PRIMED AREA AND DOUBLER IAW B727 SRM 51-10-2. 2L73 4F RTA3WE 20050607000362005060700036NM 2005 6 7 DHL2005740546 120050329A5311 FRAME BOEING727 7272Q9 138448MNM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 REMOVED PREVIOUS REPAIR AT FS AT 560 BTW 16R AND 17R IAW B 727 SRM 51-30-2. FABRICATED NEW FRAME REPAIR MAT USED 7075T6 .071 PO 9001737 DIM 6" BY 5" IAW B727 SRM 53-10-2 FIG 3 AND 51-40-3 FIG 1. ALODINED AND PRIMED PART AND AREA IAW B727 SRM 51-10-3. INSTALLED FRAME REPAIR IAW B727 SRM 51-40-3 FIG 1. 2L73 4F RTA3WE 20050607000532005060700053EU 2005 6 7 RAIA00505011 120050513A79308582 PRESSURE SWITCH JETAIRJETSTMJETSTM4101 1500501EU NR 2 MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03566HK6535 41084 FLT 5415 - STL - RT OIL PRESSURE LOW WARNING INDICATION. MAINTENANCE REMOVED AND REPLACED NR 2 OIL LOW PRESSURE SWITCH. 2L72 4T RTA41NM 20050607000612005060700061EU 2005 6 7 MAC5403 120050408A243430E0227B GENERATOR FOKKERF27 F27MK500 4990629EU LEFT OVERTEMP A MTNAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CRCRUISE 1 SO33716FE 10471 EN ROUTE THE LEFT GENERATOR INDICATED AND OVERHEAT CONDITION. THE CREW MADE AN EMERGENCY IN POA FOR REPAIRS. 2H72 4T A817 20050607000632005060700063SO 2005 6 7 CHQA200500101 120050519A33503025103 LIGHT EMB 135 EMB135LR 3260305SO EMERGENCY EXIT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11844RP 145620 LEFTHAND OVERWING EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY ON THE LEFTHAND OVERWING FAIRING IAW EMB 135 AMM 33-50-10. OPS CHECK GOOD. 2L72 4F RTT00011AT 20050607000692005060700069SW 2005 6 7 AC2A100762 120050319A2432RG407A1 BATTERY BELL 430 430 1182150SW MASTER WEAK E AC2AO OTHER O OTHER NRNOT REPORTED 1 SO07430CM428 49090 BATTERY IS WEAK. CHARGED BATTERY AND PERFORMED CAPACITY CHECK. FAILED 1ST CHECK (23 MINUTES). PERFORMED CONDITIONING CHARGE, RESTED AND PERFORMED 2ND CHECK. FAILED 2ND CHECK (30 MINUTES). WORK PERFORMED IAW MFG BATTERY MANUALS. REPLACED BATTERY. 1G72 3U RTH9SW 20050607000732005060700073SW 2005 6 7 ALGA100793 120050309A6320205040245001 DRIVE GEAR BELL 412 412 1182202SW TRANSMISSION FAILED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW035NBCZ A182 33179 TRANSMISSION DISASSEMBLED FOR METAL, FOUND DUPLEX BEARING BREAKING DOWN. REMOVED AND REPLACED DUPLEX BEARING P/N 205-040-245-001. 1G72 4U H4SW 20050607000742005060700074EU 2005 6 7 TXER100820 120050422A7100365A54801200 BAFFLE UROCOPEC155 EC155B 8681000EU ENGINE WORN B TXERO OTHER O OTHER NRNOT REPORTED 1 SW09155EW 6660 WORN BAFFLE. 1G72 3U H10EU 20050607000922005060700092EA 2005 6 7 QXEA200500890 120050503A5315 FLOORBEAM CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FUSELAGE INTERIOR FLOOR SUPPORT CROSSBEAM AT STATION 280 IS CORRODED ALONG TOP FLANGE. REPAIRED IAW REO 670-53-11-047. 2L72 4F RTA21EA 20050607000982005060700098EA 2005 6 7 QXEA200500895 120050502A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FORWARD FUSELAGE LOWER SKIN PANEL ROCK CHIP DAMAGE AT STATION 561.00 BETWEEN STRINER 27 AND 25L. REPAIRED IAW CRJ 700 SRM 51-12-00-001-001-A01, 51-21-11-001-001-A01, 51-25-01-001-001-A01 AND 53-31-01-101-003-A01. 2L72 4F RTA21EA 20050607001002005060700100EA 2005 6 7 QXEA200500888 120050503A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FORWARD FUSELAGE LOWER SKIN PANEL ROCK CHIP DAMAGE STATION 434.00 TO 453.00 BETWEEN STRINGER 26L AND 24L. REPAIRED IAW CRJ700 SRM 51-26-00-001-001-A01, 53-21-01-101-006-A01 AND 51-25-16-001-001-A01. 2L72 4F RTA21EA 20050607001062005060700106EA 2005 6 7 QXEA200500904 120050509A5210 STRUCTURE CNDAIRCL600 CL6002C10 1390015EA ZONE 800 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - PASSENGER DOOR FORWARD EDGE DENTED. REPAIRED IAW CRJ700 AMM 52-00-00-790-801, REO 670-52-11-108 AND HORIZON AIR EA R-52-250. 2L72 4F RTA21EA 20050607001142005060700114EA 2005 6 7 QXEA200500903 120050502A5230 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 800 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - AFT BAGGAGE BAY DOOR EXTERIOR SURFACE HAS GOUGE AT DOOR HANDLE CUTOUT, FORWARD TOP EDGE. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01, 51-25-16-001-001-A01 AND SRM 51-21-11-001-001-A01. 2L72 4F RTA21EA 20050607001192005060700119EA 2005 6 7 QXEA200500915 120050428A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FUSELAGE INTERIOR LEFT OUTBOARD SIDE SEAT RAIL HAS PITTING AND SURFACE CORROSION ON INNER MOST SURFACE AND INSIDE SURFACE AT STATIONS 753-754. REPAIRED IAW REO 670-53-00-013. 2L72 4F RTA21EA 20050607001202005060700120EA 2005 6 7 QXEA200500906 120050503A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FUSELAGE INTERIOR RIGHT LOWER WEB OF STATION BULKHEAD IS CORRODED ALONG THE FLOOR LINE. REPAIRED IAW REO 670-53-11-052, REV A. 2L72 4F RTA21EA 20050607001232005060700123EA 2005 6 7 QXEA200500911 120050428A5340 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FUSELAGE INTERIOR LEFT INBOARD FLOOR SEAT RAIL HAS PITTING CORROSION AND SCRATCHES AT THE FOLLOWING LOCATIONS, STATION 663-682. REPAIRED IAW REO 670-53-00-013. 2L72 4F RTA21EA 20050607001252005060700125EA 2005 6 7 QXEA200500907 120050428A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FUSELAGE INTERIOR RIGHT INBOARD FLOOR SEAT RAIL HAS PITTING CORROSION ON INNER SURFACE AT SEVERAL LOCATIONS. REPAIRED IAW REO 670-53-00-013. 2L72 4F RTA21EA 20050607001372005060700137EU 2005 6 7 YENA200532 120050520A4990 APU AIRBUS320 A320232 3930326EU APU BAY OVERSERVICED A YENAH DEACTIVATE SYST/CIRCUITS WB INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 EA15543JB 1823 ODOR DURING DESCENT. TURNED OFF LIVE TV SYS, ODOR WENT AWAY, COCKPIT ONLY. F/A'S DID NOT REPORT ODOR. SURVEILLANCE SYS NORMAL. LIVE TV MASTER SWITCH ON O/H TURNED OFF. ALL COCKPIT FUNCTIONS NORM. ODOR EMITTED FROM COCKPIT FRONT GASPERS. WHILE TRYING TO DUP WRITE UP ON GROUND W/MX SAME ODOR NOTICED WITH APU'S & BOTH PACS RUNNING. ODOR COMING FROM ECS (PACS & AC SYS) PILOT DEBRIEFED & INFORMED MX PACKS (ECS SYS) RUNNING SAME ODOR APPEARED IN COCKPIT & CABIN WITH LIVE TV SYS OFF, FOUND APU OVERSERVICED CKD. DECON OF ENVIRON CONTROL SYS. CHANGED RECIRC FILTERS & OZONE FILTERS. NO ODOR NOTICED. OPS & SYS CK FOR INFO MASTER SWITCH SHUTS SYS OF "LIVE TV" NOT CSS SYS. NO DEFECT NOTED WITH LIVE TV. 2L72 4F RTA28NM 20050607001482005060700148EA 2005 6 7 QXEA200500932 120050502A5753 BRACKET CNDAIRCL600 CL6002C10 1390015EA ZONE 600 WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - RIGHT WING, OUTBOARD FLAP, INBOARD SIDE ROLLER GUIDE BRACKET WORN. REPAIRED IAW CRJ700 SRM 57-51-02-201-001-A01 AND SRM 51-42-21-001-001-A01. 2L72 4F RTA21EA 20050607001532005060700153EA 2005 6 7 QXEA200500926 120050510A5310 DOOR FRAME CNDAIRCL600 CL6002C10 1390015EA ZONE 200 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - AFT BAGGAGE DOOR SURROUND STRUCTURE FORWARD LOWER COAMING HAS GOUGES. REPAIRED IAW REO 670-53-61-168 AND HORIZON AIR EA R-53-324. 2L72 4F RTA21EA 20050607001572005060700157EA 2005 6 7 COMA0560310 120050518A335020131A BATTERY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSDISCHARGED A COMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SO01472CA8093 615 7667 FLIGHT 5411 - EMERGENCY LIGHTS ARE INOP. REPLACED THE EMERGENCY BATTERIES. 2L72 4F RTA21EA 20050607001582005060700158EA 2005 6 7 COMA0560311 120050518A291673031 RESERVOIR CNDAIRCL600 CL6002B19 1900309EA NR 3 UNRELIABLE A COMAO OTHER JS WARNING INDICATION AFFECT SYSTEMS APAPPROACH 1 SO01962CA23183 7123 FLIGHT 5142 - GEAR DISAGREE WARNING. REPLACED THE NR 3 HYDRAULIC RESERVOIR. 2L72 4F RTA21EA 20050607001592005060700159EA 2005 6 7 COMA0560312 120050515A21707536893 COALESCER BAG CNDAIRCL600 CL6002B19 1900309EA LT & RT DIRTY A COMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO01467CA 7637 FLIGHT 5462 - STRONG OILY ODOR IN COCKPIT WHEN BLEED AIR SWITCHED FROM APU TO ENGINES. REPLACED COALESOR SOCKS. 2L72 4F RTA21EA 20050607001602005060700160EA 2005 6 7 COMA0570052 120050520A3220521051 TORQUE TUBE CNDAIRCL600 CL6002C10 1390015EA NLG CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01368CA6764 10075 NLG TORQUE TUBE AND OUTER CYCLINDER ARE CORRODED. PERFORMED A MAJOR REPAIR TO NLG BY REMOVING AND REPLACING THE TORQUE TUBE P/N 52105-1 IAW CRJ 700 AMM 32-21-22-400-801-A02 AND REMOVING CORROSION ON OUTER CYLINDER IAW GOODRICH SCR DAO NR 94-0-01 AND BOMBARDIER REO 670-32-21-053. REFERENCE BOMBARDIER SB 670BA-32-013 REV B AND GOODRICH 52000-32-16 DATED MAY 20/04. 2L72 4F RTA21EA 20050607001612005060700161NM 2005 6 7 05FDEA00697 120050329A5347S49291477075T65 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 MAIN DECK, ALONG STA 822 TO STA 835 LBL 27.5 SEAT TRACK CROWN FOUND CORRODED. MAIN DECK, SEAT TRACK CROWN CORROSION ALONG STA 822 TO STA 835 LBL 27.5. REMOVED AND FOUND EXCEED LIMITS AS PER SRM 53-70-00 FIG 3 VOL I. DISCREPANT SEAT TRACK TRIM OUT FROM STA 815 TO 850 LBL 27.5 AS PER SRM 53-70-00 FIG 1 VOL I AND REPROTECTED AS PER SRM 51-21-01 VOL II. HFEC CARRIED OUT AND FOUND NO CRACK EVIDENT. REPAIR PARTS REWORKED FROM S4932154-707513511 & S4929147-7075T6511 AND FABRICATED SPLICE PLATE FROM 7075T6 (0.05) AS PER SRM 53-70-00 FIG 1 VOL I. REPAIR PARTS REPROTECTED AS PER SRM 51-21-01 VOL II AND INSTALLED AS PER SRM 53-70-00 FIG 1 VOL I. 2L73 4F RTA22WE 20050607001622005060700162NM 2005 6 7 05FDEA00840 120050405A5320S2932021 FLOOR SUPPORT DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 CENTER CARGO COMPARTMENT, STA 1841 FLOOR SUPPORT AT X-15 FOUND CRACK AS MARKED. CENTER CARGO COMPARTMENT, STA 1841 FLOOR SUPPORT AT X-15 REMOVED AS PER SRM 51-31-01 VOL II. FLOOR SUPPORT FABRICATED AS PER DWG AGA 7170 AND INSTALLED NEW FABRICATED FLOOR SUPPORT AS PER SRM 51-31-01 VOL II. MINOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050607001662005060700166NM 2005 6 7 QXEA200500948 120050515A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09412QX 4059 PDX - DOCUMENT FUSELAGE SKIN CUTOUTS FABRICATION OF FILLERS AND DOUBLER AND OK TO INSTALL AND INSTALLATION OF PERMANENT REPAIR. REPAIRED IAW HORIZON AIR EA 6-53-363D AND RD 8/4-53-1235, ISSUE 1, SECTION 3. 2H72 4T RTA13NM 20050607001672005060700167NM 2005 6 7 QXEA200500949 120050515A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09412QX 4059 PDX - INSPECTED BLENDED AREA IN FUSELAGE BELLY AND CHECK DEPTH PER EA 6-53-362 D AND RD 8/4-53-1233, REPROTECT SURFACE. BLENDED IAW RD 8/4-53-1233 AND HORIZON AIR EA 6-53-362D AND FOUND TO BE WITHIN LIMITS. PRIMED IAW RD 8/4-53-1233 2H72 4T RTA13NM 20050607001712005060700171NM 2005 6 7 QXEA200500943 120050515A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09412QX 4059 PDX - 2 NICKS BELOW LAV SERVICE DOOR, 7 INCHES BELOW FORWARD CORNER. REPAIRED IAW RD 8/4-53-666. 2H72 4T RTA13NM 20050607001742005060700174NM 2005 6 7 QXEA200500946 120050516A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 200 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09412QX 4059 PDX - LEFT FUSELAGE HAS DENTS. REPAIRED IAW HORIZON AIR EA 6-53-551. 2H72 4T RTA13NM 20050607001752005060700175NM 2005 6 7 05FDEA01367 120050518A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 FWD CARGO BAY FRAME IS CREASED BS 600, STR 24L TO 25L. *S/D* REPAIRED FRAME PER SRM 51-40-3 AT BS 600 STR 24L-25L. 2L73 4F RTA3WE 20050607001762005060700176NM 2005 6 7 05FDEA01375 120050519A5230 SEAL DEPRESSOR BOEING727 727200 138407ENM CARGO DOOR DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25264FE 21626 AFT LOWER CARGO DOOR NR 2 FWD CORNER DAMAGED. 2L73 4F RTA3WE 20050607001772005060700177EA 2005 6 7 COMA0570054 120050520A5311CC670341757 FRAME CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01368CA6764 10075 FS 280 - FUSELAGE TRANSVERE BEAM IS CORRODED BEYOND LIMITS. PERFORMED A MAJOR REPAIR TO FS 280 TRANSVERSE BEAM BY REMOVING CORRODED BEAM AND INSTALLING NEW BEAM P/N CC670-34175-71AW CRJ 700 SRM 51-42-06-001-001-A01 AND INSTALLING REPAIR DOUBLERS P/NS 670-53-11-047-2 AND 670-53-11-047-3 AND INSTALLED RADIUS PLATE PN 670-53-11-047-4 IAW BOMBARDFIER REO 670-53-11-047 REV A. 2L72 4F RTA21EA 20050607001782005060700178EA 2005 6 7 COMA0570055 120050516A2782766383C ACTUATOR CNDAIRCL600 CL6002C10 1390015EA SLATS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01371CA5286 3101 10082 FLIGHT 5472, SLATS FAIL CAUTION. REPLACED LT INBOARD SLAT ACTUATOR. 2L72 4F RTA21EA 20050607001802005060700180NE 2005 6 7 PNSA050503 220050510A7200 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LEFT BIRD INGESTION A PNSAA UNSCHED LANDING CRJF.O.D. PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 AL03677PA 328 785288 DEPARTING DUT CREW OBSERVED BIRDS (SEAGULLS) ON ROTATION. CREW REPORTED INGESTING 3 BIRDS IN LT ENGINE AND TORQUE ROLLED BACK TO 20 PERCENT. ENGINE OVERTEMP LIGHT CAME FOR 20 SECONDS WITH ASSOCIATED COMPRESSOR STALL. AFTER 1.5 MINUTES TORQUE CAME BACK TO 60 PERCENT THEN RETURNED TO NORMAL AND ALL OTHER PARAMETERS WERE NORMAL. FLIGHT CONTINUED TO CDB WHERE A UNSCHEDULED LANDING WAS MADE DUE TO WEATHER IN DUT. MAINTENANCE INSPECTED AIRCRAFT IN CDB AND AIRCRAFT WAS FERRIED TO ANC FOR ENGINE REPLACEMENT. 2L72 4T4 TRTA52EU E8NE 20050607001812005060700181NM 2005 6 7 QXEA200500952 120050519A3320404930 LIGHT DHAV DHC8 DHC8202 2809007NM ZONE 200 BURNED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM09345PH 476 SEA- HOT ELECTRICAL SMELL, SMOKE SEEMS TO BE COMING FROM AREA ABOVE FLIGHT ATTENDANT CLOSET. MAINTENANCE FOUND FLUORESCENT LIGHT SOCKET ON OVERHEAD CABIN LIGHT AT SEAT 1DE BURNT AND SMOKING. REMOVED AND REPLACED FLUORESCENT OVERHEAD CABIN LIGHT AT SEAT 1DE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050607001822005060700182CE 2005 6 7 ACE052105 120050521A561010138402523 WINDSHIELD BEECH 1900 1900C 1154161CE COCKPIT CRACKED E YADAO OTHER O OTHER DEDESCENT 1 AL03113AX 2344 UC41 PILOT REPORTED LT WINDSHIELD CRACKED ON DESCENT. REPLACED FAILED WINDSHIELD (OUTER PLY FAILED). 2L72 4T RTA24CE 20050607001862005060700186EU 2005 6 7 05FDEA01392 120050520A5730 SKIN AIRBUS310 A310203 3930313EU RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25403FE 230 RIGHT WING FUEL CUTOUT FOR PANEL 650HB HAS ONE EXISTING PLUG BROKEN ON ONE SIDE. REMOVED DOME NUT IAW A310 SRM 51-40-21. REMOVED PLUG IAW A310 SRM 51-40-51. REAMED HOLE TO 0.4215 TO REMOVE CRACK IAW A310-SRM 51-40-44. NO DEFECTS NOTED IAW NTM 51-10-01. REPAIRED HOLE IAW EA 6-5710-88828 PT1 AND TD J1/S1/00726/2005. INSTALLED DOME NUT IAW A310 SRM 51-40-21, DOME SEALED IAW A310 SRM 51-76-20. THIS IS A MAJOR REPAIR PER FEDEX GMM 6-2-100. 2L72 4F RTA35EU 20050607001872005060700187 2005 6 7 05FDEA01405 420050520A3417 ADC AIRBUS300 A300F4605R 3930327EU NR 1 MALFUNCTIONED A FDEAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 SO25672FE 779 ON TAKEOFF ROLL, CAPTAIN HAD NO AIRSPEED INDICATION ON PFD, REJECTED TAKEOFF 80 KTS. PURGED NR 1 PITOT TUBE OF FOREIGN MATERIAL AND REMOVED AND REPLACED NR 1 ADC PER AB MM 34-11-34. PERFORMED LOW LEVEL LEAK CK AS PRECAUTION. NR 1 AIRSPEED NOW CKS NORMAL DURING LEAK CHECK. OK TO CONTINUE. PREMATURE REMOVAL/INSTALLATION OFF MFG 4045053-914. 2L72 4F RTA35EU 20050607001892005060700189NM 2005 6 7 QXEA200500954 120050523A5230 HANDLE BOMBDRDHC8 DHC8402 1390042NM ZONE 800 LACK OF LUBE A QXEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM09405QX 4047 GEG - ON FLIGHT 2322 (SEA-GTF), FLIGHT DIVERTED TO GEG. INTERMITTENT FORWARD BAGGAGE DOOR WARNING LIGHT. UPON AIRCRAFT ARRIVAL, EXAMINED FORWARD BAGGAGE DOOR HANDLE AND FOUND DOOR SECURE, BUT AFT PORTION OF HANDLE SLIGHTLY PROTRUDED. CLEANED AND LUBED DOOR HANDLE MECHANISM. OPERATIONAL TEST GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050607001912005060700191CE 2005 6 7 20030850 120050523A32301143880003 POWERPACK BEECH 1900 1900D 1154162CE HYD SYSTEM MALFUNCTIONED A GLBAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 NM03169GL4541 UE169 UPON APPROACH WHEN LANDING GEAR SELECTED DOWN, GEAR WOULD NOT EXTEND. FLIGHT CREW USED THE MANUAL GEAR DOWN HAND PUMP TO EXTEND GEAR SUCCESSFULLY AND LANDED. MAINTENANCE DISCOVERED HYDRAULIC POWER PACK CIRCUIT BREAKER WAS TRIPPED. RESET CIRCUIT BREAKER AND PERFORMED GEAR SWING AND COULD NOT DUPLICATE. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA24CE 20050607001952005060700195WP 2005 6 7 IXXA0500077O 120050522A3897 WIRE DOUG DC8 DC862 3021970WP WATER PUMP BURNED A IXXAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW11799AL763733138 45922335 DURING CRUISE AT APPROX 1 HOUR AND 20 MINUTES INTO FLIGHT FROM KSUU, F/A CALLED AND REPORTED A BURNING ODOR IN THE LEFT LAV. THE POWER SOURCE WAS ISOLATED AND ODOR WAS STILL PRESENT. CREW DIVERTED AIRCRAFT TO KSFO AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND FOUND SOURCE TO BE COMING FROM THE WATER PUMP. ELECTRIC WIRING DISCONNECTED AND C/B COLLARD. THIS ITEM WAS TRANSFERRED TO DMI 32156 IN ACCORDANCE WITH ATI MEL AND IS A CATAGORY D. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F 4A25 20050608000012005060800001SO 2005 6 8 X6PA200500003 120050523A272063420006 BAR PIPER PA34 PA34200 7103405SO RUDDER PEDAL FRACTURED E X6PAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 SO33152BW5388 347250187 LEFT RUDDER PEDAL BAR ASSEMBLY 63420-006 FRACTURED AT RIGHT OUTBOARD WELD. FRACTURE OF CONTROL TUBE CAUSED A LOSS OF STEERING AND RUDDER CONTROL. CORROSION FOUND ON THE INSIDE WALL OF THE TUBE AT THE BREAK. 1L72 3O A7SO 20050630000022005063000002EU 2005 6 30 SA05079 120050623A4990 APU AIRBUS320 A320214 3930316EU APU BAY LEAKING A USAAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 EA19118US 1264 ICT FLT 100 EN ROUTE SAN TO PHL - DURING THE FLIGHT, THE NR 1 IDG LOW OIL PRESSURE LIGHT ILLUMINATED. THE IDG WAS DISCONNECTED PER PROCEDURES. SHORTLY AFTER THE APU WAS STARTED, THE APU HAD AN AUTO-SHUTDOWN. THE FLIGHT DIVERTED TO THE NEAREST SUITABLE AIRPORT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE SERVICED BOTH THE NR 1 ENGINE IDG AND THE APU DUE TO LOW OIL LEVELS. LEAK CHECKED OK. 2L72 4F RTA28NM 20050608000072005060800007NM 2005 6 8 05FDEA01381 120050520A5713 STRINGER BOEING727 727200 138407ENM RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 RT WING UPPER STR 9 CRACKED AT WS 656.5. REPAIRED STRINGER PER FED EX EA 7-5710-86294. 2L73 4F RTA3WE 20050608000112005060800011WP 2005 6 8 ARWA20050507 120050528A2497 WIRE DOUG DC8 DC863F 302198FWP NR 2 GENERATOR OPEN A ARWAJA DUMP FUEL UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 SO19441J 45988 AFTER TAKEOFF, ZNS ON NR 2 GENERATOR WITH LEFT EMERGENCY BUS POWER FAIL LIGHT ON. PERFORMED ABNORMAL CHECKLIST TO NO AVAIL; PERFORMED FUEL DUMP AS PER CHECKLIST. TRANSFERRED TO DMI 19258 AS PER MEL 24-1 CAT-C (ON T/S FOUND NR 2 GENERATOR CAUSING FAIL ZNS). OPENED PYLON PANELS, TROUBLESHOT NR 2 GEN. WIRES, FOUND OPEN; REPAIRED AS PER M/M 24-00-01, OPS CHECK GOOD; CLOSED PYLON PANELS IAW M/M 71-00 AND SRM 51-3-0. CLEARED DMI NR 19258. 2L74 4F 4A25 20050608000122005060800012EA 2005 6 8 DJFA2005104 120050531A3260600509679 CONTROLLER CNDAIRCL601 CL6012A12 1900303EA COCKPIT BROKEN E DJFAO OTHER P NO WARNING INDICATION LDLANDING 1 EA23627CW 3027 AFTER MLG SELECTED DOWN, LT MLG INDICATOR LIGHTS DID NOT ILLUMINATE. CREW TESTED BULBS AND PERFORMED A FLY-BY PAST TOWER. CONTROLLER REPORTED THAT MLG APPEARED TO BE DOWN AND LOCKED. A MANUAL MLG EXTENSION PERFORMED AND AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LIGHT BULBS FOR THE GEAR INDICATION. UPON FURTHER INVESTIGATION IT DISCOVERED THAT SOCKET FOR LT DOWN AND LOCKED INDICATION IN MLG CONTROLLER BROKEN. MLG CONTROLLER REPLACED. OPS CHECK GOOD, AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21AE 20050608000132005060800013SO 2005 6 8 RAIA00505026 120050527A7500 COUPLING EMB 145 EMB145LR 3260212SO BLEED AIR SYS LOOSE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03829HK 145281 FLT 3528-RIC NR 1 BLEED LEAK INDICATION. MAINTENANCE DEFERRED PER MEL 36-11-05. MAINTENANCE SECURED LOOSE COUPLING IN BAG BAY. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050608000142005060800014NM 2005 6 8 SB05066 120050603A3260 CIRCUIT BREAKER BOEING737 7374B7 1384702NM P6-2 PANEL TRIPPED A USAAO OTHER O OTHER DEDESCENT 1 EA19448US 24892 UPON LOWERING LANDING GEAR, CAPTAIN REPORTED THE NOSE LANDING GEAR UNSAFE LIGHT ILLUMINATED. CREW ACCOMPLISHED A FLYBY OF THE TOWER WHEREAS THE GEAR WAS CONFIRMED DOWN. CREW THEN NOTICED THE AIR/GROUND RELAY AND LIGHTS CIRCUIT BREAKER WAS POPPED. CREW RESET CIRCUIT BREAKER AND RECEIVED A SAFE GEAR INDICATION. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE CHECKED RETENTION ON CIRCUIT BREAKER P6-2 C21 AIR/GROUND RELAY. NO DEFECTS NOTED. INSPECTED NOSE GEAR PROX SWITCHES, WIRES AND NOSE GEAR. NO DEFECTS NOTED. AIRCRAFT OK FOR SERVICE. 2L72 4F RTA16WE 20050608000152005060800015EA 2005 6 8 COMA0560321 120050601A5210 DOOR FRAME CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01932CA 7038 THREE CRACKS FOUND PAX DOOR FRAME FS 320.00. REPAIRED IAW REO 601R-52-11-402. 2L72 4F RTA21EA 20050608000162005060800016EA 2005 6 8 COMA0560322 120050601A5712 RIB CNDAIRCL600 CL6002B19 1900309EA WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01932CA 7038 LT AND RT BATT RIB CRACKED. REPAIRED I/A/W REO 601R-57-51-046 AND REO 601R-57-51-211. 2L72 4F RTA21EA 20050608000172005060800017EA 2005 6 8 COMA0560323 120050601A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01932CA 7038 SKIN CRACKED AT NLG OUTOUT AFT RADIUS. REPAIRED IAW REO 601R-53-11-048. 2L72 4F RTA21EA 20050608000182005060800018EA 2005 6 8 COMA0560324 120050601A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01932CA 7038 CLIP CRACKED AT FS 280 WL30 AFT SIDE. REPAIRED IAW REO 601R-53-11-171. 2L72 4F RTA21EA 20050608000202005060800020EA 2005 6 8 COMA0560326 120050601A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01710CA 7241 LT 621.00 FRAME CRACKED. REPAIRED IAW REO 601R-53-61-117. 2L72 4F RTA21EA 20050608000212005060800021EA 2005 6 8 COMA0560327 120050601A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01710CA 7241 LT FRAME CRACKED AT STR 10. REPAIRED IAW REO 601R-53-61-487. 2L72 4F RTA21EA 20050608000242005060800024EU 2005 6 8 2005UALA00446 220050516A7510 ANTI-ICE VALVE BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU NR 1 ENGINE INOPERATIVE A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29350UA 24301 DIVERTED DUE TO INOPERATIVE NR 1 ENGINE ANTI-ICE VALVE. NR 1 ENGINE COWLING ANTI ICE VALVE FAILED.REPLACED VALVE PER AMM 30-21-11. NO FURTHER INCIDENT REPORTED. 2L72 4F4 FRTA16WE E21EU 20050608000262005060800026 2005 6 8 2005UALA00448 420050512A2565D31516113 SLIDE AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29830UA 1243 SLIDE HAD BEEN DEPLOYED CAUSING HOLES IN INFLATION TUBE AND HEAVY SEAM DEGRADATION. PROBABLE CAUSE OF HOLES IN THE INFLATABLE IS FOREIGN OBJECT DAMAGE (FOD) DURING DEPLOYMENT OR PERHAPS DUE TO HANDLING DURING TRANSPORTATION. SINCE THE DAMAGE WAS BEYOND THE CMM ALLOWED REPAIR LIMITS, THE UNIT WAS SENT TO THE OEM FOR REPAIR. THE OEM WILL HAVE TO EVALUATE THE EXTENT OF THE DAMAGE AND PERFORM OEM REPAIRS WHERE APPLICABLE. 2L72 4F4 FRTA28NM E40NE 20050608000272005060800027 2005 6 8 2005UALA00449 420050513A256562774414 SLIDE BOEING777 777222 1385219NM PWA PW4077PW4077 NE FOD A UALAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP29771UA 26932 WHEN SLIDE OPENED THERE WAS A SANDBAG AND SCREWDRIVER PACKING INSIDE SLIDE. COMPONENT SHOP MAINTENANCE QUALITY ISSUE. SHOP MECHANIC TRAINING COULD BE THE PROBABLE CAUSE. SHOP THAT PERFORMED THIS DISCREPANT PACKING NO LONGER EXISTS. SLIDE IS NOW MAINTAINED BY AN OSV SHOP. PACKING DISCREPANCY IS CONSIDERED AN ISOLATED INCIDENT. 2L72 4F4 FRTT0001SE E46NE 20050608000282005060800028 2005 6 8 2005UALA00451 420050515A3441 IRU BOEING757 757222 1384956NM PWA 2037 PW2037 NE RIGHT FAILED A UALAA UNSCHED LANDING O OTHER DEDESCENT 1 WP29541UA 25253 FLIGHT DIVERTED DUE TO RIGHT IRU FAILURE, VISIBILITY RESTRICTIONS AND LOW CEILINGS. CENTER IRU FAULT LIGHT ON, IRU FAIL. REPLACED THE CENTER IRU AND OPS CHECK PER AMM. 2L72 4F4 FRTA2NM E17NE 20050608000302005060800030NM 2005 6 8 2005UALA00453 120050519A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29502UA 24623 FWD GALLEY STA 365 RBL 11 FLOORBEAM TOP IS CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS. FABRICATED ANGLE REPAIR IAW MM 53-00-98 AND INSTALLED PER MM 53-00-98 2L72 4F4 FRTA2NM E17NE 20050608000322005060800032NM 2005 6 8 2005UALA00455 120050519A5320 INTERCOSTAL BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29502UA 24623 AFT CARGO INTERCOSTAL IS CORRODED BS 1360 TO 1380 RBL 26. REMOVED CORROSION AND FABRICATED INTERCOSTAL RPR AND INSTALLED PER SRM 53-00-04 AND BAC DWG 146N5427 2L72 4F4 FRTA2NM E17NE 20050608000332005060800033NM 2005 6 8 2005UALA00456 120050519A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29502UA 24623 LEFT SIDE OF ACFT BETWEEN FR 740 & 760 STRS 15L AND 16L HAS 1 DENT. FABRICATED DOUBLER RPR PER SRM 53-00-01 AND INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050608000342005060800034NM 2005 6 8 2005UALA00457 120050519A3350 LIGHT BOEING737 737322 1384676NM ROW 15 SHORTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29338UA 24242 EMERGENCY EXIT FLOOR LIGHTS BEYOND ROW 15 INOP. LIGHT STRIP SHORTED, REPLACED. 2L72 4F RTA16WE 20050608000352005060800035NM 2005 6 8 2005UALA00458 120050519A5330 SKIN BOEING737 737322 1384676NM FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29313UA 23674 EXTERIOR FUSELAGE BELOW 1R BETWEEN FRAMES 277 AND 294 STR 22R AND 23R BELOW A REPAIR DENTED. REMOVED THE DAMAGE FABRICATED A DOUBLER AND TRIPLER PER SRM 53-00-01 AND INSTALLED THE REPAIR PER SRM 53-00-01. 2L72 4F RTA16WE 20050608000442005060800044NM 2005 6 8 L0FR200500006 120050524A32462607081 WHEEL BOEING747 747200 1384847NM MLG CRACKED B Q2SAK NONE O OTHER ININSP/MAINT 1 AL03 CRACKED KEY BOSS IDENTIFIED WITH EDDY CURRENT PER HONEYWELL COMPONENT MAINTENANCE MANUAL 32-45-12 APPENDIX A, KEY BOSS NDT INSPECTION AREA. 2L74 4F RTA20WE 20050608000462005060800046NM 2005 6 8 72300182 120050504A5311 FRAME BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAEG CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 1 INCH AREA OF CORROSION ON FRAME. 2L73 4F4 FRTA3WE E2EA 20050608000482005060800048NM 2005 6 8 72300184 120050413A5340 FITTING BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAEG CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 1.5 INCH AREA OF CORROSION ON FITTING. 2L73 4F4 FRTA3WE E2EA 20050608000502005060800050NM 2005 6 8 72300186 120050418A5340 FITTING BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE STRINGER CRACKED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 INCH CRACK ON STRINGER FITTING. 2L73 4F4 FRTA3WE E2EA 20050608000582005060800058EU 2005 6 8 MALA050426 120050519A3020 DUCT SAAB SF340 340B 7860101EU LT INTAKE HEAT DAMAGED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15447XJ 340B447 AIR TURNBACK, LT INTAKE HEAT INOPERATIVE. REMOVED AND REPLACED LOWER DUCT. 2L72 4T RTA52EU 20050608000622005060800062NM 2005 6 8 CALA0500161 120050523A524065554787 GATE BOEING737 7373T0 1384582NM R-2 DOOR CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714325 23455 INSPECTION FOUND THE R-2 DOOR LOWER GATE CORRODED ON INTERIOR AND EXTERIOR SURFACE. THE LOWER GATE WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20050608000642005060800064NM 2005 6 8 CALA0500163 120050523A5315141A5504 FLOORBEAM BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2724212 28772 INSPECTION FOUND FLOORBEAM CORRODED AT STA 328, RBL 45 TO RBL 49. THE FLOORBEAM WAS REPAIRED IAW ECRA 5321-01227. 2L72 4F RTA16WE 20050606000052005060600005 2005 6 6 UPS05144492 420050518A2565 CYLINDER AIRBUS300 A300B4622R 3930312EU PAX DOOR SLIDE DISCHARGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01129UP 0813 MAIN CABIN DOOR SLIDE INOPERATIVE. SERVICED FWD DOOR EMERGENCY ACTUATOR CYLINDER PER MM 52-10-14-3. THIS CLEARS M302648. 2L72 4F RTA35EU 20050303000722005030300072WP 2005 3 3 0500189947 120050211A2910 LINE DOUG DC9 DC931 3022065WP HYD SYSTEM LEAKING A NWAAO OTHER K FLUID LOSS CRCRUISE 1 GL018938E 47161 DURING FLIGHT, THE AIRCRAFT LOST PRESSURE AND A TOTAL LOSS OF FLUID FROM THE RIGHT HYDRAULIC SYSTEM. COMPLIED WITH COM PROCEDURES AND AIRCRAFT CONTINUED TO ORIGINAL DESTINATION. THE LANDING AT BTR WAS UNEVENTFUL. MAINTENANCE FOUND A LINE COMING FROM THE ELECTRIC HYDRAULIC PUMP LEAKING AND REPLACED IT. ALSO, PER PROCEDURES, THE ELECTRIC PUMP, ENGINE DRIVEN PUMP, AND ALL SYSTEM FILTERS WERE REPLACED. THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20041221000562004122100056NM 2004 12 21 A6WA200440204 120050113A5314 KEELBEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29307UA 23668 KEEL BEAM LOWER CHORD BS 685-695 IS CRACKED. TRIMMED OUT CRACKED LOWER CHORD. INSTALLED REPAIR ANGLE AND STRIP. 2L72 4F4 FRTA16WE E2GL 20050303000732005030300073WP 2005 3 3 0500219610 120050220A2170 COUPLING DOUG DC9 DC932 3022066WP WATER SEPARATOR SEPARATED A NWAAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 GL01610NW 47432 DURING CRUISE FLIGHT, THE CABIN CONTINUED TO CLIMB. WHEN CABIN PRESSURE REACHED 9500 FEET, THE CREW SWITCHED TO MANUAL PRESSURE CONTROL AND STILL UNABLE TO STOP THE LOSS OF PRESSURE. BOTH PACKS WERE AT FULL COLD WITH 18-20 PSI, ALL ANTI-ICE OFF, AND OUTFLOW VALVE AT FULL CLOSE. COMPLIED WITH COM PROCEDURES, DECLARED AN EMERGENCY, DESCENDED TO 10,000 FEET, AND CONTINUED TO DESTINATION. MAINTENANCE AT STL DISCOVERED TWO SEPARATED COUPLINGS AT THE RIGHT WATER SEPARATOR AND ONE AT THE LEFT AIR CYCLE MACHINE. CLAMPS WERE SECURED AND THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20050303000752005030300075NE 2005 3 3 P5CA0501319 220050209A73207321686004 ACTUATOR BOEING747 747230B 1384889NM GE CF6 CF650E2 30018NE FUEL CONDITION INOPERATIVE A P5CAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 EA15509MC 21221 517297 DURING ENGINE START NR 3 ENGINE WOULD NOT LIGHT OFF. TROUBLESHOT, FOUND FUEL CONDITION ACTUATOR INOP. REMOVED & REPLACED CONDITION ACTUATOR PER MM 76-11-00. OPS NORMAL. 2L74 4F4 F A20WE E23EA 20050107001712005010700171NM 2005 1 7 SWAA050012 120050102A53156545834 FLOORBEAM BOEING737 7373K2 13844BANM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29345SA 23786 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM T-CAP AT BS 344, LBL 9, CORRODED. REMOVED AND REPLACED FLOORBEAM T-CAP PER SRM. 2L72 4F RTA16WE 20050107001752005010700175NM 2005 1 7 SWAA050028 120050104A531565C25723 FLOORBEAM BOEING737 7373K2 13844BANM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29345SA 23786 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM WEB AT BS 617, RBL 63, CRACKED. REMOVED AND REPLACED WEB PER SRM. 2L72 4F RTA16WE 20050107001762005010700176NM 2005 1 7 SWAA050029 120050104A53156545810 FLOORBEAM BOEING737 7373K2 13844BANM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29345SA 23786 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM UPPER T-CAP AT BS 312, LBL 12 TO LBL 13, CORRODED. REPAIRED FLOORBEAM PER EA. 2L72 4F RTA16WE 20050107001802005010700180NM 2005 1 7 SWAA050013 120050102A53206517685 FITTING BOEING737 7373K2 13844BANM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29345SA 23786 DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR UPPER FWD CORNER, AT DOOR CUTOUT, CORNER V-FITTING CRACKED. REMOVED AND REPLACED FITTING PER SRM. 2L72 4F RTA16WE 20050107001872005010700187NM 2005 1 7 SWAA050019 120050103A256065C16820 ATTACH FITTING BOEING737 7373K2 13844BANM CABIN CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29345SA 23786 DURING SCHEDULED 1/2D CHECK, FOUND L1 DOOR EVAC SLIDE AFT GIRT BAR ATTACH FITTING, CORRODED. REMOVED AND REPLACED FITTING PER MM. 2L72 4F RTA16WE 20050107002022005010700202NM 2005 1 7 SWAA050025 120050104A575465C26603192 STRUCTURE BOEING737 7375H4 138449DNM L/E SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29527SW 26569 DURING SCHEDULED C4 CHECK, FOUND RT WING NR 4 L/E SLAT DELAMINATED. REMOVED AND REPLACED NR 4 L/E SLAT PER MM. 2L72 4F RTA16WE 20050107002042005010700204 2005 1 7 SWAA050021 420050104A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29365SW 26576 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050107002062005010700206NM 2005 1 7 SWAA050023 120050104A551265C25727 SKIN BOEING737 7375H4 138449DNM HORIZ STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29501SW 24178 DURING SCHEDULED C4 CHECK, FOUND RT HORIZONTAL STAB, LOWER SKIN AT STA 140, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050107002072005010700207 2005 1 7 SWAA050024 420050104A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29656SW 28401 DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050107002082005010700208NM 2005 1 7 SWAA050030 120050105A533065662134 STRAP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29636WN 27709 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN STRAP UNDER APU DRAIN RESERVOIR, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20050107002142005010700214NM 2005 1 7 SWAA050026 120050104A3350D71702001 BATTERY BOEING737 7373H4 1384600NM CABIN DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29330SW 23694 DURING SCHEDULED 1/4D CHECK, FOUND EMERGENCY EXIT LIGHT AT BS 673, LOW CHARGE. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20050107002152005010700215NM 2005 1 7 SWAA050027 120050104A55146547598 FITTING BOEING737 7373K2 13844BANM HORIZ STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29345SA 23786 DURING SCHEDULED 1/2D CHECK, FOUND HORIZONTAL STAB CENTER SECTION UPPER FITTING AND THRUST BEAM, CRACKED. REMOVED AND REPLACED FITTING PER MM. 2L72 4F RTA16WE 20050107002162005010700216NM 2005 1 7 SWAA050008 120050102A53116516301 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29398SW 27692 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 188, STRINGER 17L, CRACKED. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20050107002172005010700217NM 2005 1 7 SWAA050009 120050102A55346547450 FITTING BOEING737 7373H4 1384600NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29398SW 27692 DURING SCHEDULED D-CHECK, FOUND VERTICAL FIN REAR SPAR LT AND RT PRIMARY ATTACH CLEVIS FWD AND AFT LUGS CORRODED. REPAIRED VERTICAL FIN PER ER. 2L72 4F RTA16WE 20050307000432005030700043EA 2005 3 7 QXEA200500244 120050210A5242 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 800 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - MAIN AVIONIC COMPARTMENT DOOR HAS THREE AREAS ABRAIDED BY CLOSING HANDLE ON OUTER SKIN. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01, 51-21-11-001-001-A01, 51-25-06-001-001-A01 AND 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050107001852005010700185NM 2005 1 7 SWAA050017 120050103A32407816903 CONTROL MODULE BOEING737 7373H4 1384600NM MLG W/W LEAKING A SWAAA UNSCHED LANDING K FLUID LOSS CRCRUISE 1 SW29615SW 27698 DIVERSION/DECLARED EMERGENCY. AT CRUISE ALTITUDE LOST B-SYSTEM HYDRAULIC FLUID QUANTITY. REMOVED AND REPLACED B-SYSTEM BRAKE CONTROL MODULE PER MM. 2L72 4F RTA16WE 20050107002052005010700205NM 2005 1 7 SWAA050022 120050104A53306545857 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29343SW 24151 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 950, ABOVE STRINGER 19R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20050107002092005010700209 2005 1 7 SWAA050031 420050105A256563550 SLIDE BOEING737 7377H4 1384404NM L1 & R1 DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29703SW 27837 DURING SCHEDULED HC1 CHECK, FOUND L1 AND R1 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED SLIDES PER MM. 2L72 4F RTA16WE 20050107002122005010700212NM 2005 1 7 SWAA050010 120050102A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29330SW 23694 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 500C + 6, ABOVE STRINGER 15R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20050110000912005011000091NM 2005 1 10 USAA041049 120050109A554265C2584151 SKIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU RUDDER DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19435US41422 24557 PIT - Q1 - RUDDER SKIN, .1250 INCH X .2500 INCH AREA, DAMAGE, LT SIDE 5.5 INCH FWD OF T/E 62.5 INCH UP FROM BOTTOM. PREPARED DAMAGED AREA, LIGHT SANDING, INSTALLED MULTI LAYERED REPAIR IAW SRM AND EA. 2L72 4F4 FRTA16WE E21EU 20050111000342005011100034EU 2005 1 11 AWXA200500013 120050105A3397ABS0374A24 CABLE AIRBUS320 A320232 3930326EU CABIN PULLED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28639AW 471 PHX - EEL - DURING E-08 CHECK FUNCTIONAL TEST OF THE EMERGENCY LIGHT SYSTEM, THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 12 RT WAS FOUND INOPERATIVE. MAINTENANCE FOUND BOTH WIRES PULLED OUT OF THE TERMINALS AT EMERGENCY ESCAPE PATH LIGHT FIXTURE SEAT ROW 12 RT, RE-TERMINATED WIRES WITH NEW TERMINAL LUGS, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050111000362005011100036EU 2005 1 11 AWXA200500018 120050108A3350321454 POWER SUPPLY AIRBUS320 A320231 3930325EU CABIN FAILED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28631AW293071514 077 LAS - EEL - DURING 8-DAY CHECK THE LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL) FAILED TEST. MAINTENANCE REMOVED AND REPLACED LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050111000422005011100042NM 2005 1 11 AWXA200500002 120050103A3397BMS13311122 WIRE BOEING757 7572S7 1384962NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28903AW 23323 PHX - EEL - DURING 4-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT ON THE END OF SEAT ROW 10 LT HAD TWO LAMPS INOPERATIVE. MAINTENANCE REPLACED BOTH LAMPS, NO HELP. REPAIRED BROKEN WIRE AT FORWARD EMERGENCY ESCAPE PATH LIGHT SEAT ROW 10 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20050111000432005011100043NM 2005 1 11 AWXA200500003 120050103A3397BMS13311122 WIRE BOEING757 7572S7 1384962NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28903AW 23323 PHX - EEL - DURING 4-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 24 LT WAS INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 24 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20050111000442005011100044EU 2005 1 11 AWXA200500004 120050102A2910NAS16128 PACKING AIRBUS320 A320231 3930325EU HYDRAULIC SYS RUPTURED A AWXAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 WP28629AW 076 PHX - EMERGENCY LANDING - FLT 0270 - EN ROUTE FROM IAH TO PHX RECEIVED CLASS 1 ECAM MESSAGE FOR GREEN HYDRAULIC LOW RESERVOIR THAT WAS FOLLOWED BY GREEN LOW PRESSURE, AS A PRECAUTION DECLARED EMERGENCY LANDING. MAINTENANCE REPLACED A RUPTURED PACKING ON PLUG, INSTALLED ON GREEN HYDRAULIC MANIFOLD NEAR PRESSURE TRANSDUCER (1065GN). LEAK CHECK WAS GOOD. 2L72 4F RTA28NM 20050107001722005010700172NM 2005 1 7 SWAA050032 120050105A53116546539 FRAME BOEING737 7373K2 13844BANM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29345SA 23786 DURING SCHEDULED 1/2D CHECK, FOUND FRAME INNER CHORD AT LT BS 616, WL 208, CRACKED. REMOVED AND REPLACED FRAME CHORD SECTION PER T1-153-018. 2L72 4F RTA16WE 20050107001792005010700179 2005 1 7 SWAA050016 420050103A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29371SW 26598 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050107001862005010700186NM 2005 1 7 SWAA050018 120050103A53126546568 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29330SW 23694 DURING SCHEDULED 1/4D CHECK, FOUND 3 EACH CRACKS AT PANEL NR 7 AND ONE EACH CRACK AT PANEL NR 2, ON BULKHEAD WEB AT BS 1016. REPAIRED BULKHEAD WEB PER EA. 2L72 4F RTA16WE 20050107002032005010700203NM 2005 1 7 SWAA050020 120050104A2782654456114 ACTUATOR BOEING737 7372H4 138448CNM NR 3 SPOILER FAILED A SWAAA UNSCHED LANDING F FLT CONT AFFECTED NRNOT REPORTED 1 SW29094SW 23053 AIR TURNBACK, NR 3 SPOILER STUCK IN UP POSITION, WITH HYDRAULIC PRESSURE. REMOVED AND REPLACED NR 3 SPOILER ACTUATOR PER MM. 2L72 4F A16WE 20050107002132005010700213NM 2005 1 7 SWAA050011 120050102A5315BAC1509100146 FLOORBEAM BOEING737 7373K2 13844BANM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29345SA 23786 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM AT BS 767 + 5, LBL 13, CORRODED. REPAIRED FLOORBEAM PER EA. 2L72 4F RTA16WE 20050111000102005011100010WP 2005 1 11 AALA20050003 120050101A323039370335503 CYLINDER DOUG DC9 DC983 3022083WP LT MLG BROKEN A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21568AA 49349 PHX - EN ROUTE PHX TO ORD LEFT MAIN GEAR WOULD NOT RETRACT AFTER TAKEOFF. RETURNED PHX AND LANDED WITHOUT INCIDENT. FOUND LEFT GEAR BUNGEE CYLINDER ROD END BROKEN. REMOVED AND REPLACED LEFT GEAR CYLINDER. ACCOMPLISHED GEAR SWING AND LUBE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050111000262005011100026NE 2005 1 11 AWXA200500016 220050107A75325950041108 BLEED VALVE AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE NR 1 ENGINE MALFUNCTIONED A AWXAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 WP28626AW12844 65 CLIMBOUT 8000 FT LOUD BANG LT SIDE, ALL ENG IND NORM. TURNED BACK. A SECTION OF NR 1 ENG I/B C-DUCT INNER LINER FOUND MISSING IN AREA OF 10TH STAGE BLEED VALVE. FOUND SMALL DENT IN L/E OF STAB 10 INCHES FROM OB END. R&R LT HORIZONTAL STAB END CAP, NR 1 ENG LT TRANSLATING SLEEVE ASSY, NR 1 ENG RT IB TR. FOUND NR 1 ENG NOZZLE ASSY DAMAGED. REPLACED COMMON NOZZLE ASSY, CKS GOOD. REPLACED 10TH STAGE BLEED VALVE & SOLENOID VALVE, CKS GOOD. THRUST REVERSER AND SLEEVE WERE REPAIRED IAW ROHR/IAE V2500 CMM 78-30-00 REV. 12. THE 10TH STAGE SOLENOID VALVE WAS FOUND TO FAIL SOLENOID PULL IN TEST ON "B" COIL. NO TROUBLE WAS FOUND WITH THE 10TH STAGE BLEED VALVE AT VENDOR 2L72 4F4 FRTA28NM E311NE 20050111000482005011100048 2005 1 11 AWXA200500008 420050102A2210 YAW DAMPER AIRBUS320 A320232 3930326EU NR 1 LEAKING A AWXAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 WP28661AW 1284 EN ROUTE FROM EWR TO PHX RECEIVED ECAM MESSAGE FOR GREEN HYD RESERVOIR LOW. DECLARED EMERGENCY & LANDED WITHOUT FURTHER DIFFICULTY. MAINTENANCE TROUBLESHOT & FOUND FLUID LEAKING FROM THE TOP OF NR 1 YAW DAMPER (3CC1), ISOLATED THE NR 1 YAW DAMPER AND ISSUED MEL 22-63-01, COND 1, YAW DAMPER NR 1 INOP. MX R & R NR 1 YAW DAMPER SERVO (3CC1) IAW T/C R6B27302, LEAK AND OPS CHECK WAS GOOD. VENDORS INCOMING TEST OF YAW DAMPER S/N 2636 CONFIRMED REASON FOR REMOVAL FOR FAILING INSULATION TEST. UNIT WAS DISASSEMBLED AND MODIFICATION KIT WAS INSTALLED, REPLACED BASE PLATE AND PACKINGS. REPAIR AND TEST ACCOMPLISHED IAW CMM 27-26-51, ISS 11. 2L72 4F RTA28NM 20050111000492005011100049NM 2005 1 11 CALA0500005 120050109A531565C33950 FLOORBEAM BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714613 27326 INSPECTION FOUND FLOORBEAM CORRODED AT SCREW HOLE ON FORWARD FLANGE AT STA 986.5, RBL 43 TO RBL 44. THE CORROSION WAS REMOVED AND A REPAIR STRAP WAS INSTALLED IAW SRM 53-00-51, FIGURE 203. 2L72 4F RTA16WE 20050111000522005011100052 2005 1 11 CALA0500002 420050102A2565 CABLE BFGOODRICH BOEING767 767224 1385170NM EVAC SLIDE DEFECTIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW276915413538 PG0304 30433 THE LT OVERWING SLIDE WAS PARTIALLY DEPLOYED WHILE PERFORMING MAINTENANCE. THE DOOR OPENED BUT, THE SLIDE DID NOT INFLATE. INVESTIGATION FOUND THAT THE LT INFLATION CABLE WAS NOT OPERATING PROPERLY AND IT WOULD NOT ACTIVATE THE INFLATION BOTTLE FOR SLIDE DEPLOYMENT. THE LT OVERWING SLIDE AND INFLATION CABLE WERE REMOVED AND REPLACED IAW MM 25-65-01 AND 25-65-04. 2L72 4F RTA1NM 20050111000532005011100053NM 2005 1 11 CALA0500003 120050108A52105079454 SKIN BOEING737 7373T0 1384582NM L1 DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714358 23943 INSPECTION FOUND A .75 INCH CRACK IN L-1 DOOR SKIN AT UPPER AFT INSPECTION HOLE. THE SKIN WAS REPAIRED IAW ECRA 5210-01812. 2L72 4F RTA16WE 20050111000542005011100054NM 2005 1 11 CALA0500004 120050109A531565C33950 FLOORBEAM BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714613 27326 INSPECTION FOUND FLOORBEAM CORRODED AT SCREW HOLE ON FORWARD FLANGE AT STA 986.5, RBL 29. THE CORROSION WAS REMOVED AND A STRAP REPAIR WAS INSTALLED IAW SRM 53-00-51, FIGURE 203. 2L72 4F RTA16WE 20050111000552005011100055EA 2005 1 11 COMA0560024 120050103A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA RIGHT MALFUNCTIONED A COMAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 SO01442CA10125 7483 FLIGHT 5690, FLAPS FAIL CAUTION. REPLACED THE RT BPSU. 2L72 4F RTA21EA 20050111000572005011100057EA 2005 1 11 COMA0560026 120050103A335059465 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA CABIN DEFECTIVE A COMAK NONE L NO TEST TXTAXI/GRND HDL 1 SO01949CA 7080 FLIGHT 5198, EMERGENCY FLOOR PATH LIGHTING INOP AT ROW 2 THRU 5. REPLACED WIRE CONNECTOR. 2L72 4F RTA21EA 20050111000622005011100062EA 2005 1 11 COMA0560023 120050102A3030 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A COMAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO01960CA 7117 FLIGHT 5164, LEFT AND RIGHT AOA HEAT CAUTION. RESET SYSTEM. COULD NOT DUPLICATE. 2L72 4F RTA21EA 20050111000632005011100063EA 2005 1 11 COMA0560025 120050103A3010 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA COCKPIT ACTIVATED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01977CA 7157 FLIGHT 5880, RT WING OVERHEAT CAUTION, DEFERRED MAINT PER MEL. 2L72 4F RTA21EA 20050111000642005011100064EA 2005 1 11 COMA0560022 120050102A329717300221 WIRE HARNESS CNDAIRCL600 CL6002B19 1900309EA NLG FAULTY A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01973CA 7146 FLIGHT 4990 NWS INOP MESSAGE. REPLACED THE NLG WOW HARNESS. 2L72 4F RTA21EA 20050111000662005011100066EA 2005 1 11 COMA0560017 120050102A5230 DOOR CNDAIRCL600 CL6002B19 1900309EA CARGO DOOR UNSECURE A COMAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 SO01924CA 7026 FLIGHT 5326 DISPLAY COOL MESSAGE. FOUND CARGO DOOR AJAR, CLOSED DOOR, OPERATIONAL CHECK SATISFACTORY. 2L72 4F RTA21EA 20050111000672005011100067EA 2005 1 11 COMA0560019 120050101A26136243843 OVERHEAT SENSOR CNDAIRCL600 CL6002B19 1900309EA LT WING FAULTY A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01981CA 7163 FLIGHT 5224 LEFT WING OVERHEAT MESSAGE WHEN DEICE SELECTED OFF. REPLACED THE OVERHEAT SENSOR. 2L72 4F RTA21EA 20050111000822005011100082EA 2005 1 11 COMA0570007 120050104A2760 WARNING SYSTEM CNDAIRCL600 CL6002C10 1390015EA COCKPIT MALFUNCTIONED A COMAO OTHER N FALSE WARNING CRCRUISE 1 SO01371CA 10082 FLIGHT 5283, INBOARD FLIGHT SPOILER AND SPOILERON CAUTION. RESET CONTROL UNIT, COULD NOT DUPLICATE. SYSTEM TEST SATISFACTORY. 2L72 4F RTA21EA 20050111000982005011100098 2005 1 11 DL76G050002 420050102A2397 WIRE BOEING767 767332 1382001NM CABIN DAMAGED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO271604R 30180 SEAT 4G HANDSET INOP. SPARKING AND SMOKE IN AREA. REPLACED UPCU. PN D250708651 SN 1299026427 2L72 4F RTA1NM 20050111001032005011100103NE 2005 1 11 DL738050006 220050104A7311795740000 HEAT EXCHANGER BOEING737 737832 13844CFNM CFMINTCFM567CFM567B2US 13802NE NR 2 ENGINE LEAKING A DALAA UNSCHED LANDING K FLUID LOSS CLCLIMB 1 SO27379DA 30349 874871 AFTER TAKEOFF RAMP REPORTED TO TMC THAT NR 2 ENG WAS LEAKING FUEL ON TAXI OUT OF SMF. AIRCRAFT DIVERTED INTO SFO FOR MTC. MTC IN PROGRESS. FOUND FUEL/OIL HEAT EXCHANGER LEAKING. REPLACED SAME. 2L72 4F4 FRTA16WE E2GL 20050111001052005011100105NM 2005 1 11 DL738050012 120050109A2750113A39103 BELLCRANK BOEING737 737832 13844CFNM T/E FLAP BROKEN A DALAO OTHER F FLT CONT AFFECTED LDLANDING 1 SO27386DA 30373 WHEN FLAPS EXTENDED TO 1 AT 210 KTS AIRCRAFT ROLLED LEFT, BEYOND 1, ROLL MOMENT REMAINED. FOUND LT OUTBOARD AFT FLAP CONTROL BELLCRANK BROKEN. REPLACED SAME. 2L72 4F RTA16WE 20050111001102005011100110 2005 1 11 SWIA200514338 420050102A3418501125904 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA STALL WARNING MALFUNCTIONED A SWIAO OTHER N FALSE WARNING CLCLIMB 1 NM07453SW 7743 ON TAKEOFF, AT GEAR UP, STALL FAIL CAUTION MESSAGE ILLUMINATED. REPLACED STICK PUSHER ACTUATOR IAW MM 27-35-15. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050111001112005011100111SO 2005 1 11 SWIA200514339 120050106A27223081401003 ACTUATOR EMB 120 EMB120ER 3260203SO RUDDER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TOTAKEOFF 1 NM07187SW9702 5267 120037 ON TAKEOFF, THE RIGHT RUDDER HAD VERY LIMITED TRAVEL. REPLACED GREEN HYDRAULIC RUDDER ACTUATOR IAW 27-22-02. OPS AND LEAK CHECK GOOD. 2L72 4T RTA31SO 20050111001142005011100114EA 2005 1 11 SWIA200514325 120050101A2740 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB MALFUNCTIONED A SWIAC ABORTED TAKEOFF FJ FLT CONT AFFECTED WARNING INDICATION TOTAKEOFF 1 NM07932SW 7714 WHEN CLEARED FOR T/O PRIOR TO THRUST APPLICATION, RECEIVED THE MACH TRIM CAUTION MESSAGE AND STAB CHANNEL 2 INOP STATUS MESSAGE. REPLACED HORIZONTAL STAB ACTUATOR MOTOR CONTROL UNIT, HST ACTUATOR AND HSTCU IAW CRJ MM 27-42-01 AND 27-42-05, OPERATIONAL CHECK GOOD. P/N (HSTA) 8396-3, S/N OFF 749, P/N (MCU) 7062-3, S/N OFF 804, P/N (HSTCU) 7060-9, S/N OFF 175. 2L72 4F RTA21EA 20050111001162005011100116EA 2005 1 11 SWIA200514327 120050101A274070608 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TOTAKEOFF 1 NM07918SW6543 6543 7645 STAB TRIM AND MACH TRIM CAUTION ILLUMINATED AFTER TAKEOFF. REMOVED AND REPLACED HSTCU IAW CRJ 200 MM 27-41-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050111001202005011100120 2005 1 11 SWIA200514331 420050102A22166225734002 SERVO EMB 120 EMB120ER 3260203SO RUDDER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07212SW9946 9946 120276 RUDDER PEDAL BINDING TO THE LEFT. REMOVED AND REPLACED RUDDER SERVO IAW EMB MM 22-10-05. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050107001772005010700177NM 2005 1 7 SWAA050014 120050102A53306545772 SKIN BOEING737 7373H4 1384600NM FUSELAGE WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29341SW 24091 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN UNDER DORSAL FIN FROM BS 867 TO BS 973, WORN. REPAIRED FUSELAGE SKIN PER EA. 2L72 4F RTA16WE 20050107001782005010700178NM 2005 1 7 SWAA050015 120050103A335007912 COVER BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29332SW 23696 EEPLS FLOOR TRACK COVER, LOOSE. REMOVED AND REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20050112000252005011200025EU 2005 1 12 05FDEA00037 120050106A5730 SKIN AIRBUS310 A310222 3930315EU LT WING CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25454FE 278 ACCOMPLISH MAINTENANCE C-CHECK, ORIGINAL PLAN DATE WAS ENTERED ON: 23JUL04. NON-ROUTINE LT WING - CORROSION FOUND ON UPPER SURFACE STA 813 RIB 13 TO STA 874 RIB 14 INTERSECTION WITH STRINGER 7. REPAIRED IAW FAX REF 942-034715/005/2004 DATED 12/27/2004 AND FEDEX EA 6-5710-81827. NDT INSP IAW 51-10-08 PT6. PAINTED IAW SRM 51-75-10-8. 2L72 4F RTA35EU 20050112000272005011200027NM 2005 1 12 SWAA050044 120050107A3260189921 SENSOR BOEING737 737301 1384611NM LT MLG FAULTY A SWAAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW29659SW 23229 LT MLG UNSAFE LIGHT ILLUMINATED IN FLIGHT. CYCLED GEAR HANDLE, NO HELP. REMOVED AND REPLACED LT MLG UPLOCK SENSOR PER MM. 2L72 4F RTA16WE 20050112000402005011200040SO 2005 1 12 C2XA04SD014 120050103A3397 WIRE EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCONNECTED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716987 145261 SDF - EMERGENCY LIGHT ON GALLEY BULKHEAD INOP. WIRE DISCONNECTED. RECONNECTED EMERGENCY LIGHT WIRE. OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE. 2L72 4T RTT00011AT 20050112000412005011200041NM 2005 1 12 UPS05443630 120050104A5410 STRINGER BOEING747 747121 1384871NM NR 3 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE:N/A FOUND CRACK ON NR 3 PYLON STRINGER, LT JUST FWD OF NAC STA 221, AREA MARKED IN RED. STRINGER IS CRACKED FROM TOP TO BOTTOM. STARTED DRILLING OUT FASTENERS IN STIFFENER & STRINGER REMOVED STIFFENER AND RIB FABRICATED REPAIR PARTS. ALODINED, PRIMED, INSTALLED AND PAINTED REPAIR PARTS AND REPAIR PER SRM 54-10-03. 2L74 4F A20WE 20050112000422005011200042NM 2005 1 12 05FDEA00009 120050103A5754 SLAT TRACK DOUG MD11 MD11 3023602NM LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 LEFT HAND WING, SLAT TRACK NR 16 INBOARD RIB FOUND CRACKED. REMOVED AND REPLACED PER SRM 51-33-01 AND SRM 51-35-01. NR 16 SLAT TRACK ADJUSTMENT AND TEST CARRIED OUT PER AMM 27-80-00-2. OUTBOARD SLAT OPERATIONAL TEST CARRIED OUT PER AMM 27-80-00-5. 2L73 4F RTA22WE 20050112000492005011200049SO 2005 1 12 C2XA05CL001 120050105A33501317 BULB EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2717169 14500844 DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHT IN THE CEILING OUTSIDE THE COCKPIT DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT BULB IN THE CEILING OUTSIDE COCKPIT DOOR. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RT 20050112000502005011200050NM 2005 1 12 UPS05243629 120050106A3350 LIGHT BOEING727 72730C 1384009NM L1 DOOR INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919UP 19012 L1 DOOR EMERGENCY LIGHT INOP. RESEATED BULB, OPS CHECK GOOD. 2L73 4F A3WE 20050112000512005011200051NM 2005 1 12 SWAA050039 120050106A53306545776 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29667SW 23063 DURING SCHEDULED SERVICE CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 752 AND BS 769, BETWEEN STRINGERS 23L AND 24L. REPAIRED SKIN SECTIONS PER EA. 2L72 4F RTA16WE 20050112000532005011200053NM 2005 1 12 SWAA050040 120050106A5312BAC1517 STIFFENER BOEING737 7373K2 13844BANM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29345SA 23786 DURING SCHEDULED 1/2D CHECK, FOUND VERTICAL STIFFENER AT BS 663, RBL 5, CRACKED. REMOVED AND REPLACED STIFFENER PER SRM. 2L72 4F RTA16WE 20050112000542005011200054SO 2005 1 12 C2XA05IA005 120050106A33501317 LAMP EMB 145 EMB145ER 3260211SO GALLEY BURNED OUT A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714939 145030 IAH - CREW REPORTED THAT THE BACKLIGHTING IN THE EMERGENCY EXIT LIGHT OVER THE GALLEY DOOR WAS INOP. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (THIS PART IS NOT SERIALIZED & HAS NO S/N). 2L72 4F RTT00011AT 20050112000562005011200056SO 2005 1 12 C2XA05IA006 120050106A335074441 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714959 145091 IAH - CREW REPORTED THAT THE EMERGENCY EXIT LIGHT ABOVE THE F/A JUMPSEAT WAS INOP. MAINTENANCE RESECURED THE LIGHT ASSY, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (THIS PART HAS NO S/N AND TIMES ARE NOT TRACKED). 2L72 4T RTT00011AT 20050112000612005011200061CE 2005 1 12 DXTA200500513 120050104A3260 LIMIT SWITCH CESSNA750 750 2076810CE MLG OUT OF RIG E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07936QS 7500036 GEAR HANDLE WOULD NOT COME UP ON DEPARTURE. GEAR SIGNED DOWN AND LOCKED (THREE GREEN). PERFORMED RIG PROCEDURE ON ALL 3 SQUAT SWITCHES. PERFORMED FUNCTIONAL CHECK ALL OK. OPS CHECKED GOOD IAW CITATION 750 MM 32-30-01. 2L72 4J RTT00007WI 20050112000662005011200066NM 2005 1 12 UPS05543628 120050105A2752 ACTUATOR BOEING757 75724APF 1384969NM LE SLATS MALFUNCTIONED A IPXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01442UP 27387 L/E SLAT DISAGREE EICAS MSG DISPLAYED. RAN CHECKLIST, CONDITION REMAINED UNCHANGED. RAN L/E SLAT ASSYMETRY CHECKLIST, PROCEEDED TO SAT AT FL 180 AND 230 KTS. LANDED WITHOUT INCIDENT. INSPECTED AND LUBED LEFT WING L/E PER MM 12-21-08-3. REMOVED AND REPLACED NR 3 O/B T ROTARY ACTUATOR PER MM 27-81-18-4 DUE TO OVERLOAD IND POPPED. PERFORMED ADJ/TEST REQUIRED PER MM 27-81-00-5. NO DEFECTS NOTED AT THIS TIME. 2L72 4F RTA2NM 20050112000682005011200068NM 2005 1 12 05FDEA00005 120050103A5330 SKIN DOUG MD11 MD11 3023602NM ZONE 100 MISREPAIRED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25577FE 48469 FORWARD CARGO STA 602 TO STA 615 BETWEEN LONGERON LT 44 AND LT46 IS A REPAIR THAT DOES NOT LOOK TO BE FROM THE SRM. REPAIR EVALUATED AND FOUND NOT CONFORMING TO SRM CHAPTER 53. REPAIR CARRIED OUT AS PER FEDEX EA 1-5330-77979. 2L73 4F RTA22WE 20050114000032005011400003EU 2005 1 14 05FDEA00034 120050106A5410 FAIRING AIRBUS310 A310 EU NR 2 PYLON CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25454FE 278 NR 2 PYLON, AFTER FIXED FAIRING WITH CRACK AT LT. REMOVED IAW AMM 54-55-00. REPAIRED IAW FEDEX EA 6-5480-81822. INSTALED IAW AMM 54-55-00. 2L72 4F RTA35EU 20050114000042005011400004EU 2005 1 14 05FDEA00038 120050106A5330 SKIN AIRBUS310 A310 EU RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25454FE 278 RT WING CORROSION FOUND ON UPPER SURFACE STA 813 RIB 13 TO STA 874 RIB 14 INTERSECTION WITH STRINGER 7. CORROSION REMOVED AND REPAIRED IAW EA 6-5710-81827. 2L72 4F RTA35EU 20050114000102005011400010EU 2005 1 14 05FDEA00026 120050106A5330 SKIN AIRBUS310 A310 EU FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25454FE 278 FUSELAGE - REPAIR AT APROX. FS 63 STR 42 RT. REPAIRED IAW SRM 53-17-12, FIG 203. 2L72 4F RTA35EU 20050114000192005011400019CE 2005 1 14 DXTA200500526 120050110A2612 FIRE LOOP CESSNA500 560CESSNA 2076750CE LT ENGINE CHAFED E DXTAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 GL07372QS 5600372 LEFT FIRE WARNING LIGHT ILLUMINATED ON TAXI IN. INSPECTED COCKPIT INDICATION LIGHTS AND COULD NOT FIND ANY FAULTS. INSPECTED L/H ENGINE FIRE LOOP & FOUND 2 CLAMPS PINCHING INSULATORS & MAKING CONTACT WITH FIRE LOOP. REMOVED CLAMPS & INSULATORS. REINSTALLED ISOLATORS & CLAMPS AND REPOSITIONED FIRE LOOP SO NO CONTACT WAS MADE WITH CLAMPS. ALL WORK PERFORMED I/A/W CESSNA 560 M/M CHAPTER 26-11-01. FUNCTIONALLY TEST GOOD. NO DEFECTS NOTED 2L72 4F RTA22CE 20050118000052005011800005NE 2005 1 18 05FDEA00062 220050110A7532 BLEED VALVE AIRBUS300 A300F4605R 3930327EU GE CF6 CF680C2A5 NE NR 2 MALFUNCTIONED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25654FE 738 ON CLIMBOUT NR 2 HP BLEED VALVE FAULTED, APP FL 280 LOSS BOTH PACKS. RESET OF PACKS AT 10,000 RESULTED IN NORMAL OPS. DID BITE CHECK OF PNEUMATIC CONTROLLERS, PER TSM 26-00-00, FAULTED NR 2 HP VALVE, DID BITE CHECK OF PACK CONTROLLER PER 21-60-00, NO FAULTS FOUND. CREW RAN ENGS AND PACKS ON GROUND. RELEASED FOR SERVICE PER MEL/CDL: 36-11-03. REPLACED BROKEN SENSE LINE ON HP VALVE PER A300-600 MM 36-00-00 SMP. REACTIVATED NR 2 HP VALVE PER A300-60 MM 36-11-12-9-02. RAN NR 2 ENGINE PER A300-600 JRH AND PERFORMED OPS CHECK OF HP VALVE. 2L72 4F4 FRTA35EU E13NE 20050118000072005011800007EU 2005 1 18 05FDEA00057 120050108A5330 DOUBLER AIRBUS310 A310222 3930315EU FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25422FE 346 FUSELAGE SKIN DOUBLER AT LT STA 926 AT APPROX 6:30 POS. REQUIRES FURTHER EVALUATION PER FAR 121.368. AFTER EVALUATION OF REPAIR, REPLACEMENT REQUIRED, REWORKED REPAIR IAW EA 6-5330-85452 REF N00855. 2L72 4F RTA35EU 20050118000092005011800009WP 2005 1 18 05FDEA00059 120050108A3020 VALVE DOUG DC10 DC1030 3023501WP NR 1 ENG ANTIICEMALFUNCTIONED A FDEAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SO25307FE 48291 ON CLIMBOUT, TURNED ON ANTI-ICE, NR 1 ENG ANTI-ICE DISAGREE LIGHT CAME ON. RAN RED TABS & NO HELP. DISAGREE LIGHT STAYED ON FOR ENTIRE FLT. FOUND SUPPLE DUCT TO ANTI-ICE VALVE BROKEN. REMOVED AND REPLACED NR 1 ENG ANTI-ICE VALVE AND DUCT ASSY REF-30-22-02-2, RAN NR 1 ENG REF-JRH AND ANTI-ICE VALVE CYCLES NORMAL. 2L73 4F A22WE 20050118000102005011800010NM 2005 1 18 05FDEA00060 120050109A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 MAIN DECK CARGO, SEAT TRACK BETWEEN STA Y= 1099 TO Y= 1129, X= 27.50V FOUND WORN. REPAIRED PER SRM 53-70-00 VOLUME I, FIGURE 1 2L73 4F RTA22WE 20050118000122005011800012NE 2005 1 18 0500036624 220050112A7230 ENGINE BOEING747 747251B 1384892NM PWA JT9 JT9D7Q 52054NE NR 1 BIRD INGESTION A NWAAC ABORTED TAKEOFF CT F.O.D. ENGINE CASE PENETRATION TOTAKEOFF 1 GL01624US 21706 702177 THE CREW ABORTED TAKEOFF AT APPROXIMATELY 100 KTS AFTER SUFFERING A BIRD STRIKE ON THE NR 1 ENGINE. MAINTENANCE INSPECTED THE ENGINE AND FOUND AN UNCONTAINED FAILURE OF A FAN BLADE HAD OCCURRED. THE ENGINE WAS REPLACED. OPERATIONAL CHECK GOOD. 2L74 4F4 F A20WE E3NE 20050118000132005011800013NM 2005 1 18 UPS05443640 120050106A3350S1356B37 LIGHT BOEING747 747SR46 1384816NM CABIN INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01680UP 20923 CREW STAIRS EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTS PER MM 33-51-07. 2L74 4F RTA20WE 20050118000142005011800014 2005 1 18 UPS05643639 420050108A2565600307FRB LIFE RAFT BOEING767 76734AF 1385212NM CONTAINER ACTIVATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01326UP 27752 FOUND LIFE RAFT S/N Q47, SELF INFLATED IN STOWAGE CONTAINER. DEFERRED D25-62-1-2 WAITING FOR CLOSING LOG PAGE. LIFE RAFT REMOVED FROM A/C. REPLACED LIFE RAFT, ETOIS SIGN OFF REQUIRED THIS CLEARS DFRL M294789. 2L72 4F RTA1NM 20050118000152005011800015NM 2005 1 18 0500035807 120050110A5210 BOLT BOEING757 757351 1384991NM PAX DOOR BACKED OUT A NWAAK NONE O OTHER ININSP/MAINT 1 GL01587NW 32986 DOOR 2L ARMING FLAP DOES NOT EXTEND WHEN DOOR IS ARMED. FOUND BOLT TO RETRACTABLE DOOR LINKAGE LEVERS BACKED OUT. REINSTALLED BOLT WITH LOCTITE PER EA 58-195881, SEC III AND PLACED ON MONITOR. 2L72 4F RTA2NM 20050118000162005011800016NM 2005 1 18 0500045648 120050109A21216067723 FAN BOEING757 757251 1384970NM CABIN FAILED A NWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL01548US443292380 26495 LEVELING OFF AT 33,000 FT, NOTICED INTERMITTENT AIR CONDITIONING RELATED SMOKE IN COCKPIT AND CABIN. DECLARED AN EMERGENCY AND DIVERTED TO PHX AND LANDED UNEVENTFULLY. REPLACED RECIRCULATION FAN. OPERATIONAL CHECK GOOD. 2L72 4F RTA2NM 20050118000192005011800019NM 2005 1 18 AWXA200500023 120050102A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 DURING C-17 CHECK A 3 INCH CRACK WAS FOUND IN FUSELAGE SKIN EXTENDING FROM RIVET HOLE AT BS 727C, STR 15 LT. MAINTENANCE CUT OUT DAMAGE IN FUSELAGE AT BS 727C, STR 15 LT, PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A FILLER, DOUBLER, AND TRIPLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-01 FIG 229 PG 334-335. 2L72 4F RTA16WE 20050325000342005032500034EA 2005 3 25 SWIA200514750 120050307A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07442SW 7609 FS 621 FLOORBEAM ANGLE RBL 42 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-61-117 REV B. 2L72 4F RTA21EA 20050325000472005032500047NM 2005 3 25 05FDEA00615 120050321A5710 STIFFENER BOEING727 727200 138407ENM FUEL CELL CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 RIGHT WING INTERIOR FUEL CELL UPPER STIFFENER NR 10 IS CRACKED AT WS 686.5. REPAIRED FUEL CELL UPPER STIFFNER NR 10 AT WS 686.5 PER EA 7-5710-86251. 2L73 4F RTA3WE 20050325000492005032500049NM 2005 3 25 QXEA200500418 120050207A5730 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - LEFT WING, FUEL PANEL 522CT BOTTOM SURFACE OF PANEL PITTING AND FRETTING CORROSION AROUND PANEL ATTACH HOLES. REPAIRED IAW RD 8/4-57-428. 2H72 4T RTA13NM 20050325000512005032500051NM 2005 3 25 QXEA200500423 120050201A5730 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 600 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - RT WING ANCHOR NUTS AROUND PANEL 622AT ARE CORRODED AND BROKEN AT ALL LOCATIONS. REPAIRED IAW Q400 SRM 51-42-05-330-001. 2H72 4T RTA13NM 20050325000572005032500057WP 2005 3 25 DHL2005805507 120050220A5531 FRAME DOUG DC8 DC873F 302199FWP VERTICAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 VERTICAL STABILIZER L/E FORMER CRACKED 1.000 AT STA ZFS 198.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE AND FABRICATED ANGLE DOUBLER (2EA) (AL7075-T6 0.032) IAW SRM 55-2-0 PG 7-8 FIG 2. CLEANED, TREATED AND PRIMED AREA, ANGLE DOUBLERS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED ANGLE DOUBLERS IAW SRM 51-1-21 PG 2, SRM 51-1-20D PG 9. TORQUED IAW SRM 51-3-1 PG 2A TABLE II. 2L74 4F RT4A25 20050325000582005032500058WP 2005 3 25 DHL2005805509 120050220A5531 FRAME DOUG DC8 DC873F 302199FWP VERTICAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 VERTICAL STABILIZER L/E FORMER CRACKED 1.000, STA ZFS 96.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE AND FABRICATED (2EA) ANGLE DOUBLERS (AL7075-T6 0.032) IAW SRM 55-2-0 PG 7-8 FIG 2. CLEANED, TREATED AND PRIMED AREA, ANGLE DOUBLERS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED ANGLE DOUBLERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. TORQUED IAW SRM 51-3-1 PG 2A TABLE II. 2L74 4F RT4A25 20050325000652005032500065EA 2005 3 25 COMA0560197 120050321A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01494CA 7765 FLIGHT 5527 LEFT T/R UNLOCKED CAUTION. SECURED T/R AND DEFERRED MAINT PER MEL. 2L72 4F RTA21EA 20050325000722005032500072WP 2005 3 25 DHL2005805518 120050308A534774529523 CARGO TRACK DOUG DC8 DC873F 302199FWP CARGO BAY WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT NR 7 TRACK PLUG LUGS WORN AT STA 228.000. REMOVED DETERIORATED TRACK PLUG IAW SRM 51-3-0 PG 1-2. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW TRACK PLUG IAW SRM 51-3-0 PG 1-2. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050325000812005032500081NM 2005 3 25 QXEA200500428 120050128A5730 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - LEFT WING FUEL PANEL AT 522AT, BOTTOM SURFACE HAS AREAS OF CORROSION AROUND SCREW HOLES. REPAIRED IAW Q400 SRM SUB TASK 57-10-35-910-001. 2H72 4T RTA13NM 20050325000862005032500086NM 2005 3 25 QXEA200500430 120050201A2810 LINE BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - TWO FUEL LINES IN THE LEFT FUEL TANK HAVE BEEN CHAFING, LINES ARE LOCATED IN THE FORWARD TANK SECTION UNDER PANEL 523AT. REPAIRED IAW DHC-8 400 SRM SUB TASK 28-11-06-400-801 AND 28-11-06-420-001. 2H72 4T RTA13NM 20050325000902005032500090NM 2005 3 25 SWAA050868 120050321A3350101073 LENS BOEING737 7377H4 1384404NM EMERGENCY EXIT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29483WN 32472 R2 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM. 2L72 4F RTA16WE 20050325000942005032500094 2005 3 25 SWAA050872 420050321A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29724SW 27856 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050325001172005032500117NM 2005 3 25 05FDEA00512 120050315A3230A42006028305 SOLENOID BOEING727 727200 138407ENM MLG MALFUNCTIONED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25496FE 21670 DURING FLIGHT TEST LANDING GEAR HANDLE WOULD NOT GO PAST OFF POSITION, THEN AFTER WAITING FOR 3 TO 4 SECONDS THE LANDING GEAR HANDLE WOULD BE ALLOWED TO MOVE TO RETRACT POSITION. PROBLEM WOULD BE INTERMITTENT. *S/D* REMOVED AND REPLACED LANDING GEAR CONTROL LEVER LOCK SOLENOID PER FED EX M/M 32-31-016-4. 2L73 4F RTA3WE 20050325001332005032500133 2005 3 25 SWAA050788 420050314A256565659723 BRACKET BOEING737 7373H4 1384600NM R2 DOOR SLIDE LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29655WN 28400 DURING SCHEDULED 1/4D CHECK, FOUND R2 DOOR EVAC SLIDE GIRT BAR FLOOR AFT BRACKET LOOSE. 2L72 4F RTA16WE 20050325001362005032500136NM 2005 3 25 QXEA200500387 120050124A5340 STOP FITTING BOMBDRDHC8 DHC8401 1390041NM ZONE 200 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - AFT FUSELAGE - AFT ENTRY DOOR SURROUND STRUCTURE AFT STOP FITTING GOUGED AT STATION 698.00 AND STRINGER 19P. 2H72 4T RTA13NM 20050328000012005032800001SO 2005 3 28 SWIA200514781 120050207A5315 BUTTSTRAP EMB 120 EMB120ER 3260203SO FLOORBEAM CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0758733 120197 PILOT SIDE OUTBOARD BUTTSTRAP IS CORRODED IN SEVERAL AREAS. ITEM FOUND AT C-CHECK INSPECTION. REPLACED BUTTSTRAP IAW EMB 120 SRM 51-40-02. 2L72 4T RTA31SO 20050328000032005032800003SO 2005 3 28 SWIA200514783 120050207A5523 ROD END EMB 120 EMB120 3260201SO ELEVATOR TRIM CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0758733 120197 RIGHT ELEVATOR TRIM TAB ROD END CORRODED. ITEM FOUND AT C-CHECK INSPECTION. FWD OUTBOARD ROD END AT HORIZONTAL STAB T/E REPLACED IAW AMM 27-32-00. 2L72 4T RTA31SO 20050328000042005032800004SO 2005 3 28 SWIA200514784 120050207A2720 ROD END EMB 120 EMB120ER 3260203SO RUDDER CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0758733 120197 RUDDER CONTROL RODS, AFT ROD ENDS CORRODED AT TRAILING RUDDER CONNECTION. ITEM FOUND AT C-CHECK INSPECTION. AFT ENDS OF RUDDER CONTROL RODS AT TRAILING RUDDER CONNECTION REPLACED IAW AMM 27-21-02. 2L72 4T RTA31SO 20050328000082005032800008SO 2005 3 28 SWIA200514765 120050207A5315 FLOORBEAM EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0758733 120197 RIGHT FLOORBEAM ANGLE AT FRAME 38 TO 44 IS CORRODED. ITEM FOUND AT C-CHECK INSPECTION. CORROSION BLENDED AND ASSESSED IAW EMB 120 SRM 53-00-01, FIG 101. FOUND TO BE WITHIN LIMITS. DEPTH .002, REPROTECTED AREA IAW EMB 120 SRM 51-21-02 & AMM 20-30-05. 2L72 4T RTA31SO 20050328000172005032800017SO 2005 3 28 SWIA200514774 120050207A5347 SEAT TRACK EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0758733 120197 RT AFT SEAT TRACK AT YR 479.00 IS BADLY CORRODED. (ITEM FOUND AT C-CHECK INSPECTION.) RT AFT SEAT TRACK AT YR479.00 REPLACED IAW EMB 120 SRM 51-25-00, 51-22-00 AND 51-40-02. 2L72 4T4 TRTA31SO E20NE 20050328000232005032800023NM 2005 3 28 BB05022 120050323A2710285T0015116 LOCKOUT BOEING757 7572B7 1384964NM GE CF6 CF680 30025NE STAB TRIM FAULTY A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19653US4556845568 24894 PHL FL 1237, CREW RECEIVED THE EICAS MESSAGES (AIL LOCKOUT) AND (RUDDER RATIO), AND THE ASSOCIATED LIGHTS. CREW WAS ALSO HAVING PROBLEMS WITH THE AUTO THROTTLES DISENGAGING REPEATEDLY. FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RT STAB TRIM AND AILERON LOCKOUT MODULE (SAM), AND REPAIRED THE RT ENGINE MEC TO EEC CABLE. 2L72 4F4 FRTA2NM E13NE 20050328000312005032800031SO 2005 3 28 SWIA200514780 120050207A5320 BUTTSTRAP EMB 120 EMB120ER 3260203SO FUSLEAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0758733 120197 CO-PILOTS SIDE OB BUTTSTRAP IS CORRODED IN SEVERAL SPOTS. (ITEM FOUND AT C-CHECK INSPECTION.) REPLACED BUTT STRAP IAW EMB 120 SRM 51-40-02. 2L72 4T RTA31SO 20050328000392005032800039EU 2005 3 28 05FDEA00623 120050321A5347 SEAT TRACK AIRBUS310 A310 EU FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 MDCC SONE 241, RT NR 2 SEATRACK, FR54.2 HAS 1-EA GOUGES AREA ON SCALOPE HOLE. REMOVED DAMAGED SEAT TRACK FITTING AT MDCC ZONE 241 RT NR 2 FR54.2 AND REPLACED WITH NEW SEAT TRACK FITTING P/N A5381114620000 IAW A310 SRM 51-40-21. 2L72 4F RTA35EU 20050328001262005032800126NM 2005 3 28 UPS05244172 120050310A5753 FITTING BOEING727 72722C 138400FNM NR 5 FLAP TRACK CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 INSPECTION TYPE:C NR 5 FLAP TRACK FWD SUPPORT FITTING P/N 65-21651 HAS PITTING CORROSION ON HOLE FOR SPECIAL STUD. REPAIR CARRIED OUT IAW AAAE EO 2005-021-003. 2L73 4F A3WE 20050328001302005032800130NM 2005 3 28 UPS05444176 120050314A5347BAC15201566 SEAT TRACK BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE:C M/D- BS 1780 RBL 95 SEAT TRACK CROWN FOUND CORRODED. CORROSION BLEND OUT 0.045 X 1 X 2 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. SEAT TRACK REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050328001462005032800146NM 2005 3 28 UPS05444186 120050312A5320AND101341406 FLOOR SUPPORT BOEING747 747121 1384871NM FUSELAGE4 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE:C M/D- BS 2350 - 2360 RBL 55 FLOOR SUPPORT FOUND CORRODED. CORROSION BLEND OUT 0.030 X 1 X 2 INCH, EXCEED SRM 53-10-01 FIG 1 LIMIT. FLOOR SUPPORT REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050328001642005032800164CE 2005 3 28 DXTA200500639 120050321A3230049801001 CONTROL BOX CESSNA560 560XL 2076702CE MLG MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07631QS 5605131 AFTER TAKEOFF GEAR WOULD NOT RETRACT. TROUBLESHOT SYSTEM AND FOUND LANDING GEAR CONTROL UNIT NOT FUNCTIONING PROPERLY. REMOVED CONTROL UNIT S/N - 0110 AND INSTALLED CONTROL UNIT S/N - 0088. PERFORMED OPERATIONAL CHECK, NO DEFECTS NOTED AT THIS TIME IAW CE560XL AMM 32-30-01, 32-01-00. 2L72 4F RTA22CE 20050328001702005032800170SO 2005 3 28 153303202005 120050320A32501159SCH4033 SOLENOID GULSTMG1159 GIV 3980115SO NLG STEERING FAILED E N93AC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO13467QS 1533 STEER BY WIRE FAIL MESSAGE ON ROLLOUT. 2L72 4F RTA12EA 20050328001822005032800182NM 2005 3 28 AALA20050218 120050228A5315 FLOORBEAM BOEING767 767323 1385205NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21357AA 24038 AFW - FLOORBEAM AT STATION 325 (GENERAL LOCATION SECTION 41) HAS CORROSION REMOVAL ON UPPER SURFACE. MATERIAL REMAINING IS BEYOND SRM LIMITS. AREA IS 1.0 INCH BY 1.0 INCH WITH A DEPTH OF .026 INCHES. COMPLETELY REMOVED CORROSION AND ENSURED BLEND AREA WAS CRACK FREE. REFINISHED BLEND AREA WITH ALODINE AND TWO COATS BMS1011 PRIMER. FILLED BLEND WITH BMS595. AIRCRAFT RETURNED TO SERVICE WITH NOTED CONDITION. 2L72 4F RTA1NM 20050328001832005032800183WP 2005 3 28 0500379954 120050308A5313 LONGERON DOUG DC9 DC931 3022065WP FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01921RW 47164 DURING M-CHECK FOUND CORROSION FROM BS 737-756 ON LONGERON 29L. REPAIRED PER EA 99-203145. 2L72 4F A6WE 20050328001932005032800193 2005 3 28 SWIA200514757 420050322A3418 COMPUTER EMB 120 EMB120ER 3260203SO STALL WARNING INTERMITTENT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07569SW 120344 STALL WARNING SYSTEM 2 FAILS INTERMITTENTLY ON GROUND AND IN FLIGHT. REPLACED NR 2 STALL COMPUTER. OPERATIONAL CHECK GOOD. P/N: C-81806-1, S/N OFF: 342. 2L72 4T RTA31SO 20050328001952005032800195EA 2005 3 28 SWIA200514759 120050320A2711 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA AILERON TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07955SW 7817 AILERON TRIM WILL NOT GO LEFT; TRIM ONLY GOES RIGHT. REPLACED AILERON/RUDDER TRIM PANEL. OPERATIONAL CHECK GOOD IAW 27-12-10 CRJ AMM. 2L72 4F RTA21EA 20050328002012005032800201 2005 3 28 SWAA050882 420050322A256565C19901 CABLE BOEING737 7373H4 1384600NM L2 DOOR SLIDE MISROUTED A SWAAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW29339SW 24090 DURING SCHEDULED RON CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE LATCH CABLE MISROUTED. REROUTED CABLE PER MM. 2L72 4F RTA16WE 20050328002042005032800204NM 2005 3 28 SWAA050885 120050322A53306545765 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 529, STR 28L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050328002062005032800206NM 2005 3 28 SWAA050887 120050322A53116558280 FRAME BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 360, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050328002082005032800208NM 2005 3 28 SWAA050889 120050322A53116520722 FRAME BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 24R. REPAIRED FRAME PER PAE ER. 2L72 4F RTA16WE 20050328002112005032800211NM 2005 3 28 SWAA050892 120050322A3350612825 BATTERY PACK BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29738CB 27870 DURING SCHEDULED MV2 CHECK, FOUND SEVERAL EMERGENCY EXIT BULLNOSE LIGHTS INOP AT ROW 7 ABC TO ROW 18 ABC. REMOVED AND REPLACED BATTERY PACKS PER MM. 2L72 4F RTA16WE 20050329000052005032900005WP 2005 3 29 ASAA0580129 120050227A532199365471 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 OKC- HV-CHECK, FOUND CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050329000382005032900038EA 2005 3 29 SIMA200506801 120050308A335020131A BATTERY PACK CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT DISCHARGED A SIMAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SW21501BG 10017 OMA - FLT 4079 - FLIGHT ATTENDANT REPORTED THE EMERGENCY LIGHT SWITCH WAS IN THE ON POSITION AND EMERGENCY LIGHTS WERE DEAD. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT BATTERY PACKS IAW CRJ MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTA21EA 20050329000592005032900059NM 2005 3 29 USAA050325 120050225A5330 SKIN BOEING737 7374B7 1384702NM FUSELAGE PUNCTURED A USAAK NONE O OTHER ININSP/MAINT 1 EA19438US40959 24560 PIT - FOUND SKIN PUNCTURED .5 INCH BY .5 INCH, BS 727A PLUS 10 AT BL 0. REMOVED DAMAGE AND INSTALLED DOUBLER PER EA 79988. (M) 2L72 4F RTA16WE 20050329000612005032900061NM 2005 3 29 USAA050321 120050211A554265C2584151 SKIN BOEING737 7373B7 1384580NM RUDDER DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU50570 23706 PIT - FOUND EXIT COMPOSITE SURF, 2 INCHES LONG BY .125 INCH WIDE SINGLE LAYER DAMAGE, RUDDER RT SIDE 57 INCH FROM BOTTOM, 10 INCH FROM T/E. INSTALLED REPAIR PLYS, SEALED, REFINISHED PER SRM 51-70-17, EA 79999. (M) 2L72 4F RTA16WE 20050329000722005032900072NM 2005 3 29 S2YA05017 120050219A21601762D000001 CONTROL UNIT DORNERDO32 DO328300 NM ENVIRONMENTAL SMOKE A S2YAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL13355SK 3124 FLT 2273 - EWR-MKE - DURING FLIGHT, THE CREW GOT A LAVATORY SMOKE DETECTOR INDICATION AND NOTICED SMOKE IN THE COCKPIT. THE CREW DONNED THEIR 02 MASKS AND DIVERTED TO BUFFALO, NY. MAINTENANCE INSPECTED THE A/C AND FOUND THE RT ECS UNIT, COLD AIR UNIT, VIBRATING AND MAKING A LOUD GRINDING NOISE. MAINTENANCE REPLACED THE ECS AND WITH OPERATIONAL CHECKS GOOD THE A/C WAS RETURNED TO SERVICE. (M) 2H72 4T RTA55NM 20050329000802005032900080EA 2005 3 29 SIMA200506601 120050303A335020131A BATTERY PACK CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT INOPERATIVE A SIMAK NONE O OTHER ININSP/MAINT 1 SW21509AE6256 10078 XNA - DURING SCHEDULED MAINTENANCE CHECK, EMERGENCY LIGHT AT FS 416 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AN EMERGENCY POWER SUPPLY UNIT IAW CRJ MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTA21EA 20050329000882005032900088NM 2005 3 29 USAA050326 120050220A5311 FRAME BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19428US40959 24560 PIT - FOUND FRAME CRACKED .25 INCH, JUST BELOW FLOOR ON FRAME 616L. INSTALLED DOUBLER PER TYPICAL REPAIR 53-62-01. (M) 2L72 4F RTA16WE 20050329000912005032900091NM 2005 3 29 UIEA200500019 120050314A575365B151611 LINK BOEING747 7472D7B 1384803NM TE FLAP GOUGED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15527MC 22471 DURING D-CHECK, DEEP GOUGE FOUND ON THE EDGE OF THE INBOARD LINK ON THE NR 18 VARIABLE CAMBER FLAP. BLENDED OUT DAMAGE FROM SURFACE OF LINK. NDT INSPECTED TO ENSURE CRACK AND DEFECT CONDITION. SHOP PREENED PER SOPM 20-10-03, INTENSITY .006A2. REFINISHED LINK TO DESIGN STANDARD. (M) 2L74 4F RTA20WE 20050329001142005032900114NM 2005 3 29 SWAA050907 120050324A55536547450 FITTING BOEING737 7373H4 1384600NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29605SW 27956 DURING SCHEDULED D-CHECK, FOUND VERTICAL STAB FITTING LT & RT PRIMARY CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER SRM. 2L72 4F RTA16WE 20050329001152005032900115NM 2005 3 29 SWAA050908 120050324A55536546874 DRAG ANGLE BOEING737 7373H4 1384600NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29605SW 27956 DURING SCHEDULED D-CHECK, FOUND VERTICAL STAB LT & RT DRAG ANGLES CORRODED. REMOVED AND REPLACED ANGLES PER SRM. 2L72 4F RTA16WE 20050329001162005032900116NM 2005 3 29 SWAA050909 120050324A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29605SW 27956 DURING SCHEDULED D-CHECK, FOUND CORROSION ON SHEAR TIE AT BS 727 C, BL 0. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050329001202005032900120NM 2005 3 29 72300088 120050325A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 20 X 3 INCH AREA OF CORROSION ON ENTIRE STRINGER FROM STA 460 TO STA 480. 2L73 4F4 FRTA3WE E2EA 20050329001222005032900122NM 2005 3 29 72300090 120050325A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 4 X 1 INCH AREA OF CORROSION ON STRINGER. 2L73 4F4 FRTA3WE E2EA 20050329001232005032900123NE 2005 3 29 20052 220050326A7200PW121 ENGINE DHAV DHC8 DHC8103 1386005NM PWA PW121 PW121 52124NE NR 2 FOD A KPVAO OTHER CRJF.O.D. PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 WP13806WP346454008 357 PCE120142 RIGHT ENGINE MADE POPPING NOISE DURING CRUISE AND INDICATED TORQUE FLUCTUATION AND SLIGHT VIBRATION. NO OTHER LIGHTS OR INDICATIONS WERE OBSERVED. REMOVED AND REPLACED NR 2 ENGINE ASSY IAW AIA FORM M-105. OPS AND LEAK CHECK GOOD. 2H72 4T4 TRTA13NM E20NE 20050329001242005032900124 2005 3 29 HSYA01031505 420050316A3442066031140000 INDICATOR CESSNA208 208B 2073701CE RADAR SMOKE E HSYAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 NM05766FE 208B0260 SMOKE COMING FROM THE RADAR INDICATOR. 1H71 3T A37CE 20050329001272005032900127CE 2005 3 29 DXTA200500643 120050326A3150 WARNING LIGHT RAYTHNDH125 HAWKER800XP 7150012CE GARRTTTFE731TFE7315BR WP FUEL FILTER ILLUMINATED E DXTAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL07867QS 258576 P107690 DURING T/O ROLL AT 80 KTS ENG 2 FUEL ANNUNCIATORS ILLUMINATED. T/O ABORTED, ANNUNCIATOR EXTINGUISHED WHEN POWER REDUCED, THEN RE-ILLUMINATED AFTER RUNNING NR 2 ENGINE UP AGAIN TO FULL STATIC POWER AFTER 5-7 SECONDS. COULD NOT DUPLICATE SQK RAN ENGINES AT MAX POWER FOR 3 MIN, TWICE. REMOVED NR 1 ENG FUEL FILTER, NO DEBRIS NOTED. INSTALLED NEW FILTER, RAN ENGINES AT MAX PWR FOR THREE MINUTES FUEL ANNUNCIATOR DID NOT ILLUMINATE, NO LEAKS NOTED IAW TFE 731-5BR M/M 73-21-02. 2L72 4F4 FRTA3EU E6WE 20050329001282005032900128NM 2005 3 29 SWAA050911 120050324A53116546539 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29606SW 27926 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, RBL 65, WL 201. REPAIRED FRAME PER PAE ER. 2L72 4F RTA16WE 20050329001302005032900130NM 2005 3 29 SWAA050913 120050325A53226546549 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29607SW 27927 DURING SCHEDULED D-CHECK, FOUND CORROSION ON FUSELAGE SHEAR TIE AT B3 767, LBL 8, WL 148. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20050329001332005032900133NM 2005 3 29 SWAA050916 120050324A3350D71702001 BATTERY BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED SPECIAL VISIT, FOUND L1 DOOR LOWER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050329001342005032900134NM 2005 3 29 SWAA050917 120050324A53116546546 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29656SW 28401 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE BELT FRAME CORRODED AT BS 787, LBL 51.5. REPAIRED FRAME PER SWA EA. 2L72 4F RTA16WE 20050329001352005032900135NM 2005 3 29 SWAA050918 120050324A57436582770 SUPPORT BEAM BOEING737 7373Q8 1384670NM LT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND LT MLG SUPPORT BEAM CORRODED AT FASTENER HOLES. REPAIRED BEAM PER PAE ER. 2L72 4F RTA16WE 20050329001372005032900137NM 2005 3 29 SWAA050920 120050325A53306545765 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 515, STR 16L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050329001392005032900139NM 2005 3 29 SWAA050922 120050325A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 19L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050329001422005032900142NM 2005 3 29 SWAA050925 120050325A53306545776 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 980, STR 21L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050329001442005032900144NM 2005 3 29 SWAA050927 120050325A53306545776 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29690SW 23783 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 919 TO BS 922, STR 21R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050329001462005032900146NM 2005 3 29 SWAA050929 120050324A3350BR2013 LIGHT BOEING737 7373Q8 1384670NM ROWS 7-9 PEELING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 FWD END OF EEPLS AT ROW 7 TO ROW 9 PEELING. REMOVED AND REPLACED EEPLS STRIP PER MM. 2L72 4F RTA16WE 20050329001482005032900148SO 2005 3 29 MASA200500144 120050222A3260355022002 CONTROL UNIT EMB 145 EMB145LR 3260212SO MLG INOPERATIVE A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07843MJ6852 145478 RETURNED TO THE FIELD FOR A LANDING GEAR AIR GROUND FAIL MESSAGE ON EICAS WHICH PREVENTED THE GEAR FROM BEING RETRACTED. THE AIRCRAFT ALSO EXPERIENCED A DUAL REVERSER DISAGREE AT 2500 FEET. MAINTENANCE IS CURRENTLY TROUBLESHOOTING. MX REPLACED LANDING GEAR ELECTRONIC CONTROL UNIT. 2L72 4T RTT00011AT 20050329001492005032900149SO 2005 3 29 MASA200500147 120050223A783083990168 SWITCH EMB 145 EMB145LR 3260212SO THRUST REVERSER INOPERATIVE A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07833MJ1595 145327 ABORTED TAKEOFF FOR A E2 REVERSER DISAGREE ON TAKEOFF ROLL. MAINTENANCE DEACTIVATED THE THRUST REVERSER AND PLACED IT ON MEL. MX REPLACED STOW SWITCH AND RIGGED OPS CHECK GOOD. 2L72 4T RTT00011AT 20050329001502005032900150SO 2005 3 29 MASA200500175 120050303A5313 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE CHAFED A MASAK NONE O OTHER ININSP/MAINT 1 SW07850MJ 145568 IN C-CHECK, STRINGER 19 RT IS CHAFED OUT OF LIMITS AND HAS BEEN REPAIRED IAW SRM 53-24-02. 2L72 4T RTT00011AT 20050329001532005032900153SO 2005 3 29 MASA200500178 120050303A531114522459003 FRAME EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A MASAK NONE O OTHER ININSP/MAINT 1 SW07850MJ 145568 IN C-CHECK RAMP AT BL 0 FRAME 19 & 20 IS CORRODED AND HAS BEEN REPLACED IAW SRM 51-40-02. 2L72 4T RTT00011AT 20050329001542005032900154SO 2005 3 29 MASA200500179 120050303A532014522460013 BUTTSTRAP EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A MASAK NONE O OTHER ININSP/MAINT 1 SW07850MJ7322 145568 IN C-CHECK, BUTTSTRAP AT BL 0 BETWEEN FRAME 20 AND FRAME 23 IS CORRODED AND HAS BEEN REPLACED IAW SRM 51-40-02. 2L72 4T RTT00011AT 20050329001562005032900156SO 2005 3 29 MASA200500181 120050303A532014522461011 STRAP EMB 145 EMB145LR 3260212SO THRESHOLD CORRODED A MASAK NONE O OTHER ININSP/MAINT 1 SW07850MJ7322 145568 IN C-CHECK, RT SERVICE DOOR THRESHOLD IS CORRODED AND HAS BEEN REPAIRED IAW SRM 53-21-10 AND THE STRAP LOACTED AT FR23 HAS BEEN REPLACED. 2L72 4T RTT00011AT 20050329001572005032900157SO 2005 3 29 MASA200500182 120050303A5520 SKIN EMB 145 EMB145LR 3260212SO ELEVATOR LIGHTNING STRIKEA MASAK NONE O OTHER ININSP/MAINT 1 SW07850MJ7322 145565 145568 IN C-CHECK, RT ELEVATOR HAS LIGHTNING STRIKE DAMAGE AT TRAILING EDGE. DAMAGE HAS BEEN REPAIRED IAW IC2005-145/1116. 2L72 4T RTT00011AT 20050329001592005032900159SO 2005 3 29 MASA200500199 120050310A2150 A/C PACK EMB 145 EMB145LR 3260212SO NR 2 SMOKE A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW07829MJ 145228 SMOKE IN THE CABIN ON THE GROUND COMING FROM PACK 2. PACK 2 WAS PLACED ON MEL. MAINTENANCE COULD NOT DUPLICATE, OPS CHECKED NORMAL. 2L72 4T RTT00011AT 20050329001602005032900160NM 2005 3 29 CALA0500088 120050325A531565C339503 FLOORBEAM BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714609 27322 INSPECTION FOUND THE MAIN CABIN FLOORBEAM CORRODED AT STA 986.5, LBL 43. REPAIRED IAW ECRA 5321-01211. 2L72 4F RTA16WE 20050329001612005032900161NM 2005 3 29 CALA0500089 120050325A3350D71701100 BATTERY PACK BOEING737 737724 13844BYNM EMERGENCY LIGHT INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2724729 28945 THE EMERGENCY AISLE LIGHT BATTERY PACK AT SEAT ROW 19 LT LOWER SIDEWALL FAILED CHECK. THE BATTERY PACK WAS REMOVED AND REPLACED. 2L72 4F RTA16WE 20050329001632005032900163SO 2005 3 29 MASA200500211 120050313A5210 SEAL EMB 145 EMB145LR 3260212SO PAX DOOR GATE LEAKING A MASAO OTHER O OTHER CRCRUISE 1 SW07850MJ 145568 A LOUD PRESSURIZATION SQUEAL COMING FROM THE MAIN PAX DOOR. MAINTENANCE RE-INSTALLED THE FLAPPER SEAL ON THE TOP OF THE DOOR. MAINTENANCE COULD NOT DUPLICATE ANY FURTHER FAULTS WITH PAX DOOR ON THE GROUND. 2L72 4T RTT00011AT 20050329001652005032900165SO 2005 3 29 MASA200500217 120050315A2120 ODOR EMB 145 EMB145LR 3260212SO CABIN DETECTED A MASAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW07827MJ 145217 RETURNED TO THE GATE DUE TO HOT OIL SMOKE SMELL AND VISIBLE SMOKE REPORTED IN CABIN BY F/A. MAINTENANCE RAN BOTH ENGINES AND BOTH PACKS AND WERE UNABLE TO DUPLICATE DISCREPANCY. A/C DEPARTED WITHOUT FURTHER INCIDENT. 2L72 4T RTT00011AT 20050329001662005032900166SO 2005 3 29 MASA200500219 120050314A532014529150003 ANGLE EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A MASAK NONE O OTHER ININSP/MAINT 1 SW07825MJ11111 145179 IN CHECK, FLOOR RISER AT RT CORRODED FR 23. REMOVED RT OUTBOARD CLIP ON RISER OUT OF LIMIT. FAB NEW PER SAMPLE AND INSTALLED. 2L72 4T RTT00011AT 20050329001672005032900167SO 2005 3 29 MASA200500220 120050314A534714532605011 SEAT TRACK EMB 145 EMB145LR 3260212SO FUSLEAGE CORRODED A MASAK NONE O OTHER ININSP/MAINT 1 SW07825MJ11111 145179 IN C-CHECK, SEAT TRACK AT LT Y479 CORRODED FROM FR 18 TO FR 24, OUT OF LIMITS REF SRM 53-00-11. REPLACED TRACK. 2L72 4T RTT00011AT 20050329001682005032900168SO 2005 3 29 MASA200500221 120050314A532014521699003 BUTTSTRAP EMB 145 EMB145LR 3260212SO FLOOR SUPPORT CORRODED A MASAK NONE O OTHER ININSP/MAINT 1 SW07825MJ11111 145179 IN C-CHECK, BUTT STRAP CORRODED AT LT Y4790 FROM FR 18 TO FR 24 OUT OF LIMITS REF SRM 53-21-10. REPLACED BUTT STRAP. 2L72 4T RTT00011AT 20050329001692005032900169SO 2005 3 29 MASA200500222 120050314A533012020333049 SKIN EMB 145 EMB145LR 3260212SO FUSELAGE DENTED A MASAK NONE O OTHER ININSP/MAINT 1 SW07825MJ 145179 IN C-CHECK, PERFORM PERMANENT REPAIR ON SKIN FORWARD OF APU DOOR DUE 1034 FC SHARP DENT REPAIRED, EXTERNAL REPAIR DOUBLER REF SRM 53-32-01. 2L72 4T RTT00011AT 20050329001712005032900171NM 2005 3 29 BB05023 120050326A29136506606 PUMP BOEING767 7672B7 1385107NM GE CF6 CF680C2B2 30025NE RT ENGINE FAILED A USAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA19653US2121621216 24894 695424 EN ROUTE, CREW RECEIVED THE EICAS MESSAGE R HYD PRIM PUMP AND NOTED DECREASING HYDRAULIC QUANTITY AND PRESSURE. CREW SECURED THE RIGHT EDP. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT EDP. 2L72 4F4 FRTA1NM E13NE 20050329001732005032900173NM 2005 3 29 BB05024 120050328A3397 WIRE BOEING767 7672B7 1385107NM EMERGENCY LIGHT DETACHED A USAAK NONE O OTHER ININSP/MAINT 1 EA19656US 26847 FOUND EMERGENCY LIGHTS AT ROW 19-28, LEFT SIDE, INOPERATIVE. MAINTENANCE FOUND A DETACHED WIRE AT ROW 28 AND SECURED IT. 2L72 4F RTA1NM 20050329001762005032900176EA 2005 3 29 6045447120105 120050201A27419960013 SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED E J7SABA EMER. DESCENT UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SW05323FX 5447 AFTER TAKEOFF CREW COULD NOT ACTUATE MACH/STAB TRIM WARNING CAS MESSAGE ON EICAS. EMERGENCY DECLARED AND AIRCRAFT RETURNED TO DEPARTURE AIRPORT WITHOUT INCIDENT. MAINTENANCE REPLACED FAULTY TRIM DISCONNECT SWITCH. 2L72 4F RTA21EA 20050329001782005032900178 2005 3 29 UPS05144199 420050327A2565 LIGHT AIRBUS300 A300B4622R 3930312EU PAX DOOR SLIDE INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01159UP 0848 SLIDE TEST LIGHT ON MAIN ENTRY DOOR INOP. REMOVED AND REPLACED ASPSU BATTERY PACKS IAW MM 52-73-18-4, CKS GOOD IAW MM 52-73-00-1 501. 2L72 4F RTA35EU 20050329001792005032900179NM 2005 3 29 UPS05444197 120050325A3350S135610A BATTERY BOEING747 747121 1384871NM EMERGENCY LIGHT DISCHARGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE:A CHECK EMERGENCY LIGHT IN CIRCULAR CEILING LIGHT WILL NOT TAKE A CHARGE. REPLACED BATTERY PACK EMERGENCY LIGHT, OPS CHECKS OK. 2L74 4F A20WE 20050329001812005032900181EU 2005 3 29 CHQA200500063 120050326A3350 LIGHT EMB ERJ170ERJ170100LR EU CABIN MALFUNCTIONED A CHQAO OTHER O OTHER LDLANDING 1 GL11631RW 17000007 UPON LANDING, THE EMERGENCY LIGHTS TURNED ON WITH THE SWITCH IN THE ARMED POSITION. PERFORMED ELECTRICAL POWER RESET IAW 33-50-00-810-805A. OPS CHECK GOOD IAW EMB 170 AMM 33-50-00. 2L74 4F RTA56NM 20050329001822005032900182SO 2005 3 29 CHQA200500064 120050327A33501317 BULB EMB 135 EMB135KL 3260302SO EMERGENCY LIGHT BURNED OUT A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11295SK 145513 LEFT HAND AFT OVERWING EMERGENCY EXIT LIGHT IS INOP. RELAMPED LEFT HAND AFT OVERWING EMERGENCY EXIT LIGHT. OPS CHECK GOOD IAW EMB 140 AMM 33-50-09. 2L72 4F RTT00011AT 20050329001842005032900184EU 2005 3 29 AWXA200500360 120050324A3397ABS0374A24 CABLE AIRBUS320 A320232 3930326EU EMERGENCY LIGHT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28647AW 762 LAX - EEL - DURING 8-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 21 LT INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 21 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050329001872005032900187NM 2005 3 29 AWXA200500363 120050302A3150BACC18Z3R CIRCUIT BREAKER BOEING737 73733A 1384673NM COCKPIT DEFECTIVE A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28174AW 23633 LAS - ABORTED TAKEOFF - FLT 0399 - ON TAKEOFF AT LAS EN ROUTE FOR DFW THE TAKEOFF CONFIGURATION WARNING HORN SOUNDED COUNTINUOUSLY, RETURNED TO GATE. MAINTENANCE REMOVED EXCESSIVE GREASE AT SWITCHED S132 AND S546, REPLACED LEADING EDGE FLAP CIRCUIT BREAKER AS A PRECAUTION. TAKEOFF WARNING SYSTEM TEST WAS GOOD PER T/C A1B31009. 2L72 4F RTA16WE 20050329001892005032900189SO 2005 3 29 SWIA200514766 120050207A5320 BUTTSTRAP EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0758733 120197 LEFT BUTT STRAP AT FRAME 38 TO 44 IS CORRODED AT 479.00. ITEM FOUND AT C-CHECK INSPECTION. REPLACED BUTT STRAP IAW EMB 120 SRM 57-40-02. 2L72 4T RTA31SO 20050329001902005032900190NM 2005 3 29 QXEA200500385 120050119A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 200 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - AFT FUSELAGE, AFT ENTRY DOOR SURROUND STRUCTURE FORWARD LATCH TRACK GOUGED, STATION 6680, STRINGER 17P. 2H72 4T RTA13NM 20050329001942005032900194NM 2005 3 29 QXEA200500383 120050119A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 100 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - FUSELAGE EXTERNAL SKIN AT STATION X7.5 AND STRINGER 28L HAS A NICK. REPAIRED IAW RD 8/4-53-66, ISSUE 1, PAGE 5, STEPS 1 THROUGH 6. 2H72 4T RTA13NM 20050329001952005032900195NM 2005 3 29 SWAA050790 120050314A534065C27314 STRINGER CLIP BOEING737 737317 138447PNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29686SW 23175 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON STRINGER CLIP AT BS 767, STR 26R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050329001962005032900196 2005 3 29 SWAA050770 420050314A256563562101 SLIDE BOEING737 7377H4 1384404NM L1 DOOR READS LOW A SWAAK NONE O OTHER ININSP/MAINT 1 SW29724SW 27856 L1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATING LOW. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20050329001982005032900198 2005 3 29 SWAA050772 420050314A25656557463 FITTING BOEING737 7373H4 1384600NM L1 DOOR GIRT BARCORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29605SW 27956 DURING SCHEDULED D-CHECK, FOUND CORROSION ON L1 DOOR EVAC SLIDE GIRT BAR FLOOR FITTINGS. REMOVED AND REPLACED FITTINGS PER SRM. 2L72 4F RTA16WE 20050329002002005032900200NM 2005 3 29 SWAA050792 120050314A53306545768 SKIN BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29686SW 23175 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 375, ABOVE STR 15L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050329002032005032900203NM 2005 3 29 SWAA050793 120050314A53126546568 WEB BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29686SW 23175 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE WEB CRACKED AT BS 1016 BULKHEAD, 1 O'CLOCK POSITION. REPAIRED WEB PER SWA EA. 2L72 4F RTA16WE 20050329002042005032900204NM 2005 3 29 QXEA200500376 120050124A5753 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 600 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - RIGHTHAND INBOARD FLAP HAS THREE AREAS WHERE IT IS CHAFING WITH THE UPPER SHROUD AND HAS WORN THROUGHT TO THE METAL. REPAIRED IAW Q400 SRM 57-51-30-940-001, 57-51-30-320-801. 2H72 4T RTA13NM 20050329002052005032900205GL 2005 3 29 C2XA05CL016 220050315A7200 ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 1 SMOKE A C2XAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SW27125646141 145618 CAE312180 CLE - FLIGHT 2115 THE CREW REPORTED SMOKE IN CABIN AND FLIGHT DECK FROM PACKS. THE AIRCRAFT RETURNED TO LGA AND MAINTENANCE PLACED PACK NR 1 ON MEL. THE AIRCRAFT HEATING AND AIR CONDITIONING SYSTEM WAS TESTED THE NEXT DAY AND FOUND TO BE OPERATING CORRECTLY, AND THE SOURCE OF THE SMOKE WAS THE NR 1 ENGINE. MAINTENANCE REPLACED THE NR 1 ENGINE AND THE OPERATIONAL CHECKS WERE GOOD WITH NO SMOKE OR FUMES DETECTED. 2L72 4T4 FRTT00011ATTE6CH 20050329002062005032900206SO 2005 3 29 C2XA05BT016 120050309A3350744437 SIGN EMB 145 EMB145LR 3260212SO FUSELAGE FAULTY A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713988 145265 DURING 4A INSPECTION IN BTV, MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT SIGN AT SEAT 12A AREA TO BE NOT OPERATING. REMOVED AND REPLACED EMERGENCY EXIT SIGN AT 12A AREA IAW EMB145 MM 33-50-14. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050329002072005032900207EU 2005 3 29 MALA050234 120050224A5411 LONGERON SAAB SF340 340B 7860101EU RT NACELLE CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15414XJ 340B414 RIGHT NACELLE, I/B SIDE, INSIDE FWD ELECTRONIC BAY, INBOARD LOWER LONGERON IS CHAFED. THE DAMAGE IS ACCEPTABLE IAW SAAB DOCUMENT 340S0S008258. 2L72 4T RTA52EU 20050329002122005032900212EU 2005 3 29 MALA050220 120050224A3060 LEAD SAAB SF340 340B 7860101EU ROTOL R390 R3904123F27 NE DE ICE SYSTEM BROKEN A MALAO OTHER E VIBRATION/BUFFET CRCRUISE 1 GL15415XJ 340B415 AIR RETURN DUE TO VIBRATION FELT INFLIGHT. INSPECTED ALL COMMON AREAS ON AIRCRAFT THAT CAUSE VIBRATION. FOUND NOTHING THAT COULD VIBRATE. AFTER REMOVING LT SPINNER FOUND ROUGHLY A 1/4 POUND OF GREASE BUILT UP ON ONE SIDE OF SPINNER. ALSO FOUND ONE DE-ICE LEAD BROKEN AND SUSPECT ICING BUILD UP THAT THREW PROP OUT OF BALANCE. INSPECT LT AND RT PROP HUBS FOR OIL. 2L72 4T RTA52EU 6 CP31NE 20050329002152005032900215WP 2005 3 29 05FDEA00358 120050303A3411HG280D4 COMPUTER DOUG DC10 DC1010 3022110WP NR 2 MALFUNCTIONED A FDEAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO25395FE9597 9597 46629 ON ROTATION THE FIRST OFFICERS ALTIMETER DESCENDED TWO THOUSAND FEET (-2000). ALTIMETER REMAINED 2000 FT BELOW THE CAPT'S ALT AND STANDBY ALT REMAINDER OF FLIGHT. SWITCHED CADC'S, NO CHANGE - ALT STATIC SOURCE NO CHANGE. REMOVED AND REPLACED NR 2 AIR DATA COMPUTER IAW DC10-10 AMM 34-16-01-2. NR 2 ALTIMETER SYSTEM OPERATIONAL CHECKS NORMAL, NO DISCREPANCIES NOTED. PREMATURE REMOVAL/INSTALLATION, OFF MFG HG280D4, POS P2 SRL 465, TAG A03096, ON MFG HG280D80 SRL 115, TAG 590682. 2L73 4F A22WE 20050329002172005032900217WP 2005 3 29 IXXA05000180 120050313A5280 SEAL DOUG DC8 DC862F 3021972WP NLG DOOR MISSING A IXXAO OTHER E VIBRATION/BUFFET CLCLIMB 1 SW1171CX 661672461 45961 UPON CLIMBOUT FROM KBWI EN ROUTE TO KWRI AFTER GEAR RETRACTION CREW NOTED AIR NOISE FROM UNDER COCKPIT FLOOR. AFTER GEAR RECYCLE, UNDER AIR LOAD NOISE DECREASED. CREW PROCEEDED TO KWRI AND MADE AN UNEVENTFUL LANDING. UPON INSPECTION MX NOTED NLG DOOR SEAL ON RT SIDE MISSING AND INSTALLED A SERVICEABLE SEAL. AIRCRAFT RETURNED TO SERVICE. 2L74 4F 4A25 20050329002192005032900219NM 2005 3 29 SWAA050794 120050314A53306545768 SKIN BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29686SW 23175 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 445, STR 24R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050330000012005033000001WP 2005 3 30 ASAA0580122 120050227A532199365521 FLOOR PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE CABIN DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 OKC HV-CHECK - CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (K) 2L72 4F4 FRTA6WE E9NE 20050330000022005033000002NM 2005 3 30 USAA050340 120050303A5755 SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU NR 6 SPOILER DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19519AU50516 23705 CLT - Q2 - NR6 SPOILER, 2 INCH X 6 INCH, DELAMINATION. NR 6 SPOILER TOP SURFACE IB, 6 INCHES FROM T/E. APPLIED COMPOSITE REPAIR IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050330000032005033000003EU 2005 3 30 KBM2005F00041 120050312A2121050143 MOTOR SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE BLOWER INCORRECT E KBMAK NONE O OTHER ININSP/MAINT 1 WP19230SH 2337 5 INCH BLOWER MOTOR, ARMATURE NO POSITIONED CORRECTLY. REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20050330000042005033000004WP 2005 3 30 ASAA0580123 120050227A532199365851 FLOOR PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE CABIN DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 OKC HV - CHECK - CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (K) 2L72 4F4 FRTA6WE E9NE 20050330000052005033000005EA 2005 3 30 A6WA200540100 120050316A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31413AW 7585 LT INTERCOSTAL AT FS 484.0 AT LBL 36 CRACKED, .5 INCH LONG. PERFORMED A REPAIR AT 484.0 LBL 36 BY CUTTING OUT DAMAGED AREA AND INSTALLING NEW ANGLE IAW REO. (K) 2L72 4F4 FRTA21EA E15NE 20050330000202005033000020WP 2005 3 30 ASAA0580107 120050215A53105912494501 DOOR FRAME DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE GOUGED A ASAAO OTHER O OTHER NRNOT REPORTED 1 NM02943AS 53018 OKC C-CHECK - FWD CARGO DOOR JAMB GOUGED. REPLACED DAMAGED SECTION IAW EA. (K) 2L72 4F4 FRTA6WE E9NE 20050330000262005033000026CE 2005 3 30 R9E2005F00000 120050301A5511 SPAR BEECH 1900 1900D 1154162CE HORIZONTAL STAB CORRODED E R9EAO OTHER O OTHER NRNOT REPORTED 1 SO1746AR 10903 UE27 DURING AN (I) CHECK INSPECTION THE UPPER AND LOWER HORIZONTAL SPAR CAPS WERE FOUND WITH CORROSION IN THE AREA OF THE ELEVATOR HINGES. THIS AREA WAS NOT TREATED OR PRIMED BY THE FACTORY DURING AC MANUFACTURE AND THUS WAS CONDUCIVE TO CORROSION. THIS IS CONSIDEREED TO BE AFACTORY DEFECT REQUIRING INSPECTION, CORROSION CONTROL AND REPAIRS IAW MFG FIELD REPAIR DETAILS. 2L72 4T RTA24CE 20050328000562005032800056 2005 3 28 ASMF200503007 420050309A2200285A1010106 MODULE BOEING737 737* NM AUTOFLIGHT FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23906AM1083 29356 CAPTAIN REPORTED THAT MESSAGE (SPD LIM FLAG IN PFD) WAS SHOWN. REPORT WAS DEFERRED IAW MEL 34-2-1. AIRCRAFT RETURNED TO PLATFORM BECAUSE OF MACH TRIM, AUTO SLAT, LIGHT SPEED TRIM AND YAW DAMPER FAILED. FIM 22-11 TASK 810-811 WAS PERFORMED AND THE SMYD WAS REPLACED IAW MM 27-32-21, TESTED CORRECT, DEFERRED REPORT WAS CLOSED. 2L72 4F RTA16WE 20050328001252005032800125NM 2005 3 28 UPS05244170 120050308A5523 TAB BOEING727 72722C 138400FNM RT ELEVATOR DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 INSPECTION TYPE:C EVIDENCE OF DELAMINATION TO RT ELEVATOR TAB UPPER INBOARD SURFACE. TAB REPLACED IAW MM 27-30-11 & 27-30-00. 2L73 4F A3WE 20050328001272005032800127NM 2005 3 28 UPS05444173 120050314A5347BAC15201566 SEAT TRACK BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE:C M/D- BS 2130 TO 2140 LBL 75 SEAT TRACK FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.045 X 1 X 1 INCH. CORROSION BLEND OUT 0.045 X 1 X 1 INCH, EXCEED SRM 53-10-01 FIG 1 LIMITS. SEAT TRACK REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050328001312005032800131NM 2005 3 28 UPS05444177 120050314A5347 SEAT TRACK BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE:C M/D- BS 1800 TO 1920 RBL 11 SEAT TRACK FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.040 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 16. 2L74 4F A20WE 20050328001362005032800136NM 2005 3 28 CALA0500087 120050318A5311146N1013 FRAME BOEING757 757224 1384958NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714106 27296 INSPECTION FOUND AFT CARGO PIT FRAME CORRODED AT BS 1440, RBL 9, BETWEEN S28R AND S29R. A REPAIR WAS PERFORMED IAW ECRA 5310-04467. A DIP WAS ISSUED TO PERFORM A PERMANENT REPAIR AFTER 10 MONTHS, BUT BEFORE 3-14-2006. 2L72 4F RTA2NM 20050328001422005032800142NM 2005 3 28 UPS05444182 120050313A5320 FLOOR SUPPORT BOEING747 747121 1384871NM M/D CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE:C M/D-BS 1650 LBL 118 FLOOR SUPPORT FOUND CORRODED. CORROSION BLEND OUT 0.035 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. FLOOR SUPPORT REPAIRED AS PER SRM 51-40-03 FIG 1. 2L74 4F A20WE 20050328001482005032800148NM 2005 3 28 UPS05244165 120050315A5330 SKIN BOEING727 72722C 138400FNM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 INSPECTION TYPE:C AREAS OF LITE SURFACE CORROSION FOUND ON INNER FUSELAGE SKIN SURFACE OF LWR SURFACE OF INTERNAL DOUBLER BETWEEN S3L & S2L BS 630 TO 660 AT VARIOUS LOCATIONS. REPAIR CARRIED OUT IAW SRM 53-30-03. 2L73 4F A3WE 20050328001552005032800155NM 2005 3 28 UPS05444189 120050312A532265B133731 STIFFENER BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE:C M/D- STA 1435 RBL 65 WHEEL WELL UPPER SKIN ATTACH STIFFENER FOUND CRACKED, LENGTH .375 INCH. STIFFENER REPLACED AS PER SRM 51-30-02 & SRM 51-10-01 PG 9. 2L74 4F A20WE 20050328001562005032800156NM 2005 3 28 UPS05444191 120050310A5414707500063IN FRAME BOEING747 747121 1384871NM NR 3 NACELLE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE:C NR 3 PYLON NAC STA 250 O/B FRAME LOWER TO WEB ATTACHMENT AREA CRACKED, LENGTH 1.5 INCH. FRAME REPAIRED AT LOWER PORTION AS PER SRM 54-10-03 FIG 1. 2L74 4F A20WE 20050328001612005032800161WP 2005 3 28 UPS05844160 120050217A53405890314U2 ATTACH FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE:C1 AC COMPT FS 55.00 MAIN CABIN SUBFLOOR AREA RBL 48.00 FWD O/B SIDE OF FLOORBEAM INTERSECTION VERTICAL ATTACH FITTING HAS A CRACK BETWEEN FASTENERS. REMOVED AND REPLACED VERTICAL ATTACH FITTING AT FS 55.00 RBL 48.00 IAW SRM 51-1-21 AND 51-1-20D. 2L74 4F RT4A25 20050328001662005032800166EU 2005 3 28 RAIA00503012 120050323A2697 WIRE JETAIRJETSTMJETSTM4101 1500501EU SMOKE DETECTOR BROKEN A RAIAD RETURN TO BLOCK L NO TEST TXTAXI/GRND HDL 1 CE03554HK 41067 STL - POD AND AFT SMOKE SYSTEM WILL NOT TEST. MAINTENANCE REPAIRED BROKEN WIRE TO TEST CONNECTOR AND OPS CHECK GOOD. 2L72 4T RTA41NM 20050328001812005032800181NE 2005 3 28 69805 220050316A73203033260 LINE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE NR 1 BROKEN A AMWAB EMER. DESCENT O OTHER CLCLIMB 1 CE07242YV UE242 ON CLIMBOUT NR 1 PROP RPM DECREASED WITH NO PROP LEVER INPUT. PLACED PROP TO FULL RPM POSITION & RPM DECREASE. TRIED TO MATCH RPM ON BOTH ENG, STOPPED WHEN NR 2 GOOD ENG WAS 1300 RPM. ENG HAD OUT OF SYNC PROP BEAT, ACFT YAWING. TORQUE ON NR 1 ENG ROSE, RPM'S DROPPED. OIL PRESSURE AT BOTTOM OF GREEN ARC/TOP OF YELLOW ARC. NR 1 PROP 200 RPM, WINDMILLING WITHOUT ANY FORWARD POWER. CREW SHUT DOWN NR 1 ENG, FOLLOWED CHECKLISTS & PROCEDURES. DIVERTED TO LIT, EMERGENCY VEHICLES AND EQUIPMENT STANDING BY. APPROACH TO LIT WAS UNEVENTFUL AND CREW SHUTDOWN AIRCRAFT AT TAXIWAY. MX LINED GCU PARAMS, REMOVED & REPLACED P-3 LINES, ADJUSTED BETA VALVE ACCOMPLISHING ENG RIGGING. 2L72 4T4 TRTA24CE E26NE 20050328001882005032800188NM 2005 3 28 BB05019 120050321A335020121 CHARGER BOEING767 767201 1385125NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19648US 23900 PHL FOUND AFT RIGHT DOOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER (M734). 2L72 4F RTA1NM 20050328001902005032800190SO 2005 3 28 138903172005 120050317A2433 CONVERTER GULSTM GULSTMG1159 GIV 3980115SO ALTERNATOR FAILED E N93AA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO13489QS 43A0539 1389 RIGHT ALTERNATOR FAILED CONVERTER / ALTERNATOR ISOLATION CHECK. 2L72 4F RTA12EA 20050328002092005032800209NM 2005 3 28 SWAA050890 120050322A53116546531 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 492, STR 24R. REPAIRED FRAME PER PAE ER. 2L72 4F RTA16WE 20050328002122005032800212NM 2005 3 28 SWAA050893 120050322A3350BR2013 LIGHT BOEING737 7377H4 1384404NM FWD CABIN PEELING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29766SW 29806 DURING SCHEDULED MV1 CHECK, FOUND FWD CABIN EEPLS STRIP PEELING. REMOVED AND REPLACED EEPLS STRIP PER MM. 2L72 4F RTA16WE 20050329000042005032900004WP 2005 3 29 ASAA0580135 120050227A5230 SKIN DOUG DC9 DC983 3022083WP CARGO DOOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 HV-CHECK, MID CARGO BAY DOOR IS DENTED. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050329000082005032900008WP 2005 3 29 ASAA0580138 120050227A5230 SKIN DOUG DC9 DC983 3022083WP CARGO DOOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 OKC - HV-CHECK, AFT CARGO BAY DOOR IS DENTED. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050329000262005032900026WP 2005 3 29 ASAA0580127 120050227A532199365471 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 OKC - HV-CHECK, FOUND CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050329000502005032900050NM 2005 3 29 USAA050318 120050211A554265C24584151 SKIN PANEL BOEING737 7373B7 1384580NM RUDDER DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU50570 23706 PIT - FOUND COMPOSITE SKIN PANEL DELAMINATED .1875 INCH DIAMETER SINGER LAYER DAMAGE, RUDDER LT SIDE 70 INCHES FROM BOTTOM, 9 INCHES FROM T/E. INSTALLED REPAIR PLYS PER SRM 51-70-17, EA 79999. (M) 2L72 4F RTA16WE 20050329000572005032900057NM 2005 3 29 USAA050333 120050301A53201135094 FLOOR SUPPORT BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19438US 24560 PIT - FOUND FLOOR SUPPORT CORRODED 1 INCH BY 8 INCH AREA, FORWARD ENTRANCE FLOOR SUPPORT. CORROSION LEVEL 1, TASK NR C53-107-01. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-40-02. (M) 2L72 4F RTA16WE 20050329000662005032900066NM 2005 3 29 USAA050308 120050208A5320 FLOOR SUPPORT BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19780AU39018 24997 PIT - FOUND FLOOR SUPPORT CORRODED .75 INCH DIAMETER, BETWEEN STRAP 500 AND 500A RBL 9. INSTALLED ANGLE DOUBLER PER TYPICAL REPAIR 53-10-06B. (M) 2L72 4F RTA16WE 20050329000692005032900069EA 2005 3 29 ASOA05100 120050204A2120 ODOR CNDAIRCL600 CL6002B19 1900309EA CABIN DETECTED A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO27917EV 7769 FLT 4155 - DURING APPROACH INTO ATL FROM GTR, THE CREW NOTICED A STRONG FUEL SMELL IN THE COCKPIT. SUBSEQUENTLY THE FLIGHT ATTENDANT REPORTED A FUEL SMELL IN THE CABIN. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE CHECKED THE LEFT AND RIGHT ENGINES FOR FUEL LEAKS AND NONE WERE NOTED. MAINTENANCE ALSO GROUND RAN THE AIRCRAFT ENGINES AND PACKS WITH NO SMELL REOCCURRING. MAINTENANCE DETERMINED THE FUEL SMELL TO BE RESIDUAL FUEL FROM REPLACEMENT OF THE AUXILIARY POWER UNIT SOLENOID VALVE AFTER THE PREVIOUS FLIGHT. (M) 2L72 4F RTA21EA 20050329000742005032900074EA 2005 3 29 A6WA200540103 120050316A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31413AW 7585 LEFT CARGO FLOOR SUPPORT ANGLE AT FS 621 CRACKED AT 1 INCH. (M) REMOVED CRACKED SECTION OF FLOOR SUPPORT ANGLE AT FS 621 LT AND INSTALLED REPAIR ANGLE IAW MFG REO. (K) 2L72 4F RTA21EA 20050329000782005032900078 2005 3 29 S2YA05012 420050205A34206224565001 GYRO BEECH 1900 1900D 1154162CE VERTICAL INOPERATIVE A S2YAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL13801SK24306 UE80 FLT 6116 - IMT-MKE - BEFORE TAKEOFF, THE CREW REPORTED THE FO DISPLAY UNIT WENT BLANK, WHEN THEY TRIED TO RESET IT THE CA DISPLAY WENT BLANK ALSO. THE CREW RETURNED TO THE GATE AND REPORT THE RED ATT AND FD FLAP ON THE FO ADI. THE AIRCRAFT WAS FERRIED BACK TO MKE. MAINTENANCE REPLACED THE NR 2 VERTICAL GYRO AND OPERATIONAL CHECKED THE SYSTEM. WITH NO FURTHER DISCREPANCIES NOTED THE A/C WAS RETURNED TO SERVICE. (M) 2L72 4T RTA24CE 20050329000872005032900087NM 2005 3 29 USAA050327 120050223A5340 SUPPORT BOEING737 7374B7 1384702NM ANTENNA CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19438US40959 24560 PIT - FOUND ANTENNA SUPPORT CRACKED 1.5 INCH, 1 INCH, .6250 INCH AT STATION 727D S27L AND S27R. FABRICATED REPAIR ANGLE, TRIMMED, FITTED, HEAT TREATED PER SRM 53-60-01. (M) 2L72 4F RTA16WE 20050329000992005032900099SO 2005 3 29 SIMA200506602 120050226A532014521725015 SILL EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21804AE 145487 SAW - DURING CPCP INSPECTION, MAINTENANCE FOUND THE AFT SERVICE DOOR SILL CORRODED BETWEEN FRAMES 22-23. INSTALLED NEW SILL IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050329001042005032900104WP 2005 3 29 ASAA0580128 120050227A532199365831 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 OKC - HV-CHECK, CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050329001172005032900117NM 2005 3 29 SWAA050910 120050324A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29605SW 27956 DURING SCHEDULED D-CHECK, FOUND CORROSION ON SHEAR TIE AT BS 787, RBL 18. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050329001192005032900119NM 2005 3 29 72300087 120050325A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 20 X 3 INCH AREA OF CORROSION ON ENTIRE STRINGER FROM STA 460 TO STA 480. 2L73 4F4 FRTA3WE E2EA 20050329001252005032900125CE 2005 3 29 DXTA200500641 120050324A321367421701 STRUT CESSNA750 750 2076810CE NLG UNDERSERVICED E DXTAO OTHER WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 GL07929QS1750 7500129 AFTER TAKEOFF ON GEAR RETRACTION GOT ALL 3 GREEN LIGHTS AND THE RED UNLOCK LIGHT STAYED ON. COULD HEAR THE LOUD AIR NOISE AND THE GEAR CYCLING AT LEAST 4 TIMES. FINALLY THE GEAR CAME COMPLETELY UP AND THE UNLOCK LIGHT WENT OUT. JACK AIRCRAFT & CONFIRMED DISCREPANCY. SERVICE NOSE STRUT IAW CE750 MM 12-10-38. NOTE: NOSE STRUT FAILED TO EXTEND PRIOR TO RETRACTION. CYCLED LANDING GEAR FIVE TIMES WITH NO DEFECTS NOTED IAW CE750 MM 32-30-00. 2L72 4J RTT00007WI 20050329001262005032900126CE 2005 3 29 DXTA200500642 120050324A326067420292 CAM CESSNA750 750 2076810CE SQUAT SWITCH WORN E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07930QS4071 7500130 AFTER TAKEOFF WENT TO RETRACT THE GEAR AND THE HANDLE WOULD NOT MOVE. THE GEAR WAS STUCK IN THE DOWN POSITION. RETURNED TO DEPARTURE POINT. TROUBLESHOT DISCREPANCY TO A WORN NOSE GEAR SQUAT SWITCH CAM. REMOVED WORN CAM AND INSTALLED A NEW NOSE GEAR SQUAT SWITCH CAM WITH NEW HARDWARE. OPERATIONAL CHECK GOOD. WORK PERFORMED IAW CHAPTER 32-20-02 OF THE CITATION 750 CMM AND 32-00-01 OF THE CITATION 750 MM. 2L72 4J RTT00007WI 20050329001292005032900129NM 2005 3 29 SWAA050912 120050325A5320BAC1503 SUPPORT ANGLE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29607SW 27927 DURING SCHEDULED D-CHECK, FOUND CORROSION AT BS 270, SUPPORT ANGLE CHORD, BETWEEN RBL 11 TO LBL 11. REPAIRED CHORD PER SRM. 2L72 4F RTA16WE 20050329001312005032900131NM 2005 3 29 SWAA050914 120050325A53116520722 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29607SW 27927 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 24R. REPAIRED FRAME PER PAE ER. 2L72 4F RTA16WE 20050329001322005032900132NM 2005 3 29 SWAA050915 120050324A3350D71702001 BATTERY BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED SPECIAL VISIT, FOUND L1 & R1 DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACKS PER MM. 2L72 4F RTA16WE 20050329001382005032900138NM 2005 3 29 SWAA050921 120050325A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 740, STR 23L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050329001402005032900140NM 2005 3 29 SWAA050923 120050325A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 23R. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050329001452005032900145NM 2005 3 29 SWAA050928 120050325A53306545774 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29690SW 23783 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 727 D TO BS 727 E, STR 19R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050329001622005032900162SO 2005 3 29 MASA200500202 120050311A49004501968C APU EMB 145 EMB145LR 3260212SO APU BAY FAILED A MASAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NRNOT REPORTED 1 SW07835MJ121539990 145353 AN APU FAIL AND GENERATE A SMELL IN THE CABIN. MX FOUND THAT THE APU HAD SIEZED AND PLACED IT ON MEL. MAINTENANCE REPLACED THE APU. 2L72 4T RTT00011AT 20050329001642005032900164SO 2005 3 29 MASA200500212 120050313A2150 A/C PACK EMB 145 EMB145LR 3260212SO NR 2 SMOKE A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW07829MJ 145228 IND HAD PACK 2 GENERATING SMOKE. THE PACK WAS PLACED ON MEL. MAINTENANCE PERFORMED OPERATIONAL CHECK AND THE SYSTEM OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050329001802005032900180EU 2005 3 29 SA05034 120050324A4990 SWITCH AIRBUSA321 A321211 3930370EU APU LEAKING A USAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA19181UW 1531 EN ROUTE, PHL TO LAX. AFTER TAKEOFF, AND FOR SEVERAL THOUSAND FEET, A STRONG OILY ODOR WAS NOTICED COMING FROM THE AIR CONDITIONING SYSTEM. ODOR DISSIPATED. FLIGHT CONTINUED TO LAX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND OIL LEAK IN APU. MAINTENANCE REPLACED THE APU. OPERATIONALLY AND LEAK CHECKS OK. THE SHOP FINDINGS INDICATED THAT THE LOW OIL PRESSURE SWITCH HAD AN INTERNAL LEAK. THE SWITCH WAS REPLACED. (K) 2L72 4F RTA28NM 20050329001972005032900197NM 2005 3 29 SWAA050771 120050314A53106547978 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29605SW 27956 DURING SCHEDULED D-CHECK, FOUND L1 DOOR CREASE BEAM WEB CORRODED BETWEEN BS 312 TO BS 344, LBL 63, WL 208. REPAIRED CREASE BEAM PER SRM. 2L72 4F RTA16WE 20050329001992005032900199NM 2005 3 29 SWAA050791 120050314A53206546544 FLOOR SUPPORT BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29686SW 23175 DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL BEAM UPPER T-CHORD CRACKED AT BS 660.5, BL 0. REPAIRED T-CHORD PER SWA EA. 2L72 4F RTA16WE 20050329002082005032900208SO 2005 3 29 C2XA05IA046 120050317A2611FDS765A2 SMOKE DETECTOR EMB 145 EMB145XR 3260214SO LAVATORY INOPERATIVE A C2XAO OTHER N FALSE WARNING CLCLIMB 1 SW27141175917 5917 145674 CREW REPORTED A LAV SMOKE WARNING IN FLIGHT. MX OPERATIONALLY CHECKED LAV SMOKE DETECTOR WITH NO DEFECTS. IN PBC, REPEATED, LAV SMOKE DETECTOR PLACED ON MEL 26-14-00 CAT-C CTL NR 050058, AIRCRAFT RETURN TO SERVICE. IN IAH, MX VERIFIED NORMAL OPERATION OF LAV SMOKE DETECTOR. REMOVED MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. IN GRR, CREW AGAIN REPORTED A LAV SMOKE INDICATION DURING CLIMB WITH NO SMOKE NOTED. THE SMOKE DETECTOR WAS PLACED ON MEL 26-14-00 CAT-C CTL 050066, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED IN IAH ON FLIGHT 2906 MX REMOVED & REPLACED LAV SMOKE DETECTOR, OPS CHECKED WITH NO DEFECTS, REMOVED MEL, RETURNED TO SERVICE. 2L72 4F RT 20050329002092005032900209EU 2005 3 29 MALA050225 120050126A3260 DOWNLOCK SWITCH BAC 146 AVRO146RJ85A1500097EU MLG DIRTY A MALAO OTHER N FALSE WARNING CLCLIMB 1 GL15505XJ E2313 UPON INITIAL GEAR RETRACTION L GEAR RED UNSAFE LIGHT AND GEAR HANDLE IN TRANSIT LIGHT REMAINED ON. AFTER RECYCLING GEAR THE L GEAR LIGHT WENT OUT AND THE R GEAR UNSAFE LIGHT ILLUMINATED WITH GEAR HANDLE INTRANSIT LIGHT ON. AIRCRAFT ACCELERATED NORMALLY ON CLIMB. FOUND DOWNLOCK SWITCH AND UPLOCK SWITCHES DIRTY. CLEANED AND LUBED SWITCHES. PERFORMED GEAR SWINGS SEVERAL TIMES. ALL CHECKS GOOD IAW AVRO AMM 32-30-00. 2H74 4F RTA49EU 20050329002102005032900210EU 2005 3 29 MALA050228 120050223A5753 PANEL SAAB SF340 340B 7860101EU TE FLAP CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15423XJ 340B423 DURING 4Y/2Y CHECK IN BNA FOUND I/B UPPER SURFACE OF LT FLAP ON ACCESS PANEL S41AT IS CHAFED OUT OF LIMITS. DAMAGE IS ACCEPTABLE IAW MESABA EOS57082. 2L72 4T RTA52EU 20050330000062005033000006EU 2005 3 30 KBM2005F00040 120050311A770056337078012 SIGHT GLASS SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE NG GAUGE LOOSE E KBMAK NONE O OTHER ININSP/MAINT 1 WP19351WM 2167 NG GAUGE, COVER, GLASS LOOSE. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050330000302005033000030NM 2005 3 30 UIEA200500005 120050127A2913650666 PUMP BOEING747 747230B 1384889NM GE CF6 CF650E2 30018NE HYD SYSTEM LEAKING A UIEAH DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA15512MC 21220 530319 NR 1 HYDRAULIC CONTENTS RAPIDLY DEPLETED DURING FLIGHT. APPROPRIATE DRILLS CARRIED OUT. REMOVED AND REPLACED NR 1 ENGINE EDP IAW MM 29-11-05. NO EVIDENCE OF LEAKS AFTERWARDS. SERVICED NR 1 HYDRAULIC SYSTEM TO FULL. INSPECTED PRESS AND CASE DRAIN FILTERS. SECURED ENGINE COWL AND SHUT ACCESS. (EA15200502556) (K) 2L74 4F4 F A20WE E23EA 20050330000322005033000032 2005 3 30 KBM2005F00009 420050212A3452066106200 TRANSPONDER SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE COCKPIT INOPERATIVE E KBMAK NONE O OTHER ININSP/MAINT 1 WP19350SH 2957 UNIT RAMP CHECK INOPERATIVE, TRANSPONDER, REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20050330001092005033000109CE 2005 3 30 O2G2005F00002 120050118A325166084687 COMPUTER LEAR 60 60LEAR 5170707CE NLG STEERING FAILED E O2GAD RETURN TO BLOCK G MULTIPLE FAILURE TXTAXI/GRND HDL 1 NE0314TU 026 NOSE STEERING FAILED AT START OF TAXI. AIRCRAFT MOVED 10 FEET, UNABLE TO RETAIN CONTROL THROUGH ALTERNATE MEANS. SHUT DOWN AIRCRAFT. TROUBLESHOT AIRCRAFT, DOWNLOAD FAULTS FROM STEERING COMPUTER. FOUND RELAY FAULT, ORDERED REPLACEMENT NOSE WHEEL STEERING COMPUTER. (K) 2L72 4F RTA10CE 20050330001212005033000121EA 2005 3 30 O2G2005F00003 120050113A3260 PROXIMITY SWITCH CNDAIRCL600 CL6002B16 1900305EA GE CF34 CF34* NE NLG FAILED E O2GAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 NE03653AC2530 5153 FLASHING RED IN GEAR HANDLE IN FLIGHT, GEAR UP. REPLACED FAILED PROXIMITY SWITCH FOR NOSE GEAR DOOR CLOSED. (K) 2L72 4F4 FRTA21EA E15NE 20050330001322005033000132EU 2005 3 30 O3X020109442 120050211A29101379305A77 LINE BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UAR 01514WP HYD SYSTEM BURST A O3XAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO03944AE 108 944 AIRCRAFT WAS ENROUTE, THE CREW NOTICED ONE HYDRAULIC GAUGE FLUCTUATING AND FINALLY GOING TO ZERO AND THE OTHER GAUGE AT ZERO. THEY WENT THROUGH THE PROCEDURES FOR HYDRAULIC FAILURE. THE GEAR WAS EXTENDED. THE NOSE INDICATED DOWN AND LOCKED. THE MAINS WERE PUMPED DOWN USING THE EMERGENCY GEAR EXTENSION PROCEDURES. FLAPS WERE LOWERED USING THE HAND PUMP. THE AIRCRAFT LANDED WITHOUT INCIDENT AND SHUTDOWN ON THE RUNWAY. THE PASSENGERS WERE BUSSED TO TERMINAL AND THE AIRCRAFT WAS TOWED BY MAINTENANCE BACK ONTO RAMP. MAINTENANCE FOUND THE RT ENGINE HYDRAULIC LINE HAD BURST. THE LINE WAS REMOVED AND REPLACED. LT AND RT HYD PUMPS WERE ALSO REPLACED, LEAK AND OPS CHECKED. 2L72 4T4 TRTA56EU E4WE 20050330001332005033000133NE 2005 3 30 BJNA050103 220050126A7261 LINE BOEING737 737282 13844ATNM PWA JT8 JT8D17A 52049NE ENGINE OIL LEAKING A BJNAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP11344TM587 23044 NR 1 ENGINE LOST ENGINE OIL QUANTITY AND ILLUMINATED THE LOW OIL PRESSURE LIGHT. ENGINE WAS SHUTDOWN AND WIND MILLED APPROX 20 MIN. INSPECTION FOUND THE ENGINE GEARBOX P-5 PORT THREADS STRIPPED AND THE PORTS BANJO FITTING FOR THE OIL PRESSURE SWITCH LINE LEAKING OIL. INSTALLED A HELICAL COIL IAW SRM. INSPECTED CHIP DETECTORS AND OIL FILTER,, RAN ENGINE LEAK CHECKED OK. (K) 2L72 4F4 FRTA16WE E2EA 20050330001342005033000134NM 2005 3 30 BJNA050104 120050202A33506104781 BATTERY PACK BOEING737 737282 13844ATNM PWA JT8 JT8D17 52049NE EMERGENCY LIGHT DISCHARGED A BJNAK NONE L NO TEST ININSP/MAINT 1 WP11233TM 23043 DURING A MAINTENANCE WALK AROUND CHECK, THE AFT RT SERVICE DOOR (R2) EMERGENCY EXIT ESCAPE SLIDE LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REOMVED AND REPLACED THE BATTERY PACK FOR THE AFT RT SERVICE DOOR (R2 EMERGENCY EXIT SLIDE LIGHT IAW MM. EMERGENCY EXIT LIGHTS NOW OPERATE NORMALLY. (K) 2L72 4F4 FRTA16WE E2EA 20050330001352005033000135NM 2005 3 30 BJNA050101 120050108A33501619 BULB BOEING737 737282 13844ATNM PWA JT8 JT8D17 52049NE EMERGENCY LIGHT BURNED OUT A BJNAK NONE L NO TEST ININSP/MAINT 1 WP11344TM 23044 DURING A MAINTENANCE WALK AROUND CHECK, THE LT SERVICE DOOR L2 EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE LIGHT BULB OF THE L2 EMERGENCY EXIT LIGHT IAW MM. LIGHT NOW FUNCTIONS NORMALLY. (K) 2L72 4F4 FRTA16WE E2EA 20050330001362005033000136NM 2005 3 30 BJNA050102 120050121A33506104789 BATTERY PACK BOEING737 737282 13844ATNM PWA JT8 JT8D17 52049NE EMERGENCY LIGHT DISCHARGED A BJNAK NONE L NO TEST ININSP/MAINT 1 WP11344TM 23044 DURING A MAINTENANCE WALK AROUND CHECK, THE LT SERVICE DOOR L2 EMERGENCY EXIT LIGHT WOULD NOR ILLUMINATE. MAINTENANCE DISCOVERED THAT THE BATTERIES WERE DISCHARGED. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK OF THE L2 EMERGENCY EXIT LIGHT IAW MM. LIGHT NOW FUNCTIONS NORMALLY. (K) 2L72 4F4 FRTA16WE E2EA 20050330001382005033000138CE 2005 3 30 IMJ2005F00000 120050111A361065550393 ELBOW CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE BLEED AIR LINE RUPTURED E IMJAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA2515SK 5600395 AC FAILURE OF NR2 ENG OB BRAIDED BLEED AIR LINE. FAILURE HAPPENED ABOUT 5 MIN AFTER T/O, WHILE INITATING A CLIMB FROM 2000 FT TO 6000 FT. FIRE WARNING ANNUN ILLUMINATED, PWR WAS REDUCED, THE EMERGENCY CHECKLIST WAS INITIATED, EMERGENCY WAS DELCARED. UPON REDUCTION IN PWR, FIRE ANNUN EXTINGUISHED. UNEVENTFUL LANDING WAS MADE. MAINT FOUND RUPTURED OB BLEED AIR LINE (ELBOW). THIS LINE IS ACCORDION STYLE FLEX LINE COVERED BY WIRE BRADING WITH A 90 DEGREE FITTING AT ONE END, STRAIGHT (V) BAND TYPE FITTING ON OTHER. SIMILAR LINE ON THE OPPOSITE SIDE WAS INSPECTED, FOUND ALSO TO BE LEAKING. DUE TO BRAIDED COVERING IT IS IMPOSSIBLE TO SEE CRACKS UNLESS THIS LINE IS REMOVED AND EXAMINED FROM THE INSIDE. 2L72 4F4 FRTA22CE E25EA 20050330001572005033000157SO 2005 3 30 UG82005F00002 120050121A32601159SCAV5131 SQUAT SWITCH GULSTMGV GULFSTREAMGV3980116SO RROYCEBR700 BR700710A110 NE MLG CONTAMINATED E UG8AA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL235101 4017 550 GROUND SPOILER RED LIGHT CAME ON DURING TAKEOFF. ALSO HAD AMBER WOW FAULT. BLOW DRIED AND CLEANED LT AND RT MLG WEIGHT ON WHEEL SWITCHES AND CONNECTORS. FAULTS CLEARED AND AIRCRAFT RETURNED TO SERVICE. (GM05003) (K) 2L72 4F4 FRTA12EA E00057EN 20050328001972005032800197NM 2005 3 28 DHL2005745007 120050325A3260 SWITCH BOEING727 727224 1384076NM MLG DOOR OUT OF ADJUST A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01745DH 20665 ON GEAR RETRACTION OUT OF YYZ, RT GEAR DOOR LIGHT REMAINED ILLUMINATED ON S/O PANEL AND FRONT PANEL WITH GEAR HANDLE IN OFF POSITION. RECYCLED HANDLE WITH SAME RESULTS. PERFORMED GEAR DOOR WARNING LIGHT ILLUMINATED WITH GEAR HANDLE UP OR OFF, ABNORMAL PROCEDURE WITH GEAR HANDLE IN UP POSITION WITH LIGHT EXTINGUISHED ON APPROACH, CYCLED GEAR WITH SAME INDICATIONS. ADJUSTED RT MAIN GEAR DOOR SWITCH. OPS CHECKS GOOD IAW B727 MM 32-62-11, OKAY FOR CONTINUED SERVICE. 2L73 4F A3WE 20050328002072005032800207NM 2005 3 28 SWAA050888 120050322A53116547979 FRAME BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND FUSELAGE CHORD CRACKED AT BS 727, RBL 30. REPAIRED CHORD PER PAE ER. 2L72 4F RTA16WE 20050328002132005032800213SO 2005 3 28 SWIA200514760 120050207A5347 SEAT TRACK EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0758733 120197 LEFT OUTBOARD AFT SEAT TRACK CORRODED AT FR 39 TO FR.32 (SIDEWALL). ITEM FOUND AT C-CHECK INSPECTION. SEAT TRACK REPLACED IAW EMB 120 SRM 51-25-00, 51-22-00, 51-40-02. 2L72 4T RTA31SO 20050328002142005032800214EA 2005 3 28 COMA0560200 120050323A3320BR900022 BALLAST CNDAIRCL600 CL6002B19 1900309EA LIGHT INOPERATIVE A COMAO OTHER O OTHER NRNOT REPORTED 1 SO01971CA 7145 FLIGHT 5082 BURNING TYPE ODOR IN COCKPIT WHILE USING APU OR 10TH STAGE BLEED AIR. REPLACED THE FLIGHT ATTENDANT STATION LIGHTING BALLAST. 2L72 4F RTA21EA 20050329000072005032900007WP 2005 3 29 ASAA0580137 120050227A5230 SKIN DOUG DC9 DC983 3022083WP CARGO DOOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 OKC - HV-CHECK, MID CARGO BAY DOOR IS DENTED. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050329000252005032900025WP 2005 3 29 ASAA0580125 120050227A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 OKC - HV-CHECK, CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050329000292005032900029WP 2005 3 29 ASAA0580126 120050227A532199365831 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 OKC - HV-CHECK, FOUND CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050329000372005032900037EA 2005 3 29 A6WA200540096 120050313A5330601R3301066 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DENTED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31430AW 7719 RIGHT SIDE FORWARD FUSELAGE DAMAGED BELOW CO-PILOTS WINDOW. COMPLIED WITH FLUSH REPAIR IAW BOMBARDIER, INC REO 601R-53-00-061 REV A AND BRAS EO 601R-53-6107C. (M) 2L72 4F RTA21EA 20050329000462005032900046NM 2005 3 29 USAA050302 120050223A5315 FLOORBEAM BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19442US40275 24841 CLT - FOUND FLOORBEAM CORRODED 2 INCHES BY 101 INCHES, STATION 344 ENTIRE T-CAP. INSTALLED NEW SECTION OF FLOORBEAM PER SRM 53-10-51. (M) 2L72 4F RTA16WE 20050329000472005032900047NM 2005 3 29 USAA050332 120050220A5311 FRAME BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19438US 24560 PIT - FOUND FRAME CRACKED .25 INCH, STATION 616 FRAME JUST BELOW FLOOR. DOUBLER INSTALLED PER TYPICAL REPAIR 53-62-01. (M) 2L72 4F RTA16WE 20050329000512005032900051NM 2005 3 29 USAA050313 120050211A57401120260 ATTACH FITTING BOEING737 7373B7 1384580NM ACCESS PANEL CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU50570 23706 PIT - FOUND ATTACH RING CORRODED 1 INCH BY 20 INCH AREA, ACCESS PANEL NR 7405. DEFECTIVE PART REPLACED WITH IDENT PART PER AMM 57-00-00. (M) 2L72 4F RTA16WE 20050329000522005032900052NM 2005 3 29 USAA050323 120050211A554265C2584151 SKIN BOEING737 7373B7 1384580NM RUDDER DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU50570 23706 PIT - FOUND EXT COMPOSITE SURF WITH DELAMINATION 5 INCHES LONG BY .125 INCH WIDE SINGLE LAYER DAMAGE, RUDDER RT IDE 114 INCH FROM BOTTOM 7 INCH FROM T/E. INSTALLED REPAIR PLYS, SEALED AND REFINISHED PER SRM 51-70-17, EA 79999. (M) 2L72 4F RTA16WE 20050329000682005032900068NM 2005 3 29 USAA050304 120050223A5315 FLOORBEAM BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19442US40275 24841 CLT - FOUND FLOORBEAM CORRODED 101 INCH BY 2 INCH, STATION 312 ENTIRE T-CAP. INSTALLED NEW SECTION OF FLOORBEAM IAW SRM 53-10-51. (M) 2L72 4F RTA16WE 20050329000822005032900082SO 2005 3 29 SIMA200506604 120050301A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21801AE 145469 ABI - DURING AN IMBV INSPECTION, THE CENTER OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. PERFORMED A CUT OUT TO REMOVE CORROSION. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIRS DONE IAW EMB 145 SRM, SRM EMB-145/1142 REV 28, CHAPTER 53-22-10 FIG 201. (M) 2L72 4F RTT00011AT 20050329000902005032900090NM 2005 3 29 USAA050319 120050211A554265C2584151 SKIN PANEL BOEING737 7373B7 1384580NM RUDDER DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU50570 23706 PIT - FOUND COMPOSITE SKIN PANEL WITH DELAMINATION 3 INCH BY .0625 INCH SINGLE LAYER DAMAGE, 165 INCHES FROM BOTTOM, 13 INCHES FROM T/E RUDDER LT SIDE. INSTALLED REPAIR PLYS PER SRM 51-70-17, EA 79999. (M) 2L72 4F RTA16WE 20050329000952005032900095SO 2005 3 29 SIMA200506603 120050226A531514522460015 GUSSET EMB 135 EMB135KL 3260302SO FLOORBEAM CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21804AE 145487 SAW - DURING CPCP INSPECTION MAINTENANCE, FOUND THE GUSSET OVER LEFT OUTBOARD FLOORBEAM BETWEEN FRAMES 16-17 HAS CORROSION. INSTALLED NEW GUSSET IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050329001012005032900101EA 2005 3 29 A6WA200540102 120050316A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31413AW 7585 RIGHT CARGO FLOOR SUPPORT ANGLE AT FS 621 CRACKED .5 INCH LONG. (M) REMOVED CRACKED SECTION OF FLOOR SUPPORT ANGLE AT FS 621 RT AND INSTALLED REPAIR ANGLE IAW MDG REO. (K) 2L72 4F RTA21EA 20050329001182005032900118NM 2005 3 29 72300086 120050325A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 AREAS OF CORROSION: 5 X 2 INCH FROM STA 480 TO STA 485, 2 X 1 INCH FROM STA 560 TO STA 562, 10 X 2 INCH FROM STA 600 TO STA 610, 5 X 1 INCH FROM STA 655 TO STA 660. 2L73 4F4 FRTA3WE E2EA 20050329001522005032900152SO 2005 3 29 MASA200500177 120050303A532014521721009 BUTTSTRAP EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A MASAK NONE O OTHER ININSP/MAINT 1 SW07850MJ7322 145568 IN C-CHECK, BUTT STRAP AT BL 0 FROM FRAME 14-17 IS CORRODED. PART HAS BEEN REPAIRED IAW SRM 53-21-10. 2L72 4T RTT00011AT 20050329001582005032900158SO 2005 3 29 MASA200500198 120050309A2750 CONTROL SYSTEM EMB 145 EMB145LR 3260212SO TE FLAPS MALFUNCTIONED A MASAO OTHER J WARNING INDICATION APAPPROACH 1 SW07837MJ 145367 A FLAP FAIL ON APPROACH. CONTRACT MAINTENANCE WAS ABLE TO REST AND PERFORM OPERATIONAL TEST OF FLAP SYSTEM WITH NO DEFECTS NOTED. 2L72 4T RTT00011AT 20050329001742005032900174NM 2005 3 29 SB05040 120050327A33501012721 LIGHT BOEING737 7373B7 1384580NM SEAT 22C FAILED A USAAK NONE O OTHER ININSP/MAINT 1 EA19389US 23311 MAINTENANCE REPORTED THE LOW LEVEL SEAT MOUNTED EMERGENCY LIGHT AT ROW 10 ABC INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AT SEAT 10 ABC. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050329001832005032900183WP 2005 3 29 WX0500034 120050321A335060030431 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A WX0AK NONE O OTHER ININSP/MAINT 1 WP19862GA 49556 MAINTENANCE REPORTED EMERGENCY CEILING LIGHTS INOPERATIVE AFT CABIN FROM SEAT ROW 31 TO AFT LAVATORIES. MAINTENANCE REMOVED AND REPLACED AFT CABIN BATTERY PACK. SYSTEM OPERATIONALLY CHECKS GOOD IAW MM 33-53-00. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050329001852005032900185NM 2005 3 29 AWXA200500361 120050324A315035EN254 SWITCH BOEING737 73733A 1384673NM COCKPIT SHORTED A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28174AW 23633 PHX - ABORTED TAKEOFF - FLT 0506 - ON TAKEOFF AT PHX EN ROUTE TO YVR UPON ADVANCING THROTTLES AND BRAKE RELEASE THE TAKEOFF CONFIGURATION WARNING HORN SOUNDED, ALL EFFORTS TO SILENCE HORN FAILED. RETURNED TO GATE. MAINTENANCE FOUND STABILIZER NOSE UP SWITCH (S132) SHORTED. REPLACED AND ADJUSTED SWITCH (S132) IAW AMM 31-26-24, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050329001862005032900186NM 2005 3 29 AWXA200500362 120050314A5320654585567 WEB BOEING737 737375 13844BNNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 MCN - MAJOR REPAIR - DURING C-05 CHECK CORROSION WAS FOUND ON LOWER SURFACE OF R-2 DOOR SILL AFT WEB AT RBL 44, BETWEEN BS 988 AND BS 993, WL 208. MAINTENANCE CUT OUT DAMAGED R-2 DOOR SILL AFT WEB AT RBL 44, FROM BS 988 TO BS 993; FABRICATED A NEW REPLACEMENT WEB PER DWG 65-45855; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050329001912005032900191NM 2005 3 29 QXEA200500388 120050124A5320 DOOR FRAME BOMBDRDHC8 DHC8401 1390041NM ZONE 200 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - AFT FUSELAGE - AFT ENTRY DOOR SURROUND STRUCTURE FORWARD UPPER STOP FITTING GOUGED AT STATION 668.900 AND STRINGER 11P. REPAIRED IAW Q400 SRM 51-25-10-370-001 AND 51-25-15-370-001. 2H72 4T RTA13NM 20050329001932005032900193NM 2005 3 29 QXEA200500380 120050117A5320 STOP FITTING BOMBDRDHC8 DHC8401 1390041NM ZONE 200 CHIPPED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - PROTECTIVE COATINGS ON FORWARD BAGGAGE DOOR SURROUND STOP FITTING CHIPPED AND SCRATCHED. REPAIRED IAW DHC-8 400 SRM 51-14-00-800-801 AND SRM 51-14-00-350-803. 2H72 4T RTA13NM 20050329002112005032900211EU 2005 3 29 MALA050230 120050222A5230 SKIN SAAB SF340 340B 7860101EU CARGO DOOR DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15423XJ 340B423 DURING 4Y/2Y CHECK IN BNA FOUND CARGO DOOR IS DENTED IN THE LOWER AFT CORNER. THE DENTS ARE ACCEPTABLE AS IAW MESABA EOS52037. 2L72 4T RTA52EU 20050329002142005032900214EU 2005 3 29 MALA050226 120050204A3240 BRAKE SAAB SF340 340B 7860101EU MLG OVERHEATED A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 GL15414XJ 340B414 ON LANDING ROLL A/C PULLED TO THE RIGHT. POST FLIGHT NOTED LT O/B BRAKE SMOKING. REMOVED LT O/B WHEEL ASSY. INSPECTED WHEEL BEARING AXLE. CONFIRMED BRAKE ASSY ACTUATES. NO OBVIOUS DISCREPANCY NOTED. REINSTALLED WHEEL ASSY IAW JOB CARD 3240-301&302. OBSERVED CREW PERFORM HIGH SPEED TAXI. A/C DID NOT PULL LEFT OR RIGHT WHEN CAPT OR F/O PEDALS OPERATED INDEPENDENTLY. POST TAXI NOTED LT O/B BRAKE SMOKES. SUSPECT BRAKE LEAKS UNDER HIGH PSI. REMOVED AND REPLACED LT O/B ASSY IAW TASK CARD 3240-301. P/N ON/OFF 5012589-3, S/N ON JAN 97-0336, S/N OFF DEC01-0442. TAXI CHECK GOOD. BRAKES OPERATE NORMALLY. 2L72 4T RTA52EU 20050330000292005033000029 2005 3 30 UIEA200500004 420050126A25657A124836 SLIDE BOEING747 747212B 1384886NM GE CF6 CF650E2 30018NE CABIN FAILED A UIEAO OTHER L NO TEST NRNOT REPORTED 1 EA15808MC 21048 UPPER DECK EMERGENCY ESCAPE SLIDE DID NOT PROPERLY DEPLOY WHEN ACTIVATED. (EA15200503933) 2L74 4F4 F A20WE E23EA 20050330000402005033000040WP 2005 3 30 ASAA0580121 120050227A532199365651 FLOOR PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE CABIN DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 OKC HV-CHECK - CABIN FLOOR PANEL IS FEREL DAMAGED. REPLACED FLOOR PANEL. (K) 2L72 4F4 FRTA6WE E9NE 20050330000822005033000082CE 2005 3 30 G1I2005F00000 120050117A3210 LANDING GEAR BEECH 200 200BEECH 1152920CE PWA PT6 PT6A41 52043EA MALFUNCTIONED E G1IAA UNSCHED LANDING O OTHER LDLANDING 1 AL01204JS BB842 DURING TRAINING FLIGHT, THE LANDING GEAR WOULD NOT EXTEND NOR THE HANDLE LIGHT ILLUMINATE WHEN GEAR DOWN WAS SELECTED. GEAR WAS EXTENDED MANUALLY AND THE AIRCRAFT MADE A NORMAL LANDING. THIS CONDITION WAS ENCOUNTERED AFTER REPEATED GEAR EXTENSION/ RETRACTION DURING TRAINING FLIGHTS. A CONTRIBUTING FACTOR MAY BE THE -30 DEGREE F TEMPERATURES ENCOUNTERED. MAINTENANCE DISCOVERED THE 60 AMP BREAKER FOR THE EXTENSION/ RETRACT MOTOR LOCATED UNDER THE FLOOR POPPED. THE CONDITION COULD NOT BE DUPLICATED IN THE HEATED HANGER. AIRCRAFT RELEASED FOR SERVICE. 1L72 4T4 T A24CE E4EA 20050330000842005033000084NM 2005 3 30 S2YA04004 120050218A2421ALT3524 GENERATOR DORNERDO32 DO328300 NM PWA 306 PW306B NE LT AC FAILED A S2YAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL13351SK8814 3223 3108 DURING FLIGHT, THE CREW NOTED A CAS MESSAGE FOR LT AC GENERATOR FAIL AND WOULD NOT RESET. THE CREW CONSULTED MX AND DISPATCH. THE DECISION WAS MADE TO PERFORME AN AIR-TURN-BACK. UPON ARRIVAL IN MX, INSPECTED THE SYSTEM AND REPLACED THE LT AC GENERATOR. MX RETURNED THE AC TO SERVICE WITH NO FURTHER DEFECTS.(K) 2H72 4T4 FRTA55NM E35NE 20050330001102005033000110EU 2005 3 30 COE2005F00000 120050120A7797RK43337A WIRE HARNESS FOKKERF27 F27MK600 4990706EU RROYCEDART DART5327R 54509NE RT NACELLE INOPERATIVE A COEAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 NM13741FE 10387 NR 2 TGT FLUCUTATED BETWEEN 0 AND 600 DEGREES IN FLIGHT. AIRCRAFT RETURNED TO AIRPORT. NO EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. FOUND BROKEN WIRE ON CONNECTOR PLUG BACKSHELL AT FIREWALL. ENTIRE HARNESS WAS REPLACED. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2H72 4T4 T A817 E297 20050330001142005033000114EA 2005 3 30 REXA05002 120050101A2750855D10011 BPSU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FLAPS FAILED A REXAO OTHER J WARNING INDICATION CRCRUISE 1 SO258674A5291 7674 FLAPS FAILED AT ZERO AT FLIGHT LEVEL 310. QRH FOLLOWED, DECLARED EMERGENCY, UNEVENTFUL ZERO FLAPS LANDING MADE. SYSTEM WOULD NOT RESET. REPLACED RT BPSU (BRAKE POSITION SENSING UNIT) IAW AMM. OPERATIONALLY TESTED GOOD. (K) 2L72 4F4 FRTA21EA E15NE 20050330001152005033000115CE 2005 3 30 GUU2005F00001 120050114A3240 BRAKE ASSY BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE MLG MALFUNCTIONED A GUUAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO1717541 UE203 DURNG TAXI, LT AND RT BRAKES FEEL SPONGY. REQUIRES ADDITIONAL PRESSURE TO APPLY BRAKES. BELD ALL FOUR BRAKES. OPERATIONAL CHECK NORMAL. (K) 2L72 4T4 TRTA24CE E26NE 20050330001202005033000120NE 2005 3 30 GAIA05002OP 220050118A7261MS9021116 O-RING BOEING727 7272J0 138407ENM PWA JT8 JT8D15 52051NE NR 2 ENGINE DAMAGED A GAIAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW07284KH 21108 DURING CRUISE THE FLIGHT CREW SHUT DOWN THE NR 2 ENGINE DUE TO LOSS OF OIL QUANTITY AND PRESSURE. THE AIRCRAFT DIVERTED, AND MADE AN UNEVENTFUL LANDING. REMOVED AND REINSTALLED NR 2 ENGINE FUEL PUMP, REPLACED FUEL PUMP GARLOC SEAL AND SHAFT O-RING PACKING. OPS CHECK AND LEAK CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2L73 4F4 FRTA3WE E2EA 20050330001582005033000158CE 2005 3 30 UG82005F00003 120050120A323062171073 SPACER CESSNA650 650 2076802CE GARRTTTFE731TFE731* 01518WP UPLOCK HOOK MISSING D UG8AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL235117 6507064 LANDING GEAR UNLOCK LIGHT WOULD NOT EXTINGUISH WHEN RETRACTING. FOUND LT MAIN GEAR UPLOCK HOOK ACTUATOR MOUNTING ATTACH BOLT SPACER, PN 6217107-3 PREVIOUSLY NOT INSTALLED. REF. CE-650 IPC 32-30-00-02, ITEM 82. THIS CONDITION ALLOWED HORIZONTAL SHIFTING OF UPLOCK HOOK ACTUATOR DURING ACTUATION OF THE UPLOCK HOOK. INSTALLED NEW SPACER, PN 621707-3. PERFORMED LANDING GEAR OPERATIONAL CHECK. LANDING GEAR OPEATION CHECK IS SATISFACTORY IAW THE CE-650 MM. AIRCRAFT RETURNED TO SERVICE. (K) 2L72 4F4 F A9NM E6WE 20050330001672005033000167SO 2005 3 30 FPI2005F00002 220050113A8520 CONNECTING ROD BEECH 58 58 1152740CE CONT O520 IO520* 17032SO ENGINE LOOSE E FPIAK NONE O OTHER ININSP/MAINT 1 SO1593DF 3364 1676 TH61 299048R A MAIN BEARING IN THE ENGINE SPUN, CUTTING OFF OIL SUPPLY TO CONNECTING ROD NR 2 CYLINDER. CONNECTING ROD LET GO AND WENT THRU ENGINE CASE. ENGINE RETURNED TO MFG AS CORE. (K) 1L72 3O3 O 3A16 E5CE 20050330001732005033000173EU 2005 3 30 BMAC050003 120050128A3000037918811403 LINE BAG JETSTMJETSTM3101 1500215EU O2/METH MISLOCATED A B16AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO35525PA 666 PILOT REPORTED: LT MAIN LANDING GEAR IN TRANSION LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. FOUND LT MLG HANGING UP ON WATER METHANOL LINE. REPLACED LINE IAW AMM AND PERFORMED MLG SWINGS IAW AMM. OPS CHECKED GOOD AND LEAK CHECK, GOOD. (NE05200504537) (K) 2L72 4T RTA21EU 20050330001752005033000175WP 2005 3 30 DHL2005805579 120050318A5340 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FITTING CRACKED 0.500 STA 798.000 RBL 25. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21, SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. FABRICATED NEW FITTING (AL7075-T651) IAW DRAWING 4751820. PERFORMED NDT INSP IAW NDT SPM PART 08-00-02 TO 07. CLEANED, TREATED AND PRIMED AREA AND NEW FITTING IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050330001762005033000176CE 2005 3 30 DJFA2005071 120050328A3220 LANDING GEAR BEECH MU300 400A 1155402CE NOSE MALFUNCTIONED E DJFAO OTHER O OTHER DEDESCENT 1 EA23446CW RK346 CREW REPORTED THAT DURING DESCENT THROUGH FL 250 AT APPROXIMATELY 300 KTS THE NOSE GEAR EXTENDED AND LOCKED DOWN. THE CREW SLOWED THE AIRCRAFT TO 200 KTS AND EXTENDED THE GEAR. THE MAIN GEAR EXTENDED NORMALLY. A FLY-BY WAS PERFORMED SO TOWER COULD VISUALLY CONFIRM GEAR WAS DOWN. AIRCRAFT LANDED NORMALLY IN KBHM. 2H72 4F RTA16SW 20050330001772005033000177CE 2005 3 30 DJFA2005073 120050328A5610 WINDSHIELD BEECH 200 B200 1152922CE COCKPIT FAILED E DJFAO OTHER O OTHER CLCLIMB 1 EA23615TA BB1745 CREW REPORTED THAT THE RIGHT WINDSHIELD SHATTERED IN FLIGHT WHILE AIRCRAFT WAS CLIMBING THROUGH FL 210 TO 230. WINDSHIELD HEAT WAS ON AND OAT WAS 10 DEGREES CELSIUS. 1L72 4T A24CE 20050330001802005033000180NM 2005 3 30 72300108 120050328A5340 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050330001812005033000181NM 2005 3 30 72300107 120050328A5340 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 6 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050330001832005033000183NM 2005 3 30 72300105 120050328A5340 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 6 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050330001852005033000185NM 2005 3 30 72300103 120050328A5340 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 6 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050330001872005033000187NM 2005 3 30 72300101 120050328A5340 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 6 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050330001882005033000188NM 2005 3 30 72300100 120050328A5340 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 6 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050330001912005033000191NM 2005 3 30 72300097 120050323A5340 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 6 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050330001922005033000192NM 2005 3 30 72300096 120050323A5340 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X .5 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050330001942005033000194NM 2005 3 30 72300094 120050323A5340 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A .5 INCH X .5 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050330001982005033000198SO 2005 3 30 LR7A05037 120050327A532034319322 SUPPORT LKHEED382 382G 526414USO FUSELAGE DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03405LC 5025 DURING CARGO OFF LOADING AT RODN, CARGO COMPARTMENT FS 792 SUPPORT STRUT TUBE DAMAGED BY CARGO IMPACT AT WL 195, RBL 61. INSPECTED FOR SECONDARY DAMAGE, NONE NOTED. AIRCRAFT FERRIED UNPRESSURIZED TO RJTY. AT RJTY REPAIRED IAW SRM SMP 583 53-50-24. 2H74 4T A1SO 20050330002002005033000200SO 2005 3 30 LR7A05035 120050306A5311 FRAME LKHEED382 382G 526414USO FUSLEAGE MISDRILLED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2850 4763 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED / MIS-DRILLED FUSELAGE LINER HOLES AT FS 762E, WL 148, LBL 65. REPAIRED IAW LAC MEA 382-53-04-074 R1. 2H74 4T A1SO 20050330002012005033000201SO 2005 3 30 LR7A05034 120050306A5311 FRAME LKHEED382 382G 526414USO FUSELAGE MISDRILLED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2850 4763 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED / MIS-DRILLED FUSELAGE LINER HOLES AT FS 324E, WL 147, LBL 65. REPAIRED IAW LAC MEA 382-53-04-074 R1. 2H74 4T A1SO 20050330002052005033000205SO 2005 3 30 LR7A05030 120050306A5311 FRAME LKHEED382 382G 526414USO FUSELAGE MISDRILLED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2850 4763 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED / MIS-DRILLED FUSELAGE LINER HOLES AT FS 384, WL 148, LBL 65. REPAIRED IAW LAC MEA 382-53-04-074 R1. 2H74 4T A1SO 20050330002102005033000210SO 2005 3 30 LR7A05025 120050306A5311 FRAME LKHEED382 382G 526414USO FUSELAGE MISDRILLED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2850 4763 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED / MIS-DRILLED FUSELAGE LINER HOLES AT FS 807E WL 148 LBL 65. REPAIRED IAW LAC MEA 382-53-04-073 R1. 2H74 4T A1SO 20050330002112005033000211SO 2005 3 30 LR7A05024 120050306A5311 FRAME LKHEED382 382G 526414USO FUSELAGE MISDRILLED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2850 4763 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED / MIS-DRILLED FUSELAGE LINER HOLES AT FS 768E, WL 148, LBL 65. REPAIRED IAW LAC MEA 382-53-04-073 R1. 2H74 4T A1SO 20050330002132005033000213SO 2005 3 30 LR7A05022 120050306A5311 FRAME LKHEED382 382G 526414USO FUSELAGE MISDRILLED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2850 4763 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED / MIS-DRILLED FUSELAGE LINER HOLES AT FS 767, WL 152, RBL 66. REPAIRED IAW LAC MEA 382-53-04-073 R1. 2H74 4T A1SO 20050330002142005033000214SO 2005 3 30 LR7A05021 120050306A5311 FRAME LKHEED382 382G 526414USO FUSELAGE MISDRILLED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2850 4763 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED / MIS-DRILLED FUSELAGE LINER HOLES AT FS 747, WL 148, RBL 65. REPAIRED IAW LAC MEA 382-53-04-073 R1. 2H74 4T A1SO 20050330002152005033000215SO 2005 3 30 LR7A05020 120050306A5311 FRAME LKHEED382 382G 526414USO FUSELAGE MISDRILLED A LR7AK NONE W INADEQUATE Q C ININSP/MAINT 1 AL03404LC 2850 4763 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED / MIS-DRILLED FUSELAGE LINER HOLES AT FS 707, WL 148, LBL 65. REPAIRED IAW LAC MEA 382-53-04-073 R1. 2H74 4T A1SO 20050330002172005033000217SO 2005 3 30 LR7A05018 120050306A5311 FRAME LKHEED382 382G 526414USO FUSELAGE MISDRILLED A LR7AK NONE W INADEQUATE Q C ININSP/MAINT 1 AL03404LC 2850 4763 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED / MIS-DRILLED FUSELAGE LINER HOLES AT FS 667, WL 148, RBL 65. REPAIRED IAW LAC MEA 382-53-04-073 R1. 2H74 4T A1SO 20050330002182005033000218SO 2005 3 30 LR7A05017 120050306A5311 FRAME LKHEED382 382G 526414USO FUSELAGE MISDRILLED A LR7AK NONE W INADEQUATE Q C ININSP/MAINT 1 AL03404LC 2850 4763 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED / MIS-DRILLED FUSELAGE LINER HOLES AT FS 657, WL 175, LBL 77. REPAIRED IAW LAC MEA 382-53-04-073 R1. 2H74 4T A1SO 20050330002202005033000220SO 2005 3 30 LR7A05015 120050306A5311 FRAME LKHEED382 382G 526414USO FUSELAGE MISDRILLED A LR7AK NONE W INADEQUATE Q C ININSP/MAINT 1 AL03404LC 2850 4763 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED, MIS-DRILLED FUSELAGE LINER HOLES AT FS 637, WL 176, LBL 77. REPAIRED IAW LAC MEA 382-53-04-073 R1. 2H74 4T A1SO 20050330002232005033000223SO 2005 3 30 LR7A05012 120050306A5320 BEAM LKHEED382 382G 526414USO FUSLEAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2850 4763 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5321 FOUND CRACK ON RT BOW BEAM FS 557, WL 197, RBL 63. REPAIRED IAW SRM SMP 583 FIG 53-40-14. 2H74 4T A1SO 20050330002262005033000226SO 2005 3 30 LR7A05009 120050306A5312 BULKHEAD LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2850 4763 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND AFT FUSELAGE CARGO COMP BULKHEAD CRACKED AT RT FS 970, WL 280, RBL 15. REPAIRED IAW SRM SMP 583 FIG 53-50-06. 2H74 4T A1SO 20050330002282005033000228SO 2005 3 30 LR7A05007 120050306A5312 BULKHEAD LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2850 4763 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND AFT FUSELAGE INTERIOR BULKHEAD CRACKED AT FS 1020, WL 280 LBL 15. REPAIRED IAW SRM SMP 583 FIG 53-50-7. 2H74 4T A1SO 20050330002292005033000229SO 2005 3 30 LR7A05006 120050306A5320344555 FRAME LKHEED382 382G 526414USO WING TO BODY CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2850 4763 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5324 FOUND RT UPPER MLG WW WING TO FUSELAGE FAIRING FORMER CRACKED AT FS 522-528, WL 236, RBL 72. REPAIRED IAW LAC MEA 382-57-05-025. 2H74 4T A1SO 20050330002302005033000230SO 2005 3 30 LR7A05005 120050306A5330 SKIN LKHEED382 382G 526414USO FUSELAGE DENTED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2850 4763 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5321 FOUND BELLY SKIN SCRATCHED AND DENTED AT FS 297E - 345E, BL 40L - 40R. SKIN REPLACED FS 297E - 245E, BL 61L/R IAW SMP583 CHP 51-60 & 51-70. 2H74 4T A1SO 20050330002322005033000232NM 2005 3 30 EIA2005040 120050222A5314 KEELBEAM BOEING747 747SR46 1384816NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09478EV 21033 KEEL BEAM BS 1355-1365 LBL 10 WL 100 CORROSION. CORROSION REMOVED PER SRM 53-10-01, REPAIR FABBED AND INSTALLED PER ECRA 478-51-173-1. 2L74 4F RTA20WE 20050330002332005033000233NM 2005 3 30 EIA2005039 120050222A5314 KEELBEAM BOEING747 747SR46 1384816NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09478EV 21033 BS 1375-1380 WL 95-100 LBL 10 KEEL BEAM CORROSION. CORROSION REMOVED PER SRM 63-10-01, REPAIR PARTS FABBED AND INSTALLED PER ECRA 478-51-173-1. 2L74 4F RTA20WE 20050330002342005033000234NM 2005 3 30 EIA2005038 120050222A5313 STRINGER BOEING747 747SR46 1384816NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09478EV 21033 BS 2260 STR 43R INNER CHORD CRACK. DAMAGE REMOVED, REPAIR FABBED AND INSTALLED PER ECRA 478-51-173-1. 2L74 4F RTA20WE 20050330002352005033000235NM 2005 3 30 EIA2005037 120050222A5311 FRAME BOEING747 747SR46 1384816NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09478EV 21033 BS 1840 STR 11R FRAME CRACKED. DAMAGE REMOVED, FABBED AND INSTALLED REPAIR PER ECRA 478-51-173-1. 2L74 4F RTA20WE 20050330002382005033000238NM 2005 3 30 EIA2005034 120050222A5311 FRAME BOEING747 747SR46 1384816NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09478EV 21033 BS 1780 STR 13R FRAME CRACKED. DAMAGE REMOVED, REPAIR PARTS FABBED AND INSTALLED PER SRM 53-10-04. 2L74 4F RTA20WE 20050330002392005033000239NM 2005 3 30 EIA2005033 120050222A5311 FRAME BOEING747 747SR46 1384816NM FUSELAGE CRACKED A EIAAK NONE R PARTIAL RPM/PWR LOSS ININSP/MAINT 1 NM09478EV 21033 BS 880 LT STR 8L - 9L TENSION TIE FRAME CRACKED. DAMAGED AREA REMOVED, REPAIR FABBED AND INSTALLED PER ECRA 478-51-173-1. 2L74 4F RTA20WE 20050330002402005033000240NM 2005 3 30 EIA2005032 120050222A5340 STRINGER CLIP BOEING747 747SR46 1384816NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09478EV 21033 BS 800 STR 11L TENSION TIE CRACK. DAMAGE REMOVED, REPAIR FABBED AND INSTALLED PER ECRA 478-51-173-1. 2L74 4F RTA20WE 20050330002412005033000241NM 2005 3 30 EIA2005028 120050222A5315 FLOORBEAM BOEING747 747273C 1384896NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09471EV 20651 BS 420 UPPER FLOORBEAM TOP CHORD AT RBL 57 AND OUTBOARD HAS NUMEROUS (5) FASTENER HOLES WITH CRACK INDICATIONS (RBL 57.75, 58.25, 63, 67.5, AND 89.5). REMOVED AND REPLACED STA 420 FLOORBEAM UPPER CHORD DUE TO NUMEROUS CRACK INDICATIONS PER SERVICE BULLETIN 747-53A2429 P11. DRILLED PER B747 SRM 51-30-05 PAGES 6-9, ALODINED PER B747 SRM 51-10-02 PAGES 7-8 AND PRIMED PER BSOPM 20-41-02 PAGE 7-9. 2L74 4F A20WE 20050331000012005033100001WP 2005 3 31 DHL2005805555 120050320A5340 CLIP DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT CLIP WORN, STA 834.000 L-17R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-13-05 EO AST050220 DATE 03-08-05. REMOVED DAMAGED CLIP IAW SRM 51-1-21 PAGE 1. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. FABRICATED NEW CLIP (AL7075-T6 0.070) IAW EO AST050220. CLEANED, TREATED AND PRIMED AREA AND NEW CLIP IAW SRM 51-1-8B. INSTALLED NEW CLIP IAW EO AST 050220, SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050331000082005033100008 2005 3 31 ASAA0580091 420050210A25653961899501 LANYARD DOUG DC9 DC983 3022083WP L1 DOOR SLIDE BROKEN A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 OKC - HV-CHECK, FORWARD PAX (L-1) DOOR EMERGENCY EXIT SLIDE FAILED TO DEPLOY DURING TEST PER TASKCARD 28425002 STEP 2. THE CAUSE WAS DETERMINED TO BE A BROKEN GIRT BAR-TO-SLIDE COVER LATCH LANYARD. IT WAS BROKEN AT THE LATCH END. THE ENTIRE EMERGENCY SLIDE ASSEMBLY, INCLUDING THE DEFECTIVE LANYARD, WAS SHIPPED TO ASA ENGINEERING FOR REVIEW. A REPLACEMENT ASSEMBLY WAS INSTALLED ON AIRCRAFT. (M) 2L72 4F RTA6WE 20050331000322005033100032WP 2005 3 31 DHL2005805544 120050320A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT L-ANGLE FRAME HOLES (2EA) MISDRILLED, STA 920.000 BETWEEN L-12 AND L-13R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 02-28-05, EO AST 050206 DATE 02-24-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. FABRICATED NEW CLIP (AL7075-T6 0.080) IAW EO AST050206. CLEANED, TREATED AND PRIMED AREA (MISDRILLED HOLES) AND NEW CLIP IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (NAS1097AD). INSTALLED NEW CLIP IAW EO AST 050206, SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050331000342005033100034WP 2005 3 31 DHL2005805543 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT INBOARD FLANGE Z-FRAME HOLES (2EA) MISDRILLED AT STA 300.000 L-10L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-05-05, EO AST 050205 DATE 02-21-05. CLEANED, TREATED AND PRIMED AREA MISDRILLED HOLES IAW SRM 51-1-8B. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD5-6) IAW EO AST 050205, SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050331000352005033100035WP 2005 3 31 DHL2005805524 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT INBOARD FLANGE Z-FRAME HOLES (2EA) MISDRILLED AT STA 960.000, L-12, L-13L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-05-05 EO AST050205 DATE 02-21-05. CLEANED, TREATED AND PRIMED AREA MISDRILLED HOLES IAW SRM 51-1-8B. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD6-5) IAW EO AST050205, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050331000372005033100037EU 2005 3 31 05FDEA00671 120050328A5330 DOUBLER AIRBUS310 A310222 3930315EU FUSLEAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 REPAIR NEEDS EVALUATION FOR FAA APPROVED DATA AND MAJOR OF MINOR CLASSIFICATION. ITEM 12 ON LIST. FUSELAGE FLUSH ROUND DOUBLER LOWER LT SIDE FR35 INSTALLED NEW REPAIR IAW A310 SRM 53-10-12, AND A310 AMM 25-54-10-2, REPAIR IS CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100. 2L72 4F RTA35EU 20050331000382005033100038EU 2005 3 31 05FDEA00672 120050328A5347 SEAT TRACK AIRBUS310 A310222 3930315EU FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 AFTER REMOVAL OF SEAT TRACK NR 3 RT BETWEEN FRAMES 45-54. FOUND BRACE FITTING AT FRAME 47/48 ATTACH POINT CRACKED 1.2 INCH LONG ON INBOARD SIDE OF TRACK. REPAIRED IAW EA 6-5310-79122. 2L72 4F RTA35EU 20050331000392005033100039EU 2005 3 31 05FDEA00673 120050328A5542 SKIN AIRBUS310 A310222 3930315EU RUDDER MISREPAIRED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25419FE 345 REPAIR NEEDS EVALUATION FOR FAA APPROVED DATA AND MAJOR OR MINOR CLASSIFICATION. FLUSH REPAIR LT SIDE RUDDER LOWER T/E. ITEM 36 OF LIST. FLUSH REPAIR IS FOUND TO BE NOT CONFORM WITH A310-200 SRM 55-41-0. REMOVED IMPROPER REPAIR AND INSTALL PROPER REPAIR IAW A310-200 SRM 55-41-12 REPAIR 7. REINSTALLED LIGHTING STRIP A310-200 SRM 55-41-12 FIG 207. RESTORED SURFACE PROTECTION AFTER COMPOSITE WORK IAW A310-200 SRM 51-75-10. REPAIR IS CLASSIFIED AS MINOR IAW FEDEX GMM 6-2-100. 2L72 4F RTA35EU 20050331000402005033100040EU 2005 3 31 05FDEA00674 120050328A5330 SKIN AIRBUS310 A310222 3930315EU FUSLEAGE MISREPAIRED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25419FE 345 REPAIR NEEDS EVALUATION FOR FAA APPROVED DATA AND MAJOR OR MINOR CLASSIFICATION. ITEM NR 24 ON LIST. FUSELAGE DOUBLER LOWER RT SIDE AT FR70. REMOVED UNAPPROVED REPAIR IAW A310-200 SRM 51-40-21, INSTALLED NEW REPAIR IAW A310-200 SRM 53-10-12 FIG 224, REPAIR IS DETERMINED TO BE MINOR IAW FEDEX GMM 6-2-100. 2L72 4F RTA35EU 20050331000422005033100042WP 2005 3 31 DHL2005805545 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBOARD FLANGE (2EA) MISDRILLED HOLES STA 1400.000 L-12R TO L-13R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-07-05, EO AST 050201 DATED 02-17-05. PERFORMED DETAIL VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO AST050201, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050331000442005033100044WP 2005 3 31 DHL2005805578 120050318A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT (8EA) MISDRILLED HOLES IN L-12R STA 520.000 - 540.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-15-05 EO AST 050216 DATED 03-02-05. PERFORMED DETAIL VISUAL INSPECTION, NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO AST050216, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050331000452005033100045WP 2005 3 31 DHL2005805595 120050324A534056150402 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 MAIN CABIN INTERIOR FRAME FITTING CRACKED 3.500 STA 980.000 L-17R AND L-18R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FRAME FITTING IAW SRM 51-1-20D PG 21, SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FRAME FITTING (P/N 5615040-2) IAW SRM 51-1-20D PG 9, SRM 51-3-0 PG 1. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050331000462005033100046WP 2005 3 31 DHL2005805608 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSLEAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT INBOARD FLANGE Z-FRAME HOLES (3EA) MISDRILLED AT STA 300.000 L-17L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-05-05 EO AST 050205 DATE 02-21-05. CLEANED, TREATED AND PRIMED (AREA) MISDRILLED HOLES IAW SRM 51-1-8B. PERFORMED DETAILED VISUAL INSPECTION, NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO AST 050205, SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050331000482005033100048WP 2005 3 31 DHL2005805557 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBOARD FLANGE HOLES (2EA) MISDRILLED AT STA 1500.000 L-12 L-13R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-07-05, EO AST 050201 DATE 02-17-05. PERFORMED DETAILED VISUAL INSPECTION, NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO AST050201, SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050331000492005033100049WP 2005 3 31 DHL2005805526 120050319A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBOARD FLANGE (2EA) MISDRILLED HOLES, STA 1500.000 L-9L L-10L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-05-05, EO AST050205 DATED 02-21-05. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA AT STA 1500.000 L-10L IAW SRM 51-1-8B. PERFORMED DETAIL VISUAL INSPECTION NO CRACK FOUND, REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD6-4) IAW EO AST050205, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050331000502005033100050NM 2005 3 31 05FDEA00663 120050328A5311 FRAME BOEING727 727200 138407ENM FUSELAGE MISDRILLED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25481FE 21463 FOUND STUB FRAME BS 985 RT SIDE TO BE MISDRILLED AND CRACKED AT TWO SHEAR TIE LOCATIONS. REMOVED AND REPLACED STUB FRAME AT BS 985 PER SRM 51-30-02. 2L73 4F RTA3WE 20050329001212005032900121NM 2005 3 29 72300089 120050325A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 20 X 3 INCH AREA OF CORROSION ON ENTIRE STRINGER FROM STA 500 TO STA 520. 2L73 4F4 FRTA3WE E2EA 20050329001362005032900136NM 2005 3 29 SWAA050919 120050325A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747 + 2, STR 24R. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050329001412005032900141NM 2005 3 29 SWAA050924 120050325A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 777, STR 24L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050329001432005032900143NM 2005 3 29 SWAA050926 120050326A53306545776 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29683SW 24008 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 970, STR 18L. REPAIRED PER SWA EA & SRM. 2L72 4F RTA16WE 20050329001512005032900151SO 2005 3 29 MASA200500176 120050303A521014522460015 GUSSET EMB 145 EMB145LR 3260212SO PAX DOOR CORRODED A MASAK NONE O OTHER ININSP/MAINT 1 SW07850MJ7322 145568 IN C-CHECK, GUSSET AT PAX DOOR OPENING IS CORREDED AND HAS BEEN REPLACED IAW SRM 51-40-02. 2L72 4T RTT00011AT 20050329001552005032900155SO 2005 3 29 MASA200500180 120050303A532014521725651 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A MASAK NONE O OTHER ININSP/MAINT 1 SW07850MJ7322 145568 IN C-CHECK, SILL ASSEMBLY JUST FWD OF SERVICE DOOR IS CORRODED AND WILL BE REPLACED IAW SRM 51-40-02. 2L72 4T RTT00011AT 20050329001702005032900170SO 2005 3 29 MASA200500223 120050316A335020131A BATTERY PACK EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSINOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07845MJ 145502 THE LT OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOP. THE LIGHT WAS PLACED ON MEL AND THE A/C DEPARTED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED POWER SUPPLY. 2L72 4T RTT00011AT 20050329001722005032900172NM 2005 3 29 20051 120050317A2910NAS16128 PACKING DHAV DHC8 DHC8103 1386005NM HYD LINE CUT A KPVAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 WP13805WP 353 NR 1 HYD SYSTEM FAILURE (ISO VALVE). CAUTION PANEL DID NOT HAVE NR 1 ISO VALVE CAUTION LIGHT, ONLY A LINE. EMERGENCY LANDING OGG. ENGINE SHUT DOWN ON RUNWAY. INSPECTED NR 1 HYD SYSTEM FOR LEAKS AND FOUND LT OUTER WING FITTING REDUCER PACKING RIPPED. REMOVED & REPLACED LT OUTER WING FITTING REDUCER PACKING AS REQUIRED. FOR NR 1 ISO VALVE CAUTION LIGHT WITH ONLY A LINE, C/W WALKAROUND INSPECTION AND HAVE DETERMINED THIS AIRCRAFT TO BE IN A SAFE CONDITION FOR A FERRY FLIGHT FROM OGG TO HNL ONLY IAW GMM PG 4.7 TO 4.10. REMOVED A BLANK FILTER AS MOD 8/1985 NOT INCORPORATED ON THIS AIRCRAFT. INSTALLED NR 1 HYD ISO VLV CAUTION LIGHT FILTER IN PROPER LOCATION PER DHC 8 MM 33-12-01 PG 4. OPS CHECK GOOD. 2H72 4T RTA13NM 20050329001752005032900175WP 2005 3 29 WX05000343 120050321A335060030431 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A WX0AK NONE O OTHER ININSP/MAINT 1 WP19862GA 49556 MAINTENANCE REPORTED EMERGENCY CEILING LIGHTS INOPERATIVE AFT CABIN FROM SEAT ROW 31 TO AFT LAVATORIES. MAINTENANCE REMOVED AND REPLACED AFT CABIN BATTERY PACK. SYSTEM OPERATIONALLY CHECKS GOOD IAW MM 33-53-00. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050329001882005032900188SO 2005 3 29 SWIA200514762 120050207A5320 INTERCOSTAL EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0758733 120197 INTERCOSTAL AT FRAME 40 BETWEEN CENTER AND RT FLOORBEAMS IS CORRODED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED INTERCOSTAL IAW EMB SRM 51-40-02. 2L72 4T RTA31SO 20050329001922005032900192NM 2005 3 29 QXEA200500389 120050203A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 100 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - FUSELAGE EXTERNAL SKIN RIGHT SIDE STATION X112.5 AND STRINGER 20 HAS TWO DENTS. REPAIRED IAW Q400 RD 8/4-53-1144 AND HORIZON AIR EA 6-53-512. 2H72 4T RTA13NM 20050329002182005032900218 2005 3 29 380WL0003 420050305A2230 CABLE BOEING737 7373G7 1384595NM AUTOTHROTTLES OUT OF RIG A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05380WL 23218 AUTOTHROTTLE KICKS OFF DURING FLIGHT. RIGGED LEFT THROTTLE FLEX CABLE PER MM 76-11-00. AUTOTHROTTLE CHECKS GOOD. 2L72 4F RTA16WE 20050329002202005032900220EU 2005 3 29 05FDEA00508 120050314A5512 FAIRING AIRBUS310 A310222 3930315EU HORIZONTAL STAB DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 REPAIR NEEDS EVALUATION FOR FAA APPROVED DATA AND MAJOR OR MINOR CLASSIFICATION, FLUSH REPAIR LT HORIZONTAL STAB L/E FAIRING 331CB L/E OUTBOARD END. THIS REPAIR ON THE LT HORIZONTAL STAB L/E FAIRING 331CB WAS FOUND TO BE IAW A310-200 SRM 55-12-12, FIG 201. CLASSED AS A MINOR REPAIR PER FEDEX GMM 6-2-100, AND IS NOT BOUND BY ANY REPETITIVE INSPECTION REQUIREMENTS. (OPEN) 2L72 4F RTA35EU 20050330001842005033000184NM 2005 3 30 72300104 120050328A5340 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 6 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050330002062005033000206SO 2005 3 30 LR7A05029 120050306A5311 FRAME LKHEED382 382G 526414USO FUSELAGE MISDRILLED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2850 4763 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED / MIS-DRILLED FUSELAGE LINER HOLES AT FS 364, WL 148, LBL 65. REPAIRED IAW LAC MEA 382-53-04-074 R1. 2H74 4T A1SO 20050330002072005033000207SO 2005 3 30 LR7A05028 120050306A5311 FRAME LKHEED382 382G 526414USO FUSELAGE MISDRILLED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2850 4763 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED / MIS-DRILLED FUSELAGE LINER HOLES AT FS 323, WL 148, LBL 65. REPAIRED IAW LAC MEA 382-53-04-074 R1. 2H74 4T A1SO 20050330002162005033000216SO 2005 3 30 LR7A05019 120050306A5311 FRAME LKHEED382 382G 526414USO FUSLEAGE MISDRILLED A LR7AK NONE W INADEQUATE Q C ININSP/MAINT 1 AL03404LC 2850 4763 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED / MIS-DRILLED FUSELAGE LINER HOLES AT FS 687, WL 148, RBL 65 AND LBL 65. REPAIRED IAW LAC MEA 382-53-04-073 R1. 2H74 4T A1SO 20050330002192005033000219SO 2005 3 30 LR7A05016 120050306A5311 FRAME LKHEED382 382G 526414USO FUSELAGE MISDRILLED A LR7AK NONE W INADEQUATE Q C ININSP/MAINT 1 AL03404LC 2850 4763 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED / MIS-DRILLED FUSELAGE LINER HOLES AT FS 647, WL 148, LBL 65. REPAIRED IAW LAC MEA 382-53-04-073 R1. 2H74 4T A1SO 20050330002242005033000224SO 2005 3 30 LR7A05011 120050306A5343 FITTING LKHEED382 382G 526414USO NLG CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2850 4763 DURING SCHEDULED C5 INSPECTION PER JOB CARD HST5301 FOUND CRACK ON NLG FWD DOOR ASSY LT HINGE FITTING AT FS 165. REPAIRED IAW LAC MEA 382-53-05-027. 2H74 4T A1SO 20050330002372005033000237NM 2005 3 30 EIA2005035 120050222A5340 STRINGER CLIP BOEING747 747SR46 1384816NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09478EV 21033 BS 820 LT TENSION TIE CRACKED STR 10AL - 10L. DAMAGE REMOVED, FABBED AND INSTALLED REPAIR PER ECRA 478-51-173-1. 2L74 4F RTA20WE 20050331000412005033100041WP 2005 3 31 DHL2005805643 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBOARD FLANGE (1EA) HOLE MISDRILLED AT STA 600.000 L-12.5R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-07-05 EO AST 050201 DATE 02-17-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLE WITH RIVET (MS20470AD) IAW EO AST 050201 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050331000472005033100047WP 2005 3 31 DHL2005805546 120050303A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 FWD ACCY COMPT FRAME CRACKED 3.000 AT STA 55.000 L-23L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 2, TR 53-110, TR 53-125, SRM 53-3-3 FIG 3. REMOVED FASTENERS IAW SRM 51-1-20D PAGE 21, SRM 51-1-21 PG 1. CUT OUT DAMAGED SECTION AND FABRICATED NEW FRAME SEGMENT(AL 7075.0 0.071) AND SPLICE DOUBLERS 2EA (AL7075 0 0.071) IAW SRM 53-2-0 FIG 2 SHEET 5, 6, 7, 8 SRM 53-3-3 FIG 3, SRM 51-1-4 PG 1. HEAT TREATED IAW SRM 51-1-1 PG 1-13-17. PERFORMED NDT INSP IAW NDT SPM PART 06-10-01-001. NO CRACK FOUND. CLEANED, TREATED AND PRIMED REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SRM 53-2-0 FIG 2 SHEET 5, 6, 7, 8. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050331000512005033100051EU 2005 3 31 05FDEA00664 120050328A5414 PANEL AIRBUS310 A310222 3930315EU NR 2 NACELLE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 REPAIR NEEDS EVALUATION FOR FAA APPROVED DATA AND MAJOR OR MINOR CLASSIFICATION. NR 2 ENGINE NACELLE ENGINE EXHAUST TO NACELLE TRANSITION PANEL 30 INCHES FWD OF AFT. ITEM 46 OF LIST. REMOVED DOUBLER IAW A310-200 SRM 51-4-21 TO EVALUATE REPAIR FOR SRM CONFORMANCE AND DETERMINE MAJOR/MINOR REPAIR CLASSIFICATION, REINSTALLED DOUBLER IAW A310-200 SRM 51-40-21 AND EA 6-5480-87206. 2L72 4F RTA35EU 20050331000522005033100052EU 2005 3 31 05FDEA00665 120050328A5311 FRAME AIRBUS310 A310222 3930315EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 A/C COMPARTMENT FRAME 42, 5 O'CLOCK POSITION FRAME IS CORRODED. REMOVED CORROSION AND REPAIRED FR 42 AT 5 O'CLOCK POSITION IAW EA 6-5310-87135. 2L72 4F RTA35EU 20050331000552005033100055NM 2005 3 31 05FDEA00679 120050328A5340AAA70881 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CAC - LONGERON SPLICE 51L, FOUND CRACKED AT STA 6-80. REMOVED AS PER SRM 51-33-01 VOL II. FABRICATED IAW DRAWING NR AAA7088. FABRICATED PART INSTALLED IAW SRM 51-33-01 VOL II AND FEDEX EA 1-5310-83095. 2L73 4F RTA22WE 20050331000572005033100057NM 2005 3 31 05FDEA00681 120050328A5347ADA83901 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 MAIN DECK, SEAT TRACK RBL 27.5 FOUND WITH SCRATCHES AT STA 758. CARRIED OUT REPAIR IAW SRM 53-70-00 FIGURE 1 VOLUME I. 2L73 4F RTA22WE 20050331000582005033100058NM 2005 3 31 05FDEA00682 120050328A5347ADA83891 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 MAIN DECK, SEAT TRACK LBL 47.5 FOUND WITH SCRATCHES AT STA 936. CARRIED OUT REPAIR IAW SRM 53-70-00 FIGURE 1 VOLUME I. 2L73 4F RTA22WE 20050331000602005033100060NM 2005 3 31 05FDEA00683 120050328A5347AEA73256 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 MAIN DECK, SEAT TRACK RBL 47.5 CORRODED AT STA 1401. CARRIED OUT REPAIR IAW SRM 53-70-00 VOLUME I FIGURE 1. 2L73 4F RTA22WE 20050331000612005033100061EA 2005 3 31 COMA0560209 120050326A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01494CA 7765 FLIGHT 5045 EN ROUTE YHZ-BOS RECEIVED A T/R UNLOCK MESSAGE, CREW DECLARED AN EMERGENCY AND DIVERTED TO BGR. AIRCRAFT LANDED WITHOUT INCIDENT. DEFERRED THE LEFT THRUST REVERSER PER MEL 78-30-01. 2L72 4F RTA21EA 20050331000622005033100062EA 2005 3 31 COMA0560210 120050325A77004033T65P03 SENSOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE RT ENGINE FAULTY A COMAC ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 SO01735CA16310 7267 FLIGHT 5065 DURING TAKEOFF ROLL THE RIGHT ENGINE WOULD NOT SPOOL ABOVE 30 PERCENT N1, ABORTED T/O AND RETURNED TO THE GATE. REPLACED THE RIGHT ENGINE T2 SENSOR. 2L72 4F4 FRTA21EA E15NE 20050331000662005033100066WP 2005 3 31 0500409869 120050327A272025878650 COMPUTER DOUG DC9 DC951 3022051WP RUDDER MALFUNCTIONED A NWAAO OTHER F FLT CONT AFFECTED TOTAKEOFF 1 GL01778NC53953777 48100 DURING TAKEOFF CLIMB AFTER GEAR RETRACTION, THE CREW EXPERIENCED FULL THROW RUDDER DEFLECTIONS. AIRCRAFT WAS DIFFICULT TO CONTROL UP THROUGH 6000 FEET AND THEN, PER COM, THE YAW DAMPER WAS TURNED OFF AND CREW ASSUMED MANUAL RUDDER CONTROL. AIRCRAFT PERFORMED WELL IN MANUAL AND FLIGHT RETURNED TO AN UNEVENTFUL LANDING BACK TO MSP. MAINTENANCE REPLACED THE STABILIZER AUGMENTATION COMPUTER, THE YAW DAMPER ACTUATOR, AND THE RUDDER POWER PACK. RUDDER RIGGING WAS CHECKED AND A TEST FLIGHT WAS COMPLETED AS SATISFACTORY. 2L72 4F RTA6WE 20050331000672005033100067EU 2005 3 31 0500393239 120050327A2120 SMOKE AIRBUS320 A320212 3930322EU COCKPIT DETECTED A NWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 GL01339NW 367 SMOKE ODOR WAS DETECTED DURING DESCENT. DECLARED AN EMERGENCY AND LANDED UNEVENTFULLY AT MEM. REPLACED THE NR 1 FORWARD OVEN AND CLEANED VENTILATION FILTER BEND NR 2 FORWARD OVEN. OBSERVED SMOKE AT AFT LOWER CORNER OF FIRST OFFICER'S SLIDING WINDOW. REPLACED NR 2 WINDOW HEAT COMPUTER BUT SMOKE WAS STILL PRESENT AT THE SLIDING WINDOW. APPLIED MEL PROVISIONS AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA28NM 20050331000692005033100069NM 2005 3 31 05FDEA00685 120050328A5347AFA7795505 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 MAIN DECK, SEAT TRACK AT 47.5 CORRODED AT STA 1581. CARRIED OUT REPAIR IAW SRM 53-70-00 VOLUME I FIGURE 1. 2L73 4F RTA22WE 20050331000702005033100070NM 2005 3 31 05FDEA00686 120050328A5347AFA7795505 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 MAIN DECK, SEAT TRACK 47.5 FOUND CORRODED AT STA 1605. CARRIED OUT REPAIR IAW SRM 53-70-00 VOLUME I FIGURE 1. 2L73 4F RTA22WE 20050331000712005033100071NM 2005 3 31 05FDEA00687 120050328A5347AFA7740503 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 MAIN DECK, SEAT TRACK LBL 75 CORRODED AT STA 1608. FOUND WITHIN LIMIT AS PER SRM 53-70-00 VOLUME I FIGURE 3. REWORKED AREA PROTECTED AND PAINTED AS PER SRM 51-21-01 VOLUME II. 2L73 4F RTA22WE 20050331000732005033100073NM 2005 3 31 05FDEA00689 120050328A5347AFA7795505 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 MAIN DECK, SEAT TRACK 47.5 CORRODED AT STA 1661 TO STA 1751. REPAIRED IAW SRM 53-70-00 FIGURE 1 VOLUME I. 2L73 4F RTA22WE 20050331000742005033100074NM 2005 3 31 05FDEA00690 120050328A5347AFA7795505 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 MAIN DECK, SEAT TRACK RBL 47.5 CORRODED AT STA 1885. CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II. 2L73 4F RTA22WE 20050331000762005033100076WP 2005 3 31 DHL2005805612 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBOARD FLANGE (2EA) MISDRILLED HOLES STA 1480.000 L-10L L-9L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-05-05 EO AST 050205 DATED 02-21-05. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. PERFORMED DETAIL VISUAL INSPECTION NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD5-4) IAW EO AST 050205 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050331000802005033100080WP 2005 3 31 DHL2005805650 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME (1EA) MISDRILLED HOLE AT STA 500.000 L-10R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-07-05 EO AST 050201 DATE 02-17-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLE WITH RIVET (MS20470AD) IAW EO AST 050201 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050331000812005033100081WP 2005 3 31 DHL2005805663 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBOARD FLANGE (2EA) MISDRILLED HOLES, STA 1320.000 L-10L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-05-05 EO AST 050205 DATE 02-21-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED MISDRILLED HOLES PLUGGING WITH RIVETS (MS20470AD5-4) IAW EO AST 050205 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050331000822005033100082WP 2005 3 31 DHL2005805644 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBOARD FLANGE (1EA) HOLE MISDRILLED STA 540.000 L-12R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-07-05 EO AST 050201 DATE 02-17-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED (MISDRILLED HOLE) AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLE WITH RIVET (MS20470AD) IAW EO AST 050201 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050331000832005033100083WP 2005 3 31 DHL2005805670 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME (2EA) MISDRILLED HOLES AT STA 620.000 L-10L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-05-05 EO AST 050205 DATE 02-21-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD5-6) IAW EO AST 050205 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050331000852005033100085WP 2005 3 31 DHL2005805682 120050320A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME HOLES (4EA) MISDRILLED STA 902.000 L-10R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 02-25-05 EO AST 050207 DATE 02-19-05. FABRICATED DOUBLER STRAP (AL7075T6 0.250) IAW EO AST 050207. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA AND DOUBLER STRAP IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (NAS1091AD) INSTALLED DOUBLER STRAP (NEW) IAW EO AST 050207, SRM 51-1-21 PAGE 1 (MS20470AD). 2L74 4F RT4A25 20050331000872005033100087WP 2005 3 31 DHL2005805523 120050313A57403645611U BRACKET DOUG DC8 DC873F 302199FWP BOOST PUMP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 NR 4 ALT TANK BOOSTER PUMP BRACKET CRACKED (FWD). REMOVED CRACKED BRACKET IAW SRM 51-1-20D PG 21. INSTALLED NEW BRACKET TO NR 4 ALT TANK BOOSTER PUMP IAW SRM 51-1-20D PG 9. TORQUED HI-LOKS IAW SRM 51-3-1 TABLE II. 2L74 4F RT4A25 20050331000882005033100088WP 2005 3 31 DHL2005805662 120050321A53133779658U502 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 LONGERON END FITTINGS, LONGERON BATHTUB FITTING CRACKED 2.000 STA 902.000 L-10L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PAGE 1. REMOVED BATHTUB FITTING (DAMAGED) IAW SRM 51-1-20D PAGE 21, SRM 51-3-0 PAGE 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW BATHTUB FITTING (P/N 3779658U502) IAW SRM 51-1-20D PAGE 9, SRM 51-3-0 PAGE 1, SRM 51-1-23. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050331000922005033100092WP 2005 3 31 DHL2005805664 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME (2EA) MISDRILLED HOLES AT STA 540.000 L-10R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-07-05 EO AST 050201 DATE 02-17-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO AST 050201 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050331000942005033100094WP 2005 3 31 DHL2005805666 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT INBOARD FLANGE J-FRAME (1EA) HOLE MISDRILLED AT STA 1000.000 L-10L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 02-25-05 EO AST 050203 DATE 02-28-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO AST 050203 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050331000962005033100096WP 2005 3 31 DHL2005805651 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBOARD FLANGE (2EA) MISDRILLED HOLES AT STA 1340.000 L-10R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-07-05 EO AST 050201 DATE 02-17-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO AST 050201 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050331000972005033100097EA 2005 3 31 SWIA200514787 120050322A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07440SW5445 5445 7589 RIGHT SPOILERON FAULT MESSAGE. REMOVED AND REPLACED RIGHT INBOARD PCU OF RIGHT SPOILERON IAW CRJ 600 MM 27-62-01, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050331000992005033100099EA 2005 3 31 SWIA200514789 120050323A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07439SW 7578 AFT OVERHEAD EMERGENCY LIGHT INOP. RELAMPED AFT OVERHEAD EMERGENCY LIGHT, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050331001002005033100100SO 2005 3 31 SWIA200514790 120050322A3350 LAMP EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07580SW 120348 ONE OF TWO RED EMERGENCY FLOOR PATH LIGHTING ARE INOPERATIVE AT THE FORWARD DOOR. RELAMPED FORWARD RED EMERGENCY FLOOR PATH LIGHTING. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050331001022005033100102EA 2005 3 31 SWIA200514792 120050327A2750860D10018ABCD CONTROLLER CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED APAPPROACH 1 NM07917SW 7641 FLAPS HALF SPEED ON APPROACH WHEN SELECTING FROM FLAPS 30-45 DEGREES. REPLACED FECU IAW MM 27-51-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050331001032005033100103EA 2005 3 31 SWIA200514793 120050326A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07906SW 7510 CEILING EMERGENCY LIGHT NR 3 INOPERATIVE. RELAMPED CEILING EMERGENCY LIGHT NR 3 IAW CRJ 200 MM 33-51-16. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050331001042005033100104SO 2005 3 31 SWIA200514794 120050324A3350 BULB EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07218SW 120287 F/A REPORTS RED FLOOR EMERGENCY LIGHT BURNT OUT. REPLACED BULB FOR FLOOR EMERGENCY LIGHT AS REQUIRED, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050331001052005033100105WP 2005 3 31 DHL2005805652 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBOARD FLANGE MISDRILLED HOLE, STA 1480.000 L-13R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-07-05 EO AST 050201 DATE 02-17-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLE WITH RIVET (MS20470AD) IAW EO AST 050201 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050331001062005033100106WP 2005 3 31 DHL2005805665 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT INBOARD FLANGE J-FRAME HOLES (2EA) MISDRILLED AT STA 980.000 L-10L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 02-25-05 EO AST 050203 DATE 02-18-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO AST 050203 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050331001072005033100107WP 2005 3 31 DHL2005805653 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO INTERIOR FRAME INBOARD FLANGE HOLES (2EA) MISDRILLED STA 1240.000 BETWEEN L-12 AND L-13R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-07-05 EO AST 050201 DATE 02-17-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO AST 050201 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050331001092005033100109WP 2005 3 31 DHL2005805655 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBOARD FLANGE (1EA) HOLE MISDRILLED STA 620.000 L-12R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-07-05 EO AST 050201 DATE 02-17-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLE WITH RIVET (MS20470AD) IAW EO AST 050201 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050331001112005033100111EA 2005 3 31 SWIA200514795 120050322A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07943SW 7762 EMERGENCY LIGHT AT ROW 2 INOPERATIVE. RELAMPED EMERGENCY LIGHT AT ROW 2. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050331001132005033100113NM 2005 3 31 0500385521 120050209A5320 PLATE BOEING757 757251 1384970NM FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01521US 23209 DURING H-CHECK FOUND CORROSION ON THE UPPER SURFACE OF AFT DECK PLATE BS 1708 TO 1720 LBL 60 TO RBL 60. REPAIRED PER EA 55-202110. 2L72 4F RTA2NM 20050331001142005033100114WP 2005 3 31 DHL2005805679 120050320A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME HOLES (4EA) MISDRILLED 0.1875, STA 902.000 L-9 L-10L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-09-05 EO AST 050208 DATE 02-21-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. FABRICATED DOUBLER STRAP (AL7075T6 0.250) IAW EO AST050208. CLEANED, TREATED AND PRIMED AREA AND NEW DOUBLER STRAP IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (NAS1097AD6). INSTALLED DOUBLER STRAP IAW EO AST 050208 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050331001152005033100115WP 2005 3 31 DHL2005805680 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT Z-FRAME INBOARD FLANGE HOLES (2EA) MISDRILLED AT STA 240.000 L-12 L-13L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-05-05 EO AST 050205 DATE 02-21-05. PERFORMED DETAILED VISUAL INSPECTION, NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD6-5) IAW EO AST 050205 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050331001162005033100116WP 2005 3 31 DHL2005805624 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBOARD FLANGE HOLES (2EA) MISDRILLED AT STA 1400.000 L-12 AND L-13L. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-05-05 EO AST 050205 DATE 02-21-05. CLEANED, TREATED AND PRIMED (AREA) MISDRILLED HOLES IAW SRM 51-1-8B. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD 6-4) IAW EO AST 050205 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050331001172005033100117WP 2005 3 31 DHL2005805625 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME (2EA) MISDRILLED HOLES AT STA 600.000 L-10L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-05-05 EO AST 050205 DATED 02-21-05. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA AT STA 600.000 L-10L IAW SRM 51-1-8B. PERFORMED DETAIL VISUAL INSPECTION. NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD 5-6) IAW EO AST050205 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050331001182005033100118SO 2005 3 31 21200003002 120050201A24343656624R ALTERNATOR PIPER PA32 PA32300 7103212SO LYC O540 IO540K1A5 41532EA HARTZLHCC2Y HCC2YK2 GL ENGINE FOULED E Z8TAO OTHER J WARNING INDICATION CRCRUISE 1 WP134127R45 5 3240455 RL711148 CH35895B ON APPROACH, ELECTRICAL POWER LOSS. AFTER CONTACT WITHTOWER, COMM 1 RADIO TURNED OFF, WITHIN 3-5 SEC C/B FOR ALTERNATOR OUTPUT TRIPPED & INSTRUMENT PANEL LIGHTS DIMMED, AMP GAUGE SHOW DISCHARGE OF BATTERY. TURNED OFF NON ESSENTIAL ELECTRICAL EQUIPMENT & RESET C/B & C/B POPPED BACK OUT. LT C/B OUT & ATTEMPTED RECYCLE COMM 1, TRANSMIT BUT NOT RECEIVE, LOW BATTERY. NO ENG DIFFICULTIES. AFTER LANDING INSPECTED FUSES, FOUND OUTER MARKER BEACON FUSE BLOWN. EXCESSIVE DIRT FOUND ON ALTERNATOR & SURROUNDING CONNECTIONS. BUILD UP CAUSED SHORT IN CONNECTIONS TO ALTERNATOR & CONNECTED COMPONENTS. ALTERNATOR & ENG COMPT CHECKED & CLEANED. BATTERY CHARGED, FUSE REPLACED, RUNUP CHECK & NO ABNORM ELECTRICAL SYSTEM. 1L71 3O3 O A3SO 1E4 5 CP920 20050331001212005033100121WP 2005 3 31 DHL2005805641 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBOARD FLANGE HOLES (2EA) MISDRILLED AT STA 1400.000 L-10R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-07-05 EO AST 050201 DATE 02-17-05. PERFORMED DETAILED VISUAL INSPECTION, NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO AST050201 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050331001222005033100122WP 2005 3 31 DHL2005805676 120050321A5310 HEAT EXCHANGER DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 A 0.500 CRACK IN SKIN OF RT PRIMARY HEAT EXCHANGER AFT UPPER CORNER STA -12.000 L-24R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-16-05 DWG X83-R07 REV IR DATED 03-16-05. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. CUT OUT DAMAGED SECTION IAW DWG X83-R07. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER (AL2024-T3 0.050) REPAIR TRIPLER (AL2024-T3 0.063) AND FILLER (AL2024-T3 0.100) IAW DWG X83-R07. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW DWG X83-R07 SRM 51-1-20D PG 9, SRM 51-1-21 PG 1, SRM 51-3-0 PG 1 SRM 51-1-26. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050331001242005033100124WP 2005 3 31 DHL2005805600 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBOARD FLANGE (2EA) MISDRILLED HOLES AT STA 1320.000 L-12R TO L-13R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-07-05 EO AST 050201 DATED 02-17-05. PERFORMED DETAIL VISUAL INSPECTION NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO AST050201, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050331001252005033100125WP 2005 3 31 DHL2005805599 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT Z-FRAME INBOARD FLANGE HOLES (2EA) MISDRILLED AT STA 1240.000 L-10L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-05-05 EO AST 050205 DATE 02-21-05. CLEANED, TREATED AND PRIMED (AREA) MISDRILLED HOLES IAW SRM 51-1-8B. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD5-4) IAW EO AST050205, SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050331001262005033100126WP 2005 3 31 DHL2005805616 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT Z-FRAME INBOARD FLANGE HOLES (2EA) MISDRILLED AT STA 1260.000 L-10L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-05-05 EO AST 050205 DATE 02-21-05. CLEANED, TREATED AND PRIMED (AREA) MISDRILLED HOLES IAW SRM 51-1-8B. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD5-5) IAW SRM 51-1-21 PAGE 1, EO AST 050205. 2L74 4F RT4A25 20050331001272005033100127WP 2005 3 31 DHL2005805618 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBOARD FLANGE (1EA) MISDRILLED HOLE STA 240.000 L-12R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-07-05 EO AST 050201 DATED 02-17-05. PERFORMED DETAIL VISUAL INSPECTION NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLE WITH RIVET(MS20470AD) IAW EO AST 050201 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050331001282005033100128WP 2005 3 31 DHL2005805622 120050321A53403750257 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 AFT CARGO COMPT SPLICE FITTING CRACKED 9.000 STA 1040.000 - STA 1060.000 L-31R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PAGE 1. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-20D PAGE 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW SPLICE FITTING IAW SRM 51-1-20D PAGE 9. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050401000022005040100002 2005 4 1 KBM2005F00045 420050317A34225040017901 GYRO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE COCKPIT FAILED E KBMAK NONE O OTHER ININSP/MAINT 1 WP19351WM 2167 ATTITUDE GYRO UNIT TUMBLES. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050401000122005040100012 2005 4 1 UIEA200500006 420050203A343019900135 CONTROL PANEL BOEING747 7472D7B 1384803NM GE CF6 CF650E2 30018NE ILS FAILED A UIEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA15526MC 22337 AIRCRAFT DIVERTED DUE TO (ILS LOC AND GS NOT RECEIVABLE) ON BOTH CAPTAIN AND FO HSI, ALL FLAGS VISIBLE ON BOTH SIDES INDICATING COMPLETE FAILURE OF THE ILS NAV CONTROL PANEL. REPLACED ILS CONTROL PANEL IAW MM 34-31-01 PERFORMED OPS CHECK ON ILS SYSTEM OK IAW MM34-31-00 FOUND WORKING SATISFACTORY. (K) 2L74 4F4 FRTA20WE E23EA 20050401000142005040100014NM 2005 4 1 USAA050337 120050302A5340 STRINGER CLIP BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19442US40275 24841 CLT - Q6 - TIE CLIP, .3750 INCH CRACK, STA 827, STRINGER 3R. REPLACED TIE CLIP IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050401000232005040100023NM 2005 4 1 USAA050344 120050307A5754 SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU NR 5 SLAT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19519AU50516 23705 CLT - Q2 - NR 5 SLAT SKIN, 38 INCH CRACK, NR 5 SLAT LE SKIN. INSTALLED REPAIR DOUBLER IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050401000242005040100024NM 2005 4 1 USAA050346 120050307A5330 SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19519AU50516 23705 CLT - Q6 - FUSELAGE SKIN, .5 INCH CRACK, LOWER HINGE CUT-OUT FWD SERVICE DOOR. INSTALLED REPAIR DOUBLER IAW TR 52-10-13. (K) 2L72 4F4 FRTA16WE E21EU 20050401000332005040100033EA 2005 4 1 A6WA200540099 120050315A5210601R317725S DRAG ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31413AW 7585 PASSENGER DOOR AFT DRAG ANGLE CRACKED. REPAIRED PAX DOOR AFT DRAG ANGLE IAW REO 601R-52-11-513 REV A BY CUTTING OUT (CRACKED ANGLE AND INSTALLING NEW ANGLE). 2L72 4F4 FRTA21EA E15NE 20050401000462005040100046NM 2005 4 1 USAA050358 120050302A552265C25746131 SKIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU LT ELEVATOR DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19438US40959 24560 PIT - Q4 - COMP SKIN LT ELEVATOR, 2.5 INCH LENGTH X .125 INCH WIDTH, COMPOSITE DAMAGE, STA 55 AT PANEL CENTER TOP SURFACE LT ELEV. INSTALLED REPAIR PLIES IAW SRM AND EA. (K) 2L72 4F4 FRTA16WE E21EU 20050401000492005040100049NM 2005 4 1 USAA050343 120050307A5754 SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU NR 5 SLAT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19519AU50516 23705 CLT - Q2 - NR 5 SLAT SKIN, SEVERAL .250 INCH CRACKS, NR 5 SLAT LOWER SKIN L/E. INSTALLED REPAIR DOUBLER. (K) 2L72 4F4 FRTA16WE E21EU 20050401000502005040100050NM 2005 4 1 USAA050347 120050307A5751 ANGLE BOEING737 7374B7 1384702NM WRIGHTR3350 R3350* 67040EA OB LT AILERON CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19781AU39081 25020 CLT - C2 - ANGLE, .250 INCH CRACK, CLOSE-OUT WEB JUST OB OF LT AILERON QUADRANT. REPLACED WITH FABRICATED ANGLE IAW SRM 51-10-02. (K) 2L72 4F4 RRTA16WE E272 20050401000512005040100051NM 2005 4 1 USAA050355 120050303A554165C2584151 SPAR BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU RUDDER LE CHIPPED A USAAK NONE O OTHER ININSP/MAINT 1 EA19438US40959 24560 PIT - Q4 - RUDDER L/E SPAR, .2500 INCH X .1250 INCH DEEP CHIP IN EDGE CHIP, LT L/E SPAR TAB. BLEND OUT REPAIR, HFEC INSPECTION AND VISUAL, SEALED IAW EA 79967. (K) 2L72 4F4 FRTA16WE E21EU 20050401000522005040100052EA 2005 4 1 A6WA200540097 120050315A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31415AW 7593 RT SIDE FS 621-FS 625.3 INTERCOSTAL AT STR 14R IS CRACKED NEAR RADIUS APPROX .60 INCH. INSTALLED NEW RT INTERCOSTAL AT FS 621-625.3, STR 14R IAW BRAS EO 601R-53-6157. (K) 2L72 4F4 FRTA21EA E15NE 20050401000722005040100072NM 2005 4 1 USAA050353 120050224A575465C26603102 SKIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU NR 4 SLAT CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19438US40959 24560 PIT - Q4 - SLAT, 8 INCH LONG X 3 INCH WIDE AREA, CHAFED. NR 4 SLAT IB T/E LOWER SKIN SURFACE. INSTALLED FILLER AND INTERNAL DOUBLER, KEY CORE AND TOP DOUBLER, SEALED EDGE AND REFINISHED IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050401000832005040100083EA 2005 4 1 A6WA200540109 120050316A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31415AW 7593 FLOORBEAM ANGLE AT FS 621 LT SIDE IS CRACKED 1 INCH. PERFORMED REPAIR TO RT FS 621 FLOORBEAM ANGLE IAW BOMBARDIER REO 601R-53-117 REV C. (M) 2L72 4F4 FRTA21EA E15NE 20050401000842005040100084EA 2005 4 1 A6WA200540118 120050314A5322 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31413AW 7585 LT FS 625, WO OBLIQUE ANGLE IS CRACKED. REMOVED AND REPLACED LT 621.00 ANGLE AT STR 14 LT IAW SRM. (K) 2L72 4F4 FRTA21EA E15NE 20050401000912005040100091NM 2005 4 1 USAA050351 120050310A5343 SUPPORT FITTING BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU MLG CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19519AU50516 23705 CLT - Q2 - SUPPORT FITTING, .1250 INCH CRACK, MLG AFT SUPPORT FITTING. REPAIRED IAW TR57-40-13. (K) 2L72 4F4 FRTA16WE E21EU 20050401000922005040100092CE 2005 4 1 HYI2005F00003 120050216A5410585410411 BEAM CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO MCAULY3AF32C3AF32C505 GL LT NACELLE CRACKED E HYIAO OTHER O OTHER NRNOT REPORTED 1 NE01406GA21255 402C0329 DURING ENGINE NACELLE INSPECTION, FOUND 1.5 INCH CRACK ON TOP REAR RADIUS OF CROSSOVER BEAM. REMOVED BEAN AND INSTALLED NEW BEAM IAW MFG MM. (NE01200502852) (K) 1L72 3O3 O A7CE E8CE 5 CP22EA 20050111000082005011100008WP 2005 1 11 AALA20050001 120050102A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21110HM 49787 RDU - OVERHEAD EMERGENCY LIGHTS AT ROWS 7 TO 11 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT ROWS 7 TO 11. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050111000092005011100009WP 2005 1 11 AALA20050002 120050101A335060030451 BATTERY DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21966TW 53616 AUS - CEILING EMERGENCY LIGHTS AT ROWS 28 THROUGH 31 INOPERATIVE. REPLACED BATTERIES FOR CEILING EMERGENCY LIGHTS AT ROWS 28 THROUGH 31. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050111000112005011100011WP 2005 1 11 AALA20050004 120050101A36105953625521 DUCT DOUG DC9 DC982 3022082WP A/C BAY CRACKED A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21407AA 49318 DFW - EN ROUTE DFW TO TUS TAIL COMPARTMENT HIGH TEMPERATURE LIGHT CAME ON DURING CLIMB. RETURNED DFW AND LANDED WITHOUT INCIDENT. REPLACED CRACKED Y-DUCT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050111000222005011100022NM 2005 1 11 AALA20050006 120050107A33508039001 BATTERY DOUG MD80 MD83 3023681NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW219412W 53187 SFO - DURING OVERNIGHT MAINTENANCE EMERGENCY OVERHEAD AISLE LIGHTS INOPERATIVE AT ROWS 12-16. REPLACED EMERGENCY OVERHEAD AISLE LIGHTS BATTERY AT 14DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RT 20050111000242005011100024NM 2005 1 11 AALA20050009 120050106A3350 CONNECTOR BOEING757 757223 1384957NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21635AA 24593 JFK - EMERGENCY EXIT LIGHT OVER 3L INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY CHARGER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050111000322005011100032NM 2005 1 11 AWXA200500019 120050109A2560P4010021 BATTERY BOEING757 7572S7 1384962NM FLASHLIGHT DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28901AW 23321 PHX - EMERGENCY EQUIPMENT - DURING INSPECTION THE FORWARD EMERGENCY FLASHLIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20050111000352005011100035EU 2005 1 11 AWXA200500014 120050105A33501012881 LIGHT AIRBUS320 A320231 3930325EU CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28636AW 098 PHX - EEL - DURING 8-DAY CHECK FUNCTIONAL TEST OF THE EMERGENCY LIGHT SYSTEM, THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 22 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 22 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050111000412005011100041NM 2005 1 11 AWXA200500001 120050103A3397964411 WIRE BOEING737 7373S3 1384711NM CABIN BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 PHX - EEL - DURING INSPECTION FOUND BROKEN WIRES AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 12 LT. MAINTENANCE REPLACED EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 12 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050111000452005011100045EU 2005 1 11 AWXA200500005 120050104A33501013081 LIGHT AIRBUS320 A320231 3930325EU CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28636AW 098 PHX - EEL - FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 11 RT SIDEWALL WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 11 RT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050111000472005011100047EU 2005 1 11 AWXA200500007 120050103A335032145410 POWER SUPPLY AIRBUS320 A320232 3930326EU CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28656AW13206126 1079 PHX - EEL - DURING P-02 CHECK THE AFT CABIN EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AFT LT EMERGENCY POWER SUPPLY UNIT (13WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050111000562005011100056EA 2005 1 11 COMA0560016 120050102A3222 TORQUE LINK CNDAIRCL600 CL6002B19 1900309EA NLG DISCONNECTED A COMAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 SO01989CA 7215 FLIGHT 5061, GEAR DISAGREE WARNING. FOUND NLG TORQUE LINKS DISCONNECTED. RECONNECTED TORQUE LINKS AND A/C RETURNED TO SERVICE. 2L72 4F RTA21EA 20050111000682005011100068EA 2005 1 11 COMA0560020 120050101A3260 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A COMAO OTHER N FALSE WARNING APAPPROACH 1 SO01709CA 7238 FLIGHT 5316, GEAR DISAGREE WARNING. COULD NOT DUPLICATE. FUNCTIONAL TEST OF LANDING GEAR EXTENSION AND RETRACTION SYSTEM NORMAL, NO DEFECTS FOUND. 2L72 4F RTA21EA 20050111000752005011100075EA 2005 1 11 COMA0560027 120050104A2760 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A COMAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01958CA 7111 FLIGHT 5650, FLIGHT SPOILER FAULT AND GROUND SPOILER FAULT. RESET THE SPOILER SYSTEM, COULD NOT DUPLICATE. OPERATIONAL CHECK SATISFACTORY. 2L72 4F RTA21EA 20050111000952005011100095NM 2005 1 11 DL757050008 120050104A2560 GIRT BAR BOEING757 757232 1384965NM L2 DOOR JAMMED A DALAA UNSCHED LANDING O OTHER CLCLIMB 1 SO27625DL 22915 A/C WOULD NOT PRESSURIZE AFTER T/O. OUTFLOW VALVE FULLY CLOSED, FOUND L2 DOOR GIRT BAR JAMMED IN FWD END OF DOOR. REPLACED BAR AND FITTINGS. 2L72 4F RTA2NM 20050111000962005011100096NM 2005 1 11 DL738050001 120050101A3230161A61143 SPRING BOEING737 737832 13844CFNM LT MLG MISSING A DALAA UNSCHED LANDING D INFLIGHT SEPARATION CLCLIMB 1 SO273754A NONE 29626 LEFT MAIN GEAR DID NOT RETRACT, RED GEAR LIGHT REMAINED ILLUMINATED WITH GEAR IN OFF POSITION. BOTH GREEN GEAR DOWN INDICATIONS OVERHEAD AND MAIN CONSOLE WERE ILLUMINATED. FOUND ONE LT MLG UPLOCK SPRING MISSING. REPLACED BOTH SPRINGS. JACKED A/C AND PERFORMED GEAR RETRACTION PER MM, GEAR SWING OK. 2L72 4F RTA16WE 20050111000972005011100097NM 2005 1 11 DL75A050009 120050106A3350333101582 BATTERY PACK BOEING757 757212 1384951NM CABIN NOT SEATED A DALAK NONE N FALSE WARNING TOTAKEOFF 1 SO27757AT 23127 ON TAKEOFF EMERGENCY LIGHTS ON RIGHT SIDE OF CABIN ILLUM. ON PREFLIGHT THIS MORNING FOUND RIGHT EMERGENCY CHARGER C/B POPPED. RESET AFTER TAKEOFF, DISCOVERED RIGHT EMERGENCY CHARGER C/B POPPED AGAIN, LEFT OUT. INSPECTED CHARGER AND CANNON PLUG. RESET BATTERY PACK IN CRADLE. C/B NOW SECURE AND ALL LIGHT OPERATE CORRECTLY. 2L72 4F RTA2NM 20050111001012005011100101NE 2005 1 11 DL76P050005 220050103A7200PW40603 ENGINE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 2 FAILED A DALAA UNSCHED LANDING EYAVIBRATION/BUFFET ENGINE STOPPAGE FLAME/FIRE CLCLIMB 1 SO27140LL28000 25988 727745 INFLIGHT SHUTDOWN OF RIGHT ENGINE. CLIMBING THROUGH FL 260 WITH ALL ENG INDICATIONS NORMAL AND POWER AT CLIMB SETTING, ACFT SHUDDERED VIOLENTLY WITH LOUD BANG. RIGHT ENG HAD FAILED. ACCOMPLISHED ENGINE FAILURE CHECKLIST AND RETURNED TO TPA. PASSENGER REPORTED FLAMES COMING FROM RIGHT ENG. ENGINE INDICATIONS AT TIME OF FAILURE SHOWED NO N1, N2 OR EPR INDICATIONS. FUEL FLOW WAS ZERO AND ENG WAS COMPLETELY INOP AT TIME THAT CHECKLIST WAS ACCOMPLISHED. REPLACED ENGINE. 2L72 4F4 FRTA1NM E24NE 20050111001022005011100102NM 2005 1 11 DL764050010 120050108A3350 LIGHT BOEING767 767432ER 1385134NM CABIN MISSING A DALAK NONE O OTHER ININSP/MAINT 1 SO27841MH 29714 SEAT 26B EMERGENCY ESCAPE PATH LIGHT MISSING 1 EA BULB AND LENS. REPLACED SAME. 2L72 4F RTA1NM 20050111001042005011100104NE 2005 1 11 DLM88050007 220050105A7314739001000 PUMP DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 ENGINE FAILED A DALAC ABORTED TAKEOFF X ENGINE FLAMEOUT TOTAKEOFF 1 SO27917DL 49573 725551 ON T/O ROLL THE NR 2 ENGINE ROLL BACK AND SHUT DOWN. MTC INSPECTED THE INTAKE, EXHAUST AND FUEL CONTROL LINKAGE, NO TROUBLE FOUND. ENGINE WILL NOT START, NO FUEL FLOW. REPLACED FUEL PUMP AND CONTROL. 2L72 4F4 FRTA6WE E9NE 20050111001062005011100106NE 2005 1 11 DL738050013 220050109A7530106200821 SHUTOFF VALVE BOEING737 737832 13844CFNM CFMINTCFM567CFM567B2US 13802NE NR 1 ENGINE LEAKING A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27378DA 30265 874845 LEFT ENGINE BLEED TRIP OFF AROUND 20K FT, COULD NOT RESET. ENGINE DUCT PRESSURE WAS SPLIT L-15 RT 40 PSI ON CLIMBOUT. REPLACED LEFT PRSOV RAN ENGINE AT POWER, OPS OK. 2L72 4F4 FRTA16WE E2GL 20050111001072005011100107NM 2005 1 11 DL73S050011 120050109A5753 FAIRING BOEING737 737232 1384475NM T/E FLAP LOOSE A DALAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO27320DL 23092 AFTER T/O EXP VIBRATION, LIGHT TO MODERATE, APPROX 12,000 AND 300 KTS. SLOWED TO 250 VIBRATION SUBSIDED SOMEWHAT. EXPERIENCED VIBRATION THRU 210 KTS LIGHT. FOUND E/E DOOR SEAL OUT OF POSITION. REPAIRED SAME. FOUND 2 FLAP FAIRINGS LOOSE. TIGHTENED SAME. 2L72 4F RTA16WE 20050111001192005011100119SO 2005 1 11 SWIA200514330 120050102A3350 SIGN EMB 120 EMB120ER 3260203SO CABIN DETACHED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07586SW 120354 LOWER EXIT SIGN AT ROW 6 NEEDS TO BE RE-ATTACHED. REPLACED LOWER EMERGENCY, EXIT SIGN AT ROW 6 IAW MM 33-51-02, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050111001212005011100121EA 2005 1 11 SWIA200514332 120050102A2721 TRIM PANEL CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07936SW 7726 RUDDER TRIM WILL NOT MOVE NOSE LEFT. REPLACED RUDDER TRIM PANEL. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050111001372005011100137SO 2005 1 11 SWIA200514334 120050103A27523431001001 ACTUATOR EMB 120 EMB120ER 3260203SO T/E FLAP MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07270YV 120270 NACELLE FLAP DISAGREEMENT WHEN FLAPS RETRACTED. REPLACED RIGHT NACELLE FLAP ACTUATOR PER MM 27-50-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050112000232005011200023CE 2005 1 12 DXTA200500525 120050110A3260 WARNING LIGHT RAYTHNDH125 HAWKER800XP 7150012CE RT MLG ILLUMINATED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07873QS 258573 FOLLOWING GEAR RETRACTION THE RT MAIN GEAR UNSAFE LIGHT REMAINED ILLUMINATED, IT TOOK 2 GEAR RECYCLES TO EXTINGUISH THE UNSAFE CONDITION. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA3EU 20050112000692005011200069NM 2005 1 12 05FDEA00007 120050103A5511 SPAR DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 RIGHT HAND HORIZONTAL STABILIZER: STA XE159 RIB NR 12 LOWER FRONT TO REAR SPAR FOUND CORRODED. REPAIRED IAW FEDEX EA 1-5510-78109. 2L73 4F RTA22WE 20050112000702005011200070NM 2005 1 12 05FDEA00008 120050103A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 RT HORIZONTAL STABILIZER, STA XE159 TO 176.5 RIB 12 TO 13 INTERSPAR LOWER MID PLANK FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01. OUT OF LIMITS AS PER SRM 55-00-01. REPAIRED AS PER EA 1-5510-78108. 2L73 4F RTA22WE 20050112000722005011200072SO 2005 1 12 C2XA05IA001 120050104A335074441 LIGHT EMB 145 EMB145ER 3260211SO GALLEY INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714939 145030 IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHT IN THE GALLEY WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT ASSEMBLY, OPS CK WITH NO DEFECTS. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. NOTE - THIS PART IS NOT SERIALIZED, AND IS NOT TRACKED. 2L72 4F RTT00011AT 20050113000462005011300046CE 2005 1 13 DXTA200500515 120050105A2910 LINE CESSNA650 650 2076802CE HYDRAULIC SYS UNKNOWN E DXTAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07789QS 6507089 ON LANDING ROLL OUT,THE LEFT BRAKE PEDAL WENT TO THE STOP WITHOUT ANY BRAKING OCCURRING ON THE LEFT MAINS. TAXI CHECK A/C COULD NOT DUPLICATE. HOOKED UP PRESS GAUGES TO LT BRAKE ASSY APPLY HYD PRESS + GET 2000 PSI OUT OF BOTH BRAKE ASSY. BLED BRAKES. TAXI A/C OPS CHECKED GOOD IAW 650 MM CH 32-42-00 2L72 4F A9NM 20050113000472005011300047 2005 1 13 DXTA200500514 420050104A3140 LIMIT SWITCH CESSNA560 560XL 2076702CE STAB POSITION FAILED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07624QS 5605302 NO TAKEOFF LIGHT WILL NOT GO OUT ON GROUND, HORN SOUNDS WHEN POWER IS ADVANCED ALL ASSOCIATED SYSTEMS CHECKED / NO PROBLEMS INDICATED. FOUND STAB POSITION SWITCHES OUT OF ADJUSTMENT AND CORROSION ON SPEED BRAKE SWITCH CONNECTORS. ADJUSTED HORIZONTAL STAB POSITION SWITCHES NR 6 & 7. CLEANED SPEED BRAKE CONNECTORS PROO1 & PLOO1. OPS CHECK NO TAKEOFF WARNING SYSTEM . OPS CHECK NORMAL. WORK PERFORMED IAW CE-560 XL M.M. CHAPT 27-40-00 AND CHAP 27-61-00. 2L72 4F RTA22CE 20050114000022005011400002EU 2005 1 14 05FDEA00033 120050106A5753 SKIN AIRBUS310 A310 EU TE FLAP DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25454FE 278 NON-ROUTINE NR N00380. RT WING REPAIR ON INBD FLAP LWR SURFACE T/E. VERIFIED THAT THE EXISTING REPAIR WAS PERFORMED IAW FEDEX EA 6-5710-63790. 2L72 4F RTA35EU 20050114000052005011400005EU 2005 1 14 05FDEA00039 120050106A5730 SKIN AIRBUS310 A310 EU RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25454FE 278 RT WING - CORROSION FOUND ON UPPER SURFACE STA 1659 RIB 27 TO STA 1713 RIB 28 INTERSECTION WITH STRINGER 12. CORROSION REMOVED AND REPAIRED IAW EA 6-5710-81827. 2L72 4F RTA35EU 20050114000062005011400006NM 2005 1 14 05FDEA00081 120050112A3233651781915 ACTUATOR BOEING727 727100 1384036NM MLG LEAKING A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25151FE 19147 UPON GEAR RETRACT AFTER T/O RED RT GEAR LIGHT ILLUMINATED & AMBER RT MLG DOOR LIGHT ON S/O PANEL ILLUMINATED. MOVED GEAR HANDLE TO DOWN POS. 3 GREEN DOWN/LOCKED INDICATION & NO RED RT AMBER LIGHTS RAISED GEAR HANDLE AND RED RT GEAR LIGHT AND RT MLG DOOR LIGHT ILLUMINATED. NOTICE A QTY DECREASED TO .6 GALLONS MOVED GEAR HANDLE TO OFF & GOT GREEN RT GEAR LIGHT, RED RT GEAR LIGHT OFF & AMBER R MLG DOOR LITE ON S/O PANEL. APPLIED QRH AND LANDED EVENTFULLY. HYD QTY NEVER GOT TO 0 AND NEVER GOT LOW PRESS LITES. FOUND RT MLG LOCK ACTUATOR CRACKED AND LEAKING. R&R RT MLG LOCK ACTUATOR PER MM 32-32-061-4 NO LEAKS NOTED OPS CK OF MLG IAW MM B727-100 32-32-0 A/C OK 4 FLT 2L73 4F RTA3WE 20050114000072005011400007EU 2005 1 14 05FDEA00027 120050106A5330 SKIN AIRBUS310 A310 EU FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25454FE 278 FUSELAGE REPAIR AT APROX. FS 1 STR 56 LT. VERIFIED THAT THE EXISTING REPAIR WAS PERFORMED IAW FEDEX EA 6-5310-81826. 2L72 4F RTA35EU 20050114000202005011400020CE 2005 1 14 DXTA200500517 120050105A522062112525 LOCKPIN CESSNA650 650 2076802CE EMERGENCY EXIT DAMAGED E DXTAK NONE O OTHER ININSP/MAINT 1 GL07779QS 6507079 STARBOARD EMERGENCY EXIT HATCH HANDLE DOES NOT TURN PROPERLY. REMOVED LOCK PIN ASSY PN 6211252-5 INSTALLED NEW LOCK PIN ASSY OF SAME PN REMOVED GUIDE ASSY PN 5211252-2 INSTALLED NEW GUIDE ASSY OF SAME PN. OPS CHECK GOOD. REINSTALLED HATCH ALL WORK PERFORMED IAW CE-650 MM CHAPTER 52-20-00. 2L72 4F A9NM 20050114000212005011400021CE 2005 1 14 DXTA200500520 120050107A323099125374 CYLINDER CESSNA560 560XL 2076702CE MLG MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 GL07699QS2828 5605199 RED UNLOCK LIGHT ON GEAR FLASHED (OR CYCLED) AFTER GEAR RETRACTION. UPON EXTENDING GEAR, HAD 2 "BUMPS" LIKE HYDRAULIC ACTUATION RESULTING IN MOMENTARY LOSS OF DOWN & LOCKED INDICATIONS. GEAR WAS BLOWN DOWN. RT ACTUATOR LEAKING EXCESSIVELY, REMOVED AND REPLACED RT MLG ACTUATOR IAW CE 560XL M/M 32-30-04. LEAK AND OP CHECKED GOOD. PERFORMED MAIN LANDING GAER FUNCTIONAL TEST. CHECKED GOOD. SWUNG GEAR MULTIPLE TIMES. NO DISCREPECIES NOTED. REF CE 560XL M/M 32-01-00.0 2L72 4F RTA22CE 20050114000282005011400028EA 2005 1 14 05011651 120050111A2740 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A VTZAO OTHER J WARNING INDICATION CLCLIMB 1 EA27651BR 7426 CREW REPORT ON 01/11 STATED THAT IMMEDIATELY AFTER T/O THE STAB TRIM AND MACH TRIM CAUTION MSGS POSTED AT THE SAME TIME. RETRIEVED FAULT CODES FROM MDC. PERFORMED HSTCU OPS TEST PER 27-40-00. OPS CHECK GOOD. 2L72 4F RTA21EA 20050114000292005011400029NM 2005 1 14 UPS05M43642 120050110A5210 MECHANISM DOUG MD11 MD11F 3023600NM PAX DOOR MALFUNCTIONED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01272UP 48571 INSPECTION TYPE:N/A, LT ENTRY DOOR WILL NOT ARM ESCAPE SLIDE WHEN CLOSED. MANIPULATED EMERGENCY FLIPPER MECHAMISM WHILE MOVING EMERGENCY HANDLE FROM OUTSIDE. PERFORMED FUNCTIONAL CHECK OF ARMING DOOR PER MM 52-10-00, DOOR OPERATES AND ARMS NORMALLY. 2L73 4F RTA22WE 20050118000232005011800023NM 2005 1 18 AWXA200500028 120050106A575465C26602212 WEDGE BOEING737 7373Q8 1384670NM NR 5 SLAT DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK A DISBOND AREA WAS FOUND IN NR 5 SLAT WEDGE ON UPPER SURFACE AT INBOARD END BETWEEN SS 131.50 AND SS 132.50. MAINTENANCE CUT OUT DAMAGE IN NR 5 SLAT WEDGE AT UPPER INBOARD END; FABRICATED A FILLER AND DOUBLER; BONDED REPAIR PARTS TO SLAT IAW B737-300 SRM 51-70-10 FIG 31. 2L72 4F RTA16WE 20050118000262005011800026NM 2005 1 18 05FDEA00002 120050102A5313 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 WASTE TANK COMPT LONGERON 41A LT CORRODED AT STA 1965 - 1967. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20050118000272005011800027NM 2005 1 18 05FDEA00003 120050102A5512 PANEL DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 LT HORIZONTAL STAB LEADING EDGE ACCESS PANEL 331BT LOWER OUTBOARD MOUNTING LUG FOUND WITH SURFACE CORROSION. CORROSION REPAIRED AS PER FEDEX EA 1-5510-78106, 2L73 4F RTA22WE 20050118000312005011800031NM 2005 1 18 05FDEA00004 120050103A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25605FE 48514 MAIN DECK CARGO, SEAT TRACK AT STA Y= 791.75 TO Y= 859, X= 8.5 DAMAGED AT FLANGED AREA. REPAIRED PER SRM 53-70-00 VOLUME I, FIGURE 1 2L73 4F RTA22WE 20050118000342005011800034NM 2005 1 18 SWAA050045 120050107A143065C16820 FASTENER BOEING737 7375H4 138449DNM R1 DOOR MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29521SW 25320 L1 DOOR EVAC SLIDE MOUNTING FASTENER MISSING. REMOVED AND REPLACED FASTENER PER MM. 2L72 4F RTA16WE 20050118000362005011800036NM 2005 1 18 SWAA050047 120050107A335065C270921 BATTERY BOEING737 7375H4 138449DNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29523SW 26565 DURING SCHEDULED A2 CHECK, FOUND FWD SERVICE DOOR EMERGENCY ESCAPE SLIDE LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20050118000422005011800042CE 2005 1 18 DXTA200500524 120050110A3213 STRUT CESSNA750 750 2076810CE NLG DISCHARGED E DXTAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 GL07936QS 7500036 AFTER TAKEOFF GEAR HANDLE WOULD NOT COME UP. FOUND NOSE STRUT NOT PROPERLY SERVICED. SERVICED NOSE STRUT IAW CESSNA 750 MM 12-10-38. CYCLED GEAR MULTIPLE TIMES, OPS CHECKS GOOD. 2L72 4J RTT00007WI 20050118000562005011800056WP 2005 1 18 MWEA050004 120050104A531199115055 FRAME DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31805ME 48031 APPARENT CRACK LOCATED AT STATION 83.550 OUTBOARD LEFT 10 INCH FROM CENTER. FABRICATED AND INSTALLED REPAIR ANGLE. 2L72 4F A6WE 20050602001602005060200160NM 2005 6 2 DLM88050270 120050513A323339281375001 ACTUATOR DOUG MD88 MD88 3023688NM NLG BROKEN A DALAA UNSCHED LANDING O OTHER CLCLIMB 1 SO27949DL 49880 LOUD BANG WHEN GEAR RETRACTION ATTEMPTED. NLG WOULD NOT LOCK UP. GOT THREE GREENS WHEN HANDLE PLACED BACK TO DOWN. FOUND NLG RETRACT ACTUATOR BROKEN AND ROD END PULLED OUT OF ACTUATOR. ROD END HAD FALLEN BACK AND MOVEMENT OF GEAR CAUSED PENETRATION THROUGH WHEEL WELL BULKHEAD. REPLACED ACTUATOR AND REPAIRED DAMAGE 2L72 4F RTA6WE 20050602001732005060200173NM 2005 6 2 P9RA20050082 120050519A2400 ODOR BOEING757 757236 1384971NM RROYCERB211 RB211* 54555NE COCKPIT DETECTED A P9RAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11522NA 25133 EN ROUTE, FLT LEVEL 360, ELECTRICAL FUMES IN COCKPIT AND CABIN. HAD ENGINE ANTI ICE ON AND CONT IGNITION ON. SMELL DISSIPATED WHEN THESE ITEMS WERE SELECTED OFF. PERFORMED INSPECTIONS OF ENGINES, AIR CONDITIONING PACKS, IGNITION SYSTEMS. GROUND RAN AIRCRAFT WITH ENGINE ANTI-ICE ON AND OFF. ALL SYSTEMS OPERATED NORMALLY. NO ELECTRICAL ODOR NOTED. TEST PERFORMED IAW WITH APPLICABLE MM REFERENCES. NO COMPONENTS REPLACED AT THIS TIME. 2L72 4F4 FRTA2NM A12EU 20050602001762005060200176EU 2005 6 2 MALA050425 120050519A3020 MODULE SAAB SF340 340B 7860101EU DEICE SYSTEM MALFUNCTIONED A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 GL15426XJ 340B426 THE CREW REPORTED THAT THE RT INTAKE HEAT SYSTEM WAS CYCLING AND A SLIGHT BURNT SMELL ASSOCIATED WITH THE INTAKE HEAT BEING ON. RETURNED TO DTW. REPLACED LOWER DUCT AND DEICE MODULE. 2L72 4T RTA52EU 20050602001792005060200179WP 2005 6 2 DHL2005807532 120050516A57203704841501 FITTING DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH86990 45990 NR 2 MAIN TANK FWD FITTING CRACK 1.000 STA XRS 74.000 AT INBD SIDE, S-51 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED, AND APPLIED COATING MATERIAL AREA IAW SRM 51-1-12. INSTALLED NEW FITTING (PN 3704841-501) AND SRM 51-1-20D PG 9, SRM 51-3-0 PG 1, SRM 51-1-23, SRM 51-1-11. TORQUED IAW SRM 51-3-1. REFER TO NR 036403 FOR LEAK CHECK. 2L74 4F RT4A25 20050602001802005060200180 2005 6 2 DHL2005807529 420050517A34435616101 CAP DOUG DC8 DC873F 302199FWP DOPPLER SYS CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH86990 45990 DOPPLER ANTENNA HOUSING CAP HAS TWO CRACKS OF 1.000, STA -99.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, JC EA53100131-001-D, EA05920, DRAWING 5616101. REMOVED DAMAGED CAP IAW SRM 51-1-20D PG 21, SRM 51-1-21 PG 1. FABRICATED CAP (P/N 5616101-47 SP, AL7075"O"0.125) IAW DWG 5616101, EA05920, SRM 51-1-4 PG.1, DPS 3.69-4 REV "AM" R-1. HEAT TREATED IAW SRM 51-1-1 PG 1-13-17 DPS 7.00-1 REV "BK". PERFORMED NDT INSP IAW NDT SPM PART 08.00-02 TO 07. CLEANED, TREATED AND PRIMED AREA AND NEW CAP IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW CAP IAW SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050602001862005060200186WP 2005 6 2 DHL2005807535 120050516A532037504972 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH86990 45990 AFT ACCY COMPT FRAME FITTING 1.000 CRACK (STA 660.000-670.000, L-35R TO L-36). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING (PN 3750497U2) IAW SRM 51-1-20D PG 9, SRM 51-3-0 PG 1, SRM 51-1-11. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050606000042005060600004NM 2005 6 6 DHL2005741510 120050414A5755 SKIN BOEING727 7272Q9 138448MNM NR 4 SPOILER DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 NR 4 SPOILER UPPER SURFACE HAS A DENT. CUT OUT DENT AT NR 4 SPOILER APPROX 2 INCHES DIA. FABRICATED FILLER AN DOUBLER FROM .020 2024-T3 PO NR 9001310, BONDED FILLER AN DOUBLER, CURED AN CLEANED AN SEALED IAW B727 SRM 57-50-2 FIG 9 AN 51-40-20 FIG 30. 2L73 4F RTA3WE 20050606000092005060600009WP 2005 6 6 UPS05844485 120050505A5712 RIB DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE: C3, LT WING L/E AT XFS 385.000 LWR RIB CRACKED 2 INCHES LONG MIDDLE OF RIB. FABRICATED AND INSTALLED RIB FORMER AND 2 EA REPAIR ANGLES IAW DWG 5769603, SRM 51-3-2, 57-2-1 AND 51-3-2. 2L74 4F RT4A25 20050606000242005060600024EA 2005 6 6 COMA0560304 120050514A5210601R31998312 SKIN CNDAIR CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01929CA27330 7035 7035 DURING HEAVY MAINTENANCE CHECK, THE PAX DOOR FORWARD AND AFT BOTTOM CORNERS WERE FOUND TO BE CORRODED. BOTH PARTS WERE REPLACED WITH FACTORY NEW PARTS USING THE CL 6002B-19 STRUCTURAL REPAIR MANUAL 2L72 4F RTA21EA 20050606000412005060600041WP 2005 6 6 AALA20050337 120050517A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21262AA 49290 ORD - EMERGENCY LIGHTS IN TAIL COMPARTMENT INOPERATIVE. REPLACED BATTERY PACK B528 FOR EMERGENCY LIGHTS IN TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050606000422005060600042WP 2005 6 6 AALA20050340 120050518A3350P4010049 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21234AA 49181 MIA - EMERGENCY LIGHTS AT ROWS 27 TO 36 INOPERATIVE. REPLACED BATTERY PACK FOR AFT FLOOR PROXIMITY EMERGENY LIGHTS FOR ROWS 27 TO 36. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050606000452005060600045NM 2005 6 6 AALA20050341 120050519A3397 CONNECTOR BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21177AN 32396 JFK - SEAT MOUNTED EMERGENCY LIGHTS AT SEAT 2B INOPERATIVE. FOUND SIDEWALL CONNECTOR LOOSE AT SEAT 2B. RECONNECTED CONNECTOR FOR SEAT MOUNTED EMERGENCY LIGHTS AT SEAT 2B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050606000522005060600052NM 2005 6 6 AWXA200500590 120050427A5312 BULKHEAD BOEING737 7373B7 1384580NM FUSELAGE SCRATCHED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28332AW 23384 MCN - MAJOR REPAIR - DURING C-18 CHECK NUMEROUS SCRATCHES WERE FOUND AROUND FASTENERS ON BS 178 BULKHEAD COMMON TO FASTENER AND DOME NUT LOCATIONS AT LT BL 6 BETWEEN WL 150 AND WL 182. THE DEEPEST SCRATCH WAS MEASURED 0.004 INCH DEEP AND FOUND BEYOND LIMITS PER B737-300 SRM 53-10-08, FIGURE 101. MAINTENANCE REPAIRED IAW AMERICA WEST AIRLINES ENGINEERING REPAIR 03-5310-05133-ES2. 2L72 4F RTA16WE 20050606000642005060600064NM 2005 6 6 05FDEA01343 120050517A5330ADA30001 SKIN DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25580FE 48471 UPON REMOVAL OF DOME NUT STRAP TO FACILITATE SATCOM MOD AT STA 949 FUSELAGE SKIN ADJACENT TO LONGERON 1L 1 EACH FASTENER HOLE FOUND ELONGATED. REPAIRED AS PER FEDEX EA NR 1-5330-86609. THIS REPAIR CLASSIFIED AS MINOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050606000732005060600073NM 2005 6 6 05FDEA01306 120050516A5320AKC75425 BRACKET DOUG MD11 MD11 3023602NM ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25580FE 48471 TAILCONE FORWARD SECTION: LT UPPER DOOR TEE BRACKET BELOW THE HINGE ASSEMBLY FORWARD MOST EDGE FOUND CRACKED AS MARKED. CRACKED AREA REPAIRED AS PER FEDEX EA NR 1-5350-86610. 2L73 4F RTA22WE 20050606000742005060600074NM 2005 6 6 05FDEA01307 120050516A5340ADA8424525B FITTING DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25580FE 48471 FORWARD CARGO COMPARTMENT,FOUND BILGE LOCATION AT STATION 1130, LONGERON 51L WITH SPLICE CRACKED AS MARKED. NEW SPLICE FITTING MACHINED AS PER DRAWING NO.ADA 8424. FORWARD CARGO COMPARTMENT AT STATION 1130, LONGERON 51L CRACKED SPLICE FITTING REMOVED AND NEW SPLICE FITTING INSTALLED AS PER SRM 51-31-01 VOLUME II. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050606000772005060600077NM 2005 6 6 05FDEA01372 120050519A5512ALC8121502 PANEL DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25621FE 48792 HORIZONTAL STABILIZER RIGHT HAND FORWARD SPAR CAP NR 1R BARREL NUT BORE CORROSION REMOVAL FOUND EXCEEDED LIMITATIONS. REWORKED AS PER FEDEX EA 1-5510-83008. 2L73 4F RTA22WE 20050606001022005060600102 2005 6 6 MAC5401 420050403A8300K966002 GEARBOX FOKKERF27 F27MK500 4990629EU RIGHT LEAKING A MTNAE ENGINE SHUTDOWN J WARNING INDICATION DEDESCENT 1 SO33728FE 10657 EN ROUTE TO GSO FROM ILM THE CREW OBSERVED A MASTER WARNING, THEN THE RIGHT GEAR BOX LIGHT. THE RIGHT ENGINE WAS SHUT DOWN AND THE PIC DECLARED AN EMERGENCY. THE A/C LANDED IN GSO WITHOUT FURTHER INCIDENT. 2H72 4T A817 20050606001042005060600104EA 2005 6 6 QXEA200500874 120050504A5210 ATTACH ANGLE CNDAIRCL600 CL6002C10 1390015EA ZONE 800 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - PASSENGER DOOR AFT SIDE STRINGER TO DOOR SHELL ATTACH ANGLE CRACKED AT ASSIST MOTOR. REPAIRED IAW REO 670-52-11-072. 2L72 4F RTA21EA 20050606001062005060600106EA 2005 6 6 QXEA200500876 120050502A5230 SEAL CNDAIRCL600 CL6002C10 1390015EA ZONE 800 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FORWARD BAGGAGE DOOR CHAFED AT LOWER FORWARD AND AFT EDGES AT SEAL. REPAIRED IAW CRJ-700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20050607000072005060700007EA 2005 6 7 QXEA200500866 120050429A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FUSELAGE EXTERIOR, LOWER SKIN HAS CHAFE DAMAGE FROM FAIRING JOINT STRAP AT STATION 974 AND BLO 0.00. REPAIRED IAW CRJ-700 SRM 51-42-21-001-001-A01, 51-25-16-001-001-A01, 51-42-21-001-001-A01 AND HORIZON AIR EA R-53-319. 2L72 4F RTA21EA 20050607000132005060700013EA 2005 6 7 QXEA200500873 120050429A5210 STRINGER CNDAIRCL600 CL6002C10 1390015EA ZONE 800 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - PASSENGER DOOR AFT SIDE STAIR STRINGER CRACKED UP AND DOWN AT STOWAGE BRACKET. REPAIRED IAW REO 670-52-11-104 AND CRJ 700 SRM 51-41-01-001-001-A01. 2L72 4F RTA21EA 20050607000212005060700021NM 2005 6 7 DHL2005740528 120050327A5330 SKIN BOEING727 7272Q9 138448MNM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH21930 21930 DENT R/SIDE FUSELAGE SKIN 3 INCHES FWD OF STA 1342.4 STRINGER 23R. REMOVED FASTENERS FOR ACCESS IAW B727 SRM 51-30-2. CUT OUT DAMAGED AREA 3 BY 1.5 INCHES IAW B727 SRM 53-30-3 FIG 1. FABRICATED FILLER SIZE 3 BY 1.5 INCHES FROM 2024T3 .050 PO NR 9002093 AND DOUBLER FOR 2024T3 .063 SIZE 7 BY 7.750 INCHES PO 9001978 IAW B727 SRM 53-30-2 FIG 3 AND 53-30-3 FIG 1. TREATED AND PRIMED PARTS AND AREA IAW B727 SRM 51-10-2 AND INSTALLED PARTS IAW B727 SRM 53-30-3 FIG1 2L73 4F RTA3WE 20050607000302005060700030NM 2005 6 7 DHL2005740539 120050328A5310 TORQUE BOX BOEING727 7272Q9 138448MNM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 REF. FLIGHTSTAR NR 104834 DISCREPANCY - RT LOWER TORQUE BOX CRACKED AT ST 1230. CORRECTIVE ACTION - STAP DRILLED CRACK .250 TERMINATED AT END OF CRACK ON RH LOWER TORQUE BOX BS1230 IAW B727 SRM 51-10-1. HFEC INSP. PER 727 NDT PT.6 51-00-00 FIG.23 NO CRACKS NOTED BEYOND STOP HOLE. FABRICATED DOUBLER, MAT. USED ID 53-10-2 FIG.6 FROM 7075T6 .032 PO# 900573 DIM. 4"X 3 1/2" IAW B727 SRM 51-40-2 FIG.1. ALODINED & PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED DOUBLER REPAIR IAW SRM 51-40-2 FIG.1. 2L73 4F RTA3WE 20050607000502005060700050NM 2005 6 7 DHL2005740557 120050331A5410 STRUCTURE BOEING727 7272Q9 138448MNM NR 2 NACELLE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 DENT LT SIDE FUSELAGE STA 1374, NR 2 ENGINE SUPPORT STRUCTURE. REMOVED FASTENERS AT LT SIDE FUSELAGE SKIN STA 1374 NR 2 ENGINE SUPPORT STRUCTURE IAW B727 SRM 51-40-2 FIG 1. FABRICATED DOUBLER REPAIR MAT USED 2024T3 .050 PO NR 9002093 SIZE 5 1/4" BY 5 1/4" IAW B727 SRM 51-40-2 FIG 1 AND 54-30-2 FIG 4. ALODINED AND PRIMED PART AND AREA IAW B727 SRM 51-30-2 AND INSTALLED DOUBLER IAW B727 SRM 54-30-2 FIG 4 AND 51-30-2. 2L73 4F RTA3WE 20050607000552005060700055SO 2005 6 7 RAIA00505013 120050516A2740 TRIM SYSTEM EMB 145 EMB145LR 3260212SO STABILIZER MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03811HK 145256 FLT 3567 - PIT - BOTH PRIMARY AND SECONDARY PITCH TRIM INOPERATIVE. MAINTENANCE CYCLED PITCH TRIM CUT OUT SWITCHES AND OPS CHECKED BOTH TRIM SWITCHES WITH NO DEFECTS NOTED. 2L72 4T RTT00011AT 20050607000592005060700059GL 2005 6 7 RAIA00505017 220050519A7230 SPINNER EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL ENGINE SEPARATED A RAIAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 CE03814HK 145046 311524 FLT 5699 - STL - CREW HEARD "BANG" AND UPON INVESTIGATION SAW HOLE IN FAN COWL. ENGINE SHUT DOWN IN FLIGHT. MAINTENANCE REMOVED AND REPLACED ENGINE DUE TO DAMAGE CAUSED BY FAN SPINNER SEPARATION FROM FAN DURING FLIGHT. 2L72 4T4 FRTT00011ATTE6CH 20050607000622005060700062 2005 6 7 BB05040 420050519A2565D30654122 SLIDE BOEING757 757225 1384959NM L1 DOOR DETACHED A USAAK NONE O OTHER ININSP/MAINT 1 EA19608AU 22204 PHL - L1 DOOR SLIDE LIGHT INOPERATIVE. MAINTENANCE REATTACHED THE GIRT BAR CHUTE TO THE SLIDE ASSEMBLY. 2L72 4F RTA2NM 20050607000672005060700067WP 2005 6 7 DHL2005809004 120050521A33505708458505 BATTERY PACK DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT INTERMITTENT A DHLAK NONE O OTHER ININSP/MAINT 1 SO01809DH 46047 EMERGENCY LIGHT WORK INTERMITTENLY DURING PREFLIGHT CHECK. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK ASSY IAW 33-50-1, OPS CK NORMAL. 2L74 4F RT4A25 20050607000682005060700068WP 2005 6 7 U2RA3218 120050523A5311 FRAME DOUG DC8 DC863F 302198FWP FUSELAGE DAMAGED A U2RAK NONE O OTHER ININSP/MAINT 1 GL23921R 684252039 46145 FUSELAGE FRAME DAMAGED AT STATION 1560, L21L. 2L74 4F 4A25 20050607000712005060700071EU 2005 6 7 TXER100777 120050427A3412C16196AB PROBE UROCOPEC155 EC155B 8681000EU OAT BROKEN B TXERO OTHER O OTHER NRNOT REPORTED 1 SW09588CF 6662 PROBE BROKEN. 1G72 3U H10EU 20050607000722005060700072EU 2005 6 7 TXER100778 120050427A3412C16196AB PROBE UROCOPEC155 EC155B 8681000EU OAT BROKEN B TXERO OTHER O OTHER NRNOT REPORTED 1 SW09588CF 6662 PROBE BROKEN. 1G72 3U H10EU 20050607000762005060700076EU 2005 6 7 SSHA100897 120050512A2913A5026780 PUMP AEROSPAS355 AS355* EU TMECA ARRIELARRIEL1 60030NE HYD SYSTEM FAILED E SSHAB EMER. DESCENT F FLT CONT AFFECTED CLCLIMB 1 WP135206J 3100 PILOT REPORTED LOSS OF HYDRAULICS SHORTLY AFTER TAKEOFF. INSPECTION FOUND THAT HYDRAULIC PUMP HAD FAILED INTERNALLY. PUMP WAS REMOVED AND REPLACED. AIRCRAFT WAS RETURNED TO SERVICE. 1G72 3U3 U H11EU E19EU 20050607000852005060700085CE 2005 6 7 DXTA200500733 120050521A2497 WIRE CESSNA500 560CESSNA 2076750CE CARGO BAY BURNED E DXTAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL07315QS 5600315 DURING POSTFLIGHT, SMELLED ACRID ELECTRICAL SMELL INSIDE NOSE BAGGAGE COMPARTMENT. SMELL CAME FROM BEHIND PANEL ON AFT SIDE OF NOSE BAGGAGE COMPARTMENT. PERFORMED WIRE BUNDLE/ELECTRICAL COMPONENT INSPECTION, NO DEFECTS NOTED. ACTIVATED EQUIPMENT, FUNCTION CHECKS GOOD. NO SMELL OF ELECTRICAL BURNING PRESENT. WORK DONE IAW CESSNA CITATION MODEL 560 ULTRA MM CH 20-21-03. 2L72 4F RTA22CE 20050607000902005060700090NM 2005 6 7 ASMF200505019 120050516A2400 GENERATOR DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE LT ENGINE OUT OF ALIGNMENTW ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23831LF 53050 725561 AIRCRAFT RETURNED TO PLATFORM, LT ENGINE DID NOT ACCELERATE, N2 DECREASED BELOW 50 PERCENT AND LT GENERATOR WAS FOUND OUT OF LINE. ACCELERATION CHAMBER WAS DRAINED AND LUBRICATED, LT ENGINE WAS TESTED IAW MM 73-20-03, ALL CORRECT. 2L72 4F4 FRT E9NE 20050607001152005060700115EA 2005 6 7 QXEA200500905 120050505A5230 INSERT CNDAIRCL600 CL6002C10 1390015EA ZONE 800 SPINNING A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FORWARD BAGGAGE DOOR RUBBER MOUNTS FOR INTERNAL PANEL HAVE SPINNING INSERTS. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01. 2L72 4F RTA21EA 20050607001172005060700117EA 2005 6 7 QXEA200500909 120050428A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FUSELAGE INTERIOR LEFT INBOARD FLOOR SEAT RAIL HAS PITTING CORROSION ON INNER SURFACE AT THE FOLLOWING LOCATIONS, STATION 415-417 AND 478. REPAIRED IAW REO 670-53-00-013. 2L72 4F RTA21EA 20050607001222005060700122EA 2005 6 7 QXEA200500910 120050428A5340 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FUSELAGE INTERIOR LEFT INBOARD FLOOR SEAT RAIL HAS PITTING CORROSION AND SCRATCHES AT THE FOLLOWING LOCATIONS: STATION 506-583. REPAIRED IAW REO 670-53-00-013. 2L72 4F RTA21EA 20050607001242005060700124EA 2005 6 7 QXEA200500912 120050428A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FUSELAGE INTERIOR RIGHT SIDE SEAT RAIL HAS SURFACE CORROSION AND GOUGE AT STATION 613.0. REPAIRED IAW REO 670-53-00-013. 2L72 4F RTA21EA 20050607001312005060700131EA 2005 6 7 QXEA200500919 120050505A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FUSELAGE BELLY SKIN HAS IMPACT MARKS BETWEEN STATION 228.42 AND 265.00, LEFT STRINGER 25 AND RIGHT STRINGER 25. REPAIRED IAW REO 670-53-11-062 AND HORIZON AIR EA R-53-332. 2L72 4F RTA21EA 20050607001382005060700138NM 2005 6 7 DL75K050283 120050512A5414 SKIN BOEING757 757232 1384965NM NR 1 PYLON CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27645DL 24216 APPROX 1 INCH CRACK IN PYLON TORQUE BOX INBOARD SIDE, UPPER FWD CORNER OF FWD ACCESS HOLE, PREVIOUSLY STOP DRILLED. REFERENCE NR CARD 291 PSV 17 CHECK. INSTALLED PERMANENT REPAIR PER SRM 54-51-01D FIG 203. 2L72 4F RTA2NM 20050607001422005060700142NE 2005 6 7 DL738050287 220050522A7200 COVER BOEING737 737832 13844CFNM GE CFM56 CFM567B24 NE NR 1 ENGINE LOOSE A DALAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO273758Y11888 30814 889511 NR 1 ENG OIL QTY TOP ZERO. ENG OIL PRESS TO REDLINE. FLT CREW COMPLETED ENG FAILURE SHUTDOWN PER QRH CHECK LIST. UNEVENTFUL SINGLE ENG LANDING AT SLC. NR 1 ENG WINDMILL WITH POS PRESS AT ALL TIMES. FOUND NR 1 ENG TURNING PAD COVER LOOSE. REPLACED O-RINGS ON COVER SERVICED OIL TO FULL RAN ENG AND LEAK CHECKED GOOD. NO EEC FAULTS. NO DMS FAULTS. C/W INFLIGHT ENG SHUTDOWN WINDMILL INSP PER MM, OK FOR SERVICE. 2L72 4F4 FRTA16WE E00055EN 20050607001452005060700145EA 2005 6 7 QXEA200500929 120050428A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FUSELAGE INTERIOR LEFT FLOOR SEAT RAIL HAS GOUGES, PITTING AND SURFACE CORROSION AT THE FOLLOWING LOCATIONS, STATION 695-836.5. REPAIRED IAW REO 670-53-00-013. 2L72 4F RTA21EA 20050607001542005060700154EA 2005 6 7 QXEA200500927 120050428A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FUSELAGE INTERIOR RIGHT SEAT RAIL HAS PITTING AND SURFACE CORROSION AT THE FOLLOWING LOCATIONS, STATION 693-697, 709, 726, 797-800 AND 826-836.5. REPAIRED IAW REO 670-53-00-013. 2L72 4F RTA21EA 20050607001562005060700156EA 2005 6 7 QXEA200500937 120050507A3220 PISTON CNDAIRCL600 CL6002C10 1390015EA ZONE 700 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - NOSE LANDING GEAR PISTON ASSEMBLY HAS CHAFING DAMAGE BETWEEN TORQUE LINK ATTACH LUGS. REPAIRED IAW REO 670-32-21-005, REV A AND HORIZON AIR EA R-32-188. 2L72 4F RTA21EA 20050607001642005060700164NM 2005 6 7 05FDEA00845 120050405A5720AEA7243502 SPLICE DOUG MD11 MD11 3023602NM RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 RIGHT WING I/B FLAP, I/B ACTUATOR ENCLOSURE CUTOUT FOUND FUSELAGE STIFFENER CRACKED. RIGHT WING I/B FLAP, I/B ACTUATOR ENCLOSURE CUTOUT CRACK SPLICE REMOVED AND NEW SPLICE INSTALLED AS PER SRM 51-33-01 VOL II & SRM 51-35-01 VOL II, NEW SPLICE PART NUMBER: FX AEA 7243-502 FABRICATED AS PER DRAWING AEA 7243. 2L73 4F RTA22WE 20050607001682005060700168NM 2005 6 7 QXEA200500950 120050514A5750 SHROUD BOMBDRDHC8 DHC8401 1390041NM ZONE 600 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09412QX 4059 PDX - RIGHT WING INBOARD LOWER TRAILING EDGE SHROUD INBOARD RIVET AT SIXTH BRACKET HAS CRACK AT AFT INBOARD. REPAIRED IAW RD 8/4-57-261. 2H72 4T RTA13NM 20050607001702005060700170NM 2005 6 7 QXEA200500942 120050514A5720 SHROUD BOMBDRDHC8 DHC8401 1390041NM ZONE 600 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09412QX 4059 PDX - RT WING IB, LOWER TRAILING EDGE SHROUD 6TH FORWARD BRACKET FROM IB EDGE IS CRACKED. REPAIRED IAW RD 8/4-57-253 AND Q400 SRM 51-42-15. 2H72 4T RTA13NM 20050607001832005060700183EU 2005 6 7 05FDEA01389 120050520A7120 BUSHING AIRBUS310 A310203 3930313EU ENGINE MOUNT CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25403FE 230 NR 1 ENGINE FWD MOUNT FITTING BOLTS LOWER AND TOP SURFACE OF HOLE HAS LITE CORROSION. REMOVED AND REPLACED 4 EACH BUSHINGS ON NR 1 ENGINE MOUNT PER A310 SRM 54-51-81 PG 205 AND EA 6-5450-89149. REMOVED CORROSION ON UPPER AND LOWER SURFACE AND 4 EA BOLT HOLES PER SRM A310 54-51-81 PG 107/108, 109/110. APPLIED CAD PLATING TO BARE METAL PER PS 01-02-21. APPLIED TOPCOAT PER A310 SRM 54-51-81 PG 103. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR PER FEDEX GMM 6-2-100. 2L72 4F RTA35EU 20050607001932005060700193GL 2005 6 7 SD72005F00000 220050228A732123034702 FUEL CONTROL BELL 206 206A 1181508SW ALLSN 250C 250C20 03013GL ENGINE FAILED E SD7AO OTHER O OTHER NRNOT REPORTED 1 NM116255N 2824 129 CAE821555 PILOT REPORTED DECAY OF N2 RPM WHEN ATTEMPTING TO REAPPLY COLLECTIVE FOLLOWING GRADUAL DECENT IN LOW ALTITUDE CRUISE FLIGHT. PRECAUTIONARY LANDING ACCOMPLISHED. SUBSEQUENT GROUND RUNS SHOWED MAXIMUM ACHIEVABLE N2 RPM OF 80 PERCENT. TEMPORARY REPLACEMENT WITH LIKE PART NUMBER FUEL CONTROL CORRECTED N2 RPM LOSS. EXCESSIVE DROOP STILL NOTED. FUEL CONTROL AND GOVERNOR SYSTEM SUBSEQUENTLY REPLACED BY BENDIX SYSTEM. CECO COMPONENTS SENT FOR INSPECTION AND OVERHAUL. (K) 1G71 3U3 U H2SW E4CE 20050608000032005060800003NE 2005 6 8 2005UALA00443 220050516A7200 ENGINE AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE NR 1 FLAMED OUT A UALAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 WP2954UA 1731 V10667 NR 1 ENGINE FLAMED OUT AT FL360. ALL PARAMETERS ROLLED BACK TOGETHER. RESTARTED AT FL 200. THE PMA S/N FAAG6915FL03 ARRIVED AT SFOEP ON 5/26/2005. THE PMA SHAFT WAS IN ONE PIECE, THE NUT P/N NAS1291C7 WAS STILL IN PLACE, HOWEVER, P/N 4B0286 HAD A FREE RUN. IT APPEARED THAT ALL THE GEAR SPLINES WERE GONE ON THE SHAFT. THE EXISITING BREAKING TORQUE OF THE NUT WAS 30 IN-LBS VERSUS 509-550 IN-LBS. IAE AND UAL ARE CURRENTLY DISCUSSING POSSIBLE LONG TERM DESIGN FIXES TO THIS PROBLEM. 2L72 4F4 FRTA28NM E40NE 20050608000042005060800004NM 2005 6 8 2005UALA00444 120050514A2530 THERMISTER BOEING777 777222 1385219NM COFFEEMAKER DAMAGED A UALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP29206UA 0752 30212 BANG THEN SMOKE COMING OUT OF TOP OF COFFEEMAKER. STRONG ELECTRICAL BURNING ODOR. MANUFACTURERS OF COFFEEMAKER AND RELAY CONFIRM FAILURE OF THE ELECTROMECHANICAL RELAY WHICH HAD REACHED ITS SERVICEABLE LIFE. RELAY FAILURE LED TO WATER TANK OVERHEAT AND MELTING OF THE THERMISTOR POTTING COMPOUND. THERMISTOR ELECTRICAL LEAD AND MELTING COMPOUND BELIEVED TO BE SOURCE OF SMOKE. 2L72 4F RTT0001SE 20050608000052005060800005NM 2005 6 8 2005UALA00445 120050516A5230 SKIN BOEING737 737322 1384676NM CARGO DOOR DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29312UA 23673 FWD CARGO DOOR EXTERNAL SKIN HAS SEVERAL DENTS INSIDE THE AREA OF FWD EDGE. REMOVED DAMAGE AND INSTALLED DOUBLER REF SRM 52-30-01 AND SRM 52-00-01 DURING DOOR OVERHAUL DURING HMV4. 2L72 4F RTA16WE 20050608000062005060800006NM 2005 6 8 05FDEA01380 120050520A5713 STRINGER BOEING727 727200 138407ENM RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 RT WING UPPER STR 10 CRACKED AT WS 686.5 REPAIRED STRINGER PER FED EX EA 7-5710-86294. 2L73 4F RTA3WE 20050608000102005060800010WP 2005 6 8 UPS05844571 120050601A5610 WINDSHIELD DOUG DC8 DC871F 302199DWP COCKPIT FAILED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 F/O'S WINDSHIELD SHATTERED WHEN TURNED ON. APPLIED SEALANT TO F/O WINDSHIELD, REF MM 56-10-02-2. D303437 CLOSED 2L74 4F RT4A25 20050608000682005060800068EU 2005 6 8 MALA050433 120050519A5311 FRAME BAC 146 AVRO146RJ85A1500097EU FUSELAGE SCRATCHED A MALAK NONE O OTHER ININSP/MAINT 1 GL15519XJ E2344 DURING LINE CHECK AFTER C3 INSPECTION FOUND SCRATCH IN FUSELAGE AT FRAME 23 LT .004 MATERIAL LOSS CLASS A DENT PER AVMAX. 2H74 4F RTA49EU 20050608000742005060800074NM 2005 6 8 SWAA051448 120050518A53306545777 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 953, STR 21L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050608000762005060800076 2005 6 8 SWAA051450 420050518A25656970843 LATCH BOEING737 7373H4 1384600NM GIRT BAR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29642WN 27715 DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR LATCH ASSY OUT OF ADJUST. ADJUSTED LATCH ASSY PER MM. 2L72 4F RTA16WE 20050608000782005060800078NM 2005 6 8 SWAA051452 120050518A335065C27093 LIGHT BOEING737 7373H4 1384600NM R1 DOOR INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29650SW 27720 DURING SCHEDULED SERVICE CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REPAIRED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20050608000882005060800088NM 2005 6 8 SWAA051462 120050519A53116546559 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29664WN 23495 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 928, STR 25R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050608000902005060800090NM 2005 6 8 SWAA051464 120050519A53306545777 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29664WN 23495 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 948, STR 25R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050608000922005060800092NM 2005 6 8 SWAA051466 120050519A33506556633 LIGHT BOEING737 7373T5 1384608NM MID CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29696SW 23064 DURING SCHEDULED RON CHECK, FOUND RT OVERWING EMERGENCY WALL LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20050608000972005060800097CE 2005 6 8 FFS2005F00004 120050505A2730 BELLCRANK BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA HARTZLHCB4M HCB4MP3 GL ELEVATOR MISMANUFACTURED A FFSAK NONE W INADEQUATE Q C ININSP/MAINT 1 AL01575F UC99 IN ATTEMPTING TO RIG THE ELEVATOR SYSTEM, IT WAS DISCOVERED THE RIGGING HOLE FOR THE FORWARD ELEVATOR BELLCRANK WAS DAMAGED IN THE UPPER ELEVATOR BELLCRANK SUPPORT. IT APPEARED THAT THE HOLE HAD BEEN TORN BY MOVEMENT OF THE BELLCRANK WITH THE RIG PIN INSTALLED. ADDITIONALLY IT WAS DISCOVERED THAT THE RIGGING HOLE IN THE LOWER BELLCRANK SUPORT DID NOT EXIST, IE. IT HAD NEVER BEEN DRILLED. (K) 2L72 4T4 TRTA24CE E4EA 6 CP56GL 20050608000982005060800098EU 2005 6 8 SIMA200512506 120050428A5330AL2024T3 SKIN SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE FUSELAGE DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21316CE23597 340B348 AIRCRAFT ARRIVED FOR REPAIR OF DAMAGE TO THE LT AFT FUSELAGE BETWEEN STA 6980 AND 720 AND BETWEEN STRINGERS 1516 AND 1518. PERFORMED A 20.6 INCH X 2.75 INCH CUT OUT OF THE DAMAGED AREA FROM STA 693 TO 713.6 AND PERFORMED A NDT INSPECTION. FABRICATED 3 SHIMS, DOUBLER, TRIPLER AND 2 FRAME STIFFENERS. REPAIR DONE IAW MFG REPAIR STATEMENT 340SDS008364. (K) 2L72 4T4 TRTA52EU E8NE 20050608000992005060800099NM 2005 6 8 DHL2005741526 120050421A5311 FRAME BOEING727 7272Q9 138448MNM FUSELAGE BENT A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH46665 21931 FRAME BENT AT FUSE STA 680 STR 24R. FOUND DENT TO BE OUT OF LIMITS ON STA 680 STR 24R IAW B727 SRM 53-10-1 FIG 1 SIZE 2 INCHES BY 2 1/2 INCHES CUTOUT FABRICATED ANGLE REPAIR FROM 7075T6 .071 SIZE 12 INCHES BY 3 INCHES PO NR 900573 IAW B727 SRM 51-40-3 FIG 1. TREATED AND PRIMED PART AND AREA IAW B727 SRM 51-10-2. INSTALLED REPAIR ANGLE IAW B727 SRM 51-40-3. 2L73 4F RTA3WE 20050608001022005060800102NM 2005 6 8 DHL2005741527 120050421A5311 FRAME BOEING727 7272Q9 138448MNM FUSELAGE BENT A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH46665 21931 BENT FRAME AT STA 500 STR 25R. CUT OUT DAMAGED AREA DIM 3 INCHES BY 1/8 INCHES ON FRAME STA 500 STR 25R IAW B727 SRM 51-10-1. FABRICATED REPAIR ANGLE FROM 7075T6 .063 SIZE 13 3/8 INCHES BY 3 1/8 INCHES PO NR 9001660 IAW B727 SRM 51-40-3 FIG1. TREATED AND PRIMED PART AND AREA IAW B727 SRM 51-10-2. INSTALLED REPAIR ANGLE IAW B727 SRM 51-40-3 FIG 1. 2L73 4F RTA3WE 20050608001032005060800103EU 2005 6 8 05FDEA01477 120050527A2910 O-RING AIRBUS310 A310203 3930313EU HYDRAULIC SYS CUT A FDEAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO25402FE 201 ECAM ALERTED HYD RSVR LO LEVEL ON GREEN SYSTEM. ALL INDICATIONS (GAUGE, ECAM SYNOPTIC) SHOWED AND VERIFIED. QRH CONSULTED AND COMPLIED WITH MANUAL GEAR GRAVITY EXT PROCEDURES ACCOMPLISHED. TOWED TO GATE DUE NO NOSE WHEEL STEERING. T/S FOUND HYD LEAK FROM GREEN HYD MANIFOLD FITTING FOUND O-RING CUT. REPLACED O-RING PER SMP. LEAK CHECK GOOD. RESTORED LANDING GEAR FREEFALL SYSTEM TO NORMAL OPERATING CONDITION PER A310MM CHP 32-33-00-2 PG 201-202. 2L72 4F RTA35EU 20050608001052005060800105WP 2005 6 8 05FDEA01480 120050530A5730 SKIN DOUG DC10 DC1010 3022110WP RT WING DAMAGED A FDEAO OTHER O OTHER UKUNKNOWN 1 SO25571FE 47830 RIGHT WING, INBOARD FLAP, UPPER SKIN WITH EXISTING REPAIR WITH DEFORMED AREA. REMOVED EXISTING REPAIR PER SRM 51-35-01, PAGE 1/13. CUT OUT DAMAGED AREA PER SRM 57-10-00, PAGE 85. PERFORMED NEW REPAIR PER SRM 57-10-00, PAGE 85. 2L73 4F A22WE 20050608001072005060800107WP 2005 6 8 05FDEA01481 120050530A5730 SKIN DOUG DC10 DC1010 3022110WP LT WING NICKED A FDEAO OTHER O OTHER UKUNKNOWN 1 SO25571FE 47830 LEFT WING LEADING EDGE, STA XORS 164 WITH NICKS. REPAIRED DAMAGED LEADING EDGE IAW SRM 57-10-00, FIG 28. 2L73 4F A22WE 20050608001082005060800108NM 2005 6 8 05FDEA01482 120050530A5320 SPLICE DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 CENTER CARGO, STA 1536 LONGERON 49L SPLICE FOUND CRACKED A5A7114-511. CRACKED LONGERON 49L SPLICE REMOVED AND REPLACED WITH NEW FABRICATED SPLICE PER DWG A5A7114 AND SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2L73 4F RTA22WE 20050608001092005060800109NM 2005 6 8 2005UALA00460 120050520A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29502UA 24623 AFT PIT FRAME PREVIOUS REPAIR IS CORRODED AT STA 1600 - STR 25L TO 27L. REMOVED DAMAGE AND FABBED NEW PRODUCTION SPLICE AND ANGLE REPAIR AND INSTALLED PER REO-G10504B AND SRM51-40-02 AND EVA-50287. 2L72 4F4 FRTA2NM E17NE 20050608001112005060800111NM 2005 6 8 2005UALA00462 120050520A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE GOUGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29502UA 24623 FRAME STA 1520 FROM STR 22R TO 25R IS GOUGED FROM SCREWS IN 6 PLACES. REMOVED DAMAGE AND ACP HFEC NO CRACKS INDICATED. PER REO G10474 FABRICATED NESTLED ANGLE REPAIR AND INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050608001122005060800112NM 2005 6 8 2005UALA00463 120050520A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29502UA 24623 AFT PIT FUSELAGE FRAME IS DENTED AT STA 1520, STR 25L. REMOVED DAMAGE AND INSTALLED J ANGLE REPAIR PER RE0-G10463, EVA-50283, AND SRM51- 40-02. 2L72 4F4 FRTA2NM E17NE 20050608001132005060800113NM 2005 6 8 2005UALA00464 120050520A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29502UA 24623 FUSELAGE SKIN DENTED STA 600 STR 17L DENT IS APPROX 3 INCHES BY .067 DEEP. RMV DAMAGE AREA AND ACP HFEC WITH NO CRACK INDICATION FABRICATED REPAIR AND INSTALLED PER MM 53-30-92 2L72 4F4 FRTA2NM E17NE 20050608001152005060800115NM 2005 6 8 2005UALA00466 120050520A5320 DOUBLER BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29502UA 24623 AFT CABIN FLOOR SHEAR WEB DOUBLER IS CORRODED STA 1681, RBL 48-55. REMOVED EXISTING REPAIR, REMOVED CORROSION INSTALLED DOUBLER REPAIR PER REO-G10512C AND SRM51-20-01 2L72 4F4 FRTA2NM E17NE 20050608001172005060800117 2005 6 8 2005UALA00468 420050521A2565 SLIDE BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE LEFT DEFECTIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29674UA 29242 DURING REMOVAL OF THE LEFT OVER WING SLIDE IT WAS FOUND TO BE DEFECTIVE. 2L72 4F4 FRTA1NM E24NE 20050608001192005060800119NM 2005 6 8 2005UALA00470 120050520A5313 STRINGER BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29313UA 23674 AFT PIT STA787+2 TO 787+4 STR 25L UPPER FLANGE IS EXFOLIATED LBL24-24. FABRICATED AND INSTALLED PARTS PER SRM 53-00-03. 2L72 4F4 FRTA16WE E2GL 20050608001212005060800121NM 2005 6 8 2005UALA00472 120050414A2530 RECEPTACLE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE GALLEY FAILED A UALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 WP29371UA 24540 AFT VACUUM CB OUT. FA REPORTED SPARKS IN GALLEY POPPED. FAILED RECEPTACLE NOT RECOVERED. AMT SAYS FOUND IT IN TWO PIECES. CAUSE OF FAILURE MAY BE DETERIORATION OVER TIME. INCONCLUSIVE WITHOUT FAILED PART. 2L72 4F4 FRTA16WE E2GL 20050608001232005060800123 2005 6 8 2005UALA00474 420050523A2565 ASPIRATOR AIRCRUISERS D31516113 AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE EVAC SLIDE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29430UA A6909 568 FOUND ASPIRATOR CRUSHED, FLAPS STUCK AND HOLE IN ASPIRATOR. THE PROBABLE CAUSE OF ASPIRATOR DAMAGE IS INCORRECT PREVIOUS PACKING OF THE SLIDE ASSEMBLY THAT RESULTED IN THE ASPIRATOR DEFORMATION. THE SHOP REPORT THAT THE SLIDE WOULD NOT HAVE DEPLOYED IS UNFOUNDED. THE ASPIRATOR MIGHT STILL FUNCTION WITH LESS EFFICIENCY THAN THE DESIGN IF THERE WAS A DEPLOYMENT BUT THAT WOULD MEAN LONGER TIME FOR THE SLIDE TO INFLATE. THE ASPIRATOR WAS REPLACED WITH A SERVICEABLE ONE. 2L72 4F4 FRTA28NM E40NE 20050608001242005060800124NM 2005 6 8 2005UALA00475 120050525A3350 STRIP BOEING777 777222 1385219NM PWA PW4077PW4077 NE CABIN DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29771UA 26932 3E SEAT PATH EMERGENCY LIGHTING STRIP RIPPED OFF BY FA. MISSING EMERGENCY LIGHT WAS REPLACED. 2L72 4F4 FRTT0001SE E46NE 20050608001262005060800126NM 2005 6 8 2005UALA00477 120050525A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE MISDRILLED A UALAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP29559UA 26657 LT FUSE SKIN AT STA 1181 STR 16L HAS DRILL DAMAGE. REMOVED DAMAGED AREA AND FABRICATED FREEZE PLUG AND DOUBLER PER REO G09831 AND EVA-40157 2L72 4F4 FRTA2NM E17NE 20050608001272005060800127NM 2005 6 8 2005UALA00478 120050524A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29559UA 26657 FUSELAGE FRAME AT STA 600 BETWEEN STR 24L AND 24L REQUIRE DTA TO BE ACCOMPLISHED. REMOVED FRAME SECTION AND FABRICATED REPAIR PARTS PER REO G09843 REV 1. 2L72 4F4 FRTA2NM E17NE 20050608001282005060800128NM 2005 6 8 2005UALA00479 120050524A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29560UA 26660 AFT PIT FUSELAGE FRAME IS DENTED AT STA 1440 LT AT FLOOR TRANSITION PANEL. DAMAGE IS ON INBOARD FLANGE IN TWO PLACES. FRAME HAS BEEN REPAIRED PER TIMCO REO G-09850, REV A, WITH A J-ANGLE PER EVA 40168. 2L72 4F4 FRTA2NM E17NE 20050608001302005060800130EU 2005 6 8 SIMA200513101 120050508A33206500110 SOCKET SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE CABIN LIGHTING BURNED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21381AE 340B381 CREW REPORTED THE WINDOW LIGHT SOCKET BURNED AT ROW 9A. MAINTENANCE REPLACED THE FLUORESCENT LAMP HOLDER AND LAMP OVER SEAT 9A IAW MM. OPS CHECK WAS GOOD AND AC WAS RETURNED TO SERVICE. (SW21200501028) (K) 2L72 4T4 TRTA52EU E8NE 20050608001312005060800131NM 2005 6 8 2005UALA00481 120050526A3150 WARNING SYSTEM BOEING747 747422 1384935NM PWA 4056 PW4056 NE COCKPIT ACTIVATED A UALAO OTHER N FALSE WARNING UKUNKNOWN 1 WP29187UA 26877 EVAC ALARM ACTIVATED. DOOR 1 RH COMMAND SWITCH IN ON POSITION. MECHANICS FOUND THAT DOOR 1 RIGHT COMMAND SWITCH WAS IN THE "ON" POSITION. SELECTED THE SWITCH TO THE "OFF" POSITION AND THE SYSTEM CHECKED OUT NORMAL. NO OTHER HITS SINCE. 2L74 4F4 FRTA20WE E24NE 20050608001352005060800135NM 2005 6 8 05FDEA01484 120050530A3211 SUPPORT DOUG MD11 MD11 3023602NM LANDING GEAR CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 CENTER LANDING GEAR, RIGHT HAND TRUNNION SUPPORT FITTING PILLOW BLOCK MATING SURFACE CORRODED. REMOVED AND REPLACED AS PER CMM 32-15-01. 2L73 4F RTA22WE 20050608001372005060800137NE 2005 6 8 05FDEA01487 220050530A7230 FLANGE DOUG MD11 MD11 3023602NM GE CF6 CF680C2D1F 30025NE NR 2 ENGINE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 NR 2 ENGINE, WHILE CARRYING OUT FEDEX EA 1-7223-74401 PART 2 ENGINE - AFT FAN CASE T-FLANGE GROUND HANDLING MOUNT CRACK DRILL STOP. FOUND FORWARD T-FLANGE AND AFT T-FLANGE CRACKS PROPAGATED. REPAIRED PER AMM 72-33-00-300-801. 2L73 4F4 FRTA22WE E31N3 20050608001392005060800139NM 2005 6 8 AALA20050344 120050523A3350 LIGHT BOEING757 757223 1384957NM SEAT 9L BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21698AN 26980 DFW - EMERGENCY LIGHT ASSEMBLY AT SEAT 9L BROKEN AND EMERGENCY LIGHT ASSEMBLY AT SEAT 25C MISSING. REPLACED EMERGENCY LIGHT ASSEMBLY FOR SEAT 9L AND 25C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050608001402005060800140NE 2005 6 8 05FDEA01489 220050530A7200 CASE DOUG MD11 MD11 3023602NM GE CF6 CF680C2D1F 30025NE NR 2 ENGINE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 NR 2 ENGINE, RIGHT HAND CASE APPROXIMATELY TWO O' CLOCK POSITION CRACKED, FOUND ON FLANGE AT BORE COOLING VALVE LOWER FASTENER HOLE. COMPLIED WITH FEDEX EA 1-7223-90165. 2L73 4F4 FRTA22WE E31N3 20050608001422005060800142WP 2005 6 8 AALA20050346 120050521A3350P4010049 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21570AA 49352 ORD - MOST EMERGENCY ESCAPE PATH LIGHTS IN CABIN INOPERATIVE. REPLACED FORWARD AND MID BATTERY PACKS FOR EMERGENCY ESCAPE PATH LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050608001442005060800144WP 2005 6 8 I5HA0558002 120050306A71206825231A TIE CVAC 580 580 2422806WP ALLSN 501D 501D13 03004GL RT ENGINE CRACKED A I5HAO OTHER O OTHER NRNOT REPORTED 1 GL23585P 163 DURING A ROUTINE INSP, A CRACK WAS DISCOVERED AT THE POWER SECTION END ON THE IB TIE STRUT ON THE RT ENGINE. CRACK WAS LOCATED IN THE WELD AREA ON THE END CLOSEST TO THE POWER SECTION. A THROUGH INSPECTION WAS DONE ON THE REST OF THE ENGINE FOR EVIDENCE OF OTHER CRACKS. NONE WERE FOUND AND THERE WAS NO INDICATION OF ENGINE VIBRATIONS. THE IB AND OB TIE STRUTS AND THE ASSOCIATED FITTING ON THE IB SIDE OF THE POWER SECTION WERE REMOVED AND REPLACED. THE LT ENGINE TIE STRUTS WERE INSPECTED FOR CRACKS. NONE WERE FOUND. THE AC WAS RETURNED TO SERVICE . MFG WAS CONTACTED AD INFORMED US THAT THERE HAVE BEEN PROBLEMS WITH CORROSION FORMING AND CAUSING CRACKS IN THE WELD AREAS OF THE TIE STRUTS. (K) 2L72 4T4 TRT E282 20050608001472005060800147NM 2005 6 8 05FDEA01491 120050529A2910 HYDRAULIC LINE DOUG MD11 MD11 3023602NM HYDRAULIC SYS LEAKING A FDEAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO25603FE 48459 ABOUT 2.5 HRS FROM TOUCHDOWN, GOT LEVEL 1 HYD 3 OFF, FOLLOWED BY LEVEL 2 HYD 3 FAIL. LOST ALL HYD 3 QTY FOLLOWED QRH PROCEDURES AND DID ALT GEAR EXTENSION. A/C TOWED TO GATE FROM RUNWAY. FLEX LINE INSTALLED IN HYD SYSTEM NR 3 LOCATED AT TRIM MOTOR VALVE BLOCK, HORZ STAB REMOVED AND REPLACED NR 3 ENGINE DRIVEN PUMP PER AMM 29-11-20-4 AND CASE DRAIN MANIFOLD FILTERS FOR LT (UPPER) EDP PER AMM29-12-41-2. BLED EDP AND SUPPLY LINES PER AMM 29-03-00-2. DRY MOTOR THE ENG PER AMM 71-00-00-51 AND PERFORMED LEAK CHECK SATISFACTORY. 2L73 4F RTA22WE 20050608001482005060800148NM 2005 6 8 05FDEA01492 120050530A5713 STRINGER DOUG MD11 MD11 3023602NM LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 LEFT HAND WING LOWER FUEL TANK AT XORS= 733, S-38 FOUND STRINGER END CRACKED. TRIMMED OUT AND INSTALLED WITH FABRICATED SPLICE ANGLE AS PER SRM 57-20-00 FIGURE 10 VOLUME I. NDT INSPECTION AT TRIMMED OUT AREA FOUND NO CRACK EVIDENT. REPAIR CLASSIFIED AS MAJOR REPAIR PER GMM 6-2-100. 2L73 4F RTA22WE 20050608001522005060800152NM 2005 6 8 05FDEA01495 120050530A5347 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 MAIN DECK, SEAT TRACK AT STA 635 LBL = 9 FOUND CRACKED. REMOVED AND REPLACED WITH REWORKED SEAT TRACK AS PER SRM 53-70-00 VOLUME I, FIGURE 1. 2L73 4F RTA22WE 20050608001562005060800156WP 2005 6 8 ASMF200505022 120050521A3241 CONTROL UNIT DOUG DC9 DC987 3022087WP ANTI SKID SYS MALFUNCTIONED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23204AM 49404 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF ANTI SKID LIGHTS TURNED ON. THE CIRCUIT BREAKER AND ANTI SKID MODULE WERE RESEATED WITH NEGATIVE RESULTS, THE AUTO BRAKE SYSTEM WAS RESEATED IAW MM 32-43-00, TESTED CORRECT. DURING OVERNIGHT SERVICE, THE ANTI-SKID CONTROL BOX WAS TESTED IAW MM 32-43-04, ALL CORRECT. 2L72 4F RTA6WE 20050608001582005060800158NM 2005 6 8 ASMF200505024 120050522A80123927965 SHUTOFF VALVE DOUG MD80 MD83 3023681NM LT ENGINE FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23945AS240463727 49643 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE, DURING LEFT ENGINE STARTED, THE START VALVE OPEN LIGHT DID NOT TURN OFF. THE CIRCUIT BREAKERS WERE RESEATED, CROSS FEED AND CONNECTORS WERE CHECKED AND FAILURE CONTINUED. THE REPORT WAS DEFERRED IAW MEL 80-1. DURING TRANSIT SERVICE START VALVE WAS REPLACED IAW MM 80-10-02, TESTED CORRECT. DEFERRED REPORT WAS CLOSED. 2L72 4F RT 20050608001622005060800162 2005 6 8 E812005F00000 420050426A3444 COMPUTER BEECH MU300 400A 1155402CE TAWS MALFUNCTIONED B E81RO OTHER O OTHER NRNOT REPORTED 1 GL03438LX RK202 TROUBLESHOT PILOT REPORT OF TAWS SYSTEM AND RADAR INOPERATIVE. FOUND TAWS8000 SYSTEM LOCKED UP. NO RESPONSE WHEN COMPUTER CONNECTED FOR TROUBLESHOOTING. REPLACED TAWS8000 UNIT WITH REPAIRED UNIT, SYSTEM OPERATIONS NORMAL. FOUND RADAR INOPERATIVE DUE TO REMOTE RELAY REMOVING RADAR SOURCE FROM SYSTEM DUE TO TAWS8000 SYSTEM FAILURE. RADAR OPERATIONS RETURNED TO NORMAL WITH TAWS SYSTEM CIRCUIT BREAKER PULLED. TRANSIENT AIRCRAFT, MAINTENANCE RECORDS NOT AVAILABLE. (M) 2H72 4F RTA16SW 20050608001642005060800164WP 2005 6 8 ASMF200505025 120050522A2612892809040002 FIRE LOOP DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE RT ENGINE FAILED W ASMFO OTHER N FALSE WARNING NRNOT REPORTED 1 SW23755RA 49727 725634 DURING TRANSIT CHECK, FIRE ALARMS IN BOTH ENGINES DID NOT OPERATE AND ONLY LIGHTS TURNED ON. DURING REVISION DETECTED FIRE WARNING AURAL SWITCH OPERATED CORRECTLY. AMPLIFIER CONNECTORS WIRING WAS VERIFIED, SYSTEM CHECKED OKAY. DURING REVISION DETECTED THE RIGHT ENGINE AMPLIFIER WITH FAILURE. AMPLIFIER DETECTOR UNIT A2-6 WAS REPLACED, TESTED CORRECT. REJECTED TAKEOFF AS A CONSEQUENCE OF RIGHT ENGINE DID NOT REACH TAKEOFF EPRS OF 1.98, IT STAYED IN 1.80 EPR INCREASING EGT TEMPERATURE. AIRCRAFT SENT TO HANGAR, PT7 & PT2 LEAK CHECK PERFORMED, PRBC LINES TIGHTENED, ACCELERATION CHAMBER AND ANTI SURGE VALVES WERE LUBRICATED, RUDDER PT2 UNION REPLACED AND REMOTE CONTROL TRIM PERFORMED, TESTED CORRECT. 2L72 4F4 FRTA6WE E9NE 20050608001662005060800166WP 2005 6 8 ABXA050130 120050520A53305910228 SKIN DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 FUSELAGE SKIN CRACKED FS 1090, APPROXIMATELY 4 INCHES TO THE LEFT OF VERTICAL STAB. MANUFACTURED REPAIR DOUBLER FROM 2014-T6 .063 PO 408448187. REPAIRED AREA IAW DC-9 SRM 53-01. 2L72 4F A6WE 20050608001672005060800167 2005 6 8 ABXA050122 420050520A2565101623303 SLIDE BOEING767 767281 1385109NM PAX DOOR DEPLOYED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23774AX139 22789 LIFE RAFT SLIDE DEPLOYED WITHOUT BEING ARMED. THE LOWER FORWARD ENTRY DOOR HUNG WHILE TRYING TO CLOSE IT. WHEN THE DOOR WAS RAISED FOR RE-CLOSURE, THE SLIDE DEPLOYED. INSPECTED DOOR AND GIRT BAR ATTACHMENTS. NO DEFECTS NOTED. REMOVED AND REPLACED SLIDE ASSEMBLY IAW B767 MM 25-66-01. 2L72 4F RTA1NM 20050608001722005060800172WP 2005 6 8 ABXA050124 120050509A3350 BATTERY DOUG DC9 DC941 302207NWP EMERGENCY LIGHT INOPERATIVE A ABXAK NONE O OTHER ININSP/MAINT 1 GL23963AX 47780 EMERGENCY EXIT LIGHTS WOULD NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERIES IAW DC-9 AMM 33-53-02-4. OPS CHECKED GOOD. 2L72 4F A6WE 20050608001732005060800173EA 2005 6 8 A6WA200540170 120050515A3211601R5721003L BUSHING CNDAIRCL600 CL6002B19 1900309EA LT MLG MIGRATED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31454AW 7842 LEFT MLG FORWARD TRUNNION AFT BUSHING MIGRATED ON OUTBOARD EDGE .0015. INSTALLED NEW BUSHINGS, P/N 601R-57-21-003-41, IN FORWARD TRUNNION IAW BOMBARDIER, INC REO 601R-57-21-003-REV B. (M) 2L72 4F RTA21EA 20050608001762005060800176WP 2005 6 8 ABXA050127 120050520A53305910228 SKIN DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 FUSELAGE SKIN CRACKED FS 1090, ONE O'CLOCK POSITION FACING AFT. CRACK APPROXIMATELY 2.5 INCHES LONG, LEFT SIDE OF VERTICAL STABILIZER. MANUFACTURED REPAIR DOUBLER FROM 2014T6 .063 PO 408448187. REPAIRED AREA IAW DC-9 SRM 53-01. 2L72 4F A6WE 20050608001792005060800179WP 2005 6 8 ABXA050128 120050521A53229911840166 SHEAR TIE DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 SHEAR TIE CRACKED AT STA 1090, 8 INCHES OUTBOARD OF RT CENTER LINE. REMOVED AND REPLACED SHEAR TIE AT STA 1090 IAW DC-9 SRM 51-30-5 AND 53-30-2. 2L72 4F A6WE 20050608001812005060800181EA 2005 6 8 A6WA200540169 120050504A533046891 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE LIGHTNING STRIKEA A6WAK NONE O OTHER ININSP/MAINT 1 GL31451AW 7832 PERMANENT REPAIR IS REQUIRED FOR LIGHTNING STRIKE DAMAGE AT FS 364, STRINGER 8L. REPAIRED LIGHTNING STRIKE DAMAGE TO FUSELAGE IAW BRAS EO 601R-53-6363A. (M) 2L72 4F RTA21EA 20050608001832005060800183NM 2005 6 8 DHL2005740565 120050324A5532 SKIN BOEING727 7272Q9 138448MNM VERTICAL STAB DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 VERT STAB ABOVE RT FIN STA 133 LOWER RUDDER SURF IS DENTED NEAR T/E. EVALUATED DENTED AREA AT VERT STAB ABOVE RT FIN STA 133 LOWER RUDDER SURF TRIM OUT DAMAGED SKIN SIZE 1/2" BY 3/4" IAW B727 SRM 55-30-3 AND 51-10-1. FABRICATED DOUBLER REPAIR SIZE 2" BY 2.5" MAT USED 2024-T3 .032 PO 9002034 IAW B727 SRM 55-20-3 FIG 1. APPLY ALODINE AND PRIME IAW B727 SRM 51-10-2. INSTALLED DOUBLER REPAIR AT VERT STAB BELOW FIN STA 133 LOWER RUDDER SURFACE IAW B727 SRM 51-30-2 AND 55-20-3 FIG 1. 2L73 4F RTA3WE 20050608001872005060800187SW 2005 6 8 KBM2005F00086 120050409A79312060751881 GAUGE BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL ENG OIL PRESSUREINOPERATIVE A KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19667JM 3444 ENGINE OIL PRESSURE GAUGE, ENGINE OIL PRESSURE EXCEEDS HIGH RED LINE, REMOVED AND REPLACE. 1G71 3U3 U H2SW E4CE 20050608001922005060800192WP 2005 6 8 0500799977 120050525A2170 CLAMP DOUG DC9 DC931 3022065WP WATER SEPARATOR SEPARATED A NWAAO OTHER J WARNING INDICATION CRCRUISE 1 GL019341 47390 DURING CRUISE AT FL330, THE AIRCRAFT LOST CABIN AUTO PRESSURIZATION AND CREW COULD NOT MAINTAIN IT IN MANUAL EITHER. FLIGHT PERFORMED AN EMERGENCY DESCENT TO 10,000 FEET AND DIVERTED TO A NORMAL SAFE LANDING AT ATL. CABIN ALTITUDE MADE IT TO 12,000 FT DURING DESCENT. MAINTENANCE DISCOVERED A LOOSE COUPLING AT THE AFT END OF THE LEFT WATER SEPARATOR. THE COUPLING WAS RESECURED, THE VESSEL WAS LEAK CHECKED, AND NO PROBLEMS WERE FOUND. THE AIRCRAFT HAS RETURNED TO SERVICE. 2L72 4F A6WE 20050608001962005060800196NM 2005 6 8 DHL2005741530 120050427A5310 DOOR FRAME BOEING727 7272Q9 138448MNM FUSELAGE CHAFED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH46665 21931 MAIN CARGO DOOR CUT-OUT FRAME CHAFED AT AFT LOWER CORNER AS MARKED AT BS 620L. CLEANED AREA FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 1. REMOVED SKIN, SIDE GUIDE AND WEDGE IAW B727 SRM 51-30-2 FIG 7. LOCATED, DRILLED AND TRIMMED INNER SKIN WEB AND SIDE GUIDE AT BS620 IAW AEISTC CHAPTER 52 PAGE 52 FIG 5211. TREATED AND PRIMED NEW PARTS IAW B727 SRM 51-10-2. INSTALLED INNER SKIN AE727-1-032A-17 PO NR 509681,WEDGE AE-5083-11, PO NR 509681 AND SIDE GUIDE PN-AE4109-11 PO NR 509681 IAW AEI CHAPTER 52 PAGE 52 FIG 5211 CHAPTER 25 PAGE 60 FIG 2517. 2L73 4F RTA3WE 20050608001992005060800199EA 2005 6 8 A6WA200540181 120050524A5753 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE T/E FLAP DENTED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31455AW 7848 LT IB FLAP HAS A DENT 22 INCHES FROM IB EDGE AND 14 INCHES FROM THE DENT IS 2 INCH X 2 INCH X 0.55 INCH. LOWER SKIN. PERFORMED A MAJOR REPAIR B4 INSTALLING A 8 INCH X 16 INCH NON-FLUSH REPAIR. (K) 2L72 4F4 FRTA21EA E15NE 20050608002002005060800200NM 2005 6 8 05FDEA00650 120050328A5312AGA71704 BULKHEAD DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 AFT CARGO HAS EXFOLIATING CORROSION AT STA 1841 BULKHEAD LT SIDE X = 24. AFT CARGO AT STA 1841 BULKHEAD LT SIDE X:24 REPAIRED AREA AS PER SRM 53-00-01 VOL I FIG 10. MINOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050608002012005060800201EU 2005 6 8 095332 120050409A6120 AUTOCOARSEN SYS SAAB SF340 SF340A 7850100EU COCKPIT UNKNOWN A UHLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL1743SZ 340A043 FLIGHT 7892 HPN IAD, AUTOCOARSEN LIGHT ON STATUS PANEL WENT OUT WHEN CTOT WAS ENGAGED AND T/O POWER WAS SET. 2L72 4T RTA52EU 20050608002022005060800202EU 2005 6 8 200506011 120050601A3260 WARNING LIGHT SAAB SF340 SF340A 7850100EU COCKPIT ILLUMINATED A UHLAK NONE J WARNING INDICATION CLCLIMB 1 GL17121CQ 121 FLIGHT 7881 SCE/IAD, GEAR UNSAFE LIGHT STAYED ON AFTER DEPARTURE. CYCLED GEAR, LIGHT STAYED ON, FLIGHT CONTINUED TO IAD. 2L72 4T RTA52EU 20050608002032005060800203EU 2005 6 8 UPS05144567 120050527A3350 LIGHT AIRBUS300 A300B4622R 3930312EU CABIN INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01159UP 0848 INSPECTION TYPE:N/A LAV EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT. 2L72 4F RTA35EU 20050608002042005060800204NM 2005 6 8 UPS05644568 120050528A2560 SMOKE GOGGLES BOEING767 76734AF 1385212NM COCKPIT DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01316UP 27744 INSPECTION TYPE:N/A 1ST OBS SMOKE GOGGLES DAMAGED. REPLACED 1ST OBS SMOKE GOGGLES IAW MM 25-64-00. 2L72 4F RTA1NM 20050608002072005060800207WP 2005 6 8 UPS05844554 120050524A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE:C3 RIGHT O/B LEADING EDGE LWR RIB CRACKED AT XFS 772.250. STOP DRILLED CRACK, FABRICATED REPAIR ANGLE, AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-2-0 FIG 2, 51-1-20D, AND 51-1-21. 2L74 4F RT4A25 20050608002082005060800208WP 2005 6 8 UPS05844555 120050524A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE:C3 RIGHT O/B LEADING EDGE LWR RIB CRACKED AT XFS 778. STOP DRILLED CRACK, FABRICATED REPAIR ANGLE, AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-2-0 FIG 2, 51-1-20D, AND 51-1-21. 2L74 4F RT4A25 20050608002092005060800209WP 2005 6 8 UPS05844556 120050524A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE:C3 RIGHT O/B LEADING EDGE LWR RIB CRACKED AT XFS 609. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-2-0 FIG 2, 51-1-20D, 51-1-21. 2L74 4F RT4A25 20050608002102005060800210WP 2005 6 8 UPS05844557 120050524A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE:C3 RIGHT O/B LEADING EDGE UPPER RIB CRACKED AT XFS 603.750. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 57-2-0 FIG 2 AND 51-1-20D. 2L74 4F RT4A25 20050608002112005060800211WP 2005 6 8 UPS05844558 120050525A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE:C3 RIGHT CENTER WING L/E UPPER RIB CRACKED AT XFS 291. CRACK TERMINATES AT FASTENER HOLE. FABRICATED AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-2-0 FIG 2, 51-1-20D, AND 51-1-21. 2L74 4F RT4A25 20050608002122005060800212WP 2005 6 8 UPS05844560 120050525A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE:C3 RT CENTER WING L/E UPPER RIB CRACKED AT XFS 297. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-2-0 FIG 2, 51-1-20D, AND 51-1-21. 2L74 4F RT4A25 20050608002132005060800213WP 2005 6 8 UPS05844561 120050523A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE:C3 CRACKED LONGERON AT STA 1756 L15L AND LOOSE BOLT. REMOVED AND REPLACED DAMAGED SECTION OF LONGERON AND INSTALLED SPLICE FITTING IAW DC-8 SRM 53-2-2 FIG 10 AND 51-1-21. 2L74 4F RT4A25 20050608002172005060800217WP 2005 6 8 UPS05844565 120050525A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE:C3, RIGHT CENTER WING L/E UPPER RIB CRACKED AT XFS 495. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR ANGLE IAW DC8 SRM 57-2-0 FIG 2, 51-1-20D, AND 51-1-21. 2L74 4F RT4A25 20050608002182005060800218WP 2005 6 8 UPS05844566 120050525A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE:C3 RIGHT CENTER WING L/E LWR RIB CRACKED AT XFS 304. CUT OUT DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR FILLER & ANGLE IAW DC-8 SRM 57-2-0 FIG 2, 51-1-20D, AND 51-1-21. 2L74 4F RT4A25 20050608002212005060800221WP 2005 6 8 UPS05844572 120050525A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE:C3 RIGHT WING O/B LEADING EDGE LWR RIB CRACKED AT XFS 623.500. CRACK TERMINATES AT FASTENER HOLE, FABRICATED, AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-2-0 FIG 2, 51-1-20D, AND 51-1-21. 2L74 4F RT4A25 20050608002222005060800222WP 2005 6 8 UPS05844573 120050525A5712 RIB DOUG DC8 DC873F 302199FWP R WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE:C3 RIGHT WING CENTER L/E UPPER RIB CRACKED AT XFS 454. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR ANGLE IAW DC8 SRM 57-2-0 FIG 2, 51-1-20D, AND 51-1-21. 2L74 4F RT4A25 20050608002242005060800224WP 2005 6 8 UPS05844575 120050525A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE:C3 RIGHT WING CENTER L/E LWR SURFACE FASTENER HOLES ELONGATED AT XFS 527. FABRICATED REPAIR DOUBLER, INSTALLED CONICAL WASHERS, AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 57-2-0, 51-1-11, AND 51-1-21. 2L74 4F RT4A25 20050608002252005060800225EA 2005 6 8 A6WA200540179 120050519A3211601R577100323 BUSHING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT TRUNNION MIGRATED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31455AW 7848 RT AFT MAIN LANDING GEAR TRUNNION BUSHING MIGRATED .058 INCH. REMOVED RT AFT MLG TRUNNION BUSHING AND INSTALLED NEW SERVICEABLE BUSHING IAW MFG REO. (K) 2L72 4F4 FRTA21EA E15NE 20050607000412005060700041NM 2005 6 7 DHL2005740553 120050329A5320BAC149897 SPLICE BOEING727 7272Q9 138448MNM STRINGER CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 STR 27L AT BS 680 IS CORRODED. STR 27L AT FRAME 680 STRINGER SPLICE FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 1. REMOVED AND FABBED FROM P/N BAC1498-97 PO NR 3160113 1 FT LONG IAW B727 SRM 53-10-2 FIG 9 AND INSTALLED STRINGER SPLICE IAW B727 SRM 53-10-3 FIG 2. 2L73 4F RTA3WE 20050607000422005060700042NM 2005 6 7 DHL2005740552 120050329A5320 SPLICE BOEING727 7272Q9 138448MNM STRINGER CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 REMOVED STRINGER SPLICE FOUND TO BE OUT OF LIMITS IAW B727 SRM 51-30-2 AT STR 28 LT BS 480, FABRICATED NEW STRINGER SPLICE MAT USED 7075T6 .040 PO 9001068 DIM 13" BY 4" IAW B727 SRM 51-20-1 AND 53-10-2 FIG 9. ALODINED AND PRIMED PART AND AREA IAW B727 SRM 51-10-2. INSTALLED SPLICE REPAIR IAW B727 SRM 51-20-1 AND 53-10-2 FIG 9. 2L73 4F RTA3WE 20050607000462005060700046NM 2005 6 7 DHL2005740538 120050420A5312 BULKHEAD BOEING727 7272Q9 138448MNM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 REMOVED EXISTING RADAR MOUNTING BRACKETS 4 EA IAW B727 SRM 51-30-2. FAB BRACKETS 4 EA CHANNEL SUPPORT FROM 2024T3 .080 DIM 6.8" BY 1.9" PO 9001811 AND STIFFENER FROM 2024T3 .050 DIM 3.3" BY 1.2" P.O 9001417 AND RADIOS FILLER FROM 7075T6 .125 DIM 1.9 BY 1.9 P.O 2706118 IAW B727 DWG 69-40/300. TREATED AND PRIMED PARTS AND BARE METAL IAW B727 SRM 51-10-2. INSTALLED PARTS, BRACKETS, STIFFENERS AND RADIUS FILLER 4 EA IAW B727 DWG 69-44300. 2L73 4F RTA3WE 20050607000542005060700054SO 2005 6 7 RAIA00505012 120050513A801135059106 STARTER EMB 145 EMB145LR 3260212SO RIGHT INOPERATIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03840HK4949 145341 FLT 8025 - IAD - RT STARTER INOP. MAINTENANCE REMOVED AND REPLACED NR 2 AIR TURBINE STARTER. 2L72 4T RTT00011AT 20050607000772005060700077SW 2005 6 7 AC2A100900 120050508A334001077090501 STROBE BELL 430 430 1182150SW EXTERIOR LIGHTS BURNED OUT B AC2AK NONE O OTHER ININSP/MAINT 1 SO07430CM 49090 ONE ROW OF LEDS BURNED OUT / REPLACED LIGHT ASSY. 1G72 3U RTH9SW 20050607000822005060700082CE 2005 6 7 DXTA200500736 120050521A3297 CONNECTOR CESSNA750 750 2076810CE LANDING GEAR DIRTY E DXTAO OTHER E VIBRATION/BUFFET CRCRUISE 1 GL07989QS 7500089 7500089 DURING CRUISE AT FL190, A LOUD THUMP WAS HEARD AMD FELT FROM THE NOSE COMPARTMENT ON THREE OCCASSIONS. JACKED A/C C/W GEAR BUMP TROUBLESHOOTING PER CE 750 MM CHAPTER 32-30-00. CLEANED ELECTRICAL CONNECTORS AT UPLOCK SWITCH HARNESS TO A/C PLUG PG005. OPS CHECK NORMAL. VERIFIED P/N ON LND GEAR CONTROL MODULE TO BE 0014637-2. NO DEFECTS NOTED AT THIS TIME. 2L72 4J RTT00007WI 20050607001022005060700102CE 2005 6 7 DJFA2005098 120050519A3244AHA1814 WHEEL RAYTHNDH125 HAWKER800XP 7150012CE MLG BROKEN E DJFAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 EA23803TA 3 258455 THE FOLLOWING IS BEING REPORTED PER ROC/FAA REQUEST. WHILE AIRCRAFT WAS TAXIING FOLLOWING LANDING THE LEFT INBOARD MAIN WHEEL ASSEMBLY HAD FAILED. THE LOWER ROTATING BEACON WAS HIT BY THE WHEEL ASSEMBLY AND WAS BROKEN. MAINTENANCE REPLACED THE NR 2 MAIN WHEEL ASSEMBLY AND REPLACED THE LOWER BEACON. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA3EU 20050607001042005060700104NM 2005 6 7 UPS05544500 120050520A2120 ODOR BOEING757 75724APF 1384969NM CABIN DETECTED A IPXAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO01451UP 27739 INSPECTION TYPE:N/A FLT CREW SMELLED AN ELECTRICAL BURNING ODOR, NO SMOKE NOTICED. CREW DIVERTED AND DECLARED EMERGENCY. OPERATED ENGINES, PACKS, PRESSURIZED TO 5 PSI DIFF. OPERATED ALL ELECTRICAL EQUIPMENT. INSPECTED ALL EQUIPMENT PANELS AND AVIONIC RACKS. NO DEFECTS OR ELECTRICAL ODORS WERE NOTICED. 2L72 4F RTA2NM 20050607001112005060700111EA 2005 6 7 QXEA200500896 120050502A5230 FRAME CNDAIRCL600 CL6002C10 1390015EA ZONE 200 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FUSELAGE AFT BAGGAGE BAY DOOR SURROUND HAS GOUGES ON DOOR FRAME TRACK FLANGES MID WAY UP FORWARD AND AFT TRACKS. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01 AND 51-25-00-001-001-A01. 2L72 4F RTA21EA 20050607001132005060700113EA 2005 6 7 QXEA200500902 120050502A5230 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 800 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - AFT BAGGAGE BAY DOOR EXTERIOR SURFACE HAS GOUGE ON TOP EDGE. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01, 51-25-16-001-001-A01 AND 51-21-11-001-001-A01. 2L72 4F RTA21EA 20050607001162005060700116EA 2005 6 7 QXEA200500913 120050426A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FUSELAGE INTERIOR LEFT SIDE SEAT RAIL HAS SCRATCHES AT STATION 399 AND 460 ON MOST INNER SURFACE. REPAIRED IAW REO 670-53-00-013. 2L72 4F RTA21EA 20050607001262005060700126CE 2005 6 7 DJFA2005099 120050520A3297 WIRE BEECH MU300 400A 1155402CE MLG DAMAGED E DJFAO OTHER N FALSE WARNING APAPPROACH 1 EA23792TA RK264 CREW REPORTED THAT AFTER GEAR WAS SELECTED DOWN THEY HAD ONLY RECEIVED INDICATION FOR THE NOSE AND LEFT MAIN GEAR AND THE RED GEAR HANDLE LIGHT RAN THROUGH THE PROPER SEQUENCE. THE INDICATOR LIGHTS WERE CHECKED AND THE RIGHT BULB DID TEST GOOD. THE GEAR WAS CYCLED AND CREW RECEIVED THE SAME INDICATION. GEAR HORN WAS RECEIVED WHEN FLAPS WERE SELECTED AND POWER MOVED TO IDLE WITH GEAR RETRACTED. THE GEAR HORN SILENCED WHEN GEAR WAS THEN SELECTED DOWN. GROUND PERSONNEL PROVIDED TWO VISUAL CONFIRMATIONS THAT GEAR WAS DOWN. AIRCRAFT MADE AN UNEVENTFUL LANDING IN KBOS AND EMERGENCY EQUIPMENT WAS STANDING BY. MAINTENANCE REPAIRED WIRING AND PERFORMED A SATISFACTORY LAMP CHECK. AIRCRAFT WAS RETURNED TO SERVICE.2H72 4F RTA16SW 20050607001292005060700129EA 2005 6 7 QXEA200500924 120050502A5310 DOOR FRAME CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - AFT BAGGAGE DOOR SURROUND STRUCTURE LOWER SILL HAS TWO SPOTS OF CORROSION AT STATION 1015 AND 1031. REPAIRED IAW HORIZON AIR EA R-53-324 AND REO 670-53-61-168. 2L72 4F RTA21EA 20050607001402005060700140NM 2005 6 7 DLM88050285 120050520A5260 SENSOR DOUG MD88 MD88 3023688NM AFT STAIRWAY MALFUNCTIONED A DALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO27919DL 49584 AFT STAIRWAY DOOR MESSAGE ILLUMINATED WHEN POWER ADVANCED FOR TAKEOFF. MESSAGE REMAINED ILLUMINATED UNTIL CLEARING RUNWAY. MAX SPEED AT RTO 25 KTS. CLEANED AND LUBED ROLLERS AND SWITCHES. 2L72 4F RTA6WE 20050607001492005060700149EA 2005 6 7 QXEA200500933 120050502A5730 ACCESS PANEL CNDAIRCL600 CL6002C10 1390015EA ZONE 600 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - RIGHT WING, FUEL ACCESS PANEL 611AB SOME FRETTING CORROSION FOUND. REPAIRED IAW CRJ700 SRM 51-21-11-001-001-A01. 2L72 4F RTA21EA 20050607001552005060700155EA 2005 6 7 QXEA200500928 120050428A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FUSELAGE INTERIOR RIGHT FLOOR SEAT RAIL HAS PITTING AND SURFACE CORROSION AT THE FOLLOWING LOCATIONS, STATION 890 AND 904-905. REPAIRED IAW REO 670-53-00-013. 2L72 4F RTA21EA 20050607001632005060700163EA 2005 6 7 COMA0570053 120050520A531267053110521 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01368CA6764 10075 FS 280 LEFT AND RIGHT LOWER BULKHEAD WEBS (FLOOR LEVEL) ARE CORRODED BEYOND LIMITS. PERFORMED A MAJOR REPAIR TO FS 280 LOWER BULKHEAD WEBS BY REMOVING AND REPLACING CORRODED WEBS IAW CRJ 700 SRM 51-42-06-001-001-A01 P/NS 670-53-11-052-1 AND 670-53-11-052-2. 2L72 4F RTA21EA 20050607001652005060700165NM 2005 6 7 QXEA200500947 120050514A5311 FRAME BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09412QX 4059 PDX - CORROSION ON LOWER FRAME MEMBER AROUND SCREW HOLES FROM STATION X71.20 TO BY 44.80. REPAIRED IAW DHC-8-400 SRM 51-42-05. 2H72 4T RTA13NM 20050607001692005060700169NM 2005 6 7 QXEA200500941 120050514A5720 SHROUD BOMBDRDHC8 DHC8401 1390041NM ZONE 600 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09412QX 4059 PDX - RIGHT WING INBOARD LOWER TRAILING EDGE SHROUD THIRD BRACKET FROM INBOARD END FORWARD BRACKET CRACKED. REPAIRED IAW RD 8/4-57-253. 2H72 4T RTA13NM 20050607001722005060700172NM 2005 6 7 QXEA200500944 120050515A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09412QX 4059 PDX - NICKS ON DOUBLER AFT EDGE OF LAV SERVICE DOOR. REPAIRED IAW DHC-8-400 SRM 51-21-10 AND 51-25-10. 2H72 4T RTA13NM 20050607001732005060700173NM 2005 6 7 QXEA200500945 120050514A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09412QX 4059 PDX - NICKS ON BELLY SKIN APPROXIMATELY LEFT STRINGER 31 FROM BY 19.50, AFT APPROXIMATELY 33 INCH TO BY 12.00 INBOARD TO STRINGER 33. REPAIRED IAW HORIZON AIR EA 6-53-537. 2H72 4T RTA13NM 20050607001792005060700179EA 2005 6 7 COMA0570056 120050516A3230533405 SELECTOR VALVE CNDAIRCL600 CL6002C10 1390015EA MLG INOPERATIVE A COMAO OTHER JS WARNING INDICATION AFFECT SYSTEMS APAPPROACH 1 SO01367CA6912 10069 FLIGHT 5296 - GEAR DISAGREE WARNING. REPLACED THE LANDING GEAR SELECTOR VALVE. 2L72 4F RTA21EA 20050607001842005060700184EU 2005 6 7 05FDEA01390 120050520A5754 SLAT TRACK AIRBUS310 A310203 3930313EU RT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25403FE 230 RIGHT WING NR 3 SLAT, NR 10 TRACK, SLAT ATTACH POINT FITTING DAMAGED ON REMOVAL OF SLAT KNUCKLE. UPON REMOVAL OF RT NR 3 SLAT, NR 10 TRACK ATTACH POINT FITTING WAS DAMAGED AND LOWER SKIN OF NR 3 SLAT NR 10 TRACK. BLENDED GOUGES FOUND TO BE WITHIN LIMITS. ALODINED, PRIMED AND TOP COATED. CUTOUT OF DAMAGED SKIN, NO CRACKS FOUND. FABBED FILLER AND DOUBLER, REMOVED AND REINSTALLED 2 EA BUSHINGS, ALL IAW FEDEX EA 6-5750-89194. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR PER FEDEX GM 6-2-100. 2L72 4F RTA35EU 20050608000082005060800008NM 2005 6 8 05FDEA01443 120050524A5713 STRINGER BOEING727 727200 138407ENM LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 LT WING UPPER STR 9 CRACKED AT WS 656.50. REPAIRED STRINGER PER FED EX EA 7-5710-86294 2L73 4F RTA3WE 20050608000192005060800019EA 2005 6 8 COMA0560325 120050601A5743 DRAG ANGLE CNDAIRCL600 CL6002B19 1900309EA MLG CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01932CA 7038 LT AND RT MLG DRAG ANGLES CRACKED AT WS 53.00. REPAIRED I/A/W CRJ SRM 51-42-20. 2L72 4F RTA21EA 20050608000222005060800022EA 2005 6 8 COMA0560328 120050601A5310 DOOR FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01710CA 7241 PAX DOOR FRAME CRACKED AT FS 320 AND 338. REPAIRED IAW REO 601R-52-11-402. 2L72 4F RTA21EA 20050608000232005060800023EA 2005 6 8 COMA0560329 120050601A5312 RIB CNDAIRCL600 CL6002B19 1900309EA RT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01710CA 7241 RT BATT RIB CRACKED. REPAIRED IAW REO 601R-57-51-046. 2L72 4F RTA21EA 20050608000432005060800043NM 2005 6 8 L0FR200500003 120050422A3246260356116 WHEEL BOEING747 747200 1384847NM MLG CRACKED B Q2SAK NONE O OTHER ININSP/MAINT 1 AL03 INBOARD WHEEL HALF CRACKED AT TORQUE LUG KEY BOSS. 2L74 4F RTA20WE 20050608000472005060800047NM 2005 6 8 72300183 120050301A5311 FRAME BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 SEVERAL AREAS OF CORROSION ON FRAME. 2L73 4F4 FRTA3WE E2EA 20050608000492005060800049NM 2005 6 8 72300185 120050224A5315 FLOORBEAM BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 1 INCH AREA OF CORROSION ON FLOORBEAM UPPER CHORD. 2L73 4F4 FRTA3WE E2EA 20050608000532005060800053NM 2005 6 8 AT0500015 120050523A33508039491 BATTERY PACK BOEING717 717200 1383700NM EMERGENCY LIGHTSINOPERATIVE A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15963AT 55024 EMERGENCY LIGHTS AT BUSINESS SEATS AND FRONT ROW COACH INOPERATIVE. FOUND WRONG LAMPS INSTALLED SEAT ROWS 1-10. RELAMPED EPL ROWS 1-10. REMOVED AND REPLACED EMERGENCY BATTERY ASSEMBLY B5-118. ALSO REPAIRED LOOSE CONNECTION AT ROW 10, EMERGENCY LIGHTS OPS CHECK NORMAL REF WDM 33-51-141, 33-51-144, MM 33-51. 2L72 4F TRA6WE 20050608000572005060800057NE 2005 6 8 GUU2005F00013 220050211A7200 BLADE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE RT ENGINE FAILED A GUUAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NRNOT REPORTED 1 SO298755016986 UE205 114436 DURING FLIGHT, DETECTED SMOKE IN THE COCKPIT AND CABIN. RT ENGINE LOW PRESSURE ANNUNCIATOR ILLUMINATED. REMOVED AND REPLACED RT ENGINE. OPERATIONAL CHECK NORMAL. NOTE: VERIFIED TO BE 2ND STAGE PT BLADE FAILURE. (K) 2L72 4T4 TRTA24CE E26NE 20050608000592005060800059NE 2005 6 8 GUU2005F00014 220050216A72503044800 BLADE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE LT ENGINE FAILED A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO298153816869 UE199 PCEPS0057 DURING TAKEOFF ROLL, WITH LT ENGINE AT APPROXIMATELY 1,000 LBS OF TORQUE, UNUSUAL NOISE HEARD. LT ENGINE CEASED. ABORTED TAKEOFF. DETERMINED LT POWER SECTION SEIZED. REMOVED AND REPLACED LT ENGINE ASSEMBLY AND ROUTED FAILED UNIT FOR FURTHER ANALYSIS AND REPAIR. OPS CHECK NORMAL. NOTE: VERIFIED TO BE 2ND STAGE PT BLADE FAILURE. (CLOSED 5/4/05) (K) 2L72 4T4 TRTA24CE E26NE 20050608000612005060800061NM 2005 6 8 CALA0500160 120050521A5315143N5015 FLOORBEAM BOEING757 757224 1384958NM STA CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717105 27295 INSPECTION FOUND FLOORBEAM CORRODED AT STA 720, RBL 20.5 TO RBL 50.5. REPAIRED IAW SRM 53-00-51. 2L72 4F RTA2NM 20050608000632005060800063NM 2005 6 8 CALA0500162 120050523A53106546566 DOOR FRAME BOEING737 7373T0 1384582NM STA CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714325 23455 INSPECTION FOUND THE R-2 AFT DOOR FRAME CORRODED AT STA 996, RBL 48. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-70-11. 2L72 4F RTA16WE 20050608001012005060800101CE 2005 6 8 F2P2005F00000 120050516A7120265102218 MOUNT CESSNA208 208B 2073701CE PWA PT6 PT6* 52043EA ENGINE CRACKED E F2PAK NONE O OTHER ININSP/MAINT 1 SO1752JJ 301 208B1079 DURING INSPECTION FOR A PILOT REPORTED ENGINE OIL LEAK, CRACKS WERE FOUND ON THE FORWARD ENGINE MOUNT. CRACKS ON BOTTOM LT CORNER ALONG WELD JOINING THE HORIZONTAL AND VERTICAL TUBE, MEASURES 2.5 INCHES AND 3.2500 INCHES IN LENGTH. CRACKS ON BOTTOM RT CORNER ALONG WELD AND ENGINE MOUNT BOSS MEASURES 1.7500 INCH AND 2 INCHES IN LENGTH. TECH SUPPORT ADVISED TO CHECK THE SHIMMY DAMPNER FOR A BROKEN ROLL PIN THAT SECURES THE PISTON TO SHAFT. SHIMMY DAMPNER DISASSEMBLED, NO DEFECTS FOUND. RECOMMEND STRONGER ENGINE MOUNT. (K) 1H71 3T3 T A37CE E2NE 20050608001042005060800104WP 2005 6 8 05FDEA01478 120050529A2611 SMOKE DETECTOR DOUG MD10 MD1010F 3022112WP CABIN FAULTY A FDEAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO25394FE 46628 AT FL 360 GOT LVL 3 CABIN SMOKE ALERT (ONE OF THE MID CABIN 7 OR 8). DECLARED EMERGENCY, AND DIVERTED INTO KTUL. MEL. MAIN DECK CENTERLINE SMOKE DETECTORS INOP. DISPATCH PER MEL 27-17-01-03 A NR 2 CENTER SMOKE DET INOP SMOKE DET C/P DISCONNECTED AND STOWED. REMOVED AND REPLACED NR 2 SMOKE DETECTOR PER M/M 26-15-01-4 & TESTED PER 26-15-01-5. 2L73 4F RTA22WE 20050608001102005060800110NM 2005 6 8 2005UALA00461 120050520A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP2902UA 24623 FWD PIT FRAME IS DENTED AT STA 600 STR 24L. CUT OUT DAMAGE AND ACP HFEC WITH NO CRACK INDICATED. FABRICATED RPR PER REO G-1042 AND INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050608001252005060800125NM 2005 6 8 2005UALA00476 120050517A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29546UA 25367 MAJOR REPAIR ACCOMPLISHED ON SKIN AT STA 1701 AND STR 18R. 2L72 4F4 FRTA2NM E17NE 20050608001292005060800129NM 2005 6 8 2005UALA00480 120050525A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29313UA 23674 RT AFT FUSELAGE SKIN REPLACEMENT NEEDS DOUBLER REMOVAL AND INSTALLATION AFTER AFT SKIN IS REPLACED. REMOVED THE DOUBLER, ACCOMPLISHED HFEC OF THE HOLES. FOUND NO CRACKS, FABRICATED AND INSTALLED STRUCTURAL FILLER, DOUBLER AND TRIPLER PER SRM 51-00-01. 2L72 4F4 FRTA16WE E2GL 20050616001442005061600144NM 2005 6 16 05FDEA01508 120050602A2910 HYDRAULIC LINE BOEING727 727200 138407ENM HYDRAULIC SYS RUPTURED A FDEAHBA DEACTIVATE SYST/CIRCUITSEMER. DESCENT UNSCHED LANDING K FLUID LOSS CLCLIMB 1 SO25272FE 22037 A-HYD SYSTEM FLUID LOSS / ISOLATED TO -A- PUMP NR 2. AFTER SHUTDOWN, THE -A- SYSTEM QTU. READ 2.5 GALLONS AND THE FLUID SHUTOFF SWITCHES WERE NOT TURNED OFF. OPENED COUPLING AND MOTORED ENGINE. FOUND PRESSURE LINE FROM THE PUMP TO THE FIREWALL RUPTURED. 2L73 4F RTA3WE 20050608001432005060800143NE 2005 6 8 05FDEA01488 220050530A7200 CASE DOUG MD11 MD11 3023602NM GE CF6 CF680C2D1F 30025NE NR 2 ENGINE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 NR 2 ENGINE, LEFT HAND CASE APPROXIMATELY 7 - 8 O' CLOCK POSITION, FOUND CRACKED. REPAIRED PER AMM 72-33-00-300-801. 2L73 4F4 FRTA22WE E31N3 20050608001462005060800146EU 2005 6 8 05FDEA01490 120050530A27504907905 CONTROLLER AIRBUS310 A310222 3930315EU T/E FLAP MALFUNCTIONED A FDEAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SO25452FE53621454 313 ON TAKEOFF FROM FRA, GOT FLAP SYSTEM 2 FAULT. RESELECTED FLAPS TO SLATS/FLAPS 20/20, WHICH DID NOT FIX THE PROBLEM. WENT TO HOLDING AND WORKED THE PROBLEM. RETURNED TO FRA AND LANDED. REMOVED AND REPLACED NR 2 SFCC PER MM 27-51-18-4. SYS OPS CHECK OK. PREMATURE REMOVAL/INSTALLATION OFF MFG 49-079-05. 2L72 4F RTA35EU 20050608001492005060800149NM 2005 6 8 05FDEA01493 120050530A5713 STRINGER DOUG MD11 MD11 3023602NM RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 RIGHT HAND WING LOWER FUEL TANK AT XORS= 733, S-10 FOUND STRINGER END CRACKED. REPAIRED AS PER SRM. 2L73 4F RTA22WE 20050608001512005060800151NM 2005 6 8 05FDEA01494 120050530A5347 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 MAIN DECK, SEAT TRACK AT STA 635 RBL = 9 FOUND CRACKED. REMOVED AND REPLACED WITH REWORKED SEAT TRACK AS PER SRM 53-70-00 VOLUME I, FIGURE 1. 2L73 4F RTA22WE 20050608001572005060800157 2005 6 8 ASMF200505023 420050521A2565100503121 SLIDE DOUG DC9 DC987 3022087WP TAILCONE DEPLOYED W ASMFK NONE W INADEQUATE Q C ININSP/MAINT 1 SW23204AM133494320 49404 DURING TRANSIT CHECK THE GROUND HANDLING SERVICES COMPANY PERSONNEL OPERATED THE AFTER EXIT DOOR IN THE EMERGENCY FORM, WHICH RESULTED IN THE TAILCONE SEPARATION AND DEPLOYMENT OF THE EVACUATION SLIDE. THE TAIL CONE HIT THE GROUND AND HAD A 6 X 2 INCH CRACK, IT WAS REPAIRED WITH HIGH SPEED TAPE APPLIED AT THE STATION. AIRCRAFT PERFORMED A NON REVENUE FLIGHT TO MEXICO MAIN BASE, TAIL CONE AND SLIDE WERE REPLACED IAW MM 53-53-00 AND 25-62-01 RESPECTIVELY, ALL CORRECT. 2L72 4F RTA6WE 20050608001592005060800159NM 2005 6 8 HNAA0500047 120050524A575585711503101 BRACKET DHAV DHC8 DHC8102 2809003NM SPOILER CRACKED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07940HA4229642296 156 DURING C-CHECK INSPECTION THE OUTBOARD ROLL SPOILER MOUNTING BRACKET WAS FOUND TO BE CRACKED ON BOTTOM INBOARD SIDE. REMOVED AND REPLACED SPOILER BRACKET. 2H72 4T RTA13NM 20050608001822005060800182NM 2005 6 8 05FDEA01410 120050523A5315 FLOORBEAM DOUG MD11 MD11 3023602NM FUSELAGE DEFORMED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25631FE 48454 FWD CARGO COMPARTMENT, AT STA 1079 FLOORBEAM FOUND DEFORMED AS MARKED. FLOORBEAM REMOVED AS PER SRM 51-35-01 VOL II. NEW FLOOR BEAM INSTALLED AS PER DRAWING AFA 0039 AND SRM 51-35-01 VOL II. MINOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050608001852005060800185GL 2005 6 8 KBM2005F00084 220050325A72406870992J COMBUST CHAMBER BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL LT ENGINE CRACKED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19667JM 3444 COMBUSTION CAN, CRACKED ON LEFT SIDE. REMOVED AND REPLACED. (K) 1G71 3U3 U H2SW E4CE 20050608001862005060800186EA 2005 6 8 MASA200500328 120050502A2740 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA E/E BAY MALFUNCTIONED A MASAO OTHER O OTHER CRCRUISE 1 SW0727314 7291 ASH 6317 PHX TO BIL. THE AIRCRAFT HAD A MACH/STAB TRIM CAUTION MESSAGE IN FLIGHT. WITH DIRECTION FROM MAINTENANCE CONTROL THE PILOT RESET THE SYSTEM IN FLIGHT. WHEN THE AIRCRAFT LANDED IN BIL, CONTRACT MAINTENANCE RE-REACKED HSTCU AND RESET SYSTEM. OPERATIONAL CHECK WAS GOOD AND NO OTHER DEFECTS NOTED AT THIS TIME. 2L72 4F RTA21EA 20050608001892005060800189EU 2005 6 8 KBM2005F00088 120050410A2822P9412209 PUMP SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE FUEL BOOST SEIZED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH792 2884 FUEL BOOST PUMP, UNIT SEIZED, BLOWS CIRCUIT FUSE W/POWER APPLIED. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050608001912005060800191CE 2005 6 8 052305N304CS1 120050523A2133 OUTFLOW VALVE CESSNA500 550 2076604CE CABIN PRESSURE MALFUNCTIONED E Z5FAGBA O2 MASK DEPLOYED EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NE03304CS 5500847 AT FL 350 EXPERIANCED LOUD BANG AND RAPID LOSS OF PRESSURIZATION. DECLARED EMERGENCY, DESCENDED RAPIDLY AND DEPLOYED PASSENGER OXYGEN MASKS (2 PAX ON BOARD). DIVERTED TO DALLAS LOVE FIELD AND LANDED ASAP. AIRCRAFT INSPECTED AND REPAIRED AT FACTORY AUTHORIZED SERVICE CENTER, JET AVIATION. OUTFLOW VALVE WAS REPLACED AFTER ALL SYSTEM FUNCTION TESTS WERE COMPLIED WITH AND NO DEFINITIVE CAUSE WAS IDENTIFIED. THE AIRCRAFT COMPLIED WITH AN OPERATIONAL CHECK FLIGHT AND NO DEFECTS NOTED. 1L72 4F A22CE 20050608001942005060800194EA 2005 6 8 MASA200500388 120050524A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA EXTERIOR INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW0775987 7405 THE AIRCRAFT WAS RON LAS NIGHT AND SCHEDULED FOR A SERVICE CHECK INSPECTION. DURING THE WALK AROUND IT WAS DISCOVERED THE RIGHT SIDE FORWARD EXTERIOR EMERGENCY LIGHT WAS NOT ILLUMINATING. MAINTENANCE REPLACED THE LIGHT BULB AND OPS CHECKED GOOD. 2L72 4F RTA21EA 20050608002142005060800214WP 2005 6 8 UPS05844562 120050523A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE:C3 LONGERON 15R CRACKED AT STA 1756. REMOVED AND REPLACED DAMAGED SECTION OF LONGERON AND INSTALLED SPLICE FITTING IAW DC-8 SRM 53-2-2 FIG 10 AND 51-1-20D. 2L74 4F RT4A25 20050608002152005060800215WP 2005 6 8 UPS05844563 120050524A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE:C3, RIGHT OUTBOARD L/E LWR RIB CRACKED AT XFS 822.500. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-2-0 FIG 2 AND 51-1-21. 2L74 4F RT4A25 20050609000062005060900006SO 2005 6 9 C2XA05TY044 120050517A532014532636401 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714902 145496 TYS - DURING A INSPECTION CORROSION WAS FOUND AT THE LEFT OMEGA BEAM AT FRAME 25. MAINTENANCE BLENDED AND REMOVED CORROSION AND FINISHED THE REPAIR AT FRAME 25 IAW EMB 145 SRM 53-22-10. 2L72 4T RTT00011AT 20050609000082005060900008SO 2005 6 9 C2XA05SH039 120050520A532014521700007 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714938 145029 SHV - DURING C-CHECK THE LT OMEGA BEAM HAS CORROSION AROUND NUT PLATE BETWEEN FRAMES 22 AND 23. MAINTENANCE REPAIRED LT OMEGA BEAM NUT PLATE AT FRAME 22.5 AND RIVET HOLE CRACK AT FRAME 22 IAW SRM 51-30-01; 51-40-02 AND EC5320-01241. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050609000092005060900009SO 2005 6 9 C2XA05SH040 120050523A532014521713005 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2729906 145472 SHV - DURING C-CHECK THE CENTER OMEGA BEAM CORRODED AT FR 20. MAINTENANCE REMOVED 1 CORRODED CENTER OMEGA BEAM AT FR 20 AND INSTALLED 1 CENTER OMEGA BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050609000142005060900014NM 2005 6 9 05FDEA01406 120050523A5320 INTERCOSTAL DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25631FE 48454 MAIN DECK, AT STATION 1900 TO 1921 RT INTERCOSTAL AT LONGERON 4 FOUND CRACKED. REMOVED IAW SRM 51-35-01 VOL II AND NEW INTERCOSTAL INSTALLED AS PER SRM 51-31-01 VOL II. NEW INTERCOSTAL FABRICATED AS PER DRAWING AGA 3121 REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2L73 4F RTA22WE 20050609000152005060900015NM 2005 6 9 05FDEA01407 120050523A5320 INTERCOSTAL DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25631FE 48454 MAIN DECK, CENTER AND AFT ATTIC AREA AT STA 1581 INTERCOSTAL AT LONGERON 7R LOCATION FOUND CRACK AS MARKED. CRACKED INTERCOSTAL AT CENTRE AND AFT ATTIC AREA AT STA 1581 LONGERON 7R REMOVED AS PER SRM 51-35-01 VOL II AND NEW INTERCOSTAL INSTALLED AS PER SRM 51-31-01 VOL II. NEW INTERCOSTAL FABRICATED AS PER DWG AFA 7761. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050609000162005060900016NM 2005 6 9 05FDEA01408 120050523A5320 INTERCOSTAL DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25631FE 48454 MAIN DECK, CENTER AND AFT ATTIC AREA AT STA 1641 RT INTERCOSTAL FOUND CRACK AT LONGERON 7R LOCATION AS MARKED. 2L73 4F RTA22WE 20050609000172005060900017NM 2005 6 9 05FDEA01409 120050523A5315 FLOORBEAM DOUG MD11 MD11 3023602NM FUSELAGE DEFORMED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25631FE 48454 FWD CARGO COMPARTMENT, AT STA 6-30 FLOORBEAM FOUND DEFORMED AS MARKED. FLOORBEAM REMOVED AS PER SRM 51-35-01 VOL II. NEW FLOOR BEAM INSTALLED AS PER DRAWING AFA 0039 AND SRM 51-35-01 VOL II. MINOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050609000192005060900019NM 2005 6 9 05FDEA01411 120050523A5340 SUPPORT BRACKET DOUG MD11 MD11 3023602NM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25631FE 48454 FWD CARGO COMPARTMENT, AT STA 6-10 RT FLOORBEAM SUPPORTING BRACKET ASSY FOUND DAMAGED AS MARKED. BRACKET REMOVED AS PER SRM 51-35-01 VOL II. NEW FLOOR BEAM STRUT BRACKET INSTALLED AS PER DWG ADA0033 AND AS PER SRM 51-35-01 VOL II. MINOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050609000202005060900020NM 2005 6 9 05FDEA01412 120050523A5340 SUPPORT BRACKET DOUG MD11 MD11 3023602NM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25631FE 48454 FWD CARGO COMPARTMENT, AT STA 6-30 FLOORBEAM LT AND RT SUPPORTING BRACKET ASSY FOUND DAMAGED AS MARKED. REMOVED AS PER SRM 51-35-01 VOL II. NEW SUPPORT BRACKET LT AND RT INSTALLATED AS PER DWG ADA0033 AND SRM 51-35-01 VOL II. MINOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050609000212005060900021NM 2005 6 9 05FDEA01413 120050524A5315 FLOORBEAM DOUG MD11 MD11 3023602NM FUSELAGE DEFORMED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25631FE 48454 FWD CARGO COMPARTMENT, AT STA 1099 FLOORBEAM FOUND DEFORM AS MARKED. REMOVED AS PER SRM 51-31-01 VOL II. NEW FLOORBEAM INSTALLED AS PER DWG AFA 0039 AND AS PER SRM 51-31-01 VOL II. MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050609000242005060900024NM 2005 6 9 05FDEA01416 120050524A5320 INTERCOSTAL DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25631FE 48454 MAIN DECK CABIN, AFT CABIN AT STA 1701 RT AT LONGERON 7R LOCATION FOUND INTERCOSTAL CRACK AS MARKED. REMOVED AS PER SRM 51-35-01 VOL II AND NEW INTERCOSTAL INSTALLED AS PER SRM 51-31-01 VOL II. NEW INTERCOSTAL FABRICATED AS PER DWG AFA 7761. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2L73 4F RTA22WE 20050609000252005060900025NM 2005 6 9 C1HA200596004 120050422A5315 FLOORBEAM BOEING727 7272J4 1384006NM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15696CA 22574 MAIN PASSENGER CABIN STA 1130 LBL 26 TO 46 TOP OF FLOORBEAM CORRODED. 2L73 4F RTA3WE 20050609000262005060900026NM 2005 6 9 05FDEA01417 120050524A5347 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25631FE 48454 MAIN DECK CABIN, AFT CABIN AT STA 1964 LBL 107 CURVED SEAT TRACK FOUND CORRODED AT LAVATORY TIE DOWN FITTING AS MARKED. TRIM OUT FROM STA 1751 LBL 107. NEW SEAT TRACK REPLACED FROM AFA 7789-545 AND CARRIED OUT REPAIR AS PER SRM 53-70-00 FIG 1 VOL I. NEW SEAT TRACK AND REPAIR PARTS LOCATED AND INSTALLED AS PER SRM 53-70-00 FIG 1 VOL I AND SRM 51-31-01 VOL II. CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050609000292005060900029NM 2005 6 9 C1HA200596005 120050422A5315 FLOORBEAM BOEING727 7272J4 1384006NM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15696CA 22574 MAIN PASSENGER CABIN STA 1030 LBL 24 TO RBL 24 TOP OF FLOORBEAM CORRODED. 2L73 4F RTA3WE 20050609000302005060900030NM 2005 6 9 C1HA200596006 120050423A5320 FLOOR SUPPORT BOEING727 7272J4 1384006NM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15696CA 22574 MAIN PASSENGER CABIN B/L 15L STA 1137 FLOOR SUPPORT CORRODED. 2L73 4F RTA3WE 20050609000362005060900036NM 2005 6 9 C1HA200596011 120050427A5313 LONGERON BOEING727 7272J4 1384006NM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15696CA 22574 E&E COMPT STA 440 LONGERON 26R, CORRODED. CENTER AND BOTTOM OF LONGERON UNDER FRAME REPLACED STRINGER FROM STA 429 TO 431 IAW SRM 53-10-2 FIG 1. 2L73 4F RTA3WE 20050609000382005060900038NM 2005 6 9 C1HA200596012 120050413A5313 STRINGER BOEING727 7272J4 1384006NM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15696CA 22574 FWD ASSY COMP STA 312, STRINGER 27L IS CORRODED UNDER FRAME (C53-111-03-02) STRINGER SPLICE REPAIR IAW SRM 53-10-3 FIG 3. 2L73 4F RTA3WE 20050609000392005060900039CE 2005 6 9 DXTA200500741 120050523A3246315381 WHEEL CESSNA750 750 2076810CE MLG OUT OF BALANCE E DXTAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 GL07999QS135 7500203 EXCESSIVE NOSE WHEEL SHIMMY ON TAKEOFF ROLL CAUSED YD OFF MESSAGE ABORTED TAKE OFF. REMOVED LT AND RT NOSE WHEELS, INSTALLED OVERHAULED NOSE WHEEL ASSEMBLIES IAW M/M CHAPTER 32-41-01. 2L72 4J RTT00007WI 20050609000402005060900040 2005 6 9 XN0A1238 420050524A3416 INDICATOR AIRBUS300 A300B4203 3930306EU ALTIMETER FAILED A XN0AA UNSCHED LANDING O OTHER NRNOT REPORTED 1 GL23472AS 125 BTB DUE FAIL FLAG ON NR 1 ALT FLAG IN VIEW. REMOVED AND REPLACED NR 1 ALT INDICATOR. OPS CK NORMAL IAW MM 34-12-21 (STATUS:ORIG/CLOSED) 2L72 4F RTA35EU 20050609000422005060900042NM 2005 6 9 F3LA200500022 120050522A5210 COVER AIRBUSA319 A319111 3930336NM GEARBOX CRACKED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03917FR 3933 1890 DURING C-2 CHECK, INSPECTION REPORTED CRACK IN L2 DOOR GEARBOX COVER. REPAIRED L2 DOOR GEARBOX COVER PER EA A9-52R-10886. PAINTED L2 DOOR GEARBOX COVER PER AMM 25-00-00-540. 2L72 4F RTA28NM 20050609000432005060900043SO 2005 6 9 LR7A05093 120050521A5230 SKIN LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL CARGO DOOR CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 12 4698 DURING SCHEDULED (A) CHECK INSPECTION IAW JOB CARD HA1200 FOUND CARGO DOOR EXTERNAL STRAP GOUGED AND SKIN CRACKED APPROX. 1.5 IN. BY SUSPECTED CARGO LOADING IMPACT AT FS 1001 LBL 40. DAMAGE DISPOSITION IAW EDY96-1. AIRCRAFT FERRIED UNPRESSURIZED FOR REPAIR. REPAIRED IAW LAC MEA 382-52-05-053. NR 135028. 2H74 4T4 T A1SO E282 20050609000442005060900044EU 2005 6 9 U30A200500003 120050505A5210 STRUCTURE AIRBUS320 A320214 3930316EU GE CFM56 CFM56* 13802NE PAX DOOR DAMAGED A U30AK NONE O OTHER ININSP/MAINT 1 EA17260AV10726 1564 DURING POST FLIGHT, DAILY INSPECTION, GROUND EQUIPMENT INDUCED DAMAGE WAS FOUND TO LOWER AFT CORNER OF L2 (LT AFT PAX/CREW ) DOOR. MAINTENANCE INSPECTED THE DOOR IAW SRM. MAINTENANCE ALSO PERFORMED A HFEC (HIGH FREQUENCY EDDY CURRENT) INSPECTION IN COMPLIANCE WITH MFG RAS (REPAIR DESIGN APPROVAL SHEET, EASA APPROVED), REPAIR REF: 2005-30-04-001 AND 2005-30-05-001. AIRCRAFT CAN REMAIN IN SERVICE FOR 50 FLT CYCLES IAW RAS. CURRENT FC ON 29 APR IS 4036. ON 5 MAY 05, TAT 10726, TC 4053, THE DOOR WAS PERMANENTLY REPAIRED WITH AN EXTERNAL DOUBLER IAW SRM 52-10-00, PAR 5C, FIG. 203 AND USA 3000 E.O. 05-52-002, DATED 2 MAY 2005. FAA FORM 337, MAJOR REPAIR AND ALTERATION, DATED 5 MAY 05 HAS BEEN COMPLETED. 2L72 4F4 FRTA28NM E2GL 20050609000462005060900046EU 2005 6 9 UPS05144510 120050523A2560 SMOKE BARRIER AIRBUS300 A300B4622R 3930312EU CARGO BAY TORN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01136UP 0819 INSPECTION TYPE:N/A CURTAIN BETWEEN AFT LOWER CARGO AND BULK CARGO IS TORN UPPER CENTER. REMOVED AND REPLACED CURTAIN WITH REF TO MM 25-56-11-2. 2L72 4F RTA35EU 20050609000472005060900047WP 2005 6 9 UPS05844504 120050422A53404640162502N FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE: C1, MAIN CABIN FRAME TO CUSP FITTING HAS HEAVY CORROSION AT STA 1580 L21L. REMOVED AND REPLACED CUSP FITTING AT STA 1580 L21L IAW DC-8 SRM 51-1-20D AND 51-3-0. 2L74 4F RT4A25 20050609000482005060900048WP 2005 6 9 UPS05844505 120050425A534037592582N FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE:C1 LONGERON SPLICE FITTING HAS HEAVY CORROSION AT STA 1270 L35R. REMOVED AND REPLACED LONGERON SPLICE FITTING IAW DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20050609000492005060900049WP 2005 6 9 UPS05844506 120050423A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE: C1, SEVERE CORROSION ON FRAME/ANGLE AT FS 380 (LONGERON) LBL 33. REMOVED CORROSION ON LONGERON AND FOUND OUT OF LIMITS IAW DC-8 SRM 51-1-8. INSTALLED LONGERON SPLICE FITTING IAW DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20050609000502005060900050WP 2005 6 9 UPS05844507 120050516A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE: C1, FOUND CORROSION AT AFT MANUFACTURING SPLICE 6 O`CLOCK. CUT OUT CORROSION, FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-1 FIG 7, 53-5-3 FIG 1, 51-1-20D, AND 51-1-21. 2L74 4F RT4A25 20050609000522005060900052WP 2005 6 9 U2RA3201 120050524A5330 SKIN DOUG DC8 DC863F 302198FWP FUSELAGE CORRODED A U2RAK NONE O OTHER ININSP/MAINT 1 GL23921R 684252039 46145 TOP OF LT MAIN LANDING GEAR TOP SURFACE CORRODED APPROXIMATELY 1 X 4 INCHES AT STATION 860, LBL 40 TO LBL 44. 2L74 4F 4A25 20050609000542005060900054 2005 6 9 COMA0560313 420050520A221070609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA AUTO PILOT MALFUNCTIONED A COMAA UNSCHED LANDING JF WARNING INDICATION FLT CONT AFFECTED CRCRUISE 1 SO01486CA17689805 7707 FLIGHT 5651 AUTO PILOT DISCONNECT WARNING AND PITCH DOWN AND LOSS OF 500 FT. REPLACED THE HSTCU. 2L72 4F RTA21EA 20050609000552005060900055EA 2005 6 9 COMA0560315 120050523A5350 FAIRING CNDAIRCL600 CL6002B19 1900309EA FUSELAGE LOOSE A COMAA UNSCHED LANDING WE INADEQUATE Q C VIBRATION/BUFFET CLCLIMB 1 SO01912CA 7011 FLIGHT 5112 LOUD THUMPING NOISE AFTER TAKEOFF. FOUND AERODYNAMIC BELLY FAIRING LOOSE WITH SEALANT MISSING. TIGHTENED LOOSE SCREWS AND APPLIED SEALANT. 2L72 4F RTA21EA 20050609000562005060900056EA 2005 6 9 COMA0560318 120050522A5270 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA CARGO DOOR FALSE ACTIVATIONA COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01941CA 7050 FLIGHT 5568 CARGO DOOR CAUTION MESSAGE. COULD NOT DUPLICATE. FOUND NO DEFECTS IN CARGO DOOR OR WARNING SYSTEM. 2L72 4F RTA21EA 20050609000572005060900057EA 2005 6 9 SWIA200515024 120050518A2740 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07447SW 7677 STAB TRIM AND MACH TRIM CAUTION MESSAGES INFLIGHT. REPLACED THE F/O'S STAB TRIM SWITCH. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050609000592005060900059EA 2005 6 9 SWIA200515026 120050521A2740 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA COCKPIT INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07955SW 7817 CAPT STAB TRIM ONLY WORK IN THE NOSE DOWN, NOSE UP IT IS INOPERATIVE. REPLACED CAPTAINS STAB TRIM SWITCH AS REQUIRED IAW CRJ MM 27-41-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050609000602005060900060EA 2005 6 9 SWIA200515027 120050520A274070609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM INOPERATIVE A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07951SW797 797 7795 STAB CH1 INOP STATUS MESSAGE INFLIGHT. REPLACED HSTCU WITH A SERVICEABLE UNIT. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050609000622005060900062EA 2005 6 9 SWIA200515029 120050520A274070623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07957SW 7829 STAB CH1 INOP MSG AFTER LANDING. REPLACED MOTOR CONTROL UNIT IAW CRJ AMM 27-42-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050609000632005060900063SO 2005 6 9 SWIA200515030 120050522A27503472001001 CONTROL UNIT EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07250YV1147111471 120250 LEFT OUTBOARD FLAP SHOWED DISAGREEMENT AFTER TAKEOFF AFTER SELECTING FLAPS UP. REPLACED FCU IAW MM 27-50-06. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050609000642005060900064SO 2005 6 9 SWIA200515031 120050520A27203081401003 ACTUATOR EMB 120 EMB120ER 3260203SO RUDDER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CLCLIMB 1 NM07188SW113677771 120039 AFTER TAKEOFF RIGHT RUDDER HAD LIMITED TRAVEL. REPLACED BLUE SYSTEM RUDDER ACTUATOR IAW MM 27-22-02. 2L72 4T RTA31SO 20050609000652005060900065EA 2005 6 9 SWIA200515032 120050520A274070623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07959SW 7840 STAB CH2 C/B WON'T RESET. REPLACED MOTOR CONTROL UNIT. OPERATIONAL CHECKS GOOD IAW CRJ MM 27-41-00. 2L72 4F RTA21EA 20050609000662005060900066EA 2005 6 9 SWIA200515033 120050520A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA EMERGENCY EXIT BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07930SW 7713 MAIN CABIN DOOR EMERGENCY EXIT LIGHT BROKEN. REPAIRED LIGHT ASSY AS REQUIRED. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050609000672005060900067EA 2005 6 9 SWIA200515034 120050522A2740 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA COCKPIT INOPERATIVE A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07952SW 7805 F/O'S STAB TRIM SWITCH INOPERATIVE. REPLACED F/O'S STAB TRIM SWITCH PER 27-41-05. 2L72 4F RTA21EA 20050609000682005060900068SO 2005 6 9 SWIA200515035 120050517A2752 CONNECTOR EMB 120 EMB120ER 3260203SO TE FLAP ACTUATORDIRTY A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07215SW 120281 ON TAXI OUT, FLAP DISAGREEMENT WHEN FLAP LEVER SELECTED TO FLAPS 15 DEGREES POSITION. CLEANED ALL FLAP ACTUATORS CONNECTORS. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050609000692005060900069EA 2005 6 9 SWIA200515036 120050522A271010231007 DAMPER CNDAIRCL600 CL6002B19 1900309EA ELEVATOR MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07943SW5571 5571 7762 INTERMITTENT FLUTTER DAMPER STATUS MESSAGE IN FLIGHT. REPLACED LEFT AILERON AND NR 4 ELEVATOR FLUTTER DAMPER IAW 27-15-05, 27-34-05 CRJ MM. OPERATIONAL CHECK GOOD. P/N: 1023100-7, S/N OFF: HAI5124, S/N OFF: HAI5118. 2L72 4F RTA21EA 20050609000712005060900071EA 2005 6 9 SWIA200515038 120050518A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY MALFUNCTIONED A SWIAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 NM07455SW 7760 CARGO SMOKE WARNING ON GROUND IN SLC. REPLACED FWD & AFT SMOKE DETECTOR IAW 06-15-01. P/N 473597-19; S/N OFF 2274, S/N OFF 2275. 2L72 4F RTA21EA 20050609000722005060900072EA 2005 6 9 SWIA200515039 120050517A2730 SENSOR CNDAIRCL600 CL6002C10 1390015EA LT ELEVATOR MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CRCRUISE 1 NM07726SK 10190 ELEVATOR SPLIT CAUTION MSG INFLIGHT. REPLACED LEFT ELEVATOR RVDT. OPERATIONAL CHECK GOOD. REF CRJ MM 27-34-10. 2L72 4F RTA21EA 20050609000732005060900073EA 2005 6 9 SWIA200515040 120050518A274070609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07460SW 7803 BOTH STAB TRIMS DISENGAGED EN ROUTE. REPLACED HSTCU IAW MM 27-41-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050609000742005060900074EA 2005 6 9 SWIA200515041 120050521A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY MALFUNCTIONED A SWIAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 NM07443SW 7638 SMOKE CARGO WARNING ON THE GROUND, NO SMOKE OBSERVED. REMOVED AND REPLACED FWD CARGO SMOKE DETECTOR IAW M/M 26-15-01. OPERATIONAL CHECK GOOD. P/N 478597-19; S/N OFF 1929. 2L72 4F RTA21EA 20050609000752005060900075EA 2005 6 9 SWIA200515042 120050521A27605120011 PCU CNDAIRCL600 CL6002C10 1390015EA SPOILER MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07732SK694 694 10194 INBOARD FLIGHT SPOILERS CAUTION & INBOARD SPOILERONS CAUTION MSG. REPLACED LEFT INBOARD MULTI FUNCTION SPOILER PCU IAW CRJ MM 27-62-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050609000762005060900076EA 2005 6 9 SWIA200515043 120050519A2740 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA ELEVATORS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07934SW 7722 F/O`S TRIM SWITCH STICKS (RIGHT SIDE OF SWITCH). REPLACED F/O`S ELEVATOR TRIM SWITCH ON F/O`S YOKE. OPERATIONAL CHECK GOOD PER MM 27-40-00. 2L72 4F RTA21EA 20050609000772005060900077EA 2005 6 9 SWIA200515044 120050517A335020131A BATTERY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCHARGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07912SW 7595 ONE CEILING LEVEL EMERGENCY FLOODLIGHT INOPERATIVE. REPLACED NR 4 EMERGENCY BATTERY PACK IAW MM 33-51-04. OPERATIONAL CHECK GOOD. P/N: 2013-1A, S/N OFF: 44576. 2L72 4F RTA21EA 20050609000792005060900079EA 2005 6 9 SWIA200515046 120050521A27604916405 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07416SW 7089 SPOILERONS FAULT STATUS MESSAGE ILLUMINATED. REPLACED NR 2 SECU IAW MM 27-61-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050609000812005060900081WP 2005 6 9 ARWA20050506 120050523A7931VT0306D TRANSMITTER DOUG DC10 DC1030F 3023504WP OIL PRESSURE MALFUNCTIONED A ARWAD RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TXTAXI/GRND HDL 1 SO19478CT 47819 LOG PAGE NR 117738. DURING TAXI, ENGINE NR 1 OIL PRESSURE INDICATOR DROPPED TO (ZERO). ALL OTHER PARAMETERS NORMAL, RETURN TO BLOCK IAW AOM ALTERNATE PROCEDURES. REMOVED AND REPLACED ENGINE NR 1 OIL PRESSURE TRANSMITTER IAW MM 79-33-01. OPERATIONAL CHECK FOUND NORMAL IAW MM 71-00-00. 2L73 4F RTA22WE 20050609000822005060900082WP 2005 6 9 ABXA050132 120050516A542099582214 WEB DOUG DC9 DC931 3022065WP RT ENG PYLON CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23906AX 47072 CRACK INSIDE PYLON UNDER PANEL 8206. REPAIRED CRACK IAW DC-9 SRM 54-01. 2L72 4F A6WE 20050609000832005060900083WP 2005 6 9 ABXA050131 120050516A53205956034535 SUPPORT DOUG DC9 DC931 3022065WP FWD FUSELAGE BROKEN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23906AX 47072 FLOOR TRACK SUPPORT BROKE OFF BETWEEN LONGERON 28 RIGHT, LONGERON 27 RIGHT, AFT OF CARGO DOOR. FABRICATED NEW SUPPORT AND REPAIRED AREA IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 20050609000852005060900085WP 2005 6 9 ABXA050134 120050518A5340991968914 ANGLE DOUG DC9 DC931 3022065WP CABIN CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23906AX 47072 CRACKED VERTICAL ANGLE BELOW RIGHT BUTT LINE 44 TRACK AT STA 617 FLOORBEAM. REMOVED AND REPLACED ANGLE IAW DC9 SRM 51-30-5. 2L72 4F A6WE 20050609000942005060900094NM 2005 6 9 SWAA051473 120050520A5313BAC1498155 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 312 TO BS 322, STR 27R. REPLACED STRINGER SECTION PER SRM. 2L72 4F RTA16WE 20050609000962005060900096NM 2005 6 9 SWAA051475 120050520A53226546529 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND 4 EA FUSELAGE SHEAR TIES CRACKED AT BS 400, BS 500A, BS 500B & BS 520, STR 15R TO STR 16R. REPAIRED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20050609000972005060900097NM 2005 6 9 SWAA051476 120050520A53226546529 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 500, STR 14R TO STR 15R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050609000982005060900098NM 2005 6 9 SWAA051477 120050520A53226546529 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 500D, STR 16R TO STR 17R. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050609001012005060900101NM 2005 6 9 SWAA051480 120050520A53116546548 FRAME BOEING737 7373H4 1384600NM AFT CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 13L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050609001032005060900103NM 2005 6 9 SWAA051482 120050520A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727D, STR 20L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050609001062005060900106NM 2005 6 9 SWAA051485 120050520A53116552879 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME ANGLE CRACKED AT BS 947, LBL 23, WL 180. REMOVED AND REPLACED ANGLE PER SRM. 2L72 4F RTA16WE 20050609001072005060900107NM 2005 6 9 SWAA051486 120050521A3350604222 BATTERY PACK BOEING737 7373K2 13844BANM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29340LV 23738 DURING SCHEDULED A2 CHECK, FOUND FWD LT & RT LOWER EMERGENCY EXIT DOOR SIGN LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK & CHARGER PER MM. 2L72 4F RTA16WE 20050609001082005060900108NM 2005 6 9 SWAA051487 120050522A53306545765 SKIN BOEING737 7373H4 1384600NM FUSLEAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29352SW 24888 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 500A + 10, STR 19R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050609001092005060900109NM 2005 6 9 SWAA051488 120050522A56105717623122 WINDOW BOEING737 7373H4 1384600NM COCKPIT ARCED A SWAAO OTHER O OTHER NRNOT REPORTED 1 SW29382SW 26588 R2 COCKPIT WINDOW ARCED & CRACKED. REMOVED AND REPLACED R2 WINDOW PER MM. 2L72 4F RTA16WE 20050609001102005060900110NM 2005 6 9 SWAA051489 120050521A3350311500 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT UNSECURE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29423WN 29827 EEPLS LENS NOT SECURED. SECURED LENS PER MM. 2L72 4F RTA16WE 20050609001122005060900112NM 2005 6 9 SWAA051491 120050520A5240141A1715 GATE BOEING737 7377H4 1384404NM L1 DOOR CRACKED A SWAAO OTHER O OTHER NRNOT REPORTED 1 SW29457WN 33856 L1 DOOR UPPER GATE AFT CORNER CRACKED. MX FERRY TO DALLAS FOR REPAIRS. REMOVED AND REPLACED UPPER GATE PER MM. 2L72 4F RTA16WE 20050609001152005060900115NM 2005 6 9 SWAA051494 120050520A552265C25727 SKIN BOEING737 7373H4 1384600NM LT ELEVATOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29654SW 28399 DURING SCHEDULED RON CHECK, FOUND LT ELEVATOR OUTBOARD T/E CRACKED APPROX 22 OUTBOARD OF ELEVATOR TAB. REPAIRED LT ELEVATOR PER SRM. 2L72 4F RTA16WE 20050609001162005060900116NM 2005 6 9 SWAA051495 120050522A5753 SKIN BOEING737 7373G7 1384595NM LT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29670SW BN877 23784 DURING SCHEDULED RON CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2L72 4F RTA16WE 20050609001172005060900117 2005 6 9 SWAA051496 420050522A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29705SW 27839 R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR STRAPS LOOSE. SECURED STRAPS PER MM. 2L72 4F RTA16WE 20050609001182005060900118NM 2005 6 9 SWAA051497 120050521A3350604222 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29723SW 27855 DURING SCHEDULED MV2 CHECK, FOUND RT EMERGENCY EXIT BATTERY INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20050609001192005060900119EA 2005 6 9 SWIA200515048 120050210A5347 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07590SW 7077 LT SIDE SEAT RAIL BETWEEN FS 449.85 - 449.00 IS CORRODED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED IAW CRJ SRM 51-04-11, 51-41-02, 51-25-16. 2L72 4F RTA21EA 20050609001202005060900120EA 2005 6 9 SWIA200515049 120050210A5347 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07590SW 7077 LT SIDE SEAT RAIL BETWEEN FS 364 - 409 + 16 IS CORRODED, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED LT SIDE SEAT RAIL B/W FS 364-409 + 16 IAW CRJ SRM 51-41-02 PART 3. 2L72 4F RTA21EA 20050609001222005060900122EA 2005 6 9 SWIA200515051 120050210A5347 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07590SW 7077 LT SIDE SEAT RAIL BETWEEN FS 409.00 + 112 AND FS 449.85 IS CORRODED ITEM FOUND AT C-CHECK INSPECTION. INSTALLED LT SIDE SEAT RAIL BETWEEN FS 409.00 + 112 ANS FS 449.85 IAW CRJ 200 SRM 51-41-04. 2L72 4F RTA21EA 20050609001272005060900127EA 2005 6 9 SWIA200515056 120050210A5320 SILL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07590SW 7077 CARGO COMPT RT FLOOR SILL PLATE RBL 41.0 BETWEEN FS 610.0 AND FS 621.0 CORRODED ON UPPER PLATE, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED PARTS INSTALLED IAW REO 601R-53-61-1301. 2L72 4F RTA21EA 20050609001302005060900130CE 2005 6 9 DJFA2005097 120050519A326041HE16 SWITCH BEECH MU300 400A 1155402CE LT GEAR DOOR DEFECTIVE E DJFAO OTHER J WARNING INDICATION APAPPROACH 1 EA23471CW RK161 CREW REPORTED THAT FOLLOWING GEAR EXTENSION THEY RECEIVED 3 GREEN LIGHTS ALONG WITH 2 RED LIGHTS IN GEAR HANDLE. GEAR WAS CYCLED, AND THE SAME INDICATION WAS OBSERVED. AIRCRAFT PERFORMED A GO-AROUND AND TOWER COMMUNICATED THAT THE GEAR AND GEAR DOORS APPEARED TO BE DOWN. CREW TESTED LANDING GEAR AURAL WARNING AND DID NOT RECEIVE THE WARNING HORN. AN EMERGENCY WAS DECLARED AND EMERGENCY GEAR EXTENSION WAS PERFORMED. THE RED GEAR HANDLE LIGHTS REMAINED ILLUMINATED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. WHILE ON TAXI, THE RED LIGHTS IN THE GEAR HANDLE HAD EXTINGUISHED. MAINTENANCE REPLACED A DEFECTIVE IB LT GEAR DOOR SWITCH. THE OPERATIONAL CHECK PROVED GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4F RTA16SW 20050609001312005060900131WP 2005 6 9 AALA20050350 120050522A2120 APU DOUG DC9 DC983 3022083WP APU BAY INOPERATIVE A AALAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 SW21439AA 49457 TPA - SMOKE AND ODOR IN CABIN. RETURNED TPA AND LANDED WITHOUT INCIDENT. PERFORMED SPECIAL ITEMS CARD 21 92 12 PACK BURN OUT AND OVERWEIGHT LANDING. REPLACED SEPARATOR BAG AND ACCOMPLISHED FUNCTIONAL CHECK FLIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050607001852005060700185EU 2005 6 7 05FDEA01391 120050520A5730 SKIN AIRBUS310 A310203 3930313EU RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25403FE 230 RIGHT WING OUTER FUEL CUTOUT FOR PANEL 650PB HAS TWO HOLES DOUBLE DRILLED. CHAMFERED 1 EACH HOLE IAW SRM A310 51-40-44. FOUND TO BE WITHIN LIMITS IAW A310 SRM 57-20-12 FIG 201. REPAIRED 1 EACH HOLE WITH BUSHING IAW EA 6-5710-88828 PT1 AND TD/J1/S1/00726/2005. INSTALLED DOME NUT IAW A310 SRM 51-40-21. DOME SEALED IAW A310 SRM 51-76-20. THIS IS A MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L72 4F RTA35EU 20050607001882005060700188NM 2005 6 7 QXEA200500953 120050521A3260301450301 PSEU BOMBDRDHC8 DHC8401 1390041NM ZONE 200 INOPERATIVE A QXEAO OTHER N FALSE WARNING CRCRUISE 1 NM09401QX7874 7874 4031 LAX - ON FLIGHT 2445, GEAR DOOR AMBER LIGHT R/L CAME ON AND RIGHT RED GEAR UNSAFE LIGHT CAME ON MOMENTARILY THEN EXTINGUISHED. MAINTENANCE REMOVED AND REPLACED PSEU. CYCLED GEAR SEVERAL TIMES, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050608000092005060800009SO 2005 6 8 CHQA200500103 120050528A3320 SOCKET EMB 145 EMB145LR 3260212SO INTERIOR LIGHTS BURNED A CHQAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL11271SK 145305 A STRONG ELECTRICAL SMELL WAS NOTED IN CABIN DURING PASSENGER BOARDING WITH THE APU ON AND PACKS RUNNING. MAINTENANCE INSPECTED THE SIDE WALL AND DISCOVERED THE FLUORESCENT LIGHT SOCKET WAS BURNT AT SEAT 7A. REMOVED LIGHT BULB FORM SOCKET 7A. REMOVED LIGHT BULB FORM SOCKET 7A AND PLACED ON MEL 33-20-001 CAT C TICKET 17849. REMOVED AND REPLACED SIDEWALL LIGHT ASSEMBLY AT SEAT 7A IAW EMB 145 AMM 33-20-00. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050608000252005060800025 2005 6 8 2005UALA00447 420050510A2565 SLIDE BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN TORN A UALAK NONE O OTHER ININSP/MAINT 1 WP29527UA 24995 TORN INFLATABLE SEAM IN DOG LEG. BEYOND SCOPE OF CMM. SEAM AT DOGLEG DISBONDED DURING AIR RETENTION TEST. DISBOND WAS BEYOND CMM REPAIR LIMITS. UNIT WAS RETURNED TO OEM FOR REPAIR AND INFLATABLE WAS REPLACED. 2L72 4F4 FRTA2NM E17NE 20050608000292005060800029NM 2005 6 8 2005UALA00452 120050518A3397 WIRE BOEING737 737322 1384676NM ROW 17 CUT A UALAK NONE O OTHER ININSP/MAINT 1 WP29347UA 24251 AFT EEL LIGHTS FROM ROW 17 AFT INOP. FEEDER CABLE CUT OR DAMAGED - REPLACED. 2L72 4F RTA16WE 20050608000312005060800031NM 2005 6 8 2005UALA00454 120050519A5320 SHEAR WEB BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29502UA 24623 AFT CABIN FLOOR SHEAR WEB IS CORRODED AT STA 1681 LBL 60. REMOVED CORROSION AND FABRICATED NEW TEE CAP. REPAIRED AND INSTALLED PER MM 53-00-98 2L72 4F4 FRTA2NM E17NE 20050608000362005060800036 2005 6 8 2005UALA00459 420050519A2565D31516113 ASPIRATOR AIRBUS320 A320232 3930326EU ESCAPE SLIDE FOD A UALAK NONE O OTHER ININSP/MAINT 1 WP29456UA 1128 PLASTIC BLOCK FOUND IN ASPIRATOR. THE PLASTIC BLOCK FOUND STUCK IN THE ASPIRATOR IS A FOREIGN OBJECT THAT IS NOT PART OF THE SLIDE ASSY. THIS TEFLON BLOCK WITH BEVELED CORNERS AND WITH A RED STRAP LOOKS LIKE IT HAD BEEN SPECIALLY FABRICATED FOR SOME UNKNOWN PURPOSE. HOW IT GOT STUCK IN THE ASPIRATOR HAS REMAINED UNKNOWN. IT IS SUSPECTED HOWEVER THAT THIS BLOCK WAS USED TO CHOCK THE ASPIRATOR FLAPPER IN THE OPEN POSITION TO RELIEVE THE PRESSURE DURING PACKING OF THE SLIDE. 2L72 4F RTA28NM 20050608000702005060800070EU 2005 6 8 DAT2005F00003 120050506A2910SD3730311XAC LINE STBROSSD3 SD360 8100606EU PWA PT6 PT6* 52043EA HYDRAULIC SYS LEAKING E DATAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 GL13367AC24976 SH3626 NORMAL DESCENT APPROACH AND FINAL CHECK LIST COMPLETE ALL SYSTEMS NORMAL THROUGH THE TOUCHDOWN. AFTER TOUCHDOWN BOTH THE HYD WCP WARNING LIGHTS ILLUMINATED. CHECK BRAKES AND NO RESPONSE. SELECTED EMERGENCY BRAKE AND USED FULL REVERSE TO STOP ON RUNWAY. THEN CLEARED RUNWAY AND PARKED ON THE 1ST TAXIWAY WHERE WE WERE TOWED INTO THE RAMP. A MECHANIC WAS DISPATCHED. THE STEERING ACTUATOR LINE WAS REMOVED AND REPLACED IAW MM. OPS CHECK GOOD AND AC WAS RETURNED TO SERVICE. (K) 2H72 4T3 T A41EU E2NE 20050608000722005060800072NM 2005 6 8 SWAA051446 120050518A53116516301 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 188, LT SIDE, WL 208. REPAIRED STUB FRAME PER SRM. 2L72 4F RTA16WE 20050608000772005060800077NM 2005 6 8 SWAA051451 120050518A3350101073 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29642WN 27715 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM. 2L72 4F RTA16WE 20050608000792005060800079NM 2005 6 8 SWAA051453 120050519A3350101114 BULB BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29200WN 32482 DURING SCHEDULED RON CHECK, FOUND L2 DOOR EXTERNAL EMERGENCY LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050608000812005060800081NM 2005 6 8 SWAA051455 120050519A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 727E, BL 0 & LBL 7. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050608000832005060800083NM 2005 6 8 SWAA051457 120050519A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 767, LBL 4 TO RBL 4. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050608000852005060800085 2005 6 8 SWAA051459 420050519A256565C16820 HOOK BOEING737 7373H4 1384600NM L1 DOOR GIRT BARLOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29351SW 24572 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED HOOK PER SRM. 2L72 4F RTA16WE 20050608000872005060800087NM 2005 6 8 SWAA051461 120050519A53306545774 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29664WN 23495 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D + 14.25, STR 20L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050608000892005060800089NM 2005 6 8 SWAA051463 120050519A53306545775 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29664WN 23495 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747 - 2, STR 21L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050608000912005060800091NM 2005 6 8 SWAA051465 120050519A53306545765 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29691WN 23781 DURING SCHEDULED C1 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS AT BS 496 & BS 500D + 12, STR 10L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050608000932005060800093 2005 6 8 SWAA051467 420050519A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29710SW 27844 R1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20050608000952005060800095NM 2005 6 8 SWAA051469 120050519A57536546435 SKIN BOEING737 7377H4 1384404NM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29768SW 30587 DURING SCHEDULED 5Y CHECK, FOUND LT WING T/E OUTBOARD AFT FLAP DELAMINATED. REPAIRED FLAP PER SRM. 2L72 4F RTA16WE 20050608001062005060800106NM 2005 6 8 DHL2005741528 120050420A5330 SKIN BOEING727 7272Q9 138448MNM FUSELAGE BENT A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH46665 21931 FUSELAGE SKIN BENT AT RT FWD AIRSTAIR CUTOUT AT STA 1223. REMOVED FASTENERS AS REQUIRED FOR ACCESS IAW B727 SRM 51-30-2. CUT-OUT DAMAGED AREA 10 INCHES BY 3/4 INCH AND FABRICATED DOUBLER FROM 2024 T3 .050 PO NR 900219 AND DOUBLER FROM 2024 T3 .050 PO NR 9002297 14 INCHES BY 3 INCHES IAW B727 SRM 53-30-2 FIG 3 AND 51-40-2 FIG 3 AND 51-40-2 FIG 1 PART TREATED AND PRIMED IAW B727 SRM 51-10-2 PART INSTALLED IAW B727 SRM 51-40-2 FIG 1. 2L73 4F RTA3WE 20050608001142005060800114NM 2005 6 8 2005UALA00465 120050520A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29502UA 24623 AFT PIT FUSELAGE FRAME IS DENTED AT STA 1480 STR 25L. CUT OUT DAMAGE AND ACP HFEC WITH NO CRACK INDICATION. PER GSO TIMCO REO G10464, FABRICATED RPR AND INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050608001162005060800116NM 2005 6 8 2005UALA00467 120050520A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE PUNCTURED A UALAK NONE O OTHER ININSP/MAINT 1 WP29383UA 24658 3-4 INCH DIAMETER HOLE PUNCTURED IN FUSELAGE SKIN ON RIGHT SIDE OF AIRCRAFT 6 FEET AFT OF RADOME AND 12 INCHES ABOVE NLG DOOR CUTOUT. SKIN IS ALSO DENTED 2 INCHES ABOVE PUNCTURE. THIS IS A MAJOR REPAIR INSTALLED DOUBLER AND TRIPLER PER SRM 53-10-01 FIG 211 DE TAIL IV. 2L72 4F4 FRTA16WE E2GL 20050608001182005060800118EU 2005 6 8 2005UALA00469 120050523A2913887673 PUMP AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE HYDRAULIC SYS FAILED A UALAA UNSCHED LANDING K FLUID LOSS APAPPROACH 1 WP29474UA 1475 LOST GREEN HYD SYSTEM WHILE IN A HOLDING PATTERN ABOVE PLANNED DESTINATION. GREEN SYSTEM EDP REPLACED AWAITING FINDINGS FROM THE VENDOR (ARINC). REPLACED NR 1 ENG DRIVEN PUMP, REF MM29-11-51. REPLACED CASE DRAIN FILTER, PDI NOT POPPED. NO DEBRIS FOUND IN FILTER. FILTER PLACED IN CONTAINER WITH PUMP. 2L72 4F4 FRTA28NM E40NE 20050608001342005060800134NM 2005 6 8 05FDEA01483 120050530A3211 SUPPORT DOUG MD11 MD11 3023602NM LANDING GEAR CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 CENTER LANDING GEAR, LT TRUNNION SUPPORT FITTING PILLOW BLOCK EMITTING RUST. REMOVED AND REPLACED PER CMM 32-15-01. PILLOW BLOCK ASSEY REMOVED AND REPLACED PER CMM 32-15-01. 2L73 4F RTA22WE 20050608001532005060800153WP 2005 6 8 05FDEA01496 120050531A5420 STIFFENER DOUG MD10 MD1010F 3022112WP GE CF6 CF66D 30020GL NR 1 STRUT GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25391FE 46625 COMPLY WITH EA 8-7254-89506 ENGINE - TURBINE - TMF STRUT NR 1 STIFFENER GOUGE REPAIR. COMPLIED WITH EA 8-7254-89506. 2L73 4F4 FRTA22WE E23EA 20050608001602005060800160EA 2005 6 8 A6WA200540166 120050508A2760 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA COCKPIT ACTIVATED A A6WAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL31447AW 7812 ON TAKEOFF, ABORTED TAKEOFF DUE TO SPOILERON CONFIG WARNING. NOTE SPEED 60 KNOTS, BTMS HIGHEST READING 4 AND 2. SENT MECHANIC FROM IAS TO BTV. PERFORMED FUNCTION CHECK OF SECU SYSTEM, AND BITE CHECK. ALL CHECKED GOOD PER 27-61-05. (M) 2L72 4F RTA21EA 20050608001652005060800165EA 2005 6 8 A6WA200540167 120050512A2430 DCU CNDAIRCL600 CL6002B19 1900309EA ELECTRICAL SYS MALFUNCTIONED A A6WAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL31422AW 7341 DC ESS BUS CAUTION MESSAGE, SYSTEMS APPEARED TO BE UNAFFECTED, CBP4-B3 POPPED. RECYCLED C/B AND REMOVED AND REPLACED NR 2 DCU. OPS CHECK NORMAL IAW AMM 24-31-00. (M) 2L72 4F RTA21EA 20050608001682005060800168 2005 6 8 ABXA050123 420050523A2565 SLIDE BOEING767 767231 1385131NM PAX DOOR MALFUNCTIONED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23702AX 22566 MAIN ENTRY DOOR SLIDE WOULD NOT ARM. CYCLED MAIN ENTRY DOOR SEVERAL CYCLES. SLIDE ARM MECHANISM ARMED AND DISARMED AS REQUIRED. ALL CHECKS GOOD IAW B767 AMM. 2L72 4F RTA1NM 20050608001692005060800169 2005 6 8 A6WA200540174 420050515A3160 DISPLAY CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A A6WAA UNSCHED LANDING G MULTIPLE FAILURE CLCLIMB 1 GL31410AW 7490 CAPTAINS MFD FAILED INFLIGHT, UNABLE TO USE REVISIONARY FUNCTION F/O PFD ERRATIC AND STAB TRIM 1 AND 2 AND MACH TRIM DISENGAGES. INTERROGATED MDC, NO CURRENT FAULTS FOUND, RE-SET CAPTS MFD CB FOR FAILED CAPTS MFD, CND. FAULT PERFORMED NR 1 AND NR 2 ENGINE RUNS CYCLED 1 AND 2 GENERATOR MFD AND PFD FOR FAULTS. PERFORMED HFTCU FAULT ISOLATION TASK IAW 27-40-00 FOR STAB TRIM DISENGAGED. (M) 2L72 4F RTA21EA 20050608001742005060800174WP 2005 6 8 AMTA200500458 120050519A3350 LIGHT LKHEED1011 10113853 5265020WP RROYCERB211 RB211524B4 54555NE CABIN INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11161AT 1219 EMERGENCY FLOOR PATH LIGHTS 2-6 HJK, INOPERATIVE. REPLACED FWD GALLEY EGRESS STRIP AND RECONNECTED CONNECTOR AT ROW 2, EGRESS. OPS CHECKS GOOD. (K) 2L73 4F4 F A23WE E12EU 20050608001752005060800175WP 2005 6 8 ABXA050126 120050518A571436429831 FITTING DOUG DC8 DC863F 302198FWP CENTER WING CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23816AX 46093 DURING LINE MAINTENANCE, FOUND THE CENTER WING TANK FRONT SPAR LT SUPPORT FITTING CRACKED AT STA XCW 67. REPLACED FITTING IAW DC-8 SRM 51-3-0. 2L74 4F 4A25 20050608001782005060800178NM 2005 6 8 ABXA050125 120050518A5270 WARNING LIGHT BOEING767 767281 1385109NM EMERGENCY DOOR INTERMITTENT A ABXAO OTHER N FALSE WARNING CRCRUISE 1 GL23797AX 23147 EMERGENCY DOOR LIGHT FLASHED INTERMITTENTLY IN TURBULENCE. FOUND EMERGENCY DOOR LIGHT FLICKERING ON GROUND. NO EICAS MESSAGE. CODE 007 ON PSEU. RESEATED CARD 3 AND 4 IN PSEU. RETESTED PSEU IAW B767 MM 32-09-04. NO FAULTS NOTED. DOOR LIGHT EXTINGUISHED. 2L72 4F RTA1NM 20050608001802005060800180WP 2005 6 8 ABXA050129 120050520A53305910228 SKIN DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 FUSELAGE SKIN CRACKED FS 1090, APPROXIMATELY 2 INCHES TO THE RIGHT SIDE OF VERTICAL STAB, SKIN CRACKED OUT OF HI-LOK APPROXIMATELY .25 INCH LONG. REPAIRED FUSELAGE SKIN AT FS 1090, RIGHT SIDE OF VERTICAL STAB IAW DC-9 SRM 53-01. 2L72 4F A6WE 20050608001842005060800184EA 2005 6 8 A6WA200540176 120050516A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE DENTED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31452AW 7835 RT AFT FUSELAGE SKIN AT FS 590, 11 INCHES BELOW LOW PRESSURE EXT AIR DOOR HAS DENT AND GOUGE. REPAIRED LOWER AFT FUSELAGE SKIN AT FS 590 BETWEEN STRINGERS 21L AND 25R BY REMOVING EXISTING REPAIR AND INSTALLING A LARGER EXTERNAL DOUBLER IAW BRAS EO. (K) 2L72 4F4 FRTA21EA E15NE 20050608001952005060800195NM 2005 6 8 DHL2005741529 120050427A5330 SKIN BOEING727 7272Q9 138448MNM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH46665 21931 ACCOMPLISH IDENTIFICATION OF EXISTING REPAIR ON FUSELAGE SKIN AT STA 1333 AT STR 26L PER ASTAR FCD 500001-003-B. REMOVED EXISTING REPAIR PLATE FUSELAGE SKIN STA 1333 STR 26L IAW B727 SRM 51-30-2 DIM3 3/4 INCH BY 2 INCHES. FABRICATED NEW DOUBLER FROM 2024T3 .063 PO NR 9001684 DIM 9 1/4 INCHES BY 5 9/16 INCHES IAW B727 SRM 53-30-2 FIG 3 AND 53-30-3 FIG1. TREATED AND PRIMED NEW DOUBLER AND REPAIR AREA IAW B727 SRM 51-10-2. INSTALLED NEW DOUBLER IAW B727 SRM 51-30-2. 2L73 4F RTA3WE 20050608002052005060800205WP 2005 6 8 UPS05844552 120050524A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE:C3 RIGHT O/B LEADING EDGE RIB CRACKED AT XFS 678.750 (LOWER RIB). STOP DRILLED CRACK, FABRICATED REPAIR ANGLE, AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-2-0 FIG 2, 51-1-20D, AND 51-1-21. 2L74 4F RT4A25 20050608002162005060800216WP 2005 6 8 UPS05844564 120050525A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE:C3 RIGHT CENTER WING L/E UPPER RIB CRACKED AT XFS 416. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR ANGLE IAW DC8 SRM 57-2-0 FIG 2, 51-1-20D, AND 51-1-21. 2L74 4F RT4A25 20050608002192005060800219WP 2005 6 8 UPS05844569 120050525A5720 DOUBLER DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE:C3, CENTER WING L/E UPPER INNER DOUBLER CRACKED .5 INCH LONG AT XFS 422. REMOVED INNER DOUBLER, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW DC-8 SRM 51-1-21 AND DWG 5769891. 2L74 4F RT4A25 20050608002202005060800220WP 2005 6 8 UPS05844570 120050525A5720 DOUBLER DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE:C3, RIGHT CTR WING L/E LWR INNER DOUBLER AROUND DRAIN HOLE CRACKED .5 INCH LONG AT XFS 335. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT INNER DOUBLER IAW DC8 SRM 57-3-3 FIG 5 AND 51-1-21. 2L74 4F RT4A25 20050609000032005060900003CE 2005 6 9 ACE052405 120050524A28221143890425 DIAPHRAGM ROMEC BEECH 1900 1900C 1154161CE FUEL PUMP RUPTURED E YADAK NONE K FLUID LOSS TXTAXI/GRND HDL 1 AL03114AX UC66 PIREP - FUEL LEAKING FROM NR 1 ENGINE GANG DRAIN. REPLACED LOW PSI DUEL PUMP DUE RUPTURED DIAPHRAGM. 2L72 4T RTA24CE 20050609000072005060900007SO 2005 6 9 C2XA05SH038 120050520A533012041320067 SKIN PANEL EMB 145 EMB145ER 3260211SO FWD FUSELAGE LIGHTNING STRIKEA C2XAK NONE O OTHER ININSP/MAINT 1 SW2714938 145029 DURING C-CHECK VARIOUS LIGHTNING STRIKE ON SKIN PNL 214. MAINTENANCE REPAIR SKIN PNL 214 ABOVE STR 13R AFT FR 1A IAW EC 5330-01465. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20050609000112005060900011SO 2005 6 9 C2XA05CL039 120050522A521014533990403 BAR EMB 135 EMB135ER 3260203SO CABIN DOOR BINDING A C2XAO OTHER O OTHER TXTAXI/GRND HDL 1 SW2715509 145238 CLE FLIGHT 2944 THE CREW REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN. MAINTENANCE INSPECTED AND ADJUSTED THE UPPER AND LOWER STABILIZER BARS OF THE MAIN CABIN DOOR. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20050609000122005060900012NM 2005 6 9 C1HA200596002 120050422A5320 INTERCOSTAL BOEING727 7272J4 1384006NM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15696CA 22574 MAIN PASSENGER CABIN STA 304 TO 312 RBL 55, UNDER CONTROL CABIN BULKHEAD BOTTOM ANGLE, INTERCOSTAL CORRODED FWD END. 2L73 4F RTA3WE 20050609000232005060900023NM 2005 6 9 05FDEA01415 120050524A5320 INTERCOSTAL DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25631FE 48454 MAIN DECK CABIN - AFT CABIN AT STA 1661 RT AT LONGERON 7R LOCATION FOUND INTERCOSTAL CRACK AS MARKED. CRACKED INTERCOSTAL AT MAIN DECK CABIN, AFT AT STA 1661 RH LONGERON 7R REMOVED AS PER SRM 51-35-01 VOL II AND NEW INTERCOSTAL INSTALLED AS PER SRM 51-31- 01 VOL II. NEW INTERCOSTAL FABRICATED AS PER DWG AFA 7761. REPAIR CLASSIFIED AS PER MINOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050609000312005060900031NM 2005 6 9 C1HA200596007 120050425A5315 FLOORBEAM BOEING727 7272J4 1384006NM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15696CA 22574 MAIN PASSENGER CABIN STA 344 LBL 19 TO 57 FLOORBEAM TOP CORRODED. 2L73 4F RTA3WE 20050609000332005060900033NM 2005 6 9 C1HA200596009 120050426A5311 FRAME BOEING727 7272J4 1384006NM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15696CA 22574 FUSELAGE INTERIOR STA 312 LOWER LT HORIZONTAL WALKBEAM, AND FRAME CORRODED (GENERATING ITEM C53-111-03-02) FUSELAGE INTERIOR STA 304 - LOWER LT FRAME HAS CORROSION. REPAIRED CHORD PER CAEO 727-5316-02 AND SRM 53-10-4 FIG 7. 2L73 4F RTA3WE 20050609000412005060900041NM 2005 6 9 F3LA200500021 120050522A5210 COVER AIRBUSA319 A319111 3930336NM GEARBOX CRACKED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03917FR 3933 1890 DURING C-2 CHECK, INSPECTION REPORTED CRACK IN R2 DOOR GEARBOX COVER. REPAIRED R2 DOOR GEARBOX COVER PER EA A9-52R-10886. PAINTED R2 DOOR GEARBOX COVER PER AMM 25-00-00-340. 2L72 4F RTA28NM 20050609000512005060900051WP 2005 6 9 UPS05844508 120050428A5312 PRESSURE PANEL DOUG DC8 DC873F 302199FWP RT MLG WW CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE:C1 CORROSION ON RT W/W CEILING AT STA 863 RBL 42 AND 48 UNDER LONGERONS, ON WEB, AND DOUBLER IN MAIN CABIN IS BULGED. CUT OUT CORROSION, FABRICATED AND INSTALLED REPAIR IAW SAA SK 880-7620 56 AND EO DC-8-5310-22195-A. 2L74 4F RT4A25 20050609000782005060900078EA 2005 6 9 SWIA200515045 120050516A2750860D10018ABCD CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07720SW 7297 RECEIVED FLAPS HALF SPEED. REPLACED FECU IAW 27-57-05. OPERATIONAL CHECK GOOD. P/N 860D100-18ABCD, S/N OFF 741. 2L72 4F RTA21EA 20050609000862005060900086EA 2005 6 9 COMA0560314 120050520A2910AE127631 LINE CNDAIRCL600 CL6002B19 1900309EA HYDRAULIC SYS LEAKING A COMAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO01721CA 7259 FLIGHT 5088 HYDRAULIC SYSTEM NR 1 LOW PRESSURE CAUTION, QUANTITY INDICATED 0. REPLACED HIGH PRESSURE LINE IN LEFT HAND ENGINE PYLON. 2L72 4F RTA21EA 20050609000902005060900090NM 2005 6 9 DHL2005740561 120050327A5542 SKIN BOEING727 7272Q9 138448MNM RUDDER DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH46106 21930 VERT STAB BELOW FIN STA 133 RT LOWER RUDDER SURF IS DENTED NEAR T/E CORRECTIVE ACTION: EVALUATED DENTED AREA AT VERT STAB FIN STA 133 RT LOWER RUDDER SURF IAW B727 SRM 55-40-1 FOUND OUT OF LIMITS TRIM OUT DAMAGED AREA. SIZE 1/2" BY 3/4" IAW B727 SRM 55-30-3- AND 51-10-1. FABRICATED DOUBLER REPAIR SIZE 2" BY 2.5" MAT USED 2024T3 .032 PO NR 9002034 IAW B727 SRM 55-20 -3 FIG 1. APPLIED ALODINE AND PRIMER AT THE AREA AND PARTS IAW B727 SRM 51-10-2. INSTALLED DOUBLER REPAIR AT VERT STAB BELLOW FIN STA 133RT LOWER RUDDER SURFACE IAW B727 SRM 51-30-2 AND 55-20-3 FIG1. 2L73 4F RTA3WE 20050609001232005060900123EA 2005 6 9 SWIA200515052 120050210A5347 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07590SW 7077 RT SIDE SEAT RAIL BETWEEN FS 409.00 + 16 - FS 409.00 + 112 IS CORRODED ITEM FOUND AT C-CHECK INSPECTION. INSTALLED RT SIDE SEAT RAIL BETWEEN FS 409.00 + 16 - FS 409.00 + 112 IAW CRJ 200 AND MM 20-21-00-910-001. 2L72 4F RTA21EA 20050609001252005060900125EA 2005 6 9 SWIA200515054 120050210A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07590SW 7077 CRACKED FRAME FLANGE AT FS 605 AND STRINGER 9 LT SIDE ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-61-1305. 2L72 4F RTA21EA 20050609001292005060900129EA 2005 6 9 SWIA200515058 120050223A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07956SW 7077 FS 621 LT FLOORBEAM ANGLE AT LBL 41 IS CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FLOOR SUPPORT ANGLE IAW CRJ REO 601R-53-61-117 REV B. 2L72 4F RTA21EA 20050609001322005060900132WP 2005 6 9 AALA20050351 120050522A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21982TW 53632 DFW - CEILING EMERGENCY LIGHTS AT ROW 3D INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROW 3D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050609001352005060900135NE 2005 6 9 AALA20050349 220050522A7200 ENGINE BOEING757 757223 1384957NM RROYCERB211 RB211535E4B3 NE NR 1 LEAKING A AALAO OTHER K FLUID LOSS CRCRUISE 1 SW21689AA 25731 31027 NR 1 ENGINE WAS SHUT DOWN IN FLIGHT DUE TO LOSS OF OIL QUANTITY AND OIL PRESSURE AT FLIGHT LEVEL 360. SINGLE ENGINE OPERATION FOR 90 MINUTES. AIRCRAFT DIVERTED TO MIA. REPLACED NR 1 ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA2NM E12EU 20050609001362005060900136EU 2005 6 9 AWXA200500591 120050521A3233C247300016 ACTUATOR AIRBUS320 A320231 3930325EU UPLOCK FAULTY A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28644AW3691417622 317 DURING CLIMB SELECTING GEAR UP & NLG FAILED TO RETRACT & RECEIVED A RED UNLOCK LIGHT. SELECTED GEAR DOWN & GEAR FAILED TO EXTEND (MAINS, NOSE SHOWED GREEN/RED UNLK.) SELECTED GEAR UP & GEAR RETRACTED WITH NORMAL INDICATIONS. SELECTED GEAR DOWN WITH NORMAL EXTENSION & INDICATIONS. MX R & R LGCIU NR 1 & 2 AS A PRECAUTIONARY MEASURE IAW AMM. OPS CK GOOD. MX ADDITIONALLY R & R NLG PROX SENSORS 19GA, 24GA, 25GA, 30GA, & 31GA PER AMM & R & R NLG DOWNLOCK SENSOR 18GA IAW MM. OPS CK GOOD. MX R & R NLG UPLOCK ACTUATOR 2530GM IAW AWA TASKCARD NR R4N32307 OPS & FUNCTIONAL CKS GOOD. 2L72 4F RTA28NM 20050609001372005060900137EU 2005 6 9 AWXA200500592 120050522A323011409015 SELECTOR VALVE AIRBUS320 A320231 3930325EU MLG MALFUNCTIONED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28634AW 091 EN ROUTE, PILOTS REPORTED DURING CLIMB & DURING MLG RETRACTION A GRINDING NOISE & ECAM MESSAGE MLG NOT UPLOCKED. CYCLED MLG IAW MX AND UPON RETRACTION SAME NOISE ON RT MLG DOWN. ACFT RETURNED & LANDED WITHOUT INCIDENT. MX R & R MLG SELECTOR VALVE IAW AMM. OPS CK GOOD AIW AWA TASKCARD. PART IS NOT TRACKED BY S/N BUT AMWEST RECORDS SHOW ONLY 1 SELECTOR VALVE HAVING A REPAIR ORDER REQUESTED ON 05/22/05 (THE DATE OF INCIDENT), RO 2224169. THE VENDOR REPORT FOR THIS PARTICULAR UNIT, RO 2224169, STATES THAT THIS UNIT FAILED PRETEST, REVEALING AN INTERNAL LEAK IN THE UNIT. SEVERAL SEALS WERE REPLACED. THIS UNIT WAS TESTED AND REPAIRED IAW CMM 32-32-34 REV. 13. 2L72 4F RTA28NM 20050609001382005060900138NM 2005 6 9 AWXA200500593 120050520A335020131A BATTERY PACK BOEING757 7572S7 1384962NM EMERGENCY EXIT FAULTY A AWXAK NONE O OTHER ININSP/MAINT 1 WP28906AW 23568 PHX - EEL - DURING 4-DAY CHECK, THE LT EMERGENCY EXIT EXTERIOR SLIDE LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IAW B757 MM 33-51-07. OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20050609001402005060900140NM 2005 6 9 AWXA200500595 120050504A53106552878533 STRUCTURE BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28322AW 25400 MCN - MAJOR REPAIR - DURING C-14 CHECK, CORROSION WAS FOUND ON THE L2 INNER CHORD LOCATED AT BS 978, BS 982, BS 991, LT BL 46, WL 209. MAINTENANCE FOUND THE CORROSION TO BE OUT OF LIMITS PER B737-300 SRM 53-60-51-1. MAINTENANCE REMOVED AND REPLACED INNER CHORD IAW B737-300 SRM 51-40-02-0, FIGURES 8 AND 12. 2L72 4F RTA16WE 20050609001422005060900142NM 2005 6 9 AWXA200500597 120050518A575465C2679913 SKIN BOEING737 7373G7 1384595NM ZONE 500 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28322AW 25400 DURING C-14 CHECK A CRACK WAS FOUND ON THE NR 1 SLAT LOWER SKIN AT SLAT STATION 256 TO SLAT STATION 260. MAINTENANCE REPAIRED THE NR 1 SLAT LOWER SKIN AT STATION 256 - 260 IAW B737-300 SRM CHAPTER 57-43-01-2 FIGURE 206 AND DWG 65C26779. 2L72 4F RTA16WE 20050609001432005060900143NM 2005 6 9 AWXA200500598 120050506A5322654583312 SHEAR TIE BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28322AW 25400 DURING C-14 CHECK, A CRACK WAS DISCOVERED AT A SHEAR TIE WEB, BS 196.5, WL 207, RT BL 29. MAINTENANCE REMOVED WEB, FABRICATED NEW WEB AND INSTALLED IAW B737-300 SRM 51-40-02-0 FIGURE 8, 12 AND BOEING DRAWING NR 65-45833. 2L72 4F RTA16WE 20050609001442005060900144NM 2005 6 9 AWXA200500599 120050505A5312651758267 BEAM BOEING737 7373G7 1384595NM BULKHEAD CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28322AW 25400 DURING C-14 CHECK, BS 178 BULKHEAD VERTICAL BEAM WAS FOUND TO BE CRACKED IN WEB, LT BL 17.1 WL 183. MAINTENANCE REPAIRED CRACK AT BS 178 BULKHEAD VERTICAL BEAM AT LT BL 17.1, WL 183, IAW B737-300 SRM 53-10-08-2, FIGURE 212. 2L72 4F RTA16WE 20050609001462005060900146NM 2005 6 9 AWXA200500601 120050518A53136562208502 STRINGER BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28322AW 25400 DURING C-14 CHECK, A CRACK WAS FOUND ON STRINGER AT STR 3R BS 663.75. MAINTENANCE REPAIRED STR 3R BS 663.75 IAW B737 300 SRM 53-00-03-2 FIGURE 204 AND DWG65-62208. 2L72 4F RTA16WE 20050609001472005060900147NM 2005 6 9 AWXA200500602 120050505A5310651758322 BEAM BOEING737 7373G7 1384595NM BULKHEAD CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28322AW 25400 DURING C-14 CHECK, BS 178 BULKHEAD VERTICAL BEAM WEB AT WL 175, LT BL 5.7, WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED BULKHEAD VERTICAL BEAM WEB IAW B737-300 SRM 53-10-08-2, FIGURE 212. 2L72 4F RTA16WE 20050609001482005060900148NM 2005 6 9 AWXA200500603 120050506A53206517685634 INTERCOSTAL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28322AW 25400 DURING C-14 CHECK, INTERCOSTAL WEB WAS FOUND CRACKED AT BS 294, LT STRINGER 16. MAINTENANCE REMOVED AND INSTALLED NEW INTERCOSTAL AT BS 294, LT STRINGER 16 IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5300-05138-SS5. 2L72 4F RTA16WE 20050609001512005060900151GL 2005 6 9 AWXA200500606 220050523A7310 TUBE BOEING737 7373G7 1384595NM CFMINTCFM56 CFM563B1US GL NR 1 ENGINE DIRTY A AWXAE ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TXTAXI/GRND HDL 1 WP28302AW 24009 DEN - ENGINE START ATTEMPT - FLT 489 WHILE STARTING NR 1 ENGINE AT APPROXIMATELY 28 PERCENT N2 FUEL FLOW DECREASED TO ZERO. MAINTENANCE TROUBLESHOT SYSTEM IAW MM 28-22-00-1 STEPS 1-4, MM 71-00-41-1 STEP 1, 71-00-42-01, 71-00-59-1. MAINTENANCE PERFORMED A CHECK AND CLEANED OUT THE CDP TUBE. MAINTENANCE INSPECTED THE MAIN ENGINE CONTROL AND SPECIFIC GRAVITY WITH NO FAULTS FOUND. MAINTENANCE RAN ENGINE 4 COMPLETE CYCLES. ENGINE CHECK GOOD. 2L72 4F4 FRTA16WE E2GL 20050609001522005060900152NM 2005 6 9 AWXA200500607 120050505A5753 SKIN BOEING737 7373U3 13844CCNM ZONE 500 DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28335AW 28740 DURING C-6 CHECK, THE LT INBOARD FOREFLAP WAS FOUND TO BE DISBONDED ON THE UPPER SURFACE, 36 INCHES FROM OUTBOARD END, LT WBL 146.275 TO LT WBL 148.275. MAINTENANCE REPAIRED DISBONDED AREA IAW B737-300 SRM 51-70-10-0, FIGURE 31. 2L72 4F RTA16WE 20050609001542005060900154NM 2005 6 9 AWXA200500609 120050505A5753 SKIN BOEING737 7373U3 13844CCNM ZONE 600 DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28335AW 2554 28740 DURING C-6 CHECK, THE RT OUTBOARD, AFT FLAP WAS FOUND TO BE DISBONDED ON THE LOWER SURFACE, APPROXIMATELY 6.54 INCHES FROM INBOARD END. FURTHER INSPECTION FOUND WATER IN HONEYCOMB STRUCTURE. DUE TO WATER IN HONEYCOMB STRUCTURE, MAINTENANCE REMOVED AND REPLACED THE RT OUTBOARD, AFT FLAP IAW AMERICA WEST AIRLINES TASK CARD NR R3M27034. 2L72 4F RTA16WE 20050609001552005060900155NM 2005 6 9 DHL2005740562 120050324A5730 SKIN BOEING727 7272Q9 138448MNM LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 L/WING T/E UPPER SURFACE CRACKED AT NR 4 SPOILER HINGE CUTOUT (NR3). REMOVED FASTENER AT L/WING T/E UPPER AT NR 4 SPOILER HINGE CUTOUT NR 3 IAW B727 SRM 51-30-2, STOP DRILL CRACK .250 TERMINATED AT END OF CRACK IAW B727 SRM 51-10-1. FABRICATED DOUBLER REPAIR, MAT USED 7075 T6 .071 PO 9001737 SIZE 5 3/4" BY 4 1/4" IAW B727 SRM 57-30-4 FIG 10, NDT AREA IAW B727 NDT M/M CD51-00-00 PART 6 FIG 23. NO DEFECTS NOTED, ALODINED AND PRIMED PART IAW B727 SRM 51-10-2. INSTALLED PARTS IAW B727 SRM 57-30-4 FIG 10. 2L73 4F RTA3WE 20050609001562005060900156NM 2005 6 9 DHL2005740563 120050327A5542 SKIN BOEING727 7272Q9 138448MNM RUDDER DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 VERT STAB ABOVE RT FIN STA 133 LOWER RUDDER SURF IS DENTED NEAR T/E. EVAULATED DENTED AREA AT VERT STAB ABOVE RT FIN STA 133 LOWER RUDDER SURF. TRIM OUT DAMAGED SKIN SIZE 1/2" BY 3/4" IAW B727 SRM 55-30-3 AND 51-10-1. FABRICATED DOUBLER REPAIR SIZE 2" BY 2.5" MAT USED 2024-T3 .032 PO 9002034 IAW B727 SRM 55-20-3 FIG 1. ALODINED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED DOUBLER REPAIR AT VERT STAB BELOW FIN STA 133 LOWER RUDDER SURFACE IAW B727 SRM 51-30-2 AND 55-20-3 FIG 1. 2L73 4F RTA3WE 20050609001572005060900157WP 2005 6 9 DHL2005801007 120050525A3297 ELEC CONNECTOR DOUG DC8 DC873F 302199FWP MLG DIRTY A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01801DH 46033 AFTER GEAR RETRACTION DURING CLIMB-OUT, RT DOOR UNSAFE LIGHT FLASHED INTERMITTENTLY STOPPED AFTER UPLATCH CHECK. CLEANED GEAR DOOR SWITCH/ELECTRICAL CONNECTOR. OPS CK'D PER MM DC8 MM 32-30-0 AND 32-31-0. NO DEFECTS NOTED ON GROUND AT THIS TIME. 2L74 4F RT4A25 20050609001582005060900158WP 2005 6 9 DHL2005801008 120050525A3260H202413 SWITCH DOUG DC8 DC873F 302199FWP MLG MALFUNCTIONED A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01801DH 46033 WHEN RETRACTING GEAR AFTER A MISSED APPROACH INTO MEX, RIGHT DOOR UNSAFE LIGHT ILLUMINATED WITH GEAR HANDLE UP. REMOVED AND REPLACED RT MAIN LANDING DOOR SWITCH IAW MM 32-31-5 CHECKED OPERATION OK SW P/N H20-2413. 2L74 4F RT4A25 20050609001612005060900161NM 2005 6 9 05FDEA00652 120050328A5512ALC8100XXX PANEL DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576F 48501 RIGHT HORIZONTAL STABILIZER UPPER BARREL NUT NR 06 HAS BORE CORROSION EXCEEDING LIMITS. BARREL NUT BORE NR 06 RIGHT REPAIRED IAW EA 1-5510-78133 ATTACHMENT 11, HORIZONTAL STABILIZER BARREL NUT BORE REWORK/ REPAIR AD 2003-22-08. MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050609001622005060900162NM 2005 6 9 05FDEA00653 120050328A5512ALC8100XXX PANEL DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576F 48501 RIGHT HORIZONTAL STABILIZER UPPER BARREL NUT NR 08 HAS BORE CORROSION EXCEEDING LIMITS. BARREL NUT BORE NR 08 RIGHT REPAIRED IAW EA 1-5510-78133 ATTACHMENT 12, HORIZONTAL STABILIZER BARREL NUT BORE REWORK/ REPAIR AD 2003-22-08. MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050609001662005060900166NM 2005 6 9 05FDEA00703 120050330A5512ALC8100XXX PANEL DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 LEFT HORIZONTAL STABILIZER UPPER BARREL NUT NR 25 HAS BORE CORROSION EXCEEDING LIMITS. BARREL NUT BORE NR 25 LT REPAIRED IAW EA 1-5510-78133 ATTACHMENT 5, HORIZONTAL STABILIZER BARREL NUT BORE REWORK/ REPAIR AD 2003-22-08. MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050609001702005060900170NM 2005 6 9 05FDEA00718 120050331A5512ALC8100XXX PANEL DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 RIGHT HORIZONTAL STABILIZER UPPER BARREL NUT NR 18 HAS BORE CORROSION EXCEEDING LIMITS. BARREL NUT BORE NR 18 RT REPAIRED IAW EA 1-5510-78133 ATTACHMENT 15, HORIZONTAL STABILIZER BARREL NUT BORE REWORK/ REPAIR AD 2003-22-08. MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050609001762005060900176NM 2005 6 9 05FDEA00773 120050331A5512ALC8100XXX PANEL DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 LEFT HORIZONTAL STABILIZER UPPER BARREL NUT NR 29 HAS BORE CORROSION EXCEEDING LIMITS. BARREL NUT BORE NR 29 LEFT REPAIRED IAW EA 1-5510-78133 ATTACHMENT 7, HORIZONTAL STABILIZER BARREL NUT BORE REWORK/ REPAIR AD 2003-22-08. MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050609001792005060900179NM 2005 6 9 05FDEA00776 120050331A5512ALC8100XXX PANEL DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 LT HORIZONTAL STABILIZER UPPER BARREL NUT NR 27 HAS BORE CORROSION EXCEEDING LIMITS. BARREL NUT BORE NR 27 LT REPAIRED IAW EA 1-5510-78133 ATTACHMENT 6, HORIZONTAL STABILIZER BARREL NUT BORE REWORK/ REPAIR AD 2003-22-08. MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050609001812005060900181NM 2005 6 9 05FDEA00799 120050402A5512ALC8100XXX PANEL DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 LT HORIZONTAL STABILIZER UPPER BARREL NUT NR 35 HAS BORE CORROSION EXCEEDING LIMITS. BARREL NUT BORE NR 35 LT REPAIRED IAW EA 1-5510-78133 ATTACHMENT 10, HORIZONTAL STABILIZER BARREL NUT BORE REWORK/ REPAIR AD 2003-22-08. MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050609001842005060900184NM 2005 6 9 05FDEA01445 120050524A5315 FLOORBEAM BOEING727 727200 138407ENM FUSLEAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 AFT CARGO, STA 1130 FLOORBEAM LWR CHORD CORRODED AT NUT CLIP LOCATIONS LBL 60 TO RBL 60 (C53-113-01, 2). *S/D* REPAIRED FLOORBEAM PER SRM 53-10-8. 2L73 4F RTA3WE 20050609001862005060900186 2005 6 9 KBM2005F00062 420050405A34225050010902 GYRO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE COCKPIT SPINNING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19115SH31 3141 D.G. SPINS IN FLIGHT. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050609001882005060900188EU 2005 6 9 KBM2005F00064 120050405A6420 HUB SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE TAIL ROTOR CUT E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19115SH 3141 T/R HUB HAS CUT AROUND THE RUBBER, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050609001902005060900190EU 2005 6 9 KBM2005F00066 120050512A212105008471 MOTOR SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE BLOWER FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P10 2347 BLOWER MOTOR CAUSES CIRCUIT BREAKER TO TRIP. REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20050609001922005060900192 2005 6 9 KBM2005F00068 420050516A3422103002201 GYRO SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE COCKPIT SPINNING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P28 2347 D.G. SPINS ON ITS OWN, RANDOMLY THROUGHOUT FLIGHT. REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20050609001962005060900196EU 2005 6 9 KBM2005F00074 120050515A21210500844 MOTOR SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE BLOWER FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH1128 2337 A/C BLOWS WARM AIR. REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20050609001972005060900197 2005 6 9 KBM2005F00075 420050323A34225050010902 GYRO SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE COCKPIT INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH595 2337 D.G. INOPERATIVE, SPINS IN FLIGHT. REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20050609001982005060900198EU 2005 6 9 KBM2005F00076 120050322A80000174078030 DRAIN VALVE SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1D1 NE STARTER LEAKING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV1589 3296 START DRAIN VALVE, UNIT HAS INTERNAL LEAK. REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20050609002022005060900202EU 2005 6 9 MALA050434 120050522A3030QR50V SENSOR SAAB SF340 340B 7860101EU PITOT HEAT FAILED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15442XJ 340B442 LT PITOT HEAT FAILED EN ROUTE TO TVC. RAN QRH PROBLEM REMAINED AFTER RESETTING CB. CB WAS NOT TRIPPED. DIVERTED TO CWA. REMOVED AND REPLACED LT PITOT HEAT AC CURRENT SENSOR, PN QR5OV PER SAAB AMM 30-32-05-2. OPS CHECK GOOD. 2L72 4T RTA52EU 20050609002032005060900203EU 2005 6 9 MALA050436 120050525A3213 STRUT BAC 146 AVRO146RJ85A1500097EU LT MLG DAMAGED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15521XJ E2346 AFTER TAKEOFF AT APPROX 100-200 FT RAD ALT THE FD AND AUTOTHROTTLES FAILED AND THE NO CAT 3 LAND ILLUMINATED ON THE FGS ADVISORY. THE LANDING GEAR SELECTOR COULD NOT BE MOVED FROM THE DOWN POSITION UNTIL APPROX 2 MIN AFTER LIFT OFF. THEN THEY WERE ABLE TO SELECT GEAR UP NORMALLY. RESELECTED FLIGHT DIRECTORS. THEY WORKED NORMALLY, HOWEVER AUTO THROTTLES REMAINED INOP. MAINTENANCE AND DISPATCH NOTIFIED AND RETURNED TO DTW. REMOVED AND REPLACED LEFT MLG SHOCK STRUT IAW MESABA JC 3210-503. SEE FOR DETAILS. ALL CHECKS GOOD. 2H74 4F RTA49EU 20050609002042005060900204EU 2005 6 9 KBM2005F00080 120050423A7931704A37642043 TRANSMITTER SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE OIL PRESS FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1937SH 437 2300 ENGINE OIL INDICATION AT -0-. REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20050609002052005060900205NE 2005 6 9 KBM2005F00081 220050503A7261703A53000001 OIL TANK SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1D NE CRACKED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1953SH 2009 OIL TANK, PORT NECK CRACKED. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050609002062005060900206SW 2005 6 9 KBM2005F00082 120050302A6210206010200133 BLADE BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL MAIN ROTOR DAMAGED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1973DP 887 2513 M/R BLADE, RE BLENDED DOUBLER. INSPECTED AND REPAIRED. (K) 1G71 3U3 U H2SW E4CE 20050609002072005060900207CE 2005 6 9 KBM2005F00083 120050402A62408DJ150WAD1 INDICATOR CESSNA501 501 2076603CE ALLSN 250C 250C20B 03013GL DUAL TACH FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19677JM1216 5010052 DUAL TACH, NEEDLE WILL NOT PROVIDE READING. REMOVED AND REPLACED. (K) 1L72 4F3 U A27CE E4CE 20050609002102005060900210WP 2005 6 9 AALA20050356 120050524A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217530 49922 SEA - EMERGENCY LIGHTS AT TAILCONE SLIDE L2 694 AND AFT EXIT L2 671 AND L2 615 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT TAIL CONE SLIDE AND AFT EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050609002112005060900211WP 2005 6 9 AALA20050357 120050525A3350 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT LOOSE A AALAK NONE O OTHER ININSP/MAINT 1 SW21451AA 49477 ORD - CEILING EMERGENCY LIGHTS AT ROWS 27 TO 30 INOPERATIVE. RESEATED BATTERIES IN PACK B5 107 FOR CEILING EMERGENCY LIGHTS AT ROWS 27 TO 30. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050609002122005060900212NM 2005 6 9 AALA20050358 120050525A3350 LIGHT BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21371AA 25198 SFO - WITH ALL POWER REMOVED FROM AIRCRAFT COCKPIT OVERHEAD EMERGENCY LIGHT ILLUMINATES. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY IN COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050609002142005060900214NM 2005 6 9 AALA20050353 120050524A3350 LIGHT BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21682AA 25339 MIA - EMERGENCY LIGHTS AT FORWARD SEAT 17D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHTS A FORWARD SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050610000012005061000001EU 2005 6 10 KBM2005F00089 120050514A2910704A34412034 LINE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE HYDRAULIC SYS LEAKING E KBMAO OTHER K FLUID LOSS NRNOT REPORTED 1 WP19966SH 3787 OIL LEAKING FROM HYDRAULIC LINE. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050610000022005061000002NM 2005 6 10 CALA0500164 120050525A5347143A531051 SEAT TRACK BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2724212 28772 INSPECTION FOUND LT O/B SEAT TRACK CORRODED BETWEEN BS 360 AND 380 CLOSET MOUNT TRACK, LBL 45.5. THE SEAT TRACK WAS REMOVED AND REPLACED IAW ECRA 5321-01226. 2L72 4F RTA16WE 20050610000032005061000003NM 2005 6 10 CALA0500165 120050525A5315147A55061 FLOORBEAM BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2724212 28772 INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, LBL 43 TO RBL 29. THE FLOORBEAM WAS REPAIRED IAW ECRA 5321-01222. 2L72 4F RTA16WE 20050610000052005061000005NM 2005 6 10 CALA0500168 120050516A5320141N516151 INTERCOSTAL BOEING757 757224 1384958NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717105 27295 INSPECTION FOUND GALLEY SUPPORT INTERCOSTAL CORRODED AT BS 365-377, RBL 60. THE INTERCOSTAL WAS REPLACED IAW SRM 51-40-02. 2L72 4F RTA2NM 20050610000062005061000006NM 2005 6 10 CALA0500169 120050520A5320143N54341 INTERCOSTAL BOEING757 757224 1384958NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717105 27295 INSPECTION FOUND INTERCOSTAL CORRODED BETWEEN BS 680 AND 700, RBL 56, WL 208.1. THE INTERCOSTAL WAS REPLACED IAW SRM 51-40-02. 2L72 4F RTA2NM 20050610000072005061000007NM 2005 6 10 CALA0500170 120050526A53106547959 DOOR FRAME BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714325 23455 INSPECTION FOUND THE AFT CARGO COMPARTMENT DOOR CUTOUT FORWARD FRAME CORRODED ON I/B SIDE AT STA 794, L26R TO L27R. THE CORRODED AREA WAS CUT OUT AND DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-70-11. 2L72 4F RTA16WE 20050610000082005061000008EU 2005 6 10 KBM2005F00090 120050409A24359560115450 MAGNETIC SEAL SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE STARTER GEN LEAKING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19966SH294 3787 STARTER GENERATOR MAG SEAL LEAKING. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050610000152005061000015EU 2005 6 10 MALA050437 120050413A5411 STRINGER BAC 146 AVRO146RJ85A1500097EU NOSE COWL CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15503XJ E2310 DURING C2 INSPECTION, FOUND 1 CRACKED STRINGER NR 2 ENGINE ON BULKHEAD AFT OF NOSE COWL. 2H74 4F RTA49EU 20050610000172005061000017CE 2005 6 10 DXTA200500752 120050602A324199123052 TRANSDUCER CESSNA500 560CESSNA 2076750CE ANITI SKID SYS INOPERATIVE E DXTAD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07371QS6225 5600471 DURING TAXI BOTH PEDALS ON RT SEAT BECAME SOFT, ANTI-SKID LIGHTS CAME ON. AFTER PUMPING THE PEDALS THE LIGHT WENT OUT, AND THE BRAKES FELT NORMAL. THIS HAPPENED THREE SEPERATE TIMES DURING TAXI. REPLACED LT ANTI-SKID TRANSDUCER AND BLED BRAKES. OPS CHECK GOOD IAW CESSNA 32-42-07 AND 32-42-00. 2L72 4F RTA22CE 20050610000182005061000018WP 2005 6 10 DXTA200500750 220050602A7314306071016 PUMP RAYTHNDH125 HAWKER800XP 7150012CE GARRTTTFE731TFE7315BR WP NR 2 ENG FUEL INOPERATIVE E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07867QS 258576 P107690 NR 2 ENGINE FUEL ANNUNCIATOR ILLUMINATED AT 40 KNOTS ON T/O STATIC POWER, ARMED APR AT BRAKE RELEASED, T/O ABORTED. REMOVED INOP FUEL PUMP & INSTALLED AN OVERHAULED UNIT AS REQUIRED, OPS & LEAK CHECK GOOD. ALL WORK PERFORMED IAW HONEYWELL TFE-731-5BR MM CHAPTER 73-20-01. 2L72 4F4 FRTA3EU E6WE 20050610000192005061000019NM 2005 6 10 05FDEA01507 120050601A5347A5A7082502 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 MAIN DECK CARGO, SEAT TRACK AT STA 5-0 TO STA 5-35, X = -9 FOUND CORRODED. MAIN DECK CARGO, SEAT TRACK AT STA 5-0 TO STA 1531, X = -9 REMOVED AND REPLACED AT EXISTING SPLICES PER SRM 53-70-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 2L73 4F RTA22WE 20050610000212005061000021NM 2005 6 10 05FDEA01506 120050601A5347A5A7082502 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 MAIN DECK CARGO, SEAT TRACK AT STA 5-93, X = -75 FOUND CORRODED. MAIN DECK CARGO, SEAT TRACK AT STA 5-0 TO STA 1531, X = -75 REMOVED AND REPLACED AT EXISTING SPLICES PER SRM 53-70-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2L73 4F RTA22WE 20050610000232005061000023NM 2005 6 10 CALA0500171 120050526A25308203110000A OVEN BOEING737 737524 1384721NM AFT GALLEY INOPERATIVE A CALAAH UNSCHED LANDING DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW271465419573 28915 THE FLIGHT ATTENDANTS REPORTED SMOKE IN THE AFT GALLEY AND AN ASSOCIATED ELECTRICAL ODOR WHILE EN ROUTE FROM IAH TO MSP. WHEN THE GALLEY POWER WAS TURNED OFF AND OVEN CIRCUIT BREAKERS WERE PULLED THE SMOKE BEGAN TO DISSIPATE. THE AIRCRAFT WAS DIVERTED TO OKC WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THAT THE NR 1 AFT GALLEY OVEN HAD FAILED INTERNALLY. THE OVEN WAS REMOVED AND REPLACED AND OPERATIONAL CHECKS WERE GOOD IAW MM 25-00-00. IN ADDITION, THE RECIRCULATION FAN FILTER WAS REMOVED AND REPLACED IAW MM 21-21-23. 2L72 4F RTA16WE 20050610000252005061000025NM 2005 6 10 CALA0500173 120050521A5320141A5410 INTERCOSTAL BOEING737 737824 13844BZNM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2724212 28772 INSPECTION FOUND A 3/4 INCH CRACK IN INTERCOSTAL AT STA 312-328, RBL 50. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-51, 51-20-01, AND 51-40-02. 2L72 4F RTA16WE 20050610000272005061000027NM 2005 6 10 CALA0500175 120050521A5320141A5410 INTERCOSTAL BOEING737 737824 13844BZNM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2724212 28772 INSPECTION FOUND A 3/4" CRACK IN INTERCOSTAL AT STA 312-328, LBL 38. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 53-10-51, 51-20-01, AND 51-40-02, 2L72 4F RTA16WE 20050610000292005061000029SO 2005 6 10 C2XA05CL029 120050428A33977287501643 WIRE HARNESS EMB 145 EMB145LR 3260212SO LIGHT BURNED A C2XAK NONE B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW2714960 145100 CLE FLIGHT NR 2249, THE CREW REPORTED AN UNIDENTIFIED BURNING ODOR AT THE REAR OF THE AIRCRAFT. MAINTENANCE INSPECTED THE CABIN AREA AND FOUND THE CENTER/LEFT CABIN LIGHT NOT ILLUMINATED AND THE LIGHT ASSEMBLY BURNED. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AND THE OPERATIONAL TESTS WERE GOOD WITH NO MORE BURNING SMELL. 2L72 4T RTT00011AT 20050610000332005061000033SO 2005 6 10 C2XA05BT032 120050527A33503025101 LIGHT EMB 145 EMB145LR 3260212SO FUSELAGE FAULTY A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713964 145123 BTV-CO2366, DURING 1A INSPECTION, MAINTENANCE FOUND THE RIGHT FORWARD WING EMERGENCY LIGHT TO BE NOT WORKING. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY IAW EMB145 AMM NR 33-50-10, OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050610000352005061000035EU 2005 6 10 DHL2005801012 220050606A72008063211 MEC DOUG DC8 DC873F 302199FWP CFMINTCFM56 CFM563C1 13802EU NR 1 ENGINE MALFUNCTIONED A DHLAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 SO01801DH 46033 AT FL.360. NR 1 ENGINE FLAMED OUT. NR 1 MAIN FUEL QUANTY GUAGE WAS SHOWING 2000 LBS. W/INTERMITTED FUEL SELECTED. THERE WAS NO MASTER CAUTION OR NR 1QT.LOW LIGHT. REPLACED NR 1 ENGINE MEC PER CFM 56 M/M CH. 73-21-10. OPS CHECKS NORMAL ON ENGINE RUN. FAULT 51 TREE COMPLETED PER CFM M/M 71-00-00. 2L74 4F4 FRT4A25 E21EU 20050610000382005061000038EU 2005 6 10 MALA050440 120050413A5411 STRINGER BAC 146 AVRO146RJ85A1500097EU NOSE COWL CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15503XJ E2310 DURING C2 INSPECTION, FOUND 1 CRACKED STRINGERS NR 2 ENGINE ON BULKHEAD AFT OF NOSE COWL. 2H74 4F RTA49EU 20050610000402005061000040EU 2005 6 10 MALA050443 120050413A5411 STRINGER BAC 146 AVRO146RJ85A1500097EU NOSE COWL CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15503XJ E2310 DURING C2 INSPECTION, FOUND 1 CRACKED STRINGER NR 2 ENGINE ON BULKHEAD AFT OF NOSE COWL. 2H74 4F RTA49EU 20050610000422005061000042EU 2005 6 10 MALA050445 120050413A5411 STRINGER BAC 146 AVRO146RJ85A1500097EU NOSE COWL CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15503XJ E2310 DURING C2 INSPECTION, FOUND 1 CRACKED STRINGER NR 2 ENGINE ON BULKHEAD AFT OF NOSE COWL. 2H74 4F RTA49EU 20050610000452005061000045NM 2005 6 10 AWXA200500612 120050504A532065479553 STRAP BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28322AW 25400 MCN - MAJOR REPAIR - DURING C-14 CHECK, CORROSION WAS FOUND ON INTERNAL DOUBLER IN THE AFT CARGO COMPARTMENT AT BS 847, BETWEEN STRINGERS 26 RT AND 27 RT. THE CORROSION WAS OUT OF LIMITS IAW B737-300 SRM 53-60-53-1, FIGURE 101. MAINTENANCE REPAIRED INTERNAL DOUBLER IN THE AFT CARGO COMPARTMENT AT BS 847, BETWEEN STRINGERS 26 RT AND 27 RT IAW AMERICA WEST AIRLINES ENGINEERING ORDER 03-5300-05145-SS1. 2L72 4F RTA16WE 20050610000492005061000049NE 2005 6 10 HSY2005F00003 220050204A7310AS3209009 O-RING CESSNA208 208B 2073701CE PWA PT6 PT6A114 52043NE FUEL SYSTEM FAILED E HSYAO OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM05903FE 208B0003 (MRR NR 01-020405) DURING DEPARTURE, PILOT NOTICED AN ENGINE POWER LOSS AND FLUCTUATION AND ABORTED THE TAKEOFF. AFTER REDUCING POWER, THE PILOT EXPERIENCED A STRONG FUEL SMELL IN THE COCKPIT. MAINTENANCE FOUND THAT THE NR 10 FUEL NOZZLE TRANSFER TUBE WAS LOOSE AND LEAKING FUEL. REPLACED ALL O-RINGS, FUEL NOZZLE GASKET AND RESCUED TRANSFER TUBE AND FUEL NOZZLE. (NM05200503118) (K) 1H71 3T3 T A37CE E4EA 20050610000542005061000054NM 2005 6 10 SWAA051498 120050523A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 520, STR 16R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050610000552005061000055NM 2005 6 10 SWAA051499 120050523A532269353656 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 360, STR 14R TO STR 15R. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050610000572005061000057NM 2005 6 10 SWAA051501 120050523A53206546833 WEB BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FLOOR WEB CRACKED AT BS 188 TO BS 196, LBL 30, WL 208. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050610000592005061000059NM 2005 6 10 SWAA051503 120050523A53156545410 FLOORBEAM BOEING737 7373H4 1384600NM CABIN FLOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29353SW 24889 DURING SCHEDULED 1/2D CHECK, FOUND NR 1 & NR 4 LONGITUDINAL FLOORBEAMS CRACKED AT BS 639. REPAIRED BEAMS PER SRM. 2L72 4F RTA16WE 20050610000612005061000061NM 2005 6 10 SWAA051505 120050523A53146545866 KEELBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29353SW 24889 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE KEEL BEAM CORRODED AT BS 500D TO BS 540, STR 28R. REPAIRED KEEL BEAM PER SRM. 2L72 4F RTA16WE 20050610000622005061000062NM 2005 6 10 SWAA051507 120050523A5754 SKIN BOEING737 7373H4 1384600NM LT WING SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29353SW 24889 DURING SCHEDULED 1/2D CHECK, FOUND LT WING NR 2 L/E SLAT DELAMINATED. REPAIRED SLAT PER SRM. 2L72 4F RTA16WE 20050610000642005061000064NM 2005 6 10 SWAA051509 120050523A3350207377 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29403WN 29815 EEPLS LENS MISSING AT FWD END. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20050613000032005061300003NM 2005 6 13 SWAA051537 120050524A534065C27314 STRINGER CLIP BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 500D, STR 3R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050613000042005061300004NM 2005 6 13 SWAA051539 120050524A53116546532 FRAME BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 9L & STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050613000072005061300007NM 2005 6 13 SWAA051542 120050524A53116546526 FRAME BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050613000092005061300009 2005 6 13 SWAA051513 420050522A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED A2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050613000112005061300011NM 2005 6 13 SWAA051516 120050524A531169353656 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 360, STR 14L TO STR 15L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050613000142005061300014NM 2005 6 13 SWAA051519 120050524A53116546559 FRAME BOEING737 7373H4 1384600NM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 927, RBL 7. REMOVED & REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20050613000152005061300015NM 2005 6 13 SWAA051520 120050524A3350101073 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 DURING SCHEDULED C4 CHECK, FOUND RT AFT OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2L72 4F RTA16WE 20050608000692005060800069NM 2005 6 8 GAIA05020OP 120050423A33501000679 LIGHT BOEING727 727223 1384074NM PWA JT8 JT8D9A 52048NE COCKPIT INOPERATIVE A GAIAK NONE O OTHER ININSP/MAINT 1 SW07854AA 20995 DURING PREFLIGHT, EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHTS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (K) 2L73 4F4 F A3WE E2EA 20050608000712005060800071NM 2005 6 8 SWAA051445 120050518A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 490, STR 26R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050608000732005060800073NM 2005 6 8 SWAA051447 120050518A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29322SW 23343 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 15R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050608000752005060800075NM 2005 6 8 SWAA051449 120050518A57536546435 SKIN BOEING737 7373H4 1384600NM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED SERVICE CHECK, FOUND LT WING T/E OUTBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM. 2L72 4F RTA16WE 20050608000802005060800080NM 2005 6 8 SWAA051454 120050519A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 706, STR 10R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050608000822005060800082NM 2005 6 8 SWAA051456 120050519A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND 2 EA FUSELAGE SHEAR TIES CORRODED AT BS 727C & BS 747, LBL 18. REPAIRED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20050608000842005060800084NM 2005 6 8 SWAA051458 120050519A53226936642 SHEAR TIE BOEING737 7373H4 1384600NM FWD BULKHEAD CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 178 BLKHD, RBL 31, WL 208. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050608000862005060800086NM 2005 6 8 SWAA051460 120050518A324426066712 TIRE BOEING737 7373H4 1384600NM RT MLG WHEEL SEPARATED A SWAAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SW29356SW 25251 DURING T/O, NR 4 MAIN TIRE TREAD SEPARATED. FOUND RT WING INBOARD AFT T/E FLAP, MIDFLAP, FOREFLAP & GROUND SPOILER DAMAGED. REMOVED AND REPLACED NR 4 MLG TIRE/WHEEL ASSY. MX FERRY TO PHX, RERMOVED AND REPLACED RT FOREFLAP, AFT FLAP & GROUND SPOILER ASSY PER MM. REPAIRED RT MIDFLAP PER SRM. 2L72 4F RTA16WE 20050608000942005060800094NE 2005 6 8 SWAA051468 220050519A7230737L334G02 BLADE BOEING737 7377H4 1384404NM GE CFM56 CFM567B24 NE NR 2 ENGINE TORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29737JW 27869 874162 DURING SCHEDULED HC2 CHECK, NR 2 ENGINE FAILED BOROSCOPE INSPECTION. SEVERAL NR 4 STAGE HPC BLADES TORN. REMOVED AND REPLACED NR 2 ENGINE PER MM. 2L72 4F4 FRTA16WE E00055EN 20050608000962005060800096EU 2005 6 8 DAT2005F00004 120050427A1430B3339 ATTACH BOLT STBROSSD3 SD330 8100602EU PWA PT6 PT6A45R 52043EA HARTZLHCB5M HCB5MP3 GL RT PROPELLER LOOSE E DATAO OTHER O OTHER NRNOT REPORTED 1 GL13938MA1957 SH3046 PS84063 EVA2127 DURING SCHEDULED MAINTENANCE OF COMPLYING WITH AD (PROP TORQUE) ON THE RT PROPELLER IN ACC`S HANGAR, (3) PROP ATTACH BOLTS WERE FOUND LOOSE, BUT NOT BROKEN. AD STATES WHEN LOOSE BOLTS ARE FOUND THE PROPELLER IS TO BE REMOVED AND INSPECTED, THE FLANGE MATING SURFACES. THE RT PROPELLER AND POWER SECTION WERE REMOVED DUE TO FRETTING BEYOND .0015 LIMITATIONS IAW THE AD. SERVICEABLE POWER SECTION WAS INSTALLED IAW THE MM. THEN AN OVERHAULED PROPELLER WAS INSTALLED IAW THE MM. OPS AND LEAK CHECK GOOD. AD WAS COMPLIED WITH IAW MFG SB AND NO DEFECTS FOUND AS WRITTEN UP ON ACC`S MDW. THE AD IS NEXT DUE AT 26280.2 TAT. AC WAS RETURNED TO SERVICE. (K) 2H72 4T4 T A41EU E4EA 6 CP44GL 20050608001202005060800120NM 2005 6 8 2005UALA00471 120050520A5340 STRINGER CLIP BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29313UA 23674 AFT PIT STA 727A STR 25L STR CLIP TO FRAME HAS A GAP. REMOVED AND REPLACED STR CLIP REF SRM 51-40-02. 2L72 4F4 FRTA16WE E21EU 20050608001222005060800122NM 2005 6 8 2005UALA00473 120050524A2120 ODOR BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE COCKPIT DETECTED A UALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP29370UA 24539 ACRID ELECTRICAL SMELL IN COCKPIT. NOT NOTED IN CABIN AND NO VISIBLE SMOKE. ELECTICAL SMELL IN FLIGHT DECK COULD ONLY BE SIMULATED WHEN TURNING ON WINDOW HEAT. REPLACED WINDOW HEAT SWITCH MODULE 69-37346-310 (MR30009). UNIT MR30009-9 WAS SENT TO SHOP 147. LEAD DANNY KEUNG HAD UNIT CHECKED BUT FOUND NOTHING WRONG WITH IT. 2L72 4F4 FRTA16WE E2GL 20050608001322005060800132EU 2005 6 8 2005UALA00482 120050526A2597 ELECTRICAL SYS AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE GALLEY UNKNOWN A UALAK NONE O OTHER ININSP/MAINT 1 WP29406UA 454 FLIGHT ATTENDANT SHOCKED WHILE HOLDING THE G1 AND G2 GALLEY COUNTER TOPS, DURING POWER TRANSFER FROM GROUND TO APU. INSPECTION AND VERIFICATION OF THE ELECTRICAL GROUNDING OF BOTH HOT GALLEY AND COLD GALLEY SECTIONS WERE ACCOMPLISHED IN ACCORDANCE WITH THE AMM 25-33-41. NO SIMILAR INCIDENT HAS BEEN REPORTED SINCE THE ACCOMPLISHMENT OF GROUNDING VERIFICATION. 2L72 4F4 FRTA28NM E40NE 20050621001272005062100127EU 2005 6 21 AWXA200500698 120050613A3350321454 POWER SUPPLY AIRBUS320 A320232 3930326EU EMERGENCY LIGHT INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28639AW5208434587 471 LAS - EEL - FLT 741 - IN LAS PILOT REPORTED LEFT EMERGENCY WING EXIT ON ECAM DOOR PAGE. MAINTENANCE REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY EXIT POWER SUPPLY UNIT 11WL, S/N 0485. OPERATIONAL CHECKS GOOD. 2L72 4F RTA28NM 20050608001382005060800138NE 2005 6 8 AALA20050343 220050519A7320 PUMP DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE NR 1 ENGINE INOPERATIVE A AALAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 SW21416AA 49327 725816 IAH - CLIMBING THROUGH FLIGHT LEVEL 270 LEFT NR 1 ENGINE SPOOLED DOWN AND LOST. NO OVERTEMP ON EXHAUST GAS TEMPERATURE AND N1 AND N2 WINDMILL INDICATION NORMAL. NR 1 FUEL FLOW ZERO. NO RESPONSE FROM THROTTLE MOVEMENT. REMOVED AND REPLACED LT ENGINE FUEL CONTROL AND FUEL PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 F A6WE E9NE 20050608001412005060800141WP 2005 6 8 AALA20050345 120050524A335040030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21287AA 49299 ORD - EMERGENCY EXIT LIGHTS ABOVE LEFT HAND AND RIGHT HAND FORWARD WING EXITS INOPERATIVE. REPLACED BATTERY PACK AT POSITION B5103 FOR EMERGENCY LIGHTS ABOVE OVERWING EXITS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050608001452005060800145NE 2005 6 8 ASMF200505021 220050521A732176960615 FCU DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE RT ENGINE FAILED W ASMFC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW23755RA9751 17 49727 725634 AIRCRAFT REJECTED TAKEOFF AS A CONSEQUENCE OF RIGHT ENGINE DID NOT ACCELERATE INCREASING TEMPERATURE TO 600 DEGREES AT STATIC TAKEOFF WITH 30 DEGREES AT ATMOSPHERE TEMPERATURE. AT PLATFORM, RIGHT ENGINE WAS STARTED GETTING 580 DEGREES AT 1.20 OF EPR. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE, RIGHT FCU AND FUEL PUMP FILTER WERE REPLACED IAW MM 73-20-01 AND 73-12-01 RESPECTIVELY. THE PT2 AND PT7 LEAK CHECK WAS PERFORMED IAW MM 77-11-01, ALL CORRECT. EGT SYSTEM INDICATION CHECK WAS PERFORMED IAW MM 77-21-04, ALL CORRECT. A 500 HOURS BOROSCOPIC INSPECTION WAS PERFORMED IAW MM 72-00-00, NOT DETECTING DAMAGES. 2L72 4F4 FRTA6WE E9NE 20050608001702005060800170EA 2005 6 8 A6WA200540173 120050515A3610 SHUTOFF VALVE CNDAIRCL600 CL6002B19 1900309EA BLEED AIR SYS FAULTY A A6WAA UNSCHED LANDING O OTHER CLCLIMB 1 GL31415AW 7593 L-PACK HIGH PRESS WHINE, XFERRED TO ENGINE BLEED. WHEN DUCT PRESS 60 PSI OR GREATER. REMOVED AND REPLACED L-PRSOV IAW AMM 2-151-43. FUNCTIONAL TEST OF PRSOV GOOD IAW AMM 21-51-43. (M) 2L72 4F RTA21EA 20050608001772005060800177EA 2005 6 8 A6WA200540171 120050417A5330 SKIN PANEL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DENTED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31457AW 7854 REPAIR DENT IN FUSELAGE SKIN AT FS 202.75 STRINGER 13R. REMOVED SKIN PANEL 601R33010-26 ON RT SIDE OF AIRCRAFT FS 202.75, STRINGER 13R, AND INSTALLED NEW SKIN PANEL 601R33010-26 IAW CRJ200FRM 51-42-06, 51-42-13, 51-42-21 AND CRJ 200 AMM 51-23-00 AND DRAWING 601R33010. (M) 2L72 4F RTA21EA 20050608001882005060800188EA 2005 6 8 A6WA200540175 120050517A5753 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE T/E FLAP DENTED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31452AW 7835 RT IB FLAP LOWER SKIN HAS A DENT 2 INCHES X 2.5 INCHES AND .077 INCH DEEP. DENT IS 24 INCHES FROM IB EDGE AND 2 INCHES FROM TRAILING EDGE. REPAIRED RT IB FLAP LOWER SKIN BY INSTALLING FLUSH REPAIR IAW BRAS EO. (K) 2L72 4F4 FRTA21EA E15NE 20050608001932005060800193EA 2005 6 8 A6WA200540168 120050504A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE LIGHTNING STRIKEA A6WAK NONE O OTHER ININSP/MAINT 1 GL31451AW 7832 PERMANENT REPAIR REQUIRED FOR LIGHTNING STRIKE DAMAGE AT FS 394, STRINGER 8L. REPAIRED LIGHTNING STRIKE DAMAGE IAW BRAS EO 601-R-53-6364A. (M) 2L72 4F RTA21EA 20050608001972005060800197NM 2005 6 8 HNAA0500049 120050524A533085330022011 SKIN PANEL DHAV DHC8 DHC8102 2809003NM FUSELAGE CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07943HA4181241812 167 A 6 INCH CRACK WAS FOUND IN FUSELAGE SKIN EMINATING FROM PRESSURIZATION DRAIN AFT. PERFORMING ULTRASOUND INSPECTION VERIFIED NUMEROUS AREAS OF DISBOND/CORROSION BETWEEN WAFFLE DOUBLER AND SKIN PANEL. DAMAGED AREA FROM X425 TO X445 STRINGER 30P TO 31S. REMOVED AND REPLACED SKIN PANEL. 2H72 4T RTA13NM 20050608001982005060800198NM 2005 6 8 HNAA0500048 120050524A533085310026013 SKIN PANEL DHAV DHC8 DHC8102 2809003NM FUSELAGE CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07943HA4181241812 167 SKIN PANEL DISBOND FOUND DURING C-CHECK INSPECTION. CORROSION BETWEEN WAFFLE DOUBLER AND SKIN PANEL. PANEL DISTORTED AROUND RIVET ROWS AND RIVETS FAILED (HEADS MISSING). VERIFIED DISBOND USING ULTRASOUND. DISBOND OF PANEL IS BETWEEN X123 AND X167, STR 32S AND 30P. REMOVE AND REPLACE ENTIRE SKIN PANEL. 2H72 4T RTA13NM 20050608002062005060800206WP 2005 6 8 UPS05844553 120050524A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE:C3 RIGHT O/B LEADING EDGE LWR RIB CRACKED AT XFS 660. STOP DRILLED CRACK, FABRICATED REPAIR ANGLE, AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-2-0 FIG 2, 51-1-20D, AND 51-1-21. 2L74 4F RT4A25 20050608002232005060800223WP 2005 6 8 UPS05844574 120050525A572057695891517 SPLICE DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE:C3 RIGHT WING CENTER L/E INTERNAL DOUBLER SPLICE CRACKED .5 INCH LONG AT XFS 42 9. REMOVED 2 EA CRACKED SPLICES, FABRICATED, AND INSTALLED 2 EA REPLACEMENT SPLICES IAW DC-8 SRM 51-1-20D, DWG 5769589-15 & -17. 2L74 4F RT4A25 20050609000042005060900004NM 2005 6 9 PIDA20050022 120050514A3350 BULB BOEING737 737317 138447PNM EMERGENCY LIGHT BURNED OUT A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05375PA 23812 LIGHT BURNED OUT AT RT EMERGENCY EXIT DOOR. REPLACED BULB, OPS NORMAL. 2L72 4F RTA16WE 20050609000052005060900005SO 2005 6 9 C2XA05SH037 120050517A532014530644401 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714938 145029 SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION ON I/B SIDE FROM FRAME 36 TO FRAME 38. REPAIRED LT OMEGA BEAM AT FRAME 38 IAW EMB 145 SRM 53-21-10, SECTION 2, FIGURE 201, SHEET 3 & EC 5320-01231 (ORIG). 2L72 4F RTT00011AT 20050609000222005060900022NM 2005 6 9 05FDEA01414 120050524A5315 FLOORBEAM DOUG MD11 MD11 3023602NM FUSELAGE DEFORMED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25631FE 48454 FWD CARGO COMPARTMENT, AT STA 6-10 FOUND FLOORBEAM DEFORM AS MARKED. REMOVED AS PER SRM 51-35-01 VOL II. NEW FLOORBEAM INSTALLED AS PER DWG AFA 0039 AND AS PER SRM 51-35-01 VOL II. MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050609000272005060900027NM 2005 6 9 05FDEA01418 120050524A5347 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25631FE 48454 MAIN DECK CABIN - AFT CABIN AT STA 1964 RBL 107 CURVED SEAT TRACK FOUND CORRODED AT LAVATORY TIE DOWN FITTING AREA AS MARKED. REPLACED FROM AFA 7789-542 AND CARRIED OUT REPAIR AS PER SRM 53-70-00 FIG1 VOL I. NEW SEAT TRACK AND REPAIR PARTS LOCATED AND INSTALLED AS PER SRM 53-70-00 FIG 1 VOL I AND SRM 51-31-01 VOL II. CLASSIFIED MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050706001182005070600118NM 2005 7 6 05FDEA01747 120050630A534760154924 SEAT TRACK BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25272FE 22037 SEAT TRACK STA 480 - 690 AT LBL 45 HAS CORROSION . REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2 2L73 4F RTA3WE 20050609000282005060900028NM 2005 6 9 05FDEA01420 120050524A5313 LONGERON DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25631FE 48454 CTR CARGO COMPT STA 1710 LONG 50 LT EXISTING LONGERON CRACKED SECTION REPLACED. LONGERON REPAIR AT CTR CARGO COMPT STA 1710 LONG 50 LT EVALUATED FOUND CARRIED OUT IAW SRM 53-10-00 FIG 1 AND FIG 2 VOL I. EO 1-5100-7-5001 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2L73 4F RTA22WE 20050706001192005070600119NM 2005 7 6 05FDEA01748 120050630A534760654924 SEAT TRACK BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25272FE 22037 SEAT TRACK LBL 24 IS CORRODED 690 - 740. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-30-2 2L73 4F RTA3WE 20050609000322005060900032NM 2005 6 9 C1HA200596008 120050421A5330 SKIN BOEING727 7272J4 1384006NM FUSELAGE BULGED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15696CA 22574 LOWER FUSELAGE BULGE IN SKIN FWD EDGE OF NOSE JACK PAD FOUND CORROSION ON THE INTERNAL DOUBLER. REMOVED AND REPLACED INTERNAL DOUBLER AT THE NOSE JACK PAD SRM 53-30-3 FIG 3. 2L73 4F RTA3WE 20050609000342005060900034NM 2005 6 9 C1HA200596010 120050506A5322 SHEAR TIE BOEING727 7272J4 1384006NM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15696CA 22574 STA 304 LOWER LT FRAME SHEAR TIE HAS CORROSION. REPAIRED SHEAR TIE PER SRM 53-10-4. 2L73 4F RTA3WE 20050609000352005060900035NM 2005 6 9 05FDEA00923 120050410A5512ALC8100XXX PANEL DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576F 48501 LT HORIZONTAL STABILIZER UPPER BARREL NUT NR 02 HAS BORE CORROSION EXCEEDING LIMITS. BARREL NUT BORE NR 02 LT REPAIRED IAW EA 1-5510-78133 ATTACHMENT 43, HORIZONTAL STABILIZER BARREL NUT BORE REWORK/ REPAIR AD 2003-22-08. MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050609000372005060900037EU 2005 6 9 F3LA200500018 220050422A7261 COVER BOEING737 7373L9 1384470NM CFMINTCFM56 CFM563B2 13802EU ENGINE MISSING A F3LAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 NM03313FL 26442 856183 AIR RETURN TO DEN, ON CLIMB-OUT, BOTH ENGINE OIL QUANTITY INDICATORS WENT TO ZERO. BOTH OIL PRESSURE INDICATORS WENT TO ZERO. BOTH LOW OIL PRESSURE LIGHTS ILLUMINATED. ENGINES OPERATED APPROXIMATELY 15 MINUTES IN THAT CONDITION UNTIL LANDING, WHICH WAS WITHOUT INCIDENT. BOTH ENGINE EGT'S, VIBRATION AND OIL TEMPS REMAINED NORMAL FOR DURATION OF ENGINE OPERATIONS. INSPECTED BOTH ENGINES AND DETERMINED OIL LOSS WAS DUE TO N2 GEARBOX ROTATION DRIVE ACCESS COVERS NOT INSTALLED ON EITHER ENGINE. BOTH ENGINES ARE IN THE PROCESS OF BEING REPLACED. ENGINE INFORMATION IS AS FOLLOWS: CFM56-3B2. NR 1 ENGINE, S/N 856183, 32111.70 HRS., 24091 CYC NR 2 ENGINE, S/N 857192, 32907.4 HRS., 24616 CYC. 2L72 4F4 FRTA16WE E21EU 20050609000452005060900045NM 2005 6 9 DHL2005740560 120050329A5311 FRAME BOEING727 7272Q9 138448MNM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 FRAME BS540 SHOW DENT BTW STR16R AND 17R PREVIOUS FRAME REPAIR. REMOVED PREVIOUS REPAIR AT FS FRAME BS 540 BTW 16R AND 17R IAW B727 SRM 51-30-2. FABRICATED NEW FRAME REPAIR MAT USED 7075 T6 .071 PO NR 9001737 DIMENSION 6" BY 5" IAW B727 SRM 53-10-2 FIG 3 AND 51-40-3 FIG 1. ALODINED AND PRIMED PART AND AREA IAW B727 SRM 51-10-2. INSTALLED ANGLE IAW B727 SRM 51 40-3 FIG 1. 2L73 4F RTA3WE 20050609000612005060900061SO 2005 6 9 SWIA200515028 120050521A3350 LIGHT EMB 120 EMB120ER 3260203SO EMERGENCY EXIT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07296SW 120325 EMERGENCY LIGHT ABOVE SEAT 9C NOT ILLUMINATED. RELAMPED EMERGENCY EXIT LIGHT ABOVE 9C. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050609000882005060900088EA 2005 6 9 COMA0560317 120050520A329717300263 WIRE HARNESS CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A COMAO OTHER J WARNING INDICATION CRCRUISE 1 SO01976CA 7151 FLIGHT 5134 GEAR DISAGREE WARNING. REPLACED THE NLG DOWNLOCK PROX SENSOR HARNESS. 2L72 4F RTA21EA 20050609000932005060900093NM 2005 6 9 SWAA051472 120050520A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND CORROSION ON FUSELAGE SHEAR TIE AT BS 827, RBL 4 & LBL 17. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050609000952005060900095NM 2005 6 9 SWAA051474 120050520A5313BAC1498155 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 500A, STR 16R. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20050609000992005060900099NM 2005 6 9 SWAA051478 120050520A53116516301 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 188, RT SIDE, WL 208. REPAIRED STUB FRAME PER SRM. 2L72 4F RTA16WE 20050609001022005060900102NM 2005 6 9 SWAA051481 120050520A53206545410 FLOOR SUPPORT BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 709, RBL 25. REPAIRED BEAMS PER BFG ER. 2L72 4F RTA16WE 20050609001042005060900104NM 2005 6 9 SWAA051483 120050520A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727B, STR 23R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050609001112005060900111NM 2005 6 9 SWAA051490 120050521A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29443WN 29838 FWD ENTRY EEPLS COVER BROKEN & LIGHT INOP. REMOVED AND REPLACED EEPLS PER MM. 2L72 4F RTA16WE 20050609001132005060900113NM 2005 6 9 SWAA051492 120050520A3350207377 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29475WN 32474 FWD END OF EEPLS LENS MISSING. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20050609001142005060900114NM 2005 6 9 SWAA051493 120050520A3350101114 BULB BOEING737 7375H4 138449DNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29512SW 24189 DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050609001212005060900121EA 2005 6 9 SWIA200515050 120050210A5347 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07590SW 7077 LT SIDE SEAT RAIL BETWEEN FS 409.00 + 16 - FS 409.00 + 112 IS CORRODED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED IAW CRJ SRM 51-40-11, 51-41-02, 51-41-04 AND 51-25-16. 2L72 4F RTA21EA 20050609001282005060900128EA 2005 6 9 SWIA200515057 120050223A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07956SW 7825 MAIN FUSELAGE; FLOORBEAM AT RBL 9.0 HAS OB ATTACH ANGLE CRACKED AT FS 280.00, ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-21-11, 51-25-16, 51-23-00. 2L72 4F RTA21EA 20050609001332005060900133NM 2005 6 9 AALA20050347 120050420A2530 OVEN BOEING767 767323 1385205NM GALLEY INOPERATIVE A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21349AN 33088 GLA INFLIGHT T0083/20APR FRA-ORD CREW REPORTED SMOKE COMING OUT FROM OVERHEAD AREA BY LT NR 1 DOOR IN FLIGHT. UTILITY BUSSES TURNED OFF AND SMOKE DISSIPATED. DIVERTED TO GLA AND OVERWEIGHT LANDING MADE WITHOUT INCIDENT. FOUND SMOKE SOURCE FROM OUTBOARD NUMBER ONE OVEN IN FORWARD GALLEY. FOUND SOURCE OF SMOKE FROM OUTBOARD NR 1 OVEN IN FORWARD GALLEY. PLACARDED OVEN AND COLLARED CIRCUIT BREAKER. INSPECTED FOR OVERWEIGHT LANDING. SYSTEM GROUND CHECKED NORMAL OPERATION. AT ORD REPLACED FIRST CLASS OVEN ELECTRICAL CONNECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA1NM 20050609001392005060900139EU 2005 6 9 AWXA200500594 120050522A3350321454 EPSU AIRBUS320 A320231 3930325EU EMERGENCY LIGHT FAULTY A AWXAK NONE O OTHER ININSP/MAINT 1 WP28646AW4174441744 271 PHX - EEL - DURING 8-DAY CHECK, A LT EMERGENCY POWER SUPPLY UNIT AND BATTERY PACK FAILED TEST. MAINTENANCE REMOVED AND REPLACED THE LT EMERGENCY POWER SUPPLY UNIT AND BATTERY PACK. OPERATIONAL CHECK WAS GOOD. BATTERY PACK INFORMATION: MANUFACTURER: DIEHL GMBH, PART NUMBER: 3214-30. 2L72 4F RTA28NM 20050609001412005060900141NM 2005 6 9 AWXA200500596 120050502A5330654577882 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28322AW 25400 DURING C-14 CHECK, A CRACK WAS DISCOVERED AT THE R-2 DOOR CUTOUT, FORWARD LOWER CORNER AT A FASTENER HOLE, BS 957, RT STRINGER 17. MAINTENANCE REPAIRED CRACK IAW B737-300 SRM 53-60-01-2 FIGURE 203. 2L72 4F RTA16WE 20050609001452005060900145NM 2005 6 9 AWXA200500600 120050503A5311651630086 FRAME BOEING737 7373G7 1384595NM BULKHEAD CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28322AW 25400 DURING C-14 CHECK, BS 178 BULKHEAD CHORD, LT SIDE AT WL 207, WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED BULKHEAD CHORD IAW B737-300 SRM 51-40-02-0 FIGURES 8 AND 12. 2L72 4F RTA16WE 20050609001492005060900149NM 2005 6 9 AWXA200500604 120050504A531565C3394225 FLOORBEAM BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28322AW 25400 DURING C-14 CHECK, CORROSION WAS FOUND ON TOP AND BOTTOM SECTIONS OF T-CAP LOCATED AT BS 328, WL 208, RT BL 23 TO BL 49. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW B737-300 SRM 53-10-51-1, FIGURE 101. MAINTENANCE REPAIRED T-CAP IAW B737-300 SRM 53-10-51-2, FIGURE 205. 2L72 4F RTA16WE 20050609001602005060900160EU 2005 6 9 KBM2005F00060 120050326A2400374GC01Y CONTROL BOX SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE GENERATOR INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1937SH 1527 2300 ECE BOX, INOPERATIVE, GENERATOR LIGHT WOULD NOT GO OUT DURING RUN-UP. REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20050609001652005060900165NM 2005 6 9 05FDEA00702 120050330A5512ALC8100XXX PANEL DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 LEFT HORIZONTAL STABILIZER UPPER BARREL NUT NR 1 HAS BORE CORROSION EXCEEDING LIMITS. BARREL NUT BORE NR 01 LT REPAIRED IAW EA 1-5510-78133 ATTACHMENT 01, HORIZONTAL STABILIZER BARREL NUT BORE REWORK/ REPAIR AD 2003-22-08. MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050609001672005060900167NM 2005 6 9 05FDEA00704 120050330A5512ALC8100XXX PANEL DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 LEFT HORIZONTAL STABILIZER UPPER BARREL NUT NR 23 HAS BORE CORROSION EXCEEDING LIMITS. BARREL NUT BORE NR 23 LT REPAIRED IAW EA 1-5510-78133 ATTACHMENT 4, HORIZONTAL STABILIZER BARREL NUT BORE REWORK/ REPAIR AD 2003-22-08. MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050609001682005060900168NM 2005 6 9 SB05064 120050526A3350BR9279109 LIGHT BOEING737 7373B7 1384580NM GE CFM56 CFM56* 13802NE FWD OF R1 DOOR INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19515AU 23701 MAINTENANCE FOUND THE INTERIOR EMERGENCY EXIT LIGHT ASSEMBLY, FORWARD OF THE FORWARD SERVICE DOOR, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EXIT LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA16WE E2GL 20050609001722005060900172NM 2005 6 9 05FDEA00720 120050331A5512ALC8100XXX PANEL DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 RIGHT HORIZONTAL STABILIZER UPPER BARREL NUT NR 12 HAS BORE CORROSION EXCEEDING LIMITS. BARREL NUT BORE NR 12 RT REPAIRED IAW EA 1-5510-78133 ATTACHMENT 13, HORIZONTAL STABILIZER BARREL NUT BORE REWORK/ REPAIR AD 2003-22-08. MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050609001732005060900173NM 2005 6 9 05FDEA00769 120050331A5512ALC8100XXX PANEL DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 RIGHT HORIZONTAL STABILIZER UPPER BARREL NUT NR 32 HAS BORE CORROSION EXCEEDING LIMITS. BARREL NUT BORE NR 32 RIGHT REPAIRED IAW EA 1-5510-78133 ATTACHMENT 21, HORIZONTAL STABILIZER BARREL NUT BORE REWORK/ REPAIR AD 2003-22-08. MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050609001742005060900174NM 2005 6 9 05FDEA00770 120050331A5512ALC8100XXX PANEL DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 RIGHT HORIZONTAL STABILIZER UPPER BARREL NUT NR 30 HAS BORE CORROSION EXCEEDING LIMITS. BARREL NUT BORE NR 30 RT REPAIRED IAW EA 1-5510-78133 ATTACHMENT 20, HORIZONTAL STABILIZER BARREL NUT BORE REWORK/ REPAIR AD 2003-22-08. MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050609001802005060900180WP 2005 6 9 P9RA20040084 120050521A3260833703 PROXIMITY SENSOR DOUG DC9 DC983 3022083WP MLG DOOR OUT OF ADJUST A P9RAO OTHER N FALSE WARNING CLCLIMB 1 SO11989PG 49845 GEAR DOOR OPEN LIGHT ILLUMINATED ON CLIMB-OUT AND CRUISE WITH HYDRAULIC PUMP LOW. EXTINGUISHED WITH PUMP HIGH. AIRCRAFT FERRIED FOR MAINTENANCE PURPOSES. TROUBLESHOT AND FOUND LT AND RT MAIN LANDING GEAR DOOR SENSORS OUT OF ADJUSTMENT. SHIMMED SENSORS TO MINIMUM CLEARANCE IAW MM. DOOR INDICATION CHECKED GOOD. 2L72 4F RTA6WE 20050609001822005060900182NM 2005 6 9 05FDEA00931 120050411A5512ALC8100XXX PANEL DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 RIGHT HORIZONTAL STABILIZER UPPER BARREL NUT NR 33 HAS BORE CORROSION EXCEEDING LIMITS. BARREL NUT BORE NR 33 RT REPAIRED IAW EA 1-5510-78133 ATTACHMENT 33, HORIZONTAL STABILIZER BARREL NUT BORE REWORK/ REPAIR AD 2003-22-08. MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050609001832005060900183 2005 6 9 KBM2005F00061 420050330A3422103002301 GYRO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE COCKPIT TUMBLES E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19115SH 3141 D. G. TUMBLES IN FLIGHT. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050609001892005060900189EU 2005 6 9 KBM2005F00065 120050515A21210500844 MOTOR SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE BLOWER FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P14 2347 A/C BLOWS HOT AIR, CIRCUIT BREAKER POPS AFTER 5 MINUTES. REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20050609002092005060900209EU 2005 6 9 KBM2005F00087 120050511A5620 RAIL SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE WINDOW CRACKED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH 1115093 2884 LT SLIDING DOOR WINDOW (STORM WINDOW) RAIL CRACKED. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050609002132005060900213NM 2005 6 9 AALA20050354 120050517A3350D71701100 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21968AN 30095 TUL - BATTERY PACKS FOR EMERGENCY LIGHTS IN CABIN FAILED TEST PER CARD 2311. REPLACED BATTERY PACKS FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20050610000122005061000012 2005 6 10 HSY2005F00000 420050315A3446066031140000 INDICATOR CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE RADAR UNSERVICEABLE E HSYAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 NM05766FE 208B0260 AIR RETURNED, DUE TO PILOT EXPERIENCING SMOKE IN THE COCKPIT. PILOT NOTICED THE RADAR INDICATOR BLINKING OFF AND ON. MAINT CONFIRMED THAT THE SMOKE WAS COMING FROM THE RADAR INDICATOR. THE RADAR SYSTEM WAS DEFERRED AND IT WAS CONFIRMED THAT NO POWER WAS TO THE SYSTEM. PARTS ORDERED. (K) 1H71 3T3 T A37CE E4EA 20050610000142005061000014EU 2005 6 10 MALA050441 120050413A5411 STRINGER BAC 146 AVRO146RJ85A1500097EU NOSE COWL CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15503XJ E2310 DURING C2 INSPECTION, FOUND 1 CRACKED STRINGER NR 2 ENGINE ON BULKHEAD AFT OF NOSE COWL. 2H74 4F RTA49EU 20050610000242005061000024NM 2005 6 10 CALA0500172 120050512A5320141A5410 INTERCOSTAL BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2726210 28770 INSPECTION FOUND INTERCOSTAL CORRODED AT STA 947-967, RBL 50, I/B OF R-2 DOOR FRAME. THE INTERCOSTAL WAS REPAIRED IAW ECRA 5321-01218. 2L72 4F RTA16WE 20050610000262005061000026NM 2005 6 10 CALA0500174 120050521A5320141A54103 INTERCOSTAL BOEING737 737824 13844BZNM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2724212 28772 INSPECTION FOUND A 1/2 INCH CRACK IN INTERCOSTAL AT STA 270-294, LBL 50. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-51, 51-20-01, AND 51-40-02. 2L72 4F RTA16WE 20050610000322005061000032SO 2005 6 10 C2XA05RI008 120050525A3230 LANDING GEAR EMB 145 EMB145ER 3260211SO MAINS MALFUNCTIONED A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2715926 145005 AFTER TAKEOFF, THE CREW REPORTED THAT THE NOSE LANDING GEAR WOULD NOT RETRACT AND A LANDING GEAR DISAGREE MESSAGE ILLUMINATED. THE AIRCRAFT RETURNED TO IAD AND LANDED WITHOUT INCIDENT. THE AIRCRAFT FERRIED TO RIC WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND PERFORMED MULTIPLE LANDING GEAR EXTENSION AND RETRACTION OPERATIONAL CHECKS. THE LANDING GEAR OPERATIONALLY CHECKED GOOD WITHOUT ANY FAULTS BEING NOTED AND THE AIRCRAFT WAS RETURNED TO SERVICE. AIRCRAFT HOURS 16863 CYCLES 15207. 2L72 4F RTT00011AT 20050610000342005061000034 2005 6 10 P9RA20050085 420050528A2565767 BULB BOEING757 757236 1384971NM R2 R4 DOOR SLIDEINOPERATIVE A P9RAO OTHER O OTHER NRNOT REPORTED 1 SO11521NA 25592 JFK - R2 AND R4 DOOR SLIDES WILL NOT INDICATE ARMED. RELAMPED SLIDE ARM INDICATORS IAW M/M. 2L72 4F RTA2NM 20050610000522005061000052GL 2005 6 10 ALG2005F00027 220050506A732323076061 GOVERNOR BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL ENGINE MALFUNCTIONED E ALGAO OTHER J WARNING INDICATION APAPPROACH 1 SW03117AL24 24 2391 CAE800139FA ON SHORT FINAL TO AIRLOG FLYWAY, POWER WAS REDUCED FOR LANDING, AC YAWED RT WITH INCREASE IN ENGINE NOISE, COLLECTIVE WAS INCREASE AND THROTTLE WAS REDUCED TO CONTROL ENGINE SPEED. ACCOMPLISHED A GO-AROUND AND LANDED USING MANUAL THROTTLE CONTROL, MAX N2 AND N1 WAS 110 PERCENT FOR LESS THAN A SECOND. MAINTENANCE REPLACED GOVERNOR, FUEL CONTROL AND FUEL PUMP IAW MAINTENANCE CONTROL, COMPLIED WITH A 30 MINUTE GROUND RUN OF AC AND NO DEFECTS NOTED. COMPLIED WITH AN OVERSPEED INSPECTION OF THE AIRFRAME AND ENGINE ALSO DO DEFECTS NOTED. DID CONTINUITY CHECK OF FUEL CONTROL AND GOVERNOR SYSTEMS, NO DEFECTS FOUND. ALL WORK DONE IAW MFG MM AND ENGINE MFG MM. (K) 1G71 3U3 U H2SW E4CE 20050613000052005061300005NM 2005 6 13 SWAA051540 120050524A531165C22909 FRAME BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050613000062005061300006NM 2005 6 13 SWAA051541 120050524A53116546529 FRAME BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050613000102005061300010NM 2005 6 13 SWAA051514 120050524A53116546541 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 3L TO STR 3R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050613000162005061300016NM 2005 6 13 SWAA051521 120050524A53306545777 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29344SW 24152 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947.5, STR 24R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050613000172005061300017NM 2005 6 13 SWAA051522 120050524A53216546833 WEB BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED SPECIAL VISIT, FOUND 2 EA FUSELAGE FLOOR WEB CRACKS BETWEEN BS 188 TO BS 196, LBL 30 & RBL 30, WL 208. REPAIRED WEB SECTIONS PER SRM. 2L72 4F RTA16WE 20050613000182005061300018NM 2005 6 13 SWAA051523 120050524A53126516300 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE BULKHEAD WEB CRACKED AT BS 178, LBL 25, WL 207. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050613000192005061300019 2005 6 13 SWAA051524 420050524A256565659723 PLATE BOEING737 7373H4 1384600NM GIRT BAR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29353SW 24889 DURING SCHEDULED 1/2D CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR ATTACH FWD PLATE CORRODED. REMOVED AND REPLACED GIRT BAR PLATE PER SRM. 2L72 4F RTA16WE 20050613000202005061300020NM 2005 6 13 SWAA051525 120050524A53206545410 FLOOR SUPPORT BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29353SW 24889 DURING SCHEDULED 1/2D CHECK, FOUND LONGITUDINAL FLOOR SUPPORT CRACKED AT BS 664, BL 0. REPAIRED SUPPORT PER SWA EA. 2L72 4F RTA16WE 20050613000222005061300022NM 2005 6 13 SWAA051527 120050524A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29353SW 24889 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050613000242005061300024NM 2005 6 13 SWAA051529 120050524A53206545410 FLOOR SUPPORT BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29353SW 24889 DURING SCHEDULED 1/2D CHECK, FOUND LONGITUDINAL FLOOR SUPPORT CRACKED AT BS 665-673. REPAIRED SUPPORT PER SWA EA. 2L72 4F RTA16WE 20050613000272005061300027NM 2005 6 13 SWAA051532 120050524A53306545765 SKIN BOEING737 7373L9 1384470NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29658SW 23332 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 500D + 3, STR 12R. REPAIRED SKIN PER BFG ER. 2L72 4F RTA16WE 20050613000282005061300028NM 2005 6 13 SWAA051533 120050524A53206546529 SHEAR TIE BOEING737 737301 1384611NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500C, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050613000312005061300031NM 2005 6 13 SWAA051544 120050525A53306545800 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29524SW 26566 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 258, STR 19L TO STR 22L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050613000322005061300032NM 2005 6 13 SWAA051545 120050525A55236959227 BUSHING BOEING737 7373H4 1384600NM RT ELEVATOR TAB WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29626SW 27702 DURING SCHEDULED C3 CHECK, RT ELEVATOR TAB FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED NR 1 HINGE BUSHING & HARDWARE PER MM. 2L72 4F RTA16WE 20050613000342005061300034NM 2005 6 13 SWAA051551 120050525A53226546538 SHEAR TIE BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 616, STR 7R TO STR 8R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050613000382005061300038NM 2005 6 13 SWAA051555 120050525A531165C25228 FRAME BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727C, STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050613000402005061300040NM 2005 6 13 SWAA051557 120050525A53116546594 FRAME BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727E, STR 23R TO STR 24R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050613000412005061300041NM 2005 6 13 SWAA051558 120050525A534065C27314 STRINGER CLIP BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727E, STR 22R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050613000432005061300043NM 2005 6 13 PCSA0518051 120050518A2916 COVER BOEING727 727233 138408ANM PWA JT8 JT8D17 52049NE FILTER LEAKING A PCSAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO29395AJ 21100 DURING CLIMB CREW REPORTED LOSS OF HYDRAULIC (A) SYSTEM. AIRCRAFT WAS DIVERTED AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND FEEL COMPUTER FILTER COVER LEAKING HYDRAULIC FLUID. REMOVED AND REPLACED FEEL COMPUTER FILTER CAP AND O-RING IAW MM CH 20-10-11, SERVICED HYDRAULIC SYSTEM IAW MM CH 12-12-0, NO LEAKS NOTED. REMOVED A & B CASE DRAIN FILTERS, INSPECTED FOR CONTAMINATION AND REPLACED FILTERS IAW MM. NO CONTAMINATION NOTED. CYCLED FLAPS AND FLIGHT CONTROLS, PRESSURIZED HYDRAULIC SYSTEM AND LEAKED CHECK GOOD, AND RECHECKED HYDRAULIC QTY. HYDRAULIC SYSTEM PRESSURE CHECKED AND LEAK CHECK NORMAL IAW MM CH-29-11-41 AND 29-12-21. AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 FRTA3WE E2EA 20050613000472005061300047SW 2005 6 13 ALG2005F00029 120050429A7712222375077119 TRANSDUCER BELL 407 407 1182206SW ALLSN 250C 250C47B GL TORQUE PRESSURE FLUCTUATES E ALGAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW03405AL 53480 CAE847257 ON TAKE OFF THE TORQUE GAUGE FLUCTUATED 60 PERCENT TO 70 PERCENT, RETURNED TO BASE AND REPORTED THE MALFUNCTION TO MAINTENANCE. MAINTENANCE CHANGED THE TORQUE PRESSURE TRANSDUCER AND OPS CHECK WAS GOOD, WORK DONE IAW MM. (K) 1G71 3U3 UO H2SW E1GL 20050613000502005061300050WP 2005 6 13 DHL200580110 120050527A3297 WIRE DOUG DC8 DC873F 302199FWP MLG DOOR IND LOOSE A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01801DH 46033 DOOR NOT LATCHED LIGHT VERY SLOW TO GO OUT AFTER GEAR RETRACTION DOOR NOT LATCHED LIGHT BRIEFLY ILLUMINATED WHEN FLAPS REACHED UP POSITION NORMAL GEAR UPLATCH CHECK NO LIGHTS ON S/O PANEL. INSPECTED TERMINAL ENDS AND FOUND LOOSE CONNECTIONS AT TERMINAL STRIP REMOVED AND REPLACED TERMINAL CONNECTORS AND RESECURED IAW 20-50-1, PERFORMED OPS CHECK. OPS CHECK NORMAL IAW 32-31-1. 2L74 4F RT4A25 20050613000512005061300051NM 2005 6 13 05FDEA00721 120050331A5313AEA0435U503 LONGERON DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 MAIN DECK, AT STA 1219 LT FRAME TO FLOORBEAM INTERSECTION AT LONGERON 27 LEFT FOUND CRACKED. MAIN DECK, DISCREPANT LONGERON AT STA 1219 LT L-27 REMOVED AND REPLACED WITH NEW LONGERON: AEA 0435U503. NEW LONGERON LOCATED AND INSTALLED AS PER DRAWING AEA7605. MAJOR REPAIR AS PER GMM6-2-100. 2L73 4F RTA22WE 20050613000542005061300054NM 2005 6 13 05FDEA01466 120050525A5330 SKIN DOUG MD11 MD11 3023602NM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25631FE 48454 FWD FUSELAGE STA 999 LONG 40/42 RT NEW DOUBLER INSTALLED. REPAIRED AS PER SRM 53-50- 00 VOL I, FIG 6. MINOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050613000552005061300055NM 2005 6 13 05FDEA01467 120050525A5310 DOOR FRAME DOUG MD11 MD11 3023602NM CARGO BAY DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25631FE 48454 AT DOOR JAMB AFT CARGO DOOR STA 1959 LOWER EXISTING DENT/SCRATCH BLEND OUT. REPAIRED AS PER SRM 53-00-00, VOL I FIG 16 (SHT 9). MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050613000562005061300056EA 2005 6 13 VTZA200500083 120050526A5320601R3117117 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27659BR 7509 INTERCOSTAL CRACKED AT .25 INCH IN LENGTH ON LT INBOARD SIDE AT FS 484 LEFT BETWEEN BL 27.00. 2L72 4F RTA21EA 20050613000582005061300058EA 2005 6 13 VTZA200500085 120050526A5320601R311719 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27659BR 7509 INTERCOSTAL CRACKED AT .250 INCH IN LENGTH ON RT SIDE AT FS 484 BL 36.00. 2L72 4F RTA21EA 20050613000592005061300059EA 2005 6 13 VTZA200500086 120050526A5320601R311719 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27659BR 7509 INTERCOSTAL CRACKED AT .250 IN LENGTH ON RT OUTBD SIDE AT FS 484 LEFT BETWEEN BL 36.00. 2L72 4F RTA21EA 20050613000602005061300060EA 2005 6 13 VTZA200500087 120050526A5340601R3501163 PLATE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27659BR 7509 CARGO LANDING PLATE IS CRACKED AT RIVETS ATTACHING IT TO THE INTERCOSTALS .250 INCH. 2L72 4F RTA21EA 20050613000612005061300061EA 2005 6 13 VTZA200500088 120050526A5712601R107091 RIB CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27659BR 7509 LT BATT RIB IS CRACKED 1.5 INCH. 2L72 4F RTA21EA 20050613000642005061300064NM 2005 6 13 QXEA200500956 120050526A7931AP7761000100DW TRANSMITTER DHAV DHC8 DHC8202 2809007NM OIL PRESSURE INOPERATIVE A QXEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM09379PH103897301 530 BOI - FLIGHT 2204 - THE NR 2 OIL PSI GAUGE WAS FLUCTUATING RANDOMLY TO 15 PSI. ALL OTHER INDICATIONS NORMAL. THE AIRCRAFT RETURNED TO FIELD. MAINTENANCE REPLACED THE NR 2 ENGINE OIL PRESSURE TRANSMITTER AND RESHIMMED NR 2 OIL PRESSURE REGULATOR IAW P&W MM 72-00 PG 503. OPS CHECKS NORMAL. NO LEAKS NOTED. A/C OK FOR SERVICE. 2H72 4T RTA13NM 20050613000652005061300065NM 2005 6 13 UPS05644512 120050526A2560MXP21000 SMOKE GOGGLES BOEING767 76734AF 1385212NM COCKPIT DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01308UP 27761 SMOKE GOGGLES IN CENTER ACM (AFT) DOES NOT ADJUST, STRAP OVER STRETCHED, (05 SUPERNUMERARY POSITION). REPLACED CENTER ACM SMOKE GOGGLES PER IPC 25-64-57. 2L72 4F RTA1NM 20050613000662005061300066NM 2005 6 13 DL76P050290 120050523A2150211080107 ACM BOEING767 767332 1382001NM RIGHT FAILED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27143DA 25991 ACFT DIVERTED DUE TO SMOKE IN CABIN . RAN ENG USED BLEED AIR FOUND RT PACK TEMP OUT 200 DEG. REPLACED RIGHT ACM. 2L72 4F RTA1NM 20050613000682005061300068NM 2005 6 13 DLM88050293 120050526A2560MV10 MEGAPHONE DOUG MD88 MD88 3023688NM CABIN INOPERATIVE A DALAK NONE O OTHER ININSP/MAINT 1 SO27964DL 49983 AFT CABIN MEGAPHONE INOPERATIVE. REPLACED MEGAPHONE. 2L72 4F RTA6WE 20050613000702005061300070NM 2005 6 13 AWXA200500615 120050526A2613 WARNING LIGHT BOEING737 73733A 1384673NM ENG OVERTEMP ILLUMINATED A AWXAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 WP28173AW 23632 ON TAKEOFF ROLL AT LAS EN ROUTE TO SJC AT APPROXIMATELY 80-100 KTS. PILOT REPORTED AN ENGINE OVERTEMP. MX COMPLIED WITH POWER ASSURANCE TEST IAW AWA TASK CARD F5M71003 AND POWER ASSURANCE CHECK TEST 5 AND TROUBLESHOOTING CHART 71-00-42-1 STEPS 1, 2, 3 AND 25 WITH NO FAULTS FOUND. MX PERFORMED AN ELECTRICAL CHECK OF THE EGT HARNESSES, NO FAULTS FOUND. MAINTENANCE CONFIRMED EGT TEMPERATURES FOR BOTH ENGINES WERE WITHIN LIMITS DURING 5 MINUTE POWER RUNS. AIRCRAFT WAS RELEASED TO SERVICE. 2L72 4F RTA16WE 20050613000732005061300073EU 2005 6 13 MALA050451 120050525A5347 SEAT TRACK BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15506XJ E2314 DURING C2 INSPECTION, FOUND LEFT INBOARD FORWARD SEAT RAIL CORRODED NEAR FRAME 18. 2H74 4F RTA49EU 20050613000742005061300074EU 2005 6 13 MALA050453 120050525A5347 SEAT TRACK BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15506XJ E2314 DURING C2 INSPECTION, FOUND RIGHT OUTBOARD SEAT RAIL CORRODED NEAR FRAME 18. 2H74 4F RTA49EU 20050613000792005061300079EU 2005 6 13 MALA050446 120050525A5347 SEAT TRACK BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15506XJ E2314 DURING C2 INSPECTION, FOUND RIGHT INBOARD SEAT RAIL CORRODED NEAR FRAME 18. 2H74 4F RTA49EU 20050613000802005061300080EU 2005 6 13 MALA050447 120050525A5320 GUSSET BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15506XJ E2314 DURING C2 INSPECTION, FOUND GUSSET PLATE AT FRAME 18 LBL 22 CORRODED. 2H74 4F RTA49EU 20050613000812005061300081EU 2005 6 13 MALA050448 120050525A5320 GUSSET BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15506XJ E2314 DURING C2 INSPECTION, FOUND GUSSET PLATE AT FRAME 43 LBL6 CORRODED. 2H74 4F RTA49EU 20050613000822005061300082EU 2005 6 13 MALA050457 120050525A5320 GUSSET BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15506XJ E2314 DURING C2 INSPECTION, FOUND GUSSET PLATE AT FRAME 20 RT BETWEEN INBOARD AND OUTBOARD SEAT RAILS CORRODED. 2H74 4F RTA49EU 20050613000892005061300089WP 2005 6 13 AALA20050359 120050527A3350 CONNECTOR HONEYWELL DOUG DC9 DC982 3022082WP BATTERY PACK LOOSE A AALAK NONE O OTHER ININSP/MAINT 1 SW21295AA 49307 SFO - RIGHT NR 1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. FOUND BATTERY PACK CONNECTOR LOOSE. RESECURED CONNECTOR FOR BATTERY PACK FOR RIGHT NR 1 DOOR EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050613000902005061300090NM 2005 6 13 AALA20050360 120050524A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21937AN 29532 TUL - EMERGENCY LIGHTS IN FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20050613000952005061300095WP 2005 6 13 IXXA05SMN02S 120050427A5340 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX 45993 DURING ROUTINE C-CHECK INSPECTION, FWD CARGO COMPT INTERIOR. SPLICE FITTING CRACKED, STA 600.00 - STA 620.000, L-31R. REMOVED CRACKED FITTING IAW DC-8 SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING (ALCLAD 7075 T6 51) IAW DWG 3750257. PERFORMED NDT INSPECTION TO FITTING IAW NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED AREA + NEW FITTING IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11 PAGE 9. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D PAGE 9. TORQUED IAW DC-8 SRM 51-3-1. 2L74 4F RT4A25 20050613000992005061300099SO 2005 6 13 RAIA00505019 120050520A324631551 WHEEL EMB 145 EMB145 3260210SO NLG OUT OF ROUND A RAIAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 CE03801HK 145053 FLT 3518 - STL - NOSE WHEEL VIBRATION. MAINTENANCE REMOVED AND REPLACED NOSE WHEEL ASSEMBLIES. 2L72 4F RTT00011AT 20050613001002005061300100SO 2005 6 13 RAIA00505020 120050521A3234 SWITCH EMB 145 EMB145LR 3260212SO MLG CORRODED A RAIAA UNSCHED LANDING O OTHER CRCRUISE 1 CE03822HK 145069 FLT - LIT - LANDING GEAR LEVER WOULD NOT MOVE TO THE UP POSITION. MAINTENANCE CLEANED ALL AOG SWITCHES AND OPS CHECKED OK. 2L72 4T RTT00011AT 20050613001012005061300101SO 2005 6 13 RAIA00505021 120050522A801135059106 STARTER EMB 145 EMB145LR 3260212SO LT ENGINE INOPERATIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03819HK5297 1439 145062 FLT 5505 - JAX - LEFT ENGINE WILL NOT START. MAINTENANCE REMOVED AND REPLACED AIR TURBINE STARTER. 2L72 4T RTT00011AT 20050613001022005061300102 2005 6 13 RAIA00505022 420050524A34207003360948 AHRS JETAIRJETSTMJETSTM4101 1500501EU NR 2 INOPERATIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03564HK3729 41081 FLT 5464 - STL - FO'S AHRS FAILED. MAINTENANCE REMOVED AND REPLACED NR 2 AHRU. 2L72 4T RTA41NM 20050613001032005061300103SO 2005 6 13 RAIA00505023 120050525A801232153581 CONTROL VALVE EMB 145 EMB145LR 3260212SO STARTER STUCK A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03847HK150451561 14500857 FLT 7998 - RDU - LEFT START VALVE SHOWS OPEN. MAINTENANCE REMOVED AND REPLACED STARTER CONTROL VALVE. 2L72 4T RTT00011AT 20050613001052005061300105NM 2005 6 13 HNAA0500046 120050526A7931APT761000100DW TRANSMITTER DHAV DHC8 DHC8102 2809003NM PWA PW120 PW123 NE ENG OIL PRESSUREFALSE INDICATIONA HNAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA07333EN2771127711 134 NR 2 ENGINE OIL PRESSURE WENT TO ZERO PSI AND THEN WENT TO 40 PSI WITH NO OIL PRESSURE LIGHT AFTER TAKEOFF. REMOVED AND REPLACED THE NR 2 ENGINE OIL PRESSURE TRANSMITTER. 2H72 4T4 TRTA13NM E20NE 20050613001082005061300108NM 2005 6 13 SWAA051562 120050526A32341030875 SOLENOID BOEING737 7373H4 1384600NM MLG HANDLE FAULTY A SWAAA UNSCHED LANDING O OTHER CLCLIMB 1 SW29635SW 27708 AIR TURNBACK, LANDING GEAR HANDLE WOULD NOT RAISE PAST OFF POSITION. CYCLED LANDING GEARS AND SAME PROBLEM. USED GEAR LEVER OVERRIDE TRIGGER TO RAISE GEARS. REMOVED AND REPLACED LANDING GEAR HANDLE LOCK OUT SOLENOID PER MM. 2L72 4F RTA16WE 20050613001102005061300110NM 2005 6 13 SWAA051564 120050526A3350101114 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29480WN 33998 EMERGENCY EXIT LIGHT LENS MISSING NEXT TO R2 DOOR. INSTALLED LENS ASSY PER MX NOTE. LATER AT MCO REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20050613001122005061300112NM 2005 6 13 SWAA051566 120050526A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 861 TO BS 864, ABOVE STR 16L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050613001152005061300115NM 2005 6 13 SWAA051573 120050526A5313BAC1498 STRINGER BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 620, STR 4L. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20050613001172005061300117NM 2005 6 13 SWAA051575 120050526A53306545772 SKIN BOEING737 7373H4 1384600NM UPPER FUSELAGE WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29353SW 24889 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN WORN AT DORSAL FIN AREA, BS 875 TO BS 886, LBL 4. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050613001192005061300119NM 2005 6 13 SWAA051577 120050524A53306523693 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING WALK AROUND INSP, FOUND 2 SKIN CRACKS AT BS 390, STR 16R, & BS 470, STR 17R. REPAIRED SKIN PER SRM & SWA EA. 2L72 4F RTA16WE 20050613001232005061300123WP 2005 6 13 P9RA20050086 120050528A3260 WARNING LIGHT DOUG DC9 DC982 3022082WP MLG FALSE INDICATIONA P9RAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO11135NJ 49440 SFB - RED UNSAFE NOSE GEAR INDICATION AFTER TAKEOFF. CYCLED ONCE, STILL HAD RED UNSAFE IN RETRACT POSITION. RETURNED TO SFB. LANDED AT 142,000 LBS. LANDING WAS SMOOTH. INSPECTED AIRCRAFT PER M/M FOR OVERWEIGHT LANDING CONDITION. NO DEFECTS WERE NOTED. GEAR PINS INSTALLED AND SAFETIED. AIRCRAFT FERRIED TO JAX FOR MAINTENANCE. JAX MAINTENANCE ENTRY. LUBRICATED NOSE LANDING GEAR PER M/M. RETRACTED NOSE LANDING GEAR; ALL INDICATIONS NORMAL. AIRCRAFT PERFORMED LOCAL ACCEPTANCE FLIGHT WITH NO FURTHER DISCREPANCIES. NO PARTS REPLACED AS A RESULT OF THIS EVENT. 2L72 4F A6WE 20050613001242005061300124NM 2005 6 13 DHL2005741520 120050417A5311 FRAME BOEING727 7272Q9 138448MNM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH46665 21931 CORROSSION ON FRAME AT BS 990 BETWEEN 30 AND 29R STRINGERS. EVALUATED CORROSION ON FRAME BS 990 BETWEEN STR 29R AND 30 FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 1. REMOVED FLOOR SUPPORT BRACKET AND STRINGER CLIP IAW B727 SRM 51-30-2. CUT OUT DAMAGED SECTION ON FRAME DIM 4 1/2" BY 1/4" IAW B727 SRM 53-10-4 FIG 15. FABRICATED REPAIR ANGLE 7075T6 .050 PO NR 9002118 DIM 4 1/2" BY 1" BY 1" IAW B727 SRM 53-10-4 FIG 15. TREATED AND PRIMED REPAIR PART AND AREA IAW B727 SRM 51-10-2. INSTALLED REPAIR IAW B727 SRM 53-10-4 FIG 15. INSTALLED FLOOR SUPPORT FLOOR SUPPORT BRACKET AND STRINGER CLIP IAW B727 SRM 51-30-2. 2L73 4F RTA3WE 20050613001252005061300125EA 2005 6 13 COMAO560319 120050524A3260864808 PSEU CNDAIRCL600 CL6002B19 1900309EA MLG MALFUNCTIONED A COMABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01709CA1787611199 7238 FLT 5183 - DISPLAY COOL CAUTION, CABIN ALTITUDE WARNING AND BURNING ODOR IN COCKPIT. REPLACED THE PSEU. 2L72 4F RTA21EA 20050609000102005060900010SO 2005 6 9 C2XA05SH042 120050523A532014521713005 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717984 145246 SHV - DURING C-CHECK THE RT OMEGA BEAM NUT PLATE IS CORRODED JUST AFT OF FRAME 23. MAINTENANCE INSTALLED HAT BEAM REPAIR ON RT OMEGA BEAM AT NUT PLATE HOLE AFT OF FR 23 IAW EMB SRM 53-21-10 FIG 206. INSTALLED NUT PLATE IAW EC 5320-01137. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050609000132005060900013NM 2005 6 9 05FDEA01398 120050521A5330 SKIN BOEING727 727233 138408ANM FUSELAGE DEFORMED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25264FE 21626 WHILE WORKING NOSE AREA DOUBLER FOUND SKIN DEFORMED ALONG LT SIDE. REPLACED DOUBLER PER FED-EX EA 7-5330-86293. 2L73 4F RTA3WE 20050609000182005060900018NM 2005 6 9 C1HA200596003 120050422A5320 INTERCOSTAL BOEING727 7272J4 1384006NM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15696CA 22574 MAIN PASSENGER CABIN STA 304 TO 312 RBL 45, UNDER CONTROL CABIN BULKHEAD BOTTOM ANGLE, INTERCOSTAL CORRODED FWD END. 2L73 4F RTA3WE 20050609000582005060900058EA 2005 6 9 SWIA200515025 120050522A2780766389L CONTROLLER CNDAIRCL600 CL6002C10 1390015EA NR 1 MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07707SK 10003 SLATS HALF SPEED STATUS MSG. REPLACED NR 1 SFECU IAW AMM 27-51-05. OPERATIONAL CHECK GOOD. P/N OFF 766389L, S/N OFF 0714. 2L72 4F RTA21EA 20050609000702005060900070EA 2005 6 9 SWIA200515037 120050520A2740 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CRCRUISE 1 NM07710BR 7852 STAB TRIM AND MACH TRIM CAUTION MSGS AT ALTITUDE. REPLACED F/O'S TRIM SWITCH IAW CRJ MM 27-41-30. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050609000802005060900080EA 2005 6 9 SWIA200515047 120050520A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07903SW 7425 EXTERIOR EMERGENCY LIGHT JUST FORWARD OF LEFT OVERWING EXIT INOP. RELAMPED EMERGENCY EXTERIOR LIGHT AS NEEDED. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050609000842005060900084WP 2005 6 9 ABXA050133 120050517A531199196182N FRAME DOUG DC9 DC931 3022065WP CABIN CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23906AX 47072 RIGHT CENTER MAIN FRAME AT STA 718 REQUIRES REPLACEMENT PER DC-9 SERVICE BULLETIN 53-100, PAGE 11, ITEM 1E. REMOVED AND REPLACED MAIN FRAME AT STA 718 IAW EA 53400324-001-2. 2L72 4F A6WE 20050609000872005060900087EA 2005 6 9 COMA0560316 120050523A3260 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA MLG ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01709CA 7238 FLIGHT 9483 GEAR DISAGREE WARNING. FOUND NLG REQUIRED SERVICED. SERVICED NLG IAW MM. 2L72 4F RTA21EA 20050609000912005060900091 2005 6 9 SWAA051470 420050521A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29207WN 34012 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050609000922005060900092NM 2005 6 9 SWAA051471 120050522A3350101114 BULB BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED A2 CHECK, FOUND EMERGENCY BULLNOSE LIGHT INOP AT ROW 17 ABC. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050609001002005060900100NM 2005 6 9 SWAA051479 120050520A53216517590 FLOOR PANEL BOEING737 7373H4 1384600NM COCKPIT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND 2 EA FUSELAGE FLOOR WEB CRACKS BETWEEN BS 188 TO BS 196, LT & RT SIDE, WL 208. REPAIRED FLOOR WEB PER SRM. 2L72 4F RTA16WE 20050609001052005060900105NM 2005 6 9 SWAA051484 120050520A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 847, LBL 17, WL 149. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050609001242005060900124EA 2005 6 9 SWIA200515053 120050210A5347 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07590SW 7077 RT SIDE SEAT RAIL BETWEEN FS 364.00 - FS 409.00 + 16 IS CORRODED ITEM FOUND AT C-CHECK INSPECTION. REPLACED RT SIDE SEAT RAIL BETWEEN FS 364.00 - FS 409 + 16 IAW CRJ SRM 51-40-11, 51-41-02, 51-41-04, 51-25-16. 2L72 4F RTA21EA 20050609001262005060900126EA 2005 6 9 SWIA200515055 120050210A5320 SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07590SW 7077 PAX CABIN UNDER FLOOR AT FS 559 VERTICAL POST RBL 27.0 INBD FLANGE CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-41-280. 2L72 4F RTA21EA 20050609001342005060900134NM 2005 6 9 AALA20050348 120050523A3260434093003 LIGHT BOEING767 767323 1385205NM COCKPIT MELTED A AALAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SW21386AA 27060 SMOKE FROM GEAR HANDLE SLOT ON SHORT FINAL AFTER GEAR CONFIRMED DOWN LOCKED. LEFT GEAR LIGHT WENT OUT. SMOKE FOR 10 SECONDS. LANDING NORMAL. REPLACED LEFT MAIN GEAR ANNUNCIATOR LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050609001502005060900150NM 2005 6 9 AWXA200500605 120050524A3260106122615 SENSOR BOEING737 7373G7 1384595NM MLG FAULTY A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28154AW 23776 PHX - AIR TURNBACK - FLT 788 - ON CLIMB-OUT OUT OF PHX EN ROUTE TO PDX WITH LANDING GEAR LEVER IN THE OFF POSITION, THE RIGHT MAIN GEAR INDICATED DOWN AND GREEN WITH NO RED TRANSIT. PILOTS CYCLED THE GEAR WITH NO CHANGE IN INDICATIONS, HOWEVER, THE LEFT MAIN GEAR WAS INDICATING TRANSIT WHEN THE LIGHT SHOULD HAVE BEEN OUT. MAINTENANCE REMOVED AND REPLACED THE M981 DOWN LOCK LOGIC CARD IAW 32-09-20-4. HO HELP. MAINTENANCE REMOVED AND REPLACED THE RT MAIN GEAR DOWNLCIK SENSOR S73 IAW MM 32-61-31-4 AND AWM 32-64-01. MAINTENANCE PERFORMED TWO GEAR SWINGS AND OPERATIONALLY CHECKED FOR 6 CYCLES WITH NO DEFECTS NOTED. AIRCRAFT RELEASE TO SERVICE. 2L72 4F RTA16WE 20050609001532005060900153NM 2005 6 9 AWXA200500608 120050507A53116546539 FRAME BOEING737 7373U3 13844CCNM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28335AW 28740 DURING C-6 CHECK, A CRACK WAS FOUND ON FRAME BS 616 INNER CHORD AT WL 204 ORIGINATING COMMON TO FASTENER HOLE. MAINTENANCE REPAIRED CRACK AT FRAME BS 616 INNER CHORD AT WL 204 IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5300-05141-RC2. 2L72 4F RTA16WE 20050609001642005060900164NM 2005 6 9 05FDEA00701 120050329A5512ALC8100XXX PANEL DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 LEFT HORIZONTAL STABILIZER UPPER BARREL NUT NR 21 HAS BORE CORROSION EXCEEDING LIMITS. BARREL NUT BORE NR 21 LT REPAIRED IAW EA 1-5510-78133 ATTACHMENT 3, HORIZONTAL STABILIZER BARREL NUT BORE REWORK/ REPAIR AD 2003-22-08. MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050609001712005060900171NM 2005 6 9 05FDEA00719 120050331A5512ALC8100XXX PANEL DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 RIGHT HORIZONTAL STABILIZER UPPER BARREL NUT NR 16 HAS BORE CORROSION EXCEEDING LIMITS. BARREL NUT BORE NR 16 RIGHT REPAIRED IAW EA 1-5510-78133 ATTACHMENT 14, HORIZONTAL STABILIZER BARREL NUT BORE REWORK/ REPAIR AD 2003-22-08. MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050609001942005060900194SW 2005 6 9 KBM2005F00071 120050413A770012444412 GAUGE BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL TOT FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19188TV52 2704 TOT GAUGE, INDICATES -0- BELOW 250 DEGREES C. REMOVED AND REPLACED. (K) 1G71 3U3 U H2SW E4CE 20050609001952005060900195EU 2005 6 9 KBM2005F00073 120050324A6420350A33215300 BEARING SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1 60030NE TAIL ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19215LA826 2143 LAMINATED BEARINGS WORN. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050609001992005060900199 2005 6 9 KBM2005F00077 420050402A34215040111920 INDICATOR SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE HORIZON INTERMITTENT E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19345SH1748 3345 ATTITUDE INDICATOR CAGES BUT WILL UNCAGE A FEW MINUTES LATER. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050609002002005060900200 2005 6 9 KBM2005F00078 420050504A2312064105430 RADIO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1B 6OO30NE VHF DISTORTED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH464 2957 VHF RADIO, RECEIVES BROKEN, DISTORTED. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050609002012005060900201EU 2005 6 9 KBM2005F00079 120050331A771456337078012 INDICATOR SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE NG ERRATIC E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19351WM 2167 N.G., GAUGE NEEDLE AND DIGITS ARE ERRATIC INTERMITTENTLY. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050609002082005060900208SW 2005 6 9 KBM2005F00085 120050405A771422A690 TACH GENERATOR BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL ENGINE INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19667JM 3444 TACH GENERATOR, INOPERATIVE 95 PERCENT OF THE TIME, DOES NOT PROVIDE SIGNAL TO INDICATE GAUGES. REMOVED AND REPLACED. (K) 1G71 3U3 U H2SW E4CE 20050610000042005061000004NM 2005 6 10 CALA0500166 120050520A5347140N20692 SEAT TRACK BOEING757 757224 1384958NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717105 27295 INSPECTION FOUND SEAT TRACK SECTIONS CORRODED BETWEEN STA 720 AND 740, AT RBL 25 AND RBL 45.5. THE SEAT TRACK SECTIONS WERE REPLACED IAW SRM 51-40-02 AND 51-40-05. 2L72 4F RTA2NM 20050610000112005061000011EU 2005 6 10 MALA050346 120050413A5411 STRINGER BAC 146 AVRO146RJ85A1500097EU NOSE COWL CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15503XJ E2310 DURING C2 INSPECTION, FOUND 1 CRACKED STRINGER, NR 2 ENGINE ON BULKHEAD AFT OF NOSE COWL. 2H74 4F RTA49EU 20050610000132005061000013EU 2005 6 10 MALA050439 120050413A5411 STRINGER BAC 146 AVRO146RJ85A1500097EU NOSE COWL CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15503XJ E2310 DURING C2 INSPECTION, FOUND 1 CRACKED STRINGER NR 2 ENGINE ON BULKHEAD AFT OF NOSE COWL. 2H74 4F RTA49EU 20050610000282005061000028WP 2005 6 10 U2RA3056 120050526A273147105423 BELLCRANK DOUG DC8 DC871F 302199DWP RT ELEVATOR DISCONNECTED A U2RAK NONE O OTHER ININSP/MAINT 1 GL23872SJ813327 46040 DURING INSPECTION, RT ELEVATOR GEARED TAB OUTBOARD CRANK P/N 4710542-3 FOUND DISCONNECTED FROM LINK P/N 271442-501. NOTE: AIRCRAFT IS CURRENTLY CLASSIFIED PART 91. 2L74 4F RT4A25 20050610000302005061000030SO 2005 6 10 C2XA05CL038 120050520A33501317 LAMP EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713994 145291 DURING ROUTINE MAINTENANCE, THE EMERGENCY LIGHT AT SEAT 12A WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE LAMP. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20050610000312005061000031SO 2005 6 10 C2XA05BT031 120050525A335010111911 LIGHT EMB 145 EMB145LR 3260212SO FUSELAGE FAULTY A C2XAO OTHER O OTHER NRNOT REPORTED 1 SW2713955 145075 EWR-CO2455, CREW REPORTED, "EMERGENCY LIGHT BELOW COCKPIT DOOR DOESN'T WORK." MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BELOW THE COCKPIT DOOR IAW EMB145 AMM NR 33-50-05, OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050610000562005061000056NM 2005 6 10 SWAA051500 120050523A53116516301 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STUB FRAME CRACKED AT BS 188, LT SIDE, WL 208. REMOVED AND REPLACED STUB FRAME PER SRM. 2L72 4F RTA16WE 20050610000582005061000058NM 2005 6 10 SWAA051502 120050523A53126516300 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE BULKHEAD WEB CRACKED AT BS 178, LBL 25, WL 207. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050610000602005061000060NM 2005 6 10 SWAA051504 120050523A57126545445 RIB BOEING737 7373H4 1384600NM RT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29353SW 24889 DURING SCHEDULED 1/2D CHECK, FOUND RT WING RIB LOWER CHORD CRACKED AT WBL 135.5, BETWEEN STR 2 & STR 3. REPAIRED RIB PER SWA ACO. 2L72 4F RTA16WE 20050610000632005061000063 2005 6 10 SWAA051508 420050523A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29394SW 27380 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050610000652005061000065NM 2005 6 10 SWAA051510 120050521A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 DURING PREFLIGHT CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 757, STR 18L TO STR 19L. TEMP REPAIRED SKIN & MX FERRY TO PHX. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050613000012005061300001NM 2005 6 13 SWAA051511 120050523A335015AT17 SWITCH BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29770SA 30589 DURING SCHEDULED 5Y CHECK, ALL EMERGENCY LIGHTS ILLUMINATED WITH NO ELECTRICAL POWER ON & COCKPIT LIGHT SWITCH OFF. REMOVED AND REPLACED EMERGENCY LIGHT SWITCH PER WDM & MM. 2L72 4F RTA16WE 20050613000022005061300002NM 2005 6 13 SWAA051535 120050524A53116546549 FRAME BOEING737 737301 1384611NM AFT CARGO BAY CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 767, LBL 10. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050613000082005061300008NM 2005 6 13 SWAA051512 120050523A261235008307 MODULE BOEING737 7377H4 1384404NM COCKPIT FAULTY A SWAAO OTHER N FALSE WARNING DEDESCENT 1 SW29208WN 29856 DECLARED EMERGENCY. MLG WW FIRE WARNING LIGHT ILLUMINATED INTERMITTANTLY. REMOVED AND REPLACED OVERHEAT MODULE PER MM. 2L72 4F RTA16WE 20050613000122005061300012NM 2005 6 13 SWAA051517 120050524A53106547978 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND FUSELAGE CREASE BEAM WEB CORRODED AT BS 747 TO BS 767, RBL 65, WL 208. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM. 2L72 4F RTA16WE 20050613000132005061300013NM 2005 6 13 SWAA051518 120050524A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 947, STR 26R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050613000292005061300029NM 2005 6 13 SWAA051534 120050524A5313BAC1498 STRINGER BOEING737 737301 1384611NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 500B, STR 27R. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20050613000362005061300036NM 2005 6 13 SWAA051553 120050525A55516551524 FITTING BOEING737 737301 1384611NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND LT & RT HORIZONTAL STAB FITTING LUG FACES CORRODED. REPAIRED LUG FACES PER SRM. 2L72 4F RTA16WE 20050613000422005061300042 2005 6 13 SWAA051559 420050525A256563550 SLIDE BOEING737 7377H4 1384404NM R1 & R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29714CB 27848 DURING SCHEDULED HC2 CHECK, FOUND R1 & R2 DOOR EMERGENCY EVAC SLIDES OUT OF ADJUST. ADJUSTED SLIDES PER MM. 2L72 4F RTA16WE 20050613000442005061300044CE 2005 6 13 71033 120050526A3210 STRUT WIPER BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA MLG LOOSE A AMWAK NONE O OTHER ININSP/MAINT 1 CE07133YV PAA61098 UE133 ON A WALK AROUND (PREFLIGHT) THE CREW DISCOVERED THE STRUT WIPER WAS LOOSE. MAINTENANCE REMOVED AND REPLACED THE RT MAIN LANDING GEAR ASSEMBLY. 2L72 4T3 TRTA24CE E2NE 20050613000462005061300046NE 2005 6 13 ALG2005F00028 120050508A3210 VALVE SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL MLG LEAKING E ALGAC ABORTED TAKEOFF K FLUID LOSS TOTAKEOFF 1 SW03519AL 760058 WHILE HOVERING OUT FOR TAKEOFF, NOTICED HYDRAULIC FLUID ON THE HELIPAD. RETURNED TO PAD TO INVESTIGATE AND SHUTDOWN HELICOPTER AND THEN CONTACTED MAINTENANCE. MAINTENANCE FOUND LANDING GEAR VALVE BUTTON POPPED. RESET THE BUTTON AND COMPLIED WITH LANDING GEAR OPERATIONAL CHECK AND LEAK CHECK. THE OPS CHECK WAS GOOD AND NO LEAKS COULD BE FOUND. WORK WAS DONE IAW MM. (K) 1G72 3U3 U H1NE E1GL 20050613000492005061300049SW 2005 6 13 ALG2005F00030 120050512A7931206075677103 GAUGE BELL 206 206L1 1182107SW ALLSN 250C 250C28B 03013GL OIL TEMP PRESS INOPERATIVE E ALGAO OTHER P NO WARNING INDICATION CLCLIMB 1 SW033199P 45790 CAE860345 ON INITIAL TAKEOFF AFTER ESTABLISHING A POSITIVE RATE OF CLIMB, CROSS CHECKED THE INSTRUMENT PANEL AND HAD NO INDICATION OF ENGINE OIL TEMPERATURE OR PRESSURE. NOTIFIED TOWER MADE 180 DEGREE TURN AND RETURNED TO BASE AND LANDED. MAINTENANCE REMOVED AND REPLACED THE ENGINE OIL PRESSURE/TEMPERATURE GAUGE IAW MM. (K) 1G71 3U3 U H2SW E1GL 20050613000522005061300052NM 2005 6 13 05FDEA01471 120050526A5320 GUIDE DOUG MD11 MD11 3023602NM FUSELAGE MISREPAIRED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25631FE 48454 FWD CARGO COMPT, FROM STA 959 TO STA 999 FOUND LT LOWER LONGITUDINAL PALLET GUIDE ASSY SUSPECT WITH INCORRECT SRM REPAIRS. NEW CHANNEL REPAIRED AS PER SRM 53-70-00 VOL I FIG 6. MINOR REPIAR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050613000532005061300053NM 2005 6 13 05FDEA01465 120050525A5310 DOOR FRAME DOUG MD11 MD11 3023602NM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25631FE 48454 FWD CARGO AFT DOOR JAMB STA 999 RT EXISTING NICK BLEND OUT. REPAIRED AS PER SRM 53-50-00 FIG 6 VOL I. MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050613000672005061300067NM 2005 6 13 DLM88050292 120050524A56105887275501 WINDSHIELD DOUG MD88 MD88 3023688NM COCKPIT CRACKED A DALAA UNSCHED LANDING O OTHER CRCRUISE 1 SO27907DL 49538 CENTER WINDSHIELD BEGAN BUBBLING AT CRUISE 20 MINUTES INTO THE FLIGHT. AREA TURNED BLACK AND STARTED TO CRACK. AIR TURNBACK TO CVG. REPLACED WINDSHIELD. 2L72 4F RTA6WE 20050613000692005061300069 2005 6 13 AWXA200500614 420050526A34162057011 ALTIMETER BOEING737 737301 1384611NM COCKPIT FAULTY A AWXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP28326AW221689858 23258 AT CRUSE ALTITUDE OF 360FL CABIN ALTITUDE HORN CAME ON & CABIN PRESSURE UNCONTROLLABLE. A BLEED TRIP OCCURRED ON NR 1 PACK ALONG WITH 2 DUCT OVERHEATS IN 3 MIN ACFT DESCENDED TO 11,000 FT IN STANBY MODE & CABIN PRESSURE RETURNED 10 MIN LATER. DIVERTED TO ELP. MX FOUND A PUSHED PIN AT CONNECTOR TO OUTFLOW VALVE & REPLACED CONNECTOR. MX R & R OUTFLOW VALVE HEATER GASKET IAW BMM 21-31-12-2 AND PERFORMED AN OPS TEST IAW AWA TASK CARD A6A21001. MX R & R CAPTAINS ELECTRICAL ALTIMETER IAW AWA TASKCARD R1B34010. OPS CK GOOD. TEAR DOWN REPORT SHOWS THAT THE BAROMETER WIPER WAS STIFF AND MOTOR WAS SLUGGISH ON THE ALTIMETER. THE UNIT WAS OVERHAULED AND THE BEARINGS WERE REPLACED IAW CMM 34-12-12 REV. 1. 2L72 4F RTA16WE 20050613000762005061300076EU 2005 6 13 MALA050454 120050525A5320 SILL BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15506XJ E2314 DURING C2 INSPECTION, FOUND PASSENGER DOOR SILL CORRODED. 2H74 4F RTA49EU 20050613000772005061300077EU 2005 6 13 MALA050455 120050525A5320 GUSSET BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15506XJ E2314 DURING C2 INSPECTION, FOUND GUSSET PLATE AT FRAME 18, RBL38 CORRODED. 2H74 4F RTA49EU 20050613000842005061300084NM 2005 6 13 102 120050527A53476549558 SEAT TRACK BOEING737 7373L9 1384470NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE GOUGED B K NONE O OTHER ININSP/MAINT 1 SO15312FL 24569 CABIN LT IB SEAT TRACK HAS NUMEROUS GOUGES STA. 540 TO 727E. S/O 109001, N/R 22850 2L72 4F4 FRTA16WE E21EU 20050613000872005061300087NM 2005 6 13 AALA20050361 120050518A5330 SKIN BOEING767 767323 1385205NM FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21361AA 24042 DUB - AIRCRAFT MAINTENANCE DISCOVERED A ONE INCH CRACK BETWEEN TWO RIVETS AT STRINGER 37 LEFT AT STATION 1219. ACCOMPLISHED TEMPORARY REPAIR FABRICATE REPAIR DOUBLER OF 2024T3 0.063 TO 0.080 THICK. INSTALL WET WITH SEALANT. INSTALL USING 3/16 PROTRUDING HEAD BLIND RIVETS USING EXISTING FASTENER PATTERNS. INSTALL AT MINIMUM TWO ROWS OF FASTENERS PAST CRACK IN EACH DIRECTION TO AIRCRAFT SKIN CRACK AT STATION 1219 STRINGER 37 LEFT PER SRM/AFW ENGINEERING INSTRUCTIONS FOR FERRY FLIGHT TO AFW BASE FOR FURTHER EVALUATION AND PERMANENT REPAIR. ACCOMPLISHED PERMANENT REPAIR PER MRB 767 2697. 2L72 4F RTA1NM 20050613000912005061300091WP 2005 6 13 IXXA05 120050429A5740 FITTING DOUG DC8 DC871F 302199DWP RT WING CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX 45993 DURING ROUTINE C-CHECK INSPECTION, RT WING L/E INBOARD STUB WING UPPER SURFACE SCREWS OXIDIZED, XW 257.000. REMOVED OXIDIZED SCREWS IAW DC-8 SRM 51-3-0 PAGE 1. INSTALLED NEW SCREWS ON RT L/E INBOARD STUD WING UPPER SURFACE, XW 257.000 IAW DC-8 SRM 51-3-0 PAGE 1. TORQUED FASTENERS IAW DC-8 SRM 51-3-1. 2L74 4F RT4A25 20050613000942005061300094WP 2005 6 13 IXXA05SMN55S 120050429A5340 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX 45993 DURING ROUTINE C-CHECK INSPECTION, FWD CARGO COMPT - INTERIOR SPLICE FITTING CRACKED, STA 440.000 - STA 460.00, L-34L 3. REMOVED CRACKED FITTING IAW DC-8 SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING (ALCLAD 7075 T6 51) IAW DWG 3750330. PERFORMED NDT INSPECTION TO FITTING IAW NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED AREA + NEW FITTING IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO IAW DC-8 SRM 51-1-11 PAGE 9. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D PAGE 9. TORQUED IAW DC-8 SRM 51-3-1. 2L74 4F RT4A25 20050613000962005061300096NE 2005 6 13 ASMF200505027 220050524A7200 ENGINE BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE LEFT FAILED W ASMFE ENGINE SHUTDOWN J WARNING INDICATION DEDESCENT 1 SW23805AM 16474 26272 726732 CAPTAIN REPORTED THAT DURING DESCENT AT 18500 FEET, THE LEFT ENGINE OIL FILTER LIGHT CAME ON. THE ABNORMAL PROCEDURE 05-14 WAS PERFORMED AND THE A/T ARMED SWITCH WAS SHUT OFF AND THE ACCELERATOR WAS HELD BUT LIGHT CONTINUED. ENGINE WAS SHUT DOWN. AT PLATFORM, THE CHIP DETECTOR WAS CHECKED AND METALLIC PARTICLES WERE FOUND. THE LEFT ENGINE WAS REPLACED IAW MPCM 71-00-02, TESTED CORRECT. 2L72 4F4 FRTA2NM E17NE 20050613001262005061300126EA 2005 6 13 COMA0570057 120050527A3222521011 CYLINDER CNDAIRCL600 CL6002C10 1390015EA NLG CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01371CA6530 10082 NLG OUTER CYLINDER P/N 52101-1 S/N BA0049 IS CORRODED. CORROSION REPAIRED I/A/W BOMBARDIER REO 670-32-21-054 AND GOODRICH SCR 0008-04 REV C. 2L72 4F RTA21EA 20050613001272005061300127EA 2005 6 13 COMA0570058 120050527A531267053110521 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01371CA6530 10082 FS 280 BULKHEAD LOWER WEBS ARE CORRODED BEYOND LIMITS FROM LBL 36 TO RBL 36. REPLACED THE FS 280 BULKHEAD LOWER WEBS IAW BOMBARDIER INC REO 670-53-11-052 REV A REPAIR NR 2. 2L72 4F RTA21EA 20050613001282005061300128EA 2005 6 13 COMA0570059 120050527A5343CC670341757 BEAM CNDAIRCL600 CL6002C10 1390015EA MLG CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01371CA6530 10082 TRANSVERSE BEAM AT FS 280 FROM LBL36 TO RBL36 IS CORRODED ALONG UPPER AND LOWER EDGES. REPLACED THE TRANSVERSE BEAM AT FS 280 IAW BOMBARDIER REO 670-53-11-047 REV C. 2L72 4F RTA21EA 20050613001292005061300129NM 2005 6 13 SB05065 120050528A335020121 POWER SUPPLY BOEING737 7373B7 1384580NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19371US 22950 CLT - MAINTENANCE REPORTED THE EMERGENCY LIGHT BATTERY PACK AT LOCATION M1135 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050613001312005061300131NM 2005 6 13 0500776719 120050516A3310270102 LIGHT BOEING747 747251F 1384898NM COCKPIT INOPERATIVE A NWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL01619US 21321 DURING CLIMB-OUT, SMOKE FILLED FLIGHT DECK. AIRCRAFT RETURNED TO SIN AND LANDED WITHOUT INCIDENT. SIN MAINTENANCE FOUND FE PANEL LIGHT CB POPPED. FE DIMMER WAS BURNED. MEL'D COCKPIT LIGHTS, AND COLLARED BREAKER AND WILL REPLACE DIMMER IN NRT. NRT MAINTENANCE 17MAY05 REMOVED AND REPLACED FFE DIMMER. MEL REMOVED OPERATION CHECKS NORMAL. REF LOG 2357883 AND 2357686. 2L74 4F A20WE 20050613001332005061300133NM 2005 6 13 CALA0500177 120050529A323369355006 ACTUATOR BOEING737 7373T0 1384582NM LT MLG INOPERATIVE A CALAO OTHER J WARNING INDICATION APAPPROACH 1 SW277635542491 23593 THE LT MLG GREEN LIGHT DID NOT ILLUMINATE FOR SEVERAL MINUTES WHEN GEAR WAS EXTENDED ON APPROACH INTO IAH. THE AIRCRAFT LANDED WITHOUT INCIDENT. WHEN MAINTENANCE PERFORMED A GEAR SWING THE LT MAIN GEAR DID NOT EXTEND, BUT MANUAL EXTENSION WAS GOOD. THE LT MLG UPLOCK ACTUATOR WAS REMOVED AND REPLACED IAW MM 32-32-41. IN ADDITION, THE GEAR WAS LUBRICATED AND THE LT MLG DOWNLOCK SENSOR WAS CHECKED AND FOUND WITHIN LIMITS. AN ADJUSTMENT/TEST WAS PERFORMED IAW MM 32-32-00 AND ALL OPERATION CHECKED GOOD. 2L72 4F RTA16WE 20050613001362005061300136NM 2005 6 13 F3LA200500023 120050527A2150759D0000 CONTROLLER AIRBUSA319 A319111 3930336NM A/C PACK OVERHEATED A F3LAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 NM03934FR 2238 2287 AIR TURNBACK - ON CLIMB-OUT, FLIGHT CREW REPORTED A NR 2 AIR CONDITIONING PACK OVERHEAT ECAM MESSAGE. NR 1 PACK WAS ALREADY ON MEL. RETURNED TO SEA AND DECLARED AN EMERGENCY. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED NR 2 AIR CONDITIONING PACK CONTROLLER. 2L72 4F RTA28NM 20050613001382005061300138NM 2005 6 13 DHL2005741521 120050417A5522 SKIN BOEING727 7272Q9 138448MNM ELEVATOR DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 LEFT ELEV LWR SKIN HAS 3EA DENTS AFT OF NR 4 BALANCE BAY. DAMAGED AREA 3 EA DENTS FOUND TO BE OUT OF LIMITS IAW B727 SRM 55-20-1 FIG 1. CUT OUT DAMAGED AREA DIM 3" BY 2" ON LT ELEVATOR LOWER SKIN AND FABBED REPAIR DOUBLER FROM 2024T3 .032 DIM 5 3/4" BY 4" PO NR 9001634 IAW B727SRM 55-20-3 FIG 4. DOUBLER TREATED AND PRIMED AND INSTALLED IAW B7287 SRM 51-10-2 AND 55-20-3 FIG 4 LT ELEVATOR REBALANCED IAW B727 SRM 51-80-7. 2L73 4F RTA3WE 20050613001412005061300141EA 2005 6 13 MASA200500355 120050514A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0717275 7275 ASH 6404 - LAS TO COS - THE CREW NOTED THAT THE EMERGENCY EXIT LIGHTED SIGN HAS 2 OF 5 BULBS INOP. MAINTENANCE RELAMPED. 2L72 4F RTA21EA 20050613001442005061300144CE 2005 6 13 DXTA200500743 120050527A284099144272 LIMIT SWITCH CESSNA750 750 2076810CE FUEL TANK INOPERATIVE E DXTAH DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL07999QS2547 7500203 DURING A 52 MINUTE FLIGHT IN CRUISE, "WING TANK O'FULL R" AMBER CAS MESSAGE ILLUMINATED 3 DIFFERENT TIMES. EACH TIME LOST APPROX 100-200 LBS OF FUEL. REMOVED AND REPLACED FLOAT SWITCH IAW CE 750 MM 28-20-07. 2L72 4J RTT00007WI 20050613001462005061300146CE 2005 6 13 DXTA200500742 120050525A5753 GUARD CESSNA650 650 2076802CE TE FLAPS LOOSE E DXTAO OTHER F FLT CONT AFFECTED TOTAKEOFF 1 GL07715QS 6507105 ON TAKEOFF FLAPS (20) WOULD NOT RETRACT TO ZERO. FLAP HANDLE WOULD NOT MOVE FROM DETENT. UPON LANDING AND SHUTDOWN, FLAPS THEN RETRACTED NORMALLY. OPERATED FLAPS NUMEROUS CYCLES AND FOUND NO FAILURE, HOWEVER, FOUND THE FLAP HANDLE SIDE GUARDS LOOSE. REMOVED FLAP HANDLE AND TIGHTENEND SIDE GUARDS, REINSTALLED FLAP HANDLE ASSY FLAPS. OPS CHECK GOOD IAW THE MODEL 650 MM 27-54-01. 2L72 4F A9NM 20050613001492005061300149NM 2005 6 13 UPS05444516 120050520A5311 FRAME BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C U/D - STA 600 FRAME CRACKED AT STRINGER S-8R AREA (CRACK LENGTH .5 INCH). U/D STA 600 AT STRINGER S-8R FRAME REPAIRED AS PER SRM 53-10-04 FIG 54. 2L74 4F A20WE 20050613001512005061300151NM 2005 6 13 UPS05444519 120050518A5313 STRINGER BOEING747 747123F NM CARGO BAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C FWD CARGO COMPT STR 39L CRACKED AT BS 745 (CRACK LENGTH 1.25 INCH). FWD CARGO COMPT BS 755 TO 770 STR 39L REPAIRED AS PER SRM 53-10-03 FIG 1 & STRINGER SPLICE REINSTALLED AFTER REPAIRED AS PER SRM 51-30-02. 2L74 4F A20WE 20050613001532005061300153NM 2005 6 13 UPS05444521 120050517A5313 STRINGER BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C M/D - BS 2180 - 2200 STR 11L STRINGER END FOUND CRACKED (CRACK LENGTH .75 INCH). M/D - BS 2180 - 2210 STR 11L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4. 2L74 4F A20WE 20050613001552005061300155NM 2005 6 13 UPS05444523 120050520A5315 FLOORBEAM BOEING747 747123F NM FUSELAGE MISDRILLED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C CABIN - U/D BS 380 FWD FLANGE OF FLOORBEAM FLOOR PANEL ATT HOLES SHORT EDGE MARGIN FOUND AT RBL 39, 40 & 41 AREA. CABIN - U/D BS 380 FWD FLANGE OF FLOORBEAM RBL 39, 40 & 41 AREA REPAIRED AS PER UPS EO B747-5320-12407 APPENDIX D PLAN C. 2L74 4F A20WE 20050613001572005061300157NM 2005 6 13 UPS05444526 120050520A5315 FLOORBEAM BOEING747 747123F NIR NM PWA JT9 JT9D3 52050NE FUSELAGE DAMAGED A IPXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C CABIN- U/D BS 380 FWD FLANGE OF FLOORBEAM FLOOR PANEL ATT. HOLES SHORT EDGE MARGIN FOUND AT RBL 20 INCHES AND 24.5 INCHES. CABIN - U/D BS 380 FLOORBEAM FWD FLANGE RBL 20 INCHES AND 24.5 INCHES AREA REPAIRED IAW EO B747-5320-12407-D PLAN C. 2L74 4F4 FRTA20WE E20EA 20050613001592005061300159NM 2005 6 13 UPS05444528 120050520A5313 STRINGER BOEING747 747123F NM PWA JT9 JT9D3 52050NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C U/D - LT SIDE BS 640 STR END S-9L CRACKED ( CRACK LENGTH 1INCH ) U/D LT SIDE BS 640 STR 9L REPAIRED IAW SRM 53-10-03 FIG 2. 2L74 4F4 F A20WE E20EA 20050613001612005061300161NM 2005 6 13 UPS05444530 120050520A5313 STRINGER BOEING747 747123F NM PWA JT9 JT9D3 52050NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C U/D STA 560 STRINGER S-9R END CRACKED. ( CRACK LENGTH .4375 INCH ) U/D - BS 560 STR -9R REPAIRED IAW SRM 53-10-03 FIG 2. 2L74 4F4 F A20WE E20EA 20050613001632005061300163NM 2005 6 13 UPS05444532 120050518A532065B119542 FLOOR SUPPORT BOEING747 747123F NM PWA JT9 JT9D3 52050NE FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C U/D- BS 420-440 BL 0 FLOOR (L) SUPPORT FOUND CORROSION. CORROSION BLEND OUT 0.033 INCH X .7500 INCH X 1INCH EXCEED SRM 53-10-01 FIG 1 LIMIT, U/D BS 420-440 BL 0 FLOOR (L) SUPPORT REPLACED IAW SRM 51-10-01. 2L74 4F4 F A20WE E20EA 20050613001652005061300165NM 2005 6 13 UPS05444534 120050518A5313 STRINGER BOEING747 747123F NM PWA JT9 JT9D7A 52054NE CARGO BAY CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C BULK CARGO COMPT - BS 1924 S32R STRINGER END CORRODED. CORROSION BLEND OUT 0.040 INCH X .8750 INCH X 1INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. BULK CARGO COMPT - BS 1924 S-32R STRINGER REPAIRED IAW SRM 53-10-01 FIG 1. 2L74 4F4 F A20WE E20EA 20050613001672005061300167NM 2005 6 13 UPS05444536 120050518A5320 FLOOR SUPPORT BOEING747 747123F NM PWA JT9 JT9D7A 52054NE FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE: C U/D - BS 520-530 RBL 82, FLR SUPPORT (L) ANGLE LWR FACE FOUND CORROSION. CORROSION BLEND OUT 0.025 INCH X .8750 INCH X 2 INCHES EXCEED SRM 53-10-01 FIG 1 LIMITS, U/D BS 520-530 RBL 82 INCH FLR SUPPORT (L) ANGLE REPAIRED IAW SRM 51-40-04 FIG 2. 2L74 4F4 F A20WE E20EA 20050613001692005061300169NM 2005 6 13 UPS05444538 120050519A5347 SEAT TRACK BOEING747 747123F NM PWA JT9 JT9D7A 52054NE FUSLEAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE: C M/D - BS 600-640 LBL 90 SEAT TRACK OB FLANGE COR. CORROSION BLEND OUT 0.034 INCH X .8750 INCH X 0.5 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. M/D SEAT TRACK REPAIRED IAW SRM 53-10-05 FIG 1A AT BS 570-640 LBL 90. 2L74 4F4 F A20WE E20EA 20050613001712005061300171NM 2005 6 13 UPS05444540 120050514A5320 SUPPORT BOEING747 747123F NM PWA JT9 JT9D7A 52054NE AFT CARGO CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE: C AFT CARGO COMPT - BS 1914 LBL 25 AND LBL 47 AFT FIXED END STOP LWR SUPPORT CRACKED. ( CRACK LENGTH .7500 INCH TO 1INCH ) AFT CARGO COMPT - BS 1914 LBL 25 AND LBL 47 AFT FIXED END STOP LWR SUPPORT REPAIRED IAW SRM 51-40-03 FIG 2. 2L74 4F4 F A20WE E20EA 20050613001732005061300173NM 2005 6 13 UPS05444542 120050520A5313 STRINGER BOEING747 747123F NM PWA JT9 JT9D7A 52054NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C M/D-BS 742, S 3AL STRINGER END FOUND CRACK AS MARKED. ( CRACK LENGTH 1.5 INCHES ) M/D BS 742 STR 3AL STRINGER REPAIRED IAW SRM 53-10-03 FIG 10. 2L74 4F4 F A20WE E20EA 20050613001752005061300175NM 2005 6 13 UPS05444544 120050519A5347 SEAT TRACK BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C M/D - BS 756 RBL 33 SEAT TRACK O/B FLANGE CORRODED. CORROSION BLEND OUT 0.039 X .875 X 1.25 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT, M/D BS 670 - 770 RBL 33 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A. 2L74 4F A20WE 20050613001782005061300178NM 2005 6 13 UPS05444547 120050519A5347 CARGO TRACK BOEING747 747123F NM CARGO BAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C M/D - BS 520, LBL 11, TIE DOWN TRACK FOUND HEAVY CORROSION CRACK (CRACK LENGTH 2.5 X 1 INCH). TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05. 2L74 4F A20WE 20050613001802005061300180WP 2005 6 13 UPS05844550 120050524A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE:C3 RIGHT OUTBOARD L/E SKIN HAS CORROSION AT XFS 554. CUT OUT DAMAGED AREA OF L/E SKIN IAW DC-8 SRM 57-02-01 FIG 14. FABRICATED REPAIR DOUBLER & FILLER AND INSTALLED IAW DC-8 SRM 57-02-01 FIG 14, 51-1-26, AND 51-1-21. 2L74 4F RT4A25 20050613001912005061300191EU 2005 6 13 AWXA200500619 120050503A5347D5713014720000 SEAT TRACK AIRBUS320 A320232 3930326EU FUSLEAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28639AW 471 DURING C08 CHECK, GALVANIC CORROSION WAS FOUND ON SEAT TRACK BEAM -Y765 BETWEEN FS 36 TO FS 41. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK BEAM -Y765 BETWEEN FS 36 TO FS 41; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050613001932005061300193EU 2005 6 13 AWXA200500621 120050503A5347D5311278220201 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28639AW 471 DURING C08 CHECK, EXFOLIATION CORROSION WAS FOUND ON RT SEAT TRACK BEAM -Y1292 AT FS 12 TO FS 24. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK BEAM -Y1292 AT FS 12 TO FS 24; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050613001942005061300194EU 2005 6 13 AWXA200500622 120050503A5347D53371112001 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28639AW 471 DURING C08 CHECK, GALVANIC CORROSION WAS FOUND ON RT OUTBOARD SEAT TRACK BEAM -Y1292 AT FS 41 TO FS 47. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK BEAM -Y1292 AT FS 41 TO FS 47; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050613001952005061300195EU 2005 6 13 AWXA200500623 120050503A5347D5337111001000 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28639AW 471 DURING C08 CHECK GALVANIC CORROSION WAS FOUND ON RT INBOARD SEAT TRACK BEAM -Y765 AT FS 41 TO FS 47. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK BEAM -Y765 AT FS 41 TO FS 47; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050613001962005061300196EU 2005 6 13 AWXA200500624 120050503A5347D5311278220201 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28639AW 471 SAL - MAJOR REPAIR - DURING C08 CHECK GALVANIC CORROSION WAS FOUND ON RT INBOARD SEAT TRACK BEAM -Y765 AT FS 12 TO FS 24. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK BEAM -Y765 AT FS 12 TO FS 24; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050613001972005061300197EU 2005 6 13 AWXA200500625 120050504A5347D5337111000800 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28639AW 471 DURING C08 CHECK, GALVANIC CORROSION WAS FOUND ON LT INBOARD SEAT TRACK BEAM Y765 AT FS 45. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK BEAM Y765 AT FS45; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11. 2L72 4F RTA28NM 20050613001982005061300198EU 2005 6 13 AWXA200500626 120050504A5347D53230464200 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28639AW 471 SAL - MAJOR REPAIR - DURING C08 CHECK GALVANIC CORROSION WAS FOUND ON SEAT TRACK BEAM -Y765 AT FR24 TO FR35. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK BEAM -Y765 AT FR24 TO FR35; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11. 2L72 4F RTA28NM 20050613001992005061300199EU 2005 6 13 AWXA200500627 120050504A5347DAN2001T79511 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28639AW 471 DURING C08 CHECK, GALVANIC CORROSION WAS FOUND ON LT OUTBOARD SEAT TRACK BEAM Y1292 AT FS 53. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK BEAM Y1292 AT FS 53; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 AND A320 SRM 53-00-15. 2L72 4F RTA28NM 20050613002002005061300200EU 2005 6 13 AWXA200500628 120050504A5347D5371112000 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28639AW 471 DURING C08 CHECK, GALVANIC CORROSION WAS FOUND ON LT OUTBOARD SEAT TRACK BEAM Y1292 AT FS 41 TO FS 47. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK BEAM Y1292 AT FS 41 TO FS 47; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11. 2L72 4F RTA28NM 20050613002012005061300201EU 2005 6 13 AWXA200500629 120050511A5315D5347218820200 FLOORBEAM AIRBUS320 A320232 3930326EU FUSLEAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28639AW 471 DURING C08 CHECK, GALVANIC CORROSION WAS FOUND ON FLOORBEAM Y1162 AT FS 68 TO FS 69. MAINTENANCE REMOVED FLOORBEAM Y1162 AT FS 68 TO FS 69; FABRICATED A NEW REPLACEMENT FLOORBEAM PER DWG D53472088; INSTALLED REPAIR PART IAW A320 SRM 51-42-11. 2L72 4F RTA28NM 20050614000012005061400001NM 2005 6 14 103 120050527A53476549558 SEAT TRACK BOEING737 7373L9 1384470NM GE CFM56 CFM56* 13802NE FUSELAGE GOUGED B K NONE O OTHER ININSP/MAINT 1 SO15312FL 24569 CABIN RT OB SEAT TRACK HAS NUMEROUS GOUGES STA. 540 TO 727E. S/O 109001, N/R 22858 2L72 4F4 FRTA16WE E2GL 20050614000022005061400002EU 2005 6 14 AWXA200500630 120050506A5320D53112821200 FLOOR SUPPORT AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28639AW 471 SAL - MAJOR REPAIR - DURING C08 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM -Y254 AT FR 12 TO FR 20. MAINTENANCE INSTALLED NEW FLOORBEAM -Y254 AT FR 12 TO FR 20 IAW A320 SRM 51-42-11. 2L72 4F RTA28NM 20050614000032005061400003EU 2005 6 14 AWXA200500631 120050505A5320D5348004320401 SILL AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28639AW 471 SAL - MAJOR REPAIR - DURING C08 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM SILL Y1732 AT FR 66. MAINTENANCE REPLACED FLOORBEAM SILL Y1732 AT FR 66 IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050614000052005061400005EU 2005 6 14 AWXA200500633 120050506A5320D53112818202 FLOOR SUPPORT AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28639AW 471 SAL - MAJOR REPAIR - DURING C08 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM Y254 BETWEEN FS 16 AND FS 18. MAINTENANCE REMOVED FLOORBEAM Y254 BETWEEN FS 16 AND FS 18; FABRICATED A NEW REPLACEMENT FLOORBEAM PER A320 SRM 53-11-14, PAGE 213 AND 214, FIGURE 202; INSTALLED REPAIR PART IAW A320 SRM 51-42-11. 2L72 4F RTA28NM 20050614000062005061400006EU 2005 6 14 AWXA200500634 120050505A5347D53472098000 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28639AW 471 SAL - MAJOR REPAIR - DURING C08 CHECK, GALVANIC CORROSION WAS FOUND ON FLOORBEAM DUMMY RAIL Y920 BETWEEN FS 65 AND FS 67. MAINTENANCE REMOVED DAMAGED DUMMY RAIL Y920 BETWEEN FS 65 AND FS 67; FABRICATED A NEW REPLACEMENT DUMMY RAIL PER DWG D53472040; INSTALLED REPAIR PART IAW A320 SRM 51-42-11. 2L72 4F RTA28NM 20050614000072005061400007EU 2005 6 14 AWXA200500635 120050508A5743R57248003002 NUT AIRBUS320 A320232 3930326EU RT MLG CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28639AW 471 SAL - LANDING GEAR - DURING C08 CHECK, CORROSION WAS FOUND ON THE RETAINING NUT FOR THE FWD PINTLE BEARING ON THE RT MAIN LANDING GEAR. MAINTENANCE REMOVED AND REPLACED RETAINING NUT IAW A320 SRM 57-26-13. 2L72 4F RTA28NM 20050614000102005061400010EU 2005 6 14 AWXA200500638 120050506A5310D53471124201 SHEAR PLATE AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28639AW 471 DURING C08 CHECK, GALVANIC CORROSION WAS FOUND AT SHEAR PLATE Y1200 BETWEEN FS 69 TO FS 70. MAINTENANCE REMOVED AND REPLACED SHEAR PLATE Y1200 BETWEEN FS 69 TO FS 70 IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050614000112005061400011EU 2005 6 14 AWXA200500639 120050506A5310D53480020697 SHEAR PLATE AIRBUS320 A320232 3930326EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28639AW 471 DURING C08 CHECK, A CRACK WAS FOUND AT SHEAR PLATE -Y1300 BETWEEN FS 68 TO FS 69. MAINTENANCE REMOVED AND REPLACED SHEAR PLATE -Y1300 BETWEEN FS 68 TO FS 69 IAW A320 SRM 51-42-11, PAGE 7. 2L72 4F RTA28NM 20050614000122005061400012EU 2005 6 14 AWXA200500640 120050505A5310D5348002069601 SHEAR PLATE AIRBUS320 A320232 3930326EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28639AW 471 DURING C08 CHECK, A CRACK WAS FOUND AT SHEAR PLATE Y1300 BETWEEN FS 68 TO FS 69. MAINTENANCE REMOVED AND REPLACED SHEAR PLATE Y1300 BETWEEN FS 68 TO FS 69 IAW A320 SRM 51-42-11, PAGE 7 AND A320 SRM 51-72-11. 2L72 4F RTA28NM 20050614000132005061400013NM 2005 6 14 AWXA200500641 120050528A3150 WARNING LIGHT BOEING737 7373S3 1384711NM COCKPIT FALSE ACTIVATIONA AWXAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 WP28315AW 23734 FLT 440 - ON TAKEOFF ROLL AT LAS EN ROUTE TO IAH, A LOW SPEED ABORTED TAKEOFF OCCURRED DUE TO A REPORT OF A TAKEOFF CONFIGURATION WARNING HORN SOUNDED AT THROTTLE ADVANCEMENT. MAINTENANCE PERFORMED A TAKEOFF SYSTEM WARNING TEST IAW AWA TASKCARD NR A1B31009. NO FAULTS FOUND. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050614000152005061400015NM 2005 6 14 P5CA0501358 120050518A5310 STRUCTURE BOEING747 747230B 1384889NM NLG WW CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 EA15508MC 21644 NOSE GEAR WHEEL BOX STRUCTURE FOUND SEVERAL CRACKS AT STATION 320L BETWEEN WL 140 AND 150, AT STATION 300R BETWEEN WL 170 AND 180, AT STATION 300L AT WL 175. ACCOMPLISHED INTERIM REPAIR PER BOEING INSTRUCTIONS SEP-SIN-05-00574C AND 1-1HZQME AND FAA FORM 8100-9. 2L74 4F A20WE 20050614000172005061400017SO 2005 6 14 CHQA200500105 120050530A3350MS25231316 BULB EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT BURNED OUT A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11832RP 145676 MAIN AIRSTAIR DOOR EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED MAIN DOOR STAIRS EMERGENCY LIGHT BULB IAW EMB 135 AMM 33-50-10. OPS CHECK GOOD. 2L72 4F RTT00011AT 20050614000182005061400018SO 2005 6 14 CHQA200500106 120050531A33501316 BULB EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT BURNED OUT A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11837RP 145715 MAIN AIRSTAIR DOOR EMERGENCY LIGHT ON RAILING IS INOP. REMOVED AND REPLACED LAMP ASSEMBLY ON RAILING IAW EMB 135 AMM 33-50-10. OPS CHECK GOOD. 2L72 4F RTT00011AT 20050614000242005061400024EA 2005 6 14 VTZA200500094 120050529A5320601R311719 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27660BR 7519 INTERCOSTAL CRACKED AT .250 INCH IN LENGTH ON RT OUTBOARD SIDE AT 484 LEFT BETWEEN BL 36.00. 2L72 4F RTA21EA 20050614000252005061400025EA 2005 6 14 VTZA200500095 120050529A5320601R35031239 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27660BR 7519 RT FS 621 FLOOR SUPPORT IS CRACKED AT 1 INCH. 2L72 4F RTA21EA 20050614000282005061400028SO 2005 6 14 C2XA05SD021 120050526A335066903 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714907 145468 SDF - FWD CABIN FLOOR EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED FWD CABIN FLOOR EMERGENCY LIGHT. OPS CHECK GOOD, AIRCRAFT RELEASED AND RETURNED TO SERVICE. 2L72 4T RTT00011AT 20050614000292005061400029SO 2005 6 14 C2XA05CL041 120050528A335078241 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714950 145061 CLE - THE CREW REPORTED THE EMERGENCY EXIT SIGN ON THE FORWARD WIND SCREEN WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 3 INVERTER. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20050614000312005061400031SO 2005 6 14 C2XA05BT034 120050531A3350110049 CHARGER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT FAULTY A C2XAO OTHER O OTHER NRNOT REPORTED 1 SW2726545 145558 CREW REPORTED WING FUSELAGE FRONT FAIRING AND NR 1 AISLE PATH EMERGENCY LIGHTS ARE NOT WORKING. MAINTENANCE REMOVED AND REPLACED NR 1 EMERGENCY LIGHT BATTERY CHARGER IAW EMB145 AMM 33-50-04. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050614000342005061400034NM 2005 6 14 05FDEA00696 120050329A5347ADA73492 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 MAIN DECK, AT STA 889 LBL 75.25 SEAT TRACK CROWN FOUND CORRODED. MAIN DECK, STA 869 TO STA 909 LBL 75.25 CORROSION SEAT TRACK REMOVED AND REPAIRED AS PER SRM 53-70-00 VOL II. REPAIR SEAT TRACK AND SPLICE FABRICATED AS PER SRM 53-70-00 VOL II FIG 1. CLASSIFIED AS MAJOR REPAIR PER GMM 6-1-100. 2L73 4F RTA22WE 20050614000402005061400040NM 2005 6 14 AALA20050362 120050526A5245 DOOR BOEING767 767323 1385205NM LT A/C PACK INFLT SEPARATIONA AALAA UNSCHED LANDING DE INFLIGHT SEPARATION VIBRATION/BUFFET CLCLIMB 1 SW217375A 25202 WHILE CLIMBING THROUGH 11000 FEET A LOUD BANG AND AIRCRAFT SHUDDER WAS HEARD AND FELT IN AIRFRAME. VIBRATIONS AND RUMBLE COULD BE FELT IN AIRFRAME. POST FLIGHT REVEALED LEFT PACK DOOR HAD DEPARTED AIRCRAFT. LEFT PACK DOOR REPLACED AND STRUCTURE REPAIRED PER BILL OF WORK DATED 26MAY2005 AT AFW. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050614000412005061400041NM 2005 6 14 AALA20050366 120050530A3350BPS73 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21661AA 25295 JFK - ON APPROACH, THE EMERGENCY EXIT LIGHTS ILLUMINATED AND THEN EXTINGUISHED ON TOUCHDOWN. REPLACED BATTERY PACK M10798 FOR EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050614000432005061400043EU 2005 6 14 AALA20050368 120050531A3350P4010051124 BATTERY PACK AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217055A 462 JFK - DURING B CHECK, FOUND SEAT MOUNTED EMERGENCY LIGHTS ON RIGHT AFT CABIN FROM ROWS 28 BACK INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS ON RIGHT AFT CABIN FROM ROWS 28 BACK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20050614000452005061400045WP 2005 6 14 AALA20050363 120050527A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2133502 49739 SAT OVERHEAD EMERGENCY LIGHTS AT ROW 20 AND BACK INOPERATIVE. REPLACED BATTERY PACK AND BATTERIES FOR OVERHEAD EMERGENCY LIGHTS AT ROW 20 AND BACK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050614000472005061400047WP 2005 6 14 AALA20050364 120050527A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21412AA 49323 DTW - EMERGENCY LIGHTS IN AFT AIR STAIR COMPARTMENT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN AFT AIR STAIR COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050614000482005061400048NM 2005 6 14 QXEA200500959 120050518A5753 FLAP TRACK BOMBDRDHC8 DHC8402 1390042NM ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09412QX 4059 PDX - LEFTHAND NR 4 FLAP TRACK FORWARD MOUNT POINT HOLES HAVE SUSPECTED CORROSION. REPAIRED IAW HORIZON AIR EA 6-57-346 AND RD 8/4-57-479. 2H72 4T RTA13NM 20050614000512005061400051EU 2005 6 14 TRBA2005031 120050504A2841749760 INDICATOR AEROSPATR72 ATR72212A 8680902EU PWA PW120 PW127 NE COCKPIT INTERMITTENT A TRBAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO29538AT 538 WHILE IN CRUISE, RT FUEL GAUGE READING DROPPED QUICKLY, SHOWING 600 POUNDS OF FUEL IMPALANCE. AIRCRAFT DIVERTED FOR MAINTENANCE. REPLACED RT FUEL QUANTITY INDICATOR. (K) 2H72 4T4 TRTA53EU E20NE 20050614000532005061400053SO 2005 6 14 O2G2005F00009 120050511A31101159CAV3731007 CONTROL PANEL GULSTMG1159 GIV 3980115SO RROYCETAY TAY6108 NE COCKPIT FAILED E O2GAO OTHER G MULTIPLE FAILURE TOTAKEOFF 1 NE03624BP336 1093 EPMP PANEL BLANK WITH POWER APPLIED. REMOVED AND REPLACED EPMP PANEL. (K) 2L72 4F4 FRTA12EA E25NE 20050614000542005061400054WP 2005 6 14 ASAA0580145 120050228A53219957918524 FLOORBOARD DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02975AS 53451 C-CHECK, CABIN FLOOR PANEL HAT SECTION IS CRACKED. REPLACED HAT SECTION. (K) 2L72 4F4 FRTA6WE E9NE 20050614000562005061400056WP 2005 6 14 ASAA0580147 120050228A5320SR09520089 SPACER DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE DOOR BEAM CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02975AS 53451 C-CHECK - AFT CARGO BAY DOOR BEAM SPACER IS CORRODED. REPLACED SPACER. (K) 2L72 4F4 FRTA6WE E9NE 20050614000572005061400057WP 2005 6 14 ASAA0580148 120050228A5320993053573 CUSP WEB DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02975AS 53451 C-CHECK - FWD CARGO BAY CUSP WEB ABOVE DOOR HINGE INS PUNCTURED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER. (K) 2L72 4F4 FRTA6WE E9NE 20050614000602005061400060EA 2005 6 14 SWIA200515067 120050527A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07979SW 7954 BOTH RED LIGHTS ON OVERHEAD EXIT SIGN INOPERATIVE. RELAMPED BOTH RED LIGHTS AT OVERHEAD EXIT SIGN. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050614000612005061400061EA 2005 6 14 SWIA200515068 120050529A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07957SW 7829 LEFT FORWARD OVERWING EMERGENCY LIGHT INOP. REPLACED BULB OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050614000642005061400064EA 2005 6 14 SWIA200515071 120050527A33502013BR BATTERY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCHARGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07594SW2836 2836 7285 RIGHT SIDE GALLEY EXIT LIGHT INOPERATIVE. REPLACED NR 1 ELBP IAW MM 33-51-04. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050614000662005061400066EA 2005 6 14 SWIA200515073 120050525A271010231007 DAMPER CNDAIRCL600 CL6002B19 1900309EA AILERON MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07943SW5635 5635 7762 CREW REPORTS FLUTTER DMAPER STATUS MSG INFLIGHT. REPLACED FLUTTER DAMPER ON RIGHT HAND AILERON IAW MM CHAPTER 27-15-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050614000682005061400068EA 2005 6 14 SWIA200515075 120050527A2740 SWITCH CNDAIRCL600 CL6002B19 1900309EA TRIM SYSTEM STICKING A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07435SW 7555 F/O'S TRIM SWITCH IS STICKING. REPLACED F/O'S TRIM SWITCH IAW MM 27-41-05. 2L72 4F RTA21EA 20050614000702005061400070EA 2005 6 14 SWIA200515077 120050529A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07910SW 7566 FFOD LEFT SPOILERON SPOILERONS FAULT MESSAGE. REPLACED LEFT SPOILERON O/B PCU IAW CRJ MM 27-62-01. OPERATIONAL CHECK GOOD. P/N: 27000-7, S/N OFF: 2450. 2L72 4F RTA21EA 20050614000752005061400075EA 2005 6 14 SWIA200515082 120050526A5610 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAO OTHER O OTHER CRCRUISE 1 NM07439SW 7578 RT WINDSHIELD CRACKED EN ROUTE. REPLACED RIGHT WINDSHIELD IN ACCORDANCE WITH 56-11-00, 56-11-01, 56-12-01. P/N OFF 601R33033-14, S/N OFF 01173H1516. 2L72 4F RTA21EA 20050614000762005061400076EA 2005 6 14 SWIA200515083 120050531A274070609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07465SW1127 1127 7845 MACH TRIM CAUTION AND STAB TRIM CHANNEL 2 STATUS MESSAGES DISPLAYED IN FLIGHT. REPLACED HSTCU IAW MM 27-41-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050614000812005061400081 2005 6 14 P5CA0501359 420050519A22102593362927 CONTROL PANEL BOEING747 747341 13848AMNM AUTOPILOT SYS INOPERATIVE A P5CAK NONE O OTHER ININSP/MAINT 1 EA15355MC 23395 ON PRE-FLIGHT CREW REPORTS UNABLE TO ENGAGE EITHER -A- OR -B- AUTOPILOT. REPLACED P10 MODE CONTROL PANEL. OPS NORMAL PER MM 22-11-06. 2L74 4F RTA20WE 20050614000822005061400082NM 2005 6 14 USAA050581 120050504A5320 INTERCOSTAL BOEING737 737400 138449ANM FUSELAGE DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US 24781 CLT - FOUND INTERCOSTAL PREVIOUSLY REPAIRED DAMAGE UNKNOWN, FUSELAGE NOSE SECTION STATION 312 TO 328 RBL 11.5. MAJOR REPAIR REMOVED INTERCOSTAL AND INSTALLED NEW INTERCOSTAL IAW SRM 53-60-04 FIG 201. (M) 2L72 4F RTA16WE 20050614000832005061400083NM 2005 6 14 USAA050582 120050504A5311 FRAME BOEING737 7374B7 1384702NM FUSELAGE DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US 24781 CLT - FRAME HAS PREVIOUSLY REPAIRED DAMAGE UNKNOWN, STATION 787 BETWEEN STRINGER 8R AND 9R. REPAIRED PER SRM 53-00-01 FIG 202. (M) 2L72 4F RTA16WE 20050609001592005060900159WP 2005 6 9 DHL2005801009 120050526A3260 SWITCH DOUG DC8 DC873F 302199FWP MLG DOOR OUT OF ADJUST A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01801DH 46033 AFTER TAKEOFF UPON GEAR RETRACTION, THE RED DOORS NOT LATCHED LIGHT AND THE RIGHT DOOR UNSAFE LIGHT ILLUMINATED WITH THE GEAR HANDLE UP. BOTH LIGHTS EXTINGUISHED AFTER 10 SECONDS. ADJUSTED RIGHT MAIN GEAR DOOR SWITCH. PERFORMED OPERATIONS CK SYSTEM, OP CHECK GOOD IAW MM 33-31-5. 2L74 4F RT4A25 20050609001632005060900163NM 2005 6 9 05FDEA00657 120050328A5512ALC8100XXX PANEL DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 LEFT HORIZONTAL STABILIZER UPPER BARREL NUT NR 19 HAS BORE CORROSION EXCEEDING LIMITS. BARREL NUT BORE NR 19 LT REPAIRED IAW EA 1-5510-78133 ATTACHMENT 2, HORIZONTAL STABILIZER BARREL NUT BORE REWORK/ REPAIR AD 2003-22-08. MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050609001692005060900169NM 2005 6 9 05FDEA00717 120050331A5512ALC8100XXX PANEL DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 RIGHT HORIZONTAL STABILIZER UPPER BARREL NUT NR 20 HAS BORE CORROSION EXCEEDING LIMITS. BARREL NUT BORE NR 20 RT REPAIRED IAW EA 1-5510-78133 ATTACHMENT 16, HORIZONTAL STABILIZER BARREL NUT BORE REWORK/ REPAIR AD 2003-22-08. MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050609001752005060900175WP 2005 6 9 P9RA20050083 120050520A3260 PROXIMITY SWITCH DOUG DC9 DC983 3022083WP MLG DOOR DIRTY A P9RAO OTHER N FALSE WARNING CLCLIMB 1 SO11989PG 49845 GEAR DOOR OPEN LIGHT ILLUMINATED INTERMITTENTLY DURING CLIMB AND INITIAL CRUISE. PERFORMED LUBE SERVICE TO LT AND RT MAIN GEAR DOORS, ROLLERS AND ACTUATORS. CLEANED PROXIMITY SWITCHES AND TARGETS AS REQUIRED. OPERATED DOORS SEVERAL TIMES WITH NORMAL INDICATIONS IAW M/M. NO PART REPLACEMENT. 2L72 4F RTA6WE 20050609001772005060900177NM 2005 6 9 05FDEA00774 120050331A5512ALC8100XXX PANEL DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 LEFT HORIZONTAL STABILIZER UPPER BARREL NUT NR 31 HAS BORE CORROSION EXCEEDING LIMITS. BARREL NUT BORE NR 31 LT REPAIRED IAW EA 1-5510-78133 ATTACHMENT 08, HORIZONTAL STABILIZER BARREL NUT BORE REWORK/ REPAIR AD 2003-22-08. MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050609001782005060900178NM 2005 6 9 05FDEA00775 120050331A5512ALC8100XXX PANEL DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 LEFT HORIZONTAL STABILIZER UPPER BARREL NUT NR 33 HAS BORE CORROSION EXCEEDING LIMITS. BARREL NUT BORE NR 33 LEFT REPAIRED IAW EA 1-5510-78133 ATTACHMENT 09, HORIZONTAL STABILIZER BARREL NUT BORE REWORK/ REPAIR AD 2003-22-08. MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050609001852005060900185NM 2005 6 9 05FDEA01461 120050525A5340 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 STRINGER CLIP CRACKED AT BS 825 STR 7R. *S/D* REPLACED STRINGER CLIP PER SRM 51-30-2. 2L73 4F RTA3WE 20050609001872005060900187 2005 6 9 KBM2005F00063 420050405A310025791161 VOLTMETER SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE COCKPIT STICKS E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19115SH 3141 VOLTMETER, NEEDLE STICKS. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050609001912005060900191EU 2005 6 9 KBM2005F00067 120050508A21210500847 MOTOR SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE BLOWER FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P1001 2347 7 INCH BLOWER MOTOR, INDUCES CIRCUIT BREAKER FAILURE. REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20050609001932005060900193SW 2005 6 9 KBM2005F00070 120050516A770012444412 GAUGE BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL TOT STUCK E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19188TV 2704 TOT GAUGE, STUCK AT TOP WHEN POWER SWITCH IS TURNED ON, DOES NOT FUNCTION PROPERLY. REMOVED AND REPLACED. (K) 1G71 3U3 U H2SW E4CE 20050610000102005061000010SO 2005 6 10 O2G2005F00007 120050301A78301159CP4081 SOLENOID GULSTMG1159 GIV 3980115SO RROYCETAY TAY6118 EU LT ENG T/R LOCK FAILED E O2GAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NE03195WS 1050 LT THRUST REVERSER WOULD NOT STOW AFTER GROUND CHECK BEFORE TAKEOFF. REPLACED SECONDARY LOCK SOLENOID ACTUATOR. (K) 2L72 4F4 FRTA12EA E25NE 20050610000162005061000016NM 2005 6 10 05FDEA01497 120050531A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 UPPER CARGO COMPARTMENT, SEAT TRACK AT STA 1269 TO STA 1381, X= - 27 FOUND WITH CORROSION. 27 REMOVED AND REPLACED AT EXISTING SPLICES PER SRM 53-70-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED MAJOR GMM 6-2-100. 2L73 4F RTA22WE 20050610000202005061000020NM 2005 6 10 05FDEA01516 120050603A5310651627910 BEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 CORROSION ON LONGITUDIONAL BEAM BS 740 - 840 RBL 45. REPLACED LONGITUDINAL BEAM PER SRM 51-30-2. 2L73 4F RTA3WE 20050610000222005061000022CE 2005 6 10 DJFA2005102 120050529A215073838426 ACM CESSNA500 560CESSNA 2076750CE ODOR E DJFAG O2 MASK DEPLOYED BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 EA23501CW 2649 5600050 AFTER TAKE OFF THE CREW REPORTED AN ODOR OF SULFUR IN THE CABIN. AT 2,000 AGL THE EMERGENCY PRESSURIZATION SYSTEM ENGAGED, AND CREW DONNED THEIR OXYGEN MASKS. THE AIRCRAFT RETURNED TO KLEX AND AN EMERGENCY EVACUATION OF THE AIRCRAFT WAS PERFORMED ON THE TAXIWAY. MAINTENANCE ISSUED MEL 21-1 FOR THE AIR CYCLE MACHINE. THE AIRCRAFT IS TO BE OPERATED WITHOUT PRESSURIZATION UNDER THE MEL. ON 06 JUNE 2005, MAINTENANCE REPLACED THE ACM, HEAT EXCHANGER, AND COALESCER FILTER. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA22CE 20050610000362005061000036EU 2005 6 10 DHL2005366001 120050605A261230903827 SQUIB AIRBUS300 A300B4203 3930306EU APU BAY FAILED A DHLAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO01366DH 249 APU FIRE WARNING, COMPLETED APU FIRE EMERGENCY CKLIST. INSPECTED APU, NO EVIDENCE OF FIRE WAS FOUND. FALSE ALARM. TRANSFERED EXT SYS TO DMI LOG PER MEL 26-22-06 CAT C AS DMI NR 21158. APU IS NOT TO BE USED. PLACARD INSTALLED. REF DMI 21156 APU WARNING COMPLETED APU FIRE EMERGENCY CK LIST (APU NOT TO BE USED DO TO FIRE EXTING. INOP. REPLACED FIRE BOTTLE SQIB IAW 26-23-12. OPS CK GOOD. THIS CLEARS DMI 21156. PLACARD REMOVED PN 30903827. 2L72 4F RTA35EU 20050610000372005061000037EU 2005 6 10 MALA050438 120050413A5411 STRINGER BAC 146 AVRO146RJ85A1500097EU NOSE COWL CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15503XJ E2310 DURING C2 INSPECTION, FOUND 1 CRACKED STRINGER NR 2 ENGINE ON BULKHEAD AFT OF NOSE COWL. 2H74 4F RTA49EU 20050610000392005061000039EU 2005 6 10 MALA050442 120050413A5411 STRINGER BAC 146 AVRO146RJ85A1500097EU NOSE COWL CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15503XJ E2310 DURING C2 INSPECTION, FOUND 1 CRACKED STRINGER NR 2 ENGINE ON BULKHEAD AFT OF NOSE COWL. 2H74 4F RTA49EU 20050610000412005061000041EU 2005 6 10 MALA050444 120050413A5411 STRINGER BAC 146 AVRO146RJ85A1500097EU NOSE COWL CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15503XJ E2310 DURING C2 INSPECTION, FOUND 1 CRACKED STRINGER NR 2 ENGINE ON BULKHEAD AFT OF NOSE COWL. 2H74 4F RTA49EU 20050610000432005061000043NM 2005 6 10 AWXA200500610 120050525A3233D23613000 ACTUATOR AIRBUSA319 A319132 3930340NM MLG BYPASSING A AWXAO OTHER J WARNING INDICATION CLCLIMB 1 WP28803AW 931 FLT 605 EN ROUTE TO DEN PILOT REPORTED THE NOSE LANDING GEAR WAS SLOW TO RETRACT AT APPROXIMATELY 20 SECONDS ECAM MESSAGE LANDING GEAR NOT UPLOCKED AND LANDING GEAR DOORS NOT CLOSED. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR ACTUATING CYLINDER PER AIRBUS AMM 32-31-22-04. MAINTENANCE SWUNG THE GEAR PER AWA TASKCARD F4N32301. SUBMITTED FOR INFORMATIONAL PURPOSES. TEAR DOWN REPORT SHOWS THAT THE UNIT'S OPERATIONAL TEST WAS NORMAL IN SHOP. NO FAULTS WERE FOUND. UNIT WAS OVERHAULED AND TESTED IAW MESSIER DOWTY CMM 32-37-12 REV. 2. 2L72 4F RTA28NM 20050610000442005061000044NM 2005 6 10 AWXA200500611 120050502A534069285552 ATTACH ANGLE BOEING737 7373B7 1384580NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28332AW 23384 MCN - MAJOR REPAIR - DURING C-18 CHECK, A CRACK WAS FOUND AT A LOWER DOOR STOP FITTING ATTACH ANGLE, THAT WAS LOCATED AT BS 349, STRINGER 16L. MAINTENANCE REMOVED, FABRICATED AND REPLACED LOWER DOOR STOP FITTING ATTACH ANGLE IAW AMERICA WEST AIRLINES ENGINEERING REPAIR 03-5300-05135-SS1. 2L72 4F RTA16WE 20050610000462005061000046NM 2005 6 10 AWXA200500613 120050502A33501703661 SOCKET BOEING737 7373G7 1384595NM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28322AW 25400 DURING C-14 CHECK, EPLS HARNESS LOCATED BETWEEN BS 360 AND BS 947, WAS FOUND TO HAVE DAMAGE TO CONNECTORS AND WIRE SPLICES . MAINTENANCE REMOVED AND REPLACED DAMAGED CONNECTORS AND WIRE SPLICES FOR EPLS HARNESS IAW BSWPM 20-42-01, BSWPM 20-90-14, AND BSWPM 20-30-12. OPERATIONAL CHECK WAS COMPLIED WITH IAW TASK CARD NR A1C33006. SOCKET PN 170366-1, WIRE SPLICE PN 0436-37, PIN PN 3402202. 2L72 4F4 FRTA16WE E2GL 20050610000472005061000047CE 2005 6 10 HSY2005F00001 120050114A7933 SENSOR BEECH 1900 1900 1154160CE PWA PT6 PT6A65B 52043EA OIL TEMP DEFECTIVE E HSYAO OTHER N FALSE WARNING CRCRUISE 1 NM057254R UB22 (MRR NR 01-011405) LOSS OF NR 1 ENGINE OIL PRESSURE. LOOSE AND LEAKING OIL TEMPERATURE SENSOR. LOOSE BUT IN SERVICEABLE CONDITION. REMOVED TEMPERATURE SENSOR, INSPECTED, AND REINSTALLED. RAN ENGINE AND FOUND NO FURTHER DEFECTS. (NM05200502782) (K) 2L72 4T4 TRTA24CE E4EA 20050610000482005061000048CE 2005 6 10 HSY2005F00002 120050124A29101013880175 HOSE BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA HYDRAULIC SYS LEAKING E HSYAO OTHER K FLUID LOSS NRNOT REPORTED 1 NM05122GL UC122 (MRR NR 02-012405) LOSS OF HYDRAULIC PRESSURE AND QUANTITY LED TO THE INABILITY TO OPERATE THE LANDING GEAR WITH NORMAL PROCEDURES. LANDING GEAR HAD TO BE EXTENDED MANUALLY WITH THE HAND PUMP. NOTE: THIS WAS A PILOT TRAINING FLIGHT ONLY. FAILED LANDING GEAR HYDRAULIC SYSTEM HOSE. REMOVED AND REPLACED HYDRAULIC HOSE. (NM05200502790) (K) 2L72 4T4 TRTA24CE E4EA 20050610000502005061000050NE 2005 6 10 KNK2005F00000 220050510A72000292005220 ENGINE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE MALFUNCTIONED E KNKAO OTHER O OTHER NRNOT REPORTED 1 WP13112AK7001 3254 9644 ENGINE WOULD NOT ROTATE FOR ENGINE DAILY RINSE. TRIED TO TURN COMPRESSOR AND IT WAS VERY HARD TO TURN. REMOVED N6 ACCY TO CHECK FOR POSSIBLE CAUSE AND COMPRESSOR WAS STILL TIGHT. BORE SCORED COMBUSTION CHAMBER AND 1ST STAGE BLADES AND FOUND NO ABNORMALLIES. SUSPECTED COKING PROBLEM ON FUEL NOZZLE. (K) 1G71 3U3 U H9EU E19EU 20050610000512005061000051GL 2005 6 10 ALG2005F00026 220050512A7261 ENGINE BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL MAKING METAL E ALGAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW03198H 3647 CAE835206 DURING TAKEOFF, ENGINE CHIP LIGHT ILLUMINATED SO AC RETURNED TO BASE. MAINTENANCE CLEANED AND INSPECTED BOTH PLUGS, FOUND 2 SMALL SLIVERS ON THE LOWER PLUG. INSPECTED BOTH FILTERS FOUND OK, DRAINED AND RESERVICED OIL TANK. COMPLIED WITH A 30 MINUTE GROUND RUN, NO OTHER DEFECTS NOTED. (K) 1G71 3U3 U H2SW E4CE 20050613000232005061300023NM 2005 6 13 SWAA051528 120050524A53146545866 KEELBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29353SW 24889 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE KEELBEAM CORRODED AT BS 500D TO BS 540, STR 28L. REPAIRED KEELBEAM PER SRM. 2L72 4F RTA16WE 20050613000252005061300025NM 2005 6 13 SWAA051530 120050524A33509250071 BULB BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29458WN 33857 EEPLS INOP AT FWD END. RELAMPED PER MM. 2L72 4F RTA16WE 20050613000262005061300026NM 2005 6 13 SWAA051531 120050524A3350101114 BULB BOEING737 7377H4 1384404NM EMERGENCY EXIT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29499WN 32481 DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM. 2L72 4F RTA16WE 20050613000332005061300033NM 2005 6 13 SWAA051546 120050525A55236959227 BUSHING BOEING737 7373H4 1384600NM RT ELEVATOR TAB WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29627SW 27935 DURING SCHEDULED C3 CHECK, RT ELEVATOR TAB FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED NR 1 HINGE BUSHING & HARDWARE PER MM. 2L72 4F RTA16WE 20050613000352005061300035NM 2005 6 13 SWAA051552 120050525A53116546541 FRAME BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 1, STR 2L & STR 2R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050613000392005061300039NM 2005 6 13 SWAA051556 120050525A5313BAC1498 STRINGER BOEING737 737301 1384611NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 351 TO BS 370, STR 22L. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2L72 4F RTA16WE 20050613000452005061300045CE 2005 6 13 71037 120050526A3240 BRAKE BEECH 1900 1900D 1154162CE MLG MALFUNCTIONED A AMWAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE07176YV UE176 ON TAXI TO GATE BRAKES WERE SPONGY. MAINTENANCE COULD NOT DUPLICATE THE DISCREPANCY. THEREFORE NO PARTS WERE USED. 2L72 4T RTA24CE 20050613000622005061300062EA 2005 6 13 VTZA200500089 120050526A5712601R102328 RIB CNDAIRCL600 CL6002B19 1900309EA RT WING CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27659BR 7509 RT BATT RIB IS CRACKED .750 INCH BETWEEN ATTACHING FASTENERS. 2L72 4F RTA21EA 20050613000722005061300072EU 2005 6 13 MALA050450 120050525A5260 AIRSTAIR TRACK BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15506XJ E2314 DURING C2 INSPECTION, FOUND BOTH AIRSTAIR FLOOR RAILS CORRODED. 2H74 4F RTA49EU 20050613000752005061300075EU 2005 6 13 MALA050452 120050525A5753 FLAP TRACK BAC 146 AVRO146RJ85A1500097EU RT TE FLAP WORN A MALAK NONE O OTHER ININSP/MAINT 1 GL15506XJ E2314 DURING C1 INSPECTION, FOUND RIGHT FLAP TAB LEADING EDGE WITH WEAR MARKS BEYOND LIMITS UNDER PANEL 641EB 2H74 4F RTA49EU 20050613000982005061300098GL 2005 6 13 RAIA00505018 220050519A7230 ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 1 DAMAGED A RAIAA UNSCHED LANDING O OTHER CRCRUISE 1 CE03814HK 145046 311524 FA HEARD LOUD NOISE FROM AFT OF AIRCRAFT, INSPECTION REVEALED HOLE IN FAN COWL OF NR 1 ENGINE. MAINTENANCE INSPECTION IDENTIFIED FAN SPINNER MISSING AND HOLES IN COWL, REMOVED AND REPLACED NR 1 ENGINE. 2L72 4T4 FRTT00011ATTE6CH 20050613001042005061300104EU 2005 6 13 RTAIA00505024 120050526A6120 SWITCH JETAIRJETSTMJETSTM4101 1500501EU CONDITION LEVER OUT OF ALIGNMENTA RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03565HK 41082 TAKEOFF CONFIGURATION WARNING INDICATION. MAINTENANCE ADJUSTED CONDITION LEVER SWITCHES. 2L72 4T RTA41NM 20050613001062005061300106NM 2005 6 13 SWAA051560 120050526A3350101114 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29609SW 27929 EMERGENCY EXIT LIGHT LENS MISSING NEXT TO FWD F/A'S SEAT. INSTALLED LENS ASSY PER MM. 2L72 4F RTA16WE 20050613001682005061300168NM 2005 6 13 UPS05444537 120050519A5347 SEAT TRACK BOEING747 747123F NM PWA JT9 JT9D7A 52054NE FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE: C M/D - BS 782 RBL 33 SEAT TRACK IB FLANGE COR. CORROSION BLEND OUT 0.022 INCH X 0.5 INCH X 0.5 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. M/D - RBL 33 INCH SEAT TRACK REPAIRED IAW SRM 53-10-05 FIG 1A BTN BS 770-810. 2L74 4F4 F A20WE E20EA 20050613001702005061300170NM 2005 6 13 UPS05444539 120050518A5313 STRINGER BOEING747 747123F NM PWA JT9 JT9D7A 52054NE FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE: C FWD CARGO BS 960-980 STR 47R FOUND CORRODED AS MARKED. CORROSION BLEND OUT 0.075 INCH X .7500 INCH X 1.75 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT, FWD CARGO COMPT - BS 970-980 STR 47R STRINGER REPAIRED IAW SRM 53-10-03 FIG 1. 2L74 4F4 F A20WE E20EA 20050613001722005061300172NM 2005 6 13 UPS05444541 120050516A532069B620491 PLATE BOEING747 747123F NM PWA JT9 JT9D7A 52054NE FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C M/D BS 1100 RBL 75 TIE DOWN FTG ATT PLATE FOUND CORRODED. CORROSION BLEND OUT 0.028 INCH X 1.5 INCH X 3 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT, M/D BS 1100 RBL 75 INCH TIE DOWN FTG ATT PLATE REPLACED IAW SRM 51-10-01 PG 9. 2L74 4F4 F A20WE E20EA 20050613001822005061300182NM 2005 6 13 DHL2005741524 120050421A5313BAC1498143 STRINGER BOEING727 7272Q9 138448MNM FUSLEAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 STR 27R FUSELAGE STA 700 CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGED SECTION OF STRINGER SIZE 17" IAW B727 SRM 53-10-3 FIG. FABBED STR FROM BAC1498-143 SIZE 17" PO NR 5096198 AND SPLICE FROM BAC1498-132 SIZE 10" PO NR 4246286 IAW B727 53-10-3 FIG 1. TREATED AND PRIMED PARTS AND AREA IAW B727 SRM 51-10-2 AND INSTALLED STR SECTION AND SPLICE IAW B727 SRM 53-10-3 FIG 1 AND 51-30-2. 2L73 4F RTA3WE 20050613001842005061300184NM 2005 6 13 P5CA0501352 120050518A5210 STIFFENER BOEING747 747230B 1384889NM NR 4 DOOR CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 EA15508MC 21644 NR 4R DOOR INTERNAL STIFFENER JUST FORWARD OF WINDOW CUT-OUT FOUND CRACKED. ACCOMPLISHED REPAIR PER BOEING 1-1I26OS AND FAA FORM 8100-3. 2L74 4F A20WE 20050613001862005061300186NM 2005 6 13 P5CA0501354 120050518A5414 SKIN BOEING747 747230B 1384889NM NR 2 PYLON WORN A P5CAK NONE O OTHER ININSP/MAINT 1 EA15508MC 21644 NR 2 PYLON INBOARD ACCESS PANEL CUTOUT AT NAC STATION 280-300 WORN AT EDGE. ACCOMPLISHED REPAIR PER BOEING INSTRUCTIONS 1-1IO8DO AND FAA FORM 8100-3. 2L74 4F A20WE 20050613001882005061300188NM 2005 6 13 P5CA0501356 120050518A5312 BULKHEAD BOEING747 747230B 1384889NM FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 EA15508MC 21644 BS 1241 LEFT SIDE CANTED BULKHEAD HAS CRACK IN WEB AREA ABOVE BULKHEAD FITTING. ACCOMPLISHED REPAIR PER BOEING INSTRUCTIONS 1-1I9Y5F AND FAA FORM 8100-9. 2L74 4F A20WE 20050613001902005061300190NM 2005 6 13 AWXA200500618 120050504A531165465415001 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28322AW 25400 DURING C-14 CHECK, FRAME AT BS 663.75 WAS FOUND CRACKED AT STRINGERS 1 LT, 2 LT, AND 3 LT. MAINTENANCE REPAIRED FRAME AT BS 663.75, AT STRINGERS 1 LT, 2 LT, AND 3 LT IAW B737-300 SRM 53-00-07-2, FIGURE 209. 2L72 4F RTA16WE 20050613001922005061300192EU 2005 6 13 AWXA200500620 120050505A5347D5347217220290 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28639AW 471 DURING C08 CHECK, GALVANIC CORROSION WAS FOUND ON SEAT TRACK BEAM Y1292 BETWEEN FS 64 TO FS 67. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK BEAM Y1292 BETWEEN FS 64 TO FS 67; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050614000192005061400019WP 2005 6 14 DJFA2005101 220050527A726130751604 ENGINE RAYTHNDH125 HAWKER800XP 7150012CE GARRTTTFE731TFE7315BR WP LEFT LEAKING E DJFAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 EA23847CW501 258647 P107916 CREW REPORTED THAT DURING CLIMBOUT, THE LEFT ENGINE OIL PRESSURE BEGAN TO DROP. AS AIRCRAFT CLIMBED, THE OIL PRESSURE MOVED INTO THE YELLOW ARC. AN EMERGENCY WAS DECLARED AND AIRCRAFT RETURNED TO KPBI WITHOUT FURTHER INCIDENT. MAINTENANCE DISCOVERED THAT THE LEFT ENGINE OUTBOARD OIL CAP WAS NOT SECURED AND WAS FOUND WITHIN THE COWLING. THE LEFT ENGINE OIL WAS SERVICED WITH 3 QUARTS OF OIL AND THE OIL CAP WAS RESECURED. THE CHIP DETECTOR WAS INSPECTED WITH NO NOTED DEBRIS. THE ENGINE WAS GROUND RUN WITH NO NOTED DISCREPANCIES AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA3EU E6WE 20050614000222005061400022EA 2005 6 14 VTZA200500092 120050529A5320601R3117117 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27660BR 7519 INTERCOSTAL CRACKED AT .250 INCH IN LENGTH ON LT OUTBOARD SIDE AT FS 484 BL 36.00. 2L72 4F RTA21EA 20050614000322005061400032SO 2005 6 14 C2XA05TY045 120050524A3350110049 CHARGER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT FAILED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714558 145598 SDF, DURING A SCHEDULED ROUTINE CHECK THE AFT FUSELAGE EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 BATTERY CHARGER, OPERATIONAL CHECKED GOOD IAW EMB-145 MM 33-50-04. 2L72 4T RTT00011AT 20050614000372005061400037NM 2005 6 14 DHL2005741525 120050422A5310 WEB BOEING727 7272Q9 138448MNM DOOR FRAME CHAFED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH46665 21931 REMAIN CARGO DOOR , CUTOUT FRAME CHAFED AT FWD BOTTOM CORNER AT BS 480L. CLEANED AREA FOUND MAJOR DAMAGED AND IS OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 1. REMOVED SKIN SIDE GUIDE AND WEDGE IAW B727 SRM 51-30-2 FIG 7. LOCATED TRIMMED AND DRILLED INNER WEB AND SIDE GUIDE AT BS 480 IAW AEI STC CHAPTER 52, PG 52, FIG 5211 AND CHAPTER 25 PAGE 60 FIG 2517. TREATED AND PRIMED NEW PARTS IAW B727 SRM 51-10-2. INSTALLED INNER WEB SKIN AE 727-1032A-17 PO NR 509681 WEDGE AE5083-12 PO NR 509681 AND SIDE GUIDE AE4109-11 PO NR 509681 IAW AEI CHAPTER 52 PAGE 52, FIG 5211 AND CHAPTER 25 PAGE 60 FIG 2517. 2L73 4F RTA3WE 20050614000502005061400050EU 2005 6 14 TRBA2005033 120050512A261251315125 WIRE HARNESS AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FIRE DETECT SYS BURNED A TRBAA UNSCHED LANDING N FALSE WARNING APAPPROACH 1 SO29448AM 448 ON APPROACH INTO EIS, RT ENGINE FIRE INDICATION ILLUMINATED. ENGINE SHUTDOWN AND INDICATION DISAPPEARED. NO EMERGENCY DECLARED NEITHER EXTINGUISHER DISCHARGED. REPLACED ENGINE ELECTRIC HARNESS. (K) 2H72 4T4 TRTA53EU E20NE 20050614000552005061400055WP 2005 6 14 ASAA0580146 120050228A53219957918524 FLOORBOARD DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE CRACKED E ASAAK NONE O OTHER ININSP/MAINT 1 NM02975AS 53451 C-CHECK - CABIN FLOOR PANEL HAT SECTION IS CRACKED. REPLACED HAT SECTION. (K) 2L72 4F4 FRTA6WE E9NE 20050614000652005061400065 2005 6 14 SWIA200515072 420050527A34183995100208 COMPUTER CNDAIRCL600 CL6002B19 1900309EA STALL WARNING MALFUNCTIONED A SWIAO OTHER N FALSE WARNING CLCLIMB 1 NM07588SW 7069 STALL FAIL MSG AFTER TAKEOFF. REPLACED STALL PROTECTION UNIT IAW 27-34-00. OPERATIONAL CHECK GOOD. P/N: 3995100208, S/N OFF: 338. 2L72 4F RTA21EA 20050614000722005061400072EA 2005 6 14 SWIA200515079 120050527A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07710BR9386 9386 7852 FLIGHT SPOILERS FAULT STATUS MESSAGE. REPLACED RIGHT FLIGHT SPOILER OUTBOARD PCU PER MM 27-62-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050614000842005061400084NM 2005 6 14 USAA050584 120050501A5320 ANGLE BOEING737 7374B7 1384702NM FUSELAGE DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US 24781 CLT - FOUND ANGLE BRACKET WITH PREVIOUSLY REPAIRED DAMAGE UNKNOWN, STATION 500G, S28R. MAJOR REPAIR INSTALL NEW BRACKET IAW SRM 51-10-02. (M) 2L72 4F RTA16WE 20050614000862005061400086NM 2005 6 14 USAA050586 120050501A5347 SEAT TRACK BOEING737 7374B7 1384702NM FUSLEAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US 24781 CLT - FOUND SEAT TRACK CRACKED .500 INCH, LOWER RADIUS BELOW FLOOR, RBL 24.5, STATION 727B. REMOVED DAMAGED SECTION, SPLICED IN NEW SECTION IAW 53-00-52, EA 96533. (M) 2L72 4F RTA16WE 20050614000882005061400088NM 2005 6 14 USAA050588 120050501A5347 SEAT TRACK BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US 24781 CLT - FOUND SEAT TRACK CRACKED IN LOWER RADIUS OF SEAT TRACK, STATION 727B, RBL 45.5. SPLICED IN NEW SECTION OF SEAT TRACK. (M) 2L72 4F RTA16WE 20050614000902005061400090NM 2005 6 14 USAA050590 120050505A5730 SKIN BOEING737 7374B7 1384702NM WING CRACKED A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19439US 24781 CLT - FOUND WING SKIN CRACKED 1 INCH, LOWER WING SKIN AT STATION 135.72 JUST ABOVE THE OUTBOARD PYLON FUSE PIN. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER IAW 57-41-02. (M) 2L72 4F RTA16WE 20050614000942005061400094NM 2005 6 14 USAA050594 120050505A5754 WEDGE BOEING737 7374B7 1384702NM NR 5 SLAT DEBONDED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US39931 24781 CLT - FOUND SLAT WEDGE DISBOND 4 INCHES BY 4 INCHES, OUTBOARD END OF UPPER AND LOWER SKIN OF NR 5 SLAT. SDA COMPLETE ACCOMPLISHED COMPOSITE REPAIR IAW 57-42-04. (M) 2L72 4F RTA16WE 20050614000962005061400096NM 2005 6 14 USAA050599 120050507A5340 STRINGER CLIP BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19439US 24781 CLT - FOUND TIE CLIP CRACKED .5 INCH, STATION 747 STRINGER 24R. REPLACED TIE CLIP IAW SRM 51-40-02. (M) 2L72 4F RTA16WE 20050614000972005061400097NM 2005 6 14 USAA050600 120050509A5347 SEAT TRACK BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19439US 24781 CLT - FOUND SEAT TRACK CRACKED 1 INCH, BS 747 AND STRINGER 26R. SDA COMPLETED REPAIRED PER 737-4 SRM 53-00-53 AND 53-60-53. (M) 2L72 4F RTA16WE 20050614000992005061400099NM 2005 6 14 USAA050562 120050428A5414 SKIN BOEING737 7374B7 1384702NM NR 1 PYLON CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US 24781 CLT - FOUND SKIN CRACKED .500 INCH, NR 1 PYLON, INBOARD SIDE, AFT ACCESS PANEL 5724 CUTOUT, LOWER AFT CORNER. INSTALLED DOUBLER IAW TR 54-50-07. (M) 2L72 4F RTA16WE 20050614001012005061400101NM 2005 6 14 USAA050560 120050428A5311 FRAME BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19439US 24781 CLT - FOUND FRAME CRACKED 1 INCH BS 500 FRAME RBL 1. CUT OUT CRACKED AREA OF FRAME. FABRICATED AND INSTALLED REPAIR IAW SRM 51-70-11. (M) 2L72 4F RTA16WE 20050614001032005061400103SO 2005 6 14 CHQA200500107 120050601A2497 CONTACTOR EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL ELECTRICAL BURNED A CHQAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL11380SK 145613 ON CLIMB OUT OF STL THROUGH ACCELERATION ALTITUDE, THE FLIGHT CREW NOTICED A SLIGHT BURNING SMELL IN THE COCKPIT AREA. THE FLIGHT ATTENDANT REPORTED IT SMELLED A LITTLE LIKE SOMETHING IS BURNING IN THE FRONT OF THE CABIN. AN EMERGENCY WAS DECLARED AND A REQUEST TO RETURN AND TO HAVE EMERGENCY EQUIPMENT STANDING BY WAS MADE. BY NOW THE SMELL WAS EVEN STRONGER. THE FLIGHT RETURNED TO THE FIELD AND LANDED UNEVENTFULLY. MAINTENANCE TROUBLESHOT THE ELECTRICAL ODOR TO BURNED CONTACTORS KO081 AND KO293. REMOVED AND REPLACED SAID CONTACTORS IAW EMB 140 MM 24-34-00. OPS CHECK GOOD. NO ODOR NOTED. 2L72 4F4 FRTT00011ATTE6CH 20050614001502005061400150NM 2005 6 14 SWAA051637 120050602A335065C27093 LIGHT BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29646SW 28331 L1 DOOR EMERGENCY EXIT LOWER LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20050614001512005061400151NM 2005 6 14 SWAA051638 120050602A53116516301 FRAME BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 188, LEFT SIDE, WL 208. REPAIRED STUB FRAME PER SRM. 2L72 4F RTA16WE 20050614001522005061400152NM 2005 6 14 SWAA051639 120050602A53106546833 FLOOR PANEL BOEING737 737301 1384611NM COCKPIT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND 2 EA FUSELAGE FLOOR WEB CRACKS AT BS 188 TO BS 196, LEFT & RIGHT SIDE, WL 208. REMOVED AND REPLACED WEB SECTIONS PER SRM. 2L72 4F RTA16WE 20050614001532005061400153 2005 6 14 SWAA051640 420050602A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29701GS 27836 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050614001542005061400154 2005 6 14 SWAA051641 420050602A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29715SW 27849 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050614001572005061400157NM 2005 6 14 SWAA051623 120050601A53126546568 BULKHEAD BOEING737 7377H4 1384404NM AFT CABIN CANNING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29757LV 29850 DURING SCHEDULED HC2 CHECK, FOUND BS 1016 AFT PRESS BULKHEAD OIL CANNED AT STR 2L. REPAIRED AFT PRESS BULKHEAD PER SWA EA. 2L72 4F RTA16WE 20050614001582005061400158NM 2005 6 14 SWAA051612 120050601A53306545857 BEAR STRAP BOEING737 7373H4 1384600NM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29353SW 24889 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN BEAR STRAP CORRODED AT BS 767, STR 25R TO STR 26R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050614001592005061400159NM 2005 6 14 SWAA051613 120050601A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29353SW 24889 DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE CORRODED AT BS 847, STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SWA EA. 2L72 4F RTA16WE 20050614001612005061400161NM 2005 6 14 SWAA051615 120050601A291065C26839 LINE BOEING737 7373H4 1384600NM B-HYD SYS LEAKING A SWAAA UNSCHED LANDING K FLUID LOSS NRNOT REPORTED 1 SW29387SW 26602 AIR TURNBACK. LOST B-SYSTEM HYDRAULIC FLUID. REMOVED AND REPLACED HYDRAULIC LINE FROM B-SYSTEM MODULE TO B-SYSTEM HYDRAULIC ACCOUSTIC FILTER PER MM. 2L72 4F RTA16WE 20050614001632005061400163NM 2005 6 14 SWAA051618 120050601A532269353656 SHEAR TIE BOEING737 737301 1384611NM E & E BAY CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 360, STR 27L TO STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050614001642005061400164NM 2005 6 14 SWAA051619 120050601A53126546568551 STRINGER BOEING737 737301 1384611NM AFT PRESS BLKHD CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND BS 1016 AFT PRESS BULKHEAD RADIAL STRINGER CRACKED AT 8 O'CLOCK POSITION. REPAIRED RADIAL STRINGER PER SRM. 2L72 4F RTA16WE 20050615000392005061500039 2005 6 15 SWAA051605 420050531A256563550 SLIDE BOEING737 7377H4 1384404NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29494WN 33868 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050615000412005061500041NM 2005 6 15 SWAA051607 120050531A5313BAC1498 STRINGER BOEING737 737301 1384611NM E & E BAY CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 363, STR 25R. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2L72 4F RTA16WE 20050615000432005061500043NM 2005 6 15 SWAA051609 120050531A57546573714 WEDGE BOEING737 737301 1384611NM NR 4 SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND NR 4 L/E SLAT UPPER INBOARD T/E WEDGE DELAMINATED. REMOVED AND REPLACED NR 4 SLAT PER MM. 2L72 4F RTA16WE 20050615000452005061500045 2005 6 15 SWAA051611 420050531A2565D31354 SLIDE BOEING737 7373G7 1384595NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29690SW 23783 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050615000472005061500047 2005 6 15 SWAA051670 420050606A256565C16820 HOOK BOEING737 7377H4 1384404NM L1 GIRT BAR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29795SW 30606 L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED HOOK PER MM. 2L72 4F RTA16WE 20050615000492005061500049NM 2005 6 15 SWAA051672 120050606A53306545765 SKIN BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED FROM BS 517 TO BS 519, STR 12R. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050118000082005011800008WP 2005 1 18 05FDEA00058 120050108A2780 CONTROL UNIT DOUG MD10 MD1010F 3022112WP SLATS MALFUNCTIONED A FDEAO OTHER N FALSE WARNING APAPPROACH 1 SO25372FE 46610 ON FINAL RECEIVED SLAT DISAGREE ALERT, WENT AROUND. BEGAN QRH PROCEDURE. RECOVERED LANDING SLAT, ELECTED TO LEAVE A/C CONFIGURED, UNEVENTFUL APPROACH AND LANDING. CYCLED C/B D-8 AUTO SLAT EXTEND AND E-8 AUTO SLAT EXTEND CONTROL PERFORMED R-T-S FCC-1 AND FCC-2 NO FAULT DISPLAYED OPERATED SLATS/FLAPS SEVERAL TIMES. ALERT CLEARED DID NOT RETURN. OPS CHECK NORMAL PER SMP. AIRCRAFT OK FOR SERVICE. 2L73 4F RTA22WE 20050118000352005011800035NM 2005 1 18 SWAA050046 120050107A3350610478 BATTERY BOEING737 7372H4 138448CNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29083SW 22732 DURING SCHEDULED A2 CHECK, FOUND CENTER AISLE OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F A16WE 20050118000412005011800041NM 2005 1 18 05FDEA00006 120050103A5754 SKIN DOUG MD11 MD11 3023602NM ZONE 500 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 LT WING, NR 2 SLAT EXTERIOR, FOUND 2EA DOUBLER REPAIR AND 1EA CUTOUT REPAIR. REMOVED AND REPLACED AS PER AMM 27-80-20 AND FUNCTIONAL CHECK CARRIED OUT AS PER AMM 27-80-00, FOUND SATISFACTORY. 2L73 4F RTA22WE 20050118000432005011800043NM 2005 1 18 DXTA200500522 120050109A2710 AILERON AMD FALC50FALCON2000 2730170NM LOCKED E DXTAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 GL07224QS 124 AFTER T/O FLAP RETRACTION AILERON LOCKED, VERY HARD TO MOVE. NO FLAP ASYMMETRY LIGHT. PITCH OK, PERFORMED NO FLAP LANDING AT LAX. ITEM IS UNDER INVESTIGATION. 2K73 4F RTA50NM 20050118000462005011800046SO 2005 1 18 C2XA05TY002 120050104A553314521904401 HINGE EMB 145 EMB145LR 3260212SO VERTICAL STAB WORN A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714953 145071 DURING A 4C INSPECTION THE RT AND LT VERTICAL STABLIZER SPHERICAL BEARING HOUSINGS WERE FOUND WORN. MAINTENANCE REAM AND INSTALL NEW BUSHINGS IAW EC5510-01107. 2L72 4T RTT00011AT 20050118000522005011800052NM 2005 1 18 MWEA05005 120050104A33506011779 BATTERY PACK BOEING717 717200 1383700NM EMERGENCY LIGHT INOPERATIVE A MWEAK NONE O OTHER ININSP/MAINT 1 GL31912ME 55175 LEFT AND RIGHT EXTERNAL EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY POWER SUPPLY. 2L72 4F TRA6WE 20050118000542005011800054WP 2005 1 18 MWEA050002 120050104A531199115056 FRAME DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31805ME 48031 APPARENT CRACK LOCATED AT STATION 83.550 OUTBOARD RIGHT, 10 INCHES FROM THE CENTER LINE 4. FABRICATED AND INSTALLED REPAIR ANGLE. 2L72 4F A6WE 20050118000652005011800065NM 2005 1 18 QXEA200500060 120050110A242011520924 GCU BOMBDRDHC8 DHC8401 1390041NM ZONE 100 INOPERATIVE A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09413QX7520 4060 MFR - NR 1 AC GENERATOR CAUTION LIGHT ILLUMINATED UNABLE TO RESET PER ABNORMAL CHECKLIST. MAINTENANCE REMOVED AND REPLACED NR 1 AC GCU AND GENERATOR. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050118000702005011800070EA 2005 1 18 QXEA200500056 120050110A5210 DOOR CNDAIRCL600 CL6002C10 1390015EA MAIN PAX DIRTY A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX7365 10031 THE MAIN CABIN DOOR IS DIFFICULT TO OPEN FROM THE OUTSIDE. MAINTENANCE INSPECTED THE DOOR AND CLEANED THE SAME. THE DOOR WAS ALSO LUBED. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20050118000762005011800076NM 2005 1 18 SWAA050054 120050110A52306546921230 STOP FITTING BOEING737 7373H4 1384600NM CARGO DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29384SW 26590 DURING SCHEDULED C1 CHECK, FOUND FWD CARGO DOOR LOWER AFT DOOR STOP FITTING CUTOUT CRACKED. REMOVED AND REPLACED DOOR PER MM. 2L72 4F RTA16WE 20050118000832005011800083SO 2005 1 18 C2XA05IA010 120050106A2150C1431234 DUAL VALVE EMB 145 EMB145LR 3260212SO NR 1 A/C PACK INOPERATIVE A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW27139642229 2229 145123 EWR - CREW REPORTED THAT THE NR 1 PACK WAS BLOWING ONLY WARM AIR IN AUTO & MANUAL MODES WITH MINIMAL AIRFLOW, AND A BURNING SMELL AT LOW POWER SETTINGS. THE AIRCRAFT WAS RELEASED ON MEL 21-51-00-1 CONTROL NR 048227. FLIGHT 3138 IAH MAINTENANCE REMOVED AND REPLACED THE NR 1 PACK DUAL VALVE, OPERATIONALLY CHECKED WITH NO DEFECTS. REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050118000842005011800084NM 2005 1 18 05FDEA00084 120050112A5754 SKIN DOUG MD11 MD11 3023602NM NR 5 SLAT WARPED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25384FE 46617 LEFT WING, NR 5 SLAT LEADING EDGE SURFACE IS EXCESSIVELY WARPED THE ENTIRE WIDTH DUE TO TOO MUCH HEAT. LT WING NR 5 SLAT REMOVED AND REPLACED. 2L73 4F RTA22WE 20050118000872005011800087NM 2005 1 18 SWAA050056 120050110A534365C10300 FITTING BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29358SW 26595 DURING SCHEDULED RON, FOUND NLG ACTUATOR UPPER ATTACH FITTING GUSSET HAS A CRACK AT RADIUS. REMOVED AND REPLACED NLG GUSSET FITTING PER SRM. 2L72 4F RTA16WE 20050118001342005011800134NM 2005 1 18 05FDEA00017 120050104A5312 BULKHEAD BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25286FE 22623 1183 BULKHEAD REPAIR. COMPLIED WITH EA 7531055423 REPAIRED HOLE IN 1183 BULKHEAD. 2L73 4F RTA3WE 20050118001352005011800135NM 2005 1 18 05FDEA00018 120050104A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25286FE 22623 STRINGER 22L IS CORRODED AT STA 1180. REPAIRED STRINGER 22L IAW SRM 53-10-3 PG 48 DETAIL 1. 2L73 4F RTA3WE 20050118001362005011800136NM 2005 1 18 05FDEA00019 120050104A5754 RIB BOEING727 727100 1384036NM NR 5 SLAT CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25151FE 19147 SECOND INBOARD RIB IS CRACKED IN LEADING EDGE OF NR 5 SLAT. REMOVED AND REPLACED RIB IAW SRM 51-10-1. 2L73 4F RTA3WE 20050118001382005011800138SO 2005 1 18 C2XA05IA002 120050104A3350W763805320 WIRE EMB 145 EMB145 3260210SO EMERGENCY LIGHT LOOSE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714959 145091 CRP - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHT ON THE BULKHEAD NEAR THE MAIN PAX DOOR WAS INOPERATIVE. MAINTENANCE RESECURED A LOOSE WIRE ON THE LIGHT ASSY, OPS CHECKED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. PART HAS NO SERIAL NUMBER. 2L72 4F RTT00011AT 20050118001422005011800142NE 2005 1 18 05FDEA00023 220050105A7261 ENGINE AIRBUS300 A300F4605R 3930327EU GE CF6 CF680 30025NE NR 2 LEAKING A FDEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO25654FE 738 705246 APPROACHING LEVEL OFF AT FL330 THE NR 2 OIL QUANTITY ON BOTH THE DIAL AND ECAM WAS 4 GALLONS. OVER THE NEXT TWO MINUTES BOTH INDICATORS DROPPED SLOWLY TO ZERO (WITH ENGINE ADVISORY). THEN THE OIL PRESSURE ON THE NR 2 ENGINE DROPPED FROM 36 TO 24 PSI AND STARTED TO FLUCTUATE. ATB TO MEM. AT 8000 FT BOTH THE OIL QUANTITY AND PRESSURE BEGAN TO RETURN TO NORMAL. ON FINAL APPROACH BOTH HAD RETURNED TO NORMAL. 2L72 4F4 FRTA35EU E13NE 20050118001512005011800151CE 2005 1 18 DXTA200500511 120050103A3240991205050 MASTER CYLINDER CESSNA560 560XL 2076702CE BRAKES MALFUNCTIONED E DXTAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07604QS31 5605204 LEFT BRAKE PEDAL ON LEFT SIDE GOES ALL THE WAY DOWN WHEN BRAKES APPLIED. TROUBLESHOT LEFT BRAKE TO MASTER CYLINDER. REMOVED AND REPLACED PILOT'S LT WHEEL BRAKE MASTER CYLINDER WITH A SERVICEABLE INSPECTED BRAKE MASTER CYLINDER IAW ESSNA 560XL MM CHAPTER 32-42-02. BLED BRAKE SYSTEM IAW CESSNA 560XL MAINTENANCE MANUAL CHAPTER 32-42-00. LEAK AND OPERATIONAL CHECKS SATISFACTORY. 2L72 4F RTA22CE 20050118001522005011800152CE 2005 1 18 DXTA200500508 120050103A5210 SEAL CESSNA500 560CESSNA 2076750CE DOOR MALFUNCTIONED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07315QS 5600315 ON TAKEOFF HEARD A POPING NOISE FOLLOWED BY A DOOR SEAL LIGHT AND CABIN DOOR LIGHT. INSPECTED DOOR SEAL AS REQUIRED. PURGED SERVICE AIR SYSTEM AND DOOR SEAL WITH N2 EVACUATING ALL MOISTURE AS REQUIRED. OPS AND LEAK CHECK GOOD. ALL WORK PERFORMED IAW CE-560 MM CHAPTER 21-31-00. 2L72 4F RTA22CE 20050118001532005011800153CE 2005 1 18 DXTA200400510 120050103A3260652750115 ATTACH ANGLE CESSNA500 560CESSNA 2076750CE MLG OUT OF ALIGNMENTE DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07367QS 5600367 RED GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. EXTENDED GEAR AND CYCLED GEAR THREE GREEN, NO RED WHEN LOWERED. FOUND LT MLG DOOR ANGLE HITTING GEARBOX IN UP POSITION, NOT ALLOWING LT MLG TO GO INTO UPLOCK POSITION. FITTED NEW 6527501-15 ANGLE NR 6527501-20 SPLICE PLATE PER CESSNA EEDS DNG 6527501. INSTALLED FASTENERS IAW CESSNA 500 SERIES SRM CH 51-30-03, GEAR SWING OPS CHECK GOOD IAW CESSNA 560 MM CH 32-01-00 (LANDING GEAR FUNCTIONAL TEST) CLEARANCE CHECK GOOD. 2L72 4F RTA22CE 20050118001542005011800154CE 2005 1 18 DXTA200500512 120050103A2916 RESERVOIR CESSNA560 560XL 2076702CE HYD SYSTEM LOW E DXTAO OTHER WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 GL07631QS 5605131 LANDING GEAR WOULD NOT RETRACT. INSPECTED SYSTEM PER M/M 32-30-00, RAN GEAR UP & DOWN SEVERAL TIME NO DEFECTS NOTED, OPS CHECK GOOD. SERVICED HYD RESERVOIR. 2L72 4F RTA22CE 20050118001552005011800155NM 2005 1 18 05FDEA00024 120050106A5310 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25235FE 21329 BS 1148 CORROSION ON SHEAR TIE AND SKIN BS 1148 BETWEEN STRINGERS 28R & 29R. REMOVED CORROSION SHEAR TIE FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 REPAIRED PER SRM 53-10-04. 2L73 4F RTA3WE 20050118001572005011800157NM 2005 1 18 C1HA200574001 120050103A213132167421 MIXING VALVE BOEING727 727225 1384077NM A/C PACK FAILED A C1HAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15674MG 21450 RT PACK MIXING VALVE WOULD NOT MOVE AFTER DEPARTURE. UPON CLIMBOUT TO ALTITUDE STARTED TO LOSE PRESSURIZATION, LT PACK WOULD NOT HOLD PRESSURIZATION AND THEN GOT A DUCT OVERHEAT ON BOTH SIDE. LOST ALL PRESSURIZATION COM 2.21.2 COMPLY WITH ATC NOTIFIED. EMERGENCY DECLARED, RETURNED TO SLC. SWAPPED FWD PACK VALVE PROBLEM SWAPPED TO LT SIDE PLACED ON MEL 21-2-1 CONTROL NR C-06804 CAT C LT PACK VALVE INOP PER MEL 21-2-1 NEED TO PLACARD LT PACK INOP MEL 21-1-1 CAT C CONTROL NR C06805 REF M/M 21-55-71. REPACKED OXYGEN MASK REF M/M 35-21-00. REMOVED AND REPLACED LT PACK VALVE, OPS CHECKED GOOD REF 21-55-71 AND MM 05-51-101. 2L73 4F A3WE 20050118001582005011800158SO 2005 1 18 C2XA05BT002 120050103A335078241 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT FAILED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716919 145393 EWR - PILOT REPORTED OVERHEAD EMERGENCY EXIT LIGHT OVER ROW 12 OUT. MAINTENANCE REMOVED AND REPLACED NR 3 INVERTER IAW EMB 145 MM 33-50-11. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050118001592005011800159SO 2005 1 18 C2XA05IA007 120050106A33501317 LAMP EMB 145 EMB145ER 3260211SO GALLEY BURNED OUT A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714939 145030 IAH - CREW REPORTED THAT THE EMERGENCY EXIT LIGHT ON THE SERVICE DOOR WAS INOPERATIVE. MAINTENENCE RELAMPED THE AFFECTED LIGHT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THIS PART HAS NO S/N AND TIMES ARE NOT TRACKED. 2L72 4F RTT00011AT 20050118001602005011800160SO 2005 1 18 C2XA05IA008 120050106A335066367 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713964 145123 DURING MAINTENANCE INSPECTION, ONE AISLE PATH EMERGENCY LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THIS PART HAS NO S/N AND TIMES ARE NOT TRACKED. 2L72 4T RTT00011AT 20050118001612005011800161SO 2005 1 18 C2XA05IA009 120050106A335074441 LIGHT EMB 145 EMB145ER 3260211SO GALLEY INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714939 145030 CRP - MAINTENANCE REPORTED THAT THE EMERGENCY LIGHT OVER THE SERVICE DOOR WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THIS PART HAS NO S/N AND TIMES ARE NOT TRACKED. 2L72 4F RTT00011AT 20050118001642005011800164WP 2005 1 18 MWEA050006 120050106A55229937804501 DOUBLER DOUG DC9 DC981 3022081WP ELEVATOR DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31805ME 48031 DAMAGE ON LEFT ELEVATOR SKIN, BOTTOM SIDE 24 INCHES FROM INBOARD END, APPROXIMATELY MID-CHORD. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20050118001662005011800166SO 2005 1 18 SWIA200514341 120050101A2797 WIRE EMB 120 EMB120ER 3260203SO FLAP CONNECTOR CHAFED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07189SW 120048 AFTER SELECTING FLAPS 15, CONTROL FAULT LIGHT ILLUMINATED. REPAIRED CHAFED WIRES AT RIGHT OUTBOARD FLAP ACTUATOR CONNECTOR. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050118001692005011800169EA 2005 1 18 SWIA200514344 120050104A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLT SPOILERS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07589SW1393 1393 7072 ON TAXI OUT, RECEIVED SPOILERONS FAULT STATUS MESSAGE. REMOVED AND REPLACED LEFT SPOILERON INBOARD PCU IAW AMM 27-62-01. OPERATIONAL CHECKS GOOD. 2L72 4F RTA21EA 20050118001702005011800170EA 2005 1 18 SWIA200514345 120050104A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CRCRUISE 1 NM07916SW6969 6969 7634 EN ROUTE STAB TRIM CH 2 AND MACH TRIM CAME ON. REMOVED AND REPLACED HSTA IAW CRJ 200 MM 27-42-01 AND HSTCU IAW CRJ 200 MM 27-42-05. OPERATIONAL CHECK GOOD. P/N 7062-3, S/N OFF 1104. 2L72 4F RTA21EA 20050118001712005011800171SO 2005 1 18 SWIA200514346 120050101A3350 LAMP EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM0716731 120190 EMERGENCY LIGHT ABOVE 3BC IN CENTER AISLE CEILING IS INOPERATIVE. RELAMPED CENTER AISLE CEILING EMERGENCY LIGHT ABOVE 3BC WITH SERVICEABLE BULB. REF AMM 33-00-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050118001762005011800176SO 2005 1 18 LR7A05002 120050106A5230 SKIN LKHEED382 382G 526414USO CARGO DOOR DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC10 4698 DURING SCHEDULED A CHECK PER JOB CARD HA1200 FOUND HOLE IN SKIN AT FS 898, WL 200, BL 53R. REPAIRED CARGO DOOR SKIN PER SRM 51-140 PG 38-39 FIG 51-140-12. 2H74 4T A1SO 20050118001772005011800177NM 2005 1 18 05FDEA00041 120050106A5347ACA74141 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 MAIN DECK CARGO, SEAT TRACK BETWEEN STA Y= 1341 TO Y= 1401, X= - 47.50 FOUND WORN. REPAIRED PER SRM 53-70-00 VOLUME I, FIGURE 1. 2L73 4F RTA22WE 20050118001782005011800178NM 2005 1 18 05FDEA00042 120050106A5347ACA74141 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 MAIN DECK CARGO, SEAT TRACK BETWEEN STA Y= 1501 TO Y= 5-11, X= 8.50 FOUND WORN. SPLICED AND TRIMMED PER SRM 51-33-01 VOLUME II; AND REPAIRED PER SRM 53-70- 00 VOLUME I, FIGURE 1. 2L73 4F RTA22WE 20050118001812005011800181NM 2005 1 18 05FDEA00048 120050107A5310 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25240FE 20978 REPAIR SHEAR TIE AT BS 380 BETWEEN STR 15 & 16 LT TO ACCOMPLISH 9G BARRIER MOD. 2L73 4F RTA3WE 20050118001842005011800184NM 2005 1 18 05FDEA00049 120050107A2611 FIRE LOOP BOEING727 727200 138407ENM APU BAY MALFUNCTIONED A FDEAFA ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO25216FE 22937 APU FIRE WARNING LIGHT IN HANDLE AND FIRE WARNING ON GLARESHIELD CAME ON. PULLED FIRE HANDLE, LIGHT STAYED ON. DISCHARGED APU BOTTLE, LIGHT STAYED ON. LIGHT EXTINGUISHED ON DESCENT INTO IAH 10 MIN LATER. LIGHT CONTINUED TO FLICKER IN HANDLE INTERMITTENT IN DESCENT & ON GROUND. CHECKED APU FIRE SENSOR LOOP AND SHOOK DOWN CONNECTORS ON APU. NO FAULTS NOTED. CLEANED C/P D4858P AND R421 PER WDM. REMOVED AND REPLACED APU FIRE DET OPERATION UNIT PER MM 26-15-003-4. REMOVED AND REPLACED FIRE BOTTLE PER MM 26-23-001-4. 2L73 4F RTA3WE 20050118001862005011800186WP 2005 1 18 05FDEA00051 120050107A3020 VALVE DOUG DC10 DC1030F 3023504WP ANTI ICE SYS STICKING A FDEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO25301FE 46800 DURING CRUISE, SELECTED ENGINE ANTI-ICE ON, ENGINE NR 2 ANTI-ICE WOULD NOT OPEN, RECEIVED LEVEL 1 ALERT - ENGINE NR 2 ANTI-ICE DISAGREE. CONTACTED MX VIA ACARDS, MX SUGGESTED A RESET OF C/B ON MX PANEL UPPER MX R-25. PULLED AND RESET C/B, NO CHANGE. FOUND NR 2 COWL ANTI-ICE VALVE STICKING. REPLACED VALVE PER MD-10-30 M/M 30-22-02-2. ALSO REPLACED LOW PRESSURE SWITCH S1-1046 AND HI-PRESSURE SWITCH S1-108 8 AS PRECAUTIONARY. LEAK CHECK AND OP CHECKS GOOD ON GROUND RUN PER JRH. 2L73 4F RTA22WE 20050118001882005011800188NM 2005 1 18 05FDEA00054 120050108A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 MAIN DECK, SEAT TRACK HORIZONTAL FLANGE UPPER SURFACE AT STA Y= 5-11 TO Y= 5-53, X= -75.25 FOUND FLOOR PANEL MOUNTING HOLE SHORT OF EDGE MARGIN. REPAIRED IAW SRM 53-70-00 VOLUME I, FIGURE 1. 2L73 4F RTA22WE 20050118001912005011800191NM 2005 1 18 SWAA050033 120050106A33501619 LAMP BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED PM CHECK, FOUND FWD SERVICE DOOR EMERGENCY EXTERIOR LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050118001922005011800192NM 2005 1 18 SWAA050034 120050106A52306547952524 STOP FITTING BOEING737 7373H4 1384600NM CARGO DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29336SW 23940 DURING SCHEDULED C2 CHECK, FOUND AFT CARGO DOOR LOWER AFT DOOR STOP FITTING CUTOUT CRACKED. REMOVED AND REPLACED DOOR PER MM. 2L72 4F RTA16WE 20050118001932005011800193NM 2005 1 18 SWAA050035 120050106A3350OL307IBPEGL LAMP BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29634SW 27937 DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT AT ROW 17 ABC, INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050118001942005011800194NM 2005 1 18 SWAA050036 120050106A3350OL307IBPEGL LAMP BOEING737 7373A4 1384585NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29669SW 23752 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT AT ROW 5 DEF INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050118001952005011800195NM 2005 1 18 SWAA050037 120050106A53306545767 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29678AA 23290 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 482B, STRINGER 15L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20050118001962005011800196NM 2005 1 18 SWAA050038 120050106A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29791SW 27886 DURING SCHEDULED MV2 CHECK, FOUND 2 EACH LENSES MISSING FROM EEPLS AT ROWS 12C AND 10C. REMOVED AND REPLACED LIGHT LENSES PER MM. 2L72 4F RTA16WE 20050118001972005011800197NM 2005 1 18 SWAA050041 120050106A53306545774 SKIN BOEING737 7373K2 13844BANM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29345SA 23786 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT BS 727E + 10, STRINGER 26R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050118001982005011800198NM 2005 1 18 SWAA050042 120050106A53106546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29330SW 23694 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 747, RBL 6 TO LBL 6, DAMAGED. REMOVED AND REPLACED SHEAR TIE SECTION PER SRM. 2L72 4F RTA16WE 20050118002032005011800203SO 2005 1 18 LR7A05001 120050104A3350449105 LIGHT LKHEED382 382G 526414USO CABIN FAILED A LR7AK NONE L NO TEST ININSP/MAINT 1 AL03405LC20 5025 DURING SCHEDULED A CHECK PER JOB CARD HA1200 OVERHEAD ESCAPE HATCH FLIGHT DECK EMERGENCY EXIT LIGHT WILL NOT TEST. REPLACED AND OPS CHECKED LIGHT ASSY PER SMP 581 33-50. 2H74 4T A1SO 20050118002042005011800204NM 2005 1 18 SWAA050052 120050109A335010107451 LIGHT BOEING737 7375H4 138449DNM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29515SW 25154 AFT ENTRY EMERCENCY EXIT SIGN LOOSE. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2L72 4F RTA16WE 20050119000042005011900004 2005 1 19 SWAA050043 420050107A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29646SW 28331 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050119000052005011900005NM 2005 1 19 SWAA050048 120050108A57536546430190 SKIN BOEING737 7373H4 1384600NM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29343SW 24151 DURING SCHEDULED C1 CHECK, FOUND RT WING INBOARD T/E FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM. 2L72 4F RTA16WE 20050119000072005011900007NM 2005 1 19 SWAA050050 120050108A5753654643489 SKIN BOEING737 7375H4 138449DNM TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29519SW 25318 DURING SCHEDULED A2 CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2L72 4F RTA16WE 20050119000092005011900009NE 2005 1 19 DXTA200500519 220050107A720031B489201 ENGINE BRAERO1000 BAE1251000A 1500104EU PWA 305 PW305B 52128NE NR 2 OVERHEATED E DXTAC ABORTED TAKEOFF MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 GL07533QS6529 259033 PCE305010 OVERTEMP NR 2 ENGINE ON TAKEOFF, TEMPERATURE WENT TO 797 DEGREES FOR 2 SECONDS. ABORTED TAKEOFF. ITEM IS UNDER INVESTIGATION. 2L72 4F4 FRTA3EU E35NE 20050119000102005011900010CE 2005 1 19 DXTA200500518 120050106A2170 WATER SEPARATOR CESSNA750 750 2076810CE COCKPIT ODOR E DXTAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL07979QS 7500079 THERE IS A STRONG OILY SMELL IN THE COCKPIT ONCE THE APU IS RUNNING AND THE BLEED AIR IS SELECTED ON. FOUND BOTH WATER SEPARATOR FILTER SOCKS DIRTY. CLEANED FILTER AND FOUND COCKPIT WATER SEPARATOR VALVE STUCK OPEN. CLEANED AND LUBED VALVE. RE-INSTALLED WATER SEPARATOR TO INSTALL ORIGINAL CONFIG. PERFORMED ENGINE RUN, OPS CHECKS GOOD IAW CE-750 MM 21-10-00. 2L72 4J RTT00007WI 20050119000192005011900019 2005 1 19 2005UALA00008 420050101A3436 WARNING SYSTEM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE WX RADAR SYS ACTIVATED A UALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP29375UA 24640 ABORTED TAKEOFF AT 100 KNOTS DUE TO WINDSHEAR WARNING INDICATION. OPS CHECK OF WEATHER RADAR TRANSCEIVER PERFORMED, AND NO FAULT FOUND. 2L72 4F4 FRTA16WE E2GL 20050119000232005011900023NE 2005 1 19 2005UALA00012 220050102A7230 BLADE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 1 ENGINE FAILED A UALAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION DEDESCENT 1 WP29416UA 479 AT 10,000 FT THROTTLE AT NORMAL SETTING JUST ABOVE IDLE, LOUD NOISE WAS HEARD FROM NR 1 ENGINE. EGT WENT RED AND VIBRATION INDICATION STAYED AT 6.0. REPLACED NR 1 ENGINE. TEARDOWN REVELAED A STAGE THREE BLADE FAILED IN THE DOVE TAIL AREA. THIS PROBLEM IS NOT LIMITED TO ANY ONE PART NUMBER. OEM IS DEVELOPING A NEW DESIGN C3 BLADE FOR FLEET INCORPORATION. 2L72 4F4 FRTA28NM E40NE 20050119000252005011900025NM 2005 1 19 2005UALA00015 120050101A2121 BEARING BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE COOLING FAN FAILED A UALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP29658UA 27113 FLT CREW REPORTS ELECTRICAL ODOR AND LIGHT HAZE IN COCKPIT. THE FORWARD EQUIPMENT COOLING EXHAUST FAN FAILED. SHOP FINDINGS DETERMINED BEARING FAILURE TO BE THE ROOT CAUSE. 2L72 4F4 FRTA1NM E24NE 20050119000352005011900035NM 2005 1 19 2005UALA00029 120050105A5330 SKIN BOEING777 777222 1385219NM PWA PW4077PW4077 NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29776UA 26937 CRACK INDICATIONS WERE FOUND ON SKIN IN HOLE COMMON TO WING AND BODY FAIRING FITTING ONE PLACE ON EACH SIDE AT BS 972, FASTENER HOLE NR 20 LT SIDE, AND FASTENER HOLE NR 18 RT SIDE, STRAKLET ATTACH FITTING. HOLES REPAIRED BY OVERSIZING TO REMOVE CRACK INDICATION AND INSTALLING LARGER DIAMETER FASTENERS. 2L72 4F4 FRTT0001SE E46NE 20050119000442005011900044NM 2005 1 19 DXTA200500507 120050101A52804AS2650200431 DOOR GULSTM200 200 4500308NM MLG BENT E DXTAO OTHER J WARNING INDICATION CLCLIMB 1 GL07703QS1925 060 LEFT MAIN GEAR WOULD NOT INDICATE UP, UPON GEAR RETRACTION (RED, UNKNOWN WAS SHOWING). JACKED AIRCRAFT AND ACCOMPLISHED RIGGING CHECK FOUND LT MLG I/B DOOR TO BE BENT. REMOVED AND REPLACED DOOR & RIGGED IAW G-200 MM 32-10-10. 2L72 4F RTA53NM 20050118000182005011800018NM 2005 1 18 AWXA200500017 120050109A21337110033 OUTFLOW VALVE BOEING737 737301 1384611NM ZONE 218 MALFUNCTIONED A AWXABG EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION CRCRUISE 1 WP28324AW436065797 23261 EN ROUTE EXPERIENCED CABIN PRESSURE LOSS, DONNED O2 MASKS & EXECUTED EMERGENCY DESCENT. MANUALLY DEPLOYED CABIN O2 MASKS (MASKS WERE NOT USED), STANDBY & MANUAL DID NOT WORK, TRIED AGAIN LATER AND STANDBY DID WORK. LANDED AT PHX WITHOUT FURTHER INCIDENT, EMERGENCY WAS NOT DECLARED. MX RE-STOWED MASKS AND REPLACED AFT OUTFLOW VALVE IAW BMM 21-31-11-4. PERFORMED HEATER TEST OF AFT OUTFLOW VALVE AND CABIN PRESSURE TEST, BOTH TESTS WERE GOOD. FUNCTIONAL TEST OF OUTFLOW VALVE SN 860743 CONFIRMED REASON FOR REMOVAL FOR FAILING PRETEST FINDING MOTOR AND GEARBOX ASSEMBLY INOPERATIVE AND SLUGGISH. REPLACED SERVOMOTOR AND BRAKE ASSEMBLY AND 2 EACH ANNULAR BALL BEARINGS. RETESTED UNIT IAW 21-33-00 REV. 19. 2L72 4F RTA16WE 20050118000332005011800033SO 2005 1 18 C2XA05IA004 120050105A33503025103 LIGHT EMB 145 EMB145ER 3260211SO FUSELAGE INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713929 145009 CRP - CREW REPORTED THAT THE LEFT WING EMERGENCY LIGHT WAS INOP. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT, OPS CHECKED WITH NO DEFECTS. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. NO TIMES ARE AVAILABLE ON THIS PART. 2L72 4F RTT00011AT 20050118000552005011800055WP 2005 1 18 MWEA050003 120050104A533099115055 SKIN DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31805ME 48031 APPARENT CRACK AT STATION 83.550 FRAME LEFT SIDE. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20050118000682005011800068WP 2005 1 18 0500021240 120050108A4920TSCP7004B APU DOUG DC10 DC1030 3023501WP APU BAY SMOKE A NWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL01240NW74440749 48319 DURING CLIMB, FLIGHT ATTENDANT REPORTED MULTIPLE SMOKE DETECTORS SOUNDING AND SMOKE/SMELL IN THE CABIN. FLIGHT CREW RETURNED TO DEPARTURE AIRPORT PERFORMING AN UNEVENTFUL LANDING. MAINTENANCE REPLACED THE APU. OPERATIONAL CHECK GOOD. 2L73 4F A22WE 20050118000692005011800069NM 2005 1 18 QXEA200500058 120050110A2611 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM CARGO BAY MALFUNCTIONED A QXEAO OTHER N FALSE WARNING CRCRUISE 1 NM09357PH 504 THE SMOKE WARNING CAME ON INTERMITTENTLY, ABOUT 6 TIMES, EACH TIME EXTINGUISHING AFTER ABOUT 3 SECONDS. MAINTENANCE INSPECTED THE CARGO AREA AND FOUND NO EVIDENCE OF SMOKE OR OVERHEAT. TESTS WERE PERFORMED ON THE 1 AND 2 SMOKE DETECTORS. BOTH CHECKED GOOD. THE NR 2 SMOKE DETECTOR WAS DEFERRED AS A PRECAUTION. THE AIRCRAFT WAS RETURNED TO SERVICE. SDR TO REMAIN OPEN PENDING FURTHER INFORMATION. THE SMOKE DETECTORS WERE REPLACED, OPERATIONAL CHECKS WERE GOOD, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050118001492005011800149CE 2005 1 18 DXTA200500505 120050102A2910 LINE CESSNA500 560CESSNA 2076750CE HYDRAULIC SYS LEAKING E DXTAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 GL07399QS 5600510 AFTER INITAL GEAR EXTENSION THERE WAS NO PRESSURE IN EITHER PILOT OR CO-PILOT BRAKE PEDALS, RECYCLING THE GEAR CORRECTED THE PROBLEM. NO LIGHTS ILLUMINATED AFTER NORMAL LANDING CO-PILOTS BRAKES LOST PRESSURE AND WENT TO THE FLOOR. CO-PILOTS BRAKES COULD BE PUMPED TO RESTORE BRAKE OPERATION. TROUBLESHOT SYSTEM. BLEED BRAKES, OPS CHECKED SATISFACTORY. ALL WORK IAW CESSNA 560 MM 32-40-00. 2L72 4F RTA22CE 20050118001822005011800182WP 2005 1 18 0500019885 120050105A2910 LINE DOUG DC9 DC951 3022051WP HYD SYSTEM FAILED A NWAAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 GL01401EA 47682 THE AIRCRAFT EXPERIENCED A COMPLETE LOSS OF HYDRAULIC FLUID FROM THE RT SYS AFTER THE LANDING GEAR WAS EXTENDED FOR LANDING. LANDING WAS UNEVENTFUL AT MCI BUT CFR WAS ON STANDBY. MAINTENANCE FOUND A FAILED HYDRAULIC LINE IN THE WHEEL WELL. THE LINE, RIGHT ENGINE DRIVEN PUMP, AND ELECTRIC AUXILIARY HYDRAULIC PUMP WERE ALL REPLACED. SYSTEM WAS RESERVICED AND LEAK CHECKED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050118001832005011800183NM 2005 1 18 05FDEA00040 120050106A5347ACA74141 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 MAIN DECK, SEAT TRACK BETWEEN STA Y= 1219 TO Y= 1239, X= -47.50 FOUND WORN. SPLICED AND REPAIRED PER SRM 53-70-00 VOLUME I, FIGURE 1. 2L73 4F RTA22WE 20050118001852005011800185NM 2005 1 18 05FDEA00050 120050107A5320 STIFFENER DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 FUSELAGE EXTERIOR, STIFFENER STA 1256 TO STA 1301 ON FUSELAGE SKIN FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5310-78117. 2L73 4F RTA22WE 20050118001892005011800189NM 2005 1 18 05FDEA00055 120050108A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25605FE 48514 MAIN DECK CARGO, SEAT TRACK BETWEEN STA Y= 710 TO Y= 715, X= -8.50 SCALLOP FOUND WORN. REPAIRED PER SRM 53-70-00 VOLUME I, FIGURE 1. 2L73 4F RTA22WE 20050119000422005011900042NM 2005 1 19 DXTA200400509 120050103A2120F2MA721407A1 DUCT AMD FALC50FALCON2000 2730170NM AIR DISTRIBUTIONSPLIT E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL07218QS4041 118 SMOKE SMELL & HAZE IN AFT CABIN AFTER T/O. SHUTOFF LT CABIN PAX SMOKE CLEARED. INSPECTED LT & RT TEMP SENSORS, A/C DUCTING AND AREA IN BAGGAGE UNIT, NO DEFECTS NOTED. INSPECTED FWD SERVICE COMPT, FOUND BLOWN INSULATION. FOUND DUCT SPLIT APART & MISSING INSULATION FROM INSIDE. REMOVED ALL PANELS, DUCT, VACUUMED BOTH AIR DUCTS. REINSTALLED CABIN SIDEWALLS. ALL SWITCHES AND LIGHT OPS CHECK GOOD. VERIFIED ALL DUCTING CLEANED, AND SECURED. REINSTALLED BAGGAGE COMPT FLOORING, SIDEWALLS AND CEILING PANELS. REINSTALLED ALL VANITY PANELS THAT WERE REMOVED. ALL LIGHTS AND ACCESSORIES OPS CHECK GOOD IN LAV AND BAGGAGE COMPT. SERVICEABLE DUCT WAS INSTALLED. OPS CHECK GOOD ON A/C SYSTEM. 2K73 4F RTA50NM 20050119000872005011900087EA 2005 1 19 A6WA200540007 120050102A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE GOUGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31449AW 7818 FOUND DENT/GOUGE IN LEFT SIDE AFT FUSELAGE SKIN AT FS 612, BETWEEN STRINGERS 24L AND 25L. MEASURES 2 INCH BY 1.8 INCH BY .040 INCH DEEP. PERFORMED A MAJOR REPAIR B4 CUTTING AWAY DAMAGED SKIN AND INSTALLING PN EXTERNAL DOUBLER IAW CRJ SRM 53-00-31 REPAIR NR 1. (M) 2L72 4F RTA21EA 20050120000022005012000002NM 2005 1 20 SWAA050085 120050113A53306545776 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29679AA 23291 DURING SCHEDULED C4 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS BETWEEN BS 927 AND BS 947, BETWEEN STRINGERS 21L AND 22L. REPAIRED SKIN SECTIONS PER SRM. 2L72 4F RTA16WE 20050120000042005012000004NM 2005 1 20 SWAA050069 120050111A531565C25723 BRACKET BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29365SW 26576 DURING SCHEDULED 1/4D CHECK, FOUND SUPPORT BRACKETS AT BS 616, LBL 64 AND RBL 64, CRACKED. REPAIRED BRACKETS PER SRM T1-153-018. 2L72 4F RTA16WE 20050120000052005012000005NM 2005 1 20 SWAA050099 120050116A3350OL307IBPEGL LAMP BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 DURING SPV, FOUND EMERGENCY EXIT BULLNOSE LIGHT AT ROW 6 ABC, INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050118000242005011800024NM 2005 1 18 05FDEA00063 120050111A5730 SKIN DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 RT WING, CORROSION FOUND BETWEEN XOS= 680 TO XOS= 725 UPPER SURFACE SPAR AREA. COMPLIED WITH FEDEX EA 1-5710-81591, CORROSION REMOVAL AND REPAIR. CORROSION REMOVED AT XORS STA 714 AS PER SRM 51-21-01 VOL. II FOUND WITHIN LIMITS AS PER SRM 57-10-00 FIG. 32 VOL. I. 2L73 4F RTA22WE 20050118000382005011800038NM 2005 1 18 05FDEA00045 120050107A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25605FE 48514 MAIN DECK CARGO, SEAT TRACK BETWEEN STA Y= 1841 TO Y= 1871, X= - 8.50 FOUND CORRODED. REMOVED AND REPAIRED PER SRM SRM 53-70-00 VOLUME I, FIGURE 1. 2L73 4F RTA22WE 20050118000532005011800053WP 2005 1 18 MWEA050001 120050104A531199115056 FRAME DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31805ME 48031 APPARENT CRACK AT STATION 83.550 FRAME. NR 99115056 RIGHT SIDE. FABRICATED AND INSTALLED REPAIR ANGLE. 2L72 4F A6WE 20050118000862005011800086NM 2005 1 18 SWAA050055 120050110A53306545774 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 727E, STRINGER 18R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050118001632005011800163CE 2005 1 18 DXTA200500516 120050105A3230327 BULB CESSNA560 560XL 2076702CE MLG INDICATOR INOPERATIVE E DXTAO OTHER J WARNING INDICATION APAPPROACH 1 GL07676QS 5605176 DURING LANDING CHECK WHEN SELECTING LANDING GEAR DOWN, DID NOT GET GREEN SAFE NOSE GEAR INDICATION. CHECKED ROTARY TEST AND INDICATED NOSE GEAR GREEN LIGHT INOP. PERFORMED MANUAL GEAR EXTENDED IAW CHECKLIST AND BLEW THE NOSE GEAR DOWN. TROUBLESHOT TO BAD NOSE GEAR INDICATION LIGHT BULBS. REPLACED WITH NEW BULBS. RESET BLOW DOWN N2 BOTTLE. PLACED AIRCRAFT ON JACKS. CYCLED LANDING GEAR SYSTEM SEVERAL TIMES TO BLEED HYDRAULIC SYSTEM. OPS CHECK GOOD. LEAK CHECK GOOD. WORK DONE IAW 560XL MM CHAPTER 32-01-00. SERVICED GEAR BLOW DOWN BOTTLE IAW 560 MM CHAPTER 12-12-01. 2L72 4F RTA22CE 20050118001672005011800167EA 2005 1 18 SWIA200514342 120050104A215078279015 ACM CNDAIRCL600 CL6002B19 1900309EA LEFT SMOKE A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM07437SW6346 6346 7564 DURING OPERATION OF LEFT AIR CONDITIONING PACK RECEIVED SMOKE IN COCKPIT. REPLACED LEFT AIR CYCLE MACHINE IAW MM 21-50-00, OPERATIONAL CHECKS GOOD. 2L72 4F RTA21EA 20050118001722005011800172 2005 1 18 SWIA200514347 420050102A22168220260001 MOUNT CNDAIRCL600 CL6002B19 1900309EA ELEVATOR SERVO MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED DEDESCENT 1 NM07464SW 7827 AUTOPILOT PITCH SERVO SEEMS TO HAVE ENGAGED ITSELF AFTER F/O HAD DISENGAGED IT DURING DESCENT. REMOVED AND REPLACED ELEVATOR SERVO MOUNT IAW CRJ MM 22-11-14. 2L72 4F RTA21EA 20050118001802005011800180NM 2005 1 18 05FDEA00046 120050107A5314 KEELBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25235FE 21329 BS 950A+8 RBL 8 CORROSION ON KEELBEAM. REPAIRED PER FED EX SR DRAWING NR SR27-53-023 REV A 2L73 4F RTA3WE 20050118001992005011800199EU 2005 1 18 05FDEA00061 120050110A5312 PRESSURE PANEL AIRBUS310 A310222 3930315EU NLG WW CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25422FE 346 NOSE LANDING GEAR WHEEL WELL CEILING PRESSURE WEB PNL HAS CORROSION BETWEEN FR16 AND 14B BETWEEN LBL 18 TO RBL 18 REF N00114. REMOVED CORROSION AND REPAIRED IAW EA 6-5330-55395. 2L72 4F RTA35EU 20050119000112005011900011CE 2005 1 19 DXTA200500521 120050107A3246315381 WHEEL CESSNA750 750 2076810CE MLG VIBRATION E DXTAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 GL07942QS476 7500024 EXPERIENCED EXTREME VIBRATION APPROX 60-80 KTS ON TAKEOFF ROLL. ABORTED TAKEOFF. VIBRATION WAS EXTREME ENOUGH TO DISENGAGE YAW DAMPER AND KNOCK PFD'S OFF LINE. TAKEOFF WAS IN ASPEN, NO SNOW, BUT EXTREME COLD. REMOVED AND REPLACED BOTH LEFT AND RIGHT NOSE WHEEL ASSEMBLIES IAW CESSNA 750 MM CHAPTER 32-41-01. 2L72 4J RTT00007WI 20050119000332005011900033NM 2005 1 19 2005UALA00025 120050104A5230 SEAL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CARGO DOOR LEAKING A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29312UA 23673 AIRCRAFT RETURNED WITH CABIN PRESSURE PROBLEM. SEAL REPLACED AND RIGGED THE FORWARD CARGO DOOR. 2L72 4F4 FRTA16WE E2GL 20050119000362005011900036 2005 1 19 2005UALA01298 420050101A3436 WARNING SYSTEM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE WINDSHEAR ACTIVATED A UALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP29375UA 24640 ABORTED TAKEOFF AT 100 KNOTS DUE TO WINDSHEAR WARNING INDICATION. REPLACED EMERGENCY LIGHT ON SEAT 42R. 2L72 4F4 FRTA16WE E2GL 20050119000432005011900043CE 2005 1 19 DXTA200500506 120050102A3411 PITOT LINE CESSNA750 750 2076810CE OBSTRUCTED E DXTAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 GL07961QS 7500061 ON THE T/O ROLL FGC B FAILED AND LOST THE YD AND MACH TRIM. ABORTED THE T/O AND WHEN EXITING THE RUNWAY THE SYSTEM RESET. TROUBLESHOT AND DISCONNECTED PITOT (PILOT & COPILOT), LINES CLEANED OUT WATER AND / OR DEBRIS, RECONNECTED AND PERFORMED OPS CHECK AND LEAK CHECK. CHECKS GOOD. COULD NOT DUPLICATE SQUAWK IAW CE 750 34-11-07, LEAK CHECK NORMAL IAW PART 43 APP E PARA A AS PER 91.411. 2L72 4J RTT00007WI 20050120000032005012000003NM 2005 1 20 SWAA050059 120050111A55526959227 BUSHING BOEING737 7373H4 1384600NM RT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 DURING SCHEDULED C4 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 ELEVATOR TAB BUSHING PER MM. 2L72 4F RTA16WE 20050120000062005012000006NM 2005 1 20 05FDEA00092 120050114A551165174313 RIB BOEING727 727100 1384036NM ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25107FE 19202 STABILIZER-ELEVATOR HINGE SUPPORT RIB INSPEC - S/B 727-55A0091 R1 COMPLY WITH EO 7-5510-7-5001. FOUND CRACK IN RIB AT ELEVATOR STA 50.50 DURING INSPECTION IAW EO 7-5510-5001. REMOVED AND REPLACED RIB IAW EO 7-5510-5001. 2L73 4F RTA3WE 20050120000082005012000008NM 2005 1 20 SWAA050110 120050117A53106546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29365SW 26576 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE, AFT CARGO COMPARTMENT BS 807, STRINGER 25L, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050120000112005012000011NM 2005 1 20 05FDEA00094 120050114A554265727 SKIN BOEING727 727200 138407ENM RUDDER DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25235FE 21329 SHARP CREASE ON LOWER RUDDER, LEFT HAND SIDE TOWARDS THE BOTTOM. REPLACED LOWER RUDDER PER MM 27-20-001. 2L73 4F RTA3WE 20050120000182005012000018EA 2005 1 20 COMA0570009 120050109A7830 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA THRUST REVERSER ILLUMINATED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01642CA 10125 FLIGHT 5683 LT THRUST REVERSER UNSAFE CAUTION MESSAGE. DEFERRED MAINT PER MEL. 2L72 4F RTA21EA 20050428000782005042800078CE 2005 4 28 DXTA200500668 120050409A2120 SMOKE CESSNA560 560XL 2076702CE CABIN DETECTED E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL07652QS 5605152 SMOKE AND ELECTRICAL SMELL IN CABIN AFTER T/O. EMERGENCY PRESS ON AND AIR DUCT OVERHEAT CAUTIONS LIGHTS ON. ALL CAUTION LIGHTS OUT PRIOR TO LANDING. T/S RAN ENGINE OPS CHECKED A/C ENVIRONMENTAL SYS, NO DEFECTS NOTED. CHECKED CABIN, PRESSURIZATION SYS NO DEFECTS NOTED. INSPECTED ACM AND DUCTING NO DEFECTS NOTED. CHECK TEP SENSORS, NO DEFECTS NOTED. NO FURTHER SMELL IN COCKPIT. CREW REPORTED THAT DISCREPANCY WENT AWAY BEFORE LANDING. DATA REF CE560XL M/M 21-51-00. 2L72 4F RTA22CE 20050120000192005012000019NM 2005 1 20 2005UALA00055 120050113A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29302UA 23643 STA 616 FRAME INNER CHORD IS CRACKED FROM BOTTOM FASTENER BELOW STR 17 LT. CUT-OUT DAMAGE AND INSTALLED ANGLE DOUBLER. 2L72 4F4 FRTA16WE E2GL 20050120000202005012000020NM 2005 1 20 2005UALA00056 120050113A5315 FLOORBEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29302UA 23643 STA 947 FLOORBEAM HAS MATERIAL LOSS FROM CORROSION AT LBL 4. REMOVED CORROSION INTALLED REPAIR STRAP. 2L72 4F4 FRTA16WE E2GL 20050120000232005012000023WP 2005 1 20 ABXA050014 120050105A534049125401N FITTING DOUG DC9 DC931 3022065WP FLOORBEAM CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23929AX 45874 FLOORBEAM SUPPORT UPPER END FITTING CRACKED AT BOTH BOLT HOLES FS 965 AT LEFT BUTTLINE 32. REMOVED AND REPLACED FLOORBEAM SUPPORT UPPER END FITTING IAW DC-9 SRM 51-30-1 AND DC-9 SRM 51-30-5. 2L72 4F A6WE 20050120000242005012000024WP 2005 1 20 ABXA050006 120050104A53404912515 FITTING DOUG DC9 DC931 3022065WP AFT FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23929AX 45874 CORRODED BATHTUB FITTING LONGERON 29 LEFT STA 996. REMOVED AND REPLACED FITTING AT LONGERON 29 LEFT IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20050120000262005012000026WP 2005 1 20 ABXA050008 120050104A523059101415 PAN DOUG DC9 DC931 3022065WP CARGO DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23929AX 45874 TWO CRACKS EMINATING FROM HILOC HOLE AT AFT LOWER DOOR STOP ON FORWARD LOWER CARGO DOOR. REPAIRED AREA AND REMOVED AND REPLACED BRACKET IAW DC-9 SRM 52-03, 51-30-2, 51-20-5, AND 51-30-1. 2L72 4F A6WE 20050120000302005012000030WP 2005 1 20 AALA20050014 120050109A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21982TW 53632 SFO - CEILING EMERGENCY LIGHTS AT ROWS 27 AND 29 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS FOR ROWS 27 AND 29. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050120000312005012000031NM 2005 1 20 AALA20050010 120050107A3397 WIRE BOEING767 767323 1385205NM EMERGENCY LIGHT BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW2139365 24046 SFO - CEILING EMERGENCY EXIT LIGHT AT MID GALLEY RIGHT INOPERATIVE. REPAIRED BROKEN WIRES IN FORWARD CARGO PIT CEILING FOR CEILING EMERGENCY EXIT LIGHTS AT MID GALLEY RIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050120000322005012000032NM 2005 1 20 AALA20050012 120050108A3350P4010049 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21699AN 27051 JFK - EMERGENCY LIGHT AT MID CABIN SEATS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT MID CABIN SEATS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050120000332005012000033NM 2005 1 20 AALA20050013 120050108A3350P4010049 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21699AN 27051 JFK - EMERGENCY LIGHTS AT FORWARD CABIN, MID CABIN, AND AFT CABIN INOPERATIVE. REPLACED BATTERY PACKS AT FIRST CLASS GALLEY FOR FORWARD CABIN EMERGENCY LIGHTS. REPLACED BATTERY PACK IN CEILING ABOVE SEAT 19EFG FOR MID CABIN EMERGENCY LIGHTS, AND REPLACED BATTERY PACK IN AFT GALLEY FOR AFT CABIN EMERGENY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050120000382005012000038WP 2005 1 20 ABXA050010 120050104A523059101415 PAN DOUG DC9 DC931 3022065WP CARGO DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23929AX 45874 FORWARD LOWER CARGO DOOR PAN CRACKED BETWEEN LATCH AND STOP FROM GOUGE. REPAIRED FORWARD LOWER CARGO DOOR PAN IAW DC-9 SRM 52-05. 2L72 4F A6WE 20050120000432005012000043NM 2005 1 20 AWXA200500029 120050112A335032145410 POWER SUPPLY AIRBUSA319 A319132 3930340NM ZONE 242 DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28807AW1589120 1064 LAS - EEL - DURING A-04 CHECK FOUND THE RT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RT OVERWING EMERGENCY POWER SUPPLY UNIT (12WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050120000462005012000046NE 2005 1 20 AWXA200500032 220050112A75302607MK2 ACTUATOR AIRBUSA319 A319132 3930340NM IAE V2500 V2500A1 NE NR 1 ENG VSV MALFUNCTIONED A AWXAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 WP28832AW11177 1643 ON TAKEOFF ROLL AT PDX EN ROUTE FOR PHX AT APPROXIMATELY 40 KTS RECEIVED ECAM MESSAGE ENG 1 COMPRESSOR VANE FAULT, REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE VARIABLE STATOR VANE (VSV) ACTUATOR IAW T/C R5M75303, PERFORMED ENGINE RUN, OPERATIONAL CHECK AND LEAK CHECK WAS GOOD. ACTUATOR CONFIRMED FAILURE OF UNIT FOR FAILING ELECTRICAL BONDING RESISTANCES AND PISTON VELOCITIES OUT OF TOLERANCE. DISASSEMBLED UNIT AND FOUND TORQUE MOTOR SCREENS AT LACQUER LEVEL (L.L.) 3, AND SERVO VALVE ASSEMBLY & INLET FILTER AT L.L. 1. REPLACED TORQUE MOTOR AND CLEANED SERVO VALVE AND INLET FILTER, RE-CERTIFIED UNIT AND RETURNED TO SERVICE IAW CMM 75-32-61, REV. 1. 2L72 4F4 FRTA28NM E311NE 20050120000492005012000049NM 2005 1 20 CALA0500013 120050117A531565C339502 FLOORBEAM BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2733608 27321 INSPECTION FOUND FLOORBEAM CORRODED AROUND SCREW HOLES AT STA 986, RBL 3 TO RBL 12. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51. 2L72 4F RTA16WE 20050120000512005012000051NM 2005 1 20 SWAA050129 120050118A575565C2525121A SKIN BOEING737 7373T5 1384608NM LT WING SPOILER DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29667SW 23063 DURING SCHEDULED 1/4D CHECK, FOUND LT WING NR 3 SPOILER DELAMINATED. REMOVED AND REPLACED LT WING NR 3 SPOILER PER MM. 2L72 4F RTA16WE 20050120000632005012000063NM 2005 1 20 05FDEA00088 120050113A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 MAIN DECK CARGO, SEAT TRACK HORIZONTAL FLANGE UPPER SURFACE AT STA Y= 5-11 TO Y= 5-33, X= 75.25 FOUND FLOOR PANEL MOUNTING FOUND CORRODED AND WITH SHORT EDGE DISTANCE. CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I, FIGURE 1. 2L73 4F RTA22WE 20050120000652005012000065EU 2005 1 20 05FDEA00122 120050118A5730 PANEL AIRBUS310 A310203 3930313EU FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25413FE 397 PANEL 550JB HAS 2 EACH ELONGATED HOLES. COMLIED WITH EA 6-5710-85600 BY INSTALLING 2 EACH REPAIR BUSHINGS. 2L72 4F RTA35EU 20050120000672005012000067EU 2005 1 20 05FDEA00124 120050118A5730 PANEL AIRBUS310 A310203 3930313EU RT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25413FE 397 PANEL LAND ON RIGHT WING ACCESS HOLE 650JB HAS 1 EACH ELONGATED HOLE. COMPLIED WITH EA 6-5710-85600 BY INSTALLING REPAIR BUSHING. 2L72 4F RTA35EU 20050120000692005012000069NM 2005 1 20 2005UALA00052 120050111A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29503UA 24624 EXTERIOR FUSELAGE AT STA 1420 BETWEEN STR 28R AND 30R, SKIN IS CREASED. FRAME SHEAR TIES WERE REPLACED. 2L72 4F4 FRTA2NM E17NE 20050120000712005012000071NM 2005 1 20 2005UALA00030 120050107A5322 SHEAR TIE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29577UA 26693 AFT PIT SHEAR TIE CORRODED, BS 1440 STR 29L-30L. FABRICATED AND INSTALLED NEW SHEAR-TIE. 2L72 4F4 FRTA2NM E17NE 20050120000732005012000073NM 2005 1 20 2005UALA00032 120050107A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29577UA 26693 AFT CARGO PIT FRAME UPPER FLANGE DENTED, BS 1340 STR 25L-26L. INSTALLED J ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20050120000742005012000074NM 2005 1 20 2005UALA00033 120050107A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29577UA 26693 AFT CARGO PIT FRAME UPPER FLANGE DENTED AT BS 1480 STR 25LTO 26L. INSTALLED J ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20050120000752005012000075NM 2005 1 20 2005UALA00034 120050107A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29577UA 26693 AFT CARGO PIT FRAME UPPER FLANGE DENTED AT BS 1380 STR 25L TO 26L. INSTALLED J ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20050120000762005012000076GL 2005 1 20 0500051236 220050112A7200 ENGINE DOUG DC10 DC1030 3023501WP GE CF6 CF650C 30018GL NR 3 FAILED A NWAAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 GL01236NW 46934 455314 WHILE AT CRUISE, THE CREW REPORTED THE NR 3 ENGINE FAILED WITH NO INDICATION OF OIL PRESSURE OR N2 SPEED. THE CREW SECURED THE ENGINE PER COM AND CONTINUED TO AMS LANDING WITHOUT INCIDENT. THE ENGINE WAS REPLACED. OPERATIONAL CHECK GOOD. 2L73 4F4 F A22WE A23EA 20050120000772005012000077NM 2005 1 20 SWAA050131 120050118A5755 ATTACH FITTING BOEING737 7373H4 1384600NM RT WING SPOILER BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29365SW MA4654 26576 DURING SCHEDULED 1/4D CHECK, FOUND RT WING NR 5 SPOILER UPPER LUG AT OUTBOARD ACTUATOR BROKEN. REMOVED AND REPLACED RT WING NR 5 SPOILER PER MM. 2L72 4F RTA16WE 20050120000782005012000078NM 2005 1 20 SWAA050119 120050118A291050605 VALVE BOEING737 7373H4 1384600NM NR 2 ENGINE LEAKING A SWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW29301SW 22941 AIR TURNBACK, DURING CLIMB NR 2 ENGINE DRIVEN HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED, WITH LOSS OF SYSTEM-B HYDRAULIC FLUID. REMOVED AND REPLACED NR 2 T/R SHUTTLE VALVE PER MM. 2L72 4F RTA16WE 20050120000792005012000079NM 2005 1 20 SWAA050120 120050118A3350D71702001 BATTERY BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29656SW 28401 DURING SCHEDULED SERVICE CHECK, FOUND LT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20050120000802005012000080EU 2005 1 20 05FDEA00029 120050106A5330 SKIN AIRBUS310 A310222 3930315EU FUSELAGE DAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25454FE 278 COMPLY WITH AGING 9-AGING-INSPECTION. NON-ROUTINE, FUSELAGE - REPAIR AT APPROX FS 69 STR 50 RT. *S/D* VERIFIED THAT THE EXISTING REPAIR WAS PERFORMED IAW SRM 53-10-12, FIG 225. 2L72 4F RTA35EU 20050120000812005012000081 2005 1 20 SWAA050088 420050114A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29639SW 27712 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050120000822005012000082 2005 1 20 SWAA050089 420050114A2565D31354 SLIDE BOEING737 7375H4 138449DNM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29502SW 24179 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050120000852005012000085NE 2005 1 20 VNAA0501001 220050104A7261 SCAVENGE PUMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 2 ENGINE MALFUNCTIONED A VNAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL05223JS 7892 GEE950034 DURING CRUISE AT FL 350 THE CREW OF FLIGHT 2293 (CLT TO MSP) REPORTED OIL PRESSURE FLUCTUATING 22-42 PSI AND OIL TEMPERATURE HIGHER THAN NORMAL ON THE NR 2 ENGINE. THE AIRCRAFT DIVERTED TO DAY AND MADE AN UNEVENTFUL LANDING. AFTER TROUBLESHOOTING THE SYSTEM PSA MAINTENANCE REMOVED THE NR 2 ENGINE LUBE/SCAVANGE PUMP, CLEANED THE INLET SCREENS, AND REINSTALLED THE PUMP IAW CRJ 200 AMM 79-21-01. AN OPERATIONAL CHECK FLIGHT WAS FLOWN ON 01/05/05 AND ALL SYSTEMS OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050120000862005012000086EA 2005 1 20 VNAA0501002 120050106A2700DL2428M4 ACTUATOR CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE PITCH FEEL FAILED A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL05703PS1720 10137 SHORTLY AFTER TAKEOFF FROM CLT THE AMBER PITCH FEEL CAUTION LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO CLT AND MADE AN UNEVENTFUL LANDING. PSA MAINTENANCE AFTER TROUBLESHOOTING REMOVED & REPLACED THE NR 2 PITCH FEEL ACTUATOR IAW CRJ 700 AMM 27-31-23-400-801-A01. THE PITCH FEEL SYSTEM OPERATIONALLY CHECKED GOOD IAW CRJ 700 AMM 27-31-00-710-802-A02. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050120000872005012000087 2005 1 20 VNAA0501003 420050107A3418 PITOT LINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE OBSTRUCTED A VNAAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 GL05209PS 7874 ON A REPOSITIONING FLIGHT, DURING TAKEOFF ROLL AT DAY, THE CAPTAIN LOST IAS READOUT ON HIS PRIMARY FLIGHT DISPLAY AND PREFORMED A REJECTED TAKEOFF AT 95 KTS. PSA MAINTENACE FOUND WATER IN THE PILOT'S AND COPILOT'S PITOT LINES. THE CONTAMINATION WAS REMOVED FROM THE PITOT LINES IAW CRJ 200 AMM 34-11-00-100-801 AND -802. BOTH SYSTEMS LEAK CHECKED GOOD IAW CRJ 200 AMM 34-11-00-790-802. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050120000882005012000088EA 2005 1 20 VNAA0501004 120050110A29136619002 PUMP CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE HYD SYSTEM FAILED A VNAAO OTHER O OTHER NRNOT REPORTED 1 GL05706PS770 10150 EN ROUTE FROM STL TO CLT THE HYD EDP 1A CAUTION MESSAGE ILLUMINATED. THE CREW OF FLIGHT 2214 FOLLOWED CRJ 700 QRH PROCEDURES. HYDRAULIC PRESSURE, TEMPERATURE, AND QUANTITY WERE GOOD WITH PUMP 1B OPERATING. THE FLIGHT CONTINUED TO CLT AND MADE AN UNEVENTFUL LANDING. THE AIRCRAFT WAS FERRIED TO DAY WHERE PSA MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP IAW CRJ 700 AMM 29-11-01-400-801. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050120000892005012000089EA 2005 1 20 VNAA0501005 120050103A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS ILLUMINATED A VNAAO OTHER F FLT CONT AFFECTED DEDESCENT 1 GL05261PS 7959 DURING DESCENT INTO PHL THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED. POSITION OF THE FLAPS WAS NOT REPORTED. THE CREW OF FLIGHT 2445 FOLLOWED THE CRJ 200 QRH PROCEDURES AND MADE AN UNEVENTFUL LANDING. PSA MAINTENANCE CYCLED THE FLAP CONTROL CHANNEL 1 & 2 CIRCUIT BREAKERS AND CYCLED THE FLAPS IAW CRJ 200 SL 00-001 FAULT ISOLATION GUIDE. THE FLAPS OPERATIONALLY CHECKED GOOD AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050120000912005012000091 2005 1 20 SWAA050101 420050117A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29726SW 27858 DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050120000932005012000093NM 2005 1 20 SWAA050112 120050117A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29606SW 27926 DURING SCHEDULED D-CHECK, FOUND 2 EACH STRINGER CLIPS CRACKED AT BS 706, BETWEEN STRINGERS 11R AND 11L. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20050120000952005012000095NM 2005 1 20 SWAA050086 120050113A554265C25841 SKIN BOEING737 7373K2 13844BANM RUDDER CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29345SA 23786 DURING SCHEDULED 1/2D CHECK, FOUND TOP RT SIDE OF RUDDER CORRODED. REMOVED AND REPLACED RUDDER PER MM. 2L72 4F RTA16WE 20050120000972005012000097NM 2005 1 20 SWAA050070 120050111A53206545833 FLOOR SUPPORT BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29358SW 26595 DURING SCHEDULED RON, FOUND FLOOR PANEL SUPPORT ANGLE AT BS 270, FROM LBL 9.5 TO RBL 9.5, CORRODED. REPAIRED FLOOR SUPPORT PER SRM. 2L72 4F RTA16WE 20050120000992005012000099NM 2005 1 20 UPS05443654 120050109A5347 SEAT TRACK BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C - BS 520 - 540 LBL 46 SEAT TRACK CORRODED AS MARKED. U/D BS 520 - 560 LBL 46 SEAT TRACK REPAIR PARTS FABRICATED AS PER SRM 53-10-05 FIG 6. CORROSION BLEND OUT 0.060 X 1 X 1 INCHES EXCEED SRM LIMIT. 2L74 4F A20WE 20050120001012005012000101NM 2005 1 20 SWAA050060 120050111A3350612825 BATTERY BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29640SW 27713 DURING SCHEDULED A1 CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHTS AT ROWS 12 DEF AND 14 DEF, INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20050120001032005012000103NM 2005 1 20 SWAA050062 120050111A551265C25727 SKIN BOEING737 7375H4 138449DNM HORIZONTAL STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29514SW 25153 DURING SCHEDULED C4 CHECK, FOUND RT HORIZONTAL STAB SKIN AT BS 140, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050120001102005012000110NM 2005 1 20 UPS05443658 120050108A5311 FRAME BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C, FWD CARGO COMPT - SUPPORT FRAME WEB SURFACE FOUND CRACKED AT STA 880 BETWEEN STRINGER 37L TO STRINGER 38L. SUPPORT FRAME REPAIRED PER SRM 53-10-04 FIG 52. 2L74 4F A20WE 20050120001172005012000117NM 2005 1 20 CALA0500007 120050114A531565C339502 FLOORBEAM BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2733608 27321 INSPECTION FOUND FLOORBEAM CORRODED AROUND SCREW HOLES AT STA 986.5, RBL 29. REPAIRED IAW SRM 53-00-51, FIGURE 203. 2L72 4F RTA16WE 20050120001192005012000119WP 2005 1 20 CALA0500012 120050117A531327779223 LONGERON DOUG DC9 DC982 3022082WP STA CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2735836 49441 INSPECTION FOUND A .75 INCH CRACK IN LONGERON 4L AT STA 160. A NEW LONGERON SECTION WAS SPLICED IN IAW SRM 53-02 FIGURE 18. 2L72 4F A6WE 20050120001212005012000121NM 2005 1 20 SWAA050064 120050111A53126545819 PRESSURE PANEL BOEING737 7373A4 1384585NM NLG WW CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED C1 CHECK, FOUND 3 EACH CRACKS AT NLG W/W FWD UPPER WEB AT BS 233, BS 234, BS 238, UPPER RIVET ROW. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050120001232005012000123NM 2005 1 20 SWAA050102 120050117A335065C34691 LIGHT BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29727SW 27859 DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHTS AT ROWS 1 ABC AND 2 ABC, INOP. REMOVED AND REPLACED LIGHT ASSY'S PER MM. 2L72 4F RTA16WE 20050120001252005012000125NM 2005 1 20 UPS05443663 120050107A531165B209334 FRAME BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C M/D - BS 660, BET S25 - 26R, FRAME I/B CHORD O/B FACE FOUND CRACK. FRAME I/B CHORD REPLACED PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050120001292005012000129NM 2005 1 20 AALA20050011 120050107A3397 WIRE BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW2139365 24046 SFO - EMERGENCY LIGHTS AT ROWS 32 TO 40 INOPERATIVE. REPAIRED WIRING AT ROW 38H BATTERY PACK FOR EMERGENCY LIGHTS AT ROWS 32 TO 40. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050120001302005012000130NM 2005 1 20 AALA20050019 120050110A3350 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21178AA 32398 JFK - EMERGENCY LIGHTS AT L1 DOOR AND LEFT HAND SEATS OF FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK AND CHARGER FOR EMERGENCY LIGHTS AT L1 DOOR AND LEFT HAND SEATS OF FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050120001312005012000131NM 2005 1 20 AALA20050018 120050110A3397 CONNECTOR BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21640A 24598 MIA - EMERGENCY LIGHT AT 1L INOPERATIVE. REPLACED CONNECTORS FOR EMERGENCY LIGHT AT 1L. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050120001322005012000132WP 2005 1 20 AALA20050015 120050109A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW219627R 53597 BOS - EMERGENCY LIGHTS AT FORWARD AND AFT RAFT STORAGE LOCATION INOPERATIVE. REPLACED BATTERY PACK IN OVERHEAD BIN FOR EMERGENCY LIGHTS AT FORWARD AND AFT RAFT STORAGE LOCATION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050120001332005012000133WP 2005 1 20 AALA20050021 120050111A2530 OVEN DOUG DC9 DC983 3022083WP GALLEY DIRTY A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21972TW 53622 DFW - SHORTLY AFTER TAKEOFF SMOKE CAME THROUGH BOTTOM OF COCKPIT DOOR. AIRCRAFT RETURNED TO DFW AND LANDED OVERWEIGHT AT 135,000 WITHOUT INCIDENT. FOUND FIRST CLASS OVEN NUMBER 212 POSITION SMOKING. CLEANED AND REMOVED GREASE FROM OVEN. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050120001342005012000134EU 2005 1 20 AALA20050022 120050111A3233 ACTUATOR AIRBUS300 A300B4605R 3930308EU HYD SYSTEM LEAKING A AALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW217083A 645 PTY - GREEN SYSTEM HYDRAULIC LOSS. AFTER ONE AND ONE HALF HOURS OF FLIGHT. QUANTITY LEVEL IN GREEN SYSTEM COST. CHECKLIST COMPLIED WITH AND RECOVERED ENOUGH OF GREEN SYSTEM FOR GEAR EXTENSION AND NOSE GEAR STEERING IN MIA. LANDED MIA WITHOUT INCIDENT. FOUND HYDRAULIC LEAK AT RIGHT NOTCH FLAP ACTUATOR. REPLACED RIGHT NOTCH FLAP ACTUATOR. NO FURTHER LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20050120001352005012000135WP 2005 1 20 05FDEA00096 120050115A7601580291751 THROTTLE CABLE DOUG DC10 DC1030 3023501WP NR 2 ENGINE FROZEN A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25309FE 48298 NR 2 ENGINE THRUST LEVER REMAINED FROZEN AT 80 PERCENT ON DESCENT INTO SJC. DID A PRECAUTIONARY SHUTDOWN AT 10,000 FT. NO OTHER PROBLEMS NOTED. UPON CREW DEBRIEF FOUND NR 2 THROTTLE LEVER STUCK AT 1/3 TRAVEL. MOVED THROTTLE LEVER AND FOUND SLIGHT BIND WHICH ENDED UPON FURTHER CYCLES. QUESTIONED CREW ON SHUTDOWN, AND OIL PRESSURE WAS PRESENT. FOUND NR 2 ENG THROTTLE CABLE TO BE OF THE SEALED TYPE AND THUS CANNOT BE LUBRICATED / BLOWN OUT. REQUIRES CABLE ASSY. 2L73 4F A22WE 20050120001362005012000136NM 2005 1 20 05FDEA00114 120050117A551165382038 SPAR BOEING727 727200 138407ENM HORIZONTAL STAB DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25465FE 21289 RT HAND HORIZ STAB REAR SPAR LWR CHORD HAS DAMAGE FASTENER HOLE AT NR 4 BAL BAY. *S/D* TRIMMED DAMAGED AREA OUT, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 55-10-5. 2L73 4F RTA3WE 20050120001382005012000138WP 2005 1 20 AALA20050023 120050112A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGNECY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21218AA 49168 AUS - OVERHEAD EMERGENCY LIGHT AT SEAT ROW 9DEF INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHT AT ROW 9DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050120001392005012000139NE 2005 1 20 AWXA200500020 220050108A7320FMU550MK1 FMU AIRBUSA319 A319132 3930340NM IAE V2524 V2524A5 NE NR 1 ENGINE MALFUNCTIONED A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28820AW15102 1397 BOS - ABORTED TAKEOFF - FLT 0068 - ON TAKEOFF AT BOS EN ROUTE FOR PHX RECEIVED ECAM INDICATIONS, ENG 1 FADEC, ENG 1 COMPRESSOR, ENG 1 FAIL, ENG 1 FUEL CTRL FAULT. REJECTED TAKEOFF AT LOW SPEED. MAINTENANCE TROUBLESHOT AND REPLACED NR 1 ENGINE FUEL METERING UNIT (FMU) IAW T/C R5M73308, LEAK AND OPERATIONAL CHECK WAS GOOD. TEAR DOWN REPORT CONFIRMED FAULT. TESTED UNIT IAW CMM BASIC. PERFORMANCE OF FMU CONSIDERED UNACCEPTABLE WITH DETERATION BEING ATTRIBUTED TO HEAVY FUEL LACQUER IN MAIN INLET FILTER. AFTER REPLACING MAIN INLET FILTER, PERFOMANCE OF THIS FMU RESTORED TO ACCEPTABLE LIMITS. 2L72 4F4 FRTA28NM E40NE 20050120001412005012000141NM 2005 1 20 AWXA200500022 120050110A2920NAS161210 PACKING BOEING737 7373S3 1384711NM LT WING TORN A AWXAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP28313AW 23712 LAS - DIVERSION - FLT 0765 - APPROXIMATELY 20 MINUTES OUT OF PHX EN ROUTE TO SMF NOTICED HYDRAULIC FLUID LEAKING FROM THE TOP OF LEFT WING, ALSO OBSERVED B-SYSTEM HYDRAULIC QUANTITY DECREASING, FLUID LEVEL STABILIZED AT 1/2 QUANTITY ON INDICATOR, DIVERTED INTO LAS FOR REPAIR. MAINTENANCE FOUND LEAK COMING FROM FITTING AT NR 3 SPOILER, REPLACED 2 EACH O-RING SEALS ON FITTING FOR NR 3 SPOILER, LEAK CHECK WAS GOOD. 2L72 4F RTA16WE 20050120001422005012000142NM 2005 1 20 DL738050021 120050110A29177321124005 MODULE BOEING737 737832 13844CFNM HYD RESERVOIR CONTAMINATED A DALAO OTHER J WARNING INDICATION CRCRUISE 1 SO273766 30820 ENG 1 AND ENG 2 HYD PUMPS LOW PRESS LIGHTS ILLUM IN FLT. FOUND EVIDENCE OF MOISTURE/WATER IN HYD RSVR PRESS MOD. DISCONNECTED LINES AT HYD RSVR PRESS MODULE & AT -A- AND -B- RSVRS. BLEW LINES WITH DRY NITROGEN. REPLACED HYD RSVR PRESS MODULE AND RECONNECTED LINES. OPS OK. 2L72 4F RTA16WE 20050118000662005011800066 2005 1 18 QXEA200500059 420050111A2310CDU3933AE04 CDU BOMBDRDHC8 DHC8401 1390041NM ZONE 100 INOPERATIVE A QXEAO OTHER O OTHER CRCRUISE 1 NM09406QX3475 193 4048 LAX - NR 1 ARCDU FAILED IN CRUISE FLIGHT, ACCOMPLISHED E/A CHECKLIST. SYSTEM RESTORED. MAINTENANCE REMOVED AND REPLACED NR 1 ARCDU. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050118000972005011800097SO 2005 1 18 C2XA05TY001 120050103A324021582 BRAKE EMB 145 EMB145ER 3260211SO MLG LEAKING A C2XAD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SW2714940 145033 A/C WAS BEING PUSHED BACK WHEN PILOT APPLIED BRAKES, THE NR 2 BRAKE SHUTTLE VALVE STARTED LEAKING. MAINTENANCE REMOVED AND REPLACED THE NR 1 AND 2 BRAKE CONTROL VALVES AND NR 1, 3 AND 4 BRAKES IAW EMB 145 AMM 32-49-03. OPS CHECKS WAS GOOD AND A/C RELEASED. 2L72 4F RTT00011AT 20050118001372005011800137NM 2005 1 18 05FDEA00020 120050104A5313 SPLICE BOEING727 727100 1384036NM STRINGER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25151FE 19147 STRINGER 4R SPLICE IS CRACKED ON EACH SIDE OF FRAME AT STA 480. REMOVED AND REPLACED STRINGER 4R SPLICE AT STA 480 IAW SRM 51-10-1. 2L73 4F RTA3WE 20050118001562005011800156EU 2005 1 18 05FDEA00025 120050106A5510 STRUCTURE AIRBUS310 A310222 3930315EU HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25422FE 346 HORIZONTAL STAB CENTER BOX TOP SIDE HAS APPROX 50 SQ INCH OF CORROSION ON AND UNDER FAST HEADS REF N-CARD N-00822. COMPLIED WITH EA 6-5510-84509 REMOVING FASTENERS CORROSION FLAP PEENING & REINSTALLING FASTENERS IAW A310 SRM 51-74-10, 51-29-00 & 51-40-21. 2L72 4F RTA35EU 20050118001622005011800162NM 2005 1 18 C1HA200574002 120050103A2131 CONTROLLER BOEING727 727225 1384077NM CABIN PRESSURE MALFUNCTIONED A C1HAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15674MG 21450 ABOUT 50 MINUTES OUT OF SLC, CLIMBING TO FL250 THE CREW HAD LOST CABIN PRESSURE. ARNC CALL WAS PLACED TO DISPATCH, MXCTL WAS ALSO ON THE LINE. FLT DESCENDED TO FL230, THEN TO FL210, THEN TO FL 190. CABIN WAS HOLDING AT THAT LEVEL. DISPATCH RAN A POINT ALOFT FLT PLAN AND FL190, LANDING WITH MINIMAL FUEL INTO IND. WEATHER EN ROUTE AND AT THE DESTINATION WAS POOR. FOR SAFETY REASONS, DISPATCH AND SOC ELECTED TO DIVERT THE FLT INTO DEN. 2L73 4F A3WE 20050118001652005011800165EA 2005 1 18 SWIA200514340 120050103A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLT SPOILER INOPERATIVE A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07445SW2532 2532 7651 RIGHT SPOILERON NR 3 PCU INOPERATIVE. REMOVED AND REPLACED RIGHT OUTBOARD SPOILER ON PCU WITH SERVICEABLE UNIT IAW MM 27-62-01. REPLACED RIGHT SECU WITH SERVICEABLE UNIT, MM 27-60-00. OPERATIONAL CHECK GOOD. P/N 49-164-06, S/N OFF: 01624. 2L72 4F RTA21EA 20050118001682005011800168EA 2005 1 18 SWIA200514343 120050104A2720 TRANSDUCER CNDAIRCL600 CL6002B19 1900309EA RUDDER MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07957SW 7829 NO FULL LEFT RUDDER INDICATION ON EICAS. REMOVED AND REPLACED RUDDER RCS TRANSDUCER, OPERATIONAL CHECK GOOD IAW 22-24-05. 2L72 4F RTA21EA 20050118001872005011800187NM 2005 1 18 05FDEA00053 120050108A5730 SKIN DOUG MD11 MD11 3023602NM ZONE 500 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 INNER LT WING LOWER SKIN AT XORS= 85 FOUND WITH 3.5 INCH DENT. COMPLIED WITH FEDEX EA 1-5710-81592. 2L73 4F RTA22WE 20050118001902005011800190NM 2005 1 18 05FDEA00056 120050108A5710 STRUCTURE DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 LT WING, TRAILING EDGE UPPER CHORD AT XORS= 1042 FOUND CORRODED. REPAIR CARRIED OUT AT LEFT HAND WING, TRAILING EDGE UPPER CHORD AT XORS= 1042 AS PER FEDEX EA 1-5710-81589, FOUND EXCEEDED LIMITS AS PER SRM 57-20-00 VOLUME I, FIGURE 16. 2L73 4F4 FRTA22WE E13NE 20050119000032005011900003NM 2005 1 19 SWAA050053 120050109A3260806002 MODULE BOEING737 7373Y0 1384671NM E&E BAY FAULTY A SWAAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW29682SW 23496 ATB / DECLARED EMERGENCY. NLG RED UNSAFE LIGHT ILLUMINATED IN FLIGHT. NLG GREEN DOWN AND LOCKED LIGHT ILLUMINATED INTERMITTENTLY. REMOVED AND REPLACED M1214, PER MM. 2L72 4F RTA16WE 20050119000062005011900006NM 2005 1 19 SWAA050049 120050108A53306545772 SKIN BOEING737 7373H4 1384600NM FUSELAGE WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29649SW 27719 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT DORSAL FIN WORN. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20050119000082005011900008 2005 1 19 SWAA050051 420050109A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29643SW 27716 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050119000122005011900012CE 2005 1 19 DXTA200500523 120050110A3240 PEDAL CESSNA560 560XL 2076702CE BRAKES DAMAGED E DXTAO OTHER S AFFECT SYSTEMS LDLANDING 1 GL07604QS 5605204 PILOTS LEFT BRAKE PEDAL WENT TO FLOOR ON LANDING ROLL. CO-PILOTS BRAKES WORKED FINE. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20050119000322005011900032NM 2005 1 19 2005UALA00024 120050105A2120 DOOR BOEING747 747422 1384935NM PWA 4056 PW4056 NE NR 2 A/C PACK BROKEN A UALAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 WP29171UA 24322 CHRONIC WRITE UP BANGING IN FLOOR BEHIND DOOR 2L, 5 ROWS BACK ALSO STOP WITH NR 2 PACK OFF. THE NR 2 AIR CONDITIONING PACK INLET DOOR WAS FOUND BROKEN. THE DOOR WAS REPLACED AND THE AIRCRAFT HAS HAD NO FURTHER PROBLEMS. 2L74 4F4 FRTA20WE E24NE 20050119000372005011900037NM 2005 1 19 MAMA040915 120050104A5230 DOOR BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CARGO DOOR LEAKING A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29312UA 23673 AIRCRAFT RETURNED WITH CABIN PRESSURE PROBLEM. 2L72 4F4 FRTA16WE E2GL 20050120000252005012000025WP 2005 1 20 ABXA050007 120050104A523059101415 PAN DOUG DC9 DC931 3022065WP CARGO DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23929AX 45874 TWO CRACKS EMINATING FROM HILOC HOLE AT UPPER FORWARD DOOR STOP ON FORWARD LOWER CARGO DOOR. REPAIRED AREA IAW DC-9 SRM 52-03. 2L72 4F A6WE 20050120000292005012000029WP 2005 1 20 ABXA050011 120050104A523039260461 SUPPORT FITTING DOUG DC9 DC931 3022065WP CARGO DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23929AX 45874 FORWARD LOWER CARGO DOOR STOP SUPPORT FITTING CRACKED AFT OF FORWARD HINGE INSIDE LIGHTING HOLE. REMOVED AND REPLACED FITTING ON FORWARD LOWER CORNER DOOR AFT OF FORWARD HINGE IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20050120000362005012000036NM 2005 1 20 AWXA200500035 120050103A53306545774105 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK A 6 INCHES CRACK WAS FOUND IN FUSELAGE SKIN AT BS 727D+17, STR 22 LT. MAINTENANCE CUT OUT CRACK IN FUSELAGE SKIN AT BS 727D+17, STR 22 LT; PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A FILLER, DOUBLER, AND TRIPLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-01 FIG 229. 2L72 4F RTA16WE 20050120000482005012000048NM 2005 1 20 SWAA050130 120050118A5313BAC1498 STRINGER BOEING737 7373T5 1384608NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29667SW 23063 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER 26R AT BS 500D + 2, CORRODED. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2L72 4F RTA16WE 20050120000502005012000050NM 2005 1 20 UPS05443656 120050108A5313 STRINGER BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C U/D - BS 560, S9R, STRINGER END FOUND CRACK. STRINGER REPAIR PER SRM 53-10-03 FIG 2. 2L74 4F A20WE 20050120000522005012000052NM 2005 1 20 2005F00010 120050114A5343652165120 ATTACH FITTING BOEING727 7272M7 138407SNM MLG DAMAGED A DHLAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01750DH 21951 PORK CHOP FITTING RT MLG DAMAGED AND MISALIGNED. 2L73 4F A3WE 20050120000542005012000054EU 2005 1 20 UPS05143669 120050118A5270 WARNING SYSTEM AIRBUSA300 A300F4622R 3930360EU COCKPIT DOOR INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01122UP 0807 INSPECTION TYPE:N/A WHEN OPENING DOOR, TESTED CREW ENTRY DOOR SLIDE WARNING BUZZER DID NOT SOUND. WARNING LIGHT STILL ILLUMINATES. WORKED FINE WHEN DEPARTED. PERFORMED OPERATION TEST OF DOOR PER 52-10-11-6, OPS CHECK OK. 2L72 4F RTA35EU 20050120000562005012000056NM 2005 1 20 UPS05443650 120050109A5347 SEAT TRACK BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 BS 480 - 500 RBL 66 SEAT TRACK CORRODED AS MARKED. SEAT TRACK PART FABRICATED AS PER SRM 51-10-01 PG 9. CORROSION BLEND OUT 0.050 X 2 X 2 INCHES EXCEED SRM LIMIT. 2L74 4F A20WE 20050120000582005012000058NM 2005 1 20 UPS05443652 120050108A5313 STRINGER BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C - BS 736 - 738, S8R, STRINGER END FOUND CRACK. STRINGER REPAIRED PER SRM 53-10-03 FIG 2. 2L74 4F A20WE 20050120000602005012000060NM 2005 1 20 05FDEA00085 120050112A5313 LONGERON DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 MAIN DECK, LONGERON 18L AT STA Y= 535 FOUND WITH DENT. FOUND MOUNTING FASTENER LOOSE LONGERON 18L AT STA Y= 535 - LOOSE FASTENERS REMOVED AND REPLACED PER SRM 51-31-01 VOLUME I 2L73 4F RTA22WE 20050120000902005012000090NM 2005 1 20 SWAA050100 120050116A57436937877 FITTING BOEING737 7373H4 1384600NM RT & LT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29650SW 27720 DURING SCHEDULED SERVICE CHECK, FOUND RT AND LT FWD OUTBOARD HANGER FITTINGS CORRODED. REPAIRED HANGER FITTINGS PER EA. 2L72 4F RTA16WE 20050120000922005012000092NM 2005 1 20 SWAA050111 120050117A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29606SW 27926 DURING SCHEDULED D-CHECK, FOUND 2 EACH STRINGER CLIPS CRACKED BETWEEN BS 560 AND BS 580, STRINGER 11R. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20050120000942005012000094NM 2005 1 20 SWAA050113 120050117A5511 SPAR BOEING737 7373H4 1384600NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29606SW 27926 DURING SCHEDULED D-CHECK, FOUND LT AND RT HORIZONTAL STAB FWD SPAR FWD AND AFT CLEVIS LUGS CORRODED. REPAIRED HORIZONTAL STAB PER SRM. 2L72 4F RTA16WE 20050120000962005012000096NM 2005 1 20 SWAA050087 120050113A53126545409 PRESSURE PANEL BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29667SW 23063 DURING SCHEDULED 1/4D CHECK, FOUND 3 EACH CRACKS ON BEADED PRESSURE WEB AT BS 663, BETWEEN LBL 33 AND RBL 39. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050120001002005012000100NM 2005 1 20 UPS05443655 120050108A5313 STRINGER BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C - BS 640, S9R, STRINGER END FOUND CRACK. STRINGER REPAIR PER SRM 53-10-03 FIG 2. 2L74 4F A20WE 20050120001022005012000102NM 2005 1 20 SWAA050061 120050111A53306545774 SKIN BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 752, STRINGER 24L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20050120001042005012000104 2005 1 20 SWAA050063 420050111A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29740SW 29276 DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050120001052005012000105WP 2005 1 20 05FDEA00095 120050114A7601C803833 THROTTLE CABLE DOUG MD10 MD1010F 3022112WP ENGINE CONTAMINATED A FDEAE ENGINE SHUTDOWN F FLT CONT AFFECTED DEDESCENT 1 SO25565FE 46996 ON DESCENT NR 2 ENGINE THROTTLE WOULD NOT RETARD. ENGINE STUCK AT 85 PERCENT N2, FUEL FLOW WAS INOP. PERFORMED PRECAUTIONARY SHUTDOWN. PURGED CABLE OF MOISTURE PER MM SUPPLEMENT 76-11-01 -2 / 5A STEP 6, ALL TEST PAST PER MM 76-11-01-2 PARAGRAPH 4. 2L73 4F RTA22WE 20050120001062005012000106 2005 1 20 05FDEA00097 420050115A34529650976003212 COMPUTER DOUG MD10 MD1010F 3022112WP ZONE 200 MALFUNCTIONED A FDEAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO25392FE 46626 DURING APPROACH TO RWY 35R AT MCO GOT TOO LOW TERRAIN WARNING. AT 400 FEET ON GLIDE SLOPE AND LOC EXECUTED MISSED APPROACH AND RETURNED TO SAME RWY. THE SAME THING HAPPENED ON SECOND APPROACH. TOO LOW TERRAIN, WARNING CONTINUED TO TOUCHDOWN. REMOVED & REPLACED ENHANCED GROUND PROXIMITY WARNING COMPUTER. 2L73 4F RTA22WE 20050120001072005012000107EU 2005 1 20 05FDEA00098 120050116A7333 FUEL FILTER AIRBUS300 A300F4605R 3930327EU NR 1 ENGINE CLOGGED A FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25654FE 738 TAKEOFF REJECTED AT 90 KTS FOR NR 1 FUEL ENG FUEL CLOG ECAM & WARNING. REMOVED AND REPLACED MAIN FUEL FILTER AS PER MM 73-12-02-4F. NO CONTAMINATION FOUND. ENGINE RUN AND LEAK CHECK GOOD. OK FOR SERVICE. FILTER CPN 41823. 2L72 4F RTA35EU 20050120001082005012000108NM 2005 1 20 05FDEA00099 120050116A5320 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 CENTER ACCESSORY COMPARTMENT FORWARD OF DOOR AT LONGERON L47 LONGERON SPLICE DAMAGED. CENTER ACCESSORY COMPARTMENT FORWARD OF DOOR AT LONGERON L47 DAMAGED LONGERON SPLICE REMOVED AS PER SRM 51-33-01 VOL II AND SRM 51-35-01 VOL II. LONGERON SPLICE FABRICATED AS PER SRM 53-00-01 FIG 2 VOL I AND INSTALLED AS PER SRM 51-33-01 VOL II AND SRM 51-35-01 VOL II. 2L73 4F RTA22WE 20050120001092005012000109NM 2005 1 20 UPS05443657 120050108A5313 STRINGER BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C U/D - BS 620, S9R, STRINGER END FOUND CRACK. STRINGER REPAIR PER SRM 53-10-03 FIG 2. 2L74 4F A20WE 20050120001112005012000111NM 2005 1 20 UPS05443659 120050109A5315 FLOORBEAM BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C - FLOORBEAM BS 340 LBL 11 - 39 UPPER CHORD CORRODED. REPAIR PARTS FABRICATED AS PER SRM 53-10-07 FIG 23. CORROSION BLEND OUT 0.050 X 2 X 2 INCHES EXCEED SRM LIMIT. 2L74 4F A20WE 20050120001122005012000112NM 2005 1 20 UPS05443660 120050108A5313 STRINGER BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C U/D - BS 680, S9R, STRINGER END FOUND CRACK. STRINGER REPAIRED PER SRM 53-10-03 FIG 2. 2L74 4F A20WE 20050120001162005012000116WP 2005 1 20 AALA20050016 120050110A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21965TW 53615 DFW - CEILING EMERGENCY EXIT LIGHTS ABOVE FORWARD ENTRY AREA INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHTS ABOVE FORWARD ENTRY AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050120001202005012000120NM 2005 1 20 SWAA050071 120050112A5310907822 STRUCTURE BOEING737 7373H4 1384600NM HINGE BOX CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR CUTOUT LOWER HINGE BOX, CRACKED. REMOVED AND REPLACED FWD ENTRY DOOR HINGE BOX PER SRM. 2L72 4F RTA16WE 20050120001222005012000122 2005 1 20 SWAA050090 420050114A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29369SW 26580 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050120001242005012000124NM 2005 1 20 SWAA050114 120050117A53116546539 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29606SW 27926 DURING SCHEDULED D-CHECK, FOUND FRAME CHORD AT BS 616, RBL 65, CRACKED. REPAIRED FRAME CHORD SECTION PER ER. 2L72 4F RTA16WE 20050120001262005012000126 2005 1 20 SWAA050121 420050118A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29401WN 29813 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050120001282005012000128WP 2005 1 20 AALA20050017 120050110A3350 SOCKET DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW2176201 53291 DFW - EMERGENCY LIGHT AT SEAT 7D FORWARD INOPERATIVE. REPLACED LIGHT SOCKET FOR EMERGENCY LIGHT FOR SEAT 7D FORWARD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050120001432005012000143NM 2005 1 20 05FDEA00080 120050111A5711 SPAR CAP DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 RT WING, REAR SPAR UPPER CAP AT STA 1044 FOUND WITH CORROSION. REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA 1-5710-81590 2L73 4F RTA22WE 20050120001442005012000144EU 2005 1 20 05FDEA00083 120050112A7830 WARNING LIGHT AIRBUS310 A310222 3930315EU PWA JT9 JT9D* NE THRUST REVERSER ILLUMINATED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25420FE 339 715437 NR 2 ENG REV GREEN LIGHT WITH ECAM WARNING AFTER T/O. NO BUFFETING. AIR TURNBACK TO LIM. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-C. ENGINE 2, THRUST REVERSER INOP. THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POSITION. T/R VISUALLY INSPECTED, NO DAMAGE FOUND, NO MANUAL STOW ACTION REQUIRED. SUSPECT INDICATION PROBLEM. MOCC NOTIFIED, CONFERENCE CALL DONE IAW GMM. A/C OK TO CONTINUE. 2L72 4F4 FRTA35EU E20EA 20050120001452005012000145NM 2005 1 20 SWAA050083 120050113A53116558280 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29606SW 27926 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 360, STRINGER 9R, CRACKED. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20050120001462005012000146 2005 1 20 SWAA050084 420050113A2565D31354 SLIDE BOEING737 7373A4 1384585NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29679AA 23291 DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050120001472005012000147SO 2005 1 20 SWIA200514353 120050108A27503431001001 ACTUATOR EMB 120 EMB120ER 3260203SO NACELLE FLAP MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07235SW1067210672 120310 BOTH NACELLE FLAPS INDICATE DISAGREEMENT WHEN RETRACTED. REMOVED & REPLACED LEFT NACELLE FLAP ACTUATOR AS REQUIRED IAW MM 27-50-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050120001482005012000148SO 2005 1 20 SWIA200514354 120050108A3397 CONNECTOR EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT LOOSE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07560SW 120334 FLOOR LEVEL EMERGENCY LIGHT (1ST LIGHT BULB) INOPERATIVE. RESECURED LOOSE CONNECTION ON FORWARD WHITE FLOOR EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050120001492005012000149EA 2005 1 20 SWIA200514355 120050108A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLIGHT SPOILERS MALFUNCTIONED A SWIAL ABORTED APPROACH F FLT CONT AFFECTED APAPPROACH 1 NM07979SW7 7 7954 ON FINAL WHILE DEPLOYING FLIGHT SPOILERS TO 1/4 THE AIRCRAFT ROLLED RIGHT (UNCOMMANDED). REMOVED AND REPLACED FLIGHT SPOILER PCU OUTBOARD ON THE RIGHT WING IAW CRJ MM 27-62-01, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050120001502005012000150 2005 1 20 SWIA200514356 420050107A3418C818061MODA COMPUTER EMB 120 EMB120ER 3260203SO STALL WARNING INTERMITTENT A SWIAO OTHER J WARNING INDICATION CRCRUISE 1 NM07569SW 120344 F/O STALL WARNING CAME ON INFLIGHT, AURAL WARNING, LIGHT ON MAP. REMOVED AND REPLACED NR 2 STALL WARNING COMPUTER WITH SERVICEABLE UNIT. OPERATIONAL CHECK GOOD IAW MM 27-34-04. 2L72 4T RTA31SO 20050120001512005012000151 2005 1 20 SWIA200514357 420050108A3418 CONTROL PANEL EMB 120 EMB120ER 3260203SO STALL WARNING MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07232SW 120306 ON FFOD STALL WARNING TEST, PUSHER IS INOP ON BOTH SIDES AND POPS BOTH PUSHER CIRCUIT BREAKERS (D31 & D32). REMOVED AND REPLACED THE STALL WARNING CONTROL PANEL. SYSTEMS BOTH CHECK GOOD. 2L72 4T RTA31SO 20050120001522005012000152NM 2005 1 20 DL757050014 120050104A8010784750A4 STARTER BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 1 ENGINE FAILED A DALAK NONE O OTHER ININSP/MAINT 1 SO27682DA42209 26958 716325 MAIN ENGINE STARTER CAME TO THE SHOP WITH SEPARATED INLET HOUSING AND A PIECE MISSING FROM TURBINE ROTOR. REMOVED FROM NR 1 ENGINE DUE TO FAILURE. 2L72 4F4 FRTA2NM E17NE 20050121000022005012100002NM 2005 1 21 DL757050016 120050109A3350 WIRE BOEING757 757232 1384965NM EMERGENCY LIGHT BROKEN A DALAK NONE L NO TEST ININSP/MAINT 1 SO27619DL 22909 EMERGENCY TRACK LIGHTING INOP AT ROW 30D, 36D, 45D. REPAIRED WIRING AT 3 LOCATIONS. 2L72 4F RTA2NM 20050121000042005012100004NM 2005 1 21 DL757050018 120050110A2780 CONTROL UNIT BOEING757 757232 1384965NM SLATS MALFUNCTIONED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27613DL 22820 LEADING EDGE SLAT DISAGREE CAME ON 23,000 FT AT 300 KTS. SLOWED TO 235 KTS AND RTN TO LAND. FLAP/SLATS WERE UP WITH NO LIGHT FOR 10-15 MINS. WING AND ENG ANTI-ICE WAS ON. FSEU 1 AND 2 FAULTED SLAT LOSS. T/S PER FIM. ALL SLAT LOSS SWS CK GOOD FROM E5 RACK CONNECTORS. WHEN TAPPING ON LT OUTBOARD SW METER STARTED SHOWING SOME RESISTENCE. REPLACED LT OUTBOARD SW PER MM. 2L72 4F RTA2NM 20050121000052005012100005NM 2005 1 21 DL757050019 120050111A3240326001194 WHEEL BOEING757 757232 1384965NM RT MLG NR 7 DAMAGED A DALAA UNSCHED LANDING D INFLIGHT SEPARATION CLCLIMB 1 SO27670DN 25331 ON TAKEOFF NR 7 MAIN TIRE RETREAD THREW CORD. TIRE FOD CAUSED DAMAGE TO THE RIGHT INBOARD FLAP AND SEVERED HYDRAULIC LINES IN RIGHT GEAR WELL. REPLACED TIRE. REPAIRED DAMAGE. 2L72 4F RTA2NM 20050121000072005012100007EA 2005 1 21 SWIA200514358 120050107A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLT SPOILERS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07595SW 7292 SPOILERONS FAULT MESSAGE. REPLACED RIGHT INBOARD AND OUTBOARD SPOILERON PCU IAW CRJ MM 27-62-01. OPERATIONAL CHECK GOOD. P/N 27000-7, S/N MAL-0989, S/N OFF 3287. 2L72 4F RTA21EA 20050121000082005012100008NM 2005 1 21 CALA0500008 120050114A53306545775594 SKIN BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2759302 23353 INSPECTION FOUND A .5 INCH CRACK IN SKIN AFT OF RT WING TO BODY FAIRING, 10 INCHES AFT OF EMERGENCY LIGHT (JUST 2 INCHES FORWARD OF BS 727E AT S23R). INSTALLED SKIN REPAIR IAW ECRA 5330-03409. A DIP WAS ISSUED TO INSPECT THE REPAIR WITHIN 60,000 FLIGHT CYCLES PER PART 2A AND REINSPECT EVERY 25,000 FLIGHT CYCLES PER PART 2B. 2L72 4F RTA16WE 20050121000102005012100010 2005 1 21 CALA0500010 420050114A2565 LIGHT BFGOODRICH DOUG DC9 DC982 3022082WP R-2 DOOR SLIDE INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2783870 48056 WHEN THE R-2 SERVICE DOOR SLIDE WAS DEPLOYED DURING TESTING, THE SLIDE LIGHTS FAILED TO ILLUMINATE. THE R-2 DOOR SLIDE WAS REMOVED AND REPLACED. 2L72 4F A6WE 20050121000132005012100013SO 2005 1 21 SWIA200514360 120050107A5210 MECHANISM EMB 120 EMB120ER 3260203SO PAX DOOR LACK OF LUBE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07580SW 120348 PAX DOOR HARD TO OPEN. REMOVED PAX DOOR TRIM, CLEANED AND LUBED DOOR MECHANISMS, RE-INSTALLED DOOR TRIM, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050121000142005012100014EA 2005 1 21 SWIA200514361 120050109A274170609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07916SW97 97 7634 STAB CHANNEL 2 WOULD NOT ENGAGE. REMOVED AND REPLACED HSTCU PER CRJ 200 MM 27-41-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050121000152005012100015SO 2005 1 21 SWIA200514362 120050105A5230 BUSHING EMB 120 EMB120ER 3260203SO CARGO DOOR SEIZED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07562SW 120336 MCD IS VERY HARD TO OPEN/CLOSE. REMOVED AND REPLACED FORWARD INTERMEDIATE TORQUE TUBE BUSHING PER EMB 120 MM 52-11-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050121000162005012100016SO 2005 1 21 SWIA200514363 120050105A27523431001001 ACTUATOR EMB 120 EMB120ER 3260203SO NACELLE FLAP MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07580SW1131611316 120348 ON GROUND WHEN FLAPS ARE RETRACTED FROM 45 DEGREES TO UP NACELLE FLAPS ARE SLOWER THAN OTHER SEGMENTS RESULTING IN DISAGREEMENT. REMOVED AND REPLACED LEFT NACELLE FLAP ACTUATOR PER EMB 120 MM 27-50-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050121000182005012100018NM 2005 1 21 DLM88050022 120050112A3220 STRUT DOUG MD88 MD88 3023688NM NLG DISCHARGED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27921DL 49645 AFTER TAKEOFF NOSE GEAR RED LIGHT ON WITH GEAR HANDLE UP. SERVICED NOSE STRUT. 2L72 4F RTA6WE 20050121000212005012100021NM 2005 1 21 DL738050025 120050113A2530 OVEN BOEING737 737832 13844CFNM FWD GALLEY ODOR A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO273758Y 30814 FLT ATTENDANT SMELLED ELECT SMOKE FROM SEAT AT 1L DOOR. PERSISTED 3 TO 4 MIN, THEN DISSIPATED. A/C RETURNED TO JFK. FLT ATTENDANT REPORTED SMELL ONLY, NO SMOKE. SUSPECT RESIDUAL FUMES FROM DEACT OVEN, IN FWD GALLEY. REMOVED CONNECTORS FROM OVEN AND DEACT BUN WARMER. LOAD A/C ELECTRICALLY AND PERFORMED POWER RUN, NO FUMES OR SMELLS. AC RETURNED TO SERVICE. 2L72 4F RTA16WE 20050121000232005012100023NM 2005 1 21 DL76L050027 120050113A3350 FUSE BOEING767 767332 1382001NM BATTERY PACK FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27194DN 28451 SEAT E-PATH LIGHTS INOP ROWS 1-5. REPLACED FUSE ON BATTERY PACK M9008. OPS OK. 2L72 4F RTA1NM 20050121000242005012100024NM 2005 1 21 UPS05543647 120050114A2560 SMOKE GOGGLES BOEING757 75724APF 1384969NM COCKPIT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01406UP 23728 INSPECTION TYPE:N/A SMOKE GOGGLES AT AFT COURIER SEAT ARE CRACKED. REPLACED SMOKE GOGGLES. 2L72 4F RTA2NM 20050121000262005012100026NM 2005 1 21 UPS05M43648 120050116A2560 LENS DOUG MD11 MD11F 3023600NM SMOKE GOGGLES CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01250UP MIDDLE COURIER SEAT SMOKE GOGGLES LENS CRACKED. INSTALLED SMOKE GOGGLES AT MIDDLE COURIER SEAT. 2L73 4F RTA22WE 20050121000272005012100027NM 2005 1 21 DL76G050028 120050113A3350 LAMP BOEING767 767332 1382001NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE O OTHER ININSP/MAINT 1 SO271613B 32776 SEATS 2 A/B AND 2 F/G E-PATH LIGHTS INOP. RELAMPED AND REPLACED LENS, OPS CHECK OK. 2L72 4F RTA1NM 20050121000282005012100028NM 2005 1 21 05FDEA00047 120050107A5310 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25240FE 20978 REPAIR SHEAR TIE AT BS 380 BETWEEN STR 14 & 15 LT TO ACCOMPLISH 9G MOD. REPAIRED PER SRM 53-10-4. 2L73 4F RTA3WE 20050121000352005012100035EA 2005 1 21 SWIA200514366 120050111A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLT SPOILERS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TOTAKEOFF 1 NM07917SW6710 6710 7641 AFTER T/O THE FLIGHT SPOILER FAULT MESSAGE DISPLAYED ON ED2. REMOVED AND REPLACED RIGHT INBOARD FLIGHT SPOILER PCU IAW CRJ MM 27-62-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050121000372005012100037EA 2005 1 21 COMA0560036 120050106A3010 ANTI-ICE SYSTEM CNDAIRCL600 CL6002B19 1900309EA FALSE INDICATIONA COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01941CA 7050 FLIGHT 4959 ANTI ICE DUCT WARNING. COULD NOT DUPLICATE. INSPECTED AND OPERATIONAL CHECKS WERE NORMAL. 2L72 4F RTA21EA 20050121000392005012100039NM 2005 1 21 SWAA050122 120050118A555218A80101 BOLT BOEING737 7373H4 1384600NM LT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29315SW 23337 DURING SCHEDULED C4 CHECK, LT ELEVATOR CONTROL TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR CONTROL TAB BOLT PER MM. 2L72 4F RTA16WE 20050121000402005012100040NM 2005 1 21 SWAA050115 120050117A53116546526 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29606SW 27926 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 400, STRINGER 9R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20050121000412005012100041NM 2005 1 21 SWAA050116 120050117A53206545834 STRUCTURE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29606SW 27926 DURING SCHEDULED D-CHECK, FOUND ZEE CHORD AT BS 270, BETWEEN RBL 11 TO LBL 11, CORRODED. REMOVED AND REPLACED ZEE CHORD PER SRM. 2L72 4F RTA16WE 20050121000422005012100042NM 2005 1 21 SWAA050117 120050117A53106545833 WEB BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29606SW 27926 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 353, LBL 62, CORRODED. REMOVED AND REPLACED WEB PER SRM. 2L72 4F RTA16WE 20050121000442005012100044NM 2005 1 21 UPS05443664 120050107A5315 FLOORBEAM BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C M/D - BS 1500 RBL 38 FLOORBEAM FOUND CORRODED. FLOORBEAM REPAIR PARTS FABRICATED PER SRM 51-40-04 FIG 1. CORROSION BLEND OUT 0.050 X 1 X 1 INCH EXCEED SRM LIMIT. 2L74 4F A20WE 20050121000452005012100045NM 2005 1 21 UPS05443665 120050108A5313 STRINGER BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C - STRINGER END BS 990 S-9L CRACKED. STRINGER REPAIRED PER SRM 53-10-03 FIG 2. 2L74 4F A20WE 20050121000462005012100046NM 2005 1 21 UPS05443666 120050108A5313 STRINGER BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C - STRINGER END BS 990 S-7L CRACKED. STRINGER REPAIRED PER SRM 53-10-03 FIG 2. 2L74 4F A20WE 20050121000492005012100049NM 2005 1 21 SWAA050065 120050111A53306545800 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 290, STRINGER 15R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20050121000502005012100050 2005 1 21 SWIA200514367 420050111A3418C818171 TRANSDUCER EMB 120 EMB120ER 3260203SO STALL WARNING INOPERATIVE A SWIAO OTHER J WARNING INDICATION CRCRUISE 1 NM07289YV 120289 STALL WARNING SYSTEM NR 2 FAILED IN FLIGHT. REPLACED RIGHT TRANSDUCER ASSY, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050121000512005012100051EA 2005 1 21 SWIA200514368 120050110A5610 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAO OTHER O OTHER CRCRUISE 1 NM07465SW 7845 LEFT WINDSHIELD SHATTERED AT 21,200 FT. REMOVED AND REPLACED LEFT WINDSHIELD IAW 56-11-01. P/N NP139321-11, S/N OFF 03136H4230. 2L72 4F RTA21EA 20050121000522005012100052SO 2005 1 21 SWIA200514369 120050109A4900 APU EMB 120 EMB120ER 3260203SO APU BAY SMOKE A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM07218SW 120287 ON INITIAL POWER UP AFTER STARTING APU AND TURNING ON PACKS BOTH PACK FAIL LIGHTS ILLUMINATED & LAV SMOKE ALARM SOUNDED. F/A NOTED SMOKE SMELL IN CABIN. COULD NOT DUPLICATE PAC FAIL. NO DISCREPANCIES IN AIR CONDITIONING SYSTEM, GASPER FANS, APU BLEED, CROSS BLEED. OPERATIONAL CHECK GOOD. NO FURTHER BURNING SMELL. 2L72 4T RTA31SO 20050121000542005012100054NM 2005 1 21 SWAA050103 120050117A5313BAC1498 STRINGER BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29667SW 23063 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER 27L, AT BS 1016, CRACKED. REPAIRED STRINGER SECTION PER SRM. 2L72 4F RTA16WE 20050121000562005012100056NM 2005 1 21 05FDEA00101 120050116A5313 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 CENTER ACCESSORY COMPARTMENT AT STA 6-90 LONGERON R49 INSIDE STEP HAS CORROSION. CENTER ACCESSORY COMPARTMENT AT STA 6-90 LONGERON R49 INSIDE STEP REMOVED AS PER SRM 51-33-01 VOL II AND SRM 51-35-01 VOL II. LONGERON SPLICE FABRICATED AS PER DRAWING AGA7026 AND INSTALLED AS PER SRM 51-33-01 VOL II AND SRM 51-35-01 VOL II. 2L73 4F RTA22WE 20050121000572005012100057NM 2005 1 21 SWAA050072 120050112A3350604222 BATTERY BOEING737 7375H4 138449DNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29527SW 26569 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR LOWER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20050121000582005012100058WP 2005 1 21 05FDEA00109 120050117A5531AMC72691 SPAR DOUG DC10 DC1010 3022110WP ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25395FE 46629 VERTICAL STABILIZER AFT CENTER SPAR HAS CRACK STATION ZFR 328, YV237.628. REMOVED PANEL AND WEB IAW DC10 SRM 51-35-01 VOL 2. REPAIRED CENTER SPAR DOUBLER IAW FEDEX EA 8-5530-83960, STABILIZER - VERTICAL AFT CENTER SPAR DOUBLER CRACK-REPAIR. REINSTALLED PANEL AND WEB IAW DC10 SRM 51-35-01 VOL 2. 2L73 4F A22WE 20050121000592005012100059WP 2005 1 21 05FDEA00110 120050117A5751NRC6041503 BALANCE WEIGHT DOUG DC10 DC1010 3022110WP ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25395FE 46629 LEFT WING OUTBOARD AILERON CENTER BALANCE WEIGHT CORRODED. 2L73 4F A22WE 20050121000602005012100060WP 2005 1 21 05FDEA00111 120050117A5753AMC73051 HINGE DOUG DC10 DC1010 3022110WP ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25395FE 46629 LEFT WING INBOARD FLAP HINGE OUTBOARD PIVOT BUSHING GALLED AND PITTED. MEASURED BORE DIAMETER, FOUND TO BE OUT OF LIMITS IAW DAC CMM 57-52-01, ON NON-ROUTINE N00390. FABRICATED, INSTALLED AND HONED BUSHING TO A FINAL INNER DIAMETER OF .9995-1.0005 INCHES IAW DAC CMM 57-52-01 AND FEDEX EA 8-5750-83956, WINGS- LEFT HAND INBOARD FLAP, OUTBOARD HINGE BRACKET OVERSIZED PIVOT BORE- REPAIR. 2L73 4F A22WE 20050121000612005012100061NM 2005 1 21 05FDEA00113 120050117A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25465FE 21289 CRACKED FRAME BS 320 LBL 45 WL 148.5. *S/D* REPAIRED CRACKED FRAME AT BS 320, LBL 45, WL 148.5 IAW SRM 51-40-3 FIG 1 AND SRM 51-40-2 FIG 1. 2L73 4F RTA3WE 20050121000622005012100062NM 2005 1 21 QXEA200500061 120050112A2160 CONTROLLER BOMBDRDHC8 DHC8401 1390041NM TEMP UNKNOWN A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09406QX 4048 YEG - THE FLIGHT RETURNED TO GATE AFTER THE CREW WAS UNABLE TO CONTROL THE TEMPERATURE IN EITHER MANUAL OR AUTO. MAINTENANCE INSPECTED THE AIRCRAFT AND THEN CYCLED THE SHIP POWER. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050121000632005012100063NE 2005 1 21 DL73S050029 220050113A7300 SHAFT BOEING737 737232 1384475NM PWA JT8 JT8D15A 52051NE FUEL PUMP FAILED A DALAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SO27311DL 23083 709155 FUEL PUMP SHAFT SHEARED AT ROTATION. RUNWAY EXCURSION ON RETURN IN BAD WEATHER. REPLACING NR 2 ENGINE FUEL PUMP AND CONTROL. 2L72 4F4 FRTA16WE E2EA 20050121000642005012100064NM 2005 1 21 05FDEA00103 120050116A5313 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 CENTER ACCESSORY COMPARTMENT LONGERON RT 47 UNDER STEP IS CORRODED THROUGH. REPAIR LONGERON AND SPLICE FABRICATED AS PER SRM 53-10-00 VOL I FIG 2 AND INSTALLED AS PER SRM 53-10-00 VOL I FIG 2. 2L73 4F RTA22WE 20050121000652005012100065NM 2005 1 21 05FDEA00104 120050116A5313 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 CENTER ACCESSORY COMPARTMENT FORWARD OF DOOR AT LONGERON L46 LONGERON SPLICE FOUND DAMAGED. CENTER ACCESSORY COMPARTMENT FORWARD OF DOOR AT LONGERON L46 DAMAGED LONGERON SPLICE REMOVED AS PER SRM 51-33-01 VOL II AND SRM 53-00-01 VOL I. LONGERON SPLICE FABRICATED AS PER SRM 53-10-00 VOL I AND INSTALLED AS PER SRM 51-33-01 VOL II AND SRM 53-00-01 VOL I. 2L73 4F RTA22WE 20050121000662005012100066EA 2005 1 21 COMA0560028 120050109A2750860D10018 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01811CA5360 2418 7380 FLIGHT 5681 FLAPS FAIL CAUTION. REPLACED THE FECU. 2L72 4F RTA21EA 20050121000672005012100067EA 2005 1 21 COMA0560030 120050110A32304622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG UNRELIABLE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01979CA16818 7159 FLIGHT 5452 GEAR DISAGREE WARNING. REPLACED THE NLG PRIORITY VALVE. 2L72 4F RTA21EA 20050121000702005012100070EA 2005 1 21 COMA0560035 120050105A2750855D1009 POWER SUPPLY CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01442CA6263 60 7483 FLIGHT 9466 FLAPS FAIL CAUTION. REPLACED THE RIGHT BPSU. 2L72 4F RTA21EA 20050120000092005012000009NM 2005 1 20 2005UALA00053 120050112A5610 WINDSHIELD BOEING757 757222 1384956NM PWA 2037 PW2037 NE COCKPIT CRACKED A UALAA UNSCHED LANDING O OTHER CRCRUISE 1 WP29512UA 24809 DIVERTED DUE TO A CRACK IN THE CAPT SIDE WINDSHIELD, LEFT TO RIGHT EDGE WITH WINDOW HEAT ARCING. WINDOW HEAT FAILURE. REPLACED WINDOW, AND WINDOW HEAT CONTROL. 2L72 4F4 FRTA2NM E17NE 20050120000102005012000010NM 2005 1 20 05FDEA00093 120050114A5350 FAIRING BOEING727 727100 1384036NM CARGO DOOR MISSING A FDEAK NONE O OTHER ININSP/MAINT 1 SO25185FE 18871 ON ARRIVAL FOUND AFT CARGO DOOR MOVABLE FAIRING MISSING FROM AIRCRAFT. INSTALLED AFT CARGO DOOR MOVABLE FAIRING PER 727-100 MM 52-33-00-4. OPS CHECK GOOD. 2L73 4F RTA3WE 20050120000212005012000021NM 2005 1 20 2005UALA00057 120050113A5314 KEELBEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29307UA 23668 KEEL BEAM LOWER CHORD BS 685-695 IS CRACKED. TRIMMED OUT CRACKED LOWER CHORD. INSTALLED REPAIR ANGLE AND STRIP. 2L72 4F4 FRTA16WE E2GL 20050120000622005012000062WP 2005 1 20 05FDEA00087 120050112A3000DC10487250 RETAINER DOUG DC10 DC1030 3023501WP ZONE 600 BROKEN A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25308FE 48297 AT FL350 WHEN WING ANTI-ICE WAS TURNED ON THE NR 1 PNEU PRESSURE WENT TO FULL SCALE AND BOTH WING ANTI-ICE DISAGREE LIGHTS CAME ON. THE CONFIG WAS NR 1 AND NR 2 PNEU SUPPLIES OPEN 1-3 ISO VALVE OPEN, 1-2 CLOSED AND NR 1 PACK ON. NR 3 PNEU SUPPLY WAS DEFERRED PRIOR TO FLT. ACCOMP CHECK OF NR 1 PSC, NO FAULTS NOTED. FOUND RT OUTBOARD FAULT INDICATOR LOGGED ON PNEU MANIFOLD FAULT INDICATOR. CHECKED WING ANTI -ICE DUCTING AND FOUND RT NR 5 TO NR 6 RETAINER FOR INTERCONNECT JOINT DAMAGED AND INTERCONNECT JOINT NOT CONNECTED TO OUTBOARD ANTI-ICE DUCT. REMOVED AND REPLACED RETAINER AND PERI SEALS FOR INTERCONNECT DUCT. LEAK CHECK NORMAL. RAN NR 1 AND NR 3 ENGS. ALL READINGS NORMAL. 2L73 4F A22WE 20050120001372005012000137NE 2005 1 20 05FDEA00116 220050117A7200 ENGINE AIRBUS310 A310222 3930315EU PWA JT9 JT9D7R4E1 52054NE SMOKE A FDEAC ABORTED TAKEOFF EB VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SO25419FE4027 1044 345 AT 80 KTS A/C STARTED TO SHUDDER CONTINUOUSLY. A/C STARTED VEERING TO THE RIGHT REQUIRING CONTINUOUS LEFT RUDDER INPUT TO KEEP A/C ON RWY CENTERLINE. AIRPLANE BEHIND, WHO HAD TAXIED INTO POSITION & HOLD REPORTED SMOKE COMING OUT OF THE ENGINE AREA. ABORTED AT AROUND 95 KTS. NO ENGS PARAMETERS WERE EXCEEDED. 2L72 4F4 FRTA35EU E3NE 20050120001402005012000140NM 2005 1 20 AWXA200500021 120050110A335032145410 EPSU AIRBUSA319 A319132 3930340NM ZONE 242 FAULTY A AWXAK NONE O OTHER ININSP/MAINT 1 WP28807AW20213 1064 LAX - EEL - DURING THRU FLIGHT INSPECTION THE RT OVERWING EMERGENCY POWER SUPPLY UNIT WAS FOUND WITH A FAULT. MAINTENANCE REMOVED AND REPLACED RT OVERWING EMERGENCY POWER SUPPLY UNIT (12WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050121000172005012100017SO 2005 1 21 SWIA200514364 120050109A3350 SOCKET EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07580SW 120348 AFT WHITE EMERGENCY FLOOR LIGHT IS INOPERATIVE. REPLACED AFT WHITE EMERGENCY FLOOR LIGHT SOCKET ASSY. OPERATIONAL CHECK GOOD. REF 33-50-02. 2L72 4T RTA31SO 20050121000222005012100022NM 2005 1 21 DL73S050026 120050113A3320059397 BALLAST BOEING737 737232 1384475NM CABIN LIGHTS INOPERATIVE A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO27319DL 23091 CREW REPORTED ACRID SMELL THROUGHTOUT CABIN. INSP E/E COMP, CARGO BAYS, CABIN BALLAST. FOUND BALLAST OF SEAT 2CD BAD. REPLACED BALLAST. A/C OK FOR SERVICE. 2L72 4F RTA16WE 20050121000432005012100043NM 2005 1 21 SWAA050118 120050117A53106546818 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29606SW 27926 DURING SCHEDULED D-CHECK, FOUND RT AND LT CREASE BEAM WEBS BETWEEN BS 727B AND BS 747, CORRODED. REMOVED AND REPLACED CREASE BEAM WEBS PER SRM. 2L72 4F RTA16WE 20050121000472005012100047NM 2005 1 21 UPS05443667 120050109A5347 SEAT TRACK BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C - BS 1000 LBL 33 O/B SEAT TRACK FLANGE CORRODED. M/D BS 990 - 1000 LBL 33 SEAT TRACK REPAIR PARTS FABRICATED AS PER SRM 53-10-05 FIG 1A. CORROSION BLEND OUT 0.050 X 1 X 1 INCH EXCEED SRM LIMIT. 2L74 4F A20WE 20050121000482005012100048NE 2005 1 21 UPS05443672 220050119A7261 ENGINE BOEING747 747121 1384871NM PWA JT9 JT9D7A 52054NE NR 4 FAILED A IPXAO OTHER K FLUID LOSS NRNOT REPORTED 1 SO01681UP 19661 IFSD NR 4 ENGINE LOSING OIL PRESSURE CREW RECEIVED OIL PRESS LT BY PASS LT IND AND OIL QTY READ ZERO. NR 4 ENGINE SHUTDOWN. OIL FILTER COVERED WITH BLACK PASTE AND OIL DRAINED WAS BLACK. OIL IN TAILPIPE. ENGINE CHANGED SCHEDULED. R/R NR 4 ENG PER TC 5000 HIGH POWER RUN CHECK ALL RGE OPS NORMAL 2L74 4F4 F A20WE E20EA 20050121000682005012100068EA 2005 1 21 COMA0560034 120050108A5240 DOOR CNDAIRCL600 CL6002B19 1900309EA SERVICE DOOR NOISY A COMAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 SO01409CA 7441 FLIGHT 5119 EXTREMELY LOUD NOISE FROM NOSE AREA OF AIRCRAFT. FOUND 02 SERVICE DOOR OPEN. INSPECTED DOOR, NO DEFECTS. 2L72 4F RTA21EA 20050121000752005012100075NM 2005 1 21 2005UALA00035 120050107A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29577UA 26693 AFT PIT STA 1520 FRAME HAS A DENT BETWEEN STR 25L AND 26L ON UPPER FLANGE. INSTALLED ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20050121000762005012100076NM 2005 1 21 05FDEA00090 120050113A5330 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 AFT FUSELAGE, RT SIDE BEDROOM COMPARTMENT, FORWARD MOST TOP FITTING EDGE FOUND WITH CRACKED. CRACKED FITTING REMOVED PER SRM 51-33-01 VOLUME II. NEW FITTING FABRICATED PER DOUGLAS DRAWING NR: AJC7140 AND INSTALLED PER SRM 51-33-01 VOLUME II 2L73 4F RTA22WE 20050121000782005012100078NM 2005 1 21 SWAA050066 120050111A53306545765 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 500D + 3, ABOVE STRINGER 12R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20050121000792005012100079NM 2005 1 21 SWAA050092 120050115A3350D71702001 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29703SW 27837 DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT LIGHT BATTERY M1670, INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20050121000802005012100080NM 2005 1 21 SWAA050105 120050117A57536546430130 SKIN BOEING737 7373H4 1384600NM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29365SW 26576 DURING SCHEDULED 1/4D CHECK, FOUND RT WING INBOARD FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM. 2L72 4F RTA16WE 20050121000812005012100081NM 2005 1 21 UPS05643671 120050118A2721 CONTROL CABLE BOEING767 76734AF 1385212NM RUDDER TRIM OUT OF RIG A IPXAO OTHER O OTHER NRNOT REPORTED 1 SO01307UP 27760 A/C REQUIRED 5 UNITS OF RUDDER TRIM IN CLIMB, 3 UNITS IN CRUISE. T/S IN PROGRESS. ACCOMPLISHED FIM 27-21-00 FIG 109 TO STEP 36 NO FAULTS FOUND. CHECKED RUDDER RATIO CHANGER SYS PER 27-21-00-5 RUDDER TRIM CONTROL SYS AND YA YAW DAMPNER 27-21-00-5 NO FAULTS FOUND. 2L72 4F RTA1NM 20050121000842005012100084 2005 1 21 SWAA050076 420050113A2565D31354 SLIDE BOEING737 7372H4 138448CNM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29096SW 23055 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20050121000862005012100086NM 2005 1 21 SWAA050078 120050113A3350OL307IBPEGL LAMP BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29329SW 23693 DURING SCHEDULED C3 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT AT ROW 21 ABC, INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050121000872005012100087NM 2005 1 21 SWAA050079 120050113A57306545407 SKIN BOEING737 7373H4 1384600NM RT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29367SW 26578 DURING SCHEDULED C1 CHECK, FOUND RT WING LOWER SURFACE SKIN OUTBOARD OF NR 2 ENGINE PYLON MID SPAR FITTING, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20050121000882005012100088NM 2005 1 21 SWAA050080 120050113A53106546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29606SW 27926 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE IN AFT CARGO COMPARTMENT BS 767, RBL 8, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050121000892005012100089NM 2005 1 21 SWAA050081 120050113A53116546525 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29606SW 27926 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 380, STRINGER 9L, CRACKED. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20050121000922005012100092EU 2005 1 21 05FDEA00107 120050117A7333 FILTER AIRBUS300 A300F4605R 3930327EU GE CF6 CF680 30025NE NR 1 FUEL SYSTEMCLOGGED A FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25654FE 738 705209 TAKEOFF REJECTED AT 90 KTS FOR NR 1 FUEL ENG FUEL CLOG ECAM & WARNING. REMOVED AND REPLACED MAIN FUEL FILTER AS PER MM 73-12-02-4F. NO CONTAMINATION FOUND. ENG RUN AND LEAK CHECK GOOD. OK FOR SERVICE. FILTER CPN 41823. 2L72 4F4 FRTA35EU E13NE 20050121000932005012100093WP 2005 1 21 05FDEA00108 120050117A5751NRC6041503 BALANCE WEIGHT DOUG DC10 DC1010 3022110WP ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25395FE 46629 LEFT WING OUTBOARD AILERON INBOARD BALANCE WEIGHT CORRODED. REMOVED AND REPLACED LEFT WING OUTBOARD AILERON INBOARD BALANCE WEIGHT IAW FEDEX EA 8-5751- 83958, WINGS-REPLACEMENT OF CORRODED LEFT HAND, OUTBOARD AILERON BALANCE WEIGHT. 2L73 4F A22WE 20050121000942005012100094NM 2005 1 21 2005UALA00036 120050107A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29577UA 26693 AFT PIT STA 1580 FRAME HAS A DENT BETWEEN STR 25L AND 26L ON UPPER FLANGE. INSTALLED ANGLE DOUBLER. 2L72 4F4 FRTA2NM E17NE 20050121000972005012100097EU 2005 1 21 2005UALA00038 120050103A3350 BATTERY AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29483UA 1586 EMERGENCY EXIT AISLE LIGHT INOP AT SEAT 1C. REPLACED BATTERY AND CHARGER 110WL1. 2L72 4F4 FRTA28NM E40NE 20050121000982005012100098NM 2005 1 21 2005UALA00039 120050107A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29577UA 26693 FUSELAGE SKIN IS DAMAGED AT BS 1712 STR 14R. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20050121001012005012100101WP 2005 1 21 AALA20050024 120050112A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21218AA 49168 AUS - FORWARD AUXILIARY OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD AUXILIARY OVERWING EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050121001032005012100103NM 2005 1 21 SWAA050124 120050118A5755 SKIN BOEING737 7373H4 1384600NM RT WING SPOILER DEBONDED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29374SW AA1021 26582 DURING SCHEDULED C4 CHECK, FOUND RT WING NR 6 SPOILER DISBONDED. REMOVED AND REPLACED RT NR 6 SPOILER PER MM. 2L72 4F RTA16WE 20050121001042005012100104NM 2005 1 21 SWAA050125 120050118A5340907822 FITTING BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR LOWER HINGE BOX CRACKED. REMOVED AND REPLACED FWD ENTRY DOOR LOWER HINGE BOX PER SRM. 2L72 4F RTA16WE 20050121001062005012100106NM 2005 1 21 SWAA050127 120050118A53116546546 SHEAR TIE BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29680AA 23505 DURING SPV, FOUND 4 EACH SHEAR TIES BETWEEN BS 727C AND BS 767, STRINGER 4L, CRACKED. REMOVED AND REPLACED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20050121001072005012100107NM 2005 1 21 SWAA050128 120050118A5311573149 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29390SW 26593 DURING SCHEDULED C4 CHECK, FOUND L1 COCKPIT WINDOW POST UPPER CORNER, CRACKED. REPAIRED WINDOW POST PER SRM. 2L72 4F RTA16WE 20050121001092005012100109NM 2005 1 21 2005UALA00044 120050110A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29580UA 26698 MAIN CABIN, RIGHT SIDE, FLOORBEAM STA 324, RBL 28 - RBL 70, TOP T-CAP SURFACE CORRODED BEYOND LIMITS. FABRICATED & INSTALLED REPAIR STRAPS. 2L72 4F4 FRTA2NM E17NE 20050121001102005012100110NM 2005 1 21 2005UALA00045 120050110A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29580UA 26698 MAIN CABIN, RIGHT SIDE FLOORBEAM STA 365, TOP TEE CAP SURFACE CORRODED BEYOND LIMITS BL 0 - RBL 70 AT R-1 DOOR THRESHOLD. FABRICATED & INSTALLED TEE CHORD, REPAIR ANGLES AND STRAPS. 2L72 4F4 FRTA2NM E17NE 20050121001142005012100114NM 2005 1 21 2005UALA00049 120050110A2420 CSD BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE ELECTRICAL OVERSERVICED A UALAA UNSCHED LANDING W INADEQUATE Q C CRCRUISE 1 WP29921UA 25388 DIVERTED TO SLC DUE TO ELECTRICAL PROBLEMS. FOUND CSD OVERSERVICED WITH OIL. CHECKED CSD CHIP DETECTOR, ALL DIFF. PRESSURE INDICATORS, ALL OK. SERVICED OIL TO PROPER LEVEL. RAN ENGINE AT IDLE. RESIDUAL VOLTS=19, FREQS 400, 119 VOLTS ALL NORMAL. GENERATOR OPS. CHECK NORMAL. 2L72 4F4 FRTA16WE E2GL 20050121001162005012100116WP 2005 1 21 UPS05843668 120050119A33505708458503 BATTERY PACK DOUG DC8 DC871F 302199DWP EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS DO NOT CHECK. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK. OPS CHECK OK IAW 33-50-00. 2L74 4F RT4A25 20050121001172005012100117EA 2005 1 21 COMA0560031 120050107A2710 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA ELEVATOR UNKNOWN A COMAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 SO01427CA 7460 FLIGHT 5134 T/O ABORTED DUE TO STIFF ELEVATOR CONTROL. COULD NOT DUPLICATE. INSPECTED ELEVATOR CONTROL SYSTEM, NO DEFECTS FOUND. FLIGHT CHECK SATISFACTORY. 2L72 4F RTA21EA 20050121001182005012100118EA 2005 1 21 SWIA200514370 120050112A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07449SW 7699 MOVING FLAPS FROM 0 TO FLAPS 8, RECEIVED FLAPS FAIL MESSAGE. REMOVED AND REPLACED ALL LEFT AND RIGHT FLAP ACTUATORS WITH SERVICEABLE ACTUATORS IAW MM 27-53-01 AND 57-23-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050121001202005012100120EA 2005 1 21 SWIA200514372 120050112A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07957SW 7829 FLOOR LEVEL EMERGENCY LIGHTS BETWEEN ROWS 2-5 INOP. INSTALLED SERVICEABLE GREEN FLOOR LEVEL LIGHTING STRIP AT ROW 2C IAW CRJ 200 MM 33-51-00, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050121001212005012100121SO 2005 1 21 SWIA200514373 120050111A273152991 ACTUATOR EMB 120 EMB120ER 3260203SO ELEVATOR TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED DEDESCENT 1 NM07299SW 120329 ON DESCENT FROM FLIGHT LEVEL 270 A/P FAILED FOUND ELEVATOR TRIM FROZEN. REPLACED BOTH LEFT AND RIGHT ELEVATOR TRIM TAB LINEAR ACTUATORS IAW EMB 120 MM 27-32-02 AND ACCOMPLISHED CABLE TENSION IAW EMB 120 MM 27-00-01 PAGE 209 FIG 201. OPERATIONAL CHECK GOOD. P/N 5299-1, S/N OFF 735, 742. 2L72 4T RTA31SO 20050121001222005012100122EA 2005 1 21 SWIA200514374 120050113A2611 SMOKE DETECTOR CNDAIRCL600 CL6002C10 1390015EA LAVATORY CONTAMINATED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM07709SK 10159 AFT LAV SMOKE WARNING INFLIGHT FOR 5 SECONDS. F/A FOUND NO SIGN OF SMOKE OR FIRE. CLEANED SOME DUST FROM AFT LAV SMOKE DETECTOR. OPERATIONAL CHECK WITH SMOKE DETECTOR TESTER SPRAY GOOD. 2L72 4F RTA21EA 20050121001232005012100123SO 2005 1 21 SWIA200514375 120050112A3350 LAMP EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07560SW 120334 FLOOR EMERGENCY LIGHT OUT. RELAMPED WHITE FLOOR EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050121001242005012100124NM 2005 1 21 SWAA050108 120050117A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29365SW 26576 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 727E + 13, STRINGER 23L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050121001252005012100125NM 2005 1 21 SWAA050109 120050117A53306545769 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29365SW 26576 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 378, LBL 2.80, CRACKED. REPAIRED SKIN ER EA. 2L72 4F RTA16WE 20050121001282005012100128SO 2005 1 21 SWIA200514376 120050115A21332091G010800 OUTFLOW VALVE EMB 120 EMB120ER 3260203SO CABIN PRESSURE MALFUNCTIONED A SWIABGA EMER. DESCENT O2 MASK DEPLOYED UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM07301YV9384 8045 120301 RAPID DEPRESSURIZATION IN FLIGHT CABIN ALT LIGHT ILLUMINATED AND PAX O2 MASKS DEPLOYED. REMOVED AND REPLACED ELECTRO PNEUMATIC OUTFLOW VALVE IAW 21-30-03. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050121001292005012100129NM 2005 1 21 SWAA050067 120050111A3350D71701100 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29740SW 29276 DURING SCHEDULED HC1 CHECK, MID CABIN RT AND LT EMERGENCY EXIT LIGHT BATTERIES FAILED TEST. REMOVED AND REPLACED RT AND LT BATTERIES PER MM. 2L72 4F RTA16WE 20050121001302005012100130 2005 1 21 SWAA050098 420050116A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR DEPLOYED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29440LV 29835 R2 DOOR EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050121001362005012100136NM 2005 1 21 SWAA050095 120050115A5552REMP4M6 BEARING BOEING737 737301 1384611NM LT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED C4 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR BEARING AND SLEEVE ON LT CLEVIS PER MM. 2L72 4F RTA16WE 20050121001372005012100137NM 2005 1 21 SWAA050096 120050115A53306545766 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED C4 CHECK, FOUND 3 EACH FUSELAGE SKIN CRACKS BETWEEN BS 440 AND BS 480, STRINGER 10R. REPAIRED SKIN SECTIONS PER EA. 2L72 4F RTA16WE 20050121001422005012100142NM 2005 1 21 SWAA050074 120050112A57536573732 SKIN BOEING737 7373T5 1384608NM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29667SW 23063 DURING SCHEDULED 1/4D CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REPAIRED FLAP PER SRM. 2L72 4F RTA16WE 20050121001432005012100143NM 2005 1 21 SWAA050075 120050112A53106545877 DOOR FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29365SW 26576 DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR FRAME NR 3 AFT DOOR STOP CASTING CUTOUT CRACKED. REPAIRED DOOR FRAME PER TR T1-152-003. 2L72 4F RTA16WE 20050121001452005012100145EA 2005 1 21 SWIA200514378 120050112A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLT SPOILERS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07407SW1176011760 7034 RIGHT INBOARD FLIGHT SPOILER MESSAGE. REPLACED RIGHT INBOARD FLIGHT SPOILER PCU IAW MM 27-62-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050121001482005012100148NM 2005 1 21 05FDEA00089 120050113A2612 CONTROL UNIT BOEING727 727200 138407ENM FIRE DETECTOR CONTAMINATED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25270FE 22035 CARGO SMOKE IN LOWER, FORWARD CARGO COMPARTMENT. DISCHARGED NR 1 BOTTLE. CARGO SMOKE ON FRONT PANEL AND S/O'S PANEL ILLUMINATED FOR APPROXIMATELY 2 SECONDS. REMOVED AND REPLACED NR 1 LOWER CARGO COMPMENT FIRE BOTTLE, TESTS GOOD. FOUND LOWER CARGO COMPMENT CONTROL ELECTRONIC UNIT FULL OF WATER. REMOVED AND REPLACED LOWER CARGO COMPMENT CEU, TESTS GOOD. 2L73 4F RTA3WE 20050121001492005012100149NM 2005 1 21 05FDEA00091 120050114A5320AEA7330521 CHANNEL DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 MAIN DECK CARGO, FLOOR PANEL SUPPORT, J-CHANNEL UPPER SURFACE AT STA Y= 1381 BETWEEN X= 8.50 AND X= -8.50 FOUND CORRODED. NEW J-CHANNEL FABRICATED PER DRAWING NR.: AEA7392 AND INSTALLED PER SRM 51-35-01 VOLUME I. 2L73 4F RTA22WE 20050121001502005012100150EA 2005 1 21 COMA0560038 120050106A3350362624 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A COMAO OTHER O OTHER NRNOT REPORTED 1 SO01937CA 7044 FLIGHT 5164 EMERGENCY LIGHTS ARE INOP BETWEEN ROW 2-7. REPLACED THE FLEXIBLE LAMP SECTION. 2L72 4F RTA21EA 20050121001522005012100152NM 2005 1 21 SWAA050135 120050119A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29606SW 27926 DURING SCHEDULED D-CHECK, FOUND 2 EACH STRINGERS CRACKED AT BS 992, STRINGER 13R AND STRINGER 15R. REMOVED AND REPLACED STRINGER SECTIONS PER SRM. 2L72 4F RTA16WE 20050121001542005012100154NM 2005 1 21 SWAA050137 120050119A55526959227 BUSHING BOEING737 7375H4 138449DNM LT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29523SW 26565 DURING SCHEDULED C2 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 HINGE BUSHING PER MM. 2L72 4F RTA16WE 20050121001562005012100156 2005 1 21 SWAA050139 420050119A256563550 SLIDE BOEING737 7377H4 1384404NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29770SA 30589 DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050121001672005012100167NE 2005 1 21 ASMF200501005 220050111A7200 BLADE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE RT ENGINE DAMAGED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23161PL 49764 725518 DURING TRANSIT CHECK A BLADE WAS DETECTED DAMAGED BECAUSE OF FOD ON RT ENGINE. BLADE WAS BENDED ON UPPER TIP WITH .4375 INCHES OF LENGTH AND .2500 OF DEPTH. DAMAGE WAS WITHIN LIMITS IAW MM 72-00-00 AND WAS REWORKED IAW MM 72-00-00, ALL CORRECT. 2L72 4F4 FRTA6WE E9NE 20050124000252005012400025NE 2005 1 24 FE5F200500001 220050105A7320 FUEL CONTROL BOEING757 757200 1384950NM PWA PW2037PW2037M 52117NE RT ENGINE MALFUNCTIONED W FE5FBA EMER. DESCENT UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 WP03 29611 P726518 A/C WAS NORMAL OPERATION AFTER TAKE OFF. WHILE ALTITUDE 35000 FEET, THE PILOT TRIED TO CONTACT CONTROL CENTER BY HF RADIO. BUT AFTER DECREASE AIR SPEED TO 230 NM , RT ENG GOT SHUTDOWN. THE PILOT IAW QRH LOWER ALTITUDE TO 18000 FEET, FINISHED RT ENH START PROCEDURE. AFTER THAT, PILOT CHECK RT ENG INSTRUMENT SHOWED NORMAL. THE A/C LANDED SAFELY AT 14:13(LOCAL TIME). AFTER A/C LANDED, THE MAINTENANCE TECHNICIAN PERFORMED FUNCTION CHECK WAS NORMAL. NEXT DAY (JAN 06),6 TECHNICIANS FROM TAIPEI TO PALAU FOR BORESCOPE INSPECTION, AND MORE TEST AS FOLLOWS: PERFORMED BORESCOPE INSPECTION OK, IAW AMM 73-00-00 REPLACED FCU (FUEL CONTROL UNIT). CHECK ALL ENG CONCERNED WIRE AND CABLE OK. RUNNING ENG TEST OK. 2L72 4F4 FRTA2NM E17NE 20050124000482005012400048EU 2005 1 24 CX7A194J0507 120050114A2611CGAB120101 SMOKE DETECTOR SAAB SF340 340B 7860101EU CARGO BAY DEFECTIVE A CX7AA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL03302CE7174 502 340B193 DURING CLIMB SHORTLY AFTER TAKEOFF, CARGO SMOKE WARNING ILLUMINATED, RAN CHECKLIST AND DISCHARGED FIRE BOTTLE. RETURNED TO AIRPORT. AFT CARGO SMOKE DETECTOR FOUND DEFECTIVE. 2L72 4T RTA52EU 20050124000532005012400053EU 2005 1 24 CX7A194J0502 120050102A2611 WARNING LIGHT SAAB SF340 340B 7860101EU SMOKE DETECTOR FALSE INDICATIONA CX7AO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL03309CE 340B201 AVIONICS SMOKE CWP ILLUMINATED. 2L72 4T RTA52EU 20050124000552005012400055EA 2005 1 24 MASA200500032 120050113A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSBURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0775991 7422 CLOSED/SUP ASH 7173 IAD, HAD AN AFT CABIN EMERGENCY FLOOD LIGHT INOP. THE LIGHT WAS PLACED ON MEL 1/14/05. MAINTENANCE REPLACED THE BULB. 2L72 4F RTA21EA 20050124000562005012400056EU 2005 1 24 MALA050112 120050109A3020 DUCT SAAB SF340 340B 7860101EU LT INTAKE BURNED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15428XJ 340B428 LEFT INTAKE LIGHT ILLUMINATED INTERMITTENTLY ABOUT EVERY 20 SECONDS IN FLIGHT. NO OTHER ABNORMAL INDICATIONS. AIR RETURN TO DTW. MAINTENANCE FOUND LOWER DUCT BURNED. REMOVED AND REPLACED LOWER DUCT LT SIDE, OPS CHECK GOOD IAW SAAB MM 30 SN/OFFL180888, SN/ON L290548. 2L72 4T RTA52EU 20050124000592005012400059EU 2005 1 24 MALA050104 120050103A2120 SMOKE SAAB SF340 340B 7860101EU CABIN DETECTED A MALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL15443XJ 340B443 INFLIGHT TO CMX THE CREW REPORTED SMOKE IN THE CABIN. AIRCRAFT DIVERTED TO RHI. NO OTHER INFORMATION AVAILABLE AT THIS TIME. 2L72 4T RTA52EU 20050124000652005012400065NM 2005 1 24 2005UALA00027 120050101A2597 WIRE HARNESS BOEING777 777222 1385219NM PWA PW4077PW4077 NE OVEN ARCED A UALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 WP29771UA 26932 OVEN DOES NOT HEAT ENOUGH. FOUND CB POPPED. WHEN RESET CB, A VERY, VERY SERIOUS ARC OCCURRED BEHIND OVEN. LATER FOUND CHARRED WIRES BEHIND OVEN. EXAMINATION OF ANOTHER AIRCRAFT REVEALED EXTREMELY TIGHT CLAMPING OF R53 HARNESS USING TIE-WRAP ON SELF-STICK STANDOFF. IT IS NOW BELIEVED THAT THIS METHOD OF CLAMPING INDUCES CHAFING AND SUBSEQUENT CONTACT BETWEEN CONDUCTORS AND SHORT CIRCUITING. GALLEY MANUFACTURER STATES THEY DO NOT USE TIEWRAP/STICKON AS A MEANS OF WIRE SUPPORT. EG3924 ISSUED TO AFFECTED AIRCRAFT TO CHECK HARNESSES AND REMOVE TIEWRAP/STICK-ON IF INSTALLED. NO OTHER ANOMALIES REPORTED. ALERT BULLETIN "TRIPPED CIRCUIT BREAKERS - RESETTING" ISSUED 1/24/05. NO FURTHER ACTION REQUIRED. 2L72 4F4 FRTT0001SE E46NE 20050124000722005012400072EA 2005 1 24 05010695 120050110A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA LAVATORY DEFECTIVE A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27695BR 7772 TOILET SMOKE CAUTION POSTED. INSPECT COALESCER SOCKS WITH BLACK LIGHT FOR SIGNS OF OIL RUN ENGINES TO DUPLICATE CONDITION AND ISOLATE THE SOURCE (LT, RT, AND APU). INSPECT DUCTS ON BOTH SIDES FOR SIGNS OF OIL WITH BLACK LIGHT EXAMINE HEAT EXCHANGERS FOR OIL OR RESIDUAL. REPLACE SMOKE DETECTOR. 2L72 4F RTA21EA 20050124000792005012400079NM 2005 1 24 QXEA200500063 120050112A30607826895 BRUSH BLOCK DHAV DHC8 DHC8202 2809007NM ZONE 100 BURNED A QXEAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 NM09351PH6626 43 490 SEA - ON FLT NR 2047, RT TRU CAUTION MESSAGE, ALSO NR 2 SPU AUX POWER AND RT STALL WARNING ILLUMINATED AT THE SAME TIME. RT STALL WARNING WAS INTERMITTENTLY ILLUMINATING ON AND OFF THROUGHOUT FLT. MAINTENANCE FOUND NR 2 PROP BRUSH BLOCK BURNED/ARCHED. REMOVED AND REPLACED BRUSH BLOCK. PERFORMED FUNCTIONAL TEST OF PROP DE-ICE SYSTEM. RESET RT TRU CIRCUIT BREAKER. NO OTHER DEFECTS. PERFORMED STALL WARNING TEST, NO DEFECTS NOTED. ALL CAUTION LIGHTS EXTINGUISHED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050124000802005012400080WP 2005 1 24 ARWA20050101 120050111A27314710541 CRANK ASSY DOUG DC8 DC863F 302198FWP ELEVATOR TAB BROKEN A ARWAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 SO19661AV 45969 DURING FLIGHT CONDITION CHECK ON THE ELEVATOR CHECK EPI WILL NOT SATISFACTORY RESPOND TO ELEVATOR INPUTS. RETURN TO BLOCK. ON PARKING CHECK UNABLE TO SET GUST LOCK ON. FOUND RT ELEVATOR GEARED TAB INBOARD DRIVE MECHANISM CRANK ASSEMBLY BROKEN. REMOVED AND REPLACED SUBJECT CRANK ASSEMBLY IN ACCORDANCE WITH MM 27-30-3 AND OPERATIONAL CHECK IAW MM 27-30-3, FOUND SATISFACTORY. INSPECTED GUST LOCK SYSTEM, NO DEFECTS NOTICED IN ACCORDANCE WITH DC-8 MM 27-70-0. 2L74 4F 4A25 20050124000812005012400081 2005 1 24 ARWA20050103 420050113A3414 ADC DOUG DC10 DC1010 3022110WP COCKPIT MALFUNCTIONED A ARWAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO1968041 46900 ABORTED TAKEOFF AT 75 KTS DUE TO NO AIRSPEED INDICATION AND FLAG ON FIRST OFFICER'S AIRSPEED INDICATOR. RESET ANALOGUE DIGITAL CONVERTER (ADC) AND PERFORMED TEST ACCORDING TO MM 34-130. OPERATIONAL CHECK NORMAL. 2L73 4F A22WE 20050124000842005012400084NM 2005 1 24 QXEA200500011 120050103A3297471515 WIRE HARNESS BOMBDRDHC8 DHC8401 1390041NM NLG WOW FAILED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09405QX139 4047 SEA - FLIGHT 2351 - THE FLIGHT RETURNED TO FIELD AFTER TAKEOFF, THE GEAR FAILED TO RETRACT WHEN SELECTED. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE NOSE GEAR ELECTRICAL HARNESS. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050120000272005012000027WP 2005 1 20 ABXA050009 120050104A523049202331 SUPPORT FITTING DOUG DC9 DC931 3022065WP CARGO DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23929AX 45874 FORWARD LOWER CARGO DOOR SUPPORT FITTING CRACKED AT STOP BOLT HOLE. REMOVED AND REPLACED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5. 2L72 4F A6WE 20050120000282005012000028WP 2005 1 20 ABXA050013 120050105A5330591140311 SKIN DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23929AX 45874 LEFT NOSE SKIN AT STA 69.5 FORWARD OF CAPTAIN'S WINDSHIELD WIPER MOTOR NEEDED STRIPPED AT AREA MARKED. REPAIRED AREA IAW DC-9 JOB CARD EA 53100075-003-2. 2L72 4F A6WE 20050120000392005012000039WP 2005 1 20 ABXA050012 120050105A5330591140312 SKIN DOUG DC9 DC931 3022065WP FWD FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23929AX 45874 RIGHT NOSE SKIN CRACKED AT 2 RIVETS AT FS 76.5 FORWARD OF FIRST OFFICER'S WINDSHIELD WIPER MOTOR. REPAIRED AREA IAW DC-9 JOB CARD EA 53100074-003-1. 2L72 4F A6WE 20050120000422005012000042NM 2005 1 20 CALA0500006 120050111A5310655053141 DOOR FRAME BOEING737 737524 1384721NM EXT PWR DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714655 28916 INSPECTION FOUND A 2 INCH CRACK IN EXTERNAL POWER ACCESS DOOR AFT FRAME FLANGE AT STA 243.7-251.6, RBL 20 - RBL 21. REPAIRED IAW ECRA 5330-03402. 2L72 4F RTA16WE 20050120000532005012000053 2005 1 20 UPS05143661 420050117A2565 WARNING LIGHT AIRBUSA300 A300F4622R 3930360EU COCKPIT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01159UP 0848 EVACUATION SLIDE WARNING LIGHT INOP. EVAC SLIDE BUZZER AND LIGHT OPS NORMAL. THIS CLEARS M295390 PER MM 52-73-12-4 2L72 4F RTA35EU 20050120000552005012000055 2005 1 20 UPS05143670 420050119A2565 WARNING SYSTEM AIRBUSA300 A300F4622R 3930360EU DOOR SLIDE INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01122UP 0807 THE DOOR SLIDE ARMED AURAL WARNING AT THE DOOR DID NOT TEST PROPERLY PRIOR TO OPENING THE ENTRY DOOR AFTER LANDING. EVACUATION SLIDE WARNING BUZZER DEFERRED PER A300 MEL 52-73-01-2 M 295473 ASSIGNED. RESET C/B'S 2WN & 1WN PERFORMED TEST IAW AMM 25-63-00-5 THIS CLEARS M 295473 PLACARD REMOVED. 2L72 4F RTA35EU 20050120000572005012000057NM 2005 1 20 UPS05443651 120050105A5313 STRINGER BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C - BS 1680 LT S-L8 STRINGER FOUND CRACKED. STRINGER REPAIRED PER SRM 53-10-03 FIG 4. 2L74 4F A20WE 20050120000592005012000059NM 2005 1 20 UPS05443653 120050109A5347 SEAT TRACK BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C U/D - BS 480 LBL 46 SEAT TRACK CORRODED AS MARKED. U/D BS 480 - 500 LBL 46 SEAT TRACK REPAIR PARTS FABRICATED AS PER SRM 53-10-05 FIG 6. CORROSION BLEND OUT 0.050 X 1 X 2 INCHES EXCEED SRM LIMIT. 2L74 4F A20WE 20050120000612005012000061NM 2005 1 20 05FDEA00086 120050112A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 MAIN DECK CARGO, SEAT TRACK BETWEEN STA Y= 1781 TO Y= 1801, X= 47.50 FOUND CORRODED. REPAIRED IAW SRM 51-2101. 2L73 4F RTA22WE 20050120000642005012000064NM 2005 1 20 05FDEA00117 120050117A5347 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25589FE 48491 THE ONE RESTRANT (SECOND FROM CTR LINE) FOR POS 2R AFT IN MAIN CARGO COMPARTMENT IS INOP. S/M WILL NEED EXTENSIVE GROUND TIME TO PERFORM SEAT TRACK REPAIR. DUE TO FLT SCHEDULE ITEM REMAINS ON MEL. REPAIRED DAMAGED SEAT TRACK PER SRM 53-70-00 FIG 1. 2L73 4F RTA22WE 20050120000662005012000066EU 2005 1 20 05FDEA00123 120050118A5730 PANEL AIRBUS310 A310203 3930313EU LT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25413FE 397 PANEL 550GB HAS 1 EACH ELONGATED HOLE ON PANEL LAND, LEFT WING. COMPLIED WITH EA 6-5710-85600 BY INSTALLING REPAIR BUSHING. 2L72 4F RTA35EU 20050120000682005012000068NM 2005 1 20 2005UALA00051 120050111A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29503UA 24624 LEFT EXTERIOR FUSELAGE AT STA 620, STR 16L, REPAIR DOUBLER IS DENTED. REMOVED EXISTING DOUBLER AND REPLACED SKIN DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20050120000702005012000070NM 2005 1 20 2005UALA00023 120050104A2121732591E FAN BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN FAILED A UALAH DEACTIVATE SYST/CIRCUITS O OTHER CRCRUISE 1 WP29198UA 28716 ELECTRICAL SMELL IN CABIN. SMELL DISSIPATED WITH BOTH RECIRC FANS TURNED OFF. THE UNDER FLOOR LEFT RECIRCULATION FAN MOTOR FAILED. THE FAN WAS REPLACED AND THE AIRCRAFT HAS HAD NO FURTHER PROBLEMS. 2L74 4F4 FRTA20WE E24NE 20050120000722005012000072NM 2005 1 20 2005UALA00031 120050107A5322 SHEAR TIE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29577UA 26693 AFT PIT SHEAR TIE CORRODED, BS 1420 STR 28L-29L. FABRICATED AND INSTALLED NEW SHEAR-TIE. 2L72 4F4 FRTA2NM E17NE 20050121000012005012100001NM 2005 1 21 DL76S050015 120050110A3213161T11301 AXLE BOEING767 767332 1382001NM RT MLG BROKEN A DALAK NONE O OTHER ININSP/MAINT 1 SO27132DN 24981 NR 8 MAIN LANDING GEAR TIRE FOUND AT 30 DEGREE ANGLE UPON WALKAROUND INSP BY MTC, FOUND AXLE BROKEN. REPLACED SAME. REPAIRED WIRING HARNESS. 2L72 4F RTA1NM 20050121000032005012100003NM 2005 1 21 DL738050017 120050109A361032145525 SHUTOFF VALVE BOEING737 737832 13844CFNM GE CFM56 CFM567B24 NE NR 1 ENGINE MALFUNCTIONED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27378DA 30265 874845 LEFT ENGINE BLEED TRIPPED OFF AROUND 20000 FT, COULD NOT RESET. ENG DUCT PRESS WAS SPLIT L-15 AND R-40 PSI ON CLIMBOUT. T/S PER FIM. REPLACED PRECOOLER CTL VLV AND PRSOV PER MM. REPLACED REDUCER FOR BLEED AIR REG SUPPLY LINE. ALL LEAK CHECK GOOD. RAN ENG PER PFHB. PNEU SYS CKS GOOD. 2L72 4F4 FRTA16WE E00055EN 20050121000112005012100011NM 2005 1 21 CALA0500011 120050114A5210140N26249 COLLAR BOEING757 757324 1384930NM L-2 DOOR BROKEN A CALAK NONE O OTHER ININSP/MAINT 1 SW2757857 32816 THE L-2 DOOR GUST LOCK MECHANISM WAS FOUND BROKEN. THE BROKEN LOCK COLLAR WAS REPLACED IAW MM 52-11-08. 2L72 4F RTA2NM 20050121000122005012100012EA 2005 1 21 SWIA200514359 120050107A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07928SW 7701 ROW 8D FLOOR LEVEL EXIT FAILS TO ILLUMINATE. REPLACED ROW 8D FLOOR LEVEL SIGN, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050121000202005012100020NE 2005 1 21 DL76G050024 220050112A7200CF680C2B6F ENGINE BOEING767 767332 1382001NM GE CF6 CF680C2B6F 30025NE NR 2 WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO271603 30925 29695 704702 NR 2 ENG BORO INSP OF HPT STAGE 2 NOZZLES ATL/TMC TMC 5-1087. REPLACED ENGINE DUE TO FAILED BORO. 2L72 4F4 FRTA1NM E13NE 20050121000252005012100025NM 2005 1 21 UPS05543649 120050116A56101199517140 WINDOW BOEING757 75724APF 1384969NM COCKPIT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01427UP 25458 F/O'S SLIDING WINDOW DOES NOT OPEN. REMOVED AND REPLACED F/O'S SLIDING WINDOW GEARBOX IAW MM 56-11-04-4. CHECKED SATISFACTORY. 2L72 4F RTA2NM 20050121000532005012100053NM 2005 1 21 SWAA050091 120050114A53306552988 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29679AA 23291 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 947, STRINGER 21L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20050121000552005012100055NM 2005 1 21 SWAA050104 120050117A53106546569 SHEAR TIE BOEING737 7373T5 1384608NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29667SW 23063 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT AFT CARGO COMPARTMENT BS 927, RBL 3, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050121000822005012100082 2005 1 21 SWAA050123 420050118A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 & R1 DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29315SW 23337 DURING SCHEDULED C4 CHECK, FOUND L1 AND R1 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED L1 AND R1 DOOR EVAC SLIDES PER MM. 2L72 4F RTA16WE 20050121000832005012100083EA 2005 1 21 COMA0560037 120050106A2613355523255 OVERHEAT LOOP CNDAIRCL600 CL6002B19 1900309EA RT WHEELWELL MALFUNCTIONED A COMAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 SO01941CA 7050 FLIGHT 9487 ANTI ICE DUCT WARNING. REPLACED THE RIGHT WHEEL WELL SENSING LOOP. 2L72 4F RTA21EA 20050121000852005012100085NM 2005 1 21 SWAA050077 120050113A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29401WN 29813 EEPLS COVER AT ROW 1 ABC, CRACKED. REMOVED AND REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20050121000902005012100090NM 2005 1 21 SWAA050082 120050113A53116546550 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29606SW 27926 DURING SCHEDULED D-CHECK, FOUND 3 EACH FRAMES CRACKED BETWEEN BS 787 AND BS 907, STRINGER 9L. REPAIRED FRAME SECTIONS PER SRM. 2L72 4F RTA16WE 20050121000912005012100091WP 2005 1 21 05FDEA00106 120050117A30205132001 VALVE DOUG MD10 MD1010F 3022112WP ANTI ICE SYSTEM MALFUNCTIONED A FDEAC ABORTED TAKEOFF J WARNING INDICATION CRCRUISE 1 SO25374FE 46612 ENG 3 A-ICE DISAGREEMENT, LEVEL ONE ALERT ILLUMINATED STEADY WITH SWITCH IN EITHER POSITION. ENG NR 3 ANTI-ICE VALVE - INOP, FOUND OLD VALVE WAS BINDING SEVERLY AND DISAGREE LIGHT SWITCH WAS INOP ON VALVE. REMOVED AND REPLACED NR 3 NOSE COWL ANTI-ICE VALVE. 2L73 4F RTA22WE 20050121000952005012100095EA 2005 1 21 COMA0570008 120050109A2150 ACM CNDAIRCL600 CL6002C10 1390015EA SMOKE A COMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO01374CA 10090 FLIGHT 5230 SMOKE SMELL IN CABIN. COULD NOT DUPLCIATE. RAN ENGINES AND APU, NO DEFECTS FOUND. 2L72 4F RTA21EA 20050121000992005012100099NM 2005 1 21 2005UALA00040 120050106A2612 FIRE DETECTOR BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE APU MALFUNCTIONED A UALAFA ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP29911UA 25255 APU FIRE LIGHT ILLUMINATED WITH THE APU SHUTDOWN. CREW REPORTED THAT AFTER TAKEOFF THEY HAD APU FIRE WARNING INDICATION WITH THE APU SHUTDOWN. CREW DISCHARGED APU FIRE BOTTLE. APU FIRE WARNING INDICATION WENT OUT THEN BEGAN TO FLASH AND CAME BACK ON STEADY. PERFORMED TROUBLESHOOTING OF APU FIRE WARNING SYSTEM AND FOUND APU FIRE DETECTOR M334 WITH LOW RESISTANCE. REPLACED DETECTOR M334, APU FIRE BOTTLE. APU FIRE DETECTION SYSTEM TESTED NORMAL. 2L72 4F4 FRTA16WE E2GL 20050121001022005012100102NM 2005 1 21 2005UALA00042 120050110A5320 INTERCOSTAL BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29580UA 26698 MAIN CABIN AFT SIDE OF STA 365 FLOORBEAM, RBL 45 SEAT TRACK END, TOP SURFACE OF INTERCOSTAL CORRODED BEYOND LIMITS AT FLOORBEAM ATTACHMENT. FABRICATED & INSTALLED DOUBLER AND FILLER. 2L72 4F4 FRTA2NM E17NE 20050121001052005012100105NM 2005 1 21 SWAA050126 120050118A53306545772 SKIN BOEING737 7373A4 1384585NM FUSELAGE WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29669SW 23752 DURING SCHEDULED SERVICE CHECK, FOUND UPPER FUSELAGE SKIN, RT SIDE OF DORSAL FIN BETWEEN BS 870 AND BS 912, LT SIDE OF DORSAL FIN BETWEEN BS 861 AND BS 966, WORN. REPAIRED SKIN SECTIONS PER EA. 2L72 4F RTA16WE 20050121001122005012100112NM 2005 1 21 2005UALA00047 120050110A5313 STRINGER BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29905UA 25005 STATION 482 STRINGER 16R IS CRACKED. INSTALLED SPLICED REPAIR. 2L72 4F4 FRTA16WE E2GL 20050121001152005012100115NE 2005 1 21 UPS05843662 220050118A7200 ENGINE DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE NR 2 FLAMED OUT A IPXAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION APAPPROACH 1 SO01708UP 46048 NR 2 ENGINE FLAMED OUT IN FLIGHT. A/C IS OOS. PERFORMED STEP 4 UP TO FUEL FILTER REPLACEMENT ON FIGURE 139 SHEET 1 OF MM 71 00 00. TS (558010) PERFORMED ENG MAINT RUN PER MM 71-00-00-1, NO DEFECTS NOTED. A/C OK FOR SERVICE. 2L74 4F4 FRT4A25 E2GL 20050121001312005012100131NM 2005 1 21 SWAA050057 120050111A3350101331 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29326SW 23690 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EXIT SIGN LENS MISSING. REMOVED AND REPLACED LENS PER MM. 2L72 4F RTA16WE 20050121001352005012100135NM 2005 1 21 SWAA050094 120050115A53306545772 SKIN BOEING737 7373H4 1384600NM FUSELAGE WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29324SW 23414 DURING SPV, FOUND FUSELAGE SKIN BETWEEN BS 860 AND BS 880, RBL 3, WORN. REPAIRED SKIN PER ER AND SRM. 2L72 4F RTA16WE 20050121001382005012100138NM 2005 1 21 SWAA050097 120050116A2560P2070001 FLASHLIGHT BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29795SW 30606 AFT OUTBOARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT AND BATTERY PER MM. 2L72 4F RTA16WE 20050121001402005012100140EA 2005 1 21 COMA0560032 120050107A3350364911 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A COMAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01721CA 7259 FLIGHT 5681 EMERGENCY FLOOR LIGHTS INOP AT ROW 1 AND 2. REPLACED THE FLEXIBLE LIGHT STRIP. 2L72 4F RTA21EA 20050121001442005012100144SO 2005 1 21 SWIA200514377 120050115A3520 DOOR EMB 120 EMB120ER 3260203SO O2 MASK BLOCKED A SWIAG O2 MASK DEPLOYED O OTHER CRCRUISE 1 NM07301YV 120301 PAX O2 MASKS DROPPED DURING DEPRESSURIZATION. MASKS IN ROW 3 DID NOT DROP. CREW MASKS WERE DEPLOYED. CLEANED THE USED MASKS AND RE-PACKED AND STOWED. ROW 3 PAX O3 MASK DOOR INTERFERES WITH ADJACENT ACCESS PANEL. TRIMMED EDGE OF ACCESS PANEL AS NEEDED TO PROVIDE CLEARANCE FOR O2 MASK DOOR. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050124000122005012400012 2005 1 24 ASMF200501011 420050117A2200 COMPUTER DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE COCKPIT MALFUNCTIONED W ASMFD RETURN TO BLOCK GJ MULTIPLE FAILURE WARNING INDICATION TXTAXI/GRND HDL 1 SW23861LF 49826 AIRCRAFT RETURNED TO PLATFORM DURING ENGINES STARTING AND GENERATORS SWITCHING FD AND SPD FLAGS WERE SHOWN ON LT ADI, LT FMA AND RT FP WERE INOPERATIVE, YAW DAMPER WAS OFF AND MACH TRIM INOPERATIVE ANNUNCIATOR LIGHTS CAME ON. AT PLATFORM, BOTH DFGC COMPUTERS WERE RESET TROUGH THEIR CIRCUIT BREAKERS E-8, E-9, E-20 AND E-21 IAW MM 22-01-01. FD TEST WAS PERFORMED , ALL CORRECT. 2L72 4F4 FRTA6WE E9NE 20050124000902005012400090 2005 1 24 SA05004 420050105A2565D31516113 SLIDE AIRBUSA319 A319112 3930323EU PASSENGER CABIN READS LOW A USAAK NONE O OTHER ININSP/MAINT 1 EA19741UW136415352 1269 TPA - THE R-1 DOOR SLIDE INDICATED LOW PRESSURE. MAINTENANCE REPLACED THE R-1 DOOR SLIDE. OK FOR SERVICE. 2L72 4F RTA28NM 20050124001002005012400100EU 2005 1 24 AWXA200500056 120050103A3397D9299200900200 WIRE HARNESS AIRBUS320 A320232 3930326EU SEAT ROW 13 LT BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28656AW 1079 PHX - EEL - DURING P-02 CHECK FUNCTIONAL TEST OF EMERGENCY LIGHT SYSTEM THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 13 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT WIRE HARNESS FROM BULKHEAD DISCONNECT TO LIGHT ASSEMBLY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050124001022005012400102EU 2005 1 24 AWXA200500058 120050111A5347D53371110001 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28621AW 053 SAL - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON RT INBOARD SEAT TRACK BETWEEN FS 42 AND FS 44. MAINTENANCE REMOVED CORRODED RT INBOARD SEAT TRACK FROM FS 42 TO FS 44; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050124001052005012400105NM 2005 1 24 AWXA200500048 120050107A533065C45772 SKIN BOEING737 737300 1384610NM FUSELAGE CHAFED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 MCN - MAJOR REPAIR - DURING 8-DAY CHECK FUSELAGE SKIN WAS FOUND CHAFED IN 3 PLACES BELOW DORSAL FIN AT BS 860, STR 1. MAINTENANCE TRIMMED DAMAGED AREAS ON FUSELAGE SKIN AT BS 860, STR 1; FABRICATED -1, -8, -9, AND -10 FILLERS, AND 3 EACH WEAR STRIPS AND REPAIR STRAPS; INSTALLED REPAIR PARTS IAW E.R. 03-5300-05016-SS1. 2L72 4F RTA16WE 20050124001122005012400112WP 2005 1 24 WX0500001 120050102A3260 PROXIMITY SWITCH DOUG DC9 DC983 3022083WP MLG DIRTY A WX0AL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 WP19891GA 49423 LAS - ON FINAL APPROACH WITH GEAR AND FLAPS DOWN, HAD GEAR UNSAFE LIGHT AND HORN LEFT MAIN. WENT AROUND AND CYCLED GEAR WITH NO FURTHER INDICATIONS. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND MASKING TAPE AND DEBRIS ON LEFT MAIN GEAR DOWN LOCK PROXIMITY SWITCH. MAINTENANCE REMOVED AND CLEANED PROXIMITY SWITCH, PERFORMED BITE TEST IAW MM 32-60-04. NO FAULTS SHOWN. AIRCRAFT RETURNED TO SERVICE 2L72 4F RTA6WE 20050124001132005012400113WP 2005 1 24 WX0500004 120050107A2780833605 PSEU DOUG DC9 DC983 3022083WP SLATS FAILED A WX0AC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP19863GA 49911 CUN - CREW REPORTED SLATS ANNUNCIATOR WARNING DURING TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE. MAINTENANCE PERFORMED AUTO TEST ON PSEU, TEST SHOWED INTERNAL FAULTS 580, 620 AND 840. DISAGREE LIGHT STAYED ILLUMINATED AFTER RERACK OF PSEU AND RESET OF BREAKER AND POWER DOWN. MAINTENANCE REMOVED AND REPLACED PSEU IAW 27-81-00. BITE TEST GOOD, DISAGREE LIGHT EXTINGUISHED IMMEDIATELY AND AFTER OPERATIONAL CHECK OF SLATS. AIRCRAFT RETURNED TO SERVICE . 2L72 4F RTA6WE 20050124001142005012400114WP 2005 1 24 WX0500006 120050111A33507732 LAMP DOUG DC9 DC987 3022087WP EMERGENCY LIGHT INOPERATIVE A WX0AK NONE O OTHER ININSP/MAINT 1 WP19948MA 49778 LAS - MAINTENANCE DISCOVERED ROW 27 EMERGENCY TRACK LIGHT MISSING LAMP AND LENS AND ROW 29 EMERGENCY TRACK LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BULB AND INSTALLED A NEW LENS AT ROW 27 AND REPLACED THE BULB AT ROW 29 IAW 33-53-01. EMERGENCY TRACK LIGHTING SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE . 2L72 4F RTA6WE 20050124001172005012400117WP 2005 1 24 WX0500002 120050104A3350 BULB DOUG DC9 DC987 3022087WP EMERGENCY LIGHT INOPERATIVE A WX0AK NONE O OTHER ININSP/MAINT 1 WP19948MA 49778 LAS - MAINTENANCE REPORTED OVERHEAD EMERGENCY LIGHTS AT ROW 18, 20 AND 22 INOPERATIVE. MAINTENANCE REPLACED BULBS IAW AMM 33-52-00-05. SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE . 2L72 4F RTA6WE 20050124001232005012400123NM 2005 1 24 QXEA200500055 120050110A6120 AUTOFEATHER SYS DHAV DHC8 DHC8202 2809007NM MALFUNCTIONED A QXEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM09357PH 504 YVR FLIGHT NR 2185 ABORTED TAKEOFF, AUTOFEATHER DID NOT ARM ON TAKEOFF ROLL. PLACED ON MEL. 2H72 4T RTA13NM 20050124001262005012400126EU 2005 1 24 CX7A194J0508 120050117A2612472326 FIRE LOOP SAAB SF340 340B 7860101EU NR 2 ENGINE CHAFED A CX7AD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL03300CE 340B184 NR 2 ENGINE SPORADIC SHORT FIRE WARNINGS AT LOW POWER SETTINGS, FIRE DETECT FAIL CAME ON, ON THE GROUND AND WENT OUT. 2L72 4T RTA52EU 20050124001272005012400127NM 2005 1 24 QXEA200500030 120050105A521085210246001 DOOR DHAV DHC8 DHC8202 2809007NM MAIN CABIN DOOR DIRTY A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09353PH16981 496 PDX - FLIGHT 2197 - THE FLIGHT ATTENDANT REPORTS THE MAIN CABIN DOOR IS DIFFICULT TO OPEN AND CLOSE. MAINTENANCE INSPECTED THE DOOR AND CLEANED AND LUBED SAME. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050124001282005012400128NM 2005 1 24 QXEA200500031 120050104A521085210246001 DOOR DHAV DHC8 DHC8202 2809007NM MAIN PAX DIRTY A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09345PH17866 476 SEA - FLIGHT 2235 - CREW REPORTS THE MAIN CABIN DOOR DIFFICULT TO OPEN. MAINTENANCE INSPECTED THE DOOR AND CLEANED THE DEBRIS FROM SAME. OPERATIONAL CHECKS WERE PERFORMED AND WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050124001292005012400129SO 2005 1 24 RAIA00501011 120050105A3610S2U2228 SEAL EMB 145 EMB145LR 3260212SO BLEED LINE FAILED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03813HK 145044 5771- STL- BLEED NR 2 LEAK DURING CLIMB-OUT. MAINTENANCE, REMOVED AND REPLACED SEALS IN BLEED LINE UNDER SEAT 18A. 2L72 4T RTT00011AT 20050124001312005012400131EU 2005 1 24 RAIA00501012 120050105A2731 SWITCH JETAIRJETSTMJETSTM4101 1500501EU ELEVATOR TRIM OUT OF ADJUST A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03566HK 41084 5490- STL- CONFIG WARNING AT 68KTS. MAINTENANCE ADJUSTED ELEVATOR TRIM SWITCH. 2L72 4T RTA41NM 20050124001322005012400132 2005 1 24 RAIA00501010 420050105A34257003110901 INDICATOR JETAIRJETSTMJETSTM4101 1500501EU EHSI FAILED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03568HK16560 41086 3637- PIT- EHSI SCREEN FAILED DURING TAXI OUT. MAINTENANC, REMOVED AND REPLACED EHSI SCREEN. 2L72 4T RTA41NM 20050124001332005012400133SO 2005 1 24 RAIA00501013 120050105A3350 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCONNECTED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03817HK 145058 MX- STL- EMERGENCY OVERWING EXIT LIGHT INOP. MAINTENANCE RE-SECURED CONNECTOR ON EMERGENCY EXIT LIGHT. 2L72 4T RTT00011AT 20050124001342005012400134EU 2005 1 24 RAIA00501017 120050108A2760 WARNING LIGHT JETAIRJETSTMJETSTM4101 1500501EU SPOILERS ILLUMINATED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03568HK 41086 3666- GSO- LEFT SPOILER LIGHT CAME ON DURING TAXING. MAINTENANCE, DEFERRED SPOILERS PER MEL 27-3 CAT C. 2L72 4T RTA41NM 20050124001352005012400135SO 2005 1 24 RAIA00501022 120050105A3260852701 PROXIMITY SWITCH EMB 145 EMB145 3260210SO MLG MALFUNCTIONED A RAIAO OTHER J WARNING INDICATION LDLANDING 1 CE03804HK2756 145082 3522- PIT- AIR/ GROUND EICAS MESSAGE FAIL. MAINTENANCE REMOVED AND REPLACED MLG WOW PROXY SWITCH. 2L72 4F RTT00011AT 20050124001362005012400136EU 2005 1 24 YENA200502 120050103A2121VD390003 FAN AIRBUS320 A320232 3930326EU RECIRCULATION BURNED A YENAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15527JB13669 1557 AT 37,000 FT SMELLED STRONG SULFUR ODOR IN C/P. SHORTLY AFTER, SAME SMELL REPORTED IN AFT MAIN CABIN (NO SMELL IN LAVS). SMELL DISAPPEARED AFTER 2-3 MIN. ABOUT 5 MIN LATER, STRONG BURNING ELECTRICAL SMELL IN C/P PLUS THROUGHOUT CABIN. RAN SMOKE/AVIONICS SMOKE CHECKLIST AND SMELL DISAPPEARED. EMERGENCY DIVERTED. PERFORMED TSM NR 24-00-00-810-823 FOUND LT CABIN RECIRC FAN SUPPLY C/B POPPED (15HG). VERIFIED ASSOCIATED WIRING INTEGRITY FOR 15HG AND VISUALLY VERIFIED FAN 15HG CAUSE OF ODOR. ITEM WAS TRANSFERRED PER MEL 21-21-01. UPON ARRIVAL AT JFK CABIN RECIRCULATION FAN (15HG) REPLACED IAW AMM 21-21-51. ALL OPS CHECK OK. 2L72 4F RTA28NM 20050124001392005012400139NM 2005 1 24 05FDEA00112 120050117A2800 WARNING LIGHT DOUG MD11 MD11 3023602NM COCKPIT ILLUMINATED A FDEAJA DUMP FUEL UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO25584FE 48436 AT FL310 WITH FUEL SYSTEM AUTO LVL 2 ALERT "TNK WING OVERFILL". COMPLIED WITH QRH PROCEDURES. WITH FUEL SYSTEM IN MANUAL & CROSS FEED MANIFOLD PRESSURIZED) RECEIVED SAME LVL 2 ALERT "TANK WING OVERFILL". SWITCHED TO AUTO (OPPOSITE CONTROLLER) ALERT WENT OUT & FUEL FAILED TO PUMP FROM AUX TO FILL TANK 1,2 OR 3 WITH AUX FUEL AT 10.5. DUMPED FUEL (90K) & RTN TO KIX. MEL: ACN RELEASED PER MEL/CDL: 28-21-03-02. EXPIRES 26JAN05 MAIN TANK 2 FILL VALVE - INOP CLOSED. KIX: MX REPLACED CRACKED FUEL MANIFOLD ASSY, FUEL SHUT OFF VALVE BODY ASSY AND CONTROLLER ASSY. OPS CHECKED OK PER MM. RETURNED TO SERVICE. . 2L73 4F RTA22WE 20050124001402005012400140 2005 1 24 P9RA20050064 420050107A2565S10225 PROXIMITY SENSOR BOEING757 757236 1384971NM R4 DOOR SLIDE DIRTY A P9RAK NONE O OTHER ININSP/MAINT 1 SO11522NA 25133 AIRCRAFT IN MAINTENANCE CCS, DOOR 4R SLIDE ARM LIGHT INOPERATIVE. PLACARDED AND PLACED ON MEL. MAINTENANCE ENTRY 1-08-2005 SFB REF MEL 25-66-5. CLEANED SWITCH CONTACTS. OPS CHECKED GOOD AND CLEARED MEL. NO PARTS CHANGED. 2L72 4F RTA2NM 20050124001412005012400141SO 2005 1 24 RAIA00501009 120050105A3020C1460092 VALVE EMB 145 EMB145LR 3260212SO ANTI-ICE SYSTEM FAILED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03818HK6704 145059 ENGINE NR 1 ANTI-ICE FAIL MESSAGE. DEFERRED NR 1 ENGINE ANTI-ICE PER MEL 30-21-01 CAT C. REMOVED AND REPLACED NR 1 ENGINE ANTI-ICE VALVE. 2L72 4T RTT00011AT 20050124001422005012400142NM 2005 1 24 QXEA200500054 120050109A213192146A010401 CONTROLLER BOMBDRDHC8 DHC8401 1390041NM ZONE 200 FAILED A QXEAO OTHER J WARNING INDICATION DEDESCENT 1 NM09413QX2410 4060 LAX - FLIGHT 2342 - THE AIRCRAFT STARTED TO LOSE PRESSURIZATION WHILE FLYING THROUGH MODERATE TURBULANCE AND STRONG UP AND DOWN DRAFTS. THE FLIGHT ATTENDANT REPORTED HEARING NOISES FROM THE GALLEY SERVICE DOOR. MAINTENANCE INSPECTED THE GALLEY SERVICE DOOR AND FOUND NO DEFECTS. THE AUTO PRESSURE CONTROL WAS PLACED ON MEL. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. SDR TO REMAIN OPEN PENDING CLOSURE OF THE MEL. GEG CLEAANED ICE FROM THE AFT SERVICE DOOR AND REPLACED THE AUTO PRESSURE CONTROLLER. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050124001432005012400143WP 2005 1 24 AALA20050020 120050110A3397021975003 WIRE HARNESS DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW2159523 49915 DFW EMERGENCY ESCAPE PATH LIGHT HARNESS AT SEAT 4EF INOPERATIVE. REPLACED HARNESS. SYSTEM GROUND CHECKED NORMAL OPERATION. (SUPP CLOSED) 2L72 4F A6WE 20050125000022005012500002CE 2005 1 25 DXTA200500546 120050119A323099141961 CONTROL MODULE CESSNA650 650 2076802CE MLG MALFUNCTIONED E DXTAO OTHER J WARNING INDICATION APAPPROACH 1 GL07792QS2929 6507092 GEAR WOULD NOT EXTEND, ATTEMPTED SECOND TIME AFTER SEVERAL MINUTES LEFT AND RIGHT MAINS EXTENDED. THEN AFTER 30 OR SO SECONDS NOSE CAME DOWN. TROUBLESHOT PROBLEM TO LANDING GEAR CONTROLLER. INSTALLED REPAIRED LANDING GEAR CONTROLLER. PERFORMED TIMED EXTEND RETRACT TEST. CHECKED GOOD. PERFORMED LOGIC MODULE CIRCUIT TEST. CHECKED GOOD. PERFORMED LANDING GEAR ADJUSTMENT TEST CHECKED GOOD WORK DONE IAW CHAP 32-46-00 OF THE CE650 MM. 2L72 4F A9NM 20050125000032005012500003CE 2005 1 25 DXTA200500547 120050119A3230 BLOCK CESSNA750 750 2076810CE MLG LOOSE E DXTAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL07903QS 7500162 DURING CLIMBOUT TO ALTITUDE HEARD KNOCKING NOISE AND FELT BUMP FROM NOSE WHEEL AREA SEVERAL TIMES. FOUND RT NOSE LANDING GEAR PILLOW BLOCK LOOSE. REMOVED AND INSTALLED NEW BLOCK ASSY, OPS CHECK NORMAL WORK IAW CESSNA 750 MM CHPT 32-30-00. 2L72 4J RTT00007WI 20050125000042005012500004NE 2005 1 25 DXTA200500550 220050122A720030358005D ENGINE CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE LEFT STOPPED E DXTAO OTHER YJ ENGINE STOPPAGE WARNING INDICATION TXTAXI/GRND HDL 1 GL07313QS4584 5600325 PCE500135 ON COMPLETION OF THE SPOILER TEST THE LT ENGINE QUITS. OPERATED SPEED BRAKES THRU SEVERAL CYCLES, VERIFIED 85 PERCENT SWITCHES RETRACT THE SPEED BRAKES, PERFORMED SEVERAL SLAM CHECKS OF LEFT AND RIGHT ENGINES. NO DEFECTS NOTED, SPEED BRAKES AND ENGINE THROTTLE CONTROL SYSTEMS OPERATE NORMALLY AT THIS TIME. ALL WORK PERFORMED IAW CE 560 M/M 27-61-00 AND 76-11-00. 2L72 4F4 FRTA22CE E25EA 20050125000052005012500005EA 2005 1 25 SWIA200514408 120050115A5610 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07918SW 7645 CAPTAINS SIDE WINDOW HAS MULTIPLE CRACKS THAT SPAN THE LENGTH OF WINDOWS. REMOVED AND REPLACED LT SIDE WINDOW IAW AMM 56-12-01. P/N NP139322-5, S/N OFF 01352H5316. 2L72 4F RTA21EA 20050125000062005012500006CE 2005 1 25 DXTA200500551 120050122A3297UNK WIRE HARNESS CESSNA560 560XL 2076702CE MLG CHAFED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07650QS 5605150 DURING APPROACH, SELECTED GEAR DOWN, HEARD THE GEAR DEPLOY BUT GOT NO SAFE LIGHT INDICATION. GEAR WARN C/B POPPED & RESET IT TO FIND 3 GREEN, LANDED NORMAL. TROUBLESHOT FAULT WITH TEAM XL AND ISOLATED FAULT TO A CHAFED WIRE HARNESS IN THE LEFT WHEEL. REPAIRED HARNESS AND THE OPERATIONAL CHECKS WERE GOOD IN ACCORDANCE WITH THE 560 XL MM 32-20-00. 2L72 4F RTA22CE 20050125000082005012500008CE 2005 1 25 DXTA200500543 120050119A5320661503513 ATTACH BRACKET CESSNA560 560XL 2076702CE ACM CRACKED E DXTAK NONE O OTHER ININSP/MAINT 1 GL07645QS 5605145 ACM SUPPORT BRACKET CRACKED WHERE RUDDER BIAS CONTROL VALVE ATTACHES. REMOVED AND REPLACED THE CRACKED BRACKET IAW THE 560 XL MM 21-50-00 SRM 51-40-03; 04; 06; AND 08. 2L72 4F RTA22CE 20050125000112005012500011EA 2005 1 25 COMA0560054 120050118A2750 DRIVE SHAFT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS LACK OF LUBE A COMAO OTHER WJ INADEQUATE Q C WARNING INDICATION APAPPROACH 1 SO01470CA 7650 FLIGHT 5342 DURING APPROACH TO CVG RECEIVED A FLAP FAIL MESSAGE. LUBRICATED THE FLAP FLEX DRIVE SHAFTS. 2L72 4F RTA21EA 20050125000142005012500014EU 2005 1 25 MALA050133 120050113A5610NF20216526 WINDSCREEN BAC 146 AVRO146RJ85A1500097EU COCKPIT DELAMINATED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15535XJ E2371 F/O'S A SCREEN LAMINATION FAILED. MAINTENANCE REPLACED F/O'S A SCREEN P/N OFF NF20216-526, P/N ON SPSBAS146-1-2-1, S/N 26 IAW AVRO MM 56-10-11. 2H74 4F RTA49EU 20050125000152005012500015EU 2005 1 25 MALA050134 120050113A3020NH24668 DUCT SAAB SF340 340B 7860101EU INTAKE HEAT DAMAGED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15415XJ 340B415 RIGHT INTAKE HEAT INOP. AIR RETURN TO MEM. MAINTENANCE REPLACED RIGHT LOWER INLET DUCT REFER AMM CHAP 30 P/N ON/OFF NH24668, S/N OFF L211774, S/N ON L197704. TEST IS GOOD. 2L72 4T RTA52EU 20050125000172005012500017EU 2005 1 25 MALA050115 120050118A5320 SEAT TRACK SAAB SF340 340B 7860101EU FUSLEAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15360PX 340B220 DURING 6Y/4Y INSPECTION IN YYC, SEAT TRACK AT LBL 18.3 CORRODED OUT OF LIMITS FROM FS 520 TO FS 686.888. DAMAGE WILL BE REPAIRED IAW MESABA EO S53060. AIRCRAFT RETURNED TO SERVICE 1/18/05. 2L72 4T RTA52EU 20050125000192005012500019EU 2005 1 25 MALA050139 120050118A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15360PX 340B220 DURING 6Y/4Y INSPECTION IN YYC, GALLEY SEAT TRACK P/N 7253721-459 IS CORRODED OUT OF LIMITS AND WILL BE REPLACED IAW SRM 51-40-27. AIRCRAFT RETURNED TO SERVICE 01/18/2005. 2L72 4T RTA52EU 20050125000202005012500020EU 2005 1 25 MALA050140 120050120A5410NF24668057 INLET SAAB SF340 340B 7860101EU LT NACELLE CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15360PX 340B220 DURING 6Y/4Y INSPECTION IN YYC, LT NACELLE, INLET PROTECTION DEVICE P/N NF24668-057 IS CHAFED COMPLETELY THROUGH AND IS BEING REPLACED. AIRCRAFT RETURNED TO SERVICE 01/18/2005. 2L72 4T RTA52EU 20050125000212005012500021NM 2005 1 25 05FDEA00073 120050111A5310 CREASE BEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25235FE 21329 CORROSION ON CREASE BEAM BS 450, RBL 60, WL 208. *S/D* REPAIRED IAW SRM 53-10-1. 2L73 4F RTA3WE 20050125000232005012500023EA 2005 1 25 SWIA200514407 120050118A2720DL2428M9MOD1 ACTUATOR CNDAIRCL600 CL6002C10 1390015EA RUDDER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07710SK 10170 RUDDER LIMIT FAULT STATUS MSG. APPEARED ON INITIAL POWER UP. REMOVED AND REPLACED NR 2 RUDDER LIMITER ACTUATOR IAW CRJ700 MM 27-25-03. OPERATIONAL CHECKS GOOD IAW CHAPTER 27-25-00. P/N DL2428M9MOD1, S/N 0604. 2L72 4F RTA21EA 20050125000252005012500025EU 2005 1 25 MALA050130 120050110A7710 CONNECTOR SAAB SF340 340B 7860101EU DECU LOOSE A MALAO OTHER N FALSE WARNING DEDESCENT 1 GL15403XJ 340B403 LEFT PROP NP INDICATION WENT TO ZERO WHEN PROPS WENT TO MAX ON FINAL. AFTER LANDING IT WENT BACK TO NORMAL. MAINTENANCE COULD NOT DUPLICATE PROBLEM. UPON INSPECTION OFF LEFT ENGINE YELLOW HARNESS FOUND CONNECTOR TO DECU EXTREMELY LOOSE AND CONNECTOR TO NP SENSOR ALSO LOOSE. TIGHTENED CANNON PLUGS. OPS CHECK OK. 2L72 4T RTA52EU 20050125000272005012500027NM 2005 1 25 UPS05243686 120050110A5754 BRACKET BOEING727 727185C 138406NNM NR 1 KRUGER FLAPCRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 INSPECTION TYPE:C, NR 1 KRUEGER FLAP TRUNNION BRACKET IS CRACKED ON O/B SIDE. BRACKET REPLACED IAW DRG 65-16275. 2L73 4F A3WE 20050125000312005012500031NM 2005 1 25 UPS05443675 120050106A5711 SPAR BOEING747 747123 1384873NM LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C, LT WING UPPER REAR SPAR SIDE OF BODY SPLICE FOUND CRACK AT NR 1 HOLE AT SPAR CHORD (REFER FIGURE FOR DETAILS ). HOLE REPAIRED AS PER S/B 747-57A2314. 2L74 4F A20WE 20050125000322005012500032NM 2005 1 25 UPS05443676 120050108A5710 SPLICE BOEING747 747123 1384873NM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE: C, RIGHT WING STA 1241 UPPER REAR SPAR SIDE - OF - BODY SPLICE PLATE AREA FOUND HOLE NR 3 CRACKED AT WING UPPER SKIN AND INTERNAL SPLICE FITTING APPROX 0.040 INCH REFER ATTACHED SKETCH. HOLE REPAIRED AS PER SB 747-57A2314. 2L74 4F A20WE 20050125000352005012500035SO 2005 1 25 C2XA05CL002 120050109A21508166501 CONDENSER EMB 145 EMB145XR 3260214SO NR 1 PACK DIRTY A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SW27241036036 145645 CLE FLIGHT 2484 THE CREW REPORTED THE NR 1 PACK EMITS STRONG ODOR WHEN BLEED OUTPUT IS LOW. MAINTENANCE INSPECTED AND RELEASED A/C IAW MEL 21-51-00/2. MAINTENANCE REPLACED THE MIXER CONDENSOR. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RT 20050125000382005012500038NM 2005 1 25 SWAA050169 120050122A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SPV, FOUND FUSELAGE SKIN AT BS 759, STRINGER 19R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050125000402005012500040NM 2005 1 25 SWAA050171 120050122A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SPV, FOUND FUSELAGE SKIN AT BS 911, STRINGER 25L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050125000412005012500041 2005 1 25 SWAA050172 420050122A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF LIMITS A SWAAK NONE O OTHER ININSP/MAINT 1 SW29630WN 27705 DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EVAC SLIDE IND OUT OF LIMITS. REMOVED AND REPLACED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050125000422005012500042 2005 1 25 SWAA050173 420050122A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29623SW 27933 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050125000432005012500043NM 2005 1 25 SWAA050174 120050123A3350101114 LAMP BOEING737 7373A4 1384585NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29678AA 23290 DURING SCHEDULED A2 CHECK, FOUND AFT ENTRY DOOR LOWER EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM. 2L72 4F RTA16WE 20050125000442005012500044NM 2005 1 25 SWAA050175 120050123A2752569670 MOTOR BOEING737 7373G7 1384595NM TE FLAPS FAULTY A SWAAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SW29691WN 23781 AIR TURNBACK, DECLARED EMERGENCY. AFTER TAKEOFF FLAPS WOULD NOT RETRACT OR EXTEND. REMOVED AND REPLACED FLAP DRIVE MOTOR PER MM. 2L72 4F RTA16WE 20050125000482005012500048NM 2005 1 25 SWAA050179 120050123A52106545871132 GUSSET BOEING737 7373H4 1384600NM PAX DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29653SW 28398 DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR AFT LWR CORNER GUSSET, CRACKED. REMOVED AND REPLACED SERVICE DOOR PER MM. 2L72 4F RTA16WE 20050125000492005012500049WP 2005 1 25 DXTA200500541 220050114A73108975131 FILTER ELEMENT RAYTHNDH125 HAWKER800XP 7150012CE GARRTTTFE731TFE7315R 01518WP FUEL SYSTEM CLOGGED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07873QS 258573 P107689 LEFT ENG FUEL LOOKUP LIGHT ILLUMINATED ON TAKEOFF ROLL FOLLOWING APPLICATION OF TAKEOFF POWER. REMOVED AND REPLACED LT & RT ENGINE FUEL FILTERS USING CUSTOMER SUPPLIED FILTERS. RAN A/C AND CHECKED FOR LEAKS, NO LEAKS NOTED. OPS CHECK GOOD. WORK DONE IAW TFE 731 5BR M/M 73-21-02. 2L72 4F4 FRTA3EU E6WE 20050125000502005012500050EA 2005 1 25 COMA0560065 120050120A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01797CA 7344 FLIGHT 5790 RECEIVED A FLAP FAIL CAUTION MESSAGE AFTER PUSHBACK FROM ATL GATE. AIRCRAFT RETURNED TO THE GATE. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE FIRST EVENT, MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2L72 4F RTA21EA 20050125000532005012500053WP 2005 1 25 AALA20050038 120050121A2740 MOTOR DOUG DC9 DC982 3022082WP STAB TRIM INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW21218AA 49168 ORD - EN ROUTE ORD-DCA LEVELING OFF AT 5000 FEET WITH AUTOPILOT ON, AUTOPILOT TRIM LIGHT CAME ON WITH NOSE UP PITCH. DISCONNECTED AUTOPILOT AND RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED ALT STABILIZER TRIM MOTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050125000552005012500055WP 2005 1 25 AALA20050040 120050123A3350 CHARGER DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW21422AA 49334 TUL - EN ROUTE STL-DFW BATTERY CHARGER LIGHT CAME ON. CIRCUIT BREAKER POPPED. LANDED TUL WITHOUT INCIDENT. REPLACED BATTERY CHARGER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050125000572005012500057CE 2005 1 25 DXTA200500544 120050120A5320661503515 SUPPORT BRACKET CESSNA560 560XL 2076702CE FUSELAGE CRACKED E DXTAK NONE O OTHER ININSP/MAINT 1 GL07645QS 5605145 THE RIGHT SIDE SUPPORT BRACKET IS CRACKED C/T THE ECM. REMOVED AND REPLACED BRACKET REF 560XL IPC 21-51-00 AND 560XL SRM 51-40-03. 2L72 4F RTA22CE 20050125000592005012500059CE 2005 1 25 DXTA200500542 120050118A2720 PITCH CONTROL CESSNA750 750 2076810CE COCKPIT ILLUMINATED E DXTABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07971QS 7500071 SHORTLY AFTER DEPARTURE IAD PITCH FEEL FAIL AMBER CAS MESSAGE ILLUMINATED, WENT OUT AFTER A SHORT TIME BUT CAME BACK ON THROUGHOUT FLIGHT CONTROLS WERE VERY HEAVY IN PITCH AND ROLL. - (M2B) GAINED ACCESS TO PITCH FEEL LINEAR ACTUATORS. CHECKED CANNON PLUGS, NO DAMAGE FOUND. CHECKED LOGIC CARD MODULE FOR PITCH FEEL NO DAMAGE FOUND. C/W SATISFACTORY OPERATIONAL CHECK OF PITCH FEEL SYSTEM. UNABLE TO DUPLICATE DISCREPANCY. ALL WORK IAW CE 750 MM 27-30-00. 2L72 4J RTT00007WI 20050125000612005012500061CE 2005 1 25 DXTA200500555 120050124A2910 LINE CESSNA750 750 2076810CE HYD SYSTEM LEAKING E DXTAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 GL07983QS 7500083 UPON LOWERING GEAR HANDLE A/C LOST ALL -A- SYSTEM FLUID. FOLLOWED EMERGENCY CHECKLIST, POST FLIGHT DISCOVERED FLUID IN NOSE WHEEL WELL. ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20050125000622005012500062NM 2005 1 25 DXTA200500556 120050123A3240 WARNING LIGHT AMD FALC50FALCON2000 2730170NM RT BRAKES ILLUMINATED E DXTAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL07284QS 185 ON TAXI OUT AMBER BRAKE LIGHT ILLUMINATED AND RT BRAKE MINELCO TRIPPED. COMPUTER SHOWS CODE 424 RIGHT PEDAL SWITCH. ITEM IS UNDER INVESTIGATION. 2K73 4F RTA50NM 20050125000632005012500063CE 2005 1 25 DXTA200500548 120050121A1420 CONNECTOR CESSNA560 560XL 2076702CE MLG ACTUATOR DIRTY E DXTAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL07676QS 5605176 LANDING GEAR UNLOCK LIGHT WILL NOT EXTINGUISH AFTER GEAR RETRACTION. HYDRAULIC SYSTEM STAY PRESSURIZED, IT SOUNDS AND FEELS LIKE THE GEAR IS RETRACTING. GROUND OBSERVER ALSO SAID THE GEAR APPEARED TO BE RETRACTING. INSPECTED ALL GEAR, NO DEFECTS NOTED. CLEANED ACTUATOR CONNECTORS. CYCLED GEAR 20 TIMES. COULD NOT DUPLICATE. ALL GEAR MAKE GOOD CONTACT ON UPLOCK SWITCHES AND UPLOCK HOOKS. LANDING GEAR OPS CHECK GOOD IAW 560XL MM 32-01-00. 2L72 4F RTA22CE 20050125000642005012500064 2005 1 25 DXTA200500538 420050111A34207014300901 DISPLAY CESSNA500 560CESSNA 2076750CE COCKPIT INOPERATIVE E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07377QS 5600377 DURING TAKEOFF ROLL WHILE ACCELERATING THROUGH 60 KTS THE CO-PILOTS NR 2 PFD SCREEN WENT BLANK FOLLOWED BY A DISPLAY OF A RED -X-, THEN DISPLAYED A NORMAL SCREEN. TAKEOFF WAS ABORTED. REMOVED AND REPLACED CO-PILOT PFD. OP CHECKED GOOD IAW CITATION ULTRA MM 22-05-24. 2L72 4F RTA22CE 20050125000652005012500065CE 2005 1 25 DXTA200500539 120050116A7603 CONTROL LEVER CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE THROTTLE MALFUNCTIONED E DXTAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 GL07306QS 5600266 PCE500019 LEFT ENGINES SHUTS DOWN WHEN THROTTLE BROUGHT BACK TO FLIGHT IDLE. SUSPECT QUADRANT SWITCH. RAN ACFT, FOUND IDLE TO LOW. PERFORMED POWER CONTROLS ADJUSTMENT, SET IDLE, FLIGHT IDLE ADJUSTMENTS. CHECKED TAKEOFF POWER AND CUTOFF. OPS CHECK GOOD ALL IAW CE560 MM 71-01-03. 2L72 4F4 FRTA22CE E25EA 20050125000662005012500066 2005 1 25 SWAA050146 420050120A2565D31354 SLIDE BOEING737 7375H4 138449DNM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29502SW 24179 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050125000672005012500067NM 2005 1 25 SWAA050147 120050120A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29795SW 30606 EEPLS COVER AT ROW 5 ABC, LOOSE. SECURED COVER PER MM. 2L72 4F RTA16WE 20050125000682005012500068NM 2005 1 25 SWAA050148 120050120A2560PH22300L GLOWSTRIP BOEING737 7373H4 1384600NM CABIN WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED C4 CHECK, FOUND EMERGENCY EXIT PHOTOLUMINESCENT STRIP AT ROW 8 ABC, WORN. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER MM. 2L72 4F RTA16WE 20050125000692005012500069 2005 1 25 SWAA050149 420050120A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 & L1 DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED C4 CHECK, FOUND R1 AND L1 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED BOTH R1 AND L1 DOOR EVAC SLIDES PER MM. 2L72 4F RTA16WE 20050125000712005012500071NM 2005 1 25 SWAA050151 120050120A53156545833 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29606SW 27926 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM WEB AT BS 246, RBL 9, CORRODED. REMOVED AND REPLACED FLOORBEAM WEB PER ER. 2L72 4F RTA16WE 20050121000062005012100006NM 2005 1 21 DLM88050020 120050110A2120 ODOR DOUG MD88 MD88 3023688NM COCKPIT DETECTED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27910DL 49541 DURING CRUISE AT FL 310 ODOR OF BURNING RUBBER PRESENT IN COCKPIT FOR ABOUT 30 SECONDS, OVENS WERE OFF AND HAD NOT BEEN USED. PACKS NORMAL. ALL SYSTEMS INDICATE NORMAL. T/S PER OPN 5088 PERFORMED OPN 5088 AND 5089 NO TROUBLE FOUND. 2L72 4F RTA6WE 20050121000092005012100009WP 2005 1 21 CALA0500009 120050116A53206044887075T6 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2735836 49441 INSPECTION FOUND CENTER FLOOR SUPPORT BETWEEN I/B AND MIDDLE SEAT TRACKS CORRODED AROUND SCREW HOLES AT LT SIDE STA 1155, BL 0 TO LBL 30. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-01. 2L72 4F A6WE 20050121000192005012100019NM 2005 1 21 DLM88050023 120050112A2741279001350 MOTOR DOUG MD88 MD88 3023688NM PRIMARY TRIM UNSERVICEABLE A DALAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO27914DE 49957 PRIMARY TRIM MOTOR QUIT IN FLIGHT. REPLACED PRIMARY TRIM MOTOR. CHECKS OK PER AMM. 2L72 4F RTA6WE 20050121000382005012100038NM 2005 1 21 05FDEA00072 120050111A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25235FE 21329 BS 675, STR 27R CORROSION ON STRINGER. *S/D* REPAIRED PER SRM 53-10-3. 2L73 4F RTA3WE 20050121000962005012100096NM 2005 1 21 2005UALA00037 120050107A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29577UA 26693 AFT PIT STA 1600 FRAME HAS A DENT BETWEEN STR 25L AND 26L ON UPPER FLANGE. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20050121001112005012100111NM 2005 1 21 2005UALA00046 120050109A5340 STRINGER CLIP BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29905UA 25005 STRINGER CLIP IS CRACKED AT STA 685 STR 3L. REPLACED STRINGER CLIP. 2L72 4F4 FRTA16WE E2GL 20050121001262005012100126NM 2005 1 21 SWAA050106 120050117A57536573732 SKIN BOEING737 7373H4 1384600NM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29365SW 26576 DURING SCHEDULED 1/4D CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED T/E AFT FLAP PER MM. 2L72 4F RTA16WE 20050121001332005012100133EU 2005 1 21 SWAA050068 220050111A7200 BLADE BOEING737 7377H4 1384404NM CFMINTCFM56 CFM562AFR 13802EU NR 2 ENGINE DISTORTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29740SW 29276 874454 DURING SCHEDULED HC1 CHECK, FOUND SEVERAL 1ST STAGE LPT BLADES DISTORTED. REMOVED AND REPLACED NR 2 ENGINE PER MM. 2L72 4F4 FRTA16WE E21EU 20050121001342005012100134NM 2005 1 21 SWAA050093 120050115A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29324SW 23414 DURING SPV, FOUND FUSELAGE SKIN AT BS 500D + 4, STRINGER 12R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050121001412005012100141EA 2005 1 21 COMA0560033 120050107A2740 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA STAB TRIM FALSE INDICATIONA COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01931CA 7037 FLIGHT 5076 MACH AND STAB TRIM CAUTION. COULD NOT DUPLICATE. SYSTEM OPERATIONAL CHECKS SATISFACTORY. 2L72 4F RTA21EA 20050121001532005012100153NM 2005 1 21 SWAA050136 120050119A53116546529 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29606SW 27926 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 440, RBL 6, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20050124000182005012400018NM 2005 1 24 ASMF200501006 120050112A2820408854 VALVE BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE RT SIDE LEAKING W ASMFK NONE K FLUID LOSS ININSP/MAINT 1 SW23806AM11532 26273 DURING FUEL SERVICE WAS DETECTED HIGH SUPPLY PRESSURE ON FUEL DISPENSER (80 PSI), PROMOTING FUEL LEAK ON RT CENTRAL TANK VALVE. AIRCRAFT WAS FUELED THROUGH LT VALVE AND RT VALVE WAS DEFERRED IAW MEL 28-21-1. DURING OVERNIGHT SERVICE RT FUEL VALVE WAS REPLACED AND TESTED IAW MM 28-21-12, ALL CORRECT AND DEFERRED REPORT WAS CLOSED. 2L72 4F4 FRTA2NM E17NE 20050124000192005012400019WP 2005 1 24 ASMF200501009 120050116A29101474253 SELECTOR VALVE DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE HYD SYSTEM LEAKING W ASMFK NONE K FLUID LOSS ININSP/MAINT 1 SW23751RA15947 49779 DURING TRANSIT CHECK WAS DETECTED AN HYDRAULIC LEAK ON RT MAIN LANDING GEAR WELL. WELL WAS CLEANED AND SYSTEM WAS PRESSURIZED AND NO LEAK WAS DETECTED, HYDRAULIC SYSTEM WAS RECHARGED WITH 4 QUARTERS, ALL CORRECT. AT AGU, HYDRAULIC LEAK WAS DETECTED ON RIGHT SPOILER SELECTOR VALVE. SELECTOR VALVE LINES WERE TIGHTENED AND SYSTEM WAS CHECKED BY LEAKS IAW MM 29-10-26, ALL CORRECT. AT MEX VALVE WAS REPLACED AND TESTED IAW MM 29-10-06, HYDRAULIC SYSTEM WAS RECHARGED AT CORRECT LEVEL, ALL CORRECT. 2L72 4F4 FRTA6WE E9NE 20050124000632005012400063 2005 1 24 2005UALA00013 420050103A2565 SLIDE BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29522UA 24931 SLIDE FAILS AIR RETENTION TEST. MULTIPLE SEAM DEGRADATION CAUSED SLIDE TO FAIL AIR RETENTION TEST. 2L72 4F4 FRTA2NM E17NE 20050124000662005012400066NM 2005 1 24 AWXA200500049 120050108A555169730953 HINGE PIN BOEING737 737300 1384610NM HORIZONTAL STAB CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 MCN - MAJOR REPAIR - DURING 8-DAY CHECK CORROSION WAS FOUND ON LT HORIZONTAL STABILIZER OUTER HINGE PIN BS 1138, WL 255. MAINTENANCE REMOVED AND REPLACED LT HORIZONTAL STABILIZER OUTER HINGE PIN IAW AWA T/C E6C55102. 2L72 4F RTA16WE 20050124000702005012400070NE 2005 1 24 243733 220050113A7320 ECU SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE LT ENGINE FAILED A UHLAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL17118SD 118 LEFT ENGINE ERRATIC TQ FLUXUATES, ENGINE OVERTEMPS MULTIPLE TIMES. ENGINE SHUT DOWN MANUALLY. REMOVED AND REPLACED ECU, IAW GE CT7 M/M 74-00-00, GROUND RAN 45 MINS IAW GE CT7 M/M 71-00-00-5. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. 2L72 4T4 TRTA52EU E8NE6 20050124000712005012400071 2005 1 24 AALA20050028 420050115A2565100505201 SLIDE DOUG DC9 DC983 3022083WP L2 DOOR FAILED A AALAK NONE L NO TEST ININSP/MAINT 1 SW219621A 53592 LGA LEFT 2 DOOR SLIDE WAS NOT DISARMED AND CATERING OPENED DOOR. SLIDE EXTENDED BUT DID NOT INFLATE. REPLACED SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA6WE 20050124000752005012400075EU 2005 1 24 071632 120050114A2611 WARNING LIGHT SAAB SF340 SF340A 7850100EU CARGO SMOKE ILLUMINATED A UHLAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL1719XS 340A019 AVIONICS AND CARGO SMOKE LIGHTS ILLUM. ON THE CWP, DURING TAXI OUT, RETURNED TO THE GATE. AIRCRAFT AWAITING MAINTENANCE. 2L72 4T RTA52EU 20050124001012005012400101EU 2005 1 24 AWXA200500057 120050112A5347D5311209220209 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28621AW 053 SAL - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON CABIN FLOOR STRUCTURE SEAT TRACK Y1292 LT BETWEEN FS 20 AND FS 22. MAINTENANCE REMOVED CORRODED SEAT TRACK Y1292 LT FROM FS 20 TO FS 22; FABRICATED A NEW REPLACEMENT SEAT TRACK PER DWG D53112812; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050124001042005012400104NM 2005 1 24 QXEA200500006 120050101A21331036722 OUTFLOW VALVE DHAV DHC8 DHC8202 2809007NM ZONE 100 FAILED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09348PH17363 484 SEA - FLIGHT 2271 - THE FLIGHT RETURNED TO GATE WHEN AFTER STARTING THE NR 2 ENGINE AND BLEED AIR, THE CABIN DESCENDED AT 3000 FEET PER MINUTE. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE NORMAL OUTFLOW VALVE. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050124001152005012400115WP 2005 1 24 WX0500005 120050108A2420 CSD DOUG DC9 DC983 3022083WP LEFT OVERSERVICED A WX0AA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 WP19861GA 49557 CUN - CREW REPORTED LEFT CSD OIL ANNUNCIATOR ILLUMINATED ON CLIMB-OUT WITH LEFT CSD INDICATOR AT RED LINE. CREW REDUCED THRUST, INDICATION DROPPED BETWEEN YELLOW ARCS, THEN RIGHT CSD OIL ANNUNCIATOR ILLUMINATED AND RIGHT CSD INDICATOR AT RED LINE. DURING DESCENT BOTH CSD’S INDICATED NORMAL WITH POWER REDUCED. AIRCRAFT LANDED IN AN OVERWEIGHT CONDITION WITHOUT INCIDENT. MAINTENANCE COMPLETED OVERWEIGHT LANDING INSPECTION IAW MM 05-51-04 WITH NO DAMAGE FOUND. MAINTENANCE FOUND CSD’S OVER-SERVICED, DRAINED SUFFICIENT OIL TO BRING CSD’S TO PROPER LEVEL AND INSPECTED CHIP DETECTORS. AIRCRAFT RETURNED TO SERVICE . 2L72 4F RTA6WE 20050124001222005012400122NM 2005 1 24 QXEA200500066 120050114A5210 DOOR DHAV DHC8 DHC8202 2809007NM MAIN PAX DIRTY A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09363PH14933 520 SEA - FLIGHT 2171 - THE MAIN CABIN DOOR IS HARD TO OPEN. MAINTENANCE INSPECTED THE DOOR AND THEN CLEANED AND LUBED SAME. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050124001302005012400130NM 2005 1 24 SB05003 120050111A335020131A BATTERY PACK BOEING737 7373B7 1384580NM EMERGENCY LIGHT DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19375US 22954 PIT - MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT SEAT ROWS 17 THRU 22 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT STATION 975 FOR SEAT ROWS 17 THRU 22. ALSO, REPAIRED A PIN IN CANNON PLUG WHICH WAS FOUND BAD. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050125000012005012500001CE 2005 1 25 DXTA200500553 120050123A2750 WARNING LIGHT CESSNA750 750 2076810CE TE FLAPS ILLUMINATED E DXTAO OTHER J WARNING INDICATION APAPPROACH 1 GL07979QS 7500079 FLAPS FAIL AMBER CAS MESSAGE ILLUMINATED ON APPROACH TO LANDING WHEN HANDLE EXTENDED. FLAPS REMAINED FULLY UP WITH SLATS EXTENDED. ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20050125000332005012500033NM 2005 1 25 UPS05443677 120050106A5711 SPAR BOEING747 747123 1384873NM LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C, LEFT WING UPPER REAR SPAR OF BODY SPLICE FOUND CRACK AT NR 8 HOLE UPPER SPLICE FITTING RUNNING AFT. BOLT HOLE REWORK AS PER S/B 747-57A2314. 2L74 4F A20WE 20050125000372005012500037NM 2005 1 25 SWAA050168 120050122A3350D71702001 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29743SW 29279 DURING SCHEDULED RON, FOUND FWD LT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20050125000452005012500045NM 2005 1 25 SWAA050176 120050122A3350285A178010 CIRCUIT CARD BOEING737 7377H4 1384404NM EMERGENCY LIGHTSFAULTY A SWAAK NONE O OTHER ININSP/MAINT 1 SW29410WN 27897 EMERGENCY EXIT LIGHTS ILLUMINATE WHEN ARMED IS SELECTED ON P5 PANEL. REMOVED AND REPLACED AFT F/A STATION PC CARD PER MM. 2L72 4F RTA16WE 20050125000462005012500046NM 2005 1 25 SWAA050177 120050121A53306545765 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29669SW 23752 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 520, STRINGER 12L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20050125000472005012500047NM 2005 1 25 SWAA050178 120050123A57536546434301 SKIN BOEING737 7373H4 1384600NM LT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29653SW 28398 DURING SCHEDULED 1/4D CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED LEFT T/E AFT FLAP PER MM. 2L72 4F RTA16WE 20050125000562005012500056WP 2005 1 25 AALA20050051 120050121A3350 CHARGER DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21939AS 49657 DFW - AFT EMERGENCY LIGHTS BETWEEN AFT LAVS INOPERATIVE. REPLACED BATTERY PACKS AND TWO LIGHT BULBS FOR EMERGENCY LIGHTS BETWEEN AFT LAVS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050125000702005012500070 2005 1 25 SWAA050150 420050120A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 & R2 DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29327SW 23691 DURING SCHEDULED C3 CHECK, FOUND L2 AND R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED BOTH L2 AND R2 DOOR EVAC SLIDES PER MM. 2L72 4F RTA16WE 20050125000722005012500072NM 2005 1 25 SWAA050161 120050120A53126545819 PRESSURE PANEL BOEING737 7373A4 1384585NM NLG W/W CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29679AA 23291 DURING SCHEDULED SERVICE CHECK, FOUND NOSE WHEEL WELL CEILING WEB AT LEFT PRESSURE PANEL STATION 249, LBL 2, CRACKED. REPAIRED WEB PER EA. 2L72 4F RTA16WE 20050125000742005012500074 2005 1 25 SWAA050163 420050121A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29408WN 27895 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050125000802005012500080EA 2005 1 25 COMA0560043 120050114A3350362624 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A COMAO OTHER O OTHER NRNOT REPORTED 1 SO01934CA 7042 FLIGHT 5645 EMERGENCY LIGHTS ARE INOP. REPLACED THE FLEXIBLE LAMP SECTION. 2L72 4F RTA21EA 20050125000842005012500084EA 2005 1 25 COMA0560051 120050112A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01507CA 7796 FLIGHT 4972 FLAPS FAILED CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20050125000862005012500086EA 2005 1 25 COMA0560063 120050118A5297K601R507473S WIRE HARNESS CNDAIRCL600 CL6002B19 1900309EA CABIN DOOR FAULTY A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01959CA 7116 FLIGHT 5037 DURING CLIMBOUT OF LGA RECEIVED AN OVERBOARD COOL CAUTION MESSAGE. CREW DECLARED AN EMERGENCY, DIVERTED TO JFK AND LANDED WITHOUT INCIDENT. REPLACED THE CABIN DOOR WIRING HARNESS. 2L72 4F RTA21EA 20050125000892005012500089EA 2005 1 25 COMA0560056 120050118A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01966CA 7132 FLIGHT 5786 DURING APPROACH TO HPN RECEIVED A FLAP FAIL MESSAGE, FLAPS REMAINED A ZERO DEGREES WHEN SELECTED TO DEPLOY. CREW DECLARED AN EMERGENCY, ABORTED APPROACH AND LANDED SAFELY WITHOUT INCIDENT. COMPLIED WITYH AD 98-20-01 FLAP CAUTION MESSAGE FIRST EVENT, MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2L72 4F RTA21EA 20050125000932005012500093EA 2005 1 25 COMA0560058 120050118A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01729CA 7265 FLIGHT 5762 FLAP FAIL CAUTION MESSAGE DISPLAYED DURING CRUISE WHEN FLAPS WERE SELECTED FROM 0 TO 8 DEGREES, CREW DECLARED AN EMERGENCY AND FLIGHT DIVERTED TO JFK. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE FIRST EVENT, MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURHTER FLAP CAUTION MESSAGES. 2L72 4F RTA21EA 20050125000942005012500094SO 2005 1 25 SWIA200514403 120050118A3397 WIRE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07562SW 120336 FLOOR EMERGENCY LIGHTING INOPERATIVE AT GALLEY. REPAIRED WIRES AS REQUIRED. 2L72 4T RTA31SO 20050125000952005012500095SO 2005 1 25 SWIA200514404 120050115A3350 BULB EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07567SW 120342 TOP EMERGENCY LIGHT ON PAX DOOR IS INOPERATIVE. REPLACED LIGHT BULB. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050125000982005012500098NM 2005 1 25 05FDEA00128 120050119A5310 STOP FITTING BOEING727 727200 138407ENM PAX DOOR DAMAGED A FDEAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 SO25465FE 21289 INTERNAL ANGLE AT NR 7 LEFT DOOR STOP HAS MECHANICAL DAMAGE (DRILLED INTO). REMOVED AND REPLACED NR 7 LEFT DOOR STOP FITTING AS PER SRM 51-30-5, 51-30-2. 2L73 4F RTA3WE 20050125001002005012500100SO 2005 1 25 SWIA200514410 120050116A273152991 ACTUATOR EMB 120 EMB120ER 3260203SO ELEVATOR TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07216SW 120285 ELEVATOR TRIM IS DIFFICULT TO MOVE AND RATCHETS DURING HAND MOVEMENT INFLIGHT. REPLACED LEFT AND RIGHT TRIM ACTUATOR ASSEMBLIES IAW MM 27-32-02. P/N 5299-1, S/N OFF 980, 728. 2L72 4T RTA31SO 20050125001022005012500102WP 2005 1 25 UPS05843682 120050120A292057155A PUMP DOUG DC8 DC871F 302199DWP STBY RUDDER LEAKING A IPXAO OTHER KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO01772UP 46072 INSPECTION TYPE:N/A ON CLIMBOUT HYD FLUID QTY LOSS. FOLLOWED EMERGENCY PROCEDURE CHECK LIST. ON LANDING REMOVED AND REPLACED EMERGENCY STBY RUDDER PUMP. SERVICED & RAN AND OPS CHECKED NORMAL. 2L74 4F RT4A25 20050125001032005012500103 2005 1 25 UPS05M43681 420050119A2565CM36B BULB DOUG MD11 MD11F 3023600NM ESCAPE SLIDE INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01254UP 48406 DOOR R1 BOTTLE PRESSURE TEST LIGHT INOP. PLACED R1 DOOR EVAC DOOR SLIDE PRESS TO TEST LIGHT ON DEFERRAL M-295479 IAW MD MEL 25-61-2. PERFORMED DMP 25-61-2. REMOVED AND REPLACED BATTERIES AND BULBS IAW MM 25-61-04, CHECKED FOUND SATISFACTORY. THIS CLEARS DEFERRAL M295479. 2L73 4F RTA22WE 20050125001042005012500104NM 2005 1 25 DXTA200500534 120050115A2750 RESOLVER AMD FALC50FALCON2000 2730170NM SLATS/FLAPS MALFUNCTIONED E DXTAO OTHER SJ AFFECT SYSTEMS WARNING INDICATION CLCLIMB 1 GL07298QS 98 AFTER T/O, FLAP ASYM LIGHT ON AND SLIGHT ROLLING. FLAP INDICATES SLIGHTLY DOWN AND SLATS EXTENDED. GAINED ACCESS TO FLAP ASYM RESOLVERS & FOUND LT RESOLVER CABLE LOOSE. RESET RESOLVER AS REQUIRED, OPS CHECK GOOD. ALL WORK PERFORMED IAW FALCON 2000 MM CHAPTER 27-502. 2K73 4F RTA50NM 20050125001052005012500105NM 2005 1 25 SWAA050181 120050123A53116546529 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29606SW 27926 DURING SCHEDULED D-CHECK, FOUND FRAME AT FWD CARGO COMPT BS 440, STRINGER 24R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20050125001062005012500106NM 2005 1 25 SWAA050182 120050123A531165C2910 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29606SW 27926 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 500D, STRINGER 27L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20050125001092005012500109EA 2005 1 25 COMA0560044 120050114A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01442CA 7483 FLIGHT 4953 FLAPS FAILED CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20050125001112005012500111EA 2005 1 25 SWIA200514411 120050115A2760C13045BA03 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA SPOILERS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07719SK 10188 STAB CH 2 INOP STATUS MESSAGE. REPLACED NR 2 SSCU IAW MM 27-61-05. OPERATIONAL CHECK GOOD. P/N C13045BA03, S/N OFF 826. 2L72 4F RTA21EA 20050125001132005012500113EA 2005 1 25 COMA0560053 120050118A2750 DRIVE SHAFT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS LACK OF LUBE A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01466CA 7627 FLIGHT 4995 DURING APPROACH TO MHT RECEIVED A FLAP FAIL MESSAGE. FERRIED AIRCRAFT TO CVG FOR LUBRICATION OF THE FLEX DRIVE SHAFTS. 2L72 4F RTA21EA 20050125001152005012500115SO 2005 1 25 C2XA05BT005 120050117A3350602043 SIGN EMB 145 EMB145LR 3260212SO EMERGENCY EXIT FAILED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712540 145537 CREW REPORTED, EMERGENCY EXIT [SIGN] LIGHT ON BULKHEAD IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT SIGN ASSEMBLY IAW EMB145 AMM 33-50-15, OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050125001162005012500116EA 2005 1 25 COMA0560064 120050119A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION CLCLIMB 1 SO01779CA 7306 FLIGHT 5316 DURING CLIMBOUT OF CVG RECEIVED A FLAP FAIL CAUTION, FLIGHT DIVERTED BACK TO CVG. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE FIRST EVENT MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A, B, C AN E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2L72 4F RTA21EA 20050125001212005012500121NM 2005 1 25 2005UALA00062 120050115A5300 DRAIN VALVE BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE AFT CARGO BAY NOT CLOSED A UALAA UNSCHED LANDING O OTHER CLCLIMB 1 WP29902UA 25002 AT FL250 UNABLE TO HOLD CABIN ALTITUDE. CABIN CLIMBING AT 1000 FPM. DRAIN VALVE IN BOTH THE AFT CARGO PIT AND E/E DOOR NOT CLOSING. LUBED FWD ONE AND CLEANED DEBRIS FROM AFT PIT DOOR VALVE. 2L72 4F4 FRTA16WE E2GL 20050125001232005012500123WP 2005 1 25 MWEA050013 120050121A5330591143357 SKIN DOUG DC9 DC981 3022081WP FUSELAGE DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31805ME 48031 DENT IN FUSELAGE SKIN AT STATION 1277-1281, 1.5 INCHES BELOW LONGERON 7 RIGHT. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20050126000012005012600001SO 2005 1 26 CHQA200500014 120050120A3350 BATTERY EMB 135 EMB135LR 3260305SO EMERGENCY LIGHTSDISCONNECTED A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11844RP 145620 EMERGENCY LIGHTS ON FLOOR BETWEEN ROWS 7 THROUGH 10 ARE INOP. FOUND EMERGENCY BATTERY NR 4 DISCONNECTED. RECONNECTED BATTERY IAW EMB 135 AMM 33-50-04. OPS CHECK GOOD. REPLACED LIGHT STRIP DUE TO BROKEN WIRE IAW EMB 135 AMM 33-20-00. 2L72 4F RTT00011AT 20050126000022005012600002SO 2005 1 26 CHQA200500017 120050125A3350375924 SIGN EMB 145 EMB145LR 3260212SO EMERGENCY EXIT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11285SK 145435 FORWARD EMERGENCY LIGHTED EXIT SIGN IS INOP. REMOVED AND REPLACED FORWARD EMERGENCY LIGHTED SIGN IAW EMB 145 AMM 33-50-14-4. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050126000042005012600004SO 2005 1 26 CHQA200500016 120050124A2120 ODOR EMB 145 EMB145LR 3260212SO CABIN/COCKPIT DETECTED A CHQAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 GL11283SK 145424 DURING CLIMB A LAV SMOKE MESSAGE APPEARED ON EICAS. THE FLIGHT ATTENDANT INVESTIGATED AND FOUND NO INDICATION OF FIRE OR SMOKE IN ANY PART OF THE CABIN OR LAVATORY. EICAS INDICATIONS WERE EXTINGUISHED WITHIN ONE MINUTE. THE AIRCRAFT RETURNED TO FIELD IN ROC AS A PRECAUTION WITH NO FURTHER INCIDENT. PRIOR TO THE FLIGHT THE AIRCRAFT WAS DEICED WITH TYPE 1 DEICE FLUID. THE RECOMMENDED THREE MINUTE WAIT FROM DEICING TO BLEED AND PACK OPERATION WAS OBSERVED. ONCE THE BLEEDS AND PACK WERE TURNED ON THE USUAL AMOUNT OF BURNED SUGAR SMELL WAS NOTED. MAINTENANCE PERFORMED GROUND RUNS WITH BLEEDS AND PACKS RUNNING. NO SMELL OR SMOKE WAS NOTED. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050126000092005012600009EU 2005 1 26 CHQA200500013 120050123A2750 CONTROL UNIT EMB ERJ170ERJ170100LR EU TE FLAPS MALFUNCTIONED A CHQAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL11638RW 17000053 FLIGHT 9283 - DTW TO SYR - AFTER PASSING 1000 FT, A SLAT/FLAP LEVER DISAGREE MESSAGE APPEARED ON EICAS. IT WAS FOLLOWED BY A FLAP FAIL MESSAGE. AFTER LEVELING OFF AT 13,000 FT, THE SLAT OPERATED NORMALLY, BUT THE FLAPS STILL INDICATED FAILED. THE FLAPS WERE VISUALLY CHECKED AND DETERMINED TO BE BETWEEN FULL UP AND FLAP 1 POSITION. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO CMH WHERE IT LANDED WITHOUT EVENT. MAINTENANCE INSPECTED THE FLAPS AND FOUND THEM TO BE AT 2 DEGREES. MAINTENANCE RESET THE FLAP SYSTEM IAW EMB 170 AMM AND THE FLAP SYSTEM OPS CHECKED GOOD. 2L74 4F RTA56NM 20050126000102005012600010WP 2005 1 26 MWEA050009 120050118A5330591142267 SKIN DOUG DC9 DC981 3022081WP FUSELAGE DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31805ME 48031 FUSELAGE SKIN HAS SEVERAL DENTS FROM STATION 1278 TO 1282 FROM LONGERON 1 TO 6 LEFT. FABRICATED AND INSTALLED SKIN. 2L72 4F A6WE 20050126000122005012600012WP 2005 1 26 MWEA050014 120050121A5330591143351 SKIN DOUG DC9 DC981 3022081WP FUSELAGE DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31805ME 48031 DENT IN FUSELAGE SKIN AT STATION 1280, 1.5 INCHES BELOW LONGERON 7 LEFT. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20050126000132005012600013WP 2005 1 26 MWEA050015 120050121A5330591140885 SKIN DOUG DC9 DC981 3022081WP FUSELAGE DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31805ME 48031 FUSELAGE SKIN DENT AT STATION 541.1 1 INCH AFT OF FRAME AND 3/4 INCH ABOVE LONGERON 5 LEFT. FABRICATED AND INSTALLED DOUBLER AND FILLER. 2L72 4F A6WE 20050126000142005012600014WP 2005 1 26 MWEA050016 120050121A5230591014167 ANGLE DOUG DC9 DC981 3022081WP AFT CARGO DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31805ME 48031 AFT CARGO DOOR HAS A CRACK IN ANGLE AT LOWER AFT PART OF DOOR VIEWED FROM INTERIOR STRUCTURE. REMOVED AND REPLACED DOUBLER. 2L72 4F A6WE 20050126000152005012600015 2005 1 26 MWEA050012 420050120A2565 BOTTLE DOUG DC9 DC981 3022081WP SLIDE DISCHARGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31812ME BAI051 48006 TAILCONE EVACUATION SLIDE BOTTLE IS LOW. REMOVED AND REPLACED TAILCONE EVACUATION SLIDE. 2L72 4F A6WE 20050126000232005012600023NM 2005 1 26 QXEA200500070 120050112A24307826895 BRUSH BLOCK DHAV DHC8 DHC8202 2809007NM ZONE 100 INOPERATIVE A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09355PH8866 203 500 RT TRU CAUTION LIGHT AND R STALL WARNING CAUTION LIGHT CAME ON, RETURNED TO GATE. MAINTENANCE FOUND NR 2 PROP BRUSH BLOCK SHORTED AND FUSE FOR PHASE "B" OF NR 2 AC ELECTRIC SYSTEM BLOWN. REMOVED AND REPLACED NR 2 BRUSH BLOCK AND REPLACED NR 2 PHASE "B" FUSE AC CONTACTOR BOX. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050126000242005012600024SO 2005 1 26 RAIA00501015 120050108A3610AS56226 SEAL EMB 145 EMB145LR 3260212SO BLEED AIR SYS LEAKING A RAIAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 CE03816HK 145055 5619- BDL- NR 1 AND NR 2 BLEED LEAK, SMOKE SMELL IN CABIN AND FLIGHT DECK. MAINTENANCE REMOVED AND REPLACED BLEED LINE SEALS ON NR 2 SIDE. 2L72 4T RTT00011AT 20050126000272005012600027EU 2005 1 26 RAIA00501019 120050108A2437DVM41B VOLTMETER JETAIRJETSTMJETSTM4101 1500501EU ELECTRICAL SYS FAILED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03568HK13969 41086 3663- RIC- VOLT/AMP METER FAIL. REMOVED AND REPLACED AMP/VOLT METER. 2L72 4T RTA41NM 20050126000282005012600028EU 2005 1 26 RAIA00501018 120050108A243051539019E GCU JETAIRJETSTMJETSTM4101 1500501EU RT GENERATOR MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03572HK4575 41091 3630- PIT- RIGHT GENERATOR LIGHT AND ELECTRIC CAP ILLUMINATED WHEN RIGHT GENERATOR SWITCH SELECTED "ON". REMOVED AND REPLACED NR 2 GCU. 2L72 4T RTA41NM 20050126000292005012600029SO 2005 1 26 RAIA00501001 120050102A27503631001005 CONTROL UNIT EMB 145 EMB145LR 3260212SO TE FLAPS MALFUNCTIONED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03819HK6135 145062 4614 - DEN - TAKEOFF CONFIGURATION WARNING. MAINTENANCE REMOVED AND REPLACED FLAP ELECTRONIC CONTROL UNIT. 2L72 4T RTT00011AT 20050126000302005012600030EU 2005 1 26 RAIA00501021 120050105A793141SG107100G14 TRANSMITTER JETAIRJETSTMJETSTM4101 1500501EU NR 2 ENGINE FAILED A RAIAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 CE03554HK21055 41067 5478- STL- LOW OIL PRESSURE ON RIGHT ENGINE DURING TAXI. REMOVED AND REPLACED NR 2 ENGINE OIL PRESSURE TRANSMITTER. 2L72 4T RTA41NM 20050126000412005012600041WP 2005 1 26 ABXA050003 120050106A21308D3721 PRESSURE SWITCH DOUG DC9 DC931 3022065WP CABIN PRESSURE DEFECTIVE A ABXAG O2 MASK DEPLOYED O OTHER CLCLIMB 1 GL23945AX1538 47551 SHORTLY AFTER T/O, FLOW LIGHT ON AUTO PRESSURE CONTROLLER ILLUMINATED. TRANSFER LOCKOUT AND STANDBY LIGHT ALSO ON. RAN ABNORMAL PER MANUAL SECTION 21, CHAPTER 3. FLOW LIGHT, TRANSFER LOCKOUT AND STANDBY LIGHTS REMAINED ON. WENT TO MANUAL. STILL UNABLE TO CONTROL. RAN ABNORMAL SECTION 21, CHAPTER 3 (LT A/C TURNED OFF). CONTINUED FLT AT 10,000 FT. NOTE: CREW WAS ON OXYGEN THROUGHOUT THE FLT. RESET ALL C/B`S PULLED PER THE CREW ABNORMAL. FOUND PACKS WOULD NOT OPERATE IN 'ARMED' POSITION. (A/C AUTO SHUTOFF SW.) PUT SWITCH IN OVERRIDE, OPERATED BOTH PACKS, PRESSURIZED A/C TO 7.5 PSID. PRESS SYSTEM CHECKED GOOD IN AUTO AND MANUAL. R/R`D BOTH LT AND RT AFT FUSELAGE PRESSURE SWITCHES AND OPS CHECKED THEM IAW DC-9 AMM 2L72 4F A6WE 20050126000422005012600042WP 2005 1 26 ABXA050004 120050111A793131801040 TRANSMITTER DOUG DC8 DC863F 302198FWP NR 4 OIL PRESS DEFECTIVE A ABXAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 GL23811AX8 46113 NR 4 ENGINE OIL PRESSURE BEGAN FLUXUATING IN CRUISE AND THEN WENT TO '0' PSI. NO LOW OIL PRESSURE LIGHT CAME ON. ALL OTHER ENG PARAMETERS NORMAL. SECURED NR 4 ENGINE AT 0340Z. REMOVED AND REPLACED ENGINE OIL STRAINER. NO CONTAMINATES NOTED. REPLACED MAIN ENGINE OIL FILTER IAW DC-8 MM 79-20-07. REPLACED OIL PRESSURE TRANSMITTER IAW DC-8 MM 79-32-01. PERFORMED ENGINE RUN. NO FLUXATION NOTED. SYSTEM LEAK CHECKED GOOD. 2L74 4F 4A25 20050126000432005012600043NM 2005 1 26 ABXA050005 120050107A5340015T10595 FITTING BOEING767 767281 1385109NM FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23788AX 23021 LEFT FORWARD OUTER CHORD FITTING CRACKED PER DETAILED VISUAL INSPECTION IAW JC NEA53800004-001 AND AD 2001-09-13. REPAIRED LEFT FORWARD OUTER CHORD FITTING IAW S/B 767-53A-0078. 2L72 4F RTA1NM 20050126000452005012600045NM 2005 1 26 QXEA200500062 120050108A3010 DEICE SYSTEM BOMBDRDHC8 DHC8401 1390041NM WING MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09417QX1448 4086 SEA FLIGHT NR 2430 DURING DESCENT AND CRUISE, THE DE-ICE PRESS CAUTION LIGHT CAME ON. RUNNING THE APPROPRIATE CHECKLIST EXTINGUISHED THE LIGHT BUT IT CAME BACK ON WHEN BOOTS WERE SELECTED BACK ON. THE LEFT, MOST OUTBOARD BOOT SEGMENT LIGHT FLICKERED OFF AND ON SEVERAL TIMES INSTEAD OF REMAINING ON STEADILY. BOOT PRESSURE ON BOTH SIDES WAS NORMAL THROUGHOUT ALL OPERATIONS. MAINTENANCE REPLACED NR 1 DDV. PERFORMED FUNCTIONAL TEST OF THE AIRFRAME PNEUMATIC DE-ICING SYSTEM. FUNCTIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050126000472005012600047EU 2005 1 26 MALA050114 120050110A3060666000219 LEAD SAAB SF340 340B 7860101EU NR 3 PROP BLADE DAMAGED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15453XJ 340B453 WITH PROP DEICE SELECTED NORM, THE LEFT PROP CAUTION LIGHT ILLUMINATED AND THE LEFT PROP DEICE LIGHT WENT OUT. AIR RETURN TO MSP. MAINTENANCE FOUND BAD PROP LEAD, REPLACED NR 3 PROP BLADE LEAD PN 666000219, OPS CHECK GOOD PER DOWTY PROP CMM 61-10-39. 2L72 4T RTA52EU 20050126000512005012600051EA 2005 1 26 05004630 120050104A3220 LANDING GEAR CNDAIRCL600 CL6002B19 1900309EA NOSE INOPERATIVE A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27630BR 7255 GEAR DISAGREE AFTER TAKEOFF, NOSE GEAR DID NOT COME UP. PERFORMED GEAR SWINGS AND CHECKED PROX SENSORS GAPS ON NLG REF AMM CH 32-61-05. NO DEFECTS NOTED AT THIS TIME. 2L72 4F RTA21EA 20050126000642005012600064EA 2005 1 26 QXEA200500014 120050104A2750 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA TE FLAPS UNKNOWN A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09617QX 10130 THE FLIGHT RETURNED TO THE GATE AFTER THE CREW RECEIVED A FLAP FAULT STATUS MESSAGE. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND NO FAULTS IN THE MDC. THE INHIBITS OF THE SFECU FLAP CHANNEL 1 WERE CLEARED AND A SELF TEST OF THE SFECU 1 WAS INITIATED. NO FAULTS WERE FOUND, OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20050126000662005012600066EA 2005 1 26 05006629 120050106A3620 DUCT CNDAIRCL600 CL6002B19 1900309EA 14TH STAGE FAILED A VTZAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 EA27629BR 7251 EVENT SUMMARY ON 01/06 STATED ENGINE SHUTDOWN DUE TO QRH 1H 14TH STAGE BLEED DUCT FAIL. INSP LT 14 STAGE BLEED AIR SYSTEM. FOUND PYLON TO FUSELAGE TEFLON INSERT STUCK TO ONE SIDE. RESET INSERT TO PROPER LOCATION AND OPS CHK GOOD. NO FURTHER DEFECTS, REF 36-21-00. 2L72 4F RTA21EA 20050126000742005012600074EU 2005 1 26 CX7A194J0503 120050102A26121734362450 DETECTOR SAAB SF340 340B 7860101EU LT TAILPIPE SATURATED A CX7AO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL03314CE 340B335 LEFT HAND TAILPIPE HOT ILLUMINATED. 2L72 4T RTA52EU 20050126000792005012600079WP 2005 1 26 ABXA050001 120050102A3260 CONNECTOR DOUG DC9 DC931 3022065WP POSITION SWITCH LOOSE A ABXAO OTHER N FALSE WARNING CLCLIMB 1 GL23924AX 47403 EMERGENCY DECLARED, HAD GEAR DOOR OPEN LIGHT IN CRUISE FLIGHT. PERFORMED ABNORMALS, NO HELP. ON APPROACH, AFTER GEAR EXT, STILL HAD DOOR OPEN LIGHT. PERFORMED ABNORMALS. PULLED EMERGENCY GEAR RELEASE. MECHANICS MET THE AIRCRAFT. TIED DOORS UP AND PINNED ALL 3 GEAR. VERIFIED LOOSE CONNECTOR ON DOOR POSITION SWITCH. RESECURED PLUG, OPS CHECKED GOOD. 2L72 4F A6WE 20050126000882005012600088NM 2005 1 26 AWXA200500051 120050108A555169730962 HINGE PIN BOEING737 737300 1384610NM HORIZONTAL STAB CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 MCN - MAJOR REPAIR - DURING 8-DAY CHECK CORROSION WAS FOUND ON RT HORIZONTAL STABILIZER OUTER HINGE PIN BS 1138, WL 255. MAINTENANCE REMOVED AND REPLACED RT HORIZONTAL STABILIZER OUTER HINGE PIN IAW AWA T/C E6C55101. 2L72 4F RTA16WE 20050126000892005012600089EU 2005 1 26 AWXA200500052 120050111A5315D53472188202 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28621AW 053 SAL - MAJOR REPAIR - DURING C-4 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM Y1292 LT, BETWEEN FS 68 AND FS 69. MAINTENANCE REMOVED CORRODED FLOORBEAM Y1292 LT FROM FS 68 TO FS 69; FABRICATED A NEW REPLACEMENT FLOORBEAM INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050126000912005012600091EU 2005 1 26 AWXA200500054 120050112A5347D53112609200 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28621AW 053 SAL - MAJOR REPAIR - DURING C-4 CHECK EXFOLIATION CORROSION WAS FOUND ON LONGITUDINAL FLOORBEAM (DUMMY RAIL) -Y1379.5 RT AT FS 16. MAINTENANCE REMOVED CORRODED DUMMY RAIL -Y1379.5 RT AT FS 16; FABRICATED A NEW REPLACEMENT DUMMY RAIL; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050126000932005012600093 2005 1 26 YENA200501 420050101A23303042865102 ELECTRICAL BOX AIRBUS320 A320232 3930326EU CABIN UNKNOWN A YENAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 EA15559JB3360 1917 CABIN CREW REPORTS ELECTRICAL FUMES ON SHORT FINAL. FUME DISSIPATED WHEN LIVE TV TURNED OFF. FUMES IDENTIFIED NEAR ROW 17. INSPECTED ROW 17 DEF SEB COVER AND DETECTED DRIED AND BURNT BEVERAGE RESIDUE. CLEANED RESIDUE AND REINSTALLED SEAT 17 DEF SEB COVER. DEACTIVATED LTV SYS PER MM 23-39-00. LTV SYSTEM PLACED ON MEL 25-22-03 CAT D, CTL NR L02830. COMPLIED WITH INFO NOTICE 2004-T023TR AND TSM TASK 24-00-00-810. UPON ARRIVAL AT JFK REMOVED AND REPLACED SEB AT SEAT 17 DEF IAW LTV MM 23-39-00. OPERATOIN CHECK OK. 2L72 4F RTA28NM 20050126000962005012600096NM 2005 1 26 DHL2005770001 120050112A3260 SWITCH BOEING727 7272B7 138407LNM MLG DIRTY A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01770AT 21953 DOORS WARNING LIGHT ILLUMINATED ON FRONT PANEL, NOSE GEAR DOOR AMBER ILLUMINATED S/O PANEL. INSPECTED, CLEANED, AND LUBED NOSE GEAR DOOR SWITCHES, CKS GOOD IAW M/M 32-62-00. 2L73 4F A3WE 20050126000982005012600098EU 2005 1 26 AALA20050036 120050113A3260 PROXIMITY SENSOR AIRBUS300 A300B4605R 3930308EU MLG INOPERATIVE A AALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW2177080 626 MIA - ON TAKEOFF WITH LANDING GEAR POSITION DETECTOR SWITCH IN NR 2 COULD NOT RAISE GEAR. SWITCHED TO DETECTOR 1 AND GEAR WAS RAISED. REPLACED PROXIMITY DETECTOR UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20050126000992005012600099NE 2005 1 26 AALA20050034 220050115A7200 ENGINE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE RIGHT FAILED A AALAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 SW21973TW 53623 718047 YVR - INFLIGHT T814/15, ENGINE FAILURE ON TAKEOFF AT APPROXIMATELY 1000 FEET. LOUD BANG AND AIRCRAFT SHUDDERED FOLLOWED BY IMMEDIATE YAW TO THE RIGHT. NO FIRE OR AURAL INDICATIONS. RIGHT ENGINE PULLED TO IDLE UNTIL SHUTDOWN APPROXIMATELY 2 MINUTES LATER. ACCOMPLISHED SUM OF LEFT HAND, RIGHT HAND AND CENTER FUEL TANKS. CHANGED ENGINE DUE TO METAL IN TAILPIPE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA6WE E9NE 20050126001002005012600100NM 2005 1 26 BB05001 120050102A5610141T480149 WINDOW BOEING767 7672B7 1385107NM COCKPIT L1 FAILED A USAAA UNSCHED LANDING O OTHER CRCRUISE 1 EA19655US1939619396 25257 PHL - FL 98 - ENROUTE, THE L1 WINDOW OUTER PANE SHATTERED. NO PRESSURIZATION LOSS OCCURRED, HOWEVER THE CAPTAIN COULD NOT SEE OUT THE WINDOW. FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE L1 WINDOW. 2L72 4F RTA1NM 20050126001022005012600102WP 2005 1 26 ARWA20050102 120050112A3260 WARNING LIGHT DOUG DC8 DC863F 302198FWP MLG ILLUMINATED A ARWAO OTHER J WARNING INDICATION CRCRUISE 1 SO19784AL 46135 AFTER GEAR RETRACTION, GEAR NOT LATCHED LIGHT REMAINTED ILLUMINATED, PERFORMED ABNORMAL CHECKLIST. CHECKED ALL WIRING FOR GEAR LATCH LIGHT. JACKED A/C PERFORMED GEAR SWING SEVERAL TIMES. CHECK ALL THREE GEARS FOR CONDITION AND FOUND NORMAL. UNABLE TO DUPLICATE. CHECKED CIRCUIT PER WIRING DIAGRAM SERVICE BULLETIN NR 32-156 PAGES 26 AND 27, WIRING FOUND NORMAL, UNABLE TO DUPLICATE ON GROUND. 2L74 4F 4A25 20050126001032005012600103SO 2005 1 26 CHQA200500001 120050101A3350 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11258SK 145768 LEFT AFT OVERWING EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED LIGHT BULB IAW EMB 145 AMM 3-50-10. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050126001072005012600107WP 2005 1 26 P9RA20050063 120050104A335010030431 POWER SUPPLY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A P9RAK NONE O OTHER ININSP/MAINT 1 SO1110801 49127 AIRCRAFT IN MAINTENANCE SYR, COCKPIT EMERGENCY LIGHTING WILL NOT TURN OFF. REMOVED AND REPLACED POWER UNIT PER MM. 2L72 4F A6WE 20050126001092005012600109EU 2005 1 26 SA05005 120050104A5744D5758640300000 FAIRING AIRBUSA321 A321211 3930370EU LEFT WING MISSING A USAAO OTHER D INFLIGHT SEPARATION NRNOT REPORTED 1 EA19188US 1724 DCA - DURING OVERNIGHT SERVICE WALK AROUND INSPECTION, MAINTENANCE FOUND THE LEFT WING FLAP TRACK 3A FAIRING ASSEMBLY MISSING THE FORWARD FAIRING AND DAMAGE TO THE AFT FAIRING. MAINTENANCE REMOVED THE AFT FAIRING. ENGINEERING AUTHORIZATION WAS OBTAINED TO OPERATE THE AIRCRAFT WITHOUT THE FAIRINGS, BUT WITH CERTAIN RESTRICTIONS. MAINTENANCE REPLACED THE FORWARD FAIRING AND REPAIRED AND INSTALLED THE AFT FAIRING. THE ENGINEERING AUTHORIZATION WAS CLOSED OUT. 2L72 4F RTA28NM 20050126001112005012600111SO 2005 1 26 CHQA000602 120050101A3350 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11258 145768 LEFT AFT OVERWING EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED LIGHT BULB IAW EMB 145 AMM 3-50-10. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050126001122005012600112EU 2005 1 26 MALA050119 120050108A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15425XJ 340B425 DURING 4Y/2Y CHECK IN BNA, SEAT TRACK AT BL0 BETWEEN FS 294 AND FS 319 IS CORRODED OUT OF LIMITS AND HAS BEEN REPAIRED IAW MESABA EO NR 53079. REFER EAMS WO NR 211363, TASK 1512 FOR ADDITIONAL INFORMATION. AIRCRAFT WAS RELEASED 1/11/05. 2L72 4T RTA52EU 20050126001132005012600113EU 2005 1 26 MALA050120 120050108A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15425XJ 340B425 DURING 4Y/2Y CHECK IN BNA, SEAT TRACK AT LBL 18.3 BETWEEN FS 294-319 IS CORRODED OUT OF LIMITS AND HAS BEEN REPAIRED IAW MESABA EO NR S53079. REFER EAMS WO NR 211363, TASK 1511 FOR ADDITIONAL INFORMATION. AIRCRAFT WAS RELEASED 1/11/05. 2L72 4T RTA52EU 20050121000742005012100074NM 2005 1 21 05FDEA00105 120050116A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 MAIN DECK CARGO, SEAT TRACK BETWEEN STA Y= 755 TO Y= 840, X= 47.50 FOUND WORN.CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I, FIGURE 1. 2L73 4F RTA22WE 20050121001002005012100100NM 2005 1 21 2005UALA00041 120050107A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29577UA 26693 AFT PIT FRAME STA 1500, STR 25L AND 26L HAS DENT UPPER FLANGE. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20050121001082005012100108NM 2005 1 21 2005UALA00043 120050110A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29580UA 26698 FLOORBEAM AT STA 1640, RBL 58-RBL 60 CORRODED BEYOND LIMITS. INSTALLED REPAIR ANGLE, FILLER, STRAP. 2L72 4F4 FRTA2NM E17NE 20050121001132005012100113NM 2005 1 21 2005UALA00048 120050109A5310 SHEAR WEB BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29907UA 25007 LEFT SHEAR WEB AT STA 194 IS CRACKED AT WL 207. REPLACED SHEAR WEB. 2L72 4F4 FRTA16WE E2GL 20050121001272005012100127NM 2005 1 21 SWAA050107 120050117A5312BAC1514 STIFFENER BOEING737 7373T5 1384608NM PRESSURE BLKHD CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29667SW 23063 DURING SCHEDULED 1/4D CHECK, FOUND RADIAL STIFFENER AT AFT PRESSURE BULKHEAD BS 1016, 6 O'CLOCK POSITION CORRODED. REPAIRED STIFFENER PER ACO. 2L72 4F RTA16WE 20050121001322005012100132NM 2005 1 21 SWAA050058 120050111A2560655681915 BUTTON BOEING737 7373H4 1384600NM ESCAPE ROPE STUCK A SWAAK NONE O OTHER ININSP/MAINT 1 SW29394SW 27380 CAPTAIN'S EMERGENCY ESCAPE ROPE DOOR BUTTON STUCK. ADJUSTED AND LUBED BUTTON PER MM. 2L72 4F RTA16WE 20050121001392005012100139EA 2005 1 21 COMA0560029 120050109A274083963 MOTOR CNDAIRCL600 CL6002B19 1900309EA STABILIZER UNRELIABLE A COMAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 SO01966CA175377585 7132 FLIGHT 5803 STAB TRIM CAUTION. REPLACED THE STAB TRIM ACTUATOR. 2L72 4F RTA21EA 20050121001512005012100151NM 2005 1 21 SWAA050134 120050119A53116546550 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29606SW 27926 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 787, STRINGER 9R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20050121001552005012100155NM 2005 1 21 SWAA050138 120050119A33506556633 LIGHT BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29439WN 29834 DURING SCHEDULED MV3 CHECK, FOUND RT AND LT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED RT AND LT OVERWING LIGHT ASSY'S PER MM. 2L72 4F RTA16WE 20050124000132005012400013 2005 1 24 ASMF200501010 420050117A22104034241974 COMPUTER DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE LT SIDE FAILED W ASMFC ABORTED TAKEOFF GE MULTIPLE FAILURE VIBRATION/BUFFET TOTAKEOFF 1 SW23160PL6118 49763 CAPTAIN REPORTED DFGC MISC DATA FAIL LEGEND ON BOTH MCDUS SCRATCH PADS, AUTOMATIC PILOT 1 AND 2 WERE UNABLE DURING FIVE MINUTES AFTER TAKEOFF, ATS WAS UNABLE WITH FMAS IN TAKEOFF MODE, CAPTAIN VHF NAV OSCILLATING, CRUISE INDICATOR WITHOUT MOVEMENT IN ND SCREEN AND STRONGER VIBRATION IN NOSE LANDING GEAR. STP WAS CHECKED DETECTING FAILURE CODES RELATED TO DFGC NR 1. DURING OVERNIGHT SERVICE, IT WAS PERFORMED BITE TO CADC´S AND DFGC NR 1 WAS REPLACED, AUTOMATIC PILOT SYSTEM, CRS VALUES AND WIRING WERE CHECKED, LT EPR'S TRANSMITTER WIRING WAS CHECKED, BITE TO BOTH CADC´S AND ATS WERE PERFORMED, RELAY R2-47 WAS REPLACED AND NOSE LANDING GEAR WAS SERVICED, ALL TESTS WERE CORRECT. 2L72 4F4 FRTA6WE E9NE 20050124000582005012400058NM 2005 1 24 RYNA200500002 120050117A5315 FLOORBEAM BOEING737 737201 1384454NM FUSELAGE CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07240AU5546055460 22355 MAIN CABIN FLOOR BEAM, UPPER CHORD, UPPER SURFACE CORRODED AT BS 1006, LBL 29. REMOVED CORROSION ON FLOOR BEAM, FABRICATED, TREATED AND INSTALLED REPAIR PARTS. 2L72 4F A16WE 20050124000762005012400076EU 2005 1 24 243781 120050116A7700 CTOT PANEL SAAB SF340 SF340A 7850100EU COCKPIT MALFUNCTIONED A UHLAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 GL17118SD 118 LEFT ENGINE TORQUE MOMENTARILY DROPPED ON CLIMB-OUT WITH CTOT ON. AIRCRAFT RETURNED TO FIELD AND MTX DETERMINED THAT THE TORQUE DROP ONLY OCCURS WITH CTOT ENGAGED. MTX DEFERRED THE CTOT AND THE AIRCRAFT CONTINUED ON WITH THE SCHEDULED FLIGHTS. 2L72 4T RTA52EU 20050124001212005012400121 2005 1 24 221471 420050113A3431 INDICATOR SAAB SF340 SF340A 7850100EU VOR SYSTEM INOPERATIVE A UHLAA UNSCHED LANDING O OTHER DEDESCENT 1 GL1714XS 340A014 BOTH VOR`S INOP. NEEDLES MOVING ALL AROUND ERRATICLY, AIRCRAFT AWAITING MAINTENANCE. 2L72 4T RTA52EU 20050124001382005012400138NM 2005 1 24 05FDEA00115 120050117A5414 SKIN BOEING727 727200 138407ENM NR 2 NACELLE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25465FE 21289 NR 2 ENGINE INLET INNER SKIN DAMAGED 16.5 IN FWD OF ACCESS DOOR LBL 2. REPAIRED PER SRM 54-10-3 FIG. 7 2L73 4F RTA3WE 20050125000132005012500013EU 2005 1 25 MALA050138 120050117A2560P4010021 FLASHLIGHT BAC 146 AVRO146RJ85A1500097EU CABIN INOPERATIVE A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15526XJ E2351 AFT CABIN EMERGENCY FLASHLIGHT NOT FLASHING (INDICATING). MAINTENANCE REPLACED AFT CABIN EMERGENCY FLASHLIGHT P/N P4-01-0021, OPS CHECK GOOD. 2H74 4F RTA49EU 20050125000262005012500026EU 2005 1 25 MALA050131 120050111A5220 DOOR BAC 146 AVRO146RJ85A1500097EU EMERGENCY EXIT DAMAGED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15524XJ E2349 RIGHT FWD EMERGENCY EXIT DOOR WAS DAMAGED AND WOULD NOT OPEN. MAINTENANCE REPAIRED DOOR IAW EO A52067. REMOVED FWD SERVICE DOOR FOR REPAIR, INSTALLED DOOR IAW AMM 52-41-00. PERFORMED CABIN LEAK RATE AS PER AMM 21-30-00-501. FOUND SERVICEABLE. 2H74 4F RTA49EU 20050125000282005012500028NM 2005 1 25 UPS05243687 120050111A5754 HOOK BOEING727 727185C 138406NNM NR 2 SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 INSPECTION TYPE:C SUSPECT CRACK ON NR 2 SLAT O/B HOOK UPPER FASTENER. HFEC CARRIED OUT IAW NDTM 51-00-00 FIG 4. RESULT - CRACK CONFIRMED. REPAIR CARRIED OUT IAW SRM 57-50-3 FIG 10. 2L73 4F A3WE 20050125000302005012500030NM 2005 1 25 UPS05443674 120050107A5711 SPAR BOEING747 747123 1384873NM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C, RT WING UPPER REAR SPAR SIDE OF BODY SPLICE NR 11 FASTENER HOLE CRACKED AT UPPER SKIN LAYER APPROX 0.060 INCH RUNNING AFT. HOLE REPAIRED AS PER SB 747-57A2314. 2L74 4F A20WE 20050125000342005012500034NM 2005 1 25 UPS05443678 120050108A5711 SPAR BOEING747 747123 1384873NM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C, RIGHT WING UPPER REAR SPAR SIDE-OF-BODY SPLICE PLATE FITTING CRACK FOUND AT HOLE NR 5 RUNNING FWD APPROX 0.060 INCH AND AFT APPROX .125 INCH. PLS REFER ATTACH FIG. HOLE REPAIRED AS PER S/B 747-57A2314. 2L74 4F A20WE 20050125000512005012500051NM 2005 1 25 SWAA050140 120050119A3350D71702001 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT FAILED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29770SA 30589 DURING SCHEDULED HC2 CHECK, LT AFT EMERGENCY EXIT LIGHT FAILED TEST. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20050125000542005012500054WP 2005 1 25 AALA20050039 120050122A3260 PROXIMITY SWITCH DOUG DC9 DC982 3022082WP MLG INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW217519A 49896 MIA - EN ROUTE MIA-DFW NOSE LANDING GEAR WOULD NOT RETRACT. RETURNED MIA AND LANDED WITHOUT INCIDENT. REPLACED PROXIMITY SWITCH ELECTRONIC UNIT AND CLEANED NOSE GEAR UP SENSOR. CYCLED NOSE GEAR NUMEROUS CYCLES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050125000602005012500060CE 2005 1 25 DXTA200500557 120050118A3260 DOWNLOCK SWITCH CESSNA560 560XL 2076702CE MLG MALFUNCTIONED E DXTAO OTHER E VIBRATION/BUFFET CLCLIMB 1 GL07650QS 5605150 DID NOT GET ANY GEAR INDICATION LIGHTS WHEN LANDING GEAR WAS EXTENDED GEAR CIRCUIT BREAKER WAS POPPED. RESET C/B & IT POPPED AGAIN. RESET C/B A 2ND TIME AND IT STAYED IN. BLEW GEAR DOWN MANUALLY PER THE CESSNA EMERGENCY CHECKLIST. FOUND MINOR CORROSION ON LT MLG SWITCH PLUG PL 003. THAT CAUSES GEAR WARNING BREAKER TO POP. CLEANED CANNON PLUG WITH LPS CONTACT CLEANER. RECONFIGURATE GEAR & BRAKE PNEUMATIC SYSTEM. SERVICED BOTTLE TO CORRECT PRESSURE WITH NITROGEN. PERFORMED LANDING GEAR SYSTEM FUNCTIONAL TEST, TESTED NORMAL. BLED HYDRAULIC SYSTEM. WORK PERFORMED IAW CE560 XL MM CHAP 32-01-00 AND 12-13-01. 2L72 4F RTA22CE 20050125000732005012500073NM 2005 1 25 SWAA050162 120050121A2913887477 PUMP BOEING737 7377H4 1384404NM HYD SYSTEM LEAKING A SWAAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW29737JW 27869 DECLARED EMERGENCY, A-HYDRAULIC SYSTEM FAILURE, QUANTITY LOSS. REMOVED AND REPLACED A-SYSTEM HYDRAULIC PUMP AND CASE DRAIN FILTERS PER MM. 2L72 4F RTA16WE 20050125000792005012500079SO 2005 1 25 C2XA05TY004 120050113A555314525669001 FITTING EMB 145 EMB145LR 3260212SO STAB TO FUSELAGECORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714953 145071 TYS, DURING A SCHEDULED INSPECTION, THE VERTICAL STAB TO FUSELAGE FITTING ATTACH BRACKET WAS FOUND FRETTING ON SKIN AT FRAME 75. MAINTENANCE REMOVED THE STAB FITTING AT FRAME 75, CLEANED AND INSPECTED THE SKIN AND FITTING (NO CORROSION OR DAMAGE WAS FOUND), ALODINED, APPLIED SEALANT AND REINSTALLED IAW-EC5310-01288, EC5310-01314, 135/145-SRM-51-40-02, 51-10-02 AND AMM-21-31-00. 2L72 4T RTT00011AT 20050125000922005012500092EA 2005 1 25 COMA0560039 120050113A5210G80040 SEAL CNDAIRCL600 CL6002B19 1900309EA PAX DOOR INOPERATIVE A COMAA UNSCHED LANDING O OTHER CLCLIMB 1 SO01427CA 7460 FLIGHT 5179 CABIN WOULD NOT PRESSURIZE. REPLACED THE CABIN DOOR SEAL. 2L72 4F RTA21EA 20050125000962005012500096SO 2005 1 25 SWIA200514405 120050118A3350D36604001 BATTERY EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT DISCHARGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07270YV 120270 ALL EXIT SIGNS (4 TOTAL) AT OVERWING EMERGENCY EXITS DO NOT LIGHT UP. REPLACED CABIN EMERGENCY LIGHTS BATTERY. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050125000972005012500097EU 2005 1 25 05FDEA00127 120050119A7830 WARNING LIGHT AIRBUS300 A300F4605R 3930327EU GE CF6 CF680 30025NE THRUST REVERSER ILLUMINATED A FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25662FE 761 705239 ENGINE NR 2 REV PRESSURIZED ECAM WARNING ON TAKEOFF ROLL. DISCONTINUED TAKEOFF. NO REV OR REV UNLOCK LIGHTS. ACN RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A CATEGORY: C EXPIRATION: 28JAN05 MEL 78-30-01-A: ENGINE (IDENTIFY 1 OR 2) 2 THRUST REVERSER INOP. THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POSITION. REMOVED AND REPLACED PRESSURE REGULATOR SHUT OFF VALVE. 2L72 4F4 FRTA35EU E13NE 20050125001012005012500101NM 2005 1 25 UPS05543689 120050114A3350 BULB BOEING757 75724APF 1384969NM EMERGENCY LIGHT BURNED OUT A IPXAK NONE O OTHER ININSP/MAINT 1 SO01459UP 25480 EMERGENCY LIGHTS UNARMED INDICATOR LIGHT BURNED OUT. RELAMPED UNARMED IND LIGHT ASSY, OPS CHECK NORMAL. 2L72 4F RTA2NM 20050125001082005012500108EA 2005 1 25 COMA0560042 120050113A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY MALFUNCTIONED A COMAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO01467CA 7637 FLIGHT 5393 CARGO SMOKE MESSAGE. BOTTLES DISCHARGED. COULD NOT DUPLICATE. NO EVIDENCE OF SMOKE OR FIRE, REPLACED FIRE BOTTLES AND SMOKE DETECTORS. 2L72 4F RTA21EA 20050125001122005012500112EA 2005 1 25 COMA0560052 120050118A2750865D1007 PDU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAULTY A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01962CA22306 7123 FLIGHT 5786 DURING APPROACH TO CVG RECEIVED A FLAP FAIL MESSAGE AT 20 DEGREE SETTING. REPLACED THE FLAP POWER DRIVE UNIT. 2L72 4F RTA21EA 20050125001242005012500124 2005 1 25 MWEA050017 420050123A2565113317 SLIDE DOUG DC9 DC981 3022081WP SERVICE DOOR HUNG UP A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 GIRT BAR FLAP HANGING UP AT FORWARD GALLEY SERVICE DOOR. REMOVED AND REPLACED FORWARD SERVICE DOOR EVACUATION ASSEMBLY. 2L72 4F A6WE 20050126000322005012600032CE 2005 1 26 DJFA2004046 120050105A3310 CONTROL PANEL BEECH MU300 400A 1155402CE COCKPIT LIGHTS ARCED E DJFAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA23746TA RK146 CREW REPORTED THAT THEY HEARD A POPPING SOUND COMING FROM THE CIRCUIT BREAKER PANEL. ARCING HAD OCCURRED FROM THE BOTTOM OF THE CIRCUIT BREAKER PANEL FOLLOWED BY A NOTICEABLE SMOKY SMELL. APPROXIMATELY TEN SECONDS LATER THE ARCING HAD EXTINGUISHED AND VAPOR HAD CLEARED. THE CIRCUIT BREAKER PANEL LIGHTS WERE FOUND TO BE INOPERATIVE, AND A SMALL MELTED AREA ON THE PANEL WAS HOT TO THE TOUCH. THE LIGHTING FOR THE PANEL WAS ISOLATED AS WELL AS THE HEAT SOURCE WHEN THE CIRCUIT BREAKER FOR THE PANEL LIGHTING WAS PULLED. THE FLIGHT PROCEEDED WITHOUT FURTHER INCIDENT. MAINTENANCE ISSUED MEL 33-6 FOR THE CIRCUIT BREAKER PANEL LIGHTING. 2H72 4F RTA16SW 20050126000342005012600034WP 2005 1 26 P9RA20050061 120050101A5280 DOOR DOUG DC9 DC982 3022082WP NLG MALFUNCTIONED A P9RAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO1110801 49127 SYR-SYR AIR RETURN. VIBRATION NOTED UPON GEAR RETRACTION. SUSPECT NOSE GEAR DOORS DID NOT LOCK UP DURING RETRACTION. SUSPECT OVERWEIGHT INTO SYR. PERFORMED OVERWEIGHT LANDING INSPECTION PER M/M. NO DEFECTS NOTED. CLOSED NOSE GEAR DOOR. OPS CHECKED GOOD PER M/M. NO PARTS REPLACED AND NO PRIOR HISTORY OF DISCREPANCY. 2L72 4F A6WE 20050126000492005012600049EU 2005 1 26 MALA050110 120050108A3213 STRUT SAAB SF340 340B 7860101EU NLG UNDERSERVICED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15402XJ 340B402 LANDING GEAR INTRANSIT LIGHT REMAINED ON WELL AFTER GEAR HANDLE WAS SELECTED UP. PERFORMED QRH. CONDITION REMAINED. AIR RETURN TO CID. MAINTENANCE SUSPECT NLG NEVER EXTENDED FULLY TO ENGAGE CENTERING CAM. AFTER PROPER SERVICING STRUT RAN GEAR EXTENSION/RETRACTION THRU SEVERAL TIMES. OPS CHECK GOOD. ALL INDICATIONS NORMAL. 2L72 4T RTA52EU 20050126000502005012600050EU 2005 1 26 MALA050116 120050103A3350 POWER SUPPLY SAAB SF340 340B 7860101EU EMERGENCY LIGHT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15413XJ 340B413 LT AND RT VERTICAL AND HORIZONTAL EMERGENCY OVERWING LIGHT INOP. POWER SUPPLY FAILED, PN 3301-51. REFER TO 409 NR 230034 FOR ADDITIONAL INFORMATION. 2L72 4T RTA52EU 20050126000522005012600052NM 2005 1 26 BB05002 120050110A24506TC610 CIRCUIT BREAKER BOEING757 757225 1384959NM COCKPIT BROKEN A USAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA19606AU 22202 PHL - FL 618 - DURING CRUISE, THE LEFT CENTER OVER-RIDE PUMP CIRCUIT BREAKER ON THE P6 PANEL CAUSED SMOKE IN THE COCKPIT. CREW PULLED CIRCUIT BREAKER, WHICH BROKE APART. SMOKE ABATED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE CIRCUIT BREAKER AND REPAIRED THE TERMINAL END. THE LEFT FUEL PUMP WAS REPLACED AS A PRECAUTIONARY MEASURE. 2L72 4F RTA2NM 20050126000822005012600082EA 2005 1 26 MASA200500039 120050116A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSBURNED OUT A MASAO OTHER O OTHER TXTAXI/GRND HDL 1 SW07593ML 7465 ASH 2934 PHL TO YDW, HAD A LT EXTERNAL OVERWING EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED THE LIGHT. 2L72 4F RTA21EA 20050126000862005012600086SO 2005 1 26 MASA200500042 120050117A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSBURNED OUT A MASAK NONE O OTHER ININSP/MAINT 1 SW07827MJ 145217 N827MJ, THE AIRCRAFT WAS ON R.O.N. AND SCHEDULED FOR A ROUTINE CHECK INSPECTION. DURING THE WALK AROUND IT WAS DISCOVERED THAT THE RT EXTERNAL OVERWING EMERGENCY LIGHT WAS NOT ILLUMINATING. MAINTENANCE REPLACED THE LIGHT BULB AND OPERATIONAL CHECKED GOOD. 2L72 4T RTT00011AT 20050126000872005012600087NM 2005 1 26 AWXA200500050 120050108A555169730963 HINGE PIN BOEING737 737300 1384610NM HORIZONTAL STAB CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 MCN - MAJOR REPAIR - DURING 8-DAY CHECK CORROSION WAS FOUND ON LT HORIZONTAL STABILIZER INNER HINGE PIN BS 1138, WL 255. MAINTENANCE REMOVED AND REPLACED LT HORIZONTAL STABILIZER INNER HINGE PIN IAW AWA T/C E6C55102. 2L72 4F RTA16WE 20050126000902005012600090EU 2005 1 26 AWXA200500053 120050111A5315D53472172202 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28621AW 053 SAL - MAJOR REPAIR - DURING C-4 CHECK GALVANIC CORROSION WAS FOUND ON FLOOR BEAM Y1292 LT, BETWEEN FS 66 AND FS 68. MAINTENANCE REMOVED CORRODED FLOORBEAM Y1292 LT FROM FS 66 TO FS 68; FABRICATED A NEW REPLACEMENT FLOORBEAM INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050126001082005012600108NM 2005 1 26 WRLA2005003 120050105A2150 A/C PACK DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE NR 1 ODOR A WRLAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO11803 48474 "LAV SMOKE" IN COMBINATION WITH A STRONG OILY SMOKE SMELL IN BOTH CABIN AND COCKPIT ON DEPARTURE. TURNING OFF NR 1 PACK ELIMINATED BOTH "LAV SMOKE" INDICATION AND SMELL. "LAV SMOKE" WAS IN FWD LAV. OPEN PACK COMPARTMENT AND RAN PACK, TEMPERATURE AND ALL OPERATION NORMAL. 2L73 4F4 FRTA22WE E24NE 20050126001152005012600115NM 2005 1 26 WRLA2005002 120050104A2150 A/C PACK DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE NR 1 SMOKE A WRLAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO11271 48518 DURING START OF TAXI, SMOKE FROM AIR CONDITIONING DUCT IN COCKPIT. NR 1 AIR CONDITIONING PACK WAS SELECTED OFF. NO FURTHER CREW ACTION TAKEN. AIRCRAFT RETURNED TO BLOCKS. ENTERED IN DMI M21JA0405-13 PER MEL 21-51-1, NR 1 PACK INOP. 2L73 4F4 FRTA22WE E24NE 20050126001162005012600116NM 2005 1 26 2005UALA00080 120050120A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29580UA 26698 AFT PIT STA 1480 FRAME IS DENTED ON INBD FLANGE, APPROXIMATELY STR 26L. REPAIRED FRAME FLANGE WITH NESTED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20050126001172005012600117NM 2005 1 26 2005UALA00081 120050120A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29580UA 26698 FWD PIT FRAME DENTED ON INBD FLANGE AT STA 620 JUST BELOW STR 24L. REPAIRED FRAME FLANGE WITH NESTED J-ANGLE. 2L72 4F4 FRTA2NM E17NE 20050126001212005012600121 2005 1 26 MWEA050007 420050112A3418 STALL WARNING BOEING717 717200 1383700NM FLIGHT CONTROL FALSE INDICATIONA MWEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL31909ME 55173 STALL WARNING BARBER POLL WENT TO 310 KNOTS AND SAME TIME STICK SHAKER ACTIVATED. PERFORMED RETURN TO SERVICE ON NR 1 AND NR 2 STALL WARNING SYSTEM AND FLIGHT CONTROL COMPUTER, ALL TEST PASSED, INSPECTED STATIC PORTS PITOT TUBES AND ANGLE-OF-ATTACK VANES. NO DISCREPANCY NOTED. OK FOR RETURN TO SERVICE. RELIABILITY ACTION NOTICE TO PURGE PITOT SYSTEM SUMPS. 2L72 4F TRA6WE 20050126001232005012600123GL 2005 1 26 CHQA200500007 220050114A7200AE3007A13 ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 1 LEAKING A CHQAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL11577RP657 657 14500862 CAE312704 FLIGHT 6399 CMH-BDL - AFTER TAKEOFF, A LAV SMOKE MESSAGE APPEARED ON EICAS. A HAZE WAS SEEN IN THE COCKPIT AND A LIGHT SMOKE COULD BE SEEN IN THE GALLEY. AFTER THE CHECKLISTS FOR LAV SMOKE WERE COMPLIED WITH, THE MESSAGE EXTINGUISHED. THE AIRCRAFT RETURNED TO FIELD AND LANDED UNEVENTFULLY. MAINTENANCE TROUBLESHOT THE SYSTEM AND FOUND THE OIL SMELL AND RESIDUE INSIDE BLEED AIR DUCTS. REMOVED AND REPLACED NR 1 ENGINE WITH NEW AND OPS CHECK AND LEAK CHECK GOOD PER EMB J/C CE720001. 2L72 4T4 FRTT00011ATTE6CH 20050126001252005012600125NM 2005 1 26 QXEA200500067 120050114A2611PU90461S SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM LAVATORY FAILED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09347PH17643 480 PDX - FLIGHT 2034 - THE CREW REPORTS THE LAVATORY SMOKE DETECTOR IS SOUNDING INTERMITTENTLY. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE LAVATORY SMOKE DETECTOR. THE ENGINES WERE RUN AND NO SMELLS OR SMOKE WERE NOTED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050126001262005012600126NM 2005 1 26 2005UALA00064 120050116A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29196UA 28715 MOUNTED EEL LIGHT AT SEATS 6AB, 7AB, AND 8AB ARE INOP. REPLACED POWER SUPPLY M6003, TEST OK. 2L74 4F4 FRTA20WE E24NE 20050126001312005012600131EU 2005 1 26 MALA050107 120050105A2460 WARNING LIGHT SAAB SF340 340B 7860101EU LT ESS BUSS ILLUMINATED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15416XJ 340B416 LT MAIN AND ESS BUSS BREAKER POPPED INFLIGHT. AIR RETURN TO DTW. MAINTENANCE RAN BOTH ENGINES, APPLIED HEAVY LOAD ON PDU. NO FAULTS NOTED. REFER TO LOG PG NR 1276924-4 FOR ADDITIONAL INFORMATION. 2L72 4T RTA52EU 20050126001322005012600132EU 2005 1 26 MALA050108 120050105A3230 LANDING GEAR BAC 146 AVRO146RJ85A1500097EU MAINS ICED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15530XJ E2364 AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT. SPOILER UNLOCKED ILLUMINATED AND AUTO THROTTLES DISCONNECTED AND WOULD NOT RE-ENGAGE. AIR RETURN TO DTW. MAINTENANCE NOTED GEAR (MAIN) TO BE BADLY ICED UP SENT TO HANGAR FOR THAW. PERFORMED GEAR SINGS IAW AVRO MM CHAP 32. ALL CHECKS GOOD. 2H74 4F RTA49EU 20050126001332005012600133EU 2005 1 26 MALA050111 120050108A3260 SQUAT SWITCH SAAB SF340 340B 7860101EU MLG LACK OF LUBE A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15423XJ 340B423 AFTER TAKEOFF IN DTW, THE GEAR UNSAFE LIGHT WOULD NOT EXTINGUISH AFTER THE GEAR WAS RETRACTED. FOLLOWED QRH AND THE GEAR WOULD STILL NOT RETRACT. ALL HYDRAULIC INDICATIONS NORMAL. AIR RETURN TO DTW. MAINTENANCE CLEANED AND SWUNG GEAR. LUBED SQUAT SWITCHES. ALL CHECKS GOOD IAW SF340 MM CHAP, 32. 2L72 4T RTA52EU 20050126001342005012600134EU 2005 1 26 MALA050117 120050108A5320 STRUCTURE SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15425XJ 340B425 DURING 4Y/2Y CHECK IN BNA, RT WRAPAROUND PN 7253710-243 IS CORRODED OUT OF LIMITS AND HAS BEEN REPLACED IAW SRM 51-40-21 REFER EAMS WO NR 211363, TASK 1535 FOR ADDITIONAL INFORMATION. AIRCRAFT WAS RELEASED 1/11/05. 2L72 4T RTA52EU 20050126001362005012600136NM 2005 1 26 DHL2005781001 120050104A213039854021 SHUTOFF VALVE BOEING727 727227 1384078NM LT A/C PACK MALFUNCTIONED A DHLABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01781DH 21996 AT FL 270 CABIN ALTITUDE AURAL WARNING SOUNDED AND ALTITUDE ALERTER ILLUMINATED AND AURAL WARNING SOUNDED. UNABLE TO CONTROL CABIN ALTITUDE EXECUTED EMERGENCY DESCENT RETURNED TO DEPARTURE AIRPORT. (AUS) T/S SYS, RAN ENGINES AND PERF DECAY CK PER M/M 05-51-71, CKD WITHIN LIMITS. SUSPECTED EQUIPMENT COOLING BLOWER CTRL VALVE OF BINDING. REMOVED AND REPLACED VALVE PER M/M 21-58-21. SUSPECT LACK OF AIR FLOW FROM LT PACK. REMOVED AND REPLACED LEFT PACK VALVE PER M/M 21-55-71. PERF OPS CK OF PRESS CTRL SYS IAW. 2L73 4F A3WE 20050126001402005012600140CE 2005 1 26 DJFA2005048 120050109A7110128910008602 COWLING BEECH MU300 400A 1155402CE ZONE 400 DETACHED E DJFAO OTHER D INFLIGHT SEPARATION CLCLIMB 1 EA23743TA RK271 CREW REPORTED THAT DURING CLIMB-OUT OF KTEB AT APPROXIMATELY 5,000 FT, THEY HAD FELT A SMALL BUMP. THE REST OF THE FLIGHT WAS WITHOUT INCIDENT. WHILE PERFORMING THE POSTFLIGHT INSPECTION IT WAS DISCOVERED THAT THE LOWER HALF OF THE RIGHT COWLING HAD BEEN TORN AWAY WITH MOST OF THE FASTENERS REMAINING IN PLACE AND LOCKED. MAINTENANCE FITTED AND INSTALLED THE COWLING SUPPORT FRAMES AND A REPLACEMENT COWLING FOR THE RIGHT SIDE. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4F RTA16SW 20050126001422005012600142CE 2005 1 26 DJFA2005049 120050109A760345AS4201039 CABLE ASSY BEECH MU300 400A 1155402CE POWER LEVER BINDING E DJFAA UNSCHED LANDING O OTHER CRCRUISE 1 EA23708TA RK178 CREW REPORTED THAT WHILE AT CRUISE FL390 FOR APPROXIMATELY 15 MINUTES, THEY WERE UNABLE TO ADJUST THE LEFT POWER LEVER AS IT WOULD NOT MOVE. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS DIVERTED TO KELP. WHILE DESCENDING THROUGH FL220 THE LEFT POWER LEVER HAD COME LOOSE. CREW MADE A NORMAL 2 ENGINE APPROACH AND LANDING IN KELP. MAINTENANCE REPLACED THE LEFT AFT POWER LEVER CONTROL CABLE. RUN UP CHECKS WERE GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4F RTA16SW 20050126001522005012600152 2005 1 26 225981 420050103A3431 COMPUTER SAAB SF340 SF340A 7850100EU VOR SYSTEM INCORRECT A UHLAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 GL1735SZ 35 BOTH VOR'S OFF CENTER LINE 2-5 MILES. ATC RECORDS 20 DEGREES OFF WHILE BOTH VOR'S SHOW CENTERED IN AIRCRAFT. HARRISBURG SHOWS CENTERLINE AT V377 WHILE ATC SHOWS 2 MILES OFF. AIRCRAFT WAS FLYING 2 MILES OFF COURSE WHEN NAVIGATING WITH BOTH VOR'S. AIRCRAFT RETURNED TO IAD IS AWAITING MAINTENANCE. 2L72 4T RTA52EU 20050126001602005012600160NM 2005 1 26 AWXA200500039 120050116A3397BMS13311122 WIRE BOEING737 7373G7 1384595NM ZONE 900 BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28158AW 23780 PHX - EEL - DURING INSPECTION MAINTENANCE FOUND THE LT AFT GALLEY EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED BROKEN WIRE TO LT AFT GALLEY EMERGENCY EXIT LIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050126001702005012600170EA 2005 1 26 MASA200500043 120050117A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSBURNED OUT A MASAK NONE O OTHER ININSP/MAINT 1 SW0775999 7471 N75999, THE AIRCRAFT WAS ON R.O.N. AND SCHEDULED FOR A ROUTINE CHECK INSPECTION. DURING THE WALK AROUND IT WAS DISCOVERED THAT THE RIGHT SIDE MID EXTERIOR OVERWING EMERGENCY LIGHT WAS NOT ILLUMINATING. MAINTENANCE REPLACED THE LIGHT BULB AND OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050126001742005012600174EU 2005 1 26 AWXA200500040 120050115A3240C247030014A VALVE AIRBUS320 A320231 3930325EU ZONE 190 BYPASSING A AWXAO OTHER O OTHER TXTAXI/GRND HDL 1 WP28620AW4465828275 052 AFTER TOUCH DOWN, THE BRAKES LOCKED UP ON TAXIWAY, AIRCRAFT UNABLE TO TAXI TO GATE, SHUTDOWN AND DISEMBARKED PASSENGERS ON TAXIWAY. MAINTENANCE REMOVED AND REPLACED PARKING BRAKE SELECTOR VALVE IAW AMM 32-45-51, LEAK AND OPERATIONAL CHECKS WERE GOOD. CONFIRMED FAILURE OF UNIT FINDING ONE SIDE OF THE MOTOR WAS INOPERATIVE AND FLUID LEAKAGE AT RETURN PORT VALVES. REPLACED MOTOR AND SEALS AND RE-ACCOMPLISHED FUNCTIONAL TEST IAW CMM 32-47-24, REV. 4. 2L72 4F RTA28NM 20050127000012005012700001EA 2005 1 27 COMA0560066 120050117A27308220260001 SERVO CNDAIRCL600 CL6002B19 1900309EA ELEVATOR INSTALLED A COMAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SO01427CA10946 7460 FLIGHT 5154 ON FINAL WITH A/P OFF, FO'S ELEVATOR CONTROLS JAMMED. WHEN PRESSURE APPLIED CONTROLS BROKEN FREE. COULD NOT DUPLICATE INSPECTION OF FLIGHT CONTROLS FOUND NO DEFECTS. REPLACED THE ELEVATOR SERVO MOUNT FOR TROUBLE SHOOTING. 2L72 4F RTA21EA 20050127000022005012700002EA 2005 1 27 COMA0560067 120050119A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA RIGHT UNRELIABLE A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01977CA6806 7157 FLIGHT 5725, FLAPS FAILED WHEN SELECTED TO 20 DEGREES. REPLACED THE RT BPSU. 2L72 4F RTA21EA 20050127000032005012700003CE 2005 1 27 DELA20050001 120050114A2120 SMOKE LEAR 35 31 5170530CE GARRTTTFE731TFE73123B WP COCKPIT DETECTED E DELAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 CE03888CP 31003 99103 IMMEDIATELY FOLLOWING TAKEOFF, THE FLIGHT CREW OBSERVED AN ODOROUS VAPOR IN THE CABIN. FOLLOWING CONTACT WITH ATC AND REDUCING CABIN AIR INFLOW, THE CREW IMMEDIATELY RETURNED TO THE DEPARTURE AIRPORT UNEVENTFULLY. THE SMOKE OR VAPOR ACCUMULATION BEGAN DISSIPATING FOLLOWING ENGINE POWER REDUCTION. THIS INFORMATION WILL BE UPDATED AS FURTHER INFORMATION IS ACQUIRED. 2L72 4F4 FRTA10CE E6WE 20050127000052005012700005NM 2005 1 27 P9RA20050065 120050117A33502013A1 BATTERY PACK BOEING757 757236 1384971NM EMERGENCY LIGHT INOPERATIVE A P9RAK NONE L NO TEST ININSP/MAINT 1 SO11962PG 24119 AIRCRAFT IN MAINTENANCE ORD, DOORS 2L AND 2R EMERGENCY LIGHTING INOPERATIVE. REMOVED AND REPLACED BATTERY PACKS FOR EMERGENCY LIGHTS IAW MM. L2 DOOR PART INFORMATION, PART NUMBER 2013A1, SERIAL NUMBER OFF 24696, BATTERY PACK. R2 DOOR AS STATED BELOW. 2L72 4F RTA2NM 20050127000082005012700008EU 2005 1 27 YENA200514 120050122A3150350E018312020 COMPUTER AIRBUS320 A320232 3930326EU NR 1 FLT WARNINGFAILED A YENAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA15506JB1220959 1235 ON CLIMB THROUGH FL300 ECAM WARNING ENG 1 N2 OVER LIMIT, THERE WAS NO INDICATION OF N2 OVER LIMIT NO RED TICK WAS VISIBLE AND ENG PARAMETERS WERE NORMAL;, REDUCED POWER TO IDLE AND ELECTED NOT TO SHUT DOWN ENGINE RETURNED TO FLL, OVER WEIGHT LANDING. PERFORMED TSM 31-53-00-810-868, REMOVED AND REPLACED FWC NR 1 AND 2 DUE TO PARTS AVAILABILITY IAW MM 31-53-34, OPS CK GOOD. REMOVED AND REPLACED NR 1 ENG EEC PRECAUTIONARY IAW MM 73-22-34-04. PERFORMED IDLE RUN-UP AND OPS CK OF FADEC SYS IAW MM F73-22-00, NO FAULTS NOTED ALL PARAMETERS NORMAL. 2L72 4F RTA28NM 20050127000092005012700009NM 2005 1 27 P9RA20050066 120050116A335020131A BATTERY PACK BOEING757 757236 1384971NM EMERGENCY LIGHT INOPERATIVE A P9RAK NONE L NO TEST ININSP/MAINT 1 SO11522NA 25133 AIRCRAFT IN MAINTENANCE DTW, EMERGENCY LIGHTS AT R2 DOOR INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK IAW MM. 2L72 4F RTA2NM 20050127000102005012700010 2005 1 27 YENA200508 420050112A2565 INDICATOR AIRBUS320 A320232 3930326EU RT SLIDE INOPERATIVE A YENAO OTHER P NO WARNING INDICATION TXTAXI/GRND HDL 1 EA15597JB 2307 RT WHITE SLIDE INDICATION NOT PRESENT. TURNED PIN CLOCKWISE AND BACK TO ORIGINAL POSITION INDICATION NORMAL 25-64-00. 2L72 4F RTA28NM 20050127000132005012700013NM 2005 1 27 UPS05243698 120050111A5754 RIB BOEING727 727185C 138406NNM NR 8 SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 INSPECTION TYPE: C, NR 8 LE SLAT STRUCTURE HAS CRACKED RIB JUST O/B OF ACTUATOR ATTACH POINT. REPAIR CARRIED OUT IAW SRM 57-50-03. 2L73 4F A3WE 20050127000152005012700015NM 2005 1 27 UPS05243700 120050113A5753 BRACKET BOEING727 727185C 138406NNM NR 5 FLAP TRACK CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 INSPECTION TYPE: C, NR 5 FLAP TRACK, FWD O/B FAIRING ATTACH ANGLE BRACKET IS CRACKED. BRACKET REPLACED IAW SRM 51-20-1. 2L73 4F A3WE 20050127000182005012700018EU 2005 1 27 YENA200512 120050118A52702LA00546700 CONTROL PANEL AIRBUS320 A320232 3930326EU L-2 DR POSITION SHORTED A YENAO OTHER O OTHER NRNOT REPORTED 1 EA15528JB13364 1591 L-2 DOOR PASSING THROUGH FL200 AND FL190 DISARMED AND STAYED DISARMED UNTIL LANDING AND DEPLANING. ITEM PLACED ON MEL C#L05701 CAT C CONDITION NR 2 REFERENCE MEL 25-60-04 MX-4 UPDATED. MCC NOTIFIED. PLACARD INSTALLED. MEL CLEARED WITH TSM CORRECTIVE ACTIONS. PERFORMED TSM TASK NR 52-73-00-810-801 AND TSM TASK 52-13-00-810-806, FOUND CAB PRESS WARNING PANEL 17WN1 ON L-2 DOOR SHORTED INTERNALLY AT PINS A AND B REF ASM 52-73-02, ALSO FOUND L-2 SLIDE ARM PROX SWITCH 7WN1 INTERNALLY DAMAGED DUE TO FAILURE OF 17WN1 TEF ASM 52-73-01. WIRING VERIFIED OK BETWEEN MODULES 7WN1, 3WN1 AND 17WN1 IAW 52-73-01. REMOVED AND REPLACED 17WN1 IAW 52-73-22-401, OPS CHECK OK. R/R 7WN1 IAW AMM 52-73-11-401. OPS CHECK OK. 2L72 4F RTA28NM 20050127000192005012700019NM 2005 1 27 UPS05243702 120050111A5753 SUPPORT ANGLE BOEING727 727185C 138406NNM NR 3 FLAP TRACK CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 INSPECTION TYPE: C, NR 3 FLAP TRACK FAIRING SUPPORT ANGLE CRACKED AT I/B AFT END. FAIRING SUPPORT ANGLE REPAIRED IAW SRM 51-20-01. 2L73 4F A3WE 20050127000262005012700026NM 2005 1 27 UPS05443696 120050107A5347 SEAT TRACK BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C - STA 1482 LBL 99 SEAT TRACK FLANGE CORROSION. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.050 INCH BY 1 INCH BY 1 INCH. CORROSION BLEND OUT EXCEED SRM 53-10-01 FIG 1 LIMITS, REPAIR REFER TO SRM 53-10-05 FIG 1A. 2L74 4F A20WE 20050127000282005012700028 2005 1 27 YENA200511 420050116A2565 PROXIMITY SENSOR AIRBUS320 A320232 3930326EU ESCAPE SLIDE INOPERATIVE A YENAO OTHER O OTHER LDLANDING 1 EA15528JB 1591 L2 DOOR SLIDE WILL NOT DISARM. DEF INDICATION TO MEL 25-60-04, CONTROL NR L05690 AS PER KROA MCC, VERIFIED THAT ASS SLIDE IS ARMED CAT B. MEL WAS CLEARED ON REMOVED AND REPLACED DOOR ARM PROX SENSOR AS PER AMM 52-71-00, OPS CHECK OK. 2L72 4F RTA28NM 20050127000332005012700033SO 2005 1 27 RAIA00501035 120050114A32608005701 PROXIMITY SWITCH EMB 145 EMB145 3260210SO MLG MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03804HK3928 145082 3578 - PIT- LANDING GEAR WOULD NOT RETRACT. MAINTENANCE INSPECTED AIRCRAFT AND FOUND BOTH LEFT DOWN LOCK PROX SWITCHES INOP. REMOVED AND REPLACED ONE PROX SWITCH AND CLEANED OTHER. 2L72 4F RTT00011AT 20050127000372005012700037SO 2005 1 27 RAIA00501037 120050116A7830 WARNING LIGHT EMB 145 EMB145LR 3260212SO THRUST REVERSER ILLUMINATED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03810HK 145231 3519- PIT- EICAS MESSAGE THRUST REVERSE DISAGREE DURING TAKEOFF. MAINTENANCE PERFORMED, OPS CHECKOF THRUST REVERSE. 2L72 4T RTT00011AT 20050127000392005012700039 2005 1 27 RAIA00501007 420050104A34257510100831 DISPLAY EMB 145 EMB145LR 3260212SO NR 1 NAVIGATION INOPERATIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03840HK7365 1827 145341 NAV DISPLAY NR 1 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 1 NAV UNIT. 2L72 4T RTT00011AT 20050124000872005012400087NM 2005 1 24 QXEA200500052 120050108A2760 SPOILER BOMBDRDHC8 DHC8401 1390041NM OUTBOARD INOPERATIVE A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09410QX 4053 THE FLIGHT RETURNED TO GATE WHEN THE CREW NOTICED THAT THE OUTBOARD SPOILERS GROUND SPOILERS DO NOT EXTEND WHEN THE FLIGHT/TAXI SWITCH IS IN THE FLIGHT MODE. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE SYSTEM ON MEL. THE SPOILER POWER UNIT WAS FOUND BAD AND WAS REPLACED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050124001162005012400116WP 2005 1 24 WX0500003 120050107A2133 OUTFLOW VALVE DOUG DC9 DC983 3022083WP CABIN PRESSURE OBSTRUCTED A WX0ABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP19868GA 49554 DURING FLT AT APPROX 25,000 FT, HAD IND`S OF INCREASED RATE OF CLIMB THAT EXCEEDED 1000 FPM. ATTEMPTED TO ADJUST RATE OF CLIMB WITH CONTROL KNOB. REPEATED ATTEMPTS DID NOT SLOW RATE, AFTER LEVEL OFF AT 35,000 FT CABIN PRESS CONTROLLER CONTINUED TO INDICATE CLIMB. PERFORMED QRH CHECKLIST, INEFFECTIVE AT CONTROLLING PRESSURE. MANUAL CONTROL DIFFICULT TO MOVE & REQUIRED EXCESS FORCE, CABIN ALT EXCEEDED 10,000 FT. CREW DONNED O2 MASKS. DIVERTED TO DEN. DURING DESCENT CABIN ALTITUDE EXCEEDED 14,000 FT & PAX O2 PNLS OPENED. A/C LANDED DEN W/O FURTHER INCIDENT. MX FOUND EXCESSIVE PAINT ON NOZZLE VALVE. MX REMOVED PAINT. PRIMARY, STANDBY & MANUAL OPS ALL CHECKED GOOD IAW MM. A/C RETURNED TO SERVICE . 2L72 4F RTA6WE 20050124001242005012400124NM 2005 1 24 QXEA200500013 120050104A521085210246001 STOP DHAV DHC8 DHC8202 2809007NM MAIN CABIN DOOR OUT OF ADJUST A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09360PH7575 515 CREW REPORTS THE MAIN CABIN DOOR HARD TO OPEN. MAINTENANCE INSPECTED THE DOOR AND FOUND THE FORCE REQUIRED TO OPEN THE DOOR WAS 35 LBS. THE DOWN LIMIT STOP WAS ADJUSTED IAW THE AMM AND THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050125000072005012500007CE 2005 1 25 DXTA200500554 120050123A3230 LANDING GEAR CESSNA750 750 2076810CE NOSE MALFUNCTIONED E DXTAO OTHER J WARNING INDICATION CLCLIMB 1 GL07975QS 7500175 DEPARTING TAMPA, THE NOSE GEAR FAILED TO RETRACT FOR SEVERAL SECONDS AFTER THE MAIN GEAR WAS UP AND LOCKED. A GREEN NOSE GEAR LIGHT AND AN UNLOCKED LIGHT ON DURING THIS TIME. ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20050125000092005012500009NM 2005 1 25 SWAA050167 120050121A2910651782121 MODULE BOEING737 7377H4 1384404NM MLG WW LEAKING A SWAAO OTHER K FLUID LOSS DEDESCENT 1 SW29719SW 27853 DECLARED EMERGENCY, A-SYSTEM HYDRAULIC FAILURE, QUANTITY LOSS. REMOVED AND REPLACED A-SYSTEM FILTER MODULE O-RING PER MM. 2L72 4F RTA16WE 20050125000102005012500010NM 2005 1 25 UPS05243685 120050112A575165217287 HINGE BOEING727 727185C 138406NNM LT OB AILERON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 INSPECTION TYPE:C, LEFT O/B AILERON O/B BALANCE PANEL FWD IDLER HINGE CRACKED. HINGE REPLACED IAW 51-30-2. 2L73 4F A3WE 20050125000182005012500018NE 2005 1 25 MALA050137 220050118A7200 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RIGHT MALFUNCTIONED A MALAEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 GL15362PX 340B258 GEE785766 RIGHT GEN FAIL LIGHT ILLUMINATED RIGHT ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED. OIL PRESSURE DROPPED TO ZERO ENGINE SHUT DOWN IN COMPLIANCE WITH QRH. DIVERTED A/C TO RST. MAINTENANCE REPLACED RIGHT ENGINE PER TASK CARD 7100-301, P/N ON CT7-9B, S/N ON GE-E785350, S/N OFF GE-E-785766. 2L72 4T4 TRTA52EU E8NE 20050125000222005012500022EA 2005 1 25 SWIA200514406 120050115A2760C13045BA03 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA SPOILER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07716SK 10180 SSCU 2 FAULT MESSAGE ON ED2. REMOVED AND REPLACED SSCU 2 IAW AMM 27-61-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050125000242005012500024EU 2005 1 25 MALA050132 120050113A2435 STARTER GEN SAAB SF340 340B 7860101EU NR 2 ENGINE FAILED A MALAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 GL15427XJ 340B427 DURING BATTERY START ON NR 2 ENGINE MOTORED TO 22 PERCENT, INTRODUCED FUEL GOT LIGHT OFF, FOLLOWED BY A DECREASE IN ROTATION AND A FIRE SIGNAL FROM THE RAMP AGENT. RIGHT HANDLE PULLED AND FIRE BOTTLE FIRED. RAN, NO FIRE. MAINTENANCE REMOVED AND REPLACED RIGHT ENGINE FIRE BOTTLE AND FWD CARTRIDGE BOTTLE S/N OFF 2470EL, S/N ON 24722EL. REPLACED STARTER GEN S/N OFF 3310, S/N ON 7570. PERFORMED GENERAL ENGINE INSPECTION. NO DEFECTS NOTED. PERFORMED GROUND RUNS, ALL CHECKS GOOD. 2L72 4T RTA52EU 20050125000292005012500029NM 2005 1 25 UPS05443673 120050106A5711 SPAR BOEING747 747123 1384873NM LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C, LT WING UPPER REAR SPAR SIDE OF BODY SPLICE FOUND CORROSION CRACK AT HOLE NR 4 AT INTERNAL SPLICE FITTING (REFER FIGURE FOR DETAILS ). HOLE REPAIRED AS PER SB 747-57A2317. 2L74 4F A20WE 20050125000392005012500039NM 2005 1 25 SWAA050170 120050122A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SPV, FOUND FUSELAGE SKIN AT BS 751, STRINGER 18L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050125000522005012500052 2005 1 25 SWAA050166 420050122A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29434WN 32454 R2 DOOR EVAC SLIDE FELL, OUT DID NOT DEPLOY. REINSTALLED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050125000582005012500058CE 2005 1 25 DXTA200500545 120050119A3260387 BULB CESSNA560 560XL 2076702CE MLG INDICATOR INOPERATIVE E DXTAO OTHER J WARNING INDICATION LDLANDING 1 GL07676QS 5605176 LANDING - RIGHT GEAR DOWN LIGHT WOULD NOT TURN GREEN. RECYCLED GEAR, CHECK ROTARY TEST, LIGHT OUT. EMERGENCY GEAR EXTEND AND LANDED. REPLACED RIGHT GEAR DOWN LIGHT BULB P/N 387. RESET EMERGENCY GEAR EXTEND AND CARRIED OUT GEAR RETRACTION REF A/C M/M CH32-01-00 PG 501. PNEUMATIC BOTTLE FOR LANDING GEAR SERVICED TO 2000 PSI AS PER M/M 12-13-01 PG 301. 2L72 4F RTA22CE 20050125000772005012500077CE 2005 1 25 DXTA200500549 120050121A4920 APU RAYTHNDH125 HAWKER800XP 7150012CE APU BAY SMOKE E DXTAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL07845QS 258545 ON GROUND APU WILL FILL CABIN WITH EXHAUST WHEN BLEED AIR ON. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA3EU 20050125000812005012500081EA 2005 1 25 COMA0560046 120050111A33504626 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A COMAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01811CA 7380 FLIGHT 5753 EMERGENCY LIGHT AT ROW 1 IS INOP. REPLACED LAMP. 2L72 4F RTA21EA 20050125000822005012500082EA 2005 1 25 COMA0560047 120050111A4920 APU CNDAIRCL600 CL6002B19 1900309EA APU BAY SMOKE A COMAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO01785CA 7326 FLIGHT 5834 APU SMELLED LIKE FUEL, SMOKE COMING FROM INTAKE. COULD NOT DUPLICATE. INSPECTED APU FOR FUEL LEAKS. NO DEFECTS FOUND. 2L72 4F RTA21EA 20050125000832005012500083EA 2005 1 25 COMA0560050 120050112A3350362624 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A COMAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01914CA 7012 FLIGHT 5694 FWD SECTION OF CABIN EMERGENCY LIGHTING IS INOP. REPLACED FLEX LAMP. 2L72 4F RTA21EA 20050125000872005012500087EA 2005 1 25 COMA0570010 120050116A27505911330 CONTROL HANDLE CNDAIRCL600 CL6002C10 1390015EA TE FLAPS STUCK A COMAA UNSCHED LANDING O OTHER CLCLIMB 1 SO01391CA 10108 FLIGHT 5670 FLAPS/SLATS CONTROL HANDLE IS STUCK. REPLACED FLAPS/SLATS SELECTOR LEVER. 2L72 4F RTA21EA 20050125000902005012500090SO 2005 1 25 C2XA05BT004 120050113A21508152401 HEAT EXCHANGER EMB 145 EMB145 3260210SO NR 1 A/C PACK ODOR A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW2719966 145131 CREW REPORTED, BURNING SMELL IN COCKPIT. MAINTENANCE RAN NR 1 AIR CONDITIONING PACK FOR 20 MINUTES WITH NO SMELL NOTED IAW EMB145 MM 21-51-00, OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20050125001072005012500107SO 2005 1 25 C2XA05TY003 120050113A532014522178005 SILL EMB 145 EMB145LR 3260212SO SERVICE DOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714953 145071 TYS, DURING A SCHEDULED INSPECTION THE SERVICE DOOR SILL WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE DOOR SILL IAW EMB-145-AMM-21-31-00 / 135/145 SRM 51-40-00 AND 52-20-03, CABIN LEAKAGE AND FUNCTIONAL CHECKED GOOD. 2L72 4T RTT00011AT 20050125001142005012500114SO 2005 1 25 C2XA05BT003 120050113A3350110049 POWER SUPPLY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT FAULTY A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714543 145553 DURING ROUTINE CHECK IN BTV MAINTENANCE FOUND BOTH OVERWING EMERGENCY LIGHTS NOT FUNCTIONING. REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY POWER SUPPLY IAW EMB145 AMM 33-50-04, OPS CHECKED SYSTEM GOOD. 2L72 4T RTT00011AT 20050125001172005012500117NM 2005 1 25 CALA0500014 120050119A53306545774575 SKIN BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2759302 23353 INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE SKIN EIGHT INCHES FORWARD OF STA 727E AND BELOW STRINGER 22L. AN INTERIM REPAIR WAS PERFORMED IAW ECRA 5330-03410. A DIP WAS ISSUED TO INSPECT PER PART 2 WITHIN 60,000 FLIGHT CYCLES FROM REPAIR INSTALLATION AND THEN REINSPECT EVERY 25,000 CYCLES. 2L72 4F RTA16WE 20050125001222005012500122NM 2005 1 25 2005UALA00079 120050120A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29580UA 26698 LT FUSELAGE SKIN AT BS 610 AND STR 16L IS DENTED ON A PREVIOUS REPAIR DOUBLER. REPAIRED SKIN WITH A DOUBLER-TRIPLER. 2L72 4F4 FRTA2NM E17NE 20050126000032005012600003SO 2005 1 26 CHQA200500015 120050121A3260 CONNECTOR EMB 145 EMB145LR 3260212SO MLG LOOSE A CHQAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL11260SK 145128 FLIGHT 3082 - CHS-LGA - AFTER GEAR RETRACTION ON TAKEOFF, LG AIR/GND FAIL MESSAGE APPEARED ON EICAS. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO THE FIELD AND LANDED NORMALLY. MAINTENANCE CLEANED ALL PROXIMITY SWITCHES AND FOUND A LOOSE CONNECTOR WHICH WAS RESECURED. OPS CHECK GOOD PER EMB 145 AMM. 2L72 4T RTT00011AT 20050126000572005012600057EA 2005 1 26 05003645 120050103A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A VTZAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 EA27645BR 7383 FLAP FAIL AT 8 PERCENT RT BPSU, FECU, WIRING BPSU. RESET SYSTEM, OPS CHECKED GOOD IAW 27-50-00. 2L72 4F RTA21EA 20050126000682005012600068WP 2005 1 26 MWEA050010 120050116A335060030451 BATTERY DOUG DC9 DC981 3022081WP ROW 14 & 16 INOPERATIVE A MWEAK NONE O OTHER ININSP/MAINT 1 GL31803ME 48029 EMERGENCY CEILING LIGHTS BETWEEN SEAT 14 AND 16 INOPERATIVE. REMOVED AND REPLACED EMERGENCY CEILING LIGHT BATTERIES. 2L72 4F A6WE 20050126000752005012600075NM 2005 1 26 QXEA200500003 120050101A216080053533 CONTROL PANEL DHAV DHC8 DHC8202 2809007NM ZONE 200 FAILED A QXEAO OTHER J WARNING INDICATION APAPPROACH 1 NM09348PH154631204 484 THE EMERGENCY/ABNORMAL CHECKLIST WAS COMPLIED WITH WHEN THE FLIGHT COMPARTMENT DUCT CAUTION LIGHT ILLUMINATED ON DESCENT. MAINTENANCE REPLACED THE CAUTION LIGHTS PANEL AND PERFORMED OPERATIONAL CHECKS. THE CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050126000812005012600081EA 2005 1 26 MASA200500035 120050115A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSBURNED OUT A MASAK NONE O OTHER ININSP/MAINT 1 SW0775991 7422 N75991 THE AIRCRAFT WAS ON R.O.N. AND SCHEDULED FOR A ROUTINE CHECK INSPECTION. DURING THE WALKAROUND IT WAS DISCOVERED THAT THE AFT INTERIOR CEILING EMERGENCY LIGHT WAS NOT ILLUMINATING. MAINTENANCE REPLACED THE LIGHT BULB AND OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050126000952005012600095EA 2005 1 26 05006671 120050106A2740 SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB MACH TRIM MALFUNCTIONED A VTZAO OTHER J WARNING INDICATION CLCLIMB 1 EA27671BR 7572 STAB AND MACH TRIM KICKED OFF LINE ON CLIMB-OUT. PERFORMED OPS CHECK OF STAB AND MACH TRIM ENGAGE SWITCHES IAW AMM 27-41-15 AND AMM 27-41-20. NO DEFECTS NOTED AT THIS TIME. 2L72 4F RTA21EA 20050126000972005012600097WP 2005 1 26 AALA20050032 120050117A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21218AA 49168 MIA - EMERGENCY LIGHT IN COCKPIT OVERHEAD INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT IN COCKPIT OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050126001062005012600106NM 2005 1 26 QXEA200500012 120050102A27603958001005 DUMP VALVE BOMBDRDHC8 DHC8401 1390041NM RT SPOILER FAILED A QXEAO OTHER F FLT CONT AFFECTED DEDESCENT 1 NM09410QX7556 4053 GTF - FLIGHT 2321 - DURING THE DESCENT, FULL LEFT WING DOWN AILERON TRIM WAS REQUIRED TO FLY STRAIGHT. THE CREW NOTICED THE RIGHT INBOARD SPOILER WAS PARTIALLY EXTENDED ON THE PFCS DURING THE DESCENT. AFTER TOUCHDOWN, THE ROLL SPLR INBOARD CAUTION ILLUMINATED AND THE RIGHT INBOARD SPOILER WAS FULLY EXTENDED. MAINTENANCE INTERROGATED THE CDS AND FOUND AN "INBD GROUND VALVE" MESSAGE IN THE FAULT HISTORY. THE FAULT WAS CLEARED AND GROUND RUNS WERE PERFORMED. MAINTENANCE WAS UNABLE TO DUPLICATE THE WRITE UP. THE UPPER INBOARD SPOILER LIFT DUMP VALVE WAS REPLACED. OPERATIONAL AND LEAK CHECKS WERE PERFORMED AND ALL WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050126001222005012600122NM 2005 1 26 2005UALA00063 120050115A5315 FLOORBEAM BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29907UA 25007 FLOORBEAM CORRODED ON AFT FLANGE STA 986 FROM RBL 10 TO LBL 6. SUPPLEMENTAL DATA UPDATE, MAJOR REPAIR ACCOMPLISHED. CUT-OUT DAMAGE AND INSTALLED REPAIR ANGLE AND FILLER. 2L72 4F4 FRTA16WE E2GL 20050126001432005012600143EU 2005 1 26 CX7A194J0501 120050102A26121734362450 DETECTOR SAAB SF340 340B 7860101EU LT TAILPIPE SATURATED A CX7AC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL03300CE 340B184 LEFT TAILPIPE HOT LIGHT ILLUMINATED ON TAKEOFF. 2L72 4T RTA52EU 20050126001472005012600147EU 2005 1 26 SA05001 120050101A335032145410 EPSU AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT FAULTY A USAAK NONE O OTHER ININSP/MAINT 1 EA19754UW8248 1328 THE EMERGENCY LIGHTS ON THE LEFT SIDE OF THE CABIN WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT IN THE FORWARD LEFT POSITION. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20050126001492005012600149EU 2005 1 26 SA05003 120050102A2120 ODOR AIRBUSA319 A319112 3930323EU CABIN DETECTED A USAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA19722US 1097 IN CRUISE FLT, CABIN CREW REPORTED A RUBBER/ELECTRIC ODOR AROUND ROW 18. THE VIDEO ENTERTAINMENT SYS TURNED OFF. ODOR SUBSIDED, BUT CAME BACK BRIEFLY. ODOR SUBSIDED AGAIN & REMAINED THAT WAY FOR THE REST OF THE FLIGHT. MX COULD NOT DUPLICATE THE ODOR. PLACED THE VIDEO ENTERTAINMENT SYSTEM ON MEL. 2L72 4F RTA28NM 20050126001922005012600192EU 2005 1 26 CX7A194J0504 120050102A26121734362450 DETECTOR SAAB SF340 340B 7860101EU LT TAILPIPE SATURATED A CX7AO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL03303CE 340B194 LT TAIL PIPE HOT INDICATION AFTER POWERING UP A/C DURING PREFLIGHT. 2L72 4T RTA52EU 20050127000142005012700014NM 2005 1 27 UPS05243699 120050110A5752 TAB BOEING727 727185C 138406NNM AILERON DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 INSPECTION TYPE: C, LT O/B AILERON TAB DELAMINATED AT UPPER I/B END. AILERON TAB REPAIRED IAW SRM 51-40-20. 2L73 4F A3WE 20050127000222005012700022NM 2005 1 27 UPS05443692 120050107A5313 LONGERON BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE :C, STR BS 1120 S-7L CRACKED, M/D BS 1120 STR 7L STRINGER. REPAIRED CARRIED OUT IAW SRM 53-10-03 FIG 4. 2L74 4F A20WE 20050127000302005012700030SO 2005 1 27 RAIA00501025 120050111A7500 BLEED AIR SYS EMB 145 EMB145LR 3260212SO NR 2 ENGINE LEAKING A RAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03816HK 145055 5662- PHL- BLEED LEAK NR 2 INFLIGHT, CHECKLIST ENGINE SHUTDOWN. MAINTENANCE COULD NOT DUPLICATE ON GROUND, INSPECTED BLEED SYSTEM FOR LEAKS, CHECK GOOD. 2L72 4T RTT00011AT 20050127000322005012700032SO 2005 1 27 RAIA00501029 120050112A7500 O-RING EMB 145 EMB145LR 3260212SO BLEED AIR SYS FAILED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03816HK 145055 5618- STL- NR 2 BLEED LEAK MESSAGE ON EICAS. MAINTENANCE REMOVED AND REPLACED NR 2 BLEED LINE O-RING. 2L72 4T RTT00011AT 20050127000352005012700035SO 2005 1 27 RAIA00501023 120050110A4990 OIL CAP EMB 145 EMB145 3260210SO APU UNSECURE A RAIAA UNSCHED LANDING WKBINADEQUATE Q C FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 CE03803HK 145077 3607- RIC- LAV SMOKE ON EICAS IN FLIGHT. MAINTENANCE INSPECTED FOUND APU OIL SERVICE CAP UNSECURED, CLEANED APU COWLING. 2L72 4F RTT00011AT 20050127000852005012700085SO 2005 1 27 CHQA200500002 120050111A2120 ODOR EMB 145 EMB145LR 3260212SO CABIN DETECTED A CHQAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL11578RP 14500865 AFTER TAKEOFF, A LAV SMOKE WARNING MESSAGE APPEARED ON EICAS. A SHORT TIME LATER A ODOR AND HAZE WERE NOTED IN THE COCKPIT. AFTER ACCOMP CABIN FIRE AND SMOKE PROCEDURES, EICAS MESSAGE WENT AWAY ALONG WITH THE ODOR AND HAZE. THE F/A CHECKED THE LAV AND BAG COMPT AND FOUND TO TRACE OF SMOKE OR FIRE. AN EMERG WAS DECLARED, THE PLANE RETURNED TO FIELD W/O INCIDENT. MX INSPECTED THE LAV FOR EVIDENCE OF SMOKE AND NONE WAS FOUND. SET UP THE A/C IN SAME CONFIGURATION AS IT WAS FOR TAKEOFF AND DID MAX POWER RUNS. THE A/C CHECKED OK NO ODORS NOTED. A TEST FLT WAS PERFORMED TO VERIFY NO FURTHER PROBLEMS. NO SMOKE OR ODOR WAS NOTED DURING THE TEST FLT AND THE A/C WAS RETURNED TO SERVICE. 2L72 4T RTT00011AT 20050127000872005012700087SO 2005 1 27 CHQA200500003 120050112A2611FDS765A2 SMOKE DETECTOR EMB 145 EMB145LR 3260212SO LAVATORY DIRTY A CHQAO OTHER N FALSE WARNING CLCLIMB 1 GL11578RP 14500865 FLIGHT 6450 IND TO CVG - DURING CLIMB-OUT, A LAV SMOKE WARNING MESSAGE BRIEFLY APPEARED ON EICAS. THE FLIGHT ATTENDANT INSPECTED THE LAV AND FOUND NO EVIDENCE OF SMOKE OR FIRE. THE CABIN GASPERS WERE MISTING SLIGHTLY PRIOR TO THE INDICATION. INSPECTED LAV SMOKE DETECTOR AND FOUND EXCESSIVE DUST IN THE UNIT. CLEANED AND TESTED LAV SMOKE DETECTOR WITH NO FURTHER DEFECTS NOTED. OPS CHECK GOOD IAW EMB 26-14-01. 2L72 4T RTT00011AT 20050127000942005012700094EU 2005 1 27 YENA200509 120050116A2120 ODOR AIRBUS320 A320232 3930326EU CABIN DETECTED A YENAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15509JB 1270 CABIN CREW REPORTED BURNING RUBBER ODOR IN CRUISE OF FLT. ODOR BARELY DETECTABLE. INSPECTED THE AIRCRAFT CABIN IAW (ATA 23-39)LIVE TV SYSTEM INTEGRITY CHECK CONCERNING ELECTRICAL ODORS AND FOUND LIVE TV SYSTEM SATISFACTORY WITH NO EVIDENCE OF ELECTRICAL ODORS, LTV SYSTEM OPERATING IAW LTV MM 23-39-00. AS PER FLT CREW REPORT RUBBER ODOR IN AFT CABIN BARELY DETECTABLE AS PER AMM TSM TASK 26-15-00-810-814 NO ODOR DETECTED IN AFT CABIN, CHECK NORMAL, ALSO COMPLIED W/TSM 24-00-00-810-823- NO DEFECT NOTICED. 2L72 4F RTA28NM 20050127001032005012700103NM 2005 1 27 DHL2005784001 120050111A3242 BRAKE BOEING727 727227 1384078NM NR 4 FAILED A DHLAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO01784DH 22001 AC REQUIRES EXCESSIVE POWER TO TAXI AND CAME TO A COMPLETE STOP TWICE W/ NO BRAKE APPLICATION AT LESS THAN 150.0 LBS. REMOVED AND REPLACED NR 4 BRAKE AND T/W ASSY IAW B-727-200 MM CH 32-41-32 AND 32-45-1, LEAKS CHECK GOOD IAW 32-41-32. 2L73 4F A3WE 20050127001112005012700111SO 2005 1 27 SWIA200514428 120050121A2797 WIRE EMB 120 EMB120ER 3260203SO SENSOR CONNECTORLOOSE A SWIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM07235SW 120310 TAKEOFF AURAL WARNING TAKEOFF TRIM HEARD ON TAKEOFF ROLL. TRIM WAS INSIDE GREEN BAND. ABORTED, RETURNED TO GATE. REPAIRED SENSOR WIRING WITH NEW CONNECTOR. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050127001132005012700113NM 2005 1 27 UPS05443758 120050125A3350 BATTERY PACK BOEING747 747200 1384847NM R1 DOOR INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 EMERGENCY LIGHTS INOP OVER R-1 DOOR. REPLACED BATTERY PACK PER MM 33-51-02. 2L74 4F RTA20WE 20050127001162005012700116EU 2005 1 27 DHL2005362001 120050115A293069520002000NC0A PACKING AIRBUS300 A300B4203 3930306EU FILTER BOWL LEAKING A DHLAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO01362DH 84 GREEN HYD LOW LEVEL LIGHT ILLUM IN CRUISE. MWP HYD LIGHT ILLUM, NEEDLE BELOW RED DOT. RAN HYD FLUID LOSS ABNORMAL PROCEDURE. FOUND GREEN SYS FILTER BOWLS. REMOVED AND REPLACED PACKINGS. SERVICED PER 29-00-00, RAN ENGS PER JRH, NO LEAKS NOTED. ALL 3 SYSTEMS OP NORMAL, OK FOR SERVICE. 2L72 4F RTA35EU 20050127001182005012700118NM 2005 1 27 0500115518 120050121A2913623303 PUMP BOEING757 757251 1384970NM HYD SYSTEM LEAKING A NWAAH DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL01518US5889830101 23206 DURING FLIGHT, THE CENTER HYDRAULIC PUMPS WERE TURNED OFF DUE TO THE HYDRAULIC QUANTITY AND PRESSURE WENT TO ZERO. LANDING WAS UNEVENTFUL. FOUND ELECTRIC PUMP LEAKING AT THE LOWER SEEP HOLE. REPLACED THE PUMP AND SERVICED SYSTEM. OPERATIONAL CHECK GOOD. 2L72 4F RTA2NM 20050127001202005012700120NM 2005 1 27 QXEA200500122 120050125A6120 SWITCH DHAV DHC8 DHC8202 2809007NM POWER LEVER OUT OF ADJUST A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09357PH 504 SEA - FLIGHT 2357 AUTOFEATHER SYSTEM FAILS TEST. INSPECTED POWER LEVER SWITCHES 6121-58 AND 6121-59 AND FOUND THAT 6121-58 WAS NOT ADJUSTED QUITE TIGHT ENOUGH. ADJUSTED POWER LEVER SWITCH 6121-58 IAW -8 200, ENGINE RIG MANUAL 1-82ER, PART 7, PARAGRAPH 4-4D. PERFORMED AUTOFEATHER SYSTEM AND POWER UPTRIM TEST. OPERATIONAL CHECK GOOD. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050127001212005012700121NM 2005 1 27 DHL2005782001 120050115A2730680005007 PCU BOEING727 727227 1384078NM ELEVATOR FAILED A DHLAO OTHER KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO01782DH 1741 21998 AFTER GEAR RETRACTION LOST ALL A-SYS HYD FLUID, PERFORMED ABNORMAL CHECKLIST. RIGHT ELEVATOR PCU FAILED. REPLACED PER 27-30-81. TESTS SERV PER 27-30-81. SERV HYD PER M/M 12-12-0. RAN ENG'S PER JRH 5.2 AND PURGED FLT CONTROLS. NO FURTHER DEFECTS NOTED. 2L73 4F A3WE 20050127001222005012700122CE 2005 1 27 200105 120050118A3310 ANNUNCIATOR BEECH 1900 1900D 1154162CE COCKPIT ACTIVATED A NSVAO OTHER J WARNING INDICATION CRCRUISE 1 EA27191CJ UE19 ANNUNCIATOR SERVICE LIGHT ILLUMINATED IN FLIGHT. 2L72 4T RTA24CE 20050127001302005012700130NM 2005 1 27 05FDEA00138 120050121A5754ARC25121 HINGE DOUG DC10 DC10 N/A-SDRNM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25395FE 46629 LEFT WING INBOARD FLAP HINGE INBOARD PIVOT BUSHING GALLED AND PITTED. MEASURED BORE DIAMETER, FOUND TO BE OUT OF LIMITS IAW DAC CMM 57-52-01, ALODINE AND PRIMED BORE IAW DC10-10 SRM 51-21-01 VOL 2, FABRICATED, INSTALLED AND HONED BUSHING TO A FINAL INSIDE DIAMETER OF .9995 - 1.0005 IAW DAC CMM 57-52-01 AND FEDEX EA 8-5750-83956, WINGS, LEFT HAND INBOARD FLAP, OUTBOARD HINGE BRACKET, OVERSIZED PIVOT BORE REPAIR, REFERENCE NON-ROUTINE; N00390. 2L73 4F RTA22WE 20050127001312005012700131WP 2005 1 27 UPS05843735 120050106A53403755854U1 FITTING DOUG DC8 DC873F 302199FWP CARGO PIT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01868UP 45968 INSPECTION TYPE: C3, BANANA FITTING CRACKED AT STA 1200 LONGERON 26L. CUT WEB ABOVE L27L TO FOM FITTING REMOVAL. REMOVED AND REPLACED FITTING REF SRM 51-1-20D, 51-1-8. REPAIRED WEB REF DWG9751879 USING SHT2024-T3 /.020 PER SRM 53-2-0 FIG 1D, 51-1-21, 51-1-20D. 2L74 4F RT4A25 20050127001322005012700132WP 2005 1 27 UPS05843736 120050106A531337585931 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01868UP 45968 INSPECTION TYPE:C3, LONGERON 34R CRACKED STA 1260-1280. REMOVED SPLICE FITTINGS AT STA 270 & 1350. OPENED BELLY SKIN FROM L31 LT TO L31 RT TO FOM FROM STA 1300-1350. CLEANED, TREATED, PRIMED AREA. REMOVED AND REPLACED LONGERON 34R FROM STA 1270-1350. REINSTALLED BELLY SKIN & SPLICE FITTINGS REF SRM 51-1-20D, 51-1-21, 51-1-8. 2L74 4F RT4A25 20050127001332005012700133WP 2005 1 27 UPS05843737 120050105A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01868UP 45968 INSPECTION TYPE:C3 LONGERON 15L CRACKED UNDER SHEAR TIE AT STA 1734. REMOVED SHEAR TIE AT STA 1734. REMOVED LONGERON SECTION FROM STA 1766 - APPROX STA 1725. FAB REPLACEMENT LONGERON SECTION FROM EXTRUSION S1616757, 2 SPLICE STRAPS FROM SHT7075T6-.080, -39 SPLICE FITTING FROM EXTRUSION S2645716 & INSTALLED REPAIR REF SRM 53-2-2 FIG 10, 11 51-1-8, EO DC8-5340-8038, 51-1-20D, RE-INSTALLED SHEAR TIE REF SRM 51-1-20D. 2L74 4F RT4A25 20050127001342005012700134WP 2005 1 27 UPS05843738 120050105A5313 LONGERON DOUG DC8 DC873F 302199FWP MAIN CABIN CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01868UP 45968 INSPECTION TYPE:C3 LONGERON 15L CRACKED AT SHEAR TIE STA 1754. REMOVED END FITTING, CLIP, LONGERON SECTION FROM 1744 - 1766. FAB REPLACEMENT LONGERON SECTION FROM S1616757, 2 STRAPS FROM SHT 7075T6-.080, SPLICE FITTING FROM S2645716. TREATED, PRIMED, INSTALLED ALL REPAIR & REMOVED PARTS REF SRM 51-1-8, 53-2-2 FIG 10 & 11, 51-1-20D. 2L74 4F RT4A25 20050127001352005012700135WP 2005 1 27 UPS05843739 120050113A532037592221 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01868UP 45968 INSPECTION TYPE:C3, LONGERON SPLICE FITTING CORRODED BEYOND LIMITS, STA 1260 - 1280 L34L. REMOVED AND REPLACED SPLICE FITTING REF SRM 51-1-20D, 51-1-8. 2L74 4F RT4A25 20050127001362005012700136WP 2005 1 27 UPS05843740 120050105A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01868UP 45968 INSPECTION TYPE:C3 LONGERON 14L CRACKED UNDER SHEAR TIE AT STA 1756. REMOVED END FITTING, INTERNAL DOUBLER & CLIP. CUT & REMOVED LONGERON SECTION FROM 1747 - 1766. FAB REPLACEMENT LONGERON SECTION FROM S1616757, 2 STRAPS FROM SHT7075T6-.080, SPLICE FITTING FROM S2645716. TREATED, PRIMED & INSTALLED ALL REMOVED AND REPAIR PARTS REF SRM 53-2-2 FIG 10 & 11, 51-1-8, 51-1-20D. 2L74 4F RT4A25 20050127001372005012700137EA 2005 1 27 COMA0560080 120050121A339759465 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT UNRELIABLE A COMAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01446CA 7546 FLIGHT 5290 ROW 10 EMERGENCY LIGHT IS INOP. SECURED LOOSE WIRE CONNECTION AT ROW 10. 2L72 4F RTA21EA 20050127001382005012700138NM 2005 1 27 0500095511 120050120A5414 SKIN BOEING757 757251 1384970NM PYLON CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01511US 23199 DURING L-CHECK, FOUND CRACK IN NR 2 STRUT SKIN. REPAIRED PER EA 55-201934. 2L72 4F RTA2NM 20050127001392005012700139WP 2005 1 27 0500109864 120050121A5330 SKIN DOUG DC9 DC951 3022051WP FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01773NC 47775 DURING H-CHECK FOUND LT ACCESS KIDNEY PANEL BELOW LEADING EDGE WING TO BODY FAIRING HAS CORROSION ON SKIN INNER DOUBLER AT INBOARD CORNER SURFACE. REPAIRED PER EA 98-201833. 2L72 4F RTA6WE 20050127001402005012700140NM 2005 1 27 QXEA200500100 120050116A5230502213 SEAL BOMBDRDHC8 DHC8401 1390041NM CARGO DOOR DAMAGED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09413QX7612 4060 GEG - FLIGHT 2353 - THE FLIGHT RETURNED TO FIELD AFTER THE CREW HEARD A LOUD POP AND THE AIRCRAFT RAPIDLY DEPRESSURIZED. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE AFT CARGO DOOR SEAL. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050127001412005012700141EU 2005 1 27 05FDEA00148 120050124A5313 STRINGER AIRBUS310 A310203 3930313EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25405FE 237 FR54-FR54.1 RT STR 44 CORROSION ON STRINGER (FOUND DURING CLEANUP FOR CPC APPLICATION). CLEANED CORROSION, FOUND TO BE OUT OF LIMITS PER A310-200 SRM 53-10-00. SPLICED IN NEW STRINGER SECTION WITH NEW END FITTING IAW A3010-200 SRM 53-10-14 FIG 201. ALODINED, PRIMED, AND TOP COATED IAW A310-200 SRM 51-23-00. WORK DOCUMENTED ON NRC N00646. 2L72 4F RTA35EU 20050127001422005012700142EU 2005 1 27 05FDEA00149 120050124A5313 STRINGER AIRBUS310 A310203 3930313EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25405FE 237 FR72-FR73 RIGHT STG 55 HAS CORROSION (FOUND DURING CPC APPLICATION). CLEANED CORROSION, FOUND TO BE OUT OF LIMITS IAW A310-200 SRM 53-10-00. CUT OUT DAMAGED SECTION AND SPLICED IN NEW STRINGER SECTION IAW A310-200 SRM 53-10-14 FIG 201. ALODINED, PRIMED AND TOP COATED IAW A310-200 SRM 51-23-00. 2L72 4F RTA35EU 20050127001432005012700143WP 2005 1 27 UPS05843742 120050121A33506012235 BATTERY PACK DOUG DC8 DC871F 302199DWP EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01755UP 46055 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS WILL NOT TEST. REMOVED AND REPLACED EMERGENCY EXIT BATTERY PACK, CHECKS OK MM 33-50-01-2. 2L74 4F RT4A25 20050127001442005012700144NM 2005 1 27 SCNA05002 120050118A2131 CONTROLLER BOEING737 737800* NM CABIN PRESSURE MALFUNCTIONED A SCNAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15PHHZI 28380 CREW REPORTED LOST PRESSURIZATION AT FL 200. DESCENDED TO 10,000 BUT MASKS DROPPED BEFORE LEVEL OFF. RECOVERED PRESSURIZATION WHEN OUTFLOW VALVE MOVED. FROM THEN ON AUTO WORKED. MAINTENANCE PERFORMED DCPC BITE CHECK PER FIM 21-31 TASK 815 & 825, DURING REPACK OF PASSENGER OXYGEN MASKS, 6 MASK TABS WERE BROKEN RESULTING IN 4 OXYGEN GENERATORS NOT FIRING, 1 MASK RUBBER WAS PULLED OFF THE MASK BASE, 1 MASK LANYARD WAS BROKEN AND ONE MASK LANYARD SWEDGE WAS PULLED OUT RESULTING IN THE OXYGEN GENERATOR NOT FIRING, 2 RELEASE CABLES WERE BROKEN RESULTING IN 2 OXYGEN GENERATORS NOT FIRING, 1 SPLIT RING WAS NOT ATTACHED TO THE LANYARD, AND 1 MASK WAS MISSING A LANYARD. 2L72 4F RTA16WE 20050127001452005012700145EA 2005 1 27 COMA0560075 120050121A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA LT FLAPS UNRELIABLE A COMAO OTHER J WARNING INDICATION CRCRUISE 1 SO01966CA1630412 7132 FLIGHT 5008 FLAPS FAILED CAUTION. REPLACED THE LEFT BPSU. 2L72 4F RTA21EA 20050127001462005012700146EA 2005 1 27 QXEA200500114 120050122A2520 PANEL CNDAIRCL600 CL6002C10 1390015EA CABIN LOOSE A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09617QX3043 10130 OKC - FLIGHT 4188 - THE FLIGHT RETURNED TO GATE WHEN AN OVERHEAD PANEL IN THE CABIN FELL DOWN DURING THE TAXI OUT. MAINTENANCE INSPECTED THE OVERHEAD AND THEN RESECURED THE PANEL. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20050127001472005012700147EA 2005 1 27 05020651 120050120A3260 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA MLG ACTIVATED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27651BR 7426 EVENT SUMMARY STATED GEAR DISAGREE. REMOVED AND REPLACED MLG PRIORITY VALVE IN REF TO CRJ MM 32-32-15, NO FIX. FOUND AIR IN NR 3 HYD SYSTEM, DRAINED AIR AND SERVICED HYD SYSTEM IAW CRJ AMM 12-12-29. CREW WROTE THE FOLLOWING, LEFT GEAR UP DISAGREE ON RETRACTION, CLEARED ITSELF IN 1 MINUTE, HYD PUMP 3 WAS 2300 LBS. D/L CODES FROM PSEU AND A HARD FAIL WAS DISCOVERED ON LT MLG CODES WAS LEFT GEAR UPLOCK FAR. DID NOT HAVE A CHANCE TO DO GEAR SWINGS BUT BELIEVED GEAR WAS SLOW TO COME UP. FOUND NR 3 ACCUMULATOR LOW, SERVICED NR 3 ACCUMULATOR IAW CRJ AMM 12-12-29 D/L LOADED CODES FROM PSEU AND RESET PSEU. GEAR SWINGS OP CHECK GOOD. MLG SELECTOR VALVE, NO LEAK NOTED. 2L72 4F RTA21EA 20050127001482005012700148NM 2005 1 27 QXEA200500119 120050119A28202810070101 VALVE DHAV DHC8 DHC8202 2809007NM NR 2 NACELLE LEAKING A QXEAK NONE K FLUID LOSS ININSP/MAINT 1 NM09358PH16080 506 PDX - DURING A MAINTENANCE WALKAROUND FUEL WAS FOUND LEAKING FROM THE SINGLE POINT REFUELING VALVE DRAIN HOLE. THE AREA WAS INSPECTED AND THE REFUEL / DEFUEL ADAPTER WAS REPLACED. OPERATIONAL AND LEAK CHECKS WERE PERFORMED AND ALL WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050127001492005012700149WP 2005 1 27 UPS05843743 120050104A5310577263837 BEAM DOUG DC8 DC873F 302199FWP BULKHEAD CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01868UP 45968 INSPECTION TYPE:C3 AFT PRESSURE BULKHEAD HORIZONTAL -J- BEAM CRACKED, AFT SIDE, NEAR L13R. STOP DRILLED CRACK, VERIFIED REF SPM06-10-01.001. FABRICATED REPAIR PARTS FROM SHT 7075-0-.100. HEAT TREATED TO T6. INSTALLED REPAIR REF EO DC8-5310-6598-C. 2L74 4F RT4A25 20050127001502005012700150WP 2005 1 27 UPS05843744 120050102A5730576954534 DOUBLER DOUG DC8 DC873F 302199FWP RT WING L/E CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01868UP 45968 INSPECTION TYPE:C3 INNER DOUBLER CRACKED AT DRAIN HOLE NEAR XFS 591, RIGHT WING O/B LEADING EDGE. REMOVED OLD REPAIR DOUBLER, STOP DRILLED CRACK, NDT VERIFIED STOP DRILL FAB REPLACEMENT INTERNAL DOUBLER FROM SHT7075T6-.080. REMOVED AND REPLACED INNER DOUBLER AND REINSTALLED REPAIR DOUBLER, REF SRM 57-2-1 FIG 3A, 51-1-21, 51-1-8, 51-1-20D, DWG 5769545, NDT SPM 06-10-01.001. 2L74 4F RT4A25 20050127001512005012700151WP 2005 1 27 UPS05843745 120050125A3350 BATTERY PACK DOUG DC8 DC871F 302199DWP EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01755UP 46055 EMERGENCY EXIT LIGHT INOP. REPLACED EMERG LIGHT BATTERY PACK PER WDM 33-50-01. OPS CK OK. 2L74 4F RT4A25 20050127001562005012700156NM 2005 1 27 QXEA200500099 120050116A33501014011 LIGHT DHAV DHC8 DHC8202 2809007NM ZONE 200 MALFUNCTIONED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - ALL THREE BETA LIGHT ASSEMBLIES ON EMERGENCY EXIT DOOR HANDLES FAILED BRIGHTNESS TEST. MAINTENANCE REMOVED AND REPLACED ALL THREE BETA LIGHT ASSEMBLIES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050127001592005012700159NM 2005 1 27 QXEA200500117 120050121A6120 POTENTIOMETER DHAV DHC8 DHC8202 2809007NM AUTOFEATHER SYS OUT OF ADJUST A QXEAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 NM09351PH 490 SEA - FLIGHT 2203 TAKEOFF ABORTED AT 60 KTS DUE TO FAILURE OF AUTOFEATHER TO ARM. MAINTENANCE ADJUSTED NR 1 AND NR 2 ENGINE POWER LEVER POTENTIOMETERS IAW Q200 MM ER TR ER-10, DATED MAR 25/2004, PART 7, PAGE 32 TO 35, PARAGRAPH 5-1 A, B, C, (1) THRU (38). OPERATIONAL CHECK GOOD. ALL PARAMETERS ARE WITHIN FIGURE 501. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050127001612005012700161WP 2005 1 27 CALA0500016 120050121A5712993758917 RIB DOUG DC9 DC982 3022082WP LT WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2735836 49441 INSPECTION FOUND A .75 INCH CRACK IN RIB AND DOUBLER AT LT WING LEADING EDGE INTERNALLY BETWEEN NR 9 AND NR 10 SLAT TRACK CUTOUTS, STA XRS 324. THE CRACKED RIB AND CLIP ANGLE WERE REMOVED AND A NEW RIB AND CLIP ANGLE WERE INSTALLED IAW SRM 51-10-03, 51-30-02, AND 51-30-05. 2L72 4F A6WE 20050127001632005012700163NM 2005 1 27 0500075523 120050120A5315 FLOORBEAM BOEING757 757251 1384970NM FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01523US 23617 DURING H-CHECK, FOUND CORROSION ON FLOORBEAM AT BS 365 RBL 1 TO RBL 62. REPAIRED PER EA 55-202245. 2L72 4F RTA2NM 20050127001642005012700164NM 2005 1 27 AWXA200500072 120050121A3260S00074 PROXIMITY SWITCH BOEING737 737375 13844BNNM RT MLG FALSE INDICATIONA AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28336AW 23707 ON DEPARTURE FROM LAS EN ROUTE TO DFW AFTER RAISING THE LANDING GEAR AN UNSAFE RT HAND MLG UNSAFE RED LIGHT APPEARED AND REMAINED ILLUMINATED. PILOT CYCLED THE LANDING GEAR ONCE AT DIRECTION OF LAS MX. LIGHT REMAINED ILLUMINATED AND AIRCRAFT DIVERTED TO PHX. MAINTENANCE REMOVED AND REPLACED S00074 PROXIMITY SENSOR IAW MM 32-61-21-4 AND REPLACED CONNECTOR D4536P FOR DISCREPANT LOCKING FUNCTION PER BMM 20-61-11. NUMEROUS GEAR SWINGS PERFORMED WITH OPERATIONAL TESTS FOUND OK. 2L72 4F RTA16WE 20050125000752005012500075NM 2005 1 25 SWAA050164 120050121A3350101114 LAMP BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29748SW 29800 DURING SCHEDULED MV2 CHECK, FOUND FWD RT EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM. 2L72 4F RTA16WE 20050125000762005012500076NM 2005 1 25 SWAA050180 120050123A53106546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29653SW 28398 DURING SCHEDULED 1/4D CHECK, FOUND 2 EACH SHEAR TIES BETWEEN BS 747E AND BS 767, BETWEEN STRINGERS 27R AND 26R, CORRODED. REMOVED AND REPLACED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20050125000782005012500078CE 2005 1 25 DXTA200500552 120050123A3234 HANDLE CESSNA560 560XL 2076702CE MLG STUCK E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07650QS 5605150 COULD NOT RAISE GEAR HANDLE TO RETRACT GEAR AFTER T/O. INSPECTED GEAR HANDLE AND FOUND IT TO BE BINDING. REMOVED GEAR HANDLE WHEEL AND CLEANED SLIDING SAFETY SHAFT INSTALLED GEAR HANDLE WHEEL AND PERFORMED GEAR SWING, OPS CHECK GOOD. WORK DONE IAW 560XL M/M 32-30-00. 2L72 4F RTA22CE 20050125000852005012500085EA 2005 1 25 COMA0560057 120050118A2750 DRIVE SHAFT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS LACK OF LUBE A COMAO OTHER J WARNING INDICATION DEDESCENT 1 SO01976CA 7151 FLIGHT 5905 DURING DESCENT TO YYZ RECEIVED A FLAP FAIL MESSAGE. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE FIRST EVENT, MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3, (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. AIRCRAFT WAS FERRIED TO CVG WHERE THE FLEX DRIVE SHAFTS WERE LUBRICATED. 2L72 4F RTA21EA 20050125000912005012500091SO 2005 1 25 C2XA05CL003 120050117A32608005701 SWITCH EMB 145 EMB145LR 3260212SO MLG DIRTY A C2XAO OTHER J WARNING INDICATION CLCLIMB 1 SW2711548 145565 CLE FLIGHT 2056 THE CREW REPORTED AFTER TAKEOFF THE LEFT GEAR WOULD NOT RETRACT. MAINTENANCE INSPECTED AND CLEANED THE LEFT GEAR PROXIMITY SWITCHES. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20050125000992005012500099EA 2005 1 25 SWIA200514409 120050116A2740 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MOTOR MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07932SW 7714 ON TAXI-OUT STATUS MESSAGE, STAB CH1 INOP. REMOVED AND REPLACED HORIZONTAL STAB TRIM ACTUATOR AND MOTOR CONTROL UNIT IAW CRJ MM 27-40-00, 27-42-01 AND 27-42-05. P/N 8396-3, S/N OFF 969, P/N 7062-3, S/N OFF 1002. 2L72 4F RTA21EA 20050125001182005012500118NM 2005 1 25 CALA0500015 120050121A3350D71702030 CHARGER BOEING737 737824 13844BZNM EMERGENCY LIGHT INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2773270 31632 THE OVERWING DOOR EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE (LEFT OUTSIDE FORWARD AND RIGHT OUTSIDE FORWARD AND AFT). THE BATTERY CHARGER WAS REMOVED AND REPLACED IAW MM 33-51-00. OPERATION CHECKED GOOD ON AFT RIGHT LIGHT. RELAMPED FORWARD LEFT AND FORWARD RIGHT BULBS AND OPERATION CHECKED GOOD. 2L72 4F RTA16WE 20050125001192005012500119SO 2005 1 25 C2XA05TY005 120050113A575114569009408 FITTING EMB 145 EMB145XR 3260214SO RT AILERON DAMAGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2721129 145703 TYS, DURING A SCHEDULED INSPECTION THE RIGHT AILERON TO PCA ATTACH FITTING HOUSING WAS GOUGED AND ELONGATED. MAINTENANCE REMOVED AND REPLACED THE FITTING IAW EMB-145XR-AMM 27-11-00 AND EC5750-01177. 2L72 4F RT 20050125001202005012500120SO 2005 1 25 C2XA05IA012 120050120A3397W763805320 WIRE EMB 145 EMB145 3260210SO EMERGENCY LIGHT LOOSE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716961 145103 EWR - FLIGHT 3450, THE CREW REPORTED THAT THE FORWARD EMERGENCY EXIT LIGHT OVER THE FLIGHT ATTENDANT SEAT WAS INOPERATIVE. MAINTENANCE REPAIRED A LOOSE WIRE, OPERATIONALLY CHECKED GOOD, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050126000062005012600006SO 2005 1 26 CHQA200500011 120050122A3350RPS1B BATTERY PACK EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSDISCHARGED A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11565RP 145679 THE EMERGENCY LIGHTS WERE LEFT IN THE ARMED POSITION BY THE PREVIOUS CREW ON SHUTDOWN. THE BATTERIES ARE NOW DEAD. REMOVED AND REPLACED ALL FOUR EMERGENCY LIGHT BATTERIES IAW EMB 145 AMM 33-50-04. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050126000082005012600008 2005 1 26 CHQA200500012 420050122A31607023460803 DISPLAY EMB ERJ170ERJ170100LR EU COCKPIT UNSERVICEABLE A CHQAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL11638RW260 260 17000053 FLIGHT 7750 - ORD-SYR - WHILE IN LEVEL CRUISE FLIGHT PFD 1 FAILED. ABOUT 1 SECOND LATER, A LARGE FLAME EMANATED FROM BENEATH THE INSTRUMENT PANEL. IT WAS FOLLOWED BY A LARGE SHOWER OF SPARKS AND SMOKE. AN EMERGENCY WAS DECLARED AND THE FLIGHT LANDED IN DTW SINCE IT WAS THE CLOSEST AVAILABLE AIRPORT. THE AIRCRAFT LANDED UNEVENTFULLY. MAINTENANCE INSPECTED THE PFD AND FOUND MOLTEN METAL AT THE RUDDER PEDALS RIGHT BELOW WHERE THE PFD WOULD SIT. THE WIRING BUNDLES BEHIND THE PFD WERE INSPECTED AND ALL LOOKED GOOD. NO OTHER DAMAGE IS NOTED. THE PFD UNIT HAD A DISTINCT SHORT SMELL FROM INSIDE. REMOVED AND REPLACED PFD IAW EMB 170 AMM. OPS CHECK GOOD. 2L74 4F RTA56NM 20050126000112005012600011WP 2005 1 26 MWEA050011 120050118A5330591142268 SKIN DOUG DC9 DC981 3022081WP FUSELAGE DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31805ME 48031 FUSELAGE SKIN HAS SERVERAL DENTS FROM STATION 1279 TO 1283 FROM LONGERON 2 RIGHT TO 6 RIGHT. FABRICATED AND INSTALLED SKIN. 2L72 4F A6WE 20050126000222005012600022NM 2005 1 26 QXEA200500068 120050114A2120 VALVE DHAV DHC8 DHC8202 2809007NM NR 1 & 2 STUCK A QXEAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION APAPPROACH 1 NM09347PH17643 480 RDM - FLIGHT 2162 - THE CREW REPORTS THE LAVATORY SMOKE DETECTOR SOUNDED DURING THE APPROACH FOR LANDING. MAINTENACE INSPECTED THE AIRCRFAFT AND REPLACED THE NR 1 AND NR 2 P2.5/3.0 SWITCHING VALVES. THE ENGINES WERE RUN AND THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050126000252005012600025SO 2005 1 26 RAIA00501016 120050109A3240 CONTROL UNIT EMB 145 EMB145LR 3260212SO BRAKE ASSY MALFUNCTIONED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03842HK 14500830 8080- IAD- BRAKES LACK EFFECTIVENESS AT FIRST, THEN SUDDENLY LOCKED UP, CAPT AND F/O LEFT AND RIGHT BRAKE PEDALS. MAINTENANCE, BRAKE CONTROL UNIT MESS ON CMC, NO EICAS MESSAGES. CLEARED CMC MESSAGE AND OPS CHECKED BRAKES. 2L72 4T RTT00011AT 20050126000262005012600026SO 2005 1 26 RAIA00501020 120050105A5610163500111 WINDSHIELD EMB 145 EMB145LR 3260212SO COCKPIT CRACKED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03849HK3132 145002 8053- EWR- CPT WINDSHIELD CRACKED. REMOVED AND REPLACED CPT WINDSHIELD. 2L72 4T RTT00011AT 20050126000312005012600031EU 2005 1 26 RAIA00501014 120050106A24001PF2 RELAY JETAIRJETSTMJETSTM4101 1500501EU MASTER SWITCH FAILED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03567HK 41085 5543- STL- AVIONICS BUSS, NO CONTROL WITH MASTER SWITCH. REMOVED AND REPLACED 1PF2 RELAY FOR LEFT AVIONICS MASTER SWITCH. 2L72 4T RTA41NM 20050126000552005012600055SO 2005 1 26 MASA200500028 120050111A335078241 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT FAILED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07836MJ 145359 ASH 2861 CLT TO GSP, EMERGENCY ESCAPE PATH LIGHTING WOULD NOT ILLUMINATE. MAINTENANCE REPLACED EMERGENCY LIGHTING INVERTER AND BATTERY PACK. NO FURTHER DEFECTS NOTED. BATTERY PACK P/N 2013-1A. 2L72 4T RTT00011AT 20050126000852005012600085NM 2005 1 26 QXEA200500051 120050107A3060 SEAL BOMBDRDHC8 DHC8401 1390041NM LEFT PROP LOOSE A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09411QX 4055 PDX FLIGHT NR 2353 PROP DE-ICE MASTER CAUTION LIGHT ILLUMINATED ENROUTE FROM GEG. EMERGENCY CHECKLIST ACCOMPLISHED. ATTEMPTED ONE RESET AS PER CHECKLIST. PROP DE-ICE LIGHT REMAINTED ILLUMINATED. MAINTENANCE REMOVED NR 2 SPINNER, INSPECTED PROP LEADS. ALL LEADS SECURE ON BLADES AND SPINNER BULKHEAD. FOUND RUBBER SEAL LOOSE. NO PARTS REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050126001102005012600110EU 2005 1 26 MALA050118 120050108A5320 STRUCTURE SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15425XJ 340B425 DURING 4Y/2Y CHECK IN BNA, LT WRAP AROUND PN 7253710-243 IS CORRODED OUT OF LIMITS AND HAS BEEN REPLACED IAW SRM 51-40-21 REFER EAMS WO NR 211363, TASK 1534 FOR ADDITIONAL INFORMATION. AIRCRAFT WAS RELEASED 1/11/05. 2L72 4T RTA52EU 20050126001202005012600120NM 2005 1 26 MWEA050008 120050110A521059100817 SKIN BOEING717 717200 1383700NM PAX DOOR BENT A MWEAK NONE O OTHER ININSP/MAINT 1 GL31913ME 55176 PASSENGER DOOR LOWER SKIN IS BENT AT FORWARD AND AFT CORNERS. INSTALLED DOUBLER ON LOWER DOOR SKIN. 2L72 4F TRA6WE 20050126001242005012600124GL 2005 1 26 CHQA200500008 220050114A7200AE3007A13 ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 1 LEAKING A CHQAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL11578RP663 663 14500865 FLIGHT 6374 CHM-LGA - ON INITIAL CLIMB-OUT OF CMH AT 1000 FEET, LAV SMOKE MESSAGE APPEARED ON EICAS WITH THE ASSOCIATED TRIPLE CHIME. THE FLIGHT ATTENDANT CALLED WITH THE CABIN EMERGENCY ADDRESS BUTTON AND STATED THE CABIN WAS FULL OF SMOKE. AN EMERGENCY WAS DECLARED AND ALL CHECKLIST WERE COMPLETED. THE EICAS MESSAGE EXTINGUISHED AND THE SMOKE DISSIPATED. THE FLIGHT LANDED SAFELY BACK IN CMH. MAINTENANCE FOUND SIGNS OF AN OIL LEAK IN THE NR 1 ENGINE. REMOVED AND REPLACED NR 1 ENGINE IAW EMB J/C CE720001. OPS CHECK GOOD WITH NO SMOKE NOTED. 2L72 4T4 FRTT00011ATTE6CH 20050126001302005012600130EU 2005 1 26 MALA050103 120050102A2460A2043C PDU SAAB SF340 SF340A 7850100EU AUTOCOARSEN SYS MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL1599XJ 340A099 AFTER DEPARTING SCE, RT ESS BUSS FAIL. COMPLETED QRH, TALKED TO MAINTENANCE, RETURNED TO SCE ON FINAL AUTOCOARSEN DIDN'T ARM. MAINTENANCE REPLACED RT PDU W/ SERVICABLE UNIT PN OFF/ON A2043C SN OFF/CG-81563, SN ON/CL-73104 REF SF340 MM CHAPTER 24. OPS TEST GOOD RAN AIRCRAFT PERFORMED AUTOCOARSEN SYSTEM TEST REF SF340 MM 71-00-00, ALL CHECKS GOOD AT THIS TIME. 2L72 4T RTA52EU 20050126001352005012600135NM 2005 1 26 DHL2005742001 120050104A3260656021132 ACCESSORY UNIT BOEING727 727225 1384077NM MLG MALFUNCTIONED A DHLAO OTHER N FALSE WARNING CRCRUISE 1 SO01742DH 21290 RIGHT RED GEAR LIGHT ILLUMINATES INTERMITTANTLY. REMOVED AND REPLACED LANDING GEAR ACC BOX AND OPS CHECKED SYSTEM IAW B-M/M 32-62-00, NO DEFECTS NOTED. 2L73 4F A3WE 20050126001532005012600153EU 2005 1 26 MALA050121 120050108A53477253721459 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15425XJ 340B425 DURING 4Y/2Y CHECK IN BNA, GALLEY SEAT TRACK IS CORRODED OUT OF LIMITS AND HAS BEEN REPLACED PN 7253721-459 IAW SRM 51-40-27. REFER EAMS WO NR 211363, TASK 1503 FOR ADDITIONAL INFORMATION. AIRCRAFT WAS RELEASED 1/11/05. 2L72 4T RTA52EU 20050126001542005012600154SO 2005 1 26 CHQA200500009 120050116A3350RPS1B BATTERY PACK EMB 145 EMB145EP 3260221SO EMERGENCY LIGHT UNSERVICEABLE A CHQAK NONE O OTHER ININSP/MAINT 1 GL11978RP 145169 FLIGHT 9395 BUF - UPON ARRIVAL AT THE AIRCRAFT IN THE MORNING, THE EMERGENCY LIGHTS WERE FOUND TO BE LEFT ON IN THE ARMED POSITION OVERNIGHT. THE EMERGENCY LIGHTS WOULD COME ON FOR 1-3 SECONDS THEN EXTINGUISH. INSPECTED AIRCRAFT AND FOUND IT TO BE SAFE FOR A MAINTENANCE FERRY FLIGHT FROM BUF TO IND. UPON ARRIVAL IN IND, MAINTENANCE REMOVED AND REPLACED ALL FOUR EMERGENCY LIGHT BATTERIES IAW CHQ J/C E33-50-04-720-001. OPS CHECK GOOD IAW CHQ J/C E3350-00-710-001. 2L72 4F RTT00011AT 20050126001572005012600157WP 2005 1 26 AALA20050027 120050114A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21941AS 49925 DFW - EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED EXTERIOR EMERGENCY LIGHT BATTERY PACK AND CHARGER ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050126001592005012600159NM 2005 1 26 AWXA200500038 120050115A3350964411 LIGHT BOEING737 7373G7 1384595NM SEAT ROW 4 LT INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28303AW 24010 LAS - EEL - DURING 8-DAY CHECK FUNCTIONAL TEST OF EMERGENCY LIGHTING SYSTEM THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 4 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 4 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050126001622005012600162NM 2005 1 26 2005UALA00068 120050117A2120 ODOR AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE COCKPIT DETECTED A UALAA UNSCHED LANDING O OTHER CLCLIMB 1 WP29828UA 1031 ELECTRICAL SMELL OBSERVED IN THE FLIGHT DECK. NSPECTED GALLEY AREAS AS WELL AS AVIONICS COOLING FANS. FLIGHT CREW HAD NO OTHER ABNORMAL INDICATIONS OR SYSTEM MALFUNCTIONS. ACCOMPLISHED POWER RUNS AND REPLACED AEVC FILTER CARTRIDGE AS PRECAUTINARY MEASURES. NO TRIPPED BREAKERS FOUND. CAUSE UNDETERMINED. 2L72 4F4 FRTA28NM E40NE 20050126001632005012600163 2005 1 26 2005UALA00084 420050120A3414 INDICATOR BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE AIRSPEED MALFUNCTIONED A UALAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 WP29372UA 24637 ABORTED TAKEOFF DUE TO F/O AIR SPEED INDICATOR. REPLACED FIRST OFFICERS AIR SPEED INDICATOR. 2L72 4F4 FRTA16WE E2GL 20050126002092005012600209EU 2005 1 26 RAIA00501002 120050102A2430A2105F PDU JETAIRJETSTMJETSTM4101 1500501EU RT BUSS FAILED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03556HK5809 41073 5516 - SPI - RIGHT ESSENTIAL BUSS FAILED. MAINTENANCE REMOVED AND REPLACED RIGHT POWER DISTRIBUTION UNIT. 2L72 4T RTA41NM 20050126002102005012600210NM 2005 1 26 P5CA0501298 120050103A2150 A/C PACK BOEING747 747341 13848AMNM NR 2 ODOR A P5CAB EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 EA15355MC 23395 NR 2 A/C PACK HAS LOUD NOISE AND STRONG SMELL DURING OPERATION (ELECTRICAL). DEACTIVATED NR 2 A/C PACK PER MEL NR 21-1-2C. ITEM TRANSFERRED TO DMI CONTROL NR 33592. 2L74 4F RTA20WE 20050127000112005012700011EU 2005 1 27 YENA200507 120050112A3240C20225410 BRAKE ASSY AIRBUS320 A320232 3930326EU NR 4 FAILED A YENAK NONE O OTHER ININSP/MAINT 1 EA15507JB103442120 1240 NR 4 BRAKE WORN TO LIMITS. NR 4 MAIN WHEEL ASSY HEAT SHIELD DAMAGED. REMOVED AND REPLACED NR 4 BRAKE ASSY IAW 32-42-27. REMOVED AND REPLACED NR 4 MAIN WHEEL ASSY IAW 32-41-11 (NOTE: NR 4 BRAKE HAD INTERNAL STRUCTURAL FAILURE CAUSING DAMAGE TO NR 4 MAIN WHEEL ASSEMBLY HEAT SHIELD. DAMAGE DISCOVERED DURING BRAKE CHANGE). 2L72 4F RTA28NM 20050127000162005012700016NM 2005 1 27 UPS05243701 120050111A5753 SUPPORT ANGLE BOEING727 727185C 138406NNM NR 4 FLAP TRACK CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 INSPECTION TYPE: C, NR 4 FLAP TRACK FAIRING SUPPORT ANGLE CRACKED AT O/B SIDE AT MLG BEAM. FAIRING SUPPORT ANGLE REPAIRED IAW SRM 51-20-1. 2L73 4F A3WE 20050127000172005012700017 2005 1 27 YENA200510 420050116A2565 GIRT BAR AIRBUS320 A320232 3930326EU ESCAPE SLIDE MISINSTALLED A YENAK NONE O OTHER ININSP/MAINT 1 EA15528JB 1591 L2 DOOR SLIDE WILL NOT ARM. EVALUATION REVEALED SLIDE BAR WAS INSTALLED INCORRECTLY. INSTALLED BAR CORRECTLY IAW 52-10-00, NO ADJUSTMENT NECESSARY OR RIGGING REQUIRED, OPS CHECK GOOD. SLIDE ARMED INDICATION. 2L72 4F RTA28NM 20050127000212005012700021NM 2005 1 27 UPS05443691 120050107A5310 SHEAR TIE BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE: C, FWD CARGO COMPT SUPPORT FRAME SHEAR TIE FOUND CRACKED AT STA 780 STR 33 TO STR 34. SHEAR TIE REPAIRED PER SRM 53-10-04 FIG 4. 2L74 4F A20WE 20050127000242005012700024NM 2005 1 27 UPS05443694 120050105A5313 STRINGER BOEING747 747123F NM FUSLEAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C - BS 1540 LT, 11L STRINGER FOUND CRACKED. M/D BS 1540 CTR 11L STRINGER REPAIR CARRIED OUT IAW SRM 53-10-03 FIG 4. 2L74 4F A20WE 20050127000272005012700027EU 2005 1 27 YENA200506 120050112A3350825UN01A4AD0A SWITCH AIRBUS320 A320232 3930326EU EMEGENCY LIGHT FAILED A YENAK NONE L NO TEST ININSP/MAINT 1 EA15580JB4940 2136 EMERGENCY EXIT LIGHTS REMAIN ON. REMOVED AND REPLACED EMERGENCY LIGHT SWITCH (4WL) AS PER AMM 20-00-00. OPS TEST CKS OK AS PER AMM 33-51-00. 2L72 4F RTA28NM 20050127000402005012700040 2005 1 27 RAIA00501008 420050105A3425HG20104C02 COMPUTER EMB 145 EMB145LR 3260212SO AHRS FAILED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03813HK3658 2229 145044 ATT/HDG FAILED RIGHT SIDE. MAINTENANCE REMOVED AND REPLACED THE FO'S AHRS. 2L72 4T RTT00011AT 20050127000412005012700041NM 2005 1 27 ASMF200501003 120050105A2131 CONTROLLER BOEING737 737 UTILSYSNM NR 2 MALFUNCTIONED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23997AM 30283 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF "AUTO FAIL" LIGHT TURNED ON. BITE IN PRESSURIZATION CONTROLLER NR 2 WAS PERFORMED AND FAIL CONTINUE. DURING MAINTENANCE REVISION, CIRCUIT BREAKER P6-4 F3 WAS DETECTED ACTIVATED, CIRCUIT BREAKER WAS RESEATED AND LIGHT TURNED OFF, SYSTEM WAS TESTED IAW MM 21-31-00, ALL CORRECT. 2L72 4F RTA16WE 20050127001232005012700123EA 2005 1 27 05014655 120050114A3620 DUCT CNDAIRCL600 CL6002B19 1900309EA ANTI ICE SYSTEM FAILED A VTZAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 EA27655BR 7457 EVENT SUMMARY STATED THAT HIGH SPEED ABORT DUE TO MX. REMOVED AND REPLACED BLEED AIR CONTROL UNIT PER OPS CHECK OF ANTI ICE SYSTEM WITH NO DEFECTS NOTED. 2L72 4F RTA21EA 20050127001522005012700152WP 2005 1 27 UPS05843746 120050111A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01868UP 45968 INSPECTION TYPE:C3 FUSELAGE SKIN CRACKED AT STA 1350 L35R. CUT OUT DAMAGED SKIN, NDT VERIFIED, ALL DAMAGE REMOVED. FAB FILLER FROM SHT2024T3-.071 & DOUBLER FROM SHT2024T3-.080 REF SRM 51-9-0, 53-2-1 FIG 8, 53-4-0 FIG 21A, 53-4-1 FIG 16. INSTALLED REPAIR PER SRM 51-1-21, 51-1-20D, 51-1-8, 53-2-1 FIG 8. 2L74 4F RT4A25 20050127001542005012700154NM 2005 1 27 373PA0052 120050122A3350 CHARGER BOEING737 7373Y0 1384671NM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05373PA 23749 LEFT AFT EMERGENCY EXIT LIGHT BATTERY CHARGER INOP, STA 968. REPLACED BATTERY CHARGER PER MM 33-51-51. 2L72 4F RTA16WE 20050127001582005012700158WP 2005 1 27 UPS05843748 120050104A5340577267895 CLIP DOUG DC8 DC873F 302199FWP MAIN CABIN CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01868UP 45968 INSPECTION TYPE:C3, FOUND CRACKED CLIP IN MAIN CABIN, LONGERON 3L. FABRICATED REPLACEMENT CLIP FROM SHT2024T3-.040 REF DWG 5772678. REMOVED & REPLACED CLIP REF SRM 51-1-8, 51-1-20D. 2L74 4F RT4A25 20050127001652005012700165 2005 1 27 234TR0027 420050124A22104038891916 COMPUTER BOEING737 737228 13844AGNM NR 2 ADI MALFUNCTIONED A PIDAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO05234TR 23004 NUMBER 2 ADI HAS FLIGHT DIRECTOR FLAG. REPLACED NR 2 FLIGHT CONTROL COMPUTER. OPS CHECKS GOOD PER MM 22-11-01. 2L72 4F RTA16WE 20050127001672005012700167NM 2005 1 27 DHL2005746002 120050120A3350MISC062 BATTERY BOEING727 727224 1384076NM EMERGENCY LIGHT INOPERATIVE A DHLAK NONE O OTHER ININSP/MAINT 1 SO01746DH 22252 EMERGENCY EXIT LIGHTED SIGN OVER ENTRY DOOR IS INOP. REMOVED & REPLACED ENTRYWAY EMERGENCY EXIT LIGHTED SIGN BATTERIES P/N MISC062 IAW MM 33-50-71. 2L73 4F A3WE 20050127001682005012700168NE 2005 1 27 05024804 220050124A7530 RING ASSEMBLY AIRBUSA319 A319132 3930340NM IAE V2524 V2524A5 NE VARI GUIDE VANE LACK OF LUBE A VTZAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA27804BR 2296 V11736 ENGINE 1 COMPRESSOR VANE ECAM MESSAGE ON TAKEOFF. ABORTED TAKEOFF. MX RESECURED AND RESAFTIED LOOSE LINE ON VGV ACT. LUBRICATED VGV RING ARMS AND PERFORMED GND ENG RUNS WITH NO FURTHER DEFECTS NOTED AT THIS TIME IAW TSM CH 75-30-00. 2L72 4F4 FRTA28NM E40NE 20050127001692005012700169EA 2005 1 27 05025628 120050125A7712 ENGINE CNDAIRCL600 CL6002B19 1900309EA NR 1 SPLIT A VTZAO OTHER F FLT CONT AFFECTED CLCLIMB 1 EA27628BR 7240 EVENT SUMMARY STATED THAT 1 N2 SPLIT AFTER TAKEOFF, READ AS HIGH AS 2.2. ALL OTHER PARAMETERS MATCHED. REMOVED AND REPLACED ENG SPEED CONTROL PANEL IAW AMM 73-21-00. OPS CHECK GOOD. 2L72 4F RTA21EA 20050127001712005012700171NM 2005 1 27 AT0500003 120050112A49504502423A APU BOEING717 717200 1383700NM APU BAY ODOR A ZZDAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO15978AT 55037 AFTER APU START, INTRODUCED APU AIR, SMELLED ACRID PLACTIC SMELL AND CABIN STARTED FILLING WITH SMOKE. RAMP CREW REPORTED SEEING SMOKE AROUND TAIL AND HEARD A LOUD POP. REMOVED AND REPLACED APU. 2L72 4F TRA6WE 20050127001722005012700172 2005 1 27 IXXA0500001O 420050113A3441 TRANSCEIVER DOUG DC8 DC871 302199AWP WX RADAR SYS INOPERATIVE A IXXAA UNSCHED LANDING O OTHER CLCLIMB 1 SW11829BX887331098 45994 DURING CLIMBOUT FROM KIAH THE WEATHER RADAR WOULD NOT COME OUT OF TEST PATTERN WITH FAIL LIGHT ON. CREW RETURNED TO KIAH AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED, INSPECTED AND REINSTALLED THE RADAR RT. THE OPERATIONAL CHECK WAS GOOD PER ALL APPLICABLE MANUALS AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F 4A25 20050127001732005012700173WP 2005 1 27 IXXA0500002O 120050113A2612878464 SENSING ELEMENT DOUG DC8 DC873F 302199FWP NR 4 ENGINE INTERMITTENT A IXXAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW11602AL9434432 45991 DURING CRUISE FROM KTOL THE FIRE WARNING LIGHT AND BELL CAME ON FOR THE NR 4 ENGINE. NO OTHER INDICATIONS WERE NOTED. CREW RETURNED AIRCRAFT TO KTOL AND LANDED WITHOUT INCIDENT. AN INSPECTION IS ON GOING. AS SOON AS THE INFORMATION IS AVAILABLE IT WILL BE PROVIDED. MAINTENANCE OHM CHECKED FIRE WARNING SYSTEM, FINDING INTERMITTENT PROBLEM. REMOVED AND REPLACED 5 FIRE SENSING ELEMENTS, CHECKED BLEED LINES FOR LEAKS WITH NONE NOTED. RAN AIRCRAFT TO POWER AND FIRE WARNING CHECKED GOOD PER ALL APPLICABLE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20050127001742005012700174WP 2005 1 27 IXXA0500003O 120050106A2612 INSULATOR DOUG DC8 DC873F 302199FWP FIRE LOOP BROKEN A IXXAE ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 SW11606AL91796549 46044 DURING CRUISE FROM FJDG TO RJTY NR 2 ENGINE SHORT CIRCUIT LIGHT ILLUMINATED, NO ASSOCIATED FIRE WARNING OR BELL. FIRE WARNING WOULD NOT TEST. CREW PERFORMED A PRECAUTIONARY SHUTDOWN OF NR 2 ENGINE. SHORT CIRCUIT LIGHT EXTINGUISHED WITH ENGINE SHUTDOWN. CREW LANDED AIRCRAFT IN RJTY WITHOUT INCIDENT. MAINTENANCE CLEANED DIRT AND CORROSION FROM BOTH ENDS OF FIRE DETECTOR LOOPS. REVERSED BOTH CONNECTORS. ALSO FOUND BROKEN CLIP INSULATOR. REPLACED INSULATOR SYSTEM AND THE OPERATIONAL CHECK WAS GOOD PER ALL APPLICABLE MANUALS, AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20050127001762005012700176NM 2005 1 27 DHL2005784003 120050126A2612 WARNING LIGHT BOEING727 727227 1384078NM NR 3 FIRE DETECTFALSE INDICATIONA DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01784DH 22001 FIRE PROTECTION SYSTEM ENG NR 3 DETECTION CIRCUIT LIGHT ILLUMINATED. COULD NOT DUPLICATE. PERFORMED VISUAL INSPECTION NO DEFECTS NOTED. OPS NORMAL IAW 26-11-0. 2L73 4F A3WE 20050127001772005012700177WP 2005 1 27 DHL2005804002 120050115A5297 WIRE DOUG DC8 DC873F 302199FWP CARGO DOOR LOOSE A DHLAO OTHER N FALSE WARNING DEDESCENT 1 SO01804DH 46124 AFTER PUSHBACK MAIN CARGO DOOR SYS-B WOULD NOT TEST DURING DESCENT FORWARD CARGO DOOR PROXIMTY C/B POPPED. TRANSFERRED TO DMI 19261 PER MEL 52-2-1 CAT-C FOUND BROKE WIRE IN MCD HARNESS SHORTING OUT (B-SYS) WARNING. SECURED WIRE TO PREVENT SHORTING AND ITEM IS UNDER DMI ENTERED IN ITEM 1P SAM. REF DMI 19261: AFTER PUSHBACK MN CARGO DOOR SYS-B WOULD NOT TEST. REPLACED MN CARGO DOOR ELECTRICAL JUMPER. OPS NORMAL PER MM 52-70-0. THIS CLEARS DMI 19261. 2L74 4F RT4A25 20050127001812005012700181WP 2005 1 27 UPS05843752 120050104A534037552461 FITTING DOUG DC8 DC873F 302199FWP CARGO BAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01868UP 45968 INSPECTION TYPE:C3, SPLICE FITTING CRACKED ON LONGERON 34R AT STA 600 - 620. REMOVED AND REPLACED FITTING PER SRM 51-1-20D, 51-1-8. 2L74 4F RT4A25 20050127001822005012700182WP 2005 1 27 UPS05843753 120050105A571297532973 RIB DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01868UP 45968 INSPECTION TYPE:C3, LT WING ATTACHMENT RIB CRACKED AT XW454. CUT OUT DAMAGE, VERIFIED PER NDT SPM06-10-01.001. FABRICATED REPAIR DOUBLER FROM SHT7075-0-.100 & FILLER FROM SHT7075T6-.090 REF DWG 9753297. HEAT TREAT TO T6 PER DPS7.00-1. INSTALLED REPAIR PER SRM 57-2-0 FIG 2 & 2A, 51-1-8, 51-1-21, 51-1-20D. 2L74 4F RT4A25 20050127001832005012700183WP 2005 1 27 UPS05843754 120050104A57305769891 DOUBLER DOUG DC8 DC873F 302199FWP LT WING CTR L/E CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01868UP 45968 INSPECTION TYPE:C3, LEFT WING CENTER L/E INTERNAL DOUBLER CRACKED BETWEEN XFS 422.75 & XOLDI 6.225. FABRICATED REPLACEMENT DOUBLER FROM SHT7075T6-.080 PER DWG 5769891. REMOVED & REPLACED DOUBLER PER SRM 51-1-8, 51-1-20D, 51-1-21, 51-1-15. 2L74 4F RT4A25 20050128000022005012800002NM 2005 1 28 05FDEA00179 120050126A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 CABIN SEAT TRACK DAMAGED AT STA Y = 1059, X = 48. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE 1, VOLUME I. 2L73 4F RTA22WE 20050128000052005012800005NM 2005 1 28 05FDEA00137 120050121A5751 BALANCE WEIGHT DOUG DC10 DC10 N/A-SDRNM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25395FE 46629 RIGHT WING OUTBOARD AILERON 1 EACH BALANCE WEIGHT HAS CORROSION OUTBOARD SIDE OF ACTUATOR. REMOVED AND REPLACED RIGHT WING OUTBOARD AILERON BALANCE WEIGHT, BALANCE WITHIN LIMITS IAW FEDEX EA 8-5751-83957, WINGS REPLACEMENT OF CORRODED RIGHT HAND OUTBOARD AILERON BALANCE WEIGHT. 2L73 4F RTA22WE 20050128000072005012800007EU 2005 1 28 AWXA200500064 120050108A5321D5367200300000 FLOOR PANEL AIRBUS320 A320231 3930325EU CARGO BAY DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28621AW 053 SAL - MAJOR REPAIR - DURING C-04 CHECK FORWARD CARGO COMPARTMENT FLOOR PANEL 131AF WAS FOUND DELAMINATED. MAINTENANCE REMOVED DELAMINATED FLOOR PANEL 131AF FROM FR 24 TO FR 34; FABRICATED A NEW REPLACEMENT FLOOR PANEL AND DOUBLER; INSTALLED REPLACEMENT PARTS IAW EO 5326-01007. 2L72 4F RTA28NM 20050128000082005012800008NM 2005 1 28 DHL2005760002 120050122A3350 COVER BOEING727 7272B7 138407LNM EMERGENCY LIGHT DISLODGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01760AT 21954 EMERGENCY EXIT LIGHT COVER FELL OFF OVERTOP COCKPIT DOOR. RE-SECURED LIGHT COVER PER 25-00-0 AND STANDARD PRACTICES. 2L73 4F A3WE 20050128000132005012800013EA 2005 1 28 05014665 120050114A2750 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A VTZAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA27665BR 7534 CREW REPORT STATED ON TAXI OUT, THE F/O SELECTED FLAPS TO 8 DEGREES AND A FLAP FAIL CAUTION APPEARED ON ED1. COMPLIED WITH THE QRH AND CYCLED THE APPLICABLE CIRCUIT BREAKERS. THE FLAP FAIL INDICATION REAPPEARED. AFTER TALKING TO MX RTG. RECONNECT LT, RT PDU FOR AFTER TROUBLESHOOTING. CLOSE ACCESS PANELS AT OUTBOARD FLAP STATIONS. RIGGED RT FLAP CONTROL SYSTEM. REMOVED AND REPLACED FECU. 2L72 4F RTA21EA 20050128000142005012800014WP 2005 1 28 IXXA0500013O 120050118A2130 REGULATOR DOUG DC8 DC862F 3021972WP NR 2 ENGINE FAILED A IXXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW1171CX 657822075 45961 DURING CRUISE FROM PKWA, TAKEOFF PLUS 45 MINS TURNED ON RECIR FAN AND HEARD LOUD BANG FROM AREA UNDER CAPTAIN SEAT, COULD NOT STOP CABIN FROM CLIMBING. GOT CONTROL OF CABIN AT ABOUT 15,000, ACFT ALTITUDE CABIN WAS AT 10,2000. TURNED BLEED OFF ON LEFT SIDE, PRESSURE WOULD NOT GO DOWN. MANIFOLD PRESS AND TEMP STAYED AT 35 PSI AND 200C. MAINTENANCE TROUBLESHOT AND FOUND A LEAKING BLEED HEAT EXCHANGER ON NR 1 ENGINE PYLON. ALSO FOUND BAD PRESS REGULATOR ON NR 2 ENGINE. MAINTENANCE DEFERRED BOTH PER ALL APPLICABLE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F 4A25 20050128000152005012800015NM 2005 1 28 SCNA05001 120050102A3350 LIGHT BOEING737 737800* NM CABIN LOOSE A SCNAO OTHER O OTHER NRNOT REPORTED 1 GL15PHHZX 28248 FLIGHT CREW REPORTED EMERGENCY FLOOR LIGHTING STRIP LOOSE. MAINTENANCE RESECURED FLOOR TRACK LIGHTING. 2L72 4F RTA16WE 20050128000162005012800016NM 2005 1 28 QXEA200500139 120050126A5210 CAM BOMBDRDHC8 DHC8401 1390041NM AFT PAX DOOR STICKING A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09415QX2956 4081 THE FLIGHT ATTENDANT REPORTED THE REAR PASSENGER EXIT WAS BINDING ON THE RIGHT SIDE AND DIFFICULT TO OPEN. MAINTENANCE INSPECTED THE DOOR AND FOUND THE UPPER AND LOWER CAMS STICKING. THE CAMS WERE CLEANED AND LUBED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050128000172005012800017NM 2005 1 28 05FDEA00164 120050125A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 CABIN SEAT TRACK DAMAGED AT STA Y = 1421, X = -8. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE 1, VOLUME I. 2L73 4F RTA22WE 20050128000212005012800021NM 2005 1 28 05FDEA00168 120050125A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 CABIN SEAT TRACK DAMAGED AT STA Y = 1126, X = -48. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE 1, VOLUME I. 2L73 4F RTA22WE 20050128000222005012800022NM 2005 1 28 05FDEA00173 120050126A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25235FE 21329 BS 720A, LBL 34, WL 167 DENT ON FRAME. REPAIRED FRAME BS 702A, LBL 36 PER SRM 53-10-1. 2L73 4F RTA3WE 20050128000242005012800024NM 2005 1 28 05FDEA00141 120050121A5330ADA3139501 SKIN DOUG DC10 DC10 N/A-SDRNM ZONE 100 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25395FE 46629 FIRST OFFICERS PRIMARY STATIC PORT HAS EXTERNAL DOUBLER REPAIR WITHIN REDUCED VERTICAL SEPARATIONS. MINIMUN CONTROLLED AREA AT THE 9 TO 10 O'CLOCK POSITION PREVENTING REDUCED VERTICAL SEPARATION OPERATION UNDER FEDEX DC10-10 SRM 53-00-00. REPAIR WAS ACCOMPLISHED PER FEDEX EA 8-5330-83961. 2L73 4F RTA22WE 20050128000252005012800025NM 2005 1 28 UPS05443733 120050107A534065B38600153 STRINGER CLIP BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C M/D - BS 1040 S9R STRINGER TIE CLIP FOUND CRACKED. STRINGER CLIP REPLACED PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050128000272005012800027EA 2005 1 28 SWIA200514429 120050117A2750865D1007 PDU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 NM07939SW 7742 AFTER EXTENDING FLAPS TO 20 DEGREES IN-FLIGHT, RECEIVED A FLAPS HALFSPEED STATUS MESSAGE. REMOVED AND REPLACED FLAP POWER DRIVE UNIT (MOTOR). OPERATIONAL CHECK GOOD IAW MM 27-52-01. 2L72 4F RTA21EA 20050128000282005012800028NE 2005 1 28 DHL2005784002 220050121A7261 OIL CAP BOEING727 727227 1384078NM PWA JT8 JT8D17 52049NE ENGINE LOOSE A DHLAO OTHER J WARNING INDICATION CRCRUISE 1 SO01784DH 22001 OIL QUANTITY ENGINE 32 4.25 DECREASED TO 1.25 INFLIGHT PERFORMED ABNORMAL PROC. INSPECTED 32 ENG OIL QTY FOUND OIL CAP LOOSE RESECURED. SERVICED 32 ENG TO FULL. RESECURED OIL CAP REF M/M 12-15-1. 2L73 4F4 F A3WE E2EA 20050128000292005012800029NM 2005 1 28 05FDEA00143 120050121A5347ACA74141 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 MAIN DECK CARGO, SEAT TRACK BETWEEN STA Y= 879 TO Y= 929, X= -47.50 FOUND WORN. MAIN DECK CARGO, SEAT TRACK BETWEEN STA Y= 879 TO Y= 929, X= -47.50 CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I. 2L73 4F RTA22WE 20050128000312005012800031NM 2005 1 28 05FDEA00064 120050111A5320 STIFFENER DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 MAIN DECK, CENTER TANK, REAR SPAR UPPER CHORD ATTACHED STIFFENER FOUND CORRODED AT STA Y= 1371, X= 117 FORWARD OF SLANT PANEL. MAIN DECK, CENTER TANK, CORROSION ON REAR SPAR UPPER CHORD AT STA Y= 1371, X= 117. REMOVED AND REPROTECTED PER SRM 51-21-01 VOLUME II. ORIGINAL THICKNESS= 0.180 INCH, MATERIAL REMOVED= 0.031 INCH, REMAINING THICKNESS= 0.149, WITHIN LIMITS PER SRM 57-00-01 VOLUME 1. 2L73 4F RTA22WE 20050128000322005012800032NM 2005 1 28 05FDEA00145 120050122A5720 BRACKET BOEING727 727200 138407ENM LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25480FE 21462 LEFT WING L/E, LOWER SURFACE SUPPORT BRACKET IS CRACKED AT WS 165 (INBOARD OF NR 3 K-FLAP ACTUATOR). REMOVED BRACKET IAW SRM 51-30-2. FABRICATED NEW BRACKET FROM 2024-T3 .050 BATCH 0000837762 IAW SRM 51-10-1. INSTALLED NEW BRACKET IAW SRM 51-30-2. 2L73 4F RTA3WE 20050128000352005012800035NE 2005 1 28 P5CA0501305 220050120A7261 LINE BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE NR 3 ENG OIL CHAFED A P5CAE ENGINE SHUTDOWN K FLUID LOSS CRCRUISE 1 EA15920FT 22237 702115 NR 3 ENG OIL PRESS FLUCTUATES FROM 35 TO 45 PSI. ENG OIL PRESS LIGHT BLINKS ON & OFF. ALSO OIL QTY WENT FROM 3/4 TO 1/4 AND BACK TO 1/2. FOUND UPPER ENGINE OIL LINE AT OIL FILTER HOUSING CHAFED. REPLACED CHAFED LINE, COI ISSUED/ AMM 20-11-18. 2L74 4F4 F A20WE E3NE 20050128000362005012800036EU 2005 1 28 DXTA200500535 120050115A5320 BLANKET BRAERO1000 BAE1251000 1500287EU FUSELAGE LOOSE E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07505QS 259005 FIVE SECONDS AFTER ADDING TAKEOFF POWER REAR BAY OVERHEAT LOOKUP LIGHT ILLUMINATED. LIGHT WENT OUT TWO SECONDS AFTER THROTTLE REDUCED TO IDLE. RAN ENGINES. CHECKED FOR LEAKS, NO LEAKS FOUND AT THIS TIME. FOUND HEAT BLANKET NOT SECURE ON EXPANSION PIPE OUTBOARD TEMP CONTROL VALVE. RADIATING HEAT ON OVERHEAT LOOP. SECURED BLANKET. RAN UP FULL POWER 30 SEC 3 TIMES WITH NO OVERHEAT LIGHT IAW HAWKER 1000 M/M 26-13-00. 2L72 4F RTA3EU 20050128000382005012800038CE 2005 1 28 DXTA200500532 120050114A323099146371 MANIFOLD CESSNA750 750 2076810CE NLG FAILED E DXTAO OTHER O OTHER CLCLIMB 1 GL07900QS4368 7500123 CLIMBING THROUGH 20,000 FT A VERY LOUD BANG EMITTED FROM THE NOSE GEAR COMPARTMENT. FIVE MINUTES LATER THERE WAS A SECOND LOUD BANG. THERE WAS ANOTHER LESS VOCAL BANG ENCOUNTERED AND SEVERAL IN THE DESCENT. REMOVED LANDING GEAR MANIFOLD. INSTALLED MODIFIED MANIFOLD ASSY P/N 8218-2. OPS AND LEAK CHECK OF MANIFOLD CHECKS GOOD. WORK PERFORMED IAW CHAPTER 32-30-00 AND 32-30-02 OF THE CE750 MM. 2L72 4J RTT00007WI 20050128000392005012800039CE 2005 1 28 DXTA200500540 120050117A7830 TAB CESSNA500 560CESSNA 2076750CE THRUST REVERSER BENT E DXTAO OTHER EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 GL07352QS 5600352 APPARENT PARTIAL THRUST REVERSER DEPLOYMENT AT CRUISE FLIGHT 30,000 FT. RIGHT UNLOCK LIGHT WAS ON, DEPLOY LIGHT DID NOT LIGHT. RUMBLING AND DECELERATION WAS FELT. METAL TAB ON OUTBOARD SIDE OF RIGHT THRUST REVERSER IS BENT UPWARD APPROXIMATELY .5 INCH. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20050128000402005012800040CE 2005 1 28 DXTA200500536 120050115A3230 ROLLER CESSNA750 750 2076810CE MLG LACK OF LUBE E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07912QS 7500012 ON DEPARTURE RED UNLOCK GEAR ILLUMINATED, RECYCLED THE GEAR: NORMAL DOWN AND LOCKED. RETURNED THE GEAR AND LIGHT STAYED ON. COULD NOT VERIFY DISCREPANCY IN HANGAR. BUT INSPECTED UPLOCK SYSTEM FOR ALL THREE GEARS. FOUND RIGHT GEAR UPLOCK ROLLER DIFFICULT TO TURN. REMOVED, CLEANED LUBED REINSTALLED UPLOCK ROLLERS ON ALL GEARS. VERIFIED UPLOCK HOOKS ALL MOVE FREELY. LUBRICATED UPLOCK HOOK PIVOT POINTS. OPERATED LANDING GEAR MULTIBLE TIMES & NO FAULTS NOTED. ALL WORK IAW CESSNA 750 MM 32-30-00. 2L72 4J RTT00007WI 20050128000432005012800043EA 2005 1 28 SWIA200514426 120050119A5210 CONTROL CABLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR MISROUTED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07405SW 7029 CABIN DOOR DIFFICULT TO CLOSE. REROUTED DOOR CABLE AS REQUIRED. OPERATED PAX DOOR SEVERAL TIMES. OPERATIONAL CHECKS GOOD. 2L72 4F RTA21EA 20050128000442005012800044EA 2005 1 28 SWIA200514427 120050121A2740 SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB CHANNEL DIRTY A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07932SW 7714 RECEIVED A-STAB CHANNEL 2 INOP STATUS MESSAGE AND A-MACH TRIM CAUTION MESSAGE. CLEANED AND LUBRICATED SWITCH, PERFORMED BITE CHECK IN HSTCU, OPERATIONAL CHECKED GOOD. 2L72 4F RTA21EA 20050128000482005012800048EA 2005 1 28 05020697 120050120A2740 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA DUAL STAB TRIM FAILED A VTZAA UNSCHED LANDING J WARNING INDICATION DEDESCENT 1 EA27697BR 7787 EVENT SUMMARY STATED DUAL STAB TRIM AND MACH TRIM FAIL IN FLT. REMOVED AND REPLACED STAB/MACH TRIM PANEL. OPS CHECK GOOD. 2L72 4F RTA21EA 20050128000512005012800051CE 2005 1 28 DXTA200500530 120050112A2910 WARNING LIGHT CESSNA560 560XL 2076702CE HYD SYSTEM ILLUMINATED E DXTAO OTHER J WARNING INDICATION APAPPROACH 1 GL07641QS 5605295 ON APPROACH WHEN FLAPS WERE SELECTED TO 15 DEG LOW HYD FLOW LT & RT CAUTION LIGHTS ILLUMINATED. THAT WAS FOLLOWED BY LOW HYD LEVEL AT AROUND THE SAME TIME THE FLAPS REACHED 15 DEG BECAUSE OF THE POTENTIAL FOR HYDRAULIC FLUID LOSS, AND EMERGENCY GEAR EXTENSION WAS PERFORMED. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20050128000542005012800054NM 2005 1 28 05FDEA00136 120050121A5753ARC25122 HINGE DOUG DC10 DC10 N/A-SDRNM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25395FE 46629 RIGHT WING INBOARD FLAP HINGE OUTBOARD PIVOT BUSHING GALLED AND PITTED. MEASURED BORE DIAMETER, FOUND TO BE OUT OF LIMITS IAW CMM 57-52-01, ALODINE AND PRIMED BORE IAW DC10-10 SRM 51-21-01. FABRICATED, INSTALLED AND HONED BUSHING TO A FINAL INSIDE DIAMETER OF .9995 - 1.0005 IAW DAC CMM 57-52-01 AND FEDEX EA 8-5750-83995, RT INBOARD FLAP, OUTBOARD HINGE BRACKET OVERSIZE PIVOT BORE - REPAIR. REFERENCE NON-ROUTINE N00385. 2L73 4F RTA22WE 20050128000552005012800055NM 2005 1 28 DHL2005760003 120050122A3350 LENS BOEING727 7272B7 138407LNM EMERGENCY LIGHT LOOSE A DHLAK NONE O OTHER ININSP/MAINT 1 SO01760AT 21954 FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT LENS WILL NOT STAY IN PLACE (FALLS OFF). RESET FWD ENTRY DOOR EMERGENCY EXIT LIGHT LENS COVER. LENS SECURE. OPS CHECK SERVICABLE PER 727 MM 33-50-71. 2L73 4F A3WE 20050128000562005012800056GL 2005 1 28 ARWA20050104 220050116A7200 ENGINE DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL NR 2 FAILED A ARWAEA ENGINE SHUTDOWN UNSCHED LANDING C F.O.D. CLCLIMB 1 SO1968041 46900 451548 NR 2 ENGINE FAILED ON ROTATION. ENGINE SHUTDOWN IN ACCORDANCE WITH CHECKLIST. AIRCRAFT RETURNED TO MSLP WITHOUT ANY FURTHER INCIDENT. ACCOMPLISHED RED BORDER 019056; REMOVED AND REPLACED NR 2 ENGINE IN ACCORDANCE WITH ARROW AIR DC-10 WORK CARD 142R7101M. PERFORMED ENGINE RUN IN ACCORDANCE WITH MM 11-00-00; ALL SYSTEMS INVOLVED OPERATIONAL CHECK OK. 2L73 4F4 F A22WE E23EA 20050128000572005012800057NM 2005 1 28 05FDEA00156 120050125A5347S4929147 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 MAIN DECK SEAT TRACK RBL 107 FOUND WITH SCRATCHES AT STA 1189 TO STA 1223. DAMAGED SEAT TRACK AT MAIN DECK STA 1189 TO STA 1223 RBL 107 CUT AS PER SRM 53-70-00 FIG 1 VOL I & REMOVED AS PER SRM 51-31-01 VOL II. REPAIR SEAT TRACK & SPLICE, FABRICATED AND INSTALLED AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20050128000582005012800058NM 2005 1 28 CALA0500018 120050121A531565C33950 FLOORBEAM BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2733608 27321 INSPECTION FOUND FLOORBEAM CORRODED AROUND SCREW HOLE AT STA 986, LBL 44, L17L. REPAIRED IAW SRM 53-60-51. 2L72 4F RTA16WE 20050128000622005012800062NE 2005 1 28 AT0500004 220050114A7200 SEAL BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE BULLET LOOSE A ZZDAE ENGINE SHUTDOWN E VIBRATION/BUFFET CRCRUISE 1 SO15906AT R5259104 55087 N1 VIBRATION ON RIGHT ENGINE INCREASED OVER TIME FROM 4.0 TO 7.0 AT 310. ON DESCENT VIBRATION TO 9.0 AND WAS FELT THROUGHOUT AIRCRAFT. ICING IN CLIMB, ENGINE ONLY NO WING OR TAIL. TEMP AT 310 - 40 C. ENGINE ONLY ICE WAS USED. REMOVED AND REPLACED AIR INTAKE ROTATING FAIRING AND NOSE IAW B717 AMM 72-38-01, OPS CHECKS NORMAL. RAN ENGINE VIB WITHIN LIMITS, OK FOR SERVICE. FOUND OMEGA SEAL ON OLD NOSE CONE SEPARATED FROM SPINNER, REF 52EB03. 2L72 4F4 FTRA6WE E00061EN 20050128000642005012800064NM 2005 1 28 UPS05443711 120050108A5311 FRAME BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C - BS 760, BETWEEN STR 5 - 8R, FRAME FOUND CRACK. M/D BS 760 BETWEEN STR 5R AND STR 8R FRAME REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 54. 2L74 4F A20WE 20050128000662005012800066NM 2005 1 28 UPS05443713 120050107A5313 STRINGER BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C - BS 1000 TO 1020 S10R STRINGER END FOUND CRACKED. M/D BS 1000 TO BS 1030 STR 10R STRINGER REPAIR CARRIED OUT IAW SRM 53-10-03 FIG 4. 2L74 4F A20WE 20050128000672005012800067NM 2005 1 28 UPS05443714 120050108A5311 FRAME BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C - FRAME BS 760 STR CUTOUT CRACKED AT S-6L AND S-7L. M/D BS 760 BETWEEN STR 6L AND STR 7L FRAME REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 54. 2L74 4F A20WE 20050128000682005012800068NM 2005 1 28 05FDEA00163 120050125A5313 FITTING BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25465FE 21289 WHILE WORKING EO 7-5340-7-4315F PT 2 FOUND 3 EACH HOLES WITH CRACK INDICATION IN LT HAND 940 STR 18A FITTING. REPAIRED BS 940 STR 18A FITTINGS IAW FEDEX EA 7-5340-72401. 2L73 4F RTA3WE 20050128000692005012800069EU 2005 1 28 MALA050125 120050108A5320 POST SAAB SF340 340B 7860101EU COCKPIT DOOR CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15425XJ 340B425 DURING C-CHECK IN YYC, COCKPIT DOOR RT VERTICAL POST AT RBL 10.5 IS CORRODED AT FLOOR LEVEL AND WILL BE REPAIRED IAW MESABA EO. REFER EAMS WORK ORDER 211363, TASK 1509 FOR ADDITIONAL INFORMATION A/C RETURNED TO SERVICE 1/12/2005. 2L72 4T RTA52EU 20050128000702005012800070NM 2005 1 28 05FDEA00181 120050127A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 CABIN SEAT TRACK DAMAGED AT STA Y = 910, X = 48. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE 1, VOLUME I. 2L73 4F RTA22WE 20050128000712005012800071NM 2005 1 28 05FDEA00182 120050127A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 CABIN SEAT TRACK DAMAGED AT STA Y = 910, X = -48. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE 1, VOLUME I. 2L73 4F RTA22WE 20050128000722005012800072NM 2005 1 28 05FDEA00184 120050127A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 CABIN SEAT TRACK DAMAGED AT STA Y = 805, X = 48. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE 1, VOLUME I. 2L73 4F RTA22WE 20050128000732005012800073NM 2005 1 28 05FDEA00185 120050127A5320 WEB DOUG MD11 MD11 3023602NM ZONE 700 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 CENTER WHEEL WELL FORWARD LEFT HAND VERTICAL WEB FOUND CRACK APPROXIMATELY 4 INCHES LONG FROM BOTTOM. CRACKED DOUBLER REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. 2L73 4F RTA22WE 20050128000742005012800074EU 2005 1 28 05FDEA00186 120050127A7830 THRUST REVERSER AIRBUS300 A300F4605R 3930327EU NR 1 ENGINE INOPERATIVE A FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25686FE 804 NR 1 REVERSER PRESSURIZED ECAM ALERT ON INITIAL TAKEOFF. NR 1 THRUST REVERSER INOP. THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POSITION. 2L72 4F RTA35EU 20050128000752005012800075EA 2005 1 28 VNAA0501007 120050120A1420 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS CONTAMINATED A VNAAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL05226JS 7895 FLAPS SELECTED TO 8 DEG ON APPROACH, FLAPS FAIL CAUTION MESSAGE ILLUM. RIGHT FLAPS INDICATED 0 DEG & LEFT 2 DEG. C/W QRH, DECLARED AN EMERGENCY, MADE AN UNEVENTFUL LANDING WITH ZERO FLAPS. MX DEPLOYED FLAPS TO 20 DEG, AIRCRAFT FERRIED TO DAY. MX INSPECTED & FOUND SKEW DETECTION UNIT CONNECTORS CONTAMINATED WITH GLYCOL. CANNON PLUGS CLEANED IAW STANDARD MAINTENANCE PROCEDURES. AS PRECAUTION FLAP ELECTRONIC CONTROL UNIT WAS REPLACED IAW CRJ 200 AMM 27-51-05-000-801/400-801. THE REMOVED UNIT WAS PUT INTO QUARANTINE. THE FLAP RIGGING WAS CHECKED IAW CRJ 200 AMM 27-54-00-710-801 AND THE FLAP SYSTEM WAS OPERATIONALLY CHECK GOOD IAW CRJ 200 AMM 27-54-00-710-801. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050128000762005012800076EA 2005 1 28 VNAA0501006 120050118A2760270007 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE SPOILERS FAILED A VNAAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL05251PS1401 7931 DURING APPROACH TO PIT, WHEN THE FLIGHT SPOILER HANDLE WAS MOVED TO DEPLOY, A FLIGHT SPOILER FAULT WHITE STATUS MESSAGE WAS DISPLAYED. THE PILOT RETURNED THE FLIGHT SPOILER HANDLE TO THE NORMAL POSITION AND MADE AN UNEVENTFUL LANDING. NO INCORRECT FLIGHT SPOILER POSITION OR HANDLING ABNORMALITIES WERE REPORTED BY THE CREW. AFTER TROUBLESHOOTING THE SYSTEM PSA MAINTENANCE REMOVED & REPLACE THE LT INBOARD & OUTBOARD FLIGHT SPOILER POWER CONTROL UNITS IAW CRJ 200 AMM 27-62-01-000-801/400-801. RIGGING AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050128000782005012800078NM 2005 1 28 05FDEA00183 120050127A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 CABIN SEAT TRACK DAMAGED AT STA Y = 805, X = -28. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE 1, VOLUME I. 2L73 4F RTA22WE 20050126001272005012600127NM 2005 1 26 2005UALA00065 120050116A2910 HYDRAULIC SYSTEM BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE RIGHT FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29676UA 30028 RETURNED TO LAX DUE TO RIGHT HYDRAULIC SYSTEM FAILURE. LOSS OF FLUID DUE TO FAILED O-RING ON CASE DRAIN MODULE DIFFERENTIAL PRESSURE INDICATOR BOSS. REPLACED O-RING AND RESERVICED HYDRAULIC SYSTEM. 2L72 4F4 FRTA1NM E24NE 20050126001452005012600145NM 2005 1 26 QXEA200500010 120050103A5230502213 SEAL BOMBDRDHC8 DHC8401 1390041NM FWD CARGO DOOR FAILED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09405QX26 4047 BOI - FLIGHT 2344 - THE FLIGHT WAS DIVERTED TO BOI WHEN THE CREW RECEIVED A CABIN PRESSURE WARNING LIGHT BETWEEN 15-16 THOUSAND FEET. BOI MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE AFT CARGO DOOR SEAL. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050126001482005012600148EU 2005 1 26 SA05002 120050102A5610NP1653116 WINDSHIELD AIRBUSA319 A319112 3930323EU COCKPIT CRACKED A USAAH DEACTIVATE SYST/CIRCUITS A FLAME/FIRE CRCRUISE 1 EA19701UW17661 890 DURING CRUISE AT FL 370, THE FIRST OFFICER'S WINDSHIELD BEGAN TO ARC AND DELAMINATE DIAGONALLY THE ENTIRE LENGTH OF WINDSHIELD. FOLLOWED THE QRH PROCEDURES AND PULLED CIRCUIT BREAKERS AF10 AND X14. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FIRST OFFICER'S WINDSHIELD ASSEMBLY AND THE NR 2 WINDSHIELD HEAT COMPUTER. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20050126001672005012600167EU 2005 1 26 AWXA200500055 120050111A5310D53480043203 BEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28621AW 053 DURING C-4 CHECK EXFOLIATION CORROSION WAS FOUND ON R-2 DOOR LOWER SILL BEAM AT FS 68 - 4 INCHES. MAINTENANCE REPAIRED R-2 DOOR LOWER SILL BEAM AT FS 68 - 4" IAW A320 SRM 53-41-14, FIG 201. 2L72 4F RTA28NM 20050126001752005012600175NM 2005 1 26 QXEA200500064 120050110A2610 SWITCH BOMBDRDHC8 DHC8401 1390041NM LEAK OVERTEMP MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09412QX 4059 NR 1 BLEED HOT CAUTION ILLUMINATED ON TAKEOFF ROTATION. NR 1 BLEED SELECTED AFT PER CHECKLIST. LIGHT WENT OUT WHEN NR 1 BLEED SELECTED OFF. THERE WAS AN UNUSUALLY HOT SMELL/ODOR NOTED TOWARD LATER PORTION OF TAKEOFF ROLL. MAINTENANCE REPLACED NACELLE DUCT LEAK OVERTEMP SWITCH. GROUND RAN NR 1 ENGINE, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050127000042005012700004GL 2005 1 27 RAIA00501027 220050111A741223057324 IGNITER BOX EMB 145 EMB145EP 3260221SO ALLSN AE300 AE3007A GL LT ENGINE FAILED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03827HK9921 145021 5665 - STL- ON TAXI OUT FROM GATE, LEFT ENGINE WOULD NOT LIGHT OFF. MAINTENANCE REMOVED AND REPLACED ENGINE BOTTOM IGNITER BOX CHANNEL. 2L72 4F4 FRTT00011ATTE6CH 20050127000122005012700012NM 2005 1 27 UPS05243697 120050111A5754 RIB BOEING727 727185C 138406NNM NR 5 SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 INSPECTION TYPE:C NR 5 LE SLAT STRUCTURE HAS THREE RIBS CRACKED BETWEEN O/B TRACK AND O/B EDGE OF SLAT. REPAIRED CRACKED RIBS 3 PLACES AT NR 5 LE SLAT IAW SRM 57-50-03 FIG 9. 2L73 4F A3WE 20050127000202005012700020NM 2005 1 27 UPS05243707 120050113A5754 SKIN BOEING727 727185C 138406NNM NR 6 SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 INSPECTION TYPE: C, LE SLAT ACCESS PANEL (NR 6 SLAT) HAS 1/2 INCH CRACK ON SKIN. REPAIR CARRIED OUT IAW SRM 51-10-01, 51-40-02 AND 51-30-02. 2L73 4F A3WE 20050127000232005012700023NM 2005 1 27 UPS05443693 120050106A5310 SHEAR TIE BOEING747 747123F NM FUSLEAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C M/D - FRAME BS 1438 SHEAR TIE CRACKED BTN S-23L/S-24L. M/D BS 1438 BETWEEN STR 23L/STR 24L FRAME SHEAR TIE REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 4. 2L74 4F A20WE 20050127000252005012700025NM 2005 1 27 UPS05443695 120050111A5741 FITTING BOEING747 747123F NM WING TO BODY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C RT WING BS 1241 UPPER REAR SPAR SIDE-TO-BODY KICK FITTING AREA FOUND CRACK AT TERMINAL FITTING NR 2 HOLE. HOLE REPAIRED AS PER SB 747-57A2314. 2L74 4F A20WE 20050127000292005012700029EA 2005 1 27 COMA0560071 120050123A3231601R751461 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA NLG DOOR FAULTY A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01937CA5638 7044 FLIGHT 5315 - AFTER TAKEOFF FROM ATL, THE NOSE GEAR DOORS WOULD NOT CLOSE, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. REPLACED THE NOSE DOOR SELECTOR VALVE. 2L72 4F RTA21EA 20050127000312005012700031SO 2005 1 27 RAIA00501024 120050110A3240142093 CONTROL UNIT EMB 145 EMB145LR 3260212SO BRAKE ASSY MALFUNCTIONED A RAIAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 CE03842HK1100 14500830 8088 - IAD - UNCOMMANDED BRAKE LOCK-UP. MAINTENANCE REMOVED AND REPLACED BRAKE CONTROL UNIT. 2L72 4T RTT00011AT 20050127000362005012700036SO 2005 1 27 RAIA00501036 120050115A7830 CONNECTOR EMB 145 EMB145LR 3260212SO PROXIMITY SWITCHDAMAGED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03815HK 145048 5752- STL- LEFT AIR/GROUND FAILED, ENGINE 1 AND ENGINE 2 THRUST REVERSE DISAGREED. MAINTENANCE REMOVED AND REPLACED CONNECTOR TO NOSE AIR/GROUND PROX SWITCH. 2L72 4T RTT00011AT 20050127000672005012700067NM 2005 1 27 QXEA200500005 120050102A6120 AUTOFEATHER SYS DHAV DHC8 DHC8202 2809007NM INOPERATIVE A QXEAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 NM09357PH 504 PDX FLIGHT NR 2185 NO ARM LIGHT ON TAKEOFF ROLL FOR AUTOFEATHER SYSTEM. REJECTED TAKEOFF AT 65 KTS. AUTOFEATHER SYSTEM CHECK ACCOMPLISHED PRIOR TO TAXI OUT. MAINTENANCE REPLACED NR 1 AND NR 2 ENGINE WIRING HARNESS. COMPLIED WITH AUTOFEATHER SYSTEM OPERATION CHECK. CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050127001122005012700112EA 2005 1 27 COMA0560077 120050123A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01466CA 7627 FLIGHT 5004 - DURING CVG APPROACH RECEIVED A FLAP FAIL MESSAGE, CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE FIRST EVENT MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER CAUTION MESSAGES. 2L72 4F RTA21EA 20050127001142005012700114NM 2005 1 27 DHL2005746001 120050120A1100 PLACARD BOEING727 727224 1384076NM NR 2 FUEL CELL DETERIORATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01746DH 22252 PUSH, PULL, & EMERGENCY EXIT PLACARDS BELOW F/O'S SLIDING WINDOW ARE EITHER MISSING OR UNREADABLE. RT WING NR 2 FUEL TANK SUMP DRAIN PLACARD IS DETERIORATED. REMOVED & REPLACED PLACARDS IAW B727 MM 20-10-10. REMOVED & REPLACED PLACARD IAW B727 MM 20-10-10. 2L73 4F A3WE 20050127001152005012700115EA 2005 1 27 COMA0560078 120050122A275011045D100101 COUPLING CNDAIRCL600 CL6002B19 1900309EA TE FLAPS WORN A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01470CA 7650 FLIGHT 5545 FLAPS FAIL CAUTION. REPLACED RT FLEX SHAFT. 2L72 4F RTA21EA 20050127001172005012700117EU 2005 1 27 YENA200515 120050125A3350 WIRE AIRBUS320 A320232 3930326EU EMERGENCY LIGHT BROKEN A YENAK NONE O OTHER ININSP/MAINT 1 EA15521JB 1452 R1 DOOR SIDEWALL EMERGENCY EXIT LIGHT ASSEMBLY INOP. REPAIRED BROKEN WIRE TO LIGHT ASSEMBLY. OP CHECK GOOD PER ESPM 20-53-00. 2L72 4F RTA28NM 20050127001192005012700119NM 2005 1 27 QXEA200500121 120050121A6120 AUTOFEATHER SYS DHAV DHC8 DHC8202 2809007NM FAILED A QXEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM09351PH 490 SEA - FLIGHT 2203 TAKEOFF ABORTED AT 60 KTS DUE TO FAILURE OF AUTOFEATHER TO ARM. DEFERRED IAW MRL 61-2. REF RSI 345810. 2H72 4T RTA13NM 20050127001752005012700175NE 2005 1 27 DHL2005760004 220050125A7200 ENGINE BOEING727 7272B7 138407LNM PWA JT8 JT8D17 52049NE NR 1 SHUTDOWN A DHLAD RETURN TO BLOCK Y ENGINE STOPPAGE TXTAXI/GRND HDL 1 SO01760AT 21954 NR 1 ENGINE AUTO-SHUTDOWN WHEN NR 2 ENGINE WAS STARTED. RESTARTED NR 1 ENGINE, NO DEFECTS NOTED. 2L73 4F4 F A3WE E2EA 20050127001802005012700180WP 2005 1 27 UPS05843751 120050106A53403755847U2 FITTING DOUG DC8 DC873F 302199FWP CARGO BAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01868UP 45968 INSPECTION TYPE:C3, CRACKED BANANA FITTING AT STA 1160 LONGERON 33R. GAINED ACCESS TO FITTING. REMOVED AND REPLACED FITTING PER SRM 51-1-20D, 51-1-8, 51-3-0. RESTORED AREA TO ORIGINAL CONFIG. 2L74 4F RT4A25 20050127001842005012700184EA 2005 1 27 COMA0560076 120050122A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAK NONE J WARNING INDICATION TXTAXI/GRND HDL 1 SO01467CA 7637 FLIGHT 5328 RECEIVED A FLAP FAIL CAUTON MESSAGE DURING PREFLIGHT WHEN SELECTING 20 DEGREE POSITION. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2L72 4F RTA21EA 20050127001942005012700194EA 2005 1 27 COMA0560074 120050122A3260 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA MLG FALSE INDICATIONA COMAO OTHER N FALSE WARNING APAPPROACH 1 SO01995CA 7229 FLIGHT 5401 RECEIVED A NOSE LANDING GEAR DISAGREE CAUTION DURING APPROACH INTO NAS. INTERROGATED PSEU, CHECKED UPLOCK GAP AND SENSOR FOR SECURITY AND CYCLED GEAR MULTIPLE TIMES. DISCREPANCY COULD NOT BE DUPLICATED BY MAINTENANCE. 2L72 4F RTA21EA 20050127001962005012700196NM 2005 1 27 757BJ0015 120050117A2710 CONTROL CABLE BOEING757 757236 1384971NM AILERONS FRAYED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05757BJ 22176 AILERON CABLE FRAYED AT NR 1 FLAP TRACK. REPLACED CABLE PER MM 27-00-01 AND COMPLIED WITH BOEING SB 757-27-0109. 2L72 4F RTA2NM 20050127002012005012700201EU 2005 1 27 AWXA200500061 120050111A5347D5337111200500 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28621AW 053 SAL - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON RT OUTBOARD SEAT TRACK BETWEEN FR 44 AND FR 46. MAINTENANCE REMOVED CORRODED SECTION OF RT OUTBOARD SEAT TRACK FROM FR 40 TO FR 46; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050127002032005012700203EU 2005 1 27 AWXA200500063 120050111A5315D53472075000 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28621AW 053 SAL - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1732 LT BETWEEN FR 65 AND FR 66. MAINTENANCE REMOVED CORRODED BEAM Y1732 LT FROM FR 65 TO FR 66; FABRICATED A NEW REPLACEMENT BEAM PER DWG D53474250; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050128000012005012800001EU 2005 1 28 05FDEA00178 120050126A272081681 ACTUATOR AIRBUS310 A310222 3930315EU RUDDER MALFUNCTIONED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25448FE 260 AFTER TAKEOFF AND FLAPS RETRACTED, BOTH NR 1 & 2 RUDDER FAULT. WOULD NOT RESET, EXTENDED THE FLAPS & THE RUDDER FAULT WENT AWAY. REMOVED AND REPLACED RUDDER VARIABLE STOP ACTUATOR PER A310-200 MM 27-23-23-4. TEST GOOD ON SYS 1 & 2 PER MM 27-23-00-5. PREMATURE REMOVAL/INSTALLATION, OFF MFG 8168-1. 2L72 4F RTA35EU 20050128000092005012800009EA 2005 1 28 05014676 120050114A3030 HEATER CNDAIRCL600 CL6002B19 1900309EA AOA VANE FAILED A VTZAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA27676BR 7644 CREW REPORT STATED THAT DURING TAXI OUT RECEIVED CAUTION MESSAGE (R AOA HEAT FAIL). CONTACTED MX CTRL AND RTG. SWAPPED AIRCRAFT. REMOVED AND REPLACED NR 1 ADSHC IAW 30-31-15. OPS CHECK GOOD. 2L72 4F RTA21EA 20050128000112005012800011 2005 1 28 COMA0560073 420050123A31606229810016 DISPLAY CNDAIRCL600 CL6002B19 1900309EA COCKPIT FAULTY A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01458CA8046 7613 FLIGHT 5251 DURING TAKEOFF RECEIVED FLAGS ON CAPTAINS FLIGHT DISPLAY FOLLOWED BY LOSS OF ADI SCREEN. ABORTED TAKEOFF AND RETURNED TO THE GATE. REPLACED THE NR 1 PRIMARY FLIGHT DISPLAY. 2L72 4F RTA21EA 20050128000202005012800020NM 2005 1 28 05FDEA00167 120050125A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 CABIN SEAT TRACK DAMAGED AT STA Y = 6-80, X = -48. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE 1, VOLUME I. 2L73 4F RTA22WE 20050128000262005012800026NM 2005 1 28 UPS05443734 120050126A2120 UNKNOWN BOEING747 747200 1384847NM COCKPIT FUMES A IPXAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO01522UP 21936 AFTER TAKEOFF THERE WERE STRONG FUMES IN COCKPIT. CREW DECLARED AN EMERGENCY AND LANDED SAFELY IN SDF. RAN ALL 3 PACKS, NO DEFECTS NOTED. OK FOR CONTINUED SERVICE 2L74 4F RTA20WE 20050128000372005012800037CE 2005 1 28 DXTA200500533 120050114A31507013348943 DAU CESSNA750 750 2076810CE COCKPIT FAILED E DXTAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TXTAXI/GRND HDL 1 GL07943QS159 7500043 DAU 2B MISCOMP CAS MESSAGE CYCLED THREE TIMES. STAYED ON THE THIRD TIME, ALL ENGINE INDICATORS, OIL, FUEL FLOW, FUEL QUANTITIES, ETC. FAILED DAU FAIL CAS MESSAGE CAME ON. THIS WAS FOLLOWED BY A STRONG BURNING ODOR. MESSAGES CLEARED TAXIING IN. REMOVED NR 2 DAU, PER CUSTOMER REQUEST REPOSITIONED NR 1 DAU P/N 7013348-943, S/N 96050518 TO THE NR 2 POSITION. INSTALLED NEW DAU IN THE NR 1 POSITION P/N 7013348-943, S/N 00053440, REF MM 31-41-00, OPS CHECKED SYSTEMS WITH NO DEFECTS NOTED AT THIS TIME. RE-INSTALLED BAGGAGE PNLS. 2L72 4J RTT00007WI 20050128000412005012800041CE 2005 1 28 0107200501 120050104A31101143840111 PEDESTAL BEECH 1900 1900D 1154162CE COCKPIT FIRE A NSVADF RETURN TO BLOCK ACTIVATE FIRE EXT. A FLAME/FIRE TXTAXI/GRND HDL 1 EA27172MJ UE72 FLAMES VISIBLE UNDER CENTER PEDESTAL NEAR RUDDER TRIM CONTROL KNOB. 2L72 4T RTA24CE 20050128000462005012800046EU 2005 1 28 AWXA200500065 120050108A5321D5367202200000 FLOOR PANEL AIRBUS320 A320231 3930325EU FUSELAGE DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28621AW 053 DURING C-04 CHECK AFT CARGO COMPARTMENT FLOOR PANEL 151DF WAS FOUND DELAMINATED. MAINTENANCE REMOVED DELAMINATED FLOOR PANEL 151DF FROM FR 47 TO FR 59; FABRICATED A NEW REPLACEMENT FLOOR PANEL AND DOUBLER; INSTALLED REPLACEMENT PARTS IAW EO 5326-01007. 2L72 4F RTA28NM 20050128000502005012800050NE 2005 1 28 DXTA200500529 220050111A720030358005D ENGINE CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE LEFT MALFUNCTIONED E DXTAE ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TXTAXI/GRND HDL 1 GL07306QS 5600266 PCE500019 LEFT ENGINE SHUTDOWN WHEN THROTTLES WERE BROUGHT IDLE. PERFORMED LT ENGINE RUN OPERATIONAL CHECK AND NO DEFECTS NOTED. REMOVED LT LOWER COWLING TO INSPECT FUEL CONTROL, STARTER GENERATOR, AND INSPECTED QUADRANT AND NO DEFECTS WERE NOTED. COULD NOT DUPLICATE SQUAWK. ALL WORK DONE IAW CE 560 ULTRA MM CHAPTER 71-01-02, 73-30-03, 24-31-00 & 76-11-00. 2L72 4F4 FRTA22CE E25EA 20050128000592005012800059EA 2005 1 28 05018705 120050118A2611PU90421R3 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA LAVATORY FAILED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27705BR 7470 LAV SMOKE INDICATION ON TAKEOFF. MX PERFORMED ENGINE RUNS AT T/O POWER WITH PACKS FULL HOT AND SLIGHTLY PRESSURIZED SEVERAL TIMES, NO LAV SMOKE INDICATIONS. REMOVED AND REPLACED LAV SMOKE DETECTOR, OPS CHECK GOOD. 2L72 4F RTA21EA 20050128000602005012800060EA 2005 1 28 SWIA200514430 120050117A27604916405 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07903SW6274 6274 7425 OUTBOARD AND INBOARD SPOILER FAULT STATUS. REPLACED NR 2 SECU IAW CRJ AMM REF CHAP 27-60-00. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050128000612005012800061NM 2005 1 28 UPS05243710 120050107A575464834315 CASTING BOEING727 727185C 138406NNM NR 3 K-FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 INSPECTION TYPE:C, NR 3 KRUEGER FLAP INBOARD HINGE, FIXED LEADING EDGE CASTING HAS EVIDENCE OF INTERGRANULAR CORROSION. REPLACED AND INSTALLED NEW CASTING IAW DRG 64-8343. 2L73 4F A3WE 20050128000772005012800077EA 2005 1 28 VNAA0501008 120050123A5230 HANDLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CARGO DOOR UNSECURE A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL05220PS 7887 AFTER TAKEOFF FROM DCA FLIGHT 2445 WAS CLIMBING THRU 8000 FT WHEN THE CARGO DOOR CAUTION MESSAGE ILLUMINATED. THE CREW DECIDED TO RETURN TO DCA TO HAVE MAINTENANCE INSPECT THE CARGO DOOR. NO EMERGENCY WAS DECLARED. NO LOSS OF PRESSURIZATION WAS REPORTED. THE FLIGHT LANDED WITHOUT INCIDENT. UPON INSPECTION THE CARGO DOOR HANDLE WAS FOUND UNSTOWED. CONTRACT MAINTENANCE AT DCA OPS CHECKED THE CARGO DOOR HANDLE AND RESECURED THE DOOR IAW CRJ 200 AMM 52-31-03-710-801 AND AMM 52-31-03-710-002. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050128000792005012800079NM 2005 1 28 QXEA200500110 120050119A33506050251 BATTERY PACK BOMBDRDHC8 DHC8401 1390041NM EMERGENCY LIGHT INOPERATIVE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09412QX 4059 SEA - MAIN CABIN DOOR EMERGENCY LIGHTING WILL ONLY STAY ILLUMINATED FOR 3 SECONDS. REMOVED AND REPLACED FORWARD BATTERY PACKS. OPS CHECKED GOOD. WAITING FOR REMOVAL INFORMATION. 2H72 4T RTA13NM 20050128000802005012800080NM 2005 1 28 0500086743 120050118A3040NP103801111 WINDOW BOEING747 747249F 1384849NM COCKPIT FAILED A NWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL01643NW9593 9593 22245 DURING FLIGHT, HEATING ELEMENT ON WINDOW 1L OVERHEATED AND SMOKED. WINDOW HEAT WAS TURNED OFF AND SMOKE STOPPED. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. WINDOW WAS MEL'D AND LATER REPLACED 19JAN05 IN SIN. OPERATIONAL CHECK GOOD. 2L74 4F A20WE 20050128000822005012800082EU 2005 1 28 AWXA200500066 120050102A5321D5367202300000 FLOOR PANEL AIRBUS320 A320231 3930325EU CABIN DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28621AW 053 SAL - MAJOR REPAIR - DURING C-04 CHECK AFT CARGO COMPARTMENT FLOOR PANEL 151GF WAS FOUND DELAMINATED. MAINTENANCE REMOVED DELAMINATED FLOOR PANEL 151GF FROM FR 47 TO FR 49; FABRICATED A NEW REPLACEMENT FLOOR PANEL AND DOUBLER; INSTALLED REPLACEMENT PARTS IAW EO 5326-01007. 2L72 4F RTA28NM 20050128000832005012800083NM 2005 1 28 HNAA0500003 120050117A2913570347 PUMP DHAV DHC8 DHC8102 2809003NM HYD SYSTEM FAILED A HNAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA07908HA 015 WHILE EN ROUTE FROM CLT TO LYH THE CAPT CALLED MAINTENANCE CONTROL WITH A HYD PUMP CAUTION LIGHT. AFTER TROUBLESHOOTING IT WAS FELT BEST TO DIVERT TO ROA. CREW DID NOT DECLARE AN EMERGENCY. ALSO FOUND HYD SOV FAILED IN CLOSED POSITION. P/N AND S/N OFF AV16B2003D, M26622. 2H72 4T RTA13NM 20050128000862005012800086NM 2005 1 28 AWXA200500069 120050108A53206554862503 INTERCOSTAL BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1 INCH CRACK WAS FOUND ON LT AFT LAVATORY SUBFLOOR PAN TO AFT PRESSURE BULKHEAD CLOSEOUT WEB (INTERCOSTAL FLOOR SEAL) AT BS 1032, LBL 27.38. MAINTENANCE REMOVED DAMAGED PORTION OF INTERCOSTAL FLOOR SEAL AT BS 1032, LBL 27.38; FABRICATED A REPAIR PLATE; INSTALLED REPAIR PART IAW B737-300 SRM 51-70-13 FIG 1. 2L72 4F RTA16WE 20050128000922005012800092EU 2005 1 28 05FDEA00158 120050122A3260 PROXIMITY SWITCH AIRBUS310 A310222 3930315EU NLG DIRTY A FDEAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO25417FE 333 LOWERING GEAR ON APPROACH EDDF NOSE GEAR NO GREEN DOWN INDICATION, DOOR LIGHT ILLUMINATED BOTH SYSTEMS. RECYCLED 3 TIMES, SAME RESULT. EXECUTED GO-AROUND. ON CLIMBOUT NOSE GEAR SHOWED DOWN AND LOCKED, BOTH SYSTEMS. T/S PER WD 32-61-02,32-62-01 AND 32-62-02. CLEANED PROX SW C/P'S. NO FAULTS INDICATED ON PROX BITE UNIT. LUBRICATED NLG PER W/C 05T0001. PERFORMED GEAR SWING PER W/C 47T0011. CYCLED GEAR 3 TIMES EACH SYSTEM, ALL INDICATIONS NORMAL. 2L72 4F RTA35EU 20050128000952005012800095NM 2005 1 28 QXEA200500096 120050108A5347 SEAT TRACK DHAV DHC8 DHC8102 2809003NM ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09369PH 513 PDX - LEFT HAND CENTER SEAT TRACK NR 4 HAS GOUGES AT FRAME 350 TO 364. REPAIRED IAW SRM 51-40-11. 2H72 4T RTA13NM 20050128000972005012800097NM 2005 1 28 QXEA200500098 120050108A5347 SEAT TRACK DHAV DHC8 DHC8102 2809003NM ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09369PH 513 PDX - LEFT HAND CENTER SEAT TRACK NR 4 HAS GOUGES AT FRAME 405 TO 417. REPAIRED IAW SRM 51-40-11. 2H72 4T RTA13NM 20050128000982005012800098NM 2005 1 28 QXEA200500090 120050108A5347 SEAT TRACK DHAV DHC8 DHC8102 2809003NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09369PH 513 PDX - RIGHT HAND CENTER TRACK NR 7 HAS LITE CORROSION AT X210.100 TO FRAME 234.500. REPAIRED IAW SRM 51-40-11. 2H72 4T RTA13NM 20050128001012005012800101NM 2005 1 28 UPS05443716 120050108A5311 FRAME BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C - BS 960, S8R, FRAME FOUND CRACK. FRAME REPAIRED PER SRM 53-10-04 FIG 54. 2L74 4F A20WE 20050128001022005012800102NM 2005 1 28 QXEA200500111 120050118A2420 WARNING LIGHT BOMBDRDHC8 DHC8401 1390041NM AC GENERATOR ILLUMINATED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09405QX 4047 YYC - FLIGHT 2331 - AFTER ENGINE START, NR 2 AC GENERATOR CAUTION CAME ON. MAINTENANCE RESET AC GENERATOR IAW EMERGENCY AND ABNORMAL CHECKLIST. NR 2 AC GENERATOR CAUTION EXTINGUISHED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050128001042005012800104NM 2005 1 28 UPS05443718 120050104A571265B078368 RIB BOEING747 747123 1384873NM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C, RT WING NR 23 O/B ARM I/B RIB O/B FACE -D- POINT AREA SUSPECT CRACK. RIB REPAIRED AS PER RS R-57-41-35223 AND EO B747-5740-21619-A. 2L74 4F A20WE 20050128001052005012800105WP 2005 1 28 ARWA20050105 120050120A275257726913 ACTUATOR DOUG DC8 DC862F 3021972WP TE FLAP FAILED A ARWAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO19791AL 46150 SPLIT FLAPS INTO SJO, RETURN TO PTY. REMOVED AND REPLACED RT FLAPS INBOARD ACTUATING CYLINDER IN ACCORDANCE WITH DC8 MM 27-51-9. OPERATIONAL CHECK NORMAL IN ACCORDANCE WITH DC8 MM 27-50-0. NO ADJUSTMENT WAS NEEDED. 2L74 4F 4A25 20050128001062005012800106NM 2005 1 28 UPS05443719 120050105A541165B903107780 FRAME BOEING747 747123 1384873NM NR 4 NACELLE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C, NR 4 NACELLE STRUT REAR MOUNT BULKHEAD FWD OUTBOARD FRAME WEB FOUND CRACKED (REFER ATTACH SKETCH FOR LOCATION). REAR ENG MOUNT BULKHEAD FRAME REPAIRED PER RS R54-53-35228 AND ENGINEERING FILE NUMBER 747-54-20050. 2L74 4F A20WE 20050128001082005012800108NM 2005 1 28 05FDEA00174 120050126A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25235FE 21329 BS 720, RBL 39, STR 24, WL 163 FRAME DENTED. REPAIRED FRAME AT BS 720, STR 24, RBL 39, WL 163 PER SRM 51-40-3. 2L73 4F RTA3WE 20050128001092005012800109NM 2005 1 28 757BJ0013 120050117A5340 ATTACH ANGLE BOEING757 757236 1384971NM FUSELAGE DAMAGED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05757BJ 22176 ATTACH ANGLE DAMAGED BENEATH THE LEFT TRANSITION ANGLE IN THE AFT CARGO BIN AT BS 1360. REPLACED ANGLE PER SRM 51-30-01, 51-40-05, AND 51-40-02. 2L72 4F RTA2NM 20050128001102005012800110NM 2005 1 28 757BJ0014 120050117A2710 CONTROL CABLE BOEING757 757236 1384971NM AILERONS WORN A PIDAK NONE O OTHER ININSP/MAINT 1 SO05757BJ 22176 AILERON CABLE WORN AT THE NR 8 FLAP TRACK. REPLACED CABLE PER MM 27-00-01 AND COMPLIED WITH BOEING SB 757-27-0109. 2L72 4F RTA2NM 20050128001122005012800112NE 2005 1 28 DHL2005365002 220050125A72619143M92P04 GARLOCK SEAL AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE ENGINE LEAKING A DHLAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO01365DH 149 CREW REPORTED THAT ACFT LOSING OIL QUANTITY FROM 18 QUARTS BEFORE TAKEOFF THEN 10 QUARTS SHORTLY AFTER TAKEOFF,THEN DOWN TO 3 QUARTS AT 0545Z AND AT 0612Z 1 QT OIL QUANTITY REPORTED. NR 1 CSD LEAKING AT GARLOCK GEARBOX DRAIN CAVITY. R/R GARLOCK SEAL & O-RING IAW CFM BUILDUP 72. R/R OF CSD IAW MM 24-11-11. SEE OPS AND LEAK CHECK ITEM 8M LOG 35363. 2L72 4F4 FRTA35EU E23EA 20050128001132005012800113SO 2005 1 28 RAIA00501045 120050121A2760 PROXIMITY SWITCH EMB 145 EMB145LR 3260212SO SPOILERS DIRTY A RAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03816HK 145055 JAX - ENGINE 1 REV DISAGREE SPOILER FAIL MESSAGE ON EICAS. MAINTENANCE INSPECTED AND CLEANED LANDING GEAR PROX SWITCHES. 2L72 4T RTT00011AT 20050128001142005012800114 2005 1 28 RAIA00501042 420050119A3418 SENSOR JETAIRJETSTMJETSTM4101 1500501EU STALL WARNING MALFUNCTIONED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03553HK 41066 ON TAKEOFF BOTH STALL LIGHTS CAME ON. ABORTED TAKEOFF. MAINTENANCE RESET STALL WARNING AOA SENSORS AND PERFORMED OPERATIONAL CHECK. 2L72 4T RTA41NM 20050128001152005012800115SO 2005 1 28 RAIA00501049 120050120A213122250N030301 CONTROLLER EMB 145 EMB145 3260210SO CABIN PRESSURE FAILED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03821HK8828 145068 STL - AUTO PRESSURIZATION INOP MESSAGE. MAINTENANCE REMOVED AND REPLACED AUTO PRESSURIZATION CONTROLLER. 2L72 4F RTT00011AT 20050128001172005012800117WP 2005 1 28 RAIA00501046 220050121A7421Y2092 IGNITER JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33112UHR WP NR 1 ENGINE FAILED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03555HK 41072 ABE - NR 1 ENGINE WILL NOT START. MAINTENANCE REMOVED AND REPLACED IGNITERS ON LEFT ENGINE. 2L72 4T4 TRTA41NM E4WE 20050128001182005012800118SO 2005 1 28 RAIA00501048 120050122A3020102AU1AF PROBE EMB 145 EMB145LR 3260212SO NR 1 ENGINE FAILED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03814HK8133 145046 STL - TAT NR 1 HEAT INOP EICAS WITH OVERRIDE IN ENGINE DURING TAXI. MAINTENANCE REMOVED AND REPLACED NR 1 TAT PROBE. 2L72 4T RTT00011AT 20050128001222005012800122NM 2005 1 28 UPS05443721 120050106A5313 STRINGER BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C M/D - STR END BS 1476 S-15L CRACKED. CRACKED STRINGER REPAIRED PER RS 53-41-35226 AND ENGINEERING FILE NUMBER 747-53-20202. 2L74 4F A20WE 20050128001262005012800126WP 2005 1 28 05FDEA00152 120050124A5753NRC6068514 SUPPORT DOUG DC10 DC1010CF 3023502WP ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25363FE 48263 COMPLY WITH EA 8-5750-55430 WINGS - FLAP VANE SUPPORT CORROSION REWORK RIGHT O/B FLAP. COMPLIED WITH EA 8-5750-55430. 2L73 4F RTA22WE 20050128001282005012800128NM 2005 1 28 SWAA050188 120050124A53306545774 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29664WN 23495 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN AT BS 787, STRINGER 18L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050128001292005012800129NM 2005 1 28 SWAA050189 120050124A53306545767 SKIN BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29686SW 23175 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 482, STRINGER 10R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050128001312005012800131NM 2005 1 28 SWAA050183 120050124A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 500A,STRINGER 16R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20050128001342005012800134NM 2005 1 28 SWAA050186 120050124A53106519603 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29606SW 27926 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB BETWEEN BS 360 AND BS 380, LBL 64, CORRODED. REMOVED AND REPLACED WEB SECTION PER SRM. 2L72 4F RTA16WE 20050131000012005013100001NM 2005 1 31 SWAA050204 120050125A53156545734 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29602SW 27953 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM ZEE CHORD AT BS 270, BETWEEN LBL 11 AND RBL 11, CORRODED. REMOVED AND REPLACED ZEE CHORD PER SRM. 2L72 4F RTA16WE 20050131000022005013100002 2005 1 31 SWAA050191 420050125A2565D31354 SLIDE BOEING737 7373T5 1384608NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29694SW 23061 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050131000042005013100004NM 2005 1 31 SWAA050193 120050125A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 427, STRINGER 17L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20050131000052005013100005NM 2005 1 31 SWAA050194 120050125A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 947, STRINGER 20L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050131000092005013100009NM 2005 1 31 SWAA050205 120050125A2560PH22300L GLOWSTRIP BOEING737 7373H4 1384600NM CABIN DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29655WN 28400 DURING SCHEDULED PM CHECK, FOUND FWD RT PHOTOLUMINESCENT STRIP DELAMINATED. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER MM. 2L72 4F RTA16WE 20050131000102005013100010NM 2005 1 31 SWAA050206 120050125A53306545765 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 500C, STRINGER 16L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20050131000142005013100014NM 2005 1 31 SWAA050210 120050125A3350B21506 FUSE BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29783SW 29809 DURING SPV, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED FUSE PER MM. 2L72 4F RTA16WE 20050131000152005013100015NM 2005 1 31 SWAA050202 120050125A531165C22909 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29602SW 27953 DURING SCHEDULED D-CHECK, FOUND FWD CARGO COMPARTMENT FRAME AT BS 500C, BETWEEN STRINGERS 27R AND 28L, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20050131000162005013100016NM 2005 1 31 SWAA050203 120050125A53116546534 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29602SW 27953 DURING SCHEDULED D-CHECK, FOUND FWD CARGO COMPARTMENT FRAME AT BS 520, BETWEEN STRINGERS 27L AND 28L, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20050131000272005013100027EA 2005 1 31 COMA0560055 120050118A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION DEDESCENT 1 SO01479CA 7675 FLIGHT 5354 DURING FINAL APPROACH TO BOS RECEIVED A FLAP FAIL MESSAGE WHEN FLAPS SELECTED TO 30 DEGREES. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE FIRST EVENT, MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2L72 4F RTA21EA 20050131000292005013100029EA 2005 1 31 COMA0560060 120050118A5210 SPRING CNDAIRCL600 CL6002B19 1900309EA DOOR HANDLE OUT OF ADJUST A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01917CA 7017 FLIGHT 5385 CABIN DOOR UNSAFE WARNING CLIMBOUT OF LGA. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. ADJUSTED CABIN DOOR HANDLE INNER SPRING. 2L72 4F RTA21EA 20050131000302005013100030EA 2005 1 31 COMA0560062 120050117A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION LDLANDING 1 SO01977CA 7157 FLIGHT 5903 FLAPS FAIL CAUTION MESSAGE. COULD NOT DUPLICATE. INSPECTED FLAP SYSTEM PER AD 98-20-01, NO DEFECTS FOUND. 2L72 4F RTA21EA 20050131000322005013100032NM 2005 1 31 UPS05443722 120050106A5313 STRINGER BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C - STR END BS 1484 S-17L CRACKED. CRACKED STRINGER REPAIRED PER RS 53-41-35227 AND ENGINEERING FILE NUMBER 747-53-20203. 2L74 4F A20WE 20050131000332005013100033NM 2005 1 31 UPS05443724 120050107A551365B02778600 STRINGER BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C - LEFT BS 2658 STR 13 FOUND CRACKED. STRINGER REPLACED AS PER SRM 50-10-01. 2L74 4F A20WE 20050131000372005013100037NM 2005 1 31 UPS05443728 120050107A534065B38600170 STRINGER CLIP BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 BS 1060 STR 5R, STRINGER TIE CLIP FOUND CRACKED. M/D BS 1060 STR 5R, STRINGER TIE CLIP REPLACED IAW SRM 51-10-01 PAGE 9. 2L74 4F A20WE 20050131000382005013100038EA 2005 1 31 05020641 120050120A2740601R517063 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA STAB/MACH FAULTY A VTZAA UNSCHED LANDING O OTHER CRCRUISE 1 EA27641BR 7349 STAB CHANNEL NR 1 MESSAGE. RTF. REMOVED AND REPLACED STAB/MACH PANEL. OPS CHECK GOOD. 2L72 4F RTA21EA 20050131000392005013100039NM 2005 1 31 249TR0103 120050103A2121245201 GASPER FAN BOEING737 7372K5 138448XNM CABIN BURNED OUT A PIDAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO05249TR 22598 GASPER FAN CREATES A SMELL OF SMOKE IN FORWARD SECTION OF CABIN. REPLACED GASPER FAN AND OPS CHECKED GOOD PER MM 21-24-21. NOTE: NO FURTHER WRITE UPS AS OF 01/17/2005. TEAR DOWN REPORT INDICATED IMPELLER DIFFICULT TO ROTATE BY HAND. INSPECTION REVEALED BEARING FAILURE CAUSED UNIT MALFUNCTION. 2L72 4F RTA16WE 20050131000412005013100041WP 2005 1 31 DHL2005801001 120050119A2611 BULB DOUG DC8 DC873F 302199FWP SMOKE DETECTOR BURNED OUT A DHLAO OTHER LP NO TEST NO WARNING INDICATION NRNOT REPORTED 1 SO01801DH 46033 NR 14 SMOKE DETECTOR DOES NOT PRESS TO TEST. REMOVED AND REPLACED BULBS AT NR 14 SMOKE DETECTOR. OPS CHECK OK IAW MM 26-10-6. P/N 376. 2L74 4F RT4A25 20050131000442005013100044SO 2005 1 31 SWIA200514415 120050117A27503075001007 FCU EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07187SW2872 2872 120037 AFTER LANDING FLAPS STAYED AT 45 DEGREES. INSTALLED A SERVICEABLE FCU. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050131000452005013100045SO 2005 1 31 SWIA200514416 120050116A2750 FCU EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07290SW 120317 FLAP CONTROL FAULT ON FLAP RETRACTION ON GROUND. REMOVED AND REPLACED FLAP CONTROL UNIT AND FLAP SELECTOR HANDLE. OPERATIONAL CHECK GOOD IAW 27-50-01. 2L72 4T RTA31SO 20050131000462005013100046EA 2005 1 31 SWIA200514417 120050115A27604916406 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07925SW5622 5622 7682 SPOILERON FAULT AND GROUND SPOILER FAULT. REMOVED AND REPLACED NR 2 SECU IAW MM 27-61-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050131000472005013100047 2005 1 31 SWIA200514418 420050119A34183995100208 COMPUTER CNDAIRCL600 CL6002B19 1900309EA STALL WARNING MALFUNCTIONED A SWIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM07936SW3036 3036 7726 STALL FAIL CAUTION ILLUMINATED ON TAKEOFF. REMOVED AND REPLACED STALL PROTECTION COMPUTER IAW CRJ 200 MM ATA CHPT 27-35-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050131000522005013100052NM 2005 1 31 SWAA050143 120050119A5313BAC1498 STRINGER BOEING737 7373T5 1384608NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29667SW 23063 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER 26R, BETWEEN BS 1006 AND 1016, CORRODED. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2L72 4F RTA16WE 20050131000532005013100053NM 2005 1 31 SWAA050144 120050119A53106546529 SHEAR TIE BOEING737 7373T5 1384608NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29667SW 23063 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 500D, STRINGER 26L, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050131000542005013100054NM 2005 1 31 SWAA050145 120050119A5315BAC1509100146 FLOORBEAM BOEING737 7373T5 1384608NM AFT CARGO COMPT CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29667SW 23063 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPARTMENT FLOORBEAM AT BS 772, LBL 8, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER EA. 2L72 4F RTA16WE 20050131000572005013100057NM 2005 1 31 DHL2005750001 120050115A5270914CE13 SWITCH BOEING727 7272M7 138407SNM MCD LATCH INOPERATIVE A DHLAK NONE J WARNING INDICATION ININSP/MAINT 1 SO01750DH 21951 LATCHES UNLOCKED LIGHT ON CARGO DOOR PANEL OUT WITH DOOR OPEN. REMOVED AND REPLACED Q-TUBE LATCH LOCK SWITCH IAW B-727-200 FRIEGHTER M/M CHAPTER 24 PG 28, 29. P/N 914CE1-3 INSTALLED, OPS CHECK SERVICEABLE. 2L73 4F A3WE 20050131000582005013100058GL 2005 1 31 DHL2005365001 220050115A7320 CABLE AIRBUS300 A300B4203 3930306EU GE CF6 CF6* 30020GL ZONE 400 OUT OF ADJUST A DHLAEF ENGINE SHUTDOWN ACTIVATE FIRE EXT. GB MULTIPLE FAILURE SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO01365DH 149 ENG NR 2 WOULD NOT SHUTDOWN WHEN FUEL LEVER MOVED TO OFF. ENGINE SHUTDOWN WITH FIRE HANDLE. MAINTENANCE INDICATED SMOKE FROM NR 2 ENGINE AND NR 1 FIRE BOTTLE WAS DISCHARGED. ADJUSTED HP SHUTOFF VALVE FLEXIBLE CABLE IAW MM 76-12-31. OPS CK GOOD IAW 76-12-31 AND JRH. REF L/P 009983 ITEMS 4M & 5M FOR FIRE BOTTLE. REFERENCED ITEM 2P LP 009983 ENG 2 NR 1 FIRE BOTTLE DISCHARGED. REFERENCED ITEM 4M LP 009984 FIRE BOTTLE MISSING CARTRIDGE. REMOVED AND REPLACED FIRE EXTINGUISHER BOTTLE IAW MM 26-21-11, OPS TEST OK. INSTALLED FIREX CARTRIDGE IAW MM 26-21-13. 2L72 4F4 FRTA35EU E23EA 20050131000592005013100059NM 2005 1 31 05FDEA00125 120050118A5320 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25596FE 48554 LONGERON SPLICE FOUND CRACKED AT STA 1531 LONGERON 30R. SPLICE FABRICATED AS PER DWG AEA7643 REPLACED AS PER SRM 51-31-01 VOL2. 2L73 4F RTA22WE 20050131000602005013100060NM 2005 1 31 05FDEA00126 120050118A5320 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25596FE 48554 LONGERON SPLICE FOUND CRACKED AT STA 1531 LONGERON 29R. NEW SPLICE MACHINED AS PER DWG AEA7643 AND INSTALLED AS PER SRM 51-31-01 VOL 2. 2L73 4F RTA22WE 20050131000612005013100061SO 2005 1 31 SWIA200514412 120050112A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT DISCHARGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07297SW9436 9436 120327 F/A REPORT, CENTER SECTION OF EMERGENCY LIGHTS INOPERATIVE. REPLACED CENTER ELBP. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050131000642005013100064NM 2005 1 31 P5CA0501306 120050120A29133508806 PUMP BOEING747 747283B 1384867NM NR 2 HYD SYSTEM LEAKING A P5CAO OTHER K FLUID LOSS CRCRUISE 1 EA15921FT 21575 LOSS OF NR 2 HYDRAULIC SYSTEM. HYDRAULIC QUANTITY WENT FROM 6.5 GALLONS TO ZERO IN LESS THAN 5 SECONDS. FOUND NR 2 ENG EDP CASING CRACKED. REMOVED NR 2 EDP PER MM 29-11-05 AND DEFERRED PER MEL 29-1A. 2L74 4F A20WE 20050131000652005013100065NM 2005 1 31 P5CA0501307 120050121A29133508806 PUMP BOEING747 747283B 1384867NM NR 2 HYD SYSTEM LEAKING A P5CAE ENGINE SHUTDOWN K FLUID LOSS CLCLIMB 1 EA15921FT 21575 DURING CLIMB NR 2 ENGINE OIL QTY DROPPED TO ZERO. AFTER 5 MINUTES OIL PRESSURE 40 PSI AND FLUCTUATING. OIL TEMPERATURE NORMAL. ENGINE SHUTDOWN. REPLACED EDP PER MM 29-141-05. LEAK AND OPS CHECK OK PER MM 29-11-05. 2L74 4F A20WE 20050131000662005013100066WP 2005 1 31 DHL2005804001 120050114A2611 LAMP DOUG DC8 DC873F 302199FWP SMOKE DETECTOR INOPERATIVE A DHLAO OTHER PL NO WARNING INDICATION NO TEST NRNOT REPORTED 1 SO01804DH 46124 NR 13 SMOKE DETECTOR WILL NOT TEST. RELAMPED NR 13 SMOKE DETECTOR IAW MM 26-10-6. 2L74 4F RT4A25 20050131000672005013100067NM 2005 1 31 SWAA050199 120050125A53306545772 SKIN BOEING737 7373H4 1384600NM FUSELAGE WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN BETWEEN BS 875 AND BS 878, STRINGER 1, WORN. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20050131000702005013100070 2005 1 31 SWIA200514431 420050114A3197 WIRE EMB 120 EMB120ER 3260203SO WARNING SYSTEM BROKEN A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07582SW 120350 TAKEOFF TRIM AURAL WARNING WHEN TRIM IS IN THE GREEN BAND. A BROKEN WIRE WAS REPAIRED. OPERATIONAL CHECK GOOD REFERENCING 27-00-00. 2L72 4T RTA31SO 20050131000722005013100072NM 2005 1 31 UPS05443729 120050105A534065B38600Y160 STRINGER CLIP BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C M/D - BS 1640 LT STR 3L TIE CLIP FOUND CRACKED. M/D BS 1640 STR 3L TIE CLIP REPLACED IAW SRM 51-10-01 PAGE 9. 2L74 4F A20WE 20050131000762005013100076NM 2005 1 31 QXEA200500113 120050120A33506038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007NM ZONE 200 INOPERATIVE A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09345PH6653 33 476 DURING TAXI, THE FLIGHT ATTENDANT NOTIFIED THE FLIGHT CREW THAT DURING THE AUTOFEATHER TEST THE FLOOR PROX LIGHTING AT 1DE HAD THREE LIGHTS THAT WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 FLOOR STRIP LIGHT AND POWER SUPPLY. OPS CHECK GOOD. 2H72 4T RTA13NM 20050131000772005013100077WP 2005 1 31 CALA0500020 120050122A53479957871531S SEAT TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2735836 49441 INSPECTION FOUND CAPTAIN'S AFT I/B SEAT TRACK CORRODED AT STA 83.55 - 101.55, LBL 10. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-01. 2L72 4F A6WE 20050131000792005013100079NM 2005 1 31 SWAA050154 120050120A57536546434370 SKIN BOEING737 7375H4 138449DNM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29519SW 25318 DURING SCHEDULED C3 CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED T/E FLAP PER MM. 2L72 4F RTA16WE 20050131000802005013100080NM 2005 1 31 SWAA050155 120050120A53306545776 SKIN BOEING737 7373T5 1384608NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29667SW 23063 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE INNER SKIN AT BS 989.5 BETWEEN STRINGER 24L AND STRINGER 25L, CORRODED. REMOVED AND REPLACED SKIN SECTION PER SRM. 2L72 4F RTA16WE 20050131000822005013100082EU 2005 1 31 MALA050129 120050111A5230 SKIN BAC 146 AVRO146RJ85A1500097EU CARGO DOOR DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15517XJ E2335 DURING C-CHECK IN YYC, FWD CARGO COMPARTMENT OUTER DOOR SKIN DAMAGE (GOUGE) APPROXIMATELY .080 INCH L X .060 INCH W X .012 INCH D, LOCATION 8.5 INCHES FROM DOOR FWD EDGE AND 10.25 FROM LOWER EDGE. REFER TO 409 224657 FOR ADDITIONAL INFORMATION. AC RETURNED TO SERVICE 1/12/05. 2H74 4F RTA49EU 20050131000832005013100083NM 2005 1 31 SWAA050156 120050120A53306545774 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29667SW 23063 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 727D + 13, STRINGER 19R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050131000842005013100084NM 2005 1 31 UPS05443730 120050108A532065B164201 STIFFENER BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C - BS 1080 RBL 99 BELOW FLOOR STIFFENER FOUND CRACKED. M/D BS 1080 RBL 99 BELOW FLOOR STIFFENER REPLACED IAW SRM 51-10-01 PAGE 9. 2L74 4F A20WE 20050131000862005013100086EA 2005 1 31 05023690 120050123A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ILLUMINATED A VTZAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA27690BR 7739 ABORTED TAKEOFF FOR THRUST REVERSER UNSAFE MESSAGE. PERFORMED OPS CHECK AND ENGINE RUN. NO DEFECT NOTED. 2L72 4F RTA21EA 20050131000872005013100087EA 2005 1 31 QXEA200500102 120050118A32134900018 STRUT CNDAIRCL600 CL6002C10 1390015EA RT MLG BINDING A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09605QX7517 10022 ON LIFT-OFF, THE CREW RECEIVED A WOW INPUT CAUTION MESSAGE. THE OVERRIDE WAS USED TO RAISE THE GEAR. WHEN THE GEAR WAS RAISED, THE WOW INPUT CAUTION WAS EXTINGUISHED FOLLOWED BY A GEAR DISAGREE CAUTION WHICH REMAINED ILLUMINATED FOR APPROXIMATELY 5 SECONDS. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE RIGHT MAIN LANDING GEAR STRUT AFTER DETERMINING THAT THE STRUT WAS BINDING. OPERATIONAL CHECKS WERE PERFORMED AND WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20050131000882005013100088NM 2005 1 31 SWAA050200 120050125A57536546435335 SKIN BOEING737 7373H4 1384600NM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29392SW 27379 DURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED T/E AFT FLAP PER MM. 2L72 4F RTA16WE 20050131000892005013100089EA 2005 1 31 SWIA200514414 120050111A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY MALFUNCTIONED A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07925SW 7682 WHILE PAX BOARDING AND BAGGAGE LOADING, RECEIVED A SMOKE CARGO WARNING WITH ASSOCIATED WARNINGS. CARGO COMPARTMENT WAS CHECKED, AND NO FIRE OR SMOKE NOTED. REPLACED FORWARD CARGO SMOKE DETECTOR. OPERATIONAL CHECK GOOD. REF CRJ MM CHAP 26-15-00. 2L72 4F RTA21EA 20050131000912005013100091EU 2005 1 31 05FDEA00130 120050120A5530 SPAR AIRBUS310 A310203 3930313EU ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25405FE 237 VERTICAL FIN REAR SPAR R & L PANEL SUPPORT STRUCTURE HAS MODERATE CORROSION AT PANEL ATTACH POINTS. REMOVED CORROSION IAW A310-200 SRM. APPLIED SURFACE PROTECTION IAW A310-200 SRM 51-23-10. AT RT SIDE RIB 26, TRIMMED OUT DAMAGED SECTION OF TOP FLANGE, INSTALLED 2024-T3 FILLER, AND 2024-T3 0.063 STRAP IAW EA 6-5530-85551 DATED 01/04/05. 2L72 4F RTA35EU 20050131000932005013100093NM 2005 1 31 05FDEA00132 120050120A5311 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25596FE 48554 MAIN DECK CARGO COMPARTMENT LEFT AFT FUSELAGE UPPER MAIN FRAME AT STA 1681 FOUND WITH DENT. MAIN FRAME AT STA 1721 BETWEEN LONGERON 11L TO 13L REPAIRED AS PER SRM 53-30-00 FIG1 VOL1. REFER TRACKING EA 1-5310-81680. 2L73 4F RTA22WE 20050131000942005013100094NM 2005 1 31 05FDEA00133 120050120A5311 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25596FE 48554 MAIN DECK CARGO COMPARTMENT LEFT AFT FUSELAGE UPPER MAIN FRAME AT STA 1701 FOUND WITH DENT. REPAIRED AS PER SRM 53-30-00 FIG1 VOL1. REFER TRACKING EA 1-5310-81698. 2L73 4F RTA22WE 20050131000952005013100095NM 2005 1 31 SWAA050157 120050120A53126546568 BULKHEAD BOEING737 7373T5 1384608NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29667SW 23063 DURING SCHEDULED 1/4D CHECK, FOUND PRESSURE BULKHEAD WEB AT BS 1016, LBL 1, CORRODED. REPAIRED WEB PER ACO. 2L72 4F RTA16WE 20050131000962005013100096NM 2005 1 31 SWAA050158 120050120A53306545769 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29667SW 23063 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT FWD ENTRY DOOR CUTOUT AFT LOWER CORNER, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20050127000762005012700076EA 2005 1 27 QXEA200500050 120050103A5710 PAN CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09608QX 10026 PDX - RIGHT HAND STUB WING PRESSURE PAN HAS TWO CRACKS WHERE THE NR 2 PRESSURE HYDRAULIC LINE PASSES THROUGH. REPAIRED IAW SRM 51-42-06-001-0001-A01, SRM 51-23-00 AND SRM 51-42-06. 2L72 4F RTA21EA 20050127000842005012700084SO 2005 1 27 CHQA200500005 120050112A3260 SQUAT SWITCH EMB 135 EMB135KL 3260302SO MLG CONTAMINATED A CHQAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL11373SK 145543 FLIGHT 5880 ATL TO STL - AFTER GEAR RETRACTION AN LG AIR/GRD FAIL MESSAGE APPEARED ON EICAS. GEAR RETRACTED NORMALLY AND INDICATED UP. THE AIRCRAFT WAS DIVERTED TO IND AND AN EMERGENCY WAS DECLARED. THE BRAKE SYSTEM DEGRADED AFTER LANDING BUT THE AIRCRAFT LANDED NORMALLY. MAINTENANCE PERFORMED AIR/GROUND WARNING SYSTEM SIMULATION AND ADJUSTMENT TEST IAW EMB 140 AMM 32-63-00. AIR/GROUND SYSTEM OPS CHECKS GOOD AT THIS TIME. CLEANED WOW SWITCHES ON GEAR. 2L72 4F RTT00011AT 20050127000882005012700088SO 2005 1 27 CHQA200500006 120050112A2740 WARNING LIGHT EMB 145 EMB145LR 3260212SO COCKPIUT ILLUMINATED A CHQAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL11281SK 145391 AT APPROXIMATELY 1000 FT CPT PTTRIM SW FAIL MESSAGE APPEARED ON EICAS. A MINUTE OR TWO LATER A PTTRIM BACKUP SW FAIL MESSAGE APPEARED ON EICAS. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO FIELD IN PVD WITHOUT INCIDENT. MAINTENANCE DRAINED H20 FROM ADC SYSTEMS. ADC SYSTEMS OPS CHECK GOOD. TROUBLESHOT PITCH TRIM SYSTEMS PER FIM. NO DEFECTS WERE FOUND. BOTH BACK UP AND MAIN PITCH TRIMS OPS CHECK GOOD. AIRCRAFT WAS TEST FLOWN WITH NO DEFECTS NOTED. 2L72 4T RTT00011AT 20050127001532005012700153WP 2005 1 27 UPS05843747 120050103A5730576954533 DOUBLER DOUG DC8 DC873F 302199FWP LT WING L/E CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01868UP 45968 INSPECTION TYPE:C3, LEFT WING O/B LEADING EDGE LOWER INTERNAL DOUBLER CRACKED NEAR XFS 623. FABRICATED REPLACEMENT DOUBLER FROM SHT7075T6-.080 REF DWG 5769545. REMOVED & REPLACED DOUBLER REF SRM 51-1-8, 51-1-21, 51-1-20D. 2L74 4F RT4A25 20050127001552005012700155NM 2005 1 27 SWAA050187 120050124A53116546465 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29606SW 27926 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 992, RBL 55, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20050127001572005012700157NM 2005 1 27 QXEA200500116 120050123A2611473054 DETECTOR DHAV DHC8 DHC8202 2809007NM CARGO BAY DIRTY A QXEAO OTHER N FALSE WARNING APAPPROACH 1 NM09355PH16777 500 PDX - FLIGHT 2287 - ON FINAL APPROACH, AT 2000 FEET, THE MASTER WARNING/SMOKE ALARM SOUNDED. NO FUMES OR ODORS WERE DETECTED. MAINTENANCE INSPECTED BOTH BAG BAY SMOKE DETECTORS FOR LOOSE CONNECTORS, CHAFED WIRES AND ANY OBVIOUS DEFECTS, NONE WERE NOTED. BOTH DETECTORS WERE CLEANED AND OPERATIONAL CHECKS WERE PERFORMED. THE CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050127001602005012700160EA 2005 1 27 05015656 120050115A2611 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA LAV SMOKE DETECTFALSE INDICATIONA VTZAO OTHER N FALSE WARNING CLCLIMB 1 EA27656BR 7485 EVENT SUMMARY STATED LAV SMOKE INDICATION. INSPECTED BOTH PACKS AND WATER SOCKS. NO DEFECTS NOTED. INSPECTED LAV LIGHTS. NO DEFECTS FOUND. PERFORMED EXTENSIVE ENGINE RUNS. NO DEFECTS FOUND. A/C OK FOR SERVICE. 2L72 4F RTA21EA 20050127001622005012700162WP 2005 1 27 CALA0500017 120050121A5315S2912399 FLOORBEAM DOUG DC9 DC982 3022082WP FUSLEAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2735836 49441 INSPECTION FOUND FLOORBEAM CORRODED AT STA 180, LBL 12 TO LBL 37. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-3 AND 51-30-2. 2L72 4F A6WE 20050127001862005012700186WP 2005 1 27 ABXA050015 120050109A53155644657503 FLOORBEAM DOUG DC8 DC863F 302198FWP RT O/B LOWER CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23814AX 46041 CORROSION DISCOVERED ON FLOORBEAM AT STA 920, LOCATED AT OUTBOARD END OF THE BEAM LOWER RIGHT FLANGE. CORROSION IS BEYOND 20 PERCENT OF MATERIAL THICKNESS. REPAIRED BEAM BY CUTTING AND REMOVING AFFECTED AREA AND SPLICING IN NEW SECTION IAW REA D853-51248-MR. 2L74 4F 4A25 20050127001902005012700190WP 2005 1 27 ABXA050019 120050106A5311591359577 FRAME DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23970AX 47494 FRAME CRACKED AT LONGERON 13 RIGHT, STA 1152. REPAIRED FRAME IAW DC-9 SRM 53-03 AND 51-30-5. 2L72 4F A6WE 20050127001922005012700192WP 2005 1 27 ABXA050020 120050106A523059101575 PAN DOUG DC9 DC941 302207NWP AFT CARGO DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23970AX 47494 CRACK IN RADIUS OF INNER PAN AT AFT LATCH CAM. REPAIRED CRACKED PAN IAW DC-9 SRM 52-05. 2L72 4F A6WE 20050127001952005012700195NM 2005 1 27 HNAA0500004 120050118A3260 SENSOR DHAV DHC8 DHC8201 2809001NM WOW OUT OF ADJUST A HNAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA07983HA 478 WOW CAUTION LIGHT ILLUMINATED AT 400 FEET WITH GEAR UP. LEFT O/B WOW SENSOR GAP TO LARGE, RE-ADJUSTED SENSOR. MORE TO FOLLOW. 2H72 4T RTA13NM 20050127001972005012700197NM 2005 1 27 757BJ0016 120050117A335020131A BATTERY PACK BOEING757 757236 1384971NM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05757BJ 22176 FORWARD RIGHT EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK. OPS CHECKS OK. 2L72 4F RTA2NM 20050128000032005012800003NM 2005 1 28 05FDEA00180 120050127A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 CABIN SEAT TRACK DAMAGED AT STA Y = 1029, X = 48. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE 1, VOLUME I. 2L73 4F RTA22WE 20050128000102005012800010NM 2005 1 28 HNAA0500001 120050105A3297 WIRE HARNESS DHAV DHC8 DHC8102 2809003NM MLG MISROUTED A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07912HA 040 AFTER TAKEOFF NOSE GEAR WOULD NOT RETRACT AND LT & RT GEAR DOORS REMAINED OPEN, NOSE GEAR RED TRANSIT LIGHT STAYED ILLUMINATED. LT AND RT MAINS RETRACTED NORMALLY. REROUTED ELECTRICAL HARNESS AND SEATED CONNECTORS, OPS CHECK GOOD. 2H72 4T RTA13NM 20050128000192005012800019NM 2005 1 28 05FDEA00166 120050125A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 CABIN SEAT TRACK DAMAGED AT STA Y = 6-70 TO Y = 6-90, X = -8. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE 1, VOLUME I. 2L73 4F RTA22WE 20050128000302005012800030GL 2005 1 28 05FDEA00144 220050121A7261 ENGINE DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL NR 2 LEAKING A FDEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO2540061 46973 NR 2 ENGINE OIL LEAK. ON CLIMBOUT NR 2 ENG OIL QTY DROPPED 18 QTS TO 9 QTS ON FINAL NR 2 OIL READ 3 QTS, AFTER LANDING NR 2 OIL QTY WAS 9 PTS. REMOVED & REPLACED B-SUMP SCAVENGE LINE IAW MM 79-00-01-1. FUEL SHROUD REMOVED AND REPLACED REF WRI 73-10/0359. RAN NR 2 ENG HIGH PWR PER JRH OPENED NR 2 ENG CORE COWL CHECKED FOR LEAKS, NO LEAKS NOTED. CLOSED NR 2 ENG CORE COWL PER AMM 79-00-01-1. 2L73 4F4 F A22WE E23EA 20050128000342005012800034NM 2005 1 28 05FDEA00147 120050123A5313 LONGERON DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25596FE 48554 RIGHT ATTIC AREA FOUND LONGERON 6R SPLICE FITTING CRACKED AT STA 1521-1541. SPLICE FITTING FABRICATED AS PER DWG 7112 AND REPLACED AS PER SRM 51- 33-01 VOL 2. 2L73 4F RTA22WE 20050128000422005012800042CE 2005 1 28 ACE011205 120050112A2842 ANNUNCIATOR BEECH 1900 1900C 1154161CE FUEL FEED ACTIVATED E YADAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 AL03112AX UC45 PILOT REPORTED RIGHT HAND ENGINE FUEL FEED ANNUNCIATOR ON INTERMITTENTLY AFTER TAKEOFF. RETURNED FOR UNEVENTFUL LANDING. MAINTENANCE COULD NOT DUPLICATE THE PROBLEM. SYSTEM DEFERRED FOR ADDITIONAL REPORTS. 2L72 4T RTA24CE 20050128000532005012800053 2005 1 28 DXTA200500531 420050111A34427014300901 DISPLAY CESSNA500 560CESSNA 2076750CE NR 2 PFD FAILED E DXTAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 GL07377QS 5600377 DURING TAKEOFF ROLL WHILE ACCELERATING THROUGH 60 KTS THE COPILOTS NR 2 PFD SCREEN WENT BLANK FOLLOWED BY A DISPLAY OF A RED -X-, THEN DISPLAYED A NORMAL SCREEN. TAKEOFF WAS ABORTED. REMOVED AND REPLACED CO-PILOT PFD. OP CHECKED GOOD IAW CITATION ULTRA MM 22-05-24. 2L72 4F RTA22CE 20050128000872005012800087WP 2005 1 28 DHL2005803001 120050115A80113978921 SHUTOFF VALVE DOUG DC8 DC873 302199CWP STARTER FAILED A DHLAE ENGINE SHUTDOWN KSJFLUID LOSS AFFECT SYSTEMS WARNING INDICATION CLCLIMB 1 SO01803DH3567 3567 1048RC 46123 START VALVE OPEN LIGHT ILLUMINATED NEAR TOP OF CLIMB, OIL PRESSURE LIGHT ILLUMINATED AND ENGINE WAS SHUTDOWN WITH 10 PSI OF OIL PRESSURE ON GAUGE AND 0 OIL QUANTITY SHUTDOWN NR 3 ENGINE AT 22:05. FOUND STARTER FAILED WHICH CAUSED OIL LOSS. REMOVED AND REPLACED NR 3 ENGINE STARTER AND STARTER SHUTOFF VALVE. PERFORMED ENGINE RUN ON NR 3 ENGINE (HIGH POWER) IAW JRH STARTER AND STARTER SHUTOFF OPS AND LEAK CHECKS GOOD IAW 80-10-1. FOUND DAMAGE TO NR 3 ENGINE RT FAN COWL CAUSED BY STARTER FAILURE. REMOVED AND REPLACED 3 ENGINE RT FAN COWL DOOR IAW 71-10-2. 2L74 4F RT4A25 20050128000902005012800090EA 2005 1 28 05020624 120050120A2150 A/C PACK CNDAIRCL600 CL6002B19 1900309EA LEFT OVERHEATED A VTZAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 EA27624BR 7211 EVENT SUMMARY STATED LT PACK OVERHEAT IN AUTO, ADG AUTO DEPLOY. REMOVED AND REPLACED DEPLOYMENT SQUIB. RETRACTED ADG. SYSTEM OPS CHECK GOOD. 2L72 4F RTA21EA 20050128000912005012800091NM 2005 1 28 05FDEA00157 120050125A5347S4929147 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 CABIN SEAT TRACK AT STA 791 LBL 27.5 FOUND TO HAVE BOLTS INSTALLED WRONGLY. SEAT TRACK AT STA 740 TO STA 815 REMOVED AS PER SRM 51-31-01 VOL II. REPAIR SEAT TRACK & SPLICE FABRICATED AND INSTALLED AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20050128000992005012800099NM 2005 1 28 QXEA200500093 120050108A5347 SEAT TRACK DHAV DHC8 DHC8102 2809003NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09369PH 513 PDX - LEFT HAND CENTER SEAT TRACK NR 4 HAS CORROSION ON FLANGE AT STATION 234.500. REPAIRED IAW SRM 51-40-11. 2H72 4T RTA13NM 20050128001032005012800103NM 2005 1 28 UPS05443717 120050112A5330 SKIN BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C, CORROSION INDICATOR REVEALED ON FUSELAGE UPPER SKIN AT BS 1820 TO BS 1825 STR 46L. CORROSION BLEND OUT 0.035 X 2 X 2 INCHES EXCEED SRM LIMIT. OVER LAPPING SKIN REPLACED AS PER SRM 53-30-03 FIG 17 AND REPAIR DOUBLER AND FILLER INSTALLED AS PER SRM 53-30-03 FIG 17. 2L74 4F A20WE 20050128001072005012800107NM 2005 1 28 UPS05443720 120050108A531365B044216 STRINGER BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C M/D - STR END BS 739 S-8L CRACKED. CRACKED STRINGER REPAIRED PER RS 53-21-35238 AND ENGINEERING FILE NUMBER 747-53-20206. 2L74 4F A20WE 20050128001162005012800116SO 2005 1 28 RAIA00501044 120050120A2130D389926FA98SN CONNECTOR EMB 145 EMB145 3260210SO WOW SWITCH BROKEN A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03821HK 145068 STL - LG AIR/GRD FAIL EICAS MESSAGE AFTER TAKEOFF. PRESSURIZATION LOSS DURING DESCENT. MAINTENANCE INSPECTED LANDING GEAR AIR/GRD WOW SWITCH. FOUND RIGHT WOW SWITCH PIN BROKEN. REPLACED CONNECTOR. 2L72 4F RTT00011AT 20050128001272005012800127SO 2005 1 28 C2XA05BT006 120050119A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713913 145438 DURING SERVICE AND ROUTINE CHECK IN BTV MAINTENANCE FOUND THE EMERGENCY LIGHT INOPERATIVE AT SEAT 12A PSU. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY BULB AT SEAT 12A PSU IAW EMB145 AMM 33-50-07. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050128001302005012800130NM 2005 1 28 SWAA050190 120050124A53306545765 SKIN BOEING737 7377H4 1384404NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29760SW 27874 DURING SCHEDULED 5Y CHECK, FOUND LOWER FUSELAGE SKIN BETWEEN BS 500 + 8 AND BS 500A + 12, AT AIRFONE ANTENNA, CORRODED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050128001332005012800133NM 2005 1 28 SWAA050185 120050124A57546573714 ATTACH FITTING BOEING737 7373H4 1384600NM LT WING SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29602SW 27953 DURING SCHEDULED D-CHECK, FOUND LT WING L/E NR 3 SLAT ACTUATOR ATTACH FITTING CRACKED. REPAIRED SLAT FITTING PER SRM. 2L72 4F RTA16WE 20050131000062005013100006NM 2005 1 31 SWAA050195 120050125A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 358, STRINGER 18R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20050131000982005013100098NM 2005 1 31 SWAA050160 120050120A52106545871 DOOR FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29653SW 28398 DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR FRAME AT AFT LOWER CORNER CRACKED. REMOVED AND REPLACED FWD SERVICE DOOR PER MM. 2L72 4F RTA16WE 20050131000992005013100099SO 2005 1 31 C2XA05RI001 120050113A335066367 LIGHT EMB 145 EMB145LR 3260212SO CABIN BURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2717984 145246 RIC - DURING ROUTINE INSPECTION, MAINTENANCE FOUND EMERGENCY LIGHT FLOOR STRIP, BY SEAT 6A, INOP. MAINTENANCE REMOVED AND REPLACED STRIP. OPERATIONAL CHECK WAS PERFORMED SUCCESSFULLY. THE ACFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20050131001012005013100101CE 2005 1 31 160105 120050116A5270 ANNUNCIATOR BEECH 1900 1900D 1154162CE E/E BAY DOOR ACTIVATED A NSVAO OTHER J WARNING INDICATION CRCRUISE 1 EA27172MJ UE72 CABIN DOOR ANNUCIATOR IN FLIGHT. 2L72 4T RTA24CE 20050131001022005013100102NM 2005 1 31 05FDEA00070 120050111A5310 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25235FE 21329 BS 720C, STR 28L - STR 27L CORROSION ON SHEAR TIE. *S/D* REPAIRED SHEAR TIE PER SRM 53-10-4. 2L73 4F RTA3WE 20050131001032005013100103EU 2005 1 31 UPS05143688 120050119A3242E16289 CONTROL UNIT AIRBUSA300 A300F4622R 3930360EU BRAKES INOPERATIVE A IPXAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01124UP 0808 INSPECTION TYPE:N/A ON TAXI OUT LEFT BRAKES WERE DRAGGING. A/C CAME TO A STOP AT IDLE POWER SETTING. ALL BRAKE TEMPS ON LEFT SIDE WERE HIGHER THAN NORMAL (110-150 LEFT) (35-50 RIGHT SIDE). ON T/O LEFT BRAKE TEMPS WENT TO 24C. T/S PER 1300 TSM 32-42-00-1. JACKED AND CHECKED CONDITION/SECURITY OF WHEEL/BRAKE ASSEMBLIES - BLED NORMAL BRAKE SYSTEM PER A300 MM 32-42-00-3. PERFORMED BITE TEST OF BSC11 - FAULT CODES 242 & 246 PER TABLE NOTE 1 REPLACED BRAKE SYSTEM CONTROL UNIT PER A300 MM 32-42-72-4. 2L72 4F RTA35EU 20050131001042005013100104NM 2005 1 31 UPS05243683 120050113A5340 FITTING BOEING727 727185C 138406NNM AFT CARGO BAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 INSPECTION TYPE:C, SUSPECT CRACK ON CLEAT AT STR 29L ON FWD SIDE OF BS 1110 AFT CARGO BAY. HFEC CARRIED OUT IAW NDTM 51-00-00 FIG 4. CRACK CONFIRMED. REMOVED CRACKED CLEAT, FABRICATED AND INSTALLED NEW CLEAT IAW SRM 51-30-02. 2L73 4F A3WE 20050131001052005013100105NM 2005 1 31 UPS05243684 120050113A5340 FITTING BOEING727 727185C 138406NNM AFT CARGO BAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 INSPECTION TYPE:C SUSPECT CRACK ON CLEAT AT STR 28L ON FWD SIDE OF BS 1070 AFT CARGO BAY. HFEC CARRIED OUT IAW NDTM 51-00-00 FIG 4. RESULT CRACK CONFIRMED. REMOVED CRACKED CLEAT, FABRICATED AND INSTALLED NEW CLEAT IAW SRM 51-20-1. 2L73 4F A3WE 20050131001072005013100107NM 2005 1 31 2005F00013 120050114A3211658638824 ATTACH FITTING BOEING727 7272M7 138407SNM RT MLG TRUNNION DEFORMED B DHLAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01750DH 21951 RT WING LG TRUNNION HALVES BENT AND GOUGED. 2L73 4F A3WE 20050131001082005013100108SO 2005 1 31 C2XA05SH003 120050119A532014530628001 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2736915 145421 SHV - DURING C-CHECK CENTER OMEGA BEAM INNER SURFACE HAS CORROSION BETWEEN FR 24 & 25. MAINTENANCE REMOVED THE DAMAGE AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-23-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050131001142005013100114EA 2005 1 31 COMA0560041 120050116A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01466CA 7627 FLIGHT 5614 FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20050131001152005013100115EA 2005 1 31 COMA0560048 120050111A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT LOOSE A COMAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01713CA 7245 FLIGHT 5509 - 3 EMERGENCY LIGHTS INOP. REPAIRED LOOSE WIRING. 2L72 4F RTA21EA 20050131001182005013100118NM 2005 1 31 757BJ0011 120050117A5350 DRAG ANGLE BOEING757 757236 1384971NM FUSELAGE WORN A PIDAK NONE O OTHER ININSP/MAINT 1 SO05757BJ 22176 WEAR ON THE VERTICAL LEG OF THE LEFT FIN ATTACH ANGLE (DRAG ANGLE) BETWEEN BS 1164 AND BS 1720. REPAIRED PER EA 53-319. 2L72 4F RTA2NM 20050131001192005013100119NM 2005 1 31 QXEA200500101 120050116A213192146A010401 CONTROLLER BOMBDRDHC8 DHC8401 1390041NM ZONE 200 FAILED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09414QX7719 4061 DURING THE CLIMB FROM YEG, THE PRESSURIZATION FAILED. THE CHECKLIST WAS FOLLOWED AND PRESSURIZATION WAS FOUND TO BE CONTROLLABLE IN MANUAL MODE. MAINTENANCE INSPECTED THE AIRCRAFT AND DEFERRED THE AUTO PORTION OF THE PRESSURIZATION SYSTEM. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. SDR TO REMAIN OPEN PENDING CLEARANCE OF THE MEL. *S/D* MAINTENANCE REPLACED THE PRESSURE CONTROLLER. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050131001212005013100121NM 2005 1 31 SWAA050201 120050125A53116546593 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29602SW 27953 DURING SCHEDULED D-CHECK, FOUND FWD CARGO COMPARTMENT FRAME AT BS 500A, BETWEEN STRINGERS 28L AND 28R, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20050131001222005013100122NM 2005 1 31 UPS05443731 120050107A534065B386001169 STRINGER CLIP BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C - BS 620 S15L FRAME TIE CLIP FOUND CRACK. TIE CLIP REPLACED PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050131001232005013100123NM 2005 1 31 UPS05443732 120050107A534065B38600170 STRINGER CLIP BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C M/D - BS 1040 S3R STRINGER TIE CLIP FOUND CRACKED. STRINGER CLIP REPLACED PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050131001252005013100125NM 2005 1 31 QXEA200500089 120050108A5347 SEAT TRACK DHAV DHC8 DHC8102 2809003NM ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09369PH 513 PDX - RIGHT HAND CENTER SEAT TRACK NR 7 HAS PITTING AND GOUGES FROM FRAME 262.50 TO FRAME 214.400. REPAIRED IAW SRM 51-40-11. 2H72 4T RTA13NM 20050131001332005013100133NM 2005 1 31 UPS05443772 120050109A5210 WEB BOEING747 747123 1384873NM R3 DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C - R3 DOOR LOWER WEB CRACKED AT LOWER GATE PUSH ROD CUTOUT. LOWER WEB REPAIRED AS PER SRM 51-40-02 FIG 1. 2L74 4F A20WE 20050131001342005013100134NM 2005 1 31 UPS05443773 120050108A5313 STRINGER BOEING747 747123 1384873NM FUSLEAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C - BS 736 - 738, S23R STRINGER END FOUND CRACK. M/D BS 736 TO BS 738 S-23R STRINGER END REPAIRED AS PER RS 53-61-35230 AND ENGINEERING FILE NUMBER 747-53-20204. 2L74 4F A20WE 20050131001382005013100138NM 2005 1 31 UPS05443799 120050104A5312 BULKHEAD BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C, LEFT BLG WHEEL WELL AFT BULKHEAD STA 1480 APU DUCT PASSING HOLE CUTOUT SUSPECT CRACKED AT 10:30 POSITION AS MARKED. LEFT BS 1480 BULKHEAD WEB APU DUCT CUTOUT REPAIR CARRIED OUT AS PER EO B747-5310-C APPENDIX B FIG 4 AND DWG 144U2602. 2L74 4F A20WE 20050131001432005013100143NM 2005 1 31 UPS05443804 120050113A5313 STRINGER BOEING747 747123 1384873NM BS - CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C M/D BS 1580 TO BS 1600 AFT RT WINDOW FORGING REMOVED FOUND STRINGER CORROSION CRACKED. CORROSION BLEND OUT 0.100 X 1 X 10 EXCEED SRM LIMIT. STRINGER SEGMENT AND SPLICE ANGLE REWORKED REFER COMPONENT WORK PROCESS CARD SEQUENCE NR HE70480-1, -2, -3 FOR DETAILS. 2L74 4F A20WE 20050131001462005013100146WP 2005 1 31 UPS05843757 120050105A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01868UP 45968 INSPECTION TYPE:C3 LONGERON 14R CRACKED UNDER CLIP AT STA 1756. REMOVED DAMAGE SECTION OF L14R FROM APPROX STA 1745-1766. REMOVED SHEAR TIE, END FITTING TO FOM. FAB REPLACEMENT LONGERON SECTION FROM S1616757, 2 SPLICE STRAPS FROM SHT7075T6-.080, AND 1 SPLICE FITTING FROM S2645716. TREAT, PRIMED, AND INSTALLED ALL PARTS REF SRM 53-2-2, 51-1-8, 51-1-20D, 51-1-21. 2L74 4F RT4A25 20050131001482005013100148WP 2005 1 31 UPS05843760 120050111A5210 SKIN DOUG DC8 DC873F 302199FWP L1 DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01868UP 45968 INSPECTION TYPE:C3, L1 DOOR LOWER HINGE CUTOUT CRACKED ON FRAME. REMOVED LOCAL INTERCOSTAL & SEAL RETAINER TO FOM. STOP DRILLED CRACK & VERIFIED PER NDT/SPM06-10-01.001. FAB REPAIR DOUBLER FROM SHT 2024T3-0 -.071. INSTALLED ALL PARTS REF SRM 52-3-1 FIG 1, 51-1-8, 51-1-21, 51-3-0. 2L74 4F RT4A25 20050131001502005013100150WP 2005 1 31 UPS05843780 120050113A574074549374 FITTING DOUG DC8 DC871F 302199DWP RT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01701UP 45938 INSPECTION TYPE:C3 RT WING STA XW97 CANOE SUPPORT FITTING ATTACH BOLT HOLES CORRODED & GOUGED. REMOVED AND REPLACED FITTING REF SRM 51-3-2, 51-1-20D, 51-3-0, MM 20-16-00, 27-51-12. 2L74 4F RT4A25 20050131001512005013100151WP 2005 1 31 UPS05843781 120050113A57405804007509 FITTING DOUG DC8 DC871F 302199DWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01701UP 45938 INSPECTION TYPE:C3, CLIP CRACKED IN NR 1 ALT TANK AT NR 1 PYLON SKATE ANGLE BETWEEN STR 62 & 63 XRS508.997 LT WING INT. FAB REPLACEMENT CLIP PER DWG5804007 FROM BAR7075T6. DYE-PEN INSP PER DPS 4.707; NO CRACKS NOTED. REMOVED AND REPLACED FITTING REF SRM 51-1-20D, 51-1-15 , 51-1-8. LEAK CHECK C/W ON TC8000. 2L74 4F RT4A25 20050131001532005013100153WP 2005 1 31 UPS05843786 120050108A53403779762U501 FITTING DOUG DC8 DC871F 302199DWP MAIN CABIN CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01701UP 45938 INSPECTION TYPE:C1, LONGERON 8R END FITTING CRACKED AT STA 676. REMOVED AND REPLACED END FITTING IAW SRM 51-1-20D, 51-1-8. 2L74 4F RT4A25 20050131001552005013100155WP 2005 1 31 UPS05843788 120050107A5310REFDWG5597646 WEB DOUG DC8 DC871F 302199DWP L1 DOOR FRAME CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01701UP 45938 INSPECTION TYPE:C1, L1 DOOR FWD TORQUE WEB CRACKED BELOW SWITCH PANEL, NEAR L16L STA 25. STOP DRILLED CRACK AND NDT VERIFIED PER 53-2-0, NDT/SPM06-10-01.001. FAB REPAIR ANGLE FROM SHT7075T6-.063, TREAT, PRIME AND INSTALL SAME REF SRM 53-2-0, 51-1-8, 51-1-21, 51-1-20D, DWG5597646. 2L74 4F RT4A25 20050131001562005013100156WP 2005 1 31 UPS05843789 120050110A5310 WEB DOUG DC8 DC871F 302199DWP R1 DOOR FRAME CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01701UP 45938 INSPECTION TYPE:C1, R1 DOOR JAMB TORQUE WEB CRACKED ABOVE UPPER DOOR HINGE ARM STA 150- 155, NEXT TO L14R. CUT OUT DAMAGE, NDT VERIFIED REF NDT/SPM06-10-01.001. FAB DOUBLER FROM SHT2024T3-.050, TREAT, PRIME & INSTALLED SAME REF SRM 53-2-0 FIG 1F, 51-1-8, 51-1-21, 51-1-20D, DWG 5615700. 2L74 4F RT4A25 20050131001592005013100159NM 2005 1 31 AWXA200500081 120050127A33501012721 LIGHT BOEING737 737301 1384611NM SEAT ROW 12 LT INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28325AW 23260 PHX - EEL - DURING 8-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT INOPERATIVE AT SEAT ROW 12 LT. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 12 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050131001602005013100160EU 2005 1 31 AWXA200500082 120050112A5347ASNA2223 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28621AW 053 SAL - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON CABIN FLOOR SEAT TRACK Y765 BETWEEN FR 20 AND FR 23. MAINTENANCE REMOVED AND REPLACED SEAT TRACK Y765 FROM FR 20 TO FR 23 IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050131001632005013100163EU 2005 1 31 AWXA200500073 120050125A335032145410 EPSU AIRBUS320 A320231 3930325EU EMERGENCY LIGHT DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28626AW353093872 65 SEA - EEL - MX REPORTED LT AFT EPSU WAS FAULTING (INTERNAL LOAD) AND ASSOCIATED FLOOR PATHWAY LIGHTS DID NOT ILLUMINATE. MX REMOVED AND REPLACED THE AFT LT EMERGENCY POWER SUPPLY UNIT (13WL) IAW AWA TASKCARD R1C33303. OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050131001642005013100164EU 2005 1 31 AWXA200500074 120050124A335032145410 EPSU AIRBUS320 A320232 3930326EU ZONE 242 DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28642AW336477264 584 JFK - EEL - MX REPORTED EMERGENCY LIGHT TEST FAILED ON CIDS PANEL RT FAIL MESSAGE. MAINTENANCE REMOVED AND REPLACED RT OVERWING EMERGENCY POWER SUPPLY UNIT (12WL) IAW TASKCARD R1C33303, OPERATIONAL TEST GOOD. 2L72 4F RTA28NM 20050131001652005013100165NM 2005 1 31 AWXA200500075 120050125A335032145410 EPSU AIRBUSA319 A319132 3930340NM ZONES 241 & 242 DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28807AW203596 1064 DURING 8-DAY CHECK FOUND LT OVERWING EMERGENCY POWER SUPPLY UNIT (EPSU) INOPERATIVE. MX REMOVED AND REPLACED BOTH THE LT & RT OVERWING EPSU'S IAW T/C R1C33303. OPERATIONAL CHECK OF EMERGENCY LIGHTING WAS GOOD. 2L72 4F RTA28NM 20050131001662005013100166NM 2005 1 31 AWXA200500076 120050125A3397BMS13311122 WIRE BOEING757 7572S7 1384962NM SEAT ROW 7 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28901AW 23321 PHX - EEL - DURING A-06 CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 7 LT INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 7 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20050131001692005013100169EU 2005 1 31 AWXA200500086 120050111A5315D53472800 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28621AW 053 SAL - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM -Y1292 BETWEEN FR 66 AND FR 68. MAINTENANCE REMOVED CORRODED FLOORBEAM -Y1292 FROM FR 66 TO FR 68; FABRICATED A NEW REPLACEMENT FLOORBEAM PER DWG D53472800; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050131001702005013100170EU 2005 1 31 AWXA200500087 120050112A5347D5337111000000 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28621AW 053 SAL - MAJOR REPAIR - DURING C-04 CHECK INTERGRANULAR CORROSION WAS FOUND ON LT INBOARD SEAT TRACK BETWEEN FR 42 AND FR 44. MAINTENANCE REMOVED CORRODED LT INBOARD SEAT TRACK FROM FR 42 TO FR 44; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050131001782005013100178NM 2005 1 31 QXEA200500133 120050122A5753 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09410QX 4053 PDX - LEFT HAND WING OUTBOARD FLAP UPPER SKIN HAS CHAFE MARKS AT WS YW 211 AND YW 240. REPAIRED IAW Q400 SRM 51-25-05-370-801 AND HORIZON AIR EA 6-57-89A. 2H72 4T RTA13NM 20050131001792005013100179NM 2005 1 31 QXEA200500135 120050119A5730 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09410QX 4053 PDX - 523AT COUNTERSINKS HAVE FRETTING CORROSION. REPLACED PANEL 857/3043-003. 2H72 4T RTA13NM 20050131001822005013100182NM 2005 1 31 QXEA200500138 120050124A5312 PRESSURE PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09410QX 4053 PDX - DOME NUT PLATES HAS A HOLE IN IT, PRESSURE PANEL 122BR. REPAIRED IAW DHC-8-200 SRM 51-42-05, SRM 51-23-00 AND AMM TASK 51-21-01-340-801. 2H72 4T RTA13NM 20050131001832005013100183NM 2005 1 31 QXEA200500124 120050117A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 130 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09410QX 4053 PDX - LEFT HAND INBOARD SEAT TRACK HAS SCRATCH MARKS AND CORROSION INSIDE CHANNEL, 15 INCHES LONG AREA AT FUSELAGE STATION 90.00. REPAIRED IAW SRM 51-40-15. 2H72 4T RTA13NM 20050131001842005013100184NM 2005 1 31 SWAA050217 120050126A3350101331 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED C4 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM. 2L72 4F RTA16WE 20050131001862005013100186NM 2005 1 31 QXEA200500127 120050117A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09410QX 4053 PDX - RIGHT INBOARD SEAT TRACK CORROSION APPROXIMATELY X40.00. REPLACED IAW SRM 51-40-15 AND 51-42-05-330-801. 2H72 4T RTA13NM 20050131001892005013100189NM 2005 1 31 QXEA200500131 120050117A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09410QX 4053 PDX - CORROSION AROUND RIVETS ON LEFT HAND FORWARD INBOARD SEAT TRACK OUTER FLANGE FROM X19.4 TO X1.0. REPLACED IAW SRM 51-42-05-330-801. 2H72 4T RTA13NM 20050131001902005013100190NM 2005 1 31 SWAA050218 120050126A53116546546 FRAME BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29680AA 23505 DURING SPV FOUND BELT FRAME AT BS 908, STRINGER 4R, CRACKED. REPAIRED BELT FRAME PER SRM. 2L72 4F RTA16WE 20050131001912005013100191NM 2005 1 31 SWAA050219 120050126A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 767, STRINGER 24R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050131001922005013100192NM 2005 1 31 SWAA050220 120050126A57536546434351 SKIN BOEING737 7375H4 138449DNM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29526SW 26568 DURING SCHEDULED C1 CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED LT WING T/E AFT FLAP PER MM. 2L72 4F RTA16WE 20050131001932005013100193NM 2005 1 31 SWAA050221 120050126A555265C25796 TAB BOEING737 7375H4 138449DNM LT ELEVATOR FAILED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29526SW 26568 DURING SCHEDULED C1 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR TAB PER MM. 2L72 4F RTA16WE 20050131001942005013100194NM 2005 1 31 SWAA050229 120050127A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29349SW 24408 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 792, STRINGER 17L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20050131001962005013100196NM 2005 1 31 SWAA050231 120050127A53406551698 SPLICE BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29680AA 23505 DURING SPV, FOUND STRINGER SPLICE AT BS 908, STRINGER 4R, CRACKED. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20050131001982005013100198NM 2005 1 31 SWAA050233 120050127A57536546434301 SKIN BOEING737 7375H4 138449DNM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29502SW 24179 DURING SCHEDULED C1 CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED LT WING T/E AFT FLAP PER MM. 2L72 4F RTA16WE 20050131002032005013100203NM 2005 1 31 SWAA050238 120050127A53116546529 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29602SW 27953 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 400, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20050131002052005013100205NM 2005 1 31 SWAA050240 120050127A53116546550 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29602SW 27953 DURING SCHEDULED D-CHECK, FOUND 3 EACH FRAMES CRACKED BETWEEN BS 827 AND BS 907, STRINGER 8L. REMOVED AND REPLACED FRAME SECTIONS PER SRM. 2L72 4F RTA16WE 20050201000042005020100004SO 2005 2 1 UG82005F00001 120050112A32311159WH504107 DOOR GULSTMGV GULFSTREAMGV3980116SO RROYCEBR700 BR700710A110 NE LT MLG BINDING E UG8AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL235102 551 WHEN LANDING GEAR WAS RETRACTED AFTER TAKEOFF, THE LT MLG DOOR REMAINED OPEN. LANDING GEAR WAS CYCLED IAW AFM. THE DOOR WOULD CLOSE WITH THE GEAR SELECTED DOWN BUT WOULD REMAIN OPEN WITH IT SELECTED UP. LT WHEEL WELL, DOOR, UPLOCK, LINKAGE AND PLUMBING WERE INSPECTED FOR DAMAGE, NO DAMAGE FOUND. LANDING GEAR SWING IDENTIFIED LT LANDING GEAR FAIRING DOOR TO WING SKIN GAP TO BE INSUFFICIENT AND CAUSING IB DOOR TO NOT SEQUENCE CLOSED. MLG DOOR CLEARANCE PROVIDED IAW MM. LANDING GEAR OPS CHECKS IAW MM ARE GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (CNTL NR: GM 05-001) (K) 2L72 4F4 FRTA12EA E00057EN 20050201000482005020100048WP 2005 2 1 ASMF200501004 120050107A57545922532502 SKIN DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE NR 2 SLAT DAMAGED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23205AM 49405 DURING TRANSIT CHECK WERE DETECTED FUEL PANEL AND SLAT NR 2 DAMAGED. INSPECTION WAS PERFORMED AND DAMAGES WERE DETECTED OUT OF LIMITS, THEREFORE AIRCRAFT WAS SENT TO THE HANGAR. SLAT NR 2 AND FUEL PANEL WERE REPLACED IAW MM 27-80-01 AND 57-30-03, RESPECTIVELY, TESTED CORRECT. 2L72 4F4 FRTA6WE E9NE 20050201001152005020100115 2005 2 1 VW3R20050002 420050128A2565700129013 GAUGE BFGOODRICH DOUG MD88 MD88 3023688NM SLIDE BOTTLE STUCK B VW3RK NONE O OTHER ININSP/MAINT 1 WP09 PW0266 AFTER OVERHAULING THE PRESSURE REGULATOR USED ON THE EVACUATION SLIDE INFLATION SYSTEM, DURING THE CHARGING PROCESS THE GAUGE STAYED AT 3000 PSI AFTER THE PRESSURE WAS RELEASED. THE GAUGE WAS REMOVED FROM SERVICE. 2L72 4F RTA6WE 20050127001852005012700185NM 2005 1 27 05FDEA00139 120050121A5753ARC25122 HINGE DOUG DC10 DC10 N/A-SDRNM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25395FE 46629 RIGHT WING INBOARD FLAP HINGE INBOARD PIVOT BUSHING GALLED AND PITTED. MEASURED BORE DIAMATER, FOUND TO BE OUT OF LIMITS IAW DAC CMM 57-52-01. ALODINE AND PRIMED BORE IAW DC10-10 SRM 51-21-01 VOL 2, FABRICATED, INSTALLED AND HONED BUSHING TO A FINAL INSIDE DIAMETER OF .9995-1.0005 IAW DAC CMM 57-52-01 AND FEDEX EA 8-5750-83955, RIGHT HAND INBOARD FLAP, OUTBOARD HINGE BRACKET OVERSIZE PIVOT BORE- REPAIR, REFERENCE NON-ROUTINE N00386. 2L73 4F RTA22WE 20050127001872005012700187WP 2005 1 27 ABXA050017 120050106A52303926046503 FITTING DOUG DC9 DC941 302207NWP FWD CARGO CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23970AX 47494 UPPER AFT STOP TEE FITTING CRACKED FORWARD LOWER CARGO DOOR. REPLACED FITTING IAW DC-9 SRM 51-30-1, 51-30-2 AND 51-30-4. 2L72 4F A6WE 20050127001892005012700189WP 2005 1 27 ABXA050018 120050106A53119919617502 FRAME DOUG DC9 DC941 302207NWP CABIN CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23970AX 47494 FORWARD OVER WHEEL WELL FRAME RIGHT SIDE, REQUIRED REPLACEMENT PER JC NEA 53400100-002-40, FRAME CRACKED FORWARD AND AFT FLANGE. REMOVED AND RE-INSTALLED NEW FRAME AT STA 737 IAW EA 53400 322-001-3. 2L72 4F A6WE 20050127001912005012700191WP 2005 1 27 ABXA050016 120050105A551059109629 SUPPORT DOUG DC9 DC941 302207NWP HORZONTAL STAB DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23970AX 47494 HORIZONTAL STAB JACKSCREW HAD DAMAGED THREAD NEAR THE SELF-LOCKING LOWER STOP NUT. REPLACED JACKSCREW IAW DC-9 MM. 2L72 4F A6WE 20050127001932005012700193WP 2005 1 27 ABXA050021 120050107A5320591015845 PAN DOUG DC9 DC941 302207NWP AFT CARGO DOOR CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23970AX 47494 AFT LOWER CARGO DOOR CUTOUT LOWER PAN CORRODED AND FORWARD LOWER CORNER OF PAN BULGED WITH 3 RIVETS THROUGH THE SKIN POPPED. REMOVED DOOR PAN / SCUFF PLATE / WEB. REMOVED AND REPLACED -45 DOUBLER. CLEANED CORROSION ON DOOR PAN AND RE-INSTALLED DOOR PAN / WEB / SCUFF PLATE IAW DC-9 SRM 51-10-3, 51-30-1, 51-30-5 AND 51-30-2. 2L72 4F A6WE 20050127001982005012700198NM 2005 1 27 QXEA200500106 120050119A5270401020101 SENSOR BOMBDRDHC8 DHC8401 1390041NM MAIN CABIN DOOR BROKEN A QXEAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 NM09416QX2828 4083 SEA - THE FLIGHT RETURNED TO GATE AFTER THE CREW RECEIVED A FUSELAGE DOOR WARNING LIGHT. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE FORWARD PASSENGER DOOR CLOSED SENSOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050128000062005012800006EU 2005 1 28 XN0A1222 120050108A2710 TENSIONER AIRBUS300 A300B4203 3930306EU AILERONS LACK OF LUBE A XN0AD RETURN TO BLOCK W INADEQUATE Q C TXTAXI/GRND HDL 1 GL23224KW 073 DURING FLIGHT CONTROL CHECK LINE FOUND AILERONS TO FEEL STIFF. LUBED AILERON TENSIONER AND INPUT ROADS. OPS CHECKED NORMAL ON GROUND IAW 27-10-00. 2L72 4F RTA35EU 20050128000122005012800012EA 2005 1 28 COMA0560079 120050122A3230 DRAG BRACE CNDAIRCL600 CL6002B19 1900309EA MLG LACK OF LUBE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01933CA 7040 FLIGHT 5466 GEAR DISAGREE WARNING. NLG DID NOT RETRACT. CLEANED AND LUBED NLG DRAG BRACE. RETRACTION CHECKS WERE SATISFACTORY. 2L72 4F RTA21EA 20050128000182005012800018NM 2005 1 28 05FDEA00165 120050125A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 CABIN SEAT TRACK DAMAGED AT STA Y = 1372, X = 48. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE 1, VOLUME I. 2L73 4F RTA22WE 20050128000232005012800023NM 2005 1 28 757BJ0012 120050117A5313 STRINGER BOEING757 757236 1384971NM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05757BJ 22176 CORROSION IN STRINGER 29 (BL 0) FROM BS 418 TO BS 426.5. REPLACED SECTION OF STRINGER PER SRM 51-10-00 AND BOEING DRAWING 141N3270. 2L72 4F RTA2NM 20050128000332005012800033NM 2005 1 28 05FDEA00146 120050122A53156089318 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25480FE 21462 STA 340, FLOORBEAM HAS DENT & CORROSION IN DIFFERENT AREAS. REMOVED DAMAGED AREA & REPAIR PARTS IAW SRM 51-30-2. FABRICATED NEW T-CAP FROM 60- 893/18 BATCH 833835 & REPAIR SPLICES FROM 60-3408/18 BATCH 812526 & 7075-T6 .063C BATCH 784273 IAW SR 27-53-007. INSTALLED REPAIR PARTS, SPLICES & T-CAP IAW SR 27-53-007. 2L73 4F RTA3WE 20050128000452005012800045EA 2005 1 28 QXEA200500120 120050124A2150GG670950103 CONTROL VALVE CNDAIRCL600 CL6002C10 1390015EA ZONE 200 FAILED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09605QX7569 10022 FLT RETURNED TO THE GATE WHEN DURING THE TAXI OUT THE CREW RECEIVED A RT PACK MASTER CAUTION. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE RT PACK TEMPERATURE CONTROL VALVE. OPERATIONAL AND LEAK CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20050128000472005012800047EA 2005 1 28 05020676 120050120A2740 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB TRIM FAILED A VTZAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA27676BR 7644 EVENT SUMMARY STATED STAB TRIM FAILURE. PERFORMED BITE AND OPS CHECK OF HSTCU AND FUNCTION CHECK OF HSTA. OPS CHECK GOOD. 2L72 4F RTA21EA 20050128000492005012800049EA 2005 1 28 05021649 120050121A2760 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA SPOILERS ILLUMINATED A VTZAB EMER. DESCENT J WARNING INDICATION APAPPROACH 1 EA27649BR 7414 EVENT SUMMARY STATED SPOILER FAULT MESSAGE. FLAPS 20 LANDING. EMERGENCY DECLARED. CYCLED POWER AND PERFORMED BITE CHECK ON SECU'S, OPS CHECK GOOD. 2L72 4F RTA21EA 20050128000522005012800052CE 2005 1 28 DXTA200500527 120050110A3260SG006 DOWNLOCK SWITCH CESSNA750 750 2076810CE MLG FAILED E DXTAO OTHER J WARNING INDICATION CLCLIMB 1 GL07996QS 7500196 ON TAKEOFF NOSE GEAR CAME UP NORMAL, THROUGHT 10,000 FT NOTICED NOSE GEAR INDICATED DOWN. LIGHT WAS INTERMITTANT DURING FLIGHT. BLEW GEAR DOWN. UNSAFE LIGHT CAME ON FOR ABOUT 10 SECONDS, THEN WENT OUT. INSPECTED NLG DOWNLOCK SWITCH SG006 AND CONNECTOR PG006. ALSO INSPECTED AND RE-SEATED LANDING GEAR LOGIC MODULE NC002, FOUND NO DEFECTS. PERFORMED LANDING GEAR OPERATIONAL TEST REF 750 M/M 32-00-01. LANDING GEAR OPERATES NORMAL. 2L72 4J RTT00007WI 20050128000632005012800063NM 2005 1 28 UPS05243741 120050126A3510 BOTTLE BOEING727 72725C 138400HNM COCKPIT OXYGEN EMPTY A IPXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01947UP 19722 OXYGEN BOTTLE EMPTIED DURING FLIGHT. REPLACED CREW OXYGEN BOTTLE. PERFORMED LEAK TEST. NO LEAKS NOTED. 2L73 4F A3WE 20050128000652005012800065NM 2005 1 28 UPS05443712 120050108A5311 FRAME BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C - BS 740, BETWEEN S7 - 8R, FRAME FOUND CRACK. M/D BS 740 BETWEEN STR 7R AND STR 8R FRAME REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 54. 2L74 4F A20WE 20050128000942005012800094NM 2005 1 28 QXEA200500095 120050108A5347 SEAT TRACK DHAV DHC8 DHC8102 2809003NM ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09369PH 513 PDX - LEFT HAND CENTER SEAT TRACK NR 4 HAS GOUGES AT FRAME 313 AND 330. REPAIRED IAW SRM 51-40-11. 2H72 4T RTA13NM 20050128001112005012800111WP 2005 1 28 DHL2005801002 120050126A2612 FIRE WARNING DOUG DC8 DC873F 302199FWP NR 2 ENGINE ACTIVATED A DHLAFD ACTIVATE FIRE EXT. RETURN TO BLOCK A FLAME/FIRE TXTAXI/GRND HDL 1 SO01801DH 46033 NR 2 ENGINE FIRE WARNING, THE CREW BLEW BOTH FIRE BOTTLES. AFTER STARTING ENG DURING PUSHBACK--HAD ENG NR 2 FIRE WARNING.COMPLETED EMER. CHECK LIST. FIRED BOTH BOTTLES--FIRE WARNING LIGHT AND BELL CONTINUED TO ACTUATE AFTER SHUTDOWN. R/R NR 2 ENG RT CORE FIRE DET. LOOP ASSY PER DC-8 M/M 26-10-1 NO HELP.T/S DOWN TO CONN. P1-7007 (NR 2 ENG LT CORE TO PYLON CONN) R/R CONN. PER DC-8 MM 20-50-1. RAN ENG PER JRH 12.2 OPS CHECKS SERVICABLE. 2L74 4F RT4A25 20050128001192005012800119SO 2005 1 28 RAIA00501047 120050122A7830 WARNING LIGHT EMB 145 EMB145LR 3260212SO THRUST REVERSER ILLUMINATED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03817HK 145058 STL - NR 1 ENGINE DISAGREE MESSAGE ON EICAS ON TAKEOFF. MAINTENANCE DEFERRED THRUST REV PER MEL 78-30-00 CAT C. PERFORMED OPS CHECK ON NR 1 ENGINE THRUST REVERSE, OPS CHECK GOOD. 2L72 4T RTT00011AT 20050128001232005012800123NM 2005 1 28 05FDEA00175 120050126A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25235FE 21329 BS 1030, STR 25R FRAME IS DENTED. REPAIRED PER SRM 51-40-3. 2L73 4F RTA3WE 20050128001242005012800124NM 2005 1 28 QXEA200500112 120050119A243011521086 GCU BOMBDRDHC8 DHC8401 1390041NM ZONE 100 INOPERATIVE A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09414QX7551 6446 4061 PDX - FLIGHT 2575 - NR 2 DC GENERATOR CAUTION LIGHT CAME ON. MAINTENANCE REMOVED AND REPLACED NR 2 DC GENERATOR GCU. GROUND RAN. OPERATIONAL CHECKS NORMAL. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050202000012005020200001NM 2005 2 2 SB05018 120050128A2761 O-RING BOEING737 7373B7 1384580NM NR 6 SPOILER ACTDAMAGED A USAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA19391US 23313 CLT - FLT556 - DURING CRUISE, ENROUTE FROM TPA TO DCA, CREW REPORTED LOSING SYSTEM B HYDRAULIC FLUID. FLIGHT DIVERTED TO CLT AND LANDED WITH A HYDRAULIC QUANTITY READING OF 1/4. THE B SYSTEM ENGINE DRIVEN PUMP LIGHT ALSO ILLUMINATED ON LANDING AND WAS ON FOR APPROXIMATELY 10 MINUTES. FLIGHT TAXIED TO THE GATE UNDER OWN POWER. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE RIGHT WING NR 6 FLIGHT SPOILER ACTUATOR LEAKING HYDRAULIC FLUID FROM DAMAGED O-RING ON CHECK VALVE. REMOVED AND REPLACED O-RING. OPERATIONAL CHECK AND LEAK CHECK GOOD. RESERVICED HYDRAULIC FLUID. 2L72 4F RTA16WE 20050202000022005020200002EU 2005 2 2 SA05008 120050120A3350321431 EPSU AIRBUSA321 A321211 3930370EU EMERGENCY LIGHT DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19162UW 1412 DCA - THE EMERGENCY LIGHT SYSTEM FAILED THE SYSTEM TEST. MAINTENANCE REPLACED THE FORWARD EMERGENCY POWER SUPPLY UNIT BATTERY. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20050202000042005020200004EU 2005 2 2 BA05001 120050121A3350321431 BATTERY AIRBUS330 A330323 3930335EU DOOR 3L DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW 337 PHL - FOUND BATTERY AT DOOR 3L FAULTING DURING TEST (15WL). MAINTENANCE REPLACED THE BATTERY. 2L72 4F RTA46NM 20050202000052005020200005EU 2005 2 2 SA05010 120050127A5610 WINDSHIELD AIRBUSA319 A319112 3930323EU COCKPIT CRACKED A USAAH DEACTIVATE SYST/CIRCUITS O OTHER DEDESCENT 1 EA19703UW 904 CLT - FLT 1140 EN-ROUTE BZE - CLT. THE CAPTAIN'S OUTER WINDSHIELD PANE CRACKED AT 11,000 FT. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE CAPTAIN'S WINDSHIELD. WINDSHIELD ANTI-ICE OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20050202000062005020200006EU 2005 2 2 AALA20050041 120050121A2841 INDICATOR AIRBUS300 A300B4605R 3930308EU FUEL QTY INOPERATIVE A AALAA UNSCHED LANDING P NO WARNING INDICATION CRCRUISE 1 SW2114068 511 EN ROUTE JFK-STI 30 MINUTES INTO FLIGHT LEFT HAND OUTER FUEL TANK QUANTITY AT 4300. RIGHT OUTER 8100 AND BOTH INNERS AT APPROXIMATELY 14000. FUEL USED WAS THE SAME FOR BOTH ENGINES. RETURNED JFK AND LANDED WITHOUT INCIDENT WITH LEFT HAND OUTER QUANTITY FULL 8200. SUMPED WATER OUT OF LEFT OUTER FUEL TANK. TANK QUANTITY READS NORMAL. FUEL QUANTITY INDICATING NO HARD FAULTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20050202000092005020200009NE 2005 2 2 AALA20050044 220050123A7200 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE RIGHT DAMAGED A AALAA UNSCHED LANDING C F.O.D. CLCLIMB 1 SW21505AA 49799 718470 EN ROUTE PHL-DFW, COMPRESSOR STALL ON RIGHT ENGINE AFTER TAKEOFF. POWER WAS REDUCED AND STALLS CLEARED. ALL ENGINE INDICATIONS REMAINED IN NORMAL RANGE. RIGHT ENGINE KEPT RUNNING FOR APPROACH. LANDED PHL WITHOUT INCIDENT. REPLACED NUMBER 2 ENGINE DUE TO FOD DAMAGE INCURRED OVERTEMP. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 F A6WE E9NE 20050202000122005020200012WP 2005 2 2 AALA20050045 120050119A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21445AA 49471 DFW - EMERGENCY LIGHTS IN CEILING ABOVE ROWS 15 THROUGH 20 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN CEILING ABOVE ROWS 15 THROUGH 20. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050202000162005020200016WP 2005 2 2 AALA20050047 120050124A3230 RETRACT CYLINDER DOUG DC9 DC982 3022082WP NLG INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW217519A 49896 AFTER TAKEOFF, NOSE GEAR FAILED TO RETRACT. FLEW EXTENDED DOWN WIND TO BURN FUEL. LANDED AT MIA WITHOUT INCIDENT. REPLACED NOSE GEAR INNER CYLINDER. ACCOMPLISHED NOSE LANDING AND DOORS CHECK. CHECK FLIGHT COMPLETED. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050202000712005020200071EU 2005 2 2 AALA20050046 120050121A3246 WHEEL AIRBUS300 A300B4605R 3930308EU NLG INOPERATIVE A AALAO OTHER O OTHER APAPPROACH 1 SW2134078 615 UNABLE TO EXTEND NOSE WHELL ON FINAL APPROACH. USED GRAVITY EXTENSION AND NOSE GEAR LOWERED. LANDED BOS WITHOUT INCIDENT AND AIRCRAFT TOWED TO GATE DUE TO LOSS OF NOSE WHEEL STEERING. PULLED CVR CIRCUIT BREAKER. CLOSED NOSE WHEEL DOORS TO ACTIVATE SEQUENCE VALVE FOR STEERING TO RETURN. NO VISUAL DISCREPANCIES NOTED. AIRCRAFT IS BEING FERRIED TO JFK FOR FURTHER TROUBLE SHOOTING. 2L72 4F RTA35EU 20050202000772005020200077NM 2005 2 2 AALA20050056 120050126A3350 SOCKET BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21606AA 27057 LAS - EMERGENCY LIGHTS FROM ROW 16 TO 25 AND FOUR EXIT SIGNS AT OVERWING HATCH INOPERATIVE IN TEST MODE. AIRCRAFT FERRIED TO DFW FOR EVALUATION. FOUND LIGHT SOCKET AT FORWARD SEAT 16 SHORTED. REPLACED LIGHT SOCKET AND BATTERY PACK FOR EMERGENCY LIGHTS FROM ROW 16 TO 25 AND FOUR EXIT SIGNS AT OVERWING HATCH. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050203000012005020300001EA 2005 2 3 COMA0560092 120050124A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01976CA 7151 FLIGHT 5106 FLAPS FAILED WHEN SELECTED TO 20 DEGREES. INSPECTED FLAP SYSTEM PER AD 98-20-01, NO DEFECTS FOUND. 2L72 4F RTA21EA 20050203000052005020300005WP 2005 2 3 05FDEA00197 120050129A5754NRB62351 SKIN DOUG MD10 MD1010F 3022112WP NR 7 SLAT DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25363FE 48263 COMPLY WITH EA 8-5710-55426 WINGS - BASIC, LT, LEADING EDGE NR 7 SLAT SKIN REPAIR AT XOS=947.65. COMPLIED WITH EA 8-5710-55426. 2L73 4F RTA22WE 20050203000082005020300008NM 2005 2 3 QXEA200500141 120050127A3350VS4551 RELAY DHAV DHC8 DHC8202 2809007NM ZONE 100 INOPERATIVE A QXEAO OTHER O OTHER CRCRUISE 1 NM09374PH 528 PDX - EMERGENCY LIGHTS STAYED ON DURING THE ENTIRE FLIGHT. MAINTENANCE REMOVED AND REPLACED 2431 K6 RELAY IN DC CONTACTOR BOX. CYCLED GROUND POWER AND VERIFIED OPERATION OF RELAY AND OPERATION OF THE EMERGENCY LIGHTS. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050203000092005020300009NM 2005 2 3 SWAA050249 120050130A53106546569 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29602SW 27953 DURING SCHEDULED D-CHECK, FOUND AFT CARGO COMPARTMENT SHEAR TIE AT BS 1006, LBL 1, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050203000102005020300010NM 2005 2 3 SWAA050250 120050130A53116546550 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29602SW 27953 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 787, STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20050203000112005020300011NM 2005 2 3 SWAA050251 120050130A53116546548 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29602SW 27953 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 767, BETWEEN RBL 8 AND RBL 12, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20050203000132005020300013 2005 2 3 SWAA050253 420050128A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29713SW 27847 DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050203000142005020300014NM 2005 2 3 SWAA050254 120050129A57536546435336 SKIN BOEING737 7373H4 1384600NM RT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29378SW 26585 DURING SCHEDULED C2 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RT WING OUTBOARD T/E AFT FLAP PER MM. 2L72 4F RTA16WE 20050203000152005020300015NM 2005 2 3 SWAA050255 120050129A33501619 LIGHT BOEING737 7377H4 1384404NM RT OVERWING INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29497WN 32479 DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050203000162005020300016NM 2005 2 3 SWAA050256 120050130A3350D71702001 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29755SA 27871 DURING SCHEDULED MV2 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM. 2L72 4F RTA16WE 20050203000182005020300018SO 2005 2 3 SWIA200514442 120050124A27523431001001 ACTUATOR EMB 120 EMB120ER 3260203SO NACELLE FLAP MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07271YV9905 9188 120271 FLAPS NACELLE DISAGREEMENT. REPLACED LEFT NACELLE ACTUATOR PER MM 27-50-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050203000192005020300019EA 2005 2 3 COMA0560084 120050124A5712 RIB CNDAIRCL600 CL6002B19 1900309EA LT PYLON CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01978CA 7158 LEFT HAND PYLON LOWER RIB AT FS 605.00 CRACKED. REPAIRED IAW REO 601R-54-61-038. 2L72 4F RTA21EA 20050203000212005020300021EA 2005 2 3 COMA0560083 120050124A5210 STRUCTURE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01978CA 7158 TWO CRACKS FOUND BETWEEN PAX FS 320.00 AND 329.00 AT DATUM ONE. REPAIRED IAW REO 601R-52-11-638 AND 601R-52-11-643. 2L72 4F RTA21EA 20050203000242005020300024NM 2005 2 3 SWAA050261 120050130A53116546569 SHEAR TIE BOEING737 7373K2 13844BANM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29340LV 23738 DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE AT BS 947.5, STRINGER 27L, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050203000252005020300025NM 2005 2 3 SWAA050262 120050130A53106546569 SHEAR TIE BOEING737 7373K2 13844BANM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29340LV 23738 DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE AT BS 967, STRINGER 24R, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050203000272005020300027NM 2005 2 3 SWAA050269 120050201A531165C22908 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29602SW 27953 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 500B, BETWEEN STRINGERS 27L AND 28R, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20050203000282005020300028EA 2005 2 3 COMA0560082 120050125A32304622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG FAULTY A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01914CA1708 7012 FLIGHT 5721 DURING APPROACH RECEIVED A NLG DISAGREE WARNING. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED THE NLG PRIORITY VALVE. 2L72 4F RTA21EA 20050203000312005020300031EA 2005 2 3 COMA0560081 120050125A3260 UPLOCK TARGET CNDAIRCL600 CL6002B19 1900309EA MLG OUT OF ADJUST A COMAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 SO01995CA 7229 FLIGHT 5146 DURING APPROACH RECEIVED A GEAR DISAGREE WARNING. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. ADJUSTED THE NLG LANDING GEAR UPLOCK TARGET GAP. 2L72 4F RTA21EA 20050203000342005020300034SO 2005 2 3 SWIA200514457 120050128A2731 ACTUATOR EMB 120 EMB120ER 3260203SO ELEVATOR TRIM INOPERATIVE A SWIAD RETURN TO BLOCK F FLT CONT AFFECTED CRCRUISE 1 NM07294SW 120321 UPON LEVEL OFF AT 250 ELEVATOR TRIM WHEEL WOULD NOT ROLL FORWARD. REMOVED AND REPLACED BOTH ELEVATOR TRIM ACTUATORS IAW 27-32-02. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050203000362005020300036EA 2005 2 3 SWIA200514459 120050127A3397 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07908SW 7540 LOWER EMERGENCY EXIT SIGN ON RIGHT OVERWING EXIT DOES NOT ILLUMINATE. REPAIRED CONNECTOR AT RIGHT OVERWING EXIT LIGHT. OPERATIONAL CHECKED GOOD. 2L72 4F RTA21EA 20050203000402005020300040SO 2005 2 3 SWIA200514432 120050124A5210 MECHANISM EMB 120 EMB120ER 3260203SO PAX DOOR DIRTY A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07215SW 120281 MAIN CABIN DOOR HARD TO OPEN. CHECKED DOOR, CLEANED AND LUBED ROLLERS, LUBED HANDLE, OPERATIONAL CHECK SATISFACTORY. 2L72 4T RTA31SO 20050203000412005020300041EA 2005 2 3 SWIA200514433 120050124A27604916420 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07963SW 7865 OUTBOARD GROUND SPOILER STATUS AND FLIGHT SPOILER MESSAGE ON GROUND. REPLACED NR 1 SECU. OPERATIONAL CHECK GOOD REF CRJ MM CHAP 27-60-00. 2L72 4F RTA21EA 20050203000422005020300042EA 2005 2 3 SWIA200514443 120050123A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07917SW 7641 EMERGENCY LIGHT OVER ROW 2 INOPERATIVE. RELAMPED EMERGENCY LIGHT BULB OVER ROW 2. OPERATIONAL CHECKS GOOD. 2L72 4F RTA21EA 20050203000442005020300044SO 2005 2 3 SWIA200514445 120050125A3397 WIRE EMB 120 EMB120ER 3260203SO EMEGENCY LIGHT DAMAGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07560SW 120334 FORWARD FLOOR EMERGENCY LIGHTS INOPERATIVE (FIRST 4 LIGHTS). REPAIRED MAIN POWER WIRE. REPLACED FUSE. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050203000472005020300047 2005 2 3 SWAA050271 420050201A2565D31354 SLIDE BOEING737 7373Q8 1384670NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29685SW 23401 DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. REMOVED AND REPLACED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050203000562005020300056SO 2005 2 3 RAIA00501054 120050125A36108583C000002 PRECOOLER EMB 145 EMB145ER 3260211SO NR 2 ENGINE FAILED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03808HK12473 145157 PIT- NR 2 BLEED OVERTEMP UPON ENTERING ICING CONDITIONS. MAINTENANCE REMOVED AND REPLACED NR 2 PRECOOLER. 2L72 4F RTT00011AT 20050203000572005020300057EU 2005 2 3 RAIA00501055 120050126A30406249922 CONTROLLER AEROSPATR42 ATR42300 8680920EU WINDSHIELD HEAT MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03426TE162 228 STL - F/O WINDSHIELD HEAT INOP IN ICING CONDITIONS. MAINTENANCE REMOVED AND REPLACED RIGHT SIDE WINDSHIELD HEAT CONTROLLER. 2H72 4T RTA53EU 20050203000582005020300058SO 2005 2 3 RAIA00501056 120050124A36108166101 VALVE EMB 145 EMB145ER 3260211SO BLEED SYSTEM FAILED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03808HK12473 145157 PIT - NR 1 AND NR 2 BLEED OVERTEMP DURING CLIMB IN ICING CONDITIONS. MAINTENANCE REMOVED AND REPLACED FAN AIR VALVES. 2L72 4F RTT00011AT 20050203000592005020300059EU 2005 2 3 RAIA00501057 120050126A24348260121 GENERATOR AEROSPATR42 ATR42300 8680920EU NR 2 FAILED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03426TE21090835 228 STL - NR 2 DC GENERATOR FAULTED AFTER ENGINE START. MAINTENANCE REMOVED AND REPLACED NR 2 GENERATOR. 2H72 4T RTA53EU 20050203000602005020300060EU 2005 2 3 RAIA00501058 120050127A7921SYLC522454 ACTUATOR JETAIRJETSTMJETSTM4101 1500501EU OIL COOLER DOOR MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03572HK3027 41091 BWI - LEFT OIL COOLER FLAP STUCK IN THE OPEN POSITION IN AIR. MAINTENANCE REMOVED AND REPLACED LEFT OIL FLAP ACTUATOR. 2L72 4T RTA41NM 20050203000612005020300061SO 2005 2 3 RAIA00501059 120050130A324015851 PRESSURE SWITCH EMB 145 EMB145LR 3260212SO EMERGENCY BRAKE FAILED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03818HK5229 145059 STL - NO TAKEOFF CONFIGURATION, EICAS MESSAGE. MAINTENANCE REMOVED AND REPLACED EMERGENCY PARKING BRAKE PRESSURE SWITCH. 2L72 4T RTT00011AT 20050203000692005020300069WP 2005 2 3 DHL2004809515 120050105A53403750257U1 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SO01809DH91189 46047 FWD CARGO COMPT SPLICE FITTING CRACKED 3.000, STA 600.000 TO STA 620.000 L-31L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW SPLICE FITTING IAW SRM 51-1-20D PG 9, SRM 51-3-0 PG 1, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050128000812005012800081 2005 1 28 HNAA0500002 420050114A344236144758600 RADAR DHAV DHC8 DHC8102 2809003NM WX SYSTEM INOPERATIVE A HNAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA07827EX 390 WEATHER RADAR SPIKING ON CLIMOUT, TURNS AND ON DESCENT. THE SCREEN GOES BLANK OCCASIONALLY. REMOVED AND REPLACED WEATHER RADAR RT, OPS CHECK GOOD. 2H72 4T RTA13NM 20050128000932005012800093NM 2005 1 28 QXEA200500088 120050108A5347 SEAT TRACK DHAV DHC8 DHC8102 2809003NM ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09369PH 513 PDX - RIGHT HAND SEAT TRACK NR 7 HAS GOUGES AT STATION 312.350 FRAME TO 333.300 FRAME. REPAIRED IAW SRM 521-40-11. 2H72 4T RTA13NM 20050128000962005012800096NM 2005 1 28 QXEA200500097 120050108A5347 SEAT TRACK DHAV DHC8 DHC8102 2809003NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09369PH 513 PDX - LEFT HAND CENTER SEAT TRACK NR 4 HAS GOUGES AND CORROSION AT FRAME 378 TO 330 TO 395. REPAIRED IAW SRM 51-40-11. 2H72 4T RTA13NM 20050128001202005012800120EU 2005 1 28 RAIA00501043 120050119A7930 ENGINE JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114GR 01514NE LEFT FAILED A RAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03568HK16578 41086 75108 RIC - LEFT ENGINE OIL PRESSURE CAP AND GAUGE CONFIRM PRESSURE DROP. ENGINE SHUT DOWN IN FLIGHT. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE AND PM MODULE. 2L72 4T4 TRTA41NM E18NE 20050128001212005012800121WP 2005 1 28 CALA0500021 120050124A5347593056675 SEAT TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2735836 49441 INSPECTION FOUND LEFT I/B CABIN SEAT TRACK CORRODED FROM STA 1022-1250, LBL 25. THE SEAT TRACK WAS REPLACED IAW SRM 53-05, FIGURE 4. 2L72 4F A6WE 20050128001252005012800125EU 2005 1 28 05FDEA00150 120050124A5320 SUPPORT AIRBUS310 A310203 3930313EU ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25405FE 237 FWD CARGO PIT ENTRYWAY LWR SILL HAS CRACKED SUPPORT AT FR22. CRACK IS ON LOWER SIDE AND IS 2.5 INCH LONG. REMOVED AND REPLACED SUPPORT IAW A310-200 SRM 51-72-10. ALODINED, PRIMED, AND TOPCOATED AS REQUIRED IAW A310-200 SRM 51-21-10. REAPPLIED CPC IN AFFECTED AREA IAW A310-200 SRM 51-23-20. 2L72 4F RTA35EU 20050128001322005012800132NM 2005 1 28 SWAA050184 120050124A57536546486130 WEDGE BOEING737 7373H4 1384600NM RT WING DEBONDED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29361SW 26572 DURING SCHEDULED C4 CHECK, FOUND RT WING INBOARD MID FLAP T/E WEDGE DISBONDED. REMOVED AND REPLACED T/E WEDGE PER MM. 2L72 4F RTA16WE 20050131000032005013100003NM 2005 1 31 SWAA050192 120050125A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 805, STRINGER 18L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050131000112005013100011NM 2005 1 31 SWAA050207 120050125A53206551698 SPLICE BOEING737 7373A4 1384585NM STRINGER CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29680AA 23505 DURING SPV, FOUND STRINGER SPLICE AT BS 908, STRINGER 4R, CRACKED. REMOVED AND REPLACED STINGER SPLICE PER SRM. 2L72 4F RTA16WE 20050131000182005013100018NM 2005 1 31 05FDEA00159 120050125A5210 SKIN BOEING727 727200 138407ENM L1 DOOR DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25465FE BN162 21289 LBL 70 FWD ENTRY DOOR EXTERNAL SKIN DAMAGED 15.750 INCH FROM LEADING EDGE 15 INCH FROM LOWER EDGE. REMOVED OUT OF LIMITS EXTERNAL SKIN, FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 53-10-1, 51-30-2, AND 52-00-3. 2L73 4F RTA3WE 20050131000262005013100026SO 2005 1 31 C2XA05IA011 120050120A335074441 CONNECTOR EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT LOOSE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714939 145030 THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHT OVER THE SERVICE DOOR WAS INOPERATIVE. MAINTENANCE RESECURED A LOOSE CONNECTOR ON THE AFFECTED LIGHT, OPS CHECKED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THIS PART IS NOT SERIALIZED AND NO TIMES/CYCLES ARE AVAILABLE. 2L72 4F RTT00011AT 20050131000362005013100036NM 2005 1 31 UPS05443727 120050107A534065B38600170 STRINGER CLIP BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C - BS 1040 STR 1R, STRINGER TIE CLIP FOUND CRACKED. M/D BS 1040 STR 1R, STRINGER TIE CLIP REPLACED IAW SRM 51-10-01 PAGE 9. 2L74 4F A20WE 20050131000422005013100042NM 2005 1 31 QXEA200500118 120050121A27202379003001 REGULATOR DHAV DHC8 DHC8202 2809007NM ZONE 200 FAILED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09368PH14628 512 THE FLIGHT RETURNED TO FIELD WHEN AFTER TAKEOFF THE CREW RECEIVED A FULL RUDDER PRESSURE, NR 1 RUDDER HYDRAULIC, AND RUDDER PRESSURE CAUTIONS. MAINTENANCE INSPECTED THE SYSTEM AND REPLACED THE DUAL PRESSURE REGULATOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050131000432005013100043NM 2005 1 31 SWAA050152 120050120A53106545808 DOOR FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29606SW 27926 DURING SCHEDULED D-CHECK, FOUND FWD SERVICE DOOR FWD LWR STUB FRAME CORRODED. REPAIRED FRAME PER ER. 2L72 4F RTA16WE 20050131000492005013100049EA 2005 1 31 SWIA200514420 120050118A3397 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT LOOSE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07948SW 7789 EMERGENCY FLOOR LIGHTS INOPERATIVE (MIDDLE SECTION). RECONNECTED ELECTRICAL CONNECTOR FOR THE FLOOR EMERGENCY LIGHTS AT ROW 9CD, EMERGENCY LIGHTS, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050131000682005013100068NM 2005 1 31 QXEA200500107 120050119A1420 CONNECTOR DHAV DHC8 DHC8202 2809007NM ZONE 200 CONTAMINATED A QXEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM09368PH14955 512 PDX - FLIGHT 2092 - THE FLIGHT RETURNED TO FIELD WHEN AFTER TAKEOFF THE CREW RECEIVED A RUDDER PRESSURE, FULL RUDDER PRESSURE, AND RUDDER HYDRAULIC CAUTIONS LIGHTS. MAINTENANCE INSPECTED THE SYSTEM AND FOUND MOISTURE IN CONNCETORS P3, P4, P9 AND P10. THE CONNCETORS WERE CLEANED, DRIED, AND GELTEK TAPE WAS APPLIED. OPERATIONAL CHECKS WERE PERFORMED AND WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050131000712005013100071NM 2005 1 31 DHL2005754001 120050115A5270914CE13 SWITCH BOEING727 727223 1384074NM CARGO DOOR PANELINOPERATIVE A DHLAK NONE N FALSE WARNING ININSP/MAINT 1 SO01754DH 22008 LATCHES UNLOCKED ON CARGO DOOR PANEL LIGHT INOP. REMOVED AND REPLACED TORQUE TUBE LATCH LOCK SWITCH IAW AEI M/M CH 24 PG 28, OPS CK NORMAL. P/N INST 914CE1-3. 2L73 4F A3WE 20050131000732005013100073EA 2005 1 31 05017669 120050117A2150 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA LT A/C PACK ILLUMINATED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27669BR 7545 ABORTED TAKEOFF FOR LT PACK HIGH TEMPERATURE MESSAGE. MX OPS CHECK GOOD. 2L72 4F RTA21EA 20050131000752005013100075EA 2005 1 31 05017703 120050117A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA LAVATORY INTERMITTENT A VTZAO OTHER N FALSE WARNING CLCLIMB 1 EA27703BR 7467 LAV SMOKE INDICATION MOMENTARY ON TAKEOFF. NO SMOKE ODOR PRESENT. MX INSPECTED COALESCER BAGS. NO OIL NOTED. 2L72 4F RTA21EA 20050131000812005013100081EU 2005 1 31 MALA050128 120050113A3350330151 POWER SUPPLY SAAB SF340 340B 7860101EU EMERGENCY LIGHTSINOPERATIVE A MALAO OTHER L NO TEST NRNOT REPORTED 1 GL15406XJ 340B406 EMERGENCY LIGHTS AT 7LN, 9LN, 10LN, 42LN, 43LN & 44LN INOP. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY AT 20LN. P/N 3301-51. 2L72 4T RTA52EU 20050131001062005013100106NM 2005 1 31 2005F00012 120050114A57126516260 RIB BOEING727 7272M7 138407SNM RT WING DAMAGED A DHLAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01750DH 21951 OUTBOARD RT WING RIBS DAMAGED. 2L73 4F A3WE 20050131001092005013100109NM 2005 1 31 QXEA200500115 120050121A2820AV24B1343D ACTUATOR DHAV DHC8 DHC8202 2809007NM FUEL SHUTOFF FAILED A QXEAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 NM09374PH146722371 528 FLT RETURNED TO FIELD WHEN THE CREW WAS UNABLE TO TRANSFER FUEL FROM THE RIGHT TANK. MAINTENANCE INSPECTED THE SYSTEM AND THEN REPLACED THE REFUEL/DEFUEL SHUT-OFF VALVE ACTUATOR ASSEMBLY. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050131001242005013100124NM 2005 1 31 QXEA200500092 120050108A5347 SEAT TRACK DHAV DHC8 DHC8102 2809003NM ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09369PH 513 PDX - RIGHT HAND CENTER SEAT TRACK NR 7 HAS GOUGES AT FRAME 397 TO 412. REPAIRED IAW SRM 51-40-11. 2H72 4T RTA13NM 20050131001272005013100127NM 2005 1 31 UPS05243791 120050108A5330 SKIN BOEING727 727185C 138406NNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 INSPECTION TYPE:C SUSPECT CORROSION BETWEEN SKIN AND INTERNAL STRUCTURE BS 294 BETWEEN S18R + S19R ON CLOSER INSPECTION CORROSION FOUND TO BE WELL WITHIN LIMITS IAW SRM 53-30-01. A SMALL CRACK WAS FOUND COMING FROM A FASTENER HOLE. AREA CUT OUT IAW SRM 53-30-03. HFEC CARRIED OUT, NO DEFECTS FOUND. REPAIR DOUBLER FABRICATED AND INSTALLED IAW 53-30-3. 2L73 4F A3WE 20050131001312005013100131NM 2005 1 31 UPS05443767 120050107A531365B0436645 STRINGER BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C M/D - BS 742 - 744 STR 23R, STRINGER END FOUND CRACK. M/D BS 742 TO BS 744 S-23R STRINGER END REPAIRED AS PER RS : 53-61-35230 AND ENGINEERING FILE NUMBER 747-53-20204. 2L74 4F A20WE 20050131001322005013100132NM 2005 1 31 UPS05443770 120050106A5311 FRAME BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C M/D - BS 1372, BETWEEN STR 22 - 23R, FRAME I/B CHORD O/B FACE FOUND CRACK. M/D FRAME I/B CHORD REPAIRED AT BS 1372 BETWEEN S-22R AND S-23R AS PER RS 53-62-35246 AND ENGINEERING FILE NUMBER 747-53-20208. 2L74 4F A20WE 20050131001442005013100144WP 2005 1 31 UPS05843755 120050106A531337585931 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01868UP 45968 INSPECTION TYPE:C3 LONGERON 34L CRACKED AT STA 1260-1280. REMOVED SPLICE AT STA 1270 L34L. REMOVED L34L FROM SPLICE AT STA 1350 TO STA 1270. FAB & INSTALL REPLACEMENT LONGERON SECTION FROM 3758593-1 BETWEEN STA 1270-1350 AND SPLICE FITTING AT STA 1270 REF SRM 51-1-21, 51-1-20D, 51-1-8, 51-1-15. 2L74 4F RT4A25 20050131001492005013100149WP 2005 1 31 UPS05843778 120050106A534058942822 CLIP DOUG DC8 DC873F 302199FWP CARGO BAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01868UP 45968 INSPECTION TYPE:C3 CRACK INSIDE THE NR 4 -T- BOLT BACKUP FITTING STA 320 REMOVED FITTING TO FOM. FOUND BOTH ATTACH CLIPS CRACKED (-1 & -2). REMOVED & REPLACED BOTH ATTACH CLIPS AND RE-INSTALLED BACKUP FITTING REF SRM 51-1-20D, 51-3-0, 53-2-0 FIG 2D, 51-1-8, 51-1-15. 2L74 4F RT4A25 20050131001522005013100152WP 2005 1 31 UPS05843782 120050113A53403758497U2 FITTING DOUG DC8 DC871F 302199DWP CARGO BAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01701UP 45938 INSPECTION TYPE:C1 INTERCOSTAL-TO-FRAME ATTACH FITTING CRACKED AT STA 1140 LONGERON 35R. REMOVED AND REPLACED FITTING REF SRM 51-1-20D, 51-1-8, 51-1-15. 2L74 4F RT4A25 20050131001622005013100162EU 2005 1 31 AWXA200500084 120050112A5315D5311261320009 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28621AW 053 SAL - MAJOR REPAIR - DURING C-04 CHECK INTERGRANULAR CORROSION WAS FOUND ON LONGITUDINAL FLOORBEAM -Y189 BETWEEN FR 20 AND FR 21. MAINTENANCE REMOVED CORRODED LONGITUDINAL FLOORBEAM -Y189 FROM FR 20 TO FR 21; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 53-11-14. 2L72 4F RTA28NM 20050131001712005013100171EU 2005 1 31 AWXA200500088 120050111A5315D53070011 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28621AW 053 SAL - MAJOR REPAIR - DURING C-04 CHECK INTERGRANULAR CORROSION WAS FOUND ON FLOORBEAM Y1292 AT FR 66. MAINTENANCE REMOVED CORRODED FLOORBEAM Y1292 AT FR 66; FABRICATED A NEW REPLACEMENT FLOORBEAM PER DWG D53472040; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050131001722005013100172EU 2005 1 31 AWXA200500089 120050112A5347D53112092205 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28621AW 053 SAL - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON RT INBOARD SEAT TRACK BETWEEN FR 21 AND FR 24. MAINTENANCE REMOVED CORRODED RT INBOARD SEAT TRACK FROM FR 21 TO FR 24; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050131001812005013100181NM 2005 1 31 QXEA200500137 120050124A5312 PRESSURE PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09410QX 4053 PDX - HOLES IN DOME NUTS IN PRESSURE PANEL 121BL. REPAIRED IAW DHC-8-200 SRM 51-42-00, SRM 51-23-00 AND AMM TASK 51-21-01-340-801. 2H72 4T RTA13NM 20050131001882005013100188NM 2005 1 31 QXEA200500125 120050117A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09410QX 4053 PDX - RIGHT INBOARD SEAT TRACK CORROSION APPROXIMATELY X3.00. REPLACED IAW DHC-8 400 SRM 51-40-15 AND 51-42-05-330-801. 2H72 4T RTA13NM 20050131001952005013100195NM 2005 1 31 SWAA050230 120050127A53306545774 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED RON, FOUND FUSELAGE SKIN AT BS 760, STRINGER 18R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050131002062005013100206NM 2005 1 31 SWAA050241 120050127A53106546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29602SW 27953 DURING SCHEDULED D-CHECK, FOUND 3 EACH SHEAR TIES CORRODED BETWEEN BS 727E AND BS 787, LBL 18 AND RBL 9. REMOVED AND REPLACED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20050202000112005020200011NM 2005 2 2 SB05007 120050118A3350210310005 FUSE BOEING737 7374B7 1384702NM POWER SUPPLY BLOWN A USAAK NONE O OTHER ININSP/MAINT 1 EA19777AU 24979 PIT - MAINTENANCE REPORTED THE AFT SERVICE DOOR EXTERIOR EMERGENCY ESCAPE SLIDE LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE 5 AMP FUSE (E-1) AT POWER SUPPLY M1137. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050202000132005020200013NM 2005 2 2 AALA20050049 120050125A3350 CHARGER BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21179AA 32397 ORD - FORWARD GALLEY EMERGENCY LIGHT CHARGER INOPERATIVE. REPLACED FORWARD GALLEY EMERGENCY LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050202000152005020200015NM 2005 2 2 AALA20050059 120050118A3350 CONVERTER BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21664AA 25298 MIA - EMERGENCY LIGHT AT SEAT 26D INOPERATIVE. FOUND LOOSE CONVERTER AT SEAT HARNESS. RESEATED LOOSE CONVERTER AT SEAT 26D HARNESS FOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050202000202005020200020NE 2005 2 2 AALA20050054 220050125A7200 ENGINE DOUG DC9 DC983 3022083WP PWA JT8 JT8D217 52053NE RIGHT INOPERATIVE A AALAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SW21984TW 53634 726862 DFW - FIFTEEN MINUTES BEFORE LANDING THE RIGHT ENGINE OIL QUANTITY WENT TO ZERO. AFTER A COUPLE OF MINUTES THE AMBER LOW OIL QUANTITY LIGHT CAME ON QUICKLY FOLLOWED BY THE RED LIGHT. THE RIGHT ENGINE WAS SHUTDOWN PER CHECKLIST. THE SHUTDOWN WAS NORMAL. THEN ENGINE WINDMILLED FOR 8 TO 10 MINUTES UNTIL LANDING. LANDED DFW WITHOUT INCIDENT. FLIGHT DATA RECORDER DOWNLOADED PER ENGINEERING. REPLACED NUMBER TWO ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA6WE E9NE 20050202000212005020200021NM 2005 2 2 AALA20050048 120050124A2120 ODOR BOEING757 757223 1384957NM COCKPIT DETECTED A AALAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SW21195AN 32389 STRONG BURNING SMELL PLUS LIGHT SMOKE ON FINAL AT 4000 FEET. NOTICED STRONG SMELL ON TAKEOFF FROM LGA. NO OTHER INDICATIONS. DISSIPATED ON LANDING. NOTHING IN CABIN REPORTED BY FLIGHT ATTENDANT. ACCOMPLISHED FAULT ISOLATION PROCEDURES 21 00 01. NO SMOKE OR BURNING SMELL NOTICED. PERFORMED EXTENSIVE INSPECTION IN COCKPIT AND AIRCRAFT BAY AREA. UNABLE TO LOCATE ANY EVIDENCE OF SMOKE. INSPECTED ELECTRONIC EQUIPMENT AREA WITH NO DISCREPANCIES NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050202001072005020200107NM 2005 2 2 AALA20050035 120050115A21214100943B FAN BOEING777 777223 1385213NM RECIRCULATION INOPERATIVE A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21774AN 29581 MIA - INFLIGHT T2031/15, ON DESCENT PASSING 10000 SMOKE IN COCKPIT. DISAPPATED AND RETURNED AT 6000. SMELLED ACRID ELECTRICAL SMELL. WENT ON OXYGEN AND LANDED. SMOKE WENT AWAY. SMOKE WAS VISIBLE IN COCKPIT DURING EVENT. REPLACED LOWER RECIRCULATION FAN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20050202001202005020200120WP 2005 2 2 WRLA2005001 120050102A5730 PANEL DOUG DC10 DC1030 3023501WP GE CF6 CF650C2 30018NE WING TO BODY CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11352 47838 LEFT SIDE UNDER WING TO FUSELAGE PANEL NR 153DB ON BOTTOM SURFACE HAS EXFOLIATE CORROSION BETWEEN STATIONS 1239 AND 1321. REMOVED WING TO FUSELAGE PANEL NR 153DB AND ACCOMPLISHED REPAIR TO LT WING FUSELAGE PER ERA 05-53-001 REV NC DATED 01/07/05 PART 1. ACCOMPLISHED ULTRASONIC AND LIQUID PENETRANT INSPECTION, NO CRACKS FOUND. REINSTALLED PANEL NR 153DB PER SRM 51-31-01. FUELED UPPER AUX TANK AND PERFORMED STATIC LEAK CHECK, NIL FOUND. 2L73 4F4 F A22WE E23EA 20050203000062005020300006 2005 2 3 QXEA200500140 420050128A22107003975901 CONTROL PANEL DHAV DHC8 DHC8202 2809007NM ZONE 100 AFCS INOPERATIVE A QXEAO OTHER O OTHER CRCRUISE 1 NM09356PH164223835 502 SEA - ON FLIGHT NUMBER 2244, IN CRUISE MOST FLIGHT GUIDANCE COMPUTER BUTTONS WERE INOPERATIVE. AUXILARY BUTTONS WORKED. WHEN NAV SEL BUTTON WAS PUSHED IN ENGAGED THE AUTO PILOT. MAINTENANCE REMOVED AND REPLACED FLIGHT GUIDANCE COMPUTER CONTROL PANEL. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050203000072005020300007NM 2005 2 3 QXEA200500146 120050130A242011522184 GENERATOR BOMBDRDHC8 DHC8401 1390041NM ZONE 100 INOPERATIVE A QXEAO OTHER O OTHER LDLANDING 1 NM09407QX7005 964 4049 SMF - ON FLIGHT 2415, ON SHORT FINAL RECEIVED A -R AC BUS- AND -NR 2 AC GEN- CAUTION LIGHT, RAN CHECKLIST, UNABLE TO CORRECT THE NR 2 AC GEN CAUTION LIGHT BUT THE R AC BUS CAUTION LIGHT WENT OUT. MAINTENANCE REMOVED AND REPLACED THE NR 2 AC GEN. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050203000172005020300017NM 2005 2 3 SWAA050257 120050128A2710AN201KP4A BEARING BOEING737 7373H4 1384600NM AILERON STICKING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29360SW 26571 CREW REPORTS AILERON CONTROL STICKING. REMOVED AND REPLACED RT CONTROL COLUMN BEARING PER MM. 2L72 4F RTA16WE 20050203000222005020300022NM 2005 2 3 SWAA050259 120050128A53306545765 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 FUSELAGE SKIN AT BS 500B, STRINGER 17L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20050203000322005020300032NM 2005 2 3 P5CA0501309 120050120A325069B461728 MODULE BOEING747 747341 13848AMNM NLG STEERING MALFUNCTIONED A P5CAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA15355MC 23395 BODY GEAR STEERING LIGHT ILLUMINATED, PRIMARY AND ALTERNATE. REPLACED BGS MODULE PER MM 32-53-00. ALL OPS & IND, OK PER 32-53-00. 2L74 4F RTA20WE 20050203000392005020300039EA 2005 2 3 SWIA200514462 120050128A2750865D1007 PDU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07409SW 7056 FLAP FAIL MESSAGE. REPLACED PDU IAW CRJ MM 27-52-01, OPERATIONAL CHECK GOOD. P/N 865D100-7, S/N OFF 179. 2L72 4F RTA21EA 20050203000652005020300065GL 2005 2 3 RAIA00501053 220050123A7421CH318981 IGNITER EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 2 ENGINE INOPERATIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03812HK 145373 ORF - NR 2 ENGINE WILL NOT START TRIED CROSS-BLEED AND APU. MAINTENANCE REMOVED AND REPLACED BOTTOM IGNITER ON NR 2 ENGINE. 2L72 4T4 FRTT00011ATTE6CH 20050203000742005020300074WP 2005 2 3 ABXA050023 120050121A2741 LIMIT SWITCH DOUG DC9 DC941 302207NWP RUDDER TRIM MALFUNCTIONED A ABXAO OTHER F FLT CONT AFFECTED CRCRUISE 1 GL23974AX 47623 ALTERNATE TRIM (LONG) CIRCUIT BREAKER TRIPPED. PER FLIGHT CONTROL, CREW DECLARED AN INFLIGHT EMERGENCY. REPLACED ALT LIMIT SWITCH IAW DC-9 AMM 27-40-00. OPS CHECKED GOOD. 2L72 4F A6WE 20050203000762005020300076WP 2005 2 3 DHL2004809518 120050114A57405761746U19 BRACKET DOUG DC8 DC873F 302199FWP LT WING BROKEN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01809DH91189 46047 LT WING TRACK ASSY BRACKET BROKEN, XW 104.000. REMOVED AND REPLACED BRACKET ON LT WING TRACK ASSY XW 104.000 IAW SRM 51-3-0 PG 1, SRM 51-1-27A PG 1-4. 2L74 4F RT4A25 20050203000772005020300077WP 2005 2 3 DHL2004809516 120050105A534047723971 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01809DH91189 46047 AFT FUSELAGE FITTING CRACKED 1.000, NEXT L-17R STA 1766.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA AND NEW FITTING IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-3-0 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20050203000812005020300081NM 2005 2 3 SWAA050273 120050201A5530176A310126 ANGLE BOEING737 7377H4 1384404NM VERTICAL STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29744SW 29490 DURING SCHEDULED HC1 CHECK, FOUND RT VERTICAL STABILIZER FITTING ATTACH ANGLE AT STA 1007, CRACKED. REPAIRED STABILIZER PER EA. 2L72 4F RTA16WE 20050203000852005020300085 2005 2 3 SWAA050264 420050201A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29654SW 28399 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050203000872005020300087NM 2005 2 3 SWAA050266 120050201A53106546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29602SW 27953 DURING SCHEDULED D-CHECK, FOUND 4 EACH SHEAR TIES BETWEEN BS 727D AND BS 787, FROM LBL 11 TO RBL 14, CORRODED. REMOVED AND REPLACED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20050203000882005020300088NM 2005 2 3 SWAA050267 120050201A53156545410 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29602SW 27953 DURING SCHEDULED D-CHECK, FOUND 2 EACH LONGITUDINAL FLOORBEAMS CRACKED AT BS 727A +18, BETWEEN RBL 23 AND RBL 48. REPAIRED FLOORBEAMS PER ER. 2L72 4F RTA16WE 20050203000902005020300090WP 2005 2 3 DHL2004809525 120050117A534097540242 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01809DH91189 46047 AFT CARGO COMPT RT TUNNEL FITTING CRACKED 2.000, STA 1220.000. REMOVED CRACKED FITTING IAW SRM 53-1-0 PG 1, SRM 51-1-20D PG 1, SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9, SRM 51-3-0 PG 1, SRM 51-1-21 PG 1, SRM 51-3-1 PG 2A. 2L74 4F RT4A25 20050203000962005020300096EA 2005 2 3 SWIA200514454 120050127A5610 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAA UNSCHED LANDING O OTHER CRCRUISE 1 NM07710BR 7852 CAPTAINS WINDSHIELD CRACKED AT 350. REMOVED AND REPLACED CAPTAINS WINDSHIELD ASSY IAW AMM 56-11-01. P/N OFF 601R33033-17, S/N OFF 03150H5464. 2L72 4F RTA21EA 20050203000972005020300097SO 2005 2 3 SWIA200514455 120050127A5210 LATCH EMB 120 EMB120ER 3260203SO PAX DOOR LACK OF LUBE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07581SW 120349 MAIN CABIN DOOR WILL NOT LATCH CLOSED. LUBED PAX DOOR AS NECESSARY AT DOOR HANDLE, VERIFIED MOVEMENT OF DOOR. OPERATIONAL CHECK GOOD. DOOR LOCK ALIGNMENT MARKS ALIGN. 2L72 4T RTA31SO 20050203000982005020300098SO 2005 2 3 SWIA200514456 120050127A27523430001007 ACTUATOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07290SW7740 7740 120317 DURING FLAP RETRACTION, RECEIVED FLAP CONTROL FAULT ON OUTBOARD FLAP PAIRS. REPLACED LEFT OUTBOARD FLAP ACTUATOR WITH SERVICEABLE UNIT. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050203000992005020300099WP 2005 2 3 DHL2004809517 120050106A5313S1616757 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01809DH91189 46047 AFT FUSELAGE L-17R CRACKED 3.000, STA 1766.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 53-5-3 FIG 5 SHEET 1. REMOVED DAMAGED LONGERON IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW LONGERON SEGMENT (EXTRUSION S1616757) IAW SRM 51-1-20D PG 9, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20050203001012005020300101WP 2005 2 3 ABXA050022 120050122A32607000010101 WARNING SWITCH DOUG DC9 DC931 3022065WP NLG DEFECTIVE A ABXAO OTHER N FALSE WARNING DEDESCENT 1 GL23929AX3529 45874 NOSE GEAR UNSAFE RED WARNING LIGHT ILLUMINATED DURING UPLATCH CHECK (APPROX 10,000 FT MSL), COMPLIED WITH ABNORMAL. RECYCLED LANDING GEAR AND GOT GOOD DOWN AND LOCK (GREEN INDICATORS) WHEN THE LANDING GEAR WAS RETRACTED, THE NOSE GEAR UNSAFE LIGHT CAME ON AGAIN AND REMAINED ON. GEAR EXTENSION FOR LANDING WAS NORMAL. FOUND NOSE GEAR UPLOCK SWITCH BAD, INTERMITTENT OPERATION. REMOVED AND REPLACED NOSE GEAR UPLOCK SWITCH IAW ABX DC-9 AMM 32-60-01-2-0101. OPS CHECKED GOOD IAW ABX DC-9 AM 32-60-00-1-0101. 2L72 4F A6WE 20050203001032005020300103WP 2005 2 3 AALA20050066 120050131A3350 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21953U 49267 MSP - EMERGENCY LIGHTS AT AFT FLIGHT ATTENDANT AREA INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT AFT FLIGHT ATTENDANT AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050613000212005061300021NM 2005 6 13 SWAA051526 120050524A53206545410 FLOOR SUPPORT BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29353SW 24889 DURING SCHEDULED 1/2D CHECK, FOUND LONGITUDINAL FLOOR SUPPORT UPPER TEE CHORD CRACKED AT BS 660, BL 0. REPAIRED TEE CHORD PER SWA EA. 2L72 4F RTA16WE 20050613000302005061300030NM 2005 6 13 SWAA051543 120050525A53306545767129 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 17R TO STR 18R. REPAIRED SKIN PER BFG ER & SWA EA. 2L72 4F RTA16WE 20050613000372005061300037NM 2005 6 13 SWAA051554 120050525A534065C27314 STRINGER CLIP BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 706, STR 2L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050613000482005061300048SO 2005 6 13 DJFA2005100 120050520A3320189720 INVERTER EMB 135 EMB135BJ 3260306SO ALLSN AE300 AE3007A GL CABIN LIGHTING OVERHEATED E DJFAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA23928CW E145528 CREW NOTICED AN ODOR IN THE AIRCRAFT CABIN. ODOR WAS IDENTIFIED AND WAS DESCRIBED TO BE CHEMICAL IN NATURE. SOURCE OF ODOR WAS FOUND TO BE COMING FROM CABIN LIGHTING. WHEN CABIN LIGHTING WAS TURNED OFF THE ODOR HAD DISSIPATED. AIRCRAFT DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ISSUED MEL 33-20-00-1 FOR THE CABIN LIGHTING SYSTEM. ON 26 MAY 2005 MAINTENANCE REPLACED AN INVERTER FOR THE LIGHTING. THE OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRT TE6CH 20050613000572005061300057EA 2005 6 13 VTZA200500084 120050526A5320601R3117117 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27659BR 7509 INTERCOSTAL CRACKED AT .250 IN LENGTH ON LT OUTBOARD SIDE AT FS 484 BETWEEN BL 36.00. 2L72 4F RTA21EA 20050613000712005061300071NM 2005 6 13 AWXA200500616 120050525A3397BMS13311122 WIRE BOEING737 7373G7 1384595NM EMERGENCY LIGHT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 DEN - EEL - DURING 4-DAY CHECK, EMERGENCY FLOOR PROXIMITY LIGHT AT SEAT 15C WAS FOUND TO BE INOPERATIVE. FURTHER INSPECTION FOUND A BROKEN WIRE LEADING TO THE EMERGENCY FLOOR PROXIMITY LIGHT AT SEAT 15C. MAINTENANCE REPAIRED WIRING AND OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050613000782005061300078EU 2005 6 13 MALA050456 120050525A5320 GUSSET BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15506XJ E2314 DURING C2 INSPECTION, FOUND GUSSET PLATE AT FRAME 18, RBL36 CORRODED. 2H74 4F RTA49EU 20050613000832005061300083EU 2005 6 13 MALA050449 120050525A5320 FLOOR SUPPORT BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15506XJ E2314 DURING C2 INSPECTION, FOUND FLOOR SUPPORT PLATE CORRODED BETWEEN FRAME 18 AND FRAME 19. 2H74 4F RTA49EU 20050613000862005061300086NE 2005 6 13 WRNA200500013 220050521A7200 ENGINE BOEING747 7472U3B 1384846NM PWA JT9 JT9D7Q 52054NE NR 1 DAMAGED A WRNAA UNSCHED LANDING O OTHER CLCLIMB 1 SO05922FT 22768 702203 NR1 ENGINE COMPRESSOR STALLED AT FL 11.5, AIRCRAFT RETURNED. LANDING NORMAL. ENGINE BOROSCOPE COMPLIED WITH, NO DISCREPANCIES NOTED. NR 1 ENGINE FAN CASING ACOUSTIC LINERS FROM 1O`CLOCK TO 8 O'CLOCK POSITION DAMAGED. REMOVED AND REPLACED PANELS IAW 72-31-08, NR1 ENGINE INTAKE ACOUSTIC LINER BEARING FAN BLADE RUB STRIP DAMAGED, REMOVED AND REPLACED LINER IAW 72-31-00. AIRCRAFT RETURNED TO SERVICE. 2L74 4F4 FRTA20WE E3NE 20050613000882005061300088WP 2005 6 13 AALA20050355 120050526A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21564AA 49346 DFW - CEILING EMERGENCY LIGHTS ABOVE ROWS 12 TO 16 AND 22 TO 29 INOPERATIVE. REPLACED BATTERY PACKS FOR CEILING EMERGENCY LIGHTS ABOVE ROWS 12 TO 16 AND 22 TO 29. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050613000922005061300092WP 2005 6 13 IXXA05SMN04S 120050427A5340 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE COCKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX 45993 DURING ROUTINE C-CHECK INSPECTION, FWD CARGO COMPT - INTERIOR SPLICE FITTING CRACKED, STA 440.000 - STA 460.00, L-34L 3. REMOVED CRACKED FITTING IAW DC-8 SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING (ALCLAD 7075 T6 51) IAW DWG 3750330. PERFORMED NDT INSPECTION TO FITTING IAW NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED AREA + NEW FITTING IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO IAW DC-8 SRM 51-1-11 PAGE 9. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D PAGE 9. TORQUED IAW DC-8 SRM 51-3-1. 2L74 4F RT4A25 20050613000932005061300093WP 2005 6 13 IXXA05SMN055S 120050427A5340 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX 45993 DURING ROUTINE C-CHECK INSPECTION, FWD CARGO COMPT - INTERIOR SPLICE FITTING CRACKED, STA 440.000 - STA 460.00, L-34L 3. REMOVED CRACKED FITTING IAW DC-8 SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING (ALCLAD 7075 T6 51) IAW DWG 3750330. PERFORMED NDT INSPECTION TO FITTING IAW NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED AREA + NEW FITTING IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO IAW DC-8 SRM 51-1-11 PAGE 9. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D PAGE 9. TORQUED IAW DC-8 RM 51-3-1. 2L74 4F RT4A25 20050613000972005061300097WP 2005 6 13 ASMF200505028 120050525A526059618925001 ACTUATOR DOUG DC9 DC987 3022087WP STAIR FAILED W ASMFA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW231075T 49724 AIRCRAFT RETURNED OF FLIGHT AS A CONSEQUENCE OF PRESSURIZATION WAS UNSTABLE DURING CLIMB. AT PLATFORM, THE VENTRAL STAIRWAY WAS ADJUSTED IAW MM 52-63-00. PRESSURIZATION CONTROLLERS BITE WERE PERFORMED, SYSTEM VALVES WERE REVISED, MANUAL SYSTEM OPERATION WAS PERFORMED IAW MM 21-32-03, ALL CORRECT. DURING OVERNIGHT SERVICE, THE PRESSURIZATION SYSTEM WAS CHECKED IAW MM 21-32-00, TESTED CORRECT. THE VENTRAL STAIRWAY ACTUATOR WAS REPLACED IAW MM 52-63-02, TESTED CORRECT. 2L72 4F RTA6WE 20050613001072005061300107NM 2005 6 13 SWAA051561 120050526A3350101114 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29627SW 27935 EMERGENCY EXIT LIGHT LENS FELL OFF NEXT TO L1 DOOR. SECURED LENS PER MM. 2L72 4F RTA16WE 20050613001092005061300109 2005 6 13 SWAA051563 420050526A2565D31354 SLIDE BOEING737 7377H4 1384404NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29709SW 27843 L1 DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. DID NOT DEPLOYED. INSTALLED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20050613001112005061300111NM 2005 6 13 SWAA051565 120050526A53306545766 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29667SW 23063 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, BELOW STR 12R. REPAIRED SKIN PER SRM & SWA EA. 2L72 4F RTA16WE 20050613001132005061300113NM 2005 6 13 SWAA051567 120050526A53116546547 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND BS 727 INBOARD FUSELAGE CHORD CORRODED AT RBL 10 TO LBL 10, WL 148. REMOVED AND REPLACED CHORD SECTION PER SRM. 2L72 4F RTA16WE 20050613001142005061300114NM 2005 6 13 SWAA051572 120050526A53306545768 SKIN BOEING737 737301 1384611NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN TEAR STRAP CORRODED AT BS 370, STR 25L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050613001162005061300116NM 2005 6 13 SWAA051574 120050526A53306552988 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29353SW 24889 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 944, STR 24R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050613001182005061300118NM 2005 6 13 SWAA051576 120050524A53306523693 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING WALK AROUND INSP, FOUND FUSELAGE SKIN CRACKED AT BS 312, STR 18R. REPAIRED SKIN PER SRM & SWA EA. 2L72 4F RTA16WE 20050613001202005061300120NM 2005 6 13 SWAA051578 120050524A5753 SKIN BOEING737 7373H4 1384600NM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW BN923 22940 DURING SCHEDULED SERVICE CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED FLAP ASSY PER MM. 2L72 4F RTA16WE 20050614000042005061400004EU 2005 6 14 AWXA200500632 120050506A5320D53112836200 FLOOR SUPPORT AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28639AW 471 SAL - MAJOR REPAIR - DURING C08 CHECK, EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM -Y189 BETWEEN FS 20 TO FS 23. MAINTENANCE REMOVED FLOORBEAM -Y189 AT FS 20 TO FS 23; FABRICATED A NEW REPLACEMENT FLOORBEAM PER DWG D53111473; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050614000142005061400014NM 2005 6 14 P5CA0501357 120050518A5522 SKIN BOEING747 747230B 1384889NM LT ELEVATOR CHAFED A P5CAK NONE O OTHER ININSP/MAINT 1 EA15508MC 21644 LEFT INBOARD ELEVATOR TOP LEADING EDGE SKIN FOUND CHAFED. ACCOMPLISHED REPAIR PER BOEING INSTRUCTIONS 1-1HR8MP AND FAA FORM 8100-9. 2L74 4F A20WE 20050614000162005061400016GL 2005 6 14 CHQA200500104 220050530A72614252070 CARBON SEAL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL ENGINE LEAKING A CHQAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL11281SK6134 145391 CAE312342 FLIGHT 3179 SDF-LGA - WHILE CLIMBING THROUGH 14,000 FEET, THE E1 OIL PRESSURE WENT TO AMBER. OIL QUANTITY ON MFD WAS 3 QUARTS. SHUT DOWN ENGINE IAW QRH AND RETURNED TO FIELD. REMOVED AND REPLACED LEAKING E1 CARBON SEAL IAW EMB 145 AMM 72-61-02-4. OPS CHECK AND LEAK CHECK GOOD. 2L72 4T4 FRTT00011ATTE6CH 20050614000202005061400020NM 2005 6 14 PCSA0526051 120050526A2730680005007 PCU BOEING727 727227 1384078NM ELEVATOR MALFUNCTIONED A PCSAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 SO29794AJ 21243 ON TAXI OUT CONTROL YOKE JAMMED WILL NOT MOVE FWD. AC RETURNED TO RAMP. AIRCRAFT WAS FERRIED BACK TO MIAMI. NO DEFECTS REPORTED ON FLIGHT. REMOVED FLOOR PANEL, INSPECTED CONTROL CABLES EBL, EAL, EBR, EAR & PULLEYS BS 540, 740, 870, 950 & 1050 NO DEFECTS. OPEN PANELS ON TOP OF VERTICAL STAB TO GAIN ACCESS FOR INSPECTION OF CABLES AND PULLEYS, NO DEFECTS. OPEN LH & RH PANEL TO ELEVATOR PCU'S FOUND COLLAR MISSING FROM THRU BOLTS AT RH PCU TAB ROD REACTION LINK, REMOVED & REPLACED ELEVATOR PCU. INSPECTED LH & RH ELEVATOR TAB CONTROL ROD FOR CORRECT INSTALLATION PER BOEING ISAR 97-06-2735-10. CASTELLATED NUTS & COTTER PINS INSTALLED IAW SPM 20-50-01/2 & IPC 27-30-00-31. TEST FLT PERFORMED WITH NO DEFECTS. 2L73 4F A3WE 20050614000212005061400021EA 2005 6 14 VTZA200500091 120050529A5320601R3117117 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27660BR 7519 INTERCOSTAL CRACKED AT.250 IN LENGTH ON LT INBOARD SIDE AT FS 484 LEFT BETWEEN BL 27.00. 2L72 4F RTA21EA 20050614000352005061400035NM 2005 6 14 05FDEA00705 120050330A5320NGA631345 CHANNEL DOUG MD11 MD11 3023602NM FUSLAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 AFT CARGO HAS LONGERON U-CHANNEL AT STA 1954 LONGERON 43R WITH CORROSION. AFT CARGO LONGERON 43R U-CHANNEL REMOVED AND REPLACED NEW FABRICATED AS PER DWG NGA 6313 AT STA 1954. 2L73 4F RTA22WE 20050614000362005061400036NM 2005 6 14 05FDEA00777 120050401A5754ARC4125501 FITTING DOUG MD11 MD11 3023602NM LT WING FLAPS CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 LT WING O/B FLAP HAS CRACK ON STRUCTURE AT STOP BOLT. LT WING O/B FLAP CRACKED STOP FITTING REMOVED. NEW FITTING HOLES TRANSFERRED AND INSTALLED AS PER SRM 51-33-01 AND 51-31-01 VOL II. MAJOR CLASSIFICATION AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050614000382005061400038EA 2005 6 14 A6WA200540180 120050519A3210601R572100373 BUSHING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT MLG TRUNNION MIGRATED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31455AW 7848 LT AFT MLG TRUNNION BUSHING MIGRATED .053 INCH. REMOVED LT AFT MLG TRUNNION BUSHING AND INSTALLED NEW SERVICEABLE BUSHING IAW MFG REO. (K) 2L72 4F4 FRTA21EA E15NE 20050614000392005061400039EA 2005 6 14 A6WA200540178 120050518A493038004883 APU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FLAMED OUT A A6WAO OTHER X ENGINE FLAMEOUT NRNOT REPORTED 1 GL31412AW 7582 APU AUTOSHUT AND GRD CREW ADVISED FLAME COME OUT OF INTAKE. LOUD BANG WHEN SHUTDOWN. DISCHARGED BOTTLES. INSP APU AREA, NO EVIDENCE OF FIRE, C/W (M) ACTION IAW MEL. (K) 2L72 4F4 FRTA21EA E15NE 20050614000462005061400046NM 2005 6 14 AALA20050367 120050530A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21901AN 29503 LGA - RIGHT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR RIGHT AFT OVERWING EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20050614000492005061400049EU 2005 6 14 SDR2005030 120050505A2750BHC1001 VALVE AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE LT WING FLAP LEAKING A TRBAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 SO29355AT23454 355 DURING APPROACH TO TORTOLA ISLAND (EIS), THE FLAPS UNLOCK WARNING CAME ON. UNABLE TO LAND. AIRCRAFT RETURNED TO SAN JAUN. REPLACED FLAP BLOCK VALVE. (K) 2H72 4T4 TRTA53EU E20NE 20050614000522005061400052SO 2005 6 14 O2G2005F00008 120050512A32601159SCAV4571 DOWNLOCK SWITCH GULSTMG1159 GIV 3980115SO RROYCETAY TAY6118 EU NLG FAILED E O2GAO OTHER G MULTIPLE FAILURE DEDESCENT 1 NE03225CX 1467 NO NOSE WHEEL STEERING OR TAXI LIGHTS. REMOVED AND REPLACED NOSE LANDING GEAR DOWNLOCK SWITCH. (K) 2L72 4F4 FRTA12EA E25NE 20050614000592005061400059WP 2005 6 14 ASAA0580149 120050228A5320993051257 CUSP WEB DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02975AS 53451 C-CHECK - AFT CABIN UPPER CUSP MEMBRANE IS CORRODED. REMOVED DAMAGED SECTION. INSTALL REPAIR DOUBLER. (K) 2L72 4F4 FRTA6WE E9NE 20050614000622005061400062EA 2005 6 14 SWIA200515069 120050529A273010231007 DAMPER CNDAIRCL600 CL6002B19 1900309EA ELEVATOR MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07943SW 7762 FLUTTER DAMPNER STATUS MSG INFLIGHT. REMOVED AND REPLACED NR 1 & 2 ELEVATOR FLUTTER DAMPNERS IAW CRJ MM 27-34-05. 2L72 4F RTA21EA 20050614000672005061400067EA 2005 6 14 SWIA200515074 120050530A274070623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07465SW 7845 INFLIGHT, MACH TRIM AND STAB TRIM CHANNEL 2 DISENGAGED. REPLACED HSTA IAW MM 27-42-01 AND HSMCU IAW MM 27-42-05. OPERATIONAL CHECK GOOD IAW MM 27-41-00. P/N: 8396-3, S/N OFF: 1116. 2L72 4F RTA21EA 20050614000732005061400073EA 2005 6 14 SWIA200515080 120050524A2750 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM07919SW 7657 FLAPS FAIL IN 20 DEGREE POSITION UPON TAKEOFF. RIGGED LEFT BPSU IAW MM 27-51-10. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050614000772005061400077EA 2005 6 14 SWIA200515084 120050531A5610 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAO OTHER O OTHER DEDESCENT 1 NM07443SW 7638 DURING DESCENT INTO SLC, F/O'S SIDE WINDOW CRACKED. REPLACED RIGHT SIDE WINDOW PER MM 56-12-01. OPERATIONAL CHECK GOOD. P/N OFF 601R33033-12, S/N OFF 01353H5453. 2L72 4F RTA21EA 20050614000802005061400080NM 2005 6 14 QXEA200500961 120050531A521085217645101 BUSHING MTSBSI BOMBDRDHC8 DHC8402 1390042NM PAX DOOR HINGE UNKNOWN A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09413QX 4060 SEA - ON FLIGHT 2435 THE AFT PASSENGER DOOR WAS HARD TO OPERATE (OPEN). AIRCRAFT WAS FERRIED FROM SEA-PDX WHERE THE MAIN HINGE WAS ADJUSTED AND A NEW UPPER BOLT AND UPPER AND LOWER BUSHINGS WERE INSTALLED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050614000872005061400087NM 2005 6 14 USAA050587 120050503A5340 ATTACH ANGLE BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US 24781 CLT - FOUND ANGLE BRACKET CRACK IN INTERCOSTAL FORWARD ATTACH ANGLE, STATION 500G, S28R. INSTALL NEW BRACKET IAW SRM 51-10-02. (M) 2L72 4F RTA16WE 20050614000922005061400092NM 2005 6 14 USAA050592 120050505A573065C26601197 SKIN BOEING737 7374B7 1384702NM NR 1 SLAT DEBONDED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US39931 24781 CLT - FOUND NR 1 SLAT DISBOND 1 INCH, UNDERSIDE AT INBOARD AUX TRACK. SDA COMPLETED ACCOMPLISHED COMPOSITE REPAIR IAW SRM 57-43-02. (M) 2L72 4F RTA16WE 20050614001562005061400156NM 2005 6 14 SWAA051622 120050601A53156545410 FLOORBEAM BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CRACKED AT BS 727A + 17.5, RBL 44 & RBL 46, WL 208. REPAIRED FLOORBEAM PER BFG ER. 2L72 4F RTA16WE 20050614001652005061400165NM 2005 6 14 SWAA051620 120050601A532065C27314 STRINGER CLIP BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 887, STR 9L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050615001482005061500148NM 2005 6 15 SWAA051666 120050605A53306545775 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29357SW 26594 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 769, STR 24L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050615001502005061500150NM 2005 6 15 SWAA051668 120050605A53306545767 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 391, STR 26L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050615001522005061500152NM 2005 6 15 SWAA051592 120050530A55536546874 LUG BOEING737 737301 1384611NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND LT & RT VERTICAL STAB FWD & AFT FAILSAFE CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER. 2L72 4F RTA16WE 20050615001542005061500154NM 2005 6 15 SWAA051594 120050530A5315141A5170 FLOORBEAM BOEING737 737301 1384611NM COCKPIT FLOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND COCKPIT FLOORBEAM UPPER CHORD CORRODED AT BS 260, LBL 9 TO RBL 9, WL 208. REPAIRED FLOORBEAM PER BFG ER. 2L72 4F RTA16WE 20050615001562005061500156NM 2005 6 15 SWAA051597 120050529A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727, STR 14R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050615001582005061500158NM 2005 6 15 SWAA051599 120050530A335090083 LIGHT BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29720WN 27854 DURING SCHEDULED RON CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20050615001602005061500160 2005 6 15 SWAA051601 420050528A256563562101 SLIDE BOEING737 7377H4 1384404NM L1 DOOR FAULTY A SWAAK NONE O OTHER ININSP/MAINT 1 SW29732SW 27864 L1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATING LOW. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20050615001622005061500162NM 2005 6 15 SWAA051644 120050605A53306545765 SKIN BOEING737 7373H4 1384600NM FWD CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 524, RBL 7, WL 148. REPAIRED SKIN PER BFG ER. 2L72 4F RTA16WE 20050615001632005061500163NM 2005 6 15 SWAA051645 120050605A53156956038 FLOORBEAM BOEING737 7373H4 1384600NM CABIN FLOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 663, BL 0, WL 206. REPAIRED WEB PER BFG ER. 2L72 4F RTA16WE 20050615001642005061500164NM 2005 6 15 SWAA051646 120050605A57126545445 RIB BOEING737 7373H4 1384600NM RT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND RT WING RIB LOWER CHORD CRACKED AT WBL 135.5, BETWEEN STR 2 & STR 3. REPAIRED RIB PER BFG ER. 2L72 4F RTA16WE 20050615001652005061500165NM 2005 6 15 SWAA051647 120050605A57126545456 RIB BOEING737 7373H4 1384600NM LT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND LT WING RIB UPPER FLANGE CRACKED AT WS 453, STR 12. REMOVED AND REPLACED RIB PER SRM. 2L72 4F RTA16WE 20050615001662005061500166NM 2005 6 15 SWAA051648 120050605A53306545776 SKIN BOEING737 7373H4 1384600NM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 927, LBL 15. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050615001672005061500167NM 2005 6 15 SWAA051649 120050604A33504500837 LIGHT BOEING737 7373H4 1384600NM R1 DOOR INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29330SW 23694 DURING SCHEDULED SERVICE CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20050616000052005061600005NM 2005 6 16 DU4R106 120050527A5511 BUSHING BOEING737 7373L9 1384470NM HORIZONTAL STAB CORRODED B DU4RO OTHER O OTHER ININSP/MAINT 1 SO15312FL 24569 LT HORIZONTAL STAB AFT SPAR, UPPER ATTACH LUG, CENTER SECTION, AFT FACE HAS CORROSION AROUND BUSHING. S/O 109001, N/R 22994 2L72 4F RTA16WE 20050616000122005061600012CE 2005 6 16 ENHA0509 120050301A242010300BR ALTERNATOR CESSNA207 207A 2073604CE ENGINE FAILED E ENHAO OTHER O OTHER NRNOT REPORTED 1 AL039973M 96 20700771 ALTERNATOR FAILED. 1H71 3O A16CE 20050616000132005061600013SO 2005 6 16 ENHA0510 120050327A2420ALU8521R ALTERNATOR PIPER PA31 PA31350 7103110SO ENGINE FAILED E ENHAO OTHER O OTHER NRNOT REPORTED 1 AL0378GA 287 318352030 ALTERNATOR NOT CHARGING. 1L72 3O A20SO 20050616000162005061600016CE 2005 6 16 ENHA0513 120050413A242010300BR ALTERNATOR CESSNA207 207A 2073604CE ENGINE MALFUNCTIONED E ENHAO OTHER O OTHER NRNOT REPORTED 1 AL039874M 9 20700745 VERY LOW RIPPLE VOLTAGE PRODUCED BY UNIT, DROPS OFFLINE UNDER LOAD. 1H71 3O A16CE 20050616000192005061600019CE 2005 6 16 ENHA0516 120050527A242010300BR ALTERNATOR CESSNA207 207A 2073604CE ENGINE MALFUNCTIONED E ENHAO OTHER O OTHER NRNOT REPORTED 1 AL039973M 184 20700771 AMMETER SHOWS NO CHARGE DISCHARGE, ALT INOP. 1H71 3O A16CE 20050616000202005061600020NM 2005 6 16 DU4R108 120050531A5320 PAN BOEING737 7373L9 1384470NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED B DU4RK NONE O OTHER ININSP/MAINT 1 SO15312FL 24569 RT FLOOR PAN AT BS 1016 WL208.1 CORRODED. S/O 109001, N/R 22825 2L72 4F4 FRTA16WE E21EU 20050616000252005061600025NM 2005 6 16 SWAA051651 120050603A53306545777 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29331SW 23695 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050616000272005061600027NM 2005 6 16 SWAA051653 120050604A3350 BATTERY BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29349SW 24408 DURING SCHEDULED RON CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20050616000282005061600028NM 2005 6 16 SWAA051654 120050604A5230BAC1505100543 TEE FITTING BOEING737 7373H4 1384600NM AFT CARGO DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29353SW 24889 DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO DOOR LOWER AFT TEE FITTING CRACKED AT FITTING ATTACH POINT. R & R LOWER TEE FITTING PER SRM. 2L72 4F RTA16WE 20050616000312005061600031NM 2005 6 16 SWAA051657 120050604A2121 BEARING BOEING737 7373H4 1384600NM COOLING BLOWER WORN A SWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW29610WN 7904 27696 DIVERSION, SMOKE & FUMES REPORTED IN FWD & AFT CABIN. FOUND EQUIPMENT COOLING BLOWER BEARINGS WORN. REMOVED AND REPLACED EQUIPMENT COOLING BLOWER PER MM. 2L72 4F RTA16WE 20050616000322005061600032NM 2005 6 16 SWAA051658 120050603A3350101114 BULB BOEING737 7373Q8 1384670NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED RON CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB PER MM. 2L72 4F RTA16WE 20050616000332005061600033NM 2005 6 16 SWAA051659 120050604A3350101073 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29703SW 27837 L2 DOOR EMERGENCY EXIT LENS CRACKED. REMOVED AND REPLACED LENS PER MM. 2L72 4F RTA16WE 20050616000342005061600034NM 2005 6 16 SWAA051660 120050604A2750 DRIVE ASSY BOEING737 7377H4 1384404NM FLAP TRACK BROKEN A SWAAA UNSCHED LANDING D INFLIGHT SEPARATION NRNOT REPORTED 1 SW29709SW 27843 DIVERSION/DECLARED EMERGENCY, FLIGHT ATTENDANT NOTIFIED COCKPIT THAT PIECE OF LT WING WAS FALLING OFF. VISUAL INSPECTION CONFIRMED THAT NR 2 OUTBOARD T/E FLAP TRACK FAIRING CANOE EXTENDED BELOW WING. REMOVED AND REPLACED NR 2 OUTBOARD T/E FLAP TRACK FAIRING CANOE DRIVE ROD PER MM. 2L72 4F RTA16WE 20050616000352005061600035 2005 6 16 SWAA051661 420050603A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29715SW 27849 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050616000362005061600036NM 2005 6 16 SWAA051643 120050605A53206545410 FLOOR SUPPORT BOEING737 7373H4 1384600NM CABIN FLOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL FLOOR SUPPORT CRACKED AT BS 727A + 18, LBL 25, WL 208. REPAIRED FLOOR PER BFG ER. 2L72 4F RTA16WE 20050616000392005061600039NM 2005 6 16 SWAA051678 120050607A53306545769 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29352SW 24888 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT EQUIPMENT COOLING EXHAUST AFT CUTOUT, BS 378.13, LBL 2.80. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050616000402005061600040NM 2005 6 16 SWAA051679 120050607A53306545777 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29352SW 24888 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 25R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050616000422005061600042NM 2005 6 16 SWAA051681 120050607A3350207377 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29352SW 24888 DURING SCHEDULED C4 CHECK, FOUND LT & RT OVERWING EMERGENCY EXIT LIGHT LENSES LOOSE. SECURED LIGHT LENSES PER MM. 2L72 4F RTA16WE 20050616000432005061600043 2005 6 16 SWAA051682 420050607A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29384SW 26590 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20050616000452005061600045NM 2005 6 16 SWAA051684 120050607A335020131A BATTERY PACK BOEING737 7375H4 138449DNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29525SW 26567 DURING SCHEDULED SPECIAL VISIT, FOUND FWD, CENTER & AFT CABIN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACKS PER MM. 2L72 4F RTA16WE 20050616000462005061600046NM 2005 6 16 SWAA051673 120050607A55236959227 BUSHING BOEING737 7373H4 1384600NM LT ELEVATOR TAB WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29325SW 23689 DURING SCHEDULED C4 CHECK, LT ELEVATOR TAB FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR TAB NR 1 HINGE BUSHING & HARDWARE PER MM. 2L72 4F RTA16WE 20050616000472005061600047 2005 6 16 SWAA051674 420050607A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29347SW 24374 DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050621001342005062100134 2005 6 21 SWAA051765 420050616A256565C16820 HOOK BOEING737 7373H4 1384600NM L1 DOOR GIRT BARLOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED GIRT BAR HOOK PER MM. 2L72 4F RTA16WE 20050621001352005062100135NM 2005 6 21 SWAA051766 120050616A3350101073 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED C4 CHECK, FOUND EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 17. SECURED LENS PER MM. 2L72 4F RTA16WE 20050621001372005062100137NM 2005 6 21 SWAA051768 120050616A53116546532 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND 2 EA FUSELAGE FRAME CRACKS AT BS 480, STR 9L & STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050621001462005062100146NM 2005 6 21 DHL2005741547 120050414A575465172769 RIB BOEING727 7272Q9 138448MNM NR 4 SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 NR 4 SLAT I/B & O/B ROD END ATTACH RIBS CRACKED. REMOVED DAMAGED PARTS AND INSTALLED NEW IAW B727 SRM 51-30-2, AREA NR 4 SLAT I/B & O/B ROD END ATTACH RIBS. P/N 65-17276U11, PO 5079120 AND P/N 65-17276-9, PO 5079118. 2L73 4F RTA3WE 20050621001472005062100147NM 2005 6 21 2005UALA00450 120050517A5330 BEAR STRAP BOEING737 737322 1384676NM AFT CARGO DOOR DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29314UA 23675 AFT CARGO DOOR CUTOUT BEAR STRAP HAS PRE-EXISTING CUTOUT FOR REPAIR. *S/D* MAJOR REPAIR. INSTALLED DOUBLER-TRIPLER REPAIR PER SRM 53-00-01 FIG 230. 2L72 4F RTA16WE 20050621001612005062100161EA 2005 6 21 COMA0560341 120050608A7910 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA OIL SYSTEM ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01498CA 7792 FLIGHT 5701 - RIGHT ENGINE OIL PRESSURE WARNING. SERVICED RIGHT ENGINE WITH 3.5 QTS OIL, PERFORMED OIL CONSUMPTION RUN AND LEAK CHECK WITH SATISFACTORY RESULT. 2L72 4F RTA21EA 20050621001642005062100164EA 2005 6 21 COMA0570062 120050609A7830 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA THRUST REVERSER ILLUMINATED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01376CA 10092 FLIGHT 5173 - RIGHT THRUST REVERSER UNSAFE WARNING DURING AKEOFF.DEFERRED MAINTENANCE ON THRUST REVERSER PER MEL. 2L72 4F RTA21EA 20050621001762005062100176NM 2005 6 21 2005UALA00505 120050605A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29503UA 24624 AFT PIT LT SIDE STA 1440 FRAME HAS A DENT ON INBOARD FLANGE BETWEEN STR 25L AND 26L. REPAIRED FRAME WITH A FABRICATED PRODUCTION SPLICE ANGLE DOUBLER PER TIMCO REO(EVA) G10548, REV B. 2L72 4F4 FRTA2NM E17NE 20050621001822005062100182NM 2005 6 21 2005UALA00511 120050605A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP2953UA 25277 DENT IN FUSELAGE FROM APPROXIMATELY STATION 1720 TO 1701. DENT IS BETWEEN STRINGER 22L & 23L. INSTALLED DOUBLER PER SRM 53-00-01 REPAIR NR 3. 2L72 4F4 FRTA2NM E17NE 20050621001882005062100188NM 2005 6 21 2005UALA00519 120050606A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29128UA 30023 SEAT 41H EEL LIGHT IS INOP. SEAT 41H EEL LIGHT BURNED OUT - REPLACED. OK 2L74 4F4 FRTA20WE E24NE 20050621002002005062100200NE 2005 6 21 2005UALA00532 220050609A7200 ENGINE BOEING757 757222 1384956NM PWA 2037 PW2037 NE RIGHT MALFUNCTIONED A UALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 WP29574UA 26686 727200 DIVERTED DUE TO RT ENGINE OIL QTY AND PRESSURE IND. RT ENGINE SHUTDOWN. IN CRUISE LOSS OIL QTY & PRESSURE. CREW SHUTDOWN ENGINE. UPON LANDING FOUND EXHAUST OIL WETTED. ENGINE REMOVED. UPON DISASSEMBLY OF ENGINE FOUND NR 5 BEARING BAY HEAVILY COKED & NR 5 SCAVENGE LINE BLOCKED WITH COKE. UPON SEPARATION OF LPT FROM EXHAUST CASE FOUND NR 5 BEARING CARBON SEAL ASSEMBLIES CARBON ELEMENT SPINNING FREE WITH AXIAL PLAY BETWEEN FRONT & REAR SEAL PLATE ASSY. AXIAL PLAY DEMONSTRATES A INSUFFICIENT TORQUE OF THE SEAL PLATES IN THE ASSEMBLY. ROOT CAUSE OF THE OIL LOSS IS MISASSEMBLED NR 5 CARBON SEAL ASSY. 2L72 4F4 FRTA2NM E17NE 20050622000022005062200002NM 2005 6 22 BB05042 120050618A521065B08213X SPROCKET BOEING757 757225 1384959NM L2 DOOR MISINSTALLED A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19606AU 20008 22202 BFM - DURING HEAVY MAINTENANCE CHECK, FOUND THE L2 DOOR POWER ASSIST SPROCKET INSTALLED UP-SIDE DOWN. MAINTENANCE REINSTALLED THE SPROCKET CORRECTLY. 2L72 4F RTA2NM 20050622000122005062200012NM 2005 6 22 SWAA051799 120050619A534065C27314 STRINGER CLIP BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29508SW 24185 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 344, STR 10R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050622000322005062200032NM 2005 6 22 SWAA051798 120050619A5313BAC1498 STRINGER BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29508SW 24185 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2L72 4F RTA16WE 20050622000382005062200038NM 2005 6 22 SWAA051813 120050617A3150 PSEU BOEING737 7377H4 1384404NM WARNING HORN FAULTY A SWAAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW29756SA 27872 AIR TURNBACK/DECLARED EMERGENCY. TAKEOFF WARNING HORN SOUNDED AT ROTATION. T/E FLAP INDICATED SPLIT R- 5 DEGREES, L- 2 1/2 DEGREES. FLAPS WOULD NOT RESPOND TO FLAP HANDLE MOVEMENT IN FLIGHT. FOUND PSEU FAULT, C/W FIM TASK AND RESET AURAL WARNING CIRCUIT BREAKER PER MM. 2L72 4F RTA16WE 20050622000412005062200041CE 2005 6 22 ACE060305 120050603A2997MS24171D1 RELAY BEECH 1900 1900C 1154161CE HYD PUMP MALFUNCTIONED E YADAO OTHER J WARNING INDICATION APAPPROACH 1 AL03112AX UC45 PIREP - LANDING GEAR HANDLE HAD TO BE CYCLED SEVERAL TIMES BEFORE GEAR WOULD EXTEND. MAINTENANCE COULD NOT DUPLICATE. REPLACED HYDRAULIC PUMP MOTOR RELAY FOR T/S (COULD NOT VERIFY RELAY FAILURE). 2L72 4T RTA24CE 20050622000422005062200042CE 2005 6 22 DXTA200500778 120050615A324631538 WHEEL CESSNA750 750 2076810CE MLG VIBRATES E DXTAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 GL07930QS608 7500130 ON TAKEOFF, ACCELERATING THROUGH 70 KIAS AIRCRAFT VIBRATION OCCURRED THAT WAS SEVERE ENOUGH TO CAUSE DU1, DU2, AND DU3 TO MOMENTARILY BLANK. DU'S BACK ON LINE AFTER REJECTED TAKEOFF. REPLACED BOTH NOSE WHEEL ASSY IAW CE 750 M/M CHAP 32-41. NO DEFECTS NOTED, LT WHEEL ASSY P/N 3-1538-1, S/N OFF 0101, S/N ON 0243, RT WHEEL ASSY P/N 3-1538-1, S/N OFF 0428, S/N ON 0510. 2L72 4J RTT00007WI 20050622000442005062200044CE 2005 6 22 DXTA200500772 120050608A3240 O-RING RAYTHNDH125 HAWKER800XP 7150012CE BRAKE ASSY LEAKING E DXTAD RETURN TO BLOCK E VIBRATION/BUFFET TXTAXI/GRND HDL 1 GL07874QS 258474 WHEEL BRAKES GRABBY AT LOWER GROUND SPEEDS, PULSATES THROUGHOUT AIRCRAFT. GENERALLY BELOW 60 KNOTS. PERFORMED MAXARET FUNCTION TEST. FOUND NR 4 TO BE LEAKING. REMOVED & REPLACED O-RING & REINSTALLED IAW HAWKER 800XP AMM 32-40-101. NET JETS PILOTS FUNCTION CHECKED BRAKE SYSTEM AT HIGH SPEED & LOW SPEED FOLLOWING MAINTENANCE WITH NO DISCREPANCY IAW HAWKER 800XP AMM 32-40-00. 2L72 4F RTA3EU 20050622000472005062200047CE 2005 6 22 DXTA200500776 120050614A3230 LANDING GEAR CESSNA500 560CESSNA 2076750CE LT MAIN MALFUNCTIONED E DXTAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 GL07341QS 5600341 LEFT MAIN GEAR WOULD NOT RETRACT DURING GEAR RETRACTION. LEFT MAIN STAYED DOWN WITH GREEN INDICATION & RED GEAR UNSAFE LIGHT ILLUMINATED. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20050622000482005062200048CE 2005 6 22 DXTA200500780 120050617A3230 LANDING GEAR RAYTHNDH125 HAWKER800XP 7150012CE LT MAIN MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07873QS 258573 LEFT MAIN GEAR WOULD NOT RETRACT NORMALLY AFTER TAKEOFF. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA3EU 20050622000512005062200051NM 2005 6 22 SB05072 120050617A523010608211 SEAL BOEING737 7373B7 1384580NM FWD CARGO DOOR OUT OF TRACK A USAAG O2 MASK DEPLOYED J WARNING INDICATION CRCRUISE 1 EA19532AU 24479 CABIN ALTITUDE WARNING HORN ACTIVATED AS ACFT BEGAN A SLOW UNCONTROLLABLE CLIMB IN CABIN PRESSURE. OUTFLOW VALVE REPORTED TO BE CLOSED ENTIRE TIME. CREW DESCENDED FLIGHT TO 14,000 FT WHERE PRESSURE STABILIZED. O-2 MASKS DEPLOYED AS A PRECAUTION. FLT LANDED AT CLT WITHOUT FURTHER INCIDENT. NO EMERGENCY DECLARED. MX FOUND FWD CARGO DOOR SEAL OUT OF RETAINER TRACK. RESECURED SEAL & REPAIRED SEVERAL LEAKS ALONG SERVICE DOORS & ENTRY DOORS. R & R AFT OUTFLOW VALVE DUE TO LEAKAGE PER MM. REPLACED ALL DEPLETED OXYGEN GENERATORS AND REPACKED MASKS. ACCOMPLISHED PRESSURIZATION CHECK JOB CARD J321-30-00. ALL INDICATIONS ARE WITHIN LIMITS. AIRCRAFT OK FOR SERVICE. 2L72 4F RTA16WE 20050622000622005062200062NM 2005 6 22 QXEA200501055 120050601A5330 SKIN BOMBDRDHC8 DHC8402 1390042NM ZONE 100 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09415QX 4081 PDX - RT FUSELAGE SKIN HAS ONE NICK ALONG STRINGER 37X AT X17.85. REPAIRED IAW RD 8/4-53-505. 2H72 4T RTA13NM 20050622000732005062200073NM 2005 6 22 USAA200506001 120050607A5330 SKIN BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19777 3.2 INCH CRACK FOUND AT BS 727E S23R. REPAIR DOUBLER PER SRM 53-00-01. 2L72 4F RTA16WE 20050622000852005062200085NM 2005 6 22 QXEA200500983 120050404A2750 LIGHT BOMBDRDHC8 DHC8402 1390042NM FLAP CONTROL SYSFALSE INDICATIONA QXEAO OTHER N FALSE WARNING APAPPROACH 1 NM09403QX 4037 FLAP POWER CAUTION LIGHT IN FLIGHT AFTER SELECTING FLAPS 5 DEGREES. ACCOMPLISHED CHECKLIST, FLAPS RESET. NO CAUTION LIGHT UPON MX ARRIVAL. NO FAULTS IN CDS. FLIGHT CREW INDICATED NO FURTHER FAULTS AFTER RESET. NO PARTS REPLACED. ACFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050622000882005062200088NM 2005 6 22 QXEA200501052 120050604A5347 SEAT TRACK BOMBDRDHC8 DHC8402 1390042NM ZONE 200 WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09415QX 4081 PILOTS INBOARD SEAT TRACK HAS WEAR ON TOP SURFACE. REPAIRED IAW Q400 SRM 51-40-07, AMM TASK 25-11-01-00-801, SRM 51-42-15, 51-25-10 AND 25-11-01. 2H72 4T RTA13NM 20050622000952005062200095NM 2005 6 22 QXEA200501057 120050528A5753 SKIN BOMBDRDHC8 DHC8402 1390042NM ZONE 600 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09415QX 4081 RT INBOARD FLAP CHAFED ON INBOARD SIDE TOP SIDE 6 INCHES FROM FUSELAGE. REPAIRED IAW DHC 8 400 SRM 51-14-00 AND HORIZON AIR EA +-57-331. 2H72 4T RTA13NM 20050622000982005062200098CE 2005 6 22 DXTA200500753 120050603A3233AIR48502 ACTUATOR RAYTHNDH125 HAWKER800XP 7150012CE LT MLG MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07873QS2338 258573 LT MLG CAME UP ABOUT HALF WAY AND STOPPED. SAME INDICATION AS PREVIOUS WRITE-UP. LT MLG RED LIGHT. NO OTHER LIGHTS OR HORN. LANDED AT 22000 LBS WEIGHT. CHANGED LT MLG ACTUATOR MM 32-30-27. CYCLED GEAR 10 TIMES. LEAK CHECK AND OPS OK 2L72 4F RTA3EU 20050622001042005062200104NM 2005 6 22 QXEA20051021 120050521A242031708011A GENERATOR BOMBDRDHC8 DHC8402 1390042NM NR 2 FAILED A QXEAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM09539DS6464 5271 4016 AFTER PUSHBACK AND TAKING PROPS OUT OF FEATHER, NR 2 AC GENERATOR CAUTION LIGHT ILLUMINATED. CHECKED ALL C/B'S TO MAKE SURE THEY WERE IN. COMPLETED NR 2 AC GENERATOR CHECKLIST. LIGHT DIDN'T EXTINGUSH. REMOVED AND REPLACED NR 2 AC GENERATOR. OPS CHECK GOOD. ACFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050622001092005062200109SO 2005 6 22 SIMA200515703 120050525A532014525381003 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21646AE 145213 ABI - DURING AN MBV INSPECTION, A PREVIOUS REPAIR ON FRAME 20 AT THE LEFT OMEGA BEAM WAS FOUND CORRODED. REMOVED THE PREVIOUS REPAIR PARTS TO REMOVE THE CORROSION. FABRICATED A DOUBLER, PLATE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 29, CHAPTERS 53-21-10 AND 51-40-02. (M) 2L72 4T RTT00011AT 20050622001112005062200111EU 2005 6 22 ASOA05452 120050520A3350LP1670 LAMP AEROSPATR72 ATR72 EU EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27630AS 336 DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY FLOOR LIGHT STRIP JUST FORWARD OF SEAT 14D WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY FLOOR LIGHT STRIP JUST FORWARD OF SEAT 14D. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20050622001352005062200135EU 2005 6 22 USAA050719 120050523A5320 FLOOR SUPPORT AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19717UW 1069 FOUND FLOOR SUPPORTS CORRODED 2 INCHES BY 2 INCHES, Y1292 R BETWEEN FRAME 66 AND 69. CORROSION LEVEL 2, TASK JA-260-53500. DEFECTIVE PART REPLACED WITH IDENT PART. (M) 2L72 4F RTA28NM 20050622001462005062200146EU 2005 6 22 USAA050721 120050521A5311 FRAME AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19717UW 1069 PIT - FOUND FRAME CORRODED 2 INCH BY 1 INCH AREA, TOP OF FRAME 17 - Y31. FABRICATED REPAIR ANGLES PER SRM 53-11-15. (M) 2L72 4F RTA28NM 20050622001492005062200149EU 2005 6 22 USAA050720 120050521A5315 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19717UW 1069 PIT - FOUND FLOORBEAM ANGLE BRACKET CORRODED 2 INCHES BY 1 INCH, FRAME 17 - Y 31 INCH. CORROSION LEVEL 2, TASK JA-220-53500. FABRICATED ANGLE BRACKET PER SRM 53-11-15. (M) 2L72 4F RTA28NM 20050622001512005062200151SO 2005 6 22 SIMA200513102 120050508A2720626249101 PRESSURE SWITCH EMB 145 EMB145LR 3260212SO RUDDER CONTROL INOPERATIVE A SIMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21632AE 145143 DFW - FLT 3359 - CREW REPORTED THE RUDDER SYSTEM 1-2 FAILED AFTER TAKEOFF AT BETWEEN 150-170 KNOTS. MECHANICAL REVERSION WAS CHECKED THROUGH RUDDER. DIDN’T SEEM OVERLY STIFF. COMPLETED AOM CHECKLIST AND RETURNED TO FIELD. MAINTENANCE REMOVED AND REPLACED RUDDER SYSTEM 2 PRESSURE SWITCH IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20050622001522005062200152NM 2005 6 22 USAA050714 120050601A5320 INTERCOSTAL BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19445US40360 24863 CLT - FOUND INTERCOSTAL CORRODED 6 INCHES, AFT CARGO COMPARTMENT INTERCOSTAL AT INBOARD SIDE OF DOOR SILL. FABRICATED AND INSTALLED A NEW INTERCOSTAL IAW BOEING DRAWING 65-47957 AND SRM 51-10-02. (M) 2L72 4F RTA16WE 20050622001692005062200169EA 2005 6 22 ASOA05394 120050502A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27884AS 7513 DURING HANGAR MAINTENANCE IN MCN, THE FORWARD EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A LAMP IN THE FORWARD EMERGENCY CEILING LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050622001792005062200179EA 2005 6 22 ASOA05438 120050514A3350362624 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27838AS 7276 DURING HANGAR MAINTENANCE IN BTR, THE EMERGENCY FLOOR TRACK LIGHTING AT ROW 5 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A BROKEN EMERGENCY FLOOR LIGHT STRIP AT ROW 5. OPERATIONAL CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050622001902005062200190EA 2005 6 22 ASOA05437 120050514A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27930EV 8014 DURING A GROUND INSPECTION IN CAE, THE LOWER EMERGENCY EXIT SIGNS AT ROW 8 ON BOTH SIDES WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMPS IN THE LOWER EMERGENCY EXIT SIGNS AT ROW 8 ON BOTH SIDES. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050622001912005062200191EA 2005 6 22 ASOA05435 120050514A52106003145017 BEARING CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BINDING A ASOAK NONE O OTHER ININSP/MAINT 1 SO27832AS 7243 FLT 4358 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WAS FOUND DIFFICULT TO OPEN AND CLOSE. MAINTENANCE REMOVED AND REPLACED THE AFT ROLLER BEARINGS ON THE PASSENGER DOOR. OPERATIONAL CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050622001962005062200196EU 2005 6 22 ASOA05408 120050507A33507012210 LAMP AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27633AS 344 DURING HANGAR MAINTENANCE IN MCN, THE AFT TWO MINUTE EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE AFT TWO MINUTE EMERGENCY EXIT LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20050622002032005062200203EA 2005 6 22 MASA200500228 120050317A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA MAIN PAX STUCK A MASAO OTHER O OTHER TXTAXI/GRND HDL 1 SW0727172 7172 ASH 2629 FROM PHL TO YYZ AFTER ARRIVAL THE FLIGHT ATTENDANT COULD NOT OPEN THE MAIN PASSENGER DOOR. CONTRACT MX ATTEMPTED TO FIX THE DOOR BUT DID NOT SUCCEED. ATTEMPT WAS MADE TO FERRY TO PHL BUT DUE TO CUSTOMS DEICING AND FUELING ISSUES THE AIRCRAFT WAS GROUNDED IN YYZ. CONTRACT MX WILL TRY TO FIX, IF UNSUCCESSFUL, AIRCRAFT WILL FERRY TO PHL. 2L72 4F RTA21EA 20050622002092005062200209EA 2005 6 22 MASA200500111 120050214A5100 UNKNOWN CNDAIRCL600 CL6002B19 1900309EA UNKNOWN A MASAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SW0775998 7336 ASH 7111 CLE TO IAD ABORTED TAKEOFF DUE TO THE AIRCRAFT PULLING TO THE LEFT WITH FULL RIGHT RUDDER DEFLECTION. 2/15/05 MAINTENANCE PERFORMED NOSE WHEEL STEERING SYSTEM ECU ADJUSTMENT CHECK IAW CRJ 200 AMM 32-51-10, OPS CHECKED GOOD. 2L72 4F RTA21EA 20050622002132005062200213 2005 6 22 MASA200500152 420050223A34106229336400 AHRS CNDAIRCL600 CL6002B19 1900309EA NR 1 FAILED A MASAO OTHER I FLT. ATTITUDE INST. APAPPROACH 1 SW07171563202 7156 ASH 2736 PHL - MCI. ON APPROACH CAPTAINS SIDE INSTRUMENTS FAILED. CPT DECLARED EMERGENCY AND LANDED UNEVENTFULLY. MAINTENANCE REPLACED NR 1 AHARS. OPS CHECK GOOD. 2L72 4F RTA21EA 20050622002152005062200215NM 2005 6 22 CALA0500200 120050616A3350ADD71701100 BATTERY PACK BOEING737 737724 13844BYNM EMERGENCY LIGHT INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2713720 28939 A SECTION OF EMERGENCY TRACK LIGHTS IN AFT CABIN WERE FOUND INOPERATIVE. THE BATTERY PACK IN AFT CEILING (A/C LEFT) WAS REMOVED AND REPLACED. 2L72 4F RTA16WE 20050622002282005062200228WP 2005 6 22 DHL2005807545 120050525A5313S2641455 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH86990 45990 FUSELAGE CTR SECTION LONGERON 34R CORRODED (STA 1400.000-1440.000) (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CORROSION FROM L-34R (STA 1400.000-1440.000) IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED L-34R IAW SRM 51-1-20D PG 21. FABRICATED NEW LONGERON (EXTRUSION P/N S2641455, 7075T6511) IAW SRM 53-4-1 FIG 43A ITEM "K", SRM 51-2-0 FIG 50, HEAT TREATED IAW SRM 51-1-1 PG 1, 13, 17, DPS 7.00-1 REV "BK", SRM 51-1-4 PG 1, DPS 3.69-4 REV "AM" R-1. PERFORMED NDT INSP IAW NDT SPM PART 08-00-02 TO 07. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW LONGERON IAW SRM 51-1-20D PG 9. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050622002292005062200229WP 2005 6 22 DHL2005807541 120050520A2721 HINGE DOUG DC8 DC873F 302199FWP RUDDER TAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH86990 45990 RUDDER CONTROL TAB HINGE NR 3 CRACKED. REMOVED RUDDER TAB IAW MM 27-21-2 PG 201-202. REMOVED AND REPLACED NR 3 HINGE BRACKET IAW SRM 51-1-21 PG 1-2. REINSTALLED RUDDER TAB IAW MM 27-21-2 PG 202-205. ADJUSTED RUDDER TRIM CONTROL SYSTEM IAW MM 27-20-0 PG 505-506. INSPECTED AND CHECKED RUDDER AND TAB IAW MM 27-21-1 PG 601-605. REFER TO NR 036397 FOR OPS CHECK. 2L74 4F RT4A25 20050622002372005062200237NM 2005 6 22 DHL2005784502 120050515A5754 SKIN BOEING727 727227 1384078NM NR 3 SLAT DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01784DH 22001 NR 3 SLAT UPPER SKIN IS DENTED AT WING STA.495. EVALUATED AREA TO BE CREASED AND OUT OF LIMITS IAW B727 SRM 57-50-1 FIG 2. CUT OUT DAMAGED AREA AND FABBED FILLER IAW B727 SRM 57-50-3 FIG 1 REPAIR 4. REPAIR PARTS TREATED AND PRIMED IAW B727 SRM 51-10-2 AND INSTALLED IAW B727 SRM 57-50-3 FIG 1, REPAIR 4. 2L73 4F A3WE 20050622002402005062200240NM 2005 6 22 DHL2005784504 120050515A5753 SKIN BOEING727 727227 1384078NM TE FLAP DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01784DH 22001 LT INBD FORE FLAP IS DELAMINATED ON LOWER SURFACE, WBL 124. REMOVED LT I/B FORE FLAP IAW B727 MM 27-51-00. CUT OUT DELAMINATED AREA AND FABBED FILLER 2 INCH DIA AND DOUBLER AND BONDED REPAIR PARTS IAW B727 SRM 57-50-2 FIG 3 AND 51-40-20 FIG 3. REINSTALLED LT INBOARD FORE FLAP IAW B727 MM 27-51-00, OPS CHECK GOOD IAW B727 MM 27-51-00. 2L73 4F A3WE 20050622002452005062200245NM 2005 6 22 DHL2005784508 120050516A5755 SKIN BOEING727 727227 1384078NM SPOILER DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01784DH 22001 NR 7 SPOILER PANEL HAS SMALL DELAMINATION AT INBD TRAILING EDGE CORNER AND TRAILING EDGE PHENOLIC RUB STRIP IS LOOSE AND PEELING OFF, AT WBL 90. REPAIRED. 2L73 4F A3WE 20050622002462005062200246NM 2005 6 22 DHL2005784509 120050516A5311 FRAME BOEING727 727227 1384078NM FUSELAGE BENT A DHLAK NONE O OTHER ININSP/MAINT 1 SO01784DH 22001 FWD CARGO FRAME AT BS 680 RIGHT, BENT ABOVE STR 27R TO STR 26R. FOUND DENT TO BE OUT OF LIMITS. CUT OUT DAMAGED AREA, SIZE 1 3/4" BY 1" IAW B727 SRM 53-10-1 FIG 1. FABRICATED ANGLE REPAIR USING 7075-T6 .063 PO 900489, DIM 14 3/16" BY 3 5/8" IAW B727 SRM 53-10-2 FIG 3. ALODINE AND PRIME PART AND AREA IAW B727 SRM 51-10-2. INSTALLED PART IAW B727 SRM 51-40-3 FIG 1. 2L73 4F A3WE 20050622002482005062200248NM 2005 6 22 DHL2005784511 120050517A5500 SKIN BOEING727 727227 1384078NM EMPENNAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01784DH 22001 EMPENNAGE SKIN CREASED BS 1243 AT STR.24R DAMAGED AREA FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-30-1 FIG 1. WITH NO DEFECTS NOTED TO STRINGER. REPAIED IAW B727 SRM 51-10-2 AND 53-30-3 FIG 3. 2L73 4F A3WE 20050623000012005062300001WP 2005 6 23 AALA20050384 120050611A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21296AA 49308 DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT 16D AND 18D HAS ONE LAMP INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT 16D AND 18D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050623000202005062300020EA 2005 6 23 MASA200500423 120050531A3230 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA MLG MALFUNCTIONED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07653ML 7039 ASH 2836 PHL. A GEAR DISAGREE MESSAGE DISPLAYED ON EICAS UPON GEAR EXTENSION. THE CREW ADVISED THAT THE GEAR CAME DOWN AFTER 20 SECONDS. THE AIRCRAFT WAS FERRIED TO PHL WHERE MX COULD NOT DUPLICATE THE FAULT. MX REPLACED THE PRIORITY VALVE, SELECTOR VALVE AND GEAR DOOR SEQUENCING VALVE FOR PREVENTITIVE MX. 2L72 4F RTA21EA 20050623000222005062300022EA 2005 6 23 MASA200500442 120050605A5210 TORQUE TUBE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR OUT OF ADJUST A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0737178 7178 ASH 6460 PHX. MAIN CABIN DOOR THAT WOULD NOT OPEN UPON ARRIVAL. ADJUSTED LATCH TORQUE TUBE ROD END. 2L72 4F RTA21EA 20050623000592005062300059 2005 6 23 ASMF200506005 420050603A34189650449002 COMPUTER DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE STALL WARNING FAILED W ASMFC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW23583MD7944 49659 AIRCRAFT RETURNED OF FLIGHT, AFTER ROTATION, THE DISAGREE IN SLAT PANEL, AUTO SLAT FAIL AND STALL INDICATION FAILURE IN ANNUNCIATOR PANEL LIGHTS COME ON. BOTH COMPUTERS WERE VERIFIED AND IN THE NR 1 APPEARED SIF LIGHT WITH FAILURE AND IN THE NR 2 AUTO SLAT LIGHT COME ON. BOTH STALL WARNING COMPUTERS AND LT ATTACH ANGLE SENSOR WERE REPLACED IAW MM 34-19-01 / 02 RESPECTIVELY, TESTED CORRECT. 2L72 4F4 FRTA6WE E9NE 20050623000602005062300060NE 2005 6 23 ASMF200506006 220050604A75323830041105 BLEED VALVE BOEING757 757200 1384950NM PWA 2037 PW2037 NE LT ENGINE FAILED W ASMFC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW23703AM27826 27203 726736 CAPTAIN REPORTED THAT DURING TAKEOFF, THE LT ENGINE EGT REACHED 647 DEGREE C. AIRCRAFT WAS SENT TO THE HANGAR AND LT ENGINE 2.5 BLEED ACTUATOR WAS REPLACED IAW MM 75-32-01 AND TESTS WERE PERFORMED IAW MM 71-00-00, ALL CORRECT. DURING OVERNIGHT SERVICE, THE LT ENGINE BAROSCOPIC INSPECTION WAS PERFORMED TO THE COMBUSTION CHAMBERS AND T1, T2 AND T3 UPPER AND LOWER TURBINES. NO DAMAGES WERE FOUND IAW MPCM 72-00-00. 2L72 4F4 FRTA2NM E17NE 20050623000612005062300061WP 2005 6 23 ASMF200506007 120050604A2720 SENSOR DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE RUDDER TRAVEL DIRTY W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23205AM 49405 AIRCRAFT RETURNED TO PLATFORM, DURING TAXING AND FLIGHT CONTROL TESTS THE RUDDER TRAVEL UNRESTRICTED LIGHT TURNED OFF. THE D1-33 AND D1-34 TARGET SENSORS WERE CLEANED AND ADJUSTED IAW MM 27-20-00, TESTED CORRECT. DURING OVERNIGHT SERVICE, THE TARGET SENSORS OF RUDDER TRAVEL UNRESTRICTED LIGHT WERE TESTED IAW MM 27-20-00, ALL CORRECT. 2L72 4F4 FRTA6WE E9NE 20050623000622005062300062NM 2005 6 23 ASMF200506008 120050605A7930 WARNING LIGHT BOEING737 737* NM CFMINTCFM567CFM567B22 13802NE RT ENGINE OIL ILLUMINATED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23851AM 33789 891646 AIRCRAFT RETURNED TO PLATFORM, RT ENGINE LOW OIL PRESSURE INDICATION DURING TAXING. RAN ENG CONNECTOR AND SWAP / CHANGE TRANSMITTER CHANNEL WERE CLEANED IAW MM 72-00-00, TESTED CORRECT. DURING OVERNIGHT SERVICE, THE NON ROUTINE CARD A0077753 WAS ISSUED FOR PERFORM BITE TO THE RT ENGINE CDU AND LOW OIL PRESSURE TEST IN RT ENGINE TO RED OR AMBER ZONES. 2L72 4F4 FRTA16WE E00055EN 20050623000632005062300063NM 2005 6 23 ASMF200506004 120050603A3213 STRUT BOEING737 737* NM GE CFM56 CFM56* 13802NE NLG LEAKING W ASMFK NONE K FLUID LOSS ININSP/MAINT 1 SW23904AM 28262 DURING OVERNIGHT SERVICE, WAS DETECTED AN HYDRAULIC LEAK IN SHOCK STRUT OF NOSE LANDING GEAR. THE SEALS WERE REPLACED BUT WHEN TAKING OUT THE PISTON, A BUSHING WAS DETECTED DAMAGED. THE SHOCK STRUT OF NOSE LANDING GEAR SEALS WERE REPLACED IAW MM 32-21-11, TESTED CORRECT. 2L72 4F4 FRTA16WE E2GL 20050623000652005062300065NE 2005 6 23 T48R20050012 220050612A7200798404 BLADE DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE NR 2 ENGINE FRACTURED B GTIAK NONE O OTHER ININSP/MAINT 1 GL09821NK 4500 49508 718446 ENGINE WAS REMOVED FROM 821NK NR 2 POSITION FOR VISIBLE TURBINE DAMAGE. INSPECTION REVEALED THE T-4 BLADES MISSING/FRACTURED AT THE BASE OF BLADE WITH CORRESPONDING DAMAGE TO THE T-3 VANES. 2L72 4F4 F A6WE E9NE 20050623000662005062300066EA 2005 6 23 A6WA200540189 120050530A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31418AW 7618 THE LT AND RT SIDE UNDERFLOOR SUPPORT ANGLE IS CRACKED 1.0 INCH AT FS 621, LBL 40 AND RBL 40, WL 73. REPAIRED INTERCOSTALS IAW REO. (K) 2L72 4F4 FRTA21EA E15NE 20050623000682005062300068EU 2005 6 23 KBM2005F00103 120050530A6710123668P BALL JOINT SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1D NE MAIN ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1953SH 2009 BALL JOINTS, BOTH WORN, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050623000722005062300072EU 2005 6 23 KBM2005F00107 120050530A6510350933215300 BEARING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1B 6OO30NE TAIL ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH774 2957 LAMINATED BEARINGS ARE WORN, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050623000732005062300073EU 2005 6 23 KBM2005F00110 120050601A2197 WIRE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE FAN MISWIRED E KBMAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 WP19351WM 2167 ELECTRICAL BOX, FAN MOTORS ARE HOT WIRED. WRONG INTERNAL WIRE CONNECTION. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050623000752005062300075EA 2005 6 23 5336002 120050613A261324412047 FIRE LOOP CNDAIRCL600 CL6002B16 1900305EA LT TAILPIPE FAULTY E ERYAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE07212RR7098 5336 DURING NORMAL CRUISE, LH JET PIPE OVERHEAT ANNUNCIATOR ILLUMINATED. FOLLOWED CHECK LIST AND RETURNED TO AIRPORT FOR UNEVENTFUL LANDING. TROUBLESHOT PROBLEM TO DEFECTIVE FIRE LOOP. REPLACED FIRE LOOP, OPS CHECK, RETURN A/C TO SERVICE. 2L72 4F RTA21EA 20050623000762005062300076NE 2005 6 23 C1HA200583002 220050612A7230 COMPRESSOR BOEING727 7272S7 138407ZNM PWA JT8 JT8D* NE NR 2 ENGINE STALLED A C1HAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION LDLANDING 1 GL15683CA 22490 688761 NR 2 ENGINE COMPRESSOR STALL DURING APPROACH WHILE FULLY CONFIGURED AND 1.4 EPR PERFORMED VISUAL INSPECTION OF INLET AND EXHAUST. PERFORMED ENGINE RUN AT VARIOUS POWER SETTINGS. PERFORMED ACCEL AND DECEL CHECK. CHECKED ANTI-SURGE BLEED VALVE SCHEDULING ALL PARAMETERS NORMAL REF. MM 71-00-00 OK FOR SERVICE 2L73 4F4 F A3WE E2EA 20050623000772005062300077NM 2005 6 23 P5CA0501363 120050531A2782178800106 ACTUATOR BOEING747 747230B 1384889NM L/E DEVICES FAILED A P5CAK NONE O OTHER ININSP/MAINT 1 EA15508MC 21644 NR 22 LEADING EDGE PANEL BROKEN. REPLACED NR 22 LEADING EDGE PANEL, 2 ROTARY ACTUATORS AND TORQUE TUBE. RIGGED AND OPS CHECK IAW MM 27-81-00. 2L74 4F A20WE 20050623000782005062300078EA 2005 6 23 SWIA200515129 120050612A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA RT SPOILER MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07441SW 7602 FLIGHT SPOILER FAULT STATUS MSG. REPLACED RT OUTBOARD FLIGHT SPOILER PCU IAW AMM 27-62-01. OPS CHECK GOOD, PN 27000-7 SN/OFF MAL-5097. 2L72 4F RTA21EA 20050623000822005062300082SO 2005 6 23 SWIA200515133 120050613A27523431001001 ACTUATOR EMB 120 EMB120ER 3260203SO NACELLE FLAPS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07234SW1101211012 120308 WHEN RETRACTING FLAPS AFTER LANDING, FLAP DISAGREEMENT. R & R LT NACELLE FLAP ACTUATOR IAW 27-50-00 CMM. OPS CHECK GOOD. 2L72 4T RTA31SO 20050623000832005062300083SO 2005 6 23 SWIA200515134 120050608A2720 ACTUATOR EMB 120 EMB120ER 3260203SO RUDDER CONTROL MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07217SW 120286 RT RUDDER PEDAL JAMMED EN ROUTE. R & R RUDDER PCU, GREEN HYD SYSTEM RUDDER ACTUATOR, AND BLUE HYD SYSTEM RUDDER ACTUATOR IAW AMM 27-22-20; 27-22-02; 27-22-01. OPS CHECK GOOD, 2L72 4T RTA31SO 20050623000842005062300084EA 2005 6 23 SWIA200515135 120050608A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07457SW 7773 MIDDLE LT EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED MIDDLE LT EXTERIOR EMERGENCY LIGHT. OPS CHECK GOOD IAW AMM 33-51-21. 2L72 4F RTA21EA 20050623000852005062300085EU 2005 6 23 0500813242 120050613A2120 ODOR AIRBUS320 A320212 3930322EU CABIN DETECTED A NWAABA EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL01342NW 381 ELECTRICAL ODOR IN CABIN. ODOR THEN DETECTED IN COCKPIT. DIVERTED AND LANDED UNEVENTFULLY. ODOR CONTINUED THROUGHOUT FLIGHT. INSP ACFT INTERIOR, PERFORMED CIDS TEST OF LIGHTING SYSTEM WITH NO DEFECTS FOUND. ALL CIRCUIT BREAKERS VERIFIED CLOSED. INSP CARGO AND E/E COMPARTMENTS WITH NO DEFECT FOUND. RAN AIR CONDITIONING PACKS. NO ODOR NOTED. ACFT RETURNED TO SERVICE. 2L72 4F RTA28NM 20050623000862005062300086SO 2005 6 23 CHQA200500113 120050613A2710 WARNING LIGHT EMB 135 EMB135KL 3260302SO AILERON CONTROL ACTIVATED A CHQAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL11299SK 145532 DURING CLIMB AT FL210, RECEIVED "AILERON SYS 1 FAIL" EICAS MESSAGE. LEVELED OFF AT FL230 AND TOLD ATC TO STAND BY. FOLLOWED QRH AND TURNED OFF AILERON SYSTEM 1 AND SLOWED TO 250 KIAS. EMERGENCY DECLARED WITH ATC AND F/A PREPARED CABIN FOR EMERGENCY LANDING. LANDED WITHOUT FURTHER INCIDENT. MX TROUBLESHOT ACFT AND COULD NOT DUPLICATE FAULT. OPS CHECK GOOD IAW EMB AMM. 2L72 4F RTT00011AT 20050623000882005062300088WP 2005 6 23 0500809856 120050601A291339563751 PUMP DOUG DC9 DC951 3022051WP HYDRAULIC SYS LEAKING A NWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL01765NC 47718 AFTER ACFT LEVELLED OFF AT FL 290, PILOT NOTICED DROP IN RT HYDRAULIC SYSTEM QUANTITY FROM 6 QTS TO 4 QTS. QUANTITY CONTINUED TO SLOWLY DECREASE AND WHEN REACHED 2 QTS COM PROCEDURES WERE COMPLIED WITH. CREW REQUESTED LONGEST RUNWAY. GEAR EXTENSION NORMAL BUT RT SYSTEM QUANTITY WAS "0" QTS, ACFT LANDED WITHOUT INCIDENT. MX REPLACED RT ENGINE DRIVEN PUMP AND CASE DRAIN (DUE TO FAILED CASE DRAIN PIPE), AUX PUMP, AND QUANTITY INDICATOR. LEAK CHECKS GOOD AND ACFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050623000902005062300090EA 2005 6 23 QXEA200500990 120050416A5270 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA APU DOOR ILLUMINATED A QXEAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM09613QX 10045 ON TAXI OUT, RECEIVED APU DOOR OPEN CAUTION UPON APU SHUTDOWN. COMPLIED WITH EMERGENCY CHECKLIST. COMPLETED FLIGHT WITH APU RUNNING. MX REPLACED RVDT. FUNCTIONAL TESTED GOOD THROUGH SEVERAL CYCLES. ACFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20050623000912005062300091WP 2005 6 23 DXTA200500749 220050601A73108975131 FUEL FILTER RAYTHNDH125 HAWKER800XP 7150012CE GARRTTTFE731TFE7315BR WP RT ENGINE CONTAMINATED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07867QS 258576 P107690 ON T/O RT ENGINE FUEL ANNUNICATOR ILLUMINATED. REMOVED RT ENGINE FUEL FILTER ELEMENT, P/N NR 897513-1 AND FILTER HOUSING O-RING P/N NR M25988/1-134 AND INSTALLED NEW FILTER AND O-RING, SAME P/N NRS. RAN ACFT RT ENGINE FOR 25 MINUTES AND NO RT ENGINE FUEL ANNUNCIATOR CAME ON, LEAK CHECK OF FILTER HOUSING, FITTINGS, AND LINES GOOD. NO LEAKS NOTED. WORK PERFORMED IAW HONEYWELL LIGHT MM. 2L72 4F4 FRTA3EU E6WE 20050623000922005062300092CE 2005 6 23 DXTA200500751 120050602A3210 LANDING GEAR RAYTHNDH125 HAWKER800XP 7150012CE LEFT MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07873QS 258573 LT MLG WOULD NOT COME UP AFTER DEPARTURE. JACKED ACFT AND PERFORMED EXTENSION AND RETRACTION CHECKS PER HAWKER 800 XP MM CHAPTER 32-30-00. COULD NOT DUPLICATE LT GEAR FAILURE. PERFORMED 10 FAULT FREE RETRACTIONS. SERVICED HYDRAULIC SYSTEM PER CHAPTER 12-29-00 PAGE 306. 2L72 4F RTA3EU 20050623000942005062300094NM 2005 6 23 QXEA200501029 120050609A242123088002B GENERATOR DHAV DHC8 DHC8202 2809007NM ZONE 200 MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION APAPPROACH 1 NM09354PH2984 43 498 NR 2 AC GENERATOR CAUTION LIGHT ILLUMINATED ON APPROACH AS STANDBY HYDRAULIC PUMPS WERE SELECTED ON. CYCLED NR 2 AC GENERATOR SWITCH AS PER EMERGENCY CHECKLIST. LIGHTS EXTINGUSHED. REPLACED NR 2 AC GENERATOR. OPS CHECK GOOD. ACFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050623000952005062300095NM 2005 6 23 QXEA200501030 120050609A5210 DOOR DHAV DHC8 DHC8202 2809007NM ZONE 200 LACK OF LUBE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09366PH 510 MAIN CABIN DOOR DIFFICULT TO OPEN FROM INSIDE. LUBRICATED DOOR HINGE POINTS AND LATCH MECHANISM. NO PARTS REPLACED. ACFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050623000962005062300096SO 2005 6 23 RAIA00505027 120050527A2197 WIRE EMB 145 EMB145LR 3260212SO CABIN PRESS SYS BROKEN A RAIAA UNSCHED LANDING O OTHER CLCLIMB 1 CE03834HK 145269 COULD NOT MAINTAIN CABIN PRESSURE. MX REPAIRED BROKEN WIRE. SYSTEM OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050623000972005062300097NM 2005 6 23 QXEA200501006 120050604A3297471515 WIRE HARNESS BOMBDRDHC8 DHC8402 1390042NM NR 2 NLG WOW MALFUNCTIONED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09413QX410 4060 AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. ACFT RETURNED AND ACCOMPLISHED UNEVENTFUL LANDING. MX REPLACED WOW NR 2 NLG HARNESS. OPS CHECKS GOOD. ACFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050623000992005062300099EA 2005 6 23 VTZA200500096 120050531A3244DR27921T TIRE CNDAIRCL600 CL6002B19 1900309EA LT MLG FAILED A VTZAO OTHER O OTHER LDLANDING 1 EA27659BR 196 7509 NR 2 MAIN TIRE TREAD SEPARATED ON TAKEOFF CAUSING DAMAGE TO LEFT INBOARD FLAP. 2L72 4F RTA21EA 20050623001002005062300100NM 2005 6 23 UPS05444579 120050516A531569B142725 FLOORBEAM BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE: C, BS 1100 RBL 80-95 FLOORBEAM, FOUND CORRODED. CORROSION BLENDED OUT FLOORBEAM UPPER TEE REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050623001012005062300101NM 2005 6 23 QXEA200501008 120050606A323154C546349 SOLENOID VALVE DHAV DHC8 DHC8202 2809007NM LT MLG DOOR MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09374PH13851 528 DURING CRUISE (225 KNOTS), LT MLG DOOR OPENED FULLY. GEAR HANDLE WAS IN THE "UP" POSITION. PERFORMED ALTERNATE GEAR EXTENSION AND LANDED WITHOUT FURTHER INCIDENT. ACFT FERRIED FOR REPAIRS. MX REPLACED SOLENOID VALVE. OPS CHECKS GOOD. ACFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050623001032005062300103NM 2005 6 23 QXEA200501011 120050530A33506138001 BATTERY PACK BOMBDRDHC8 DHC8402 1390042NM EMERGENCY LIGHTSINOPERATIVE A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09405QX3527 1592 4047 EMERGENCY LIGHTS INOP. MX REPLACED BATTERY PACK ASSEMBLY. OPS CHECK GOOD. ACFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050623001052005062300105NM 2005 6 23 QXEA200501010 120050604A33506519020 LIGHT DHAV DHC8 DHC8202 2809007NM CABIN INOPERATIVE A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09362PH 518 EMERGENCY LIGHTS AT ROW 1 INOP. MX REPLACED LIGHT SEGMENT AS REQUIRED. OPS CHECKS GOOD. ACFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050623001062005062300106NM 2005 6 23 QXEA200501013 120050425A2434 GENERATOR DHAV DHC8 DHC8202 2809007NM NR 2 MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM09349PH 486 AFTER ENGINE START, DC BUSS CAUTION LIGHT ILLUMINATED. RESET BUSS OK. NR 2 GENERATOR WOULD NOT RESET. MX STARTED NR 1 AND 2 ENGINES, DESELECTED EXTERNAL POWER SWITCH. TURNED NR 2 GENERATOR OFF, CAUTION LIGHT ILLUMINATED. TURNED NR 2 GENERATOR ON, LIGHT WENT OUT. NO DEFECTS NOTED, ALL VOLTAGES NORMAL. OPS CHECKS GOOD. ACFT RETURNED TO SERVICE. NO PARTS REPLACED. 2H72 4T RTA13NM 20050623001072005062300107EA 2005 6 23 QXEA200500991 120050519A5311 FRAME CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09616QX 10128 FUSELAGE STATION FORWARD SIDE OF FRAME STATION X1088 BETWEEN STRINGER 9R AND 10R HYDRAULIC LINE ATTACH CLIP BROKEN OFF AND FRAME CHAFED. REPAIRED IAW REO 670-53-61-170 AND HORIZON AIR EA R-53-337. 2L72 4F RTA21EA 20050623001102005062300110NM 2005 6 23 QXEA200501016 120050428A33506104781 BATTERY DHAV DHC8 DHC8202 2809007NM EMERGENCY LIGHTSINOPERATIVE A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09356PH27834 502 WHEN PERFORMING OPS CHECK OF EMERGENCY LIGHTS, FOUND EXIT SIGNS AT GALLEY CEILING AND MID-CABIN TO BE INOP. REPLACED EMERGENCY POWER SUPPLY BATTERIES PS2 AND PS5. OPS CHECKS GOOD. ACFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050623001112005062300111NM 2005 6 23 QXEA200500960 120050531A5330 SKIN DHAV DHC8 DHC8202 2809007NM FUSELAGE LIGHTNING STRIKEA QXEAA UNSCHED LANDING O OTHER CLCLIMB 1 NM09350PH 488 DURING CLIMB, LIGHTNING STRIKE NOTED TO FRONT OF ACFT. LANDING GEAR UP AT TIME. ACFT RETURNED AND ACCOMPLISHED UNEVENTFUL LANDING. MX PERFORMED LIGHTNING STRIKE INSP AND FOUND EVIDENCE OF LIGHTNING DAMAGE AT RADOME, FORWARD LT FUSELAGE, UPPER FUSELAGE, AND RT AILERON AND STATIC DISCHARGER. 2H72 4T RTA13NM 20050623001122005062300112 2005 6 23 QXEA200500967 420050510A3418 WARNING LIGHT BOMBDRDHC8 DHC8402 1390042NM STALL WARNING ILLUMINATED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09400QX 4030 MASTER CAUTION ILLUMINATED WITH NR 2 STALL SYSTEM FAILURE AND PUSHER SYSTEM FAIL CAUTION LIGHTS. PERFORMED CHECKLIST. LIGHT CYCLED INTERMITTENTLY OFF AND ON. PERFORMED OPS CHECK OF NR 1 AND NR 2 SHAKER PUSHER SYSTEM AS PER AMM 27-33-00-710-802, OPS CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050623001132005062300113NM 2005 6 23 QXEA200500970 120050517A2750 WARNING LIGHT BOMBDRDHC8 DHC8401 1390041NM TE FLAP CONTROL ILLUMINATED A QXEAO OTHER J WARNING INDICATION APAPPROACH 1 NM09539DS 4016 FLAP POWER CAUTION LIGHT ILLUMINATED SELECTING FLAPS FROM ZERO TO 5 DEGREES. COMPLIED WITH CHECKLIST AND RESET FLAP CONTROL CIRCUIT BREAKER AND FLAP POWER CAUTION LIGHT EXTINGUISHED. FLAPS OPERATED NORMALLY. NO PARTS REPLACED. ACFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050623001152005062300115NM 2005 6 23 QXEA200500969 120050503A2750 CONTROL SYSTEM BOMBDRDHC8 DHC8402 1390042NM TE FLAPS MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION APAPPROACH 1 NM09403QX 4037 WHEN SELECTING FLAPS, FLAP POWER CAUTION LIGHT ILLUMINATED, FOLLOWING EMERGENCY CHECKLIST, UNABLE TO RESTORE POWER TO FLAP SYSTEM. CONDUCTED ZERO FLAP LANDING WITHOUT FURTHER INCIDENT. MX COMPLIED WITH SL DH8-400-SL-27-002A, CAUTION LIGHT EXTINGUISHED. COMPLIED WITH OPS CHECK IAW AMM 27-50-00, PAGES 501-203. OPS CHECK GOOD. NO PARTS REPLACED. ACFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050623001192005062300119NM 2005 6 23 QXEA200500973 120050511A3010 DEICE SYSTEM BOMBDRDHC8 DHC8402 1390042NM AIRFOIL ANTI-ICEMALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09416QX377 4083 OUTSIDE RT GREEN TAIL LIGHT ILLUMINATES MOMENTARILY, DEICE PRESSURE 20 PSI WITH ON LT LIGHT ILLUMINATING AND "ISO" SELECTED PER CHECKLIST. MX REPLACED RT OUTBOARD DDV. PERFORMED FUNCTIONAL TEST OF AIRFRAME DEICING SYSTEM. ALL CHECKED GOOD. ACFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050623001202005062300120EA 2005 6 23 QXEA200500974 120050507A2120 ODOR CNDAIRCL600 CL6002C10 1390015EA CABIN DETECTED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM09607QX 10024 BOTH F/A COMPLAINED ABOUT ACRID CHEMICAL ODOR IN AFT CABIN VICINITY OF LAVATORY THAT CAUSED BOTH TO HAVE HEADACHES. DURING CREW DE-BRIEFING, ODOR WAS NOT PRESENT WITH APU SHUTDOWN. MX RAN APU AT FULL HOT WITH ALL GASPERS OPEN AND FULL COLD FOR APPROX 30 MINUTES. NO ACRID ODOR COULD BE NOTED IN CABIN. GROUND RAN ACFT AT CRUISE FOR APPROX 10 MINUTES AT FULL HOT, NO ODOR COULD BE NOTICED. NO PARTS REPLACED. ACFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20050623001212005062300121NM 2005 6 23 QXEA200500976 120050518A2120 ODOR DHAV DHC8 DHC8202 2809007NM COCKPIT DETECTED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 NM09362PH162131045 518 ON CLIMB OUT NOTED STRONG ODOR AND HAZE IN BOTH COCKPIT AND CABIN. ODOR APPEARED TO COME FROM BLEED AIR SYS. COULD NOT ISOLATE ODOR FROM NR 1 OR 2 BLEED SYSTEM. REPLACED DUAL HEAT EXCHANGER. CLEANED AIR DUCTS AND RAN ACFT WITH BOTH BLEEDS ON. NO FURTHER SMELL OR HAZE NOTED. ACFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050623001222005062300122 2005 6 23 QXEA200501017 420050411A3420 DISPLAY DHAV DHC8 DHC8202 2809007NM ZONE 200 INACCURATE A QXEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM09349PH 486 HEADING MISMATCH INTERMITTENTLY DISPLAYED IN ADVISORY DISPLAY. COMPLIED WITH CHECKLIST PROCEDURE, MESSAGE RETURNED SEVERAL TIMES. COMPLIED WITH IAW CHECKS AND NO HEADER ON MISMATCH MESSAGE OCCURRED, COMPLIED WITH AMM TASK 34-21-00-40-801. OPS CHECKS GOOD. NO PARTS REPLACED. ACFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050623001252005062300125NM 2005 6 23 QXEA200501020 120050525A242051608003 GCU DHAV DHC8 DHC8202 2809007NM ZONE 100 FAILED A QXEAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM09368PH112872158 512 NR 1 AC GENERATOR CAUTION LIGHT FAILED TO EXTINGUISH AFTER START UP. RESET AC AS PER CHECKLIST AND LIGHT EXTINGUISHED. GOT LIGHT AGAIN ON TAKEOFF ROLL AND RESET AGAIN AND LIGHT EXTINGUISHED. NR 1 AC GENERATOR LIGHT DID NOT COME ON FOR REST OF FLIGHT. REMOVED AND REPLACED NR 1 AC GCU. PERFORMED FUNCTIONAL CHECK, TESTED GOOD. ACFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050623001272005062300127NM 2005 6 23 QXEA200501009 120050601A3297471512 WIRE HARNESS BOMBDRDHC8 DHC8402 1390042NM NLG WOW MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION LDLANDING 1 NM09400QX959 4030 NOSE WHEEL STEERING FAILURE AND CAUTION ILLUMINATED ON LANDING. ABLE TO RESET PER CHECKLIST. NWS FAIL AND AGAIN IAS FAIL ON BOTH PFD'S AND WOW CAUTION. MX REPLACED PSEU WOW NR 2 HARNESS. OPS CHECKS GOOD. ACFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050623001292005062300129NM 2005 6 23 USAA050579 120050426A5320 ANGLE BOEING757 757225 1384959NM RROYCERB211 RB211535E4 54555NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19608AU 22204 BFM - C4 CHECK - ANGLE AREA EXCEEDS 30 PERCENT OF LENGTH, CRACKED AND BROKEN, BS 860-880 BL0. REMOVED ANGLE, FAB NEW FOR SAMPLE AND INSTALLED NEW IAW SRM. (K) 2L72 4F4 FRTA2NM E12EU 20050623001312005062300131NM 2005 6 23 SB05071 120050616A33501012721 LIGHT BOEING737 7373B7 1384580NM GE CFM56 CFM56* 13802NE SEAT ROW 22 SHORTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19511AU 23594 CLT MAINTENANCE REPORTED THE EMERGENCY LIGHT AT SEAT ROW 22 WAS SHORTED. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AND THE FUSE IN THE EMERGENCY LIGHT BATTERY PACK BETWEEN AFT GALLEYS. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA16WE E2GL 20050623001332005062300133NM 2005 6 23 QXEA200501059 120050615A8010 WARNING LIGHT BOMBDRDHC8 DHC8402 1390042NM COCKPIT FALSE ACTIVATIONA QXEAE ENGINE SHUTDOWN N FALSE WARNING TXTAXI/GRND HDL 1 NM09409QX 4051 LAX FLIGHT 4424 START SELECT LEVER DID NOT RECENTER AFTER STARTING NR 2 ENGINE. START SELECT LIGHT REMAINED ILLUMINATED. AIRCRAFT SHUT DOWN AND POWERED DOWN PER ABNORMAL CHECKLIST. MAINTENANCE CYCLED AIRCRAFT POWER. RESTARTED BOTH ENGINES. BOTH DC GENERATORS ON LINE. NO FURTHER DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050623001342005062300134EA 2005 6 23 MASA200500464 120050613A3620 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA ENGINE ILLUMINATED A MASAE ENGINE SHUTDOWN J WARNING INDICATION DEDESCENT 1 SW0747239 7239 ASH 7137 CLT, ON INITIAL DESCENT PILOT HAD A RT 14TH DUCT WARNING. THE MESSAGE DID NOT EXTINGUISH WHEN THE SYSTEM WAS TURNED OFF, SO THE CREW ELECTED TO SECURE THE ENGINE. AFTER A BRIEF PERIOD THE MESSAGE WENT AWAY AND THE CREW ELECTED TO RESTART THE ENGINE AND THE PLANE LANDED UNEVENTFULLY WITH OUT FURTHER INCIDENT. 2L72 4F RTA21EA 20050623001432005062300143NM 2005 6 23 72300202 120050323A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 3 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050623001442005062300144NM 2005 6 23 72300203 120050407A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 2 INCH AREA OF CORROSION ON STRINGER. 2L73 4F4 FRTA3WE E2EA 20050623001482005062300148NM 2005 6 23 DHL2005741573 120050425A5347 SEAT TRACK BOEING727 7272Q9 138448MNM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 SEAT TRACK 48 RT BS 760 TO 848 CORRODED. REMOVED SEAT TRACK AT BS 760-848 R&L 48 IAW B727 SRM 51-30-2 REPLACED, DRILL & LOCATED FASTENER HOLES IN PART (8FT) IAW B727 SRM 51-30-2 FIG1 TREATED & PRIMED AREA PART IAW B727 SRM 51-10-2 REMOVED & REINSTALLED FLOOR BOARDS E & F PANEL AT BS 760-848 IAW B727 SRM 51-30-2 FIG9 2L73 4F RTA3WE 20050623001492005062300149NM 2005 6 23 QXEA20050161 120050515A33506038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007NM ZONE 200 INOPERATIVE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09355PH* 9462 500 PDX-AFT TWO RED LIGHTS ON FLOOR TRACK LIGHTING AT ROW 1DE INOPERATIVE. REMOVED AND REPLACED PS6 POWER SUPPLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050623001502005062300150 2005 6 23 QXEA200501060 420050616A3442MI5853505 TRANSCEIVER DHAV DHC8 DHC8202 2809007NM ZONE 100 MALFUNCTIONED A QXEAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 NM09361PH119046466 516 PDX-ON FLIGHT 2058, PDX-OTH RETURN TO FIELD, RADAR GIVES NO RETURNS AND SHOWS RED SPOKES. REMOVED AND INSTALLED NEW WEATHER RADAR R/T. SYSTEM TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050623001512005062300151EU 2005 6 23 HK200522A 120050617A2910 LINE BAG JETSTMJETSTM3201 1500217EU HYD SYSTEM RUPTURED A B EMER. DESCENT K FLUID LOSS APAPPROACH 1 SW994381 898 ACFT SUFFERED AN EMERGENCY APPROACH & LANDING DUE TO COMPLETE HYD FLUID LOSS. LINE NEAR GROUND TEST PRESSURE COUPLING IN LT OF ACFT BETWEEN LOWER FUSELAGE & CARGO PACK RUPTURED. ALL HYD FLUID LOST, ENTERED COCKPIT THROUGH THE LT AIR CON DUCT, SOAKING CREW & PAX IN HYD FLUID. AFTER A VISUAL INSP, FOUND HYD LINE RESTS IN UPPER PART OF AIR CON DUCT THAT’S AFT OF WATER SEPARATOR. EVEN THOUGHT THE HYD LINE HAD A CLAMP IT STILL IN CONTACT WITH DUCT. WEAR CAUSED BOTH COMPOSITE A/C DUCTS & HYD LINE TO RUPTURE, CAUSING LOSS OF HYD POWER AND DAMAGE OF A/C DUCT IN SAME AREA AS HYD LINE, ALLOWING FLUID TO GET INTO CABIN. HYD LINE REPLACED, A/C DUCT REPAIRED & A/C DUCTS WERE CLEANED. FLT TEST & GROUND TEST OK. 2L72 4T RTA56EU 20050623001582005062300158NM 2005 6 23 DL75K050319 120050610A3350 SOCKET BOEING757 757232 1384965NM EMERGENCY LIGHT DAMAGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27651DL 24391 EMERGENCY LIGHT AT 29 ABC INOPERATIVE REPLACED LENS AND SOCKET ASSY 2L72 4F RTA2NM 20050623001592005062300159NM 2005 6 23 DLM88050320 120050611A2150219001545 ACM DOUG MD88 MD88 3023688NM LEFT FAILED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27918DL 49583 ODOR IN FLIGHT COMPARTMENT DURING CLIMB - REPLACED LEFT AIR CYCLE MACHINE 2L72 4F RTA6WE 20050623001602005062300160NM 2005 6 23 DL764050321 120050613A3350336701252 BATTERY PACK BOEING767 767* NM L3 DOOR DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27842MH 29715 L3 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK. 2L72 4F RTA1NM 20050623001612005062300161NM 2005 6 23 DL764050322 120050613A3150 WARNING LIGHT BOEING767 767432ER 1385134NM GE CF6 CF680C2B2 30025NE NR 1 ENGINE FALSE INDICATIONA DALAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO27832MH12751 29704 704929 LT ENGINE EGT RED BOXED AT 975 ABORTED T/O AT 80KNTS - T/S PER FIM - NO EXCEEDENCES RECORDED 2L72 4F4 FRTA1NM E13NE 20050623001632005062300163NM 2005 6 23 DL75K050324 120050615A2910 LINE BOEING757 757232 1384965NM HYD SYSTEM LEAKING A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO27649DL 24389 LT HYD SYS FAILURE. QUANITY DROPPED TO 1.6. GEAR AND FLAPS EXTENDED NORMALY. REPAIRED LEAK. 2L72 4F RTA2NM 20050623001662005062300166NM 2005 6 23 WRLA200589 120050614A5512 PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 ITEM: DURING C04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST LT BARREL NUT HOLE NR 9.(OPEN) 2L73 4F4 FRTA22WE E24NE 20050623001672005062300167NM 2005 6 23 WRLA200590 120050614A5512 PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST LT BARREL NUT HOLE NR 13.(OPEN) 2L73 4F4 FRTA22WE E24NE 20050623001682005062300168NM 2005 6 23 WRLA200591 120050614A5512 PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST LT BARREL NUT HOLE NR 14.(OPEN) 2L73 4F4 FRTA22WE E24NE 20050623001702005062300170NM 2005 6 23 WRLA200593 120050614A5512 PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST LT BARREL NUT HOLE NR 18.(OPEN) 2L73 4F4 FRTA22WE E24NE 20050623001712005062300171NM 2005 6 23 WRLA200594 120050614A5512 PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST LH BARREL NUT HOLE NR 23.(OPEN) 2L73 4F4 FRTA22WE E24NE 20050623001722005062300172NM 2005 6 23 WRLA200595 120050614A5512 PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098, FOUND CORROSION IN HST LT BARREL NUT HOLE NR 25.(OPEN) 2L73 4F4 FRTA22WE E24NE 20050623001732005062300173NM 2005 6 23 WRLA200596 120050614A5512 PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098, FOUND CORROSION IN HST LT BARREL NUT HOLE NR 26.(OPEN) 2L73 4F4 FRTA22WE E24NE 20050624000032005062400003NM 2005 6 24 WRLA2005102 120050614A5512 PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098, FOUND CORROSION IN HST LT BARREL NUT HOLE NR 33. 2L73 4F4 FRTA22WE E24NE 20050624000062005062400006EA 2005 6 24 COMA0570067 120050614A5320 DOOR FRAME CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01340CA7435 10062 CORROSION FOUND NEAR POTABLE WATER DOOR AT FS 364 APPROXIMATELY 3 INCHES LONG, 700 INCHES WIDE AND BETWEEN .005 AND .007 INCHES DEEP. REMOVED CORROSION AT POTABLE WATER DOOR SURROUND AREA IAW BOMBARDIER EO 601R-53-6620. 2L72 4F RTA21EA 20050624000072005062400007NM 2005 6 24 WRLA2005107 120050616A5512 PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE NR 19. 2L73 4F4 FRTA22WE E24NE 20050624000112005062400011NM 2005 6 24 WRLA2005109 120050616A5512 PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE 23. 2L73 4F4 FRTA22WE E24NE 20050624000132005062400013NM 2005 6 24 WRLA2005111 120050616A5512 PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE NR 26. 2L73 4F4 FRTA22WE E24NE 20050131000072005013100007NM 2005 1 31 SWAA050196 120050125A5755 SKIN BOEING737 7373H4 1384600NM NR 3 SPOILER DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 33600 22949 DURING SCHEDULED C2 CHECK, FOUND LT WING NR 3 SPOILER DELAMINATED. REMOVED AND REPLACED LT WING NR 3 SPOILER PER MM. 2L72 4F RTA16WE 20050131000082005013100008NM 2005 1 31 SWAA050197 120050125A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SPV, FOUND STRINGER CLIP AT BS 887, STRINGER 1, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20050131000122005013100012NM 2005 1 31 SWAA050208 120050125A53306545765 SKIN BOEING737 7373TO 138447GNM FUSELAGE CHAFED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29697SW 23838 DURING SCHEDULED A2 CHECK, FOUND UPPER FUSELAGE SKIN BETWEEN BS 867 AND 887, AT DORSAL FIN, CHAFED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20050131000132005013100013NM 2005 1 31 SWAA050209 120050125A53306545774 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29524SW 26566 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 787, STRINGER 25L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050131000172005013100017NM 2005 1 31 05FDEA00153 120050124A3080 LINE DOUG MD11 MD11 3023602NM NR 3 ENGINE LEAKING A FDEAJA DUMP FUEL UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO25618FE 48754 ENG - 3 A-ICE DISAG, ILLUMINATED WITH SWITCH OFF. TURNED SWITCH ON, DISAG LT STILL ON. TURNED A/I OFF, DISAG LT STAYED ON FOR APPROX 15 MINUTES THEN WENT OUT. MEL 24JAN05 RELEASED FOR SERVICE PER MEL/CDL: 30-22-01-02-A CATEGORY: C EXPIRATION: 03FEB05 ENG NR 3 ANTI-ICE VALVE INOP. FOUND NR 3 ENG AI VALVE MUSCLE AIR LINE LEAKING. REMOVED AND REPLACED LINE IAW SMP RAN ENG PER JRH AND A/I VALVE OPS CHECKS GOOD. 2L73 4F RTA22WE 20050131000192005013100019NM 2005 1 31 05FDEA00160 120050125A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25465FE 21289 FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR UPPER HINGE CUTOUT. REPAIRED PER EO 7-5330-7-2345 PT 3. 2L73 4F RTA3WE 20050131000202005013100020NM 2005 1 31 05FDEA00161 120050125A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25235FE 21329 MAIN CARGO DOOR CUTOUT DOUBLER, FASTENER HOLE DOUBLE DRILLED, BS 675 STR 26L. REPAIRED PER SRM 53-10-3. 2L73 4F RTA3WE 20050131000242005013100024EA 2005 1 31 SWIA200514424 120050123A2751855D1003 POSITION SENSOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED DEDESCENT 1 NM07403SW1122211222 7028 INBOUND TO SLC AT 18,000 FEET FLAP FAIL CAUTION MESSAGE APPEARED. REMOVED AND REPLACED RIGHT SIDE BPSU IAW 27-51-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050131000252005013100025EA 2005 1 31 SWIA200514425 120050122A2760 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07407SW 7034 NO -T/O CONFIG OK- MESSAGE. REPLACED NR 1 AND NR 2 SECU IAW MM TASKS 27-61-05-000-801 AND 27-61-05-400-801. REPLACED LEFT OUTBOARD FLIGHT SPOILER PCU IAW MM TASKS 27-62-01-000-801 AND 27-62-01-400-801. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050131000282005013100028EA 2005 1 31 COMA0560059 120050118A2750857SD1007 DRIVE SHAFT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS SHEARED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01924CA 7026 FLIGHT 5142 RECEIVED A FLAP FAIL MESSAGE DURING APPROACH TO SYR. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE FIRST EVENT, MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. AIRCRAFT WAS FERRIED TO CVG WHERE THE NR 4 FLEX DRIVE SHAFT WAS REPLACED. 2L72 4F RTA21EA 20050131000312005013100031NM 2005 1 31 SWAA050198 120050125A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 943, STRINGER 25R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050131000342005013100034NM 2005 1 31 UPS05443725 120050107A534065B38600170 STRINGER CLIP BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C - BS 1040 S2R STRINGER TIE CLIP FOUND CRACKED. M/D BS 1040 STR 2R STRINGER TIE CLIP REPLACED IAW SRM 51-10-01 PAGE 9. 2L74 4F A20WE 20050131000352005013100035NM 2005 1 31 UPS05443726 120050108A5320 INTERCOSTAL BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C M/D - BS 1220 RBL 118 BELOW FLOOR INTERCOSTAL WEB FOUND CRACKED. WEB REPAIR PER SRM 51-40-02 FIG 1. 2L74 4F A20WE 20050131000402005013100040 2005 1 31 249TR0104 420050103A2210 CIRCUIT BREAKER BOEING737 7372K5 138448XNM AUTOPILOT SYS TRIPPED A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05249TR 22598 AUTO PILOT WILL NOT FOLLOW COMMANDED INPUTS FROM PILOT AND FLIGHT DIRECTOR. RESET STABILIZER TRIM CIRCUIT BREAKER. SYSTEM TESTS GOOD PER MM 22-11-01. 2L72 4F RTA16WE 20050131000482005013100048EA 2005 1 31 SWIA200514419 120050111A335020131A BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCHARGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07980SW7133 7133 7955 EMERGENCY CABIN CEILING FLOODLIGHTS AT ROWS 5 & 13 BURNED OUT. REMOVED AND REPLACED EMERGENCY BATTERY PACK NR 4 IAW AMM 33-51-04. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050131000502005013100050NM 2005 1 31 QXEA200500109 120050117A2700 FLT CONTROLS DHAV DHC8 DHC8202 2809007NM SLUGGISH A QXEAO OTHER F FLT CONT AFFECTED TOTAKEOFF 1 NM09353PH 496 DURING THE INITIAL ROTATION, THE FIRST OFFICER NOTED GREATER THAN NORMAL BACK PRESSURE AND SLOWER THAN NORMAL ROTATION TIME AFTER ANTI ICING WITH TYPE III FLUID IN PASCO. MAINTENANCE INSPECTED THE AIRCRAFT FLIGHT CONTROLS INCLUDING THE ELEVATOR SYSTEM, ELEVATOR TRIM, AND ELEVATOR CONTROL SYSTEM WITH FUNCTIONAL CHECKS OF THE SAME. OPERATIONAL CHECKS AND CHECK FLIGHT WERE PERFORMED. ALL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050131000512005013100051NM 2005 1 31 SWAA050142 120050119A5313BAC1498 STRINGER BOEING737 7373T5 1384608NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29667SW 23063 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER 23L, AT BS 500C, CORRODED. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2L72 4F RTA16WE 20050131000552005013100055NM 2005 1 31 0500065523 120050112A5310 SUPPORT BEAM BOEING757 757251 1384970NM SEAT TRACK CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01523US 23617 DURING H-CHECK FOUND CORROSION ON SEAT TRACK SUPPORT BEAM AT BS 365 RBL 23 TO RBL 27. REPAIRED PER EA 55-202244. 2L72 4F RTA2NM 20050131000562005013100056NM 2005 1 31 DHL2005760001 120050115A5270 SWITCH BOEING727 7272B7 138407LNM RT MLG DOOR DIRTY A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01760AT 21954 AFTER T/O DURING CLIMB RT GEAR DOOR LIGHT ILLUMINATED. COMPLETED ABNORMAL PROCEDURE LIGHT EXTINGUISHED. CLEANED & INSPECTED RT GEAR DOOR SWITCH, CYCLED DOOR SEVERAL TIMES, OPS CHECK NORMAL IAW M/M 32-62-00. 2L73 4F A3WE 20050131000622005013100062EA 2005 1 31 SWIA200514413 120050114A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07955SW 7817 SPOILERONS FAULT STATUS MESSAGE COULD NOT CLEAR. REPLACED LEFT OUTBOARD SPOILERON (NR 3) PCU WITH SERVICEABLE UNIT. OPERATIONAL CHECK GOOD. ALL WORK PERFORMED IAW CRJ MM CH 27. P/N 27000-7, S/N OFF 6976. 2L72 4F RTA21EA 20050131000632005013100063NM 2005 1 31 AT0500001 120050106A213392145A010101 OUTFLOW VALVE BOEING717 717200 1383700NM CABIN PRESSURE FAILED A ZZDAO OTHER J WARNING INDICATION CRCRUISE 1 SO15894AT 55046 CABIN INFLOW LOW, CABIN CLIMBED 300-400 FT/MIN BEST CASE 1700-1800 FT/MIN WORST CASE, FORCED DESCENT TO MAINTAIN CABIN ALTITUDE OUTFLOW. VALVE FAILED TO CLOSE IN AUTO OR MANUAL. REMOVED AND REPLACED CPC. 2L72 4F TRA6WE 20050131000692005013100069NM 2005 1 31 SWAA050132 120050119A3350311500 LENS BOEING737 7373K2 13844BANM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29345SA 23786 DURING SCHEDULED C2 CHECK, FOUND EMERGENCY EXIT BULL NOSE LIGHT LENS AT ROW 6 ABC, LOOSE. SECURED LIGHT LENS PER MM. 2L72 4F RTA16WE 20050131000742005013100074EA 2005 1 31 05017645 120050117A2750 FCU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A VTZAO OTHER J WARNING INDICATION APAPPROACH 1 EA27645BR 7383 FLAPS FAIL AT 0 DEGREES. MX RESET FECU. CYCLED FLAPS THROUGH 3 TIMES. NO FAULT NOTED. 2L72 4F RTA21EA 20050131000782005013100078NM 2005 1 31 SWAA050153 120050120A53306545774 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 747, STRINGER 18L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050131000852005013100085NM 2005 1 31 QXEA200500091 120050108A5347 SEAT TRACK DHAV DHC8 DHC8102 2809003NM ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09369PH 513 PDX - RIGHT HAND CENTER SEAT TRACK NR 7 HAS GOUGES IN TRACK FROM STATION FRAME 350.00 TO FRAME 374. REPAIRED IAW SRM 51-40-11. 2H72 4T RTA13NM 20050131000902005013100090EA 2005 1 31 COMA0560061 120050114A274070609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA AVIONICS MALFUNCTIONED A COMAA UNSCHED LANDING JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 SO01491CA5587 7756 FLT 5501 STAB TRIM AND MACH TRIM CAUTION. REPLACED THE HSTCU. 2L72 4F RTA21EA 20050131000922005013100092NM 2005 1 31 05FDEA00131 120050120A5311 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25596FE 48554 MAIN DECK CARGO COMPARTMENT LT AFT FUSELAGE UPPER MAIN FRAME AT STA 1661 FOUND WITH DENT. MAIN FRAME AT STA 1661 BETWEEN LONGERON 11L TO 13L REPAIRED AS PER SRM 53-30-00 FIG1 VOL1. REFER TRACKING EA 1-5310-81679. 2L73 4F RTA22WE 20050131001122005013100112NM 2005 1 31 QXEA200500104 120050118A30607826895 BRUSH BLOCK DHAV DHC8 DHC8102 2809003NM ZONE 500 MALFUNCTIONED A QXEAA UNSCHED LANDING O OTHER CLCLIMB 1 NM09361PH2319 388 516 SEA - FLIGHT 2180 RETURNED TO FIELD NR 1 PROP HUB SPARKING. MAINTENANCE REPLACED THE BRUSH BLOCK. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050131001132005013100113EA 2005 1 31 COMA0560040 120050116A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01977CA 7157 FLIGHT 5462 FLAPS FAIL CAUTION. 0RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20050131001262005013100126NM 2005 1 31 QXEA200500094 120050108A5347 SEAT TRACK DHAV DHC8 DHC8102 2809003NM ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09369PH 513 PDX - LEFT HAND CENTER SEAT TRACK NR 4 HAS GOUGE AT FRAME 282 TO FRAME 299. REPAIRED IAW SRM 51-40-11. 2H72 4T RTA13NM 20050131001282005013100128NM 2005 1 31 UPS05243792 120050110A5312 PRESSURE PANEL BOEING727 727185C 138406NNM NLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 INSPECTION TYPE:C, NLG WHEEL WELL HAS 3 SUSPECT CRACKS AT RT AFT PRESSURE PANEL CUTOUT. TWO AT LWR FWD CORNER AND ONE NEAR UPPER AFT CORNER. REPAIR CARRIED OUT IAW AAAE EO 2005-001-004. 2L73 4F A3WE 20050131001292005013100129NM 2005 1 31 UPS05443764 120050107A5347 SEAT TRACK BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C - BS 1480 - 1500 RBL 11 SEAT TRACK O/B FLANGE FOUND CORRODED. SEAT TRACK REPAIR PARTS FABRICATED PER SRM 53-10-05 FIG 14. CORROSION BLEND OUT 0.040 X 1 X 3 INCHES EXCEED SRM LIMIT. 2L74 4F A20WE 20050131001362005013100136NM 2005 1 31 UPS05443796 120050106A534065B38600197 STRINGER CLIP BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C - BS 1160 S15L STRINGER TIE CLIP FOUND CRACKED. TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050131001372005013100137NM 2005 1 31 UPS05443798 120050106A534065B0794227 CLIP BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C, LOWER FUSELAGE LT INTERNAL NOSE L/G WHEEL WELL VERTICAL BEAM HORIZONTAL STIFFENER ATTACH CLIP FOUND CRACKED AT STA 300 WL 150. STIFFENER ATTACH CLIP REPLACED PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050131001392005013100139NM 2005 1 31 UPS05443800 120050107A5340 ATTACH ANGLE BOEING747 747123 1384873NM FWD CARGO BAY CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C, FWD CARGO COMPT - SUPPORT FRAME UPPER CHORD LOWER ATTACH ANGLE SURFACE FOUND CORROSION AT STA 700 LBL 38. ANGLE REPLACED AS PER SRM 51-10-01 PG 9. CORROSION BLEND OUT 0.040 X 1 X 2 INCH. 2L74 4F A20WE 20050131001422005013100142NM 2005 1 31 UPS05443803 120050113A5313 STRINGER BOEING747 747123 1384873NM BS - CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C BS 1560 TO BS 1580 AFT RT WINDOW FORGING REMOVED FOUND STRINGER CORROSION CRACKED. CORROSION BLEND OUT 0.060 X 1 X 7 INCH, EXCEED SRM LIMIT. FLAP PEEN CARRIED OUT AS PER SRM 51-10-07 AND SOPM 20-10-03, STRINGER SEGMENT AND SPLICE ANGLE REWORKED REFER COMPONENT WORK PROCESS CARD SEQUENCE NR HE70480 -1, -2, -3 FOR DETAILS. 2L74 4F A20WE 20050131001472005013100147WP 2005 1 31 UPS05843759 120050105A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01868UP 45968 INSPECTION TYPE:C3 LONGERON 15R CRACKED UNDER SHEAR TIE AT STA 1754. REMOVED END FITTING AND CLIP TO FOM. REMOVED DAMAGED SECTION OF L15R FROM APPROX STA 1745-1766. FAB REPLACEMENT LONGERON SECTION FROM S1616757, SPLICE STRAPS FROM SHT7075T6-.080, SPLICE FITTING FROM S2645716. TREAT, PRIME & INSTALL ALL PARTS REF SRM 53-2-2, 51-1-8, 51-1-21, 51-1-20D. 2L74 4F RT4A25 20050131001542005013100154WP 2005 1 31 UPS05843787 120050110A53503705290 FITTING DOUG DC8 DC871F 302199DWP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01701UP 45938 INSPECTION TYPE:C1, TAIL CONE ATTACH FITTING CRACKED ON L36, STA 1875. REMOVED AND REPLACED FITTING IAW SRM 51-1-21, 51-1-20D, 51-1-8, 51-3-0. 2L74 4F RT4A25 20050131001572005013100157WP 2005 1 31 UPS05843806 120050128A7930 WARNING LIGHT DOUG DC8 DC871F 302199DWP NR 4 ENGINE ILLUMINATED A IPXAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01772UP 46072 INSPECTION TYPE:N/A ATB - NR 4 ENG OIL PRESS LIGHT CAME ON IN FLT. OIL PRESS AT CLIMB THRUST WAS 60 & OPS AFTER SHUTDOWN (WINDMILLING). NR 4 ENG LOW OIL PRESSURE LIGHT DEFERRED PER MEL 79-6 OIL PRESSURE & OIL QTY WERE NORMAL PER FLT CREW, PLACARD INSTALLED M296095. 2L74 4F RT4A25 20050131001582005013100158NM 2005 1 31 AWXA200500080 120050127A33501012623 LIGHT BOEING737 737301 1384611NM SEAT ROW 11 LT INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28325AW 23260 PHX - EEL - DURING 8-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH SIGN INOPERATIVE AT SEAT ROW 11 LT. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH SIGN AT SEAT ROW 11 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050131001612005013100161EU 2005 1 31 AWXA200500083 120050111A5347D57130147200 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28621AW 053 SAL - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON LT INBOARD SEAT TRACK BETWEEN FR 38 AND FR 40. MAINTENANCE REMOVED AND REPLACED LT INBOARD SEAT TRACK FROM FR 38 TO FR 40 IAW A320 SRM 51-72-11 PG 1 & 2. 2L72 4F RTA28NM 20050131001682005013100168EU 2005 1 31 AWXA200500085 120050117A5347D57130147202 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28621AW 053 SAL - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON LT OUTBOARD SEAT TRACK BETWEEN FR 40 AND FR 42. MAINTENANCE REMOVED CORRODED LT OUTBOARD SEAT TRACK FROM FR 40 TO FR 42; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050131001742005013100174NM 2005 1 31 QXEA200500123 120050124A5230 BRACKET BOMBDRDHC8 DHC8401 1390041NM ZONE 800 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09410QX 4053 PDX - LOWER AFT SUPPORT ROLLER BRACKET IS CRACKED AT AFT BAG DOOR. REPAIRED IAW DHC Q400 AMM TASK 52-31-00-720-801, PARAGRAPH 1-3. 2H72 4T RTA13NM 20050131001762005013100176NM 2005 1 31 QXEA200500136 120050117A5320 FLOOR SUPPORT BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09410QX 4053 PDX - CABIN FLOOR SUPPORT ANGLE CORRODED ON TOP FLANGE, X19.4 INBOARD OF MAIN CABIN DOOR AFT HINGE RECESS. REPAIRED IAW Q400 SRM 51-21-00. 2H72 4T RTA13NM 20050131001772005013100177NM 2005 1 31 QXEA200500129 120050117A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09410QX 4053 PDX - RIGHT INBOARD SEAT TRACK CORROSION APPROXIMATELY X94.00. REPLACED IAW SRM 51-40-15 AND 51-42-05-330-801. 2H72 4T RTA13NM 20050131001802005013100180NM 2005 1 31 QXEA200500130 120050117A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09410QX 4053 PDX - THE HOLES FOR THE LAV BOLTS HAVE CORROSION AROUND THEM ON THE RIGHT INBOARD FORWARD SEAT RAIL. REPLACED IAW DHC8/400 SRM 51-40-15 AND SRM 51-42-05-330-801. 2H72 4T RTA13NM 20050131001852005013100185NM 2005 1 31 QXEA200500126 120050127A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09410QX 4053 PDX - RIGHT INBOARD SEAT TRACK CORROSION APPROXIMATELY X 22.00. REPLACED IAW SRM 51-40-15 AND SRM 51-42-05-330-801. 2H72 4T RTA13NM 20050131001992005013100199NM 2005 1 31 SWAA050234 120050127A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29331SW 23695 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 792, STRINGER 19L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050131002042005013100204NM 2005 1 31 SWAA050239 120050127A53406546546 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29602SW 27953 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE AT BS 907, STRINGER 4R, CRACKED. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20050201001142005020100114 2005 2 1 VW3R200500001 420050127A2565700129014 GAUGE BFGOODRICH DOUG MD88 MD88 3023688NM SLIDE BOTTLE STUCK B K NONE O OTHER ININSP/MAINT 1 WP09 PW0267 AFTER OVERHAULING THE PRESSURE REGULATOR USED ON THE EVACUATION SLIDE INFLATION SYSTEM, DURING THE CHARGING PROCESS THE GAUGE ON THE PUMP WAS SHOWING PRESSURE BUT THE SUSPECT GAUGE WAS NOT RECORDING ANY PRESSURE (THE NEEDLE STAYED AT ZERO). THE GAUGE WAS REMOVED FOR SERVICE. 2L72 4F RTA6WE 20050202000102005020200010EU 2005 2 2 SA05007 120050116A5610NP1653116 WINDSHIELD AIRBUSA319 A319112 3930323EU ZONE 200 CRACKED A USAAH DEACTIVATE SYST/CIRCUITS O OTHER CRCRUISE 1 EA19769US12574 1391 PIT- FLIGHT 130 - EN-ROUTE DEN TO PIT - DURING THE FLIGHT, THE FIRST OFFICER RIGHT FORWARD OUTSIDE WINDSHIELD CRACKED. FLIGHT FOLLOWED THE QRH AND CONTINUED TO PIT. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FIRST OFFICER'S WINDSHIELD. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20050202000192005020200019NM 2005 2 2 AALA20050052 120050125A3397 CONNECTOR BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21654A 24612 DFW - EMERGENCY LIGHT AT SEAT 24D INOPERATIVE. REPINNED CONNECTOR AT SEAT 24D FOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050202000462005020200046EA 2005 2 2 05005679 120050105A2120 ODOR CNDAIRCL600 CL6002B19 1900309EA CABIN DETECTED A VTZAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NRNOT REPORTED 1 EA27679BR 7662 CREW REPORT STATED COCKPIT SMOKE INDICATION FOR LAV. HORRIBLE ODOR IN CABIN. NO FIRE DETECTED. REMOVED AND REPLACED COALESCER BAGS AND LAV SMOKE DETECTOR. OPS CHECK GOOD. 2L72 4F RTA21EA 20050202000722005020200072NM 2005 2 2 DHL2005770002 120050113A5270 SWITCH BOEING727 7272B7 138407LNM NLG DOOR LOOSE A DHLAO OTHER J WARNING INDICATION LDLANDING 1 SO01770AT 21953 DURING LANDING, THE GEAR EXT DOORS LIGHT ILLUMINATED ON FDW PANEL AND NOSE GEAR DOOR LT ON SO PANEL REMAINED ILLUMINATED AFTER ALL THREE GEARS INDICATED DOWN AND LOCKED. BOTH LIGHTS EXTINGUISHED WHEN NOSE TOUCHED DOWN. FOUND RT NOSE GEAR DOOR SWITCH LOSE, RETIGHTED SWITCH, CK NORMAL IAW MM 32-62-00. 2L73 4F A3WE 20050202000752005020200075NM 2005 2 2 AALA20050053 120050125A3350 SWITCH BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21354AA 24035 UNARM LIGHT DOES NOT ILLUMINATE WHEN EMERGENCY LIGHTS ARE IN THE OFF POSITION. CLEANED EMERGENCY LIGHT SWITCH CONTACTS PER FOR EMERGENCY SWITCH UNARM LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050202000762005020200076NE 2005 2 2 AALA20050055 220050125A7200 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE RIGHT SHUTDOWN A AALAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 SW21224AA 49174 718537 DFW - ON CLIMB-OUT AT 8500 FEET, HEARD LOUD BOOM FROM RIGHT ENGINE. ENGINE SPOOLED DOWN TO WINDMILL. WINDMILLED FOR 16 MINUTES. DOWNLOADED FLIGHT DATA RECORDER PER ENGINEERING. REPLACED NUMBER TWO ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 F A6WE E9NE 20050202001082005020200108WP 2005 2 2 AALA20050026 120050114A3397 WIRE HARNESS DOUG DC9 DC982 3022082WP EMERGENCY LIGHT FAULTY A AALAK NONE O OTHER ININSP/MAINT 1 SW21422AA 49334 BOS - SEAT MOUNTED EMERGENCY LIGHTS AT SEAT ROW 7DEF INOPERATIVE. FOUND CONNECTION FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 7DEF FAULTY NEAR SIDEWALL. SECURED PIN FOR WIRE HARNESS AND RECONNECTED HARNESS FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT ROW 7DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050131000972005013100097NM 2005 1 31 SWAA050159 120050120A52306549889 TEE FITTING BOEING737 7373T5 1384608NM AFT CARGO DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29667SW 23063 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO DOOR LOWER OUTBOARD TEE CHORD CRACKED. REPAIRED DOOR CHORD PER RO 0520018-74R. 2L72 4F RTA16WE 20050131001002005013100100NM 2005 1 31 2005F00011 120050114A3211651929774 ATTACH FITTING BOEING727 7272M7 138407SNM MLG TRUNNION GOUGED A DHLAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01750DH 21951 RT MAIN LANDING GEAR TRUNNION ATTACH HOLES DAMAGED AND GOUGED. 2L73 4F A3WE 20050131001102005013100110NM 2005 1 31 QXEA200500105 120050118A32208800137 STRUT DHAV DHC8 DHC8202 2809007NM NLG DISCHARGED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09362PH15163 518 SEA - FLIGHT 2024 - FLIGHT RETURNED TO THE GATE AFTER RECEIVING A WEIGHT ON WHEELS CAUTION MESSAGE. MAINTENANCE INSPECTED THE AIRCRAFT AND SERVICED THE NOSE STRUT. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050131001112005013100111SO 2005 1 31 C2XA05SH004 120050119A532014530627001 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2736915 145421 SHV - DURING C-CHECK THE LEFT OMEGA BEAM HAS CORROSION BETWEEN FR 22 & 25. MAINTENANCE REMOVED THE DAMAGE AREA AND PERFORMED A DOUBLER REPAIR EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050131001162005013100116EA 2005 1 31 COMA0560049 120050111A301011513361 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA AVIONICS MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01949CA125696083 7080 FLIGHT 5147 WING OVERHEAT MESSAGE. REPLACED THE CONTROLLER. 2L72 4F RTA21EA 20050131001172005013100117EA 2005 1 31 COMA0560045 120050110A2750855D10011 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS UNRELIABLE A COMAO OTHER J WARNING INDICATION CRCRUISE 1 SO01487CA5913 2815 7729 FLIGHT 5725 FLAPS FAIL CAUTION MESSAGE. REPLACED THE LEFT BPSU. 2L72 4F RTA21EA 20050131001202005013100120NM 2005 1 31 QXEA200500103 120050118A5270 WARNING LIGHT DHAV DHC8 DHC8202 2809007NM CARGO DOOR ILLUMINATED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09348PH 484 SEA - FLIGHT 2078 - DURING PUSHBACK, THE CARGO COMPARTMENT DOOR WARNING LIGHT ILLUMINATED. MAINTENANCE INSPECTED AND VERIFIED THAT THE DOOR WAS CLOSED AND PLACED SYSTEM ON MEL. SDR TO REMAIN OPEN PENDING CLOSURE OF MEL. 2H72 4T RTA13NM 20050131001302005013100130NM 2005 1 31 UPS05443765 120050106A5311 FRAME BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C - FRAME BS 1372 INNER FLANGE CRACKED AT S-22L. INNER FRAME REPAIRED PER RS 53-42-35235 AND ENGINEERING FILE NUMBER 747-53-20205. 2L74 4F A20WE 20050131001352005013100135NM 2005 1 31 UPS05443775 120050107A5320 WEB BOEING747 747123 1384873NM AFT CARGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C, AFT CARGO COMPT RT STA 1660 - 1680 STRINGER 30 WEB SUPPORT BOTTOM SURFACE CORROSION AS MARK. CORROSION BLEND OUT 0.030 X 2 X 2 INCHES EXCEED SRM LIMIT. WEB SUPPORT AND TIE CLIP REPLACED AS PER SRM 51-10-01. 2L74 4F A20WE 20050131001402005013100140NM 2005 1 31 UPS05443801 120050109A5347 SEAT TRACK BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C - BS 1160 - 1220 RBL 97 SEAT TRACK I/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.050 X 1 X 2 INCH. SEAT TRACK CUT OFF AT BS 1070 RBL 98 AS PER SRM 51-10-01. REPROTECTED AS PER SRM 51-10-02. SEAT TRACK REPAIR PARTS FABRICATED PER SRM 53-10-05 FIG 34. 2L74 4F A20WE 20050131001412005013100141NM 2005 1 31 UPS05443802 120050109A5347 SEAT TRACK BOEING747 747123 1384873NM BS CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:C M/D - BS 1180 RBL 97 I/B SEAT TRACK SUPPORT FOUND CORRODED. CORROSION BLEND OUT 0.050 X 1 X 1 INCH, EXCEED SRM LIMIT. SEAT TRACK REPAIR PARTS FABRICATED PER SRM 53-10-05 FIG 34. 2L74 4F A20WE 20050131001452005013100145WP 2005 1 31 UPS05843756 120050108A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01868UP 45968 INSPECTION TYPE:C3, RT WING CENTER L/E RIB CRACKED AT XFS 335.25. NDT VERIFIED CRACK TERMINATES AT RIVET HOLE REF SPM06-10-01.001. FAB 2 STACKED REPAIR ANGLES FROM SHT 7075T6-.040. INSTALLED REPAIR PER SRM 57-3-3 FIG 5, 57-2-0 FIG 2, 51-1-8, 51-1-21, 51-1-20D. 2L74 4F RT4A25 20050131001672005013100167NM 2005 1 31 AWXA200500077 120050125A3350321430 BATTERY AIRBUSA319 A319132 3930340NM ZONE 241 DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28813AW 1223 DEN - EEL - DURING 4-DAY CHECK THE LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL) HAD A BATTERY FAULT. MAINTENANCE REMOVED AND REPLACED THE BATTERY AT LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050131001732005013100173NM 2005 1 31 QXEA200500132 120050120A5320 SILL BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09410QX 4053 PDX - FORWARD PASSENGER DOOR LOWER SILL PLATE HAS CORROSION AROUND NUT PLATES AND INBOARD EDGE ON LOWER SIDE. REPAIRED IAW SRM 51-21-00, 51-21-10 AND RD 8/4-53-1143. 2H72 4T RTA13NM 20050131001752005013100175NM 2005 1 31 QXEA200500134 120050119A5730 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09410QX 4053 PDX - 522BT COUNTERSINKS HAVE FRETTING CORROSION. REPLACED PANEL. 2H72 4T RTA13NM 20050131001872005013100187NM 2005 1 31 QXEA200500128 120050117A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09410QX 4053 PDX - RIGHT INBOARD SEAT TRACK CORROSION APPROXIMATELY X68.00. REPLACED IAW SRM 51-40-15 AND SRM 51-42-05-330-801. 2H72 4T RTA13NM 20050131001972005013100197NM 2005 1 31 SWAA050232 120050127A53406551698 SPLICE BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29680AA 23505 DURING SPV, FOUND STRINGER SPLICE AT BS 360, STRINGER 4L, CRACKED. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20050131002002005013100200NM 2005 1 31 SWAA050235 120050127A53116558280 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29602SW 27953 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 360, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20050131002012005013100201NM 2005 1 31 SWAA050236 120050127A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29602SW 27953 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 360, STRINGER 5L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20050131002022005013100202NM 2005 1 31 SWAA050237 120050127A53116546529 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29602SW 27953 DURING SCHEDULED D-CHECK, FOUND FRAME SECTION AT BS 400, STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20050131002072005013100207NM 2005 1 31 SWAA050242 120050127A53156546810 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29602SW 27953 DURING SCHEDULED D-CHECK, FOUND 2 EACH FLOORBEAMS CRACKED AND CORRODED BETWEEN BS 947 AND BS 986, LBL 53 AND RBL 48. REMOVED AND REPLACED FLOORBEAM SECTIONS PER ER. 2L72 4F RTA16WE 20050202000032005020200003NM 2005 2 2 BB05003 120050123A335020121 CHARGER BOEING757 7572B7 1384964NM EMERGENCY LIGHT FAULTY A USAAK NONE O OTHER ININSP/MAINT 1 EA19630AU 27808 CLT - FOUND EMERGENCY LIGHT AT ROW 13 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER (M10919). 2L72 4F RTA2NM 20050202000072005020200007WP 2005 2 2 AALA20050042 120050120A4900 PRESSURE SWITCH DOUG DC9 DC982 3022082WP RT CSD INOPERATIVE A AALAA UNSCHED LANDING K FLUID LOSS CRCRUISE 1 SW2159523 49915 EN ROUTE DFW-CMH RIGHT HAND CONSTANT SPEED DRIVE LOW OIL PRESSURE LIGHT ON WITH APU ON MEL. LANDED LIT WITHOUT INCIDENT. REPLACED RIGHT HAND CSD OIL PRESSURE SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED. 2L72 4F A6WE 20050202000142005020200014WP 2005 2 2 AALA20050050 120050125A3397 WIRE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21433AA 49451 SJC - EMERGENCY LIGHTS IN TAIL CONE COMPARTMENT INOPERATIVE. REPAIRED BROKEN WIRE FOR EMERGENCY LIGHTS IN TAIL CONE COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050202000962005020200096NM 2005 2 2 QXEA200500053 120050109A2751 WARNING LIGHT BOMBDRDHC8 DHC8401 1390041NM TE FLAPS FALSE INDICATIONA QXEAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 NM09415QX 4081 PDX - FLIGHT 2309 - THE FLIGHT RETURNED TO THE GATE AFTER RECEIVING A FLAP POWER CAUTION LIGHT WHEN THE FLAP SELECTION WAS MADE. MAINTENANCE INSPECTED THE AIRCRAFT AND COMPLIED WITH THE FAULT ISOLATION MANUAL. OPERATIONAL CHECKS WERE PERFORMED AND WERE GOOD. NO DEFECTS WERE NOTED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050202001212005020200121 2005 2 2 YENA200513 420050120A2565 CABLE AIRBUS320 A320232 3930326EU SLIDE BOTTLE SHEARED A YENAK NONE O OTHER ININSP/MAINT 1 EA15552JB9019 A8415 1861 ON C2 CHECK, ON ACCOMPLISHING JOB CARD 522100-02-1 FOUND CABLE FOR RT OVERWING SLIDE BOTTLE BROKEN AT THE BOTTLE CONNECTION, ON THE BOTTLE SIDE NOT ON THE AIRCRAFT SIDE. REMOVED AND REPLACED RT BOTTLE ASSEMBLY. 2L72 4F RTA28NM 20050202001232005020200123 2005 2 2 YENA200504 420050108A23303042865102 ELECTRICAL BOX AIRBUS320 A320232 3930326EU SEAT 19DEF ODOR A YENAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15520JB5215 5215 1446 ROW 19 D, E, F SMOKE SMELL/ELECTRICAL (NO ACTUAL SMOKE). SECURED OVERHEAD POWER TO TV'S. SMELL DISAPPEARED. ACCOMPLISHED INFOMATION NOTICE 2004TO23TR AND FOUND SEB AT 19E W/EVIDENCE OF ELECTRICAL ODOR. PLACED TV'S 19 DEF ON MEL 25-22-03D CTL NR 07178. REMOVED AND REPLACED SEB 19E IAW LTV MM 23-39-00, OPS CHECK GOOD, MCC NOTIFIED, MX4 UPDATED, MEL CLEARED. 2L72 4F RTA28NM 20050203000022005020300002SO 2005 2 3 SWIA200514441 120050122A3350 BULB EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07292SW 120319 EMERGENCY LIGHT OVER PAX DOOR INOPERATIVE. REPLACED BULB IN EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050203000032005020300003NM 2005 2 3 05FDEA00195 120050128A4910AJC7207259 SKIN DOUG MD11 MD11 3023602NM ZONE 400 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 APU EXHAUST DOOR ACTUATOR AT CUTOUT FOUND PREVIOUS REPAIR CHAFED. PREVIOUS REPAIR ON APU EXHAUST DOOR ACTUATOR AT CUTOUT AREA EVALUATED AND FOUND NOT IAW SRM 53-00-01 FIG 5 VOL I. EXISTING DOUBLER FOR REPAIRED APU SKIN AT APU EXHAUST DOOR ACTUATOR CUTOUT AREA REMOVED AND REPLACED AS PER SRM 51-35-01 VOL II. 2L73 4F RTA22WE 20050203000042005020300004NM 2005 2 3 05FDEA00196 120050129A5315FXBAC14902831 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25480FE 21462 MCD, STA 480, RBL 24.50 TO BL 0.00, FLOORBEAM HAS CORROSION. REMOVED CORROSION IAW SRM 53-10-1 FIG 4, PAGE 19, ORIG MATERIAL .140 AFTER REWORK .085 FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AREA IAW SRM 53-10-8. MATERIAL ID AS BAC 1518-338 7075-T6 511 FABBED REPAIR PARTS IAW SRM 53-10-8 FIG 3 TABLE I AND MAE TRAVELER T5/486895. INSTALLED REPAIR PARTS IAW SRM 51-30-2. 2L73 4F RTA3WE 20050203000122005020300012NM 2005 2 3 SWAA050252 120050130A53216545833 WEB BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29602SW 27953 DURING SCHEDULED D-CHECK, FOUND FLOORWEB AT BS 178, LBL 24, CRACKED. REMOVED AND REPLACED FLOOR WEB SECTION PER SRM. 2L72 4F RTA16WE 20050203000202005020300020NM 2005 2 3 SWAA050258 120050128A53306545768 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 312, STRINGER 18R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20050203000232005020300023NM 2005 2 3 SWAA050260 120050130A3350101073 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29331SW 23695 DURING SCHEDULED 1/4D CHECK, FOUND AFT ENTRY DOOR EMERGENCY EXIT LIGHT LENS, CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20050203000262005020300026NM 2005 2 3 SWAA050268 120050201A53106546529 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29602SW 27953 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 500, STRINGER 28R, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050203000292005020300029EA 2005 2 3 COMA0560087 120050125A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01978CA 7158 FLOORBEAM AT RBL 27 CORRODED BEYOND LIMITS AT FS 559.00 + 32 - FS 574.00. REPAIRED IAW CRJ SRM 51-42-22, 51-21-11, 51-42-21, 51-42-13, 51-42-10. 2L72 4F RTA21EA 20050203000302005020300030NM 2005 2 3 SWAA050270 120050201A53306545765 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29685SW 23401 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 524, STRINGER 10L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20050203000332005020300033NM 2005 2 3 P5CA0501308 120050121A7830 THRUST REVERSER BOEING747 747283B 1384867NM PWA JT9 JT9D70A 52054NE NR 4 ENGINE INOPERATIVE A P5CAO OTHER O OTHER LDLANDING 1 EA15921FT 21575 689166 NR 4 ENGINE THRUST REVERSER WOULD NOT DEPLOY AFTER LANDING. NR 4 ENGINE THRUST REVERSER DEACTIVATED PER MEL 78-01-2A. REF MM 78-31-00. 2L74 4F4 F A20WE E3NE 20050203000352005020300035EA 2005 2 3 SWIA200514458 120050128A274170609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07411SW 7067 MACH TRIM DISENGAGES WHEN CAPTAINS PITCH TRIM IS ACTUATED. REPLACED MACH TRIM ENGAGE/DISENGAGE SWITCH IAW MM 27-41-25. REPLACED HSTCU IAW CRJ MM 27-41-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050203000372005020300037EA 2005 2 3 SWIA200514460 120050130A2741 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA COCKPIT STUCK A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07903SW 7425 CAPTAINS SIDE YOKE STAB TRIM STICKY DURING OPERATIONS. REMOVED AND REPLACED CAPTAINS SIDE STAB TRIM SWITCH, OPERATIONAL CHECK GOOD IAW CRJ MM 27-41-05. 2L72 4F RTA21EA 20050203000382005020300038EA 2005 2 3 SWIA200514461 120050125A5210 PIN CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07903SW 7425 MAIN CABIN DOOR WILL NOT OPEN FROM THE INSIDE WHEN CLOSED. REPLACED BROKEN PIN INSIDED THE INNER/OUTER DOOR HANDLE MECHANISM PER CMM 52-11-03 AND AMM 52-11-02. DOOR OPERATION CHECKS GOOD. 2L72 4F RTA21EA 20050203000432005020300043SO 2005 2 3 SWIA200514444 120050123A3350 BULB EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07560SW 120334 EMERGENCY FLOOR LIGHT INOPERATIVE (1ST BULB). RELAMPED FLOOR EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050203000482005020300048EU 2005 2 3 RAIA00501062 120050128A3260 WARNING SYSTEM JETAIRJETSTMJETSTM4101 1500501EU CONFIGURATION ACTIVATED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03563HK 41079 PIT- CONFIGURATION WARNING ON TAKEOFF. MAINTENANCE PERFORMED FUNCTIONAL TEST AND HIGH SPEED TAXI UNABLE TO DUPLICATE. 2L72 4T RTA41NM 20050203000552005020300055EU 2005 2 3 RAIA00501050 120050118A3251AIR860122 SELECTOR VALVE JETAIRJETSTMJETSTM4101 1500501EU NLG STEERING MALFUNCTIONED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03552HK14287 41057 STL- WITH FULL RUDDER DEFLECTION AIRCRAFT STILL PULLING TO THE RIGHT. MAINTENANCE REMOVED AND REPLACED STEERING SELECTOR VALVE. 2L72 4T RTA41NM 20050203000622005020300062EU 2005 2 3 RAIA00501060 120050128A3260 WARNING SYSTEM JETAIRJETSTMJETSTM4101 1500501EU CONFIGURATION ACTIVATED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03566HK 41084 STL - TAKEOFF CONFIGURATION WARNING ON TAKEOFF. MAINTENANCE PERFORMED ENGINE GROUND RUN AND TAKEOFF CONFIGURATION WARNING TESTED GOOD. 2L72 4T RTA41NM 20050203000632005020300063SO 2005 2 3 RAIA00501051 120050119A213122250N030301 CONTROLLER EMB 145 EMB145 3260210SO CABIN PRESSURE FAILED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03821HK8828 145068 STL - CABIN WOULD PRESSURIZE IN AUTO OR MANUAL MODE. MAINTENANCE REMOVED AND REPLACED PRESS CONTROLLER, PERFORMED GROUND CHECK. 2L72 4F RTT00011AT 20050203000642005020300064SO 2005 2 3 RAIA00501052 120050122A3000 WARNING LIGHT EMB 145 EMB145 3260210SO ANTI-ICE SYSTEM ILLUMINATED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03805HK 145096 RIC - ANTI-ICE FAIL EICAS MESSAGE. MAINTENANCE C/W TROUBLESHOOTING PROCEDURES, OPS CHECKED GOOD. 2L72 4F RTT00011AT 20050203000682005020300068WP 2005 2 3 DHL2004809521 120050117A57403645612U BRACKET DOUG DC8 DC873F 302199FWP BOOST PUMP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01809DH91189 46047 NR 4 ALT TANK AFT BOOSTER PUMP BRACKET CRACKED. REMOVED AND REPLACED AFT BOOSTER PUMP BRACKET (NR 4 ALT TANK) IAW SRM 51-1-20D PG 9, 21 SRM 51-3-1 PG 2A. 2L74 4F RT4A25 20050203000792005020300079WP 2005 2 3 DHL2004809522 120050117A5740 BRACKET DOUG DC8 DC873F 302199FWP SLOT DOOR BROKEN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01809DH91189 46047 LEFT OUTBOARD SLOT UPPER DOOR BRACKET BROKEN. REMOVED AND REPLACED BROKEN BRACKET TO OUTBOARD SLOT DOOR UPPER DOOR IAW MM 27-80-2 PG 201-202, MM 20-16-0 PG 201-208. 2L74 4F RT4A25 20050203000802005020300080NM 2005 2 3 SWAA050272 120050201A575465C26603102 SKIN BOEING737 7375H4 138449DNM RT WING SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29507SW 24184 DURING SCHEDULED SERVICE CHECK, FOUND RT WING NR 4 L/E SLAT DELAMINATED. REMOVED AND REPLACED NR 4 L/E SLAT PER MM. 2L72 4F RTA16WE 20050203000822005020300082NM 2005 2 3 SWAA050274 120050201A575465C26602311A SKIN BOEING737 7373H4 1384600NM LT WING SLAT DEBONDED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29617SW 27700 DURING SCHEDULED C4 CHECK, FOUND LT WING NR 2 L/E SLAT DISBONDED. REMOVED AND REPLACED NR 2 L/E SLAT PER MM. 2L72 4F RTA16WE 20050203000832005020300083NM 2005 2 3 SWAA050275 120050201A53106547973 CREASE BEAM BOEING737 7373K2 13844BANM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29340LV 23738 DURING SCHEDULED 1/2D CHECK, FOUND 3 EACH LT CREASE BEAM WEBS CRACKED AT BS 580, BS 620 AND BS 640. REMOVED AND REPLACED CREASE BEAM WEB SECTIONS PER SRM. 2L72 4F RTA16WE 20050203000842005020300084NM 2005 2 3 SWAA050263 120050201A33506556633 LIGHT BOEING737 7373H4 1384600NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29356SW 25251 DURING SCHEDULED RON, FOUND RT OVERWING EMERGENCY EXIT LIGHT, BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20050203000862005020300086NM 2005 2 3 SWAA050265 120050201A55536562274 ATTACH FITTING BOEING737 7373H4 1384600NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29602SW 27953 DURING SCHEDULED D-CHECK, FOUND VERTICAL STABILIZER PRIMARY CLEVIS FWD AND AFT LUGS CORRODED. REPAIRED VERTICAL STABILIZER PER ER. 2L72 4F RTA16WE 20050203001022005020300102EA 2005 2 3 SWIA200514463 120050128A5610 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAO OTHER O OTHER CRCRUISE 1 NM07457SW 7773 WHILE CRUISING AT FL350 F/O'S WINDSHIELD CRACKED. REMOVED AND REPLACED F/O'S WINDSHIELD ASSY IAW 56-11-01 AMM OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050203001042005020300104NM 2005 2 3 AALA20050068 120050201A3350 PIN BOEING767 767323 1385205NM BATTERY PACK BENT A AALAK NONE O OTHER ININSP/MAINT 1 SW2139365 24046 CDG - EMERGENCY EXIT LIGHTS AT SEAT 40HJ INOPERATIVE. FOUND BENT PIN ON BATTERY PACK M734. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHTS AT SEAT 40HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050203001082005020300108NM 2005 2 3 AALA20050063 120050130A3350 BATTERY BOEING777 777223 1385213NM EMERGENCY EXIT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21755AN 30263 DFW - EMERGENCY LIGHT AT SEAT 21C INOPERATIVE. REPLACED BATTERY FOR EMERGENCY LIGHT AT SEAT 21C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20050203001092005020300109NM 2005 2 3 AALA20050072 120050127A3350 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21652AA 24610 DFW - RIGHT AFT EXTERIOR OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK/CHARGER ASSEMBLY FOR RIGHT AFT EXTERIOR OVERWING EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050203001102005020300110WP 2005 2 3 AALA20050064 120050131A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217521A 49898 SFO - FIRST CLASS OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FIRST CLASS OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050203001132005020300113EA 2005 2 3 COMA0560091 120050126A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01483CA 7689 FLIGHT 5329 FLAPS FAIL CAUTION. INSPECTED AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20050203001142005020300114EA 2005 2 3 COMA0560098 120050129A2120 SMOKE CNDAIRCL600 CL6002B19 1900309EA COCKPIT DETECTED A COMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO01940CA 7048 FLIGHT 5128 SMOKE IN COCKPIT AFTER T/O. COULD NOT DUPLICATE. FOUND NO EVIDENCE OF SMOKE, OPERATED ALL SYSTEMS AND FOUND NO DEFECTS. 2L72 4F RTA21EA 20050203001152005020300115EA 2005 2 3 COMA0560101 120050130A56101393225 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A COMAO OTHER O OTHER CRCRUISE 1 SO01709CA8362 7238 FLIGHT 5530 PILOTS SIDE WINDOW CRACKED. REPLACED WINDOW. 2L72 4F RTA21EA 20050203001172005020300117EA 2005 2 3 COMA0560099 120050130A3260864202 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01956CA 7105 FLIGHT 5443 GEAR DISAGREE WARNING AFTER T/O. REPLACED THE LT NLG DOWNLOCK PROXIMITY SENSOR. 2L72 4F RTA21EA 20050203001212005020300121NM 2005 2 3 SWAA050287 120050201A33506042221 BATTERY BOEING737 737317 138447PNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 DURING SCHEDULED SERVICE CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20050203001222005020300122NM 2005 2 3 SWAA050288 120050201A3350D71702001 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT FAILED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29793SA 27888 DURING SCHEDULED HC1 CHECK, MID CABIN RT EMERGENCY EXIT LIGHT BATTERY FAILED TEST. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20050203001232005020300123 2005 2 3 SWAA050289 420050201A256563550 SLIDE BOEING737 7377H4 1384404NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29793SA 27888 DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050203001052005020300105WP 2005 2 3 AALA20050065 120050131A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21416AA 49327 DFW - CEILING EMERGENCY LIGHTS FROM ROW 24 TO 31 INOPERATIVE. REPLACED BATTERY PACKS FOR CEILING EMERGENCY LIGHTS AT ROWS 24 TO 31. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050203001112005020300111WP 2005 2 3 AALA20050069 120050201A3350 CONTACT HONEYWELL DOUG DC9 DC982 3022082WP BATTERY PACK DIRTY A AALAK NONE O OTHER ININSP/MAINT 1 SW217536A 49990 TPA - OVERWING FORWARD EMERGENCY EXIT LIGHTS INOPERATIVE. CLEANED BATTERY CONTACTS FOR OVERWING FORWARD EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050203001162005020300116EA 2005 2 3 COMA0560097 120050129A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA PAX DOOR OVERSERVICED A COMAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 SO01966CA 7132 FLIGHT 5165 CABIN DOOR OUTER HANDLE CAUTION. CLEANED EXCESS GREASE FROM DOOR HANDLE, NO DEFECTS FOUND. 2L72 4F RTA21EA 20050203001182005020300118NM 2005 2 3 SWAA050284 120050201A574369378775 FITTING BOEING737 7373H4 1384600NM LT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29653SW 28398 DURING SCHEDULED SERVICE CHECK, FOUND LT MLG FWD OUTBOARD HAGER FITTING, CORRODED. REPAIRED FITTING PER EA. 2L72 4F RTA16WE 20050203001252005020300125WP 2005 2 3 AALA20050070 120050127A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW2159523 49915 TPA - EMERGENCY LIGHT ABOVE CATWALK AND TAIL CONE INOPERATIVE. REPLACED BATTERY PACK IN AFT RIGHT HAND LAVATORY AND REPAIRED BROKEN WIRE AT AFT CEILING ABOVE CATWALK FOR EMERGENCY LIGHTS ABOVE CATWALK AND TAIL CONE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050203001272005020300127WP 2005 2 3 DHL2004809523 120050120A5753 STRUCTURE DOUG DC8 DC873F 302199FWP TE FLAPS WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01809DH91189 46047 RT WING OUTBOARD FLAP UPPER FWD PLATING WORN, XF 227.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 01-19-05, DWG X32-R04 REV-A DATE 01-19-05. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. TRIMMED OUT DAMAGED PLATING SEGMENT IAW DWG X32-R04. PERFORMED ND INSPECTION IAW DC8 NDT SPM PART 06-10-01-001, DWG X32-R04. FABRICATED NEW PLATING SEGMENT (AL7075-T6 0.071) INTERNAL SPLICE (AL7075-T6 0.080) IAW DWG X32-R04. CLEANED TREATED AND PRIMED AREA, INTERNAL SPLICE AND NEW PLATING SEGMENT INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS WITH NEW FASTENERS IAW DWG X32-R04, SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20050203001282005020300128WP 2005 2 3 DHL2004809520 120050114A5230 SUPPORT DOUG DC8 DC873F 302199FWP CARGO DOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01809DH91189 46047 B-CARGO DOOR RT ROLLER SUPPORT CRACKED. REMOVED B-CARGO DOOR IAW MM 52-32-1 PG 201. REMOVED AND REPLACED RT ROLLER SUPPORT IAW OHM 52-3-5 PG 1-2. REINSTALLED B-CARGO DOOR IAW MM 52-32-1 PG 201-203. OPS CHECKED GOOD IAW MM 52-30-0 PG 7-11. 2L74 4F RT4A25 20050203001332005020300133WP 2005 2 3 DHL2004809529 120050117A53403750545502 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01809DH91189 46047 AFT CARGO COMPT SPLICE FITTING CRACKED 2.000 BETWEEN STA 1060.000 AND STA 1040.000, L-35R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED SPLICE FITTING IAW DC8 SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 10-13, SRM 51-1-21 PG 1. TORQUED IAW SRM 51-3-1 PG 2A. 2L74 4F RT4A25 20050203001382005020300138EA 2005 2 3 COMA0560089 120050127A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA RT TE FLAPS UNRELIABLE A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01989CA181301510 7215 FLIGHT 5142 FLAPS FAIL CAUTION. REPLACED THE RT BPSU. 2L72 4F RTA21EA 20050203001392005020300139EU 2005 2 3 RAIA00501061 120050128A3260 WARNING LIGHT JETAIRJETSTMJETSTM4101 1500501EU CONFIGURATION ILLUMINATED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03563HK 41079 PIT - CONFIGURATION WARNING ILLUMINATED ON TAKEOFF. MAINTENANCE OPS CHECKED AND PERFORMED HIGH SPEED TAXI UNABLE TO DUPLICATE. 2L72 4T RTA41NM 20050203001412005020300141NM 2005 2 3 UPS05243763 120050111A531265229135 STRUCTURE BOEING727 727185C 138406NNM FIREWALL CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 INSPECTION TYPE:C, SUSPECT CRACK ON LT CHORD ABOVE NR 2 ENGINE HORIZONTAL FIREWALL AT UPPER END OF CHORD. HFEC CARRIED OUT IAW NDTM PART 6 51-00-00, FIG 4. CRACK FOUND TO BE 5.0 INCH IN LENGTH. CHORD REMOVED AND NEW CHORD DRILLED OFF AND INSTALLED IAW SRM 51-30-02. 2L73 4F A3WE 20050203001432005020300143NM 2005 2 3 UPS05243768 120050110A7120 BUSHING BOEING727 727185C 138406NNM NR 3 ENG MOUNT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 INSPECTION TYPE:C, ENGINE NR 3 FWD MOUNT FITTING HAS PITTING CORROSION IN BOTH O/B (LARGE) HOLES. FWD O/B HOLE BUSHING REMOVED OHM 20-50-03. HFEC CARRIED OUT IAW NDTM 51-00-00 FIG 13, NO DEFECTS FOUND. REPAIRED IAW UPS EO B727-5440-11592-A. 2L73 4F A3WE 20050203001442005020300144NM 2005 2 3 UPS05243769 120050110A5280651756395 DOOR BOEING727 727185C 138406NNM NLG CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 INSPECTION TYPE:C, NLG LT FWD DOOR HAS EVIDENCE OF CORROSION UNDER SEAL RETAINER. LT NLG DOOR REMOVED AND REPLACED IAW AMM 32-22-01. 2L73 4F A3WE 20050203001462005020300146NM 2005 2 3 UPS05243776 120050106A5414 PANEL BOEING727 727185C 138406NNM NR 3 PYLON DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 INSPECTION TYPE:C, ENGINE NR 3 PYLON PANEL 5508 IS DELAMINATED INNER SURFACE FWD END. PANEL REPAIRED IAW MM 20-60-04. 2L73 4F A3WE 20050203001482005020300148NM 2005 2 3 UPS05243783 120050110A5320 WEB BOEING727 727185C 138406NNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 INSPECTION TYPE:C, RT VENTRAL STAIRWAY TORQUE BOX WEB SKIN CRACK EXTENDING BEYOND STOP DRILL HOLE ON FWD O/B END ADJACENT TO FUEL SHROUD HOLE & CRACK ON DOUBLER AT AFT SIDE BS 1263. REPAIR CARRIED OUT IAW EO B727-5310-1239-E. 2L73 4F A3WE 20050203001502005020300150NM 2005 2 3 SWAA050223 120050127A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 370, STRINGER 26L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20050203001522005020300152NM 2005 2 3 SWAA050225 120050127A57536546435277 SKIN BOEING737 7373H4 1384600NM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED C4 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED T/E AFT FLAP PER MM. 2L72 4F RTA16WE 20050203001532005020300153NM 2005 2 3 SWAA050226 120050127A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SPV, FOUND STRINGER CLIP AT BS 887, STRINGER 2L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20050203001552005020300155NM 2005 2 3 SWAA050228 120050127A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 747, STRINGER 19R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050203001582005020300158NM 2005 2 3 AWXA200500079 120050127A335020121 CHARGER BOEING737 7373Y0 1384671NM FUSELAGE DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28334AW 23747 DEN - EEL - DURING 4-DAY CHECK FOUND R-2 DOOR EXTERNAL EMERGENCY ESCAPE LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY CHARGER M1136 AND BATTERY CHARGER M1137. REPLACED SPLICE SP2988 AND WIRE W1160-C-1 PER WDM 33-51-31 PAGE 1, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050203001592005020300159WP 2005 2 3 CALA0500022 120050126A5320991061267 STRUCTURE DOUG DC9 DC982 3022082WP SUBFLOOR CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2735836 49441 INSPECTION FOUND SUBFLOOR CORRODED UNDER LEFT O/B SEAT TRACK AT STA 1174, LBL 60. THE CORRODED AREA WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 51-70-4. 2L72 4F A6WE 20050203001602005020300160NM 2005 2 3 CALA0500023 120050106A5315146N5089 FLOORBEAM BOEING757 757224 1384958NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717104 27294 INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 1640, RBL 3. THE CORROSION WAS REMOVED AND THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, FIGURE 203. 2L72 4F RTA2NM 20050203001622005020300162WP 2005 2 3 CALA0500025 120050127A5320993653469 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2735836 49441 INSPECTION FOUND A 1 INCH CRACK AT FORWARD O/B END OF FORWARD ENTRY FLOOR SUPPORT TEE AT STA 180, RBL 43. A REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 2. 2L72 4F A6WE 20050203001642005020300164NM 2005 2 3 CALA0500027 120050127A5320143N5434 INTERCOSTAL BOEING757 757224 1384958NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717104 27294 INSPECTION FOUND RT SIDE INTERCOSTAL CORRODED ON TOP SURFACE AT BS 680, RBL 56, WL 207. THE CORRODED SECTION OF INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-30-01, FIGURE 7 AND 51-40-02, FIGURE 3 & 12. 2L72 4F RTA2NM 20050203001652005020300165NM 2005 2 3 QXEA200500142 120050129A3297471515 WIRE HARNESS BOMBDRDHC8 DHC8401 1390041NM NLG BROKEN A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09400QX8933 4030 SEA - FLIGHT 2439 - AFTER TAKEOFF, THE CREW WAS UNABLE TO GET THE LANDING GEAR TO RETRACT. THE LANDING GEAR FAILS TO RETRACT CHECKLIST WAS COMPLIED WITH BUT THE GEAR STILL WOULD NOT RETRACT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NOSE LANDING GEAR WOW NR 2 HARNESS BROKEN. THE HARNESS WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050203001662005020300166WP 2005 2 3 CALA0500028 120050128A53159958238 FLOORBEAM DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2735836 49441 INSPECTION FOUND FLOORBEAM CORRODED AT STA 1322 UNDER RT LAV, RBL 20. THE CORRODED SECTION OF FLOORBEAM WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 79A. 2L72 4F A6WE 20050203001672005020300167SO 2005 2 3 SWIA200514439 120050123A3350 COVER EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07578SW 120346 EMERGENCY EXIT LIGHT NEAR MAIN CABIN DOOR COVER IS BROKEN. REPLACED EMERGENCY LIGHT NEAR CABIN DOOR IAW MM 33-51-02, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050203001692005020300169NM 2005 2 3 ABXA050025 120050128A3260 WARNING LIGHT BOEING767 767281 1385109NM MLG ILLUMINATED A ABXAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 GL23768AX 22786 EICAS MESSAGE GEAR DISAGREE DISPLAYED AND GEAR AMBER LIGHT ILLUMINATED WITH GEAR DOWN LIGHTS ILLUMINATED. INITIALLY THERE WAS NO RIGHT MAIN GREEN LIGHT DOWN. THE LIGHT CAME ON DURING RETURNING FOR APPROACH. PERFORMED BITE OF PSEU AND FOUND LANDING GEAR LEVER SWITCH SYSTEM NR 1 AND NR 2 FAULTED. PUT HANDLE IN FULLY DOWN POSITION AND LANDING POSITION INDICATING OPS CHECKED GOOD IAW B767 MM 32-61-00. PERFORMED FIM 32-30-00. INSPECTED GEAR SWITCHES AND NO DEFECTS NOTED. NOTE: THIS FLIGHT PERFORMED A GO-AROUND. THE CREW SPECIFICALLY REPORTED THAT THEY DID NOT RECYCLE THE GEAR. FLIGHT CONTROL REPORTED THAT THE CREW DID DECLARE AN EMERGENCY ON THEIR FINAL APPROACH. 2L72 4F RTA1NM 20050203001702005020300170EA 2005 2 3 COMA0560093 120050126A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01982CA 7168 FLIGHT 5436 LEFT FLAP POSITION INDICATES 20 DEGREES AND RIGHT FLAP INDICATES 0 DEGREES. INSPECTED AND OPERATED FLAP SYSTEM, NO DEFECTS FOUND. COULD NOT DUPLCIATE. 2L72 4F RTA21EA 20050203001722005020300172NM 2005 2 3 CALA0500030 120050127A3397285W00294 CONTROL UNIT BOEING777 777224 1385225NM CABIN SHORTED A CALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW2778004 27580 A STRONG BURNING ODOR WAS OBSERVED THROUGHOUT THE CABIN AFTER TAKEOFF FROM IAH. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE OVERHEAD ELECTRONIC UNIT (OEU) FOR WORK LIGHTS AT L-3 AND R-3 DOOR AT FAULT. THE OEU WAS REMOVED AND REPLACED IAW MM 23-33-02-000-803. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00001SE 20050203001732005020300173EA 2005 2 3 SWIA200514465 120050106A5310 BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07438SW 7574 MAIN FUSELAGE FS 280 AT RBL 9.0 LOWER FLANGE CRACKED ON TRANSVERSE BEAM AND OUTBOARD CLIP CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-11-171 REV A. 2L72 4F RTA21EA 20050203001742005020300174EA 2005 2 3 SWIA200514466 120050106A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07438SW 7574 FS 280 RBL 9.0 INBOARD ATTACH CLIP CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00. 2L72 4F RTA21EA 20050203001752005020300175EA 2005 2 3 SWIA200514467 120050106A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA FLOORBEAM CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07438SW 7574 FS 280 LEFT FLOORBEAM LBL 9.0 OUTBOARD ATTACH CLIP CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00. 2L72 4F RTA21EA 20050203001762005020300176EA 2005 2 3 SWIA200514468 120050106A5340 SUPPORT FITTING CNDAIRCL600 CL6002B19 1900309EA FLOORBEAM CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07438SW 7574 FUSELAGE; FLOORBEAM SIDEWEB OUTBOARD SIDE HAS A CRACKED SUPPORT FITTING FS 460.00 RBL 9.0. ITEM FOUND AT C-CHECK INSPECTION. FITTING REPLACED IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-25-16, 51-21-11. 2L72 4F RTA21EA 20050203001822005020300182EA 2005 2 3 COMA0560086 120050125A5712 RIB CNDAIRCL600 CL6002B19 1900309EA WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01978CA 7158 CRACK FOUND TO BATT RIB ASSEMBLY AT WS 53.60 IN MLG BAY RIGHT HAND. REPAIRED IAW REO 601R-57-51-046. 2L72 4F RTA21EA 20050203001832005020300183 2005 2 3 SWAA050243 420050128A256563550 SLIDE BOEING737 7377H4 1384404NM L2 & R2 DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29411WN 29821 L2 AND R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED L2 AND R2 DOOR EVAC SLIDES PER MM. 2L72 4F RTA16WE 20050203001842005020300184 2005 2 3 SWAA050244 420050128A256563550 SLIDE BOEING737 7377H4 1384404NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29440LV 29835 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050203001852005020300185NM 2005 2 3 SWAA050245 120050128A5755654645262A HINGE BOEING737 7373H4 1384600NM RT WING SPOILER BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED C3 CHECK, FOUND RT WING NR 5 GROUND SPOILER HINGE BROKEN. REMOVED AND REPLACED RT WING NR 5 GROUND SPOILER PER MM. 2L72 4F RTA16WE 20050203001862005020300186NM 2005 2 3 SWAA050246 120050128A53306545772 SKIN BOEING737 7373H4 1384600NM FUSELAGE CHAFED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SPV, FOUND FUSELAGE SKIN CHAFED AT DORSAL FIN CONTACT AREA, FROM LT AND RT BS 863 TO 883, RT BS 911 TO 929, AND LT BS 964 TO BS 969. REPAIRED SKIN SECTIONS PER ER. 2L72 4F RTA16WE 20050203001872005020300187NM 2005 2 3 SWAA050247 120050130A53116546530 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29602SW 27953 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 480, STRINGER 8R, CRACKED. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20050203001912005020300191NM 2005 2 3 SWAA050291 120050201A534065C27314 STRINGER CLIP BOEING737 7373K2 13844BANM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29340LV 23738 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP AT BS 663, STRINGER 10L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20050203001982005020300198NM 2005 2 3 SWAA050281 120050201A53156545833 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 DURING SPV, FOUND 2 EACH CRACKS ON FLOORBEAM WEB BETWEEN BS 188 TO BS 196, AT LBL 30 AND RBL 30. REMOVED AND REPLACED WEB SECTIONS PER SRM. 2L72 4F RTA16WE 20050203001992005020300199NM 2005 2 3 SWAA050282 120050201A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29361SW 26572 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 767, STRINGER 25L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050203002012005020300201WP 2005 2 3 AALA20050073 120050128A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21566AA 49348 TUL - OVERHEAD EMERGENCY LIGHTS AT ROWS 25 TO 29 INOPERATIVE. REPLACED BATTERY PACK AT STATION 1190 FOR OVERHEAD EMERGENCY LIGHTS AT ROWS 25 TO 29. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050203002032005020300203WP 2005 2 3 AALA20050076 120050130A25308201110000D OVEN DOUG DC9 DC983 3022083WP GALLEY DIRTY A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW219619V 53566 AUS - INFLIGHT CREW REPORTED SMOKE IN FIRST CLASS GALLEY. FOUND NUMBER ONE OVEN DIRTY AND SMOKING AROUND HEATER ELEMENT. STEAM CLEANED NUMBER ONE OVEN. RAN OVEN ONE HOUR AND CLEANED ELEMENTS AND INTERIOR OF OVEN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050301000122005030100012NM 2005 3 1 UPS05443924 120050211A5711 FITTING BOEING747 747123 1384873NM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, RT WING REAR SPAR UPPER SPLICE FITTING AT BS 1241 NR 4 HOLE FOUND CRACKED AT INTERNAL SPLICE FITTING APPROX 0.060 INCH. HOLE REWORK PER SB 747-57A2314. 2L74 4F A20WE 20050207000062005020700006NM 2005 2 7 SWAA050300 120050202A53106545410 CREASE BEAM BOEING737 7373K2 13844BANM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29340LV 23738 DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM WEB BETWEEN BS 616 AND BS 639, RBL 70, CRACKED. REMOVED AND REPLACED CREASE BEAM WEB PER SRM. 2L72 4F RTA16WE 20050207000102005020700010EU 2005 2 7 05FDEA00199 120050129A5230 SKIN AIRBUS300 A300B4622 3930401EU CARGO DOOR DENTED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25716FD 358 POST FLT WALK AROUND FOUND DENT ON LOWER FWD CORNER OF LOWER FWD CARGO DOOR. DENT IS O/B OF DOOR SEAL. DENT MEASURES 2.75 INCH LONG AND .75 INCH DEEP. TERMINATING ACTION ACCOMPLISHED FOR EA 6-5230-85502 AT 28,081:53 H 30,451 C. REMOVED AND REPLACED CORNER PLATE OF FWD CARGO, LOWER FWD CORNER. COMPLIED WITH FED EX EA 6-5230-85502 PT3. 2L72 4F RTA35EU 20050207000112005020700011NM 2005 2 7 QXEA200500144 120050127A5230502213 SEAL BOMBDRDHC8 DHC8401 1390041NM CARGO DOOR DAMAGED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09409QX7745 4051 THE FLIGHT WAS DIVERTED WHEN DURING THE CLIMB, THE CREW RECEIVED A CABIN PRESSURE MASTER WARNING. THE CHECK LISTS WERE COMPLIED WITH BUT THE CREW WAS UNABLE TO CONTROL THE PRESSURIZATION. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE AFT CARGO DOOR SEAL. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050207000122005020700012NM 2005 2 7 2005UALA00087 120050122A5330146W63511 SKIN PANEL BOEING777 777222 1385219NM PWA PW4077PW4077 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29775UA36561 26947 EXTERNAL FUSELAGE SKIN DAMAGED 30 INCHES BELOW AFT BULK CARGO DOOR. MAJOR REPAIR ACCOMPLISHED. DAMAGE WAS CUT OUT AND EXTERNAL REPAIR ACCOMPLISHED PER 777 SRM 53-00-01, REPAIR 7, ZONE B. 2L72 4F4 FRTT0001SE E46NE 20050207000142005020700014NM 2005 2 7 2005UALA00089 120050123A3350 LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE ROW 1 DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29528UA 25018 EMERGENCY EQUIPMENT LIGHT DAMAGED ROW 1. REPLACED STRIP 2L72 4F4 FRTA2NM E17NE 20050207000182005020700018NM 2005 2 7 CALA0500039 120050202A531165C479592 FRAME BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712319 23370 INSPECTION FOUND AFT CARGO COMPARTMENT FORWARD DOOR JAMB FRAME CORRODED AT LATCH FITTING, STA 787, S19R TO S27R. A NEW FRAME WAS INSTALLED IAW SRM 51-40 AND ECRA 5310-04456. 2L72 4F RTA16WE 20050207000222005020700022NM 2005 2 7 2005UALA00092 120050125A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE AFT PIT STA DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29597UA 28750 AFT PIT STA 1580 FRAME IS DENTED ON INBOARD FLANGE AT STR 25. MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME FLANGE WITH NESTED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20050207000242005020700024NM 2005 2 7 2005UALA00094 120050125A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29597UA 28750 AFT PIT FUSELAGE FRAME INNER FLANGE IS DENTED AT BS 1440, STR 25L. MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME FLANGE WITH A NESTED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20050207000252005020700025NM 2005 2 7 2005UALA00095 120050125A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29597UA 28750 AFT PIT FUSELAGE FRAME INNER FLANGE IS DENTED AT BS 1400, STR 25L. *S/D* DAMAGE DUE TO TYPICAL CARGO LOADING IN AFT PIT. MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME FLANGE WITH NESTED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20050207000262005020700026NM 2005 2 7 SWAA050293 120050202A53156546809 FLOORBEAM BOEING737 7373H4 1384600NM FUSLAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29603SW 27954 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 947, LBL 20, CORRODED. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20050207000272005020700027NM 2005 2 7 SWAA050294 120050202A53116546558 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29603SW 27954 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 908, STRINGER 8L, CRACKED. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20050207000282005020700028NM 2005 2 7 SWAA050295 120050202A531165C22909 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29603SW 27954 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 500C, RBL 2, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20050207000292005020700029NM 2005 2 7 SWAA050296 120050202A53156545812 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29603SW 27954 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 328, BETWEEN RBL 54 TO RBL 59, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM. 2L72 4F RTA16WE 20050207000302005020700030NM 2005 2 7 SWAA050297 120050202A3350101073 LENS BOEING737 7373A4 1384585NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29680AA 23505 DURING SPV, FOUND R1 DOOR EMERGENCY EXIT LIGHT LENS, BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20050207000312005020700031NM 2005 2 7 SWAA050298 120050202A53306545772 SKIN BOEING737 7373A4 1384585NM FUSELAGE DEBONDED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29680AA 23505 DURING SPV, FOUND FUSELAGE SKIN BETWEEN BS 887 AND BS 897, BETWEEN STRINGERS 5L AND 9L, DISBONDED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050207000332005020700033NM 2005 2 7 2005UALA00026 120050101A2613899252 SENSING ELEMENT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE NR 1 ENGINE DAMAGED A UALAE ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 WP29322UA 23954 722206 CREW REPORT NR 1 ENG -A- OVERHEAT LIGHT ILLUMINATED. *S/D* CREW REPORTED NR 1 ENGINE -A- LOOP OVERHEAT LIGHT ILLUMINATED. SHUTDOWN ENGINE AND DISCHARGED BOTH FIRE EXTINGUISHER BOTTLES. OVERHEAT DETECTION LOOP -B- WAS INOPERATIVE AND DEFERRED, ELIMINATING REDUNDANCY FEATURE OF THE OVERHEAT DETECTION SYSTEM. PERFORMED TROUBLESHOOTING OF OVERHEAT DETECTION SYSTEM. FOUND LOWER FAN CASE LOOP -A- DETECTOR M1121 INTERMITTENT. INSTALLED SERVICEABLE OVERHEAT DETECTOR LOOP. 2L72 4F4 FRTA16WE E2GL 20050207000342005020700034WP 2005 2 7 05FDEA00201 120050129A78309007M61G08 BLOCKER DOOR DOUG MD10 MD1010F 3022112WP ZONE 400 DEBONDED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25363FE 48263 NR 3 ENGINE RIGHT T/R NR 4 BLOCKER DOOR BROKE. REMOVED AND REPLACED NR 3 RIGHT T/R NR 4 BLOCKER DOOR IAW MD-10-10 MM 78-32-06-2. 2L73 4F RTA22WE 20050207000362005020700036EU 2005 2 7 05FDEA00210 120050201A5315 FLOORBEAM AIRBUS310 A310203 3930313EU ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25405FE 237 MDDC FLOORBEAM AT FR37 LT SIDE CRACKED AT VERTICAL STIFFENER, FWD SIDE. REPAIRED FLOORBEAM BY INSTALLATION OF REPAIR ANGLES IAW A310-200 SRM 53-10-15 FIG 201, SH2. 2L72 4F RTA35EU 20050207000392005020700039EU 2005 2 7 05FDEA00214 120050201A5310 BEAM AIRBUS300 A300B4622 3930401EU ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25716FD 358 LOWER FLANGE UPPER SURFACE OF LONGITUDINAL BEAM 5 LT AT FRAME 52A HAS A .5 INCH LONG CRACK, VERIFIED BY EDDY CURRENT INSPECTION. STOP DRILLED CRACK AND DOUBLE FLUSH PLUGGED HOLE PER EO 6-5310-7-5010 SECTION C8. 2L72 4F RTA35EU 20050208000042005020800004NM 2005 2 8 05FDEA00241 120050204A5311 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 MAIN DECK - DENT MARKS AT RIGHT HAND FRAME AT STA Y= 1681 LONGERON 12. LONGERON 12 REPAIRED PER SRM 53-30-00 VOLUME I, FIGURE 1. 2L73 4F RTA22WE 20050208000052005020800005NM 2005 2 8 05FDEA00069 120050111A5310 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25235FE 21329 BS 720A, RBL 25, WL 153 SHEAR TIE CORROSION. REPAIRED PER SRM 53-10-4. 2L73 4F RTA3WE 20050208000072005020800007EU 2005 2 8 05FDEA00218 120050201A5320A53986743205 PLATE AIRBUS310 A310203 3930313EU ZONE 100 BENT A FDEAK NONE O OTHER ININSP/MAINT 1 SO25425FE 264 PLATE AND SEC-L BENT AND BROKEN BETWEEN FR86 AND FR87. REMOVED PLATE AND FABRICATED NEW SEC-L. INSTALLED NEW SEC-L AND PLATE IN A/C. 2L72 4F RTA35EU 20050208000082005020800008WP 2005 2 8 CALA0500031 120050129A5321S3932194B48118 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE DELAMINATED A CALAK NONE O OTHER ININSP/MAINT 1 SW2735836 49441 INSPECTION FOUND LT CENTER FLOOR PANEL DELAMINATED AND HOLES PUNCHED IN PANEL AT STA 465-541, LBL 20 TO LBL 40. A NEW PANEL WAS INSTALLED IAW SRM 53-05, PAGE 122B. 2L72 4F A6WE 20050208000132005020800013EU 2005 2 8 05FDEA00226 120050202A5753A57960112221 RIB AIRBUS300 A300B4622 3930401EU ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25716FD 358 AFTER REMOVAL OF I/B FLAP TOP SKIN, PERFORMED HIDDEN DAMAGE INSPECTION AND FOUND NR 2 AIRFOIL RIB AFT SECTION HAS CRACKED APPROX 8.5 INCHES LONG AND NR 3 RIB ON TOP SIDE ANGLE SUPPORT STRUCTURE HAS CRACKED APPROX 2.5 INCHES LONG AND 2 EA STIFFENERS WITH CRACKS ON CORNER WEB AS MARKED. REMOVED AND REPLACED RIB 25A. FABRICATED 2 EA BRACKETS P/N A57960114-209 & A57960114-221. REMOVED AND REPLACED 2 EA BRACKETS IAW DWG A57960114, A57960005 AND EA 6-5750- 85635. 2L72 4F RTA35EU 20050208000142005020800014EU 2005 2 8 05FDEA00227 120050202A5753A57960007001 SKIN AIRBUS300 A300B4622 3930401EU ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25716FD 358 AFTER REMOVAL OF CHAFF PLATE ON RIGHT I/B FLAP, DID HIDDEN DAMAGE INSP FOR N00064, AND FOUND I/B FLAP TOP SKIN HAS 2 EA CRACKS. REPLACED SKIN IAW DWG A57960007 AND EA 6-5750-85635. 2L72 4F RTA35EU 20050208000162005020800016EU 2005 2 8 05FDEA00229 120050202A5230A5237008120600 PLATE AIRBUS300 A300B4622 3930401EU ZONE 800 DENTED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25716FD 358 POST FLT WALKAROUND FOUND DENT ON LOWER FWD CORNER OF LOWER FWD CARGO DOOR. DENT IS O/B OF DOOR SEAL. DENT MEASURES 2.75 INCHES LONG AND .75 INCH DEEP. TERMINATING ACTION ACCOMPLISHED FOR EA 6-5230-85502 AT 28,081:53 H 30,451 C. REMOVED AND REPLACED CORNER PLATE OF FWD CARGO, LOWER FWD CORNER. COMPLIED WITH FED EX EA 6-5230-85502 PT3. 2L72 4F RTA35EU 20050208000212005020800021NM 2005 2 8 DLM88050041 120050117A4990 CAP DOUG MD88 MD88 3023688NM PWA JT8 JT8D NE APU OIL LEAKING A DALAO OTHER KBJFLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 SO27965DL13215 49984 P80528 BOTH AFT LAV SMOKE DETECTION WENT OFF IN FLIGHT. FOUND APU OIL LEAK AT CAP. REPLACED CAP/O-RING. CLEANED APU INLET AND PERFORMED A DUCT BURNOUT PER THE M/M. 2L72 4F4 FRTA6WE E2EA 20050208000222005020800022NM 2005 2 8 SWAA050309 120050203A53116558280 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29603SW 27954 DURING SPV, FOUND FRAME AT BS 360, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20050208000232005020800023NM 2005 2 8 05FDEA00235 120050203A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 100 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 SEAT TRACK CROWN AREA AT APPROXIMATE STA Y= 1701, X= 27.5 FOUND WORN. SMOOTHENED, MATERIAL REMOVED= 0.006", ORIGINAL THICKNESS= 0.414", REMAINING THICKNESS= 0.408" WITHIN PER SRM 53-10-00 VOLUME I, FIGURE 3. 2L73 4F RTA22WE 20050208000262005020800026NM 2005 2 8 DLM88050042 120050117A3320 BALLAST DOUG MD88 MD88 3023688NM ROW 22 LEFT BIN OVERHEATED A DALAH DEACTIVATE SYST/CIRCUITS MB OVER TEMP SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27976DL 53257 AT GATE WHILE BOARDING, A PAX NOTICED SMOKE FROM ROW 22 LEFT OVERHEAD BIN. INSPECTED AREA AND FOUND SIDEWALL LIGHT BALLAST OVERHEATED. REPLACED SAME. 2L72 4F RTA6WE 20050208000292005020800029NM 2005 2 8 DLM88050045 120050119A53119923406504 FRAME DOUG MD88 MD88 3023688NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27909DL 49540 FUSELAGE FRAME AT STATION 886 CRACKED ON FLANGE BELOW FLOOR LINE ADJACENT TO LONGERON 18R. FRAME REPLACED IAW ERA 095971-14. 2L72 4F RTA6WE 20050208000312005020800031NE 2005 2 8 DL738050047 220050120A7261CFM567 ENGINE BOEING737 737832 13844CFNM CFMINTCFM567CFM567B22 13802NE NR 2 LEAKING A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO27376DA17524 29624 874488 AFTER 1 HR 30 MIN RIGHT ENGINE OIL QTY WENT TO 4 WITH A LOW LIGHT. AFTER 40 MORE MINUTES OIL QTY WENT TO 3. DESCENT QTY WENT TO 5. AFTER SHUTDOWN QTY WENT TO 12. SERVICED NR 2 ENGINE WITH 26 PINTS OF OIL BAGGED ENGINE DRAINS AND RAN AT PWR. NO LEAKS NOTED, ALSO LOOKED IN INLET AND TAIL PIPE NO INDICATION OF OIL LEAKS. RETURN TO SERVICE. 2L72 4F4 FRTA16WE E00055EN 20050208000322005020800032NM 2005 2 8 DL76S050048 120050121A5512185T1003 SKIN BOEING767 767332 1382001NM HORIZONTAL STAB DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO27128DL 24078 DELAMINATION WAS FOUND ON FWD TORQUE BOX SKIN OF LT HORIZONTAL STABILIZER. DAMAGE WAS LOCATED ON UPPER SKIN, AT FRONT SPAR STA 108. REPAIRED PER ERA 096372-14. 2L72 4F RTA1NM 20050208000332005020800033NM 2005 2 8 1HA200597001 120050128A2781 POSITION SWITCH BOEING727 727270 138408PNM LE FLAPS OUT OF ADJUST A C1HAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL15697CA 23052 L/E FLAPS [AMBER] LIGHT REMAINED ILLUMINATED UPON CLIMB AT/FLAP RETRACTION. NR 5 L/E FLAP ALSO ILLUMINATED ON F/E'S AUX PANEL. ADJUSTED NR 5 L/E FLAP POSITION SWITCH ACTUATOR ARM IAW 727 MM 27-82-11. ALL OPS & INDICATIONS NORMAL, OK FOR CONTINUED SERVICE. 2L73 4F RTA3WE 20050208000372005020800037WP 2005 2 8 DHL2004809526 120050118A53205653923505 PANEL DOUG DC8 DC873F 302199FWP FUSELAGE DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01809DH91189 46047 AFT FUSELAGE 732 LWR PANEL EDGE UNBONDED AND DELAMINATED, STA 980.000 TO STA 1060.000. REMOVED DELAMINATED PANEL IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PANEL ASSY IAW SRM 51-3-0. 2L74 4F RT4A25 20050208000382005020800038WP 2005 2 8 DHL2004809519 120050114A53305654557503 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01809DH 46047 LT FWD ADF SENSE ANTENNA PANEL INTERNAL SKIN DELAMINATED (STA 810.000-855.000). REMOVED LT FWD ADF SENSE ANTENNA PANEL IAW SRM 51-3-0 PG 1. CLEANED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW LT FWD ADF SENSE ANTENNA PANEL IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20050208000412005020800041WP 2005 2 8 DHL2004809527 120050117A573056551651 SKIN DOUG DC8 DC873F 302199FWP LT WING DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01809DH91189 46047 LT WING - REMOVE AND INSTALL NR 1 SPOILER FOR DELAMINATION ON UPPER SKIN, XW 5.000 TO XW 90.000. REMOVED AND REPLACED NR 1 SPOILER (O/H CONDITION) ON LT WING XW 5.000 TO XW 90.000 (LT WING) IAW MM 27-61-1 PG 201-205. 2L74 4F RT4A25 20050208000452005020800045NM 2005 2 8 P5CA0501311 120050127A21507644763 VALVE BOEING747 747230B 1384889NM NR 3 A/C PACK FAILED A P5CAK NONE O OTHER ININSP/MAINT 1 EA15509MC 21221 NR 3 PACK HAD NO CONTROL FROM FLIGHT ENGINEERS STATION. PACK STAYS ON AND WILL NOT SHUT DOWN. REMOVED AND REPLACED FLOW CONTROL VALVE PER MM 21-51-00. 2L74 4F A20WE 20050208000462005020800046NE 2005 2 8 DL764050030 220050113A7200CF680C2B8F ENGINE BOEING767 767432ER 1385134NM GE CF6 CF680 30025NE NR 2 WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO27826MH1142411424 29697 704929 NR 2 ENGINE REPLACED ATL 1/13/05 FOR VANE WEAR. 2L72 4F4 FRTA1NM E13NE 20050208000482005020800048NM 2005 2 8 DL73S050032 120050114A2780 PROXIMITY SWITCH BOEING737 737232 1384475NM NR 1 SLAT OUT OF ADJUST A DALAA UNSCHED LANDING J WARNING INDICATION LDLANDING 1 SO27314DA 23086 SELECTED FLAPS AND L/E TRANSIT AMBER LIGHT ILLUMINATED. CONFIRMED BY L/E AMBER LIGHTT ON OVERHEAD PNL. FOLLOWED QRH PROCEDURES AND PLANNED FLAP 15 LANDING. ON SHORT FINAL L/E FLAP GREEN LIGHT ILLUMINATED AND SELECTED FLAPS 30. RIGGED NR 1 L/E FLAP EXTENDED PROX SWITCH, CKS GOOD. 2L72 4F RTA16WE 20050208000492005020800049NM 2005 2 8 DLM88050033 120050115A38208921460G5 WATER HEATER DOUG MD88 MD88 3023688NM FWD LAVATORY SHORTED A DALAB EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO27931DL 49718 DURING DESCENT FWD LAV SMOKE DETECTOR WENT OFF. F/A NOTED A CHEMICAL SMELL WHEN THE DOOR WAS OPENED. REPLACED OVERHEATED WATER HEATER. 2L72 4F RTA6WE 20050208000502005020800050 2005 2 8 DL76G050034 420050115A2565DPN333780101 BATTERY BOEING767 767324 1385203NM ESCAPE SLIDE DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27394DL 27394 P-61 SQUIB TEST PANEL WON`T TEST CORRECTLY. REPLACED TEST PANEL, 2 EMERGENCY BATTERIES (M961 &M962 ) & 1 CHARGER ASSY. OPS CHECKS GOOD. 2L72 4F RTA1NM 20050208000512005020800051NM 2005 2 8 DL733050035 120050115A213365657151 OUTFLOW VALVE BOEING737 737347 1384647NM AFT FUSELAGE CONTAMINATED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO272310 23596 AIRCRAFT FAILED TO PRESSURIZE. FOUND PRESSURE RELIEF VALVE STUCK OPEN. 2L72 4F RTA16WE 20050208000582005020800058NM 2005 2 8 05FDEA00204 120050130A5313A5A70291 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 CENTER CARGO LONGERON CRACKED AT STA 1538 L45L. REPAIR CARRIED OUT AT CENTER CARGO LONGERON AT STA 1538 L45L AS PER SRM 53-10-00 FIG 1 VOL I. 2L73 4F RTA22WE 20050208000592005020800059NM 2005 2 8 05FDEA00205 120050131A5730 SKIN DOUG MD11 MD11 3023602NM CENTER WING BOX CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25625FE 48444 DURING AIRPLANE PASSENGER TO FRIGHT CONVERSION: FOUND MANY SEVERE CORROSION ON UPPER SKIN OF THE CTR BOX WING LT SIDE STA 1199;1219 AND 1229 X= 100 RH SIDE STA 1199;1219 AND 1229 X=-100. REMOVE FASTENERS IN THE AFFECTED AREA, REMOVED CORROSION PER SRM 57-20-00 VOL II FIG 12, PERFORMED HFEC SHOT PEEN THE REWORKED AREA PER MD11-SRM HFEC TO INSURE NO CRACK. INSTALLED 1 FIRST O/O FASTENERS AND APPLIED SEALANT AND FUEL VAPOR BARRIER COATING. 2L73 4F RTA22WE 20050208000722005020800072NM 2005 2 8 DL733050050 120050121A49208598129E APU BOEING737 737347 1384647NM APU BAY FIRE A DALAF ACTIVATE FIRE EXT. A FLAME/FIRE TXTAXI/GRND HDL 1 SO27313WA36778 23599 060154 AFTER LANDING STARTED APU. TAXIED TO GATE, DURING ENGINE SHUTDOWN HAD APU FIRE LIGHT. ACCOMPLISHED QRH PROCEDURE. MAINTENANCE INSPECTED, FIRE BOTTLE FOUND DISCHARGED. REMOVED BATHTUB AND INSPECTED APU FOR DAMAGE. FIRE WAS LIMITED TO TAILPIPE AREA. REAR FIRE LOOP WIRING DAMAGED IN AREA OF TAILPIPE. NO OTHER DAMAGE NOTED. REPLACED APU. 2L72 4F RTA16WE 20050208000732005020800073NM 2005 2 8 DL757050051 120050121A3397 WIRE BOEING757 757232 1384965NM EMERGENCY LIGHT DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27641DL 23995 EMERGENCY LIGHT AT 23D INOP. FOUND BROKEN WIRE UNDER SEAT 23F. REPAIRED WIRE. 2L72 4F RTA2NM 20050208000742005020800074NM 2005 2 8 DLM90050052 120050121A3340 SWITCH DOUG MD90 MD9030 3023690NM LANDING LIGHT SPARKS A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 SO27916DN 53396 WING LANDING LIGHT SWITCH SHOT OUT SPARKS AND POPPED VERY LOUD AS LIGHTS WERE TURNED ON. OPS CHECKED LIGHTS AND INSPECTED BEHIND SWITCH PANEL, NO TROUBLE FOUND. 2L72 4F RTA6WE 20050208000822005020800082NM 2005 2 8 05FDEA00067 120050111A5330 SKIN BOEING727 727200 138407ENM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25235FE 21329 EXTERNAL SKIN GOUGED AT LAP SPLICE, BS 337, RT SIDE, 21 INCHES O/B OF NOSE WHEEL WELL CUTOUT. *S/D* REPAIRED SKIN DAMAGE PER SRM 53-30-3. 2L73 4F RTA3WE 20050208000932005020800093EA 2005 2 8 SWIA200514487 120050126A2760 PRESSURE SWITCH CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 NM07918SW 7645 ON SHORT FINAL RECEIVED SPOILERONS FAULT AND OUTBOARD GROUND SPOILER FAULT STATUS MESSAGES. REMOVED AND REPLACED ANCP LOW PSI SWITCH 1B. PERFORMED SECU CHECKS IAW 27-61-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050208000942005020800094NM 2005 2 8 AWXA200500167 120050206A3246314396 WHEEL BOEING737 737301 1384611NM MLG OVERHEATED A AWXAC ABORTED TAKEOFF MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 WP28325AW 23260 PHX - ABORTED TAKEOFF - FLT 227 - ON TAKEOFF AT APPROX 135 KTS. A BIRD STRIKE WAS REPORTED HITTING THE FORWARD LEFT AND RIGHT WINDSHIELDS. TAKEOFF WAS ABORTED. MX PERFORMED A BIRD STRIKE INSPECTION IAW TASKCARD I8M05030. NO DAMAGE NOTED. MX PERFORMED AN INSPECTION AND BORESCOPE OF THE LEFT AND RIGHT MAIN LANDING GEAR AXLE TUBE ASSEMBLIES IAW TASKCARD F8M32001. NO DAMAGE OR DISCOLORIZATION NOTED. MX REMOVED AND REPLACED ALL 4 BRAKE ASSEMBLIES IAW TASKCARD R4M32014. MX REMOVED AND REPLACED ALL 4 MLG WHEEL ASSEMBLIES IAW R4M32013. NR 2 TIRE ASSY S/N OFF 1998, NR 3 TIRE ASSY S/N OFF 1737, NR 4 TIRE ASSY S/N OFF 4437, NR 2 BRAKE ASSY S/N OFF 7425, NR 3 BRAKE ASSY S/N OFF 1905, NR 4 BRAKE ASSY S/N OFF 3873. 2L72 4F RTA16WE 20050208000962005020800096NM 2005 2 8 750WL0013 120050204A2750285N001132 FSEU BOEING757 757200 1384950NM NR 1 MALFUNCTIONED A PIDAO OTHER J WARNING INDICATION CRCRUISE 1 SO05750WL 23928 DURING CRUISE AT 35,000 , A/T DISC LIGHT ILLUMINATED FOLLOWED BY LOSS OF AUTO THROTTLE. RECEIVED INTERMITTENT STATUS MESSAGE, FLAP/SLAT ELEC AND WARN ELEX. DURING APPROACH RECEIVED A CONFIG WARNING GEAR NOT DOWN. UPON SELECTION OF FLAPS 1, INDICATOR MOVED MIDWAY, THEN TO 1, THEN BACK TO MIDPOINT, THEN TO 1. DURING SHORT FINAL LEADING EDGE AND TRAILING EDGE ILLUMINATED. REPLACED NR 1 FSEU PER MM 27-51-00. PERFORMED SYSTEM OPERATION TEST PER MM 27-51-00. PERFORMED OPS TEST OF ADC PER MM 34-12-00 AND CONFIG WARNING PER MM 31-51-00. ALL SYSTEMS AND INDICATIONS TEST NORMAL. 2L72 4F RTA2NM 20050208001032005020800103EA 2005 2 8 05033661 120050202A2923848847 PUMP CNDAIRCL600 CL6002B19 1900309EA HYDRAULIC SYS INOPERATIVE A VTZAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 EA27661BR 7520 GEAR DISAGREE INDICATION ON APPROACH. CREW EXECUTED GO-AROUND AND ASKED ATC FOR DELAYING VECTORS WHILE RUNNING QRH. MX FOUND HYD PUMP NR 3A INOP. REMOVED AND REPLACED PUMP. 2L72 4F RTA21EA 20050208001062005020800106WP 2005 2 8 UPS05843856 120050106A534037549301 FITTING DOUG DC8 DC873F 302199FWP CARGO BAY CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01868UP 45968 INSPECTION TYPE:C3 LOWER NR 5 T-BOLT BACKUP FITTING CORRODED BEYOND LIMITS AT C-PIT TORQUE BOX. REMOVED AND REPLACED FITTING REF SRM 53-2-0 FIG 1F, 51-1-20D. 2L74 4F RT4A25 20050208001072005020800107WP 2005 2 8 UPS05843857 120050105A7830 FITTING DOUG DC8 DC871F 302199DWP THRUST REVERSER CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01701UP 45938 INSPECTION TYPE:C1 FITTING CRACKED AT LOWER CORNER OF NR 1 OUTBOARD T/R BLOCKER DOOR POCKET. STOP DRILLED CRACK. FABBED STIFFENER AND REPAIR ANGLE AND INSTALLED IAW EO CFM-7830-5209 APPROX B. 2L74 4F RT4A25 20050208001122005020800112EA 2005 2 8 05032675 120050201A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DAMAGED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27675BR 7635 AFT SECTION OF EMERGENCY LIGHTING INOP. REPLACED POWER SUPPLY CABLE AND LIGHTING STRIP. 2L72 4F RTA21EA 20050208001132005020800113NM 2005 2 8 SWAA050319 120050204A5311654765961 FRAME BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29505SW 24182 DURING SCHEDULED C2 CHECK, FOUND AFT CARGO DOOR FWD FRAME AT THIRD STOP CRACKED. REPAIRED FRAME PER EA. 2L72 4F RTA16WE 20050208001142005020800114NM 2005 2 8 SWAA050320 120050204A53306545857 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29505SW 24182 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT AFT SERVICE DOOR UPPER HINGE, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050208001162005020800116NM 2005 2 8 SWAA050322 120050204A57536546435336 SKIN BOEING737 7373H4 1384600NM TE FLAPS DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29634SW 27937 DURING SCHEDULED RON, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RIGHT T/E AFT FLAP PER MM. 2L72 4F RTA16WE 20050208001172005020800117NM 2005 2 8 SWAA050323 120050204A53306545766 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29352SW 24888 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 520, STRINGER 12R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20050208001192005020800119NM 2005 2 8 AALA20050087 120050205A3397 CONNECTOR BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21950AN 30087 LAX - EMERGENCY LIGHT AT SEAT 7D INOPERATIVE. REPLACED END CONNECTOR AT SIDE WALL FOR EMERGENCY LIGHT AT SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20050208001242005020800124EA 2005 2 8 SWIA200514506 120050202A2120 SMOKE CNDAIRCL600 CL6002B19 1900309EA COCKPIT DETECTED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM07978SW 7953 ON TAXI IN/PARKING AT GATE TRANSFERRED BLEEDS TO APU AND SMOKE BEGAN FILLING COCKPIT AND CABIN. PURGED CABIN AND COCKPIT OF SMOKE. OPERATED BOTH PACKS FOR 20 MINUTES. COULD NOT DUPLICATE DISCREPANCY. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050208001262005020800126EA 2005 2 8 05038705 120050207A5210601R317725 ANGLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27705BR 7470 C-CHECK FINDING: PASSENGER DOOR AFT DRAG ANGLE CRACKED 2 INCHES LONG IN RADIUS JUST FWD OF PASSENGER DOOR ASSIST CABLE PULLEY MOUNT BRACKET. 2L72 4F RTA21EA 20050208001272005020800127SO 2005 2 8 SWIA200514488 120050128A2611 SMOKE DETECTOR EMB 120 EMB120ER 3260203SO LAVATORY MALFUNCTIONED A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07298SW 120328 SMOKE ALARM IN LAV GOES OFF INTERMITTENTLY. NO SMOKE OR FIRE NOTED. REPLACED SMOKE ALARM WITH SERVICEABLE UNIT. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050208001312005020800131EA 2005 2 8 VNAA0501012 120050131A2750860D10018 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS FAILED A VNAAO OTHER F FLT CONT AFFECTED CRCRUISE 1 GL05230PS1852 7904 WHILE IN CRUISE FLIGHT AT 29,000 FEET THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED. THE CREW OF FLIGHT 2286 FOLLOWED QRH PROCEDURES AND CONTINUED THE FLIGHT TO CAK, DECLARED AN EMERGENCY AND MADE AN UNEVENTFUL LANDING. PSA MAINTENANCE REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT IAW CRJ 200 AMM 27-51-05-000-801. OPERATIONAL CHECKS OF THE FLAP SYSTEM WERE GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050203001062005020300106EU 2005 2 3 AALA20050071 120050127A3350P4010049 BATTERY PACK AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW2119059 469 BOS - LEFT HAND SIDE OF FIRST CLASS EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGNECY LIGHTS AT LEFT HAND SIDE OF FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20050203001072005020300107NM 2005 2 3 AALA20050062 120050130A3350 SIGN BOEING777 777223 1385213NM EMERGENCY EXIT MISSING A AALAK NONE O OTHER ININSP/MAINT 1 SW21755AN 30263 DFW - EXTERIOR EMERGENCY EXIT SIGN AT RIGHT NR ONE DOOR MISSING. INSTALLED NEW EXTERIOR EMERGENCY EXIT SIGN OR RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20050203001192005020300119NM 2005 2 3 SWAA050285 120050201A57436959886 STRUCTURE BOEING737 7373H4 1384600NM LT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29653SW 28398 DURING SCHEDULED SERVICE CHECK, FOUND LT GEAR, LT STAB ASSY, CORRODED. REMOVED AND REPLACED LT STAB ASSY PER MM. 2L72 4F RTA16WE 20050203001202005020300120NM 2005 2 3 SWAA050286 120050201A531065353656 SHEAR TIE BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29680AA 23505 DURING SPV, FOUND 2 EACH CRACKS ON SHEAR TIES AT BS 360, ABOVE AND BELOW STRINGER 14L. REMOVED AND REPLACED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20050203001472005020300147NM 2005 2 3 UPS05243777 120050106A5414 PANEL BOEING727 727185C 138406NNM NR 1 PYLON DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 INSPECTION TYPE:C, ENGINE NR 1 PYLON PANEL 5408 IS DELAMINATED INNER SURFACE FWD END. PANEL REPAIRED IAW SRM 51-40-20. 2L73 4F A3WE 20050203001772005020300177EA 2005 2 3 SWIA200514469 120050106A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07438SW 7574 PULLEY INTERCOSTAL HAS A CRACKED OUTBOARD FLANGE FS 484.00; RBL 36.0. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-41-059 REV A. 2L72 4F RTA21EA 20050203001892005020300189EA 2005 2 3 COMA0560090 120050127A2750855D10011 BPSU CNDAIRCL600 CL6002B19 1900309EA RT TE FLAPS UNRELIABLE A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01483CA6680 2858 7689 FLIGHT 5341 FLAPS FAIL CAUTION. REPLACED THE RIGHT BPSU. 2L72 4F RTA21EA 20050203001922005020300192NM 2005 2 3 SWAA050292 120050201A53106546529 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29331SW 23695 DURING SCHEDULED 1/4D CHECK, FOUND FWD CARGO COMPARTMENT SHEAR TIE AT BS 500, BL 0, CORRODED. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050203001942005020300194NM 2005 2 3 SWAA050277 120050201A335065C33304 LIGHT BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29356SW 25251 EMERGENCY EXIT LIGHT AT FWD F/A'S SEAT, LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20050203002002005020300200NM 2005 2 3 SWAA050283 120050201A531565C25723 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29602SW 27953 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CHORD AT RIGHT BS 616, CRACKED. REPAIRED FLOORBEAM CHORD PER ER. 2L72 4F RTA16WE 20050203002022005020300202WP 2005 2 3 AALA20050060 120050126A3220 PISTON DOUG DC9 DC982 3022082WP NLG INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW217519A 49896 ORD - INFLIGHT AFTER TAKEOFF NOSE GEAR OR DOORS WOULD NOT RETRACT. NOSE LANDING GEAR INDICATION WAS DOWN FLUSH BUT VERY LOUD AIRFLOW DISRUPTION AROUND COCKPIT. RED NOSE GEAR INDICATION AND TWO GREENS ON THE MAINS. CYCLED GEAR WITH SAME INDICATIONS. GOOD DOWN AND LOCKED INDICATION. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. OUT OF SERVICE TO HANGAR FOR EVALUATION. REPLACED NOSE TURNING TUBE AND PISTON ASSEMBLY. SERVICED STRUT WITH NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050203002062005020300206NM 2005 2 3 AALA20050061 120050127A3350 WIRE BOEING767 767223 1385123NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21329AA 22329 SFO - RIGHT NUMBER TWO DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED WIRE FOR RIGHT NUMBER TWO DOOR EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050207000082005020700008NM 2005 2 7 SWAA050315 120050203A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29331SW 23695 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 518, STRINGER 12R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20050207000152005020700015NM 2005 2 7 2005UALA00090 120050123A3350 LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE ROW 15 INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29314UA 23675 AFT CABIN EEL LIGHTS INOP FROM ROWS 15 TO AFT GALLEY. REPLACED EEL CABLE AND MISSING END CAP. 2L72 4F4 FRTA16WE E2GL 20050207000162005020700016NM 2005 2 7 QXEA200500148 120050131A2730 WARNING LIGHT BOMBDRDHC8 DHC8401 1390041NM PITCH TRIM ILLUMINATED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09417QX 4086 THE FLIGHT RETURNED TO GATE AFTER THE CREW RECEIVED A PITCH TRIM CAUTION UPON PUSHBACK. MAINTENANCE INSPECTED THE SYSTEM AND CLEARED THE FAULTS BY CYCLING THE FCS ECU 1 AND 2 CIRCUIT BREAKERS. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050207000202005020700020 2005 2 7 2005UALA00091 420050121A2565 SLIDE BOEING747 747451 1384940NM PWA 4056 PW4056 NE FAILED A UALAK NONE WL INADEQUATE Q C NO TEST ININSP/MAINT 1 WP29105UA 26473 SLIDE SUFFERED DAMAGE DURING DEPLOYMENT TO INFLATABLE, ABRASIONS ON EXPOSED HOSES AND 3 HOSES FAILED HYDRO TESTING. LEAKING AT THE WELDED AREA ON TUBING. SLIDE DAMAGED DUE TO IMPROPER HANDING AFTER DEPLOYMENT. REPAIRED INFLATABLE HOLES AND REPLACED HOSES. 2L74 4F4 FRTA20WE E24NE 20050207000212005020700021EU 2005 2 7 05FDEA00200 120050129A5310 DOOR FRAME AIRBUS300 A300B4622R 3930312EU FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25716FD 358 AFT CARGO DOOR AFT FRAME UPPER SIDE AFTER REMOVAL OF UPPER DOOR SILL SECTION TO RECTIFY N00021, FOUND 1 AREA OF CORROSION ON AFT FRAME REAR FACE SURFACE SURROUNDING NUT PLATE. REMOVED CORROSION IAW A300-600 SRM 51-74-10 AND REPAIRED AFT CARGO DOOR AFT FRAME UPPER SIDE IAW A300-600 SRM 53-17-13 FIG 201A, REF EA 6-5310-85605. 2L72 4F RTA35EU 20050207000232005020700023NM 2005 2 7 2005UALA00093 120050125A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29597UA 28750 AFT PIT AT STA 1540 FRAME INBOARD FLANGE IS DENTED AT STR 25R. MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME FLANGE WITH NESTED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20050207000352005020700035NM 2005 2 7 05FDEA00211 120050201A5312 BULKHEAD BOEING727 727200 138407ENM FUSLEAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25235FE 21329 BS 740 RBL 8 WL 148 CORROSION AFT SIDE OF BULKHEAD. FOUND CORROSION OUT OF LIMITS PER SRM 53-10-1 REPLACED SUPPORT DOUBLER PER EA 7-5310-86238 AND SRM 51-30-2, 51-10-2 & 51-40-2. 2L73 4F RTA3WE 20050207000372005020700037EU 2005 2 7 05FDEA00212 120050201A5511 RIB AIRBUS300 A300B4622 3930401EU ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25716FD 358 LT HORIZONTAL STAB T/E, JUST O/B OF RIB 3, 1 EA AREA OF CORROSION ON WEB ATTACH UPPER FLANGE LOWER SURFACE. REMOVED CORROSION PER A300600 SRM 51-74-10, MATERIAL LOSS OUT OF LIMITS PER A300600 SRM 55-10-00. FABRICATED AND INSTALLED REPAIR ANGLE IAW A300600 SRM 55-11-21 FIG 224. 2L72 4F RTA35EU 20050208000122005020800012EU 2005 2 8 05FDEA00225 120050202A5230A5237008320200 FITTING AIRBUS300 A300B4622 3930401EU ZONE 800 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25716FD 358 WHILE COMPLYING WITH HIDDEN DAMAGE INSPECTION FOR S00012, FOUND CORNER FITTING (ITEM 30 FIG 2 SHEET 1 SRM 52-31-00 PG 12) CRACKED WITH PREVIOUS REPAIR, AND CRACK HAS MIGRATED 1 INCH PAST STOP DRILL. REMOVED AND REPLACED CORNER FITTING IAW A300-600 SRM 51-72-10. 2L72 4F RTA35EU 20050208000182005020800018NM 2005 2 8 05FDEA00231 120050130A3230 BRACKET DOUG MD11 MD11 3023602NM SCISSOR LINK BROKEN A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25614FE 48528 RIGHT MAIN LANDING GEAR DID NOT RETRACT ON T/O. CYCLED GEAR AND LANDED UNEVENTFULLY. FOUND RIGHT MLG SCISSOR LINK BRACKET BROKEN DURING INSPECTION. APPEARS WIRING CONDUIT MAY HAVE HUNG UP ON DOOR LATCH MECHANISM DURING RETRACTION. RIGHT MLG DOOR LATCH NOT DAMAGED. REPLACED CONDUIT GUIDE. ACCOMPLISHED A/C JACKING AND RIGHT MLG SWING AND ADJUSTMENT TEST. ALL TESTS PASSED. NO DEFECTS NOTED. A/C OK FOR CONTINUED SERVICE. 2L73 4F RTA22WE 20050208000472005020800047NM 2005 2 8 DL73G050031 120050114A5753654648482 SPAR BOEING737 737330 13844BJNM WING, MID FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27241DL 23833 DURING SHOP VISIT, THE NR 3 MID FLAP FRONT SPAR ASSEMBLY WAS FOUND WITH A CRACKED LOWER CHORD AND DENTED WEB. DAMAGE WAS DUE TO SERVICE DAMAGE. REPAIRED PER ERA 093135-14. 2L72 4F RTA16WE 20050208000542005020800054NM 2005 2 8 DLM88050039 120050117A2910240S5895031 LINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE HYD SYSTEM FAILED A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO27923DL 49705 718226 RIGHT HYDRAULIC PRESSURE WENT TO ZERO IN FLIGHT. QTY WENT TO 6, THEN 2, THEN 7. USED ALT GEAR EXTENSION. LANDED SAFELY. FOUND HYD PRESSURE LINE IN PYLON FAILED. REPLACED SAME. 2L72 4F4 FRTA6WE E9NE 20050208000552005020800055 2005 2 8 DL76L050040 420050117A3446S231T290207 SWITCH BOEING767 767332 1382001NM COCKPIT OVERHEATED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO27197DN 28454 ON APPROACH LATCHED THE EGPWS INHIBIT SWITCH, HAD ELECTRICAL ODOR IN COCKPIT. SVO FOUND INHIBIT SWITCH WARM WHEN LATCHED IN. REPLACED P3-1 PANEL. 2L72 4F RTA1NM 20050208000602005020800060NM 2005 2 8 DL767050049 120050121A2780849703 PSEU BOEING767 767232 1385132NM LE FLAPS MALFUNCTIONED A DALAA UNSCHED LANDING J WARNING INDICATION LDLANDING 1 SO27102DA 22214 ON FLAP RETRACTION GOT L/E FLAP DISAGREE. ON FINAL GOT L/E FLAP ASYM PLI WAS FLUCTUATING POS 5 DEG TO POS 12 DEG. T/S PER FIM 27-81-00. PSEU FAULTS CARD NR 10 AND SHOWS CODES 305 421 422 AND 301. REPLACED PSEU. FSEU SHOWS OUTBD SLAT RVDT MISSING AND 603 FLAP LVR RVDT MISRIG. RESET FSEU. RAN FLAPS AND SLATS NUMEROUS TIMES. OPS CK OK. NO FURTHER FAULTS. 2L72 4F RTA1NM 20050208000762005020800076NM 2005 2 8 DL76L050054 120050123A1430 BOLT BOEING767 767332 1382001NM LT MLG SHEARED A DALAK NONE O OTHER ININSP/MAINT 1 SO271200K 28457 MLG WHEEL TIE BOLT SHEARED. REPLACED WHEEL ASSY. 2L72 4F RTA1NM 20050208000792005020800079 2005 2 8 DL76L050057 420050125A34164039892904 INDICATOR BOEING767 767332 1382001NM ALTIMETER UNSERVICEABLE A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27189DN 25990 F/O ALTIMETER INOP AFTER T/O. RESET C/B, NO HELP. REPLACED F/O`S ALTIMETER PER A/C MM 34-13-01-404. ALT CHECKS OK. 2L72 4F RTA1NM 20050208000982005020800098NM 2005 2 8 AALA20050083 120050204A3350P4010049 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21691AA 25697 LAX - EMERGENCY LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED MODULE P4010051112 BY DME CORPORATION AND BATTERY PACK FOR EMERGENCY LIGHTS IN FIRST CLASS. FOUND LOOSE WIRE UNDER SEAT 5F. SECURED AND ROUTED WIRES FOR EMERGENCY LIGHTS AT SEAT 5F. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050208000992005020800099NM 2005 2 8 SWAA050318 120050204A3350D71702001 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29401WN 29813 DURING SCHEDULED MV3 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20050208001002005020800100NM 2005 2 8 SWAA050334 120050206A5330571769 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29603SW 27954 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN AT LEFT NR 1 FLIGHT DECK WINDOW UPPER OUTBOARD CORNER CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050208001022005020800102GL 2005 2 8 CHQA200500024 220050131A72612307356 CARBON SEAL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 1 ENGINE LEAKING A CHQAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL11268SK 145270 CAE311482 FLIGHT 3217 - LGA-PHL - WHILE EN ROUTE A LAV SMOKE MASTER WARNING APPEARED ON EICAS. THE APPROPRIATE QRH CHECKLIST WAS COMPLETED. THE FLIGHT ATTENDANT CHECKED THE LAV AND SAW NO SMOKE OR FIRE AND NO SMELL WAS PRESENT ANYWHERE IN THE AIRCRAFT. THE EICAS MESSAGE WENT OUT AND THE FLIGHT CONTINUED UNEVENTFULLY. THE AIRCRAFT WAS FERRIED FROM PHL TO IND WITH THE NR 1 BLEED SYSTEM OFF. MAINTENANCE FOUND THE NR 0 CARBON SEAL TO BE LEAKING. REMOVED AND REPLACED THE NR 1 ENGINE NR 0 CARBON SEAL IAW ROLLS ROYCE MM 72-25-24-400-801, 72-21-300-400-801, AND 72-21-30-410-001. PERFORMED ENGINE CHECK RUN IAW 72-00-00-700-801. NO LEAKS OR SMELL NOTED AT THIS TIME. 2L72 4T4 FRTT00011ATTE6CH 20050208001082005020800108EA 2005 2 8 050327034 120050201A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27703BR 7467 INTERCOSTAL CRACK ON OUTBOARD SIDE AT FS 484 RIGHT. 2L72 4F RTA21EA 20050208001232005020800123SO 2005 2 8 CHQA200500021 120050128A2611 SMOKE DETECTOR EMB 145 EMB145LR 3260212SO LAVATORY MALFUNCTIONED A CHQAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL11268SK 145270 FLIGHT 3083 - ROC-DCA - AFTER BOARDING THE AIRCRAFT TAXIED TO THE DEICE PAD FOR DEICING. AFTER THREE MINUTES THE BLEEDS AND PACKS WERE TURNED ON AND THE AIRCRAFT DEPARTED NORMALLY. DURING CLIMB OUT AT 10,000 FEET, A LAV SMOKE WARNING WAS ON EICAS. THE FLIGHT ATTENDANT VERIFIED THERE WAS NO SMOKE OR IN THE CABIN OR THE LAV. THE QRH WAS FOLLOWED AND THE MESSAGE EXTINGUISHED. A VERY SLIGHT SMELL OF GLYCOL WAS NOTED. THE AIRCRAFT RETURNED TO FIELD IN ROC FOR A NORMAL LANDING. MAINTENANCE PERFORMED FIM TASK 72-00-00-810-814. OPERATED BOTH PACKS WITH THE ENGINES AND APU RUNNING. COULD NOT DUPLICATE THE SMELL OR SMOKE. OPS CHECK GOOD WITH NO DEFECTS NOTED. 2L72 4T RTT00011AT 20050208001392005020800139 2005 2 8 SWAA050324 420050204A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1,R2 & L1 DOORSOUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29352SW 24888 DURING SCHEDULED C3 CHECK, FOUND R1, R2, L1 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED R1, R2, L1 SLIDES PER MM. 2L72 4F RTA16WE 20050208001422005020800142NM 2005 2 8 05FDEA00187 120050127A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25235FE 21329 BS 1030 STR 25L FRAME DENTED. REPAIRED PER SRM 51-40-3. 2L73 4F RTA3WE 20050208001442005020800144NM 2005 2 8 05FDEA00189 120050128A5320FXFAB6913713 ANGLE BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25210FE 22932 RIGHT MAIN LANDING GEAR WHEEL WELL AFT BULKHEAD UPPER OUTBOARD HORZ SUPPORT ANGLE IS CRACKED. *S/D* REMOVED & REPLACED DAMAGED ANGLE IAW SRM 51-10-1 & SRM 51-30-2. NEW ANGLE FABRICATED ON MAE TRAVELER T5/486632. 2L73 4F RTA3WE 20050208001462005020800146EA 2005 2 8 SWIA200514478 120050102A5320 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07948SW 7789 STA 280 RIGHT INBOARD BRACKET CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALL BRACKET AT STA 286 RIGHT INBOARD PER CRJ 200 SRM 51-42-20 PG 23 51-42-07 PG 13. 2L72 4F RTA21EA 20050208001472005020800147EA 2005 2 8 SWIA200514479 120050102A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07948SW 7789 STA 280, RIGHT AT RBL 9.1 BRACKET OUTBOARD OF FLOOR SUPPORT WEB CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED BRACKET AT STA 280 RT RBL 9.1 PER CRJ 2000 SRM 51-42-20 PG 23, 51-42-07 PG 13. 2L72 4F RTA21EA 20050208001492005020800149EA 2005 2 8 SWIA200514481 120050129A2752 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED APAPPROACH 1 NM07937SW 7735 ON APPROACH FLAPS FAILED AT 0 DEGREES WITH ASSOCIATED FLAPS FAIL CAUTION MESSAGE. REMOVED AND REPLACED ALL FLAP ACTUATORS AND RIGGED FLAPS IAW AMM 27-53-01, 27-53-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050208001502005020800150 2005 2 8 SWIA200514482 420050131A34258220044001 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA FLT DIRECTOR MALFUNCTIONED A SWIAO OTHER P NO WARNING INDICATION CRCRUISE 1 NM07975SW4098 4098 7951 ALT PRE-SELECT CHANGES ALTITUDE ON ITS OWN ANYTIME: +/- 1,200 FT. REMOVED AND REPLACED FCP IAW 27-11-07. OPERATIONAL CHECK GOOD. THIS AIRCRAFT IS GOOD FOR CONTINUED CATII/RVSM OPERATIONS. 2L72 4F RTA21EA 20050208001512005020800151SO 2005 2 8 SWIA200514483 120050130A5210 MECHANISM EMB 120 EMB120ER 3260203SO PAX DOOR DIRTY A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07215SW 120281 F/A REPORTS MCD IS DIFFICULT TO OPEN AND CLOSE WITH RED HANDLE. LUBRICATED DOOR IAW MM 12-21-15. TURNED HYDRAULIC ON, HELD THE PUSH BUTTON FOR DOOR ASSIST UNTIL THE DOOR MADE CONTACT WITH MICROSWITCH. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050208001522005020800152EA 2005 2 8 SWIA200514484 120050131A2710AL00102 ACTUATOR CNDAIRCL600 CL6002C10 1390015EA AILERON ROLL MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07732SK 10194 AILERON TRIM INDICATION WOULD MOVE BOTH LWD/ RWD TRIM 0 DEGREES TO 15 DEGREES ON ITS OWN (INDICATION ONLY). REMOVED AND REPLACED AILERON ACTUATOR IAW CRJ 700 MM 27-12-01. PERFORMED OPERATIONAL CHECK IAW CRJ 700 MM 27-11-00. 2L72 4F RTA21EA 20050208001572005020800157NM 2005 2 8 05FDEA00232 120050203A5753ARC4125501 STOP FITTING DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 LEFT HAND WING, OUTBOARD FLAP STOP FITTING FOUND CRACKED. REMOVED AND REPLACED PER DRAWING ARC4102 AND SRM 51-33-01 VOLUME II. 2L73 4F RTA22WE 20050208001622005020800162NM 2005 2 8 CALA0500043 120050206A335020131A BATTERY PACK BOEING737 737524 1384721NM EMERGENCY LIGHT INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2711656 28917 THE OVERHEAD EMERGENCY EXIT LIGHT AT OVERWING HATCHES FAILED TO REMAIN ILLUMINATED WHEN ACTIVATED DURING TEST. THE BATTERY PACK FOR ZONE UNDER LT OVERWING EXIT WAS REMOVED AND REPLACED IAW SRM 33-51-51. 2L72 4F RTA16WE 20050208001702005020800170NE 2005 2 8 DL73S050060 220050126A7200 ENGINE BOEING737 737232 1384475NM PWA JT8 JT8D15A 52051NE NR 2 MALFUNCTIONED A DALAE ENGINE SHUTDOWN J WARNING INDICATION APAPPROACH 1 SO27308DL53254 23080 709131 AFTER TAKEOFF WHEN THROTTLES RETARDED NR 2 ENGINE REMAINED AT 1.6 EPR. REPLACED FUEL CONTROL. 2L72 4F4 FRTA16WE E2EA 20050208001732005020800173NM 2005 2 8 DL76L050063 120050127A2612M10427 LOGIC CARD BOEING767 767332 1382001NM FIRE WARNING SYSFAILED A DALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO27173DN 24800 FWD CARGO FIRE WARNING LIGHT AND FIRE BELL ACTIVATED IN FLT. REPLACED M10427 CARD. 2L72 4F RTA1NM 20050208001752005020800175 2005 2 8 390WL0001 420050207A2210 SELECTOR BOEING737 7373G7 1384595NM AUTOFLIGHT SYS UNKNOWN A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05390WL 23219 AUTO FLIGHT MODE CONTROL PANEL VERTICAL SPEED SELECTOR INOP. PLACED ON MEL 22-14-(1). NO FAILURES OR IN FLIGHT FAULTS NOTED. PASSED AUTO PILOT TESTS FOR DFCS GROUP 11.56. NO FAULTS EXIST CURRENT OR INFLIGHT. CLEARS MEL 11-14-1. 2L72 4F RTA16WE 20050208001772005020800177NM 2005 2 8 DL777050065 120050127A25301105011 COFFEEMAKER BOEING777 777232 1385232NM MID GALLEY SHORTED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27861DA 29952 GALLEY 431 COFFEEMAKER 410 SHOCKED F/A. REPLACED SAME. 2L72 4F RTT00001SE 20050208001782005020800178NM 2005 2 8 QXEA200500145 120050128A2611473054 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM CARGO BAY FAILED A QXEAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 NM09361PH1611914906 516 YVR - FLIGHT 2210 - THE FLIGHT RETURNED TO THE GATE WHEN DURING THE TAXI OUT THE CREW RECEIVED A SMOKE AND MASTER WARNING LIGHT. MAINTENANCE INSPECTED THE AIRCRAFT AND MEL'D THE NR 2 SMOKE DETECTOR. *S/D* 02/02/05 - THE NUMBER 2 SMOKE DETECTOR WAS REPLACED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050208001842005020800184EU 2005 2 8 05FDEA00217 120050201A5320A53986743205 PLATE AIRBUS310 A310203 3930313EU ZONE 100 BROKEN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25425FE 264 PLATE AND SEC-L BENT AND BROKEN BETWEEN FR86 AND FR87. REMOVED PLATE AND FABRICATED NEW SEC-L. INSTALLED NEW SEC-L AND PLATE IN A/C. 2L72 4F RTA35EU 20050208001852005020800185NM 2005 2 8 DL76L050066 120050128A21216067071 FAN BOEING767 767332 1382001NM FWD CARGO FAILED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 SO27177DN 25122 AFTER LANDING ENCOUNTERED VERY STRONG SMELL OF ELECTRICAL BURNING NO VISIBLE SMOKE. REPLACED A/C GROUND BOOST FAN. 2L72 4F RTA1NM 20050208001872005020800187WP 2005 2 8 CALA0500036 120050201A52305910141105 SKIN DOUG DC9 DC982 3022082WP CARGO DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2735836 49441 INSPECTION FOUND A 1 INCH CRACK BELOW LOWER FORWARD LATCH OF MID CARGO DOOR SKIN. THE DOOR SKIN WAS REPAIRED IAW SRM 52-05, FIGURE 26A. 2L72 4F A6WE 20050208001892005020800189NM 2005 2 8 DL76S050068 120050128A2120 SMOKE BOEING767 767332 1382001NM CABIN DETECTED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO27136DL 23146 VISIBLE HAZE / FUMES IN AFT CABIN WITH ENGINE ANTI-ICE ON. RAN ENGINE AND APU WITH PACKS ON, RAN CARGO HEAT, RAN GALLEY OVENS AND ENTERTAINMENT SYSTEM. RAN POTABLE WATER COMPRESSOR, NO SIGNS OF FUMES OR HAZE. 2L72 4F RTA1NM 20050208001902005020800190 2005 2 8 DL76L050069 420050130A2397 WIRE BOEING767 767332 1382001NM ENTERTAIN SYS CHAFED A DALAO OTHER M OVER TEMP CRCRUISE 1 SO27189DN 25990 F/A REPORT SEAT 1A ENTERTAINMENT CONTROL WIRE SHORTED OUT. SHOWS SIGNS OF BURNS ON ELECTRICAL CHORD. REPLACED SAME. 2L72 4F RTA1NM 20050208001912005020800191NM 2005 2 8 CALA0500038 120050202A335020121 CHARGER BOEING737 737524 1384721NM EMERGENCY LIGHT INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2711641 28902 THE EMERGENCY LIGHTS ON SEAT ROWS 5-9 DID NOT ILLUMINATE DURING TEST. THE EMERGENCY EXIT LIGHT BATTERY CHARGER AT RT OVERWING EXIT WAS REMOVED AND REPLACED IAW MM 33-51-51. 2L72 4F RTA16WE 20050209000012005020900001WP 2005 2 9 05FDEA00250 120050205A5753ARC2747 SKIN DOUG DC10 DC1030F 3023504WP ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25304FE 46629 LEFT WING INBOARD FLAP, LOWER SKIN AT TRACK LOWER FILLET FAIRING TRAILING EDGE AREA, HAS SURFACE CORROSION, XIFH 126.650-XIFH 120.908. REMOVED FAIRING AND WEDGE, FABRICATED AND INSTALLED REPAIR IAW FEDEX EA8-5710-83969, WINGS - LEFT HAND INBOARD FLAP, LOWER SKIN REPLACEMENT- REPAIR AND DC10 SRM 51-35-01 VOL 1, 51-33-01 VOL II AND 51-35-01 VOL II. 2L73 4F RTA22WE 20050209000022005020900002NM 2005 2 9 05FDEA00259 120050206A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 BARREL NUT BORE NR 25L CORROSION REMOVAL FOUND EXCEEDED LIMITS. CORROSION REMOVED AND REPAIRED PER FEDEX EA# 1-5510-81726. 2L73 4F RTA22WE 20050209000032005020900003NM 2005 2 9 05FDEA00257 120050206A5753 STOP FITTING DOUG MD11 MD11 3023602NM TE FLAPS CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25620FE 48791 RIGHT HAND WING, OUTBOARD FLAP STOP FITTING FOUND CRACKED. STOP FITTING REMOVED AND REPLACED PER DRAWING 4125 AND SRM 51-33-01 VOLUME II. 2L73 4F RTA22WE 20050209000052005020900005WP 2005 2 9 05FDEA00251 120050205A2540 SEAL DOUG DC10 DC1030F 3023504WP ZONE 200 LEAKING A FDEAK NONE O OTHER ININSP/MAINT 1 SO25304FE 46629 LAVATORY, WHEN A FLASHLIGHT IS PLACED IN TRASH CAN THE INNER AND OUTER TRASH RECEPTACLE DOORS AND TRASH CAN LEAKS LIGHT. SEALED LAVATORY TRASH RECEPTACLE IAW FEDEX EA 8-2540-83964, EQUIPMENT/FURNISHINGS - LAVATORY WASTE COMPARTMENT SEALS - REPAIR. 2L73 4F RTA22WE 20050209000102005020900010 2005 2 9 05FDEA00206 420050131A34614059050912 FMC DOUG MD11 MD11 3023602NM NR 1 FAILED A FDEAA UNSCHED LANDING GJ MULTIPLE FAILURE WARNING INDICATION CLCLIMB 1 SO25599FE 48598 CLIMBING THROUGH FL380 EXPERIENCED POWER INTERUPTION WITH NO APPARENT CAUSE. LOST BOTH A/P'S AND ATS WITH MAP FAIL ALERT ON BOTH SIDES AND IRS/NAV X'D OUT ON CAPT'S PFD. CAPT'S MCDU DISPLAY REVERTED TO ACARS - APPLICATION MENU. F/O SELECTED STBY OPERATION. INITIALLY F/O MCDU WOULD NOT TUNE A VOR FREQUENCY. LATER IN DESCENT F/O NAV/RAD TUNED OK. AP1 AND AP2 RETURNED TO NORMAL BUT ATS REMAINED INOP IN 1 AND 2 POSITIONS. INTERROGATED DEU'S 1, 2, & 3. FAULT HISTORY SHOWED FMC 1 FAILURE. REMOVED AND REPLACED FMC 1. AUTOTHROTTLES, FCC'S ALL OPS CHECK NORM PER M/M. RETURNED TO SERVICE. 2L73 4F RTA22WE 20050209000122005020900012EU 2005 2 9 05FDEA00162 120050125A7830 WARNING LIGHT AIRBUS300 A300F4605R 3930327EU THRUST REVERSER ILLUMINATED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25657FE 748 ON THROTTLE ADVANCEMENT FOR T/O RECEIVED ENG 1 REVERSER PRESSURIZED. REJECT NORMAL. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01- CATEGORY: C EXPIRATION: 04FEB05 MEL 78-30-01-A: ENGINE (IDENTIFY 1 OR 2) 1 THRUST REVERSER INOP. THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POSITION. REPLACED DIRECTIONAL PILOT VALVE (DPV) AS PRECAUTIONARY PER A300 M/M 78-31-06-2 PARA 3A. REQUIRES TEST (SYR). PERFORMED A FUNCTIONAL TEST OF THE DPV PER THE MM 78-31-06-2 PG 208 STEP 7(1). REACTIVATED NUMBER 1 ENGINE REVERSER AND FUNCTIONAL TEST PER MM 78-31-00 (EWR). 2L72 4F RTA35EU 20050209000142005020900014EU 2005 2 9 05FDEA00207 120050201A5510 ATTACH FITTING AIRBUS310 A310203 3930313EU ZONE 300 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25405FE 237 RIGHT HORIZONTAL STABILIZER UPPER SPAR AT RIB 5 HAS DAMAGED HOLE THROUGH SPAR CAP AND ELEVATOR ATTACH FITTING. STOP-DRILLED HOLE TO 0.4350. FABRICATED ONE COUNTERSINK TYPE -A- BUSHING AND ONE SHOULDER TYPE -C- BUSHING AND SHRUNK FIT BUSHINGS INTO SPAR AND ELEVATOR ATTACH FITTING, RESPECTIVELY. OPENED BUSHING HOLE TO 0.250 NOMINAL SIZE AND INSTALLED BLUE PRINT FASTENER. ALL WORK PERFORMED IAW FEDEX EA 6-5510-85484 AND AIRBUS RAS/CASA/3942/2005 AND DOCUMENTED ON NRC N00530. 2L72 4F RTA35EU 20050209000182005020900018NM 2005 2 9 05FDEA00171 120050125A5347S4929147 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 SEAT TRACK AT CABIN STA 791 LBL 41.5 HAVE BOLTS INSTALLED WRONG. SEAT TRACK AT CABIN STA 791 LBL 41.5 REMOVED AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-31-01 VOL II. REPAIR SEAT TRACK & SPLICE, FABRICATED & INSTALLED AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20050209000202005020900020EA 2005 2 9 SWIA200514504 120050202A2760 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 NM07442SW 7609 RECEIVED A FLIGHT SPOILER FAULT MESSAGE UPON CLIMBOUT. REMOVED AND REPLACED RIGHT FLIGHT SPOILER INBOARD PCU IAW CRJ MM 27-62-01 AND NR 2 SECU IAW CRJ MM 27-61-05, OPERATIONAL CHECK GOOD. P/N 27000-7, S/N OFF 0392, MAL-5175, P/N OFF 49-164-06, S/N OFF 01534. 2L72 4F RTA21EA 20050209000222005020900022NM 2005 2 9 P5CA0501310 120050129A53478121688 SEAT TRACK BOEING747 747283B 1384867NM FUSELAGE BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 EA15921FT 21575 ON PREFLIGHT FOUND BOTH SEAT TRACKS BROKEN ON THE F/O'S SEAT (AFT SEAT TRACK). REMOVED & REPLACED BOTH LT & RT AFT SEAT TRACKS PER AMM 25-11-00. 2L74 4F A20WE 20050209000232005020900023EA 2005 2 9 050327031 120050201A5230 PLATE CNDAIRCL600 CL6002B19 1900309EA CARGO BAY CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27703BR 7467 CARGO LANDING PLATE CRACKED AT RIVETS ATTACHING IT TO INTERCOSTALS. 2L72 4F RTA21EA 20050209000362005020900036EA 2005 2 9 05033651 120050202A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A VTZAO OTHER J WARNING INDICATION APAPPROACH 1 EA277426 7426 EVENT SUMMARY STATED FLAP FAIL AT 0 DEGREES. INSPECTED FLAP FAIL NO BINDING OR STOPPAGE REF 27-54-00. PERFORMED TORQUE CHECK OF FLAP SYSTEM. 2L72 4F RTA21EA 20050209000382005020900038EA 2005 2 9 05033671 120050203A2150 A/C PACK CNDAIRCL600 CL6002B19 1900309EA RIGHT ODOR A VTZAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 EA27671BR 7572 ON 02/02 SMOKE TOILET CAUTION MSG ON APPROACH AT 1500 FT WITH SMOKE DETECTOR GOING OFF. AT 1500 FT ON APPROACH WITH OILY SMELL COMING FROM RT PACK. DEFERRED IAW MEL 21-51-01-01. 2L72 4F RTA21EA 20050209000402005020900040NM 2005 2 9 05FDEA00220 120050202A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 MAIN DECK, SEAT TRACK CROWN AREA AT APPROXIMATE STA Y= 1092 TO Y= 1095, X= -47.5 FOUND WORN. SEAT TRACK REMOVED FROM EXISTING SPLICE AT STA Y= 1129 AND CUT AT Y= 1159, X= -47.5 PER SRM 53-70-00 VOLUME I, FIGURE 1. NEW SEAT TRACK AND REPAIR PARTS FABRICATED AND INSTALLED PER SRM 53-70-00 VOLUME I, FIGURE 1. 2L73 4F RTA22WE 20050209000422005020900042NM 2005 2 9 05FDEA00222 120050202A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 MAIN DECK - SEAT TRACK CROWN AREA AT APPROXIMATE STA Y= 1304, X= - 75.5 FOUND WORN. CUT AND REMOVED PER SRM 53-70-00 VOLUME I, FIGURE 1. NEW SEAT TRACK AND REPAIR PARTS FABRICATED AND INSTALLED PER SRM 53-70-00 VOLUME I, FIGURE 1. 2L73 4F RTA22WE 20050209000442005020900044NM 2005 2 9 SWAA050301 120050202A335007912 LIGHT BOEING737 7377H4 1384404NM ROW 3 ABC LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29408WN 27895 EEPLS STRIP AT ROW 3 ABC, LOOSE. REMOVED AND REPLACED EEPLS STRIP PER MM. 2L72 4F RTA16WE 20050209000512005020900051SO 2005 2 9 CHQA200500020 120050127A335066903 LIGHT EMB 135 EMB135KL 3260302SO SEAT 1&2A INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11378SK 145593 EMERGENCY FLOOR EGRESS LIGHTING AT SEAT 1 AND 2A IS INOPERATIVE. REPLACED FLOOR PROXIMITY STRIP LIGHT. OPS CHECK GOOD IAW EMB 140 AMM 33-50-00. 2L72 4F RTT00011AT 20050209000522005020900052NM 2005 2 9 UPS05543860 120050206A5410 PYLON BOEING757 75724APF 1384969NM NR 2 ENGINE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01422UP 25324 NR 2 ENGINE PYLON CRACKED. RT ENGINE FIRESHIELD ABOVE AND AFT OF REAR ENG MOUNT IS CRACKED. REMOVED DAMAGED FIRESHIELD AND DRILLED NEW SHIELD AND INSTALLED LOCK FASTENERS IN UPPER LEG AS PER DWG 311N3570. FINISHED INSTALLATION OF RT ENGINE FIRE SHIELD IAW DWG 311N2570 AND B757 SRM 51-10-00 2L72 4F RTA2NM 20050209000532005020900053NM 2005 2 9 UPS05543861 120050205A3350 LAMP BOEING757 75724APF 1384969NM EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01456UP 25477 EMERGENCY EXIT UNARMED LIGHT INOP. RELAMPED, OPS NORMAL. 2L72 4F RTA2NM 20050209000542005020900054WP 2005 2 9 UPS05843851 120050117A575336523132 STOP FITTING DOUG DC8 DC873F 302199FWP RT WING TE FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01868UP 45968 INSPECTION TYPE: C3, RIGHT STA 98 FLAP UPSTOP FITTING CRACKED. GAINED ACCESS TO REPAIR SITE. REMOVED & REPLACED FITTING REF SRM 51-3-0, 51-1-8, 51-1-21, 51-1-15. RESTORED REPAIR AREA. 2L74 4F RT4A25 20050209000552005020900055WP 2005 2 9 UPS05843852 120050105A53403755842U1 FITTING DOUG DC8 DC873F 302199FWP CARGO BAY CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01868UP 45968 INSPECTION TYPE:C3 TORQUE BOX FITTING CORRODED BEYOND LIMITS AT STA 1220 L30L. REMOVED AND REPLACED FITTING REF SRM 51-1-8, 51-1-21, 51-1-20D. 2L74 4F RT4A25 20050209000562005020900056SO 2005 2 9 CHQA200500022 120050129A3242 CONNECTOR EMB 135 EMB135LR 3260305SO BRAKE SYSTEM LOOSE A CHQAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL11839RP 145724 FLIGHT 6255 - FLL-RIC - SHORTLY AFTER BEGINNING TAXI OUT, THE BRAKE PEDAL WAS DEPRESSED WITH NO BRAKE ACTUATION. THE BRAKE PEDAL WAS FULLY DEPRESSED AND APPROXIMATELY 5 SECONDS LATER, THE BRAKES ABRUPTLY FULLY APPLIED. THE AIRCRAFT WAS BROUGHT TO A COMPLETE STOP AND WAS TUGGED BACK TO THE GATE. THE EMERGENCY BRAKE FUNCTIONED PROPERLY AND A BRAKE DEGRADED MESSAGE APPEARED ON EICAS. MAINTENANCE FOUND A LOOSE CONNECTOR ON THE BRAKE CONTROL UNIT. RESECURED ALL CONNECTIONS AND TAXI CHECKED THE AIRCRAFT. TAXI CHECK AND OPS CHECK GOOD. 2L72 4F RTT00011AT 20050209000582005020900058SO 2005 2 9 CHQA200500023 120050130A335078241 STATIC INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT UNSERVICEABLE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11264SK 145221 MAIN DOOR EMERGENCY EXIT SIGN IS INOP. FOUND THE STATIC INVERTER FAULTY FOR THE MAIN DOOR EMERGENCY EXIT SIGN. REMOVED AND REPLACED THE STATIC INVERTER IAW EMB 145 AMM 33-50-11. EMERGENCY LIGHTS OPS CHECK GOOD. 2L72 4T RTT00011AT 20050209000592005020900059SO 2005 2 9 CHQA200500019 120050127A3350 LIGHT EMB 135 EMB135LR 3260305SO CABIN OUT OF POSITION A CHQAK NONE O OTHER ININSP/MAINT 1 GL11839RP 145724 EMERGENCY FLOOR LIGHTING STRIP WAS FOUND TO BE ON THE WRONG POSITION. REPOSITIONED EMERGENCY FLOOR LIGHTING STRIPS AS PER EMB 135 MM 33-50-12. OPS CHECK GOOD. 2L72 4F RTT00011AT 20050209000612005020900061NM 2005 2 9 05FDEA00190 120050128A5310 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25235FE 21329 BS 500, RBL 35, WL 161 DENT ON FRAME. REPAIRED PER SRM 53-10-1, 51-40-3 2L73 4F RTA3WE 20050209000632005020900063WP 2005 2 9 AALA20050082 120050206A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21481AA 49656 RIGHT AND LEFT HAND EMERGENCY ESCAPE PATH HATCH AND FORWARD EXIT DOOR LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR RIGHT AND LEFT HAND EMERGENCY ESCAPE PATH HATCH AND FORWARD EXIT DOOR LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050209000652005020900065 2005 2 9 SWAA050316 420050204A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29371SW 26598 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050209000672005020900067 2005 2 9 SWIA200514492 420050201A34183995100208 COMPUTER CNDAIRCL600 CL6002B19 1900309EA STALL WARNING MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CRCRUISE 1 NM07710BR 7852 STALL FAIL MESSAGE ON INFLIGHT. REMOVED AND REPLACED STALL WARNING COMPUTER IAW MM 27-35-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050209000682005020900068SO 2005 2 9 SWIA200514493 120050128A3350 FIXTURE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07224SW 120294 LEFT OVERWING EMERGENCY EXIT LOWER RIGHT FIXTURE BROKEN. REMOVED AND REPLACED EMERGENCY EXIT LOWER LIGHT FIXTURE IAW MM 33-51-00, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050209000732005020900073NM 2005 2 9 SWAA050329 120050206A5754SWKRS073405 BEARING BOEING737 7373H4 1384600NM NR 6 SLAT WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 MOVING FLAPS FROM 5 TO 10 DEGREES BOTH PILOTS HEARD A LOUD POP AND A THUMP, ALL INDICATIONS NORMAL. REMOVED AND REPLACED NR 6 L/E SLAT BEARINGS PER SERVICE LETTER AND MM. 2L72 4F RTA16WE 20050209000752005020900075WP 2005 2 9 AALA20050078 120050201A33500201720003 SOCKET DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21251AA 49270 LAX - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 7D FORWARD INOPERATIVE. REPLACED SOCKET FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 7D FORWARD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050209000802005020900080EA 2005 2 9 COMA0570013 120050201A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA FUSELAGE DAMAGED A COMAK NONE O OTHER ININSP/MAINT 1 SO01374CA5175 10090 FS 280 LT AND RT BULKHEADS ON THE FWD SIDES HAVE APPROXIMATELY 25 HOLES ELONGATED. REPAIRED DISCREPANT FASTENER HOLES IAW BRAS EO 610R-53-5930. 2L72 4F RTA21EA 20050209000842005020900084WP 2005 2 9 CALA0500035 120050131A523059101419 PAN DOUG DC9 DC982 3022082WP CARGO DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2735836 49441 INSPECTION FOUND A .75 INCH CRACK AT CORNER OF LOWER FORWARD INNER PAN OF FORWARD CARGO DOOR. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 26A. 2L72 4F A6WE 20050209000902005020900090NM 2005 2 9 SWAA050215 120050126A53106547979 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29602SW 27953 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB FROM BS 727B TO BS 727D, RBL 70, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB PER SRM. 2L72 4F RTA16WE 20050209000922005020900092EA 2005 2 9 COMA0560088 120050127A335064641 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BROKEN A COMAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01783CA 7315 FLIGHT 4936 FLOOR EMERGENCY LIGHT AT ROW 1 IS INOP. REPLACED BROKEN POWER CABLE ASSY. 2L72 4F RTA21EA 20050209000932005020900093NE 2005 2 9 P5CAO501312 220050201A7200CF650E2 ENGINE BOEING747 747230B 1384889NM GE CF6 CF650E2 30018NE NR 3 STALLED A P5CAE ENGINE SHUTDOWN MRJOVER TEMP PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 EA15508MC46260 21644 530349 DURING CRUISE AT FL 310, NR 3 ENGINE COMPRESSOR STALLED, EGT WENT TO 500 DEGREES, N1 50 PERCENT, N2 40 PERCENT. PERFORMED RESTART THE ENGINE WOULD NOT START PAST 30 PERCENT N1, 40 PERCENT N2, WITH EGT AT 625 DEGREES & F/F AT 400 PPH. THROTTLE MOVEMENT HAD NO EFFECT. ENGINE SHUT DOWN. REMOVED AND REPLACED NR 3 ENGINE PER MM 71-00-02. PERFORMED ENGINE RUN PER 71-00-00. ALL PARAMETERS & INDICATION NORMAL. 2L74 4F4 F A20WE E23EA 20050209000942005020900094NM 2005 2 9 AT0500007 120050206A3520 OXYGEN MASK BOEING737 73776N 13844CHNM CABIN DEPLOYED A ZZDAO OTHER O OTHER CLCLIMB 1 SO15176AT 32654 SEAT 1 ABC AND 28 ABC O2 MASKS DROPPED ON CLIMBOUT. PRSSURIZATION REMAINS NORMAL, O2 GENERATORS DID NOT FIRE. BOTH SEAT ROWS ARE BLOCKED AND NOT USABLE. PERFORMED A MANUAL DROP OF ALL PAX O2 MASKS AND OPS CHECKED NORMAL. T/S PSU WIRING TO PSU SWITCH MODULES AND ALL CHECKED GOOD. ITEM REMAINS ON MEL. 2L72 4F RTA16WE 20050209000962005020900096EA 2005 2 9 050387054 120050207A5320 SILL CNDAIRCL600 CL6002B19 1900309EA CARGO BAY CORRODED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27705BR 7470 CARGO BAY FLOOR SILL AT FS 562.72 - 589 CORRODED. 2L72 4F RTA21EA 20050209000972005020900097NM 2005 2 9 AALA20050025 120050113A3397 CONNECTOR DOUG MD80 MD83 3023681NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21951TW 53470 SFO - FORWARD SEAT MOUNTED EMERGENCY LIGHT AT SEAT 3E INOPERATIVE. REPLACED FORWARD CONNECTOR FOR FORWARD SEAT MOUNTED EMERGENCY LIGHT AT SEAT 3E. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RT 20050209000992005020900099EA 2005 2 9 SWIA200514471 120050106A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA INTERCOSTAL CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07438SW 7574 INTERCOSTAL CLIP IS CRACKED FS 625.00, STR14L. ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIP IAW CRJ SRM 51-04-11, 51-42-00 AND 51-25-16. 2L72 4F RTA21EA 20050209001012005020900101WP 2005 2 9 UPS05843854 120050106A531337588931 LONGERON DOUG DC8 DC873F 302199FWP CARGO BAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01868UP 45968 INSPECTION TYPE: C3, LONGERON 35L CRACKED STA 1260-1280. REMOVED 2 CLIPS & 1 INTERCOSTAL AT STA 1270. REMOVED SPLICE FITTING AT STA 1350. REMOVED SPLICE FITTING AT STA 1270. REMOVED AND REPLACED LONGERON SECTION FROM 1270-1350. REINSTALLED ALL FOM PARTS. ALL REF SRM 51-1-20D, 51-1-21, 51-20-00. 2L74 4F RT4A25 20050209001032005020900103NM 2005 2 9 SWAA050330 120050206A53306545766 SKIN BOEING737 7373K2 13844BANM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29340LV 23738 DURING SCHEDULED 1/2D CHECK, FOUND FUELAGE SKIN AT BS 517, STRINGER 12R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20050209001052005020900105CE 2005 2 9 DJFA2005055 120050203A32425010614 BRAKE ASSY BEECH MU300 400A 1155402CE LT MLG WORN E DJFAO OTHER O OTHER LDLANDING 1 EA23709TA696 RK180 CREW REPORTED, AFTER LANDING THE BRAKES FAILED AFTER 50 KTS. EMERGENCY BRAKING SYSTEM WAS USED TO STOP THE AIRCRAFT. MAINTENANCE FOUND THE LEFT AND RIGHT BRAKE ASSEMBLIES TO BE WORN. THE LEFT AND RIGHT BRAKE ASSEMBLIES WERE REPLACED. MANUAL AND POWER BRAKE BLEEDING WAS PERFORMED FOR BOTH LEFT AND RIGHT BRAKE ASSEMBLIES. THE EMERGENCY BRAKE HYDRAULIC TANK AND NITROGEN BOTTLE WERE SERVICED. A SATISFACTORY OPERATIONAL TAXI TEST OF THE BRAKE AND ANTI-SKID SYSTEM WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4F RTA16SW 20050209001062005020900106 2005 2 9 MASA200500036 420050115A2340526011 CONTROL UNIT DHAV DHC8 DHC8202 2809007NM AUDIO SYSTEM FAILED A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW07989HA3089 427 THE CREW CALLED IN WITH THE PTT SWITCHES STICKING WHEN SELECTED ON TRANSMITT MODE AND A FAINT BURNING SMELL. CONTACT MAINTENANCE WAS CALLED AND RERACKED THE REMOTE ELECTRONICS UNIT AND THE CAPTAINS SIDE STARTED WORKING, SO THE AIRCRAFT WAS FERRIED TO PHX FOR FURTHER REPAIRS. MAINTENANCE REPLACED THE AUDIO REMOTE CONTROL UNIT. 2H72 4T RTA13NM 20050209001082005020900108WP 2005 2 9 MWEA050018 120050125A5347SRO9530111U15 SEAT TRACK DOUG DC9 DC981 3022081WP FIRST OFFICER WORN A MWEAK NONE O OTHER ININSP/MAINT 1 GL31805ME 48031 THE FIRST OFFICER'S OUTBOARD AFT SEAT TRACK IS WORN AT THE LOCK PIN HOLES. REMOVED AND REPLACED TRACK ASSEMBLY. 2L72 4F A6WE 20050209001102005020900110WP 2005 2 9 MWEA050019 120050128A71105930645509 NOSE COWL DOUG DC9 DC981 3022081WP RT ENGINE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31805ME 48031 RIGHT ENGINE COWL INTERNAL HAS CORROSION AT FORWARD CAP ANGLE ATTACHMENT TO INNER BARREL. REMOVED AND REPLACED NOSE COWL. 2L72 4F A6WE 20050209001112005020900111EA 2005 2 9 MASA200500001 120050101A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSBURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0775996 7375 CABIN CEILING EMERGENCY EXIT LIGHT INOP. MAINTENANCE PLACED THE CEILING LIGHT ON MEL. MAINTENANCE RELAMPED, OPS CHECKED GOOD. 2L72 4F RTA21EA 20050209001122005020900112EA 2005 2 9 MASA200500002 120050101A33501317 BULB CNDAIRCL600 CL6002D24 1390016EA EMERGENCY LIGHTSBURNED OUT A MASAK NONE O OTHER ININSP/MAINT 1 SW07908FJ 15008 THE CREW REPORTED A CEILING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE RELAMPED, OPS CHECKED GOOD. 2L72 4F RTA21EA 20050209001152005020900115GL 2005 2 9 DXTA200500562 220050126A732023061826 FUEL FILTER CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL LT ENGINE BYPASSING E DXTAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 GL07926QS 7500026 CAE330104 ON TAKEOFF ROLL, FUEL FILTER BYPASS L CAS MESSAGE DISPLAYED. REMOVED & REPLACED LT ENGINE FUEL FILTER, RESET BYPASS INDICATOR. PERFORMED ENGINE RUN FOR LEAK CHECK AND HIGH POWER FOR ANY CAS MESSAGE. LEAK CHECK GOOD, NO BYPASS MESSAGE. OPERATIONAL CHECK SATISFACTORY IAW NJA CESSNA CITATION 750 PILOT OPERATIONAL CHECKLIST. 2L72 4J4 FRTT00007WITE6CH 20050209001162005020900116SO 2005 2 9 MASA200500052 120050122A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSBURNED OUT A MASAK NONE O OTHER ININSP/MAINT 1 SW07825MJ 145179 AN AFT EMERGENCY CEILING LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LAMP, OPS CHECK GOOD. 2L72 4T RTT00011AT 20050209001172005020900117CE 2005 2 9 DXTA200500561 120050126A326066187046 CIRCUIT BOARD CESSNA560 560XL 2076702CE MLG FAILED E DXTAO OTHER J WARNING INDICATION APAPPROACH 1 GL07650QS3836 5605150 NO GEAR INDICATION LIGHTS WHEN LANDING GEAR EXTENDED. GEAR CIRCUIT BREAKER POPPED. DURING CHECKLIST, WHEN C/B WAS RESET, MOMENTARILY GOT 3 GREEN LIGHTS, THEN C/B POPPED AGAIN. GEAR WAS BLOWN DOWN PER CHECKLIST. TROULBLESHOT SYSTEM, CHECKED POWER WIRES 1PC044-1- PC043, 1PC044-BP029, & GP1009-BPC029 FOR SHORTS TO GROUND WITH A MEGOMETER, ALL WIRES CHECKED GOOD. ISOLATED PROBLEM TO THE GEAR LOGIC PCBNZ004. REPLACED IT WITH A NEW UNIT. OPS CHECK GOOD IAW CE560XL WDM 32-60-01, 91-20-04 & MM 32-30-00. 2L72 4F RTA22CE 20050209001182005020900118CE 2005 2 9 DXTA200500560 120050125A5280 LATCH RAYTHNDH125 HAWKER800XP 7150012CE MLG DOOR BROKEN E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07873QS 258573 AFTER RETRACTION RT MAIN GEAR UNSAFE LIGHT REMAINED ILLUMINATED (RED LIGHT). RETRACTED GEAR AT 30 TIMES AT DIFFERENT PRESSURES NO DEFECTS NOTED. WIGGLED WIRES AT TERMINAL BLOCK IN WING ROOT WITH GEAR UP AND LOCKED. NO DEFECTS NOTED. ALL LIGHTS OPERATING NORMAL. INSPECTED RT LANDING GEAR, NOTICED RT INBOARD DOOR LATCH BROKEN OFF. REMOVED AND REPLACED LATCH. SWUNG GEAR SEVERAL TIMES, NOTED NO DEFECTS. 2L72 4F RTA3EU 20050209001192005020900119CE 2005 2 9 DXTA200500558 120050124A212157034EX FAN CESSNA500 560CESSNA 2076750CE CABIN BURNED OUT E DXTAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 GL07348QS 5600348 DESCENDING THROUGH 16,000 FT HEAVY SMOKE IN COCKPIT. SMELLED OILY BUT WAS UNABLE TO DETERMINE THE SOURCE. NOTICED CABIN FAN C/B POPPED DURING SHUTDOWN. REPLACED DEFOG BLOWER ASSY PER CE560 M/M 21-21-01, OPS CHECKED GOOD. 2L72 4F RTA22CE 20050209001202005020900120CE 2005 2 9 DXTA200500559 120050125A323399144522 ACTUATOR CESSNA750 750 2076810CE NLG FAILED E DXTAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 GL07975QS458 7500175 T/O GEAR HANDLE UP, NOSE GEAR CAME UP REAL SLOW WITH ACCOMPANYING LOUD AIR NOISES AND CLUNKING FROM NOSE GEAR WHEEL WELL. REOCCURRING WRITE UP. REMOVED ACTUATOR AND INSTALLED RENTAL UNIT. SYSTEM OPERATIONAL AND LEAK CHECKS GOOD. INSTALLED UNIT HAS 245 CYCLES, IAW CE-750 M/M CH 32-30-03. 2L72 4J RTT00007WI 20050209001212005020900121EA 2005 2 9 MASA200500004 120050103A335059257 INVERTER CNDAIRCL600 CL6002B19 1900309EA NR 3 INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0777302 7302 THE PILOT REPORTED TWO SECTIONS OF THE EMERGENCY ESCAPE PATH LIGHTING INOP AND THE RIGHT OVERWING EXIT SIGN INOP. MAINTENANCE REPLACED THE NR 3 INVERTER. 2L72 4F RTA21EA 20050209001242005020900124NM 2005 2 9 AWXA200500172 120050126A534069353521 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 MCN - MAJOR REPAIR - DURING C-16 CHECK A .1875 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT BS 380, STR 22 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 380, STR 22 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-35352; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050209001252005020900125NM 2005 2 9 AWXA200500173 120050124A5315654503412 STRAP BOEING737 7373G7 1384595NM FLOORBEAM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 MCN - MAJOR REPAIR - DURING C-16 CHECK A .125 INCH CRACK WAS FOUND IN STRAP LOCATED ON LOWER SIDE OF FLOORBEAM AT BS 314, BL -0-. MAINTENANCE STOP DRILLED CRACK ON STRAP; PERFORMED AN HFEC INSPECTION TO VERIFY CRACK CONTAINED; FABRICATED A REPAIR PLATE PER DWG 65-45834; INSTALLED REPAIR PART IAW B737-300 SRM 53-10-51 FIG 204. 2L72 4F RTA16WE 20050209001262005020900126SO 2005 2 9 MASA200500006 120050103A335078241 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSINOPERATIVE A MASAO OTHER L NO TEST ININSP/MAINT 1 SW07830MJ 145259 NR 2 AND NR 3 FLOOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE INVERTER. 2L72 4T RTT00011AT 20050209001272005020900127SO 2005 2 9 MASA200500007 120050104A3350 SIGN EMB 145 EMB145LR 3260212SO EMERGENCY EXIT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07836MJ 145359 THE RIGHT HAND OVERWING INTERIOR EXIT SIGN INOP. CONTRACT MAINTENANCE RESET THE SYSTEM AND THE SIGN OPERATED NORMALLY. AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. 2L72 4T RTT00011AT 20050203001352005020300135EA 2005 2 3 COMA0560100 120050130A3230 LANDING GEAR CNDAIRCL600 CL6002B19 1900309EA NOSE LACK OF LUBE A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01988CA 7204 FLIGHT 5843 GEAR DISAGREE WARNING. CLEANED AND LUBED NLG. RETRACTION CHECKS NORMAL. 2L72 4F RTA21EA 20050203001402005020300140NM 2005 2 3 UPS05243762 120050112A5280 DOOR BOEING727 727185C 138406NNM TAIL SKI CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 INSPECTION TYPE:C, CORROSION FOUND AT TAIL SKID DOOR UPPER ATTACH POINTS BS 1183 S 28L + 28R. ON REMOVAL OF PANEL IT WAS FOUND TO BE CORRODED BEYOND LIMITS IAW 53-30-1. NEW PANEL FABRICATED IAW SRM 51-20-1. TAIL SKID MOUNTING CASTING SHOW SIGNS OF WEAR. NEW SUPPORT ANGLES FABRICATED IAW SRM 51-20-1 FIG 7. 2L73 4F A3WE 20050203001422005020300142NM 2005 2 3 UPS05243766 120050110A7120 BUSHING BOEING727 727185C 138406NNM NR 1 ENG MOUNT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 INSPECTION TYPE:C, ENGINE NR 1 FWD MOUNT FITTING HAS PITTING CORROSION IN ALL MOUNT HOLES. AFT O/B HOLE CORRODED BUSHING REMOVED IAW OHM 20-50-03. HFEC CARRIED OUT IAW NDTM 51-00-00 FIG 13, NO DEFECTS FOUND. REPAIRED IAW UPS EO B727-5440-11592-A. 2L73 4F A3WE 20050203001452005020300145NM 2005 2 3 UPS05243774 120050111A5330 SKIN BOEING727 727185C 138406NNM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 INSPECTION TYPE:C, AREA OF LITE SURFACE CORROSION ON SKIN BELOW S4L AT BS 1183. CORROSION FOUND TO BE RUNNING UNDER LAP. FURTHER RECTIFICATION CARRIED OUT IAW UPS EO B727-5330-0509. 2L73 4F A3WE 20050203001512005020300151NM 2005 2 3 SWAA050224 120050127A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 390, STRINGER 15R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20050203001562005020300156EA 2005 2 3 COMA0560085 120050125A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01978CA 7158 CRACK FOUND AT FS 484.00 OUTBOARD OF RBL 27 INTERCOSTAL OUTBOARD CLIP RIGHT HAND CABIN FLOOR. REPAIRED IAW REO 601R-53-41-059. 2L72 4F RTA21EA 20050203001572005020300157NM 2005 2 3 AWXA200500078 120050126A335032145410 EPSU AIRBUSA319 A319132 3930340NM ZONE 241 DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28807AW23294 1064 PHL - EEL - DURING 8-DAY CHECK FOUND BOTH THE LT AND RT OVERWING EMERGENCY POWER SUPPLY UNITS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BOTH LT AND RT OVERWING EMERGENCY POWER SUPPLY UNITS, OPERATIONAL TEST WAS GOOD. PART NAME; EPSU, MFG; DIEHL GMBH, P/N; 3214-54-10, S/N; 2958, TT; 13214, TC; 5249, TSR; 8. 2L72 4F RTA28NM 20050203001612005020300161WP 2005 2 3 CALA0500024 120050126A5347593056671 SEAT TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2735836 49441 INSPECTION FOUND LT MIDDLE SEAT TRACK CORRODED FROM STA 1022-1250, S18L. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-05, FIGURE 4F. 2L72 4F A6WE 20050203001782005020300178EA 2005 2 3 SWIA200514470 120050106A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07438SW 7574 PULLEY INTERCOSTAL HAS 2 CRACKED FLANGES; FS 484.00; LBL 27.0 + LBL 36.0. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED CRJ REO 601R53-41-059 REV A. 2L72 4F RTA21EA 20050203001792005020300179NM 2005 2 3 ABXA050024 120050122A5755 FITTING BOEING767 767231 1385131NM LT WING SPOILER CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23707AX 22570 LEFT WING SPOILER TORQUE TUBE HINGE FITTING CRACKED AT RSS 714.10. REMOVED AND REPLACED HINGE FITTING. 2L72 4F RTA1NM 20050203001802005020300180EA 2005 2 3 COMA0560094 120050125A2750865D1007 PDU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01470CA7630 7650 FLIGHT 4933 FLAPS FAIL CAUTION. REPLACED THE FLAP PDU. 2L72 4F RTA21EA 20050203001812005020300181EA 2005 2 3 COMA0560095 120050124A5270 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA PAX DOOR OUT OF ADJUST A COMAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO01976CA 7151 FLIGHT 4963 CABIN DOOR OUTER HANDLE CAUTION MESSAGE. ADJUSTED THE DOOR HANDLE PROXIMITY SENSOR. 2L72 4F RTA21EA 20050203001902005020300190NM 2005 2 3 SWAA050290 120050201A53106547973 CREASE BEAM BOEING737 7373K2 13844BANM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29340LV 23738 DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM WEB AT BS 580, RBL 70, CRACKED. REMOVED AND REPLACED WEB PER SRM. 2L72 4F RTA16WE 20050203001932005020300193NM 2005 2 3 SWAA050276 120050201A3350PH22300L LIGHT BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29356SW 25251 EEPLS STRIP AT ROWS 6 ABC AND 7 ABC, LOOSE. SECURED EEPLS STRIP PER MM. 2L72 4F RTA16WE 20050203001952005020300195NM 2005 2 3 SWAA050278 120050201A335065C27093 LIGHT BOEING737 7373H4 1384600NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29609SW 27929 FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT ASSY, BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20050208000022005020800002NM 2005 2 8 05FDEA00239 120050204A5311 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 DENT MARKS FOUND AT LEFT HAND FRAME STA Y= 1681 LONGERON 14. LONGERON 14 REPAIRED PER SRM 53-30-00 VOLUME I, FIGURE 1. 2L73 4F RTA22WE 20050208000032005020800003NM 2005 2 8 05FDEA00240 120050204A5311 FRAME DOUG MD11 MD11 3023602NM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 DENT MARK FOUND AT RIGHT HAND FRAME STA Y= 1641 LONGERON 12. LONGERON 12 REPAIRED PER SRM 53-30-00 VOLUME I, FIGURE 1. 2L73 4F RTA22WE 20050208000092005020800009NM 2005 2 8 CALA0500032 120050130A53116547959502 FRAME BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712319 23370 INSPECTION FOUND A 1.75 INCH CRACK IN FRAME AT NR 5 STOP, UNDER STOP, IN RADIUS (STA 794.3, AFT CARGO DOOR OPENING FORWARD FRAME, L18R TO L27R). REPAIRED IAW BOEING DRAWING 65C35243. 2L72 4F RTA16WE 20050208000172005020800017NM 2005 2 8 05FDEA00230 120050202A3260 WARNING LIGHT BOEING727 727200 138407ENM NLG ILLUMINATED A FDEAO OTHER J WARNING INDICATION CRCRUISE 1 SO25465FE 21289 DURING MANUAL EXTENSION WHEN NOSE GEAR WAS UNLOCKED, BOTH MAINS SHOWED UNSAFE. JACKED ACFT, PERFORMED NOSE GEAR MANUAL EXTENSION, SYSTEM TEST SEVERAL TIMES WITH FLAPS AT DIFFERENT SETTINGS AND PRESSURE ON AND OFF. SYSTEM FUNCTIONAL CHECKS GOOD IAW FED EX M/M 32-34-000-5. DOWN JACKED ACFT IAW FED EX M/M 07-11-000-2. 2L73 4F RTA3WE 20050208000192005020800019EA 2005 2 8 COMA0560103 120050130A2910AE7127631 LINE CNDAIRCL600 CL6002B19 1900309EA NR 1 HYD SYSTEM LEAKING A COMAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO01938CA 7046 FLT 5885 NR 1 HYDRAULIC SYSTEM LOW PRESSURE WARNING. REPLACED LEAKING HYDRAULIC LINE. 2L72 4F RTA21EA 20050208000272005020800027 2005 2 8 DL757050043 420050118A2320 RADIO BOEING757 75726D 1384907NM COCKPIT F/O MALFUNCTIONED A DALAC ABORTED TAKEOFF G MULTIPLE FAILURE TOTAKEOFF 1 SO27900PC 28446 COULD NOT TRANSMIT OR RECEIVE ON EITHER RADIO. REPLACED F/O COMM SEL PNL, OPS NORMAL. INSPECTED PLUG/WIRING, ALL NORMAL. OK FOR SERVICE. 2L72 4F RTA2NM 20050208000772005020800077NE 2005 2 8 DL777050055 220050123A7397 CONNECTOR BOEING777 777232 1385232NM RROYCERB211 RB21122* 54555NE NR 1 ENGINE BURNED A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27867DA 29743 051228 EICAS MESSAGE ENG FUEL FILTER L CAME ON ABOUT 2 HOURS INFLT. FOUND PIN 3 OF CONNECTOR OF DIFF PRESS SWITCH BURNT. REPLACED PIN, SWITCH AND FILTER. 2L72 4F4 FRTT00001SEA12EU 20050208000782005020800078NM 2005 2 8 DL76S050056 120050121A5512185T10011 SKIN BOEING767 767332 1382001NM HORIZONTAL STAB DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO27128DL 24078 THE UPPER SKIN OF THE LT HORIZ STABILIZER WAS FOUND WITH AN AREA OF DELAMINATION ON THE UPPER AND LOWER SURFACE OF THE ALUMINUM HONEYCOMBE SANDWICH ASSEMBLY. THE DELAMS WERE REMOVED WITH A 14 X 8 INCH CUTOUT AND A 13 X 9 INCH CUTOUT. THE CUTOUTS WERE REPAIRED WITH AN ALUMINUM DOUBLER METAL BOND REPAIR PROCEDURE PER ER/A 096372-14. 2L72 4F RTA1NM 20050208001012005020800101NM 2005 2 8 AT0500005 120050126A302032157083 SHUTOFF VALVE BOEING717 717200 1383700NM RROYCEBR700 BR700710A110 NE RT ANTI ICE SYS INOPERATIVE A ZZDAO OTHER J WARNING INDICATION CRCRUISE 1 SO15977AT 55036 PILOT GOT A RIGHT ANTI-ICE DISAGREE LIGHT ON THE EAD. REMOVED AND REPLACED THE RIGHT ENGINE ANTI-ICE VALVE. 2L72 4F4 FTRA6WE E00057EN 20050208001042005020800104EA 2005 2 8 05035632 120050204A2741 SWITCH CNDAIRCL600 CL6002B19 1900309EA TRIM DISCONNECT INOPERATIVE A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27632BR 7268 STAB AND MACH TRIM FAILURE ON CLIMBING PHASE. MX REPLACED DISCONNECT SWITCHES. 2L72 4F RTA21EA 20050208001112005020800111EA 2005 2 8 050327037 120050201A5320 PLATE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27703BR 7467 CARGO LANDING PLATE CORRODED AROUND NUT PLATES ON TOP SURFACE. 2L72 4F RTA21EA 20050208001182005020800118WP 2005 2 8 AALA20050086 120050205A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21598AA 53288 DFW - EMERGENCY ESCAPE PATH LIGHT IN TAIL CONE INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY ESCAPE PATH LIGHT IN TAIL CONE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050208001202005020800120WP 2005 2 8 AALA20050085 120050205A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21958U 49703 DFW - OVERHEAD EMERGENCY LIGHT AT ROWS 14 TO 17 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT ROW 14. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050208001252005020800125SO 2005 2 8 SWIA200514507 120050126A3397 WIRE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07288SW 120316 EMERGENCY LIGHTS BETWEEN ROW 2 & 5 INOPERATIVE. REPLACED BLOWN FUSE AND REPAIRED WIRES. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050208001292005020800129EA 2005 2 8 VNAA0501011 120050128A2133 OUTFLOW VALVE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN PRESSURE DIRTY A VNAAO OTHER J WARNING INDICATION CLCLIMB 1 GL05258PS 7941 DURING CLIMBOUT FROM YOW THE AIRCRAFT FAILED TO PRESSURIZE. THE CREW OF FLIGHT 2269 CONTINUED TO DESTINATION (PHL) UNPRESSURIZED. PSA MAINTENANCE CLEANED THE PRIMARY OUTFLOW VALVE. THE SYSTEM OPERATIONALLY CHECKED GOOD IAW CRJ 200 AMM 21-31-00-710-802. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050208001322005020800132EA 2005 2 8 VNAA0501013 120050131A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LAVATORY FALSE ACTIVATIONA VNAAO OTHER N FALSE WARNING NRNOT REPORTED 1 GL05221PS 7889 THE SMOKE TOILET WARNING MESSAGE ILLUMINATED IN FLIGHT AND WENT OUT AFTER ONE MINUTE. PSA MAINTENANCE PERFORMED AN INSPECTION OF THE LAVATORY AND THE AUTOMATIC FIRE EXTINGUISHER. NO EVIDENCE OF SMOKE, FIRE, OR DEFECTS WERE FOUND. THE LAVATORY SMOKE DETECTOR SYSTEM OPERATIONALLY TESTED GOOD IAW CRJ 200 AMM 26-26-01-210-801 & 26-16-01-710-801. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050208001332005020800133EA 2005 2 8 VNAA0501014 120050117A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A VNAAO OTHER F FLT CONT AFFECTED LDLANDING 1 GL05228PS 7897 ON SHORT FINAL INTO PHL THE FLAPS STUCK AT 30 DEGREES WHEN THE CREW OF FLIGHT 2304 SELECTED FLAPS 45. THE FLIGHT LANDED UNEVENTFULLY. PSA MAINTENANCE RESET CIRCUIT BREAKERS AND CYCLED THE FLAPS IAW BOMBARDIER SERVICE LETTER RJ-SL-00-001. THE FLAP SYSTEM OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050208001432005020800143NM 2005 2 8 05FDEA00188 120050127A5330 SKIN BOEING727 727200 138407ENM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25203FE 22925 STA 1130 STR 28L IS BULGING 1 RIVET PULLED AND RIVET SHEARED. REMOVED FLOOR PANEL STA 1070-STA 1183 AFT PIT FOR ACCESS IAW SRM 51-30-2. REMOVED EXISTING REPAIR DOUBLER AT STA 1130 IAW SRM 51-30-02. FOUND CORROSION UNDER REPAIR DOUBLER, REMOVED DAMAGED AREA IAW SRM 53-30-3. FABBED REPAIR DOUBLER AND FILLER IAW SRM 53-30-3 FIG 3. INSTALLED NEW REPAIR DOUBLER AND FILLER IAW SRM 53-30-3 FIG 3. INSTALLED FLOOR PANELS IAW SRM 51-30-2. 2L73 4F RTA3WE 20050208001452005020800145EA 2005 2 8 SWIA200514477 120050102A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07948SW 7789 THE 621 LOWER ANGLE CRACKED ON LEFT SIDE. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW REO 601R-53-61-117, CRJ 200 SRM 51-42-06 PG 11, 51-42-20 PG 24-28. 2L72 4F RTA21EA 20050208001612005020800161WP 2005 2 8 CALA0500042 120050206A53479957871535 SEAT TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2735836 49441 INSPECTION FOUND F/O'S AFT O/B SEAT TRACK CORRODED. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-40-01. 2L72 4F A6WE 20050208001832005020800183EU 2005 2 8 05FDEA00216 120050201A5310 BEAM AIRBUS300 A300B4622 3930401EU ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25716FD 358 LOWER FLANGE UPPER SURFACE OF LONGITUDINAL BEAM 5 LT AT FRAME 51A HAS A .5 INCH LONG CRACK. VERIFIED BY EDDY CURRENT INSPECTION. STOP DRILLED CRACK AND DOUBLE FLUSH PLUGGED HOLE PER EO 6-5310-7-5010 PT1 SECTION C7. 2L72 4F RTA35EU 20050208001882005020800188NM 2005 2 8 CALA0500037 120050202A53116546539 FRAME BOEING737 737524 1384721NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718611 27324 INSPECTION FOUND A 1 INCH CRACK THROUGH RIVET IN LT FRAME WHERE FRAME JOINS CABIN FLOORBEAM AT STA 616, LBL 64. THE CRACKED AREA WAS CUT OUT AND AN ANGLE DOUBLER REPAIR WAS INSTALLED IAW ECRA 5311-01158. 2L72 4F RTA16WE 20050208001922005020800192NM 2005 2 8 05FDEA00209 120050201A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25235FE 21329 STR 27R BS 735 WL 145 IS CRACKED. REPAIRED PER SRM 53-10-3. 2L73 4F RTA3WE 20050209000172005020900017NM 2005 2 9 05FDEA00170 120050125A5347S4929147 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 100 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 SEAT TRACK AT CABIN STA 791 LBL 8.5 HAVE BOLTS INSTALLED WRONG. SEAT TRACK AT CABIN STA 745 TO STA 815 LBL 8.5 REMOVED AS PER SRM 51-31-01 VOL II. REPAIR SEAT TRACK, FABRICATED & INSTALLED AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20050209000602005020900060NM 2005 2 9 QXEA200500150 120050131A2810 O-RING DHAV DHC8 DHC8202 2809007NM FUEL VALVE LEAKING A QXEAO OTHER K FLUID LOSS NRNOT REPORTED 1 NM09375PH12624 529 PDX - FLIGHT 2268 - THERE WAS A FUEL LEAK NOTED BY THE SINGLE POINT REFUELING DOOR. MAINTENANCE INSPECTED THE AREA AND REPLACED THE MASTER REFUEL/DEFUEL VALVE O-RINGS. OPERATIONAL AND LEAK CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050209000622005020900062NM 2005 2 9 05FDEA00191 120050128A534066144723 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25235FE 21329 GOUGE ON LOWER SURFACE OF STR 6L, STRINGER SPLICE BS 951. REPLACED PER SRM 51-30-2 AND 53-10-1 2L73 4F RTA3WE 20050209000642005020900064WP 2005 2 9 05FDEA00248 120050205A5753ARC25121 HINGE DOUG DC10 DC1030F 3023504WP ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25304FE 46629 LEFT WING OUTBOARD FLAP OUTBOARD HINGE, INBOARD PIVOT BORE CORRODED. REMOVED CORROSION, FABRICATED OVERSIZED BUSHING, INSTALLED AND HONED BUSHING TO FINAL INSIDE DIAMETER OF 0.8745-0.8755 IAW DAC CMM 57-52-02 AND FEDEX EA 8-5710-83967, PRIMED BORE IAW DC10-30 SRM 51-21-01 VOL II. 2L73 4F RTA22WE 20050209000662005020900066NM 2005 2 9 SWAA050317 120050204A3350604222 BATTERY BOEING737 7377Q8 1384418NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29799SW 28209 DURING SCHEDULED MV3 CHECK, FOUND R1 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20050209000702005020900070NM 2005 2 9 SWAA050326 120050205A53306545774 SKIN BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 747, STRINGER 21R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050209000722005020900072NM 2005 2 9 SWAA050328 120050206A3350D71701100 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29717SA 27851 DURING SCHEDULED MV2 CHECK, FOUND LT MID CABIN EMERGENCY EXIT LIGHT BATTERY INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20050209000762005020900076WP 2005 2 9 AALA20050067 120050131A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21228AA 49178 TPA - EMERGENCY EXIT LIGHT AT FORWARD GALLEY AISLE WALL INOPERATIVE. REPAIRED BROKEN WIRE IN AISLE FLOOR TRACK FOR EMERGENCY EXIT LIGHT AT FORWARD GALLEY AISLE WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050209000782005020900078EA 2005 2 9 COMA0560096 120050128A2750860D10018 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION CRCRUISE 1 SO01483CA6694 7689 FLIGHT 5632 FLAPS FAIL CAUTION. REPLACE THE FECU. 2L72 4F RTA21EA 20050209000812005020900081WP 2005 2 9 ABXA050027 120050120A5410591326245 ATTACH ANGLE DOUG DC9 DC941 302207NWP LT ENG PYLON CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23971AX 47497 LOWER LEFT PYLON ATTACH ANGLE WAS CRACKED INBOARD OF PYLON ACCESS PANEL 8101. REPAIRED AREA IAW DC-9 SRM 54-04. 2L72 4F A6WE 20050209000832005020900083WP 2005 2 9 ABXA050026 120050117A5320D036051 CUSP WEB DOUG DC9 DC941 302207NWP CABIN CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23971AX 47497 CUSP WEB CRACKED AT FS 984, 1010, 1030 - 1040, LEFT BUTT LINE 54, UNDER SEAT TRACK. REPLACED CUSP WEB IAW DC-9 SRM 51-30-1 AND 51-30-2. 2L72 4F A6WE 20050209001142005020900114CE 2005 2 9 DXTA200500563 120050126A3241 BRAKE CESSNA CESSNA500 560CESSNA 2076750CE ANTI SKID SYS MALFUNCTIONED E DXTAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07326QS 4546 5600526 BRAKES WORKED NORMALLY AFTER LANDING, AS AIRCRAFT DECELERATED THROUGH APPROXIMATELY 20 KTS, THE BRAKES FAILED. BRAKE PRESSURE RECOVERED WHEN BRAKE PEDALS WERE PUMPED. REMOVED AND REPLACED LEFT AND RIGHT WHEEL ANTI-SKID TRANSDUCERS AFTER TROUBLESHOOTING SYSTEM. PERFORMED ANTI-SKID DIAGNOSTIC PER M/M. TAXIED AIRCRAFT. ANTI-SKID SYSTEM PERFORMED SATISFACTORY, ALL WORK DONE IAW C560 M/M CH 32-42-00. 2L72 4F RTA22CE 20050209001382005020900138SO 2005 2 9 MASA20050048 120050120A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07836MJ 145359 PILOT REPORTED SEVERAL SECTIONS OF THE EMERGENCY FLOOR PATH LIGHTING INOP. MAINTENANCE RESET THE SYSTEM AND WERE UNABLE TO DUPLICATE THE DISCREPANCY. 2L72 4T RTT00011AT 20050209001432005020900143SO 2005 2 9 CHQA200500027 120050207A3350 LIGHT EMB 135 EMB135LR 3260305SO CABIN INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11838RP 145720 NUMBER 2 OVERHEAD EMERGENCY EXIT LIGHT IS INOP. FOUND CANNON PLUG P8639 DISCONNECTED. RECONNECTED CANNON PLUG. OPERATIONAL CHECK OF EMERGENCY LIGHTS IS SATISFACTORY PER EMB 135 MM 33-50-00. 2L72 4F RTT00011AT 20050209001452005020900145NM 2005 2 9 DXTA200500570 120050201A3260D233360001 PROXIMITY SWITCH AMD FALC50FALCON2000 2730170NM MLG FAILED E DXTAO OTHER J WARNING INDICATION APAPPROACH 1 GL07229QS1875 129 LANDING GEAR HANDLE FLASHED RED FOLLOWED BY LN3 GEAR CONTROL C/B POPPING. FOLLOWED ABNORMAL GEAR EXT CHECKLIST W/ONE RESET OF C/B GEAR EXTENDED NORMALLY AND LANDING GEAR CONTROL C/B POPPED AGAIN. REMOVED BAD SWITCH AND INSTALLED NEW PROXY SWITCH AT LT MAIN LANDING GEAR. COMPLIED WITH FUNCTION TEST OF MLG EXTENSION / RETRACTION IAW FALCON 2000 MAINTENANCE MANUAL 32-600 AND 32-300. 2K73 4F RTA50NM 20050209001472005020900147CE 2005 2 9 DXTA200500572 120050201A3260NPN PROXIMITY SWITCH CESSNA750 750 2076810CE MLG OUT OF RIG E DXTAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL07975QS 7500175 AFTER TAKEOFF GEAR HANDLE COULD NOT BE MOVE TO THE UP POSITION. TROUBLESHOT TO INCORRECTLY RIGGED NLG SQUAT SWITCH. RERIGGED SWITCH IAW 750 MM CH 32-60-00. GEAR OPERATIONALLY CHECKS GOOD. 2L72 4J RTT00007WI 20050209001542005020900154CE 2005 2 9 DXTA200500566 120050130A3240 BRAKE ASSY CESSNA500 560CESSNA 2076750CE MALFUNCTIONED E DXTAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07311QS 5600311 THE RIGHT HAND SIDE BRAKE PEDALS NEED TO BE DEPRESSED FULLY AND THEN PUMPED TO RECEIVE ADEQUATE BRAKING ACTION. ON THE LAST LANDING, BRAKE PEDALS WERE PUSHED TO FLOOR THEN PUMPED. BLED BRAKE SYSTEM PER CHAPTER 32-42-00 OF THE CITATION 560 MM, OPERATIONAL AND LEAK CHECK GOOD. 2L72 4F RTA22CE 20050209001582005020900158WP 2005 2 9 DHL2004809531 120050110A5753 SKIN DOUG DC8 DC873F 302199FWP LT WING TE FLAP DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01809DH91189 46047 LT WING INBD FLAP UPPER SKIN DEFLECTED, XW 2.000 TO XW 91.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED DAMAGED PANEL PLATING IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. FABRICATED NEW PANEL PLATING (AL2024-T3 0.050) IAW BOEING MESSAGE 1-XW84N, DWG SEMAN ED 3808. CLEANED, TREATED AND PRIMED AREA AND NEW PANEL PLATING INTERIOR IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW PANEL PLATING IAW BOEING MESSAGE 1-XW84N, DWG SEMAN ED-3808 SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. IAW FAX BOEING NUMBER 1-XW84N THIS REPAIR IS TEMPORARY TO NEXT AIRCRAFT CHECK -C- WITH DETAILED VISUAL INSPECTION TO SKIN AND RIBS AT INTERVALS OF 500 FLIGHT HOURS. 2L74 4F RT4A25 20050209001602005020900160WP 2005 2 9 0500131237 120050104A5730 SKIN DOUG DC10 DC1030 3023501WP RT WING CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01237NW 47844 DURING H-CHECK FOUND CRACK ON RT WING LEADING EDGE SKIN AT XOS 693. REPAIRED PER EA 12-202235. 2L73 4F A22WE 20050209001672005020900167EU 2005 2 9 RAIA00502003 120050202A3411 SENSOR JETAIRJETSTMJETSTM4101 1500501EU AIR DATA MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03551HK 41040 STL - LT P1 AND STATIC AIR DATA LIGHT ILLUMINATED. MAINTENANCE REPLACED CURRENT SENSOR TO LT STATIC PORT HEATER. 2L72 4T RTA41NM 20050209001692005020900169EU 2005 2 9 RAIA00502004 120050203A3097 WIRE JETAIRJETSTMJETSTM4101 1500501EU WARNING HORN DAMAGED A RAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03563HK 41079 PIT - RT ELEVATOR HORN ANTI-ICE FAULTED IN FLIGHT. MAINTENANCE DEFERRED PER MEL 30-18 CAT B. SUBSEQUENTLY - REPAIRED WIRE AT HJ11. 2L72 4T RTA41NM 20050209001702005020900170WP 2005 2 9 RAIA00502002 220050202A7200 ENGINE JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE331* 01514WP LEFT VIBRATION A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03553HK 41066 BWI - LT OIL CONTAM LIGHT IN-FLIGHT ENGINE STATS GOOD BUT FELT VIBRATION IN LEFT ENGINE. MAINTENANCE PERFORMED MAG-CHIP ADJUSTMENT/TEST. OPS CHECK AND NO ENGINE VIBRATION'S NOTED AT THIS TIME. 2L72 4T3 TRTA41NM E2WE 20050209001712005020900171EU 2005 2 9 RAIA00502005 120050203A300031058993 TRANSDUCER JETAIRJETSTMJETSTM4101 1500501EU TORQUE SENSOR FAILED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03572HK7260 41091 LT AND RT IEC CAPTION ILLUMINATED. MAINTENANCE REMOVED AND REPLACED NEGATIVE TORQUE SENSING TRANSDUCER. 2L72 4T RTA41NM 20050209001722005020900172CE 2005 2 9 DXTA200500575 120050203A3240651710575 LINE CESSNA500 560CESSNA 2076750CE BRAKES CHAFED E DXTAO OTHER S AFFECT SYSTEMS LDLANDING 1 GL07361QS 5600361 UPON LANDING COPILOT LEFT BRAKE PEDAL WENT TO FULL DOWN W/O BRAKING AIRCRAFT, HARD RIGHT TURN UNTIL RIGHT BRAKE LEASED. FOUND LT BRAKE CROSSOVER LINE RUBBING ON RUDDER CABLE TO RUDDER PEDAL TORQUE TUBE ATTACH ARM (LT), RUBBING CAUSED HOLE IN LINE. REMOVED AND REPLACED BRAKE LINE WITH NEW, BLED BRAKES, OPS CHECK GOOD IAW CIT 560 ULTRA M/M CH 20-10-06 & 32-42-00. 2L72 4F RTA22CE 20050209001742005020900174CE 2005 2 9 DJFA2005056 120050206A3244 TIRE CESSNA500 560CESSNA 2076750CE NLG FAILED E DJFAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA23501CW 5600050 CREW REPORTED, UPON GEAR RETRACTION AFTER TAKEOFF RECEIVED A RED GEAR UNSAFE WARNING LIGHT. CREW DECLARED AN EMERGENCY DUE TO THE SUSPICION THAT A NOSE WHEEL TIRE HAD BLOWN. AIRCRAFT LANDED IN KORL WITHOUT FURTHER INCIDENT. AFTER LANDING IT WAS DISCOVERED A TIRE DID NOT BLOW OUT. 2L72 4F RTA22CE 20050209001752005020900175NE 2005 2 9 DHL2005760005 220050204A7200 ENGINE BOEING727 7272B7 138407LNM PWA JT8 JT8D17A 52049NE NR 1 FLAMED OUT A DHLAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION TXTAXI/GRND HDL 1 SO01760AT 21954 715301 ENGINE NR 1 FLAMED OUT AFTER 30 SEC OF IDLE. ATTEMPTED 2ND START PER MX CONTROL, NO LIGHT OFF, NO FUEL FLOW. PERFORMED ABNORMAL PROCEDURE PER AOM. ATTEMPTED ANOTHER START WITHOUT ANY PROBLEM. ENGINE IDLES NORMALLY. RESET FIRE HANDLE AND ATTEMPTED RESTART. NORMAL START OCCURRED. NR 1 ENG OPS CHECKS GOOD IAW B727MM 80-11-00 AND JRH 5.2 2L73 4F4 F A3WE E2EA 20050209001772005020900177NM 2005 2 9 DHL2005741001 120050203A7830 WARNING LIGHT BOEING727 7272Q9 138448MNM THRUST REVERSER ILLUMINATED A DHLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01740DH 21930 NR 3 THRUST REVERSER LIGHT ILLUMINATED PRIOR TO TAKEOFF ROLL PER ASTAR SAFETY REPORT. CREW CYCLED REVERSER SEVERAL TIMES AND RAN ENGINE UP. REVERSER LIGHT DID NOT COME ON AGAIN. 2L73 4F RTA3WE 20050209001782005020900178NM 2005 2 9 SWAA050311 120050203A3350604222 BATTERY BOEING737 7373T5 1384608NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29667SW 23063 DURING SCHEDULED SERVICE CHECK, FOUND FWD GALLEY LOWER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20050209001792005020900179NM 2005 2 9 SWAA050312 120050203A53306545776 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29696SW 23064 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 927 + 6, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050209001802005020900180NM 2005 2 9 C1HA200583001 120050122A3260 WARNING LIGHT BOEING727 7272S7 138407ZNM TAIL SKID ILLUMINATED A C1HAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL15683CA 22490 AFTER T/O WITH GEAR RETRACTED TAIL SKID LIGHT ILLUM ON S/O PANEL, PER COM GEAR RECYCLED. ON RETRACTION LT & RT MAIN GEAR UNSAFE LIGHTS (RED) ILLUM AND LT & RT MAIN GEAR DOOR LIGHTS ON S/O PANEL. RED DOORS LIGHT ON FWD PANEL ILLUM. GEAR EXTENDED NORMALLY & ALL LIGHTS NORMAL. RETURNED TO AIRPORT. PERFORMED INSPEC OF LANDING GEAR RELATED COMPONENTS IN WHEEL WELL, NO DEFECTS. INSPEC PNEUMATIC DOOR & TAIL SKID, PNEUMATIC DOOR OK, TAIL SKID HAD MINOR SCRATCH. T/S SYS, ALL ASPECTS OF MX WERE FAVORABLE. DURING DEPARTURE NORMAL RETRACTION INDICATIONS WERE WITNESSED. UPON ARRIVAL AT MSP NORMAL EXTENTION INDICATIONS WERE WITNESSED. MX PERFORMED INSPECTIONS PRIOR TO FLT. 2L73 4F A3WE 20050209001812005020900181CE 2005 2 9 DJFA2005050 120050107A323345AS38510008 ACTUATOR BEECH MU300 400A 1155402CE RIGHT DEFECTIVE E DJFAA UNSCHED LANDING O OTHER LDLANDING 1 EA23442CW RK42 CREW REPORTED, AFTER NUMEROUS ATTEMPTS TO LOWER THE GEAR, DID NOT RECEIVE 3 GREEN LIGHTS. AN ALTERNATE EXTENSION WAS PERFORMED AND AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED BOTH MAIN LANDING GEAR DOWNLOCK SWITCHES, AND INSTALLED A NEW CONTROLLER. OPERATIONAL CHECKS WERE GOOD. PROBLEM HAD REOCCURRED DURING TEST FLIGHT. MAINTENANCE REPLACED THE RIGHT MAIN LANDING GEAR DOWNLOCK ACTUATOR. TEST FLIGHT WAS SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4F RTA16SW 20050209001822005020900182WP 2005 2 9 DHL2005807002 120050129A3241 WARNING LIGHT DOUG DC8 DC873F 302199FWP ANTI SKID SYS ILLUMINATED A DHLAO OTHER J WARNING INDICATION LDLANDING 1 SO01807DH 45990 WHEN GEAR EXTENDED ANTI-SKID LIGHT ILLUMINATED ALONG WITH -LFO- & -LFI-. PERFORMED ABNORMAL PROCEDURE, NORMAL LANDING ACCOMPLISHED. FOUND CANNON PLUG ON ANTI-SKID VALVE FOR LFO, LFI TO BE INSECURE, RESECURED IAW DC-8 M/M 32-43-0, CHECKS GOOD. 2L74 4F RT4A25 20050209001842005020900184NM 2005 2 9 SWAA050333 120050206A55116551524 SPAR BOEING737 7373Q8 1384670NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND RT AND LT HORIZONTAL STABILIZER FWD AND AFT SPARS, UPPER ATTACH LUGS AND CLEVIS, CORRODED. REPAIRED HORIZONTAL STAB PER SRM. 2L72 4F RTA16WE 20050209001872005020900187NM 2005 2 9 SWAA050331 120050206A53156546811 FLOORBEAM BOEING737 7373K2 13844BANM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29340LV 23738 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM AT BS 967, RBL 18, CORRODED. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20050209001882005020900188WP 2005 2 9 MWEA050020 120050204A2560A12SA MEGAPHONE DOUG DC9 DC981 3022081WP CABIN INOPERATIVE A MWEAK NONE O OTHER ININSP/MAINT 1 GL31812ME 48006 MEGAPHONE FOUND INOPERATIVE DURING CABIN CHECK. INSTALLED SERVICEABLE MEGAPHONE. 2L72 4F A6WE 20050209001902005020900190EA 2005 2 9 SWIA200514472 120050106A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07438SW 7574 CARGO FLOOR SUPPORT ANGLE AT FS 621.00 RBL 42.0 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FLOOR SUPPORT ANGLE AT FS 621 AND RBL42, IAW CRJ REO 601R-53-61-117, REV B. 2L72 4F RTA21EA 20050209001922005020900192EA 2005 2 9 SWIA200514474 120050106A5340 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07438SW 7574 CARGO COMPARTMENT FS 605.00 TRANSVERSE BEAM ATTACH ANGLE FOR LANDING PLATE STOP FITTING CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-41-02, 51-41-04. 2L72 4F RTA21EA 20050209001942005020900194EA 2005 2 9 SWIA200514476 120050122A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07954SW 7815 FS 484 LT INTERCOSTAL OUTBOARD FLANGE LBL 36 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED INTERCOSTAL FS 484 LT, O/B, LBL 36, IAW CRJ REO 601R-53-41-059, REV. A 2L72 4F RTA21EA 20050209001952005020900195SO 2005 2 9 SWIA200514435 120050120A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT DISCHARGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07270YV8110 1998 120270 MID CABIN EMERGENCY LIGHTS INTERMITTENT DURING TEST. REPLACED EMERGENCY BATTERY PACK AT MID CABIN. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050209001962005020900196SO 2005 2 9 SWIA200514436 120050115A5210 DOOR EMB 120 EMB120ER 3260203SO MAIN PAX LACK OF LUBE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07236SW 120312 MAIN CABIN DOOR VERY DIFFICULT TO OPEN. LUBRICATED MAIN DOOR. 2L72 4T RTA31SO 20050209001982005020900198EA 2005 2 9 SWIA200514438 120050124A3350 CHARGER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07591SW 7079 RIGHT HAND ABOVE WING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED NR 2 CHARGER/SUPPLY ASSY IAW 33-52-00, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050209001992005020900199NM 2005 2 9 DHL2005762001 120050120A3242 BRAKE ASSY BOEING727 7272B7 138407LNM NR 2 MALFUNCTIONED A DHLAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01762AT 22162 LEFT BRAKE STICKS AND CHATTERS WHEN TAXIING. BLEED NR 2 BRAKE IAW MM 32-41-00. TAXIED A/C, OPS CKS GOOD. OK TO CONTINUE. 2L73 4F A3WE 20050209002012005020900201EA 2005 2 9 05023644 120050123A2760 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERS OUT OF RIG A VTZAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA27644BR 7379 ABORTED TAKEOFF DUE TO SPOILER CONFIGURATION WARNING. MX FOUND RT INBOARD PCU OUT OF RIG. RE-RIGGED. 2L72 4F RTA21EA 20050210000442005021000044SO 2005 2 10 SIMA200500601 120050102A3350AD20131A BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21636AE 145160 ORD - FLT 4238 - TWO AISLE EMERGENCY LIGHT STRIPS ARE INOPERATIVE. REPLACED NR 3 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20050203001492005020300149NM 2005 2 3 SWAA050222 120050127A3350101331 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29604SW 27955 DURING SCHEDULED PM CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS, LOOSE. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20050203001542005020300154NM 2005 2 3 SWAA050227 120050127A57536546486 PANEL BOEING737 7373H4 1384600NM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED C2 CHECK, FOUND RT WING INBOARD MIDFLAP WEDGE PANEL DELAMINATED. REPAIRED MIDFLAP WEDGE PANEL PER SRM. 2L72 4F RTA16WE 20050203001632005020300163NM 2005 2 3 CALA0500026 120050107A5315141N51911 FLOORBEAM BOEING757 757224 1384958NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717104 27294 INSPECTION FOUND CENTER FLOORBEAM CORRODED BETWEEN STA 345 AND 365, BL 0. THE CORRODED SECTION OF FLOORBEAM WAS REPAIRED IAW SRM 51-40-03, PARAGRAPH 4 AND 7. 2L72 4F RTA2NM 20050203001682005020300168EA 2005 2 3 SWIA200514440 120050122A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLT SPOILERS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07435SW 7555 APPLIED HYDRAULICS AND GOT A LEFT SPOILERON CAUTION MESSAGE. REPLACED LEFT INBOARD AND OUTBOARD PCU IAW MM 27-62-01. REPLACED CB4CN. OPERATIONAL CHECK GOOD. P/N: 27000-7, S/N OFF: 5175, S/N OFF: MAL3758. 2L72 4F RTA21EA 20050203001882005020300188NM 2005 2 3 SWAA050248 120050130A53106546529 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29602SW 27953 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 500A, STRINGER 16R, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050203001962005020300196 2005 2 3 SWAA050279 420050201A2565D31354 SLIDE BOEING737 7373A4 1384585NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29679AA 23291 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050203001972005020300197NM 2005 2 3 SWAA050280 120050201A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29326SW 23690 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 787, STRINGER 19L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050203002042005020300204WP 2005 2 3 AALA20050077 120050201A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW2133502 49739 SEA - OVERHEAD EMERGENCY EXIT LIGHTS AT AFT ENTRY AISLE INOPERATIVE. REPLACED BATTERY PACK B527 AT RIGHT HAND AFT LAVATORY FOR OVERHEAD EMERGENCY EXIT LIGHTS AT AFT ENTRY AISLE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050203002052005020300205WP 2005 2 3 AALA20050075 120050130A3350 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW2176202 53292 ORD - TWO EMERGENCY LIGHTS IN AFT CABIN AT LOWER SLIDE INOPERATIVE. REPLACED BATTERY PACK B527 FOR EMERGENCY LIGHTS IN AFT CABIN AT LOWER SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050207000072005020700007EU 2005 2 7 05FDEA00242 120050204A2910 LINE AIRBUS310 A310222 3930315EU HYD SYSTEM LEAKING A FDEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO25455FE 331 HYDRAULIC GREEN SYSTEM FAILURE (LOW FLUID), FOLLOWED ECAM AND QRH. EXTENDED LANDING GEAR MANUALLY. DECLARED EMERGENCY LANDED MANILA. REPLACED HYDRAULIC LINE WITH TEMPORARY FLEX LINE AND SERVICE WITH HYDRAULIC FLUID. REPLACED TEMPORARY FLEX LINE P/N A292192180000 PER STD PRACTICES 20-23-11 PARAGRAPH -F-. NOTED THAT HYDRAULIC FLUID QUANTITY DID NOT GO BELOW LOW QUANTITY MARK. LEAK CHECK PERFORMED, TWO TEMP FLEXIBLE HOSES INSTALLED TO FLAP CTL OIL REFERENCE: AMM SUP 20-23-11-0, MPN A2901075800000, CPN 2910934. 2L72 4F RTA35EU 20050207000092005020700009EU 2005 2 7 05FDEA00198 120050129A5511 SPAR AIRBUS310 A310203 3930313EU HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25405FE 237 RT HORIZONTAL STAB UPPER TRAILING EDGE LOWER SURFACE FROM INBOARD END AND EXTENDING OUTBOARD 31.0 INCHES. THERE IS LIGHT TO SEVERE CORROSION AROUND AND BETWEEN NUT PLATES. REMOVED CORROSION IAW A310-200 SRM 51-74-10 AND FOUND A SECTION OUT OF LIMITS IAW A310-200 SRM 55-10-00. CUT OUT DAMAGED SECTION (RIB 3 TO RIB 5) AND FABRICATED REPAIR PARTS IAW A310-200 SRM 55-11-21 FIG 219. INSTALLED REPAIR PARTS IAW A310-200 SRM 55-11-21 AND 51- 40-21. 2L72 4F RTA35EU 20050207000172005020700017NM 2005 2 7 QXEA200500149 120050130A275144281508010 INDICATOR DHAV DHC8 DHC8202 2809007NM COCKPIT FALSE INDICATIONA QXEAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 NM09362PH12516 518 SEA - FLIGHT 2291 - THE FLIGHT RETURNED TO THE GATE WHEN AFTER SELECTING THE FLAPS TO 5 DEGREES, THE INDICATOR WAS SHOWING THE FLAP POSITION OUT OF THE WHITE ARC. MAINTENANCE REPLACED THE FLAP INDICATOR AND PERFORMED OPERATIONAL CHECKS. THE CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050207000192005020700019WP 2005 2 7 CALA0500040 120050203A53109957852 DOOR FRAME DOUG DC9 DC982 3022082WP FUSLEAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2735836 49441 INSPECTION FOUND A 1.75 INCH CRACK IN NWW LT DOOR JAMB AT UPPER LOCK FASTENER FOR SPRAY DEFLECTOR GUARD, STA 45. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 110. 2L72 4F A6WE 20050207000322005020700032NM 2005 2 7 SWAA050299 120050202A335020121 BATTERY BOEING737 7375H4 138449DNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29521SW 25320 DURING SCHEDULED SERVICE CHECK, FOUND LT EXTERIOR EMERGENCY EXIT LIGHT AND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20050207000382005020700038EU 2005 2 7 05FDEA00213 120050201A5753A57942252210 BEAM AIRBUS300 A300B4622 3930401EU ZONE 500 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25716FD 358 LEFT WING NR 2 FLAP TRACK BEAM OUTBOARD SIDE ROLLER PATH HAS THREE WEAR MARKS. REF FED EX EA 6-5720-85940, LT WING NR 2 FLAP TRACK BEAM O/B 3 EA AREAS FOUND TO BE ACCEPTABLE AS IS TO CONTINUE SERVICE, AND TO BE CHECKED AT NEXT C-CHECK. 2L72 4F RTA35EU 20050208000012005020800001 2005 2 8 05FDEA00215 420050201A3414 INDICATOR DOUG DC10 DC1010 3022110WP COCKPIT INACCURATE A FDEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO25389FE 46623 A 70 KT DIFFERENCE BETWEEN CAPT & F/O MACH VMO FLAG INDICATOR. CAPT SHOWING 250 & F/O SHOWING 340 AT FL 260 MACH WARNING HORN WAS GOING OFF. ATB MHT. T/S SYSTEM PER TAFI 34-13-00 REPLACED NR 1 CADC AND MACH AIRSPEED INDICATOR. CLEANED PITOT LINES WITH NITROGEN NO OBSTRUCTIONS FOUND. PERFORMED PITOT TEST OF SYSTEM BOTH CAPT & F/O INDICATORS CHECK NORMAL. RETURNED TO SERVICE. 2L73 4F A22WE 20050208000062005020800006EU 2005 2 8 05FDEA00233 120050203A5753 SKIN AIRBUS300 A300B4622 3930401EU RT WING TE FLAP DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25716FD 358 RIGHT HAND WING INBOARD FLAP TOP SKIN COMPLY WITH EA 6-5750-85635. REMOVED AND REINSTALLED SKIN WITH REPLACEMENT FASTENERS PER SB 300-57-6098 FIG 3 SHEET 2, IAW FEDEX EA 6-5750-85635 REV-A AND DRAWING A579600005. 2L72 4F RTA35EU 20050208000152005020800015EU 2005 2 8 05FDEA00228 120050202A5754A5786550600200 SLAT TRACK AIRBUS300 A300B4622 3930401EU ZONE 600 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25716FD 358 M-TYPE-MOD 716-27-80-0264, NR 8 SLAT TRACK HAS SIDE ROLLER WEAR SPOTS. BLENDED AND POLISHED TRACK ROLLER WEAR SPOTS FOUND ONE AREA OUT OF ALLOWABLE DAMAGE LIMITS IAW A-300 SRM 57-40-00 3.A.(3)(D). THE TRACK MAYBE RETURNED TO SERVICE PROVIDED THE AREA IS INSPECTED FOR FURTHER WEAR AT EVERY C-CHECK IAW A300 SRM 57-40 00 3.A.(3)(D). REMOVED AND REPLACED NR 8 RIGHT WING SLAT TRACK IAW A300 -600 AMM 27-80-14-4. REMOVED AND REPLACED NR 8 RIGHT SLAT TRACK ECCENTRIC BOLT IAW A300-600 AMM 27-80-14-4. OPS CHECK GOOD. 2L72 4F RTA35EU 20050208000202005020800020EA 2005 2 8 COMA0570011 120050201A531267053110521 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01374CA5175 10090 FS 280 LT AND RT BULKHEADS HAVE MAJOR CORROSION ON AFT SIDE ALONG THE BOTTOM EDGES. REPLACED LOWER WEBS AT FS 280 BULKHEAD IAW BOMBARDIER AEROSPACE REO 670-52-11-052 AND BRAS EO 601R-53-5930. 2L72 4F RTA21EA 20050208000242005020800024NM 2005 2 8 SWAA050313 120050203A5753 SKIN BOEING737 7373T5 1384608NM LT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29696SW 2245 23064 DURING SCHEDULED CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED LT WING T/E AFT FLAP PER MM. 2L72 4F RTA16WE 20050208000252005020800025NM 2005 2 8 SWAA050314 120050203A2121215201 FAN BOEING737 7373H4 1384600NM E&E BAY OVERHEATED A SWAAA UNSCHED LANDING MB OVER TEMP SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW29396SW 27690 DIVERSION, F/A'S REPORTED SMOKE SMELL FROM FWD AND MID CABIN, NO SMOKE AT ANYTIME. REMOVED AND REPLACED GASPER FAN PER MM. 2L72 4F RTA16WE 20050208000282005020800028NE 2005 2 8 DL76L050044 220050119A7210PW40603 ENGINE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 2 SHUTDOWN A DALAEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 SO27174DN51045 24802 724146 RT ENG SHUTDOWN BY CREW DUE TO VIBS/LOW OIL PRESSURE/LOSS OF OIL QTY. A/C DIVERTED TO NCE. REPLACED ENGINE. 2L72 4F4 FRTA1NM E24NE 20050208000302005020800030NM 2005 2 8 DL76G050046 120050120A3397 WIRE HARNESS BOEING767 767324 1385203NM FWD GALLEY CHAFED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO27394DL 27394 F/A RECEIVING SHOCKS WHEN CONTACTING METAL DOOR IN FWD GALLEY NEAR COFFEEMAKERS. REPAIRED CHAFED GALLEY POWER WIRES. 2L72 4F RTA1NM 20050208000522005020800052NM 2005 2 8 DL757050037 120050116A2910321002874 CONTROL VALVE BOEING757 757232 1384965NM BRAKES INGESTED A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO27652DL 24392 RIGHT HYD QTY DROPPED TO .43 WITH RT AUTOPILOT TRIP. FOUND RT SYS QTY AT .43 WITH LT HYD QTY AT 1.33. REPLACED PARKING BRAKE VALVE AND ANTI-SKID SHUTTLE VALVES. 2L72 4F RTA2NM 20050208000532005020800053NM 2005 2 8 DL777050038 120050117A3350 FUSE BOEING777 777232 1385232NM POWER SUPPLY BLOWN A DALAK NONE L NO TEST ININSP/MAINT 1 SO27862DA 14241 29734 AFT ZONE EMERGENCY PATH LIGHTS INOP. REPLACED POWER SUPPLY. 2L72 4F RTT00001SE 20050208000562005020800056NM 2005 2 8 05FDEA00202 120050130A5330AJC7059502 SKIN DOUG MD11 MD11 3023602NM ZONE 100 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 APU EXHAUST AREA UPPER DOOR HINGE FUSELAGE SKIN FOUND WITH REPAIR. EXISTING REPAIR ON APU EXHAUST AREA UPPER DOOR HINGE FUSELAGE SKIN REMOVED AS PER SRM 51-35-01 VOL I. NEW REPAIR DOUBLERS FABRICATED AND INSTALLED AS PER SRM 53-20-00, FIG 4 VOL I & SRM 53-00-01 FIG 5 VOL II. 2L73 4F RTA22WE 20050208000572005020800057NM 2005 2 8 05FDEA00203 120050130A5313A5A70311 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 CENTER CARGO LONGERON 47 LT CORRODED AT STA 5-111 TO 5-121. CENTER CARGO LONGERON 47 LT CORRODED AT STA 5-111 TO 5-121 LONGERON REPAIR CARRIED OUT AS PER SRM 53-10-00 FIG 1, VOL I. 2L73 4F RTA22WE 20050208000752005020800075NE 2005 2 8 DL76G050053 220050122A7261CF680C2B6F ENGINE BOEING767 767332 1382001NM GE CF6 CF680C2B6F 30025NE NR 1 LEAKING A DALAK NONE KJ FLUID LOSS WARNING INDICATION ININSP/MAINT 1 SO271612T1610716107 30575 706319 DURING L/O CHECK OIL LEAK IN D-SUMP AREA BEYOND M/M LIMITS. REPLACED ENGINE. 2L72 4F4 FRTA1NM E13NE 20050208000802005020800080NM 2005 2 8 DL764050058 120050125A3350336701252 CHARGER BOEING767 767432ER 1385134NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27836MH 29709 ON SERVICE FOUND AFT LT EMERGENCY LIGHT INOP. REMOVED AND REPLACED POWER SUPPLY ASSY PER M/M, CHECKS GOOD. 2L72 4F RTA1NM 20050208000972005020800097EA 2005 2 8 SWIA200514505 120050203A2741 SWITCH CNDAIRCL600 CL6002B19 1900309EA TRIM DISCONNECT MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CRCRUISE 1 NM07926SW 7687 AT FL 340 STAB TRIM & MACH TRIM CAUTION MESSAGE ILLUMINATED IN FLIGHT. REMOVED AND REPLACED COPILOT'S TRIM DISCONNECT SWITCH. OPERATIONAL CHECK GOOD. WORK CONDUCTED IAW CRJ 200 MM CHAPTER 27-41-30. 2L72 4F RTA21EA 20050208001052005020800105EA 2005 2 8 050327032 120050201A5210 STRIKER CNDAIRCL600 CL6002B19 1900309EA PAX DOOR DENTED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27703BR 7467 PAX DOOR SEAL STRIKER PLATE DENTED FROM IMPACT WITH DOOR PINS. 2L72 4F RTA21EA 20050208001092005020800109EA 2005 2 8 050327035 120050201A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27703BR 7467 LEFT OBLIQUE ANGLE AT FS 625 CRACKED. 2L72 4F RTA21EA 20050208001102005020800110EA 2005 2 8 050327036 120050201A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27703BR 7467 RIGHT OBLIQUE ANGLE AT FS 625 CRACKED. 2L72 4F RTA21EA 20050208001152005020800115NM 2005 2 8 SWAA050321 120050204A53306552988107 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29505SW 24182 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT AFT ENTRY DOOR UPPER AFT CORNER, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20050208001212005020800121NM 2005 2 8 SWAA050335 120050206A53116546550 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29603SW 27954 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 787, LBL 22, CORRODED. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20050208001282005020800128EA 2005 2 8 SWIA200514489 120050126A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07908SW 7540 EMERGENCY LIGHT STRIP ON RIGHT SIDE BETWEEN ROWS 5 AND 8 INOPERATIVE. REPLACED LIGHT POWER STRIP TO CENTER EMERGENCY LIGHT STRIP. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050208001302005020800130EA 2005 2 8 VNAA0501010 120050127A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS ILLUMINATED A VNAAO OTHER J WARNING INDICATION CLCLIMB 1 GL05230PS 7904 DURING CLIMBOUT FROM BHM, AS THE FLAPS WERE RETRACTED TO ZERO DEGREES, THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED. THE CREW OF FLIGHT 2276 FOLLOWED THE QRH, CONTINUED THE FLIGHT TO PHL, AND MADE AN UNEVENTFUL LANDING. THE CREW DID DECLARE AN EMERGENCY AND THE CABIN WAS PREPPED FOR AN EMERGENCY LANDING. PSA MAINTENANCE IN PHL INSPECTED AND OPERATIONALLY CHECKED THE FLAP SYSTEM IAW CRJ 200 FIM 27-50-00. ALL FLAP SYSTEMS CHECKED GOOD AND NO DEFECTS WERE FOUND. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050208001342005020800134EA 2005 2 8 VNAA0502001 120050203A2710 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE AILERONS ILLUMINATED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL05254PS 7935 DURING TAKEOFF ROLL AT PHL THE CREW OF FLIGHT 2470 RECEIVED A CONFIG AILERON WARNING WHEN THE YOKE WAS MOVED FOR CROSSWIND CORRECTION. THE CREW ABORTED THE TAKEOFF AND TAXIED BACK TO THE GATE. PSA MAINTENANCE FOUND THE AILERON TRIM SET OUT OF THE TAKEOFF RANGE. OPERATIONAL CHECKS OF THE AILERON SYSTEM WERE PERFORMED IAW CRJ 200 AMM 27-11-00-710-801. ALL CHECKS WERE GOOD WITH NO DISCREPANCIES FOUND. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050208001382005020800138WP 2005 2 8 AALA20050080 120050203A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21451AA 49477 DTW - OVERHEAD EMERGENCY LIGHTS AT ROWS 29 AND 30 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT ROWS 29 AND 30. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050208001532005020800153SO 2005 2 8 SWIA200514485 120050126A273152991 ACTUATOR EMB 120 EMB120ER 3260203SO ELEVATOR TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07216SW32 32 120285 ELEVATOR TRIM WHEEL MORE FIRM THAN NORMAL TO OPERATE IN FLIGHT. REMOVED AND REPLACED LEFT ELEVATOR TRIM ACTUATOR IAW MM 27-32-02. 2L72 4T RTA31SO 20050208001542005020800154EA 2005 2 8 SWIA200514486 120050130A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07919SW 7657 EMERGENCY LIGHT CEILING AT ROW 5 INOPERATIVE. REPLACED LAMP IAW AMM 33-51-16. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050208001562005020800156NM 2005 2 8 05FDEA00155 120050125A5347S4929148 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 MAIN DECK SEAT TRACK RBL 107 FOUND WITH SCRATCHES AT STA 5-70 TO STA 1531. DAMAGED SEAT TRACK AT MAIN DECK RBL 107, STA 5-70 TO STA 1531 REMOVED AS PER SRM 51-31-01 VOL II. REPAIR SEAT TRACK, FABRICATED AS PER DWG A5A7084 & INSTALLED AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20050208001602005020800160WP 2005 2 8 CALA0500041 120050203A57309936823503 PANEL DOUG DC9 DC982 3022082WP LT WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2735836 49441 INSPECTION FOUND A 2 INCH CRACK IN UPPER TRAILING EDGE PANEL LOCATED FORWARD OF O/B SIDE OF GROUND SPOILER, LEFT UPPER WING, XRS 91.0 TO 111.5. A NEW PANEL WAS INSTALLED IAW SRM 51-30-2. 2L72 4F A6WE 20050208001642005020800164NM 2005 2 8 DLM88050059 120050126A4990 APU DOUG MD88 MD88 3023688NM APU BAY LEAKING A DALAC ABORTED TAKEOFF KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SO27993DL 53345 AFTER TAKEOFF, F/A REPORTED FUMES/SMOKE IN CABIN. COMPLIED WITH QRH CABIN FUMES CLEARED. PERFORMED DUCT BURNOUT OPERATIONS. 2L72 4F RTA6WE 20050208001712005020800171NM 2005 2 8 DL76L050061 120050126A3397UKN WIRE BOEING767 767332 1382001NM P64 PANEL SHORTED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO27184DN 27111 LOOSE WIRE UNDER COCKPIT SUNSHADE BY P6 PANEL CAUSED SPARK WHEN MOVED. CAPPED WIRE ON THE P64 PANEL WHICH ILLUMINATES P6 FLOOD CB PANEL. 2L72 4F RTA1NM 20050208001742005020800174NE 2005 2 8 DL76L050064 220050117A7210PW40603 ENGINE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 2 FAILED A DALAO OTHER O OTHER NRNOT REPORTED 1 SO27189DN56358 25990 724151 DUE NR 1 OP 50103 7TH STG HPC BLADES INSPECTION. REPLACED ENGINE. 2L72 4F4 FRTA1NM E24NE 20050209000072005020900007NM 2005 2 9 05FDEA00260 120050206A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 BARREL NUT BORE NR 30R CORROSION REMOVAL FOUND EXCEEDED LIMITS. CORROSION REMOVED AND REPAIRED PER FEDEX EA 1-5510-81726. 2L73 4F RTA22WE 20050209000092005020900009EU 2005 2 9 05FDEA00261 120050207A5531 RIB AIRBUS310 A310203 3930313EU ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25405FE 237 VERTICAL STAB R&L TIP ATTACH FLANGES CORRODED AROUND HOLES AND UNDER NUT PLATES. REMOVED AND REPLACED RIB FLANGES IAW A310-200 SRM 51-72-10. APPLIED SURFACE PROTECTION IAW A310-200 SRM 51-73-10. 2L72 4F RTA35EU 20050209000692005020900069NM 2005 2 9 SWAA050325 120050205A25606547661 LATCH BOEING737 7372H4 138448CNM ESCAPE ROPE DOORBROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29096SW 23055 DURING SCHEDULED A1 CHECK, FOUND F/O ESCAPE ROPE DOOR LATCH BROKEN. REMOVED AND REPLACED LATCH PER MM. 2L72 4F A16WE 20050209000712005020900071NM 2005 2 9 SWAA050327 120050206A335065C34691 LIGHT BOEING737 7373H4 1384600NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED A2 CHECK, FOUND EMERGENCY EXIT LIGHT HOUSING AT ROW 1 DEF, CRACKED. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2L72 4F RTA16WE 20050209000742005020900074WP 2005 2 9 AALA20050074 120050130A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW2176202 53292 ORD - FIRST CLASS CABIN CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK OVER SEAT ROW DEF IN FIRST CLASS FOR CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050209000772005020900077EA 2005 2 9 05033677 120050202A2923848847 PUMP CNDAIRCL600 CL6002B19 1900309EA HYDRAULIC SYS CRACKED A VTZAO OTHER KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 EA27677BR 7652 HYDRAULIC SYSTEM NR 3 LOST NEARLY ALL FLUID AFTER NORMAL LANDING. A/C WAS TUGGED BACK TO GATE. MX FOUND CRACKED FITTING ON AFT END OF ACMP PUMP. REMOVED AND REPLACED PUMP. 2L72 4F RTA21EA 20050209000792005020900079EA 2005 2 9 COMA0570012 120050201A53106705110471 BEAM CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01374CA5175 10090 TRANSVERSE BEAM AT FS 280 FROM LBL 36 TO RBL 36 IS CORRODED ALONG THE UPPER AND LOWER EDGES. REPLACED THE TRANSVERSE BEAM AT FS 280 IAW BOMBARDIER AEROSPACE REO 670-52-11-047, BRAS EO 610R-53-5930 AND CRJ 700 SRM 51-42-06-001 AO1. 2L72 4F RTA21EA 20050209000822005020900082WP 2005 2 9 ABXA050028 120050131A531599581861 FLOORBEAM DOUG DC9 DC941 302207NWP AFT CARGO CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23971AX 47497 FLOORBEAM CORRODED ON LOWER FLANGE STA 1013 AT CARGO DOOR UPLATCH BRACKET. REPAIRED IAW DC-9 SSRM K07411. 2L72 4F A6WE 20050209000882005020900088NM 2005 2 9 SWAA050212 120050126A143018A80101 BOLT BOEING737 7373H4 1384600NM LT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29372SW 26599 DURING SCHEDULED C4 CHECK, LT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT TAB HARDWARE PER MM. 2L72 4F RTA16WE 20050209000912005020900091NM 2005 2 9 SWAA050216 120050126A53406547979 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29602SW 27953 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 941, RBL 56, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB PER SRM. 2L72 4F RTA16WE 20050209000952005020900095EA 2005 2 9 050387053 120050207A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27705BR 7470 C-CHECK FINDING: FS 484 AT RBL 9 INTERCOSTAL CRACKED IN THE RADIUS. 2L72 4F RTA21EA 20050209000982005020900098EA 2005 2 9 05035655 120050204A3240 HANDLE CNDAIRCL600 CL6002B19 1900309EA PARKING BRAKE LACK OF LUBE A VTZAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA27655BR 7457 TWO ABORTED TAKEOFFS FOR RED EICAS 1 BRAKE MSG FOLLOWED BY CONFIG BRAKE WARNING. MX FOUND PARKING BRAKE HANDLE STICKING IN THE UP POSITION INTERMITTENTLY. LUBED PARK BRAKE HANDLE. 2L72 4F RTA21EA 20050209001002005020900100EA 2005 2 9 SWIA200514434 120050123A3520 OXYGEN MASK CNDAIRCL600 CL6002B19 1900309EA ROWS 8 A&B DEPLOYED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07439SW 7578 THE O2 MASKS FELL, ROWS 8A & B. SECURED O2 MASKS AT 8A & B. 2L72 4F RTA21EA 20050209001042005020900104NM 2005 2 9 AWXA200500171 120050124A5315654581211 FLOORBEAM BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 MCN - MAJOR REPAIR - DURING C-16 CHECK A .5 INCH CRACK WAS FOUND IN ANGLE ON FORWARD SIDE OF FLOORBEAM AT BS 328, LBL 26. MAINTENANCE REMOVED CRACKED ANGLE AT BS 328, LBL 26; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 65-45812; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050209001072005020900107WP 2005 2 9 0500159985 120050202A5753 STRINGER DOUG DC9 DC932 3022066WP TE FLAP CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01985US 47479 DURING H-CHECK FOUND CRACK IN RT FLAP LEADING EDGE STRINGER. REPAIRED PER EA 99-201832. 2L72 4F A6WE 20050209001092005020900109NM 2005 2 9 0500125523 120050121A5347 SEAT TRACK BOEING757 757251 1384970NM FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01523US 23617 DURING H-CHECK FOUND CORROSION ON SEAT TRACK AT BS 1640 LBL 24 AND 45.5. REPAIRED PER EA 55-20262. 2L72 4F RTA2NM 20050209001132005020900113EA 2005 2 9 MASA200500003 120050102A3350 SIGN CNDAIRCL600 CL6002B19 1900309EA EMERGENCY EXIT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0777302 7302 CREW REPORTED THAT TWO ADJACENT EMERGENCY FLOOR PROXIMITY LIGHT STRIPS WERE INOP AND THAT THE RIGHT OVERWING EXIT EMERGENCY EXIT SIGN WAS INOP. MAINTENANCE RESECURED THE TWO STRIPS AND OPS CHECKED GOOD AND THE OVERWING EXIT SIGN OPS CHECKED GOOD AS WELL. 2L72 4F RTA21EA 20050209001532005020900153CE 2005 2 9 DXTA200500565 120050129A3230 CABLE CESSNA750 750 2076810CE MLG OUT OF RIG E DXTAO OTHER E VIBRATION/BUFFET CRCRUISE 1 GL07900QS 7500123 A LOUD BANG WAS HEARD IN THE NOSE COMPARTMENT, FELT LIKE NOSE GEAR WAS TRYING TO CYCLE UP AND DOWN, NO VISUAL INDICATION IN FLIGHT DECK. FOUND NOSE GEAR FREE FALL CABLE TENSION HIGH, HOLDING BACK UPLOCK ABOUT .125 INCH. RIGGED SWITCH, C/W GEAR SWING, OPS CHECKED GOOD IAW 750 MM CH 32-30-05. 2L72 4J RTT00007WI 20050209001572005020900157EU 2005 2 9 DJFA2005053 120050125A213310327813 OUTFLOW VALVE BRAERODH125 BAE125800A 1500285EU LEFT OPEN E DJFAB EMER. DESCENT J WARNING INDICATION CLCLIMB 1 EA23816CW 258016 CREW REPORTED, WHILE ON A TEST FLIGHT FOR A REQUIRED AOA SYSTEM TEST, CLIMBING THROUGH FL290 A LOUD BANG WAS HEARD COMING FROM THE LEFT FORWARD FUSELAGE AREA. THE CABIN VSI RATE NEEDLE WAS PEGGED AT +2500 FPM. OXYGEN MASKS WERE DONNED AND AN EMERGENCY WAS DECLARED. DURING EMERGENCY DESCENT AIRCRAFT WAS CLEARED TO 10,000 FT. AIRCRAFT LANDED AT KDAL WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT OUTFLOW / SAFETY VALVE, FLOW CONTROL VALVE, AND THE NR 1 MIXING VALVE. TEST FLIGHT WAS SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA3EU 20050209001612005020900161NM 2005 2 9 0500145523 120050125A5754 SKIN BOEING757 757251 1384970NM NR 9 SLAT CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01523US 23617 DURING H-CHECK FOUND CRACKED COVE SKIN PANELS AT NR 9 LEADING EDGE SLAT OUTBOARD DRIVE TRACK. REPAIRED PER EA 55-202250. 2L72 4F RTA2NM 20050209001632005020900163CE 2005 2 9 DXTA200500568 120050131A3260 WARNING LIGHT CESSNA750 750 2076810CE NLG MALFUNCTIONED E DXTAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL07941QS 7500141 LANDING GEAR RED UNLOCK LIGHT STAYED ILLUMINATED AFTER GEAR RETRACTION. AUDIBLE CYCLING NOTED. WIND NOISE LOUDER THEN NORMAL UPON RETRACTION. NOSE GEAR LIGHT SEEMED TO TAKE LONGER THAN NORMAL ON EXTENSION. ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20050209001682005020900168SO 2005 2 9 RAIA00502001 120050201A7930AC3085235 O-RING EMB 145 EMB145LR 3260212SO NR 1 ENGINE LEAKING A RAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03843HK 14500822 STL - IN FLIGHT LOW OIL PRESSURE AND OIL QUANTITY NR 1 ENGINE. COMPLETE CHECKLIST PERFORMED PRECAUTIONARY SHUTDOWN. MAINTENANCE INSPECTED AND FOUND OIL FILTER O-RING BROKEN. REMOVED AND REPLACED OIL FILTER HOUSING O-RING. 2L72 4T RTT00011AT 20050209001732005020900173CE 2005 2 9 DXTA200500578 120050204A3240215671 BRAKE CESSNA750 750 2076810CE MLG SMOKE E DXTAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07919QS1260 7500224 DURING TAXI AND LANDING NOTICED BRAKES WERE VERY STICKY. ALSO AFTER PARKING NOTICED THE RIGHT SIDE MAINS, INBOARD AND OUTBOARD WERE SMOKING FOR UP TO 40 MINUTES AFTER PARKING. TROUBLESHOT BRAKE SYSTEM, REMOVED AND REPLACED NR 3 & NR 4 MLG BRAKE ASSEMBLIES. OPS AND LEAK CHECK GOOD IAW CE750 MM 32-42-00. 2L72 4J RTT00007WI 20050209001832005020900183EU 2005 2 9 DHL2005367001 120050130A3020 VALVE AIRBUS300 A300B4203 3930306EU ANTI ICE SYS FAILED A DHLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01367DH 265 NACELLE ANTI-ICE VALVE ON ENGINE NR 1 DISAGREEMENT LIGHT ILLUMINATED. REPLACED NR 1 NACELLE ANTI-ICE VALVE PER AMM 30-21-11, OPS CHECK NORMAL. 2L72 4F RTA35EU 20050209001892005020900189WP 2005 2 9 UPS05843855 120050104A5712 RIB DOUG DC8 DC873F 302199FWP LEFT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01868UP 45968 INSPECTION TYPE:C3 RIB CRACKED AT UPPER END, LT WING STA XFS 828.75. STOP DRILLED CRACK AND NDT VERIFIED PER NDT/SPM06-10-01.001. FAB DOUBLER AND FILLER FOM SHT7075T6-.050, TREATED, PRIMED & INSTALLED SAME REF SRM 57-3-0 FIG 20, 57-2-0 FIG 2, 51-1-8, 51-1-21, 51-1-20D, 57-3-3 FIG 7. 2L74 4F RT4A25 20050209001912005020900191EA 2005 2 9 SWIA200514473 120050106A5320 SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07438SW 7574 AFT EQUIPMENT COMPARTMENT ACM SUPPORT STRUCTURE HAS A CRACKED SUPPORT FRAME. ITEM FOUND AT C-CHECK INSPECTION. REPLACED SUPPORT FRAME IAW CRJ SRM 51-42-06. 2L72 4F RTA21EA 20050209001932005020900193EA 2005 2 9 SWIA200514475 120050122A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07954SW 7815 FS 280 RT FLOORBEAM RLB 9.0 OUTBOARD ATTACH ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-23-00, 51-42-21, 51-21-11. 2L72 4F RTA21EA 20050209001972005020900197EA 2005 2 9 SWIA200514437 120050122A2750860D10018 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED LDLANDING 1 NM07937SW 7735 FLAPS FAILED AT 0 WHEN SELECTED DOWN FOR LANDING. REPLACED FECU PER 27-51-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050209002002005020900200EA 2005 2 9 05023651 120050123A2611PU90421R3 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA LAVATORY DEFECTIVE A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27651BR 7426 TOILET SMOKE EICAS MESSAGE. INSPECTED LAV LIGHTS, PACK COALESCER BAGS AND PERFORMED RUNS. NO DEFECT NOTED. REMOVED AND REPLACED SMOKE DETECTOR. 2L72 4F RTA21EA 20050209002022005020900202WP 2005 2 9 DHL2005807001 120050119A27603719596502 CRANK ASSY DOUG DC8 DC873F 302199FWP SPOILERS BROKEN A DHLAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SO01807DH 45990 RUDDER NEEDS CONSTANT TRIM CHANGES WITH SPEED AND FLAP CHANGES. A MAXIMUM OF FOUR UNITS OF RIGHT RUDDER TRIM IS REQUIRED DURING APPROACH WITH FLAPS DOWN, TO ZERO TRIM ON RUDDER WITH FLAPS UP. FOUND TWO CRANKS BROKEN ON RIGHT WING GROUND SPOILER. REMOVED AND REPLACED CRANKS P/N 3719596-502 IAW MM 27-60-0. TESTED SPOILERS, OPERATION OK. 2L74 4F RT4A25 20050209002042005020900204NM 2005 2 9 2005F00014 120050114A5343651621578 BEAM BOEING727 7272M7 138407SNM MLG GOUGED A DHLAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01750DH 21951 RIGHT WING MAIN LANDING GEAR SUPPORT BEAM GOUGED AND CORROSION. 2L73 4F A3WE 20050210000762005021000076NE 2005 2 10 HALA0500007 220050102A7200 ENGINE BOEING767 76733A 1385209NM PWA 4060 PW4060 52119NE NR 2 SURGES A HALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 WP13593HA 33424 729137 FLT 22 - HNL - PER ACARS REPORT NR 2 ENGINE SURGE OCCURRED, T/O POWER AT 1.40 EPR. ENGINE RECOVERED IN 4 SECS. ENGINE CHANGE IN WORK. (M) 2L72 4F4 FRTA1NM E24NE 20050210001232005021000123NM 2005 2 10 DLM88050073 120050201A53305911401179 SKIN DOUG MD88 MD88 3023688NM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27912DL 49543 FUSELAGE SKIN BUSHED ADJACENT TO THE AIRSTAIR DOOR CUTOUT AT TWO LOCATIONS BETWEEN LONGERONS 21L AND 22L. REPAIRED I/A/W ERA 096251-14. 2L72 4F RTA6WE 20050210001242005021000124NM 2005 2 10 DLM88050084 120050203A5330 ATTACH ANGLE DOUG MD88 MD88 3023688NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27938DL 49811 FS 1422 VERTICAL STAB TO FUSELAGE INTERFACE: CRACK REPAIR. THE LT AND RT ATTACH ANGLES FOR THE INTERFACE BETWEEN THE VERTICAL STABILIZER AND THE FUSELAGE WERE FOUND CRACKED. THE UNDERLYING SKIN ON THE RT SIDE AT FS 1422 WAS ALSO FOUND CRACKED. THE ANGLES WERE REPAIRED PER DAC S/B DC9-53-223 AND THE SKIN WAS REPAIRED WITH A TITANIUM DOUBLER PER ER/A 096670-14AD. 2L72 4F RTA6WE 20050210001302005021000130NM 2005 2 10 AWXA200500155 120050105A534069366001 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 MCN - MAJOR REPAIR - DURING C-18 CHECK, A 1/4 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT BS 277, STR 10 RT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 277, STR 10 RT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-36600; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050210001322005021000132NM 2005 2 10 AWXA200500157 120050112A532069165096 ANGLE BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 MCN - MAJOR REPAIR - DURING C-18 CHECK A 1/4 INCH CRACK WAS FOUND IN ANGLE AT BS 349, LOWER SIDE OF STR 16 LT. MAINTENANCE REMOVED CRACKED ANGLE AT BS 349, STR 16 LEFT; FABRICATED A NEW REPLACEMENT ANGLE; INSTALLED REPAIR PART IAW ER 03-5300-05028-ES3. 2L72 4F RTA16WE 20050210001332005021000133NM 2005 2 10 AWXA200500158 120050112A534069265552 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 MCN - MAJOR REPAIR - DURING C-18 CHECK A 3/16 INCH CRACK WAS FOUND IN ATTACH CLIP AT BS 349, STR 16 LEFT. MAINTENANCE REMOVED CRACKED ATTACH CLIP AT BS 349, STR 16 LEFT; FABRICATED A NEW REPLACEMENT CLIP; INSTALLED REPAIR PART IAW ER 03-5300-05028-ES3. 2L72 4F RTA16WE 20050208001352005020800135EA 2005 2 8 05038681 120050207A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCONNECTED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27681BR 7680 EMERGENCY FLOOR TRACK LIGHTING INOP. RECONNECTED POWER LEADS. OPS CHECK GOOD. 2L72 4F RTA21EA 20050208001362005020800136EA 2005 2 8 SWIA200514490 120050129A274170609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07411SW32 32 7067 MACH TRIM MESSAGE (AMBER) WHEN F/O USES YOKE SWITCH. REPLACED PITCH TRIM SWITCH IAW 27-41-05. REPLACED HSTCU IAW 27-41-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050208001372005020800137NM 2005 2 8 AT0500006 120050204A3520 OXYGEN MASK BOEING737 73776N 13844CHNM CABIN DEPLOYED A ZZDAO OTHER N FALSE WARNING CLCLIMB 1 SO15176AT 32654 VARIOUS O2 MASKS DROPPED, GENERATORS WERE NOT ACTIVIATED CABIN ALTITUDE STEADY AT 7000 FT. RESTOWED ALL O2 MASKS, VERIFIED O2 GEN NOT DISCHARGED AS PER MM 35-22-31. 2L72 4F RTA16WE 20050208001402005020800140EA 2005 2 8 050387052 120050207A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27705BR 7470 FS 484 AT RBL 36 & LBL 36 INTERCOSTALS CRACKED IN THE RADIUS. 2L72 4F RTA21EA 20050208001482005020800148EA 2005 2 8 SWIA200514480 120050130A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07937SW 7735 NR 2 CEILING LEVEL EMERGENCY FLOODLIGHT INOPERATIVE. RELAMPED NR 2 CEILING LEVEL EMERGENCY LIGHT, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050208001552005020800155EA 2005 2 8 COMA0560102 120050130A2841 INDICATOR CNDAIRCL600 CL6002B19 1900309EA FUEL QTY ERRATIC A COMAO OTHER N FALSE WARNING CRCRUISE 1 SO01798CA 7348 FLIGHT 5483 LEFT WING FUEL QUANTITY INDICATION IS ERRATIC. DEFER MAINT PER MEL. 2L72 4F RTA21EA 20050208001582005020800158GL 2005 2 8 P5CAO501313 220050203A753279027014 BLEED VALVE BOEING747 74746NF 13848BTNM GE CF6 CF680C2* GL NR 2 ENGINE DEFECTIVE A P5CAO OTHER J WARNING INDICATION CRCRUISE 1 EA15451PA 30809 706214 NR 2 ENGINE BLEED EICAS MESSAGE. REMOVED AND REPLACED NR 2 PRV PER 36-11-19. OPS CHECK NORMAL. 2L74 4F4 FRTA20WE E23EA 20050208001862005020800186NM 2005 2 8 DL767050067 120050128A4920 ENGINE BOEING767 767232 1385132NM GE CF6 CF680 30025NE APU FAILED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO27110DL19821 22222 P1848 WHILE RUNNING APU ON GND WITH PACKS ON MTC NOTICED SMOKE IN THE CABIN AND SMOKE OUT OF APU EXHAUST. FOUND APU COMPRESSOR OUTLET DRIPPING OIL. REPLACED APU. 2L72 4F4 FRTA1NM E13NE 20050209000042005020900004NM 2005 2 9 05FDEA00258 120050206A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 MAIN DECK SEAT TRACK LBL 107 CORRODED AT STA 1966. REMOVED AND REPLACED WITH NEW SEAT TRACK FROM STA 1531 TO STA 2007 LBL 107 AS PER SRM 51-33-01 VOL II AND SRM 51-35-01 VOL II. 2L73 4F RTA22WE 20050209000062005020900006WP 2005 2 9 05FDEA00252 120050205A5753ARC2290 SPAR DOUG DC10 DC1030F 3023504WP ZONE 500 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25304FE 46992 LEFT HAND INBOARD FLAP WEDGE UPPER FORWARD ATTACH POINT AT OUTBOARD EDGE OF PANEL FIFTH (5) HOLE IS ELONGATED. FABRICATED AND INSTALLED BUSHING IAW FEDEX EA 8-5710-83968, WINGS- LEFT HAND INBOARD FLAP, INBOARD FLAP WEDGE OVERSIZE BOLT HOLE- REPAIR, AND DC10 SRM 51-39-01 VOL 1 AND 51-35-01 VOL II. 2L73 4F RTA22WE 20050209000082005020900008WP 2005 2 9 05FDEA00253 120050205A5410AUB71385 SUPPORT FITTING DOUG DC10 DC1010 3022110WP ZONE 400 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25395FE 46629 NR 1 PYLON, STATION YN256, MOUNT BRACKET FOR LEFT AND RIGHT THRUST REVERSER ACTUATORS, OPEN/CLOSE BEARING WORN AND GOUGED. COMPLIED WITH FEDEX EA 8-5450-83973, NACELLES/PYLON - NR 1 PYLON FAN REVERSER JACK SCREW SUPPORT FITTING GOUGED - REPAIR, REMOVED AND REPLACED LEFT HAND AND RIGHT HAND BEARING IAW BOEING SOPM 20-50-03. 2L73 4F A22WE 20050209000112005020900011EU 2005 2 9 05FDEA00154 120050125A78303205227 PILOT VALVE AIRBUS300 A300F4605R 3930327EU THRUST REVERSER MALFUNCTIONED A FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25664FE 768 AFTER MOMENTARY RUNUP OF 60 PERCENT N1, APPLIED TOGA LEVERS & STANDARD POWER SET. ECAM SHOWED NR 1 THRUST REVERSER PRESSURIZED. REJECTED T/O AT 60 KNOTS. PREVIOUS WRITE-UP ON THRUST REVERSER. MEL 25JAN05. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A CATEGORY: C EXPIRATION: 04FEB05. REMOVED AND REPLACED NR 1 T/R DIRECTIONAL PILOT PRESSURE VALVE IAW M/M 78-31-06-2-F LEAK CHECK NORMAL AND OPS NORMAL. 2L72 4F RTA35EU 20050209000132005020900013EU 2005 2 9 05FDEA00208 120050201A7120 MOUNT AIRBUS310 A310203 3930313EU ZONE 400 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25405FE 237 NR 1 ENGINE PYLON FWD ENGINE MOUNT FITTING HAS CORROSION ON MOUNTING FACE AND AROUND MOUNTING HOLES UPPER SIDE. REMOVED CORROSION FROM MOUNT FACE IAW A310-200 SRM 51-74-10, FOUND TO BE WITHIN LIMITS A310-200 SRM 54-51-81 FIG 104. SPOT-FACED UPPER AFT I/B & O/B HOLES IAW A310-200 SRM 51-11-80. FOUND AFT O/B HOLE TO BE WITHIN LIMITS IAW A310-200 SRM 54-51-81 FIG 104 SHT 1. FOUND AFT I/B HOLE BEYOND LIMITS A310-200 SRM 54-51-81 FIG 104 SHT 1. AFT I/B HOLE IS ACCEPTABLE IAW FEDEX EA 6-5450-85609 AND AIRBUS INTERIM RAS 034934/010/2005. PERFORMED DYE PENETRANT INSPECTION IAW A310-200 NDT 51-91-00. NO CRACKS NOTED. APPLIED CADMIUM PLATING AND HI-TEMP PLATING IAW A310-200 SRM 51-75-10. 2L72 4F RTA35EU 20050209000152005020900015NM 2005 2 9 QXEA200500147 120050131A242011522183 GENERATOR BOMBDRDHC8 DHC8401 1390041NM ZONE 100 INOPERATIVE A QXEAO OTHER H ELECT. POWER LOSS-50 PC CLCLIMB 1 NM09403QX9139 4201 4037 NR 1 AC GEN CAUTION LIGHT ON CLIMBOUT. RECYCLED NR 1 AC GEN SWITCH CAUTION LIGHT REMAINED ILLUMINATED. LEFT SWITCH IN OFF POSITION PER EMERGENCY CHECKLIST. MAINTENANCE INTERROGATED EPCU AND FOUND FAULT CODE 27. REPLACED NR 1 AC GCU, NO HELP. REPLACED NR 1 AC GEN. PERFORMED OPERATIONAL TEST OF THE VARIABLE FREQUENCY GEN SYSTEM, TESTED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050209000162005020900016NM 2005 2 9 05FDEA00169 120050125A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25603FE 48459 CABIN SEAT TRACK DAMAGED AT STA Y = 1090, X = -48. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE 1, VOLUME I. 2L73 4F RTA22WE 20050209000242005020900024EA 2005 2 9 050327033 120050201A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27703BR 7467 INTERCOSTAL CRACKED ON INBOARD SIDE AT FS 484 LEFT. 2L72 4F RTA21EA 20050209000252005020900025EA 2005 2 9 05034626 120050203A3230 TORQUE LINK CNDAIRCL600 CL6002B19 1900309EA NLG MISINSTALLED A VTZAB EMER. DESCENT WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 EA27626BR 7225 EVENT SUMMARY STATED UNSAFE NOSE GEAR UP INDICATION. CREW FOLLOWED QRH. EMERGENCY DECLARED. SUSPECT TORQUE LINKS NOT PROPERLY INSTALLED. INSPECTED NLG. PERFORMED NLG SWING. NO DEFECTS NOTED. 2L72 4F RTA21EA 20050209000312005020900031WP 2005 2 9 DHL2004809514 120050103A5310 CROSSBEAM DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01809DH91189 46047 AFT ACCY COMPT CROSS BEAM CORRODED STA 1680.000 RBL 12 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 51-2-1 FIG 1 (SHEET 7, 12), TR 51-130. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. CUT OUT DAMAGED SECTION IAW SRM 51-2-1 FIG 1 (SHEET 7, 12). FABRICATED FILLER (AL7075T6 0.100) REPAIR ANGLE (EXTRUSION LS4339 0.170) IAW SRM 51-2-1 FIG 1 SHEET 7, 12, SRM 53-7-3 FIG 10. CLEANED, TREATED AND PRIMED AREA, FILLER AND REPAIR ANGLE IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW SRM 51-2-1 FIG 1 (SHEET 7, 12) SRM 51-1-20D PG 9, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20050209000372005020900037EA 2005 2 9 05033653 120050202A2741 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA MACH TRIM FAILED A VTZAO OTHER J WARNING INDICATION APAPPROACH 1 EA277438 7438 STAB & MACH TRIM FAILURE ON APPROACH. RESET HSTCS SYSTEM IAW MM BAS SERVICE LETTER RJ-SL-27-083 SYSTEM. OPS CHECK GOOD. 2L72 4F RTA21EA 20050209000392005020900039NM 2005 2 9 05FDEA00219 120050202A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 MAIN DECK - SEAT TRACK CROWN AREA AT APPROXIMATE STA Y= 1049, X= -8.5 FOUND WORN. SEAT TRACK CUT AND REMOVED FROM EXISTING SPLICE AT STA Y= 1069 AND Y= 1129, X= -8.5 PER SRM 53-70-00 VOLUME I, FIGURE 1. NEW SET TRACK AND REPAIR PARTS FABRICATED AND INSTALLED PER PER SRM 53-70-00 VOLUME I, FIGURE 1. 2L73 4F RTA22WE 20050209000412005020900041NM 2005 2 9 05FDEA00221 120050202A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 MAIN DECK, SEAT TRACK CROWN AREA AT APPROXIMATE STA Y= 1238 TO Y= 1286, X= -47.5 FOUND WORN. CUT AND REMOVED PER SRM 53-70-00 VOLUME I, FIGURE 1. NEW SEAT TRACK AND REPAIR PARTS FABRICATED AND INSTALLED PER SRM 53-70-00 VOLUME I, FIGURE 1. 2L73 4F RTA22WE 20050209000432005020900043SO 2005 2 9 SWIA200514491 120050115A2910 LINE EMB 120 EMB120ER 3260203SO HYD SYSTEM LEAKING A SWIAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 NM07186SW 120034 AFTER GEAR EXTENSION, GREEN HYDRAULIC LOW LEVEL LIGHT, THE GUAGE CONFIRMED ZERO QUANTITY. REPLACED GEAR DOWN HYDRAULIC FLEXIBLE LINE ON RIGHT MAIN GEAR. SERVICED HYDRAULICS TO PROPER LEVEL. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050209000452005020900045 2005 2 9 SWAA050302 420050203A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29646SW 28331 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050209000462005020900046 2005 2 9 SWAA050303 420050203A2565 BOTTLE BOEING737 7375H4 138449DNM L1 DOOR SLIDE LOW A SWAAK NONE O OTHER ININSP/MAINT 1 SW29513SW 0957A 24190 L1 DOOR EVAC SLIDE INDICATION, LOW PRESSURE. REMOVED AND REPLACED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050209000472005020900047NM 2005 2 9 SWAA050304 120050203A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED THRU CHECK, FOUND FUSELAGE SKIN AT BS 500A + 15, ABOVE STRINGER 16R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050209000482005020900048NM 2005 2 9 SWAA050305 120050203A551265C25727 SKIN BOEING737 7373H4 1384600NM HORIZONTAL STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29322SW 23343 DURING SCHEDULED C4 CHECK, FOUND RT AND LT LOWER HORIZONTAL STAB SKIN AT AFT SPAR, STATION 148, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050209000492005020900049NM 2005 2 9 SWAA050306 120050203A52406545871114 DOOR FRAME BOEING737 7373H4 1384600NM FWD SERVICE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29341SW 24091 DURING SCHEDULED C2 CHECK, FOUND FWD SERVICE DOOR LOWER FRAME AFT CORNER CRACKED. REMOVED AND REPLACED FWD SERVICE DOOR PER MM. 2L72 4F RTA16WE 20050209000502005020900050NM 2005 2 9 SWAA050307 120050203A53116516301 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 DURING SCHEDULED SPV CHECK, FOUND FRAMES AT RT AND LT BS 188, LBL 33 AND RBL 33, CRACKED. REMOVED AND REPLACED FRAME SECTIONS PER SRM. 2L72 4F RTA16WE 20050209000852005020900085WP 2005 2 9 AALA20050081 120050204A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21939AS 49657 SFO - AFT TAIL CONE EMERGENCY LIGHT AND OVERHEAD EMERGENCY AISLE PATH LIGHT INOPERATIVE. REPLACED TWO EACH BATTERY PACKS ABOVE RIGHT HAND AFT LAV FOR TAIL CONE EMERGENCY LIGHT AND OVERHEAD EMERGENCY AISLE PATH LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050209000862005020900086WP 2005 2 9 AALA20050084 120050204A3350 SOCKET DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21266AA 49291 DFW - FORWARD EMERGENCY ESCAPE PATH LIGHT AT SEAT 7D INOPERATIVE. REPLACED SOCKET FOR FORWARD EMERGENCY ESCAPE PATH LIGHT AT SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050209000872005020900087 2005 2 9 SWAA050211 420050126A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR DEPLOYED A SWAAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW29611SW 27697 L1 DOOR EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050209000892005020900089NM 2005 2 9 SWAA050213 120050126A3350101073 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29372SW 26599 DURING SCHEDULED C4 CHECK, FOUND AFT SERVICE DOOR LOWER EMERGENCY EXIT LIGHT LENS, MISSING. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20050209001522005020900152NM 2005 2 9 DXTA200500564 120050128A3233C242570021 ACTUATOR AMD FALC50FALCON2000 2730170NM MLG MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07281QS1204 81 AFTER GEAR RETRACTION LEFT GEAR RED LIGHT INDICATOR DID NOT GO OUT. INSPECTION AFTER LANDING, GEAR DOOR WAS CLOSED BUT RED LIGHT REMAINED ON. REMOVED AND REPLACED THE LT MLG DOOR UPLOCK WITH A SERVICEABLE -REPAIRED- UNIT PER THE F-2000 M/M 32-300. ALL CHECKS WERE SATISFACTORY; NO DEFECTS WERE NOTED AT THIS TIME. 2K73 4F RTA50NM 20050210000012005021000001EA 2005 2 10 A6WA200540012 120050107A5310 PLUG CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31411ZW 7569 MWC - 170 PANEL 131AL HAS DAMAGED FREEZE PLUG AT NR 2 IN CLOCKWISE POSITION, EXCEEDS DIAMETER OF .343 INCH PER BOMBARDIER REO 601R-53-11-162. (M) 2L72 4F RTA21EA 20050210000112005021000011EA 2005 2 10 A6WA200540008 120050104A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31411ZW 7569 FOUND RIGHT FS 621 ANGLE IS CRACKED. REPAIRED RIGHT FS 621 ANGLE IAW BOMBARDIER REO 601R-53-61-117 REV B BY INSTALLING REPAIR ANGLE. (M) 2L72 4F RTA21EA 20050210000142005021000014EA 2005 2 10 A6WA200540001 120050102A215078279015 ACM CNDAIRCL600 CL6002B19 1900309EA LEFT ODOR A A6WAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL31415AW 7593 SMOKE IN CABIN ASSOCIATED WITH APU BLEED AIR HAZE IN COCKPIT AND CABIN. REMOVED AND REPLACED LEFT AIR CYCLE MACHINE, COMPLIED WITH OPS CHECK IAW CRJ AMM 21-51-10, NO SMOKE SMELL NOTED. (M) 2L72 4F RTA21EA 20050210000642005021000064 2005 2 10 A6WA200560001 420050103A2565 BOTTLE BAC 146 146200A 1500266EU ESCAPE SLIDE LOW A A6WAK NONE O OTHER ININSP/MAINT 1 GL31608AW 0123 E2049 FORWARD PAX DOOR ESCAPE SLIDE PRESSURE GAUGE NEEDLE IS IN THE NO-GO AREA. MAINTENANCE REMOVED AND REPLACED EVACUATION. (M) 2H74 4F A49EU 20050210001102005021000110EA 2005 2 10 A6WA200540011 120050104A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31411ZW 7569 FOUND LEFT FS 621 ANGLE IS CRACKED. REPAIRED LEFT FS 621 ANGLE IAW BOMBARDIER, INC REC 601R-53-61-117 REV B B4 INSTALLING REPAIR ANGLE. (M) 2L72 4F RTA21EA 20050210001222005021000122NM 2005 2 10 AWXA200500154 120050105A575465C266851 WEDGE BOEING737 7373G7 1384595NM SLATS DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 MCN - MAJOR REPAIR - DURING C-18 CHECK, FOUND THE A PREVIOUS REPAIR ON UPPER INBOARD END OF NR 4 SLAT WEDGE DELAMINATED BETWEEN SLAT STA 12.25 AND 16.25. MAINTENANCE REMOVED DAMAGED SKIN ON UPPER INBOARD END OF NR 4 SLAT WEDGE; FABRICATED A FILLER AND REPAIR DOUBLER; BONDED REPAIR PARTS TO SLAT WEDGE IAW B737-300 SRM 51-70-10, FIG 31. 2L72 4F RTA16WE 20050210001252005021000125EA 2005 2 10 05636028 120050128A2613 OVERHEAT LOOP CNDAIRCL600 CL6002B19 1900309EA ENGINE MALFUNCTIONED A VTZAE ENGINE SHUTDOWN N FALSE WARNING APAPPROACH 1 EA27636BR 7307 EVENT SUMMARY STATED ENG SHUTDOWN DURING FLIGHT. REMOVED AND REPLACED LT 14TH STAGE OVERHEAT LOOP REF 26-12-00. OPS CHECK GOOD AT THIS TIME. 2L72 4F RTA21EA 20050210001272005021000127GL 2005 2 10 C2XA05IA017 220050201A7200AE3007A1P ENGINE EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL LEFT DAMAGED A C2XAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 SW27139646865 6865 145123 CAE311516 IAH - FLIGHT 2720, THE CREW REPORTED THAT DURING FLIGHT THEY SMELLED A BURNED PACK SMELL WITH NO INDICATION OF SMOKE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20050210001342005021000134NM 2005 2 10 AWXA200500159 120050112A534069265553 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 MCN - MAJOR REPAIR - DURING C-18 CHECK A 1/4 INCH CRACK WAS FOUND IN CLIP AT STR 16 LT BETWEEN BS 348 AND BS 351. MAINTENANCE REMOVED CRACKED CLIP AT STR 16 LT BETWEEN BS 348 AND BS 351 FABRICATED A NEW REPLACEMENT CLIP; INSTALLED REPAIR PART IAW ER 03-5300-05028-ES3. 2L72 4F RTA16WE 20050210001392005021000139EU 2005 2 10 SA05009 120050125A3040 CONTROLLER AIRBUS320 A320214 3930316EU WINDSHIELD HEAT FAILED A USAAH DEACTIVATE SYST/CIRCUITS A FLAME/FIRE CRCRUISE 1 EA19113UW 1141 PHX - FLT 1011 EN-ROUTE, PHL - PHX, DURING FLIGHT, THE FIRST OFFICER'S WINDSCREEN STARTED TO ARC AND DELAMINATE. THE CREW PULLED THE WINDSHIELD HEAT CIRCUIT BREAKER. THE FLIGHT CONTINUED TO PHX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE F/O WINDSHIELD AND WINDOW HEAT CONTROLLER. OK FOR SERVICE. 2L72 4F RTA28NM 20050210001402005021000140EU 2005 2 10 SB05014 220050124A73207139M91G01 PMC BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU NR 2 ENGINE FAULTY A USAAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 EA19516AU2866511379 23702 725104 IAD - FLT1187 - ON CLIMB-OUT FROM IAD, EN ROUTE TO CLT, THE NR 2 ENGINE SURGED AS N1 ROLLED BACK 10 PERCENT AND BEGAN TO FLUCTUATE 4-5 PERCENT THEREAFTER. AIRCRAFT BEGAN TO YAW AND ROLL. AT 11,000 FEET, CREW DISENGAGED AUTOPILOT BUT PROBLEM CONTINUED. FLIGHT RETURNED TO FIELD AT IAD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE INSPECTED ENGINE INLET AND EXHAUST AREA. NO FAULTS FOUND. GROUND RUN OF NR 1 AND NR 2 ENGINE CHECKS NORMAL. RELEASED AIRCRAFT ON MEL 73-7. BOTH PMC'S ARE OFF. MAINTENANCE ACCOMPLISHED TROUBLESHOOTING AND REPLACED THE NR 2 PMC PER MM 73-21-04. OPERATIONAL CHECK GOOD. REMOVED AND CLEARED MEL 73-7. 2L72 4F4 FRTA16WE E21EU 20050210001412005021000141NM 2005 2 10 SB05013 120050123A3397 WIRE BOEING737 737301 1384611NM SEAT ROW 4ABC OPEN A USAAK NONE O OTHER ININSP/MAINT 1 EA19573US 23560 BWI - MAINTENANCE REPORTED THE EMERGENCY LIGHT AT SEAT 4ABC INOPERATIVE. MAINTENANCE REPAIRED AN OPEN IN WIRING AT SEAT ROW 4ABC. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050210001422005021000142NM 2005 2 10 C8GA20050002 120050119A2781 SWITCH BOEING727 727230 1384080NM LE FLAPS MALFUNCTIONED A C8GAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO15357KP 20675 FLT 738 FROM TOL TO MIO, AFTER TAKEOFF, THE LEADING EDGE FLAP AMBER LIGHT ILLUMINATED. AIRCRAFT RETURNED TO TOL AND LANDED WITHOUT INCIDENT. ADJUSTED THE NR 2 LEADING EDGE FLAP POSITION INDICATING SWITCH. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L73 4F A3WE 20050210001482005021000148NM 2005 2 10 UPS05443809 120050107A5313 STRINGER BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 BS 1460 - 1480 S8R STRINGER END FOUND CRACKED. STRINGER REPAIRED PER RS R53-41-35249 AND ENGINEERING FILE NUMBER 747-53-20215. 2L74 4F A20WE 20050210001492005021000149NM 2005 2 10 UPS05443810 120050107A5313 STRINGER BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 BS 1480 - 1500 S8R STRINGER END FOUND CRACKED. STRINGER REPAIRED AS PER HX RS R-53-41-35249 AND ENGINEERING FILE NUMBER: 747-53-20215. 2L74 4F A20WE 20050210001532005021000153NM 2005 2 10 SB05006 120050117A335020121 CHARGER BOEING737 7374B7 1384702NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19437US 24559 MCO - MAINTENANCE REPORTED THE EMERGENCY AISLE LIGHTS AT SEAT ROWS 10 AND 11 AND AT THE AFT LEFT OVERWING INOPERATIVE. MAINTENANCE REMOVED AND REPLACED CHARGER ASSEMBLY NR 3 AND THE BATTERY PACK. OPERATIONAL CHECK NORMAL. 2L72 4F RTA16WE 20050210001562005021000156NM 2005 2 10 SB05012 120050122A3350081691 HOLDER BOEING737 7373B7 1384580NM SEAT 13C FAILED A USAAK NONE O OTHER ININSP/MAINT 1 EA19511AU 23594 PHL - MAINTENANCE REPORTED THE EMERGENCY LIGHT AT SEAT 13C INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE HOLDER AT SEAT 13C. OPERATIONAL CHECK NORMAL. 2L72 4F RTA16WE 20050210001592005021000159EU 2005 2 10 AWXA200500096 120050114A5321D5367180500100 FLOOR PANEL AIRBUS320 A320231 3930325EU FUSELAGE DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28621AW 053 SAL - MAJOR REPAIR - DURING C-04 CHECK FOUND PASSENGER CABIN FLOOR PANEL 262FF DELAMINATED. MAINTENANCE REMOVED DAMAGED AREA OF FLOOR PANEL 262FF, PERFORMED BOND REPAIR IAW A320 SRM 53-02-00, FIG 201. 2L72 4F RTA28NM 20050210001622005021000162NE 2005 2 10 BA05002 220050124A723057A821001 BLADE AIRBUS330 A330323 3930335EU PWA 4168 PW4168A NE RT ENGINE SHINGLED A USAAA UNSCHED LANDING CE F.O.D. VIBRATION/BUFFET CLCLIMB 1 EA19676UW 375 733466 AFTER TAKEOFF, CREW HAD VIBRATION INDICATIONS FROM THE RIGHT ENGINE. THE CREW ALSO REPORTED AIRFRAME VIBRATION. FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE NR 1 FAN BLADE SET (24 TOTAL). DAMAGE DUE TO GROUND INGESTION OF SNOW/SLUSH PRIOR TO TAKEOFF. 2L72 4F4 FRTA46NM 20050210001632005021000163EA 2005 2 10 05027708 120050127A361032156222 SHUTOFF VALVE CNDAIRCL600 CL6002B19 1900309EA RT A/C PACK DEFECTIVE A VTZAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA27708BR 7575 ABORTED TAKEOFF FOR RT PACK OVERPRESSURE. MAINTENANCE REMOVED AND REPLACED PRSOV. 2L72 4F RTA21EA 20050210001642005021000164EU 2005 2 10 AWXA200500097 120050110A5321D5367321100000 FLOOR PANEL AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28621AW 053 SAL - MAJOR REPAIR - DURING C-04 CHECK, CORROSION WAS FOUND ON FACESHEET OF AFT CARGO COMPARTMENT FLOOR PANEL 161AF. MAINTENANCE REMOVED DAMAGED FLOOR PANEL 161AF; FABRICATED A NEW REPLACEMENT FLOOR PANEL; INSTALLED REPLACEMENT PART IAW A320 SRM 53-02-00, FIG 209. 2L72 4F RTA28NM 20050210001652005021000165EU 2005 2 10 AWXA200500098 120050111A5347D53472090003 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28621AW 053 SAL - MAJOR REPAIR - DURING C-04 CHECK, CORROSION WAS FOUND ON SEAT RAIL BEAM ASSEMBLY -Y765 AT FR 64+14". MAINTENANCE REMOVED DAMAGED AREA OF SEAT RAIL UPPER FLANGE -Y765 FROM FS 64 TO FS 65; FABRICATED A REPAIR ANGLE; INSTALLED REPAIR PART IAW ER 26-5341-05020-RC1. 2L72 4F RTA28NM 20050210001752005021000175NM 2005 2 10 AWXA200500151 120050107A532065539711 CHANNEL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 MCN - MAJOR REPAIR - DURING C-18 CHECK, A 1/2 INCH CRACK WAS FOUND IN AFT CARGO DOOR HOLD OPEN BRACKET INTERCOSTAL (CHANNEL) AT BS 795, RBL 18, WL 206. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT BS 795, RBL 18, WL 206; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER DWG 69-53971; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050210001772005021000177NM 2005 2 10 AWXA200500153 120050103A57536546486155 WEDGE BOEING737 7373G7 1384595NM TE FLAPS DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 MCN - MAJOR REPAIR - DURING C-18 CHECK, FOUND THE LT INBOARD MID FLAP WEDGE DELAMINATED AT THE OUTBOARD END BETWEEN WBL 164 AND WBL 168. MAINTENANCE REMOVED DAMAGED SKIN ON LT INBOARD MID FLAP WEDGE; FABRICATED A FILLER AND REPAIR DOUBLER; BONDED REPAIR PARTS TO MID FLAP WEDGE IAW B737-300 SRM 51-70-10, FIG 30. 2L72 4F RTA16WE 20050210001802005021000180NM 2005 2 10 DL76G050085 120050203A4900 BATTERY BOEING767 767332 1382001NM APU OVERHEATED A DALAH DEACTIVATE SYST/CIRCUITS MB OVER TEMP SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO271608 33163 30573 PRIOR TO DEPARTURE BURNED SMELL REPORTED IN THE BACK OF THE CABIN. MTC FOUND THE APU BATTERY HOT. REPLACED BATTERIES AND CHARGER. 2L72 4F RTA1NM 20050211000022005021100002NM 2005 2 11 SB05005 120050115A3397 WIRE BOEING737 737301 1384611NM MID CABIN FAULTY A USAAK NONE O OTHER ININSP/MAINT 1 EA19340US 23237 PHL - MAINTENANCE REPORTED SEVERAL EMERGENCY EXIT ROW LIGHTS INOPERATIVE. MAINTENANCE REPAIRED WIRING. OPERATIONAL CHECK OF EMERGENCY LIGHTS GOOD. 2L72 4F RTA16WE 20050211000032005021100003NM 2005 2 11 SB05016 120050126A3310106180022 LIGHT BOEING737 737301 1384611NM COCKPIT FAILED A USAAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 EA19353US 23556 CLT - FLT1435 - DURING DESCENT INTO CLT FROM ORD, CREW REPORTED SMOKE ENTERING COCKPIT FROM BEHIND FIRST OFFICER "PULL UP" ANNUNCIATOR LIGHT ON FIRST OFFICER'S INSTRUMENT PANEL. ALSO, ALL LIGHTS ASSOCIATED WITH THE LIGHT TEST SWITCH ILLUMINATED. MOVING TEST SWITCH TO DIM POSITION EXTINGUISHED LIGHTS. FOUND CIRCUIT BREAKER SECTION 6 OF INDICATOR LIGHTS (MASTER, DIM) HAD TRIPPED. SMOKE THEN DISSIPATED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE L385 LIGHT ASSEMBLY BELOW THE FIRST OFFICER'S GLARESHIELD. LIGHTS TEST NORMAL. GPWS TESTS NORMAL. 2L72 4F RTA16WE 20050211000042005021100004NM 2005 2 11 AWXA200500161 120050108A5340650163312 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 MCN - MAJOR REPAIR - DURING C-18 CHECK, A 3/16 INCH CRACK WAS FOUND IN CLIP ON FORWARD SIDE OF BS 294, STR 13 LT. MAINTENANCE REMOVED CRACKED CLIP AT BS 294, STR 13 LT; FABRICATED A NEW REPLACEMENT CLIP; INSTALLED REPAIR PART IAW ER 03-5300-05031-SS3. 2L72 4F RTA16WE 20050211000052005021100005NM 2005 2 11 AWXA200500162 120050108A53206517684638 WEB BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 MCN - MAJOR REPAIR - DURING C-18 CHECK A 1/4 INCH CRACK WAS FOUND IN LOWER WEB AT BS 294, STR 12 LT. MAINTENANCE REMOVED CRACKED LOWER WEB AT BS 294, STR 12 LT, AND 2 EACH BRACKETS; FABRICATED A NEW REPLACEMENT WEB AND 2 EACH BRACKETS; INSTALLED REPAIR PARTS IAW ER 03-5300-05031-SS3. 2L72 4F RTA16WE 20050211000082005021100008NM 2005 2 11 AWXA200500165 120050108A5320651768469 ANGLE BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 MCN - MAJOR REPAIR - DURING C-18 CHECK, A 1/4 INCH CRACK WAS FOUND IN ANGLE AT BS 303.9, STR 13 LT. MAINTENANCE REMOVED CRACKED ANGLE AT BS 303.9, STR 13 LT; FABRICATED A NEW REPLACEMENT ANGLE; INSTALLED REPAIR PART IAW ER 03-5300-05031-SS3. 2L72 4F RTA16WE 20050211000092005021100009EA 2005 2 11 05029675 120050129A2410720846D GCU CNDAIRCL600 CL6002B19 1900309EA NR 2 GENERATOR DEFECTIVE A VTZAD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 EA27675BR 7635 GENERATOR 2 TRIPPED ON TAXI OUT. MAINTENANCE REMOVED AND REPLACED GCU. 2L72 4F RTA21EA 20050211000112005021100011SO 2005 2 11 C2XA05SH005 120050126A531514521713005 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716520 145372 SHV - DURING C-CHECK, THE CENTER OMEGA BEAM FS 17-23 IS CORRODED. MAINTENANCE REMOVED AND REPLACED CENTER OMEGA BEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050211000142005021100014NM 2005 2 11 DL75A050076 120050201A5330143N31211 SKIN BOEING757 757212 1384951NM FUSELAGE TOOL DAMAGE A DALAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO27752AT 23128 TOOLING DAMAGE TO THE FUSELAGE SKIN AT STATION 899 AND STR 3L. REPAIRED IAW ERA 096211-14. 2L72 4F RTA2NM 20050211000162005021100016NM 2005 2 11 UPS05443816 120050106A531165B0460011 FRAME BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 FRAME BS 1416 INNER FLANGE CRACKED AT S-22L. M/D FRAME INNER FLANGE REPAIRED AT BS 1416 S-22L AS PER RS : R-53-42-35233 AND ENGINEERING FILE NUMBER : 747-53-20219. 2L74 4F A20WE 20050211000182005021100018NM 2005 2 11 UPS05443832 120050109A532165B1635112 FLOOR PANEL BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 STA 1170 TO 1250, BTN L11 AND R11 FLR METAL PNL SKIN FOUND CORR. METAL FLOOR PANEL REPAIRED AS PER RS R53-20-35251 AND EO B747-5320- 21675-A AND THIS METAL PANEL NEED REPLACEMENT WITHIN 18 MONTHS OR 1000 CYCLES WHICHEVER OCCURS FIRST. CORROSION BLEND OUT DEPTH 0.040 INCH WIDTH 2 INCHES LENGTH 5 INCH OUT OF SRM 53-10-01 FIG 1 LIMIT. 2L74 4F A20WE 20050211000192005021100019NM 2005 2 11 UPS05443833 120050109A532165B1635112 FLOOR PANEL BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 STA 1020 TO 1110, BTN L11" AND R11" FLR METAL PNL SKIN FOUND CORROSION. FLOOR PANEL REPAIRED AS PER RS R53-20-35251 AND EO B747-5320-21675-A AND THIS METAL PANEL NEED REPLACEMENT WITHIN 18 MONTHS OR 1000 CYCLES WHICHEVER OCCURS FIRST. CORROSION BLEND OUT DEPTH 0.004" WIDTH 1" LENGTH 4" WITHIN SRM 53-20-01 FIG 1 LIMITS. 2L74 4F A20WE 20050211000212005021100021NM 2005 2 11 UPS05443841 120050131A2560 BATTERY BOEING747 747212B 1384886NM FLASHLIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01526UP 21937 EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERY, OPS CK GOOD AT THIS TIME. 2L74 4F A20WE 20050211000222005021100022SO 2005 2 11 C2XAO5TY006 120050124A532014521700007 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713936 145025 TYS - DURING A SCHEDULED 4C INSPECTION, THE LT OMEGA BEAM BETWEEN FS 22 AND FS 23 HAS A BLENDED AREA BELOW LIMITS NEXT TO A NUTPLATE. MAINT CUTOUT THE EFFECTED AREA, FAB`D A SPLICE REPAIR FROM A NEW PART AND FAB`D AN INTERNAL ANGLE, DRILL, ALODINED, PRIMED AND INSTALLED IAW EC 5320-01205. REMOVED TOPCAP AND L-PROFILE AT THE REPAIR AREA AND REINSTALL IAW EMB 135/145 SRM 52-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL AT END OF THE C-CHECK. 2L72 4F RTT00011AT 20050211000232005021100023SO 2005 2 11 C2XA05BT008 120050125A272015793101 PRESSURE SWITCH EMB 145 EMB145LR 3260212SO RUDDER FAULTY A C2XAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SW2712540 145537 EWR - CO2514, CREW REPORTED, ON SHORT FINAL, AUTOPILOT DISCONNECTED, YAW DAMPENER FAIL, AND RUDDER SYSTEM NR 1 AND NR 2 FAIL INDICATION, CREW DECLARED AN EMERGENCY AND LANDED UNEVENTFULLY. MAINTENANCE REMOVED AND REPLACED NR 1 AND NR 2 RUDDER PRESSURE SWITCHES. OPS CHECKED GOOD, REQUIRES SYSTEM TEST FLIGHT. FLEW AIRCRAFT AND FOUND TEST FLIGHT SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20050211000242005021100024SO 2005 2 11 C2XA05TY007 120050124A5530KSC357620V BEARING EMB 145 EMB145ER 3260211SO VERTICAL STAB WORN A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716944 145045 TYS DURING A MODIFICATION OF AIRCRAFT, INSPECTION FOUND THE VERTICAL STAB, LEFT HAND SPHERICAL BEARING HAD AXIAL AND LATERAL PLAY. MAINTENANCE REAMED THE THE VERTICAL BEARING HOUSING AND INSTALL NEW BUSHINGS IAW EC5510-01108. ALL WORK WAS ACCOMPLISHED AND OPS CHECKS GOOD. A/C WAS REL AFTER ALL WORK WAS C/W WITH. 2L72 4F RTT00011AT 20050211000282005021100028EU 2005 2 11 AWXA200500128 120050201A3350321430 BATTERY AIRBUS320 A320232 3930326EU ZONE 263 DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28648AW 770 CMH - EEL - DURING 4-DAY CHECK, THE BATTERY PACK AT THE LT AFT EMERGENCY POWER SUPPLY UNIT FAILED TEST. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT LT AFT EMERGENCY POWER SUPPLY UNIT (13WL), OPERATIONAL CHECK TEST GOOD. 2L72 4F RTA28NM 20050211000342005021100034NM 2005 2 11 AWXA200500134 120050120A532065535953 REVEAL BOEING737 7373Q8 1384670NM R1 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK, A 3/4 INCH CRACK WAS FOUND IN R-1 DOOR FORWARD UPPER CORNER REVEAL. MAINTENANCE REMOVED CRACKED REVEAL FROM BS 298 TO BS 306, STR 10 RT TO STR 11 RT, INSTALLED NEW REPLACEMENT PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050211000392005021100039EU 2005 2 11 AWXA200500102 220050130A73209342M30G02 TUBE BOEING737 7373G7 1384595NM CFMINTCFM56 CFM563B2 13802EU NR 2 ENGINE BACKED OUT A AWXAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 WP28160AW 23782 PHX - AIR TURN BACK - FLT 0893 - AFTER TAKEOFF AT PHX EN ROUTE FOR SEA WHILE CLIMBING THROUGH FL 230 THE NR 2 ENGINE SPOOLED DOWN TO IDLE, LEVELED OFF AT FL 240, ALL ENGINE PARAMETERS NORMAL EXCEPT ENGINE AT IDLE AND NO RESPONSE TO THROTTLE MOVEMENT, TURNED BACK TO PHX FOR REPAIR. MAINTENANCE FOUND CDP AIR TUBE THAT SENSES AIR PRESSURE FROM HIGH PRESSURE COMPRESSOR TO MEC COMPLETELY BACKED AT COMPRESSOR SIDE. RECONNECTED TUBE TO COMPRESSOR AND SAFETIED, RAN ENGINE TO TAKEOFF POWER, NO DEFECTS NOTED. 2L72 4F4 FRTA16WE E21EU 20050211000442005021100044 2005 2 11 WRLA2005005 420050125A3457 GPS DOUG DC10 DC1030F 3023504WP GE CF6 CF650C2 30018NE NR 3 MALFUNCTIONED A WRLAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO11304 47928 ITEM: WOA174/25 DAY/LAX AIR TURNBACK DUE TO FAILURE OF NAVIGATION SYSTEM. AFTER TO, NR 3 GPS WORKED BUT WOULD NOT CROSS TALK. AFTER 2:30 MIN CAPT LOST HIS ROLL BAR AND NR 1 GPS WOULD NOT PROVIDE NAV DATA. SHORTLY AFTERWARDS NR 2 GPS HAD ALERT "NAV DATA BASE PROCESSOR FAILED" ALL UNITS BEGAN TO DRIFT UP TO 6.7 MILES AT NAV TRACK GATEWAY REQUIRING AIRCRAFT TO TURN BACK TO KDAY WITH UNRELIABLE NAV SYSTEMS. REMOVED AND REPLACED NR 3 GPS NPU IAW HONEYWELL SYSTEM MM, NO HELP. ENTERED IN DMI M34JA2605-141 PER MEL 34-45. 2L73 4F4 FRTA22WE E23EA 20050211000452005021100045EA 2005 2 11 05028668 120050128A2611 SMOKE CNDAIRCL600 CL6002B19 1900309EA LAVATORY DETECTED A VTZAO OTHER J WARNING INDICATION CLCLIMB 1 EA27668BR 7544 EVENT SUMMARY STATED SMOKE IN LAV INDICATION, RTF. INSP AC RAN PACKS CHECKED LTS IAW 05-50-00. 2L72 4F RTA21EA 20050211000462005021100046NM 2005 2 11 UPS05543842 120050130A3350 LIGHT BOEING757 75724APF 1384969NM EMERGENCY EXIT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01471UP 28842 EMERGENCY LIGHT ON FUSELAGE BELOW CREW ENTRY DOOR IS INOP. ACCOMPLISHED TEST OF EXTERIOR EMERGENCY LIGHT BELOW CREW ENTRY DOOR PER MM 33-51-06-2 LIGHT CK OK. 2L72 4F RTA2NM 20050211000472005021100047WP 2005 2 11 UPS05843846 120050108A53403779978 ATTACH FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01701UP 45938 MAIN CABIN STA 835.5 L18L, FRAME ATTACH FITTING CRACKED. REMOVED AND REPLACED FRAME ATTACH FITTING AT STA 853.5 L18L, IAW SRM 51-1-20D. 2L74 4F RT4A25 20050211000482005021100048WP 2005 2 11 UPS05843847 120050105A7830 FITTING DOUG DC8 DC871F 302199DWP THRUST REVERSER CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01701UP 45938 NR 4 ENG OTBD T/R COWL HAS CRACK (0.625) IN UPPER CORNER FITTING, JUST AFT OF UPPER BLOCKER DOOR. (TRANSLATING COWL) STOP DRILLED CRACK AND INSTALLED TWO STIFFENERS IAW CFM-7830-5209-A AND SRM 51-1-20D. 2L74 4F RT4A25 20050211000492005021100049WP 2005 2 11 UPS05843848 120050112A5753 SUPPORT FITTING DOUG DC8 DC871F 302199DWP FLAP TRACK CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01701UP 45938 RT STA 98 FLAP SUPPORT FITTING (CANOE) HAS CORROSION UNDER FLAP TRACK AREA, O/B SURFACE .025 DEEP I/B SURFACE IS .006 DEEP. UNDERCUT AND REMOVED CORROSION .050 AND FABRICATED AND INSTALLED REPAIR FILLERS PER SB 27-164 PAGE 8. 2L74 4F RT4A25 20050211000512005021100051WP 2005 2 11 UPS05843835 120050108A531337585931 LONGERON DOUG DC8 DC871F 302199DWP L36 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01701UP 45938 LONGERON 36 HAS 1 INCH CRACK ON RT UPPER FLANGE IN RADIUS BETWEEN F/S 1260-1280. REMOVED AND REPLACED DAMAGED LONGERON SECTION IAW DWG 5750322 AND SRM 51-1-20D FROM F/S 1260-1360 L36. 2L74 4F RT4A25 20050211000522005021100052WP 2005 2 11 UPS05843836 120050107A5313 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01701UP 45938 MAIN CABIN LONGERON CRACKED AT STA 1760 L15L. REMOVED DAMAGED SECTION OF LONGERON AND FABRICATED SPLICE AND LONGERON SECTION INSTALLED IAW SRM'S 53-2-2 FIG10, 51-1-21, 53-2-0,51-1-20D AND DC8-53B-OO9-39. 2L74 4F RT4A25 20050211000542005021100054WP 2005 2 11 UPS05843838 120050107A5312 PRESSURE BLKHD DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01701UP 45938 MAIN CABIN, AFT PRESSURE BULKHEAD CRACKED, RBL 50 UPPER SIDE. CUTOUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER, FILLERS AND FINGER DOUBLER IAW SRM'S 53-2-5 FIG 14A, 51-1-21, 51-1-20D AND DWG SRO8530007. 2L74 4F RT4A25 20050211000562005021100056SO 2005 2 11 C2XA05IA013 120050121A3350 CONNECTOR EMB 145 EMB145XR 3260214SO INVERTER DIRTY A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2711121 145683 IAH - FLIGHT 3252, THE CREW REPORTED THAT THE FORWARD EMERGENCY LIGHT IN THE GALLEY WAS INOPERATIVE. MAINTENANCE CLEANED THE INVERTER CONNECTOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THIS PART IS NOT SERIALIZED, AND NO TIMES ARE AVAILABLE 2L72 4F RT 20050211000572005021100057SO 2005 2 11 C2XA05IA014 120050121A33501317 BULB EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT BURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2734110 145658 IAH - FLIGHT 3334, CREW REPORTED AN EMERGENCY LIGHT IN THE CABIN AS BEING INOPERATIVE. MAINTENANCE REPLACED THE LIGHT BULB IN THE AFFECTED LIGHT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20050211000612005021100061NM 2005 2 11 UPS05M43840 120050129A3350 LIGHT DOUG MD11 MD11F 3023600NM COCKPIT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP OVERHEAD COCKPIT EMER LIGHT INOP. RELAMPED, OP CK GOOD IN REF TO MM 33-50-00. 2L73 4F RTA22WE 20050211000622005021100062EU 2005 2 11 AWXA200500090 120050130A3241C202163382D32 CONTROL UNIT AIRBUS320 A320231 3930325EU BRAKE/STEERING FAULTY A AWXAO OTHER J WARNING INDICATION LDLANDING 1 WP28624AW400512846 055 ON LANDING, RECEIVED ECAM MESSAGE "BRAKING/STEERING CONTROL UNIT (BSCU) FAULT CH. 2 INCHES, WHEN CLEARING RUNWAY BRAKES LOCKED UP MOMENTARILY. MAINTENANCE REMOVED AND REPLACED THE BSCU IAW AMM 32-42-34-04, OPERATIONAL CHECK WAS GOOD. COULD NOT DUPLICATE REASON FOR REMOVAL, UNIT WAS TESTED PER CMM 32-47-27, REV. 11 WITH NO FAULTS FOUND. 2L72 4F RTA28NM 20050211000632005021100063EU 2005 2 11 AWXA200500091 120050128A2560P4010021 BATTERY AIRBUS320 A320232 3930326EU ZONE 900 DISCHARGED A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28671AW 2077 ORD - EMERGENCY EQUIPMENT, MAINTENANCE FOUND THE FORWARD GALLEY EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD GALLEY EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050211000652005021100065EU 2005 2 11 AWXA200500093 120050129A335032145410 EPSU AIRBUS320 A320232 3930326EU ZONE 242 FAULTY A AWXAK NONE O OTHER ININSP/MAINT 1 WP28650AW24201 856 LAS - EEL - DURING 8-DAY CHECK FUNCTIONAL TEST OF EMERGENCY LIGHT SYSTEM, RT OVERWING EMERGENCY POWER SUPPLY UNIT (12WL) FAULTED. MAINTENANCE REMOVED AND REPLACED RT OVERWING EMERGENCY POWER SUPPLY UNIT (12WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050211000682005021100068NM 2005 2 11 SB05019 120050130A3097 WIRE BOEING737 7374B7 1384702NM NR 2 P/S PROBE BROKEN A USAAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 EA19448US 24892 PIT - FLT1466 - CREW REPORTED THE FIRST OFFICER'S PITOT STATIC NR 2 AUX STATIC LIGHT ILLUMINATED. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND A BROKEN WIRE ON PITOT STATIC PROBE CONNECTOR. REPAIRED SAME PER MM 30-31-00. SYSTEM CHECKS GOOD. 2L72 4F RTA16WE 20050211000702005021100070NM 2005 2 11 UPS05M43843 120050131A3510 OXYGEN BOTTLE DOUG MD11 MD11F 3023600NM NR 4 LOW A IPXAK NONE O OTHER ININSP/MAINT 1 SO01250UP NR 4 OXYGEN BOTTLE LOW 7.5. REMOVED AND REPLACED NR 4 OXYGEN BOTTLE PER MM 35-11-01, LEAK CK GOOD. 2L73 4F RTA22WE 20050211000712005021100071NM 2005 2 11 SB05004 120050111A3397 WIRE BOEING737 7374B7 1384702NM EMERGENCY LIGHT BROKEN A USAAK NONE O OTHER ININSP/MAINT 1 EA19781AU 25020 CREW REPORTED EXPOSED WIRES IN THE FORWARD COAT CLOSET. MAINTENANCE REPAIRED BROKEN WIRES, FOR EMERGENCY LIGHTS, IN FORWARD COAT CLOSET. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050209001282005020900128EA 2005 2 9 MASA200500009 120050104A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSBURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0717231 7231 CREW REPORTED 1 CEILING ESCAPE LIGHT INOP. THE LIGHT WAS MEL'ED. MAINTENANCE RELAMPED, OPS CHECKED GOOD. 2L72 4F RTA21EA 20050209001292005020900129EA 2005 2 9 MASA200500010 120050104A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSDAMAGED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0777195 7195 THE PILOT REPORTED THE EMERGENCY FLOOR PATH LIGHTING INOP. MAINTENANCE REPAIRED WIRE TO THE FLOOR PATH LIGHTING STRIP, OPS CHECKED GOOD. 2L72 4F RTA21EA 20050209001302005020900130EA 2005 2 9 MASA200500012 120050105A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSBURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0775987 7405 A/C N75987 ON THE RON AND SCHEDULED FOR A ROUTINE CHECK INSPECTION DURING THE WALKAROUND IT WAS DISCOVERED THE RIGHT SIDE FORWARD EXTERIOR EMERGENCY LIGHT NOT ILLUMINATING. MAINTENANCE REPLACED THE LIGHT BULB AND OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050209001312005020900131EA 2005 2 9 MASA200500013 120050105A3350100865 BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07759988029 7336 THE FIRST ROW EMERGENCY EXIT PATH LIGHTING STRIP LIGHT INOP. MAINTENANCE REPLACED THE EMERGENCY LIGHTING POWER SUPPLY AND BATTERY PACK. BATTERY PACK P/N 2013-1A, S/N OFF 61657 TT 498 TC 451. 2L72 4F RTA21EA 20050209001322005020900132NM 2005 2 9 AWXA200500174 120050125A534069353522 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 MCN - MAJOR REPAIR - DURING C-16 CHECK A .1875 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT BS 727D, STR 20 RT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 727D, STR 20 RT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 65C25229; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050209001342005020900134SO 2005 2 9 MASA200500014 120050106A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSBURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07827MJ 145217 A PASSENGER DOOR ENTRY EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LAMP. 2L72 4T RTT00011AT 20050209001352005020900135EA 2005 2 9 MASA200500020 120050107A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSBURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0775993 7372 FORWARD CABIN EMERGENCY FLOOD LIGHT INOP. MAINTENANCE REPLACED THE BULB. 2L72 4F RTA21EA 20050209001372005020900137SO 2005 2 9 MASA200500025 120050109A3350 LIGHT EMB 145 EMB145LR 3260212SO GALLEY DOOR INOPERATIVE A MASAO OTHER O OTHER TXTAXI/GRND HDL 1 SW07828MJ 145218 THE GALLEY DOOR EMERGENCY EXIT LIGHT INOP. WHEN MAINTENANCE ARRIVED THE LIGHT WAS WORKING NORMALLY. A/C DEPARTED WITHOUT FURTHER INCIDENT. 2L72 4T RTT00011AT 20050209001402005020900140SO 2005 2 9 MASA200500062 120050127A3350744425 SIGN EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSINOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07836MJ 145359 AIRCRAFT WAS ON RON AND SCHEDULED FOR A 2 DAY EN ROUTE INSPECTION. DURING THE WALKAROUND IT WAS DISCOVERED THE LEFT HAND ROW 12 SIDEWALL EMERGENCY LIGHT SIGN WAS NOT ILLUMINATING. MAINTENANCE REPLACED THE LIGHT EXIT SIGN. OPERATIONAL CHECK GOOD. 2L72 4T RTT00011AT 20050209001422005020900142SO 2005 2 9 CHQA200500025 120050203A3350 LIGHT EMB 135 EMB135LR 3260305SO CABIN INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11833RP 145687 RIGHT HAND OVERWING EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED THE RIGHT HAND OVERWING EMERGENCY EXIT LIGHT ASSEMBLY IAW EMB 135 MM 33-50-10. OPS CHECK GOOD. 2L72 4F RTT00011AT 20050209001442005020900144NE 2005 2 9 CHQA200500026 220050204A7250AS3217186 RETAINING RING EMB ERJ170ERJ170100LR EU GE CF34 CF348E5 30015NE NR 2 ENGINE MISSING A CHQAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL11645RW 17000064 GEE192146 FLIGHT FROM CURACAO CUR TO FLL FOR AIRCRAFT DELIVERY - AFTER DEPARTING CUR AND CLIMBING TO 38,000 FEET, THE CREW NOTICED THE OIL QUANTITY WAS DIMINISHING ON ENGINE 2. THE OIL PRESSURE BEGAN TO DROP SOON AFTER. THE RIGHT ENGINE WAS SHUTDOWN AND THE AIRCRAFT RETURNED TO CUR FOR AN UNEVENTFUL LANDING. THE OIL LOSS WAS DUE TO THE RETAINING RING P/N AS3217-186 WAS MISSING WHICH HOLDS THE CAP COVER P/N 4117T32P02 ON THE C OIL SUMP. REMOVED AND REPLACED RETAINING RING. OPS CHECK GOOD. 2L74 4F4 FRTA56NM E00063EN 20050209001462005020900146CE 2005 2 9 DXTA200500569 120050131A2730 CONTROL CABLE CESSNA500 560CESSNA 2076750CE ELEVATOR FRAYED E DXTAK NONE O OTHER ININSP/MAINT 1 GL07367QS 5600367 DURING INSPECTION FOUND ELEVATOR PRIMARY FLIGHT CONTROL CABLE FRAYED IN TAIL CONE. PIN BOTH FORE & AFT SECTIONS & USE CABLE BLOCKS TO REMOVE & REPLACE CABLE. PULL OLD CABLE OUT. RUN NEW CABLE. RIG SYSTEM & BRING UP TENSIONS PER CESSNA 560 MM CHAPTER 27-31-00. 2L72 4F RTA22CE 20050209001482005020900148SO 2005 2 9 RAIA00501063 120050117A3246 BEARING EMB 145 EMB145LR 3260212SO NLG WHEEL FAILED A RAIAD RETURN TO BLOCK E VIBRATION/BUFFET TXTAXI/GRND HDL 1 CE03847HK 14500857 PVD - THUMBING NOISE COMING FROM NOSE GEAR, REPORT RIGHT NOSE TIRE ANGLED. MAINTENANCE REMOVED AND REPLACED BOTH NOSE TIRES, INSPECTED AND FOUND NR 2 BEARING FAILURE. 2L72 4T RTT00011AT 20050209001492005020900149EU 2005 2 9 RAIA00501064 120050130A1420 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU AOG SWITCH DIRTY A RAIAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 CE03571HK 41090 JLN - ABORTED TAKEOFF DUE TO CONFIGURATION RED BETA LIGHT, RIGHT STALL ETC. MAINTENANCE CLEANED AND RESECURED LOOSE AOG SWITCH CONNECTOR, OPS CHECK GOOD. 2L72 4T RTA41NM 20050209001502005020900150NM 2005 2 9 DHL2005743510 120050112A5340652427649 STRINGER CLIP BOEING727 727225 1384077NM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01743DH 22438 MAIN CABIN TENSION TIE FITTING HAS CORROSION STA 1183 LBL 63-65 WL 208.1. REMOVED 17L STA 1183 STRINGER END FITTING AND ATTACH ANGLE, DRILLED NEW END FITTING P/N 65-24276-49, FABRICATED NEW CLOSE OUT ANGLE USING .080 7075-0 PO 0003006. ANGLE HEAT TREATED ON PEMCO TRAVELER 763N001000. DRILLED, ALODINED DEBURRED, PRIMED AND INSTALLED STRINGER END FITTING AND CLOSE OUT ANGLE IAW B727 SRM 51-30-5, 51-30-2, 51-10-2. FAB, DRILLED, ALODINED, PRIMED AND INSTALLED STA 1183 LT NEW CLOSE OUT DUST COVER AND 2 ATTACH ANGLES USING 2024T3-020 PO 0430694 IAW B727 SRM 51-30-5, 51-30-2, 51-10-2. 2L73 4F A3WE 20050209001552005020900155CE 2005 2 9 DXTA200500567 120050130A7603 POWER CABLE CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE POWER LEVER OUT OF RIG E DXTAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS LDLANDING 1 GL07352QS 5600352 PCE500209 ON LANDING THE POWER LEVERS WERE BROUGHT TO IDLE AND LEFT ENGINE FAILED (AT IDLE). ADJUSTED FLOW DIVIDER TO FUEL CONTROL INTERCONNECT ROD FOR PROPER IDLE DETENT. RIGGED AFT POWER CONTROL CABLE TO PROVIDE SLIP FIT OF ROD END AT BOLT. GROUND RAN AND NUMEROUS RAPID POWER LEVER REDUCTIONS TO IDLE DID NOT CAUSE ENGINE TO SHUT DOWN, ALL WORK PERFORMED IN ACCORDANCE WITH CESSNA 560 MAINTENANCE MANUAL CHAPTER 76-11-00. 2L72 4F4 FRTA22CE E25EA 20050209001642005020900164WP 2005 2 9 DHL2004809528 120050120A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01809DH91189 46047 LWR FUSELAGE EXTERIOR SKIN CORRODED AT STA 1690.000 (L-28L TO L-28R). PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW SRM 51-1-20D PG 21, SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. CUT OUT CORRODED SECTION. PERFORMED NDT INSPECTION IAW NDT SPM PART 06-10-01-001. FABRICATED (8EA) INTERNAL DOUBLERS (AL7075-T6 0.050) AND (8EA) INTERNAL FINGER DOUBLERS (AL7075-T6 0.032) AND EXTERNAL SPLICE DOUBLER (AL7075-T6 0.063) AND NEW PLATING SEGMENT (AL7075-T6 0.050). CLEANED, TREATED AND PRIMED AREA AND REPAIRED PARTS. APPLIED PRC SEALANT TO FAYING SURFACES. INSTALLED REPAIRED PARTS WITH NEW FASTENERS. TORQUED FASTENERS. 2L74 4F RT4A25 20050210001262005021000126SO 2005 2 10 C2XA05IA016 120050201A3230355022002MOD2 CONTROL UNIT EMB 135 EMB135LR 3260305SO MLG INOPERATIVE A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW27175241002610026 145399 IAH - FLIGHT 2893, THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LGEU (LANDING GEAR ELECTRONIC UNIT), OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050210001282005021000128SO 2005 2 10 C2XA05TY009 120050127A3260JD38999 CONNECTOR EMB 145 EMB145LR 3260212SO LT MLG DAMAGED A C2XAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW2711536 145520 TYS, CONTINUATION OF CONTROL NR C2XA05TY008, AIR RETURN FOR LANDING GEAR AIR GROUND FAIL ON TAKEOFF. MAINTENANCE FOUND THE LEFT MLG FORWARD AND AFT WOW PROX SWITCHES ONLY 250K RESISTANCE, SHOULD BE 1.4M. MAINTENANCE REMOVED AND REPLACED THE LEFT GEAR CANNON PLUG CONNECTORS AND ALL 4 PROX SWITCHES, (P/N 80-057-01, S/N'S 2898, 2783 AND 2885 TSO 3099.9, CYC 2419 / S/N 3437 TSO 3332, CYC 2617. TEST FLEW SATISFACTORY AND WAS RELEASED TO SERVICE. 2L72 4T RTT00011AT 20050210001372005021000137NM 2005 2 10 AWXA200500160 120050104A531365C3079911 STRINGER BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 MCN - MAJOR REPAIR - DURING C-18 CHECK A 1/4 INCH CRACK WAS FOUND IN LEFT WHEEL WELL STRINGER 18A SHEAR WEB AT AFT END, CRACK EMANATING FROM LOWER INBOARD FASTENER HOLE BS 725. MAINTENANCE CUTOUT CRACK IN LEFT WHEEL WELL STRINGER 18A SHEAR WEB, PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST, FABRICATED A FILLER AND GUSSET REPAIR; INSTALLED REPAIR PARTS IAW ER 03-5300-05027-ES1. 2L72 4F RTA16WE 20050210001432005021000143NM 2005 2 10 C8GA20050003 120050119A2130 ISOLATION VALVE BOEING727 727227 1384078NM CABIN PRESSURE MALFUNCTIONED A C8GAB EMER. DESCENT O OTHER CRCRUISE 1 SO15308AS 22002 FLT 712 FROM TOL TO DEN, IN CRUISE AT 31000 FEET, AIRCRAFT RAPIDLY DEPRESSURIZED. CREW EMERGENCY DESCENDED TO 14000 FEET AND STABILIZED PRESSURE AT 5 PSID. AIRCRAFT CONTINUED TO DEN AND LANDED WITHOUT INCIDENT. SWAPPED ENGINE BLEED VALVES WITH NR 2 ISOLATION VALVE. PERFORMED ENGINE RUN TO OPS CHECK SYSTEM. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L73 4F A3WE 20050210001462005021000146NM 2005 2 10 UPS05443807 120050106A5311 FRAME BOEING747 747123F NM FUSELAGE CHAFED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 BS 980, STR 26R FRAME I/B CHORD FOUND DEEP CHAFING MARK. FRAME I/B CHORD REPAIRED PER RS 53-62-35225 AND EO B747-5310-21667-A. 2L74 4F A20WE 20050210001702005021000170NM 2005 2 10 DLM88050074 120050201A5330593666751 SKIN DOUG MD88 MD88 3023688NM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27911DE 49967 FUSELAGE SKIN DAMAGED AT TWO LOCATIONS BETWEEN STATIONS 1250 AND 1287 AND LONGERONS 29L AND 30. REPAIRED I/A/W ERA 096383-14. 2L72 4F RTA6WE 20050211000102005021100010EA 2005 2 11 05030621 120050130A7120 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA ENGINE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27621BR 7186 TWO CRACKS FOUND ON ENGINE SUPPORT BEAM UPPER WEB AT LBL+RBL 7.3 CRACK AT LBL 7.3 IS FROM RIVET HOLE TO WEB EDGE CRACK AT RBL 7.3 EXTENDED .9 INCES OFF THE RIVET HOLE. 2L72 4F RTA21EA 20050211000172005021100017NM 2005 2 11 UPS05443821 120050106A5311 FRAME BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 FRAME BS 1600 INNER FLANGE CRACKED BTN S-25 / S-26L. INNER FLANGE REPAIRED PER RS R53-62-35240 AND EO B747-5310-21668-A. 2L74 4F A20WE 20050211000202005021100020NM 2005 2 11 UPS05443839 120050131A2560 CRASH AX BOEING747 747123F NM EMERGENCY EQUIP DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 CRASH AX NEEDS TO HAVE DEFECTS BLENDED. REMOVED AND REPLACED CRASH AX WITH SERVICEABLE PART OK FOR SERVICE. 2L74 4F A20WE 20050211000272005021100027SO 2005 2 11 C2XA05CL005 120050120A3297W001064324 WIRE EMB 145 EMB145 3260210SO MLG BROKEN A C2XAO OTHER J WARNING INDICATION CLCLIMB 1 SW2727962 145110 CLE FLIGHT NR 3329 - THE CREW REPORTED THE LANDING GEAR WARNING CAME ON EVERY TIME THE THRUST LEVERS WERE REDUCED ABOVE 15,000 FEET. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A BROKEN WIRE. MAINTENANCE REPAIRED WIRE NR W001-0643-24 AND OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20050211000552005021100055NM 2005 2 11 C8GA20050004 120050126A341165594573 PITOT LINE BOEING727 727227 1384078NM AIRSPEED IND LOOSE A C8GAC ABORTED TAKEOFF G MULTIPLE FAILURE TOTAKEOFF 1 SO158942759050 21365 FLT 739 FROM CLT TO BNA, ON TAK OFF, F/O AIRSPEED INDICATOR SHOWED NO INDICATION. ABORTED TAKEOFF AND RETURNED TO GATE. FOUND PITOT/STATIC LINE TO INDICATOR DISCONNECTED. RECONNECTED LINE. SYSTEM OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE 2L73 4F A3WE 20050211000602005021100060SO 2005 2 11 C2XA05BT007 120050125A3350602043 SIGN EMB 145 EMB145ER 3260211SO EMERGENCY EXIT LOOSE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713935 145022 YUL- CO3442, CREW REPORTED, BULKHEAD EXIT SIGN WILL NOT ILLUMINATE. MAINTENANCE RECONNECTED LOOSE CONNECTOR AT EMERGENCY EXIT SIGN, OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20050211000662005021100066EU 2005 2 11 AWXA200500094 120050112A5320D53112198200 FITTING AIRBUS320 A320231 3930325EU L1 DOOR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28621AW 053 SAL - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND AROUND HOLE OF L-1 DOOR LOWER SILL SUPPORT ANGLE (FITTING) BETWEEN FS 16 AND FS 20. MAINTENANCE REMOVED CORRODED L-1 DOOR LOWER SILL SUPPORT ANGLE; FABRICATED A NEW REPLACEMENT SUPPORT ANGLE PER DWG D53112225; INSTALLED REPAIR PART IAW A320 SRM 51-42-11. 2L72 4F RTA28NM 20050211000852005021100085NM 2005 2 11 AWXA200500118 120050102A5320654587547 WEB BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON R-1 DOOR THRESHOLD SHEAR WEB BETWEEN BS 344 AND BS 360, RBL 64 AND RBL 68. MAINTENANCE REMOVED CORRODED SHEAR WEB FROM BS 344 TO BS 360, RBL 64 TO RBL 68; FABRICATED A NEW REPLACEMENT SHEAR WEB PER DWG 65-45875; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050211000862005021100086NM 2005 2 11 AWXA200500138 120050103A531165479602 FRAME BOEING737 7373Q8 1384670NM FUSLEAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK, GALVANIC CORROSION WAS FOUND ON UPPER SURFACE, UPPER FLANGE, OF FRAME AT BS 847, RBL 17.50. MAINTENANCE CUTOUT CORRODED SECTION OF FRAME AT BS 847, RBL 17.50; FABRICATED A 2 EACH ANGLES, A FILLER, SUPPORT CHANNEL, CLIP, AND STRAP, INSTALLED REPAIR PARTS IAW E.R. 03-5302-05028-ES2. 2L72 4F RTA16WE 20050211000932005021100093NM 2005 2 11 AWXA200500139 120050104A575465C26601179 WEDGE BOEING737 7373G7 1384595NM SLATS DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 MCN - MAJOR REPAIR - DURING C-18 CHECK, THE LOWER SURFACE OF NR 1 SLAT WEDGE WAS FOUND DELAMINATED FROM SLAT STA 358 TO 369. MAINTENANCE REMOVED DAMAGE FROM LOWER SURFACE OF NR 1 SLAT WEDGE; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-10, FIG 30. 2L72 4F RTA16WE 20050211000952005021100095NM 2005 2 11 AWXA200500141 120050104A521065458715 FRAME BOEING737 7373G7 1384595NM R1 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 MCN - MAJOR REPAIR - DURING C-18 CHECK A 3/8 INCH CRACK WAS FOUND IN AFT FRAME OF R-1 DOOR AT 3RD AFT STOP PIN BRACKET BS 328, STR 14 RT. MAINTENANCE STOP DRILLED CRACK IN AFT FRAME OF R-1 DOOR AT 3RD AFT STOP PIN BRACKET BS 328, STR 14 RT; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 51-70-11. 2L72 4F RTA16WE 20050211000972005021100097NM 2005 2 11 AWXA200500143 120050107A5315654681025 FLOORBEAM BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 MCN - MAJOR REPAIR - DURING C-18 CHECK, EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM UPPER CHORD AT BS 967, RBL 48, WL 208. MAINTENANCE REMOVED DAMAGE ON FLOORBEAM UPPER CHORD AT BS 967, RBL 48; FABRICATED A STRAP; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-51, FIG 203. 2L72 4F RTA16WE 20050211001032005021100103EU 2005 2 11 AWXA200500146 120050202A3397D9299200900200 WIRE HARNESS AIRBUS320 A320232 3930326EU SEAT ROW 15 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28656AW 1079 PHX - EEL - DURING 8-DAY TEST OF THE EMERGENCY LIGHTING SYSTEM FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 15 LT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT HARNESS BETWEEN CONNECTOR 5157VCA AND EMERGENCY LIGHT AT SEAT ROW 15 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050211001042005021100104NM 2005 2 11 AWXA200500147 120050202A27512061141 INDICATOR BOEING737 73733A 1384673NM TE FLAPS MALFUNCTIONED A AWXAO OTHER JF WARNING INDICATION FLT CONT AFFECTED LDLANDING 1 WP28173AW1646228 23632 ON FINAL APPROACH, WHILE CONFIGURING FOR LANDING, FLAPS BECAME SPLIT WITH LT FLAP AT 11 DEGREES & RT FLAP AT 15 DEGREES, A SLIGHT ROLL NOTED ON CONTROLS. LE SLATS ALL NORMAL WITH GREEN LIGHTS, DECLARED EMERGENCY & LANDED WITHOUT FURTHER EVENT. MX PERFORMED A VISUAL INSPECTION OF FLAPS & CHKD FOR SECURITY. WHILE RUNNING FLAPS UP & DOWN, OBSERVED A NEEDLE SPLIT ON INDICATOR AT 30 & 40 UNITS FOR A FEW SECONDS. R & R FLAP POSITION INDICATOR IAW T/C R1B27001, OPS CHECK GOOD. CONFIRMED REASON FOR REMOVAL FINDING COMPARATOR TEST & POINTER WERE OUT OF TOLERANCE. ADJUSTED COMPARATOR SWITCH, SHIMMED SYCHRO, CLEANED UNIT, CALIBRATED, & REACCOMPLISHED FUNCTIONAL TEST IAW CMM 27-50-03. 2L72 4F RTA16WE 20050211001052005021100105NM 2005 2 11 UPS05443814 120050113A531365B048752 STRINGER BOEING747 747123F NM FUSLAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 BS 1080 TO BS 1100 AFT RT WINDOW FORGING REMOVED FOUND STR CORROSION CRACKED. CORROSION BLEND OUT 0.100" BY 1" BY 5" EXCEED SRM LIMIT. ALL REPAIR PARTS AND NEW STRINGER SEGMENT INSTALLED AS PER RS R-53-41-35252 AND ENGINEERING FILE NUMBER : 747-53-20221. 2L74 4F A20WE 20050211001062005021100106NM 2005 2 11 UPS05443815 120050113A531365B048752 STRINGER BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 BS 1020 TO 1040 AFT RT WINDOW FORGING REMOVED FOUND STR CORROSION CRACKED. CORROSION BLEND OUT 0.100 BY 1 BY 10 INCHES EXCEED SRM LIMIT. ALL REPAIR PARTS AND NEW STRINGER SEGMENT INSTALLED AS PER RS R-53-41-35252 AND ENGINEERING FILE NUMBER : 747-53-20221. 2L74 4F A20WE 20050211001072005021100107NM 2005 2 11 UPS05443817 120050107A531365B072291 STRINGER BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 STR END BS 1003 S-3L CRACKED. STRINGER REPAIRED PER RS R-53-41-35231 AND ENGINEERING FILE NUMBER 747-53-20216. 2L74 4F A20WE 20050211001102005021100110NM 2005 2 11 UPS05443820 120050106A5311 FRAME BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 FRAME BS 1540 INNER FLANGE CRACKED BTN S-25L / S-26L. INNER FRAME REPAIRED PER RS R-53-62-35241 AND EO B747-5310-21656-A. 2L74 4F A20WE 20050214000012005021400001NM 2005 2 14 SWAA050365 120050208A53116549921 CREASE BEAM BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB FROM BS 360 TO BS 380, LBL 64, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB PER SRM. 2L72 4F RTA16WE 20050426000982005042600098NM 2005 4 26 SWAA051031 120050408A575565C2525121A SPOILER BOEING737 7373H4 1384600NM RT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED C4 CHECK, FOUND RT WING NR 9 SPOILER DELAMINATED. REMOVED AND REPLACED NR 9 SPOILER PER MM. 2L72 4F RTA16WE 20050214000022005021400002NE 2005 2 14 COMA0560113 220050206A72616087T04P06 PUMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE LT ENGINE MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01982CA3844 7168 FLIGHT 5487 LEFT ENGINE OIL PRESSURE WARNING. REPLACED THE LUBE AND SCAVENGE PUMP. 2L72 4F4 FRTA21EA E15NE 20050214000042005021400004NM 2005 2 14 SWAA050337 120050207A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29366SW 26577 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 520, BETWEEN STRINGERS 10L AND 14L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20050214000052005021400005NM 2005 2 14 SWAA050338 120050207A3350101114 LAMP BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29645SW 28330 DURING SCHEDULED C2 CHECK, FOUND L2 DOOR LOWER EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050214000062005021400006 2005 2 14 SWAA050339 420050207A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29649SW 27719 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050214000072005021400007NM 2005 2 14 SWAA050340 120050207A53306545774 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN AT BS 727E + 10, STRINGER 19R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050214000082005021400008NM 2005 2 14 SWAA050341 120050207A53126546568 BULKHEAD BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND BULKHEAD PRESSURE DOME WEB AT BS 1016, 1 O`CLOCK POSITION, CRACKED. REPAIRED WEB PER ER. 2L72 4F RTA16WE 20050214000142005021400014EA 2005 2 14 MASA200500054 120050124A3350364911 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSBROKEN A MASAK NONE O OTHER ININSP/MAINT 1 SW07591ML 7388 EMERGENCY FLOOR LIGHTS INTERMITTENT AFT OF THE EXIT ROW. ACFT AOG FOR A POWER CABLE ASSY. 1/24/05 MAINTENANCE REPLACED EMERGENCY LIGHT CABLE STRIP, OPS CHECKED GOOD. 2L72 4F RTA21EA 20050214000152005021400015NM 2005 2 14 SWAA050366 120050208A53306545776 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29691WN 23781 DURING SCHEDULED CHECK, FOUND FUSELAGE SKIN AT BS 941, STRINGER 21L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050214000162005021400016NM 2005 2 14 SWAA050367 120050208A5313BAC1498 STRINGER BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29503SW 24180 DURING SCHEDULED SERVICE CHECK, FOUND STRINGER AT BS 941, STRINGER 23R, CRACKED. REPAIRED STRINGER SECTION PER SRM. 2L72 4F RTA16WE 20050214000172005021400017NM 2005 2 14 SWAA050368 120050208A53156545805 SUPPORT BOEING737 7373K2 13844BANM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29340LV 23738 DURING SCHEDULED 1/2D CHECK, FOUND FLOOR SUPPORT AT BS 267, FROM LBL 12 TO RBL 12, CORRODED. REPAIRED FLOOR SUPPORT PER EA. 2L72 4F RTA16WE 20050214000182005021400018NM 2005 2 14 SWAA050369 120050208A53156545805 FLOORBEAM BOEING737 7373K2 13844BANM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29340LV 23738 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM AT BS 277, FROM LBL 39 TO RBL 47, CORRODED. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20050214000192005021400019NM 2005 2 14 SWAA050370 120050208A2910AE82448J B-NUT BOEING737 7373H4 1384600NM NR 1 HYD SYSTEM LOOSE A SWAAK NONE KJ FLUID LOSS WARNING INDICATION ININSP/MAINT 1 SW29602SW 27953 A-SYSTEM HYDRAULICS FAILED. RECONNECTED NR 1 ENGINE HYDRAULIC SUPPLY LINE B-NUT PER MM. 2L72 4F RTA16WE 20050214000222005021400022SO 2005 2 14 RAIA00502009 120050204A7830 WARNING LIGHT EMB 145 EMB145 3260210SO THRUST REVERSER ILLUMINATED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03821HK 145068 ENGINE NR 2 THRUST REVERSE FAIL MESSAGE DURING PUSHBACK. MAINTENANCE DEFERRED THRUST REVERSE PER MEL 78-30-00 CAT-C. CLEARED DMI-OPS CHECK GOOD - COULD NOT DUPLICATE - NO CMC MESSAGES. 2L72 4F RTT00011AT 20050214000242005021400024EU 2005 2 14 RAIA00502006 120050203A3251AIR141516 PINION GEAR JETAIRJETSTMJETSTM4101 1500501EU MLG MALFUNCTIONED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03568HK5245 41086 AIRCRAFT MADE A SHARP TURN TO THE RIGHT UPON LANDING. MAINTENANCE REMOVED AND REPLACED RACK AND PINION. C/W GEAR SWING AND TAXI AIRCRAFT CHECK. 2L72 4T RTA41NM 20050214000252005021400025NM 2005 2 14 SWAA050372 120050208A53306545769 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29507SW 24184 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT FWD LT CORNER OF AIR CONDITIONER CUTOUT, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20050214000262005021400026NM 2005 2 14 QXEA200500153 120050203A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 PDX - RIGHT HAND FORWARD INBOARD SEAT TRACK HAS HEAVY CORROSION IN NUMEROUS LOCATIONS. REPLACED IAW DHC-8 SRM 51-42-00 AND SRM 51-40-15. 2H72 4T RTA13NM 20050214000342005021400034NM 2005 2 14 QXEA200500152 120050202A522085227011103 SEAL BOMBDRDHC8 DHC8401 1390041NM EMERGENCY DOOR LEAKING A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09403QX9143 4037 BOI - FLIGHT 2362 - THE FLIGHT RETURNED TO FIELD WHEN SHORTLY AFTER TAKEOFF THE RIGHT FORWARD EMERGENCY EXIT STARTED LEAKING AIR. 02/04/05 MAINTENANCE INSPECTED THE DOOR SEAL AND REPLACED THE UPPER SEAL ON THE LOWER FORWARD EMERGENCY EXIT DOOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050214000362005021400036NM 2005 2 14 SB05022 120050202A4940360581217 STARTER BOEING737 7373B7 1384580NM APU FAULTY A USAAO OTHER H ELECT. POWER LOSS-50 PC DEDESCENT 1 EA19391US5051648909 23313 AT THE BEGINNING OF DESCENT INTO CLT, AN APU OVERSPEED OCCURRED RESULTING IN AN APU SHUTDOWN. THIS RESULTED IN A SINGLE GENERATOR OPERATION SINCE THE NR 1 ENGINE GENERATOR WAS ALREADY ON MEL. CREW COMPLIED WITH QUICK REFERENCE HANDBOOK PROCEDURES AND LANDED AT CLT WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE APU STARTER. LEAK CHECK AND OPERATIONAL CHECK GOOD. CLEARED MEL ON NR 1 ENGINE GENERATOR WITH THE REPLACEMENT OF THE GENERATOR AND CSD. 2L72 4F RTA16WE 20050214000372005021400037 2005 2 14 SWAA050373 420050208A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29650SW 27720 R2 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050214000382005021400038NM 2005 2 14 CALA0500044 120050207A2497286A0802 WIRE HARNESS BOEING737 7373T0 1384582NM LT FLAP WELL SHORTED A CALAD RETURN TO BLOCK X ENGINE FLAMEOUT TXTAXI/GRND HDL 1 SW2763305 23356 THE NR 1 ENGINE WAS SLOW TO SPOOL AND THEN FLAMED OUT ON TAXI OUT IN PHL. THE AIRCRAFT WAS RETURNED TO THE GATE. THE DAMAGED WIRES WERE REPLACED. BOEING EXAMINED THE WIRE HARNESS & FOUND THE INSULATION ON THE WIRES DETERIORATED TO THE EXTENT THAT THE WIRE CONDUCTORS HAD BEEN EXPOSED. THE MOST SIGNIFICANT INSULATION DAMAGE WAS OBSERVED AT AN AREA OF THE HARNESS WHERE THE WIRES TRANSITION FROM BEING COVERED WITH A SLEEVED FABRIC TO PLAIN WIRE. MOISTURE BEING RETAINED BY THE SLEEVING & A BEND IN THE WIRE HARNESS IS BELIEVED TO BE THE CAUSE OF THE DETERIORATION AT THE TRANSITION POINT. 2L72 4F RTA16WE 20050214000392005021400039NM 2005 2 14 2005UALA00112 120050131A2612 WARNING LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CARGO FIRE FALSE INDICATIONA UALAF ACTIVATE FIRE EXT. N FALSE WARNING APAPPROACH 1 WP29178UA 24385 FIRE CARGO FWD MSG ON UPPER EICAS ON FINAL APPROACH. FWD CARGO FIRE BOTTLES WERE DISCHARGED ON ARRIVAL. A CHECK OF THE FORWARD CARGO PIT AFTER LANDING REVEALED NO EVIDENCE OF A FIRE. THE SMOKE DETECTORS WERE COVERED WITH MOISTURE. THIS IS CONSISTENT WITH SIMILAR EVENT ON UNITED 747-400 AIRCRAFT IN THE PAST. IT SUGGESTS THE CARGO WAS PROBABLY SOME SORT OF PRODUCE THAT HAD NOT BEEN PROPERLY WRAPPED TO CONTAIN ITS MOISTURE. FALSE FIRE WARNINGS DUE TO MOISTURE IN THE CARGO PIT ARE A LIMITATION OF BOEING'S SMOKE DETECTION SYSTEM DESIGN. 2L74 4F4 FRTA20WE E24NE 20050214000402005021400040NM 2005 2 14 2005UALA00083 120050120A5311 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP29907UA 25007 BS 178 BULKHEAD ON THE UPPER LT CHORD WAS FOUND TO HAVE INSUFFECENT EDGE DISTANCE AT WL 230 FOR REQUIRED OVERSIZING OF FASTENER HOLES. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE AND INSTALLED SPLICE REPAIR. 2L72 4F4 FRTA16WE E2GL 20050214000412005021400041EU 2005 2 14 2005UALA00101 120050128A5270 PROXIMITY SENSOR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CARGO DOOR MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29414UA 472 AFT CARGO DOOR WARNING LIGHT ILLUMINATED. REPLACED THE AFT CARGO DOOR PROXIMITY SENSOR 32WV AND CONNECTOR. 2L72 4F4 FRTA28NM E40NE 20050214000422005021400042NM 2005 2 14 2005UALA00108 120050129A2840 ACTUATOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUEL TRANSFER MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29537UA 25157 UNWANTED FUEL TRANSFER INDICATION. DEFECTIVE CROSS-FEED VALVE ACTUATOR.REPLACED CROSS-FEED VALVE. 2L72 4F4 FRTA2NM E17NE 20050427000052005042700005NM 2005 4 27 DHL2005781549 120050216A5530 STIFFENER BOEING727 727227 1384078NM VERTICAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A C-CHECK,THE FOLLOWING DISCREPANCIES WERE NOTED; VERT STA FIN STA 180, STR 5-8 LT IS CRACKED AT FRAME ATTACH BOLT. REMOVED FASTENERS FOR ACCESS, CUT OUT DAMAGE, DIM 5 X 3 STIFFENER AND REMOVED FILLER IAW B 727 SRM 55-30-4 FIG 1. FABRICATED STIFFENER REPAIR P/N BAC1517-1367 POX. 501953 DIM. 5 X 3 SPLICE P/N AND10134-1201 POX. 501952 DIM 19 X 2.250 FILLER P/N 7075-T6 .100, PO 9001777 DIM 19 X .5, SPLICE P/N AND10133-1401 POX. 501952 DIM.19 X 2, FILLER P/N 7075-T6 .090, PO 9911586 DIM, 19 X .5, CLIP P/N AND10133-1401 POX. 501952 DIM, 2 X 2, IAW B727 SRM55-30-4 FIG 1. TREATED AND PRIMED STIFFENER REPAIR, IAW B727 SRM 51-10-2. INSTALLED STIFFENER REPAIR AT VERT STAB FIN STA 180 STR 8L IAW B727 SRM 52L73 4F A3WE 20050214000462005021400046NM 2005 2 14 2005UALA00114 120050131A5512 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE HORIZ STAB LE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29302UA 23643 RT HORIZ LEADING EDGE DENT APPROX 7 FT FROM INBOARD EDGE. DENT IS APPROX 5 INCHES IN LENGTH, 1.5 INCH WIDE AND .125 IN DEPTH. REPAIR ACCOMPLISHED. INTERIM DOUBLER REPAIR REPLACED WITH PERMANENT FLUSH REPAIR. 2L72 4F4 FRTA16WE E2GL 20050214000482005021400048SO 2005 2 14 C2XA05IA018 120050203A335020131A BATTERY PACK EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713992123251419 145284 EWR - FLIGHT 2879, THE CREW REPORTED THAT THE EMERGENCY LIGHTS WOULD NOT STAY ON. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050214000502005021400050SO 2005 2 14 C2XA05IA020 120050203A3350201318 BATTERY PACK EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW27139798851 1419 145181 EWR - FLIGHT 2879, THE CREW REPORTED THAT THE EMERGENCY LIGHTS WOULD NOT STAY ON. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050214000522005021400052SO 2005 2 14 C2XA05TY011 120050204A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BLOWN A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717560 145605 TYS - DURING A 1A CHECK THE LT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOP. MAINTENANCE REMOVED AND REPLACED THE BULB AND OPS CHECK GOOD. A/C RELEASED AFTER FINAL-1A CHECK WAS C/W. 2L72 4T RTT00011AT 20050214000662005021400066EA 2005 2 14 COMA0560104 120050202A301014463108 ANTI-ICE SYSTEM CNDAIRCL600 CL6002B19 1900309EA RT WING CRACKED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01938CA 7046 FLIGHT 5869 RIGHT WING ANTI ICE DUCT WARNING. REPLACED THE OUTBOARD PICOLO TUBE. 2L72 4F RTA21EA 20050214000672005021400067EA 2005 2 14 COMA0560105 120050202A291673011 RESERVOIR CNDAIRCL600 CL6002B19 1900309EA NR 1 HYD SYS MALFUNCTIONED A COMAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO01981CA114237513 7163 FLIGHT 5280 HYDRAULIC SYSTEM NR 1 QUANTITY INDICATING 35 PERCENT. REPLACED THE NR 1 HYDRAULIC RESERVOIR. 2L72 4F RTA21EA 20050214000682005021400068EA 2005 2 14 COMA0560106 120050202A2121 FAN CNDAIRCL600 CL6002B19 1900309EA CARGO BAY FAILED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01466CA 7627 FLIGHT 5752 CARGO FAN FAIL. DEFERRED MAINT PER MEL. 2L72 4F RTA21EA 20050214000722005021400072EA 2005 2 14 QXEA200500162 120050119A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 FUSELAGE OUTER SKIN IS NICKED AT FS 5423.0 BETWEEN STRINGERS 26R-27. REPAIRED IAW HORIZON AIR EA R-53-261 AND CRJ REO 670-53-21-070. 2L72 4F RTA21EA 20050214000732005021400073EA 2005 2 14 QXEA200500163 120050119A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - FUSELAGE OUTER SKIN IS NICKED AT STATION 431.0 BETWEEN STRINGERS 26R-27. REPAIRED IAW HORIZON AIR EA R-53-261 AND CRJ 700 REO 670-53-21-070. 2L72 4F RTA21EA 20050214000762005021400076EA 2005 2 14 QXEA200500164 120050119A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 FUSELAGE OUTER SKIN IS NICKED AT STATION 440.0 BETWEEN STRINGERS 26R-27. REPAIRED IAW HORIZON AIR EA R-53-161 AND CRJ 700 REO 670-53-21-070. 2L72 4F RTA21EA 20050214000782005021400078EA 2005 2 14 QXEA200500158 120050116A5320 STRIKER CNDAIRCL600 CL6002C10 1390015EA ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - FORWARD CENTER FUSELAGE, LEFT HAND FORWARD BAGGAGE BAY DOOR SURROUND STRUCTURE, AFT SEAL STRIKER GOUGED. REPAIRED IAW HORIZON AIR EA R-53-257 AND REO 670-53-31-023. 2L72 4F RTA21EA 20050214000792005021400079NM 2005 2 14 P5CA0501317 120050209A272260130005 ACTUATOR BOEING747 747123 1384873NM RUDDER MALFUNCTIONED A P5CAO OTHER J WARNING INDICATION NRNOT REPORTED 1 EA15858FT 20109 INBOUND CREW REPORTED RUDDER RATIO LIGHT ON STEADY. T/S FOUND LOWER RUDDER ACTUATOR STUCK IN HIGH SPEED MODE. REMOVED AND REPLACED LOWER RUDDER RATIO ACTUATOR AND CONTROLLER PER MM 27-21-12. ALL OPS NORMAL. 2L74 4F A20WE 20050214000802005021400080NM 2005 2 14 SB05024 120050206A335020131A BATTERY BOEING737 7374B7 1384702NM EMERGENCY LIGHT DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19781AU 25020 PIT - FOUND R1 DOOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. 2L72 4F RTA16WE 20050214000822005021400082EA 2005 2 14 QXEA200500156 120050115A5320 STRIKER CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - FORWARD CENTER FUSELAGE, LEFT HAND FORWARD BAGGAGE DOOR SURROUND STRUCTURE FORWARD UPPER SEAL STRUCTURE CHAFED. REPAIRED IAW HORIZON AIR EA R-53-255 AND REO 670-53-31-022. 2L72 4F RTA21EA 20050214000832005021400083EA 2005 2 14 QXEA200500161 120050119A5320 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 FUSELAGE OUTER SKIN IS NICKED AT FS 374.0 BETWEEN STRINGERS 24R-25R. REPAIRED IAW SRM 53-21-01-006-A01 AND HORIZON AIR EA R-53-260. 2L72 4F RTA21EA 20050214000842005021400084EA 2005 2 14 QXEA200500160 120050126A5230 HINGE CNDAIRCL600 CL6002C10 1390015EA ZONE 800 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - FORWARD BAGGAGE DOOR AFT INBOARD HINGE ARM HAS IMPACT DAMAGE ON AFT FACE. REPAIRED IAW HORIZON EA R-52-213 AND CRJ REO 670-52-35-055, REV A. 2L72 4F RTA21EA 20050214000852005021400085 2005 2 14 BB05004 420050130A2565140N276217 GIRT BAR BOEING757 7572B7 1384964NM L 2 DOOR UNSERVICEABLE A USAAK NONE O OTHER ININSP/MAINT 1 EA19623AU 27244 PHL - FOUND L2 GIRT BAR IN NEED OF REPLACEMENT. REPLACED L2 DOOR GIRT BAR. 2L72 4F RTA2NM 20050214000862005021400086NE 2005 2 14 IXXA0500015O 220050205A7200 ENGINE DOUG DC8 DC862 3021970WP PWA JT3D JT3D7 52039NE NR 4 FAILED A IXXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW11799AL756762440 45922335 671276 DURING CLIMBOUT FROM KBWI, NR 4 ENGINE OIL PRESSURE LIGHT CAME ON. OIL PRESSURE/QUANTITY NORMAL. OIL TEMP WAS SLIGHTLY HIGHER THEN OTHERS AT 105C. COMPLETED CHECKLIST AND LIGHT WOULD NOT GO OUT. CREW SHUT DOWN ENGINE INFLIGHT THEN DIVERTED AIRCRAFT TO KWRI AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED, REPLACED AND RAN NR 4 ENGINE AND THE OPERATIONAL AND LEAK CHECK WERE GOOD PER ALL APPLICABLE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F4 F 4A25 1E8 20050214000882005021400088EU 2005 2 14 SA05014 120050202A335032145410 EPSU AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT FAULTY A USAAK NONE L NO TEST ININSP/MAINT 1 EA19717UW10334556 1069 THE MID CABIN LEFT EMERGENCY POWER SUPPLY UNIT FAILED TEST. MAINTENANCE REPLACED THE LEFT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20050214000902005021400090NM 2005 2 14 QXEA200500151 120050203A3040SYLZ50970 CONTROLLER DHAV DHC8 DHC8202 2809007NM WINDSHIELD HEAT FAILED A QXEAA UNSCHED LANDING A FLAME/FIRE CLCLIMB 1 NM09351PH162708431 490 THE FLIGHT RETURNED TO FIELD AFTER THE HEAT ELEMENT FOR THE F/O'S WINDSHIELD SPARKED AND DEVELOPED A SMALL FLAME. THE FLAME WENT OUT WHEN THE WINDSHIELD HEAT WAS TURNED OFF. A CRACK WAS ALSO DISCOVERED ON THE F/O'S WINDSHIELD. MAINTENANCE REMOVED THE NR 2 HEAT CONTROLLER AND THE WIRE TERMINAL. MAINTENANCE ALSO REMOVED AND REPLACED THE CRACKED WINDSHIELD. C/W OPERATIONAL TEST OF THE F/O WINDSHIELD HEAT IAW 30-41-00-710-801. OPERATIONAL AND VISUAL CHECKS GOOD. NO DAMAGE NOTED TO WINDSHIELD FRAME OR SURROUNDING AREA. 2H72 4T RTA13NM 20050214000912005021400091NM 2005 2 14 BB05005 120050201A335020121 CHARGER BOEING757 7572B7 1384964NM L4 DOOR INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19631AU 27809 CLT - FOUND EMERGENCY SLIDE LIGHT L56 (AT L4 DOOR) INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY (M737). 2L72 4F RTA2NM 20050214000942005021400094CE 2005 2 14 68346 120050110A32439038000133 MASTER CYLINDER BEECH 1900 1900D 1154162CE BRAKE SYSTEM DAMAGED A AMWAO OTHER O OTHER LDLANDING 1 CE07139ZV UE139 ALL FOUR BRAKE PEDALS SPONGY ON LANDING. REMOVED AND REPLACED RT SIDE OUTBOUND MASTER BRAKE CYCLINDER. P/N 90-380001-33 (OFF), S/N 7984 (ON), P/N 90-380001-33 (OFF), S/N 3119 (OFF). 2L72 4T RTA24CE 20050214000952005021400095CE 2005 2 14 68374 120050111A7720 INDICATOR BEECH 1900 1900D 1154162CE ITT READS LOW A AMWAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 CE07127ZV UE127 AFTER T/O AND APPROXIMATELY 10 MINUTES INTO FLIGHT. CREW NOTICED RIGHT HAND ITT INDICATOR DROPPED TO ZERO. TOOK INSTRUCTIONS RTF ABQ LANDED AND TAXIED TO GATE WITH NO FURTHER INCIDENT. 2L72 4T RTA24CE 20050214000962005021400096CE 2005 2 14 68657 120050123A5270 ANNUNCIATOR BEECH 1900 1900D 1154162CE CARGO DOOR ILLUMINATED A AMWAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE07143YV UE143 AFTER T/O FROM PIT TO DUJ, CARGO DOOR ANNUNCIATOR ILLUMINATED. A/C RETURNED TO FIELD WITH NO FURTHER INCIDENT. NO DAMAGE FOUND ON AIRCRAFT. LOCKED CARGO DOOR AND PRESSURIZED AIRCRAFT. NO DEFECTS NOTED. 2L72 4T RTA24CE 20050214001002005021400100EU 2005 2 14 SA05020 120050210A335032145410 EPSU AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT FAULTY A USAAK NONE L NO TEST ININSP/MAINT 1 EA19714US17059 1046 THE EMERGENCY LIGHTS FAILED TEST. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY TESTS OK. 2L72 4F RTA28NM 20050214001012005021400101EA 2005 2 14 COMA0560109 120050205A2750860D10018ABCD CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA E/E BAY MALFUNCTIONED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01940CA200503210 7048 FLIGHT 5322 FLAPS FAIL CAUTION. REPLACED THE FECU. 2L72 4F RTA21EA 20050214001022005021400102EA 2005 2 14 COMA0560112 120050205A7931 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA RT ENGINE ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01786CA 7333 FLT 5167 RT ENGINE OIL PRESSURE WARNING. COULD NOT DUPLICATE. INSPECTED ENGINE AND FOUND NO DEFECTS. CLEANED TRANSDUCER WIRING CONNECTIONS, GROUND RUNS SATISFACTORY. 2L72 4F RTA21EA 20050214001032005021400103EA 2005 2 14 COMA0560107 120050202A5100 UNKNOWN CNDAIRCL600 CL6002B19 1900309EA UNKNOWN UNKNOWN A COMAO OTHER E VIBRATION/BUFFET CRCRUISE 1 SO01978CA 7158 FLIGHT 5780 SEVERE TURBULANCE DURING FLIGHT, LASTED 15 TO 20 SECONDS. C/W TURBULANCE INSPECTION, NO DEFECTS FOUND. 2L72 4F RTA21EA 20050210001092005021000109EA 2005 2 10 A6WA200540010 120050105A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23463AW 7878 FOUND DENT IN LEFT SKIN FROM FS 235 TO FS 265 BETWEEN STRINGER 17L AND STRINGER 19L. REPAIRED DENT IN FUSELAGE SKIN FROM FS 235 TO FS 265 BETWEEN STRINGER 17L AND STRINGER 19L IAW BRAS EO 601R-53-5788A. (M) 2L72 4F RTA21EA 20050210001452005021000145 2005 2 10 UPS05143831 420050130A2565 SLIDE AIRBUSA300 A300F4622R 3930360EU FWD ENTRY DOOR INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01135UP 0818 FWD ENTRY DOOR SLIDE ARM (ESCAPE SLIDE) WILL NOT TEST PROPERLY. AURAL WARNING BUT NO LIGHT. RESEATED AUTONOMOUS STANDBY PWR SUPPLY UNIT PER A300 AMB 3-52-05-004 AND AMM 52-73-18-4, OPS CK OK. 2L72 4F RTA35EU 20050210001472005021000147NM 2005 2 10 UPS05443808 120050108A5313 STRINGER BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 BS 1480 - 1485, S6L, STRINGER END FOUND CRACKED. STRINGER REPAIRED PER RS R53-41-35249 AND ENGINEERING FILE NUMBER 747-53-20215. 2L74 4F A20WE 20050210001512005021000151NM 2005 2 10 UPS05443812 120050108A5313 STRINGER BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 BS 1482 - 1485, STR 13R, STRINGER END FOUND CRACK. STRINGER REPAIRED PER RS 53-41-35250 AND ENGINEERING FILE NUMBER 747-53-20214. 2L74 4F A20WE 20050210001572005021000157SO 2005 2 10 C2XA05CL004 120050119A27528855001003 ACTUATOR EMB 145 EMB145XR 3260214SO WING FLAP FROZEN A C2XAO OTHER J WARNING INDICATION CLCLIMB 1 SW2724128 145700 CLE FLIGHT NR 3182, THE CREW REPORTED FLAP FAILURE, FLAPS SELECTED TO 9 DEGREES AND FAILED. MAINTENANCE INSPECTED THE AIRCRAFT AND WATER PRESENT IN THE NR 2 FLAP ACTUATOR. MAINTENANCE REPLACED THE NR 2 FLAP ACTUATOR, ALL OPERATIONAL CHECKS GOOD. 2L72 4F RT 20050211000062005021100006NM 2005 2 11 AWXA200500163 120050108A534069620541 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 MCN - MAJOR REPAIR - DURING C-18 CHECK A 3/16 INCH CRACK WAS FOUND IN CLIP ON FORWARD SIDE OF BS 294, STR 11 LT. MAINTENANCE REMOVED CRACKED CLIP AT BS 294, STR 11 LT; FABRICATED A NEW REPLACEMENT CLIP; INSTALLED REPAIR PART IAW ER 03-5300-05031-SS3. 2L72 4F RTA16WE 20050211000072005021100007NM 2005 2 11 AWXA200500164 120050105A53206517684642 INTERCOSTAL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 MCN - MAJOR REPAIR - DURING C-18 CHECK, A 1/4 INCH CRACK WAS FOUND IN INTERCOSTAL AT STR 7 LT, BETWEEN BS 294 AND BS 303. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT STR 7 LT, FROM BS 294 TO BS 303; FABRICATED A NEW REPLACEMENT INTERCOSTAL; INSTALLED REPAIR PART IAW ER 03-5300-05031-SS3. 2L72 4F RTA16WE 20050211000152005021100015NM 2005 2 11 DL76L050086 120050204A5522 SKIN BOEING767 767332 1382001NM LT ELEVATOR DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27175DN 24803 WHILE PERFORMING ELEVATOR PCA BELLCRANK CHECK MX FOUND UPPER SURFACE OF LEFT INBD ELEVATOR WITH SLIGHT DAMAGE. REPAIRED PER SRM 55-20-01 AND 51-70-17. 2L72 4F RTA1NM 20050211000252005021100025SO 2005 2 11 C2XA05CL006 120050122A3610 BLEED AIR SYS EMB 145 EMB145LR 3260212SO CONTAMINATED A C2XAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SW2714923 145318 CLE - FLT NR 2139 - AFTER TAKEOFF, THE CREW GOT THE LAVATORY SMOKE INDICATION ON THE EICAS WITH A NOTICABLE SMOKE SMELL. RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND FOUND DE-ICING FLUID IN THE BLEED SYSTEM. CLEARED DE-ICING FLUID FROM BLEED SYSTEM. ALL OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20050211000262005021100026SO 2005 2 11 C2XA05TY008 120050126A32608005701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212SO MLG DEFECTIVE A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2711536 145520 TYS - A/C WAS DEPARTING BHM WHEN THE ICAS MESSAGE SHOWED GEAR NOT RETRACTED. A/C RETURNED TO BLOCK AND MAINTENANCE REMOVED AND REPLACED THE LGEU, BUT DID NOT FIX PROBLEM. A/C WAS FERRIED TO TYS AND MAINTENANCE REMOVED AND REPLACED THE NR 1 AND NR 2 PROX SWITCHES. A/C WAS REL FOR A TEST FLIGHT AND TEST FLIGHT WAS SATISFACTORY. A/C WAS THEN REL FOR REVENUE SERVICE. 2L72 4T RTT00011AT 20050211000292005021100029EU 2005 2 11 AWXA200500129 120050201A3350321454 EPSU AIRBUS320 A320232 3930326EU ZONE 221 DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28649AW401396429 803 PHX - EEL - DURING E-06 CHECK FUNCTIONAL TEST OF THE EMERGENCY LIGHT SYSTEM FOUND THE EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 1-5 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT FORWARD EMERGENCY POWER SUPPLY UNIT (10WL), OPERATIONAL TEST WAS GOOD. 2L72 4F RTA28NM 20050211000532005021100053WP 2005 2 11 UPS05843837 120050108A5340SAA37799781 ATTACH FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01701UP 45938 MAIN CABIN AT STA 702 LBL (LONGERON 13LH) FRAME ATTACH FITTING CRACKED. REMOVED, FABRICATED AND REPLACED FRAME ATTACH FITTING AT F/S 702 L13L IAW 51-1-20-D, DWG3779978 AND SAA TRAVELER 0035. 2L74 4F RT4A25 20050211000642005021100064EU 2005 2 11 AWXA200500092 120050129A3397ABS0374A24 CABLE AIRBUS320 A320231 3930325EU SEAT ROW 9 RT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 CMH - EEL - DURING 4-DAY CHECK, FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 9 RT INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE TERMINAL FOR EMERGENCY ESCAPE PATH LIGHT SEAT ROW 9 RT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050211000672005021100067EU 2005 2 11 AWXA200500095 120050109A5330D5348011420802 DOUBLER AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28621AW 053 SAL - MAJOR REPAIR - DURING C-04 CHECK, INTERGRANULAR CORROSION WAS FOUND BETWEEN INTERNAL DOUBLER AND BASE OF AFT POTABLE WATER DOOR FS 65-66, STR 40 LT. MAINTENANCE REMOVED CORRODED INTERNAL DOUBLER AT BASE OF AFT POTABLE WATER DOOR FROM FS 65 TO FS 66, STR 37 LT TO STR 42 LT; CLEANED AND PRIMED AREA BENEATH DOUBLER; FABRICATED A NEW REPLACEMENT DOUBLER PER DWG D53480030; INSTALLED REPAIR PART IAW A320 SRM 51-42-11. 2L72 4F RTA28NM 20050211000802005021100080NM 2005 2 11 AWXA200500115 120050108A5340693535214 STRINGER CLIP BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK A 5/16 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT BS 867, STR 1. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 867, STR 1; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-35352; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 3, 4, 6, 7, AND 8. 2L72 4F RTA16WE 20050211000842005021100084NM 2005 2 11 SB05017 120050127A3397 WIRE BOEING737 737301 1384611NM P-18 PANEL FAULTY A USAAK NONE O OTHER ININSP/MAINT 1 EA19563AU 23551 PVD - MAINTENANCE REPORTED THE EMERGENCY LIGHTS WOULD NOT SHUTOFF. MAINTENANCE REPAIRED WIRING AT THE EMERGENCY LIGHT CIRCUIT BREAKER ON THE P-18 PANEL. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050211000962005021100096NM 2005 2 11 AWXA200500142 120050105A5315654581217 ATTACH ANGLE BOEING737 7373G7 1384595NM FLOORBEAM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 MCN - MAJOR REPAIR - DURING C-18 CHECK, A 1 INCH CRACK WAS FOUND IN MAIN CABIN FLOORBEAM ATTACH ANGLE AT BS 328, LBL 46. MAINTENANCE REMOVED CRACKED FLOORBEAM ATTACH ANGLE AT BS 328, LBL 46; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 65-45812; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050211001002005021100100NM 2005 2 11 UPS05443813 120050106A5313 STRINGER BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 BS 1476 - 1478 STR 13R STRINGER END FOUND CRACK. STRINGER REPAIRED PER RS 53-41-35250 AND ENGINEERING FILE NUMBER 747-53-20214. 2L74 4F A20WE 20050211001092005021100109NM 2005 2 11 UPS05443819 120050110A531165B0417815 FRAME BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 BS 940, S25L FRAME I/B CHORD FOUND CRACK. M/D BS 940 FRAME AT S-25L, FRAME REPAIRED PER RS R-53-22-35244 AND EO B747-5310-21670-A. 2L74 4F A20WE 20050214000112005021400011SO 2005 2 14 MASA200500016 120050106A335078241 POWER SUPPLY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSINOPERATIVE A MASAK NONE O OTHER ININSP/MAINT 1 SW07828MJ 145218 CREW REPORTED THE OVERWING DOOR AT 12A EMERGENCY LIGHT INOP. MAINTENANCE REPLACED A LIGHT STRIP BUT DID NOT FIX THE PROBLEM. MAINTENANCE RESECURED A LOOSE WIRE AND REPLACED THE POWER SUPPLY (OVERWING LT EXIT MARKER P/N 7444-25). 2L72 4T RTT00011AT 20050214000352005021400035EU 2005 2 14 YENA200516 120050127A3240 CONTROL UNIT AIRBUS320 A320232 3930326EU PARKING BRAKE INOPERATIVE A YENAO OTHER O OTHER TXTAXI/GRND HDL 1 EA15547JB 1849 PARKING BRAKE INOP WHILE IN -ON- POSITION. RESET BSCU. PERFORMED OPERATIONAL CHECK OF PARKING BRAKE. CHECKS GOOD IAW AMM 32-45-00. 2L72 4F RTA28NM 20050214000442005021400044EU 2005 2 14 2005UALA00102 120050130A2100 WARNING LIGHT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE COCKPIT ILLUMINATED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29476UA 1508 VENT AVIONICS FAULT WITH VENT SKIN VALVE MESSAGE. ECAM PAGE SHOWS SKIN AIR OUTLET VALVE (22HQ) AT FAULT. PERFORMED CFDS TEST, CONFIRMED VALVE AT FAULT AND REPLACED. 2L72 4F4 FRTA28NM E40NE 20050214000512005021400051SO 2005 2 14 C2XA05IA021 120050203A335020131A BATTERY PACK EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW27139797747 1419 145181 EWR - FLIGHT 2879, THE CREW REPORTED THAT THE EMERGENCY LIGHTS WOULD NOT STAY ON. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050214000712005021400071EA 2005 2 14 QXEA200500154 120050115A5210 HOUSING CNDAIRCL600 CL6002C10 1390015EA ZONE 800 WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - FUSELAGE FORWARD PASSENGER DOOR HAS WEAR DAMAGE FROM OUTER CLOSER HANDLE STOP ON INNER SURFACE OF HANDLE HOUSING. REPAIRED IAW HORIZON AIR EA R-52-212 AND REO 670-52-11-085. 2L72 4F RTA21EA 20050214000742005021400074EA 2005 2 14 QXEA200500165 120050119A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - FUSELAGE OUTER SKIN IS NICKED AT STATION 457.0 BETWEEN STRINGER 25L AND 26L. REPAIRED IAW HORIZON AIR EA R-53-262 AND CRJ 700 REO 670-53-21-070. 2L72 4F RTA21EA 20050214000872005021400087EA 2005 2 14 MASA200500059 120050125A33501317 BULB CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHTSBURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07502MJ 10050 THE CREW REPORTED A LOWER EMERGENCY EXIT LIGHT INOPERATIVE. THE ITEM WAS PLACED ON DEFERRAL SINCE AT LEAST 50 PERCENT OF THE BULBS REMAINED OPERATIVE. 1/26/05 MAINTENANCE RELAMPED, OPS CHECKED GOOD. 2L72 4F RTA21EA 20050214000892005021400089WP 2005 2 14 IXXA0500014O 120050129A261292274473 RELAY DOUG DC8 DC873F 302199FWP FIRE WARNING DEFECTIVE A IXXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW11602AL94435122 45991 NR 4 ENGINE FIRE WARNING LIGHT AND BELL CAME ON DURING CLIMB AT 36,000 FT. CREW SHUT DOWN ENGINE, HAD NO OTHER INDICATION. ENGINE SHORT CIRCUIT LIGHT WOULD NOT TEST. CREW CONTINUED TO HAVE GOOD OIL PRESSURE ON ENGINE. MAINTENANCE REMOVED AND REPLACED O/B FIRE BOTTLE. CHECKED ALL ENGINE FIRE DETECTOR ELEMENTS AND FIRE WARNING CONNECTORS. REMOVED AND REPLACED NR 4 ENGINE FIRE CONTROL RELAY AND SYSTEMS CHECK IS NORMAL PER ALL APPLICABLE MANUALS AND AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20050214000922005021400092NM 2005 2 14 BB05006 120050201A335020121 CHARGER BOEING757 7572B7 1384964NM R4 DOOR INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19631AU 27809 CLT - FOUND R4 DOOR EMERGENCY EXIT SIGN LIGHT INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY (M736). 2L72 4F RTA2NM 20050214001072005021400107SO 2005 2 14 MASA200500063 120050127A3350RPS1B BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT FAILED A MASAK NONE O OTHER ININSP/MAINT 1 SW07840MJ 145429 LT FWD OUTSIDE EMERGENCY LIGHT WILL NOT ILLUMINATE. CAE MX DEFERRED THE LIGHT IAW MEL 33-50-00-1. LATER IN THE DAY, CLT MX CLEARED THE DEFERRAL BY REPLACING THE LIGHT SOCKET AND EMERGENCY BATTERY. LIGHT P/N 30-2510-3. 2L72 4T RTT00011AT 20050214001122005021400112EA 2005 2 14 MASA200500078 120050201A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSBURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0717358 7358 EMERGENCY LIGHT SIGN BY AIRSTAIR DOOR HAS 2 BULBS INOP. MAINTENANCE RELAMPED. 2L72 4F RTA21EA 20050214001132005021400113EA 2005 2 14 MASA200500079 120050204A3350 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DIRTY A MASAK NONE O OTHER ININSP/MAINT 1 SW0775991 7422 ENCOUNTERED FLOOR EMERGENCY LIGHT STRIPS INOP. MAINTENANCE REMOVED AND CLEANED CONNECTOR. LIGHTS OPS CHECKED GOOD AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20050214001182005021400118NM 2005 2 14 SWAA050382 120050209A53306545776 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 937, STRINGER 23R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050214001222005021400122NM 2005 2 14 SWAA050386 120050209A533065C337251 SKIN BOEING737 7373K2 13844BANM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29340LV 23738 DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR LOWER HINGE CUTOUT LOWER RADIUS, CRACKED. REPAIRED SKIN PER BOEING SB. 2L72 4F RTA16WE 20050214001232005021400123NM 2005 2 14 SWAA050387 120050209A53156546824 FLOORBEAM BOEING737 7373K2 13844BANM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29340LV 23738 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM UPPER CHORD AT BS 1006, LBL 19, CORRODED. REPAIRED FLOORBEAM CHORD PER SRM AND BAC DRAWING. 2L72 4F RTA16WE 20050214001242005021400124 2005 2 14 SB05023 420050204A256565655983 BRACKET BOEING737 7373B7 1384580NM L1 DOOR GIRT BAROUT OF ADJUST A USAAK NONE O OTHER ININSP/MAINT 1 EA19387US 22959 CLT - THE L1 DOOR GIRT BAR WOULD NOT STAY ATTACHED. MAINTENANCE ADJUSTED THE GIRT BAR ATTACH BRACKETS. 2L72 4F RTA16WE 20050214001262005021400126NM 2005 2 14 AWXA200500184 120050208A3350BR964411 LIGHT BOEING737 7373G7 1384595NM SEAT ROW 2 LT FAULTY A AWXAK NONE O OTHER ININSP/MAINT 1 WP28322AW 25400 LAS - DURING B-04 CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 2 LEFT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 2 LEFT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050214001282005021400128NM 2005 2 14 AWXA200500175 120050125A534069353521 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 MCN - MAJOR REPAIR - DURING C-16 CHECK A .5 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT BS 767, STR 20 RT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 767, STR 20 RT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 65-46549; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050214001302005021400130NM 2005 2 14 AWXA200500177 120050125A534069353521 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 MCN - MAJOR REPAIR - DURING C-16 CHECK A .75 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT BS 787, STR 25 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 787, STR 25 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 65-46550; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050214001322005021400132NM 2005 2 14 AWXA200500179 120050123A5753 SKIN BOEING737 7373G7 1384595NM FORE FLAP DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 MCN - MAJOR REPAIR - DURING C-16 CHECK THE UPPER SURFACE OF THE LT INBOARD FORE FLAP WAS FOUND DELAMINATED 32.5 INCHES TO 37.5 INCHES FROM THE OUTBOARD END. MAINTENANCE CUT OUT DAMAGE IN UPPER SURFACE OF LT INBOARD FORE FLAP; FABRICATED A CORE FILLER AND EXTERNAL DOUBLER; BONDED REPAIR PARTS TO FLAP IAW B737-300 SRM 51-70-10 FIG 18. 2L72 4F RTA16WE 20050214001342005021400134SO 2005 2 14 MASA200500080 120050206A3350 SIGN EMB 145 EMB145LR 3260212SO EMERGENCY EXIT INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07852MJ 145567 EMERGENCY EXIT SIGN AT ROW 12 INOP. MAINTENANCE SECURED THE ELECTRICAL CONNECTION TO THE LIGHT ASSEMBLY. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050214001362005021400136EA 2005 2 14 MASA200500084 120050207A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSBURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07591ML 7388 ONE EMERGENCY LIGHT IN OVERHEAD INOP. MAINTENANCE COMPLIED WITH MEL PROCEDURES. 2/7/05 MAINTENANCE RELAMPED, OPS CHECK GOOD. 2L72 4F RTA21EA 20050214001382005021400138NM 2005 2 14 SWAA050374 120050209A3350101331 COVER BOEING737 7377H4 1384404NM EMER EXIT SIGN DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29705SW 27839 RIGHT OVERWING EMERGENCY EXIT SIGN FELL OFF. REINSTALLED SIGN COVER PER MM. 2L72 4F RTA16WE 20050214001402005021400140 2005 2 14 SWAA050376 420050209A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29637SW 27710 DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050214001412005021400141NM 2005 2 14 SWAA050378 120050209A53106546818 CREASE BEAM BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 840, LBL 65, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB PER SRM. 2L72 4F RTA16WE 20050214001422005021400142NM 2005 2 14 SWAA050379 120050209A57436582770 FITTING BOEING737 7373Q8 1384670NM LT WING CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND LT WING GEAR SPAR FITTING CORRODED. REMOVED AND REPLACED SPAR FITTING PER BAC DRAWING. 2L72 4F RTA16WE 20050214001432005021400143NM 2005 2 14 SWAA050389 120050209A55516551524 FITTING BOEING737 7373H4 1384600NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29603SW 27954 DURING SCHEDULED D-CHECK, FOUND LT AND RT HORIZONTAL STABILIZER FITTING FWD AND AFT SPARS CLEVIS LUGS CORRODED. REPAIRED FITTING PER SRM. 2L72 4F RTA16WE 20050214001452005021400145NM 2005 2 14 SWAA050342 120050207A534065C27314 STRINGER CLIP BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 807, STRINGER 25L, CORRODED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20050214001472005021400147CE 2005 2 14 DXTA200500528 120050115A3030M6106 RELAY CESSNA750 750 2076810CE PITOT HEAT INOPERATIVE E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07996QS 7500196 DURING T/O THE AMBER MESSAGE P/S RAT HEAT OFF ILLUMINATED WITH THE P/S HEAT SWITCHES IN THE ON POSITION. AFTER BRINGING THE THROTTLES TO IDLE THE CAS MESSAGE TURNED CYAN WITH THE P/S SWITCHES STILL IN THE ON POSITION. REMOVED AND REPLACED RELAY KCOO4 AND P/S SWITCH CESSNA 750MM 30-30-01, PERFORMED OPS CHECKS IAW CESSNA 750MM30-32-00 PILOT/ STATIC HEAT CHECKS SERVICEABLE. 2L72 4J RTT00007WI 20050214001482005021400148NM 2005 2 14 SWAA050343 120050207A534065C27314 STRINGER CLIP BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 787, STRINGER 20R, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20050214001492005021400149NM 2005 2 14 SWAA050344 120050207A53206546811 WEB BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND FLOOR SHEAR WEB AT BS 1014, LBL 37, CORRODED. REMOVED AND REPLACED WEB SECTION PER SRM. 2L72 4F RTA16WE 20050214001502005021400150NM 2005 2 14 SWAA050345 120050207A53156546810 FLOORBEAM BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 967, FROM LBL 27 TO RBL 27, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM. 2L72 4F RTA16WE 20050214001512005021400151NM 2005 2 14 SWAA050346 120050207A53116546557 FRAME BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 887, STRINGER 8R, CRACKED. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20050214001522005021400152NM 2005 2 14 SWAA050347 120050207A335065C34691 LIGHT BOEING737 7375H4 138449DNM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29524SW 26566 DURING SCHEDULED SERVICE CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT BETWEEN ROWS 16 DEF AND 17 DEF, INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20050214001532005021400153NM 2005 2 14 SWAA050348 120050207A33501619 LAMP BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29709SW 27843 DURING SCHEDULED MV2 CHECK, FOUND FWD ENTRY DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050214001542005021400154NM 2005 2 14 SWAA050349 120050207A533065C337251 SKIN BOEING737 7373K2 13844BANM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29340LV 23738 DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR UPPER HINGE CUTOUT LOWER RADIUS, CRACKED. REPAIRED SKIN PER BOEING SB. 2L72 4F RTA16WE 20050214001552005021400155NM 2005 2 14 SWAA050350 120050207A531565C33940 FLOORBEAM BOEING737 7373K2 13844BANM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29340LV 23738 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM AT BS 294, FROM LBL 35 TO LBL 49, CORRODED. REPAIRED FLOORBEAM SECTION PER EA. 2L72 4F RTA16WE 20050214001562005021400156NM 2005 2 14 SWAA050351 120050207A53106546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29603SW 27954 DURING SCHEDULED D-CHECK, FOUND AFT CARGO COMPARTMENT SHEAR TIE AT BS 787, RBL 4, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050214001572005021400157NM 2005 2 14 2005UALA00116 120050201A5230 STRUCTURE BOEING747 747422 1384935NM PWA 4056 PW4056 NE CARGO DOOR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29107UA 26900 LOWER AFT CORNER OF FWD CARGO DOOR CRACKED. DAMAGE WAS CAUSED BY IMPROPER OPERATION OF THE DOOR. DOOR WAS LOWERED ONTO CONTAINER LOADER. DAMAGED SKIN WAS REMOVED, AND THE DOOR WAS REPAIRED. 2L74 4F4 FRTA20WE E24NE 20050214001592005021400159NM 2005 2 14 SWAA050352 120050207A53106545833 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29603SW 27954 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM CHORD AT RIGHT BS 188, CRACKED. REMOVED AND REPLACED CREASE BEAM CHORD SECTIONS PER SRM. 2L72 4F RTA16WE 20050214001612005021400161EA 2005 2 14 COMA0560111 120050205A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01981CA 7163 FLIGHT 5437 FLAPS FAIL CAUTION. COULD NOT DUPLICATE. INSPECTED FLAP SYSTEM IAW AD98-20-01. NO DEFECTS FOUND. 2L72 4F RTA21EA 20050214001632005021400163NM 2005 2 14 SWAA050353 120050207A53156545834 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29603SW 27954 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 294, FROM RBL 37 TO RBL 54, CORRODED. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20050214001652005021400165NM 2005 2 14 SWAA050355 120050207A53206920158 WEB BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29603SW 27954 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM WEB BETWEEN BS 188 AND BS 194, FROM LBL 30 TO RBL 30, CRACKED. REMOVED AND REPLACED FLOORBEAM WEB PER SRM. 2L72 4F RTA16WE 20050214001732005021400173NM 2005 2 14 P5CA0501314 120050204A2910272U12001048 LINE BOEING747 74746NF 13848BTNM HYD SYSTEM CRACKED A P5CAO OTHER K FLUID LOSS NRNOT REPORTED 1 EA15450PA 30808 LOSS OF NR 3 HYDRAULIC FLUID. TROUBLESHOT AND FOUND NR 3 EDP PRESSURE LINE UNDER THE GAP PANEL CRACKED. REPLACED LINE WITH FLEX LINE PER GMM 3-17-1, COI 450-017. OPS & LEAK CHECK OK PER 20-11-18. 2L74 4F RTA20WE 20050214001762005021400176NM 2005 2 14 2005UALA00107 120050130A5532 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE VERTICAL STAB LEDENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29302UA 23643 VERTICAL STAB LEADING EDGE IS DENTED AT L/E STA 104. REMOVED DENT DAMAGE AND INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20050214001772005021400177WP 2005 2 14 AALA20050079 120050202A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21432AA 49350 SEA - AFT TAIL CONE EMERGENCY LIGHT ON LEFT SIDE INOPERATIVE ON TEST OF LOWER TAIL CONE HANDLE. FOUND WIRE BROKEN FROM THREE WIRE SPLICE IN TAIL CONE AREA. RESPLICED BROKEN WIRE IN AFT TAIL CONE AREA FOR EMERGENCY LIGHT ON LEFT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050214001792005021400179NM 2005 2 14 SWAA050363 120050208A53156546801 FLOORBEAM BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CHORD AT BS 360, BL 0, CORRODED. REMOVED AND REPLACED CHORD SECTION PER SRM. 2L72 4F RTA16WE 20050301000132005030100013NM 2005 3 1 UPS05443925 120050211A5711 FITTING BOEING747 747123 1384873NM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, RT WING REAR SPAR UPPER SPLICE FITTING AT BS 1241 HOLE NR 8 FOUND CRACKED AT SPLICE FITTING APPROX 0.040 INCH. HOLE REWORKED PER BSB 747-57A2314. 2L74 4F A20WE 20050215000152005021500015SO 2005 2 15 SIMA200500905 120050104A532014521721005 STRAP EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21632AE 145143 DURING CPCP INSPECTION MAINTENANCE FOUND THE FORWARD STRAP AT FRAME 14 CORRODED ON THE UPPER SURFACE. REPAIRED SILL IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200502484) (K) 2L72 4T4 FRTT00011ATTE6CH 20050215000162005021500016SO 2005 2 15 SIMA200500908 120050106A27303621001011 CONTROL UNIT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL AVIONIC BAY INOPERATIVE A SIMAO OTHER O OTHER TXTAXI/GRND HDL 1 SW21675AE 14500806 CREW REPORTED A DUAL PITCH TRIM FAILURE DURING TAXI AFTER LANDING. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200502367) (K) 2L72 4T4 FRTT00011ATTE6CH 20050215000192005021500019EA 2005 2 15 ASOA05042 120050118A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27903EV 7621 DURING A C-CHECK, THE LT AND RT CLIPS AT FS 625 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LT AND RT CLIPS AT FS 625. (K) 2L72 4F4 FRTA21EA E15NE 20050215000252005021500025SO 2005 2 15 SIMA200501904 120050109A531314533888001 STRINGER EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21735TS 145386 DURING AN IMBV MAINTENANCE FOUND A PREVIOUS REPAIR ON STRINGER 19R AT JUNCTION 5 BETWEEN FRAMES 52 AND 53 WAS FOUND CHAFED. REMOVED THE EXISTING DAMAGED REPAIR ANGLE AND SHIMS. FABRICATED A REPAIR ANGLE AND 2 SHIMS. REPAIR DONE IAW SRM. (SW21200502482) (K) 2L72 4F4 FRTT00011ATTE6CH 20050215000272005021500027EU 2005 2 15 BMAC040019 120050106A5210 HANDLE BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110UG 01514WP PAX DOOR OUT OF ADJUST A B16AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NE05536PA 681 PILOT REPORTED: DOOR CAP LIGHT CAME ON DURING FLIGHT. PERFORMED DOOR HANDLE ADJUSTMENTS IAW AMM. OPS CHECKED GOOD AT THIS TIME. 2L72 4T4 TRTA21EU E4WE 20050301000152005030100015NM 2005 3 1 UPS05443928 120050210A5315 FLOORBEAM BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, M/D BS 1500 RBL 5-10 FLOORBEAM FOUND CORROSION. CORROSION BLEND OUT 2 X 2 X 0.060 INCH FLOORBEAM REPAIRED PER SRM 51-40-04 FIG 1. 2L74 4F A20WE 20050215000372005021500037EA 2005 2 15 ASOA05012 120050104A5210600380591 ANCHOR FITTING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF348C1 NE PAX DOOR CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27823AS 7196 7196 DURING C-CHECK, THE PASSENGER DOOR FORWARD CABLE ANCHOR FITTING AND PLATE WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE PASSENGER DOOR FORWARD CABLE ANCHOR FITTING AND PLATE. (K) 2L72 4F4 FRTA21EA EOOO63EN 20050215000402005021500040EA 2005 2 15 ASOA05015 120050106A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27826AS 7210 DURING A C-CHECK, THE RT AFT CORNER OF THE NLG CUTOUT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE RT FUSELAGE SKIN RADIUS AT FS 235 IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050215000412005021500041EA 2005 2 15 ASOA05018 120050107A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27835AS 7258 DURING OVERNIGHT SERVICE, THE EMERGENCY LIGHT AT THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT LAMP AT THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050301000172005030100017NM 2005 3 1 UPS05443920 120050210A5730 SKIN BOEING747 747123 1384873NM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, RT WING REAR SPAR UPPER SPLICE FITTING AT BS 1241 HOLE NR 11 FOUND CRACKED AT WING SKIN APPROX 0.040 INCH. HOLE REWORKED PER BSB 747-57A2314. 2L74 4F A20WE 20050210001352005021000135NM 2005 2 10 DHL2005743500 120050108A531465564418 KEELBEAM BOEING727 727225 1384077NM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01743DH3834038340 22438 AFT CARGO COMP STA 950F,S29R KEEL BEAM LWR CHORD CRACKED IN VERT LEG LWR RADIUS APPROX 4 INCHES. JACKED AND SHORED A/C REMOVED FLOOR SUPPORT, STR CLIPS, GUSSET, WING TO BODY FAIRINGS, STR 30 STA 950-950A, STR 29R STA 950-1009 AND INTERCOSTAL. CUT HOLE IN SKIN 950A-950B MAT ID STR 30 BAC1498-146 PO NR 90506949 ,HAT SECTION BAC 1498-131, KEEL BEAM CHORD 65-56441-8, FILLER .180 2024T3 PO 9304989,-3 REPAIR DOUBLER .100 2024T3 PO 00442440,-5 REPAIR DOUBLER .080 2024T3 PO 00331565. FAB`D, LOCATED, DRILLED, AND TRIMMED PARTS. ALODINED, PRIMED AND INSTALLED REPAIR PARTS IAW EA PD 27-53-121,PD 27-53-122,B727 SRM 51-10-2,51-30-2,51-50-1,M/M 27-51-22. REMOVED JACKING AND SHORING. 2L73 4F A3WE 20050210001382005021000138EA 2005 2 10 05031703 120050131A7120 SUPPORT CNDAIRCL600 CL6002B19 1900309EA ENGINE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27703BR 7467 ENGINE SUPPORT BEAM CRACKED ON RIGHT HAND LOWER ACCESS PANEL CUTOUT. INBOARD FORWARD EDGE AT 75 IN LENGTH AT RBL 36.2 WATER LINE 111.09 2L72 4F RTA21EA 20050210001442005021000144NM 2005 2 10 SB05015 120050126A2410735511A CSD BOEING737 737301 1384611NM NR 1 ENGINE FAILED A USAAHA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING JH WARNING INDICATION ELECT. POWER LOSS-50 PC CRCRUISE 1 EA19558AU448342973 23512 ORF - FLT178 - DURING CRUISE, EN ROUTE FROM CLT TO BOS, THE NR 1 ENGINE CSD HIGH OIL TEMPERATURE LIGHT ILLUMINATED. THE APU WAS ALREADY ON MEL, SO THE CREW DISCONNECTED THE NR 1 ENGINE CSD AND DIVERTED TO ORF WHERE THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE CSD PER MM 24-11-11-4 ALONG WITH THE OIL COOLER PER MM 24-11-21. OPERATIONAL CHECK AND LEAK CHECK GOOD. CLEARED APU MEL 49-1 WITH THE REPLACEMENT OF THE APU M280 MODULE. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050210001502005021000150NM 2005 2 10 UPS05443811 120050107A5313 STRINGER BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 STR END BS 1485 S-8L CRACKED. STRINGER REPAIRED PER RS 53-1-35249 AND ENGINEERING FILE NUMBER 747-53-20215. 2L74 4F A20WE 20050210001542005021000154NM 2005 2 10 SB05008 120050118A21337110033 OUTFLOW VALVE BOEING737 7374B7 1384702NM CABIN PRESSURE FAULTY A USAAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 EA19779AU6583 6583 24996 RSW - FLT1052 - DURING CRUISE AT FL250, EN ROUTE FROM CLT TO RSW, A/C LOST PRESSURIZATION JUST SW OF JAX. CREW CAUGHT THE PROBLEM BEFORE THE CABIN PRESSURE DROPPED ENOUGH TO DEPLOY THE OXYGEN MASKS. CREW DESCENDED FLT TO 10,000 FT AND THEN LANDED AT RSW WITHOUT FURTHER INCIDENT. AN EMERGENCY WAS DECLARED. MX REMOVED AND REPLACED THE AFT OUTFLOW VALVE PER MM 21-31-111-4 AND THE FORWARD OUTFLOW VALVE PER MM 21-43-11-4. OPERATIONAL CHECK AND LEAK CHECK GOOD. ALSO, REMOVED AND REPLACED THE LEFT ENGINE PRECOOLER CONTROL VALVE SENSOR PER MM 36-12-45, DUE TO A MEL FOR A DUCT PRESSURE SPLIT. OPERATIONAL CHECK GOOD. REPAIRED MULTIPLE HULL LEAKS AND ACCOMPLISHED SATISFACTORY CABIN LEAK RATE CHECK. 2L72 4F RTA16WE 20050210001682005021000168 2005 2 10 05026651 420050126A3418 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA STALL WARNING ILLUMINATED A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27651BR 7426 EVENT SUMMARY STATED THAT STALL FAIL MSG ON CLIMB-OUT. NO FAULT CODES IN MDC. RESET SPS. INSPECTED BOTH AOA VANES. OPS CHK GOOD. 2L72 4F RTA21EA 20050210001692005021000169WP 2005 2 10 DHL2004809524 120050120A5312 PRESSURE PANEL DOUG DC8 DC873F 302199FWP MLG WW CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01809DH91189 46047 MAIN CARGO COMPT MLG PRESSURE PANEL SKIN CRACKED STA 907.000 LBL 41. (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 01-19-05 DWG X32-R05 REV A DATE 01-19-05. REMOVED EXISTING REPAIR IAW DWG X32-R05, SRM 51-1-21 PG.1, SRM 51-3-0 PG.1. TRIMMED OUT DAMAGED AREA IAW DWG X32-R05. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. FAB`D SHIMS 4EA (AL7075-T6 0.063, 0.010), FILLERS 2A (AL7075-T6 0.063) AND EXTERNAL REPAIR DOUBLER (AL7075-T6 0.063) IAW DWG X32-R05. CLEANED, TREATED AND PRIMED AREA AND REPAIRED PARTS IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED REPAIRED PARTS IAW DWG X32-R05, SRM 51-1-20D PG.9, SRM 51-3-0 PG.1, SRM 51-1-21 PG.1, TORQUE2L74 4F RT4A25 20050210001712005021000171NM 2005 2 10 DL75A050075 120050201A5330143N31311 SKIN BOEING757 757212 1384951NM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27752AT 23128 TOOLING DAMAGE TO THE FUSELAGE SKIN AT STATION 453 AND STR 4L. REPAIR IAW ERA 096138-14. 2L72 4F RTA2NM 20050210001762005021000176NM 2005 2 10 AWXA200500152 120050104A5330654577614 SKIN BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 MCN - MAJOR REPAIR - DURING C-18 CHECK, EXFOLIATION CORROSION WAS FOUND ON EDGE OF SKIN AROUND AFT LOWER AIRPHONE ANTENNA BETWEEN BS 787 AND BS 807, STR 27 LT AND STR 27 RT. MAINTENANCE REMOVED AIRPHONE ANTENNA AND CUTOUT CORRODED SKIN FROM BS 787 TO BS 807, STR 27 LT TO STR 27 RT; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-01, FIG 229. 2L72 4F RTA16WE 20050211000122005021100012EA 2005 2 11 05026656 120050126A4900 DUCT CNDAIRCL600 CL6002B19 1900309EA APU BAY CONTAMINATED A VTZAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA27656BR 7845 EVENT SUMMARY STATED LAV SMOKE MSG. OPERATED A/C OFF BOTH ENGINES AND APU. NOTED SLIGHT GLYCOL SMELL. REMOVED AND REPLACED SOCKS AND CLEANED EXTERNAL RESIDUE IN APU BAY. OPERATED SYSTEM AGAIN AND SMELL DISAPPEARED REF CRJ MM 21-50-00. REMOVED AND REPLACED BOTH COALESCER SOCKS DUE IAW CRJ MM 21-51-13. INSPECTED AIR RT AND LT AIR DUCTS IN APU BAY NO OIL RESIDUE FOUND IN DUCTS REF CRJ MM 21-51-00. EXAMINED LT AND RT HEAT EXCHANGERS NO OIL RESIDUE NOTED IN REF TO CRJ MM 21-51-07. FOUND GLYCOL EXTERNALLY ON DUCTS IN APU BAY. CLEANED GLYCOL OFF EXTERNAL DUCTING IN REF TO CRJ MM 21-51-00. NO OIL NOTED INSIDE ECS DUCTING OR HEAT EXCHANGERS. 2L72 4F RTA21EA 20050211000132005021100013NM 2005 2 11 AWXA200500166 120050108A532066142081 WEB BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 MCN - MAJOR REPAIR - DURING C-18 CHECK, A 3/16 INCH CRACK WAS FOUND IN LOWER WEB AT BS 294, STR 11 LT. MAINTENANCE REMOVED CRACKED LOWER WEB AT STR 11 LT FROM BS 294 TO BS 303.9, AND 2 EACH BRACKETS; FABRICATED A NEW REPLACEMENT WEB AND 2 EACH BRACKETS; INSTALLED REPAIR PARTS IAW ER 03-5300-05031-SS1. 2L72 4F RTA16WE 20050211000382005021100038NM 2005 2 11 AWXA200500101 120050131A3397BR963180 WIRE HARNESS BOEING737 7373Y0 1384671NM SEAT ROW 17 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 PHX - EEL - DURING 4-DAY CHECK, FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 17 LEFT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED WIRE HARNESS TO EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 17 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050211000502005021100050WP 2005 2 11 UPS05843834 120050107A53103758496U2 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01701UP 45938 LWR CARGO PIT STA 1140 L34R UPPER FWD FITTING CRACKED ON THE FRAME. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2L74 4F RT4A25 20050211000582005021100058SO 2005 2 11 C2XA05IA015 120050125A3350110049 POWER SUPPLY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714543 145553 MCI - DURING MAINTENANCE INSPECTION, BOTH THE LT AND RT EXTERIOR OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT BATTERY POWER SUPPLY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050211000592005021100059SO 2005 2 11 C2XA05BT009 120050128A33503025101 LIGHT EMB 145 EMB145ER 3260211SO FUSELAGE FAULTY A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714933 145018 EWR---CO2383, CREW REPORTED RIGHT FORWARD EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED RIGHT FORWARD EXTERIOR EMERGENCY EXIT LIGHT HOUSING IAW EMB145 AMM NR 33-50-10, OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20050211000692005021100069EU 2005 2 11 BA05003 120050130A2497242260108 WIRE AIRBUS330 A330323 3930335EU APU GENERATOR SHORTED A USAAA UNSCHED LANDING AH FLAME/FIRE ELECT. POWER LOSS-50 PC CLCLIMB 1 EA19678US 3457CE 388 CLT - FL 94 AFTER TAKEOFF, THE CREW NOTED THAT THE NR 1 IDG FAULTED. ALTHOUGH THE APU WAS OPERATIONAL, THE APU AFT FUEL PUMP WAS ON MEL AND THE CREW ELECTED TO RETURN TO CLT. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND FIELD WIRE 2422-60108 SHORTING TO THE SHIELD WIRE. THE WIRE WAS REPAIRED, SEPARATED AND INSULATED. 2L72 4F RTA46NM 20050211000992005021100099NM 2005 2 11 AWXA200500145 120050104A532065C334191 SHEAR WEB BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 MCN - MAJOR REPAIR - DURING C-18 CHECK, A 1/2 INCH CRACK WAS FOUND IN AFT CABIN CENTER FLOOR SHEAR WEB AT BS 1023, BL "0". MAINTENANCE REMOVED CRACKED SHEAR WEB AT BS 1023, BL "0"; FABRICATED A NEW REPLACEMENT SHEAR WEB PER DWG 65C32677; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050211001022005021100102SO 2005 2 11 C2XA05SH007 120050202A361014531227403 DUCT EMB 145 EMB145LR 3260212SO BLEED SYSTEM DAMAGED A C2XAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 SW2710575 145640 SHV - DURING CLIMB, ENG NR 2 HAS FIRE WARNING INDICATION. MAINTENANCE INSPECT AND FOUND UPPER BLEED DUCT DAMAGE NO FIRE WAS EVIDENT. REPLACE BOTH UPPER BLEED DUCTS PER EMB 145AMM 36-11-09. PERFORMS GROUND OPPERATIONAL CHECK AND LEAK CHECK PER AMM 72-00-00. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE 2L72 4T RTT00011AT 20050214000032005021400003 2005 2 14 SWAA050336 420050207A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29648SW 27718 R1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050214000092005021400009NM 2005 2 14 P5CA0501318 120050209A2400 GENERATOR BOEING747 74746NF 13848BTNM MALFUNCTIONED A P5CAD RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TXTAXI/GRND HDL 1 EA15451PA 30809 CREW REPORTED RETURN TO BLOCKS DUE NR 2, 3 AND 4 GENERATORS WOULD NOT PARALLEL. RESET SPLIT SYSTEM BREAKER, PERFORMED BCU-1 AND BCU-2 SYSTEM GROUND TEST PER MM 24-11-00. ALL OPS NORMAL. 2L74 4F RTA20WE 20050214000122005021400012EA 2005 2 14 MASA200500045 120050119A33501317 BULB CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHTSBURNED OUT A MASAK NONE O OTHER TXTAXI/GRND HDL 1 SW07509MJ 10094 THE CREW REPORTED THE FLOOR LEVEL EXIT SIGN AT THE SERVICE DOOR HAD 2 OF 5 BULBS INOPERATIVE. THE LIGHT WAS PLACED ON DEFERRAL. 1/21/05 MAINTENANCE RELAMPED, OPS CHECKED GOOD. 2L72 4F RTA21EA 20050214000212005021400021EU 2005 2 14 RAIA00502008 120050204A3150 WARNING HORN JETAIRJETSTMJETSTM4101 1500501EU CONFIGURATION ACTIVATED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TXTAXI/GRND HDL 1 CE03566HK 41084 STL - CONFIG WARNING ON TAKEOFF. MAINTENANCE ADJUSTED LEFT CONDITION LEVER SWITCH. OPS CHECK GOOD. 2L72 4T RTA41NM 20050214000472005021400047EA 2005 2 14 COMA0560110 120050205A2750860D10018ABCD CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01982CA187934597 7168 FLIGHT 5535 FLAPS FAIL CAUTION. REPLACED THE FECU. 2L72 4F RTA21EA 20050214000692005021400069NM 2005 2 14 P5CA0501316 120050208A3610 VALVE BOEING747 747230B 1384889NM NR 2 ENGINE FAILED A P5CAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA15509MC 21221 NR 2 PYLON VALVE FAILED TO OPEN ON ENGINE START. DEFERRED NR 2 ENGINE PYLON VALVE PER MEL 36-5-2. TRANSFERRED TO DMI 33793. 2L74 4F A20WE 20050214000772005021400077EA 2005 2 14 QXEA200500157 120050116A5320 STRIKER CNDAIRCL600 CL6002C10 1390015EA ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - FORWARD CENTER FUSELAGE, LEFT HAND FORWARD BAGGAGE BAY DOOR SURROUND STRUCTURE, FORWARD SEAL STRIKER GOUGED. REPAIRED IAW HORIZON AIR EA R-53-257 AND REO 670-53-31-023. 2L72 4F RTA21EA 20050214000812005021400081EA 2005 2 14 QXEA200500159 120050121A5230 HINGE CNDAIRCL600 CL6002C10 1390015EA ZONE 800 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - FORWARD BAGGAGE DOOR FORWARD INBOARD HINGE ARM HAS CHAFING DAMAGE ON FORWARD FACE. REPAIRED IAW HORIZON AIR EA R-52-213 AND REO 670-52-35-055, REV A. 2L72 4F RTA21EA 20050214000972005021400097CE 2005 2 14 68755 120050128A3242 BRAKE ASSY BEECH 1900 1900D 1154162CE LEFT WEAK A AMWAO OTHER O OTHER NRNOT REPORTED 1 CE07244YV UE244 ON CREWS FIRST FLIGHT CHECKS LEFT BRAKE WAS WEAK. A/C RETURNED TO THE HANGAR. MTC BLED BRAKES AND A/C RETURNED TO SERVICE. BLED BRAKES. 2L72 4T RTA24CE 20050214001052005021400105EU 2005 2 14 SA05012 120050201A5610NP1653116 WINDSHIELD AIRBUSA319 A319112 3930323EU COCKPIT CRACKED A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19712US17541 1038 DURING CLIMB, THE FIRST OFFICER'S WINDSHIELD CRACKED. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FIRST OFFICER'S WINDSHIELD. OK FOR SERVICE. 2L72 4F RTA28NM 20050214001082005021400108EA 2005 2 14 MASA200500071 120050130A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSBURNED OUT A MASAK NONE O OTHER ININSP/MAINT 1 SW0737342 7342 AIRCRAFT WAS ON RON AND SCHEDULED FOR A ROUTINE CHECK INSPECTION. DURING THE WALKAROUND IT WAS DISCOVERED THE RT OVERWING MID EXTERIOR EMERGENCY LIGHT NOT ILLUMINATING. MAINTENANCE REPLACED THE LIGHT BULB, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050214001102005021400110SO 2005 2 14 MASA200500073 120050131A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSBURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07829MJ 145228 REPORTED AN EMERGENCY OVERHEAD FLOOD LIGHT INOP AT ROW 12. MAINTENANCE REPLACED THE LAMP. 2L72 4T RTT00011AT 20050214001162005021400116NM 2005 2 14 SWAA050380 120050209A531069353656 SHEAR TIE BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 360, STRINGER 14R, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050214001272005021400127NM 2005 2 14 AWXA200500185 120050123A53206552878529 WEB BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF SHEAR WEB BETWEEN BS 1009 AND BS 1015, LBL 41 AND LBL 45, WL 207.5. MAINTENANCE REMOVED CORRODED SHEAR WEB FROM BS 1009 TO BS 1015, LBL 41 TO LBL 45; FABRICATED A NEW REPLACEMENT SHEAR WEB PER DWG 65-52878; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050214001292005021400129NM 2005 2 14 AWXA200500176 120050125A534069353521 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 MCN - MAJOR REPAIR - DURING C-16 CHECK A .625 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT AFT CARGO COMPARTMENT BS 867, STR 24 RT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT AFT CARGO COMPARTMENT BS 867, STR 24 RT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-35352; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050214001312005021400131NM 2005 2 14 AWXA200500178 120050125A534069353522 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 MCN - MAJOR REPAIR - DURING C-16 CHECK A .75 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT BS 727E, STR 20 RT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 727E, STR 20 RT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 65C25230; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050214001332005021400133NM 2005 2 14 AWXA200500180 120050126A534069353521 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 MCN - MAJOR REPAIR - DURING C-16 CHECK A .25 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT BS 480, STR 26 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 480, STR 26 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 65C25229; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050214001352005021400135SO 2005 2 14 MASA200500081 120050206A3350 SIGN EMB 145 EMB145LR 3260212SO EMERGENCY EXIT INOPERATIVE A MASAK NONE O OTHER ININSP/MAINT 1 SW07853MJ 145464 CLT-BNA, EMERGENCY EXIT SIGN ROW 12F WOULD NOT ILLUMINATE. MAINTENANCE SECURED CONNECTOR TO THE LIGHT ASSY. NO FURTHER DEFECTS NOTED. 2L72 4T RTT00011AT 20050214001372005021400137NM 2005 2 14 SWAA050388 120050209A53156546811 FLOORBEAM BOEING737 7373K2 13844BANM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29340LV 23738 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM TEE CAP AT BS 986, LBL 15, CORRODED. REPAIRED FLOORBEAM PER TRM T1-453-037. 2L72 4F RTA16WE 20050214001392005021400139NM 2005 2 14 SWAA050375 120050209A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29351SW 24572 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 935, STRINGER 25R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050215000092005021500009SO 2005 2 15 SIMA200501915 120050114A532014524131005 BRACKET EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21738NR 145401 DURING CPCP INSPECTION MAINTENANCE FOUND THE MAIN CABIN DOOR SHAPE U HAS CORROSION AROUND NUTPLATES AT FRAME 16. INSTALLED NEW CABIN DOOR U-SHAPE BRACKET IAW SRM. AIRCRAFT RETURNED TO SERVICE. (SW21200502486) (K) 2L72 4F4 FRTT00011ATTE6CH 20050215000242005021500024EU 2005 2 15 A6WA200560002 120050111A3240AHA23312 BRAKE BAC 146 146200A 1500266EU LYC ALF502ALF502R5 41580NE NR 4 INOPERATIVE A A6WAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL31609AW16790257 E2070 GREEN HYDRAULIC SYSTEM LOW, YELLOW SYSTEM HIGH. ABORTED TAKE-OFF AT LESS THAN 5 KTS. MAINTENANCE SERVICED AS REQUIRED. MAINTENANCE REMOVED AND REPLACED NR 4 BRAKE ASSEMBLY. (K) 2H74 4F4 F A49EU E6NE 20050215000322005021500032EA 2005 2 15 ASOA05029 120050114A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27905EV 7632 DURING HANGAR MAINTENANCE, THE LT EXTERIOR SECOND FROM THE FROM EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT EXTERIOR SECOND FROM THE FRONT EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050215000502005021500050EU 2005 2 15 BMAC040018 120050103A32345148YM15AS SELECTOR SWITCH BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110UG 01514WP MLG INOPERATIVE A B16AA UNSCHED LANDING O OTHER CLCLIMB 1 NE05535PA 687 PILOT REPORTED: ON TAKE-OFF, GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. RETURNED TO DEPARTURE. REMOVED AND REPLACED LANDING GEAR SELECTOR SWITCH IAW AMM. OPERATIONALLY CHECKED OK AT THIS TIME. (K) 2L72 4T4 TRTA21EU E4WE 20050215000522005021500052EA 2005 2 15 ASOA05024 120050112A3260864202 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE MLG UPLOCK OUT OF ADJUST A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27820AS DCL50096 7188 AFTER TAKEOFF, THE CREW RECEIVED A (GEAR UP DISAGREE) MESSAGE. THE QRH WAS COMPLIED WITH, AND EMERGENCY DECLARED AND THE AIRCRAFT RETURNED TO DEPARTURE, LANDING SAFELY. MAINTENANCE ADJUSTED THE UPLOCK PROXIMITY TARGET ON THE LEFT MAIN LANDING GEAR (MLG). OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050215000582005021500058SO 2005 2 15 SIMA200500906 120050104A532014521725613 SILL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21632AE 145143 DURING CPCP INSPECTION MAINTENANCE FOUND THE FORWARD SILL AT SERVICE DOOR CORRODED UPPER SURFACE. INSTALLED FWD SILL AT SERVICE DOOR IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200502484) (K) 2L72 4T4 FRTT00011ATTE6CH 20050215000592005021500059EA 2005 2 15 ASOA05007 120050103A5320 SILL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27826AS 7210 DURING A C-CHECK, THE CARGO COMPARTMENT DOOR SILL PLATE WAS FOUND TO BE CORRODD, CHAFED AND CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CARGO COMPARTMENT DOOR SILL PLATE IAW SRM. (K) 2L72 4F4 FRTA21EA E15NE 20050215000632005021500063EU 2005 2 15 USAA050030 120050101A5315D5347217220290 FLOORBEAM AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19713UW17339 1040 BFM - S1 - BEAM, 1.5 INCH L X 1.5 INCH W X .035 INCH D, CORROSION; LEVEL 2; TASK NR JA260-53500, MAIN CABIN FLOOR FR 66-68, Y1292. REMOVED AND REPLACED BEAM IAW SRM. (K) 2L72 4F4 FRTA28NM E37NE 20050215000662005021500066EA 2005 2 15 ASOA05021 120050109A3250 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE NLG STEERING ILLUMINATED A ASOAO OTHER J WARNING INDICATION CLCLIMB 1 SO27713EV 10081 DURING CLIMB OUT, THE CREW RECEIVED AN (NWS INOP MSSG) ON EICAS. THE NOSE WHEEL STEERING (NWS) FAULT SUBSEQUENTLY CLEARED AND THE AIRCRAFT CONTINUED. THE QRH WAS COMPLIED WITH AND THE CREW RESET THE NWS SYSTEM UPON LANDING IN IAH SAFELY. THE TOWER ROLLED EMERGENCY EQUIPMENT AS A PRECAUTION. MAINTENANCE RE RACKED THE NOSE WHEEL ELECTRONIC CONTROL UNIT AND NO FAULTS WERE FOUND. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA EOOO63EN 20050215000672005021500067NE 2005 2 15 ALG2005F00011 120050105A3297 WIRE SKRSKYS76 S76 8143010NE ALLSN 250C 250C30S 03013GL MLG BROKEN E ALGAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 SW03707AL 760189 DURING LANDING PHASE TO MC506 (OCEAN VICTORY) THE LANDING GEAR WOULD NOT EXTEND. NOTICED THE CIRCUIT WAS OUT. TRIED TO RESET IT BUT WOULD NOT STAY IN. DIVERTED AIRCRAFT FOR MAINTENANCE. MAINTENANCE FOUND WIRE BROKEN AT PIN R (CONNECTOR PLUG P105) REPAIRED BROKEN WIRE AND COMPLIED WITH LANDING GEAR RETRACTION CHECK, NO DEFECTS NOTED. (K) 1G72 3U3 U H1NE E1GL 20050215000782005021500078EA 2005 2 15 A6WA200540014 120050107A3210 BUSHING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT MLG TRUNNION MIGRATED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31446AW 7806 THE LT MLG AFT TRUNNION BUSHING IS MIGRATED .045 INCH. REMOVED AND REPLACED LT MLG AFT TRUNNION BUSHING IAW REO. (K) 2L72 4F4 FRTA21EA E15NE 20050215000802005021500080EU 2005 2 15 USAA050029 120050101A5315D53472090002000 FLOORBEAM AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19713UW17339 1040 BFM - S1 -FLOORBEAM, 2 INCH DIA X .04 INCH DEPTH, CORROSION; LEVEL 2; TASK NR JA-260-53500, 66-65 FRAME, Y765, MAIN CABIN FLOOR. REMOVED AND REPLACED BEAM IAW SRM. (K) 2L72 4F4 FRTA28NM E37NE 20050215001012005021500101SO 2005 2 15 SIMA200501202 120050107A532014525381003 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21654AE 145437 DURING AN MBV INSPECTION THE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE DAMAGED AREA. FABRICATED A DOUBLER, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (SW21200502478) (K) 2L72 4T4 FRTT00011ATTE6CH 20050215001082005021500108SO 2005 2 15 SIMA200500903 120050104A532014522460009 GUSSET EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21632AE 145143 DURING CPCP INSPECTION MAINTENANCE FOUND THE GUSSET ON HAT BEAM CORRODED IN NUMEROUS SPOTS. MAINTENANCE REPLACED THE GUSSET IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200502484) (K) 2L72 4T4 FRTT00011ATTE6CH 20050215001232005021500123EA 2005 2 15 A6WA200540013 120050107A3210 BUSHING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT MLG TRUNNION MIGRATED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31446AW 7806 THE RT MLG AFT TRUNION BUSHING IS MIGRATED .059 INCH. REMOVED AND REPLACED RT MLG AFT TRUNNION BUSHING IAW REO. (K) 2L72 4F4 FRTA21EA E15NE 20050215001272005021500127EA 2005 2 15 ASOA05002 120050101A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27823AS 7196 DURING A C-CHECK, THE LT IB FS 484 INTERCOSTAL AT BL 27 TO 36 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LT IB FS 484 INTERCOSTAL AT BL 27 TO 36 IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050215001322005021500132EA 2005 2 15 ASOA05014 120050105A5312 PRESSURE BLKHD CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27826AS 7210 DURING A C-CHECK, THE FORWARD PRESSURE BULKHEAD IN THE HYDRAULIC BAY AT FS 202.75, BL23.71 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FORWARD PRESSURE BULKHEAD IN THE HYDRAULIC BAY AT FS 202.75, BL 23.71 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FORWARD PRESSURE BULKHEAD IN THE HYDRAULIC BAY AT FS 202.75, BL 23.71 IAW REO. (K) 2L72 4F4 FRTA21EA E15NE 20050215001332005021500133NM 2005 2 15 S2YA04005 120050118A2400 CONTROL PANEL DORNERDO32 DO328300 NM PWA 306 PW306B NE GENERATOR INOPERATIVE A S2YAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL13360SK 106 3136 DURING TAKEOFF ROLL, THE CREW NOTED A CAS MESSAGE FOR RT GENERATOR FAIL. THE CREW ABORTED TAKEOFF AND RETURNED TO GATE. MX INSPECTED THE SYSTEM AND REPLACED THE 1VE PANEL. MX RETURNED THE AC TO SERVICE WITH NO FURTHER DEFECTS. (K) 2H72 4T4 FRTA55NM E35NE 20050301000112005030100011NM 2005 3 1 UPS05443923 120050210A5711 FITTING BOEING747 747123 1384873NM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, RT WING REAR SPAR UPPER SPLICE FITTING AT BS 1241 HOLE NR 5 FOUND CRACKED .125 INCH. HOLE REWORKED PER BSB 747-57A2314. 2L74 4F A20WE 20050215001412005021500141EU 2005 2 15 USAA050027 120050101A5315D5347219320000 FLOORBEAM AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19713UW17339 1040 BFM - S1 - BEAM, 2.0 INCH X 2.0 INCH W X .02 INCH D, CORROSION; LEVEL 2; TASK NR JA-260-53500, BETWEEN FRAME 69-66, Y-765 MAIN CABIN FLOOR. REMOVED AND REPLACED BEAM IAW SRM. (K) 2L72 4F4 FRTA28NM E37NE 20050301000252005030100025NM 2005 3 1 DHL2005751502 120050225A5344AE5201 HINGE BOEING727 727264 138408MNM ZONE 200 BROKEN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01751DH 22982 MAIN CARGO DOOR, FAIL SAFEHINGE AFT SEGMENT AT FS 640.0, 14 LUGS BROKEN ON AIRFRAME SIDE. ACCOMPLISHED HFEC INSP OF HINGE ON MAIN CARGO DOOR AND FOUND NO OTHER HINGES CRACKED. REMOVED FASTENERS AND REMOVED (2 EA) SECTIONS OF INTERIOR GILLINER AT FS 640 TO GAIN ACCESS FOR HINGE REPLACEMENT. REMOVED FASTENERS AND REMOVED AFT SECTION OF FAILSAFE HINGE FUSELAGE SIDE AT FS 640. FABRICATED NEW SECTION OF HINGE FROM MS20001-16-7200 PO 0530161 HINGE MATERIAL IAW AEI MM CH 52 PG 15-20. POSITIONED AND DRILLED, DEBURRED NEW SECTION OF HINGE IAW B727 SRM 51-30-2. ALODINED AND PRIMED NEW SECTION OF HINGE. INSTALLED NEW SECTION OF HINGE IAW B727 SRM 51-30-2. RESTORED FINISH. REINSTALLED (2 EA) SECTIONS GILLINER. 2L73 4F A3WE 20050215001572005021500157NE 2005 2 15 ASOA05005 220050103A7261601R600501 LINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT ENGINE LOOSE A ASOAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO27875AS 7559 872200 DURING CLIMB OUT, CREW NOTICED FLUCTUATION IN RT ENG OIL PRESS OF 45-80 PSI WITH ALL OTHER INSTRUMENTS INDICATING NORMAL. AS CLIMB OUT PROGRESSED, OIL PRESS FLUCTUATIONS BEGAN DROPPING TOWARD 25 PSI ACCOMPANIED BY RT ENG OIL PRESS MESSAGE. QRH WAS COMPLIED WITH AND PWR LEVER REDUCED TO IDLE, STABILIZING OIL PRESSURE AT 27-32 PSI. CREW SHUTDOWN RT ENG AND DECLARED AN EMERGENCY. AC RETURNED AND LANDED SAFELY. INSP LUBE SYST AND TIGHTENED LINE TO OIL PRESS TRANSDUCER, PRESS SWITCH. ALSO, CHANGED LUBE ELEMENT, FLUSHED OIL TANK AND SUP LINE, INSPECTED, CLEANED SCREEN FOR CHIP DETECTOR. OPS AND LEAK CHECK GOOD. AC WAS PLACED ON OIL CONSUMPTON CK FOR 5 DAYS. AC OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050215001592005021500159EA 2005 2 15 ASOA05003 120050102A5210601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27884AS 7515 7513 DURING HANGAR MAINTENANCE, THE LOWER STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE LOWER STEP ON THE PASSENGER DOOR. (K) 2L72 4F4 FRTA21EA E15NE 20050215001642005021500164EA 2005 2 15 ASOA05028 120050114A3350OL3071BPEGPL LAMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27909EV 7858 DURING AN A-CHECK, THE LT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT OVERWING EMERGENCY EXIT LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050217000012005021700001NM 2005 2 17 USAA050086 120050101A5315 FLOORBEAM BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A K NONE O OTHER ININSP/MAINT 1 EA19522AU49282 23857 FLOORBEAM, 1INCH X 1 INCH AREA (2 EA) CORROSION; LEVEL 1; TASK NR C53-107-01, STA 328 FROM RBBL TO IB SEAT TRACK. REMOVED CORRODED SECTION, FABRICATED NEW AND INSTALLED IAW 53-10-51. (K) 2L72 4F4 FRTA16WE E21EU 20050211000832005021100083SO 2005 2 11 C2XA05SH006 120050127A532014521700007 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716520 145372 SHV - DURING C-CHECK, THE LT OMEGA BEAM AY FR 19-23 CORRODED. MAINTENANCE REMOVED THE DAMAGE AREA AND PERFORMED REPAIR IAW EMB 135 SRM 53-21-10 SECTION 9 FIGURE 208. THE AIRCRAFT WAS APPROVED FOR RETURNED TO SERVICE. 2L72 4F RTT00011AT 20050211000942005021100094NM 2005 2 11 AWXA200500140 120050107A5320654581211 STIFFENER BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 MCN - MAJOR REPAIR - DURING C-18 CHECK, A 3/8 INCH CRACK WAS FOUND IN FLOOR STIFFENER AT BS 328, LBL 27. MAINTENANCE REMOVED CRACKED STIFFENER AT BS 328, LBL 27, FROM WL 204 TO WL 208; FABRICATED A NEW REPLACEMENT STIFFENER PER DWG 65-45812; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050211000982005021100098NM 2005 2 11 AWXA200500144 120050106A5752654645522C TAB BOEING737 7373G7 1384595NM AILERON DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 MCN - MAJOR REPAIR - DURING C-18 CHECK, THE UPPER SURFACE OF RT AILERON TAB WAS FOUND DELAMINATED AT OUTBOARD END BETWEEN WBL 414.25 AND WBL 415.25. MAINTENANCE REMOVED DAMAGE FROM UPPER SURFACE OF RT AILERON TAB AND PERFORMED BOND REPAIR IAW B737-300 SRM 51-70-07, FIG 9. 2L72 4F RTA16WE 20050211001082005021100108NM 2005 2 11 UPS05443818 120050106A531165B0417815 FRAME BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 BS 940, STR 25L, FRAME FOUND CRACK. M/D BS 940 FRAME AT S-25L REPAIRED AS PER RS R-53-22-35244 AND EO B747-5310-21670-A. 2L74 4F A20WE 20050214000132005021400013EA 2005 2 14 MASA200500053 120050123A335059465 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSBROKEN A MASAK NONE O OTHER ININSP/MAINT 1 SW0777302 7302 BIL - LAS. EMERGENCY ESCAPE PATH LIGHTING FROM ROW 8 AFT INOP. MAINTENANCE FOUND THE RECEPTICLE BAD. A/C FERRIED TO PHX FOR REPAIRS. 1/24/05 MAINTENANCE REPLACED FLOOR TRACK (TOP) P/N 5872-8 AND REMOVED AND REPLACED ELECTRIC CABLE. 2L72 4F RTA21EA 20050214000202005021400020NM 2005 2 14 SWAA050371 120050208A53306550570 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29507SW 24184 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT AFT ENTRY DOOR UPPER HINGE CUTOUT, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050214000232005021400023SO 2005 2 14 RAIA00502007 120050204A3412102AU1AF PROBE EMB 145 EMB145LR 3260212SO NR 1 TAT FAILED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03829HK5077 145281 NR 1 TAT FAULT. MAINTENANCE REMOVED AND REPLACED NR 1 TAT PROBE. 2L72 4T RTT00011AT 20050214000492005021400049SO 2005 2 14 C2XA05IA019 120050203A335020131A BATTERY PACK EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713992112871419 145284 EWR - FLIGHT 2879, THE CREW REPORTED THAT THE EMERGENCY LIGHTS WOULD NOT STAY ON. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050214000702005021400070NM 2005 2 14 BB05007 120050210A3610212N30511 DUCT BOEING757 757225 1384959NM LT BLEED SYS BLOWN A USAAA UNSCHED LANDING D INFLIGHT SEPARATION CRCRUISE 1 EA19602AU 22196 PHL EN ROUTE, CREW NOTED A LEFT ENGINE BLEED DUCT LEAK. FLIGHT DIVERTED TO PHL. MAINTENANCE FOUND THE LEFT BLEED DUCT BLOWN OUT IN THE LEFT WING LEADING EDGE, AND ONE BLOW OUT MISSING AND ONE BLOW OUT PANEL DAMAGED. THE DUCT WAS REPLACED, REPAIRED THE LEFT GENERATOR FEEDER WIRE, REPLACED THE LEFT WING INBOARD LOWER PRESSURE RELIEF PANEL, AND REPAIRED SKIN DAMAGE. 2L72 4F RTA2NM 20050214000752005021400075EA 2005 2 14 QXEA200500155 120050115A5330 FITTING CNDAIRCL600 CL6002C10 1390015EA ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 FORWARD CENTER FUSELAGE, LEFT HAND FORWARD BAGGAGE BAY DOOR SURROUND STRUCTURE, FORWARD LOWER GUIDE FITTING GOUGED. REPAIRED IAW HORIZON AIR EA R-53-284 AND REO 670-53-31-021. 2L72 4F RTA21EA 20050214000932005021400093CE 2005 2 14 68236 120050105A3242 BRAKE ASSY BEECH 1900 1900D 1154162CE MLG ICED A AMWAO OTHER O OTHER TXTAXI/GRND HDL 1 CE07131YV UE131 ON TAXI OUT, A/C SLOWED TO A STOP ON THE ACTIVE TAXI WAY ENTERING THE RUNWAY AND WOULD NOT PROGRESS FWD. MX REMOVED ICE FROM THE BRAKES, A/C THEN WAS ABLE TO MOVE AND RETURNED TO GATE WITH NO FURTHER INCIDENT. CLEANED LEFT AND RIGHT BRAKES WITH DEICING FLUID. 2L72 4T RTA24CE 20050214000982005021400098NM 2005 2 14 SB05025 120050209A335020131A BATTERY BOEING737 7374B7 1384702NM EMERGENCY LIGHT DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19446US 24873 PIT - FOUND EMERGENCY AISLE LIGHTS AT ROWS 3, 4 AND 5 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY SUPPLY ASSEMBLY. 2L72 4F RTA16WE 20050214000992005021400099EA 2005 2 14 COMA0560114 120050206A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01716CA 7250 FLIGHT 5089 FLAPS FAIL CAUTION. RESET FLAP SYSTEM PER AD 98-20-01 AND DEFERRED MAINT PER MEL. 2L72 4F RTA21EA 20050214001092005021400109SO 2005 2 14 MASA200500072 120050131A335066367 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A MASAO OTHER O OTHER TXTAXI/GRND HDL 1 SW07839MJ 145416 AIRCRAFT WAS ON RON AND SCHEDULED FOR A ROUTINE INSPECTION. DURING THE WALKAROUND IT WAS DISCOVERED THE 4TH EMERGENCY LIGHTED FLOOR STRIP NOT ILLUMINATED. REPLACED THE LIGHTED FLOOR STRIP. OPERATIONAL CHECK GOOD. 2L72 4T RTT00011AT 20050214001112005021400111EA 2005 2 14 MASA200500077 120050201A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0777181 7181 EMERGENCY LIGHTS IN CABIN ILLUMINATE WITH THE FLIGHT DECK SWITCH IN THE ARMED POSITION. MAINTENANCE RESET THE CIRCUIT BREAKER, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050214001172005021400117NM 2005 2 14 SWAA050381 120050209A3350612825 BATTERY BOEING737 7373TO 138447GNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29697SW 23838 DURING SCHEDULED A2 CHECK, FOUND FWD SERVICE DOOR EMERGENCY EXIT LOWER LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20050214001202005021400120NM 2005 2 14 SWAA050384 120050209A143018A80101 BOLT BOEING737 7375H4 138449DNM LT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 DURING SCHEDULED C2 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE BOLT PER MM. 2L72 4F RTA16WE 20050214001212005021400121 2005 2 14 SWAA050385 420050209A256563550 SLIDE BOEING737 7377H4 1384404NM L1 & R1 DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29775SW 30590 DURING SCHEDULED HC2 CHECK, FOUND L1 AND R1 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED L1 AND R1 DOOR EVAC SLIDES PER MM. 2L72 4F RTA16WE 20050214001252005021400125EU 2005 2 14 AWXA200500183 120050208A33501013101 SIGN AIRBUS320 A320231 3930325EU EMERGENCY EXIT INOPERATIVE A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28628AW 67 ORD - EMERGENCY EXIT LIGHT INOPERATIVE AT AFT OVERWING EXIT, RIGHT SIDE WALL MOUNTED. MAINTENANCE REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY AT RIGHT AFT OVERWING EXIT; OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050422000562005042200056NM 2005 4 22 2005UALA00192 120050227A521065C80736256 SEAL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE L1 DOOR TORN A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29388UA 24663 UNABLE TO PRESSURIZE THE AIRCRAFT. DOOR 1L LEAKING. SEAL TORN BY LOWER HINGE AREA. REPLACED LOWER HINGE SEAL. REPLACED L1 DOOR SNUBBER. ADJUSTED DOOR STOPS. 2L72 4F4 FRTA16WE E2GL 20050214001582005021400158NM 2005 2 14 2005UALA00117 120050203A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29514UA 24839 EXTERNAL FUSELAGE SKIN DAMAGED STA 1618 AT STR 19L. INSTALLED SKIN AND STRINGER REPAIRS. 2L72 4F4 FRTA2NM E17NE 20050214001622005021400162EU 2005 2 14 YENA200517 120050204A5270 PROXIMITY SWITCH AIRBUS320 A320232 3930326EU PAX DOOR MALFUNCTIONED A YENAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 EA15594JB 2284 DOOR OPEN WARNING AFT LEFT. REMOVED AND REPLACED CABIN OVERPRESSURE INDICATOR IAW 52-73-21. REMOVED AND REPLACED WARNING LIGHT PANEL IAW AMM 52-73-21 L-2, DOOR INDICATION OPS CHECK NORMAL. REOCCURRED AT NEXT STATION. AFT LEFT CABIN DOOR ECAM AND DOOR INDICATED OPEN DURING TAXI. REMOVED AND REPLACED CABIN L-2 DOOR PROX SWITCH 17WV1 REF AMM 52-73-21 AND 52-71-00 FOR OPS CHECK AND AMM 52-71-11-04, SYSTEM OPS CHECK OK. NO FURTHER INDICATION. 2L72 4F RTA28NM 20050214001642005021400164NM 2005 2 14 SWAA050354 120050207A53156545834 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29603SW 27954 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM ZEE CHORD AT BS 270, FROM LBL 7 TO RBL 8, CORRODED. REMOVED AND REPLACED ZEE CHORD PER SRM. 2L72 4F RTA16WE 20050214001672005021400167NM 2005 2 14 2005UALA00118 120050203A2560 BRACKET BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE TORQUE BAR BROKEN A UALAK NONE O OTHER ININSP/MAINT 1 WP29662UA 27159 TORQUE BAR SUPPORT BRACKETS BROKEN. INSTALLED NEW SUPPORT BRACKETS. 2L72 4F4 FRTA1NM E24NE 20050214001692005021400169NM 2005 2 14 SWAA050357 120050208A53306545772 SKIN BOEING737 7373H4 1384600NM FUSELAGE WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29335SW 23939 DURING SCHEDULED SERVICE CHECK, FOUND UPPER FUSELAGE SKIN BETWEEN LEFT & RIGHT BS 870 AND BS 890, WORN. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20050214001712005021400171NM 2005 2 14 SWAA050359 120050208A53116546548 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29603SW 27954 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 767, FROM LBL 17 TO RBL 17, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20050214001742005021400174NM 2005 2 14 2005UALA00105 120050130A2613 OVERHEAT LOOP BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE WING-BODY OVRHT DAMAGED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29917UA 25384 DIVERTED TO SFO DUE TO WING BODY OVERHEAT INDICATION. CREW REPORTED RIGHT WING BODY OVERHEAT LIGHT ILLUMINATED DURING CLIMB. PERFORMED TROUBLESHOOTING OF THE OVERHEAT DETECTION SYSTEM AND CONFIRMED A SHORT WITH RIGHT WING LEADING EDGE OVERHEAT DETECTOR LOOP M1204. REPLACED OVERHEAT DETECTOR LOOP M1204. 2L72 4F4 FRTA16WE E2GL 20050215000892005021500089 2005 2 15 KBM2005F00008 420050104A34168800T ENCODER SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE ALT DIGITIZER INACTIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19966SH 3787 ALT DIGITIZER OFF. AOG (K) 1G71 3U3 U H9EU E19EU 20050215001022005021500102SO 2005 2 15 SIMA200500901 120050103A27303621005009 CONTROL UNIT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL AVIONIC BAY INOPERATIVE A SIMAO OTHER O OTHER CRCRUISE 1 SW21615AE 145087 DURING CRUISE FLIGHT THE CAPTAIN REPORTED A DUAL PITCH TRIM FAILURE. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT IAW MM AND CLEANED THE BACKUP TRIM SWITCHES. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200502358) (K) 2L72 4T4 FRTT00011ATTE6CH 20050215001122005021500112SO 2005 2 15 SIMA200501206 120050107A531314528473001 STRINGER EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21654AE 145437 DURING AN INSPECTION THE HOLDING STRINGER AT FRAME 50 AND STRINGER 13L WAS FOUND TO HAVE ONE DAMAGED HI-LOCK HOLE. REMOVED DAMAGED HOLDING STRINGER. INSTALLED NEW FASTENER IAW SRM. (SW21200502478) (K) 2L72 4T4 FRTT00011ATTE6CH 20050215001262005021500126EU 2005 2 15 A6WA200560004 120050112A2440 RECEPTACLE BAC 146 146300A 1500267EU LYC ALF502ALF502R5 41580NE SPARKS A A6WAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 GL31614AW E3132 EXTERNAL AC POWER RECEPTICAL SPARKS EXCESSIVELY AND SCORCHED WHEN ATTEMPTING TO CONNECT EXTERNAL POWER. AIRCRAFT ELECTRICAL SYSTEM OPS NORMAL. MAINTENANCE INSPECTED AREA, FOUND NO EVIDENCE OF SHORTING OR OPEN WIRES. (K) 2H74 4F4 FRTA49EU E6NE 20050215001282005021500128NE 2005 2 15 AMTA200500023 220050104A7261 B-NUT BOEING737 73783N 13844HINM CFMINTCFM567CFM567B2US 13802NE NR 2 ENGINE OIL LOOSE A AMTAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL11313TZ 32580 889716 ENGINE NR 2 OIL QUANTITY LOW. ENGINE OIL PRESSURE FLUCTUATIONS DURING APPROACH. OIL PRESSURE REACHED RED LINE AFTER CLEARING R/W. SHUTDOWN NR 2 ENGINE DURING TAXI. FOUND LOOSE B-NUT, TIGHTENED SAME ON TRANSFER GEAR BOX VENT LINE. LEAK CHECK, OK. (K) 2L72 4F4 FRTA16WE E2GL 20050215001392005021500139EA 2005 2 15 A6WA200540009 120050105A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE DENTED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31463AW 7878 DENT ON LT SKIN FROM FS 193, 00 TP FS 202.75 BETWEEN STR 18L AND STR 20L. REPAIRED DENT IN FUSELAGE SKIN FROM FS 193.00 TO FS 202.75 BETWEEN STR 18L AND 20L IAW BRAS EO. (K) 2L72 4F4 FRTA21EA E15NE 20050215001682005021500168EU 2005 2 15 USAA050028 120050101A5315D5347209200000 FLOORBEAM AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19713UW17339 1040 BFM - S1 - FLOORBEAM, 1.5 INCH L X 1.5 INCH W X .027 IN D, CORROSION; LEVEL 2; TASK NR JA-260-53500, FRAME 70 TO 66 Y765. REMOVED AND REPLACED BEAM IAW SRM. (K) 2L72 4F4 FRTA28NM E37NE 20050217000042005021700004 2005 2 17 GUU2005F00004 420050127A34206226190204 COMPUTER EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE AHRS SHORTED A GUUAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO17266AS 120188 DURING FLIGHT, FIRST OFFICERS EFIS TOP BUTTONS INOPERATIVE WITH STRONG BURNING SMELL. LANDED WITHOUT INCIDENT. MAINTENANCE FERRY. FOUND AHRS COMPUTER SHORTED. REMOVED AND REPLACED AHRS COMPUTER OPERATIONAL CHECK NORMAL. (K) 2L72 4T4 TRTA31SO E20NE 20050217000052005021700005NM 2005 2 17 USAA050199 120050102A5320 INTERCOSTAL BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE BURNED A USAAK NONE O OTHER ININSP/MAINT 1 EA19436US41647 24558 PIT - Q3 - INTERCOSTAL UNK SIZE- ARC BURN DAMAGE; GROUND STUD GD 3252, STA 344-360, LBL60 WL 204. REPLACED INTERCOSTAL IAW EA. (K) 2L72 4F4 FRTA16WE E21EU 20050217001382005021700138SO 2005 2 17 1408012205 120050122A27521159SCC20043 ACTUATOR GULSTMG1159 GIV 3980115SO TE FLAPS FAILED E N93AA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO13401QS4275 1408 IN FLIGHT FLAPS SELECTED 10 DEGREES, MOVED 7-8 DEGREES, STAB DID NOT MOVE AT ALL. 2L72 4F RTA12EA 20050217001422005021700142EA 2005 2 17 200501305 120050124A7330660526AS TRANSMITTER DHAV DHC2 DHC2MK1 2800102EA FUEL FLOW INOPERATIVE B HJBRO OTHER O OTHER NRNOT REPORTED 1 AL0562353 1363 FUEL FLOW TRANSDUCER HAS NO OUTPUT SIGNAL. 1H71 3R A806 20050217001442005021700144NE 2005 2 17 071711 220050128A7320 EEC SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE NR 1 ENGINE MALFUNCTIONED A UHLAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 GL1719XS 340A019 LEFT ITT WAS 60 DEGREES HIGHER THAN RIGHT ON TAKEOFF. DURING CLIMBOUT LEFT ITT CONTINUED CLIMBING TO 100 DEGREES DIFFERENCE. UNABLE TO MAKE CHARTED TQ ON LT ENGINE BY 30 PERCENT. ALL OTHER INDICATIONS NORMAL. AIRCRAFT RETURNED TO IAD AND MAINTENANCE REPLACED THE NR 1 ENGINE CONTROL UNIT. 2L72 4T4 TRTA52EU E8NE6 20050217001452005021700145NM 2005 2 17 AWXA200500196 120050128A5753693720910 GIMBAL JOINT BOEING737 7373G7 1384595NM TE FLAPS CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 MCN - MAJOR REPAIR - DURING C-16 CHECK GALVANIC CORROSION WAS FOUND ON RT INBOARD MID FLAP OUTBOARD GIMBAL SHAFT OUTER SUPPORT. MAINTENANCE REMOVED AND REPLACED RT INBOARD MID FLAP OUTBOARD GIMBAL SHAFT OUTER SUPPORT IAW B737-300 OHM 57-53-22. 2L72 4F RTA16WE 20050217001502005021700150NM 2005 2 17 AWXA200500200 120050128A5753694065110 GIMBAL JOINT BOEING737 7373G7 1384595NM TE FLAPS CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 MCN - MAJOR REPAIR - DURING C-16 CHECK EXFOLIATION CORROSION WAS FOUND ON RT INBOARD MID FLAP INBOARD GIMBAL OUTER SUPPORT. MAINTENANCE REMOVED AND REPLACED RT INBOARD MID FLAP INBOARD GIMBAL OUTER SUPPORT IAW B737-300 OHM 57-53-22. 2L72 4F RTA16WE 20050214001042005021400104EA 2005 2 14 COMA0560108 120050201A32304622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG UNRELIABLE A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01959CA10695397 7116 FLIGHT 5035 GEAR DISAGREE WARNING. REPLACED THE NLG PRIORITY VALVE. 2L72 4F RTA21EA 20050214001062005021400106EU 2005 2 14 SA05013 120050202A335032145410 EPSU AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT FAULTY A USAAK NONE L NO TEST ININSP/MAINT 1 EA19726US12067917 1136 PIT - THE AFT EMERGENCY POWER SUPPLY UNIT FAILED TEST. MAINTENANCE REPLACED THE AFT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20050214001142005021400114EU 2005 2 14 SA05016 120050206A3260839902 PROXIMITY SENSOR AIRBUS320 A320214 3930316EU MLG FAULTY A USAAO OTHER N FALSE WARNING CLCLIMB 1 EA19106US 1044 EN ROUTE MSY TO CLT - AFTER TAKEOFF, THE LANDING GEAR INDICATES DOWN AFTER THE LANDING GEAR LEVER WAS MOVED UP. UPON ARRIVAL, THE LANDING GEAR HAD AMBER -X- INDICATIONS ON THE WHEEL PAGE. MAINTENANCE REPLACED THE LEFT MAIN LANDING GEAR EXTENSION PROX SENSOR, FIN 23GA. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20050214001152005021400115 2005 2 14 SA05015 420050205A2565 LANYARD AIRBUS320 A320214 3930316EU ESCAPE SLIDE LOOSE A USAAO OTHER O OTHER TXTAXI/GRND HDL 1 EA19110UW 1112 CLT - PRIOR TO DEPARTURE, THE CABIN CREW COULD NOT GET ESCAPE SLIDE TO ARM AT DOOR 2R. MAINTENANCE SECURED A LOOSE LANYARD ON SLIDE AT 2R DOOR. SLIDE ARMING OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20050214001192005021400119NM 2005 2 14 SWAA050383 120050209A52406545871523 FRAME BOEING737 7375H4 138449DNM SERVICE DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 DURING SCHEDULED C2 CHECK, FOUND FWD SERVICE DOOR LOWER FRAME AT AFT LOWER STOP, CRACKED. REMOVED AND REPLACED FWD SERVICE DOOR MM. 2L72 4F RTA16WE 20050214001442005021400144NM 2005 2 14 AWXA200500181 120050124A5315654583470 STRAP BOEING737 7373G7 1384595NM FLOORBEAM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 MCN - MAJOR REPAIR - DURING C-16 CHECK A .75 INCH CRACK WAS FOUND IN STRAP LOCATED ON LOWER SIDE OF FLOORBEAM AT BS 314, LBL 11. MAINTENANCE STOP DRILLED CRACK ON STRAP; PERFORMED AN HFEC INSPECTION TO VERIFY CRACK CONTAINED; FABRICATED A REPAIR PLATE PER DWG 65-45834; INSTALLED REPAIR PART IAW B737-300 SRM 53-10-51 FIG 204. 2L72 4F RTA16WE 20050214001462005021400146NM 2005 2 14 AWXA200500182 120050104A5320654868719 ANGLE BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 MCN - MAJOR REPAIR - DURING C-18 CHECK A .25 INCH CRACK WAS FOUND IN L-ANGLE ON LT WHEEL WELL CUTOUT, FORWARD SIDE OF WEB AT OUTER CORNER JUST BELOW SUPPORT ROD BS 679, LBL 50. MAINTENANCE REMOVED CRACKED ANGLE (LOWER CHORD) AT BS 679, LBL 50; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 65-488687; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050214001602005021400160NM 2005 2 14 2005UALA00103 120050129A2131 CONTROLLER BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN PRESSURE FAILED A UALAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 WP29378UA 24653 AT 32,000 FEET CABIN, FLIGHT MADE EMERGENCY DESCENT FROM 32,000 TO 15,000 DUE TO CABIN PRESSURE PROBLEM. CABIN PRESSURE CONTROLLER FAILED. REPLACED CONTROLLER. 2L72 4F4 FRTA16WE E2GL 20050214001662005021400166NM 2005 2 14 2005UALA00104 120050129A2130 UNKNOWN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN PRESSURE UNKNOWN A UALAA UNSCHED LANDING O OTHER CLCLIMB 1 WP29327UA 24147 RETURNED TO SFO DUE TO PRESSURIZATION PROBLEM. FOUND EXCESSIVE LEAK AROUND E&E COMPARTMENT DOOR. REPLACED E&E COMPARTMENT DOOR SEAL. 2L72 4F4 FRTA16WE E2GL 20050214001682005021400168NM 2005 2 14 SWAA050356 120050208A3350101114 COVER BOEING737 7373A4 1384585NM EMERGENCY LIGHT DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 EMERGENCY EXIT LIGHT COVER AT ROW 13 ABC, FEEL OFF. REMOVED AND REPLACED LIGHT COVER PER MM. 2L72 4F RTA16WE 20050214001702005021400170NM 2005 2 14 SWAA050358 120050208A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29351SW 24572 DURING SCHEDULED CHECK, FOUND FUSELAGE SKIN AT BS 935, STRINGER 25R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050214001722005021400172NM 2005 2 14 P5CA0501315 120050206A2830107969 VALVE BOEING747 747249F 1384849NM FUEL JETTISON LEAKING A P5CAK NONE K FLUID LOSS ININSP/MAINT 1 EA15920FT 22237 DURING WALKAROUND OBSERVED FUEL LEAKING FROM RIGHT FUEL JETTISON MANIFOLD. REMOVED AND REPLACED RIGHT FUEL JETTISON NOZZLE VALVE PER BOEING MM 28-31-03. OPS CHECK OK. 2L74 4F A20WE 20050214001752005021400175NM 2005 2 14 2005UALA00106 120050130A5315 FLOORBEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29302UA 23643 CABIN FLOORBEAM HAS CORROSION REMOVAL BEYOND LIMITS AT STA 967 LBL 18. INSTALLED STRAP REPAIR. 2L72 4F4 FRTA16WE E2GL 20050214001782005021400178NM 2005 2 14 SWAA050362 120050208A531565C33940 FLOORBEAM BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CHORD AT BS 294, LBL 11, CORRODED. REMOVED AND REPLACED FLOORBEAM CHORD PER SRM. 2L72 4F RTA16WE 20050214001802005021400180NM 2005 2 14 SWAA050364 120050208A53156545810 FLOORBEAM BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CHORD AT BS 328, FROM LBL 49 TO RBL 55, CORRODED. REMOVED AND REPLACED CHORD SECTION PER SRM. 2L72 4F RTA16WE 20050215000112005021500011EU 2005 2 15 USAA050026 120050102A5321 FLOORBOARD AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19713UW17339 1040 BFM - S1- FLOORBOARD, 4.0 INCH X 2.5 INCH AREA, DELAMINATION, FR 20-24 +Y 500, -Z240. REPAIRED DAMAGED AREA IAW SRM. (K) 2L72 4F4 FRTA28NM E37NE 20050215000172005021500017SO 2005 2 15 SIMA200501905 120050111A532014522178005 SILL EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21735TS 145386 DURING AN IMBV INSPECTION OF AIRCRAFT, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. REMOVED AHT CORRODED SERVICE DOOR CENTER SILL AND INSTALLED SERVICEABLE SILL. REPAIR DONE IAW SRM. (SW21200502482) (K) 2L72 4F4 FRTT00011ATTE6CH 20050215000182005021500018EA 2005 2 15 ASOA05039 120050118A5320601R3501153 PLATE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27903EV 7621 DURING A C-CHECK, THE CARGO COMPARTMENT FLOOR LANDING SILL PLATE AT FS605 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO COMPARTMENT FLOOR LANDING SILL PLATE AT FS 605 IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050215000222005021500022SO 2005 2 15 SIMA200501203 120050104A532014522178005 SILL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21654AE 145437 DURING AN IMBV INSPECTION THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED SERVICE DOOR CENTER SILL. INSTALLED NEW SILL IAW SRM. (SW2120050478) (K) 2L72 4T4 FRTT00011ATTE6CH 20050215000532005021500053EU 2005 2 15 ASOA05025 120050112A33501021309111 LIGHT AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE CABIN MISSING A ASOAK NONE O OTHER ININSP/MAINT 1 SO27634AS 370 DURING HANGAR MAINTENANCE, THE EMERGENCY FLOOR LIGHT STRIP BULB AT ROW 14-B WAS FOUND MISSING FROM THE END OF THE WIRE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT STRIP AT ROW 14-B. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2H72 4T4 TRTA53EU E20NE 20050215000652005021500065EA 2005 2 15 ASOA05017 120050107A5210601R3198045 STEP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27830AS 7236 7236 DURING AN A-CHECK, THE LOWER STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE LOWER STEP ON THE PASSENGER DOOR. 2L72 4F4 FRTA21EA E15NE 20050215000682005021500068NM 2005 2 15 AMTA200500043 120050113A3397 CONNECTOR BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE EMERGENCY LIGHTSPULLED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11527AT 30886 EGRESS LIGHTS (FLOOR) FROM ROW 28 TO 30 INOPERATIVE. FOUND CONNECTOR PULLED OUT AT ROW 30. RESEATED CONNECTOR, OPS OK. 2L72 4F4 FRTA2NM E12EU 20050215001112005021500111EU 2005 2 15 S6G2005F00000 120050106A64201098131081 PIN AGUSTAA109 A109C 0260118EU ALLSN 250C 250C20 03013GL T/R HUB ASSY CRACKED E S6GAK NONE O OTHER ININSP/MAINT 1 GL1560NM 4070 A0198PIN 7651 AFTER DISASSEMBLY OF T/R HUB ASSY, REQUIRED DUE TO SCHEDULED 600 HOUR INSPECTION AND RETENTION STRAP REPLACEMENT (CLOSE TO RETIREMENT LIFE), FOUND STRAP PIN (PN 109-8131-08-1, TSN 4070) AND RETENTION STRAP (PN 109-8131-07-1 TSN 1735). ALSO, REPLACED STRAP PIN AND STRAP PLUG FOR OTHER RETENTION STRAP DUE TO SAME TSN AS CRACKED STRAP PIN. NOTE: ROTORCRAFT DIRECTORATE AND AGO ARE NOTIFIED. FOR FURTHER INFO CONTACT FSDO-GL15 1G72 3U3 U H7EU E4CE 20050215001612005021500161EA 2005 2 15 ASOA05001 120050101A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27848AS 7339 DURING A GROUND INSPECTION, THE LEFT FORWARD EXTERIOR EMERGEINCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT FORWARD EXTERIOR EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050217001432005021700143NM 2005 2 17 WRLA2005006 120050128A2841 INDICATOR DOUG MD11 MD11 3023602NM PWA 4460 PW4460 NE FUEL QTY MALFUNCTIONED A WRLAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO11279 48756 AIRCRAFT DIVERTED TO CHA DUE TO IN CRUISE NR 2 ENGINE FUEL QUANTITY LOW ALERT CAME ON, FUEL INDICATIONS WERE: NR 1 ENGINE 700 LBS, NR 2 ENGINE 0 LBS AND NR 3 ENGINE 600 LBS. MANIFOLD DRAIN ALERT CAME ON. SWAPPED CONTROLLERS BUT INDICATIONS REMAINED. PROBED FUEL LEVEL STICKS IAW MD11 AMM 12-11-07, NR 1 TANK STICK NR 4: 27", NR 2 TANK STICK NR 1: 14" & STICK NR 3: 14", NR 3 TANK STICK NR 4: 27". FUEL STICKS CORRESPOND WITH ASSOCIATED FUEL QUANTITY ON AIRCRAFT. PERFORMED FUEL QUANTITY BITE TEST IAW MM 28-42-00, SYSTEM OPERATIONS CHECKS GOOD. 2L73 4F4 FRTA22WE E24NE 20050217001472005021700147NM 2005 2 17 AWXA200500198 120050128A575369372099 GIMBAL JOINT BOEING737 7373G7 1384595NM TE FLAPS CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 MCN - MAJOR REPAIR - DURING C-16 CHECK EXFOLIATION CORROSION WAS FOUND ON LT INBOARD MID FLAP OUTBOARD GIMBAL SHAFT OUTER SUPPORT. MAINTENANCE REMOVED AND REPLACED LT INBOARD MID FLAP OUTBOARD GIMBAL SHAFT OUTER SUPPORT IAW B737-300 OHM 57-53-22. 2L72 4F RTA16WE 20050217001492005021700149NM 2005 2 17 AWXA200500201 120050128A5753655058516 PLATE BOEING737 7373G7 1384595NM TE FLAPS CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 MCN - MAJOR REPAIR - DURING C-16 CHECK EXFOLIATION CORROSION WAS FOUND ON RT INBOARD MID FLAP OUTBOARD GIMBAL INDEX PLATE. MAINTENANCE REMOVED AND REPLACED RT INBOARD MID FLAP OUTBOARD GIMBAL INDEX PLATE IAW B737-300 OHM 57-53-22. 2L72 4F RTA16WE 20050217001532005021700153NM 2005 2 17 AWXA200500213 120050131A555365538344 FITTING BOEING737 7373G7 1384595NM FUSE TO VERTICALCORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 MCN - MAJOR REPAIR - DURING C-16 CHECK CORROSION WAS FOUND ON RT OUTBOARD DRAG ANGLE FITTING, FUSELAGE TO VERTICAL STABILIZER FORWARD FACE. MAINTENANCE REMOVED CORRODED RT OUTBOARD DRAG ANGLE FITTING; FABRICATED A NEW REPLACEMENT FITTING PER DWG 65-53834; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050217001542005021700154NE 2005 2 17 COMA0560117 220050131A7200CF343A1 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE RIGHT MALFUNCTIONED A COMAO OTHER J WARNING INDICATION CRCRUISE 1 SO01806CA1011754 7359 807522 FLIGHT 5852 RT ENGINE OIL PRESSURE WARNING. REPLACED THE RT ENGINE. 2L72 4F4 FRTA21EA E15NE 20050217001592005021700159EU 2005 2 17 AWXA200500215 120050204A5320D53475765206 SILL AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28659AW 1166 SAL - MAJOR REPAIR - DURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND AROUND FASTENER HOLES ON SILL BEAM AT BULK CARGO DOOR FR 60+11 INCHES, STR 38 RT. MAINTENANCE CUT OUT DAMAGED SECTION OF SILL BEAM AT BULK CARGO DOOR FR 60+11 INCHES, STR 38 RT; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW A320 SRM 53-41-49 FIG 203. 2L72 4F RTA28NM 20050217001602005021700160EU 2005 2 17 AWXA200500216 120050204A5320D53475763206 SILL AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28659AW 1166 SAL - MAJOR REPAIR - DURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND AROUND FASTENER HOLES ON SILL BEAM AT BULK CARGO DOOR FR 61, STR 38 RT. MAINTENANCE CUT OUT DAMAGED SECTION OF SILL BEAM AT BULK CARGO DOOR FR 61, STR 38 RT; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW A320 SRM 53-41-49 FIG 203. 2L72 4F RTA28NM 20050217001632005021700163EU 2005 2 17 AWXA200500189 120050205A5347D53472090002 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28659AW 1166 SAL - MAJOR REPAIR - DURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM SEAT RAIL Y765, AT FR 66. MAINTENANCE REMOVED CORRODED FLOORBEAM SEAT RAIL Y765, FROM FR 64 TO FR 66; FABRICATED A NEW REPLACEMENT FLOORBEAM SEAT RAIL PER DWG 18D53472040; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050217001642005021700164EU 2005 2 17 AWXA200500212 120050205A5315D53112600200 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28659AW 1166 SAL - MAJOR REPAIR - DURING BC-4 CHECK CORROSION WAS FOUND ON FLOORBEAM Y520 AT FR 16. MAINTENANCE REMOVED CORRODED SECTION OF FLOORBEAM Y520 FROM FR 12 TO FR 16; FABRICATED A NEW REPLACEMENT SECTION OF BEAM PER DWG D53112825; INSTALLED REPAIR PART IAW A320 SRM 51-42-11. 2L72 4F RTA28NM 20050217001652005021700165EU 2005 2 17 AWXA200500210 120050205A5315D53472189204 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28659AW 1166 SAL - MAJOR REPAIR - DURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM -Y1292 AT FR 68. MAINTENANCE REMOVED CORRODED FLOORBEAM -Y1292 FROM FR 68 TO FR 70; FABRICATED A NEW REPLACEMENT FLOORBEAM PER DWG D53472040; INSTALLED REPAIR PART IAW A320 SRM 51-42-11. 2L72 4F RTA28NM 20050217001662005021700166EU 2005 2 17 AWXA200500203 120050205A5315D53472172205 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28659AW 1166 SAL - MAJOR REPAIR - DURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM -Y1292 AT FR 66+8 INCHES. MAINTENANCE REMOVED CORRODED FLOORBEAM -Y1292 FROM FR 66 TO FR 68; FABRICATED A NEW REPLACEMENT SECTION OF FLOORBEAM PER DWG D53472040; INSTALLED REPAIR PART IAW A320 SRM 51-42-11. 2L72 4F RTA28NM 20050217001672005021700167EU 2005 2 17 AWXA200500204 120050205A5320D53480043203 SILL AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28659AW 1166 SAL - MAJOR REPAIR - DURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SILL -Y1732 AT FR 66. MAINTENANCE CUT OUT DAMAGE IN LOWER SILL -Y1732 AT FR 66; FABRICATED A REPAIR ANGLE; INSTALLED REPAIR PART IAW A320 SRM 53-41-14, FIG 201. 2L72 4F RTA28NM 20050217001682005021700168EU 2005 2 17 AWXA200500205 120050205A5315D5347220922000 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28659AW 1166 SAL - MAJOR REPAIR - DURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM -Y765 AT FR 66. MAINTENANCE REMOVED CORRODED FLOORBEAM -Y765 AT FR 66; FABRICATED A NEW REPLACEMENT SECTION OF FLOORBEAM PER DWG D53472090; INSTALLED REPAIR PART IAW A320 SRM 51-42-11. 2L72 4F RTA28NM 20050217001692005021700169EU 2005 2 17 AWXA200500206 120050205A5315D53472090000 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28659AW 1166 SAL - MAJOR REPAIR - DURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM Y1292 AT FR 66+3 INCHES. MAINTENANCE REMOVED CORRODED FLOORBEAM Y1292 FROM FR 66 TO FR 69; FABRICATED A NEW REPLACEMENT SECTION OF FLOORBEAM PER DWG D53472090; INSTALLED REPAIR PART IAW A320 SRM 51-42-11. 2L72 4F RTA28NM 20050217001702005021700170EU 2005 2 17 AWXA200500207 120050205A5315D53472188204 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28659AW 1166 SAL - MAJOR REPAIR - DURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM Y1292 AT FR 68. MAINTENANCE REMOVED CORRODED FLOORBEAM Y1292 FROM FR 68 TO FR 70; FABRICATED A NEW REPLACEMENT SECTION OF FLOORBEAM PER DWG D53472040; INSTALLED REPAIR PART IAW A320 SRM 51-42-11. 2L72 4F RTA28NM 20050217001712005021700171EA 2005 2 17 VNAA0502002 120050205A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS ILLUMINATED A VNAAO OTHER J WARNING INDICATION DEDESCENT 1 GL05258PS 7941 ON DESCENT INTO PIT, WITH FLAPS STILL AT ZERO, THE FLAPS DEGRADED STATUS MESSAGE ILLUMINATED AND THE OVERSPEED RASTOR APPEARED ON THE AIRSPEED READ OUT. THE FLAPS OPERATED NORMALLY ON EXTENSION AND THE CREW MADE AN UNEVENTFUL LANDING. CONTRACT MAINTENANCE AT PIT PERFORMED AN OPERATIONAL TEST OF THE FLAPS IAW CRJ 200 AMM 27-54-00-710-801 AND AN OPERATIONAL TEST OF THE SKEW DETECTION SYSTEM IAW CRJ 200 AMM 27-51-15-710-802. ALL OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050217001722005021700172EU 2005 2 17 AALA20050089 120050206A3350 TERMINAL AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHT LOOSE A AALAK NONE O OTHER ININSP/MAINT 1 SW2190070 513 JFK - EMERGENCY EXIT LIGHT AT REAR OF RIGHT 2 DOOR IS INOPERATIVE. TIGHTENED TERMINALS ON LIGHT ASSEMBLY FOR EMERGENCY EXIT LIGHT AT REAR OF RIGHT 2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20050217001752005021700175NM 2005 2 17 QXEA200500202 120050206A3040SYZ50970 CONTROLLER DHAV DHC8 DHC8202 2809007NM WINDSHIELD HEAT MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION TOTAKEOFF 1 NM09349PH17659 486 SEA - LEFT WINDSHIELD HOT CAUTION LIGHT ILLUMINATED. DID CHECKLIST, LIGHT EXTINGUISHED. OAT -1 NO ICE, PRECIPITATION. MAINTENANCE REPLACED THE PILOTS WINDSHIELD CONTROLLER IAW AMM 31-41-00. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050217001762005021700176EA 2005 2 17 VNAA0502004 120050206A2750860D10018 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS FAILED A VNAAO OTHER O OTHER NRNOT REPORTED 1 GL05226JS1528 7895 AFTER LANDING AT CAK THE CREW OF FLIGHT 2286 REPORTED A FLAPS HALFSPEED STATUS MESSAGE. PSA MAINTENANCE REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT IAW CRJ 200 AMM 27-51-05-400-801. THE OPERATIONAL TEST WAS GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050217001772005021700177NM 2005 2 17 DL764050089 120050206A3810 LINE BOEING767 767432ER 1385134NM POTABLE WATER FAILED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27842MH 29715 AT FL320 APPROX 100 NME OF KSFO, COCKPIT FILLED UP WITH HAZE AND HOT SMOKEY SMELL. FLIGHT ATTENDANTS REPORTED RECEIVING ELECTRICAL SHOCKS FROM IFE ENTERTAINMENT SYSTEM. DECLARED EMERGENCY AND LANDED IN SFO. AFTER LANDING FOUND POTABLE WATER TANK EMPTY AND FWD E AND E COMPARTMENT FULL OF WATER. REPLACED CRACKED LINE. 2L72 4F RTA1NM 20050218000012005021800001NM 2005 2 18 2005UALA00077 120050119A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29341UA 24245 LT FUSE SKIN IS DENTED AT STA 897 BETWEEN STR 24L AND 25L. SUPPLEMENTAL DATA UPDATE, MAJOR REPAIR ACCOMPLISHED. CUT-OUT DAMAGE AND INSTALLED REPAIR DOUBLER, TRIPLER AND FILLER. 2L72 4F4 FRTA16WE E2GL 20050218000052005021800005NM 2005 2 18 05FDEA00129 120050120A5210 SKIN BOEING727 727200 138407ENM PAX DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25465FE 21289 CRACK AT FWD ENTRY DOOR CUTOUT UPPER HINGE, REPAIR PER EO 7-5330-7-2345 PT 2. REPAIRED FWD ENTRY DOOR CUT OUT UPPER HINGE CRACK PER EO 7-5330-7-2345 PART 2 2L73 4F RTA3WE 20050218000062005021800006 2005 2 18 2005UALA00086 420050121A2565B14056015 O-RING AIRCRUISERS BOEING757 757222 1384956NM PWA 2037 PW2037 NE SLIDE BOTTLE LEAKING A UALAK NONE O OTHER ININSP/MAINT 1 WP29548UA 0564 25396 DOOR 1 RIGHT SLIDE LOW BOTTLE PRESSURE. SUPPLEMENTAL DATA UPDATE FILLER VALVE O-RING LEAKING. REPLACED O-RING. 2L72 4F4 FRTA2NM E17NE 20050218000072005021800007NM 2005 2 18 05FDEA00134 120050121A5753NRC672501 VANE DOUG MD11 MD11 3023602NM ZONE 500 DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 LT HAND WING, INBOARD FLAP VANE LOWER CENTER SKIN FOUND DELAMINATED WHICH MEASURES 36.0 INCHES IN LENGTH AND 14.0 INCHES IN WIDTH AT STA 216.300 - 279.345 DELAMINATION AT LEFT HAND WING, INBOARD FLAP VANE LOWER CENTER SKIN AT STA 216.300 - 279.345 REPAIRED PER FEDEX EA 1-5750-81678. 2L73 4F RTA22WE 20050218000092005021800009EU 2005 2 18 AWXA200500037 120050112A2742 ACTUATOR AIRBUS320 A320232 3930326EU RUDDER FAILED A AWXAO OTHER JF WARNING INDICATION FLT CONT AFFECTED DEDESCENT 1 WP28654AW 1050 ON ARRIVAL, RECEIVED ECAM MESSAGE "F/CTL STABILIZER JAM. MX TROUBLESHOT IAW TSM 27-40-00-810-807, BITE TEST INDICATED "THS ACTR POS ERROR 9CE OF ELAC2", PERFORMED VISUAL INSPECTION OF MECHANICAL LATCHED INDICATOR, INDICATOR WAS NOT EXTENDED. TSM RECOMMENDS REPLACEMENT OF THS ACTUATOR (9CE). MAINTENANCE R & R THS ACT (9CE) IAW AMM 27-41-51-04, OPS TEST GOOD. COULD NOT VERIFY REASON FOR REMOVAL IN RELATION TO JAMMED CONDITION. 2L72 4F RTA28NM 20050218000142005021800014EU 2005 2 18 SA05019 120050209A335032145410 POWER SUPPLY AIRBUS320 A320214 3930316EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19117UW 1224 FOUND FAULT ON LEFT AFT EMERGENCY EXIT LIGHT. MAINTENANCE REPLACED THE EPSU. 2L72 4F RTA28NM 20050218000152005021800015SO 2005 2 18 RAIA00501039 120050117A7830 ACTUATOR EMB 145 EMB145LR 3260212SO THRUST REVERSER OUT OF ADJUST A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03810HK 145231 NR 2 ENGINE THRUST REVERSER DISAGREE. DEFERRED NR 2 ENGINE THRUST REVERSER PER MEL 78-34-00. ADJUSTED NR 2 THRUST REVERSER UPPER LEVER STOW ACTUATOR. 2L72 4T RTT00011AT 20050218000222005021800022 2005 2 18 SA05006 420050111A2565D30664105 SLIDE AIRBUSA319 A319112 3930323EU PASSENGER CABIN UNSECURE A USAAK NONE O OTHER ININSP/MAINT 1 EA19711UW7268 1955 1033 LGA - THE FRONT RIGHT SERVICE DOOR SLIDE COVER WAS FOUND LOOSE. UPON FURTHER INSPECTION, THE LACING AT THE BOTTOM OF THE SLIDE WAS ALSO FOUND LOOSE, ALLOWING FOR THE SLIDE TO EXPAND SLIGHTLY, DISPLACING THE SLIDE COVER. MAINTENANCE REPLACED THE SLIDE ASSEMBLY. OK FOR SERVICE. 2L72 4F RTA28NM 20050218000242005021800024NM 2005 2 18 05FDEA00082 120050112A5313 STRINGER BOEING727 727200 138407ENM FUSLEAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25235FE 21329 BS 640, RBL 15 WL 154 CORROSION ON STRINGER. REPAIRED PER SRM 53-10-3 2L73 4F RTA3WE 20050218000272005021800027NM 2005 2 18 05FDEA00120 120050118A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25465FE 21289 BS 410 DRILL START NOTED IN SKIN AT L-BAND ANTENNA NR 1 AT BS 410: AT FWD END LT MOUNT HOLE. DAMAGE ON SKIN AT FWD LT BAND ANTENNA MOUNT HOLE FOUND TO BE OUL.. CUT OUT DAMAGE , FABRICATED PART, ALODINED, PRIMED AND INSTALLED IAW SRM 53-10-1, 53-30-3 2L73 4F RTA3WE 20050218000332005021800033NM 2005 2 18 05FDEA00140 120050121A5311ABA7035 FRAME DOUG DC10 DC10 N/A-SDRNM ZONE 100 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25395FE 46629 STATION 322 ON LEFT SIDE OF NOSE FUSELAGE JUST BELOW COCKPIT FLOOR FRAME IS DENTED. REFERENCE NON-ROUTINE N01203. COMPLIED WITH FEDEX EA 8-5310-83962, 2L73 4F RTA22WE 20050218000362005021800036NM 2005 2 18 05FDEA00102 120050116A5320S1243787 INTERCOSTAL DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 FLOOR STRUCTURE INTERCOSTAL LOWER CHORD CORRODED AT STA 1821 TO STA 1841, LBL 27. REMOVED AS PER SRM 51-35-01 VOL II. NEW INTERCOSTAL FABRICATED AS PER DWG ACA7582 AND INSTALLED AS PER SRM 51-35-01 VOL II. 2L73 4F RTA22WE 20050218000392005021800039EU 2005 2 18 AWXA200500168 120050204A3350321454 EPSU AIRBUS320 A320232 3930326EU EMEGENCY LIGHT FAULTY A AWXAK NONE O OTHER ININSP/MAINT 1 WP28640AW493999178 448 DURING 8 DAY CHECK THE EMERGENCY PATH LIGHTS DID NOT ILLUMNATE IN THE FWD ENTRY AREA. MX REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT INCLUDING THE BATTERY PACK IAW 33-51-38-740-050. OPERATIONAL CHECK GOOD. 2L72 4F RTA28NM 20050218000402005021800040NM 2005 2 18 AWXA200500169 120050204A2560P4010021 BATTERY AIRBUSA319 A319132 3930340NM FLASHLIGHT DISCHARGED A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28831AW 1576 EMERGENCY EQUIPMENT - MAINTENANCE FOUND THE AFT EMERGENCY FLASHLIGHT INOPERATIVE. MX REMOVED AND REPLACED THE AFT EMERGENCY FLASHLIGHT. OPERATIONAL CHECK GOOD. 2L72 4F RTA28NM 20050218000412005021800041WP 2005 2 18 05FDEA00234 120050203A5397 WIRE HARNESS DOUG MD10 MD1010F 3022112WP FUSELAGE LOOSE A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25384FE 46617 WIRE BUNDLE 9102/AFT RIDING ON FWD RELAY PANEL OUTBOURD FRAME TOP RIGHT CORNER ,REF DWG SP10240263 FRAME 4 OF 4,G-G (31) REPOSITIONED AND SECURED WIRE BUNDLE AS PER EA.8-2400-84061 ON FWD RELAY PANEL. (WIRE INSTALATION FWD&AFT RELAY PANEL HARNESS ADJUST. 2L73 4F RTA22WE 20050218000422005021800042CE 2005 2 18 DJFA2005046 120050105A33101283800031 PANEL BEECH MU300 400A 1155402CE COCKPIT MELTED E DJFAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA23746TA RK146 KPSP - KLAS TRIP ID# 743429 CREW REPORTED THAT THEY HEARD A POPPING SOUND COMING FROM THE CIRCUIT BREAKER PANEL. ARCHING HAD OCCURED FROM THE BOTTOM OF THE CIRCUIT BREAKER PANEL FOLLOWED BY A NOTICABLE SMOKEY SMELL. APPROXIMATELY TEN SECONDS LATER THE ARCHING HAD EXTINGUISHED AND VAPOR HAD CLEARED. THE CIRCUIT BREAKER PANEL LIGHTS WERE FOUND TO BE INOPERATIVE, AND A SMALL MELTED AREA ON THE PANEL WAS HOT TO THE TOUCH. THE LIGHTING FOR THE PANEL WAS ISOLATED AS WELL AS THE HEAT SOURCE WHEN THE CIRCUIT BREAKER FOR THE PANEL LIGHTING WAS PULLED. THE FLIGHT PROCEDED WITHOUT FURTHER INCIDENT. MAINTENANCE ISSUED MEL 33-6 FOR THE CIRCUIT BREAKER PANEL LIGHTING.ON 14 JANUARY, 2005 MAINTENANCE REMOVED AND REPLACED THE 2H72 4F RTA16SW 20050218000442005021800044CE 2005 2 18 DELA200500002 120050128A325026182768 POSITION SENSOR LEAR LEAR 55 55LEAR 5170702CE NLG STEERING MALFUNCTIONED E DELAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03522WK 088 AFTER TAKE-OFF, NLG FAILED TO GO TO UP AND LOCKED POSITION. MLG SELECTED DOWN WITH 3 GREEN INDICATED. ACFT RETURNED TO DEPARTURE AIRPORT FOLLOWING 20 MIN OPS TO LOWER LANDING WEIGHT TO BELOW OVERWEIGHT LIMIT. UNEVENTFULL LANDING AND POSITION TO PARKING. PIC NOTED NOSE WHEEL STEERING INOPERATIVE/SLUGGISH ON TAXI. MX NOTED THAT UPON ELECTRICAL POWER APPLICATION THAT THE NOSE WHEEL STEERING MADE AN UNCOMMANDED REPOSITIONING. AS T/S CONTINUED NOSE WHEEL STEERING OBSERVED TO CONTINUALLY ROTATE STRUT. FAULTY OPS OF THE NLG STEERING FOLLOW-UP AND COMPUTER WAS FOUND. NOSE STEERING COMPUTER AND FOLLOW-UP WERE REPLACED AND SYSTEM TEST FOUND TO BE SATISFACTORY. LANDING GEAR EXTENSTION AND RETRACTION TESTS SATISFACTORY. 2L72 4F A10CE 20050222000012005022200001 2005 2 22 SWAA050418 420050214A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29375SW 26583 R2 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050215000812005021500081EU 2005 2 15 USAA050031 120050101A5315D5347218820400 FLOORBEAM AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19713UW 1040 BFM - S1 - FLOORBEAM, 3.0 INCH L X 2.0 INCH W X .025 INCH D, CORROSION; LEVEL 2; TASK NR JA260-53500, MAIN CABIN FLOOR, FR 68-69 Y 1292. REMOVED AND REPLACED FLOORBEAM IAW SRM. (K) 2L72 4F4 FRTA28NM E37NE 20050215000832005021500083EU 2005 2 15 USAA050002 120050107A5315 FLOORBEAM AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19737US 1245 CLT- RON- FLOORBEAM, 1 INCH SQUARE CORROSION AT FRAME 16, Y765 AT ATTACH FITTING. TRIMMED OFF DAMAGE, INSTALLED REPAIR ANGLES AND FILLER IAW EA AND SRM. (K) 2L72 4F4 FRTA28NM E37NE 20050215001162005021500116EA 2005 2 15 ASOA05006 120050103A5330 DOUBLER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27826AS 7210 DURING C-CHECK, THE PASSENGER DOOR FRAME DOUBLER AT THE AFT AREA UPPER IB OF THE UPPER AFT SEAL WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE PASSENGER DOOR FRAME DOUBLER AND OUTER SKIN IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050215001402005021500140EA 2005 2 15 ASOA05041 120050118A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27903EV 7621 DURING A C-CHECK, THE RT IB CLIP AT FS 280 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE RT IB CLIP AT FS 280. (K) 2L72 4F4 FRTA21EA E15NE 20050217001392005021700139NM 2005 2 17 AWXA200500194 120050123A57536546431280 SKIN BOEING737 7373G7 1384595NM FORE FLAP DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 MCN - MAJOR REPAIR - DURING C-16 CHECK THE UPPER SURFACE OF THE RT OUTBOARD FORE FLAP WAS FOUND DELAMINATED 10 INCHES FROM THE INBOARD END. MAINTENANCE REMOVED DAMAGED AREA OF UPPER RT OUTBOARD FORE FLAP; FABRICATED A CORE FILLER AND DOUBLER; BONDED REPAIR PARTS TO FLAP IAW B737-300 SRM 51-70-10 FIG 18. 2L72 4F RTA16WE 20050217001482005021700148NM 2005 2 17 AWXA200500199 120050128A575369406575 GIMBAL JOINT BOEING737 7373G7 1384595NM TE FLAPS CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 MCN - MAJOR REPAIR - DURING C-16 CHECK EXFOLIATION CORROSION WAS FOUND ON LT INBOARD MID FLAP INBOARD GIMBAL OUTER SUPPORT. MAINTENANCE REMOVED AND REPLACED LT INBOARD MID FLAP INBOARD GIMBAL OUTER SUPPORT IAW B737-300 OHM 57-53-22. 2L72 4F RTA16WE 20050217001512005021700151NM 2005 2 17 AWXA200500188 120050128A532069353654 FLOOR SUPPORT BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 MCN - MAJOR REPAIR - DURING C-16 CHECK 2 EACH CRACKS WERE FOUND IN FLOOR SUPPORT ATTACH ANGLE BETWEEN BS 380 AND BS 400, BL-0. MAINTENANCE REMOVED CRACKED FLOOR SUPPORT ATTACH ANGLE FROM BS 380 TO BS 400, AT BL-0; FABRICATED A NEW REPLACEMENT ATTACH ANGLE; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 12. 2L72 4F RTA16WE 20050217001572005021700157EA 2005 2 17 COMA0560118 120050204A3260 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA MLG ILLUMINATED A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01941CA 7050 FLIGHT 5130 GEAR DISAGREE WARNING. COULD NOT DUPLICATE. C/W EXTENSION AND RETRACTION CHECKS, NO DEFECTS FOUND. 2L72 4F RTA21EA 20050217001582005021700158EU 2005 2 17 AWXA200500214 120050204A5320D53475765206 SILL AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28659AW 1166 SAL - MAJOR REPAIR - DURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND AROUND FASTENER HOLES ON SILL BEAM AT BULK CARGO DOOR FR 60, STR 38 RT. MAINTENANCE CUTOUT DAMAGED SECTION OF SILL BEAM AT BULK CARGO DOOR FR 60, STR 38 RT; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW A320 SRM 53-41-49 FIG 203. 2L72 4F RTA28NM 20050217001612005021700161EU 2005 2 17 AWXA200500217 120050204A5320D53475765206 SILL AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28659AW 1166 SAL - MAJOR REPAIR - DURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND AROUND FASTENER HOLES ON SILL BEAM AT BULK CARGO DOOR FR 62+3 INCHES, STR 38 RT. MAINTENANCE CUTOUT DAMAGED SECTION OF SILL BEAM AT BULK CARGO DOOR FR 62+3 INCHES, STR 38 RT; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW A320 SRM 53-41-49 FIG 203. 2L72 4F RTA28NM 20050217001622005021700162EA 2005 2 17 COMA0570014 120050204A561013932112 WINDSHIELD CNDAIRCL600 CL6002C10 1390015EA COCKPIT CRACKED A COMAO OTHER O OTHER APAPPROACH 1 SO01653CA3241 10129 FLIGHT 5399 COPILOT WINDSHIELD IS CRACKED. REPLACED WINDSHIELD. 2L72 4F RTA21EA 20050217001742005021700174WP 2005 2 17 AALA20050088 120050206A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21493AA 49731 TUL - OVERHEAD EMERGENCY LIGHTS AT AFT GALLEY SERVICE DOOR INOPERATIVE. REPLACED BATTERY PACK AT STATION 1190R FOR OVERHEAD EMERGENCY LIGHTS AT AFT GALLEY SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050217001802005021700180EA 2005 2 17 VNAA0502005 120050207A21331037708 OUTFLOW VALVE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN PRESSURE FAILED A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL05248PS2260 7925 DURING CLIMB AFTER TAKEOFF (MSP TO PHL) CABIN ALT CAUTION LIGHT ILLUMINATED. CREW OF FLIGHT 2473 FOLLOWED QRH PROCEDURES. PRESSURIZATION WOULD NOT RESET AND INOPERATIVE IN AUTO AND MANUAL MODES. THE CREW ELECTED TO DIVERT TO DAY WHERE THE AIRCRAFT MADE AN UNEVENTFUL LANDING. PSA MAINTENANCE TROUBLESHOT THE SYSTEM AND DETERMINED PRIMARY OUTFLOW VALVE FAULTY. DUE TO UNAVAILABILITY OF A SERVICEABLE OUTFLOW VALVE PRESSURIZATION SYSTEM DEFERRED IAW WITH MEL 21-32-01 CODE C. AIRCRAFT THEN RELEASED FOR SERVICE. UPON RECEIPT OF A SERVICEABLE OUTFLOW VALVE PSA MAINTENANCE REMOVED AND REPLACED THE PRIMARY OUTFLOW VALVE IAW CRJ 200 AMM. ALL OPERATIONAL TESTS GOOD. MEL CLEARED AND AIRCRAFT RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050218000082005021800008NM 2005 2 18 05FDEA00135 120050121A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25235FE 21329 REPAIR ON FLOORBEAM UPPER CORD BS 344, WL 208, LBL 20.5 TO RBL 70, 90.5 INCHES LONG NEEDS EVALUATION TO DETERMINE PER SRM OR APPROVED DATA . REMOVED AND REPLACED FLOORBEAM UPPER CHORD BS 344, WL 208, LBL 65 TO RBL 65 IAW SRM 51-30-2 & 53-10-8 2L73 4F RTA3WE 20050218000132005021800013EU 2005 2 18 SA05018 120050208A3350 LIGHT AIRBUSA321 A321211 3930370EU CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19165US 1431 FOUND THE EMERGENCY LIGHT TEST SYSTEM INOPERATIVE. MAINTENANCE RESET THE CIDS SYSTEM. TEST PERFORMED SATISFACTORILY. 2L72 4F RTA28NM 20050218000232005021800023WP 2005 2 18 UPS05843690 120050120A5230 DOOR DOUG DC8 DC871F 302199DWP CARGO BAY OPEN A IPXAO OTHER O OTHER LDLANDING 1 SO01729UP 46029 NR 3 PIT DOOR OPENED ON LANDING A/C OOS. 11832 ASSIGNED TO THIS WRITE UP 0557984 C/W ALL ITEMS ON ECA FORM 11832, SYS OPS CK OK. 2L74 4F RT4A25 20050218000342005021800034WP 2005 2 18 05FDEA00151 120050120A5280 SKIN DOUG DC10 DC1010 3022110WP ZONE 700 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25365FE 46601 LT MLG DOOR HAS CRACKED SKIN AND DAMAGED HINGE FITTINGS PN. 2L73 4F A22WE 20050222000742005022200074NM 2005 2 22 USAA050003 120050107A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19376US54857 22955 CLT - FOUND SKIN CRACKED 1.750 INCH, STATION 74-2 AT STRINGER 19R. INSTALLED DOUBLER IAW 53-00-01. (M) 2L72 4F RTA16WE 20050222000792005022200079NM 2005 2 22 USAA050043 120050104A53206553595501 REVEAL BOEING737 737301 1384611NM SERVICE DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19590US51294 23935 PIT - FOUND REVEAL CRACKED 2 INCHES, UPPER FORWARD CORNER FORWARD SERVICE DOOR REVEAL. REPLACED REVEAL PER EA 79744. (M) 2L72 4F RTA16WE 20050222000922005022200092EU 2005 2 22 USAA050153 120050126A5315 FLOORBEAM AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19101UW 0936 CLT - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH, FR 66 (Y765). INSTALLED REPAIR ANGLES IAW EA 96224. (M) 2L72 4F RTA28NM 20050222000942005022200094NM 2005 2 22 USAA050023 120050112A5330 SKIN BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19447US 24874 CLT - FOUND SKIN 2.5 INCHES CRACK, STATION 727G STRINGER 22L. INSTALLED DOUBLER IAW SRM 53-00-1. (M) 2L72 4F RTA16WE 20050222000952005022200095NM 2005 2 22 USAA050044 120050110A5330 SKIN BOEING737 7374B7 1384702NM FUSELAGE DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19779AU39025 24996 PIT - FOUND SKIN OUT OF LIMITS 2 INCHES BY 1.6250 INCH BY .018 INCH, RT SIDE, STATION 420 STRINGER 14R. REMOVED DAMAGE, INSTALLED DOUBLER REPAIR PER SRM 53-00-01 FIG 231. (M) 2L72 4F RTA16WE 20050222001222005022200122NM 2005 2 22 USAA050061 120050101A5730BMS44 SKIN BOEING737 7373B7 1384580NM WING DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19518AU49476 23704 PIT - FOUND LOWER SKIN CORE BOND DELAMINATED 6 INCH BY 4.5 INCH AREA, 34 INCHES FROM F/B EDGE. REMOVED DAMAGE, INSTALLED FILLERS, DOUBLERS PER SRM 51-70-10. (M) 2L72 4F RTA16WE 20050222001252005022200125NM 2005 2 22 USAA050064 120050111A575465C2660399A SKIN BOEING737 7373B7 1384580NM L/E SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19374US 22953 PIT - FOUND TOP SKIN CORE BOND DELAMINATED 2.5 INCH BY 2.5 INCH AREA, NR 3 SLAT INBOARD TRAILING EDGE. REMOVED DAMAGED SKIN AND CORE, INSTALLED NEW CORE, DOUBLERS PER SRM 51-70-10. (M) 2L72 4F RTA16WE 20050222001282005022200128NM 2005 2 22 USAA050070 120050101A5330 SKIN BOEING737 7373B7 1384580NM FUSLEAGE CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19522AU49282 23857 PIT - FOUND SKIN CHAFED, .023 INCH DEEP, SKIN STATION 860-880 AT DORSAL FIN. INSTALLED DOUBLER, TRIPLER AND BONDED STAINLESS RUB STRIP PER SRM 53-60-01 FIG 209. (M) 2L72 4F RTA16WE 20050222001312005022200131NM 2005 2 22 USAA050006 120050110A5754 SKIN BOEING737 737301 1384611NM L/E SLAT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19574US49365 23739 CLT - FOUND SLAT SKIN CRACKED 1 INCH, LOWER TRAILING EDGE OF SKIN, 6 INCHES OUTBOARD OF ACTUATOR ON THE NR 4 LE SLAT. INSTALLED DOUBLER. (M) 2L72 4F RTA16WE 20050222001322005022200132NM 2005 2 22 USAA050024 120050101A5315 FLOORBEAM BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19518AU 23704 PIT - FOUND CHORD AND ANGLE CORRODED AT SCREW HOLES, STATION 344 RBBL -13 TO LBBL -24. CORROSION LEVEL 1, TASK NR C53-107-02. REMOVED T-CAP, FABRICATED NEW CHORD AND ANGLE SPLICES, INSTALLED PER SRM 53-10-51. (M) 2L72 4F RTA16WE 20050222001342005022200134NM 2005 2 22 USAA050054 120050101A532069371024 ANGLE BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19522AU49282 23857 PIT - FOUND ANGLE CRACKED .25 INCH LONG, EDGE OF SUPPORT ANGLE AT FS 294.5, FORWARD LOWER CORNER AT FLOOR LINE. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-40-02. (M) 2L72 4F RTA16WE 20050222001352005022200135NM 2005 2 22 USAA050057 120050101A5320 BEAM BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19522AU49282 23857 PIT - FOUND BEAM CRACKED 1 INCH, FORWARD OF FRAME 639 RIGHT SIDE CREASE BEAM. MODIFIED PART C/C 1109171 AND INSTALLED PER TYPICAL REPAIR 53-10-02 REV A. (M) 2L72 4F RTA16WE 20050222001372005022200137NM 2005 2 22 USAA050048 120050101A5313 STRINGER BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19522AU53410 23857 PIT - FOUND STRINGER CRACKED .125 INCH, FRAME 380 AT S16R. REPAIR FILLER AND FABRICATED SHEAR TIE PR SRM 53-00-07. (M) 2L72 4F RTA16WE 20050222001392005022200139NM 2005 2 22 USAA050058 120050113A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19353US48785 23556 CLT - FOUND SKIN CRACKED 1 INCH, STATION 727D AT STRINGER 23L. INSTALLED DOUBLER IAW SRM 53-00-01. (M) 2L72 4F RTA16WE 20050222001402005022200140NM 2005 2 22 USAA050052 120050101A5753 SKIN BOEING737 7373B7 1384580NM RT MIDFLAP CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19522AU49282 23857 PIT - FOUND FLAP SKIN LEADING EDGE WITH CHAFE MARK .020 BY 4.25 INCH LONG BY .5 INCH WIDE, RT OUTBOARD MID FLAP ADJACENT TO OUTBOARD FLAP TRACK. (M) 2L72 4F RTA16WE 20050222001422005022200142NM 2005 2 22 USAA050056 120050101A53206623574 ATTACH FITTING BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19522AU49282 23857 PIT - FOUND ATTACH CLIP CRACKED .125 INCH, STRINGER TO FRAME ATTACH CLIP AT BS 706, S-11L. DEFECTIVE PART REPLACED WITH IDENT PART PER BOEING DWG 66-23574. (M) 2L72 4F RTA16WE 20050222001432005022200143NM 2005 2 22 USAA050066 120050101A5320 ANGLE BOEING737 7373B7 1384580NM FUSELAGE BROKEN A USAAK NONE O OTHER ININSP/MAINT 1 EA19522AU49282 23857 PIT - FOUND ANGLES BROKEN, RAM AIR INLET DUCT UPPER SUPPORT LEFT SIDE. DEFECTIVE PART REPLACED WITH IDNT PART PER TYPICAL REPAIR 21-50-07C. (M) 2L72 4F RTA16WE 20050222001452005022200145NM 2005 2 22 USAA050071 120050104A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE TORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19522AU49282 23857 PIT - FOUND SKIN WITH .5 INCH TEAR, STATION 1025 LBBL 33. PART REPLACED PR JOB CARD J3-58-53500-C-010. (M) 2L72 4F RTA16WE 20050222001462005022200146NM 2005 2 22 USAA050072 120050101A5320 INTERCOSTAL BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19522AU49282 23857 PIT - FOUND INTERCOSTAL CRACKED .125 INCH, FORWARD END INTERCOSTAL FASTENER BS 328 LBBL 44. REPLACED INTERCOSTAL PER SRM 53-10-51. (M) 2L72 4F RTA16WE 20050222001472005022200147NM 2005 2 22 USAA050073 120050101A5320 BEAM BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19522AU49282 23857 PIT - FOUND BEAM CRACKED .75 INCH, STATION 616 BELOW RT SIDE CREASE BEAM. ROUTED OUT CRACK, INSTALLED FILLER AND REPAIR ANGLE PER TYPICAL REP 53-62-01. (M) 2L72 4F RTA16WE 20050222001492005022200149NM 2005 2 22 USAA050050 120050101A5320 INTERCOSTAL BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 NM01522AU49282 23857 PIT - FOUND INTERCOSTAL CRACKED .25 INCH, INTERCOSTAL AT BL0 BETWEEN STATION 344 AND 360. INSTALLED DOUBLER, STOP DRILLED PER SRM 51-70-11. (M) 2L72 4F RTA16WE 20050222001512005022200151NM 2005 2 22 USAA050060 120050101A5730BMS44 SKIN BOEING737 7373B7 1384580NM WING DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19518AU49476 23704 PIT - FOUND LOWER SKIN CORE BOND DELAMINATED 6 INCH BY 6 INCH AREA, BOTTOM SIDE 14 INCHES FROM INBOARD END. REMOVED DAMAGE, INSTALLED INTERNAL DOUBLERS AND FILLRS PER SRM 51-70-10. (M) 2L72 4F RTA16WE 20050217001402005021700140NM 2005 2 17 AWXA200500195 120050123A5753 SKIN BOEING737 7373G7 1384595NM FORE FLAP DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 MCN - MAJOR REPAIR - DURING C-16 CHECK THE UPPER SURFACE OF THE RT OUTBOARD FORE FLAP WAS FOUND DELAMINATED 103.5 INCHES FROM THE OUTBOARD END. MAINTENANCE REMOVED DAMAGED AREA OF UPPER RT OUTBOARD FORE FLAP; FABRICATED A CORE FILLER AND DOUBLER; BONDED REPAIR PARTS TO FLAP IAW B737-300 SRM 51-70-10 FIG 18. 2L72 4F RTA16WE 20050217001462005021700146NM 2005 2 17 AWXA200500197 120050128A575365505889 GIMBAL JOINT BOEING737 7373G7 1384595NM TE FLAPS CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 MCN - MAJOR REPAIR - DURING C-16 CHECK GALVANIC CORROSION WAS FOUND ON LT INBOARD MID FLAP OUTBOARD GIMBAL SHAFT INDEX PLATE. MAINTENANCE REMOVED AND REPLACED LT INBOARD MID FLAP OUTBOARD GIMBAL SHAFT INDEX PLATE IAW B737-300 OHM 57-53-22. 2L72 4F RTA16WE 20050217001732005021700173EU 2005 2 17 AALA20050090 120050206A3350 CONNECTOR AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHT LOOSE A AALAK NONE O OTHER ININSP/MAINT 1 SW2190070 513 JFK - CEILING MOUNTED EMERGENCY EXIT LIGHT AT SEAT 3G INOPERATIVE. RESEATED CONNECTOR ON LIGHT ASSEMBLY FOR CEILING MOUNTED EMERGENY EXIT LIGHT AT SEAT 3G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20050217001792005021700179SO 2005 2 17 RAIA00502011 120050207A2133 CONNECTOR EMB 145 EMB145LR 3260212SO OUTFLOW VALVE LOOSE A RAIAA UNSCHED LANDING O OTHER CLCLIMB 1 CE03823HK 145475 STL - AT 3700 HAD LARGE CABIN CLIMB/DESCENT SWINGS IN AUTO AND MANUAL. MAINTENANCE SECURED LOOSE DUCT ON NR 2 PACK AND OUTFLOW VALVE CONNECTOR. 2L72 4T RTT00011AT 20050218000022005021800002CE 2005 2 18 DXTA200500579 120050204A2910 LINE CESSNA750 750 2076810CE HYD SYSTEM CHAFED E DXTAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL07934QS 7500034 FL 200 ON CLIMBOUT LOST LEFT HYDRAULIC SYSTEM FOLLOWED BY THE PTU. TURNED ON "A" PUMP LOST THAT ALSO. ON DESCENT LOST RIGHT SYSTEM. BLEW DOWN THE GEAR, USED EMERGENCY BRAKES. SIGNIFICANT SMOKE IN THE COCKPIT. CLEANED ALL HYDRAULIC FLUID. REPLACED HYDRAULIC LINE WHICH CHAFED THROUGH WARM AIR DUCT. REPLACED AIR DUCT ALSO. IAW MODEL 750 M.M. 29-10-01. SERVICED HYDRAULIC SYSTEMS AND BLED A & B HYDRAULIC SYSTEMS. IAW 750 M.M. 12-10-15. POST RUN PLANE TO PURGE BLEED AIR SYSTEM. LEAK & OPERATIONAL CHECK GOOD. 2L72 4J RTT00007WI 20050218000032005021800003 2005 2 18 2005UALA00085 420050121A2565B192461 PLATE BOEING777 777222 1385219NM PWA 4360 PW4360 13816NM ESCAPE SLIDE DISTORTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29229UA 30557 BOTTLE WOULD NOT FIRE WHEN THE FIRING CABLE WAS PULLED, THEREFORE THE SLIDE WOULD NOT INFLATE. SUPPLEMENTAL DATA UPDATE RESERVOIR VALVE ASSEMBLY COVER PLATE WAS PUSHED IN CAUSING PULLEY TO NOT ROTATE. REPLACED COVER PLATE AND PULLEY ASSEMBLY. 2L72 4F4 RRTT0001SE A18NM 20050218000042005021800004NM 2005 2 18 2005UALA00078 120050119A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29341UA 24245 STA 341-359 HAS 3 DENTS ABOVE STR 21R. CUT OUT DAMAGE AND INSTALLED DOUBLER AND TRIPLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20050218000162005021800016NM 2005 2 18 AT0500002 120050110A213192144A020101 CONTROLLER BOEING717 717200 1383700NM CABIN AIR INOPERATIVE A ZZDAO OTHER J WARNING INDICATION CRCRUISE 1 SO15894AT 55046 AT CRUISE ALTITUDE CABIN INFLOW LOW MESSAGE CAME ON QRH PROCEDURES FOLLOWED AND DESCENT TO FL 24.0 WA BEGUN. CABIN CONTINUED TO CLIMB W/OUT FLOW, VALVE CLOSED DURING DESCENT. CABIN ALT REACHED 12,000 AT MAXIMUM. DESCENT CONTINUED UNTIL CABIN BELOW 10,000'. LATER DURING FLIGHT CABIN INFLOW LOW MESSAGE WENT AWAY, MANUAL PRESSURE WAS USED AT A/C ALT AT 11,000. REMOVED AND REPLACED NR 2 CPC. 2L72 4F TRA6WE 20050218000282005021800028NM 2005 2 18 05FDEA00121 120050118A5320 STOP FITTING BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25465FE 21289 BS 950 LBL 40 WL 149 LT WHEEL WELL AFT BODY DOOR STOP FITTING ASSY HAS CRACKED ANGLE. 2L73 4F RTA3WE 20050218000292005021800029EU 2005 2 18 SA05017 120050208A335032145410 EPSU AIRBUSA321 A321211 3930370EU EMERGENCY LIGHT FAULTY A USAAK NONE L NO TEST ININSP/MAINT 1 EA19165US14073 1431 TPA - THE AFT EMERGENCY POWER SUPPLY UNIT REQUIRED REPLACEMENT. MAINTENANCE REPLACED THE AFT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20050218000312005021800031EA 2005 2 18 QXEA200500057 120050111A2612 FIRE LOOP CNDAIRCL600 CL6002C10 1390015EA RT ENGINE SHORTED A QXEAO OTHER N FALSE WARNING CRCRUISE 1 NM09609QX 10031 CREW REPORTS THAT THEY RECEIVED A FIRE SYSTEM FAULT STATUS MESSAGE CAME ON DURING CRUISE FLIGHT AND WENT OUT ON DESCENT. MAINTENANCE INSPECTED THE AIRCRAFT AND INTERROGATED THE MDC. THE MDC REPORTS THE RT ENGINE LOOP HAS AN INTERMITTENT SHORT CIRCUIT. THE SYSTEM WAS PLACED ON MEL. REPORT TO REMAIN OPEN PENDING FURTHER INFORMATION. PERFORMED THE PROCEDURE IAW THE FAULT ISOLATION MANUAL AND PERFORMED OPERATIONAL CHECKS OF THE FIDEX SYSTEM. ALL CHECKS WERE GOOD AND NO FAULTS WERE NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20050218000352005021800035NM 2005 2 18 05FDEA00100 120050116A5320AGA70261 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 LONGERON 49 SPLICE LT CORRODED AT STA 5-119. CORROSION REMOVED AS PER SRM 51-21-01 VOL II. 2L73 4F RTA22WE 20050222000582005022200058NM 2005 2 22 USAA050059 120050101A5310 DOOR FRAME BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19443US38634 24842 PIT - FOUND FRAME CORRODED 1 INCH IN DIAMETER, STATION 492.4, FORWARD CARGO DOOR FRAME AFT LOWER STOP FITTING. CUT OUT DAMAGE, TRIMMED ANGLE TO SIZE AND SHAPE, FABRICATED FILLER, TREATED, PRIMED PER SRM 51-70-11. (M) 2L72 4F RTA16WE 20050222000892005022200089NM 2005 2 22 USAA050049 120050101A5311 FRAME BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19522AU49282 23857 PIT - FOUND RIVET CRACKED .125 INCH, FRAME 360, RIVET AT S9L. INSTALLATION OF TWO, REPAIR ANGLES PER TYP REP 53-10-20A. (M) 2L72 4F RTA16WE 20050222001212005022200121NM 2005 2 22 USAA050046 120050106A14306546431279 RIVET BOEING737 7373B7 1384580NM LT FOREFLAP LOOSE A USAAK NONE O OTHER ININSP/MAINT 1 EA19374US 22953 PIT - FOUND LT WING FOREFLAP 42 LOOSE RIVETS, LT WING OUTBOARD FOREFLAP APPROX 42 INCHES. DEFECTIVE PART REPLACED WITH IDENT PART. (M) 2L72 4F RTA16WE 20050222001242005022200124NM 2005 2 22 USAA050063 120050107A575465C26602214A SKIN BOEING737 7373B7 1384580NM L/E SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU53313 23700 PIT - FOUND TOP SKIN CORE BOND DELAMINATED 3 INCHES BY 3 INCHES, NR 5 SLAT OUTBOARD TRAILING EDGE. REMOVED DAMAGE, INSTALLED NEW CORE, FILLERS, DOUBLERS PER SRM 51-70-10. (M) 2L72 4F RTA16WE 20050222002862005022200286NM 2005 2 22 SWAA050498 120050220A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 450, BETWEEN STRINGERS 28R AND 28L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20050222002872005022200287NM 2005 2 22 SWAA050419 120050214A57436959886 FITTING BOEING737 7373H4 1384600NM LT MLG DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29654SW 28399 DURING SCHEDULED A1 CHECK, FOUND LT MLG OUTBOARD AFT HANGER FITTING, DAMAGED. REMOVED AND REPLACED FITTING PER MM. 2L72 4F RTA16WE 20050222002882005022200288NM 2005 2 22 SWAA050420 120050214A53116546525 FRAME BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 380, STRINGER 9R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20050222002892005022200289NM 2005 2 22 SWAA050421 120050214A53206551698 SPLICE BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND 2 EACH STRINGER SPLICES FROM BS 400 TO BS 420, STRINGER 4R, CRACKED. REMOVED AND REPLACED STRINGER SPLICES PER SRM. 2L72 4F RTA16WE 20050222002932005022200293NM 2005 2 22 SWAA050500 120050220A53306545778 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 946.5, STRINGER 11R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20050222002942005022200294 2005 2 22 SWAA050501 420050220A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR UNSERVICEABLE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 DURING SCHEDULED PM CHECK, FOUND L1 DOOR EVAC SLIDE PRESSURE IND OUT OF LIMITS. REMOVED AND REPLACED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050222002952005022200295NM 2005 2 22 SWAA050502 120050220A3350101331 LENS BOEING737 7373A4 1384585NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29679AA 23291 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM. 2L72 4F RTA16WE 20050222002982005022200298NM 2005 2 22 SWAA050482 120050218A3350OL3071BPEGL LIGHT BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29424WN 29828 EEPLS LIGHT AT ROW 1 ABC, INOP. RELAMPED PER MM. 2L72 4F RTA16WE 20050222002992005022200299NM 2005 2 22 SWAA050440 120050215A53156545410 FLOORBEAM BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29502SW 24179 DURING SCHEDULED 1/2D CHECK, FOUND 4 EACH CRACKS ON FLOORBEAM UPPER CHORD BETWEEN BS 659 AND BS 668, RBL 24.82. REPAIRED FLOORBEAM CHORD PER EA. 2L72 4F RTA16WE 20050222003012005022200301NM 2005 2 22 SWAA050401 120050211A256069769861 LATCH BOEING737 7373H4 1384600NM COCKPIT OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29335SW 23939 F/O'S ESCAPE SLIDE ROPE COVER RELEASE KNOB, STUCK. ADJUSTED AND LUBED LATCH PER MM. 2L72 4F RTA16WE 20050222003022005022200302NM 2005 2 22 SWAA050402 120050211A57536546435334 FLAP BOEING737 7373H4 1384600NM RT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 DURING SCHEDULED C3 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RT OUTBOARD T/E AFT FLAP PER MM. 2L72 4F RTA16WE 20050217001522005021700152NM 2005 2 17 AWXA200500202 120050130A531366142101 SHEAR TIE BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 MCN - MAJOR REPAIR - DURING C-16 CHECK A 1 INCH CRACK WAS FOUND IN STRINGER SHEAR TIE CLIP AT BS 294, STR 11 LT. MAINTENANCE REMOVED CRACKED SHEAR TIE CLIP AT BS 294, STR 11 LT; FABRICATED A NEW REPLACEMENT SHEAR TIE CLIP; INSTALLED REPAIR PART IAW ER 03-5300-05042-RC1. 2L72 4F RTA16WE 20050217001552005021700155NM 2005 2 17 AWXA200500190 120050131A575369372099 GIMBAL JOINT BOEING737 737301 1384611NM TE FLAPS CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK INTERGRANULAR CORROSION WAS FOUND ON LT INBOARD MIDFLAP OUTBOARD GIMBAL OUTER SUPPORT AT WBL 184. MAINTENANCE REMOVED AND REPLACED LT INBOARD MID FLAP OUTBOARD GIMBAL OUTER SUPPORT IAW SOPM 20-50-01. 2L72 4F RTA16WE 20050217001562005021700156NM 2005 2 17 AWXA200500191 120050131A575365505889 GIMBAL JOINT BOEING737 737301 1384611NM TE FLAPS CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK INTERGRANULAR CORROSION WAS FOUND ON LT INBOARD MIDFLAP OUTBOARD GIMBAL INDEX PLATE AT WBL 184. MAINTENANCE REMOVED AND REPLACED LT INBOARD MID FLAP OUTBOARD GIMBAL ASSEMBLY IAW SOPM 20-50-01. 2L72 4F RTA16WE 20050217001782005021700178EU 2005 2 17 AALA20050091 120050207A3350 CIRCUIT BOARD AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHT BURNED A AALAK NONE O OTHER ININSP/MAINT 1 SW2191050 423 JFK - EMERGENCY EXIT LIGHT AT LEFT 2 DOOR INOPERATIVE. FOUND BURNED CIRCUIT BOARD ON LIGHT ASSEMBLY AT LEFT NUMBER 2 DOOR FOR EMERGENCY EXIT LIGHT. REPLACED LIGHT ASSEMBLY AT 63WL FOR EMERGENCY EXIT LIGHT AT LEFT NUMBER 2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20050218000172005021800017NM 2005 2 18 USAA050101A 120050104A5330 SKIN BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19440US39006 24811 FOUND SKIN CRACKED 1.5 INCHES, STATION 727D STRINGER 23R. INSTALLED DOUBLER IAW SRM 53-00-01. (M) 2L72 4F RTA16WE 20050218000212005021800021NM 2005 2 18 QXEA200500069 120050114A33506038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007NM ZONE 200 INOPERATIVE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09345PH1251 93 476 FLOOR TRACK EMERGENCY LIGHTING, 2 LIGHTS INOPERATIVE AT FORWARD RH EMERGENCY EXIT DOOR. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY 3352 PS2. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050218000252005021800025EU 2005 2 18 05FDEA00118 120050117A5414 SKIN AIRBUS310 A310203 3930313EU NACELLE DENTED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25409FE 273 INSPECTED UPPER AND LOWER SKINS, FOUND NO DAMAGE ON UPPER SKIN, LOWER SKIN HAS MINOR DAMAGE IN SKIN SURFACE NEAR FWD LT CORNER. REPAIRED SKIN DAMAGE. 2L72 4F RTA35EU 20050218000262005021800026EU 2005 2 18 05FDEA00119 120050118A5315A5327535020000 FLOORBEAM AIRBUS300 A300F4605R 3930327EU FUSELAGE DAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25673FE 780 FLOORBEAM DAMAGE FR65 / Y1456. 2L72 4F RTA35EU 20050222000602005022200060NM 2005 2 22 USAA050069 120050101A575465C2660399A SKIN BOEING737 7373B7 1384580NM NR 3 SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19522AU 23857 PIT - FOUND SLAT DELAMINATED 4 INCHES BY 6 INCHES, NR 3 SLAT. REMOVED TOP SKIN CORE AND DAMAGE, INSTALLED FILLER, DOUBLER PER SRM 51-70-09. (M) 2L72 4F RTA16WE 20050222000962005022200096NM 2005 2 22 USAA050045 120050106A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19374US55727 22953 PIT - FOUND SKIN CRACKED, AFT ENTRY DOOR LOWER HINGE CUTOUT. DOUBLER INSTALLED PER TYPICAL REPAIR 53-60-10 AND EA 79782. (M) 2L72 4F RTA16WE 20050222001332005022200133NM 2005 2 22 USAA050025 120050101A52406545871132 STRUCTURE BOEING737 7374B7 1384702NM SERVICE DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19443US38634 24842 PIT - FOUND FWD SERVICE DOOR CRACKED 1.25 INCHES, LOWER A/C STOP FITTING INNER DOUBLER AT FASTENER. MANUFACTURED NEW DOULER AND INSTALLED PER BOEING DWG 6969854. (M) 2L72 4F RTA16WE 20050222001362005022200136NM 2005 2 22 USAA050067 120050101A5311 FRAME BOEING737 7373B7 1384580NM FUSELAGE BROKEN A USAAK NONE O OTHER ININSP/MAINT 1 EA19522AU49282 23857 PIT - FOUND FRAME BROKEN OUT EDGES, DOOR FRAME STATION 492 AT STATION 27R, LOWER AFT CORNER OF CARGO DOOR FRAME. FABRICATED DOUBLER PER SRM 51-70-13. (M) 2L72 4F RTA16WE 20050222001382005022200138NM 2005 2 22 USAA050051 120050101A575465C2660399 SKIN BOEING737 7373B7 1384580NM L/E SLAT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19522AU49282 23857 PIT - FOUND NR 3 SLAT CRACKED .125 INCH, LOWER SURFACE AT MID SPAN RIVET HOLE. INSTALLED DOUBLER PER SRM 57-43-01 FIG 206. (M) 2L72 4F RTA16WE 20050222002912005022200291NM 2005 2 22 SWAA050424 120050214A575365C357101 FLAP BOEING737 7375H4 138449DNM LT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29502SW 24179 DURING SCHEDULED 1/2D CHECK, FOUND LT WING OUTBOARD FOREFLAP DELAMINATED. REPAIRED FOREFLAP PER SRM. 2L72 4F RTA16WE 20050222002922005022200292NM 2005 2 22 SWAA050499 120050220A5330655298873 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT AFT ENTRY DOOR CUTOUT LOWER FWD CORNER CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20050222002962005022200296NM 2005 2 22 SWAA050480 120050218A335007912 STRIP BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29638SW 27711 EEPLS LIGHT STRIP AT ROW 9 ABC, LOOSE. SECURED EEPLS STRIP PER MM. 2L72 4F RTA16WE 20050222003002005022200300NM 2005 2 22 SWAA050441 120050215A53156545410 FLOORBEAM BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29502SW 24179 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM UPPER CHORD AT BS 664, RBL 24.75, CRACKED. REPAIRED FLOORBEAM CHORD PER EA. 2L72 4F RTA16WE 20050222003032005022200303NM 2005 2 22 SWAA050403 120050211A3350D71702001 BATTERY BOEING737 7373H4 1384600NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29355SW 25250 DURING SCHEDULED SERVICE CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHT BATTERY PACK WEAK. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20050222003042005022200304NM 2005 2 22 SWAA050404 120050211A3350PH22300L STRIP BOEING737 7373H4 1384600NM CABIN DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29359SW 26596 DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT PHOTOLUMINESCENT STRIP BETWEEN ROWS 1 ABC AND 2 ABC, DAMAGED. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER MM. 2L72 4F RTA16WE 20050222003072005022200307NM 2005 2 22 SWAA050407 120050211A531069353656 SHEAR TIE BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 380, BETWEEN STRINGERS 13L AND 14L, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050222001022005022200102NM 2005 2 22 USAA050047 120050101A5320 WEB BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19517AU53410 23703 PIT - FOUND WEB CRACKED 1 INCH, STATION 664 8 INCHES OUTBOARD OF LT INVD SEAT TRACK. PRESSURE DECK WEB REPAIR PER SRM 53-60-51. (M) 2L72 4F RTA16WE 20050222001272005022200127NM 2005 2 22 USAA050065 120050101A5320 CLIP BOEING737 7373B7 1384580NM FUSELAGE BROKEN A USAAK NONE O OTHER ININSP/MAINT 1 EA19522AU49282 23857 PIT - FOUND BROKEN FRAME CLIP, STATION 597 STRINGER 8R. REMOVED AND REPLACED FRAME CLIP PER SRM 51-40-00. (M) 2L72 4F RTA16WE 20050222001412005022200141NM 2005 2 22 USAA050055 120050101A5210507945178 DOOR FRAME BOEING737 7373B7 1384580NM PAX DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19522AU49282 23857 PIT - FOUND FORWARD ENTRY DOOR CRACKED .125 INCH, DOOR FRAME NR 6 DOOR STOP AFT SIDE. CUT OUT DAMAGE, INSTALLED DOUBLER PER TYPICAL REP 52-10-16. (M) 2L72 4F RTA16WE 20050222001442005022200144NM 2005 2 22 USAA050068 120050101A5754 PANEL BOEING737 7373B7 1384580NM L/E SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19522AU49282 23857 PIT - FOUND PANEL DELAMINATED, INBOARD AND OUTBOARD ENDS OF NR 5 SLAT PANEL. INSTALLED DOUBLER PER SRM 51-70-10. (M) 2L72 4F RTA16WE 20050222001502005022200150NM 2005 2 22 USAA050053 120050101A575465C22601179 SKIN BOEING737 7373B7 1384580NM L/E SLAT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19522AU 23857 PIT - FOUND NR 1 SLAT WITH .125 INCH CRACKS ON 6 RIVET HOLES, CENTER OF SLAT BY ACTUATOR MOUNT LOWER SKIN. INSTALLED DOUBLER PER SRM 57-43-01 FIG 206. (M) 2L72 4F RTA16WE 20050222001522005022200152NM 2005 2 22 USAA050062 120050113A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19393US 23315 PIT - FOUND SKIN CRACKED 2.5 INCHES, 1 INCH ABOVE S23L AT BS 745. INSTALLED DOUBLER PER SRM 53-00-01 FIG 229. (M) 2L72 4F RTA16WE 20050222002902005022200290NM 2005 2 22 SWAA050423 120050214A532065C27314 STRINGER CLIP BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 500D, STRINGER 8L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20050222003052005022200305NM 2005 2 22 SWAA050405 120050211A33506556633 SIGN BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29390SW 26593 DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING DOOR EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED SIGN PER MM. 2L72 4F RTA16WE 20050222003062005022200306NM 2005 2 22 SWAA050406 120050211A5320BAC1514 STIFFENER BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29603SW 27954 DURING SCHEDULED D-CHECK, FOUND RADIAL STIFFENER AT BS 1016, BL 0, CORRODED. REPAIRED STIFFENER PER ER. 2L72 4F RTA16WE 20050223002182005022300218NM 2005 2 23 UPS05443822 120050106A5311 FRAME BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 BS 1560, STR 26R, FRAME I/B CHORD FOUND CRACK. FRAME REPAIRED PER RS R-53-62-35243 AND EO B747-5310-21669-A. 2L74 4F A20WE 20050223002202005022300220NM 2005 2 23 UPS05443824 120050107A5313 STRINGER BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 STR END BS 1476 S-6L CRACKED. CRACKED STRINGER REPAIRED PER RS R53-41-35242 AND ENGINEERING FILE NUMBER : 747-53-20217. 2L74 4F A20WE 20050223002212005022300221NM 2005 2 23 UPS05443825 120050113A531365B048752 STRINGER BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 BS 1220 TO 1240 AFT RT WINDOW FORGING REMOVED FOUND STR CORROSION CRACKED. CORROSION BLEND OUT 0.080" BY 1" BY 5" EXCEED SRM LIMIT. NEW STRINGER SEGMENT, SPLICE ANGLE AND REPAIR STRAP INSTALLED AS PER RS R-53-41-35245 AND ENGINEERING FILE NUMBER : 747-53-20220. 2L74 4F A20WE 20050223002252005022300225NM 2005 2 23 UPS05443829 120050113A5313 STRINGER BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 BS 1560 - 1580 AFT RHS WINDOW FORGING REMOVED FOUND STRINGER CORROSION CRACKED. CORROSION BLEND OUT 0.040" BY 1" BY 5" EXCEED SRM LIMIT. NEW STRINGER SEGMENT AND SPLICE ANGLE INSTALLED AS PER SRM 51-40-04 FIG 3. STRINGER SEGMENT AND SPLICE ANGLE REWORKED REFER COMPONENT WORK PROCESS CARD SEQUENCE NR HE70522-1, -2, -3 FOR DETAILS. 2L74 4F A20WE 20050223002262005022300226WP 2005 2 23 UPS05843866 120050201A531156410165 FRAME DOUG DC8 DC871 302199AWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01701UP 45938 FRAME AND SPLICE CORRODED BEYOND LIMITS AT STA 1420 L34R-L36. REMOVED SPLICE FTG AND CUT OUT CORRODED FRAME SECTION BETWEEN L36 AND L34R. FAB REPLACMENT SPLICE FROM SHT 7075-0-.063 HEAT TREAT TO T6. FAB FRAME SECTION FROM EXTR 2641520. INSTALLED PARTS REF SRM 51-1-20D, 53-4-1 FIG 51, 51-3-2, 51-1-8, DWGS 2616545, S2537716, DPS7.00-1. 2L74 4F 4A25 20050223002292005022300229WP 2005 2 23 UPS05843872 120050210A5610 WINDSHIELD DOUG DC8 DC873F 302199FWP COCKPIT CRACKED A IPXAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO01808UP 46008 CAPTAIN'S LT SIDE WINDSHIELD CRACKED. BACK TO BLOCK. REMOVED AND REPLACED LT SIDE WINDSHIELD, WINDSHIELD HEAT CONTROLLER, LOWER POWER RELAY AND HIGH POWER RELAY IAW DC8 AMM 56-10-02-2, OPS CHECK GOOD. 2L74 4F RT4A25 20050223002302005022300230 2005 2 23 UPS05143871 420050209A2565 SLIDE AIRBUSA300 A300F4622R 3930360EU CABIN UNSERVICEABLE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01159UP 0848 ESCAPE SLIDE PRESSURE NEEDLE SHOWS IN RED RANGE, DEFERRED M296868. REMOVED AND REPLACED ESCAPE SLIDE PER A300 CH MM 25-61-21-4 M296868 CLEARED, PLACARD REMOVED. 2L72 4F RTA35EU 20050223002312005022300231NM 2005 2 23 UPS05243877 120050201A5730 SKIN BOEING727 7271A7C 13840X2NM LT WING DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01935UP 20143 SUSPECT CRACK ON LT WING DOOR, ON INNER SKIN AT UPPER FWD END. REPAIR CARRIED OUT IAW SRM 51-40-2. 2L73 4F A3WE 20050223002332005022300233NM 2005 2 23 UPS05243879 120050203A5720 ANGLE BOEING727 7271A7C 13840X2NM LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01935UP 20143 LT WING PANEL ON UPPER SURFACE ABOVE NR 1 TRANSMISSION AFT FAIRING I/B ANGLE AND REPAIR CRACKED. ANGLE REPLACED IAW SRM 51-30-01 AND 51-30-02. 2L73 4F A3WE 20050223002382005022300238WP 2005 2 23 UPS05843876 120050105A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01868UP 45968 FLOORBEAM LOWER FWD FLANGE HAS A 4.00 INCH CRACK F/S 920 RBL 65.0. FLOORBEAM SPLICE SEGMENT REPAIRED FROM RBL 31.40 TO RBL 70.0 IAW SAA SK 868-105. 2L74 4F RT4A25 20050223002452005022300245NM 2005 2 23 UPS05243890 120050202A5315 FLOORBEAM BOEING727 7271A7C 13840X2NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01935UP 20143 CORROSION ON FLOORBEAM AT BS 680 LBL 56 FOUND ON REMOVAL OF FLOOR PANELS FOR DOOR SILL INSPECTION. REPAIR CARRIED OUT IAW SRM 51-10-2, 53-10-8, 51-20-4 AND AAAE EO 2005-01 0-004 UPS ENGINEERING FILE NR 727-53-20183. 2L73 4F A3WE 20050223002462005022300246NM 2005 2 23 UPS05243896 120050131A5755 SPOILER PANEL BOEING727 7271A7C 13840X2NM NR 13 SPOILER DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01935UP 20143 NR 13 SPOILER PANEL HAS AREA OF DELAM AT SITE OF PREVIOUS REPAIR UNDER SURFACE. SPOILER PANEL REMOVED IAW MM 27-61-01. SPOILER PANEL REPAIRED IAW SRM 51-40-20. SPOILER PANEL REINSTALLED IAW 27-61-01. 2L73 4F A3WE 20050223002502005022300250NM 2005 2 23 UPS05543904 120050216A2560 SMOKE GOGGLES BOEING757 75724APF 1384969NM COCKPIT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01449UP 27738 FWD OBS GOGGLES GLASS CRACKED. REPLACED SMOKE GOGGLES WITH SERVICEABLE PAIR. 2L72 4F RTA2NM 20050223002542005022300254EU 2005 2 23 UPS05143910 120050219A2560ABS030903 LIMIT SWITCH AIRBUSA300 A300F4622R 3930360EU EVAC SLIDE INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01127UP 0811 ESCAPE SLIDE DOES NOT ARM ONLY AFTER NUMEROUS TRIES. REMOVED AND REPLACED LIMIT SWITCH 13WN IAW MM 52-73-13-4, OPS CK. 2L72 4F RTA35EU 20050223002582005022300258NM 2005 2 23 QXEA200500009 120050103A5270 WARNING SYSTEM BOMBDRDHC8 DHC8401 1390041NM COCKPIT MALFUNCTIONED A QXEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM09404QX 4046 YYC - FLIGHT 2331 - FLIGHT RETURNED TO FIELD WHEN AFTER TAKEOFF, THE CREW RECEIVED A FORWARD CARGO DOOR WARNING. MAINTENANCE INSPECTED THE DOOR AND FOUND THAT IT WAS SECURE. OPERATIONAL CHECKS WERE PERFORMED AND WERE ALL GOOD. MAINTENANCE WAS UNABLE TO DUPLICATE THE WRITE-UP. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050223002592005022300259NM 2005 2 23 QXEA200500029 120050105A33401014011 LIGHT DHAV DHC8 DHC8202 2809007NM LT WING DEFECTIVE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09352PH 494 PSC - LT UNDERWING EMERGENCY EXIT BETA LIGHT FAILED BRIGHTNESS CHECK. MAINTENANCE REMOVED AND REPLACED BETA LIGHT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050223002832005022300283NM 2005 2 23 QXEA200500074 120050103A5330 SKIN DHAV DHC8 DHC8202 2809007NM FUSELAGE DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09350PH 488 SEA - ON PREFLIGHT, A DENT WAS NOTICED ON THE RIGHT FUSELAGE. MAPPED DENTS AND FORWARDED INFORMATION TO ENGINEERING IAW EA NR 2-53-590. 2H72 4T RTA13NM 20050224000302005022400030EA 2005 2 24 SWIA200514569 120050129A5310 BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07440SW 7589 MAIN FUSELAGE FS 280.00 RBL 9.0 LOWER FLANGE OF TRANSVERSE BEAM CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FS280, RBL 9 LOWER FLANGE OF TRANSVERSE BEAM IAW CRJ REO 601R-53-11-171 REV A. 2L72 4F RTA21EA 20050224000312005022400031NM 2005 2 24 05FDEA00294 120050215A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 BARREL NUT BORE NR 34R CORROSION REMOVAL FOUND EXCEEDED LIMITS. CORROSION REMOVED AND REPAIRED PER FEDEX EA 1-5510-81726. 2L73 4F RTA22WE 20050224000332005022400033CE 2005 2 24 DXTA200500596 120050215A2612991203611 FIRE LOOP CESSNA560 560XL 2076702CE RT ENGINE INTERMITTENT E DXTAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL07601QS 5605301 RIGHT FIRE LIGHT ILLUMINATED MOMENTARAILY FOR A FEW SECONDS DURING CRUISE. WENT OUT WHEN POWER WAS REDUCED. REPLACED RT FIRE DETECTOR LOOP WITH NEW REF 560 XL CH 26-11-01. OPERATIONAL CHECK SATISFACTORY. 2L72 4F RTA22CE 20050224000342005022400034EU 2005 2 24 DXTA200500594 120050215A2910 LINE BRAERO1000 HAWKER1000 7450005EU HYDRAULIC SYS LEAKING E DXTAO OTHER K FLUID LOSS LDLANDING 1 GL07545QS 259045 ON LANDING BRAKES WERE VERY SOFT AND MADE STOPPING THE AIRPLANE DIFFICULT. ALSO CO-PILOTS BRAKES CONFIRMED THE BRAKE ISSUE. LEFT PEDAL ON CO-PILOTS SIDE WENT TO FULL TRAVEL. BLED CO-PILOT BRAKES IAW HAWKER 1000 MM 32-40-00. OPERATIONAL CHECK SATISFACTORY. 2L72 4F RTA3EU 20050224000352005022400035NM 2005 2 24 DL76L050116 120050217A7920PW40603 ENGINE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 2 MAKING METAL A DALAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SO27189DN33939 25990 727649 ENGINE SHUTDOWN IN FLIGHT DUE TO LOSS OF OIL PRESSURE. FOUND METAL ON CHIP DETECTORS. REPLACED ENGINE. 2L72 4F4 FRTA1NM E24NE 20050224000362005022400036EU 2005 2 24 YENA200505 120050110A2560 PIN AIRBUS320 A320232 3930326EU RT SLIDE UNSECURE A YENAO OTHER J WARNING INDICATION UKUNKNOWN 1 EA15597JB 2307 ON BOARDING, EMERGENCY EXIT ROW SLIDE ARM INDICATOR INTERMITTENT A/C RIGHT. SECURED AFT RT EMERGENCY LATCH PIN IAW MM, OPS CK NORM 52-21-00. 2L72 4F RTA28NM 20050224000382005022400038 2005 2 24 YENA200503 420050105A23303042865102 ELECTRICAL BOX AIRBUS320 A320232 3930326EU CABIN FAULTY A YENAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15529JB7274 5351 1610 BURNING SMELL IN PROXIMITY OF ROWS 7 AND 8. ACCOMPLISHED INFO NOTICE 2004-T023TR SYSTEM OPS CHKD OK. REMOVED AND REPLACED SEB AT 7E AS STATED IN INFO NOTICE AS PRECAUTIONARY. 2L72 4F RTA28NM 20050222002972005022200297NM 2005 2 22 SWAA050481 120050218A3350101073 COVER BOEING737 7373H4 1384600NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29638SW 27711 FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT COVER, MISSING. REMOVED AND REPLACED COVER PER MM. 2L72 4F RTA16WE 20050223002192005022300219NM 2005 2 23 UPS05443823 120050106A531165B0188843 FRAME BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 FRAME BS 1394 INNER FLANGE CRACKED AT S-22L. M/D FRAME AT BS 1394 S-22L INNER FLANGE REPAIRED PER RS R-53-42-35229 AND ENGINEERING FILE NUMBER : 747-53-20218. 2L74 4F A20WE 20050223002372005022300237WP 2005 2 23 UPS05843875 120050203A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01868UP 45968 TAIL COMPT 60 L17R HAS 2.5 IN CRACK AT END FITTING STA 1771 (LWR SURFACE OF UPPER LEG). REMOVED FABRICATED AND INSTALLED L17R STA 1771 IAW SRM'S 53-2-2 FIG10, 51-1-21, 51-1-20D, 51-3-0 AND DWG 5649327. 2L74 4F RT4A25 20050223002402005022300240EU 2005 2 23 UPS05143886 120050211A3350 LIGHT AIRBUSA300 A300F4622R 3930360EU MAIN ENTRY INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01160UP 0005 MAIN ENTRY DOOR SLIDE LT CENTER LIGHT SEGMENT OUT. RELAMPED CK GOOD, 52-73-11-4. 2L72 4F RTA35EU 20050223002422005022300242NM 2005 2 23 UPS05M43885 120050212A2560MXP21000 SMOKE GOGGLES DOUG MD11 MD11F 3023600NM COCKPIT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01252UP JRT- COURIER SEAT SMOKE GOGGLES HAS CRACKED LENS. REMOVED AND REPLACED RT COURIER SEAT SMOKE GOGGLES IAW MM 25-00-00. 2L73 4F RTA22WE 20050223002532005022300253EU 2005 2 23 UPS05143903 120050217A30406664157 CONTROLLER AIRBUSA300 A300F4622R 3930360EU COCKPIT FAULTY A IPXAK NONE O OTHER DEDESCENT 1 SO01143UP 0826 F/O WINDSHIELD CRACK OUT OF LIMITS; REPLACE RT WINDOW TEMP CONTROLLER. REMOVED AND REPLACED TEMP CONTROLLER (20DG)MM 30-42-00. 2L72 4F RTA35EU 20050223002552005022300255NM 2005 2 23 UPS05543909 120050219A3510MC1025104 OXYGEN MASK BOEING757 75724APF 1384969NM COCKPIT LEAKING A IPXAK NONE O OTHER ININSP/MAINT 1 SO01461UP 28265 CAPTAINS O2 MASK LEAKS FROM MOUTH PIECE DURING MASK TEST. REPLACED MASK ASSY IAW B757 MM CHAPT 35. 2L72 4F RTA2NM 20050224000422005022400042 2005 2 24 AWXA200500208 420050214A2565D5211052200000 BAR AIRBUS320 A320231 3930325EU L-2 DOOR BINDING A AWXAK NONE O OTHER ININSP/MAINT 1 WP28626AW 65 PHX - EES - DURING 4-DAY CHECK THE L-2 EMERGENCY SLIDE GIRT BAR FAILED RETRACTION TEST. MAINTENANCE REMOVED AND REPLACED L-2 EMERGENCY SLIDE GIRT BAR IAW T/C R1C25304, FUNCTIONAL TEST WAS GOOD. 2L72 4F RTA28NM 20050224000432005022400043NM 2005 2 24 AWXA200500209 120050214A3397BMS13311122 WIRE BOEING737 7373G7 1384595NM SEAT ROW 7 LT DISCONNECTED A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28305AW 24012 PHX - EEL - FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 7 LT WAS INOPERATIVE. MAINTENANCE REPAIRED WIRE THAT WAS PULLED FROM CONNECTOR AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 7 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050224000442005022400044EU 2005 2 24 AWXA200500211 120050214A3260ABS012110 PROXIMITY SENSOR AIRBUS320 A320232 3930326EU ZONE 711 FAULTY A AWXAO OTHER J WARNING INDICATION CLCLIMB 1 WP28602AW 565 PHX - LANDING GEAR - AFTER DEPARTING PHX EN ROUTE TO LAS ECAM INDICATED THE LANDING GEAR WAS NOT UP AND LOCKED, FLIGHT CREW CONFIRMED THAT NLG GEAR WAS DOWN BY NOISE LEVEL AND INDICATIONS, RECYCLED THE LANDING GEAR PER ECAM INSTRUCTIONS AND GEAR RETRACTED, PROCEEDED TO LAS AND LANDED WITHOUT FURTHER EVENT. AIRCRAFT WAS MAINTENANCE FERRIED BACK TO PHX AND MAINTENANCE FOUND NLG PROXIMITY SENSORS 24GA & 25GA Z DIMENSIONS EXCEED LIMITS. REMOVED AND REPLACED PROXIMITY SENSOR 24GA IAW AMM 32-31-33, AND ADJUSTED BOTH SENSORS. PERFORMED LANDING GEAR RETRACTION CHECK, NO DEFECTS NOTED. 2L72 4F RTA28NM 20050224000452005022400045SO 2005 2 24 SWIA200514543 120050209A3350 CONNECTOR EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT LOOSE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07220SW 120288 FOUR FLOOR LEVEL EMERGENCY LIGHTS OUT. RECONNECTED LIGHT CONNECTOR UNDER FLOOR AT SEAT 3A, OPERATIONAL CHECKS NORMAL. 2L72 4T RTA31SO 20050224000462005022400046SO 2005 2 24 SWIA200514544 120050211A2750 HANDLE EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED DEDESCENT 1 NM07220SW 120288 ON DEPARTURE, FLAPS DID NOT FULLY RETRACT. REPLACED FLAP HANDLE. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050224000472005022400047EA 2005 2 24 SWIA200514545 120050217A2750766389L CONTROLLER CNDAIRCL600 CL6002C10 1390015EA TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07730SK 10193 FLAP 1/2 SPEED STATUS MESSAGE. REMOVED AND REPLACED SFECU IAW AMM 27-51-05, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050224000482005022400048 2005 2 24 SWIA200514546 420050217A3418C12851AA03 COMPUTER CNDAIRCL600 CL6002C10 1390015EA STALL WARNING MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07730SK 10193 UPON ARRIVAL IN COS, NOTED STALL FAIL CAUTION. REPLACED SPC PER AMM 27-35-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050224000502005022400050SO 2005 2 24 SWIA200514547 120050215A3350 LAMP EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07301YV 120301 ONE EMERGENCY FLOOR LIGHT IN GALLEY WILL NOT ILLUMINATE. RELAMPED EMERGENCY FLOOR LIGHT, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050224000522005022400052 2005 2 24 SWIA200514548 420050215A3418C818171 TRANSDUCER EMB 120 EMB120ER 3260203SO STALL WARNING INOPERATIVE A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07213SW1118911189 120277 WHEN SIDE SLIP HEATER SWITCH IS TURNED ON, RECEIVED AN INOP LIGHT WITH A DE-ICE LIGHT ON THE MAP. REPLACED TRANSDUCER ASSY PER MM 27-00-00, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050224000532005022400053EA 2005 2 24 05048656 120050217A5310 STRUCTURE CNDAIRCL600 CL6002B19 1900309EA LAVATORY BURNED A VTZAB EMER. DESCENT MJ OVER TEMP WARNING INDICATION CLCLIMB 1 EA27656BR 7485 EVENT SUMMARY STATED LAV SMOKE IND, EMERGENCY DECLARED. PERFORMED ENG AND APU RUNS. COULD NOT DUPLICATE SMOKE. INSPECTED AND FOUND LAV WALL BEHIND ORDINANCE SIGN BURNED AND DAMAGED. REPAIRED WALL. OPS CHECK GOOD. 2L72 4F RTA21EA 20050224000552005022400055EA 2005 2 24 05048675 120050217A2750 SHAFT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS DAMAGED A VTZAO OTHER J WARNING INDICATION APAPPROACH 1 EA27675BR 7635 EVENT SUMMARY STATED FLAPS FAIL AT 0 DEG ON APPROACH. REMOVED AND REPLACED LT FLAP FLEX SHAFT. 2L72 4F RTA21EA 20050224000562005022400056EA 2005 2 24 05011683 120050111A3030 HEATER CNDAIRCL600 CL6002B19 1900309EA PITOT/STATIC SYSMALFUNCTIONED A VTZAA UNSCHED LANDING O OTHER CLCLIMB 1 EA27683BR 7692 RT PITOT HEAT FAILURE. MX RESET STATIC HEATER IAW 30-31-00. OPS CHECK GOOD. 2L72 4F RTA21EA 20050224000592005022400059NM 2005 2 24 DL764050119 120050217A3350331202195 LAMP BOEING767 767432ER 1385134NM SEAT ROW 22 ABC SHORTED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27829MH 29700 WORKING ETOPS PRE-DEPARTURE CHECK FOUND EMERGENCY EXIT LIGHTS AT SEAT ROWS 17 ABC TO 24 ABC INOP. REPLACED SHORTED TRACK LIGHT LAMP AT 22 ABC. 2L72 4F RTA1NM 20050224000612005022400061NM 2005 2 24 05FDEA00289 120050215A5320 ANGLE DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25591FE 48527 AFT FUSELAGE DOGHOUSE UPP COMPT FWD MOST TOP BULKHEAD TO CROWN ANGLE PLATE, SUSPECT CRACK AT RT EDGE. ANGLE PLATE REMOVED AS PER SRM 51-31-01 VOL II. ANGLE FABRICATED AS PER DWG AJC7372 AND INSTALLED AS PER SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20050224000652005022400065NM 2005 2 24 05FDEA00292 120050215A5311AFA00333 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25591FE 48527 MAIN DECK SIDE WALL STRUCTURE FRAME STA 1761 FOUND WITH DENT ON INNER CHORD AT L-12. CARRIED OUT REPAIR AS PER SRM 53-30-00 FIG 1 VOL I. 2L73 4F RTA22WE 20050224000662005022400066NM 2005 2 24 05FDEA00293 120050215A5330 SKIN DOUG MD11 MD11 3023602NM ZONE 100 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 STA 595 BELOW LONGERON 38 RT SKIN SPLICE LOCK FASTENER HOLES FOUND MOUNTED WITH A DOUBLER & 06 EA NUT PLATES. SKIN PANEL REPLACEMENT WAS COMPLIED WITH. 2L73 4F RTA22WE 20050224000692005022400069EA 2005 2 24 COMA0560122 120050213A304011513361 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA DE ICE SYSTEM MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01435CA21232937 7473 FLIGHT 5823 WING OVERHEAT MESSAGE. REPLACED THE TEMP CONTROL UNIT. 2L72 4F RTA21EA 20050224000722005022400072EA 2005 2 24 COMA0570018 120050215A531267053110521 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA FUSLAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01369CA5902 10079 FS 280 LT AND RT BULKHEADS HAVE MAJOR CORROSION ON AFT SIDE ALONG THE BOTTOM EDGES. REPLACED LOWER WEBS AT FS 280 BULKHEAD IAW BOMBARDIER AEROSPACE REO 670-53-11-052 AND BRAS EO 601R-53-5986, 601R-53-5987, AND 601R-53-5977. 2L72 4F RTA21EA 20050224000752005022400075NM 2005 2 24 SB05021 120050131A335020121 POWER SUPPLY BOEING737 7374B7 1384702NM CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19777AU 24979 CLT - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHTS ON SEATS 24L AND 25L INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE M1137 EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECK NORMAL. 2L72 4F RTA16WE 20050224000782005022400078 2005 2 24 SWAA050410 420050212A256565C16280 HOOK BOEING737 7377H4 1384404NM GIRT BAR DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29430WN 33659 R1 DOOR EVAC SLIDE GIRT BAR FWD HOOK HAS SHEARED RIVET. REMOVED AND REPLACED RIVET PER MM. 2L72 4F RTA16WE 20050224000792005022400079NM 2005 2 24 SB05009 120050118A335020131A BATTERY PACK BOEING737 737401 1384701NM CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19404US 23886 CLT - MAINTENANCE FOUND SEVERAL EMERGENCY LIGHTS IN THE AFT GALLEY AREA INOPERATIVE. MAINTENANCE REPLACED THE M1137 AND M1197 BATTERY PACKS. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050224000812005022400081NM 2005 2 24 SB05010 120050122A3260390FW04A10 SENSOR BOEING737 737301 1384611NM NLG FAULTY A USAAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 EA19558AU 23512 CMH - FLT 184 ON APPROACH TO CMH FROM CLT, CREW RECEIVED A NOSE LANDING GEAR RED UNSAFE LIGHT AFTER GEAR EXTENSION. A FLYBY OF THE TOWER CONFIRMED THE GEAR WAS DOWN. CREW CHECKED VIEWPORT AND STRIPES WERE ALIGNED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. AN EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE NOSE LANDING GEAR LOCK SENSOR OUT OF RIG. ADJUSTED SENSOR PER MM 32-61-41-401. OPERATIONAL CHECK GOOD. HOWEVER, LATER IN THE DAY WHILE TAXIING TO THE GATE, THE NOSE LANDING GEAR RED UNSAFE LIGHT BEGAN CYCLING ON AND OFF. MAINTENANCE THEN REPLACED THE NOSE LANDING GEAR LOCK SENSOR PER MM 32-61-41-424. GEAR SWING AND INDICATION CHECK GOOD. 2L72 4F RTA16WE 20050224000822005022400082EU 2005 2 24 AWXA200500218 120050204A5320D53475765206 BEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28659AW 1166 SAL - MAJOR REPAIR - DURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND AROUND FASTENER HOLES ON SILL BEAM AT BULK CARGO DOOR FR 62+12 INCH, STR 38 RT. MAINTENANCE CUT OUT DAMAGED SECTION OF SILL BEAM AT BULK CARGO DOOR FR 62+12 INCH, STR 38 RT; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW A320 SRM 53-41-49 FIG 203. 2L72 4F RTA28NM 20050224000892005022400089NM 2005 2 24 AWXA200500223 120050130A5330655298871 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 MCN - MAJOR REPAIR - DURING C-16 CHECK A .1875 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT L-2 DOOR UPPER HINGE CUTOUT BS 955, STR 10 LT. MAINTENANCE CUT OUT CRACK IN L-2 DOOR UPPER HINGE CUTOUT BS 955, STR 10 LT; FABRICATED A FILLER AND REPAIR PLATE; INSTALLED REPAIR PARTS IAW 53-60-01 FIG 205. 2L72 4F RTA16WE 20050224000902005022400090NM 2005 2 24 AWXA200500224 120050122A52106545871503 SKIN BOEING737 737301 1384611NM R1 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK A .75 INCH CRACK WAS FOUND IN R-1 DOOR INNER WEB AT FORWARD END, AFT OF NR 4 DOOR STOP BS 328, RBL 60, WL 240. MAINTENANCE CUT OUT CRACK IN R-1 DOOR INNER WEB; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW 51-70-13. 2L72 4F RTA16WE 20050224000912005022400091NM 2005 2 24 AWXA200500225 120050121A5754 SKIN BOEING737 737301 1384611NM NR 3 SLAT ASSY DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK THE LOWER SURFACE SKIN OF THE NR 3 SLAT WAS FOUND DELAMINATED AT SLAT STA 14.5. MAINTENANCE REMOVED PREVIOUS REPAIR AND DAMAGED AREA OF LOWER NR 3 SLAT SKIN; FABRICATED A CORE FILLER AND EXTERNAL DOUBLER; BONDED REPAIR PARTS TO SLAT IAW 51-70-10, FIG 24. 2L72 4F RTA16WE 20050224000942005022400094NM 2005 2 24 AWXA200500227 120050121A533065734577566 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK A 1 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT BS 874, A .5 INCH ABOVE STR 24 RT RIVET ROW. MAINTENANCE CUT OUT CRACK IN FUSELAGE SKIN AT BS 874, STR 24 RT; FABRICATED A DOUBLER; INSTALLED REPAIR PART IAW 53-00-10 FIG 229. 2L72 4F RTA16WE 20050224000952005022400095NM 2005 2 24 AWXA200500228 120050122A53116545808188 FRAME BOEING737 737301 1384611NM FUSLEAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK A 1 INCH CRACK WAS FOUND IN MAIN CABIN FRAME AT R-1 DOOR BS 294.5, STR 7 RT. MAINTENANCE CUT OUT CRACK IN FRAME AT R-1 DOOR BS 294.5, STR 7 RT; FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED REPAIR PARTS IAW 51-70-11. 2L72 4F RTA16WE 20050224000962005022400096NM 2005 2 24 AWXA200500229 120050123A5330654576972 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK A .1875 INCH CRACK WAS FOUND IN FUSELAGE SKIN EMANATING FROM FASTENER HOLE AT BS 445, BL 0. MAINTENANCE REMOVED EXISTING REPAIR DOUBLER AND CUT OUT DAMAGED AREA OF SKIN AT BS 445, BL 0; PERFORMED A HFEC INSPECTION OF CUT OUT TO VERIFY NO CRACKS EXIST; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW ER 03-5331-05034-RC1. 2L72 4F RTA16WE 20050224000972005022400097NM 2005 2 24 05FDEA00299 120050216A5330 SKIN BOEING727 727200 138407ENM FUSELAGE LIGHTNING STRIKEA FDEAK NONE O OTHER ININSP/MAINT 1 SO25496FE 21670 LIGHTING STRIKE IN SKIN AT BS 188, 13 INCHES BELOW STR 17L. *S/D* REPAIRED PER SRM 53-30-03. 2L73 4F RTA3WE 20050224001002005022400100NM 2005 2 24 05FDEA00301 120050217A5312AJC7238503 BULKHEAD DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 WASTE TANK COMPT - AFT PRESSURE BULKHEAD CORRODED 16 INCHES BELOW CABIN FLOOR LBL 62, IMMEDIATELY BELOW FUEL LINE FEED THROUGH. WASTE TANK COMPT - AFT PRESSURE BULKHEAD BELOW CABIN FLOOR LBL 62, IMMEDIATELY BELOW FUEL LINE FEED THROUGH CORRODED PANEL REMOVED AS PER SRM 51-35-01 VOL II & SRM 51-33-01 VOL II. FABRICATED PANEL AS PER DRAWING AJC7238 AND INSTALLED AS PER SRM 51-35-01 VOL II & SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20050224001032005022400103NM 2005 2 24 05FDEA00303 120050217A5320 STRAP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25496FE 21670 STABILIZING STRAP CRACKED AT BS 381, RBL 24, WL 200 IN THE E-BAY. 2L73 4F RTA3WE 20050224001042005022400104EA 2005 2 24 COMA0570019 120050211A2611 SMOKE WARNING CNDAIRCL600 CL6002C10 1390015EA LAVATORY FALSE INDICATIONA COMAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01669CA 10176 FLIGHT 9457 FWD AND AFT LAV SMOKE MESSAGE DURING T/O. COULD NOT DUPLICATE. INSPECTED AND FOUND NO EVIDENCE OF SMOKE AND OPERATIONAL CHECK OF SMOKE DETECTION SYSTEM WAS SATISFACTORY. 2L72 4F RTA21EA 20050224001052005022400105NE 2005 2 24 MALA050141 220050210A7200 BEARING SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE NR 2 FAILED A MALAE ENGINE SHUTDOWN J WARNING INDICATION NRNOT REPORTED 1 GL15457XJ 340B457 CREW REPORTED LOUD BANG, FOLLOWED BY CHIP LIGHT, OIL PRESSURE LOSS, AND OVERTEMP. IN FLIGHT SHUTDOWN. NR 2 BEARING FAILURE. NO FURTHER INFO AT THIS TIME 2L72 4T4 TRTA52EU E8NE 20050224001112005022400111NM 2005 2 24 RYNA200500003 120050117A5320 INTERCOSTAL BOEING737 737201 1384454NM FUSELAGE CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07240AU5546055460 22355 MAIN CABIN FLOOR BEAM INTERCOSTAL CRACKED AT BS 328 TO 344, LBL 45. REPAIRED CRACKED INTERCOSTAL AT BS 328 TO 344, LBL 45. 2L72 4F A16WE 20050224001152005022400115SO 2005 2 24 RAIA00501005 120050104A3610S2U2228 SEAL EMB 145 EMB145LR 3260212SO BLEED AIR SYS BLOWN A RAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03817HK 145058 5761 - STL - BLEED LEAK INDICATION IN FLIGHT. MAINTENANCE REMOVED AND REPLACED BLOWN DUCT SEALS IN NR 2 BLEED SYSTEM. 2L72 4T RTT00011AT 20050224001182005022400118NE 2005 2 24 RAIA00501040 220050113A7200TPE33114 ENGINE JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114HR 01514NE RIGHT FAILED A RAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03553HK17310 41066 76111 3643- PIT- RIGHT ENGINE ERRATIC/RIGHT ENGINE OIL PRESSURE RED CAP LIGHT/IN FLIGHT SHUTDOWN PER QRH. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE. 2L72 4T4 TRTA41NM E18NE 20050224001202005022400120EU 2005 2 24 RAIA00501032 120050112A3260AIR135670 UPLOCK SWITCH JETAIRJETSTMJETSTM4101 1500501EU NLG FAULTY A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03561HK 41077 5515 - STL- RED LIGHT IN GEAR HANDLE ILLUMINATED. MAINTENANCE REPLACED NOSE LANDING GEAR UPLOCK SWITCH, OPS CHECK GOOD. 2L72 4T RTA41NM 20050224001282005022400128 2005 2 24 RAIA00501006 420050104A342570031901 HSI JETAIRJETSTMJETSTM4101 1500501EU COCKPIT FAILED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03568HK170982933 41086 3641 - PIT - FO'S EHSI TUBE FAILED. MAINTENANCE REMOVED AND REPLACED FO'S EHSI. 2L72 4T RTA41NM 20050224001292005022400129SO 2005 2 24 RAIA00501003 120050103A3350 LIGHT EMB 145 EMB145EP 3260221SO CABIN INOPERATIVE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03826HK 145016 5727 - STL - AFT CABIN OVERHEAD EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED LIGHT BULBS. 2L72 4F RTT00011AT 20050224001302005022400130EU 2005 2 24 RAIA00501004 120050103A3297 WIRE JETAIRJETSTMJETSTM4101 1500501EU LT BRAKE BROKEN A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03564HK 41081 5524 - STL - BRAKE ANTI-SKID WARNING. MAINTENANCE DEFERRED ANTI-SKID PER MEL 32-6. SUBSEQUENTLY REPAIRED BROKEN WIRE TO LEFT INBOUND SENSOR AT CONNECTOR. 2L72 4T RTA41NM 20050224001402005022400140CE 2005 2 24 DXTA200500593 120050214A3240 BRAKE CESSNA500 560CESSNA 2076750CE MLG MALFUNCTIONED E DXTAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07337QS 5600437 DURING TAXI FOR TAKEOFF SIC HAD NO BRAKES. PIC CHECKED NO BRAKES. USED EMERGENCY BRAKES TO SLOW DOWN. TRIED BRAKES AGAIN AND APPEARED NORMAL. CAME TO A STOP, SAW ANTISKID LIGHT ON. RAN THE CHECKLIST, RESET CIRCUIT BREAKER AND LIGHT STAYED ON. TURNED ANTISKID OFF. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20050224001492005022400149EA 2005 2 24 SWIA200514571 120050129A5320 WEB CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07440SW 7589 AFT EQUIPMENT BAY ESB HAS A CRACK; FS 625.00 RBL - 38.0 LOWER WEB. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED LOWER WEB IAW CRJ REO 601R-53-61-358, REV A. 2L72 4F RTA21EA 20050224001522005022400152EA 2005 2 24 SWIA200514573 120050129A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07440SW 7589 AFT EQUIPMENT BAY INTERCOSTAL CUP IS CRACKED; FS 625.00 STR 14L. ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIP IAW CRJ SRM 51-40-11, 51-42-06, AND 51-25-16. 2L72 4F RTA21EA 20050224001542005022400154EA 2005 2 24 SWIA200514574 120050129A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07440SW 7589 AFT EQUIPMENT BAY INTERCOSTAL CUP IS CRACKED; FS 625.00 STR 14R. ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIP IAW CRJ SRM 51-40-11, 51-42-06, AND 51-25-16. 2L72 4F RTA21EA 20050224001552005022400155EA 2005 2 24 SWIA200514575 120050129A5340 SUPPORT CNDAIRCL600 CL6002B19 1900309EA HYD MANIFOLD CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07440SW 7589 AFT EQUIPMENT COMPARTMENT NR 1 HYDRAULIC SUPPORT MANIFOLD IS CRACKED IN LOWER AFT CORNER; FS 718.00. ITEM FOUND AT C-CHECK INSPECTION. HYDRAULIC SUPPORT BRACKET REPAIRED IAW CRJ REO 601R-53-62-031 REV A/C. 2L72 4F RTA21EA 20050224001562005022400156EA 2005 2 24 SWIA200514576 120050129A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07440SW 7589 CARGO COMPARTMENT FLOOR SUPPORT ANGLE CRACKED AT FS 621.00 RLB 42.0. ITEM FOUND AT C-CHECK INSPECTION. SUPPORT ANGLE REPAIRED IAW CRJ REO 601R-53-61-117 REV "B'. 2L72 4F RTA21EA 20050224001592005022400159EA 2005 2 24 SWIA200514578 120050202A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07955SW 7817 MAIN FUSELAGE FLOORBEAM AT RBL 9.0 ATTACH ANGLES CRACKED AT FS 280.00. ITEM FOUND AT C-CHECK INSPECTION. ANGLES REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-25-16, 51-23-00. 2L72 4F RTA21EA 20050224001602005022400160EA 2005 2 24 SWIA200514579 120050215A5740 ATTACH FITTING CNDAIRCL600 CL6002B19 1900309EA WING DAMAGED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07590SW 7077 FORWARD WING ATTACH FITTING, FORWARD SIDE, FLANGED BUSHING HAS COMPLETE SEPARATION OF FLANGE FROM BUSHING SLEEVE. ITEM FOUND AT C-CHECK INSPECTION. RT WING FITTING/BUSHING REPAIRED IAW REO 601R-57-21-564 155.2. 2L72 4F RTA21EA 20050224001632005022400163EU 2005 2 24 05FDEA00268 120050209A5313 STRINGER AIRBUS310 A310203 3930313EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25405FE 237 AFT PIT FR60 STRINGER 48 RT JUST BELOW DOOR FRAME CORRODED. REPLACED CORRODED STRINGER, THREE SPLICE ANGLES, AND TWO BRACKETS IAW A310-200 SRM 53-10-14. RESTORED PROTECTIVE COATING IAW A310-200 SRM 51-23-00. 2L72 4F RTA35EU 20050224001662005022400166 2005 2 24 05FDEA00267 420050209A34606223342001 CONTROLLER BOEING727 727200 138407ENM FLT DIRECTOR SMOKE A FDEAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO25482FE2040 21464 AFTER TAKEOFF WHEN GEAR HANDLE WAS RAISED, SMOKE WAS OBSERVED COMING FROM UNDER INSTRUMENT PANEL AT CENTER. SMOKE WAS A PURPLISH COLOR WITH AN ACRID SMELL INDICATING ELECTRICAL ORIGIN. ALSO NOTED FLT DIR- 2, AC C/B POPPED. SMOKE STOPPED AFTER APPROX 1 MIN. BUT SMELL STILL NOTICEABLE IN COCKPIT DURING APPROACH / LANDING AND AFTER BLOCK IN. PER CREW DEBRIEF, SMOKE WAS COMING FROM FLIGHT DIRECTOR MODE CONTROLLER. REPLACED FLIGHT DIRECTOR MODE CONTROLLER. VERIFIED STRONG BURN SMELL FROM CONTROLLER WHEN REMOVED. 2L73 4F RTA3WE 20050224001672005022400167SO 2005 2 24 MASA200500044 120050118A335020131A BATTERY EMB 145 EMB145LR 3260212SO CABIN DISCHARGED A MASAK NONE L NO TEST TXTAXI/GRND HDL 1 SW07832MJ5583 145310 ASH 2737 IN JAN, PILOT REPORTED NUMEROUS OVERHEAD EMERGENCY EXIT LIGHTS INOP. AIRCRAFT WAS FERRIED TO CLT WHERE MAINTENANCE REPLACED THE BATTERY. 2L72 4T RTT00011AT 20050224001692005022400169SO 2005 2 24 MASA200500027 120050111A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN MALFUNCTIONED A MASAK NONE O OTHER ININSP/MAINT 1 SW07836MJ 145359 ASH 2866 IN CLT, PILOT REPORTED SEVERAL STRIPS OF EMERGENCY PATH LIGHTING INOP. MAINTENANCE INSPECTED THE SYSTEM AND WERE NOT ABLE TO DUPLICATE THE PROBLEM. 2L72 4T RTT00011AT 20050224001702005022400170EA 2005 2 24 05042669 120050211A3610 SHUTOFF VALVE CNDAIRCL600 CL6002B19 1900309EA LT A/C PACK FAILED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27669BR 1593 EVENT SUMMARY STATED LT PACK HIGH PRESSURE WARNING. REMOVED AND REPLACED 10TH STAGE BLEED AIR SOV. OPS CHECK GOOD. 2L72 4F RTA21EA 20050224001722005022400172EA 2005 2 24 COMA0560125 120050211A2750601R930043 CONTROL HANDLE CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01785CA1625710921 7326 FLIGHT 4961 FLAPS FAIL CAUTION. REPLACED THE FLAP CONTROL HANDLE. 2L72 4F RTA21EA 20050224001732005022400173NM 2005 2 24 SWAA050483 120050218A53306545772 SKIN BOEING737 7373Q8 1384670NM FUSELAGE WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29317WN 24068 DURING SPV, FOUND UPPER RT AND LT FUSELAGE SKIN FROM BS 860 TO BS 887, UNDER DORSAL FIN, WORN. REPAIRED SKIN PER ER. 2L72 4F RTA16WE 20050224001762005022400176SO 2005 2 24 SWIA200514532 120050212A3350 BULB EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07580SW 120348 ONE EMERGENCY LIGHT OUT. RELAMPED INOPERATIVE LIGHT ASSEMBLY ON THE FLOOR EMERGENCY STRIP, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050224001802005022400180 2005 2 24 SWIA200514534 420050208A34183995100208 COMPUTER CNDAIRCL600 CL6002B19 1900309EA STALL PROTECTIONMALFUNCTIONED A SWIAO OTHER N FALSE WARNING CLCLIMB 1 NM07453SW 7743 STALL FAIL CAUTION MESSAGE ILLUMINATED SHORTLY AFTER TAKEOFF. REPLACED STALL PROTECTION COMPUTER IAW 27-35-01. OPERATIONAL CHECK GOOD. P/N: 39-951-002-08, S/N OFF: 249. 2L72 4F RTA21EA 20050223002242005022300224NM 2005 2 23 UPS05443828 120050113A531365B048773 STRINGER BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 BS 980 - 1000 AFTER LT WINDOW FORGING REMOVED FOUND STR CORROSION CRACKED. CORROSION BLEND OUT 0.060" BY 1" BY 3" EXCEED SRM LIMIT. NEW STRINGER SEGMENT AND SPLICE ANGLE INSTALLED AS PER RS R-53-41-35234 AND ENGINEERING FILE NUMBER : 747-53-20213. 2L74 4F A20WE 20050223002272005022300227WP 2005 2 23 UPS05843867 120050107A5311REFDWG5753892 FRAME DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01701UP 45938 A-PIT FRAME CORRODED AND MISDRILLED AT STA 280 L32R. CUT OUT DAMAGE, NDT VERIFIED ALL DAMAGE REMOVED PER NDTSPM 06-10-01.001. FAB REPAIR ANGLE FROM SHT 7075-0-.080 HEAT TREAT TO T6 PER DPS7.00-1. FAB FILLERS FROM SHT 7075T6-.080. INSTALLED ALL PARTS REF'S DC8-53A-011, SRM 53-4-1 FIG 40 SHT 9, 51-1-8, 51-1-20D. 2L74 4F RT4A25 20050223002282005022300228WP 2005 2 23 UPS05843869 120050209A2730179894 ACTUATOR DOUG DC8 DC871F 302199DWP COCKPIT MALFUNCTIONED A IPXAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO01748UP 45948 CREW LOST NR 2 INS WITH A WARNING LIGHT. SMELLED ELECTRICAL FUMES FROM PEDESTAL AREA. TURNED NR 2 INS OFF. NOTICED PTC WAS NOT FULLY RETRACTED AND HAD 3/8 EXTENSION SHOWING. FOLLOWED PROCEDURES FOR PTC NOT FULLY RETRACTED. CREW DECLARED EMERGENCY W/TULSA. REMOVED AND REPLACED PTC ACTUATOR AND TESTED PER MM 27-30-07. OPS CHECKS GOOD ON GROUND. 2L74 4F RT4A25 20050223002352005022300235NM 2005 2 23 UPS05543884 120050212A2560 SMOKE GOGGLES BOEING757 75724APF 1384969NM COCKPIT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01448UP 27737 CAPTS SMOKE GOGGLES CRACKED. REPLACED CAPTS GOGGLES. 2L72 4F RTA2NM 20050223002362005022300236WP 2005 2 23 UPS05843874 120050203A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01868UP 45968 C3 TAIL 60 COMPT L17LHAS 1.5 CRACK AT END FITTING STA 1771 (LWR SURFACE OF UPPER LEG). REMOVED FABRICATED AND REPLACED LONGERON 17L STA 1771 IAW SRM'S 51-1-21, 51-1-20D, 51-3-0 AND DWG 5649327. 2L74 4F RT4A25 20050223002392005022300239 2005 2 23 UPS05143870 420050210A2565 SLIDE AIRBUSA300 A300F4622R 3930360EU L1 DOOR READS LOW A IPXAK NONE O OTHER ININSP/MAINT 1 SO01153UP 0839 EMERGENCY ESCAPE SLIDE PRESSURE SHOWS IN THE RED M296931 ASSIGNED. INSPECTED L1 ESCAPE SLIDE AND FOUND PRESSURE WITHIN LIMITS PER MM 25-61-21-4 OK FOR SVD, PLACARD REMOVED. 2L72 4F RTA35EU 20050223002432005022300243NM 2005 2 23 UPS05243888 120050201A5320 ANGLE BOEING727 7271A7C 13840X2NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01935UP 20143 AFT AIRSTAIRS ANGLE CRACKED AT FORWARD SIDE OF BS 1203 FRAME LT AT S13L. STOP DRILLED CRACK IAW 51-10-1. HFEC CARRIED OUT IAW NDTM PT6 51-00 -00, CRACK CONTAINED BY STOP DRILLED HOLE. REFER TO UPS FILE NUMBER 727-53-20182. 2L73 4F A3WE 20050223002442005022300244NM 2005 2 23 UPS05243889 120050128A5523 TAB BOEING727 7271A7C 13840X2NM RT ELEVATOR DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01935UP 20143 SLIGHT DELAMINATION ON RT ELEVATOR TAB. DELAMINATED OUT OF LIMITS IAW 51-20-1. ELEVATOR TAB REMOVED AND REPAIRED IAW SRM 51-40-20 REPAIR NR 5. TAB BALANCED AND WEIGHED IAW SRM 51-80 -09. TAB REINSTALLED IAW MM 27-30-11. 2L73 4F A3WE 20050223002492005022300249NM 2005 2 23 UPS05243900 120050131A5755 SPOILER PANEL BOEING727 7271A7C 13840X2NM NR 10 SPOILER DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01935UP 20143 NR 10 SPOILER PANEL HAS AREAS OF DELAMINATION ON UPPER SURFACE. SPOILER REMOVED IAW MM 27-62-01. SPOILER PANEL REPAIRED IAW SRM 51-40-2. SPOILER PANEL REINSTALLED IAW MM 27-62-01. 2L73 4F A3WE 20050223002662005022300266NM 2005 2 23 QXEA200500015 120050102A7334 PRESSURE SWITCH DHAV DHC8 DHC8202 2809007NM NR 1 ENGINE DEFECTIVE A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09375PH 529 SEA FLIGHT NR 2052 IN CRUISE NR 2 ENGINE FUEL BYPASS FILTER CAUTION ILLUMINATED, RAN CHECKLIST. NO ENGINE SURGES, ALL OPS OK ON APPROACH WHEN POWER WAS BROUGHT BACK CAUTION CAME ON AND OFF SEVERAL TIMES. MAINTENANCE REPLACED NR 1 ENGINE HP FUEL FILTER (NO CONTAMINATION FOUND) AND NR 1 ENGINE FUEL PUMP PRESSURE DIFFERENTIAL SWITCH. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050223002802005022300280NM 2005 2 23 QXEA200500065 120050110A335018271 BATTERY DHAV DHC8 DHC8202 2809007NM CABIN DISCHARGED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09348PH1410514105 484 PDX - EMERGENCY EXIT SIGN ABOVE MAIN CABIN DOOR ENTRANCE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED PS1 POWER SUPPLY BOX AND INSTALLED BATTERY. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050224000572005022400057NM 2005 2 24 DL767050118 120050216A5312148T2610156 PRESSURE BLKHD BOEING767 767232 1385132NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27107DL 22219 MFEC INSPECTION OF THE AFT PRESSURE DOME WEB AT THE STIFFENER 16R LAP JOINT REVEALED 2 CRACKS IN THE AFT WEB PIECE. BHEC INSPECTION REVEALED 3 MORE CRACKED HOLES. THE DAMAGED SECTION OF WEB WAS REMOVED WITH A CUT OUT AND REPAIRED WITH AN ALUMINUM REPAIR DOUBLER PER ER/A 096897-14. 2L72 4F RTA1NM 20050224000602005022400060EU 2005 2 24 05FDEA00288 120050214A5270ABS030901 SWITCH AIRBUS310 A310222 3930315EU L1 DOOR MALFUNCTIONED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25452FE 313 PASSING APPROX 10,000 FT ON DEPARTURE, GOT SC AND ECAM WARNING FOR L1 DOOR UNSAFE. AFTER LEVELING OFF AND FOLLOWING ECAM PROCEDURE TO DEPRESSURIZE, FIRST OFFICER CHECKED THE DOOR WHICH INDICATED UNSAFE. UNEVENTFUL RETURN TO CDG. DESCENDING TO 4,000 FT WITH THE AIRCRAFT DEPRESSURIZED, L1 UNSAFE INDICATION AND ECAM WENT. FOUND LT DOOR HANDLE LOOSE. ADJ/TEST PERFORMED AS PER AMM:52-10-20-5. A/C RELEASED FOR SERVICE. 2L72 4F RTA35EU 20050224000622005022400062EU 2005 2 24 05FDEA00290 120050215A5730 SKIN AIRBUS310 A310203 3930313EU RT WING DAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25431FE 316 ELONGATED HOLES IN THE RT LWR WING SKIN AT 1 FASTENER HOLE FOR MANHOLE COVER 650KB. 2L72 4F RTA35EU 20050224000672005022400067EA 2005 2 24 05008620 120050108A3240 SWIVEL CNDAIRCL600 CL6002B19 1900309EA RT MLG BRAKE MISINSTALLED A VTZAO OTHER WS INADEQUATE Q C AFFECT SYSTEMS LDLANDING 1 EA27620BR 7179 BLOWN TIRE ON TAKEOFF. FERRIED THE AIRCRAFT DUE TO MULTIPLE NR 4 TIRE. MX OPS CHECKED ANTI-SKID SYSTEM. FOUND RT MLG BRAKE SWIVEL ASSY, INSTALLED BACKWARDS. REMOVED AND REPLACED NR 4 BRAKE. 2L72 4F RTA21EA 20050224000702005022400070EA 2005 2 24 COMA0560123 120050212A3260 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA MLG FALSE ACTIVATIONA COMAO OTHER N FALSE WARNING APAPPROACH 1 SO01821CA 7420 FLIGHT 5112 GEAR DISAGREE WARNING. COULD NOT DUPLICATE. RETRACT AND EXTENSION CHECKS WERE SATISFACTORY. 2L72 4F RTA21EA 20050224000732005022400073NM 2005 2 24 SB05020 120050131A2612 WARNING SYSTEM BOEING737 737401 1384701NM COCKPIT MALFUNCTIONED A USAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19421US 23988 MCO - FLT 1430 - ON CLIMB-OUT FROM MCO, EN ROUTE TO DCA, THE NR 1 ENGINE OVERHEAT LIGHT FOR THE 'B' FIRE LOOP ILLUMINATED AND WOULD NOT RESET. THE NR 1 ENGINE 'A' FIRE LOOP WAS ALREADY ON MEL. FLIGHT RETURNED TO FIELD AT MCO AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE INSPECTED THE NR 1 ENGINE FAN AND CORE AREA FOR AIR LEAKS AND DAMAGED FIRE LOOPS. NO DEFECTS NOTED. RAN ENGINE AT TAKEOFF POWER FOR SEVERAL MINUTES. ALL PARAMETERS NORMAL. THE NR 1 ENGINE 'A' FIRE LOOP REMAINS ON MEL. 2L72 4F RTA16WE 20050224000882005022400088NM 2005 2 24 AWXA200500222 120050131A533065458001186 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 MCN - MAJOR REPAIR - DURING C-16 CHECK A .1875 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT FORWARD EDGE OF L-1 DOOR UPPER HINGE CUTOUT BS 302, STR 10 LT. MAINTENANCE TRIMMED OUT CRACK IN L-1 DOOR UPPER HINGE CUTOUT BS 302, STR 10 LT; FABRICATED 2 EACH FILLERS AND A REPAIR PLATE; INSTALLED REPAIR PARTS IAW 51-10-01 FIG 205. 2L72 4F RTA16WE 20050224000922005022400092NM 2005 2 24 SB05011 120050122A49203804286242 APU BOEING737 7373B7 1384580NM APU BAY MALFUNCTIONED A USAAK NONE JH WARNING INDICATION ELECT. POWER LOSS-50 PC CRCRUISE 1 EA19391US3873638736 23313 BDL - FLT902 - EN ROUTE FROM PHL TO BDL, THE NR 1 ENG CSD LOW OIL PRESSURE LIGHT ILLUMINATED. CREW DISCONNECTED THE CSD PER QUICK REF HANDBOOK PROCEDURES AND STARTED THE APU. AFTER APPROX TEN MINUTES OF USE, THE APU OVERSPEED LIGHT ILLUMINATED AND THE APU SHUTDOWN. FLT LANDED AT BDL WITHOUT FURTHER INCIDENT. MX RECONNECTED AND SERVICED THE NR 1 ENGINE CSD OIL. ACCOMPLISHED OPERATIONAL CHECK AND FOUND FREQUENCY LOW. ADJUSTED FREQUENCY TO LIMITS PER MM 24-11-11. OPERATIONAL CHECK AND FUNCTIONAL CHECK NORMAL. RESET APU OVERSPEED AND ACCOMPLISHED NORMAL APU START. CHECKED APU GENERATOR OUTPUT. APU RUNS GOOD AND CARRIES LOAD. ACCOMPLISHED NUMEROUS APU STARTS. ALL CHECKED NORMAL. 2L72 4F RTA16WE 20050224001162005022400116SO 2005 2 24 RAIA00501034 120050113A2120 DUCT EMB 145 EMB145LR 3260212SO A/C BAY BLOWN A RAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03815HK 145048 5651- STL- LEFT PACK FAULT, LOUD NOISE. MAINTENANCE INSPECTED AND FOUND BLOWN DUCT BY NR 1 PACK, REATTACHED BLOWN DUCT AND SECURED CLAMPS. 2L72 4T RTT00011AT 20050224001192005022400119SO 2005 2 24 RAIA00501030 120050112A3620110415041 THERMAL SWITCH EMB 145 EMB145LR 3260212SO VENTRAL BAY DEFECTIVE A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03816HK 145055 5615- STL- NR 2 ENGINE BLEED LEAK LIGHT ILLUMINATED, BLEEDS ON OR OFF. MAINTENANCE REMOVED AND REPLACED TWO BLEED THERMAL SWITCHES IN THE AFT VENTRAL BAY. 2L72 4T RTT00011AT 20050224001212005022400121SO 2005 2 24 RAIA00501033 120050113A3697 WIRE EMB 145 EMB145LR 3260212SO BLEED AIR SYS DAMAGED A RAIAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 CE03816HK 145055 5663 - STL- NR 2 BLEED LEAK. MAINTENANCE REPAIRED WIRES ON BLEED AIR TEMP SENSOR. 2L72 4T RTT00011AT 20050224001332005022400133SO 2005 2 24 RAIA00501026 120050111A3350 CONNECTOR EMB 145 EMB145LR 3260212SO CABIN NOT SEATED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03817HK 145058 MX- STL- EMERGENCY LIGHT 12 C AND D ARE OUT. MAINTENANCE RESEATED CONNECTOR ON EMERGENCY LIGHT AS 12 C AND D. 2L72 4T RTT00011AT 20050224001412005022400141CE 2005 2 24 DXTA200500586 120050211A3240AE2463509G01 HOSE CESSNA500 560CESSNA 2076750CE BRAKES LEAKING E DXTAO OTHER KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 GL07366QS 5600466 POWER BRAKE SYSTEM FAILURE ON TAXI. POWER BRAKE LOW PRESS AND ANTISKID INOP LIGHTS ON. NO BRAKE PRESSURE. TROUBLESHOT SYSTEM AND FOUND RT MAIN GEAR BRAKE LINE (FLEXHOSE) P/N AE2463509G0150, LEAKING WHEN GEAR IS OFF GROUND. REMOVED LINE AND INSTALLED A NEW ONE P/N AE2463509G0150, NO S/N. BLED BRAKES AND SERVICED RESERVOIR WITH NO FURTHER LEAKS NOTED. WORK DONE WITH REFERENCE CE560 ULTRA MM 32-42-00 AND 20-10-06. 2L72 4F RTA22CE 20050224001442005022400144EA 2005 2 24 05049656 120050218A2611 SMOKE WARNING CNDAIRCL600 CL6002B19 1900309EA LAVATORY FALSE ACTIVATIONA VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27656BR 7485 SMOKE TOILET MESSAGE ON CLIMB PHASE. MX RAN ENGINES AND GOT MESSAGE WHEN RT ENGINE PACK ON. REMOVED AND REPLACED HEAT EXCHANGER, ACM, AIR CONDITIONER CONTROL PANEL. NO OIL FOUND WHILE BORESCOPING RT ENGINE. 2L72 4F RTA21EA 20050224001482005022400148WP 2005 2 24 P9RA20050062 120050102A2400 ODOR DOUG DC9 DC982 3022082WP CABIN DETECTED A P9RAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO1110801 49127 SFB TAXI OUT. RETURNED TO GATE. FLIGHT ATTENDANT REPORTED AN ELECTRICAL ODOR IN AFT SECTION OF AIRCRAFT. LOWERED AFT INTERIOR CEILING PANEL AND INSPECTED WIRING. NO DEFECTS OR DAMAGE NOTED. NO ELECTRICAL BURNING ODOR NOTED IN THE AFT SECTION OF THE CABIN. REINSTALLED AFT CEILING PANEL. 2L72 4F A6WE 20050224001582005022400158EA 2005 2 24 SWIA200514577 120050202A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07955SW 7817 MAIN FUSELAGE FLOORBEAM AT LBL 9.0 HAS OUTBOARD ATTACH ANGLE CRACKED AT FS 280.00. ITEM FOUND AT C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-21-11, 51-25-16, 51-23-00. 2L72 4F RTA21EA 20050224001682005022400168EA 2005 2 24 05042643 120050211A2741 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB MACH TRIM FAILED A VTZAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 EA271027 1027 EVENT SUMMARY STATED STAB/MACH TRIM FAIL. C/W BOMBARDIER SERVICE LETTER RJ-SL-27-083. REMOVED AND REPLACED HSTCU. OPS CHECK GOOD. 2L72 4F RTA21EA 20050224001752005022400175EA 2005 2 24 05043669 120050211A3610 SHUTOFF VALVE CNDAIRCL600 CL6002B19 1900309EA A/C PACK FAILED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27669BR 1593 EVENT SUMMARY STATED LT PACK HIGH PRESSURE WARNING. REMOVED AND REPLACED 10TH STAGE BLEED AIR SOV. OPS CHECK GOOD. 2L72 4F RTA21EA 20050224001852005022400185EA 2005 2 24 SWIA200514537 120050211A2611 SMOKE DETECTOR CNDAIRCL600 CL6002C10 1390015EA LAVATORY MALFUNCTIONED A SWIAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 NM07709SK 10159 ON TAKEOFF ROLL, RECEIVED SMOKE AFT LAV RED WARNING MSG, ABORTED TAKEOFF. NO SMOKE/FIRE REPORTED BY FLIGHT ATTENDANTS. REMOVED AND REPLACED LAV SMOKE DETECTOR IAW AMM 26-10, OPERATIONAL CHECK GOOD. P/N PU90-421R3, S/N OFF 08782. 2L72 4F RTA21EA 20050224001872005022400187NM 2005 2 24 SWAA050503 120050220A3260655825029 CIRCUIT CARD BOEING737 7373K2 13844BANM E&E BAY FAULTY A SWAAA UNSCHED LANDING N FALSE WARNING DEDESCENT 1 SW29345SA 23786 DIVERSION, AFTER TAKEOFF NOSE GEAR WOULD NOT RETRACT. CYCLED GEAR, NO HELP. REMOVED AND REPLACED S 846, S 845, M 1215 AND M 983, CARDS PER MM. 2L72 4F RTA16WE 20050224001892005022400189NM 2005 2 24 SWAA050505 120050220A5531 SPAR BOEING737 7373Q8 1384670NM VERTICAL FIN CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND VERTICAL FIN FWD AND AFT SPAR, RT AND LT CLEVIS LUGS, CORRODED. REPAIRED VERTICAL FIN PER ER. 2L72 4F RTA16WE 20050224001922005022400192NM 2005 2 24 SWAA050457 120050217A53306545800 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 270, STRINGER 10L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20050224001942005022400194NM 2005 2 24 SWAA050459 120050217A551265C25727 SKIN BOEING737 7373Q8 1384670NM HORIZONTAL STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN AT STATION 127, CRACKED. REPAIRED SKIN PER ER. 2L72 4F RTA16WE 20050224001952005022400195NM 2005 2 24 SWAA050460 120050217A555165C25154 FITTING BOEING737 7373Q8 1384670NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND LT HORIZONTAL STABILIZER LOWER THRUST BRACE LOWER ATTACH FITTING CORRODED. REPAIRED THRUST FITTING PER SRM. 2L72 4F RTA16WE 20050224001962005022400196NM 2005 2 24 SWAA050461 120050217A55116547500 SPAR BOEING737 7373Q8 1384670NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND LT HORIZONTAL STABILIZER REAR SPAR UPPER CHORD, CORRODED. REPAIRED CHORD PER SRM. 2L72 4F RTA16WE 20050224001982005022400198NM 2005 2 24 SWAA050462 120050217A53206545410 BEAM BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND 2 EACH LONGITUDINAL BEAMS FROM BS 540 TO BS 727, BETWEEN BS RBL 24 TO RBL 45, CORRODED. REPAIRED LONGITUDINAL BEAMS PER ER. 2L72 4F RTA16WE 20050224001992005022400199CE 2005 2 24 DXTA200500583 120050211A3234 HANDLE CESSNA560 560XL 2076702CE MLG INOPERATIVE E DXTAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 GL07604QS 5605204 AFTER TAKEOFF GEAR HANDLE WOULD NOT MOVE, THEREFORE COULD NOT RETRACT THE GEAR. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20050224002012005022400201EA 2005 2 24 VNAA0502003 120050205A2711 TRIM SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE AILERONS MALFUNCTIONED A VNAAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 GL05258PS 7941 THE CREW OF FLIGHT 2405 REPORTED THAT APPROXIMATELY 25 PERCENT LEFT AILERON TRIM AND 15 - 20 PERCENT LEFT RUDDER TRIM WAS REQUIRED FOR STRAIGHT AND LEVEL FLIGHT. CONTRACT MAINTENANCE IN PIT PERFORMED AN OPERATIONAL TEST OF THE AILERON TRIM SYSTEM IAW CRJ 200 AMM 27-11-00-710-802 AND AN OPERATIONAL TEST OF THE RUDDER TRIM SYSTEM IAW CRJ 200 AMM 27-21-00-710-802. ALL TEST WERE GOOD WITH NO DEFECTS FOUND. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050224002022005022400202EA 2005 2 24 VNAA0502006 120050208A5210G80082 SEAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR LEAKING A VNAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL05202PS 7858 DURING CLIMB AFTER TAKEOFF, AT 1000 FEET, THE CABIN STARTED CLIMBING WITH THE AIRCRAFT AND A LOUD SQUEAL WAS HEARD COMING FROM THE FORWARD CABIN. THE CREW OF FLIGHT 2321 RETURNED TO DAY AND MADE AN UNEVENTFUL LANDING. PSA MAINTENANCE FOUND THE PASSENGER DOOR SEAL DAMAGED. THE SEAL WAS REMOVED AND REPLACED IAW CRJ200 AMM 52-11-10-000-803 & 400-803. THE PRESSURIZATION OPERATIONAL TEST WAS GOOD IAW CRJ 200 AMM 21-31-00-863-005. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050224002042005022400204EA 2005 2 24 VNAA0502008 120050208A2730 TRANSMITTER CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE RT ELEVATOR OUT OF POSITION A VNAAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 GL05725PS 10186 AFTER DEPARTURE (CLT TO TLH) THE ELEVATOR SPLIT CAUTION MESSAGE ILLUMINATED. THE CREW OF FLIGHT 2232 FOLLOWED THE QRH, RETURNED TO CLT, AND MADE AN UNEVENTFUL LANDING. PSA MAINTENANCE AT CLT REPOSITIONED THE RT ELEVATOR POSITION TRANSMITTER IAW CRJ 700 AMM 27-34-10-400-801-A02. THE SYSTEM OPERATIONAL TEST WAS GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050224002052005022400205EA 2005 2 24 VNAA0502009 120050209A2730 TRANSMITTER CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE RT ELEVATOR OUT OF POSITION A VNAAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 GL05725PS 10186 DURING CLIMBOUT (IAD TO CLT) THE ELEVATOR SPLIT CAUTION MESSAGE ILLUMINATED. THE CREW OF FLIGHT 2231 FOLLOWED THE QRH, RETURNED TO IAD, AND MADE AN UNEVENTFUL LANDING. THE AIRCRAFT WAS INSPECTED BY CONTRACT MAINTENANCE AND THE DISCREPANCY WAS DETERMINED TO BE INDICATION ONLY. THE AIRCRAFT WAS THEN FERRIED TO DAY WHERE PSA MAINTENANCE FOUND THE RT ELEVATOR POSITION TRANSMITTER OUT OF ADJUSTMENT. THE RT TRANSMITTER WAS ADJUSTED IAW CRJ 700 AMM 27-34-10-820-801-A01. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050224002072005022400207NM 2005 2 24 SWAA050463 120050217A53106545410 BEAM BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND 3 EACH CRACKS ON LONGITUDINAL BEAMS FROM BS 540 TO BS 727B, FROM RBL 45 TO LBL 24. REPAIRED BEAMS PER ER. 2L72 4F RTA16WE 20050224002092005022400209NM 2005 2 24 SWAA050466 120050217A53116546532 FRAME BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND 2 EACH FRAMES CRACKED AT BS 480, STRINGER 8R AND STRINGER 8L. REPAIRED FRAME SECTIONS PER SRM. 2L72 4F RTA16WE 20050224002112005022400211NM 2005 2 24 SWAA050468 120050217A53156545833 FLOORBEAM BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CHORD AT BS 270, FROM LBL 11 TO RBL 11, CORRODED. REMOVED AND REPLACED CHORD PER SRM. 2L72 4F RTA16WE 20050224002132005022400213EA 2005 2 24 SWIA200514550 120050213A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07906SW 7510 AFT CABIN CEILING CEMERGENCY LIGHT INOPERATIVE. RELAMPED AFT CABIN CEILING EMERGENCY LIGHT IAW MM 33-51-16. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050224002142005022400214NM 2005 2 24 05FDEA00306 120050218A5330 SKIN BOEING727 727200 138407ENM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25496FE 21670 GOUGE IN SKIN AT BS 1069, 1 INCH ABOVE STR 25R. *S/D* REPAIRED SKIN PER SRM 53-30-3. 2L73 4F RTA3WE 20050224002162005022400216NM 2005 2 24 05FDEA00309 120050218A5330 SKIN BOEING727 727200 138407ENM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25496FE 21670 FUSELAGE SKIN GOUGED AT BS 1207, RBL 20, JUST O/B OF THE PNEUMATIC START GROUND CONNECTION ACCESS PANEL. 2L73 4F RTA3WE 20050224002182005022400218NM 2005 2 24 SWAA050470 120050217A53106519603 CREASE BEAM BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM INNER CHORD ANGLE AT BS 360, LBL 64, CORRODED. REMOVED AND REPLACED CREASE BEAM CHORD ANGLE PER SRM. 2L72 4F RTA16WE 20050224002202005022400220NM 2005 2 24 DL76K050105 120050211A324026124121A BRAKE ASSY BOEING767 767332 1382001NM NR 8 FIRE A DALAD RETURN TO BLOCK A FLAME/FIRE TXTAXI/GRND HDL 1 SO27178DZ 30596 NR 8 MAIN BRAKE FIRE AT PISTON CLOSEST TO QUICK DISCONNECT AFTER ARRIVAL AT GATE IN MCO. REPLACED NR 8 BRAKE. REPLACED NR 8 MAIN TIRE AS A PRECAUTION. INSPECTED AXLE AND AREA FOR SIGNS OF DAMAGE, NONE FOUND. 2L72 4F RTA1NM 20050224002212005022400221NM 2005 2 24 DLM90050106 120050212A494027044823 STARTER DOUG MD90 MD9030 3023690NM APU FAILED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27912DN 53392 AFTER APU START ELECTRICAL SMELL IN CABIN. APU STARTER FAILED. REPLACED APU STARTER. 2L72 4F RTA6WE 20050224002222005022400222NM 2005 2 24 DL733050107 120050214A3350 CONNECTOR BOEING737 737347 1384647NM PAX SEAT 22D/E/FDAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27302WA 23182 EMERGENCY PATH LIGHTING INOP AT 22D/E/F. FOUND ON ROUTINE MAINTENANCE INSPECTION. REPAIRED DAMAGED SIDEWALL CONNECTOR AT 22D/E/F. 2L72 4F RTA16WE 20050224002232005022400223NM 2005 2 24 DL738050108 120050215A3620 VALVE BOEING737 737832 13844CFNM CFMINTCFM567CFM567B22 13802NE NR 2 ENG PRECOOLFAILED A DALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO273759 9425 38015 888572 AS POWER WAS SET FOR T/O RT BLEED TRIP OFF LIGHT ILLUMINATED, 20 KTS ABORTED T/O. ACCOMPLISHED NNC PROCEDURE. THERE WAS A SPLIT ON LT AND RT DUCT PRESSURE. AFTER RESET, BLEED OPENED AND LT AND RT DUCT PRESSURE RETURNED TO NORMAL. REMOVED AND REPLACED PRECOOLER VALVE. RAN ENGINE PER PFHB. MSG DID NOT RETURN. 2L72 4F4 FRTA16WE E00055EN 20050224002242005022400224NM 2005 2 24 DL73S050109 120050213A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27305DL 23077 A CRACK WAS FOUND IN THE FUSELAGE SKIN JUST BELOW STRINGER 18R RUNNING ALONG THE MILL LINE OF THE BONDED INTERNAL DOUBLER. THE CRACK IS TYPICAL OF AD 2004-18-06. THE CRACK WAS REMOVED WITH A CUTOUT TO THE SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737 SRM AND ER/A 096927-14AD. 2L72 4F RTA16WE 20050224002262005022400226EA 2005 2 24 05043626 120050212A531160036030 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27626BR 7225 RIGHT FS 718 FRAME IS CRACKED AT .75 INCH IN LENGTH STR 10R - STR 12R. 2L72 4F RTA21EA 20050224002342005022400234NM 2005 2 24 05FDEA00304 120050217A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25496FE 21670 FUSELAGE SKIN DAMAGE AT BS 1187 O/B SIDE OF THE TAIL JACK ACCESS PANEL. *S/D* REPAIRED FUSELAGE SKIN BS 1187 PER SRM 53-30-3. 2L73 4F RTA3WE 20050224002362005022400236NM 2005 2 24 AWXA200500232 120050207A5310654681282 CREASE BEAM BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK A .75 INCH CRACK WAS FOUND IN WEB UNDER CREASE BEAM INNER CHORD AT BS 986.5, LBL 43. MAINTENANCE REMOVED DAMAGED WEB FROM BS 986.5 TO BS 1016, LBL 37 TO LBL 45; FABRICATED A NEW REPLACEMENT WEB PER DWG 65-46812; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 3 & 12. 2L72 4F RTA16WE 20050224002402005022400240NM 2005 2 24 CALA0500045 120050210A53116546559 FRAME BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718611 27324 INSPECTION FOUND FRAME IN AFT BAGGAGE BIN CORRODED AT STA 907 ABOVE S21R. A REPAIR WAS INSTALLED IAW SRM 51-70-11. 2L72 4F RTA16WE 20050224002412005022400241NM 2005 2 24 CALA0500047 120050220A53116546533503 FRAME BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717309 23360 INSPECTION FOUND STA 500 FRAME CORRODED AT SKIN ATTACH POINT BETWEEN S27R AND S28R, RBL 11-RBL 16. A FRAME REPAIR WAS INSTALLED IAW SRM 53-00-07, FIGURE 203. 2L72 4F RTA16WE 20050224002422005022400242NM 2005 2 24 CALA0500048 120050220A5313BAC1498161 STRINGER BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717309 23360 INSPECTION FOUND STRINGER 27L CORRODED AT RIVET HOLES BETWEEN STA 500 AND 500B. THE CORRODED SECTION OF STRINGER WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-00-03, FIGURE 201. 2L72 4F RTA16WE 20050224002432005022400243NM 2005 2 24 CALA0500049 120050221A21508102098 ACM BOEING777 777224 1385225NM LEFT SEIZED A CALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW27270151203 28678 SMOKE APPEARED IN THE CABIN AND COCKPIT WHILE EN ROUTE FROM HKG TO EWR. THE CREW DONNED OXYGEN MASKS AND COMPLETED THE APPROPRIATE CHECKLIST. THE SMOKE QUICKLY DISSIPATED. THE ACM L AND FCV L EICAS MESSAGES WERE ALSO OBSERVED. THE AIRCRAFT WAS DIVERTED TO NRT WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT ACM SEIZED WITH A BLADE MISSING AND THE DIFFUSER HOUSING WAS DETERIORATED. THE LT ACM AND DIFFUSER HOUSING WERE REMOVED AND REPLACED IAW MM 21-52-02 AND 21-52-06. LEAK AND OPERATIONAL CHECKS WERE GOOD. THE UPPER FLOW CONTROL VALVE (PACK AIR SUPPLY VALVE) WAS ALSO REMOVED AND REPLACED IAW MM 21-51-01. 2L72 4F RTT00001SE 20050224002442005022400244NM 2005 2 24 SWAA050477 120050131A3350D71702001 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29746SW 29798 DURING SPV, FOUND LT EMERGENCY EXIT AISLE LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20050224002452005022400245NM 2005 2 24 SWAA050478 120050217A276065463607 MIXER BOX BOEING737 7373H4 1384600NM SPOILER FAULTY A SWAAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 SW29622SW 27932 CREW REPORTS AILERONS BINDING. REMOVED AND REPLACED SPOILER MIXER AND RATIO CHANGER PER MM. 2L72 4F RTA16WE 20050224002482005022400248NM 2005 2 24 SWAA050447 120050216A53116516301 FRAME BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 188, RBL 33, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20050224002492005022400249NM 2005 2 24 SWAA050448 120050216A53206920158 WEB BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND FLOOR WEB FROM BS 188 TO BS 196, LBL 32 TO RBL 32, CRACKED. REMOVED AND REPLACED FLOOR WEB PER SRM. 2L72 4F RTA16WE 20050224002502005022400250NM 2005 2 24 UPS05543916 120050222A3510 OXYGEN BOTTLE BOEING757 75724APF 1384969NM COCKPIT LOW A IPXAK NONE O OTHER ININSP/MAINT 1 SO01450UP 25472 CREW OXY PRESSURE LOW OXY PRESSURE 0 PSI. REMOVED AND REPLACED CREW OXYGEN BOTTLE PER MM 12-15-08-3. 2L72 4F RTA2NM 20050224002562005022400256WP 2005 2 24 ARWA20050205 120050213A2910577412063004 LINE DOUG DC8 DC863F 302198FWP HYD SYSTEM LEAKING A ARWAO OTHER K FLUID LOSS LDLANDING 1 SO19906R 46087 AFTER LANDING LOST HYDRAULIC PRESSURE; QUANTITY DOWN TO AUX LEVEL. REMOVED AND REPLACED BOGIE TRIM CYLINDER (BTC) HYDRAULIC LINE AS PER MM 32-33-1. LEAK CHECK OK, NO LEAKS NOTED. 2L74 4F 4A25 20050224002572005022400257NM 2005 2 24 DHL2005740001 120050211A5210 HANDLE BOEING727 7272Q9 138448MNM PAX DOOR LOOSE A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01740DH 21930 OUTSIDE HANDLE ON FORWARD ENTRY DOOR SOMETIMES MOVES OUT INTO SLIPSTREAM AND ROTATES WHILE EN ROUTE. STOWED OUTSIDE HANDLE PER MM 52-11-01, OPS CHECK GOOD. 2L73 4F RTA3WE 20050224002592005022400259NM 2005 2 24 DHL2005745002 120050222A3260656021138 ACCESSORY UNIT BOEING727 727224 1384076NM MLG MALFUNCTIONED A DHLAK NONE J WARNING INDICATION ININSP/MAINT 1 SO01745DH 20665 AFTER GEAR RETRACTION, NOSE GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED. DOORS LIGHT ON S/O STATUS PANEL EXTINGUISHED. GEAR PINS INSTALLED. REMOVE BEFORE FLIGHT. REPLACED LANDING GEAR ACCESSORY UNIT. OPS CHECKS GOOD IAW B727 M/M 32-09-121. REMOVED AND STOWED LANDING GEAR SAFETY PINS IAW B727 M/M 32-00-11. 2L73 4F A3WE 20050224002612005022400261NM 2005 2 24 DHL2005780001 120050222A2560 COVER BOEING727 727223 1384074NM ESCAPE ROPE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01780DH 22006 F/O ESCAPE ROPE HATCH WILL NOT STAY CLOSED DUE TO A CRACK IN PLASTIC CASING. REPAIRED CRACK IN CASING IAW B-M/M 25-00-11, OPS CHECK GOOD. 2L73 4F A3WE 20050224002652005022400265SO 2005 2 24 RAIA00502012 120050208A3610CA33020AS5682 SEAL EMB 145 EMB145LR 3260212SO BLEED DUCT LEAKING A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03817HK 145058 STL - BLEED 1 & 2 LEAK WARNING. MAINTENANCE REMOVED AND REPLACED DUCT CLAMP AND SEAL. 2L72 4T RTT00011AT 20050224002672005022400267NM 2005 2 24 05FDEA00298 120050215A5330 SKIN DOUG MD11 MD11 3023602NM ZONE 100 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 EXTERIOR SURFACE STRAP AT STA 5-121, L48R EXISTING FASTENER HOLE FOUND ELONGATED. REPAIRED AS PER FEDEX EA 1-5310-78111. 2L73 4F RTA22WE 20050224002692005022400269NM 2005 2 24 SWAA050426 120050215A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 FOUND FUSELAGE SKIN AT BS 450, STRINGER 16R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050224002712005022400271NM 2005 2 24 SWAA050427 120050215A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED C4 CHECK, FOUND AT BS 500C + 4, STRINGER 17L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20050224002722005022400272NM 2005 2 24 SWAA050428 120050215A53306552988 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED C4 CHECK, FOUND FOUND FUSELAGE SKIN AT BS 1012, STRINGER 24R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20050224002732005022400273NM 2005 2 24 SWAA050429 120050215A57536546435335 SKIN BOEING737 7373H4 1384600NM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED C3 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP, DELAMINATED. REMOVED AND REPLACED LT WING T/E AFT FLAP PER MM. 2L72 4F RTA16WE 20050224002742005022400274NM 2005 2 24 SWAA050430 120050215A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 910, STRINGER 24R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050223002222005022300222NM 2005 2 23 UPS05443826 120050113A531365B048724 STRINGER BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 BS 1438 TO 1460 AFT RT WINDOW FORGING REMOVED FOUND STR CORROSION CRACKED. CORROSION BLEND OUT 0.100" BY 1" BY 5" EXCEED SRM LIMIT. NEW STRINGER SEGMENT, REPAIR STRAP AND SPICE ANGLE INSTALLED AS PER RS R-53-41-35248 AND ENGINEERING FILE NUMBER : 747-53-20223. 2L74 4F A20WE 20050223002232005022300223NM 2005 2 23 UPS05443827 120050113A531365B048711 STRINGER BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 BS 1560 TO 1580 AFT LT WINDOW FORGING REMOVED FOUND STR CORROSION. CORROSION BLEND OUT 0.040 INCH BY 1" BY 5" EXCEED SRM LIMIT. NEW STRINGER SEGMENT AND SPLICE ANGLE INSTALLED AS PER RS R-53-61-35239 AND ENGINEERING FILE NUMBER : 747-53-20222. 2L74 4F A20WE 20050223002322005022300232NM 2005 2 23 UPS05243878 120050201A5755 CASTING BOEING727 7271A7C 13840X2NM NR 8 SPOILER CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01935UP 20143 NR 8 SPOILER I/B END HINGE CASTING IS CRACKED AT FASTENER HOLE. HINGE CASTING REPLACED IAW SRM 51-30-2. 2L73 4F A3WE 20050223002342005022300234NM 2005 2 23 UPS05243880 120050131A5280 SUPPORT BRACKET BOEING727 7271A7C 13840X2NM NLG DOOR CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01935UP 20143 NLG DOOR FWD WALL SUPPORT BRACKET CORRODED. SUPPORT REPLACED IAW SRM 51-10-1, SRM 51-30-2 AND 53-10-00. 2L73 4F A3WE 20050223002412005022300241WP 2005 2 23 UPS05843887 120050215A3510 REGULATOR DOUG DC8 DC873F 302199FWP O2 BOTTLE LEAKING A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 DURING OXYGEN TEST, NOISE HEARD COMING FROM OXYGEN BOTTLES. REMOVED AND REPLACED CREW 02 BOTTLE REGULATOR WITH REF TO MM 35 10 04 2. OPS CKS OK. OK FOR SERVICE. 2L74 4F RT4A25 20050223002472005022300247NM 2005 2 23 UPS05243897 120050131A5755 SPOILER PANEL BOEING727 7271A7C 13840X2NM NR 11 SPOILER DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01935UP 20143 SPOILER PANEL NR 11 HAS AREA OF DELAMINATION ON UPPER SURFACE. NR 11 SPOILER PANEL REMOVED IAW MM 27-61-01. PANEL REPAIRED IAW SRM 51-40-20. SPOILER PANEL REINSTALLED IAW 27-61-01. 2L73 4F A3WE 20050223002482005022300248NM 2005 2 23 UPS05243899 120050131A5755651734748 SPOILER PANEL BOEING727 7271A7C 13840X2NM NR 3 SPOILER DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01935UP 20143 NR 3 SPOILER HAS 2 AREAS OF DELAMINATION, 1 ON THE UPPER SURFACE AND ONE ON THE LOWER SURFACE. SPOILER PANEL REPLACED IAW MM 27-61-01. 2L73 4F A3WE 20050223002562005022300256NM 2005 2 23 UPS05M43912 120050219A2560 SMOKE GOGGLES DOUG MD11 MD11F 3023600NM CABIN CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01270UP JUMP SEAT AREA RIGHT SIDE SMOKE GOGGLES NEED REPLACED LENS CRACKED. REPLACED SMOKE GOGGLES. 2L73 4F RTA22WE 20050224000512005022400051EA 2005 2 24 05007644 120050107A3150 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27644BR 7379 ANTI-ICE DUCT WARNING MESSAGE ON CLIMB-OUT. MX PERFORMED, OPS CHECK OF ANTI-ICE SYSTEM GOOD. 2L72 4F RTA21EA 20050224000542005022400054 2005 2 24 05011673 420050111A34183995100208 COMPUTER CNDAIRCL600 CL6002B19 1900309EA STALL WARNING DEFECTIVE A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27673BR 7599 STALL FAIL MESSAGE ON TAKEOFF. MX REMOVED AND REPLACED SPC. OPS CHECK GOOD IAW 27-35-01. 2L72 4F RTA21EA 20050224000632005022400063 2005 2 24 05006660 420050106A34183995100208 COMPUTER CNDAIRCL600 CL6002B19 1900309EA STALL WARNING FAULTY A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27660BR 7519 STALL FAIL MESSAGE IN CLIMB PHASE. MX REMOVED AND REPLACED SPC. 2L72 4F RTA21EA 20050224000642005022400064WP 2005 2 24 05FDEA00291 120050215A4950 BUTTERFLY VALVE DOUG DC10 DC1030 3023501WP BLEED VALVE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25309FE 48298 DURING COMPLIANCE WITH WIC 49C1701 SEQ 267, FOUND APU NR 2 SYSTEM LOW PRESSURE BLEED VALVE BUTTERFLY CRACKED AND WITH MISSING MATERIAL THAT RESULTED TO NR 2 ENGINE CHANGE. 2L73 4F A22WE 20050224000682005022400068EA 2005 2 24 05048670 120050217A3250 TILLER CNDAIRCL600 CL6002B19 1900309EA COCKPIT STUCK A VTZAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA27670BR 1117 EVENT SUMMARY STATED TILLER STUCK TO LEFT ON TAKEOFF ROLL, RTG. REMOVED AND REPLACED NWS MODULE. 2L72 4F RTA21EA 20050224000712005022400071EA 2005 2 24 COMA0570017 120050215A531067053110471 BEAM CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01369CA5902 10079 TRANSVERSE BEAM AT FS 280 FROM LBL 36 TO RBL 36 IS CORRODED ALONG THE UPPER AND LOWER EDGES. REPLACED THE TRANSVERSE BEAM AT FS 280 IAW BOMBARDIER AEROSPACE REO 670-53-11-047, BRAS EO'S 610R-53-5986, 601R-53-5987, 601R-53-5977 AND CRJ 700 SRM 51-42-06-001-001-AO1. 2L72 4F RTA21EA 20050224000772005022400077NM 2005 2 24 SWAA050408 120050211A53116546579 FRAME BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 1128, RBL 26, CORRODED. REMOVED AND REPLACED FRAME SECTION PER BAC DRAWING, SRM. 2L72 4F RTA16WE 20050224000802005022400080NM 2005 2 24 SWAA050411 120050213A531069353656 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 DURING SPV, FOUND SHEAR TIE AT BS 360, BETWEEN STRINGERS 14R AND 15R, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050224000852005022400085EU 2005 2 24 AWXA200500219 120050205A5315D53112091200 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28659AW 1166 SAL - MAJOR REPAIR - DURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOOR SUPPORT BEAM Y1292 AT FR 16. MAINTENANCE CUT OUT DAMAGED SECTION OF FLOOR SUPPORT BEAM Y1292 AT FR 16; FABRICATED A NEW SECTION OF BEAM AND SPLICE REPAIR; INSTALLED REPAIR PARTS IAW A320 SRM 53-11-14 FIG 202. 2L72 4F RTA28NM 20050224000862005022400086EU 2005 2 24 AWXA200500220 120050205A5315D53112090200 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28659AW 1166 SAL - MAJOR REPAIR - DURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOOR SUPPORT BEAM Y765 AT FR 16. MAINTENANCE CUT OUT DAMAGED SECTION OF FLOOR SUPPORT BEAM Y765 AT FR 16; FABRICATED A NEW SECTION OF BEAM AND A SPLICE REPAIR; INSTALLED REPAIR PARTS IAW A320 SRM 53-11-14 FIG 202. 2L72 4F RTA28NM 20050224000872005022400087 2005 2 24 AWXA200500221 420050205A2565D37865110 CONTAINER AIRBUS320 A320232 3930326EU RT WING SLIDE DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28659AW 1166 SAL - EES - DURING BC-4 CHECK THE EXTERIOR SURFACE OF THE RT OVERWING SLIDE STOWAGE CONTAINER WAS FOUND DELAMINATED AT THE FORWARD LOWER CORNER. MAINTENANCE REMOVED AND REPLACED THE RT OVERWING SLIDE ASSEMBLY IAW T/C C1A25301. 2L72 4F RTA28NM 20050224000992005022400099EU 2005 2 24 05FDEA00300 120050217A2170 COALESCER BAG AIRBUS310 A310222 3930315EU CABIN AIR CONTAMINATED A FDEAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO25447FE 251 ON FINAL NR 2 TURBINE INLET TEMP AT 100C, ECAM ADVISORY FLASHING, SHORTLY THEREAFTER SMELLED FUMES IN COCKPIT. TURNED OFF NR 2 PACK. DECLARED EMERGENCY. COMPLIED WITH CFM PROCEDURES, LANDED UNEVENTFULLY. BITE CHECKED NR 2 PACK TEMP CONTROLLER (NO FAULTS FOUND). REPLACED NR 2 PACK WATER SEPARATOR COALESCER BAG IAW M/M 21-51-16-3. NR 2 PACK OPERATES NORMALLY, OK FOR SERVICE. 2L72 4F RTA35EU 20050224001022005022400102NM 2005 2 24 05FDEA00302 120050217A5330 SKIN BOEING727 727200 138407ENM FUSELAGE LIGHTNING STRIKEA FDEAK NONE O OTHER ININSP/MAINT 1 SO25496FE 21670 LIGHTING STRIKE IN RIVET AT BS 312, 3 INCHES ABOVE STR 21L. REPAIRED SKIN AT BS 312 3 INCHES ABOVE STR 21L PER SRM 53-30-3. 2L73 4F RTA3WE 20050224001072005022400107 2005 2 24 DXTA200500588 420050212A22109516X166 CABLE CESSNA750 750 2076810CE ACTUATOR CRACKED E DXTAO OTHER E VIBRATION/BUFFET CRCRUISE 1 GL07903QS 7500162 AT FL410 WITH AUTOPILOT ENGAGED, ACFT BEGAN 10 DEG LT & RT ROLL OSCILLATION WITH A 1 SEC TIME AMPLITUDE. OSCILLATIONS CONTINUED 18 MINS. OPS NORMAL WITH AP DISENGAGED. DESCENDED TO FL360. RE-ENGAGED AP & 5 MINS LATER AUTO PILOT ENGAGED, OSCILLATIONS BEGAN AGAIN WITH CYAN CAS MESSAGE AILERON RATIO LOW. CONFIRMED LT AILERON OSCILLATING. ALL HYD PRESS & QTY NORMAL. FOUND FWD FUSELAGE AILERON CABLE TENSION HIGH. ADJUSTED Y2 TURN IN SPEC. CHECKED & FOUND LT AILERON POSITION DRIVE COUPLER CRACKED, REPLACED AILERON RESOLVER FLEX LINE. CHECKED & FOUND A+B AILERON RATIO ACTUATORS LEAKING, REPLACED BOTH ACTUATORS. INSTALLED FWD FAIRING PANELS, INSPECTED RIG & CONDITION OF AILERON RESOLVER SYS, NO DEFECTS. 2L72 4J RTT00007WI 20050224001172005022400117SO 2005 2 24 RAIA00501038 120050116A3412102AU1AF PROBE EMB 145 EMB145LR 3260212SO NR 1 TAT FAILED A RAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03842HK1127 14500830 7994- STL- NR 1 TAT HEAT FAULT MESSAGE. MAINTENANCE REPLACED NR 1 TAT PROBE. 2L72 4T RTT00011AT 20050224001322005022400132SO 2005 2 24 RAIA00501031 120050112A2150 COUPLING EMB 145 EMB145LR 3260212SO HEAT EXCHANGER LOOSE A RAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03815HK 145048 5658 - MKE- PACK 1 VALVE CLOSED UNCOMMANDED IN FLIGHT. MAINTENANCE DEFERRED AIR CONDITIONING PACK SYSTEM PER MEL 21-51-00 CAT C. SUBSEQUENTLY, RE-SECURED COUPLING ON HEAT EXCHANGER, OPS CHECK GOOD. 2L72 4T RTT00011AT 20050224001452005022400145EA 2005 2 24 05050679 120050219A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A VTZAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 EA27679BR 7662 FLAP FAILURE AT 0 DEGREES ON APPROACH. DIVERTED DUE TO RUNWAY TOO SHORT. MX OPS CHECKED FLAP SYSTEM. 2L72 4F RTA21EA 20050224001502005022400150EA 2005 2 24 SWIA200514572 120050129A5320 WEB CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07440SW 7589 AFT EQUIPMENT BAY ESB HAS A CRACK; FS 625.00 LBL - 38.0 LOWER WEB. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED LOWER WEB IAW CRJ REO 601R-53-61-358 REV A. 2L72 4F RTA21EA 20050224001742005022400174EA 2005 2 24 COMA0560121 120050214A3010 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA ANTI ICE SYSTEM FALSE INDICATIONA COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01916CA 7014 FLIGHT 5532 ANTI-ICE DUCT WARNING. COULD NOT DUPLICATE. OPERATIONAL CHECK OF ANTI ICE SYSTEM WAS NORMAL. 2L72 4F RTA21EA 20050224001782005022400178EA 2005 2 24 SWIA200514533 120050207A2721 SWITCH CNDAIRCL600 CL6002B19 1900309EA RUDDER TRIM FAILED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07969SW 7876 AILERON TRIM SWITCH ONLY WORKS IN ONE DIRECTION. REMOVED AND REPLACED AILERON/RUDDER TRIM PANEL IAW CRJ MM 27-22-00. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050224001862005022400186NM 2005 2 24 SWAA050484 120050218A53116546533 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 DURING SPV, FOUND FRAME AT BS 500, STRINGER 9L, CRACKED. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050224002032005022400203EA 2005 2 24 VNAA0502010 120050210A27303A2237B SENSOR CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE LT ELEVATOR FAILED A VNAAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 GL05725PS67 10186 DURING CRUISE (CLT TO TLH) THE ELEVATOR SPLIT CAUTION MESSAGE ILLUMINATED. THE CREW OF FLIGHT 2245 FOLLOWED THE QRH, DIVERTED TO JAX, AND MADE AN UNEVENTFUL LANDING. THE AIRCRAFT WAS INSPECTED BY CONTRACT MAINTENANCE AND THE DISCREPANCY WAS DETERMINED TO BE INDICATION ONLY. THE AIRCRAFT WAS THEN FERRIED TO DAY WHERE PSA MAINTENANCE REMOVED AND REPLACED THE RH ELEVATOR POSITION TRANSMITTER WITH A SERVICEABLE UNIT IAW CRJ 700 AMM 27-34-10-000-801-A02 AND 27-34-10-400-801-A02. THE TRANSMITTER WAS ADJUSTED IAW CRJ 700 AMM 27-34-10-820-801-A01 AND RIL 0194. THE SYSTEM OPERATIONALLY CHECKED GOOD IAW CRJ 700 AMM 27-34-10-710-801-A01. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050224002282005022400228NM 2005 2 24 SWAA050473 120050217A53106547977 CREASE BEAM BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 638, CRACKED. REMOVED AND REPLACED CREASE BEAM WEB PER SRM. 2L72 4F RTA16WE 20050224002302005022400230NM 2005 2 24 SWAA050475 120050217A57116545321 SPAR BOEING737 7373Q8 1384670NM RT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND RT WING REAR SPAR UPPER CHORD AT STATION 223, CRACKED. REMOVED AND REPLACED REAR SPAR SECTION PER ER AND BAC DRAWING. 2L72 4F RTA16WE 20050224002352005022400235NM 2005 2 24 AWXA200500231 120050216A3397BMS13311122 WIRE BOEING757 7572S7 1384962NM SEAT ROW 23 LT BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28902AW 23322 PHX - EEL - DURING 4-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 23 LT INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 23 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20050224002462005022400246NM 2005 2 24 SWAA050479 120050217A53156546811 FLOORBEAM BOEING737 7375H4 138449DNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29502SW 24179 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM TEE CAP AT BS 986, FROM RBL 48 TO BL 0, CORRODED. REPAIRED TEE CAP PER EA. 2L72 4F RTA16WE 20050224002512005022400251NM 2005 2 24 UPS05643918 120050222A2560 SMOKE GOGGLES BOEING767 76734AF 1385212NM COCKPIT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01330UP 27756 INSPECTION TYPE:N/A, F/O SMOKE GOGGLES CRACKED. INSTALLED NEW SET OF SMOKE GOGGLES. 2L72 4F RTA1NM 20050224002752005022400275NE 2005 2 24 20030779 320050105A6110HCE4A3I PROPELLER BEECH 1900 1900D 1154162CE HARTZLHCE4A HCE4A3I NE LT ENGINE DEFECTIVE A GLBAK NONE E VIBRATION/BUFFET ININSP/MAINT 1 NM03122UX16330770 UE122 HJ558 WHILE MAINTENANCE WAS PERFORMING A PRE-RELEASE AUTOFEATHER TEST, UNUSUAL VIBRATION WAS NOTED COMING FROM LT ENGINE AND PROP. ENGINE WAS SHUTDOWN WITHOUT INCIDENT AND UPON INVESTIGATION INTERNAL FAILURE WAS OBVIOUS DUE TO BLADE MOVEMENT. PROPELLER REMOVED FROM AIRCRAFT FOR TEARDOWN INVESTIGATION AND SPECIAL SOAP SAMPLE WAS TAKEN. 2L72 4T RTA24CE 5 CP10NE 20050224002882005022400288WP 2005 2 24 AALA20050115 120050211A2120 SMOKE DOUG DC9 DC982 3022082WP CABIN DETECTED A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21574AA 53151 DFW INFLIGHT T2324/11 - STRONG ODOR OF OILY SMELL IN COCKPIT AT LIFT OFF. F/A REPORTED SMOKE IN CABIN. ALSO, VERY LIGHT HAZE IN COCKPIT. TURNED OFF RECIRCULATION FAX AND OPENED RADIO RACK VENTURE IN ATTEMPT TO REMOVE SMOKE. ACCOMPLISHED SMOKE OR FUME REMOVAL CHECK LIST. FLIGHT ATTENDANT REPORTED SMOKE BEGAN TO DISSIPATE ABOUT THREE MINUTES LATER BUT SMOKE IN SMALL AMOUNTS REMAINED UNTIL LANDING. FLIGHT ATTENDANT REPORTED SMOKE WAS WORSE IN AFT CABIN THAN IN FORWARD CABIN. ACCOMPLISHED WORKCARDS 5701, 21 96 01 AND 21 92 12 (PACK BURN) AND REPLACED COALESCER BAGS AND CLEANED OUT COALESCER FAN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050224002902005022400290NM 2005 2 24 AALA20050093 120050207A33500201922001 LIGHT BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21372AA 25199 SFO - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 32B INOPERATIVE. REPLACED LIGHT ASSEMBLY AT SEAT 32AB FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 32B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050224002922005022400292NM 2005 2 24 AALA2005112 120050209A2612 FIRE LOOP BOEING767 767223 1385123NM RT ENGINE DEFECTIVE A AALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW21325AA 22326 20 MINUTES INTO FLIGHT THE RIGHT ENGINE LOOP 1 EICAS MESSAGE CAME ON INTERMITTENTLY FOR ABOUT 10 TO 20 SECONDS AT A TIME. ABOUT FIVE MINUTE LATER THE SYSTEM FAIL LIGHT CAME ON. RESET IT ONCE BUT IT CAME BACK WITH BOTH 1 AND 2 LOOPS INDICATING FAILED. DIVERTED TO STL. REPLACED RIGHT ENGINE TS45 AND TS46 FIRE LOOPS ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050224002942005022400294WP 2005 2 24 AALA20050097 120050207A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21219AA 49171 DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT 22D INOPERATIVE. REPLACED THE SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT 22D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050224002952005022400295WP 2005 2 24 AALA20050113 120050210A2150 ACM DOUG DC9 DC982 3022082WP A/C BAY LEAKING A AALAA UNSCHED LANDING KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21408AA 49319 LAX - AFTER TAKEOFF AT ABOUT 200 FEET, SMELL OF SMOKE AND VISIBLE SMOKE IN COCKPIT AND CABIN. SMELL AND SMOKE CONTINUED FOR SEVERAL MINUTES TO APPROXIMATELY 5000 FEET. ALL ENGINE AND AIR CONDITIONING PACKS APPEAR NORMAL. REPLACED COALESCER BAGS IN AIR CONDITIONING WATER SEPARATOR. FOUND INTERNAL OIL LEAK ON LEFT HAND AIR CYCLE MACHINE. INSTALLED NEW CLAMP AND SHIMMED AIR CYCLE MACHINE TO HEAT EXCHANGER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050224002972005022400297WP 2005 2 24 AALA20050104 120050212A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW217518A 49895 SFO - CEILING EMERGENCY LIGHTS OVER SEATS 17 TO 21 INOPERATIVE. REPLACED BATTERY PACK B5104 FOR CEILING EMERGENCY LIGHTS OVER SEATS 17 TO 21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050224002992005022400299WP 2005 2 24 AALA20050108 120050213A3350 LIGHT DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW219402W 53138 DFW - SEAT MOUNTED EMERGENCY LIGHTS AT SEATS 8D AND 18D INOPERATIVE. REPLACED THE SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AT SEATS 8D AND 18D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050224003012005022400301WP 2005 2 24 AALA20050096 120050207A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21489AA 49682 DFW - AFT SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT 27D INOPERATIVE. REPLACED THE AFT SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT 27D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050225000042005022500004NM 2005 2 25 SWAA050449 120050216A53306545800 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN AT FWD SERVICE DOOR LOWER HINGE CUTOUT, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050225000052005022500005EA 2005 2 25 COMA0560120 120050208A3350364911 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A COMAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01937CA 7044 FLIGHT 5908 FORWARD SECTION OF EMERGENCY FLOOR PATH LIGHTING IS INOP. REPLACED FORWARD SECTION OF FLEX LAMP. 2L72 4F RTA21EA 20050225000072005022500007EU 2005 2 25 AWXA200500233 120050214A321348290 BEARING AIRBUS320 A320232 3930326EU NR 1 AXLE DISINTEGRATED A AWXAO OTHER O OTHER TXTAXI/GRND HDL 1 WP28654AW 1050 UPON ARRIVAL, ACFT WAS TAXIING TO GATE A RAMPER OBSERVED SPARKS COMING OUT OF LT OUTBOARD WHEEL ASSEMBLY AND NOTICED THE BRAKE FAN WAS RUNNING. MAINTENANCE REMOVED THE NR 1 WHEEL ASSEMBLY AND FOUND THE INNER BEARING HAD DISINTEGRATED; THE OUTER BEARING WAS NOT DAMAGED. AFTER REMOVING BRAKE, FOUND AXLE SLEEVE BENT & MELTED TO THE LOWER AXLE LEG, HAD TO CUT THE SLEEVE TO REMOVE IT. REMOVED AND REPLACED LT MLG SHOCK ABSORBER IAW T/C R4M32307, AND NR 1 AXLE SLEEVE ASSEMBLY. REPLACED BOTH THE NR 1 & NR 2 WHEEL/TIRE AND BRAKE ASSEMBLIES, THE NR 1 AXLE ANTISKID TACHOMETER WAS ALSO REPLACED DUE TO HEAT DAMAGE. 2L72 4F RTA28NM 20050225000082005022500008EA 2005 2 25 COMA0560119 120050208A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01936CA 7043 FLIGHT 5144 FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINT PER MEL AND AD 98-20-01. 2L72 4F RTA21EA 20050225000102005022500010NM 2005 2 25 SWAA050451 120050216A53116546525 FRAME BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 380, STRINGER 13L, CRACKED. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20050225000112005022500011NM 2005 2 25 SWAA050452 120050216A53306545765 SKIN BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29686SW 23175 DURING SCHEDULED C3 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS FROM BS 500D, BS 520, STRINGER 12R. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20050225000122005022500012NM 2005 2 25 SWAA050453 120050216A3350101073 LENS BOEING737 737317 138447PNM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29686SW 23175 DURING SCHEDULED C3 CHECK, FOUND R2 DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS, BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20050225000142005022500014NM 2005 2 25 SWAA050454 120050216A52306547953 TEE FITTING BOEING737 7375H4 138449DNM AFT CARGO DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29502SW 24179 DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO DOOR AFT LOWER TEE CHORD, CRACKED. REMOVED AND REPLACED TEE CHORD PER SRM. 2L72 4F RTA16WE 20050225000152005022500015NE 2005 2 25 DXTA200500601 220050219A720031J190001 ENGINE CESSNA560 560XL 2076702CE PWA 545 PW545A NE NR 1 LEAKING E DXTAA UNSCHED LANDING KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07670QS3774 5605170 PCEDB0349 DURING FLIGHT CREW & PASSENGERS NOTICED FUMES IN CABIN. AFTER LANDING FOUND OIL LEAKING FROM NR 1 ENGINE & NO OIL SHOWING ON SIGHT GAUGE. ENGINE CHANGE CURRENTLY IN WORK. 2L72 4F4 FRTA22CE E00059EN 20050225000172005022500017NM 2005 2 25 AWXA200500235 120050208A5315 FLOORBEAM BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM STIFFENER ANGLE ON AFT SIDE FLOORBEAM AT BS 328, BETWEEN RBL 43 AND RBL 60. MAINTENANCE REMOVED CORRODED FLOORBEAM STIFFENER ANGLE AT BS 328, FROM RBL 43 TO RBL 60; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 65-45812; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 12. 2L72 4F RTA16WE 20050225000182005022500018NM 2005 2 25 AWXA200500236 120050122A53206545834259 STIFFENER BOEING737 737301 1384611NM FLOOR SUPPORT CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK GALVANIC CORROSION WAS FOUND ON FLOOR SUPPORT STIFFENER AT LBL 11, BETWEEN BS 331 AND BS 341. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT STIFFENER AT LBL 11, FROM BS 331 TO BS 341; FABRICATED A NEW REPLACEMENT STIFFENER PER DWG 65-45834; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 12. 2L72 4F RTA16WE 20050225000192005022500019NM 2005 2 25 AWXA200500237 120050122A53206545834260 STIFFENER BOEING737 737301 1384611NM FLOOR SUPPORT CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOOR SUPPORT STIFFENER AT RBL 11, BETWEEN BS 315 AND BS 326. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT STIFFENER AT RBL 11, FROM BS 315 TO BS 326; FABRICATED A NEW REPLACEMENT STIFFENER PER DWG 65-45834; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 12. 2L72 4F RTA16WE 20050225000202005022500020NM 2005 2 25 AWXA200500238 120050124A33501012621 LIGHT BOEING737 7373G7 1384595NM FUSELAGE BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 MCN - MAJOR REPAIR - DURING C-16 CHECK FOUND THE EMERGENCY EXIT LIGHT BROKEN AT THE LOWER FORWARD SIDE OF R-1 DOOR. MAINTENANCE REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT THE LOWER FORWARD SIDE OF R-1 DOOR, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050225000212005022500021NM 2005 2 25 AWXA200500239 120050122A52106545871515 DOOR FRAME BOEING737 7373G7 1384595NM R1 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 MCN - MAJOR REPAIR - DURING C-16 CHECK A .375 INCH CRACK WAS FOUND IN R-1 DOOR FRAME AT 4TH DOOR STOP CUTOUT FROM BOTTOM BS 328, RBL 65, WL 249. MAINTENANCE TRIMMED OUT CRACK IN R-1 DOOR FRAME; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW ER 03-5200-05048-ES2. 2L72 4F RTA16WE 20050225000222005022500022NM 2005 2 25 AWXA200500240 120050122A52106545871515 DOOR FRAME BOEING737 7373G7 1384595NM R-1 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 MCN - MAJOR REPAIR - DURING C-16 CHECK A .375 INCH CRACK WAS FOUND IN R-1 DOOR FRAME AT 3RD DOOR STOP CUTOUT FROM BOTTOM BS 328, RBL 65, WL 249. MAINTENANCE TRIMMED OUT CRACK IN R-1 DOOR FRAME; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW ER 03-5200-05048-ES2. 2L72 4F RTA16WE 20050225000232005022500023CE 2005 2 25 DXTA200500598 120050218A494023080005 STARTER HONEYWELL GTCP36150W RAYTHNDH125 HAWKER800XP 7150012CE APU FAILED E DXTAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 GL07893QS 101 P546 258393 UPON LANDING CREW SMELLED ELECTRICAL BURNING OF UNKNOWN ORIGINAL IN COCKPIT, NO SMOKE OBSERVED. NO SMELL IN CABIN, WINDSCREEN HEAT OFF. APU STARTER GENERATOR FOUND TO BE CAUSE OF PROBLEM. 2L72 4F RTA3EU 20050225000242005022500024CE 2005 2 25 DXTA200500599 120050218A3241MP50B1 PUMP CESSNA560 560XL 2076702CE FWD SERVICE BAY FAILED E DXTAA UNSCHED LANDING JBSWARNING INDICATION SMOKE/FUMES/ODORS/SPARKS AFFECT SYSTEMS CRCRUISE 1 GL07699QS3020 5605199 LOW BRAKE PRESSURE AND ANTI-SKID INOP. ANNUNCIATORS ILLUMINATED WITH MASTER CAUTION. BRAKE PUMP WOULD NOT RUN. SMELL OF ELECTRICAL BURN IN COCKPIT. AFTER APPROX 5 MINUTES LIGHTS EXTINGUISHED AND PUMP OPERATED AGAIN. 2L72 4F RTA22CE 20050225000252005022500025NM 2005 2 25 DHL2005781502 120050211A5754 SKIN BOEING727 727227 1384078NM NR 4 SLAT DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A C-CHECK, LT WING L/E SKIN DENTED 15 INCHES I/B OF NR 4 SLAT I/B TRACK. CUT OUT DAMAGED AREA LT WING LEADING EDGE SKIN I/B NR 4 SLAT I/B TRACK DIM .75 X .75 INCH IAW B727 SRM 57-30-4 FIG 1. FABRICATED DOUBLER REPAIR MATL USED 2024-T3 .050 PO 9001873 DIM 3.25 X 3.75 IAW B727 SRM 57-30-3 FIG 3 AND 57-30-4 FIG 1, TREATED AND PRIMED IAW B727 SRM 51-10-2, INSTALLED REPAIR DOUBLER AT LT WING L/E SKIN I/B NR 4 SLAT I/B TRACK IAW B727 SRM 51-30-2. 2L73 4F A3WE 20050225000282005022500028EA 2005 2 25 SWIA200514568 120050129A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA FLOORBEAM CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07440SW 7589 MAIN FUSELAGE FS 280.00 RBL 9.0 INBOARD CLIP CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIP IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, AND 51-23-00. 2L72 4F RTA21EA 20050225000312005022500031NM 2005 2 25 SWAA050442 120050216A2121215201 GASPER FAN BOEING737 7373A4 1384585NM E & E BAY OVERHEATED A SWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW29678AA 23290 DIVERSION, DECLARED EMERGENCY. F/A REPORTED A BURNING ELECTRICAL SMELL IN CABIN. REMOVED AND REPLACED GASPER FAN PER MM. 2L72 4F RTA16WE 20050225000332005022500033NM 2005 2 25 DHL2005740002 120050218A3350 COVER BOEING727 7272Q9 138448MNM EMERGENCY LIGHT DISLODGED A DHLAO OTHER O OTHER CLCLIMB 1 SO01740DH 21930 AFT EMERGENCY LIGHT COVER FELL OFF ON CLIMBOUT. RESECURED LIGHT ASSY AND OPS CHECKED GOOD IAW MM 33-50-01. 2L73 4F RTA3WE 20050225000362005022500036EA 2005 2 25 COMA0560115 120050209A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01479CA 7675 FLIGHT 5469 FLAPS FAIL CAUTION. INSPECTED FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20050225000382005022500038NM 2005 2 25 05FDEA00311 120050219A5312NJC60403 BULKHEAD DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25591FE 48527 DENT COMMON TO THE AFT PRESSURE BULKHEAD WEB AT STA 2007 RBL 5.50, 70 INCHES ABOVE FLOOR PANEL. REPETITIVE INSPECTION ARE REQUIRED AT EACH SUBSEQUENT C-CHECK AS PER FEDEX EA 1-5340-81609 PART 2. 2L73 4F RTA22WE 20050225000422005022500042CE 2005 2 25 DXTA200500606 120050221A2731 CONTROL SYSTEM RAYTHNDH125 HAWKER800XP 7150012CE ELEVATOR TRIM MALFUNCTIONED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07873QS 258573 ELEVATOR/AILERON TRIM LIGHT ILLUMINATED AS POWER LEVERS WERE ADVANCED. RAN TRIMS FULL TRAVEL BOTH WAYS WOULD NOT EXTINGUISH. 2L72 4F RTA3EU 20050225000432005022500043CE 2005 2 25 DXTA200500605 120050221A215073838433 ACM CESSNA750 750 2076810CE CABIN COOLING DISINTEGRATED E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 GL07908QS1776 7500108 DESCENDING FROM FL 410, LOAD POP HEARD FROM REAR OF AIRPLANE AND SMOKE SMELL FILLED THE COCKPIT. PER CHECKLIST ISOLATED THE COCKPIT PAC AND THE SMOKE DISSIPATED. TROUBLESHOT TO COCKPIT ACM TURBINE (COMING APART). REMOVED & REPLACED COCKPIT ACM IAW CE 750 MM 21-51-00. OPERATIONAL CHECKS GOOD. 2L72 4J RTT00007WI 20050225000462005022500046NM 2005 2 25 375PA0031 120050221A5314 KEELBEAM BOEING737 737317 138447PNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05375PA 23812 CORROSION ON HORIZONTAL FLANGE OF THE RIGHT KEEL BEAM AT BS 520 AT RBL 6.5. REPAIRED PER EA 53-030. 2L72 4F RTA16WE 20050225000492005022500049SO 2005 2 25 CHQA200500036 120050217A2611 WARNING LIGHT EMB 145 EMB145LR 3260212SO LAVATORY ILLUMINATED A CHQAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL11576RP 14500856 FLIGHT 6300 MCO-FLL - DURING CLIMBOUT A LAV SMOKE MESSAGE APPEARED ON EICAS AND A SLIGHT HAZE WAS NOTED IN THE COCKPIT. THE AIRCRAFT RETURNED TO THE FIELD FOR AN UNEVENTFUL LANDING. MAINTENANCE PERFORMED ENGINE RUNS IAW EMB 145 RR AMM 71-00-01. PERFORMED LAV SMOKE OPERATIONAL CHECK IAW EMB 145 AMM 26-14-00. ALL SYSTEMS OPS CHECK GOOD WITH NO DEFECTS NOTED. 2L72 4T RTT00011AT 20050225000522005022500052SO 2005 2 25 CHQA200500033 120050216A3350 LAMP EMB 135 EMB135KL 3260302SO EMERGENCY LIGHT BURNED OUT A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11377SK 145579 LEFT OVERWING EMERGENCY EGRESS LIGHT IS INOP. RELAMPED IAW EMB 140 MM 33-50-07. 2L72 4F RTT00011AT 20050225000542005022500054EA 2005 2 25 COMA0560130 120050216A27801104SD100201 DRIVE SHAFT CNDAIRCL600 CL6002B19 1900309EA LT WING WORN A COMAA UNSCHED LANDING O OTHER CRCRUISE 1 SO01819CA 7415 FLIGHT 5808 DURING CRUISE FLIGHT RECEIVED A FLAP FAIL CAUTION, CREW DECLARED AN EMERGENCY AND LANDED AT CVG WITHOUT INCIDENT. REPLACED LEFT WING FLEX DRIVE SHAFT NR 2. 2L72 4F RTA21EA 20050225000572005022500057EU 2005 2 25 MALA050156 120050214A3260 UPLOCK BAC 146 AVRO146RJ85A1500097EU MLG INOPERATIVE A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15502XJ E2307 LEFT MAIN GEAR INTRANSIT LIGHT AS WELL AS HANDLE LIGHT REMAINED ON FOR 20-30 SEC, CYCLED GEAR AND BOTH REMAINED ILLUMINATED. A/C TO BE FERRIED FROM DSM TO DTW WITH LT MLG UPLOCK INDICATION INOP. A/C TO BE FLOWN WITH VISUAL CONFRONTATION OF GEAR RETRACTION IF NORMAL GEAR UP INDICATION. NO FLT RESTRICTIONS IF TRANSIT LIGHT STAYS ON A ALTITUDE RESTRICTIONS TO 20,000 FT, MAX AIRSPEED OF 210 KNOTS. FOUND LT UPLOCK PROXIMITY SWITCH WIRE BAD INSIDE THE SWITCH. REMOVED AND REPLACED LT UPLOCK PROX SWITCH CYCLE GEAR SEVERAL TIMES. OPS CHECK GOOD ON GROUND IAW AVRO MM 32-30-00. P/N 8-018-01. 2H74 4F RTA49EU 20050225000592005022500059EU 2005 2 25 MALA050152 120050214A5320 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15430XJ 340B430 DURING 4Y/2Y CHECK FOUND SEAT TRACK AT LBL 18.3 FROM FS 297 TO FS 310 IS CORRODED AND HAS BEEN REPAIRED IAW SRM 53-70-60. 2L72 4T RTA52EU 20050225000602005022500060EU 2005 2 25 MALA050148 120050207A5320 AIRSTAIR TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15402XJ 340B402 DURING 4K CHECK FOUND RAIL ASSEMBLY, P/N 7253710-871 BETWEEN FS 258 AND 288 IS CORRODED AND WILL BE REPLACED IAW SRM 51-40-21. 2L72 4T RTA52EU 20050225000612005022500061SO 2005 2 25 CHQA200500031 120050213A2120 ENGINE EMB 145 EMB145LR 3260212SO CONTAMINATED A CHQAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL11258JQ 145768 CLIMBING AT 10,000 FT A BURNING SMELL WAS NOTED IN THE COCKPIT. WITHIN A FEW SECONDS, THE SMELL GOT REALLY STRONG AND THE PILOT'S NOSE AND EYES BEGAN TO BURN. THE FLIGHT ATTENDANT AND PASSENGERS ALSO NOTICED THE SMELL. THE CREW CALLED ATC AND ATC DECLARED AN EMERGENCY. THERE WAS NO INDICATION OF SMOKE OR A FIRE ON EICAS. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED UNEVENTFULLY. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND DE-ICING GLYCOL IN THE ENGINE INLETS. MAINTENANCE ALSO INSPECTED THE BLEED LINES AND BLEED VALVES IAW EMB 145 AMM 36-00-00. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050225000622005022500062SO 2005 2 25 CHQA200500028 120050207A3350 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT LOOSE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11267SK 145268 EMERGENCY EXIT LIGHT AT AFT GALLEY IS INOP. FOUND CANNON PLUG UNDER GALLEY CEILING PANEL LOOSE. RESECURED LOOSE CANNON PLUG PER EMB 145 WM 20-50-00. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050225000662005022500066NM 2005 2 25 375PA0032 120050221A5314 KEELBEAM BOEING737 737317 138447PNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05375PA 23812 CORROSION ON THE I/B SIDE OF THE RIGHT KEEL BEAM FORWARD OF BS 540. REPAIRED PER EA 53-028. 2L72 4F RTA16WE 20050225000682005022500068NM 2005 2 25 375PA0034 120050221A5330 PLATE BOEING737 73739A 138447PNM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05375PA 23812 L1 DOOR FORWARD SILL PLATE CRACKED. WELDED PER BAC SPEC 5975. 2L72 4F RTA16WE 20050225000692005022500069EA 2005 2 25 COMA0560127 120050214A3010601R593201 ANTI-ICE SYSTEM CNDAIRCL600 CL6002B19 1900309EA LT WING FAULTY A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01963CA 7127 FLIGHT 5574 RECEIVED A LEFT WING ANTI-ICE WARNING DURING CRUISE FLIGHT, RETURNED TO CVG. REPLACED THE LEFT WING LEADING EDGE INBOARD AND MIDDLE ANTI ICE SENSORS. 2L72 4F RTA21EA 20050225000702005022500070EA 2005 2 25 COMA0560128 120050216A27501104SD100501 DRIVE SHAFT CNDAIRCL600 CL6002B19 1900309EA LT WING WORN A COMAA UNSCHED LANDING O OTHER CRCRUISE 1 SO01819CA 7415 FLIGHT 5808 DURING CRUISE FLIGHT RECEIVED A FLAP FAIL CAUTION, CREW DECLARED AN EMERGENCY AND LANDED AT CVG WITHOUT INCIDENT. REPLACED LEFT WING FLEX DRIVE SHAFT NR 5. 2L72 4F RTA21EA 20050228000022005022800002EU 2005 2 28 RAIA00502029 120050219A3150 SWITCH JETAIRJETSTMJETSTM4101 1500501EU WARNING SYS DIRTY A RAIAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 CE03563HK 41079 RIC - TAKEOFF CONFIGURATION WARNING INDICATION AT 65 KNOTS. MAINTENANCE CLEANED CONDITION LEVER MICRO SWITCH AND OPS CHECKED OKAY. 2L72 4T RTA41NM 20050228000032005022800003SO 2005 2 28 MASA200500141 120050221A573014565200406 SKIN EMB 145 EMB145LR 3260212SO LEADING EDGE ERODED A MASAK NONE O OTHER ININSP/MAINT 1 SW07851MJ7186 145572 IN C-CHECK LEADING EDGE II ON RT WING IS ERODED OUT OF LIMITS. DAMAGE HAS BEEN BLENDED IAW SRM 57-40-00, REMAINING MATERIAL IS ACCEPTABLE IAW EMBRAER ENGINEERING DOCUMENT IC2005-145/0934. 2L72 4T RTT00011AT 20050228000042005022800004SO 2005 2 28 RAIA00502030 120050224A2150 A/C PACK EMB 145 EMB145LR 3260212SO NR 2 INOPERATIVE A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03843HK 14500822 RT PACK DEFERRED WITH LT PACK INOP. MAINTENANCE CLEARED RIGHT-HAND PACK DEFERRAL BY OPS CHECK OKAY NR 2 PACK. 2L72 4T RTT00011AT 20050228000062005022800006NM 2005 2 28 AWXA200500254 120050122A5315654581098 FLOORBEAM BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOORBEAM UPPER CHORD AT BS 312, BETWEEN LBL 9 AND RBL 36, WL 208. MAINTENANCE CUT OUT DAMAGE IN FLOORBEAM UPPER CHORD AT BS 312, FROM LBL 9 TO RBL 36; FABRICATED A NEW REPLACEMENT SECTION OF UPPER CHORD AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-510 FIG 205. 2L72 4F RTA16WE 20050228000092005022800009EU 2005 2 28 AWXA200500257 120050224A3220 LANDING GEAR AIRBUS320 A320231 3930325EU NOSE INOPERATIVE A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28625AW 064 AIR TURNBACK, ON CLIMBOUT OF ORD EN ROUTE TO PHX AFTER SELECTING LANDING GEAR TO THE UP POSITION THE NOSE GEAR WOULD NOT RETRACT, TURNED BACK TO ORD FOR REPAIR. AIRCRAFT CURRENTLY OUT OF SERVICE. MAINTENANCE REPACKED NLG SHOCK STRUT IAW T/C R4N32305, ALSO REPLACED NLG DOWNLOCK SPRING AND LOWER LOCK SPRING ATTACH PIN PER AMM 32-21-18, LEAK AND OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA28NM 20050228000102005022800010SO 2005 2 28 MASA200500117 120050215A532014521718007 PROFILE EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A MASAK NONE O OTHER ININSP/MAINT 1 SW07851MJ7186 145572 IN C-CHECK PROFILE P/N 145-21718-007 IS CORRODED AND IS BEING REPLACED IAW SRM 51-40-02. 2L72 4T RTT00011AT 20050228000112005022800011SO 2005 2 28 MASA200500088 120050201A532014522459003 SUPPORT ANGLE EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A MASAK NONE O OTHER ININSP/MAINT 1 SW07848MJ7375 145530 IN C-CHECK, SUPPORT ANGLE P/N 145-22459-003 IS HEAVILY CORRODED AND HAS BEEN REPLACED WITH NEW PART. 2L72 4T RTT00011AT 20050228000122005022800012SO 2005 2 28 MASA200500089 120050201A532014522460013 GUSSET EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A MASAK NONE O OTHER ININSP/MAINT 1 SW07848MJ7375 145530 IN C-CHECK GUSSET IS CORRODED OUT OF LIMITS AT BL 0 AND WILL BE REMOVED AND REPLACED. 2L72 4T RTT00011AT 20050228000142005022800014SO 2005 2 28 MASA200500091 120050202A5313PE11034K5 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE CHAFED A MASAK NONE O OTHER ININSP/MAINT 1 SW07848MJ7375 145530 IN C-CHECK, STRINGER 19 LT AND 19 RT ARE CHAFED OUT OF LIMITS AND HAVE BEEN REPAIRED IAW SRM 53-24-02. 2L72 4T RTT00011AT 20050228000162005022800016EU 2005 2 28 MALA050150 120050214A53207253711245 PLATE SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15430XJ 340B430 DURING 4Y/2Y CHECK FOUND LT WRAP-AROUND P/N 7253711-245 IS CORRODED AND HAS BEEN REPLACED IAW SRM 51-40-21. 2L72 4T RTA52EU 20050228000182005022800018EA 2005 2 28 MASA200500096 120050209A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSBURNED OUT A MASAO OTHER O OTHER TXTAXI/GRND HDL 1 SW077291Z 7291 PHX-BIL EMERGENCY FLOODLIGHT NR 1 INOP. MAINTENANCE RELAMPED, OPS CHECK GOOD. 2L72 4F RTA21EA 20050228000202005022800020SO 2005 2 28 MASA200500103 120050212A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW72835MJ 145353 ASH - CLT TO CRW HAD 2 FLOOR EMERGENCY EXIT LIGHT STRIPS REPORTED TO BE INOP BY THE CREW. MAINTENANCE FOUND THE LIGHT STRIPS TO BE OPERATING NORMALLY, AND COULD NOT DUPLICATE THE DISCREPANCY. AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. 2L72 4T RTT00011AT 20050228000212005022800021SO 2005 2 28 MASA200500107 120050212A3397 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT LOOSE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07826MJ 145214 ASH - CLT FORWARD OVERHEAD EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE SECURED CONNECTOR TO THE LIGHT ASSEMBLY. NO FURTHER DEFECTS NOTED. 2L72 4T RTT00011AT 20050228000222005022800022EA 2005 2 28 MASA200500109 120050213A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSBURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0717231 7231 A LEFT AFT EMERGENCY FLOOD LIGHT INOP. MAINTENANCE REPLACED THE LAMP. OPS CHECKED GOOD. 2L72 4F RTA21EA 20050228000232005022800023 2005 2 28 COMA0560132 420050216A3410 COMPENSATOR CNDAIRCL600 CL6002B19 1900309EA COCKPIT FAILED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01979CA 7159 FLIGHT 5713 DURING CLIMBOUT OF CVG RECEIVED MULTIPLE EFIS COMP MON MESSAGES AND ALL COMPASSES WERE UNREADABLE. AIRCRAFT RETURNED TO CVG. PERFORMED FULL RECOMPENSATION OF NR 1 AND NR 2 REMOTE COMPENSATING UNITS. 2L72 4F RTA21EA 20050228000242005022800024EU 2005 2 28 RAIA00502016 120050210A3150 WARNING LIGHT JETAIRJETSTMJETSTM4101 1500501EU SPOILERS ILLUMINATED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03563HK 41079 TAKEOFF CONFIG WARNING DURING TAXI. MAINTENANCE DEFERRED GROUND SPOILER SYSTEM PER MEL 3671. REMOVE AND REPLACE LT SPOILER ACTUATOR 2L72 4T RTA41NM 20050228000252005022800025SO 2005 2 28 RAIA00502013 120050209A324021582 BRAKE ASSY EMB 145 EMB145EP 3260221SO LT MLG DRAGGING A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03827HK1017 145021 STL - LEFT O/B BRAKE TEMP IN CAUTION RANGE. MAINTENANCE REMOVED AND REPLACED NR 1 BRAKE. 2L72 4F RTT00011AT 20050228000262005022800026EU 2005 2 28 RAIA00502015 120050210A3240 SWITCH JETAIRJETSTMJETSTM4101 1500501EU PARKING BRAKE FAILED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03572HK 41091 GSO - TAKEOFF CONFIG WARNING ON TAKEOFF. MAINTENANCE ADJUSTED PARKING BRAKE MICRO-SWITCH. 2L72 4T RTA41NM 20050228000272005022800027EU 2005 2 28 RAIA00502017 120050212A28209409124 ACTUATOR JETAIRJETSTMJETSTM4101 1500501EU FUEL SHUTOFF INOPERATIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03558HK7365 3448 41071 PIT - RIGHT FUEL SOV WILL NOT OPEN. MAINTENANCE REMOVED AND REPLACED RT FUEL SOV ACTUATOR. 2L72 4T RTA41NM 20050224000412005022400041 2005 2 24 WRLA2005007 420050206A2565AWD9830507 SLIDE DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE R1 DOOR MALFUNCTIONED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 ITEM: DURING "C4" CHECK IN TPE R1 SLIDE DEPLOY TEST FAILED, THE SLIDE FELL INSIDE THE GALLEY AREA, AND NOT OUTSIDE THE AIRCRAFT AS IT SUPPOSED TO. 2L73 4F4 FRTA22WE E24NE 20050224000492005022400049NM 2005 2 24 WRLA2005004 120050109A3210ARG70765511 CYLINDER DOUG MD11 MD11 3023602NM PWA 4460 PW4460 NE LT MLG WORN A WRLAHJA DEACTIVATE SYST/CIRCUITSDUMP FUEL UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO11801 48472 AT APPROX 1+00 FLIGHT "SYS3ELEV" OFF ALERT ILLUMINATED. HYDRAULIC SYSTEM WAS AT 4.7GAL, DEACTIVATED NR 3 ENGINE PUMPS. HYDRAULIC QTY STABILIZED, DIVERTED TO KATL. REPRESSURIZED FOR LANDING USING RMP, HYD QTY REMAINED STABLE. DECREASED TO 2.8GAL AT LANDING GEAR EXTENSION. AFTER FUEL DUMP, TANK 2 LT AFT PUMP INOP. REMOVED AND REPLACED LT MLG TRUCK BEAM TRIM CYLINDER IAW MM32-37-01-401, BLED SYSTEM PER MM 32-37-01-400-801 AND PERFORMED OPERATIONAL CHECK PER MM 32-37-00-710-801. OPERATION AND LEAK CHECK GOOD. OPERATED ALL FLIGHT CONTROL SURFACES, RUN ENGINES AND OPERATED GEAR UP/DOWN HANDLE. NO ADDITIONAL HYD LEAKS NOTED. TOPPED OFF SYSTEM FLUIDS, OK FOR SERVICE. 2L73 4F4 FRTA22WE E24NE 20050224000742005022400074EA 2005 2 24 05044649 120050213A3397487191 SOCKET CNDAIRCL600 CL6002B19 1900309EA CONNECTOR BROKEN A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27649BR 7414 FLOOR EMERGENCY LIGHT INOP AT ROW 8. FOUND BROKEN WIRE CONNECTOR. 2L72 4F RTA21EA 20050224000832005022400083NM 2005 2 24 SB05001 120050105A335020131A BATTERY PACK BOEING737 737301 1384611NM CABIN DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19591US 23936 PVD - MAINTENANCE REPORTED THE AFT CABIN SEAT MOUNTED EMERGENCY LIGHTS DIM. MAINTENANCE REMOVED AND REPLACED THE AFT BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050224000842005022400084 2005 2 24 DXTA200500582 420050210A2200 AILERON CESSNA750 750 2076810CE LEFT OSCILLATES E DXTAA UNSCHED LANDING I FLT. ATTITUDE INST. CRCRUISE 1 GL07903QS 7500162 DURING FLIGHT AT FL410 WITH AUTOPILOT ENGAGED, AIRCRAFT BEGAN 10 DEGREE LEFT AND RIGHT ROLL OSCILLATION WITH A 1 SEC TIME AMPLITUDE. OSCILLATIONS CONTINUED FOR 18 MINS. OPS ARE NORMAL WITH AP DISENGAGED. DESCENDED TO FL360, RE-ENGAGED AP AND 5 MINS LATER AUTO PILOT ENGAGED AND OSCILLATIONS BEGAN AGAIN WITH CYAN CAS MESSAGE, AILERON RATIO LOW. VISUALLY CONFIRMED AT LEAST LEFT AILERON OSCILLATING. ALL HYD PRESS AND QTY NORMAL. ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20050224000932005022400093NM 2005 2 24 AWXA200500226 120050131A5754 SKIN BOEING737 737301 1384611NM NR 2 SLAT ASSY DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK THE UPPER SURFACE SKIN OF THE NR 2 SLAT WAS FOUND DELAMINATED AT THE OUTBOARD END, SLAT STA 251. MAINTENANCE CUT OUT DAMAGED AREA OF UPPER NR 2 SLAT SKIN FROM SS 249.77 TO SS 254.27; FABRICATED A CORE FILLER AND EXTERNAL DOUBLER; BONDED REPAIR PARTS TO SLAT IAW 51-70-10 FIG 16. 2L72 4F RTA16WE 20050224001092005022400109CE 2005 2 24 DXTA200500589 120050212A3210 LANDING GEAR CESSNA750 750 2076810CE NOISY E DXTAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL07912QS 7500012 DURING GEAR RETRACTION RIGHT AFTER TAKEOFF LOUD THUMPING NOISE WAS HEARD. ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20050224001102005022400110NM 2005 2 24 DXTA200500585 120050211A2612 FIRE DETECTOR AMD FALC50FALCON2000 2730170NM CARGO BAY FALSE ACTIVATIONE DXTAO OTHER N FALSE WARNING DEDESCENT 1 GL07203QS 198 DURING DESCENT (16000 FT) FIRE BELL SOUNDED LT WHEEL WELL OVERHEAT AND BAGGAGE FIRE ILLUMINATED AT SAME TIME. BAGGAGE LIGHT EXTINGUISHED AFTER 5 SECS, WHEEL WELL REMAINED ON. EXECUTED PHASE 1 CHECKLIST. LIGHT EXTINGUISHED ON IT'S OWN AT 200 KTS BEFORE GEAR WAS EXTENDED LANDED UNEVENTFULLY. PERFORMED OPERATIONAL TESTS OF GEAR WELL AND BAGGAGE FIRE WARNING SYSTEMS. NO DEFECTS NOTED. INSPECTED GEAR WELL AND BAGGAGE SENSORS, NO DEFECTS NOTED. INSPECTED GEAR WELL AND BAGGAGE SENSORS. NO DEFECTS NOTED. COULD NOT DUPLICATE DISCREPANCY AT THIS TIME. ALL WORK DONE IAW CH 26-104 AND 26-10-00 OF THE F-2000 MM. 2K73 4F RTA50NM 20050224001122005022400112CE 2005 2 24 DXTA200500592 120050213A3260 WARNING LIGHT CESSNA750 750 2076810CE MLG ILLUMINATED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07975QS 7500175 DURING LANDING GEAR RETRACTION ALL THREE GEAR (GREEN) LIGHT EXTINGUISHED, HOWEVER THE UNLOCK LIGHT REMAINED ON FOR 15-20 SECONDS. AIR NOISE ACCOMPANIED UNLOCK LIGHT. UNABLE TO DETERMINE IF GEAR WAS OUT OF DOORS. ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20050224001342005022400134SO 2005 2 24 RAIA00501028 120050111A7732241244013002 SENSOR EMB 145 EMB145 3260210SO NR 1 ENGINE MALFUNCTIONED A RAIAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 CE03804HK15849 145082 3606- STL- NR 1 ENGINE LP VIBRATION PEGGED ON STOP. MAINTENANCE REMOVED AND REPLACED EMV UNIT. 2L72 4F RTT00011AT 20050224001422005022400142NM 2005 2 24 CALA0500046 120050214A52107057745 SNUBBER BOEING757 757324 1384930NM L-2 DOOR FAULTY A CALAK NONE O OTHER ININSP/MAINT 1 SW27578529947 32811 THE L-2 DOOR WAS DIFFICULT TO OPEN AND CLOSE. THE L-2 DOOR SNUBBER WAS AT FAULT. THE L-2 DOOR ROTARY SNUBBER WAS REMOVED AND REPLACED IAW MM 52-11-10, PAGE 401. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA2NM 20050224001432005022400143NM 2005 2 24 AT0500008 120050207A3520 OXYGEN MASK BOEING737 73776N 13844CHNM CABIN DEPLOYED A ZZDAO OTHER O OTHER CLCLIMB 1 SO15176AT 32654 PAX AND F/A O2 MASKS DROPPED DURING CLIMB. RESTORED O2 MASKS PER AMM 35-22-31. 2L72 4F RTA16WE 20050224001472005022400147EA 2005 2 24 SWIA200514570 120050129A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07440SW 7589 PULLEY INTERCOSTAL ANGLE AT FS 484 LBL 27.0 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ REO 601R-53-41-059 REV A. 2L72 4F RTA21EA 20050224001642005022400164WP 2005 2 24 05FDEA00266 120050208A5330 SKIN DOUG DC10 DC1030 3023501WP FUSELAGE PUNCTURED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25302FE 46801 AMJ PUNCTURED SKIN LT SIDE APPROX 10 FT FWD OF LWR FWD CARGO DOOR. FABRICATED REPAIR FILLER DOUBLERS REF SRM VOL 1 53-20-00 FIG 6 SHEET 11. INSTALLED CLASS 111 REPAIR REF SRM 53-20-00 FIG 6 SHEET 11, TO STAY IN OIL OFF TO 5000 CYCLES. 2L73 4F A22WE 20050224001822005022400182EA 2005 2 24 SWIA200514535 120050210A2750 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS OUT OF RIG A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07413SW 7102 AIRCRAFT REQUIRE'S LEFT RUDDER TRIM 1/2 WAY BETWEEN CENTER AND FIRST HASH MARK AND RIGHT AILERON TRIM 1/2 WAY BETWEEN CENTER AND FIRST HASH MARK. RE-RIGGED ALL FLAP IAW MM 27-53-05 AND RIGGED RIGHT AILERON PCU'S IAW CRJ MM 27-11-00. PERFORMED INFLIGHT FUNCTIONAL CHECK OF TRIM SYSTEM, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050224001882005022400188NM 2005 2 24 SWAA050504 120050220A53306545776 SKIN BOEING737 7373T0 1384582NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29684WN 23941 DURING SCHEDULED A1 CHECK, FOUND 3 EACH FUSELAGE SKIN CRACKS FROM BS 967 TO BS 986, STRINGER 23L. REPAIRED SKIN SECTIONS PER EA. 2L72 4F RTA16WE 20050224001902005022400190NM 2005 2 24 SWAA050455 120050217A575465C26686 WEDGE BOEING737 7373H4 1384600NM NR 4 SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED C4 CHECK, FOUND RT WING NR 4 L/E SLAT WEDGE DELAMINATED. REPAIRED PER MM. 2L72 4F RTA16WE 20050224001912005022400191NM 2005 2 24 SWAA050456 120050216A2761 SEAL BOEING737 737301 1384611NM ACTUATOR BLOWN A SWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW29659SW 23229 DIVERSION, DECLARED EMERGENCY. A-SYSTEM ENGINE LOW PRESSURE LIGHT ILLUMINATED, FOLLOWED BY A-SYSTEM HYDRAULIC FLUID LOSS. REMOVED AND REPLACED RT WING INBOARD FLIGHT SPOILER ACTUATOR O-RING PER MM. 2L72 4F RTA16WE 20050224001932005022400193NM 2005 2 24 SWAA050458 120050217A531169353656 SHEAR TIE BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SPV, FOUND SHEAR TIE AT BS 360, STRINGER 27R, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050224001972005022400197EA 2005 2 24 SWIA200514549 120050214A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07905SW 7437 EMERGENCY LIGHT BY LAVATORY INOPERATIVE. REPLACED EMERGENCY LIGHT BY LAVATORY. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050224002002005022400200CE 2005 2 24 DXTA200500581 120050209A3260 WARNING LIGHT CESSNA500 560CESSNA 2076750CE MLG ILLUMINATED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07367QS 5600367 AFTER TAKEOFF GEAR RETRACTION RED GEAR UNLOCKED LIGHT REMAINED ILLUMINATED AND HYD PRESS ON LIGHT ILLUMINATED. GEAR WAS CYCLED BUT LIGHTS REMAINED ON. WHEN GEAR C/B WAS PULLED PER CHECKLIST RIGHT MAIN GEAR HAD GREEN LIGHT, WHEN C/B WAS RESET GEAR LIGHT. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20050224002122005022400212NM 2005 2 24 SWAA050469 120050217A53156545815 FLOORBEAM BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD AT BS 344, FROM LBL 7 TO RBL 9, CORRODED. REPAIRED CHORD PER SRM. 2L72 4F RTA16WE 20050224002152005022400215NM 2005 2 24 05FDEA00308 120050218A5711 FRAME BOEING727 727200 138407ENM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25496FE 21670 LT WING CORROSION FIXED L/E FRAME WEB LWR T-CHORD AT FSS 236. 2L73 4F RTA3WE 20050224002192005022400219NM 2005 2 24 05FDEA00295 120050215A5330 SKIN DOUG MD11 MD11 3023602NM ZONE 100 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 STA 595 BELOW LONGERON 42 RT SKIN SPLICE FOUND MOUNTED WITH A 01EA DOUBLER & 06 EA NUT PLATES. SKIN PANEL REPLACEMENT WAS COMPLIED WITH. 2L73 4F RTA22WE 20050224002252005022400225NM 2005 2 24 SWAA050471 120050217A57436567172 FITTING BOEING737 7373Q8 1384670NM RT MLG BEAM CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND RT MLG BEAM STABILIZER LINK FITTING, CORRODED. REMOVED AND REPLACED FITTING PER SRM. 2L72 4F RTA16WE 20050224002272005022400227NM 2005 2 24 SWAA050472 120050217A57436959886 FITTING BOEING737 7373Q8 1384670NM RT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND RT MLG STABILIZER LINK FWD ATTACH FITTING, CORRODED. REMOVED AND REPLACED FWD FITTING PER SRM. 2L72 4F RTA16WE 20050224002292005022400229NM 2005 2 24 SWAA050474 120050217A57116545321 SPAR BOEING737 7373Q8 1384670NM LT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND LT WING REAR SPAR AT STATION 285, 12 O'CLOCK POSITION, CRACKED. REMOVED AND REPLACED REAR SPAR SECTION PER ER AND BAC DRAWING. 2L72 4F RTA16WE 20050224002472005022400247NM 2005 2 24 SWAA050445 120050216A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN AT BS 727C + 5, STRINGER 2R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050224002522005022400252NM 2005 2 24 DHL2005741002 120050217A3234 CONTROL HANDLE BOEING727 7272Q9 138448MNM MLG MALFUNCTIONED A DHLAO OTHER F FLT CONT AFFECTED CLCLIMB 1 SO01741DH 21931 AFTER TAKEOFF GEAR HANDLE WOULD NOT GO UP PAST OFF. PERFORMED ABNORMAL CHECKLIST, RAISED GEAR CONTINUED TO CVG WITHOUT FURTHER INCIDENT. PERFORM OPS CHECK OF LANDING GEAR CONTROL HANDLE PER B727 MM 32-31-11, OPS NORMAL. NO DEFECTS NOTED. 2L73 4F RTA3WE 20050224002532005022400253NM 2005 2 24 HNAA0400176 120050105A3230 CONNECTOR DHAV DHC8 DHC8102 2809003NM NLG NOT SEATED A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07912HA 040 AFTER TAKEOFF NOSE GEAR WOULD NOT RETRACT AND LT/RT GEAR DOORS REMAINED OPEN, NOSE GEAR RED TRANSIT LIGHT STAYED ILLUMINATED. LT AND RT MAINS RETRACTED NORMALLY. REROUTED ELECTRICAL HARNESS AND SEATED CONNECTOR OPS CHECK GOOD. 2H72 4T RTA13NM 20050224002632005022400263WP 2005 2 24 ARWA20050204 120050212A2611 SMOKE DETECTOR DOUG DC10 DC1030 3023501WP CARGO BAY MALFUNCTIONED A ARWAF ACTIVATE FIRE EXT. N FALSE WARNING DEDESCENT 1 SO19524MD 46999 DURING DESCENT TIME 02:34 LOWER FORWARD CARGO SMOKE LIGHT COMES ON. PROCEEDED TO ACCOMPLISHED EMERGENCY CHECKLIST. DISCHARGED CYL NR 1. TRANSFERRED TO DMI 18988 IN ACCORDANCE WITH MEL 26-21 CAT-C PLACARD INSTALLED LOWER CARGO COMPARTMENTS MUST REMAIN EMPTY. TRANSFERRED TO DMI 18988 IN ACCORDANCE WITH MEL 26-21. RESERVED FORWARD CARGO COMPARTMENT FAN C/B'S C3 (CIRCUIT BRAKERS) OPERATIONAL CHECK IN ACCORDANCE WITH MM 21-27-06 FOUND NORMAL. THIS CLEARED DMI 18988. REMOVED AND REPLACED NR 1 LOWER CARGO FIRE EXTINGUISHED CONTAINER IN ACCORDANCE WITH MM 26-22-02. TESTED AND FOUND NORMAL IAW MM 26-22-02. 2L73 4F A22WE 20050224002642005022400264NM 2005 2 24 05FDEA00297 120050215A5330 SKIN DOUG MD11 MD11 3023602NM ZONE 100 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 STA 595 BETWEEN LONGERON 45 RT TO 46 RT NOSE JACK FITTING HI-LOK FASTENER HOLES FOUND MOUNTED WITH 06 EA NUT PLATES. SKIN PANEL REPLACEMENT WAS COMPLIED WITH. 2L73 4F RTA22WE 20050224002772005022400277NM 2005 2 24 SWAA050432 120050215A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 DURING SPV, FOUND STRINGER CLIP AT BS 580, STRINGER 11R, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20050224002792005022400279NM 2005 2 24 SWAA050434 120050215A534065C27314 STRINGER CLIP BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 500C, STRINGER 15R, CRACKED. REPAIRED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20050225000032005022500003NM 2005 2 25 DHL2005763002 120050217A2622SY1441 EXTINGUISHER BOEING727 727264 138408MNM CABIN DISCHARGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01763AT 22983 ENTRYWAY FIRE EXTINGISHER GAUGE IN THE RECHARGE ZONE. REMOVED AND REPLACED FIRE EXTINGISHER BOTTLE IAW MM 26-22-00. 2L73 4F A3WE 20050225000092005022500009NM 2005 2 25 SWAA050450 120050216A53106547980 CREASE BEAM BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB FROM BS 927 TO BS 947, LBL 55, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB PER SRM. 2L72 4F RTA16WE 20050225000262005022500026EA 2005 2 25 050406261 120050209A5210 SKIN CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27626BR 7225 PHASE III PAX DOOR CRACKED .75 INCH ON SKIN AT APPROXIMATELY FS 338.9 AND INTERCOSTAL AT DATUM NR 1. 2L72 4F RTA21EA 20050225000322005022500032EA 2005 2 25 QXEA200500205 120050209A5320 COVER CNDAIRCL600 CL6002C10 1390015EA ACM EXHAUST CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 MAINTENANCE FOUND THE RIGHT SIDE AIR CYCLE MACHINE EXHAUST COVER CRACKED. THE EXHAUST COVER AND DUCT WERE REPLACED. 2L72 4F RTA21EA 20050225000372005022500037EA 2005 2 25 COMA0560124 120050211A5610NP1393215 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A COMAA UNSCHED LANDING O OTHER CRCRUISE 1 SO01816CA124443581 7398 FLIGHT 5100 PILOTS WINDSHIELD CRACKED. REPLACED WINDSHIELD. 2L72 4F RTA21EA 20050225000442005022500044CE 2005 2 25 DXTA200500607 120050222A3150 WARNING SYSTEM CESSNA750 750 2076810CE FADEC ACTIVATED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07971QS 7500071 ON TAKEOFF ROLL AT 50 KNOTS, MASTER CAUTION WITH EICAS MESSAGES FADEC FAULT L A-B AND FADEC FAULT R A-B. TAKEOFF WAS ABORTED. MESSAGES EXTINGUISHED AS ACFT CLEARED THE RUNWAY. 2L72 4J RTT00007WI 20050225000452005022500045NM 2005 2 25 375PA0030 120050221A5320 SPLICE BOEING737 737317 138447PNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05375PA 23812 STRINGER 28 LT SPLICE IS CORRODED AT BS 907. REPLACED STRINGER SPLICE PER SRM 51-10-02 AND 51-40-02. 2L72 4F RTA16WE 20050225000472005022500047NM 2005 2 25 373PA0053 120050210A335020131A BATTERY BOEING737 7373Y0 1384671NM EMERGENCY LIGHT INOPERATIVE A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05373PA 23749 EMERGENCY EXIT LIGHT AT R-2 DOOR INOP. REPLACED BATTERY PER MM 33-51-51. 2L72 4F RTA16WE 20050225000502005022500050SO 2005 2 25 CHQA200500034 120050216A3350 LIGHT EMB 135 EMB135KL 3260302SO CABIN INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11378SK 145593 RIGHT OVERWING EMERGENCY EGRESS LIGHT IS INOP. RELAMPED RIGHT OVERWING EMERGENCY EGRESS LIGHT IAW EMB 140 MM 33-50-07. 2L72 4F RTT00011AT 20050225000562005022500056EU 2005 2 25 MALA050155 120050214A5240 DOUBLER SAAB SF340 340B 7860101EU GPU CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15430XJ 340B430 DURING 4Y/2Y CHECK FOUND GPU DOOR SURROUND DOUBLER IS CRACKED AND HAS BEEN REPLACED IAW SRM 51-40-21 (P/N 7253711-175). 2L72 4T RTA52EU 20050225000582005022500058EU 2005 2 25 MALA050151 120050214A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15430XJ 340B430 DURING 4Y/2Y CHECK FOUND SEAT TRACK AT BL 0 FROM FS 297 TO FS 310 IS CORRODED AND HAS BEEN REPAIRED IAW SRM 53-70-60. 2L72 4T RTA52EU 20050225000632005022500063SO 2005 2 25 CHQA200500029 120050209A3350 BULB EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT BURNED OUT A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11841RP 145737 RIGHT FUSELAGE TOP EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED LIGHT BULB IAW 145 AMM 33-50-10. OPS CHECK GOOD. 2L72 4F RTT00011AT 20050225000652005022500065SO 2005 2 25 CHQA200500032 120050214A3350RPS1B BATTERY PACK EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCHARGED A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11292SK 145488 AFT OVERWING LEFT AND RIGHT AISLE FLOOR RUNNER EMERGENCY EXIT LIGHTS ARE INOP. REMOVED AND REPLACED NR 2 AFT EMERGENCY POWER SUPPLY IAW EMB 145 AMM 33-50-00. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050228000052005022800005EU 2005 2 28 RAIA00502031 120050224A2760 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU SPOILERS DIRTY A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03560HK 41076 STL - RIGHT-HAND SPOILER FAIL MESSAGE. MAINTENANCE REPLACED SPOILERS ON DEFERRAL PER MEL. CLEANED SPOILER CONNECTORS AND OPS CHECK OK. 2L72 4T RTA41NM 20050228000072005022800007NM 2005 2 28 AWXA200500255 120050122A53206517688174 SILL BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON L-1 DOOR SILL LOWER INNER CHORD AT LBL 58, BETWEEN BS 298 AND BS 343, WL 208. MAINTENANCE REMOVED DAMAGED SECTION OF L-1 DOOR SILL LOWER INNER CHORD AT LBL 58, FROM BS 298 TO BS 343; FABRICATED A NEW REPLACEMENT SECTION OF INNER CHORD PER DWG 65-17688; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050228000352005022800035NM 2005 2 28 375PA0033 120050221A5720 STIFFENER BOEING737 73739A 138447PNM WING DAMAGED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05375PA 23812 VERTICAL STIFFENER FOR THE FRONT SPAR BULKHEAD AT RBL 6.25 WAS TRIMMED OFF TO ALLOW FOR REPAIR OF KEEL BEAM (SDR 375PA0032). REPAIRED PER EA 57-029. 2L72 4F RTA16WE 20050228000432005022800043EA 2005 2 28 05040626 120050209A5210 LONGERON CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27626BR 7225 PHASE III PAX DOOR CRACKED ON LONGERON AT FS 338.9 AND DATUM NR 1 RUNNING UNDER BOTTOM STEP RISER 1.25 INCH LONG. 2L72 4F RTA21EA 20050228000442005022800044EU 2005 2 28 05FDEA00269 120050209A5313 STRINGER AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25405FE 237 UPON CLEANING FOR CPC ON NRC00393/FEDEX EA 6-5100-84269 FOUND CORROSION ON STRINGERS 53L AND 54L BETWEEN FRAMES 54 TO 54.2. REPAIRED IAW FEDEX EA 6-5315-85997 PART 1. 2L72 4F RTA35EU 20050228000452005022800045NM 2005 2 28 SWAA050435 120050215A53306545768 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN AT BS 360, STRINGER 14L, CRACKED. REPAIRED SKIN PER ER. 2L72 4F RTA16WE 20050228000502005022800050EA 2005 2 28 SWIA200514522 120050207A2750855D10011 SENSOR CNDAIRCL600 CL6002B19 1900309EA BRAKE POSITION MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07455SW 7760 FLAPS FAIL MSG. REMOVED AND REPLACED BOTH LEFT AND RIGHT BPSU'S IAW MM CH 27-51-10. OPERATIONAL CHECK GOOD. P/N 855D100-11, S/N OFF 2019, 1944. 2L72 4F RTA21EA 20050228000522005022800052EA 2005 2 28 SWIA200514524 120050207A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLT SPOILER MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07442SW8421 8421 7609 UPON TAXI OUT ABQ, HAD SPOILERON FAULT STATUS MESSAGE. REMOVED AND REPLACED RT INBOARD SPOILERON PCU WITH A SERVICEABLE UNIT IAW 27-62-01, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050228000552005022800055NM 2005 2 28 DHL2005745001 120050208A3260 ACCESSORY UNIT BOEING727 727224 1384076NM MLG MALFUNCTIONED A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01745DH 20665 DURING CLIMBOUT THE RED GEAR UNSAFE LIGHT ILLUMINATED WHEN THE GEAR HANDLE WAS PLACED IN THE OFF POSITION. THE AMBER -R GEAR DOOR- LIGHT WAS ALSO ILLUMINATED ON THE S/O PANEL. ABNORMAL PROCEDURE COMPLIED. REMOVED & REPLACED LANDING GEAR ACCESSORY UNIT PER 32-09-121. GND CHECKS GOOD. 2L73 4F A3WE 20050228000562005022800056EA 2005 2 28 05043652 120050212A335020131A BATTERY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT WEAK A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27652BR 7429 FWD EMERGENCY LIGHTS INOP. REPLACED NR 1 EMERGENCY BATTERY. 2L72 4F RTA21EA 20050228000592005022800059WP 2005 2 28 ARWA20050108 120050130A3210 LANDING GEAR DOUG DC8 DC863F 302198FWP LACK OF LUBE A ARWAO OTHER J WARNING INDICATION CRCRUISE 1 SO19784AL 46135 GEAR NOT LATCHED LIGHT ILLUMINATED. REMAINED ILLUMINATED AFTER COMPLETING GEAR NOT LATCHED LIGHT ILLUMINATED CHECKLIST. CHECK LANDING GEAR MECHANISM, LUBRICATED SAME, PERFORM GEAR SWING IN ACCORDANCE WITH MM 32-30-0. ALL LIGHTS OPERATED OK IN ACCORDANCE WITH MM 12-80-0 AND DID NOT DUPLICATE FAIL AT THIS TIME. 2L74 4F 4A25 20050228000602005022800060NM 2005 2 28 05FDEA00286 120050214A5347ADA83901 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25591FE 48527 MAIN DECK CARGO SEAT TRACK FOUND CRACKED AT STA 905 LT 28 INCHES. CARRIED OUT REPAIR AS PER SRM 53-70-00 FIG 1 VOL I. 2L73 4F RTA22WE 20050228000612005022800061NE 2005 2 28 05FDEA00287 220050214A7200 ENGINE DOUG MD10 MD1010F 3022112WP GE CF6 CF66K 30020NE NR 1 VIBRATION A FDEAJA DUMP FUEL UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO25399FE 48262 AT FL 340 EXPERIENCED NR 1 ENGINE VIBRATION, N1 ROLLED BACK TO 34%, N2 62% FF 690 LBS. EXECUTED ENG FIRE SEVERE DAMAGE CHECKLIST, FUEL DUMP ABOUT 3000 LBS, DECLARED EMERGENCY LANDING 18C. INSPECTED INTAKE AND EXHAUST. NO DEFECTS NOTED. BOROSCOPE INSPECTED NR 1 ENGINE PER W/C 72X3501, NO DEFECTS NOTED, ENGINE OK FOR SERVICE. AFTER BOROSCOPE FOUND LOOSE B-NUT ON CDP LINE AT COMPRESSOR CASE. PERFORMED BOROSCOPE INSPECTION OF NR 1 ENG PER W/C 72X3501. NO DEFECTS NOTED. HOOKED UP VIBE SENSOR AND TACH WIRE ON NR 1 ENG FOR VIBE RUN. PERFORMED VIBE SURVEY PER MD-10-10 AMM 72-00-00-51, INDICATIONS ARE LESS THAN 1.0 MILS AT 3400, 3200 AND 3000 RPM. ENGINE RAN PER JRH. 2L73 4F4 FRTA22WE E23EA 20050228000642005022800064WP 2005 2 28 05FDEA00264 120050204A5720ARC70082 SILL DOUG DC10 DC1030F 3023504WP ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25316FE 48314 FOUND CRACK IN RIGHT WING ISLAND SILL PART ARC7008-2. 2L73 4F RTA22WE 20050228000652005022800065NM 2005 2 28 05FDEA00265 120050208A5330 SKIN BOEING727 727200 138407ENM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25235FE 21329 WHILE WORKING ROUTINE CARD 7-5330-2342 P1 FOUND GOUGE IN FUSELAGE SKIN CROWN AREA BS 1061 BETWEEN STR 1R & 2R, 35 INCHES FWD OF S-DUCT HOUSING L/E. *S/D* GOUGE FOUND TO BE OUT OF LIMITS, REPAIRED AREA PER SRM 53-30-3. 2L73 4F RTA3WE 20050228000662005022800066GL 2005 2 28 MASA200500019 220050107A72614252070 CARBON SEAL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 1 ENGINE LEAKING A MASAK NONE K FLUID LOSS ININSP/MAINT 1 SW07848MJ7221 145530 CAE311972 DURING 400FH SYSTEM AND POWERPLANT CHECK, 40 CC'S OF OIL WAS FOUND WHEN STARTER DRAIN ADAPTER WAS REMOVED. IAW MESA FORM M867ERJ MAGNETIC CARBON SEAL MUST BE REPLACED WITHIN 50FH. RO EMB 145-72-1050 WAS CREATED, WITH TASK MRO02000 CREATED TO TRACK PERMANENT REPAIR. 2L72 4T4 FRTT00011ATTE6CH 20050228000692005022800069SO 2005 2 28 MASA200500047 120050119A7830 SWITCH EMB 145 EMB145LR 3260212SO THRUST REVERSER OUT OF RIG A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07833MJ 145327 ASH - CLT TO STL ABORTED TAKEOFF AND RETURNED TO THE GATE DUE TO A NR 2 ENGINE THRUST RVERSER DISAGREE. MAINTENANCE COMPLIED WITH THE MEL. MAINTENANCE SHIMMED AND RIGGED SWITCHED, OPS CHECK GOOD. 2L72 4T RTT00011AT 20050228000712005022800071NM 2005 2 28 05FDEA00285 120050214A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 BARREL NUT BORE NR 1R CORROSION REMOVAL FOUND EXCEEDED LIMITS. CORROSION REMOVED AND REPAIRED PER FEDEX EA 1-5510-81726 2L73 4F RTA22WE 20050228000732005022800073SO 2005 2 28 MASA200500050 120050121A2913971808 PUMP EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 1 ENGINE INOPERATIVE A MASAH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CRCRUISE 1 SW07827MJ9352 145217 CAE312089 CLE TO CLT FLIGHT CREW REPORTED A NR 1 HYDRAULIC SYSTEM OVERTEMP CONDITION IN FLIGHT. AS PER CFM, SHUTDOWN HYDRAULIC PUMPS AND WAITED 15 MINUTES FOR OVERTEMP CONDITION TO COOL. ATTEMPTED TO TURN NR 1 HYDRAULICS ON. NEITHER ENGINE DRIVEN NOR ELECTRIC PUMPS WERE PRODUCING PRESSURE. CREW DECLARED AN EMERGENCY AND CONTINUED INTO CLT. WHILE DESCENDING THROUGH 10,000 FT THE CREW REPORTED THAT HYDRAULIC PRESSURE RETURNED AND LANDED WITH NO FURTHER PROBLEMS. MAINTENANCE FOUND THE NR 1 HYDRAULIC PRESSURE FILTER DP INDICATOR POPPED. MX REPLACED PRESSURE FILTER P/N 318298-5 AND NR 1 ENGINE DRIVEN HYDRAULIC PUMP. THE FDR AND CVR REMOVED FOR QUARANTINE. 2L72 4T4 FRTT00011ATTE6CH 20050228000742005022800074EU 2005 2 28 05FDEA00270 120050209A5330 SKIN AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25405FE 237 AFT PIT BETWEEN FR 54.1 & FR 54.2 BILGE CENTER ON SKIN AND STR 55L TO STR 55R CORROSION FOUND UPON CLEANING AREA FOR CPC ON NRC 00393/FEDEX EA 6-5100-84269. REPAIRED IAW FEDEX EA 6-5315-85997 PART 1. 2L72 4F RTA35EU 20050228000752005022800075EA 2005 2 28 COMA0570016 120050215A322267053110471 CYLINDER CNDAIRCL600 CL6002C10 1390015EA NLG CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01369CA5902 10079 NLG OUTER CYLINDER IS CORRODED. CORROSION REPAIRED IAW BOMBARDIER REO 670-32-21-036 AND GOODRICH SCR 0008-04 REV C. 2L72 4F RTA21EA 20050228000762005022800076NM 2005 2 28 SWAA050413 120050213A53306545767 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29506SW 24183 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 482 + 16, STRINGER 10L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050228000772005022800077NM 2005 2 28 SWAA050414 120050213A5315654656812 FLOORBEAM BOEING737 7373K2 13844BANM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29340LV 23738 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM AT BS 1016, RBL 31, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER EA. 2L72 4F RTA16WE 20050228000782005022800078NM 2005 2 28 SWAA050415 120050213A533065C20843 SKIN BOEING737 7373K2 13844BANM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29340LV 23738 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT BS 351, STRINGER 20L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20050228000792005022800079NM 2005 2 28 SWAA050416 120050213A534065C27314 STRINGER CLIP BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29502SW 24179 DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO COMPARTMENT STRINGER CLIP AT BS 807, STRINGER 25L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20050228000822005022800082NM 2005 2 28 SWAA050391 120050210A53116546539 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29603SW 27954 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 616, RBL 63, CRACKED. REPAIRED FRAME SECTION PER EA. 2L72 4F RTA16WE 20050228000832005022800083NM 2005 2 28 SWAA050392 120050210A53116520722 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 DURING SCHEDULED C3 CHECK, FOUND FWD CARGO DOOR CUTOUT FRAME AT BS 440, UPPER SIDE OF LOWER STOP CRACKED. REPAIRED FRAME PER EA. 2L72 4F RTA16WE 20050228000842005022800084NM 2005 2 28 SWAA050393 120050210A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 787, STRINGER 19L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050228000852005022800085 2005 2 28 SWAA050394 420050210A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29364SW 26575 DURING SCHEDULED RON, L1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. RE-INSTALLED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050228000862005022800086EA 2005 2 28 MASA200500065 120050128A3220 PACKING CNDAIRCL600 CL6002B19 1900309EA NLG STRUT LEAKING A MASAO OTHER J WARNING INDICATION CLCLIMB 1 SW0727185 7185 GRR TO PHL HAD A NOSE GEAR DISAGREE AFTER TAKEOFF FROM GRR. THE CREW CYCLED THE GEAR TO CLEAR THE FAULT IN FLIGHT. MAINTENANCE IS CURRENTLY TROUBLESHOOTING FAULT. MAINTENANCE REPACKED THE STRUT. 2L72 4F RTA21EA 20050228000872005022800087SO 2005 2 28 MASA200500074 120050131A5270JE5 SWITCH EMB 145 EMB145LR 3260212SO SERVICE DOOR INOPERATIVE A MASAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 SW07844MJ 145481 CLT HAD A SERVICE DOOR INDICATION INOP. MAINTENANCE PLACED DOOR INDICATION SYSTEM ON MEL. MAINTENANCE REMOVED AND REPLACED SWITCH. OPS GOOD. 2L72 4T RTT00011AT 20050228000882005022800088EU 2005 2 28 AWXA200500230 120050212A2782830A000002 ACTUATOR AIRBUS320 A320231 3930325EU SLAT NR 4 TRIPPED A AWXAO OTHER J WARNING INDICATION LDLANDING 1 WP28634AW48741 091 ON APPROACH, RECEIVED ECAM MESSAGE FOR F/CTL SLATS FAULT; DECLARED PRECAUTIONARY EMERGENCY LANDING AND LANDED WITHOUT FURTHER EVENT. MX TROUBLESHOT SLAT SYS PER TSM 27-81-00-810-810, SLAT SYSTEM OPERATED NORMALLY. INSP OF SLAT ACT FOUND RT OTBD NR 4 SLAT ACT 6087CM TORQUE LIMITER TRIPPED. REPLACED RT OTBD NR 4 SLAT ACT IAW AMM 27-84-49-04, OPS CHK GOOD. FUNCTIONAL TEST OF SLAT ACT CONFIRMED REASON FOR REMOVAL, UNIT FAILED LOW TEMP TEST, FRICTION PLATES WORN OUT OF LIMITS, & A BEARING FOUND BINDING CAUSING EFFICIENCY PROBLEMS. REPLACED FRICTION PLATES & ALL BEARINGS. ACT MODIFIED TO SB 830A-27-01, REPAIRS & TESTING ACCOMPLISHED IAW CMM 27-82-14, REV. 4. 2L72 4F RTA28NM 20050228000892005022800089 2005 2 28 SWAA050395 420050210A2565D31354 SLIDE BOEING737 737301 1384611NM L2 DOOR READS LOW A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED RON, FOUND L2 DOOR EVAC SLIDE LOW PRESSURE IND. REMOVED AND REPLACED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050228000902005022800090NM 2005 2 28 SWAA050396 120050210A57436552235 FITTING BOEING737 7373Q8 1384670NM LT WING CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND LT MLG STABILIZER BEAM FWD LUG, CORRODED. REMOVED AND REPLACED LT MLG FITTING PER MM. 2L72 4F RTA16WE 20050228000912005022800091NM 2005 2 28 SWAA050397 120050210A335065C27093 LIGHT BOEING737 7377H4 1384404NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29425LV 29829 DURING SCHEDULED MV2 CHECK, FOUND AFT GALLEY DOOR OVERHEAD EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20050228000942005022800094 2005 2 28 SWAA050400 420050210A256565C16820 HOOK BOEING737 7375H4 138449DNM GIRT BAR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29502SW 24179 DURING SCHEDULED 1/2D CHECK, FOUND GIRT BAR FLOOR FITTING ASSY AT BS 344, LBL 59, CORRODED. REMOVED AND REPLACED GIRT BAR FITTING ASSY PER SRM. 2L72 4F RTA16WE 20050228000952005022800095NM 2005 2 28 05FDEA00271 120050210A5310 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25235FE 21329 REPAIR SHEAR TIE AT BS 380 BETWEEN STR 15 AND 16 LT TO COMPLY WITH FED EX EO 7-5340-5002 P1. *S/D* REPAIRED PER SRM 51-20-1, 51-20-4, 51-30-2. 2L73 4F RTA3WE 20050228000982005022800098NM 2005 2 28 05FDEA00279 120050211A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 BARREL NUT BORE NR 26L CORROSION REMOVAL FOUND EXCEEDED LIMITS. REMOVED AND REPLACED PER SRM 51-33-01 VOLUME II. 2L73 4F RTA22WE 20050228000992005022800099NM 2005 2 28 05FDEA00280 120050212A57306518552 SKIN PANEL BOEING727 727233 138408ANM FUSLEAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25258FE 20940 OVERWING BOX, TANK TOP, HAS CORROSION AT BODY STATION 840 RIGHT BUTT LINE 12.0. REPAIRED OVERWING BOX FUEL TANK, STATION 840 AT RIGHT BUTT LINE 12.0 IAW FEDEX EA 7-5730-83992, WINGS-UPPER SKIN PANEL, CENTER TANK CORROSION-REPAIR. 2L73 4F RTA3WE 20050228001012005022800101NM 2005 2 28 AWXA200500186 120050209A335020121 CHARGER BOEING737 7373B7 1384580NM FUSLEAGE FAILED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28332AW 23384 DURING OPERATIONAL CHECK OF EMERGENCY LIGHT SYSTEM THE L-2 DOOR EXTERIOR EMERGENCY EXIT LIGHT WAS FOUND TO HAVE VERY WEAK ILLUMINATION. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY CHARGER M1197, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050228001022005022800102NM 2005 2 28 AWXA200500187 120050209A3397BMS13311122 WIRE BOEING737 7373G7 1384595NM SEAT ROW 21 LT BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28158AW 23780 PHX - EEL - DURING 4-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 21 LT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN EMERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 21 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050228001032005022800103NE 2005 2 28 AWXA200500192 220050210A75302607MK2 ACTUATOR AIRBUSA319 A319132 3930340NM IAE V2524 V2524A5 NE NR 1 ENGINE VSV FAILED A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28817AW 1373 ON TAKEOFF ROLL, AT APPROXIMATELY 60 KTS PILOTS RECEIVED ECAM MESSAGE DUAL VSV FAULT. REJECTED TAKEOFF, & RETURNED TO GATE. MX R & R NR 1 ENGINE VARIABLE STATOR VANE (VSV) ACTUATOR IAW T/C R5M75303, PERFORMED AN ENGINE RUN & THE OPS AND LEAK CHK GOOD. CONFIRMED FAILURE OF UNIT, ROOT CAUSE IDENTIFIED AS BLOCKAGE OF SERVO VALVE PORT FILTERS WITH FUEL LACQUER (LEVEL 4). 2L72 4F4 FRTA28NM E40NE 20050228001042005022800104NM 2005 2 28 05FDEA00273 120050210A5530651680310 TIE BOEING727 727200 138407ENM VERTICAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25235FE 21329 CORROSION VERTICAL STAB TENSION TIE LT AFT VERTICAL BOLT HOLE AIRCRAFT AND TENSION TIE. *S/D* REPAIRED PER EA 7-5530-86241. 2L73 4F RTA3WE 20050228001062005022800106NM 2005 2 28 05FDEA00275 120050210A5530651680310 TIE BOEING727 727200 138407ENM VERTICAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25235FE 21329 CORROSION VERTICAL STAB TENSION TIE LT FWD VERTICAL BOLT HOLE AIRCRAFT AND TENSION TIE. *S/D* REPAIRED PER EA 7-5530-86241. 2L73 4F RTA3WE 20050228001082005022800108NM 2005 2 28 05FDEA00278 120050211A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 BARREL NUT BORE NR 15R CORROSION REMOVAL FOUND EXCEEDED LIMITS. CORROSION REMOVED AND REPAIRED PER FEDEX EA 1-5510-81726. 2L73 4F RTA22WE 20050228001092005022800109GL 2005 2 28 05FDEA00312 220050218A7200 ENGINE DOUG MD10 MD1010F 3022112WP GE CF6 CF66D 30020GL NR 2 VIBRATION A FDEAEFJAENGINE SHUTDOWN ACTIVATE FIRE EXT. DUMP FUEL UNSCHED LANDING CETF.O.D. VIBRATION/BUFFET ENGINE CASE PENETRATION CLCLIMB 1 SO25394FE66671 46628 451481 ON TAKEOFF NR 2 THROTTLE REQUIRED ONE KNOB WIDTH BEYOND 1 & 3 ON CLIMBOUT AT 3000 FT AGL RECEIVED AIR MANF 2 FAIL WITH NOTICEABLE AIRFRAME VIBRATION. ENG 2 OIL TEMP HIGH ALERT FOLLOWED WITH PEAK OIL TEMP OF 201 DEGREES C. ENGINE WAS SHUTDOWN AND NR 2 ENGINE FIRE EXTINGUISHER DISCHARGED. INSPECTED INLET AND FOUND BIRD STRIKE DAMAGE. BORESCOPED FOUND SREVICABLE.REPLACED 2EA DAMAGED FAN BLADES, REPAIRED 11 EA BLADES, PERFORMED VIBE SURVEY AND TRIM BALANCE. REPLACED 6 FAN LINER SEGMENTS, REPEAIRED 2 HOLES IN THE COWLING. FOUND BAD OIL TEMP SENSOR,REPLACED. REPLACED RT BELLMOUTH ASSY DO TO DAMAGE AND REPLACED A DAMAGED FUEL LINE SWEDGE, LEAKING FUEL. OK FOR SERVICE. 2L73 4F4 FRTA22WE E23EA 20050228001102005022800110CE 2005 2 28 DXTA200500597 120050218A21708323712 COALESCER BAG RAYTHNDH125 HAWKER800XP 7150012CE CABIN AIR CONTAMINATED E DXTAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 GL07852QS 258452 DURING OCF FOR ENGINE CHANGE, WITH APPLICATION OF MAX CONTINUOUS POWER, DETECTED A VERY STRONG SMELL (ASSOCIATED WITH AN OIL/EXHAUST AND BURNING ODOR). REMOVED AND REPLACED WATER SOCK IAW HAWKER 800XP AMM 21-10-95, OPERATIONAL CHECK GOOD. 2L72 4F RTA3EU 20050228001122005022800112EA 2005 2 28 SWIA200514553 120050208A5210 FITTING CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07590SW 7077 PAX DOOR LOWER CORNER FITTINGS CORRODED; FS 312.00 + FS 346.00. ITEM FOUND AT C-CHECK INSPECTION. REPLACED FITTINGS IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-21-11, 51-25-16 MOD SUM TC601R16637 REV A, TC601R16876 REV "A". 2L72 4F RTA21EA 20050228001152005022800115EA 2005 2 28 SWIA200514556 120050208A5210 FRAME CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07590SW 7077 PAX DOOR INNER DOOR SUB-FRAME IS CRACKED; FS 335.70 UPPER END OF DOOR. ITEM FOUND AT C-CHECK INSPECTION. REPLACED SUB-FRAME IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-21-11, 51-25-16. 2L72 4F RTA21EA 20050228001162005022800116EA 2005 2 28 SWIA200514557 120050208A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07590SW 7077 FUSELAGE PULLEY INTERCOSTAL HAS CRACKED OUTBOARD REMOTE ANGLE FS 484.00 RBL-36.0. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE CRJ SRM 51-40-11, 51-25-06, 51-25-16, 51-42-06, 51-42-21, 51-23-00, 51-21-11. 2L72 4F RTA21EA 20050228001172005022800117EA 2005 2 28 SWIA200514558 120050208A5320 SILL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07590SW 7077 CABIN BELOW FLOOR, CORROSION UNDER FLOOR SILL AT FS 394.0 LBL 48.0. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ SRM 51-21-06, 53-00-00 FIG 102 AND 51-25-06. 2L72 4F RTA21EA 20050228001182005022800118EA 2005 2 28 SWIA200514559 120050208A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07590SW 7077 FUSELAGE FRAME FS 364 STR 8R FLANGE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FRAME IAW CRJ REO 601R-53-21-561. 2L72 4F RTA21EA 20050228001192005022800119EA 2005 2 28 SWIA200514560 120050208A5210 ANGLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR DAMAGED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07590SW 7077 PASSENGER DOOR INTERNAL STRUCTURE ANGLE IS DAMAGED AT DOOR DATUM 6; FS 331.13. ITEM FOUND AT C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-42-06, 51-42-21, 51-23-00 AND 51-25-16. 2L72 4F RTA21EA 20050228001202005022800120EA 2005 2 28 SWIA200514561 120050208A5210 FRAME CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07590SW 7077 PAX DOOR INNER DOOR SUB-FRAME IS CRACKED; 323.30 UPPER END OF DOOR. ITEM FOUND AT C-CHECK INSPECTION. REPLACED SUB-FRAME IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-21-11, 51-25-16. 2L72 4F RTA21EA 20050228001212005022800121EA 2005 2 28 SWIA200514562 120050208A5230 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA CARGO DOOR CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07590SW 7077 CARGO DOOR INTERIOR AFT LOWER CORNER VERTICAL INTERCOSTAL IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED INTERCOSTAL IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, 51-21-11 AND 51-25-16. 2L72 4F RTA21EA 20050228001222005022800122EA 2005 2 28 SWIA200514563 120050209A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07463SW 7820 MAIN FUSELAGE FLOORBEAM AT RBL 9.0 HAS ATTACH ANGLES CRACKED AT FS 280.00. ITEM FOUND AT C-CHECK INSPECTION. ANGLES REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-21-11, 51-25-16, 51-23-00 2L72 4F RTA21EA 20050228001232005022800123EA 2005 2 28 SWIA200514564 120050209A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07463SW 7820 THREE SUPPORT CRACKS FOUND ON FRAME JUST AFT OF ELECTRONICS BAY DOOR, MARKED. ITEM FOUND AT C-CHECK INSPECTION. HFEC INSPECTION ON 3 SUSPECT CRACKS AS REQUESTED ON E & E BAY DOOR FRAME STRUCTURE, NO CRACKS FOUND. NDTM PT1 51-20-06. 2L72 4F RTA21EA 20050228001252005022800125NE 2005 2 28 ARWA20050201 220050202A732171128726 FUEL CONTROL DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7A 52039NE NR 4 ENGINE FAILED A ARWAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SO19906R 46087 671440 ON TAKEOFF, LOSS ENGINE OIL PRESSURE PRIOR TO V-1 ABORTED TAKEOFF; ALSO NOTICED COMPRESSOR STALLED. TROUBLESHOOTING FOUND NR 4 ENGINE FUEL CONTROL UNIT (FCU) LEAKING. REMOVED AND REPLACED FUEL CONTROL UNIT IN ACCORDANCE WITH MM 73-20-1. OPERATIONAL CHECK FOUND NORMAL IN ACCORDANCE WITH MM 71-00. 2L74 4F4 F 4A25 1E8 20050228001282005022800128EU 2005 2 28 DHL2005362002 120050212A3240 RESERVOIR AIRBUS300 A300B4203 3930306EU BRAKE SYS LOW A DHLAO OTHER E VIBRATION/BUFFET TXTAXI/GRND HDL 1 SO01362DH 84 LEFT BRAKE CHATTERS. FOUND BRAKE SYS RESERVOIR LOW. SERVICED RESERVOIR AS PER MM 12-12-32. TAXIED A/C PER JRH 20.1. OPS NORMAL. 2L72 4F RTA35EU 20050228001312005022800131EA 2005 2 28 COMA0570015 120050209A3397 GROUND WIRE CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT DIRTY A COMAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01658CA 10148 FLIGHT 5221 EMERGENCY EXIT SIGN AT ROW 13 IS INOP. CLEANED GROUND WIRE STUD, SYSTEM OPERATION SATISFACTORY. 2L72 4F RTA21EA 20050228001322005022800132NM 2005 2 28 AWXA200500193 120050212A3397BR964411 LIGHT BOEING737 7373Q8 1384670NM SEAT ROW 7 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 PHX - EEL - DURING 4-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 7 LT INOPERATIVE. MAINTENANCE FOUND WIRES PULLED FROM CONNECTOR OF EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 7 LT, REMOVED AND REPLACED LIGHT ASSEMBLY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050228001332005022800133WP 2005 2 28 DXTA200500584 220050210A73008975131 FILTER ELEMENT CESSNA650 650 2076802CE GARRTTTFE731TFE7314R 01518WP NR 1 ENG FUEL CLOGGED E DXTAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS TXTAXI/GRND HDL 1 GL07797QS 6507097 PP102308 AFTER TWO NORMAL ENGINE STARTS AND WHILE THE ENGINES WERE RUNNING, BEFORE TAXI CHECKS THE NUMBER 1 ENGINE FLAMED OUT. CHECKED AND CONFIRMED RIGGING OK, CHECKED FILTER BOWL AND FILTER, NO SIGNS OF WATER OR CONTAMINENTS, NO FAULTS ON DEEC'S, OPS CHECKS OF ENGS GOOD, POSITIVE ACCELERATION AND GOOD SLAM CHECK OF THROTTLE LEVERS. REPLACED NR 1 ENG FUEL FILTER, OP AND LEAK CHECK GOOD. 2L72 4F4 F A9NM E6WE 20050228001342005022800134NE 2005 2 28 DXTA200500587 220050211A7300 QUICK DISCONNECT BRAERO1000 HAWKER1000 7450005EU PWA 305 PW305B 52128NE NR 1 ENGINE CONTAMINATED E DXTAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 GL07549QS 259049 PCE305056 ON A ROLLING TAKEOFF NR 1 ENGINE DID NOT SPOOL UP TO FULL POWER I FIRST NOTICED A SPLIT IN N2 RPM THEN SAW N1 RPM ON NR 1 ENGINE WAS ABOUT 5 PERCENT BELOW TAKEOFF POWER. RAN FADEC CODES AND IT IS SHOWING KB ON CHANNEL B ON ALL LINES. TROUBLESHOT SQUAWK FOUND MOISTURE IN CONNECTOR, P4 ON EEC NR 1 AND MOISTURE IN CONNECTOR J22. CLEANED AND DRIED CONNECTORS AND COVERED CONNECTORS WITH F4 TAPE. FOLLOWED TROUBLESHOOTING TABLE FOC FAULT CODE KB. WORK DONE IAW P&W FAULT ISOLATION HANDBOOK 30B1409 AND P&WC MM 76-10-00. 2L72 4F4 FRTA3EU E35NE 20050228001362005022800136CE 2005 2 28 DXTA200500591 120050213A2910 LINE CESSNA560 560XL 2076702CE HYDRAULIC SYS LEAKING E DXTAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07639QS 5605139 BRAKES ARE SPONGY, LEFT SIDE IS WORSE THAN THE RIGHT SIDE. LEFT BRAKE ALMOST GOES TO HTE FLOOR FOR ANY REACTION. FOUND AIR IN BRAKE SYSTEM, BLED BRAKE SYSTEM IAW 560XL MM 32-42-00, TAXI CHECK GOOD. 2L72 4F RTA22CE 20050228001382005022800138NE 2005 2 28 AT0500009 220050213A7200 ENGINE BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE LEFT INOPERATIVE A ZZDAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 SO15930AT 55072 13181 ON CLIMBOUT ENGINE LEFT SURGE ALERT CAME ON. ALL ENGINE PARAMETERS NORMAL. AT ABOUT 13,000 LEFT ENGINE FAILED, SEVERE DAMAGE SUSPECTED. REPLACED ENGINE. 2L72 4F4 FTRA6WE E00061EN 20050228001392005022800139NM 2005 2 28 DHL2005763001 120050215A2612 FIRE DETECTOR BOEING727 727264 138408MNM CARGO BAY FALSE INDICATIONA DHLAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 SO01763AT 22983 FWD CARGO FIRE LIGHT ILLUMINATED. PERFORMED INSP OF THE FWD CARGO BAY & SMOKE DETECTION SYS PER M/M 26-16-00, NO DEFECTS NOTED. 2L73 4F A3WE 20050228001432005022800143EA 2005 2 28 SWIA200514540 120050209A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLIGHT SPOILER MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CRCRUISE 1 NM07953SW 7813 SPOILERONS FAULT STATUS MESSAGE IN FLIGHT. REMOVED AND REPLACED RIGHT INBOARD SPOILERON PCU IAW CRJ MM 27-62-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050228001452005022800145EA 2005 2 28 SWIA200514542 120050205A5240 ROD END CNDAIRCL600 CL6002B19 1900309EA SERVICE DOOR OUT OF ADJUST A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07920SW 7660 SERVICE DOOR REQUIRES EXCESSIVE FORCE TO OPEN. REPLACED ROD ENDS AND ADJUSTED SERVICE DOOR UPPER ATTACHMENT ARM AND CLEANED DOOR SEAL. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050228001472005022800147EA 2005 2 28 VNAA0502011 120050211A3150 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE GROUND SPOILERS FALSE INDICATIONA VNAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL05242JS 7911 AT THE START OF TAKEOFF ROLL AT DCA THE CREW REPORTED A TAKEOFF CONFIG WARNING AND THE GND SPLR DEPLOY CAUTION MESSAGE ILLUMINATED. THE CREW OF FLIGHT 2428 ABORTED THE TAKEOFF AND RETURNED TO THE GATE. CONTRACT MAINTENANCE PERFORMED TAKEOFF CONFIG OPERATIONAL CHECKS IAW CRJ 200 FIM 22-12-00. NO DEFECTS WERE NOTED. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050228001492005022800149NM 2005 2 28 05FDEA00236 120050203A5347ACA7399501 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 MAIN DECK - SEAT TRACK CROWN AREA AT APPROXIMATE STA Y= 715, X= 47.5 FOUND WORN. MAIN DECK - SEAT TRACK CROWN AREA AT APPROXIMATE STA Y= 715, X= 47.5 REPAIR PARTS FABRICATED AND INSTALLED AS PER SRM 53-70-00 VOLUME I, FIGURE 1. 2L73 4F RTA22WE 20050228001522005022800152EU 2005 2 28 05FDEA00224 120050202A2750A57960010201 PLATE AIRBUS300 A300B4622 3930401EU ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25716FD 358 RIGHT WING T/E INBOARD FLAP UPPER SURFACE INBOARD END FLAP TRACK ROLLER CHAFING PLATE IS CRACKED. REMOVED AND REPLACED CHAFING PLATE IAW DWG A579-60005. 2L72 4F RTA35EU 20050228001532005022800153NE 2005 2 28 DL73S050091 220050208A7200 ENGINE BOEING737 737232 1384475NM PWA JT8 JT8D15A 52051NE NR 1 MALFUNCTIONED A DALAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 SO27319DL49579 700308 23091 700308 FLT 7000 FT CLIMB EPR 250 - CLIMBING CLEAN HEARD LOUD BOOM WITH A/C SHUDDER ONCE. ALL ENG IND NORM AND STEADY. PNEU NORM. NO VISIBLE DAMAGE FROM CABIN F/A'S. ATB CVG UNEVENTFUL. DECLARED EMERGENCY WITH CVG DEPT CONTROL. BORO BOTH ENGINES, OK. FOUND LEFT ENGINE ANTI-ICE VLV LIGHT FLICKERING AT POWER. REPLACED ANTI-ICE VLV, OPS CHECKS OK. 2L72 4F4 FRTA16WE E2EA 20050228001552005022800155NM 2005 2 28 DLM88050093 120050208A3810 WATER HEATER DOUG MD88 MD88 3023688NM AFT LEFT LAV OVERHEATED A DALAD RETURN TO BLOCK MB OVER TEMP SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27922DL 49646 AFT LEFT LAV HAD SMOKE / ELECT BURNING SMELL EMITTING FROM IT. REPLACED OVERHEATED WATER HEATER AND CONNECTOR. 2L72 4F RTA6WE 20050228001562005022800156NM 2005 2 28 DLM90050094 120050208A4940 STARTER DOUG MD90 MD9030 3023690NM APU INOPERATIVE A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27909DA 53389 APU WOULD NOT START. REPLACED APU STARTER AND START CONTROL RELAY. REPLACED WIRE AT B1-1058 PIN 5A. 2L72 4F RTA6WE 20050228001572005022800157WP 2005 2 28 05FDEA00254 120050205A5720ARC0549 HANGER ASSY DOUG DC10 DC1030F 3023504WP ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25304FE 46992 RIGHT WING LOWER AFT BEAM SUPPORT FITTING PN ARC0459-2 REQUIRES FABRICATION. FABRICATED FITTING ARC0459-2 IAW DAC DWG ARC0459-2 AND FEDEX EA 8-5732-83971, WINGS- RIGHT HAND WING, LOWER AFT BEAM, SUPPORT HANGER. 2L73 4F RTA22WE 20050228001582005022800158WP 2005 2 28 05FDEA00255 120050205A5311AEA7165 FRAME DOUG DC10 DC1030F 3023504WP ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25304FE 46992 FRAME AND INTERCOSTAL CORRODED AT STATION 1461 RIGHT WHEEL WELL INTERIOR AREA. COMPLIED WITH FEDEX EA 8-5310-83975, FUSELAGE- CORROSION DAMAGE TO LT STATION 1505, LONGERON 35 FRAME- REPAIR, AND FEDEX EA 8-5310-83974, AFT WHEEL WELL- PRESSURE BULKHEAD TEE FRAME REPAIR. 2L73 4F RTA22WE 20050228001592005022800159EU 2005 2 28 05FDEA00244 120050203A5270 SWITCH AIRBUS300 A300B4622 3930401EU CARGO DOOR OUT OF ADJUST A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25716FD 358 AFTER TAKEOFF MAIN DECK CARGO DOOR OPEN CAME ON. CABIN ALT WAS CLIMBING ALSO. DEFERRED PER MEL 52-71-01. RELEASED FOR SERVICE PER MEL/CDL: 52-71-01 CATEGORY: C. MAIN DOOR CLOSED & LOCKED INDICATION ON ECAM DOOR PAGE - INOP. MAIN PERFORMED OPERATIONAL ADJUSTMENT, AND TEST PROCEDURES IAW A300-600 AMM 52-71-00-5, FOUND SWITCH 49WS OUT OF RIG, ADJUSTED, AND VERIFIED SWITCH ADJUSTMENT IAW A300-600 AMM 52-71-11-5 SUPP AMM 52-71-11-5, DOOR INDICATION OPERATIONAL CHECKS NORMAL. 2L72 4F RTA35EU 20050228001632005022800163NM 2005 2 28 375PA00355 120050221A361032895625 VALVE BOEING737 737317 138447PNM RT ENG PRECOOLERFAILED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05375PA 23812 RIGHT ENGINE PRECOOLER VALVE CRACKED. REPLACED PRECOOLER VALVE PER MM 63-12-35. 2L72 4F RTA16WE 20050228001642005022800164NM 2005 2 28 375PA0036 120050221A5245 PANEL BOEING737 73739A 138447PNM LT RAM AIR GOUGED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05375PA 23812 LEFT RAM AIR CLOSE OUT PANEL GOUGED. REPAIRED PER SRM 51-70-13. 2L72 4F RTA16WE 20050228001652005022800165EA 2005 2 28 COMA0570021 120050222A2730FE304000000AMD LIMITER CNDAIRCL600 CL6002C10 1390015EA VERTICAL STAB MALFUNCTIONED A COMAO OTHER F FLT CONT AFFECTED CRCRUISE 1 SO01379CA5107 10102 DURING TEST FLIGHT WITH AUTOPILOT ENGAGED, AIRCRAFT EXPERIENCES PITCH OSCILLATIONS BETWEEN +/-20 TO 800 FPM VSI. PITCH DISCONNECT HANDLE PULLED IN FLIGHT AND REVEALED LAG IN LEFT SIDE PITCH CONTROL SYSTEM. PERFORMED FLIGHT CONTROL PATH INSPECTION AND FOUND THE LEFT ELEVATOR LOAD LIMITER BAD (CONNECTING ROD SEPARATED FROM SPRING HOUSING). REPLACED FAILED LOAD LIMITER WITH SERVICEABLE PART. 2L72 4F RTA21EA 20050228001672005022800167NM 2005 2 28 SWAA050521 120050222A3350101114 LAMP BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29325SW 23689 DURING SCHEDULED C3 CHECK, FOUND L1 & R1 DOOR EMERGENCY EXIT SIGNS INOP. RELAMPED L1 & R1 EXIT SIGNS PER MM. 2L72 4F RTA16WE 20050228001682005022800168NM 2005 2 28 SWAA050522 120050222A3350D71702001 BATTERY BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29650SW 27720 DURING SCHEDULED A2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050228001692005022800169NM 2005 2 28 SWAA050523 120050222A53116546539 FRAME BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29507SW 24184 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED FRAME AT LT FWD LOWER CORNER EMERGENCY EXIT AT BS 616. REPAIRED FRAME PER TYPICAL REPAIR MANUAL. 2L72 4F RTA16WE 20050228001712005022800171NM 2005 2 28 SWAA050525 120050222A53106935371 SHEAR WEB BOEING737 7375H4 138449DNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29507SW 24184 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT SHEAR WEB, BS 956, RBL 21. REMOVED AND REPLACED SHEAR WEB ANGLE PER SRM. 2L72 4F RTA16WE 20050224002082005022400208 2005 2 24 SWAA050464 420050217A25656557463 FITTING BOEING737 7373Q8 1384670NM GIRT BAR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND GIRT BAR FITTING AT BS 344, LBL 59, CORRODED. REMOVED AND REPLACED GIRT BAR FITTING PER SRM. 2L72 4F RTA16WE 20050224002102005022400210NM 2005 2 24 SWAA050467 120050217A53156546811 FLOORBEAM BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD AT BS 986.5, FROM LBL 50 TO RBL 50, CORRODED. REPAIRED FLOORBEAM CHORD PER ER. 2L72 4F RTA16WE 20050224002312005022400231NM 2005 2 24 SWAA050476 120050131A3350101114 LAMP BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29746SW 29798 DURING SPV, FOUND R1 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM. 2L72 4F RTA16WE 20050224002682005022400268NM 2005 2 24 SWAA050425 120050214A53306550570 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT R2 DOOR CUTOUT FWD LOWER CORNER, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20050224002782005022400278NM 2005 2 24 SWAA050433 120050215A2560PH22300L GLOWSTRIP BOEING737 737317 138447PNM CABIN DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29661SW 23173 DURING SCHEDULED A1 CHECK, FOUND 2 EACH SECTIONS OF EMERGENCY EXIT PHOTOLUMINESCENT STRIPS IN FWD CABIN, DELAMINATED. REMOVED AND REPLACED PHOTOLUMINESCENT STRIPS PER MM. 2L72 4F RTA16WE 20050224002842005022400284WP 2005 2 24 AALA20050099 120050207A3222 SCHRADER VALVE DOUG DC9 DC982 3022082WP NLG DEFECTIVE A AALAA UNSCHED LANDING O OTHER CLCLIMB 1 SW21583AA 53160 DFW INFLIGHT T1181/07 - UNABLE TO RETRACT NOSE GEAR AFTER TAKEOFF. RAN CHECKLIST. NO DAMAGE TO NOSE GEAR AREA. FOUND NOSE STRUT FLAT. REPLACED SCHRADER VALVE AND SERVICED NOSE GEAR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050224002862005022400286WP 2005 2 24 AALA20050101 120050208A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21428AA 49340 SFO - CEILING EMERGENCY LIGHTS BETWEEN ROWS 27 TO 30 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS BETWEEN ROWS 27 TO 30. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050224002962005022400296WP 2005 2 24 AALA20050109 120050213A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW219402W 53138 DFW - EMERGENCY LIGHT BATTERY PACK ASSEMBLIES AT B523, B5104 AND L2694 INOPERATIVE. REPLACED BATTERY PACK FOR B523, B5104 AND L2694 FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050224002982005022400298NM 2005 2 24 AALA20050105 120050212A3397 WIRE BOEING777 777223 1385213NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW21794AN 30256 MIA - EMERGENCY LIGHT IN FIRST CLASS AT COAT CLOSET FLOOR INOPERATIVE. REPAIRED BROKEN WIRE AND REPLACED SOCKET FOR EMERGENCY LIGHT IN FIRST CLASS AT COAT CLOSET FLOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20050224003002005022400300NE 2005 2 24 AALA20050111 220050130A7200 ENGINE BOEING767 767323 1385205NM GE CF6 CF680C2B6F 30025NE LEFT MALFUNCTIONED A AALAA UNSCHED LANDING REJPARTIAL RPM/PWR LOSS VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 SW21371AA 25198 690267 MAN - CLIMBING AT FL280 LEFT ENGINE EXPERIENCED TWO COMPRESSOR STALLS. INDICATION ACCOMPANIED WITH HIGH VIBRATION. N2 VIBRATIONS WERE FIVE UNITS. ENGINE POWER WAS REDUCED TO IDLE FOR DESCENT AND LANDING. EVENT RECORD SWITCH PRESSED AT IDLE POWER. LATER ON DECENT EICAS MESSAGE CAME ON LEFT WING ANTI-ICE. REPLACED LEFT ENGINE PER WORK CARD 71 93 01. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA1NM E13NE 20050225000022005022500002NM 2005 2 25 DHL2005751500 120050213A5730 SKIN BOEING727 727264 138408MNM LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01751DH 22982 LEFT WING L/E STA 644.5 HAS CORROSION. CUT OUT CORROSION DAMAGE IN LT WING L/E AT STA 644.5. FABRICATED -1 FILLER USING .040 2024T3 PO 0442771, -2 DOUBLER USING .050 2024T3 PO 0440785. DRILLED DEBURRED, ALODINED, PRIMED AND INSTALLED DOUBLER & FILLER IAW B727 SRM 57-30-4, 51-10-2, 51-30-2. 2L73 4F A3WE 20050225000062005022500006NM 2005 2 25 QXEA200500207 120050208A5230 FITTING BOMBDRDHC8 DHC8401 1390041NM CARGO DOOR CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09412QX 4059 THE AFT BAGGAGE DOOR AFT LOWER FITTING IS CRACKED AT THE LOWER RIB. THE ROLLER GUIDE BRACKET CRACK WAS STOP DRILLED, ALODINED AND PRIMED. 2H72 4T RTA13NM 20050225000132005022500013NM 2005 2 25 05FDEA00310 120050219A5311AFA00333 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25591FE 48527 MAIN DECK LT SIDEWALL STRUCTURE FRAME STA 1761 FOUND WITH DENT ON INNER CHORD AT L-12. CARRIED OUT REPAIR AS PER SRM 53-30-00 FIG 1 VOL I. 2L73 4F RTA22WE 20050225000162005022500016NM 2005 2 25 AWXA200500234 120050220A33503114981 REFLECTOR BOEING737 7373G7 1384595NM EMERGENCY LIGHT CORRODED A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28305AW 24012 PHX - EEL - DURING INSPECTION FOUND THE L-2 DOOR EXTERNAL EMERGENCY ESCAPE LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED L-2 DOOR EXTERNAL EMERGENCY ESCAPE LIGHT REFLECTOR ASSEMBLY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050225000342005022500034NM 2005 2 25 DHL2005746003 120050218A3350 LIGHT BOEING727 727224 1384076NM CABIN MALFUNCTIONED A DHLAO OTHER O OTHER LDLANDING 1 SO01746DH 22252 ON TOUCHDOWN EMERGENCY EXIT LIGHTS CAME ON. RE-INSTALLED CABIN EMERGENCY EXIT LIGHT PER MM 33-50-101, OPS CHECK GOOD. 2L73 4F A3WE 20050225000352005022500035NM 2005 2 25 SWAA050443 120050216A323065C268781 VALVE BOEING737 7375H4 138449DNM MLG FAULTY A SWAAO OTHER O OTHER NRNOT REPORTED 1 SW29512SW 24189 LANDING GEAR HANDLE WOULD NOT RETRACT. REMOVED AND REPLACED RT MLG SNUBBING VALVE PER MM. 2L72 4F RTA16WE 20050225000532005022500053EA 2005 2 25 COMA0560129 120050216A27801104SD100301 DRIVE SHAFT CNDAIRCL600 CL6002B19 1900309EA LT WING TE FLAPSWORN A COMAA UNSCHED LANDING O OTHER CRCRUISE 1 SO01819CA 7415 FLIGHT 5808 DURING CRUISE FLIGHT RECEIVED A FLAP FAIL CAUTION, CREW DECLARED AN EMERGENCY AND LANDED AT CVG WITHOUT INCIDENT. REPLACED LEFT WING FLEX DRIVE SHAFT NR 3. 2L72 4F RTA21EA 20050225000642005022500064SO 2005 2 25 CHQA200500030 120050212A3350 LIGHT EMB 135 EMB135LR 3260305SO CABIN INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11844RP 145620 AFT EMERGENCY EXIT LIGHTS ARE INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHTS 1, 2, 3 AND 4 IAW EMB 135 AMM 33-50-04. OPS CHECK GOOD. 2L72 4F RTT00011AT 20050228001782005022800178NM 2005 2 28 DL73S050097 120050208A531165528752 FRAME BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27330DL 23102 A FASTENER HOLE COMMON TO THE OUTER CHORD OF THE AFT FRAME OF THE L2 DOOR CUTOUT (FS 992, BETWEEN STRINGERS 7L & 8L) WAS FOUND CRACKED. THE HOLE WAS OVERSIZED AND AN INSURANCE CUT MADE TO REMOVE THE CRACK. THE OVERSIZED HOLE WAS REPAIRED WITH AN ALUMINUM BUSHING AND AN ALUMINUM REPAIR STRAP PER ER/A 096806-14. 2L72 4F RTA16WE 20050228001792005022800179NM 2005 2 28 DL764050098 120050209A25301105011 COFFEEMAKER BOEING767 767432ER 1385134NM MID GALLEY ARCED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27845MH 29719 NR 2 MID GALLEY COFFEEMAKER INOP. C/B POPPED AFTER ARCING OCCURRED. REPLACED SAME. 2L72 4F RTA1NM 20050228001822005022800182NM 2005 2 28 DL757050101 120050208A5415012N88884 FITTING BOEING757 757232 1384965NM NR 2 PYLON DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27622DL 22912 FITTING REWORK REQUIRED FOR NR 2 AND NR 5 HOLES ON THE RIGHT WING SUPPORT FITTING. REPAIRED IAW ERA 389530-14AD. 2L72 4F RTA2NM 20050228001832005022800183NM 2005 2 28 SWAA050436 120050215A57436552235 FITTING BOEING737 7373Q8 1384670NM LT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND LT MLG AFT SPAR SUPPORT BEAM STABILIZER FITTING LUG FACES, CORRODED. REMOVED AND REPLACED SUPPORT FITTING PER BAC DRAWING AND SRM. 2L72 4F RTA16WE 20050228001862005022800186NM 2005 2 28 375PA0040 120050221A5315 FLOORBEAM BOEING737 73739A 138447PNM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05375PA 23812 AFT CARGO FLOOR PANEL SUPPORT ANGLE CRACKED AT NUT PLATE AT BS 727D +7 AT LBL 7. REPAIRED PER SRM 53-00-53. 2L72 4F RTA16WE 20050228001872005022800187NM 2005 2 28 375PA0041 120050221A5320 FLOOR SUPPORT BOEING737 737317 138447PNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05375PA 23812 AFT CARGO FLOOR PANEL SUPPORT ANGLE HAS CORROSION AT BS 727D +7 AT RBL 7. REPAIRED PER SRM 53-00-53. 2L72 4F RTA16WE 20050228001882005022800188NM 2005 2 28 375PA0042 120050221A5320 FLOOR SUPPORT BOEING737 737317 138447PNM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05375PA 23812 AFT CARGO FLOOR PANEL SUPPORT ANGLE CRACKED AT NUT PLATE AT BS 727D + 7 AT RBL 3. REPAIRED PER SRM 53-00-53. 2L72 4F RTA16WE 20050228001922005022800192WP 2005 2 28 AALA20050123 120050217A3397 WIRE DOUG DC9 DC982 3022082WP BATTERY PACK INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21216AA 49167 ORD - CEILING MOUNTED EMERGENCY LIGHTS AT SEAT ROWS 23 TO 26 INOPERATIVE. SECURED LOOSE WIRE ON OVERHEAD EMERGENCY LIGHTS BATTERY PACK FOR SEAT ROWS 23 TO 26. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050228001932005022800193NM 2005 2 28 AALA20050131 120050220A3350 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21192AN 32386 DFW - AFT OVERWING EMERGENCY LIGHT AT RIGHT WING INOPERATIVE. REPLACED BATTERY PACK ASSEMBLY FOR AFT OVERWING EMERGENCY LIGHT AT RIGHT WING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050228001942005022800194NM 2005 2 28 05FDEA00068 120050111A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25235FE 21329 BS 720D PLUS 18, STR 23R STRINGER CORROSION. REMOVED & FABRICATED NEW STRINGER AND 2 HAT CHANNELS SRM 53-10-2, 51-30-2. 2L73 4F RTA3WE 20050228002022005022800202NM 2005 2 28 SWAA050491 120050218A53306545766 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 500D, STRINGER 4R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20050228002032005022800203NM 2005 2 28 SWAA050492 120050219A5753 SKIN BOEING737 7373H4 1384600NM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW BN1282 28035 DURING SCHEDULED SERVICE CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED LT WING FLAP PER MM. 2L72 4F RTA16WE 20050228002052005022800205NM 2005 2 28 SWAA050494 120050219A2560P4010021 BATTERY BOEING737 7377H4 1384404NM FLASHLIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29774SW 27882 DURING SCHEDULED RON, FOUND FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2L72 4F RTA16WE 20050228002082005022800208SO 2005 2 28 MASA200500113 120050214A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07826MJ 145214 CLT TO PHF AFT OVERHEAD EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE. MAINTENANCE REPLACED THE LIGHT. NO FURTHER DEFECTS NOTED. 2L72 4T RTT00011AT 20050228002092005022800209SO 2005 2 28 MASA200500114 120050214A3350 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT LOOSE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07828MJ 145218 CLT TO BNA FWD CABIN FLOOR EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE. MAINTENANCE SECURED ELECTRICAL CONNECTOR TO LIGHTING STRIP. NO FURTHER DEFECTS NOTED. 2L72 4T RTT00011AT 20050228002122005022800212EA 2005 2 28 05049677 120050218A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A VTZAL ABORTED APPROACH O OTHER APAPPROACH 1 EA27677BR 7652 FLAP FAIL AT 0 DEGREES ON APPROACH. NORMAL NO FLAP LANDING. MX RESET FLAP SYSTEM. 2L72 4F RTA21EA 20050228002132005022800213NM 2005 2 28 375PA0028 120050221A5315 FLOORBEAM BOEING737 73739A 138447PNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05375PA 23812 CORROSION ON FLOORBEAM T-CAP AT BS 344 FROM LBL 19 TO LBL 30. REPAIRED PER SRM 53-10-51. 2L72 4F RTA16WE 20050228002142005022800214NM 2005 2 28 375PA0029 120050221A5315 FLOORBEAM BOEING737 73739A 138447PNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05375PA 23812 CORROSION ON FLOORBEAM T-CAP AT BS 312 AT LBL 19. REPAIRED PER SRM 53-10-51. 2L72 4F RTA16WE 20050228002152005022800215EA 2005 2 28 COMA0560133 120050218A2750860D10018ABCD CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION DEDESCENT 1 SO01976CA7901 3344 7151 FLIGHT 5142 FLAPS FAIL MESSAGE. REPLACED THE FECU. 2L72 4F RTA21EA 20050228002172005022800217EA 2005 2 28 COMA0560138 120050220A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01966CA 7132 FLIGHT 5250 FLAPS FAIL CAUTION. COULD NOT DUPLICATE. INSPECTED FLAPS PER AD 98-20-01. NO DEFECTS FOUND. 2L72 4F RTA21EA 20050228002232005022800223EU 2005 2 28 CHQA200500039 120050221A2752C1548112 ACTUATOR EMB ERJ170ERJ170100LR EU TE FLAPS UNSERVICEABLE A CHQAO OTHER J WARNING INDICATION DEDESCENT 1 GL11635RW579 579 17000056 FLIGHT 7723 IAD-MSY - AFTER SELECTING FLAPS DOWN A FLAP FAIL MESSAGE APPEARED ON EICAS AND THE FLAPS WOULD NOT MOVE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED UNEVENTFULLY. THE AIRCRAFT WAS FERRIED TO IND FOR MAINTENANCE. MAINTENANCE TROUBLESHOT THE AIRCRAFT AND REMOVED AND REPLACED THE LEFT HAND OUTBOARD FLAP ACTUATOR. OPS CHECK GOOD. 2L74 4F RTA56NM 20050228002262005022800226EA 2005 2 28 SWIA200514565 120050209A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07463SW 7820 FLOOR SUPPORT ANGLE CRACKED AT FS 621.00 RBL 41.0. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FLOOR SUPPORT IAW CRJ REO 601R-53-61-117. 2L72 4F RTA21EA 20050228002292005022800229NM 2005 2 28 SWAA050531 120050222A53116546550 FRAME BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 887, STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050228002302005022800230NM 2005 2 28 SWAA050532 120050222A53116546550 FRAME BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 907, STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050228002362005022800236NM 2005 2 28 SWAA050535 120050222A534065C27314 STRINGER CLIP BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP AT BS 767, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20050228002372005022800237NM 2005 2 28 SWAA050536 120050222A534065C27314 STRINGER CLIP BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND 2 EA CRACKED STRINGER CLIPS AT BS 727E, BETWEEN STR 5L AND 7L. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20050228002382005022800238NM 2005 2 28 SWAA050537 120050222A534065C27314 STRINGER CLIP BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND 3 EA CRACKED STRINGER CLIPS AT BS 727D, BETWEEN STR 4L AND 6L. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20050228002392005022800239NM 2005 2 28 05FDEA00071 120050111A5313 STRINGER BOEING727 727200 138407ENM N/A CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25235FE 21329 BS 720E PLUS 12 - BS, STR 23R CORROSION. CORROSION 100 PERCENT IN MATERIAL REMOVED AND REPLACED STRINGER PER SRM 53-10-2 AND 51-10-2. 2L73 4F RTA3WE 20050228002412005022800241NM 2005 2 28 05FDEA00192 120050128A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25235FE 21329 BS 680, LBL 35, WL 162, DENT ON FRAME. REPAIRED PER SRM 51-40-3. 2L73 4F RTA3WE 20050228002462005022800246SO 2005 2 28 SIMA200502503 120050116A532014525381 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21735TS 145386 DURING AN IMBV INSPECTION MAINTENANCE FOUND THE LT OMEGA BEAM TO BE CORRODED AT FRAME 25. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED A DOUBLER, FILLER AND TWO SHIMS. REPAIR DONE IAW SRM. (K) 2L72 4F4 FRTT00011ATTE6CH 20050228002522005022800252SO 2005 2 28 SIMA200502802 120050126A3350 CONNECTOR EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL CABIN DISCONNECTED A SIMAK NONE L NO TEST TXTAXI/GRND HDL 1 SW21819AE 145566 EMERGENCY EXIT SIGN ABOVE SEAT, 3B INOPERATIVE. RECONNECTED THE CONNECTOR PLUG AT ROW 3B EMERGENCY EXIT SIGN. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200503030) (K) 2L72 4F4 FRTT00011ATTE6CH 20050228002532005022800253SO 2005 2 28 SIMA200503801 120050205A3350744437 LIGHT EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL EXTERIOR INOPERATIVE A SIMAK NONE L NO TEST TXTAXI/GRND HDL 1 SW21735TS 145386 CREW REPORTED THE LT FUSELAGE EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200503029) (K) 2L72 4F4 FRTT00011ATTE6CH 20050228002542005022800254SO 2005 2 28 SIMA200503805 120050204A33502013A BATTERY EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL CABIN DISCHARGED A SIMAK NONE L NO TEST TXTAXI/GRND HDL 1 SW21716AE 145264 CREW REPORTED THE NR 2 FLOOR PROXIMITY EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A EMERGENCY BATTERY IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200503028) (K) 2L72 4F4 FRTT00011ATTE6CH 20050228002552005022800255SO 2005 2 28 SIMA200503401 120050130A532014525381003 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21635AE 145158 THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED A DOUBLER, FILLER, TWO SHIMS AND PLATE. REPAIR DONE IAW SRM. (K) 2L72 4T4 FRTT00011ATTE6CH 20050228002562005022800256SO 2005 2 28 SIMA200502501 120050116A532014525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21735TS 145386 DURING AN INSPECTION MAINTENANCE FOUND THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 25. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED A DOUBLER, FILLER AND TWO SHIMS. REPAIR DONE ISW SRM. (K) 2L72 4F4 FRTT00011ATTE6CH 20050228002602005022800260SO 2005 2 28 SIMA200503413 120050127A532014524131005 CHANNEL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER TXTAXI/GRND HDL 1 SW21637AE 145170 FOUND SHAPE U UNDER FORWARD CABIN FLOOR AT LOWER MAIN DOOR OPENING BETWEEN FRAMES 14 AND 18 CORRODED AROUND NUTPLATES. REPLACED SHAPE U AT MAIN CABIN DOOR SILL AREA IAW SRM. AC RETURNED TO SERVICE. (K) 2L72 4T4 FRTT00011ATTE6CH 20050228002672005022800267SO 2005 2 28 SIMA200503409 120050127A532014522460009 GUSSET EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21637AE 145170 FOUND GUSSET UNDER CABIN FLOOR FRAME 20 TO 23 HAS CORROSION IN SEVERAL AREAS OF UPPER SURFACE. REPLACED GUSSET IAW SRM. AC RETURNED TO SERVICE. (K) 2L72 4T4 FRTT00011ATTE6CH 20050228002682005022800268SO 2005 2 28 SIMA200501914 120050113A532014521700007 DOUBLER EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21738NR 145401 DURING CPCP INSPECTION MAINTENANCE FOUND THE OMEGA BEAM AT FRAME 20 LT SIDE CORRODED. MAINTENANCE REPLACED CORRODED DOUBLER IAW SRM. AIRCRAFT RETURNED TO SERVICE. (SW21200502486) (K) 2L72 4F4 FRTT00011ATTE6CH 20050228002692005022800269SO 2005 2 28 SIMA200501917 120050115A532014521725613 SILL EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21738NR 145401 DURING CPCP INSPECTION, MAINTENANCE FOUND THE SERVICE DOOR FORWARD SILL HAS CORROSION IN SEVERAL AREAS OF THE UPPER SURFACE. MAINTENANCE REMOVED AND REPLACED THE SERVICE DOOR FORWARD WEB (SILL) IAW SRM. AIRCRAFT RETURNED TO SERVICE. (SW21200502486) (K) 2L72 4F4 FRTT00011ATTE6CH 20050228002712005022800271SO 2005 2 28 SIMA200503407 120050127A532014522461011 DOUBLER EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21637AE 145170 FOUND DOUBLER UNDER CABIN FLOOR AT FRAME 20 CORRODED ON UPPER SURFACE. REPLACED DOUBLER UNDER CABIN FLOOR IAW SRM. AC RETURNED TO SERVICE. (K) 2L72 4T4 FRTT00011ATTE6CH 20050228002742005022800274SO 2005 2 28 SIMA200503405 120050125A532014522178005 CHANNEL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21637AE 145170 FOUND SERVICE DOOR CHANNEL BETWEEN FRAME 20-22 HAS CORROSION AROUND NUTPLATES UPPER SURFACE. INSTALLED NEW SERVICE DOOR CHANNEL IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4T4 FRTT00011ATTE6CH 20050228002762005022800276SO 2005 2 28 SIMA200503402 120050128A532014521713005 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21635AE12044 145158 THE GALLEY CENTER BEAM WAS FOUND TO BE CORRODED. REMOVED THE CORRODED GALLEY CENTER BEAM. INSTALLED NEW BEAM IAW SRM. (K) 2L72 4T4 FRTT00011ATTE6CH 20050228002892005022800289SO 2005 2 28 SIMA200501912 120050113A532014524131007 CHANNEL EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21738NR 145401 DURING CPCP INSPECTION, MAINTENANCE FOUND THE MAIN CABIN DOOR SILL AFT U-SHAPE HAS CORROSION AROUND NUTPLATES. MAINTENANCE REMOVED AND NEW CABIN DOOR SILL AFT U-SHAPE BRACKET SRM. AIRCRAFT RETURNED TO SERVICE. (SW21200502486) (K) 2L72 4F4 FRTT00011ATTE6CH 20050228002992005022800299GL 2005 2 28 SIMA200500910 220050104A7200AE3007A ENGINE EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL NR 2 FAILED A SIMAA UNSCHED LANDING O OTHER TOTAKEOFF 1 SW21823AE 145582 NR 2 ENGINE FAILED DURING TAKEOFF ACCOMPANIED BY A NOISE THAT SOUNDED LIKE A COMPRESSOR STALL. MAINTENANCE REMOVED AND REPLACED THE RT ENGINE IAW MM. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200502355) (K) 2L72 4F4 FRTT00011ATTE6CH 20050228003002005022800300SO 2005 2 28 SIMA200501906 120050112A531514521721009 FLOORBEAM EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21735TS 145386 DURING AN IMBV INSPECTION, A PREVIOUS REPAIR ON FORWARD DIGITAL WAS FOUND TO BE CORRODED. REMOVED THE EXISTING DAMAGED REPAIR. FABRICATED 2 DOUBLERS, AND FILLER. REPAIR DONE IAW SRM. (SW21200502482) (K) 2L72 4F4 FRTT00011ATTE6CH 20050228003152005022800315SO 2005 2 28 SIMA200502801 120050124A532014522178005 SILL EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21706RG11566 145194 FOUND SERVICE DOOR CENTER SILL PREVIOUS REPAIR WAS FOUND CORRODED. REMOVED EXISTING SERVICE DOOR SILL AND INSTALLED NEW SILL SRM. (SW21200503066) (K) 2L72 4F4 FRTT00011ATTE6CH 20050228003212005022800321SO 2005 2 28 SIMA200501919 120050113A532014525480003 SILL EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21735TS 145386 DURING AN IMBV INSPECTION, THE BAGGAGE DOOR SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED BAGGAGE DOOR SILL. INSTALLED NEW SILL, REPAIR DONE IAW SRM. (SW21200502482) (K) 2L72 4F4 FRTT00011ATTE6CH 20050228003252005022800325SO 2005 2 28 SIMA200501913 120050113A532014522178005 CHANNEL EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21738NR 145401 DURING CPCP INSPECTION, MAINTENANCE FOUND THE SERVICE DOOR CHANNEL HAS CORROSION AROUND NUTPLATES. MAINTENANCE REMOVED AND REPLACED SERVICE DOOR CENTER SILL CHANNEL IAW SRM. AIRCRAFT RETURNED TO SERVICE. (SW21200501913) (K) 2L72 4F4 FRTT00011ATTE6CH 20050228003282005022800328SO 2005 2 28 SIMA200501204 120050106A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21846AE 145692 DURING AN INSPECTION OF AIRCRAFT THE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE DAMAGED AREA TO REMOVE THE CORROSION. FABRICATED AN EXTERNAL ANGLE, FILLER PLATE AND 2 SHIMS. REPAIR DONE IAW SRM. (SW21200502476) (K) 2L72 4F4 FRTT00011ATTE6CH 20050301000052005030100005NM 2005 3 1 QXEA200500211 120050205A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 PDX - RIGHTHAND INBOARD SEAT TRACK CORROSION APPROXIMATELY X705 TO X712. REPAIRED IAW RD 8/4-53-884. 2H72 4T RTA13NM 20050301000062005030100006NM 2005 3 1 QXEA200500213 120050202A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 PDX - RIGHTHAND INBOARD SEAT TRACK CORROSION APPROXIMATELY X721 TO X732. REPAIRED IAW RD 8/4-53-884. 2H72 4T RTA13NM 20050301000072005030100007NM 2005 3 1 QXEA200500214 120050202A5420 SUPPORT BRACKET BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 PDX - LT DIAPHRAM SUPPORT BRACKET AT NACELLE TO OUTBOARD WING JUNCTION IS CRACKED. REPAIRED IAW DHC-8 400 SRM 51-40-15. 2H72 4T RTA13NM 20050301000082005030100008NM 2005 3 1 QXEA200500215 120050202A5420 SUPPORT BRACKET BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 PDX - RIGHTHAND DIAPHRAM SUPPORT BRACKET AT NACELLE TO OUTBOARD WING JUNCTION IS CRACKED. REPAIRED IAW DHC08 400 SRM 51-40-15, 51-42-05 AND 51-42-45. 2H72 4T RTA13NM 20050301000302005030100030NM 2005 3 1 UPS05443931 120050207A5410 WEB BOEING747 747123 1384873NM NR 2 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, NR 2 PYLON REAR LOWER WEB AT NAC STN 212 I/B EDGE UPPER SURFACE RIVETS HOLES FOUND CRACKED. NAC STN 212 REAR LOWER WEB REPAIRED PER SRM 54-10-03 FIG 2. 2L74 4F A20WE 20050301000312005030100031EA 2005 3 1 050546233 120050223A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27623BR 7192 INTERCOSTAL CRACKED AT .250 INCH IN LENGTH ON RT INBOARD SIDE AT FS 484 LEFT BETWEEN BL 27.00 AND 36.00. 2L72 4F RTA21EA 20050301000352005030100035EA 2005 3 1 SWIA200514624 120050220A335020131A BATTERY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07464SW 7827 FORWARD FACING CEILING EMERGENCY SIGN HAS A BURNED OUT BULB. REPLACED NR 2 EMERGENCY LIGHT BATTERY PACK AND CHARGER IAW 33-00-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050301000422005030100042SO 2005 3 1 C2XA05CL009 120050213A3230MS17986C616 PIN EMB 145 EMB145XR 3260214SO NOSE GEAR INSTALLED A C2XAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 SW2711121 145683 CLE - CREW REPORTED THAT THE NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THAT THE NOSE GEAR SAFETY PIN HAD NOT BEEN REMOVED. MAINTENANCE REMOVED THE NOSE GEAR SAFETY PIN AND RETURNED AIRCRAFT TO SERVICE. 2L72 4F RT 20050301000482005030100048SO 2005 3 1 C2XA05SD015 120050216A291014531063415 HOSE EMB 145 EMB145XR 3260214SO HYD SYSTEM RUPTURED A C2XAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW2712126 145693 NR 1 ENG, ENGINE DRIVEN HYD PUMP PRESSURE LINE RUPTURED. THE LOCATION OF THE RUPTURE WAS ABOUT THE MIDDLE OF THE LINE. MAINTENANCE REMOVED AND REPLACED PRESSURE LINE AND ENGINE DRIVEN HYDRAULIC PUMP. HYD SYSTEM WAS SERVICED, OPS & LEAK CHECKED GOOD. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. 2L72 4F RT 20050301000492005030100049SO 2005 3 1 C2XA05TY018 120050219A551014520736004 FITTING EMB 145 EMB145LR 3260212SO VERTICAL STAB WORN A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714952 145067 DURING A 4C INSPECTION THE HORIZONTAL TO VERTICAL STAB RT SPHERICAL BEARING HOUSING IN THE VERTICAL STABILIZER FITTING WAS FOUND WORN. MAINTENANCE REAMED THE RT SPHERICAL HOUSING, INSTALLED NEW INTERNAL AND EXTERNAL BUSHINGS, AND COMPLIED WITH A DIEHEDRAL AND INCIDENCE CHECK. AIRCRAFT TO BE RELEASED UPON COMPLETION OF SCHEDULED CHECK. 2L72 4T RTT00011AT 20050301000522005030100052SO 2005 3 1 C2XA05TY019 120050218A32347455503 LEVER EMB 145 EMB145LR 3260212SO MLG MALFUNCTIONED A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2716951 145063 LANDING GEAR DISAGREE MESSAGE UPON ATTEMPTED RETRACTION OF L/G. ACFT RETURNED TO FIELD. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR SELECTOR LEVER AND THE NLG PROXIMITY SENSOR. LANDING GEAR OPERATION CHECK SATISFACTORY. ACFT RELEASED TO SERVICE. 2L72 4T RTT00011AT 20050301000612005030100061EA 2005 3 1 SWIA200514630 120050221A2760C13045BA03 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA SPOILERS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07715SK 10179 STAB/SPLR FAULT STATUS MSG ILLUMINATED. REPLACED NR 1 SSCU AS REQUIRED PER AMM 27-61-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050301000632005030100063SO 2005 3 1 SWIA200514631 120050221A275012064207611 LEVER EMB 120 EMB120ER 3260203SO FLAP SELECTOR MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED LDLANDING 1 NM07578SW3766 3766 120346 CONTROL FAULT WHEN SELECTED FLAPS 15 DEGREES TO 0 DEGREES. REPLACED FLAP HANDLE IAW 27-50-00, OPERATIONAL CHECK GOOD IAW 27-60-00. 2L72 4T RTA31SO 20050301000662005030100066SO 2005 3 1 SWIA200514633 120050219A5270 SWITCH EMB 120 EMB120ER 3260203SO CABIN DOOR DIRTY A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07581SW 120349 MAIN CABIN DOOR DOES NOT CLOSE NORMALLY. REPLACED SHIM STACK, INSPECTED/CLEANED DOOR MICROSWITCHES, CLEANED AND LUBRICATED ALL FITTINGS AND ATTACH DOOR JOINTS. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050301000692005030100069EA 2005 3 1 A6WA200540016 120050108A35103801950110 FLEX LINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE OXYGEN SYSTEM LEAKING A A6WAK NONE O OTHER TXTAXI/GRND HDL 1 GL31427ZW 7685 OXYGEN LOW PRESSURE. WHILE TROUBLESHOOTING FOUND LINE (PN 3801950110) TO CAPTAINS MASK BOX LEAKING. REMOVED AND REPLACED OXYGEN FLEX LINE TO BOTTOM OF CAPTAINS SIDE OXYGEN MASK RETAINER BOX TO COCKPIT FLOOR. LEAK CHECK GOOD. (K) 2L72 4F4 FRTA21EA E15NE 20050301000702005030100070EA 2005 3 1 A6WA200540019 120050117A21707536893 COALESCER BAG CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE A/C BAY DIRTY A A6WAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL31455AW 7848 SUSPECT LT PACK. PERFORMED OPS CHECK OF BOTH LT AND RT PACKS. RT OPS NORMAL, LT PACK EMITS ODOR DURING OPERATION. REMOVED AND REPLACED COALESCER SOCK ON LT PACK. OPS CHECK NORMAL. (K) 2L72 4F4 FRTA21EA E15NE 20050301000712005030100071EA 2005 3 1 A6WA200540021 120050118A5270D3899926WE26SN CONNECTOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR LOOSE A A6WAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL31418AW 7618 PASSENGER DOOR OUTER HANDLE MESSAGE ILLUMINATED DURING FLIGHT. DIVERTED, FOUND PAX DOOR HARNESS PLUG (P7MB) LOOSELY CONNECTED. REMOVED, INSPECTED AND CLEANED DOOR HARNESS. REPLACED DOOR HARNESS, OPS CHECK GOOD. (K) 2L72 4F4 FRTA21EA E15NE 20050301000722005030100072EA 2005 3 1 A6WA200540018 120050108A5610NP13932111 WINDSCREEN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE COCKPIT CRACKED A A6WAO OTHER O OTHER CRCRUISE 1 GL31456ZW2858 7849 CAPTAINS WINDSHIELD SHATTERED IN CRUISE. REMOVED AND REPLACED CAPTAINS WINDSCREEN. OPS CHECK GOOD. (K) 2L72 4F4 FRTA21EA E15NE 20050301000742005030100074EA 2005 3 1 A6WA200540023 120050129A495038301552 MANIFOLD CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE APU CHAFED A A6WAK NONE B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL31411ZW 7569 STRONG ODOR OF JET FUEL IS PRESENT WITH PACKS ON WHILE ON GROUND. FOUND APU PRIMARY MANIFOLD CHAFED THROUGH BY STARTER CONTROL VALVE. REPLACED MANIFOLD IAW AMM AND REPOSITIONED CONTROL VALVE. GROUND RAN AND LEAK AND OPS CHECK GOOD. (K) 2L72 4F4 FRTA21EA E15NE 20050301000762005030100076EA 2005 3 1 A6WA200540026 120050126A3211 BUSHING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT MLG TRUNNION MIGRATED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31414ZW 7586 RT MLG AFT TRUNNION BUSHING IS MIGRATED .046 INCH. REMOVED MIGRATED BUSHING AND INSTALLED 2ND OVERSIZED BUSHING MODIFIED TO A 1ST OVERSIZED IAW EO. 2L72 4F4 FRTA21EA E15NE 20050301000772005030100077EA 2005 3 1 A6WA200540027 120050127A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT WING CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31414ZW 7586 FOUND CORROSION ON RT LOWER WING PLANK UNDER THE FOLLOWING FUEL PANELS 640BB AND 650GB. PERFORMED A MAJOR REPAIR BY REMOVING CORROSION IAW REO. (K) 2L72 4F4 FRTA21EA E15NE 20050301000782005030100078EA 2005 3 1 A6WA200540036 120050125A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31412AW 7582 RT SIDE FS621 THROUGH 625.3 INTERCOSTAL AT STR 14R IS CRACKED IN RADIUS APPROXIMATELY 1.0 INCH. FABRICATED INTERCOSTAL FROM S6144-3 7075 T62-050 INSTALLED IAW CRJ-200 SRM 51-42-06. (M) (K) 2L72 4F4 FRTA21EA E15NE 20050301000812005030100081EA 2005 3 1 A6WA200540043 120050207A4920 APU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE APU BAY SEIZED A A6WAO OTHER A FLAME/FIRE ININSP/MAINT 1 GL31415AW 7593 APU FAILED, REQUESTED INSPECTION. COMPLIED WITH APU INSPECTION FOUND APU TO BE SEIZED. APU INLET EXHAUST NO DEFECTS NOTED. ALSO SUSPECT BAD FCU. COMPLIED WITH ACTION PLACARD PLACED ON MEL. MAINTENANCE VERIFIED APU SEIZED. REMOVED AND REPLACED APU ASSEMBLY. (K) 2L72 4F4 FRTA21EA E15NE 20050301000842005030100084EA 2005 3 1 A6WA200540028 120050127A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE WING CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31414ZW 7586 MWC 170 CORROSION EXISTS ON LOWER WING PLANK UNDER FUEL PANEL 510AB. PERFORMED A MAJOR REPAIR BY REMOVING CORROSION IAW REO. (K) 2L72 4F4 FRTA21EA E15NE 20050301000872005030100087EA 2005 3 1 A6WA200540030 120050124A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31414ZW 7586 LT SIDE FS621 THROUGH FS 625.3 INTERCOSTAL AT STR 14L IS CRACKED IN RADIUS APPROXIMATELY 1.0 INCH LONG. (K) REMOVED AND REPLACED FS 621-625.3 INTERCOSTAL ANGLE AT STRINGER 14L IAW BRAS EO 601R-53-5933. (M) 2L72 4F4 FRTA21EA E15NE 20050301000892005030100089EA 2005 3 1 A6WA200540044 120050205A5720 DOUBLER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT WING MISMANUFACTURED A A6WAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL31412AW 7582 WHILE PERFORMING SB 601R57037 (WING SPAR MOD) IT WAS DISCOVERED THAT THE JOINT STRAP ON THE RT WING LACKS PROPER LENGTH FOR EDGE DISTANCE. COMPLIED WITH BRAS EO 601R575944A, BY FABRICATING DOUBLER FROM 2024T3, .050 INCH AND USING TO EXTEND CUTLINES TO OBTAIN EDGE DISTANCE FOR JOINT STRAP. (K) 2L72 4F4 FRTA21EA E15NE 20050301000972005030100097EA 2005 3 1 A6WA200540038 120050123A52426003328333 SUPPORT BRACKET CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE GPU RECEPTICAL CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31413AW 7585 GPU RECEPTACLE IS BENT EXTERNAL DOOR WILL NOT CLOSE. REMOVED CRACKED SUPPORT ASSY AND INSTALLED NEW SUPPORT ASSY (PN 600-33283-33) IAW CRJ SRM, PAINTED IAW SRM. SOLID RIVETS INSTALLED IAW SRM. (K) 2L72 4F4 FRTA21EA E15NE 20050301000982005030100098EA 2005 3 1 A6WA200540035 120050125A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31412AW 7582 LT SIDE FS621 THROUGH 625.3 INTERCOSTAL AT STR 14L IS CRACKED IN RADIUS APPROXIMATELY 1.0 INCH. (K) REMOVED AND REPLACED INTERCOSTAL IAW CRJ 200 SRM 51-42-06. (M) 2L72 4F4 FRTA21EA E15NE 20050301001042005030100104NE 2005 3 1 A6WA200540042 220050204A7230 COMPRESSOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE ENGINE VIBRATION A A6WAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL31432AW 7257 RETURNED TO DEPARTURE, DUE TO HIGH N1 FAN VIBRATION 2.8 IN CLIMB POWER SET ITT AND N1 NORMAL. INSPECTED NR 2 ENGINE INLET FAN BLADES, EXHAUST AND CHIP DETECTORS. NO DEFECTS FOUND. GROUND RAN ENGINE VIBRATION .8 MILS WITHIN LIMITS REF CF34 ENG MANUAL 72-00-00, TESTING 01 PAGE 1325 AND 1326. (M) 2L72 4F4 FRTA21EA E15NE 20050301001092005030100109NM 2005 3 1 AMTA200500049 120050115A1430 FASTENER BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE FUSELAGE LIGHTNING STRIKEA AMTAK NONE O OTHER ININSP/MAINT 1 GL11515AT 27598 LIGHTNING STRIKE DAMAGED 2 FASTENERS FORWARD AND ADJACENT TO THE L1 DOOR. REPAIRED DAMAGE BY REPLACING DAMAGED FASTENERS IAW PART 1 OF ERA. (K) 2L72 4F4 FRTA2NM E12EU 20050301001102005030100110NM 2005 3 1 AMTA200500050 120050115A5330 SKIN BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE FUSELAGE LIGHTNING STRIKEA AMTAK NONE O OTHER ININSP/MAINT 1 GL11515AT 27598 FUSELAGE SKIN LIGHTNING STRIKE DAMAGE, BLIND FASTENER INSTALLED, FS 297, BL0 TIME LIMITED REPAIR. REPAIRED DAMAGE IAW PAR 1 OF ERA. (K) 2L72 4F4 FRTA2NM E12EU 20050224002762005022400276NM 2005 2 24 SWAA050431 120050215A3350D71702001 BATTERY BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED C3 CHECK, FOUND OVERHEAD CENTER AISLE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20050224002852005022400285WP 2005 2 24 AALA20050100 120050208A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21417AA 49328 SAT - CEILING EMERGENCY LIGHTS AT LAST THREE ROWS IN CABIN INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT LAST THREE ROWS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050224002872005022400287NM 2005 2 24 AALA20050114 120050210A3520 RELAY BOEING767 767323 1385205NM CABIN FAILED A AALAK NONE O OTHER ININSP/MAINT 1 SW21397AN 29604 LAX - PASSENGER OXYGEN SYSTEM FAILED DROP TEST. REPLACED TIME DELAY RELAY K466 FOR PASSENGER OXYGEN SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050224002892005022400289WP 2005 2 24 AALA20050092 120050206A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21249AA 49269 ORD - CEILING EMERGENCY LIGHTS AT ROWS 7 TO 12 INOPERATIVE. REPLACED BATTERY PACK AT B5101 FOR CEILING EMERGENCY LIGHTS AT ROWS 7 TO 12. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050224002912005022400291WP 2005 2 24 AALA20050107 120050212A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21442AA 49468 DEN - CEILING EMERGENCY LIGHTS BETWEEN AFT LAVATORY INOPERATIVE. REPLACED BATTERY PACK AT B527 FOR CEILING EMERGENCY LIGHTS BETWEEN AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050224002932005022400293WP 2005 2 24 AALA20050095 120050207A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21489AA 49682 DFW - FORWARD SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT 27D INOPERATIVE. REPLACED THE FORWARD MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT 27D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050225000012005022500001NM 2005 2 25 DHL2005764500 120050218A5753 SKIN BOEING727 727264 138408MNM TE FLAP DEBONDED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01764AT 22984 RT INBOARD MID FLAP UPPER SKIN TO T/E WBL 200 PREVIOUS FIBERGLASS REPAIR BECOME DISBONDED (PEELING OFF). REMOVED TWO EACH PREVIOUS FIBERGLASS REPAIRS & CLEANED AREA FOR NEW REPAIR IAW B727 SRM 51-40-20 FIG 30. FABRICATED TWO EACH SKIN REPLACEMENTS APPROX 4 X 11 INCHES AND 4 X 10 INCHES AND ONE SPLICE PLATE APPROX 3 X 4 INCHES USING 2024T3 .016 IAW B727 SRM 57-50-2 FIG 3. CLEANED, PREPPED, APPLIED ADHESIVE PRIMER & ADHESIVE TO ALL REPAIR SURFACES FOR BONDING. INSTALLED PARTS & BAGGED FOR BONDING IAW B727 SRM 51-40-20 FIG 30. CURED REPAIR CLEANED AND PERFORMED POST INSP WITH NO DELAM NOTED IAW B727 SRM 51-40-20. ALODINED, PRIMED IAW B727 SRM 51-40-20. 2L73 4F A3WE 20050225000272005022500027EA 2005 2 25 SWIA200514567 120050129A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA FLOORBEAM CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07440SW 7589 MAIN FUSELAGE FS 280.00 LBL 9.0 OUTBOARD CLIP CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIP IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00. 2L72 4F RTA21EA 20050225000512005022500051SO 2005 2 25 CHQA200500035 120050217A3350 LIGHT EMB 135 EMB135KL 3260302SO CABIN DISCONNECTED A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11378SK 145593 MAIN CABIN DOOR EMERGENCY EGRESS LIGHT IS INOP. FOUND GROUND WIRE MISSING FOR LIGHT ASSEMBLY. CLEANED BONDING SURFACE FOR GROUND AND REINSTALLED TERMINAL. OPS CHECK GOOD IAW EMB 140 MM 33-50-0. 2L72 4F RTT00011AT 20050225000552005022500055EU 2005 2 25 MALA050149 120050214A5250 ANGLE SAAB SF340 340B 7860101EU COCKPIT DOOR CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15430XJ 340B430 DURING 4Y/2Y CHECK FOUND COCKPIT DOOR, T-ANGLE POST AT LBL 10 IS CORRODED AND HAS BEEN REPAIRED IAW MESABA EOS53185. 2L72 4T RTA52EU 20050225000672005022500067EA 2005 2 25 COMA0560126 120050217A4910755469E IDG CNDAIRCL600 CL6002B19 1900309EA RT ENGINE FAULTY A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01999CA18455 7230 FLIGHT 5744 DURING CRUISE FLIGHT RECEIVED A LOW APU OIL PRESSURE CAUTION MESSAGE, IDG DEFERRED, AIRCRAFT DIVERTED TO RDU. REPLACED THE RIGHT INTEGRATED DRIVE GENERATOR. 2L72 4F RTA21EA 20050228000292005022800029CE 2005 2 28 DXTA200500600 120050218A21501173T0635 SWITCH CESSNA500 560CESSNA 2076750CE ACM OVERTEMP FAILED E DXTAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 GL07322QS6803 5600421 AT FL 410 RECEIVED THE EMERGENCY PRESS LIGHT. RAN THE CHECKLIST AND RESET THE SYSTEM BACK TO NORMAL. THE CABIN ALTITUDE WENT TO 9000 FEET. THE RATE CONTROLLER SEEMED TO HAVE NO AFFECT AND COULD NOT GET THE CABIN ALTITUDE TO COME DOWN TO THE PROPER ALTITUDE. DESCENDED TO FL 390 AND THE CABIN STABILIZED AT 0200 FEET AND 8.0 DIFF. UPON DIVERSION TO KICT THE CABIN RATE SUDDENLY JUMPED TO 6000 FPM AND THE CABIN ALT IMMEDIATELY WENT THRU 10,000 FEET. DECLARED AN EMERGENCY AND DIVERTED INTO KLIT. CAUSE TRACED TO FAILED ACM OVERTEMP SWITCH. 2L72 4F RTA22CE 20050228000362005022800036EA 2005 2 28 COMA0560131 120050216A27811104SD100101 DRIVE SHAFT CNDAIRCL600 CL6002B19 1900309EA LT WING SLAT WORN A COMAA UNSCHED LANDING O OTHER CRCRUISE 1 SO01819CA 7415 FLIGHT 5808 DURING CRUISE FLIGHT RECEIVED A FLAP FAIL CAUTION, CREW DECLARED AN EMERGENCY AND LANDED AT CVG WITHOUT INCIDENT. REPLACED LEFT WING FLEX DRIVE SHAFT NR 1. 2L72 4F RTA21EA 20050228000412005022800041NM 2005 2 28 DHL2005752001 120050211A2560MR10042N SMOKE HOOD BOEING727 727223 1384074NM COCKPIT DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01752DH 22466 CREW PBE ON COCKPIT DOOR HAS RED BUTTON EXTENDED BEYOND BOX. REMOVED AND REPLACED CREW PBE IAW B-M/M 25-60-02. 2L73 4F A3WE 20050228000682005022800068SO 2005 2 28 MASA200500038 120050116A261014522277403 DUCT EMB 145 EMB145LR 3260212SO CABIN BURNED A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW07826MJ 145214 ASH - CLT CREW FOUND CABIN FILLED WITH SMOKE UPON ARRIVAL TO AIRCRAFT. MAINTENANCE TROUBLESHOT FAULT TO BURNT CABIN SUPPLY DUCTS UNDER THE FLOORBOARDS AND ARE WAITING FOR REPLACEMENT PARTS. MAINTENANCE REPLACED DUCTS AND TEMP SWITCH P/N 1173T0783, CABIN SUPPLY OVERTEMP SWITCH P/N 815291-61, AMBIENT TEMP SWITCH P/N 815289-2. 2L72 4T RTT00011AT 20050228000702005022800070NM 2005 2 28 05FDEA00284 120050213A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 BARREL NUT BORE NR 3L CORROSION REMOVAL FOUND EXCEEDED LIMITS. REMOVED AND REPAIRED PER FEDEX EA 1-5510-81726, 2L73 4F RTA22WE 20050228000812005022800081 2005 2 28 SWAA050390 420050210A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR READS LOW A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 R1 DOOR EVAC SLIDE LOW PRESSURE IND. REMOVED AND REPLACED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050228000932005022800093NM 2005 2 28 SWAA050399 120050210A5313BAC1498 STRINGER BOEING737 7375H4 138449DNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29502SW 24179 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 25L AT BS 970, CORRODED. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2L72 4F RTA16WE 20050228000962005022800096NM 2005 2 28 05FDEA00272 120050210A5310 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25235FE 21329 REPAIR SHEAR TIE AT BS 380 BETWEEN STR 14 AND 15 TO COMPLY WITH FED EX EO 7-5340-7--5002 P1. REPAIRED PER SRM 51-20-1, 51-20-4, 51-30-2. 2L73 4F RTA3WE 20050228000972005022800097NM 2005 2 28 05FDEA00277 120050210A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 BARREL NUT BORE NR 14R CORROSION REMOVAL FOUND EXCEEDED LIMITS. REMOVED AND REPLACED PER SRM 51-33-01 VOLUME II. 2L73 4F RTA22WE 20050228001072005022800107NM 2005 2 28 05FDEA00276 120050210A5530651680310 TIE BOEING727 727200 138407ENM VERTICAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25235FE 21329 CORROSION VERTICAL STAB TENSION TIE RT AFT VERTICAL BOLT HOLE AIRCRAFT AND TENSION TIE. *S/D* REPAIRED PER EA 7-5530-86241. 2L73 4F RTA3WE 20050228001112005022800111WP 2005 2 28 ARWA20050203 120050210A79311G1741A PRESSURE SWITCH DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE NR 1 ENGINE OIL FAILED A ARWAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO19906R 46087 671358 ON CLIMBOUT FROM MIAMI, NR 1 ENGINE OIL LIGHT ILLUMINATED, PERFORMED ABNORMAL OIL PRESSURE LIGHT ILLUMINATED CHECKLIST. LIGHT REMAINED ON. SHUTDOWN ENGINE NR 1. ALL OTHER INDICATIONS WERE NORMAL. RETURNED TO KMIA WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 ENGINE OIL LOW PRESSURE SWITCH IN ACCORDANCE WITH MM 79-32-2 AND SYSTEM OPERATIONAL CHECK NORMAL ON ENGINE RUN-UP IN ACCORDANCE WITH MM 71-00. 2L74 4F4 F 4A25 1E8 20050228001242005022800124WP 2005 2 28 AALA20050098 120050207A3350 LIGHT DOUG DC9 DC982 3022082WP SEAT 19D INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21226AA 49176 DFW - AFT EMERGENCY ESCAPE PATH LIGHT AT SEAT 19D INOPERATIVE. REPLACED AFT EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT 19D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050228001412005022800141EA 2005 2 28 SWIA200514538 120050212A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07449SW 7699 ENTRY WAY FLOOR LEVEL EMERGENCY LIGHT HAS INOPERATIVE BULB. RELAMPED BULB, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050228001422005022800142EA 2005 2 28 SWIA200514539 120050209A2721 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA RUDDER INOPERATIVE A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07953SW 7813 RUDDER TRIM SWITCH INOPERATIVE. REMOVED AND REPLACED RUDDER TRIM PANEL IAW AMM 27-41-25, OPERATIONAL CHECKED GOOD. 2L72 4F RTA21EA 20050228001482005022800148EA 2005 2 28 05042675 120050211A2750 FCU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A VTZAO OTHER F FLT CONT AFFECTED APAPPROACH 1 EA271705 1705 EVENT SUMMARY STATED FLAPS FAILED AT 0 DEGREES. RESET FECU. FLAP SYSTEM OPS CHECK GOOD. 2L72 4F RTA21EA 20050228001602005022800160EU 2005 2 28 05FDEA00262 120050207A5753 SKIN AIRBUS310 A310203 3930313EU ZONE 600 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25405FE 237 RIGHT I/B FLAP LWR T/E DELAMINATED. REMOVED EXISTING REPAIR. DRIED HONEYCOMB CORE IAW A310-200 SRM 51-77-10 PARA 2(G). INSTALLED DOUBLER ON UPPER AND LWR SKINS IAW A310-200 SRM 57-53-12 PARA 11. INSTALLED RIVETS IN T/E IAW A310-200 SRM 51-40-21. 2L72 4F RTA35EU 20050228001622005022800162NM 2005 2 28 DL76L050095 120050208A2120 ODOR BOEING767 767332 1382001NM A/C COMPARTMENT DETECTED A DALAC ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SO27175DN 24803 AFTER APU STARTED ON THE GROUND BOTH PACKS WERE TURNED ON. AN OILY SMELL WAS EVIDENT IN THE COCKPIT. AFTER TAKEOFF THE SMOKE DETECTOR IN THE FWD MID CABIN LAV CAME ON AND THE SAME OILY SMELL WAS EVIDENT IN BOTH THE CABIN AND COCKPIT. OILY SMELL DISSIPATED AFTER APPROX 15 MIN OF FLT. RAN APU AND PACKS FOR 1 HR, NO OILY SMELL DETECTED. 2L72 4F RTA1NM 20050228001732005022800173NM 2005 2 28 SWAA050527 120050222A571265C800091 RIB BOEING737 7375H4 138449DNM LT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29507SW 24184 DURING SCHEDULED 1/2D CHECK, FOUND BOTH LT & RT WING LOWER T-CHORDS CRACKED AT WBL 135.5, BETWEEN STR 2 & 3. REPAIRED T-CHORDS PER SWA EA. 2L72 4F RTA16WE 20050228001762005022800176NM 2005 2 28 05FDEA00193 120050128A5531 STRINGER BOEING727 727200 138407ENM VERTICAL STAB CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25235FE 21329 STRINGER CRACKED IN VERTICAL FIN AT VERT FIN STA 110.4 STRINGER 7 LEFT. *S/D* REPAIRED PER SRM 55-30-4. 2L73 4F RTA3WE 20050228001812005022800181NE 2005 2 28 DL76G050100 220050210A7230CF680C2B6F ENGINE BOEING767 767324 1385203NM GE CF6 CF680C2B6F 30025NE NR 2 DAMAGED A DALAK NONE J WARNING INDICATION ININSP/MAINT 1 SO27394DL21199 27394 706113 BORESCOPE NR 2 ENG BOOSTER (LPC) AND HPC PER AMM TASK 72-00-00-206-H00 DUE TO PARAMETER SHIFT ON ENG. TREND AND RECENT FAN BLADE REPLACEMENT FOR IMPACT. ENGINE FAILED BOROSCOPE INSPECTION. REPLACED ENGINE. 2L72 4F4 FRTA1NM E13NE 20050228001892005022800189EA 2005 2 28 05052625 120050221A3220 LANDING GEAR CNDAIRCL600 CL6002B19 1900309EA NOSE MALFUNCTIONED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27625BR 7214 GEAR DISAGREE MESSAGE AND NLG WOULD NOT RETRACT. MX PERFORMED GEAR SWINGS SEVERAL TIMES. NO DEFECT NOTED. 2L72 4F RTA21EA 20050228001902005022800190WP 2005 2 28 AALA20050117 120050215A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21258AA 49288 DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT 9D AND 18D INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT 9D AND 18D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050228002042005022800204NM 2005 2 28 SWAA050493 120050219A33506556633 LIGHT BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29352SW 24888 LEFT OVERWING EMERGENCY EXIT LIGHT COVER LOOSE. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2L72 4F RTA16WE 20050228002072005022800207EA 2005 2 28 MASA200500106 120050212A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSBURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0797325 7325 ASH - PHX REPORTED ONE CABIN CEILING EXIT LIGHT INOP. MAINTENANCE MEL'ED THE EXIT LIGHT. MAINTENANCE RELAMPED, OPS CHECKED GOOD. 2L72 4F RTA21EA 20050228002282005022800228 2005 2 28 DL76G050110 420050215A3460 COMPUTER BOEING767 767332 1382001NM FLT DIRECTOR INOPERATIVE A DALAO OTHER G MULTIPLE FAILURE APAPPROACH 1 SO271610D 30594 DURING DIVERSION FOR WEATHER INTO SKG, CAPT PITOT MSG ILLUMINATED ON FINAL. AFTER GO AROUND - AILERON LOCKOUT MSG RUDDER RATIO MSG LT AND RT EEC MSG ILLUM. F/O FLT DIR STOPPED WORKING. DISCOVERED C/B K-15 ON P6-3 PANEL POPPED. RESET, ALL RETURNED TO NORMAL. RUDDER RATIO LIGHT FIM PROCEDURE 27-21-00 PG 107 AND 27-09-00 PG 107 CHECK OUT OF SYS OK. AIL LOCKOUT FIM 27-11-00 CHECK OUT OK. PIMU LT AND RT BITE OK. REMAIN GROUND RUN UP FOR SYS VERIFICATION GOOD. 2L72 4F RTA1NM 20050228002402005022800240NM 2005 2 28 05FDEA00075 120050111A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25235FE 21329 BS 720F, STR 23R STRINGER CORROSION (C53-111-01). *S/D* CORROSION 100 PERCENT IN MATERIAL REMOVED AND REPLACED STRINGER PER SRM 53-10-2 & 51-30-2. 2L73 4F RTA3WE 20050228002442005022800244EU 2005 2 28 RAIA00502022 120050215A7931 WARNING SYSTEM JETAIRJETSTMJETSTM4101 1500501EU RT ENGINE OIL MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03557HK 41074 GSO - RIGHT ENGINE OIL PRESSURE WARNING INDICATION. MAINTENANCE TROUBLESHOT AND FOUND GAUGE INDICATION OK; DEFERRED OIL PRESSURE WARNING SYSTEM IAW MEL. REMOVE AND REPLACE NR 2 PRESSURE SWITCH. 2L72 4T RTA41NM 20050228002612005022800261SO 2005 2 28 SIMA200503412 120050127A532014524131007 CHANNEL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21637AE 145170 FOUND SHAPE U UNDER FORWARD CABIN FLOOR AT LOWER MAIN DOOR OPENING BETWEEN FRAME 14 AND 18 CORRODED AROUND NUTPLATES. REPLACED SHAPE U AT PAX DOOR SILL AREA IAW SRM. AC RETURNED TO SERVICE. (K) 2L72 4T4 FRTT00011ATTE6CH 20050228002642005022800264EA 2005 2 28 SIMA2005004 120050101A335020131A BATTERY PACK CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE CABIN DISCHARGED A SIMAK NONE L NO TEST TXTAXI/GRND HDL 1 SW21506AE 10056 CABIN EMERGENCY LIGHT SWITCH LEFT SELECTED ON, LIGHT ARE INOPERATIVE. REPLACED NR 1, 2, 3, AND 4 EMERGENCY BATTERY PACKS. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. PN 2013-1A, SN (NR1 72797), (NR2 65477), (NR3 82281), AND (NR4 84125). (SW21200503034) (K) 2L72 4F4 FRTA21EA EOOO63EN 20050228002662005022800266SO 2005 2 28 SIMA200503411 120050128A532014521721005 STRAP EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21637AE 145170 FOUND STRAP UNDER FORWARD CABIN FLOOR BETWEEN FRAMES 14 AND 16, HAS CORROSION ON UPPER FORWARD SURFACE. REMOVED CORROSION ON STRAP UNDER FORWARD CABIN FLOOR BETWEEN FRAMES 14 AND 16 IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4T4 FRTT00011ATTE6CH 20050228002732005022800273SO 2005 2 28 SIMA200503406 120050125A534714530659011 SEAT TRACK EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21637AE 145170 FOUND LT FORWARD SEAT TRACK CORRODED. REPLACED SEAT TRACK IAW AMM. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4T4 FRTT00011ATTE6CH 20050228002822005022800282SO 2005 2 28 SIMA200501201 120050106A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21846AE 145692 DURING AN MBV INSPECTION THE CENTER OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE DAMAGED AREA TO REMOVE THE CORROSION. FABRICATED A DOUBLER, FILLER AND TWO SHIMS. REPAIR DONE IAW SRM. (SW21200502476) (K) 2L72 4F4 FRTT00011ATTE6CH 20050228002862005022800286SO 2005 2 28 SIMA200501907 120050113A532014522460013 GUSSET EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21738NR 145401 DURING INSPECTION THE FORWARD CABIN FLOOR GUSSET FRAME 20 TO FRAME 23 HAS CORROSION IN SEVERAL AREAS. INSTALLED NEW FLOOR GUSSET IAW SRM. AIRCRAFT RETURNED TO SERVICE. (SW21200502486) (K) 2L72 4F4 FRTT00011ATTE6CH 20050228003142005022800314SO 2005 2 28 SIMA200501916 120050115A532014522461011 DOUBLER EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21738NR 145401 DURING CPCP INSPECTION MAINTENANCE FOUND THE FORWARD CABIN DOUBLER AT FRAME 20 HAS CORROSION NEAR IB EDGE. MAINTENANCE REMOVED AND REPLACED NEW DOUBLER IAW SRM. AIRCRAFT RETURNED TO SERVICE. (SW21200502486) (K) 2L72 4F4 FRTT00011ATTE6CH 20050228003222005022800322SO 2005 2 28 SIMA200501908 120050113A532013500469401 ANGLE EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21738NR 145401 DURING CPCP INSPECTION MAINTENANCE FOUND THE FORWARD CABIN PROFILE (Z) AT FRAME 22 HAS CORROSION IN SEVERAL FORWARD SURFACE AREAS. MAINTENANCE REMOVED AND REPLACED NEW PROFILE (Z) IAW SRM. AIRCRAFT RETURNED TO SERVICE. (SW21200502486) (K) 2L72 4F4 FRTT00011ATTE6CH 20050228003292005022800329EU 2005 2 28 SIMA200501903 120050117A335066363 LIGHT SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE CABIN INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21382AE 340B382 CREW REPORTED FLOOR PROXIMITY EMERGENCY LIGHT STRIP AT ROW 9/10 TO BE INOPERATIVE. LIGHT WAS PUT ON MEL AT THIS TIME. MAINTENANCE REMOVED AND REPLACED THE LIGHT STRIP IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200502551) (K) 2L72 4T4 TRTA52EU E8NE 20050301000162005030100016NM 2005 3 1 UPS05443919 120050209A5730 SKIN BOEING747 747123 1384873NM LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, LT WING REAR SPAR UPPER SPLICE FITTING AT BS 1241 HOLE NR 11 FOUND CRACKED AT WING SKIN APPROX 0.060 INCH. HOLE REWORKED AT BSB 747-57A2314. 2L74 4F A20WE 20050301000322005030100032SO 2005 3 1 SWIA200514622 120050217A2751 ANNUNCIATOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER N FALSE WARNING APAPPROACH 1 NM07268UE 120207 ON APPROACH, WHEN SELECTING FLAPS, RECEIVED CONTROL FAULT WITH FLAP DISAGREE. REMOVED AND REPLACED ANNUNCIATOR ASSY, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050301000342005030100034NE 2005 3 1 SWIA200514623 220050221A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE RIGHT SMOKE A SWIAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 NM07903SW 7425 AFTER APPLYING TAKEOFF THRUST, NOTICED A STRONG OIL SMOKE SMELL IN THE AIRCRAFT. SMELL DISAPPEARED AFTER SEVERAL MINUTES IN FLIGHT. RECEIVED SMOKE TOILET MESSAGE DURING INITIAL CLIMBOUT. REMOVED AND REPLACED RIGHT ENGINE. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20050301000382005030100038EA 2005 3 1 SWIA200514627 120050220A5610 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAO OTHER O OTHER DEDESCENT 1 NM07438SW 7574 ON DESCENT F/O SIDE WINDOW CRACKED. REPLACED F/O SIDE WINDOW IAW MM 56-12-01. OPERATIONAL CHECK GOOD. P/N NP-139322-6, S/N OFF 01165H49955. 2L72 4F RTA21EA 20050301000472005030100047SO 2005 3 1 C2XA05IA028 120050215A2612 FIRE WARNING EMB 145 EMB145LR 3260212SO APU FALSE ACTIVATIONA C2XAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW2712900 145511 CLE - THE CREW REPORTED A MOMENTARY APU FIRE MASTER WARNING IN FLIGHT DURING START. THE AIRCRAFT LANDED AT CLE WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE APU, PERFORMED OPERATIONAL CHECKS WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050301000732005030100073EA 2005 3 1 A6WA200540020 120050118A3222 SEAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NLG STRUT FAILED A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31404AW 7294 AFTER TAKEOFF, RECEIVED RED NOSE DOOR GEAR MESSAGE AND RED GEAR DISAGREE MESSAGE. REMOVED AND REPLACED NOSE LANDING GEAR STRUT SEALS. RESERVICED NLG STRUT, OPS CHECK GOOD. (K) 2L72 4F4 FRTA21EA E15NE 20050301000752005030100075EA 2005 3 1 A6WA200540024 120050128A3260 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE COCKPIT MALFUNCTIONED A A6WAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL31449AW 7878 UPON GEAR RETRACTION, NOSE DOOR END GEAR DISAGREE WARNING MESSAGE ILLUMINATED. CYCLED NLG WITH LINKS ATTACHED OPS CHECK GOOD OK FOR RETURN TO SERVICE IAW. (K) 2L72 4F4 FRTA21EA E15NE 20050301000962005030100096EA 2005 3 1 A6WA200540031 120050124A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31414ZW 7586 RT SIDE FS621 THROUGH FS623.3 INTERCOSTAL AT STR 14R IS CRACKED IN RADIUS APPROXIMATELY 1.1 INCH LONG. REMOVED AND REPLACED FS 621-625.3 INTERCOSTAL ANGLE AT STRINGER 14R IAW BRAS EO 601R-53-5933. (M) (K) 2L72 4F4 FRTA21EA E15NE 20050301001082005030100108NE 2005 3 1 ALG2005F00013 120050119A3246 FLOAT SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL LANDING GEAR DEPLOYED E ALGAK NONE O OTHER ININSP/MAINT 1 SW03518AL 760134 AFTER LANDING, ON EI309, WHILE COMPLETING THE (AFTER LANDING CHECK LIST) THE CO-PILOT INADVERTENTLY DEPLOYED THE FLOATS. THE MECHANIC DEFLATED ALL FLOATS AND REPACKED FRONT FLOATS AND REPLACED RT AND LT FLOAT GEAR DOORS, ALSO CHANGED ALL 4 FLOAT BOTTLES. (K) 1G72 3U3 U H1NE E1GL 20050301001122005030100112NM 2005 3 1 AMTA200500168 120050213A2613 WARNING SYSTEM BOEING757 75733N 1384931NM RROYCERB211 RB21122* 54555NE COCKPIT MALFUNCTIONED A AMTAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL11557TZ 32591 LT ENG OVHT EICAS CAME ON AT CRUISE ALT (40000) PERFORMED ENG OVHT CHECK LIST AND SHUTDOWN LT ENG. PERFORMED FIM 26-12-00, FIG 103 FOUND NO DEFECTS. RAN ENGINE TO HIGH POWER SETTING WITH NO DEFECTS. OPERATIONAL CHECK NORMAL. (K) 2L72 4F4 FRTA2NM A12EU 20050301001182005030100118NM 2005 3 1 AMTA200500096 120050127A3397 WIRE BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE CABIN DISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11522AT 29330 EGRESS TRACK LIGHTING AT SEAT ROWS 5-9, INOPERATIVE. CONNECTED WIRING AT ROW 5. OPS GOOD. 2L72 4F4 FRTA2NM E12EU 20050301001202005030100120NM 2005 3 1 USAA050089 120050101A5320 FLOOR SUPPORT BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19522AU49282 23857 PIT - Q3 - FLOOR SUPPORT, 1 INCH X 2 INCH AT 3 AREAS; CORROSION; LEVEL 1; TASK NR C53-107-02, STA 947.5-966 RBBL. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-10-00. 2L72 4F4 FRTA16WE E21EU 20050301001212005030100121NM 2005 3 1 USAA050095 120050101A5754652660117 STRUCTURE BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU L/E SLAT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19517AU 23703 PIT - Q6 - NR 1 SLAT, .1250 INCH CRACKS-2 EA; LOWER T-CHORD, AFT ROW OF FASTENERS, APPROX 40 INCHES FROM IB EDGE. INSTALLED DOUBLER IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050301001222005030100122 2005 3 1 EM05002 420050212A2230426000183 THROTTLE CONTROL EMB ERJ170ERJ170100 EU COCKPIT DEFECTIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19803MD1297 17000015 AUTO THROTTLE FAIL ON POWER UP. MAINTENANCE REMOVED AND REPLACED AUTO THRUST CONTROL QUADRANT. 2L74 4F RTA56NM 20050301001232005030100123NM 2005 3 1 USAA050085 120050119A5320 THRESHOLD BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19522AU49282 23857 PIT - Q3 - WEB PLATE, .2500 INCH AROUND, CORROSION; LEVEL 1; TASK NR C53-202-01; AFT CARGO DOOR THRESHOLD AROUND NUT PLATE HOLES. DEFECTIVE PART REPLACED WITH IDENT PART IAW DWG 65-47957 AND SRM 51-40-03. (K) 2L72 4F4 FRTA16WE E21EU 20050301001242005030100124NM 2005 3 1 USAA050162 120050109A53451133022 BRACKET BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19521AU52728 23856 PIT - Q6 - BRACKET, 10 INCHES LONG CRACK; VHF COMM ANT BRACKET, STA 500-500A FWD BAGGAGE PIT; REMOVED AND REPLACED CRACKED BRACKET, BLENDED CORROSION IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050301001262005030100126NM 2005 3 1 USAA050164 120050103A532069353593 INTERCOSTAL BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19521AU52728 23856 PIT - Q6 - BAFFLE, 1 INCH CRACK; AFT CARGO BIN STA 927 S-25L; FABRICATED AND INSTALLED NEW BAFFLE IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050301001272005030100127NM 2005 3 1 USAA050165 120050101A5320654683452 CHANNEL BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19521AU52728 23856 PIT - Q6 - CHANNEL, .7500 INCH CRACK; ST277, BL0, FWD CABIN FLOOR; DEFECTIVE PART REPLACED WITH IDENT PART IAW MFG DWG. (K) 2L72 4F4 FRTA16WE E21EU 20050301001282005030100128NM 2005 3 1 USAA050087 120050101A5320 ANGLE BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19522AU49282 23857 PIT - Q3 - ANGLE, 1 INCH DIA. SPOT; EXFOLIATED CORROSION; BS 530, RT AT KEELBEAM, S-27R. KEELBEAM SECTION, -2 DOUBLER, -1 STRAP IAW TYP. REP. 53-60-09. 2L72 4F4 FRTA16WE E21EU 20050301001302005030100130EU 2005 3 1 SA05026 120050227A5610NP1653116 WINDSHIELD AIRBUSA319 A319112 3930323EU COCKPIT CRACKED A USAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA19721UW16993 1095 CLT - FLT 200 EN-ROUTE MSP TO CLT, DURING FLIGHT, THE FIRST OFFICER'S WINDSHIELD BEGAN TO ARC, AND THEN CRACK. CREW PULLED THE CIRCUIT BREAKER FOR THE WINDSHIELD ANTI-ICE HEAT AND DESCENDED TO FL 230. FLIGHT CONTINUED TO CLT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FIRST OFFICER'S WINDSHIELD. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20050301001312005030100131NM 2005 3 1 USAA050090 120050104A5311 FRAME BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19517AU 23703 PIT - Q6 - FRAME, .0625 INCH CRACK, CRACK RADIATING FROM RIVET AT STA 827S-9R. INSTALLED DOUBLER IAW SRM 53-10-20A. (K) 2L72 4F4 FRTA16WE E21EU 20050301001332005030100133NM 2005 3 1 USAA050098 120050101A5320 STIFFENER BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19517AU53410 23703 PIT - Q6 - STIFFENER, .5 INCH CRACK; STIFFENER CRACKED BETWEEN S-12R AND S13R AT STA 291. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM AND DWG. (K) 2L72 4F4 FRTA16WE E21EU 20050301001342005030100134NM 2005 3 1 USAA050091 120050101A5311 FRAME BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19517AU53410 23703 PIT - Q6 - FRAME - .1250 INCH CRACK, RADIATING FROM RIVET HOLE AT STA 907 S-9R. DOUBLER INSTALLED IAW SRM 53-10-20A. 2L72 4F4 FRTA16WE E21EU 20050301001362005030100136NM 2005 3 1 USAA050099 120050101A52306547962524M STRUCTURE BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU AFT CARGO DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19517AU53410 23703 PIT - Q6 - AFT CARGO DOOR, .4375 INCH CRACK; BOTTOM OUTER T-CHORD FASTENER HOLE, LOWER AFT END; INSTALLED FABRICATED PART IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050301001382005030100138NM 2005 3 1 SB05029 120050220A33503004321 SOCKET BOEING737 7373B7 1384580NM EXTERIOR DIRTY A USAAK NONE L NO TEST ININSP/MAINT 1 EA19390US 23312 BDL - MAINTENANCE REPORTED THE EXTERIOR EMERGENCY LIGHT AT THE L1 DOOR INOPERATIVE. MAINTENANCE CLEANED SOCKET AND RELAMPED. OPERATIONAL CHECK NORMAL. 2L72 4F RTA16WE 20050301001402005030100140EU 2005 3 1 USAA050032 120050101A5315D5347219021000 FLOORBEAM AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19713UW 1040 BFM - S1 - FLOORBEAM, 1 INCHL X 1 INCH W X .03 INCH D, CORROSION; LEVEL 2; TASK NR JA260-53500, MAIN CABIN FLOOR FR 64-66, Y1292. REMOVED AND REPLACED FLOORBEAM IAW SRM. (K) 2L72 4F4 FRTA28NM E37NE 20050301001412005030100141NM 2005 3 1 USAA050088 120050101A53206543854256 INTERCOSTAL BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19522AU49282 23857 PIT - Q3 - INTERCOSTAL, 1 INCH DIA (4 EA AREAS) CORROSION ; LEVEL 1; TASK NR C53-107-01, RBBL 10 BS 312 TO 328. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-10-02. (K) 2L72 4F4 FRTA16WE E21EU 20050302000012005030200001EU 2005 3 2 ASOA05087 120050112A5315 FLOORBEAM AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27534AS 463 DURING A C-CHECK, THE FLOORBEAMS AT FR 36, 38 AND 39 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAMS AT FR 36, 38 AND 39 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAMS AT FR 36, 38 AND 39 IAW SRM. (K) 2H72 4T4 TRTA53EU E20NE 20050302000032005030200003EU 2005 3 2 ASOA05089 120050112A5320S5367800821602 FLOOR SUPPORT AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27534AS 463 DURING A C-CHECK, THE Z-FLOOR SUPPORT BETWEEN FR 39 TO 41, STRINGER 14R WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE Z-FLOOR SUPPORT BETWEEN FR 39 TO 41, STRINGER 14R IAW SRM. (K) 2H72 4T4 TRTA53EU E20NE 20050302000042005030200004EU 2005 3 2 ASOA05090 120050112A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27534AS 463 DURING A C-CHECK, THE SEAT TRACK BETWEEN FR 36 TO 39 ON THE RT SIDE WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK BETWEEN FR 36 TO 39 ON THE RT SIDE IAW SRM. (K) 2H72 4T4 TRTA53EU E20NE 20050302000052005030200005EU 2005 3 2 ASOA05094 120050118A5753S5751203220300 RIB AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE T/E FLAP CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27534AS 463 DURING A C-CHECK, THE RT IB FLAP L/E RIB WAS FOUND TO BE CRACKED BEYOND LIMITS AT RIB 6. MAINTENANCE REMOVED AND REPLACED THE RT IB FLAP L/E RIB AT RIB 6 IAW SRM. (K) 2H72 4T4 TRTA53EU E20NE 20050302000062005030200006 2005 3 2 S2YA05008 420050131A31606229682002 PROCESSOR BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE COCKPIT FAILED A S2YAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL1387SK UE87 BEFORE FLIGHT, THE CREW REPORTED BOTH CAPTAIN`S DISPLAY TUBES FAILED, THEY RETURNED TO THE GATE FOR MECHANIC. MECHANIC SWAPPED THE DPU-84 DISPLAY PROCESSORS AND ALL DISPLAYS WERE OPERATIONAL, WITH NO FURTHER DISCREPANCIES NOTED THE AC WAS RETURNED TO SERVICE. (K) 2L72 4T4 TRTA24CE E26NE 20050302000152005030200015EA 2005 3 2 ASOA05046 120050119A1430N3537 NUT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN MISSING A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27902EV 7620 DURING A GROUND INSPECTION, THE FORWARD EMERGENCY FLOOR LEVEL FLOODLIGHT BY THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE FOUND A NUT MISSING ON THE GROUND STUD TO THE FORWARD EMERGENCY FLOOR LEVEL FLOODLIGHT BY THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050302000192005030200019NM 2005 3 2 USAA050200 120050113A321165C32102 SUPPORT BEAM BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU LT MLG GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19436US 24558 PIT - Q3 - MLG SUPPORT BEAM, .025 DEEP .250 X .125 (4 EA) GOUGE; LT MLG SUPPORT BEAM, LOWER FLANGE AFT EDGE 37 INCHES OB OF IB EDGE. (K) 2L72 4F4 FRTA16WE E21EU 20050302000222005030200022EU 2005 3 2 ASOA05092 120050115A5320S5307030922500 FLOOR SUPPORT AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27534AS 463 DURING A C-CHECK, THE FLOOR SUPPORT ANGLE BETWEEN FR 43 TO 44 RT WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT ANGLE BETWEEN FR 43 TO 44 RT IAW SRM. (K) 2H72 4T4 TRTA53EU E20NE 20050302000232005030200023EA 2005 3 2 ASOA05096 120050126A5320 CHANNEL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT MLG WW CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27847AS 7335 DURING A C-CHECK, THE MLG WHEEL WELL CHANNEL AT FS 529, RHS UNDER THE UPLOCK BOX WAS FOUND BENT AND CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE MLG WHEEL WELL CHANNEL AT FS 529, RHS IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050302000242005030200024NE 2005 3 2 HALA0500208 220050213A7200 ENGINE BOEING767 767300 1385204NM PWA 4060 PW4060 52119NE LEFT STALLED A HALAK NONE RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 WP13590HA 33467 ATB - LT ENGINE, AT ABOUT 300 FT STALLED ONCE, PRIOR TO POWER REDUCTION- (2) PRIOR TO POWER REDUCTION AT ABOUT 600 FT. RT ENGINE STALLED ONCE. AIRCRAFT DIVERTED, WHERE AN UNEVENTFUL LANDING WAS MADE. REPAIR IN WORK. (K) 2L72 4F4 FRTA1NM E24NE 20050302000262005030200026NM 2005 3 2 USAA050155 120050101A573065C26701 SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU RT WING CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19521AU52728 23856 PIT - Q6 - SKIN, APPROX 1 INCH CRACK; NR 2 ENG OB WING/LEADING EDGE AT SLAT STA3.25, LWR SKIN PANEL. FABRICATED SKIN FILLER/ DOUBLER IAW TYP REP. (K) 2L72 4F4 FRTA16WE E21EU 20050302000362005030200036NM 2005 3 2 AMTA200500152 120050206A2613 WARNING SYSTEM BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE COCKPIT ACTIVATED A AMTAK NONE J WARNING INDICATION CRCRUISE 1 GL11559TZ 32593 LT STRUT OH DET 1 DISPLAYED. NO ANOMALIES FOUND IAW FIM. OPS CHECK GOOD AT THIS TIME IAW AMM. (K) 2L72 4F4 FRTA2NM E12EU 20050302000372005030200037NM 2005 3 2 AMTA200500158 120050209A3397 WIRE BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE CABIN DISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11524AT 30233 EGRESS LIGHTS IN AFT SECTION (SEVERAL) INOPERATIVE. RECONNECTED WIRE AS REQUIRED. OPS CHECK, OK. (K) 2L72 4F4 FRTA2NM E12EU 20050302000382005030200038NM 2005 3 2 S2YA05006 120050118A3244AHA22262 TIRE DORNERDO32 DO328300 NM PWA 306 PW306B NE MLG LOW A S2YAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL13351SK4740 3108 BEFORE FLIGHT, DURING TAXI THE CREW WAS NOTIFIED THAT ONE OF THE TIRES WAS LOW. THE AC RETURNED TO THE GATE. MECHANIC REPLACED THE NR3 WHEEL ASSY, WITH NO FURTHER DISCREPANCIES NOTED THE AC WAS RETURNED TO SERVICE. (K) 2H72 4T4 FRTA55NM E35NE 20050302000462005030200046CE 2005 3 2 N382005F00001 120050121A2612244039L5 FIRE LOOP LEAR 35 35A 5170602CE GARRTTTFE731TFE731* 01518WP LT ENGINE DEFECTIVE E N38AO OTHER N FALSE WARNING NRNOT REPORTED 1 EA05825LJ9748 496 LT ENGINE FIRE T-HANDLE WAS FLASHING. NO OTHER INDICATIONS OF FIRE. PERFORMED RESISTANCE CHECK OF LT ENGINE FIRE LOOPS AND FOUND CENTER CONDUCTOR RESISTANCE OF ACCESSORY GB LOOP READING HIGH. REPLACED LT ENGINE ACCESSORY GB LOOP. FUNCTIONAL CHECK AND GROUND RUN OK. (K) 2L72 4F4 F A10CE E6WE 20050302000532005030200053 2005 3 2 GAIA05003OP 420050128A344220412323110 INDICATOR BOEING727 727223 1384074NM PWA JT8 JT8D9A 52048NE COCKPIT SHORTED A GAIAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SW07856AA 20997 DURING DESCENT THE RADAR SCREEN FLARED BRIGHTLY, THE RADAR TCAS DISPLAY WENT OUT. SHORTLY AFTERWARD A STRONG ELECTRICAL SMELL WAS NOTICED. THE RADAR AND TCAS WERE TURNED OFF AND ASSOCIATED CIRCUIT BREAKERS WERE PULLED. THE SMELL DISSIPATED WITHIN A FEW MINUTES. THE AC MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED RADAR INDICATOR. INSPECTED ASSOCIATED WIRING AND RESET CIRCUIT BREAKERS. OPS CHECK GOOD. AC WAS RETURNED TO SERVICE. (K) 2L73 4F4 F A3WE E2EA 20050302000552005030200055NM 2005 3 2 HALA0500176 120050207A5312 BULKHEAD BOEING767 767300 1385204NM FUSELAGE CRACKED A HALAK NONE O OTHER ININSP/MAINT 1 WP13584HA 24258 WHILE COMPLYING WITH AD, A 7 INCH CRACKED WAS FOUND IN THE NOSE WW, AFT BULKHEAD, RT VENT CORD AT B.SB 287, RBL, 25, WL 168-175. REPAIR IN WORK. 2L72 4F RTA1NM 20050302000562005030200056CE 2005 3 2 S2YA05002 120050103A3010 TUBE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE LT STABILIZER DAMAGED A S2YAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL1387SK UE87 DURING FLIGHT, THE TAIL DEICE BECAME INOPERATIVE. DUE TO ENROUTE WEATHER, THE CREW PERFORMED AN AIR-TURN-BACK. THE SYSTEM WAS INSPECTED AND MECHANIC REPAIRED THE EVA TUBING IN THE LT STABILIZER ABOVE THE LOGO LIGHT. THE SYSTEM WAS INSPECTED AND WITH NO FURTHER DISCREPANCIES THE AC WAS RETURNED TO SERVICE. (K) 2L72 4T4 TRTA24CE E26NE 20050302000582005030200058NM 2005 3 2 S2YA05003 120050105A3242AHA22274 BRAKE ASSY DORNERDO32 DO328300 NM PWA 306 PW306B NE LT MLG FROZEN A S2YAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL13356SK8911 2016 3163 BEFORE FLIGHT, DURING TAXI FROM GATE TO DEICE RAMP THE CREW WAS NOTIFIED THAT LT TIRE WAS NOT ROTATING. THE AC RETURNED TO THE GATE. MECHANIC DISCOVERED THE NR 1 TIRE FLAT AND THE LT BRAKES FROZEN. MECHANIC REPLACED BOTH LT WHEEL ASSEMBLIES AND THE BRAKE. WITH NO FURTHER DISCREPANCIES NOTED THE AC WAS RETURNED TO SERVICE. (K) 2H72 4T4 FRTA55NM E35NE 20050330001662005033000166SO 2005 3 30 N3B2005F00000 220050110A8520642399 CONNECTING ROD CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO NR 6 CYLINDER LOOSE E N3BAK NONE O OTHER ININSP/MAINT 1 SW01775RC700 402C0311 IT APPEARS FOR SURE THAT NUT ON CONNECTING ROD CAP, LOOSEN. BOLT HEAD SHEARED OFF. ENGINE STOPPED RUNNING SOOP AFTERWARD. (BOLT NR 629340) (K) 1L72 3O3 O A7CE E8CE 20050330001712005033000171CE 2005 3 30 S2YA05009 120050114A32301013880083 VALVE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE MLG INOPERATIVE A S2YAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL13831SK24305 UE83 SHORTLY AFTER TAKEOFF OF FLIGHT, THE CREW WAS UNABLE TO RETRACT THE GEAR. THE CREW PERFORMED AN AIR-TURN-BACK. MECHANIC INSPECTED THE SYSTEM AND REPLACED THE MLG HANDLE/SWITCH BUT OPS CHECKS WERE STILL BAD. MECHANIC REPLACED THE GROUND SERVICE VALVE AND PERFORMED A GEAR SWING, WITH NO FURTHER DISCREPANCIES NOTED, AC WAS RETURNED TO SERVICE. (K) 2L72 4T4 TRTA24CE E26NE 20050330001892005033000189NM 2005 3 30 72300099 120050323A5340 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 2 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050330001972005033000197NM 2005 3 30 72300091 120050328A5340 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 6 X 1 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050330002022005033000202SO 2005 3 30 LR7A05033 120050306A5311 FRAME LKHEED382 382G 526414USO FUSELAGE MISDRILLED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2850 4763 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED / MIS-DRILLED FUSELAGE LINER HOLES AT FS 732, WL 148, LBL 65. REPAIRED IAW LAC MEA 382-53-04-074 R1. 2H74 4T A1SO 20050330002032005033000203SO 2005 3 30 LR7A05032 120050306A5311 FRAME LKHEED382 382G 526414USO FUSELAGE MISDRILLED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2850 4763 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED / MIS-DRILLED FUSELAGE LINER HOLES AT FS 702, WL 148, LBL 65. REPAIRED IAW LAC MEA 382-53-04-074 R1. 2H74 4T A1SO 20050330002082005033000208SO 2005 3 30 LR7A05027 120050306A5311 FRAME LKHEED382 382G 526414USO FS MISDRILLED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2850 4763 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED / MIS-DRILLED FUSELAGE LINER HOLES AT FS 291, WL 148, RBL 65. REPAIRED IAW LAC MEA 382-53-04-074 R1. 2H74 4T A1SO 20050330002092005033000209SO 2005 3 30 LR7A05026 120050306A5311 FRAME LKHEED382 382G 526414USO FUSELAGE MISDRILLED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2850 4763 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED / MIS-DRILLED FUSELAGE LINER HOLES AT FS 283, WL 148, LBL 65 & RBL 65. REPAIRED IAW LAC MEA 382-53-04-074 R1. 2H74 4T A1SO 20050330002122005033000212SO 2005 3 30 LR7A05023 120050306A5311 FRAME LKHEED382 382G 526414USO FUSELAGE MISDRILLED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2850 4763 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED / MIS-DRILLED FUSELAGE LINER HOLES AT FS 787 WL 178 AND 205, RBL 77. REPAIRED IAW LAC MEA 382-53-04-073 R1. 2H74 4T A1SO 20050330002222005033000222SO 2005 3 30 LR7A05013 120050306A5312 BULKHEAD LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2850 4763 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND AFT FUSELAGE RT BULKHEAD INBOARD CAP & WEB CRACKED AT FS 1012, WL 260, RBL 62. WEB & CAP REPLACED IAW SRM SMP 583 CHP 51-60 & 51-70. 2H74 4T A1SO 20050330002252005033000225SO 2005 3 30 LR7A05010 120050306A5553344101L FITTING LKHEED382 382G 526414USO HORIZONTAL STAB GOUGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2850 4763 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5511 FOUND VERTICAL STAB ATTACH TO HORIZONTAL STAB FITTING MAIN BOLT HOLE WITH THREAD TYPE GOUGES AT FS 1043, WL 287, LBL 15. REPLACED FITTING IAW SRM SMP583 CHP 51-60 & 51-70. 2H74 4T A1SO 20050330002272005033000227SO 2005 3 30 LR7A05008 120050306A5320 STIFFENER LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2850 4763 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND AFT FUSELAGE CARGO COMP STIFFENER EDGE CRACKED AT LT FS 940 WL 280 LBL 16-18. REPLACED STIFFENER IAW SRM SMP 583 CHP 51-60 & 51-70. 2H74 4T A1SO 20050330002362005033000236NM 2005 3 30 EIA2005036 120050222A5314 KEELBEAM BOEING747 747SR46 1384816NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09478EV 21033 BS 1360 KEEL BEAM LWR ANGLE UPPER SURFACE CORROSION WL 95, LBL 10. CORROSION REMOVED PER SRM 53-10-01, FABBED AND INSTALLED REPAIR PER SRM 51-10-01 AND 51-30-02. 2L74 4F RTA20WE 20050331000592005033100059EA 2005 3 31 COMA0560208 120050328A3097 LEAD CNDAIRCL600 CL6002B19 1900309EA WINDOW HEAT FAILED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01812CA 7381 FLIGHT 5480 RECEIVED A LEFT WINDOW HEAT CAUTION DURING CLIMBOUT OF HSV, AIRCRAFT RETURNED TO THE FIELD. CONNECTED WINDOW ELECTRICAL LEADS TO SPARE TERMINALS. 2L72 4F RTA21EA 20050331000642005033100064EA 2005 3 31 COMA0560211 120050325A2621365000183 FIRE BOTTLE CNDAIRCL600 CL6002B19 1900309EA AFT CARGO LOW A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01487CA6452 7729 FLIGHT 5360 DURING CLIMBOUT OF MCO RECEIVED A CARGO FIRE EXTINGUISHING BOTTLE LOW PRESSURE CAUTION, AIRCRAFT RETURNED TO THE FIELD. REPLACED THE CARGO FIRE EXTINGUISHER CONTAINER. 2L72 4F RTA21EA 20050331000792005033100079WP 2005 3 31 DHL2005805639 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT Z-FRAME INBOARD FLANGE HOLES (2EA) MISDRILLED AT STA 1140.000 L-12L L-13L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-05-05 EO AST 050205 DATE 02-21-05. CLEANED, TREATED AND PRIMED (AREA) MISDRILLED HOLES IAW SRM 51-1-8B. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD6-4) IAW EO AST 050205 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050331000842005033100084WP 2005 3 31 DHL2005805678 120050324A7830 STIFFENER DOUG DC8 DC873F 302199FWP THRUST REVERSER CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 NR 1 ENG LT T/R EXTERIOR STIFFENER CRACKED 0.500 STA YN 210.000, 12 O'CLOCK POSITION (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS FROM REPAIR AREA IAW CFM 56 MM 70-43-33 SRM 51-1-20D PG 21. STOP DRILLED CRACK IAW EO AST050221. PERFORMED NDT INSP OF AREA IAW NDT SPM PART 06-10-01-001. FABRICATED STIFFENER (AMS40412024AV4G1-T351) NEW ANGLE (301 1/4H 0.080) AND REPAIR DOUBLER (301 1/4H 0.080) IAW EO AST 050221. NDT INSPECTED STIFFENER IAW NDT SPM PART 08-00-02-07. CLEANED, TREATED AND PRIMED AREA AND ANODIZER REPAIR PARTS IAW CFM 56 MM 70-61-31. INSTALLED REPAIR PARTS IAW EO AST 050221 SRM 51-1-20D PG 9. TORQUED IAW SRM 51-3-1. PERFORMED CHECK OUT IAW DC8-70 MM 78-00 PAR 3B PG 202, GOOD. 2L74 4F RT4A25 20050331000902005033100090WP 2005 3 31 DHL2005805672 120050321A5730 DOUBLER DOUG DC8 DC873F 302199FWP RT WING DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 RT WING CTR L/E OUTBOARD SLOT VANE EXISTING DOUBLER EDGE DISTANCE AND FASTENERS HOLES SPACE NOT ALLOWABLE, STA XOLDO 67.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-16-05 DWG X83-R03 REV IR DATED 02-24-05. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. CUT OUT DAMAGED SECTION IAW DWG X83-R03. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01.001. FABRICATED REPAIR DOUBLER (AL7075T6 0.071) INTERNAL DOUBLER (AL7075-T6 0.050) AND FILLER (AL7075T6 0.063) IAW DWG X83-R03. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW DWG X83-R03 SRM 51-1-21 PG 1, SRM 51-1-20D PG 9, SRM 51-3-0 PG 1. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050331000982005033100098EA 2005 3 31 SWIA200514788 120050322A2750860D10018 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED LDLANDING 1 NM07597SW 7293 FLAP FAIL AFTER LANDING. REPLACED FECU WITH SERVICEABLE UNIT IAW CRJ MM 27-51-05. 2L72 4F RTA21EA 20050331001082005033100108WP 2005 3 31 DHL2005805654 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME HOLES (2EA) MISDRILLED STA 879.000 L-10R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 02-25-05 EO AST 050203 DATE 02-18-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD6-4) IAW EO AST 050203 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050331001192005033100119WP 2005 3 31 DHL2005805667 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME (2EA) MISDRILLED HOLES AT STA 520.000 L-10L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-05-05 EO AST 050205 DATE 02-21-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD5-5) IAW EO AST 050205 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050331001202005033100120WP 2005 3 31 DHL2005805640 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME (2EA) MISDRILLED HOLES AT STA 520.000 L-10R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-07-05 EO AST 050201 DATED 02-17-05. PERFORMED DETAIL VISUAL INSPECTION, NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO AST050201 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050401000072005040100007NE 2005 4 1 M7K2005F00001 220050316A7230 COMPRESSOR UROCOPEC130 EC130B4 8680989EU TMECA ARRIELARRIEL2B NE ENGINE SEIZED E M7KAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP19803MH 3735 23036 PILOT EXPERIENCED FLICKERING ENGINE CHIP LIGHT IN CRUISE FLIGHT AND AS A PRECAUTION PREPARED TO LAND AT FIRST SUITABLE LOCATION. ON APPROACH TO LANDING, CHIP LIGHT CAME ON STEADY AND COMPRESSOR STALL OCCURRED. SOME ROTOR SPEED DROP OCCURRED WITH LOW ROTOR WARNING SOUNDING IN THE PILOT HEADSET. AIRCRAFT WAS LANDED WITHOUT INCIDENT. ENGINE CONTINUED RUNNING UNTIL INCIDENT. ENGINE CONTINUED RUNNING UNTIL THROTTLE WAS SHUT DOWN WHEN GAS PRODUCER SPEED DECAYED, RAPIDLY. COMPRESSOR FOUND LOCKED UP. ENGINE RETURNED TO MFG FOR REPAIR. (WP19200505750) (K) 1G72 3U3 U H9EU E00054EN 20050401000092005040100009 2005 4 1 KBM2005F00044 420050314A34225050031904 GYRO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE DIRECTIONAL MALFUNCTIONED E KBMAO OTHER O OTHER CRCRUISE 1 WP19351WM227 2167 DIRECTIONAL GYRO SPINS IN FLIGHT, WILL NOT HOLD CONSTANT HEADING. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050401000322005040100032EA 2005 4 1 A6WA200540098 120050315A53206013501251 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31415AW 7593 LT SIDE FS621-FS625.3 INTERCOSTAL AT STR 14L IS CRACKED NEAR RADIUS, APPROX .70 INCH. INSTALLED NEW LT INTERCOSTAL AT FS 621-625.3, STR 14L IAW BRAS EO 601R-53-6157. (K) 2L72 4F4 FRTA21EA E15NE 20050401000422005040100042NM 2005 4 1 USAA050345 120050307A5340 ANGLE BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19442US40275 24841 CLT - Q6 - ANGLE, .025 INCH CRACK, STATION 500G-520 BL0. REPLACED WITH FABRICATED PART IAW SRM 51-30-01, DWG NR 69-35365, AND SRM 51-10-02. (K) 2L72 4F4 FRTA16WE E21EU 20050401000702005040100070NM 2005 4 1 USAA050348 120050307A5344 HINGE BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE SERVICE DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19390US54352 23312 CLT - UNSCHED - HINGE CASTING, 1 INCH X 1 INCH CRACK, LT AFT SERVICE DOOR HINGE BOX. (K) 2L72 4F4 FRTA16WE E2GL 20050404000162005040400016EA 2005 4 4 O2G2005F00005 120050310A326055022 PROXIMITY SWITCH CNDAIRCL600 CL6002B16 1900305EA GE CF34 CF34* NE MLG FAILED E O2GAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NE03601VH4633 5043 WOW INPUT FAIL ANNUNCIATOR CAME ON AFTER TAKEOFF. REPLACED LT NOSE AND LT MAIN LANDING GEAR OB PROXIMITY SWITCH. (NE03200506802) (K) 2L72 4F4 FRTA21EA E15NE 20050404000702005040400070NM 2005 4 4 USAA050350 120050310A5330 SKIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19442US 24841 CLT - Q6 - SKIN, 2.25 INCH X 7 INCH, PREVIOUS REPAIR, SCAB PATCH, STATION 178, STRINGER 17L. SPLICE STRAP INSTALLED IAW EO 5300V157. (K) 2L72 4F4 FRTA16WE E21EU 20050404001012005040400101CE 2005 4 4 MXI2005F00000 120050223A32314IENI6 SWITCH BEECH MU300 400A 1155402CE PWA JT15 JT15* 52060NE GEAR DOOR FAILED E MXIAO OTHER J WARNING INDICATION LDLANDING 1 EA21141DR RK184 THE LANDING GEAR WOULD NOT EXTEND WITH GEAR HANDLE DOWN. GEAR WAS LOWERED USING THE MANUAL EMERGENCY EXTENSION AND THE GEAR DOORS WERE CLOSED USING THE PNEUMATIC GEAR BOTTLE. PROBABLE CAUSE WAS THE HIGH RESISTANCE IN THIS SWITCH AND THE GEAR DOOR CLOSED SWITCH. (K) (EA21200504860) 2H72 4F4 TRTA16SW E1NE 20050404001172005040400117WP 2005 4 4 DHL2005805645 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBOARD FLANGE (2EA) MISDRILLED HOLE, STA 100.000 L-19R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-07-05 EO AST 050201 DATE 02-17-05. PERFORMED DETAIL VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA AT STA 100.000 L-19R IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO AST 050201 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050404001192005040400119WP 2005 4 4 DHL2005805603 120050320A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME HOLE MISDRILLED STA 660.000 BETWEEN L-12 AND L-13L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-15-05 EO AST 050211 DATE 02-24-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED AREA (MISDRILLED HOLE) IAW SRM 51-1-8B. FABRICATED DOUBLER ANGLE (7075.0.0125) IAW EO AST 050211 SRM 51-1-4 PAGE 1. PERFORMED HEAT TREATMENT IAW SRM 51-1-1 PAGE 1, 13, 17. CLEANED, TREATED AND PRIMED NEW DOUBLER ANGLE IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (NAS1097AD) IAW EO AST 050211 SRM 51-1-21 PAGE 1. INSTALLED DOUBLER ANGLE WITH RIVETS (MS20470AD) IAW EO AST 050211 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050404001222005040400122WP 2005 4 4 DHL2005805562 120050320A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT CLIP FRAME HOLES (3EA) MISDRILLED AT STA 960.000 L-13R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-13-05, EO AST 050220 DATE 03-08-05. REMOVED DAMAGED CLIP IAW SRM 51-1-21 PAGE 1. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. FABRICATED NEW CLIP (AL7075-T6 0.063) IAW EO AST 050220. CLEANED, TREATED AND PRIMED AREA AND NEW CLIP IAW SRM 51-1-8B. INSTALLED NEW CLIP IAW EO AST 050220, SRM 51-1-21 PAGE 1 (MS20470AD). 2L74 4F RT4A25 20050404001252005040400125WP 2005 4 4 DHL2005805601 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBOARD FLANGE (2EA) MISDRILLED HOLES AT STA 1040.000 L-10R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-07-05 EO AST 050201 DATED 02-17-05. PERFORMED DETAIL VISUAL INSPECTION NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO AST 050201, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050404001352005040400135WP 2005 4 4 DHL2005805584 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CABIN INTERIOR FRAME INBOARD FLANGE HOLES (2EA) MISDRILLED AT STA 1240.000 L-10R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 02-25-05, EO AST 050203 DATE 02-18-05. PERFORMED DETAILED VISUAL INSPECTION, NO CRACK FOUND. CLEANED, TREATED AND PRIMED AREA (MISDRILLED HOLES) IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO AST 050203, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050404001392005040400139WP 2005 4 4 DHL2005805533 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT INBOARD FLANGE Z-FRAME HOLES (3EA) MISDRILLED AT STA 300.000 L-11L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-05-05 EO AST 050205 DATE 02-21-05. CLEANED, TREATED AND PRIMED (AREA) MISDRILLED HOLES IAW SRM 51-1-8B. PERFORMED VISUAL INSPECTION (DETAILED). NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD5-6) IAW EO AST 050205. 2L74 4F RT4A25 20050404001472005040400147NM 2005 4 4 2005UALA00258 120050323A2613 WIRE BOEING757 757222 1384956NM PWA 2037 PW2037 NE OVERHEAT LOOP DAMAGED A UALAB EMER. DESCENT J WARNING INDICATION DEDESCENT 1 WP29537UA 25157 LANDED UNDER AMBER ALERT DUE TO NR 2 ENGINE OIL FILTER BYPASS LIGHT. DETECTED A BROKEN SHIELD WIRE AT OIL FILTER SWITCH CONNECTOR. RETURNED TO ORD DUE TO NR 2 ENGINE OVERHEATED AND SHUTDOWN. SUPPLEMENTAL DATA UPDATE CREW REPORTED NR 2 ENGINE OVERHEAT INDICATION AT CLIMB. CREW SHUT DOWN NR 2 ENGINE PER QRC. PERFORMED TROUBLESHOOTING OF THE OVERHEAT DETECTION SYSTEM. FOUND NR 2 ENGINE CORE DETECTOR M1122, LOOPS A & B WITH LOW RESISTANCE SHORT TO GROUND. REMOVED AND REPLACED OVERHEAT DETECTOR CORE LOOPS A & B. ENGINE OVERHEAT DETECTION SYSTEM TESTED NORMAL. REPAIRED SHIELD WIRE. REPLACED OIL FILTER AND DIFFERENTIAL PRESSURE SWITCH. 2L72 4F4 FRTA2NM E17NE 20050404001562005040400156EU 2005 4 4 05FDEA00638 120050325A5730A57350005201 SKIN AIRBUS310 A310203 3930313EU ZONE 600 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25401FE 191 PANEL LAND AT 650GB HAS 12 EA ELONGATED HOLES. REPAIRED 8 EA HOLES IAW A310-200 SRM 51-40-44 FIG 1. COMPLIED WITH EA 6-5710-87184 BY INSTALLING 4 EA REPAIR BUSHINGS FOR REMAINING 4 HOLES. 2L72 4F RTA35EU 20050404001572005040400157EU 2005 4 4 05FDEA00639 120050325A5730A57350005200 SKIN AIRBUS310 A310203 3930313EU ZONE 500 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25401FE 191 PANEL LAND AT 550 HB HAS 4 EA ELONGATED HOLES. REPAIRED 1 EA HOLE IAW A310-200 51-40-44 FIG 1. COMPLIED WITH EA 6-5710-87184 BY INSTALLING 3 EA REPAIR BUSHINGS FOR REMAINING 3 HOLES. 2L72 4F RTA35EU 20050404001582005040400158EU 2005 4 4 05FDEA00640 120050325A5730A57350005200 SKIN AIRBUS310 A310203 3930313EU ZONE 500 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25401FE 191 PANEL LAND AT 550 GB HAS 5 EA ELONGATED HOLES. REPAIRED 3 EA HOLES IAW A310-200 SRM 51-40-44 FIG 1. COMPLIED WITH EA 6-5710-87184 BY INSTALLING 1 EA REPAIR BUSHING FOR REMAINING HOLE. 2L72 4F RTA35EU 20050404001592005040400159EU 2005 4 4 05FDEA00666 120050328A5313 STRINGER AIRBUS310 A310222 3930315EU FUSLEAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 REPAIR NEEDS EVALUATION FOR FAA APPROVED DATA AND MAJOR OR MINOR CLASSIFICATION. TAIL CONE DOUBLER LT SIDE AT FR 102. ITEM 34 OF LIST. REMOVED FABRICATED AND REPLACED STRINGER. REMOVED AND FABRICATED NEW SKIN DOUBLER. REPAIRED BUTT JOINT PER A310 SRM 51-40-21, SRM 53-19-12, SRM 51-71-40, ALODINED, PRIMED AND TOP COATED PER A310 SRM 51-75-10. REPAIR IS CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100. 2L72 4F RTA35EU 20050404001602005040400160EU 2005 4 4 05FDEA00667 120050328A5313 LONGERON AIRBUS310 A310222 3930315EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 MAIN DECK CARGO FR12 STA 1067 LONGERON 2ND FROM CENTER IS CORRODED. REMOVED CORROSION IAW A310 SRM 53-10-00. REMOVED & REPLACED DAMAGED SECTION IAW A310 SRM 51-72-10. 2L72 4F RTA35EU 20050404001612005040400161EU 2005 4 4 05FDEA00668 120050328A5310 STRUCTURE AIRBUS310 A310222 3930315EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 BETWEEN FRAME 91 AND 95 (AFT OF THS BOX) BILGE AREA AND AROUND ACCESS THRESHOLD 300 SQ INCHES OF BARE METAL WITH LITE SURFACE CORROISION. REMOVED AND REPLACED CORRODED STRUCTURE AT FR91 TO 95 AND STR 16 LT IAW A310 SRM 51-40-21 AND DWG'S A53989325, A53989300, A53989559, A53989330, A53986001. 2L72 4F RTA35EU 20050404001652005040400165NM 2005 4 4 05FDEA00661 120050328A2612 WARNING LIGHT BOEING727 727200 138407ENM CARGO SMOKE ILLUMINATED A FDEAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO25258FE 20940 LOWER CARGO SMOKE LIGHT ILLUMINATED ON T/O 70 KTS. RTO, NO OTHER INDICATIONS, LIGHT WENT OUT DURING DECELERATION. MEL 26MAR05, RELEASED FOR SERVICE PER MEL/CDL: 26-19-C CATEGORY: C EXPIRATION: 05APR05 MEL 26-19-C: SMOKE DETECTION IN THE AFT LOWER CARGO COMPARTMENT INOP. OHMED AND MEGGED WIRING TO THE FWD LIGHT L9109 TO THE CONTROL PANEL REF 727-200 WDM 26-23-00, ALL CKS GOOD. CHECKED THE LIGHT SOCKET, CHECKS GOOD. REMOVED AND REPLACED CSCP, OPS CKS GOOD PER 727-200 M/M 26-17-001-5. OK FOR SERVICE. 2L73 4F RTA3WE 20050404001662005040400166EA 2005 4 4 MASA200500214 120050313A79304120T17P02 PRESSURE SWITCH CNDAIRCL600 CL6002D24 1390016EA GE CF34 CF348C1 NE NR 1 ENGINE INOPERATIVE A MASAED ENGINE SHUTDOWN RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW07927LR360 15027 194259 RETURNED TO GATE FOR LEFT ENGINE OIL PRESSURE WARNING MESSAGE UPON ENGINE START. PILOT DID SHUT THE ENGINE DOWN AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE PRESSURE SWITCH AND IT OPS CHECKED GOOD. 2L72 4F4 FRTA21EA EOOO63EN 20050404001692005040400169NM 2005 4 4 05FDEA00648 120050327A5712ARB2850505 RIB DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 LT WING NR 16 SLAT TRACK INBOARD RIB FOUND CRACKED. REMOVED AND REPLACED WITH NEW RIB IAW SRM 51-33-01 VOLUME II. 2L73 4F RTA22WE 20050404001702005040400170NM 2005 4 4 05FDEA00649 120050327A5712ARB2850506 RIB DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 RT WING NR 16 SLAT TRACK INBOARD RIB FOUND CRACKED. REMOVED AND REPLACED WITH NEW RIB AS PER SRM 51-33-01 VOLUME II. 2L73 4F RTA22WE 20050404001712005040400171CE 2005 4 4 DJFA2005072 120050326A3260 BULB CESSNA525 525 2076601CE MLG INDCATOR INOPERATIVE E DJFAO OTHER P NO WARNING INDICATION LDLANDING 1 EA23226CW 5250326 CREW DID NOT RECEIVE A LEFT MAIN GEAR DOWNLOCK INDICATION AFTER GEAR EXTENSION. AN EMERGENCY GEAR EXTENSION WAS PERFORMED BY BLOWING THE GEAR DOWN. THE AIRCRAFT LANDED IN MYAT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT MAIN GEAR LIGHT BULB AND SERVICED THE EMERGENCY GEAR AND BRAKE PNEUMATIC BOTTLE. A GEAR SWING WAS PERFORMED AND OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 1L72 4F RTA1WI 20050404001722005040400172NM 2005 4 4 AWXA200500371 120050324A534069353501 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 MCN - MAJOR REPAIR - DURING C-16 CHECK A .375 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT BS 520, STR 15 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 520, STR 15 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-35330; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050404001732005040400173NM 2005 4 4 AWXA200500372 120050303A532269730575 SHEAR TIE BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 MCN - MAJOR REPAIR - DURING C-16 CHECK A .3125 INCH CRACK WAS FOUND IN SHEAR TIE AFT OF BS 500D, ABOVE STR 13 LT. MAINTENANCE REMOVED CRACKED SHEAR TIE AT BS 500D, STR 13 LT; FABRICATED A NEW REPLACEMENT SHEAR TIE PER DWG 69-73057; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050404001742005040400174NM 2005 4 4 AWXA200500373 120050301A531165479602 FRAME BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 MCN - MAJOR REPAIR - DURING C-16 CHECK GALVANIC CORROSION WAS FOUND ON FORWARD AND AFT SIDE OF FRAME AT BS 847 BETWEEN STR 25 RT AND STR 26 RT. MAINTENANCE BLENDED OUT CORROSION ON FRAME AND PERFORMED HFEC INSPECTION OF EXISTING HOLES COMMON TO REPAIR. REMOVED AND REPLACED LOWER SILL WEB AND CLIP; FABRICATED A REPAIR ANGLE PER DWG 65-47960; INSTALLED REPAIR PARTS IAW ER 03-5362-05083-ES1. 2L72 4F RTA16WE 20050404001762005040400176EU 2005 4 4 AWXA200500375 120050325A3250 SERVO AIRBUS320 A320231 3930325EU NLG STEERING MALFUNCTIONED A AWXAO OTHER J WARNING INDICATION APAPPROACH 1 WP28633AW 082 ON APPROACH INTO PHX EN ROUTE FROM ATL RECEIVED ECAM MESSAGE FOR NOSE WHEEL STEERING FAULT, DECLARED EMERGENCY AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE FOUND THE CENTRALIZED FAULT DISPLAY SYSTEM FAULTED BOTH BRAKE STEERING CONTROL UNIT CHANNELS FOR NLG SERVO CONTROL UNIT (6GC). DISCONNECTED AND RESET CONNECTOR AT NLG SERVO CONTROL UNIT (6GC), FAULT CLEARED AND DID NOT RETURN. REMOVED AND REPLACED NLG SERVO CONTROL UNIT (6GC) IAW AMM 32-51-51-04, LEAK AND OPERATIONAL CHECKS WERE GOOD. FUNCTIONAL TEST OF NLG SERVO CONTROL UNIT S/N U416 CONFIRMED REASON FOR REMOVAL, UNIT FAILED VOLTAGE BALANCE TEST, REPLACED SERVO VALVE PER CMM 32-57-01, REV. 8. 2L72 4F RTA28NM 20050404001772005040400177EU 2005 4 4 05FDEA00510 120050314A5320 PANEL AIRBUS310 A310222 3930315EU CARGO BAY CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 BULK CARGO CEILING PANEL SUPPORT CENTER BETWEEN FRAMES 65 AND 66 HAS SEVERE EXFOLIATED CORROSION FROM END, BACK 6 INCHES. REMOVED STRAP IAW A310-200 SRM 50-40-21. REPLACED STRAP FOR CEILING PANEL SUPPORT IAW A310-200 SRM 50-40-21. 2L72 4F RTA35EU 20050404001832005040400183SO 2005 4 4 SWIA200514767 120050207A5320 FLOOR SUPPORT EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0758733 120197 LEFT OMEGA BEAM AT FR 44 IS CORRODED UNDERNEATH AROUND A/NUTS AT YL479.0. ITEM FOUND AT C-CHECK INSPECTION. BUTT STRAP REPLACED AND OMEGA BEAM REPLACED IAW EMB 120 SRM 51-40-02, 51-25-00, 51-22-00. 2L72 4T RTA31SO 20050404001912005040400191NM 2005 4 4 SWAA050752 120050310A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 375, STR 26L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050404001922005040400192NE 2005 4 4 MALA050231 220050128A7200 ENGINE BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE NR 1 FAILED A MALAE ENGINE SHUTDOWN J WARNING INDICATION NRNOT REPORTED 1 GL15524XJ E2349 NR 1 ENGINE FAILED IN FLIGHT, HEARD A LOUD BANG, ENGINE SHUT DOWN. THE AIRCRAFT WAS INSPECTED IAW THE MESABA REQUIREMENT AS LISTED ON THE 3 ENGINE FERRY 02 TASK CARD AND WAS FOUND TO BE SAFE FOR THE INTENDED FERRY FLIGHT FROM DTW TO MSP. APU MUST BE RUNNING WITH APU GEN SW ON TO APU AIR SELECTED OFF. FLIGHT RESTRICTED TO 25,000 FT. 2H74 4F4 FRTA49EU E6NE 20050404001942005040400194EA 2005 4 4 ASOA05203 120050305A5712 RIB CNDAIRCL600 CL6002B19 1900309EA RT WING CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27904EV 7628 DURING A C-CHECK IN MCN, THE RIGHT BATT RIB ASSEMBLY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE RIGHT BATT RIB ASSEMBLY AT WS 53.60 IAW ASA EO 600-57-039A. (M) 2L72 4F RTA21EA 20050404001972005040400197EA 2005 4 4 ASOA05212 120050307A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27904EV 7628 DURING A C-CHECK IN MCN, THE FS 484 ANGLES AT LBL 36 AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FS 484 ANGLES AT LBL 36 AND RBL 36 IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20050404001992005040400199WP 2005 4 4 ASAA0580085 120050207A532199365811 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE FRAYED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02960AS 53074 OKC - DURING C-CHECK, FOUND CABIN FLOORBOARD PANEL IS FRAYING. FIBERGLASS OVERLAY REPAIRED. (M) 2L72 4F RTA6WE 20050404002002005040400200EA 2005 4 4 ASOA05219 120050304A2910 HYDRAULIC SYSTEM CNDAIRCL600 CL6002B19 1900309EA NR 1 LEAKING A ASOAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO27867AS 7463 DURING CRUISE FROM ATL-FNT, THE CREW NOTICED THE NR 1 HYDRAULIC SYSTEM QUANTITY HAD FALLEN TO 45 PERCENT. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT DIVERTED TO CVG AND LANDED SAFELY. MAINTENANCE INSPECTED AND SERVICED THE NR 1 HYDRAULIC SYSTEM. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050405000012005040500001EA 2005 4 5 ASOA05200 120050304A5210601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27835AS 7258 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR TOP STEP WAS FOUND CRACKED AT THE OUTBOARD FORWARD AND AFT CORNERS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR TOP STEP. OPERATIONAL CHECKS GOOD. (M) 2L72 4F RTA21EA 20050405000022005040500002EU 2005 4 5 ASOA05196 120050207A5320 STRUCTURE AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27633AS 344 DURING A C-CHECK IN YUL, THE OUTER CHORD AT FRAME 14 LEFT WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE OUTER CHORD AT FRAME 14 LEFT IAW SRM 51-25-04. (M) 2H72 4T RTA53EU 20050405000032005040500003WP 2005 4 5 ASAA0580097 120050215A53305936434501 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02943AS 53018 OKC - DURING C-CHECK, FUSELAGE SKIN DENTED. REMOVED DAMAGED AREA. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050405000092005040500009WP 2005 4 5 ASAA0580084 120050207A53219936651505 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02960AS 53074 OKC - DURING C-CHECK, FOUND CABIN FLOORBOARD PANEL IS FRAYING. FIBERGLASS OVERLAY REPAIRED. (M) 2L72 4F RTA6WE 20050405000102005040500010WP 2005 4 5 ASAA0580093 120050215A533059114013 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02943AS 53018 OKC - DURING C-CHECK, FOUND FUSELAGE SKIN DENTED. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLER AND DOUBLER. (M) 2L72 4F RTA6WE 20050405000112005040500011EU 2005 4 5 ASOA05198 120050214A5720 WEB AEROSPATR72 ATR72212 8680945EU WING CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27633AS 344 DURING A C-CHECK IN YUL, THE WEB IN WING BOX FRAME 28 RIGHT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE WEB IN THE WING BOX FRAME 28 RT IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20050405000142005040500014EA 2005 4 5 ASOA05199 120050304A27501104SD100101 DRIVE SHAFT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS DAMAGED A ASOAO OTHER J WARNING INDICATION APAPPROACH 1 SO27909EV 7658 FLT 4571 - DURING APPROACH INTO YUL FROM ATL, UPON SELECTING THE FLAPS TO EIGHT DEGREES A FLAP FAIL CAUTION MESSAGE WAS RECEIVED WITHT THE FLAP INDICATOR SHOWING ZERO DEGREES. THE QRH WAS COMPLIED WITH AND THE CREW REQUESTED EMERGENCY VEHICLES TO BE ROLLED AS A PRECAUTION. A ZERO FLAP LANDING WAS ACCOMPLISHED WITH THE AIRCRAFT LANDING SAFELY. MAINTENANCE INSPECTED THE FLAPS AND RESET THE FLAPS SYSTEM IAW ASA EO 600-27-0004. NO DEFECTS WERE NOTED AND SYSTEM OPERATIONS WERE GOOD. UPON FURTHER INSPECTION MAINTENANCE FOUND THE LEFT AND RIGHT NR 1 AND THE RIGHT NR 4 FLEX SHAFTS DAMAGED. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT NR 1 AND THE RIGHT NR 4 FLEX SHAFTS. OPERATIONAL CHECKS GOOD. AIRCRAFT 2L72 4F RTA21EA 20050405000212005040500021WP 2005 4 5 ASAA0580047 120050131A532199366881 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DEBONDED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - DURING C-CHECK, PAX CABIN FLOOR PANEL HAS SOFT, DISBONDING SPOT. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050405000232005040500023WP 2005 4 5 ASAA0580069 120050131A52305936038501 BEAM DOUG DC9 DC983 3022083WP CARGO DOOR CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - DURING C-CHECK, FOUND AFT CARGO BAY DOOR BEAM IS CORRODED. REPLACED BEAM. (M) 2L72 4F RTA6WE 20050405000252005040500025WP 2005 4 5 ASAA0580082 120050131A5712993751735 RIB DOUG DC9 DC983 3022083WP LT WING CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - DURING C-CHECK, LT WING FIXED LEADING EDGE RIB LOWER L-ANGLE IS CRACKED. REPLACED ANGLE. (M) 2L72 4F RTA6WE 20050405000262005040500026WP 2005 4 5 ASAA0580056 120050131A532199366401 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - C-CHECK, PAX CABIN FLOOR PANEL DENTED, GOUGED, AND DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050405000282005040500028WP 2005 4 5 ASAA0580083 120050207A532199365811 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE FRAYED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02960AS 53074 OKC - DURING C-CHECK, FOUND CABIN FLOORBOARD PANEL IS FRAYING. FIBERGLASS OVERLAY REPAIRED. (M) 2L72 4F RTA6WE 20050405000362005040500036WP 2005 4 5 ASAA0580080 120050131A573059304953 SKIN DOUG DC9 DC983 3022083WP LT WING GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - DURING C-CHECK, FOUND LEFT WING OUTBOARD FLAP VANE LEADING EDGE IS GOUGED. REMOVED DAMAEGD AREA. INSTALLED REPAIR FILLER AND DOUBLER. (M) 2L72 4F RTA6WE 20050405000382005040500038WP 2005 4 5 ASAA0580081 120050131A533059360001 SKIN DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - DURING C-CHECK, FOUND FUSELAGE SKIN CORRODED AND PITTED ON INSIDE JUST ABOVE LONGERON 3L. REMOVED DAMAGED AREA. INSTALLED REPAIR FILLER, DOUBLER, AND FINER DOUBLER. (M) 2L72 4F RTA6WE 20050405000392005040500039WP 2005 4 5 ASAA0580062 120050131A532199365841 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - DURING C-CHECK, PAX CABIN FLOOR PANEL IS PUNCTURED. CORE PLUG REPAIRED. (M) 2L72 4F RTA6WE 20050405000402005040500040WP 2005 4 5 ASAA0580078 120050131A53205910082 WEB DOUG DC9 DC983 3022083WP FUSLEAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - FOUND DURING C-CHECK, L1 DOOR CUTOUT INNER WEB IS CRACKED. REMOVED DAMAGED AREA. INSTALLED REPAIR FILLER AND DOUBLER. (M) 2L72 4F RTA6WE 20050405000412005040500041WP 2005 4 5 ASAA0580067 120050131A5320993055812 CUSP WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - DURING C-CHECK, LONGERON CUSP WEB CORRODED IN MID CARGO BAY. REMOVED DAMAGE. INSTALLED FILLER AND REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050405000432005040500043WP 2005 4 5 ASAA0580061 120050131A53219936640501 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - DURING C-CHECK, PAX CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050405000442005040500044WP 2005 4 5 ASAA0580064 120050131A532059364423 CUSP WEB DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - DURING C-CHECK, LONGERON CUSP WEB CRACKED IN MID CARGO BAY. STOP DRILLED CRACK. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050405000452005040500045WP 2005 4 5 ASAA0580070 120050131A53205936443 WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - DURING C-CHECK, FOUND LONGERON STRAP (WEB) CORRODED IN AFT CARGO BAY. REMOVED DAMAGE. TREATED/PRIMED PER EA 5310-02444. (M) 2L72 4F RTA6WE 20050405000482005040500048WP 2005 4 5 ASAA0580073 120050131A534039364741 SPLICE DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - DURING C-CHECK, FOUND LONGERON STRINGER SPLICE CORRODED. REPLACED SPLICE. (M) 2L72 4F RTA6WE 20050405000502005040500050WP 2005 4 5 ASAA0580059 120050131A532199365831 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - FOUND DURING C-CHECK, PAX CABIN FLOOR PANEL IS CRACKED, PUNCTURED, AND DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050405000522005040500052WP 2005 4 5 ASAA0580058 120050131A532199365831 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - DURING C-CHECK, PAX CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050405000572005040500057WP 2005 4 5 ASAA0580051 120050131A53219936537503 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE BROKEN A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - DURING C-CHECK, PAX CABIN FLOOR PANEL HAS CORRODED AND BROKEN INSERTS. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050405000602005040500060WP 2005 4 5 ASAA0580045 120050131A532199366391 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - C-CHECK, PAX CABIN FLOOR PANEL HAS PULLED STRANDS OF FIBERGLASS. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050405000652005040500065WP 2005 4 5 ASAA0580053 120050131A532199579212 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - DURING C-CHECK, PAX CABIN FLOOR PANEL HAS ELONGATED HOLE. INSTALLED REPAIR FILLER AND DOUBLER HAT SECTION AND SPLICE. (M) 2L72 4F RTA6WE 20050405000662005040500066EU 2005 4 5 ASOA05215 120050228A5714 DOUBLER AEROSPATR72 ATR72212 8680945EU WING BOX CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27530AS 453 DURING A C-CHECK IN YUL, THE DOUBLER IN THE WING BOX AT FRAME 28A LT WAS FOUND CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE DOUBLER IN THE WING BOX AT FRAME 28A LT IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20050405000702005040500070EA 2005 4 5 ASOA05208 120050305A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27880AS 7606 DURING A C-CHECK IN MCN, THE ENGINE SUPPORT BEAM AT BL 36.20 RT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE ENGINE SUPPORT BEAM AT BL 36.20 RT IAW ASA EO 600-53-0070. (M) 2L72 4F RTA21EA 20050405000732005040500073EA 2005 4 5 ASOA05083 120050131A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27848AS 7339 DURING HANGAR MAINTENANCE IN BTR, THE ENGINE SUPPORT BEAM AT BL 36.20 RT AT THE RIGHT ACCESS PANEL WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE PERFORMED THE PERMANENT REPAIR TO THE ENGINE SUPPORT BEAM AT BL 36.20 RT AT THE RIGHT ACCESS IAW ASA EO 600-53-0070 AND ASA EO 600-53-0234. (M) 2L72 4F RTA21EA 20050405000742005040500074EU 2005 4 5 ASOA05194 120050205A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27633AS 344 DURING A C-CHECK IN YUL, THE OUTBOARD SEAT TRACK BETWEEN FRAME 29-36 LEFT WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE OUTBOARD SEAT TRACK BETWEEN FRAME 29-36 LEFT IAW SRM 51-25-04. (M) 2H72 4T RTA53EU 20050405000752005040500075EU 2005 4 5 ASOA05193 120050205A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27633AS 344 DURING A C-CHECK IN YUL, THE OUTBOARD SEAT TRACK BETWEEN FRAME 25-26 LEFT WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE OUTBOARD SEAT TRACK BETWEEN FRAME 25-26 LEFT IAW SRM 51-25-04. (M) 2H72 4T RTA53EU 20050405000762005040500076WP 2005 4 5 ASAA0580086 120050207A533059360071 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02960AS 53074 OKC - DURING C-CHECK, FOUND FUSELAGE DENTED NEAR RIGHT ENGINE COWL DRAIN MAST. COLD WORKED AND INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050405000772005040500077WP 2005 4 5 ASAA0580087 120050207A5230591014192 STRUCTURE DOUG DC9 DC983 3022083WP CARGO DOOR CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02960AS 53074 OKC - DURING C-CHECK, FORWARD CARGO BAY DOOR FORWARD AND AFT LOWER EDGES CHAFED. REMOVED DAMAGED AREA AND INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050405000782005040500078WP 2005 4 5 ASAA0580054 120050131A53219957918501 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - DURING PAX CABIN FLOOR PANEL HAS TWO CRACKED RIBS. INSTALLED REPAIR HAT CHANNEL AND SPLICE. (M) 2L72 4F RTA6WE 20050331000532005033100053WP 2005 3 31 DHL2005805527 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBOARD FLANGE (2EA) MISDRILLED HOLES, STA 1500.000 L-13L L-12L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-05-05 EO AST 050205 DATED 02-21-05. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA AT STA 1500.000 L-12L IAW SRM 51-1-8B. PERFORMED DETAIL VISUAL INSPECTION NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD6-4) IAW EO AST 050205, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050331000542005033100054WP 2005 3 31 DHL2005805525 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBOARD FLANGE (2EA) MISDRILLED HOLES, STA 1400.000 L-10L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-05-05, EO AST050205 DATED 02-21-05. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA AT STA 1400.000 L-10L IAW SRM 51-1-8B. PERFORMED DETAIL VISUAL INSPECTION NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD5-4) IAW EO AST-050205, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050331000632005033100063CE 2005 3 31 69959 120050325A2497 WIRE BEECH 1900 1900D 1154162CE NR 1 INVERTER DAMAGED A AMWAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 CE07165YV UE165 CREW REPORTED STRONG ELECTRICAL SMELL IN COCKPIT. FIRST OFFICER OBSERVED SMOKE FROM AVIONICS BAY AREA. ALL AIRCRAFT SYSTEMS WERE OPERATING NORMALLY. REMOVED AND REPLACED INVERTER. NR 1 INVERTER WIRING AT A226 PANEL BROKEN AND LOOSE CAUSING ARCING. REPAIRED WIRING AS REQUIRED AND INVERTER. OPS CHECK SATISFACTORY. 2L72 4T RTA24CE 20050331000652005033100065EA 2005 3 31 COMA0560212 120050326A3350110049 CHARGER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT FAULTY A COMAK NONE L NO TEST ININSP/MAINT 1 SO01818CA 7408 FLIGHT 4949 DURING PREFLIGHT INSPECTION FOUND THE EMERGENCY LIGHTING POWER SUPPLY NR 2 INOPERATIVE. REPLACED THE BATTERY CHARGER ASSEMBLY. 2L72 4F RTA21EA 20050331000892005033100089NM 2005 3 31 DHL2005782500 120050318A5753 SKIN BOEING727 727227 1384078NM TE FLAPS DEBONDED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 LEFT INBOARD T/E FOREFLAP DISBONDED AT /TE. CUT OUT DISBONDED AREA AT T/E APPROX 4.5 X 1.75 INCH, REMOVED DAMAGED CORE APPROX 4.5 X 1.75 INCH AND VACUUM BAGGED FOR MOISTURE REMOVAL. FABRICATED REPLACEMENT SKIN APPROX 4.5 X 1.75 INCH EXTERNAL DOUBLER 3.5 X 7.5 INCH FROM 2024T3 .016 PO 9001660 AND REPLACEMENT CORE APPROX 4.5 X 1.75 INCH FROM DUR-5052-4.4-3/16-N-.050 PO 9911139. CLEANED, PREPPED, APPLIED ADHESIVE PRIMER AND ADHESIVE TO REPAIR PARTS AND SURFACES. VACUUM BAGGED FOR BONDING. BONDED, CLEANED, TREATED, PRIMED AND SEALED REPAIR ALL MAINTENANCE ACTIONS ACCOMPLISHED IAW B727 SRM 57-50-2 FIG 3 AND 51-40-20 FIG 2. 2L73 4F A3WE 20050331000912005033100091WP 2005 3 31 DHL2005805673 120050321A5310 HEAT EXCHANGER DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 A 0.250 CRACK IN LT PRIMARY HEAT EXCHANGER AFT LWR CORNER STA -12.000 L-27L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-16-05 DRAWING X83-R04 REV IR DATED 03-01-05. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. CUT OUT DAMAGED SECTION IAW DWG X83-R04. PERFORMED NDT INSP IAW DC8 NDT SPM 06-10-01-001. FABRICATED REPAIR DOUBLER (AL2024T3 0.050) REPAIR TRIPLER (AL2024T3 0.063) AND FILLER (2024T3 0.100) IAW DWG X83-R04. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW DWG X83-R04, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9, SRM 51-3-0 PG 1. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050331000932005033100093WP 2005 3 31 DHL2005805668 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT Z-FRAME INBOARD FLANGE HOLES (2EA) MISDRILLED AT STA 1000.000 L-12 L-13L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-05-05 EO AST 050205 DATE 02-21-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD6-5) IAW EO AST 050205 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050331000952005033100095 2005 3 31 SWIA200514786 420050320A34178220372445 ADC CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A SWIAA UNSCHED LANDING SJ AFFECT SYSTEMS WARNING INDICATION CRCRUISE 1 NM07918SW50 50 7645 DURING FLIGHT FROM ORD, CAPTAIN`S ALTIMETER JUMPED ERRATICALLY BETWEEN 22.00 - 32.00. UNABLE TO RESET WITH BARO KNOB TO PROPER SETTING. DIVERT TO CAK. REMOVED AND REPLACED NR 1 ADC IAW AMM 34-11-00. OPERATIONAL CHECK GOOD. A/C REMAINS CAT II & RVSM. 2L72 4F RTA21EA 20050331001102005033100110WP 2005 3 31 DHL2005805642 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME (2EA) MISDRILLED HOLE AT STA 520.000 L-12L TO L-13L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-05-05 EO AST 050205 DATED 02-21-05. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA AT STA 520.000 L-12L TO L-13L IAW SRM 51-1-8B. PERFORMED DETAIL VISUAL INSPECTION, NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD6-5) IAW EO ASTR 050205 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050331001232005033100123WP 2005 3 31 DHL2005805615 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME (2EA) MISDRILLED HOLES AT STA 880.000 L-10L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 02-25-05 EO AST 050203 DATED 02-18-05. PERFORMED DETAIL VISUAL INSPECTION, NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD5-4) IAW EO AST 050203 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050401000052005040100005CE 2005 4 1 HYI2005F00004 120050307A2520420121 SEAT CESSNA402 402C 207590RCE CONT O520 TSIO520* 17040SO CABIN BROKEN E HYIAK NONE O OTHER ININSP/MAINT 1 NE012611X11500 402C0072 PILOT REPORTED FIXED BACK DOUBLE PASSENGER SEAT BROKEN. MAINTENANCE FOUND SEAT SEPARATED FROM PEDASTAL. REMOVED AND REPLACED SEAT AND SENT BACK TO ORIGINAL MFG FOR REPAIR. SEAT WAS INSTALLED UNDER AVIATION FABRICATOR STC SA2716CE. (K) 1L72 3O3 O A7CE E8CE 20050401000222005040100022NE 2005 4 1 RU32005F00000 220050318A7310M25988 PACKING BEECH 300 300BEECH 1152930CE PWA PT6 PT6A60A 52043NE FUEL FILTER CUT D RU3AO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SW1570 64 FF5 PCE95379 INBOUND TO DESTINATION, NOTICED A THIN STREAM OF CLEAR LIQUID COMING FROM THE TOP VENTS OF THE LT ENGINE. THE CREW DECIDED TO RETURN TO HOME STATION TO HAVE FLUID AND POSSIBLE LEAK REPAIRED. REPLACED DEFECTIVE FUEL FILTER O-RING ON LT ENGINE. (K) 2L72 4T4 T A24CE E4EA 20050401000712005040100071NM 2005 4 1 USAA050349 120050310A5330 SKIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19442US40275 24841 CLT - Q6 - SKIN, 2.25 INCH X 7 INCHES. PREVIOUS REPAIR, SCAB PATCH INSTALLED, STATION 178, STRINGER S17R. INSTALLED SPLICE STRAP IAW EO 5300V157. (K) 2L72 4F4 FRTA16WE E21EU 20050401000742005040100074EA 2005 4 1 A6WA200540122 120050316A5712561444 RIB CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT MLG WW CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31413AW 7585 LT HAND MLG WHEEL WELL AT SS 48.30, FS 523.8, BATT RIB IS CRACKED 1.2500 INCH LONG. REPAIRED LT WING BATT RIB AT WS 53.60 IAW MFG REO. (K) 2L72 4F4 FRTA21EA E15NE 20050404000352005040400035EU 2005 4 4 KBM2005F00037 120050305A6520350A33215300 BEARING SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1D NE TAIL ROTOR CUT E KBMAK NONE O OTHER ININSP/MAINT 1 WP1953SH 498 2009 BEARING HAS MULTIPLE CUTS AROUND THE RUBBER. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050404000382005040400038EA 2005 4 4 A6WA20050033 120050125A5712 RIB CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT WING CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31412AW 7582 LT WING STATION 53.6 BUTT RIB IS CRACKED, 1 INCH LONG IN UPPER AFT RADIUS. REPAIRED LT WING STATION 53.60, BATT RIB IAW MFG REPAIR EO 601R-57-51-046, REV B. 2L72 4F4 FRTA21EA E15NE 20050404000562005040400056CE 2005 4 4 HYI2005F00002 120050131A3210536379 BOLT CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO MLG SHEARED E HYIAK NONE O OTHER ININSP/MAINT 1 NE0126514929 929 402C0344 828706 UPON ENGINE START, AFTER SEVERAL ROTATIONS, PROP STOPPED AND WOULD NOT TURN. MECHANIC FOUND CRANKSHAFT LARGE GEAR ATTACH BOLTS SHEARED AND GEAR DISLODGED FROM CRANKSHAFT. MECHANIC REMOVED AND REPLACED ENGINE AND RETURNED AIRCRAFT TO SERVICE. (NE01200502601) (K) 1L72 3O3 O A7CE E8CE 20050404000582005040400058SO 2005 4 4 GAJ2005F00000 120050207A7697 GROUND WIRE PIPER PA31 PA31350 7103110SO LYC O540 TIO540* 41532EA RT THROTTLE SHORTED E GAJAO OTHER O OTHER NRNOT REPORTED 1 NM113528Y 317952149 A .2500 INCH X .5000 INCH PIECE OF FOD (A SHIM GLUED ONTO THE RT THROTTLE LEVER TO (MAKE) THE SWITCH ,( NOT INSTALLED BY CURRENT OPER)FELL ONTO A HOT TERMINAL OF THE RT THROTTLE SWITCH AND GROUND CAUSING AN ELECTRICAL ARC WHICH RESULTED IN A PRECAUTIONARY LANDING IMMEDIATELY AFTER ROTATION AT TAKEOFF, DURING DAYTIME OPS. DAMAGE WAS LIMITED TO A BLOWN DIODE, WHICH RESULTED IN A FALSE GEAR WARNING LIGHT. AFTER RETRACTION OF LANDING GEAR, THROTTLE SWITCHES WERE ADJUSTED, DIODE WAS REPLACED AND A HARD LANDING INSPECTION WITH 12 CYCLES WAS ACCOMPLISHED. AIRCRAFT WAS THEN RETURNED TO PART OPS. (NM11200502069) (NM11200502176) 1L72 3O3 O A20SO E14EA 20050404000752005040400075EA 2005 4 4 N382005F00003 120050216A4900722822 GCU CNDAIRCL600 CL6002A12 1900304EA APU BURNED E N38ABA EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA05163WG3174 3057 UPON AIRCRAFT TEST FLIGHT FOR COMPLETION OF TAWS INSTALLATION. AIRCRAFT EXPERIENCED SMOKE IN THE CABIN AND COCKPIT. CREW DECLARED AND EMERGENCY LANDING AND PERFORMED AN UNEVENTFUL LANDING, USING NORMAL PUBLISHED EMERGENCY PROCEDURE. TROUBLESHOOTING FOUND THE APU GCU BURNED OUT (4) DIODE BOARD GCU REPLACED WITH AN OVERHAULED UNIT AND OPS CHECKED OK. (K) 2L72 4F RTA21EA 20050404000812005040400081NE 2005 4 4 AJC2005F00001 220050307A720030600405 ENGINE ISRAEL1125 ASTRASPX 4500205EU GARRTTTFE731TFE73140 29001NE RIGHT VIBRATION A AJCAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 EA25387PA800 145 P113241 AC DEPARTED, ENROUTE, AT FL360 THE RT ENG DEEC COMPUTER TRIPPED TO MANUAL MODE, FOLLOWED BY LOSS OF N1 GGE INDICATION. FLIGHT CONTINUED NORMALLY, EXPERIENCED A RT ENG VIBRATION WHICH CLIMBED TO .8 ON THE VIBRATION INDICATOR. REDUCED POWER ON RT ENG TO 75 PERCENT. VIBRATION STOPPED, FLEW AC AT REDUCED POWER AND DIVERTED FOR MAINT, LANDED SAFELY WITHOUT INCIDENT. CREW DID NOT DECLARE EMERGENCY. ENG MFG TECH ADVISED REMOVING ENG FOR EVALUATION, INSTALLING LOANER. RT ENG WAS REMOVED AND REPLACED. OPS CHECK AND LEAK CHECKS GOOD ON GROUND RUN UP. AC WAS RETURNED TO SERVICE. FOLLOW UP WITH MFG EVALUATION AND REPAIR OF ORIGINAL ENG. (EA25200506570) (K) 2L72 4F4 FRTA16NM E1NM 20050404001152005040400115WP 2005 4 4 DHL2005805621 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME (2EA) MISDRILLED HOLES AT STA 460.000 L-10L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-05-05 EO AST 050205 DATED 02-21-05. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA AT STA 460.000 L-10L. PERFORMED DETAIL VISUAL INSPECTION NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD 5.6) IAW EO AST 050205 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050404001162005040400116WP 2005 4 4 DHL2005805620 120050320A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBOARD FLANGE (1EA) MISDRILLED HOLE AT STA 1140.000 L-6R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-04-05 EO AST 050217 DATED 03-03-05. PERFORMED DETAIL VISUAL INSPECTION NO CRACK FOUND. PERFORMED CLEANING, TREATED AND PRIMING OF MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLE WITH RIVET (MS20470AD) IAW EO AST 050217 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050404001242005040400124WP 2005 4 4 DHL2005805583 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBOARD FLANGE (2EA) MISDRILLED HOLES AT STA 1140.000 L-10R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-07-05, EO AST 050201 DATED 02-17-05. PERFORMED DETAIL VISUAL INSPECTION NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO AST050201, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050404001272005040400127WP 2005 4 4 DHL2005805566 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME (2EA) MISDRILLED HOLES AT STA 717.000 L-9L TO L-10L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 02-25-05, EO AST050203 DATED 02-18-05. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. PERFORMED DETAIL VISUAL INSPECTION NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD5-6) IAW EO AST 050203, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050404001382005040400138CE 2005 4 4 DJFA2005069 120050324A3260 BULB CESSNA525 525 2076601CE MLG INDICATOR INOPERATIVE E DJFAO OTHER P NO WARNING INDICATION LDLANDING 1 EA23239CW 5250339 WHILE LANDING IN KTEB THE LEFT MAIN LANDING GEAR INDICATION WAS NOT RECEIVED WHEN GEAR WAS SELECTED DOWN. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE LIGHT BULB FOR THE GEAR INDICATION TO BE BURNED OUT. THE BULB WAS REPLACED, AND THE LANDING GEAR WAS CYCLED 15 TIMES. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 1L72 4F RTA1WI 20050404001412005040400141NE 2005 4 4 BSYA200500005 220050304A7261 WARNING LIGHT CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE MCAULY3AF34C3GFR34C703 GL CHIP DETECTOR ILLUMINATED E BSYAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL073RY 208B0436 PCE19196 942217 ON ROUTE FROM OMA TO APA, ENGINE CHIP LIGHT CAME ON SHORTLY AFTER DEPARTURE, AIRCRAFT TRIED TO RETURN TO OMA WHEN THE ENGINE FAILED. AN EMERGENCY LANDING ON HIGHWAY. CAUSE UNKNOWN AT THIS TIME. 1H71 3T3 T A37CE E4EA 5 CP60GL 20050404001442005040400144NM 2005 4 4 2005UALA00255 120050318A5210143W3311 SKIN BOEING777 777222 1385219NM PWA PW4077PW4077 NE PAX DOOR DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29778UA15301 26940 DENT FWD OF DOOR 2L, LOWER SIDE. *S/D* EXISTING DENT RE-EVALUATED AND REPAIRED AT BS 655, STR 26L - 27L. REPAIR WAS ACCOMPLISHED PER UA-EVA-50135. 2L72 4F4 FRTT0001SE E46NE 20050404001492005040400149EU 2005 4 4 05FDEA00636 120050325A5730A57350005201 SKIN AIRBUS310 A310203 3930313EU ZONE 600 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25401FE 191 PANEL LAND AT 650MB HAS 8 EA ELONGATED HOLES. REPAIRED 5 HOLES IAW A310-200 SRM 51-40-44 FIG 1, AND COMPLIED WITH EA 6-5710-87184 BY INSTALLING 3 EA REPAIR BUSHINGS FOR REMAINING 3 HOLES. 2L72 4F RTA35EU 20050404001782005040400178CE 2005 4 4 DXTA200500624 120050311A5755 SUPPORT BRACKET CESSNA560 560XL 2076702CE SPEED BRAKE DAMAGED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07662QS 5605262 NO TAKEOFF LIGHT AND HORN CAME ON AT TAKEOFF POWER AND TAKEOFF ROLL INITIATION. FLAPS 15, SPEED BRAKE RETRACTED, TRIMS SET FOR T/O). FOUND RT SPEED BRAKE SWITCH JAM NUT BEING PUSHED UP BY SPEED BRAKE DOOR SUPPORT BRACKET, CAUSING PLUNGER TO RELAX. ADJUSTED SPEED BRAKE SWITCHES, RAN A/C AND CYCLED SPEED BRAKES, FLAPS AND TRIM FOR 1 HOUR, NO FAULTS NOTED IAW CE560XL MM 27-61-00. 2L72 4F RTA22CE 20050404001792005040400179CE 2005 4 4 DXTA200500626 120050312A3230 UPLOCK CABLE CESSNA560 560XL 2076702CE MLG OUT OF ADJUST E DXTAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL07617QS 5605509 WHILE IN CRUISE AT FL410, CREW HEARD CLUNK SOUND FROM GEAR AREA, RED GEAR UNSAFE LIGHT ILLUMINATED AND HYD PRESS LIGHT ILLUMINATED STEADY. PULLED HYD CONTROL CB, HYD PRESS EXTINGUISHED, GEAR UNSAFE REMAINED ILLUMINATED. FOUND NOSE GEAR FREEFALL CABLE TO BE TIGHT & PREVENTING FUEL UPLOCK HOOK & SWITCH ENGAGEMENT. ADJUSTMENT NOSE GEARS UPLOCK CABLE TO ALLOW FULL UPLOCK HOOK & SWITCH ENGAGEMENT PER CE560 XL MM 32-30-08. BLED HYDRAULIC SYSTEM & SERVICED EMERGENCY GEAR BOTTLE PER CE 560 XL MM 12-13-01. OPS CHECK LANDING GEAR SYSTEM NORMAL AT THIS TIME. 2L72 4F RTA22CE 20050404001822005040400182CE 2005 4 4 DXTA200500629 120050313A2720 LINK CESSNA750 750 2076810CE RUDDER OUT OF ADJUST E DXTAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 GL07960QS 7500160 DURING CRUISE FLIGHT AT HIGH SPEED LEFT RUDDER WILL NOT TRIM WITH AUTO PILOT OFF, LEFT RUDDER JAMMED. SLOW SPEED OPERATES NORMALLY. VERIFIED NO TRAVEL TO LEFT AT 332 KNOTS. ADJUSTED TRIM BUNGEE + SUMMING LINK. ADJUSTED COMMAND BUNGEE IAW CE 750 MM 27-20-00. ACCOMPLISHED RIG CHECK IAW CE 750 MM 27-20-00. RIG CHECK GOOD. 2L72 4J RTT00007WI 20050404001882005040400188NM 2005 4 4 SWAA050750 120050310A524065C36231 SKIN BOEING737 737317 138447PNM R1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29686SW 23175 DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR SKIN CRACKED AT UPPER DOOR HINGE CUTOUT. REPAIRED SKIN PER SRM & SWA ACO. 2L72 4F RTA16WE 20050404001892005040400189NM 2005 4 4 C1HA200575001 120050319A7931 WARNING LIGHT BOEING727 727225 1384077NM PWA JT8 JT8D15A 52051NE NR 3 ENGINE ILLUMINATED A C1HAE ENGINE SHUTDOWN J WARNING INDICATION DEDESCENT 1 GL15675MG 22553 696560 INFLIGHT NR 3 LOW OIL BYPASS PRESSURE LIGHT ILLUMINATED. INFLIGHT SHUTDOWN PER COM 2.72.12. 2L73 4F4 F A3WE E2EA 20050404001902005040400190NM 2005 4 4 SWAA050751 120050310A53306545765 SKIN BOEING737 7373TO 138447GNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29697SW 23838 DURING WALK-AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 510, STR 16R. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050404001952005040400195WP 2005 4 4 ASAA0580100 120050215A532199365821 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02943AS 53018 OKC - DURING C-CHECK, FOUND PAX CABIN FLOOR PANEL DELAMINATED. FIBERGLASS BOND REPAIRED. (M) 2L72 4F RTA6WE 20050404001962005040400196WP 2005 4 4 ASAA0580095 120050215A533059364341 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02943AS 53018 OKC - DURING C-CHECK, FOUND FUSELAGE SKIN DENTED. RECONTOURED DAMAGED AREA. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050404002012005040400201EA 2005 4 4 ASOA05205 120050305A7120 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA ENGINE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27904EV 7628 DURING A C-CHECK IN MCN, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT L 0 IAW ASA EO 600-53-0072A. (M) 2L72 4F RTA21EA 20050405000132005040500013EA 2005 4 5 ASOA05201 120050305A33506100976 LAMP CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27707EV 10057 FLT 4413 - DURING A GROUND INSPECTION IN SLC, THE EMERGENCY CEILING LIGHT AT ROWS 16 AND 17 WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY CEILING LIGHT AT ROWS 16 AND 17. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050405000152005040500015WP 2005 4 5 ASAA0580094 120050215A533059360041 SKIN DOUG DC9 DC983 3022083WP FUSLEAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02943AS 53018 OKC - DURING C-CHECK, FOUND FUSELAGE SKIN DENTED. RECONTOURED DAMAGED AREA. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050405000222005040500022WP 2005 4 5 ASAA0580060 120050131A53219936640501 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - DURING C-CHECK, PAX CABIN FLOOR PANEL IS CRACKED, PUNCTURED, CRUSHED, AND DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050405000612005040500061WP 2005 4 5 ASAA0580048 120050131A53219936639501 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - DURING C-CHECK, FOUND PAX CABIN FLOOR PANEL HAS PULLED STRANDS OF FIBERGLASS. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050405000642005040500064WP 2005 4 5 ASAA0580046 120050131A53219936582503 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - DURING C-CHECK, PAX CABIN FLOOR PANEL HAS PULLED STRANDS OF FIBERGLASS. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050405000672005040500067EA 2005 4 5 ASOA05206 120050305A5310 DOUBLER CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27870AS 7530 DURING AN A-CHECK IN BTR, THE DOUBLER AT FS 640, LBL 45 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE DOUBLER AT FS 640, LBL 45. (M) 2L72 4F RTA21EA 20050405000682005040500068EU 2005 4 5 ASOA05197 120050204A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27633AS 344 DURING A C-CHECK IN YUL, THE SEAT TRACK BETWEEN FRAME 41 AND 44 RT WAS FOUND TO BE CORRODED IN THE CROWN BETWEEN FRAME 41-42 BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK BETWEEN FRAME 41 AND 44 RIGHT IAW SRM 51-25-04. (M) 2H72 4T RTA53EU 20050405000692005040500069EU 2005 4 5 ASOA05190 120050205A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27633AS 344 DURING A C-CHECK IN YUL, THE OUTBOARD SEAT TRACK BETWEEN FRAME 29-36, RBL 40 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE OUTBOARD SEAT TRACK BETWEEN FRAME 29-36, RBL 40 IAW SRM 51-25-04. (M) 2H72 4T RTA53EU 20050405000822005040500082EU 2005 4 5 ASOA05214 120050226A5740 BRACKET AEROSPATR72 ATR72212 8680945EU LT WING BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27530AS 453 DURING A C-CHECK IN YUL, THE OMEGA BRACKET ON THE LEFT SIDE OF THE FLAP BEAM AT RIB 8 WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE OMEGA BRACKET ON THE LEFT SIDE OF THE FLAP BRAM AT RIB 8 IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20050405000842005040500084WP 2005 4 5 ASAA0580099 120050215A533059114017 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02943AS 53018 OKC - DURING C-CHECK, FOUND FUSELAGE SKIN DENTED. REMOVED DAMAGED AREA. INSTALLED REPAIR FILLER AND DOUBLER. (M) 2L72 4F RTA6WE 20050405000852005040500085WP 2005 4 5 ASAA0580092 120050215A533059114017 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02943AS 53018 OKC - FOUND C-CHECK FUSELAGE SKIN DENTED. REPLACED DAMAGED SECTION. (M) 2L72 4F RTA6WE 20050405000862005040500086WP 2005 4 5 ASAA0580096 120050215A5330 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02943AS 53018 OKC - DURING C-CHECK, FOUND FUSELAGE SKIN DENTED. RECONTOURED DAMAGED AREA. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050405000872005040500087WP 2005 4 5 ASAA0580088 120050207A5712993758815 RIB DOUG DC9 DC983 3022083WP RT WING LE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02960AS 53074 OKC - FOUND C-CHECK, RIGHT WING L/E HAS CRACKED RIB. STOP DRILLED CRACK. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050405000882005040500088WP 2005 4 5 ASAA0580089 120050207A5532991196213 PANEL DOUG DC9 DC983 3022083WP VERTICAL STAB CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02960AS 53074 OKC - DURING C-CHECK, VERTICAL STABILIZER PANEL 6308C IS CHAFED. REPLACED PANEL. (M) 2L72 4F RTA6WE 20050405000922005040500092EU 2005 4 5 ASOA05216 120050302A5740 BRACKET AEROSPATR72 ATR72212 8680945EU WING BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27530AS 453 DURING A C-CHECK IN YUL, THE OMEGA BRACKET AT THE FLAP FARING OUTBOARD SIDE OF THE FLAP ARM AT RIB 13 LEFT WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE OMEGA BRACKET AT THE FLAP FARING OUTBOARD SIDE OF THE FLAP ARM AT RIB 13 LEFT IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20050405000932005040500093EU 2005 4 5 ASOA05213 120050225A5740 BRACKET AEROSPATR72 ATR72212 8680945EU WING BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27530AS 453 DURING A C-CHECK IN YUL, THE OMEGA BRACKET ON THE LEFT WING INBOARD SIDE OF THE OUTBOARD FLAP AT RIB 13 WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE INBOARD OMEGA BRACKET AT RIB 13 LEFT IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20050405000942005040500094EA 2005 4 5 ASOA05217 120050305A5210601R3167011 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27904EV 7628 DURING A C-CHECK IN MCN, THE TOP STEP ON THE PASSENGER DOOR WAS FOUND CRACKED AT THE VERTICAL SUPPORT HINGE ATTACH POINT. MAINTENANCE IS REMOVING AND REPLACING THE TOP STEP ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20050405000962005040500096WP 2005 4 5 ASAA0580052 120050131A532199365411 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - DURING C-CHECK, PAX CABIN FLOOR PANEL HAS PULLED STRANDS OF FIBERGLASS. FIBERGLASS BOND REPAIRED. (M) 2L72 4F RTA6WE 20050405001002005040500100WP 2005 4 5 ASAA0580076 120050131A534039364741 SPLICE DOUG DC9 DC983 3022083WP LONGERON CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - DURING C-CHECK, FOUND LONGERON STRINGER SPLICE CORRODED. REPLACED SPLICE. (M) 2L72 4F RTA6WE 20050405001022005040500102EA 2005 4 5 QXEA200500455 120050303A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - RIGHT HAND INBOARD SEAT RAIL AT STATION X677 HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01 AND HORIZON AIR EA R-53-285. 2L72 4F RTA21EA 20050405001052005040500105EA 2005 4 5 QXEA200500454 120050303A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - RIGHT HAND INBOARD SEAT RAIL AT STATION X647 HAS PITTING CORROSION ON INSIDE SURFACE. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01 AND HORIZON AIR EA R-53-285. 2L72 4F RTA21EA 20050405001082005040500108EA 2005 4 5 MASA200500049 120050121A3610 CLAMP CNDAIRCL600 CL6002B19 1900309EA BLEED AIR DUCT LOOSE A MASAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW0775987 7405 ASH 7106 CAE TO IAD RETURNED TO FIELD DUE TO SMOKE IN THE CABIN. MAINTENANCE FOUND A LOOSE CLAMP ON A DUCT ON THE 10TH STAGE BLEED SYSTEM. TIGHTENED CLAMP AND OPS CHECKED GOOD. 2L72 4F RTA21EA 20050405001112005040500111EA 2005 4 5 MASA200500242 120050321A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA EMERGENCY EXIT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW077291Z 7291 ASH 6231 PHX - SBP, LEFT HAND FORWARD EMERGENCY EXIT LIGHT INOP. MAINTENANCE COULD NOT DUPLICATE THE DISCREPANCY, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050405001122005040500112CE 2005 4 5 69932 120050323A5220 HANDLE BEECH 1900 1900D 1154162CE EMERGENCY DOOR UNSECURE A AMWAK NONE W INADEQUATE Q C ININSP/MAINT 1 CE07127ZV UE127 UPON PREFLIGHT WALK AROUND INSPECTION, CREW NOTICED 6F EMERGENCY DOOR EXTERIOR HANDLE POPPED OUT. MAINTENANCE RESECURED DOOR WITH NO FURTHER INCIDENT. THEREFORE NO PARTS WERE USED. 2L72 4T RTA24CE 20050405001192005040500119EA 2005 4 5 VTZA200500022 120050328A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27657BR 7491 RT FS 718 FRAME CRACKED AT 1 INCH IN LENGTH CRACK IN RADIUS. 2L72 4F RTA21EA 20050405001202005040500120EA 2005 4 5 VTZA200500025 120050328A5346601R536066 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA LT ENGINE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27657BR 7491 RT ENGINE SUPPORT BEAM IS CRACKED IN LOWER WEB AT .75 INCH. 2L72 4F RTA21EA 20050405001232005040500123EA 2005 4 5 VTZA200500027 120050328A5320601R3117117 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27657BR 7491 INTERCOSTAL CRACKED AT .250 INCH IN LENGTH ON LT OUTBOARD SIDE AT FS 484 BETWEEN BL 27.00. 2L72 4F RTA21EA 20050405001242005040500124EA 2005 4 5 VTZA200500028 120050328A5320601R311719 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27657BR 7491 INTERCOSTAL CRACKED AT .25 INCH IN LENGTH ON RT INBOARD SIDE AT FS 484 BETWEEN BL 36.00. 2L72 4F RTA21EA 20050405001272005040500127EA 2005 4 5 VTZA200500020 120050318A5320601R35031239 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27708BR 7575 RT FS 621 FLOOR SUPPORT IS CRACKED AT 1 INCH IN RADIUS. 2L72 4F RTA21EA 20050405001282005040500128EA 2005 4 5 MASA200500061 120050126A2150 A/C PACK CNDAIRCL600 CL6002B19 1900309EA BOTH OVERHEATED A MASAA UNSCHED LANDING MBJOVER TEMP SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SW07592ML 7388 CLOSED/SUP -ASH 2963 RETURNED TO THE FIELD DUE TO BOTH PACKS OVERTEMP. FLIGHT CREW REPORTED THEY CYCLED BLEED VALVES TWICE BUT FAULT DID NOT CLEAR. THEY ALSO GOT AN ENVIRONMENTAL SMELL IN THE CABIN. EVACUATED AIRCRAFT ON TAXI-WAY IN PHL. MAINTENANCE CAN NOT DUPLICATE FAULT REQUESTED TEST FLIGHT TO TRY AND DUPLICATE. 1/27 MAINTENANCE COULD NOT DUPLICATE ON GROUND. TEST FLEW AIRCRAFT AND COULD NOT DUPLICATE, SIGNED OFF AS OPS CHECKD GOOD. 2L72 4F RTA21EA 20050405001292005040500129EA 2005 4 5 QXEA200500463 120050223A5320 SILL CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - FUSELAGE INTERNAL AFT, LEFT HAND, FS 1000 TO FS 1047 SURROUND STRUCTURE, AFT BAGGAGE BAY DOOR, LOWER SILL IS CORRODED AROUND ANCHOR NUTS. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01. 2L72 4F RTA21EA 20050405001302005040500130EA 2005 4 5 QXEA200500465 120050304A5340 CHANNEL CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - FUSELAGE TO WING BODY FAIRING STIFFENER CHANNEL HAS CHAFFING DAMAGE AT THE AFT END. REPAIRED IAW CRJ700 SRM 51-21-16-001-001-A01 AND REO 670-53-61-155 AND HORIZON AIR EA R-53-284. 2L72 4F RTA21EA 20050405001332005040500133EA 2005 4 5 QXEA200500461 120050302A5753 VANE CNDAIRCL600 CL6002C10 1390015EA ZONE 600 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - RIGHT HAND INBOARD FLAP VANE LEADING EDGE HAS CHAFE MARK AT WS 88. REPAIRED IAW CRJ700 SRM 57-53-02-101-001-A01 AND SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050405001392005040500139NM 2005 4 5 MASA200500159 120050226A3350 CONNECTOR DHAV DHC8 DHC8202 2809007NM EMERGENCY LIGHT DIRTY A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07449YV 449 CLOSED/SUP - ASH 6322 PHX - EMERGENCY LIGHTS REMAIN ON WHEN BOTH LIGHT SWITCHES ON/ARM ARE IN THE OFF POSITION. PHX MAINTENANCE TROUBLESHOOTING WITH GJT MAINTENANCE. MAINTENANCE CLEANED THE CONNECTION AND OPS CHECKED GOOD. 2H72 4T RTA13NM 20050405001402005040500140EA 2005 4 5 MASA200500208 120050312A33501317 BULB CNDAIRCL600 CL6002D24 1390016EA EMERGENCY LIGHTSBURNED OUT A MASAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SW07907FJ 15007 CLOSED/SUP - ASH 6445 PHX - TUS - RETURNED TO GATE FLOOD LIGHT TRIPS CIRCUIT BREAKER. MAINTENANCE PLACED FLOOD LIGHT ON MEL 3/14/05. MX REPLACED BULB, OPS CHK GOOD. 2L72 4F RTA21EA 20050405001412005040500141EA 2005 4 5 MASA200500210 120050313A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSBURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07652ML 7036 ASH 2683 PHL - BNA HAD AN AFT CEILING EMERGENCY EXIT FLOOD LIGHT INOP. THE LIGHT WAS PLACED ON MEL 3/13/05. MAINTENANCE RELAMPED, OPS CHECKED GOOD. 2L72 4F RTA21EA 20050405001422005040500142SO 2005 4 5 MASA200500218 120050315A3350 SIGN EMB 145 EMB145LR 3260212SO EMERGENCY EXIT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07826MJ 145214 ASH 2673 FROM CLT TO CAK HAD THE RT OVERWING EMERGENCY EXIT SIGN INOP. MAINTENANCE RESECURED THE SIGN ASSY AND IT OPERATED NORMALLY. A/C DEPARTED WITHOUT FURTHER INCIDENT. 2L72 4T RTT00011AT 20050405001432005040500143EA 2005 4 5 QXEA200500459 120050303A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - LEFT HAND INBOARD SEAT RAIL AT STATION X677 HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01 AND HORIZON AIR EA R-53-283. 2L72 4F RTA21EA 20050405001442005040500144EA 2005 4 5 MASA200500238 120050319A3397 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSDISCONNECTED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0727314 7314 ASH 6383 PHX - MFR EMERGENCY LIGHTS AT PASSENGER DOOR INOP. MAINTENANCE RECONNECTED THE CONNECTOR, OPS CHECKED GOOD. 2L72 4F RTA21EA 20050405001452005040500145SO 2005 4 5 MASA200500239 120050320A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSBURNED OUT A MASAK NONE O OTHER ININSP/MAINT 1 SW07852MJ 145567 ON RON AND SCHEDULED FOR A 2 DAY ENROUTE INSPECTION DURING THE WALK AROUND IT WAS DISCOVERED THE ROW 14 CEILING EMERGENCY LIGHT NOT ILLUMINATING. REPLACED THE LIGHT BULB, OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050405001462005040500146 2005 4 5 AWXA200500376 420050325A341787232329V03 AIR DATA MODULE AIRBUS320 A320232 3930326EU ZONE 120 MALFUNCTIONED A AWXAC ABORTED TAKEOFF I FLT. ATTITUDE INST. TOTAKEOFF 1 WP28651AW24731 866 ON TAKEOFF ROLL AT FLL EN ROUTE FOR LAS NOTICED AIR SPEED DIFFERENCE OF 20 KTS, CAPTAINS AIRSPEED 60 KTS, FIRST OFFICERS 40 KTS, REJECTED TAKEOFF AT 60 KTS AND RETURNED TO GATE. AIRCRAFT WAS MAINTENACE FERRIED TO PHX WHERE MAINTENANCE PERFORMED AN INTERFACE TEST OF ALL THREE AIR DATA MODULES (ADM) PER RECOMMENDATIONS OF TSM 34-13-00-810-998A, NR 2 ADM FAULTED. REMOVED AND REPLACED NR 2 ADM IAW T/C R2A34306, OPERATIONAL CHECK WAS GOOD. FUNCTIONAL TEST OF AIR DATA MODULE S/N 2432 CONFIRMED REASON FOR REMOVAL, SENSOR WAS FOUND TO BE OUT OF TOLERANCE, INSTALLED NEW FLIGHT SOFTWARE TO FIT ZERO CURVE, FUNCTIONAL TEST WAS GOOD IAW CMM 34-11-17, REV. 3. 2L72 4F RTA28NM 20050405001482005040500148NM 2005 4 5 05FDEA00709 120050330A5711 SPAR CAP DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RIGHT HAND WING UPPER REAR SPAR CAP FOUND CORRODED AT XORS= 980 ARC7413-2. CARRIED OUT AS PER FEDEX EA 1-5710-82938. 2L73 4F RTA22WE 20050405001502005040500150NM 2005 4 5 05FDEA00710 120050330A5347 CARGO TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25583FE 48421 MAIN DECK CARGO COMPARTMENT FLOOR TRACK AT STA 635, WL 8.5, FOUND CRACKED APPROXIMATELY THREE (3) INCHES LONG. REMOVED PER SRM 51-31-01 VOLUME II. SEAT TRACK AND SPLICE FABRICATED PER SRM 53-70-00 VOL I, FIG 1. REPAIR PARTS INSTALLED PER SRM 50-70-00 VOL I, FIG 1 AND SRM 51-31-00 VOL II. 2L73 4F RTA22WE 20050405001512005040500151NM 2005 4 5 05FDEA00734 120050331A4910656471910 INTAKE BOEING727 727227 1384078NM APU CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 APU AIR INTAKE HOUSING HAS CORROSION ON MOUNTING FLANGE ALONG LOWER SIDE. 2L73 4F A3WE 20050405001522005040500152NM 2005 4 5 05FDEA00735 120050331A5310 SHEAR WEB BOEING727 727233 138408ANM FUSLEAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25272FE 22037 CORROSION IN SHEAR WEB BS 1166 LBL 29-33 WL 208. 2L73 4F RTA3WE 20050405001532005040500153EU 2005 4 5 05FDEA00625 120050321A5313A53610797234 LONGERON AIRBUS310 A310 EU ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 MAIN DECK CARGO FR 14 LONGERON 4TH FROM CENTERLINE CORRODED OUT OF LIMITS. REMOVED AND REPLACED LONGERON A53610797234 WITH NEW PART IAW A310 SRM 51-72-10. 2L72 4F RTA35EU 20050405001552005040500155EU 2005 4 5 05FDEA00627 120050321A5311 FRAME AIRBUS310 A310 EU FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 REF. SNRM# N00525 MAIN CABIN FRAME 37 CLS ADAPTER -Y040 IS GOUGED AND CRACKED (BETWEEN SEAT TRACK 2 AND 3 LT). REMOVED AND REPLACED CLS ADAPTER PER A310 SRM 51-72-10 TREATED, PRIMED AND TOP COATED AREA AND FASTENERS PER A310-200 SRM 51-75-10. 2L72 4F RTA35EU 20050405001562005040500156EU 2005 4 5 05FDEA00628 120050220A2760 CONTROL PANEL AIRBUS330 A300* EU SPOILERS MALFUNCTIONED A FDEAO OTHER O OTHER DEDESCENT 1 SO25653FE 736 WHEN SPEED BRAKES WERE DEPLOYED, ALL SPOILERS DEPLOYED EXCEPT NR 6 AND NR 7 ON THE RIGHT WING THIS CAUSED A WING ROCK THAT IN TURNED CAUSED THE PLANE TO START A 10 DEGREE BANK. FOUND LT NR 5 SPOILER ONLY ATTACHED AT ACT CONNECTION. REPLACED SPOILER PANEL, DAMAGE TO WING AT NR 5 SPOILER PERFORMED A THOROUGH VISUAL INSPECTION OF REAR SPA DEFERRED UNTIL COMPLIANCE WITH E.A. 6-5730-87052 ON LT NR 5 SPOILER, AND EA 6-5750-87053 ON RT NR 5 SPOILER. REPAIRED DAMAGE TO WING SKIN INBD/OTBD OF NR 5 LT IAW 2L72 4F RTA26NM 20050405001572005040500157NM 2005 4 5 72300039 120050117A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 SEVERAL SMALL AREAS OF CORROSION ON BOTTOM OF STRINGER. 2L73 4F4 FRTA3WE E2EA 20050405001632005040500163NM 2005 4 5 AALA20050225 120050328A3260834503 SQUAT SWITCH BOEING757 757223 1384957NM MLG INOPERATIVE A AALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW21693AA 26973 SJU INFLIGHT T0815/28MAR - AFTER TAKEOFF FROM JFK, EICAS MESSAGE NOSE AIR GROUND DISAGREE. LANDED SJU WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR COMPRESSED PROXIMITY SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050405001712005040500171WP 2005 4 5 AALA20050226 120050328A33506011779 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21968TW 53618 DTW - LOWER EMERGENCY EXIT LIGHT AT LEFT OVERWING EMERGENCY EXIT DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT LEFT OVERWING EMERGENCY EXIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050405001722005040500172EU 2005 4 5 AALA20050220 120050324A3350BR964814 SOCKET AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW2114061 471 JFK - EMERGENCY LIGHT OUT OF ITS SOCKET AT SEAT 27G. REPLACED EMERGENCY LIGHT SOCKET AT SEAT 27G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20050405001732005040500173NM 2005 4 5 AALA20050221 120050325A3350D71702001 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21795AN 30257 NRT - EMERGENCY LIGHTS AT DOOR FOUR LEFT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT DOOR FOUR LEFT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20050405001802005040500180NM 2005 4 5 72300050 120050301A5340 STRINGER CLIP BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 1.5 INCH BY 2 INCH AREA OF CORROSION ON STRINGER CLIP. 2L73 4F4 FRTA3WE E2EA 20050405001822005040500182NM 2005 4 5 72300052 120050201A5322 ANGLE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 APPROX 3 INCH BY 7 INCH AREA OF CORROSION ON CLOSE OUT ANGLE. 2L73 4F4 FRTA3WE E2EA 20050405001872005040500187NM 2005 4 5 UPS05444206 120050314A534769B622687 CARGO TRACK BOEING747 747121 1384871NM CARGO BAY CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 M/DECK BS 1880 RBL 50 INCH TIE DOWN FTG ATT PLATE FOUND CORRODED. CORROSION BLEND OUT 0.025 INCH BY 1 INCH BY 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT, BS 1880 RBL 50 INCH TIE DOWN FTG. REEPLACED AS PER MM 20-51-01. 2L74 4F A20WE 20050405001892005040500189NM 2005 4 5 UPS05444208 120050323A534065B387532 FITTING BOEING747 747121 1384871NM FLOOR SUPPORT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE:C M/DECK BS 2019 RBL 60 BELOW FLOOR SUPPORT FTG FOUND CRACK AFTER BS 2020 FLOOR FTG REMOVAL, CRACK LENGTH 3/8 INCH. M/DECK BS 2019 RBL 60 INCH BELOW FLOOR SUPT FTG REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02. 2L74 4F A20WE 20050405001912005040500191NM 2005 4 5 UPS05444210 120050313A534769B620491 CARGO TRACK BOEING747 747121 1384871NM CARGO BAY CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 M/DECK BS 1500 LBL 75 INCH TIE DOWN FTG ATTACH PLATE FOUND CORRODED. CORROSION BLEND OUT 0.030 INCH BY 1 INCH BY 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT, TIE DOWN FTG REPLACED AS PER MM 20-51-01. 2L74 4F A20WE 20050405001922005040500192NM 2005 4 5 UPS05444211 120050314A534769B620761 CARGO TRACK BOEING747 747121 1384871NM FUSLEAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 M/DECK BS 1720 LBL 78 INCH AND 85 INCH TIE DOWN FTG ATTACH PLATE FOUND CORRODED. CORROSION BLEND OUT 0.030 INCH BY 1 INCH BY 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT, TIE DOWN FTG AND PLATE REPLACED AS PER MM 20-51-01 FTG P/N: 69B62076-1, PLATE P/N: 69B62100-1. 2L74 4F A20WE 20050228000082005022800008NM 2005 2 28 AWXA200500256 120050122A5315654581266 FLOORBEAM BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOORBEAM UPPER CHORD AT BS 328, BETWEEN LBL 29 AND RBL 32, WL 208. MAINTENANCE CUT OUT DAMAGE IN FLOORBEAM UPPER CHORD AT BS 328, FROM LBL 35 TO RBL 67; FABRICATED A NEW REPLACEMENT SECTION OF UPPER CHORD AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-51 FIG 205. 2L72 4F RTA16WE 20050228000152005022800015SO 2005 2 28 MASA200500092 120050109A2560A1140001002 BULB EMB 145 EMB145LR 3260212SO FLASHLIGHT BURNED OUT A MASAH DEACTIVATE SYST/CIRCUITS O OTHER NRNOT REPORTED 1 SW07842MJ 145457 CLT HAD AN F/O EMERGENCY FLIGHT OUT. MAINTENANCE REPLACED A FLIGHTLIGHT LAMP. 2L72 4T RTT00011AT 20050228000172005022800017SO 2005 2 28 MASA200500094 120050209A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN MISINSTALLED A MASAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW07836MJ 145359 ASH - CLT 2 ADJACENT EMERGENCY FLOOR PROXIMITY LIGHT STRIPS WERE INOP. MAINTENANCE FOUND THEM IMPROPERLY INSTALLED AND REINSTALLED THEM PROPERLY AND PERFORMED THE OPS CHECKS. CHECKED GOOD. 2L72 4T RTT00011AT 20050228000192005022800019SO 2005 2 28 MASA200500099 120050211A33503025103 LIGHT EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSINOPERATIVE A MASAK NONE O OTHER ININSP/MAINT 1 SW07826MJ 145214 ON RON AND SCHEDULED FOR A ROUTINE CHECK INSPECTION, DURING THE WALK AROUND IT WAS DISCOVERED THAT THE LEFT HAND EXTERNAL OVERWING EMERGENCY LIGHT NOT ILLUMINATING. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AFTER TROUBLESHOOTING. OPERATIONAL CHECK GOOD. 2L72 4T RTT00011AT 20050228000282005022800028SO 2005 2 28 RAIA00502014 120050209A2150 A/C PACK EMB 145 EMB145LR 3260212SO LEFT MALFUNCTIONED A RAIAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CE03822HK 145069 LT PACK OVERLOAD WARNING AND SMOKE. MAINTENANCE DEFERRED NR 1 PACK PER MEL. REMOVED AND REPLACED NR 1 PACK VALVE. 2L72 4T RTT00011AT 20050228000332005022800033NM 2005 2 28 DXTA200500602 120050219A5720 PANEL GULSTM200 200 4500308NM FUEL VENT LEAKING E DXTAO OTHER K FLUID LOSS CRCRUISE 1 GL07720QS772 085 FUEL LEAKING OUT OF RT WING IN FRONT OF AILERON ON TOP. AIRCRAFT WAS INFLIGHT FOR 1.4 HRS AND LOST APPROX 1000 LBS OF FUEL OVER THE NORMAL BURN. INSPECTED RT WING FOUND SEEPAGE FROM RT BOTTOM WING VENT (NACA SCOOP). OPEN WING PANEL 640UT, REMOVED OLD SEALANT AROUND VENT SCOOP, CLEANED AREA PER G200 MM 28-10-00 PG 201 TASK 28-10-00-1410-801. SEALED AREA TASK 28-10-0-390-801 PARA G PG 206 WITH PR1440 B1/2 (MIL SPEC 8802). CLOSED PANEL 640NT. COMPLIED WITH LEAK CHECK OF PANEL AND SCOOP, LEAK CHECKED GOOD. 2L72 4F RTA53NM 20050228000342005022800034EA 2005 2 28 SWIA200514551 120050208A5315 CLIP CNDAIRCL600 CL6002B19 1900309EA FLOORBEAM CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07590SW 7077 FS 280 LEFT FLOORBEAM AT LBL 9.0 INBOARD AND OUTBOARD ATTACH CLIPS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLES IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00. 2L72 4F RTA21EA 20050228000402005022800040NM 2005 2 28 QXEA200500206 120050209A5330 PANEL DHAV DHC8 DHC8202 2809007NM FUSELAGE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09350PH 488 PANEL 122AR HAS 2 BAD NUTPLATES. THE TWO BAD NUTPLATES WERE REPLACED WITH NEW. 2H72 4T RTA13NM 20050228000462005022800046WP 2005 2 28 05FDEA00305 120050217A2611 SMOKE DETECTOR DOUG DC10 DC1030F 3023504WP CARGO BAY MALFUNCTIONED A FDEAO OTHER N FALSE WARNING DEDESCENT 1 SO25303FE 46802 CRG FIRE LWR AFT ALERT ON DESCENT. CREW FIRED 1 BOTTLE AND DECLARED EMERGENCY, NO EVIDENCE OF ANY FIRE IN AFT OR CENTER CARGO COMPART OR CONTAINERS AS THEY WERE OFF LOADED. REMOVED AND REPLACED LWR FWD CARGO FIRE EXT IAW M/M 26-22-01-4. REMOVED AND REPLACED MSC IAW M/M 31-12-01-4, OPS CHECK NORMAL. INSPECTED WIRING IN AFT LWR CARGO PER REF TO MD-10 FIM 26-14-02, NO DEFECTS NOTED AT THIS TIME. REMOVED AND REPLACED BOTH SMOKE DET IN CENTER CARGO COMP AND BOTH DET IN AFT CARGO COMP PER MM 26-14-01-4 AND PERFORMED ADJ/TEST OF LOWER CARGO COMP FIRE/SMOKE DETECTION SYSTEM PER MM 26-14-01-5. NO DEFECTS NOTED. OK FOR SERVICE. 2L73 4F RTA22WE 20050228000472005022800047EA 2005 2 28 SWIA200514552 120050208A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA FLOORBEAM CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07590SW 7077 FS 280 RIGHT FLOORBEAM AT RBL 9.0 OUTBOARD ATTACH CLIP CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIP IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00. 2L72 4F RTA21EA 20050228000482005022800048EA 2005 2 28 05041643 120050210A2740 COMPUTER CNDAIRCL600 CL6002B19 1900309EA MACH TRIM MALFUNCTIONED A VTZAO OTHER O OTHER CLCLIMB 1 EA27643BR 7363 MACH TRIM FAILURE WITH STAB CHANNEL 2 FAIL. MX COMPLIED WITH BOMBARDIER SL 27-083. NO CURRENT FAULT FOUND AT THIS TIME. 2L72 4F RTA21EA 20050228000572005022800057NE 2005 2 28 ARWA20050106 220050125A7200 ENGINE DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE NR 1 MALFUNCTIONED A ARWAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO19784AL666994606 46135 669160 NR 1 ENGINE OIL PRESSURE LIGHT ILLUMINATED; OIL PRESS GAUGE INDICATED 25 PSI, FOLLOWED BY A LOSS OF OIL QUANTITY, WENT TO ZERO. PERFORMED OIL PRESSURE LIGHT ILLUMINATED CHECKLIST; THEN, PERFORMED IN-FLIGHT ENGINE SHUTDOWN ABNORMAL CHECKLIST. ENGINE SHUTDOWN AT 18:17Z, AFTER EVALUATION, CONTINUE TO MIA. REMOVED AND REPLACED NR 1 ENGINE IN ACCORDANCE WITH ARROW AIR TASK CARD DC8UN-003; PERFORMED ENGINE RUN-UP FOUND NORMAL IN ACCORDANCE WITH DC8 MM 71-00. 2L74 4F4 F 4A25 1E8 20050228000802005022800080NM 2005 2 28 SWAA050417 120050213A5320BAC1498 WEB BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29502SW 24179 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER WEB AT BS 295, STRINGER 16L, CRACKED. REMOVED AND REPLACED STRINGER WEB SECTION PER SRM. 2L72 4F RTA16WE 20050228000922005022800092NM 2005 2 28 SWAA050398 120050210A53126545409 PRESSURE PANEL BOEING737 7373K2 13844BANM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29340LV 23738 DURING SCHEDULED 1/2D CHECK, FOUND BEADED PRESSURE WEB AT BS 664, LBL 31, CRACKED. REPAIRED PRESSURE WEB PER SRM. 2L72 4F RTA16WE 20050228001132005022800113EA 2005 2 28 SWIA200514554 120050208A5210 FRAME CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07590SW 7077 PAX DOOR INNER FRAME IS CRACKED; FS 320.10 UPPER END OF DOOR. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED DOOR FRAME FS 320.10 UPPER END IAW CRJ REO 601R-52-11-402 REV "B". 2L72 4F RTA21EA 20050228001142005022800114EA 2005 2 28 SWIA200514555 120050208A5210 FRAME CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07590SW 7077 PAX DOOR INNER DOOR FRAME IS CRACKED; FS 338.90 UPPER END OF DOOR. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED DOOR FRAME FS 338.90 UPPER END IAW CRJ REO 601R-52-11-402 REV B. 2L72 4F RTA21EA 20050228001462005022800146EA 2005 2 28 VNAA0502007 120050208A2750855D10011 BPSU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS FAILED A VNAAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 GL05230PS1907 7904 DURING CRUISE FLIGHT WITH FLAPS SELECTED TO ZERO DEGREES THE FLAPS FAIL CAUTION MESSAGE ILLLUMINATED. THE CREW OF FLIGHT 2292 (YOW TO PHL) DIVERTED THE FLIGHT TO YUL AND MADE AN UNEVENTFUL LANDING. THE AIRCRAFT WAS FERRIED TO DAY WHERE PSA MAINTENANCE REMOVED AND REPLACED THE LT FLAP BRAKE AND POSITION SENSOR UNIT IAW CRJ 200 AMM 27-51-10-000-801 AND 27-51-10-400-801. RIGGING/OPERATIONAL CHECKS WERE GOOD IAW CRJ200 AMM 27-51-10-830-801 AND 27-54-00-710-801. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050228001512005022800151NM 2005 2 28 05FDEA00238 120050203A5311ACA73512 FRAME DOUG MD11 MD11 3023602NM ZONE 200 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 MAIN DECK - RIGHT HAND SIDE FRAME G-NET ATTACHED YOKE ASSEMBLY AT STA Y=535 TOP AND BOTTOM PART FOUND WITH CHAFED MARK. MAIN DECK - RIGHT HAND SIDE FRAME G-NET ATTACHED YOKE ASSEMBLY AT STA Y=535, CHAFED MARK REMOVED PER SRM 53-00-01 VOLUME I, FIGURE 3. MATERIAL REMOVED= 0.005; ORIGINAL MATERIAL THICKNESS= 0.140 INCH, REMAINING MATERIAL THICKNESS= 0.135 INCH. ALLOWABLE LIMIT= 0.20T. 2L73 4F RTA22WE 20050228001662005022800166 2005 2 28 COMA0560134 420050218A22106225027101 SERVO CNDAIRCL600 CL6002B19 1900309EA ELEVATOR MALFUNCTIONED A COMAO OTHER F FLT CONT AFFECTED CRCRUISE 1 SO01729CA16015 7265 FLIGHT 4941 ELEVATOR CONTROL STIFF AUTO PILOT DISCONNECTED. REPLACED THE ELEVATOR SERVO. 2L72 4F RTA21EA 20050228001702005022800170NM 2005 2 28 SWAA050524 120050222A53106547979 CREASE BEAM BOEING737 7375H4 138449DNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29507SW 24184 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON CREASE BEAM Z-ANGLE, RT SIDE, BETWEEN BS 927 AND BS 1006. REMOVED AND REPLACED RT CREASE BEAM Z-ANGLE PER SRM. 2L72 4F RTA16WE 20050228001772005022800177NM 2005 2 28 05FDEA00194 120050128A5531 STRINGER BOEING727 727200 138407ENM VERTICAL STAB CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25235FE 21329 STRINGER CRACKED IN VERTICAL FIN AT FIN STA 180.6 STRINGER 3 LEFT. *S/D* FABRICATED AND INSTALLED REPAIR PARTS PER SRM 55-30-4 FIG 1. 2L73 4F RTA3WE 20050228001802005022800180NM 2005 2 28 DLM88050099 120050208A5241 SEAL DOUG MD88 MD88 3023688NM GALLEY DOOR LEAKING A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27970DL 43173 ACFT WOULD NOT PRESSURIZE, RETURNED TO CVG LOUD NOISE FROM AFT GALLEY DOOR SEAL. OPENED DOOR / INSP DOOR SEAL, NO TROUBLE FOUND. PRESS CKD ACFT NORMALLY. 2L72 4F RTA6WE 20050228001912005022800191WP 2005 2 28 AALA20050122 120050217A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21561AA 53091 DEN - EMERGENCY LIGHT IN CABIN INOPERATIVE. REPLACED BATTERY PACK AT B5101 FOR EMERGENCY LIGHT IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050228001962005022800196NM 2005 2 28 SWAA050485 120050218A3350101073 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED C4 CHECK, FOUND FWD ENRTY DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20050228001972005022800197NM 2005 2 28 SWAA050486 120050218A53306545774 SKIN BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29661SW 23173 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 737, STRINGER 19R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050228002012005022800201NM 2005 2 28 SWAA050490 120050218A53306545767 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 482 + 2, STRINGER 10L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050228002102005022800210SO 2005 2 28 MASA200500121 120050216A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN INTERMITTENT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07853MJ 145464 ASH - PHL AN OVERWING EXIT LIGHT SIGN INOP. MAINTENANCE CYCLED THE EMERGENCY EXIT LIGHT SWITCH AND COULD NOT DUPLICATE FAULT. 2L72 4T RTT00011AT 20050228002162005022800216EA 2005 2 28 COMA0560135 120050218A3231 DOOR CNDAIRCL600 CL6002B19 1900309EA NLG OUT OF ADJUST A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01966CA 7132 FLIGHT 5825 NOSE DOOR OPEN WARNING AFTER GEAR EXTENSION. ADJUSTED THE LT NLG DOOR. 2L72 4F RTA21EA 20050228002212005022800221NE 2005 2 28 AALA20050118 220050215A7320 SWITCH BOEING767 767223 1385123NM GE CF6 CF680A 30025NE ZONE 100 INOPERATIVE A AALAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS CLCLIMB 1 SW21339AA 22336 LAX - INFLIGHT T0019/15 LEFT ENGINE ROLLED BACK AT 300 FEET. FULL CONTROL MOVED CUTOFF AND RUN. ENGINE NORMAL AT TOUCHDOWN. THROTTLES PARKED UP THROUGH TOUCHDOWN AND ROLLOUT. REVERSED NORMALLY. REPLACED LEFT HAND ENGINE FUEL FILTER AND LEFT AND RIGHT HAND FUEL CUT OFF SWITCHES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA1NM E13NE 20050228002222005022800222SO 2005 2 28 CHQA200500037 120050220A3350 LAMP EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11262SK 145168 LEFT HAND FORWARD EMERGENCY EXIT LIGHT IS INOP. RELAMPED PER EMB 145 MM 33-50-10. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050228002352005022800235SO 2005 2 28 RAIA00502019 120050210A3020 VALVE EMB 145 EMB145LR 3260212SO NR 2 ENG ANTIICEMALFUNCTIONED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03847HK 14500857 STL - ENGINE ANTI-ICE FAIL INDICATION NR 2 ENGINE. MAINTENANCE DEFERRED NR 2 ENGINE ANTI-ICE VALVE PER MEL. 2L72 4T RTT00011AT 20050228002432005022800243SO 2005 2 28 RAIA00502018 120050209A2613M1195175242 SENSOR EMB 145 EMB145LR 3260212SO NR 1 ENGINE DEFECTIVE A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03837HK 145255 STL - BLEED LEAK INDICATION NR 1 ENGINE. MAINTENANCE REMOVED AND REPLACED BLEED LEAK SENSOR IN NR 1 PYLON. 2L72 4T RTT00011AT 20050228002572005022800257SO 2005 2 28 SIMA200503803 120050129A5330AL2024T3 SKIN EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE GOUGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21706RG 145194 DURING AN INSPECTION OF AIRCRAFT, THE BAGGAGE DOOR CUT OUT WAS FOUND TO BE GOUGED AT THE AFT LOWER CORNER OUTER SKIN. REMOVED THE DAMAGED OUTER SKIN MY MAKING A CUTOUT. FABRICATED A FILLER AND DOUBLER. REPAIR DONE IAW SRM. (K) 2L72 4F4 FRTT00011ATTE6CH 20050228002582005022800258SO 2005 2 28 SIMA200503101 120050129A5330 SKIN EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE GOUGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21706RG 145194 DURING AN MBV INSPECTION THE BAGGAGE DOOR CUT OUT WAS FOUND TO BE GOUGED AT THE AFT LOWER CORNER OUTER SKIN. REMOVED THE DAMAGED OUTER SKIN BY MAKING A CUTOUT. FABRICATED A FILLER, DOUBLER FOR REPAIR. REPAIR DONE IAW SRM. (SW21200503066) (K) 2L72 4F4 FRTT00011ATTE6CH 20050228002632005022800263SO 2005 2 28 SIMA200503804 120050201A533014533888001 SKIN EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE LIGHTNING STRIKEA SIMAK NONE O OTHER ININSP/MAINT 1 SW21635AE 145158 DURING AN MBV INSPECTION, A LIGHTNING STRIKE WAS FOUND ON THE LT SIDE OF THE FUSELAGE BETWEEN FRAMES 32 AND 33 AT STRINGER 6L. REMOVED THE DAMAGE BY MAKING A CUT OUT. FABRICATED A FILLER, OUTER DOUBLER AND AN INNER DOUBLER. REPAIR DONE IAW SRM. (K) 2L72 4T4 FRTT00011ATTE6CH 20050405001952005040500195EU 2005 4 5 05FDEA00739 120050331A5410A5451526850200 GUSSET AIRBUS310 A310 EU ZONE 400 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 NR 1 PYLON OUTBD SIDE AT RIB 16 ANGLE HAS 3 SQ INCHES OF CORROSION. REMOVED AND REPLACED GUSSET IAW A310-200 SRM 51-72-10. 2L72 4F RTA35EU 20050228002722005022800272SO 2005 2 28 SIMA200503408 120050127A532014521725015 SILL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21637AE 145170 FOUND RT SILL AFT OF SERVICE DOOR HAS CORROSION ON FWD UPPER SURFACE AT FRAME 22. REMOVED CORROSION FROM WEB IAW SRM. AC RETURNED TO SERVICE. (K) 2L72 4T4 FRTT00011ATTE6CH 20050228002882005022800288SO 2005 2 28 SIMA200501911 120050113A531514521713605 FLOORBEAM EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21738NR 145401 DURING CPCP INSPECTION MAINTENANCE FOUND THE FORWARD CABIN FLOORBEAM HAT SECTION HAS CORROSION THROUGH TOP IB EDGE AT FR 20 IAW SRM. AIRCRAFT RETURNED TO SERVICE. (SW21200502486) (K) 2L72 4F4 FRTT00011ATTE6CH 20050228002982005022800298EA 2005 2 28 SIMA200503404 120050128A3350110049 POWER SUPPLY CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE CABIN DISCHARGED A SIMAK NONE L NO TEST TXTAXI/GRND HDL 1 SW21521AE3125 67 10142 DURING A CHECK INSPECTION, FOUND NR 1 EMERGENCY POWER SUPPLY INOPERATIVE. REPLACED NR 1 EMERGENCY POWER SUPPLY. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (K) (SW21200503055) 2L72 4F4 FRTA21EA EOOO63EN 20050228003202005022800320SO 2005 2 28 SIMA200501918 120050113A532014521713005 BEAM EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21735TS 145386 DURING AN IMBV INSPECTION THE CENTER HAT BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED THE CORRODED CENTER HAT BEAM AND INSTALLED SERVICEABLE ONE. REPAIR DONE IAW SRM AND EA. (SW21200502482) (K) 2L72 4F4 FRTT00011ATTE6CH 20050228003242005022800324SO 2005 2 28 SIMA200501910 120050113A531514521721009 FLOORBEAM EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21738NR 145401 DURING CPCP INSPECTION MAINTENANCE FOUND THE FORWARD CABIN FLOOR DIGITAL HAS CORROSION IN SEVERAL AREAS OF UPPER SURFACE. MAINTENANCE REMOVED AND REPLACED THE FLOOR DIGITAL IAW SRM. AIRCRAFT RETURNED TO SERVICE. (SW21200502486) (K) 2L72 4F4 FRTT00011ATTE6CH 20050301000092005030100009NM 2005 3 1 QXEA200500218 120050204A5313 STRINGER BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 PDX - STRINGER 295 IS CORRODED AT STATION X-32 TO X-16. REPAIRED IAW DHC-8 400 SRM 51-21-10 AND SRM 51-25-10. 2H72 4T RTA13NM 20050301000102005030100010NM 2005 3 1 QXEA200500219 120050204A5313 STRINGER BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 PDX - STRINGER 275 IS CORRODED AT STATION X-1C. REPAIRED IAW Q400 SRM 51-21-10 AND 51-25-10. 2H72 4T RTA13NM 20050301000142005030100014NM 2005 3 1 UPS05443926 120050211A5711 FITTING BOEING747 747123 1384873NM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, RT WING REAR SPAR UPPER SPLICE FITTING AT BS 1241 HOLE NR 6 FOUND CRACKED AT SPLICE FITTING APPROX 0.040 INCH. HOLE REWORKED PER BSB 747-57A2314. 2L74 4F A20WE 20050301000212005030100021NM 2005 3 1 UPS05443921 120050210A5730 SKIN BOEING747 747123 1384873NM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, RT WING REAR SPAR UPPER SPLICE FITTING AT BS 1241 FOUND HOLE NR 12 CRACKED AT WING SKIN APPROX 0.040 INCH. HOLE REWORKED PER BSB 747-57A2314. 2L74 4F A20WE 20050301000242005030100024NM 2005 3 1 DHL2005751501 120050225A5344AE5201 HINGE BOEING727 727264 138408MNM CARGO DOOR BROKEN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01751DH 22982 MAIN CARGO DOOR, FAIL SAFEHINGE AFT SEGMENT AT FS 640.0, 14 LUGS BROKEN ON AIRFRAME SIDE. ACCOMPLISHED HFEC INSP OF HINGE ON MAIN CARGO DOOR AND FOUND NO OTHER HINGES CRACKED IAW B727 NDT MANUAL PART 06. REMOVED FASTENERS AND REMOVED (2 EA) SECTIONS OF INTERIOR GILLINER AT FS 640 TO GAIN ACCESS FOR HINGE REPLACEMENT. REMOVED FASTENERS AND REMOVED AFT SECTION OF FAIL SAFE HINGE FUSELAGE SIDE AT FS 640. FABRICATED NEW SECTION OF HINGE FROM MS20001-16-7200 PO# 0530161 HINGE MATERIAL IAW AEI MM CH 52 PG 15-20. POSITIONED AND DRILLED, DEBURRED NEW SECTION OF HINGE. ALODINED AND PRIMED NEW SECTION OF HINGE. INSTALLED NEW SECTION OF HINGE RESTORED FINISH. REINSTALLED (2 EA) SECTIONS GILLINER. 2L73 4F A3WE 20050301000402005030100040EA 2005 3 1 SWIA200514629 120050215A2720 PIVOT ASSY CNDAIRCL600 CL6002B19 1900309EA RUDDER PEDALS WORN A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07909SW 7558 KLUNKING NOISE AND FEEL IN CAPTAINS RUDDER PEDALS. INSTALLED NEW FRONT PIVOT ASSY ON CAPT'S SIDE RUDDER PEDALS IAW AMM 27-21-05, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050301000412005030100041WP 2005 3 1 0500169967 120050208A5320 ANGLE DOUG DC9 DC931 3022065WP CUSP WEB CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019331 47263 DURING M-CHECK FOUND CORROSION ON LT CUSP TEE ANGLE. REPAIRED PER EA 99-200923. 2L72 4F A6WE 20050301000542005030100054SO 2005 3 1 C2XA05TY020 120050218A3260852701 PROXIMITY SENSOR EMB 145 EMB145LR 3260212SO MLG MALFUNCTIONED A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2716951 145063 LANDING GEAR DISAGREE MESSAGE UPON ATTEMPTED RETRACTION OF L/G. ACFT RETURNED TO FIELD. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR PROXIMITY SENSOR. LANDING GEAR OPERATION CHECK SATISFACTORY. ACFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20050301000642005030100064SO 2005 3 1 SWIA200514632 120050218A2750 CONNECTOR EMB 120 EMB120ER 3260203SO TE FLAPS LOOSE A SWIAO OTHER F FLT CONT AFFECTED LDLANDING 1 NM07188SW 120039 DURING LANDING ROLLOUT, FLAP CONTROL FAULT OF OUTBOARD PAIR AT FLAPS. REPLACED ELECTRICAL CONNECTOR AND PINS ON LEFT OUTBOARD FLAP ACTUATOR ELECTRICAL CONNECTOR. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050301000942005030100094EA 2005 3 1 A6WA200540041 120050202A5542 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RUDDER DENTED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31414ZW 7586 SKIN IS DENTED ON THE LT SIDE SKIN PANEL BETWEEN RS 108.25 AND 113.98 THE DENT MEASURES 2.2 INCHES LONG X 2 INCHES WIDE. PERFORMED A MAJOR REPAIR TO THE RUDDER SKIN ON LT SIDE BY TRIMMING OUT DAMAGE, LPI, FABED DOUBLER AND INSTALLED IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050301001012005030100101EA 2005 3 1 A6WA200540022 120050122A4920 APU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE APU BAY FAILED A A6WAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 GL31439AW 7753 APU FAILED AND SHUTDOWN ON TAKEOFF ROLL AND ROTATION. TRIED TO RELIGHT ON DESCENT, RAN APPROXIMATELY 3 MINUTES AND SHUTDOWN. STRONG FUEL SMELL PRESENT IN CABIN. PERFORMED APU OPS CHECK IAW AMM. INSPECTED AND FOUND NO EVIDENCE OF FUEL LEAK. NO FAULTS ON ECU. OK FOR CONTINUED SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050301001032005030100103EA 2005 3 1 A6WA200540017 120050108A262189900741 FIRE BOTTLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE AFT CARGO BAY LOW A A6WAF ACTIVATE FIRE EXT. P NO WARNING INDICATION ININSP/MAINT 1 GL31412AW2019 66 7582 LT ENGINE SQUIB LIGHT WILL NOT ILLUMINATE. FOUND LT ENGINE FIRE BOTTLE LOW PRESSURE. REMOVED AND REPLACED BOTTLE. (K) 2L72 4F4 FRTA21EA E15NE 20050301001192005030100119NM 2005 3 1 USAA050084 120050101A5320 THRESHOLD BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19522AU49282 23857 PIT - Q3 - WEB PLATE, .2500 INCH AROUND, CORROSION; LEVEL 1; TASK NR C53-20201, AFT CARGO DOOR THRESHOLD; CORROSION AROUND NUT PLATE HOLES. DEFECTIVE PART REPLACED WITH IDENT PART IAW DWG NR 65-47957. (K) 2L72 4F4 FRTA16WE E21EU 20050301001352005030100135NM 2005 3 1 USAA050094 120050101A53201133883 STRAP BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19517AU 23703 PIT - Q6 - STRAP, CRACKED IN HALF, 3 INCH CRACK; LOWER FLOORBEAM STA 312 AND 328 LBBL 12. DEFECTIVE PART REPLACED WITH IDENT PART IAW DWG. AND SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050301001372005030100137NM 2005 3 1 SB05027 120050218A335020131A BATTERY PACK BOEING737 7373B7 1384580NM CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19383US 22956 PHL - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHTS ABOVE THE AFT LEFT SERVICE DOOR AND THE AFT RIGHT SERVICE DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACKS. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050302000182005030200018SO 2005 3 2 GUU2005F00005 120050125A3260 PROXIMITY SWITCH EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE LT MLG DIRTY A GUUAA UNSCHED LANDING JE WARNING INDICATION VIBRATION/BUFFET CLCLIMB 1 SO17268AS 120202 AFTER TAKEOFF, WITH LANDING GEAR SELECTED UP, LT MAIN RED (A) ANNUNCIATOR REMAINED ILLUMINATED WITH LOUD VIBRATION. SELECTED LANDING GEAR DOWN. AIR RETURN. LANDED WITHOUT INCIDENT. CLEANED LT LANDING GEAR DOOR PROXIMITY SWITCHES. LANDING GEAR EXTENSION AND RETRACTION NORMAL. INDICATIONS NORMAL. (K) 2L72 4T4 TRTA31SO E20NE 20050302000412005030200041NM 2005 3 2 USAA050092 120050103A5720654532421 PLATE BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU LT WING FATIGUED A USAAK NONE O OTHER ININSP/MAINT 1 EA19517AU53410 23703 PIT - Q6 - MAIN LANDING GEAR FG; INSTALLATION OF REAR SPAR FATIGUE PLATE; INSTALLATION OF REAR SPAR FATIGUE PLATE; LT REAR SPAR UPPER CHORD BETWEEN WBL 150 AND 126. FABRICATED DOUBLER AND INSTALLED IAW EA 79629. (K) 2L72 4F4 FRTA16WE E21EU 20050302000592005030200059CE 2005 3 2 S2YA05005 120050115A612018984001 SOLENOID BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE RT PROP GOVERNORINOPERATIVE A S2YAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL13831SK UE83 BEFORE FLIGHT, THE CREW REPORTED RT PROP WOULD NOT SPOOL UP, THEY RETURNED TO THE GATE FOR MECHANIC. MECHANIC REPLACED THE RT PROP GOVERNOR FOR TROUBLESHOOTING BUT THE PROBLEM REMAINED. MECHANIC REPLACED THE RT LOW PITCH SOLENOID AND OPERATIONAL CHECKS WERE GOOD. WITH NO FURTHER DISCREPANCIES NOTED THE AC WAS RETURNED TO SERVICE. 2L72 4T4 TRTA24CE E26NE 20050302000772005030200077SO 2005 3 2 GUU2005F00006 120050126A3260 CONNECTOR EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE LT MLG LOOSE A GUUAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO17268AS 120202 AFTER TAKEOFF WITH LANDING GEAR SELECTED UP, LT MAIN RED (A) ANNUNCIATOR REMAINED ILLUMINATED WITH LOUD VIBRATION. SELECTED LANDING GEAR DOWN. AIR RETURN. LANDED WITHOUT INCIDENT. CLEANED A AND B SYSTEM PROXIMITY SWITCHES ON LT GEAR. TIGHTENED (A) SYSTEM PROXIMITY SWITCH CONNECTOR PLUG. LANDING GEAR EXTENSION AND RETRACTION OPERATIONAL CHECK NORMAL. 2L72 4T4 TRTA31SO E20NE 20050302000782005030200078NM 2005 3 2 UIEA2005005 120050127A2913650666 PUMP BOEING747 747230B 1384889NM GE CF6 CF650* 30018NE NR 1 ENGINE LEAKING A UIEAH DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA15512MC 21220 NR 1 HYD CONTENTS RAPIDLY DEPLETED DURING FLIGHT. APPROPRIATE DRILLS CARRIED OUT. REMOVED AND REPLACED NR 1 ENGINE EDP IAW MM. NO EVIDENCE OF LEAKS AFTERWARDS. SERVICED NR 1 HYD SYSTEM TO FULL. INSPECT PRESS AND CASE DRAIN FILTERS. SECURED ENGINE COWL AND SHUT ACCESS. (K) 2L74 4F4 F A20WE E23EA 20050302000832005030200083NM 2005 3 2 USAA050113 120050101A5320 FLOOR SUPPORT BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19517AU53410 23703 PIT - Q6 - FLOOR SUPPORT, 20 INCH X 1.5 INCH AREA, CORROSION; TOP OF FLOOR SUPPORT BETWEEN STA 947-967, RBL 46; DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-40-02-1 AND 51-40-03. (K) 2L72 4F4 FRTA16WE E21EU 20050302000872005030200087EU 2005 3 2 USAA050034 120050101A5315D53112818200400 FLOORBEAM AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19713UW17339 1040 BFM - S1 - FLOORBEAM, 2.0 INCH X 2.0 INCH X .050 INCH AREA, CORROSION; LEVEL 2; TASK NR JA220-53500, MAIN CABIN FLOORBEAM AT FR21, BL Y254. INSTALLED REPAIR ANGLE AND FILLER IAW SRM. (K) 2L72 4F4 FRTA28NM E37NE 20050302000882005030200088EU 2005 3 2 USAA050036 120050101A5320D5347112420100 WEB AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19713UW17339 1040 BFM - S1 - WEB, 1 INCH X 1 INCH W X .07 INCH D, CORROSION, LEVEL 2; TASK NR JA260-53500, FR 70-69, Y1292 MAIN CABIN FLOOR. REMOVED AND REPLACED WEB. (K) 2L72 4F4 FRTA28NM E37NE 20050302000902005030200090NM 2005 3 2 USAA050100 120050101A5311 FRAME BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19517AU 23703 PIT - Q6 - FRAME, .1562 INCH IN RADIUS (2 HOLES); STA 440 S-24L (FWD CARGO BIN); INSTALLED FABRICATED REPAIR DOUBLER IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050302000912005030200091NM 2005 3 2 USAA050105 120050101A5311 FRAME BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19517AU53410 23703 PIT - Q6 - FRAME, .2500 INCH CRACK; BS 907 FRAME BETWEEN STRINGERS S-1 AND S-2R. DOUBLERS INSTALLED IAW SRM 53-00-07, FIG 201 WITH MINOR DEVIATION IAW EA 79620. (K) 2L72 4F4 FRTA16WE E21EU 20050302000922005030200092NM 2005 3 2 USAA050107 120050101A575465C26602217 STRUCTURE BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU L/E SLAT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19517AU53410 23703 PIT - Q6 - NR 2 SLAT, .1250 INCH CRACKS (3 EA); LOWER T CHORD AFT ROW OF FASTENERS AT ACTUATOR MOUNT; INSTALLED DOUBLER IAW SRM 57-43-01, FIG 206. (K) 2L72 4F4 FRTA16WE E21EU 20050302001012005030200101NM 2005 3 2 USAA050102 120050101A5210507945178 SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU PAX DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19517AU 23703 PIT - Q6 - FWD ENT DOOR, .1250 INCH CRACKS (3 EA); INTER SKIN AND FRAME AT NR 6 AFT DOOR STOP AND INTER SKIN AT NR 7 DOOR STOP AFT. INSTALLED DOUBLERS IAW TYP. REP. 52-10-16. (K) 2L72 4F4 FRTA16WE E21EU 20050302001032005030200103NM 2005 3 2 USAA050108 120050103A5330 SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19517AU53410 23703 PIT - Q6 - SKIN, 2.2500 INCH CRACK; FUSELAGE SKIN AT FWD SVC DOOR CUT OUT AFT; CUT OUT CRACKED AREAS AND INSTALLED REPAIR DOUBLERS IAW SRM 53-10-01 AND EA 79657. (K) 2L72 4F4 FRTA16WE E21EU 20050302001052005030200105NM 2005 3 2 USAA050103 120050101A5320 STIFFENER BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19517AU53410 23703 PIT - Q6 - STIFFENER; .5 INCH CRACK; FLOORBEAM STIFFENER BS 328, LBL 28. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-10-02 AND MFG DWG. (K) 2L72 4F4 FRTA16WE E21EU 20050302001092005030200109NM 2005 3 2 USAA050112 120050101A5754 SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU L/E SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19517AU53410 23703 PIT - Q6 - SKIN, 6.5 INCH X 4.5 INCH AREA DELAMINATION; NR 5 SLAT OB END; REMOVED TOP SKIN AND CORE AND REPLACED IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050302001102005030200110EU 2005 3 2 USAA050004 120050110A5320 BEAM AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19737US13952 1245 CLT - RON- BEAM, 2 INCH AREA, CORROSION, FRAME 16 LBL 32 FLOOR LEVEL. INSTALLED REPAIR ANGLE IAW SRM. (K) 2L72 4F4 FRTA28NM E37NE 20050302001122005030200112NM 2005 3 2 USAA050119 120050101A53201137215 FLOOR SUPPORT BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19517AU53410 23703 PIT - Q6 - FLOOR SUPPORT, 16 INCH WIDE SPREAD CORROSION; CORROSION; LEVEL 1; TASK C53-107-01, 02; BS 312 AND 328 BL0 RT 10 INCHES; DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-40-02. (K) 2L72 4F4 FRTA16WE E21EU 20050302001132005030200113NM 2005 3 2 USAA050118 120050101A5320 SILL BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19517AU 23703 PIT - Q6 - DOOR SILL, 1 INCH X 1 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-107-01, FWD SVC DOOR SILL (AFT) AT NUT PLATE. REPAIRED IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050302001142005030200114NM 2005 3 2 USAA050154 120050101A5320 FLOOR SUPPORT BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19521AU52547 23856 PIT - Q6 - FLOOR SUPPORT, 1 INCH CRACK; STA 540, BL0.0; REPLACED SUPPORT BRACKET IAW SRM 53-00-51. (K) 2L72 4F4 FRTA16WE E21EU 20050302001152005030200115NM 2005 3 2 USAA050115 120050101A521065554787 GATE BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU AFT ENTRY CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19517AU53410 23703 PIT - Q6 - AFT ENTRY LWR EXHAUST, 1 INCH X 1 INCH AREA (4 PLACES) CORROSION; LEVEL 1; TASK NR C53-107-01; LOWER EXHAUST GATE LOWER IB SURFACE. DEFECTIVE PART REPLACED WITH IDENT PART NR. (K) 2L72 4F4 FRTA16WE E21EU 20050302001162005030200116NM 2005 3 2 USAA050116 120050101A532065C334191 WEB BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19517AU53410 23703 PIT - Q6 - SHEAR WEB, 2 INCH X 2 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-202-01, BS 1016, LBL 16 SHEAR WEB; DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-10-02 AND MFG DWG. (K) 2L72 4F4 FRTA16WE E21EU 20050302001172005030200117NM 2005 3 2 USAA050157 120050101A5240 DOOR FRAME BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU SERVICE DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19521AU52728 23856 PIT - Q6 - DOOR EDGE FRAME, .1250 INCH CRACK; FWD SERVICE DOOR, UPPER MIDDLE DOOR STOP CUTOUT, AFT EDGE FRAME; INSTALLED DOUBLER IAW TYP REP. (K) 2L72 4F4 FRTA16WE E21EU 20050302001182005030200118NM 2005 3 2 USAA050161 120050108A5210 SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU PAX DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19521AU52728 23856 PIT - Q6 - INNER SKIN, APPROX .5 INCH LONG; MAIN ENTRANCE DOOR AFT SIDE AT NR 7 STOP; INSTALLED DOUBLER IAW TYP REP. (K) 2L72 4F4 FRTA16WE E21EU 20050302001192005030200119NM 2005 3 2 USAA050156 120050101A575465C26601179 SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU L/E SLAT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19521AU52728 23856 PIT - Q6 - NR 1 SLAT, 1 INCH CRACK; LOWER SKIN AFT ROW RIVETS AT NR 2 AUX TRACK. INSTALLED DOUBLER IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050302001202005030200120EU 2005 3 2 USAA050039 120050101A5315D5347218920200 FLOORBEAM AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19713UW17339 1040 BFM - S1 - FLOORBEAM, 2.0 INCH X 2.0 INCH X .036 INCH, CORROSION; LEVEL 2; TASK NR JA260-53500, MAIN CABIN FLOOR, Y1292, FR69-68, Z240. REMOVED AND REPLACED WITH NEW PART (BEAM) IAW SRM. (K) 2L72 4F4 FRTA28NM E37NE 20050302001212005030200121EU 2005 3 2 USAA050038 120050101A5320D5348004320501 SILL AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19713UW17339 1040 BFM - S1 - SILL, 1.5 INCH X 1.5 INCH X .065 INCH, CORROSION; LEVEL 2; TASK NR JA-26053500, FR 63-64, Y1732, Z240. REMOVED AND REPLACED SILL IAW SRM. (K) 2L72 4F4 FRTA28NM E37NE 20050302001232005030200123EU 2005 3 2 USAA050040 120050101A5315D5347217220390 FLOORBEAM AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19713UW17339 1040 BFM - S1 - FLOORBEAM, 2.0 INCH X 2.0 INCH X .027 INCH, CORROSION; LEVEL 2 TASK NR JA260-53500, MAIN CABIN FLOOR, Y1292, FR 68-66, Z240. REMOVED AND REPLACED WITH NEW PART, FLOORBEAM, IAW SRM. (K) 2L72 4F4 FRTA28NM E37NE 20050302001242005030200124EU 2005 3 2 USAA050041 120050101A5320D5347219021100 BEAM AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19713UW17339 1040 BFM - S1- BEAM, 1.0 INCH X 1.0 INCH X .035 INCH, CORROSION; LEVEL 2; TASK NR JA260-53500, MAIN CABIN FLOOR Y1292, FR 65-66, Z240. REMOVED AND REPLACED WITH NEW PART ( BEAM ) IAW SRM. (K) 2L72 4F4 FRTA28NM E37NE 20050302001272005030200127NM 2005 3 2 USAA050160 120050101A575465C26601180 SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU L/E SLAT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19521AU52728 23856 PIT - Q6 - NR 6 SLAT, .5 INCH CRACK; LOWER SKIN AFT ROW RIVET 4 INCHES FROM OB END; INSTALLED DOUBLER IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050302001292005030200129NM 2005 3 2 USAA050159 120050101A53206935365 INTERCOSTAL BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19521AU52728 23856 PIT - Q6 - INTERCOSTAL, NUMEROUS CRACKS, .5 INCH. .7500 INCH, 1.5 INCH; SCREW HOLES UPPER FLANGE OF INTERCOSTAL, BS 380-400. REPAIR ANGLE INSTALLED IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050302001382005030200138EU 2005 3 2 USAA050005 120050110A5320 BEAM AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19737US 1245 CLT - RON - BEAM, 2 INCH AREA, CORROSION, FRAME 16, LBL 22 FLOOR LEVEL. INSTALLED REPAIR ANGLE AND DOUBLER IAW SRM. (K) 2L72 4F4 FRTA28NM E37NE 20050302001392005030200139NM 2005 3 2 USAA050082 120050101A53206936656 WEB BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19522AU49282 23857 PIT - FOUND WEB CRACKED 1.25 INCH, STATION 927-947.5 INTERCOSTAL CRACKED 1.25 INCH FROM FORWARD CORNER. INSTALLED SAME PART PER DWG 69-36656. (M) 2L72 4F RTA16WE 20050302001402005030200140NM 2005 3 2 USAA050166 120050101A5313 STRINGER BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19521AU 23856 PIT - FOUND STRINGER CRACKED 1.5 INCHES LONG, FS 380 STRINGER 15R. SPLICED IN NEW SECTION OF STRINGER PER SRM 53-00-03, FIG 201, DWG 65-45768. (M) 2L72 4F RTA16WE 20050302001412005030200141NM 2005 3 2 USAA050079 120050102A5713 STRINGER BOEING737 7373B7 1384580NM RT WING CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19522AU 23857 PIT - FOUND STRINGER CRACKED .5 INCH, RT WING WBL 479 AT S-8. REPAIR ANGLES PER EA 79684. (M) 2L72 4F RTA16WE 20050302001422005030200142NM 2005 3 2 USAA050083 120050105A5713 STRINGER BOEING737 7373B7 1384580NM RT WING CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19522AU49282 23857 PIT - FOUND STRINGER CRACKED .3750 INCH AT S-8 UPPER STRINGER AT WBL 355 AT ATTACH BOLT ON, RT WING. INSTALLED REPAIR ANGLES PER EA 79684. (M) 2L72 4F RTA16WE 20050302001432005030200143NM 2005 3 2 USAA050173 120050101A5315 FLOORBEAM BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19521AU52728 23856 PIT - FOUND FLOORBEAM CORRODED 1 INCH BY .75 INCH AREA, FLOORBEAM STATION 328 RBBL 24.50 LBBL 24.50. CORROSION LEVEL 1. REMOVED CORROSION, FABRICATED STRAP REPAIR PER SRM 53-00-51 PAGE 212-215 AND 53-10-51 PAGE 114. (M) 2L72 4F RTA16WE 20050302001442005030200144NM 2005 3 2 USAA050167 120050111A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19521AU52728 23856 PIT - FOUND SKIN CHAFFING AND FRETTING WEAR 25.5 BY 30 INCH, BS 860 BETWEEN STRINGER 3L AND 3R. DAMAGE REMOVED, DOUBLER INSTALLED PER SRM 53-60-01 FIG 209. (M) 2L72 4F RTA16WE 20050302001452005030200145NM 2005 3 2 USAA050168 120050101A575465C2660300 SKIN BOEING737 7373B7 1384580NM L/E SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19521AU 23856 PIT - FOUND TOP SKIN/CORE BOND DELAMINATED 3 INCHES BY 2 INCHES AREA, NR 3 SLAT INBOARD T/E. REMOVED DELAMINATED TOP SKIN AND CORE MATERIAL, BONDED IN NEW CORE, INSTALLED TOP DOUBLER PER SRM 51-70-10. (M) 2L72 4F RTA16WE 20050302001462005030200146NM 2005 3 2 USAA050169 120050101A575165C2591118A SKIN BOEING737 7373B7 1384580NM RT AILERON DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19521AU 23856 PIT - FOUND COMPOSITE SKIN DELAMINATED 1 INCH AREA, RT AILERON TAB OUTBOARD T/E. INSTALLED REPAIR PLYS PER SRM 51-60-01 AND 51-70-16. (M) 2L72 4F RTA16WE 20050302001472005030200147NM 2005 3 2 USAA050170 120050101A575465C26601179 SKIN BOEING737 7373B7 1384580NM L/E SLAT BENT A USAAK NONE O OTHER ININSP/MAINT 1 EA19522AU49282 23857 PIT - FOUND SLAT EXT SKIN BENT AREA 3.5 INCH BY 1.5 INCH AREA, NR 1 SLAT UPPER T/E SURFACE INBOARD END. REMOVED DAMAGED AREA, INSTALLED FILLER AND INTERNAL DOUBLER PER SRM 51-70-10. (M) 2L72 4F RTA16WE 20050302001492005030200149NM 2005 3 2 USAA050172 120050101A53201123578 FLOOR SUPPORT BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19521AU52728 23856 PIT - FOUND FLOOR SUPPORT CORRODED 1 INCH BY .5 INCH IN THREE AREAS, FLOORBEAM FROM STATION 967-986 LBL 18. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-10-02. (M) 2L72 4F RTA16WE 20050302001512005030200151NM 2005 3 2 USAA050191 120050105A5315BAC1505100186 FLOORBEAM BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19436US 24558 PIT - FOUND UPPER CHORD CORRODED 8 INCH BY 2 INCH, STATION 312 LBL 8 TO RBL 7 FLOOR UPPER CHORD. REPLACED UPPER CHORD PER SRM 53-10-51 FIG 205. (M) 2L72 4F RTA16WE 20050302001522005030200152NM 2005 3 2 USAA050193 120050117A53206547957 WEB BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19436US41647 24558 PIT - FOUND WEB CRACKED 1 INCH BY 2 INCH AREA AROUND NUT PLATE, AFT CARGO THRESHOLD WEB STATION 800 TO 833 PLATE. CORROSION LEVEL 1. REMOVED WEB AND REPLACED WITH NEW WEB PER SRM 53-60-15, 51-40-02. (M) 2L72 4F RTA16WE 20050302001532005030200153NM 2005 3 2 USAA050195 120050116A53451134821 MOUNT BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19436US41647 24558 PIT - FOUND MOUNT GALLEY AFT CORRODED 3 INCH BY 3 INCH AREA, LEFT AFT GALLEY MOUNT BS 990, BS 1016 LBL 32.10. REPLACED MOUNT LEFT AFT GALLEY PER SRM 51-40-00. (M) 2L72 4F RTA16WE 20050302001542005030200154NM 2005 3 2 USAA050175 120050101A5315 FLOORBEAM BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19521AU52728 23856 PIT - FOUND FLOORBEAM CORRODED .5 INCH BY .5 INCH AREAS AROUND 6 NUTPLATES, FLOORBEAM STATION 967 17L-17R. TOP CP REPAIR, FLOOR EXTRUSION AND SPLICES PER TYPICAL REPAIR 53-10-05B. (M) 2L72 4F RTA16WE 20050302001552005030200155NM 2005 3 2 USAA050176 120050101A575465C26602217 SKIN BOEING737 7373B7 1384580NM L/E SLAT CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19521AU52728 23856 PIT - FOUND LOWER SKIN SURFACE WITH CHAFE DAMAGE, 1.5 INCH BY 2.5 INCH, NR 2 SLAT INBOARD CORNER AND OUTBOARD CORNER LOWER SURFACE. (M) 2L72 4F RTA16WE 20050302001592005030200159NM 2005 3 2 USAA050188 120050121A5312 BULKHEAD BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19778AU38617 24980 PIT - FOUND FORWARD BULKHEAD WEB CRACKED .25 INCH, WL 218 AND LBL 12. INSTALLED DOUBLER PER SRM 53-10-08. (M) 2L72 4F RTA16WE 20050302001602005030200160NM 2005 3 2 USAA050189 120050112A5320 BRACKET BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19521AU52547 23856 PIT - FOUND DOUBLER BRACKET CRACKED, FS 500-500A, VHF NR 2 ANTENNA MOUNT BRACKET. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 51-40-02. (M) 2L72 4F RTA16WE 20050302001642005030200164NM 2005 3 2 USAA050076 120050101A5320654578310 SUPPORT BRACKET BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19522AU 23857 PIT - FOUND ANTENNA CHANNEL, SUPPORT BRACKETS WITH THREE .5 INCH CRACKS, BETWEEN STATION 500/500A, STRINGER 28L-28R, VHF-2 ANTENNA CHANNEL. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M) 2L72 4F RTA16WE 20050228000132005022800013SO 2005 2 28 MASA200500090 120050201A532014521713005 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO FUSLEAGE CORRODED A MASAK NONE O OTHER ININSP/MAINT 1 SW07848MJ7375 145530 IN C-CHECK, OMEGA BEAM (HAT BEAM) IS CORRODED OUT OF LIMITS AT BL 0 AND WILL BE REMOVED AND REPLACED. 2L72 4T RTT00011AT 20050228000322005022800032NM 2005 2 28 DHL2005781501 120050211A5754 SKIN BOEING727 727227 1384078NM NR 2 SLAT GOUGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING AN C-CHECK, NR 2 SLAT SKIN GOUGED AT I/B SLAT HOOK. REMOVED FASTENERS FOR ACCESS AT NR 2 SLAT SKIN AT I/B SLAT HOOK IAW B727 SRM 51-30-2, FABRICATED DOUBLER REPAIR, MAT USED 2024-T3 .125 PO 9001068, DIM 5.5 X 3.5 INCHES IAW B727 SRM 57-50-3 FIG 10. ALODINE AND PRIMED PART IAW B727 SRM 51-10-2, INSTALLED COUNTERSINKED REPAIR WASHERS IAW B727 SRM 51-30-8 FIG 4. INSTALLED DOUBLER REPAIR IAW B727 SRM 57-50-3 FIG 10. 2L73 4F A3WE 20050228000372005022800037EA 2005 2 28 COMA0570020 120050216A3251481051 PRESSURE SWITCH CNDAIRCL600 CL6002C10 1390015EA NLG FAULTY A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01379CA 10102 FLIGHT 5803 RECEIVED A STEERING CAUTION MESSAGE AFTER TAKEOFF FROM CVG, AIRCRAFT RETURNED TO FIELD. REPLACED THE STEERING PRESSURE SWITCH. 2L72 4F RTA21EA 20050228000422005022800042EA 2005 2 28 050406263 120050209A5210 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27626BR 7225 PHASE III PAX DOOR CRACKED ON INNER RADIUS OF INTERCOSTAL AT FS 338.9 AND DATUM NR 1, .75 INCH CRACK. 2L72 4F RTA21EA 20050228000492005022800049SO 2005 2 28 SWIA200514521 120050207A275012064207615CON SELECTOR EMB 120 EMB120ER 3260203SO TE FLAP MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 NM0758733399 399 120197 WHEN SELECTING FLAPS 25 ON APPROACH GOT THE FLAP LIGHT WITH ADVANCED SWS LIGHT ON MAP. REMOVED AND REPLACED FLAP SELECTOR LEVER. OPERATIONAL CHECK GOOD REF 27-50-00. 2L72 4T RTA31SO 20050228000512005022800051EA 2005 2 28 SWIA200514523 120050204A2740 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07411SW 7067 CREW REPORTS STAB CHANNEL 1 WON'T STAY ENGAGED IN FLIGHT. REMOVED AND REPLACED MOTOR CONTROL UNIT AND HORIZONTAL STAB TRIM ACTUATOR IAW 27-42-05 AND 27-42-01. OPERATIONAL CHECK GOOD. P/N 7062-3, S/N OFF 704, P/N 8396-3, S/N OFF 693. 2L72 4F RTA21EA 20050228000582005022800058WP 2005 2 28 ARWA20050107 120050126A5242 DOOR DOUG DC10 DC1010 3022110WP E/E BAY UNSECURE A ARWAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO1968041 46900 AFTER TAKEOFF UNABLE TO PRESSURIZE. SECURED AFT AVIONICS DOOR IN ACCORDANCE WITH MM 52-00-00 AND PRESSURIZED AIRCRAFT IN ACCORDANCE WITH MM 21-30-00. OPERATIONAL CHECK NORMAL. 2L73 4F A22WE 20050228000672005022800067SO 2005 2 28 MASA200500021 120050108A2560 FLASHLIGHT EMB 145 EMB145LR 3260212SO COCKPIT INOPERATIVE A MASAO OTHER L NO TEST ININSP/MAINT 1 SW07842MJ 145457 ASH - CLT CREW REPORTED THE EMERGENCY FLIGHT DECK FLASHLIGHT INOP. MAINTENANCE CLEANED THE SWITCH AND OPS CHECKED THE FLASHLIGHT. 2L72 4T RTT00011AT 20050228000722005022800072NM 2005 2 28 SWAA050412 120050213A53106546536 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 DURING SPV FOUND SHEAR TIE AT BS 540, STRINGER 10R, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050228001002005022800100EU 2005 2 28 05FDEA00281 120050213A5330 SKIN AIRBUS310 A310222 3930315EU FUSELAGE DAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25420FE 339 ACCOMPLISH MAINTENANCE C-CHECK, DURING AGING AIRCRAFT INSPECTION AN EXISTING REPAIR DOUBLER WAS FOUND ON THE LOWER FWD CARGO DOOR. DOUBLER WAS REMOVED DURING C4 CHECK AT LIS SCRATCH MARK BLENDED. HFEC INSPECTION OF THE AREA. NEW FASTENERS PAINTED. 2L72 4F RTA35EU 20050228001052005022800105NM 2005 2 28 05FDEA00274 120050210A5530651680310 TIE BOEING727 727200 138407ENM VERTICAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25235FE 21329 CORROSION VERTICAL STAB TENSION TIE RT FWD VERTICAL BOLT HOLE AIRCRAFT AND TENSION TIE. *S/D* REPAIRED PER EA 7-5530-86241. 2L73 4F RTA3WE 20050228001272005022800127NM 2005 2 28 DHL2005742002 120050212A7720 WARNING LIGHT BOEING727 727225 1384077NM NR 2 ENGINE ILLUMINATED A DHLAO OTHER M OVER TEMP TXTAXI/GRND HDL 1 SO01742DH 21290 ABORTED START OF ENGINE NR 2 AT KIAD. DUE TO ABNORMALLY RAPID EGT RISE. AFTER START LEVER PLACED IN START DETENT THERE WAS A SLIGHT DELAY IN EGT RISE. LIMITS WERE NOT EXCEEDED. SECOND ATTEMPT WAS NORMAL. PERFORMED ENGINE START ON NR 2 ENGINE PER ASTAR JRH 5.2. NO ABNORMAL INDICATIONS WERE NOTED DURING ENGINE START. REF ASTAR JRH B-727 LIMITATIONS CHAPT 4.3. OPS CHECK OF NR 2 ENGINE IS NORMAL, AND STARTING. 2L73 4F A3WE 20050228001292005022800129EU 2005 2 28 05FDEA00223 120050202A7830 LIMIT SWITCH AIRBUS300 A300F4605R 3930327EU THRUST REVERSER FAILED A FDEAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25686FE 804 ON T/O AFTER BRK REL AND STANDARD POWER SET APPROX 50 KTS HAD AMBER ECAM 1 THR REV UNLOCK WITH AMBER REV UNLOCK ON PANEL ABOVE ENG INSTRUMENTS. ACN RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A CATEGORY: C. ENGINE 1 THRUST REVERSER INOP. THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POSITION. LOCKED OUT 1 T/R IN ACCORDANCE WITH MEL 78-30-01-A. DURING TAKEOFF SUSPECT BAD RT ELECTRICAL LIMIT SWITCH. DEACTIVATED 1 T/R PER MEL 78-30-01-A. REMOVED AND REPLACED 1 ENGINE RIGHT REVERSER FEEDBACK TRANSDUCER PER MM 78-31-07. RAN ENGINE PER JRH AND OPERATED 1 REVERSER WITH NO DEFECTS NOTED. ITEM CLEARED. 2L72 4F RTA35EU 20050228001302005022800130EA 2005 2 28 COMA0560116 120050210A275011045D100201 COUPLING CNDAIRCL600 CL6002B19 1900309EA NR 2 FLAPS WORN A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01966CA 7132 FLIGHT 5738 FLAPS FAIL CAUTION. REPLACED THE RT WING NR 2 FLEX DRIVE SHAFT. 2L72 4F RTA21EA 20050228001352005022800135CE 2005 2 28 DXTA200500590 120050213A3260 PROXIMITY SWITCH CESSNA500 560CESSNA 2076750CE MLG DIRTY E DXTAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 GL07379QS 5600479 UPON GEAR RETRACTION, GEAR RETRACTED NORMALLY. AFTER HYD PRESS ON LIGHT EXTINGUISHED, RIGHT MAIN GEAR LOWER WITHOUT COMMAND. CLEANED & INSPECTED RT MAIN GEAR UPLOCK ACTUATOR ASSY & MICROSWITCH FOUND DEBRIS ON ACTUATOR & MICROSWITCH FOUND ROLLER ON GEAR STICKING. CLEANED & LUBED ROLLER. LUBED UPLOCK ACTUATOR & MICROSWITCH. PERFORMED MULTIPLE GEAR SWINGS, OPS CHECK GOOD, NO OTHER DEFECTS NOTED AT THIS TIME. ALL WORK DONE IAW CESSNA 560 ULTRA MM 32-30-00. 2L72 4F RTA22CE 20050228001372005022800137EU 2005 2 28 DHL2005362003 120050216A3240 FAN AIRBUS300 A300B4203 3930306EU NR 3 BRAKE INOPERATIVE A DHLAO OTHER M OVER TEMP TXTAXI/GRND HDL 1 SO01362DH 84 CLEARING RUNWAY BRAKE NR 3 TEMP INDICATOR PEGGED HIGH AND BRAKE TEMP LIGHT ILLUMINATED. DURING ROLLOUT A/C WEAVED RIGHT SEVERAL TIMES AS IF A BRAKE ON THE RIGHT SIDE WAS NOT RELEASING. FOUND NR 3 BRAKE FAN INOP. REPLACED BRAKE FAN IAW MM 32-48-11. OP'S CHECKS GOOD. 2L72 4F RTA35EU 20050228001402005022800140WP 2005 2 28 05FDEA00249 120050205A5753ARC25121 HINGE DOUG DC10 DC1030F 3023504WP ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25304FE 46629 LEFT HAND OUTBOARD FLAP INBOARD HINGE, INBOARD PIVOT BORE CORRODED. REMOVED CORROSION, FABRICATED OVERSIZED BUSHING, INSTALLED AND HONED TO FINAL INSIDE DIAMETER OF 0.8745-0.8755 INCHES, IAW DAC CMM 57-52-02 AND FEDEX EA 8-5710-83965, WINGS- LEFT HAND OUTBOARD FLAP, INBOARD HINGE BRACKET OVERSIZED PIVOT BORE- REPAIR. PRIMED BORE IAW DC10-30 SRM 51-21-01 VOL II. 2L73 4F RTA22WE 20050228001442005022800144SO 2005 2 28 SWIA200514541 120050211A3040 RCCB EMB 120 EMB120ER 3260203SO WINDSHIELD SMOKE A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM07235SW 120310 TWENTY MINUTES INTO FLIGHT, SMOKE FROM LOWER LEFT PANEL OCCURRED. REPLACED AND SECURED LEFT WINDSHIELD RCCB, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050228001502005022800150NM 2005 2 28 05FDEA00237 120050203A5311ACA73511 FRAME DOUG MD11 MD11 3023602NM ZONE 200 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25620FE 48791 MAIN DECK - LEFT HAND SIDE FRAME G-NET ATTACHED YOKE ASSEMBLY AT STA Y=535 TOP AND BOTTOM REPAIR ANGLE FOUND WITH CHAFED MARK. MAIN DECK - LEFT HAND SIDE FRAME G-NET ATTACHED YOKE ASSEMBLY, CHAFED EXISTING REPAIR ANGLE AT STA Y=535, REMOVED PER SRM 51-31-01 VOLUME II. NEW REPAIR ANGLE FABRICATED AND INSTALLED PER FEDEX DRAWING SRM-53-503. 2L73 4F RTA22WE 20050228001542005022800154NM 2005 2 28 DL738050092 120050208A7930795740114 FILTER BOEING737 737832 13844CFNM GE CFM56 CFM567B24 NE NR 2 ENG OIL CLOGGED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27375DA 29623 875387 OIL FILTER BYPASS LIGHT ON RT ENGINE ILLUMINATED. REPLACED FILTER BOWL ASSY. 2L72 4F4 FRTA16WE E00055EN 20050228001612005022800161EU 2005 2 28 05FDEA00263 120050207A5312 BULKHEAD AIRBUS310 A310203 3930313EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25405FE 237 BULKHEAD 39 INTERIOR SIDE HAS CORROSION ON LWR FLANGE AND RT STRINGERS 43, 45, 46, 47, 49-50. REMOVED FWD AND AFT STRINGER TIES, BULKHEAD T-CHORD SPLICE ANGLES IAW A310-200 SRM 51-40-21. CLEANED CORROSION IAW A310-200 SRM 51-74-10 AND FOUND BULKHEAD WEB AT STR 51 OUT OF LIMITS. REMOVED DAMAGED SECTION AND INSTALLED FILLER, SHIMS, AND DOUBLER IAW EA6-5315-85548. REPLACED STR 55 END FITTING. REMAINING PARTS SERVICEABLE IAW EA 6-5315-86003. TREATED CORROSION AND PRIMED REMAINING STRUCTURE IAW A310-200 SRM 51-21-00. RE-ASSEMBLED BULKHEAD IAW A310-200 SRM 51-40-21. TOPCOATED AFFECTED AREA IAW A310-200 SRM 51-21-00. 2L72 4F RTA35EU 20050228001722005022800172NM 2005 2 28 SWAA050526 120050222A5210507945 MECHANISM BOEING737 7373H4 1384600NM L1 DOOR INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29606SW 27926 L1 DOOR WOULD NOT OPEN. INSTALLED RELEASE MECHANISM RETAINING SCREW PER MM. 2L72 4F RTA16WE 20050228001752005022800175NM 2005 2 28 SWAA050529 120050222A53116546529 FRAME BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND BS 440 FRAME CRACKED AT STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050228001852005022800185NM 2005 2 28 375PA0037 120050221A5330 SKIN BOEING737 73739A 138447PNM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05375PA 23812 AFT SERVICE DOOR TOP HINGE CUTOUT IN FUSELAGE SKIN CRACKED. REPAIRED PER SRM 53-60-01. 2L72 4F RTA16WE 20050228001982005022800198NM 2005 2 28 SWAA050487 120050218A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29687SW 23388 DURING SCHEDULED C1 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS FROM BS 756 TO BS 757, BETWEEN STRINGERS 21R AND 22R. REPAIRED SKIN SECTIONS PER SRM. 2L72 4F RTA16WE 20050228002002005022800200NM 2005 2 28 SWAA050489 120050218A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 867, STRINGER 23R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050228002112005022800211EA 2005 2 28 MASA200500129 120050218A3350487190 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSCRIMPED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07715SF 7115 ASH - PHL ONE SEGMENT OF THE FLOOR PATH LIGHTING INOP. MAINTENANCE REPLACED THE CONNECTOR. 2L72 4F RTA21EA 20050228002192005022800219EA 2005 2 28 COMA0560140 120050221A2621365000183 FIRE BOTTLE CNDAIRCL600 CL6002B19 1900309EA CARGO BAY MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01416CA252583572 7450 FLIGHT 9752 CARGO FIRE BOTTLE LOW CAUTION. REPLACED THE CARGO FIRE BOTTLE. 2L72 4F RTA21EA 20050228002202005022800220NM 2005 2 28 SWAA050530 120050222A53116546550 FRAME BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 827, STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050228002272005022800227WP 2005 2 28 05FDEA00256 120050205A5730 ACCESS PANEL DOUG DC10 DC1030F 3023504WP ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25304FE 46992 LEFT HAND WING LEADING EDGE SKIN CRACKED AT STATION XORS 530, AROUND REFUELING STATION ACCESS PANEL INBOARD CORNER. COMPLIED WITH EA 8-5710-8352, WINGS- LEFT HAND LEADING EDGE TEE CRACK AT REFUELING DOOR CUTOUT- REPAIR. 2L73 4F RTA22WE 20050228002312005022800231NM 2005 2 28 SWAA050533 120050222A534065C27314 STRINGER CLIP BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP AT BS 807, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20050228002322005022800232NM 2005 2 28 SWAA050534 120050222A534065C27314 STRINGER CLIP BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND 2 EA CRACKED STRINGER CLIPS BETWEEN BS 767 AND BS 787 STR 11L. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20050228002422005022800242NM 2005 2 28 SWAA050538 120050222A534065C27314 STRINGER CLIP BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP AT BS 727D, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20050228002472005022800247SO 2005 2 28 SIMA200501902 120050118A4950 SMOKE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL CABIN DETECTED A SIMAO OTHER B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW21646AE 145213 SMOKE IN CABIN REPORTED BY CREW AFTER APU START. APU PUT ON MEL AT THIS TIME. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. SEVERAL STARTS WERE PERFORMED WITH NO SMOKE NOTED. MEL WAS RESTORED AND AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4T4 FRTT00011ATTE6CH 20050228002492005022800249SO 2005 2 28 SIMA200500907 120050101A3350110049 CHARGER EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL CABIN INOPERATIVE A SIMAK NONE L NO TEST TXTAXI/GRND HDL 1 SW21817AE 145554 CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHTS AT ROWS 7 THROUGH 11 TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 EMERGENCY BATTERY CHARGER IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200503041) (K) 2L72 4F4 FRTT00011ATTE6CH 20050228002622005022800262SO 2005 2 28 SIMA200502504 120050123A2120 ODOR EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL CABIN DETECTED A SIMAK NONE B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW21639AE 145182 DURING TAXI CREW REPORTED FUEL SMELL IN THE CABIN AND COCKPIT. PASSENGER REPORTED THE SMELL AT ROW 8. MAINTENANCE GROUND RUN ENGINES TO CHECK AIR CONDITION SYSTEM FOR FUEL ODOR. NONE WAS DETECTED AT THIS TIME. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200503049) (K) 2L72 4T4 FRTT00011ATTE6CH 20050228002652005022800265SO 2005 2 28 SIMA200502803 120050127A3350 LIGHT EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL CABIN MALFUNCTIONED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21834AE 145631 EMERGENCY FLOOR LIGHTING AT ROWS 7 THRU 11 DIM AFTER 30 SECONDS. PERFORMED OPERATIONAL CHECK OF EMERGENCY FLOOR LIGHTS WITH NO DISCREPANCIES NOTED. RETURNED TO SERVICE. (SW21200503032) (K) 2L72 4F4 FRTT00011ATTE6CH 20050228003122005022800312SO 2005 2 28 SIMA200501205 120050106A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21846AE 145692 DURING AN INSPECTION, THE LT OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE DAMAGED AREA TO REMOVE CORROSION. FABRICATED A FILLER, DOUBLER AND 2 SHIMS. REPAIR DONE IAW SRM. (SW21200502476) (K) 2L72 4F4 FRTT00011ATTE6CH 20050228003232005022800323SO 2005 2 28 SIMA200501909 120050113A532014522459003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21738NR 145401 DURING CPCP INSPECTION MAINTENANCE FOUND THE FORWARD CABIN FLOOR SUPPORT AT FRAME 20 HAS CORROSION THROUGH AFT END AT LAP JOINT WITH GUSSET. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM. AIRCRAFT RETURNED TO SERVICE. (SW21200502486) (K) 2L72 4F4 FRTT00011ATTE6CH 20050301000022005030100002SO 2005 3 1 C2XA05BT010 120050202A32347455503 CONTROL LEVER EMB 145 EMB145ER 3260211SO MLG FAULTY A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2715926 145005 CREW REPORTED, LANDING GEAR LEVER/DISAGREEMENT WARNING ON RETRACTION, NOSE GEAR RED HATCHED INDICATION. PERFORMED CHECKLIST, RECYCLED GEAR, GEAR INDICATED NORMAL AFTER RECYCLE. EXTENDED NORMALLY FOR AIR-RETURN LANDING IN NEWARK. MAINTENANCE REMOVED AND REPLACED LANDING GEAR LEVER IAW EMB145 MM 32-32-01. PERFORMED LANDING GEAR OPERATIONAL CHECK MULTIPLE TIMES, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20050301000042005030100004NM 2005 3 1 QXEA200500210 120050202A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 PDX - RT INBOARD SEAT TRACK CORROSION APPROXIMATELY X696. REPAIRED IAW RD 8/4-53-884. 2H72 4T RTA13NM 20050301000292005030100029NM 2005 3 1 UPS05443930 120050208A5312 BULKHEAD BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, BS 1480 BULKHEAD APU DUCT CUTOUT FOUND 3 FASTENER HOLES CRACKED. BS 1480 BULKHEAD REPAIRED PER SB 747-53-2309 UPS EO B747-5310-3100-C & DWG 144U2602. 2L74 4F A20WE 20050301000372005030100037EA 2005 3 1 SWIA200514626 120050221A5610 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAO OTHER O OTHER CRCRUISE 1 NM07913SW 7597 LEFT SIDE WINDOW ON FLIGHT DECK SHATTERED IN FLIGHT AT FL350, DELTA WAS 8.2. OUTER AND CORE SHATTERED. REMOVED AND REPLACED LT SIDE WINDOW ON FLIGHT DECK IAW CRJ 200 MM ATA CHPT 56-12-01. OPERATIONAL CHECK GOOD. P/N OFF 601R33033-11, S/N OFF 01176H1629. 2L72 4F RTA21EA 20050301000392005030100039SO 2005 3 1 SWIA200514628 120050220A27523430001007 ACTUATOR EMB 120 EMB120ER 3260203SO OUTBOARD FLAP MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07584SW8352 8352 120352 REPEATED FLAP CONTROL FAULTS (APPROX 5) DURING CLIMB, CRUISE, DESCENT. REPLACED LEFT FLAP OUTBOARD FLAP ACTUATOR WITH SERVICEABLE UNIT IAW MM 27-50-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050301000792005030100079EA 2005 3 1 A6WA200540040 120050202A1430 FASTENER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE WING MISLOCATED A A6WAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL31414ZW 7586 UNABLE TO ACHIEVE EDGE DISTANCE ON JOINT STRAP (PN 601R1004654) WHILE COMPLYING WITH SB 601R57037 DUE TO EXISTING FASTENER BEING MISLOCATED. PERFORMED A MAJOR ALTERATION TOO, BY SHIFTING THE CUTLINE TO PROVIDE MINIMUM EDGE DISTANCE ON THE EXISTING FASTENERS, FABED NEW DOUBLE IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050301000882005030100088EA 2005 3 1 A6WA200540032 120050126A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31414ZW 7586 CABIN FLOOR SUPPORT STRUCTURE AT FS280, LBL 9.0. THE OB CLIP IS CRACKED IN RADIUS AT TOP. (K) REMOVED CRACKED CLIP AND INSTALLED NEW FABRICATED CLIP IAW BRAS EO 601R-53-5924. (M) 2L72 4F4 FRTA21EA E15NE 20050302000022005030200002NE 2005 3 2 ALG2005F00014 120050124A32977655200110107 WIRE HARNESS SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL NLG UNSERVICEABLE E ALGAK NONE N FALSE WARNING TXTAXI/GRND HDL 1 SW03518AL 760134 ON RUN-UP, LANDING GEAR NOSE WHEEL GREEN LIGHT GOES OFF AND RED UNSAFE LIGHT COMES ON (KEEPS REPEATING), GREEN LIGHT COMES ON AND THE RED LIGHT GOES OUT. MAINTENANCE REMOVED LT NOSE WHEEL HARNESS (DOWN AND LOCK) AND INSTALLED SERVICEABLE HARNESS, OPS CHECK OF THE SYSTEM WAS FOUND TO BE OK. (K) 1G72 3U3 U H1NE E1GL 20050302000252005030200025NM 2005 3 2 AMTA200500169 120050213A2613 WARNING SYSTEM BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE COCKPIT ACTIVATED A AMTAK NONE J WARNING INDICATION CRCRUISE 1 GL11559TZ 32593 STATUS MSG R TURB OH DET 2 DISPLAYED. PERFORMED FIM 26-13-00, FIGS 103 AND 104 MSG. 2L72 4F4 FRTA2NM E12EU 20050302000732005030200073NM 2005 3 2 AMTA200500135 120050203A1430 FASTENER BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE FUSELAGE LIGHTNING STRIKEA AMTAK NONE O OTHER ININSP/MAINT 1 GL11515AT 27598 LIGHTNING STRIKE DAMAGE TO FASTENER IN THE FS 900 BUTT JOINT BETWEEN THE S4R LAP SPLICE AND STRINGER S3R. COMPLIED WITH ERA. 2L72 4F4 FRTA2NM E12EU 20050302000862005030200086EU 2005 3 2 USAA050035 120050101A5320D5347112420000 WEB AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19713UW17339 1040 BFM - S1 - WEB, 1 INCH L X 1 INCH W X .06 INCH D, CORROSION; LEVEL 2; TASK NR JA260-53500, FR 69-70, Y1292 MAIN CABIN FLOOR SUPPORT WEB. REMOVED AND REPLACED WEB IAW SRM. (K) 2L72 4F4 FRTA28NM E37NE 20050302001022005030200102NM 2005 3 2 USAA050106 120050101A5320 INTERCOSTAL BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19517AU53410 23703 PIT - Q6 - INTERCOSTAL, .5 INCH CRACK; LT AND RT SIDES OF FWD ATTACH ANGLE AND INTERCOSTAL BELOW CABIN FLOOR STA 254 BL0. MANUFACTURED NEW INTERCOSTAL IAW MFG DWG 65-45833 AND SRM 51-20-01, 51-40-00. (K) 2L72 4F4 FRTA16WE E21EU 20050302001062005030200106NM 2005 3 2 USAA050104 120050101A5320 CHANNEL BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19517AU53410 23703 PIT - Q6 - L CHANNEL, 2 INCH LONG BETWEEN NUT PLATES CRACKED; S5A STRINGER LT SIDE STA 1140 TO 1145. REMOVED AND REPLACED STRINGER AND DOUBLERS IAW SRM 53-00-01 AND FIG 221 AND TYP REP 53-80-40. (K) 2L72 4F4 FRTA16WE E21EU 20050302001222005030200122EU 2005 3 2 USAA050037 120050101A5320D53480093204 SILL AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19713UW17339 1040 BFM- S1- SILL , 1.0 INCH X 1.0 INCH X .06 INCH, CORROSION; LEVEL 2; TASK NR JA260-53500, FR 65-66, Y 1732, Z240. REMOVED AND REPLACED SILL IAW SRM. (K) 2L72 4F4 FRTA28NM E37NE 20050302001482005030200148NM 2005 3 2 USAA050171 120050101A5315 FLOORBEAM BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19521AU 23856 PIT - FOUND FLOORBEAM CORRODED 18 INCHES LONG, LBBL 8 STATION 344. CORROSION LEVEL 1. WEB MFG PER 53-00-51 FIG 202. (M) 2L72 4F RTA16WE 20050302001502005030200150NM 2005 3 2 USAA050174 120050101A5320 SUPPORT BRACKET BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19521AU52728 23856 FOUND WALL SUPPORT BRACKET CORRODED 1 INCH BY .5 INCH AREA AROUND 6 SCREW HOLES, STATION 500D 26R-26L. REMOVED AND REPLACED WALL SUPPORT BRACKET. (M) 2L72 4F RTA16WE 20050302001572005030200157NM 2005 3 2 USAA050192 120050112A532065C333671 INTERCOSTAL BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19436US41647 24558 PIT - FOUND INTERCOSTAL CORRODED 2 INCH BY 2 INCH AND 4 INCH BY 4 INCH, BS 947 TO 967 LBL 50. CORROSION LEVEL 1, TASK C53-107-102. REPLACED WITH BOEING PART PER SRM 51-40-04. (M) 2L72 4F RTA16WE 20050302001582005030200158NM 2005 3 2 USAA050196 120050116A53201123759 ANGLE BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19436US41647 24558 PIT - FOUND Z-ANGLE CORRODED 4 INCH BY 8 INCH AREA, AT NUT PLATE HOLES, RT Z-ANGLE AT AFT SERVICE DOOR BS 950-990. REMOVED AND REPLACED Z-ANGLE PER SRM 51-40-00. (M) 2L72 4F RTA16WE 20050302001612005030200161NM 2005 3 2 USAA050190 120050101A53201133482 TIE CLIP BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19436US41647 24558 PIT - FOUND STRINGER TIE CLIP CRACKED, .5 INCH IN RADIUS AREA, STRINGER TIE CLIP, STATION 1006, STRINGER 2R. DEFECTIVE PART REPLACED WITH IDENT PART PER TYPICAL REPAIR 57-50-55. (M) 2L72 4F RTA16WE 20050302001622005030200162NM 2005 3 2 USAA050197 120050120A5755 SUPPORT FITTING BOEING737 7374B7 1384702NM NR 4 SPOILER CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19436US41647 24558 PIT - FOUND SPOILER CHAFED .5 INCH, NR 4 GROUND SPOILER INBOARD SUPPORT FITTING. INSTALLED ANGLE PER TYP REPAIR 57-50-14. (M) 2L72 4F RTA16WE 20050302001672005030200167NM 2005 3 2 USAA050074 120050101A5310 CREASE BEAM BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19522AU49282 23857 PIT - FOUND CREASE BEAM CRACKED 2.5 INCHES, AFT OF FRAME 616 RT SIDE CREASE BEAM. MODIFIED PART INSTALLED PER TYPICAL REPAIR 53-10-02 REV A. (M) 2L72 4F RTA16WE 20050303000012005030300001NM 2005 3 3 SWAA050581 120050225A53146545866 KEELBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29320SW 23341 DURING SCHEDULED C1 CHECK, FOUND LT KEELBEAM CORRODED AT BS 540. REPAIRED KEEL BEAM PER SRM. 2L72 4F RTA16WE 20050303000022005030300002 2005 3 3 SWAA050582 420050226A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 DURING SCHEDULED RON CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. REINSTALLED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050303000032005030300003 2005 3 3 SWAA050583 420050227A25656551463 LATCH BOEING737 7377H4 1384404NM GIRT BAR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29772SW 27880 R1 DOOR EVAC SLIDE GIRT BAR LATCH OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE GIRT BAR LATCH PER MM. 2L72 4F RTA16WE 20050303000052005030300005NM 2005 3 3 SWAA050585 120050226A2560P4010021 BATTERY BOEING737 7373H4 1384600NM FLASHLIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 DURING SCHEDULED SERVICE CHECK, FOUND 2 EA CABIN EMERGENCY FLASHLIGHTS INOP AT FWD AND AFT CABIN. REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERIES PER MM. 2L72 4F RTA16WE 20050303000062005030300006EA 2005 3 3 SWIA200514634 120050222A2760C13045BA03 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA GROUND SPOILERS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07730SK 10193 INBOARD GROUND SPOILER FAULT STATUS MESSAGE. REPLACED NR 1 SSCU. OPERATIONAL CHECK GOOD IAW CRJ AMM REF CHAP 27-60-00. 2L72 4F RTA21EA 20050303000072005030300007EA 2005 3 3 SWIA200514635 120050215A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA FLOORBEAM CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07699BR 7801 CLIP AT STA 625 RIGHT SIDE APPROX STR 15 IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. 2L72 4F RTA21EA 20050303000122005030300012EA 2005 3 3 QXEA200500201 120050124A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - LEFTHAND OUTBOARD SIDE FACING SEATRAIL AT STATION 550 TO 569 HAD PITTING CORROSION. REPAIRED IAW CRJ700 REO 670-53-00-060, REV B AND HORIZON AIR EA R-53-266. 2L72 4F RTA21EA 20050303000142005030300014NM 2005 3 3 QXEA200500208 120050209A5347 CARGO TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 PDX - AFT CARGO LEFTHAND INBOARD TRACK CORROSION ON OUTBOARD FLANGE APPROXIMATELY X672 TO X691. REPAIRED IAW DHC-8 400 SRM 51-42-05-330-801. 2H72 4T RTA13NM 20050303000152005030300015NM 2005 3 3 QXEA200500209 120050202A5347 CARGO TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 PDX - AFT CARGO RIGHTHAND INBOARD TRACK CORROSION ON OUTBOARD FLANGE APPROXIMATELY X672 TO X692. REPAIRED IAW DHC-8-4- SRM 51-42-05 AND SRM 51-40-10. 2H72 4T RTA13NM 20050303000172005030300017NM 2005 3 3 P5CA0501321 120050212A2150 SMOKE BOEING747 747123 1384873NM AIR CON SYS DETECTED A P5CAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 EA15858FT 20109 CREW REPORTED WHEN POWER WAS REDUCED FOR DESCENT. SMOKE WAS SEEN COMING FROM AIR CONDITIONING SYSTEM. GRADUALLY REDUCED TO NOTHING OVER 15 MINUTES TIME. INSPECTED AIR CONDITIONING SYSTEM AND ACM’S. PERFORMED OPERATION CK PER 21-20-00. NO DEFECTS NOTED. OPS NORMAL. 2L74 4F A20WE 20050303000182005030300018NM 2005 3 3 SWAA050565 120050224A3350207377 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29462WN 32466 FWD END OF EEPLS LENS MISSING. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20050303000212005030300021NM 2005 3 3 SWAA050568 120050224A55236959227 BUSHING BOEING737 7373H4 1384600NM RT ELEVATOR TAB WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29358SW 26595 DURING SCHEDULED C1 CHECK, RT ELEVATOR TAB FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED UPPER & LOWER BUSHINGS, PUSHROD BOLT & TAB MECHANISM LINKS PER MM. 2L72 4F RTA16WE 20050303000222005030300022NM 2005 3 3 SWAA050569 120050224A3350079123 COVER BOEING737 7373H4 1384600NM EMERGENCY LIGHT WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29627SW 27935 DURING SCHEDULED C2 CHECK, FOUND FWD END OF EEPLS COVER WORN. REMOVED AND REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20050303000232005030300023EA 2005 3 3 050546234 120050223A5310 DOOR FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27623BR 7192 PAX DOOR FRAME TOP RADIUS CRACKED AT 1 INCH IN LENGTH FORWARD OF DATUM 1 AT FS 320.90. 2L72 4F RTA21EA 20050303000262005030300026WP 2005 3 3 NACA20050066 120050112A326020HS2 DOWNLOCK SWITCH DOUG DC6 DC6 3021702WP RT MLG FROZEN A NACAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 AL0343872 533294 RIGHT MAIN LANDING GEAR WARNING LIGHT SHOWING GEAR NOT DOWN AND LOCKED. REPLACED RIGHT MAIN LANDING GEAR DOWNLOCK SWITCH. CHECKED GOOD. FOUND WATER FROZEN IN RIGHT MAIN GEAR DOWNLOCK SWITCH. 2L74 4R A781 20050303000272005030300027NM 2005 3 3 SWAA050572 120050224A53106546579 SHEAR TIE BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND CORROSION ON SHEAR TIE AT BS 907, BL 0, WL 160. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050303000282005030300028NM 2005 3 3 SWAA050573 120050224A321165461067 FITTING BOEING737 7373Q8 1384670NM LT MLG STRUT CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND CORROSION ON LT MLG LOWER STRUT FITTING. REMOVED AND REPLACED LT MLG LOWER STRUT FITTING PER MM. 2L72 4F RTA16WE 20050303000292005030300029NM 2005 3 3 SWAA050574 120050224A53106545815 SHEAR TIE BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND CORROSION ON SHEAR TIE AT BS 344, RBL 17. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050303000302005030300030NM 2005 3 3 SWAA050575 120050224A53306545774 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29512SW 24189 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACK AT BS 750, STR 23L. REPAIRED FUSELAGE SKIN PER SRM. 2L72 4F RTA16WE 20050303000312005030300031NM 2005 3 3 SWAA050576 120050224A3350D71701100 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29704SW 27838 DURING SCHEDULED HC2 CHECK, FOUND EMERGENCY EXIT LIGHTS, LT SIDE, CENTER CABIN INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM. 2L72 4F RTA16WE 20050303000332005030300033EA 2005 3 3 050546235 120050223A5310 DOOR FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27623BR 7192 PAX DOOR FRAME TOP RADIUS CRACKED AT 1 INCH IN LENGTH FORWARD OF DATUM 1 AT FS 338.90. 2L72 4F RTA21EA 20050303000342005030300034EA 2005 3 3 050546236 120050223A5210 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27623BR 7192 PAX DOOR INTERCOSTAL TOP RADIUS CRACKED AT 1 INCH IN LENGTH AT DATUM 1 FS 338. 2L72 4F RTA21EA 20050303000362005030300036EA 2005 3 3 050546238 120050223A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27623BR 7192 RIGHT FS 718 FRAME CRACKED AT 1 INCH IN LENGTH. CRACK IS BELOW EXISTING REPAIR. 2L72 4F RTA21EA 20050303000372005030300037NM 2005 3 3 SWAA050578 120050224A53206545410 FLOOR SUPPORT BOEING737 7375H4 138449DNM CENTER WING BOX CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29507SW 24184 DURING SCHEDULED 1/2D CHECK, FOUND 3 EA CRACKS AT NR 2 LONGITUDINAL FLOOR SUPPORT AT BS 656, BS 665, & BS 669. REPAIRED BEAM PER SWA EA. 2L72 4F RTA16WE 20050303000392005030300039NM 2005 3 3 SWAA050580 120050224A53306545819 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29320SW 23341 DURING SCHEDULED C1 CHECK, FOUND SKIN CRACKED ON RT SIDE OF NLG WW AT BS 259, WL 174. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050303000402005030300040NM 2005 3 3 SWAA050586 120050227A2560P2070001 FLASHLIGHT BOEING737 7373H4 1384600NM AFT CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 DURING SCHEDULED SERVICE CHECK, FOUND 1 EA EMERGENCY FLASHLIGHT CRACKED AT AFT CABIN. REMOVED AND REPLACED EMERGENCY FLASHLIGHT PER MM. 2L72 4F RTA16WE 20050303000412005030300041NM 2005 3 3 SWAA050587 120050226A3350207377 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29427WN 29831 DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LENS ASSY PER MM. 2L72 4F RTA16WE 20050303000442005030300044NM 2005 3 3 SWAA050590 120050225A3350079123 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29462WN 32466 FWD END OF EEPLS COVER LOOSE. REINSTALLED EEPLS COVER PER MM. 2L72 4F RTA16WE 20050303000452005030300045NM 2005 3 3 SWAA050591 120050226A335090083 BATTERY BOEING737 7375H4 138449DNM R1 DOOR INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29523SW 26565 DURING SCHEDULED SERVICE CHECK, FOUND R1 DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050303000492005030300049NM 2005 3 3 SWAA050612 120050228A335065C27095 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INTERMITTENT A SWAAO OTHER O OTHER NRNOT REPORTED 1 SW29743SW 29279 CABIN EMERGENCY BULLNOSE LIGHTS INTERMITTENT DURING FLIGHT. REMOVED AND REPLACED BULLNOSE LIGHTS BATTERY PACK PER MM. 2L72 4F RTA16WE 20050303000502005030300050NM 2005 3 3 SWAA050613 120050228A53116546529 FRAME BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 9R. REPAIRED FUSELAGE FRAME PER SRM. 2L72 4F RTA16WE 20050303000512005030300051NM 2005 3 3 SWAA050614 120050228A531169353656 FRAME BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACK AT BS 380, STR 9R. REPAIRED FUSELAGE FRAME PER SRM. 2L72 4F RTA16WE 20050303000522005030300052NM 2005 3 3 SWAA050615 120050228A53116545805 FRAME BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 277, STR 14R. REPAIRED FRAME WEB PER SRM. 2L72 4F RTA16WE 20050303000532005030300053NM 2005 3 3 SWAA050616 120050228A53116545810 FRAME BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 303.9, STR 4L. REPAIRED FRAME WEB PER SRM. 2L72 4F RTA16WE 20050303000562005030300056NM 2005 3 3 SWAA050594 120050225A5313BAC1498 STRINGER BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON FUSELAGE STRINGER SPLICE BETWEEN BS 350 & BS 370, STR 28R. REPAIRED FUSELAGE STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20050303000572005030300057NM 2005 3 3 SWAA050595 120050225A531069353656 SHEAR TIE BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON SHEAR TIE AT BS 380, LBL 5 TO RBL 5, WL 148. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050303000592005030300059NM 2005 3 3 SWAA050597 120050225A55516551524 FITTING BOEING737 7373Q8 1384670NM HORIZONTAL STABSCORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND LT & RT HORIZONTAL STAB FITTING LUG FACES CORRODED. REPAIRED HORIZONTAL LUG FITTINGS PER SRM. 2L72 4F RTA16WE 20050303000612005030300061NM 2005 3 3 SWAA050601 120050225A53116546529 FRAME BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 9R. REPAIRED FUSELAGE FRAME PER SRM. 2L72 4F RTA16WE 20050303000622005030300062NM 2005 3 3 SWAA050602 120050225A53206551698 SPLICE BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER SPLICE CRACKED AT BS 360, STR 15L. REPAIRED FUSELAGE STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20050303000642005030300064NM 2005 3 3 SWAA050604 120050225A53106547978 CREASE BEAM BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND CORROSION ON LT CREASE BEAM WEB AT BS 727D, LBL 68. REPAIRED CREASE BEAM WEB PER SRM. 2L72 4F RTA16WE 20050303000652005030300065NM 2005 3 3 SWAA050605 120050225A534065C27314 STRINGER CLIP BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 DURING SCHEDULED SPECIAL VISIT, FOUND CRACKED STRINGER CLIP AT BS 807, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20050303000662005030300066NM 2005 3 3 SWAA050606 120050227A57436959886 FITTING BOEING737 7373H4 1384600NM LT WING CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29652SW 27722 DURING SCHEDULED SERVICE CHECK, FOUND CORROSION ON LT MLG STABILIZER FITTING. REMOVED AND REPLACED LT MLG STAB FITTING PER MM. 2L72 4F RTA16WE 20050303000672005030300067NM 2005 3 3 SWAA050607 120050227A53306545776 SKIN BOEING737 7375H4 138449DNM FUSELAGE WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29507SW 24184 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN, UPPER LOBE, WORN BETWEEN BS 870 & BS 887, RT SIDE & BETWEEN BS 878 & BS 880, LT SIDE. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050303000682005030300068NM 2005 3 3 SWAA050608 120050227A5313BAC1498 STRINGER BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29507SW 24184 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED STRINGER AT BS 360, STR 15L. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20050303000692005030300069NM 2005 3 3 SWAA050609 120050227A53126547978 PRESSURE PANEL BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29329SW 23693 DURING SCHEDULED QD CHECK, FOUND FUSELAGE BEADED PRESSURE WEB CRACKED AT BS 665, LBL 30. REPAIRED FUSELAGE WEB PER SRM. 2L72 4F RTA16WE 20050303000702005030300070NM 2005 3 3 SWAA050610 120050227A57436582770 FITTING BOEING737 7373H4 1384600NM LT WING CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29329SW 23693 DURING SCHEDULED QD CHECK, FOUND CORROSION ON LT MLG STABILIZER BEAM ATTACH FITTING. REMOVED AND REPLACED LT MLG STABILIZER BEAM ATTACH FITTING PER MM. 2L72 4F RTA16WE 20050228001742005022800174NM 2005 2 28 SWAA050528 120050222A33506574550 LIGHT BOEING737 7373Q8 1384670NM R2 DOOR INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND R2 DOOR ESCAPE SLIDE LIGHT INOP. REMOVED AND REPLACED LIGHT HOUSING PER SRM. 2L72 4F RTA16WE 20050228001992005022800199NM 2005 2 28 SWAA050488 120050218A541569765171 ANGLE BOEING737 7373Q8 1384670NM NR 2 ENG PYLON CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29687SW 23388 DURING SCHEDULED CHECK, FOUND NR 2 ENGINE UPPER PYLON ATTACH ANGLE, CRACKED. REMOVED AND REPLACED ATTACH ANGLE PER EA. 2L72 4F RTA16WE 20050228002062005022800206NM 2005 2 28 SWAA050495 120050219A2612 FIRE DETECTOR BOEING737 7373H4 1384600NM CARGO BAY FALSE INDICATIONA SWAAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 SW29607SW 27927 DIVERSION, DECLARED EMERGENCY. FWD CARGO FIRE LIGHT ILLUMINATED ON DEPARTURE, DISCHARGED BOTH BOTTLES. INSPECTED BOTH FWD AND AFT CARGO BINS, PER MM, NO DEFECTS NOTED. 2L72 4F RTA16WE 20050228002182005022800218EA 2005 2 28 COMA0560139 120050221A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01455CA 7592 FLIGHT 5239 FLAPS FAIL CAUTION DURING TAXI. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20050228002242005022800224SO 2005 2 28 CHQA200500038 120050220A2611 SMOKE DETECTOR EMB 145 EMB145LR 3260212SO LAVATORY FALSE INDICATIONA CHQAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL11576RP 14500856 AFTER TAKEOFF A LAV SMOKE INDICATION APPEARED ON EICAS. NO VISUAL SMOKE WAS NOTED. RETURNED TO THE FIELD. INSPECTED LAVATORY SMOKE DETECTOR AND PERFORMED SMOKE DETECTOR TEST IAW EMB 145 AMM 26-15-00. PERFORMED TAKEOFF POWER GROUND ENGINE RUNS. NO DEFECTS NOTED. 2L72 4T RTT00011AT 20050228002252005022800225NM 2005 2 28 DLM88050102 120050210A253050459 OVEN DOUG MD88 MD88 3023688NM F/C GALLEY SMOKE A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27947DL 49878 F/C OVEN SMOKES EXCESSIVELY WHEN TURNED ON. REPLACED OVEN IN F/C GALLEY. OPS CHECK OK. 2L72 4F RTA6WE 20050228002452005022800245EU 2005 2 28 RAIA00502023 120050215A3150 SWITCH JETAIRJETSTMJETSTM4101 1500501EU SPOILERS OUT OF ADJUST A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03563HK 41079 TAKEOFF CONFIGURATION WARNING ON TAKEOFF. MAINTENANCE TROUBLESHOT AND DEFERRED GROUND SPOILER SYSTEM PER MEL. ADJUSTED LEFT CONDITION LEVER SWITCH. 2L72 4T RTA41NM 20050228002482005022800248SO 2005 2 28 SIMA200502502 120050116A532014525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21735TS 145386 DURING AN INSPECTION MAINTENANCE FOUND A PREVIOUS REPAIR ON THE LT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. REMOVED THE CORRODED REPAIR PARTS. FABRICATED A DOUBLER, FILLER, PLATE AND TWO SHIMS. REPAIR DONE IAW SRM. (K) 2L72 4F4 FRTT00011ATTE6CH 20050228002502005022800250SO 2005 2 28 SIMA200502401 120050121A5610NP15131111 WINDSHIELD EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL CABIN CRACKED A SIMAA UNSCHED LANDING O OTHER CLCLIMB 1 SW21842AE 145673 ON CLIMB OUT AT 11,000 FL CAPTAINS WINDSCREEN SHATTERED RETURNED TO AIRPORT, LANDED SAFELY. NO LOSS OF CABIN PRESSURIZATION. REPLACED CAPTAIN WINDSHIELD. AC RETURNED TO SERVICE. (SW21200503048) (K) 2L72 4F4 FRTT00011ATTE6CH 20050228002512005022800251SO 2005 2 28 SIMA200500402 120050101A3350110049 CHARGER EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL CABIN INOPERATIVE A SIMAK NONE L NO TEST TXTAXI/GRND HDL 1 SW21817AE 145554 EMERGENCY FLOOR LIGHTS AT ROWS 7 THROUGH 11 INOPERATIVE. REPLACED NR 3 EMERGENCY BATTERY CHARGER. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200503043) (K) 2L72 4F4 FRTT00011ATTE6CH 20050228002592005022800259SO 2005 2 28 SIMA200401901 120050116A3350110049 POWER SUPPLY EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL CABIN DISCHARGED A SIMAK NONE L NO TEST TXTAXI/GRND HDL 1 SW21718AE 145275 CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHT AFT OF ROW 9 TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 BATTERY POWER SUPPLY UNIT IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4F4 FRTT00011ATTE6CH 20050228002902005022800290SO 2005 2 28 SIMA200500911 120050105A361014536587402 COUPLING EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL BLEED AIR SYS DAMAGED A SIMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21653AE 145433 CREW REPORTED A BLEED 1 LEAK FOLLOWED BY A LOUD BANG FOLLOWED BY A BLEED 2 MESSAGE. CREW DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RT BLEED COUPLING IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200502363) (K) 2L72 4T4 FRTT00011ATTE6CH 20050301000012005030100001NE 2005 3 1 NACA20050006 220050224A8530356994 CYLINDER DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE NR 17 CRACKED A NACAE ENGINE SHUTDOWN K FLUID LOSS TXTAXI/GRND HDL 1 AL036174C976 976 44075 P33324 NR 1 ENGINE FEATHERED ON GROUND DUE TO OIL LEAK. REPLACED NR 17 CYLINDER DUE TO A CRACKED HEAD. OP AND LEAK CHECK GOOD. 2L74 4R4 R 6A3 5E8 20050301000032005030100003EA 2005 3 1 QXEA200500200 120050121A7110 COWLING CNDAIRCL600 CL6002C10 1390015EA ZONE 400 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - RT UPPER CORE COWL, FORWARD STRUCTURE, JUST FORWARD OF HEAT SHIELD HAD CHAFE DAMAGE. REPAIRED IAW CRJ700 SRM 51-25-06-001-001-A01, REO 670-54-23-325 AND HORIZON AIR EA R-54-72. 2L72 4F RTA21EA 20050301000222005030100022NM 2005 3 1 UPS05443922 120050210A5730 SKIN BOEING747 747123 1384873NM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE:C, RHW REAR SPAR UPPER SPLICE FITTING AT BS 1241 FOUND CRACKED AT HOLE NR 7 AT SKIN APPROX 0.040 INCH. HOLE REWORKED PER BSB 747-57A2314. 2L74 4F A20WE 20050301000262005030100026NE 2005 3 1 P5CA0501324 220050222A7200 ENGINE BOEING747 747283B 1384867NM PWA JT9 JT9D70A 52054NE NR 1 MALFUNCTIONED A P5CAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 EA15921FT 21575 689167 CREW REPORTED NR 1 ENGINE WOULD NOT MAKE TAKEOFF EPR. INSPECTED NR 1 ENGINE PER MM 71-00-00, OPENED MEL 77-4-1 FOR EPR UNRELIABLE. 2L74 4F4 F A20WE E3NE 20050301000362005030100036EA 2005 3 1 SWIA200514625 120050220A27604916406 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07452SW6143 6143 7716 FLIGHT SPOILER AND INBOARD GROUND SPOILER MSG (STATUS) WILL NOT CLEAR. REMOVED AND REPLACED NR 2 SECU WITH A SERVICEABLE SECU IAW 27-00-00. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050301000952005030100095EA 2005 3 1 A6WA200540029 120050131A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31414ZW 7586 LT FS 621.00 ANGLE IS CRACKED. CUT AWAY DAMAGED SECTION OF ANGLE AND INSTALLED A REPAIR ANGLE IAW REO. (K) 2L72 4F4 FRTA21EA E15NE 20050301001112005030100111NM 2005 3 1 AMTA200500046 120050116A5330 SKIN BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE FUSELAGE LIGHTNING STRIKEA AMTAK NONE O OTHER ININSP/MAINT 1 GL11515AT 27598 LIGHTNING STRIKE DAMAGE TO SKIN OF AIRCRAFT, FS 627 AT S-5L. REPAIRED DAMAGE IAW ERA. (K) 2L72 4F4 FRTA2NM E12EU 20050301001252005030100125NM 2005 3 1 USAA050163 120050106A5314 KEELBEAM BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19521AU52728 23856 PIT - Q6 - KEELBEAM, 1 INCH CRACK; STA540 39R; REPLACED SECTION OF FWD KEELBEAM, SPLICES MFGD IAW TYP REP 53-60-09. (K) 2L72 4F4 FRTA16WE E21EU 20050301001292005030100129NM 2005 3 1 USAA050093 120050101A575465C2660399A SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU L/E SLAT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19517AU53410 23703 PIT - Q6 - RIVET HOLES, .1250 INCH TO .2500 INCH - 7 RIVET HOLES, CRACKED; LWR SKIN AFT FASTENER ROW CENTERED ON SLAT ACT. AREA. INSTALLED DOUBLER IAW SRM 57-43-01.(K) 2L72 4F4 FRTA16WE E21EU 20050301001322005030100132NM 2005 3 1 USAA050096 120050101A5320 ANGLE BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19517AU 23703 PIT - Q6 - L ANGLE, 1.2500 INCH CRACK; L ANGLE FOR 360 FRAME AT STR 14L. MANUFACTURED NEW L ANGLE IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050302000422005030200042CE 2005 3 2 S2YA05004 120050106A3610 BLEED AIR SYS BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE RIGHT MALFUNCTIONED A S2YAA UNSCHED LANDING O OTHER CLCLIMB 1 GL1392SK UE92 BEFORE FLIGHT, THE CREW REPORTED A RT BLEED AIR PROBLEM, THEY CONSULTED WITH MECHANIC WHO INSTRUCTED THE CREW TO RUN THE ENGINES TO LET THE SYSTEM WARM UP. AFTER RUNNING THE ENGINES THE PROBLEM COULD NOT BE DUPLICATED. WITH NO FURTHER DISCREPANCIES NOTED THE AC WAS RETURNED TO SERVICE. SHORTLY AFTER TAKEOFF OF FLIGHT, THE CREW REPORTED A RT BLEED AIR PROBLEM, THEY CONSULTED WITH MECHANIC DISPATCH AND IT WAS DETERMINED THE AC NEEDED TO RETURN. THE CREW PERFORMED AN AIR-TURN-BACK. MECHANIC RAN THE ENGINES BUT WHERE UNABLE TO DUPLICATE THE PROBLEM. MECHANIC PERFORMED A LEAK CHECK OF THE EVA TUBING AND PURGED ANY MOISTURE. WITH NO FURTHER DISCREPANCIES NOTED THE AC WAS RETURNED TO SERVICE. (K) 2L72 4T4 TRTA24CE E26NE 20050302000472005030200047NE 2005 3 2 S2YA05001 220050103A75324067B000004 SHUTOFF VALVE DORNERDO32 DO328300 NM PWA 306 PW306B NE LEFT MALFUNCTIONED A D RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL13354SK 3126 BEFORE FLIGHT, DURING TAXI OUT THE CREW GOT A BLEED SOV AND LT PACK FAIL CAS MESSAGE, THEY CONSULTED WITH MECHANIC BUT WHERE UNABLE TO GET IT TO CLEAR. THE AC RETURNED TO THE GATE. MECHANIC SWAPPED PRESSURE AND HIGH PRESSURE VALVES. WITH NO FURTHER DISCREPANCIES NOTED THE AC WAS RETURNED TO SERVICE. NOTE: AS OF 2/08/05 THIS PROBLEM HAS NOT COME BACK. (K) 2H72 4T4 FRTA55NM E35NE 20050302000742005030200074NM 2005 3 2 AMTA200500091 120050126A2613 WARNING SYSTEM BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE COCKPIT MALFUNCTIONED A AMTAK NONE N FALSE WARNING CRCRUISE 1 GL11561TZ 33526 LT STRUT O/H DET 1 DISPLAYED. PERFORMED FIM 261200FIG103/104 NO FAULTS FOUND ALSO AFLOTS CARD INDICATIONS LED INDICATE NO FAILURES. (K) 2L72 4F4 FRTA2NM E12EU 20050302000752005030200075CE 2005 3 2 KC82005F00003 120050124A3260446EN19 SQUAT SWITCH LEAR 25 25 5170506CE GE CJ610 CJ6105 30006NE LT MLG FAILED E KC8AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL2339CK 005 AFTER TAKEOFF, THE LANDING GEAR FAILED TO RETRACT. PILOT RETURNED TO DEPARTURE. FOUND LT MAIN GEAR SQUAT SWITCH FROZEN AND THE INTERNAL MICRO SWITCHES REMAINED IN THE GROUND MODE. REPLACED SQUAT SWITCH WITH NEW SQUAT SWITCH. ALL WORK PERFORMED IAW SRM. (K) 2L72 4J4 J A10CE 1E16 20050302000852005030200085NM 2005 3 2 USAA050152 120050126A5330 SKIN BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19340US50590 23237 CLT - RON - SKIN, 1.750 INCH CRACK, STRINGER 23R STATION 727E; INSTALLED DOUBLER. (K) 2L72 4F4 FRTA16WE E2GL 20050302000952005030200095NM 2005 3 2 USAA050111 120050101A5754 SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU L/E SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19517AU53410 23703 PIT - Q6 - SKIN, 4 INCH X 4 INCH AREA DELAMINATION; NR 5 SLAT IB END; REMOVED TOP SKIN, CORE, REPLACED CORE AND TOP SKIN IAW SRM 57-70-10. (K) 2L72 4F4 FRTA16WE E21EU 20050302001042005030200104NM 2005 3 2 USAA050101 120050101A53306545722166 SKIN PANEL BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19517AU53410 23703 PIT - Q6 - SKIN PANEL, .015 INCH X 4 INCH LONG; CHAFED; FWD OF STA 867 TO JUST AFT OF STA 887, STR 2L AND 2R. DOUBLER INSTALLED AND TRIPLER IAW TYP. REP.53-30-02, REV B. (K) 2L72 4F4 FRTA16WE E21EU 20050302001112005030200111NM 2005 3 2 USAA050117 120050101A53206546812169 FLOOR SUPPORT BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19517AU53410 23703 PIT - Q6 - FLOOR SUPPORT, 1 INCH DIA AREAS ( 8 EA ); CORROSION; LEVEL 1; TASK NR C53-107-02; FLOOR SUPPORT BS 967-986.5, RBL 17 INCHES. DEFECTIVE PART, REPLACED WITH IDENT PART IAW SRM AND MFG DWG. (K) 2L72 4F4 FRTA16WE E21EU 20050302001562005030200156NM 2005 3 2 USAA050177 120050127A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19396US52325 23318 CLT - FOUND SKIN CRACKED, STATION 727D STRINGER S24L. INSTALLED DOUBLER IAW SRM 53-00-01. (M) 2L72 4F RTA16WE 20050302001662005030200166NM 2005 3 2 USAA050077 120050101A5713 STRINGER BOEING737 7373B7 1384580NM RT WING CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19522AU 23857 PIT - FOUND UPPER STRINGER 2 INCH CRACK, WBL 505 RT WING. INSTALLED REPAIR ANGLES WITH MINOR DEVIATION PER EA 79684 AND SRM 57-00-03. (M) 2L72 4F RTA16WE 20050303000192005030300019 2005 3 3 SWAA050566 420050224A256563551101 SLIDE BOEING737 7377H4 1384404NM L2 DOOR DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29740SW 29276 L2 DOOR EVAC SLIDE PRESSURE INDICATION LOW. REMOVED AND REPLACED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050303000242005030300024NM 2005 3 3 SWAA050571 120050224A53116546551 FRAME BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 807, STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050303000322005030300032 2005 3 3 SWAA050577 420050224A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29742SW 29278 DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. REINSTALLED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050303000422005030300042NM 2005 3 3 SWAA050588 120050225A3350101114 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29361SW 26572 RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED EMERGENCY EXIT LIGHT LENS PER MM. 2L72 4F RTA16WE 20050303000582005030300058NM 2005 3 3 SWAA050596 120050225A531069353656 SHEAR TIE BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON SHEAR TIE AT BS 344, LBL 8-12, WL 148. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050303000782005030300078NM 2005 3 3 SWAA050619 120050228A53116516301 FRAME BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17L & 17R. REPAIRED FUSELAGE FRAME PER SRM. 2L72 4F RTA16WE 20050303000792005030300079NM 2005 3 3 SWAA050620 120050228A53306545774 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29677AA 23289 DURING SCHEDULED A2 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS BETWEEN BS 749 TO BS 761, BELOW STR 19R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050303000802005030300080NM 2005 3 3 SWAA050621 120050228A5340BAC1490 ATTACH ANGLE BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME TO SKIN ATTACH ANGLE CRACKED AT BS 400, STR 14L. REPAIRED FUSELAGE ATTACH ANGLE PER SRM. 2L72 4F RTA16WE 20050303000812005030300081NM 2005 3 3 SWAA050622 120050228A534065C27314 STRINGER CLIP BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 DURING SCHEDULED SPECIAL VISIT, FOUND CRACKED STRINGER CLIP AT BS 807, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20050303000822005030300082NM 2005 3 3 SWAA050625 120050228A53106545871 DOOR FRAME BOEING737 7373H4 1384600NM R1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29329SW 23693 DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR AFT FRAME CRACKED AT 3RD STOP FITTING. REPAIRED R1 DOOR FRAME PER SRM. 2L72 4F RTA16WE 20050303000832005030300083NM 2005 3 3 SWAA050626 120050228A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29329SW 23693 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR, LOWER HINGE. REPAIRED FUSELAGE SKIN PER SRM. 2L72 4F RTA16WE 20050303000852005030300085 2005 3 3 SWAA050611 420050228A25656551463 HOOK BOEING737 7377H4 1384404NM GIRT BAR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29723SW 27855 DURING SCHEDULED RON CHECK, FOUND L1 DOOR EMERGENGY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED GIRT BAR HOOK PER MM. 2L72 4F RTA16WE 20050303000882005030300088NM 2005 3 3 CALA0500060 120050227A531565C33950 FLOORBEAM BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717614 27327 INSPECTION FOUND CABIN FLOORBEAM CORRODED AT AFT FLANGE OF UPPER CHORD, STA 986, LBL 14 TO LBL 18. THE CORRODED AREA WAS CUT OUT AND ANGLES WERE INSTALLED IAW SRM 53-60-51. 2L72 4F RTA16WE 20050303000892005030300089NM 2005 3 3 CALA0500061 120050227A53156545810101 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714337 23575 INSPECTION FOUND A 1.625 INCH CRACK IN FORWARD GALLEY FLOORBEAM WEB AT STA 312, RBL 18. THE WEB WAS REPAIRED IAW ECRA 5310-04462. 2L72 4F RTA16WE 20050303000902005030300090NM 2005 3 3 CALA0500062 120050227A5315BAC1505100246 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714337 23575 INSPECTION FOUND FLOORBEAM CORRODED IN E&E COMPARTMENT ON RT SIDE ABOVE AIRFONE CONTROL BOX AT STA 312, RBL 21. THE FLOORBEAM UPPER CHORD WAS REMOVED AND REPLACED IAW SRM 53-00-51. 2L72 4F RTA16WE 20050303000922005030300092NM 2005 3 3 SWAA050552 120050223A53106546546 SHEAR TIE BOEING737 7375H4 138449DNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29507SW 24184 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON SHEAR TIE AT BS 787, BETWEEN STR 26R & 27R. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050303000942005030300094NM 2005 3 3 SWAA050556 120050223A3350101073 LENS BOEING737 7373H4 1384600NM R1 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29648SW 27718 R1 DOOR LOWER EMERGENCY EXIT SIGN LENS LOOSE. SECURED EXIT SIGN LENS PER MM. 2L72 4F RTA16WE 20050303000952005030300095 2005 3 3 SWAA050557 420050223A2565D31354 SLIDE BOEING737 7375H4 138449DNM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29528SW 26570 L1 DOOR EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050303000982005030300098NM 2005 3 3 SWAA050560 120050223A534065C27314 STRINGER CLIP BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND CORROSION ON STRINGER CLIP AT BS 727E, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20050303001002005030300100NM 2005 3 3 SWAA050562 120050223A3350D71702001 BATTERY PACK BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29776WN 30591 DURING SCHEDULED HC2 CHECK, FOUND RT MID, LT & RT AFT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACKS PER MM. 2L72 4F RTA16WE 20050303001022005030300102SO 2005 3 3 RAIA00502024 120050215A7830 WARNING LIGHT EMB 145 EMB145 3260210SO THRUST REVERSER ILLUMINATED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03821HK 145068 LT ENGINE THRUST REVERSER DISAGREE INDICATION. MAINTENANCE CYCLED POWER AND OPS CHECKED LEFT T/R WITH NO DEFECTS NOTED. 2L72 4F RTT00011AT 20050303001032005030300103EU 2005 3 3 RAIA00502026 120050216A3150 POSITION SWITCH JETAIRJETSTMJETSTM4101 1500501EU CONDITION LEVER OUT OF ADJUST A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03563HK 41079 ERI - TAKEOFF CONFIGURATION WARNING INDICATION. MAINTENANCE ADJUSTED LT CONDITION LEVER POSITION SWITCH, AND OPS CHECKED GOOD. 2L72 4T RTA41NM 20050303001052005030300105SO 2005 3 3 RAIA00502021 120050214A21302014AB MODULE EMB 145 EMB145 3260210SO CABIN PRESSURE INOPERATIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03803HK15188 145077 PIT - ALL CABIN PRESSURIZATION INDICATIONS WENT BLANK. MAINTENANCE REMOVED AND REPLACED THE CABIN PRESSURE ACQUISITION MODULE. 2L72 4F RTT00011AT 20050303001082005030300108NM 2005 3 3 SWAA050542 120050222A534065C27314 STRINGER CLIP BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP AT BS 727B, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20050303001092005030300109NM 2005 3 3 SWAA050543 120050222A534065C27314 STRINGER CLIP BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP AT BS 727B, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20050303001112005030300111NM 2005 3 3 SWAA050545 120050222A534065C27314 STRINGER CLIP BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP AT BS 727A, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20050303001132005030300113NM 2005 3 3 AWXA200500241 120050120A52106545871 FRAME BOEING737 737301 1384611NM R1 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 DURING C-18 CHECK A .75 INCH CRACK WAS FOUND IN R-1 DOOR AT 3RD STOP PIN BRACKET FROM THE BOTTOM ON AFT SIDE OF DOOR BS 328, STR 14 RT. MAINTENANCE TRIMMED OUT CRACK IN R-1 DOOR AT 3RD STOP PIN BRACKET FROM THE BOTTOM; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW ER 03-5200-05034-RC2A. 2L72 4F RTA16WE 20050303001152005030300115NM 2005 3 3 AWXA200500243 120050128A575465C2679413 SKIN BOEING737 7373G7 1384595NM NR 2 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 DURING C-16 CHECK 4 EACH .25 INCH CRACKS WERE FOUND AT FASTENER HOLES ON LOWER NR 2 SLAT SKIN. MAINTENANCE FASTENERS AND PREVIOUS REPAIR IN LOWER NR 2 SLAT SKIN FROM SLAT STA 158.5 T0 SLAT STA 165; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-43-01 FIG 206. 2L72 4F RTA16WE 20050303001172005030300117EU 2005 3 3 MALA050158 120050220A3000 ANTI-ICE VALVE SAAB SF340 SF340A 7850100EU GE CT7TP CT79B 30030NE RIGHT MALFUNCTIONED A MALAO OTHER J WARNING INDICATION CRCRUISE 1 GL1527XJ 340A027 RT AIR VALVE ILLUMINATED IN FLIGHT. RAN QRH AND RECYCLED, NO CHANGE. REPLACED ANTI-ICE VALVE IAW ENGINE MAINTENANCE MANUAL CH 75-00-00. P/N ON/OFF 6058T80P03. S/N OFF COMD0563. OPS CHECK GOOD. 2L72 4T4 TRTA52EU E8NE 20050303001192005030300119EU 2005 3 3 MALA050160 120050217A5320 STRUCTURE SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15424XJ 340B424 RT WRAP AROUND P/N 7253710-243, AT FS 294 IS CORRODED AND HAS BEEN REPLACED IAW SRM 51-40-21. 2L72 4T RTA52EU 20050303001212005030300121EU 2005 3 3 MALA050162 120050217A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15424XJ 340B424 DURING 4Y/2Y CHECK FOUND SEAT TRACK AT BL 0, FROM FS 297 TO FS 310 IS CORRODED AND IS BEING REPAIRED IAW SRM 53-70-60. 2L72 4T RTA52EU 20050303001222005030300122EU 2005 3 3 MALA050163 120050217A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15424XJ 340B424 DURING 4Y/2Y CHECK FOUND SEAT TRACK AT LBL 18.3 IS CORRODED, FROM FS 297 TO FS 310. DAMAGE IS BEING REPAIRED IAW SRM 53-70-60. 2L72 4T RTA52EU 20050303001242005030300124NM 2005 3 3 DHL2005750002 120050218A3260 UPLOCK SENSOR BOEING727 7272M7 138407SNM NLG OUT OF ADJUST A DHLAO OTHER EJ VIBRATION/BUFFET WARNING INDICATION NRNOT REPORTED 1 SO01750DH 21951 IN MODERATE CHOP AUDIBLE THUMP FROM NOSE GEAR WITH ASSOCIATED INTERMITTENT NOSE GEAR LIGHT ILLUMINATED. PLACING GEAR HANDLE UP MADE INDICATIONS NORMAL IF GEAR HANDLE REMAINED UP. JACKED NOSE GEAR PER MM 7-11-0-4A. PERFORMED NOSE GEAR OPERATIONAL CHECK PER MM 32-33-00. ADJUSTED NOSE GEAR UP POSITION SWITCH PER MM 32-61-01. CYCLED SEVERAL TIMES, CHECKS GOOD. 2L73 4F A3WE 20050303001272005030300127NM 2005 3 3 SWAA050551 120050222A53106519603 CREASE BEAM BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND CRACK AT LT CREASE BEAM WEB AT BS 375. REPAIRED BEAM WEB PER SRM. 2L72 4F RTA16WE 20050303001282005030300128EA 2005 3 3 COMA0560136 120050219A5270840534 PROXIMITY SWITCH CNDAIRCL600 CL6002B19 1900309EA PAX DOOR UNRELIABLE A COMAO OTHER N FALSE WARNING CRCRUISE 1 SO01957CA 7109 FLIGHT 5148 CABIN DOOR OUTER HANDLE CAUTION. REPLACED PROXIMITY SWITCH DI17. 2L72 4F RTA21EA 20050303001292005030300129NM 2005 3 3 AALA20050119 120050217A3397 CONNECTOR BOEING757 757223 1384957NM EMERGENCY LIGHT LOOSE A AALAK NONE O OTHER ININSP/MAINT 1 SW21637AM 24595 DFW - EMERGENCY LIGHT AT SEAT 32D INOPERATIVE. SECURED WIRES AT CONNECTOR FOR EMERGENCY LIGHT AT SEAT 32D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050303001332005030300133EU 2005 3 3 AALA20050124 120050217A3260 PROXIMITY SENSOR AIRBUS300 A300B4605R 3930308EU MLG INOPERATIVE A AALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW2170074 517 JFK - INFLIGHT T1291/17 ALL THREE LANDING GEAR WOULD NOT RETRACT IN SYSTEM ONE OR TWO. REPLACED PROXIMITY BOX FOR LANDING GEAR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20050303001342005030300134NM 2005 3 3 AALA20050129 120050219A3350BPS73 BATTERY PACK BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW2139365 24046 JFK - EMERGENCY LIGHTS FROM ROW 31H BACK OF AIRCRAFT INOPERATIVE. REPLACED BATTERY PACK AND CHARGER ASSEMBLY M739 FOR EMERGENCY LIGHTS AT ROW 31H TO BACK OF AIRCRAFT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050303001352005030300135WP 2005 3 3 AALA20050126 120050218A4990AAP0302A APU DOUG DC9 DC982 3022082WP APU BAY LEAKING A AALAO OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21957U 49702 DFW - AIRCRAFT HAD A HAZEY LOOK THROUGHOUT THE ENTIRE CABIN AND THERE WAS A MUSTY TYPE SMELL. THE HAZEY LOOK BECAME VERY THICK AND THE SMELL GOT MUCH STRONGER. FOUND APU LEAKING OIL. REPLACED THE APU. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050303001372005030300137WP 2005 3 3 AALA20050128 120050218A2170 COALESCER BAG DOUG DC9 DC983 3022083WP A/C PACK CONTAMINATED A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21961TW 53611 DFW - INFLIGHT T368/18 THE CABIN WAS FULL OF SMOKE ON LANDING. INSPECTED APU INLET AND AIRCRAFT TAIL SECTION. FOUND NO OIL OR HYDRAULIC FLUID LEAKS. RAN AIR CONDITIONING PACKS WITH APU AIR AND ENGINE AIR WITH NO SMOKE NOTED. AS PRECAUTIONARY REPLACED WATER SEPARATOR BAGS AND PACK BURN OUT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050303001392005030300139EU 2005 3 3 MALA050169 120050221A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15414XJ 340B414 DURING 4K CHECK IN BNA FOUND SEAT TRACK AT LBL 18.3 IS CORRODED FROM FS 296 TO FS 300. DAMAGE HAS BEEN REPAIRED IAW SRM 53-70-60. FOUND DURING 4Y/2Y CHECK IN BNA. 2L72 4T RTA52EU 20050303001432005030300143EU 2005 3 3 MALA050188 120050211A3350501122804 POWER SUPPLY SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A MALAK NONE L NO TEST ININSP/MAINT 1 GL15429XJ 340B429 EMERGENCY POWER SUPPLY P/N 501-1228-04, S/N 4586 FAILED SCHEDULED CAPACITY CHECK. REPLACED 12 EA CELLS P/N 549-1170-01. UNIT PASSES CMM TESTS, RTS 2/15/05. 2L72 4T RTA52EU 20050303001442005030300144EU 2005 3 3 MALA050191 120050206A33506122751 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU EMERGENCY LIGHT INOPERATIVE A MALAK NONE L NO TEST ININSP/MAINT 1 GL15536XJ E2372 BATTERY PACK P/N 61-2275-1, S/N 9912232 FAILED SCHEDULED CAPACITY CHECK. REPLACED BATTERY ASSEMBLY P/N 61-2274-1. UNIT PASSES CMM CHECKS, RTS 2/8/05. 2H74 4F RTA49EU 20050307000012005030700001EU 2005 3 7 MALA050232 120050227A3150 WARNING LIGHT SAAB SF340 340B 7860101EU COCKPIT ILLUMINATED A MALAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL15411XJ 340B411 FLIGHT IDLE STOP CAUTION LIGHT ILLUMINATED ON GEAR RETRACTION. REPLACED RELAY. 2L72 4T RTA52EU 20050307000032005030700003NM 2005 3 7 252TR0029 120050222A5330 SKIN BOEING737 737228 13844AGNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05252TR 23001 CORROSION AROUND THE FORWARD LAVATORY DUMP VALVE, I/B SIDE. REPLACED CORRODED SUPPORT ANGLE PER BAC DWG 65-55757 AND SRM 51-10-2. 2L72 4F RTA16WE 20050307000052005030700005NE 2005 3 7 MALA050233 220050227A7200 ENGINE SAAB SF340 340B 7860101EU GE CT7TS CT71 30030NE RIGHT MAKING METAL A MALAO OTHER J WARNING INDICATION CRCRUISE 1 GL15436XJ 340B436 DURING CRUISE FLIGHT RT ENGINE CHIP DETECTOR LIGHT ILLUMINATED AND THEN IT CYCLED ON AND OFF. ANOTHER 6 TO 8 TIMES BEFORE LANDING IN ROA. REMOVED AND REPLACED RT ENGINE IAW 71000-301, S/N ON GE-E785738, S/N OFF GE-E285693 IAW 7100-301. ALL CHECKS GOOD. 2L72 4T4 URTA52EU E8NE 20050307000072005030700007NM 2005 3 7 05FDEA00345 120050303A534065453136 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 BONUS HOLES IN STRINGER CLIP AT BS 950A STR 7R. REPLACED PER SRM 51-30-2. 2L73 4F RTA3WE 20050307000082005030700008NM 2005 3 7 AWXA200500288 120050302A2560P4010021 BATTERY BOEING737 73733A 1384673NM ZONE 900 - LAVATDISCHARGED A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28166AW 23627 SMF - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD FLIGHT ATTENDANTS EMERGENCY FLASHLIGHT WAS NOT BLINKING. MAINTENANCE REMOVED AND REPLACED THE BATTERY IN THE FORWARD GALLEY EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050307000092005030700009NM 2005 3 7 AWXA200500289 120050227A3234655421925 LEVER BOEING737 7373G7 1384595NM COCKPIT BINDING A AWXAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 WP28303AW 24010 ON APPROACH, AFTER LOWERING LANDING GEAR & SELECTING FLAPS 15, SPEED 150 KTS, ALL 6 LANDING GEAR LIGHTS ILLUMINATED. CYCLED GEAR & LIGHTS REMAINED ON, SELECTED FLAPS TO 25 & RECEIVED AURAL UNSAFE GEAR WARNING, ABORTED APPROACH. CYCLED GEAR AGAIN & LANDING GEAR INDICATED DOWN WITH 3 GREEN LIGHTS, DECLARED EMERGENCY & LANDED. MX TROUBLESHOT PERFORMED OPS TESTS OF CIRCUIT CARDS M986 7 M983, BOTH CARDS CHECKED GOOD. DURING TEST FOUND LANDING SELECTION LEVER NOT FULLY SEATED IN DOWN POSITION CAUSING IMPROPER GEAR INDICATION. FERRIED TO PHX, FOUND GEAR LEVER WAS BINDING IN THE IN & OUT DIRECTION. REMOVED P3 PANEL & CLEANED BUILD UP FROM HANDLE SURFACE & LUBRICATED SLIDING SURFACES, OPS CHECK GOOD. 2L72 4F RTA16WE 20050307000102005030700010NM 2005 3 7 AWXA200500290 120050124A5320655287646 SILL BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON L-2 DOOR SILL INNER CHORD BETWEEN BS 950 AND BS 994, LBL 50. MAINTENANCE REMOVED CORRODED L-2 DOOR SILL INNER CHORD FROM BS 917 TO BS 1016, LBL 50; FABRICATED A NEW REPLACEMENT INNER CHORD PER DWG 65-52878; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050307000112005030700011NM 2005 3 7 AWXA200500291 120050120A53306545776100 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK A 1 INCH CRACK WAS FOUND IN FUSELAGE SKIN ON LT AFT SIDE OF WING TO BODY FAIRING BS 727E, STR 24 LT. MAINTENANCE CUT OUT DAMAGE IN FUSELAGE SKIN BS 727E, STR 24 LT; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A FILLER, DOUBLER, AND TRIPLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-01 FIG 229. 2L72 4F RTA16WE 20050307000122005030700012NM 2005 3 7 AWXA200500292 120050203A53306545772162 SKIN BOEING737 737301 1384611NM FUSELAGE WORN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK FOUND FUSELAGE SKIN WORN IN SEVERAL AREAS AT LT AND RT DORSAL FIN SEALS BETWEEN BS 860 AND BS 907.5. MAINTENANCE CUT OUT DAMAGE IN FUSELAGE SKIN AT LT AND RT DORSAL FIN SEALS FROM BS 860 TO BS 907.5; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED 2 EACH FILLERS & WEAR STRAPS, A DOUBLER AND TRIPLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-60-01 FIG 209. 2L72 4F RTA16WE 20050307000132005030700013NM 2005 3 7 05FDEA00325 120050302A5754ARB1668501 SKIN DOUG MD11 MD11 3023602NM NR 3 SLAT CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 LEFTHAND WING NR 3 SLAT, LOWER SURFACE, MOST LOWER, FAIRING FOUND CHAFING DAMAGE AGAINST THE FAIRING DOOR OF THE ANTI-ICE TELESCOPIC DUCT. LEFTHAND WING NR 3 SLAT, LOWER SURFACE REPAIRED AS PER FEDEX EA 1-5740-78105. TITLE: WINGS - LEADING EDGE AND LEADING EDGE DEVICES, NR 3 SLAT SKIN / XOS=467.100 / REPAIR. 2L73 4F RTA22WE 20050307000142005030700014WP 2005 3 7 05FDEA00329 120050302A5730ARC1263 PANEL DOUG MD10 MD1010F 3022112WP ZONE 600 DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25361FE 48260 RIGHT WING FIRE BOTTLE ACCESS PANEL TRAILING EDGE DELAMINATED. REPAIRED PANEL IAW FEDEX EA 8-5710-83990, WINGS - LEADING EDGE, ACCESS FIREX BOTTLE DOOR-REPAIR. 2L73 4F RTA22WE 20050307000152005030700015EA 2005 3 7 QXEA200500249 120050206A5340 NUT CNDAIRCL600 CL6002C10 1390015EA ZONE 100 UNSERVICEABLE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - FUSELAGE EXTERIOR, BELLY TCAS ANTENNA AT FUSELAGE STATION 303 HAS ONE UNSERVICEABLE ANCHOR NUT. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20050307000162005030700016EA 2005 3 7 QXEA200500250 120050210A5320 STRUCTURE CNDAIRCL600 CL6002C10 1390015EA ZONE 200 BENT A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - FUSELAGE AT PASSENGER DOOR BOTTOM FORWARD RADIOUS OF PRESSURE SEAL BENT. REPAIRED IAW CRJ700 SRM 51-24-21-001-001-A01, 51-21-11-001-001-A01, 51-25-06-001-001-A01 AND 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050307000172005030700017EA 2005 3 7 QXEA200500240 120050214A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - FUSELAGE EXTERIOR, FUSELAGE SKIN AT STATION 533 AND STRINGER 19L HAS A 6 INCH LONG SCRATCH. REPAIRED IAW CRJ700 SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01, 51-25-01-001-001-A01, HORIZON AIR EA R-53-269 AND REO 670-53-31-026, REV C. 2L72 4F RTA21EA 20050307000182005030700018EA 2005 3 7 QXEA200500241 120050214A5414 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 400 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - RT ENGINE NACELLE LIP SKIN GOUGED AT 3, 5, 9 AND 12 O'CLOCK POSITIONS. REPAIRED IAW CRJ700 SRM 53-11-05-101-001-A01 AND 54-11-01-201-001-A01. 2L72 4F RTA21EA 20050307000192005030700019EA 2005 3 7 QXEA200500242 120050214A5414 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 400 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - LEFTHAND ENGINE NACELLE, LIP SKIN GOUGED AT 3, 5 AND 11 O'CLOCK POSITIONS. REPAIRED IAW CRJ700 SRM 54-11-05-101-001-A01 AND 54-11-01-201-001-A01. 2L72 4F RTA21EA 20050307000202005030700020NM 2005 3 7 05FDEA00350 120050303A5315 FLOORBEAM BOEING727 727200 138407ENM FUSLEAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 CORROSION ON LOWER SIDE OF FLOORBEAM AT BS 1070, LBL 1 TO LBL 45, WL 200. WORK TO BE ACCOMPLISHED ON CUSTOMER CARD N01219 2L73 4F RTA3WE 20050307000212005030700021NM 2005 3 7 05FDEA00351 120050303A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 CORROSION ON LOWER SIDE OF FLOORBEAM AT BS 1130, LBL 45 TO RBL 45, WL 200. 2L73 4F RTA3WE 20050307000222005030700022WP 2005 3 7 05FDEA00352 120050303A5753ARC2747 SKIN DOUG MD10 MD1010F 3022112WP ZONE 500 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25361FE 48260 LT INBOARD FLAP LOWER SKIN, INBOARD END AFT SECTION IS CHAFED. COMPLIED WITH EA 8-5710-83979 WINGS - LT INBOARD FLAP, LOWER SKIN REPLACEMENT- REPAIR. 2L73 4F RTA22WE 20050307000232005030700023NM 2005 3 7 05FDEA00354 120050303A3230 LANDING GEAR BOEING727 727200 138407ENM NOSE MALFUNCTIONED A FDEAL ABORTED APPROACH J WARNING INDICATION LDLANDING 1 SO25265FE 21671 NOSE GEAR FAILED TO EXTEND WHEN GEAR HANDLE PLACED DOWN RED UNSAFE INDICATION. AFTER 30 SEC NOSE EXTENDED GREEN SAFE INDICATION. 2L73 4F RTA3WE 20050307000242005030700024NM 2005 3 7 05FDEA00353 120050303A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 CORROSION SPOTS UNDER FLOORBEAM LOWER SURFACE AT BS 1130 LBL 43 TO RBL 52, WL 200 IN AFT CARGO BAY. FLOOR BEAM WILL BE REPLACED ON N01035, INTERIOR 5081 AT BS 1130, LBL 65 TO RBL 65 LOWER CHORD. 2L73 4F RTA3WE 20050307000252005030700025CE 2005 3 7 DXTA200500611 120050302A2150 ISOLATION VALVE CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL A/C PACK OPEN E DXTAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL07920QS 7500120 CAE330184 AFTER STARTING THE LEFT ENGINE, ON FIRST START OF THE DAY, A STRONG ODOR OF RAW FUEL COMES INTO THE COCKPIT. PACK ISOLATION VALVE WAS OPEN. AIR COMING FROM WEMAC SMELLED CLEAN. 2L72 4J4 FRTT00007WITE6CH 20050307000262005030700026WP 2005 3 7 05FDEA00339 120050303A5730ARC0616 SKIN DOUG MD10 MD1010F 3022112WP ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25361FE 48260 RT WING PANEL INBOARD OF OUTBOARD AILERON ISLAND ABOVE FLAP OUTBOARD TRACK HAS CORROSION AND DELAMINATION. REPAIRED TRAILING EDGE WING PANEL PART NUMBER ARC0616 IAW FEDEX EA 8-5710-83980, WINGS-RIGHTHAND UPPER SK9N, TRAILING EDGE PANEL-REPAIR. 2L73 4F RTA22WE 20050307000272005030700027WP 2005 3 7 05FDEA00340 120050303A5751ARC1210 PANEL DOUG MD10 MD1010F 3022112WP ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25361FE 48260 LT INBOARD AILERON LOWER SURFACE HAS BULGING AROUNG RIVETS, AT SEAM INBOARD EDGE TO AFT SEAM, STATION XORS 402. REMOVED DAMAGES SECTION OF SKIN AND REPAIRED LEFT INBOARD AILERON LOWER SURFACE SKIN IAW FEDEX EA 8-5710-83989, WINGS - LEFT HAND INBOARD AILERON LOWER SKIN - REPAIR, AND DAC DWG ARC1210, DC10-10 SRM 51-21-01 VOL II, 51-35-01 VCOL II, 51-35-01. 2L73 4F RTA22WE 20050307000282005030700028WP 2005 3 7 05FDEA00341 120050303A5730ARC0257 PANEL DOUG MD10 MD1010F 3022112WP ZONE 500 DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25361FE 48260 LEFT WING PANEL 541 NB HAS AREAS OF DELAMINATION. REPAIRED DELAMINATION PANEL 541NB BY FABRICATING AND BONDING NEW SKINS, DOUBLER AND CORE IAW TPS 1001 REV E AND FEDEX EA 8-5610-83986, WINGS - LEFT HAND WING PANEL 541NB- REPAIR. 2L73 4F RTA22WE 20050307000292005030700029NM 2005 3 7 05FDEA00342 120050303A52416557150142 DOOR FRAME BOEING727 727200 138407ENM GALLEY DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 FWD GALLEY DOOR POSSIBLE CRACK IN DOOR FRAME NEXT TO LWR LATCH ROLLER. REMOVED AND REPLACED FWD SIDE FRAME OF DOOR IAW SRM 51-10-2, 51-00-4. 2L73 4F RTA3WE 20050307000302005030700030NM 2005 3 7 05FDEA00343 120050303A534065453136 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 BONUS HOLES IN STRINGER CLIP AT BS 950F STR 7R. REPLACED PER SRM 51-30-2. 2L73 4F RTA3WE 20050307000312005030700031EU 2005 3 7 MALA050229 120050222A5311 FRAME SAAB SF340 340B 7860101EU FUSELAGE CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15423XJ 340B423 RIGHT FRAME SECTION AT FS 686.888 IS CHAFED AND HAS BEEN REPAIRED IAW MESABA EO S53285. 2L72 4T RTA52EU 20050307000322005030700032NM 2005 3 7 QXEA200500301 120050227A2611473082 SMOKE DETECTOR BOMBDRDHC8 DHC8401 1390041NM CARGO BAY WILL NOT TEST A QXEAO OTHER L NO TEST NRNOT REPORTED 1 NM09417QX1870 4086 THE FORWARD BAGGAGE DETECTOR DOES NOT TEST OR ALERT. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE FORWARD BAGGAGE SMOKE DETECTOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050307000332005030700033EU 2005 3 7 MALA050223 120050122A2611 SMOKE DETECTOR BAC 146 AVRO146RJ85A1500097EU CARGO BAY MALFUNCTIONED A MALAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL15507XJ E2316 CARGO SMOKE DETECTOR FLASHED FOR A FEW SECONDS ON PUSHBACK. NO OTHER ASSOCIATED WARNINGS. PERFORMED SMOKE TEST PER AVRO AMM 26-12-11. NO DEFECTS OR FAULTS FOUND. NO FURTHER ACTION REQ AT THIS TIME 2H74 4F RTA49EU 20050307000342005030700034EU 2005 3 7 MALA050227 120050222A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSLEAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15423XJ 340B423 RAIL ASSEMBLY P/N 7253710-871, BETWEEN FS 258 AND FS 288 AT LBL 33 IS CORRODED OUT OF LIMITS. DAMAGE IS ACCEPTABLE IAW MESABA EOS53286. 2L72 4T RTA52EU 20050307000352005030700035EU 2005 3 7 MALA050217 120050124A5311 FRAME BAC 146 AVRO146RJ85A1500097EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15517XJ E2335 LEFT SIDE OF FUSELAGE BELOW LAPCAT FRAME 14 DENTED AND CREASED. REPAIRS CARRIED ON 409, NR 226085 AND EOA53247. 2H74 4F RTA49EU 20050307000362005030700036EU 2005 3 7 MALA050224 120050126A3260M4001265 RELAY BAC 146 AVRO146RJ85A1500097EU MLG UPLOCK MALFUNCTIONED A MALAO OTHER J WARNING INDICATION CRCRUISE 1 GL15520XJ E2345 AIRCRAFT DIVERTED FROM ATL TO CVG DUE TO RT GEAR INTRANSIT LIGHT NOT GOING OUT AFTER GEAR WAS RETRACTED. REMOVED AND REPLACED RELAY AT GF7 GEAR UPLOCK RELAY P/N ON/OFF M400-1265. OPS CHECK GOOD IAW AMM 24-09-15. 2H74 4F RTA49EU 20050307000372005030700037EA 2005 3 7 QXEA200500236 120050212A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 RT FORWARD FUSELAGE HAS TWO GOUGES APPROXIMATELY AT STATION 177.00. REPAIRED IAW CRJ 700 SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01 AND SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050307000382005030700038EA 2005 3 7 QXEA200500235 120050206A5210 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 800 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - PASSENGER DOOR AFT CORNER SKIN HAS LOOSE FASTENERS. REPAIRED IAW CRJ 700 SRM 51-42-06-001-001-A01 AND SRM 51-42-10-001-001-A01. 2L72 4F RTA21EA 20050307000392005030700039EA 2005 3 7 QXEA200500245 120050213A5321 FLOOR PANEL CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - FUSELAGE INTERIOR, FLOOR CORROSION AT STATION 280 ALONG TOP FLANGE. REPAIRED IAW CRJ700 REO 670-53-11-047 AND SRM 51-41-00-001-001-A01. 2L72 4F RTA21EA 20050302000822005030200082NM 2005 3 2 USAA050109 120050101A575465C26602257A SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU L/E SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19517AU53410 23703 PIT - Q6 - SKIN - CORE, 4 INCH X 4 INCH DELAMINATION, NR 2 SLAT IB END. REMOVED DAMAGE, INSTALLED INTERNAL DOUBLER, CORE, TOP EXT DOUBLER IAW SRM 51-70-10. (K) 2L72 4F4 FRTA16WE E21EU 20050302000842005030200084NM 2005 3 2 USAA050151 120050113A5414 SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU LT PYLON CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19521AU52547 23856 PIT - Q6 - PYLON STRUT SKIN, .7500 INCH CRACK; PYLON STRUT SKIN FOR LT ENGINE, ACCESS PANEL CUTOUT. STOP DRILL OF CRACK AND INSTALLATION AT DOUBLER IAW TYP REP 54-30-07. (K) 2L72 4F4 FRTA16WE E21EU 20050302000892005030200089EU 2005 3 2 USAA050033 120050101A5315D53111412200 FLOORBEAM AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19713UW17339 1040 BFM- S1 - FLOORBEAM, 2.0 INCH X 2.0 INCH X .020 INCH AREA, CORROSION; LEVEL 2; TSK NR JA 220-53500, MAIN CABIN FLOORBEAM AT FR 20, BL Y254. INSTALLED REPAIR ANGLE AND FILLER IAW SRM. (K) 2L72 4F4 FRTA28NM E37NE 20050302000942005030200094NM 2005 3 2 USAA050097 120050101A5311 FRAME BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19517AU53410 23703 PIT - Q6 - FRAME, .2500 INCH LENGTH; FRAME TO SKIN BRACKET AREA IN FRAME STA 360, STR 14R. INSTALLED DOUBLER REPAIR IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050302001072005030200107NM 2005 3 2 USAA050110 120050101A575465C26602257A SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU L/E SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19517AU53410 23703 PIT - Q6 - SKIN, 4 INCH X 4 INCH AREA DELAMINATION; NR 2 SLAT, OB END; REMOVED TOP SKIN, CORE, REPLACED CORE, TOP SKIN IAW SRM 51-70-10. (K) 2L72 4F4 FRTA16WE E21EU 20050302001082005030200108NM 2005 3 2 USAA050114 120050101A5315 FLOORBEAM BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19517AU53410 23703 PIT - Q6 - FLOORBEAM, .5 INCH X .5 INCH, CORROSION; LEVEL 1; TASK NR C53-107-01; TOP SURFACE OF FLOORBEAM 20 INCH RT OF BL0, BS312; INSTALLED BEAM DOUBLER IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050302001252005030200125EU 2005 3 2 USAA050042 120050102A5315D53112782200 FLOORBEAM AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19713UW 1040 BFM - S1 - FLOOR BEAM/SEAT TRACK, 2.0 INCH X 1.5 INCH X .040 INCH AREA, CORROSION, LEVEL 2; TASK NR JA220-53500 BET FR 19-20, Y1292, Z240. CUT OUT DAMAGE AND INSTALLED REPAIR ANGLES IAW SRM. (K) 2L72 4F4 FRTA28NM E37NE 20050302001282005030200128NM 2005 3 2 USAA050158 120050101A5240 DOOR FRAME BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU SERVICE DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19521AU 23856 PIT- Q6 - DOOR EDGE FRAME, .2500 INCH CRACK; FWD SERVICE DOOR, LOWER MIDDLE DOOR STOP CUTOUT, AFT EDGE FRAME; INSTALLED DOUBLER IAW TYP REP. (K) 2L72 4F4 FRTA16WE E21EU 20050302001632005030200163NM 2005 3 2 USAA050198 120050104A575465C26602223 SKIN BOEING737 7374B7 1384702NM L/E SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19426US41647 24558 PIT - FOUND TOP SKIN CORE BOND DELAMINATED 2.5 INCH BY 1.5 INCH AREA, NR 3 SLAT TOP SURFACE OUTBOARD T/E. BONDED IN NEW CORE, BOND ON TOP DOUBLER PR SRM 51-70-10. (M) 2L72 4F RTA16WE 20050302001692005030200169NM 2005 3 2 USAA050078 120050103A532069735862 INTERCOSTAL BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19522AU49282 23857 PIT - FOUND INTERCOSTAL CRACKED .5 INCH, AT KEEL BEAM BETWEEN STATION 500 AND 520 IN DISTRIBUTION BAY. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-40-02. (M) 2L72 4F RTA16WE 20050303000092005030300009EA 2005 3 3 05056682 120050225A2750 FCU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A VTZAO OTHER J WARNING INDICATION APAPPROACH 1 EA27682BR 7691 FLAP FAIL AT 0 ON APPROACH. MX RESET FECU. 2L72 4F RTA21EA 20050303000112005030300011EA 2005 3 3 050546231 120050223A7120 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA ENGINE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27623BR 7192 ENGINE SUPPORT BEAM UPPER ANGLE IS CRACKED AT .250 INCH IN LENGTH AT FS 640.00 AND LBL 8.5. 2L72 4F RTA21EA 20050303000162005030300016NM 2005 3 3 SWAA050564 120050224A3350101073 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29433LV 33716 EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED EXIT LIGHT COVER PER MM. 2L72 4F RTA16WE 20050303000202005030300020NM 2005 3 3 SWAA050567 120050224A3350604222 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29741SA 29277 DURING SCHEDULED RON CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050303000382005030300038NM 2005 3 3 SWAA050579 120050224A53206545410 FLOOR SUPPORT BOEING737 7375H4 138449DNM CENTER WING BOX CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29507SW 24184 DURING SCHEDULED 1/2D CHECK, FOUND 3 EA CRACKS AT NR 3 LONGITUDINAL FLOOR SUPPORT AT BS 665, BS 662.5, & BS 669. REPAIRED BEAM PER SWA EA. 2L72 4F RTA16WE 20050303000482005030300048NE 2005 3 3 05055656 220050224A7261 CARBON SEAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 1 LEAKING A VTZAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA27656BR 7485 EVENT SUMMARY STATED LAV SMOKE. REMOVED AND REPLACED RT ENG NR 1 CARBON SEAL. 2L72 4F4 FRTA21EA E15NE 20050303000542005030300054NM 2005 3 3 SWAA050617 120050228A53106546546 SHEAR TIE BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND CORROSION ON SHEAR TIE AT BS 847, RBL 17, WL 154. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050303000632005030300063NM 2005 3 3 SWAA050603 120050225A53106547978 CREASE BEAM BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND CORROSION ON RT CREASE BEAM WEB AT BS 727B, RBL 70. REPAIRED CREASE BEAM WEB PER SRM. 2L72 4F RTA16WE 20050303000842005030300084NM 2005 3 3 SWAA050627 120050228A524065C36231 SKIN BOEING737 7375H4 138449DNM R1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29507SW 24184 DURING SCHEDULED 1/2D CHECK, FOUND R1 DOOR SKIN CRACKED AT LOWER HINGE CUTOUT. REPAIRED R1 DOOR SKIN PER SRM. 2L72 4F RTA16WE 20050303000932005030300093 2005 3 3 SWAA050553 420050223A25656557463 FITTING BOEING737 7375H4 138449DNM GIRT BAR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29507SW 24184 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON L1 DOOR EVAC SLIDE, AFT GIRT BAR FITTING AT BS 344. REMOVED AND REPLACED GIRT BAR FITTING PER SRM. 2L72 4F RTA16WE 20050303000972005030300097NM 2005 3 3 SWAA050559 120050223A53306545774 SKIN BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29661SW 23173 DURING SCHEDULED C3 CHECK, FOUND SKIN CRACK AT BS 737, BELOW STR 19R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050303001072005030300107NM 2005 3 3 SWAA050540 120050222A534065C27314 STRINGER CLIP BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP AT BS 727C, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20050303001102005030300110NM 2005 3 3 SWAA050544 120050222A534065C27314 STRINGER CLIP BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP AT BS 727A, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20050303001122005030300112NM 2005 3 3 SWAA050547 120050222A534065C27314 STRINGER CLIP BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP AT BS 616, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20050303001262005030300126NM 2005 3 3 SWAA050550 120050222A53206551698 SPLICE BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND CRACK AT STRINGER SPLICE, BS 663, STR 7L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20050303001312005030300131NM 2005 3 3 AALA20050121 120050217A3230 CIRCUIT BREAKER BOEING737 737823 13844BZNM MLG INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21961AN 30092 MIA - AFTER TAKEOFF LANDING LEVER WOULD NOT RAISE PAST OFF POSITION. ACCOMPLISHED ALTERNATE GEAR RETRACTION PROCEDURE. GEAR RETRACTED USING OVERRIDE. FOUND CIRCUIT BREAKER B17 AND P63 PANEL POPPED LANDING GEAR LATCH AND PRESSURE WARNING. RESET CIRCUIT BREAKER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20050303001382005030300138WP 2005 3 3 AALA20050130 120050219A3397 WIRE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT DISCONNECTED A AALAK NONE O OTHER ININSP/MAINT 1 SW21984TW 53634 SFO - EMERGENCY LIGHT AT 11D INOPERATIVE. RECONNECTED SEAT EMERGENCY LIGHT AT 11D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050303001412005030300141EU 2005 3 3 MALA050185 120050131A3350501171202 POWER SUPPLY SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A MALAK NONE L NO TEST ININSP/MAINT 1 GL15415XJ 340B415 EMERGENCY POWER SUPPLY P/N 501-1712-02, S/N 1466 FAILED SCHEDULED CAPACITY CHECK. REPLACED 2 EACH CELL PACKS 549-1324-06. UNIT PASSES CMM CHECKS, RTS 2/4/05. 2L72 4T RTA52EU 20050303001422005030300142EU 2005 3 3 MALA050187 120050217A3350330151 POWER SUPPLY SAAB SF340 340B 7860101EU EMERGENCY LIGHT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15423XJ 340B423 EMERGENCY POWER SUPPLY P/N 3301-51, S/N 2063 FAILED CAPACITY CHECK. REPLACED BATTERY ASSEMBLY P/N 3301-31. PASSES CMM CHECKS, RTS 2/19/05. 2L72 4T RTA52EU 20050307000042005030700004NM 2005 3 7 05FDEA00338 120050302A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 BS 720D, RBL 4, WL 208 CORROSION ON FLOORBEAM. REPAIRED PER SRM 53-10-8 2L73 4F RTA3WE 20050307000062005030700006NM 2005 3 7 05FDEA00344 120050303A534065453136 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 BONUS HOLES IN STRINGER CLIP AT BS 950C STR 7R. REPLACED PER SRM 51-30-2. 2L73 4F RTA3WE 20050307000452005030700045EA 2005 3 7 QXEA200500237 120050215A5230 RETAINER CNDAIRCL600 CL6002C10 1390015EA ZONE 800 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - FORWARD BAGGAGE DOOR SEAL RETAINER DAMAGED AT VARIOUS LOCATIONS. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01 AND SRM 51-24-21-001-001-A01. 2L72 4F RTA21EA 20050307000472005030700047EA 2005 3 7 VNAA0502013 120050216A3610GG670800025 VALVE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE LT ENGINE BLEED FAILED A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL05168MD105 10168 WHILE CLIMBING AFTER TAKEOFF (CLT TO CLE) THE L ENG BLEED CAUTION MESSAGE ILLUMINATED. THE CREW OF FLIGHT 2239, FOLLOWED THE QRH, RETURNED TO CLT DUE TO ICING CONDITIONS AT DESTINATION, AND MADE AN UNEVENTFUL LANDING. AFTER TROUBLESHOOTING THE SYSTEM, PSA MAINTENANCE REMOVED AND REPLACED THE LT ENGINE (PRSOV) PRESSURE REGULATING AND SHUT OFF VALVE IAW CRJ 700 AMM 36-12-01-000-801-A01 & 36-12-01-400-801-A01. LEAK AND OPERATIONAL TESTS WERE GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050307000492005030700049EA 2005 3 7 VNAA0503001 120050301A3411 PITOT HEAD CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE BIRD INGESTION A VNAAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 GL05247JS 7922 AT ROTATION DURING TAKEOFF ROLL (DCA TO SDF) THE CAPTAIN'S AIRSPEED TAPE FAILED SHOWING NO INDICATION. SHORTLY THEREAFTER THE YAW DAMPNER, MACH TRIM, AND STAB TRIM, ALSO FAILED. THE CREW OF FLIGHT 2573 RETURNED TO DCA AND MADE AN UNEVENTFUL LANDING. CONTRACT MAINTENANCE AT DCA INSPECTED THE AIRCRAFT PITOT STATIC SYSTEM AND FOUND THE PILOT'S PITOT-STATIC PROBE CONTAMINATED WITH BIRD REMAINS. THE AIRCRAFT WAS FERRIED TO DAY WHERE PSA MAINTENANCE COMPLIED WITH P1 LINE CONTAMINATION REMOVAL PROCEDURES IAW CRJ 200 AMM 34-11-00-100-801 AND REMOVED AND REPLACED THE CAPTAIN'S PITOT-STATIC PROBE IAW CRJ 200 AMM 34-11-01-000-801 AND 34-11-01-400-801. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050307000512005030700051NM 2005 3 7 AWXA200500283 120050220A534724957075T73511 DUMMY RAIL AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28812AW 1178 SAL - MAJOR REPAIR - DURING BC-4 CHECK FOUND EXFOLIATION CORROSION ON UPPER FLANGE OF DUMMY RAIL -Y254 AT FR 20. MAINTENANCE CUT OUT DAMAGE IN UPPER FLANGE OF DUMMY RAIL -Y254 AT FR 20, FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED REPAIR PARTS IAW A320 SRM 53-11-14 FIG 201. 2L72 4F RTA28NM 20050307000532005030700053WP 2005 3 7 AALA20050148 120050202A2497 CABLE DOUG DC9 DC983 3022083WP OVERHEATED A AALAK NONE MJ OVER TEMP WARNING INDICATION ININSP/MAINT 1 SW21566AA 49348 TUL - GENERATOR WIRE FEEDER CABLE (APU) LEFT HAND AUXILIARY RELAY FEEDER CABLE NUMBER 3X1C2A AND 3X1D2A SHOW SIGNS OF OVERHEATING. REPLACED FEEDER CABLES MADE FROM ESO 81249. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050307000552005030700055EU 2005 3 7 CHQA200500040 120050224A3350340022 BATTERY PACK EMB ERJ170ERJ170100LR EU EMERGENCY LIGHT FAULTY A CHQAK NONE J WARNING INDICATION ININSP/MAINT 1 GL11640RW403 403 17000058 ON POWER UP AT THE GATE EMERGENCY LIGHT BATTERY FAULT MESSAGE APPEARED ON EICAS. FERRIED AIRCRAFT FROM ORD TO IND FOR MAINTENANCE. MAINTENANCE TROUBLESHOT THE AIRCRAFT AND FOUND THE NR 4 EMERGENCY BATTERY PACK FAULTY. REMOVED AND REPLACED NR 4 EMERGENCY BATTERY PACK PER AMM. OPS CHECK GOOD. 2L74 4F RTA56NM 20050307000572005030700057SO 2005 3 7 CHQA200500046 120050301A3350RPS1B BATTERY PACK EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT FAULTY A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11835RP 145702 UPON TURNING OFF THE POWER ON THE AIRCRAFT, THE AFT EMERGENCY LIGHTS ILLUMINATED AND WOULD NOT TURN OFF. REMOVED AND REPLACED THE NR 4 EMERGENCY POWER SUPPLY BATTERY IAW EMB 145 AMM 33-50-04. OPS CHECK GOOD. 2L72 4F RTT00011AT 20050307000592005030700059NM 2005 3 7 252TR0031 120050222A5320 INTERCOSTAL BOEING737 737228 13844AGNM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05252TR 23001 INTERCOSTAL ATTACH ANGLE CRACKED UNDER RIGHT TRANSITION ANGLE AT BS 947. REPLACED ATTACH ANGLE PER SRM 51-10-2. 2L72 4F RTA16WE 20050307000612005030700061NM 2005 3 7 SWAA050644 120050302A3350D71701100 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29754SW 29849 DURING SCHEDULED RON CHECK, FOUND LT & RT FWD EMERGENCY BULLNOSE LIGHTS INOP. REMOVED AND REPLACED BATTERY PACKS PER MM. 2L72 4F RTA16WE 20050307000632005030700063NM 2005 3 7 SWAA050646 120050302A53116546532 FRAME BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050307000652005030700065NM 2005 3 7 SWAA050648 120050302A534065C27314 STRINGER CLIP BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 DURING SCHEDULED SPECIAL VISIT, FOUND CRACKED STRINGER CLIP AT BS 787, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20050307000752005030700075SO 2005 3 7 MASA200500135 120050220A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07855MJ 145614 CLT TO STL HAD THE 3RD CEILING EMERGENCY EXIT FLOOD LIGHT INOP. MAINTENANCE RELAMPED THE LIGHT AND OPS CHECKED GOOD. A/C DEPARTED WITHOUT FURTHER INCIDENT. 2L72 4T RTT00011AT 20050307000772005030700077SO 2005 3 7 MASA200500139 120050221A3350 SIGN EMB 145 EMB145LR 3260212SO EMERGENCY EXIT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07826MJ 145214 CVG - CLT - AISLE OVERHEAD EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE RESECURED THE CANNON PLUG. 2L72 4T RTT00011AT 20050307000782005030700078SO 2005 3 7 MASA200500140 120050221A3350 SIGN EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07826MJ 145214 CLT - MKE, AISLE OVERHEAD EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE TESTED LIGHT AND OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050307000792005030700079SO 2005 3 7 MASA200500146 120050222A335066903 LIGHT EMB 145 EMB145LR 3260212SO CABIN FLOOR INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07828MJ 145218 CLT TO RIC - FWD FLOOR EMERGENCY LIGHT STRIP INOP. MAINTENANCE REPLACED THE FORWARD EMERGENCY LIGHT STRIP, OPS GOOD. 2L72 4T RTT00011AT 20050307000822005030700082CE 2005 3 7 DXTA200500610 120050227A3220 LANDING GEAR CESSNA650 650 2076802CE NOSE VIBRATION E DXTAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL07710QS 6507100 UPON NORMAL LANDING GEAR RETRACTION, NOSE GEAR WOULD RETRACT AND SOON AFTER (10 MIN) AUDIBLE BUMP WAS HEARD WITH NOTICABLE VIBRATION. APPROX 10 MIN LATER SAME SOUND & VIBRATION WAS HEARD A SECOND TIME, BUMP & VIBRATION WAS NOTED IN ALL PHASES OF FLIGHT. ITEM IS UNDER INVESTIGATION. 2L72 4F A9NM 20050307000862005030700086NM 2005 3 7 QXEA200500296 120050224A2810AV24B1319D3 VALVE DHAV DHC8 DHC8202 2809007NM REFUELING SYS LEAKING A QXEAK NONE O OTHER ININSP/MAINT 1 NM09362PH15340 518 PDX - MAINTENANCE FOUND THE SINGLE POINT REFUELING VALVE ADAPTER ASSEMBLY LEAKING AND REPLACED SAME. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050307000882005030700088SO 2005 3 7 CHQA200500041 120050225A33501317 LAMP EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11562RP 145451 LEFTHAND OVERWING EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED LEFTHAND OVERWING EMERGENCY EXIT LAMP IAW AMM 33-50-07-4. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050307000902005030700090EU 2005 3 7 CHQA200500044 120050225A27501700637 GEARBOX EMB ERJ170ERJ170100LR EU TE FLAPS BINDING A CHQAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 GL11635RW600 600 17000056 FLIGHT 7740 ORD-DFW - ON FINAL APPROACH INTO DFW, THE FLAPS FAILED AT THE SLAT 3/ FLAP 0 POSITION. FLAP FAIL MESSAGE APPEARED ON EICAS. THE APPROACH WAS ABORTED WHILE THE QRH WAS WORKED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED IN DFW UNEVENTFULLY. THE AIRCRAFT WAS FERRIED TO IND FOR MAINTENANCE. MAINTENANCE TROUBLESHOT THE FLAP SYSTEM AND FOUND THE RIGHTHAND INBOARD FLAP ANGLE GEARBOX TO BE BINDING. REMOVED AND REPLACED RIGHTHAND INBOARD FLAP ANGLE GEARBOX IAW EMB 170 AMM 27-50-00. OPS CHECK GOOD. 2L74 4F RTA56NM 20050307000912005030700091NM 2005 3 7 QXEA200500294 120050225A33506104781 BATTERY DHAV DHC8 DHC8202 2809007NM ZONE 200 INOPERATIVE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09362PH1884664 518 PDX - 2 BULBS ON EMERGENCY FLOOR LIGHTING INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 2 POWER SUPPLY BATTERY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050307000922005030700092NM 2005 3 7 QXEA200500295 120050226A2611473054 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM CARGO BAY MALFUNCTIONED A QXEAO OTHER N FALSE WARNING CRCRUISE 1 NM09375PH1215712157 529 SEA - FLIGHT 2027 - THE CREW REPORTED AN INTERMITTENT SMOKE WARNING LIGHT WHILE AT CRUISE. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED BOTH THE AFT AND FORWARD SMOKE DETECTORS. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050307000932005030700093NM 2005 3 7 252TR0032 120050222A5345 ATTACH BRACKET BOEING737 737228 13844AGNM RAM AIR DUCT CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05252TR 23001 RIGHT RAM AIR DUCT FORWARD UPPER O/B ATTACH BRACKET CRACKED. REPLACED ATTACH BRACKET PER SRM 51-10-2 AND 51-40-03. 2L72 4F RTA16WE 20050307000942005030700094NM 2005 3 7 252TR0033 120050222A7830 FAIRING BOEING737 737228 13844AGNM THRUST REVERSER CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05252TR 23001 RIGHT ENGINE O/B THRUST REVERSER FAIRING CRACKED AT THE I/B AFT END. WELDED PER BAC SPEC 5975. 2L72 4F RTA16WE 20050307000952005030700095NM 2005 3 7 252TR0034 120050222A5410 PANEL BOEING737 737228 13844AGNM RT NACELLE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05252TR 23001 RIGHT ENGINE I/B COWLING EXHAUST LOUVER PANEL CRACKED. WELDED PER BAC SPEC 5975. 2L72 4F RTA16WE 20050307000972005030700097SO 2005 3 7 MASA200500148 120050223A3350 SIGN EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07836MJ 145359 CLT - A LEFT OVERWING EMERGENCY EXIT SIGN THAT WAS INOPERATIVE. MAINTENANCE RESET POWER ON THE AIRCRAFT TO CLEAR FAULT. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050307000982005030700098EA 2005 3 7 MASA200500155 120050224A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSBURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0777286 7286 PHX TO MRY - OVERHEAD EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED THE LIGHT, OPS GOOD. 2L72 4F RTA21EA 20050307000992005030700099EA 2005 3 7 MASA200500157 120050226A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSBURNED OUT A MASAK NONE O OTHER ININSP/MAINT 1 SW0737342 7342 ON RON MAINTENANCE AND SCHEDULED FOR A ROUTINE CHECK INSPECTION. DURING THE WALK AROUND IT WAS DISCOVERED THE LT FORWARD EXTERIOR EMERGENCY LIGHT NOT ILLUMINATING. MAINTENANCE REPLACED THE LIGHT BULB AND OPERATIONAL CHECKED GOOD. 2L72 4F RTA21EA 20050307001002005030700100SO 2005 3 7 MASA200500158 120050226A335066367 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A MASAK NONE O OTHER ININSP/MAINT 1 SW07845MJ 145502 ON RON AND SCHEDULED FOR A 2A S&P INSPECTION. DURING THE WALK AROUND IT WAS DISCOVERED THE EMERGENCY LIGHTED FLOOR STRIP NOT ILLUMINATING. MAINTENANCE REPLACED THE LIGHTED FLOOR STRIP, OPERATIONAL CHECK GOOD. 2L72 4T RTT00011AT 20050307001012005030700101SO 2005 3 7 MASA200500160 120050226A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSBURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07847MJ 145517 CLT - FOURTH FROM FWD OVERHEAD EMERGENCY CABIN LIGHT INOP. MAINTENANCE REPLACED THE LIGHT. 2L72 4T RTT00011AT 20050307001022005030700102SO 2005 3 7 MASA200500162 120050227A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07838MJ 145384 CLT - 2Q ADJACENT EMERGENCY FLOOR PATH LIGHT STRIPS WERE INOP. MAINTENANCE CLEANED THE LIGHT STRIP CONNECTOR AND THE LIGHTS OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050307001032005030700103NM 2005 3 7 AALA20050149 120050207A5320 SUPPORT BOEING757 757223 1384957NM THRESHOLD CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21653A 24611 TUL - LEFT NR 4 DOOR THRESHOLD FORWARD DRAIN PAN SUPPORT AT STATION 1680 CORRODED THROUGH IN AREA OF 1 INCH BY 3 INCHES. REPLACED SUPPORT. 2L72 4F RTA2NM 20050307001052005030700105EA 2005 3 7 QXEA200500251 120050210A5210 STRIKER CNDAIRCL600 CL6002C10 1390015EA ZONE 200 BENT A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - FUSELAGE AT PASSENGER DOOR BOTTOM AFT RADIUS OF PRESSURE SEAL STRIKER BENT. REPAIRED IAW CRJ700 SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01 AND 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050307001072005030700107EA 2005 3 7 QXEA200500252 120050216A5210 PANEL CNDAIRCL600 CL6002C10 1390015EA ZONE 800 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - PASSENGER DOOR AFT SIDE ATTACH ANGLE BETWEEN STAIR FRAME AND DOOR PANEL CRACKED 1 INCH WHERE ASSIST MOTOR BRACKET LOCATED. REPAIRED IAW REO 670-52-11-072 AND CRJ700 SRM 51-42-22-001-001-A01. 2L72 4F RTA21EA 20050307001102005030700110NE 2005 3 7 SWAA050628 220050301A73211852M33P05 ECU BOEING737 7377H4 1384404NM CFMINTCFM567CFM567B22 13802NE NR 1 ENGINE FAULTY A SWAAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SW29742SW 29278 AIR TURNBACK, DECLARED EMERGENCY. DURING TAKEOFF ROLL, NR 1 ENGINE POWER, ALL PARAMETERS BECAME ERRATIC. THROUGH CLIMBOUT, ALL PARAMETERS FLUCTUATING, AROUND 10,000 FT, 2 LOUD COMPRESSOR STALLS. REMOVED AND REPLACED NR 1 EEC AND NR 1 VBV PER MM. 2L72 4F4 FRTA16WE E00055EN 20050307001122005030700112NM 2005 3 7 SWAA050630 120050301A3350311500 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29355SW 25250 BULLNOSE EMERGENCY EXIT LIGHT LENS BROKEN AT ROW 2. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20050307001142005030700114NM 2005 3 7 SWAA050632 120050301A53206545410 FLOOR SUPPORT BOEING737 7375H4 138449DNM MID CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29507SW 24184 DURING SCHEDULED 1/2D CHECK, FOUND CENTER CABIN LONGITUDINAL FLOOR SUPPORT CRACKED AT BS 664, BL 0. REPAIRED FLOOR SUPPORT PER SWA EA. 2L72 4F RTA16WE 20050307001162005030700116NM 2005 3 7 AWXA200500285 120050125A533065C337568 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK A .375 INCH CRACK WAS FOUND IN FUSELAGE SKIN EMANATING FROM FASTENER HOLE AT FORWARD UPPER CORNER CUTOUT OF R-1 DOOR. MAINTENANCE TRIMMED OUT CRACK IN FUSELAGE SKIN FORWARD UPPER CORNER CUTOUT OF R-1 DOOR; FABRICATED FILLERS, REPAIR STRAP & DOUBLER, AND TRIPLER; INSTALLED REPAIR PARTS IAW ER 03-5300-05055-ES1. 2L72 4F RTA16WE 20050307001182005030700118NM 2005 3 7 AWXA200500287 120050127A532069165096 CLIP BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK A .0265 INCH CRACK WAS FOUND IN RADIUS OF ANGLE CLIP AT AFT SIDE OF STRINGER SPLICE CHANNEL BS 348.2, STR 16 LT. MAINTENANCE REMOVED CRACKED ANGLE CLIP FROM BS 348.2 TO BS 351.2, STR 16 LT; FABRICATED NEW REPLACEMENT CLIP; INSTALLED REPAIR PART IAW ER 03-5300-05053-SS3. 2L72 4F RTA16WE 20050307001192005030700119NM 2005 3 7 QXEA200500297 120050226A272183910048019 CONTROL PANEL DHAV DHC8 DHC8202 2809007NM RUDDER TRIM FAILED A QXEAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 NM09346PH18570 477 SEA - FLIGHT 2184 - THE FLIGHT RETURNED TO FIELD WHEN THE CREW WAS UNABLE TO TRIM THE RUDDER TO THE RIGHT. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE AILERON/RUDDER TRIM PANEL. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050307001202005030700120NM 2005 3 7 QXEA200500298 120050226A2611473054 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM CARGO BAY FAILED A QXEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM09352PH17324 494 SEA - FLIGHT 2028 - THE FLIGHT RETURNED TO FIELD AFTER RECEIVING A BAGGAGE SMOKE WARNING AFTER TAKE-OFF. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE BAGGAGE COMPARTMENT SMOKE DETECTORS. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETUNED TO SERVICE. 2H72 4T RTA13NM 20050307001222005030700122EA 2005 3 7 QXEA200500258 120050213A5210 RIVET CNDAIRCL600 CL6002C10 1390015EA ZONE 800 LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - PASSENGER DOOR FORWARD NEWEL HAS LOOSE RIVETS AT SPRING FOR HANDRAIL STRUCTURE. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20050307001242005030700124EA 2005 3 7 QXEA200500260 120050210A5730 FASTENER CNDAIRCL600 CL6002C10 1390015EA ZONE 500 LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - LEFTHAND WING UPPER SKIN SURFACE TRAILING EDGE HAS LOOSE FASTENERS AT STATION 231.23 AND 172. REPAIRED IAW CRJ700 SRM 51-25-01-001-001-A01 AND SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20050307001262005030700126NM 2005 3 7 SWAA050635 120050301A57536546435 SKIN BOEING737 7373H4 1384600NM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29386SW 26601 DURING SCHEDULED C1 CHECK, FOUND DELAMINATION ON RT WING T/E OUTBOARD AFT FLAP. REMOVED AND REPLACED RT WING T/E OUTBOARD AFT FLAP PER MM. 2L72 4F RTA16WE 20050307001282005030700128NM 2005 3 7 SWAA050637 120050301A53116546555 FRAME BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 9L. REPAIRED FUSELAGE FRAME PER SRM. 2L72 4F RTA16WE 20050307001302005030700130NM 2005 3 7 SWAA050639 120050301A53116520722 FRAME BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 9R. REPAIRED FUSELAGE FRAME PER SRM. 2L72 4F RTA16WE 20050307001322005030700132NM 2005 3 7 SWAA050641 120050301A53206545833 WEB BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND 2 EA FLOOR WEB CRACKS BETWEEN BS 188 TO BS 196, STR 17L & STR 17R. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050307001342005030700134NM 2005 3 7 SWAA050649 120050302A53126516300 BULKHEAD BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29507SW 24184 DURING SCHEDULED 1/2D CHECK, FOUND CRACK AT BS 178 BULKHEAD, WL 198, RBL 5.7. REPAIRED BULKHEAD PER SRM. 2L72 4F RTA16WE 20050307001352005030700135NE 2005 3 7 VNAA0502012 220050215A7261 SCREEN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE SCAV PUMP DIRTY A VNAAO OTHER J WARNING INDICATION CRCRUISE 1 GL05223JS 7892 GEE950034 DURING CRUISE AT FL 360 (PHL TO MSP) THE CREW OF FLIGHT 2501 REPORTED THAT THE RT ENGINE OIL PRESSURE WAS FLUCTUATING BETWEEN 25-35 PSI. OIL TEMPERATURE WAS 132 DEGREES. THE CREW DECENDED TO FL 290 WHERE THE OIL PRESSURE STABILIZED AT 42 PSI AND ALL ENGINE INDICATIONS WERE NORMAL. THE FLIGHT CONTINUED TO MSP AND MADE AN UNEVENTFUL LANDING. AFTER CONTRACT MAINTENANCE IN MSP INSPECTED THE ENGINE FOR PROPER OIL QUANTITY THE AIRCRAFT WAS FERRIED TO DAY. PSA MAINTENANCE REMOVED THE RT ENGINE LUBE/SCAVANGE PUMP, CLEANED THE INLET SCREENS, AND REINSTALLED THE PUMP IAW CRJ 200 AMM 79-21-01-000-801 AND 79-21-01-400-801. ALL OPERATIONAL AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050307001372005030700137 2005 3 7 DLM88050104 420050210A22202589445933 ACTUATOR DOUG MD88 MD88 3023688NM RUDDER UNKNOWN A DALAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO27964DL 49983 REQD 6 DEG RT RUDDER, 1 DEG RT AILERON FOR LEVEL AND TRIMMED FLT. RETURNED CVG. REPLACED YAW DAMP ACTUATOR PER MM. PERFORMED RTS ON BOTH DFGC'S GO. 2L72 4F RTA6WE 20050307001392005030700139CE 2005 3 7 DXTA200500608 120050223A3260602751 DOWNLOCK SWITCH CESSNA750 750 2076810CE MLG FAILED E DXTAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL07979QS 7500079 IN CRUISE FLIGHT NOSE GEAR DOWN AND LOCKED LIGHT ILLUMINATED AND REMAINED ILLUMINATED. DID NOT HEAR OR FEEL EVIDENCE THAT NOSE ACTUALLY CAME DOWN. EMERGENCY PNEUMATIC BLOW DOWN PROCEDURE WAS USED AS A PRECAUTION FOR LANDING. REMOVED AND REPLACED NOSE GEAR DOWNLOCK SWITCH IAW CE750 M/M CHAPTER 32-30-05, SYSTEM OPS CHECK GOOD. 2L72 4J RTT00007WI 20050307001412005030700141NM 2005 3 7 375PA0045 120050221A5340 ATTACH FITTING BOEING737 73739A 138447PNM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05375PA 23812 INTERCOSTAL ATTACH CLIP CRACKED UNDER AFT END OF RIGHT TRANSITION ANGLE AT BS 947 BETWEEN STR 26 RT AND STR 25 RT. REPLACED ATTACH CLIP PER SRM 51-10-02. 2L72 4F RTA16WE 20050307001452005030700145EU 2005 3 7 MALA050181 120050128A33506104789 BATTERY PACK SAAB SF340 SF340A 7850100EU EMERGENCY LIGHT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL1527XJ 340A027 BATTERY PACK 61-0478-9, S/N M005. REMOVED FOR SCHEDULED CAPACITY CHECK. CAPACITY CHECK FAIL. REPLACED CELL PACK 55-2198-1. UNIT PASSES CMM TESTS, RTS 2-3/05. 2L72 4T RTA52EU 20050307001492005030700149EU 2005 3 7 MALA050175 120050127A33506104789 BATTERY PACK SAAB SF340 SF340A 7850100EU FUSELAGE FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15110XJ 340A110 BATTERY PACK 61-0478-9, S/N 1875. FAILED SCHEDULED CAPACITY CHECK. REPLACED BATTERY ASSEMBLY P/N 55-2198-1, UNIT PASSES, RTS 1/31/05. 2L72 4T RTA52EU 20050307001512005030700151NM 2005 3 7 375PA0039 120050221A5320 FLOOR SUPPORT BOEING737 737317 138447PNM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05375PA 23812 AFT CARGO FLOOR PANEL SUPPORT ANGLE CRACKED AT NUT PLATE AT BS 727D +7 AT LBL 3. REPAIRED PER SRM 53-00-53. 2L72 4F RTA16WE 20050307001532005030700153NM 2005 3 7 ABXA050034 120050206A5754114T411417 WEDGE BOEING767 767281 1385109NM LT WING SLAT DELAMINATED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23775AX 22790 WHILE PERFORMING LINE MAINTENANCE, FOUND LEFT WING NR 4 SLAT WEDGE DELAMINATED BEYOND LIMITS AT INBOARD END. REPLACED NR 4 SLAT IAW B767 MM 27-81-02-4. 2L72 4F RTA1NM 20050307001552005030700155 2005 3 7 ABXA050029 420050217A2565 GIRT BAR BOEING767 767231 1385131NM ESCAPE SLIDE FAILED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23702AX 22566 LT FORWARD ENTRY DOOR GIRT BAR FAILED TO LOCK. PLACED MED EMERGENCY ESCAPE SLIDE ON DEFERRAL AND MAINTENANCE PROCEDURES COMPLIED WITH. CLEARED DEFERRAL. FOUND SEAL ON LOWER FORWARD BUSTLE BINDING. TRIMMED SEAL ON BUSTLE AND EMERGENCY SLIDE ARMS NORMAL IAW B767 MM 25-66-05. 2L72 4F RTA1NM 20050307001572005030700157WP 2005 3 7 ABXA050032 120050121A5410995819125 ANGLE DOUG DC9 DC933F 302207AWP LT PYLON CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23935AX 47413 CRACK INDICATION ON ANGLE, UPPER INTERIOR SURFACE OF PYLON, 3RD FROM FRONT SPAR. REMOVED ANGLE, FABRICATED NEW ANGLE, REINSTALLED ANGLE IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 20050307001592005030700159WP 2005 3 7 ABXA050036 120050221A3260 CONNECTOR DOUG DC8 DC863F 302198FWP MLG DAMAGED A ABXAO OTHER N FALSE WARNING APAPPROACH 1 GL23826AX 46061 RIGHT MAIN LANDING GEAR GREEN LIGHT WOULD NOT COME ON WHEN THE GEAR WAS EXTENDED. CYCLED THE GEAR TWICE AND THE LIGHT STARTED WORKING. FOUND CORROSION ON P1-1398 AND S1-210. REMOVED AND REPLACED CONNECTOR P1-1398 AND RIGHT LANDING GEAR DOWN SWITCH S1-120. PERFORMED GEAR SWING, RIGHT LANDING GEAR INDICATION OPS CHECKED GOOD IAW DC-8 AMM 32-60-00-2. 2L74 4F 4A25 20050307001612005030700161NM 2005 3 7 AWXA200500244 120050222A33501012621 LIGHT BOEING737 737301 1384611NM RT OVERWING INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28324AW 23261 PHX - EEL - DURING 8-DAY CHECK FOUND THE EMERGENCY LIGHT ASSEMBLY AT LOWER FORWARD CORNER OF THE RT OVERWING EMERGENCY EXIT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED RT OVERWING EMERGENCY EXIT LIGHT ASSEMBLY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050307001632005030700163NM 2005 3 7 AWXA200500246 120050122A53206546877144 WEB BOEING737 7373G7 1384595NM RT MLG WW CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 MCN - MAJOR REPAIR - DURING C-16 CHECK A .875 INCH CRACK WAS FOUND IN WEB AT UPPER AFT OUTBOARD CORNER OF RT MAIN WHEEL WELL BS 727. MAINTENANCE TRIMMED OUT CRACK IN WEB AT UPPER AFT OUTBOARD CORNER OF RT MAIN WHEEL WELL BS 727; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A FILLER, RADIUS FILLER, AND GUSSET; INSTALLED REPAIR PARTS IAW ER 03-5300-05048-ES1. 2L72 4F RTA16WE 20050307001652005030700165NM 2005 3 7 AWXA200500248 120050128A521050079452 SKIN BOEING737 737301 1384611NM L1 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK A .375 INCH CRACK WAS FOUND IN L-1 DOOR EXTERNAL SKIN AT LOWER HINGE CUTOUT BS 317, STR 14 LT. MAINTENANCE CUT OUT CRACK IN L-1 DOOR EXTERNAL SKIN AT LOWER HINGE CUTOUT BS 317, STR 14 LT; FABRICATED REPAIR DOUBLER; INSTALLED REPAIR PART IAW ER 03-5210-05033-SS1. 2L72 4F RTA16WE 20050307001682005030700168EA 2005 3 7 SWIA200514525 120050206A27507805013 LEVER CNDAIRCL600 CL6002B19 1900309EA FLAP CONTROL MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CRCRUISE 1 NM07403SW1279612796 7028 FLAPS FAIL CAUTION MESSAGE DURING CRUISE. REMOVED AND REPLACED FLAP HANDLE ASSY IAW MM CH 27-51-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050307001702005030700170CE 2005 3 7 DXTA200500604 120050221A3010S100420PG SENSOR CESSNA750 750 2076810CE ANTI ICE TEMP FAILED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07971QS5254 7500071 ABORTED T/O DUE TO WING A/I HOT L CAS MESSAGE. RAN ENG, TURNED ON SLAT ALI FELT LT & RT WING L/E'S DID GET WARN. I/B LT WING L/E REMOVED TO INSPECT WING L/E A/I DUCT O-RING. ACCESSED IMT I/B, MID & O/B WING, TEMP NORMAL. COULD NOT DUPLICATE CN SUBSEQUENT ENGINE RUN. REMOVED LT I/B L/E WING, INSPECTED BLEED AIR TUBING, FOUND O-RINGS WORN. REMOVED LT WING L/E ALI TEMP SENSOR P/N S100420PG, S/N 3970A. INSTALLED A NEW SENSOR P/N-S101816PG, S/N -1004. REMOVED & REPLACED (3) O-RINGS P/N 2-214S469-40 FROM HEATED L/E LT DUCT WORK. RE-INSTALLED LT I/B HEATED L/E & WING ROOT FAIRING. RAN ENG. TUNRED ON SLAT ALI WING I/B, MID & O/B, TEMPS NORMAL. NO BLEED AIR LEAKS, OPS GOOD. RESEALED LT I/B HEATED L/E. 2L72 4J RTT00007WI 20050307001752005030700175SO 2005 3 7 MASA200500093 120050209A783083990152 SWITCH EMB EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL THRUST REVERSER WORN A MASACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SW07833MJ9850 TR0549 145327 CAE312003 ASH - CLE AIRCRAFT ABORTED TAKEOFF AND RETURNED TO THE GATE. RT REVERSER DISAGREE MESSAGE DURING TAKEOFF PRIOR TO 80 KTS. CONTRACT MAINTENANCE PERFORMED THE REQUIRED MAINTENANCE ACTION TO DEFER THE REVERSER. MAINTENANCE REPLACED STOW SWITCH. 2L72 4T4 FRTT00011ATTE6CH 20050307001762005030700176SO 2005 3 7 MASA200500100 120050211A212014522273401 DUCT EMB 145 EMB145LR 3260212SO NR 2 PACK UNKNOWN A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW07860MJ 145773 CLT TO BNA HAD THE NR 2 PACK PRODUCE A BURNING SMELL WHILE IN USE. MAINTENANCE PLACED THE PACK ON MEL. AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED 3 DUCTS, OPS CHECKED GOOD. P/N 145-22273-401, 145-22277-403 AND 145-22285-401, ALL NON SEARILIZED. 2L72 4T RTT00011AT 20050307001772005030700177SO 2005 3 7 MASA200500123 120050216A551114535184003 RIB EMB 145 EMB145LR 3260212SO EMPENNAGE CRACKED A MASAK NONE O OTHER ININSP/MAINT 1 SW07851MJ7189 145572 IN C-CHECK EMPENNAGE INTERNAL RIB IS CRACKED AND IS BEING REPLACED IAW SRM 51-40-02. 2L72 4T RTT00011AT 20050307001842005030700184NM 2005 3 7 SWAA050520 120050222A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACK AT STA 931, STR 24R. REPAIRED SKIN PER EA & SRM. 2L72 4F RTA16WE 20050307001852005030700185NM 2005 3 7 SWAA050508 120050221A3350101114 LAMP BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29363SW 26574 DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM. 2L72 4F RTA16WE 20050307001862005030700186NM 2005 3 7 SWAA050509 120050221A53116546550 FRAME BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 787, STR 9R CRACKED. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20050307001872005030700187NM 2005 3 7 SWAA050510 120050221A339765C27093 WIRE BOEING737 7375H4 138449DNM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29523SW 26565 DURING SCHEDULED SERVICE CHECK, FOUND L1 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REPAIRED WIRE PER WDM. 2L72 4F RTA16WE 20050307001882005030700188NM 2005 3 7 SWAA050511 120050221A53106519603 CREASE BEAM BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB FROM BS 360 TO BS 371, LBL 64, CORRODED. REMOVED AND REPLACED CREASE BEAM SECTION WEB PER SRM. 2L72 4F RTA16WE 20050307001892005030700189NM 2005 3 7 SWAA050512 120050221A575465C26603 SKIN BOEING737 7373Q8 1384670NM LT WING SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND NR 3 L/E SLAT DELAMINATED. REPAIRED NR 3 L/E SLAT PER SRM. 2L72 4F RTA16WE 20050307001902005030700190NM 2005 3 7 SWAA050513 120050221A57436582764 BEAM BOEING737 7373Q8 1384670NM LT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND LT MLG ATTACH BEAM CORRODED. REPAIRED ATTACH BEAM PER ER. 2L72 4F RTA16WE 20050307001912005030700191EU 2005 3 7 MALA050176 120050127A3350501171202 POWER SUPPLY SAAB SF340 340B 7860101EU EMERGENCY LIGHT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15444XJ 340B444 EMERGENCY POWER SUPPLY P/N 501-1712-02, S/N 2089 FAILED SCHEDULED CAPACITY CHECK. REPLACED 2 EA CELL PACKS P/N 549-1329-06. UNIT PASSES CMM CHECKS, UNIT RTS 1/31/05. 2L72 4T RTA52EU 20050307001922005030700192NM 2005 3 7 SWAA050514 120050221A534065C27314 STRINGER CLIP BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29502SW 24179 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP AT BS 287,STR 16L CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20050307001932005030700193NM 2005 3 7 SWAA050515 120050221A53116545805 FRAME BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29502SW 24179 DURING SCHEDULED 1/2D CHECK, FOUND FRAME AT BS 287,STR 16L CRACKED. REPAIRED FRAME SECTION PER EA. 2L72 4F RTA16WE 20050307001942005030700194 2005 3 7 SWAA050506 420050221A2565D31354 SLIDE BOEING737 7373Q8 1384670NM R1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 R1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050307001952005030700195NM 2005 3 7 CALA0500050 120050222A531565339502 FLOORBEAM BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2727610 27323 INSPECTION FOUND AFT ENTRY FLOORBEAM CORRODED AT FASTENER HOLES, STA 986.5, LBL 54 TO RBL 54. REPAIRED IAW ECRA 5310-04461. 2L72 4F RTA16WE 20050307001962005030700196NM 2005 3 7 CALA0500051 120050217A5315143N5015 FLOORBEAM BOEING757 757224 1384958NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2757111 27301 INSPECTION FOUND CORROSION ON FLOORBEAM IN L-2 DOOR AREA AT BS 720, LBL 65. REPAIRED IAW SRM 53-00-51, FIGURE 201. 2L72 4F RTA2NM 20050307001972005030700197NM 2005 3 7 CALA0500052 120050222A53106546533 SHEAR TIE BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717309 23360 INSPECTION FOUND SKIN CLIP CORRODED AT STA 500, RBL 2 IN FORWARD BAGGAGE BIN FLOOR AREA. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-00-07 FIGURE 207. 2L72 4F RTA16WE 20050307001982005030700198NM 2005 3 7 CALA0500053 120050211A53207075173 INTERCOSTAL BOEING757 757224 1384958NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2757111 27301 INSPECTION FOUND GALLEY SUPPORT INTERCOSTAL CORRODED AT BS 680-700, RBL 15. THE GALLEY SUPPORT INTERCOSTAL WAS REPLACED IAW SRM 51-40-02, PARA 4 AND 7. 2L72 4F RTA2NM 20050307001992005030700199NM 2005 3 7 CALA0500054 120050217A5315 FLOORBEAM BOEING757 757224 1384958NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2757111 27301 INSPECTION FOUND FLOORBEAM UPPER STRAP CORRODED AT BS 720 FROM LBL 60 TO RBL 60. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND REPLACED IAE SRM 51-40-05. 2L72 4F RTA2NM 20050307002002005030700200EU 2005 3 7 MALA050165 120050221A53477253721459 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15423XJ 340B423 LAV/GALLEY SEAT TRACK, P/N 7253721-459, IS CORRODED AND IS BEING REPLACED IAW SRM 51-40-27. FOUND DURING 4Y/2Y CHECK IN BNA. 2L72 4T RTA52EU 20050307002012005030700201EU 2005 3 7 MALA050166 120050221A53207253721495 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15423XJ 340B423 LAV/GALLEY SEAT TRACK PROFILE, P/N 7253721-495 IS CORRODED IAW SRM 51-40-22. FOUND DURING 4Y/2Y CHECK IN BNA. 2L72 4T RTA52EU 20050307002022005030700202EU 2005 3 7 MALA050167 120050221A53207253711245 PLATE SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15423XJ 340B423 LT WRAP AROUND, P/N 7253711-245, AT FS 294, FROM LBL 18.3 TO LBL 36, IS CORRODED AND WILL BE REPLACED. FOUND DURING 4Y/2Y CHECK IN BNA. 2L72 4T RTA52EU 20050307002032005030700203EU 2005 3 7 MALA050168 120050221A53207253710243 PLATE SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15423XJ 340B423 RT WRAP AROUND, P/N 7253710-243, IS CORRODED AND WILL BE REPLACED IAW SRM 51-40-21. FOUND DURING 4Y/2Y CHECK IN BNA. 2L72 4T RTA52EU 20050307002042005030700204EU 2005 3 7 MALA050172 120050221A53207253710243 RISER SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15414XJ 340B414 DURING 4K CHECK IN BNA FOUND RT RISER P/N 7253710-243, IS CORRODED AND WILL BE REPLACED IAW SRM 51-40-21. 2L72 4T RTA52EU 20050307002052005030700205EU 2005 3 7 MALA050173 120050204A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15402XJ 340B402 DURING 4K CHECK IN BNA FOUND SEAT TRACK AT LBL 18.3 IS CORRODED OUT OF LIMITS FROM FS 298 TO FS 345 AND WILL BE REPLACED IAW MESABA EOS53060. 2L72 4T RTA52EU 20050307002062005030700206NM 2005 3 7 375PA0035 120050221A361032895625 VALVE BOEING737 737317 138447PNM PRE COOLER CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05375PA 23812 RIGHT ENGINE PRE-COOLER VALVE CRACKED. REPLACED PER-COOLER VALVE PER MM 36-12-35. 2L72 4F RTA16WE 20050307002072005030700207NM 2005 3 7 QXEA200500224 120050211A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09365PH 526 PDX - LEFTHAND INBOARD SEAT TRACK NR 4 CORROSION ON OUTBOARD FLANGE APPROXIMATELY X203 TO X208 AND X219 TO X221. REPAIRED IAW DHC-8/200 SRM 51-40-11 AND RD 8-53-4473. 2H72 4T RTA13NM 20050307002082005030700208NM 2005 3 7 QXEA200500222 120050206A5730 PANEL DHAV DHC8 DHC8202 2809007NM ZONE 600 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09365PH 526 PDX - RIGHT WING PANEL 623AT COUNTER SINKS HAVE FRETTING. REPAIRED IAW RD 8-57-1715. 2H72 4T RTA13NM 20050307002092005030700209NM 2005 3 7 QXEA200500225 120050211A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09365PH 526 PDX - LEFTHAND INBOARD SEAT TRACK NR 5 CORROSION AROUND RIVETS ON OUTBOARD FLANGE APPROXIMATELY X510 TO X524. REPAIRED IAW DHC-8/200 SRM 51-40-11 AND RD 8-53-4472. 2H72 4T RTA13NM 20050307002102005030700210NM 2005 3 7 QXEA200500221 120050206A5730 PANEL DHAV DHC8 DHC8202 2809007NM ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09365PH 526 PDX - LEFT WING PANEL 523AT COUNTER SINKS HAVE FRETTING. REPAIRED IAW RD 8-57-1715. 2H72 4T RTA13NM 20050307002112005030700211NM 2005 3 7 QXEA200500226 120050211A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09365PH 526 PDX - LEFTHAND INBOARD SEAT TRACK NR 6 CORROSION AROUND RIVETS ON OUTBOARD FLANGE APPROXIMATELY X533 TO X540. REPAIRED IAW DHC-8/200 SRM 51-40-11 AND RD 8-53-4472. 2H72 4T RTA13NM 20050307002122005030700212EA 2005 3 7 05047676 120050216A2750 FCU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A VTZAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 EA27676BR 7644 EVENT SUMMARY STATED FLAP FAILB AT 0 DEG. REMOVED AND REPLACED FECU AND OPS CHECK GOOD. 2L72 4F RTA21EA 20050302001682005030200168NM 2005 3 2 USAA050080 120050102A5713 STRINGER BOEING737 7373B7 1384580NM RT WING CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19522AU49282 23857 PIT - FOUND STRINGER CRACKED .5 INCH, RT WING WBL 355 AT S-8. REPAIR ANGLES PER EA 79684. (M) 2L72 4F RTA16WE 20050303000042005030300004NM 2005 3 3 SWAA050584 120050227A335008163 LIGHT BOEING737 7377H4 1384404NM CABIN OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29785SW 30602 EEPLS OUT OF ADJUST ON LT SIDE AT ROW 8. REINSTALLED EEPLS PER MM. 2L72 4F RTA16WE 20050303000082005030300008EA 2005 3 3 05056669 120050225A2150 A/C PACK CNDAIRCL600 CL6002B19 1900309EA LEFT MALFUNCTIONED A VTZAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA27669BR 7545 ABORTED TAKEOFF FOR LT PACK OVERPRESSURE. PACK DEFERRED. 2L72 4F RTA21EA 20050303000102005030300010 2005 3 3 05056627 420050225A3418 COMPUTER CNDAIRCL600 CL6002B19 1900309EA STALL WARNING FAILED A VTZAO OTHER J WARNING INDICATION CLCLIMB 1 EA27627BR 7233 STALL FAIL CAUTION ON TAKEOFF. CONTINUED FLIGHT TO SCHEDULED DESTINATION. MX RESET SPC. 2L72 4F RTA21EA 20050303000132005030300013NM 2005 3 3 QXEA200500220 120050204A5313 STRINGER BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 PDX - STRINGER 27 STARBOARD SIDE, IS CORRODED AT STATION X-29 TO -26. REPAIRED IAW Q400 SRM 51-21-10 AND SRM 51-25-10. 2H72 4T RTA13NM 20050303000352005030300035EA 2005 3 3 050546237 120050223A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27623BR 7192 LEFT FS 718 FRAME CRACKED AT 1 INCH IN LENGTH. CRACK IS BELOW EXISTING REPAIR. 2L72 4F RTA21EA 20050303000432005030300043NM 2005 3 3 SWAA050589 120050225A3350101114 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29627SW 27935 L1 DOOR EMERGENCY EXIT LENS BROKEN. REMOVED AND REPLACED L1 DOOR EMERGENCY EXIT LENS PER MM. 2L72 4F RTA16WE 20050303000462005030300046NM 2005 3 3 SWAA050592 120050226A3350207377 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29445WN 29841 DURING SCHEDULED MV1 CHECK, FOUND FWD END OF EEPLS LENS MISSING. INSTALLED EEPLS LENS PER MM. 2L72 4F RTA16WE 20050303000472005030300047NM 2005 3 3 SWAA050593 120050225A5313BAC1498 STRINGER BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON FUSELAGE STRINGER SPLICE AT BS 358, STR 27R. REPAIRED FUSELAGE STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20050303000552005030300055NM 2005 3 3 SWAA050618 120050228A55116547983 RIB BOEING737 7373Q8 1384670NM LT HORIZ STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND LT HORIZONTAL STAB L/E NR 1 RIB CRACKED. REPAIRED LT HORIZONTAL STAB RIB PER SRM. 2L72 4F RTA16WE 20050303000602005030300060NM 2005 3 3 SWAA050600 120050225A534065C27314 STRINGER CLIP BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP AT BS 500D, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20050303000712005030300071NM 2005 3 3 0500175642 120050213A332013431 BALLAST BOEING757 757251 1384970NM LAV LIGHT BURNED A NWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 GL01542US 26489 ON DESCENT 28,000 FT, REAR FLIGHT ATTENDANT REPORTED ELECTRICAL SMOKE AND FUMES. INSTRUCTED FLIGHT ATTENDANT TO PULL ALL CIRCUIT BREAKERS AND DECLARED AN EMERGENCY. SMOKE DISSIPATED AND LANDING WAS UNEVENTFUL. REPLACED BURNED LAVATORY BALLAST. OPERATIONAL CHECK GOOD. 2L72 4F RTA2NM 20050303000742005030300074NM 2005 3 3 0500205807 120050216A21216455072 FAN BOEING757 757351 1384991NM CABIN RECIRC FAILED A NWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL01587NW7323 7323 32986 FLIGHT ATTENDANT REPORTED STRONG SMELL OF SMOKE AND FUMES. CO-PILOT COULD SMELL ELECTRICAL FUMES. AN EMERGENCY WAS DECLARED, DIVERTED TO HNL, AND LANDED UNEVENTFULLY. FOUND AIR CHECK VALVE AND CABIN RECIRCULATION FAN INOPERATIVE. REPLACED CHECK VALVE AND RIGHT RECIRCULATION FAN. OPERATIONAL CHECK GOOD. 2L72 4F RTA2NM 20050303000962005030300096NM 2005 3 3 SWAA050558 120050223A33509250071 LAMP BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29424WN 29828 FWD END OF EEPLS INOP. REMOVED AND REPLACED EEPLS LAMP PER MM. 2L72 4F RTA16WE 20050303000992005030300099 2005 3 3 SWAA050561 420050223A256563550 SLIDE BOEING737 7377H4 1384404NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29704SW 27838 DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. REINSTALLED L2 DOOR SLIDE PER MM. 2L72 4F RTA16WE 20050303001012005030300101 2005 3 3 SWAA050563 420050223A25656557463 FITTING BOEING737 737317 138447PNM GIRT BAR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 DURING SCHEDULED SPECIAL VISIT, FOUND R1 DOOR ESCAPE SLIDE GIRT BAR, AFT FLOOR FITTING CRACKED. REMOVED AND REPLACED R1 DOOR ESCAPE SLIDE FLOOR FITTING PER MM. 2L72 4F RTA16WE 20050303001042005030300104NE 2005 3 3 RAIA00502025 220050216A7320 EEC JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114HR 01514NE RT ENGINE MALFUNCTIONED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03563HK 41079 RDU - RIGHT ENGINE INTEGRATED ENGINE CONTROL FAULT INDICATION. MAINTENANCE RESET RT IEC AND OPS CHECKED GOOD. 2L72 4T4 TRTA41NM E18NE 20050303001062005030300106NE 2005 3 3 RAIA00502020 220050213A7311P161121 OIL COOLER JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114GR 01514NE LT ENGINE LEAKING A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03557HK18067 41074 76100 GSO - LEFT ENGINE LOW OIL PRESSURE WARNING INDICATION. MAINTENANCE REMOVED AND REPLACED NR 1 FUEL OIL COOLER. 2L72 4T4 TRTA41NM E18NE 20050303001162005030300116EU 2005 3 3 MALA050157 120050217A3030QR5OV SENSOR SAAB SF340 340B 7860101EU PITOT ANTI ICE FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15446XJ 340B446 LT PITOT ICE PROTECTION FAILED EN ROUTE (VMC DAY) RESET C/B F-27 ONCE AS PER QRH RETURN TO MSP PER MXCX. REPLACED 5HG CURRENT SENSOR AND COMPLETED FUNC TEST PER AMM 30-30-00-5. OPS CHECK GOOD. CURRENT SENSOR P/N ON/OFF QR50V. 2L72 4T RTA52EU 20050303001182005030300118EU 2005 3 3 MALA050159 120050217A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15424XJ 340B424 DURING 4Y/2Y CHECK FOUND GALLEY SEAT TRACK, P/N 7253721-459 AND PROFILE, P/N 7253721-495 ARE CORRODED. ITEMS ARE BEING REPLACED IAW SRM 51-40-21 AND 51-40-22. 2L72 4T RTA52EU 20050303001202005030300120EU 2005 3 3 MALA050161 120050217A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15424XJ 340B424 DURING 4Y/2Y CHECK FOUND SEAT TRACK AT BL 0, FROM FS 621 TO FS 686 IS CORRODED OUT OF LIMITS IN 2 AREAS AND WILL BE REPAIRED IAW MESABA EOS53078. 2L72 4T RTA52EU 20050303001232005030300123NM 2005 3 3 375PA0027 120050221A5347 SEAT TRACK BOEING737 73739A 138447PNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05375PA 23812 CORROSION IN FORWARD END OF RIGHT O/B SEAT TRACK UNDER THE WIND SCREEN. REPLACED SECTION OF SEAT TRACK PER SRM 53-00-52. 2L72 4F RTA16WE 20050303001252005030300125NM 2005 3 3 SWAA050549 120050222A534065C27314 STRINGER CLIP BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP AT BS 578, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20050303001362005030300136 2005 3 3 AALA20050127 420050218A2565 BOTTLE AIRCRUISERS BOEING757 757231 1384950NM ESCAPE SLIDE DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21716TW 28484 LAS - NR 3 RIGHT DOOR SLIDE BOTTLE PRESSURE BELOW GREEN BAND AND OUT OF LIMITS. EXPIRATION ON SLIDE IS 09/01/2005. SLIDE DID NOT DEPLOY ON TEST. REPLACED SLIDE ON NUMBER THREE RIGHT HAND DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050303001452005030300145EU 2005 3 3 MALA050180 120050125A33506122751 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU EMERGENCY LIGHT INOPERATIVE A MALAK NONE L NO TEST ININSP/MAINT 1 GL15534XJ E2370 BATTERY PACK P/N 61-2275-1, S/N 0006355 REMOVED FOR SCHEDULED CAPACITY CHECK. CAPACITY CHECK FAIL. REPLACED BATTERY ASSEMBLY P/N 61-2274-1. UNIT PASSES CMM CHECKS, RTS 1/27/05. 2H74 4F RTA49EU 20050307000022005030700002NM 2005 3 7 252TR0028 120050222A5330 SKIN BOEING737 737228 13844AGNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05252TR 23001 CORROSION IN LOWER SKIN AT STR 27 LT BETWEEN BS 500A AND BS 500B AND DAMAGE IN KEEL BEAM RUN-OUT AREA. REPAIRED PER EA 53-031. 2L72 4F RTA16WE 20050307000872005030700087SO 2005 3 7 CHQA200500043 120050227A3350ML316 LAMP EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT BURNED OUT A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11840RP 145725 AIRSTAIRS EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED AIRSTAIRS EMERGENCY EXIT LIGHT IAW EMB 135 MM 33-50-10. OPS CHECK GOOD. 2L72 4F RTT00011AT 20050307000892005030700089SO 2005 3 7 CHQA200500042 120050225A33501317 LAMP EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11276SK 145348 LEFTHAND OVERWING EMERGENCY EXIT LIGHT IS INOP. REPLACED THE LEFTHAND OVERWING EMERGENCY EXIT LIGHT BULB IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050307000962005030700096NM 2005 3 7 252TR0035 120050222A5410 PANEL BOEING737 737228 13844AGNM LT NACELLE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05252TR 23001 LEFT ENGINE O/B COWL EXHAUST LOUVER PANEL CRACKED. WELDED PER BAC SPEC 5975. 2L72 4F RTA16WE 20050307001042005030700104EA 2005 3 7 QXEA200500255 120050215A5320 STRUCTURE CNDAIRCL600 CL6002C10 1390015EA ZONE 200 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - AFT FUSELAGE - AFT BAGGAGE BAY DOOR SURROUND STRUCTURE LOWER AFT COMBING STRUCTURE GOUGED. REPAIRED IAW CRJ700 SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050307001062005030700106EA 2005 3 7 QXEA200500254 120050210A1430 RIVET CNDAIRCL600 CL6002C10 1390015EA ZONE 800 SHEARED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - PASSENGER DOOR AFT NEWEL ATTACH POINT FOR PITT PIN HAS SHEARED RIVET AND BRACKET HAS BEEN BUMPED OUT OF POSITION. REPAIRED IAW CRJ700 SRM 51-42-13-001-001-A01 AND 51-42-06-001-001-A01. 2L72 4F RTA21EA 20050307001082005030700108EA 2005 3 7 QXEA200500253 120050213A5210 PANEL CNDAIRCL600 CL6002C10 1390015EA ZONE 800 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - PASSENGER DOOR TOP RISER PANEL CRACKED AT AFT BOTTOM CORNER. REPAIRED IAW REO 670-52-11-093, HORIZON AIR EA R-52-222 AND CRJ700 SRM 51-41-02-001-001-A01, 51-42-02-001-001-A01. 2L72 4F RTA21EA 20050307001092005030700109EA 2005 3 7 QXEA200500256 120050215A5340 STRUCTURE CNDAIRCL600 CL6002C10 1390015EA ZONE 200 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - AFT FUSELAGE - AFT BAGGAGE DOOR SURROUND STRUCTURE LOWER FORWARD COMBING STRUCTURE GOUGED. REPAIRED IAW CRJ700 SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050307001362005030700136NM 2005 3 7 DL764050103 120050210A2997BMS1360TYPE WIRE BOEING767 767432ER 1385134NM RT HYD PUMP BURNED A DALAK NONE O OTHER ININSP/MAINT 1 SO27838MH 29711 RIGHT ELECT HYD PUMP WIRING BURNED. REPLACED WIRE. 2L72 4F RTA1NM 20050307001422005030700142EA 2005 3 7 05051667 120050220A2170 COALESCER BAG CNDAIRCL600 CL6002B19 1900309EA AIR CON SYS CONTAMINATED A VTZAC ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 EA27667BR 7535 ABORTED TAKEOFF DUE TO LAV SMOKE MSG, 1ST FLIGHT OF THE DAY. SLIGHT SMELL FROM PACKS. MX FOUND COALESCER BAGS DIRTY. REPLACED COALESCER BAGS. 2L72 4F RTA21EA 20050307002162005030700216SO 2005 3 7 SWIA200514529 120050203A5210 ARM EMB 120 EMB120ER 3260203SO PAX DOOR BINDING A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07215SW 120281 MAIN CABIN DOOR EXTREMELY DIFFICULT TO OPEN AND CLOSE. INSTALLED NEW ROTATING ARMS IAW 52-10-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050307002172005030700217SO 2005 3 7 SWIA200514530 120050206A27513471001001 ANNUNCIATOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER N FALSE WARNING CRCRUISE 1 NM07584SW9731 9731 120352 REPEATED FLAP CONTROL FAULTS DURING FLIGHT. REMOVED AND REPLACED ANNUNCIATOR WITH SERVICEABLE UNIT IAW 27-50-10. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050307002182005030700218EA 2005 3 7 SWIA200514531 120050208A274170609 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07951SW 7795 STAB TRIM CHANNEL 2 INOPERATIVE. INSTALLED SERVICEABLE HSTCU IAW CRJ 200 MM 27-41-01, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050307002212005030700221NM 2005 3 7 SWAA050497 120050220A335065C27093 LIGHT BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29765SW 29805 FWD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2L72 4F RTA16WE 20050307002222005030700222NM 2005 3 7 CALA0500055 120050217A53207075T73511 INTERCOSTAL BOEING757 757224 1384958NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2757111 27301 INSPECTION FOUND MAIN CABIN INTERCOSTAL CORRODED BETWEEN BS 680 AND 700, RBL 56, WL 208. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02, PARA 4 AND 7. 2L72 4F RTA2NM 20050307002232005030700223NM 2005 3 7 CALA0500056 120050223A53206545783501 CHANNEL BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717309 23360 INSPECTION FOUND A 10 INCH CRACK IN STIFFENER CHANNEL IN FORWARD CARGO BAY AT VOR ANTENNA, STA 500 BETWEEN S28L AND S28R. THE CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-40-2. 2L72 4F RTA16WE 20050307002252005030700225EA 2005 3 7 QXEA200500276 120050215A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - RIGHTHAND INBOARD SEAT RAIL AT STATION X356 TO X349 HAS PITTING CORROSION ON TOP, INSIDE AND OUTER SURFACES. REPAIRED IAW CRJ700 SRM 51-41-02-001-001-A01, HORIZON AIR EA R-53-273, SECTION 1 AND REO 670-53-21-072. 2L72 4F RTA21EA 20050307002272005030700227EA 2005 3 7 QXEA200500278 120050215A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - RIGHTHAND INBOARD SEAT RAIL AT STATION X432 TO X437 HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW HORIZON AIR EA R-53-273, REO 670-53-21-072 AND CRJ700 SRM 51-41-02-001-001-A01. 2L72 4F RTA21EA 20050307002292005030700229EA 2005 3 7 05058650 120050227A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA LAVATORY MALFUNCTIONED A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27650BR 7418 EVENT SUMMARRY STATED LAV SMOKE INDICATION, NO SMOKE PRESENT, RAN QRH. REMOVED AND REPLACED LAV SMOKE DETECTOR. 2L72 4F RTA21EA 20050307002312005030700231NM 2005 3 7 DHL2005745003 120050226A3260 SWITCH BOEING727 727224 1384076NM NLG OUT OF ADJUST A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01745DH 20665 RED GEAR DOOR LIGHT ILLUMINATED AFTER GEAR RETRACTION AND GEAR HANDLE PLACED FROM UP TO OFF. FOUND NOSE GEAR SWITCHES OUT OF ADJUSTMENT. ADJUSTED SAME PER BMM 32-62-11, PERF ADJ/TEST OF DOOR WARNING SWITCHES PER BMM 32-62-11. OPS CHECKS NORMAL, WITH NO DEFECTS NOTED. 2L73 4F A3WE 20050307002682005030700268NM 2005 3 7 SWAA050660 120050303A552365C26485 SKIN BOEING737 7373H4 1384600NM ELEVATOR TAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29367SW 26578 DURING SCHEDULED 1/4D CHECK, FOUND RT ELEVATOR TAB CRACKED AT NR 1 HINGE CUTOUT. REMOVED AND REPLACED TAB PER MM. 2L72 4F RTA16WE 20050307002692005030700269NM 2005 3 7 SWAA050661 120050303A53206545409 WEB BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29367SW 26578 DURING SCHEDULED 1/4D CHECK, FOUND CRACK ON FUSELAGE BEADED WEB AT BS 664.5, RBL 38.5. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050307002702005030700270NM 2005 3 7 SWAA050662 120050303A5310573149 WINDOW POST BOEING737 7373H4 1384600NM COCKPIT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29367SW 26578 DURING SCHEDULED 1/4D CHECK, FOUND CRACK ON L1 UPPER WINDOW POST. REPAIRED L1 WINDOW POST PER SRM. 2L72 4F RTA16WE 20050307002732005030700273NM 2005 3 7 USAA050227 120050204A52106545871523 FRAME BOEING737 7373B7 1384580NM DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU50570 23706 PIT - FOUND FRAME CRACKED .125 INCH, BETWEEN 4TH DOOR STOP FORWARD SIDE. INSTALLED DOUBLER PER TYPICAL REPAIR 52-10-11. (M) 2L72 4F RTA16WE 20050307002742005030700274NM 2005 3 7 USAA050233 120050210A5320 WEB BOEING737 7373B7 1384580NM FUSELAGE TORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU50570 23706 PIT - FOUND WEB WITH .5 INCH SQUARE SECTION TORN OUT, BS 847 AT S24R. CUT OUT DAMAGE AND INSTALLED DOUBLER SPLICE AND NEW WEB PER SRM 51-70-13. (M) 2L72 4F RTA16WE 20050307002782005030700278NM 2005 3 7 USAA050226 120050211A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19519AU50516 23705 CLT - FOUND SKIN CRACKED TWO PLACES .750 INCH EACH, STATION 663 LBL 30. INSTALLED DOUBLER PER TR 53-60-04. (M) 2L72 4F RTA16WE 20050307002792005030700279NM 2005 3 7 USAA050236 120050209A5320 STRINGER SPLICE BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU50570 23706 PIT - FOUND STRINGER SPLICE CRACKED 1 INCH IN TWO LOCATIONS, BS 908 S4L AND S4R. REMOVED TWO SPLICES, MANUFACTURED NEW AND INSTALLED PER SRM 51-40-02 AND DWG NR 65-51698. (M) 2L72 4F RTA16WE 20050307002832005030700283NM 2005 3 7 USAA050230 120050207A5311 FRAME BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU50570 23706 PIT - FOUND FRAME CRACKED .75 INCH, FS 616 S17R. INSTALLED DOUBLER PER TYPICAL REPAIR 53-62-01. (M) 2L72 4F RTA16WE 20050307002842005030700284NM 2005 3 7 USAA050238 120050214A5320 BEAM BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19519AU 23705 CLT - FOUND BEAM CORRODED 3 INCHES, STATION 312 RBL 20. ACCOMPLISHED REPAIR PER SRM 53-10-51. (M) 2L72 4F RTA16WE 20050307002852005030700285NM 2005 3 7 USAA050237 120050209A5512 SKIN BOEING737 7374B7 1384702NM HORIZ STAB CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19780AU39018 24997 PIT - FOUND HORIZ STAB CRACKED 2 INCHES, HORIZ STAB LOWER SKIN REAR SPAR STAB STATION 138.7. INSTALLED DOUBLER PER TYPICAL REPAIR 55-10-07 REV B. (M) 2L72 4F RTA16WE 20050307002862005030700286NM 2005 3 7 USAA050229 120050203A5210507945178 DOOR FRAME BOEING737 7373B7 1384580NM ENTRY DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU50570 23706 PIT - FOUND FORWARD ENTRY DOOR CRACKED .3750, FRAME AND INNER WEB AT STOPS NR 5 AND NR 6 CUTOUTS. REMOVED DAMAGE, INSTALLED DOUBLER PER TYPICAL REPAIR 51-10-16. (M) 2L72 4F RTA16WE 20050307002872005030700287NM 2005 3 7 USAA050239 120050214A5311 FRAME BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19519AU50516 23705 CLT - FOUND FRAME CRACKED 1 INCH, STATION 616 WL 200 RIGHT SIDE. FABRICATED REPAIR ANGLE AND INSTALLED PER TR 53-62-01. (M) 2L72 4F RTA16WE 20050307002882005030700288NM 2005 3 7 USAA050228 120050204A52106545871523 DOOR FRAME BOEING737 7373B7 1384580NM DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU50570 23706 PIT - FOUND FRAME CRACKED .125 INCH, FRAME FORWARD SIDE NR 3 DOOR STOP CUTOUT. INSTALLED DOUBLER PER TYPICAL REPAIR 52-10-11. (M) 2L72 4F RTA16WE 20050307002902005030700290NM 2005 3 7 UIEA200500011 120050222A2824MA11A1194 ACTUATOR BOEING747 7472D7B 1384803NM NR 2 CROSSFEED FAILED A UIEAO OTHER J WARNING INDICATION CRCRUISE 1 EA15524MC 21784 DURING CRUISE, NR 2 CROSSFEED VALVE DOES NOT OPEN. TRANSITION BLUE LIGHT STAYS ON. REMOVED AND REPLACED NR 2 CROSSFEED VALVE ACTUATOR IAW MM 28-22-02. OPS CHECK SATISFACTORILY S/N OFF 90060. (M) 2L74 4F RTA20WE 20050307002912005030700291EU 2005 3 7 2005F00019 120050129A2120 ODOR AEROSPATR72 ATR72 EU CABIN DETECTED A TRBAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO29410AT 410 ON APPROACH TO STT AN ELECTRICAL BURNING SMELL WAS FELT ON THE AFT CABIN AREA. EMERGENCY LANDING WAS DECLARED. NO FIRE EXTINGUISHER WAS USED. OPERATIONAL CHECK OF THE AIR CONDITIONING UNITS AND LIGHTING SYSTEMS WERE CONDUCTED AND FOUND NO BURNING SMELL. (M) 2H72 4T RT 20050307002922005030700292EU 2005 3 7 2005F00020 120050203A2910USP1514J4S FITTING AEROSPATR72 ATR72212 8680945EU LT MLG CRACKED A TRBAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SO29342AT 345 DURING GEAR RETRACTION, GREEN PUMP LOW PRESSURE AND LOW LEVEL LIGHTS ILLUMINATED. USED EMERGENCY GEAR EXTENSION SYSTEM. REPLACED SWIVEL FITTING AT LEFT GEAR ASSEMBLY. (M) 2H72 4T RTA53EU 20050307002942005030700294NE 2005 3 7 2005F00018 220050127A7200 ENGINE AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE RIGHT FIRE A TRBAEFA ENGINE SHUTDOWN ACTIVATE FIRE EXT. UNSCHED LANDING RA PARTIAL RPM/PWR LOSS FLAME/FIRE TOTAKEOFF 1 SO29408AT 408 127051 ON CLIMB, RIGHT ENGINE CAUGHT ON FIRE. ENGINE WAS SHUT DOWN AND RETURNED TO THE AIRPORT. REPLACED ENGINE FOR EVALUATION. (M) 2H72 4T4 TRTA53EU E20NE 20050307002952005030700295EU 2005 3 7 2005F00022 120050124A33503012000 POWER SUPPLY AEROSPATR72 ATR72212 8680945EU CABIN DISCHARGED A TRBAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO21420AT 420 DURING TAXI, THE EMERGENCY LIGHTS STAY ON ALL TIME. AIRCRAFT RETURNED TO BLOCKS. REPLACED POWER SUPPLY UNIT. (M) 2H72 4T RTA53EU 20050307003052005030700305NM 2005 3 7 GAIA05005OP 120050215A27821U1110 ACTUATOR BOEING727 727223 1384074NM L/E FLAP LEAKING A GAIAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION TOTAKEOFF 1 SW07858AA 21085 FLT 544 - FWA-DTW - DURING TAKEOFF THE 'A' SYSTEM HYDRAULIC FLUID QUANTITY DECREASED AND BOTH A-PUMP LOW PRESSURE LIGHTS ILLUMINATED. THE AIRCRAFT RETURNED TO FWA AND AN UNEVENTFUL LANDING WAS MADE. REMOVED AND REPLACED NR 2 LEADING EDGE FLAP ACTUATOR AND NR 1 AND NR 2 A-SYSTEM HYDRAULIC PUMPS. OPS CHECK AND LEAK CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20050307003072005030700307EA 2005 3 7 ASOA05060 120050122A3350211RJ76A001 STRIP CNDAIRCL600 CL6002C10 1390015EA CABIN DAMAGED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27705EV 10051 DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY FLOOR LIGHT STRIP AFT OF SEAT 12C WAS FOUND MISSING ONE RED ARROW. MAINTENANCE INSTALLED AN EMERGENCY FLOOR LIGHT STRIP AFT OF SEAT 12C. (M) 2L72 4F RTA21EA 20050307003092005030700309EA 2005 3 7 A6WA200540056 120050215A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 GL31421ZW 7346 FOUND FS 484 LBL 27 ANGLE CRACKED APPROX .30 IN RADIUS. (M) 2L72 4F RTA21EA 20050303000762005030300076NM 2005 3 3 P5CA0501320 120050208A7603 CLAMP BOEING747 747230B 1384889NM THROTTLE LOOSE A P5CAK NONE O OTHER ININSP/MAINT 1 EA15509MC 21221 ON PREFLIGHT, NR 4 THROTTLE WOULDN’T ADVANCE FORWARD. T/S FOUND SHIELD SUPPORT BRACKET CLAMPS LOOSE AT PUSH PULL CABLE. SECURED PUSH PULL SHIELD SUPPORT BRACKET CLAMPS PER MM 76-11-05. OPS CHECK OK. 2L74 4F A20WE 20050303000772005030300077WP 2005 3 3 NACA20050004 120050212A1420 CONTACT DOUG DC6 DC6A 3021706WP ELEC CONNECTOR DIRTY A NACAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 AL036174C 44075 TAKEOFF WARNING HORN DURING TAKEOFF ROLL. CLEANED CONTACTS ON FLAP INDICATOR ELECTRICAL CONNECTOR. OP CHECKED GOOD. 2L74 4R 6A3 20050303000862005030300086EA 2005 3 3 050546232 120050223A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27623BR 7192 INTERCOSTAL CRACKED AT .250 INCH IN LENGTH ON LT INBOARD SIDE AT FS 484 LEFT BETWEEN BL 27.00 AND 36.00. 2L72 4F RTA21EA 20050303000872005030300087NM 2005 3 3 CALA0500059 120050223A5730114N210715 SKIN BOEING757 757224 1384958NM LT WING DELAMINATED A CALAK NONE O OTHER ININSP/MAINT 1 SW2757111 27301 INSPECTION FOUND THE LT WING O/B FIXED LEADING EDGE SKIN TOP SURFACE DELAMINATED AT WS 380. REPAIRED IAW SRM 51-40-02, 51-70-07, 51-70-17 AND EA 5731-01010. 2L72 4F RTA2NM 20050303000912005030300091EU 2005 3 3 0500223269 120050217A5320 SILL AIRBUS320 A320212 3930322EU FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01369NW 1011 DURING H-CHECK FOUND CORROSION ON AFT RT AND LT DOOR SILLS. REPAIRED PER EA 32-202563. 2L72 4F RTA28NM 20050303001302005030300130WP 2005 3 3 AALA20050120 120050217A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21475AA 49650 DFW - AFT STAIR CENTER EMERGENCY LIGHT ASSEMBLY IS BROKEN OUT OF RIVETS AND CEILING IS HANGING. SECURED EMERGENCY LIGHT ASSEMBLY AND CEILING AT AFT STAIR CENTER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050303001322005030300132WP 2005 3 3 AALA20050125 120050218A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21478AA 49653 OVERHEAD EMERGENCY LIGHT AT ROWS 13 TO 15 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHT AT ROWS 13 TO 15. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050303001402005030300140EU 2005 3 3 MALA050184 120050215A33506104789 BATTERY PACK SAAB SF340 340B 7860101EU EMERGENCY LIGHT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15369PX 340B295 BATTERY PACK P/N 61-0478-9, S/N 2214 FAILED SCHEDULED CAPACITY CHECK. REPLACED BATTERY ASSEMBLY P/N 55-2198-1. UNIT PASSES CMM CHECKS, RTS 2/18/05. 2L72 4T RTA52EU 20050307000442005030700044EA 2005 3 7 QXEA200500246 120050210A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - FUSELAGE INTERIOR, STATION 280 BULKHEAD LOWER WEB, LEFTHAND IS CORRODED. REPAIRED IAW CRJ700 REO 670-53-11-052, REV A. 2L72 4F RTA21EA 20050307000462005030700046EA 2005 3 7 QXEA200500238 120050205A5230 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 800 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - FORWARD BAGGAGE DOOR INTERIOR STRUCTURE HAS CHAFE MARKS AT TWO LOCATIONS FROM INTERIOR PANEL. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01. 2L72 4F RTA21EA 20050307000482005030700048EA 2005 3 7 QXEA200500239 120050211A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - FUSELAGE EXTERIOR, FUSELAGE SKIN AT STATION 354 AND STRINGER 23R HAS SCRATCHES ON SKIN BELOW WATER SERVICE DOOR. REPAIRED IAW CRJ700 SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01 AND 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050307000502005030700050NM 2005 3 7 AWXA200500282 120050127A5320651768470 WEB BOEING737 737301 1384611NM FUSLEAGE CHAFED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK FOUND L-1 DOOR UPPER HINGE CUTOUT UPPER WEB CHAFED ON LOWER SIDE BETWEEN BS 294.5 AND BS 303.9, STR 13 LT. MAINTENANCE REMOVED CHAFED WEB AT L-1 DOOR UPPER HINGE CUTOUT FROM BS 294.5 TO BS 303.9, STR 13 LT; FABRICATED A NEW REPLACEMENT WEB PER DWG 65-17684; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050307000522005030700052NM 2005 3 7 AWXA200500284 120050220A5315D53472090010 FLOORBEAM AIRBUSA319 A319132 3930340NM FUSLEAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28812AW 1178 SAL - MAJOR REPAIR - DURING BC-4 CHECK FOUND EXFOLIATION CORROSION ON FLOORBEAM Y1292 AT FR 66+3 INCHES. MAINTENANCE REMOVED CORRODED SECTION OF FLOORBEAM Y1292 FROM FR 66+3 INCHES TO FR 64; FABRICATED A NEW REPLACEMENT SECTION OF FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050307000542005030700054NM 2005 3 7 AALA20050150 120050207A5320141N516OU46 FLOOR SUPPORT BOEING757 757223 1384957NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21653A 24611 TUL - FLOOR CHANNEL SUPPORT CORRODED AT RT RIB LINE NUMBER 38 AT STATION 316 TO 324 IN AN AREA OF 1 INCH BY 3 INCHES. DRILLED UP NEW INTERCOSTAL, DEBURRED, TREATED, PRIMED AND PAINTED AND INSTALLED. 2L72 4F RTA2NM 20050307000562005030700056NM 2005 3 7 252TR0036 120050222A3397 WIRE BOEING737 737228 13844AGNM EMERGENCY LIGHT BROKEN A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05252TR 23001 BOTH EMERGENCY EXIT LIGHTS IN G-2 GALLEY AREA AT FORWARD ENTRY DOOR AISLE INOP. REPAIRED BROKEN WIRES UNDER GALLEY PER SWPM 20-00. OPS CHECKS OK. 2L72 4F RTA16WE 20050307000582005030700058SO 2005 3 7 CHQA200500045 120050228A5610163500111 WINDSCREEN EMB 145 EMB145LR 3260212SO COCKPIT MELTED A CHQAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 GL11370SK1212 1212 145515 FLIGHT 3408 RDU-LGA - DURING DESCENT INTO LGA IN LIGHT ICING CONDITIONS WITH ENGINE ANTI-ICE AND WINDSHIELD HEAT ON THERE WAS A BURNING ELECTRICAL SMELL. WHITE SMOKE WAS SEEN COMING FROM UNDER THE LEFT WINDSHIELD GLARESHIELD. THE WINDSHIELD HEAT WAS TURNED OFF AND THE SMOKE STOPPED. AN EMERGENCY WAS DELCARED AND THE AIRCRAFT LANDED NORMALLY. THE SMOKE NEVER RETURNED WITH THE WINDSHIELD HEAT OFF. MAINTENANCE FOUND THE WINDSHIELD HEAT POWER WIRE MELTED TO THE PLASTIC BLOCK ON THE WINDSHIELD. REMOVED AND REPLACED CAPTAIN'S WINDSHIELD. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050307000602005030700060NM 2005 3 7 SWAA050643 120050302A3350079123 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29731SA 27863 EEPLS COVER LOOSE AT ROW 6L. SECURED EEPLS COVER PER MM. 2L72 4F RTA16WE 20050307000622005030700062 2005 3 7 SWAA050645 420050302A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29370SW 26597 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR SLIDE PER MM. 2L72 4F RTA16WE 20050307000642005030700064NM 2005 3 7 SWAA050647 120050302A531169353656 FRAME BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE BELT FRAME CRACKED AT BS 360, STR 14R. REPAIRED BELT FRAME PER SRM. 2L72 4F RTA16WE 20050307001442005030700144SO 2005 3 7 RAIA00502027 120050219A361014531128402 DUCT EMB 145 EMB145 3260210SO ANTI ICE SYSTEM CRACKED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03801HK 145053 RIC - RIGHT ENGINE ANTI-ICE FAIL INDICATION. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE HIGH STAGE BLEED DUCT. 2L72 4F RTT00011AT 20050307001462005030700146EU 2005 3 7 MALA050182 120050214A33506104981 BATTERY PACK SAAB SF340 SF340A 7850100EU EMERGENCY LIGHT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL1527XJ 340A027 BATTERY PACK P/N 61-0498-1, S/N 9804442. FAILED SCHEDULED CAPACITY CHECK. DEEP CYCLED. UNIT PASSES CMM CHECKS, RTS 2/16/05. 2L72 4T RTA52EU 20050307001482005030700148EU 2005 3 7 MALA050192 120050206A33506122751 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU EMERGENCY LIGHT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15536XJ E2372 BATTERY PACK P/N 61-2275-1, S/N 9805512. FAILED SCHEDULED CAPACITY CHECK. REPLACED BATTERY ASSEMBLY P/N 61-2274-1. UNIT PASSES CMM CHECKS, RTS 2/8/05. 2H74 4F RTA49EU 20050307001502005030700150NM 2005 3 7 375PA0038 120050221A5320 SUPPORT ANGLE BOEING737 73739A 138447PNM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05375PA 23812 SUPPORT ANGLE CRACKED AT BS 767 ABOVE STR 28 LT. REPLACED ATTACH ANGLE PER SRM 51-40-01. 2L72 4F RTA16WE 20050307001522005030700152WP 2005 3 7 ABXA050033 120050121A532099220422 FLOOR SUPPORT DOUG DC9 DC933F 302207AWP CARGO BAY CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23935AX 47413 CABIN FLOOR SUPPORT BRACE FITTING CRACKED FS 775, LONGERON 23 RIGHT. REMOVED AND REPLACED SUPPORT STRUT IAW DC-9 SRM 51-30-5 AND 51-30-2. 2L72 4F A6WE 20050307001542005030700154WP 2005 3 7 ABXA050035 120050222A335060030451 BATTERY DOUG DC9 DC933F 302207AWP EMERGENCY LIGHT DISCHARGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23932AX768 47465 EMERGENCY EXIT LIGHT WOULD NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES IAW DC-9 AMM 33-53-00. OPS CHECKED GOOD. 2L72 4F A6WE 20050307001562005030700156WP 2005 3 7 ABXA050031 120050119A53129911500183 BULKHEAD DOUG DC9 DC933F 302207AWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23935AX 47413 WEB WAS CRACKED BETWEEN LEFT UPPER RADOME GUIDE PIN AND RIVET. REPAIRED CRACKED WEB IAW DC-9 SRM 53-01. 2L72 4F A6WE 20050307001622005030700162NM 2005 3 7 AWXA200500245 120050222A3350321454 EPSU AIRBUSA319 A319132 3930340NM ZONE 221 INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28802AW405112685 924 LAS - EEL - DURING 4-DAY CHECK FUNCTIONAL TEST OF EMERGENCY LIGHT SYSTEM, THE FORWARD LT EMERGENCY POWER SUPPLY UNIT HAD AN INTERNAL FAULT. MAINTENANCE REMOVED AND REPLACED LT EMERGENCY POWER SUPPLY UNIT (10WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050307001642005030700164NM 2005 3 7 AWXA200500247 120050125A5320655572635 CHANNEL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 MCN - MAJOR REPAIR - DURING C-16 CHECK A .3125 INCH CRACK WAS FOUND IN ATTACH ANGLE FOR LINER ATTACH STRAP AT BS 727, STR 21 LT. MAINTENANCE REMOVED CRACK IN ATTACH ANGLE AT BS 727, STR 21 LT; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 65-55726; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 12. 2L72 4F RTA16WE 20050307001662005030700166NM 2005 3 7 AWXA200500249 120050124A53206545834524 INTERCOSTAL BOEING737 737301 1384611NM FUSLEAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK A .1875 INCH CRACK WAS FOUND IN UPPER RADIUS OF INTERCOSTAL AT BS 306, LBL 27. MAINTENANCE CUT OUT DAMAGE IN UPPER RADIUS OF INTERCOSTAL AT BS 306, LBL 27; FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-11. 2L72 4F RTA16WE 20050307001672005030700167EA 2005 3 7 QXEA200500300 120050227A2120 ODOR CNDAIRCL600 CL6002C10 1390015EA CABIN DETECTED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 NM09604QX 10019 THE CREW REPORTS THAT ON DESCENT, THE A/C SMELLS VERY BAD, LIKE A GYM SOCK. MAINTENANCE INSPECTED THE ACM COMPARTMENT, THE ACM AND ALL ASSOCIATED DUCTING WITH NO DEFECTS NOTED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20050307001692005030700169EU 2005 3 7 RAIA00502028 120050219A7714 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU RPM SENSOR DIRTY A RAIAD RETURN TO BLOCK YJ ENGINE STOPPAGE WARNING INDICATION TXTAXI/GRND HDL 1 CE03568HK 41086 LT ENGINE QUIT AFTER START-UP. MAINTENANCE CLEANED RPM SENSOR CONNECTOR AND OPS CHECKED GOOD. 2L72 4T RTA41NM 20050307001712005030700171NM 2005 3 7 05FDEA00315 120050222A5320 STRAP BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25496FE 21670 DAMAGE HOLE ON BS 1183 STRAP RBL 19.22 WL 273.25. REMOVED AND REPLACED STRAP PER SRM 51-30-2 AND SRM 51-30-5. 2L73 4F RTA3WE 20050307001722005030700172EA 2005 3 7 COMA0560137 120050219A3220 TORQUE LINK CNDAIRCL600 CL6002B19 1900309EA NLG DISCONNECTED A COMAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 SO01932CA 7038 FLIGHT 4955 GEAR DISAGREE WARNING, WOW OUTPUT FAIL, VIOLENT NOSE WHEEL SHIMMEY DURING LANDING. FOUND NLG TORQUE LINKS DISCONNECTED. RECONNECTED TORQUE LINKS. 2L72 4F RTA21EA 20050307001732005030700173 2005 3 7 05FDEA00246 420050205A2561 LIFE VEST DOUG DC10 DC1030F 3023504WP ZONE 200 BROKEN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25304FE 46992 BOTH COURIER SEATS LIFE VEST POUCH RETAINING STRAPS MISSING/BROKEN. ACCOMPLISHED FEDEX EA 8-2560-83856, EQUIPMENT/FURNISHING- COURIER SEAT LIFE VEST POUCH RETAINING STRAP-REPAIR. 2L73 4F RTA22WE 20050307001742005030700174WP 2005 3 7 05FDEA00247 120050205A5753ARC19842 HINGE DOUG DC10 DC1030F 3023504WP ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25304FE 46992 RIGHT WING OUTBOARD FLAP OUTBOARD SUPPORT, PIVOT ATTACH POINT INBOARD BORE CORRODED. REMOVED CORROSION, FABRICATED, INSTALLED AND HONED BUSHING TO FINAL DIAMETER OF .8745 - .8755 INCHES IAW DAC CMM 57-52-02, PRIMED BORE IAW DC10-30 SRM 51-21-01 VOL II, AND FEDEX EA 8-5710- 83966, WINGS- RIGHT HAND OUTBOARD FLAP, OUTBOARD HINGE BRACKET OVERSIZE PIVOT BORE -REPAIR. 2L73 4F RTA22WE 20050307002712005030700271EA 2005 3 7 050616396 120050302A5320601R35031239 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27639BR 7313 RIGHT FS 621 FLOOR SUPPORT IS CRACKED AT 1 INCH IN PREVIOUS REPAIR ANGLE. 2L72 4F RTA21EA 20050307002762005030700276NM 2005 3 7 USAA050224 120050207A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19390US54156 23312 CLT - FOUND SKIN CRACKED 1 INCH, AFT LEFT SERVICE DOOR CUTOUT LOWER HINGE AREA. INSTALLED DOUBLER PER TR 53-60-10. (M) 2L72 4F RTA16WE 20050307002812005030700281NM 2005 3 7 USAA050232 120050210A5311 FRAME BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU50570 23706 PIT - FOUND FRAME CRACKED .25, BS 440 BETWEEN S8R AND S9R. CUT OUT DAMAGE AND INSTALLED REPAIR ANGLES PER TYPICAL REPAIR 53-10-20A. (M) 2L72 4F RTA16WE 20050307002822005030700282NM 2005 3 7 USAA050231 120050209A5311 FRAME BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU50570 23706 PIT - FOUND FRAME CRACKED .25 INCH, FS 887 S-9R. DOUBLER REPAIR INSTALLED PER 53-10-20A. (M) 2L72 4F RTA16WE 20050307002932005030700293EU 2005 3 7 2005F00021 120050113A3260DHE1148 PROXIMITY SWITCH AEROSPATR72 ATR72212 8680945EU NLG FAULTY A TRBAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO214AE 244 ON TAKEOFF, WHEN GEAR SELECTED TO THE UP POSITION, ALL UPLOCK INDICATION ON NR 1 AND NR 2 PANELS AND THE GREEN HYD PUMP PRESSURE FLUCTUATES BETWEEN 1500 PSI TO 3000 PSI. ALSO, HEARD A HARD NOISE. AIRCRAFT RETURNED TO AIRPORT. REPLACED BOTH PROXIMITY SWITCHES AT THE NOSE GEAR. (M) 2H72 4T RTA53EU 20050307003082005030700308EA 2005 3 7 ASOA05059 120050122A3350487190 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA CABIN DAMAGED A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27826AS 7210 DURING OVERNIGHT MAINTENANCE IN SHV, THE FORWARD EMERGENCY FLOOR LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE FOUND AND REPAIRED A LOOSE CONNECTION TO THE FORWARD EMERGENCY FLOOR LIGHT STRIP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050307000402005030700040EA 2005 3 7 QXEA200500248 120050211A5321 FLOORBOARD CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - FUSELAGE INTERIOR, COCKPIT FLOORBOARD SUPPORT ANGLE AT STATION 280 IS CORRODED. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20050307000412005030700041EA 2005 3 7 QXEA200500247 120050210A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - FUSELAGE INTERIOR, FUSELAGE STATION 280 BULKHEAD, RIGHTHAND LOWER WEB IS CORRODED. REPAIRED IAW CRJ700 REO 670-53-11-052, REV A. 2L72 4F RTA21EA 20050307000422005030700042EA 2005 3 7 QXEA200500243 120050206A1430 NUT CNDAIRCL600 CL6002C10 1390015EA ZONE 300 BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - AFT RAD ALT ANTENNA AT STATION 1102, STRINGER 26L TO 27L HAS A BROKEN A- NUT AT AFT LEFT CORNER. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20050307000722005030700072EA 2005 3 7 MASA200500098 120050210A33102LA00695307 PANEL CNDAIRCL600 CL6002D24 1390016EA FLOOD LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07908FJ 15008 SAT - LAS, F/O'S FLOOD LIGHT TRIPS CIRCUIT BREAKER. PLACED FLOOD LIGHT ON MEL. 2/11/05 MAINTENANCE REPLACED F/A FLOOD LIGHT PANEL, OPS CHECK GOOD. 2L72 4F RTA21EA 20050307000732005030700073EA 2005 3 7 MASA200500131 120050218A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0717337 7337 PHX TO AUS, LT EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED THE LIGHT, OPS CHECK GOOD. 2L72 4F RTA21EA 20050307000742005030700074EA 2005 3 7 MASA200500133 120050219A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BROKEN A MASAK NONE O OTHER ININSP/MAINT 1 SW07650ML 7137 PHL - REPORTED A SECTION OF THE FLOOR PATH LIGHTING INOP. MAINTENANCE REPAIRED A BROKEN WIRE. OPS CHECK GOOD. 2L72 4F RTA21EA 20050307000762005030700076SO 2005 3 7 MASA200500137 120050220A335020131A BATTERY PACK EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07835MJ 145353 EMERGENCY FLOOR PATH LIGHTING STRIPS INOP. MAINTENANCE REPLACED THE NR 3 EMERGENCY LIGHTING BATTERY PACK. 2L72 4T RTT00011AT 20050307001112005030700111NM 2005 3 7 SWAA050629 120050301A21307110025 CONTROL PANEL BOEING737 7373H4 1384600NM CABIN PRESSURE FAULTY A SWAAO OTHER O OTHER DEDESCENT 1 SW29310SW 22949 DECENDING THROUGH 7000 FT, OUTFLOW VALVE WENT TO FULL OPEN & CABIN DIFF PRESSURE INDICATED ZERO. REMOVED AND REPLACED CABIN PRESSURE CONTROL PANEL PER MM. 2L72 4F RTA16WE 20050307001132005030700113NM 2005 3 7 SWAA050631 120050301A3350101114 LENS BOEING737 7375H4 138449DNM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29528SW 26570 LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED EMERGENCY LIGHT LENS PER MM. 2L72 4F RTA16WE 20050307001152005030700115 2005 3 7 SWAA050633 420050301A25656551463 BRACKET BOEING737 7377H4 1384404NM L1 DOOR GIRT BARLOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29713SW 27847 L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET LOOSE. SECURED BRACKET PER MM. 2L72 4F RTA16WE 20050307001172005030700117NM 2005 3 7 AWXA200500286 120050127A534069265552 STRINGER CLIP BOEING737 737301 1384611NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK A .3125 INCH CRACK WAS FOUND IN INBOARD FORWARD LOWER EDGE OF STRINGER SPLICE CHANNEL CLIP & FRAME STRAP AT BS 349, STR 16 LT. MAINTENANCE REMOVED CRACKED STRINGER SPLICE CHANNEL CLIP & FRAME STRAP AT BS 349, STR 16 LT; FABRICATED NEW REPLACEMENT CLIP & STRAP; INSTALLED REPAIR PARTS IAW ER 03-5300-05053-SS3. 2L72 4F RTA16WE 20050307001212005030700121NM 2005 3 7 QXEA200500299 120050225A2140 FILTER BOMBDRDHC8 DHC8401 1390041NM ZONE 100 FAILED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09411QX7897 4055 SEA - FLIGHT 2316 - THE FLIGHT RETURNED TO FIELD, UNABLE TO GET HEAT FROM EITHER THE CABIN OR COCKPIT PACKS. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE PACK FLOW CONTROL AND SHUTOFF VALVE FILTER. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050307001232005030700123EA 2005 3 7 QXEA200500259 120050211A5753 VANE CNDAIRCL600 CL6002C10 1390015EA ZONE 500 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - LEFTHAND INBOARD FLAP VANE INBOARD LEADING EDGE PANEL HAS CHAFE MARK. REPAIRED IAW CRJ700 SRM 51-25-06-001-001-A01 AND SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050307001252005030700125NM 2005 3 7 SWAA050634 120050301A552065C25763 HINGE FITTING BOEING737 7373H4 1384600NM RT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED C4 CHECK, FOUND EXCESSIVE PLAY ON RT ELEVATOR OUTBOARD HINGE FITTING. REPAIRED HINGE FITTING PER SWA EA. 2L72 4F RTA16WE 20050307001272005030700127NM 2005 3 7 SWAA050636 120050301A521065C36231 SKIN BOEING737 7373H4 1384600NM L1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29626SW 27702 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR SKIN CRACKED AT UPPER AFT CORNER. REPAIRED L1 DOOR SKIN PER SRM. 2L72 4F RTA16WE 20050307001292005030700129NM 2005 3 7 SWAA050638 120050301A534065C27314 STRINGER CLIP BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP AT BS 727D, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20050307001312005030700131NM 2005 3 7 SWAA050640 120050301A5313BAC1498 STRINGER BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER AT BS 360, STR 14L. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20050307001332005030700133NM 2005 3 7 SWAA050642 120050301A57556573730 SKIN BOEING737 7373Q8 1384670NM RT WING SPOILER DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND RT WING T/E NR 6 SPOILER LWR SURFACE DELAMINATED. REMOVED AND REPLACED NR 6 SPOILER ASSY PER MM. 2L72 4F RTA16WE 20050307001382005030700138NE 2005 3 7 DXTA200500595 220050215A7200 ENGINE GULSTM200 200 4500308NM PWA 306 PW306B NE RIGHT FAILED E DXTAEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 GL07703QS 060 PCECC0116 RIGHT ENGINE FAILED ON CLIMBOUT ABOUT 3 MINS AFTER TAKEOFF. FOUND ENGINE HAD INTERNAL FAILURE. REMOVED AND REPLACED RT ENGINE, LEAK CHECKED AND OPS CHECKED GOOD PER G200 MM 71-00-00. 2L72 4F4 FRTA53NM E35NE 20050307001402005030700140CE 2005 3 7 DXTA200500609 120050224A2910 B-NUT CESSNA750 750 2076810CE HYD SYSTEM LEAKING E DXTAO OTHER KE FLUID LOSS VIBRATION/BUFFET DEDESCENT 1 GL07935QS 7500135 ON DESCENT EGE NOSE GEAR BUMP (BUMP IN THE NIGHT) LOUD NOISE AND FELT IT IN THE FLOOR. FOUND A-SIDE HYDRAULICS AT 43 PERCENT AND A LOOSE B-NUT ON NLG ACTUATOR. JACKED AIRCRAFT TIGHTENED B-NUT, SERVICED HYDRAULICS WITH SKYDROL C/W GEAR SWINGS (15X), NO FAULTS FOUND DOWNJACKED AIRCRAFT, NO LEAKS NOTED IAW CE750 MM CHAPT 29-00-00. 2L72 4J RTT00007WI 20050307001432005030700143 2005 3 7 05052696 420050221A341845150340 SENSOR CNDAIRCL600 CL6002B19 1900309EA AOA VANE FAILED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27696BR 7779 STALL FAIL MESSAGE ON CLIMB. MX REMOVED AND REPLACED LT AOA VANE DUE TO HIGHER DEFLECTION THAN RT VANE. 2L72 4F RTA21EA 20050307001472005030700147EU 2005 3 7 MALA050190 120050214A33506122751 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU EMERGENCY LIGHT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15522XJ E2347 BATTERY PACK P/N 61-2275-1, S/N 9811820. FAILED SCHEDULED CAPACITY CHECK. REPLACED BATTERY ASSEMBLY P/N 61-2274-1. UNIT PASSES CMM TESTS, RTS 2/16/05. 2H74 4F RTA49EU 20050307001582005030700158NE 2005 3 7 ABXA050030 220050217A726180903601 TUBE DOUG DC9 DC931 3022065WP PWA JT8 JT8D7B 52053NE ENGINE OIL BROKEN A ABXAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL23937AX 47074 655336 NR 1 ENGINE FLAME-OUT DURING CLIMB AT 7,000 FT. OIL PRESSURE STAYED ABOVE 10 PSI FOR APPROXIMATELY 20 MINUTES DURING WINDMILLING AFTER FLAME-OUT. AIR TURNBACK TO ILN. ACCOMPLISHED TROUBLESHOOTING PER P&W MM FOR FLAME-OUT, INSPECTED INLET AND EXHAUST AREAS. FOUND PS4 LINE BROKEN AT AFT END OF LINE (MUSCLE AIR TO NR 1 ENGINE FUEL CONTROL). REMOVED AND REPLACED PS4 LINE IAW DC-9 MM 72-00-00. P/N 809036-01. OPS CHECKED GOOD ON ENGINE RUN. 2L72 4F4 F A6WE E2EA 20050307001602005030700160NM 2005 3 7 P5CA0501323 120050220A32401604010011 LIMITER BOEING747 74746NF 13848BTNM BRAKE TORQUE FAILED A P5CAO OTHER J WARNING INDICATION CLCLIMB 1 EA15454PA 30812 BRAKE LIMITER EICAS MESSAGE ON CLIMBOUT. REPLACED BRAKE TORQUE LIMITER POSITION NR 5 PER MM 32-42-20. CMC TEST SATISFACTORY. 2L74 4F RTA20WE 20050307001782005030700178NM 2005 3 7 375PA0043 120050221A5230 DOOR FRAME BOEING737 73739A 138447PNM CARGO DOOR CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05375PA 23812 AFT CARGO DOOR AFT FRAME CRACKED APPROX 16 INCHES ABOVE LOWER AFT CORNER. REPLACED FRAME PER SRM 51-40-05, 51-40-08, AND 51-10-01. 2L72 4F RTA16WE 20050307001792005030700179EA 2005 3 7 05055628 120050224A2497 CONTACTOR CNDAIRCL600 CL6002B19 1900309EA FAILED A VTZAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 EA27628BR 7240 EVENT SUMMARY STATED 628BR RTF DUE TO ELECTRICAL FAILURE. REMOVED AND REPLACED ESS BUSS CONTACTOR & ADG AUTO DEPLOY CONTROL. 2L72 4F RTA21EA 20050307001802005030700180NM 2005 3 7 SWAA050516 120050222A335007912 COVER BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29638SW 27711 EEPLS FLOOR STRIP LOOSE AT ROW 9L. RESECURED EEPLS FLOOR STRIP PER MM. 2L72 4F RTA16WE 20050307001812005030700181NM 2005 3 7 SWAA050517 120050222A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29424WN 29828 EEPLS FLOOR STRIP INOP AT ROW 1L TO 9L. REMOVED AND REPLACED EEPLS FLOOR STRIP PER MM. 2L72 4F RTA16WE 20050307001822005030700182NM 2005 3 7 SWAA050518 120050222A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29475WN 32474 DURING SCHEDULED RON CHECK, FOUND EEPLS FLOOR TRACK INOP AT ROW 1. REMOVED AND REPLACED EEPLS FLOOR TRACK COVER PER MM. 2L72 4F RTA16WE 20050307001832005030700183 2005 3 7 SWAA050519 420050222A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29743SW 29279 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR SLIDE PER MM. 2L72 4F RTA16WE 20050307002242005030700224EA 2005 3 7 QXEA200500275 120050213A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - LEFTHAND OUTBOARD SEAT RAIL AT STATION X490 TO X505 HAS PITTING CORROSION ON MOST INBOARD SURFACE. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01, 51-21-11-001-001-A01, HORIZON AIR EA R-53-272 AND REO 670-53-31-025. 2L72 4F RTA21EA 20050307002262005030700226EA 2005 3 7 QXEA200500277 120050215A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - RIGHTHAND INBOARD SEAT RAIL AT STATION X372 TO X399 HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW CRJ700 SRM 51-41-02-001-001-A01, HORIZON AIR EA R-53-273, SECTION I AND REO 670-53-21-072. 2L72 4F RTA21EA 20050307002282005030700228EA 2005 3 7 QXEA200500279 120050215A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - RIGHTHAND INBOARD SEAT RAIL AT STATION X447 HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW HORIZON AIR EA R-53-273 AND REO 670-53-21-072 REV N/C. 2L72 4F RTA21EA 20050307002302005030700230EA 2005 3 7 05056632 120050225A3250 STEERING SYS CNDAIRCL600 CL6002B19 1900309EA NLG OUT OF RIG A VTZAO OTHER J WARNING INDICATION APAPPROACH 1 EA27632BR 7268 EVENT SUMMARY STATED NWS FAILURE. RIGGED LT FEEDBACK RVDT. OPS CHECK GOOD. 2L72 4F RTA21EA 20050307002322005030700232NM 2005 3 7 AWXA200500302 120050126A33501012621 LIGHT BOEING737 737301 1384611NM L2 DOOR INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28326AW 23258 MCN - EEL - DURING C-18 CHECK FOUND THE L-2 DOOR EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED L-2 DOOR EMERGENCY EXIT SIGN, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050307002332005030700233NM 2005 3 7 AWXA200500303 120050210A53116546541504 FRAME BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK 3 EACH .25 INCH CRACKS WERE FOUND IN FUSELAGE FRAME AT BS 663.75, BETWEEN STR 2 RT & STR 3 LT. MAINTENANCE CUT OUT CRACKS IN FRAME AT BS 663.75, BETWEEN STR 2 RT & STR 3 LT; FABRICATED FILLERS AND A REPAIR ANGLE; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-07. 2L72 4F RTA16WE 20050307002342005030700234NM 2005 3 7 AWXA200500304 120050303A291065448917 MODULE BOEING737 7373Y0 1384671NM ZONE 211 FAULTY A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28323AW5236020383 23684 AFTER DEPARTURE AT APPROXIMATELY 1,000 FT A-SYSTEM HYDRAULICS AND FEEL DIFFERENTIAL LIGHT ILLUMINATED, TURNED BACK TO PHX, FLIGHT CONTROLS FELT STIFF BUT FUNCTIONAL. MAINTENANCE FOUND A-SYSTEM FLIGHT CONTROL MODULAR PACKAGE FAULTING, REPLACED MODULAR PACKAGE IAW BMM 27-09-21, OPS CHECK GOOD. FAILURE ANALYSIS TEST OF FLIGHT CONTROL MODULAR PACKAGE AND COULD NOT FIND ANY DEFECTS IN UNIT. A FULL FUNCTIONAL TEST WAS ACCOMPLISHED PER BOEING DWG 65-44891 REV. E, WITH NO DEFECTS NOTED. UNIT WAS DISASSEMBLED AND THE ONLY DEFECT FOUND WAS A SWOLLEN, SLIGHTLY DISTORTED O-RING SEAL ON POPPET ASSEMBLY FOR COMPENSATOR UNIT. (CLOSED) 2L72 4F RTA16WE 20050307002352005030700235NM 2005 3 7 AWXA200500305 120050303A33501012721 LIGHT BOEING737 7373G7 1384595NM SEAT ROW 10 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 PHX - EEL - DURING THRU-FLIGHT INSPECTION MAINTENANCE FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 10 LT BROKEN. REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 10 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050307002362005030700236NM 2005 3 7 AWXA200500306 120050120A3397 WIRE BOEING737 737301 1384611NM EMERGENCY LIGHT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - EEL - DURING C-18 CHECK BROKEN WIRES WERE FOUND AT MAIN CABIN FORWARD FLIGHT ATTENDANT STATION EMERGENCY EXIT LIGHT ASSEMBLY. MAINTENANCE REPLACED CONTACT PIN ON REMOVABLE SPLICE AT MAIN CABIN FORWARD FLIGHT ATTENDANT STATION EMERGENCY EXIT LIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050307002372005030700237NM 2005 3 7 AWXA200500307 120050217A53116547960503 FRAME BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON FRAME AT FORWARD SIDE OF BS 847 JUST INBOARD OF STR 25 RT. MAINTENANCE REMOVED DAMAGED SECTION OF FRAME AT BS 847 FROM STR 25 RT TO STR 26 RT; FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED REPAIR PARTS IAW ER 03-5300-05060-SS2. 2L72 4F RTA16WE 20050307002382005030700238NM 2005 3 7 AWXA200500308 120050220A5321D5367180500400 FLOOR PANEL AIRBUSA319 A319132 3930340NM CABIN CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28812AW 1178 SAL - MAJOR REPAIR - DURING BC-4 CHECK INTERGRANULAR CORROSION WAS FOUND ON FLOOR PANEL AT L-2 DOOR ENTRANCE. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL AT L-2 DOOR ENTRY WAY IAW T/C R1C25306. 2L72 4F RTA28NM 20050307002392005030700239NM 2005 3 7 AWXA200500309 120050213A533065479553 BEAR STRAP BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND INTERNAL SURFACE OF AFT CARGO DOOR CUTOUT LOWER FORWARD BEAR STRAP BS 807, STR 25 RT. MAINTENANCE CUT OUT DAMAGE IN AFT CARGO DOOR CUTOUT LOWER FORWARD BEAR STRAP AT BS 807, STR 25 RT; FABRICATED 2 EACH FILLERS, A DOUBLER AND TRIPLER; INSTALLED REPAIR PARTS IAW ER 03-5300-05062-ES1. 2L72 4F RTA16WE 20050307002402005030700240NM 2005 3 7 AWXA200500310 120050207A532065673129 REVEAL BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK A 1 INCH CRACK WAS FOUND IN R-2 DOOR LOWER FORWARD REVEAL AT 957, STR 17 RT. MAINTENANCE REMOVED AND REPLACED R-2 DOOR LOWER FORWARD REVEAL IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050307002412005030700241EA 2005 3 7 050606392 120050301A5712601R120327 RIB CNDAIRCL600 CL6002B19 1900309EA WING STA 53 LT CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27639BR 7313 LEFT BATTERY RIB IS CRACKED .750 INCH BETWEEN THE ATTACHING FASTENERS. 2L72 4F RTA21EA 20050307002422005030700242EA 2005 3 7 050606395 120050301A53206013521252 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27639BR 7313 RIGHT 624 OBLIQUE ANGLE IS CRACKED AT 1 INCH IN RADIUS. 2L72 4F RTA21EA 20050307002432005030700243EA 2005 3 7 050606394 120050301A53206013501251 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27638BR 7313 LEFT 624 OBLIQUE ANGLE IS CRACKED AT 1 INCH IN RADIUS. 2L72 4F RTA21EA 20050307002442005030700244EA 2005 3 7 050606391 120050301A5712601R102328 RIB CNDAIRCL600 CL6002B19 1900309EA RT WING CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27639BR 7313 RIGHT BATTERY RIB IS CRACKED .750 INCH BETWEEN THE ATTACHING FASTENERS. 2L72 4F RTA21EA 20050307002452005030700245EA 2005 3 7 QXEA200500290 120050211A5310 DOOR FRAME CNDAIRCL600 CL6002C10 1390015EA ZONE 200 BENT A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - AFT FUSELAGE - AFT BAGGAGE BAY DOOR SURROUND STRUCTURE AFT DOOR TRACK MOUNTING STRUCTURE LOWER MOUNTING BRACKET BENT. REPAIRED IAW 51-24-21-001-001-A01 AND 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050307002462005030700246EA 2005 3 7 QXEA200500281 120050212A5754 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 500 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - LT AILERON UPPER SKIN LEADING EDGE HAD CHAFED MARKS FROM SEAL. REPAIRED IAW CRJ700 SRM 51-41-01-101-001-A01, SRM 51-12-00-001-001-A01, 51-21-11-001-001-A01, 51-25-03-001-001-A01, 51-25-01-001-001-A01 AND CRJ700 AMM 57-52-32-000-809-A01. 2L72 4F RTA21EA 20050307002472005030700247EA 2005 3 7 QXEA200500282 120050210A1430 RIVET CNDAIRCL600 CL6002C10 1390015EA ZONE 600 LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - RT WING UPPER SKIN TRAILING EDGE HAS LOOSE FASTENERS AT STATION 170 AND 231.23. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A021 AND 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050307002482005030700248EA 2005 3 7 QXEA200500283 120050211A5730 ACCESS PANEL CNDAIRCL600 CL6002C10 1390015EA ZONE 600 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - RIGHTHAND WING AILERON ACCESS PANEL HAS CHAFE MARKS FROM SEAL. REPAIRED IAW CJR700 SRM 51-12-00-001-001-A01, 51-21-11-001-001-A01, 51-25-06-001-001-A01 AND 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050307002492005030700249EA 2005 3 7 QXEA200500284 120050216A5411 FRAME CNDAIRCL600 CL6002C10 1390015EA ZONE 400 WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - RT ENGINE UPPER FAN COWL INTERNAL OUTBOARD FORWARD FRAME WORN. REPAIRED IAW HORIZON AIE EA R-54-75 AND REO 670-54-14-336. 2L72 4F RTA21EA 20050307002502005030700250EA 2005 3 7 05061639 120050302A5320601R3117117 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27639BR 7313 INTERCOSTAL CRACKED AT .250 INCH IN LENGTH ON LEFT INBOARD SIDE AT FS 484 LEFT BETWEEN BL 36.00. 2L72 4F RTA21EA 20050307002512005030700251EA 2005 3 7 050616392 120050302A53116013600129 DOUBLER CNDAIRCL600 CL6002B19 1900309EA FRAME CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27639BR 7313 LEFT FS 640 FRAME DOUBLER IS CRACKED IN RADIUS AT 3 INCH IN LENGTH. 2L72 4F RTA21EA 20050307002522005030700252EA 2005 3 7 050616393 120050302A5320601R3111387 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27639BR 7313 LEFT 280 VERTICAL ANGLE IS CRACKED AT .5 INCH BETWEEN FASTENERS. 2L72 4F RTA21EA 20050307002532005030700253EA 2005 3 7 050616394 120050302A53116013600130 DOUBLER CNDAIRCL600 CL6002B19 1900309EA FRAME CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27639BR 7313 RIGHT FS 640 FRAME DOUBLER IS CRACKED IN RADIUS AT 3 INCH IN LENGTH. 2L72 4F RTA21EA 20050307002542005030700254EA 2005 3 7 VTZA200500001 120050302A5320601R3117117 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27706BR 7553 INTERCOSTAL CRACKED .250 INCH IN LENGTH OUTBOARD SIDE AT FS 484 LEFT BETWEEN BL 27.00. 2L72 4F RTA21EA 20050307002552005030700255EA 2005 3 7 VTZA200500002 120050302A5320601R35031239 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27706BR 7553 LEFT FS 621 FLOOR SUPPORT IS CRACKED AT 1 INCH. 2L72 4F RTA21EA 20050307002562005030700256EA 2005 3 7 VTZA200500003 120050302A5320601R35031239 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA ZONE 100 CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27706BR 7553 RIGHT FS 621 FLOOR SUPPORT IS CRACKED AT 1 INCH. 2L72 4F RTA21EA 20050307002572005030700257EA 2005 3 7 VTZA200500004 120050302A5320601R3111387 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27706BR 7553 LEFT 280 VERTICAL ANGLE IS CRACKED AT .5 INCH BETWEEN FASTENERS. 2L72 4F RTA21EA 20050307002582005030700258EA 2005 3 7 VTZA200500005 120050302A5320601R3111358 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27706BR 7553 RIGHT VERTICAL ANGLE IS CRACKED AT .5 INCH BETWEEN FASTENERS. 2L72 4F RTA21EA 20050307002592005030700259 2005 3 7 SWAA050651 420050303A25656970843 LATCH BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29379SW 26586 DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE, CABLE LATCH ASSY OUT OF ADJUST. ADJUSTED L1 DOOR EMERGENCY EVAC SLIDE LATCH ASSY PER MM. 2L72 4F RTA16WE 20050307002602005030700260NM 2005 3 7 SWAA050652 120050303A57546573714 SKIN BOEING737 7373H4 1384600NM LT WING SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29383SW 26589 DURING SCHEDULED C2 CHECK, FOUND LT WING, NR 2 SLAT, OUTBOARD T/E WEDGE PANEL DELAMINATED. REMOVED AND REPLACED NR 2 SLAT PER MM. 2L72 4F RTA16WE 20050307002612005030700261NM 2005 3 7 SWAA050653 120050303A53116545853 FRAME BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND CORROSION ON FUSELAGE FRAME AT BS 1006, LBL 39, WL 200. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20050307002622005030700262NM 2005 3 7 SWAA050654 120050303A3350101114 BULB BOEING737 7373A4 1384585NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29669SW 23752 DURING SCHEDULED SERVICE CHECK, FOUND 2 EA L2 DOOR LOWER EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BULBS PER MM. 2L72 4F RTA16WE 20050307002632005030700263NM 2005 3 7 SWAA050655 120050303A57536573732 SKIN BOEING737 7373G7 1384595NM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29683SW 24008 DURING SCHEDULED C4 CHECK, FOUND RT WING, T/E OUTBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED RT WING OUTBOARD AFT FLAP PER MM. 2L72 4F RTA16WE 20050307002642005030700264NM 2005 3 7 SWAA050656 120050303A53146545866 KEELBEAM BOEING737 737317 138447PNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON LT FUSELAGE KEELBEAM AT BS 540. REPAIRED KEEL BEAM PER SRM & ER. 2L72 4F RTA16WE 20050307002652005030700265NM 2005 3 7 SWAA050657 120050303A53116558280 FRAME BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 DURING SCHEDULED SPECIAL VISIT, FOUND CRACKED STUB FRAME AT BS 360, BETWEEN STR 14L & STR 15L. REMOVED AND REPLACED STUB FRAME PER SRM. 2L72 4F RTA16WE 20050307002662005030700266NM 2005 3 7 SWAA050658 120050303A53306545776 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACK AT BS 924R, STR 21R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050307002672005030700267NM 2005 3 7 SWAA050659 120050303A5313BAC1498 STRINGER BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 DURING SCHEDULED C4 CHECK, FOUND CORROSION ON FUSELAGE STRINGER AT BS 344, STR 28R. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2L72 4F RTA16WE 20050307002752005030700275NM 2005 3 7 USAA050225 120050210A5330 SKIN BOEING737 737401 1384701NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19409US46426 23879 CLT - FOUND SKIN CRACKED 2 INCHES, STATION 747 STRINGER 22L. INSTALLED DOUBLER IAW SRM 53-00-01. (M) 2L72 4F RTA16WE 20050307002772005030700277NM 2005 3 7 USAA050235 120050211A53201128323 WEB BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU50570 23706 PIT - FOUND WEB CORRODED 8 INCH BY 30 INCH AREA, BS 794-828, CORROSION LEVEL 1, TASK NR C53-202-01. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-40-00. (M) 2L72 4F RTA16WE 20050307002802005030700280NM 2005 3 7 USAA050234 120050209A55341138591 ANGLE BOEING737 7373B7 1384580NM VERTICAL STAB CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU50570 23706 PIT - FOUND SKATE ANGLE CHAFED, VERT STAB RT AND LT LOWER SKATE ANGLE. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-40-00 AND DWG 65-54842. (M) 2L72 4F RTA16WE 20050307002892005030700289NM 2005 3 7 UIEA200500010 120050222A575365B01925309C FLAP BOEING747 74747UF 1384949NM LT MIDFLAP DAMAGED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15493MC 29254 DURING WALK AROUND, MAINTENANCE FOUND DAMAGED TO LEFT OUTBOARD MIDFLAP T/E. REMOVED AND REPLACED LEFT OUTBOARD MIDFLAP IAW TASK CARD 27-51-04-404-025 REV 17 OCT 2003 S/N OFF, 000484. (M) 2L74 4F RT1384945 20050307002962005030700296NE 2005 3 7 2005F00023 220050217A7200 ENGINE AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE LEFT MALFUNCTIONED A TRBAC ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 SO29431AT 431 ON TAKEOFF ROLL, AIRCRAFT PULLED TO THE LEFT AND TORQUE INDICATION FLUCTUATED FOLLOWED BY HIGH ITT INDICATION. UPON POWER REDUCTION, THE OIL PRESSURE WARNING LIGHT CAME ONE. REMOVED ENGINE FOR INVESTIGATION. (M) 2H72 4T4 TRTA53EU E20NE 20050307003002005030700300SO 2005 3 7 SIMA200500904 120050104A532014522178005 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21632AE 145143 SAW - DURING CPCP INSPECTION, MAINTENANCE FOUND THE SERVICE DOOR SILL CORRODED. INSTALLED NEW SILL IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20050307003032005030700303 2005 3 7 2005F00016 420050217A230020412374418 POWER SUPPLY BEECH 300 300BEECH 1152930CE NR 2 COMM BURNED A RU3AB EMER. DESCENT A FLAME/FIRE APAPPROACH 1 SW1576 FF11 ON DOWNWIND AFTER BPC RUN, SMELLED ELECTRICAL BURNING. NOTICED NUMBER 2 COMM NO LEAD READOUT. PULLED CB NUMBER 2 COMM DUMPED CABIN. SMELL DID NOT DISPERSE TO OUR EXPECTATION. LANDED AIRCRAFT. FOUND NR 2 COMM POWER SUPPLY BURNED, REPLACED NR 2 COMM. (M) 2L72 4T A24CE 20050308002432005030800243NM 2005 3 8 SWAA050670 120050304A53126516300 BULKHEAD BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29661SW 23173 DURING SCHEDULED SPECIAL VISIT, FOUND 2 EA FUSELAGE WEB CRACKS AT BS 178 BULKHEAD, BETWEEN LBL 13.5 TO RBL 9 & BETWEEN WL 218 TO WL 234. REPAIRED FUSELAGE WEB PER SRM. 2L72 4F RTA16WE 20050307002722005030700272EA 2005 3 7 050616391 120050302A5320601R311719 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27639BR 7313 INTERCOSTAL CRACKED AT .250 INCH IN LENGTH ON RT INBOARD SIDE AT FS 484 LEFT BETWEEN BL 36.00. 2L72 4F RTA21EA 20050307003022005030700302 2005 3 7 2005F00017 420050217A2300 ODOR BEECH 300 300BEECH 1152930CE COCKPIT DETECTED A RU3AA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SW1576 FF11 ON DOWNWIND AFTER BPC RUN, SMELLED ELECTRICAL BURNING. NOTICED NUMBER 2 COMM NO LED READOUT. PULLED CB NR 2 COMM DUMPED CABIN. SMELL DID NOT DISPERSE TO OUR EXPECTATION. LANDED AIRCRAFT. (M) 2L72 4T A24CE 20050307003042005030700304NM 2005 3 7 GAIA05004OP 120050212A33501000677 LIGHT BOEING727 727251 138408HNM COCKPIT INTERMITTENT A GAIAK NONE O OTHER ININSP/MAINT 1 SW07279US 21158 DURING MAINTENANCE, THE CREW ENTRY DOOR EMERGENCY EXIT LIGHT WAS FOUND INTERMITTENT. REMOVED AND REPLACED EMERGENCY EXIT LIGHT. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20050307003062005030700306EU 2005 3 7 ASOA05058 120050122A5260S521764080220 STEP AEROSPATR72 ATR72212 8680945EU PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27634AS 370 FLT 4203 - DURING A GROUND INSPECTION IN ATL, THE TOP STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE TOP STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20050308002482005030800248 2005 3 8 SWAA050673 420050305A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR SLIDE PER MM. 2L72 4F RTA16WE 20050308002492005030800249 2005 3 8 SWAA050674 420050304A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR SLIDE PER MM. 2L72 4F RTA16WE 20050308002502005030800250NM 2005 3 8 SWAA050675 120050305A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACK AT BS 500D, STR 10R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050308002552005030800255NM 2005 3 8 SWAA050678 120050306A335007912 COVER BOEING737 7377H4 1384404NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29429WN 33658 EEPLS LIGHT COVER CRACKED AT EMERGENCY OVERWING EXIT. REMOVED AND REPLACED EEPLS LIGHT COVER PER MM. 2L72 4F RTA16WE 20050308002582005030800258NM 2005 3 8 SWAA050680 120050306A53306545780 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29607SW 27927 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR, UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050308002602005030800260NM 2005 3 8 SWAA050681 120050306A57546573714 WEDGE BOEING737 7373H4 1384600NM L/E SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29607SW 27927 DURING SCHEDULED D-CHECK, FOUND RT WING, NR 5 L/E SLAT, I/B END T/E WEDGE DELAMINATED. REMOVED AND REPLACED NR 5 L/E SLAT ASSY PER MM. 2L72 4F RTA16WE 20050309000122005030900012NM 2005 3 9 SWAA050684 120050306A33509250071 LAMP BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29450WN 32470 DURING SCHEDULED MV2 CHECK, FOUND FWD END OF EEPLS INOP. REMOVED AND REPLACED EEPLS BULB PER MM. 2L72 4F RTA16WE 20050309000152005030900015NM 2005 3 9 SWAA050687 120050306A534065C27314 STRINGER CLIP BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29507SW 24184 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 907, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20050309000222005030900022WP 2005 3 9 UPS05844010 120050221A53403779659U501 FITTING DOUG DC8 DC873F 302199FWP MAIN CABIN CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE: C1, LONGERON 3R END FITTING CRACKED IN MAIN CABIN, STA 902-920. REMOVED & REPLACED FITTING REF SRM 51-1-20D. 2L74 4F RT4A25 20050309000262005030900026EA 2005 3 9 COMA0560149 120050228A4920 APU CNDAIRCL600 CL6002B19 1900309EA APU BAY CONTAMINATED A COMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO01932CA 7038 FLIGHT 5886 DURING CLIMBOUT OF BWI CREW NOTED EVIDENCE OF SMOKE IN THE COCKPIT, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD, LANDING WITHOUT INCIDENT. PERFORMED ENGINE RUNS, DISCREPANCY COULD NOT BE DUPLICATED. AIRCRAFT HAD BEEN DE-ICED PRIOR TO DEPARTING BWI, SUSPECT DE-ICING FLUID ENTERED APU INLET CAUSING CONTAMINATION OF AIR DISTRIBUTION SYSTEM. 2L72 4F RTA21EA 20050309000272005030900027EA 2005 3 9 COMA0560148 120050228A329717300253 WIRE HARNESS CNDAIRCL600 CL6002B19 1900309EA NLG FAULTY A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01710CA 7241 FLIGHT 5153 AFTER TAKEOFF FROM CVG RECEIVED A GEAR UP DISAGREE MESSAGE, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. REPLACED THE NLG WIRING HARNESS ASSEMBLY. 2L72 4F RTA21EA 20050309000312005030900031WP 2005 3 9 UPS05844000 120050214A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01811UP 46089 INSPECTION TYPE:C2 EXT FUSELAGE SKIN CRACKED AT STA 1740 BETWEEN L16R & L17R. CUT OUT DAMAGE, NDT VERIFIED. FAB FILLER (SHT7075T6-.063), FINGER DOUBLER (SHT7075T6-.040), EXT DOUBLER (SHT7075T6-.071). INSTALLED SAME REF SRM 53-5-1 FIG 1, 53-2-1 FIG 7, NDT/SPM 06-10-01.001, 51-1-8. 2L74 4F RT4A25 20050309000322005030900032WP 2005 3 9 UPS05844001 120050219A5313564932750 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01811UP 46089 INSPECTION TYPE: C2, LONG 15R CRACKED AT STA 1746. DISASSEMBLED SPLICES AT STA 1726 & 1746. REMOVED SHEAR-TIES, FOUND STA 1746 ASSEMBLED WITHOUT STRAPS UNDER LONGERON. FAB LONG SECTIONS (EXTR S1616 757 & 2 STRAPS SHT7075T6-.080). TREATED, PRIMED, INSTALLED REPAIR PARTS REF SRM 53-2-0 FIG 10, DWG5649327, SRM 51-1-8, 51-1-20D. INSTALLED SHEAR TIES REF SRM 51-1-20D. 2L74 4F RT4A25 20050309000342005030900034 2005 3 9 SWAA050663 420050304A2565 BOTTLE BOEING737 7373H4 1384600NM R2 DOOR SLIDE DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29602SW 27953 R2 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATING LOW. REMOVED AND REPLACED R2 DOOR SLIDE PER MM. 2L72 4F RTA16WE 20050309000392005030900039NM 2005 3 9 SWAA050668 120050305A53146562125 KEELBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED C2 CHECK, FOUND CORROSION ON KEELBEAM, LT SIDE, BS 500D. REPAIRED KEEL BEAM PER SWA EA. 2L72 4F RTA16WE 20050309000422005030900042WP 2005 3 9 MWEA050025 120050305A56105912880508 SEAL DOUG DC9 DC982 3022082WP COCKPIT WINDOW LEAKING A MWEAA UNSCHED LANDING O OTHER CLCLIMB 1 GL31808ME 48070 FIRST OFFICER'S WINDOW WAS LEAKING AND WOULD GET LOUDER AS ALTITUDE WAS INCREASED. PRESSURIZED AIRCRAFT AND FOUND FIRST OFFICER'S WINDOW LEAKING, INSPECTED FIRST OFFICER'S CLEARVIEW SEAL AND FOUND VOID IN UPPER FORWARD CORNER. RESEALED VOIDS, PRESSURIZED AIRCRAFT TO 6.5 DIFFERENTIAL, NO LEAKS OR ABNORMAL NOISES. OK FOR SERVICE. 2L72 4F A6WE 20050309000442005030900044EA 2005 3 9 COMA0560158 120050303A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01783CA 7315 FLIGHT 5013 FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20050309000452005030900045NM 2005 3 9 UPS05443969 120050212A5315 FLOORBEAM BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, BS 460, RBL 11 - 30 FLOORBEAM WEB CORROSION FOUND. CORROSION BLEND OUT 0.025 X 1 X 3 EXCEED SRM 53-10-01 FIG 1, LIMIT FLOORBEAM WEB REPAIRED AS PER SRM 53-10-07 FIG 11. 2L74 4F A20WE 20050309000462005030900046NM 2005 3 9 UPS05443970 120050212A5315 FLOORBEAM BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, BS 460 RBL 66 - 65 FLOORBEAM WEB CORROSION FOUND. CORROSION BLEND OUT 0.025 X 1 X 4 EXCEED SRM 53-10-01 FIG 1, LIMIT FLOORBEAM WEB REPAIR AS PER SRM 53-10-07 FIG 11. 2L74 4F A20WE 20050309000472005030900047NM 2005 3 9 UPS05443971 120050214A5315 FLOORBEAM BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, BS 1700, RBL 11 - 33 FLOORBEAM FOUND CORRODED. CORROSION BLEND OUT 0.050 X 2 X 2 EXCEED SRM 53-10-01 FIG 1, LIMIT FLOORBEAM REPAIRED AS PER SRM 51-40-04 FIG 1. 2L74 4F A20WE 20050309000482005030900048NM 2005 3 9 UPS05443972 120050210A534069B142677 SUPPORT FITTING BOEING747 747123 1384873NM CARGO TRACK CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, TIE DOWN TRACK / BS 1000 B/H VERTICAL SUPPORT FTG CRACKED AT LBL 33 (CRACK LENGTH 1 INCH). M/DECK TIE DOWN TRACK BS 1000 B/H VERTICAL SUPPORT FTG REPLACED AT LBL 33 AREA AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050309000492005030900049NM 2005 3 9 UPS05443973 120050208A5347BAC15201566 SEAT TRACK BOEING747 747123 1384873NM FUSLEAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, BS 994 TO BS 995 RBL 98 SEAT TRACK CRACKED (CRACK LENGTH 1 INCH). M/ DECK BS 970 TO BS 995 RBL 98 TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A. 2L74 4F A20WE 20050309000512005030900051NM 2005 3 9 UPS05443976 120050212A5347BAC15201566 CARGO TRACK BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, BS 480-510 LBL 66 TIE DOWN TRACK I/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.041 X 1 X 3 EXCEED SRM 53-10-01 FIG 1, LIMIT TIE DOWN TRACK REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050309000532005030900053NM 2005 3 9 05FDEA00359 120050304A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 BS 950 LBL 11, WL 208 CORROSION ON FLOORBEAM (OUT OF LIMITS). REPAIRED BS 950 FLOOR BEAM LBL 11 WL 208 FED EX EA 7-5310-86259. 2L73 4F RTA3WE 20050309000582005030900058EU 2005 3 9 05FDEA00402 120050307A5511 SPAR AIRBUS310 A310222 3930315EU LT STABILIZER CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 LEFT STAB REAR SPAR STA 158, 2 INCHES OF CORROSION AND STA 258 HAS 1 INCH OF CORROSION REF N00264. REMOVED CORROSION FOUND OUT OF LIMITS, REPAIRED IAW SRM 55-11-21 FIG 215. 2L72 4F RTA35EU 20050309000592005030900059NM 2005 3 9 UPS05443980 120050212A5340 ATTACH ANGLE BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE:C, BS 440 RBL 55 INTERCOSTAL WEB ATTACH ANGLE CRACKED (CRACK LENGTH .75 INCH). ANGLE REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050309000602005030900060NM 2005 3 9 UPS05443981 120050210A5320 INTERCOSTAL BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, INTERCOSTAL BS 1300, LBL 11-33 RT O/B END CRACKED AT LWR SURFACE (CRACK LENGTH .75 INCH). INTERCOSTAL REPAIRED AS PER SRM 51-40-04 FIG 1. 2L74 4F A20WE 20050309000632005030900063NM 2005 3 9 UPS05443986 120050210A534069B620801 FITTING BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, BS 1560, RBL 18 TIE DOWN SUPPORT FITTING CORROSION FOUND. CORROSION BLEND OUT 0.020 X 1 X 1 INCH, EXCEED SRM 53-10-01 FIG 1. LIMIT FITTING REPLACED PER SRM 51-10-01. 2L74 4F A20WE 20050309000642005030900064NM 2005 3 9 UPS05443987 120050210A534069B620491 FITTING BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE:C M/D BS 1580 LBL 80 TIE DOWN SUPPORT FITTING CORROSION FOUND. CORROSION BLEND OUT 0.030 X 1 X 1 INCH, EXCEED SRM 53-10-01 LIMIT. FITTING REPLACED PER SRM 51-10-01. 2L74 4F A20WE 20050309000652005030900065 2005 3 9 CALA0500065 420050228A256580330035 BOTTLE BOEING757 757224 1384958NM L-4 DOOR SLIDE DISCHARGED A CALAK NONE O OTHER ININSP/MAINT 1 SW273413727226 30229 THE L-4 DOOR ASSIST BOTTLE WAS FOUND TO HAVE ZERO PRESSURE. THE BOTTLE WAS REMOVED AND REPLACED IAW MM 52-11-30. 2L72 4F RTA2NM 20050309000662005030900066EU 2005 3 9 05FDEA00385 120050306A5330 SKIN AIRBUS310 A310222 3930315EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 BULK PIT UNDER FLOOR FR 63 STR 44L HAS AN AREA OF CORROSION EXTENDING UNDER FRAME AND SHEAR TIE. REMOVED DAMAGED SECTION OF STRINGER AND REPAIRED IAW A310-200 SRM 53-10-14. 2L72 4F RTA35EU 20050309000672005030900067NM 2005 3 9 UPS05443989 120050210A5347AND101404004 CARGO TRACK BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, TIE DOWN TRACK BEAM LWR CHORD BS1000-1002 LBL 33 CORROSION CRACK FOUND. CRACK LENGTH 1 INCH AND CORROSION BLEND OUT 0.060 X 1 X 3 INCH, EXCEED SRM 53-10-01 LIMIT. M/D TIE DOWN TRACK BEAM LOWER CHORD REPAIRED AS PER HX RS R53-45-35264 & ENGINEERING FILE 747-53-20229. 2L74 4F A20WE 20050309000682005030900068NM 2005 3 9 UPS05443990 120050210A5330 SKIN BOEING747 747123 1384873NM R3 DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, BS 1306 BETWEEN S24-25R R3 DOOR SKIN FOUND CRACK (CRACK LENGTH 1.25 INCH). M/D BS 1306 BETWEEN STR 24R-25R DOOR 3R SKIN REPAIRED PER SRM 52-00-03 FIG 4. 2L74 4F A20WE 20050309000692005030900069NM 2005 3 9 UPS05443991 120050204A5312144U26031 BULKHEAD BOEING747 747123 1384873NM LT MLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, LT BODY L/G W/W STA 1480 BULKHEAD APU BLEED AIR DUCT CUT OUT FOUND CRACKED AT LEFT O/B SIDE LBL 100. CRACK LENGTH 2.5 INCH, LT BODY L/G W/W BS 1480 BULKHEAD APU BLEED AIR DUCT CUTOUT REPAIRED AS PER SB B747-53-2309 R1, EO B747-5310-3100-C AND DWG 144U2602. 2L74 4F A20WE 20050309000702005030900070NM 2005 3 9 UPS05443992 120050214A5315101363006 FLOORBEAM BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 BS 1700 LBL 58 - 76 FLOORBEAM FOUND CORRODED. CORROSION BLEND OUT 0.045 X 2 X 2 INCH, M/D BS 1700 BL 0 TO LBL 69 FLOORBEAM REPAIRED AS PER SRM 53-10-07 FIG 12. 2L74 4F A20WE 20050309000722005030900072EA 2005 3 9 COMA0560152 120050302A3310 LIGHT CNDAIRCL600 CL6002B19 1900309EA COCKPIT FIRE A COMAH DEACTIVATE SYST/CIRCUITS A FLAME/FIRE TXTAXI/GRND HDL 1 SO01976CA 7151 FLIGHT 5081 DURING INITIAL AIRCRAFT POWER UP THE FLIGHT OFFICER`S FLOODLIGHT CAUGHT FIRE. AIRCRAFT WAS IMMEDIATELY POWERED DOWN AND FIRE EXTINGUISHED. DEFERRED FLOOR LIGHT PER MEL 33-11-01-1. 2L72 4F RTA21EA 20050309000732005030900073EA 2005 3 9 COMA0560153 120050302A339759465 WIRE HARNESS CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DAMAGED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA 7031 FLIGHT 5397 AFT SECTION OF EMERGENCY FLOOR LIGHTING IS INOP. REPLACED WIRE CONNECTOR. 2L72 4F RTA21EA 20050309000752005030900075EU 2005 3 9 05FDEA00386 120050306A5313 STRINGER AIRBUS310 A310222 3930315EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 BULK PIT UNDER FLOOR FR 65 STG 54R HAS A 5 X 2 INCH AREA OF CORROSION ON SPLICE EXTENDING UNDER FASTENERS. REMOVED SPLICE ANGLE IAW A310-200 SRM 51-40-21. REMOVED CORROSION IAW A310-200 SRM 51-74-10. AREA OUT OF LIMITS IAW A310-200 SRM 53-10-00. REPLACED DAMAGED STRINGER IAW A310-200 SRM 53-10-14. TREATED, PRIMED, TOPCOATED IAW A310-200 SRM 51-21-10. REPLACED SPICE ANGLE IAW A310-200 SRM 51-40-21. 2L72 4F RTA35EU 20050309000792005030900079NM 2005 3 9 UPS05443947 120050208A5347LS48452 SEAT TRACK BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, BS 1110 RBL 75 SEAT TRACK WEB ATTACH STIFFENER FOUND CORRODED. CORROSION BLEND OUT 0.020 X 1 X 2 INCH EXCEED SRM 53-10-01 FIG 1, LIMIT. STIFFENER REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050309000802005030900080NM 2005 3 9 05FDEA00393 120050307A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA Y= 1100, X= 47 FOUND WITH CHAFED MARK. REMOVED PER SRM 53-70-00 VOLUME I, FIGURE 1. FABRICATED SEAT TRACK AND SPLICES INSTALLED PER SRM 53-70-00 VOLUME I, FIGURE 1. 2L73 4F RTA22WE 20050309000912005030900091NM 2005 3 9 UPS05443951 120050208A532065B164221 FLOOR SUPPORT BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, BS 1300, LBL 11- RBL 11, FLOOR SUPPORT FOUND CORRODED. CORROSION BLEND OUT 0.035 X 1 X 2 INCH EXCEED SRM 53-10-01 FIG 1, LIMIT. FLOOR SUPPORT REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050309000942005030900094EA 2005 3 9 05060657 120050301A2760 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA SPOILERS ILLUMINATED A VTZAO OTHER J WARNING INDICATION CRCRUISE 1 EA27657BR 7491 FLIGHT SPOILERS AND SPOILERON MESSAGE IN CRUISE. LANDED TO NEAREST SUITABLE AIRPORT (WHICH WAS THE SCHEDULED DESTINATION). MX RESET SECU. 2L72 4F RTA21EA 20050309000952005030900095NE 2005 3 9 DHL2005746004 220050226A7261 FILTER BOEING727 727224 1384076NM PWA JT8 JT8D15 52051NE NR 3 ENGINE BYPASSING A DHLAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01746DH 22252 NR 3 OIL FILTER BYPASS LIGHT ILLUMINATED. ABNORMAL PROCEDURE COMPLETE. REMOVED & REPLACED NR 3 ENG ASSY IAW B727 MTM 71.1. 2L73 4F4 F A3WE E2EA 20050309000992005030900099NM 2005 3 9 UPS05443959 120050210A5347BAC15201567 SEAT TRACK BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE:C M/D- BS 1600 - 1640 RBL 98 SEAT TRACK FLANGE CORROSION FOUND. CORROSION BLEND OUT 0.040 X 1 X 2 INCH EXCEED SRM 53-10-01 FIG 1, LIMIT. SEAT TRACK REPAIR AS PER SRM 53-10-05 FIG 1A. 2L74 4F A20WE 20050309001002005030900100NM 2005 3 9 UPS05443960 120050212A5347BAC15201566 CARGO TRACK BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, BS 480 - 500 LBL 84 TIE DOWN TRACK I/B FLANGE & LIP FOUND CORRODED. CORROSION BLEND OUT 0.047 X 1 X 2 INCH EXCEED SRM 53-10-01 FIG 1, LIMIT. TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A. 2L74 4F A20WE 20050309001012005030900101NM 2005 3 9 UPS05443961 120050210A5347BAC15201566 CARGO TRACK BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, BS 1480 - 1500 RBL 34, TIE DOWN TRACK FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.040 X 1 X 2 INCH EXCEED SRM 53-10-01 FIG 1, LIMIT. TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A. 2L74 4F A20WE 20050309001032005030900103NM 2005 3 9 UPS05443963 120050208A5347BAC15201566 SEAT TRACK BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, BS 996 TO 999 RBL 75 SEAT TRACK CRACKED (CRACK LENGTH 1.5 INCH). TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A AT BS 930 TO BS 1000 RBL 75 AREA. 2L74 4F A20WE 20050309001042005030900104NM 2005 3 9 UPS05443964 120050209A5347BAC15201566 SEAT TRACK BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, SEAT TRACK BS 1497 - 1500 LBL 33 RT FLANGE CORRODED. CORROSION BLEND OUT 0.030 X 1 X 2 INCH EXCEED SRM 53-10-01 FIG 1. TIE DOWN TRACK REPLACED AT BS 1480 TO BS 1600 LBL 33 AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050309001052005030900105EA 2005 3 9 QXEA200500289 120050211A5751 PANEL CNDAIRCL600 CL6002C10 1390015EA ZONE 600 WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 RT AILERON LEADING EDGE PANEL 699CB HAS A WEAR MARK FROM THE SEAL. REPAIRED IAW CRJ700 SRM 51-12-0-001-001-A01, 51-21-11-001-001-A01, 51-25-06-001-001-A01 AND SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050309001062005030900106EA 2005 3 9 QXEA200500285 120050212A7110 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 400 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 RT ENGINE LOWER CORE COWL INTERIOR SKIN HAS CHAFE MARKS AT THE 6 O'CLOCK POSITION. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01 AND 51-25-06-001-001-A01. 2L72 4F RTA21EA 20050309001082005030900108EA 2005 3 9 QXEA200500287 120050211A5753 SKIN PANEL CNDAIRCL600 CL6002C10 1390015EA ZONE 600 WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 RT WING FLAP LEADING EDGE PANEL IS WORN. REPAIRED IAW CRJ700 SRM 57-52-01-001-001-A01, 51-21-11-001-001-A01, 51-25-06-001-001-A01 AND 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050309001102005030900110NM 2005 3 9 UPS05443965 120050210A5347BAC15201566 SEAT TRACK BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, BS 1500 - 1560, LBL 98 SEAT TRACK FLANGE CORROSION FOUND. CORROSION BLEND OUT 0.045 X 1 X 2 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A AT BS 1480-1570 LBL 98 AREA. 2L74 4F A20WE 20050309001122005030900112WP 2005 3 9 UPS05843932 120050105A5330 FINGER DOUBLER DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01868UP 45968 INSPECTION TYPE: C, FINGER DOUBLER AT RBL 70 BETWEEN FS 879 - 902 HAS EXFOLIATION CORROSION. REMOVED AND REPLACED FINGER DOUBLER IAW DC8 SRM 51-1-21, DWG 5645332, AND DC8 SRM 51-1-8. 2L74 4F RT4A25 20050309001132005030900113WP 2005 3 9 UPS05843933 120050105A5712975329711 RIB DOUG DC8 DC873F 302199FWP NR 4 STUB WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01868UP 45968 INSPECTION TYPE: C, NR 4 STUB WING INBOARD L/E RIB CRACKED AT L/E. REMOVED, FABBED, AND INSTALLED NR 4 INBOARD STUB WING TAPERED FLANGE IAW DC8 SRM 51-1-21, DWG 9753297, SRM 51-1-8 AND DC8 SRM 51-1-21A. 2L74 4F RT4A25 20050309001142005030900114WP 2005 3 9 UPS05843934 120050106A53403750257U503 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01868UP 45968 INSPECTION TYPE: C, CRACK SPLICE FITTING AFT CARGO STA 1040 - 1060, L31R. REMOVED AND REPLACED SPLICE FITTING STA 1040 - 1060, L31R IAW DC8 SRM 51-1-21D, SRM 51-1-8, SRM 51-1-20 AND 51-1-11. 2L74 4F RT4A25 20050309001152005030900115NE 2005 3 9 MWEA050022 220050225A7321BR700 ENGINE BOEING717 717200 1383700NM RROYCEBR700 BR700710A110 NE LT AND RT FALSE INDICATIONA MWEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31921ME 55183 LEFT AND RIGHT ENGINE SYSTEM FAIL ALERT ANNUNCIATED. ENGINE ELECTRONIC CONTROLLER (EEC) INTERROGATION DISPLAY MAINTENANCE MESSAGES (FAULTS) 73211, 732138. PERFORMED FAULT ISOLATION MANUAL (FIM) TASKS, RETURN TO SERVICE (RTS), FUEL MATERING UNIT (FMU), EEC P20/T20 PROBES, FULL AUTHORITY DIGITAL ELECTRONIC CONTROL (FADEC), AND BOOSTER BLEED VALVE (BBV) WITH NO FAULT FOUND. PERFORMED ASSURANCE RUN, ALL CHECKED GOOD. 2L72 4F4 FTRA6WE E00057EN 20050309001212005030900121WP 2005 3 9 05FDEA00357 120050303A5730ARC0257 PANEL DOUG MD10 MD1010F 3022112WP ZONE 600 DELAMINATED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25361 48260 RT WING PANEL 641NB HAS AN AREA DELAMINATED. REPAIRED PANEL 641NB IAW EA 8-5710-83988, WINGS - RIGHT WING PANEL 641NB - REPAIR. 2L73 4F RTA22WE 20050309001232005030900123NM 2005 3 9 UPS05443939 120050212A5347BAC15201567 SEAT TRACK BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, BS 190 - 240 RBL 11 - 33 SEAT TRACK FLANGE CORROSION FOUND. CORROSION BLEND OUT 0.046 X 1 X 5 INCH EXCEED SRM 53-10-01 FIG 1, LIMIT. SEAT TRACK REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050309001262005030900126NM 2005 3 9 UPS05443942 120050214A5347BAC15201566 CARGO TRACK BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, BS 2060 - 2140, RBL 90, TIE DOWN TRACK FLANGE FOUND CORROSION CRACK (CRACK LENGTH 1 INCH). TIE DOWN TRACK REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050309001282005030900128NM 2005 3 9 UPS05443944 120050214A5347BAC15201566 SEAT TRACK BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C - BS 2060 - 2140 RBL 98 SEAT TRACK CORROSION FOUND. CORROSION BLEND OUT 0.042 X 1 X 3 EXCEED SRM 53-10-01 FIG 1, LIMIT. SEAT TRACK REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050309001292005030900129NM 2005 3 9 UPS05443945 120050214A5340 ATTACH FITTING BOEING747 747123 1384873NM FLOORBEAM CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE:C - BS 2100 RBL 90 - 98 FLOORBEAM ATTACH SPLICE CORROSION FOUND CORROSION BLEND OUT 0.035 X 1 X 2.5 EXCEED SRM 53-10-01 FIG 1, LIMIT. SPLICE REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050309001302005030900130NM 2005 3 9 UPS05443946 120050209A5315 FLOORBEAM BOEING747 747123 1384873NM M/D CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE:C - STA 1500, LBL 65 FLOORBEAM UPPER SURFACE CORROSION. CORROSION BLEND OUT 0.050 X 2 X 2 INCH EXCEED SRM 53-10-01 FIG 1, LIMIT. FLOORBEAM REPAIRED AS PER SRM 51-40-04 FIG 1. 2L74 4F A20WE 20050309001322005030900132WP 2005 3 9 UPS05843967 120050226A7603 THROTTLE DOUG DC8 DC871F 302199DWP ENGINE STUCK A IPXAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SO01729UP 46029 NR 2 THROTTLE STUCK IN IDLE DURING VISUAL APPROACH. NR 2 AND NR 3 REVERSERS USED IN FLIGHT PRIOR TO APPROACH. DURING T/S RAN ENG NR 2 & CYCLED T/R 3 TIMES AFTER CYCLING T/R THROTTLE CLD ONLY ADVANCE 2-3 BEFORE JAMB WITH ENG SHUTDOWN THROTTLE WLD MOVE FULL TRAVEL W/O JAMMING KN 0558726. PERFORMED VISUAL INSP OF NR 2 ENG T/R CAM ASSY ON PYLON, INSP THROTTLE BOX LINKAGE. RAN ENG AND SYC T/R & THROTTLE NORM C/W 76-11-00-2 A/C OK FOR SERVICE. 2L74 4F RT4A25 20050309001332005030900133NM 2005 3 9 UPS05M43954 120050226A5310 SEAL DOUG MD11 MD11F 3023600NM MAIN DECK LOOSE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP 48579 UPPER CARGO DECK GRAY LINER AT FWD LEFT BULKHEAD WALL IS PULLED AWAY FROM SIDE LINER. RESECURED SMOKE SEAL IAW MD-11 M/M 25-59-15. 2L73 4F RTA22WE 20050309001352005030900135EU 2005 3 9 05FDEA00374 120050304A5754 STRUCTURE AIRBUS310 A310222 3930315EU SLAT DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 REPAIR ON LT O/B SLAT UPPER SURFACE NEEDS EVALUATION FOR FAA APPROVED DATA AND MAJOR OR MINOR CLASSIFICATION, REF CONFORMITY INSPECTION RECORD SHEET 3 ITEM 24. REPAIR DETERMINED TO BE ACCOMPLISHED IAW A310-200 SRM 57-40-00 FIG 201. CLASSIFIED AS A MINOR REPAIR PER FEDEX GMM 6-2-100. 2L72 4F RTA35EU 20050309001362005030900136EU 2005 3 9 05FDEA00375 120050304A5347 SEAT TRACK AIRBUS310 A310222 3930315EU FUSELAGE BROKEN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 SEAT TRACK L-2 AT FRAME 52 HAS A BROKEN LUG, FOUND DURING CLS RE-INSTALLATION. REMOVED AND REPLACED SEAT TRACK SECTION IAW A310-200 SRM 53-10-16. 2L72 4F RTA35EU 20050309001382005030900138EA 2005 3 9 050606393 120050301A5310601R5211680 DOOR FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27639BR 7313 PAX DOOR FRAME TOP RADIUS CRACKED AT 1 INCH IN LENGTH FORWARD OF DATUM 1 AT FS 338.90. 2L72 4F RTA21EA 20050309001392005030900139NM 2005 3 9 DHL2005781506 120050220A5320 WEB BOEING727 727227 1384078NM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A C-CHECK, LEFT MLG W/W 950 WEB CRACKED AT AFT DOOR STOP FITTING. CUT OUT DAMAGED AREA 3.25 X 7.25, AT LEFT W/W STA 950 WEB AFT DOOR STOP FITTING IAW B727 SRM 51-40-2 FIG 1. FABRICATED REPAIR DOUBLER FROM 2024-T3 .040 PO 9001634 DIM 7.75 X 4.25 AND FILLER REPAIR FROM 2024-T3 PO 9001634 .040 IAW B727 SRM 53-10-2 FIG 5 AND 51-40-2 FIG 1. TREATED AND PRIMED DOUBLER, FILLER AND AREA IAW B727 SRM 51-10-2, INSTALLED PARTS IAW B727 SRM 51-40-2 FIG 1. 2L73 4F A3WE 20050309001402005030900140NM 2005 3 9 CALA0500066 120050304A5320656571034 STIFFENER BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716301 23352 INSPECTION FOUND 8 INCH CRACK IN STIFFENER FOR NR 3 VHF ANTENNA BETWEEN STA 727D AND 727E. A NEW STIFFENER WAS INSTALLED IAW SRM 51-40-2. 2L72 4F RTA16WE 20050309001412005030900141NM 2005 3 9 CALA0500067 120050227A53156545810 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714337 23575 INSPECTION FOUND FLOORBEAM CORRODED AT STA 312, RBL 21, RBL 36, AND RBL 49. THE FLOORBEAM UPPER CHORD WAS REMOVED AND REPLACED IAW SRM 53-00-51. 2L72 4F RTA16WE 20050309001422005030900142EA 2005 3 9 COMA0560159 120050303A3250 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA NLG STEERING ACTIVATED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01934CA 7042 FLT 5342 NWS INOP CAUTION AFTER T/O. COULD NOT DUPLICATE. OPERATIONAL TEST OF NWS SYSTEM WAS SATISFACTORY. 2L72 4F RTA21EA 20050309001432005030900143WP 2005 3 9 UPS05844014 120050222A53403779659U501 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE: C1, LONGERON FITTING CRACKED IN MAIN CABIN STA 902-910 LONG 4L. REMOVED AND REPLACED FITTING REF SRM 51-3-0, 51-1-20B, 51-1-21, 51-1-20D. 2L74 4F RT4A25 20050309001442005030900144EA 2005 3 9 COMA0560151 120050301A5244 DOOR CNDAIRCL600 CL6002B19 1900309EA OXYGEN SERVICE OPEN A COMAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 SO01805CA 7354 FLIGHT 5554 STALL FAIL CAUTION AFTER T/O. FOUND 02 SERVICE DOOR OPEN. CLOSED 02 SERVICE DOOR. 2L72 4F RTA21EA 20050308002562005030800256NM 2005 3 8 SWAA050679 120050306A57436567172 FITTING BOEING737 7373H4 1384600NM RT WING CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED RON CHECK, FOUND RT MLG STAB FITTING CORRODED. REPAIRED FITTING PER SWA EA. 2L72 4F RTA16WE 20050309000192005030900019EU 2005 3 9 UPS05144024 120050305A3350 LIGHT AIRBUS300 A300B4622R 3930312EU EMERGENCY EXIT WILL NOT TEST A IPXAK NONE O OTHER ININSP/MAINT 1 SO01121UP 0806 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS DON'T TEST PROPERLY. RELAMPED LIGHT ASSY OVER L1 DOOR, CHECKS OK. 2L72 4F RTA35EU 20050309000362005030900036 2005 3 9 SWAA050665 420050304A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED L1 DOOR SLIDE PER MM. 2L72 4F RTA16WE 20050309000372005030900037NM 2005 3 9 SWAA050666 120050306A53306545766 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACK AT BS 480, STR 17L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050309000502005030900050NM 2005 3 9 UPS05443974 120050208A5347BAC15201873 SEAT TRACK BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, BS 1165, RBL 75 SEAT TRACK FLANGE CORROSION FOUND. CORROSION BLEND OUT 0.030 X 1 X 1 EXCEED SRM 53-10-01 FIG 1, LIMIT SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 34. 2L74 4F A20WE 20050309000542005030900054EU 2005 3 9 05FDEA00360 120050304A5347A5361164020001 SEAT TRACK AIRBUS310 A310222 3930315EU ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 MDCC NR 2 SEAT TRACK RT OF CENTER LINE FROM FRAME 15 TO FRAME 18 HAS HEAVY CORROSION. REMOVED SEAT TRACK IAW A310-200 SRM 51-40-21. INSTALLED NEW SEAT TRACK IAW A310-200 SRM 51-40-21. 2L72 4F RTA35EU 20050309000562005030900056EU 2005 3 9 05FDEA00400 120050307A5313 STRINGER AIRBUS310 A310222 3930315EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 BULK PIT UNDER FLOOR STG 54L 10 IN AFT OF FR 67 IS AN AREA 5 X 2 OF CORROSION EXTENDING UNDER FASTENERS. REMOVED CORROSION FOUND OUT OF LIMITS, REPAIRED IAW 53-10-14. 2L72 4F RTA35EU 20050309000782005030900078EU 2005 3 9 05FDEA00389 120050306A5310 STRUCTURE AIRBUS310 A310222 3930315EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 BULKPIT UNDER FLOOR 5 INCHES AFT OF FR 65 STG 51R HAS AN AREA 1 X 1 INCH OF CORROSION EXTENDING UNDER FASTENERS. REMOVED CORROSION IAW A310-200 SRM 51-74-10. AREA WAS OUT OF LIMITS IAW A310-200 SRM 53-10-00. REMOVED AND REPLACED DAMAGED AREA IAW A310-200 SRM 53-10-14. TREATED, PRIMED, TOPCOATED AREA IAW A310-200 SRM 51-21-10. SEALED AREA IAW A310-200 SRM 51-76-00. 2L72 4F RTA35EU 20050309001162005030900116EU 2005 3 9 05FDEA00397 120050307A5410 SUPPORT ANGLE AIRBUS310 A310222 3930315EU NR 1 PYLON CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 NR 1 PYLON - ACCESS 475AL- RT UPPER INTERIOR ANGLE SUPPORT CRACKED IN T-SHAPED LENGTH EA WAY 1.0 INCH REF N00449. REMOVED AND REPLACED ANGLE SUPPORT IAW SRM 54-55-51. 2L72 4F RTA35EU 20050309001182005030900118EU 2005 3 9 05FDEA00399 120050307A5313 STRINGER AIRBUS310 A310222 3930315EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 BULK PIT UNDER FLOOR STG 49R FR 64 FWD 4 IN TO AFT 4 IN 1 IN I/B AND O/B OF STG HAS CORROSION EXTENDING UNDER FRAME REF N00781. REMOVED CORRODED AREA OUT OF LIMITS, REPAIRED STG IAW SRM 53-10-14. 2L72 4F RTA35EU 20050309001312005030900131WP 2005 3 9 UPS05843936 120050105A534037584911 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01868UP 45968 INSPECTION TYPE: C, CRACKS AFT CARGO PIT STA 1240 L35L. REMOVE EXISTING PRODUCTION SPLICE AND FITTING AND STOP DRILL CRACKS. FAB AND INSTALL SPLICE ANGLE. FAB AND INSTALL FRAME FITTING IAW DC8-SRM 51-1-21, 51-1-20, SR ADD DC8 5320-6176-B, SAA TRAVELER 0073 SRM 51-1-8, AND 51-3-2. 2L74 4F RT4A25 20050309001472005030900147EU 2005 3 9 05FDEA00366 120050304A5330 SKIN AIRBUS310 A310222 3930315EU TAIL CONE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 APU TAIL CONE FR 102 RT SIDE AT 3 O'CLOCK POSITION HAS A 6 INCH VERTICAL CRACK IN THE EXTERIOR SKIN. REPAIRED APU SKIN, STOPPED DRILLED CRACK IAW A310-200 SRM 53-19-12 PG 102. PERFORMED ET INSPECTION IAW A310-200 NTM 51-10-08. FABRICATED DOUBLER IAW A310-200 SRM 53-19-12 PG 207. HEAT TREATED RIVETS IAW A310-200 SRM 51-25-00. INSTALLED DOUBLER IAW A310-200 SRM 53-19-12. ALODINED, PRIMED AND TOP COATED DOUBLER IAW A310-200 SRM 51-23-20. 2L72 4F RTA35EU 20050309001492005030900149NM 2005 3 9 AWXA200500293 120050210A5311654656145 FRAME BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK 2 EACH .1875 INCH CRACKS WERE FOUND IN R-2 DOOR LOWER FORWARD FRAME SECTION BS 957, STR 16 RT. MAINTENANCE CUT OUT DAMAGE IN R-2 DOOR LOWER FORWARD FRAME SECTION; FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-11. 2L72 4F RTA16WE 20050309001522005030900152NM 2005 3 9 AWXA200500296 120050128A531165176856 STRAP BOEING737 737301 1384611NM FRAME CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK A .3125 INCH CRACK WAS FOUND IN LOWER FORWARD INBOARD EDGE OF FRAME STRAP AT BS 349, STR 16 LT. MAINTENANCE REMOVED DAMAGED FRAME STRAP AT BS 349, STR 16 LT; INSTALLED A NEW REPLACEMENT FRAME STRAP IAW ER 03-5300-05053-SS3. 2L72 4F RTA16WE 20050309001532005030900153NM 2005 3 9 AWXA200500297 120050219A5320654795710 CHANNEL BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND AFT CARGO DOOR SILL LOWER CHANNEL AT BS 837, STR 25 RT. MAINTENANCE REMOVED CORRODED AFT CARGO DOOR SILL LOWER CHANNEL AT BS 837, STR 25 RT; FABRICATED A NEW REPLACEMENT CHANNEL PER DWG 65-47957; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050309001542005030900154NM 2005 3 9 AWXA200500298 120050215A532069429494 CLIP BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK A .25 INCH CRACK WAS FOUND IN AFT CARGO COMPARTMENT FRAME ATTACH CLIP AT BS 807, STR 25 RT. MAINTENANCE REMOVED CRACKED AFT CARGO COMPARTMENT FRAME ATTACH CLIP AT BS 807, STR 25 RT; FABRICATED A NEW REPLACEMENT CLIP PER DWG 69-42949; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050309001552005030900155NM 2005 3 9 AWXA200500299 120050125A2560P2070003001 FLASHLIGHT BOEING737 737301 1384611NM ZONE 900 INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - EMERGENCY EQUIPMENT - DURING C-18 CHECK FOUND THE LT FORWARD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LT FORWARD EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050309001592005030900159NM 2005 3 9 DHL2005781504 120050221A5312 PRESSURE PANEL BOEING727 727227 1384078NM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A C-CHECK; NLG W/W BAY UPPER RT INSIDE NOSE PRESSURE ACCESS PANEL CAVITY AREA ABOVE CABLE RUNS, LWR UNDERSIDE COCKPIT FLOOR, ATTACH ANGLE AT BS 230 AT LBL 10 ATTACH ANGLE HAS EDGE CRACKED, GOING TO BUCKTAIL FASTENER HOLE AND BEYOND (EXTENDING PASS HOLE). REMOVED ANGLE AS REQ FOR FAB NEW AT NLG W/W UPPER RT BS 230 AT LBL 10 IAW B727 SRM 51-30-2. FABRICATED NEW ANGLE MAT'L USED 7075-T6 .040 PO 9001777 DIM 10.125 X 1.5 IAW B727 SRM 51-20-1 AND 53-10-2 FIG 7. ALODINED AND PRIMED IAW B727 SRM 51-10-2, INSTALLED NEW ANGLE IAW B727 SRM 53-10-2 FIG 7 AND 51-20-1. 2L73 4F A3WE 20050309001612005030900161WP 2005 3 9 UPS05844016 120050222A534136431122 ATTACH ANGLE DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE: C1, SPAR-TO-WING ATTACH ANGLE CRACKED IN MAIN CABIN SUBFLOOR, STA 798 RBL 55. FAB REPLACEMENT ANGLE REF DWG3643112 ON SAA SERVICE ORDER 7034920. REMOVED & REPLACED ANGLE REF SRM 51-1-20D, 51-3-2, 51-1-24, 51-1-20D. FUEL LEAK CHECK C/W ON TC8000. 2L74 4F RT4A25 20050309001632005030900163WP 2005 3 9 UPS05844019 120050222A534037739061 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE: C1, FITTING CRACKED UNDER FLOORBEAM, STA 700 RBL 24 MAIN CABIN. REMOVED AND REPLACED FITTING REF SRM 51-3-0, 51-1-20D. 2L74 4F RT4A25 20050309001652005030900165WP 2005 3 9 UPS05844021 120050222A5310REFDWG5645332 FINGER DOUBLER DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE: C1, FINGER DOUBLER CRACKED & HAS SHEARED RIVET HEADS IN MAIN CABIN SUBFLOOR, STA 875 LBL 5. REMOVED FINGER DOUBLER & FOUND IT HEAVILY CORRODED ON UNDERSIDE. NO CORROSION NOTED ON PRESSURE WEB. FAB REPLACEMENT FINGER DOUBLER FROM 2024T3-.050. INSTALLED & SEALED DOUBLER REF DWG5645332, SRM 51-1-21, 51-1-8, 51-1-20D, 51-1-11. 2L74 4F RT4A25 20050309001662005030900166WP 2005 3 9 UPS05844022 120050221A5340577384444 CLIP DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE: C1, TIE ANGLE CRACKED ON FWD SIDE OF AFT PRESSURE BULKHEAD TO LONG 6R. REMOVED CRACKED ANGLE. FAB REPLACEMENT ANGLE FROM SHT7075/0-.080 AND HEAT TREATED TO T6 ON SAA SERVICE ORDER 7034928. INSTALLED ANGLE REF DWG 5773844, SRM 51-1-21, DPS7.00-1. 2L74 4F RT4A25 20050309001672005030900167 2005 3 9 UPS05144003 420050222A2565 SLIDE AIRBUS300 A300B4622R 3930312EU PAX DOOR INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01133UP 0816 INSPECTION TYPE:N/A SLIDE ON MAIN ENTRY DOOR WILL NOT ARM. OPERATED DOOR ARM NORMALLY. OK FOR SERVICE, COULD NOT DUPLICATE PROBLEM. 2L72 4F RTA35EU 20050309001682005030900168 2005 3 9 UPS05144023 420050303A2565 CONNECTOR AIRBUS300 A300B4622R 3930312EU PAX DOOR SLIDE INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01158UP 0847 MAIN CABIN ENTRY DOOR, SLIDE ARMED WARNING LIGHT FAILS TO ILLUMINATE WHEN TEST SWITCH DEPRESSED. WARNING HORN OK. DEFERRED PER MEL 52-73-01-1 CNTL M298193. PLACARD INSTALLED. *S/D* RESEATED CONNECTOR ON ASPSU. OPS CHECKS NORMAL PER MM 52-73-00-5. THIS CLEARS M298193. 2L72 4F RTA35EU 20050309001702005030900170NM 2005 3 9 UPS05443996 120050214A5330 SKIN BOEING747 747123 1384873NM FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE:C FX LAP JOINT AT BS 1867 TO 1877 STR 46L FOUND LOSS OF SKIN THICKNESS DUE PREVIOUSLY BLENDED 0.013 X .5 X 4 INCH. LAP JOINT OPENED UP FOR INSPECTION FOR DEFECTS FREE, LAP JOINT REINSTALLED PER HX RS R-53-60-35259 AND UPS EO B747-5330-21779-A. 2L74 4F A20WE 20050309001712005030900171NM 2005 3 9 UPS05443997 120050205A571265B1015110 RIB BOEING747 747123 1384873NM RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE:C RIGHT WING 17 VC FLAP O/B ARM O/B RIB MOST FWD FASTENER HOLE CRACKED (CRACK LENGTH 1.25 INCH). RIGHT WING 17 VC FLAP O/B ARM O/B RIB FWD FLANGE FASTENER HOLES REPAIRED AS PER HX RS R57-41-35263 AND UPS EO B747-5740-21796-A. 2L74 4F A20WE 20050309001722005030900172NM 2005 3 9 UPS05444004 120050214A534069B0445814 SUPPORT FITTING BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE:C M/D BS 1960 RBL 60 FLOOR TRACK SUPPORT FITTING 2EA FOUND CRACKED. SUPPORT FITTINGS REPLACED PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050309001742005030900174NM 2005 3 9 UPS05444006 120050205A571265B1013714 RIB BOEING747 747123 1384873NM RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE:C RIGHT WING ILES 1057.55, 21 V/C FLAP I/B ARM O/B RIB FWD VERTICAL MOUNTING ATTACH FASTENER HOLES CRACKED (CRACK LENGTH 1 INCH). RIGHT WING 21 VC FLAP I/B ARM O/B RIB FWD VERTICAL FLANGE REPAIRED AS PER HX RS R-57-41-35262 AND UPS EO B747-5740-21822-A. 2L74 4F A20WE 20050309001752005030900175NM 2005 3 9 UPS05444007 120050222A571265B1013714 RIB BOEING747 747123 1384873NM RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE:C RIGHT W ILES 1057.55, 21 V/C FLAP I/B ARM O/B RIB MULTI CRACKS FOUND DURING RIB INSTALLATION WITH RIVET (CRACK LENGTH 1 TO 3 INCH). RIGHT WING 21 VC FLAP I/B ARM O/B RIB TOP FLANGE REPAIRED AS PER HX RS R-57-41-35262 AND UPS EO B747-5740-21822-A. 2L74 4F A20WE 20050309001762005030900176NM 2005 3 9 DHL2005781505 120050211A5754 SKIN BOEING727 727227 1384078NM SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A C-CHECK, NR 3 SLAT SKIN AT TRACK ATTACH POINT CRACKED. MAKE 2 EA STOP DRILLS WITH .25 DIA DRILL AT NR 3 SLAT SKIN AT I/B TRACK IAW B727 SRM 57-5-3 FIG 1. ACCOMPLISHED 727 HFEC INSPECTION 51-00-00 FIG 4, CRACK CONTAINMENT CONFIRMED. FAB REPAIR DOUBLER MAT'L USING 2024-T3 .080 PO 9001502 DIM 5.25 X 6.5 IAW B727 SRM 57-50-3 FIG 1 SHEET 2 AND 57-50-2 FIG 2 SHEET 1. TREATED, ALODINED AND PRIMED IAW B727 SRM 51-10-2, INSTALLED REPAIR DOUBLER AT NR 3 SLAT AT I/B SIDE IAW B727 SRM 51-30-2. 2L73 4F A3WE 20050309001782005030900178EA 2005 3 9 QXEA200500271 120050210A5753 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 500 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - LEFTHAND INBOARD FLAP LOWER SKIN SURFACE HAS CHAFE MARK FROM INBOARD HINGE FAIRING. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01. 2L72 4F RTA21EA 20050309001792005030900179EA 2005 3 9 QXEA200500272 120050210A5753 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 600 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - RIGHTHAND WING, INBOARD FLAP, LOWER SURFACE HAS PITTING AND DENTS. REPAIRED IAW CRJ700 SRM 57-52-01-101-001-A01 AND SRM 51-12-00-001-001-A01. 2L72 4F RTA21EA 20050309001802005030900180EA 2005 3 9 QXEA200500273 120050210A5280 SKIN CNDAIRCL600 CL6002C10 1390015EA MLG DOOR DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - LEFTHAND MAIN LANDING GEAR DOOR LOOSE RIVETS NEAR FORWARD HINGE, OUTBOARD SKIN. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20050309001832005030900183EA 2005 3 9 COMA0570024 120050302A5270 WARNING SYSTEM CNDAIRCL600 CL6002C10 1390015EA E/E BAY DOOR ACTIVATED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01368CA 10075 FLIGHT 5511 AVIONICS DOOR WARNING DURING T/O. DEFERRED MAINT ON DOOR WARNING PER MEL. 2L72 4F RTA21EA 20050309001852005030900185NM 2005 3 9 SWAA050669 120050304A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29360SW 26571 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACK AT BS 727D, STR 23L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050309001912005030900191EA 2005 3 9 SWIA200514612 120050219A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07951SW4717 4717 7795 STAB TRIM CH 2 WILL NOT ENGAGE. REMOVED HSTA AND MCU IAW MM 27-40-00, 27-42-01, 27-42-05. OPERATIONAL CHECK GOOD. P/N 7062-3, S/N OFF 1092. 2L72 4F RTA21EA 20050309001932005030900193EA 2005 3 9 SWIA200514613 120050219A5610 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAO OTHER O OTHER APAPPROACH 1 NM07429SW 7518 WHILE ON SHORT FINAL INTO FCA, THE CAPTAINS SIDE WINDOW DEVELOPED 3 LARGE CRACKS IN IT. REPLACED CAPTAINS SIDE WINDOW PER MM 56-12-01. OPERATIONAL CHECK GOOD. P/N NP-139322-5, S/N OFF 02164H8144. 2L72 4F RTA21EA 20050309001952005030900195EA 2005 3 9 SWIA200514614 120050220A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLT SPOILERS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07720SW8895 8895 7297 SPOILERONS FAULT MESSAGE ON TAXI OUT. REMOVED AND REPLACED LEFT SPOILERON OUTBOARD PCU IAW AMM 27-62-01. OPERATIONAL CHECK IAW AMM 27-64-00 GOOD. 2L72 4F RTA21EA 20050309001992005030900199NM 2005 3 9 DL76L050113 120050214A26105108WW BULB BOEING767 767332 1382001NM COCKPIT INTERMITTENT A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27187DN 27582 CRUISING APPROX 50W AT 32K, BLUE GRAY SMOKE FROM FRONT PANEL SMOKE IN COCKPIT. SMOKE STOPPED WHILE RUNNING SMOKE CHECKLIST. DIVERTED TO ST JOHNS. THOROUGHLY INSPECTED AIRCRAFT AND SYSTEMS, NO TROUBLE FOUND. REPLACED INTERMITTENT BULBS IN CAPTAINS LIGHT. 2L72 4F RTA1NM 20050309002002005030900200NM 2005 3 9 375PA0046 120050221A5347 SEAT TRACK BOEING737 73739A 138447PNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05375PA 23812 SEAT TRACK FROM BS 344 TO BS 380 AT LBL 25 CORRODED. REPLACED SECTION OF SEAT TRACK PER SRM 53-00-52. 2L72 4F RTA16WE 20050309002012005030900201EU 2005 3 9 MALA050186 120050216A33503301501 POWER SUPPLY SAAB SF340 340B 7860101EU EMERGENCY LIGHT FAILED A MALAK NONE O OTHER ININSP/MAINT 1 GL15423XJ 340B423 EMERGENCY POWER SUPPLY P/N 3301-501, S/N 2023 FAILED SCHEDULED CAPACITY CHECK. REPLACED BATTERY ASSEMBLY P/N 3301-31. UNIT PASSES CMM CHECKS, RTS 2/12/05. 2L72 4T RTA52EU 20050310000932005031000093EU 2005 3 10 CX7A194J0505 120050103A26131734362450 DETECTOR SAAB SF340 340B 7860101EU LT TAILPIPE SATURATED A CX7AC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL03300CE 340B184 LEFT TAILPIPE HOT LIGHT ILLUMINATED ON TAKEOFF. 2L72 4T RTA52EU 20050310000942005031000094EU 2005 3 10 CX7A194J0506 120050105A26131734362450 DETECTOR SAAB SF340 340B 7860101EU LT TAIL PIPE SATURATED A CX7AC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL03303CE 340B194 LT TAIL PIPE HOT ON TAKE OFF. ABORTED. 2L72 4T RTA52EU 20050310000952005031000095SO 2005 3 10 21200003001 120050102A78206879600 MUFFLER PIPER PA32 PA32R300 7103213SO LYC O540 IO540K1A5 41532EA HARTZLHCC2Y HCC2YK1 GL ENGINE FATIGUED E K NONE O OTHER ININSP/MAINT 1 WP134127R5785 3240445 RL711148 CH35895B DURING MX CHK, MILD CORROSION IDENTIFIED ON INTERNAL AREA OF DEFECTIVE PARTS. MULTIPLE FRAGMENTS OF METAL RANGING FROM 0.25 INCH TO 1.25 INCH DIAMETERS INSIDE OF INTERNAL BAFFLE. INSP OF EXHAUST COMPONENT FAILURES. EXHAUST MUFFLER, PN 6879900, OVERHAULED ON APRIL 23, 1998. EXHAUST MUFFLER INSTALLED ON JUNE 1, 2000. INSTALL TIME FRAME DOES NOT REFLECT EXHAUST INSTALLATION. STACK ASSY, PN 6879300, OVERHAULED ON APRIL 22, 1998 STACK ASSY INSTALLED ON JUNE 1, 2000. INSTALLATION TIME FRAME DOES NOT REFLECT STACK ASSY INSTALL. SHROUD, PN 68798-00, REPAIRED, UPON INSPECTION OF STACK ASSY, IT IS DEEMED AIRWORTHY & FREE OF METAL FATIGUE SO ONLY REPLACEMENT OF MUFFLER ASSY IS NEEDED TO CORRECT PROBLEM. 1L71 3O3 O A3SO 1E4 5 CP920 20050310000972005031000097 2005 3 10 U30A200500001 220050103A75322293B010000 BLEED VALVE AIRBUS320 A320214 3930316EU NR 2 ENGINE CRACKED A U30AO OTHER RYJPARTIAL RPM/PWR LOSS ENGINE STOPPAGE WARNING INDICATION DEDESCENT 1 EA17268AV1959 1959 2175 NR 2 ENG BEGAN COMPRESSOR STALLING. FLT CREW NOTICED THAT N1 WENT TO 43 PERCENT & FLUCTUATED BETWEEN 43 & 45 PERCENT. DECLARED AN EMERGENCY. AT ABOUT 10,000 FT, NR 2 ENGINE STABILIZED & APPEARED TO OPERATE NORMALLY. A VISUAL APPROACH TO A LANDING ON RUNWAY 6 AT RSW FLOWN. DURING ROLLOUT, AN ECAM WARNING, NR 2 ENG FAIL RECEIVED & ENG SHUTDOWN. LANDING ENDED W/O FURTHER INCIDENT. MX PERFORMED FAULT ISOLATION PROCEDURE PER TSM 73-00-00-810-865 & 72-00-00-810-807. FOUND FAULTY "IP BLEED CHECK VALVE". R&R IP CK VALVE PER AMM 36-11-44-000-040 & OPS & LEAK CK PER AMM 36-11-41-200-001, WITH NO FAULT FOUND. PERFORMED PRECAUTIONARY BOROSCOPE INSPECTION OF NR 2 ENG WITH NO UNSERVICEABLE DEFECTS NOTED. A/C RETURNED TO SER2L72 4F RTA28NM 20050310000982005031000098SW 2005 3 10 PNSA050101 120050101A27202770001073 CONTROL CABLE SWRNGNSA227 SA227AC 8780603SW RUDDER DAMAGED A PNSAHA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 AL0341NE 453 AC741B AIRCRAFT WAS PRESURIZING AT MAXIMUM RATE PRESSURIZATION CONTROLS HAD NO AFFECT DURING CLIMBOUT FROM ANC. AIRCRAFT TURNAROUND AND RETURNED TO ANC. MAINTENACE FOUND RUDDER CABLE SWAGED BALL RETAINER HAD CHAFED A HOLE IN THE OUTFLOW VALVE CONTROL CHAMBER NOT ALLOWING IT TO OPEN. RUDDER SYSTEM RIGGING WAS CHECKED AND FOUND AT MAX TRAVEL LIMITS OF 25 DEGREES. RUDDER STOPS WERE ADJUSTED TO MIN TRAVEL OF 24 DEGREES. M7 AEROSPACE HAS A KIT AVAILABLE PN 27K23013 TO INCREASE THE CLEARANCE BY SPACING THE OUTFLOW VALVE AFT WITH A THICKER GASKET. 2L72 4T RTA8SW 20050310001022005031000102SW 2005 3 10 2005F00000 120050105A56102719442003 WINDSHIELD SWRNGNSA227 SA227AC 8780603SW COCKPIT BLEW OUT E DUFABA EMER. DESCENT UNSCHED LANDING D INFLIGHT SEPARATION CLCLIMB 1 GL273108B AC509 WHILE ON CLIMB OUT, THE PILOTS WINDSHIELD BLEW OUT AND CAUSED A RAPID DE-COMPRESSION OF THE AIRCRAFT. THE PILOT TOOK EMERGENCY ACTION AND PERFORMED A RAPID DECENT TO A SUITABLE ALTITUDE. NO COMMUNICATION COULD BE ESTABLISHED WITH ANYONE DUE TO THE DAMAGE DONE TO THE PILOTS HEADSET SO 7700 WAS SQUAWKED ON THE AIRCRAFT TRANSPONDER. THE PILOT MOVED INTO THE RIGHT SEAT AND RETURNED TO THE AIRPORT, WHERE HE MADE AN UNEVENTFUL LANDING. AFTER QUESTIONING THE PILOT ABOUT THE INCIDENT, IT CAN ONLY BE SPECULATED THAT BECAUSE OF THE SEVERE COLD AIR (-40) AND WITH THE WINDSHIELD HEAT SELECTED ON, A FRACTURED DEVELOPED IN THE OUTER WINDOWPANE ALLOWING IT TO FAIL. 2L72 4T RTA8SW 20050310001102005031000110NM 2005 3 10 2005F00015 120050110A5340 BRACKET BOEING737 737282 13844ATNM FUSELAGE CORRODED B O OTHER O OTHER NRNOT REPORTED 1 SO11233TM 23043 BRACKET AT STA 950 LBL 15 HAS IG CORROSION (LEVEL 2). 2L72 4F RTA16WE 20050310001122005031000112NM 2005 3 10 2005F00026 120050110A5340 SUPPORT BRACKET BOEING737 737282 13844ATNM NLG STEERING CORRODED B O OTHER O OTHER NRNOT REPORTED 1 SO11233TM 23043 SUPPORT BRACKET FOR NOSE STEERING BRACKET PULLEYS AT BS 289 STRINGER 26 L AND 27L --IG CIRROSION (LEVEL 2) 2L72 4F RTA16WE 20050310001142005031000114NM 2005 3 10 2005F00028 120050110A5313 STRINGER BOEING737 737282 13844ATNM FUSELAGE CORRODED B O OTHER O OTHER NRNOT REPORTED 1 SW99233TM 23043 STRINGER 23L AT STA 950 BL 10L HAS IG CORROSION(LEV. 2) 2L72 4F RTA16WE 20050310001152005031000115NM 2005 3 10 2005F00029 120050110A5313 STRINGER BOEING737 737282 13844ATNM FUSELAGE CORRODED B O OTHER O OTHER NRNOT REPORTED 1 SO11233TM 23043 IG CORROSION ON SRTINGER 27L AT STATION 950 LBL5 )LEVEL2) 2L72 4F RTA16WE 20050310001182005031000118NM 2005 3 10 F3LA200500001 120050107A5610NP1653116 WINDSHIELD AIRBUSA319 A319111 3930336NM COCKPIT CRACKED A F3LAA UNSCHED LANDING O OTHER CLCLIMB 1 NM03921FR 2010 AIR TURNBACK, FLIGHT CREW REPORTED RT FWD WINDSHIELD SHATTERED IN FLIGHT AT APPROXIMATELY 20,500 FT MSL. REPLACED RT FWD WINDSHIELD AND PERFORMED TEST ON WINDOW HEAT PER AMM 56-11-11 PB401. 2L72 4F RTA28NM 20050310001192005031000119EU 2005 3 10 DJFA2005047 120050106A2510FG3010 POWER SUPPLY AMD FALC50FALCON50MYST2730106EU COCKPIT BURNED E DJFAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA23590CW 20 CREW REPORTED THAT WHILE ON SHORT FINAL WHILE RETURNING TO KTEB FOR A BLEED AIR OVERHEAT ANNUNCIATOR ILLUMINATING, THE COCKPIT HAD FILLED WITH SMOKE. FLOOR HEAT AND AIR CONDITIONING WAS TURNED OFF. AIRCRAFT LANDED IN KTEB WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FUJITSU, FUJITSU POWER SUPPLY, AND FUJITSU STYLUS DUE TO BEING BURNED. FLUID WAS FOUND TO BE LEAKING ONTO FUJITSU FROM A LEAKING COCKPIT WINDOW. WINDOW SEALS WERE REPLACED. AIRCRAFT WAS RETURNED TO SERVICE. 2L73 4F A46EU 20050308002452005030800245NM 2005 3 8 SWAA050671 120050304A551265C25727 SKIN BOEING737 7375H4 138449DNM HORIZ STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29514SW 25153 DURING SCHEDULED A2 CHECK, FOUND LT HORIZONTAL STAB LOWER SKIN CRACK AT STA 121.9, FWD OF AFT SPAR. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050308002462005030800246NM 2005 3 8 SWAA050672 120050305A3350D71702001 BATTERY BOEING737 7375H4 138449DNM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR EXTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050308002612005030800261 2005 3 8 SWAA050682 420050305A2565D31354 SLIDE BOEING737 7373A4 1384585NM L1 DOOR UNSERVICEABLE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29677AA 23289 DURING SCHEDULED SERVICE CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATING LOW. REMOVED AND REPLACED L1 DOOR SLIDE PER MM. 2L72 4F RTA16WE 20050309000162005030900016NM 2005 3 9 SWAA050688 120050306A53306545780 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29367SW 26578 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR, LOWER CORNER OF CUTOUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050309000232005030900023WP 2005 3 9 UPS05844011 120050222A534037552222 SUPPORT FITTING DOUG DC8 DC873F 302199FWP FLOORBEAM CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE: C1, MAIN CABIN FLOORBEAM FITTING CRACKED AT STA 702 LBL 25 (SUBFLOOR). REMOVED & REPLACED FITTING REF SRM 51-1-20D, 51-1-8, 51-1-11. 2L74 4F RT4A25 20050309000412005030900041WP 2005 3 9 MWEA050024 120050304A335033500025 BATTERY PACK DOUG DC9 DC981 3022081WP EMERGENCY LIGHT INOPERATIVE A MWEAK NONE O OTHER ININSP/MAINT 1 GL31807ME 48033 EMERGENCY CEILING LIGHTING SYSTEM ABOVE SEAT 28 IS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. 2L72 4F A6WE 20050309000432005030900043EA 2005 3 9 COMA0560154 120050302A491038004883 APU CNDAIRCL600 CL6002B19 1900309EA AFT EQUIP SMOKE A COMAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01810CA115431136 7370 FLIGHT 5903 TOILET SMOKE CAUTION MESSAGE AND STRONG OILY SMELL WHEN BLEED SOURCE SWITCHED TO APU. REPLACED THE APU. 2L72 4F RTA21EA 20050309000522005030900052NM 2005 3 9 UPS05443977 120050212A5347BAC15201566 CARGO TRACK BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE:C M/D- BS 480-500 LBL 68 TIE DOWN TRACK O/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.039 X 1 X 2 EXCEED SRM 53-10-01 FIG 1, LIMIT TIE DOWN TRACK REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050309000572005030900057EU 2005 3 9 05FDEA00401 120050307A5511 SPAR AIRBUS310 A310222 3930315EU RT STABILIZER CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 RIGHT STAB REAR SPAR STA 812 HAS 1 INCH OF CORROSION, 1 INCH AT STA 258, 1 INCH AT STA 158. REMOVED CORROSION FOUND OUT OF LIMITS, REPAIRED SPAR IAW SRM 55-11-21. 2L72 4F RTA35EU 20050309000612005030900061NM 2005 3 9 UPS05443982 120050210A5320 INTERCOSTAL BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, INTERCOSTAL BS 1420, LBL 11-33 HEAVY CORRODED. CORROSION BLEND OUT 0.060 X 1 X 1. EXCEED SRM 53-10-01 LIMIT. INTERCOSTAL REPAIRED AS PER SRM 51-40-04 FIG 1. 2L74 4F A20WE 20050309000742005030900074EA 2005 3 9 COMA0560157 120050305A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER N FALSE WARNING APAPPROACH 1 SO01471CA 7655 FLIGHT 5015 FLAP FAILED CAUTION. COULD NOT DUPLCIATE. INSPECTED FLAPS IAW AD 98-20-01, NO DEFECTS FOUND. 2L72 4F RTA21EA 20050309000772005030900077EU 2005 3 9 05FDEA00388 120050306A5313DAN50B04T735411 STRINGER AIRBUS310 A310222 3930315EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 BULK PIT UNDER FLOOR STG 50R FROM 10 INCHES AFT OF FR 64 TO FR 65, 1 INCH INBOARD OF STG TO 2 INCHES OUTBOARD OF STG HAS CORROSION EXTENDING ON AND UNDER BRACKETS AND STG SPLICE. REMOVED CORROSION IAW A310-200 SRM 51-74-10. AREA OUT OF LIMITS IAW A310-200 SRM 53-10-00. REMOVED DAMAGED SECTION IAW A310-200 SRM 53-10-14. TREATED AND PRIMED NEW PARTS IAW A310-200 SRM 53-10-44. INSTALLED NEW PARTS IAW A310-200 SRM 51-40-21. APPLIED TOPCOAT IAW A310-200 SRM 51-21-10. APPLIED FILLET SEAL IAW A310-200 SRM 51-76-00. 2L72 4F RTA35EU 20050309000822005030900082EU 2005 3 9 05FDEA00395 120050307A5347 ATTACH FITTING AIRBUS310 A310222 3930315EU LAVATORY ATTACH CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 LAV-A LOCKDOWN FITTING IS SEVERLY CORRODED REF N000672. REMOVED AND REPLACED LAV-A LOCKDOWN FITTING IAW SRM 51-72-10. 2L72 4F RTA35EU 20050309000832005030900083EU 2005 3 9 05FDEA00396 120050307A7830 THRUST REVERSER AIRBUS310 A310222 3930315EU NR 2 ENGINE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 NR 2 ENG B/B THRUST REVERSER HAS 3 EA AREAS BENT WITH POSS CRACKS 1 X .3 X .020, .3 X .2 X .009 AND .2 X .2 X .050 REF N00251. CLEANED UP DAMAGE IAW P&W JT9D-7R4 SRM 54-30-00. VERIFIED NO CRACKS IAW NTM 51-10-08. 2L72 4F RTA35EU 20050309000882005030900088NM 2005 3 9 UPS05443948 120050210A5320 CHANNEL BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, BS 1294, RBL 55-75 FLOOR SUPPORT U-CHANNEL UPPER FACE CORROSION FOUND CORROSION BLEND OUT 0.035 X 1 X 2 INCH EXCEED SRM 53-10-01 FIG 1, LIMIT. FLOOR SUPPORT U-CHANNEL REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050309000892005030900089NM 2005 3 9 UPS05443949 120050210A5320 CHANNEL BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, BS 1440, RBL 80-99 FLOOR SUPPORT U-CHANNEL ANCHOR NUTS AREA UPPER AND LOWER FACE FOUND CORROSION. CORROSION BLEND OUT 0.045 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1, LIMIT. FLOOR SUPPORT U-CHANNEL REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050309000902005030900090NM 2005 3 9 UPS05443950 120050212A5347 CARGO TRACK BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, BS 440 - 460 LBL 86 TIE DOWN TRACK I/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.044 X 1 X 3 INCH EXCEED SRM 53-10-01 FIG 1, LIMIT. TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A. 2L74 4F A20WE 20050309000932005030900093NM 2005 3 9 UPS05443953 120050208A5340LS48452 ATTACH BRACKET BOEING747 747123 1384873NM FUSLEAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, BS 1020, RBL 75 FLOOR SUPPORT ATTACH BRACKET CORROSION FOUND. CORROSION BLEND OUT 0.030 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1, LIMIT. BRACKET REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050309000962005030900096NM 2005 3 9 UPS05443956 120050209A5320101362409 FLOOR SUPPORT BOEING747 747123 1384873NM FUSLEAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, STN 1094-1100 LBL 75 LONGITUDINAL FLOOR SUPPORT WEB & LOWER CHORD FOUND CRACKED (CRACK LENGTH 3.5 INCH). SUPPORT WEB REPLACED PER SRM 51-10-01 PG 9. LOWER CHORD REPAIRED PER HAECO RS R53-45-35260 & UPS ENG'R FILE 747-53-20227. 2L74 4F A20WE 20050309000982005030900098NM 2005 3 9 UPS05443958 120050209A5347BAC15201567 CARGO TRACK BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, BS 1660, RBL 78 TIE DOWN TRACK I/B FLANGE LWR FACE FOUND CORRODED. CORROSION BLEND OUT 0.035 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1, LIMIT. TIE DOWN TRACK REPAIR AS PER SRM 53-10-05 FIG 1A. 2L74 4F A20WE 20050309001072005030900107EA 2005 3 9 QXEA200500286 120050210A7830 THRUST REVERSER CNDAIRCL600 CL6002C10 1390015EA ZONE 400 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 RT ENGINE TRAILING EDGE BOTTOM INBOARD CASCADE HAS A SMALL SHARP IMPACT GOUGE. REPAIRED IAW CRJ700 SRM 51-12-001-001-001-A01, 54-24-05-101-001-A01 AND 51-25-06-001-001-A01. 2L72 4F RTA21EA 20050309001092005030900109EA 2005 3 9 QXEA200500288 120050211A5753 VANE CNDAIRCL600 CL6002C10 1390015EA ZONE 600 WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 RT WING FLAP VANE PANEL 684ET IS WORN. REPAIRED IAW CRJ700 SRM 57-52-02-101-001-A01, 51-21-11-001-001-A01, 51-25-06-001-001-A01 AND 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050309001112005030900111NM 2005 3 9 UPS05443966 120050208A5347BAC15201873 SEAT TRACK BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, BS 1140 - 1160, RBL 34 TIE DOWN TRACK FLANGE FOUND CRACKED (CRACK LENGTH 2.75 INCH). BS 1070 TO BS 1210 RBL 34 INCH TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 34. 2L74 4F A20WE 20050309001222005030900122WP 2005 3 9 UPS05843935 120050104A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01868UP 45968 INSPECTION TYPE: C, RT WING O/B LEADING EDGE HAS CRACKED UPPER RIB AT STA 776. REMOVED FASTENERS, STOP DRILLED, FABBED AND INSTALLED FILLER IAW DC8 SRM 51-1-21, 57-2-0, 57-3-3 FIG 7, 57-2-0 FIG 2, 51-1-8, AND 51-1-20D. 2L74 4F RT4A25 20050309001272005030900127NM 2005 3 9 UPS05443943 120050214A5347BAC15201566 SEAT TRACK BOEING747 747123 1384873NM FUSLEAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, BS 2060 LBL 70 INCH SEAT TRACK CORROSION FOUND. CORROSION BLEND OUT 0.045 X 1 X 2 EXCEED SRM 53-10-01 FIG 1, LIMIT. SEAT TRACK REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050309001482005030900148EU 2005 3 9 05FDEA00370 120050304A5347 SEAT TRACK AIRBUS310 A310222 3930315EU ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 MAIN DECK CARGO COMP ZONE 146 AT FR 43 BETWEEN SEAT TRACKS R1 AND R2 DUMMY TRACK IS CRACKED. REMOVED AND REPLACED SEAT TRACK IAW A310-200 SRM 51-40-21 AND 51-72-10. 2L72 4F RTA35EU 20050309001772005030900177EA 2005 3 9 QXEA200500280 120050215A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - RIGHTHAND INBOARD SEAT RAIL AT STATION X479 HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW HORIZON AIR EA R-53-273, SECTION I AND REO 670-53-072, REV N/C. 2L72 4F RTA21EA 20050309001842005030900184EA 2005 3 9 COMA0560156 120050305A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01915CA 7013 FLIGHT 5116 FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20050310000592005031000059NM 2005 3 10 LCQ18 120050104A5754 SKIN BOEING737 737 UTILSYSNM SLAT CHAFED B K NONE O OTHER ININSP/MAINT 1 SW15943UA 26680 NR 2 L/E SLAT UPPER T/E LOWER SURFACE CHAFING NEAR ACTUATOR AND O/B END 2L72 4F RTA16WE 20050310001112005031000111NM 2005 3 10 2005F00025 120050110A5340 STRINGER CLIP BOEING737 737282 13844ATNM FUSELAGE CORRODED B O OTHER O OTHER NRNOT REPORTED 1 SO11233TM 23043 STRINGER TIES AT STA 947, STR.26L AND 27L -IG CORROSION (LEVEL 2). 2L72 4F RTA16WE 20050310001132005031000113NM 2005 3 10 2005F00027 120050110A5311 FRAME BOEING737 737282 13844ATNM FUSELAGE CORRODED B O OTHER O OTHER NRNOT REPORTED 1 SO11233TM 23043 IG CORROSION ON FRAME AT BS 285 FROM STRINGER 24L TO STR 28L. 2L72 4F RTA16WE 20050310001532005031000153NM 2005 3 10 C8GA20050001 120050113A291065178444440 LINE BOEING727 727223 1384074NM HYD SYSTEM SPLIT A C8GAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO15899AA56535 22015 AFTER TAKE OFF FROM SAN, "A" HYDRAULIC SYSTEM LOW LEVEL LIGHT ILLUMINATED FOLLOWED BY RAPID QUANTITY DEPLETION. TURNED OFF BOTH THE NR 1 AND 2 HYDRAULIC PUMPS AND RETURNED TO SAN. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. FOUND PRESSURE LINE SPLIT OPEN BETWEEN THE RESEVOIR AND PRESSURE MODULE. REPLACED LINE. OPS CHECK AND LEACK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L73 4F A3WE 20050310001772005031000177EA 2005 3 10 UIA0503 120050226A56001718003 WINDOW DHAV DHC8 DHC8311 1386006EA PWA PW120 PW123 NE PILOT SIDE BROKEN Z O OTHER D INFLIGHT SEPARATION CRCRUISE 1 SW9915233 402 PILOT WINDOW BROKEN AND PARTIALLY SEPARATION IN FILGHT. AFTER LANDING IAW AMM 56-10-16 REPLACED PILOT SIDE WINDOW AND IAW AMM 21-30-00 CHECK NO AIR LEAKING FOUND. 2H72 4T4 TRTA13NM E20NE 20050311000072005031100007GL 2005 3 11 SIMA200503403 220050201A7200AE3007A ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 2 DAMAGED A SIMAO OTHER MJ OVER TEMP WARNING INDICATION CRCRUISE 1 SW21664MS2496 2496 145779 CAE312522 DURING CLIMB AND CRUISE, NR 2 ENGINE HIGH ITT. FOUND CUSTOMER SERVICE MANIFOLD HAD COME OFF ENGINE. REPLACE NR 2 ENGINE ASSY. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20050311000582005031100058 2005 3 11 AMTA200500151 420050206A2565 TRACK BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE GIRT BAR DIRTY A AMTAO OTHER O OTHER CRCRUISE 1 GL11527AT 30886 GIRT BAR LGT EXITING. W/EVAC SLIDE ARMING LEVER IN ARMED POSITION AT SERVICE DOOR R1. FOUND DEBRIS IN GIRT BAR TRACK. REMOVED DEBRIS AND INSPECTED FOR DAMAGE. NO DEFECTS NOTED AND OPS CHECK OK. (K) 2L72 4F4 FRTA2NM E12EU 20050311000602005031100060WP 2005 3 11 O3X02098711 220050210A7200 ENGINE BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP RIGHT SHUTDOWN A O3XAE ENGINE SHUTDOWN O OTHER DEDESCENT 1 SO03871JX 871 AIRCRAFT DEPARTED, ENROUTE, ON DESCENT, AT APPROX 1900 FT, THE RT ENGINE SHUT ITSELF DOWN. THE CREW PERFORMED EMERGENCY PROCEDURES, CLIMBED TO APPROX 6000 FT, AND SUCCESSFULLY RESTARTED THE ENGINE. CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. (K) 2L72 4T4 TRTA56EU E4WE 20050311000662005031100066WP 2005 3 11 AMTA200500061 120050117A2700 PANEL LKHEED1011 10113853 5265020WP RROYCERB211 RB211524B4 54555NE SPOILER DELAMINATED A AMTAA UNSCHED LANDING O OTHER CRCRUISE 1 GL11164AT 1238 NR 2 R SPOILER HAS LARGE DELAMINATION. REMOVED AND REPLACED NR 2R SPOILER PANEL IAW MM. OK FOR SERVICE. (K) 2L73 4F4 F A23WE E12EU 20050311000772005031100077EA 2005 3 11 ASOA05030 120050114A5210601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27849AS 7347 7347 DURING HANGAR MAINTENANCE, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN AT THE ATTACH LINK. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. (K) 2L72 4F4 FRTA21EA E15NE 20050311000872005031100087NM 2005 3 11 LCQ28 120050117A252088549802 SEAT FRAME BOEING737 737 UTILSYSNM CFMINTCFM56 CFM563C1 13802EU CABIN MISMANUFACTURED C K NONE O OTHER ININSP/MAINT 1 SO15944UA 26683 SEAT LEGS ON REWORKED REGENT SEATS, LT AND RT P/N 885498-01, 2 EA. S/N 1068 AND 1322, ALSO P/N 885498-02, S/N'S 1275, 1073, 1070 ARE MIS-PITCHED AND WILL NOT FIT IN SEAT TRACKS. S/O 269003, N/R 23252 2L72 4F4 FRTA16WE E21EU 20050311000942005031100094NM 2005 3 11 GAIA05001ST 120050114A5755659892421 BRACKET BOEING727 727224 1384076NM PWA JT8 JT8D9A 52048NE LT WING CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW0769739 20667 DURING B-CHECK A CRACK WAS FOUND ON THE NR 3 SPOILER ACTUATOR ATTACH BRACKET AT WING STATION 501. REMOVED AND REPLACED SPOILER ACTUATOR ATTACH BRACKET. OPS CHECK AND LEAK CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L73 4F4 F A3WE E2EA 20050308002522005030800252NM 2005 3 8 SWAA050676 120050306A33501010427 COVER BOEING737 7373H4 1384600NM CABIN OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29637SW 27710 EMERGENCY EXIT LIGHT COVER NEAR F/A JUMPSEAT FELL OFF. SECURED LIGHT COVER PER MM. 2L72 4F RTA16WE 20050308002532005030800253NM 2005 3 8 SWAA050677 120050306A3350101114 LENS BOEING737 7375H4 138449DNM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29520SW 25319 LENS MISSING AT AFT GALLEY OVERHEAD EMERGENCY EXIT LIGHT. INSTALLED LIGHT LENS PER MM. 2L72 4F RTA16WE 20050308002632005030800263NM 2005 3 8 SWAA050683 120050306A3350101114 COVER BOEING737 7377H4 1384404NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29413WN 29819 DURING SCHEDULED MV3 CHECK, FOUND EMERGENCY LIGHT COVER CRACKED AT ROW 1 ABC. REMOVED AND REPLACED LIGHT COVER PER MM. 2L72 4F RTA16WE 20050309000132005030900013NM 2005 3 9 SWAA050685 120050305A3350D71702001 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29710SW 27844 DURING SCHEDULED MV2 CHECK, FOUND L1 & R1 DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACKS PER MM. 2L72 4F RTA16WE 20050309000142005030900014NM 2005 3 9 SWAA050686 120050306A532065C35740 WEB BOEING737 7375H4 138449DNM NLG WW CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29507SW 24184 DURING SCHEDULED 1/2D CHECK, FOUND NOSE W/W CEILING CRACKS ON LT & RT SIDE AT BRAKE PAD ATTACH POINT, BS 251.6. REPAIRED NOSE W/W CEILING PER SWA EA. 2L72 4F RTA16WE 20050309000172005030900017NM 2005 3 9 SWAA050689 120050306A5230AND10141 TEE FITTING BOEING737 7373H4 1384600NM CARGO DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29367SW 26578 DURING SCHEDULED 1/4D CHECK, FOUND CRACK ON AFT CARGO DOOR OUTBOARD LOWER TEE FITTING. REMOVED AND REPLACED TEE FITTING PER SRM. 2L72 4F RTA16WE 20050309000182005030900018NM 2005 3 9 SWAA050690 120050306A551265C25727 SKIN BOEING737 7373H4 1384600NM HORIZONTAL STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29367SW 26578 DURING SCHEDULED 1/4D CHECK, FOUND RT HORIZONTAL STABILIZER SKIN CRACKED AT LOWER SURFACE OUTBOARD OF FWD INBOARD BALANCE PANEL. 2L72 4F RTA16WE 20050309000202005030900020NM 2005 3 9 UPS05444027 120050304A3350 CONTROL MODULE BOEING747 747123 1384873NM EMERGENCY LIGHTSINTERMITTENT A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE:N/A EMERGENCY LIGHT CONTROL SWITCH INTERMITTENT FOR EMERGENCY LIGHTS. REMOVED AND REPLACED EMERGENCY LIGHTS CONTROL MODULE AS PER MM 33-51-09, OPS CHECKS OK. 2L74 4F A20WE 20050309000212005030900021WP 2005 3 9 UPS05844009 120050222A5320577327557 FLOOR SUPPORT DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE: C1, MAIN CABIN AFT PRESSURE BULKHEAD VERTICAL STIFFENER TO FLOORBEAM ATTACH FITTING CRACKED, SUBFLOOR LBL 25. FABRICATED REPLACEMENT FITTING REF DWG 5773275 ON SAA TRAVELER 0001. REMOVED & REPLACED FITTING REF SRM 51-1-8, 51-1-20D. 2L74 4F RT4A25 20050309000242005030900024WP 2005 3 9 UPS05844012 120050222A53103779659U501 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE: C1, BATH-TUB FITTING CRACKED ON LONG 4R, STA 902. REMOVED AND REPLACED FITTING REF SRM 51-1-20D. 2L74 4F RT4A25 20050309000252005030900025WP 2005 3 9 UPS05844013 120050219A534037799782 ATTACH FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE: C1, LONGERON ATTACH FITTING CRACKED AT STA 702 LONG 15R. FAB REPLACEMENT FITTING REF DWG3779978 ON SAA SERVICE ORDER 7034926. REMOVED & REPLACED FITTING REF SRM 51-1-20D. 2L74 4F RT4A25 20050309000282005030900028WP 2005 3 9 MWEA050023 120050228A3350 BATTERY DOUG DC9 DC981 3022081WP EMERGNCY LIGHT DISCHARGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31803ME 48029 EMERGENCY CEILING LIGHT VERY DIM. REMOVED AND REPLACED BATTERY IN POWER PACK, OPERATIONS CHECKED GOOD. 2L72 4F A6WE 20050309000292005030900029WP 2005 3 9 UPS05843998 120050222A574037552072 FITTING DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01811UP 46089 INSPECTION TYPE: C2, DURING COMPLIANCE OF EO DC8-5740-2937-E, FOUND CLIP CRACKED ON RT WING NR 3 MAIN TANK STRINGER 70. REMOVED CRACKED FITTING, FABRICATED REPLACEMENT FITTING, REF SAA TRAVE LLER 0001, INSTALLED FITTING, REF SRM 51-1-20D, 51-1-21, DWG3755207. 2L74 4F RT4A25 20050309000302005030900030WP 2005 3 9 UPS05843999 120050219A5312SRO8530007 PRESSURE BLKHD DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01811UP 46089 INSPECTION TYPE: C2, AFT PRESSURE BULKHEAD CRACKED AT APPROX RBL 26 & L12R. REMOVED EXISTING DOUBLER AT SITE. CUT OUT DAMAGE, NDT VERIFIED. FAB 2EA -9 FILLERS -25 DOUBLER, -27 DOUBLER (7075T6-.063), -19 FILLER (SHT7075T6-.090), -11 FILLER (7075T6 -.063). TREAT, PRIME, INSTALL & SEALED ALL REF SRO8530007, SRM51-1-8, MM20-30-00, NDT/SPM06-10-01.001. 2L74 4F RT4A25 20050309000332005030900033NM 2005 3 9 UPS05M44002 120050302A3350 BATTERY PACK DOUG MD11 MD11 3023602NM EMERGENCY LIGHT DISCHARGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01250UP EMERGENCY LIGHT BATTERY LOW LVL 1 ALERT ON BEFORE DEPARTURE AND AFTER LANDING. REMOVED AND REPLACED BATTERY PACK. OPS CHECK GOOD. 2L73 4F RTA22WE 20050309000352005030900035 2005 3 9 SWAA050664 420050304A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29602SW 27953 L2 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED L2 DOOR SLIDE PER MM. 2L72 4F RTA16WE 20050309000382005030900038NM 2005 3 9 SWAA050667 120050306A53246545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 506, STR 16L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050309000402005030900040EA 2005 3 9 COMA0560160 120050303A3230 LANDING GEAR CNDAIRCL600 CL6002B19 1900309EA LACK OF LUBE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01969CA 7141 FLIGHT 4987 GEAR DISAGREE WARNING. COULD NOT DUPLICATE. EXTENSION AND RETRACTION CHECKS WERE SATISFACTORY. CLEAN AND LUBED LANDING GEAR. 2L72 4F RTA21EA 20050309000552005030900055NM 2005 3 9 UPS05443979 120050212A5340 ATTACH ANGLE BOEING747 747123 1384873NM INTERCOSTAL CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, BS 420 RBL 55 INTERCOSTAL WEB ATTACH ANGLE CRACKED (CRACK LENGTH 1 INCH). ANGLE REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050309000622005030900062NM 2005 3 9 UPS05443985 120050210A534769B620491 CARGO TRACK BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, BS 1500, RBL 78 TIE DOWN SUPPORT FITTING CORROSION FOUND. CORROSION BLEND OUT 0.025 X 1 X 1 EXCEED SRM 53-10-01 LIMIT. FITTING REPLACED PER SRM 51-10-01. 2L74 4F A20WE 20050309000712005030900071NM 2005 3 9 UPS05643993 120050301A3350 CONTROL PANEL BOEING767 76734AF 1385212NM EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01315UP 27743 EMERGENCY LIGHT SWITCH PANEL ANNUNCIATOR DOES NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHT CONTROL PANEL AND PERFORMED CHECK OK IAW 33-51-08. 2L72 4F RTA1NM 20050309000762005030900076EU 2005 3 9 05FDEA00387 120050306A5320A2577166600600 CROSSBEAM AIRBUS310 A310222 3930315EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 FWD CARGO BETWEEN RT ROLLER TRACKS NR 1 AND NR 2, 4TH CROSS BEAM AFT HAS 3 INCHES OF CORROSION. REMOVED CORROSION FROM CROSS BEAM BETWEEN NR 1 AND NR 2 ROLLER TRACKS ON RT SIDE IAW A310-200 SRM 51-74-10, OUT OF LIMITS ON CORROSION REMOVAL IAW A310-200 SRM 53-10-00. REMOVED OLD CROSS BEAM AND INSTALLED NEW CROSS BEAM IAW A310-200 SRM 51-42-00. 2L72 4F RTA35EU 20050309000812005030900081NM 2005 3 9 05FDEA00394 120050307A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA Y= 5-90, X= 8.5 FOUND WITH CORROSION. REMOVED AT EXISTING SPLICE PER SRM 51-33-01 VOLUME II. REWORKED SEAT TRACK INSTALLED PER SRM 53-70-00 VOLUME I, FIGURE 1. 2L73 4F RTA22WE 20050309000922005030900092NM 2005 3 9 UPS05443952 120050210A5320 FLOOR SUPPORT BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, STA 1330, LBL 65 FLOOR SUPPORT SURFACE CORROSION. CORROSION BLEND OUT 0.035 X 1 X 2 INCH EXCEED SRM 53-10-01 FIG 1, LIMIT. FLOOR SUPPORT REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050309000972005030900097NM 2005 3 9 UPS05443957 120050210A5347BAC15201566 SEAT TRACK BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE:C M/D- BS 1580 TO 1600 LBL 98 SEAT TRACK CRACKED (CRACK LENGTH 1 INCH). SEAT TRACK REPAIRED FROM BS 1570 TO BS 1630 LBL 98 AS PER SRM 53-10-05 FIG 1A. 2L74 4F A20WE 20050309001022005030900102NM 2005 3 9 UPS05443962 120050210A5347BAC15201566 SEAT TRACK BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE:C, BS 1580-1600 LBL 33 SEAT TRACK FLANGE CORROSION FOUND. CORROSION BLEND OUT 0.045 X 1 X 2 INCH EXCEED SRM 53-10-01 FIG 1, LIMIT. TIE DOWN TRACK REPLACED AT BS 1480 TO BS 1600 LBL 33 AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050309001172005030900117EU 2005 3 9 05FDEA00398 120050307A5410 RIB AIRBUS310 A310222 3930315EU NR 1 PYLON CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 NR 1 PYLON 1 INCH AFT OF RIB 19 I/B SIDE WEB ATTACH POINT HAS A .5 INCH CRACK REF N00647. REMOVED AND REPLACED WEB AT RIB 19 IAW SRM 51-40-21 & 51-72-10. 2L72 4F RTA35EU 20050309001192005030900119WP 2005 3 9 05FDEA00355 120050303A5730ARC0269 PANEL DOUG MD10 MD1010F 3022112WP ZONE 500 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25361FE 48260 LT WING, LOWER TRAILING EDGE PANEL OVER LEFT MAIN LANDING GEAR IS DENTED AND PUNCTURED. REPAIRED PANEL ARC0269 IAW EA 8-5710-8393, WINGS - LT HAND MLG FITTING TO FUSELAGE AFT UPPER PANEL - REPAIR. 2L73 4F RTA22WE 20050309001202005030900120WP 2005 3 9 05FDEA00356 120050303A78309690M05G02 THRUST REVERSER DOUG DC10 DC1010F 3022111WP ZONE 500 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25369FE 46607 COMPLY WITH EA 8-7830-55453 TITLE EXHAUST THRUST REVERSER - REWORK OF GOUGE ON T/R SUPPORT FITTING. COMPLIED WITH EA 8-7830-55453. 2L73 4F A22WE 20050309001242005030900124NM 2005 3 9 UPS05443940 120050212A5347BAC15201567 CARGO TRACK BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE: C, BS 160 - 180 RBL 13 TIE DOWN TRACK I/B FLANGE & LIP FOUND CORRODED. CORROSION BLEND OUT 0.040 X .5 X 3 INCH EXCEED SRM 53-10-01 FIG 1, LIMIT. TIE DOWN TRACK REPLACED AS PER SRM 51-10-01 PG 1. 2L74 4F A20WE 20050309001252005030900125NM 2005 3 9 UPS05443941 120050211A5347BAC15201566 CARGO TRACK BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE:C M/D- BS 355 - 360, RBL 72, TIE DOWN TRACK FLANGE FOUND CORROSION CRACK (CRACK LENGTH 1 INCH). TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A. 2L74 4F A20WE 20050309001452005030900145EA 2005 3 9 COMA0560150 120050301A5200 DOOR CNDAIRCL600 CL6002B19 1900309EA OXYGEN SERVICE OPEN A COMAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 SO01805CA 7354 FLIGHT 5554 LOUD SQUEAL FROM NOSE AREA OF AIRCRAFT. FOUND 02 SERVICE DOOR OPEN. INSPECTED FOR DAMAGE AND CLOSED 02 SERVICE DOOR. 2L72 4F RTA21EA 20050309001462005030900146EU 2005 3 9 05FDEA00361 120050304A5347A5361164020001 SEAT TRACK AIRBUS310 A310222 3930315EU ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 MDCC NR 2 SEAT TRACK LEFT OF CENTER LINE FROM FRAME 15 TO FR 19 HAS HEAVY CORROSION. REMOVED NR 2 SEAT TRACK, SPLICE AND COUPLING IAW A310-200 SRM 51-40-21. LOCATED AND DRILLED NEW SEAT TRACK, SPLICE AND COUPLING IAW A310-200 SRM 51-40-44. INSTALLED NEW SEAT TRACK, SPLICE AND COUPLING IAW A310-200 SRM 51-40-21. 2L72 4F RTA35EU 20050309001512005030900151NM 2005 3 9 AWXA200500295 120050123A5315654681138 FLOORBEAM BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND LOWER SURFACE OF TRANVERSE FLOORBEAM T-CAP AT BS 986, BETWEEN RBL 40 AND RBL 44, WL 208. MAINTENANCE REMOVED CORRODED FLOORBEAM T-CAP AT BS 986 FROM RBL 0 TO RBL 50; FABRICATED A NEW REPLACEMENT SECTION OF T-CAP, 2 EACH SUPPORT ANGLES & STRAPS; INSTALLED REPAIR PARTS IAW ER 03-5310-05040-SS1. 2L72 4F RTA16WE 20050309001562005030900156NM 2005 3 9 AWXA200500300 120050125A2560P2070003001 FLASHLIGHT BOEING737 737301 1384611NM ZONE 900 INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - EMERGENCY EQUIPMENT - DURING C-18 CHECK FOUND THE LT AFT LAVATORY WALL EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LT AFT LAVATORY WALL EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050309001622005030900162WP 2005 3 9 UPS05844017 120050219A575356431174 WEB DOUG DC8 DC873F 302199FWP LT WING TE FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE: C1, VERTICAL WEB CRACKED IN LT FLAP COVE FWD OF, AND BELOW XW3 FLAP HINGE FITTING. STOP DRILLED CRACK. NDT VERIFIED. FAB REPAIR DOUBLER FROM SHT7075T6-.071. TREAT, PRIME, INSTALL REPAIR REF DWG5643117, NDT/SPM06-10-01.001, SRM 53-2-0 FIG 1D, 51-1-8, 51-1-21, 51-1-20D. 2L74 4F RT4A25 20050309001642005030900164WP 2005 3 9 UPS05844020 120050221A534047516262 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE: C1, ATTACH FITTING CRACKED ON LONG 11R STA 680. FAB REPLACEMENT FITTING FROM 7075 T6 PLATE ON SAA SERVICE ORDER 7034927. REMOVED AND REPLACED FITTING REF SRM 51-3-0, 51-1-21. 2L74 4F RT4A25 20050309001732005030900173NM 2005 3 9 UPS05444005 120050208A534065B172222 SUPPORT FITTING BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE:C M/D BS 1000 RBL 11 SEAT TRACK END SUPPORT FITTING FOUND CRACKED. SUPPORT FITTING REPLACED PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050309001812005030900181EA 2005 3 9 QXEA200500274 120050210A5280 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 700 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - RIGHTHAND MAIN LANDING GEAR, LOWER DOOR LOOSE RIVETS NEAR FORWARD HINGE, OUTBOARD SKIN. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20050309001822005030900182EA 2005 3 9 COMA0560155 120050302A8097 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA STARTER CONTAMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01716CA 7250 FLIGHT 5747 NO STARTER CUTOUT MESSAGE. CLEANED OIL FROM STARTER WIRING CONNECTOR. 2L72 4F RTA21EA 20050309001862005030900186EA 2005 3 9 COMA0570023 120050306A5270 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA E/E BAY DOOR FALSE INDICATIONA COMAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01369CA 10079 FLIGHT 5756 AVIONICS DOOR CAUTION. COULD NOT DUPLICATE. OPERATIONAL CHECK SATISFACTORY. 2L72 4F RTA21EA 20050309001872005030900187EA 2005 3 9 SWIA200514566 120050209A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAO OTHER O OTHER ININSP/MAINT 1 NM07463SW 7820 FLOORBEAM ANGLE CRACKED AT FS 621.00 LBL 41.0. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FLOOR SUPPORT ANGLE IAW CRJ REO 601R-53-61-117 REV B. 2L72 4F RTA21EA 20050309001882005030900188WP 2005 3 9 CALA0500057 120050120A5320991007813 CUSP WEB DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2735836 49441 INSPECTION FOUND RT CUSP CORRODED AT STA 200. A SMALL SECTION OF THE UPPER CUSP CHORD WAS TRIMMED OUT TO REMOVE LOCAL CORROSION AND A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5311-01216. 2L72 4F A6WE 20050309001892005030900189EA 2005 3 9 SWIA200514610 120050217A274070609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07929SW2786 2786 7703 STAB TRIM CH1 DISENGAGED DURING FLIGHT. REMOVED AND REPLACED HSTCU IAW CRJ 200 MM 27-41-00, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050309001902005030900190EA 2005 3 9 SWIA200514611 120050217A3350 CHARGER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07464SW 7827 EMERGENCY EXIT SIGN LOCATED ON LEFT WARDROBE INOPERATIVE. REPLACED LIGHT ASSY IAW AMM 33-51-19. REPLACED CHARGER IAW AMM 33-51-05. REPLACED BATTERY IAW AMM 33-51-04. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050309001922005030900192EU 2005 3 9 05FDEA00245 120050205A5270 WARNING LIGHT AIRBUS300 A300B4622 3930401EU CARGO DOOR ILLUMINATED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25716FD 358 MADE T/O WITH T/O CONFIG TEST SW SHOWING MAIN DECK DOOR NOT CLOSED PER MEL MX HAD VERIFIED ALL DOORS CLOSED & LOCKED AND DOORS ON ECAM WERE INDICATING CLOSED AND LOCKED. ON CLIMBOUT AT APPROX 4 PSI & 13,000 FT MSL MAIN CARGO DECK LIGHT ON ECAM WENT AMBER. NO CHANGE IN PRESSURE AND RIGHT ECAM DOOR PAGE VERIFIED AMBER LIGHT MAIN CARGO DOOR. EMERGENCY RETURN TO KOAK AND ECAM LIGHT WENT OUT ON LANDING. LANDING WEIGHT 327.3 DESCENT RATE= 220FT/MIN. HEAVY LANDING INSPECTION / WRI 05-50/2169. ALL SYSTEMS NORMAL. 2L72 4F RTA35EU 20050309001972005030900197NM 2005 3 9 DL73S050111 120050213A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27305DL 23077 THE FUSELAGE SKIN WAS FOUND WITH A CRACK AT FS 764 RUNNING ALONG THE BONDED DOUBLER MILL LINE JUST ABOVE STRINGER 19L. THE CRACK IS TYPICAL OF AD 2004-18-06. THE CRACK WAS REMOVED WITH A CUT OUT IN THE SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER B737 SRM AND PER ER/A 096925-14AD. 2L72 4F RTA16WE 20050309001982005030900198NM 2005 3 9 DL764050112 120050215A25301105011 COFFEEMAKER BOEING767 767432ER 1385134NM FWD GALLEY FAILED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27841MH 29714 FWD GALLEY NR 1 COFFEEMAKER C/B POPPED. REPLACED COFFEEMAKER WIRING AND CONNECTOR FOR REPORTED SPARKS. 2L72 4F RTA1NM 20050310000602005031000060NM 2005 3 10 LCQ19 120050104A5330 SKIN BOEING737 737 UTILSYSNM FUSELAGE GOUGED B K NONE O OTHER ININSP/MAINT 1 SW15943UA 26680 LWR EXT. OF FUSELAGE AT STA. 727 ON KEEL BEAM, BL5R HAS 4 INCH LONG GOUGE. 2L72 4F RTA16WE 20050310001042005031000104NE 2005 3 10 XN0A1220 220050106A7200 ENGINE AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE NR 1 MALFUNCTIONED A XN0AD RETURN TO BLOCK RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TXTAXI/GRND HDL 1 GL23224KW 073 AFTER ENG START ENG NR 1 REMAINED IN FLT IDLE. TRANSFERRED TO DMI 5011 PER MEL 73-30-02. CATC PLACARDS INSTALLED. (STATUS:ORIG/OPEN) 2L72 4F4 FRTA35EU E23EA 20050607000172005060700017EA 2005 6 7 QXEA200500881 120050428A5751 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 500 LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - LEFT WING UPPER SURFACE TRAILING EDGE SKIN HAS LOOSE FASTENERS AT OUTBOARD OF MULTI-FUNCTION SPOILER. REPAIRED IAW CRJ-700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20050311000912005031100091EA 2005 3 11 ASOA05019 120050107A3350601R461041 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN MISSING A ASOAK NONE O OTHER ININSP/MAINT 1 SO27922EV 7822 DURING A HANGAR CHECK, SEVERAL SECTIONS OF THE EMERGENCY FLOOR LIGHT STRIP WERE FOUND MISSING. MAINTENANCE INSTALLED EMERGENCY FLOOR LIGHTING STRIPS IN THE MISSING SECTION. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050314000052005031400005EU 2005 3 14 S9HA099271 120050210A7931704A37642043 TRANSMITTER AEROSPAS355 AS355* EU TMECA ARRIELARRIEL1 60030NE ENGINE OIL SYS DEFECTIVE E S9HAO OTHER P NO WARNING INDICATION NRNOT REPORTED 1 WP19352NT17 2553 NO OIL PRESSURE INDICATION AT START. ENGINE PRESSURE LIGHT NOT ILLUMINATED. REPLACED TRANSMITTER WITH NEW TRANSMITTER. CHECK GOOD. 1G72 3U3 U H11EU E19EU 20050314000072005031400007NE 2005 3 14 TXER099314 220050128A7261365A53801303 OIL TANK UROCOPEC155 EC155B 8681000EU TMECA ARRIELARRIEL2B NE ENGINE OIL LEAKING B TXERO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 SW09155EW 6660 OIL TANK LEAKING FROM SIGHT GLASS. 1G72 3U3 U H10EU E00054EN 20050314000102005031400010CE 2005 3 14 HYTA2005005 120050218A3710RV05268 RELIEF VALVE CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE VACUUM SYSTEM MALFUNCTIONED E HYTAK NONE O OTHER ININSP/MAINT 1 AL01900WA8110 208B0659 INSTRUMENT VACUUM SYSTEM HAD INSUFFICIENT SUCTION. ADJUSTING THE VACUUM REGULATOR HAD NO EFFECT. LOOKING THROUGH THE VACUUM EJECTOR OUTLET REVEALED A FOREIGN OBJECT RESTRICTING THE VENTURI. AN 8-32 NUT WAS RETRIEVED FROM THE VENTURI. THIS NUT CAME FROM INSIDE THE BLEED AIR RELIEF VALVE, PN RV05-268, WHICH IS MOUNTED ADJACENT TO THE INLET SIDE OF THE VENTURI. THIS NUT IS USED AS A JAM NUT TO SECURE THE RELIEF VALVE PRESSURE SETTING. SUGGEST THIS NUT COULD BE SECURED WITH LOCKTITE OR OTHER THREAD LOCKER. (K) 1H71 3T3 T A37CE E4EA 20050314000112005031400011EA 2005 3 14 A6WA200540037 120050131A5730 ACCESS PANEL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT WING CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31412AW 7582 LT WING PLANK HAS CORROSION UNDER THE FOLLOWING FUEL TANK PANELS 550BB, 540ED, 540BB, 510AB. REMOVED MINOR CORROSION FROM LT WING LOWER PLANK AT FUEL ACCESS PANELS 550BB, 540FB, 540EB, 540BB AND 510AB IAW MFG REO 601R-57-21-030 REV C. (M) 2L72 4F4 FRTA21EA E15NE 20050314000122005031400012SO 2005 3 14 BSYA200500004 120050302A3233WTC21151 ACTUATOR PIPER PA31 PA31P350 7103111SO LYC O540 TIO540J2BD 41532EA LT MLG BROKEN E BSYAL ABORTED APPROACH J WARNING INDICATION LDLANDING 1 GL0742HD 8152031 AIRCRAFT TOOK OFF, PILOT NOTICED LANDING GEAR HANDLE NOT RETURNING TO NEUTRAL AND THAT THE AC WAS YAWING. ON APPROACH, COULD NOT GET LT GEAR DOWN AND LOCK LIGHT, C/W MISSED APPROACH, THEN FINALLY GOT LT GEAR DOWN AND LOCK LIGHT, LANDED WITH NO PROBLEMS. MAINTENANCE FOUND LT GEAR ACTUATOR BROKEN. REMOVED AND REPLACED LT GEAR ACTUATOR. 1L72 3O3 ORTA8EA E14EA 20050314000142005031400014NM 2005 3 14 AMT2005F00001 120050213A2613 WARNING LIGHT BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE LT ENGINE ILLUMINATED A AMTAE ENGINE SHUTDOWN MJ OVER TEMP WARNING INDICATION CRCRUISE 1 GL11557TZ 32591 LT ENGINE OVERHEAT EICAS CAME ON AT CRUISE, ALT (40000) PERFORMED FIM 26-12-00, FIG 103, FOUND NO DEFECTS. RAN ENGINE TO HIGH POWER SETTING WITH NO DEFECTS. OPERATIONAL CHECK NORMAL. (GL11200507753) (K) 2L72 4F4 FRTA2NM E12EU 20050314000152005031400015 2005 3 14 BB05014 420050311A2565 GIRT BAR BOEING757 7572B7 1384964NM RROYCERB211 RB211535E4 54555NE L4 DOOR SLIDE OBSTRUCTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19610AU 761 27122 THE L4 DOOR WOULD NOT ARM PROPERLY. MAINTENANCE RESTOWED THE SLIDE PACK WHICH WAS OBSTRUCTING THE GIRT LINKAGE. 2L72 4F4 FRTA2NM E12EU 20050314000162005031400016EA 2005 3 14 RNV2005F00000 220050119A7261 DRIVE SHAFT CESSNA208 208B 2073701CE PWA PT6 PT6* 52043EA SCAVANGE PUMP SHEARED E RNVAO OTHER J WARNING INDICATION CRCRUISE 1 WP13305PW 208B0828 ACCESSORY DRIVE SHAFT ON THE EXTERNAL SCAVANGE PUMP SHEARED, RESULTING IN A LOSS OF OIL PRESSURE. PILOT DIVERTED THE FLIGHT. AIRCRAFT COMPONENTS OR SYSTEMS THAT RESULT IN TAKING EMERGENCY ACTIONS DURING FLIGHT (EXCEPT ACTION TO SHUTDOWN AN ENGINE). 1H71 3T3 T A37CE E2NE 20050314000182005031400018NE 2005 3 14 Z1RA099008 120050119A2497 WIRE SKRSKYS76 S76C 8143008NE AC GENERATOR CHAFED E Z1RAK NONE S AFFECT SYSTEMS ININSP/MAINT 1 SW11760AF2368 099 760523 AC GENERATOR WILL NOT COME ON LINE DURING TEST, WIRES CHAFED IN BOX ASSY. REPLACED WITH OVERHAULED ITEM (P/N 90320-1, S/N 010) RETURNED TO SERVICE. 1G72 3U NCH1NE 20050314000202005031400020NM 2005 3 14 P9RA20050069 120050217A33508100022601 LIGHT BOEING757 757236 1384971NM RROYCERB211 RB211535E4 54555NE ROW 3-8 INOPERATIVE A P9RAK NONE L NO TEST ININSP/MAINT 1 SO11958PG 24118 AC IN MAINTENANCE CVG. FLOOR EMERGENCY LIGHTING BETWEEN ROWS 3-8 INOPERATIVE. REMOVED AND REPLACED LIGHT ASSY. IAW MM. 2L72 4F4 FRTA2NM E12EU 20050314000222005031400022SO 2005 3 14 1304021605 120050216A3250 STEERING SYS GULSTMG1159 GIV 3980115SO RROYCETAY TAY6118 EU NLG MALFUNCTIONED E N93AO OTHER O OTHER TXTAXI/GRND HDL 1 SO13404QS 1304 NOSE WHEEL STEERING PULLING TO LT ON TAXI. 2L72 4F4 FRTA12EA E25NE 20050314000252005031400025NM 2005 3 14 MWEA050026 120050309A5230 DOOR BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE ACCESS COMP OPEN A MWEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31914ME 55177 LEVEL ONE ALERT FOR ACCESS COMPARTMENT DOOR. FASTENED 1 FORWARD ACCESS COMPARTMENT DOOR, HINGED LATCH FOR SENSOR. 2L72 4F4 FTRA6WE E00061EN 20050314000262005031400026NM 2005 3 14 WRLA2005083 120050310A2710KCLD4N RELAY DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE AILERON CONTROL INOPERATIVE A WRLAJA DUMP FUEL UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO11274 48633 ITEM: CI217/10 ANC/TPE AIR TURNBACK DUE TO LEVEL II (AIR DEFLECT DISAG), DUMPED FUEL AND RETURNED TO BASE. REPLACED AILERON DEFLECT CONTROL RELAY R2-5060. RTS FCC 1 AND 2 ALL PASSED. RAN AILERON TO FULL DEFLECT AND CYCLED FLAPS, ALL CHECKS NORMAL. 2L73 4F4 FRTA22WE E24NE 20050314000272005031400027NE 2005 3 14 T48R200500001 220050304A7261318486 BEARING PWA DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE SCAVENGE PUMPSCAFAILED B GTIAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL09814NK 49619 716719 ENGINE WAS REMOVED FROM AC, NR1 POSITION FOR REPORTED LOSS OF OIL QUANTITY IN FLIGHT. THE ENGINE WAS SHUTDOWN IN-FLIGHT. INCOMING INSPECTION REVEALED OIL IN THE TAILPIPE AND TURBINE AREA. DISASSEMBLY REVEALED A FAILED BEARING IN THE NR 4 AND NR 5 SCAVENGE PUMP, RESULTING IN OIL PUMP SEIZURE AND LOSS OF OIL SCAVENGING ABILITY. THE PUMP AND BEARING TIME, TIME SINCE OVERHAUL IS UNKNOWN. 2L72 4F4 FRTA6WE E9NE 20050314000502005031400050EA 2005 3 14 UIA0501 120050123A242051608003 GCU DHAV DHC8 DHC8311 1386006EA PWA PW120 PW123 NE RT GENERATOR MALFUNCTIONED Z C ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA0015225 405 DURING TAKEOFF (R AC BUSS) CAUTION LIGHT ON, A/C ABORTED TAKEOFF. CHECK FOUND RT GCU MALFUNCTIONED, IAW AMM 24-21-01 REPLACED THE GCU AND ENG RUNUP CHECK AC SYSTEM BACK NORMAL. 2H72 4T4 TRTA13NM E20NE 20050314000612005031400061 2005 3 14 UIA0502 420050202A23123094329 SWITCH DOUG MD90 MD9030 3023690NM IAE V2525 V2525D5 NE RT CONTROL COLUMJAMMED Z A UNSCHED LANDING G MULTIPLE FAILURE CRCRUISE 1 SW991791910412 53569 IN FLT RADIO COMMUNICATION FAILURE (VHF NR 1 AND NR 2). AC AIR TURN BACK. MAINTENANCE CHECK FOUND RT CONTROL COLUMN PTT SW FUNCTION NO T GOOD. CAUSED RADIO SYSTEM FAILURE. IAW AMM23-51-07 REPLACED RT CONTROL COLUMN PTT SW AND OPERATIOAL TEST SYSTEM BACK, NORMAL. 2L72 4F4 FRTA6WE A40NE 20050309001502005030900150NM 2005 3 9 AWXA200500294 120050127A53206517684642 INTERCOSTAL BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK 2 EACH .0625 INCH CRACKS WERE FOUND IN L-1 DOOR FORWARD FRAME INTERCOSTAL WEB BS 294.5, STR 7 LT. MAINTENANCE REMOVED DAMAGED L-1 DOOR FORWARD FRAME INTERCOSTAL WEB FROM BS 294.5 TO BS 303.9; FABRICATED A NEW REPLACEMENT INTERCOSTAL WEB PER DWG 65-17684; INSTALLED REPAIR PART IAW ER 03-5310-05040-SS2. 2L72 4F RTA16WE 20050309001572005030900157NM 2005 3 9 AWXA200500301 120050125A52106545871123 SKIN BOEING737 737301 1384611NM R1 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK A .3125 INCH CRACK WAS FOUND IN R-1 DOOR EXTERNAL SKIN EMANATING FASTENER HOLE AT LOWER HINGE CUTOUT BS 328, STR 15-16 RT. MAINTENANCE REMOVED EXISTING DOUBLER AND CUT OUT CRACK IN R-1 DOOR EXTERNAL SKIN; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW ER 03-5200-05090-RA5. 2L72 4F RTA16WE 20050309001582005030900158NM 2005 3 9 DHL2005781503 120050216A5754 SKIN BOEING727 727227 1384078NM SLAT GOUGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A C-CHECK, ACCOMPLISH INDENTIFICATION OF EXISTING REPAIR ON LT WING NR 4 SLAT SKIN, WS 436, PER ASTAR J/C FCD 500001-018-B. REMOVED PREVIOUS REPAIR WITH NON-COMPLIANT PER SRM AT LT WING NR 4 SLAT SKIN WS 434 IAW B727 SRM 51-30-2. FABRICATED NEW REPAIR MAT'L USED 2024 T3 .080 PO 900811 DIM 3.8750 X 5.8750 IAW B727 SRM 57-50-3 FIG 1. ALODINED AND PRIMED PART AND AREA IAW B727 SRM 51-10-2. INSTALLED DOUBLER REPAIR IAW B727 SRM 57-50-3 FIG 1. 2L73 4F A3WE 20050309001602005030900160WP 2005 3 9 UPS05844015 120050220A5312REFSRO8530007 PRESSURE BLKHD DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE: C1, AFT PRESSURE BULKHEAD CRACKED AT LBL 35 NEAR LONG 11L. REMOVED EXISTING REPAIR AT SITE. CUT OUT DAMAGE. NDT VERIFIED. FAB-27 DOUBLER (SHT7075T6-.063), -25 DOUBLER (7075T6-.032), -9 FILLERS (7075T6-.050). TREAT, PRIME & INSTALL REPAIR REF SRO8530007. 2L74 4F RT4A25 20050309001692005030900169NM 2005 3 9 UPS05443994 120050205A571265B101416 RIB BOEING747 747123 1384873NM RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 INSPECTION TYPE:C RIGHT WING 20VC FLAP I/B ARM O/B RIB I/B FACE AT ROTARY ACTUATOR AFT AREA FOUND CRACKED, CRACK LENGTH .5 INCH. RIGHT WING 20VC FLAP I/B ARM O/B RIB I/B FACE REPAIRED AS PER HX RS R57-41-35254 WITH CRACKED AREA TRIMMED OFF & INSPECTED BY NDT. NO CRACK FOUND & EO B747-5740-21781-A. 2L74 4F A20WE 20050309001942005030900194EU 2005 3 9 MALA050183 120050210A3350501171202 POWER SUPPLY SAAB SF340 SF340A 7850100EU EMERGENCY LIGHT FAILED A MALAK NONE O OTHER ININSP/MAINT 1 GL1599XJ 340A099 EMERGENCY POWER SUPPLY P/N 501-1712-02, S/N 1616 FAILED SCHEDULED CAPACITY CHECK. REPLACED 2 EACH CELL PACKS P/N 549-1324-06. UNIT PASSES CMM CHECKS, RTS 2/20/05. 2L72 4T RTA52EU 20050309001962005030900196NM 2005 3 9 QXEA200500223 120050211A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09365PH 526 PDX - RIGHTHAND INBOARD SEAT TRACK IS CORRODED AT X217 TO X237. REPAIRED IAW RD 8-53-4473 AND DHC-8/200 SRM 51-40-11. 2H72 4T RTA13NM 20050310001032005031000103NM 2005 3 10 ASMF200501002 120050105A2751 CONTROL UNIT BOEING737 737 UTILSYSNM TE FLAPS MALFUNCTIONED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23904AM 28262 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF FLAPS INDICATION OUT OF SERVICE. FSEU TEST WAS PERFORMED AND CIRCUIT BREAKERS P6-2 A8 AND A9 WERE RESEATED AND FAIL CONTINUE. FSEU WAS TESTED AGAIN IAW MM 27-51-01, ALL CORRECT. 2L72 4F RTA16WE 20050310001162005031000116WP 2005 3 10 5002 220050106A731430708507 PUMP LEAR 35 35A 5170602CE GARRTTTFE731TFE73122B 01518WP FUEL SYSTEM DEFECTIVE E BSYAD RETURN TO BLOCK RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TXTAXI/GRND HDL 1 GL0798LC 077 P74505 TAXING OUT FOR TAKEOFF RIGHT ENGINE STARTED TO DYE, RETURNED TO FBO ON THE WAY BACK ENGINE DIED AND THEY COULD NOT RELIGHT, REMOVED AND REPLACED DEFECTIVE FUEL PUMP AND CONTAMINATED FUEL CONTROL OPS. CHECKS GOOD. 2L72 4F4 F A10CE E6WE 20050310001752005031000175NM 2005 3 10 LCQ27 120050117A251088549801 SEAT FRAME BOEING737 737 UTILSYSNM CFMINTCFM56 CFM563C1 13802EU CABIN MISMANUFACTURED C K NONE O OTHER ININSP/MAINT 1 SO15944UA 26683 SEAT LEGS ON REWORKED REGENT SEATS, LT AND RT P/N 885498-01, 2 EA. S/N 1068 AND 1322, ALSO P/N 885498-02, S/N'S 1275, 1073 AND 1070 ARE MIS-PITCHED AND WILL NOT FIT IN SEAT TRACKS. S/O 269003, NR 23252 2L72 4F4 FRTA16WE E21EU 20050311000452005031100045EU 2005 3 11 BMAC05001 120050110A56101379628C403 WINDSCREEN BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110UG 01514WP COCKPIT CRACKED A B16AA UNSCHED LANDING O OTHER CLCLIMB 1 NE05538PA 751 PILOT REPORTED: DURING CLIMB OUT, (W/S) CAPTION APPEARED FOR THE RT WINDSCREEN. UPON FURTHER INSPECTION NOTICED CRACKS IN THE UPPER PORTION OF THE WINDSCREEN. CREW DECIDED TO RETURN TO DEPARTURE. REPLACED RT WINDSCREEN DUE TO CRACKING OF OUTER PANE. (K) 2L72 4T4 TRTA21EU E4WE 20050315000032005031500003CE 2005 3 15 DJFA2005065 120050310A2131 CONTROLLER RAYTHNDH125 HAWKER800XP 7150012CE CABIN PRESSURE MALFUNCTIONED E DJFAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 EA23893CW 258603 CREW REPORTED THAT WHILE CLIMBING FROM 35,000 TO 36,000 FT, HEARD A LOUD POP FROM THE REAR OF THE AIRCRAFT FOLLOWED BY A HIGH RATE OF CLIMB ON THE CABIN CONTROLLER. OXYGEN MASKS WERE DONNED AND AN EMERGENCY DESCENT WAS INITIATED. THE AIRCRAFT CABIN ALTITUDE ALERTER WENT OFF WHILE IN DESCENT. AN EMERGENCY WAS DECLARED AND A DIVERSION WAS MADE TO KTPA WHERE AN UNEVENTFUL LANDING WAS MADE. MAINTENANCE FOUND A BLOWN DUCT ON THE WATER SEPARATOR OUTLET. THE DUCT WAS RESECURED AND A CABIN LEAK RATE TEST WAS PERFORMED ALONG WITH A FUNCTIONAL CHECK OF THE PRESSURIZATION SYSTEM. NO DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA3EU 20050315000112005031500011NM 2005 3 15 EIA2005004 120050219A5313 STRINGER BOEING747 747212B 1384886NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 CORROSION UNDER STR 47 DOUBLER LT SIDE. REMOVED CORROSION PER SRM 51-10-01 BLENDED AREA FOUND TO BE WITHIN LIMITS PER 747 SRM 53-30-02 AND 53-30-01 FIG 1. 2L74 4F A20WE 20050315000152005031500015NM 2005 3 15 DL76L050131 120050224A5753113T1226 SUPPORT BEAM BOEING767 767332 1382001NM NR 2 FLAP CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27179DN 25144 COMPLIED WITH REPAIR NR 1 OF ERA 089397-14MA REV C ON LEFT INBOARD FLAP DUE TO CORROSION IN ATTACH FASTENER HOLES. 2L72 4F RTA1NM 20050315000162005031500016NM 2005 3 15 DLM88050132 120050225A2741 GEARBOX DOUG MD88 MD88 3023688NM STAB TRIM MALFUNCTIONED A DALAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO27920DL 49644 PRIMARY TRIM NOSE DOWN WOULD NOT WORK ON CLIMBOUT. ALT TRIM FUNCTIONED PROPERLY. REPLACED GEARBOX AND TRIM MOTORS. 2L72 4F RTA6WE 20050315000172005031500017NM 2005 3 15 DL76G050133 120050225A351080130700 BOTTLE BOEING767 767332 1382001NM OXYGEN SYSTEM DISCHARGED A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO271610D 30594 CREW OXYGEN PRESS INDICATED ZERO ON EICAS EN ROUTE TO ATL. DIVERTED TO SJU. REMOVED AND REPLACED CREW O2 BOTTLE. LEAK CHECK GOOD. MAINTAINED PRESSURE. OKAY FOR SERVICE. INSPECTED MASKS AT ALL 4 STATIONS, CHECKS OK. 2L72 4F RTA1NM 20050315000222005031500022NM 2005 3 15 QXEA200500308 120050223A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09413QX 4060 CORROSION ON RT OUTBOARD SEAT TRACK AT APPROXIMATELY X457.00, TOP AND INNER FLANGE. REPLACED SEAT TRACK IAW DHC-8 SRM 51-42-15 AND 51-42-05. 2H72 4T RTA13NM 20050315000232005031500023NM 2005 3 15 QXEA200500310 120050223A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09413QX 4060 PDX - CORROSION ON RIGHTHAND OUTBOARD SEAT TRACK AT APPROXIMATELY X424.00, TOP AND INNER FLANGE. REPLACED SEAT TRACK IAW DHC-8 SRM 51-42-15 AND 51-42-05. 2H72 4T RTA13NM 20050315000252005031500025NE 2005 3 15 DL73S050135 220050226A7200 ENGINE BOEING737 737232 1384475NM PWA JT8 JT8D15A 52051NE NR 1 ODOR A DALAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SO27327DL48339 23099 709175 FRONT LAV SMOKE ALARM CAME ON SHORTLY AFTER TAKEOFF AND SMOKE THIN AND WISPY, CAME FROM LAV. SMOKE SMELL EVIDENT THROUGHOUT ENTIRE AIRCRAFT. WASHED NR 1 ENGINE AND RAN ENGINE WITH PACKS. NO SMELL NOTED 2L72 4F4 FRTA16WE E2EA 20050315000272005031500027NM 2005 3 15 DL733050137 120050227A4900 APU BOEING737 737347 1384647NM APU BAY FUSES A DALAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TXTAXI/GRND HDL 1 SO27309WA 23442 CREW REPORTS FUMES IN CABIN WHILE AT THE GATE. DEPLANED PASSENGERS AND TURNED OVER TO MAINTENANCE. REPLACED APU PER MM. 2L72 4F RTA16WE 20050315000282005031500028NM 2005 3 15 DL777050138 120050217A33201014285 LIGHT BOEING777 777232 1385232NM CREW REST AREA BURNED A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO27863DA 29735 CREW REST SIDE LIGHT HAS BURNED END. REPLACED SAME. 2L72 4F RTT00001SE 20050315000292005031500029NE 2005 3 15 DL76S050139 220050228A7320 CONTROLLER BOEING767 767332 1382001NM GE CF680 CF680A2 NE NR 1 ENGINE MALFUNCTIONED A DALAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SO27135DL46611 25145 580356 NR 1 ENG WOULD NOT ACHIEVE T/O POWER WITH ANTI-ICE ON OR OFF. RETURNED TO GATE. REPLACED MAIN ENGINE CONTROLLER. 2L72 4F4 FRTA1NM E13NE 20050315000302005031500030SO 2005 3 15 C2XA05RI004 120050309A3260 LOGIC CARD EMB 145 EMB145LR 3260212SO MLG UPLOCK CORRUPTED A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2711536 145520 AFTER TAKEOFF, LG AIR/GROUND DISAGREE MESSAGE APPEARED ON EICAS. LANDING GEAR WOULD NOT RETRACT NORMALLY UNTIL OVERRIDE, THEN ENG 1-2 T/R DISAGREE MESSAGE APPEARED ON EICAS. CREW RETURNED TO CHS. ACFT WAS FERRY FLIGHT TO RIC. RIC MX PERFORMED PROX SW FUNCTIONAL CHECK AND FOUND 3RD UPLOCK LOGIC CORRUPTED. MX REMOVED AND CLEANED CONNECTORS P0774 AND P0775. MX PERFORMED RESET OF AIR GROUND LOGIC SYSTEM. LANDING GEAR RETRACTION AND EXTENSION FUNCTIONAL TEST WAS SUCCESSFULLY PERFORMED. THRUST REVERSER OPERATIONAL CHECK WAS SUCCESSFULLY PERFORMED AND ACFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20050315000312005031500031GL 2005 3 15 C2XA05IA024 220050209A720023061402 BEVEL GEAR EMB 145 EMB145XR 3260214SO ALLSN AE300 AE3007A GL NR 2 ENGINE BROKEN A C2XAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SW2714143 145739 CAE312251 BTR - FLIGHT 3334, THE CREW REPORTED THAT THE NR 2 ENGINE SHUTDOWN IN FLT. THE AIRCRAFT DIVERTED TO BTR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRT TE6CH 20050315000322005031500032WP 2005 3 15 0500339852 120050311A32443910797507 TIRE DOUG DC9 DC951 3022051WP NR 1 MLG SEPARATED A NWAAO OTHER O OTHER LDLANDING 1 GL01761NC34079318 47709 THE OB LT MLG TIRE FAILED DURING LANDING. THE MISSING TREAD AND DEFLATED TIRE WAS REPORTED BY ANOTHER AIRCRAFT DURING TAXI TO THE GATE. TIRE TREAD SEPARATION DID CAUSE DAMAGE TO THE LANDING GEAR DOOR AND TO FLAP SURFACES. THERE WAS NO REORTED DAMAGE TO ANY POWER PLANT. TIRE ADN WHEEL ASSY FOR THE NR 1 AND NR 2 POSITIONS WERE REPLACED AND ALL EXTRANEOUS DAMAGE WAS REPAIRED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050315000352005031500035EA 2005 3 15 A6WA200540039 120050131A5730 PANEL CNDAIRCL600 CL6002B19 1900309EA RT WING CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31412AW 7582 RT WING PLANK HAS CORROSION UNDER THE FOLLOWING FUEL PANELS 640BB AND 650HB. REMOVED MINOR CORROSION FROM RIGHT WING LOWER PLANK AT FUEL TANK ACCESS PANELS 340BB AND 650 HB IAW BOMBARDIER, INC REO 601R-57-21-030 REV C. (M) 2L72 4F RTA21EA 20050315000362005031500036EA 2005 3 15 A6WA200540049 120050213A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FS CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31421ZW 7346 FS 484 AT RBL 27 HAS A CRACKED ANGLE. REMOVED AND REPLACED ANGLE IAW BOMBARDIER REO 601R-53-41-059. (M) 2L72 4F RTA21EA 20050315000472005031500047EA 2005 3 15 A6WA200540063 120050130A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31414ZW 7586 FOUND RT FS 484 ANGLE AT RBL 27 IS CRACKED. REPAIRED RT FS 484 ANGLE IAW BRAS EO 601R-53-41-059. (M) 2L72 4F RTA21EA 20050315000512005031500051EA 2005 3 15 A6WA200540057 120050215A5300 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31421ZW 7346 FOUND FS 484 LBL 9 ANGLE CRACKED APPROX .40 INCH RADIUS. REPLACED ANGLE IAW BRAS EO 601R-53-5983. (M) 2L72 4F RTA21EA 20050315000542005031500054EA 2005 3 15 A6WA200540054 120050215A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31421ZW 7346 FOUD FS 280 RBL 9 OUTBOARD ANGLE CRACKED APPROX .8 INCH LONG IN RADIUS. REPLACED ANGLE IAW CRJ SRM 51-42-21 AND BRAS EO 601R-53-8992. (M) 2L72 4F RTA21EA 20050315000552005031500055EA 2005 3 15 A6WA200540067 120050202A5320601R53610045 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31414ZW 7586 FOUND LEFT FS 621 ANGLE IS CRACKED. REPAIRED LEFT FS 621 ANGLE IAW BRAS EO 601R-53-61-117. (M) 2L72 4F RTA21EA 20050315000562005031500056EA 2005 3 15 A6WA200540025 120050126A3210601R572100323 BUSHING CNDAIRCL600 CL6002B19 1900309EA LT MLG MIGRATED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31414ZW 7586 LT MAIN LANDING GEAR AFT TRUNNION BUSHING IS MIGRATED .007 INCH. REMOVED MIGRATED BUSHING AND INSTALLED A 2ND OVERSIZED BUSHING MODIFIED TO A 1ST OVERSIZED BUSHING IAW BOMBARDIER EO 601R-57-21-003 REV B AND EO 601R-57-5907A. (M) 2L72 4F RTA21EA 20050315000572005031500057EA 2005 3 15 A6WA200540064 120050130A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31414ZW 7586 RT FS 484 ANGLE AT RBL 36 IS CRACKED. REPAIRED RT FS 484 ANGLE IAW BRAS EO 601R-53-41-059. (M) 2L72 4F RTA21EA 20050315000592005031500059EA 2005 3 15 A6WA200540062 120050202A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31414ZW 7586 FOUND RT FS 621 ANGLE IS CRACKED. REPAIRED RT FS 621 ANGLE IAW BOMBARDIER REO 601-53-61-117 REV A. (M) 2L72 4F RTA21EA 20050315000612005031500061EA 2005 3 15 A6WA200540053 120050215A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31421ZW 7346 FOUND FS 280 RBL 9 INBOARD ANGLE CRACKED APPROX .7 INCHES LONG IN RADIUS. REPLACED ANGLE IAW CRJ SRM 51-42-06 AND 51-42-21. (M) 2L72 4F RTA21EA 20050315000632005031500063EA 2005 3 15 A6WA200540046 120050210A3210 BUSHING CNDAIRCL600 CL6002B19 1900309EA LT MLG MIGRATED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31447AW 7812 FOUND LT MAIN LANDING GEAR AFT TRUNNION BUSHING IS MIGRATED .041 INCH. REMOVED MIGRATED BUSHING AND INSTALLED 1ST OVERSIZED BUSHING IAW BOMBARDIER REO 601R-57-21-003 REV B. (M) 2L72 4F RTA21EA 20050315000642005031500064EA 2005 3 15 A6WA200540045 120050210A3210 BUSHING CNDAIRCL600 CL6002B19 1900309EA TRUNNION MIGRATED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31447AW 7812 RT MAIN LANDING GEAR AFT TRUNNION BUSHING IS MIGRATED .045 INCH. REMOVED MIGRATED BUSHING AND INSTALLED 1ST OVERSIZED BUSHING IAW BOMBARDIER REO 601R-57-21-003 REV B. (M) 2L72 4F RTA21EA 20050315000672005031500067EA 2005 3 15 A6WA200540065 120050130A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31414ZW 7586 LEFT FS 484 ANGLE AT LBL 36 IS CRACKED. REPAIRED LEFT FS 484 ANGLE IAW BRAS REO 601R-53-41-059. (M) 2L72 4F RTA21EA 20050315000682005031500068NM 2005 3 15 XN0A1223 120050108A7711 UNKNOWN BOEING727 727200 138407ENM NR 1 EPR UNRELIABLE A XN0AC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 GL2376753 21363 ON TAKEOFF ROLL NR 1 EPR UNRELIABLE. NR 1 EPR TO DMI 5047 IAW MEL 771 PLACARDS INSTALLED. 2L73 4F RTA3WE 20050315000692005031500069EU 2005 3 15 XN0A1224 120050119A3241 CONTROL BOX AIRBUS300 A300B4203 3930306EU ANTI-SKID SYS MALFUNCTIONED A XN0AD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL23472AS 125 ON TAXI, GREEN BRAKES VERY SPONGY, ALT BRAKES NO BRAKING. REMOVED AND REPLACED ANTI-SKID CONTROL BOX IAW A300 MM 32-42-72. SERVICED EMERGENCY BRAKE RESERVOIR IAW MM 32-44-11. SYSTEM GREEN & YELLOW, OPS CHECK GOOD IAW A300 MM 32-42-00. 2L72 4F RTA35EU 20050315000702005031500070EA 2005 3 15 A6WA200540068 120050125A5320 SILL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31414ZW 7586 FOUND CARGO DOOR SILL PLATE AT FS 589 CRACKED. REPAIRED CARGO DOOR SILL PLATE IAW BOMBARDIER REO 601R-53-61-433. (M) 2L72 4F RTA21EA 20050315000712005031500071EA 2005 3 15 A6WA200540058 120050214A5753 SKIN CNDAIRCL600 CL6002B19 1900309EA TE FLAP DENTED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31421ZW 7346 RIGHT INBOARD FLAP OUTBOARD LOWER CORNER HAS A DENT .5 INCH BY 3 INCHES BY .080 INCHES. S/D REMOVED DAMAGED SECTION OF SKIN, FABRICATED REPAIR PARTS FROM 2024.T3.050, (WVAX PO NR 40777) 2024-T3.063 (WVAC PO NR 36153) AND 2024-T3.012 (WVAC PO NR 24116). INSTALLED REPAIR PARTS IAW CRJ 200 SRM 57-52-00 REPAIR 2. (M) 2L72 4F RTA21EA 20050315000722005031500072EA 2005 3 15 A6WA200540069 120050216A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31448AW 7814 RT FS 621 ANGLE HAS A .5 INCH CRACK ON OUTBOARD RADIUS. S/D - REPAIRED CRACKED RT FS 621 ANGLE BY CUTTING AWAY DAMAGED AREA AND INSTALLING REPAIR ANGLE AND STRAP IAW BOMBARDIER REO 601R-53-61-117 REV C. (M) 2L72 4F RTA21EA 20050315000762005031500076EA 2005 3 15 A6WA200540073 120050217A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31448AW 7814 FLOOR SUPPORT ANGLE AT FS 621, LBL 36, WL 73 IS CRACKED, APPROXIMATELY .25 INCH. (M) 2L72 4F RTA21EA 20050315000792005031500079EA 2005 3 15 A6WA200540074 120050202A5210601R317725S DRAG ANGLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31412AW 7582 PAX DOOR AFT DRAG ANGLE IS CRACKED 3 INCHES LONG JUST FORWARD OF PAX DOOR ASSIST PULLEY MOUNT BRACKET. REPAIRED ANGLE IAW BRAS EO 601R-52-5929 AND BOMBARDIER, INC REO 601R-52-11-513. (M) 2L72 4F RTA21EA 20050315000812005031500081WP 2005 3 15 GTIA050029 120050209A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FTW - FOUND PAX CABIN FLOOR SUPPORT CORRODED AT FS 230 10 INCH RBL. REMOVED CORROSION AND FLOOR SUPPORT AT FS 230, FABRICATED, TREATED, PRIMED AND INSTALLED NEW FLOOR. (M) 2L72 4F A6WE 20050315000832005031500083WP 2005 3 15 GTIA050033 120050115A5315 FLOORBEAM DOUG DC9 DC982 3022082WP FUSELAGE GOUGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FTW - FOUND MID PIT STATION 655 CEIING RBL 2 FLOORBEAM GOUGED. FABRICATED FILLER, ANGLE AND SHIM. TREATED, PRIMED AND INSTALLED. (M) 2L72 4F A6WE 20050315000842005031500084WP 2005 3 15 GTIA050032 120050207A5312 BULKHEAD DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 LOWER APB AREA STATION 1338 STRINGER 28R STIFFENER CORRODED AND LEFT ANGLE CORRODED. REMOVED AND REPLACED STIFFENER AND ANLE. LOCATED AND DRILLED HOLES AND INSTALLED. (M) 2L72 4F A6WE 20050315000872005031500087CE 2005 3 15 010605 120050106A36201143800273 GAUGE BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA HARTZLHCB4M HCB4MP3 GL COCKPIT LEAKING A OEZAO OTHER O OTHER CRCRUISE 1 WP19381CR4 4 UB69 DURING CRUISE, FIRST OFFICER NOTICED THAT HIS ALTIMETER, VSI AND AIR SPEED INDICATOR BEGAN TO MOVE. SELECTED THE ALTERNATE STATIC SOURCE AND THE INSTRUMENTS RETURNED TO NORMAL READINGS. DURING DESCENT FIRST OFFICER NOTICED THAT HIS VSI WAS NOT READING THE SAME AS PILOTS. AIRCRAFT WAS FERRIED BACK TO MAIN MX BASE FOR REPAIRS. MX FOUND THE PNEUMATIC PRESSURE GAUGE WAS LEAKING CABIN AIR INTO THE STATIC CHAMBER OF THE GAUGE. THE SOURCE OF THE AIR LEAK WAS NOTED AS BEING THE ELECTRICAL CONNECTION PLUG FOR THE INTERNAL LIGHTING. THE GAUGE WAS REPLACED, A PITOT STATIC LEAK CHECK PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE. THE GAUGE WAS OVERHAULED BY AERO-MACH LABS AND HAD 4.1 HOURS TSO BEFORE IT FAILED.2L72 4T4 TRTA24CE E4EA 6 CP56GL 20050315000902005031500090EU 2005 3 15 SIMA200504101 120050208A261172111211000 SMOKE DETECTOR SAAB SF340 340B 7860101EU E/E BAY FAILED A SIMAB EMER. DESCENT N FALSE WARNING DEDESCENT 1 SW21261AE 340B261 DFW - FLT 3214 - RECEIVED AVIONICS SMOKE WARNING ON THE CENTRAL WARNING PANEL DURING DESCENT WITH NO VISIBLE SMOKE OR NO SMOKE SMELL. THE LIGHT WENT OUT AFTER LANDING. PERFORMED GENERAL VISUAL OF AVIONICS COMPARTMENT WITH NO SIGNS OF BURNING OR ANY UNUSUAL SMELL. REPLACED AVIONICS SMOKE DETECTOR. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 20050315000912005031500091EU 2005 3 15 TCA002 120050118A5610MY20268108 WINDSHIELD AMD FALC20FALCON 2720302EU COCKPIT CRACKED E E18AA UNSCHED LANDING O OTHER CRCRUISE 1 GL23326VW 27 THE COPILOT RT WINDSHIELD DEVELOPED CRACKS WHILE AIRCRAFT WAS IN CRUISE. THE PILOT RETURNED BACK TO BASE SAFELY. 2L72 4F A7EU 20050315000932005031500093EA 2005 3 15 A6WA200540075 120050131A5220 HANDLE CNDAIRCL600 CL6002B19 1900309EA ESCAPE HATCH LACK OF LUBE A A6WAK NONE O OTHER ININSP/MAINT 1 GL31412AW 7582 CREW ESCAPE HATCH OUTER HANDLE WILL NOT RELEASE. LUBRICATED HANDLE IAW CRJ 200 AMM 12-20-52-640-803. PERFORMED CHECK IAW CRJ 200 AMM 52-22-00-710-801. (M) 2L72 4F RTA21EA 20050315000952005031500095WP 2005 3 15 WX0500007 120050117A324226088921 BRAKE DOUG DC9 DC983 3022083WP NR 2 SEIZED A WX0AC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP19864GA 49912 FNL - DURING TAKEOFF ROLL WHEEL NOT TURNING, LIGHT CAME ON. ABORTED TAKEOFF BELOW 80 KIAS. NR 2 BRAKE OVERHEAT LIGHT CAME ON, TEMP PEAK AT 350 DEGREES. MAINTENANCE FOUND NR 2 BRAKE SEIZED. MAINTENANCE REMOVED AND REPLACED NR 2 BRAKE AND NR 2 TIRE ASSEMBLY IAW 32-40-01 AND 32-42-01. SERVICED TIRE TO 200 PSI IAW 12-16-01. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050310001742005031000174NM 2005 3 10 LCQ26 120050117A52306547952205 SKIN BOEING737 737 UTILSYSNM CFMINTCFM56 CFM563C1 13802EU AFT CARGO DOOR DENTED C K NONE O OTHER ININSP/MAINT 1 SO15944UA 26683 AFT CARGO DOOR SKIN HAS DENTS. S/O 269003, N/R 21401 2L72 4F4 FRTA16WE E21EU 20050310001762005031000176NM 2005 3 10 ANCF200400040 120050226A7100JT8D219 ENGINE DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE FAILED W ANCFE ENGINE SHUTDOWN Z SIGNIFICANT FAILURE REPORT ININSP/MAINT 1 SO23EICBR250422001 49939 P726956D DURING MAINTENANCE CHECKS WITH ENGINES RUNNING UP THE LT ENGINE HAD A STRONG STALL. THE LT ENGINE WAS IMMEDIATELY SWITCHED OFF. DURING THE PRELIMINARY BOROSCOPE INSPECTION, FOUND C6, C7, C13, COMBUSTION CHAMBER, T1 AND T2 IN GOOD CONDITIONS. THE DAMAGE WAS FOUND IN T4 AND HITS T3. THE INLET FAN FLANGE WAS FOUND SEPARATED. THE ENGINE TURNS WITHOUT DIFFICULTY THROUGH THE GEAR BOX AND THE FAN. THE ENGINE WILL BE SENT TO SHOP IN ORDER TO DETERMINE THE FAIL CAUSE. 2L72 4F4 FRT E9NE 20050311000442005031100044CE 2005 3 11 MXI2005F00001 120050223A32605ENI6 SWITCH BEECH MU300 400A 1155402CE PWA JT15 JT15* 52060NE RT MLG DOOR FAILED E MXIAO OTHER N FALSE WARNING LDLANDING 1 EA21414DR RK184 THE LANDING GEAR WOULD NOT EXTEND WITH GEAR HANDLE DOWN. THE LANDING GEAR WAS LOWERED USING THE MANUAL EMERGENCY EXTENSION AND THE GEAR DOORS WERE CLOSED USING THE PNEUMATIC GEAR BOTTLE. PROBABLE CAUSE WAS THE HIGH RESISTANCE IN THIS SWITCH AND THE GEAR DOOR OPEN SWITCH. (EA21200504836) (K) 2H72 4F4 TRTA16SW E1NE 20050311000562005031100056NM 2005 3 11 AMTA200500080 120050122A2612 CIRCUIT CARD BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE FIRE DETECTION LOOSE A AMTAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 GL11526AT 30735 FIRE PROTECTION SYS FAIL ILLUM, EICAS MSG FIRE/OVHT SYST DISPLAYED. EICAS STATUS MSG AFT CARGO DET 1 AND AFT CARGO DET 2 DISPLAYED. TROUBLESHOT IAW FIM. RESEATED AFOLTS CARD 6. SYSTEM TEST NORMAL. 2L72 4F4 FRTA2NM E12EU 20050311000572005031100057NM 2005 3 11 HALA0500078 120050117A27213F8202A MODULE BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE RUDDER TRIM STUCK A HALAK NONE O OTHER ININSP/MAINT 1 WP13477HA3627 55122 AILERON TRIM STUCK IN LT WING DOWN. REMOVED AND REPLACED AILERON AND RUDDER TRIM CONTROL MODULE IAW SRM. (K) 2L72 4F4 FTRA6WE E00061EN 20050311000592005031100059EU 2005 3 11 ASOA05010 120050104A33507012210 LAMP AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27530AS 1359 453 DURING A GROUND INSPECTION, THE FLIGHT ATTENDANT REPORTED THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT LAMP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2H72 4T4 TRTA53EU E20NE 20050311000922005031100092NM 2005 3 11 UIEA200500003 120050119A575365B01925311A SKIN BOEING747 74747UF 1384949NM GE CF6 CF680C2* GL LT WING TE FLAP DELAMINATED A UIEAO OTHER O OTHER TXTAXI/GRND HDL 1 EA15499MC 29260 FLIGHT CT 603, PIK-LUX 08 JAN, 2005 - IB LOG ITEM, LT OB MID FLAP PANEL DELAMINATED. MAINTENANCE PICK-UP ITEM. DURING FLAP REPLACEMENT FOUND IB CARRIAGE ASSY CORRODED. (LEVEL 1) REPLACED LT OB MID-FLAP, MM 27-51-04, REF LOG PAGE 544103. REPLACED IB CARRIAGE ASSY MM 27-51-28, REF LOG PAGE 544105. MID FLAP PN 65B01925-311A, SN 000549; CARRIAGE ASSY 65B08027-53, SN BT1055V. 2L74 4F4 FRT1384945 E23EA 20050314000012005031400001SO 2005 3 14 1322022705 120050227A56101159SCB51021 WINDSHIELD GULSTMG1159 GIV 3980115SO RROYCETAY TAY6118 EU COCKPIT CRACKED E N93AA UNSCHED LANDING O OTHER CRCRUISE 1 SO13422QS2627 1322 LT FRONT WINDSHIELD FAILED, CRACKED IN FLIGHT. 2L72 4F4 FRTA12EA E25NE 20050314000042005031400004NM 2005 3 14 SB05035 120050303A33503506892 SOCKET BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE SEAT 12ABC INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19373US 22952 MAINTENANCE REPORTED THE EMERGENCY LIGHT AT SEAT 12ABC INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT SOCKET AT SEAT 12ABC. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA16WE E2GL 20050314000212005031400021WP 2005 3 14 AALA20050183 120050304A49905940405503 APU DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE APU BAY LEAKING A AALAO OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21579AA 53156 P80431 ORD INFLIGHT T9673/4 MAR TEST FLIGHT FUMES IN CABIN SHORTLY AFTER TAKEOFF. VISIBLE BLUE SMOKE COMING FROM AFT CABIN, QUICKLY FILLED ENTIRE CABIN. TURNED OFF AIR CONDITIONER PACKS. SMOKE SLOWLY DISSIPATED. LANDED, DECLARED EMERGENCY LANDING DURING TEST FLIGHT. FOUND OIL LEAKING FROM APU. REPLACED APU. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F4 F A6WE E9NE 20050314000232005031400023CE 2005 3 14 2005F00038 120050214A771431036061 DRIVE SHAFT ALIDSG BEECH 100 B100 1152919CE GARRTTTPE331TPE3316252B 01514WP TACH GEN STRIPPED E O OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL2588FA 9001 BE74 P27149 LT ENGINE FAILED TO START NORMALLY. IN MANUAL MODE START WAS SUCCESSFUL. SUBSEQUENT START, GENERATOR WAS INOPERATIVE. EXTENSIVE TROUBLESHOOTING FINALLY DETERMINED THAT THE STARTER-GENERATOR HAD SIEZED, STRIPPING PLASTIC DRIVE ADAPTER IN ENGINE. DRIVE ADAPTER WAS REPLACED, ALONG WITH A SERVICEABLE STARTER-GENERATOR, SYSTEMS FUNCTION NORMALLY. 1L72 4T4 T A14CE E2WE 20050315000132005031500013NM 2005 3 15 DL738050129 120050223A3350 FUSE BOEING737 737832 13844CFNM EMERGENCY LIGHT BLOWN A DALAK NONE L NO TEST ININSP/MAINT 1 SO27381DA 30350 EMERGENCY LIGHTS FROM SEAT ROW 23 AFT INOP. REPLACED FUSE IN EMERGENCY BATTERY CHARGER M1672. 2L72 4F RTA16WE 20050315000182005031500018NM 2005 3 15 DL757050134 120050226A52701A08101643 SWITCH BOEING757 757232 1384965NM LAV DOOR SHORTED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27689DL 27172 REPLACED L1 LAV DOOR LOCKED SWITCH FOR ARCING. 2L72 4F RTA2NM 20050315000192005031500019CE 2005 3 15 69476 120050302A3240 BRAKE BEECH 1900 1900D 1154162CE LEFT MALFUNCTIONED A AMWAC ABORTED TAKEOFF J WARNING INDICATION TXTAXI/GRND HDL 1 CE07163YV UE163 AFTER TAXI OUT LEFT BRAKE WILL NOT RELEASE. PASSENGERS DEPLANED ON TAXIWAY. MTC DETERMINED PARKING BRAKE WAS NOT RELEASING COMPLETELY. A/C RETURNED TO GATE AND PARKING BRAKE DEFERRED PER MEL 32-7. A/C RETURNED TO SERVICE. INSTALLED PARKING BRAKE KNOB. 2L72 4T RTA24CE 20050315000242005031500024NM 2005 3 15 QXEA200500309 120050223A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09413QX 4060 PDX - CORROSION ON RIGHTHAND OUTBOARD SEAT TRACK AT APPROXIMATELY X439.00, TOP AND INNER FLANGE. REPLACED SEAT TRACK IAW DHC-8 SRM 51-42-15 AND 51-42-05. 2H72 4T RTA13NM 20050315000332005031500033EA 2005 3 15 A6WA200540051 120050215A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31421ZW 7346 FOUND FS 280 LBL 9 OUTBOARD ANGLE CRACKED APPROX .9 INCH LONG IN RADIUS. REPLACED ANGLE IAW CRJ SRM 51-42-21 AND BRAS EO 601R-535992. (M) 2L72 4F RTA21EA 20050315000372005031500037EA 2005 3 15 A6WA200540055 120050215A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31421ZW 7346 FS 484 LBL 36 INTERCOSTAL CRACKED APPROX .30 INCH RADIUS. REPLACED INTERCOSTAL IAW BOMBARDIER, IAW REO 601R-53-41-059 REV A AND BRAS STANDARD REPAIR 601R-53-00-30. (M) 2L72 4F RTA21EA 20050315000782005031500078EA 2005 3 15 A6WA200540071 120050217A3210 BUSHING CNDAIRCL600 CL6002B19 1900309EA LT MLG MIGRATED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31448AW 7814 LEFT AFT MAIN LANDING GEAR TRUNNION BUSHING IS MIGRATED .050 INCH AT WS 66. (M) 2L72 4F RTA21EA 20050315000852005031500085SO 2005 3 15 SIMA200504102 120050206A532014522178005 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21653AE 145433 DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND THE SERVICE DOOR SILL CORRODED. REMOVED EXISTING SERVICE DOOR SILL AND INSTALLED SERVICEABLE SILL. REPAIR DONE IAW EMB 145 SRM, SRM EMB-145/1142 REV 28, CHAPTERS 51-20-01, 03, 51-40-02, 03, 04, 05, 06 AND 09. (M) 2L72 4T RTT00011AT 20050315000942005031500094SO 2005 3 15 SIMA200504501 120050212A3350602024 LIGHT EMB 145 EMB145LR 3260212SO COCKPIT INOPERATIVE A SIMAK NONE O OTHER ININSP/MAINT 1 SW21681AE 14500824 RST - FLT 3986 - CREW REPORTED THE EMERGENCY AT COCKPIT STEP TO BE INOPERATIVE. MAINTENANCE REPLACED THE EXIT MARKING SIGN ASSEMBLY IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20050315000982005031500098WP 2005 3 15 GTIA050030 120050209A5320 CUSP WEB DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FOUND CABIN FS 330, FS 1022-1041, FS 1041-1060, FS 1060-1079, FS 1079-1098, FS 1307 L-18L CUSP WEB CORRODED. REMOVED CORROSION AND WEB, DRILLED AND LOCATED NEW WEB FITTING ALONG L18L, TREATED, PRIMED AND INSTALLED DOUBLER AND NEW WEB SECTION. (M) 2L72 4F A6WE 20050315001012005031500101WP 2005 3 15 GTIA050017 120050125A2120 DUCT DOUG DC9 DC982 3022082WP COLD AIR DISCONNECTED A GTIAO OTHER J WARNING INDICATION CLCLIMB 1 GL23829NK 49931 DTW - FLT 973 - AIRCRAFT WOULD NOT PRESSURIZE IN FLIGHT, AUTO OR MANUAL. FOUND COLD AIR DUCTS AT LEFT AND RIGHT ACM'S DISCONNECTED, RECONNECTED DUCTS AND PRESSURIZED AIRCRAFT. OPS CHECK GOOD. (M) 2L72 4F A6WE 20050315001032005031500103WP 2005 3 15 GTIA050027 120050209A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FOUND CABIN FLOOR SUPPORT CORRODED AT FS 195-200 14 INCH LBL. REMOVED CORROSION AND FLOOR SUPPORT, FABRICATED FLOOR SUPPORT, TREATED, PRIMED AND INSTALLED FLOOR SUPPORT. (M) 2L72 4F A6WE 20050315001042005031500104WP 2005 3 15 GTIA050026 120050209A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FTW - FOUND PASSENGER CABIN FLOOR SUPPORT CORRODED AT FS 169, 4 INCHES RBL. REMOVED CORROSION AND PORTION OF FLOOR SUPPORT, FABRICATED FLOOR SUPPORT, TREATED, PRIMED AND INSTALLED FLOOR SUPPORT. (M) 2L72 4F A6WE 20050315001052005031500105WP 2005 3 15 GTIA050025 120050115A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FOUND CABIN FLOOR SUPPORT CORRODED AT FS 160 7 INCHES LBL. REMOVED CORROSION AT FLOOR SUPPORT, FABRICATED BRACKET, LOCATED AND DRILLED AND INSTALLED NEW FLOOR SUPPORT. (M) 2L72 4F A6WE 20050315001062005031500106CE 2005 3 15 DJFA2005052 120050123A323045AS385107 ACTUATOR BEECH MU300 400A 1155402CE LT MLG FAILED E DJFAO OTHER J WARNING INDICATION APAPPROACH 1 EA23442CW5917 RK42 CREW REPORTED MX TEST FLT GEAR CYCLED TO DOWN POSITION RESULTING IN TWO GREEN & ONE RED LIGHT. LEFT MAIN GEAR DID NOT SHOW DOWN AND LOCKED, WHICH WAS CONFIRMED BY RETARDING THE THROTTLE TO ACTIVATE THE LANDING GEAR WARNING HORN. AFTER SEVERAL UNSUCCESSFUL GEAR EXTENSIONS, EMERGENCY GEAR EXTENSION PERFORMED WITH SAME INDICATIONS. LOW APPROACH MADE SO TOWER COULD IDENTIFY GEAR POSITION. TOWER STATED, GEAR APPEARED TO BE DOWN WITH THE GEAR DOORS OPEN. UNEVENTFUL LANDING. MX PULLED OVER CENTER BRACE INTO PROPER POSITION TO FULLY LOCK LEFT MAIN GEAR & OBTAIN CORRECT DOWN & LOCKED INDICATION. LEFT MAIN GEAR DOWNLOCK ACTUATOR REPLACED, OPS CHECKS GOOD. TEST FLIGHT SATISFACTORY. ACFT RETURNED TO SERVICE. 2H72 4F RTA16SW 20050315001112005031500111EU 2005 3 15 XN0A1226 120050128A5610 MECHANISM AIRBUS300 A300B4203 3930306EU F/O WINDOW LACK OF LUBE A XN0AD RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL23373PC 218 F/O WINDOW SAFETY PIN STUCK. LUBRICATED F/O WINDOW MECHANISM, OPS CHECK GOOD IAW AMM 56-10-00. 2L72 4F RTA35EU 20050315001122005031500112WP 2005 3 15 WX0500010 120050121A326039396741 SENSOR DOUG DC9 DC983 3022083WP LT MLG FAULTY A WX0AO OTHER N FALSE WARNING APAPPROACH 1 WP19891GA 49423 LEFT MAIN UNSAFE LIGHT ILLUMINATED ON SHORT FINAL (GEAR UP). GEAR EXTENDED SHOWS ALL 3 LIGHTS GREEN, GEAR DOOR OPEN LIGHT REMAINS LIT. CYCLED GEAR, GEAR DOOR OPEN LIGHT EXTINGUISHED WHEN GEAR RETRACTED BUT REMAINED ON WITH GEAR EXTENDED. LEFT MAIN UNSAFE LIGHT REMAINED ON WITH GEAR RETRACTED BUT SHOWS ALL 3 GREEN LIGHTS WHEN GEAR IS EXTENDED. LANDED WITHOUT INCIDENT. MX REMOVED & REPLACED LMLG DOOR TARGET SENSOR. INSTALLED GEAR DOOR PROXIMITY SENSOR TARGET. ADJUSTED LMLG DOOR LATCH MECHANISM & LMLG UPLOCK SENSOR. MX PERFORMED TEST OF THE PROXIMITY SWITCH ELECTRONIC UNIT IAW MM 32-60-04. AIRBORNE SYSTEM TEST SUCCESSFUL, GEAR OPERATED WITH NORMAL INDICATIONS. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050315001132005031500113WP 2005 3 15 WX0500008 120050119A33507732 LIGHT DOUG DC9 DC987 3022087WP CABIN INOPERATIVE A WX0AK NONE L NO TEST ININSP/MAINT 1 WP19945MA 49725 LAS - MAINTENANCE REPORTED EMERGENCY FLOOR TRACK LAMPS OUT AT ROW 1 AND ROW 17. MAINTENANCE RELAMPED FLOOR TRACK LIGHTS AT ROW 1 AND ROW 17. SYSTEM OPERATIONALLY CHECKED GOOD IAW MM 33-53-01. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050315001162005031500116CE 2005 3 15 DJFA2005054 120050128A30402SC1120A SENSOR BEECH MU300 400A 1155402CE COCKPIT MALFUNCTIONED E DJFAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA23430CW RK30 IN CRUISE FLT CREW NOTICED AN ELECTRICAL ODOR IN COCKPIT. ODOR SEEMED TO DISSIPATE AFTER BATTERY & MASTER GENERATOR SWITCHES WERE PLACED IN EMERGENCY POSITIONS. EMERGENCY DECLARED & ACFT LANDED. MX INSPECTED BATTERY WIRING, AREA BEHIND LAV PANEL, AND THE DUCTING IN THE REAR BAY AREA WITH NO NOTED DEFECTS. WIRING FOR LT & RT STARTER / GENERATORS INSPECTED, NO DEFECTS. ENGINES OPERATED WITH BLEED AIR SYSTEMS RUNNING. RT WINDSHIELD HEAT CURRENT SENSOR (L102S) TERMINAL-B & APPROX 2 FT OF WIRE FOUND TO OVERHEAT & MELT WITH WINDSHIELD HEAT ON. ALL OTHER SYS OPERATED NORMALLY. RIGHT WINDSHIELD CURRENT SENSOR & WIRE 4045A2-L102SB REPLACED. WINDSHIELD HEAT SYS FUNCTION CHECK NORMAL. ACFT RETURNED TO SERVICE. 2H72 4F RTA16SW 20050315001172005031500117NM 2005 3 15 FX7A200500001 120050209A27821U1110 ACTUATOR BOEING727 727231 1384079NM PWA JT8 JT8D NE L/E FLAP LEAKING A FX7AD RETURN TO BLOCK K FLUID LOSS TXTAXI/GRND HDL 1 SO1954348 21967 DURING TAXI HYDRAULIC QUANTITY DROPS TO ZERO. 2L73 4F4 F A3WE E2EA 20050315001182005031500118NE 2005 3 15 DJFA2005058 220050211A7310 FUEL SYS BEECH MU300 400A 1155402CE PWA JT15 JT15D5 52112NE FUEL TANK CONTAMINATED E DJFAO OTHER J WARNING INDICATION DEDESCENT 1 EA23448CW RK368 KMIA - KCVG CREW REPORTED THAT WHILE DESCENDING FROM 19,000 TO 11,000 FEET THE LEFT FUEL FILTER BYPASS LIGHT ILLUMINATED MOMENTARILY, THEN RE-ILLUMINATED AFTER APPROXIMATELY ONE MINUTE. SEVERAL MINUTES LATER THE RIGHT FUEL FILTER BYPASS LIGHT ILLUMINATED, AND THEN MOMENTARILY EXTINGUISHED. AN EMERGENCY WAS DECLARED, AND AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. BOTH ANNUNCIATORS WERE ILLUMINATED ON LANDING AND ROLLOUT. AT THE THRESHOLD OF THE RUNWAY BOTH FUEL FILTER BYPASS LIGHTS EXTINGUISHED. FUEL TEMPERATURE AT 11,000 FEET WAS -20 TO -22 DEGREES C. MAINTENANCE DRAINED WATER FROM THE FUEL TANKS AND PERFORMED AN ENGINE GROUND RUN WITH NO NOTED DISCREPANCIES. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4F4 FRTA16SW E25EA 20050315001192005031500119CE 2005 3 15 DJFA2005059 120050204A3260 SQUAT SWITCH BEECH MU300 400A 1155402CE RT MLG OUT OF ADJUST E DJFAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA23427CW RK27 KPBI CREW REPORTED THAT JUST AFTER ROTATION THE LEFT AND RIGHT THRUST REVERSER ARM LIGHTS HAD ILLUMINATED. THE EMERGENCY STOW BUTTONS WERE IMMEDIATELY PRESSED. THE AIRCRAFT RETURNED TO KPBI AND LANDED WITHOUT FURTHER INCIDENT. THE ARM LIGHTS HAD REMAINED ILLUMINATED FOR THE DURATION OF THE FLIGHT. MAINTENANCE VERIFIED THE DISCREPANCY AND ADJUSTED THE RIGHT MAIN LANDING GEAR GROUND SAFETY SWITCH. SEVERAL GEAR RETRACTIONS WERE PERFORMED WITH NO NOTED DISCREPANCIES. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4F RTA16SW 20050315001202005031500120CE 2005 3 15 DJFA2005060 120050211A783022500231 SWITCH BEECH MU300 400A 1155402CE THRUST REVERSER FAULTY E DJFAE ENGINE SHUTDOWN P NO WARNING INDICATION CRCRUISE 1 EA23418CW RK18 KMIA - KMCO CREW REPORTED AFTER DESCENDING TO FL 270 FELT ACFT YAW TO LEFT. PARTIAL LT T/R DEPLOYMENT, NO WARNING INDICATION RECEIVED. AIRSPEED REDUCED & LT & RT T/R EMERGENCY STOW BUTTONS ACTIVATED. LT ENG SHUT DOWN, ACFT LANDED. MX INSPECTED LT T/R & FOUND I/B ACTUATOR NOT LOCKING IN STOWED POSITION. T/S A FAULTY STOW MICROSWITCH FOUND. LT I/B STOW MICROSWITCH REPLACED & RIGGED. LT T/R CYCLED SEVERAL TIMES, NO DEFECTS. SYS FUNCTIONALLY & OPERATIONALLY CHECKED NORM. LT T/R, ENG, AFTERBODY MOUNT FLANGE & ENG MOUNTS WERE VISUALLY INSPECTED WITH NO DEFECTS. RIGGING CHECKS OF CONTROL ARMS, STOW STOPS, AND SWITCHES COMPLETED. ALL RIGGING CHECKS GOOD. ACFT RETURNED TO SERVICE. 2H72 4F RTA16SW 20050315001212005031500121 2005 3 15 XN0A1228 420050211A3423 COUPLER AIRBUS300 A300B4203 3930306EU NR 1 COMPASS DEFECTIVE A XN0AD RETURN TO BLOCK O OTHER UKUNKNOWN 1 GL23473AS 203 NR 1 COMPASS FLUCTUATING + - 20 DEGREES. REPLACED NR 1 COMPASS COUPLER, OP'S GOOD IAW A300MM 34-21-34. 2L72 4F RTA35EU 20050315001222005031500122NM 2005 3 15 200500289 120050213A571165B010245 SPAR BOEING747 747273C 1384896NM LT WING CORRODED B EIAAK NONE O OTHER ININSP/MAINT 1 WP07471EV 20651 DURING C-CHECK, FOUND CORROSION ON LEFT HAND WING LOWER FRONT SPAR CHORD. THE MAJOR REPAIR REQUIRED REPLACING 186 INCHES OF THE SPAR CHORD. 2L74 4F A20WE 20050315001232005031500123CE 2005 3 15 DJFA2005061 120050213A3260 LIGHT CESSNA525 525 2076601CE COCKPIT INOPERATIVE E DJFAO OTHER L NO TEST APAPPROACH 1 EA23216CW 5250116 KMOB - KADS CREW REPORTED PRIOR TO LANDING WHEN GEAR SELECTED DOWN LT MAIN GEAR DOWN GREEN LIGHT FAILED TO ILLUMINATE. ANNUNCIATOR TEST HAD ALSO FAILED TO ILLUMINATE LIGHT. AN ATTEMPT WAS MADE TO SWAP INDICATOR BULBS, WHICH RESULTED IN NO GREEN GEAR DOWN LIGHTS. AN EMERGENCY GEAR EXTENSION WAS PERFORMED AND AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND ALL FOUR BULBS FOR THE GEAR DOWN AND LOCKED LIGHTS TO BE UNSERVICEABLE. NEW BULBS WERE INSTALLED AND OPERATIONALLY CHECKED GOOD. THE HYDRAULIC RESERVOIR AND BLOW DOWN BOTTLE WERE SERVICED. THE LANDING GEAR WAS OPERATED THROUGH TWENTY CYCLES. SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 1L72 4F RTA1WI 20050315001252005031500125NM 2005 3 15 SWAA050438 120050215A3350300432 LIGHT BOEING737 7377H4 1384404NM EXTERIOR INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29757LV 29850 DURING SCHEDULED MV2 CHECK, FOUND FWD LT EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2L72 4F RTA16WE 20050315001272005031500127EU 2005 3 15 DHL2005362004 120050217A3241 CONTROL BOX AIRBUS300 A300B4203 3930306EU ANTI-SKID SYS MALFUNCTIONED A DHLAO OTHER MJ OVER TEMP WARNING INDICATION LDLANDING 1 SO01362DH 84 INFLIGHT WITH LANDING GEAR HANDLE IN OFF POSITION ALL ANTI-SKID RELEASE LIGHTS ILLUMINATED AFTER LANDING NR 3 BRAKE TEMP EXCEEDED 680C ALL OTHER BRAKE TEMPS NORMAL. REPLACED ANTI-SKID CONTROL BOX IAW 32-42-16. OPS CHECK GOOD DEFERRED PER MEL 32-42-09-2. ASSIGNED CONTROL NR 19723. NR 3 & 6 BRAKES DEACTIVATED. PLACARD INSTALLED. 2L72 4F RTA35EU 20050315001352005031500135CE 2005 3 15 69268 120050221A5220 HANDLE BEECH 1900 1900D 1154162CE EMERGENCY EXIT UNSECURE A AMWAK NONE O OTHER ININSP/MAINT 1 CE07143YV UE143 UPON OST FERRY FLIGHT WALK AROUND INSPECTION, CREW NOTICED EMERGENCY EXIT DOOR 6A EXIT HANDLE PARTIALLY OUT. ADVISED MX CONTROL AND EXPERIENCED NO FURTHER INCIDENT. THE DOOR WAS RESECURED, THEREFORE NO PARTS WERE USED. 2L72 4T RTA24CE 20050315001362005031500136CE 2005 3 15 68837 120050201A32421143880241 BRAKE BEECH 1900 1900D 1154162CE LEFT FAILED A AMWAO OTHER O OTHER TXTAXI/GRND HDL 1 CE07176YV71 71 UE176 AFTER TAXI IN LEFT BRAKE WEAK. REMOVED AND REPLACED LT BRAKE. 2L72 4T RTA24CE 20050315001372005031500137NM 2005 3 15 SWAA050496 120050219A291065C26839 HYDRAULIC LINE BOEING737 7373H4 1384600NM HYDRAULIC SYS LEAKING A SWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 SW29367SW 26578 DIVERSION, INFLIGHT B-HYDRAULIC SYSTEM LOW PRESSURE LIGHT ILLUMINATED. FOLLOWED BY B-SYSTEM FLUID LOSS. REMOVED AND REPLACED HYDRAULIC HOSE AT B-SYSTEM ACOUSTIC FILTER PER MM. 2L72 4F RTA16WE 20050315001392005031500139 2005 3 15 SWIA200514617 420050218A3418 STICK SHAKER EMB 120 EMB120ER 3260203SO STALL WARNING INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07308SW 120326 F/O STICK SHAKER INOPERATIVE. REPLACED STICK SHAKER IAW EMB MM 27-34-04, OPERATIONAL CHECK GOOD. P/N C-81802-2, S/N OFF 843. 2L72 4T RTA31SO 20050315001402005031500140EA 2005 3 15 SWIA200514619 120050220A2750860D10018 ECU CNDAIRCL600 CL6002B19 1900309EA T/E FLAP MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 NM07406SW 7030 ON APPROACH AT FLAPS 20 AT 160 KTS, FLAP OVERSPEED CLACKER OCCURRED WHEN FLAPS 30 DEGREES SELECTED. REMOVED AND REPLACED FECU, OPERATIONAL CHECK GOOD IAW 27-51-10. P/N 860D100-18, S/N OFF 659. 2L72 4F RTA21EA 20050315001432005031500143NM 2005 3 15 SWAA050507 120050221A3350610478 BATTERY BOEING737 7377H4 1384404NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29774SW 27882 DURING SCHEDULED RON, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20050315001442005031500144EU 2005 3 15 UPS05143927 120050221A2560 GIRT BAR AIRBUS300 A300B4622R 3930312EU COCKPIT TWISTED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01159UP 0848 INSPECTION TYPE:N/A UNABLE TO DISARM ENTRY DOOR SLIDE. HANDLE WILL TRAVEL APPROX 3/4 AFT. ECAM INDICATION REMAINS AS SLIDE ARMED. FOUND GIRT BAR SKIRT TWISTED AND BINDING RELEASE MECH. ADJUSTED SKIRT, OPS CK NORMAL PER MM 25-61-21-4. 2L72 4F RTA35EU 20050315001462005031500146 2005 3 15 YENA200518 420050216A23303042865102 ELECTRICAL BOX AIRBUS320 A320232 3930326EU CABIN MALFUNCTIONED A YENAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15554JB6454 5376 1898 IN CRUISE AT FL 300 F3, SMELLED AN ELECTRIC TYPE OF ODOR IN MAIN CABIN, AROUND SEAT 11B. CLEARED AREA, INVESTIGATION DONE, NOTHING FOUND, ODOR PERSISTED. TURNED OFF LIVE TV FROM CABIN & COCKPIT. DURING DESCENT F1 REPORTED ODOR SEEMED STRONGER. UNABLE TO LOCALIZE PROBLEM. DECLARED EMERGENCY. ON GROUND ACCOMPLISHED INFO NOTICE 2004T023TR, NO DEFECTS NOTED. ACCOMPLISHED CIDS SYSTEM CHECK, NO DEFECTS NOTED. PRECAUTIONARY LIVE TV PLACED ON MEL 25-22-03. LATER MEL WAS CLEARED UPON ACCOMPLISHMENT OF LIVE TV, OPERATIONAL CHECK PER AMM 23-39-00 AND NO FAULTS NOTED. REPLACED SEBS AT SEAT 11B AND 12B AND MEL WAS CLEARED. SEAT 11B SEB OFF S/N 4282 T/T 6564 H 2241 C, SEAT 12B SEB OFF S/N 3775 T/T 8586 H 3014 C. 2L72 4F RTA28NM 20050315001502005031500150EU 2005 3 15 MALA050189 120050219A2432501122804 BATTERY SAAB SF340 340B 7860101EU E/E BAY DISCHARGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15447XJ 340B447 EMERGENCY POWER LIGHT ON. EMERGENCY POWER SUPPLY P/N 501-1228-04, S/N 4585. REPLACED CELLS NR 1 & NR 8, P/N 549-1170-01. UNIT PASSES CMM CHECKS, RTS 2/19/05. 2L72 4T RTA52EU 20050315001512005031500151EU 2005 3 15 MALA050177 120050123A33506122751 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU CABIN FAILED A MALAK NONE O OTHER ININSP/MAINT 1 GL15513XJ E2329 BATTERY PACK P/N 61-2275-1, S/N 9803372 FAILED SCHEDULED CAPACITY CHECK. REPLACED BATTERY ASSEMBLY P/N 61-2274-1. UNIT PASSES CMM CHECKS, RTS 1/28/05. 2H74 4F RTA49EU 20050315001522005031500152EU 2005 3 15 MALA050178 120050123A33506122751 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU CABIN FAILED A MALAK NONE O OTHER ININSP/MAINT 1 GL15524XJ E2349 BATTERY PACK P/N 61-2275-1, S/N 0001247 FAILED SCHEDULED CAPACITY CHECK. REPLACED BATTERY ASSEMBLY P/N 61-2274-1, UNIT PASSES CMM CHECKS, RTS 1/25/05. 2H74 4F RTA49EU 20050315001532005031500153EU 2005 3 15 MALA050179 120050123A33506122751 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU CABIN FAILED A MALAK NONE O OTHER ININSP/MAINT 1 GL15515XJ E2333 BATTERY PACK P/N 61-2275-1, S/N 9910195 FAILED SCHEDULED CAPACITY CHECK. REPLACED BATTERY ASSEMBLY 61-2274-1. UNIT PASSES CMM CHECKS, RTS 1/25/05. 2H74 4F RTA49EU 20050315001542005031500154EU 2005 3 15 MALA050164 120050221A53207253721439 WEB SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15423XJ 340B423 REINFORCEMENT WEB, P/N 7253721-439, IS CORRODED AND WILL BE REPLACED IAW SRM 51-40-21. FOUND DURING 4Y/2Y CHECK IN BNA. 2L72 4T RTA52EU 20050315001552005031500155EU 2005 3 15 MALA050170 120050221A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15414XJ 340B414 DURING 4K CHECK IN BNA FOUND SEAT TRACK AT BL 0, FROM FS 246 TO FS 300 IS CORRODED AND HAS BEEN REPAIRED IAW SRM 53-70-60. 2L72 4T RTA52EU 20050315001562005031500156EU 2005 3 15 MALA050171 120050221A5320 RISER SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15414XJ 340B414 DURING 4K CHECK IN BNA FOUND LT RISOR AT FS 294, FROM LBL 18.3 TO LBL 30 IS CORRODED AND WILL BE REPLACED IAW SRM 51-40-21. P/N 7253711-245. 2L72 4T RTA52EU 20050315001572005031500157EU 2005 3 15 MALA050174 120050126A33506122751 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU CABIN FAILED A MALAK NONE O OTHER ININSP/MAINT 1 GL15527XJ E2352 BATTERY PACK 61-2275-1, S/N 9803377 FAILED SCHEDULED CAPACITY CHECK. REPLACED BATTERY ASSEMBLY P/N 61-2274-1. UNIT PASSES CMM CHECKS, RTS 1/31/05. 2H74 4F RTA49EU 20050315001582005031500158NM 2005 3 15 XN0A1229 120050224A2612 FIRE WARNING BOEING727 727227 1384078NM COCKPIT MALFUNCTIONED A XN0AC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL2379754 21363 ON TAKEOFF ROLL MAIN CARGO FIRE WARNING AND BELL CAME ON. PERFORMED FUNCTIONAL CHECK OF MAIN DECK CARGO SYS, SDU'S SYSTEM CHECKED NORMAL IAW SECURE A PLANE. INSPECTED MAIN CARGO DECK FOR DEFECTS, NONE FOUND. 2L73 4F A3WE 20050315001592005031500159SO 2005 3 15 C2XA05IA029 120050222A2611FAU751A4 CONNECTOR EMB 145 EMB145XR 3260214SO CABIN LOOSE A C2XAO OTHER N FALSE WARNING APAPPROACH 1 SW2716151 145758 IAH - THE CREW REPORTED A LAV SMOKE DETECTOR INDICATION IN FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A LOOSE CONNECTOR ON THE SMOKE DETECTOR PANEL. MAINTENANCE RESECURED THE CONNECTOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20050315001612005031500161SO 2005 3 15 C2XA05SH013 120050222A532014521700007 FLOOR SUPPORT EMB 145 EMB145XR 3260214SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711140 145732 SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT CARBON CROSSBEAM FR20. MAINTENANCE REMOVED THE DAMAGE AREA AND PERFORMED REPAIR IN LT OMEGA BEAM IAW EMB 145 XR SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20050315001622005031500162NM 2005 3 15 CALA0500058 120050223A3230651781914 ACTUATOR BOEING737 7373T0 1384582NM NLG MALFUNCTIONED A CALAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SW2712327 23457 THE NOSE GEAR UNSAFE LIGHT ILLUMINATED WHEN GEAR WAS EXTENDED ON APPROACH TO EWR. THE GEAR WAS CYCLED DURING A GO-AROUND AND THREE GREEN SAFE GEAR LIGHTS ILLUMINATED. A VISUAL INSPECTION OF THE GEAR ALSO REVEALED GEAR WAS DOWN AND LOCKED. THE AIRCRAFT LANDED WITHOUT INCIDENT. EXTENSIVE TROUBLESHOOTING REVEALED THE NLG LOCK ACTUATOR WAS AT FAULT. THE NLG LOCK ACTUATOR WAS REMOVED AND REPLACED IAW MM 32-33-21. IN ADDITION, THE NOSE GEAR HYDRAULIC INSTALLATION MODULE WAS REMOVED AND REPLACED IAW MM 32-33-31. LEAK AND OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20050315001632005031500163EA 2005 3 15 SWIA200514618 120050220A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07440SW 7589 EMERGENCY LIGHT BAR ABOVE GALLEY SERVICE DOOR INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BAR IAW 33-00-00, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050315001662005031500166NM 2005 3 15 AALA20050166 120050217A5315 FLOORBEAM BOEING767 767323 1385205NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW2139364 24045 AFW - FLOORBEAM AT STATION 347 AT RIGHT BUTTLINE 30 CORRODED. REMOVED CORROSION AT RIGHT BUTTLINE 30. THE BLEND IS 0.090 INCH BY 0.047 DEPTH FROM 0.090 INCH PARENT. VERIFIED ALL CORROSION WAS REMOVED. FABRICATED REPAIR STRAP OUT OF 301 1/2 H STAINLESS STEEL 0.050 INCH THICK. ALODINE ALL BARE ALUMINUM SURFACES. FINISHED BLENDS AND REPAIRED PARTS WITH 2 COATS OF BMS 10 11 PRIMER. FILLED BLENDS WITH BMS 5 95 SEALANT. INSTALLED REPAIR STRAP WET WITH BMS 5 95 SEALANT. FASTENERS INSTALLED WITH 4 60 SPACING. 2L72 4F RTA1NM 20050315001672005031500167WP 2005 3 15 AALA20050171 120050306A3350 CONTACT DOUG DC9 DC982 3022082WP EMERGENCY LIGHT DIRTY A AALAK NONE L NO TEST ININSP/MAINT 1 SW21905TW 49157 SFO - ENTRY EMERGENCY LIGHTS AT NUMBER ONE DOOR INOPERATIVE. CLEANED CONTACTS FOR POWER AND GROUND FOR LEFT NUMBER 1 ENTRY DOOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050315001682005031500168NM 2005 3 15 AALA20050161 120050227A4920 APU BOEING757 757223 1384957NM APU BAY MALFUNCTIONED A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21183AN 29593 MCO - AFTER INTERMEDIATE LEVEL OFF AT FL220 SMOKE IN COCKPIT VERY SUDDEN & EVIDENT. FIRST CLASS F/A SMELLED SMOKE, ROW 26 PASSENGER INFORMED AFT F/A SMOKE SMELLED. ACCOMPLISHED CABIN SMOKE FIRE PROCEDURE TURNING OFF BOTH UTILITY BUS SWITCHES, BOTH RECIRCULATION FAN SWITCHES & RT PACK CONTINUE SELECT. SMOKE PERSISTED 20 PLUS MINUTES THROUGH LANDING. SMOKE DETECTED COCKPIT THEN FIRST CLASS F/A THEN MID CABIN. F/A REPORTED SEEING HAZE IN CABIN. WHILE PREPARING FOR DIVERSION TO MCO NOTICED LEFT HAND ENGINE VIBRATION 3.0 (AMBER) IN NR 1 POSITION. ALL SYSTEMS OPERATED NORMAL IN DESCENT TO MCO. REPLACED APU, & REPLACED VIBRATION ACCELEROMETER TRANSMITTER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050315001692005031500169NM 2005 3 15 AALA20050194 120050313A3350 LIGHT BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21605AA 27056 AUA CEILING EMERGENCY LIGHTS AT ROW 27 TO BACK OF AIRCRAFT INOPERATIVE. REPLACED BATTERY PACK AT CEILING RIGHT HAND LAVATORY FOR CEILING EMERGENCY LIGHTS AT ROWS 27 TO BACK OF AIRCRAFT, NO HELP. AIRCRAFT BEING FERRIED TO MIA FOR FURTHER EVALUATION AND REPAIR OF EMERGENCY LIGHTS. 2L72 4F RTA2NM 20050315001712005031500171NE 2005 3 15 AALA20050190 220050312A7320FFG022AD GOVERNOR BOEING757 757223 1384957NM RROYCERB211 RB211535E4B3 NE RT ENGINE INOPERATIVE A AALAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS CRCRUISE 1 SW21674AN 29424 31055 FLL INFLIGHT T2369/12MAR RIGHT HAND ENGINE PARAMETER FLUCTUATIONS. RETURNED TO FLL AND LANDED WITHOUT INCIDENT. REPLACED RIGHT ENGINE FUEL FLOW GOVERNOR AND THE HIGH PRESSURE FUEL PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA2NM E12EU 20050315001722005031500172WP 2005 3 15 AALA20050191 120050313A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21592AA 53255 LAX - EMERGENCY LIGHT IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050315001732005031500173NM 2005 3 15 AALA20050164 120050301A3350 WIRE BOEING757 757223 1384957NM CABIN MISWIRED A AALAK NONE WL INADEQUATE Q C NO TEST ININSP/MAINT 1 SW21617AM 24525 TUL - EMERGENCY EXIT LIGHTS AT LEFT NUMBER 2 DOOR INOPERATIVE. FOUND WIRING TO LEFT NUMBER 2 DOOR FORWARD LIGHT (L752) WIRED INCORRECTLY TO BATTERY PACK M10799. CORRECTED WIRING AT PLUG ON BATTERY PACK M10799 PER WIRING DIAGRAM 33 51 21 AND 24. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050315001762005031500176WP 2005 3 15 AALA20050156 120050226A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW219403W 53139 PHX - EMERGENCY LIGHT AT AFT FLIGHT ATTENDANT POSITION INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT AFT FLIGHT ATTENDANT POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050315001812005031500181EU 2005 3 15 AALA20050174 120050306A2910A3241030600200 HYDRAULIC LINE AIRBUS300 A300B4605R 3930308EU HYDRAULIC SYS CRACKED A AALAA UNSCHED LANDING K FLUID LOSS CRCRUISE 1 SW2170072 515 MIA - GREEN SYSTEM QUANTITY SHOWED AT RED DOT. MANUALLY EXTENDED GEAR. FOUND PRESSURE LINE IN CENTER GEAR WELL CRACKED. REPLACED PRESSURE LINE IN CENTER GEAR WELL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20050315001822005031500182WP 2005 3 15 AALA20050178 120050309A3397 WIRE DOUG DC9 DC983 3022083WP CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW219401W 53137 DTW - EMERGENCY EXIT LIGHT ON SIDEWALL OF FORWARD GALLEY INOPERATIVE. REPAIRED BROKEN WIRE FOR EMERGENCY EXIT LIGHT ON SIDEWALL OF FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050315001832005031500183NM 2005 3 15 AALA20050179 120050308A3350 BATTERY PACK BOEING777 777223 1385213NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21754AN 30262 DFW - ALL EMERGENCY LIGHTS IN FIRST, BUSINESS, AND COACH FAILED FUNCTIONAL CHECK. REPLACED ALL BATTERY PACKS FOR FIRST, BUSINESS, AND COACH EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20050315001842005031500184WP 2005 3 15 AALA20050182 120050306A3260H141016 SWITCH DOUG DC9 DC982 3022082WP NLG FAILED A AALAK NONE N FALSE WARNING CLCLIMB 1 SW21472AA 49647 DEN - UPON GEAR RETRACTION GREEN NOSE GEAR LIGHT REMAINED ON, IT STAYED ON FOR THE ENTIRE FIGHT. REPLACED NOSE LANDING GEAR RETRACT SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050315001852005031500185WP 2005 3 15 AALA20050176 120050308A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW219677W 53627 MSP - CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED ALL BATTERY PACKS FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050315001862005031500186WP 2005 3 15 AALA20050177 120050210A3397 WIRE DOUG DC9 DC982 3022082WP CABIN DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21205AA 49155 ORD - FORWARD GALLEY EMERGENCY LIGHTS INOPERATIVE. REPLACED WIRING FOR FORWARD GALLEY EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050315001872005031500187WP 2005 3 15 AALA20050154 120050225A3350 CONNECTOR DOUG DC9 DC982 3022082WP CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21400AA 49311 DFW - OVERHEAD EMERGENCY PATH CEILING LIGHT AT ROWS 18, 20 AND 21 INOPERATIVE. TIGHTENED LOOSE CONNECTORS ON OVERHEAD BIN EMERGENCY LIGHT BATTERY PACK AT ROW 20 FOR OVERHEAD EMERGENCY PATH CEILING LIGHTS AT ROWS 18, 20 AND 21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050315001912005031500191WP 2005 3 15 AALA20050175 120050303A3350P4010049 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW219619V 53566 DFW - SEAT MOUNTED EMERGENCY LIGHTS FROM THE FRONT OF THE AIRCRAFT TO ROW 19 INOPERATIVE. REPLACED BATTERY PACK 2 EACH AND CHARGING MODULES 2 EA IN RIGHT HAND OVERHEAD BIN AT ROW 20 AND REPAIRED CHAFED WIRE IN RIGHT HAND SIDEWALL GRILL FOR SEAT MOUNTED EMERGENCY LIGHTS FROM THE FRONT OF THE AIRCRAFT TO ROW 19. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050315001922005031500192NE 2005 3 15 AALA20050184 220050306A7200 ENGINE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE LEFT MAKING METAL A AALAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS CRCRUISE 1 SW21939AS 49657 718444 DFW INFLIGHT T1304/6 MAR LOUD BAND AND SHUTTER. LEFT ENGINE LOST POWER. ROLLED BACK TO IDLE. ENGINE RAN AT IDLE UNTIL AFTER LANDING. ENGINE WAS SHUT DOWN AFTER LANDING. FOUND METAL IN TAILPIPE. REPLACED NUMBER ONE ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA6WE E9NE 20050315001932005031500193NE 2005 3 15 AALA20050185 220050305A732176960612 FUEL CONTROL DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE RT ENGINE MALFUNCTIONED A AALAEA ENGINE SHUTDOWN UNSCHED LANDING O OTHER CRCRUISE 1 SW21446AA 49472 718569 ELP INFLIGHT T2438/5 MAR RIGHT ENGINE FAILED TO RESPOND TO THROTTLE MOVEMENT. RIGHT ENGINE WAS STUCK AT 93 PERCENT N2, EGT 500, EPR2.02 AT FL350. CHECKLIST SHOWS A COMPLETE LOSS OF NUMBER 2 SIGNAL TO THE FUEL CONTROL UNIT. ENGINE PAGE 20. SHUT DOWN PER CHECKLIST PROCEDURE. LANDED ELP WITHOUT INCIDENT. REPLACED RIGHT HAND FUEL CONTROL AND FUEL PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 F A6WE E9NE 20050315001952005031500195NE 2005 3 15 AALA20050186 220050303A732176960612 FUEL CONTROL DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE LT ENGINE MALFUNCTIONED A AALAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS DEDESCENT 1 SW217550 53032 728079 AUS INFLIGHT T1705/3 MAR DESCENDING AT IDLE LEFT ENGINE DID NOT RESPOND AT LEVEL OFF. NUMBER 1 AND NUMBER 2 EPR WERE ALL SUB IDLE WITH NO THROTTLE RESPONSE. SHUT LEFT ENGINE DOWN AND SECURED VIA ENGINE FAILURE CHECKLIST. NO FURTHER ABNORMALITIES. REPLACED LEFT HAND FUEL CONTROL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 F A6WE E9NE 20050315001982005031500198WP 2005 3 15 AALA20050159 120050301A335060030451 BATTERY DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21262AA 49290 ORD - OVERHEAD EMERGENCY LIGHTS FROM ROWS 3 TO 9 INOPERATIVE. REINSTALLED BATTERIES INTO CHARGER HOLDER FOR OVERHEAD EMERGENCY LIGHTS FROM ROWS 3 TO 9. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050315001992005031500199WP 2005 3 15 AALA20050160 120050301A3350P4010049 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21498AA 49736 SFO - OVERWING EMERGENCY EXIT IDENTIFIER LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND MODULE AT FORWARD RIGHT OVERWING EXIT IDENTIFIER FOR OVERWING EMERGENCY EXIT IDENTIFIER LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050315002002005031500200WP 2005 3 15 AALA20050172 120050306A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW219405T 53141 DFW - OVERHEAD CEILING EMERGENCY PATH LIGHT AT ROWS 28 AND 29 AND OVERHEAD OF LEFT NUMBER 2 DOOR INOPERATIVE. REPLACED BATTERY PACK AT B5 107 FOR OVERHEAD EMERGENCY PATH LIGHT AT ROWS 28 AND 29 AND LEFT NUMBER 2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050315002012005031500201WP 2005 3 15 AALA20050163 120050302A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21234AA 49181 LAX - EMERGENCY LIGHTS ON FUSELAGE INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS ON FUSELAGE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050315002022005031500202WP 2005 3 15 ABXA050038 120050302A3260 WARNING SYSTEM DOUG DC9 DC931 3022065WP COCKPIT MALFUNCTIONED A ABXAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 GL23947AX 47004 GEAR DOOR OPEN LIGHT DID NOT GO OUT AFTER EXTENDING ON APPROACH TO ILN, WENT ON MISSED APPROACH. RECYCLED GEAR AND LIGHT WENT OUT. CYCLED GEAR DOORS SEVERAL TIMES, LIGHT OPS CHECKED GOOD IAW DC-9 MM 32-30-00. 2L72 4F A6WE 20050315002032005031500203NE 2005 3 15 GTIA050007 220050111A7200 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE NR 2 MALFUNCTIONED A GTIAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 GL23804NK 49104 TAKEOFF ROLL A/T ENGAGED AT APPROX 40 KNOTS, THROTTLES AT FLEX POWER FELT SOMETHING LIKE A BLOWN TIRE, RT ENGINE SLIGHT YAW, ABORTED TAKEOFF. REMOVED AND REPLACED NR 2 ENGINE. (M) 2L72 4F4 F A6WE E9NE 20050315002042005031500204WP 2005 3 15 ABXA050037 120050301A3297 WIRE DOUG DC8 DC863F 302198FWP RT MLG BROKEN A ABXAL ABORTED APPROACH O OTHER APAPPROACH 1 GL23826AX 46061 RIGHT MAIN LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE WITH GEAR DOWN - RED GEAR UNSAFE LIGHT NOT ON - HORN DID NOT SOUND. RECYCLED NO HELP. FOUND WIRES G321E24 AND G324N24 BROKEN INSIDE THE CONDUIT BETWEEN P1-1398 AND S3-4. REPLACED BOTH WIRES AND WIRE G320H20 AS A PRECAUTION. PERFORMED GEAR SWING (ON WORK PACK NON ROUTINE CARD 106) IAW DC-8 MM 32-60-00-2. OPS CHECKED GOOD. 2L74 4F 4A25 20050315002052005031500205NE 2005 3 15 2005F00042 120050222A32977655200904042 WIRE HARNESS SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL MLG UPLOCK DAMAGED A ALGAO OTHER J WARNING INDICATION DEDESCENT 1 SW03522AL 760236 CAE890416S DURING PRELANDING PROCEDURES LANDING GEAR LIGHTS FAILED TO ILLUMINATE UPON GEAR EXTENSION. LANDING GEAR CIRCUIT BREAKER WAS RECYCLED SEVERAL TIMES AND LANDING GEAR POSITION WAS RECYCLED SEVERAL TIMES. AFTER THE CIRCUIT BREAKERS WERE RECYCLED LANDING GEAR LIGHTS WERE ILLUMINATED ON GEAR EXTENSION AND GEAR RETRACTION POSITIONS. MAINTENANCE REMOVED UPLIMIT CABLE ASSY AND INSTALLED SERVICEABLE CABLE ASSEMBLY. PERFORMED LANDING GEAR RETRACTION TEST TWENTY TIMES WITHOUT INCIDENT. (M) 1G72 3U3 U H1NE E1GL 20050315002082005031500208WP 2005 3 15 ABXA050047 120050208A532049128232NC CHANNEL DOUG DC9 DC933F 302207AWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23933AX 47291 CORROSION AT FUSELAGE FRAME AND FLOOR SUPPORT AREA STA 200, LONGERON 18 RIGHT AREA. REMOVED FLOOR PANEL AND J-CHANNEL AND RE-INSTALLED. ALL CORROSION WORK COMPLETED ON NON ROUTINE 0259 IAW DC-9 SRM 51-30-1. 2L72 4F A6WE 20050315002092005031500209WP 2005 3 15 ABXA050051 120050208A53205956034509AX SUPPORT ANGLE DOUG DC9 DC933F 302207AWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23933AX 47291 FLOOR STRAP SUPPORT ANGLE CRACKED AFT SIDE OF FRAME FS 503 AT LONGERON 28 RIGHT. REMOVED AND REPLACED ANGLE IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20050315002102005031500210WP 2005 3 15 ABXA050041 120050207A53203924028501 FITTING DOUG DC9 DC933F 302207AWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23933AX 47291 LONGERON END FITTING CRACKED, LONGERON 26 RIGHT AT APPROXIMATELY 612 - AFT OF P-DOME. INSTALLED NEW END FITTING P/N 3924028-501 IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20050315002112005031500211WP 2005 3 15 ABXA050054 120050216A53209910078647 INTERCOSTAL DOUG DC9 DC933F 302207AWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23933AX 47291 INTERCOSTAL AT STA 194 IN AIRSTAIR DOOR WAS CRACKED AND CORRODED. REPLACED INTERCOSTAL IAW DC-9 SRM 53-30-2. 2L72 4F A6WE 20050315002132005031500213WP 2005 3 15 ABXA050044 120050208A53209910078215 ATTACH BRACKET DOUG DC9 DC933F 302207AWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23933AX 47291 FORWARD AIRSTAIR COMPARTMENT FOUND CORROSION ON DOOR SWITCH AND ATTACH BRACKET. REPLACED ATTACH BRACKET AND WEB IAW DC-9 DWG 9922405 AND DC-9 SRM. 2L72 4F A6WE 20050315002162005031500216WP 2005 3 15 ABXA050042 120050207A53203924028501 FITTING DOUG DC9 DC933F 302207AWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23933AX 47291 LONGERON END FITTING CRACKED, LONGERON 26 LEFT AT APPROXIMATELY 612, AFT OF P-DOME. REPLACED END FITTING IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20050315002192005031500219WP 2005 3 15 ABXA050049 120050208A532059124921 PAN DOUG DC9 DC933F 302207AWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23933AX 47291 NUMEROUS SPOTS OF CORROSION ON FORWARD LOWER CARGO DOOR CUTOUT PAN WEB. CLEANED AND TREATED CORROSION IAW DC-9 SRM 51-10-3. 2L72 4F A6WE 20050315002202005031500220WP 2005 3 15 ABXA050050 120050208A53205956034509AX SUPPORT ANGLE DOUG DC9 DC933F 302207AWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23933AX 47291 FLOOR STRAP SUPPORT ANGLE EXFOLIATED FS 364 AT LONGERON 28 RIGHT. REMOVED AND REPLACED ANGLE IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20050315002212005031500221WP 2005 3 15 ABXA050052 120050209A5330591140733 SKIN DOUG DC9 DC933F 302207AWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23933AX 47291 CRACK IN FUSELAGE SKIN AT SERVICE DOOR CUTOUT LOWER AFT CORNER. REPAIRED IAW REA D953-51475MR AND DC-9 SRM 53-05. 2L72 4F A6WE 20050315002222005031500222WP 2005 3 15 ABXA050053 120050215A531059174637 DOOR FRAME DOUG DC9 DC933F 302207AWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23933AX 47291 CRACK IN VENTRAL DOOR JAMB STRUCTURE AT UPPER RIGHT CORNER. REPAIRED DAMAGED VENTRAL DOOR JAMB IAW DC-9 SRM 53-05. 2L72 4F A6WE 20050315002262005031500226NM 2005 3 15 USAA050297 120050213A5320 SUPPORT ANGLE BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU50570 23706 PIT - FOUND SUPPORT ANGLE CORRODED APPROX 24 INCHES, FORWARD SERVICE DOOR FLOOR THRESHOLD SUPPORT ANGLE. REPLACED SUPPORT PER SRM 53-10-15. (M) 2L72 4F RTA16WE 20050315002272005031500227NM 2005 3 15 USAA050298 120050211A575465C26320 SKIN BOEING737 7373B7 1384580NM TE FLAP CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU50570 23706 PIT - FOUND RIGHT OUTBOARD MID FLAP CHAFED .25 INCH BY 2 INCH BY .016 INCH, OUTBOARD 4 EDGE SURFACE. DOUBLER INSTALLED PER SRM 57-53-01 FIG 208. (M) 2L72 4F RTA16WE 20050315002302005031500230NM 2005 3 15 USAA050203 120050113A5311 FRAME BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19436US41647 24558 PIT - FOUND FRAME CRACKED .25 INCH, BETWEEN STRINGER 8L AND 9L AT STATION 867. CUT OUT DAMAGED AREA, HI FREQ INSTALLED DOUBLER PER TR 53-10-20A. (M) 2L72 4F RTA16WE 20050315002342005031500234NM 2005 3 15 USAA050202 120050112A5313 STRINGER BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19436US41647 24558 PIT - FOUND STRINGER CRACKED .25 INCH, STATION 907 STRINGER 4R. DOUBLER INSTALLED PER SRM 53-00-03 FIG 201. (M) 2L72 4F RTA16WE 20050315002352005031500235NM 2005 3 15 USAA050208 120050107A5320 INTERCOSTAL BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19436US41647 24558 PIT - FOUND INTERCOSTAL CRACKED .5 INCH, 2 FASTENER HOLES STATION 500G TO 520 BL 0. INSTALLED INTERCOSTAL PER 53-30-51. (M) 2L72 4F RTA16WE 20050315002362005031500236NM 2005 3 15 USAA050205 120050101A5340 CLIP BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19436US41647 24558 PIT - FOUND FRAME CLIP CRACKED .5 INCH, STATION 706 S11L. FABRICATED AND INSTALLED NEW CLIP PER SRM 51-46-03 AND 51-70-11. (M) 2L72 4F RTA16WE 20050315002382005031500238NM 2005 3 15 USAA050207 120050112A5311 FRAME BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19426US41647 24558 PIT - FOUND FRAME CRACKED .125 INCH FROM RIVET, STATION 727D BETWEEN S8/59R. REPAIR ANGLE PER TYPICAL REPAIR 53-10-20A. (M) 2L72 4F RTA16WE 20050315002412005031500241NM 2005 3 15 USAA050211 120050101A5320 INTERCOSTAL BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19436US41647 24558 PIT - FOUND INTERCOSTAL CRACKED 1.75 INCH, STATION 384-386 IN RADIUS OF INTERCOSTAL BL 0. INSTALLED INTERCOSTAL PER 53-20-1/53-30-1. (M) 2L72 4F RTA16WE 20050315002422005031500242NM 2005 3 15 USAA050212 120050104A5230 STRUCTURE BOEING737 7374B7 1384702NM AFT CARGO DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19436US41647 24558 PIT - FOUND AFT CARGO DOOR CRACKED .25 INCH, LOWER T-CHORD AFT VERTICAL FLANGE. REMOVED AND REPLACED T-CHORD PER BOEING BLUEPRINT 65-47952. (M) 2L72 4F RTA16WE 20050315002432005031500243NM 2005 3 15 USAA050213 120050105A53401133749 MOUNT BOEING737 7374B7 1384702NM LAVATORY CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19436US41647 24558 PIT - FOUND LAV FLOOR MOUNT CORRODED 2 INCH BY 2 INCH AREA, STATION 304, LBL 12. REPLACED FITTING PER 53-10-00. CORROSION LEVEL 1. (M) 2L72 4F RTA16WE 20050315002452005031500245NM 2005 3 15 AWXA200500311 120050304A3350321430 BATTERY AIRBUSA319 A319132 3930340NM CABIN DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28823AW 1463 PHX - EEL - DURING 4-DAY CHECK FOUND THE LT MID CABIN EMERGENCY POWER SUPPLY UNIT BATTERY FAULTED. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT LT MID CABIN EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050315002462005031500246GL 2005 3 15 UIEA200500013 220050224A7320 HMU BOEING747 74747UF 1384949NM GE CF6 CF680C GL NR 2 ENGINE MALFUNCTIONED A UIEAO OTHER J WARNING INDICATION CRCRUISE 1 EA15492MC 29253 704719 PVG/ANC - NR 2 ENGINE FAILED DURING CRUISE. EICAS AND STATUS MSG. ENGINE 2 FUEL VALVE, ENGINE 2 CONTROL. WITH NO ACTION ENGINE RESTARTED IN APPROX 90 SECONDS. FOUND ACTIVE FAULT 72417 PERFORMED WIRING CHECKS PER CMCS MESSAGE INDEX. REPLACED ECU NR 2 (P/N 1820M33P08) PER MM 73-21-15, PERFORMED ECU STATIC TESTED PER MM 71-00-00 TEST 11. PERFORMED ECU ACTUATOR GROUND TEST PER MM 71-00-00 TEST, ALL OK. REMOVED AND REPLACED NR 2 ENGINE HMU (P/N 441789) IAW 73-21-14/404-035-000. (M) 2L74 4F4 FRT1384945 E23EA 20050315002472005031500247NM 2005 3 15 USAA050220 120050130A53206553595501 REVEAL BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19532AU49225 24479 PIT - FOUND REVEAL 2 INCH CRACK, UPPER FORWARD CORNER REVEAL AT FORWARD SVC DOOR CUTOUT. INSTALLED CORNER REVEAL, STRIP AND SHIM PER EA 79829B. (M) 2L72 4F RTA16WE 20050315002482005031500248WP 2005 3 15 2005F00032 120050124A5210 HOOK DOUG DC9 DC981 3022081WP PAX DOOR HOLD OUT OF ADJUST A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FLL - FLT 1581 - MAIN CABIN DOOR HARD TO CLOSE AND LOCK APPEARS NORMAL WHEN CLOSED. ADJUSTED AND SECURED ROD FOR HOLD OPEN HOOK ON L1 DOOR, OPS CHECK IAW 52-11-04. (M) 2L72 4F A6WE 20050315002492005031500249NM 2005 3 15 USAA050215 120050128A5347655384427 CARGO TRACK BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19436US41647 24558 PIT - FOUND CARGO FLOOR TIE DOWN CRACKED .125 INCH, FLOOR TIE DOWN RBBL 13.88 STATION 767 IN RADIUS. REMOVED AND REPLACED CARGO FLOOR TIE DOWN TRACK PER SRM 51-40-02. (M) 2L72 4F RTA16WE 20050315002502005031500250NM 2005 3 15 AWXA200500312 120050305A323401215209002 CHECK VALVE BOEING737 7373G7 1384595NM NLG FAILED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28157AW 23779 LAS - AIR TURNBACK - FLT 0892 - ON CLIMBOUT OF LAS EN ROUTE FOR SEA AFTER SELECTING LANDING GEAR UP THE NOSE GEAR FAILED TO RETRACT, RECYCLED THE LANDING GEAR AND NOSE REMAINED DOWN, TURNED BACK TO LAS FOR REPAIR. MAINTENANCE REMOVED AND REPLACED 2 EACH NOSE LANDING GEAR CHECK VALVES UP LINE TO NOSE LANDING GEAR UPLOCK ACTUATOR, LEAK AND OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050315002522005031500252NM 2005 3 15 USAA050217 120050125A5320 CLIP BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19436US41647 24558 PIT - FOUND CLIP CORRODED 1 INCH BY 3 INCH AREA, FRAME 795, STRINGER 27R. CORROSION LEVEL 1, TASK C53-208-01. CUT OUT DAMAGE AND INSTALLED DOUBLER REPAIR PER EA 79752, SRM 53-00-07 FIG 207. (M) 2L72 4F RTA16WE 20050314000092005031400009SO 2005 3 14 1401022705 120050227A52101159SCB42013 SEAL GULSTMG1159 GIV 3980115SO RROYCETAY TAY6118 EU DOOR DEFLATED E N93AO OTHER O OTHER CRCRUISE 1 SO13401QS1402 1408 DOOR SEAL HAD PARTIAL DEFLATION AT FLIGHT LEVEL 410. 2L72 4F4 FRTA12EA E25NE 20050314000172005031400017CE 2005 3 14 DJFA2005064 120050309A2612 WARNING LIGHT RAYTHNDH125 HAWKER800XP 7150012CE GARRTTTFE731TFE731* 01518WP CARGO FIRE DET FALSE INDICATIONE DJFAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA23729TA 258374 CREW REPORTED, AFTER TAKEOFF, BAGGAGE FIRE WARNING LIGHT BEGAN TO FLASH APPROX 3 TO 5 TIMES, THEN QUIT. 2 MIN LATER LIGHT BEGAN TO FLASH AGAIN, THEN QUIT. AFTER EACH SERIES OF FIRE LIGHTS, AN OPS CHECK OF CIRCUITS WAS MADE BY CREW. OPS CHECKS WERE NORMAL. AFTER THIRD SERIES OF FIRE WARNING LIGHTS, CREW DECLARED AN EMERGENCY AND RETURNED TO BASE. FIRE WARNING LIGHT CONTINUED TO FLASH THROUGHOUT REMAINDER OF FLIGHT. AN UNEVENTFUL OVERWEIGHT LANDING WAS MADE. NO VISIBLE SIGNS OF SMOKE WERE OBSERVED AFTER LANDING. MAINT INSP SMOKE DETECTION SYS OF FWD BAGGAGE, AFT BAGGAGE, AND LAVATORY. GROUND TESTS NORMAL. A HEAVY WEIGHT LANDING INSP WAS ACCOMPLISHED WITH NO ABNORMAL FINDINGS NOTED. AC WAS RETURNED TO SERVICE. 2L72 4F4 FRTA3EU E6WE 20050314000192005031400019EU 2005 3 14 S9HA099036 120050124A7931704A37642043 TRANSMITTER AEROSPAS355 AS355* EU TMECA ARRIELARRIEL1 60030NE ENGINE OIL PRESSREADS LOW E S9HAO OTHER N FALSE WARNING NRNOT REPORTED 1 WP19352NT31 2553 LOW OIL PRESSURE (BELOW GREEN ARC) INDICATION THROUGH OUT FLIGHT. REPLACED PRESSURE TRANSMITTER. OHMS CHECK, INDICATE HIGH OHMS. 1G72 3U3 U H11EU E19EU 20050315000022005031500002NM 2005 3 15 DL76L050128 120050224A5753113T1226 SUPPORT BEAM BOEING767 767332 1382001NM TE FLAPS CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27179DN 25144 CORROSION FOUND IN ATTACH POINTS FOR INBOARD FLAP (NR 3), C/W ERA 089397-14MA SUBMITTED MRR PER REQUIREMENTS OF THIS ERA. 2L72 4F RTA1NM 20050315000142005031500014 2005 3 15 DLM88050130 420050223A2565D29984213 SLIDE DOUG MD88 MD88 3023688NM TAILCONE DEPLOYED A DALAD RETURN TO BLOCK W INADEQUATE Q C TXTAXI/GRND HDL 1 SO27918DL 49583 TAIL CONE WAS ACCIDENTALLY DEPLOYED AT THE GATE, SLIDE DID NOT DEPLOY. REPLACED DEPLOYMENT LANYARD AND REINSTALLED TAIL CONE. 2L72 4F RTA6WE 20050315000212005031500021NM 2005 3 15 QXEA200500307 120050223A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09413QX 4060 PDX - CORROSION ON RIGHTHAND OUTBOARD SEAT TRACK AT APPROXIMATELY X474.00, TOP AND INNER FLANGE. REPLACED SEAT TRACK IAW DHC-8 SRM 51-42-15 AND 51-42-05. 2H72 4T RTA13NM 20050315000262005031500026NE 2005 3 15 DL777050136 220050227A7200TRENT892 ENGINE BOEING777 777232 1385232NM RROYCERB211 RB211* 54555NE NR 2 MAKING METAL A DALAK NONE O OTHER ININSP/MAINT 1 SO27864DA19883 29736 051201 METAL DISCOVERED IN MCD AND SCAVAGE FILTER NR 2 ENGINE. REPLACED ENGINE. 2L72 4F4 FRTT00001SEA12EU 20050315000522005031500052EA 2005 3 15 A6WA200540052 120050215A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31421ZW 7346 FS 280 LBL 9 INBOARD ANGLE CRACKED APPROX 1 INCH LONG IN RADIUS. REPLACED ANGLE IAW CRJ SRM 51-42-06 AND 51-42-21. (M) 2L72 4F RTA21EA 20050315000732005031500073EA 2005 3 15 A6WA200540070 120050216A5753 GUIDE CNDAIRCL600 CL6002B19 1900309EA TE FLAPS WORN A A6WAK NONE O OTHER ININSP/MAINT 1 GL31421ZW 7346 LEFT OUTBOARD FLAP MID BUTTE DOOR ROLLER GUIDE IS WORN, WS 235.843. S/D - REPAIRED LEFT OUTBOARD FLAP MID BUTE DOOR ROLLER GUIDE IAW BOMBARDIER INC REO 601R-57-53-019 REV NC.(M) 2L72 4F RTA21EA 20050315000802005031500080EA 2005 3 15 A6WA200540061 120050126A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31414ZW 7586 FOUND CABIN FLOOR SUPPORT STRUCTURE AT FS 280, RBL 9 BOTH CLIPS ARE CRACKED IN RADIUS AT TOP. REPAIRED CABIN FLOOR SUPPORT STRUCTURE AT FS 280 RBL 9 IAW BRAS EO 601R-53-5924. (M) 2L72 4F RTA21EA 20050315000822005031500082WP 2005 3 15 GTIA050035 120050117A5312 BULKHEAD DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 AFT PIT FS 1338 APB FORWARD WEB CORRODED AT LONG 29L TO LONGERON 29R. REMOVED CORROSION, CUT OUT DAMAGED AREA. FABRICATED DOUBLERS AND FILLERS, TREATED PRIMED AND INSTALLED. (M) 2L72 4F A6WE 20050315000882005031500088SO 2005 3 15 SIMA200503802 120050203A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21843AE 145680 ABI - DURING AN MBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. PERFORMED A CUTOUT OF THE BEAM TO REMOVED CORROSION. FABRICATED A REPAIR DOUBLER, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB-145/1142 REV 28, CHAPTER 53-21-10 FIG 201. (M) 2L72 4F RTT00011AT 20050315000962005031500096WP 2005 3 15 GTIA050034 120050111A5313 STRINGER DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 AFT ACCESSORY COMPARTMENT STATION 1418 STRINGER 2R CRACKED. CUT AND REMOVED CRACKED STRINGER 2R STATION 1418, LOCATED AND DRILLED NEW STRINGER AND REPAIR SPLICE. TREATED, PRIMED AND INSTALLED. (M) 2L72 4F A6WE 20050315001142005031500114WP 2005 3 15 WX0500009 120050120A3260833703 PROXIMITY SENSOR DOUG DC9 DC983 3022083WP LT MLG MALFUNCTIONED A WX0AO OTHER J WARNING INDICATION APAPPROACH 1 WP19891GA 49423 LAS TO COS - LEFT MAIN UNSAFE LIGHT ILLUMINATED DURING APPROACH, EMERGENCY PROCEDURES COMPLIED WITH, MLG DOORS DOWN FOR LANDING. DOOR DAMAGED UPON ROLLOUT. AIRCRAFT INSPECTED FOR FERRY FLIGHT, GEAR PINS INSTALLED AND SAFTIED FOR GEAR DOWN FERRY FLIGHT COS TO GYR. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED LMLG DOWNLOCK PROXIMITY SENSOR AND LMLG DOOR (FUSELAGE SIDE). PERFORMED DETAILED VISUAL INSPECTION FOR HIDDEN DAMAGE ON LT AND RT MLG DOORS AND SURROUNDING AREAS, NO DEFECTS NOTED. ALL SAFTIES AND GEAR PINS REMOVED. SYSTEM OPERATIONALLY CHECKED GOOD IAW MM 32-60-05. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050315001262005031500126 2005 3 15 SWAA050439 420050215A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29774SW 27882 DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050315001292005031500129NE 2005 3 15 DL76L050114 220050216A7230 COMPRESSOR BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 2 ENGINE FAILED A DALAK NONE O OTHER ININSP/MAINT 1 SO27185DN33126 27961 727738 BORESCOPE NR 2 ENG HPC DUE TO REPORT OF HARD TO START 15FEB IN AMS REF AMM TASK 72-00-0-206-344-N00. FOUND 7TH STAGE FAILED BORO. REPLACED ENGINE. 2L72 4F4 FRTA1NM E24NE 20050315001452005031500145NM 2005 3 15 MWEA050021 120050218A3350 WARNING SYSTEM BOEING717 717200 1383700NM COCKPIT FALSE INDICATIONA MWEAK NONE N FALSE WARNING ININSP/MAINT 1 GL31905ME 55169 EMERGENCY POWER TEST FAILED. PERFORMED SATISFACTORY FIM 24-24-803. OPERATIONS CHECKED OK, AIRCRAFT OK FOR SERVICE. 2L72 4F TRA6WE 20050315001652005031500165 2005 3 15 ARWA20050207 420050221A3417001048101 SWITCHING UNIT DOUG DC10 DC1010 3022110WP COCKPIT MALFUNCTIONED A ARWAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO1968041 46900 AIRSPEED FLAGGED AT HOLDING POINT RUNWAY 9, BARBER POLE STUCK AT 250 IAS NEEDLE FLUCTUATES BETWEEN ZERO (O) AND SIXTY (60) KTS. REMOVED AND REPLACED CADC SWITCHING UNIT IN ACCORDANCE WITH MM 34-16-03. OPERATIONAL CHECK NORMAL IN ACCORDANCE WITH MM 34-16-00. 2L73 4F A22WE 20050315001742005031500174NM 2005 3 15 AALA20050168 120050221A5320 SILL BOEING767 767323 1385205NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW2139364 24045 AFW - LEFTHAND LOWER SILL EMERGENCY EXIT OUTER CHORD AT STATION 861 HAD CORROSION BLENDED FROM UPPER FLANGE. AREA OF CORROSION IS 0.9 BY 3.7 WITH A DEPTH OF 0.062. REMOVED CORROSION AND DYE CHECKED AREA FOR CRACKS. HFEC THE HOLES WHERE FASTENERS WERE REMOVED. REFINISH THE BLENDED AREA WITH ALODINE AND TWO COATS BMS 10 11 PRIMER. REINSTALL FASTENERS WET WITH SEALANT, ENSURED PROPERLY SEALED. 2L72 4F RTA1NM 20050315001772005031500177NM 2005 3 15 AALA20050167 120050218A5315 FLOORBEAM BOEING767 767323 1385205NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW2139364 24045 AFW - TOP CAP OF FLOORBEAM AT STATION 325 RIGHT BUTTLINE 40 CORRODED. BLENDED BEYOND SRM LIMITS. AREA IS ONE INCH BY ONE INCH WITH DEPTH OF 0.10 BY 0.044 INCH FROM PARENT 0.090 INCH. REMOVED CORROSION. FABRICATED REPAIR STRAP OUT OF 301 1/2 H STAINLESS STEEL 0.050 INCH THICK. ALODINE ALL BARE ALUMINUM SURFACES. FINISHED BLENDS AND REPAIR PARTS WITH TWO COATS OF BMS10 11 PRIMER. FILLED BLEND WITH BMS 5 95 SEALANT. INSTALLED REPAIR STRAP WET WITH BMS 5 95 SEALANT. FASTENERS INSTALLED WITH 4 60 SPACING. 2L72 4F RTA1NM 20050315001792005031500179NM 2005 3 15 AALA20050153 120050221A5320BAC1518338 FLOOR SUPPORT BOEING757 757223 1384957NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21653A 24611 TUL - FLOORBOARD SUPPORT IS CORRODED TOP INSIDE RIGHT OF LEFT NUMBER ONE DOOR AFT CORNERS IN AN AREA OF ONE BY THREE INCHES. REPAIRED SUPPORT PER ESO 90309 DATED 2/21/05. 2L72 4F RTA2NM 20050315001882005031500188WP 2005 3 15 AALA20050155 120050225A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21579AA 53156 MSP - FORWARD OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD OVERWING EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050315001972005031500197WP 2005 3 15 AALA20050158 120050228A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21249AA 49269 MIA - OVERHEAD EMERGENCY LIGHTS ABOVE SEAT ROWS 7 TO 10 INOPERATIVE. REPLACED BATTERY PACK AFT OF SET ROW 8DEF FOR OVERHEAD EMERGENCY LIGHTS ABOVE SEAT ROWS 7 TO 10. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050315002542005031500254NM 2005 3 15 AWXA200500314 120050212A5320654795711 STRAP BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON AFT CARGO COMPARTMENT DOOR SILL UPPER STRAP BETWEEN BS 794 AND BS 847 AT STR 25 RT. MAINTENANCE REMOVED CORRODED SECTION AFT CARGO DOOR SILL UPPER STRAP FROM BS 794 TO BS 847 AT STR 25 RT; FABRICATED A NEW REPLACEMENT STRAP; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-05, FIG 2. 2L72 4F RTA16WE 20050315002552005031500255NM 2005 3 15 USAA050218 120050125A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19577US51711 23742 PIT - FOUND SKIN CRACKED .25 INCH, AFT SERVICE DOOR TOP HINGE CUTOUT. INSTALLED DOUBLER REPAIR PER SRM 53-60-01. (M) 2L72 4F RTA16WE 20050315002562005031500256NM 2005 3 15 USAA050219 120050126A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19577US51711 23742 PIT - FOUND SKIN CRACKED THREE PLACES, .125 INCH .8750 INCH AND .125 INCH, E/E COOLING DUCT SKIN, LOWER FUSELAGE BS 380 S27R AND S27L. SKIN DOUBLER INSTALLED PER EO 5300V258. (M) 2L72 4F RTA16WE 20050315002572005031500257NM 2005 3 15 AWXA200500315 120050212A531165479592 FRAME BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON AFT CARGO DOOR FORWARD TORQUE BOX FRAME AT BS 794.3, STR 25 RT. MAINTENANCE REMOVED CORRODED SECTION AFT CARGO DOOR FORWARD TORQUE BOX FRAME AT BS 794.3, STR 25 RT; FABRICATED A NEW REPLACEMENT SECTION OF FRAME; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050315002602005031500260NM 2005 3 15 USAA050291 120050215A57546526601197 SKIN BOEING737 7374B7 1384702NM NR 1 SLAT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19438US 24560 PIT - NR 1 SLAT WITH FIVE CRACKS .1875 INCH CRACKS, LOWER SKIN UNDER OUTBOARD SLAT FITTING, AFT RIVET ROW. INSTALLED DOUBLER PER SRM 57-43-01. (M) 2L72 4F RTA16WE 20050315002612005031500261EU 2005 3 15 AWXA200500318 120050307A3350DHE1141 PROXIMITY SWITCH AIRBUS320 A320232 3930326EU CABIN DEFECTIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28661AW 1284 PHX - EEL - DURING E-5 CHECK WHILE PERFORMING OPERATIONAL CHECK OF OVERWING SLIDE ARMED LIGHTS, FOUND THE RT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED PROXIMITY SWITCH (5WN2) IAW AMM 52-73-11-04, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050315002622005031500262NM 2005 3 15 AWXA200500319 120050218A5321D5367160100000 FLOOR PANEL AIRBUSA319 A319132 3930340NM FUSELAGE DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28812AW 1178 SAL - MAJOR REPAIR - DURING BC-4 CHECK FOUND FLOOR PANEL 251RF DELAMINATED. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL 251RF IAW A319 SRM 53-02-00 FIG 209. 2L72 4F RTA28NM 20050315002632005031500263NM 2005 3 15 USAA050223 120050101A5752654645521C STRUCTURE BOEING737 7374B7 1384702NM AILERON TAB CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19443US38634 24842 PIT - FOUND AILERON TAB CRACKED 2 INCHES, OUTBOARD TRAILING EDGE, OF LEFT AILERON TAB. REPLACED AILERON TAB PER MM 27-11-21. (M) 2L72 4F RTA16WE 20050315002642005031500264NM 2005 3 15 USAA050292 120050216A52306547952340 SKIN BOEING737 7374B7 1384702NM AFT CARGO DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19438US 24560 PIT - FOUND AFT CARGO DOOR CRACKED .5 INCH, UPPER AFT CORNER OF HANDLE/FLAPPER CUTOUT TO RIVET. REMOVED DAMAGE, INSTALLED DOUBLER PER SRM 52-00-01 FIG 202. (M) 2L72 4F RTA16WE 20050315002662005031500266NM 2005 3 15 USAA050293 120050217A521050795264 SKIN BOEING737 7374B7 1384702NM FWD ENTRY DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19438US 24560 PIT - FOUND FORWARD ENTRY DOOR CRACKED FOUR PLACES, .5 INCH EACH, INNER SKIN AFT EDGE AT BEAM 3, 4, 5, 6 STOP CUTOUTS. REMOVED DAMAGE, INSTALLED DOUBLER PER TYPICAL REPAIR 52-10-16. (M) 2L72 4F RTA16WE 20050315002672005031500267NM 2005 3 15 AWXA200500321 120050214A57536546431280 SKIN BOEING737 7373G7 1384595NM T/E FLAP DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28307AW 24634 MCN - MAJOR REPAIR - DURING C-14 CHECK FOUND THE UPPER RT OUTBOARD FORE FLAP DELAMINATED 92 INCHES FROM THE INBOARD END BETWEEN WBL 294.19 AND WBL 295.19. MAINTENANCE REMOVED DAMAGE ON UPPER SKIN OF RT OUTBOARD FORE FLAP FROM WBL 294.19 TO WBL 295.19; FABRICATED A SECTION OF REPLACEMENT SKIN AND A DOUBLER; BONDED REPAIR PARTS TO FORE FLAP IAW B737-300 SRM 51-70-10 FIG 31. 2L72 4F RTA16WE 20050315002682005031500268NM 2005 3 15 USAA050282 120050216A5320 FLOOR SUPPORT BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19519AU50516 23705 CLT - FOUND FLOOR SUPPORT CORRODED 1 INCH BY 1 INCH, AFT STATION 727D FLOOR SUPPORT ANGLE RBL 2.5. INSTALLED REPAIR DOUBLER IAW TR 53-10-06. (M) 2L72 4F RTA16WE 20050315002692005031500269NM 2005 3 15 USAA050283 120050216A5315 FLOORBEAM BOEING737 7373B7 1384580NM FUSELAGE DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19519AU50516 23705 CLT - FOUND FLOORBEAM WITH HOLE .250 INCH, STATION 328 RBL 25. ACCOMPLISHED T-CAP REPAIR IAW SRM 53-10-51. (M) 2L72 4F RTA16WE 20050315002712005031500271NM 2005 3 15 USAA050284 120050216A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19519AU50516 23705 CLT - FOUND SKIN CRACKED .5 INCH, BETWEEN STATIONS 360-390 E/E BAY. INSTALLED DOUBLER IAW EA 62978. (M) 2L72 4F RTA16WE 20050315002742005031500274NM 2005 3 15 AWXA200500316 120050216A575465C26602274 WEDGE BOEING737 7373G7 1384595NM L/E SLAT DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28307AW 24634 MCN - MAJOR REPAIR - DURING C-14 CHECK FOUND THE NR 5 SLAT WEDGE DELAMINATED AT INBOARD END, SLAT STA 257. MAINTENANCE REMOVED DELAMINATED AREA OF NR 5 SLAT WEDGE; FABRICATED A FILLER AND DOUBLER; BONDED REPAIR PARTS TO SLAT IAW B737-300 SRM 51-70-10 FIG 31. 2L72 4F RTA16WE 20050315002772005031500277SO 2005 3 15 C2XA05RI003 120050303A3350AD20131A POWER SUPPLY EMB 145 EMB145LR 3260212SO CABIN DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714543 14 14553 RIC - DURING ROUTINE INSPECTION, MAINTENANCE FOUND FLOOR EMERGENCY LIGHT STRIPS (AFT) OF EMERGENCY EXIT INOP AND EXTERIOR LEFT AND RIGHT AFT OVERWING EMERGENCY LIGHTS ALSO INOP. MAINTENANCE REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY POWER SUPPLY. OPERATIONAL CHECKS PERFORMED SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20050315002782005031500278SW 2005 3 15 2005F00046 120050208A2432 BATTERY BELL 206 206B 1181511SW MASTER OVERHEATED A ALGAO OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW0335WH 2736 WHILE HOT REFUELING, CUSTOMER NOTICED SMOKE/STEAM AND ACID VENTING FROM UNDER THE NOSE OF THE AIRCRAFT. BATTERY WAS VERY HOT TO THE TOUCH BUT THE BATTERY TEMPERATURE OR BATTERY HOT LIGHT WERE NOT ILLUMINATED. THE BATTERY WAS TURNED OFF AND THE AIRCRAFT WAS SHUT DOWN. MAINTENANCE REMOVED AIRCRAFT BATTERY SERIAL NUMBER 106999 AND INSTALLED SERVICEABLE BATTERY SERIAL NUMBER 112458. ALSO, REMOVED SENSOR SERIAL NUMBER EL-488 AND INSTALLED NEW SERVICEABLE SENSOR. OPS CHECK OK ON BOTH THE BATTERY AND THE SENSOR SYSTEMS. ALL WORK DONE IAW BHT 206BIII MM. (M) 1G71 3U H2SW 20050315002792005031500279SW 2005 3 15 2005F00047 120050127A6340 SENSOR BELL 407 407 1182206SW TACH GEN DIRTY A ALGAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 SW03417AL 53054 DURING TAKEOFF, THE RPM LIGHT AND HORN CAME ON. MAINTENANCE CLEANED THE NR SENSOR CONNECTOR AND GROUND OPS CHECKED GOOD, ALSO COMPLIED WITH OPS CHECK FLIGHT AND FLIGHT CHECK WAS GOOD. (M) 1G71 3U O H2SW 20050315002832005031500283SO 2005 3 15 C2XA05IA039 120050304A335020131A BATTERY PACK EMB 145 EMB145ER 3260211SO CABIN DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713936147102167 145025 IAH - FLIGHT 2057, DURING PREFLIGHT INSPECTION, THE CREW REPORTED SEVERAL EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050315002852005031500285SO 2005 3 15 C2XA05IA043 120050307A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN MALFUNCTIONED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715983 145239 IND - FLIGHT 2428, THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHT AFT OF ROW 12 WAS INOPERATIVE. THE EMERGENCY LIGHT WAS PLACED ON MEL 33-50-00/2 CONTROL NUMBER 049776, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED IN IAH ON FLIGHT 2428 WHERE MAINTENANCE OPERATIONALLY CHECKED THE EMERGENCY LIGHTS WITH NO DEFECTS FOUND, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050315002862005031500286GL 2005 3 15 2005F00049 220050121A7200 ENGINE BELL 206 206L4 1182110SW ALLSN 250C 250C30P 03013GL MALFUNCTIONED A ALGAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW0369AL 52139 DURING TAKEOFF, WITH POWER ABOVE 80 PERCENT TORQUE AIRCRAFT BEGINS VIBRATIONS INCREASING TO SEVERE WITH OSCILLATION BETWEEN 20-30 PERCENT ON TORQUE GAUGE. MAINTENANCE REMOVED AND REPLACED ENGINE ASSY WITH SERVICABLE SERIAL NUMBER CAE-890158. WORK DONE IAW BELL 206L-4 AND ROLLS ROYCE MAINTENANCE MANUALS. COMPLIED WITH OPS CHECK FLIGHT, PLUS 8 ON BELL POWER CHECK NO OTHER DEFECTS NOTED. (M) 1G71 3U3 UNCH2SW E1GL 20050315002872005031500287NM 2005 3 15 USAA050286 120050217A5315 FLOORBEAM BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19519AU 23705 CLT - FOUND FLOORBEAM T-CAP CORRODED .5 INCH BY .5 INCH, STATION LBL 34 TO RBL 60. INSTALLED T-CAP IAW SRM 53-10-51. (M) 2L72 4F RTA16WE 20050315002882005031500288SO 2005 3 15 C2XA05CL014 120050303A3350AD20131A BATTERY PACK EMB 145 EMB145LR 3260212SO CABIN DISCHARGED A C2XAK NONE L NO TEST TXTAXI/GRND HDL 1 SW2714543 145553 CLE FLIGHT 2948, THE CREW REPORTED OVERHEAD EXIT SIGNS AND AISLE PATH LIGHTING INOP. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHTING BATTERY PACK AND THE OPERATIONAL CHECK WAS GOOD. 2L72 4T RTT00011AT 20050315002902005031500290NM 2005 3 15 USAA050295 120050218A5313 STRINGER BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU50570 23706 PIT - FOUND STRINGER CRACKED 3 INCHES, BS 1138 S5A LEFT. TRIM OUT DAMAGE AND SPLICE IN NEW SECTION OF STRINGER PER TYPICAL REPAIR 53-80-04. (M) 2L72 4F RTA16WE 20050315002932005031500293NM 2005 3 15 USAA050300 120050209A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE DENTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU50570 23706 PIT - FOUND SKIN DENTED AND PUNCTURED, 1 INCH BY 1 INCH BY .125 INCH, BETWEEN S-26R AND S27R AND STA 500D PLUS 10 INCHES. REPAIR DOUBLER INSTALLED PER SRM 53-00-01 FIG 229 DETAIL XII. (M) 2L72 4F RTA16WE 20050315002952005031500295SO 2005 3 15 C2XA05TY024 120050228A321014567115406 HOUSING EMB 145 EMB145LR 3260212SO RT MLG CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714952 145067 TYS DURING A 4C INSPECTION THE RIGHT MLG FWD HOLLOW PIN HOUSING WAS FOUND WITH AREAS OF PITTING. AFTER MAINTENANCE REMOVED THE PITTING IT WAS BEYOND LIMITS AND A EC WAS CUT FOR THE REPAIR (EC5750-01239). THE HOLLOW PIN HOUSING WAS REPLACED IAW EC5750-01239. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20050315002972005031500297NM 2005 3 15 USAA050255 120050215A5320 CHANNEL BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19519AU50516 23705 CLT - FOUND U-CHANNEL WITH CORROSION ALONG ENTIRE LENGTH, FORWARD ENTRANCE DOOR SILL PLATE U-CHANNEL. REPLACED CHANNEL IAW SRM 51-10-02. (M) 2L72 4F RTA16WE 20050315002982005031500298NM 2005 3 15 USAA050256 120050215A5311 FRAME BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19519AU50516 23705 CLT - FOUND FRAME CRACKED .3750 INCH, STATION 887 STRINGER 9R. INSTALLED FILLER/DOUBLER IAW TR 53-10-20A. (M) 2L72 4F RTA16WE 20050315002992005031500299NM 2005 3 15 USAA050257 120050215A5311 FRAME BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19519AU50516 23705 CLT - FOUND FRAME CRACKED .5 INCH, STATION 827 STRINGER 9R. INSTALLED FILLER/DOUBLER IAW TR 53-10-20A. (M) 2L72 4F RTA16WE 20050315003002005031500300NM 2005 3 15 USAA050281 120050211A523005298 DOOR FRAME BOEING737 737301 1384611NM CARGO DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19585US51939 23930 PIT - FOUND DOOR WITH THREE .5 INCH CRACKS, AFT CARGO DOOR FORWARD FRAME. REMOVED AND REPLACED DOOR PER JOB CARD J3-57-52301. (M) 2L72 4F RTA16WE 20050315003022005031500302EA 2005 3 15 A6WA200540078 120050213A5320601R3117101 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31421ZW 7346 FOUND ANGLE CRACKED FS 484 AT RBL 27. REMOVED AND REPLACED ANGLE CLIP, IAW BOMBARDIER REO 601R-53-41-059. (M) 2L72 4F RTA21EA 20050315003042005031500304NE 2005 3 15 BJNA05021 220050211A7200 ENGINE BOEING737 737282 13844ATNM PWA JT8 JT8D17A 52049NE NR 2 FAILED A BJNAC ABORTED TAKEOFF EXJVIBRATION/BUFFET ENGINE FLAMEOUT WARNING INDICATION TOTAKEOFF 1 WP11344TM 23044 709303 NR 2 ENGINE FAILED ON THE BEGINNING OF TAKEOFF ROLL, 1.6 EPR HARD COMPRESSOR STALL AND ROLL DOWN. INSPECTION REVEALED EXTENSIVE DAMAGE TO THE T-1 THROUGH T-4 TURBINE BLADES, TURBINE FAILURE WAS CONTAINED. ENGINE TOTAL TIME 550207, TOTAL CYCLES 52176. SINCE LAST SOP VISIT 4178 HOURS, 2649 CYCLES. (M) FAILURE CAUSE NOT DETERMINED, ENGINE SOLD. (K) 2L72 4F4 FRTA16WE E2EA 20050315003082005031500308NM 2005 3 15 UIEA200500008 120050222A2612 FIRE LOOP BOEING747 7472D7B 1384803NM NR 4 ENGINE CHAFED A UIEAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 EA15526MC 22337 FLT EI 9867 - ON TAKEOFF ROLL, NR 4 ENGINE FIRE WARNING LIGHT AND BELL CAME ON. MAX BRAKES APPLIED AT 95 KTS. TAKEOFF ABORTED. INSPECTED NR 4 ENGINE, NO PRIMER DISCOLORATION OR ANY SIGN OF HEAT DAMAGE. PERFOMED NR 4 ENGINE PNEUMATIC LEAK CHECK, NORMAL PER 71-00-00. PERFORMED HIGH ENERGY STOP HEAT DAMAGE CONDITION INSPECTION. ALL NORMAL PER AMM 5-51-10. CHECKED NR 4 ENGINE FIRE DETECTION SYSTEM A AND B. REPAIRED INSULATION CHAFFED WIRING B-LOOP AT 12 AND 3 O'CLOCK POSITION PER 26-11-52. PERFORMED ENGINE HIGH POWER RUN UP CHECK, ALL NORMAL. REF LOG PAGES 542971, 542972 AND 542973. (M) 2L74 4F RTA20WE 20050315003092005031500309CE 2005 3 15 2005F00050 120050129A52601294000371 SEAL BEECH 1900 1900D 1154162CE AIRSTAIR DOOR TORN A GUUAO OTHER O OTHER CRCRUISE 1 SO1787557 UE246 FLT 9197 - TPA/FLL - DURING FLIGHT, CABIN EXPERIENCED RAPID DECOMPRESSION. PAX OXYGEN MASKS DEPLOYED. DIVERTED TO RSW. LANDED WITHOUT INCIDENT. NO EMERGENCY DECLARED. FOUND AIRSTAIR DOOR SEAL OUT OF TRACK AND TORN AT 12 O'CLOCK POSITION. REMOVED AND REPLACED DOOR SEAL AND STOWED OXYGEN MASKS. OPERATIONAL CHECK NORMAL. (M) 2L72 4T RTA24CE 20050315003122005031500312EU 2005 3 15 2005F00052 120050218A2612875136 SENSING ELEMENT FOKKERF28 F28MK4000 4990810EU RROYCESPEY SPEY* NE NR 2 ENGINE SHORTED A BUEAE ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 GL23159AD 11227 9213 FIRE WARNING ON THE NR 2 ENGINE INFLIGHT, THE NR 2 ENGINE FIRE WARNING SYSTEM WOULD NOT TEST. THE ENGINE WAS SHUTDOWN AND THE NR 1 FIRE BOTTLE DISCHARGED. (M) 2L72 4F4 TRTA20EU E2EU 20050315003152005031500315NM 2005 3 15 SWAA050650 120050302A53126546568 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29329SW 23693 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE WEB CRACK AT DOME CAP, BS 1016, AFT PRESSURE BULKHEAD. REPAIRED WEB PER SWA EA. 2L72 4F RTA16WE 20050315003172005031500317NM 2005 3 15 SWAA050701 120050307A55516551524 FITTING BOEING737 7373H4 1384600NM HORIZ STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29607SW 27927 DURING SCHEDULED D-CHECK, FOUND LT & RT HORIZONTAL STAB FITTING LUG FACES CORRODED. REPAIRED FITTINGS PER SRM. 2L72 4F RTA16WE 20050315003182005031500318WP 2005 3 15 GTIA050024 120050209A5320 CUSP WEB DOUG DC9 DC982 3022082WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 REPAIRED CRACK AT CUSP WEB FS 788 LBL 44, NUMEROUS OVERSIZED HOLES IN CUSP WEB TO FS 845 LBL 44. REMOVED CUSP WEB FROM FS 778-798 LBL 44, FABRICATED CUSP WEB FROM 7075-T6 .025, TREATED, PRIMED AND INSTALLED CUSP WEB. (M) 2L72 4F A6WE 20050315003192005031500319WP 2005 3 15 GTIA050016 120050124A3231 DOOR DOUG DC9 DC982 3022082WP NLG LACK OF LUBE A GTIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23803NK 48087 ACY - FLT 341 - AFTER TAKEOFF CYCLED NLG AND HAD A GEAR UNSAFE INDICATION AND A LOUD NOISE FROM GEAR DOORS BEING OPEN, DID A FLY BY AND TOWER NOTICED GEAR RETRACTED WITH GEAR DOORS STILL OPEN AND GEAR LEVER UP. AIRCRAFT RETURN TO ACY AND PERFORMED AN OVERWEIGHT LANDING. LUBED NLG DOOR ASSY AND JACKED NOSE WITH BALLAST WEIGHT AND PERFORMED NOSE GEAR RETRACTION AND EXTENSION. OPS CHECK NORMAL. CHECKED NOSE UPLOCK AND SAFE PROX SIGNAL OK. (M) 2L72 4F A6WE 20050315003212005031500321NM 2005 3 15 SWAA050703 120050307A53116546555 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29607SW 27927 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050315003232005031500323NM 2005 3 15 SWAA050704 120050307A53116558280 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29607SW 27927 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, ABOVE STR 8R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050315003242005031500324NM 2005 3 15 SWAA050705 120050307A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29607SW 27927 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050315003252005031500325WP 2005 3 15 GTIA050020 120050204A7700 LINE DOUG DC9 DC981 3022081WP PT 7 MANIFOLD BROKEN A GTIAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 GL23818NK 48018 RIGHT ENGINE PER ABNORMAL ON TAKEOFF, N1 WAS 93 PERCENT WITH RIGHT EPR 1.30, GATE RETURN AIRCRAFT TAIL SWAP. FOUND MANIFOLD LINE BROKEN AT THE PT7 MANIFOLD MOISTURE TRAP. REMOVED AND REPLACED MANIFOLD LINE, ENGINE OPS CHECK GOOD DURING RUN UP. (M) 2L72 4F A6WE 20050315003262005031500326NM 2005 3 15 SWAA050706 120050307A53106546956 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29607SW 27927 DURING SCHEDULED D-CHECK, FOUND CORROSION ON FUSELAGE CREASE BEAM WEB AT BS 410, STR 17R. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM. 2L72 4F RTA16WE 20050315003292005031500329NM 2005 3 15 SWAA050708 120050307A53116546558 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29607SW 27927 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050315003312005031500331WP 2005 3 15 GTIA050011 120050119A3213 STRUT DOUG DC9 DC981 3022081WP NLG LEAKING A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 DTW - FLT 1039 - NOSE GEAR WOULD NOT RETRACT. REPACKED NOSE STRUT, LEAK CHECK GOOD, SWUNG NOSE GEAR, OPS CHECK GOOD. (M) 2L72 4F A6WE 20050315003322005031500332NM 2005 3 15 SWAA050709 120050307A53106546569 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29607SW 27927 DURING SCHEDULED D-CHECK, FOUND CORROSION ON SHEAR TIE AT BS 1006, BL 0, WL 180. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050315003332005031500333 2005 3 15 GTIA050005 420050111A2565 LANYARD DOUG DC9 DC982 3022082WP ESCAPE SLIDE BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 FLL - L1 ESCAPE SLIDE LANYARD BROKEN. INSTALLED NEW LANYARD ON L1 DOOR SLIDE. (M) 2L72 4F A6WE 20050315003342005031500334NM 2005 3 15 SWAA050710 120050307A3350101073 LENS BOEING737 7375H4 138449DNM CABIN OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29507SW 24184 DURING SCHEDULED 1/2D CHECK, R1 DOOR EMERGENCY EXIT LIGHT COVER FELL OFF. REINSTALLED COVER PER MM. 2L72 4F RTA16WE 20050315003352005031500335WP 2005 3 15 GTIA050004 120050110A5610 WINDSHIELD DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23829NK 49931 TPA - FLT 631 - CAPTAINS WINDSHIELD IS CRACKED. REMOVED AND REPLACED CAPTAINS WINDSHIELD. (M) 2L72 4F A6WE 20050315003382005031500338NM 2005 3 15 SWAA050692 120050307A53306545774 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29664WN 23495 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 743, ABOVE STR 20L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050315003402005031500340WP 2005 3 15 GTIA050015 120050123A2497914F5674 RELAY DOUG DC9 DC983 3022083WP CROSS TIE INOPERATIVE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23834NK 49847 DTW - FLT 706 - AIRCRAFT CROSS TIE WILL NOT RESET, AIRCRAFT TAIL SWAP. REMOVED AND REPLACED AC CROSS TIE RELAY. (M) 2L72 4F RTA6WE 20050315003422005031500342NM 2005 3 15 SWAA050695 120050306A5230BAC1505 FRAME BOEING737 7373Q8 1384670NM AFT CARGO DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29317WN 24068 DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR MID FRAME CRACKED. REMOVED AND REPLACED CARGO DOOR PER MM. 2L72 4F RTA16WE 20050315003432005031500343WP 2005 3 15 GTIA050010 120050118A3213 STRUT DOUG DC9 DC982 3022082WP NLG ICED A GTIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23820NK 49126 FLT 202 - DTW - AFTER TAKEOFF GEAR WOULD NOT RETRACT, RETURNED TO DTW, NORMAL LANDING WEIGHT FOR LANDING, AIRCRAFT TAIL SWAP. UPON INSPECTION, FOUND NOSE STRUT PACKED WITH ICE, CLEANED, REPACKED AND SERVICED. (M) 2L72 4F A6WE 20050315003462005031500346EU 2005 3 15 YENA200519 120050225A5270DHE1141 PROXIMITY SWITCH AIRBUS320 A320232 3930326EU EMERGENCY EXIT INOPERATIVE A YENAK NONE O OTHER CRCRUISE 1 EA15593JB 2280 RIGHT OVERWING SLIDE DOES NOT INDICATE ARMED. REMOVED AND REPLACED PROXIMITY SWITCH FIN 5WN2 PER AMM 52-73-11, SYSTEM CHECKS NORMAL AT THIS TIME. 2L72 4F RTA28NM 20050315003472005031500347 2005 3 15 YENA200520 420050228A2330 ENTERTAIN SYS AIRBUS320 A320232 3930326EU CABIN MALFUNCTIONED A YENAK NONE B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 EA15503JB 1123 FAINT BURNING SMELL FOR SHORT DURATION SMELLED ON FRONT GALLEY. COMPLIED WITH INFO NOTICE 2004-T023TR. ALSO COMPLIED WITH TSM TASK 24-00-00-801-832. LTV FOUND TO BE INOP ALL CHANNELS, MEL'D LTV SYS (REF L/P 88796 ITEM 1). NO OTHER SMELLS OR SMOKE NOTED DURING TEST. UPON ARRIVAL AT JFK ACCOMPLISHED INFO NOTICE 2004-T023 TR, FOUND TVS WORKING SATISFACTORY AND AT THIS TIME NO BURNING SMELL NOTICED. MEL CLEARED. NO COMPONENTS CHANGED. 2L72 4F RTA28NM 20050315003482005031500348EU 2005 3 15 YENA200521 120050228A2120 SMOKE AIRBUS320 A320232 3930326EU CABIN DETECTED A YENAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15588JB 2201 CREW FROM FLIGHT 418 REPORTED POSSIBLE RUBBER SMOKE IN THE CABIN. ACCOMPLISHED INFO NOTICE 2004-T023 TR. LIVE TV OPERATION NORMAL NO FAULTS FOUND. NO EVIDENCE OF RUBBER SMOKE ODOR IN THE CABIN. NO COMPONENTS CHANGED. 2L72 4F RTA28NM 20050315003532005031500353EA 2005 3 15 05060701 120050301A3620 THERMAL SWITCH CNDAIRCL600 CL6002B19 1900309EA BLEED AIR SYS FAILED A VTZAK NONE N FALSE WARNING DEDESCENT 1 EA27701BR 7448 EVENT SUMMARY STATED 14TH STAGE BLEED AIR FAIL. REMOVED AND REPLACED STANDBY THERMAL SWITCH & HEAT SENSOR. 2L72 4F RTA21EA 20050315003542005031500354EA 2005 3 15 05064645 120050305A2751 BPSU CNDAIRCL600 CL6002B19 1900309EA T/E FLAP FAILED A VTZAK NONE J WARNING INDICATION APAPPROACH 1 EA27645BR 7383 EVENT SUMMARY STATED FLAP FAIL AT ZERO DEGREES. REMOVED AND REPLACED RT BPSU. OPS CHECK GOOD. 2L72 4F RTA21EA 20050315003552005031500355 2005 3 15 VTZA200500008 420050308A3418 STALL WARNING CNDAIRCL600 CL6002B19 1900309EA COCKPIT ACTIVATED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27654BR 7454 STALL FAIL MESSAGE ON TAKEOFF. FOUND AOA VANE DISAGREE CODE. 2L72 4F RTA21EA 20050315003562005031500356EA 2005 3 15 VTZA200500006 120050307A531260034017595 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A VTZAO OTHER O OTHER ININSP/MAINT 1 EA27639BR 7313 RT SIDE PILOTS BULKHEAD AT FS 280 BETWEEN RBL 9.0 AND LBL 9.0 HAS CORROSION ON WEB. 2L72 4F RTA21EA 20050315003642005031500364NM 2005 3 15 2005UALA00214 120050307A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29582UA 26702 BS 365 FLOORBEAM CORRODED BEYOND LIMITS BETWEEN RBL 59 TO BL 0. TEE CAP WAS TRIMMED AND REPAIR ANGLES AND STRAPS WERE USED TO SPLICE IN NEW SECTION OF TEE CAP. 2L72 4F4 FRTA2NM E17NE 20050315003652005031500365NM 2005 3 15 2005UALA00215 120050307A5320 SHEAR WEB BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29582UA 26702 SHEAR WEB AT STA 1680, RBL 74 IS CORRODED. REPAIR DOUBLERS WERE INSTALLED TO REPAIR THE AFT PRESSURE DECK WEB. 2L72 4F4 FRTA2NM E17NE 20050316000032005031600003EA 2005 3 16 6045487022205 120050222A2430 IDG CNDAIRCL600 CL6002B19 1900309EA NR 1 MALFUNCTIONED E J7SAC ABORTED TAKEOFF HJ ELECT. POWER LOSS-50 PC WARNING INDICATION TOTAKEOFF 1 SW05330FX 5487 LEFT NR 1 GEN FAIL ON TAKEOFF, WAS ABLE TO RESET. CREW ABORTED TAKEOFF AT 80 KTS AND RETURNED TO MAINTENANCE HANGER. MAINTENANCE FOUND IDG LOW ON OIL. SERVICED OIL AND FUNCTIONED CHECK PERFORMED WITH NO DEFECTS NOTED. 2L72 4F RTA21EA 20050316000052005031600005NM 2005 3 16 QXEA200500349 120050302A2913570347 PUMP DHAV DHC8 DHC8202 2809007NM HYD SYSTEM FAILED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09345PH16231182 476 SEA - FLIGHT 2074 - THE FLIGHT RETURNED TO THE GATE AFTER RECEIVING A NR 2 ENGINE HYDRAULIC PUMP CAUTION. MAINTENANCE INSPECTED THE SYSTEM AND REPLACED THE NR 2 ENGINE DRIVEN PUMP. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050316000062005031600006NM 2005 3 16 DL767050144 120050228A533014335212 SKIN BOEING767 767232 1385132NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27112DL 22224 THE FUSELAGE SKIN WAS DAMAGED BY GROUND EQUIPMENT AT FS 643 NEAR STRINGER 28R. THE DAMAGE WAS REMOVED WITH A 4.5 X 3 INCH CUTOUT IN THE SKIN. THE SKIN WAS REPAIRED WITH AN ALUMINUM DOUBLER PER ER/A 097220-14, REV A. 2L72 4F RTA1NM 20050316000092005031600009NM 2005 3 16 DL76L050147 120050302A2750 PDU BOEING767 767332 1382001NM SPARKS A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27196DN 28453 SPARKS COMING FROM PDU 9L IN AFT CARGO DURING LOADING. REPLACED RECEPTACLE. 2L72 4F RTA1NM 20050316000122005031600012NE 2005 3 16 NACA20050008 220050308A8530356995 CYLINDER DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE NR 10 FAILED A NACAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CRCRUISE 1 AL03438721174 1174 533294 P32304 NR 1 ENGINE SHUT DOWN AFTER BACKFIRING IN CRUISE AND COULD NOT RE-LEAN. REPLACED NR 10 CYLINDER DUE TO EXHAUST VALVE FAILURE. OP AND LEAK CHECK GOOD. COMPRESSION CHECK OF NR 15 CYLINDER GOOD, REPLACED WITH NEW SPARK PLUGS. 2L74 4R4 R A781 5E8 20050316000132005031600013NM 2005 3 16 2005UALA00216 120050307A5310 CREASE BEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29582UA 26702 RIGHT CREASE BEAM WEB CORRODED BETWEEN BS 1380 AND 1400 RT SIDE. DAMAGE CAUSED BY CORROSION TYPICAL FOUND ON CREASE BEAMS. CREASE BEAM WEB REPLACEMENT WAS FABRICATED AND INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050316000142005031600014NM 2005 3 16 DL764050152 120050307A2530 OVEN BOEING767 767432ER 1385134NM GALLEY ODOR A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27843MH 29716 F/A REPORTED A BURNING RUBBER SMELL IN THE NR 4 OVEN. CLEANED NR 4 OVEN. 2L72 4F RTA1NM 20050316000152005031600015NM 2005 3 16 DLM90050153 120050309A25304110001137 COFFEEMAKER DOUG MD90 MD9030 3023690NM GALLEY DIRTY A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 SO27904DA 53384 CLEANED BURNED COFFEE FROM HOT PLATE IN AFT GALLEY DUE TO BURNING SMELL. 2L72 4F RTA6WE 20050316000172005031600017NM 2005 3 16 DL738050156 120050310A3320 BALLAST BOEING737 737832 13844CFNM GALLEY LIGHTS OVERHEATED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27372DA 29620 TWENTY MINUTES IN FLT F/A REPORTED ELEC FUMES IN THE AFT GALLEY. THE F/A CHECKED OVENS AND COFFEEMAKERS AND THERE WERE NO PROBLEMS. THE FLT PERFORMED THE QRH PROCEDURES BY SECURING THE GALLEY PWR AND FAN C/B. MTC FOUND THE LIGHT BALLAST FOR THE AFT GALLEY OVERHEAD LIGHTS OVERHEATED. REPLACED LIGHT BALLAST. 2L72 4F RTA16WE 20050316000202005031600020NM 2005 3 16 2005UALA00217 120050307A5347 SEAT TRACK BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29117UA 28810 CABIN SEAT TRACK AT LBL 33.39 STA 1063-1218 IS FOUND TO BE OUT OF LIMIT AFTER DAMAGE REMOVAL. *S/D* MAJOR REPAIR ACCOMPLISHED. SEAT TRACK SECTIONS REPLACED. 2L74 4F4 FRTA20WE E24NE 20050316000222005031600022NM 2005 3 16 2005UALA00219 120050307A5753 PANEL BOEING747 747422 1384935NM PWA 4056 PW4056 NE LT WING TE FLAP DAMAGED A UALAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP29117UA 28810 LEFT WING OUTBOARD T/E AFT FLAP PANEL 588JT HAS ELONGATED HOLE. DAMAGE OCCURED DURING MAINTENANCE. REPAIRED PER EA 747-5753-13-A1252. 2L74 4F4 FRTA20WE E24NE 20050316000232005031600023NM 2005 3 16 2005UALA00221 120050309A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29582UA 26702 AFT PIT AT STA 1540, APPROX AT STR 26R FRAME IS DENTED ON THE INBOARD FLANGE. FRAME FLANGE WAS REPAIRED USING NESTED J-ANGLES. 2L72 4F4 FRTA2NM E17NE 20050316000242005031600024NM 2005 3 16 2005UALA00222 120050309A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29582UA 26702 AFT PIT FRAME IS DENTED 3 EA PLACES ON INBOARD FLANGE AT BS 1420, BETWEEN STR 23L AND 26L. FRAME FLANGE WAS REPAIRED BY EXTENDING THE EXISTING SPLICE ANGLE TO REPAIR THE DAMAGED FLANGE. 2L72 4F4 FRTA2NM E17NE 20050316000252005031600025NM 2005 3 16 2005UALA00223 120050309A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29582UA 26702 AFT PIT STA 1580 FRAME DENTED ON INBOARD FLANGE AT STR 26R. FRAME FLANGE WAS REPAIRED USING NESTED J-ANGLES. 2L72 4F4 FRTA2NM E17NE 20050316000272005031600027NM 2005 3 16 2005UALA00225 120050309A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29582UA 26702 AFT PIT STA 1480 AT STR 26L, FRAME IS DENTED ON INBOARD FLANGE. FRAME FLANGE WAS REPAIRED BY EXTENDING THE EXISTING SPLICE ANGLE TO REPAIR THE DAMAGED FLANGE. 2L72 4F4 FRTA2NM E17NE 20050316000292005031600029NM 2005 3 16 SWAA050697 120050307A53306545780 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29376SW 26584 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050316000302005031600030NM 2005 3 16 HNAA0500020 120050308A3260 INDICATOR DHAV DHC8 DHC8102 2809003NM MLG MALFUNCTIONED A HNAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA07937HA 148 AFTER SELECTING GEAR UP NOSE GEAR AMBER LIGHT AND BOTH MAIN GEAR RED INTRANSIT LIGHTS ILLUMINATED. CAPT SELECTED GEAR DOWN ALL INDICATIONS NORMAL. JACKED AIRCRAFT SWUNG GEAR SEVERAL TIMES. UNABLE TO DUPLICATE PROBLEM, GEAR OP'S CHECK GOOD. 2H72 4T RTA13NM 20050316000322005031600032NM 2005 3 16 DHL2005781538 120050215A5753 SKIN BOEING727 727227 1384078NM LT WING TE FLAP GOUGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A C-CHECK, LT WING I/B FORE FLAP GOUGED AT O/B LEADING EDGE. REMOVED PREVIOUS REPAIR IAW B727 SRM 51-30-2. FAB DOUBLER FORM 2029-T3 .063 PO 9001634 BY 4.95 X 3.1 IAW B727 SRM 57-50-4 FIG 1. TREAT AND PRIME DOUBLER AREA IAW B727 SRM 51-10-2. INSTALL DOUBLER IAW B727 SRM 57-50-4 FIG 1. 2L73 4F A3WE 20050316000332005031600033NM 2005 3 16 2005UALA00226 120050309A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29582UA 26702 AFT PIT STA 1440, STR 26L FRAME INBOARD FLANGE IS DENTED. FRAME FLANGE WAS REPAIRED USING NESTED J-ANGLES. 2L72 4F4 FRTA2NM E17NE 20050316000342005031600034 2005 3 16 SWAA050698 420050307A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29617SW 27700 R1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF HOUSING. SLIDE DID NOT DEPLOY. REINSTALLED R1 DOOR SLIDE PER MM. 2L72 4F RTA16WE 20050316000352005031600035EA 2005 3 16 COMA0560172 120050311A2916601R751113 RESERVOIR CNDAIRCL600 CL6002B19 1900309EA NR 3 HYD SYS MALFUNCTIONED A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01976CA14485 7151 FLIGHT 5673 RECEIVED A LANDING GEAR DISAGREE CAUTION DURING APPROACH, CREW DECLARED AN EMERGENCY, ABORTED 1ST APPROACH, THEN LANDED WITHOUT INCIDENT AFTER MANUAL EXTENSION OF THE LANDING GEAR. REPLACED THE NR 3 HYDRAULIC RESERVOIR. 2L72 4F RTA21EA 20050316000362005031600036NM 2005 3 16 2005UALA00227 120050309A5320 SPLICE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29582UA 26702 AFT PIT STA 1620, STRINGER 29L, LONGERON SPLICE HAS CORROSION BEYOND LIMITS. DAMAGE CAUSED BY CORROSION. REMOVED CORRODED STRINGER SPLICE AND INSTALLED NEW STRINGER SPLICE. 2L72 4F4 FRTA2NM E17NE 20050316000372005031600037NM 2005 3 16 2005UALA00228 120050309A5322 SHEAR TIE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29582UA 26702 AFT PIT STA 1280, STR 28L TO 29L FRAME SHEAR TIE IS CORRODED. DAMAGE CAUSED BY TYPICAL AFT PIT CORROSION. FABRICATED AND INSTALLED NEW SHEAR TIE. 2L72 4F4 FRTA2NM E17NE 20050316000382005031600038EU 2005 3 16 2005UALA00229 120050309A7830 WARNING LIGHT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE THRUST REVERSER ILLUMINATED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29453UA 1001 NR 2 ENGINE REVERSER FAULT INDICATION. SENSOR 23GA WAS REPLACED. 2L72 4F4 FRTA28NM E40NE 20050316000392005031600039NM 2005 3 16 2005UALA00230 120050310A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP29582UA 26702 EXTERNAL FUSELAGE SKIN HAS MULTIPLE REPAIRS BS 550 TO BS 630 STR 14L-19L. ORIGINAL DAMAGE CAUSED BY JETWAY IMPACT. MULTIPLE TIME-LIMITED REPAIRS WERE REMOVED AND A PARTIAL SKIN REPLACEMENT WAS ACCOMPLISHED. CONSTANT THICKNESS SKIN SECTION WAS SPLICED IN USING DOUBLER STRAPS AND TRIPLERS. 2L72 4F4 FRTA2NM E17NE 20050316000402005031600040NM 2005 3 16 2005UALA00231 120050310A5322 SHEAR TIE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP29582UA 26702 SHEAR TIES AT STA 580 BETWEEN STRINGERS 15L-16L, 16L-17L, AND 17L TO 18L HAVE HOLE DAMAGE. HOLE DAMAGE CAUSED DURING INSTALLATION OF EXTERNAL FUSELAGE SKIN REPAIR. SHEAR TIES WERE REMOVED, NEW SHEAR TIES WERE FABRICATED AND INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050316000422005031600042NM 2005 3 16 SWAA050699 120050306A5414311A1220 PLATE BOEING737 7373H4 1384600NM LT PYLON CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 DURING SCHEDULED SERVICE CHECK, FOUND NR 1 ENG PYLON UPPER PLATE CRACKED AT STA 234.5. REMOVED AND REPLACED PLATE PER SRM. 2L72 4F RTA16WE 20050316000432005031600043NM 2005 3 16 SWAA050700 120050306A53126516300 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29372SW 26599 DURING SCHEDULED SPECIAL VISIT, FOUND 2 EA FUSELAGE WEB CRACKS AT BS 178 BLKHD, BETWEEN WL 213 TO WL 214 & BETWEEN LBL 6.7 TO RBL 4.7. REPAIRED FUSELAGE WEB PER SRM. 2L72 4F RTA16WE 20050316000452005031600045NM 2005 3 16 2005UALA00233 120050310A5322 SHEAR WEB BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSLEAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29582UA 26702 SHEAR WEB STA 1700 CORRODED FROM RBL 8 TO RBL 38. DAMAGE CAUSED BY TYPICAL AFT PRESSURE DECK WEB CORROSION. CORROSION WAS REMOVED AND THE WEB WAS REPAIRED USING DOUBLERS. 2L72 4F4 FRTA2NM E17NE 20050316000462005031600046WP 2005 3 16 UPS05844042 120050223A53404758514501 ATTACH FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01811UP 46089 INSPECTION TYPE: C2, C-PIT FS 1150 INTERCOSTAL ATTACH FITTING CRACKED IN FWD RADIUS BETWEEN FASTENERS, BETWEEN LONGERONS 32R & 33R. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20050316000472005031600047NM 2005 3 16 DHL2005782537 120050214A5755 HINGE BOEING727 727227 1384078NM SPOILER CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A C-CHECK, NR 3 SPOILER HINGE CUTOUT CRACKED (MARKED) LT WING UPPER SURFACE. REMOVED NR 3 SPOILER PANEL TO FACILITATE OTHER MAINTENANCE IAW B727 SRM 27-62-01. REMOVED FASTENERS FOR ACCESS FOR REPAIR IAW B727 SRM 57-30-4 FIG 10. CRACK TERMINATED AT FASTENER HOLE VERIFIED IAW B727 NDT MAN PTG 51-00-00 FIG 23. FABRICATED NEW REPAIR DOUBLER FROM 7075 T6 .071 PO 900573 7 X 4 INCH DIM IAW B727 SRM 57-30-4 FIG 10. TREATED AND PRIMED DOUBLER AND AREA IAW B727 SRM 51-10-2. INSTALLED DOUBLER AT NR 3 SPOILER HINGE LT WING UPPER SURFACE IAW B727 SRM 57-30-4 TIS 10. REINSTALLED NR 3 SPOILER PANEL IAW B727-MM-27-62-01, OPS CHECK GOOD IAW B727-MM-27-62-0. 2L73 4F A3WE 20050314000922005031400092SW 2005 3 14 ALG2005F00015 120050114A6340206075545005 SENSOR BELL 206 206L1 1182107SW ALLSN 250C 250C30P 03013GL LOW ROTOR RPM CORRODED E ALGAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW032611 45417 JUST AFTER TAKEOFF, THE LOW ROTOR CAUTION LIGHT ILLUMINATED. 2 OR 3 SECONDS LATER THE LOW ROTOR RPM HORN SOUNDED. ROTOR TACH INDICATIONS WERE NORMAL, PILOT RETURNED TO BASE. UPON LANDING, THE MECHANIC REMOVED AND REPLACED BOTH THE LOW ROTOR RPM AND ENGINE. OUT SENSORS DUE TO CORROSION AND AC WAS OPS CHECKED AND RETURNED TO SERVICE. (K) 1G71 3U3 U H2SW E1GL 20050315000202005031500020NM 2005 3 15 QXEA200500306 120050223A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09413QX 4060 PDX - CORROSION ON RIGHTHAND OUTBOARD SEAT TRACK AT APPROXIMATELY X490.00, TOP AND INNER FLANGE. REPLACED SEAT TRACK IAW DHC-8 SRM 51-42-15 AND 51-42-05. 2H72 4T RTA13NM 20050315000482005031500048EA 2005 3 15 A6WA200540047 120050214A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31421ZW 7346 OBLIQUE ANGLE AT FS 625 IS CRACKED .25 INCH LONG, LEFT SIDE. REMOVED CRACKED OBLIQUE ANGLE AND INSTALLED NEW SERVICEABLE ANGLE IAW CRJ200SRM 51-42-06, P/N 601-35012-51. (M) 2L72 4F RTA21EA 20050315000652005031500065EA 2005 3 15 A6WA200540066 120050131A5210601R317725 ANGLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31414ZW 7586 PAX DOOR AFT DRAG ANGLE IS CRACKED 2 INCHES LONG JUST FORWARD OF DOOR ASSIST PULLEY MOUNT. REPAIRED ANGLE BY INSTALLING SPLICE ANGLE P/N 601R31772-5 AND IAW BOMBARDIER, INC REO 601R-52-11-513. (M) 2L72 4F RTA21EA 20050315000772005031500077EA 2005 3 15 A6WA200540072 120050217A3210 BUSHING CNDAIRCL600 CL6002B19 1900309EA RT MLG MIGRATED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31448AW 7814 RIGHT AFT MAIN LANDING GEAR TRUNNION BUSHING IS MIGRATED .041 INCH, AT WS 66. (M) 2L72 4F RTA21EA 20050315000862005031500086SO 2005 3 15 SIMA200504502 120050210A532014525381003 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21653AE 145433 ABI - DURING AN IMBV INSPECTION, THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. REMOVED THE CORROSION BY MAKING A CUTOUT. FABRICATED A FILLER, TWO SHIMS AND DOUBLER. REPAIR DONE IAW EMB SRM, SRM 145/1142, REV 28, CHAPTER 53-22-10, FIG 201. (M) 2L72 4T RTT00011AT 20050315000922005031500092EU 2005 3 15 SIMA200505901 120050225A33506013211 POWER SUPPLY SAAB SF340 340B 7860101EU EMERGENCY LIGHTSINOPERATIVE A SIMAO OTHER O OTHER NRNOT REPORTED 1 SW21235AE 340B235 DFW - FLT 3219 - CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHTS AT SEATS 8A AND 7B TO 8B TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY POWER SUPPLY IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 20050315000972005031500097WP 2005 3 15 GTIA050031 120050119A5340 FITTING DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FTW - FORWARD ENTRYWAY CORROSION AT FS 200 CUSPLINE, LONG 18L FRAME TO CUSP FITTING. REMOVED FRAME TO CUSP FITTING STATION 200 L18L-L, REMOVED CORROSION ON CUSP, REMOVED WEB L1 DOOR STATION TO 208 L18L TO L13L. FABRICATED CUSP SECTION FROM STATION 180 TO STATION 230, TREATED, PRIMED AND INSTALLED NEW CUSP SECTION. (M) 2L72 4F A6WE 20050315001002005031500100WP 2005 3 15 GTIA050018 120050127A2913 PUMP DOUG DC9 DC983 3022083WP HYD SYSTEM FAILED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23815NK 49415 FLL - FLT 271 - AUX HYDRAULIC PUMP CIRCUIT BREAKER POPPED DURING PUSH BACK, AIRCRAFT TAIL SWAP. FOUND BAD HYDRAULIC PUMP, REMOVED AND REPLACED PUMP, OPS CHECK GOOD. (M) 2L72 4F RTA6WE 20050315001022005031500102WP 2005 3 15 GTIA050028 120050209A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FTW - FOUND CABIN FLOOR SUPPORT CORRODED AT FS 200 9 INCH LBL 13 INCH LBL. REMOVED CORRODED FLOOR SUPPORT, FABRICATED FLOOR SUPPORT, TREATED, PRIMED AND INSTALLED NEW FLOOR SUPPORT. (M) 2L72 4F A6WE 20050315001082005031500108EU 2005 3 15 XN0A1225 120050127A7930 WARNING SYSTEM AIRBUS300 A300B4203 3930306EU COCKPIT MALFUNCTIONED A XN0AD RETURN TO BLOCK N FALSE WARNING CRCRUISE 1 GL23373PC 218 NR 2 ENGINE OIL CLOG LIGHT CAME ON IN FLIGHT. INSPECTED OIL FILTER AND MASTER CHIP DETECTOR. NO EVIDENCE FOUND ON INSPECTION. PERFORMED ENGINE RUN OF NR 2 ENGINE, NO DEFECTS NOTED. NR 2 ENGINE OIL CLOG LIGHT OP CHECKS NORMALLY IAW A300 M/M 79-35-00, NO DEFECT. 2L72 4F RTA35EU 20050315001242005031500124NM 2005 3 15 C1HA200578001 120050212A2910 HYDRAULIC LINE BOEING727 727225 1384077NM HYDRAULIC SYS CHAFED A C1HAA UNSCHED LANDING K FLUID LOSS CLCLIMB 1 GL15678MG 22555 AFTER TAKEOFF HYDRAULIC B-SYSTEM QUANTITY LEAK TO ZERO, ACCOMPLISHED COM EMERGENCY CHECKLIST, RETURNED FOR LANDING. FOUND CHAFED SPOILER PSI LINE IN RT WHEEL WELL AREA WHERE LINES GOES THROUGH WALKING BEAM INSTALLED TEMP FLEX LINE REF SUPPL MM 20-10-12, NO LEAKS NOTED. PLACED ON TLD C/N T00683 REF IPC 27-60-00 PAGE 0 FIG 38 ITEM 55 MSPMC ADVISED. 2L73 4F A3WE 20050315001282005031500128EA 2005 3 15 05047642 120050216A7120 SUPPORT CNDAIRCL600 CL6002B19 1900309EA RT ENGINE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27642BR 7356 A 1 INCH CRACK ON ENGINE SUPPORT BEAM RT LOWER WEB AFT OF FS 625.30, JUST RIGHT OF RBL 36.200. 2L72 4F RTA21EA 20050315001302005031500130NE 2005 3 15 DL76L050115 220050216A753080217010 SHUTOFF VALVE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE LT ENGINE MALFUNCTIONED A DALAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 SO27183DN 27110 ON TAKEOFF ROLL APPROX 95 KNOTS, LT ENG HPSOV EICAS MESSAGE ILLUMINATED. AFTER AIRBORNE DID QRH PROCEDURES TALK WITH MX AND RETURNED TO JFK. REPLACED HPSOV. 2L72 4F4 FRTA1NM E24NE 20050315001702005031500170NM 2005 3 15 AALA20050189 120050311A3040141N485061 CONNECTOR BOEING757 757223 1384957NM COCKPIT FIRE A AALAH DEACTIVATE SYST/CIRCUITS AB FLAME/FIRE SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21679AN 29589 MIA INFLIGHT T2274/11 MAR CAPTAINS SLIDING WINDOW HEAT CONNECTORS CAUGHT ON FIRE AND MELTED CONNECTIONS. WINDOW HEAT WAS SHUT OFF AND FLAMES STOPPED. LANDED MIA WITHOUT INCIDENT. REPLACED CAPTAINS SLIDING WINDOW AND HARNESS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050315001752005031500175NM 2005 3 15 AALA20050151 120050211A5315 FLOORBEAM BOEING757 757223 1384957NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21653A 24611 TUL - CORROSION AT FLOORBEAM AT RIGHTHAND BUTTLINE 0 INCH TO 24 INCH. INSTALLED REPAIR IN ACCORDANCE WITH SRM 53 00 51 2. 2L72 4F RTA2NM 20050315001802005031500180WP 2005 3 15 AALA20050173 120050307A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21979TW 53629 DTW - FORWARD ENTRY EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD ENTRY EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050315001892005031500189WP 2005 3 15 AALA20050162 120050302A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21587AA 53250 DFW - TAIL CONE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK B5 28 FOR TAIL CONE EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050315001942005031500194 2005 3 15 AALA20050187 420050306A3160066500028102 DISPLAY BOEING767 767323 1385205NM COCKPIT FAILED A AALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21358AA 24039 CDG INFLIGHT T0120/6 MAR TCAS DISPLAY STARTED SMOKING ABOUT THREE HOURS AFTER TAKEOFF. SMOKE LASTED AROUND 10 SECONDS FOLLOWED BY BURNING ELECTRICAL SMELL. TCAS DISPLAY WENT BLANK. TURNED TRANSPONDER TCAS TO STANDBY AND PULLED TCAS CIRCUIT BREAKERS. NO FURTHER SMOKE OR ELECTRIC BURNING SMELL NOTED. REPLACED TCAS DISPLAY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050315002122005031500212WP 2005 3 15 ABXA050046 120050208A532059124921 PAN DOUG DC9 DC933F 302207AWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23933AX 47291 SERVICE DOOR THRESHOLD LOWER PAN HAD A BULGE AND 3 EACH POPPED RIVETS AT AFT CORNER. REPAIRED DOOR JAMB PAN IAW DC-9 SRM 53-05. 2L72 4F A6WE 20050315002142005031500214WP 2005 3 15 ABXA050045 120050208A53115911448503 FRAME DOUG DC9 DC933F 302207AWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23933AX 47291 CORROSION ON FRAME FS 832 LONGERON 30. REPAIRED IAW DC-9 SRM 53-03. 2L72 4F A6WE 20050315002172005031500217WP 2005 3 15 ABXA050043 120050208A5210SB095201389 STRUCTURE DOUG DC9 DC933F 302207AWP ENTRY DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23933AX 47291 MAIN ENTRY DOOR CRACKED LOWER HINGE CUTOUT. REPLACED MAIN ENTRY DOOR ON NON ROUTINE 0311 IAW DC-9 SRM. 2L72 4F A6WE 20050315002182005031500218WP 2005 3 15 ABXA050048 120050208A5347S49258487075T651SEAT TRACK DOUG DC9 DC933F 302207AWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23933AX 47291 SEAT TRACK AT LEFT BUTTLINE 44 WAS CORRODED BETWEEN STA 214 AND 224. REPAIRED TRACK AND SPLICED IN NEW SECTION OF TRACK IAW DC-9 SRM 53-05. 2L72 4F A6WE 20050315002282005031500228NM 2005 3 15 USAA050221 120050201A5320 PLATE BOEING737 737301 1384611NM FUSELAEG CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19354US48721 23557 PIT - FOUND HINGE DOUBLER PLATE CRACKED .3750, MED TOP FORWARD HINGE CUTOUT INSIDE BOTTOM FORWARD CORNER. INSTALLED WEB PER SRM 51-40-02 AND DWG 65-17684. (M) 2L72 4F RTA16WE 20050315002292005031500229NM 2005 3 15 USAA050222 120050112A5320 FLOOR SUPPORT BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19521AU52547 23856 PIT - FOUND FLOOR SUPPORT CORRODED APPROX 3 INCHES BY .5 INCH, STATION 797 TO 817. FABRICATED AND INSTALLED NEW FLOOR SUPPORT PER SRM 53-00-53. (M) 2L72 4F RTA16WE 20050315002312005031500231NM 2005 3 15 USAA050204 120050113A5311 FRAME BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19436US41647 24558 PIT - FOUND FRAME CRACKED .25 INCH, BETWEEN STRINGER 8L AND 9L AT STATION 827. CUT OUT DAMAGE, HI FREQ, INSTALLED DOUBLER PER TR 53-10-20A. (M) 2L72 4F RTA16WE 20050315002332005031500233NM 2005 3 15 USAA050201 120050204A5340 STRINGER CLIP BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19519AU50538 23705 CLT - FOUND CLIP CRACKED .5 INCH, STATION 344 STRINGER 11R. REPLACED TIE CLIP IAW SRM. REPLACED TIE CLIP IAW SRM 51-10-02. (M) 2L72 4F RTA16WE 20050315002402005031500240NM 2005 3 15 USAA050210 120050106A5311 FRAME BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19436US41647 24558 PIT - FOUND FRAME CRACKED TWO PLACES .125 INCH LONG, STATION 500A BETWEEN STRINGER 8LT AND 9L OVERHEAD BIN LOWER ATTACH POINT. REINFORCED WITH PREFABRICATED DOUBLERS PER TYPICAL REPAIR 53-10-20A. (M) 2L72 4F RTA16WE 20050315002582005031500258NM 2005 3 15 USAA050289 120050214A5230 STRUCTURE BOEING737 7374B7 1384702NM CARGO DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19438US40959 24560 PIT - FOUND AFT CARGO DOOR WITH TWO .25 INCH CRACKS, LOCK FASTENER BOTTOM OUTBOARD T-CHORD AFT END. REMOVED AND REPLACED T-CHORD PER RM 51-40-02. (M) 2L72 4F RTA16WE 20050315002592005031500259NM 2005 3 15 USAA050290 120050214A5730 SKIN BOEING737 7374B7 1384702NM RT WING CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19438US40959 24560 PIT - FOUND SKIN CRACKED .5 INCH, RT WING LEADING EDGE WBL 204 AT LOWER WING SURFACE. REMOVED DAMAGE AND INSTALLED FILLER AND DOUBLER PER T/R 57-41-02. (M) 2L72 4F RTA16WE 20050315002652005031500265EU 2005 3 15 AWXA200500320 120050309A3350321454 EPSU AIRBUS320 A320232 3930326EU CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28638AW334842771 455 LAS - EEL - FLIGHT CREW REPORTED THE LT OVERWING EMERGENCY ESCAPE PATH LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL) AND BATTERY PACK, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050315002722005031500272NM 2005 3 15 AWXA200500317 120050216A575465C26603220 WEDGE BOEING737 7373G7 1384595NM L/E SLAT DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28307AW 24634 MCN - MAJOR REPAIR - DURING C-14 CHECK FOUND THE NR 4 SLAT WEDGE DELAMINATED ON LOWER SURFACE AT INBOARD END, SLAT STA 14. MAINTENANCE REMOVED DELAMINATED AREA OF NR 4 SLAT FROM SLAT STA 12.25 TO 15.25 RT; FABRICATED A FILLER AND DOUBLER; BONDED REPAIR PARTS TO SLAT IAW B737-300 SRM 51-70-10 FIG 30. 2L72 4F RTA16WE 20050315002962005031500296NM 2005 3 15 USAA050299 120050208A575465C26602108 SKIN BOEING737 7373B7 1384580NM NR 5 SLAT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU50570 23706 PIT - FOUND NR 5 SLAT SKIN CRACKED 1 INCH, OUTBOARD FORWARD EDGE ABOVE UPSTOP. INSTALLED DOUBLER PER SRM 57-43-01. (M) 2L72 4F RTA16WE 20050315003282005031500328NM 2005 3 15 SWAA050707 120050307A53116546526 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29607SW 27927 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050315003362005031500336NM 2005 3 15 SWAA050691 120050306A56105893543035 WINDOW BOEING737 7373H4 1384600NM COCKPIT CRACKED A SWAAD RETURN TO BLOCK O OTHER CLCLIMB 1 SW29331SW 23695 AIR TURNBACK. ON CLIMBOUT, L1 COCKPIT WINDOW ARCED & CRACKED IN 3 PLACES. REMOVED AND REPLACED L1 WINDOW PER MM. 2L72 4F RTA16WE 20050315003372005031500337WP 2005 3 15 GTIA050008 120050114A56105912290506 WINDSHIELD DOUG DC9 DC982 3022082WP COCKPIT DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23803NK 48087 TPA - F/O'S WINDSHIELD HAS AREA OF DELAMINATION NEAR BOTTOM AND CENTER, AREA IS APPROX 2.5 BY 4, AIRCRAFT TAIL SWAP. REMOVED AND REPLACED F/O'S SIDE WINDSHIELD. (M) 2L72 4F A6WE 20050315003492005031500349 2005 3 15 YENA200522 420050306A23303042865102 ELECTRICAL BOX AIRBUS320 A320232 3930326EU CABIN MALFUNCTIONED A YENAK NONE B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA15548JB6040 1868 TV'S 19 ABC INOP, FOUND STRONG EVIDENCE OF ELECTRICAL ODOR UNDER 19B SEAT (SEB). REMOVED AND REPLACED SEB AND COMPLETED INFO NOTICE 2004-T023TR. LIVE TV SYSTEM OPERATIONAL IAW MM 23-39-00. 2L72 4F RTA28NM 20050315003512005031500351EA 2005 3 15 05063671 120050304A2741 TRIM SYSTEM CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB MALFUNCTIONED A VTZAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA27671BR 7572 EVENT SUMMARY STATED MACH/STAB TRIM INOP MSG POSTED. RESET POWER TO A/C OPS CHECK GOOD & COMPLY WITH SL RJ-SL-27-083. 2L72 4F RTA21EA 20050315003522005031500352EA 2005 3 15 05064676 120050305A2750 ECU CNDAIRCL600 CL6002B19 1900309EA T/E FLAP MALFUNCTIONED A VTZAB EMER. DESCENT J WARNING INDICATION CLCLIMB 1 EA27676BR 7644 EVENT SUMMARY STATED FLAP FAIL AT 8 DEGREES. RESET FECU. OPS CHECK GOOD. 2L72 4F RTA21EA 20050316000072005031600007NM 2005 3 16 DL75K050145 120050301A3241 ANTI-SKID SYS BOEING757 757232 1384965NM BRAKES INOPERATIVE A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27699DL 29970 EICAS MESSAGE, ANTISKID INOP. BITE CHECK SHOWED PARKING BRAKE. RESET PARKING BRAKES SEVERAL TIMES. OPS NOW OK. BSCU TEST OK. 2L72 4F RTA2NM 20050316000102005031600010NM 2005 3 16 DL733050148 120050303A5330654577575 SKIN BOEING737 737347 1384647NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27306WA 23347 THE FUSELAGE SKIN WAS FOUND WITH A 4 INCH CRACK AT FS 870 JUST ABOVE THE BONDED DOUBLER MILL LINE AT STRINGER 23R. THE CRACK IS TYPICAL OF AD 2004-18-06. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737-300 SRM AND PER ER/A 097294-14AD. 2L72 4F RTA16WE 20050316000182005031600018NM 2005 3 16 DLM90050157 120050312A3240 BRAKE DOUG MD90 MD9030 3023690NM MLG LEAKING A DALAO OTHER KJ FLUID LOSS WARNING INDICATION LDLANDING 1 SO27904DA 53384 HYDRAULIC QTY LOW LT HAND. FOUND NR 1 BRAKE ASSEMBLY LEAKING FROM THE SIX O`CLOCK POSITION. REMOVE AND REPLACE NR 1 BRAKE ASSY AND SERVICED LT HYDRAULIC SYSTEM AS PER AMM. NO LEAKS FOUND. 2L72 4F RTA6WE 20050316000262005031600026NM 2005 3 16 2005UALA00224 120050309A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29582UA 26702 AFT PIT STA 1460 AT STR 26L FRAME IS DENTED ON INBOARD FLANGE. FRAME FLANGE WAS REPAIRED USING NESTED J-ANGLES. 2L72 4F4 FRTA2NM E17NE 20050316000282005031600028NM 2005 3 16 SWAA050696 120050307A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29354SW 25219 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 724E, STR 24L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050316000312005031600031 2005 3 16 HNAA0500021 420050310A34207003360941 AHRS DHAV DHC8 DHC8102 2809003NM NR 1 FAILED A HNAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA07826EX261818378 389 NR 1 AHRS FAILED ON CLIMBOUT. HSI/HDG MESSAGE AND ADI PITCH MISMATCH ON 800 PANEL. AFTER MAINTENANCE REMOVED AND REPLACED NR 1 AHRS F/O NOTICED HDG MISMATCH ON F/O SIDE. MAINT WAITING FOR PUSH BACK TO TAXI AIRCRAFT FOR HDG MISMATCH. MAINT TAXIED AIRCRAFT, OPS NORMAL. 2H72 4T RTA13NM 20050316000482005031600048NM 2005 3 16 DHL2005781539 120050215A5330 SKIN BOEING727 727227 1384078NM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A C-CHECK, SEVERAL DENTS ON SKIN OF AFT AIRSTAIR STA 1263. REMOVED FASTENERS ON SKIN OF AFT AIRSTAIR STA 1263 IAW B727 SRM 51-30-2. CUT OUT DAMAGE SKIN DIM 42 X 5 INCH IAW B727 SRM 52-10-2 FIG 4. FABRICATED SKIN REPAIR MAT USED 2024T3 .040 PO 9001765 DIM 42 X 25 INCH AND 1EA STRAP MAT USED 2024T3 .040 IAW B727 SRM 52-10-2 FIG 4. ALODINED AND PRIMED PARTS AND AREA IAW B727 SRM 51-10-2. INSTALLED SKIN REPAIR AND STRAP IAW B727 SRM 52-10-2 FIG 4. 2L73 4F A3WE 20050316000512005031600051WP 2005 3 16 UPS05844110 120050304A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01811UP 46089 INSPECTION TYPE: C2, INNER DENT CRACK IN O/B SKIN LEFT LOWER EMPENNAGE FS 1875 LONG 24L. REPAIRED IAW SRM 53-02-00. 2L74 4F RT4A25 20050316000552005031600055NM 2005 3 16 2005UALA00235 120050310A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29304UA 23665 DENT WITH SHARP BOTTOM ON RT SIDE OF FUSELAGE 36 INCHES BEHIND DOOR 1R AND 30 INCHES BELOW WINDOWS. DENT IS 1 INCH X 1 INCH WITH A 0.25 INCH CREASE, 0.65 INCH DEEP. CUT AND REMOVED DAMAGED, AND INSTALLED DOUBLER AND FILLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20050316000562005031600056NM 2005 3 16 2005UALA00236 120050310A5514 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE HORIZONTAL STAB DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29332UA 24193 FOUND DENT IN HORIZONTAL STAB RT SIDE ABOUT 2 FEET IN FROM TIP. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20050316000582005031600058NM 2005 3 16 DHL2005781542 120050215A5712 RIB BOEING727 727227 1384078NM RT WING GOUGED A DHLAO OTHER O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A C-CHECK, RT WING L/E CAVITY RIB GOUGED WSTA 734. REMOVED DAMAGED ANGLE IAW B727 SRM 51-30-2. FABRICATED ANGLE 20 24 T3 .040 9001634 (16 X 1.875 INCH) IAW B727 SRM 57-20-2 FIG 1 AND 51-20-1. TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED NEW ANGLE IAW B727 SRM 51-30-2. 2L73 4F A3WE 20050316000622005031600062NM 2005 3 16 DHL2005781528 120050215A5310 TORQUE BOX BOEING727 727227 1384078NM FUSELAGE LIGHTNING STRIKEA DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A C-CHECK, PREVIOUS REPAIR ON LOWER TORQUE BOX LIGHTENING HOLE IMPROPERLY DONE R/SIDE AT FWD STA 1243. REMOVED PREVIOUS REPAIR ON LOWER TORQUE BOX LIGHTENING HOLE R/SIDE AT FWD STA 1243 IAW B727 SRM B727 SRM 51-30-2. STOP DRILL CRACK 250 TERIMINATED AT END OF CRACK IAW B727 SRM 51-10-1. ACCOMPLISHED 727 HFEC INSPECTION 51-00-00 FIG 4 END OF CRACK IAW B727. FABRICATED DOUBLER REPAIR MAT IDENTIFICATION 53-10-2 FIG 6, FROM MAT 7075T6 .040 DIM 4 X 4.625 INCH PO9001068 IAW B727 SRM 51-40-2 FIG 1. ALODINED AND PRIMED IAW B727 SRM 51-10-2, INSTALLED DOUBLER REPAIR IAW B727 SRM 51-40-2 FIG 1. 2L73 4F A3WE 20050316000642005031600064EA 2005 3 16 COMA0570028 120050308A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01641CA3959 10122 FS 280 LT AND RT BULKHEADS AND TRANSVERSE BEAM HAVE MAJOR CORROSION ON AFT SIDE ALONG THE BOTTOM EDGES. REPLACED LOWER WEBS AT FS 280 BULKHEAD IAW BOMBARDIER INC REO 670-53-11-052 REV A REPAIR NR 2 AND BRAS EO 601R-53-6066. REPLACED TRANSVERSE BEAM IAW BOMBARDIER REO 670-53-11-047 REV A AND BRAS EO 601R-53-6066. 2L72 4F RTA21EA 20050316000692005031600069NM 2005 3 16 UPS05M44053 120050103A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 5 LT CORROSION ON WALL, BASE AND BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED AT BARREL NUT HOLE NR 5 LT FOUND OUT OF LIMIT PER SRM 51-21-0 1 V.2 R.36. REWORKED BARREL NUT HOLE NR 5 LT PER SRM 51-21-01 V.2 R.36. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 AT BARREL NUT HOLE NR 5 LT & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED PER EN 1118-05 FOUND WITHIN LIMIT. 2L73 4F RTA22WE 20050316000702005031600070NM 2005 3 16 UPS05444097 120050312A3350S135610A BATTERY BOEING747 747123F NM EMERGENCY LIGHT DISCHARGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:A CHECK, EMERGENCY LIGHT AT STA 570 LT AND L1 DOOR AFT SILL LIGHT IS EXTREMELY DIM. REPLACED BATTERY PACK LIGHT, OPS CHECK OK. 2L74 4F A20WE 20050316000712005031600071NM 2005 3 16 UPS05544108 120050311A2560 SMOKE GOGGLES BOEING757 75724APF 1384969NM COCKPIT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01435UP 25466 INSPECTION TYPE:N/A SMOKE GOGGLE CRACK AT SUPERNUMERARY SEAT. REPLACED SMOKE GOGGLES. 2L72 4F RTA2NM 20050316000742005031600074NM 2005 3 16 DHL2005781531 120050211A5754 SKIN BOEING727 727227 1384078NM NR 1 SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A C-CHECK, NR 1 SLAT SKIN CRACKED AT I/B TRACK ATTACH POINT (MARKED). STOP DRILLED WITH .25 INCH DIAMETER DRILL IAW B727 SRM 51-10-1 FAB. DOUBLER REPAIR WITH 2024T3 0.80 SIZE 6.5 X 6.5 INCH PO 9001502 IAW B727 SRM 57-50-3 FIG 1 & 57-50-2 FIG 2. TREATED & PRIMED DOUBLER REPAIR IAW B727 SRM 51-10-2, INSTALLED DOUBLER REPAIR IAW B727 SRM 57-50-3 FIG 1. 2L73 4F A3WE 20050316000772005031600077NM 2005 3 16 DHL2005781535 120050214A5310 STOP FITTING BOEING727 727227 1384078NM LT MLG DOOR WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A C-CHECK, LT W/W AFT DOOR STOP FITTING BS 950 HAS PLAY. REMOVED LT W/W AFT BODY FAIRING AT BS 950 AND FUEL VENT TUBE IAW B727 SRM 51-30-2. FABRICATED ANGLES (2EA) FAIRING FROM 2024T3-050 PO 9001576 DIM 19.375 X 3.3125 X .75 X .75 (2EA) IAW B727 SRM 53-10-2 FIG 5, 51-20-1 FIG 7 AND 51-30-5. TREATED AND PRIMED PARTS AND WEB AREA IAW B727 SRM 51-10-2. INSTALLED ANGLES (2EA) FITTING IAW B727 SRM 51-30-2. 2L73 4F A3WE 20050316000792005031600079NM 2005 3 16 DHL2005781532 120050214A5754 SKIN BOEING727 727227 1384078NM NR 4 SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A C-CHECK, NR 4 SLAT CRACKED AT I/B & O/B OF ACTUATOR ROD ATTACH POINT (IN LIGHTENING HOLE). REMOVED AND REPLACED NR 4 SLAT WEB (RIBS) IAW B727 SRM 51-30-2, P/N 65-17276-9, PO441715 & P/N 65-17276 PO441715. 2L73 4F A3WE 20050316000812005031600081NM 2005 3 16 QXEA200500351 120050305A2611473054 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM CARGO BAY FAILED A QXEAO OTHER N FALSE WARNING CRCRUISE 1 NM09355PH149665693 500 SEA - FLIGHT 2006 - THE CREW REPORTS THE SMOKE DETECTOR LIGHT ILLUMINATING INTERMITTENTLY DURING FLIGHT. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE FORWARD BAGGAGE COMPARTMENT SMOKE DETECTOR AND RELAMPED THE AFT SMOKE DETECTOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050316000822005031600082EA 2005 3 16 QXEA200500354 120050217A26109847101505 CHIMNEY CNDAIRCL600 CL6002C10 1390015EA FWD CARGO BAY DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09617QX3266 10130 DEN - MAINTENANCE FOUND THE FORWARD CARGO BAY CHIMNEY MESH DAMAGED AND THE DOOR SECTION. THE CHIMNEY WAS REPLACED AND THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20050316000832005031600083EA 2005 3 16 COMA0560177 120050313A3150 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA IDG ILLUMINATED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01458CA 7613 FLIGHT 5804 IDG CAUTION DURING T/O. DEFERRED MAINT PER MEL. 2L72 4F RTA21EA 20050316000842005031600084NM 2005 3 16 AALA20050188 120050311A2611 SMOKE DETECTOR BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW21181AN 29591 JFK INFLIGHT T2229/11 MAR TWO TO THREE MINUTES AFTER TAKEOFF FLIGHT ATTENDANTS REPORTED SMELLS IN THE CABIN. ALSO SMELLED FUMES IN COCKPIT BUT NO VISIBLE SMOKE. LEFT NUMBER 2 SMOKE ALARM IN LAVATORY SOUNDED. SMOKE REMOVAL PROCEDURE ACCOMPLISHED. LANDED JFK WITHOUT INCIDENT. REPLACED MID LAVATORY SMOKE DETECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050316000862005031600086NM 2005 3 16 SWAA050717 120050309A52406545871 FRAME BOEING737 7375H4 138449DNM R2 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29522SW 26564 DURING SCHEDULED C3 CHECK, FOUND R2 DOOR LOWER FRAME CRACKED AT AFT DOOR STOP FITTING. REMOVED AND REPLACED R2 DOOR PER MM. 2L72 4F RTA16WE 20050316000872005031600087NM 2005 3 16 SWAA050718 120050309A53306545780 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29522SW 26564 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER AFT CUTOUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050316000912005031600091NM 2005 3 16 SWAA050722 120050309A143018A80101 BOLT BOEING737 7373H4 1384600NM RT ELEV TAB WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED C4 CHECK, RT ELEVATOR TAB FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB CONTROL PUSHROD BOLTS & SPACERS PER MM. 2L72 4F RTA16WE 20050316000932005031600093EU 2005 3 16 05FDEA00404 120050307A5730 PANEL AIRBUS310 A310222 3930315EU LT WING DAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25446FE 224 LEFT WING PANEL 550GB HAS ONE ELONGATED HOLE (LANDING). REPAIRED PANEL 550GB LANDING IAW TD/JI/SI/00339/2005 AS PER FEDEX EA 6-5710-86051. 2L72 4F RTA35EU 20050317000012005031700001NM 2005 3 17 MWEA050027 120050310A3350 SWITCH BOEING717 717200 1383700NM EMERGENCY LIGHT ACTIVATED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31914ME 55177 EMERGENCY LIGHTS DON'T WORK WHEN SWITCH IS SELECTED ON. PERFORMED RETURN TO SERVICE CHECK, CYCLED FORWARD CABIN EMERGENCY LIGHT SWITCH AND OPERATION NORMAL. 2L72 4F TRA6WE 20050317000022005031700002NM 2005 3 17 DHL2005752002 120050316A5250 LOCK BOEING727 727223 1384074NM COCKPIT DOOR MALFUNCTIONED A DHLAO OTHER O OTHER UKUNKNOWN 1 SO01752DH 22466 COCKPIT DOOR LOCKS WHEN CLOSED AND CAN`T BE OPENED FROM OUTSIDE. CYCLED COCKPIT DOOR SEVERAL TIMES NO AUTO LOCKING FEATURE NOTED, DOOR OPS CHECKS NORMAL IAW MM 52-50-10. 2L73 4F A3WE 20050317000032005031700003NM 2005 3 17 DHL2005770003 120050316A3270 WARNING LIGHT BOEING727 7272B7 138407LNM NLG DOOR MALFUNCTIONED A DHLAO OTHER N FALSE WARNING LDLANDING 1 SO01770AT 21953 NOSE GEAR DOOR ON S/O PANEL AND RED DOOR LIGHT ILLUMINATED FOR AN EXCESSIVE PERIOD OF TIME WHEN LANDING GEAR EXTENDED. DEFERRED NOSE GEAR DOOR INDICATION PER MEL 32-1 DMI 20102 PLACARD INSTALLED. 2L73 4F A3WE 20050317000042005031700004WP 2005 3 17 DHL2005804003 120050316A2780 CONTROL SYSTEM DOUG DC8 DC873F 302199FWP LE FLAPS MALFUNCTIONED A DHLAB EMER. DESCENT JF WARNING INDICATION FLT CONT AFFECTED LDLANDING 1 SO01804DH 46124 FLAPS SPLIT DURING DEPLOYMENT TO 12 PERCENT, PERFORMED ASYMMETRIC FLAP ABNORMAL PROCEDURE AND PARTIAL FLAP LANDING PROCEDURE. LANDED A/C WITH ZERO FLAPS. AFTER R/R OG LT INBD FLAP ACTUATOR, PERFORMED GOOD OPS CHECK OF FLAPS PER DC-8 M/M 27-51-9. 2L74 4F RT4A25 20050317000052005031700005CE 2005 3 17 DXTA200500630 120050314A2910 LINE CESSNA500 560CESSNA 2076750CE HYDRAULIC SYS LEAKING E DXTAD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 GL07361QS 5600361 BRAKES FELT SPONGY, EXCESSIVE PEDAL TRAVEL BEFORE BRAKES ENGAGED. T/S SYSTEM, BLEED BRAKES. TAXI ACFT, OPS & LEAK CHECKS GOOD IAW 560 M/M CH 32-42-00. 2L72 4F RTA22CE 20050317000062005031700006CE 2005 3 17 DXTA200500631 120050314A2910 QUICK DISCONNECT CESSNA650 650 2076802CE HYD SYSTEM DIRTY E DXTAO OTHER O OTHER LDLANDING 1 GL07794QS 6507094 ON LANDING BRAKE PEDALS FELT NORMAL, HOWEVER AIRCRAFT HAD DIFFICULTY COMING TO A STOP WITH HARD BRAKING ACTION PERFORMED. TROUBLESHOT SYSTEM, FOUND RT MAIN GEAR STRUT SQUAT SWITCH ELECTRICAL CONNECTOR VERY DIRTY. CLEANED CONNECTOR, OPS CHECK GOOD, REF CITATION 650-MM CHAPTERS 32-42-00, 32-42-04, 32-42-05, 32-42-06 AND WIRING MANUAL CHAPTERS 32-40-01 AND 32-60-02. 2L72 4F A9NM 20050317000072005031700007NM 2005 3 17 UPS05244125 120050315A3510542507 REGULATOR BOEING727 72722C 138400FNM COCKPIT OXYGEN LEAKING A IPXAK NONE O OTHER ININSP/MAINT 1 SO01941UP 19196 INSPECTION TYPE:N/A CREW OXYGEN SYSTEM LEAKING AT REGULATOR DIRECTLY ABOVE BOTTLE. REMOVED AND REPLACED CREW 02 PRESS REDUCING REGULATOR PER MM 35-11-21. LEAK AND OPS CHECK GOOD. 2L73 4F A3WE 20050317000082005031700008NM 2005 3 17 UPS05544122 120050313A3350 BATTERY BOEING757 75724APF 1384969NM EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01409UP 23731 EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY AND POWER SUPPLY PER MM 33-51-07-2. 2L72 4F RTA2NM 20050317000112005031700011SO 2005 3 17 SWIA200514680 120050306A27503075001017 CONTROL UNIT EMB 120 EMB120ER 3260203SO NACELLE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07189SW3665 3665 120048 NAC FLAPS INDICATE 15 DEGREE EXTENSION ON POWER UP WITH FLAPS UP. REMOVED AND REPLACED FECU WITH SERVICEABLE UNIT, OPERATIONAL CHECK GOOD IAW 27-50-00. 2L72 4T RTA31SO 20050317000122005031700012EA 2005 3 17 SWIA200514681 120050225A5315 ATTACH FITTING CNDAIRCL600 CL6002B19 1900309EA FLOORBEAM CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07441SW 7602 FS 280 LEFT FLOORBEAM LBL 9.0 INBOARD ATTACH CLIP CRACKED. ITEM FOUND AT C-CHECK INSPECTION. CLIP TO BE REPAIRED ON 2192818 IAW CRJ REO 601R-53-11-171 REV A. 2L72 4F RTA21EA 20050317000152005031700015SO 2005 3 17 C2XA05CLO15 120050311A335078241 INVERTER EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT INOPERATIVE A C2XAO OTHER L NO TEST NRNOT REPORTED 1 SW2714943 145040 CLE FLIGHT 2322 THE CREW REPORTED THE MID CABIN EMERGENCY LIGHTS NOT ILLUMINATING DURING PREFLIGHT TEST. MAINTENANCE REPLACED THE CENTER CABIN EMERGENCY LIGHTING INVERTER AND OPERATIONAL CHECKS GOOD. 2L72 4F RTT00011AT 20050317000182005031700018SO 2005 3 17 C2XA05IA045 120050309A3350276005 FUSE EMB 145 EMB145ER 3260211SO POWER SUPPLY BLOWN A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714940 145033 IAH - FLIGHT 3341, DURING POST FLIGHT INSPECTION THE CREW REPORTED THAT THE MAIN CABIN DOOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE OPERATIONALLY CHECKED THE EMERGENCY LIGHTS WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. DURING POST FLIGHT INSPECTION ON FLIGHT 2231 IN IAH, THE CREW AGAIN REPORTED THAT THE CABIN DOOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A FUSE IN THE NUMBER ONE EMERGENCY LIGHT POWER SUPPLY, OPERATRIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TIMES ARE NOT AVAILABLE FOR THESE PARTS. 2L72 4F RTT00011AT 20050317000192005031700019SO 2005 3 17 C2XA05IA044 120050309A335020131A BATTERY PACK EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713936147102167 145025 IAH - FLIGHT 2057 DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE EXIT SIGNS OVER THE GALLEY, ROW 2B, AND THE FLT ATTENDANTS SEAT WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050317000202005031700020SO 2005 3 17 MASA200500201 120050309A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN MALFUNCTIONED A MASAO OTHER O OTHER TXTAXI/GRND HDL 1 SW07837MJ 145367 AFTER SHUTTING DOWN ACFT IN YYZ, FLIGHT CREW REPORTED THAT EMERGENCY LIGHTS WOULD NOT EXTINGUISH UNTIL CREW CYCLED THE BATTERY AND EMERGENCY LIGHT SWITCHES. CONTRACT MAINTENANCE PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHTING SYSTEM. NO DEFECTS WERE NOTED. 2L72 4T RTT00011AT 20050317000212005031700021NE 2005 3 17 AT0500012 220050311A7200BR700715A130 ENGINE BOEING717 717200 1383700NM RROYCEBR700 BR700710A110 NE NR 1 INOPERATIVE A ZZDAE ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 SO15937AT 55091 LEFT ENGINE COMPRESSOR STALLS AND ROLL BACK AT FL310. REMOVED AND REPLACED LEFT ENGINE. 2L72 4F4 FTRA6WE E00057EN 20050317000222005031700022WP 2005 3 17 MWEA050028 120050225A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT EXPOSED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31810ME 48072 EMERGENCY TRACK LIGHTING WIRES EXPOSED. REPAIRED WIRES AND SECURED END CAP IAW 20-50-00 AND 33-50-00. OPERATION CHECK GOOD. 2L72 4F A6WE 20050317000232005031700023NM 2005 3 17 SWAA050773 120050314A55516551524 FITTING BOEING737 7373H4 1384600NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29605SW 27956 DURING SCHEDULED D-CHECK, FOUND LT & RT HORIZONTAL STAB FITTING LUG FACES CORRODED. REPAIRED FITTINGS PER SRM. 2L72 4F RTA16WE 20050317000252005031700025NM 2005 3 17 SWAA050775 120050314A53106547978 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29605SW 27956 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 867 TO BS 887, LBL 67, WL 208. REPAIRED CREASE BEAM PER SRM. 2L72 4F RTA16WE 20050317000272005031700027NM 2005 3 17 SWAA050777 120050314A575465C26606 SLAT TRACK BOEING737 7373H4 1384600NM RT WING CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29605SW 27956 DURING SCHEDULED D-CHECK, FOUND RT WING, NR 4 L/E SLAT, OUTBOARD MAIN TRACK, LOWER SURFACE CORRODED. REPAIRED TRACK PER OHM. 2L72 4F RTA16WE 20050317000292005031700029EU 2005 3 17 05FDEA00406 120050307A5313 STRINGER AIRBUS310 A310222 3930315EU FUSELAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25446FE 224 BULKPIT UNDER FLOOR STRINGER 49R 6 INCHES AFT OF FR65 HAS AN AREA OF 0.5 X 0.5 INCH OF CORROSION. REMOVED CORROSION AT BULKPIT UNDER FLOOR FR65 STG 49R IAW A310-200 SRM 51-74-10. CHECKED MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW A310-200 SRM 53-10-00 FIG 104. REPAIRED STRINGER CONNECTING SECTION IAW A310-200 SRM 51-72-10. 2L72 4F RTA35EU 20050317000302005031700030EU 2005 3 17 05FDEA00407 120050307A5315 FLOORBEAM AIRBUS310 A310222 3930315EU FUSELAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25446FE 224 BULK PIT FLOOR T-CAP BETWEEN FR65 AND FR66 24 INCHES TO RT OF CTR HAS A 6 X 1 INCHES OF CORROSION. REMOVED CORRODED SECTION & INSTALLED NEW SECTION PER A310 SRM 51-72-10 & REPROTECTED FASTENERS PER A31-200 SRM 53-21-10. T-CAP WAS CORRODED BEYOND LIMITS AS GIVEN IN A310-200 SRM 53-10-00 FIG 4. CAP HAS BEEN CORRODED UP TO 50 PERCENT MAT'L LOSS BEFORE BEING WORKED. 2L72 4F RTA35EU 20050317000312005031700031NM 2005 3 17 05FDEA00409 120050308A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25592FE 48550 MAIN DECK CARGO, SEAT TRACK FOUND CRACKED AT STA 890 TO 900, LBL 27. SEAT TRACK REPAIRED AS PER SRM 53-70-00 FIG1 VOL1. 2L73 4F RTA22WE 20050317000322005031700032NM 2005 3 17 05FDEA00410 120050308A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25592FE 48550 MAIN DECK CARGO, SEAT TRACK FOUND WORN AT STA Y= 893 TO Y= 900, X=47. REPAIRED AS PER SRM 53-70-00 FIG1 VOL1. 2L73 4F RTA22WE 20050317000332005031700033NM 2005 3 17 05FDEA00411 120050308A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25592FE 48550 MAIN DECK CARGO, SEAT TRACK FOUND CRACKED AT STA 820 TO 829, RBL 27. REPAIRED AS PER SRM 53-70-00 FIG 1, VOL 1. 2L73 4F RTA22WE 20050317000342005031700034NM 2005 3 17 05FDEA00412 120050308A5311 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25592FE 48550 MAIN DECK CARGO, FUSELAGE FRAME FOUND WITH DENT AT STA Y= 1681, LONGERON 12R. REPAIR CARRIED OUT IAW SRM 53-30-00 FIG. 1 VOL. I. COMPLIED WITH FEDEX EA 1-5330-81619. 2L73 4F RTA22WE 20050317000402005031700040WP 2005 3 17 05FDEA00413 120050308A5750NRC6068509 SUPPORT DOUG DC10 DC1010 3022110WP ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25369FE 46607 COMPLY WITH EA 8-5750-55448 WINGS - FLAP VANE SUPPORT CORROSION REWORK LT OUTBOARD FLAP. COMPLIED WITH EA 8-5750-55448. 2L73 4F A22WE 20050317000482005031700048NM 2005 3 17 UPS05M44066 120050105A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 16 LT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED ON NR 16 LT BARREL NUT HOLE PER SRM 51-21-01V2.R.35, FOUND OUT OF LIMIT. REWORKED HOLE PER EN1125-05. FAB SLEEVE BUSHING PER EO MD11-551 0-19409-I. APPLIED SEALANT PR1422B1/2 ON BARREL NUT HOLE NR 16 LT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED ON BARREL NUT HOLE 16 LT PER EN1125-05, FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20050317000532005031700053EU 2005 3 17 05FDEA00414 120050308A5341 WING ROOT AIRBUS310 A310222 3930315EU RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 TWO AREAS OF CORROSION AT RT WING TO FUSE FILLET AREA FR 39 STR 34-35 REF N00735 & E-6-5310-7-3315 A1 PT8. C/W AIRBUS S/B A310-53-2069 AND EO 6-5310-7-3315 ERF N00735. 2L72 4F RTA35EU 20050317000552005031700055SO 2005 3 17 MASA200500186 120050306A3350 CONTROL SYSTEM EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07838MJ 145384 ASH 2897 CLT, EMERGENCY FLOOR PATH LIGHTING STRIP NR 2 INOP. MAINTENANCE RESET THE EMERGENCY LIGHTING SYSTEM, OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050317000562005031700056EA 2005 3 17 MASA200500188 120050306A3350 LIGHT CNDAIRCL600 CL6002C10 1390015EA CABIN MISSING A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07504MJ 10066 ASH 7247 IAD, EMERGENCY ESCAPE PATH LIGHTING STRIP WAS MISSING. MAINTENANCE RE-SECURED THE STRIP. 2L72 4F RTA21EA 20050317000572005031700057SO 2005 3 17 MASA200500190 120050307A3350 SIGN EMB 145 EMB145LR 3260212SO RT OVERWING INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07826MJ 145214 ASH 2885 CLT, RT OVERWING EMERGENCY EXIT SIGN INOP. MAINTENANCE SECURED THE SIGN CONNECTOR AND OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050317000602005031700060SO 2005 3 17 MASA200500196 120050309A3350 LIGHT EMB 145 EMB145LR 3260212SO EMERGENCY EXIT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07826MJ 145214 ASH 2957 PHL, EMERGENCY EXIT LIGHT AT CABIN DOOR INOP. MAINTENANCE OPS CHECKED AND OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050317000632005031700063NM 2005 3 17 2005UALA00189 120050225A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE GOUGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29581UA 26701 LEFT FUSELAGE SKIN STA 754 HAS 2 EA DENTS WITH GOUGE JUST ABOVE STR 16L. SKIN WAS TRIMMED OUT AND EXTERNAL DOUBLER WAS INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050317000652005031700065NM 2005 3 17 2005UALA00191 120050225A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29581UA 26701 FUSELAGE SKIN DAMAGE AT STA 600-660 STR 16L. CONSTANT THICKNESS SKIN WAS SPLICED INTO THE SKIN PANEL USING DOUBLER STRAPS AND TRIPLERS. 2L72 4F4 FRTA2NM E17NE 20050317000662005031700066NM 2005 3 17 AALA20050165 120050228A5220BACC63CB1212SN ELEC CONNECTOR BOEING777 777223 1385213NM NR 3 DOOR INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21784AN 29588 AFW - SHORTED CONNECTOR ON LEFT NR 3 DOOR CAUSED THE SQUIB TO BLOW WHILE TESTING THE EMERGENCY POWER ASSIST SYSTEM PER B0611AA. REPLACED CONNECTOR AND REPLACED RESERVOIR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20050317000732005031700073NE 2005 3 17 2005UALA00193 220050227A7230 COMPRESSOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 2 ENGINE SURGES A UALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 WP29547UA 25368 DIVERTED TO HNL DUE TO NR 2 COMPRESSOR SURGE. FOUND VSV SYSTEM 0.125 INCHES OUT OF RIG, ALL OTHER CHECKS OKAY. 2L72 4F4 FRTA2NM E17NE 20050317000742005031700074 2005 3 17 2005UALA00194 420050224A2565680150020 O-RING BOEING747 747422 1384935NM PWA 4056 PW4056 NE SLIDE BOTTLE DEFECTIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29193UA 26890 LOW BOTTLE PRESSURE IN ONE CYLINDER. REPLACED DEFECTIVE O-RING IN REGULATOR. 2L74 4F4 FRTA20WE E24NE 20050317000762005031700076 2005 3 17 2005UALA00196 420050227A2565 GIRT BAR BOEING747 747422 1384935NM PWA 4056 PW4056 NE NR 2 DOOR MALFUNCTIONED A UALAK NONE O OTHER ININSP/MAINT 1 WP29176UA 24383 DOOR 2 RIGHT GIRT BAR WILL NOT ENGAGE WITH THE ARM SWITCH, WILL ENGAGE BY MAINTENANCE ONLY. CAUSE IS NOT FULLY KNOWN AT THIS TIME. MAY BE CAUSED BY IMPROPER HANDLING OF SLIDE DURING INSTALLATION WHICH RESULTED IN SLIDE PACK BECOMING UNRAVELED AND INTERFERRING WITH THE ARMING PROCESS. SLIDE WAS REPLACED ON THE AIRCRAFT AND THE DEFECTIVE UNIT SENT FOR COMPONENT INSPECTION AND MAINTENANCE. 2L74 4F4 FRTA20WE E24NE 20050317000842005031700084WP 2005 3 17 ABXA050070 120050308A53305919707501 SKIN DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23945AX 47551 DURING ROUTINE LINE MAINTENANCE AT ILN, FOUND THE FUSELAGE SKIN CRACKED 1 INCH LONG AT STA 897 AND LONGERON 29 RT. SKIN WAS FOUND TO BE CORRODED BEYOND LIMITS ON THE INTERIOR SURFACE UNDER LONGERON 30. INSTALLED SKIN SPLICE, REPAIRED IAW DC-9 SRM 53-04 FIG 12 C, USING 2014-T6 .063 PO 408449576 FOR SKIN, AND 2014-T6 .063 PO 408450124, 2014.T6 .025 PO 04844319 FOR DOUBLER. REINSTALLED LOWER FORWARD AND AFT DOOR JAMB CORNER REPAIR IAW REA D953-51557-MR. 2L72 4F A6WE 20050317000872005031700087WP 2005 3 17 ABXA050071 120050309A53307910780 SKIN DOUG DC9 DC941 302207NWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23968AX 47499 DURING ROUTINE LINE MAINTENANCE AT ILN, FOUND THE FUSELAGE BELLY SKIN CORRODED BEYOND LIMITS AT STATION 596 AND LONGERON 30. CUT OUT CORRODED SKIN 3.5 BY 2.5 INCH AND REPAIRED IAW ABX AIR REA D953-51559. 2L72 4F A6WE 20050315000992005031500099CE 2005 3 15 DJFA2005051 120050114A2120 DUCT CESSNA650 650 2076802CE A/C BAY LEAKING E DJFAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA23359CW 6500159 DURING CRUISE OBSERVED SMOKE IN COCKPIT. AN EMERGENCY DECLARED. AT 15,000 FT SMOKE DISSIPATED SUBSTANTIALLY & TURBULENCE ENCOUNTERED. UNEVENTFUL LANDING. MX POWERED ACFT & RAN ENGINES NUMEROUS TIMES WITH FULL ELECTRICAL LOAD, OPERATED BOTH PAC'S IN AUTO & MANUAL MODES. UNABLE TO DUPLICATED. COALESCER SOCKS INSPECTED & DUCT TEMP SENSORS OPERATIONALLY TESTED. NO DEFECTS NOTED. INVESTIGATION REVEALED LEAKING DUCT OVER NR 1 & 2 TRANSPONDERS. DUCT REPOSITIONED & RESECURED. A DISCOLORED FLOOD LIGHT LENS ALSO REPLACED. ENGINES RAN AT HIGH POWER WITH BLEEDS ON. PACK AND ENGINE ANTI-ICE WERE RAN WITH NO EVIDENCE OF SMOKE OR SMELL. TEST FLIGHT PROVED SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F A9NM 20050315001072005031500107SO 2005 3 15 1316012205 120050122A32501159SCH4033 SOLENOID VALVE GULSTMG1159 GIV 3980115SO NLG STEERING FAILED E N93AO OTHER J WARNING INDICATION LDLANDING 1 SO13416QS 1316 ON TOUCHDOWN CREW RECEIVED NOSE WHEEL STEERING FAILURE MESSAGE WITH NO NOSE WHEEL STEERING. 2L72 4F RTA12EA 20050315001102005031500110NE 2005 3 15 05007 220050124A7230 COMPRESSOR BOEING747 7472B4B 138481BNM PWA JT9 JT9D7J 52054NE NR 2 ENGINE STALLED A KCSAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CLCLIMB 1 GL23710CK80296 21097 662588 NR 2 ENGINE COMPRESSOR STALL AT 31,500 FT AND AGAIN AT FL350. ENGINE SHUTDOWN. REMOVED AND REPLACED NR 2 ENGINE. PERFORMED TEST NUMBERS 3, 6, 8, 9, 11, 12, AND 16. TRIM RUNS PERFORMED. OPS AND LEAK CHECK GOOD AND FINAL PARAMETERS RECORDED. ALL WORK PERFORMED IAW B747 MM 71-00-00. 2L74 4F4 FRTA20WE E20EA 20050315001152005031500115CE 2005 3 15 ACE020105 120050201A32601003810061 UPLOCK SWITCH BEECH 1900 1900C 1154161CE NLG MALFUNCTIONED E YADAL ABORTED APPROACH J WARNING INDICATION LDLANDING 1 AL03114AX UC36 GEAR WARNING REMAINED ON AFTER GEAR INDICATED THREE GREEN. PILOT DID A GO-AROUND AND ON NEXT GEAR EXTENSION, ALL INDICATIONS NORMAL. UNEVENTFUL LANDING. MAINTENANCE REPLACED NOSE GEAR UPLOCK SWITCH. 2L72 4T RTA24CE 20050315001312005031500131CE 2005 3 15 DJFA2005062 120050220A2840 WARNING LIGHT CESSNA525 525 2076601CE COCKPIT ILLUMINATED E DJFAO OTHER J WARNING INDICATION CRCRUISE 1 EA23254CW 5250154 CREW REPORTED, 1 HR AFTER TAKEOFF AT 35,000 FT RIGHT FUEL FILTER BYPASS, & MASTER CAUTION LIGHTS ILLUMINATED. RIGHT FUEL BOOST PUMP WAS TURNED ON & ACFT BEGAN DIVERTING. LEVELING OFF 13,000 FT LEFT FUEL FILTER BYPASS LIGHT ILLUM. LEFT BOOST PUMP WAS TURNED ON & AN EMERGENCY DECLARED. ACFT LANDED. FUEL REMAINING ON BOARD 2,000 LBS. LIGHTS HAD REMAINED ILLUM UNTIL ENGINE SHUTDOWN. MX TOOK FUEL SAMPLES FROM LEFT & RIGHT WING TANKS FOR ANALYSIS. ACFT DEFUELED & SUMPED. LEFT & RIGHT ENGINE FUEL FILTERS REMOVED AND INSPECTED. NO DEFECTS IN FUEL FILTERS. NEW FUEL FILTERS INSTALLED. ACFT WAS REFUELED, AND GROUND RUN. NO FURTHER DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 1L72 4F RTA1WI 20050315001322005031500132 2005 3 15 FX7A200500002 420050212A34255223122012 INDICATOR BOEING727 727231 1384079NM PWA JT8 JT8D NE COCKPIT INOPERATIVE A FX7AA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO1954348 21967 CAPTAINS ADI INOPERATIVE. 2L73 4F4 F A3WE E2EA 20050315001382005031500138EA 2005 3 15 SWIA200514615 120050218A2751855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA T/E FLAP MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION LDLANDING 1 NM07403SW5846 5846 7028 FLAPS FAIL CAUTION MESSAGE. REPLACED RIGHT BPSU IAW MM 27-51-10. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050315001412005031500141EA 2005 3 15 SWIA200514620 120050217A2722 ACTUATOR CNDAIRCL600 CL6002C10 1390015EA RUDDER MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07719SK 27853 RUDDER LIMIT FAULT STATUS MESSAGE. REPLACED NR 1 RUDDER LIMITER ACTUATOR (A203) IAW CRJ MM 27-25-03. OPERATIONAL CHECK GOOD. P/N BA670-93490-3, S/N OFF 0513. 2L72 4F RTA21EA 20050315001602005031500160SO 2005 3 15 C2XA05SH012 120050222A532014521700007 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2722909 145459 SHV - DURING C-CHECK CORROSION ON LT OMEGA BEAM I/B SIDE BETWEEN FR20 TO FR29. MAINTENANCE REMOVED THE DAMAGE AREA AND PERFORMED REPAIR IAW EMB SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURNED TO SERVICE. 2L72 4T RTT00011AT 20050315001642005031500164WP 2005 3 15 ARWA20050206 120050220A2611 SMOKE DETECTOR DOUG DC8 DC863F 302198FWP CARGO BAY FAULTY A ARWAO OTHER N FALSE WARNING CRCRUISE 1 SO19661AV 45969 IN FLIGHT MAIN CARGO LIGHT CAME ON. FALSE ALERT; FOUND NR 1 SMOKE DETECTOR AND NR 4 SMOKE DETECTOR LIGHTS REMAINED ILLUMINATED WHILE TESTING. ENTERED ON DMI 19008 AS PER MEL 26-6 CAT-C. RELAMP NR 1 AND NR 4 BEACON LIGHT BULB AT NR 1 AND NR 4 SMOKE DETECTOR; SYSTEMS OPERATIONAL CHECK NORMAL IN ACCORDANCE WITH MM 26-10-5. THIS CLEARED DMI 19008. 2L74 4F 4A25 20050315001782005031500178NM 2005 3 15 AALA20050152 120050217A2560 CABLE BOEING757 757223 1384957NM R1 DOOR DEFECTIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21626AA 24584 TUL - RIGHT NUMBER ONE PASSENGER DOOR GIRT BAR FAILED TO DISENGAGE WHEN DOOR WAS ARMED THEN OPENED FROM THE OUTSIDE. DISARM CABLE WAS ADJUSTED TO THE MAXIMUM POSITION AND STILL WOULD NOT DISARM GIRT BAR. REPLACED DISARM CABLE AND RIGGED DOOR MECHANISM IN ACCORDANCE WITH MAINTENANCE MANUAL 52 11 20 3. 2L72 4F RTA2NM 20050315001902005031500190NM 2005 3 15 AALA20050169 120050222A5730 SKIN BOEING767 767323 1385205NM LT WING WORN A AALAK NONE O OTHER ININSP/MAINT 1 SW2139364 24045 AFW - LEFTHAND LOWER WING OF SKIN HAS TWO AREAS OF WEAR CAUSED BY WING TO BODY PANELS AT WING BUTTLINE 103 AND 105. WEAR IS BEYOND SRM LIMITS. AREA IS 36 BY 2.0 INCHES WITH A DEPTH OF 0.023 INCHES. BLEND THE WORN AREA PER SRM 51 20 01 AND DYE PENETRANT INSPECT TO ENSURE THE REWORKED AREA IS FREE OF DEFECTS. ROTOPEEN PER SOPM 20 10 03 AND REFINISH. APPLY THE TEFLON PAINT PER DRAWING 110T3102. 2L72 4F RTA1NM 20050315001962005031500196NM 2005 3 15 AALA20050157 120050227A3350BPS73 BATTERY PACK BOEING767 767323 1385205NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21359AA 24040 JFK - EMERGENCY LIGHT AT SEATS 20 AND 21 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEATS 20 AND 21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050315002062005031500206WP 2005 3 15 ABXA050039 120050302A3260 CONTACT DOUG DC9 DC933F 302207AWP COCKPIT WORN A ABXAL ABORTED APPROACH O OTHER APAPPROACH 1 GL23934AX 47462 UPON LOWERING THE LANDING GEAR, NO NOSE GEAR SAFE LIGHT. TESTED IN BRIGHT AND DIM. AFTER INITIATING A GO-AROUND, THE NOSE GEAR UNSAFE LIGHT ILLUMINATED (APPROXIMATELY 30 SECONDS). FOUND BULB CONTACTS TO BE WORN. RELAMPED, OPS CHECKED GOOD. 2L72 4F A6WE 20050315002072005031500207WP 2005 3 15 ABXA050055 120050305A21205912287511 CHECK VALVE DOUG DC9 DC932 3022066WP A/C BAY NOT SEATED A ABXAO OTHER J WARNING INDICATION CLCLIMB 1 GL23989AX 47314 CABIN PRESSURE ANNUNCIATOR ILLUMINATED PASSING 10,000 FT MSL. UNABLE TO PRESSURIZE AIRCRAFT MANUALLY OR WITH AUTOMATIC CONTROLLER. VISUALLY INSPECTED AIRCRAFT, NO DEFECTS NOTED. FOUND GROUND AIR CONDITIONING CHECK VALVE NOT SEATED. MANUALLY CYCLED CHECK VALVE FLAPPER IAW DC9 AMM 21-20-04. AIRCRAFT PRESSURIZES NORMALLY ON THE GROUND. 2L72 4F A6WE 20050315002152005031500215WP 2005 3 15 ABXA050040 120050207A53206917286505AX ATTACH FITTING DOUG DC9 DC933F 302207AWP RT MLG WW CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23933AX 47291 RIGHT WHEEL WELL BULKHEAD TO KEEL ATTACH FITTING FS 718 CRACKED. REPLACED FITTING IAW DC-9 SERVICE BULLETIN 53-80. 2L72 4F A6WE 20050315002242005031500224NE 2005 3 15 2005F00044 120050221A326076552009040441 WIRE HARNESS SKRSKYS76 S76A 8143006NE NLG UPLOCK DAMAGED A ALGAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW03522AL 760236 AFTR TAKEOFF, GEAR PLACED IN UP POSITION THREE GREEN LIGHTS STAYED ON RED LIGHT OUT WITH GEAR HANDLE UP OR DOWN POSITION. MAINTENANCE INSTALLED SERVICEABLE UPLIMIT PROXIMITY HARNESS ASSY RIGHT MAIN. REPAIRED THE NOSE UPLIMIT HARNESS, GROUND CHECK GOOD AND ALL WORK DONE IAW THE S-76 MM. (M) 1G72 3U H1NE 20050315002252005031500225WP 2005 3 15 ARWA20050301 120050302A321357591681 LINK DOUG DC8 DC863F 302198FWP LT MLG CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19441AV 45988 LEFT MAIN GEAR SCISSOR CRACKED AT BOLT HEAD OF BOLT BROKEN FOUND AT POST FLIGHT AT MSLP. REMOVED AND REPLACED BOLT AND UPPER LINK IN ACCORDANCE WITH MM 32-11-4. 2L74 4F 4A25 20050315002372005031500237NM 2005 3 15 USAA050206 120050101A5754 SKIN BOEING737 7374B7 1384702NM SLAT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19436US41647 24558 PIT - FOUND SLAT CRACKED .5 INCH, FORWARD OF INBOARD AUX TRACK LOWER SURFACE AFT FASTENER. INSTALLED DOUBLER PER SRM 57-43-01 FIG 206. (M) 2L72 4F RTA16WE 20050315002392005031500239NM 2005 3 15 USAA050209 120050109A5730 SKIN PANEL BOEING737 7374B7 1384702NM WING CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19436US41647 24558 PIT - FOUND SKIN PANEL CRACKED .5 INCH LONG, OUTBOARD SIDE OF PYLON ABOVE MID SPAR FITTING LOWER SKIN PANEL SLAT STATION 3.25. STOP DRILLED, INSTALLED FILLER AND DOUBLER FREEZE PLUG PER TR 57-41-02, SRM 51-20-10 AND EA 79764. (M) 2L72 4F RTA16WE 20050315002442005031500244NM 2005 3 15 USAA050214 120050112A5315 FLOORBEAM BOEING737 7374B7 1384702NM FUSLEAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19436US41647 24558 PIT - FOUND BEAM CORRODED 2 INCH BY 100 INCH AREA, BS 986.5 FLOORBEAM ENTIRE UPPER SURFACE. SPLICED IN NEW UPPER CAP PER TYPICAL REPAIR 53-60-01 REV A. (M) 2L72 4F RTA16WE 20050315002512005031500251NM 2005 3 15 USAA050216 120050127A5730 SKIN PANEL BOEING737 7374B7 1384702NM LT WING CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19436US41647 24558 PIT - FOUND SKIN PANEL CRACKED 1 INCH, LEFT LEADING EDGE LOWER SKIN PANEL AT SLAT STATION 3.25. FILLER AND DOUBLER INSTALLED PER TYPICAL REPAIR 57-41-02. (M) 2L72 4F RTA16WE 20050315002752005031500275 2005 3 15 CIHA200596001 420050224A3425 INDICATOR BOEING727 7272J4 1384006NM COCKPIT MALFUNCTIONED A C1HAA UNSCHED LANDING O OTHER CRCRUISE 1 GL15696CA 22574 CAPTAINS ADI SHOWED A 5 DEG BANK TURN TO THE LEFT WITH AIRCRAFT NOT IN A TURN ATTITUDE FLAG IN VIEW, WHEN DUMP VALVES WERE OPENED TANK NR 2 RT FWD AND LF AFT BOOST PUMP C/B'S POPPED, TANK NR 3 DUMP VALVE INTRANSIT LIGHT DID NOT ILLUMINATE WHEN THE VALVE SWITCH WAS MOVED TO CLOSED, REPLACED NR 1 ADI AND OPS CK GOOD PER MM 34-62-11, COMPLIED WITH FUEL BOOST PUMP CHECK PER MM 28-22-00 NR 2 RT FWD AND NR 2 LF AFT BOOST PUMP CHECK GOOD OK FOR SERVICE, PLACED ON MEL 28-9-2. CAT-C. C06970. COMPLIED WITH DDG 28-9-2. DUMP VALVE OP'S CHECK GOOD. REMOVED FROM MEL. 2L73 4F RTA3WE 20050315002802005031500280SO 2005 3 15 C2XA05IA042 120050304A3350110049 POWER SUPPLY EMB 145 EMB145LR 3260212SO CABIN DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714543 145553 BNA - DURING MAINTENANCE INSPECTION, THE OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER 4 BATTERY PACK WITH NO HELP, THE AIRCRAFT WAS RETURNED TO SERVICE ON MEL 33-50-00/1 CAT-C. THE AIRCRAFT LANDED AT IAH ON FLIGHT 2793 WHERE MAINTENANCE REMOVED AND REPLACE THE NR 4 EMERGENCY LIGHT POWER SUPPLY, OPERATIONALLY CHECKED WITH NO DEFECTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. NOTE: THIS PART IS NOT SERIALIZED, AND TIMES ARE NOT AVAILABLE. 2L72 4T RTT00011AT 20050315002812005031500281SO 2005 3 15 C2XA05IA038 120050304A335020131A BATTERY PACK EMB 145 EMB145ER 3260211SO CABIN DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW27139367444 765 145025 IAH - FLIGHT 2057, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT SEVERAL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050315002822005031500282NE 2005 3 15 2005F00048 120050206A3260 WARNING LIGHT SKRSKYS76 S76A 8143006NE MLG ILLUMINATED A ALGAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW03522AL 760236 IN FLIGHT ABOVE 130 KNOTS, AFTER TAKEOFF RETRACT LANDING GEAR, ALL LIGHT EXTINGUISHED AND ALL INDICATIONS NORMAL. AT ABOUT 130 KNOTS INDICATED AIRSPEED NOSE GEAR GREEN LIGHT CAME ON INDICATING NOSE GEAR DOWN OR NOSE GEAR DOOR OPEN. REDUCED AIRSPEED AND RECYCLED GEAR, ALL LIGHT EXTINGUISHED, ACCELERATED TO 130 KNOTS AND NOSE GEAR GREEN LIGHT ILLUMINATED, RETURNED TO ICY BASE AND CONSULTED MAINTENANCE. MAINTENANCE REMOVED NOSE ACTUATOR AND INSTALLED SERVICEABLE ACTUATOR AND CHECKED GEAR ON THE HYDRAULIC MULE NO DEFECTS FOUND. (M) 1G72 3U H1NE 20050315002912005031500291NM 2005 3 15 USAA050296 120050213A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU50526 23706 PIT - FOUND SKIN CRACKED 1.5 INCH, FORWARD SERVICE DOOR CUTOUT AFT LOWER CORNER. INSTALLED DOUBLER PER SRM 53-10-01. (M) 2L72 4F RTA16WE 20050315002942005031500294NM 2005 3 15 USAA050254 120050215A5311 FRAME BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19519AU50516 23705 CLT - FOUND FRAME CRACKED .5 INCH, STATION 827 STRINGER 9R. INSTALLED FILLER/DOUBLER REPAIR IAW TR 53-10-20A. (M) 2L72 4F RTA16WE 20050315003012005031500301SO 2005 3 15 C2XA05CL012 120050225A323422270100001 CHECK VALVE EMB 145 EMB145ER 3260211SO NLG INOPERATIVE A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW27159261643116431 145005 CLE FLIGHT 2150, CREW REPORTED THAT AFTER TAKEOFF THE NOSE LANDING GEAR FAILED TO RETRACT. RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED SYSTEM AND REMOVED AND REPLACED THE NOSE LANDING GEAR CHECK VALVE. ALL OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20050315003052005031500305NM 2005 3 15 UIEA200500007 120050210A32302670296 SEQUENCE VALVE BOEING747 7472D3B 1384805NM MLG FAILED A UIEAO OTHER EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 EA15506MC 21252 NOSE GEAR CYCLED X3 DURING CLIMB-OUT, TO DOORS OPEN AND NOSE GEAR INTRANSIT. ALSO AT THE SAME TIME RT WING DOOR ANNUNCIATOR ON AND GEAR INTRANSIT. ALL CONDITIONS ASSOCIATED WITH AIRCRAFT VIBRATION NOISE VIA AIR STREAM. ALL THREE CYCLES WERE PRECEDED BY RED GEAR WARNING LIGHT AT LANDING GEAR LEVER. FOUND RT WING GEAR DOOR SYSTEM CABLE SLIGHTLY SLACK FROM GROUND DOOR RELEASE HANDLE TO DIFFERENTIAL. ADJUSTED TENSION PER MM 32-35-00. REMOVED AND REPLACED NOSE GEAR OPERATED DOOR SEQ VALVE AND NOSE GEAR DOOR OPERATED SEQUENCE VALVE AS A PRECAUTION PER MCC REQUEST. PERFORMED GEAR RETRACTION AND EXTENSION CHECK. OPS CHECKED OK AIRCRAFT RETURNED TO SERVICE. (M) 2L74 4F RTA20WE 20050315003062005031500306SO 2005 3 15 C2XA05IA033 120050301A361014531128401 DUCT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL LT ENGINE RUPTURED A C2XAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 SW2713949 145057 CAE3007A1P IAH - FLIGHT 2654, ON TAKEOFF THE CREW REPORTED A NUMBER ONE ENGINE OVERTEMP AND FIRE WARNING. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE 13TH STAGE ENGINE BLEED TUBE TO BE RUPTURED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BLEED TUBE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THIS PART IS NOT SERIALIZED, AND TIMES ARE NOT AVAILABLE. 2L72 4T4 FRTT00011ATTE6CH 20050315003162005031500316WP 2005 3 15 GTIA050022 120050118A5320 INTERCOSTAL DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FOUND LEFT AFT FUSELAGE LONGERON 8L FS 1338 INTERCOSTAL HAS CORROSION. REMOVED INTERCOSTAL 8L FS 1338, LOCATED, DRILLED NEW INTERCOSTAL, TREATED PRIMED AND INSTALLED. (M) 2L72 4F A6WE 20050315003302005031500330NE 2005 3 15 GTIA050012 220050118A7200 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE RIGHT FAILED A GTIAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 GL23803NK 48087 FLT 1581 - ACY - ENGINE FAILURE AT FL 240, SURGE ON AIRCRAFT, RIGHT ENGINE FAILED AIRCRAFT YAWED RIGHT, NO FIRE WARNING OR INDICATION. EGT, N1 AND N2 DECREASED RAPIDLY, SHUT DOWN ENGINE AND DIVERTED IN ACY. REMOVED AND REPLACED NR 2 ENGINE. (M) 2L72 4F4 F A6WE E2EA 20050315003412005031500341NM 2005 3 15 SWAA050694 120050307A57536546435 FLAP BOEING737 7373Q8 1384670NM RT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29317WN 24068 DURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2L72 4F RTA16WE 20050315003572005031500357EA 2005 3 15 VTZA200500007 120050307A531260034017595 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27639BR 7313 RT SIDE PILOTS BULKHEAD AT FS 280 RBL 9.0 IS CRACKED AT 1.0 INCH IN WEB RADIUS. 2L72 4F RTA21EA 20050316000012005031600001NM 2005 3 16 USAA050312 120050209A55301130444 HINGE BRACKET BOEING737 7373B7 1384580NM VERT STABILIZER WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU50570 23706 PIT - FOUND HINGE PLATES WITH THREE WORN HOLES .25 INCH DIAMETER, RUDDER HINGE NR 7 PLATES ON VERTICAL STABILIZER. DEFECTIVE PART REPLACED WITH IDENT PART PER AMM 55-00-00. (M) 2L72 4F RTA16WE 20050316000022005031600002CE 2005 3 16 4511302132005 120050213A3600 CLAMP LEAR 45 45LEAR 5170805CE RT PYLON LOOSE E J7SAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW05416FX 113 CREW ADVISED, THE RIGHT PYLON OVERHEAT ILLUMINATED IN CLIMB AT FL 17.0 WITH NAC AND ANTI-ICE SELECTED TO THE OFF POSITION. CREW REDUCED RIGHT ENGINE N1 TO 75 PERCENT FOR 1 MINUTE THEN TO IDLE FOR 2 MINUTES. CAS MESSAGE WOULD NOT EXTINGUISH. CREW FOLLOWED ACFT CHECKLIST AND SHUTDOWN ENGINE IN FLIGHT. NO PAX ON BOARD. FOUND CLAMP UNDER RT PYLON LP DUCT NEAR S-144 OVERHEAT SWITCH NOT SECURE, LEAKING AIR. SECURED CLAMP AND RAN ENGINES AT POWER, NO LEAKS NOTED. OPS CHECK GOOD. 2L72 4F RTT00008WI 20050316000082005031600008NM 2005 3 16 DL757050146 120050302A5220SF15120110 SEAL BOEING757 757232 1384965NM ESCAPE HATCH LEAKING A DALAB EMER. DESCENT O OTHER CRCRUISE 1 SO27624DL 22914 CABIN ALTITUDE DISCRETE ON EICAS AND OVERHEAD PANEL AT FL335. FOUND RT AFT OVERWING EXIT HATCH SEAL LEAKING. REPLACED SEAL. 2L72 4F RTA2NM 20050316000162005031600016NM 2005 3 16 DL73S050154 120050309A490085129D APU BOEING737 737232 1384475NM APU BAY SMOKE A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27331DL35023 23103 50144 DURING APU START CABIN FILLED WITH SMOKE. RAN PACKS USING EXT CART, NO SMELL NOTED. STARTED ENGINES, NO SMELL WITH PACKS ON / OFF. FWD APU MCO PLACARD MEL 49-00-01A. 2L72 4F RTA16WE 20050316000442005031600044WP 2005 3 16 UPS05844041 120050216A55225644420508 SKIN DOUG DC8 DC873F 302199FWP ELEVATOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01811UP 46089 INSPECTION TYPE:C2 RT ELEVATOR UPPER SKIN SURFACE I/B SIDE HAS A LIGHTENING STRIKE WITH .5 INCH CRACK STA XE 50. NDT VERIFIED .5 INCH CRACK PER NDT SPM 06-10-01.001. STOP DRILLED CRACK IAW SRM 55-2-1 FIG 10. NDT VERIFIED CRACK TERMINATES AT STOP DRILL PER NDT SPM 06-10-01.001. REPAIRED RT ELEVATOR PER SRM 55-2-1 FIG 10, CALCULATED WEIGHT/BALANCE PER SRM 51-04-08. NEW BALANCE WEIGHT IS -1445.4. INSTALLED NEW BALANCE DATA PLATE. 2L74 4F RT4A25 20050316000492005031600049WP 2005 3 16 UPS05844064 120050215A57305769545109 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01811UP 46089 INSPECTION TYPE: C2 LT L/E AT APPROX 660 HAS CORROSION AND FLAKING. REPAIRED LT L/E WING UPPER SKIN REPAIR AT XFS 710-824 IAW UPS EO DC8-57-20127, SAA SK 811-933. 2L74 4F RT4A25 20050316000542005031600054NM 2005 3 16 2005UALA00234 120050310A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29582UA 26702 DOOR 4L AFT FRAME CORROSION AT STA 1681 BOTTOM OF STR 17L. DAMAGE CAUSED BY TYPICAL FLOOR STRUCTURE CORROSION. DAMAGE WAS REMOVED AND REPAIR ANGLES WERE FABRICATED AND INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050316000632005031600063NM 2005 3 16 373PA0054 120050224A335020121 CHARGER BOEING737 7373Y0 1384671NM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05373PA 23749 EMERGENCY EXIT LIGHT AT R-2 DOOR INOP. REPLACED BATTERY CHARGER PER MM 33-51-51. 2L72 4F RTA16WE 20050316000782005031600078NM 2005 3 16 DHL2005781540 120050215A5230 DOOR FRAME BOEING727 727227 1384078NM CARGO DOOR GOUGED A DHLAO OTHER O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A C-CHECK, FWD CARGO COMPT C-1 DOOR LWR FWD CORNER DOOR FRAME IS GOUGED, PUNCTURE & FLAT SPOTTED. REMOVED AND REPLACED A/C DOOR LWR FWD CORNER DOOR FRAME PO4496403, P/N 65-57146-4 IAW B727 SRM 51-30-2. 2L73 4F A3WE 20050317000102005031700010EA 2005 3 17 SWIA200514679 120050306A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07913SW7861 7861 7597 FLT SPOILERS FAULT (STATUS) ON LEFT WING SIDE. REPLACED NR 2 ACTUATOR FOR LEFT WING FLT SPOILER IAW CRJ MM 27-62-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050317000142005031700014SO 2005 3 17 C2XA05TY27 120050308A3350110049 BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DEFECTIVE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714543 145553 TYS DURING A 4A INSPECTION, INSPECTION FOUND THE AFT EMERGENCY LIGHT INOP. MAINT REMOVED AND REPLACED THE BATTERY UNIT AND OPS CHECKS GOOD. 2L72 4T RTT00011AT 20050317000162005031700016WP 2005 3 17 UPS05844113 120050221A53405750540502 FITTING DOUG DC8 DC873F 302199FWP LONGERON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE:C1 LONGERON 11L SPLICE FITTING CRACKED STA 660-680. REMOVED AND REPLACED FITTING REF SRM 51-1-21, 51-3-2, NDTSPM06-10-01. 2L74 4F RT4A25 20050317000172005031700017WP 2005 3 17 UPS05844119 120050224A53404772397U1 FITTING DOUG DC8 DC873F 302199FWP LONGERON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE:C1 LONGERON 10L END FITTING CRACKED AT STA 1770. REMOVED AND REPLACED FITTING REF SRM 51-1-21, 51-1-20D. 2L74 4F RT4A25 20050317000282005031700028NM 2005 3 17 SWAA050778 120050314A53116546550 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29605SW 27956 DURING SCHEDULED D-CHECK, FOUND 2 EA FUSELAGE FRAMES CRACKED AT BS 360 & BS 787, STR 8R TO STR 9R. REPAIRED FRAMES PER SRM. 2L72 4F RTA16WE 20050317000352005031700035NM 2005 3 17 05FDEA00502 120050312A5270 WARNING LIGHT BOEING727 727200 138407ENM AIRSTAIR DOOR ILLUMINATED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25269FE 21675 CLIMBING THROUGH FL200, AFT AIRSTAIR LIGHT ILLUMINATED. DIVERTED TO EWR ACCORDING TO QRH. MEL 12MAR05. RELEASED FOR SERVICE PER MEL/CDL: 52-06-B CATEGORY: C EXPIRATION: 22MAR05 MEL 52-06-B: AMBER AFT AIRSTAIR DOOR WARNING LIGHT INOP. C/W MX PROCEDURES PRIOR TO DEPARTURE. FOUND AFT STAIRS UPLOCK SWITCH (S268) FUNCTIONS OK, ALSO SWITCH WAS REPLACED ON 2/17/05. FOUND STAIRS UPPER HANDLE DETENT SWITCH OUT OF ADJUSTMENT. REPLACED HANDLE SWITCH (S395), AND ADJUSTED PER AWW 52-70-001-5. AFT STAIR INDICATOR SYS OPS GOOD, 52-70-001-5. RII:094451. 2L73 4F RTA3WE 20050317000392005031700039EA 2005 3 17 QXEA200500353 120050210A26119847101505 CHIMNEY CNDAIRCL600 CL6002C10 1390015EA FWD CARGO DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09608QX7847 10026 PDX - MAINTENANCE FOUND THE FORWARD CARGO BAY CHIMNEY DAMAGED AND REPLACED THE SAME. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20050317000512005031700051NM 2005 3 17 UPS05M44069 120050103A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 35 LT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED ON BARREL NUT HOLE NR 35 LT PER SRM 51-21-01.V2.R.36, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 35 LT PER SRM 51-21-01.V2.R36. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 ON BARREL NUT HOLE NR 34 LT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19049-I. REPAIR COMPLETED AT BARREL NUT HOLE NR 34 LT PER EN1141-05, FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20050317000542005031700054EU 2005 3 17 05FDEA00415 120050308A5322 SHEAR TIE AIRBUS310 A310222 3930315EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 BULK PIT UNDER FLOOR FR 68 FWD 10 IN STR 53R HAS CORROSION AN AREA EXTENDING UNDER SHEAR TIE AND FASTENERS. REPAIRED AREA IAW SRM 53-10-00 FIG 104 AND SRM 53-10-14 REF N00749. 2L72 4F RTA35EU 20050317000612005031700061NM 2005 3 17 2005UALA00187 120050225A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29581UA 26701 FUSELAGE SKIN HAS DENTS STA 413, STR, 15L - 17L. FUSELAGE SKIN WAS TRIMMED AND AN EXTERNAL DOUBLER WAS INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050317000622005031700062NM 2005 3 17 2005UALA00188 120050225A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29581UA 26701 AFT PIT STA 1360 FRAME DENTED STR 26L. FRAME WAS TRIMMED AND ANGLE DOUBLERS WERE INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050317000642005031700064NM 2005 3 17 2005UALA00190 120050227A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29583UA 26705 FLOORBEAM AT STA 324 RBL 40 CORRODED. DAMAGED AREA OF FLOORBEAM WAS REMOVED AND REPAIR PARTS FABRICATED AND INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050317000902005031700090NM 2005 3 17 2005UALA00204 120050302A5322 SHEAR TIE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29582UA 26702 AFT PIT STA 1520, RBL 11, SHEAR TIE CORRODED. REPLACEMENT SHEAR TIE WAS FABRICATED AND INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050317000952005031700095 2005 3 17 2005UALA00208 420050303A2565 O-RING BOEING757 757222 1384956NM PWA 2037 PW2037 NE SLIDE BOTTLE LEAKING A UALAK NONE O OTHER ININSP/MAINT 1 WP29595UA 28748 ESCAPE SLIDE BOTTLE HAS LOW PRESSURE. FILLER VALVE O-RING WAS LEAKING. FILLER VALVE O-RING WAS REPLACED. 2L72 4F4 FRTA2NM E17NE 20050317000972005031700097 2005 3 17 SWAA050711 420050306A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29322SW 23343 L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF HOUSING. SLIDE DID NOT DEPLOY. REINSTALLED L1 DOOR SLIDE PER MM. 2L72 4F RTA16WE 20050317001002005031700100NM 2005 3 17 SWAA050714 120050308A53106519603 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29605SW 27956 DURING SCHEDULED D-CHECK, FOUND CORROSION ON CREASE BEAM WEB AT BS 363, STR 17R. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050317001032005031700103WP 2005 3 17 0500259610 120050208A5312 STIFFENER DOUG DC9 DC932 3022066WP BULKHEAD CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01610NW 47432 DURING H-CHECK FOUND CRACK IN AFT CARGO COMPARTMENT FORWARD BULKHEAD VERTICAL STIFFENER AT BS 756 L26L. REPAIRED PER EA 99-201836. 2L72 4F A6WE 20050317001052005031700105SO 2005 3 17 CHQA200500047 120050303A335066368 LIGHT EMB 135 EMB135KL 3260302SO CABIN INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11372SK 145538 EMERGENCY EGRESS FLOOR PROXIMITY LIGHT STRIP NR 7 IN INOPERATIVE. REMOVED AND REPLACED EMERGENCY EGRESS FLOOR LIGHT IAW EMB 140 MM 33-50-00-5. 2L72 4F RTT00011AT 20050317001062005031700106NM 2005 3 17 AT0500010 120050309A291366180 PUMP BOEING717 717200 1383700NM RT ENGINE INOPERATIVE A ZZDAB EMER. DESCENT KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 SO15942AT 55005 AFTER HYD AUX & TRANS PUMPS TURNED ON DURING IN RANGE CK LIST, LEVEL 2 RT HYD QTY LO INDICATION APPEARED. PERFORMED QRH CHECKLIST & LANDED. PINNED GEAR & CHECKED GEAR DOORS UP BEFORE BEING TOWED TO GATE AT HYD INDICATED 0 QTY DURING ENTIRE PROCEDURE. FOUND LINE FROM HYD HAND PUMP TO HYD SYSTEM TO BE CRACKED. CAPPED BOTH ENDS OF DEFECTIVE LINE. REMOVED AND REPLACED RT ENGINE DRIVEN HYD PUMP AND RT SYSTEM HYD FILTERS. FOUND NO EVIDENCE OF HYD PUMP OR AUX PUMP FAILURE. 2L72 4F TRA6WE 20050317001072005031700107EA 2005 3 17 COMA0560171 120050312A5270 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA PAX DOOR ILLUMINATED A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01957CA 7109 FLIGHT 5705 DURING CLIMBOUT OF CVG RECEIVED A CABIN DOOR HANDLE MESSAGE, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. PERFORMED OPERATIONAL CHECK OF CABIN DOOR AND PRESSURIZATION, DISCREPANCY COULD NOT BE DUPLICATED. 2L72 4F RTA21EA 20050317001082005031700108EA 2005 3 17 COMA0560174 120050311A2751 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01471CA 7655 FLIGHT 5102 RECEIVED A FLAP FAIL CAUTION DURING APPROACH AT ZERO DEGREE FLAP SETTING. CREW DECLARED AN EMERGENCY, ABORTED 1ST APPROACH, THEN LANDED WITHOUT INCIDENT. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE FIRST EVENT MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A, B, C AND E), FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2L72 4F RTA21EA 20050317001092005031700109WP 2005 3 17 DHL2005802003 120050312A5270 ELEC CONNECTOR DOUG DC8 DC873 302199CWP MLG DOORS FAILED A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01802DH 46076 UPON RETRACTING LANDING GEAR DOORS NOT LATCHED LIGHT CAME ON, AS WELL AS LEFT DOOR UNSAFE ON S/O PANEL. ABNORMAL PROCEDURE GEAR OR DOOR NOT LATCHED LIGHT ILLUMINATED WAS PERFORMED, DOORS NOT LATCHED LIGHT CAME BACK ON AS WELL AS THE RIGHT DOOR UNSAFE LIGHT ON S/O PANEL. GEAR WAS CYCLED AGAIN, DOORS NOT LATCHED LIGHT CAME BACK ON WITH LEFT AND RIGHT DOOR UNSAFE LIGHTS ON S/O PANEL. GEAR WAS CYCLED A FOURTH TIME. REMOVED AND REPLACED LT & RT MLG DOOR CLOSE SWITCHES CONNECTORS, OPS CHECKED GOOD PER MM 32-60-0. 2L74 4F RT4A25 20050317001122005031700112EA 2005 3 17 SWIA200514684 120050225A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07441SW 7602 FUSELAGE PULLEY INTERCOSTAL HAS A CRACKED OUTBOARD FLANGE FS 484.00 LBL 36.0. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED AT FS 484.0 LBL 36.0 IAW REO 601R-53-41-059 REV A. 2L72 4F RTA21EA 20050317001132005031700113EA 2005 3 17 SWIA200514685 120050225A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07441SW 7602 FUSELAGE PULLEY INTERCOSTAL HAS A CRACKED OUTBOARD FLANGE AND A CRACKED ANGLE FS 484.00 RBL 27.0 - 36.0. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED AT FS 484.0 RBL 27.0 + 36.0 IAW REO 601R-53-41-059 REV A. 2L72 4F RTA21EA 20050317001152005031700115EA 2005 3 17 SWIA200514687 120050225A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07441SW 7602 AFT EQUIP BAY INTERCOSTAL CUP IS CRACKED; FS 625.00 STR 14R. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-61-100 REV NC AND CRJ REO 601R-53-61-422. 2L72 4F RTA21EA 20050317001162005031700116EA 2005 3 17 SWIA200514688 120050225A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA ENGINE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07441SW 7602 AFT EQUIP COMP ENGINE SUPPORT BEAM LOWER WEB IS CRACKED; LEFT SIDE FS 635.00 LBL 40.0. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-61-366 REV E. 2L72 4F RTA21EA 20050317001172005031700117EA 2005 3 17 SWIA200514689 120050225A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07441SW 7602 CARGO PIT FLOOR SUPPORT ANGLE CRACKED AT FS 621.00 RBL 42.0. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED DAMAGE TO FLOOR SUPPORT ANGLE, FS 621,IAW CRJ REO 601R-53-61-117 REV B. 2L72 4F RTA21EA 20050317001202005031700120NM 2005 3 17 SWAA050724 120050309A53106547979 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29607SW 27927 DURING SCHEDULED D-CHECK, FOUND CORROSION ON CREASE BEAM WEB BETWEEN BS 747 TO BS 767, LBL 70, WL 208. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM. 2L72 4F RTA16WE 20050317001222005031700122NM 2005 3 17 SWAA050726 120050309A53206558280 ANGLE BOEING737 7373H4 1384600NM FUELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29607SW 27927 DURING SCHEDULED D-CHECK, FOUND FUSELAGE ANGLE CRACKED AT BS 294, RBL 55, WL 208. REMOVED AND REPLACED ANGLE PER SRM. 2L72 4F RTA16WE 20050317001232005031700123NM 2005 3 17 SWAA050727 120050309A3350BR2013 LIGHT BOEING737 7373H4 1384600NM CABIN WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29640SW 27713 DURING SCHEDULED C4 CHECK, FOUND EEPLS STRIPS WORN ON RT SIDE AT ROW 1 AND ROW 16. REMOVED AND REPLACED EEPLS STRIPS PER MM. 2L72 4F RTA16WE 20050317001242005031700124NM 2005 3 17 SWAA050728 120050309A53306545775 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29685SW 23401 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 867, STR 24R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050317001272005031700127NM 2005 3 17 05FDEA00490 120050310A2432 RELAY DOUG MD11 MD11 3023602NM FAILED A FDEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO25591FE 48527 AT CRUISE (30 MIN INTO FLT) FL340 LEVEL ONE ALERT EMERGENCY POWER ON, ON ELECTRICAL SCHEMATIC INDICATIONS NORMAL. BATTERY VOLTAGE INITIALLY NORMAL THEN SLOWLY DECREASED TO 22V (41 INCREASING TO 67 AMP) BATTERY LOW ALERT THEN L EMERGENCY AC OFF SWITCHED EMERGENCY PWR OFF. RECOVERED MOST SYSTEMS FROM GEN PWR. RETURNED TO MEM. REMOVED AND REPLACED L/E BUSS SENSING RELAY R2-5156 AND PERFORMED ADJUSTMENT TEST IAW MD 11 AMM. ALL CHECKS NORMAL ON GROUND OK FOR SERVICE. 2L73 4F RTA22WE 20050317001282005031700128WP 2005 3 17 05FDEA00491 120050310A5330AJC7164503 PANEL DOUG DC10 DC1030F 3023504WP ZONE 100 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25311FE 46871 COMPLY WITH EA 8-5310-55460 MAIN FRAME-AFT BODY PLANK BLEND REPAIR FS 2051, L45L (P/N AJC7164-503). COMPLIED WITH EA 8-5310-55460 MAIN FRAME-AFT BODY PLANK BLEND REPAIR FS 2051, L45L (P/N AJC7164-503). 2L73 4F RTA22WE 20050317001302005031700130EU 2005 3 17 05FDEA00493 120050310A5320 FLOOR SUPPORT AIRBUS310 A310222 3930315EU FUSELAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25446FE 224 BULK PIT FLOOR SUPPORT AT FR67 FROM 12 INCHES TO LT CTR TO 36 INCHES TO LT OF CTR, 4EA AREAS OF CORROSION EXTENDING UNDER FASTENER HEADS AS MARKED. REMOVED AND REPLACED CROSS BEAM FLOOR SUPPORT IAW 51-72-10. REMOVED 4EA AREAS OF CORROSION IAW SRM 51-74-10. 2L72 4F RTA35EU 20050317001312005031700131NM 2005 3 17 05FDEA00494 120050311A7120AUB7510501 MOUNT DOUG MD11 MD11 3023602NM ZONE 400 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25592FE 48550 NR 3 PYLON FWD ENGINE MOUNT LT AFT HOLE CORRODED. REPAIRED AS PER FEDEX EA 1-5450-81617. 2L73 4F RTA22WE 20050317001392005031700139NM 2005 3 17 AWXA200500336 120050313A3397BR964411 LIGHT BOEING737 7373G7 1384595NM SEAT ROW 8 LT BROKEN A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28158AW 23780 PHX - EEL - FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 8 LT HANGS INTO THE AISLE AND HAS BROKEN WIRES. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050317001402005031700140NM 2005 3 17 SWAA050730 120050309A335065C27095 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29774SW 27882 DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050317001412005031700141EA 2005 3 17 SWIA200514661 120050301A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA LAVATORY MALFUNCTIONED A SWIAO OTHER N FALSE WARNING CLCLIMB 1 NM07903SW 7425 RECEIVED SMOKE TOILET MESSAGE DURING INITIAL CLIMBOUT. F/A VERIFIED NO SMOKE IN LAV. REMOVED AND REPLACED LAV SMOKE DETECTOR IAW CRJ AMM 26-16-01, OPERATIONAL CHECK GOOD. P/N OFF P90-421R3, S/N OFF 07589. 2L72 4F RTA21EA 20050317001422005031700142EA 2005 3 17 SWIA200514690 120050302A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07464SW 7602 CARGO PIT FLOOR SUPPORT ANGLE CRACKED AT FS 621 LBL 41. ITEM FOUND AT C-CHECK INSPECTION. FLOOR SUPPORT ANGLE REPAIRED IAW CRJ REO 601R-53-61-117 REV B. 2L72 4F RTA21EA 20050317001432005031700143NM 2005 3 17 SWAA050731 120050309A53206545409 WEB BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29686SW 23175 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE BEADED WEB CRACKED AT BS 664.5, BETWEEN LBL 30.5 TO LBL 32.0. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050317001442005031700144 2005 3 17 SWAA050732 420050309A256565C16820 HOOK BOEING737 7373H4 1384600NM GIRT BAR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29655WN 28400 DURING SCHEDULED 1/4D CHECK, FOUND BOTH R1 & L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOKS LOOSE. SECURED HOOKS PER MM. 2L72 4F RTA16WE 20050317001452005031700145NM 2005 3 17 SWAA050733 120050309A53306545766 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 450, STR 16R. REPAIRED SKIN PER SRM & SWA EA. 2L72 4F RTA16WE 20050317001462005031700146NM 2005 3 17 SWAA050734 120050309A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED C2 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS BETWEEN BS 927 TO BS 935, STR 21R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050317001472005031700147NM 2005 3 17 SWAA050735 120050309A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED C2 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS, BETWEEN BS 276 TO BS 282, STR 13L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050317001482005031700148NE 2005 3 17 SWIA200514662 220050305A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 1 LEAKING A SWIAO OTHER K FLUID LOSS NRNOT REPORTED 1 NM07936SW5259 5259 7726 873603 NR 1 ENGINE HAS OIL LEAKING, FOUND A SUMP DRAIN LEAKING BEYOND LIMITS. REMOVED AND REPLACED LEFT ENGINE ASSEMBLY IAW 71-00-00, OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20050317001542005031700154NM 2005 3 17 QXEA200500347 120050221A5414 SKIN DHAV DHC8 DHC8202 2809007NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09363PH 520 PDX - RIGHT NACELLE SKIN CRACKED FORWARD OUTBOARD CORNER OF WHEEL WELL APERTURE. REPAIRED IAW RD 8-54-72. 2H72 4T RTA13NM 20050317001582005031700158EA 2005 3 17 MASA200500163 120050227A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSBURNED OUT A MASAK NONE O OTHER ININSP/MAINT 1 SW07650ML 7137 DURING OVERNIGHT MAINTENANCE IN PHL, RT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE LIGHT BULB AND NO FURTHER DEFECTS WERE NOTED. 2L72 4F RTA21EA 20050317001592005031700159NM 2005 3 17 UPS05244037 120050105A5530 FORGING BOEING727 72725C 138400HNM VERTICAL STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 INSPECTION TYPE: SV, RIGHT VERTICAL FIN FRONT SPAR LWR FORGING. A 2 INCH VISIBLE CRACK IN FORGING STA 1229-1231. CRACK IN RADIUS AREA OF STRAP 1.75 X .25 INCH. REPAIRED LEFT AND RIGHT VERTICAL STAB FRONT SPAR FORGING FOR FERRY FLIGHT STA 1229 - 1231 IAW UPS EO B727-5530-21661-A, AND SAA SK 948-770. 2L73 4F A3WE 20050317001612005031700161NM 2005 3 17 DHL2005781545 120050215A5542 SKIN BOEING727 727227 1384078NM RUDDER CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A C-CHECK, VERT STAB FIN STA 204 RT SIDE UPPER RUDDER SKIN FWD HAS SURFACE CORROSION. REMOVED CORROSION FOUND TO BE BEYOND LIMITS, REMOVED EXISTING RIVETS, CUT OUT DAMAGED AREA DIM 3.5 X 2.25 INCH, FABRICATED REPAIR DOUBLER FROM 2024 T3 .032 PO 9001634 DIM 5.75 X 4.5 INCH AND FILLER FROM 2024 T3 .016 PO 9001660 DIM 3.5 X 2.25 INCH. TREATED, PRIMED AND INSTALLED REPAIR PARTS IAW B727 SRM 55-40-1, 51-30-2, 51-10-2 AND 55-20-3 FIG 1. 2L73 4F A3WE 20050317001622005031700162CE 2005 3 17 DXTA200500620 120050309A212157034EX BLOWER CESSNA500 560CESSNA 2076750CE CABIN FAILED E DXTAB EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07354QS 5600356 SMOKE FILLED THE CABIN. WHITE SMOKE WITH ACRID SMELL COMING FROM WEMAK VALVES. TROUBLESHOT SYSTEM TO BAD DEFOG BLOWER MOTOR. REMOVED & REPLACED DEFOG BLOWER MOTOR. OPS CHECK GOOD IAW 560 MM CH 21-21-01. 2L72 4F RTA22CE 20050317001642005031700164CE 2005 3 17 DXTA200500622 120050310A275099M5104 RESOLVER CESSNA750 750 2076810CE TE FLAPS FAULTY E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07979QS 7500079 FLAPS FAIL CAS MESSAGE APPEARED DURING FLAP EXTENSION, FLAPS REMAIN AT 0. SLATS EXTENDED PER CHECKLIST PUSHED FLAPS RESET BUTTON, DID NOT CLEAR CAS MESSAGE. HOOKED UP FLAP BRACKET BOX TO AIRCRAFT. MECHANICALLY RIGGED FLAPS. DURING ATTEMPT AT ELECTRICAL RIGGING OF FLAPS, FOUND DEAD SPOT IN RIGHT RESOLVER UNABLE TO CORRECTLY ADJUST RESOLVER TO READ CORRECT VOLTAGE. REMOVED RT RESOLVER. INSTALLED NEW RESOLVER AND MOUNT PLATE ON RT SIDE. VERIFIED MECHANICAL AND ELECTRICAL RIG AND OPS CHECKS SATISFACTORY. REF 750 MM CH 27-50-00. CLOSED ACCESS PANELS. 2L72 4J RTT00007WI 20050317001652005031700165EA 2005 3 17 COMA0560165 120050310A3350 ELEC CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT UNSECURE A COMAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01934CA 7042 FLIGHT 5787 MIDDLE TRACK EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE. RESECURED LOOSE CONNECTOR. 2L72 4F RTA21EA 20050317001662005031700166NM 2005 3 17 DHL2005781546 120050216A5753 FRAME BOEING727 727227 1384078NM TE FLAPS CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A C-CHECK, RIGHT O/B MID FLAP LWR INTERNAL FRAME CRACKED AT WS 520. REMOVED ANGLE SUPPORT INTERNAL FRAME IAW B727 SRM 51-30-2. REMOVED RIGHT O/B MIDFLAP O/B FLAP ACTUATING MECHANISM CABLE (AFA) TO FACILITATE S/M REPAIR PSC B727 M/M 27-51-71. REMOVED SEAL RETAINER & SEAL FOR ACCESS IAW B727 SRM 51-30-2 & M/M 20-30-11. REMOVED FITTING FOR ACCESS IAW B727 SRM 51-30-2. FABRICATED ANGLE SUPPORT P/N 60-4754 EXT 7075T6 .511 PO 501977 DIM 45.125 X 2 INCH IAW B727 SRM 57-50-2 FIG 6 AND 51-10-2 FIG 2. TREATED AND PRIMED IAW B727 SRM 51-10-2. LATE ENTRY ACCESS RIGHT O/B FLAP THRU AFT LOWR SKIN IAW B727 SRM 51-30-2. INSTALLED ANGLE SUPPORT IAW B727 SRM 57-10-2 FIG 1 AND 51-20-1 FIG 2. 2L73 4F A3WE 20050317001672005031700167NM 2005 3 17 05FDEA00489 120050310A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 BS 1148, STR 22 LT UPPER FRAME FLANGE IS CHAFED BY HYDRAULIC LINE. *S/D* REPAIRED EPR SRM 53-10-1, 51-40-3. 2L73 4F RTA3WE 20050317001682005031700168NM 2005 3 17 DHL2005781543 120050215A5330 SKIN BOEING727 727227 1384078NM FUSLEAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A C-CHECK, DENT AT SKIN OF AFT AIRSTAIR CUTOUT AFT OF STA 1323 BELOW STR 26R. REMOVED FASTENERS AND CUT OUT DAMAGED ARE DIM 2.875 X 1.375 INCH IAW B727 SRM 53-30-3 FIG 3. FABRICATED FILLER FROM 2024T3 .050 PO 9001873 DIM 2.875 X 1.375 INCH AND DOUBLER FROM 2024T3 .063 PO 9001634 DIM 10 X 5 INCH IAW B727 SRM 53-30-3 FIG 3. TREATED, PRIMED DOUBLER AND FILLER AREA IAW B727 SRM 51-10-2. INSTALLED DOUBLER AND FILLER ON AFT AIRSTAIR CUTOUT, SKIN STA 1323 STR 26R IAW B727 SRM 53-30-3 FIG 3. 2L73 4F A3WE 20050317001692005031700169EA 2005 3 17 COMA0560168 120050311A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSLAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01995CA 7229 LEFT HAND 640 FRAME CRACKED. REPAIRED IAW REO 601R-53-61-487 AND CRJ SRM 51-23-00, 51-25-06, 51-25-16, 51-42-06, 51-42-21, 51-41-02 AND 51-42-20. 2L72 4F RTA21EA 20050317001712005031700171EA 2005 3 17 COMA0570030 120050309A5320CC670341703 WEB CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01641CA3959 10122 THE LT AND RT LOWER WEBS BELOW THE FLOOR AT FS 280 ARE CORRODED FROM LBL 36 TO RBL 36. REMOVED THE CORRODED WEBS. FABRICATED AND INSTALLED NEW WEBS IAW BRAS EO 601R-53-6066 AND BOMBARDIER REO 670-53-11-052 REV A. 2L72 4F RTA21EA 20050317001722005031700172SO 2005 3 17 C2XA05SH016 120050222A5311MS20426AD44 FRAME EMB 145 EMB145LR 3260212SO CARGO BAY TOOL DAMAGE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713908 145465 SHV - DURING C-CHECK TOOLING MARK ON FRM 60 STR 5 L. MAINTENANCE REMOVE THE DAMAGE AREA AND PERFORMED REPAIRED IAW EMB145 SRM 53-00-04 SECTION 14 FIGURE 206. THE AIRCRAFT WAS APROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050317001732005031700173SO 2005 3 17 C2XA05BT014 120050308A212014525698403 CONTROL VALVE EMB 145 EMB145LR 3260212SO FUSELAGE FAULTY A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW2722909 145459 CREW REPORTED, STRONG SMELL OF ELECTRICAL WIRE BURNING, JUST AFTER LANDING. CLE MAINTENANCE TROUBLESHOT AIRCRAFT AND FOUND THE SMELL CAUSED BY THE COLD AIR DISTRIBUTION VALVE, MAINTENANCE RELEASED THE AIRCRAFT IAW MEL 21-24-03 CONTROL NUMBER 053226. AIRCRAFT RON IN BTV ON CO3353, MAINTENANCE REMOVED AND REPLACED THE COLD AIR DISTRIBUTION VALVE IAW EMB145 AMM 21-22-01. OPS CHECKED AND LEAK CHECKED GOOD IAW EMB145 AMM 21-20-00. MEL REMOVED AND AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20050317001772005031700177NM 2005 3 17 UPS05M44087 120050104A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 25 LT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED ON BARREL NUT HOLE NR 25 LT PER SRM 51-21-01.V2.R36, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 25 LT PER SRM 51-21-01.V2.R36. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 ON BARREL NUT HOLE NR 25 LT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED ON BARREL NUT HOLE NR 25 LT PER EN1133-05, FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20050317001792005031700179NM 2005 3 17 UPS05M44089 120050104A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 28 LT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED ON BARREL NUT HOLE NR 28 LT PER SRM 51-21-01.V2.R36, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 28 LT PER SRM 51-21-01.V2.R36. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 ON BARREL NUT HOLE NR 28 LT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED ON BARREL NUT HOLE NR 28 LT PER EN1136-05, FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20050317001802005031700180NM 2005 3 17 UPS05M44090 120050104A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 22 LT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED ON BARREL NUT HOLE NR 22 LT PER SRM 51-21-01.V2.R36, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 22 LT PER SRM 51-21-01.V2.R36. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I, APPLIED SEALANT PR1422B1/2 ON BARREL NUT HOLE NR 22 LT & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED ON BARREL NUT HOLE NR 22 LT PER EN1131-05 FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20050317001822005031700182NM 2005 3 17 QXEA200500324 120050218A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09363PH 520 PDX - RIGHTHAND OUTBOARD NR 11 SEAT TRACK HAS CORRODED LUGS AT X498. REPAIRED IAW DHC-8 200 SRM 51-40-00 AND 51-40-11. 2H72 4T RTA13NM 20050317001842005031700184NM 2005 3 17 QXEA200500327 120050218A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09363PH 520 PDX - RIGHTHAND OUTBOARD NR 11 SEAT TRACK HAS CORROSION ON TOP OF LUGS AT X434 TO X438 AND ON BOTTOM OF LUGS AT X436. REPAIRED IAW DHC-8 202 SRM 51-40-00 AND SRM 51-40-11. 2H72 4T RTA13NM 20050317001852005031700185NM 2005 3 17 QXEA200500328 120050218A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09363PH 520 PDX - RIGHTHAND OUTBOARD NR 11 SEAT TRACK HAS LITE CORROSION ON TOP OF OUTBOARD LUG AT X430. REPAIRED IAW DHC-8 200 SRM 51-40-00 AND SRM 51-40-11. 2H72 4T RTA13NM 20050317001862005031700186NM 2005 3 17 QXEA200500323 120050218A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09363PH 520 PDX - RIGHTHAND OUTBOARD NR 11 SEAT TRACK HAS DAMAGED LUGS AND CORRODED LUGS AT X486 TO X484 AND CORROSION ON BOTTOM OF LUGS AT X486. REPAIRED IAW RD 8-53-1343, DHC-8 200 SRM 51-40-00 AND 51-40-11. 2H72 4T RTA13NM 20050317001872005031700187NM 2005 3 17 QXEA200500359 120050301A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09413QX 4060 PDX - CORROSION ON RIGHTHAND OUTBOARD SEAT TRACK AT APPROXIMATELY X404.00, TOP AND INNER FLANGE. REPAIRED IAW RD 8/4-53/844 AND DHC-8 400 SRM 51-4215, 51-42-05. 2H72 4T RTA13NM 20050317001882005031700188NM 2005 3 17 QXEA200500325 120050218A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09363PH 520 PDX - RIGHTHAND OUTBOARD NR 11 SEAT TRACK HAS A LARGE SPOT OF CORROSION ON BOTTOM OF GROOVE AT X462 AND CORROSION ON LUGS FROM X466 TO X469. REPAIRED IAW DHC-8 200 SRM 51-40-00 AND SRM 51-40-11. 2H72 4T RTA13NM 20050317001892005031700189NE 2005 3 17 AT0500011 220050303A7261 LINE BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE NR 1 ENGINE LEAKING A ZZDAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO15906AT 55087 INFLIGHT ENGINE SHUTDOWN AFTER LOSS OF OIL PRESSURE. INSPECTED NR 1 ENGINE IAW AMM 72-00-00-200-805, TIGHTENED B-NUT ON OIL PUMP PRESSURE DISTRIBUTION LINE IAW AMM 79-20-00; OPS CHECK GOOD. RAN NR 1 ENGINE AT TAKEOFF POWER IAW AMM 71-00 TEST NR 2A, NO LEAKS NOTED. 2L72 4F4 FTRA6WE E00061EN 20050317001902005031700190NM 2005 3 17 QXEA200500360 120050223A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09413QX 4060 PDX - CORROSION ON RIGHTHAND OUTBOARD SEAT TRACK AT APPROXIMATELY X391.00, INNER AND TOP FLANGE. REPAIRED IAW DHC-8 400 SRM 51-42-15 AND 51-42-05. 2H72 4T RTA13NM 20050317001922005031700192NM 2005 3 17 QXEA200500330 120050217A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09363PH 520 PDX - SEAT TRACK NR 1 HAS PITTING CORROSION AT X395. REPAIRED IAW DHC-8 200 SRM 51-40-00 AND SRM 51-40-11. 2H72 4T RTA13NM 20050317001932005031700193NM 2005 3 17 QXEA200500332 120050217A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09363PH 520 PDX - SEAT TRACK NR 1 HAS PITTING CORROSION AT X364. REPAIRED IAW DHC-8 200 SRM 51-40-00 AND SRM 51-40-11. 2H72 4T RTA13NM 20050317001972005031700197NM 2005 3 17 05FDEA00487 120050310A5322 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25494FE 21532 SHEAR TIE AT BS 380 AT STR 16 NEEDS TO BE REPAIRED TO ACCOMPLISH 9G RIGID BARRIER MOD. *S/D* REPAIRED PER SRM 54-10-4. 2L73 4F RTA3WE 20050317001982005031700198NM 2005 3 17 DHL2005781541 120050215A5230 FRAME BOEING727 727227 1384078NM CARGO DOOR DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A C-CHECK, RIGHT FUSE AFT CARGO COMPT DOOR BOTH FWD & AFT LWR DOOR FRAME CORNER SECTIONS ARE FLAT SPOTTED & DENTED. REMOVED AND REPLACED AT RIGHT FUSE AFT CARGO COMPARTMENT DOOR BOTH FWD AND AFT LWR DOOR FRAME CORNER IAW 727 SRM 51-30-2 PO 501944, P/N 65-59948-502, PO 501943, P/N 65-59947-501. 2L73 4F A3WE 20050317002002005031700200NM 2005 3 17 QXEA200500311 120050223A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09413QX 4060 PDX - CORROSION ON RIGHTHAND OUTBOARD SEAT TRACK AT APPROXIMATELY X375.00, TOP AND INNER FLANGE. REPLACED SEAT TRACK IAW DHC-8 SRM 51-42-15 AND 51-42-05. 2H72 4T RTA13NM 20050317002022005031700202NM 2005 3 17 QXEA200500320 120050226A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09413QX 4060 PDX - RIGHTHAND INBOARD SEAT TRACK HAS PITTING CORROSION ON TOP OF TRACK AND INSIDE CHANNEL AT STATION X1.000. REPLACED SEAT TRACK IAW DHC-8 400 SRM 51-40-15 AND 51-42-00. 2H72 4T RTA13NM 20050317002032005031700203NM 2005 3 17 QXEA200500321 120050227A5410 BRACKET BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09413QX 4060 PDX - LEFTHAND NACELLE LOWER COWL, CHANNEL AND BRACKET ARE CRACKED ALONG OUTBOARD EDGE OF BYPASS DOOR. REPAIRED IAW DHC-8400 SRM 51-42-05. 2H72 4T RTA13NM 20050315002532005031500253NM 2005 3 15 AWXA200500313 120050122A53156545815108 FLOORBEAM BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOORBEAM UPPER CHORD AT BS 344, BETWEEN RBL 12 AND LBL 50. MAINTENANCE REMOVED CORRODED SECTION OF FLOORBEAM UPPER CHORD AT BS 344, FROM RBL 12 TO LBL 50; FABRICATED A NEW REPLACEMENT SECTION OF UPPER CHORD, 2 EACH REPAIR ANGLES, A STIFFENER, AND SHIMS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-51 FIG 205. 2L72 4F RTA16WE 20050315002702005031500270NM 2005 3 15 AWXA200500322 120050219A5340693535214 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28307AW 24634 MCN - MAJOR REPAIR - DURING C-14 CHECK A .25 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT BS 616, STR 6 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 616, STR 6 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-35352; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 12. 2L72 4F RTA16WE 20050315002732005031500273NM 2005 3 15 USAA050285 120050217A5754 SKIN BOEING737 7373B7 1384580NM NR 6 SLAT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19519AU50516 23705 CLT - FOUND SLAT SKIN CRACKED .025 INCH, NR 6 SLAT LOWER L/E. INSTALLED DOUBLER. (M) 2L72 4F RTA16WE 20050315002892005031500289NM 2005 3 15 USAA050287 120050217A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU50516 23702 CLT - FOUND EXT FUSELAGE SKIN CRACKED .5 INCH, FORWARD SERVICE DOOR LOWER HINGE CUTOUT. INSTALLED DOUBLER IAW TR 52-10-13. (M) 2L72 4F RTA16WE 20050315002922005031500292NM 2005 3 15 USAA050294 120050217A5210507945264 BEAM BOEING737 7374B7 1384702NM ENTRY DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19438US40959 24560 PIT - FOUND FORWARD ENTRY DOOR CRACKED .5 INCH, STOP CUTOUT AFT END NR 6 BEAM AFT LIP ON PAN. REMOVED DAMAGE, INSTALLED DOUBLER PER TYPICAL REPAIR 52-10-16. (M) 2L72 4F RTA16WE 20050315003032005031500303EA 2005 3 15 A6WA200540076 120050222A3213 STRUT CNDAIRCL600 CL6002B19 1900309EA NLG DISCHARGED A A6WAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 GL31431AW 7256 AFTER TAKEOFF, THE NOSE GEAR DID NOT RETRACT. SERVICED HYDRAULIC FLUID AND NITORGEN TO THE NOSE STRUT. ADJUSTED THE NOSE OLEO CENTER EXTEND SENSOR WITHIN LIMITS. (M) 2L72 4F RTA21EA 20050315003102005031500310NE 2005 3 15 2005F00051 220050126A73103035681 FILTER AEROSPATR72 ATR72212A 8680902EU PWA PW120 PW127 NE FUEL PUMP CLOGGED A TRBAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO21494AE 494 AV0020 DURING TAKEOFF, RIGHT ENGINE FUEL CLOG INDICATION CAME ON. ABORTED TAKEOFF. REMOVED AND REPLACED FUEL PUMP OUTLET FILTER. (M) 2H72 4T4 TRTA53EU E20NE 20050315003112005031500311SO 2005 3 15 C2XA05IA034 120050302A21214611028900 GASPER FAN EMB 145 EMB145XR 3260214SO CABIN MALFUNCTIONED A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 SW27141484096 4096 145751 CLE - FLIGHT 3238, THE CREW REPORTED THAT THE GASPER VENTS WERE NOT WORKING, AND AFTER RESETTING THE GASPER FAN CIRCUIT BREAKER A STRONG BURNING ODOR WAS PRESENT. MAINTENANCE MEL'D THE GASPER FAN UNDER MEL 21-23-03 CONTROL NUMBER 053036, AND THE AIRCRAFT WAS RETURNED TO SERVICE. THE AIRCRAFT RON'D AT MCI OFF OF FLIGHT 2608, WHERE MAINTENANCE REMOVED AND REPLACED THE GASPER RECIRCULATING FAN, OPERATIONALLY CHECKED WITH NO DEFECTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20050315003142005031500314WP 2005 3 15 GTIA050023 120050112A5347 SEAT TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FOUND CABIN SEAT TRACKS LEFT OUTBOARD STATION 200-484750, STATION 1022-1307 NUMEROUS AREAS HAVE GOUGES AND CORROSION OUT OF LIMITS. REMOVED CORROSION, BLENDED GOUGES AND REPLACED OUT OF LIMIT SEAT TRACKS, PRIMED AND TREATED SEAT TRACKS. (M) 2L72 4F A6WE 20050315003202005031500320NM 2005 3 15 SWAA050702 120050307A53116546550 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29607SW 27927 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050315003222005031500322WP 2005 3 15 GTIA050021 120050208A215020495055 ACM DOUG DC9 DC981 3022081WP RIGHT ODOR A GTIAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL23818NK7076 48018 SMOKE DETECTOR IN RIGHT AFT LAV WENT OFF ON TAKEOFF ACCOMPANIED BY A SMELL OF SMOKE, AIR RETURN TO FLL. REMOVED AND REPLACED RIGHT ACM AND BURN OUT OF PNEUMATIC DUCTS. REMOVED AND REPLACED BOTH, REMOVED AND REPLACED BOTH COALESCER BAGS AND LEAK CHECKED. HI POWER RUN, NO SMOKE OR SMELL IN CABIN, OPS CHECK OF SMOKE DETECTOR OK. (M) 2L72 4F A6WE 20050315003272005031500327WP 2005 3 15 GTIA050019 120050128A3213 STRUT DOUG DC9 DC983 3022083WP NLG LEAKING A GTIAO OTHER O OTHER TXTAXI/GRND HDL 1 GL23815NK 49415 FLL - FLT 395 - FOUND NOSE GEAR BOTTOMS OUT DURING TAXI, AIRCRAFT TAIL SWAP. REMOVED AND REPLACED VALVE BODY AND O-RING, SERVICED STRUT, LEAK CHECK OK. (M) 2L72 4F RTA6WE 20050315003392005031500339NM 2005 3 15 SWAA050693 120050307A57536546435 FLAP BOEING737 7373Q8 1384670NM LT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29317WN 24068 DURING SCHEDULED C4 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2L72 4F RTA16WE 20050315003502005031500350NM 2005 3 15 XN0A1230 120050301A3150 WARNING SYSTEM BOEING727 727227 1384078NM COCKPIT MALFUNCTIONED A XN0AC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL2379754 21363 TAKEOFF WARNING HORN STEADY INSTEAD OF INTEMITTENT. CLEANED AND RESET, CONNECTOR, WARNING BOX OPS CHECK GOOD AT THIS TIME IAW 727-3100. 2L73 4F A3WE 20050315003582005031500358EA 2005 3 15 050616395 120050302A5320601R3111358 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27639BR 7313 RIGHT 280 VERTICAL ANGLE IS CRACKED AT .5 INCH BETWEEN FASTENERS. 2L72 4F RTA21EA 20050315003592005031500359EA 2005 3 15 05062654 120050303A3222 PISTON CNDAIRCL600 CL6002B19 1900309EA NLG STRUT NOT SEATED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27654BR 7454 EVENT SUMMARY NOSE GEAR DOOR DISAGREE. FOUND NLG STRUT PISTON TO NOT BE FULLY SEATED. SEATED PISTON & SERVICED NLG. PERFORMED GEAR SWINGS WITH NO DEFECTS NOTED. 2L72 4F RTA21EA 20050315003602005031500360 2005 3 15 2005UALA00100 420050128A25655A29011 ASPIRATOR BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE SLIDE/RAFT LEAKING A UALAK NONE O OTHER ININSP/MAINT 1 WP29670UA 29240 LEAKING ASPIRATOR. REPLACED ASPIRATOR. 2L72 4F4 FRTA1NM E24NE 20050315003612005031500361NM 2005 3 15 2005UALA00211 120050304A5310 SHEAR TIE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29582UA 26702 AFT PIT STA 1620, RBL 2 SHEAR TIE HAS CORROSION. REPLACEMENT SHEAR TIE WAS FABRICATED AND INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050315003622005031500362NM 2005 3 15 2005UALA00212 120050306A3397 WIRE BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT FAILED A UALAK NONE O OTHER ININSP/MAINT 1 WP29187UA 26876 EMERGENCY EXIT LIGHTS WILL NOT GO OUT. THE MED 5R SLIDE LIGHT CONDUIT ASSY WAS DAMAGED WHERE CONTACT IS MADE AT THE DOOR CUTOUT. REPLACED WIRE ASSY AND INNER AND OUTER CONDUITS. 2L74 4F4 FRTA20WE E24NE 20050315003632005031500363NM 2005 3 15 2005UALA00213 120050307A5311 FRAME BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29117UA 28810 AFT PIT STA 1580, RBL 36 FRAME CAP DENTED. FRAME DENTED BY CARGO LOADING OPERATIONS. FAA-APPROVED PERMANENT REPAIR APPLIED TO FRAME INNER FLANGE. 2L74 4F4 FRTA20WE E24NE 20050315003672005031500367NE 2005 3 15 2005F00054 220050216A7200 ENGINE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE LEFT STOPPED A GUUAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO1781538 UE199 PCEPS0057 FLT 9133 - JAX - DURING TAKEOFF ROLL, WITH LEFT ENGINE AT APPROXIMATELY 1,000 LBS OF TORQUE, UNUSUAL NOISE HEARD. LEFT ENGINE CEASED. ABORTED TAKEOFF. DETERMINED LEFT POWER SECTION SEIZED. REMOVED AND REPLACED LEFT ENGINE ASSEMBLY AND ROUTED FAILED UNIT FOR FURTHER ANALYSIS AND REPAIR. OPERATIONAL CHECK NORMAL. (M) 2L72 4T4 TRTA24CE E26NE 20050316000042005031600004NM 2005 3 16 DL757050143 120050228A3411 PITOT TUBE BOEING757 757232 1384965NM UNRELIABLE A DALAA UNSCHED LANDING G MULTIPLE FAILURE CLCLIMB 1 SO27640DL 23994 ON CLIMBOUT FROM JFK IN ICING CONDITIONS LOST BOTH CAPT AND F/O AIRSPEED INDICATORS, AIRSPEED COMMAND BUGS WERE UNRELIABLE, AND LOST ALL ENGINE POWER SETTINGS INSTRUMENTS EPR N1, N2. EMERGENCY DECLARED. ONCE VFR EVERYTHING CAME BACK EXCEPT FOR EPR INDICATIONS. THOROUGHLY TESTED PITOT-STATIC SYSTEM - NTF. 2L72 4F RTA2NM 20050316000112005031600011NM 2005 3 16 DL76K050150 120050304A5753113T227143 HINGE BOEING767 767332 1382001NM TE FLAP FRACTURED A DALAK NONE O OTHER ININSP/MAINT 1 SO27176DZ NONE 29697 ON WALKAROUND FOUND LEFT INBOARD FLAP NOT FAIRED WITH WING. FOUND LEFT INBOARD FLAP HINGE ASSEMBLY BROKEN. REPLACED HINGE ASSEMBLY AND CARRIAGE RODS PER MM. 2L72 4F RTA1NM 20050316000192005031600019NM 2005 3 16 DL76S050159 120050313A2121732591A FAN BOEING767 767332 1382001NM EQUIP EXHAUST OVERHEATED A DALAO OTHER MB OVER TEMP SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27132DN 24981 EICAS MESSAGE FWD EQUIP EXHAUST FAN DISPLAYED. FWD EQUIP EXHAUST ELEC SMELL, SLIGHT SMOKE ODOR DETECTED. ATL MTC REPLACED FWD EQUIP EXHAUST FAN. EQUIP COOLING CHECKS NORMAL. 2L72 4F RTA1NM 20050316000212005031600021NM 2005 3 16 2005UALA00218 120050307A5347111U5107 SEAT TRACK BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29117UA 28810 CABIN SEAT TRACK AT RBL 33.39, STA 1168-1222 FOUND TO BE OUT OF LIMIT AFTER DAMAGE REMOVAL. *S/D* MAJOR REPAIR ACCOMPLISHED. SEAT TRACK SECTION REPLACED. 2L74 4F4 FRTA20WE E24NE 20050316000412005031600041NM 2005 3 16 2005UALA00232 120050310A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP29582UA 26702 STA 620 BETWEEN STR 16L AND 17L HAS HOLE DAMAGE. HOLE DAMAGE CAUSED DURING INSTALLATION OF AN EXTERNAL FUSELAGE SKIN REPAIR. SHEAR TIE WAS REMOVED, A REPLACEMENT SHEAR TIE WAS FABRICATED AND INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050316000502005031600050WP 2005 3 16 UPS05844109 120050311A5330 SKIN DOUG DC8 DC873F 302199FWP LONG CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01811UP 46089 INSPECTION TYPE: C2 TEMP RIVET HEAD CENTER PIN MISSING, FASTENER HEAD LOW & SKIN BULGING AT APPROX STA 380 L/S BELOW L2 DOOR. UPON FURTHER INVESTIGATION FOUND CORROSION ON BACK SIDE OF SKIN AT STA 380 LONG 29L. REPAIRED IAW SRM 53-2-1 FIG 7. 2L74 4F RT4A25 20050316000752005031600075WP 2005 3 16 0500319613 120050308A7500 BLEED AIR SYS DOUG DC9 DC932 3022066WP PWA JT8 JT8D9A 52048NE NR 1 ENGINE CONTAMINATED A NWAAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 GL01613NW 47438 666706 DURING ROTATION, SMOKE ENTERED THE COCKPIT AND CABIN. FLIGHT CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE AIRPORT PERFORMING AN UNEVENTFUL LANDING. MAINTENANCE FOUND OIL IN NR 1 ENGINE 8TH STAGE BLEED. REPLACED THE NR 1 ENGINE. OPERATIONAL CHECK GOOD. 2L72 4F4 F A6WE E2EA 20050316000902005031600090NM 2005 3 16 SWAA050721 120050309A323365448205 ACTUATOR BOEING737 7373Q8 1384670NM RT MLG MALFUNCTIONED A SWAAO OTHER J WARNING INDICATION CLCLIMB 1 SW29687SW 23388 RT MLG DID NOT INITIALLY RETRACT ON DEPARTURE. CYCLED GEAR LEVER BACK TO UP, GEAR RETRACTED. OPERATED MLG & COULD NOT DUPLICATE PROBLEM. AS A PRECAUTION, REMOVED AND REPLACED RT MLG DOWNLOCK ACTUATOR PER MM. 2L72 4F RTA16WE 20050316000922005031600092EU 2005 3 16 05FDEA00403 120050307A5730 PANEL AIRBUS310 A310222 3930315EU LT WING DAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25446FE 224 LEFT WING PANEL 550PB HAS 2 EA ELONGATED HOLES (LANDING). REPAIRED PANEL 550PB LANDING IAW TD/JI/SI/00339/2005 AS PER FEDEX EA 6-5710-86051. 2L72 4F RTA35EU 20050316000942005031600094EU 2005 3 16 05FDEA00405 120050307A5322 SHEAR TIE AIRBUS310 A310222 3930315EU FUSELAGE DAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25446FE 224 BULKPIT UNDER FLOOR FR64 FWD 8 INCHES TO AFT 14 INCHES EXTENDING 1 INCH INBOARD AND OUTBOARD OF STG 47R AND EXTENDING UNDER SHEAR TIE AND FRAME. REMOVED CORROSION IAW A310-200 SRM 51-74-10. AREA WAS OUT OF LIMITS IAW A310-200 SRM 53-10-00. REMOVED AND REPLACED DAMAGED AREA IAW A310-200 SRM 53-10-14. TREATED, PRIMED AND TOPCOATED IAW A310-200 SRM 51-21-10. SEALED AREA IAW A310-200 SRM 51-76-00. 2L72 4F RTA35EU 20050317000092005031700009 2005 3 17 UPS05544127 420050315A2561 LIFE VEST BOEING757 75724APF 1384969NM COCKPIT CONTAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01456UP 25477 DEMO LIFE VEST CONTAMINATED WITH LAV WATER. REMOVED AND REPLACED DEMO LIFE VEST. 2L72 4F RTA2NM 20050317000132005031700013EA 2005 3 17 SWIA200514682 120050225A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07441SW 7602 MAIN FUSELAGE FS 280 LBL 9.0 LOWER FLANGE CRACKED ON TRANSVERSE BEAM. ITEM FOUND AT C-CHECK INSPECTION. CRACKED FLANGE REPAIRED IAW CRJ REO 601R-53-11-171 REV A. 2L72 4F RTA21EA 20050317000262005031700026NM 2005 3 17 SWAA050776 120050314A5531BAC1506188 BEAM BOEING737 7373H4 1384600NM VERTICAL STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29605SW 27956 DURING SCHEDULED D-CHECK, FOUND RT VERTICAL FIN T/E BEAM CRACKED 4 BELOW NR 1 RUDDER HINGE. REMOVED AND REPLACED BEAM SECTION PER SRM. 2L72 4F RTA16WE 20050317000582005031700058SO 2005 3 17 MASA200500191 120050307A3350 SIGN EMB 145 EMB145LR 3260212SO EMERGENCY EXIT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07852MJ 145567 ASH 2780 CLT, CEILING EMERGENCY EXIT SIGN FWD HALF LIGHTS INOP. MAINTENANCE RESECURED THE LIGHT ASSEMBLY AND OPS CHECKED THE SYSTEM. 2L72 4T RTT00011AT 20050317000752005031700075NM 2005 3 17 2005UALA00195 120050217A5330141W330911 SKIN BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE FUSELAGE TORN A UALAK NONE O OTHER ININSP/MAINT 1 WP29793UA33223 26946 LT SIDE FUSELAGE DAMAGED. MAJOR REPAIR ACCOMPLISHED. DAMAGE TO FUSELAGE SKIN AND STRINGER AT APPROXIMATELY BS 645, STR 29L - 30L FOLLOWING CONTACT WITH AIRSTAIR CASE. MAJOR REPAIR ACCOMPLISHED ON EVA ORD-6140 -A- AND ORD-6142. 2L72 4F4 FRTT0001SE E46NE 20050317000772005031700077NM 2005 3 17 2005UALA00200 120050301A5330 BEAR STRAP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29303UA 23644 AFT CARGO DOOR AFT LOWER CORNER BEAR STRAP DAMAGED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND TRIPLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20050317000782005031700078NM 2005 3 17 2005UALA00201 120050227A3350 BATTERY PACK BOEING757 757222 1384956NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29572UA 26682 EMERGENCY LIGHT ON EXTERIOR OF AFT CARGO DOOR, EMERGENCY AISLE LIGHT AT ROW 25, AND MID AISLE EXIT SIGN LIGHT INOP. REPLACED BATTERY PACK FOR POWER SUPPLY. 2L72 4F4 FRTA2NM E17NE 20050317000802005031700080EA 2005 3 17 MASA200500164 120050301A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSBURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0727191 7191 ASH 2742 IN PHL REPORTED A PAX DOOR EMERGENCY EXIT LIGHT INOP. THE LIGHT WAS MEL'ED 3/2 MX REPLACED THE LIGHT BULB. 2L72 4F RTA21EA 20050317000812005031700081EA 2005 3 17 MASA200500169 120050302A3350 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCONNECTED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07652ML 7036 ASH 2621 PHL TO STL - EMERGENCY FLOOR TRACK LIGHTING FIRST BAR NOT ILLUMINATING. MAINTENANCE RECONNECTED THE CONNECTOR, OPS GOOD. 2L72 4F RTA21EA 20050317000862005031700086WP 2005 3 17 ABXA050069 120050308A531359177079 LONGERON DOUG DC9 DC931 3022065WP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23945AX 47551 LONGERON 30 AT STA 945 WAS CORRODED BEYOND LIMITS. REPLACED LONGERON IAW DC-9 SRM 51-30-5 AND 51-30-2. 2L72 4F A6WE 20050317000942005031700094SO 2005 3 17 CHQA200500048 120050304A3350100865 BATTERY PACK EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT FAULTY A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11571RP 14500827 UPON ENTERING THE AIRCRAFT AT THE GATE, THE EMERGENCY LIGHTS WERE ON. THE MAIN AND EMERGENCY BATTERY SWITCHES WERE IN THE OFF POSITION. REMOVED AND REPLACED ALL FOUR EMERGENCY BATTERIES IAW AMM 33-50-04. OPS CHECK GOOD IAW EMB 145 AMM 33-50-04. SERIAL NUMBERS REMOVED C02029, C02042, C01805, C01802. 2L72 4T RTT00011AT 20050317000962005031700096NM 2005 3 17 2005UALA00209 120050303A5322 SHEAR TIE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29582UA 26702 PIT SHEAR TIE HAS CORROSION, STA 1600, LBL 9. REPLACEMENT SHEAR TIE WAS FABRICATED AND INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050317000982005031700098NM 2005 3 17 SWAA050712 120050308A52406545871 FRAME BOEING737 7373H4 1384600NM R1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED C2 CHECK, FOUND R1 DOOR LOWER FRAME CRACKED AT AFT DOOR STOP FITTING CUTOUT. REMOVED AND REPLACED DOOR PER MM. 2L72 4F RTA16WE 20050317001142005031700114EA 2005 3 17 SWIA200514686 120050225A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07441SW 7602 AFT EQUIP BAY INTERCOSTAL CUP IS CRACKED; FS 625.00 STR 14L. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-61-100 REV NC AND CRJ REO 601R-53-61-422. 2L72 4F RTA21EA 20050317001182005031700118NM 2005 3 17 CALA0500076 120050311A5330654577572 SKIN BOEING737 7373T0 1384582NM FUSLEAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716301 23352 INSPECTION FOUND A 1.7 INCH CRACK IN FUSELAGE SKIN THREE INCHES AFT OF STA 727D JUST BELOW S23R ON BONDED DOUBLER LINE. THE CRACKED AREA WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5331-01178. 2L72 4F RTA16WE 20050317001252005031700125NM 2005 3 17 SWAA050729 120050309A335065C27095 BATTERY BOEING737 7377H4 1384404NM L1 DOOR INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29461WN 32465 DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EXTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050317001382005031700138EA 2005 3 17 COMA0560175 120050312A21331037708 OUTFLOW VALVE CNDAIRCL600 CL6002B19 1900309EA CABIN PRESSURE MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01815CA12824 7397 FLIGHT 5152 AIRCRAFT FAILED TO PRESSURIZE DURING CLIMBOUT OF CVG, AIRCRAFT RETURNED TO THE FIELD. REPLACED THE PRIMARY OUTFLOW VALVE. 2L72 4F RTA21EA 20050317001492005031700149 2005 3 17 SWIA200514663 420050304A3418C12851AA03 COMPUTER CNDAIRCL600 CL6002C10 1390015EA STALL WARNING MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07706SK 10149 STALL FAIL CAUTION MESSAGE. REPLACED STALL PROTECTION SYSTEM COMPUTER AND PERFORMED OPERATIONAL CHECKS, OPS CHECKED GOOD. 2L72 4F RTA21EA 20050317001512005031700151EA 2005 3 17 SWIA200514665 120050305A5240 HANDLE CNDAIRCL600 CL6002B19 1900309EA SERVICE DOOR INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07449SW 7699 GALLEY/SERVICE DOOR OUTER HANDLE DOES NOT OPEN FROM OUTSIDE. REMOVED AND REPLACED SERVICE DOOR OUTER HANDLE IAW 52-41-00 MM P/N 601R38305-5, S/N OFF 0785. 2L72 4F RTA21EA 20050317001942005031700194NM 2005 3 17 QXEA200500333 120050217A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09363PH 520 PDX - SEAT TRACK NR 1 HAS PITTING CORROSION AT X352. REPAIRED IAW DHC-8 202 SRM 51-0-00 AND SRM 51-40-11. 2H72 4T RTA13NM 20050317002042005031700204NM 2005 3 17 QXEA200500302 120050223A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09413QX 4060 PDX - CORROSION ON RIGHTHAND OUTBOARD SEAT TRACK AT APPROXIMATELY X556.00 TOP AND INNER FLANGE. REPLACED IAW DHC08 SRM 51-42-15 AND 51-42-05. 2H72 4T RTA13NM 20050317002062005031700206NM 2005 3 17 QXEA200500304 120050223A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09413QX 4060 PDX - CORROSION ON RIGHTHAND OUTBOARD SEAT TRACK AT APPROXIMATELY X523.00, TOP AND INNER FLANGE. REPLACED SEAT TRACK IAW DHC-8 SRM 51-42-15 AND 51-42-05. 2H72 4T RTA13NM 20050317002082005031700208NM 2005 3 17 QXEA200500331 120050217A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09363PH 520 PDX - SEAT TRACK NR 1 HAS SCRATCH FROM X395 TO X408. REPAIRED IAW DHC-8 200 SRM 51-40-00 AND SRM 51-40-11. 2H72 4T RTA13NM 20050317002092005031700209NM 2005 3 17 QXEA200500335 120050217A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09363PJ 520 PDX - SEAT TRACK NR 1 HAS PITTING CORROSION AT STATION X328. REPAIRED IAW DHC-8 202 SRM 51-40-00 AND SRM 51-40-11. 2H72 4T RTA13NM 20050317002112005031700211NM 2005 3 17 QXEA200500337 120050217A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09363PH 520 PDX - SEAT TRACK NR 1 HAS PITTING CORROSION AT STATION X281. REPAIRED IAW DHC-8 202 SRM 51-40-00 AND SRM 51-40-11. 2H72 4T RTA13NM 20050317002122005031700212NM 2005 3 17 QXEA200500336 120050217A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09363PH 520 PDX - SEAT TRACK NR 1 HAS PITTING CORROSION AT STATION X313. REPAIRED IAW DHC-8 202 SRM 51-40-00 AND SRM 51-40-11. 2H72 4T RTA13NM 20050317002132005031700213NM 2005 3 17 QXEA200500338 120050217A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09363PH 520 PDX - SEAT TRACK NR 1 HAS PITTING CORROSION AT STATION X279. REPAIRED IAW DHC-8 202 SRM 51-40-00 AND SRM 51-40-11. 2H72 4T RTA13NM 20050317002152005031700215NM 2005 3 17 QXEA200500357 120050301A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09413QX 4060 PDX - TOP OF LEFT INBOARD SEAT TRACK CORRODED AT X36, X28, X10, X0.0, X5.0, X9.0, X17, X20 AND X25. REPAIRED IAW DHC-8 400 SRM 51-41-00, 51-42-00, 51-42-05 AND 51-40-15. 2H72 4T RTA13NM 20050317002172005031700217NM 2005 3 17 QXEA200500339 120050218A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09363PH 520 PDX - RIGHTHAND OUTBOARD SEAT TRACK NR 10 HAS SURFACE CORROSION ON TOP OF LUGS AND PITTING IN BOTTOM OF GROOVE AT X264 TO X267. REPAIRED IAW DHC-8 202 SRM 51-40-00 AMD SRM 51-40-11. 2H72 4T RTA13NM 20050317002192005031700219NM 2005 3 17 QXEA200500340 120050217A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09363PH 520 PDX - RIGHTHAND OUTBOARD NR 10 SEAT TRACK HAS PITTING IN BOTTOM OF CHANNEL AND SURFACE CORROSION ON TOP OF LUGS AT X278 TO X281. REPAIRED IAW DHC-8 202 SRM 51-40-00 AND SRM 51-40-11. 2H72 4T RTA13NM 20050317002202005031700220NM 2005 3 17 QXEA200500341 120050217A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09363PH 520 PDX - RIGHTHAND OUTBOARD NR 10 SEAT TRACK HAS SURFACE CORROSION ON TOP OF AND ON FACE OF LUGS, AND PITTING IN BOTTOM OF CHANNEL AT X296 TO X298. REPAIRED IAW DHC-8 202 SRM 51-40-00 AND SRM 51-40-11. 2H72 4T RTA13NM 20050317002212005031700221NM 2005 3 17 DHL2005781544 120050214A5753 SKIN BOEING727 727227 1384078NM TE FLAP DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A C-CHECK, RT WING I/B MID FLAP O/B END, TRAILING EDGE IS DELAMINATED WBL 2400. REMOVED RT WING I/B MID FLAP O/B FAIRING. CUT OUT DELAM UPPER SURFACE SKIN AREA AFT APPROX 8 X 4.25 INCH. FABRICATED ONE SKIN REPLACEMENT APPROX 8 X 4.25 INCH & ONE SPLICE PLATE APPROX 4.25 X 3 INCH USING 2024-T3 .016 PO 9001660 IAW B727 SRM 57-50-2 FIG 3. CLEARED PREPPED APPLIED ADHESIVE PRIMED AND ADHESIVE TO ALL REPAIR SURFACES & BAGGED FOR BONDING IAW B727 SRM 51-40-20 FIG 30. CURED REPAIR CLEANED PREPPED & PERFORMED POST BOND INSP WITH NO DELAM NOTED IAW B727 SRM 51-40-20 PARA 0. TREATED, PRIMED & SEALED REPAIR IAW B727 SRM 51-40-20 PARA P. RE-INSTALLED RIGHT I/B MID FLAP O/B FAIRING IAW B727 SRM 51-30-2. 2L73 4F A3WE 20050317002222005031700222EA 2005 3 17 COMA0560167 120050311A5312 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DAMAGED A COMAK NONE O OTHER ININSP/MAINT 1 SO01995CA 7229 LEFT AFT ANGLE ON FS 280.00. REPAIRED IAW REO 601R-53-11-136 AND EO 10-5310-00587. 2L72 4F RTA21EA 20050317002262005031700226NM 2005 3 17 UPS05M44095 120050105A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 32 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED & REWORKED ON BARREL NUT HOLE NR 32 RT PER SRM 51-21-01.V2.R36, FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 ON BARREL NUT HOLE NR 32 RT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED ON BARREL NUT HOLE NR 32 RT PER EN1169-05, FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20050317002272005031700227NM 2005 3 17 UPS05M44098 120050109A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 10 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED & REWORKED ON BARREL NUT HOLE NR 10 RT PER SRM 51-21-01.V2.R36. FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 ON BARREL NUT HOLE NR 10 RT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED PER EN1150-05 ON BARREL NUT HOLE NR 10 RT FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20050317002282005031700228NM 2005 3 17 UPS05M44099 120050109A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 14 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED & REWORKED ON BARREL NUT HOLE NR 14 RT PER SRM 51-21-01.V2.R36, FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 ON BARREL NUT HOLE NR 14 RT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED ON BARREL NUT HOLE NR 14 RT PER EN1145-05, FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20050317002292005031700229NM 2005 3 17 UPS05M44100 120050105A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 13 LT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED & REWORKED ON BARREL NUT HOLE NR 13 LT PER SRM 51-21-01.V2.R36, FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 ON BARREL NUT HOLE NR 13 LT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED ON BARREL NUT HOLE NR 13 LT PER EN1124-05 & EO MD11-5510-19409-I, FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20050317002302005031700230NM 2005 3 17 UPS05M44101 120050109A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 7 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED & REWORKED ON BARREL NUT HOLE NR 7 RT PER SRM 51-21-01.V2.R36 FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 ON BARREL NUT HOLE NR 7 RT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED ON BARREL NUT HOLE NR 7 RT PER EN1148-05 & EO MD11-5510-19409-I, FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20050317002322005031700232NM 2005 3 17 QXEA200500318 120050223A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09413QX 4060 PDX - CORROSION ON RIGHTHAND OUTBOARD SEAT TRACK AT APPROXIMATELY X243.00, TOP AND INNER FLANGE. REPLACED SEAT TRACK IAW DHC-8 SRM 51-42-15 AND 51-42-05. 2H72 4T RTA13NM 20050317002362005031700236NM 2005 3 17 QXEA200500316 120050223A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09413QX 4060 PDX - CORROSION ON RIGHTHAND OUTBOARD SEAT TRACK AT APPROXIMATELY X292.00, TOP AND INNER FLANGE. REPLACED SEAT TRACK IAW DHC-8 SRM 51-42-15 AND SRM 51-42-05. 2H72 4T RTA13NM 20050317002372005031700237NM 2005 3 17 QXEA200500342 120050217A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09363PH 520 PDX - RIGHTHAND OUTBOARD NR 10 SEAT TRACK HAS PITTING IN BOTTOM OF CHANNEL AND BELOW LUGS FROM X308 TO X312 AND ON TOP OF LUGS FROM X308 TO X312. REPAIRED IAW DHC-8 292 SRM 51-40-00 AND SRM 51-40-11. 2H72 4T RTA13NM 20050317002382005031700238NM 2005 3 17 UPS05M44102 120050113A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 28 RT BARREL NUT HOLE FOUND WITH CORROSION ON WALL, BASE & BEARING SURFACE. CORROSION REMOVED & REWORKED ON BARREL NUT HOLE NR 28 RT PER SRM 51-21-01.V2.R.36 FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 ON BARREL NUT HOLE NR 28 RT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED ON BARREL NUT HOLE NR 28 RT PER EN1165-05 & EO MD11-5510-19409-I, FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20050317002402005031700240NM 2005 3 17 QXEA200500344 120050217A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09363PH 520 PDX - RIGHTHAND OUTBOARD NR 10 SEAT TRACK HAS SURFACE CORROSION ON TOP OF LUGS AT X361 AND FROM X373 TO X375, PITTING IN BOTTOM OF CHANNEL AT X372 TO X375. REPAIRED IAW DHC-8 202 SRM 51-40-00 AND SRM 51-40-11. 2H72 4T RTA13NM 20050317002412005031700241SO 2005 3 17 C2XA05CL013 120050227A335074441 SIGN EMB 135 EMB135LR 3260305SO EMERGENCY EXIT INOPERATIVE A C2XAK NONE L NO TEST TXTAXI/GRND HDL 1 SW2712519 145366 CLE FLT 2153, CREW REPORTED THE FORWARD EMERGENCY EXIT SIGN DID NOT ILLUMINATE DURING PREFLIGHT TESTING. MAINTENANCE REPLACED THE FORWARD BULKHEAD EMERGENCY EXIT SIGN AND FUNCTIONAL TEST GOOD. 2L72 4F RTT00011AT 20050317002422005031700242SO 2005 3 17 C2XA05TY022 120050225A335020131A BATTERY EMB 145 EMB145XR 3260214SO EMERENCY LIGHT WEAK A C2XAK NONE O OTHER ININSP/MAINT 1 SW27231394794 1369 145731 TYS - DURING A SCHEDULED 4C INSPECTION WHEN THE SERVICE/ROUTINE WAS BEING C/W THE NR 2 EMERGENCY BATTERY WAS FOUND LOW ON CHARGE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY AND OPS CHECK WAS GOOD. A/C WILL BE RELEASED WHEN ALL WORK IS C/W. 2L72 4F RT 20050317002432005031700243SO 2005 3 17 C2XA05IA037 120050303A335072875566958000 LIGHT EMB 145 EMB145XR 3260214SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714105 145649 CLE - FLIGHT 3393, DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE AISLE PATH LIGHTING BY THE GALLEY WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. NOTE: THIS PART IS NOT SERIALIZED AND TIMES ARE NOT AVAILABLE. 2L72 4F RT 20050317002442005031700244SO 2005 3 17 C2XA05RI002 120050302A33501317 BULB EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT LOOSE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714933 145018 RIC - DURING ROUTINE INSPECTION, MAINTENANCE FOUND SERVICE DOOR OVERHEAD EMERGENCY LIGHT (ONE BULB) NOT WORKING. MAINTENANCE REPOSITION BULB AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. THE ACFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20050317002452005031700245EA 2005 3 17 COMA0560164 120050309A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION DEDESCENT 1 SO01436CA 7482 FLIGHT 5911 FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20050317002472005031700247NM 2005 3 17 DHL2005781547 120050216A5542 SKIN BOEING727 727227 1384078NM RUDDER CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A C-CHECK, VERT STAB FIN STA 194 LOWER RUDDER LT SIDE UPPER T/E AT END IS CRACKED. REMOVED CRACKED BRACKET, FABRICATED NEW BRACKET FROM 2024 T3 .025 PO 9001310 DIM 3.5 X 3.5 INCH. TREATED, PRIMED AND INSTALLED BRACKET IAW B727 SRM 51-30-2, 55-30-2 FIG 1 AND 51-10-2. 2L73 4F A3WE 20050317002482005031700248NM 2005 3 17 AWXA200500323 120050310A335020131A BATTERY AIRBUSA319 A319132 3930340NM ZONE 241 DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28824AW 1490 DEN - EEL - DURING 4-DAY CHECK OPERATIONAL TEST OF EMERGENCY LIGHT SYSTEM RECEIVED A LT OVERWING EMERGENCY POWER SUPPLY UNIT BATTERY FAULT. MAINTENANCE REMOVED AND REPLACED BATTERY PACK IN THE LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050317002502005031700250NM 2005 3 17 AWXA200500325 120050131A5753655058810 GIMBAL JOINT BOEING737 737301 1384611NM TE FLAP CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - FLIGHT CONTROL - DURING C-18 CHECK GALVANIC CORROSION WAS FOUND ON RT INBOARD MID FLAP OUTBOARD GIMBAL INDEX PLATE WBL 185.0. MAINTENANCE REMOVED AND REPLACED RT INBOARD MID FLAP OUTBOARD GIMBAL ASSEMBLY IAW T/C I3R57057. 2L72 4F RTA16WE 20050317002532005031700253NM 2005 3 17 AWXA200500328 120050125A532065558722 PLATE BOEING737 737301 1384611NM R2 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK A 1.25 INCH CRACK WAS FOUND IN CLOSE PANEL BETWEEN FORWARD END OF R-2 DOOR CUTOUT AND BS 947. MAINTENANCE REMOVED CRACKED CLOSE PANEL FROM BS 947 TO BS 957, STR 14 RT TO STR 16 RT; FABRICATED A NEW REPLACEMENT CLOSE PANEL PER DWG 65-55872; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050317002552005031700255NM 2005 3 17 AWXA200500330 120050122A5320654587545 SILL BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON R-1 DOOR SILL INNER CHORD BETWEEN BS 291 AND BS 356, RBL 59, WL 208. MAINTENANCE REMOVED CORRODED R-1 DOOR SILL INNER CHORD FROM BS 291 TO BS 356, RBL 59; FABRICATED A NEW REPLACEMENT CHORD PER DWG 65-45875-45; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050317002582005031700258NM 2005 3 17 UPS05M44105 120050105A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 29 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED & REWORKED ON BARREL NUT HOLE NR 16 RT PER SRM 51-21-01.V2.R36, FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 ON BARREL NUT HOLE NR 29 RT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED ON BARREL NUT HOLE NR 29 RT PER EN1166-05 & EO MD11-5510-19409-I, FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20050317002592005031700259NM 2005 3 17 UPS05M44106 120050109A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 13 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED & REWORKED ON BARREL NUT HOLE NR 16 RT PER SRM 51-21-01.V2.R36, FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT ON BARREL NUT HOLE NR 13 RT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5 510-19409-I. REPAIR COMPLETED ON BARREL NUT HOLE NR 13 RT PER EN1153-05 & EO MD11-55 10-19409-I, FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20050317002602005031700260NM 2005 3 17 UPS05M44107 120050109A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 25 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED & REWORKED ON BARREL NUT HOLE NR 25 RT PER SRM 51-21-01.V2.R36, FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 ON BARREL NUT HOLE NR 25 RT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED ON BARREL NUT HOLE NR 25 RT PER EN1162-05 & EO MD115510-19409-I, FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20050318000042005031800004EA 2005 3 18 SWIA200514707 120050121A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07461SW 7811 RIGHT SIDE FS 621.00 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR ANGLES IAW REO 601R-53-61-117 REV B. 2L72 4F RTA21EA 20050318000062005031800006EA 2005 3 18 SWIA200514709 120050121A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07461SW 7811 TWO ANGLES CRACKED FS 280 RBL 9 (INBOARD AND OUTBOARD SIDE OF FLOORBEAM). INSTALLED ANGLES PER CRJ 200 SRM 51-42-21 AND 51-42-06. 2L72 4F RTA21EA 20050318000072005031800007EA 2005 3 18 SWIA200514710 120050121A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07461SW 7811 ANGLE CRACKED AT FS 280 LBL 9 INBOARD SIDE OF FLOORBEAM. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED ANGLE PER CRJ/200 SRM 51-42-21 AND 51-42-06. 2L72 4F RTA21EA 20050318000082005031800008EU 2005 3 18 AWXA200500337 120050315A3397FDBA5683APNK CONNECTOR AIRBUS320 A320231 3930325EU SEAT ROW 26 LT DEFECTIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28626AW 65 PHX - EEL - DURING 8-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 26 LT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT CONNECTOR AT WALL SEAT ROW 26 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050318000102005031800010EU 2005 3 18 AWXA200500339 120050315A3397E0052R8B3APNE WIRE HARNESS AIRBUS320 A320231 3930325EU SEAT ROW 26 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28632AW 81 SEA - EEL - DURING 4-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 26 LT INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE AT EMERGENCY ESCAPE PATH LIGHT CONNECTOR AT WALL CONNECTION, REPINNED CONNECTOR, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050318000112005031800011NM 2005 3 18 AWXA200500340 120050315A33501012721 LIGHT BOEING737 7373G7 1384595NM SEAT ROW 5 LT DEFECTIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 PHX - EEL - DURING 4-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE FROM SEAT ROWS 5 THROUGH 8 LT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 5 LT, OPERATIONAL CHECK OF EMERGENCY ESCAPE PATH LIGHTS WERE GOOD. 2L72 4F RTA16WE 20050318000162005031800016WP 2005 3 18 UPS05844114 120050219A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE:C1 LONGERON 15R CRACKED UNDER CANTED FRAME AT STA 1734 REMOVED LONG FROM 1725-1766, END FITTING, CLIP AT STA 1752. FAB REPLACEMENT LONG SECTIONS (S1616757 EXTRUSION), 2 SPLICE FITTINGS ON SERVICE ORDER 7034948 (S2645716 EXTRUSION), 4 REPAIR STRAPS (SHT7075T6-.080) INSTALLED ALL PARTS REF SRM 53-2-2 FIG 10, 53-5-3 FIG 5, 51-1-21, 51-1-20D, 51-1-8, DWG DC8-53B-009, NDTSPM06-10-01.001, DPS4.707. 2L74 4F RT4A25 20050318000172005031800017WP 2005 3 18 UPS05844115 120050219A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE:C1 LONGERON 14R CRACKED UNDER CANTED FRAME AT STA 1756. REMOVED LONG SECTION, END FITTING, CLIP. FAB REPLACEMENT LONG SECTION (S1616757 EXTRUSION), 2 STRAPS (SHT7075T6-.080), SPLICE FITTING ON SVC ORDER 7034949 (S2645716 EXTRUSION). INSTALLED ALL PARTS REF SRM 53-2-2 FIG 10, 51-1-20D, 51-1-21, 51-1-8, DWG DC8-53B-009, NDTSPM06-10-01.001, DPS4.707. 2L74 4F RT4A25 20050318000182005031800018WP 2005 3 18 UPS05844116 120050222A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE:C1 FUSELAGE SKIN CRACKED AT RT PRIMARY HEAT EXCHANGER CUTOUT AT LOWER AFT CORNER. CRACK APPROX 1 INCH LONG. CUT OUT DAMAGED SKIN, NDT VERIFIED. FAB DOUBLER AT FILLER FROM SHT2024 T3-.100. INSTALLED CONICAL WASHERS AND ALL REPAIR PARTS REF SRM ADDM EO DC8-5330-4732-D. 2L74 4F RT4A25 20050318000192005031800019WP 2005 3 18 UPS05844117 120050223A5330564932811 DOUBLER DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE:C1 INTERNAL DOUBLER CRACKED AT STA 1880 BETWEEN SKIN AND LONG 34R. CORRODED FROM 1861-1890. REMOVED DOUBLER FROM STA 1770-1890. FAB REPLACEMENT DOUBLER FROM SHT7075T6 -.025. INSTALLED DOUBLER REF DWG 5649328, SRM 51-1-21, 51-1-8, 51-1-20D. 2L74 4F RT4A25 20050318000202005031800020WP 2005 3 18 UPS05844118 120050217A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE:C1 FRAME CRACKED AT STA 55 BETWEEN L24R & L25R AT DUCT SUPPORT ROD MOUNT. CUT OUT CRACKED FRAME SECTION. FAB FILLER AND 2 REPAIR ANGLES FROM SHT 7075/0-.071, HEAT TREAT TO T6 ON SAA SVC ORDER 7034931. INSTALLED ALL PARTS REF SRM 53-2-0 FIG 2, 51-1-21, 53-2-0, 51-1-8, 51-1-20D, DPS7.00. 2L74 4F RT4A25 20050318000212005031800021WP 2005 3 18 UPS05844120 120050222A5347 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE:C1 MAIN CABIN SEAT TRACK SCALLOPS WORN BEYOND LIMITS STA 1360-1380, LBL 24. REMOVED FLOORBOARDS TO FOM. REMOVED SEAT TRACK FROM 1300-1460. FAB RPLACEMENT SEAT TRACK FROM S2772660 EXTRUSION. INSTALLED SEAT TRACK, NEW SPLICE FITTING, AND FLOORBOARDS REF SRM 53-2-3 FIG 12, 51-3-0, 51-1-8. 2L74 4F RT4A25 20050318000242005031800024NM 2005 3 18 UPS05M44123 120050315A3230 MECHANISM DOUG MD11 MD11F 3023600NM MLG DIRTY A IPXAO OTHER J WARNING INDICATION APAPPROACH 1 SO01251UP 48744 WHEN LANDING GEAR SELECTED DOWN DURING APPROACH 4 RED GEAR UNSAFE LIGHTS ILLUMINATED. SYNOPTIC DISPLAY INDICATED GEAR UNSAFE. AFTER APPROX 2 MINS, CYCLED GEAR UP AND BACKDOWN, ALL 4 GEAR INDICATED SAFE AS GEAR CAME DOWN SEQUENCE WAS NOTICABLY SLOWER THAN NORMAL. AIRCRAFT REMAINS OUT OF SERVICE, POSSIBLY FERRY FLIGHT TO SDF. FOUND GEAR HANDLE MECHANISM DIRTY CLEANED MECHANISM & GEAR HANDLE SWITCH, LUBED HANDLE AND BEARING OPS CK NORMAL GEAR PER 32-31-00. 2L73 4F RTA22WE 20050318000282005031800028WP 2005 3 18 WX0500032 120050308A33506011779 POWER SUPPLY DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A WX0AK NONE O OTHER ININSP/MAINT 1 WP19861GA 49557 LAS - MAINTENANCE REPORTED LEFT AND RIGHT OVERWING EMERGENCY EVACUATION LIGHTS INOPERATIVE. MAINTENANCE INSTALLED A SERVICEABLE POWER SUPPLY. SYSTEM OPERATIONALLY CHECKS GOOD IAW MM 33-53-00. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050318000292005031800029WP 2005 3 18 WX0500029 120050308A3350 LAMP DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A WX0AK NONE O OTHER ININSP/MAINT 1 WP19860GA 49786 LAS - MAINTENANCE REPORTED OVERHEAD EMERGENCY LIGHT ON FLIGHT DECK AND R-1 DOOR INOPERATIVE. MAINTENANCE RELAMPED EMERGENCY LIGHT. SYSTEM OPERATIONALLY CHECKS GOOD IAW MM 33-53-00. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050318000302005031800030WP 2005 3 18 WX0500030 120050308A3350 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A WX0AK NONE O OTHER ININSP/MAINT 1 WP19860GA 49786 LAS - MAINTENANCE REPORTED FLOOR EMERGENCY PATH LIGHTING INOPERATIVE ROWS 26 THROUGH 29. MAINTENANCE REPLACED BATTERIES IN BATTERY PACK. SYSTEM OPERATIONALLY CHECKS GOOD IAW MM 33-53-01. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050318000312005031800031WP 2005 3 18 05FDEA00543 120050315A5347S4929147 SEAT TRACK DOUG DC10 DC1010 3022110WP ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO251006048733 46970 CABIN SEAT TRACK F CORRODED FUSELAGE STATION 959 - 1130. REMOVED DAMAGED SECTION OF SEAT TRACK AND SPLICED IN NEW SECTION OF SEAT TRACK IAW DC10 SRM 53-70-00 VOL 1. 2L73 4F A22WE 20050318000322005031800032EU 2005 3 18 05FDEA00544 120050315A5310 DOUBLER AIRBUS310 A310222 3930315EU FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 REPAIR NEEDS EVALUATION FOR FAA APPROVED DATA AND MAJOR OR MINOR CLASSIFICATION ITEM NR 5 FUSELAGE, L-SHAPED DOUBLER RT SIDE ABOVE RT WING AT FR44 L-SHAPE DOUBLER, RT SIDE ABOVE WING AT FRAME A310-200 SRM 53-15-12 FIG 1 SHEET 9. 2L72 4F RTA35EU 20050318000342005031800034EA 2005 3 18 COMA0560178 120050314A5270840534 PROXIMITY SWITCH CNDAIRCL600 CL6002B19 1900309EA CABIN DOOR MALFUNCTIONED A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01713CA 7245 FLIGHT 9452 CABIN DOOR OUTER HANDLE WARNING. REPLACED PROXIMITY SWITCH DI17. 2L72 4F RTA21EA 20050318000352005031800035NM 2005 3 18 QXEA200500363 120050309A291082910010121 LINE DHAV DHC8 DHC8202 2809007NM HYDRAULIC SYS CRACKED A QXEAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 NM09355PH17025 500 BLI - FLIGHT 2136 - UPON GEAR DOWN SELECTION, THE NR 2 ENGINE HYDRAULIC FLUID QUANTITY AND PRESSURE WAS TOTALLY LOST. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NOSE LANDING GEAR DOWN HYDRAULIC LINE CRACKED. THE LINE WAS REPLACED AND OPERATIONAL CHECKS WERE PERFORMED. THE CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050318000362005031800036NM 2005 3 18 AWXA200500344 120050222A53306545871125 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28307AW 24634 MCN - MAJOR REPAIR - DURING C-14 CHECK A .25 INCH CRACK WAS FOUND IN R-1 DOOR EXTERNAL SKIN AT LOWER HINGE CUTOUT BS 300, STR 14 RT. MAINTENANCE CUT OUT DAMAGE IN R-1 DOOR EXTERNAL SKIN AT LOWER HINGE CUTOUT BS 300, STR 14 RT; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW ER 03-5200-05070-ES1. 2L72 4F RTA16WE 20050318000392005031800039SO 2005 3 18 153321505 120050215A32501159SCH4023 PRESSURE SWITCH GULSTMG1159 GIV 3980115SO NLG STEERING INOPERATIVE E N93AO OTHER O OTHER TXTAXI/GRND HDL 1 SO13467QS50 1533 NOSE WHEEL STEERING WOULD NOT SHUT OFF WHEN SELECTED OFF. 2L72 4F RTA12EA 20050318000422005031800042SO 2005 3 18 SWIA200514713 120050309A3397 TERMINAL EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT LOOSE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07580SW 120348 ONE OF TWO RED LIGHTS EMERGENCY FLOOR PATH LIGHTING ARE INOPERATIVE AT THE FORWARD DOOR. FOUND LOOSE TERMINAL CONNECTING THE BULB TO THE CIRCUIT. RESECURED LOOSE BULB, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050318000432005031800043SO 2005 3 18 SWIA200514714 120050314A3350 LAMP EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07218SW 120287 EMERGENCY FLOOR LIGHTING INOP AT ROW 8A-2 WHITE LIGHTS, NUMEROUS RED LIGHTS, & MAIN CABIN DOOR FLOOR EMERGENCY EXIT SIGN. REPLACED LAMPS AS NECESSARY, OPERATIONAL CHECKS GOOD. 2L72 4T RTA31SO 20050318000442005031800044EA 2005 3 18 SWIA200514715 120050310A3350 BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCHARGED A SWIAO OTHER O OTHER CRCRUISE 1 NM07951SW 7795 FIVE MINUTES AFTER TAKEOFF, EMERGENCY LIGHTS TURNED ON AND REMAINED ON FOR ABOUT 35 MINUTES. RESET CB4-C2 BREAKER. CHECKED CHARGER OUTPUT AT ALL FOUR PACKS AND FOUND OK. ALL ELBP'S DEAD. REMOVED AND REPLACED ALL ELBP'S. OPERATIONAL CHECKED GOOD IAW CRJ MM 33-51-04. 2L72 4F RTA21EA 20050318000462005031800046EA 2005 3 18 SWIA200514717 120050307A2721 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA RUDDER TRIM INOPERATIVE A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07923SW 7664 RUDDER TRIM DOESN'T MOVE RUDDER TRIM. REMOVED AND REPLACED RUDDER TRIM/AILERON TRIM CONTROL PANEL. OPERATIONAL CHECKS GOOD. 2L72 4F RTA21EA 20050318000502005031800050SO 2005 3 18 LR7A05004 120050203A53473556711 CARGO TRACK LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 1311 4590 DURING SCHEDULED B2 INSPECTION PER JOB CARD HSP53262 FOUND LT FS 617 25000 LB TIE DOWN FITTING CRACKED APPROX .25 INCH AT LBL 61, WL 143. REPLACED FITTING IAW SRM SMP 583 51-70. NR 2004. 2H74 4T A1SO 20050318000512005031800051EU 2005 3 18 PNSA050203 120050203A3241 BRAKE ASSY SAAB SF340 340B 7860101EU MALFUNCTIONED A PNSAD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 AL03677PA 328 DURING TAXI INTO PARKING AREA AT LIMA GATES IN ANC THE CAPTAIN STATED THERE WAS A BRAKE PROBLEM. COPILOT CHECKED BRAKES AND FOUND FULL TRAVEL OF PEDALS AND NO PRESSURE. AIRCRAFT WAS TURNED AWAY FROM GATE AND CAME TO A SLOW STOP. MAINTENANCE TOWED AIRCRAFT TO HANGAR AND PERFORMED FUNCTION CHECK OF SYSTEM WITH NO FAULT FOUND. MAINTENACE SUSPECTED POSSIBLE ANTI-SKID PROBLEM AND ASKED FLIGHT CREW FOR OPS CHECK NEXT DAY WHICH WAS NORMAL. NO ADDITIONAL PROBLEMS SINCE. 2L72 4T RTA52EU 20050318000532005031800053SO 2005 3 18 1521022405 120050224A32501159SCH4023 SOLENOID VALVE GULSTMG1159 GIV 3980115SO MLG UNKNOWN E N93AO OTHER J WARNING INDICATION APAPPROACH 1 SO13413QS548 1521 STEER BY WIRE FAIL, CAS MESSAGE CAME ON WHEN LANDING GEAR EXTENDED. 2L72 4F RTA12EA 20050318000542005031800054NM 2005 3 18 SWAA050807 120050315A53156545410 FLOORBEAM BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND 3 EA CRACKS ON LONGITUDINAL BEAM WEB AT BS 710, RBL 25, WL 201. REPAIRED BEAM PER PAE ER. 2L72 4F RTA16WE 20050321000032005032100003NM 2005 3 21 SWAA050814 120050316A335010107451 SIGN BOEING737 7373H4 1384600NM MID CABIN DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29336SW 23940 LT OVERWING EMERGENCY EXIT SIGN FELL OFF. REINSTALLED SIGN PER MM. 2L72 4F RTA16WE 20050321000052005032100005NM 2005 3 21 SWAA050816 120050316A53306545768 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29512SW 24189 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER AFT CORNER OF CUTOUT. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050321000062005032100006 2005 3 21 SWAA050817 420050316A2565D31354 SLIDE BOEING737 7375H4 138449DNM FWD CABIN OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29513SW 24190 DURING SCHEDULED C2 CHECK, FOUND R1 & L1 DOOR EMERGENCY EVAC SLIDES OUT OF ADJUST. ADJUSTED SLIDES PER MM. 2L72 4F RTA16WE 20050321000072005032100007 2005 3 21 SWAA050818 420050316A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29603SW 27954 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050321000082005032100008NM 2005 3 21 SWAA050819 120050316A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29654SW 28399 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON SHEAR TIE AT BS 747, BETWEEN RBL 7 TO RBL 11. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050321000102005032100010NM 2005 3 21 SWAA050821 120050316A53226546546 SHEAR TIE BOEING737 7373Q8 1384670NM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND CORROSION ON SHEAR TIE AT BS 747, LBL 9, WL 147. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050321000162005032100016EU 2005 3 21 MALA050258 120050310A3020 MODULE SAAB SF340 340B 7860101EU INTAKE HEAT MALFUNCTIONED A MALAO OTHER O OTHER CRCRUISE 1 GL15421XJ 340B421 RIGHT INTAKE HEAT MAT GLOWING AND BURNING IN FLIGHT. REPLACED RT LOWER DUCT AND IPD AND MODULE. 2L72 4T RTA52EU 20050321000172005032100017EU 2005 3 21 MALA050259 120050311A3250 ACTUATOR SAAB SF340 340B 7860101EU NLG STEERING MALFUNCTIONED A MALAO OTHER O OTHER TXTAXI/GRND HDL 1 GL15436XJ 340B436 AFTER DEICING AND TAXING OUT TO TAKEOFF, THE NOSE WHEEL STEERING LOCKED UP. RETURNED TO GATE. REMOVED AND REPLACED NWS ACTUATOR. 2L72 4T RTA52EU 20050321000192005032100019EU 2005 3 21 MALA050253 120050303A2731 ACTUATOR SAAB SF340 SF340A 7850100EU PITCH TRIM MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL1599XJ 340A099 MAIN PITCH TRIM INOP ON BOTH YOKES. AIR TURNBACK. REMOVED AND REPLACED MAIN PITCH TRIM ACTUATOR IAW SAAB MM-27-10-32. PITCH TRIM OPERATES NORMAL. 2L72 4T RTA52EU 20050321000202005032100020EU 2005 3 21 MALA050240 120050301A243023080031 GENERATOR SAAB SF340 340B 7860101EU RIGHT FAILED A MALAO OTHER HJ ELECT. POWER LOSS-50 PC WARNING INDICATION NRNOT REPORTED 1 GL15423XJ 340B423 RIGHT DC GENERATOR FAILED. REMOVED AND REPLACED RIGHT DC GEN P/N ON/OFF 23080-031. S/N OFF 98149 IAW SF40 AMM 24-31-05. 2L72 4T RTA52EU 20050321000222005032100022EU 2005 3 21 MALA050247 120050301A5320 SILL BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15502XJ E2307 DURING C2 CHECK IN YYC FOUND AFT SERVICE DOOR SILL CORRODED. FWD & AFT SECTION. P/N HC53850821-0024, P/N HC53850800-0024. 2H74 4F RTA49EU 20050316000722005031600072WP 2005 3 16 UPS05844039 120050220A5312 BULKHEAD DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01811UP 46089 INSPECTION TYPE:C2 AFT PRESSURE BULKHEAD IS CRACKED APPROX 1 INCH AT LBL 35 AROUND LONGERON 12L AREA. NDT VERIFIED CRACK APPROX 1.5 INCH PER NDT SPM 06-10-01.001. REPAIRED AFT PRESSURE BULKHEAD IAW SRO DWG 8530007. 2L74 4F RT4A25 20050316000732005031600073WP 2005 3 16 UPS05844040 120050217A53403755847U502 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01811UP 46089 INSPECTION TYPE:C2 C-PIT DOOR ENTRANCE FS 1220 L32R BANANA FITTING CRACKED .400 INCH LONG. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D AT FS 1220 LONG 29R TO 33R. 2L74 4F RT4A25 20050316000852005031600085NM 2005 3 16 DHL2005781533 120050214A5330 SKIN BOEING727 727227 1384078NM FUSELAGE GOUGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A C-CHECK, RT FUSELAGE L/E AREA IS GOUGED APPROX STA 720 E (MARKED). REMOVED PREVIOUS REPAIR AT RT FUELAGE L/E AREA STA 720E STR 19R IAW B727 SRM 51-30-2. FABRICATED DOUBLER REPAIR MAT USED 2024T3 .071 PO 9001765 DIM 10.5 X 9.5 INCH AND FILLER MAT USED 2024T3 .063 PO 9001634 DIM 10.5 X 5.5 INCH PO IAW B727 SRM 53-30-2 FIG 2 AND 53-30-3 FIG 14. ALODINED AND PRIMED PARTS AND AREA IAW B727 SRM 51-10-2. INSTALLED REPAIR IAW B727 SRM 53-30-3 FIG 14. 2L73 4F A3WE 20050316000882005031600088NM 2005 3 16 SWAA050719 120050309A53306545774 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29521SW 25320 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 25L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050316000892005031600089NM 2005 3 16 SWAA050720 120050309A212165771 FAN BOEING737 7373K2 13844BANM COCKPIT FAULTY A SWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW29340LV 23738 ELECTRICAL SMELL IN COCKPIT. TURNED EQUIPMENT COOLING FAN TO ALTERNATE, SMELL SUBSIDED. REMOVED AND REPLACED FAN PER MM. 2L72 4F RTA16WE 20050317000242005031700024NM 2005 3 17 SWAA050774 120050314A53106547978 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29605SW 27956 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 727C TO BS 727E, RBL 67, WL 208. REPAIRED BEAM PER SRM. 2L72 4F RTA16WE 20050317000372005031700037NM 2005 3 17 CALA0500070 120050302A53206545875070 THRESHOLD BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714337 23575 INSPECTION FOUND R-1 DOOR THRESHOLD DRAIN FRAME CORRODED AT STA 294-342, BL 0 TO RBL 36. A CHORD WAS INSTALLED IAW SRM 51-40-02 AND DRAWING 55-45875. 2L72 4F RTA16WE 20050317000382005031700038NM 2005 3 17 CALA0500071 120050307A531565C339503 FLOORBEAM BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717614 27327 INSPECTION FOUND CABIN FLOORBEAM FORWARD FLANGE OF UPPER CHORD FASTENER HOLE CORRODED AT STA 986, RBL 43 TO RBL 44. THE FLOORBEAM WAS REPAIRED IAW ECRA 5321-01209. 2L72 4F RTA16WE 20050317000502005031700050NM 2005 3 17 UPS05M44068 120050110A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 34 LT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED ON BARREL NUT HOLE NR 34 LT PER SRM 51-21-01.V2.R36, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 34 LT PER SRM 51-21-01.V2.R36. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 ON BARREL NUT HOLE NR 34 & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED ON BARREL NUT HOLE NR 34 LT PER EN1140-05 FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20050317000592005031700059SO 2005 3 17 MASA200500193 120050308A335078241 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07852MJ 145567 ASH 2824 FROM CLT TO SDF HAD THE CEILING OVERWING EMERGENCY EXIT SIGN FWD POSITION INOP. MAINTENANCE REPLACED THE SIGN ASSY P/N 8232-4 AND INVERTER AND BATTERY PACK P/N 2013-1A AND BATTERY CHARGER ASSY P/N BA5-0933-901. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050317000822005031700082SO 2005 3 17 MASA200500172 120050303A3350 ELEC CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCONNECTED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07828MJ 145218 ASH FLT 2876 CLT HAD 2 EMERGENCY EXIT LIGHTING FLOOR PROXIMITY LIGHTS INOPERATIVE. MAINTENANCE SECURED THE ELECTRICAL CONNECTION TO THE LIGHTING ASSEMBLY, OPS GOOD. 2L72 4T RTT00011AT 20050317000832005031700083SO 2005 3 17 MASA200500185 120050306A3350 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07826MJ 145214 ASH 2885 FROM CLT TO LIT HAD THE OVERWING EMERGENCY EXIT SIGN AFT PORTION INOP. MAINTENANCE SECURED EMERGENCY EXIT SIGN INVERTER AND SIGN OPERATED NORMALLY. A/C DEPARTED WITHOUT FURTHER INCIDENT. 2L72 4T RTT00011AT 20050317000852005031700085WP 2005 3 17 ABXA050068 120050305A541457530121 PANEL DOUG DC8 DC861 3021952WP NR 2 PYLON CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23853AX 46037 DURING ROUTINE LINE MAINTENANCE AT ILN, FOUND A 2.250 INCH CRACK IN NR 2 PYLON OUTBOARD PLANK AT STA YN300. REPAIRED PYLON PLANK IAW ABX AIR REA D853-51551-MR USING 17-7 PH .080 INCH, PO 408448907. 2L74 4F 4A25 20050317000892005031700089NM 2005 3 17 2005UALA00203 120050302A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29582UA 26702 CABIN FLOORBEAM HAS CORROSION ON UPPER TEE CAP STA 324, RBL 46 - 59. TRIMMED TEE CAP AND INSTALLED ANGLE AND STRAP REPAIR FOR TEE CAP SPLICE. 2L72 4F4 FRTA2NM E17NE 20050317000912005031700091NM 2005 3 17 2005UALA00205 120050302A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29582UA 26702 FLOORBEAM STA 1640, RBL 44- 48 CORRODED. DAMAGED FLOOR BEAM WAS REMOVED AND A REPAIR USING SPLICE STRAPS AND ANGLES WAS INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050317000932005031700093NE 2005 3 17 2005UALA00207 220050302A7200 COMPRESSOR BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE NR 1 ENGINE STALLED A UALAEC ENGINE SHUTDOWN ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 WP29648UA 25285 NR 1 ENGINE COMPRESSOR STALL AND AUTO SHUTDOWN. ABORTED TAKEOFF AT 50 KIAS DUE TO COMPRESSOR SURGE. CAPT REPORTED STRONG X-WIND AT 20 GUSTING 33. FOUND METAL IN THE TAILPIPE. ENGINE REPLACED AT IAD. ENGINE RETURNED TO LESSOR ON 06/08/05 WITHOUT BEING DISASSEMBLED. 2L72 4F4 FRTA1NM E24NE 20050317000992005031700099NM 2005 3 17 SWAA050713 120050308A335010107451 SIGN BOEING737 7373H4 1384600NM EMERGENCY EXIT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29374SW 26582 LT OVERWING DOOR EMERGENCY EXIT SIGN CAME LOOSE. REINSTALLED SIGN PER MM. 2L72 4F RTA16WE 20050317001012005031700101 2005 3 17 SWAA050715 420050308A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29405WN 27893 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. SLIDE DID NOT DEPLOY. REINSTALLED L1 DOOR SLIDE PER MM. 2L72 4F RTA16WE 20050317001022005031700102WP 2005 3 17 0500239610 120050202A5312 BULKHEAD DOUG DC9 DC932 3022066WP FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01610NW 47432 DURING H-CHECK FOUND CORROSION ON AFT PRESSURE BULKHEAD WEB AND DOUBLER BETWEEN L22 TO L23R. REPAIRED PER EA 96-202500. 2L72 4F A6WE 20050317001322005031700132NM 2005 3 17 UPS05M44078 120050103A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 19 LT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED ON BARREL NUT HOLE NR 19 LT PER SRM 51-21-01.V2.R36, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 19 LT PER EN1128-05. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 ON BARREL NUT HOLE NR 19 LT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED ON BARREL NUT HOLE NR 19 LT PER EN1128-05, FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20050317001552005031700155NM 2005 3 17 QXEA200500346 120050217A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09363PH 520 PDX - RIGHTHAND OUTBOARD NR 10 SEAT TRACK HAS CORROSION IN BOTTOM OF CHANNEL AT X404 AND ON TOP AT X422. REPAIRED IAW DHC-8 202 SRM 51-40-00 AND SRM 51-40-11. 2H72 4T RTA13NM 20050317001602005031700160NM 2005 3 17 UPS05544038 120050309A3350 LIGHT BOEING757 75724APF 1384969NM COCKPIT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01471UP 28842 INSPECTION TYPE:N/A EMERGENCY LIGHT UNARMED IND LIGHT INOP. RELAMPED LIGHT, OPS OK IAW MM 33-11-00-2. 2L72 4F RTA2NM 20050317001702005031700170EA 2005 3 17 COMA0570029 120050309A5315CC670341755 FLOORBEAM CNDAIRCL600 CL6002C10 1390015EA FUSLEAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01641CA3959 10122 THE TRANSVERSE BEAM AT FS 280 IS CORRODED FROM LBL 36 TO RBL 36. THE CORRODED TRANSVERSE BEAM WAS REMOVED. A NEW TRANSVERSE BEAM WAS FABRICATED AND INSTALLED IAW BRAS EO 601R-53-6066 AND BOMBARDIER REO 670-53-11-047 REV A. 2L72 4F RTA21EA 20050317001992005031700199NM 2005 3 17 QXEA200500334 120050217A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09363PH 520 PDX - SEAT TRACK NR 1 HAS PITTING CORROSION AT X342. REPAIRED IAW DHC-8 202 SRM 51-40-00 AND SRM 51-40-11. 2H72 4T RTA13NM 20050317002142005031700214NM 2005 3 17 05FDEA00497 120050311A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 BS 950, BL 59, WL 200, MECHANICAL DAMAGE ON LWR FLOORBEAM ANGLE. REPAIRED PER SRM 51-30-5, 51-30-6, 51-20-1 2L73 4F RTA3WE 20050317002162005031700216NM 2005 3 17 QXEA200500358 120050228A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09413QX 4060 PDX - LEFTHAND OUTBOARD SEAT TRACK HAS SURFACE CORROSION AT APPROXIMATELY X373. REPAIRED IAW DHC-8 400 SRM 51-42-05, 51-40-07, 51-42-00 AND 51-42-15. 2H72 4T RTA13NM 20050317002182005031700218NM 2005 3 17 QXEA200500315 120050223A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09413QX 4060 PDX - CORROSION ON RIGHTHAND OUTBOARD SEAT TRACK AT APPROXIMATELY X309.00, TOP AND INNER FLANGE. REPLACED SEAT TRACK IAW DHC-8 SRM 51-42-15 AND 51-42-05. 2H72 4T RTA13NM 20050317002332005031700233NM 2005 3 17 QXEA200500312 120050223A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09413QX 4060 PDX - CORROSION ON RIGHTHAND OUTBOARD SEAT TRACK AT APPROXIMATELY X358.00, TOP AND INNER FLANGE. REPLACED SEAT TRACK IAW DHC-8 SRM 51-42-15 AND 51-42-05. 2H72 4T RTA13NM 20050317002352005031700235NM 2005 3 17 QXEA200500314 120050223A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09413QX 4060 PDX - CORROSION ON RIGHTHAND OUTBOARD SEAT TRACK AT APPROXIMATELY X325.00, TOP AND INNER FLANGE. REPLACED SEAT TRACK IAW DHC-8 SRM 51-42-15 AND 51-42-05. 2H72 4T RTA13NM 20050317002492005031700249NM 2005 3 17 AWXA200500324 120050131A575369406575 SUPPORT BOEING737 737301 1384611NM TE FLAP CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - FLIGHT CONTROL - DURING C-18 CHECK INTERGRANULAR CORROSION WAS FOUND ON LT INBOARD MID FLAP INBOARD GIMBAL OUTER SUPPORT WBL 71.24. MAINTENANCE REMOVED AND REPLACED LT INBOARD MID FLAP INBOARD GIMBAL OUTER SUPPORT IAW BOEING SOPM 20-50-01. 2L72 4F RTA16WE 20050317002512005031700251NM 2005 3 17 AWXA200500326 120050131A5753693720910 SUPPORT BOEING737 737301 1384611NM TE FLAP CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - FLIGHT CONTROL - DURING C-18 CHECK GALVANIC CORROSION WAS FOUND ON RT INBOARD MID FLAP OUTBOARD GIMBAL OUTER SUPPORT WBL 185.0. MAINTENANCE REMOVED AND REPLACED RT INBOARD MID FLAP OUTBOARD GIMBAL OUTER SUPPORT IAW T/C I3R57057. 2L72 4F RTA16WE 20050317002542005031700254NM 2005 3 17 AWXA200500329 120050128A533065C337568 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK A .25 INCH CRACK WAS FOUND IN FUSELAGE SKIN EMANATING FROM FASTENER HOLE AT FORWARD LOWER CUTOUT OF R-2 DOOR BS 947. MAINTENANCE CUT OUT CRACK IN FUSELAGE SKIN AT FORWARD LOWER CUTOUT OF R-2 DOOR BS 947; FABRICATED 2 EACH INNER PATCHES AND TAPERED FILLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-60-01 FIG 203. 2L72 4F RTA16WE 20050317002562005031700256NM 2005 3 17 UPS05M44103 120050109A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE: C, NR 16 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED & REWORKED ON BARREL NUT HOLE NR 16 RT PER SRM 51-21-01.V2.R36 FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 ON BARREL NUT HOLE NR 16 RT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED ON BARREL NUT HOLE NR 16 RT PER EN1156-05 & EO MD11-5510-19409-I, FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20050318000012005031800001EU 2005 3 18 05FDEA00541 120050315A5311 FRAME AIRBUS310 A310222 3930315EU FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 REPAIR NEEDS EVALUATION FOR FAA APPROVED DATA AND MAJOR OR MINOR CLASSIFICATION. ITEM NR 9 ON LIST FUSELAGE, REPAIR DOUBLER, LOWER RT SIDE, AT FR 26/32 REPAIR DOUBLER FOUND TO BE IN CONFORMANCE WITH A310-200 SRM 53-10-12 FIG 205. ACTUAL LOCATION OF DOUBLER FRAME 26/32 AT STR 31 RT SIDE. 2L72 4F RTA35EU 20050318000022005031800002EU 2005 3 18 UPS05144126 120050315A3510 REGULATOR AIRBUS300 A300B4622R 3930312EU COCKPIT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01134UP 0817 INSPECTION TYPE:N/A ALL FOUR 02 BOTTLES FOUND EMPTY ON WALKAROUND. REMOVED AND REPLACED NR 3, 02 BOTTLE PRESSURE REGULATOR IAW AMM 35-11-31-4, LEAK CHECKS GOOD. 2L72 4F RTA35EU 20050318000052005031800005EA 2005 3 18 SWIA200514708 120050121A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07461SW 7811 MAIN CABIN AREA UNDER FLOOR INTERCOSTAL AT APPROX FS 485, LBL 36 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED ANGLE IAW REO 601R-53-41-059. 2L72 4F RTA21EA 20050318000092005031800009NM 2005 3 18 AWXA200500338 120050315A2560P4010021 BATTERY BOEING737 7373S3 1384711NM FLASHLIGHT DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 SNA - EMERGENCY EQUIPMENT - DURING A-01 CHECK FOUND THE AFT GALLEY EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT GALLEY EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050318000122005031800012NM 2005 3 18 AWXA200500342 120050217A1430697307116 BOLT BOEING737 7373G7 1384595NM HORIZONTAL STAB CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28307AW 24634 MCN - FLIGHT CONTROL - DURING C-14 CHECK GALVANIC CORROSION WAS FOUND ON LT HORIZONTAL STABILIZER UPPER REAR BOLT. MAINTENANCE REMOVED AND REPLACED LT HORIZONTAL STABILIZER UPPER REAR BOLT IAW T/C I6C55307. 2L72 4F RTA16WE 20050318000132005031800013NM 2005 3 18 AWXA200500343 120050219A534765538441 CARGO TRACK BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28307AW 24634 MCN - MAJOR REPAIR - DURING C-14 CHECK CORROSION WAS FOUND ON AFT CARGO COMPARTMENT TIE DOWN TRACK AT BS 773, RBL 13.80. MAINTENANCE CUT OUT DAMAGE IN AFT CARGO COMPARTMENT TIE DOWN TRACK AT BS 773, RBL 13.80; FABRICATED A REINFORCEMENT ANGLE; INSTALLED REPAIR PART IAW ER 03-5300-05072-SS1. 2L72 4F RTA16WE 20050318000262005031800026WP 2005 3 18 WX0500033 120050314A33501315 BULB DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A WX0AK NONE O OTHER ININSP/MAINT 1 WP19863GA 49911 DEN - MAINTENANCE REPORTED EMERGENCY EXIT LIGHT IN OVERHEAD AT SEAT ROW 8 INOPERATIVE. MAINTENANCE RELAMPED EXIT LIGHT AT SEAT ROW 8. SYSTEM OPERATIONALLY CHECKS GOOD IAW MM 33-53-00. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050318000272005031800027WP 2005 3 18 WX0500031 120050308A3350 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A WX0AK NONE O OTHER ININSP/MAINT 1 WP19860GA 49786 MAINTENANCE REPORTED EMERGENCY EXIT LIGHTED SIGNS AT AFT OVERWING EXITS INOPERATIVE. MAINTENANCE REPLACED BATTERIES IN BATTERY PACK. SYSTEM OPERATIONALLY CHECKS GOOD IAW MM 33-53-01. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050318000372005031800037NM 2005 3 18 05024 120050315A2612 FIRE DETECTOR BOEING747 747123 1384873NM CARGO BAY MALFUNCTIONED A KCSAO OTHER N FALSE WARNING NRNOT REPORTED 1 GL23717CK 20325 LOWER AFT CARGO COMPARTMENT FIRE WARNING LIGHT ILLUMINATED AND BELL SOUNDED (WITH CARGO HEAT ON). INSPECTED LOWER AFT CARGO COMPT FOR SIGNS OF FIRE. NO INDICATION OF FIRE FOUND. CANNOT DUPLICATE ON GROUND. INSPECTED THE CARGO HEATING SYSTEM. NO DEFECTS FOUND. 2L74 4F A20WE 20050318000452005031800045EA 2005 3 18 SWIA200514716 120050303A5610 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAO OTHER O OTHER DEDESCENT 1 NM07929SW 7703 DESCENDING OUT OF F290, F/O'S SIDE WINDOW CRACKED. REPLACED F/O WINDOW IAW CRJ AMM 56-12-01. P/N OFF: 601R33033-12, S/N OFF: 02179H9314. 2L72 4F RTA21EA 20050318000492005031800049SO 2005 3 18 LR7A05003 120050202A3230M832482910 PACKING EATON LKHEED382 382G 526414USO REGULATOR VALVE CUT A LR7AA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 AL03402LC 4698 DURING CRUISE FLIGHT CREW NOTED UTILITY HYDRAULIC SYSTEM DEPLETED AND COMPLIED WITH QRH PROCEDURES. RETURNED TO KWRI AND LANDED WITHOUT INCIDENT. FOUND LEAKAGE DUE CUT PACKING ON RT LANDING GEAR UP FLOW REGULATOR VALVE AT FS 505, RBL 62, WL 271. REPLACED PACKING IAW MM SMP 581 32-31. ACCOMPLISHED LANDING GEAR RETRACTION CHECK IAW MM SMP 581 32-00 PP 204-214. LP 20112, ITEM 1. 2H74 4T A1SO 20050321000272005032100027EU 2005 3 21 MALA050243 120050228A5280 SKIN BAC 146 AVRO146RJ85A1500097EU RT MLG DOOR DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15502XJ E2307 DURING C2 CHECK IN YYC, INSPECTED MLG DOOR, LT AS PER EOA52024. REPAIRED IAW EOA52047. FWD EDGE LWR SKIN 8 INCHES FROM TOP OF MLG DOOR SKIN CHAFED. 2H74 4F RTA49EU 20050321000282005032100028EU 2005 3 21 MALA050244 120050301A5311 FRAME BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15502XJ E2307 DURING C2 CHECK IN YYC FOUND INBOARD FWD AT FRAME 15 CORROSION FOUND ON ATTACHMENT OF FWD STOWING AIRSTAIRS RAILING. 2H74 4F RTA49EU 20050321000312005032100031EU 2005 3 21 MALA050267 120050313A5340 NUT PLATE SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15433XJ 340B433 DURING 4Y/2Y CHECK IN BNA FOUND 2 EA NUT PLATES CORRODED. FOUND SUPPORT CORRODED BETWEEN FR STA 272.0 AND 288.0. LT SIDE FABRICATED NEW PART PER SAMPLE. WORK PERFORMED ON EMB WO 211832 TASK 1505. 2L72 4T RTA52EU 20050321000332005032100033EU 2005 3 21 MALA050272 120050312A5311 FRAME SAAB SF340 340B 7860101EU FUSELAGE CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15433XJ 340B433 DURING 4Y/2Y CHECK IN BNA FOUND RT FUSELAGE FRAME STA 686 INBOARD FLANGE CHAFED FROM CARGO DOOR AFT CABLE JUST ABOVE FLOOR LEVEL. SMOOTHED OUT, PRIMED, PAINTED, AND INSTALLED WEAR STRIP. REF MESABA EOS53290. WORK PERFORMED ON EMB WO 211832 TASK 1514. 2L72 4T RTA52EU 20050321000342005032100034EU 2005 3 21 MALA050271 120050312A5320 ANGLE SAAB SF340 340B 7860101EU FUSELAGE CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15433XJ 340B433 DURING 4Y/2Y CHECK IN BNA FOUND CLOSE OUT ANGLE CHAFED OUT OF LIMIT REF RM 51-10-10, PANEL 194BR. REPLACED FABRICATE PER SAMPLE. WORK PERFORMED ON EMB WO 211832 TASK 6503. 2L72 4T RTA52EU 20050321000352005032100035EU 2005 3 21 MALA050262 120050313A1420 CONNECTOR SAAB SF340 340B 7860101EU RT PROPELLER DAMAGED A MALAO OTHER N FALSE WARNING CRCRUISE 1 GL15360PX 340B220 AFTER LEAVING MSP, THE RIGHT PROP OIL TEMP GAUGE READING ABOVE 150 DEGREES CELSIUS AND FLUXING FROM 120 DEGREES. AFTER CREW FOLLOWED QRH AND REDUCED POWER THE FLUXING SUBSIDED BUT TEMP REMAINED HIGH AROUND 100 DEGREES CELSIUS AT 45 PERCENT TORQUE. INSTALLED NEW CONNECTOR ON RIGHT PGB OIL TEMP SENSOR. OPS CHECK GOOD. 2L72 4T RTA52EU 20050321000372005032100037NM 2005 3 21 SWAA050808 120050315A55536547450 CLEVIS BOEING737 7373Q8 1384670NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND LT & RT VERTICAL STAB FITTING FWD & AFT PRIMARY CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER SRM. 2L72 4F RTA16WE 20050321000452005032100045SO 2005 3 21 CHQA200500049 120050309A335066367 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11572RP 14500828 AFT EMERGENCY FLOOR PROXIMITY LIGHT STRIP IS INOP. REMOVED AND REPLACED FLOOR PROXIMITY LIGHT STRIP IAW EMB 145 AMM 33-50-12-4. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050321000482005032100048SO 2005 3 21 CHQA200500052 120050311A3350244424 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11291SK 145486 RIGHT HAND EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED EXIT MARKER IAW EMB 145 AMM 33-50-14. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050321000502005032100050SO 2005 3 21 CHQA200500054 120050313A2120 SMOKE EMB 145 EMB145LR 3260212SO CABIN DETECTED A CHQAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 GL11279SK 145379 FLIGHT 3039 BOS-MYR - DURING INTIAL CLIMB A LAV SMOKE INDICATION APPEARED ON EICAS. THE FLIGHT ATTENDANT REPORTED THERE WAS NO EVIDENCE OF ODOR, SMOKE, OR FIRE IN THE CABIN. ALL OTHER INDICATIONS IN THE COCKPIT WERE NORMAL. THE AIRCRAFT WAS HEAVILY DE-ICED IN BOS. WITH A STRONG SUSPICION OF DE-ICING FLUID IN THE AIR CONDITIONING SYSTEM AND NO VISIBLE INDICATION OF SMOKE, THE FLIGHT WAS CONTINUED TO MYR WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED AN INSPECTION OF THE ENGINES, APU, AND LAVATORY SMOKE DETECTOR. OPS CHECK GOOD. NO SMOKE OR ODOR PRESENT. 2L72 4T RTT00011AT 20050321000522005032100052NM 2005 3 21 0500325530 120050309A5414 SKIN PANEL BOEING757 757251 1384970NM NR 2 PYLON CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01530US 23845 DURING H-CHECK FOUND CRACK IN NR 2 PYLON RT SIDE SKIN PANEL NACELLE STA 136. REPAIRED PER EA 55-202910. 2L72 4F RTA2NM 20050321000542005032100054SO 2005 3 21 CHQA200500055 120050312A335078241 STATIC INVERTER EMB 145 EMB145MP 3260216SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11974RP 145203 EMERGENCY LIGHT ON COCKPIT PARTITION EXIT MARKER IS INOP. REMOVED AND REPLACED STATIC INVERTER NR 1 IAW EMB 145 AMM 33-50-11. OPS CHECK GOOD. 2L72 4F RTT00011AT 20050321000552005032100055SO 2005 3 21 CHQA200500056 120050315A2120 ODOR EMB 145 EMB145LR 3260212SO CABIN DETECTED A CHQAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 GL11579RP 14500871 LAV SMOKE INDICATION APPEARED ON EICAS DURING CLIMBOUT. A FAINT ELECTRICAL BURNING ODOR WAS NOTED IN THE COCKPIT. RETURNED TO FIELD AND LANDED UNEVENTFULLY. THE LAV SMOKE INDICATION WENT OUT ON SHORT FINAL. THE AIRCRAFT WAS FERRIED TO CMH FOR MAINTENANCE. MAINTENANCE PERFORMED ENGINE RUNS AND TROUBLESHOT THE LAV SMOKE IAW EMB 145 FIM 21-20-00-810-801-A AND ROLLS ROYCE FIM. FOUND THE ENGINE NR 2 OIL TO BE OVERSERVICED. DRAINED OIL TO SERVICEABLE LIMITS. REMOVED CUSTOMER SERVICE MANIFOLD ON ENGINE NR 2 TO INSPECT FOR VISIBLE OIL. NO DEFECTS NOTED. PERFORMED ENGINE RUNS. NO SMELL NOTED. 2L72 4T RTT00011AT 20050321000562005032100056NM 2005 3 21 QXEA200500489 120050315A5210 DOOR BOMBDRDHC8 DHC8401 1390041NM MAIN PAX STUCK A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09413QX 4060 SMF - RAMP REPORTS THAT AFT PASSENGER DOOR IS STUCK. MAINTENANCE RESET THE AFT PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2H72 4T RTA13NM 20050321000572005032100057EA 2005 3 21 VTZA200500011 120050317A5320601R3111387 VERTICAL SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27708BR 7575 LEFT 280 VERTICAL ANGLES CRACKED AT .5 INCH BETWEEN FASTENERS. 2L72 4F RTA21EA 20050321000602005032100060EA 2005 3 21 VTZA200500012 120050317A53206013501251 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27708BR 7575 LEFT 624 OBLIQUE ANGLE IS CRACKED AT 1 INCH IN RADIUS. 2L72 4F RTA21EA 20050321000612005032100061EA 2005 3 21 VTZA200500015 120050317A5320601R3111358 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27708BR 7575 RIGHT VERTICAL ANGLE IS CRACKED AT .5 INCH BETWEEN FASTENERS. 2L72 4F RTA21EA 20050321000632005032100063EA 2005 3 21 VTZA200500010 120050317A2760 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A VTZAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA27649BR 7414 SPOILERON FAULT MESSAGE. RESET SECU'S, FUNCTIONAL CHECK OK. 2L72 4F RTA21EA 20050321000642005032100064EA 2005 3 21 VTZA200500013 120050317A53116013600130 DOUBLER CNDAIRCL600 CL6002B19 1900309EA FRAME CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27708BR 7575 RIGHT FS 640 FRAME DOUBLER IS CRACKED IN RADIUS AT 3 INCH IN RADIUS. 2L72 4F RTA21EA 20050321000652005032100065WP 2005 3 21 DHL2005807003 120050313A3150 WARNING HORN DOUG DC8 DC873F 302199FWP THRUST REVERSERSACTIVATED A DHLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01807DH 45990 ON THRUST LEVER ADVANCE PRIOR TO ACCELERATION, T/O WARNING HORN SOUNDED. RETARDED THRUST LEVERS TAXI CLEAR OF RUNWAY. CYCLED SPOILER HANDLE SEVERAL TIMES NO TAKEOFF WARNING NOTED OPS CHECK NORMAL IAW 27-60-0. 2L74 4F RT4A25 20050321000672005032100067NM 2005 3 21 F3LA200500013 120050311A2752791C000001 ACTUATOR AIRBUSA319 A319111 3930336NM TE FLAP FAULTY A F3LAO OTHER F FLT CONT AFFECTED APAPPROACH 1 NM03912FR8967 842 1803 ON APPROACH, CREW REPORTED FLAP SYSTEM JAM WHEN FLAPS 2 SELECTED, SLATS EXTENDED TO E CONFIG 3. DECLARED AN EMERGENCY. CHECKED FLAP SYSTEM. FOUND LT WING NR 1 TRANSMISSION TORQUE LIMITER TRIPPED. RESET TORQUE LIMITER. PERFORMED TEST FLIGHT, MADE 3 APPROACHES & SYSTEM TESTED NORMALLY. REMOVED & REINSTALLED PANELS 575DB, 575EB, 575BB AND 573AB. PERFORMED FRICTION CHECK OF NR 4 LT FLAP TRANSMISSION, NR 3 FLAP ACTUATOR, NR 2 FLAP ACTUATOR AND INLINE OFFSET GEARBOX AND CHECKED GOOD. FOUND NR 1 LT AND RT FLAP ACTUATOR CAVITIES FULL OF WATER. REPLACED NR 1 LT AND RT FLAP ACTUATORS PER AMM 27-54-49-PB401 AND CHECKED NORMAL. PERFORMED OPS CHECK OF FLAPS PER AMM 27-54-45-000-003 AND 27-511-49-740-068. 2L72 4F RTA28NM 20050321000692005032100069EU 2005 3 21 MALA050270 120050312A5320 ANGLE SAAB SF340 340B 7860101EU FUSELAGE CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15433XJ 340B433 DURING 4Y/2Y CHECK IN BNA FOUND CLOSE OUT ANGLE CHAFED OUT OF LIMIT REF SRM 51-10-10 PANEL 193C6. REPLACED FABRICATE PER SAMPLE. WORK PERFORMED ON EMB WO 211832 TASK 5504. 2L72 4T RTA52EU 20050321000702005032100070EU 2005 3 21 MALA050273 120050312A5320 FRAME SAAB SF340 340B 7860101EU FUSELAGE CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15433XJ 340B433 DURING 4Y/2Y CHECK IN BNA FOUND RIGHT FUSELAGE FRAME STA 686 INBOARD FLANGE CHAFED FROM CARGO PANEL 2 O'CLOCK POSITION. REPAIRED PER REPAIR ANGLE REF MESABA EO S53291. WORK PERFORMED ON EMB WO 211832 TASK 1513. 2L72 4T RTA52EU 20050321000812005032100081 2005 3 21 F3LA200500012 420050310A22103945128102 COMPUTER AIRBUSA319 A319112 3930323EU ELAC FAULTY A F3LAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM03909FR 1214 1761 FLIGHT CREW REPORTED ECAM FLIGHT CONTROL ELAC 2 PITCH FAULT (PASSING THROUGH FL180). AIRCRAFT RETURNED TO DEN AND LANDED WITHOUT INCIDENT. REPLACED NR 2 ELAC COMPUTER PER AMM 27-93-PB401; REPLACED THS ACTUATOR POSITION TRANSDUCER PER AMM 27-44-PB401; AND REPLACED ELAC SUPPLY RELAY 53CE AND RELAY PITCH TRIM ACTION MOTOR SUPPLY 36CE1. PERFORMED OPS CHECK OF THS ACTUATOR OVER TRAVEL PER AMM 27-41-00-720-001. PERFORMED CAT IIIB LAND TEST PER AMM 22-97-00-710-001. SYSTEM OPS CHECKED NORMAL. LLMP STATUS REMAINED CAT IIIB. 2L72 4F RTA28NM 20050321000822005032100082EA 2005 3 21 VTZA200500017 120050317A5320601R311719 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE SHEARED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27708BR 7575 INTERCOSTAL ON RIGHT INBOARD SIDE AT FS 484 BETWEEN BL 36.00 HAS SHEARED RIVETS. 2L72 4F RTA21EA 20050321000862005032100086NM 2005 3 21 QXEA200500483 120050314A323182420109029 PROXIMITY SENSOR BOMBDRDHC8 DHC8401 1390041NM MGL DOOR OUT OF ADJUST A QXEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM09414QX 4061 GEG - ON FLIGHT 2396 (SEA-FCA) AT CRUISE (25000 FEET) THE AFT BAGGAGE DOOR WARNING CAME ON. THERE WAS NO LOSS OF PRESSURIZATION. ACCOMPLISHED CHECKLIST, DEPRESSURIZED AIRCRAFT AND DIVERTED TO GEG, WHERE A UNEVENTFUL LANDING WAS ACCOMPLISHED. ON LANDING THE WARNING LIGHT EXTINGUISHED, THEN CYCLED ON AND OFF DURING TAXI. MAINTENANCE ADJUSTED THE DOOR LOCK PROXIMITY SENSOR. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2H72 4T RTA13NM 20050321000872005032100087NM 2005 3 21 QXEA200500372 120050202A5753 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - LEFTHAND INBOARD FLAP IS CHAFING THE UPPER WING SHROUD. REPAIRED IAW RD 8/4-57-001, ISSUE 6, PAGE 4, NOTE 9. 2H72 4T RTA13NM 20050321000902005032100090EU 2005 3 21 MALA050238 120050227A5330 SKIN BAC 146 AVRO146RJ85A1500097EU FUSELAGE DAMAGED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15535XJ E2371 THE AIRCRAFT SUFFERED DAMAGE TO THE FUSELAGE SKIN AND UNDERLYING STRUCTURE BETWEEN FRAMES 38 TO 40 AND BETWEEN 19 AND 20. THE DAMAGE WAS CAUSED BY IMPACT WITH GROUND SUPPORT EQUIPMENT. DAMAGE WAS REPAIRED IN ACCORDANCE WITH BAE REF BARA/AVR/7030/05. 2H74 4F RTA49EU 20050321000912005032100091EU 2005 3 21 MALA050250 120050302A5400 BULKHEAD BAC 146 AVRO146RJ85A1500097EU NOSE COWL CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15502XJ E2307 DURING C2 CHECK IN YYC FOUND FWD NOSE COWL BULKHEAD 2 CRACKED STIFFENERS, NR 3 ENGINE. ITEM NR 23 P/N HC716H0022-208, ITEM NR 2 P/N HC716H0022-215. 2H74 4F RTA49EU 20050321000922005032100092EU 2005 3 21 MALA050251 120050303A5347 SEAT TRACK BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15502XJ E2307 DURING C2 CHECK IN YYC FOUND RIGHT O/B SEAT RAIL BETWEEN FRAMES 44 & 45 IS CORRODED. 2H74 4F RTA49EU 20050321000942005032100094EU 2005 3 21 MALA050255 120050305A7600 CONTROL UNIT SAAB SF340 340B 7860101EU GE GE90 GE9090B NE NR 1 ENGINE MALFUNCTIONED A MALAO OTHER J WARNING INDICATION CLCLIMB 1 GL15433XJ 340B433 CLIMBING THROUGH 12800 AIRCRAFT YAWED TO THE RIGHT. RIGHT ENGINE SHOWED ZERO TORQUE, ZERO NP AND APPROXIMATELY 900 ITT. WHEN POWER WAS REDUCED RIGHT ENGINE OVERTEMP LIGHT ILLUMINATED BUT ITT REDUCED BELOW 900. OTHER ENGINE PARAMETERS APPEARED NORMAL. IGNITION LIGHT DID NOT ILLUMINATE UPON SHUTDOWN. REMOVED AND REPLACED DECU S/N ON ECDT1389, S/N OFF ECDT 1844 IAW SF340 MM 76-10-57-4. RIGHT ENGINE REPLACED RIGHT IGNITION RELAY BOROSCOPED HOT & COLD SEC OF RIGHT ENGINE, NO DAMAGE FOUND. OPS CHECK OF DECU GOOD. TORQUE AND NP GOOD. CHECK OF IGNITION LIGHT GOOD. 2L72 4T4 FRTA52EU E00049EN 20050321000962005032100096EU 2005 3 21 MALA050237 120050228A2510 SEAT BACK BAC 146 AVRO146RJ85A1500097EU COCKPIT CRACKED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15502XJ E2307 COPILOT SEAT BACK CRACKED. NO FURTHER INFO. 2H74 4F RTA49EU 20050321000972005032100097EU 2005 3 21 MALA050245 120050301A5315 FLOORBEAM BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15502XJ E2307 DURING C2 CHECK IN YYC FOUND FRAME 43, 5 INCHES LBL GUSSET CORRODED ON FLOORBEAM. MAT'L .100 INCH THICK 2024T3 AC SACLT. 2H74 4F RTA49EU 20050321000982005032100098EU 2005 3 21 MALA050256 120050307A3233 SWIVEL SAAB SF340 SF340A 7850100EU DOWNLOCK ACT BROKEN A MALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL1599XJ 340A099 JUST AFTER ROTATION GOT HYD CAUTION LIGHT ON AND MAIN PRESS DOWN TO 0 PSI. HYD QTY DECREASING FOLLOWED QRH. RETURNED TO DTW. FOUND RT DOWNLOCK ACTUATOR ROTATING SWIVEL BROKEN. REMOVED AND REPLACED SWIVEL IAW SAAB MM CHAP 32 AND BLOWN SEPARATION BOLTS WERE REPLACED IAW SAAB MM CHAP 32. ALL CHECKS GOOD. 2L72 4T RTA52EU 20050321000992005032100099NM 2005 3 21 SWAA050796 120050315A56105717623121 WINDOW BOEING737 7373Q8 1384670NM COCKPIT CRACKED A SWAAO OTHER O OTHER NRNOT REPORTED 1 SW29317WN 24068 L2 COCKPIT WINDOW ARCING & CRACKED DURING FLIGHT. REMOVED AND REPLACED L2 COCKPIT WINDOW PER MM. 2L72 4F RTA16WE 20050321001002005032100100NM 2005 3 21 SWAA050797 120050315A335010107451 SIGN BOEING737 7373H4 1384600NM MID CABIN DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29366SW 26577 LEFT OVERWING EMERGENCY EXIT SIGN FELL OFF. RE-INSTALLED SIGN PER MM. 2L72 4F RTA16WE 20050321001022005032100102 2005 3 21 SWAA050799 420050315A2565 INDICATOR BOEING737 7373H4 1384600NM ESCAPE SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 L2 DOOR EMERGENCY EVAC SLIDE INDICATOR OUT OF VIEW. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20050321001042005032100104NM 2005 3 21 SWAA050801 120050315A531165C25228 FRAME BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727C, STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050321001072005032100107NM 2005 3 21 SWAA050804 120050315A53226546569 SHEAR TIE BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 967, STR 7L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050321001082005032100108NM 2005 3 21 SWAA050805 120050315A531165C22910 FRAME BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500D, BETWEEN STR 13L & STR 14L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050321001122005032100112EA 2005 3 21 SWIA200514694 120050306A3350AD20131A BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07906SW6480 6480 7510 SERVICE DOOR EMERGENCY EXIT SIGN WILL NOT ILLUMINATE WHEN SWITCHED ON. REPLACED BATTERY PACK PER CRJ MM 33-51-04. OPERATIONAL CHECK NORMAL. 2L72 4F RTA21EA 20050321001132005032100113NM 2005 3 21 QXEA200500350 120050302A521085321986001 SEAL DHAV DHC8 DHC8202 2809007NM MAIN CABIN DOOR DIRTY A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09359PH17498 496 PDX - FLIGHT 2283 - THE FLIGHT ATTENDANT REPORTS THE MAIN CABIN DOOR IS DIFFICULT TO OPEN. MAINTENANCE INSPECTED THE AIRCRAFT AND DOOR. THE DOOR SEAL WAS CLEANED AND OPERATIONAL CHECKS WERE PERFORMED. THE CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050321001142005032100114EA 2005 3 21 SWIA200514695 120050311A2780 SENSOR CNDAIRCL600 CL6002C10 1390015EA RT SLAT MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07718SK 10184 SLAT FAULT MESSAGE PRIOR TO DEPARTURE. REPLACED RIGHT INBOARD SLAT SENSOR PER AMM 27-81-37. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050321001152005032100115NM 2005 3 21 AWXA200500331 120050124A5315654681138 FLOORBEAM BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON FLOORBEAM T-CAP AT BS 986, LBL 44, WL 208. MAINTENANCE CUT OUT DAMAGE IN FLOORBEAM T-CAP AT BS 986, FROM BL 0 TO LBL 50; FABRICATED A NEW REPLACEMENT SECTION OF T-CAP, AND 2 EACH SUPPORT ANGLES & STRAPS; INSTALLED REPAIR PARTS IAW ER 03-5310-05040-SS1. 2L72 4F RTA16WE 20050321001162005032100116NM 2005 3 21 QXEA200500371 120050202A5754 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - LEFTHAND OUTBOARD SLAT IS CHAFING THE UPPER WING SHROUD. REPAIRED IAW DHC-8 SRM 51-21-10 AND 51-25-10. 2H72 4T RTA13NM 20050321001172005032100117WP 2005 3 21 0500269885 120050302A32463910797507 WHEEL DOUG DC9 DC951 3022051WP NR 1 MLG FAILED A NWAAO OTHER O OTHER LDLANDING 1 GL01401EA 47682 ON LANDING ROLL-OUT WITH MODERATE BRAKING AND LITTLE ANTI-SKID CYCLING, THE LEFT MAIN GEAR OUTBOARD WHEEL FAILED ALLOWING TIRE DEFLATION. CREW SAFELY STOPPED THE AIRCRAFT ON THE TAXIWAY FOR INSPECTION AND THE PASSENGERS WERE TRANSPORTED TO THE TERMINAL. RUNWAY CONDITION WAS PARTIAL SNOW COVER WITH BARE SPOTS. MAINTENANCE AT DTW REPLACED THE NR 1 AND NR 2 TIRE/WHEEL ASSEMBLIES, TESTED ANTI-SKID SYSTEM, AND COMPLETED A HARD-LANDING INSPECTION. NO DAMAGE TO THE FUSELAGE OR ENGINES WERE REPORTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050321001202005032100120EA 2005 3 21 COMA0560170 120050311A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01995CA 7229 RIGHT HAND 640 FRAME CRACKED. REPAIRED IAW CRJ SRM 51-42-06, 51-42-21 AND 51-25-01. 2L72 4F RTA21EA 20050321001212005032100121SO 2005 3 21 SWIA200514696 120050311A5210 DOOR EMB 120 EMB120ER 3260203SO MAIN PAX BINDING A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07214SW 120280 MAIN CABIN DOOR VERY HARD TO OPEN AND CLOSE. ADJUSTED AND RIGGED PAX DOOR BACKSTOP SHIMS IAW EMB 120 MM 52-11-00. 2L72 4T RTA31SO 20050321001252005032100125EA 2005 3 21 SWIA200514700 120050310A3397 WIRE CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07709SK 10159 EMERGENCY EXIT SIGN ON BULKHEAD BETWEEN FIRST CLASS AND COACH INOPERATIVE. REPAIRED WIRING FOR EMERGENCY EXIT SIGN ON BULKHEAD. ALL LIGHTS CHECK GOOD. 2L72 4F RTA21EA 20050321001262005032100126EA 2005 3 21 SWIA200514701 120050301A2741 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07427SW 7497 MACH TRIM DISENGAGES EVERYTHING. REMOVED AND REPLACED STAB/MACH TRIM SWITCH PANEL. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050321001272005032100127EA 2005 3 21 SWIA200514702 120050310A335020131A BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCHARGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07433SW 7550 AFT SECTION OF EMERGENCY LIGHTS WILL NOT ILLUMINATE. REPLACED AFT EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD. P/N 2013-1A, S/N OFF 42053. 2L72 4F RTA21EA 20050321001352005032100135NM 2005 3 21 AWXA200500333 120050123A53156546812132 FLOORBEAM BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON FLOORBEAM T-CAP AT BS 1016, RBL 5, WL 208. MAINTENANCE CUT OUT DAMAGE IN FLOORBEAM T-CAP AT BS 1016, RBL 5; FABRICATED A 3 EACH REPAIR PLATES AND A FILLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-12. 2L72 4F RTA16WE 20050321001362005032100136NM 2005 3 21 AWXA200500334 120050212A532065479576 WEB BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON AFT CARGO DOOR SILL WEB BETWEEN BS 794 AND BS 799, AT STR 25 RT. MAINTENANCE REMOVED CORRODED AFT CARGO DOOR SILL WEB AT STR 25 RT, FROM BS 794 TO BS 799; FABRICATED A NEW REPLACEMENT WEB PER DWG 65-47957-6; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050321001372005032100137NM 2005 3 21 AWXA200500335 120050122A53206561777503 CHANNEL BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK A .25 INCH CRACK WAS FOUND IN STRINGER SPLICE CHANNEL AT BS 360, STR 14 LT. MAINTENANCE REMOVED CRACKED STRINGER SPLICE CHANNEL AT BS 360, STR 14 LT; FABRICATED A NEW REPLACEMENT SPLICE CHANNEL; INSTALLED REPAIR PART IAW ER 03-5300-05053-SS3. 2L72 4F RTA16WE 20050321001402005032100140NM 2005 3 21 QXEA200500484 120050315A5230 HANDLE BOMBDRDHC8 DHC8401 1390041NM CARGO DOOR UNSECURE A QXEAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 NM09409QX 4051 HLN - ON FLIGHT 2419 (BIL-SEA) FORWARD CARGO DOOR WARNING CAME ON. AIRCRAFT DIVERTED TO HLN AND ACCOMPLISHED A UNEVENTFUL LANDING. NO CFR EQUIPMENT WAS CALLED. MAINTENANCE FOUND THE HANDLE/SHAFT OF THE DOOR NOT SEATED. SEATED THE SHAFT/HANDLE, LIGHT WENT OUT. CYCLED DOOR, CHECKS OK. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2H72 4T RTA13NM 20050321001432005032100143NM 2005 3 21 QXEA200500488 120050315A5210 SEAL DHAV DHC8 DHC8202 2809007NM MAIN PAX DOOR DIRTY A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09366PH 510 SEA - ON FLIGHT 2109 FLIGHT ATTENDANT REPORTS THAT THE MAIN CABIN DOOR IS HARD TO OPEN. MAINTENANCE CLEANED DEBRIS FROM THE SEAL AREA AND LUBED THE DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2H72 4T RTA13NM 20050321001442005032100144NM 2005 3 21 QXEA200500379 120050117A5220 FITTING BOMBDRDHC8 DHC8401 1390041NM ZONE 200 CHIPPED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - ORGANIC COATING OF FORWARD PASSENGER DOOR SURROUND FITTINGS IS CHIPPED OFF. REPAIRED IAW DHC-8 400 SRM 51-14-00-350-803 AND SRM 51-28-15-370-001. 2H72 4T RTA13NM 20050321001452005032100145NM 2005 3 21 QXEA200500369 120050203A7810 SHROUD BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - LEFTHAND NACELLE AFT EXHAUST SHROUD IS CRACKED AT MID SPRING CLIPS AND AT AFT BRACKET. REPAIRED IAW RD 8/4-54-227 AND 8/4-54-009 AND HORIZON AIR EA 6-54-332. 2H72 4T RTA13NM 20050321001462005032100146WP 2005 3 21 NACA20050009 120050306A612392065 SWITCH HAMSTD DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE HAMSTD43E 43E60 NE PROPELLER BROKEN A NACAE ENGINE SHUTDOWN O OTHER TXTAXI/GRND HDL 1 AL03438722886 2886 N207939 533294 510118 N207939 NR 2 PROPELLER WOULD NOT UNFEATHER AFTER LANDING. REPLACED BROKEN BLADE SWITCH LEAD. CHECKED GOOD. 2L74 4R4 R A781 5E8 6 CP871 20050321001482005032100148EA 2005 3 21 SWIA200514704 120050308A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07912SW 7595 EXIT LIGHT AT BOARDING MAIN DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT. OPERATIONAL CHECK GOOD IAW CRJ MM CHAP 33-51-00. 2L72 4F RTA21EA 20050321001502005032100150NM 2005 3 21 UPS05544036 120050304A3350 LAMP BOEING757 75724APF 1384969NM EMERGNECY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01443UP 27388 FIVE LAMPS INOP IN EXIT LIGHT. RELAMPED EXIT LIGHT 5 EA, OPS CHECKS GOOD. 2L72 4F RTA2NM 20050321001512005032100151NM 2005 3 21 UPS05644029 120050303A5712113T1552 RIB BOEING767 76734AF 1385212NM LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01301UP 27239 INSPECTION TYPE: C LEFT WING I/B AILERON I/B HINGE RIB IS CRACKED AT UPPER TRAILING EDGE ON CHORD ATTACH FASTENERS. REPAIRED I/B AILERON I/B HINGE RIB IAW UPS ER05-1834. 2L72 4F RTA1NM 20050321001522005032100152WP 2005 3 21 UPS05844032 120050305A3350 LAMP DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 EMERGENCY LIGHTS INOP. RELAMPED, OPS CHECK GOOD. 2L74 4F RT4A25 20050321001542005032100154NM 2005 3 21 UPS05M44035 120050308A2560 SMOKE BARRIER DOUG MD11 MD11F 3023600NM COURIER COMPT TORN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01277UP 48578 INSPECTION TYPE:N/A SMOKE SCREEN ON CARGO ACCESS DOOR TORN IN THE COURIER COMPT. SECURED SLIDING RIGID CARGO BARRIER BY MD11 MM 59-16 PG 401. 2L73 4F RTA22WE 20050321001552005032100155EU 2005 3 21 RAIAOO502035 120050228A3260 SWITCH JETAIRJETSTMJETSTM4101 1500501EU NR 2 MLG DIRTY A RAIAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 CE03571HK 41090 STL - RIGHT RED BETA LIGHT CAME ON DURING TAKEOFF ROLL. MAINTENANCE CLEANED AOG SWITCH ON NR 2 MLG. 2L72 4T RTA41NM 20050321001572005032100157NM 2005 3 21 QXEA200500377 120050124A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - CABIN CENTER FLOOR SEAT TRACK NR 11 MINOR SURFACE CORROSION ON TRACK FITTING, FORWARD BAGGAGE BULKHEAD. REPAIRED IAW Q400 SRM 51-21-350-001, PARAGRAPH D. 2H72 4T RTA13NM 20050321001582005032100158CE 2005 3 21 DJFA2005063 120050302A3231MS243311 SWITCH BEECH MU300 400A 1155402CE LT MLG FALSE ACTIVATIONE DJFAO OTHER J WARNING INDICATION LDLANDING 1 EA23689TA RK327 KDET - KIND DURING APPROACH TO RUNWAY 32 IN KIND, THE GEAR HANDLE LIGHT REMAINED ILLUMINATED RED WITH ALL THREE GEAR INDICATORS SHOWING DOWN AND LOCKED. GEAR WAS CYCLED THREE TIMES WITH THE SAME RESULTS. THE TOWER HAD CONFIRMED AT LEAST ONE MAIN GEAR DOOR WAS NOT UP. EMERGENCY PROCEDURES WERE USED TO BLOW THE GEAR DOOR TO THE UP POSITION. THE PROCEDURE RESULTED IN THE GEAR HANDLE LIGHT EXTINGUISHING, AND THE DOORS BEING UP. AN UNEVENTFUL LANDING WAS MADE IN KIND. MAINTENANCE REPLACED THE LEFT MAIN GEAR DOWNLOCK SWITCH. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4F RTA16SW 20050321001592005032100159NM 2005 3 21 QXEA200500364 120050122A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - LEFTHAND SIDE OF FUSELAGE EXTERNAL SKIN AT STATION X403 TO 415 AT STRINGER 18L HAS TWO AREAS OF CORROSION. REPAIRED IAW Q400 SRM 51-42-05-380-001, 51-25-10-370-001, 51-25-15-570-001. 2H72 4T RTA13NM 20050321001602005032100160NM 2005 3 21 QXEA200500366 120050124A5410 BOOT BOMBDRDHC8 DHC8401 1390041NM ZONE 400 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - LEFTHAND BOOT TAIL PANEL 414BB MOUNTING AREA HAS SEVERAL DRILLED OFF SCREWS STUCK IN THE ANCHOR NUTS. REPLACED ANCHOR NUTS IAW TASK 51-42-35-330-801. 2H72 4T RTA13NM 20050321001612005032100161NM 2005 3 21 QXEA200500367 120050124A5414 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - LEFTHAND NACELLE LOWER AFT COWL PANEL, CHANNEL STATION XN302 IS CRACKED AT UPPER FLANGE. REPAIRED IAW RD 8/4-54-033. 2H72 4T RTA13NM 20050321001622005032100162NM 2005 3 21 QXEA200500368 120050131A5420 EJECTOR BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - LEFTHAND NACELLE AFT EXHAUST EJECTOR AFT TIP CRACKED. REPAIRED IAW RD 8/4-54-016, ISSUE 3. 2H72 4T RTA13NM 20050321001642005032100164NM 2005 3 21 QXEA200500373 120050202A5753 SHROUD BOMBDRDHC8 DHC8401 1390041NM ZONE 600 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - RIGHTHAND INBOARD FLAP IS CHAFING THE UPPER WING SHROUD. REPAIRED IAW RD 8/4-57-001, PAGE 7, NOTE 9. 2H72 4T RTA13NM 20050321001652005032100165NE 2005 3 21 DL76L050120 220050218A7297 WIRE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE RT ENGINE SHORTED A DALAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS CRCRUISE 1 SO27176DN L0172 25061 DURING CRUISE FLIGHT RIGHT ENGINE GEN DROPPED OFF LINE. FOUND FIELD WIRE SHORTED AT CSD PLUG D10966. REPAIRED SAME. 2L72 4F4 FRTA1NM E24NE 20050321001662005032100166NM 2005 3 21 DL738050123 120050220A335002019241007 LIGHT BOEING737 737832 13844CFNM 2R GALLEY BROKEN A DALAK NONE L NO TEST ININSP/MAINT 1 SO273755D 29627 GALLEY 2R EMERGENCY LIGHT DAMAGED. REPLACED LIGHT. 2L72 4F RTA16WE 20050321001682005032100168NM 2005 3 21 DL73S050125 120050220A5330 SKIN PANEL BOEING737 737247 138448DNM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27243WA 23517 THE FUSELAGE SKIN WAS FOUND WITH A 1.5 INCH LONG CRACK AT APPROX FS 727B RUNNING ALONG THE BONDED DOUBLER MILL LINE JUST BELOW STRINGER 18R. THE CRACK IS TYPICAL OF AD 2004-18-06. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER B737 SRM AND PER ER/A 097068-14AD. 2L72 4F A16WE 20050321001712005032100171NM 2005 3 21 QXEA200500381 120050128A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 200 CHIPPED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - RIGHTHAND SIDE OF FUSELAGE SKIN BETWEEN STATION X595 AND X301 HAS NUMEROUS SMALL PAINT CHIPS. REPAIRED IAW DHC-8 400 SRM 51-25-05-370-001, PARAGRAPH E AND RD 8/4-53-382, ISSUE 3, PAGE 6. 2H72 4T RTA13NM 20050321001722005032100172SO 2005 3 21 C2XA05IA040 120050304A329714526906401 WIRE HARNESS EMB 145 EMB145ER 3260211SO CENTER WING BOX INOPERATIVE A C2XAO OTHER J WARNING INDICATION DEDESCENT 1 SW2714940 145033 LFT - FLIGHT 2903, THE CREW REPORTED ON DESCENT THAT THERE WAS NO DOWN AND LOCK INDICATION ON THE RT MAIN LANDING GEAR. THE CREW DECLARED AN EMERGENCY, AND LANDED AT LFT WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE WIRE HARNESS FOR THE UPLOCK PROXIMITY SENSORS, OPERATIONALLY CHECKED THE EXTENSION/RETRACTION SYSTEM WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THIS PART IS NOT SERIALIZED, AND NO TIMES ARE AVAILABLE. 2L72 4F RTT00011AT 20050321001752005032100175SO 2005 3 21 SWIA200514667 120050307A27523430001007 ACTUATOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07584SW1127011270 120352 SELECTING FLAPS TO 15 DEGREES GOT A CONTROL FAULT. REMOVED AND REPLACED RIGHT OUTBOARD FLAP ACTUATOR IAW MM 27-50-09. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050321001792005032100179EA 2005 3 21 SWIA200514671 120050305A2760C13045BA03 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA SPOILERS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07740SK 10196 RUDDER LIMIT FAULT STATUS MESSAGE DISPLAYED ON EICAS. REPLACED NR 1 SSCU IAW CRJ 700 MM 27-61-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050321001802005032100180NM 2005 3 21 SWAA050756 120050313A534365C10300 FITTING BOEING737 7375H4 138449DNM NLG WW CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29524SW 26566 DURING SCHEDULED RON CHECK, FOUND NLG ACTUATOR UPPER ATTACH FITTING GUSSET CRACKED. REMOVED AND REPLACED GUSSET PER MM. 2L72 4F RTA16WE 20050321001812005032100181NM 2005 3 21 SWAA050757 120050313A53116546558 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29605SW 27956 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, BETWEEN STR 8R & STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050321001822005032100182NM 2005 3 21 SWAA050758 120050313A53116546555 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29605SW 27956 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, BETWEEN STR 8R & STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050321001832005032100183NM 2005 3 21 SWAA050759 120050313A53116546526 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29605SW 27956 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, BETWEEN STR 8R & STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050317000882005031700088NE 2005 3 17 2005UALA00202 220050302A7230 BEARING AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 2 ENG COMP FAILED A UALAEA ENGINE SHUTDOWN UNSCHED LANDING REJPARTIAL RPM/PWR LOSS VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 WP29425UA 508 NR 2 ENGINE COMPRESSOR STALL FOLLOWED BY OIL FILTER CLOGGED MESSAGE. SHUTDOWN ENGINE. NR 4 MAINLINE ROLLER BEARING FAILED, CAUSING ENGINE TO AUTO-SHUTDOWN. NR 4 BEARING HAD 1417 FLT HOURS FROM LAST OVERHAUL. BEARING FAILURE CONFIRMED AS CAUSED BY BEARING CAGE FAILURE. CAGE FAILURE EXACT CAUSE UNKNOWN, HOWEVER BATCH ESCAPE DURING POST-PLATING BAKE PROCEDURE HEAVILY SUSPECTED TO HAVE CAUSED HYDROGEN EMBRITTLEMENT, LEADING TO EVENTUAL FRACTURE. NO FURTHER OVERHAULED NR 4 BEARINGS WITH RE-USED CAGES WILL BE ACCEPTED BY UAL. 2L72 4F4 FRTA28NM E40NE 20050317001042005031700104NM 2005 3 17 0500246730 120050227A5311 FRAME BOEING747 747251F 1384898NM FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01640US 23888 DURING LINE CHECK FOUND CRACK IN FRAME AT BS 440 STRINGER 10L. REPAIRED PER EA 67-203062. 2L74 4F A20WE 20050317001102005031700110EA 2005 3 17 SWIA200514683 120050225A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07441SW 7602 MAIN FUSELAGE FS 280 RBL 9.0 LOWER FLANGE CRACKED ON TRANSVERSE BEAM. ITEM FOUND AT C-CHECK INSPECTION. CRACKED FLANGE REPAIRED IAW CRJ REO 601R-53-11-171 REV A. 2L72 4F RTA21EA 20050317001112005031700111EA 2005 3 17 COMA0560173 120050312A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAL ABORTED APPROACH J WARNING INDICATION DEDESCENT 1 SO01989CA 7215 FLIGHT 5116 DURING DESCENT RECEIVED A FLAP FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY. ABORTED 1ST APPROACH AT YYZ, LANDED WITHOUT INCIDENT. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE FIRST EVENT, MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2L72 4F RTA21EA 20050317001192005031700119 2005 3 17 SWAA050723 420050309A25656557463 GIRT BAR BOEING737 7373H4 1384600NM L1 DOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29607SW 27927 DURING SCHEDULED D-CHECK, FOUND CORROSION ON L1 DOOR EVAC SLIDE, FWD & AFT GIRT BAR FLOOR FITTINGS. REMOVED AND REPLACED GIRT BAR FITTINGS PER SRM. 2L72 4F RTA16WE 20050317001212005031700121NM 2005 3 17 SWAA050725 120050309A53106546817 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29607SW 27927 DURING SCHEDULED D-CHECK, FOUND CORROSION ON CREASE BEAM WEB AT BS 385, STR 17L. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM. 2L72 4F RTA16WE 20050317001262005031700126NM 2005 3 17 DHL2005781537 120050214A5755 HINGE BOEING727 727227 1384078NM SPOILER CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A C-CHECK, NR 3 SPOILER HINGE CUTOUT CRACKED (MARKED) LT WING UPPER SURFACE. REMOVED NR 3 SPOILER PANEL TO FACILITATE OTHER MAINTENANCE IAW B727 SRM 27-62-01. REMOVED FASTENERS FOR ACCESS FOR REPAIR IAW B727 SRM 57-30-4 FIG 10. CRACK TERMINATED AT FASTENER HOLE VERIFIED IAW B727 NDT MAN PTG 51-00-00 FIG 23. FABRICATED NEW REPAIR DOUBLER FROM 7075 T6 .071 PO 900573 7 X 4 INCH DIM IAW B727 SRM 57-30-4 FIG 10. TREATED AND PRIMED DOUBLER AND AREA IAW B727 SRM 51-10-2. INSTALLED DOUBLER AT NR 3 SPOILER HINGE LT WING UPPER SURFACE IAW B727 SRM 57-30-4 TIS 10. REINSTALLED NR 3 SPOILER PANEL IAW B727-MM-27-62-01. OPS CHECK GOOD IAW B727-MM-27-62-0. 2L73 4F A3WE 20050317001292005031700129EU 2005 3 17 05FDEA00492 120050310A5521 RIB AIRBUS310 A310222 3930315EU ELEVATOR DAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25446FE 224 UPON REMOVAL OF EXISTING REPAIR ON N/R N00817 ON RT ELEVATOR INBOARD T/E LWR SURFACE FOUND 2EA AREAS OF CORROSION .5 X .5 INCH 1 ON INBOARD SIDE OF REPAIR, 1 ON OUTBOARD SIDE OF REPAIR (RIB 5 AND RIB 9). REMOVED CORROSION PER A310-200 SRM 51-74-10, 1EA AREA INBOARD OF ORIGINAL REPAIR OUT OF LIMITS. REPAIR THIS AREA IAW SRM 55-21-11 CONFIG 1 FIG 203, 1EA AREA O/B OF ORIGINAL REPAIR NO MAT'L LOSS FOUND TO BE WITHIN LIMITS PER SRM 55-20-00 PB 101. APPLIED FILLER & FINISHED PER A310-200 SRM 51-75-10. 2L72 4F RTA35EU 20050317001502005031700150EA 2005 3 17 SWIA200514664 120050302A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA EXTERIOR BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07592SW 7279 ONE CEILING LEVEL EMERGENCY FLOODLIGHT INOPERATIVE. RELAMPED, OPERATIONAL CHECKS GOOD. 2L72 4F RTA21EA 20050317001522005031700152NM 2005 3 17 HNAA0500019 120050307A2930 WARNING LIGHT DHAV DHC8 DHC8102 2809003NM NR 2 HYD SYSTEM ILLUMINATED A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07815EX 321 AFTER TAKEOFF, DURING GEAR RETRACTION, NR 2 ENGINE HYD PUMP CAUTION LIGHT CAME ON. QUANTITY GOOD, GEAR RETRACTED SLOWER THAN NORMAL, 15 SECONDS OR SO, ALSO LIGHT CAME ON DURING SUBSEQUENT GEAR EXTENSION. MAINTENANCE BLEED AIR FROM SYSTEM, SERVICED HYD QUANTITY. RETURNED AIRCRAFT TO SERVICE. 2H72 4T RTA13NM 20050317001532005031700153NM 2005 3 17 QXEA200500345 120050217A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09363PH 520 PDX - RIGHTHAND OUTBOARD NR 10 SEAT TRACK HAS SURFACE CORROSION ON TOP OF LUGS AT X389 AND PITTING IN BOTTOM OF CHANNEL AT X390 TO X392. REPAIRED IAW DHC-8 202 SRM 51-40-00 AND SRM 51-40-11. 2H72 4T RTA13NM 20050317001572005031700157NM 2005 3 17 QXEA200500355 120050303A5320 BEAM BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09413QX 4060 PDX - LATERAL BEAM CORRODED AROUND GROUND POINTS, BELOW MOUNTS FOR NR 1 AND NR 2 RELAY JUNCTION BOXES. REPAIRED IAW DHC-8 400 SRM 51-21-00 AND HORIZON AIR EA 6-53-531. 2H72 4T RTA13NM 20050317001632005031700163CE 2005 3 17 DXTA200500621 120050310A2611473054 SMOKE DETECTOR RAYTHNDH125 HAWKER800XP 7150012CE CARGO BAY MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07861QS 258361 BAG FIRE LIGHT ILLUMINATED DURING CLIMBOUT AND EXTINGUISHED AFTER APPROX 10 SECS. LIGHT ILLUMINATED AGAIN AFTER A FEW MINS AND EXTINGUISHED AGAIN AFTER 10 SECS. REMOVED AND REPLACED FWD CABIN SMOKE DETECTOR. PERFORMED SMOKE DETECTION SYSTEM TEST, SYSTEM OPS CHECK GOOD. WORK DONE IAW RAYTHEON A/C HAWKER 800XP MM ADDENDA CH 26-11-00. 2L72 4F RTA3EU 20050317001742005031700174SO 2005 3 17 C2XA05SH17 120050311A532014530644403 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714950 145061 SHV - DURING C-CHECK CORROSION ON LT OMEGA BEAM I/B SIDE FWD OF FRM 44. MAINTENANCE REMOVED THE DAMAGE AREA AND PERFORMED REPAIR IAW EMB 145 SRM 53-23-10. NO FURTHER ACTION REQUIRED PER EC 5320-01219. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050317001812005031700181NM 2005 3 17 QXEA200500322 120050222A5313 STRINGER DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09363PH 520 PDX - THERE IS CORROSION ON STRINGER 33 AT APPROXIMATELY STATION X190, JUST BELOW A WIRE BUNDLE. REPAIRED IAW DHC-8-200 SRM 51-40-11, 51-20-16 AND HORIZON AIR EA 2-53-603. 2H72 4T RTA13NM 20050317001832005031700183NM 2005 3 17 QXEA200500326 120050218A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09363PH 520 PDX - RIGHTHAND OUTBOARD NR 11 SEAT TRACK HAS CORROSION ON BOTTOM OF LUG AT X455. REPAIRED IAW DHC-8 202 SRM 51-40-00 AND SRM 51-40-11. 2H72 4T RTA13NM 20050317001912005031700191NM 2005 3 17 QXEA200500329 120050217A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09363PH 520 PDX - SEAT TRACK NR 11 HAS PITTING CORROSION AT X408. REPAIRED IAW DHC-8 200 SRM 51-40-00 AND SRM 51-40-11. 2H72 4T RTA13NM 20050317001962005031700196NM 2005 3 17 05FDEA00486 120050310A5322 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25494FE 21532 SHEAR TIE AT BS 380, STR 14 NEEDS TO BE REPAIRED TO ACCOMPLISH 9G BARRIER MOD. *S/D* REPAIRED PER SRM 53-10-4. 2L73 4F RTA3WE 20050317002012005031700201NM 2005 3 17 QXEA200500319 120050226A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09413QX 4060 PDX - SEAT TRACK NR 11 HAS PITTING CORROSION AT STATION X20.0, X38.0 AND X71.0 WHICH IS EVALUATED AND DETERMINED TO BE OUT OF LIMITS. REPLACED NR 11 SEAT TRACK IAW DHC-8 400 SRM 51-42-15 AND SRM 51-42-00. 2H72 4T RTA13NM 20050317002052005031700205NM 2005 3 17 QXEA200500303 120050223A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09413QX 4060 PDX - CORROSION ON RIGHTHAND OUTBOARD SEAT TRACK AT APPROXIMATELY X540.00, TOP AND INNER FLANGE. REPLACED SEAT TRACK IAW DHC-8 SRM 51-42-15 AND SRM 51-42-05. 2H72 4T RTA13NM 20050317002312005031700231NM 2005 3 17 QXEA200500317 120050223A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09413QX 4060 PDX - CORROSION ON RIGHTHAND OUTBOARD SEAT TRACK AT APPROXIMATELY X259.00, TOP AND INNER FLANGE. REPLACED SEAT TRACK IAW DHC-8 SRM 51-42-15 AND 51-42-05. 2H72 4T RTA13NM 20050317002342005031700234NM 2005 3 17 QXEA200500313 120050223A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09413QX 4060 PDX - CORROSION ON RIGHTHAND OUTBOARD SEAT TRACK AT APPROXIMATELY X342.00, TOP AND INNER FLANGE. REPLACED SEAT TRACK IAW DHC-8 SRM 51-42-15 AND 51-42-05. 2H72 4T RTA13NM 20050317002612005031700261NM 2005 3 17 DHL2005781548 120050216A5530 STIFFENER BOEING727 727227 1384078NM VERTICAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A C-CHECK, VERT STAB FIN STA 180, STR 5-8 RT IS CRACKED AT FRAME ATTACH BOLT. REMOVED FASTENERS FOR ACCESS, CUT OUT DAMAGED STIFFENERS AND REMOVED FILLER IAW B727 SRM 55-30-4 FIG 1 (5 X 3). FABRICATED STIFFENER REPAIR P/N BAC1517-1367 PO 501953 DIM 5 X 3 INCH SPLICE P/N AND 10134-1201 PO 501952 DIM 19 X 2.25 FILLER MAT'L 7075-T6 .100 PO 501952 DIM 19 X .25 INCH CLIP P/N AND 10133-1401, FILLER P/N 7075-T6 .090 PO 501952. TREATED, PRIMED STIFFENER, AND AREA IAW B727 SRM 51-10-2. INSTALLED STIFFENER IAW B727 SRM 55-30-4 FIG 1. 2L73 4F A3WE 20050318000032005031800003EA 2005 3 18 SWIA200514706 120050121A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07461SW 7811 LEFT SIDE FS 621.00 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR PARTS IAW REO 601R-53-61-117 REV B. 2L72 4F RTA21EA 20050318000142005031800014WP 2005 3 18 UPS05844111 120050215A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE:C1 LONG 14L CRACKED NEAR STA 1760. REMOVED LONG SECTION FROM 1746-1766. REMOVED SHEAR TIE AT 1757. FABRICATED REPLACEMENT LONG SECT FROM EXTRUSION S1616757, 2 SPLICE STRAPS (SHT7075-T6 .080), REPAIR SPLICE (S2645716 EXTRUSION) ON SERVICE ORDER 7034945 & INSTALLED ALL PARTS REF DWG DC8-53B-009, SRM 53-2-2 FIG 10, 51-1-21, 51-1-20D, 51-1-8, NDTSPM06-10-01.001, DPS4.707. 2L74 4F RT4A25 20050318000152005031800015WP 2005 3 18 UPS05844112 120050219A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE:C1 LONGERON 15L CRACKED NEAR STA 1760. REMOVED LONG FROM STA 1739-1766, SHEAR TIE AT STA 1746, END FITTING AT STA 1766. FABRICATED REPLACEMENT LONG SECTION (S1616756 EXTRUSION), REPAIR SPLICE ON SERVICE ORDER 7034944 (S2645716 EXTRUSION), 2 SPLICE STRAPS (SHT7075T6-.080) INSTALLED ALL PARTS REF SRM53-2-2 FIG 10, DWG DC8-53B -009, 51-1-21, 51-1-20D, 51-1-8, NDTSPM06-10-01.001, DPS4.707. 2L74 4F RT4A25 20050318000222005031800022WP 2005 3 18 UPS05844121 120050221A5310 ANGLE DOUG DC8 DC873F 302199FWP DOOR FRAME CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE:C1 ANGLE CRACKED INSIDE L1 DOOR JAMB AT STA 35. NDT VERIFIED CRACK TERMINATED AT FASTENER HOLE. FAB REPAIR DOUBLER FROM SHT2027T3-.063. TREAT, PRIME, INSTALL REPAIR REF SRM 51-1-21, 51-1-8, 51-3-0, 53-2-0 FIG 1B, 51-1-21A, DWG 5597646. 2L74 4F RT4A25 20050318000252005031800025EA 2005 3 18 COMA0560179 120050314A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01963CA 7127 FLIGHT 5210 LEFT THRUST REVERSER UNLOCKED MESSAGE. DEFERRED MAINT ON T/R PER MEL. 2L72 4F RTA21EA 20050318000402005031800040 2005 3 18 SWIA200514711 420050312A3418C818022 SERVO EMB 120 EMB120ER 3260203SO STICK SHAKER INOPERATIVE A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07563SW1128111281 120338 CAPTAINS STICK SHAKER IS INOPERATIVE. REPLACED CAPTAINS STICK SHAKER. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050318000522005031800052SO 2005 3 18 PNSA050301 120050309A323096382 COUPLING GRUMAVG21 G21A 3951204SO MLG BROKEN E PNSALA ABORTED APPROACH UNSCHED LANDING S AFFECT SYSTEMS DEDESCENT 1 AL03741 B97 LT MAIN LANDING GEAR WOULD NOT RETRACT OR EXTEND. HUNG UP IN MID TRAVEL. DOVE AIRCRAFT AND PERFORMED SUDDEN PULL UP AND LANDING GEAR WENT TO DOWN AND LOCK POSITION. AIRCRAFT RETURNED TO DUT AND MADE A NORMAL LANDING. MAINTENANCE FOUND LT WORM GEARBOX COUPLING BROKEN. REPLACED COUPLING AND PERFORMED GEAR SWINGS WITH NORMAL OPERATION. 1H72 3R TC654 20050321000012005032100001 2005 3 21 SWAA050812 420050316A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF HOUSING. SLIDE DID NOT DEPLOY. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20050321000122005032100012NM 2005 3 21 SWAA050823 120050316A53306545767 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 420, STR 26L. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050321000132005032100013NM 2005 3 21 SWAA050824 120050316A53226546546 SHEAR TIE BOEING737 737317 138447PNM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29686SW 23175 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON SHEAR TIE AT BS 747, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050321000152005032100015EU 2005 3 21 MALA050257 120050309A3350 POWER SUPPLY SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A MALAK NONE O OTHER ININSP/MAINT 1 GL15414XJ 340B414 DURING CAPACITY CHECK, EMERGENCY POWER SUPPLIES 21LN AND 24LN FAILED CAPACITY CHECK. REMOVED AND REPLACED EMERGENCY POWER SUPPLIES 21LN AND 24LN. OPS CHECKS GOOD. 2L72 4T RTA52EU 20050321000232005032100023EU 2005 3 21 MALA050248 120050301A5414 STIFFENER BAC 146 AVRO146RJ85A1500097EU NR 4 ENG COWL CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15502XJ E2307 DURING C2 CHECK IN YYC FOUND NR 4 ENGINE FWD NOSE COWL BULKHEAD 4 CRACKED STIFFENERS. ITEM 5 P/N HC716H0022-219, ITEM 6 P/N HC716H0022-208, ITEM 22 P/N HC716H0022-230. ITEM 31 P/N HC716H0022-214. 2H74 4F RTA49EU 20050321000262005032100026EU 2005 3 21 MALA050241 120050301A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15445XJ 340B445 FUSELAGE SKIN IS CHAFED OUT OF LIMITS AT THE AFT END OF PANEL 192AR. DAMAGE IS ACCEPTABLE IAW MESABA EO S53288. REF: EAMS WORK ORDER 211770 TASK 1509. 2L72 4T RTA52EU 20050321000382005032100038NM 2005 3 21 SWAA050809 120050315A53116546541 FRAME BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND 2 EA FUSELAGE FRAME CRACKS AT BS 663, STR 3L & STR 3R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050321000402005032100040NM 2005 3 21 SWAA050811 120050315A53156546809 FLOORBEAM BOEING737 7373H4 1384600NM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29654SW 28399 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 945, LBL 12. REPAIRED BEAM PER SRM. 2L72 4F RTA16WE 20050321000432005032100043NM 2005 3 21 AALA20050202 120050316A3350 LIGHT BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21657AM 24615 DFW - EMERGENCY LIGHT AT SEAT 18D INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 18D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050321000462005032100046GL 2005 3 21 CHQA200500051 220050310A7200 ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 2 UNSERVICEABLE A CHQAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 GL11576RP1353 1353 14500856 CAE312693 FLIGHT 6236 MCO-GSO - AT APPROXIMATELY 400 FEET A LAV SMOKE MESSAGE APPEARED ON EICAS. THE TOWER WAS ALERTED AND AFTER TWO MINUTES THE MESSAGE DISAPPEARED. THE FLIGHT ATTENDANT FOUND NO EVIDENCE OF SMOKE OR FIRE ANYWHERE IN THE CABIN. THE AIRCRAFT RETURNED TO FIELD AND LANDED UNEVENTFULLY. FIRE TRUCKS MET THE AIRCRAFT AND SWEPT FOR HOT SPOTS. NO EVIDENCE OF SMOKE, HEAT, OR FIRE WERE FOUND. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE IAW EMB 145 JC CE72-00-01. OPS CHECK GOOD IAW EMB 145 AMM 71-00-01-910-801-A. NO INDICATION OF SMOKE WAS NOTED. 2L72 4T4 FRTT00011ATTE6CH 20050321000472005032100047SO 2005 3 21 CHQA200500050 120050310A335066367 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11272SK 145306 EMERGENCY FLOOR PROXIMITY LIGHTING IS INOP AT SEATS 8 AND 9. REMOVED AND REPLACED FLOOR LIGHT STRIP IAW EMB 145 AMM 33-50-12. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050321000682005032100068WP 2005 3 21 DHL2005801003 120050317A5270 SWITCH DOUG DC8 DC873F 302199FWP LT MLG DOOR MALFUNCTIONED A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01801DH 46033 UPON GEAR RETRACTION, DOOR NOT LOCKED LIGHT ON. RAN PROCEDURE, LIGHT OUT. ALSO, LIGHT ON S/O PANEL, LT DOOR UNSAFE. CLEANED & SECURED CONNECTOR FOR LT MAIN GEAR DOOR IND SWITCH. OPS CHECK OK IAW MM 32-60-00. 2L74 4F RT4A25 20050321000712005032100071EU 2005 3 21 MALA050266 120050312A5315 FLOORBEAM SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15433XJ 340B433 DURING 4Y/2Y CHECK IN BNA FOUND FLOOR FRAME AT STA 258.0 IS CORRODED. REPAIRED AFTER CORROSION REMOVAL REF SRM 53-70-30-2. 2L72 4T RTA52EU 20050321000732005032100073EU 2005 3 21 MALA050264 120050315A5250 DOOR SAAB SF340 340B 7860101EU COCKPIT MALFUNCTIONED A MALAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 GL15415XJ 340B415 ON TAKEOFF ROLL, THE COCKPIT DOOR POPPED OPEN. LOW SPEED ABORT. CLOSED AND LOCKED DOOR. NO FURTHER INFO AT THIS TIME. RESECURED DOOR. 2L72 4T RTA52EU 20050321000852005032100085NM 2005 3 21 QXEA200500485 120050315A2150 CONTROL UNIT DHAV DHC8 DHC8202 2809007NM CABIN TEMP MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09365PH 526 SEA - ON FLIGHT 2107, UNABLE TO CONTROL CABIN TEMP IN AUTO MODE. RAN CHECKLIST, STILL UNABLE TO CONTROL IN AUTO MODE. MANUAL MODE WORKS NORMALLY. PLACED ON MEL 350350. 2H72 4T RTA13NM 20050321000892005032100089 2005 3 21 MALA050239 420050228A34206227713004 DISPLAY SAAB SF340 340B 7860101EU COCKPIT MALFUNCTIONED A MALAA UNSCHED LANDING O OTHER CRCRUISE 1 GL15414XJ 340B414 INFLIGHT BOTH LT AND RT EFFIS DISPLAYS FLICKERED ON AND OFF. AT ONE POINT UNABLE TO NAVIGATE. LT PITOT HEAT FAILED. AIR RETURN TO BNA. COULD NOT DUPLICATE. REMOVED AND REPLACED NR 2 DPU AS PRECAUTION ON ON 622-7713-004. S/N ON 4767, S/N OFF 6667. NR 2 DPU/EFIS SYS. OPS CHECK GOOD IAW SF340 MM CHAPTER 34. 2L72 4T RTA52EU 20050321000932005032100093EU 2005 3 21 MALA050252 120050301A3150 WARNING LIGHT BAC 146 AVRO146RJ85A1500097EU COCKPIT ILLUMINATED A MALAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL15508XJ E2318 REPOSITIONED AIRCRAFT OFF ACTIVE RUNWAY DUE TO A CAPT RED MASTER WARNING FLASHER ILLUMINATED DURING CONFIG CHECK. CYCLED MWS DIMMER SWITCH TO OVERRIDE POSITION AS REQUIRED PER MEL 33-20-2B. CHECKS GOOD. 2H74 4F RTA49EU 20050321001052005032100105NM 2005 3 21 SWAA050802 120050315A53116546548 FRAME BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050321001062005032100106NM 2005 3 21 SWAA050803 120050315A53126546568 BULKHEAD BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND 4 EA CRACKS AT BS 1016 PRESS BULKHEAD, STR 7L, STR 15L, STR 23R & DOME CAP. REPAIRED PRESS BULKHEAD PER PAE ER. 2L72 4F RTA16WE 20050321001092005032100109EA 2005 3 21 SWIA200514691 120050314A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY MALFUNCTIONED A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07928SW 7701 WHEN POWERING UP A/C, GOT CARGO SMOKE WARNINGS. REPLACED FORWARD SMOKE DETECTOR IN CARGO COMPARTMENT. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050321001112005032100111EA 2005 3 21 SWIA200514693 120050311A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLT SPOILERS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07590SW5159 5159 7077 SPOILERON FAULT STATUS MESSSAGE. REPLACED RIGHT WING SPOILERON (OUTBOARD) PCU IAW MM 27-64-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050321001222005032100122SO 2005 3 21 SWIA200514697 120050308A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT DISCHARGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07214SW6010 6010 120280 AFT SECTION EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED LIGHT BATTERY PACK FOR AFT SECTION. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050321001242005032100124EA 2005 3 21 SWIA200514699 120050311A2750766389L CONTROLLER CNDAIRCL600 CL6002C10 1390015EA SLAT/FLAP MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 NM07718SK 10184 FLAP HALFSPEED STATUS MESSAGE ON APPROACH & LANDING. REMOVED AND REPLACED FECU IAW CRJ 700 MM 27-51-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050321001342005032100134NM 2005 3 21 AWXA200500332 120050212A532069432332 ANGLE BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON AFT CARGO DOOR SILL ATTACH ANGLE AT BS 847, BETWEEN STR 24 RT AND STR 25 RT. MAINTENANCE REMOVED CORRODED AFT CARGO DOOR SILL ATTACH ANGLE AT BS 847, FROM STR 24 RT TO STR 25 RT; FABRICATED A NEW REPLACEMENT ATTACH ANGLE PER DWG 69-43233; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050321001472005032100147EA 2005 3 21 SWIA200514703 120050309A5610 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07936SW 7726 F/O'S SIDE WINDOW CRACKED TOP TO BOTTOM. REMOVED AND REPLACED F/O'S SIDE WINDOW IAW CRJ 200 MM ATA CHPT 56-12-01. P/N OFF 601R33033-12, S/N OFF 05T4TH9290. 2L72 4F RTA21EA 20050321001532005032100153NM 2005 3 21 UPS05M44033 120050306A2560 SMOKE GOGGLES DOUG MD11 MD11F 3023600NM COCKPIT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01272UP 48571 CAPTS SMOKE GOGGLES ARE CRACKED. REMOVED AND REPLACED CAPTS SMOKE GOGGLES IAW MM11 AMM CH 35-13-03. 2L73 4F RTA22WE 20050321001632005032100163NM 2005 3 21 QXEA200500365 120050124A5320 CHANNEL BOMBDRDHC8 DHC8401 1390041NM ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - CENTER WING, PANEL 262FT FORWARD GANG CHANNEL HAS MINOR FRETTING. REPAIRED IAW RD 8/4-451, ISSUE 1. 2H72 4T RTA13NM 20050321001672005032100167NE 2005 3 21 DL76L050124 220050221A7200PW40603 ENGINE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 2 STALLED A DALAA UNSCHED LANDING ERJVIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SO27186DN45912 27962 724415 RIGHT ENGINE STALLED DURING CLIMB, BUT CONTINUED TO OPERATE. DIVERTED FLT TO LGW. REPLACED ENGINE. 2L72 4F4 FRTA1NM E24NE 20050321001692005032100169NM 2005 3 21 DL73S050126 120050220A5330 SKIN BOEING737 737247 138448DNM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27243WA 23517 THE FUSELAGE SKIN WAS FOUND WITH A 1.2 INCH CRACK NEAR FS 767, RUNNING ALONG THE BONDED DOUBLER MILL LINE JUST ABOVE STRINGER 19R. THE CRACK IS TYPICAL OF AD 2004-18-06. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER B737 SRM AND ER/A 097069-14AD. 2L72 4F A16WE 20050321001702005032100170NE 2005 3 21 DL76L050127 220050223A7200PW40603 ENGINE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 2 SURGES A DALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SO27173DN50332 24800 724147 DURING T/O FROM ATL, NR 2 ENGINE SURGED APPROX 5 TIMES. AIRCRAFT RETURNED TO ATL. REPLACED ENGINE. 2L72 4F4 FRTA1NM E24NE 20050321001772005032100177SO 2005 3 21 SWIA200514669 120050303A3350 LIGHT EMB 120 EMB120ER 3260203SO CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07190SW 120050 AFT SECTION OF EMERGENCY LIGHTS WILL NOT ILLUMINATE. REPLACED AFT OVERHEAD LIGHT SOCKET AS NECESSARY, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050321001842005032100184 2005 3 21 SWAA050760 420050312A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29458WN 33857 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. RE-INSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20050321001862005032100186 2005 3 21 SWAA050762 420050311A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29344SW 24152 L2 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATING LOW. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20050321001872005032100187EA 2005 3 21 SWIA200514672 120050301A3350 LIGHT CNDAIRCL600 CL6002C10 1390015EA SERVICE DOOR BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07738SK 10195 RIGHT LOWER EMERGENCY FLOOD LIGHT NEXT TO SERVICE DOOR IS BROKEN. REMOVED AND REPLACED EMERGENCY FLOOD LIGHT FIXTURE ON AFT GALLEY PARTITION. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050321001882005032100188NM 2005 3 21 AALA20050197 120050314A3350 WIRE BOEING737 737823 13844BZNM EMERGENCY LIGHT BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21971AN 29547 DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT 17D INOPERATIVE. REPAIRED BROKEN WIRE AT SEAT 17D FOR THE SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20050321001952005032100195SO 2005 3 21 SWIA200514674 120050308A27523430001005 ACTUATOR EMB 120 EMB120ER 3260203SO TE FLAP LEAKING A SWIAO OTHER F FLT CONT AFFECTED LDLANDING 1 NM07560SW1144411444 120334 ON LANDING BLUE SIDE HYDRAULICS FAILED WITH FLAPS 15 DEGREES. REPLACED LEFT INBOARD FLAP ACTUATOR IAW AMM 27-50-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050321001972005032100197EA 2005 3 21 SWIA200514676 120050306A2741 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 NM07427SW 7497 RECEIVED STAB TRIM MESSAGE CLIMBING THROUGH 1000 FT AGL. INSTALLED A SERVICEABLE HSTCU COMPUTER IAW CRJ MM27-70-00-720-801. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050321001992005032100199 2005 3 21 SWIA200514678 420050305A3418C818022 SERVO EMB 120 EMB120ER 3260203SO STICK SHAKER INOPERATIVE A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07289YV 120289 SHAKER DOES NOT WORK WHEN F/O'S STALL WARNING SYSTEM IS TESTED. REPLACED F/O STICK SHAKER WITH SERVICEABLE UNIT, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050321002012005032100201NM 2005 3 21 QXEA200500362 120050307A5210 MECHANISM DHAV DHC8 DHC8202 2809007NM PAX DOOR LACK OF LUBE A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09345PH18225 476 SEA - FLIGHT 2275 - THE CABIN DOOR WAS DIFFICULT TO OPEN FROM THE INSIDE OF THE AIRCRAFT. MAINTENANCE CLEANED AND LUBRICATED THE MAIN CABIN DOOR OPENING MECHANISM. MAINTENANCE PERFORMED MULTIPLE CYCLES OF OPENING THE DOOR. ALL OPERATIONS TESTED NORMAL AND NO DEFECTS WERE NOTED. AIRCRAFT GOOD FOR SERVICE. 2H72 4T RTA13NM 20050321002022005032100202SO 2005 3 21 RAIA00502032 120050227A326023092900001 UPLOCK EMB 145 EMB145LR 3260212SO NLG INOPERATIVE A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03814HK1473717 145046 NOSE LANDING GEAR WILL NOT RETRACT. MAINTENANCE REMOVED AND REPLACED NLG UPLOCK BOX. 2L72 4T RTT00011AT 20050321002032005032100203SO 2005 3 21 RAIA00502033 120050228A21201453607401 DUCT EMB 145 EMB145LR 3260212SO PRECOOLER LEAKING A RAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03810HK 145231 PIT - BLEED 2 LEAK INDICATION. MAINTENANCE REMOVED AND REPLACED THE NR 2 PRECOOLER AND PRECOOLER DUCT. 2L72 4T RTT00011AT 20050321002052005032100205NE 2005 3 21 RAIA00503001 220050303A732131059007 FUEL CONTROL JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114GR 01514NE LT ENGINE MALFUNCTIONED A RAIAD RETURN TO BLOCK XJ ENGINE FLAMEOUT WARNING INDICATION TXTAXI/GRND HDL 1 CE03568HK5370 190 41086 76082 BWI - LEFT ENGINE OIL PRESSURE DROPPED. MAINTENANCE TROUBLESHOT AND FOUND LOSS OF OIL PRESSURE DO TO LOSS OF POWER. REMOVED AND REPLACED NR 1 FUEL CONTROL UNIT. 2L72 4T4 TRTA41NM E18NE 20050321002062005032100206 2005 3 21 RAIA00503002 420050305A34177000700967 ADC JETAIRJETSTMJETSTM4101 1500501EU NR 1 INOPERATIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03559HK1687314 41075 STL - NR 1 ADC FAIL MESSAGE. MAINTENANCE REMOVED AND REPLACED NR 1 ADC. 2L72 4T RTA41NM 20050321002072005032100207EU 2005 3 21 RAIA00503003 120050308A3060 HEATER JETAIRJETSTMJETSTM4101 1500501EU MCAULY5JFR36B5JFR36C1103GL PROPELLER FAILED A RAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03562HK9949 1053 41078 951371 RIC - LT PROP HEAT FAIL. MAINTENANCE REMOVED AND REPLACED NR 1 PROP. 2L72 4T RTA41NM 6 CP15NE 20050321002092005032100209EA 2005 3 21 ASOA05020 120050108A2560111RJ7001 GLOWSTRIP CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE CABIN DAMAGED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27703EV 10038 DURING HANGAR MAINTENANCE, THE EMERGENCY FLOOR LIGHT STRIP AFT OF ROW 12-C WAS FOUND NEEDING REPLACEMENT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY PHOTO LUMINESCENT STRIP AFT OF ROW 12-C. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA EOOO63EN 20050321002112005032100211EA 2005 3 21 ASOA05022 120050109A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27832AS 7243 DURING A GROUND INSPECTION, THE EMERGENCY CEILING LIGHT AT ROW 14 A/B WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVE AND REPLACED THE EMERGENCY CEILING LIGHT LAMP AT ROW 14 A/B. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050321002132005032100213EU 2005 3 21 ASOA05032 120050115A3397M2275941229 WIRE AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE CABIN BROKEN A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27634AS 370 DURING A GROUND INSPECTION, THE EMERGENCY FLOOR TRACK LIGHT AT ROW 14 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE TO THE EMERGENCY FLOOR TRACK LIGHT AT ROW 14. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2H72 4T4 TRTA53EU E20NE 20050321002172005032100217EA 2005 3 21 ASOA05044 120050118A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27903EV 7621 DURING A C-CHECK, THE LT AND RT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LT AND RT FLOOR SUPPORT ANGLES AT FS 621 IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050321002182005032100218EA 2005 3 21 ASOA05048 120050119A3260 WARNING SYSTEM CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE COCKPIT MALFUNCTIONED A ASOAK NONE N FALSE WARNING CLCLIMB 1 SO27713EV 10081 DURING TAKEOFF, THE CREW RECEIVED A GEAR DISAGREE WARNING. THE QRH WAS COMPLIED WITH AND THE LANDING GEAR WAS RECYCLED. ALL INDICATIONS SHOWED GREEN (UP AND LOCKED). WITH ALL INDICATIONS SHOWING NORMAL, THE FLIGHT CONTINUED. AN EMERGENCY WAS DECLARED AS A PRECAUTION AND THE AIRCRAFT LANDED SAFELY. MAINTENANCE INTERROGATED THE PROXIMITY SENSOR ELECTRONIC UNIT THROUGH THE MAINTENANCE DIAGNOSTIC COMPUTER WITH NO FAULTS FOUND AND ALSO SWUNG THE LANDING GEAR NUMEROUS TIMES WITH NO FAULTS FOUND. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA EOOO63EN 20050321002192005032100219EA 2005 3 21 ASOA05057 120050121A5260601R3198067 STEP BOMBDR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27886AS 7531 DURING HANGAR MAINTENANCE, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN AT THE ATTACH LINK. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050321002232005032100223EA 2005 3 21 ASOA05043 120050118A324450105711 TIRE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT MLG DAMAGED A ASOAK NONE C F.O.D. TOTAKEOFF 1 SO27859AS 7421 AFTER DEPARTING, THE CREW WAS ADVISED THAT THE MLB TOWER HAD FOUND TIRE DEBRIS ON THE RUNWAY AND SUSPECTED IT WAS FROM THEIR AIRCRAFT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT CONTINUED ON, LANDING SAFELY UPON ARRIVAL. MAINTENANCE FOUND DAMAGE TO THE RT IB TIRE WHICH APPEARED TO BE CAUSED FROM A LARGE NAIL. MAINT REMOVED AND REPLACED THE RT IB AND RT OB MAIN TIRE AND WHEEL ASSEMBLIES. NO FURTHER DAMAGE WAS NOTED. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050321002262005032100226EA 2005 3 21 ASOA05037 120050118A5320601R31171179 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27903EV 7621 DURING A C-CHECK, THE LT AND RT FS484 INTERCOSTAL AFT CLIPS OB WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LT AND RT FS 484 INTERCOSTAL AFT CLIPS OB IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050321002272005032100227EA 2005 3 21 ASOA05009 120050102A5260601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27826AS 7210 7210 DURING A C-CHECK, THE LOWER STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE LOWER STEP ON THE PASSENGER DOOR. (K) 2L72 4F4 FRTA21EA E15NE 20050321002282005032100228EA 2005 3 21 ASOA05008 120050102A3350BR9279106 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN DAMAGED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27826AS 7210 DURING A C-CHECK, THE EMERGENCY EXIT LIGHT COVER AND BASE BY THE SERVICE DOOR WAS FOUND DAMAGED. MAINTENANCE IS REMOVING AND REPLACING THE EMERGENCY EXIT LIGHT ASSEMBLY BY THE SERVICE DOOR. (K) 2L72 4F4 FRTA21EA E15NE 20050321002302005032100230EA 2005 3 21 ASOA05012A 120050104A52106003806111 PLATE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27823AS 7196 DURING A C-CHECK, THE PASSENGER DOOR FORWARD CABLE ANCHOR FITTING AND PLATE WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE PASSENGER DOOR FORWARD CABLE ANCHOR FITTING AND PLATE. (K) 2L72 4F4 FRTA21EA E15NE 20050321002332005032100233EA 2005 3 21 ASOA05080S 120050124A3260D3899926WD18PN CONNECTOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT MLG DIRTY A ASOAK NONE N FALSE WARNING APAPPROACH 1 SO27879AS 7600 DURING APPROACH, UPON GEAR EXTENSION THE CREW RECEIVED A LT MAIN GEAR DISAGREE MESSAGE WITH AN ASSOCIATED (GEAR DISAGREE) EICAS WARNING. THE CREW INITIATED A CLIMB TO PATTERN ALTITUDE TO RUN THE CHECK LISTS AND THEN HEARD A THUD FOLLOWED BY THE LT MLG COMING DOWN AND LOCKING, ALONG WITH THE GEAR DISAGREEMENT AND ASSOCIATED WARNINGS EXTINGUISHING. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY. MAINTENANCE CLEANED THE CONNECTOR PLUGS ON THE UPLOCK AND DOWNLOCK SENSORS AND ALSO PERFORMED SEVERAL GEAR EXTENSIONS AND RETRACTIONS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050321002372005032100237EU 2005 3 21 ASOA05084 120050111A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27534AS 463 DURING A C-CHECK, THE LT SEAT TRACK BETWEEN FR 39 AND 41 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LT SEAT TRACK BETWEEN FR 39 AND 41 IAW SRM. (K) 2H72 4T4 TRTA53EU E20NE 20050321002382005032100238EA 2005 3 21 ASOA05047 120050119A32344622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NLG MALFUNCTIONED A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27846AS7445 7328 DURING TAKEOFF, UPON GEAR RETRACTION, A LOUD NOISE FROM THE NOSE GEAR WAS NOTICED ACCOMPANIED BY A MOMENTARY (DISAGREE) WARNING AND TRIPLE CHIME. THE NOISE CONTINUED FOLLOWED BY THE NOSE GEAR RETRACTING WITH ALL INDICATIONS SHOWING NORMAL. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DEPARTURE, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR PRIORITY VALVE. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050321002412005032100241EU 2005 3 21 ASOA05095 120050112A5320 INTERCOSTAL AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27534AS 463 DURING A C-CHECK, THE INTERCOSTAL BETWEEN FR 36 TO 38 ON THE LT SIDE WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTAL BETWEEN FR 36 TO 38 ON THE LT SIDE IAW SRM. (K) 2H72 4T4 TRTA53EU E20NE 20050321002422005032100242EA 2005 3 21 ASOA05050 120050120A5260601R3198067 STEP BOMBDR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27860AS 7433 7433 DURING A GROUND INSPECTION, THE PASSENGER DOOR BOTTOM STEP WAS FOUND BROKEN AT THE FORWARD ATTACH ROD. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP WAS FOUND BROKEN AT THE FORWARD ATTACH ROD. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050321002482005032100248EA 2005 3 21 ASOA05049 120050120A2910AS115060120 HYDRAULIC LINE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE HYDRAULIC SYS LEAKING A ASOAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SO27718EV 10095 DURING APPROACH, AT APPROXIMATELY 300 FT CREW RECEIVED A MASTER CAUTION SINGLE CHIME. EICAS SHOWED HYDRAULIC 2 LOW PRESSURE. PARKING BRAKE-BRAKE PRESSURE. RT THRUST REVERSER INOP, ALONG WITH FLIGHT SPOILER DEPLOY ADVISORY MESSAGES. HYDRAULIC SYNOPTIC PAGE SHOWED 35 PERCENT QUANTITY AND SYSTEM PRESSURE SHOWED ZERO WITH BOTH PUMPS OPERATING. FLIGHT CONTROL PAGE SHOWED IB FLIGHT SPOILERS TO BE SLIGHTLY DEPLOYED WITH NO DEGRADATION OF AC CONTROLLABILITY. DUE TO INSUFFICIENT FUEL CREW DECLARED AN EMERGENCY AND DIVERTED, LANDING SAFELY. MAINTENANCE PERFORMED TEMPORARY REPAIR BY REMOVING AND REPLACING THE NR 2 ELECTRIC HYDRAULIC PUMP LINE IAW REO. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050321002492005032100249EU 2005 3 21 ASOA05091 120050113A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27534AS 463 DURING A C-CHECK, THE LT IB SEAT TRACK BETWEEN FR 13 TO 17 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LT IB SEAT TRACK BETWEEN FR 13 TO 17 IAW SRM. (K) 2H72 4T4 TRTA53EU E20NE 20050321002512005032100251EA 2005 3 21 ASOA05055 120050121A3350OL3071BPEGPL LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27861AS11300 7445 DURING A C-CHECK, THE EMERGENCY EXIT LIGHT BY THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE IS REMOVING AND REPLACING THE EMERGENCY EXIT LIGHT LAMP BY THE SERVICE DOOR. (K) 2L72 4F4 FRTA21EA E15NE 20050321002542005032100254EA 2005 3 21 A6WA200540080 120050223A2120 ODOR CNDAIRCL600 CL6002B19 1900309EA CABIN DETECTED A A6WAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL31419AW 7633 STRONG ODOR OF EXHAUST NOTED WHEN THRUST LEVERS ADVANCED. OPERATED PACKS AND COULD SMELL FAINT ODOR OF DIESEL. OPERATED PACKS ON APU FOR SEVERAL MINUTES, ODOR FADED. BELIEVE AIRSTART CART INGESTED ITS OWN EXHAUST. OPERATED PACKS ON BOTH ENGINES, ODOR DID NOT RETURN, AMM 21-51-00. (M) 2L72 4F RTA21EA 20050321002552005032100255EA 2005 3 21 A6WA200540086 120050304A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31407AW 7424 THE LEFT AND RIGHT INTERCOSTAL ATTACH ANGLES/CLIPS ARE CRACKED .25 INCH AT LBL 27 AND RBL 27, FS 484, WL 73. (M) REMOVED CRACKED ANGLES AT FS 484, RBL 27 AND LBL 27. INSTALLED NEW ANGLES, IAW SRM AND BRAS STD REP. (K) 2L72 4F RTA21EA 20050321002562005032100256 2005 3 21 A6WA200540079 420050223A22106229968001 YAW DAMPER CNDAIRCL600 CL6002B19 1900309EA VERTICAL STAB DEFECTIVE A A6WAO OTHER F FLT CONT AFFECTED DEDESCENT 1 GL31413AW 7585 ON DESCENT THROUGH 9000 FEET, LOUD REPEATED BANGING SOUND FROM AIRCRAFT. COMBINED WITH SHARP REPEATED LEFT YAW MOTIONS. C/W SECU CHECKS, SPOILER AND SPOILERON CHECKS. CHECKED HYD SYSTEM HEAT EXCHANGER. CHECKED RUDDER AND RUDDER TRIM SYSTEM. COMPLIED WITH ACCEL AND DECCEL ENGINE CHECKS AND C/W VIBE CHECKS. FOUND INTERMITTENT FAILING YAW DAMP ACTUATOR NR 2. REMOVED AND REPLACED YAW DAMP ACTUATOR NR 2. (M) 2L72 4F RTA21EA 20050321002572005032100257EA 2005 3 21 A6WA200540081 120050225A56101393222 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A A6WAA UNSCHED LANDING O OTHER CLCLIMB 1 GL31455AW 7848 FIRST OFFICER FORWARD WINDSHIELD OUTER PANEL ONLY SHATTERED FAILURE OCCURRED AT 31,000 FT ON CLIMB-OUT. COMPLIED WITH QRH UNEVENTFUL LANDING SYRACUSE. REMOVED AND REPLACED FIRST OFFICERS WINDSHIELD REF MM 56-11-01. PRESSURIZED AIRCRAFT, OPS CHECK GOOD. (M) 2L72 4F RTA21EA 20050321002582005032100258NM 2005 3 21 AMTA200500187 120050216A2560 CONNECTOR BOEING757 75733N 1384931NM OVERWING ESCAPE LOOSE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11555TZ 32589 OVERWING ESCAPE BOTTLE PRESSURE WOULD NOT TEST. RESECURED CANNON PLUGS TO BOTTLES. TEST NORMAL. (M) 2L72 4F RTA2NM 20050321002602005032100260EA 2005 3 21 ASOA05117 120050208A5260601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27832AS 7243 DURING AN A-CHECK IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20050321002622005032100262EA 2005 3 21 ASOA05108 120050206A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27846AS 7328 DURING A C-CHECK IN MCN, THE FS 280 CLIPS INBOARD AND OUTBOARD ON THE LEFT AND RIGHT SIDES WRE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FS 280 CLIPS INBOARD AND OUTBOARD ON THE LEFT AND RIGHT SIDES. (M) 2L72 4F RTA21EA 20050321002632005032100263EA 2005 3 21 ASOA05105 120050206A5260601R3198067 STEP CNDAIRCL600 CL6002C10 1390015EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27719EV 10099 FLT 4161 - DURING A GROUND INSPECTION IN ATL, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050321002652005032100265EA 2005 3 21 ASOA05156 120050225A526060031980101 HINGE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27866AS 7517 FLT 4398 - DURING A GROUND INSPECTION IN SHV, THE TOP STEP HINGE ON THE PASSENGER DOOR WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE TOP STEP HINGE ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050321002662005032100266EA 2005 3 21 ASOA05155 120050225A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27863AS 7487 DURING HANGAR MAINTENANCE IN BTR, THE AFT EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE AFT EMERGENCY CEILING LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050321002672005032100267EA 2005 3 21 ASOA05103 120050206A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27924EV 7830 DURING HANGAR MAINTENANCE IN BTR, THE EMERGENCY CEILING LIGHT AT ROW 10 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY CEILING LIGHT LAMP AT ROW 10. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050321002692005032100269EA 2005 3 21 ASOA05101 120050205A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN MALFUNCTIONED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27824AS 7203 FLT 4158 - AFTER POWERING DOWN THE AIRCRAFT IN ATL, THE CREW REPORTED THAT THE EMERGENCY LIGHT REMAINED ON. THE CREW RESET THE CIRCUIT BREAKER TO THE EMERGENCY LIGHTS AND THE LIGHTS EXTINGUISHED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050321002722005032100272EA 2005 3 21 ASOA05162 120050205A5320CC67033292 FLOOR SUPPORT CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27701EV 10020 DURING HANGAR MAINTENANCE IN CKB, THE FLOOR SUPPORT CHANNEL AT FS 280 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT CHANNEL AT FS 280 IAW AS EO 700-53-0037. (M) 2L72 4F RTA21EA 20050321002732005032100273EA 2005 3 21 ASOA05168 120050212A5320 INTERCOSTAL CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27701EV 10020 DURING HANGAR MAINTENANCE IN CKB, THE RIGHT INTERCOSTAL AT RBL 36 APPROXIMATELY TEN INCHES AFT OF FS 280 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE RIGHT INTERCOSTAL AT RBL 36 APPROX TEN INCHES AFT OF FS 280 IAW ASA EO 700-53-0037. (M) 2L72 4F RTA21EA 20050321002752005032100275EA 2005 3 21 ASOA05164 120050206A5320 BEAM CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27701EV 10020 DURING HANGAR MAINTENANCE IN CKB, THE FS 280 TRANSVERSE BEAM WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE FS 280 TRANSVERSE BEAM IAW ASA EO 700-53-0037. (M) 2L72 4F RTA21EA 20050321002782005032100278EU 2005 3 21 ASOA05154 120050225A33503011052 SIGN AEROSPATR72 ATR72 EU CABIN OUT OF POSITION A ASOAK NONE O OTHER ININSP/MAINT 1 SO27643AS 413 FLT 4709 - DURING A GROUND INSPECTION IN CSG, THE EMERGENCY EXIT SIGN BY THE SERVICE DOOR WAS FOUND MISSING. THE CREW FOUND THE EMERGENCY EXIT SIGN COVER UNDER THE SERVICE CART AND MAINTENANCE REINSTALLED IT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20050321002802005032100280EA 2005 3 21 ASOA05160 120050221A5210 WEB CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27848AS 7339 DURING A C-CHECK IN MCN, THE PASSENGER DOOR RUNNER WEB LOWER AFT AREA WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE PASSENGER DOOR RUNNER WEB LOWER AFT AREA IAW BOMBARDIER REO 601R-52-11-683. (M) 2L72 4F RTA21EA 20050321002832005032100283EA 2005 3 21 ASOA05149 120050221A33501317 LIGHT CNDAIRCL600 CL6002C10 1390015EA EXTERIOR INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27738EV 10146 FLT 4744 - DURING A GROUND INSPECTION IN SLC, THE AFT EXTERIOR EMERGENCY LIGHT ON THE LEFT SIDE WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE AFT EXTERIOR EMERGENCY LIGHT ON THE LEFT SIDE. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050321002852005032100285EA 2005 3 21 ASOA05106 120050206A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27846AS 7328 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT AFT PRESSURE WALL INTERCOSTALS AT FS 625 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LEFT AND RIGH AFT PRESSURE WALL INTERCOSTALS AT FS 625. (M) 2L72 4F RTA21EA 20050321002872005032100287EA 2005 3 21 ASOA05111 120050207A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27846AS 7328 DURING A C-CHECK IN MCN, THE ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW ASA EO 600-53-0072A. (M) 2L72 4F RTA21EA 20050321002882005032100288EA 2005 3 21 ASOA05140 120050217A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27848AS 7339 DURING A C-CHECK IN MCN, THE FUSELAGE FRAME FS 718, STRINGER 10-11, LHS AND RHS WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FUSELAGE FRAME FS 718, STRINGER 10-11, LHS AND RHS IAW ASA EO 600-53-0066. (M) 2L72 4F RTA21EA 20050321002892005032100289EA 2005 3 21 ASOA05118 120050209A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA RT WING CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27828AS 7213 DURING A C-CHECK IN MCN, THE LOWER TRAILING EDGE WING PLANK AT WS 148.019 RHS WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LOWER TRAILING EDGE WING PLANK AT WS 148.019 RHS IAW ASA EO 600-57-0134A. (M) 2L72 4F RTA21EA 20050321002902005032100290EA 2005 3 21 ASOA05146 120050220A5260601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27884AS 7513 DURING HANGAR MAINTENANCE IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20050321002922005032100292EA 2005 3 21 ASOA05139 120050217A5210601R3807423 ANCHOR FITTING CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO17836AS 7263 DURING HANGAR MAINTENANCE IN MCN, THE FORWARD ANCHOR FITTING ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE FORWARD ANCHOR FITTING ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. (M) 2L72 4F RTA21EA 20050321002942005032100294EU 2005 3 21 ASOA05135 120050216A33503011210 LIGHT AEROSPATR72 ATR72212 8680945EU CABIN INTERMITTENT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27632AS 338 DURING A HANGAR CHECK IN MCN, THE EMERGENCY FLOOR LIGHT ON THE PASSENGER DOOR WAS FOUND TO OPERATE INTERMITTENTLY. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20050321002962005032100296EA 2005 3 21 ASOA05132 120050215A5210 SKIN CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27828AS 7213 DURING A C-CHECK IN MCN, THE PASSENGER DOOR INNER SKIN AT THE LOWER INTERCOSTAL AND FORWARD STEP FRAME WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE PASSENGER DOOR INNER SKIN AT THE LOWER INTERCOSTAL AND FORWARD STEP FRAME IAW ASA EO 600-52-0082. (M) 2L72 4F RTA21EA 20050321002972005032100297EA 2005 3 21 ASOA05136 120050216A2752852D10019 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA T/E FLAP FAILED A ASOAK NONE J WARNING INDICATION APAPPROACH 1 SO27910EV5643 7727 FLT 4573 - DURING APPROACH INTO YYZ FROM ATL, THE CREW RECEIVED A FLAPS FAIL MESSAGE WITH THE LEFT FLAP AT THREE DEGREES AND THE RIGHT FLAP AT FOUR DEGREES. THE QRH WAS COMPLIED WITH AND EMERGENCY EQUIPMENT WAS REQUESTED TO BE ON STANDBY AS A PRECAUTION. THE AIRCRAFT LANDED SAFELY IN YYZ. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT INBOARD AND OUTBOARD FLAP ACTUATORS. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT LANDED SAFELY IN YYZ. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT INBOARD AND OUTBOARD FLAP ACTUATORS. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050321002982005032100298EA 2005 3 21 ASOA05125 120050211A5260601R3198073 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27846AS 7328 DURING A C-CHECK IN MCN, THE TOP STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE TOP STEP ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20050321002992005032100299EA 2005 3 21 ASOA05145 120050218A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27848AS 7339 DURING A C-CHECK IN MCN, THE ENGINE SUPPORT BEAM AT BL 36.20 LEFT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTNENANCE REPAIRED THE ENGINE SUPPORT BEAM AT BL 36.20 LT IAW ASA EO 600-53-0070. (M) 2L72 4F RTA21EA 20050321003002005032100300EA 2005 3 21 ASOA05144 120050218A5320601R3117117 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27848AS 7339 DURING A C-CHECK IN MCN, THE FS 484 INBOARD CLIPS AT LBL 27 AND RBL 27 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FS 484 INBOARD CLIPS AT LBL 27 AND RBL 27 IAW WITH ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20050322000032005032200003EA 2005 3 22 A6WA200540089 120050307A3222 RETAINER CNDAIRCL600 CL6002B19 1900309EA NLG MISSING A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31444ZW 7788 AFTER TAKEOFF AT 300 FT, 160 KTS, RECEIVED GEAR UP DISAGREE NLG UPON SELECTION OF GEAR MLG UP AND LOCKED CAUTION WOW STATUS MESSAGE WOW OUTPUT FAILED FOLLOWED QRH DECLARED EMERGENCY LANDING UNEVENTFUL LANDING IN ORD. FOUND NOSE LANDING GEAR STRUT RETAIN COLLAR 90 OUT FROM WEAR DISARMED STRUT. INSPECTED FOUND LOWER RET ATN MISSING. REPLACED MINS AND RERACKED STRUT IAW 37-21-00 AND 32-21-15. NO DEFECTS NOTED. (M) 2L72 4F RTA21EA 20050322000042005032200004EA 2005 3 22 A6WA200540082 120050228A30106420002 PRESSURE SWITCH CNDAIRCL600 CL6002B19 1900309EA ANTI-ICE SYSTEM FAILED A A6WAA UNSCHED LANDING G MULTIPLE FAILURE CLCLIMB 1 GL31456ZW 7849 ON TAKEOFF IN ICING CONDITIONS, BOTH WING ANTI-ICE CAUTION MESSAGES. TRANSFERRED TO STANDBY GOT RT WING ANTI-ICE CAUTION MESSAGE. COMPLIED WITH QRH AND MANUALL OPENED 14TH STAGE VALVE MODULATED OPEN/CLOSED. LEFT WING ANTI-ICE SOV CLOSES. EXITED ICING CONDITIONS. REMOVED AND REPLACED RT ANTI-ICE PRESSURE SWITCH. OPS CHECK GOOD OF STANDBY WING ANTI-ICE SYSTEM. REF 30-12-00 OF CRJ AMM. TROUBLESHOT NORMAL WING ANTI-ICE SYSTEM AND SUSPECT RELAY K1HA AT FAULT. REMOVED AND REPLACED ANTI-ICE CONTROL PANEL. OPS CHECK GOOD. (M) 2L72 4F RTA21EA 20050322000062005032200006NE 2005 3 22 ASOA05130 220050214A7261 OIL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT ENGINE LOW A ASOAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27883AS 7504 FLT 4151 - DURING CRUISE FROM FPO-ATL, WHILE IN HOLDING PATTERN OVER ATL, CREW OBSERVED THE RT ENG OIL PRESS FLUCTUATING FROM APPROX 37 TO 50 PSI. THE CREW WAS INSTRUCTED TO DIVERT TO BHM AND THEN THEY RECEIVED A 'RT ENGINE OIL PRESSURE' MESSAGE ACCOMP BY A RED TRIPLE CHIME. THE CREW BROUGHT THE RT THRUST LEVER TO IDLE. THE QRH WAS C/W AND AN EMERGENCY WAS DECLARED. THE OIL PRESSURE VARIED FROM 30 TO 40 PSI DURING THE REMAINDER OF THE FLT WITH THE A/C LANDING SAFELY IN BHM. MX SERVICED THE RT ENG WITH THREE AND ONE-HALF QTS OF OIL AND ALSO INSP THE RT ENG OIL SYS CHIP DETECTOR, OIL FILTERS AND PERFORMED ENG RUNS FOR THIRTY MINUTES. NO DEFECTS WERE NOTED. OPS CHECKS GOOD. A/C OK FOR SERVICE. (M) 2L72 4F4 FRTA21EA E15NE 20050322000072005032200007EA 2005 3 22 ASOA05129 120050214A5210601R380742 ANCHOR FITTING CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27870AS 7530 DURING HANGAR MAINTENANCE IN MCN, THE FORWARD ANCHOR FITTING ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE FORWARD ANCHOR FITTING ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050322000082005032200008EA 2005 3 22 ASOA05147 120050220A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27905EV 7632 DURING AN A-CHECK IN MCN, THE ENGINE SUPPORT BEAM AT BL 36.20 LEFT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE PERFORMED A TEMPORARY REPAIR TO THE ENGINE SUPPORT BEAM AT BL 36.20 LEFT IAW ASA EO 600-53-0071. (M) 2L72 4F RTA21EA 20050322000092005032200009EA 2005 3 22 ASOA05143 120050218A5320601R3117117 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27848AS 7339 DURING A C-CHECK IN MCN, THE FS 484 OUTBOARD CLIPS AT LBL 36 AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FS 484 OUTBOARD CLIPS AT LBL 36 AND RBL 36 IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20050322000132005032200013EA 2005 3 22 ASOA05131 120050215A325016850101 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA NLG FAULTY A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27914EV 7752 FLT 4126 - DURING CLIMB-OUT FROM ATL-MEI, FOLLOWING ROTATION AND GEAR UP THE CREW SIMULTANEOUSLY RECEIVED MASTR CAUTION AND NOSE WHEEL STEERING (NWS) INOP MESSAGES ACCOMPANIED BY A LOUD SNUBBER SOUND FROM THE NOSE COMPARTMENT LASTING APPROXIMATELY TWO MINUTES. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO ATL, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE NOSE WHEEL STEERING SELECTOR VALVE AND SWUNG THE NOSE GEAR. MAINTENANCE ALSO REMOVED AND REPLACED BOTH NOSE WHEEL AND TIRE ASSEMBLIES. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050317002072005031700207NM 2005 3 17 QXEA200500305 120050223A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09413QX 4060 PDX - CORROSION ON RIGHTHAND OUTBOARD SEAT TRACK AT APPROXIMATELY X507.00, TOP AND INNER FLANGE. REPLACED SEAT TRACK IAW DHC-8 SRM 51-42-15 AND 51-42-05. 2H72 4T RTA13NM 20050317002102005031700210NM 2005 3 17 QXEA200500356 120050228A5410 SUPPORT BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09413QX 4060 PDX - NR 2 ENGINE LOWER COWL, BYPASS DUCT CENTER SUPPORT FRAME IS CRACKED ON UPPER FLANGE. REPAIRED IAW RD 8/4-71-016. 2H72 4T RTA13NM 20050317002392005031700239NM 2005 3 17 QXEA200500343 120050217A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09363PH 520 PDX - RIGHTHAND OUTBOARD NR 10 SEAT TRACK HAS LITE SURFACE CORROISON ON TOP OF LUGS AT X326 AND PITTING IN BOTTOM OF CHANNEL AT X340 TO X342. REPAIRED IAW DHC-8 202 SRM 51-40-00 AND SRM 51-40-11. 2H72 4T RTA13NM 20050317002462005031700246EA 2005 3 17 COMA0560166 120050311A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01995CA 7229 THREE CRACKS FOUND PAX FS 320.00, 329.00 AND 338.00. REPAIRED IAW REO 601R-52-11-684. 2L72 4F RTA21EA 20050317002522005031700252NM 2005 3 17 AWXA200500327 120050125A532065535944 REVEAL BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK A 1 INCH CRACK WAS FOUND IN R-1 DOOR UPPER AFT REVEAL. MAINTENANCE REMOVED CRACKED R-1 DOOR UPPER AFT REVEAL FROM BS 320 TO BS 328 AT STR 10 RT; FABRICATED A NEW REPLACEMENT REVEAL PER DWG 65-53594; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 4. 2L72 4F RTA16WE 20050317002572005031700257NM 2005 3 17 UPS05M44104 120050105A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 35 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED & REWORKED ON BARREL NUT HOLE NR 35 RT PER SRM 51-21-01.V2.R36, FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I, APPLIED SEALANT PR1422B1/2 ON BARREL NUT HOLE NR 35 RT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED ON BARREL NUT HOLE NR 35 RT PER EN1172-05 & EO MD110-5510-19409-I, FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20050318000232005031800023WP 2005 3 18 UPS05844128 120050315A5755 SKIN DOUG DC8 DC873F 302199FWP RT WING SPOILER DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 RT WING INBOARD SPOILER DELAMINATED. 2L74 4F RT4A25 20050318000332005031800033EU 2005 3 18 05FDEA00546 120050315A2910 LINE AIRBUS310 A310222 3930315EU HYD SYSTEM LEAKING A FDEAB EMER. DESCENT KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO25420FE 339 AFTER GEAR EXTENSION GOT GREEN HYDRO SYS LOW AIR PRESSURE LIGHT. DECLARED AN EMERGENCY AND LANDED STRAIGHT AHEAD. AFTER LANDING LOW AIR LIGHT WENT OUT. TURNED BOTH GREEN PUMPS BACK ON IAW QRH. GREEN SYSTEM RECOVERED AND CLEARED THE RUNWAY. GREEN HYD SYSTEM PRESSURE ON NR 5 SPOILER WORK NORMAL NO FAULT INDICATED. T/S ON TANK AIR PRESSURE SYSTEM IN PROGRESS. LEAK CHECK ON GREEN TANK AIR PRESSURE SYSTEM, FOUND SMALL AIR LEAK ON LINE FROM TANK TO DEPRESSURIZATION AND OVERFLOW VALVE. POSSIBLE TO TIGHT NUT. TANK PRESSURE FILLED FROM GROUND CONNECT CHECKED AFTER SEVERAL HOURS, NO CHANGE. A/C OK TO CONTINUE. 2L72 4F RTA35EU 20050318000382005031800038 2005 3 18 05019 420050222A25657A121834 SLIDE BOEING747 747212B 1384886NM UPPER DECK FAILED A KCSAO OTHER L NO TEST NRNOT REPORTED 1 GL23703CK 21939 DURING D-CHECK, TASK CARD 7DT2004 UPPER DECK EMERGENCY EVACUATION SLIDE FAILED ON DEPLOYMENT. REMOVED AND REPLACED UPPER DECK EMERGENCY EVACUATION SLIDE IAW B747 MM 25-68-02. REMOVED AND REPLACED BOTTLE IAW B747 MM 25-68-01. 2L74 4F A20WE 20050318000412005031800041EA 2005 3 18 SWIA200514712 120050312A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07912SW 7595 FORWARD CABIN CEILING LEVEL EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT BULB, OPERATIONAL CHECK GOOD. REF CRJ MM 33-51-00. 2L72 4F RTA21EA 20050318000472005031800047EA 2005 3 18 SWIA200514718 120050309A2741 SWITCH CNDAIRCL600 CL6002B19 1900309EA PITCH TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07435SW 7555 CAPTS TRIM SWITCH RIGHT HALF STICKS. REPLACED CAPTAINS PITCH TRIM SWITCH IAW MM 27-41-05-400-801. 2L72 4F RTA21EA 20050318000482005031800048 2005 3 18 SWIA200514719 420050305A2216 SERVO CNDAIRCL600 CL6002B19 1900309EA AUTOPILOT CONTAMINATED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07435SW 7555 WHEN AP (CAPT SIDE) WAS ENGAGED, REC'D AP TRIM IS LWD CAUTION, A/C BEGAN TO ROLL RIGHT WHILE FD WAS DIRECTING A LEFT TURN. DISCONNECTED IT FOR REMAINDER OF FLIGHT. CHECKED RIGGING OF RIGHT AND LEFT AILERON PCU'S IAW 27-11-00. REMOVED MOISTURE FROM AILERON/AUTOPILOT SERVO. AUTOPILOT OPERATIONAL CHECKS GOOD. 2L72 4F RTA21EA 20050321000022005032100002NM 2005 3 21 SWAA050813 120050316A2761654456114 ACTUATOR BOEING737 7373H4 1384600NM RT WING LEAKING A SWAAA UNSCHED LANDING K FLUID LOSS NRNOT REPORTED 1 SW29331SW 23695 DECLARED EMERGENCY. A SYSTEM HYDRAULIC LOST QUANTITY/PRESSURE. REMOVED AND REPLACED NR 7 SPOILER ACTUATOR PER MM. 2L72 4F RTA16WE 20050321000042005032100004 2005 3 21 SWAA050815 420050316A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29421LV 32452 DURING SCHEDULED MV2 CHECK, L1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATED LOW. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20050321000092005032100009NM 2005 3 21 SWAA050820 120050316A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29654SW 28399 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON SHEAR TIE AT BS 787, RBL 6. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050321000112005032100011NM 2005 3 21 SWAA050822 120050316A53126546568 BULKHEAD BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND BS 1016 PRESS BULKHEAD CRACKED AT STR 9R. REPAIRED PRESS BULKHEAD PER PAE ER. 2L72 4F RTA16WE 20050321000142005032100014 2005 3 21 SWAA050825 420050316A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29729SW 27861 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050321000182005032100018EU 2005 3 21 MALA050242 120050301A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15446XJ 340B446 DURING 4K CHECK IN BNA FOUND FUSELAGE SKIN IS CHAFED OUT OF LIMITS AT THE AFT END OF PANEL 192AR. DAMAGE IS ACCEPTABLE IAW MESABA EOS53288. REF EAM WORK ORDER 211770 TASK 1509. 2L72 4T RTA52EU 20050321000212005032100021EU 2005 3 21 MALA050246 120050301A5315 FLOORBEAM BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15502XJ E2307 DURING C2 CHECK IN YYC FOUND FR 43 FLOORBEAM 20 INCHES LBL GUSSET CORRODED. MAT'L .100 INCH THICK 2024T3 AL SHEET. 2H74 4F RTA49EU 20050321000292005032100029EU 2005 3 21 MALA050260 120050311A2930 PUMP BAC 146 AVRO146RJ85A1500097EU HYD SYSTEM MALFUNCTIONED A MALAO OTHER MJ OVER TEMP WARNING INDICATION CRCRUISE 1 GL15503XJ E2310 CREW REPORTED, RECEIVED GREEN HYDRAULIC HI TEMP. CREW FOLLWED QRH, THEN 45 MINUTES LATER CREW REPORTED YELLOW HYDRAULIC HI TEMP CAME ON. FOLLOWED QRH, AFTER FOLLOWING QRH FOR BOTH FAULT LIGHTS, THE LIGHTS WENT OUT. REPLACED NR 3 ENGINE DRIVEN PUMP FOR GREEN HYDRAULIC, YELLOW HYDRAULIC, GROUND RAN FOR 40 MINUTES AT HIGH POWER SETTINGS AND OPERATING ALL YELLOW SYSTEM HYD COMPONENTS. UNABLE TO DUPLICATE. 2H74 4F RTA49EU 20050321000302005032100030EU 2005 3 21 MALA050261 120050311A3260 UPLOCK SWITCH BAC 146 AVRO146RJ85A1500097EU MLG DIRTY A MALAO OTHER J WARNING INDICATION TOTAKEOFF 1 GL15532XJ E2366 LT GEAR UNSAFE LIGHT AFTER RETRACTION, GEAR HANDLE UNSAFE AS WELL. LOWERED GEAR, RETURNED FOR LANDING. CND CLEANED UPLOCK SWITCH AND LUBE UPLOCK SWITCH ON LT GEAR CYCLE. GEAR OPS CHECK GOOD ON GROUND IAW AVRO MM 32-30-00-501. 2H74 4F RTA49EU 20050321000322005032100032EU 2005 3 21 MALA050268 120050312A5320 FLOOR SUPPORT SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15433XJ 340B433 DURING 4Y/2Y CHECK IN BNA FOUND LT AND RT AISLE FLOOR FLANGE BL 0 STA 294.0 TO 297.0 IS CORRODED. AFTER CORROSION REMOVAL REPAIRED PER PARTS FABRICATION AND INSTALLED. WORK PERFORMED ON EMB WO 211832 TASK 1510/1509. 2L72 4T RTA52EU 20050321000392005032100039NM 2005 3 21 SWAA050810 120050315A53206546552 STRAP BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND CORROSION ON FUSELAGE FRAME STRAP AT BS 847, RBL 17, WL 154. REMOVED AND REPLACED STRAP PER SRM. 2L72 4F RTA16WE 20050321000422005032100042NM 2005 3 21 AALA20050201 120050316A3350 LIGHT BOEING757 757223 1384957NM CABIN BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21603AA 27054 DFW - SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AT 14D IS BROKEN AND INOPERATIVE. REPLACED THE SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AT 14D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050321000492005032100049GL 2005 3 21 CHQA200500053 220050311A7200 ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 1 UNSERVICEABLE A CHQAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 GL11579RP1015 1015 14500871 CAE312721 FLIGHT 6236 GSO-MCO - ON INITIAL CLIMB AT APPROXIMATELY 800 FEET, A LAV SMOKE WARNING APPEARED ON EICAS. THE TOWER WAS NOTIFIED AND THE FLIGHT ATTENDANT CHECKED THE CABIN FOR SIGNS OF FIRE OR SMOKE. NO EVIDENCE WAS FOUND. ON SHORT FINAL AN E1 LOW OIL PRESS WARNING APPEARED ON EICAS. THE AIRCRAFT LANDED UNEVENTFULLY BUT OVER MAX LANDING WEIGHT. THE FIRE DEPARTMENT PERFORMED A THERMAL SCAN OF THE AIRCRAFT AND NO HEAT SOURCE WAS FOUND. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE. OPS CHECK GOOD. NO SIGNS OF SMOKE PRESENT. 2L72 4T4 FRTT00011ATTE6CH 20050321000512005032100051CE 2005 3 21 PNSA050201 120050221A324309206700 PISTON CESSNA208 208B 2073701CE BRAKE ASSY DISLODGED E PNSAO OTHER KJ FLUID LOSS WARNING INDICATION LDLANDING 1 AL039310F 60 208B0490 ON LANDING AT KCG BRAKING WAS LOSS ON LT SIDE. AIRCRAFT ROLLED OUT NORMAL. MAINTENANCE FOUND TWO BRAKE PISTON SEALS ON LT BRAKE CALIPER HAD FAILED CAUSING A LOSS OF FLUID. CALIPER WAS REPLACED AND BRAKES BLED. 1H71 3T A37CE 20050321000582005032100058EA 2005 3 21 VTZA200500014 120050317A531260034017595 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27708BR 7575 RIGHT SIDE PILOTS BULKHEAD AT FS 280 RBL 9.0 IS CRACKED AT 1.0 INCH IN WEB RADIUS. 2L72 4F RTA21EA 20050321000592005032100059EA 2005 3 21 VTZA200500018 120050317A5320601R311719 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27708BR 7575 INTERCOSTAL CRACKED AT .25 INCH IN LENGTH ON RIGHT OUTBOARD SIDE AT FS 484 BETWEEN BL 27.00. 2L72 4F RTA21EA 20050321000622005032100062EA 2005 3 21 VTZA200500016 120050317A53206013521252 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27708BR 7575 RIGHT 624 OBLIQUE ANGLE IS CRACKED AT 1 INCH RADIUS. 2L72 4F RTA21EA 20050321000662005032100066EU 2005 3 21 YENA200523 120050308A212120092455101 COOLING FAN AIRBUS320 A320232 3930326EU LIVE TV RACK FROZEN A YENAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA15580JB5603 2136 DURING GROUND OPERATION RECEIVED AFT AVIONICS SMOKE ALARM. RESET ALARM SECOND TIME. ACCOMPLISHED INFO NOTICE 2004-T023TR. INSPECTED THE AFT LIVE TV RACK AND FOUND COOLING IAU MONITOR WITH EVIDENCE OF ELECTRICAL ODOR. DEACTIVATED LIVE TV SYSTEM PER MEL 25-22-00. AT JFK ON 03/11/05 FOUND AFT RACK COOLING FAN SEIZED. REMOVED AND REPLACED AFT RACK COOLING FAN AND SYSTEM REACTIVATED PER LTV MM 23-39-00. CLEARED MEL. 2L72 4F RTA28NM 20050321000722005032100072 2005 3 21 MALA050263 420050314A2350 RADIO SAAB SF340 340B 7860101EU COCKPIT MALFUNCTIONED A MALAO OTHER O OTHER CLCLIMB 1 GL15365PX 340B265 DURING CLIMBOUT FROM DTW INTERCOM STATIC BECAME SEVERE, STATIC OVER SPEAKERS WITH ALL VOLUMNS OFF. RETURNED TO DTW. REMOVED AND REPLACED REU AND F/O'S ACP. OPS CHECK GOOD. 2L72 4T RTA52EU 20050321000742005032100074EU 2005 3 21 MALA050265 120050312A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSLEAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15433XJ 340B433 DURING 4Y/2Y CHECK IN BNA FOUND RT FWD GALLEY SEAT TRACK CORRODED. REMOVED AND REPLACED TRACK AND PROFILE REF SRM 51-40-27/22. WORK PERFORMED ON EMB WO 211832 TASK 1502. 2L72 4T RTA52EU 20050321000882005032100088NM 2005 3 21 QXEA200500370 120050120A2571 RACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - LEFTHAND NOSE COMPARTMENT, BATTERY SHELF TOP SURFACES HAS MINOR SURFACE CORROSION. REPAIRED IAW DHC-8 400 SRM 51-14-00-350-803 AND 51-21-10-380-001. 2H72 4T RTA13NM 20050321001182005032100118EA 2005 3 21 COMA0560169 120050311A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01995CA 7229 INTERCOSTAL AT FS 484.00 IS CRACKED. REPAIRED IAW REO 601R-53-41-059. 2L72 4F RTA21EA 20050321001192005032100119 2005 3 21 VTZA200500009 420050309A3418 COMPUTER CNDAIRCL600 CL6002B19 1900309EA STALL WARNING MALFUNCTIONED A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27652BR 7429 STALL FAIL MESSAGE POSTED AFTER T/O. RESET STALL PROTECTION COMPUTER. NO FAULT CODES RECORDED IN COMPUTER. 2L72 4F RTA21EA 20050321001392005032100139NM 2005 3 21 QXEA200500382 120050126A5310 DOUBLER BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - FUSELAGE LAV SERVICE DOOR SURROUND LOWER MACHINED DOUBLER HAS EXFOLIATION CORROSION. REPAIRED IAW RD 8/4-114-, ISSUE 1, PAGE 5 AND HORIZON AIR EA 6-53-515. 2H72 4T RTA13NM 20050321001412005032100141NM 2005 3 21 QXEA200500375 120050124A5753 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - LEFTHAND INBOARD FLAP HAS TWO AREAS WHERE IT IS CHAFING WITH THE UPPER SHROUD AND HAS WORN THROUGH TO THE METAL FLAP SURFACE. REPAIRED IAW DHC-8 400 SRM 57-51-30-320-801 AND 57-51-30-940-001. 2H72 4T RTA13NM 20050321001422005032100142NM 2005 3 21 QXEA200500378 120050116A5330 ACCESS PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - FORWARD FUSELAGE ACCESS PANEL 121AL HAS A STRIPPED ANCHOR NUT. REPLACED ANCHOR NUT IAW DHC-8 400 SRM 51-42-05-330-001. 2H72 4T RTA13NM 20050321001732005032100173SO 2005 3 21 C2XA05IA041 120050304A2120 ODOR EMB 145 EMB145 3260210SO COCKPIT DETECTED A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW2714972 145151 EWR - FLIGHT 2331 THE CREW REPORTED A STRONG FUEL SMELL IN THE COCKPIT AFTER STARTING THE APU. MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE APU AND AIR DISTRIBUTION SYSTEMS WITH NO DEFECTS BEING NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050321001742005032100174SO 2005 3 21 SWIA200514666 120050307A3030 SENSOR EMB 120 EMB120ER 3260203SO PITOT HEAT OVERHEATED A SWIAO OTHER MB OVER TEMP SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM07271YV 120271 DURING FLIGHT STRONG ELECTRICAL BURNING ODOR NOTED BY BOTH CREW MEMBERS, ON GROUND IN LAX ODOR SEEMS TO BE ISOLATED TO COCKPIT AREA AND AUX PITOT STATIC HEAT IS NOW INOPERATIVE. INSTALLED NEW OVER CURRENT SENSOR IAW MM 30-33-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050321001762005032100176EA 2005 3 21 SWIA200514668 120050307A5610 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT FAILED A SWIAA UNSCHED LANDING O OTHER CRCRUISE 1 NM07947SW 7786 AT FL320, THE F/O'S RIGHT WINDSHIELD SHATTERED. REPLACED SIDE WINDOW IAW CRJ MM 56-12-01, OPERATIONAL CHECK GOOD. P/N NP-139322-2, S/N OFF 03007H3858. 2L72 4F RTA21EA 20050321001782005032100178EA 2005 3 21 SWIA200514670 120050303A5240 HANDLE CNDAIRCL600 CL6002B19 1900309EA SERVICE DOOR LACK OF LUBE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07920SW 7660 SERVICE DOOR WILL NOT OPEN FROM THE OUTSIDE. LUBED SERVICE DOOR INNER AND OUTER HANDLE, OPERATIONAL & FUNCTIONAL CHECK GOOD IAW CRJ 200 MM 52-41-00. 2L72 4F RTA21EA 20050321001892005032100189EU 2005 3 21 AALA20050199 120050315A3350P4010049 BATTERY PACK AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW2190070 513 JFK - SEAT MOUNTED EMERGENCY LIGHTS FROM SEAT 19C TO 28C INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS FROM SEAT 19C TO 28C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20050321001912005032100191WP 2005 3 21 AALA20050196 120050313A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21592AA 53255 LAX - EMERGENCY LIGHT IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050321001962005032100196EA 2005 3 21 SWIA200514675 120050306A27507455001 CONTROL LEVER CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED LDLANDING 1 NM07959SW1047 1047 7840 DURING FLAP RETRACTION AFTER LANDING IN DEN, FLAPS FAIL CAUTION MESSAGE. REPLACED FLAP HANDLE IAW MM 27-50-00, OPERATIONAL CHECKS GOOD. 2L72 4F RTA21EA 20050321001982005032100198EA 2005 3 21 SWIA200514677 120050305A27604916405 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED LDLANDING 1 NM07591SW6934 6934 7079 GROUND LIFT DUMP FAILED TO DEPLOY AFTER TOUCHDOWN. REPLACED NR 1 SECU IAW MM 27-61-05, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050321002002005032100200NM 2005 3 21 QXEA200500361 120050308A2150YD4N RELAY DHAV DHC8 DHC8202 2809007NM CABIN TEMP FAILED A QXEAA UNSCHED LANDING O OTHER CLCLIMB 1 NM09365PH14595 526 THE FLIGHT RETURNED TO FIELD AFTER THE CREW WAS UNABLE TO CONTROL THE CABIN TEMPERATURE. THE CREW ATTEMPTED THE UNLATCHING PROCEDURE BUT THE CABIN TEMPERATURE WOULD ONLY COOL TO 25 DEGREES WHEN ON FULL COLD. THE CABIN WOULD THEN INCREASE BACK TO 35 DEGREES AGAIN. MAINTENANCE REMOVED AND REPLACED THE 2161-K1 AND K2 RELAYS. CW OPS CHECK IAW D-8 MM 216000. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050321002042005032100204SO 2005 3 21 RAIA00502034 120050228A3610AS568226 O-RING EMB 145 EMB145 3260210SO NR 2 BLEED SYS LEAKING A RAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03821HK 145068 STL - BLEED LEAK INDICATION. MAINTENANCE REMOVED AND REPLACED O-RING AT NR 2 BLEED. 2L72 4F RTT00011AT 20050321002102005032100210EU 2005 3 21 ASOA05088 120050112A5320 INTERCOSTAL AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27534AS 463 DURING A C-CHECK, THE INTERCOSTALS BETWEEN FR 38 TO 39 ON THE LT AND RT SIDES WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTALS BETWEEN FR 38 TO 39 ON THE LT AND RT SIDES IAW SRM. (K) 2H72 4T4 TRTA53EU E20NE 20050321002142005032100214EA 2005 3 21 ASOA05033 120050115A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN PINCHED A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27902EV 7620 DURING A GROUND INSPECTION, THE LOWER FORWARD EMERGENCY LIGHT ON THE BULKHEAD BY THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE FOUND A WIRE TO THE LOWER FORWARD EMERGENCY LIGHT ON THE BULKHEAD BY THE PASSENGER DOOR PINCHED BY A TIE WRAP CAUSING THE WIRE TO PULL LOOSE FROM ITS CONNECTION. MAINTENANCE REMOVED THE TIE WRAP AND RESECURED THE CONNECTION. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050321002152005032100215EA 2005 3 21 ASOA05038 120050118A5320601R3117117 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27903EV 7621 DURING A C-CHECK, THE LT FS 484 INTERCOSTAL AFT CLIP IB WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FS 484 INTERCOSTAL AFT CLIP IB IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050321002162005032100216EA 2005 3 21 ASOA05040 120050118A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27903EV 7621 DURING A C-CHECK, THE RT LOWER OB ENGINE SUPPORT BEAM AT BL 36.20 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE RT LOWER OB ENGINE SUPPORT BEAM AT BL 36.20 IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050321002212005032100221EA 2005 3 21 ASOA05036 120050118A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27903EV 7621 DURING A C-CHECK, THE AFT EQUIPMENT BAY CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE AFT EQUIPMENT BAY CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL0 IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050321002222005032100222EU 2005 3 21 ASOA05026 120050113A3350E0029387 LIGHT AEROSPATR72 ATR72 EU PWA PW120 PW127 NE CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27642AS 395 DURING HANGAR MAINTENANCE, THE FORWARD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE WHEN THE AFT AND FORWARD 2 MINUTE LIGHT BUTTON WAS ACTIVATED. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY EXIT LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2H72 4T4 TRT E20NE 20050321002312005032100231EA 2005 3 21 ASOA05013 120050104A5320601R3117117 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27826AS 7210 DURING A C-CHECK, THE LT UPPER SURFACE OF THE PRESSURE FLOOR, FS 484 BRACKET ON THE IB AND OB WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LT IB FS 484, LBL 27 CLIP IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050321002442005032100244EA 2005 3 21 ASOA05034 120050116A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EXTERIOR INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27862AS 7476 DURING A GROUND INSPECTION, AN EXTERNAL EMERGENCY LIGHT ON THE RT SIDE WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AN EXTERNAL EMERGENCY LIGHT LAMP ON THE RT SIDE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050321002522005032100252EU 2005 3 21 ASOA05085 120050112A5320 INTERCOSTAL AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27534AS 463 DURING A C-CHECK, THE INTERCOSTALS AT FR 36 TO 38 AND FR 39 TO 40 ON THE RT SIDE IAW SRM. (K) 2H72 4T4 TRTA53EU E20NE 20050321002612005032100261EA 2005 3 21 ASOA05113 120050207A5320601R3117117 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27846AS 7328 DURING A C-CHECK IN MCN, THE INTERCOSTALS AT FS 484, LBL 36 AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE INTERCOSTALS AT FS 484, LBL 36 AND RBL 36 IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20050321002712005032100271EA 2005 3 21 ASOA05157 120050226A3234750006000 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27912EV5868 7728 DURING CLIMB-OUT FROM ROC-ATL, UPON GEAR RETRACTION THE CREW RECEIVED A GEAR DOOR OPEN RED WARNING MESSAGE. ATTEMPTS TO RECYCLE THE GEAR WERE UNSUCCESSFUL. THE QRH WAS COMPLIED WITH AND THE AIRCRAFT RETURNED TO ROC. THE TOWER ROLLED THE EMERGENCY VEHICLES AS A PRECAUTION AND THE AIRCRAFT LANDED SAFELY IN ROC. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR NLG DOOR SELECTOR VALVE. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050321002742005032100274EA 2005 3 21 ASOA05165 120050226A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27701EV 10020 DURING HANGAR MAINTENANCE IN CKB, THE FS 280 AFT BULKHEAD LOWER WEB LT/RT WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FS 280 AFT BULKHEAD LOWER WEB LT/RT IAW ASA EO 700-53-0037. (M) 2L72 4F RTA21EA 20050322000022005032200002EA 2005 3 22 A6WA200540085 120050306A2120 SCREEN CNDAIRCL600 CL6002B19 1900309EA CABIN DIRTY A A6WAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 GL31410AW 7490 DISPLAY COOL CAUTION MESSAGE INFLIGHT. MESSAGE WAS INTERMITTENT REGARDLESS OF FAN SELECTION. INSPECTED DISPLAY COOLING DUCTING, NO LEAKS NOTED. AIR FILTER GETTING DIRTY HOWEVER NOT CLOGGED. CLEANED AIR SCREEN BEHIND PFD2. ALL THREE FANS BLOW NORMALLY. NO FAULTS NOTED IAW AMM 21-24-00 AND 21-24-14 AND 21-24-19. (M) 2L72 4F RTA21EA 20050322000052005032200005SW 2005 3 22 2005F00057 120050209A2432 BATTERY BELL 206 206B 1181511SW ALLSN 250B 250B* GL ELECTRICAL SYS WEAK A ALGAO OTHER H ELECT. POWER LOSS-50 PC CRCRUISE 1 SW031078Y 2924 DURING FLIGHT THE GENERATOR FAILED, COMPLETED EMERGENCY PROCEDURES, 7-8 MINUTES LATER EXPERIENCED INTERMITTENT THEN COMPLETE ELECTRICAL FAILURE. RADIOS INOPERATIVE, 0 FUEL PRESSURE, LOW FUEL INDICATION AND FLUCTUATING TOT WITHIN YELLOW RANGE. MAINTAINED 500 FEET AND CIRCLED BEHIND SISTER SHIP AND LANDED BEHIND AIRLOG AIRCRAFT. MAINTENANCE TROUBLESHOT THE GENERATOR SYSTEM FOUND NO PROBLEMS WITH GENERATOR, IT CAME ON LINE AND STAYED ON LINE, VOLTAGE OUTPUT AT THE REGULAOR WAS GOOD AND THE VOLTAGE TO THE BATTERY WAS GOOD. REMOVED THE BATTERY DUE TO BEING WEAK, LOW VOLTAGE. GROUND RAN AIRCRAFT AND RECHECKED THE GENERATOR SYSTEM AND THE SYSTEM FUNCTIONED NORMAL, BATTERY CHARGED UP NORMAL. (M) 1G71 3U3 T H2SW E10CE 20050322000122005032200012EA 2005 3 22 ASOA05133 120050216A5260601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27838AS 7276 DURING HANGAR MAINTENANCE IN MCN, THE LOWER STEP ON THE PASSENGER DOOR WAS FOUND CRACKED AT THE STAY ROD ATTACHMENT. MAINTENANCE REMOVED AND REPLACED THE LOWER STEP ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20050322000152005032200015EU 2005 3 22 ASOA05116 120050208A3350 SWITCH AEROSPATR72 ATR72212 8680945EU CABIN DEFECTIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27632AS 338 FLT 4706 - DURING A GROUND INSPECTION IN ATL, THE EMERGENCY CEILING LIGHTS ILLUMINATED IN THE CABIN RANDOMLY WITH THE EMERGENCY LIGHTS SWITCH IN THE DISARM POSITION. MAINTENANCE CHANGED THE POLARITY ON THE EMERGENCY LIGHT SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20050322000162005032200016EA 2005 3 22 ASOA05098 120050203A5260601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27850AS 7355 DURING HANGAR MAINTENANCE IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN AT THE ATTACH LINK. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20050322000182005032200018EA 2005 3 22 ASOA05114 120050207A3350OL3071BPEGPL LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27885AS 7521 DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY FLOODLIGHT ON THE FORWARD WINDSCREEN BY THE FLIGHT ATTENDANTS STATION WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMPS IN THE EMERGENCY FLOOD LIGHT ON THE FORWARD WINDSCREEN BY THE FLIGHT ATTENDANTS STATION. (M) 2L72 4F RTA21EA 20050322000202005032200020EA 2005 3 22 ASOA05137 120050216A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27848AS 7339 DURING A C-CHECK IN MCN, THE ENGINE SUPPORT BEAM AT BL 36.20 RT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE ENGINE SUPPORT BEAM AT BL 36.20 RT IAW ASA EO 600-53-0073. (M) 2L72 4F RTA21EA 20050322000222005032200022EA 2005 3 22 ASOA05122 120050210A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA EXTERIOR INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27867AS 7463 DURING HANGAR MAINTENANCE IN BTR, THE LEFT EXTERIOR SECOND EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LEFT EXTERIOR SECOND EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050322000232005032200023EA 2005 3 22 ASOA05124 120050211A5210601R3807423 MOUNT CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27884AS 7513 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR FORWARD ANCHOR MOUNT WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR FORWARD ANCHOR MOUNT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050322000242005032200024EA 2005 3 22 ASOA05123 120050211A3350OL3071BPEGPL LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27873AS 7549 FLT 4176 - DURING A GROUND INSPECTION IN ATL, THE MID CABIN EMERGENCY EXIT LIGHT ON THE LEFT SIDE WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE MID CABIN EMERGENCY EXIT LIGHT ON THE LEFT SIDE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050322000262005032200026EA 2005 3 22 ASOA05110 120050206A2597 WIRE CNDAIRCL600 CL6002B19 1900309EA GALLEY OUT OF POSITION A ASOAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27927EV 7844 FLT 4433 - DURING CRUISE FROM ATL-EVV, THE CREW NOTICED AN ELECTRICAL BURNING SMELL IN THE COCKPIT AND THE GALLEY AREA. UPON TURNING OFF THE COFFEE MAKER AND GALLEY POWER, THE SMELL DISSIPATED. THE CREW ALSO PULLED THE GALLEY CNTL AND IND CIRCUIT BREAKER. THE FLIGHT CONTINUED WITHOUT INCIDENT WITH THE AIRCRAFT LANDING SAFELY IN EVV. MAINTENANCE FOUND A WIRE TOUCHING THE HOT SECTION OF THE COFFEE POT AND READJUSTED THE WIRE. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050322000282005032200028EA 2005 3 22 ASOA05152 120050224A3350362624 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27853AS 7374 DURING HANGAR MAINTENANCE IN BTR, AN EMERGENCY FLOOR TRACK LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR TRACK FLEX LAMP STRIP AT THE FRONT END. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050322000292005032200029EA 2005 3 22 ASOA05151 120050222A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA WING MALFUNCTIONED A ASOAK NONE FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 SO27904EV 7628 FLT 4482 - DURING APPROACH INTO MSP FROM ATL, AT APPROXIMATELY 7,000 FEET, THE CREW SELECTED THE FLAPS TO EIGHT DEGREES AND UPON REACHING TWO DEGREES A FLAPS FAILED MESSAGE WAS RECEIVED. THE QRH WAS COMPLIED WITH AND THE CREW SELECTED THE FLAPS TO ZERO DEGREES. AN EMERGENCY WAS DECLARED WITH THE AIRCRAFT LANDED SAFELY IN MSP. MAINTENANCE COMPLIED WITH ASA EO 600-27-0004A BY PERFORMING A FLAP SYSTEM RESET AND CYCLED THE FLAPS. NO DISCREPANCIES WERE NOTED. MAINTENANCE ALSO REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT FOR PREVENTATIVE MAINTENANCE. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050322000332005032200033NM 2005 3 22 BJNA050203 120050227A2560P4010021 BATTERY PACK BOEING737 737282 13844ATNM FLASHLIGHT DISCHARGED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11233TM 23043 CABIN EMERGENCY FLASHLIGHT CHARGE INDICATOR DOES NOT BLINK. REMOVED AND REPLACED THE FLASHLIGHT BATTERY PACK IAW AMM 25-69-00. (M) 2L72 4F RTA16WE 20050322000342005032200034NM 2005 3 22 BJNA05022 120050214A3350362624 LIGHT BOEING737 737282 13844ATNM CABIN INOPERATIVE A BJNAK NONE L NO TEST ININSP/MAINT 1 WP11789TM 23046 FORWARD CABIN FLOOR TRACK LIGHTING INOPERATIVE. REMOVED AND REPLACED SECTION OF TRACK LIGHTING, OPERATIONAL CHECKS OK. (M) 2L72 4F RTA16WE 20050322000352005032200035NM 2005 3 22 C7WA200300075 120050112A8097MS24264R12B3SN WIRE BOEING727 727222 1384073NM PWA JT8 JT8D5 52046NE NR 3 START VALVESHORTED A C7WAO OTHER O OTHER CRCRUISE 1 SO177642U 19915 IN FLIGHT SHUTDOWN NR 3 ENGINE START VALVE OPEN LIGHT ILLUMINATED IN ALT AT 12,000 FEET, PERFORMED ABNORMAL CHECKLIST AS REQUIRED. FOUND WIRES SHORTED IN CONNECTOR D8002 TO NR 3 ENGINE START VALVE PRESSURE SWITCH. REMOVED AND REPLACED CONNECTOR, OPS CHECK PER A/C MM CHAPTER 80-11-01. (M) 2L73 4F4 F A3WE E2EA 20050322000362005032200036NE 2005 3 22 C7WA200400074 220050111A7200 ENGINE BOEING727 727232 1384082NM PWA JT8 JT8D7B 52053NE NR 3 DAMAGED A C7WAO OTHER E VIBRATION/BUFFET CRCRUISE 1 SO17511PE 20634 654764 NR 3 THROTTLE VIBRATION FELT INFLIGHT ALL OTHER ENGINE INSTRUMENT AND INDICATIONS NORMAL, REF LOGPAGE NR 21307. C1, C2, AND C3 DAMAGE FOUND, NR 3 ENGINE REPLACED, S/N OF INSTALLED ENGINE IS 654920. (M) 2L73 4F4 F A3WE E2EA 20050322000382005032200038NM 2005 3 22 GAIA05008ST 120050301A5330 SKIN BOEING727 727214 138407RNM FUSELAGE CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07750US 21512 DURING C-CHECK, A SMALL CRACK WAS FOUND AT THE SKIN LAP AT FS 588 STRINGER 4R. CUT OUT CRACKED AREA AND INSTALLED REPAIR IAW BOEING 727 SRM CHAPTER 53-30-3 FIG 5. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20050322000402005032200040NM 2005 3 22 GAIA05010ST 120050301A5330 SKIN BOEING727 727214 138407RNM FUSELAGE CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07750US 21512 DURING C-CHECK, A SMALL CRACK WAS FOUND ON THE FUSELAGE SKIN BY THE UPPER FORWARD CORNER OF THE R1 DOOR CUTOUT. CUTOUT CRACKED AREA AND INSTALLED REPAIR IAW BOEING MESSAGE 1-71633171 AND KITTY HAWK EA B7-53-124. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20050322000442005032200044WP 2005 3 22 GTIA050009 120050116A7920 OIL FILTER DOUG DC9 DC983 3022083WP RT ENGINE DIRTY A GTIAO OTHER J WARNING INDICATION CRCRUISE 1 GL23835NK 53044 FLL - FLT 507 - RIGHT OIL STRAINER CLOG LIGHT CAME ON IN FLIGHT, LIGHT REMAINED ON ALL ENGINE INDICATIONS NORMAL, LANDED IN FLL AND LIGHT OFF DURING ROLL OUT. AIRCRAFT TAIL SWAP. REMOVED AND REPLACED OIL FILTER, DURING INSTALL OF NEW FILTER STUDS CAME OUT, INSTALLED NEW OIL FILTER STUD. OPS CHECK OK. (M) 2L72 4F RTA6WE 20050322000472005032200047WP 2005 3 22 GTIA050002 120050104A335060030431 POWER SUPPLY DOUG DC9 DC981 3022081WP A/C BAY DISCHARGED A GTIAK NONE L NO TEST ININSP/MAINT 1 GL23818NK 48018 MCO - EMERGENCY LIGHTS IN TAIL COMPARTMENT INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY. (M) 2L72 4F A6WE 20050322000482005032200048NM 2005 3 22 GTIA050003 120050104A2170 COALESCER BAG DOUG MD80 MD83 3023681NM A/C BAY DIRTY A GTIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL23828NK 49823 PBI - FLT 330 - GATE RETURN FOR SMOKE HAZE IN THE CABIN. REMOVED AND REPLACED COALESCER BAG. (M) 2L72 4F RT 20050322000512005032200051NE 2005 3 22 2005F00035 220050127A7200 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE NR 2 MALFUNCTIONED A GTIAH DEACTIVATE SYST/CIRCUITS BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 GL23829NK 49931 725676 LGA - FLT 706 - AT 4,000 FEET, ON CLIMB-OUT, AFT CABIN FILLED WITH SMOKE, LAV SMOKE DETECTOR WENT OFF, TURNED RIGHT ACM OFF AND EMERGENCY RETURN TO LGA, SMOKE DISIPATED AFTER LANDING. REMOVED AND REPLACED NR 2 ENGINE. PERFORMED BURN OUT OF HIGH PRESSURE PNEUMATIC DUCTING. (M) 2L72 4F4 F A6WE E9NE 20050322000562005032200056EU 2005 3 22 O3X05029373 120050223A29101379305A77 FLEX LINE BAG JETSTMJETSTM3201 1500217EU RT NACELLE RUPTURED A O3XAA UNSCHED LANDING K FLUID LOSS CRCRUISE 1 SO03937AE 937 AIRCRAFT DEPARTED STL, WHEN BOTH HYDRAULIC PRESSURE GAUGES WENT TO ZERO. THE CREW ACTUATED BOTH MAIN HYDRAULIC SHUTOFF COCKS. THE AIRCRAFT RETURNED TO STL AND DECLARED AN EMERGENCY. THE LANDING GEAR WAS MANUALLY LOWERED AND THE AIRCRAFT LANDED. INSPECTION REVEALED THAT THE RT HYDRAULIC PUMP PRESSURE STEEL BRAIDED FLEX LINE HAD RUPTURED CAUSING LOSS OF FLUID. THE HYDRAULIC PRESSURE FLEX LINE AND BOTH LEFT AND RT HYDRAULIC PUMPS WERE REPLACED. THE AIRCRAFT WILL FERRY TO MQY FOR SYSTEM BLEED AND SERVICE BEFORE RETURNING TO SERVICE. A FLEET CAMPAIGN IS IN PROGRESS TO REPLACE ALL P/N 1379305-A77 LINES AND TO DETERMINE IN LIFE LIMIT. (M) 2L72 4T RTA56EU 20050322000572005032200057SO 2005 3 22 SIMA200506105 120050208A532014521700007 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21805AE 145489 SAW - DURING CPCP INSPECTION, FOUND CORROSION ON LEFT OMEGA BEAM AT FRAME 20, FORWARD CABIN. COMPLIED WITH LEFT OMEGA SHAPED BEAM REPAIR IAW SRM 53-21-10. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050322000582005032200058SO 2005 3 22 SIMA200506106 120050225A531314533888001 STRINGER EMB 135 EMB135KL 3260302SO FUSELAGE GOUGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21801AE 145469 ABI - DUIRNG A IMBV INSPECTION OF AIRCRAFT, STRINGER 19R WAS FOUND TO BE GOUGED BETWEEN FRAMES 49 AND 50. BLENDED OUT THE GOUGE, PERFORMED EDDY CURRENT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED A REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 28, CHAPTER 53-24-02. (M) 2L72 4F RTT00011AT 20050322000592005032200059SO 2005 3 22 SIMA200505301 120050222A30403801D2MODA CONTROLLER EMB 135 EMB135LR 3260305SO E/E BAY MALFUNCTIONED A SIMAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SW21733KR 145368 DFW - FLT 3740 - ELECTRICAL SMELL AND SMOKE IN COCKPIT. MAINTENANCE FOUND THE NR 2 WINDSHIELD CONTROLLER BURNED. CONTROLLER WAS REMOVED AND REPLACED AND WIRE W102-0841-22 FROM CONTROLLER CANNON PLUG TO SPLICE WAS REPLACED. CONTACTOR K0002 WAS REPLACED AND FUSE ON CONTROLLER P/N 100FU01-080 WAS REPLACED. ALL WORK PERFORMED IAW EMB MM. (M) 2L72 4F RTT00011AT 20050322000632005032200063SO 2005 3 22 SIMA200505605 120050220A532014525380003 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21640AE 145183 ABI - A PREVIOUS REPAIR ON THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. REMOVED EXISTING REPAIR AND CLEANED THE AREA. FABRICATED A FILLER, PLATE, EXTERNAL ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB-145/1142 REV 28, CHAPTER 53-21-10, FIG 201. (M) 2L72 4T RTT00011AT 20050322000662005032200066SO 2005 3 22 SIMA200506102 120050211A532014521725615 SILL EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21805AE 145489 SAW - DURING CPCP INSPECTION, FOUND AFT RIGHT SILL CORRODED IN NUMEROUS AREAS. REMOVED AND REPLACED RIGHT AFT SILL AS PER SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050322000672005032200067SO 2005 3 22 SIMA200505602 120050222A531514521721009 FLOORBEAM EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21703MR 145173 THE GALLEY AREA FORWARD DIGITAL WAS FOUND CORRODED. BLENDED THE AREA TO REMOVED CORROSION AND PERFORMED NDT INSPECTION. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW EMB 145 REPAIR STATEMENT IC2005-145/0923 DATED FEB 21, 2005. (M) 2L72 4F RTT00011AT 20050322000692005032200069SO 2005 3 22 SIMA200505601 120050219A532014522178005 SILL EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21703MR11871 145173 ABI - THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED EXISTING SERVICE DOOR CENTER SILL AND CLEANED THE AREA. INSTALLED NEW SERVICE DOOR SILL. REPAIR DONE IAW EMB 145 SRM, SRM EMB-145/1142 REV 28, CHAPTER 51-40-02. (M) 2L72 4F RTT00011AT 20050322000702005032200070SO 2005 3 22 SIMA200506101 120050211A532014522461011 DOUBLER EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21805AE 145489 SAW - DURING CPCP INSPECTION, FOUND FORWARD DOUBLER CORRODED TOP AND BOTTOM SURFACES. REMOVED AND REPLACED FORWARD DOUBLER AS PER SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050322000712005032200071GL 2005 3 22 UIEA200500009 220050222A7200 ENGINE BOEING747 74747UF 1384949NM GE CF6 CF680C2* GL NR 3 VIBRATION A UIEAO OTHER E VIBRATION/BUFFET CRCRUISE 1 EA15498MC 29259 FLT GT 9991 - ENGINE NR 2 VIBRATION OCCURRED DURING CLIMB-OUT AND INTERMITTENTLY DURING FLIGHT. AFTER 4 HOURS FLIGHT TIME THE LEVEL OCCASIONALLY EXCEEDED 5.0, NR 3 EGT AVERAGED ABOUT 18 DEG HIGHER THAN THE OTHER THREE. REMOVED AND REPLACED NR 3 ENGINE IAW ATLAS AIR MAINTENANCE CARD A717107 GTI REF MM 72-00-00. REF LOG PAGE 546127. (M) 2L74 4F4 FRT1384945 E23EA 20050322000722005032200072NM 2005 3 22 USAA050314 120050216A5320 FLOOR SUPPORT BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU50570 23706 PIT - FOUND FLOOR SUPPORT CORRODED 1 INCH BY 1 INCH AREA, FLOOR SUPPORT BEAM S-26R BS 787-867. CORROSION LEVEL 1, TASK C53-208-01. REMOVED AND REPLACED FLOOR SUPPORT BEAM WITH FABRICATED BEAM PER SRM 51-40-02. (M) 2L72 4F RTA16WE 20050322000732005032200073NM 2005 3 22 USAA050317 120050211A554265C2584151 SKIN BOEING737 7373B7 1384580NM RUDDER DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU50570 23706 FOUND EXT COMPOSITE SURF DELAMINATED .5 INCH LONG BY .0625 INCH WIDE SINGLE LAYER DAMAGE, RUDDER LEFT SIDE 66 INCHES FROM BOTTOM, 14 INCHES FROM T/E. REMOVED DAMAGED MATERIAL, INSTALLED REPAIR PLYS, SEALED AND REFINISHED PER SRM 51-70-17, EA 79999. (M) 2L72 4F RTA16WE 20050322000742005032200074NM 2005 3 22 USAA050315 120050211A554265C2584151 SKIN PANEL BOEING737 7373B7 1384580NM RUDDER DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU 23706 PIT - FOUND COMPOSITE SKIN PANEL DELAMINATED .5 INCH BY .0625 INCH SINGLE LAYER DAMAGE, LT SIDE RUDDER 57 INCHES FROM BOTTOM, 34 INCHES FROM T/E. INSTALLED REPAIR PLYS PER SRM 51-70-17 AND EA 79999. (M) 2L72 4F RTA16WE 20050322000752005032200075NM 2005 3 22 USAA050316 120050211A554265C2584151 SKIN BOEING737 7373B7 1384580NM RUDDER DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU50570 23706 PIT - FOUND EXT COMPOSITE SURFACE DELAMINATED 4 INCHES LONG BY .0625 INCHE WIDE SINGLE LAYER DAMAGE, RUDDER LEFT SIDE 38 INCHES FROM BOTTOM, 13.5 INCHES FROM T/E. REMOVED DAMAGED MATERIAL, INSTALLED REPAIR PLYS, SEALED AND REFINISHED PER SRM 51-70-17 AND EA 79999. (M) 2L72 4F RTA16WE 20050322000772005032200077NM 2005 3 22 SWAA050741 120050310A3350101114 LIGHT BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB PER MM. 2L72 4F RTA16WE 20050322000822005032200082NM 2005 3 22 SWAA050746 120050310A5311963820 FRAME BOEING737 7373L9 1384470NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND 2 EA OUTBOARD CHORD CRACKS AT BS 188, LBL 29 & RBL 29, WL 207. REPAIRED CHORD PER SRM. 2L72 4F RTA16WE 20050322000842005032200084NM 2005 3 22 SWAA050748 120050310A3350207377 LENS BOEING737 7377H4 1384404NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29471WN 32471 DURING SCHEDULED HC1 CHECK, FOUND FWD END OF EEPLS LENS MISSING. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20050322000852005032200085NM 2005 3 22 SWAA050749 120050310A53306545774 SKIN BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29686SW 23175 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 760, BELOW STR 18R. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050322000862005032200086NM 2005 3 22 SWAA050736 120050310A53306545780 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050322000892005032200089 2005 3 22 SWAA050739 420050310A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29765SW 29805 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20050322000912005032200091EU 2005 3 22 BA05005 120050304A3350321431 BATTERY AIRBUS330 A330323 3930335EU CABIN FAILED A USAAK NONE O OTHER ININSP/MAINT 1 EA19676UW 375 PHL - FOUND TWO EPSU BATTERIES THAT FAILED THE BITE TEST. MAINTENANCE REPLACED THE BATTERIES. 2L72 4F RTA46NM 20050322000922005032200092EU 2005 3 22 EM05007 120050310A32349037B000103 CONTROL LEVER EMB ERJ170ERJ170100 EU COCKPIT DEFECTIVE A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19818MD302 17000039 FLIGHT 1848, IND TO PIT - THE CREW COULD NOT RETRACT THE LANDING GEAR AFTER TAKEOFF. THE FLIGHT RETURNED TO IND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL LEVER. 2L74 4F RTA56NM 20050322000932005032200093EU 2005 3 22 SA05024 120050218A5610NP1653116 WINDSHIELD AIRBUSA319 A319112 3930323EU COCKPIT ARCED A USAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA19711UW6108 1033 DURING THE FLT, THE FIRST OFFICER'S WINDSHIELD BEGAN TO ARC. THE CREW PULLED THE APPROPRIATE CIRCUIT BREAKER AND CONTINUED THE FLIGHT. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FIRST OFFICER'S WINDSHIELD. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20050322000942005032200094NM 2005 3 22 BB05013 120050306A33501000679 SIGN BOEING767 7672B7 1385107NM COCKPIT MALFUNCTIONED A USAAK NONE O OTHER ININSP/MAINT 1 EA19656US 26847 CLT - FOUND COCKPIT EXIT SIGN ILLUMINATED WITH BATTERY SWITCH OFF. MAINTENANCE REPLACED THE SIGN. 2L72 4F RTA1NM 20050322000952005032200095EU 2005 3 22 SA05022 120050219A335032145410 EPSU AIRBUSA319 A319112 3930323EU CABIN FAULTY A USAAK NONE J WARNING INDICATION ININSP/MAINT 1 EA19717UW17038174 1069 DCA - DURING TEST, THE EMERGENCY POWER SUPPLY UNIT IN THE MID LEFT CABIN POSITION PRODUCED AN EMER L FAULT MESSAGE. MAINTENANCE REPLACED THE MID LEFT CABIN EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20050322000972005032200097NM 2005 3 22 SB05037 120050303A2751 INDICATOR BOEING737 7373B7 1384580NM COCKPIT MALFUNCTIONED A USAAO OTHER N FALSE WARNING DEDESCENT 1 EA19384US 22957 ALB - FLT920 - CREW RECEIVED A SPLIT FLAP INDICATION BETWEEN POSITIONS 2 AND 5, WITH GREEN LIGHT, ON DESCENT INTO ALB. NO ROLL WAS NOTICED. CREW DECLARED AN EMERGENCY AND PROCEEDED TO GO THROUGH CHECKLIST. APPROXIMATELY TEN MINUTES LATER, AS CHECKLIST WAS BEING PERFORMED, INDICATION BEGAN OPERATING NORMALLY. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PULLED AND RESET FLAP INDICATOR CIRCUIT BREAKER. INSPECTED LEFT AND RIGHT FLAP TRANSMITTER CONNECTORS. NO DEFECTS FOUND. OPERATED FLAPS THROUGH FULL RANGE. OPERATION NORMAL. AIRCRAFT OK FOR SERVICE. 2L72 4F RTA16WE 20050322000982005032200098NM 2005 3 22 SB05039 120050306A335020131A BATTERY PACK BOEING737 737401 1384701NM CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19405US 23885 PVD - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHTS AT THE L1 DOOR WON'T ILLUMINATE DURING OPERATIONAL TEST. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050322001022005032200102NE 2005 3 22 EM05006 220050306A73214120T01P02 FMU EMB ERJ170ERJ170100 EU GE CF34 CF348E5 30015NE NR 1 ENGINE MALFUNCTIONED A USAAK NONE J WARNING INDICATION UKUNKNOWN 1 EA19802MD 17000013 GEE193130 FLIGHT 1818, DCA TO CLE - ENGINE ONE NO DISPATCH FAULT MESSAGE. MAINTENANCE TROUBLESHOT SYSTEM IAW GE, EMB FAULT CODES. REMOVED AND REPLACED FUEL METERING UNIT AND FADEC, FAULT REMAINED. REMOVED AND REPLACED FUEL PUMP, FAULT CLEARED. 2L74 4F4 FRTA56NM E00063EN 20050322001032005032200103NM 2005 3 22 BB05010 120050222A33503020441 LIGHT BOEING757 7572B7 1384964NM CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19617AU 27148 CLT - FOUND THE SLIDE FLOOD EMERGENCY LIGHTS AT DOORS L4 AND R4 INOPERATIVE. MAINTENANCE RELAMPED THE LIGHT AT L4 AND REPLACED THE LIGHT SUBASSEMBLY AT DOOR R4. 2L72 4F RTA2NM 20050322001052005032200105EU 2005 3 22 BA05004 120050224A3350321431 BATTERY AIRBUS330 A330323 3930335EU CABIN FAILED A USAAK NONE O OTHER ININSP/MAINT 1 EA19678US 388 PHL - EMERGENCY BATTERY PACKS 4L AND 1R FAILED THE CAPACITANCE CHECK. MAINTENANCE REPLACED THE BATTERY PACKS. 2L72 4F RTA46NM 20050322001062005032200106EU 2005 3 22 SA05025 120050221A5610NP1653116 WINDSHIELD AIRBUSA319 A319112 3930323EU COCKPIT CRACKED A USAAHA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING O OTHER CRCRUISE 1 EA19733UW15120 1205 DEN - FLIGHT 1 EN-ROUTE PIT TO LAX. DURING FLIGHT, THE FIRST OFFICER'S WINDOW BEGAN TO CRACK. THE CREW PULLED THE WINDSHIELD HEAT CIRCUIT BREAKER AND DIVERTED TO DEN. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FIRST OFFICER'S WINDSHIELD. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20050323000042005032300004NM 2005 3 23 DLM88050168 120050317A4920 APU DOUG MD88 MD88 3023688NM PWA JT8 JT8D NE CONTAMINATED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27903DL14041 49534 P80424 ENGINE ANTI ICE ON NOTICED FAINT OIL SMELL, SMELL DISSIPATED WHEN TURNED OFF. ANTI ICE ON, SMELL RETURNED. FOUND APU CONTAMINATED WITH SKYDROL/OIL. CLEANED APU INLET AND PERFORMED FULL DUCT BURNOUT PER OPERATION 5089 AS PRECAUTIONARY. 2L72 4F4 FRTA6WE E2EA 20050323000052005032300005NM 2005 3 23 DL757050169 120050317A2121 FAN BOEING757 757232 1384965NM RIGHT FAILED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO27621DL 22911 DURING DESCENT AT FL200, F/A ADVISED OF SMOKE SMELL IN CABIN. AT SAME TIME COCKPIT ALSO HAD A SULFUR ODOR. REPLACED RT RECIRC FAN FOR PRODUCING ODOR. 2L72 4F RTA2NM 20050323000082005032300008SO 2005 3 23 C2XA05IA047 120050318A21214611028900 FAN EMB 145 EMB145XR 3260214SO RECIRCULATION INOPERATIVE A C2XAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW27141175917 5917 145674 IAH - FLIGHT 2372, THE CREW REPORTED A LAV SMOKE INDICATION IN FLIGHT, RECIRC FAN GIVING OFF BURNING SMELL. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE PLACED THE RECIRCULATION FAN ON MEL 21-24-01/2 CAT C CONTROL NUMBER 050074, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE DISCREPANCY REPEATED AND THE AIRCRAFT AGAIN RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND REMOVED AND REPLACED THE COCKPIT RECIRCULATION FAN, OPERATIONALLY CHECKED WITH NO DEFECTS. PERFORMED GROUND RUNS WITH NO EVIDENCE OF SMOKE DETECTED, CLEARED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20050323000102005032300010NM 2005 3 23 DL76G050160 120050311A2612 LOGIC CARD BOEING767 7673P6 1385105NM E/E BAY LOOSE A DALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO27152DL 24984 FIRE/OVERHEAT SYS EICAS ADVISORY ILLUMINATED DURING TAKEOFF. RESEATED CARDS. UNABLE TO DUPLICATE. TESTED SYSTEM. 2L72 4F RTA1NM 20050323000112005032300011NM 2005 3 23 DLM88050161 120050314A3320D77311001 BALLAST DOUG MD88 MD88 3023688NM EMERGENCY LIGHT FAILED A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO27985DL 53312 SMOKE IN CABIN COMING FROM OVERHEAD ROW 15. FOUND BALLAST BAD AT ROW 14 D, E (P1-2100). REPLACED BOTH BALLAST. ALSO REPLACED HARNESS THAT IS IN POOR CONDITION (DDL 339201635). PERFORMED OPERATIONAL CHECK, CHECKS NORMAL. 2L72 4F RTA6WE 20050323000122005032300012NE 2005 3 23 DL76G050162 220050315A7200CF680C2B6F ENGINE BOEING767 767332 1382001NM GE CF6 CF680C2B6F 30025NE NR 2 LEAKING A DALAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO271612T13600 30575 706131 ENGINE SHUTDOWN BY CREW AT CRUISE DUE TO OIL QTY DROPPED TO 0 AND OIL PRESSURE STARTED FLICKERING. REPLACED ENGINE. 2L72 4F4 FRTA1NM E13NE 20050323000142005032300014NM 2005 3 23 DLM90050164 120050312A5330 SKIN DOUG MD90 MD9030 3023690NM AFT FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27905DA 53385 CRACK OF 2 INCH ON SKIN OF AFT FUSELAGE STA Y=953.604 AND INTERSECTION OF LONGERON 23 LT. REPAIRED SAME. 2L72 4F RTA6WE 20050323000152005032300015WP 2005 3 23 ABXA050072 120050307A5311991960317 FRAME DOUG DC9 DC931 3022065WP AFT CARGO CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23949AX 47325 FRAME CRACKED FS 889 AT LONGERON 29 LEFT. REPAIRED CRACKED FRAME FLANGE IAW DC-9 SRM DWG K05159. 2L72 4F A6WE 20050323000162005032300016WP 2005 3 23 ABXA050073 120050308A5320991224617 WEB DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23949AX 47325 STA 1038 BULKHEAD AT LONGERON 13 LEFT WAS CRACKED AT LIGHTENING HOLE. REPAIRED IAW DC-9 SRM 53-01. 2L72 4F A6WE 20050323000242005032300024EA 2005 3 23 SWIA200514722 120050315A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07435SW 7555 LEFT FORWARD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LEFT FORWARD EMERGENCY LIGHT IAW MM 33-51-21, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050323000292005032300029EU 2005 3 23 05FDEA00548 120050315A5347 SEAT TRACK AIRBUS310 A310222 3930315EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 NR 1 SEAT TRACK, FR61.5, FR 62.5, FR64.5, FR65.5, FR66.5, FR70.5, HAS 9 AREAS CORROSION INSIDE SCALLOPED HOLES. REMOVED CORROSION IAW SRM 51-74-10, SEVERAL AREAS OUT OF LIMITS IAW SRM 53-10-16 FIG 601. CUT OUT 2EA SEAT TRACKS FROM 2EA SEAT TRACKS IAW SRM 51-10-16 FIG 208, INSTALLED 2EA TRACKS AND SPLICES IAW 51-10-16 FIG 208. 2L72 4F RTA35EU 20050323000302005032300030CE 2005 3 23 69686 120050311A3260 BULB BEECH 1900 1900D 1154162CE MLG INDICATOR BURNED OUT A AMWAO OTHER P NO WARNING INDICATION LDLANDING 1 CE07167YV UE167 UPON GEAR EXTENSION FOR LANDING IN PIT, CREW NOTED NOSE GEAR ANNUNCIATOR DID NOT SHOW GEAR DOWN AND LOCKED. CREW C/W EMERGENCY CHECKLIST AND DECLARED AN EMERGENCY. LANDED SAFELY WITH NO FURTHER INCIDENT. MAINTENANCE FOUND BULBS BAD. MAINTENANCE RELAMPED ANNUNCIATOR AND PERFORMED GEAR SWING. OPS CHECK NORMAL. 2L72 4T RTA24CE 20050323000312005032300031EA 2005 3 23 COMA0560180 120050315A323046193 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA MLG UNRELIABLE A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01976CA1454111771 7151 FLIGHT 5387 GEAR DISAGREE WARNING. REPLACED THE MLG PRIORITY VALVE. 2L72 4F RTA21EA 20050323000352005032300035 2005 3 23 COMA0560183 420050316A3418 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA STALL FAIL ILLUMINATED A COMAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 SO01984CA 7171 FLIGHT 5687 STALL FAIL MESSAGE AFTER T/O. FOUND 02 SERVICE DOOR OPEN. CLOSED DOOR. 2L72 4F RTA21EA 20050323000362005032300036EA 2005 3 23 COMA0570031 120050315A2810T99A38603 EJECTOR CNDAIRCL600 CL6002C10 1390015EA RT FUEL TANK CRACKED A COMAO OTHER O OTHER NRNOT REPORTED 1 SO01379CA 10102 FLIGHT 5285 FUEL TRANSFERRING FROM RIGHT TANK TO CENTER TANK. REPLACED THE PRIMARY EJECTOR. 2L72 4F RTA21EA 20050323000372005032300037CE 2005 3 23 DXTA200500635 120050319A3260 WARNING LIGHT RAYTHNDH125 HAWKER800XP 7150012CE MLG ILLUMINATED E DXTAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL07873QS 258573 WHEN GEAR WAS RETRACTED ON TAKEOFF RIGHT RED LIGHT WAS ILLUMINATED. GROUND PERSONNEL NOTED THAT THE GEAR APPEARED DOWN. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA3EU 20050323000382005032300038CE 2005 3 23 DXTA200500638 120050320A2751 WARNING LIGHT CESSNA750 750 2076810CE TE FLAPS ILLUMINATED E DXTAO OTHER J WARNING INDICATION DEDESCENT 1 GL07960QS 7500160 FLAPS FAIL EICAS MESSAGE ILLUMINATED WHILE SELECTING FLAPS 5 DEG INTO EGE RAN FLAPS FAIL CHECK LIST & FLAPS WOULD NOT RESET. ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20050321000242005032100024EU 2005 3 21 MALA050249 120050301A3211 ATTACH FITTING BAC 146 AVRO146RJ85A1500097EU RT MLG CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15502XJ E2307 DURING C2 CHECK IN YYC FOUND RT MLG AFT ATTACH FITTING P/N HC321H0002-00, FOUND TO HAVE FRETTING DAMAGE ON FACE. DAMAGE .002 INCH TO .009 INCH DEEP. 2H74 4F RTA49EU 20050321000252005032100025 2005 3 21 MALA050254 420050305A2210 COMPUTER SAAB SF340 340B 7860101EU AUTOPILOT MALFUNCTIONED A MALAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 GL15423XJ 340B423 AFTER TAKEOFF AUTOTRIM WARNING AND AUTOPILOT DISCONNECT. AUTOTRIM WARNING EXTINGUISHED. CREW NOTED AN UNUSUAL SMELL IN THE FLIGHT DECK. REPORTED, SMELLS LIKE INSULATION. AIR RETURN TO DTW. PERFORMED OP CHECK OF AUTOTRIM SYSTEM. CND PROBLEM. AUTOTRIM OP CHECK GOOD. INSPECTED ELEC BAY, AVIONICS RACK AND FOUND NO DEFECTS. PERFORMED OP CHECKS OF ALL AVIONICS EQUIPMENT. ALL CHECKS GOOD. 2L72 4T RTA52EU 20050321000362005032100036EU 2005 3 21 MALA050269 120050312A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15433XJ 340B433 DURING 4Y/2Y CHECK IN BNA FOUND LEFT SIDE AISLE SEAT TRACK LBL 18.3 CORRODED AT STA 300 OUT OF LIMIT. REPAIRED DAMAGE REF SRM 53-70-60. WORK PERFORMED ON EMB WO 211832 TASK 1517. 2L72 4T RTA52EU 20050321000412005032100041NM 2005 3 21 SWAA050795 120050315A57536546435334 SKIN BOEING737 7373A4 1384585NM RT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED ON OUTBOARD EDGE LOWER SKIN. REMOVED AND REPLACED FLAP ASSY PER MM. 2L72 4F RTA16WE 20050321000442005032100044EU 2005 3 21 MALA050274 120050317A2120 SMOKE SAAB SF340 340B 7860101EU COCKPIT DETECTED A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL15414XJ 340B414 AFTER DEPARTING MQT FLIGHT 3141, SMOKE WAS EMITTING FROM THE CAPTAINS LEFT HAND SIDE PANEL. PANEL BETWEEN THE CIRCUIT BREAKERS AND THE CAPTAIN'S SIDE WINDOW. EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO MQT WITHOUT FURTHER INCIDENT. NO FURTHER INFORMATION AT THIS TIME. WILL SUBMIT INFORMATION WHEN RECEIVED. 2L72 4T RTA52EU 20050321000952005032100095EU 2005 3 21 MALA050236 120050213A2120 ODOR SAAB SF340 340B 7860101EU COCKPIT DETECTED A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL15449XJ 340B449 THE AIR IN THE CABIN AND FLIGHT DECK SMELLS VERY STRONG WITH AN ENGINE OIL ODOR. ODOR STARTED OUT VERY STRONG AT THE START OF THE FLIGHT AND CONTINUED THROUGHOUT THE FLIGHT DECREASING SLIGHTLY. THE AIR QUALITY WAS VERY BAD EVEN WITH JUST ONE BLEED ON. TESTED BOTH BLEEDS. RAN RT ENGINE 20 MINS WITH ENGINE INTAKE HEAT ON TO BURN OUT COMP WASH FLUID FROM COMP WASH. PERFORMED 2/12/05, ODOR DECREASED DURING 20 MIN RUN. AIRCRAFT RELEASED BACK TO SERVICE. 2L72 4T RTA52EU 20050321001012005032100101NM 2005 3 21 SWAA050798 120050315A3350PH22300L LIGHT BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED RON CHECK, FOUND FWD SECTION OF EEPLS STRIP LOOSE. REMOVED AND REPLACED EEPLS STRIP PER MM. 2L72 4F RTA16WE 20050321001032005032100103NM 2005 3 21 SWAA050800 120050315A53106547978 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29607SW 27927 DURING SCHEDULED D-CHECK, FOUND CORROSION ON CREASE BEAM WEB AT BS 300, WL 208, RBL 50. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050321001102005032100110SO 2005 3 21 SWIA200514692 120050309A275012064207615 SELECTOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07295SW6619 6619 120322 FLAP CONTROL FAULT WHEN SELECTING FLAPS DOWN. REPLACED FLAP SELECTOR LEVER ASSY WITH SERVICEABLE UNIT. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050321001232005032100123EA 2005 3 21 SWIA200514698 120050312A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07935SW 7725 RIGHT REAR EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED RIGHT REAR EXTERIOR EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050321001382005032100138NM 2005 3 21 QXEA200500374 120050202A5753 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 600 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - RIGHTHAND OUTBOARD FLAP IS CHAFING THE UPPER WING SHROUD. REPAIRED IAW DHC-8 SRM 51-21-12 AND 51-25-10. 2H72 4T RTA13NM 20050321001562005032100156SO 2005 3 21 126222405 120050224A3260 WARNING LIGHT GULSTMG1159 GIV 3980115SO NLG ILLUMINATED E N93AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO13462QS 1262 UPON GEAR RETRACTION MAIN NORMAL, NOSE WHEEL INDICATION GREEN AND HANDLE UNSAFE LIGHT WAS ILLUMINATED. WHEN GEAR WAS PLACED IN THE DOWN POSITION THE INDICATIONS REMAINED THE SAME. 2L72 4F RTA12EA 20050321001902005032100190WP 2005 3 21 AALA20050195 120050314A33506011779 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21963TW 53613 AUS - OVERWING EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK AT B5 49 FOR OVERWING EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050321002082005032100208EU 2005 3 21 RAIA00503004 120050308A3150 WARNING LIGHT JETAIRJETSTMJETSTM4101 1500501EU ENGINE ILLUMINATED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03568HK 41086 PIT - INTERGRADED ENGINE CONTROL FAULT INDICATION. MAINTENANCE CLEARED IEC FAULTS AND OPS CHECKED OK. 2L72 4T RTA41NM 20050321002202005032100220EU 2005 3 21 ASOA05086 120050112A5320S5337129320201 SUPPORT AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27534AS 463 DURING A C-CHECK, THE SUPPORT PLATE BETWEEN FR 13 TO 18 AT FLOOR LEVEL ON THE LT SIDE WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SUPPORT PLATE BETWEEN FR 13 TO 18 AT FLOOR LEVEL ON THE LT SIDE IAW SRM. (K) 2H72 4T4 TRTA53EU E20NE 20050321002242005032100224EU 2005 3 21 ASOA05051 120050120A3230 BRACKET AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE RT MLG CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27637AS 383 DURING HANGAR MAINTENANCE, THE RT MAIN LANDING GEAR UPSTOP BRACKET WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RT MLG UPSTOP BRACKET IAW SRM. (K) 2H72 4T4 TRTA53EU E20NE 20050321002252005032100225EA 2005 3 21 ASOA05027 120050114A3350BC50393105 COVER BRUCE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN MISSING A ASOAK NONE O OTHER ININSP/MAINT 1 SO27827AS 7212 DURING A GROUND INSPECTION, THE EMERGENCY EXIT SIGN COVER BY THE PASSENGER DOOR WAS FOUND MISSING. MAINTENANCE INSTALLED AN EMERGENCY EXIT SIGN COVER BY THE PASSENGER DOOR. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050321002322005032100232EA 2005 3 21 ASOA05016 120050105A3350BR9279013 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27914EV 7752 DURING HANGAR MAINTENANCE, THE EMERGENCY EXIT LIGHT AT THE PASSENGER DOOR IN THE FORWARD LOWER SECTION WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY AT THE PASSENGER DOOR IN THE FORWARD LOWER SECTION. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050321002352005032100235EA 2005 3 21 ASOA05052 120050121A2781 WARNING SYSTEM CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE COCKPIT MALFUNCTIONED A ASOAK NONE N FALSE WARNING APAPPROACH 1 SO27719EV 10099 DURING APPROACH, FOLLOWING SELECTION OF THE FLAPS TO 8 DEGREES, THE CREW RECEIVED A (SLATS FAIL) MESSAGE. THE QRH WAS COMPLIED WITH AND EMERGENCY VEHICLES REQUESTED TO BE ON STANDBY AS A PRECAUTION. THE AIRCRAFT LANDED SAFELY. MAINTENANCE NOTED THAT THE MAINTENANCE DIAGNOSTIC COMPUTER RECORDED AN ACTUATOR SYSTEM FAILURE-MECHANICAL JAM. MAINTENANCE VISUALLY VERIFIED THE SLATS WERE AT ZERO AND FULLY RETRACTED. THE AIRCRAFT WAS POWERED DOWN AND UP WITH THE MESSAGE CLEARING. MAINTENANCE ALSO CYCLED THE SLAT SYSTEM SEVERAL TIMES. OPERATIONAL CHECKS GOOD. AC OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA EOOO63EN 20050321002362005032100236 2005 3 21 ASOA05053 420050121A3418601R383303 VANE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE STALL WARNING MALFUNCTIONED A ASOAA UNSCHED LANDING N FALSE WARNING TOTAKEOFF 1 SO27885AS 7521 DURING TAKEOFF, THE STALL WARNING SYSTEM ACTIVATED EXCEPT THE PUSHER. THE AIRCRAFT DID NOT STALL. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED TO DEPARTURE AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE LT AOA VANE AND ALSO THE STALL PROTECTION COMPUTER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050321002402005032100240EU 2005 3 21 ASOA05093 120050117A5330 SKIN AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27534AS 463 DURING A C-CHECK, THE LOWER FUSELAGE SKIN AT THE ADF ANTENNA AREA BETWEEN FR 23 TO 23A, STRINGERS 21L-21R WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE LOWER FUSELAGE SKIN AT THE ADF ANTENNA AREA BETWEEN FR 23 TO 23A, STRINGERS 21L-21R IAW EO. (K) 2H72 4T4 TRTA53EU E20NE 20050321002432005032100243EA 2005 3 21 ASOA05056 120050121A3350PL22300LH00 LIGHT CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE GALLEY MISSING A ASOAK NONE O OTHER ININSP/MAINT 1 SO27740EV 10151 DURING A GROUND INSPECTION, THE EMERGENCY FLOOR LIGHTING NEAR THE GALLEY WAS FOUND MISSING. MAINTENANCE INSTALLED THE EMERGENCY FLOOR LIGHT STRIP NEAR THE GALLEY. (K) 2L72 4F4 FRTA21EA EOOO63EN 20050321002462005032100246EA 2005 3 21 ASOA05054 120050121A361032156222 REGULATOR VALVE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE BLEED AIR SYS MALFUNCTIONED A ASOABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27909EV6867 7658 DURING CRUISE, AT APPROXIMATELY 37,000 FT, CREW RECEIVED A RT PACK HIGH TEMP MASTER CAUTION. CREW REQUESTED DESCENT TO 25,000 FT WHILE COMPLYING WITH CHECKLIST FOLLOWED BY THE RT PACK HIGH TEMP MASTER CAUTION GOING OUT. PACK DID NOT RESET OR COME ON. UPON LEVELING TO 25,000 FT A LT PACK HIGH PRESSURE MASTER CAUTION WAS RECEIVED. CREW REQUESTED EMERGENCY DESCENT TO 10,000 FT WITH THE FIRST OFFICER COMPLYING WITH THE CHECKLIST. AN EMERGENCY WAS DECLARED WITH THE TOWER INSTRUCTING THE AIRCRAFT TO DIVERT. THE AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED RT PRESSURE REGULATING VALVE AND ALSO GROUND RAN LT PACK WITH NO DEFECTS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050321002472005032100247EA 2005 3 21 ASOA05045 120050119A5210 SEAL CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE PAX DOOR DIRTY A ASOAK NONE O OTHER ININSP/MAINT 1 SO27701EV 10020 DURING A GROUND INSPECTION, THE CREW REPORTED THE PASSENGER DOOR WAS HARD TO CLOSE WITH AN AIR LEAK NOTICED AROUND THE DOOR DURING FLIGHT. MAINTENANCE CLEANED AND INSPECTED THE PASSENGER DOOR SEAL. MAINTENANCE THEN PRESSURIZED THE AIRCRAFT WITH NO LEAKS NOTED. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA EOOO63EN 20050321002532005032100253EU 2005 3 21 ASOA05035 120050114A2750855D1009 BPSU AEROSPATR72 ATR72 EU PWA PW120 PW127 NE T/E FLAP MALFUNCTIONED A ASOAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27883AS4549 215 7504 DURING CRUISE, AT APPROXIMATELY 25,000 FEET THE CREW RECEIVED A FLAP FAIL MESSAGE WITH THE FLIGHT CONTROL PAGE SHOWING BOTH THE LT AND RT FLAPS AT ZERO DEGREES. THE QRH WAS COMPLIED WITH, AND EMERGENCY DECLARED AND THE AIRCRAFT RETURNED TO DEPARTURE, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE LT BRAKE AND POSITION SENSOR UNIT (BPSU) AND ALSO THE FLAP ELECTRONIC CONTROL UNIT (FECU). OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2H72 4T4 TRT E20NE 20050321002592005032100259NM 2005 3 21 AMTA200500218 120050226A335021007 SWITCH BOEING757 75723N 1384973NM CABIN BROKEN A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11520AT 27976 EMERGENCY LIGHT TEST SWITCHES INOPERATIVE OVER L3 AND L4 DOOR IN CABIN. REPLACED BROKEN SWITCH AND REWIRED SWITCHES CORRECTLY IAW WDM 33-51-15. (M) 2L72 4F RTA2NM 20050321002682005032100268EA 2005 3 21 ASOA05102 120050205A5210H341427 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR LACK OF LUBE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27820AS 7188 FLT 4360 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WOULD NOT OPEN FROM THE OUTSIDE. MAINTENANCE CLEANED AND LUBRICATED THE PASSENGER DOOR HANDLE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050321002702005032100270EA 2005 3 21 ASOA05158 120050226A5260601R3167013 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27838AS 7276 FLT 4533 - DURING A GROUND INSPECTION IN ATL, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN AT THE FOLDING ROD CONNECTION POINT. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050321002762005032100276EA 2005 3 21 ASOA05163 120050205A5320 DOUBLER CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27701EV 10020 DURING HANGAR MAINTENANCE IN CKB, THE FS 280 DOUBLER AT RBL 36 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FS 280 DOUBLER AT RBL 36 IAW ASA EO 700-53-0037. (M) 2L72 4F RTA21EA 20050321002772005032100277EA 2005 3 21 ASOA05161 120050222A5210 DOOR FRAME CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27828AS 7213 DURING A C-CHECK IN MCN, THE PASSENGER DOOR INNER FRAME AT FS 320 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE PASSENGER DOOR INNER FRAME AT FS 320 IAW BOMBARDIER REO 601R-52-11-678. (M) 2L72 4F RTA21EA 20050321002812005032100281EA 2005 3 21 ASOA05159 120050221A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27923EV 7826 DURING A C-CHECK IN HOT, THE FLOOR SUPPORT ANGLE AT FS 621 LEFT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FLOOR SUPPORT ANGLE AT FS 621 LT IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20050321002822005032100282EA 2005 3 21 ASOA05150 120050221A5260601R3198067 STEP CNDAIRCL600 CL6002C10 1390015EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27707EV 10057 DURING A GROUND INSPECTION IN OKC, THE STRUT ON THE PASSENGER DOOR BOTTOM STEP WAS FOUND BROKEN OFF. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ASSEMBLY AND THE CONNECTING ROD SUPPORT ON THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050321002842005032100284EA 2005 3 21 ASOA05148 120050221A5260601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27842AS 7304 FLT 4418 - DURING A GROUND INSPECTION IN ATL, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050321002862005032100286EA 2005 3 21 ASOA05112 120050207A5320601R3117117 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27846AS 7328 DURING A C-CHECK IN MCN, THE INBOARD CLIPS AT FS 484, LBL 27 AND RBL 27 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE INBOARD CLIPS AT FS 484, LBL 27 AND RBL 27 IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20050321002912005032100291EA 2005 3 21 ASOA05128 120050213A2120 SMOKE CNDAIRCL600 CL6002B19 1900309EA CABIN DETECTED A ASOAK NONE BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION APAPPROACH 1 SO27835AS 7258 FLT 4355 - DURING APPROACH INTO CVG FROM BNA, AFTER SWITCHING THE BLEEDS FROM THE ENGINES TO THE AUXILIARY POWER UNIT, THE CREW SMELLED AND SAW VISIBLE SIGNS OF SMOKE FOLLOWED BY A LAV SMOKE WARNING MESSAGE. THE AIRCRAFT LANDED SAFELY IN CVG. MAINTENANCE HAD THE FLIGHT CREW RUN THE ENGINES AND PERFORM A FUNCTIONAL CHECK OF THE PACKS. NO DEFECTS WERE NOTED. MAINTENANCE INSPECTED THE LEFT AND RIGHT AIR CYCLE MACHINES FOR OIL, INSPECTED THE DUCTING, AUXILIARY POWER UNIT AND AFT EQUIPMENT BAY FOR INDICATIONS OF SMOKE. NO OIL WAS FOUND AND NO DEFECTS WERE NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050321002932005032100293EA 2005 3 21 ASOA05138 120050217A3350BR9279232 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27836AS 7263 DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY FLOODLIGHT AT THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOODLIGHT ASSEMBLY AT THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. (M) 2L72 4F RTA21EA 20050322000012005032200001EA 2005 3 22 A6WA200540088 120050307A27413094334 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA COCKPIT STICKS A A6WAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 GL31424AW 7656 UNCOMMANDED STAB TRIM RUNAWAY. AUTOPILOT OFF, FIRST OFFICER FLYING. PILOT TRIM CLACKER OVERODE, OPS OK. FOUND FIRST OFFICERS TRIM SWITCH STICKING. REMOVED AND REPLACED SWITCH IAW 27-41-05. OPS CHECK GOOD. (M) 2L72 4F RTA21EA 20050322000102005032200010EA 2005 3 22 ASOA05142 120050217A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27848AS 7339 DURING A C-CHECK IN MCN, THE INBOARD AND OUTBOARD CLIPS AT FS 280 LEFT AND RIGHT WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE INBOARD AND OUTBOARD CLIPS AT FS 280 LEFT AND RIGHT. (M) 2L72 4F RTA21EA 20050322000142005032200014EA 2005 3 22 ASOA05127 120050213A21508084402 CONTROL VALVE CNDAIRCL600 CL6002B19 1900309EA A/C BAY DEFECTIVE A ASOAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27922EV 7822 FLT 4918 - DURING CLIMB-OUT FROM TYS-TPA, AT APPROXIMATELY 4,000 FEET WITH THE AUXILIARY POWER UNIT DEFERRED, THE CREW NOTICED A SMELL OF SMOKE IN THE COCKPIT FOLLOWED BY SMOKE FILLING THE COCKPIT. THE CREW IMMEDIATELY DONNED THEIR OXYGEN MASKS AND SUBSEQUENTLY RECEIVED A LEFT PACK OVERTEMP MESSAGE. THE QRH WAS COMPLIED WITH, AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED TO TYS. DURING DESCENT SMOKE DRIFTED INTO THE CABIN AND THEN CLEARED IN THE COCKPIT AND CABIN. THE AIRCRAFT LANDED SAFELY IN TYS. MAINTENANCE REMOVED AND REPLACED THE AIR CYCLE MACHINE DUCT ASSEMBLY DUAL BYPASS CONTROL VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050322000302005032200030EA 2005 3 22 ASOA05109 120050206A33502013BR BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA CABIN DISCHARGED A ASOAK NONE O OTHER ININSP/MAINT 1 SO17824AS 7203 FLT 4842 - DURING A GROUND INSPECTION IN ATL, THE FORWARD EMERGENCY LIGHTS WERE FOUND ILLUMINATING WITH THE EMERGENCY LIGHTS SWITCH IN THE OFF POSITION. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHTS BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050322000392005032200039NM 2005 3 22 GAIA05009ST 120050301A5330 SKIN BOEING727 727214 138407RNM FUSELAGE DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07750US 21512 DURING C-CHECK, A DENT AND GOUGE WAS FOUND AT FS 630 ON THE MAIN CARGO DOOR DOUBLER. INSTALLED 8 INCH BY 10 INCH DOUBLER REPAIR IAW KITTY HAWK EA B7-53-123. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20050322000542005032200054SO 2005 3 22 2005F00055 120050204A361022037032 DUCT EMB 120 EMB120ER 3260203SO A/C BAY LEAKING A GUUAO OTHER J WARNING INDICATION CRCRUISE 1 SO17268AS 120202 FLT 9227 - FLL/NAS - DURING FLIGHT, LEFT DUCT LEAK LIGHT ILLUMINATED. RETURNED TO FLL. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED LEFT PACK BLEED AIR DUCT. OPERATIONAL CHECK NORMAL. (M) 2L72 4T RTA31SO 20050322000622005032200062SO 2005 3 22 SIMA200506107 120050225A531314533888001 STRINGER EMB 135 EMB135KL 3260302SO FUSELAGE GOUGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21801AE 145469 ABI - DURING INSPECTION OF AIRCRAFT, STRINGER 19L AS FOUND TO BE GOUGED BETWEEN FRAMES 49 AND 50. BLENDED OUT THE GOUGE. PERFORMED EDDY CURRENT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED A REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM-145/1142 REV 28 CHAPTER 53-24-02. (M) 2L72 4F RTT00011AT 20050322000782005032200078NM 2005 3 22 SWAA050742 120050310A3350BR2013 STRIP BOEING737 7373H4 1384600NM CABIN WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED C3 CHECK, FOUND SEVERAL EEPLS STRIPS WORN. REMOVED AND REPLACED EEPLS STRIPS PER MM. 2L72 4F RTA16WE 20050322000792005032200079NM 2005 3 22 SWAA050743 120050310A53306545780 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29607SW 27927 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050322000962005032200096EU 2005 3 22 SA05023 120050220A252010BM3300 CUSHION AIRBUSA319 A319112 3930323EU CABIN CONTAMINATED A USAAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA19755US 1331 JAX FLIGHT 175, EN-ROUTE DCA TO JAX - A FUEL ODOR WAS REPORTED DURING FLIGHT, AT SEAT ROW NUMBER 15 ON THE RIGHT HAND SIDE OF THE PLANE. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND A PETROLEUM ODOR AT SEAT 14F. MAINTENANCE REPLACED THE SEAT CUSHION AND COVER ON BOTH SEAT 14E AND 14F. ODOR IS NO LONGER PRESENT. OK FOR SERVICE. 2L72 4F RTA28NM 20050322000992005032200099NM 2005 3 22 BB05008 120050212A3350 PIN BOEING757 7572B7 1384964NM CABIN FAULTY A USAAK NONE L NO TEST ININSP/MAINT 1 EA19614AU 27145 CLT - MAINTENANCE REPORTED THE L3 AND R3 DOOR EXTERIOR EMERGENCY LIGHTS DO NOT OPERATE WHEN NLG TEST SWITCH IS USED. INSIDE LIGHTS ARE ALSO INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE MALE AND FEMALE PINS AT CONNECTOR D40490 PIN D. ALSO, REPLACED EMERGENCY LIGHT TEST SWITCH S10035 AND EMERGENCY LIGHT POWER SUPPLY M734 DUE TO WEAK BATTERY. OPERATIONAL CHECK OF SYSTEM NORMAL. 2L72 4F RTA2NM 20050322001042005032200104EU 2005 3 22 BA05006 120050306A3350321431 BATTERY AIRBUS330 A330323 3930335EU CABIN FAILED A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW 342 PHL - THE 1R (12WL) AND 2L (13WL) DOOR EPSU BATTERIES FAILED THE CAPACITY TEST. MAINTENANCE REPLACED THE BATTERIES. 2L72 4F RTA46NM 20050323000012005032300001NM 2005 3 23 DL738050166 120050313A2913849589 PUMP BOEING737 737832 13844CFNM CFMINTCFM567CFM567B22 13802NE NR 2 ENGINE UNSERVICEABLE A DALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO273771K 29632 888888 NR 2 ENG HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED. AFTER ABOUT 1 HOUR B-SYSTEM FLUID LEVEL DECREASED TO ZERO. FOUND FLUID LEAKING FOR ENG DRIVEN HYD PUMP. REPLACED ENG HYD PUMP AND ELECT HYD PUMP. REPLACED EMDP AND EDP PRESSURE FILTER AND CASE DRAIN FILTER ALONG WITH B-SYSTEM RETURN FILTER. OPS CHECK AND LEAK CHECK GOOD. 2L72 4F4 FRTA16WE E00055EN 20050323000022005032300002SO 2005 3 23 C2XA05TY028 120050320A553114525669001 FITTING EMB 145 EMB145ER 3260211SO VERTICAL STAB CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715941 145035 TYS, DURING A SCHEDULED INSPECTION FRAME 75, SPAR 1 FITTING SHOWS SIGNS OF FRETTING. MAINTENANCE REMOVED THE FITTING, BLENDED CORROSION ON INNER SKIN SURFACE, DYE PENATRANT TESTED THE AREA, TREATED FOR CORROSION, DRILLED AND INSTALLED A NEW FITTING IAW EC5310-01317, EMB-135/145, SRM 51-10-03, 51-20-03, 51-40-02 AND CMP 51-21-04. 2L72 4F RTT00011AT 20050323000062005032300006SO 2005 3 23 C2XA05BT013 120050308A33501317 BULB EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT BURNED OUT A C2XAK NONE O OTHER ININSP/MAINT 1 SW2724103 145645 DURING SERVICE AND ROUTINE CHECKS ON RON MAINTENANCE FOUND THE FORWARD CABIN AISLE EMERGENCY LIGHT NOT WORKING. REMOVED AND REPLACED FORWARD CABIN AISLE EMERGENCY LIGHT LAMP IAW EMB145XR AMM 33-50-08. OPS CHECKED GOOD. 2L72 4F RT 20050323000132005032300013 2005 3 23 DL76L050163 420050315A2330 BEARING BOEING767 767332 1382001NM FAN WORN A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27177DN 110 25122 STRONG ELECTRICAL ODOR IN FLT DECK AROUND PASSENGER VIDEO SYSTEM. NO SMOKE REPORTED. TURNED IFE POWER OFF AND ODOR WENT AWAY. FOUND FWD EQUIPMENT EXHAUST FAN MAKING BEARING NOISE AND PRODUCING ODOR. REPLACED SAME. 2L72 4F RTA1NM 20050323000172005032300017GL 2005 3 23 P5CA0501330 220050316A7200CF680C2 ENGINE BOEING747 74746NF 13848BTNM GE CF6 CF680C2* GL NR 4 VIBRATION A P5CAO OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 EA15451PA 30809 706216 EXCEEDANCE REPORT ON ENGINE NR 4 VIBRATION, .4 AFTER ENGINE START. REPLACED NR 4 ENGINE DUE TO VSV LEVER ARM BROKEN ON 5TH STAGE IAW P71-00-001A/2A POLAR ENGINE CHANGE WORK CARDS. 2L74 4F4 FRTA20WE E23EA 20050323000192005032300019EU 2005 3 23 05FDEA00559 120050315A5347 SEAT TRACK AIRBUS310 A310222 3930315EU FUSELAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25419FE 345 M DECK COMP'T NR 1 SEAT TRACK, FR45.5, FR48, FR49, FR52, FR52.5 FR53.5, 6-EA AREAS OF CORROSION INSIDE SCALOPE HOLES AS MARKED. REMOVED CORROSION IAW SRM 51-74-10, OUT OF LIMITS BETWEEN FR52 & 54 IAW 53-10-16 FIG 101. CUT OUT & FABBED NEW REPAIR SECTION OF SEAT TRACK AND SPLICES IAW SRM 53-10-16 FIG 205. TREATED, PRIMED & TOPCOATED IAW SRM 51-23-20 & 51-75-10. INSTALLED SEAT TRACK & SPLICES FROM FRAME 51.5 TO 54 IAW SRM 51-10-16 FIG 205. 2L72 4F RTA35EU 20050323000212005032300021NM 2005 3 23 AALA20050204 120050317A3350 LIGHT BOEING737 737823 13844BZNM CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21926AN 29527 DFW - EMERGENCY LIGHT EXIT IDENTIFIER L 1186 AT RIGHT NUMBER ONE DOOR DAMAGED. REPLACED EMERGENCY LIGHT EXIT IDENTIFER ASSEMBLY AT L1186 AT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20050323000222005032300022EA 2005 3 23 SWIA200514720 120050312A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07406SW 7030 EMERGENCY FLOOD LIGHT IN CABIN ABOVE ROW 10 IS BURNED OUT. REMOVED AND REPLACED EMERGENCY LAMP ABOVE ROW 10. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050323000392005032300039EA 2005 3 23 VNAA0503002 120050303A2751 WARNING HORN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS ACTIVATED A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL05216PS 7882 DURING CLIMB (PIT TO IND) AT FL 280 AND 320 KTS IAS THE FLAP OVERSPEED WARNING HORN SOUNDED. AS THE CREW OF FLIGHT 2358 SLOWED THE AIRCRAFT PER THE QRH, HYDRAULIC PUMP 2B & 3B CAUTION MESSAGES ILLUMINATED. THE CREW TURNED ON ALL HYDRAULIC PUMPS. THE EICAS FLIGHT CONTROL PAGE SHOWED FLUCTUATION OF THE LEFT FLAPS FROM 0 TO 37 DEGREES. THE CREW ELECTED TO DIVERT TO DAY AND MADE AN UNEVENTFUL ZERO FLAP LANDING. PSA MAINTENANCE OPERATIONALLY CHECKED THE FLAP POSITION TRANSMITER IAW CRJ 200 AMM 27-55-01-710-801. THE SYSTEM OPERATIONALLY CHECKED GOOD. AN OPERATIONAL CHECK FLIGHT WAS PERFORMED. ALL SYSTEMS WERE FOUND TO BE SATISFACTORY. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050323000402005032300040EA 2005 3 23 VNAA0503004 120050304A2913887055 PUMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE HYD SYSTEM FAILED A VNAAO OTHER O OTHER NRNOT REPORTED 1 GL05228PS2327 7897 INBOUND TO DCA THE HYD 2 LOW PRESS MESSAGE ILLUMINATED. WHILE FOLLOWING THE QRH THE MESSAGE WENT OUT AND THE HYD EDP 2A MESSAGE APPEARED. THE CREW OF FLIGHT 2344 CONTINUED TO DESTINATION AND MADE AN UNEVENTFUL LANDING AT DCA. PSA MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE DRIVEN HYDRAULIC PUMP IAW CRJ 200 AMM 29-11-01-400-801. OPERATIONAL TESTS AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050323000412005032300041EA 2005 3 23 VNAA0503003 120050303A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A VNAAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL05260JS 7897 THE CREW OF FLIGHT 2396 REPORTED THAT THE FLAPS FAILED AT ZERO DEGREES ON APPROACH TO BTV. THE CREW DECLARED AN EMERGENCY, PREPPED THE CABIN, AND MADE AN UNEVENTFUL ZERO FLAP APPROACH AND LANDING AT BTV. CONTRACT MAINTENANCE RESET THE FLAP CONTROL UNIT IAW RSSL00-001. THE FLAP SYSTEM OPERATIONALLY CHECKED GOOD. NO DEFECTS WERE NOTED. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050323000422005032300042EA 2005 3 23 VNAA0503005 120050306A2751N6172952 DETECTION SYS CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS FAILED A VNAAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 GL05216PS2515 7882 DURING CLIMB (SDF TO LGA) THE FLAPS DEGRADED STATUS MESSAGE ILLUMINATED. THE CREW OF FLIGHT 2588 DIVERTED TO DAY, MADE AN UNEVENTFUL LANDING. AFTER TROUBLESHOOTING THE FLAP SYSTEM PER CRJ 200 FIM 27-50-00, PSA MAINTENANCE REMOVED AND REPLACED THE SKEW DETECTION UNIT IAW CRJ 200 AMM 27-51-15-000-801 AND 27-51-15-400-801. THE FLAP SYSTEM OPERATIONALLY CHECKED GOOD IAW CRJ200 AMM 27-51-15-710-802. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050323000432005032300043EA 2005 3 23 VNAA0503006 120050307A3600GG670800025 SHUTOFF VALVE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE LT ENGINE FAILED A VNAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL05703PS2111 10137 DURING CLIMB (CLT TO PWM) UPON SELECTION OF COWL ANTI ICE, THE L COWL A/I & L ENG BLEED CAUTION MESSAGES ILLUMINATED. THE SYNOPTIC PAGE SHOWED VALUES IN WHITE NOT IN AMBER. THE CREW OF FLIGHT 2234 RETURNED TO CLT AND MADE AN UNEVENTFUL LANDING. AFTER TROUBLESHOOTING PSA MAINTENANCE REMOVED & REPLACED THE LT PRESSURE REGULATING SHUTOFF VALVE IAW CRJ 700 AMM 36-12-01-400-801-A01. THE SYSTEM OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050323000442005032300044EA 2005 3 23 VNAA0503007 120050310A3250 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE NLG STEERING ILLUMINATED A VNAAO OTHER J WARNING INDICATION LDLANDING 1 GL05723PS 10181 UPON LANDING AT MKE, AFTER THE NOSE WHEEL CONTACTED THE RUNWAY, THE STEERING INOP CAUTION MESSAGE ILLUMINATED. NOSE WHEEL STEERING WAS INOPERATIVE EVEN AFTER RESETTING MULTIPLE TIMES. THE CREW OF FLIGHT 2207 CLEARED THE RUNWAY USING BRAKES AND DIFFERENTIAL POWER. THE AIRCRAFT WAS THEN TOWED TO THE GATE. CONTRACT MAINTENANCE COMPLIED WITH NWS SYSTEM RESET PROCEDURES IAW BOMBARDIER CRJ 200 SERVICE LETTER 32-019 REV B. THE NWS SYSTEM OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050323000482005032300048NM 2005 3 23 AWXA200500345 120050121A53302024T3050 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28307AW 24634 PHX - MAJOR REPAIR - DURING 4-DAY CHECK A 2.5 INCH CRACK WAS FOUND IN LT SIDE OF FUSELAGE SKIN ON LOWER AFT SIDE OF EXTERNAL EMERGENCY EXIT LIGHT BS 727E, STR 24 LT. MAINTENANCE CUT OUT DAMAGE IN FUSELAGE SKIN AT BS 727E, STR 24 LT AND PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-01, FIG 229. REPAIR PLACED ON MONITOR, RE-INSPECT AT 60,000 FLT CYCLES. 2L72 4F RTA16WE 20050323000502005032300050NM 2005 3 23 AWXA200500347 120050318A3397BMS13311122 WIRE BOEING737 7373G7 1384595NM SEAT ROW 23 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 PHX - EEL - DURING THRU FLIGHT INSPECTION FOUND EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 23 LT DID NOT ILLUMINATE, WIRING PULLED OUT FROM CONNECTOR. MAINTENANCE RE-TERMINATED BROKEN WIRE AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 23 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050323000512005032300051EU 2005 3 23 AWXA200500348 120050319A3397D9299200900200 WIRE HARNESS AIRBUS320 A320232 3930326EU SEAT ROW 5 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28649AW 803 PHX - EEL - DURING E-07 CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 5 LT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE ON EMERGENCY ESCAPE PATH LIGHT HARNESS SEAT ROW 5 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050323000522005032300052NM 2005 3 23 AWXA200500349 120050320A3350GMW15 FUSE BOEING737 7373G7 1384595NM POWER SUPPLY BLOWN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 SEA - EEL - DURING 4-DAY CHECK THE EMERGENCY EXIT LIGHT ABOVE SEAT ROW 17 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED FUSE IN EMERGENCY LIGHT POWER SUPPLY M1136, BS 747; OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050323000542005032300054 2005 3 23 237TR0009 420050308A22102591092904 INDICATOR BOEING737 737228 13844AGNM FLT DIRECTOR INOPERATIVE A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05237TR 23007 NR 1 FLIGHT DIRECTOR INOP. PLACED ON MEL 34-12. 03/14/2005: REPLACED NR 1 ADI AND OPS CHECKED PER MM 22-11-01. 2L72 4F RTA16WE 20050323000572005032300057NM 2005 3 23 SWAA050834 120050317A561058935578 WINDOW BOEING737 7373H4 1384600NM COCKPIT ARCED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29656SW 28401 DURING SCHEDULED RON CHECK, FOUND R2 COCKPIT WINDOW ARCING. REMOVED AND REPLACED WINDOW PER MM. 2L72 4F RTA16WE 20050323000582005032300058NM 2005 3 23 SWAA050835 120050317A5313BAC1498 STRINGER BOEING737 7373Q8 1384670NM AFT CARGO BAY CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND CORROSION ON STRINGER BETWEEN BS 1006 TO BS 1014, STR 26R. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2L72 4F RTA16WE 20050323000592005032300059NM 2005 3 23 SWAA050836 120050317A532269353656 SHEAR TIE BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND CORROSION ON SHEAR TIE AT BS 360, BETWEEN STR 27L & STR 28L. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050323000602005032300060NM 2005 3 23 SWAA050837 120050317A3350PH22300L LIGHT BOEING737 7373Q8 1384670NM FWD CABIN WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND FWD CABIN EEPLS STRIPS WORN. REMOVED AND REPLACED EEPLS STRIPS PER MM. 2L72 4F RTA16WE 20050323000612005032300061NM 2005 3 23 SWAA050838 120050317A53306545767 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 396, STR 24L. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050323000622005032300062NM 2005 3 23 SWAA050839 120050317A5313BAC1498 STRINGER BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED C4 CHECK, FOUND CRACKED STRINGER AT BS 443, STR 25L. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20050323000632005032300063NM 2005 3 23 BB05017 120050320A335020131A BATTERY BOEING767 7672B7 1385107NM AFT LEFT CABIN DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19656US 26847 FOUND AFT LEFT FLOOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. 2L72 4F RTA1NM 20050323000662005032300066WP 2005 3 23 UPS05844131 120050315A5755 SKIN DOUG DC8 DC873F 302199FWP RT SPOILER DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE:N/A RIGHT I/B SPOILER PANEL HAS DELAM ON O/B SIDE BOTTOM. REMOVED RIGHT I/B SPOILER IAW 27-61-01-2 TO STEP 10 PARAGRAPH NR 3. INSPECTED A/C STRUCTURE NO DEFECTS NOTED. OK TO INSTALL. INSTALLED RIGHT I/B SPOILER PANEL PER 27-61-01-2 TO STEP B6 PG 31. COMPLETED INSTALL 27-22-22-4. 2L74 4F RT4A25 20050323000672005032300067NE 2005 3 23 C1HA200593002 220050316A7200JT8D17 ENGINE BOEING727 727212 138407GNM PWA JT8 JT8D17 52049NE NR 1 OVERTEMP A C1HAEJA ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING EMJVIBRATION/BUFFET OVER TEMP WARNING INDICATION TOTAKEOFF 1 GL15293AS52232 21348 ON TAKEOFF AFTER V1 THE NUMBER 1 ENGINE HAD SEVERE FLUCTUATIONS IN ALL INSTRUMENTS WITH VIBRATIONS ON NUMBER ONE SIDE. HEARD THREE LOUD POPS NR 1 EGT WENT TO 700 DEGREES C, THREE DIFFERENT TIMES IN RAPID SUCCESSION. DUMPED FUEL RETURNED FOR LANDING. FOLLOWED COM PROCEDURES 2.72.15 AND 2.28.4. 2L73 4F4 F A3WE E2EA 20050323000682005032300068NM 2005 3 23 SWAA050844 120050318A323369448105 ACTUATOR BOEING737 7373Q8 1384670NM RT MLG FAULTY A SWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW29687SW 23388 RIGHT MLG DID INDICATE FULLY RETRACTED AFTER TAKEOFF. RECYCLED GEAR DOWN & UP, THEN INDICATED OK. REMOVED AND REPLACED RT MLG UPLOCK ACTUATOR & TRANSFER CYLINDER PER MM. 2L72 4F RTA16WE 20050323000712005032300071NM 2005 3 23 SWAA050847 120050318A52406545871 DOOR FRAME BOEING737 7375H4 138449DNM R1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29503SW 24180 DURING SCHEDULED C2 CHECK, FOUND R1 DOOR FRAME CRACKED AT AFT LOWER STOP FITTING. REMOVED AND REPLACED DOOR PER MM. 2L72 4F RTA16WE 20050323000722005032300072NM 2005 3 23 SWAA050848 120050319A256010C801 LATCH BOEING737 7373H4 1384600NM ESCAPE ROPE BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29331SW 23695 CAPTAIN'S EMERGENCY ESCAPE ROPE COMPARTMENT LATCH BROKEN. REMOVED AND REPLACED LATCH ASSY PER MM. 2L72 4F RTA16WE 20050323000742005032300074NM 2005 3 23 SWAA050850 120050320A2420106122411 GCU BOEING737 7373A4 1384585NM NR 2 FAULTY A SWAAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 SW29674AA 23252 AIR TURNBACK - DECLARED EMERGENCY. OBSERVED SMOKE FROM BEHIND F/O'S SEAT. NR 2 GCU FAILED. REMOVED AND REPLACED NR 2 GCU PER MM. 2L72 4F RTA16WE 20050323000752005032300075NM 2005 3 23 SWAA050851 120050320A53306545776 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29515SW 25154 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 25R. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050323000762005032300076 2005 3 23 SWAA050852 420050320A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29627SW 27935 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20050323000782005032300078 2005 3 23 SWAA050841 420050317A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29730SW 27862 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050323000792005032300079NM 2005 3 23 SWAA050853 120050318A2560P2070001 FLASHLIGHT BOEING737 7373H4 1384600NM FWD CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 DURING SCHEDULED A1 CHECK, FOUND FWD RT EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT ASSY PER MM. 2L72 4F RTA16WE 20050323000802005032300080SO 2005 3 23 C2XA05BT015 120050317A3350110049 CHARGER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT FAULTY A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713553 145585 DURING RON MAINTENANCE FOUND EMERGENCY LIGHTS OUT AFT OF EMERGENCY EXIT ROW OF SEATS. MAINTENANCE REMOVED AND REPLACED NR 4 BATTERY CHARGER ASSEMBLY IAW EMB145 AMM 33-50-04. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050323000812005032300081SO 2005 3 23 C2XA05CL017 120050316A30403801D2 HEATER EMB 135 EMB135ER 3260203SO WINDSHIELD BURNED A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW27165013226 145145 CLE - FLIGHT 2226 THE CREW REPORTED A HOT BURNING SMELL IN THE CABIN AND COCKPIT. MAINTENANCE REPLACED THE NR 1 WINDSHIELD HEAT CONTROL BOX AND OPERATIONAL CHECKS GOOD. 2L72 4F RTT00011AT 20050323000842005032300084NM 2005 3 23 QXEA200500393 120050131A5730 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 600 ERODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - RIGHTHAND WING TIP LEADING EDGE HAS EROSION DAMAGE TO COMPOSITE STRUCTURE. REPAIRED IAW DHC-8 Q400 SUB TASK 51-80-00-340-802, 51-25-26-370-801, 51-25-31-370-801 AND RD 8/4-57-415, PAGE 4. 2H72 4T RTA13NM 20050323000862005032300086NM 2005 3 23 QXEA200500414 120050207A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 200 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - RIGHTHAND FUSELAGE EXTERNAL SKIN AT STATIONS X298 TO 294 BETWEEN STRINGER 14-20 HAS FIVE DENTS. REPAIRED IAW RD 8/4-53-1154, ISSUE 1 AND HORIZON AIR EA 6-53-517. 2H72 4T RTA13NM 20050323000872005032300087NM 2005 3 23 QXEA200500390 120050124A5230 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - FUSELAGE EXTERNAL SKIN BELOW AFT CARGO DOOR STATION X722 TO 789, STRINGER 24 TO 31 HAS SEVERAL AREAS OF DAMAGE. REPAIRED IAW DHC-84 400 SRM 51-26-10-410-001. 2H72 4T RTA13NM 20050323000882005032300088NM 2005 3 23 QXEA200500396 120050202A5730 SHROUD BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - LEFTHAND OUTBOARD FLAP HAS A CHAFING MARK SEVERAL FEET LONG FROM CONTACT WITH THE UPPER WING SHROUD. REPAIRED IAW RD 8/4-57-423 AND HORIZON AIR EA 6-57-296. 2H72 4T RTA13NM 20050323000892005032300089NM 2005 3 23 QXEA200500413 120050207A5730 ACCESS PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 600 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - RIGHTHAND WING, RIGHTHAND FUEL PANEL 622CT, BOTTOM SURFACE OF PANEL, PITTING AND FRETTING CORROSION AROUND PANEL ATTACH HOLES. REPAIRED IAW RD -8/4-57-438, ISSUE 1 Q400 SRM 51-21-00-350-001 AND HORIZON AIR EA 6-57-312. 2H72 4T RTA13NM 20050323000902005032300090NM 2005 3 23 QXEA200500405 120050124A5230 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - FUSELAGE EXTERNAL SKIN AFT CARGO DOOR HAS A GOUGE IN SKIN AT STATION X138 BETWEEN STRINGER 31 AND 31. REPAIRED IAW Q400 SRM 53-10-31-300-001. 2H72 4T RTA13NM 20050323000912005032300091NM 2005 3 23 C1HA200593001 120050311A3297 WIRE BOEING727 727212 138407GNM MLG INDICATOR SHORTED A C1HAJA DUMP FUEL UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL15293AS 21348 AFTER T/O RED NOSE GEAR LIGHT ILLUMINATED FOLLOWED BY NOSE GEAR LIGHT (GREEN). RAN COM 2.32,23 SUCCESSFULLY BOTH LIGHTS REMAINED ILLUMINATED ENTIRE FLT. ALSO RAN 2.28.4 (FUEL DUMPING PROCEDURE) FOUND WIRE W1386-023-20 SHORTED TO CONDUIT IN NOSE WHEEL WELL AT END OF CONDUIT. REMOVED AND REPLACED SAME, AS WELL FOUND PLUG D5194 TO HAVE PIN 6 BENT OVER AND IN CONTACT WITH PIN 18. REMOVED AND RE-TERMINATED PIN 6 PER BSWPM , RESECURED ALL WIRE RUNS, OPERATED NOSE GEAR 10 TIMES, ALL INDICATIONS NORMAL. 2L73 4F A3WE 20050323000932005032300093NM 2005 3 23 SWAA050855 120050320A335090083 BATTERY PACK BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29650SW 27720 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY EMERGENCY BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050323000972005032300097NM 2005 3 23 SWAA050859 120050318A53146545866 KEELBEAM BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND CORROSION ON KEEL BEAM AT BS 727, LT OUTBOARD CHORD STRAP. REPAIRED KEEL BEAM PER SRM. 2L72 4F RTA16WE 20050323001002005032300100NM 2005 3 23 SWAA050862 120050319A3350101073 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29608SW 27928 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EMERGENCY EXTERIOR LIGHT LENS LOOSE. RE-INSTALLED LENS PER MM. 2L72 4F RTA16WE 20050323001022005032300102 2005 3 23 SWAA050864 420050320A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29743SW 29279 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. RE-INSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20050323001042005032300104EU 2005 3 23 MALA050277 120050316A2450 RELAY BAC 146 AVRO146RJ85A1500097EU FUEL PUMP MALFUNCTIONED A MALAO OTHER J WARNING INDICATION CRCRUISE 1 GL15509XJ E2321 NR 3 RT INNER FUEL PUMP LOW PRESS ILLUMINATED. REMOVED AND REPLACED C/B B11 P/N S2653-005. REMOVED AND REPLACED RELAY 3QG4, PERFORMED VOLT CHECKS ON BUSS TIE CONTACTS. CHECKS GOOD. RAN AC AT DIFFERENT POWER SETTINGS. NO FAULTS. 2H74 4F RTA49EU 20050323001052005032300105EU 2005 3 23 MALA050283 120050318A3200 LANDING GEAR BAC 146 AVRO146RJ85A1500097EU LT MAINS FAILED A MALAO OTHER A FLAME/FIRE LDLANDING 1 GL15516XJ E2334 GROUND CREW REPORTED FLAMES AROUND LT MAIN. O/B LT MAIN BRAKE TEMP 550 C, PRIOR TO STOPPING, ANTI SKID LIGHT ON. POST FLT, FOUND LT O/B TIRE FLAT, LT O/B MLG TIRE WHEEL ASSY BEARING FAILED/SEIZED, LT AXLE SUSTAINED GALLING/GOUGING ON INNER BEARING BRACE OUT OF LIMITS. LT O/B BRAKE FAN MOTOR ASSY & HARNESS DAMAGED/OVERHEAT. LT O/B ANTI SKID TRANSDUCER & HARNESS DAMAGED/OVERHEAT, LT MLG AXLE P/N 201298302, LT O/B MLG TIRE/WHEEL ASSY P/N AHA1489. REMOVED & REPLACED LT O/B BRAKE ASSY, P/N AHA2332-2, LT I/B MLG TIRE/WHEEL ASSY P/N AHA1489, LT O/B BRAKE FAN MOTOR ASSY, BRAKE TRANSDUCER, LT O/B MLG SPACER/SLEEVE, LT O/B BRAKE FAN & ANTI SKID HARNESSES. OPS/FUNC CHECKS LT BRAKE SYS & ANTI SKID SYS, CHECKS GOOD. 2H74 4F RTA49EU 20050323001062005032300106EU 2005 3 23 MALA050284 120050319A2910HTE95313 ISOLATION VALVE BAC 146 AVRO146RJ85A1500097EU HYD SYSTEM MALFUNCTIONED A MALAO OTHER M OVER TEMP CRCRUISE 1 GL15508XJ E2318 YELLOW HYD TEMP CAME ON IN FLT ENGINE 2 VALVE (NIPS) LIGHT STAYED ON WITH VALVE SHUT. HYD PRESS ON YELLOW STAYED AT 3100 PSI WITH VALVE SWITCH IN OFF POSITION. REMOVED AND REPLACED YELLOW HYD ISO VALVE P/N ON & OFF HTE9531-3, S/N ON FRTR023AX. 2H74 4F RTA49EU 20050323001082005032300108EU 2005 3 23 MALA050275 120050218A5320 FLOOR SUPPORT SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15424XJ 340B424 DURING 4Y/2Y CHECK IN BNA FOUND FWD CABIN FLOOR SUPPORT ANGLE AT FS 294 LBL 18 IS CORRODED. REMOVED ANGLE, FAB'D NEW ANGLE AS PER SAMPLE USING BONDING AND JOGGLING PROCEDURES IAW SRM 51-20-20 AND 51-20-30. ALODINE, PRIMED AND PAINTED IAW SRM 51-20-42 AND 51-20-43. INSTALLED SUPPORT ANGLE REF SRM 51-40-21. 2L72 4T RTA52EU 20050323001092005032300109EU 2005 3 23 MALA050276 120050218A5320 FLOOR SUPPORT SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15424XJ 340B424 DURING 4Y/2Y CHECK IN BNA FOUND FWD CABIN FLOOR SUPPORT ANGLE AT FS 294 BL 0 IS CORRODED. REMOVED ANGLE, FAB'D NEW ANGLE AS PER SAMPLE USING BONDING AND JOGGLING PROCEDURES IAW SRM 51-20-20 AND 51-20-30. ALODINE, PRIMED AND PAINTED IAW SRM 51-20-42 AND 51-20-43. INSTALLED SUPPORT ANGLE REF SRM 51-40-21. 2L72 4T RTA52EU 20050323001152005032300115WP 2005 3 23 DHL2005805500 120050220A5531 FRAME DOUG DC8 DC873F 302199FWP VERTICAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 VERTICAL STABILIZER LT L/E INTERNAL FORMER CRACKED 1.000, ZFS 264.750. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP DRILL ON CRACK END AND FABRICATED ANGLE DOUBLERS (2EA) (AL 7075-T6 0.032) IAW SRM 55-2-0 PG 7-8 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED ANGLE DOUBLERS WITH NEW FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. TORQUED IAW SRM 51-3-1 PG 2A. 2L74 4F RT4A25 20050323001182005032300118NM 2005 3 23 QXEA200500411 120050131A5730 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - LEFTHAND WING, LEFTHAND FUEL PANEL 523AT, PANEL REBATE WS 157.825 TO WS 190.00, FRETTING CORROSION ON TOP OF REBATE AROUND PANEL ANCHOR NUT ATTACH HOLES. REPAIRED IAW Q00 SRM 57-10-30-320-002, 51-21-10-380-001, 51-25-40-370-001, RD 8/4-57-424, ISSUE 1 AND HORIZON AIR EA 6-57-298. 2H72 4T RTA13NM 20050323001192005032300119NM 2005 3 23 QXEA200500412 120050203A5730 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - LEFTHAND WING, LEFTHAND FUEL TANK PANEL 522CT, PANEL REBATE WS 117.50 TO WS 157.825, FRETTING CORROSION ON TOP SURFACE OF REBATE AROUND PANEL ANCHOR NUT ATTACH HOLES. REPAIRED IAW Q400 SRM 57-10-30-320-002, RD 8/4-57-429, ISSUE 1 AND HORIZON AIR EA 6-57-308. 2H72 4T RTA13NM 20050323001202005032300120NM 2005 3 23 QXEA200500402 120050126A5420 ANCHOR FITTING BOMBDRDHC8 DHC8401 1390041NM ZONE 400 BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - RIGHTHAND NACELLE PANEL 424AR ATTACHMENT AREA HAS A BROKEN ANCHOR NUT AND THREE ANCHOR NUTS WITH BROKEN SCREWS STUCK INSIDE. REPAIRED IAW Q400 SRM 51-42-05-330-001, PARAGRAPH E. 2H72 4T RTA13NM 20050323001222005032300122NM 2005 3 23 QXEA200500404 120050124A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM FUSELAGE GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - FUSELAGE EXTERNAL SKIN BELOW CARGO DOOR HAS A GOUGE IN SKIN. REPAIRED IAW Q400 SRM 53-40-31-350-801 AND 53-10-31-350-801. 2H72 4T RTA13NM 20050323001232005032300123NM 2005 3 23 QXEA200500406 120050131A5730 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 600 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - RIGHT WING RIGHT FUEL TANK PANEL 622BT, PANEL REBATE WS 79.700 TO WS 117.500 FRETTING CORROSION ON TOP SURFACE OF REBATE AROUND PANEL. REPAIRED IAW Q400 SRM 57-10-30-320-002, 51-21-10-380-001 AND 51-25-40-370-001. 2H72 4T RTA13NM 20050323001242005032300124NM 2005 3 23 HNAA0500022 120050316A291082970009131 LINE DHAV DHC8 DHC8102 2809003NM HYD SYSTEM LEAKING A HNAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA07326EN2463624636 234 IN FLIGHT NR 2 HYDRAULIC SYSTEM WENT TO 1 QT AND NR 2 ISO VALVE CAUTION LIGHT ILLUMINATED. NO OTHER CAUTION LIGHTS AND QUANTITY REMAINED ABOVE 1QT. FLIGHT DIVERTED TO MDT WHERE IT WAS FOUND HYDRAULIC FLUID WAS LEAKING FROM BEHIND THE NR 2 NACELLE GRAVEL GUARD. LINES WERE CAPPED OFF AND AIRCRAFT WAS FERRIED TO SBY. INSTALLED HYDRAULIC LINE IN NR 2 NACELLE FOR GEAR DOOR DOWN PRESSURE AND REPLACED HYDRAULIC LINE IN NR 1 NACELLE FOR STAY STRUT ACTUATOR. 2H72 4T RTA13NM 20050323001252005032300125SO 2005 3 23 RAIA00503009 120050312A3010 WARNING LIGHT EMB 145 EMB145 3260210SO ANTI ICE SYSTEM ILLUMINATED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03804HK 145082 BDL - AIRFRAME ANTI-ICE INOP WARNING INDICATION. MAINTENANCE INSPECTED ANTI-ICE DETECTION SYSTEM AND PERFORMED OPS CHECK. FOUND SYSTEM OPS NORMAL. 2L72 4F RTT00011AT 20050323001272005032300127 2005 3 23 RAIA00503005 420050314A34207003110912 HSI JETAIRJETSTMJETSTM4101 1500501EU COCKPIT INOPERATIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03568HK2459122 41086 GSO - F/O'S EHSI FAILED. MAINTENANCE REMOVED AND REPLACED EHSI. 2L72 4T RTA41NM 20050323001282005032300128 2005 3 23 RAIA00503006 420050316A34207011672112 SYMBOL GENERATOR JETAIRJETSTMJETSTM4101 1500501EU NR 1 INOPERATIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03565HK171631396 41082 STL - LEFT SYMBOL GENERATOR FAILED. MAINTENANCE REMOVED AND REPLACED NR 1 SYMBOL GENERATOR. 2L72 4T RTA41NM 20050323001292005032300129EU 2005 3 23 RAIA00503008 120050317A612031056294 BETA SWITCH JETAIRJETSTMJETSTM4101 1500501EU NR 2 ENGINE INOPERATIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03558HK 41071 RIC - RIGHT BETA LIGHT DOES NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE BETA SWITCH. 2L72 4T RTA41NM 20050323001322005032300132NM 2005 3 23 QXEA200500392 120050131A5730 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 500 ERODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - LEFTHAND WING TIP LEADING EDGE HAS EROSION DAMAGE TO COMPOSITE STRUCTURE. REPAIRED IAW Q400 SUB TASK 51-80-00-340-802, 51-25-26-370-801 AND RD 8/4-57-415, PAGE 4. 2H72 4T RTA13NM 20050323001352005032300135NM 2005 3 23 QXEA200500408 120050131A5730 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 600 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - RIGHTHAND WING, RIGHTHAND FUEL PANEL 623AT, PANEL REBATE WS 157.825 TO WS 190.0, FRETTING CORROSION ON TOP SURFACE OF REBATE AROUND PANEL ANCHOR NUT ATTACH HOLES. REPAIRED IAW Q400 SRM 57-10-30-320-002, RD 8/4-57-418, ISSUE 1 AND HORIZON AIR EA 6-57-297. 2H72 4T RTA13NM 20050323001362005032300136NM 2005 3 23 QXEA200500395 120050122A5315 FLOORBEAM BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - CENTER FLOORBEAM AT STATION X32.000 DOUBLER JOINT AND RIVETS CORRODED. REPAIRED IAW Q400 SRM TASK 51-21-00-350-001, 51-21-10-380-001 AND 51-25-10-370-001. 2H72 4T RTA13NM 20050323001392005032300139NM 2005 3 23 HNAA050023 120050317A2120 SMOKE DHAV DHC8 DHC8201 2809001NM CABIN DETECTED A HNAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA07966HA 452 FLIGHT ATTENDANT REPORTS SMOKE IN CABIN. SUSPECT COMING FROM ROWS 3 OR 4 RIGHT SIDE. CONTRACT MAINTENANCE INSPECTED OVERHEAD, SIDEWALL, EMERGENCY LIGHTS AND PSU'S. NO DEFECTS NOTED. 2H72 4T RTA13NM 20050323001402005032300140NM 2005 3 23 UPS05644141 120050319A2560MXP21000 SMOKE GOGGLES BOEING767 76734AF 1385212NM COCKPIT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01328UP 27754 INSPECTION TYPE:N/A F/O'S SMOKE GOGGLES HAS A CRACK IN LENS AT NOSE PIECE .375 INCH LONG. REPLACED BROKEN GOGGLES WITH SERVICEABLE GOGGLES. 2L72 4F RTA1NM 20050323001412005032300141NM 2005 3 23 HNAA0500024 120050317A242051539008 GCU DHAV DHC8 DHC8102 2809003NM NR 2 A/C GEN FAILED A HNAAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CLCLIMB 1 EA07907HA5111451114 011 RIGHT A/C BUSS FAILED ON CLIMBOUT, RETURNED TO FIELD. REMOVED NR 2 A/C GENERATOR CONTROL UNIT. 2H72 4T RTA13NM 20050323001442005032300144NM 2005 3 23 CALA0500077 120050318A5347BAC1520792 SEAT TRACK BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714609 27322 INSPECTION FOUND SEAT TRACK CORRODED AT STA 360-375, RBL 24. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52. 2L72 4F RTA16WE 20050323001532005032300153EU 2005 3 23 MALA050280 120050316A5310 STRUCTURE SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15427XJ 340B427 DURING 4Y/2Y CHECK IN BNA FOUND CORROSION ON UPPER AND LOWER SURFACES AND BETWEEN SPLICES AT STA 258. REMOVED CORROSION, OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR ANGLES REF SAAB SRM 53-10-30; 51-20-42; 51-40-21. 2L72 4T RTA52EU 20050323001542005032300154EU 2005 3 23 MALA050281 120050316A5320 HAND RAIL SAAB SF340 340B 7860101EU AIRSTAIR CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15427XJ 340B427 DURING 4Y/2Y CHECK IN BNA FOUND CRI - REPAIR UPPER FWD HANDRAIL AT PAX DOOR STEP ASSY. FABRICATED NEW RAIL, REMOVED DAMAGED RAIL AND INSTALLED REPLACEMENT RAIL REF MESABA EO S52024. 2L72 4T RTA52EU 20050323001552005032300155EU 2005 3 23 MALA050282 120050317A5340 NUT PLATE SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15427XJ 340B427 DURING 4Y/2Y CHECK IN BNA FOUND CRI - FRS CORRODED AT NUT PLATES BETWEEN STA 686.300 TO STA 749. REMOVED CORROSION, OUT OF LIMITS. FABRICATED AND INSTALLED 5 ANGLES REF MESABA EO S53294. 2L72 4T RTA52EU 20050323001562005032300156CE 2005 3 23 DXTA200500636 120050319A5230840504 PRESSURE SWITCH CESSNA750 750 2076810CE CARGO DOOR OUT OF ADJUST E DXTABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL07901QS 7500102 AT FL 410 BAGGAGE DOOR SEAL CAS ACCOMPLISHED CHECKLIST AT FL 390 AMBER CABIN ALTITUDE FOLLOWED SHORTLY BY RED CABIN ALTITUDE LIGHT ILLUMINATED. PERFORMED EMERGENCY DESCENT THEN ACCOMPLISHED CHCEKLIST. INSPECTED BAGGAGE DOOR, DOOR SEAL. DOOR LATCHING MEHCANISM AND BAGGAGE DOOR BLEED AIR LINES. FOUND BAGGAGE DOOR SEAL VALVE & SWITCH OUT OF ADJUSTMENT. ADJUSTED BAGGAGE DOOR SEAL VALVE & SWITCH IAW CESSNA 750 M/M CHAPTER 52-31-01. C/W BAGGAGE DOOR SEAL FUNCTIONAL TEST IAW CESSNA 750 M/M CHAPTER 52-30-08, OPERATIONAL CHECK SATISFACTORY. 2L72 4J RTT00007WI 20050323001572005032300157CE 2005 3 23 DXTA200500637 120050319A324042929 ANTI-SKID SYS CESSNA500 560CESSNA 2076750CE MLG DEFECTIVE E DXTAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 GL07320QS8414 5600321 WHEN GEAR WAS SELECTED DOWN THE POWER BRAKE LOW PRESS AND ANTI SKID INOP LIGHT CAME ON AND REMAINED ON. DURING BRAKE OPERATION PEDALS WERE SOFT BUT BRAKING WAS AVAILABLE BY PUMPING THE BRAKES. - REMOVED DEFECTIVE ANTI SKID CONTROL UNIT- REPLACED WITH "SERVICABLE UNIT. ALSO FOUND CONNECTOR TO GEAR HANDLE "P-160" TO BE LOOSE IN THE TROUBLESHOOTING PROCESS. RESECURED CONNECTOR. PERFORMED SYSTEM OPRATIONAL TEST PER 32-30-01 WITH NO FAULTS 2L72 4F RTA22CE 20050323001612005032300161NM 2005 3 23 HNAA0500026 120050318A3230574205A SELECTOR VALVE DHAV DHC8 DHC8102 2809003NM MLG MALFUNCTIONED A HNAAO OTHER J WARNING INDICATION DEDESCENT 1 EA07982HA 380 GEAR WOULD NOT EXTEND ON 2ND ATTEMPT. FOLLOWED EMERGENCY CHECK LIST. PERFORMED ALT EXTENSION, GEAR DOWN AND LOCKED. INSPECTED PSEU FOR FAULT CODES NONE FOUND CYCLED GEAR 10 TIMES WITH NO DEFECT NOTED. REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE AS REQUIRED, CYCLED GEAR 5 TIMES, OPS CHECK & LEAK CHECK GOOD. 2H72 4T RTA13NM 20050323001712005032300171SO 2005 3 23 MASA200500207 120050312A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07835MJ 145353 ASH 2647 CLT. CREW REPORTED THE CEILING EMERGENCY EXIT SIGN FRONT HALF LIGHTS WERE INOP. MAINTENANCE REPLACED THE LAMPS AND IT OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050323001732005032300173EA 2005 3 23 MASA200500224 120050315A3350 POWER SUPPLY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07650ML 7137 ASH 2698 - IN PHL HAD 1ST 4 FLOOR EMERGENCY LIGHT INOP. MAINTENANCE REPLACED POWER SUPPY FOR LIGHTING STRIPS. 2L72 4F RTA21EA 20050323001762005032300176NM 2005 3 23 UPS05244134 120050311A7830 BRACKET BOEING727 72722C 138400FNM NR 1 ENGINE T/R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 INSPECTION TYPE:C ENGINE NR 1 THRUST REVERSER O/B FAIRING MID AND AFT SUPPORT BRACKET ARE CRACKED. BRACKETS REPLACED IAW MM 78-30-01. 2L73 4F A3WE 20050323001772005032300177NM 2005 3 23 UPS05244135 120050308A5230 FRAME BOEING727 72722C 138400FNM AFT CARGO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 INSPECTION TYPE:C AFT CARGO DOOR, CRACKED IN 1ST FRAME FROM TOP IN O/B RADIUS BENEATH FWD HINGE. REPAIR CARRIED OUT IAW MM 52-31-01 & SRM 51-10-01, 51-40-3, 51-10-02 & 51-30-02. REF NRC 768566 FOR INSTALLATION OF AFT CARGO DOOR. 2L73 4F A3WE 20050323001782005032300178NM 2005 3 23 UPS05644139 120050319A3350 LAMP BOEING767 76734AF 1385212NM EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01312UP 27763 MAIN ENTRY EMERGENCY LIGHT INOPERATIVE. REPLAMPED EMERGENCY LIGHT. 2L72 4F RTA1NM 20050323001792005032300179NM 2005 3 23 UPS05644140 120050319A2560 SMOKE GOGGLES BOEING767 76734AF 1385212NM CABIN CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01314UP 27742 LEFT SUPERNUMERARY SMOKE GOGGLES CRACKED. REMOVED AND REPLACED SMOKE GOGGLES. 2L72 4F RTA1NM 20050321001852005032100185 2005 3 21 SWAA050761 420050312A2565D31354 SLIDE BOEING737 7375H4 138449DNM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29505SW 24182 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. RE-INSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20050321001922005032100192EU 2005 3 21 AALA20050200 120050315A3397 CONNECTOR AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHT LOOSE A AALAK NONE O OTHER ININSP/MAINT 1 SW2190070 513 JFK - EMERGENCY LIGHT AT NR 1 RIGHT DOOR ABOVE HANDSET INOPERATIVE. RESECURED CONNECTOR FOR BATTERY PACK AT NUMBER ONE RIGHT DOOR EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20050321001942005032100194SO 2005 3 21 SWIA200514673 120050302A2750 ROD END EMB 120 EMB120ER 3260203SO TE FLAPS OUT OF ADJUST A SWIAO OTHER F FLT CONT AFFECTED DEDESCENT 1 NM07268UE 120207 FLAP DISAGREEMENT OCCURRED WHEN SELECTING FLAPS FROM 25 DEGREES TO 45 DEGREES. LUBED LEFT AND RIGHT OUTBOARD FLAP ROLLERS, CLEANED FLAP TRACKS, ADJUSTED LEFT FLAP ACTUATOR ROD END IN IAW MM 27-50-04, OPERATIONAL CHECK GOOD IAW MM 27-50-00. 2L72 4T RTA31SO 20050321002122005032100212EU 2005 3 21 ASOA05031 120050115A3350E01173110 SWITCH AEROSPATR72 ATR72 EU PWA PW120 PW127 NE CABIN MALFUNCTIONED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27642AS 395 DURING A GROUND INSPECTION, THE EMERGENCY EXIT LIGHT ABOVE THE FORWARD CABIN DOOR WAS REPORTED TO REMAIN ON CONTINUOUSLY AND THE EMERGENCY EXIT LIGHT IN THE AFT CABIN INCLUDING THE COCKPIT REMAINED ON UNTIL THE LANDING GEAR WAS UP. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTS TWO MINUTE PUSHBUTTON SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2H72 4T4 TRT E20NE 20050321002292005032100229EA 2005 3 21 ASOA05011 120050104A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27823AS 7196 DURING A C-CHECK, THE CARGO COMPARTMENT FLOORBEAM CAP STRIP AT FS 589 BETWEEN LBL 9 AND LBL 27 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CARGO COMPARTMENT FLOOR BEAM CAP STRIP AT FS 589 BETWEEN LBL 9 AND LBL 27. (K) 2L72 4F4 FRTA21EA E15NE 20050321002642005032100264EA 2005 3 21 ASOA05104 120050206A5260601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27889AS 7538 DURING HANGAR MAINTENANCE IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20050321002792005032100279EU 2005 3 21 ASOA05153 120050224A6120C1466003 SERVO VALVE AEROSPATR72 ATR72212 8680945EU RT PROPELLER FAULTY A ASOAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27532AS 458 FLT 4127 - DURING CLIMB-OUT FROM ATL-PFN, THE CREW RECEIVED AN AC WILD FAULT ON THE RIGHT ENGINE. WHILE PERFORMEING THE CHECK LIST THE CREW NOTICED THE RIGHT ENGINE TORQUE AT 38-40 PERCENT AND THE NP AT 108 PERCENT. THE CREW REDUCED THE RIGHT ENGINE POWER TO FLIGHT IDLE AND THEN ATTEMPTED TO LOWER THE NP BY SETTING THE POWER TO CLIMB WITHOUT SUCCESS WITH THE NP REMAINING AROUND 110 PERCENT. THE CREW THEN SHUT DOWN THE RIGHT ENGINE, DECLARED AN EMERGENCY AND THE AIRCRAFT RETURNED TO ATL, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE PROPELLER SERVO VALVE (PSV). OPS AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20050321002952005032100295EU 2005 3 21 ASOA05134 120050216A33507012210 LIGHT AEROSPATR72 ATR72 EU CABIN INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27630AS 336 FLT 4239 - DURING A GROUND INSPECTION IN ATL, THE FLIGHT ATTENDANT REPORTED THE EMERGENCY EXIT LIGHT OVER THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20050321003012005032100301EA 2005 3 21 ASOA05121 120050210A5320601R3117117 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27828AS 7213 DURING A C-CHECK IN MCN, THE FS 484 CLIPS AT LBL 27 AND RBL 27 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FS 484 CLIPS AT LBL 27 AND RBL 27 IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20050321003022005032100302EA 2005 3 21 ASOA05120 120050210A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27828AS 7213 DURING A C-CHECK IN MCN, THE FS 484 INTERCOSTAL AT LBL 36 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FS 484 INTERCOSTAL AT LBL 36 IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20050321003032005032100303EA 2005 3 21 ASOA05119 120050209A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27828AS 7213 DURING A C-CHECK IN MCN, THE NOSE LANDING GEAR FUSELAGE SKIN RADIUS RHS AT FS 235 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE NOSE LANDING GEAR FUSELAGE SKIN RADIUS RHS AT FS 235 IAW ASA EO 600-53-0122. (M) 2L72 4F RTA21EA 20050322000112005032200011EA 2005 3 22 ASOA05141 120050217A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27848AS 7339 DURING A C-CHECK IN MCN, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL0 IAW ASA EO 600-53-0072A. (M) 2L72 4F RTA21EA 20050322000192005032200019EA 2005 3 22 ASOA05115 120050207A5260601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27836AS 7263 DURING AN A-CHECK IN BTR, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR IAW CRJ200 AMM 52-10-00. (M) 2L72 4F RTA21EA 20050322000212005032200021EA 2005 3 22 ASOA05126 120050208A5320 SILL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27846AS 7328 DURING A C-CHECK IN MCN, THE FLOOR SILL ASSEMBLY AT FS 409 PLUS 128 TO 559 OUTBOARD OF LBL 36 AND RBL 36 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE FLOOR SILL ASSEMBLY AT FS 409 PLUS 128 TO 559 RT AND LT IAW ASA EO 600-53-0228. (M) 2L72 4F RTA21EA 20050322000412005032200041NM 2005 3 22 GAIA05011ST 120050301A5230 RIB BOEING727 727214 138407RNM NR 3 CARGO DOOR CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07750US 21512 DURING C-CHECK, A 1 INCH CRACK WAS FOUND ON THE C3 CARGO DOOR OUTER CHORD BY THE LOWER STOP FITTING. REMOVED AND REPLACED THE CRACKED FORWARD CLOSURE RIB ON THE C-3 CARGO DOOR IAW THE BOEING 727 SRM CH 51-10-1 PAR 6. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20050322000422005032200042NM 2005 3 22 GAIA05013AOP 120050303A2613 WARNING LIGHT BOEING727 727214 138407RNM COCKPIT ILLUMINATED A GAIAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SW07750US 21512 FLT 750 - MIA - DURING CLIMB-OUT, THE LOWER AFT BODY OVERHEAT LIGHT CAME ON. THE AIRCRAFT RETURNED TO MIA AND AN UNEVENTFUL LANDING WAS MADE. (M) 2L73 4F A3WE 20050322000452005032200045WP 2005 3 22 GTIA050014 120050124A5210 ROD DOUG DC9 DC981 3022081WP PAX DOOR OUT OF ADJUST A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 FLL - MAIN CABIN DOOR HARD TO CLOSE AND LOCK, APPEARS NORMAL WHEN CLOSED. ADJUSTED AND SECURED ROD FOR HOLD OPEN HOOK ON L1 DOOR, OPS CHECK IAW 52-11-04. (M) 2L72 4F A6WE 20050322000462005032200046WP 2005 3 22 GTIA050013 120050119A2910 HYDRAULIC LINE DOUG DC9 DC981 3022081WP LT MLG WW LEAKING A GTIAK NONE K FLUID LOSS ININSP/MAINT 1 GL23810NK 48015 FLL - FOUND EVIDENCE OF A HYDRAULIC LEAK IN LEFT MLG WHEEL WELL, AIRCRAFT TAIL SWAP. FOUND LEFT GROUND SPOILER UP PRESSURE LINE LEAKING. INSTALLED FLEX LINE, TRANSFERRED TO CARRYOVER, NO LEAKS NOTED. (M) 2L72 4F A6WE 20050322000492005032200049WP 2005 3 22 2005F00033 120050107A215020495055 ACM DOUG DC9 DC982 3022082WP A/C BAY MALFUNCTIONED A GTIAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL23829NK 49931 FLT 861 - JFK - ON T/O FROM LGA, F/A CALLED COCKPIT AND SAID CABIN FILLED WITH SMOKE FROM MID CABIN TO FRONT, CREW COULD SMELL SMOKE, BELIEVE IT WAS COMING FROM A/C SYS, LEVELED AT 7K FT AND ON 10 MILE FINAL SMOKE DISIPATED, AC TAXIED TO GATE UNDER OWN POWER. CHECKED AND REPLACED LT/RT COALESER BAGS. NO CONTAMINATION, CHKD LT/RT ACM'S FOR PRESENCE OF OIL CONTAMINATION IN DUCTING, NONE FOUND. CHKD AIR SUPPLY DUCT FOR CONTAMINATION, NONE FOUND. CHKD RECIRF FAN, OPS CHECK OK. RAN BOTH ENGS AT IDLE, NO EXT LEAKS NOTED. REMOVED 8TH AND 13TH STAGE END CAPS ON NR 1 AND NR 2 ENGS. NO CONTAMINATION NOTED, ACCOMP HIGH END POWER RUN. NO SMOKE OR ODOR NOTICED. R&R RT ACM AND BOTH COALESCER BAGS. (M) 2L72 4F A6WE 20050322000532005032200053WP 2005 3 22 GTIA050006 120050112A28226550934 PUMP DOUG DC9 DC981 3022081WP CENTER FUEL TANKINOPERATIVE A GTIAO OTHER O OTHER ININSP/MAINT 1 GL23811NK 48017 FLL - AFT CENTER FUEL PUMP INOPERATIVE. REMOVED AND REPLACED CENTER FUEL TANK BOOST PUMP, OPS CHECK NORMAL. (M) 2L72 4F A6WE 20050322000552005032200055SO 2005 3 22 2005F00056 120050301A2133108136251 REGULATOR GULSTMG1159 GIV 3980115SO AFT FUSELAGE FAILED A O2GAA UNSCHED LANDING O OTHER CLCLIMB 1 NE03624BP 1093 AIRCRAFT WAS CRUISING AT 43K, CREW NOTED AN EXTREMELY LOUD AIR NOISE AROUND CABIN DOOR. CREW REQUESTED A LOWER ALTITUDE AND WAS GRANTED TO 35K, THROTTLES WERE RETARDED TOWARD IDLE AND A LOUD POP WAS HEARD AROUND CABIN DOOR SEAL. CABIN PRESSURIZATION COULD NOT BE MAINTAINED. CREW DECLARED AN EMERGENCY. (M) 2L72 4F RTA12EA 20050322000612005032200061SO 2005 3 22 SIMA200506108 120050225A532014521713005 BEAM EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21801AE 145469 ABI - DURING AN IMBV INSPECTION, THE GALLEY AREA CENTER BEAM WAS FOUND TO BE CORRODED. REMOVED THE CORRODED CENTER BEAM. INSTALLED NEW BEAM IAW EMB SRM, SRM 145/1142 REV 28 CHAPTER 51-40-02. (M) 2L72 4F RTT00011AT 20050322000642005032200064SO 2005 3 22 SIMA200506104 120050208A532014572178005 SILL EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21805AE 145489 SAW - FOUND DURING CPCP INSPECTION, FOUND CORROSION ON SERVICE DOOR SILL IN FORWARD CABIN GALLEY. REMOVED AND REPLACED SERVICE DOOR SILL IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050322000682005032200068SO 2005 3 22 SIMA200505603 120050220A532014525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21703MR11871 145173 A PREVIOUS REPAIR OF LEFT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. REMOVED THE EXISTING REPAIR AND CLEANED THE AREA. FABRICATED AN EXTERNAL ANGLE, FILLER, PLATE, AND SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB-145/1142 REV 28 CHAPTERS 53-21-10 FIG 201. (M) 2L72 4F RTT00011AT 20050322000762005032200076NM 2005 3 22 SWAA050716 120050308A53306545780 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29605SW 27956 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA TYPICAL REPAIR. 2L72 4F RTA16WE 20050322000802005032200080NM 2005 3 22 SWAA050744 120050310A53116546550 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29607SW 27927 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050322000832005032200083NM 2005 3 22 SWAA050747 120050310A52406545871 DOOR FRAME BOEING737 7375H4 138449DNM R1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29522SW 26564 DURING SCHEDULED C3 CHECK, FOUND R1 DOOR LOWER FRAME CRACKED AT AFT DOOR STOP FITTING. REMOVED AND REPLACED R1 DOOR PER MM. 2L72 4F RTA16WE 20050322000882005032200088NM 2005 3 22 SWAA050738 120050310A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED C3 CHECK, FOUND 3 EA FUSELAGE SKIN CRACKS BETWEEN BS 931 TO BS 934, BETWEEN STR 23L TO STR 24L. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050322000902005032200090NM 2005 3 22 SB05034 120050302A335015AT17 SWITCH BOEING737 737301 1384611NM COCKPIT FAULTY A USAAK NONE O OTHER ININSP/MAINT 1 EA19586US 23931 SYR - MAINTENANCE REPORTED THAT WHEN THE BATTERY IS SELECTED OFF, THE EMERGENCY EXIT LIGHTS ILLUMINATE AND WILL NOT TURN OFF. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT SWITCH. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050323000072005032300007SO 2005 3 23 C2XA05TY029 120050320A531114523121407 FRAME EMB 145 EMB145ER 3260211SO FUSELAGE DAMAGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715941 145035 TYS, DURING A SCHEDULED INSPECTION THE LOWER SKIN SUPPORT BRACKET BETWEEN STR 21L AND 21R ON FR21 HAS ELONGATED HOLES. MAINTENANCE PERFORMED REPAIR WITH TWO INTERNAL L ANGLE DOUBLERS ON FR 21 BETWEEN STR 21L AND 21R. ALODINED, PRIMED AND INSTALLED IAW EC5310-01328 AND EMB 135/145 CPM 51-21-04/05. 2L72 4F RTT00011AT 20050323000092005032300009EU 2005 3 23 05FDEA00555 120050315A5510 STRUCTURE AIRBUS310 A310222 3930315EU HORIZONTAL STAB CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25419FE 345 RIGHT HORIZONTAL STAB L/E LWR CHORD FLANGE FROM STA 158 RIB 5 TO RIB 18 HAS CORROSION ON TOP AND BOTTOM SURFACE EXTENDING UNDER NUT PLATES. REMOVED CORROSION IAW A310-200 SRM 51-74-10 CHECKED LIMITS IAW A310-200 SRM 55-10-00. STRAPED & SHIMED AREA IAW A310-200 SRM 51-11-21. TREATED, PRIMED & TOPCOATED IAW A310-200 SRM 51-21-10 & 51-23-10. RIB 5 TO RIB 13 & RIB 14 TO RIB 18 IS WITHIN LIMITS IAW A310-200 SRM 55-10-00. 2L72 4F RTA35EU 20050323000202005032300020WP 2005 3 23 AALA20050205 120050317A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21290AA 49302 DFW - SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AT 12D INOPERATIVE. REPLACED THE SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT 12D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050323000252005032300025EA 2005 3 23 SWIA200514723 120050315A2740 SERVO CNDAIRCL600 CL6002B19 1900309EA ELEVATOR MALFUNCTIONED A SWIAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 NM07418SW 7446 DURING CRUISE FLIGHT AT FL290 A/C STARTED AN UNCONTROLLED DESCENT. THE AUTOPILOT DISENGAGED AND RECEIVED A AP NOSE DOWN MESSAGE. REPLACED BOTH CAPT'S AND F/O STAB TRIM SWITCHES. REPLACED ELEVATOR SERVO IAW MM 22-11-04. REPLACED ELEVATOR SERVO MOUNT IAW MM 22-11-14. COMPLIED WITH DETAILED INSPECTION OF HORIZONTAL STAB TRIM ACTUATOR IAW AMM TASK 27-42-01-220-801. NO DEFECTS NOTED. ALL SYSTEMS OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050323000272005032300027EU 2005 3 23 SA05029 120050318A335032145410 EPSU AIRBUSA319 A319112 3930323EU PAX CABIN FAULTY A USAAK NONE L NO TEST ININSP/MAINT 1 EA19713UW17968 1040 THE CABIN EMERGENCY LIGHTS WERE INOPERATIVE IN ROWS 3, 6, 11, 15 & 19 DURING TEST. MAINTENANCE REPLACED THE RIGHT SIDE, MID-CABIN EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20050323000282005032300028EU 2005 3 23 SA05030 120050319A5610NP1653116 WINDSHIELD AIRBUSA319 A319112 3930323EU COCKPIT CRACKED A USAAH DEACTIVATE SYST/CIRCUITS A FLAME/FIRE DEDESCENT 1 EA19716UW17892 1055 FLT 53 EN ROUTE CLT TO LAS. DURING DESCENT INTO LAS, THE FIRST OFFICER'S WINDSHIELD BEGAN TO ARC IN THE LOWER LEFT CORNER. IT THEN SHORTED OUT AND THE OUTER PANE CRACKED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FIRST OFFICER'S WINDSHIELD. OK FOR SERVICE. 2L72 4F RTA28NM 20050323000332005032300033EA 2005 3 23 COMA0560181 120050316A2720 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA RUDDER ACTIVATED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01796CA 7338 FLIGHT 5560 CONFIG RUDDER WARNING DURING T/O. COULD NOT DUPLICATE. OPERATIONAL TEST OF RUDDER POSTION WAS SATISFACTORY. 2L72 4F RTA21EA 20050323000342005032300034EA 2005 3 23 COMA0560182 120050315A2131 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA CABIN PRESSURE MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01729CA 7265 FLIGHT 5121 CABIN PRESSURE UNCONTROLLABLE. COULD NOT DUPLICATE. OPERATIONAL CHECK OF PRESSURIZATION SYSTEM WAS SATISFACTORY. 2L72 4F RTA21EA 20050323000462005032300046NM 2005 3 23 SWAA050831 120050317A5230 STOP FITTING BOEING737 7375H4 138449DNM CARGO DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29512SW 24189 DURING SCHEDULED C2 CHECK, FOUND RT FWD CARGO LWR DOOR STOP FITTING CRACKED. REMOVED AND REPLACED CARGO DOOR PER MM. 2L72 4F RTA16WE 20050323000492005032300049EU 2005 3 23 AWXA200500346 120050318A3397ABS0374A24 CABLE AIRBUS320 A320231 3930325EU SEAT ROW 9 RT LOOSE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28632AW 81 PHX - EEL - DURING E-01 CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 9 RT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A LOOSE WIRE AT EMERGENCY ESCAPE PATH LIGHT ASSEMBLY SEAT ROW 9 RT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050323000532005032300053NM 2005 3 23 AWXA200500350 120050309A5347BAC1520792 SEAT TRACK BOEING757 7572G7 1384963NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28908AW 24233 SAL - MAJOR REPAIR - DURING C-1 CHECK EXFOLIATION CORROSION WAS FOUND ON SEAT TRACK AT BS 1180, LBL 45.5. MAINTENANCE REMOVED DAMAGED SECTION OF SEAT TRACK AT BS 1180, LBL 45.5; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK, A STRAP, AND ANGLE; INSTALLED REPAIR PARTS IAW B757-200 SRM 53-00-52, FIG 201. 2L72 4F RTA2NM 20050323000562005032300056NM 2005 3 23 SWAA050833 120050317A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM AFT CARGO BAY CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29654SW 28399 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON SHEAR TIE AT BS 727E, LBL 8. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050323000642005032300064 2005 3 23 UPS05144133 420050317A2565 WARNING LIGHT AIRBUSA300 A300F4622R 3930360EU SLIDE WILL NOT TEST A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01146UP 0829 SLIDE SYSTEM WARNING LIGHT WILL NOT PRESS TO TEST. LIGHT OP. PERFORMED TEST OF EVACUATION WARNING SYS ON MAIN ENTRY DOOR, OPS CK GOOD. ITEM CLEARED M299091 2L72 4F RTA35EU 20050323000692005032300069NM 2005 3 23 SWAA050845 120050318A53306545777 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29503SW 24180 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER AFT CORNER SKIN CUTOUT. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050323000732005032300073NM 2005 3 23 SWAA050849 120050320A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 15R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050323000772005032300077NM 2005 3 23 SWAA050840 120050317A5313BAC1498 STRINGER BOEING737 737317 138447PNM AFT CARGO BAY CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29686SW 23175 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON STR 24L, BS 908. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20050323000822005032300082SO 2005 3 23 C2XA05BT017 120050317A215014522310403 VALVE EMB 145 EMB145XR 3260214SO NR 1 A/C PACK FAULTY A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SW2717138 145727 CREW REPORTED, PACK NR 1 PRODUCED STRONG RUBBER/PLASTIC SMELL DURING LAST 10-15 MINUTES OF FLIGHT; SMELL ASSOCIATED WITH AUTO MODE [OF PACK] ONLY, A/C. RELEASED IAW MEL 21-60-04 CATEGORY-C CONTROL NUMBER 050284. MAINTENANCE REMOVED AND REPLACED FORWARD AIR DISTRIBUTION VALVE IAW EMB145 MM 21-22-01, OPS CHECKED GOOD. 2L72 4F RT 20050323000832005032300083NM 2005 3 23 HNAA0500025 120050317A2497 BUSS DHAV DHC8 DHC8102 2809003NM RT A/C FAILED A HNAAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CLCLIMB 1 EA07907HA 011 RIGHT A/C BUSS FAILURE IN CLIMBOUT. AIRCRAFT RETURNED TO FIELD. REPLACED RIGHT HAND PROP HEAT WIRES FROM RELAY PANEL NR 1 TO RIGHT WING ROOT CONNECTOR. EVALUATION FLIGHT SATISFACTORY. 2H72 4T RTA13NM 20050323000922005032300092NM 2005 3 23 SWAA050854 120050318A53106547978 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29605SW 27956 DURING SCHEDULED D-CHECK, FOUND CORROSION ON CREASE BEAM WEB BETWEEN BS 480 & BS 500, STR 17L. REPAIRED CREASE BEAM PER SRM. 2L72 4F RTA16WE 20050323000952005032300095NM 2005 3 23 SWAA050857 120050318A53116546554 FRAME BOEING737 7373Q8 1384670NM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND CORROSION ON FUSELAGE FRAME AT BS 847, BETWEEN STR 23R & STR 25R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050323000962005032300096NM 2005 3 23 SWAA050858 120050318A5313BAC1498 STRINGER BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND CORROSION AT BS 360, STR 27L. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20050323000982005032300098 2005 3 23 SWAA050860 420050319A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29632SW 27707 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050323001032005032300103 2005 3 23 SWAA050842 420050319A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29765SW 29805 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. RE-INSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20050323001132005032300113WP 2005 3 23 DHL2005805502 120050220A5531 FRAME DOUG DC8 DC873F 302199FWP VERTICAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 VERTICAL STABILIZER L/E FORMER CRACKED 1.000, STA ZFS 104.750. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE AND FABRICATED ANGLE DOUBLER (2EA) (AL7075-T6 0.032) IAW SRM 55-2-0 PG 7-8 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 51-1-21 PG 2, SRM 51-1-20D PG 9. TORQUED IAW SRM 51-3-1 PG 2A TABLE 2. 2L74 4F RT4A25 20050323001142005032300114WP 2005 3 23 DHL2005805503 120050220A5531 FRAME DOUG DC8 DC873F 302199FWP VERTICAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 VERTICAL STABILIZER L/E FORMER CRACKED 1.000, STA ZFS 86.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE AND FABRICATED (2EA) ANGLE DOUBLER (AL7075-T6 0.032) IAW SRM 55-2-0 PG 7-8 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 51-1-21 PG 2, SRM 51-1-20D PG 9. TORQUED IAW SRM 51-3-1 PG 2A TABLE 2. 2L74 4F RT4A25 20050323001162005032300116WP 2005 3 23 DHL2005805501 120050220A5531 FRAME DOUG DC8 DC873F 302199FWP VERTICAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 VERTICAL STABILIZER LT L/E INTERNAL FORMER CRACKED 2.000, ZFS 198.500. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP DRILL ON CRACK END AND FABRICATED ANGLE DOUBLERS (2EA) (AL7075-T6 0.032) IAW SRM 55-2-0 PG 7-8 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED ANGLE DOUBLERS WITH NEW FASTENERS IAW SRM 51-1-21 PG 2, SRM 51-1-20D PG 9. TORQUED IAW SRM 51-3-1 PG 2A. 2L74 4F RT4A25 20050323001432005032300143WP 2005 3 23 UPS05844143 120050320A5610 WINDOW DOUG DC8 DC873F 302199FWP COCKPIT FAILED A IPXABA EMER. DESCENT UNSCHED LANDING O OTHER CRCRUISE 1 SO01874UP 46074 CAPTAINS LEFT SIDE FWD WINDOW SHATTERED DURING CRUISE. DECLARED EMERGENCY DESCENDED TO 10,000 FEET AND DIVERTED TO DFW. R & R CAPTAINS SIDE WINDSHIELD IAW 56-10-02-2. 2L74 4F RT4A25 20050323001452005032300145NM 2005 3 23 CALA0500078 120050319A5347BAC1520792 SEAT TRACK BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2737615 27328 INSPECTION FOUND MAIN CABIN FLOOR LT O/B SEAT TRACK CORRODED AT STA 887-927, LBL 48. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52. 2L72 4F RTA16WE 20050323001522005032300152EU 2005 3 23 MALA050279 120050316A5320 SUPPORT BRACKET SAAB SF340 340B 7860101EU AIRSTAIR CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15427XJ 340B427 DURING 4Y/2Y CHECK IN BNA FOUND CORROSION ON AIRSTAIR SUPPORT BRACKET BETWEEN STA 272 AND STA 288. LT SIDE AFT BRAKE OUT OF LIMIT AFTER CORROSION REMOVAL REF SRM 51-10-10. REPLACED BRACE, FABRICATED PART PER SAMPLE REF SRM 51-20-42/43, SRM 51-40-21. WORK PERFORMED ON EMB WO 211863 TASK 1510. 2L72 4T RTA52EU 20050323001582005032300158CE 2005 3 23 DXTA200500633 120050318A3213 STRUT CESSNA750 750 2076810CE NLG UNDERSERVICED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07982QS2728 7500182 AFTER DEPARTURE FROM MIDWAY, GEAR HANDLE WOULD NOT RELEASE FROM THE DOWN POSITION, COULD NOT BE RAISED, AIRCRAFT RETURNED FOR LANDING. JACKED ACFT AND FOUND THE NOSE STRUT NOT EXTENDING PROPERLY. CHECKED SERVICING AND FOUND THAT THE AIR PRESSURE WAS LOW. SERVICED NOSE STRUT. PERFORMED OPS CHECK OF LANDING GEAR HANDLE. NO DEFECTS NOTED AT THIS TIME IAW CE 750 MM 12-10-68. 2L72 4J RTT00007WI 20050323001592005032300159CE 2005 3 23 DXTA200500634 120050319A3260387 LIGHT CESSNA750 750 2076810CE ANNUNCIATOR BURNED OUT E DXTAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL07947QS 7500047 ON APPROACH TO 25L AT LAX, NOTICED NOSE GEAR LIGHT NOT ILLUMINATED. BLEW BOTTLE AND PULLED D-RING. DECLARED AN EMERGENCY AND LANDED UNEVENTFULLY. FOUND NOSE GEAR ANNUNCIATOR BULBS BURNT OUT. RELAMPED ANNUNCIATOR. BLED GEAR SYSTEM. SERVICED RESERVOIRS AS REQUIRED. GEAR AND ANNUNCIATOR SYSTEMS OPERATIONAL CHECKS GOOD AT THIS TIME. ALL WORK IAW CHS 12-10-15, 12-10-36 AND 32-30-00 OF THE CE 750 MM. 2L72 4J RTT00007WI 20050323001602005032300160CE 2005 3 23 69761 120050315A3010 ANNUNCIATOR BEECH 1900 1900D 1154162CE WING DE ICE SYS ILLUMINATED A AMWAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 CE07143YV UE143 THE PILOTS TOOK OFF FROM DUJ ABOUT 60NM FROM PKB. ON LAST FLIGHT OF THE DAY CHECKS, NOTICED THAT WHEN THE SURFACE DEICE WAS CYCLED THAT THE TAIL DEICE AND INBOARD WING DEICE ANNUNCIATORS REMAINED ILLUMINATED, ALONG WITH ABNORMAL INDICATIONS ON THE VACUUM AND PRESSURE GAUGES. THE ANNUNCIATORS WENT OFF AFTER SOME TIME, AND THEN RE-ILLUMINATED. THE CREW, ALONG WITH DISPATCH, DECIDED TO RETURN TO DUJ. THE OPERATIONAL CHECK WAS NORMAL AND MAINTENANCE WAS UNABLE TO DUPLICATE THE PROBLEM. THEREFORE NO PARTS WERE USED. 2L72 4T RTA24CE 20050323001622005032300162NM 2005 3 23 HNAA0500027 120050319A6120 WARNING LIGHT DHAV DHC8 DHC8102 2809003NM NR 2 PROP BETA ILLUMINATED A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07815EX 321 NR 2 PROP BETA LOCKOUT FAILURE ON CLIMBOUT. INSTALLED TEST HARNESS AT CONNECTOR J38 & J39 AND TESTED SWITCHES 6121-S10 & S1, 6141 S3 & S4. COMPLETED JOB CARD 61-20-10Q GROUND OPS CHECK OF BETA LOCKOUT. FOUND NO FAULTS WITH BETA LOCKOUT SYSTEM. 2H72 4T RTA13NM 20050323001632005032300163SO 2005 3 23 CHQA200500057 120050101A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11258JQ 145768 LEFT AFT OVERWING EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED LIGHT BULB IAW EMB 145 AMM 3-50-10. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050323001642005032300164SO 2005 3 23 CHQA200500058 120050120A335078812 LIGHT EMB 135 EMB135LR 3260305SO CABIN INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11844RP 145620 EMERGENCY LIGHTS ON FLOOR BETWEEN ROWS 7 THROUGH 10 ARE INOP. FOUND EMERGENCY BATTERY NR 4 DISCONNECTED. RECONNECTED BATTERY IAW EMB 135 AMM 33-50-04. OPS CHECK GOOD. REPLACED LIGHT STRIP DUE TO BROKEN WIRE IAW EMB 135 AMM 33-20-00. 2L72 4F RTT00011AT 20050323001652005032300165EU 2005 3 23 CHQA200500059 120050317A275017039237901 ROD EMB ERJ170ERJ170100LR EU TE FLAPS BROKEN A CHQAO OTHER J WARNING INDICATION DEDESCENT 1 GL11631RW1522 1004 17000007 ON DESCENT SLOWED TO 210KTS & DESCEND 7000 FEET. FLAPS HANDLE SELECTED TO FLAPS 1. AN EICAS MESSAGE PRESENTED FLAPS FAIL. THE INDICATION ON THE CORRESPONDING DISPLAY UNIT SHOWED SLATS 3 AND FLAPS 0 (YELLOW INDICATION). RAN THE FLAPS FAIL CHECKLIST. F/A PREPARED FOR POSSIBLE EMERGENCY LANDING. LANDED ON 9R WITH FLAPS 0 AND NO OTHER ABNORMAL EVENTS. A/C WAS UNDER MAXIMUM LANDING WEIGHT. TAXIED TO THE GATE WITH NO OTHER INCIDENTS. TROUBLESHOT FOUND BOTH LEFT I/B FLAP ROD ASSEMBLIES, P/N 170-39237-901 WERE BROKEN. REMOVED & REPLACED BOTH LEFT I/B FLAP CONTROL RODS. REMOVED & REPLACED BOTH SHIMMY DAMPNERS, P/N 2244A0000-03, S/N 00141 AND S/N 00138. OPS CHECK GOOD. 2L74 4F RTA56NM 20050323001662005032300166 2005 3 23 SWAA050826 420050317A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050323001672005032300167NM 2005 3 23 SWAA050827 120050317A3350101073 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29475WN 32474 DURING SCHEDULED RON CHECK, FOUND EMERGENCY EXIT SIGN LENS CRACKED IN AFT GALLEY. REMOVED AND REPLACED LENS PER MM. 2L72 4F RTA16WE 20050323001682005032300168NM 2005 3 23 SWAA050828 120050317A53306545775 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29508SW 24185 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STR 25L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050323001692005032300169NM 2005 3 23 SWAA050829 120050317A53306545776 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29508SW 24185 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 895, STR 25R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050323001702005032300170NM 2005 3 23 SWAA050830 120050317A53306545777 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29508SW 24185 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050323001722005032300172EA 2005 3 23 MASA200500216 120050315A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0777331 7331 LT MIDDLE FUSELAGE EMERGENCY LIGHT INOP. RELAMPED, OPS CHECK GOOD. 2L72 4F RTA21EA 20050323001742005032300174SO 2005 3 23 MASA200500229 120050318A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSBURNED OUT A MASAK NONE O OTHER ININSP/MAINT 1 SW07846MJ 145507 ON RON AND SCHEDULED FOR A ROUTINE CHECK INSPECTION, DURING THE WALKAROUND IT WAS DISCOVERED THAT THE RT EXTERNAL OVERWING EMERGENCY LIGHT NOT ILLUMINATING. REPLACED THE LIGHT BULB AND OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050323001752005032300175EA 2005 3 23 COMA0560176 120050313A3030 THERMOSWITCH CNDAIRCL600 CL6002B19 1900309EA ANTI ICE SYSTEM MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01924CA 7026 FLT 5454 WING ANTI-ICE DUCT WARNING. REPLACED WING THERMAL SWITCH FOR TROUBLESHOOTING. 2L72 4F RTA21EA 20050323001802005032300180NM 2005 3 23 DHL2005781529 120050211A5530 PANEL BOEING727 727227 1384078NM VERTICAL STAB DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A C-CHECK, VERT STAB RT SIDE TRAPIZOIDAL PANEL HAS 3 SHARP DENTS BELOW PREVIOUS REPAIR. CUT OUT DENTED AREA ON RT VERT TRAPAZOID PANEL APPROX 2 INCH DIA AND REMOVED PREVIOUS REPAIR APPROX 3 X 3.5 INCH, FABRICATED FILLERS, 1- APPROX 2 INCH DIA AND 2 - APPROX 3 X 3.5 INCH AND DOUBLER APPROX 8 X 13 INCH FROM .016 INCH 2024T3 PO9001660 BONDED FILLERS AND DOUBLERS, CURED, CLEANED, PRIMED AND SEALED IAW B727 SRM 55-30-1 FIG 2, 55-30-2 FIG AND 51-40-20 FIG 30. 2L73 4F A3WE 20050323001812005032300181NM 2005 3 23 DHL2005781530 120050211A5754 SKIN BOEING727 727227 1384078NM NR 2 SLAT GOUGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A C-CHECK, NR 2 SLAT SKIN GOUGED AT I/B SLAT HOOK (MARKED). REMOVED FASTENERS FOR ACCESS AT NR 2 SLAT SKIN AT I/B SLAT HOOK IAW B727 SRM 51-30-2. FABRICATED DOUBLER REPAIR MAT USED 2024T3 .125 PO 9001068 DIM 5.5 X 3.5 INCH IAW B727 SRM 57-50-3 FIG 10. ALODINED AND PRIMED PART IAW B727 SRM 51-10-2. INSTALLED COUNTER SINK REPAIR WASHERS IAW B727 SRM 51-30-8 FIG 4. INSTALLED DOUBLER REPAIR IAW B727 SRM 57-50-3 FIG 10. 2L73 4F A3WE 20050323001822005032300182NM 2005 3 23 AALA20050198 120050315A3350 LIGHT BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217375A 25202 SFO - EMERGENCY LIGHT AT SEAT 35H INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 35H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050323001832005032300183EU 2005 3 23 RAIA00502035 120050228A3260 SQUAT SWITCH JETAIRJETSTMJETSTM4101 1500501EU MLG DIRTY A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03571HK 41090 STL - RT RED BETA LIGHT CAME ON DURING TAKEOFF ROLL. MAINTENANCE CLEANED AOG SWITCH ON NR 2 MLG. 2L72 4T RTA41NM 20050323001842005032300184SO 2005 3 23 SWIA200514656 120050227A215022045404 ACM EMB 120 EMB120ER 3260203SO SMOKE A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 NM07236SW730 730 120312 ON DESCENT, WITH BLEED AND PACKS SELECTED ON AUTO AND LOW, RIGHT PACK FAIL INDICATION, SLIGHT SMELL OF SMOKE IN FLIGHT DECK AND CABIN. REMOVED AND REPLACED RIGHT ACM IAW EMB 120 MM 21-50-05, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050323001852005032300185EA 2005 3 23 SWIA200514657 120050305A2760C13045BA03 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA SPOILERS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07728SK117 117 10192 SPOILER/STAB FAULT STATUS MESSAGE. REPLACED NR 1 SSCU IAW CRJ 700 MM 27-61-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050323001862005032300186EA 2005 3 23 SWIA200514658 120050228A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07438SW 7574 SECOND OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050323001872005032300187SO 2005 3 23 SWIA200514659 120050225A3350 LIGHT EMB 120 EMB120ER 3260203SO EMERGENCY EXIT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07294SW 120321 ONE RED EMERGENCY EXIT FLOOR LIGHT AT MCD IS INOPERATIVE. REPLACED LIGHT ASSY, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050323001882005032300188SO 2005 3 23 SWIA200514660 120050228A3350 LIGHT EMB 120 EMB120ER 3260203SO CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07562SW 120336 EMERGENCY LIGHTS WILL NOT ILLUMINATE. CHANGED EMERGENCY LIGHTS, OPERATIONAL CHECK OK. 2L72 4T RTA31SO 20050323001892005032300189NM 2005 3 23 SWAA050763 120050311A575465C26686 SKIN BOEING737 7373H4 1384600NM LT WING SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29639SW 27712 DURING SCHEDULED C4 CHECK, FOUND OUTBOARD END NR 2 L/E SLAT LOWER SKIN CRACKED. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050323001902005032300190NM 2005 3 23 QXEA200500348 120050302A2750 TORQUE TUBE DHAV DHC8 DHC8202 2809007NM TE FLAPS BINDING A QXEAO OTHER J WARNING INDICATION APAPPROACH 1 NM09348PH17685 484 SEA - FLIGHT 2256 - ON SHORT FINAL, WHEN FLAPS WERE SELECTED, THE CREW RECEIVED A MASTER CAUTION FOR THE FLAP DRIVE. AFTER THE LANDING CHECKLIST AND FLAPS WERE SELECTED TO ZERO, THE FLAPS REMAINED AT 15 DEGREES. MAINTENANCE INSPECTED THE SYSTEM AND REPLACED THE FLAP TORQUE TUBE AND SENSOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050323001922005032300192NM 2005 3 23 AALA20050206 120050317A7720ETPU10003C SENSOR BOEING757 757223 1384957NM LT ENGINE INOPERATIVE A AALAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 SW21183AN 29593 MIA - INFLIGHT LEFT HAND ENGINE BEGAN HIGH FREQUENCY VIBRATION AND OVER TEMPERATURE AT 230 IN HEAVY PRECIPITATION. POWER WAS REDUCED TO IDLE AND DESCENT ACCOMPLISHED BUT OVER TEMPERATURE CONTINUED TO MAX ENGINE GENERATOR TEMPERATURE OF 900C. ENGINE WAS SHUTDOWN PER QRH PROCEDURE AND UNEVENTFUL FOR SINGLE ENGINE APPROACH. VISUALLY INSPECTED INLET AND EXHAUST NO DAMAGE NOTED. ACCOMPLISHED BOROSCOPE OF HPC HPT IPT AND LPT ACCOMPLISHED BITE CHECK OF EEC BVCU TPU AND AVM MONITOR. REPLACED AVM MONITOR AND ACCELORMETER. REPLACED BVCU AND TPU. REPLACED TPU SENSOR AND DEDICATED GENERATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050324000012005032400001EU 2005 3 24 05FDEA00571 120050315A5347 SEAT TRACK AIRBUS310 A310222 3930315EU CARGO DECK CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25419FE 345 M-DECK CARGO COMP'T RT NR 4 SEAT TRACK FR46, FR47, FR48, FR49.5, FR50.5, FR51.3, FR52.5, FR53.4, CORROSION INSIDE SCALOPE HOLES, 9-AREAS. REMOVED CORROSION IAW A310-200 SRM 51-74-10, OUT OF LIMITS IAW SRM 53-10-16 FIG 101. FABBED NEW SEAT TRACK IAW DWG A538-11923. REMOVED AND REINSTALLED CLS ADAPTERS AT FR46 TO FR54 IAW A310-200 SRM 51-72-10. REMOVED BAD SECTION OF TRACK & INSTALL NEW SEAT TRACK FROM FR46 TO 54 IAW SRM A310-200 51-72-10. 2L72 4F RTA35EU 20050324000022005032400002EU 2005 3 24 05FDEA00577 120050316A5753 WEDGE AIRBUS310 A310222 3930315EU TE FLAP DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 REPAIR NEEDS EVALUATION FOR FAA APPROVED DATA AND MAJOR OR MINOR CLASSIFICATION. LT WING REPAIR LOWER SURFACE I/B TRAILING EDGE FLAP FWD OF THE TRAILING EDGE WEDGE AND AFT OF NR 2 FLAP TRACK BEAM, ITEM 57 OF LIST. LT WING I/B FLAP LOWER SURFACE, AND AFT OF NR 2 TRACK BEAM REPAIR DOUBLER IS RIVETED ACCESS PANEL ON I/B FLAP ASSY DWG AND FOUND TO BE IN CONFORMANCE WITH AIRBUS DWG A579- 70100. 2L72 4F RTA35EU 20050324000102005032400010EU 2005 3 24 MALA050215 120050126A2731 TRIM SYSTEM BAC 146 AVRO146RJ85A1500097EU ELEVATOR INOPERATIVE A MALAO OTHER J WARNING INDICATION TOTAKEOFF 1 GL15508XJ E2318 ABOVE 80 KTS ON T/O ROLL FO'S MASTER WARN LIGHT AND MWS FAULT LIGHT ILLUMINATED CONTINUED ROLL AND RETURNED TO DETROIT. MWS SYSTEM OPS CHECK GOOD DURING TROUBLESHOOTING FOUND ELEVATOR TRIM INOP. TRIM WAS REPAIRED WITH DFGC SYSTEM OPS CHECK GOOD. REQ TEST RUN FOR OPS CHECK OF FO'S MWS SYSTEM 2H74 4F RTA49EU 20050324000112005032400011EU 2005 3 24 MALA050195 120050112A52807252456003 ARM SAAB SF340 340B 7860101EU MLG DOOR CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15366PX 340B267 BRACKET FOR HOLD OPEN ARM ON SPR DOOR IS CRACKED AND WILL BE REPLACED IAW SRM 51-40-21. REF EAMS WORK ORDER 211360 TASK 6501. 2L72 4T RTA52EU 20050324000132005032400013EU 2005 3 24 MALA050197 120050105A3350330151 BATTERY SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A MALAK NONE L NO TEST ININSP/MAINT 1 GL15410XJ 340B410 BATTERY POWER SUPPLY PN 3301-51 SN 1304. REPORTED INOP REPLACED BATTERY ASSY, UNIT PASSES CMM CHECKS. RTS 1/6/05 2L72 4T RTA52EU 20050324000142005032400014EU 2005 3 24 MALA505201 120050130A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15422XJ 340B422 SEAT TRACK AT BLO IS CORRODED FROM FS 630 TO FS 686. DAMAGE HAS BEEN REPAIRED IAW MESABA EO NR S53076. REF EAMS WORK ORDER 211546 TASK 1505, FOUND DURING 4Y/2Y CHECK. 2L72 4T RTA52EU 20050324000152005032400015EU 2005 3 24 MALA050202 120050130A53207253721439 WEB SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15422XJ 340B422 REINFORCEMENT WEB, PN 7253721-439 IS CORRODED OUT OF LIMITS AND HAS BEEN REPLACED IAW SRM 51-40-21. REF EAMS WORKORDER 211546 TASK 1514, FOUND DURING 4Y/2Y CHECK IN BNA. 2L72 4T RTA52EU 20050324000172005032400017NM 2005 3 24 WRLA2005039 120050207A5512 SKIN DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST RT BARREL NUT HOLE NR 28. 2L73 4F4 FRTA22WE E24NE 20050324000182005032400018NE 2005 3 24 ASMF200502013 220050224A732176960615 FUEL CONTROL DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE LT ENGINE FAILED W ASMFK NONE J WARNING INDICATION ININSP/MAINT 1 SW23214AM119412465 49585 725948 CAPTAIN REPORTED LEFT ENGINE WITH OSCILLATIONS IN ALL ITS PARAMETERS. THE COMBUSTION CHAMBER WAS SERVICED AND WATER TRAMP WAS DRAINED IAW 72-40-01, ALL CORRECT. DURING OVERNIGHT SERVICE LEFT FCU WAS REPLACED IAW MM 73-12-01 AND THE LEFT ENGINE WAS TESTED IAW MM 71-00-00, ALL CORRECT. 2L72 4F4 FRTA6WE E9NE 20050324000212005032400021WP 2005 3 24 WX0500011 120050130A5270 ANNUNCIATOR DOUG DC9 DC983 3022083WP AIRSTAIR DOOR ILLUMINATED A WX0AC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP19865GA 49998 IFP TO SJC-AFT STAIRWAY DOOR ANNUNCIATOR ILLUMINATED DURING TAKEOFF. TAKEOFF WAS ABORTED. CREW CONTACTED MAINTENANCE CONTROL, AFT STAIRWAY ANNUNCIATOR WAS DEFERRED IAW MEL 52-7. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050324000272005032400027NM 2005 3 24 2005UALA00240 120050314A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29583UA 26705 CORROSION FOUND AT BS 1480 FRAME BETWEEN STR 27L TO 28L, ON INBD FLANGE. DAMAGE CAUSED BY CORROSION. REPAIRED FRAME USING A NESTED J-ANGLE REPAIR DOUBLER. 2L72 4F4 FRTA2NM E17NE 20050324000282005032400028SO 2005 3 24 C2XA05IA022 120050209A3350110049 POWER SUPPLY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716981 145208 CHS - FLIGHT 3324, DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHTS WERE ON CONTINUOUSLY, AND ROW 5 EMERGENCY LIGHTS WERE INOPERATIVE. THE AIRCRAFT WAS FERRIED TO CLE WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO EMERGENCY LIGHT BATTERY CHARGER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050324000312005032400031EA 2005 3 24 SWIA200514652 120050228A3520 OXYGEN MASK CNDAIRCL600 CL6002B19 1900309EA CABIN DEPLOYED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07924SW 7681 WHILE AT GATE CABIN O2 MASK DEPLOYED. RESTOWED ALL PAX O2 MASK, IAW MM 35-21-09. OPERATIONAL CHECKED GOOD. 2L72 4F RTA21EA 20050324000332005032400033NM 2005 3 24 QXEA200500291 120050223A2611 SMOKE DETECTOR BOMBDRDHC8 DHC8401 1390041NM CARGO BAY WILL NOT TEST A QXEAK NONE O OTHER ININSP/MAINT 1 NM09415QX 4081 SEA - THE FORWARD CARGO SMOKE DETECTOR WILL NOT TEST. MAINTENANCE PERFORMED SEVERAL OPERATIONAL CHECKS WITH NO DEFECTS NOTED. THE DETECTOR OPERATED NORMALLY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050324000362005032400036EA 2005 3 24 COMA0560146 120050225A2750 DRIVE SHAFT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS DIRTY A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01471CA 7655 FLIGHT 5102 - DURING YFC APPROACH RECEIVED A FLAP FAIL CAUTION, CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. CLEANED AND LUBRICATED THE LEFT WING FLAP FLEX DRIVE SHAFTS AND LUBRICATED THE LEFT AND RIGHT FLAP ACTUATORS. 2L72 4F RTA21EA 20050324000392005032400039NM 2005 3 24 WRLA2005025 120050217A5512 SKIN DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST LT BARREL NUT HOLE NR 02. 2L73 4F4 FRTA22WE E24NE 20050324000422005032400042NM 2005 3 24 WRLA2005028 120050218A5512 SKIN DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST LT BARREL NUT HOLE NR 28. 2L73 4F4 FRTA22WE E24NE 20050324000432005032400043NM 2005 3 24 WRLA2005029 120050218A5512 SKIN DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST LT BARREL NUT HOLE NR 31. 2L73 4F4 FRTA22WE E24NE 20050324000452005032400045SO 2005 3 24 C2XA05CL011 120050214A3397M8372375R1624N CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT SHORTED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716981 145208 ORD FLIGHT NR2758, CREW REPORTED THAT THE EMERGENCY LIGHTS WOULD NOT SHUTOFF. AIRCRAFT WAS FERRIED TO CLE WHERE MAINTENANCE REPLACED THE CONNECTOR AT THE NR 2 EMERGENCY BATTERY. ALL OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20050324000462005032400046NE 2005 3 24 0500196729 220050214A7200 ENGINE BOEING747 747251F 1384898NM PWA JT9 JT9D7Q 52054NE NR 4 OVERHEATED A NWAAEA ENGINE SHUTDOWN UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 GL01629US 22388 702134 SHORTLY AFTER TAKEOFF, THE NR 4 ENGINE NACELLE TEMPERATURE BEGAN TO INCREASE FOLLOWED BY THE FIRE WARNING ANNUNCIATION. THE CREW FOLLOWED COM PROCEDURES AND WHEN POWER WAS REDUCED THE FIRE WARNING CEASED AND THE NACELLE TEMPERATURE BEGAN TO DECREASE. THE NR 4 ENGINE WAS SHUT DOWN AND THE FLIGHT RETURNED TO MSP LANDING WITHOUT INCIDENT. THE ENGINE WAS REPLACED. OPERATIONAL CHECK GOOD. 2L74 4F4 F A20WE E3NE 20050324000472005032400047NM 2005 3 24 WRLA2005071 120050223A5512 SKIN DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST RT BARREL NUT HOLE NR 19. 2L73 4F4 FRTA22WE E24NE 20050324000492005032400049NM 2005 3 24 WRLA2005073 120050223A5512 SKIN DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST LT BARREL NUT HOLE NR 30. 2L73 4F4 FRTA22WE E24NE 20050324000532005032400053NM 2005 3 24 WRLA2005057 120050207A5511 SPAR CAP DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST LT BARREL NUT HOLE NR 01. 2L73 4F4 FRTA22WE E24NE 20050324000542005032400054EA 2005 3 24 QXEA200500180 120050121A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - RIGHT OUTBOARD SIDE FACING SEAT RAIL, AT STATION X810, HAS PITTING CORROSION ON MOST INBOARD SURFACE. REPAIRED IAW SRM 51-21-06-001-001-A01 AND HORIZON AIR EA R-53-266. 2L72 4F RTA21EA 20050324000552005032400055EA 2005 3 24 QXEA200500181 120050122A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - LEFT OUTBOARD SIDE FACING SEAT RAIL AT STATION X796, HAS PITTING CORROSION ON INSIDE SURFACE. REPAIRED IAW CRJ SRM 51-21-06-001-001-A01 AND HORIZON AIR EA R-53-266. 2L72 4F RTA21EA 20050324000562005032400056NE 2005 3 24 HNAA0500012 220050217A7297 ELEC CONNECTOR DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE NR 2 ENGINE CONTAMINATED A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07846EX 326 120375 MASTER WARNING LIGHT FLICKERED ON/OFF IN FLT FOLLOWED BY NR 2 ENG OIL PRESSURE WARNING LIGHT ILLUMINATED F/O STATED THAT HE DID SEE PRE FLUX NR 2 ENG OIL PRESS BUT IT DID NOT GO BELOW 45 PSI. CLEANED NR 2 ENGINE LOW OIL PRESSURE CONNECTOR SERVICED OIL LEVEL TO MAX OIL LEVEL WAS 1.5 QRTS LOW, RAN AIRCRAFT, SYSTEM OPS CHECK GOOD AT THIS TIME. 2H72 4T4 TRTA13NM E20NE 20050324000592005032400059EU 2005 3 24 AWXA200500260 120050226A2780831A000002 BRAKE ASSY AIRBUS320 A320231 3930325EU LT WING OUT OF ADJUST A AWXAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 WP28633AW49096 082 ON APPROACH INTO PHX EN ROUTE FROM ATL WHEN SELECTING FLAPS 1 THE SLATS LOCKED OUT AT SLATS 1, FOLLOWED ECAM INSTRUCTIONS AND PERFORMED PRECAUTIONARY LANDING. MAINTENANCE TROUBLESHOT SLAY SYS PER TSM 27-81-00-810-815 AND FOUND LT WING TIP BRAKE ASSY BREAK OUT FORCE AT 80 IN LBS, LIMIT IS 44 IN LBS. R & R LT WING TIP BRAKE ASSY IAW AMM 27-81-00-000, OPS CHECK OF SLAT SYS GOOD. VENDOR REPORTED THAT RETURN OF WING TIP BRAKE SN 456 WAS JUSTIFIED AND CONFIRMED NOTING ON DISASSEMBLY THAT SPRING, FIG. 4-5A OF CMM 27-09-12 REV 8, WAS UNDERSIZED AND BALL BEARING, FIG 3-140A AND FIG 4-100A FROM CMM 27-09-12 REV. 8, WAS RUNNING ROUGH. UNIT WAS TESTED AND OVERHAULED IAW CMM 27-09-12 REV. 8 2L72 4F RTA28NM 20050324000602005032400060NM 2005 3 24 AWXA200500261 120050127A534069265553 CLIP BOEING737 737301 1384611NM L1 DOOR FRAME CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK, A 3" CRACK WAS FOUND IN AFT SIDE L-1 DOOR FRAME INTERCOSTAL ATTACH CLIP AT BS 348.2, STR 17 LT. MAINTENANCE REMOVED CRACKED L-1 DOOR FRAME INTERCOSTAL ATTACH CLIP AT BS 348.2, STR 17 LT; FABRICATED A NEW REPLACEMENT ATTACH CLIP; INSTALLED REPAIR PART IAW E.R. 03-5300-05053-SS3. 2L72 4F RTA16WE 20050324000642005032400064NM 2005 3 24 05FDEA00482 120050309A5330 SKIN DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25592FE 48550 RT FUSELAGE EXTERIOR SKIN BETWEEN STA 1139-1119 LT 25 CRACKED. CRACKED AREA BLENDED AS PER SRM 51-21-01 VOL2 WITH NO FURTHER CRACK AND FOUND WITHIN LIMIT AS PER SRM 53-20-00 FIG 6 VOL 1. 2L73 4F RTA22WE 20050324000672005032400067NM 2005 3 24 F3LA200500010 120050308A5320 STRAP BOEING737 7373L9 1384470NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03313FL 4372 26442 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON AFT GALLEY PAN STRAP AT BS 1016, BETWEEN RBL 30 AND LBL 30. FOUND TO BE OUT OF LIMITS PER SRM 53-60-61, FIG 101, DETAIL VII. REMOVED PAN STRAP PER SRM 51-40-02. FABRICATED NEW STRAP AND INSTALLED PER EA 53-53R-10753, SRM 51-10-02 AND SRM 51-40-02. 2L72 4F RTA16WE 20050324000692005032400069NM 2005 3 24 ANCF200400039 120050208A213121173886 CONTROLLER BOEING757 757236 1384971NM RROYCERB211 RB211535E4 54555NE CABIN PRESSURE MALADJUSTMENT W ANCFGA O2 MASK DEPLOYED UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO23506NA578991205 24771 3067730737 EICAS MSG CABIN ALTITUDE DISPLAYED, CABIN ALT AND CABIN ALTITUDE LIGHTS ILLUM. UNABLE TO RESTORE CABIN PRESS USING MANUAL MODE. AT 39000 FT CABIN ALTITUDE MSG DISPLAYED. THE CABIN ALTITUDE SHOW`S 12000 FT AND START THE DESCENT, THE DESCENT WAS ACCOMPLISHED AND THE CABIN DESCENT IN NORMAL MODE. AS PER AMM 21-31-02 PAGE BLOCK 401 AUTOMATIC PRESSURE CONTROLLER WAS REPLACED, IAW AMM 21-31-03 CABIN OUTFLOW VALVE WAS REPLACED, PRESSURIZATION CONTROL SYSTEM TEST WAS SATISFACTORY IAW AMM 21-31-00/501, P/N 2117388-6 ON AND OFF, S/N OFF 10-1976 S/N ON 113-59. 2L72 4F4 FRTA2NM E12EU 20050324000702005032400070CE 2005 3 24 2003792 120050214A53101294300433 WINDOW FRAME BEECH 1900 1900D 1154162CE CABIN CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03179GL UE179 ON ROUTINE STRUCTURAL INSPECTION, ALL THREE EMERGENCY EXIT WINDOW PANS HAVE CRACKS. WINDOW PANS REPLACED, AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA24CE 20050324000742005032400074NM 2005 3 24 DHL2005781515 120050210A7110 NOSE COWL BOEING727 727227 1384078NM NR 1 ENGINE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A "C" CHECK, NR 1 ENG NOSE COWL EXTERIOR SKIN HAS DENT AT 6 O'CLOCK POSITION; DENT OUT OF LIMITS BY A/Y RATIO A.1.9 .075=25 IAW B727SRM 54-30-1 FIG 1. REMOVED INTERNAL ANTI-ICE DUCTS TO FOLICATE S/M WORK IAW B727 M/M 30-21-14. REMOVED FASTENERS FOR ACCESS AT NR 1 ENG COWL EXTERIOR SKIN 6 O'CLOCK POSITION IAW B727 SRM 51-30-2. CUT OUT DAMAGED AREA DIM 2 INCH BY 1 INCH IAW B727 SRM 54-30-3 FIG 8. FABRICATED DOUBLE REPAIR USING 2024 T3 .040 PO 90001634 DIM. 6 INCH BY 3 3/4 INCH IAW B727 SRM 54-30-3 FIG 1, ALOIDINE AND PRIMED IAW B 727 SRM 51-10-2. INSTALLED DOUBLER REPAIR IAW B727 SRM 54-30-3 FIG 8. 2L73 4F A3WE 20050324000752005032400075WP 2005 3 24 NACA20050002 120050201A3230 LANDING GEAR DOUG DC6 DC6A 3021706WP LT AND RT MALFUNCTIONED A NACAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 AL0399330 43576 NOSE GEAR WOULD NOT RETRACT. ISOLATED RT AND LT MAIN GEAR, PERFORMED NOSE GEAR SWING. OPS CHECKED GOOD PER MI REPORT: (CHECKED UP LOCK SWITCH ACTIVATION, NO DEFECTS FOUND. HEATED SWITCH AND PERFORMED GEAR SWING. CHECKED GOOD FIRST TIME, OPERATED 4 CONSECUTIVE TIMES WITH NO DISCREPANCIES. 2L74 4R 6A3 20050324000762005032400076EA 2005 3 24 COMA0560190 120050321A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01494CA 7765 LEFT HAND ENGINE SUPPORT BEAM HAS CRACK. REPAIRED IAW REO 601R-53-61-366. 2L72 4F RTA21EA 20050324000782005032400078EA 2005 3 24 05056703 120050225A2741 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA STAB TRIM ILLUMINATED A VTZAO OTHER J WARNING INDICATION APAPPROACH 1 EA27703BR 7467 EVENT SUMMARY STATED MACH TRIM FAILURE MSG AND STAB TRIM MSG. WO CA: C/W BOMBARDIER SL 27-083. 2L72 4F RTA21EA 20050324000792005032400079NM 2005 3 24 ASMF200502009 120050213A793141800044 TRANSMITTER DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE ENGINE OIL PRESSFAILED W ASMFC ABORTED TAKEOFF EJ VIBRATION/BUFFET WARNING INDICATION TOTAKEOFF 1 SW23169PL10915 53175 718246 CAPTAIN REPORTED THAT OIL PRESS DURING TAKEOFF & CLIMB RAISING TO 70 PSI, FLASHING INDICATION CRUISE "FT 58 PS’S" REDUCING POWER. CAPTAIN REPORTED STRONG VIBRATION IN THE PAX CABIN. RT ENGINE OIL PRESS ADJUSTED IAW MM, TESTED CORRECT & ENGINE VIBRATION CHECK PERFORMED IAW MM. LATER, ACFT RETURNED TO PLATFORM 2 TIMES DUE TO SAME FAILURE. OIL PRESS TRANSMITTER REPLACED AND RT ENGINE OIL PRESS ADJUSTED IAW MM 79-20-03, TESTED CORRECT. DURING OVERNIGHT SERVICE, CSD, OIL GENERATOR & RADIATOR WERE REPLACED IAW MM, RT ENGINE MAIN OIL FILTER & CHIP DETECTORS WERE CHECKED IAW MM. RT ENGINE OIL PRESSURE VALVE REPLACED IAW MM, TESTED CORRECT. 2L72 4F4 FRTA6WE E9NE 20050324000802005032400080NM 2005 3 24 F3LA200500008 120050309A5320 SILL BOEING737 7373L9 1384470NM L2 DOOR CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03313FL 4372 26442 DURING C-4 CHECK INSPECTION, REPORTED L2 DOOR MOP SILL CORRODED. REPLACED L2 DOOR MOP SILL PER SRM 51-40-02. 2L72 4F RTA16WE 20050324000812005032400081 2005 3 24 2005UALA00241 420050313A2565 WARNING LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE L3 DOOR SLIDE MALFUNCTIONED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29553UA 25277 DOOR 3L SLIDE LIGHT WOULD NOT GO OFF WITH DOOR DISARMED. ALTHOUGH UNABLE TO DUPLICATE INCIDENT, IT IS SPECULATED CONDITION WAS CAUSED BY DIRT OR DEBRIS ON PROXIMITY SENSORS WHICH AFFECTS THE INDUCTANCE NECESSARY FOR SYSTEM OPERATION. 2L72 4F4 FRTA2NM E17NE 20050324000822005032400082NM 2005 3 24 2005UALA00242 120050314A2497 WIRE BOEING757 757222 1384956NM PWA 2037 PW2037 NE TRANSFORMER CHAFED A UALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 WP29506UA 24627 FOUND WIRES FROM K114 RELAY CHAFING ON CURRENT SENSING TRANSFORMER BRACKET. FOUND HARNESS ARCING AND SMOLDERING. P-34 ELECTRICAL POWER PANEL, WIRE W1134-0024-8 FROM RELAY K114 TERMINAL C1, WAS FOUND CHAFFED AND ARCING ON THE SUPPORT BRACKET OF CURRENT TRANSFORMER T116. REPLACED WIRE W1134-0024-8 FROM RELAY K114 TERMINAL C1 TO C/B C305 AND WIRE W1134-0009-8 FROM RELAY K114 TERMINAL C1 TO C/B C306 (WIRES ARE CRIMPED TOGETHER ON THE SAME TERMINAL AT K114 -C1). 2L72 4F4 FRTA2NM E17NE 20050324000842005032400084NM 2005 3 24 2005UALA00244 120050314A2420 GENERATOR BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE NR 1 ENGINE FAILED A UALAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 WP29381UA 24656 RETURNED TO FIELD DUE TO A LOST NR 1 ENGINE GENERATOR. FOUND THE CSD OVERSERVICED, AND THE DELTA P INDICATOR POPPED. METAL SHAVINGS WERE FOUND IN THE FILTER BOWL, SO CSD OIL SYSTEM WAS FLUSHED AND SERVICED. BOTH THE CSD AND GENERATOR WERE REPLACED. 2L72 4F4 FRTA16WE E2GL 20050324000872005032400087NM 2005 3 24 2005UALA00246 120050314A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE BULKHEAD DAMAGED A UALAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP29332UA 24193 UPPER FRAME LT SIDE STA 178 HAS LOW EDGE DISTANCE. FABRICATED AND INSTALLED A REPAIR CHORD SPLICE ANGLE, PICKING UP AN ADDITIONAL FASTENER LOCATION. 2L72 4F4 FRTA16WE E2GL 20050324000892005032400089WP 2005 3 24 ABXA050064 120050218A531159135955 FRAME DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23966AX 47510 CRACKED FRAME AT STA 1152, LONGERON 15 LEFT, FORWARD OF LEFT EPR TRANSMITTER. REPAIRED AREA IAW DC-9 SRM. 2L72 4F A6WE 20050324000902005032400090NM 2005 3 24 DHL2005781527 120050215A5311 FRAME BOEING727 727227 1384078NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A "C" CHECK, FRAME DENTED AT S25L BS950F. REMOVED FASTENER FOR ACCESS AT STA S25L BS950F IAW B727 SRM 51-30-2. CUT OUT DAMAGE AREA DIM 1.5 INCH BY 1 INCH IAW B727 SRM 51-40-3 FIG1. FABRICATED FRAME REPAIR MAT USED 7075T6 .071 PO NR 900573 DIM 9 3/4 INCH BY 4 .25 INCH IAW B727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1. ALODINED AND PRIMED PART IAW B727 SRM 51-10-2. INSTALLED FRAME REPAIR IAW B727 SRM 51-40-3 FIG 1. 2L73 4F A3WE 20050324000922005032400092NE 2005 3 24 022405N523CS1 220050224A7200 ENGINE CESSNA560 560XL 2076702CE PWA 545 PW545A NE RIGHT MALFUNCTIONED E Z5FABA EMER. DESCENT UNSCHED LANDING XP ENGINE FLAMEOUT NO WARNING INDICATION CRCRUISE 1 NE03523CS 5605507 DD0012 DURING CRUISE AT ALTITUDE 40,000 FEET, THE RIGHT ENGINE DID A UNCOMMANDED SHUTDOWN. THE CREW PUT THE AIRCRAFT INTO THE RESTART ENVELOPE AND ATTEMPTED TWO INFLIGHT RESTARTS. THE ENGINE WOULD NOT START SO AN EMERGENCY WAS DECLARED AND THE AIRCRAFT SAFELY LANDED IN CLEVELAND, OH (CLE). THE PROBLEM IS CURRENTLY BEING REVIEWED BY THE ENGINE AND AIRCRAFT OEM 2L72 4F4 FRTA22CE E00059EN 20050322000172005032200017EA 2005 3 22 ASOA05097 120050202A5260601R319805 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27827AS 7212 DURING A GROUND INSPECTION IN MHT, THE PASSENGER DOOR BOTTOM STEP ATTACH POINT FOR THE DEPLOYMENT ROD WAS FOUND BROKEN OFF FROM THE STEP. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050322000252005032200025EA 2005 3 22 ASOA05099 120050203A5260601R3198067 STEP CNDAIRCL600 CL6002C10 1390015EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27720EV 10115 DURING A C-CHECK IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20050322000272005032200027EA 2005 3 22 ASOA05107 120050206A5712 RIB CNDAIRCL600 CL6002B19 1900309EA WING CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27846AS 7328 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT BATTERY RIB ASSEMBLIES AT WS 53.60 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT BATTERY RIB ASSEMBLIES AT WLS 53.60 IAW ASA EO 600-57-039A. (M) 2L72 4F RTA21EA 20050322000372005032200037NM 2005 3 22 GAIA05007ST 120050228A5330 SKIN BOEING727 727224 1384076NM FUSELAGE DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW0769739 20667 DURING WALK AROUND, A DENT WAS FOUND ON THE FUSELAGE SKIN AT FS 343 STRINGER 24R. INSTALLED DOUBLER REPAIR IAW BOEING LETTER 1-17DF4Y AND KITTY HAWK EA B7-53-125. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20050322000432005032200043NE 2005 3 22 A6WA200540083 220050302A7200 SMOKE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 2 ENGINE DETECTED A GAIAK NONE B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL31429AW 7711 EXCESSIVE SMOKE OUT OF RT ENGINE ON SHUTDOWN ALL INDICATIONS WERE NORMAL. PERFORMED ENGINE RUN OF ENGINE NR 2 IAW CRJ AMM TASK 71-00-00-848-806. NO DEFECTS NOTED. AIRCRAFT SAFE FOR SERVICE. (M) 2L72 4F4 FRTA21EA E15NE 20050322000522005032200052WP 2005 3 22 2005F00036 120050115A2612 FIRE WARNING DOUG DC9 DC982 3022082WP AFT LAVATORY FALSE INDICATIONA GTIAO OTHER N FALSE WARNING CLCLIMB 1 GL23829NK 49931 PBI - FLT 165 - FIRE WARNING IN AFT LAVATORY DURING CLIMB-OUT, DETERMINED TO BE FALSE. ALL LAV SMOKE DETECTORS CHECK NORMAL, CHECKED APU COMPARTMENT FOR OIL LEAKS, NONE FOUND. CHECKED APU SUPPLY DUCTING FOR OIL CONTAMINATION, NONE FOUND. CHECKED NR 1 AND NR 2 8TH AND 13TH STAGE SADDLE DUCT END CAPS AND DUCTING FOR CONTAMINATION OF OIL, NON FOUND. APU OPS CHECK OK. (M) 2L72 4F A6WE 20050322000602005032200060SO 2005 3 22 SIMA200505604 120050222A5542 SKIN EMB 135 EMB135LR 3260305SO RUDDER GOUGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21703MR11871 145173 ABI - GOUGES IN RUDDER NR 1 LEADING EDGE SKIN. REMOVED DAMAGED AREA BY PERFORMING A CUTOUT. FABRICATED A FILLER AND DOUBLER. REPAIR DONE IAW EMB145 SRM, SRM 145/1142 REV 28, 51-40-02 AND EMB REPAIR STATEMENT IC2005-145/0912. (M) 2L72 4F RTT00011AT 20050322000652005032200065SO 2005 3 22 SIMA200506103 120050211A532014521725613 SILL EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21805AE 145489 SAW - DURING CPCP INSPECTION, FOUND RIGHT FORWARD SERVICE DOOR SILL CORRODED IN NUMEROUS AREAS. REMOVED AND REPLACED SILL ASSEMBLY AS PER SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050322000812005032200081NM 2005 3 22 SWAA050745 120050310A53116546525 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29607SW 27927 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050322000872005032200087NM 2005 3 22 SWAA050737 120050310A3233654491030 ACTUATOR BOEING737 7373Q8 1384670NM RT MLG MALFUNCTIONED A SWAAK NONE J WARNING INDICATION CLCLIMB 1 SW29687SW 23388 UNSAFE GEAR INDICATION UPON MLG RETRACTION. RECYCLED GEAR HANDLE. NORMAL RETRACT INDICATION. REMOVED AND REPLACED RT MLG ACTUATOR & UPLOCK ACTUATOR PER MM. 2L72 4F RTA16WE 20050322001002005032200100NM 2005 3 22 BB05011 120050223A335020131A BATTERY BOEING767 7672B7 1385107NM CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19656US 26847 MAD - SEAT 5A/B EMERGENCY LIGHT WAS INOPERATIVE, BUT DID RESET. MAINTENANCE REPLACED THE BATTERY. 2L72 4F RTA1NM 20050322001012005032200101NE 2005 3 22 EM05005 220050306A73204120T00P31 FADEC EMB ERJ170ERJ170100 EU GE CF34 CF348E5 30015NE NR 1 ENGINE MALFUNCTIONED A USAAK NONE J WARNING INDICATION NRNOT REPORTED 1 EA19802MD 17000013 GEE193130 FLIGHT 1818, DCA TO CLE - ENGINE ONE NO DISPATCH FAULT MESSAGE. MAINTENANCE TROUBLESHOT SYSTEM IAW GE, EMB FAULT CODES. REMOVED AND REPLACED FADEC AND FUEL METERING UNIT, FAULT REMAINED. 2L74 4F4 FRTA56NM E00063EN 20050323000032005032300003NM 2005 3 23 DL76L050167 120050315A2530 OVEN BOEING767 767332 1382001NM AFT GALLEY DIRTY A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO27197DN 28454 SLIGHT ELECTRICAL ODOR NOTICED IN AFT GALLEY WITH NO VISIBLE SMOKE. PULLED ALL GALLEY C/B INCLUDING AFT GALLEY LEFT AND RIGHT BREAKERS IN COCKPIT. ODOR DISSIPATED AND FLIGHT CONTINUE WITH NO FURTHER USE OF AFT GALLEY. ALSO ALL AFT GALLEY LIGHTS WERE TURNED OFF. CHECK ALL LIGHTS AND OVEN AND COFFEEMAKER FOR OPS AND ODOR, ALL OK. NOTIFY CABIN SVC TO CLEAN ALL OVEN AREA. RAN BOTH PACK AND GALLEY VENT FANS, ALL NORMAL. 2L72 4F RTA1NM 20050323000182005032300018SO 2005 3 23 C2XA05RI005 120050318A362081662410 THERMOSTAT EMB 145 EMB145XR 3260214SO NR 2 ENGINE INOPERATIVE A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW27111132713 798 145662 DURING CLIMBING, BLEED 2 OVERTEMP LIT UP, THEN BLEED 1 OVERTEMP LIT UP TOO. ICE COND MSG ON EICAS, A/I INOP (ANTI ICE)IN EICAS TOO. CREW PERFORMED AIR RETURN TO RIC. RIC MX PERFORMED TROUBLESHOOTING AND FOUND THERMOSTAT INOP. MX REMOVED AND REPLACED FAN AIR CONTROL THERMOSTAT AND PERFORMED OPERATIONAL CHECKS SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RT 20050323000232005032300023SO 2005 3 23 SWIA200514721 120050312A3397 WIRE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT DAMAGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07568SW 120343 FLOOR LEVEL E-LIGHTS AT ROWS 7A AND 8A ARE INOPERATIVE. REPAIRED SPLICE AT ROW 7A. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050323000262005032300026EA 2005 3 23 SWIA200514724 120050317A3220 LANDING GEAR CNDAIRCL600 CL6002B19 1900309EA NOSE ICED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07416SW 7089 WHEN RETRACTING LANDING GEAR, GOT RED MASTER WARNING, GEAR UP DISAGREE AND NOSE DOOR OPEN. FOUND NOSE GEAR COVERED IN ICE. THAWED NOSE GEAR AND SWUNG NOSE GEAR SEVERAL TIMES. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050323000322005032300032GL 2005 3 23 DXTA200500632 220050315A7200 ENGINE CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL RIGHT FAILED E DXTAE ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 GL07970QS 7500070 CAE330072 RT ENGINE FAIL IN FLIGHT DURING CRUISE AT FL340. RUN CHECKLIST ATTEMPTED RESTART, RESTART FAIL. FADEC FAIL RT A, FADEC FAULT RT A-B CAS MESSAGE. ITEM IS UNDER INVESTIGATION. 2L72 4J4 FRTT00007WITE6CH 20050323000452005032300045EA 2005 3 23 VNAA0503008 120050314A2810 CAP CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE FUEL CELL UNSAFETIED A VNAAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 GL05709PS 10165 EN ROUTE (CLT TO GSO) A FLIGHT ATTENDANT NOTICED A NOISE COMING FROM THE RIGHT SIDE OF THE AIRCRAFT AT THE WING AREA. THE CREW WAS NOTIFIED. THE CREW OF FLIGHT 2249 HAD NO INDICATION OF MALFUNCTIONS AND CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. THE CREW INSPECTED THE AIRCRAFT AND REPORTED THAT THE REFUEL PANEL WAS LEFT OPEN BY THE FUELER. THE FUEL CAP WAS NOT SECURED AND CAUSED DAMAGE TO THE AREA UNDER THE REFUEL ACCESS DOOR. CONTRACT MAINTENANCE INSPECTED AND PERFORMED A TEMPORARY REPAIR TO THE WING TO FUSELAGE FAIRING IAW BOMBARDIER REO 670-53-82-028. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050323000472005032300047 2005 3 23 SWAA050843 420050317A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29431WN 29845 R2 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20050323000552005032300055NM 2005 3 23 SWAA050832 120050317A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM AFT CARGO BAY CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29605SW 27956 DURING SCHEDULED D-CHECK, FOUND CORROSION ON 2 EA SHEAR TIES AT BS 767, RBL 2 & RBL 18. REMOVED AND REPLACED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20050323000652005032300065NM 2005 3 23 UPS05444129 120050312A5313 STRINGER BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE:C, BS 1278 STR 25R END FOUND CRACKED. CRACK LENGTH .75 INCH. M/DECK BS 2170-2180 STR 25R REPAIRED AS PER SRM 53-10-03 FIG 1. 2L74 4F A20WE 20050323000702005032300070NM 2005 3 23 SWAA050846 120050318A53306545775 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29503SW 24180 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STR 24L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050323000992005032300099 2005 3 23 SWAA050861 420050319A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR OUT OF LIMITS A SWAAK NONE O OTHER ININSP/MAINT 1 SW29403WN 29815 DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATING OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20050323001072005032300107 2005 3 23 MALA050285 420050321A3420H341ADM INDICATOR SAAB SF340 340B 7860101EU COCKPIT MALFUNCTIONED A MALAO OTHER O OTHER CLCLIMB 1 GL15457XJ 340B457 SHORTLY AFTER TAKEOFF FROM MSP THE GYRO FOR THE STANDBY HORIZON TUMBLED. REPLACED STANDBY HORIZON P/N ON/OFF H341ADM2. S/N ON 5329. S/N OFF 5117. 2L72 4T RTA52EU 20050323001102005032300110WP 2005 3 23 DHL2005805511 120050223A5711 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 LT OUTER WING INBOARD L/E UPPER FORMER CRACKED 0.500, XF 665.000. REMOVED FASTENERS IAW SRM 51-1-20D PG 21. PERFORMED STOP HOLE ON CRACK END AND FABRICATED ANGLE DOUBLERS (AL7075T6 0.032) (2EA) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLERS IAW SRM 51-1-8B. INSTALLED NEW ANGLE DOUBLERS (2EA) IAW SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. TORQUED IAW SRM 51-3-1 PG 2A. 2L74 4F RT4A25 20050323001332005032300133NM 2005 3 23 QXEA200500394 120050120A5320 FLOOR SUPPORT BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - CENTER FLOORBOARD NR 2 AND NR 3 STATION X32.00 MINOR CORROSION ON THE FLOOR CENTER SUPPORTS AND A-NUTS. REPAIRED IAW DHC-8 Q400 SRM SUB TASK 51-42-05-330-001, 51-21-00-350-001, 51-25-10-370-001, 51-21-10-380-001, 51-42-05-330-001, PARAGRAPH A TO D. 2H72 4T RTA13NM 20050323001372005032300137NM 2005 3 23 QXEA200500398 120050125A5753 FLAP TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 600 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - RIGHTHAND WING FLAP TRACK NR 5 CANOE FAIRING BRACKET CRACKED. REPAIRED IAW Q400 SRM 51-42-05-330-001. 2H72 4T RTA13NM 20050323001382005032300138NM 2005 3 23 QXEA200500399 120050125A5720 BRACKET BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - LEFTHAND WING FLAP TRACK NR 4 CANOE FAIRING BRACKET CRACKED. REPAIRED IAW Q400 SRM SUB TASK 51-42-05-330-001. 2H72 4T RTA13NM 20050323001422005032300142NM 2005 3 23 UPS05644142 120050319A2560 SMOKE GOGGLES BOEING767 76734AF 1385212NM COCKPIT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01325UP 27751 SMOKE GOGGLES IN CENTER JUMP SEAT HAS CRACKED LENS. REMOVED AND REPLACED SMOKE GOGGLES IN CENTER JUMP SEAT AS REQ'D REF AM 25-64-00. 2L72 4F RTA1NM 20050323001462005032300146NM 2005 3 23 CALA0500079 120050314A5320146N5318 SHEAR WEB BOEING757 757224 1384958NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714106 27296 INSPECTION FOUND SHEAR WEB CORRODED AT BS 1715, BL 0 IN G4 AREA. REPAIRED IAW SRM 53-60-51, FIGURE 203. 2L72 4F RTA2NM 20050323001472005032300147NM 2005 3 23 CALA0500080 120050308A5315143N501539 FLOORBEAM BOEING757 757224 1384958NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714106 27296 INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 720, RBL 3 TO LBL 3. REPAIRED IAW SRM 53-00-51, FIGURE 203. 2L72 4F RTA2NM 20050323001512005032300151EU 2005 3 23 MALA050278 120050316A5320 FLOOR SUPPORT SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15427XJ 340B427 CORROSION IN RT AISLE FLOORBOARD FLANGE AND RISER AT STA 294 EXTENDING AFT APPROX 10 INCHES. REMOVED CORROSION, OUT OF LIMITS. REMOVED DAMAGED SECTION AND INSTALLED NEW SECTION AND SPLICE REF MESABA EO S53060 REF 3. 2L72 4T RTA52EU 20050324000052005032400005WP 2005 3 24 05FDEA00612 120050321A5330 SKIN DOUG DC10 DC1010 3022110WP FUSELAGE BULGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25571FE 47830 DURING INSPECTION FOUND STA 348-366 X=0 WEB WITH REPAIR NOT CONFORM AND BULGE WITH CRACK. REMOVED WEB PER SRM 53-11-01, REPLACED WEB PER SRM 53-11-01, PERFORMED CUT PER DWG SP10530207-7001. (OPEN) 2L73 4F A22WE 20050324000062005032400006WP 2005 3 24 05FDEA00613 120050321A5522 SKIN DOUG DC10 DC1010 3022110WP ELEVATOR DENTED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25571FE 47830 DURING INSPECTION FOUND 1 DENT WITH NICK ON THE LEADING EDGE OF DETACHABLE ELEVATOR OF LEFT HORIZONTAL STABILIZER BETWEEN THE STA XE 88.625 AND THE STA XE 93.975 (UPPER SIDE). REMOVED LEADING EDGE PANEL BETWEEN STA 88.625 TO STA 100.455 IAW MM 20-50-07. REPAIRED IAW 55-00-01, REINSTALLED LEADING EDGE IAW 20-50-01. (OPEN) 2L73 4F A22WE 20050324000072005032400007NM 2005 3 24 05FDEA00579 120050316A5753 PAD BOEING727 727200 138407ENM NR 6 FLAP TRACK CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25480FE 21462 PITTING AND CORROSION ON AFT MOUNTING PAD ON RT WING FOR NR 6 FLAP TRACK. REMOVED CORROSION IAW SRM 51-10-6 PG 5 FIG 4, FOUND TO BE WITHIN LIMITS ORIGINAL DRWG SPECS IAW DWG 66-14734. TREATED & PRIMED IAW SRM 51-10-2, ORIGINAL MAT THICKNESS .600, REMOVED .002 REMAINING .598. 2L73 4F RTA3WE 20050324000242005032400024NM 2005 3 24 2005UALA00170 120050220A5320 FLOOR SUPPORT BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29581UA 26701 CABIN RT FLOOR SUPPORT INNER CHORD AT CUSP AREA IS CORRODED FROM STA 686 TO 740, RBL 60 TO RBL 64. 2L72 4F4 FRTA2NM E17NE 20050324000352005032400035EA 2005 3 24 QXEA200500261 120050211A5730 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 500 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - LT WING LOWER SKIN INBOARD HAS A SHARP NICK AT STATION 25. REPAIRED IAW CRJ 700 SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01 AND 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050324000402005032400040NM 2005 3 24 WRLA2005026 120050217A5512 SKIN DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST LT BARREL NUT HOLE NR 06. 2L73 4F4 FRTA22WE E24NE 20050324000482005032400048NM 2005 3 24 WRLA2005072 120050223A5512 SKIN DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST RT BARREL NUT HOLE NR 15. 2L73 4F4 FRTA22WE E24NE 20050324000502005032400050NM 2005 3 24 WRLA2005074 120050223A5512 SKIN DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST LT BARREL NUT HOLE NR 27. 2L73 4F4 FRTA22WE E24NE 20050324000522005032400052NM 2005 3 24 QXEA200400293 120050224A2750 WARNING LIGHT BOMBDRDHC8 DHC8401 1390041NM TE FLAPS ILLUMINATED A QXEAO OTHER J WARNING INDICATION APAPPROACH 1 NM09414QX7889 4061 LAX - FLIGHT 2343 - THE CHECKLIST WAS COMPLIED WITH WHEN ON APPROACH THE FLAP POWER CAUTION LIGHT ILLUMINATED. MAINTENANCE INSPECTED THE AIRCRAFT AND ACCOMPLISHED THE FLAP POWER NUISANCE CAUTION LIGHT RESET PROCEDURE. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050324000572005032400057NM 2005 3 24 AWXA200500258 120050225A2560P4010021 BATTERY BOEING737 7373G7 1384595NM ZONE 900 DISCHARGED A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28158AW 23780 PHX - EMERGENCY EQUIPMENT, FLIGHT CREW REPORTED THE EMERGENCY FLASHLIGHT OVER THE FORWARD FLIGHT ATTENDANT JUMPSEAT IS NOT INDICATING A CHARGE LIGHT. MAINTENANCE REMOVED AND REPLACED FORWARD EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050324000582005032400058NM 2005 3 24 AWXA200500259 120050226A3397BMS13311122 WIRE BOEING757 7572S7 1384962NM SEAT ROW 23 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28904AW 23566 PHX - EEL - DURING A-01 CHECK, FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 23 LT INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 23 LT. OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20050324000612005032400061NM 2005 3 24 AWXA200500262 120050124A53206545834527 INTERCOSTAL BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 MCN - MAJOR REPAIR - DURING C-18 CHECK, A 0.8125 INCH CRACK WAS FOUND IN UPPER AFT CORNER OF INTERCOSTAL AT BS 293, LBL 33, WL 208. MAINTENANCE CUTOUT DAMAGE IN INTERCOSTAL AT BS 293, LBL 33; FABRICATED A REPAIR ANGLE AND SHIM; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-11. 2L72 4F RTA16WE 20050324000722005032400072SO 2005 3 24 1408020905 120050209A325051051 MANIFOLD GULSTMG1159 GIV 3980115SO NLG STEERING MALFUNCTIONED E N93AO OTHER O OTHER TXTAXI/GRND HDL 1 SO13401QS4321 1408 NOSE STEERING PULLING TO LEFT. 2L72 4F RTA12EA 20050324000772005032400077EA 2005 3 24 X6PA200500002 220050216A731025245908 SERVO PIPER PA34 PA34200 7103405SO LYC O360 IO360C1E6 41514EA FUEL INJECTION LEAKING E X6PAK NONE KJ FLUID LOSS WARNING INDICATION ININSP/MAINT 1 SO33997BW 1760 347450064 L1191351A DURING A 100 HR INSPECTION, FUEL WAS FOUND DRIPPING FROM MIXTURE CONTROL ARM SHAFT. FUEL INJECTION SERVO REMOVED AND REPLACED. 1L72 3O3 O A7SO 1E10 20050324000882005032400088NM 2005 3 24 2005UALA00119 120050204A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29578UA 26694 FWD CABIN FLOORBEAM HAS CORROSION AROUND FASTENERS AT STA 324, RBL 51 TO RBL 52, BEAM UPPER CAP. DAMAGE DUE TO CORROSION. MAJOR REPAIR ACCOMPLISHED. DAMAGE WAS BLENDED. ANGLE REPAIR WAS INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050324000932005032400093CE 2005 3 24 ENHA2005A9001 120050114A3220 LANDING GEAR BEECH 90 65A901 1152901CE NOSE FAILED E ENHAO OTHER O OTHER LDLANDING 1 AL0370841 LM73 AIRCRAFT ENCOUNTERED LARGE SNOW BERM ON LANDING AT THE EMMONAK, ALASKA AIRPORT. AIRCRAFT EXPERIENCED NLG FAILURE AND VEERED TO RUNWAY LT SIDE COMING TO REST NOSE DOWN IN SNOW BANK. PILOT REPORTED APPROACH NORMAL WITH LIGHTED RUNWAY AND WAS UNABLE TO SEE AND AVOID SNOW DRIFTING ON THE RUNWAY. AIRCRAFT INCURRED SUBSTANTIAL DAMAGE TO THE NOSE WHEEL WELL STRUCTURE, PROPELLERS AND ENGINES. 1L72 3T 3A20 20050324000962005032400096WP 2005 3 24 ABXA050060 120050216A534039248101AX FITTING DOUG DC9 DC941 302207NWP FWD CARGO CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23966AX 47510 LONGERON 26 RIGHT CRACKED AT STA 636 THROUGH KIDNEY PANEL. REPLACED LONGERON FITTING IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 20050324000972005032400097WP 2005 3 24 ABXA050065 120050228A57403923259501 SUPPORT FITTING DOUG DC9 DC941 302207NWP WING CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23969AX 47464 RIGHT OUTBOARD TORSION BAR OUTBOARD SUPPORT FITTING CRACKED AT UPPER FORWARD FASTENER. REPLACED FITTING IAW DC-9 SRM 51-30-5 AND 51-30-2. 2L72 4F A6WE 20050324000982005032400098WP 2005 3 24 ABXA050067 120050304A53105910682507 STRUCTURE DOUG DC9 DC941 302207NWP SUBFLOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23969AX 47464 CRACK IN SUBFLOOR STA 160 RBL 6. REPAIRED AREA IAW DC-9 SRM 53-01. 2L72 4F A6WE 20050324000992005032400099NM 2005 3 24 DHL2005781525 120050211A5754 SKIN BOEING727 727227 1384078NM NR 1 SLAT DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A "C" CHECK, NR 1 SLAT L/E EXTERIOR SKIN DENTED AND SCRATCHED AT WSTA 760 (MARKED). CUT OUT DAMAGED AREA APROX 1 INCH BY 2 1/4 INCH AT NR 1 SLAT LE EXT SKIN W STA 760 IAW B727 SRM 57-50-3. FAB DOUBLER REPAIR WITH 2024T3 .080 SIZE 5 1/4 INCH BY 4.5 INCH PO 9001811 IAW B727 SRM 57-50-3 FIG 1 & 57-50-2. TREATED AND PRIMED DOUBLER REPAIR IAW B727 SRM 51-10-2. INSTALLED DOUBLER IAW B727 SRM 57-50-3 FIG1. 2L73 4F A3WE 20050324001002005032400100EU 2005 3 24 05FDEA00436 120050308A5730 PANEL AIRBUS310 A310 EU RT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 RT WING PANEL 650HB HAS 3 EA ELONGATED HOLES REF N00523. REPAIRED PANEL 650HB IAW EA 6-5710-86051. 2L72 4F RTA35EU 20050324001012005032400101EU 2005 3 24 05FDEA00437 120050308A5730 PANEL AIRBUS310 A310 EU LT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 LT WING PANEL 550HB HAS 2 EA ELONGATED HOLES REF N00520. REPAIRED HOLES IAW EA 6-5710-85051. 2L72 4F RTA35EU 20050324001022005032400102EU 2005 3 24 05FDEA00438 120050308A5730 PANEL AIRBUS310 A310 EU RT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 RT WING PANEL 650KB HAS 4 EA ELONGATED HOLES REF N00521. REPAIRED PANEL IAW EA 6-5710-86051. 2L72 4F RTA35EU 20050324001032005032400103EU 2005 3 24 05FDEA00440 120050308A5522 DOUBLER AIRBUS310 A310 EU ELEVATOR DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 REPAIR ON RT ELEVATOR I/B T/E LOWER SURFACE REQUIRES EVALUATION REF N00817. REMOVED EXISTING REPAIR AND INSTALLED CORRECT REPAIR IAW SRM 55-21-11 CONF 1 FIG 203 AND EA 6-5510-86111. 2L72 4F RTA35EU 20050324001042005032400104 2005 3 24 05FDEA00333 420050302A34164005123901 ALTIMETER DOUG DC10 DC1010 3022110WP COCKPIT READS LOW A FDEAO OTHER N FALSE WARNING CRCRUISE 1 SO25395FE18147659 46629 F/O ALTIMETER FAILED IN FLIGHT. READS 450FT LOW AND FLUCTUATES /- 30 FT AT FL280. NOT RVSM CAPABLE. REPLACED F/O'S ALTIMETER PER 34-12-01-2 1. OPS CK NORMAL. 2L73 4F A22WE 20050324001052005032400105NM 2005 3 24 05FDEA00334 120050302A5313 STRINGER BOEING727 727227 1384078NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 CORROSION IN STRINGER 26R, AFT OF BS 1148, AFT CARGO BAY. 2L73 4F A3WE 20050324001092005032400109NM 2005 3 24 ASMF200502005 120050205A2741160202100 CONTROL MODULE BOEING757 7572Q8 1384972NM STAB TRIM FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23803AM3602836028 26268 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF AFTER ENGINES STARTED, EICAS MESSAGES STAB TRIM" WAS SHOWN. REPORT WAS DEFERRED IAW MEL 27-41-2. DURING TRANSIT CHECK AT MEX, LEFT STAB TRIM CONTROL MODULE WAS REPLACED IAW MM 27-41-05, TESTED CORRECT, DEFERRED REPORT WAS CLOSED. 2L72 4F RTA2NM 20050324001112005032400111EA 2005 3 24 QXEA200500192 120050123A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - RIGHT INBOARD SEAT RAIL, AT STATION X477, HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW CRJ700 SRM 51-21-0-001-001-A01, REO 670-53-00-060, REV B AND HORIZON AIR EA R-53-266. 2L72 4F RTA21EA 20050324001122005032400112EA 2005 3 24 QXEA200500196 120050124A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - RIGHT INBOARD SEAT RAIL AT STATION X510 HAS PITTING CORROSION ON INSIDE SURFACE. REPAIRED IAW CRJ700 SRM 51-21-00-001-001-A01, REO 670-53-00-060, REV B. AND HORIZON AIR EA R-53-266. 2L72 4F RTA21EA 20050324001152005032400115EA 2005 3 24 QXEA200500268 120050212A5330 SKIN PANEL CNDAIRCL600 CL6002C10 1390015EA ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - FUSELAGE EXTERIOR, AFT LOWER STATION 981, BLO, SKIN PANEL HAS TWO GOUGES. REPAIRED IAW CRJ700 SRM 51-42-21-001-001-A01, 51-12-00-001-001-A01, REO 670-53-61-147 AND HORIZON AIR EA R-53-270. 2L72 4F RTA21EA 20050324001182005032400118 2005 3 24 200501312 420050124A3417962830A1S8 ADC CESSNA208 208B 2073701CE COCKPIT MALFUNCTIONED B HJBRO OTHER O OTHER NRNOT REPORTED 1 AL05332AK 208B0779 PILOT REPORTS 6000 FT, ALTITUDE REPORTING ERROR AT SEA LEVEL. AIR DATA COMPUTER INSTALLED AS PART OF THE CHELTON FLIGHT SYSTEM EFIS-SV SYSTEM UNDER STC NR SA02203AK. 1H71 3T A37CE 20050324001192005032400119NM 2005 3 24 DHL2005781526 120050215A5311 FRAME BOEING727 727227 1384078NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A "C" CHECK AT FLIGHTSTAR AIRCRAFT SERVICES IN JACKSONVILLE FLORIDA, THE FOLLOWING DISCREPANCY WAS NOTED; FRAME DENTED ABOVE S25R BS1050. REMOVED FASTENERS FOR ACCESS AT S25R BS 1050 IAW B727 SRM 51-30-2. CUT OUT DAMAGED AREA DIM 1 1/2 BY 1 INCH IAW B727 SRM 51-40-3 FIG 1. FABRICATE FRAME REPAIR MAT USED 7075-T6.071 PO NR 900573 DIM 10 1/2 INCH BY 4 1/2 INCH IAW B727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1. ALODINED AND PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED FRAME REPAIR IAW B727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG1. 2L73 4F A3WE 20050324001202005032400120EU 2005 3 24 F3LA200500005 120050217A2120 SMOKE AIRBUSA319 A319112 3930323EU CABIN DETECTED A F3LAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM03903FR 1560 ON INBOUND TAXI, FLIGHT CREW REPORTED SMOKE IN CABIN. RAN ENGINES PER AMM 71-00-00-710-006. CYCLED AIR CONDITIONING PACKS. RAN APU. CYCLED APU BLEED AIR. INSPECTED CARGO BINS, E/E BAYS AND CABIN FOR SMOKE. NO FAULTS NOTED, COULD NOT DUPLICATE DISCREPANCY. 2L72 4F RTA28NM 20050324001222005032400122 2005 3 24 HNAA0500013 420050220A3420 AHRS DHAV DHC8 DHC8102 2809003NM NR 1 FAILED A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07826EX 389 NR 1 AHRS FAILURE AFTER T/O RETURN TO FIELD POWER DOWN POWER UP BOTH AHRS, OPS TEST GOOD. 2H72 4T RTA13NM 20050324001232005032400123NE 2005 3 24 ASMF200502010 220050214A7200 ENGINE BOEING757 757200 1384950NM PWA 2037 PW2037 NE RIGHT LACK OF LUBE W ASMFDE RETURN TO BLOCK ENGINE SHUTDOWN J WARNING INDICATION TXTAXI/GRND HDL 1 SW23703AM 27203 726729 DURING ENGINES STARTING, RT ENGINE DID NOT STABILIZED AND WAS SHUTDOWN. OIL QTY CHECKED & REFILLED TO THE CORRECT LEVEL. RT ENGINE RESTARTED & ACFT DISPATCHED BUT IT RETURNED TO PLATFORM DUE TO DURING TAXING OIL TEMP INDICATION 177 DEGREES. ACFT SENT TO HANGAR & IT WAS INSPECTED FOR LEAKS. FIM 79-34-00 PROCEDURE WAS PERFORMED DETECTING OIL OVERFILLED OF 10 QTS, THE EXCEEDING OIL WAS DRAINED. THE OIL PRESS 11 TEST WAS PERFORMED, BEING IN GRAPHICS IAW MM 71-00-00. DURING OVERNIGHT SERVICE OIL FILTER WAS REPLACED IAW MM 79-21-16, THE CHIP DETECTORS WERE CHECKED IAW MM 79-21-10, ALL CORRECT. THE 8 AND 11 TEST FIM FOR HIGH TEMPERATURE AND OIL PRESS WERE PERFORMED IAW MM, TESTED CORRECT. 2L72 4F4 FRTA2NM E17NE 20050324001242005032400124EA 2005 3 24 JBGA200500001 120050221A56106003303025 WINDSCREEN CNDAIRCL600 CL6002B16 1900305EA COCKPIT CRACKED E JBGAO OTHER O OTHER CRCRUISE 1 GL07420ST2078 5027 PILOT FORWARD FACING WINDSHIELD OUTER PLY CRACKED. PILOT DIVERT TO ICT 2L72 4F RTA21EA 20050324001252005032400125SO 2005 3 24 C2XA05TY025 120050228A3350110049 ATTACH FITTING EMB 145 EMB145XR 3260214SO EMERGENCY BATTERDAMAGED A C2XAK NONE J WARNING INDICATION ININSP/MAINT 1 SW2713123 145688 TYS FLIGHT 3459 FROM AVL EMERGENCY LIGHTS ON WITH THE SWITCH IN OFF POSITION. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY TRAY AND OPS CHECK WAS GOOD. AIRCRAFT APPROVED FOR SERVICE. LOGGED IN LOG BOOK PAGE 1041870. 2L72 4F RT 20050324001282005032400128NM 2005 3 24 WRLA2005024 120050218A2160 CONTROLLER DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE CABIN TEMP MALFUNCTIONED A WRLAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 SO11273 48519 ITEM: WOA0974/18 JIB/KWI LEVEL 340, ABOUT 40 MIN AFTER T/O FAINT BLUE SMOKE WAS DETECTED IN THE COCKPIT. NO AIR SYSTEM ALERTS WERE ANNUNCIATED, NR 1 PACK COCKPIT INFLOW TEMPERATURE WAS 95 DEG WHILE THE TEMPERATURE SELECTOR WAS COMMANDING A COOL DOWN IN THE COCKPIT. SWITCHED AIR SYSTEM TO MANUAL AND COCKPIT INFLOW TEMPERATURE RETURNED TO NORMAL. NO ADDITIONAL ACTION WAS REQUIRED, THE SMOKE QUICKLY DISSIPATED. THE FLIGHT WAS CONTINUED TO DESTINATION WITHOUT INCIDENT. ITEM IN DMI M21FE1805-99 NR 1 PACK INOP PER MEL 21-51-01 CAT "C". 2L73 4F4 FRTA22WE E24NE 20050324001292005032400129WP 2005 3 24 05FDEA00328 120050302A5410ASL0046 LONGERON DOUG MD10 MD1010F 3022112WP ZONE 400 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25361FE 48260 NUMBER 3 ENGINE INBOARD CORE CORE COWL UPPER SEAL IS CHAFFED. FOUND CORE COWL LONGERON CHAFED WHILE REMOVING CHAFE STRIP. REPAIRED LONGERON IAW FEDEX EA 8- 5410-83991, NACELLES/PYLON- NUMBER 3 ENGINE INBOARD CORE COWL UPPER LONGERON. REPAIR, REMOVED AND REPLACED CHAFE STRIP IAW DC10-10 SRM 51-21-01 VOL II. REFERENCE NON-ROUTINE N00436. 2L73 4F RTA22WE 20050324001302005032400130SO 2005 3 24 C2XA05TY021 120050225A335020131A BATTERY PACK EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT WEAK A C2XAK NONE O OTHER ININSP/MAINT 1 SW27231397452 3786 145731 TYS - AIRCRAFT WAS IN FOR A 4C INSPECTION AND DURING THE SERVICE ROUTINE, THE NR 1 EMERGENCY LIGHT BATTERY WAS FOUND NOT CHARGED. MAINTENANCE REPLACED THE EMERGENCY BATTERY AND THE OPS CHECK WAS GOOD. A/C WILL BE REL. UPON COMPLETION OF ALL WORK. 2L72 4F RT 20050324001362005032400136EA 2005 3 24 QXEA200500229 120050215A2120 FILTER CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DIRTY A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM09604QX7814 10019 BOI - DURING DESCENT AND UNTIL SHUTDOWN, THE CREW REPORTED A STRONG SMELL COMING FROM THE ACM'S. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE LEFT AND RIGHT RECIRCULATION FAN FILTERS. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20050324001372005032400137NM 2005 3 24 QXEA200500230 120050217A521085217051101 ARM BOMBDRDHC8 DHC8401 1390041NM CABIN DOOR CRACKED A QXEAO OTHER O OTHER TXTAXI/GRND HDL 1 NM09403QX9236 4037 SEA - FLIGHT 2387 - THE MAIN CABIN DOOR IS DIFFICULT TO OPEN. MAINTENANCE INSPECTED THE DOOR AND REPLACED THE FORWARD DOOR SUPPORT. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050324001382005032400138NM 2005 3 24 QXEA200500231 120050217A5270 CONNECTOR BOMBDRDHC8 DHC8401 1390041NM LANDING GEAR LOOSE A QXEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM09414QX7834 4061 PDX - FLIGHT 2307 - THE FLIGHT RETURNED TO FIELD AFTER THE CREW RECEIVED AN ANTI-SKID MESSAGE DURING THE CLIMB. MAINTENANCE INSPECTED THE AIRCRAFT AND CLEANED AND RESECURED A LOOSE CONNECTOR FOUND ON THE RIGHT MAIN LANDING GEAR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050324001392005032400139NM 2005 3 24 QXEA200500233 120050220A33506519020 LIGHT DHAV DHC8 DHC8202 2809007NM ZONE 200 INOPERATIVE A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09357PH 504 SEA - EMERGENCY FLOOR LIGHTING ROW 1 D/E INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LIGHTING STRIP AT ROW 1 AND 2 D/E. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050324001402005032400140CE 2005 3 24 20030785 120050126A5511 SPAR BEECH 1900 1900D 1154162CE HORIZONTAL STAB CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03154GL UE154 DURING ROUTINE STRUCTURAL "I" INSPECTION, FOUR CRACKS WERE IDENTIFIED EMANATING FROM THE DE-ICE HOLE ON THE HORIZONTAL CENTER MAIN SPAR CENTER WEB SKIN APPROX 1" LONG EACH UNDER PANEL 332 ATC. REPAIR WAS MADE AND AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA24CE 20050324001412005032400141EU 2005 3 24 05FDEA00461 120050309A5280 UPLOCK HOOK AIRBUS310 A310 EU MLG DAMAGED A FDEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO25455FE 331 NOSE LANDING GEAR DOOR AMBER LIGHT ILLUMINATE ON BOTH PANELS FOLLOWED ECAM. QRH DECLARED EMERGENCY FOR OVERWEIGHT LANDING. LANDING WEIGHT 289.0 AND 250 FPM RATE OF DESCENT. NOTICEABLE VIBRATION FROM NOSE GEAR DOOR. FURTHER T/S FOUND RT UPLOCK ASSY-NLG DOOR HOOK ALWAYS SPRING BACK. REMOVED AND REPLACED RT NLG DOOR UPLOCK ASSY. 2L72 4F RTA35EU 20050324001422005032400142EU 2005 3 24 05FDEA00462 120050309A2133 OUTFLOW VALVE AIRBUS310 A310 EU CABIN PRESSURE FLUCTUATES A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25447FE 251 A/C WOULD NOT PRESSURIZE ON CLIMB-OUT OF MEM. LEVELED OFF AT 9000. CABIN VSI CLIMBING AT SAME RATE AS A/C CLIMB. NR 2 FWD AND AFT VALVES DISPLAYED FULL OPEN AND AMBER IN COLOR. NR 1 FWD AND AFT OUTFLOW VALVES OSCILLATED VIOLENTLEY OPEN AND CLOSED THROUGH FLT. RETURNED AND LANDED IN MEMPHIS. NO ECAM FAULTS DISPLAYED THROUGH OUT WITH REGARD TO REG NR 1 OR NR 2. FOUND UNION WHERE AFT NR 2 JET PUMP HALVES CONNECT VERY LOOSE. TIGHTENED CONNECTION, ALSO REMOVED JET PUMP IAW A310 MM 21-31-00-5-01. PUMP WAS CLEAN OF ANY DIRT OR OTHER OBSTRUCTIONS. REINSTALLED IAW SAME REF. REMOVED REPLACED RELAYS 60GB (RLY-MLG) AND 45GB(RLY-MLG). PERFORMED ADJ/TEST IAW A310 MM 21-31-00-5-01. ALL TESTS PASSED. 2L72 4F RTA35EU 20050324001442005032400144SO 2005 3 24 MASA200500116 120050215A532014524131009 SUPPORT ANGLE EMB 145 EMB145LR 3260212SO PAX THRESHOLD CORRODED A MASAK NONE O OTHER ININSP/MAINT 1 SW07851MJ7186 145572 IN C-CHECK, PAX DOOR ENTRANCE U-BEAM SUPPORT ANGLES ARE CORRODED AND WILL BE REPLACED IAW SRM 51-40-02. 2L72 4T RTT00011AT 20050324001452005032400145SO 2005 3 24 MASA200500118 120050215A532014522461011 STRAP EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A MASAK NONE O OTHER ININSP/MAINT 1 SW07851MJ7186 145572 IN C-CHECK, PLATE P/N 145-22461 IS CORRODED AND IS BEING REPLACED IAW SRM 51-40-02. 2L72 4T RTT00011AT 20050324001462005032400146SO 2005 3 24 MASA200500119 120050215A572014566156403 BRACKET EMB 145 EMB145LR 3260212SO LT WING TIP CRACKED A MASAK NONE O OTHER ININSP/MAINT 1 SW07851MJ7186 145572 IN C-CHECK, LT FLUX DETECTOR BRACKET IS CRACKED AND IS BEING REPAIRED IAW SRM 57-20-07. 2L72 4T RTT00011AT 20050324001472005032400147SO 2005 3 24 MASA200500120 120050215A572014566156404 BRACKET EMB 145 EMB145LR 3260212SO RT WING TIP CRACKED A MASAK NONE O OTHER ININSP/MAINT 1 SW07851MJ7186 145572 IN C-CHECK, RT FLUX DETECTOR BRACKET IS CRACKED AND IS BEING REPAIRED IAW SRM 57-20-07. 2L72 4T RTT00011AT 20050324001482005032400148SO 2005 3 24 C2XA05CL008 120050213A335078241 INVERTER EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716571 145633 DURING ROUTINE MAINTENANCE, THE EMERGENCY LIGHT FLOOR STRIPS NR 6, 7, AND 8 WERE INOP. MAINTENANCE REPLACED THE NR 6 EMERGENCY LIGHT INVERTER. ALL OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20050324001492005032400149 2005 3 24 PNSA050202 420050223A6122 GOVERNOR SAAB SF340 340B 7860101EU PROPELLER MALFUNCTIONED A PNSAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 AL03677PA 328 DURING TAKEOFF ROLL AUTOCOARSEN HIGH LIGHT DID NOT ILLUMINATE WITH POWER LEVER ADVANCE. TAKEOFF ABORTED. TAXIED CLEAR AND PERFORMED AUTOCOARSEN GROUND TEST WITH NO FAULT. TAXIED BACK TO RUNWAY AND PERFORMED NORMAL TAKEOFF, NO ADDITIONAL FAULTS ON LATER FLIGHTS. 2L72 4T RTA52EU 20050324001512005032400151EA 2005 3 24 QXEA200500195 120050124A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - RIGHT INBOARD SEAT RAIL AT STATION X492 HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW CRJ700 SRM 51-21-00-001-001-A01, REO 670-53-00-060, ERV B. AND HORIZON AIR EA R-53-266. 2L72 4F RTA21EA 20050324001522005032400152EA 2005 3 24 QXEA200500197 120050124A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - RIGHT INBOARD SEAT RAIL AT STATION 524 HAS PITTING CORROSION ON INSIDE SURFACE. REPAIRED IAW CRJ700 SRM 51-21-00-001-001-A01, REO 670-53-00-060, REV B. AND HORIZON AIR EA R-53-266. 2L72 4F RTA21EA 20050324001572005032400157NM 2005 3 24 QXEA200500216 120050215A3411 PITOT HEAD DHAV DHC8 DHC8202 2809007NM NR 1 INOPERATIVE A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09368PH 512 SEA - ON FLIGHT 2089, PITOT HEAT 1 CAUTION LIGHT ILLUMINATED IN ICING CONDITIONS. COMPLIED WITH CHECKLIST. MAINTENANCE REMOVED AND REPLACED NR 1 PITOT HEAD. PERFORMED LEAK TEST OF NR 1 PITOT SYSTEM. LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050324001582005032400158SO 2005 3 24 C2XA05IA026 120050211A3350110049 CHARGER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714543 145553 MCI - DURING MAINTENANCE INSPECTION, THE AFT OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT BATTERY CHARGER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050324001592005032400159NM 2005 3 24 DHL2005781550 120050216A5531 FRAME BOEING727 727227 1384078NM VERTICAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A "C" CHECK, FOLLOWING DISCREPANCIES WERE NOTED;VERT STAB FIN STA 180 STR 6R IS CRACKED AT FRAME ATTACH BOLT. REMOVED PANEL NR 9504 FOR ACCESS TPM FOR SHEET METAL REPAIR IAW B727 SRM 51-30-2. REMOVED FASTENERS FOR ACCESS, CUT OUT DAMAGED STIFFENER AND REMOVED FILLER IAW B727 SRM 51-30-4 FIG 1 ( 5 INCH BY 3 INCH). FABRICATED REPAIR STIFFENER P/N BAC 1517-1367 7075-T6, PO 501953 DIM 5 INCH BY 3 INCH, SPLICE P/N AND1034-1201, 075-T6 PO 501952 DIM.19" X 2 1/4" FILLER P/N 7075-T6 .180 P.O. 9201777 DIM.19" X 1/2" ,SPLICE P/N AND 10133-1401,7075-T6 DIM.19"X 2" P.O.501952, FILLER P/N 7075-T6 .090 DIM. 19"X 2" P.O.501952 DIM.2"X 2" IAW B727 SRM 55-30-4 FIG 1. TREATED AND PRIMED STIFFENER, SPLICES AND FILLERS 2L73 4F A3WE 20050324001602005032400160CE 2005 3 24 20030782 120050115A712012991004713 TRUSS BEECH 1900 1900D 1154162CE LT ENGINE CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03253GL178492001 UE253 WHILE PERFORMING OTHER NON-RELATED MAINTENANCE, THE LT ENGINE TRUSS WAS DISCOVERED TO BE COMPLETELY CRACKED THRU (360 DEGREES) ON THE LOWER LT TUBE JUST ABOVE THE ATTACH BRACKET FOR THE LOWER ENGINE AIR CAN ASSY, ADJACENT TO THE P3 BLEED LINE. NO OBVIOUS CHAFFING DAMAGE WAS NOTED, AND APPEARS TO HAVE BEEN CORRODED FROM INSIDE. ALSO, A SMALL HOLE WAS NOTED ON SAME TUBE AT TUBE WELD JUNCTION AT MAIN ATTACH POINT. TRUSS REMOVED FOR FURTHER EVALUATION BY MANUFACTURER. NEW TRUSS INSTALLED, AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA24CE 20050324001622005032400162EU 2005 3 24 249312 120050318A3260 WARNING LIGHT SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R389 R3894123F25 NE NLG ILLUMINATED A UHLAO OTHER N FALSE WARNING CLCLIMB 1 GL17158SD 158 463 DRG178787 ON 03-18-2005, APPROX 1700 (UTC), FLT 7886 SCE-IAD, AIRCRAFT N158SD DEPARTED SCE. AT ROTATION SPEED CREW HAD OBSERVED A NOSE GEAR SHOWED UNSAFE. 2L72 4T4 TRTA52EU E8NE6 6 CP30NE 20050324001662005032400166NM 2005 3 24 ASMF200503011 120050313A5330 SKIN DOUG MD80 MD83 3023681NM PAX DOOR DENTED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23861LF 49826 DURING TRANSIT CHECK SCRATCH AND DENT WERE FOUND IN THE BOTTOM OF THE MAIN DOOR BETWEEN STA Y-231, LONGERON 17 AND 18. THE SCRATCH AND DENT WERE REWORKED AND ULTRASONIC INSPECTION WAS PERFORMED IAW SRM 53-04, FIG 38, TABLE A, CONDITION 1, ALL CORRECT. 2L72 4F RT 20050324001672005032400167NM 2005 3 24 HNAA0500005 120050129A531185321156 FRAME DHAV DHC8 DHC8102 2809003NM FUSELAGE CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07936HA 145 DURING C CHECK, FOUND WIDE SPREED CORROSION THAT REQUIRED STR 31 REMOVAL AND REPLACEMENT. FRAME X253 REQUIRES A FRAME SPLICE WHICH IS A MAJOR REPAIR TO ALLOW INSTALLATION OF REPLACEMENT STRINGER. FRAME SPLICE WAS DONE IAW PIEDMONT EO 8-53-05-0024. 2H72 4T RTA13NM 20050324001682005032400168NE 2005 3 24 250TR0060 220050228A7397 WIRE BOEING737 7372K5 138448XNM PWA JT8 JT8D15A 52051NE LT ENGINE DAMAGED A PIDAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION TXTAXI/GRND HDL 1 SO05250TR 22597 702726 IN PREPARATION TO TAXI, LEFT ENGINE UNCOMMANDED SHUT DOWN AFTER START. FOUND BROKEN WIRES W368-011 AND 010 UNDER CLAMP SIX INCHES BEFORE FUEL SHUTOFF VALVE CONNECTOR 0788. PRECAUTIONARY, CHECKED RIGHT ENGINE AND DISCOVERED WIRES DAMAGED IN SAME LOCATION. REPAIRED LEFT AND RIGHT ENGINE WIRING PER SPM 24-20 AND WDM 28-21-01. INSPECTED FIVE OTHER 737-200 AIRCRAFT IN FLEET. NO OTHER DISCREPANCIES NOTED. 2L72 4F4 FRTA16WE E2EA 20050324001722005032400172EA 2005 3 24 SWIA200514643 120050223A2741 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA RUDDER TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CLCLIMB 1 NM07938SW 7741 ON CLIMB, RIGHT RUDDER TRIM WAS USED MOMENTARILY, FOLLOWED BY UNCOMMANDED FULL RIGHT RUDDER TRIM ACTIVATION, AIRCRAFT WAS RETURNED TO TRIMMED CONDITION EASILY OPPOSITE RUDDER AND CORRECTED ALL TOGETHER WITH TRIM SWITCH. NORMAL FOR REMAINDER OF FLIGHT. REPLACED AILERON/RUDDER TRIM PANEL IN REFERENCE TO CRJ 200 MM ATA CHPT 27-00-00. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050324001742005032400174SO 2005 3 24 SWIA200514644 120050224A275012064207615 SELECTOR EMB 120 EMB120ER 3260203SO TE FLAP MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07566SW6460 6460 120341 FLAPS DO NOT COME DOWN. REMOVED AND REPLACED FLAP SELECTOR LEVER ASSY WITH SERVICEABLE UNIT REF NR 27-50-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050324001752005032400175NM 2005 3 24 RYNA200500004 120050123A2520 FAN BOEING757 757200 1384950NM GALLEY OVEN WORN A RYNAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE07GJMCE 30758 DURING CRUISE FLIGHT FROM ORD, THE AFT GALLEY NR 2 OVEN FAN FAILED CAUSING SMOKE IN THE AFT GALLEY AREA. THE CREW REPORTED A LEFT UTILILITY BUSS FAULT. AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED OVEN. 2L72 4F RTA2NM 20050324001762005032400176EA 2005 3 24 SWIA200514498 120050122A5312 PRESSURE PANEL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DENTED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07954SW 7815 FSG21 PRESSURE WEB & VERTICAL STIFFENER LBL 18 WL 94.25 DENTED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-61-1273. 2L72 4F RTA21EA 20050324001782005032400178EA 2005 3 24 SWIA200514737 120050322A2741 SWITCH CNDAIRCL600 CL6002B19 1900309EA TRIM DISCONNECT MALFUNCTIONED A SWIAD RETURN TO BLOCK F FLT CONT AFFECTED NRNOT REPORTED 1 NM07944SW 7764 MACH TRIM & STAB TRIM MASTER CAUTION MESSAGES. REPLACED CAPTAIN'S TRIM DISCONNECT SWITCH. OPERATIONAL CHECK GOOD IAW CRJ200 MM 27-41-00. 2L72 4F RTA21EA 20050324001792005032400179SO 2005 3 24 SWIA200514738 120050321A3350 FUSE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07585SW 120353 FIRST THREE ROWS OF EMERGENCY LIGHTS ON FLOOR IN FRONT OF A/C DO NOT ILLUMINATE WITH EMERGENCY LIGHT SWITCH ON. INSTALLED SERVICEABLE FUSE. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050324001812005032400181EA 2005 3 24 SWIA200514740 120050110A5340 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07439SW 7578 FS 280 BL 9 LT INBOARD AND OUTBOARD BRACKETS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED FS 280 BL 9 LT INBOARD AND OUTBOARD BRACKETS IAW CRJ 200 SRM 51-42-06 PG 18, 51-40-11 PG 1, 2, 51-42-06 PG 11. 2L72 4F RTA21EA 20050324001832005032400183WP 2005 3 24 91500001 120050303A5315 FLOORBEAM DOUG DC9 DC915F 3022037WP PWA JT8 JT8D* NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23915CK 47086 MAIN DECK FLOORBEAM CORRODED AT NUT PLATES. 2L72 4F4 F A6WE E2EA 20050324001842005032400184EA 2005 3 24 SWIA200514725 120050318A2741 SWITCH CNDAIRCL600 CL6002B19 1900309EA TRIM STUCK A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07447SW 7677 F/O'S TRIM SWITCH IS STICKY. REMOVED AND REPLACED F/O'S SIDE TRIM SWITCH IAW MM 27-45-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050324001862005032400186EA 2005 3 24 SWIA200514727 120050319A2741 SWITCH CNDAIRCL600 CL6002B19 1900309EA TRIM STUCK A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07936SW 7726 F/O TRIM SWITCH STICKS. REPLACED F/O PITCH TRIM SWITCH IAW CRJ MM 27-41-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050324001892005032400189EA 2005 3 24 SWIA200514730 120050320A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07926SW 7687 SPOILERON STATUS MESSAGE ON EICAS. REMOVED AND REPLACED NR 1 HYDRAULIC SYSTEM SPOILERON PCU ON LEFT SIDE IAW CRJ MM 27-62-01. OPERATIONAL CHECK GOOD. P/N 27000-7, S/N OFF 6426. 2L72 4F RTA21EA 20050324001912005032400191EA 2005 3 24 SWIA200514732 120050319A5610 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAA UNSCHED LANDING O OTHER CRCRUISE 1 NM07956SW 7825 CAPTAIN`S WINDSHIELD SHATTERED AT FL350. REPLACED LEFT WINDSHIELD PER AMM 56-11-01. P/N OFF 601R33033-17, S/N OFF 03091H9936. 2L72 4F RTA21EA 20050324001932005032400193NM 2005 3 24 UPS05244148 120050309A5320 CHANNEL BOEING727 72722C 138400FNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 INSPECTION TYPE:C UPPER SUPPORT CHANNEL FOR EQUIP RACK CRACKED AT BS 400 BS 420 AND BS 460 LBL 17. REPAIRED CRACKS ON UPPER SUPPORT CHANNEL AT BS 400, 420, 460 LBL 17 IAW SRM 51-40-3. 2L73 4F A3WE 20050324001952005032400195NM 2005 3 24 UPS05244154 120050309A2750 SPINDLE BOEING727 72722C 138400FNM 4 FLAP CARRIAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 INSPECTION TYPE:C SURFACE CORROSION ON 4 FLAP CARRIAGE SPINDLE INNER SURFACE. CORROSION REMOVED IAW SRM 51-00-06, WITHIN LIMITS OHM 57-52-01. AREA PROTECTED IAW SRM 51-10-02. 2L73 4F A3WE 20050324001972005032400197NM 2005 3 24 UPS05444147 120050311A532269B031461 SHEAR TIE BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE:C M/D - BS 1580 S-19R FRAME ATTACH SHEAR TIE FOUND CRACKED, CRACK LENGTH .375 INCH. SHEAR TIE REPLACED AS PER SRM 51-10-01 PG 9 & INSTALLED AS PER SRM 51-30-02. 2L74 4F A20WE 20050324001992005032400199EU 2005 3 24 05FDEA00582 120050317A5347A5381192320600 SEAT TRACK AIRBUS310 A310222 3930315EU ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 MAIN DECK CARGO COMPT RT NR 3 SEAT TRACK FR45.5, FR47, FR48, FR49, FR51.5, FR52.5, CORROSION INSIDE SCALLOP HOLES 8-AERAS. REMOVED CORROSION IAW A310-200 SRM 51-74-10. TRACK WAS OUT OF LIMITS IAW A310-20 SRM 53-10-16 FIG 101. REMOVED AND REINSTALLED COUPLERS AND ATTACH FITTING IAW A310-200 SRM 51-72-10. REMOVED AND REPLACED BAD TRACK WITH NEW TRACK IAW A310-200 SRM 51-72-10. REINSTALLED CLS ADAPTERS IAW A310-200 SRM 51-72-10. 2L72 4F RTA35EU 20050324002012005032400201EU 2005 3 24 05FDEA00584 120050317A5320A537784342085 COVER AIRBUS310 A310222 3930315EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 CORROSION TWO PLACES AROUND RIVETS, FWD CARGO UNDER FLOOR AREA, FRAME 38.1 BETWEEN STRINGERS 44R AND 45R, FWD FLANGE OF WATER SERVICE PANEL. REMOVED AND REPLACED POTABLE WATER PAN AT FR38.1 IAW A310 SRM 51-72-10 AND SRM 51-40-21. 2L72 4F RTA35EU 20050325000012005032500001EU 2005 3 25 05FDEA00590 120050317A5320 INTERCOSTAL AIRBUS310 A310222 3930315EU FUSELAGE BENT A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25419FE 345 BETWEEN FR85 AND FR86 STG 35R (RT) 2EA CAPS ON INTERCOSTAL ARE BENT. INTERCOSTAL WEB & ANGLE FOUND TO BE CRACKED. REMOVED AND REPLACED WITH NEW WEB & ANGLE IAW A310 SRM 51-40-21. 2L72 4F RTA35EU 20050325000022005032500002EU 2005 3 25 05FDEA00591 120050317A5347 SEAT TRACK AIRBUS310 A310222 3930315EU FUSELAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25419FE 345 MAIN DECK CARGO COMP'T LEFT NR 5 SEAT TRACK, FR49, FR51.5, FR54, CORROSION INSIDE SCALLOP HOLES, 3-AREAS. REMOVED AND REPLACED SEAT TRACK SECTION BETWEEN FRAMES 50.5 AND 54 IAW A310-200 SRM 53-10-16. 2L72 4F RTA35EU 20050325000032005032500003NM 2005 3 25 UPS05444149 120050311A532269B031461 SHEAR TIE BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE:C M/D - BS 1560 LT BETWEEN STR 20L & 22L SHEAR TIE FOUND CRACKED, CRACK LENGHT .375 INCH. SHEAR TIE REPLACED AS PER SRM 51-10-01 PG 9 & INSTALLED AS PER SRM 51-30-02. 2L74 4F A20WE 20050325000042005032500004NM 2005 3 25 QXEA200500416 120050201A5730 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 600 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - RIGHTHAND WING, RIGHTHAND FUEL PANEL 622BT BOTTOM SURFACE OF PANEL PITTING AND FRETTING CORROSION AROUND PANEL ATTACH HOLES. REPAIRED IAW RD 8/4-57-419. 2H72 4T RTA13NM 20050325000052005032500005NM 2005 3 25 QXEA200500415 120050202A5730 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 600 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - RIGHTHAND WING, RIGHTHAND FUEL PANEL 623AT BOTTOM SURFACE OF PANEL PITTING AND FRETTING CORROSION AROUND PANEL ATTACH HOLES. REPAIRED IAW RD 8/4-57-420. 2H72 4T RTA13NM 20050325000072005032500007NM 2005 3 25 QXEA200500420 120050201A5730 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - LEFTHAND WING, LEFTHAND WING FUEL PANEL 522BT PANEL ATTACH DOMED ANCHOR NUT WS 114.50 AND STRINGER 4L ANCHOR NUT HAS UN-REMOVEABLE FOD. REPAIRED IAW Q400 SRM 51-42-05-330-001. 2H72 4T RTA13NM 20050325000082005032500008NM 2005 3 25 QXEA200500421 120050201A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 200 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - RIGHTHAND FUSELAGE EXTERNAL SKIN AT STATION X170, STRINGER 17 HAS A GOUGE. REPAIRED IAW RD 8/4-53-1156 AND HORIZON AIR EA 6-53-518. 2H72 4T RTA13NM 20050325000102005032500010NM 2005 3 25 CALA0500084 120050322A5330654677678 SKIN BOEING737 7373T0 1384582NM STA CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2759302 23353 INSPECTION FOUND THE FUSELAGE SKIN UNDER NR 3 VHF ANTENNA CORRODED, STA 727D, S29L TO S29R. INSTALLED REPAIR IAW ECRA 5331-01179. 2L72 4F RTA16WE 20050325000132005032500013NM 2005 3 25 UPS05444150 120050311A532269B031461 SHEAR TIE BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE:C M/D - BS 1580 LT BETWEEN STR 20L & 22L SHEAR TIE FOUND CRACKED, CRACK LENGTH .375 INCH. SHEAR TIE REPLACED AS PER SRM 51-10-01 PG 9 & INSTALLED AS PER SRM 51-30-02. 2L74 4F A20WE 20050325000142005032500014NM 2005 3 25 UPS05444152 120050311A532269B031461 SHEAR TIE BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE:C M/D - BS 1540 LT BETWEEN STR 20L & 22L SHEAR TIE FOUND CRACKED, CRACK LENGTH .375 INCH. SHEAR TIE REPLACED AS PER SRM 51-10-01 PG 9 & INSTALLED AS PER SRM 51-30-02. 2L74 4F A20WE 20050325000162005032500016NM 2005 3 25 UPS05444155 120050313A5313BAC1498145 STRINGER BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE:C AREA AFT OF BULK CARGO STA 2180 S42R STRINGER END CRACKED, CRACK LENGTH .75 INCH. AFT OF BULK CARGO BS 2160 TO 2180 STR 42R REPAIRED AS PER SRM 53-10-03 FIG 1. 2L74 4F A20WE 20050325000172005032500017WP 2005 3 25 UPS05844158 120050221A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE:C1, COMPT 60 L17R HAS 3 INCH CRACK AND LONGERON END FITTING HAS .5 INCH CRACK 1770. REMOVED AND REPLACED L17R AND END FITTING AT STATION 1770 IAW 51-1-8, 51-1-20D, 53-2-2 AND 51-1-21. 2L74 4F RT4A25 20050325000182005032500018WP 2005 3 25 UPS05844159 120050222A5347 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 INSPECTION TYPE: C1, AFT CARGO BS 1420 LT CUSP, APROX LBL 60 ON FWD SIDE OF FRAME, SEVERE CORROSION UNDER & AROUND NUTCLIPS APPROX .5 INCH DIA SEAT TRACK. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-2-3. REMOVED AND REPLACED SEAT TRACK SECTION AND INSTALLED SPLICES STA 1410 TO 1430 LBL 60 IAW 53-2-3 FIG 8A, 51-1-20D AND 51-3-0. 2L74 4F RT4A25 20050325000192005032500019EU 2005 3 25 05FDEA00585 120050317A5347 SEAT TRACK AIRBUS310 A310222 3930315EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 MAIN DECK CARGO COMPT RT NR 2 SEAT TRACK, FR45.5, FR46, FR46.5, FR47, FR49, FR52.5, FR53, FR54 CORROSION INSIDE SCALOPE HOLES, 9 AREAS AS MARKED. REMOVED CORROSION IAW A310 SRM 51-74-10. TRACK IS OUT OF LIMITS IAW A310 SRM 53-10-16 FIG 101. FABRICATED NEW SEAT TRACK FROM FR45 TO 54 IAW A310 DWG A538-11922. REMOVED AND REINSTALLED CLS ADAPTERS AND REMOVED OLD TRACK AND INSTALLED NEW TRACK IAW A310 SRM 51-72-10. 2L72 4F RTA35EU 20050325000202005032500020EA 2005 3 25 COMA0570033 120050321A27308221308320 COMPUTER CNDAIRCL600 CL6002C10 1390015EA PITCH TRIM MALFUNCTIONED A COMAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 SO01317CA6748 10055 FLIGHT 5020 SUSPECTED PITCH TRIM ANOMALY. REPLACED THE FLIGHT CONTROL COMPUTER. 2L72 4F RTA21EA 20050325000212005032500021EU 2005 3 25 05FDEA00586 120050317A5315 FLOORBEAM AIRBUS310 A310222 3930315EU FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 FWD PIT BAY CEILING AREA FR 38, 38 INCHES TO LT OF CTR FLOORBEAM IS CRACKED. REWORKED AREA TO INSTALL 2EA ANGLE REPAIRS PER A310-200 SRM 53-10-15. CLEAN, TREATED AND PRIMED AREA PER A310-200 SRM 51-21-10, INSTALLED 2EA REPAIR ANGLES PER A310-200 SRM 53-10-15 FIG 201. TREATED, PRIMED AND TOP COATED PER A310-200 SRM 51-21-10. 2L72 4F RTA35EU 20050325000232005032500023EU 2005 3 25 05FDEA00588 120050317A5340 FITTING AIRBUS310 A310222 3930315EU TAIL CONE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 BILGE AREA FR91, 33 INCHES TO LEFT OF CTR STG 29L FITTING FOR TAIL CONE HAS CORROSION AROUND FASTENER HOLE EXTENDING UNDER FASTENER AND FASTENER IS CORRODED. REMOVED BOLT, CLEANED CORROSION AROUND FASTENER HOLE HAD NDT VERIFY THICKNESS AND FOUND IT TO BE WITHIN LIMITS IAW A310 SRM 53-10-00 PAGE 106 TABLE 102, TOP COATED AREA IAW A310 SRM 51-75-00 AND INSTALLED SERVICEABLE HARDWARE IAW A310 SRM 51-40-21. 2L72 4F RTA35EU 20050325000242005032500024EU 2005 3 25 05FDEA00589 120050317A5313 STRINGER AIRBUS310 A310222 3930315EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 AFT CARGO COMPT AFT OF FR 601 ON RT STG 50 HAS AREA OF CORROSION. REMOVED 9EA RIVETS PER A310-200 SRM 51-40-21. REMOVED CORRSION PER A310-200 SRM 51-71-10, NDT FOR MAT LOSS FOUND TO BE OUT OF LIMITS PER A310-200 SRM 53-10-00. CUT OUT DAMAGED SECTION PER A310-200 SRM 53-10-14. TREATED AND PRIMED TOP COATED FILLER AND COUPULING PER A310-200 SRM 51-75-10. INSTALLED STG FILLER AND STG REPAIR COUPLING PER A310-200 SRM 51-40-21. 2L72 4F RTA35EU 20050325000252005032500025EA 2005 3 25 SWIA200514742 120050307A5210 ANGLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07442SW 7609 PAX DOOR AIRSTAIR AFT DRAG ANGLE IS CRACKED BESIDE DOOR ASSIST PULLEY BRACKET FS 357.00. ITEM FOUND AT C-CHECK INSPECTION. DRAG ANGLE REPAIRED IAW CRJ REO 601R-52-11-513. 2L72 4F RTA21EA 20050325000262005032500026EU 2005 3 25 05FDEA00592 120050317A5311 FRAME AIRBUS310 A310222 3930315EU FUSELAGE CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25419FE 345 MAIN CABIN FRAME 37 CLS ADAPTER -YD40 IS GOUGED AND CRACKED (BETWEEN SEAT TRACK 2 AND 3 LT). REMOVED AND REPLACED CLS ADAPTER PER A310 SRM 51-72-10. TREATED, PRIMED AND TOP COATED AREA AND FASTENERS PER A310-200 SRM 51-75-10. 2L72 4F RTA35EU 20050325000272005032500027EA 2005 3 25 SWIA200514743 120050307A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07442SW 7609 FS 280 RT FLOORBEAM RBL 9.0 INBOARD ATTACH ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13 AND 51-23-00. 2L72 4F RTA21EA 20050325000282005032500028EA 2005 3 25 SWIA200514744 120050307A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07442SW 7609 FS 280 LT FLOORBEAM RBL 9.0 INBOARD ATTACH ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13 AND 51-23-00. 2L72 4F RTA21EA 20050325000312005032500031EA 2005 3 25 SWIA200514747 120050307A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07442SW 7609 FUSELAGE PULLEY INTERCOSTAL HAS A CRACKED OUTBOARD FLANGE AND INBOARD ANGLE FS 484.00 RBL 27.0 & 36.0. ITEM FOUND AT C-CHECK INSPECTION. FS 484 RBL 27 ANGLE REPLACED IAW CRJ REO 601R-53-41-059 REV A. 2L72 4F RTA21EA 20050325000332005032500033EA 2005 3 25 SWIA200514749 120050307A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07442SW 7609 FS 621 FLOOR SUPPORT ANGLE LBL 42 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-61-117 REV B. 2L72 4F RTA21EA 20050323000852005032300085NM 2005 3 23 QXEA200500407 120050204A5730 ACCESS PANEL BOMBDRDHC8 DHC8402 1390042NM ZONE 600 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09536DS 4044 YYC - RIGHTHAND WING, RIGHTHAND FUEL TANK PANEL 622CT, PANEL REBATED WS 117.50 TO WS 157.825, FRETTING CORROSION ON TOP SURFACE OF REBATE AROUND PANEL ANCHOR NUT ATTACH HOLES. REPAIRED IAW Q400 SRM 57-10-30-320-002 AND RD 8/4-57-435, ISSUE 1. 2H72 4T RTA13NM 20050323000942005032300094NM 2005 3 23 SWAA050856 120050318A53156545410 FLOORBEAM BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND 4 EA CRACKS ON LONGITUDINAL BEAMS AT BS 727A + 17, RBL 25, RBL 45, LBL 25, LBL 45. REPAIRED BEAMS PER PAE ER. 2L72 4F RTA16WE 20050323001012005032300101NM 2005 3 23 SWAA050863 120050320A335010107451 SIGN BOEING737 7373H4 1384600NM R2 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29640SW 27713 R2 DOOR EMERGENCY EXIT SIGN FELL OFF IN FLIGHT. REINSTALLED SIGN PER MM. 2L72 4F RTA16WE 20050323001112005032300111WP 2005 3 23 DHL2005805513 120050223A5711 FRAME DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 LT OUTER WING INBOARD L/E UPPER FORMER CRACKED 0.500, XFS 597.500. REMOVED FASTENERS IAW SRM 51-1-20D PG 21. PERFORMED STOP DRILL ON CRACK END AND FABRICATED (2EA) ANGLE DOUBLERS (AL7075-T6 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLERS IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLERS WITH NEW FASTENERS IAW SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. TORQUED IAW SRM 51-3-1 PG 2A. 2L74 4F RT4A25 20050323001122005032300112WP 2005 3 23 DHL2005805510 120050305A551037014272 FITTING DOUG DC8 DC873F 302199FWP HORIZONTAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 RIGHT HORIZONTAL STABILIZER FITTING CRACKED 0.500, XFS 60.000 (LWR PART). REMOVED CRACKED FITTING IAW SRM 55-1-0 PG 1, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED NEW FITTING WITH NEW FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050323001172005032300117NM 2005 3 23 QXEA200500410 120050208A5310 MOUNT BOMBDRDHC8 DHC8401 1390041NM ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - NR 2 VHF ANTENNA MOUNT REWORK IS NOT ACCOMPLISHED REF FAA AD 2004-05-13. COMPLIED WITH IAW HORIZON AIR EA 6-53-265, 6-53-162 AND SERVICE BULLETIN 2004-05-13. 2H72 4T RTA13NM 20050323001212005032300121NM 2005 3 23 QXEA200500403 120050131A5420 WEB BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - LEFTHAND NACELLE WEB IS CRACKED JUST ABOVE FLAP TRACK NR 3. REPAIRED IAW RD 8/4-54-155, ISSUE 1 AND Q400 SRM SUB TASK 51-42-05-330-001, 51-40-15-400-001. 2H72 4T RTA13NM 20050323001262005032300126EU 2005 3 23 RAIA00503007 120050316A2750AIR135692 SWITCH JETAIRJETSTMJETSTM4101 1500501EU TE FLAPS MALFUNCTIONED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03559HK 41075 STL - FLAP SELECT SWITCH WENT TO OFF POSITION. MAINTENANCE REMOVED AND REPLACED RIGHT MLG AOG SWITICH. 2L72 4T RTA41NM 20050323001302005032300130NM 2005 3 23 QXEA200500409 120050131A5730 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - LEFTHAND WING, LEFTHAND WING FUEL TANK PANEL 522BT, PANEL REBATE WS 79.700 TO WS 117-500, FRETTING CORROSION ON TOP SURFACE OF REBATE AROUND PANEL ANCHOR NUT ATTACH HOLES. REPAIRED IAW Q400 SRM 57-10-30-320-002, RD 8/4-57-424, ISSUE 1 AND HORIZON AIR EA 6-57-298. 2H72 4T RTA13NM 20050323001312005032300131NM 2005 3 23 QXEA200500391 120050118A5320 STOP FITTING BOMBDRDHC8 DHC8401 1390041NM ZONE 200 WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - BAGGAGE DOOR SURROUND STOP FITTINGS AT STATION X728 HAS MINOR WEAR DAMAGE FROM LINER. REPAIRED IAW Q400 SUB TASKS 51-21-10-380-001, 51-25-10-370-001 AND 51-25-15-370-001. 2H72 4T RTA13NM 20050323001342005032300134NM 2005 3 23 QXEA200500397 120050124A5753 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 600 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - RIGHTHAND OUTBOARD FLAP HAS A CHAFING MARK SEVERAL FEET LONG FROM CONTACT WITH THE UPPER FLAP TOP SURFACE. REPAIRED IAW Q400 SRM 57-20-30-320-801, 57-52-30-940-001. 2H72 4T RTA13NM 20050323001482005032300148NM 2005 3 23 CALA0500081 120050321A3350D71701100 BATTERY PACK BOEING737 737824 13844BZNM EMERGENCY LIGHT INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2712218 28778 THE RT SIDE OVERHEAD EMERGENCY LIGHTS AT ROW 14 -20 WERE FOUND INOPERATIVE. THE BATTERY PACK AT ROW 19 WAS REMOVED AND REPLACED IAW MM 33-51-06 AND OPERATION OF THE EMERGENCY LIGHTS WAS RESTORED. 2L72 4F RTA16WE 20050323001492005032300149NE 2005 3 23 DL757050165 220050315A73218271041 FUEL CONTROL BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 1 ENGINE MALFUNCTIONED A DALAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SO27613DL 22820 716330 LEFT ENGINE LOST THRUST AFTER APPLICATION OF TAKEOFF THRUST. REPLACED LEFT ENGINE FUEL CONTROL UNIT. 2L72 4F4 FRTA2NM E17NE 20050323001502005032300150SO 2005 3 23 C2XA05SH019 120050320A532014521713003 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715910 145455 SHV - DURING C-CHECK THE LEFT HAND OMEGA BEAM AT FRAME 20 IS CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED REPAIR IAW EMB-145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050323001912005032300191NM 2005 3 23 AALA20050208 120050319A3350BPS73 BATTERY PACK BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21387AM 27184 LAX - TWO LEFT HAND OVERHEAD AISLE EMERGENCY LIGHTS AFT OF EXIT SIGN AT OVERWING EXITS INOPERATIVE. REPLACED BATTERY PACK FOR TWO LEFT HAND OVERHEAD AISLE EMERGENCY LIGHTS AFT OF EXIT SIGN AT OVEWING EXITS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050323001942005032300194NE 2005 3 23 AALA20050207 220050320A7200 ENGINE BOEING757 757223 1384957NM RROYCERB211 RB211535E4B3 NE LEFT OVERTEMP A AALAA UNSCHED LANDING MXJOVER TEMP ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SW21183AN 29593 31639 PHL - INFLIGHT LEFT ENGINE FAILURE ON TAKEOFF. ENGINE HAD LARGE VIBRATION FOLLOWED BY WHAT FELT LIKE SEIZURE. ENGINE GENERATOR TEMPERATURE 975C. REPORTS OF FIRE AND SMOKE BY AIR TRAFFIC CONTROL, OTHER AIRCRAFT AND PASSENGERS. NO FIRE WARNING. ENGINE SHUTDOWN PER QRH PROCEDURE. REPLACED NUMBER ONE ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA2NM E12EU 20050323001962005032300196NM 2005 3 23 AALA20050203 120050316A3397 CONNECTOR BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21799AN 30258 DFW - EMERGENCY LIGHTS IN SEAT ROWS 35 TO 40 INOPERATIVE. FOUND EMERGENCY PATH LIGHT CONNECTOR OFF ON SEAT 34 CENTER. INSTALLED CONNECTOR AT SEAT 34 CENTER FOR EMERGENCY LIGHTS IN SEAT ROWS 35 TO 40. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20050323001982005032300198NM 2005 3 23 SWAA050753 120050311A53126546568 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED C3 CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT STR 16L. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050323002002005032300200NM 2005 3 23 SWAA050755 120050312A335010107451 SIGN BOEING737 7373H4 1384600NM MID CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29376SW 26584 RIGHT OVERWING EMERGENCY EXIT SIGN LOOSE. REINSTALLED SIGN PER MM. 2L72 4F RTA16WE 20050323002022005032300202NM 2005 3 23 SWAA050766 120050312A3350101073 LENS BOEING737 7375H4 138449DNM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29505SW 24182 RIGHT OVERWING EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED LIGHT COVER PER MM. 2L72 4F RTA16WE 20050324000032005032400003EU 2005 3 24 05FDEA00578 120050316A5753 SKIN AIRBUS310 A310222 3930315EU TE FLAP DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 REPAIR NEEDS EVALUATION FOR FAA APPROVED DATA AND MAJOR OR MINOR CLASSIFICATION. RT WING RT INBOARD TRAILING EDGE FLAP LOWER SURFACE AFT AND INBOARD OF NR 2 TRACK BEAM, ITEM 43 OF LIST. RT WING RT INBOARD TRAILING EDGE FLAP LOWER SUFACE AFT AND I/B OF NR 2 FLAP TRACK BEAM DOUBLER IS RIVETED ACCESS PANEL ON I/B FLAP ASSY AND FOUND TO BE IN CONFORMANCE WITH AIRBUS DWG A579-70100. 2L72 4F RTA35EU 20050324000042005032400004WP 2005 3 24 05FDEA00611 120050321A5311 FRAME DOUG DC10 DC1010 3022110WP FUSELAGE DAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25571FE 47830 DURING INSPECTION FOUND AT STA 1701 FROM STR 45 RT TO 45 LT RETAINER WITH CORROSION. REMOVED CORROSION ON RETAINER PER SRM 51-21-01. PERFORMED CHECK LIMITS; THE MATERIAL REMOVED IS WITHIN LIMITS PER SRM 53-00-01. PROTECTED AREA PER SRM 51-21-01. (OPEN) 2L73 4F A22WE 20050324000082005032400008NM 2005 3 24 05FDEA00580 120050317A5511 RIB BOEING727 727200 138407ENM HORIZONTAL STAB CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 RIGHT HORIZONTAL STAB, INTERIOR RIB WEB CRACKED L/E STA 131, 2 INCHES FROM FWD EDGE ALONG TOP. *S/D* REPAIRED FRONT SPAR WEB, RIGHT STAB LEADING EDGE STA 131 PER SRM 55-10-4. 2L73 4F RTA3WE 20050324000092005032400009EA 2005 3 24 COMA0560143 120050225A2750855D10011 BPSU CNDAIRCL600 CL6002B19 1900309EA RT WING FAULTY A COMAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 SO01966CA6987 7132 RECEIVED A FLAP FAIL CAUTION DURING YYZ APPROACH, CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED THE RIGHT BRAKE POSITION SENSING UNIT. 2L72 4F RTA21EA 20050324000162005032400016EU 2005 3 24 MALA050194 120050122A3397 WIRE SAAB SF340 SF340A 7850100EU POWER SUPPLY BURNED A MALAK NONE O OTHER ININSP/MAINT 1 GL15110XJ 340A110 EMERGENCY POWER SUPPLY P/N 60-1321-1 S/N 16238 INSPECTION HAS BURNED WIRE INSIDE. REPAIRED GROUND WIRE. UNIT PASSES CMM CHECKS, RTS 1/25/05. 2L72 4T RTA52EU 20050324000202005032400020WP 2005 3 24 ASMF200501017 120050131A3620 VALVE DOUG DC9 DC987 3022087WP RT ENGINE MALFUNCTIONED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23803ML 49726 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF AFTER ENGINES STARTED, EICAS MESSAGES "L ENG BLEED OFF" AND "PACK BITE" WERE SHOWN. CAPTAIN REPORTED THAT PURGE VALVE OF RIGHT ENGINE DID NOT OPEN, RESTARTED RIGHT ENGINE AND THE PURGE VALVE OPENED NORMALLY. DURING OVERNIGHT SERVICE THE FIM 36-10-00 PROCEDURE WAS PERFORM AND SYSTEM WAS TESTED IAW MM 36-10-09, ALL CORRECT. 2L72 4F RTA6WE 20050324000632005032400063EU 2005 3 24 AWXA200500264 120050215A5315D5347219020200 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28647AW 762 MCN - MAJOR REPAIR - DURING 8-DAY CHECK, CORROSION WAS FOUND ON FLOORBEAM Y19 AT FS 64. MAINTENANCE REMOVED CORRODED FLOORBEAM Y19 AT FS 64; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050324000652005032400065WP 2005 3 24 05FDEA00484 120050310A5753NRC6068510 SUPPORT DOUG DC10 DC1010 3022110WP ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25369FE 46607 COMPLY WITH EA 8-5750-55451, RT OB FLAP FLAP VANE SUPPORT CORROSION REWORK. CLOSING ACTION ON 03/08/05. ON N/R S00013. COMPLIED WITH EA 8-5750-55451. 2L73 4F A22WE 20050324000732005032400073NE 2005 3 24 NACA20050005 220050215A8530356993 CYLINDER DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE NR 18 CRACKED A NACAEA ENGINE SHUTDOWN UNSCHED LANDING REJPARTIAL RPM/PWR LOSS VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 AL03993301367 1367 P35205 43576 P35205 NR 4 ENGINE SHUT DOWN, WOULD NOT TAKE A LEAN. NR 4 ENGINE NR 18 CYLINDER REPLACED. OP AND LEAK CHECKED GOOD. 2L74 4R4 R 6A3 5E8 20050324000912005032400091NE 2005 3 24 NACA20050003 220050212A8530356994 CYLINDER DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE NR 3 CRACKED A NACAE ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION DEDESCENT 1 AL036174C721 721 44075 P33688 NR 4 ENGINE SHUT DOWN DUE TO RUNNING ROUGH. NR 4 ENGINE NR 3 CYLINDER CRACKED, REPLACED CYLINDER AND OP CHECKED GOOD. 2L74 4R4 R 6A3 5E8 20050324000942005032400094WP 2005 3 24 ABXA050066 120050302A53119919619505 FRAME DOUG DC9 DC941 302207NWP CABIN CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23969AX 47464 LEFT AFT MAIN FRAME HAD A CRACK APPROXIMATELY 1.5 INCH IN LENGTH AT POINT E FORWARD FLANGE. CRACK WAS WITHIN ALLOWABLE LIMITS IAW DC-9 SERVICE BULLETIN 53-131 AND ES00913. 2L72 4F A6WE 20050324000952005032400095WP 2005 3 24 ABXA050059 120050216A534039248101 FITTING DOUG DC9 DC941 302207NWP FWD CARGO CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23966AX 47510 LONGERON 26 LEFT CRACKED AT STA 636 THROUGH KIDNEY PANEL. REMOVED AND REPLACED LONGERON END FITTING 26 LEFT AT STA 636 IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 20050324001072005032400107EA 2005 3 24 COMA0560162 120050308A30304344198100 THERMOSWITCH CNDAIRCL600 CL6002B19 1900309EA RT WING MALFUNCTIONED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01989CA 7215 WING OVERHEAT WARNING. REPLACED THE RT WING STANDBY THERMAL SWITCH. 2L72 4F RTA21EA 20050324001082005032400108EA 2005 3 24 COMA0560163 120050308A7830 PDU CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER OUT OF ADJUST A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01995CA 7229 FLIGHT 9468 - LT THRUST REVERSER UNLOCKED MESSAGE. ADJUSTED THE PDU, OPERATIONAL CHECK SATISFACTORY. 2L72 4F RTA21EA 20050324001102005032400110CE 2005 3 24 20030784 120050110A53101294300433 WINDOW FRAME BEECH 1900 1900D 1154162CE FUSELAGE CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03247GL1792917929 UE247 DURING ROUTINE STRUCTURAL INSPECTION, ALL THREE EMERGENCY EXIT WINDOW PANS WERE FOUND TO HAVE CRACKS AROUND THE RADIUS. WINDOW PANS WERE REPLACED, AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA24CE 20050324001132005032400113EA 2005 3 24 QXEA200500198 120050124A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - RIGHT INBOARD SEAT TRACK AT STATION X541 HAS PITTING CORROSION ON INSIDE SURFACE. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01, REO 670-53-00-060, REV B AND HORIZON AIR EA R-53-266. 2L72 4F RTA21EA 20050324001142005032400114EA 2005 3 24 QXEA200500199 120050124A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - RIGHT INBOARD SEAT RAIL AT STATION X571 HAS PITTING CORROSION ON INSIDE SURFACE. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01, REO 670-53-00-060, REV B. AND HORIZON AIR EA R-53-266. 2L72 4F RTA21EA 20050324001272005032400127 2005 3 24 0500359926 420050314A2212258668658 COMPUTER DOUG DC9 DC932 3022066WP AUTOPILOT MALFUNCTIONED A NWAAH DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED CRCRUISE 1 GL01926NW 47425 WHILE CRUISING AT FL340, THE AUTOPILOT PITCH BEGAN TO FLUCTUATE +/- 500 FPM WHILE IN "ALTITUDE HOLD". FLIGHT CREW SUSPECTED ALTERNATE TRIM WAS CAUSING THE DEVIATIONS. COMPLIED WITH COM PROCEDURES FOR RUNAWAY TRIM AND FLUCTUATIONS STOPPED. THEN AGAIN AT FL120, THE PRIMARY TRIM BEGAN MOVING EVEN WITH THE ALTERNATE TRIM CIRCUIT BREAKERS PULLED AND THE ELEVATOR SERVO IN OFF POSITION. ALSO, THE INBOARD MANUAL TRIM HANDLE WOULD NOT RETURN TO DETENT. LANDING AT DTW WAS UNEVENTFUL AND MAINTENANCE REPLACED THE PITCH AXIS COMPUTER AND INSTALLED A MISSING BELL CRANK ROLLER DETENT SPRING. AIRCRAFT WAS RE-QUALIFIED FOR LLM OPERATIONS AND HAS RETURNED TO SERVICE. 2L72 4F A6WE 20050324001312005032400131WP 2005 3 24 IXXA0500016O 120050303A7711JG298H2 INDICATOR DOUG DC8 DC862F 3021972WP EPR INOPERATIVE A IXXAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SW11799AL758702634 45922 CREW REJECTED TAKEOFF FROM RJTY, DUE TO LOW EPR ON NR 1 ENGINE. ALL OTHER PARAMETERS WERE NORMAL. CREW RETURNED AIRCRAFT TO BLOCKS. MAINTENANCE TROUBLESHOT TO A BAD EPR INDICATOR IN THE NR 1 POSITION. THE INDICATOR WAS REMOVED AND REPLACED AND THE OPERATIONAL CHECK GOOD PER ALL APPLICABLE MANUALS. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F 4A25 20050324001322005032400132EA 2005 3 24 QXEA200500191 120050124A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - RIGHT INBOARD SEAT RAIL, AT STATION X429, HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW CRJ700 SRM 51-21-00-001-001-A01, REO 670-53-00-060, REV B. AND HORIZON AIR EA R-53-266. 2L72 4F RTA21EA 20050324001532005032400153EA 2005 3 24 QXEA200500193 120050124A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - RIGHT INBOARD SEAT RAIL, AT STATION X459, HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW CRJ700 SRM 51-21-00-001-001-A01, REO 670-53-00-060, REV B AND HORIZON AIR EA R-53-266. 2L72 4F RTA21EA 20050324001642005032400164NE 2005 3 24 05009 220050130A7260 GARLOCK SEAL BOEING747 747206B 1384856NM PWA JT9 JT9D7R4G2 52054NE CSD FAILED A KCSAO OTHER K FLUID LOSS NRNOT REPORTED 1 GL23704CK 22299 725343 PRECAUTIONARY ENG SHUTDOWN ON NR 1 ENG DUE TO LOW OIL QTY. REMOVED AND REPLACED CONSTANT SPEED DRIVE GARLOCK SEAL IAW MM 72-61-07. REMOVED AND REPLACED TRANSFER TUBE "O" RINGS IAW MM 72-61-15 DUE TO BROKEN "O" RING. REMOVED AND REPLACED NR 1 CONSTANT SPEED DRIVE IAW MM 24-11-01, DUE TO LEAKING OIL. REMOVED AND REPLACED NR 1 GENERATOR SHAFT O-RING, DUE TO BEING BROKEN IAW MM 24-21-01. INSPECTED EXTERNAL PART OF ENG THOROUGHLY, INSPECTED VISUALLY, CK'S OK. PERFORMED ENG, RUN-UP IAW MM 71-00-00. ALL FUNCTIONAL RUN-UP CK'S AND PARAMETERS CK'S OK. NO LEAKEDS NOTED. PERFORMED WINDMILLING INSPECTION IAW MM 72-00-00. NO DEFECTS NOTED. 2L74 4F4 FRTA20WE E3NE 20050324001882005032400188SO 2005 3 24 SWIA200514729 120050314A3397 WIRE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07190SW 120050 EMERGENCY EXIT LIGHT AT ROW 9 OVERHEAD INOPERATIVE. REPAIRED BROKEN WIRE AT OVERHEAD BIN AT 9A FOR EMERGENCY EXIT LIGHT AS REQUIRED. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050324001902005032400190EA 2005 3 24 SWIA200514731 120050318A3610 DUCT CNDAIRCL600 CL6002B19 1900309EA CABIN AIR DAMAGED A SWIAGA O2 MASK DEPLOYED UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM07587SW 7062 IN CRUISE AT FL340, CABIN ALT BEGAN TO DECREASE. DESCENDED TO FL240 AND CABIN CONTINUED TO DESCEND RAPIDLY. CABIN ALTITUDE REACHED 16,000 FT AND PAX O2 MASKS DROPPED. DIVERTED TO GJT. REPLACED LT PACK SUPPLY DUCT. OPERATIONAL CHECK NORMAL IAW MM 21-31-16-710-801, 21-51-13, 21-51-00-710-801. 2L72 4F RTA21EA 20050324001922005032400192NM 2005 3 24 UPS05244146 120050310A5320 FLOOR SUPPORT BOEING727 72722C 138400FNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 INSPECTION TYPE:C FLOOR SUPPORT CRACKED AT BS 1070 LBL 14. REPLACED FLOOR SUPPORT FROM 1100 - 1060 IAW SRM 53-10-5 FIG 4. 2L73 4F A3WE 20050324001942005032400194NM 2005 3 24 UPS05244151 120050309A5320 CHANNEL BOEING727 72722C 138400FNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 INSPECTION TYPE:C UPPER SUPPORT CHANNEL FOR EQUIPMENT RACK CRACKED AT BS 420 AND 460 RBL 22. REPAIRED CRACKED UPPER SUPPORT CHANNEL IAW SRM 51-90-3 AT BS 420 TO 460. 2L73 4F A3WE 20050324001962005032400196NM 2005 3 24 UPS05444145 120050312A532069B022122 FLOOR SUPPORT BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE:C M/D - BS 2300 RBL 52 FLOOR SUPPORT FOUND CRACKED, CRACK LENGTH 0.5 INCH. M/D - BS 2300 RBL 52 FLOOR SUPPORT REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02. 2L74 4F A20WE 20050325000112005032500011NM 2005 3 25 CALA0500085 120050321A532014N51611 INTERCOSTAL BOEING757 757224 1384958NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714106 27296 INSPECTION FOUND GALLEY SUPPORT INTERCOSTAL CORRODED AT BS 334, RBL 2. REPAIRED IAW ECRA 5320-01768. 2L72 4F RTA2NM 20050325000122005032500012NM 2005 3 25 CALA0500086 120050321A5315143N55042 FLOORBEAM BOEING757 757224 1384958NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714106 27296 INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT FLOORBOARD FASTENER HOLE, BS 720, RBL 26 AND RBL 43.5. REPAIRED IAW ECRA 5320-01769. 2L72 4F RTA2NM 20050325000292005032500029EA 2005 3 25 SWIA200514745 120050307A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07442SW 7609 MAIN FUSELAGE FS 280 RBL 9.0 LOWER FLANGE CRACKED ON TRANSVERSE BEAM. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13 AND 51-23-00. 2L72 4F RTA21EA 20050325000352005032500035EA 2005 3 25 SWIA200514751 120050309A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07953SW 7813 FLOORBEAM RBL 9.0 ATTACH ANGLE IS CRACKED AT FS 280.0. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-25-16, AND 51-23-00. 2L72 4F RTA21EA 20050325000362005032500036EU 2005 3 25 05FDEA00593 120050317A5330 PANEL AIRBUS310 A310222 3930315EU LT WING DAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25419FE 345 LT WING TO FUSELAGE FILLET PANEL 3RD PANEL FWD OF T/E. REMOVED PANEL 577AL DUE TO NON CONFORMANCE IAW A310 AMM 53-10-63-4. REPAIRED PANEL IAW A310 SRM 51-77-10. TREATED PANEL IAW A310 SRM 51-75-10. INSTALLED PANEL 577AL IAW A310 AMM 53-10-63-4, COMPLETED REPAIR CONFORM TO ALL FAA APPROVED DATA. 2L72 4F RTA35EU 20050325000372005032500037 2005 3 25 237TR0010 420050316A22114038891916 COMPUTER BOEING737 737228 13844AGNM AUTOPILOT MALFUNCTIONED A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05237TR 23007 THE A-AUTO PILOT WILL NOT ENGAGE IN CWS OR CMD. PLACED A-AUTO PILOT ON MEL 22-1. 03/17/2005: REPLACED A-SYSTEM AFCS PER MM 22-11-331. OPS CHECKS GOOD. 2L72 4F RTA16WE 20050325000382005032500038EA 2005 3 25 SWIA200514752 120050309A5210 ANGLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07953SW 7813 PASSENGER DOOR AFT DRAG ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. DRAG ANGLE REPAIRED IAW CRJ REO 601R-52-11-513. 2L72 4F RTA21EA 20050325000392005032500039NM 2005 3 25 05FDEA00599 120050317A5347ADA73492 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 MAIN DECK CARGO COMPARTMENT, SEAT TRACK CROWN AT RIGHTHAND STA Y= 1090, X= -47 FOUND ELONGATED. MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT RIGHTHAND STA Y= 1049 TO Y= 1129 , X= -47 TRIMMED, REMOVED AND REWORKED SEAT TRACK INSTALLED PER SRM 53-70-00 VOLUME I, FIGURE 1. 2L73 4F RTA22WE 20050325000402005032500040NM 2005 3 25 05FDEA00600 120050318A5347ADA73492 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 MAIN DECK CARGO COMPARTMENT, SEAT TRACK CROWN FOUND CHAFED AT STA Y= 965, X= -47. MAIN DECK CARGO COMPARTMENT, CHAFED SEAT TRACK AT STA Y= 949 TO Y= 1009, X= -47. TRIMMED, REMOVED AND REWORKED SEAT TRACK INSTALLED PER SRM 53-70-00 VOLUME I FIGURE 1. 2L73 4F RTA22WE 20050325000412005032500041NM 2005 3 25 05FDEA00601 120050318A5347ADA73492 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 MAIN DECK CARGO COMPARTMENT, SEAT TRACK CROWN FOUND CHAFED AT STA Y= 965, X= -47. MAIN DECK CARGO COMPARTMENT, CHAFED SEAT TRACK AT STA Y= 949 TO Y= 1009, X= -47 TRIMMED, REMOVED AND REWORKED SEAT TRACK INSTALLED PER SRM 53-70-00 VOLUME I FIGURE 1. 2L73 4F RTA22WE 20050325000422005032500042EU 2005 3 25 05FDEA00602 120050318A5730 SKIN AIRBUS310 A310222 3930315EU LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 LEFT WING T/E BOTTOM SKIN HAS INDICATION OF CRACK ON I/B CORNER SIDE CUTOUT PANEL 581AB AS MARKED. COMPLIED WITH EA 6-5710-86028. 2L72 4F RTA35EU 20050325000452005032500045EA 2005 3 25 SWIA200514754 120050309A5320 SILL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07953SW 7813 CARGO DOOR SILL BETWEEN FS 574 - 621 HAS AREAS OF CORROSION AROUND ANCHOR NUTS. ITEM FOUND AT C-CHECK INSPECTION. BLENDED AND ASSESSED CORROSION IAW CRJ SRM 53-0-00 101, FOUND TO BE WITHIN LIMITS. MATERIAL REMOVED .001. AREA REPROTECTED IAW SRM 51-21-11, 51-25-16. 2L72 4F RTA21EA 20050325000482005032500048NM 2005 3 25 QXEA200500422 120050120A5320 SILL BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 FORWARD FUSELAGE, RIGHTHAND FORWARD EMERGENCY EXIT LOWER DOOR SILL, BETWEEN STATION 71.20 AND 96.800 STRINGER 23R CORROSION FOUND BETWEEN SILL COVER PLATE AND SILL. 2H72 4T RTA13NM 20050325000522005032500052NM 2005 3 25 QXEA200500425 120050202A5710 PLATE BOMBDRDHC8 DHC8401 1390041NM ZONE 600 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - RIGHT WING LADDER PLATE FOR PANEL 622AT HAS FRETTING CORROSION. REPAIRED IAW Q400 SRM 57-10-30-320-002 AND HORIZON AIR EA 6-57-301. 2H72 4T RTA13NM 20050325000532005032500053NM 2005 3 25 QXEA200500424 120050131A5730 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 600 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - RIGHT WING PANEL 622AT HAS FRETTING CORROSION ON BOTTOM SIDE OF PANEL. REPAIRED IAW Q400 SRM 57-10-35-992-801 AND 57-10-30-940-002. 2H72 4T RTA13NM 20050325000542005032500054WP 2005 3 25 DHL2005805508 120050220A5531 FRAME DOUG DC8 DC873F 302199FWP VERTICAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 RIGHT VERTICAL STABILIZER L/E FORMER CRACKED 1.000, STA ZFS 198.500. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE AND FABRICATED (2EA) ANGLE DOUBLERS (AL7075-T6 0.032) IAW SRM 55-2-0 PG 7-8 FIG 2. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLERS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED ANGLE DOUBLERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9, TORQUED IAW SRM 51-3-1 PG 2A TABLE II. 2L74 4F RT4A25 20050325000562005032500056WP 2005 3 25 DHL2005805506 120050224A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 LEFT OUTER WING INBOARD L/E UPPER FORMER CRACKED 0.500, XFS 603.750. REMOVED FASTENERS IAW SRM 51-1-20D PG 21, SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END AND FABRICATED ANGLE DOUBLERS (AL7075-T6 0.032) (2EA) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLERS IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 51-1-20D PG 9. TORQUED NUTS IAW SRM 51-3-1 PG 2A. 2L74 4F RT4A25 20050325000612005032500061WP 2005 3 25 DHL2005805512 120050223A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 LEFT OUTER WING INBOARD L/E UPPER FORMER CRACKED 0.500 XFS 591.500. REMOVED FASTENERS IAW SRM 51-1-20D PG 21. PERFORMED STOP DRILL ON CRACK END AND FABRICATED ANGLE DOUBLERS (2EA) (AL7075-T6 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLERS (2EA) IAW SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. TORQUED IAW SRM 51-3-1 PG 2A. 2L74 4F RT4A25 20050325000622005032500062WP 2005 3 25 DHL2005805516 120050210A57403645611U BRACKET DOUG DC8 DC873F 302199FWP BOOST PUMP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 NR 1 ALT TANK BOOSTER PUMP BRACKET CRACKED (AFT SIDE). REMOVED AND REPLACED NR 1 ALT TANK BOOSTER PUMP BRACKET IAW SRM 51-1-20D PG 21-9. TORQUED IAW SRM 51-3-1 TABLE II. 2L74 4F RT4A25 20050325000632005032500063WP 2005 3 25 DHL2005805517 120050305A561059124152 PANEL DOUG DC8 DC873F 302199FWP COCKPIT WINDOW CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 FLT COMPT RT UPPER WINDOW OUTER PANEL CRACKED. REMOVED CRACKED RT UPPER WINDOW OUTER PANEL IAW SRM 51-3-0 PG 1. INSTALLED NEW OUTER PANEL WITH NEW FASTENERS IAW SRM 51-3-0 PG 1. TORQUED IAW MM 56-10-4 PG 203. 2L74 4F RT4A25 20050325000662005032500066EA 2005 3 25 COMA0560198 120050322A5210 ROD CNDAIRCL600 CL6002B19 1900309EA DOOR BELLCRANK MISINSTALLED A COMAA UNSCHED LANDING JW WARNING INDICATION INADEQUATE Q C CLCLIMB 1 SO01739CA 7273 FLIGHT 5003 CABIN DOOR OUTER HANDLE CAUTION. DOOR INTERNAL BELLCRANK RODS INSTALLED INCORRECTLY. REINSTALLED CONTROL RODS IAW MM. 2L72 4F RTA21EA 20050325000682005032500068NE 2005 3 25 MALA050287 220050321A7200 ENGINE BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE NR 2 LEAKING A MALAA UNSCHED LANDING KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL15529XJ E2363 IN CRUISE MEM - JAX 24,000 FT THICK HEAVY SMOKE (PETROLEUM BASE ODOR) IN THE FLIGHT DECK/CABIN. NO WARNINGS IN THE FLIGHT DECK LEADING UP TO THE EVENT. EMERGENCY DECLARED AND FLIGHT 3632 DIVERTED TO ASN. LANDED WITHOUT FURTHER INCIDENT. POST FLIGHT CREW NOTED NR 2 ENGINE HAD A MASSIVE OIL LEAK ON THE GROUND. NO FURTHER INFORMATION AT THIS TIME. 2H74 4F4 FRTA49EU E6NE 20050325000692005032500069EU 2005 3 25 MALA050289 120050312A5510 SKIN BAC 146 AVRO146RJ85A1500097EU HORIZONTAL STAB ERODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15502XJ E2307 FAA FINDING BOTH LANDING HORIZONTAL STAB LEADING EDGES HAVE EROSION DAMAGE. NO FURTHER INFORMATION AT THIS TIME. 2H74 4F RTA49EU 20050325000702005032500070EU 2005 3 25 MALA050288 120050312A5343 ATTACH FITTING BAC 146 AVRO146RJ85A1500097EU MLG FAILED A MALAK NONE O OTHER ININSP/MAINT 1 GL15502XJ E2307 MLG SIDE STAY ATTACHMENT BEAM FAILED NDT AS PER SSI 53-20-171 (ALL FOUR LOCATIONS). NO FURTHER INFORMATION AT THIS TIME. 2H74 4F RTA49EU 20050325000742005032500074WP 2005 3 25 DHL2005805515 120050308A5347 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT NR 6 TRACK LUGS WORN AT STA 240.000. CUT OUT NR 6 TRACK DAMAGED SEGMENT IAW SRM 53-2-3 PG 17-19. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PLUG AND CHANNEL IAW SRM 51-3-0 PG 1-2. 2L74 4F RT4A25 20050325000752005032500075NM 2005 3 25 05FDEA00606 120050318A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 REPAIR AT EXTERNAL DOUBLER BS 1304 TO BS 1320 BETWEEN STR 16R TO STR 18R, 16 INCHES BY 9 INCHES NEEDS EVALUATION TO DETERMINE PER SRM OR APPROVED DATA. *S/D* FOUND DOUBLER NOT TO BE DONE PER SRM, REPLACED DOUBLER PER SRM 53-30-3 FIG 3. 2L73 4F RTA3WE 20050325000762005032500076NM 2005 3 25 05FDEA00607 120050318A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 REPAIR AT EXTERNAL DOUBLER BS 300 TO BS 308, RBL 41, WL 170, 8 INCHES BY 6 INCHES NEED EVALUATION TO DETERMINE PER SRM OR APPROVED DATA. *S/D* INSTALLED REPAIR DOUBLER PER SRM 53-30-3. 2L73 4F RTA3WE 20050325000782005032500078WP 2005 3 25 05FDEA00609 120050321A5330 SKIN DOUG DC10 DC1010 3022110WP FUSELAGE DAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25571FE 47830 DURING INSPECTION FOUND EXISTING REPAIR ON LOWER SKIN FUSELAGE AT STA 840-839 LONG 51-52. REMOVED EXISTING REPAIR PER SRM 53-20-00. PERFORMED NEW REPAIR PER SRM 53-20-00 FIG 6 SHEET 3. 2L73 4F A22WE 20050325000802005032500080WP 2005 3 25 DHL2005805520 120050310A534774529523 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE DETERIORATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT NR 1 TRACK PLUG DETERIORATED AT STA 320.000. REMOVED DETERIORATED NR 1 TRACK PLUG IAW SRM 51-3-0 PG 1-2. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW TRACK PLUG IAW SRM 51-3-0 PG 1-2. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050325000822005032500082NM 2005 3 25 DHL2005781562 120050303A5712 RIB BOEING727 727227 1384078NM NR 6 SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A C-CHECK, RT WING NR 6 SLAT I/B RIB AT ACTUATOR ROD ATTACH POINT IS CRACKED. REMOVED DAMAGED RIB IAW B727 SRM 51-30-2, FABRICATED NEW RIB, MATERIAL USED 2024 T3, .040 PO 9002012 DIM15 X 5.5 INCH IAW B727 SRM 57-50-2 FIG 2 AND 51-20-1 FIG 7. ALODINE AND PRIMED RIB AND AREA IAW B727 SRM 51-10-2. INSTALLED NEW RIB AT RIGHT WING NR 6 SLAT IAW B727 SRM 51-30-2, OPS CHECK/LEAK CHECK GOOD IAW B727 MM 27-81-00. LATE ENTRY, REMOVAL AND REINSTALLATION OF NR 6 SLAT ACTUATOR IS DOCUMENTED ON THE BACK OF NON-ROUTINE 95554 REINSTALLED NR 6 SLAT IAW B727 MM 27-81-11, ALL CHECK GOOD. 2L73 4F A3WE 20050325000832005032500083WP 2005 3 25 DHL2005805514 120050308A5347 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT NR 7 TRACK LUGS WORN AT STA 250.000. CUT OUT NR 7 TRACK DAMAGED SECTION IAW SRM 53-2-3 PG 17-19. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW TRACK PLUG AND CHANNEL IAW SRM 51-3-0 PG 1-2. 2L74 4F RT4A25 20050325000842005032500084WP 2005 3 25 DHL2005805519 120050310A534774529523 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT NR 1 TRACK PLUG DETERIORATED AT STA 260.000. REMOVED DAMAGED TRACK PLUG IAW SRM 51-3-0 PG 1-2. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW TRACK PLUG IAW SRM 51-3-0 PG 1-2. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050325000852005032500085WP 2005 3 25 DHL2005805522 120050316A53404751625U1 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT AFT FITTING CRACKED 4.000, STA 680.000 L-11R. REMOVED CRACKED AFT FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9. TORQUED IAW SRM 51-3-1 PG 2A. INSTALLED PLI WASHER (NEW) IAW SRM 51-1-23 (STA 680.000 L-11R). 2L74 4F RT4A25 20050325000882005032500088EA 2005 3 25 COMA0560199 120050321A5610NP1393225 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A COMAO OTHER O OTHER CRCRUISE 1 SO01528CA4439 7841 FLIGHT 5380 PILOTS SIDE WINDOW CRACKED. REPLACED PILOTS SIDE WINDOW. 2L72 4F RTA21EA 20050325000912005032500091NM 2005 3 25 SWAA050869 120050321A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29607SW 27927 DURING SCHEDULED D-CHECK, FOUND 2 EA SHEAR TIES CORRODED AT BS 767, RBL 8 & BS 787, RBL 10 TO LBL 8. REPAIRED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20050325000922005032500092NM 2005 3 25 SWAA050870 120050321A53116520722 FRAME BOEING737 7373Q8 1384670NM FWD CARGO CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND FWD CARGO COMPARTMENT CUTOUT FRAME CRACKED AT BS 490, RBL 37, WL 158. REPAIRED FRAME PER PAE ER. 2L72 4F RTA16WE 20050325000932005032500093NM 2005 3 25 SWAA050871 120050321A5315141A5170 FLOORBEAM BOEING737 7373Q8 1384670NM COCKPIT CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND COCKPIT FLOORBEAM UPPER CHORD CORRODED AT BS 260, BETWEEN RBL 2 TO LBL 9, WL 200. REPAIRED FLOORBEAM PER PAE ER & SRM. 2L72 4F RTA16WE 20050325000962005032500096NM 2005 3 25 05FDEA00515 120050315A5320 WEB BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 BS 760, RBL 61, WL 206 FLOOR SUPPORT WEB IS CRACKED. *S/D* REPAIRED PER SRM 51-40-2. 2L73 4F RTA3WE 20050325000982005032500098NM 2005 3 25 05FDEA00517 120050315A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 FRAME IS CRACKED AT BS 620, LBL 8, WL 157. REMOVED EXISTING REPAIR, FABRICATED DOUBLER, SHEAR TIE AND INSTALLED DOUBLER, AND SHEAR TIE. IAW SRM 53-10-4. 2L73 4F RTA3WE 20050325000992005032500099WP 2005 3 25 05FDEA00518 120050315A5347NFA602247 SEAT TRACK DOUG DC10 DC1010 3022110WP ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO251006048733 46970 CABIN SEAT TRACK -B- CORRODED BETWEEN FUSELAGE STATION 1850 - 1879. REMOVED AND REPLACED SEAT TRACK SECTION IAW DC10 SRM 53-70-00 VOL I AND 51-31-01 VOL 2. 2L73 4F A22WE 20050325001002005032500100EA 2005 3 25 SWIA200514734 120050318A5210 DOOR CNDAIRCL600 CL6002C10 1390015EA MAIN PAX BINDING A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07703SK 10139 MAIN CABIN DOOR IS DIFFICULT TO OPEN FROM INSIDE. LUBED CABIN DOOR. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050325001042005032500104EA 2005 3 25 COMA0560196 120050321A3230750005000 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA MLG MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01976CA21752 7151 FLIGHT 5908 MLG DID NOT EXTEND WHEN L/G SELECTED DOWN. REPLACED THE MLG SELECTOR VALVE. 2L72 4F RTA21EA 20050325001062005032500106NM 2005 3 25 SWAA050767 120050312A3350101114 LIGHT BOEING737 7375H4 138449DNM EMERGENCY EXIT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29503SW 24180 DURING SCHEDULED SERVICE CHECK, FOUND LT FORWARD EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM. 2L72 4F RTA16WE 20050325001102005032500110NM 2005 3 25 SWAA050768 120050313A53226546546 SHEAR TIE BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29686SW 23175 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 787, STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050325001112005032500111CE 2005 3 25 DXTA200500615 120050303A2121BC61A9012 BLOWER CESSNA500 560CESSNA 2076750CE CABIN ODOR E DXTAB EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL07354QS7 5600356 SAW AND SMELLED SMOKE COMING FROM THE AFT CABIN. THIS HAPPENED DURING FLIGHT AT APPROX 1600 FEET ABOVE THE GROUND, MANUVERING TO LAND. T/S SYSTEM, OPS CHECKED OVERHEAD BLOWER, NO SMOKE. NO EVIDENCE OF BINDING. RAN ACFT, TESTED ENVIROMENTAL SYSTEM, NO SMOKE SMELL IN CABIN/COCKPIT, NO SMELL WITH OVERHEAD. REMOVED COALESCER SOCK, NO EVIDENCE OF OIL. REINSTALLED SOCK, THERE IS A SMOKEY SMELL IN TAIL ACCESS AREA. ACCESSED AFT BLOWER MOTOR AT AFT TOLET AREA. REMOVED & INSTALLED NEW ONE. OPS CHECK GOOD. CLOSED ACCESS IAW 560 MM CH 21-21-06. 2L72 4F RTA22CE 20050325001122005032500112CE 2005 3 25 DXTA200500614 120050303A3260NPN UPLOCK SWITCH CESSNA750 750 2076810CE MLG OUT OF ADJUST E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07910QS 7500110 ON TAKEOFF GEAR UNLOCK LIGHT REMAINED ILLUMINATED WHEN GEAR RETRACTED. FOUND UPLOCK SWITCH ON NOSE GEAR OUT OF RIG, MADE ADJUSTMENTS AS NEED. SWUNG GEAR SEVERAL TIMES, OPS CHECK GOOD. RIG OF MLG UPLOCK SWITCHES GOOD IAW CESSNA 750 MM 32-30-05. 2L72 4J RTT00007WI 20050325001132005032500113CE 2005 3 25 DXTA200500612 120050303A3220 LANDING GEAR CESSNA650 650 2076802CE NOSE NOISY E DXTAA UNSCHED LANDING O OTHER CLCLIMB 1 GL07710QS 6507100 AFTER GEAR RETRACTION, AN AUDIBLE THUMP CAN BE HEARD. THIS IS COMING FROM THE NOSE GEAR AREA AND OCCURS ABOUT ONCE EVERY 30 SECONDS. ACCOMPLISHED FERRY FLIGHT INSPECTION TO BTL FOR MAINTENANCE. 2L72 4F A9NM 20050325001142005032500114WP 2005 3 25 DXTA200500613 220050303A73108975131 FUEL FILTER RAYTHNDH125 HAWKER800XP 7150012CE GARRTTTFE731TFE7315BR WP NR 1 ENGINE CLOGGED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07880QS 258570 NR 1 ENG FUEL LIGHT ILLUMINATED AT 60 KTS ON TAKEOFF. REMOVED AND REPLACED NR 1 ENGINE FUEL FILTER IAW HONEYWELL 731 LIGHT MAINTENANCE MANUAL CHAPTER 73-00-00. LEAK AND OPERATIONAL CHECKS SATISFACTORY. 2L72 4F4 FRTA3EU E6WE 20050325001152005032500115NM 2005 3 25 SWAA050769 120050313A53116546546 FRAME BOEING737 737317 138447PNM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29686SW 23175 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO BELTFRAME CORRODED AT BS 887, LBL 1. REPAIRED BELTFRAME PER SRM. 2L72 4F RTA16WE 20050325001182005032500118WP 2005 3 25 05FDEA00500 120050311A5610NBA6045501 WINDSCREEN DOUG DC10 DC1010 3022110WP COCKPIT CRACKED A FDEAA UNSCHED LANDING O OTHER CLCLIMB 1 SO25389FE7036 7036 46623 ON TAKEOFF ROTATION A LOUD POP AND OUTER WINDSCREEN CRACKED, BEFORE LANDING THERE WERE 2 MORE POPS WITH FURTHER CRACKING. REMOVED AND REPLACED L1 WINDOW PER MM 56-11-00-2. OPS CHECK GOOD. ALSO REMOVED AND REPLACED LEFT WINDOW HEAT CONTROLLER PER MM 30-41-01-2, OPS CHECK GOOD. 2L73 4F A22WE 20050325001202005032500120EU 2005 3 25 05FDEA00416 120050308A5322 SHEAR TIE AIRBUS310 A310222 3930315EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 BULK PIT UNDER FLOOR STR 55L FROM FR 65 TO FR 66 HAS CORROSION EXTENDS BETWEEN SPLICE ANGLE AND STR AND UNDER SHEAR TIE AT FR66 REF N00765. REPAIRED STR 55L IAW SRM 53-10-14 AND REMOVED AND REPLACED SPLICE IAW SRM 51-40-21. REMOVED CORROSION IAW SRM 51-74-10, FOUND IN LIMITS. 2L72 4F RTA35EU 20050325001232005032500123EU 2005 3 25 05FDEA00419 120050308A5320 PLATE AIRBUS310 A310222 3930315EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 BULK CARGO DOOR CUTOUT ON LWR FWD TOP EDGE OF SCUFF PLATE SURFACE CORROSION. REMOVED SCUFF PLATE AND REMOVED CORROSION IAW SRM 51-74-10 FOUND IN LIMITS IAW SRM 53-10-00. RESTORED FINISH AND REINSTALLED SCUFF PLATE IAW SRM 53-10-18-4. 2L72 4F RTA35EU 20050325001252005032500125NM 2005 3 25 SWAA050780 120050314A53116516301 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29605SW 27956 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 188, WL 208, LT & RT SIDE. REMOVED AND REPLACED FRAMES PER SRM. 2L72 4F RTA16WE 20050325001282005032500128NM 2005 3 25 SWAA050783 120050314A53106547978 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29607SW 27927 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 370, STR 17L. REMOVED AND REPLACED WEB SECTION PER SRM. 2L72 4F RTA16WE 20050325001292005032500129NM 2005 3 25 SWAA050784 120050314A3350101114 BULB BOEING737 7373H4 1384600NM EMERGENCY LIGHT INSTALLED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29630WN 27705 DURING SCHEDULED C2 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 12. REMOVED AND REPLACED BULB PER MM. 2L72 4F RTA16WE 20050325001312005032500131NM 2005 3 25 SWAA050786 120050314A3350D71702001 BATTERY PACK BOEING737 7377H4 1384404NM AFT GALLEY DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29754SW 29849 DURING SCHEDULED MV1 CHECK, FOUND EMERGENCY EXIT LIGHT BATTERY IN AFT RT GALLEY DISCHARGED. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050325001322005032500132NM 2005 3 25 SWAA050787 120050314A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29655WN 28400 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON SHEAR TIE AT BS 767, BETWEEN STR 26R & STR 27R. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050325001342005032500134NM 2005 3 25 SWAA050789 120050314A5313BAC1498 STRINGER BOEING737 737317 138447PNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29686SW 23175 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON STR 25L, BS 767. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20050325001372005032500137NM 2005 3 25 QXEA200500384 120050119A5310 TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 200 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - AFT FUSELAGE, AFT ENTRY DOOR SURROUND STRUCTURE LOWER AFT LATCH TRACK GOUGES AT STATION 698.000 AND STRINGER 20P. REPAIRED IAW DHC-8 400 SRM 51-14-0-350-803, SRM 51-21-10-380-001, 51-25-10-370-001 AND 51-25-15-370-001. 2H72 4T RTA13NM 20050328000022005032800002SO 2005 3 28 SWIA200514782 120050207A5315 BUTTSTRAP EMB 120 EMB120ER 3260203SO FLOORBEAM CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0758733 120197 BUTTSTRAP CORRODED FROM FR13-RR21 YR 479.00. ITEM FOUND AT C-CHECK INSPECTION. BUTTSTRAP REPLACED IAW EMB 120 SRM 51-40-02, 51-25-00, 51-22-00. 2L72 4T RTA31SO 20050328000052005032800005SO 2005 3 28 SWIA200514785 120050207A2730 ROD EMB 120 EMB120ER 3260203SO ELEVATOR CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0758733 120197 ELEVATOR CONTROL RODS FROM ELEVATOR TO ELEVATOR QUADRANT, ROD ENDS BADLY CORRODED. ITEM FOUND AT C-CHECK INSPECTION. BOTH LEFT AND LOWER RIGHT ELEVATOR TO ELEVATOR QUADRANT ROD ENDS REPLACED IAW AMM 27-31-00. 2L72 4T RTA31SO 20050328000062005032800006SO 2005 3 28 SWIA200514763 120050207A5320 WEB EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0758733 120197 LEFT FLOOR WEB CONNECTING TO OUTBOARD LEFT FLOORBEAM & FRAME 40 IS CORRODED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED WEB IAW SRM 51-40-02, 51-22-00, 51-70-05. 2L72 4T RTA31SO 20050328000102005032800010EA 2005 3 28 COMA0560203 120050324A2613 SENSOR CNDAIRCL600 CL6002B19 1900309EA OVERHEAT MALFUNCTIONED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01812CA 7381 FLIGHT 5443 ABORTED TAKEOFF AT 10 KTS DUE TO LEFT JET OVERHEAT CAUTION, AIRCRAFT RETURNED TO THE GATE. DEFERRED JET OVERHEAT CAUTION PER MEL 16-11-02. 2L72 4F RTA21EA 20050328000132005032800013 2005 3 28 YENA200524 420050322A2565 BOTTLE AIRCRUISERS AIRBUS320 A320232 3930326EU IAE V2500 V2500A1 NE ESCAPE SLIDE DISCHARGED A YENAK NONE O OTHER ININSP/MAINT 1 EA15527JB125713917 A7278 1557 DURING DAILY CHECK FOUND R-2 DOOR SLIDE BOTTLE PRESSURE TO BE LOW AND IN RED. REMOVED AND REPLACED R-2 SLIDE. 2L72 4F4 FRTA28NM E311NE 20050328000152005032800015SO 2005 3 28 SWIA200514772 120050207A5315 FLOORBEAM EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0758733 120197 FLOOR SUPPORT ANGLE CORRODED AT FRAME 38 RT SIDE. (ITEM FOUND AT C-CHECK INSPECTION.) FLOOR SUPPORT REPLACED IAW EMB 120 SRM 51-40-02. 2L72 4T4 TRTA31SO E20NE 20050328000162005032800016SO 2005 3 28 SWIA200514773 120050207A5320 INTERCOSTAL EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE FLOOR SUPPORT CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0758733 120197 CORROSION FOUND ON FLOOR SUPPORT AT FR. 15 L LBL22.(ITEM FOUND AT C-CHECK INSPECTION.) INTERCOSTAL REPLACED IAW SRM 51-40-02, 51-25-00, 51-22-00. 2L72 4T4 TRTA31SO E20NE 20050328000182005032800018SO 2005 3 28 SWIA200514775 120050207A5347 SEAT TRACK EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0758733 120197 RT IB SEAT TRACK AT YR 479.00 FROM FROM 13 TO 32 IS CORRODED IN SEVERAL AREAS. (ITEM FOUND AT C-CHECK INSPECTION.) REPLACED SEAT TRACK IAW EMB 120 SRM 51-40-02, 51-22-00, 51-25-00. 2L72 4T4 TRTA31SO E20NE 20050328000192005032800019SO 2005 3 28 SWIA200514776 120050207A5347 SEAT TRACK EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0758733 120197 SEAT TRACK LT IB AT YL 479.00 FROM FRM 13B TO 32 CORRODED. (ITEM FOUND AT C-CHECK INSPECTION.) INSTALLED NEW SEAT TRACK IAW EMB 120 SRM 51-22-00, 51-40-02. 2L72 4T4 TRTA31SO E20NE 20050328000212005032800021SO 2005 3 28 SWIA200514778 120050207A5320 INTERCOSTAL EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0758733 120197 INTERCOSTAL, FROM 13 FOWARD SIDE AND STR 4L, IS CRACKED. (ITEM FOUND AT C-CHECK INSPECTION.) INSTALLED NEW RIB IAW EMB 120 SRM 51-40-02, 51-25-00, 51-22-00. 2L72 4T4 TRTA31SO E20NE 20050328000222005032800022SO 2005 3 28 SWIA200514779 120050207A5320 INTERCOSTAL EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0758733 120197 INTERCOSTAL AT FRM 13 FORWARD SIDE AND STR 8L IS CRACKED. (ITEM FOUND AT C-CHECK INSPECTION.) CRACKED RIB REPLACED IAW EMB 120 SRM 51-40-02, 51-22-00, 51-25-00. 2L72 4T4 TRTA31SO E20NE 20050328000242005032800024EA 2005 3 28 COMA0560202 120050323A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE THRUST REVERSER ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01494CA 7765 FLIGHT 5084, RECEIVED A LT T/R UNLOCK CAUTION MESSAGE DURING CRUISE FLIGHT, CREW DECLARED AN EMERGENCY AND DIVERTED. AIRCRAFT LANDED WITHOUT INCIDENT. DEFERRED THRUST REVERSER IAW MEL 78-30-01. 2L72 4F4 FRTA21EA E15NE 20050328000252005032800025NM 2005 3 28 05FDEA00618 120050321A5322 SHEAR TIE BOEING727 727200 138407ENM PWA JT8 JT8D9 52048NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 N01607, WHILE WORKING N00929, CORROSION ON SKIN BS 698, FOUND CRACK AND OVERSIZED FASTENER HOLE WITH LIMITED EDGE MARGIN ON SHEAR TIE BS 700 BETWEEN STR 28L AND STR 28R, WL 148. REMOVED AND REPLACED SHEAR TIE IAW SRM 53-10-4. 2L73 4F4 FRTA3WE E2EA 20050328000262005032800026NM 2005 3 28 05FDEA00619 120050321A5322 SHEAR TIE BOEING727 727200 138407ENM PWA JT8 JT8D9 52048NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 N01608 WHILE WORKING N00929, CORROSION ON SKIN BS 698, FOUND CORROSION ON FRAME FORMED SHEAR TIE BS 700 BETWEEN STR 28L TO STR 28R, WL 148. REPAIRED SHEAR TIE PER SRM 53-10-4. 2L73 4F4 FRTA3WE E2EA 20050328000272005032800027NM 2005 3 28 05FDEA00620 120050321A5330 SKIN BOEING727 727200 138407ENM PWA JT8 JT8D9 52048NE FUSLEAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 N01530, REPAIR AT EXTERNAL DOUBLER BS 1195 BETWEEN STR 20R TO STR 22R 12 INCHES BY 9 INCHES NEEDS EVALUATION TO DETERMINE IAW SRM OR APPROVED DATA. REMOVED AND REPLACED DOUBLER IAW SRM 51-30-3 FIG 1. 2L73 4F4 FRTA3WE E2EA 20050328000282005032800028NM 2005 3 28 05FDEA00621 120050321A5210 SKIN BOEING727 727200 138407ENM PWA JT8 JT8D9 52048NE PAX DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 N00261, MAIN ENTRY DOOR EXTERIOR SKIN SHOWS EVIDENCE OF A CRACK AT PREVIOUS REPAIR, 9 INCHES BELOW AFT SIDE OF DOOR HANDLE. INSTALLED REPAIR DOUBLER IAW SRM 52-00-3. 2L73 4F4 FRTA3WE E2EA 20050328000302005032800030 2005 3 28 WRNA200500007 420050324A34174034100901 ADC AIRBUS300 A300B4203 3930306EU UNSERVICEABLE A WRNAA UNSCHED LANDING O OTHER CLCLIMB 1 SO05510TA 100 AFTER TAKEOFF, CAPTAINS AIRSPEED INDICATOR DECREASED TO ZERO (0). CAPTIANS ALTIMETER REMAINED AT 300 FT. DURING CLIMB OUT. AIRCRAFT RETURNED TO AIRPORT, LANDING NORMAL. REMOVED AND REPLACED AIR DATA COMPUTER IAW 34-12-34. OPS AND FUNCTIONAL CHECK SATISFACTORY, AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA35EU 20050328000382005032800038EU 2005 3 28 05FDEA00622 120050321A5347 SEAT TRACK AIRBUS310 A310 EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 MAIN DECK CARGO ZONE 240 LT NR4 SEAT TRACK, FR 54 AND FR 54.1 CORROSION PROPAGATED ON SEAT TRACK FLANGE SCREW HOLES 2-AREAS. BLENDED CORROSION IAW A310-200 SRM 51-74-10, 53-10-16, CHECKED LIMITS AND NOTED FOR MATERIAL LOSS, DUE TO CORROISION OUT OF LIMITS REMOVED AND REPLACED SEAT TRACK IN MAIN DECK CARGO ZONE 240 LT SEAT TRACK AT FR54 AND 54.1 IAW A310-200 SRM 51-72-10. 2L72 4F RTA35EU 20050328000452005032800045EU 2005 3 28 EGI2005F00000 120050226A6230350A31191600 STARFLEX SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE MAIN ROTOR FAILED E EGIAC ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 SW09351EV 2930 STARFLEX ARM FAILED. START PROCEEDED NORMAL UNTIL ABOUT 25-35 PERCENT NG. WHEN A SUDDEN ROTOR IMBALANCE DEVELOPED, IMMEDIATELY PULLED THE THROTTLE BACK AND APPLIED THE ROTOR BRAKE, AT THE SAME TIME, OBSERVED THAT ONE BLADE WAS TRACKING 6 INCHES LOWER THAN THE OTHER TWO BLADES. DURING ENG START, DO NOT RECALL HEARING LOUD BANG THAT ACCOMPANIED FAILURE, AS REPORTED BY OTHERS. UP UNTIL FAILURE, THERE WERE NO DETECTABLE, UNUSUAL NOISES OR VIBRATIONS. DID NOT OBSERVE ANY EXCESSIVE BLADE FLAPPING THOUGH AC DID REACT AS THOUGH MOMENTARILY UNBALANCED. AT HIGHER ROTOR RPM IT WOULD HAVE BEEN VIOLENT, AT LOW RPM, JUST A MOMENTARY SHAKE, LASTING PERHAPS 1 SECOND. (SW09200509152) (K) 1G71 3U3 U H9EU E19EU 20050404001622005040400162EU 2005 4 4 05FDEA00669 120050328A5730 SKIN PANEL AIRBUS310 A310222 3930315EU LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 LEFT WING, LEADING EDGE PANEL LAND, JUST FWD OF FLAP TRACK NR 5 PANEL LAND AND REPAIR CRACKED (MARKED). REMOVED LANDING PLATE IAW A310 SRM 51-40-2, FABBED NEW PLATE IAW DRAWING A572443982, TREATED, PRIMED AND TOPCOATED IAW A310 SRM 51-75-10. REINSTALLED LANDING PLATE IAW A310 SRM 51-75-10 AND 51-40-21 ON LT WING L/E UNDER PANEL 524EB. 2L72 4F RTA35EU 20050404001632005040400163NE 2005 4 4 05FDEA00659 220050328A7261 O-RING DOUG DC10 DC1030 3023501WP GE CF6 CF650C2 30018NE NR 1 ENGINE LEAKING A FDEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO25317FE 46835 NR 1 ENG EXCESSIVE OIL USAGE OR LOSS, AT ENG START HAD 19 QTS AFTER ENGINE START WAS APPROX 17 QTS. AT 1.5 HRS INTO FLT READ 11 QTS AND STILL DROPPING 7 QTS AT TOUCHDOWN 4 HRS 10 MIN TOTAL TIME. REMOVED NR 10 DRIVE ADAPTER, FOUND O-RING SEAL ON IDLER GEAR SECTION BAD. REMOVED AND REPLACED O-RING. INSTALLED ADAPTER PER DC10-30 MM 72-65-00-8. RECHECKED AREA WITH PRESSURE ADAPTER, NO LEAKS NOTED. REMOVED ADAPTER AND REINSTALLED SHAFTS AND COVERS. REINSTALLED GENERATOR PER DC10-30 MM 24-21-04 AND REINSTALLED CSD PER DC 10-30 MM 24-11-09. RAN ENGINE AT HIGH POWER AND RECHECKED DRAINS, NO LEAKS NOTED. 2L73 4F4 F A22WE E23EA 20050404001682005040400168NM 2005 4 4 05FDEA00647 120050326A2750 CONTROL SYSTEM BOEING727 727100 1384036NM TE FLAPS OUT OF ADJUST A FDEAB EMER. DESCENT E VIBRATION/BUFFET CRCRUISE 1 SO25194FE 19143 AIRFRAME VIB INTERMITTENT DURING CLIMB AND CRUISE. IN CLEAN CONFIG NO NOTICEABLE VIB DURING DESCENT OR CONFIG CHANGES FOR LANDING, DURING CRUISE ENG CHANGES AND SPOILER DEPLOYMENT HAD NO EFFECT. FOUND LEFT AND RIGHT TRAILING EDGE FLAP DROOP ADJ OUT OF LIMITS. ADJ ALL FLAPS IN REF B727-100 M/M 27-51-001-5 AND 27-51-011-5, ALL NOW CHECK WITHIN LIMITS. ALSO LUBED AFT FLAP ROLLERS. 2L73 4F RTA3WE 20050404001802005040400180CE 2005 4 4 DXTA200500627 120050313A326067480013 SQUAT SWITCH CESSNA750 750 2076810CE MLG OUT OF ADJUST E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07930QS 7500130 LANDING GEAR WILL NOT COME UP, LANDING GEAR HANDLE STUCK IN DOWN POSITION. INSTALLED NEW SQUAT SWITCH ASSEMBLY AND ADJUSTED IAW C750 MM CHAP 32-05-01, OPS CHECKED GOOD. 2L72 4J RTT00007WI 20050404001852005040400185SO 2005 4 4 SWIA200514769 120050207A5320 BUTTSTRAP EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0758733 120197 CENTER BUTT STRAP AT FRAME 38-44 IS CORRODED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED BUTT STRAP IAW EMB 120 SRM 51-40-02. 2L72 4T RTA31SO 20050404001932005040400193EU 2005 4 4 ASOA05191 120050205A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27633AS 344 DURING A C-CHECK IN YUL, THE INBOARD SEAT TRACKS BETWEEN FRAME 31-31 LEFT/RIGHT WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE INBOARD SEAT TRACKS BETWEEN FRAME 31-32 LT/RT IAW SRM 51-25-04. (M) 2H72 4T RTA53EU 20050404001982005040400198EA 2005 4 4 ASOA05210 120050306A5330 DOUBLER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27824AS 7203 DURING AN A-CHECK IN BTR, THE FS 640 DOUBLER AT STRINGER 10, FRAME FS 640 AND THE SKIN BUTT JOINT STRAP LEFT FS 640, STRINGER 8-13 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FS 640 DOUBLER AT STRINGER 10 AND THE FS 640 FRAME. MAINTENANCE IS REPAIRING THE SKIN BUTT JOINT STRAP LEFT, FS 640, STRINGER 8-13 IAW ASA EO 600-53-0107. (M) 2L72 4F4 FRTA21EA E15NE 20050405000072005040500007WP 2005 4 5 ASAA0580101 120050215A532199365811 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02943AS 53018 OKC - DURING C-CHECK, FOUND PAX CABIN FLOOR PANEL PEELED. FIBERGLASS BOND REPAIRED. (M) 2L72 4F RTA6WE 20050405000122005040500012EA 2005 4 5 ASOA05202 120050305A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27904EV 7628 DURING A C-CHECK IN MCN, THE ENGINE SUPPORT BEAM AT BL 36.20 LEFT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE ENGINE SUPPORT BEAM AT BL 36.20 LEFT IAW ASA EO 600-53-0070. (M) 2L72 4F RTA21EA 20050405000242005040500024WP 2005 4 5 ASAA0580077 120050131A53305910082 SKIN DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - FOUND C-CHECK, FOUND L1 DOOR CUTOUT INNER WEB IS CRACKED. REMOVED DAMAGED AREA. INSTALLED REPAIR FILLER AND DOUBLER. (M) 2L72 4F RTA6WE 20050405000272005040500027WP 2005 4 5 ASAA0580079 120050131A575359304943 SKIN DOUG DC9 DC983 3022083WP TE FLAP GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - FOUND DURING C-CHECK, LEFT WING OUTBOARD FLAP VANE HAS GOUGED ON OUTBOARD EDGE. REMOVED DAMAGED AREA. INSTALLED REPAIR FILLER AND DOUBLER. (M) 2L72 4F RTA6WE 20050405000372005040500037WP 2005 4 5 ASAA0580071 120050131A571299193297 RIB DOUG DC9 DC983 3022083WP WING LE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - DURING C-CHECK, WING LEADING EDGE RIB CRACKED, FROM WS XDS449 TO XDS499. REPLACED RIB. (M) 2L72 4F RTA6WE 20050405000422005040500042WP 2005 4 5 ASAA0580068 120050131A5320993053812 CUSP WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - FOUND DURING C-CHECK, LONGERON CUSP WEB CORRODED IN MID CARGO BAY. REMOVED DAMAGE. INSTALLED FILLER AND REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050405000512005040500051WP 2005 4 5 ASAA0580049 120050131A53219936651505 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - DURING C-CHECK, PAX CABIN FLOOR PANEL HAS BROKEN INSERTS. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050405000562005040500056WP 2005 4 5 ASAA0580065 120050131A532099305386 WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - DURING C-CHECK, LONGERON CUSP WEB CORRODED IN MID CARGO BAY. REMOVED DAMAGE. INSTALLED FILLER AND REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050405000582005040500058WP 2005 4 5 ASAA0580057 120050131A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - DURING C-CHECK, PAX CABIN FLOOR PANEL PUNCTURED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050405000712005040500071EA 2005 4 5 ASOA05204 120050305A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 NM02904EV 7628 DURING A C-CHECK IN MCN, THE CLIPS AT FS 625 LEFT/RIGHT WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CLIPS AT FS 625 LEFT/RIGHT. (M) 2L72 4F RTA21EA 20050405000722005040500072EU 2005 4 5 ASOA05195 120050205A5310 CREASE BEAM AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27633AS 344 DURING A C-CHECK IN YUL, THE CREASE BEAM BETWEEN FRAME 39-40 RT WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CREASE BEAM BETWEEN FRAME 39-40 RT IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20050405000832005040500083EA 2005 4 5 ASOA05209 120050306A5230601R3501153 PLATE CNDAIRCL600 CL6002B19 1900309EA CARGO DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27904EV 7628 DURING A C-CHECK IN MCN, THE CARGO DOOR FLOOR LANDING PLATE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO DOOR FLOOR LANDING PLATE IAW ASA EO 600-53-0117. (M) 2L72 4F RTA21EA 20050405000892005040500089WP 2005 4 5 ASAA0580090 120050207A554259102561 SKIN DOUG DC9 DC983 3022083WP RUDDER DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02960AS 53074 OKC - DURING C-CHECK, FOUND RUDDER T/E IS DELAMINATED. FIBERGLASS BOND REPAIRED. (M) 2L72 4F RTA6WE 20050405000992005040500099WP 2005 4 5 ASAA0580075 120050131A534039364741 SPLICE DOUG DC9 DC983 3022083WP STRINGER CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - DURING C-CHECK, FOUND LONGERON STRINGER SPLICE CORRODED. REPLACED SPLICE. (M) 2L72 4F RTA6WE 20050405001012005040500101EA 2005 4 5 QXEA200500451 120050304A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - RIGHT HAND INBOARD SEAT RAIL AT STATION X461 HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01 AND REO 670-53-00-013. 2L72 4F RTA21EA 20050405001032005040500103EA 2005 4 5 QXEA200500448 120050304A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - RIGHT HAND INBOARD SEAT RAIL AT STATION X363 HAS PITTING CORROSION ON TOP SURFACE. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01 AND REO 670-53-00-013. 2L72 4F RTA21EA 20050405001062005040500106EA 2005 4 5 QXEA200500444 120050304A5210 STRINGER CNDAIRCL600 CL6002C10 1390015EA PAX DOOR CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - PASSENGER DOOR FORWARD SIDE STRINGER CRACKED AT TOP STEP RISER AT STOWAGE BRACKET. REPAIRED IAW REO 670-52-11-102 AND HORIZON AIR EO R-52-228. 2L72 4F RTA21EA 20050405001072005040500107EA 2005 4 5 QXEA200500446 120050303A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - LEFT HAND OUTBOARD SEAT RAIL AT STATION X707 TO X713 HAS PITTING CORROSION ON MOST INBOARD SURFACE. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01 AND HORIZON AIR EO R-53-281. 2L72 4F RTA21EA 20050405001092005040500109EA 2005 4 5 MASA200500055 120050124A3080 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA ANTI ICE SYSTEM ILLUMINATED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07571ML 7209 ASH 2959 YOW TO PHL ABORTED TAKEOFF DUE TO ANTI-ICE DUCT WARNING AND AURAL. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF WING AND COWL ANTI-ICE SYSTEMS. OPS CHK GOOD. 2L72 4F RTA21EA 20050405001222005040500122EA 2005 4 5 VTZA200500024 120050328A5320601R35031239 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27657BR 7491 RT FS 621 FLOOR SUPPORT ANGLE IS CRACKED AT 1 INCH IN RADIUS. 2L72 4F RTA21EA 20050405001322005040500132EA 2005 4 5 QXEA200500464 120050303A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - FUSELAGE EXTERNAL BELLY SKIN HAS CHAFFING DAMAGE FROM FAIRING STIFFENER AT FS 974 AND LBL 1. REPAIRED IAW CRJ700 SRM 51-21-16-001-001-A01, HORIZON AIR EA R-53-284 AND REO 670-53-61-155. 2L72 4F RTA21EA 20050405001362005040500136EA 2005 4 5 QXEA200500457 120050303A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - LEFT HAND INBOARD SEAT RAIL AT STATION X616 HAS PITTING CORROSION ON TOP SURFACE. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01 AND HORIZON AIR EA R-53-283. 2L72 4F RTA21EA 20050405001382005040500138EA 2005 4 5 MASA200500034 120050114A212032156222 PRESSURE VALVE CNDAIRCL600 CL6002B19 1900309EA NR 2 NOT OPENED A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW077264V5847 7264 CLOSED/SUP - ASH 6320 PHX TO GJT RETURNED TO FIELD DUE TO THE RIGHT PACK HAVING HIGH PRESSURE WITH ENGINE BLEEDS. 1/14/05 MAINTENANCE REPLACED PRSOV. 2L72 4F RTA21EA 20050405001472005040500147NM 2005 4 5 AWXA200500377 120050310A575465C2660389 SKIN BOEING737 737375 13844BNNM NR 3 SLAT DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 MCN - MAJOR REPAIR - DURING C-05 CHECK, FOUND THE UPPER SURFACE OF THE NR 3 SLAT WEDGE DELAMINATED AT INBOARD END, SLAT STA 14. MAINTENANCE CUTOUT DAMAGE IN UPPER SURFACE OF NR 3 SLAT WEDGE FROM SS 12.25 TO SS 15.25; FABRICATED A CORE FILLER AND DOUBLER; BONDED REPAIR PARTS TO SLAT IAW B737-300 SRM 51-70-10, FIG 16. 2L72 4F RTA16WE 20050405001642005040500164EU 2005 4 5 AALA20050230 120050329A3350 SWITCH AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217062A 474 BOS - EMERGENCY EXIT LIGHT ARM/DISARM SWITCH WHEN IN DISARM POSITION AMBER LIGHT IS NOT ILLUMINATED. RESECURED CANNON PLUG AT EMERGENCY LIGHT ARM/DISARM SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20050405001652005040500165NE 2005 4 5 AALA20050231 220050328A7250 TURBINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE RT ENGINE FAILED A AALAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 SW21298AA 49310 708557 LAX INFLIGHT T1950/28MAR - RIGHT ENGINE CONTAINED TURBINE FAILURE. ENGINE SHUTDOWN. RETURNED TO LAX AND LANDED WITHOUT INCIDENT. REPLACED ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 F A6WE E9NE 20050405001812005040500181NM 2005 4 5 72300051 120050224A5340 STRINGER CLIP BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 1 INCH BY 3 INCH AREA OF CORROSION ON STRINGER CLIP. 2L73 4F4 FRTA3WE E2EA 20050405001932005040500193NM 2005 4 5 72300054 120050224A5320 THRESHOLD BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 SEVERAL AREAS OF CORROSION ON BOTTOM SIDE OF SERVICE DOOR THRESHOLD WEB WITHIN A 7 INCH BY 50 INCH AREA. 2L73 4F4 FRTA3WE E2EA 20050406000012005040600001NM 2005 4 6 DHL2005782553 120050316A5313 STRINGER BOEING727 727227 1384078NM CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 FUSELAGE STRINGER 22R CORRODED BS 441-470. CORROSION ON STR 22R BS 441-470 OUT OF LIMITS IAW 727 SRM 53-10-1 FIG 1. REMOVED STRINGER 22R BS 441-490 IAW 727 SRM 51-30-2. FABBED NEW FROM BAC 1498-142 PO NR 9001078 DIM 48 INCH LONG IAW 727 SRM 53-10-2 FIG 9 NEW STRINGER TREATED PRIMED AND INSTALLED IAW 727 SRM 51-10-2 AND 53-10-3 FIG 1. 2L73 4F A3WE 20050406000052005040600005EU 2005 4 6 SA05036 120050329A5610NP1653134 WINDOW AIRBUSA319 A319112 3930323EU COCKPIT CRACKED A USAAO OTHER O OTHER CRCRUISE 1 EA19705UW19214 929 SAN - FLT 91 - EN-ROUTE PHL - SAN, THE RIGHT REAR COCKPIT WINDOW CRACKED DURING FLIGHT. THE AIRCRAFT CONTINUED TO SAN AND LANDED WITHOUT FURTHER INCIDENT. 2L72 4F RTA28NM 20050406000122005040600012NM 2005 4 6 05FDEA00722 120050331A5315 FLOORBEAM DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CTR CARGO, DOOR ENTRANCE AFT AREA STA 1781 RT MOST OUTBD END LATERAL FLOORBEAM UPPER CAP FOUND CRACK. CARRIED OUT REPAIR IAW FEDEX EA 1-5310-83087. 2L73 4F RTA22WE 20050406000252005040600025NM 2005 4 6 72300066 120050202A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 APPROX 1 INCH BY 3 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050406000412005040600041NM 2005 4 6 05FDEA00296 120050215A5330 SKIN DOUG MD11 MD11 3023602NM ZONE 100 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 STA Y=595 FORWARD OF LONGERON 48R END SPLICE LOWER FUSELAGE SKIN. FOUND WITH A "FIGURE 8" OVERSIZE FASTENER HOLE. 2L73 4F RTA22WE 20050406000462005040600046EA 2005 4 6 QXEA200500472 120050302A5730 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 500 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - LEFT HAND WING LEADING EDGE SKIN HAS CHAFFED MARK FROM LEADING EDGE AT STATION 22. REPAIRED IAW CRJ700 SRM 57-41-01-101-001-A01 AND SRM 51-12-00-001-001-A01. 2L72 4F RTA21EA 20050406000582005040600058EU 2005 4 6 05FDEA00738 120050331A5410A5451526851000 GUSSET AIRBUS310 A310 EU ZONE 400 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 NR 1 PYLON OUTBD SIDE AT RIB 17 ANGLE HAS CORROSION AROUND 4 HOLES. REMOVED AND REPLACED GUSSET IAW A310-200 SRM 51-72-10. 2L72 4F RTA35EU 20050406000662005040600066NM 2005 4 6 72300076 120050117A5320 ANGLE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 1 INCH BY 29 INCH AREA OF CORROSION ON ANGLE. 2L73 4F4 FRTA3WE E2EA 20050406000722005040600072EU 2005 4 6 248232 120050322A2910 SWIVEL SAAB SF340 SF340A 7850100EU HYD TUBE CRACKED A UHLAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL1714XS 340A014 COMPLETE LOSS OF HYDRAULIC PRESSURE AND FLUID AFTER GEAR RETRACTION, HAND PUMPED GEAR DOWN PER QRH. INSPECTED AND FOUND HYDRAULIC SWIVEL TO BE CRACKED. AIRCRAFT WAITING FOR MAINTENANCE. 2L72 4T RTA52EU 20050406000862005040600086NM 2005 4 6 DHL2005782524 120050311A5730 SKIN BOEING727 727227 1384078NM RT WING ROOT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 CRACK IN RT WING ROOT UPPER SKIN LE STA 95. CUT OUT DAMAGED AREA AND FABRICATED FILLER FROM 2024T3 .050 DIM. 7.5 INCH BY 7.5 INCH PO NR 9002012, DOUBLER FROM 2024T3 .040 DIM. 3.7 INCH BY .75 INCH PO NR 9001938 IAW 727 SRM 57-30-4 FIG 5. REPAIR PARTS TREATED AND PRIMED IAW 727 SRM 51-10-2. INSTALLED REPAIR DOUBLER, FILLER, AND SHIMS IAW 727 SRM 57-30-4 FIG 5. 2L73 4F A3WE 20050406000912005040600091EU 2005 4 6 05FDEA00744 120050331A5310A5381293420000 BEAM AIRBUS310 A310 EU ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 MAIN DECK CARGO CLS ADAPTER BETWEEN R1 AND R2 AT FRAME 50 IS CORRODED. REMOVED AND REPLACED BEAM IAW A310-200 SRM 51-72-10. 2L72 4F RTA35EU 20050406000942005040600094EA 2005 4 6 SWIA200514654 120050301A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07928SW 7701 OVERHEAD EMERGENCY LIGHT NEAR LAV IS INOPERATIVE. RELAMPED OVERHEAD EMERGENCY LIGHT IAW CRJ 200 MM33-51-21, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050406000962005040600096SW 2005 4 6 ALGA099280 120050204A6200406310405101 BEARING BELL 407 407 1182206SW MAIN ROTOR ROUGH B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03687AL482 53366 ROUGH, BINDING AND AXIAL PLAY, REPLACED W/NEW. 1G71 3U O H2SW 20050406000992005040600099SW 2005 4 6 ALGA099285 120050204A6200406310405101 BEARING BELL 407 407 1182206SW MAIN ROTOR ROUGH B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03687AL482 53366 ROUGH, BINDING AND AXIAL PLAY, REPLACED W/NEW. 1G71 3U O H2SW 20050406001022005040600102EU 2005 4 6 05FDEA00549 120050315A5347 SEAT TRACK AIRBUS310 A310 EU FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 RT NR 2 SEATRACK FR 54.2, HAS 1 GOUGED AREA ON SCALOPE HOLE. REMOVED DAMAGED SEAT TRACK FITTING AT MDCC SONE 241 RT NR 2 FR 54.2 AND REPLACED WITH NEWS SEAT TRACK FITTING P/N A5381114620000 IAW A310-200 SRM 51-40-21. 2L72 4F RTA35EU 20050406001042005040600104EA 2005 4 6 QXEA200500441 120050301A5210 PANEL CNDAIRCL600 CL6002C10 1390015EA ZONE 800 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - PASSENGER DOOR AFT SIDE OF STAIR AT DOOR PANEL ANGLE IS CRACKED .75 INCH AT ASSIST MOTOR OUTER Z ATTACH. REPAIRED IAW REO 670-52-11-072. 2L72 4F RTA21EA 20050406001062005040600106EA 2005 4 6 QXEA200500438 120050227A1430 RIVET CNDAIRCL600 CL6002C10 1390015EA ZONE 200 LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC -FUSELAGE EXTERIOR HAS LOOSE RIVETS AT FS800 BETWEEN STRINGER 16 RT AND STRINGER 17 RT, AT WING TO BODY FAIRING ATTACH. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20050406001112005040600111NM 2005 4 6 SB05036 120050303A49906984301 PRESSURE SWITCH BOEING737 7373B7 1384580NM APU FAULTY A USAAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CLCLIMB 1 EA19383US 22956 BWI - FLT141 - EN ROUTE FROM DCA TO IND, AT FL270, WITH THE APU POWERING THE NR 2 GENERATOR BUS, THE APU LOW OIL PRESSURE LIGHT ILLUMINATED FOLLOWED BY AN APU AUTO SHUT DOWN. THE NR 2 ENGINE CSD WAS ALREADY ON MEL SO THE FLIGHT DIVERTED TO BWI AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE APU LOW OIL PRESSURE SWITCH. OPERATIONAL CHECK AND LEAK CHECK GOOD. SERVICED APU OIL AS REQUIRED. CLEARED MEL ON NR 2 ENGINE CSD WITH THE REPLACEMENT OF THE NR 2 ENGINE CSD. FLUSHED ALL LINES AND REPLACED SCAVENGE FILTER. OPERATIONAL CHECK AND LEAK CHECK GOOD. 2L72 4F RTA16WE 20050406001142005040600114EA 2005 4 6 SWIA200514645 120050224A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TOTAKEOFF 1 NM07437SW5520 5520 7564 ON THRUST LEVER ADVANCEMENT, RECEIVED "CONFIG SPOILERS" MESSAGE. REPLACED LEFT INBOARD FLIGHT SPOILER PCU IAW 27-62-01, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050406001182005040600118EA 2005 4 6 SWIA200514646 120050223A2750855D10011 SENSOR CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED LDLANDING 1 NM07919SW6582 6582 7657 "FLAPS FAIL" MSG WHEN SELECTING FLAPS OUT OF 0 DEGREES. REMOVED AND REPLACED RIGHT BPSU IAW CRJ27-51-10, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050406001282005040600128NM 2005 4 6 ASAA0540120 120050206A575465C26601389 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU L/E SLAT CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - L/W NR 1 SLAT LOWER L/E SKIN CRACKED. ACCESSED AREA, FABRICATED REPAIR, INSTALLED REPAIR PARTS, CLOSED AREA. (K) 2L72 4F4 FRTA16WE E21EU 20050406001382005040600138NM 2005 4 6 ASAA0540126 120050209A5534655484212 SKATE ANGLE BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU VERTICAL STAB CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02713AS 30161 PAE - VERTICAL STABILIZER SKATE STA 1001-1016, STA 2R-3R IS CHAFED. CHAFED OUT OF LIMITS, FABRICATED AND INSTALLED NEW SKATE. (K) 2L72 4F4 FRTA16WE E21EU 20050406001422005040600142NM 2005 4 6 ASAA0540100 120050204A5320654529623 FLOOR SUPPORT BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - AFT CARGO BAY CORROSION ON NR 3 FLOOR SUPPORT STRAP. REPLACED STRAP. (K) 2L72 4F4 FRTA16WE E21EU 20050406001432005040600143NM 2005 4 6 ASAA0540098 120050204A5755654645262A PANEL BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU NR 4 SPOILER DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - NR 4 SPOILER PANEL LOWER SURFACE HAS GRAVEL DAMAGE. CUT OUT SKIN AND CORE FOR 3 EACH AREAS THAT WERE OUT OF ALLOWABLE LIMITS AND REPAIRED USING HOT BOND IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050406001442005040600144NM 2005 4 6 ASAA0540081 120050203A5320654769010 SUPPORT BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - AFT CARGO BAY CORROSION ON FLOOR -TO-SIDEWALL SUPPORT. REMOVED AND REPLACED. (K) 2L72 4F4 FRTA16WE E21EU 20050406001462005040600146NM 2005 4 6 ASAA0540034 120050116A532069353521 TIE CLIP BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 OKC - STA 460 FRAME TO STRINGER AT 27R TIE CLIP IS CRACKED. REMOVED DAMAGED CLIP, FABRICATED AND INSTALLED REPLACEMENT CLIP IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050406001472005040600147NM 2005 4 6 ASAA0540083 120050203A53206541473297 SHEAR WEB BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE BENT A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - DAMAGED FLOOR SUPPORT SHEAR WEB AT B-STA 500-500A, LBL 36, WL 152. REMOVED AND REPLACED SHEAR WEB AT B-STA 500-500A, LBL36, WL 152. (K) 2L72 4F4 FRTA16WE E21EU 20050406001492005040600149NM 2005 4 6 ASAA0540132 120050209A521065299413 GUIDE ARM BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU PAX DOOR OUT OF ADJUST A ASAAK NONE O OTHER ININSP/MAINT 1 NM02780AS 25112 SEA - MAIN PASSENGER DOOR (L-1) IS VERY DIFFICULT TO CLOSE. REPLACED MAIN ENTRY DOOR GUIDE ARM ROD END AND ADJUSTED IAW AMM. (K) 2L72 4F4 FRTA16WE E21EU 20050406001502005040600150NM 2005 4 6 ASAA0540129 120050207A552265C25746 SKIN BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU LT ELEVATOR PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02709AS 28896 OKC - LT ELEVATOR HAS A SMALL PUNCTURE IN THE UPPER SKIN. COMPLIED WITH A GRAPHITE WET LAY-UP REPAIR IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050406001532005040600153NM 2005 4 6 ASAA0540131 120050211A52306547952960 SKIN BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU AFT CARGO DOOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02713AS 28896 PAE - AFT CARGO DOOR, EXTERNAL SKIN HAS 2EA DENTS AT O/B AFT CORNER AREA. REMOVED AND REPLACED AFT CARGO DOOR SKIN. (K) 2L72 4F4 FRTA16WE E21EU 20050406001552005040600155NM 2005 4 6 ASAA0540114 120050206A5320694147365 SHEAR WEB BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - FWD CARGO BAY SHEAR WEB DAMAGED AT BS 400-420, LBL 23, WL 156. REPLACED SHEAR WEB IAW SRM AND DWG. (K) 2L72 4F4 FRTA16WE E21EU 20050406001562005040600156NM 2005 4 6 ASAA0540046 120050123A575465C2660393 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU L/E SLAT CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 OKC - NR3 SLAT LOWER SKIN CRACKED AT FASTENER OB END .6 INCHES LONG. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050406001572005040600157NM 2005 4 6 ASAA0540050 120050123A551165475281 RIB BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU HORIZ STAB GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 OKC- RT HORIZONTAL STAB T/E NR3 RIB IS GOUGED ON THE OB SIDE. PREPARED AREA, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050406001602005040600160NM 2005 4 6 ASAA0540118 120050206A53226546548 SHEAR TIE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - CORROSION ON SHEAR TIE AT STA 747 RBL 8 TO RBL 13. REMOVED CORRODED SHEAR TIE, FABRICATED SHEAR TIE REPAIR ANGLE AND CLIPS AND INSTALLED. (K) 2L72 4F4 FRTA16WE E21EU 20050406001622005040600162NM 2005 4 6 ASAA0540122 120050206A532069353521 STRINGER CLIP BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - CRACKED STRINGER CLIP. REPLACED AFTER REMOVAL OF DAMAGED (CRACKED) STRINGER CLIP. (K) 2L72 4F4 FRTA16WE E21EU 20050406001662005040600166NM 2005 4 6 ASAA0540124 120050206A5320654961688 SUPPORT ANGLE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - CORROSION ON BULKHEAD SUPPORT ANGLE. REMOVED AND REPLACED. (K) 2L72 4F4 FRTA16WE E21EU 20050406001672005040600167NM 2005 4 6 ASAA0540133 120050219A52446522216120 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU NOSE COMPT DOOR LIGHTNING STRIKEA ASAAK NONE O OTHER ININSP/MAINT 1 NM02784AS 28199 PAE - LIGHTING STRIKE ON NOSE COMPARTMENT DOOR SKIN. REPAIRED LIGHTING STRIKE. (K) 2L72 4F4 FRTA16WE E21EU 20050406001682005040600168NM 2005 4 6 ASAA0510016 120050304A53116546538562 FRAME BOEING737 7372Q8C 138448SNM PWA JT8 JT8D17 52049NE FUSELAGE MISDRILLED A ASAAK NONE W INADEQUATE Q C ININSP/MAINT 1 NM02741AS 21959 OKC - FUSELAGE, STA 597 APPROX RBL 68 CABIN FLOORBEAM HAS MISDRILLED HOLES. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLE, DOUBLER, AND TRIPLER. ORDERED AND INSTALLED LOWER CHORD AND FRAME IAW SRM. (K) 2L72 4F4 F A16WE E2EA 20050406001732005040600173NM 2005 4 6 ASAA0540166 120050310A575465C266877 SKIN BOEING737 7374Q8 138447QNM PWA JT8 JT8D17A 52049NE NR 6 L/E SLAT DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02764AS 25101 PAE - NR 6 SLAT TRAILING EDGE HAS A DENT. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW SRM, REPAIR 21. (K) 2L72 4F4 FRTA16WE E2EA 20050406001762005040600176NM 2005 4 6 ASAA0510015 120050307A533065458001 SKIN BOEING737 7372Q8C 138448SNM PWA JT8 JT8D17 52049NE FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02741AS 21959 OKC - STA 209 UNDER RT FWD FAIRING, SKIN IS GOUGED AT RT AFT CORNER OF CUTOUT FOR DOOR 1103. REMOVED DAMAGE, COMPLIED WITH A HFEC IAW MFG NDT MANUAL, NO DEFECTS WERE NOTED. FABRICATED AND INSTALLED A REPAIR DOUBLER IAW EA. (K) 2L72 4F4 F A16WE E2EA 20050406001782005040600178NM 2005 4 6 ASAA0540156 120050303A532065C335375 SUPPORT BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02791AS 28886 PASSENGER CABIN, FWD GALLEY SUPPORT IS DENTED BS 354, RBL 10, WL 208. REMOVED AND REPLACED SUPPORT. (K) 2L72 4F4 FRTA16WE E21EU 20050407000012005040700001NM 2005 4 7 SWAA050969 120050329A3350PL2230LH00 LIGHT BOEING737 7377H4 1384404NM AFT CABIN DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29703SW 27837 DURING SCHEDULED MV3 CHECK, FOUND AFT CABIN EEPLS STRIP DELAMINATED. REMOVED AND REPLACED EEPLS STRIP PER MM. 2L72 4F RTA16WE 20050407000022005040700002SO 2005 4 7 C2XA05TY030 120050323A555312034100005 FITTING EMB 145 EMB145ER 3260211SO VERTICAL STAB LOOSE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715941 145035 DURING A SCHEDULED C-CHECK INSPECTION, THE NR 1 RUDDER TO VERTICAL STABILIZER LOWER HINGE FITTING ATTACH POINT BUSHING WAS FOUND TO BE MIGRATED AND LOOSE. THE DEFECTIVE BUSHING WAS REMOVED; THE FITTING HOLE WAS DIMENSIONALLY CHECKED AND FOUND TO BE WORN. MAINTENANCE OVERSIZED THE FITTING HOLE AND INSTALLED A NEW BUSHING AS PER THE EXPRESSJET ENGINEERING DOCUMENT EC5540-01034. 2L72 4F RTT00011AT 20050407000032005040700003WP 2005 4 7 ABXA050082 120050321A5310591746311 DOOR FRAME DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23975AX 47512 DOOR JAMB WAS CRACKED AT TOP LEFT STOP AT INBOARD RIVET. REPAIRED DOOR JAMB AT TOP LEFT IAW DC-9 SRM 53-05. 2L72 4F A6WE 20050407000042005040700004NM 2005 4 7 72300138 120050402A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 GOUGED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 APPROX .25 X .5 INCH GOUGE IN STRINGER. 2L73 4F4 FRTA3WE E2EA 20050407000062005040700006NM 2005 4 7 SWAA050955 120050328A3350BR2013 LIGHT BOEING737 7377H4 1384404NM FWD CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29485WN 32473 EEPLS INOP AT ROWS 3 & 4. REPAIRED EEPLS PER MM. 2L72 4F RTA16WE 20050407000092005040700009NM 2005 4 7 SWAA050936 120050328A53206547978 WEB BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29364SW 26575 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE BEADED WEB CRACKED AT BS 663, LBL 31. REPAIRED BEADED WEB PER SRM. 2L72 4F RTA16WE 20050407000142005040700014WP 2005 4 7 ABXA050079 120050321A53305910228187 SKIN DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23975AX 47512 AFT FUSELAGE HAD 7 EXTERNAL SKIN CRACKS FROM CANTED STA 1197 TO 1208, LONGERON 13 LEFT TO LONGERON 14 LEFT. CRACK LENGTHS FROM .5 TO .75 INCHES. REPAIRED AREA IAW DC-9 SRM 53-01 AND 53-10. 2L72 4F A6WE 20050407000162005040700016WP 2005 4 7 ABXA050076 120050321A5347S2914913M24000 CARGO TRACK DOUG DC9 DC941 302207NWP AFT CARGO CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23975AX 47512 CORROSION ON FLOOR TRACK STA 889 TO STA 1072, LEFT SIDE. REMOVED AND REPLACED TRACK IAW DC-9 SRM 51-30-1. 2L72 4F A6WE 20050407000172005040700017WP 2005 4 7 ABXA050077 120050321A53115911448503 FRAME DOUG DC9 DC941 302207NWP FWD CARGO CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23975AX 47512 AFT LOWER SECTION OF FRAME CORRODED FS 503, LONGERON 29 LEFT TO LONGERON 29 RIGHT. REPAIRED FRAME IAW DC-9 SRM 53-03. 2L72 4F A6WE 20050407000192005040700019WP 2005 4 7 ABXA050078 120050321A5415591326227 ATTACH ANGLE DOUG DC9 DC941 302207NWP LT ENG PYLON CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23975AX 47512 NR 1 PYLON UPPER ATTACH ANGLE HAD 1 MISSING FASTENER AND CRACKED AT STA 1056. REPAIRED AREA IAW DC-9 SRM 54-04. 2L72 4F A6WE 20050407000212005040700021NM 2005 4 7 SWAA050935 120050328A53116546539 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29364SW 26575 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, BELOW LT CREASE BEAM WEB. REPAIRED FRAME PER TYPICAL REPAIR. 2L72 4F RTA16WE 20050407000232005040700023SO 2005 4 7 LR7A05039 120050328A5330 SKIN LKHEED382 382G 526414USO FUSELAGE DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 506 4606 DURING SCHEDULED B2 INSPECTION PER JOB CARD HB5301 FOUND CARGO RAMP LOWER SKIN HOLED AT FS 762, RBL 58, WL 146. REPAIRED IAW SRM SMP 583 51-140-12. 2H74 4T A1SO 20050407000262005040700026WP 2005 4 7 ABXA050074 120050330A335060030451 BATTERY DOUG DC9 DC932 3022066WP EMERGENCY LIGHT DISCHARGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23903AX1200 47427 EMERGENCY EXIT LIGHTS FAILED TO REMAIN ON WITH POWER, FAILURE. REMOVED AND REPLACED EMERGENCY LIGHTING POWER SUPPLY IAW DC-9 MM 24-30. OPS CHECKED GOOD. 2L72 4F A6WE 20050407000282005040700028NE 2005 4 7 COMA0560220 220050329A732073664310 COMPUTER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE AVIONICS MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01443CA9386 7539 FLIGHT 5250 FUEL CHANNEL 1 AND 2 FAIL. NO FUEL INDICATION. REPLACED THE FUEL COMPUTER. 2L72 4F4 FRTA21EA E15NE 20050407000292005040700029 2005 4 7 SWAA050953 420050328A256565C168209 HOOK BOEING737 7373H4 1384600NM L1 DOOR GIRT BARLOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29386SW 26601 L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED GIRT BAR HOOK PER MM. 2L72 4F RTA16WE 20050407000322005040700032NM 2005 4 7 SWAA050960 120050329A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29338SW 23960 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 934, STR 25R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050407000342005040700034 2005 4 7 SWAA050962 420050329A256563550 SLIDE BOEING737 7377H4 1384404NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29406WN 27894 DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050407000352005040700035NM 2005 4 7 SWAA050963 120050330A5311BAC1517 FRAME BOEING737 7375H4 138449DNM E/E BAY CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29501SW 24178 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482A, BL 0. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050407000362005040700036NM 2005 4 7 SWAA050964 120050330A52406969854 GUSSET BOEING737 7375H4 138449DNM R1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29501SW 24178 DURING SCHEDULED 1/2D CHECK, FOUND R1 DOOR AFT LOWER GUSSET CRACKED. REMOVED AND REPLACED GUSSET PER SRM & BAC DRAWING. 2L72 4F RTA16WE 20050407000372005040700037NM 2005 4 7 SWAA050965 120050330A52106545768 SKIN BOEING737 7375H4 138449DNM R1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29501SW 24178 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR CUTOUT, AFT LOWER CORNER. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050407000382005040700038NM 2005 4 7 SWAA050966 120050330A53156546804 FLOORBEAM BOEING737 7375H4 138449DNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29501SW 24178 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FLOORBEAM UPPER T-CAP AT BS 986, BETWEEN RBL 45 TO LBL 45. REMOVED AND REPLACED UPPER T-CAP PER TYPICAL REPAIR MANUAL. 2L72 4F RTA16WE 20050407000402005040700040NM 2005 4 7 SWAA050968 120050330A53306545776 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, BETWEEN STR 23R TO STR 24R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050407000412005040700041NM 2005 4 7 72300136 120050323A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A .5 X 1 INCH AREA OF CORROSION ON BOTTOM OF SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050407000432005040700043NM 2005 4 7 AWXA200500382 120050403A3260189929 SENSOR BOEING737 7373G7 1384595NM FUSELAGE FAULTY A AWXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP28154AW 23776 PHX - AIR TURNBACK - AFTER TAKEOFF AT PHX EN ROUTE FOR MKE THE LANDING GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION AND THE TAKEOFF CONFIGURATION WARNING HORN SOUNDED CONTINUOUSLY AFTER THE FLAPS FULLY RETRACTED. TURNED BACK TO PHX AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE FOUND THE AIR SAFETY SENSOR WOULD NOT TEST ON E-11, REPLACED M991 CARD, SENSOR STILL FAILS, REPLACED S106 AIR SAFETY SENSOR SWITCH IAW AMM 32-09-01-401, LANDING GEAR RETRACTION CHECK WAS GOOD. 2L72 4F RTA16WE 20050407000442005040700044NM 2005 4 7 AWXA200500383 120050312A5755654645165A PANEL BOEING737 737375 13844BNNM NR 8 SPOILER DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 MCN - MAJOR REPAIR - DURING C-05 CHECK FOUND THE UPPER SURFACE OF THE NR 8 SPOILER DELAMINATED BETWEEN WS 432 AND WS 434.5. MAINTENANCE REMOVED DELAMINATED AREA OF NR 8 UPPER SURFACE SPOILER SKIN; FABRICATED A FILLER AND DOUBLER; BONDED REPAIR PARTS TO SPOILER IAW B737-300 SRM 51-70-10, FIG 31. 2L72 4F RTA16WE 20050407000482005040700048NM 2005 4 7 72300146 120050207A5311 FRAME BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1.5 X 24 INCH AREA OF CORROSION ON FRAME FLANGE AND WEB. 2L73 4F4 FRTA3WE E2EA 20050407000522005040700052NM 2005 4 7 CALA0500092 120050331A532065C2084468 FLOOR SUPPORT BOEING737 7373T0 1384582NM FUSLEAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717326 23456 INSPECTION FOUND G-1 I/B SUPPORT MOUNT BETWEEN FLOORBEAMS CORRODED AROUND SCREW HOLES AT STA 277-294, RBL 14. A NEW SUPPORT MOUNT WAS INSTALLED IAW SRM 51-40-2. 2L72 4F RTA16WE 20050407000532005040700053NM 2005 4 7 SWAA050937 120050327A3350101073 COVER BOEING737 7373H4 1384600NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 EMERGENCY EXIT LIGHT ASSY MISSING LENS COVER AT ROW 2 ABC. INSTALLED LENS COVER PER MM. 2L72 4F RTA16WE 20050407000562005040700056NM 2005 4 7 SWAA050948 120050328A53116546554 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29605SW 27956 DURING SCHEDULED D-CHECK, FOUND CORROSION ON FUSELAGE FRAME WEB AT BS 847, RBL 20, WL 160. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20050407000612005040700061EA 2005 4 7 VTZA200500038 120050331A5322601R102328 RIB CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAO OTHER O OTHER ININSP/MAINT 1 EA27638BR 7311 RIGHT BATTERY RIB IS CRACKED .750 INCH BETWEEN THE ATTACHING FASTENERS. 2L72 4F RTA21EA 20050407000622005040700062EA 2005 4 7 VTZA200500039 120050331A53116013600131 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27638BR 7311 LEFT FS 640 FRAME DOUBLER IS CRACKED IN RADIUS AT 1 INCH IN LENGTH. 2L72 4F RTA21EA 20050407000652005040700065EA 2005 4 7 VTZA200500032 120050331A5322601R107091 RIB CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27638BR 7311 LEFT BATTERY RIB IS CRACKED 1.5 INCH. 2L72 4F RTA21EA 20050407000662005040700066EA 2005 4 7 VTZA200500034 120050331A53116013600130 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27638BR 7311 RIGHT FS 640 FRAME DOUBLER IS CRACKED IN RADIUS AT 1 INCH IN LENGTH. 2L72 4F RTA21EA 20050407000702005040700070NM 2005 4 7 2005UALA00271 120050331A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29585UA 26709 CABIN FLOORBEAM CAP AT FS 365 RBL 33 CORRODED AT EXISTING REPAIR. DAMAGE TO THE FLOOR BEAM CAUSED BY TYPICAL CORROSION. REMOVED THE EXISTING REPAIR AND FABRICATED NEW T-CAP SPLICED INTO EXISTING TEE CAP. 2L72 4F4 FRTA2NM E17NE 20050407000722005040700072NM 2005 4 7 2005UALA00273 120050330A5340 STRINGER CLIP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29309UA 23670 STRINGER CLIP CRACKED AT STA 787 STRINGER 21 RIGHT. MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPLACED STRINGER CLIP. 2L72 4F4 FRTA16WE E2GL 20050407000732005040700073NM 2005 4 7 CALA0500091 120050330A31500881031006 SOCKET BOEING737 737524 1384721NM GLARESHIELD SHORTED A CALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW2718622 27526 SMOKE WITH A BURNING ODOR BEGAN COMING FROM UNDER THE CAPTAIN'S GLARESHIELD SHORTLY AFTER TAKEOFF FROM MSY. THE AIRCRAFT WAS RETURNED TO MSY WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE CAPTAIN'S AMBER MASTER CAUTION LIGHT SOCKET SHORTED. THE SOCKET WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD. NO SURROUNDING DAMAGE WAS FOUND. 2L72 4F RTA16WE 20050407000792005040700079SO 2005 4 7 C2XA05RI006 120050322A3000C1460092 VALVE EMB 145 EMB145ER 3260211SO NR 2 ENGINE FAILED A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW27149387572 7572 145029 RIC - FLIGHT CREW REPORTED BLEED NR 2 VALVE CLOSED MSG ON EICAS DURING ICE CONDITIONS. CREW PERFORMED AIR RETURN TO RIC. MX PERFORMED TROUBLESHOOTING AND REMOVED AND REPLACED ENGINE NR 2 ANTI-ICE VALVE, ENGINE NR 2 HIGH STAGE PRESS SW AND RELAY K1088. ALL OPERATIONAL CHECKS WERE PERFORMED SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20050407000812005040700081NM 2005 4 7 72300130 120050323A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 3 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050407000822005040700082EA 2005 4 7 VTZA200500030 120050331A5320601R3111387 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27638BR 7311 LEFT 280 VERTICAL ANGLE IS CRACKED AT .5 INCH BETWEEN FASTENERS. 2L72 4F RTA21EA 20050407000842005040700084EA 2005 4 7 COMA0560215 120050331A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01495CA 7774 LEFT HAND 640 FRAME CRACKED. REPAIRED IAW CRJ SRM 51-42-06, 51-42-21, 51-23-00, 51-25-06 AND 51-25-16. 2L72 4F RTA21EA 20050407000852005040700085EA 2005 4 7 COMA0560226 120050402A3150 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA COCKPIT ILLUMINATED A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01798CA 7348 FLIGHT 5464 DURING GO-AROUND DUE TO WIND SHEAR INDICATION, RECEIVED A LANDING GEAR DISAGREE WARNING. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. DFDR DOWNLOAD INDICATED NO OVERSPEED CONFIGURATION. PERFORMED LANDING GEAR EXTENSION AND RETRACTION CHECKS, DISCREPANCY COULD NOT BE DUPLICATED. 2L72 4F RTA21EA 20050407000862005040700086NM 2005 4 7 2005UALA00274 120050330A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE WORN A UALAK NONE O OTHER ININSP/MAINT 1 WP29308UA 23669 UPPER FUSELAGE SKIN WORN AT STA 868 AT LBL 5 INCHES FROM DORSAL FIN SEAL WEAR. REPAIR STRAPS, FILLERS AND WEAR STRIP INSTALLED EXTERNAL SKIN AT DORSEL FIN SEAL AREA. 2L72 4F4 FRTA16WE E2GL 20050407000882005040700088NM 2005 4 7 SWAA050939 120050327A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29322SW 23343 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 760, STR 24R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050407000902005040700090EA 2005 4 7 SWIA200514812 120050329A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAK NONE O OTHER ININSP/MAINT 1 NM07935SW 7725 CEILING LEVEL EMERGENCY FLOOD ABOVE ROW 2 INOPERATIVE. REPLACED BULB TO EMERGENCY CEILING LIGHTING AT ROW 2 AREA. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050407000912005040700091EA 2005 4 7 SWIA200514813 120050330A5610 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07948SW 7789 RIGHT WINDSHIELD CRACKED. REPLACED RIGHT WINDSHIELD WITH SERVICEABLE WINDSHIELD IAW MM 56-00-00, 56-11-01, 56-12-01. P/N NP139321-12, S/N OFF 02354H3445. 2L72 4F RTA21EA 20050407000922005040700092EA 2005 4 7 SWIA200514814 120050327A2760C13045BA03 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA SPOILERS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07715SK514 514 10179 SSCU 1 FAULT STATUS MESSAGE. INSTALLED A SERVICEABLE SSCU IAW CRJ 700 MM 27-61-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050405000912005040500091EA 2005 4 5 ASOA05218 120050308A5210601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 NM02834AS 7254 FLT 4642 - DURING A GROUND INSPECTION IN ATL, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050405000982005040500098WP 2005 4 5 ASAA0580074 120050131A5320995791811 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - DURING C-CHECK, PAX CABIN FLOOR PANEL HAS TWO CRACKED RIBS ON BOTTOM SIDE. REMOVED DAMAGED. INSTALLED REPAIR HAT SECTIONS AND SPLICES. (M) 2L72 4F RTA6WE 20050405001042005040500104EA 2005 4 5 QXEA200500452 120050304A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - RIGHT HAND INBOARD SEAT RAIL AT STATION X479.5 HAS PITTING CORROSION ON INSIDE SURFACE AROUND SCREW HOLE. REPAIRED IAW CRJ700 51-21-06-001-001-A01 AND REO 670-53-00-013. 2L72 4F RTA21EA 20050405001252005040500125EA 2005 4 5 VTZA200500023 120050328A5320601R35031238 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27657BR 7491 LT FLOOR SUPPORT ANGLE IS CRACKED AT 1 INCH IN RADIUS. 2L72 4F RTA21EA 20050405001262005040500126EA 2005 4 5 VTZA200500019 120050308A5320601R35031238 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSLEAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27708BR 7575 LT FS 621 FLOOR SUPPORT IS CRACKED AT 1 INCH IN RADIUS. 2L72 4F RTA21EA 20050405001312005040500131EA 2005 4 5 QXEA200500466 120050226A5230 VENT CNDAIRCL600 CL6002C10 1390015EA ZONE 800 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - FORWARD CARGO DOOR VENT FLAP HAS TWO GOUGES ON INSIDE FACE. REPAIRED IAW CRJ700 SRM 52-35-06-101-001-A01 AND SRM 51-12-00-001-001-A01. 2L72 4F RTA21EA 20050405001372005040500137NM 2005 4 5 BB05026 120050329A3213161N16254 AXLE BOEING757 7572B7 1384964NM NR 8 WHEEL FRACTURED A USAAO OTHER O OTHER LDLANDING 1 EA19610AU 85EJ43 27122 SJU - FL596 - UPON LANDING, CREW FELT SLIGHT PULL TO THE RIGHT ON ROLL OUT AND TAXI. ON POST-FLIGHT INSPECTION, THE NR 8 WHEEL WAS CANTED. 2L72 4F RTA2NM 20050405001492005040500149WP 2005 4 5 AALA20050222 120050327A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21424AA 49336 LGA - EMERGENCY LIGHTS FROM FIRST CLASS TO ROW 20 INOPERATIVE. REPLACED BATTERY PACK AT SEAT 20DEF FOR EMERGENCY LIGHTS FROM FIRST CLASS TO ROW 20. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050405001582005040500158NM 2005 4 5 72300040 120050114A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 SEVERAL SMALL AREAS OF CORROSION ON BOTTOM OF STRINGER 2L73 4F4 FRTA3WE E2EA 20050405001672005040500167NM 2005 4 5 AALA20050228 120050328A3233162N000135 ACTUATOR BOEING757 757223 1384957NM NLG INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21609AA 27447 SFO INFLIGHT T0392/29MAR - NOSE LANDING GEAR WOULD NOT RETRACT. RETURNED TO SFO AND LANDED WITHOUT INCIDENT. REPLACED PROXIMITY SWITCH ELECTRONIC UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050405001682005040500168NM 2005 4 5 AALA20050227 120050329A3350BPS73 BATTERY PACK BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW2139365 24046 JFK - EMERGENCY LIGHT FROM SEAT ROW 32H TO 40H INOPERATIVE. REPLACED TWO EACH BATTERY PACKS FOR EMERGENCY LIGHTS FROM SEAT ROW 32H TO 40H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050405001752005040500175NM 2005 4 5 UPS05444205 120050313A5347BAC15201890 SEAT TRACK BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 BS 1500-1580 LBL 11 SEAT TRACK FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.045 INCH BY 1 INCH BY 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. SEAT TRACK REPLACED AS PER SRM 51-10-01 P.9 2L74 4F A20WE 20050405001832005040500183NM 2005 4 5 72300053 120050201A5322 ANGLE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 2.5 INCH BY 4 INCH AREA OF CORROSION ON CLOSE OUT ANGLE. 2L73 4F4 FRTA3WE E2EA 20050405001882005040500188NM 2005 4 5 UPS05444207 120050314A534065B38753501 FITTING BOEING747 747121 1384871NM FLOORBEAM CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 M/DECK BS 2020 RBL 60 INCH BELOW FLOORBEAM SUPPORT FTG FOUND CRACKED, CRACK LENGTH 3/4 INCH. M/DECK BS 2020 RBL 60 INCH BELOW FLOORBEAM SUPPORT FTG REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02. 2L74 4F A20WE 20050405001942005040500194EA 2005 4 5 VTZA200500021 120050318A5321601R3501163 FLOOR PANEL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27708BR 7575 CARGO LANDING PLATE IS CRACKED AT RIVETS ATTACHING IT TO THE INTERCOSTALS. 2L72 4F RTA21EA 20050405001972005040500197NM 2005 4 5 05FDEA00691 120050329A5330 SKIN BOEING727 727233 138408ANM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25272FE 22037 EXTERNAL FUSELAGE SKIN GOUGED AT NR 3 CARGO DOOR CUTOUT, BS 1096 AT STR 24R. REPAIRED GOUGE PER FED-EX EA. 7-5330-86272. 2L73 4F RTA3WE 20050405001982005040500198NM 2005 4 5 72300055 120050224A5310 CREASE BEAM BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 SEVERAL AREAS OF CORROSION ON BOTTOM SIDE OF WEB WITHIN A 7 INCH BY 40 INCH AREA. 2L73 4F4 FRTA3WE E2EA 20050406000022005040600002NM 2005 4 6 DHL2005782554 120050316A5313 STRINGER BOEING727 727227 1384078NM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 FUSELAGE STRINGER 23R CORRODED BS 441-470. CORROSION ON STRINGER 23R BS 441 TO BS 470 OUT OF LIMITS IAW B727 SRM 53-10-1 TIS 1. REMOVED STRINGER SECTION 23 R BS 441 TO BS 490 IAW B727 SRM 51-30-2. FABRICATED NEW FROM BAC 1498-142 PO NR 9001078 DIM 48 INCH LONG IAW 727 SRM 53-10-2 FIG 9. NEW STRINGER TREATED AND PRIMED AND INSTALLED IAW B727 SRM 51-10-2 AND 53-10-3 FIG 1. 2L73 4F A3WE 20050406000032005040600003NM 2005 4 6 DHL2005782504 120050314A5530 STRINGER BOEING727 727227 1384078NM VERTICAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 STRINGER 9L CRACKED AT FIN STA 180.6 INSIDE VERTICAL FIN. REMOVED FASTENERS, CUTOUT DAMAGED AREA, FABBED NEW STIFFENER FROM BAC 1517-1367 PO NR 501953 DIM 5 1/2" BY 3", SPLICE FROM AND 10133-1401 PO NR 501952 DIM 19 1/8" BY 2" SPLICE FROM 10134-1201 PO NR 501952 DIM 19 1/8" BY 2" FILLER FROM 7075 T6 .080 PO#9002012 DIM 19 1/8"X 1" FILLER FROM 7075 T6 .100 PO#9911588 DIM 19 1/8"X 3/4 AND CLIP FROM AND 1033-1401 PO NR 501952 DIM 2" BY 2" IAW 727 SRM 55-30-4 FIG 1. REPAIR PARTS TREATED PRIMED AND INSTALLED IAW 727 SRM 51-10-2 AND 55-30-4 FIG 1. 2L73 4F A3WE 20050406000142005040600014NM 2005 4 6 UPS05444212 120050312A5320 SUPPORT BOEING747 747121 1384871NM AFT CARGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 AFT CARGO WALKWAY PANEL SUPPORT FOUND CORRODED BETWEEN BS 1580 AND 1600 RBL 36. CORROSION BLEND OUT 0.030 INCH BY 1 INCH BY 2 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS, WALKWAY PANEL SUPPORT REPAIRED AS PER SRM 51-40-03 FIG 2. 2L74 4F A20WE 20050406000742005040600074EA 2005 4 6 QXEA200500469 120050227A5230 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 200 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - AFT FUSELAGE BAGGAGE BAY DOOR LOWER AFT COWLING GOUGED. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01 AND SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050406000772005040600077EU 2005 4 6 05FDEA00743 120050331A5347 SEAT TRACK AIRBUS310 A310 EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 MAIN CABIN FRAME 61/62, SCALLOPS ARE WORN ON TRACK '0'. REMOVED FLOOR PANELS FOR ACCESS IAW A310-200 SRM 51-40-21. REMOVED AND REPLACED SEAT TRACK SECTION IAW A310-200 SRM 51-72-10 AND 53-10-16. REINSTALLED FLOOR PANELS IAW A310-200 SRM 51-40-21. 2L72 4F RTA35EU 20050406000782005040600078NM 2005 4 6 DHL2005745005 120050322A3260 WARNING LIGHT BOEING727 727224 1384076NM MLG DOOR ILLUMINATED A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01745DH 20665 AFTER GEAR RETRACTION GEAR HANDLE SELECTED TO OFF RED DOOR LIGHT AND AMBER RIGHT GEAR DOOR LIGHT ON SO PANEL ILLUMINATED. COMPLIED WITH ABNORMAL PROCEDURES LIGHT EXTINGUISHED. DEFERRED LANDING GEAR DOOR WARNING SYSTEM PER MEL 31-1 CAT C CONTROL 20202. 2L73 4F A3WE 20050406000812005040600081GL 2005 4 6 C2XA05CL007 220050212A7230 ENGINE EMB 135 EMB135ER 3260203SO ALLSN AE300 AE3007A GL NR 1 LEAKING A C2XAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW2716511138243499 145267 CAE310018 CLE FLIGHT NR 2153, AFTER TAKEOFF, THE CREW SAW AND SMELLED SMOKE AND THE LAV SMOKE ALARM SOUNDED. THE AIRCRAFT RETURNED TO CLE WITHOUT INCIDENT. MAINTEANCE FOUND THE NR 1 ENGINE BLOWING SMOKE INTO THE AIRCRAFT. THE NR 1 ENGINE WAS REMOVED AND REPLACED. THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20050406000832005040600083NM 2005 4 6 TSAA0552009 120050225A5270 WARNING LIGHT BOEING737 737282 13844ATNM CARGO DOOR FALSE INDICATIONA TSAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 WP13824AL 23045 FLT 211, OGG-HNL, FORWARD CARGO DOOR LIGHT CAME ON DURING TAKEOFF ROLL. ABORTED TAKEOFF PRIOR TO 80 KTS. RETURNED TO GATE. MAINTENANCE OPENED AND CLOSED THE FORWARD CARGO DOOR AND CHECKED LOCKS FOR SECURITY. OPS CHECK OK AND LIGHTS CHECK GOOD. IN HNL, FWD CARGO DOOR LIGHT ON T/O. DEFERRED PER MEL 52-3-1, FWD CARGO DOOR LIGHT COMING ON. INSPECTED DOOR AFTER CLOSING. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA16WE 20050406001172005040600117EU 2005 4 6 05FDEA00749 120050331A5310 DOOR FRAME AIRBUS310 A310 EU FUSLAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 AREA BEHIND BULK CARGO BETWEEN FRAMES 72-74 LEFT SIDE AT STRINGER 49 HAS 15 SQ" OF CORROSION. REMOVED CORROSION FR 72-74 FOUND TO BE OUT OF LIMITS IAW A310-200 SRM 53-10-00 FIG 104. REMOVED AND REPLACED STRINGER SECTION 49L FR 72 TO 78 IAW A310-200 SRM 53-10-14. 2L72 4F RTA35EU 20050406001222005040600122NM 2005 4 6 ASAA0540033 120050114A533065457751 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02755AS 25096 PAE - EXTERNAL SKIN DENTED AT BS791, RBL61, WL193, JUST FORWARD OF AFT CARGO DOOR. REPAIRED DENT ON EXTERNAL SKIN B-STA791, RBL 61, WL 193, IAW EA. (K) 2L72 4F4 FRTA16WE E21EU 20050406001262005040600126NM 2005 4 6 ASAA0540075 120050201A5347655384410 CARGO TRACK BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU CARGO BAY CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - CORROSION ON CARGO TRACK, AFT CARGO BAY, BSTA 947-940, WL 156. REMOVED CARGO TRACK AND INSTALLED NEW CARGO TRACK IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050406001322005040600132NM 2005 4 6 ASAA0540093 120050204A5322654655429 SHEAR TIE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - AFT CARGO BAY CORROSION ON SHEAR TIE. REPAIRED SHEAR TIE. (K) 2L72 4F4 FRTA16WE E21EU 20050406001352005040600135NM 2005 4 6 ASAA0540141 120050222A53206517688U180 SILL BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02791AS 28886 PAE - CORROSION ON LT ENTRY DOOR CUTOUT MOPSILL HAS CORROSION FROM BS 303 TO 360, LBL 60, WL 208. REPLACED MOPSILL. (K) 2L72 4F4 FRTA16WE E21EU 20050406001452005040600145NM 2005 4 6 ASAA0540082 120050203A532069457571 SUPPORT BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - AFT CARGO BAY CORROSION ON FLOOR-TO-SIDEWALL SUPPORT. REMOVED AND REPLACED. (K) 2L72 4F4 FRTA16WE E21EU 20050406001582005040600158NM 2005 4 6 ASAA0540115 120050206A5320694147371 SHEAR WEB BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - DAMAGED SHEAR WEB BS 460-480, LBL 36, WL 152. REPLACED SHEAR WEB IAW SRM AND DWG. (K) 2L72 4F4 FRTA16WE E21EU 20050406001592005040600159NM 2005 4 6 ASAA0540116 120050206A5320654795145 SILL BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - AFT CARGO DOOR CUTOUT CENTER SILL PLATE GOUGED. REPLACED GOUGED SILL PLATE WITH NEW IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050406001692005040600169NM 2005 4 6 ASAA0540071 120050131A524265458304 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU E/E BAY DOOR GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02709AS 28896 OKC - E/E COMPARTMENT DOOR OUTER SKIN ON RT AFT SIDE HAS A DENT AND A GOUGE. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050406001742005040600174NM 2005 4 6 ASAA0540030 120050114A521065867845 GUIDE ARM BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU L1 DOOR WORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM02778AS 25110 SEA - L-1 DOOR HARD TO OPEN AND CLOSE. REPLACED UPPER GUIDE ARM. (K) 2L72 4F4 FRTA16WE E21EU 20050406001772005040600177NM 2005 4 6 ASAA0540110 120050206A53226546548110 SHEAR TIE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - CORROSION ON SHEAR TIE AT BS 747, RBL 6 TO LBL 6. REPAIRED SHEAR TIE (FRAME) AT BS 747, RBL 6, LBL6. (K) 2L72 4F4 FRTA16WE E21EU 20050407000102005040700010NM 2005 4 7 SWAA050946 120050328A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29605SW 27956 DURING SCHEDULED D-CHECK, FOUND CORROSION ON 2 EA SHEAR TIES AT BS 787, RBL 2 & RBL 11. REMOVED AND REPLACED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20050407000112005040700011WP 2005 4 7 ABXA050083 120050321A541049125391 SPLICE DOUG DC9 DC941 302207NWP CABIN CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23975AX 47512 INBOARD FRAME FOOT ON AFT SIDE OF LEFT PYLON BULKHEAD WAS CRACKED. REPLACED CRACKED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5. 2L72 4F A6WE 20050407000122005040700012WP 2005 4 7 ABXA050084 120050322A5347S2914913M24000 SEAT TRACK DOUG DC9 DC941 302207NWP CABIN BROKEN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23975AX 47512 SEAT TRACK BROKEN IN UPPER CARGO COMPARTMENT AT FS 1041 AND LEFT BUTT LINE 44.5. SPLICED IN NEW SECTION OF SEAT TRACK AT FS 1041 - 965, LEFT BUTT LINE 44.5 IAW DC-9 SRM 53-05. 2L72 4F A6WE 20050407000202005040700020NM 2005 4 7 SWAA050934 120050328A534065C27314 STRINGER CLIP BOEING737 7375H4 138449DNM AFT CARGO CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29501SW 24178 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727 B, STR 25R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050407000252005040700025WP 2005 4 7 ABXA050080 120050321A531327779225 LONGERON DOUG DC9 DC941 302207NWP CABIN CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23975AX 47512 LONGERON 17 RIGHT CRACKED AT PYLON BULKHEAD. SPLICED IN REPAIR ON LONGERON 17 RIGHT AT PYLON BULKHEAD IAW DC-9 DWG K05864 AND DC-9 SRM. 2L72 4F A6WE 20050407000312005040700031NM 2005 4 7 72300121 120050324A5311 FRAME BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 16 INCH AREA OF CORROSION ON CHORD. 2L73 4F4 FRTA3WE E2EA 20050407000462005040700046NM 2005 4 7 72300144 120050302A5315 FLOORBEAM BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 35 INCH AREA OF CORROSION ON FLOORBEAM FLANGE. 2L73 4F4 FRTA3WE E2EA 20050407000552005040700055NM 2005 4 7 SWAA050947 120050328A53226546560 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29605SW 27956 DURING SCHEDULED D-CHECK, FOUND CORROSION ON SHEAR TIE AT BS 907, RBL 2. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050407000592005040700059NM 2005 4 7 SWAA050956 120050329A53306545766 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29526SW 26568 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 482B + 16, STR 10L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050407000632005040700063EA 2005 4 7 VTZA200500040 120050331A53206013501251 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27638BR 7311 LEFT 624 OBLIQUE ANGLE IS CRACKED AT 1 INCH IN LENGTH. 2L72 4F RTA21EA 20050407000642005040700064EA 2005 4 7 VTZA200500041 120050331A53206013501250 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27638BR 7311 RT OBLIQUE ANGLE IS CRACKED AT 1 INCH IN RADIUS. 2L72 4F RTA21EA 20050407000712005040700071NM 2005 4 7 2005UALA00272 120050330A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29309UA 23670 STA 616 FRAME IS CRACKED BELOW STR 17L. MAJOR REPAIR ACCOMPLISHED. TRIMMED DAMAGE AND INSTALLED REPAIR ANGLE. 2L72 4F4 FRTA16WE E2GL 20050407000742005040700074NM 2005 4 7 72300139 120050402A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 DAMAGED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A .25 X .25 INCH AREA OF DAMAGE ON LOWER LEG OF SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050407000832005040700083NM 2005 4 7 72300141 120050402A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 DAMAGED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A .25 X .25 INCH AREA OF DAMAGE ON VERTICAL FLANGE OF SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050407000872005040700087NM 2005 4 7 SWAA050972 120050330A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 939, BETWEEN STR 21R TO STR 22R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050407000892005040700089EA 2005 4 7 SWIA200514811 120050329A3520 OXYGEN MASK CNDAIRCL600 CL6002B19 1900309EA CABIN DEPLOYED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07445SW 7651 AFTER OPENING MAIN CABIN DOOR, ALL O2 MASKS DEPLOYED. RE-PACKED PASSENGER O2 MASKS IAW AMM 35-21-09. 2L72 4F RTA21EA 20050407000942005040700094EA 2005 4 7 SWIA200514816 120050325A27604916420 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07982SW 7956 FLIGHT SPOILER AND SPOILERONS FAULT STATUS MESSAGE APPEARED AFTER ENGINE START. REMOVED AND REPLACED NR 1 SECU IAW CRJ MM 27-61-05. OPERATIONAL CHECK GOOD. P/N 49-164-06, P/N OFF 49-164-20, S/N ON 01534, S/N OFF 03346. 2L72 4F RTA21EA 20050407000952005040700095SO 2005 4 7 SWIA200514817 120050325A275012064207615 SELECTOR EMB 120 EMB120ER 3260203SO TE FLAP MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED LDLANDING 1 NM07295SW4874 4874 120322 ON FINAL, SELECTED FLAPS 15; GOT CONTROL FAULT. REPLACED FLAP SELECTOR LEVER ASSY. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050407000972005040700097NM 2005 4 7 ASAA0540078 120050202A5322654654987 SHEAR TIE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - CORROSION ON SHEAR TIE B-STA 767, LBL 8.10, WL 146. REMOVED AND REPLACED FRAME SECTION. (K) 2L72 4F4 FRTA16WE E21EU 20050407000982005040700098NM 2005 4 7 ASAA0540080 120050202A57536546430167 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU LT FORE FLAP GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - LT IB FORE FLAP IS GOUGED 44 INCHES FROM IB END, 8 INCHES FROM T/E ON UPPER SURFACE. CUTOUT UPPER SKIN AND CORE (APPROX 56 SQ INCHES) AND REPAIRED WITH HOT BOND IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050407001012005040700101NM 2005 4 7 ASAA0540076 120050202A5320654769017 SUPPORT BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - AFT CARGO BAY CORROSION ON FLOOR TO SIDEWALL SUPPORT. REMOVED CORROSION, FABRICATED REPAIR PARTS AND INSTALLED. (K) 2L72 4F4 FRTA16WE E21EU 20050407001022005040700102NM 2005 4 7 72300142 120050402A5311 FRAME BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CRACKED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 INCH CRACK ON FRAME VERTICAL WEB BY FASTENER LOCATION. 2L73 4F4 FRTA3WE E2EA 20050407001042005040700104NM 2005 4 7 ASAA0540102 120050207A5320654652823 SUPPORT BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - FWD CARGO BAY AREAS OF CORROSION ON FLOOR TO SIDEWALL SUPPORT BS 390 TO 452, LBL 23, WL 156. REMOVED AND REPLACED FLOOR TO SIDEWALL STRAP. (K) 2L72 4F4 FRTA16WE E21EU 20050407001052005040700105EA 2005 4 7 COMA0570034 120050331A27605120011 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA LT WING SPOILER FAULTY A COMAO OTHER J WARNING INDICATION DEDESCENT 1 SO01317CA6850 10055 FLIGHT 5020 DURING DESCENT INTO CVG WHEN FLIGHT SPOILERS WERE DEPLOYED, RECEIVED SPOILERON AND FLIGHT SPOILER CAUTION MESSAGES. CREW DECLARED AN EMERGENCY, AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE RIGHT INBOARD MULTIFUNCTION SPOILER POWER CONTROL UNIT. 2L72 4F RTA21EA 20050407001072005040700107EA 2005 4 7 COMA0570035 120050331A2760 CONTROL SYSTEM CNDAIRCL600 CL6002C10 1390015EA SPOILERS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01317CA 10055 FLIGHT 5020 DURING TPA APPROACH WHEN FLIGHT SPOILERS WERE DEPLOYED, RECEIVED A SPOILERON AND FLIGHT SPOILER CAUTION MESSAGE ON EICAS PRIMARY SCREEN. CREW DECLARED AN EMERGENCY. AIRCRAFT LANDED WITHOUT INCIDENT. PERFORMED A GROUND FUNCTIONAL CHECK OF SPOILERON. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. 2L72 4F RTA21EA 20050407001102005040700110NM 2005 4 7 ASAA0540090 120050203A5320654682827 SHEAR WEB BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - DAMAGED SHEAR WEB. REMOVED AND REPLACED. (K) 2L72 4F4 FRTA16WE E21EU 20050407001112005040700111EA 2005 4 7 COMA0560214 120050331A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01495CA 7774 RIGHT HAND 640 FRAME CRACKED. REPAIRED IAW SRM 51-42-06, 51-42-21, 51-23-00, 51-25-06 AND 51-25-16. 2L72 4F RTA21EA 20050407001132005040700113EA 2005 4 7 COMA0560221 120050331A323046193 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA MLG FAULTY A COMAO OTHER J WARNING INDICATION DEDESCENT 1 SO01959CA22884 7116 FLIGHT 5607 ON APPROACH INTO SAV, RECEIVED A GEAR DISAGREE MASTER WARNING, CREW DELCARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED THE MLG PRIORITY VALVE. 2L72 4F RTA21EA 20050407001142005040700114NM 2005 4 7 ASAA0540105 120050208A5320654659245 FLOOR SUPPORT BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - AFT CARGO BAY AREAS OF CORROSION ON FLOOR SUPPORT JOGGLE FOR NR 3 FLOOR PANEL SUPPORT. REPAIRED IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050407001152005040700115EA 2005 4 7 SWIA200514799 120050316A5340 ATTACH FITTING CNDAIRCL600 CL6002B19 1900309EA FLOORBEAM CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07957SW 7829 ATTACH CLIP AT FS 589.00 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REMOVED ATTACH CLIP ANGLE IAW CRJ SRM 51-40-11 PARA 4, 51-42-21 AND 51-41-02. UPON REMOVAL OF THE ANGLE, NO CRACK FOUND. REINSTALLED ATTACH CLIP ANGLE IAW CRJ SRM 51-40-11 PARA 4, 51-42-21, 51-42-06, 51-23-00, AND 51-25-00. 2L72 4F RTA21EA 20050407001172005040700117NM 2005 4 7 ASAA0540106 120050206A532065514491 SUPPORT ANGLE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - AFT CARGO BAY CORROSION ON (Z) SUPPORT ANGLE, AFT SIDE OF 948 BULKHEAD. REMOVED, FABRICATED AND INSTALLED THE (Z) ANGLE AFTER CORROSION BLENDED OUT OF LIMITS. (K) 2L72 4F4 FRTA16WE E21EU 20050407001202005040700120NM 2005 4 7 ASAA0540079 120050202A531165465497 FAILSAFE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - CORROSION ON FAIL SAFE CHORD. B-STA 767. REMOVED AND REPLACED IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050407001212005040700121NM 2005 4 7 ASAA0540109 120050206A532069457571 FLOOR SUPPORT BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - CORROSION ON FLOOR SUPPORT. REMOVED AND REPLACED. (K) 2L72 4F4 FRTA16WE E21EU 20050407001222005040700122NM 2005 4 7 ASAA0540089 120050203A5320654682827 SHEAR WEB BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - DAMAGED SHEAR WEB. REMOVED AND REPLACED. (K) 2L72 4F4 FRTA16WE E21EU 20050407001232005040700123NM 2005 4 7 ASAA0540104 120050209A5320654769015 SUPPORT BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - FWD CARGO BAY AREAS OF CORROSION ON FLOOR TO SIDEWALL SUPPORT, BS 757 TO 897, LBL23, WL 156. REMOVED AND REPLACED FLOOR TO SIDEWALL STRAP. (K) 2L72 4F4 FRTA16WE E21EU 20050407001242005040700124EA 2005 4 7 SWIA200514802 120050328A3520 OXYGEN MASK CNDAIRCL600 CL6002B19 1900309EA ROW 12CD UNWANTED DEPLOY A SWIAO OTHER O OTHER CRCRUISE 1 NM07929SW 7703 INFLIGHT, ROW 12CD PAX O2 MASKS DROPPED. REINSTALLED O2 MASKS AT ROW 12CD IAW 35-10-00 CRJ AMM. 2L72 4F RTA21EA 20050407001252005040700125EA 2005 4 7 SWIA200514803 120050329A2740 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB INOPERATIVE A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07452SW 7716 CAPTAINS SIDE STAB TRIM SWITCH INOPERATIVE. CAPTAINS SIDE STAB TRIM SWITCH REPLACED IAW AMM TASK 27-41-05-400-801. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050407001262005040700126EA 2005 4 7 COMA0560216 120050329A32304622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG UNRELIABLE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01804CA14296 7352 FLIGHT 5222 GEAR DISAGREE WARNING NLG DID NOT RETRACT. REPLACED THE NLG PRIORITY VALVE. 2L72 4F RTA21EA 20050407001292005040700129NM 2005 4 7 ASAA0540088 120050203A5320654682827 SHEAR WEB BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - DAMAGED SHEAR WEB. REMOVED AND REPLACED. (K) 2L72 4F4 FRTA16WE E21EU 20050407001312005040700131NM 2005 4 7 ASAA0540107 120050209A53206546592503 FLOOR SUPPORT BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - CORROSION AFT CARGO BAY CORROSION AT FLOOR SUPPORT. REPAIRED IAW SRM, FABRICATED AND INSTALLED SPLICE. (K) 2L72 4F4 FRTA16WE E21EU 20050407001322005040700132NM 2005 4 7 AWXA200500394 120050301A532065479573 SILL BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 MCN - MAJOR REPAIR - DURING C-16 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT DOOR SILL WEB BETWEEN BS 794 AND BS 847, RBL 20 AND RBL 28. MAINTENANCE BLENDED OUT CORROSION ON AFT CARGO DOOR SILL WEB FROM BS 794 TO BS 847, RBL 20 TO RBL 28; FABRICATED A 2 EACH FILLERS AND A REPAIR PLATE; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-13. 2L72 4F RTA16WE 20050407001332005040700133NM 2005 4 7 ASAA0540162 120050309A5320654659270 FLOOR SUPPORT BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02794AS 28889 PAE - AFT CARGO BAY, AT PREVIOUS REPAIR, FLOOR SUPPORT CORRODED AND MISSING NUTPLATES UNDER FLOOR SPLICE AT B-STA 771, WL 156, LBL 3. REMOVED CORRODED FLOOR SUPPORT AT PREVIOUS REPAIR, FABRICATED AND INSTALLED REPAIR PARTS. (K) 2L72 4F4 FRTA16WE E21EU 20050407001342005040700134NM 2005 4 7 ASAA0540091 120050203A5320654682830 SHEAR WEB BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - DAMAGED SHEAR WEB. REMOVED AND REPLACED. 2L72 4F4 FRTA16WE E21EU 20050407001352005040700135CE 2005 4 7 DXTA200500603 120050220A3210 LANDING GEAR CESSNA560 560XL 2076702CE MAINS MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07617QS 5605509 AFTER ROTATION, GEAR SELECTED UP, AFTER 3-4 SEC GEAR MADE A CYCLING THUMPING NOISE FOR APPROX 3 SECONDS. RECEIVED A HYD FLOW & A HYD LOW CAUTION LIGHT. CYCLING STOPPED, GEAR LOCKED UP & HYD FLOW LIGHT WENT OUT. KEPT FLAPS AT 15 DEG AND RE-EXTENDED GEAR. HYD PRESS ILLUMINATED, HYD LOW WENT OUT & GEAR EXTENDED. THEN SELECTED FLAPS 35 DEG (170 KIAS) & FLAPS EXTENDED FINE, NO LIGHTS. ONCE ON GROUND, CHECKED GEAR AND GEAR WELLS, NO APPARENT LEAKS. HYD RESERVOIR WAS INDICATING APPROX 3 INCHES BELOW REFILL LINE. SERVICED HYD RESERVOIR. JACKED ACFT FOR GEAR RETRACTION TEST. OPERATED GEAR AND ALL FLIGHT CONTROLS SEVERAL TIMES. FOUND NO DEFECTS. OPS NORMAL. INSPECTED FOR HYD LEAKS, NO LEAKS NOTED. 2L72 4F RTA22CE 20050407001362005040700136NM 2005 4 7 ASAA0540036 120050116A53206547957U3 WEB BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 OKC - AFT CARGO DOOR CUTOUT LOWER SILL WEB IS CORRODED AT B STA 794 TO 847, RBL 20 TO RBL 28. REMOVED DAMAGED WEB, ORDERED AND INSTALLED A NEW WEB IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050407001372005040700137NM 2005 4 7 ASAA0540038 120050118A5755654645165 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU NR 3 SPOILER DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 OKC - NR 3 SPOILER UPPER SKIN IS DELAMINATED IN SEVERAL PLACES. UPON FURTHER INVESTIGATION NO DELAMINATION NOTED, AREAS HOWEVER DENTED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050407001382005040700138NM 2005 4 7 ASAA0540043 120050123A531165465601 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE MISDRILLED A ASAAK NONE W INADEQUATE Q C ININSP/MAINT 1 NM02771AS 25104 OKC - AFT CARGO COMPARTMENT FRAME 947 HAS A MISDRILLED HOLE STRINGER 26 R. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR DOUBLER AND SHIMS IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050407001432005040700143NM 2005 4 7 ASA044409 120050101A53476546813114 SEAT TRACK BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - SEAT TRACK, MECHANICAL DAMAGE STA 360 TO 480, RBL 45, WL208. REPLACED SEAT TRACK. (K) 2L72 4F4 FRTA16WE E21EU 20050407001472005040700147NM 2005 4 7 ASAA0540092 120050204A5320654795711 STRAP BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - AFT CARGO BAY CORROSION ON FLOOR STRAP. REPLACED FLOOR STRAP. (K) 2L72 4F4 FRTA16WE E21EU 20050407001552005040700155NM 2005 4 7 ASAA0540137 120050218A532065476903 SUPPORT BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02791AS 28886 PAE - AFT CARGO BAY, CORROSION ON FLOOR TO SIDEWALL SUPPORT, BS 727 TO BS 727E +10 INCHES, RBL 21, WL 156. REMOVED OUT OF LIMITS CORRODED FLOOR TO SIDEWALL SUPPORT, FABRICATED AND INSTALLED NEW SUPPORT. (K) 2L72 4F4 FRTA16WE E21EU 20050407001602005040700160NM 2005 4 7 ASAA0540123 120050206A53206545833255 COVER BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU COCKPIT CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - FLIGHT DECK MANUAL GEAR EXTENSION COVER CORROSION ON LOWER SURFACE. REMOVED, FABRICATED, AND INSTALLED NEW COVER. (K) 2L72 4F4 FRTA16WE E21EU 20050407001622005040700162NM 2005 4 7 ASAA0540112 120050206A5322143A3010145 SHEAR TIE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - CORROSION ON SHEAR TIE. REMOVED AND REPLACED SHEAR TIE. (K) 2L72 4F4 FRTA16WE E21EU 20050407001642005040700164NM 2005 4 7 ASAA0540117 120050206A532065C264594 FLOOR SUPPORT BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - AFT CARGO BAY, CORROSION ON NR 2 FLOOR SUPPORT STRAP AT BS 727F+7 INCHES, LBL 23 TO RBL23, WL 156. REPLACED NR 2 FLOOR SUPPORT STRAP AT BSTA 727F + 7 INCHES, LBL 23 TO RBL 23, WL 156 IN AFT CARGO BAY. (K) 2L72 4F4 FRTA16WE E21EU 20050407001692005040700169NM 2005 4 7 ASAA0540096 120050204A532265465522 SHEAR TIE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - AFT CARGO BAY CORROSION ON SHEAR TIE (FRAME). REPAIRED SHEAR TIE. (K) 2L72 4F4 FRTA16WE E21EU 20050407001712005040700171WP 2005 4 7 ASAA0580113 120050226A53219936537503 FLOOR PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 OKC HV- CHECK FLOOR PANEL HAS CORRODED FASTENERS. REPLACED FLOOR PANEL. (NM02200500849) (K) 2L72 4F4 FRTA6WE E9NE 20050407001762005040700176WP 2005 4 7 ASAA0580112 120050226A532199365481 CHANNEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FLOOR PANEL DEBONDED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 OKC HV - CHECK - CABIN FLOOR PANEL HAT CHANNEL DISBONDED. BOND REPAIRED. (K) 2L72 4F4 FRTA6WE E9NE 20050407001812005040700181NM 2005 4 7 ASAA0540101 120050204A5320654529624 STRAP BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - CORROSION ON FLOOR STRAP. REPLACED STRAP. (K) 2L72 4F4 FRTA16WE E21EU 20050407001832005040700183NM 2005 4 7 AWXA200500390 120050303A534069432331 ATTACH ANGLE BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 MCN - MAJOR REPAIR - DURING C-16 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT DOOR SILL FORWARD ATTACH ANGLE AT BS 795 BETWEEN RBL 22 AND RBL 26. MAINTENANCE REMOVED CORRODED AFT CARGO DOOR SILL FORWARD ATTACH ANGLE AT BS 795 FROM RBL 22 TO RBL 26; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 69-43233; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050407001852005040700185NM 2005 4 7 AWXA200500392 120050306A5210507845793 SKIN BOEING737 7373G7 1384595NM L-1 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 MCN - MAJOR REPAIR - DURING C-16 CHECK A 1.375 INCH CRACK WAS FOUND IN L-1 DOOR EXTERNAL SKIN AT UPPER HINGE CUTOUT BS 310, STR 14 LT. MAINTENANCE TRIMMED OUT DAMAGE IN L-1 DOOR EXTERNAL SKIN AT UPPER HINGE CUTOUT BS 310, STR 14 LT; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW ER 03-5211-05067-TH1. 2L72 4F RTA16WE 20050407001872005040700187EA 2005 4 7 COMA0560218 120050328A304016591 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA ANTI ICE FAULTY A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01403CA12364 7428 FLIGHT 5244 RECEIVED A WINDSHIELD ANTI ICE CAUTION MESSAGE DURING CRUISE FLIGHT, CREW DECLARED AN EMERGENCY AND DIVERTED TO PIT. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE LEFT WINDSHIELD TEMPERATURE CONTROLLER. 2L72 4F RTA21EA 20050407001892005040700189NM 2005 4 7 CALA0500094 120050402A53476546815127 SEAT TRACK BOEING737 7373T0 1384582NM CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717326 23456 INSPECTION FOUND LEFT I/B SEAT TRACK CORRODED AT STA 916, LBL 24.75. A NEW SECTION OF SEAT TRACK WAS INSTALLED IAW SRM 53-00-52. 2L72 4F RTA16WE 20050407001902005040700190WP 2005 4 7 ASAA0580108 120050215A5230SR09520089 SPACER DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE CARGO DOOR CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02943AS 53018 OKC C-CHECK - AFT CARGO DOOR BEAM VERTICAL SPACER CORRODED. REPLACED BEAM SPACER. (K) 2L72 4F4 FRTA6WE E9NE 20050407001932005040700193NM 2005 4 7 CALA0500096 120050403A3350ADD71701100 BATTERY PACK BOEING737 737724 13844BYNM EMERGENCY LIGHT INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2714731 28799 THE EMERGENCY AILSE LIGHTS AT ROW 15-21 WERE FOUND INOPERATIVE. THE EMERGENCY LIGHT BATTERY PACK WAS REMOVED AND REPLACED. 2L72 4F RTA16WE 20050407001962005040700196 2005 4 7 SWIA200514804 420050328A34183995100208 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STALL PROTECTIONMALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CRCRUISE 1 NM07951SW 7795 STALL FAIL CAUTION MESSAGE ILLUMINATED OUT OF 1000 FT ON DEPARTURE AND REMAINED ON UNTIL LANDING. REMOVED AND REPLACED SPS CONTROL UNIT PER CRJ MM 27-35-01, OPERATIONAL CHECK GOOD. P/N 3995100208, S/N OFF 1047. 2L72 4F RTA21EA 20050407001982005040700198NM 2005 4 7 ASAA0540094 120050204A532265465553 SHEAR TIE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - AFT CARGO BAY CORROSION ON SHEAR TIE. REPLACED DAMAGED SECTION OF SHEAR TIE B-STA 867, LBL 5 TO RBL 5, WL 154, IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050407001992005040700199NM 2005 4 7 AWXA200500393 120050228A531465621251 KEELBEAM BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 MCN - MAJOR REPAIR - DURING C-16 CHECK EXFOLIATION CORROSION AND A 2.125 INCH CRACK WERE FOUND IN KEEL BEAM RT LOWER CHORD AT RBL 6.50, BETWEEN BS 540 AND BS 541. MAINTENANCE CUT OUT DAMAGE IN KEEL BEAM RT LOWER CHORD AT RBL 6.50, FROM BS 540 TO BS 541; FABRICATED A NEW REPLACEMENT SECTION OF KEEL BEAM, 2 EACH FILLERS, A RADIUS FILLER, AND 2 EACH SPLICE ANGLES; INSTALLED REPAIR PARTS IAW ER 03-5369-05071-ES1. 2L72 4F RTA16WE 20050407002002005040700200WP 2005 4 7 ASAA0580118 120050226A53219936651515 FLOOR PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 OKC HV - CHECK - CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (NM02200500849) (K) 2L72 4F4 FRTA6WE E9NE 20050407002022005040700202WP 2005 4 7 ASAA0580117 120050226A532199365821 FLOOR PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 OKC HV- CHECK - CABIN FLOOR PANEL IS WATER DAMAGED AND HAS CORRODED FASTENERS. REPLACED FLOOR PANEL. (NM02200500849) (K) 2L72 4F4 FRTA6WE E9NE 20050407002032005040700203WP 2005 4 7 ASAA0580120 120050226A532199365851 FLOOR PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 OKC HV-CHECK - CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (NM02200500849) (K) 2L72 4F4 FRTA6WE E9NE 20050407002062005040700206WP 2005 4 7 ASAA0580105 120050215A53219936451515 FLOOR PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02943AS 53018 OCK C-CHECK - PAX CABIN FLOOR PANEL PEELED. FIBERGLASS BOND REPAIRED. (NM02200500846) (K) 2L72 4F4 FRTA6WE E9NE 20050407002082005040700208SO 2005 4 7 C2XA05SH022 120050401A5310 DOOR FRAME EMB 145 EMB145LR 3260212SO FUSELAGE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716951 145063 SHV - DURING C-CHECK CRACK FOUND ON STRINGER 14L FR 18 BOTTOM I/B HOLE ON MAIN DOOR FRAME. MAINTENANCE REAMED MAIN DOOR STOP ATTACH HOLE, FR 18 STR 14 BOTTOM I/B PER EC5310-01333. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050407002092005040700209WP 2005 4 7 ASAA0580111 120050226A532199579211 CHANNEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FLOOR PANEL DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 OKC HV-CHECK - CABIN FLOOR PANEL HAT CHANNEL DENTED. REPLACED CHANNEL. (K) 2L72 4F4 FRTA6WE E9NE 20050407002212005040700221NE 2005 4 7 COMA0560229 220050401A7261 CARBON SEAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT ENGINE LEAKING A COMAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO01473CA 7668 FLIGHT 5640 DURING CLIMB OUT OF STL, THE LT ENGINE OIL PRESSURE INDICATED 25-35 PSI, CREW DECLARED AN EMERGENCY, SHUT DOWN THE ENGINE AND DIVERTED TO CVG. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED CARBON SEALS AT AXIS, F, D AND BB. 2L72 4F4 FRTA21EA E15NE 20050407002222005040700222WP 2005 4 7 ASAA0580109 120050215A575359304763 SKIN DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE T/E FLAP GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02943AS 53018 OKC C-CHECK - LT WING T/E FLAP SKIN GOUGED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER. (K) 2L72 4F4 FRTA6WE E9NE 20050407002242005040700224NM 2005 4 7 ASAA0540073 120050130A52306547952259 RETAINER BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU CARGO DOOR DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02756AS 25097 PAE - LOWER AFT SEAL RETAINER ON AFT CARGO BAY DOOR DAMAGED. REMOVED AND REPLACED LOWER AFT SEAL RETAINER ON AFT CARGO BAY DOOR. (K) 2L72 4F4 FRTA16WE E21EU 20050407002252005040700225NM 2005 4 7 ASAA0540035 120050118A5311654655956 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 OKC - AFT CARGO COMPARTMENT STA B 927 FRAME IS CORRODED ON THE UPPER AND LOWER FLANGES, RBL 18 TO RBL 19. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND REPAIR ANGLE IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050407002302005040700230NM 2005 4 7 ASAA0540049 120050123A554465C313931 BALANCE ARM BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU RUDDER DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 OKC - RUDDER BALANCE ARM HAS DAMAGE TO TOP SKIN UPON REMOVAL. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR SKIN SECTION AND DOUBLER IAW AS EA. CRACK-(Y SHAPE 3.7 X 3.75 X 2.75). (K) 2L72 4F4 FRTA16WE E21EU 20050407002322005040700232EA 2005 4 7 SWIA200514818 120050331A2780 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA SLATS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CRCRUISE 1 NM07732SK 10194 SLAT FAULT STATUS MSG APPEARED DURING FLIGHT. REPLACED CTL-22 IAW WDM 27-81-00. OPERATIONAL CHECK GOOD IAW MM 27-81-39. 2L72 4F RTA21EA 20050407002342005040700234SO 2005 4 7 SWIA200514820 120050401A3350 LAMP EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07237SW 120314 EMERGENCY LIGHT OUT, LEFT SIDE 1ST WHITE ONE AT MAIN DOOR. RELAMPED EMERGENCY LIGHT, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050407002352005040700235NM 2005 4 7 F3LA200500002 120050114A2120 SMOKE AIRBUSA319 A319111 3930336NM CABIN DETECTED A F3LAK NONE B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 NM03902FR 1515 AFTER LANDING, FLIGHT CREW REPORTED BOTH COCKPIT AND CABIN FILLED WITH SMOKE. HEAVY BRAKING REQUIRED TO STOP AIRCRAFT ON RUNWAY TO TURN ONTO TAXI-WAY. AFTER STOPPING, BRAKE TEMPS ON LT SIDE APPROX 460 DEG, RT SIDE MID 200 DEG. PERFORMED CLEANING OF CROSSFEED, ENGINE AND APU BLEED AIR DUCTS BY RESIDUAL BURNING PER AMM 21-00-00-160-050. NO SMOKE OR DISCREPANCIES NOTED. INSPECTED BRAKES FOR OVERTEMP PER AMM 05-51-16-200-001. BRAKE TEMPS ON ALL BRAKES WITHIN AMM LIMITS. NO DEFECTS NOTED. TESTED NORMAL BRAKING SYSTEM PER AMM 32-42-00-710-001 AND TESTED ALTERNATE BRAKE SYSTEM PER AMM 32-43-00-710-001. BOTH TESTS CHECKED NORMAL. 2L72 4F RTA28NM 20050407002362005040700236EA 2005 4 7 SWIA200514821 120050403A27604916420 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07982SW 7956 LEFT SPOILERON STATUS & BOTH FLIGHT SPOILER STATUS MESSAGE. REMOVED AND REPLACED NR 2 SECU IAW MM 27-61-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050407002382005040700238NM 2005 4 7 TSAA0527001 120050113A3150 WARNING SYSTEM BOEING737 737282C 13844AUNM COCKPIT MALFUNCTIONED A TSAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP13826AL 23051 FLT 66, LIH-HNL - CONFIGURATION WARNING AT 40 KTS. PUSHED SPEEDBRAKE DOWN AND HORN STILL SOUNDING. ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE COMPLIED WITH THE CONFIGURATION WARNING PARTIAL TEST PER AMM 31-26-0, PAGE 522. ALL TESTS GOOD AND AIRCRAFT APPROVED FOR RETURN TO SERVICE. 2L72 4F RTA16WE 20050407002402005040700240EA 2005 4 7 SWIA200514823 120050329A2760270007 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07956SW 7825 SPOILERON FAULT STATUS MESSAGE DISPLAYED. REPLACED SPOILERON OUTBOARD PCU. OPERATIONAL CHECK GOOD IAW CRJ MM 27-60-00. P/N 27000-7, S/N OFF 7517. 2L72 4F RTA21EA 20050407002422005040700242NM 2005 4 7 72300109 120050323A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 2 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050407002442005040700244NM 2005 4 7 72300111 120050323A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A .75 X 6 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050407002462005040700246NM 2005 4 7 72300113 120050323A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A .5 X .75 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050407002472005040700247EU 2005 4 7 AWXA200500041 120050112A5320D53112087200 FLOOR SUPPORT AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28621AW 053 SAL - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON PASSENGER CABIN LONGITUDINAL FLOOR SUPPORT BEAM Y254 BETWEEN FS 16 AND FS 20. MAINTENANCE CUTOUT DAMAGE IN FLOOR SUPPORT BEAM Y254 FROM FS 16 TO FS 20; FABRICATED A FILLER AND REPAIR ANGLES; INSTALLED REPAIR PARTS IAW A320 SRM 53-11-14, FIG 201. 2L72 4F RTA28NM 20050407002492005040700249NM 2005 4 7 72300116 120050323A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 2 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050407002512005040700251NM 2005 4 7 72300118 120050218A5320 SHEAR WEB BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 SEVERAL AREAS OF CORROSION ON BOTTOM OF SHEAR WEB. 2L73 4F4 FRTA3WE E2EA 20050407002522005040700252EU 2005 4 7 AWXA200500042 120050111A5315D53472794200 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28621AW 053 SAL - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM Y510 AT FS 66 - 2 IN. MAINTENANCE REMOVED DAMAGED FLOORBEAM Y510 AT FS 66 - 2; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050407002542005040700254NM 2005 4 7 72300120 120050324A5311 FRAME BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 5 INCH AREA OF CORROSION ON CHORD. 2L73 4F4 FRTA3WE E2EA 20050407002562005040700256EA 2005 4 7 VTZA200500033 120050331A5343601R536066 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA LT ENGINE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27638BR 7311 LEFT ENGINE SUPPORT BEAM IS CRACKED IN LOWER WEB AT .75 INCH. 2L72 4F RTA21EA 20050405002042005040500204EA 2005 4 5 MASA200500245 120050322A3397 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT LOOSE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0717217 7217 ASH 1732 IN CLT REPORTED SEVERAL SECTIONS OF FLOOR PATH LIGHTING INOP. MAINTENANCE RESET A LOOSE CONNECTOR. OPS CHK GOOD. 2L72 4F RTA21EA 20050406000342005040600034WP 2005 4 6 ARWA20050302 120050318A2797 WIRE DOUG DC8 DC863F 302198FWP TE FLAPS DAMAGED A ARWAD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 SO19906R 46087 WING SLOT LIGHT DID NOT COME ON. REPAIR WIRES 2F MAIN CONNECTOR P1-10 IN ACCORDANCE WITH M/M 20-50-1. PERFORMED OPERATIONAL CHECK IN ACCORDANCE WITH M/M 27-52-3. 2L74 4F 4A25 20050406000472005040600047EA 2005 4 6 QXEA200500514 120050228A5410 ARM CNDAIRCL600 CL6002C10 1390015EA ZONE 400 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - LEFT HAND NACELLE LATCH DOOR HINGE ARMS ARE GOUGED. REPAIRED IAW CRJ700 SRM 51-25-00*-001-001-A01, SRM51-12-00-001-001-A01, AND SRM 54-21-00-101-001-A01. 2L72 4F RTA21EA 20050406000522005040600052NM 2005 4 6 05FDEA00711 120050330A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 MAIN DECK CARGO COMPARTMENT FLOOR TRACK AT STA 635, WL 27, FOUND CRACK APPROXIMATELY THREE (3) INCHES LONG. REPAIR TRACK AND SPLICE FABRICATED AS PER SRM 53-70-00 VOL I, FIG 1 AND INSTALLED PER SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20050406000552005040600055EA 2005 4 6 MASA200500064 120050128A3230750006000 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA NLG DISCHARGED A MASAO OTHER J WARNING INDICATION CLCLIMB 1 SW07271853291 7185 ASH 2725 STL - PHL, HAD A GEAR DISAGREE AFTER TAKEOFF FROM STL. THE CREW CYCLED THE GEAR TO CLEAR THE FAULT IN FLIGHT AND MX REPLACED THE NOSE GEAR SELECTOR VALVE WHEN THE AIRCRAFT ARRIVED IN PHL. 2L72 4F RTA21EA 20050406000762005040600076EU 2005 4 6 05FDEA00742 120050331A5347 SEAT TRACK AIRBUS310 A310 EU CABIN CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 MAIN CABIN FRAME 62 TO 73 SEAT TRACK '0' HAS SEVERAL AREAS OF CORROSION IN ZONE 250. REMOVED AND REPLACED SEAT TRACK FROM FRAME 62 TO FRAME73 IAW A310-200 SRM 51-72-10. 2L72 4F RTA35EU 20050406000792005040600079NM 2005 4 6 2005UALA00247 120050315A5322 SHEAR TIE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29583UA 26705 CORROSION FOUND AT BS 1400 FRAME FROM STR 27L TO 28L AT SHEAR TIE. DAMAGE CAUSED BY TYPICAL CORROSION. SHEAR TIE WAS REMOVED AND A NEW SHEAR TIE WAS FABRICATED AND INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050406000802005040600080SO 2005 4 6 C2XA05TY013 120050207A5532CR32126 RIVET EMB 145 EMB145ER 3260211SO VERTICAL STAB LOOSE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717928 145007 TYS, DURING A SCHEDULE INSPECTION, SMOKING RIVETS WHERE FOUND ON THE BASE OF THE VERTICAL STAB (LEFT AND RIGHT SIDES). MAINTENANCE REMOVED THE OLD RIVETS, FABRICATED AND INSTALLED DOUBLERS, (4 ON EACH SIDE) I/A/W-EC5510-01109, EMB145-SRM-51-40-02, IC2005-145/1502-A AND IC2005-145/0620. 2L72 4F RTT00011AT 20050406000892005040600089NM 2005 4 6 QXEA200500228 120050217A335061047811 BATTERY DHAV DHC8 DHC8202 2809007NM ZONE 200 INOPERATIVE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09358PH980 451 506 SEA - ROW 1 AND ROW 7 CEILING PANEL EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY PACKS 3351-PS1 AND 3352-PS3. NO OTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050406000932005040600093EA 2005 4 6 SWIA200514653 120050228A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED LDLANDING 1 NM07592SW9014 9014 7279 SPOILERON FAULT STATUS MESSAGE UPON LANDING. REPLACED RIGHT OUTBOARD PCU IAW 22-61-05, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050406000952005040600095SW 2005 4 6 ALGA099278 120050204A6200406310405101 BEARING BELL 407 407 1182206SW MAIN ROTOR ROUGH B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03687AL482 53366 ROUGH, BINDING AND AXIAL PLAY, REPLACED W/NEW. 1G71 3U O H2SW 20050406000972005040600097SW 2005 4 6 ALGA099284 120050204A6200406310405101 BEARING BELL 407 407 1182206SW MAIN ROTOR ROUGH B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03687AL482 53366 ROUGH, BINDING AND AXIAL PLAY, REPLACED W/NEW. 1G71 3U O H2SW 20050406001012005040600101SW 2005 4 6 ALGA099804 120050210A6200406310405101 BEARING BELL 407 407 1182206SW MAIN ROTOR WORN B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03XAADL609 53447 BINDING AND AXIAL PLAY BEYOND MAXIMUM LIMITS. REPLACED BY FIELD MAINTENANCE. 1G71 3U O H2SW 20050406001032005040600103NM 2005 4 6 DHL2005782513 120050310A5330 SKIN BOEING727 727227 1384078NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 3 DENTS L/FUSELAGE SKIN AFT OF STA 1342.4 BETWEEN STR 14L AND 13L. CUT OUT DAMAGED 2 EACH SIZE 1 INCH BY 1 INCH AND 1 INCH BY 1 INCH IAW B727 SRM 54-30-1. FABRICATED DOUBLER USING 2024T3 .063 PO NR 9002039 DIM 14 5/8" BY 10 1/4" IAW B727 SRM 54-30-2. ALODINED AND PRIMED PART IAW B727 SRM 51-10-2. INSTALLED DOUBLER IAW B727 SRM 54-30-2. 2L73 4F A3WE 20050406001052005040600105EA 2005 4 6 QXEA200500443 120050304A5210 STRINGER CNDAIRCL600 CL6002C10 1390015EA ZONE 800 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - PASSENGER DOOR AFT SIDE STRINGER CRACKED AT TOP STEP RISER AT HANDRAIL STOWAGE BRACKET. REPAIRED IAW CRJ700 REO 670-52-11-102 AND HORIZON AIR EA R-52-228. 2L72 4F RTA21EA 20050406001072005040600107EA 2005 4 6 QXEA200500439 120050301A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 200 WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - FUSELAGE EXTERIOR AFT BAGGAGE DOOR CUTOUT, HAS WEAR DAMAGE TO AFT SKIN AT FS 1047 WL 88. REPAIRED IAW HORIZON AIR EA R-53-277 AND REO 670-53-61-152. 2L72 4F RTA21EA 20050406001102005040600110EU 2005 4 6 05FDEA00572 120050315A5230 ACCESS PANEL AIRBUS310 A310 EU CARGO DOOR DAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25419FE 345 LOWER FUSELAGE FWD CARGO DOOR ACCESS PANEL NR 811BR HAS (2EA) CRACKS AT FASTENER HOLE. REPLACED WITH NEW ACCESS PANEL DUE TO EXCESSIVE REPAIRS AND PANEL DEFORMATION IAW A310-200 SRM 51-71-30. PAINTED IAW A310 SRM 51-75-10. 2L72 4F RTA35EU 20050406001132005040600113EU 2005 4 6 05FDEA00550 120050315A2150A2151058200000 DOOR AIRBUS310 A310 EU ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 AFTER REMOVAL OF PANEL 143GL ON SNRM N00035, FOUND RAM AIR EXHAUST DOOR SURROUND BOX TO HAVE A 10 INCH CRACK ON INBD SIDE UPPER RADIUS. REMOVED AND REPLACED LT RAM AIR EXHAUST. 2L72 4F RTA35EU 20050406001162005040600116EA 2005 4 6 QXEA200500166 120050119A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - FUSELAGE OUTER SKIN IS NICKED AT STATION 472.5 AND STRINGER 25R. REPAIRED IAW CRJ REO 670-53-21-070 AND HORIZON AIR EA R-53-259. 2L72 4F RTA21EA 20050406001342005040600134NM 2005 4 6 ASAA0540161 120050309A532065558789 SEAL DEPRESSOR BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FWD GALLEY DOOR CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02791AS 28886 PAE - FWD GALLEY DOOR CUTOUT UPPER AFT SEAL DEPRESSOR CRACKED AT 2 PLACES, STA 328, RBL 52, WL 274. REMOVED AND INSTALLED NEW FWD GALLEY DOOR CUTOUT UPPER SEAL DEPRESSOR. (K) 2L72 4F4 FRTA16WE E21EU 20050406001362005040600136NM 2005 4 6 ASAA0540159 120050303A532065C335821 SHEAR WEB BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02791AS 28886 PAE - CORROSION ON SHEAR WEB. BLENDED ON CORROSION, FUND TO BE OUT OF LIMITS, REMOVED AND REPLACED SHEAR WEB. (K) 2L72 4F4 FRTA16WE E21EU 20050406001372005040600137NM 2005 4 6 ASAA0540160 120050302A5322654659320 SHEAR TIE BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02791AS 28886 PAE - FRAME SHEAR TIE CORRODED. CORROSION FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED SHEAR TIE. (K) 2L72 4F4 FRTA16WE E21EU 20050406001482005040600148NM 2005 4 6 ASAA0540154 120050228A532065C1612935 CHANNEL BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU NLG WW CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02784AS 28199 PAE - LT CHANNEL BELOW WXR UNIT IN NOSE BAY CRACKED. REMOVED, FABRICATED AND INSTALLED LT CHANNEL BELOW WXR UNIT IN NOSE BAY. (K) 2L72 4F4 FRTA16WE E21EU 20050406001512005040600151NM 2005 4 6 ASAA0540041 120050121A57536546434 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU T/E FLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 OKC - LT WING IB AFT FLAP LOWER SKIN HAS 2 DENTS TOGETHER, 17 INCHES FROM THE IB EDGE AND 7.5 INCHES FROM THE TE A=5.3, Y=.075, A/Y= 70. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050406001522005040600152NM 2005 4 6 ASAA0540127 120050209A5534655484211 SKATE ANGLE BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU VERTICAL STAB CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02713AS 30161 PAE - VERTICAL STAB SKATE STA 1001-1016, STA 21-31 IS CHAFFED. VERTICAL SKATE CHAFED OUT OF LIMITS, FABRICATED AND INSTALLED NEW SKATE. (K) 2L72 4F4 FRTA16WE E21EU 20050406001612005040600161NM 2005 4 6 ASAA0540048 120050123A575565464525 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU NR 6 SPOILER DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 OKC - NR 6 SPOILER HAS 2 SHARP DENTS IN AREA OF ACTUATOR ATTACH. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050406001702005040600170NM 2005 4 6 ASAA0540072 120050131A52306547952 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU AFT CARGO DOOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02709AS 28896 OKC - AFT CARGO DOOR SKIN HAS A DENT WITH A CREASE 21 INCHES AFT OF THE FWD EDGE AND 38.5 INCH FROM TOP EDGE. REMOVED DAMAGE, FABRICATED AND INSTALLED A DOUBLER IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050407000052005040700005NM 2005 4 7 2005UALA00269 120050329A5315 FLOORBEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29308UA 23669 CABIN FLOORBEAM UPPER SURFACE LIGHT CORROSION AT STA 312 AT RBL 8 WL 208. REPLACED TEE CHORD. 2L72 4F4 FRTA16WE E2GL 20050407000072005040700007NM 2005 4 7 CALA0500090 120050330A5330654577567 SKIN BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714335 23573 A 3 INCH CRACK WAS FOUND IN THE FUSELAGE SKIN DURING WALKAROUND. THE CRACK WAS LOCATED APPROXIMATELY 2.5 FEET FORWARD OF AFT CARGO DOOR AND 2.5 FEET BELOW WATER LINE AND BETWEEN STRINGERS 19R AND 20R (THREE FEET FORWARD OF STA 767). A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-00-01, FIGURE 229. 2L72 4F RTA16WE 20050407000082005040700008 2005 4 7 COMA0560225 420050402A34183995100208 COMPUTER CNDAIRCL600 CL6002B19 1900309EA STALL WARNING FAULTY A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01797CA14800 7344 FLIGHT DURING TAKEOFF ROLL RECEIVED A STALL FAIL CAUTION MESSAGE, AIRCRAFT ABORTED TAKEOFF AND RETURNED TO THE GATE. REPLACED THE STALL PROTECTION COMPUTER. 2L72 4F RTA21EA 20050407000132005040700013WP 2005 4 7 ABXA050085 120050323A5347S2914913M24000 SEAT TRACK DOUG DC9 DC941 302207NWP CABIN CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23975AX 47512 UPPER CARGO LEFT SIDE BUTT LINE 44 HAD FLOOR PANEL BULGED. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK AT STA 973 - 1071, LEFT BUTT LINE 44 ON JOB CARD 0349 IAW DC-9 SRM. 2L72 4F A6WE 20050407000152005040700015WP 2005 4 7 ABXA050075 120050318A534349142571 FITTING DOUG DC9 DC941 302207NWP LT MLG CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23975AX 47512 BRACE FROM UPPER PRESSURE PANEL TO FUSELAGE CRACKED AT BOTTOM BOLT ATTACH POINT 56 INCHES LT BUTTLINE AND 19 INCHES AFT OF MAIN FRAME. REMOVED AND REPLACED BRACE IAW DC-9 SRM. 2L72 4F A6WE 20050407000272005040700027EA 2005 4 7 COMA0560219 120050329A335059465 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DAMAGED A COMAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO01914CA 7012 FLIGHT 5280 FLOOR PATH EMERGENCY LIGHT ARE INOP ROW 1 THRU 5. REPLACED THE POWER CABLE. 2L72 4F RTA21EA 20050407000302005040700030NM 2005 4 7 SWAA050954 120050329A3350207377 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29471WN 32471 FWD END OF EEPLS LENS MISSING. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20050407000332005040700033NM 2005 4 7 SWAA050961 120050329A3350101114 BULB BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29368SW 26579 DURING SCHEDULED C2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050407000392005040700039NM 2005 4 7 SWAA050967 120050330A53306545774 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29511SW 24188 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 18L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050407000452005040700045NM 2005 4 7 AWXA200500384 120050309A53206545409212 WEB BOEING737 737375 13844BNNM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 MCN - MAJOR REPAIR - DURING C-05 CHECK A 1.125 INCH CRACK WAS FOUND IN WEB AT LT MLG WHEEL WELL CEILING BS 664, LBL 32. MAINTENANCE CUT OUT DAMAGED AREA OF WEB AT BS 664, LBL 32; FABRICATED 3 EACH FILLERS, A DOUBLER & STRAP; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-60-51, FIG 203. 2L72 4F RTA16WE 20050407000582005040700058 2005 4 7 SWAA050950 420050328A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29638SW 27711 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. SLIDE DID NOT DEPLOY. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20050407000602005040700060EA 2005 4 7 VTZA200500037 120050331A5320601R3111358 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27638BR 7311 RIGHT 280 VERTICAL ANGLE IS CRACKED AT .5 INCH BETWEEN FASTENERS. 2L72 4F RTA21EA 20050407000672005040700067 2005 4 7 SWAA050970 420050329A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29706SW 27840 DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050407000682005040700068NM 2005 4 7 SWAA050971 120050330A5240MS166254162 RETAINER BOEING737 7377AD 1384502NM R2 DOOR BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29798SW 28436 R2 DOOR WILL NOT OPEN OR CLOSE, STUCK IN MID-POSITION. INSTALLED R2 DOOR HANDLE INNER BEARING RETAINER PER MM. 2L72 4F RTA16WE 20050407000692005040700069NM 2005 4 7 2005UALA00270 120050329A5315 FLOORBEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29308UA 23669 AFT CABIN FLOORBEAM T-CAP HAS CORROSION AT STA 967 LBL 17 TO RBL 12. REPLACED TEE CAP. 2L72 4F4 FRTA16WE E2GL 20050407000762005040700076EA 2005 4 7 SWIA200514797 120050316A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07957SW 7829 LT FLOORBEAM ANGLE AT FS 621.00 IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. CRACKED ANGLE REPAIRED IAW REO 601R-53-61-117 REV B. 2L72 4F RTA21EA 20050407000782005040700078SO 2005 4 7 C2XA05TY031 120050324A532014530642401 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715941 145035 TYS DURING A C-CHECK INSPECTION THE CENTER AISLE SUPPORT STRUCTURE ON THE LEFT SIDE WAS FOUND WITH CORROSION FROM FRAME 20 TO 60. MAINTENANCE REMOVED AND REPLACED THE CENTER OMEGA BEAM ASSEMBLY FROM FR 20 TO 29 AND BLENDED FROM 29 THRU 60 AND WAS FOUND WITHIN LIMITS. AREA WAS ALODINED, PRIMED AND PAINTED. 2L72 4F RTT00011AT 20050407000962005040700096NM 2005 4 7 ASAA0540086 120050203A532265465317 SHEAR TIE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - CORROSION ON SHEAR-TIE AT B-STA 440, LBL 3, WL 148. REPAIRED SHEAR TIE IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050407000992005040700099NM 2005 4 7 72300133 120050323A5330 SKIN BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 THREE AREAS OF CORROSION ON BOTTOM OF SPLICE APPROX 4 X 2 INCH, 6 X 2 INCH AND 6 X 2 INCH. 2L73 4F4 FRTA3WE E2EA 20050407001002005040700100NM 2005 4 7 72300134 120050218A5322 SHEAR WEB BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 SEVERAL AREAS OF CORROSION ON BOTTOM OF SHEAR WEB. 2L73 4F4 FRTA3WE E2EA 20050407001062005040700106NM 2005 4 7 ASAA0540108 120050206A532265C329621 SHEAR TIE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - CORROSION AFT CARGO BAY CORROSION SHEAR TIE AT BS 727G, LBL 17.20 TO RBL 13.8, WL 148. REPAIRED SHEAR TIE IAW SRM AND DWG. (K) 2L72 4F4 FRTA16WE E21EU 20050407001272005040700127NM 2005 4 7 ASAA0540084 120050203A532265465522 SHEAR TIE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - AFT CARGO BAY CORROSION ON SHEAR TIE B-STA 807, LBL5 TO RBL 5, WL 148. REPAIRED IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050407001302005040700130NM 2005 4 7 ASAA0540085 120050203A53226546548110 SHEAR TIE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - CORROSION ON SHEAR TIE B-STA 747, RLB 15 TO RBL 20. REPAIRED SHEAR TIE IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050407001392005040700139NM 2005 4 7 AWXA200500395 120050303A5330659187911 SKIN BOEING737 7373G7 1384595NM KEEL CANNING A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 MCN - MAJOR REPAIR - DURING C-16 CHECK FOUND KEEL BEAM LOWER SKIN DEFORMED BETWEEN BS 661 AND BS 726, LBL 5.0 AND RBL 5.0. MAINTENANCE REMOVED KEEL BEAM LOWER SKIN PANEL FROM BS 661 TO BS 726, LBL 5.0 TO RBL 5.0; FABRICATED A NEW REPLACEMENT KEEL BEAM SKIN PANEL AND REPAIR DOUBLERS; INSTALLED REPAIR PARTS IAW ER 03-5310-02085-TS1. 2L72 4F RTA16WE 20050407001422005040700142NM 2005 4 7 AWXA200500397 120050301A5320654795915 INTERCOSTAL BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 MCN - MAJOR REPAIR - DURING C-16 CHECK EXFOLIATION CORROSION WAS FOUND AFT CARGO COMPARTMENT SUPPORT BRACKET (INTERCOSTAL) AT BS 790, BETWEEN STR 24 & 25 RT. MAINTENANCE REMOVED CORRODED INTERCOSTAL TEE AT BS 790 FROM STR 24 RT TO STR 25 RT; FABRICATED A NEW REPLACEMENT TEE PER DWG 65-47959; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050407001462005040700146NM 2005 4 7 AWXA200500399 120050228A5311654795961 FRAME BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 MCN - MAJOR REPAIR - DURING C-16 CHECK EXFOLIATION CORROSION WAS FOUND ON FORWARD AND AFT FACE OF FRAME AT BS 794.3, STR 26 RT IN AFT CARGO COMPARTMENT. MAINTENANCE BLENDED OUT CORROSION ON FRAME AT BS 794.3, STR 26 RT; FABRICATED 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW ER 03-5311-05081-RA4. 2L72 4F RTA16WE 20050407001482005040700148NM 2005 4 7 AWXA200500400 120050228A5320654655218 FLOOR SUPPORT BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 MCN - MAJOR REPAIR - DURING C-16 CHECK CORROSION WAS FOUND IN MULTIPLE LOCATIONS AROUND NUT PLATES ON FLOOR SUPPORT IN AFT CARGO COMPARTMENT BETWEEN BS 787 AND BS 847, RBL 13.80. MAINTENANCE BLENDED OUT CORROSION ON FLOOR SUPPORT BETWEEN BS 787 AND BS 847, RBL 13.80; FABRICATED A -18 SUPPORT ANGLE, -29 SUPPORT ANGLE, -1 SUPPORT CHANNEL, & -2 REPAIR ANGLE; INSTALLED REPAIR PARTS IAW ER 03-5300-05085-HF2. 2L72 4F RTA16WE 20050407001502005040700150SO 2005 4 7 C2XA05BT019 120050406A33977337199505 WIRE HARNESS EMB 145 EMB145LR 3260212SO GALLEY DISCONNECTED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711536 145520 CREW REPORTED, EXIT ROW EMERGENCY LIGHT BURNED OUT OVER GALLEY DOOR. MAINTENANCE RECONNECTED THE CONNECTOR , OPS CHECKED GOOD IAW EMB145 AMM 33-50-00. 2L72 4T RTT00011AT 20050407001512005040700151NM 2005 4 7 ASAA0540111 120050206A5320143A120123 ANGLE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - CORROSION ON FAIL SAFE ANGLE. CUT OUT DAMAGE, INSTALLED REPAIR. (K) 2L72 4F4 FRTA16WE E21EU 20050407001522005040700152SO 2005 4 7 C2XA05BT018 120050401A335078241 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT FAULTY A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715910 145455 CREW REPORTED, EMERGENCY LIGHT OUT ABOVE GALLEY. REMOVED AND REPLACED EMERGENCY LIGHT INVERTER ABOVE GALLEY IAW EMB145 AMM 33-50-11. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050407001542005040700154SO 2005 4 7 C2XA05SD018 120050331A3350 BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713553 145585 SDF - LT AND RT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED LT OVERWING EMERGENCY LIGHT ASSY. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY NR 4 AND NR 4 CHARGER. OPS CHECK GOOD, AIRCRAFT RELEASED AND RETURNED TO SERVICE. BATTERY P/N 2013-BR, CHARGER P/N 11-0049, EMERGENCY LIGHT ASSY P/N 30-2510-3. 2L72 4T RTT00011AT 20050407001572005040700157EA 2005 4 7 COMA0560234 120050404A335020131A BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT FAULTY A COMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SO01915CA28031 7013 FLIGHT 5499 DURING TEST OF THE LIGHTING SYSTEM THE EMERGENCY LIGHTS WOULD NOT STAY ILLUMINATED. REPLACED THE EMERGENCY BATTERY PACK. 2L72 4F RTA21EA 20050407001592005040700159CE 2005 4 7 DXTA200500657 120050401A282231J240401 PRESSURE SWITCH CESSNA560 560XL 2076702CE ZONE 400 DIRTY E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07676QS701 5605176 RIGHT LO FUEL PRESS CAUTION LIGHT ILLUMINATES INTERMITTENTLY WITH ENGINE RUNNING. STILL ILLUMINATES WITH RT BOOST PUMP ON OR OFF. REMOVED & INSPECTED FUEL FILTER, FOUND FILTER TO BE DIRTY. REMOVED & REPLACED FUEL FILTER OPERATED RT ENGINE AT TAKEOFF POWER FOR 2 MINUTES SYSTEM OPS CHECKED AND LEAK CHECKED GOOD, ALL WORK DONE IAW P&W 545 M/M CHAP 73-10-05. 2L72 4F RTA22CE 20050407001612005040700161EA 2005 4 7 COMA0560240 120050404A335020131A BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT FAULTY A COMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SO01477CA7506 7670 FLIGHT 5358 DURING TEST OF THE LIGHTING SYSTEM THE FLOOR TRACK EMERGENCY LIGHTS AT ROWS 1 THROUGH 5 FAILED TO ILLUMINATE. REPLACED THE EMERGENCY BATTERY PACK. 2L72 4F RTA21EA 20050407001652005040700165EA 2005 4 7 COMA0560231 120050403A321316124101 AXLE CNDAIRCL600 CL6002B19 1900309EA NLG WORN A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01804CA14314 7352 FLIGHT 5907 DURING CLIMBOUT OF CVG, RECEIVED A LANDING GEAR DISAGREE WARNING MESSAGE, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD, LANDING WITHOUT INCIDENT. REPLACED THE NLG LOWER STRUT. ASSEMBLY. 2L72 4F RTA21EA 20050407001662005040700166NE 2005 4 7 COMA0560230 220050405A7200CF343A1 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE RIGHT OUT OF TOLERANCEA COMAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SO01710CA22809 7241 807361 FLIGHT 5267 DURING CLIMBOUT OF CVG THE RIGHT ENGINE WOULD NOT ACHIEVE CHARTED RATED THRUST. AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. REPLACED THE RIGHT ENGINE ASSEMBLY. 2L72 4F4 FRTA21EA E15NE 20050407001682005040700168EA 2005 4 7 COMA0560235 120050404A3350201310 BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT FAULTY A COMAD RETURN TO BLOCK L NO TEST TXTAXI/GRND HDL 1 SO01915CA28031 7013 FLIGHT 5499 DURING TEST OF THE LIGHTING SYSTEM THE EMERGENCY LIGHTS WOULD NOT STAY ILLUMINATED. REPLACED THE EMERGENCY BATTERY PACK. 2L72 4F RTA21EA 20050407001702005040700170EA 2005 4 7 COMA0560233 120050404A33502013BR BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT FAULTY A COMAD RETURN TO BLOCK L NO TEST TXTAXI/GRND HDL 1 SO01915CA28031 7013 FLIGHT 5499 DURING TEST OF THE LIGHTING SYSTEM LIGHTS WOULD NOT STAY ILLUMINATED. REPLACED THE EMERGENCY BATTERY PACK. 2L72 4F RTA21EA 20050407001722005040700172EA 2005 4 7 COMA0560238 120050404A335020131A BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT FAULTY A COMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SO01477CA7506 7670 FLIGHT 5358 DURING TEST OF THE LIGHTING SYSTEM THE FLOOR TRACK EMERGENCY LIGHTS AT ROWS 1 THROUGH 5 FAILED TO ILLUMINATE. REPLACED THE EMERGENCY BATTERY PACK. 2L72 4F RTA21EA 20050407001732005040700173WP 2005 4 7 ASAA0580102 120050215A532199365811 FLOOR PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02943AS 53018 OKC C-CHECK, PAX CABIN FLOOR PANEL PEELED AND DELAMINATED. FIBERGLASS BOND REPAIRED. (NM02200500846) (K) 2L72 4F4 FRTA6WE E9NE 20050407001742005040700174EA 2005 4 7 COMA0560236 120050404A33502013BR BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT FAULTY A COMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SO01915CA28031 7013 FLIGHT 5499 DURING TEST OF THE LIGHTING SYSTEM THE EMERGENCY LIGHTS WOULD NOT STAY ILLUMINATED. REPLACED THE EMERGENCY BATTERY PACK. 2L72 4F RTA21EA 20050407001752005040700175EA 2005 4 7 COMA0560237 120050404A335020131A BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT FAULTY A COMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SO01477CA7506 7670 FLGIHT 5358 DURING TEST OF THE LIGHTING SYSTEM THE FLOOR TRACK EMERGENCY LIGHTS AT ROWS 1 THROUGH 5 FAILED TO ILLUMINATE. REPLACED THE EMERGENCY BATTERY PACK. 2L72 4F RTA21EA 20050407001772005040700177CE 2005 4 7 DXTA200500652 120050331A261172111211102 SMOKE DETECTOR CESSNA650 650 2076802CE FAILED E DXTAD RETURN TO BLOCK BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TXTAXI/GRND HDL 1 GL07789QS5221 6507089 SMOKE DETECTION MASTER WARNING LIGHTS ILLUMINATED. REMOVED SMOKE DETECTOR CONTROL UNIT. REPLACED WITH REPAIRED UNIT IAW CHAP 26-12-00 OF THE CESSNA 650 MM. OPS CHECKED GOOD. 2L72 4F A9NM 20050407001782005040700178NM 2005 4 7 AWXA200500386 120050305A53206545834107 STRAP BOEING737 7373G7 1384595NM FLOORBEAM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 MCN - MAJOR REPAIR - DURING C-16 CHECK A .375 INCH CRACK WAS FOUND IN E&E COMPARTMENT FLOORBEAM LOWER FLOOR STABILIZER AT BS 328, RBL 45. MAINTENANCE STOP DRILLED CRACK IN FLOORBEAM LOWER FLOOR STABILIZER AT BS 328, RBL 45; FABRICATED A REPAIR PLATE; INSTALLED REPAIR PART IAW B737-300 SRM 53-10-51 FIG 204. 2L72 4F RTA16WE 20050407001792005040700179NM 2005 4 7 AWXA200500387 120050301A532065479576 WEB BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 MCN - MAJOR REPAIR - DURING C-16 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT DOOR SILL INBOARD WEB BETWEEN BS 794 AND BS 838, RBL 20. MAINTENANCE REMOVED CORRODED AFT CARGO DOOR SILL INBOARD WEB FROM BS 794 TO BS 838, RBL 20; FABRICATED A NEW REPLACEMENT WEB PER DWG 65-47957; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050407001802005040700180NM 2005 4 7 AWXA200500388 120050303A534069432332 ATTACH ANGLE BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 MCN - MAJOR REPAIR - DURING C-16 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT DOOR SILL AFT ATTACH ANGLE AT BS 846 BETWEEN RBL 22 AND RBL 28. MAINTENANCE REMOVED CORRODED AFT CARGO DOOR SILL AFT ATTACH ANGLE AT BS 846 FROM RBL 22 TO RBL 28; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 69-43233; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050407001822005040700182NM 2005 4 7 AWXA200500389 120050302A5320654795734 CHANNEL BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 MCN - MAJOR REPAIR - DURING C-16 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT DOOR SILL CHANNEL BETWEEN BS 794 AND BS 817, RBL 20 AND RBL 25. MAINTENANCE REMOVED CORRODED AFT CARGO DOOR SILL CHANNEL FROM BS 794 TO BS 817, RBL 20 TO RBL 25; FABRICATED A NEW REPLACEMENT CHANNEL PER DWG 65-47957; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050407001842005040700184NM 2005 4 7 AWXA200500391 120050301A575465C26602257 SKIN BOEING737 7373G7 1384595NM NR 5 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 MCN - MAJOR REPAIR - DURING C-16 CHECK 7 EACH .3125 INCH CRACKS WERE FOUND IN LOWER SURFACE SKIN OF NR 5 SLAT BETWEEN SLAT STATIONS 166 - 215. MAINTENANCE CUT OUT DAMAGE IN LOWER SURFACE SLAT SKIN FROM SS 166 TO SS 215 RT; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-43-01 FIG 206. 2L72 4F RTA16WE 20050407001862005040700186EA 2005 4 7 COMA0560241 120050403A2931848847 PUMP CNDAIRCL600 CL6002B19 1900309EA WING ROOT FAULTY A COMAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 SO01975CA21860 7150 FLIGHT 5886 DURING CRUISE FLIGHT RECEIVED A LOW HYDRAULIC NR 3 SYSTEM PRESSURE CAUTION, CREW DECLARED AN EMERGENCY AND LANDED AT JFK WITHOUT INCIDENT. REPLACED HYDRAULIC PUMP 3A. 2L72 4F RTA21EA 20050407001882005040700188NM 2005 4 7 CALA0500093 120050401A5210507945279 SKIN BOEING737 737524 1384721NM L-1 DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2737615 27328 INSPECTION FOUND A .5 INCH CRACK FROM RIVET IN L-1 DOOR AT TOP AFT CORNER. A REPAIR WAS INSTALLED IAW ECRA 5210-01822. 2L72 4F RTA16WE 20050407001912005040700191NM 2005 4 7 CALA0500095 120050402A5340656571034 SUPPORT BRACKET BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717326 23456 INSPECTION FOUND A 1.25 INCH CRACK IN ANTENNA SUPPORT BRACKET AT STA 727D + 5 INCH. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20050407001942005040700194NM 2005 4 7 72300137 120050329A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CRACKED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 APPROX 5 INCH CRACK IN STRINGER. 2L73 4F4 FRTA3WE E2EA 20050407001952005040700195NM 2005 4 7 ASAA0540045 120050123A575465C266027 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU L/E SLAT CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 OKC - NR 2 SLAT LOWER SKIN CRACKED 2 PLACES IB END AT FASTENER (.73 INCH LONG) AND CENTER (1.6 INCHES LONG). REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050407001972005040700197SO 2005 4 7 C2XA05CL018 120050325A49504951680 BLEED VALVE EMB 145 EMB145 3260210SO APU BYPASSING A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SW2727962 145110 CLE - THE CREW REPORTED A STRONG FUEL SMELL AFTER THE APU WAS STARTED. MAINTENANCE REMOVED AND REPLACED THE APU BLEED VALVE AND THE OPERATIONAL CHECKS WERE GOOD, AND NO FUEL SMELL WAS DETECTED. 2L72 4F RTT00011AT 20050407002012005040700201WP 2005 4 7 ASAA0580119 120050226A53219936651515 FLOOR PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 OKC HV-CHECK - CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (NM02200500849) (K) 2L72 4F4 FRTA6WE E9NE 20050407002042005040700204EA 2005 4 7 COMA0570036 120050331A27605120011 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA LT WING SPOILER MALFUNCTIONED A COMAO OTHER J WARNING INDICATION DEDESCENT 1 SO01317CA6850 10055 FLIGHT 5020 DURING DESCENT INTO CVG WHEN FLIGHT SPOILERS WERE DEPLOYED, RECEIVED SPOILERON AND FLIGHT SPOILER CAUTION MESSAGES, CREW DECLARED AN EMERGENCY, AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE LT OUTBOARD MULTIFUNCTION SPOILER POWER CONTROL UNIT. 2L72 4F RTA21EA 20050407002052005040700205WP 2005 4 7 ASAA0580103 120050215A532199366391 FLOOR PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02943AS 53018 OKC C-CHECK- PAX CABIN FLOOR PANEL DELAMINATED. FIBERGLASS BOND REPAIRED. (NM02200500846) (K) 2L72 4F4 FRTA6WE E9NE 20050407002072005040700207EU 2005 4 7 AWXA200500379 120050331A335032145410 POWER SUPPLY AIRBUS320 A320232 3930326EU EMERGENCY LIGHTSFAULTY A AWXAK NONE O OTHER ININSP/MAINT 1 WP28647AW128777962 762 PHX - EEL - DURING P-06 CHECK FOUND THE RIGHT OVERWING EMERGENCY POWER SUPPLY UNIT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED RIGHT OVERWING EMERGENCY POWER SUPPLY UNIT (12WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050407002102005040700210SO 2005 4 7 C2XA05IA051 120050330A3200355022022 CONTROL UNIT EMB 145 EMB145ER 3260211SO MLG FAULTY A C2XAO OTHER J WARNING INDICATION CLCLIMB 1 SW27149303374 3374 145011 DURING CLIMB THE LANDING GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. THE CREW PERFORMED AN OVER-RIDE TO RETRACT GEAR. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT (LGEU). THE GEAR OPERATIONALLY TESTED GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTT00011AT 20050407002112005040700211NM 2005 4 7 72300122 120050323A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 1 INCH AREA OF CORROSION ON BOTTOM OF STRINGER. 2L73 4F4 FRTA3WE E2EA 20050407002122005040700212NM 2005 4 7 72300123 120050323A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 4 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050407002132005040700213NM 2005 4 7 72300124 120050323A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 2 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050407002142005040700214NM 2005 4 7 72300125 120050323A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 2 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050407002152005040700215NM 2005 4 7 72300126 120050323A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 6 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050407002162005040700216NM 2005 4 7 72300127 120050323A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 3 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050407002172005040700217NM 2005 4 7 72300128 120050323A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A .75 X 4 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050407002182005040700218NM 2005 4 7 72300129 120050323A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 3 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050407002192005040700219EA 2005 4 7 COMA0560228 120050403A3010 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA ANTI ICE SYSTEM MALFUNCTIONED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01933CA 7040 FLIGHT 5175 - DURING TAKEOFF ROLL, RECEIVED A RIGHT WING ANTI ICE CAUTION, ABORTED TAKEOFF AND RETURNED TO THE GATE. C/W RTO INSPECTION AND PERFORMED AN OPERATIONAL CHECK OF THE WING ANTI ICE SYSTEM. DISCREPANCY COULD NOT BE DUPLICATED. 2L72 4F RTA21EA 20050407002202005040700220EA 2005 4 7 COMA0570037 120050403A2120 ODOR CNDAIRCL600 CL6002C10 1390015EA COCKPIT DETECTED A COMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO01340CA 10062 FLIGHT 5887 DURING CLIMBOUT OF CVG, SMOKE (ODOR) WAS NOTED IN CABIN AND COCKPIT, CREW DECLARED AN EMERGENCY, RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. PERFORMED A VISUAL INSPECTION OF CABIN LIGHTING, OPERATED APU AND AIR CONDITIONING PACKS. DISCREPANCY COULD NOT BE DUPLICATED. 2L72 4F RTA21EA 20050407002232005040700223WP 2005 4 7 ASAA0580114 120050226A532199365521 FLOOR PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 OKC HV-CHECK - CABIN FLOOR PANEL HAS CORRODED AND CRACKED FASTENERS. REPLACED FLOOR PANEL. (NM02200500849) (K) 2L72 4F4 FRTA6WE E9NE 20050407002582005040700258EA 2005 4 7 VTZA200500036 120050331A531260034017595 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27638BR 7311 RIGHT SIDE PILOTS BULKHEAD AT FS 280 RBL 9.0 IS CRACKED AT 1 INCH IN WEB RADIUS. 2L72 4F RTA21EA 20050407002602005040700260EU 2005 4 7 AWXA200500043 120050111A5320D5347112420100 SHEAR PLATE AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28621AW 053 SAL - MAJOR REPAIR - DURING C-04 CHECK INTERGRANULAR CORROSION WAS FOUND ON WEB (SHEAR PLATE) -Y1732 BETWEEN FS 69 AND FS 70. MAINTENANCE REMOVED DAMAGED SHEAR PLATE -Y1732 FROM FS 69 TO FS 70; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050407002612005040700261EA 2005 4 7 COMA0560222 120050331A32304622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG FAULTY A COMAO OTHER J WARNING INDICATION DEDESCENT 1 SO01959CA22884 7116 FLIGHT 5607 ON APPROACH INTO SAV, RECEIVED A GEAR DISAGREE MASTER WARNING, CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED THE NLG PRIORITY VALVE. 2L72 4F RTA21EA 20050407002652005040700265NM 2005 4 7 SWAA050957 120050329A552365C2638416M TAB BOEING737 7373A4 1384585NM RT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED C1 CHECK, RT ELEVATOR TAB FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB PER MM. 2L72 4F RTA16WE 20050407002662005040700266NM 2005 4 7 2005UALA00275 120050330A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE GOUGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29309UA 23670 FWD CARGO DOOR CUTOUT FWD EDGE IS GOUGED AT STR 24R. MAJOR REPAIR ACCOMPLISHED. BLENDED DAMAGE AND INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20050407002672005040700267NM 2005 4 7 2005UALA00276 120050331A5321 PRESSURE PANEL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29309UA 23670 LEFT STA 664 PRESSURE DECK WEB IS CRACKED AT APPROXIMATELY LBL 30 JUST FWD OF OUTBOARD AILERON TOWER SHAFT. MAJOR REPAIR ACCOMPLISHED. CUT OUT CRACK, FABRICATED AND INSTALLED A DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20050407002682005040700268 2005 4 7 SWIA200514805 420050327A2216 SERVO CNDAIRCL600 CL6002B19 1900309EA ELEVATOR MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED DEDESCENT 1 NM07962SW 7859 AFTER A/P DISCONNECT ON FINAL, F/O UNABLE TO MOVE ELEVATOR IN EITHER DIRECTION FOR 5 TO 7 SECONDS AFTER DISC PITCH CONTROL THEN RETURNED TO NORMAL. REPLACED ELEVATOR SERVO & SERVO MOUNT UNITS IAW 22-11-14, AND 22-11-24. OPERATIONAL CHECK GOOD. P/N 622-5027-101, S/N OFF 13XHP, P/N 822-0260-001, S/N OFF 145HP. 2L72 4F RTA21EA 20050407002702005040700270EA 2005 4 7 SWIA200514826 120050331A2752 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED APAPPROACH 1 NM07929SW 7703 FLAPS FAILED WHEN SELECTING FROM 0 DEGREES TO 8 DEGREES INFLIGHT. REPLACED FLAP ACTUATORS PER CRJ 200 MM 27-53-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050407002722005040700272EA 2005 4 7 COMA0560227 120050402A32304622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG FAULTY A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01804CA10694 7352 FLIGHT 5742 AFTER TAKEOFF THE NLG WOULD NOT RETRACT, LANDING GEAR DISAGREE WARNING MESSAGE DISPLAYED, AIRCRAFT RETURNED TO THE FIELD. REPLACED THE NLG PRIORITY VALVE. 2L72 4F RTA21EA 20050407002732005040700273NM 2005 4 7 2005UALA00263 120050328A335060243 LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FWD GALLEY DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29313UA 23674 FORWARD GALLEY EEL LIGHT INOP. REPLACED FWD GALLEY EEL LIGHT STRIP. 2L72 4F4 FRTA16WE E2GL 20050407002742005040700274NM 2005 4 7 SWAA050973 120050330A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 269, STR 16R. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050407002762005040700276NM 2005 4 7 2005UALA00268 120050329A5315 FLOORBEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29308UA 23669 AFT CABIN FLOORBEAM STA 986 RBL 16 TO RBL 28 WL 208 IS CORRODED. REPAIR ANGLE AND FLOOR BEAM T-CAP REPLACED. 2L72 4F4 FRTA16WE E2GL 20050407002772005040700277SO 2005 4 7 SWIA200514810 120050327A27503431001001 ACTUATOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED LDLANDING 1 NM07290SW9993 9993 120317 NAC FLAP DISAGREEMENT ON APPROACH TO LANDING AT SFO. REMOVED AND REPLACED LEFT NACELLE FLAP ACTUATOR WITH SERVICEABLE IAW EMB 120 MM CHPT 27-50-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050407002792005040700279NM 2005 4 7 2005UALA00264 120050327A339758781 WIRE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE ROW 15ABC DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29203UA 24718 FLOOR EEL LIGHTS ARE INOP FROM SEAT 15ABC TO 21ABC. *S/D* REPLACED EEL CABLE AND EEL LIGHT. 2L72 4F4 FRTA16WE E2GL 20050407002812005040700281NM 2005 4 7 SWAA050958 120050329A552365C2638415M TAB BOEING737 7373A4 1384585NM LT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED C1 CHECK, LT ELEVATOR TAB HAD EXCESSIVE PLAY. REMOVED AND REPLACED LT ELEVATOR TAB PER MM. 2L72 4F RTA16WE 20050407002832005040700283EU 2005 4 7 AWXA200500380 120050331A2421766219 GENERATOR AIRBUS320 A320231 3930325EU NR 1 ENGINE DAMAGED A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28627AW271046123 66 ON TAKEOFF AT LAS EN ROUTE TO MSP RECEIVED CLASS I ECAM MESSAGE ELECT IDG OIL LOW PRESSURE, REJECTED TAKEOFF AT 50 KTS. ISSUED MEL 24-20-01, COND 2 NR 1 IDG INOP. MAINTENANCE TROUBLESHOT THE NR 1 IDG PER TSM TASK 24-20-00-810 AND FOUND METALIC PARTICLES IN THE FILTER AND HOUSING ASSEMBLIES. REMOVED AND REPLACED NR 1 IDG IAW T/C R5M24301, OPERATIONAL CHECK WAS GOOD. FAILURE ANALYSIS OF IDG S/N 1593 CONFIRMED REASON FOR REMOVAL FINDING SMALL METAL PARTICLES IN SCAVENGE FILTER CAUSING IT TO CLOG. FURTHER INVESTIGATION REVEALED FIXED SPINE SHAFT INBOARD BEARING INNER RACE WAS END LOADING CAUSE BEARING FAILURE. VENDOR RECOMMENDS THIS UNIT TO BE OVERHAULED. 2L72 4F RTA28NM 20050407002872005040700287WP 2005 4 7 AALA20050029 120050115A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21557AN 53087 LAX - OVERHEAD EMERGENCY LIGHTS ABOVE AFT FLIGHT ATTENDANT STATION INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS ABOVE AFT FLIGHT ATTENDANT STATION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050407002882005040700288WP 2005 4 7 AALA20050037 120050117A3350408822101 BATTERY DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21471AA 49601 BOS - FORWARD OVERWING DOOR EXIT LIGHTS INOPERATIVE. REPLACED BATTERIES ON PATTERY PACK FOR FORWARD OVERWING DOOR EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050407002892005040700289WP 2005 4 7 AALA20050033 120050116A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21496AA 49734 SFO COCKPIT EGRESS LIGHTS INOPERATIVE. REPLACED BATTERY PACK B5 23 FOR COCKPIT EGRESS LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F A6WE 20050407002912005040700291WP 2005 4 7 AALA20050031 120050116A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21223AA 49173 DFW - OVERHEAD EMERGENCY LIGHT IN AFT CABIN L2 615 AND LAMP 1 OF L2694 IN TAIL CONE INOPERATIVE. REPLACED BATTERY PACK AND CHARGER ASSEMBLY AT B5 27 FOR OVERHEAD EMERGENCY LIGHTS IN AFT CABIN L2 615 AND LAMP 1 OF L2694 IN TAIL CONE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050407002932005040700293EU 2005 4 7 MALA050106 120050104A3230 WARNING SYSTEM BAC 146 AVRO146RJ85A1500097EU COCKPIT MALFUNCTIONED A MALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL15523XJ E2348 LT MAIN GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTED ALONG WITH GEAR INTRANSIT LIGHT IN HANDLE. QRH PROCEDURES COMPLETE BUT GEAR STILL INDICATED UNSAFE. GEAR LOCKED DOWN NORMALLY AND INDICATED NORMALLY. AIR RETURN TO MSP. MAINTENANCE CND PROBLEM CLEANED AND LUBED LT GEAR DOOR UP LOCK MECHANISM. COMPLETED SEVERAL GEAR SWINGS, ALL CHECKS GOOD. 2H74 4F RTA49EU 20050407002952005040700295EU 2005 4 7 MALA050101 120050101A2613 WARNING LIGHT SAAB SF340 340B 7860101EU COCKPIT ILLUMINATED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15362PX 340B258 RIGHT TAIL PIPE HOT MASTER WARNING LIGHT CAME ON OUR INITIAL CLIMB, PERFORMED MEMORY ITEMS AND QRH CHECK LIST WARNING LIGHT WENT OUT. AIR RETURN TO MEM. MAINTENANCE RAN AC FOR 30 MINUTES COULD NOT DUPLICATE TAIL PIPE HOT LIGHT. OPS CHECK GOOD 2L72 4T RTA52EU 20050407002962005040700296EU 2005 4 7 MALA050102 120050103A3020 THERMISTER SAAB SF340 340B 7860101EU RT ENGINE DEFECTIVE A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15411XJ 340B411 DURING CLIMB-OUT OF DTW RIGHT ENGINE INTAKE LIGHT CYCLED ON/OFF APPROXIMATELY EVERY 20 SECONDS. QRH COMPLETED. AIR RETURN TO DTW. MAINTENANCE FOUND NR 1 THERMISTOR OHM CHECK BAD IAW MM REPOSITIONED NR 1 THERMISTOR TO NR 4 POSITION. OPS CHECK OF RT INTAKE HEAT SYSTEM IAW MM ALL GOOD. 2L72 4T RTA52EU 20050407002992005040700299EU 2005 4 7 MALA050113 120050109A3260 PAD SAAB SF340 340B 7860101EU LANDING GEAR OBSTRUCTED A MALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL15442XJ 340B442 GEAR INTRANSIT LIGHT STAYS ILLUMINATED IN THE RETRACTED POSITION. AIR RETURN TO MSP. MAINTENANCE JACKED A/C PER AMM 07-10-00, SWUNG GEAR VERIFIED INTRANSIT LIGHT STAYED ON REMOVED ICE BUILD UP ON GEAR STOP PADS, SWUNG GEAR SEVERAL TIMES NO INTRANSIT LIGHT NOTED. LOWERED A/C ALL CHECKS GOOD. 2L72 4T RTA52EU 20050407003002005040700300EU 2005 4 7 MALA050126 120050111A52807252456003 BRACKET SAAB SF340 340B 7860101EU MLG DOOR CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15366PX 340B267 DURING 4Y/2Y INSPECTION IN BNA, BRACKET PN 7252456-003 FOR HOLD OPEN ARM ON SPR DOOR IS CRACKED AND WILL BE REPLACED IAW SRM 51-40-21. REFER EAMS WO NR 211360, TASK 6501 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 1/15/05. 2L72 4T RTA52EU 20050407003032005040700303NM 2005 4 7 SWAA050941 120050328A53116546546 BELTFRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29364SW 26575 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE BELTFRAME WEB CRACKED AT BS 847, BETWEEN STR 25R TO STR 26R. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050407003052005040700305NM 2005 4 7 SWAA050945 120050328A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29605SW 27956 DURING SCHEDULED D-CHECK, FOUND CORROSION ON SHEAR TIE AT BS 767, RBL 11. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050407003072005040700307NE 2005 4 7 ASMF200501015 220050119A72611026V0800 VALVE BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE LEFT ENGINE FAILED W ASMFK NONE K FLUID LOSS ININSP/MAINT 1 SW23804AM128107164 26271 726669 DURING TRANSIT CHECK WAS DETECTED A HYDRAULIC LEAK IN THE LEFT ENGINE FILTERS MODULE TUBE, TUBE WAS TIGHTENED AND ENGINE WAS MOTORIZED, BUT DURING THE PROCESS A NEW LEAK WAS DETECTED IN THE DE-OILER. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE BEARING SCAVENGE VALVE AND FILTERS MODULE LINE WERE REPLACED IAW MM 72-61-02, TESTED CORRECT. 2L72 4F4 FRTA2NM E17NE 20050407003082005040700308NM 2005 4 7 05FDEA00844 120050405A5347 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RT SEAT TRACK AT STA 1500 TO 1531, RBL-75 CORRODED. REPAIRED SEAT TRACK AND SPLICE FABRICATED AS PER SRM 51-70-00 FIGURE 1 VOL I AND INSTALLED AS PER SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20050407003142005040700314EU 2005 4 7 05FDEA00828 120050404A5522 SKIN AIRBUS310 A310 EU LT ELEVATOR DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 LT ELEVATOR TOP SURFACE BETWEEN STA468/ER16 AND STA474/ER20 IS DELAMINATION. COMPLIED WITH EA NR 6-5520-87163. 2L72 4F RTA35EU 20050407003152005040700315EU 2005 4 7 05FDEA00831 120050404A5522 SKIN AIRBUS310 A310 EU LT ELEVATOR DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 LT ELEVATOR TOP SURFACE STA 473/ER19 HAS 3EA AREAS OF CORROSION. COMPLIED WITH FEDEX EA NR 6-5520-87163. 2L72 4F RTA35EU 20050407003172005040700317EU 2005 4 7 05FDEA00833 120050404A5330 SKIN AIRBUS310 A310 EU FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 REPAIR NEEDS EVALUATION FOR FAA APPROVED DATA AND MAJOR OR MINOR CLASSIFICATION. ITEM NR 22 ON LIST FUSELAGE LOWER RT SIDE AT FR 58 THIS REPAIR WAS ACCOMPLISHED IAW FEDEX EA NR 6-5530-49627A REVISE DATE 04/25/00. THIS REPAIR IS CLASSED AS A MAJOR REPAIR AND HAS FOLLOW UP ACTION REQUIRED ALSO FRAME AND STRINGER LOCATIONS HAVE BEEN CORRECTED TO MATCH EXISTING DOUBLER INSTALLATION, REFERENCE EA6-5330-87763 PT1. 2L72 4F RTA35EU 20050407003192005040700319NM 2005 4 7 05FDEA00871 120050406A5330 SKIN BOEING727 727200 138407ENM FUSELAGE MISDRILLED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25481FE 21463 DRILL START IN FUSELAGE SKIN BELOW FWD GALLEY DOOR. REPAIRED DRILL START PER FED EX EA 7-5330-86265. 2L73 4F RTA3WE 20050407003222005040700322EU 2005 4 7 05FDEA00753 120050331A5313 STRINGER AIRBUS310 A310 EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 N00674 AREA BEHIND BULK CARGO AT FRAME 74 LEFT SIDE APPROX FR 49L HAS 7 SQ IN OF CORROSION. REMOVED CORROSION AFT OF FRAME 74 FOUND TO BE OUT OF LIMITS IAW A310-200 SRM 53-10-00 FIG 104, TABLE 102. REMOVED AND REPLACED STRINGER SECTION WITH NEW 48L FS 72-78 IAW SRM 53-10-14. 2L72 4F RTA35EU 20050407003232005040700323NM 2005 4 7 SWAA050932 120050327A53306545776 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29671SW 23785 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947.5, STR 24R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050406001652005040600165NM 2005 4 6 ASAA0540047 120050123A575565464515 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU NR 7 SPOILER DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 OKC - NR 7 SPOILER HAS 2 SHARP DENTS IN AREA OF ACTUATOR ATTACH. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050406001712005040600171NM 2005 4 6 ASAA0540040 120050121A523065479522 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU AFT CARGO DOOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 OKC - AFT CARGO DOOR DENTED IN MIDDLE, EXTERNAL SKIN. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050406001722005040600172NM 2005 4 6 ASAA0540149 120050225A531565C3394311 FLOORBEAM BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02784AS 28199 PAE - CORROSION ON FLOORBEAM AT FASTENER HOLE STA B344, LBL 25, WL 208. REPAIRED IAW SRM 53-00-51, FIG 203. (K) 2L72 4F4 FRTA16WE E21EU 20050407000182005040700018NM 2005 4 7 72300135 120050329A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 1 INCH AREA OF CORROSION ON BOTTOM OF SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050407000222005040700022SO 2005 4 7 LR7A05038 120050328A5330 SKIN LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 506 4606 DURING SCHEDULED B2 INSPECTION PER JOB CARD HB5301 FOUND PILOT'S SWING WINDOW, FWD POST CRACKED AT FS 105, LBL 35, WL 231. REPAIRED IAW LAC MEA 382-53-05-031. 2H74 4T A1SO 20050407000242005040700024SO 2005 4 7 LR7A05040 120050328A5313 LONGERON LKHEED382 382G 526414USO FUSELAGE CORRODED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 506 4606 DURING SCHEDULED B2 INSPECTION PER JOB CARD HB5301 FOUND RIGHT AFT FUSELAGE RBL 61 LONGERON CORRODED AT FS 777E, WL 146. REPAIRED IAW LAC MEA 382-53-05-032. 2H74 4T A1SO 20050407000422005040700042EU 2005 4 7 AWXA200500381 120050403A3397ABS0374A24 WIRE AIRBUS320 A320232 3930326EU SEAT ROW 22 L/H BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28604AW 1196 PHX - EEL - DURING 8-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 22 LT INOPERATIVE. MAINTENANCE FOUND AND REPAIRED A BROKEN EMERGENCY ESCAPE PATH LIGHT WIRE AT THE WALL CONNECTOR OF SEAT ROW 22 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050407000472005040700047NM 2005 4 7 72300145 120050329A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 1 INCH AREA OF CORROSION ON LOWER LEG OF SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050407000542005040700054NM 2005 4 7 SWAA050938 120050327A57536546430100 SKIN BOEING737 7373H4 1384600NM RT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29327SW 23691 RIGHT WING INBOARD T/E FOREFLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM. 2L72 4F RTA16WE 20050407000572005040700057NM 2005 4 7 SWAA050949 120050328A53116546550 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29605SW 27956 DURING SCHEDULED D-CHECK, FOUND CORROSION ON FUSELAGE FRAME AT BS 794, RBL 14, WL 156. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050407000752005040700075NM 2005 4 7 72300140 120050402A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 DAMAGED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A .25 X .25 INCH AREA OF DAMAGE ON VERTICAL PORTION OF SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050407000772005040700077EA 2005 4 7 SWIA200514798 120050316A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07957SW 7829 RT FLOORBEAM ANGLE AT FS 621.00 IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. CRACKED ANGLE REPAIRED IAW REO 601R-53-61-117 REV B. 2L72 4F RTA21EA 20050407000802005040700080SO 2005 4 7 C2XA05SH020 120050325A5330 SKIN EMB 145 EMB145LR 3260212SO FUSELAGE DENTED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715983 145239 SHV - DURING C-CHECK LT CENTER FUSELAGE 1 SKIN DENTED FWD OF LT STATIC PORT IN RVSM CRITICAL AREA. MAINTENANCE REPAIR THE DAMEGE AREA AND PERFORMED RVSM INSPECTION IAW EC5330-01450. THE AIRCRAFT WAS APRROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050407000932005040700093EA 2005 4 7 SWIA200514815 120050328A3350 LIGHT CNDAIRCL600 CL6002C10 1390015EA CABIN MISSING A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07728SK 10192 EMERGENCY LIGHTING STRIP NEAR SERVICE DOOR MISSING. REPLACED EMERGENCY LIGHT PANEL AFT PORTION OF SERVICE DOOR. 2L72 4F RTA21EA 20050407001032005040700103NM 2005 4 7 72300143 120050402A5311 FRAME BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CRACKED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A .75 INCH CRACK ON LOWER FRAME ATTACH FLANGE OF WEB. 2L73 4F4 FRTA3WE E2EA 20050407001082005040700108EA 2005 4 7 COMA0560213 120050331A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01495CA 7774 RIGHT HAND SIDE 621 FLOOR ANGLE IS CRACKED. REPAIRED IAW REO 601R-53-61-117. 2L72 4F RTA21EA 20050407001122005040700112NM 2005 4 7 ASAA0540103 120050209A5320654652837 SUPPORT BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - FWD CARGO BAY AREAS OF CORROSION ON FLOOR TO SIDEWALL SUPPORT BS 500F TO 500G, LBL 23, WL 156. (K) 2L72 4F4 FRTA16WE E21EU 20050407001162005040700116SO 2005 4 7 SWIA200514800 120050329A3397 WIRE EMB 120 EMB120ER 3260203SO EMERGENCY SIGN BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07190SW 120050 EXIT SIGN ABOVE F/A JUMPSEAT WILL NOT ILLUMINATE. REPAIRED BROKEN WIRE AT FIXTURE, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050407001192005040700119EA 2005 4 7 SWIA200514801 120050328A274070623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB MOTOR MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07929SW5018 5018 7703 CREW REPORTS STAB TRIM CONTINUOUSLY DISCONNECTS DURING FLIGHT. REMOVED AND REPLACED STAB MOTOR CONTROL UNIT IAW MM 27-40-00, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050407001282005040700128EA 2005 4 7 COMA0560217 120050330A3260 UPLOCK SWITCH CNDAIRCL600 CL6002B19 1900309EA NLG OUT OF ADJUST A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01804CA 7352 FLIGHT 5714 AFTER TAKEOFF FROM JFK, AIRCRAFT DIVERTED BACK TO THE FIELD DUE TO THE NLG NOT RETRACTING. ADJUSTED THE NLG UPLOCK SWITCH. 2L72 4F RTA21EA 20050407001492005040700149NM 2005 4 7 ASAA0510013 120050306A5330654577646 SKIN BOEING737 7372Q8C 138448SNM PWA JT8 JT8D17 52049NE FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02741AS 21959 OKC - GOUGES IN SKIN AT B-STA 727A JUST ABOVE S26R. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER, STRUCTURAL FILLER, AND DOUBLER IAW AS EA AND AAR EA. (K) 2L72 4F4 F A16WE E2EA 20050407001922005040700192NM 2005 4 7 ASAA0540044 120050123A531165C2523034 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 OKC - AFT CARGO COMPARTMENT B-STA 727E FRAME IS CORRODED ON THE FORWARD SIDE BETWEEN STR 25R AND 25L. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER, ANGLE, AND SHEAR TIE IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050407002262005040700226NM 2005 4 7 ASAA0510002 120050202A526069468061 BEARING BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE AIRSTAIRS MISSING A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 SEA - FUND HANDRAIL FITTING CORRODED, BEARING MISSING, AND RETAINER - 176 CORRODED. LOOSE BEARING/ CASTING JAMS DOOR WHEN OPENING. PIVOT POINT WAS REPAIRED WITH BUSHING IAW EA. (K) 2L72 4F4 F A16WE E2EA 20050407002272005040700227NM 2005 4 7 ASAA0540027 120050112A5310654588524 DOOR FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 OKC - E AND E BAY DOOR CUTOUT FORWARD FRAME, WEB AT STA328, LBL 0 TO 3 IS GOUGED. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050407002282005040700228NM 2005 4 7 ASAA0540042 120050121A534069353523 STRINGER CLIP BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 OKC - STRINGER CLIP AT STA 947, STR 26R, CRACKED AND CORRODED. REMOVED DAMAGED CLIP, FABRICATED AND INSTALLED A REPLACEMENT CLIP IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050407002312005040700231NM 2005 4 7 ASAA0540039 120050118A575565464519 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU NR 2 SPOILER PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 OKC - NR 2 SPOILER UPPER SKIN IS DELAMINATED AND PUNCTURED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050407002332005040700233EA 2005 4 7 SWIA200514819 120050322A27508004301 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07442SW 7609 FLAPS DEGRADED MESSAGE. INSTALLED A SERVICEABLE SKEW DATABASE IAW 27-51-15 OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050407002372005040700237EA 2005 4 7 SWIA200514822 120050403A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07927SW6044 6044 7693 STAB TRIM CH1 INOP STATUS MESSAGE WILL NOT EXTINGUISH. REMOVED AND REPLACED HORIZONTAL STAB TRIM ACTUATOR (HSTA) AND MOTOR CONTROL UNIT (MCU) IAW MM 27-40-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050407002412005040700241EA 2005 4 7 COMA0560223 120050403A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAULTY A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01709CA17446 7238 FLIGHT 5446 RECEIVED A FLAP FAIL CAUTION AFTER LANDING WHEN FLAPS WERE RETRACTED. REPLACED THE LEFT BPSU. 2L72 4F RTA21EA 20050407002432005040700243NM 2005 4 7 72300110 120050323A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 6 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050407002452005040700245NM 2005 4 7 72300112 120050323A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 4 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050407002482005040700248NM 2005 4 7 72300114 120050323A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 2 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050407002502005040700250NM 2005 4 7 72300117 120050323A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A .75 X 2.5 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050407002532005040700253NM 2005 4 7 72300119 120050218A5320 SHEAR WEB BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 SEVERAL AREAS OF CORROSION ON BOTTOM OF SHEAR WEB. 2L73 4F4 FRTA3WE E2EA 20050407002552005040700255EA 2005 4 7 VTZA200500031 120050331A5210 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27638BR 7311 PAX DOOR INTERCOSTAL TOP RADIUS CRACKED AT 1 INCH IN LENGTH AT DATUM 1 FS 338. 2L72 4F RTA21EA 20050407002572005040700257EA 2005 4 7 VTZA200500035 120050331A531260034017595 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27638BR 7311 BULKHEAD AT FS 280 BETWEEN RBL 9.0 AND LBL 9.0 HAS LEVEL 2 CORROSION ON WEB .020 INCH DEEP. 2L72 4F RTA21EA 20050407002592005040700259 2005 4 7 CALA0500098 420050404A2565D31354418 SLIDE BOEING737 737524 1384721NM L-2 DOOR DISCHARGED A CALAK NONE O OTHER ININSP/MAINT 1 SW271460146158 27314 INSPECTION FOUND THE L-2 DOOR EMERGENCY ESCAPE SLIDE BOTTLE PRESSURE LOW. THE SLIDE ASSEMBLY WAS REPLACED IAW MM 25-61-35. 2L72 4F RTA16WE 20050407002632005040700263EA 2005 4 7 SWIA200514824 120050401A2520 OXYGEN MASK CNDAIRCL600 CL6002B19 1900309EA SEATS 1CD UNWANTED DEPLOY A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07413SW 7102 THE O2 MASKS IN SEATS 1C AND D DEPLOYED AND WILL NOT STOW. REPLACED PSU AT 2C AND D. STOWED O2 MASKS AT 1C AND D. OPERATIONAL CHECK GOOD IAW 25-20-00. 2L72 4F RTA21EA 20050407002642005040700264NM 2005 4 7 SWAA050940 120050328A53116546539 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29364SW 26575 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, BELOW RT CREASE BEAM WEB. REPAIRED FRAME PER TYPICAL REPAIR. 2L72 4F RTA16WE 20050407002692005040700269SO 2005 4 7 SWIA200514825 120050401A2797 WIRE EMB 120 EMB120ER 3260203SO CONNECTOR BROKEN A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07189SW 120048 ON TAXI CHECK, FLAPS SET 15 DEGREES; OUTBOARD FLAPS CONTROL FAULT. REPAIRED BROKEN WIRES ON CONNECTOR CONNECTED TO THE RIGHT HAND OUTBOARD FLAP IAW WM 20-21-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050407002712005040700271EA 2005 4 7 SWIA200514827 120050402A27604916405 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07409SW9885 9885 7056 FLIGHT SPOILERS FAULT AND INBOARD GROUND SPOILERS FAULT STATUS MESSAGES. REPLACED NR 2 SECU IAW MM 27-61-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050407002752005040700275EU 2005 4 7 2005UALA00267 120050326A4900 IDG AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 2 SHUTDOWN A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29441UA 751 APU AUTO SHUTDOWN WITH THE NR 2 IDG DEFERRED. REPLACED PRECAUTIONARY PER SFOLM THE APU OIL PRESS SWITCH, OIL SUMP TEMP SENSOR, OIL LEVEL SENSOR, AND ECB. RAN APU ON GROUND FOR ONE HOUR WITH ELEC AND PNEU LOADS NO AUTO SHUTDOWNS. APU HAD 2 PREVIOUS GRND ASD. RPL'D FUEL CONTROL UNIT 27MAR05. NO OTHER HISTORY. OSV RECEIVED LRU'S APRIL 06, 2005 AND ALL LRU'S RECEIVED HAVE TESTED NFF EXCEPT FUEL CONTROL UNIT. FUEL CONTROL UNIT FAILED TEST DUE TO DELTA P VALVE WAS OUT OF CALIBRATION. THE ACTUATOR REGULATOR WAS DEFECTIVE AND THE DRIVE SHAFT SEAL WAS LEAKING. THE ASD, NO START CAN BE ATTRIBUTED TO A FAILING FUEL CONTROL UNIT. 2L72 4F4 FRTA28NM E40NE 20050407002782005040700278EA 2005 4 7 SWIA200514828 120050330A274084897132 MOTOR CNDAIRCL600 CL6002C10 1390015EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07709SK1744 1744 10159 STAB CH2 INOPERATIVE STATUS MESSAGE. REPLACED HSTA MOTOR NR 2 PER AMM 27-42-03. OPERATIONAL CHECK GOOD IAW 27-40-00-710-801 A02. 2L72 4F RTA21EA 20050407002802005040700280EA 2005 4 7 SWIA200514806 120050326A2760270007 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07590SW4231 4231 7077 SPOILERONS STATUS MESSAGE. REPLACED RIGHT OUTBOARD SPOILERON PCU IAW CRJ MM27-62-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050407002902005040700290WP 2005 4 7 AALA20050030 120050115A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21228AA 49178 LAX - EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACKS AT B5101, B5100, AND B5105 FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050407002922005040700292SO 2005 4 7 MASA200500026 120050111A33501317 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07828MJ 145218 ASH 2819 IN CLT, REPORTED A CABIN OVERHEAD EMERGENCY EXIT LIGHT INOP. MAINTENANCE RELAMPED THE EXIT LIGHT. 2L72 4T RTT00011AT 20050407002942005040700294EU 2005 4 7 MALA050123 120050108A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15425XJ 340B425 DURING 4Y/2Y CHECK IN BNA, SEAT TRACK AT LBL 18.3 BETWEEN FS 294-319 IS CORRODED OUT OF LIMITS AND HAS BEEN REMOVED AND REPLACED AS NEEDED IAW MESABA EO NR S53060. REFER EAMS WO NR 211363, TASK 1511 FOR ADDITIONAL INFORMATION. AIRCRAFT WAS RELEASED 1/11/05. 2L72 4T RTA52EU 20050407002972005040700297EU 2005 4 7 MALA050109 120050107A3030QR50V SENSOR SAAB SF340 340B 7860101EU LT PITOT HEAT DEFECTIVE A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15446XJ 340B446 LEFT PITOT LIGHT ILLUMINATED. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED LT PITOT HEAT CURRENT SENSOR 5HG PN ON/OFF QR50V. LT PITOT HEAT OPS CHECKS GOOD IAW SF 340 AMM CHAP 30-30-00-5. 2L72 4T RTA52EU 20050407003042005040700304NM 2005 4 7 SWAA050944 120050328A534065C27314 STRINGER CLIP BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29501SW 24178 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050407003062005040700306NM 2005 4 7 SWAA050930 120050327A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29341SW 24091 DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 919, STR 22L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050407003092005040700309NM 2005 4 7 05FDEA00852 120050405A5514 STRUCTURE DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT UPPER AFT SKIN PLANK NR29R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82942. 2L73 4F RTA22WE 20050407003102005040700310NM 2005 4 7 05FDEA00860 120050406A5514 STRUCTURE DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT UPPER FORWARD SKIN PLANK NR 5L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82991. 2L73 4F RTA22WE 20050407003112005040700311WP 2005 4 7 05FDEA00846 120050405A5753ARC25131 HINGE DOUG DC10 DC1030F 3023504WP T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25301FE 46800 FLAP MOUNTED HINGE PIVOT BORE CORROSION REPAIR P/NARC2513-1. COMPLIED WITH EA 8-5750-55462. 2L73 4F RTA22WE 20050407003122005040700312EU 2005 4 7 05FDEA00850 120050405A5315 FLOORBEAM AIRBUS310 A310 EU FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 REPAIR NEEDS EVALUATION FOR FAA APPROVED DATA AND MAJOR OR MINOR CLASSIFICATION. FLOORBEAM NR 34 R L OF CENTER LINE. COMPLIED WITH FEDEX EA NR 6-5310-87772 AND CLASSIFIED AS A MINOR REPAIR PER FEDEX EA NR 6-5310-87772 AND FEDEX GMM 6-2-100. 2L72 4F RTA35EU 20050407003162005040700316NM 2005 4 7 05FDEA00832 120050404A5330 SKIN BOEING727 727233 138408ANM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25272FE 22037 DENT IN EXTERNAL FUSELAGE SKIN AT BS 1345 BY LEFT AFT CORNER OF AIRSTAIR CUT OUT. REPAIRED DENT PER SRM 54-30-3. 2L73 4F RTA3WE 20050407003262005040700326NM 2005 4 7 72300115 120050323A5340 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 3 X 1 INCH AREA OF CORROSION ON BOTTOM OF SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050407003282005040700328NM 2005 4 7 72300132 120050330A5340 STRINGER CLIP BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 1.5 INCH AREA OF CORROSION ON STRINGER CLIP. 2L73 4F4 FRTA3WE E2EA 20050407003302005040700330EU 2005 4 7 05FDEA00566 120050315A5330 SKIN AIRBUS310 A310 EU FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 REPAIR NEEDS EVALUATION FOR FAA APPROVED DATA AND MAJOR OR MINOR CLASSIFICATION. ITEM NR 27 OF LIST FUSELAGE DOUBLER TOP RT SIDE AT FR 78. FUSELAGE DOUBLER ON TOP RT SIDE AT FRAME 78 FOUND TO BE IN CONFORMANCE WITH A310-200 SRM 53-10-12 FIG 216 THIS REPAIR IS BOUND TO INSPECTIONS AT DEFINED INTERVALS IN SRI 53-10-12-2-001. (SEE JPF). 2L72 4F RTA35EU 20050407003312005040700331NM 2005 4 7 05FDEA00714 120050330A5347 CARGO TRACK DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 MAIN DECK CARGO COMPARTMENT FLOOR TRACK AT STA Y= 635, X= 47, FOUND CRACKED APPROXIMATELY THREE (3) INCHES LONG. REMOVED SEAT TRACK IAW SRM 51-31-01 VOLUME II. FABRICATED PARTS IAW SRM 53-70-00 VOLUME I, FIGURE 1. PARTS INSTALLED IAW SRM 50-70-00 VOLUME I, FIGURE 1 AND SRM 51-31-00 VOLUME II. 2L73 4F RTA22WE 20050407003322005040700332EU 2005 4 7 05FDEA00574 120050316A5330 SKIN AIRBUS310 A310 EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 CORR B/T STR 34-35 FROM FS 39 AFT APPROX 8 IN LT REF N00850. COMPLIED WITH EA 6-5315-86078. 2L72 4F RTA35EU 20050408000022005040800002NM 2005 4 8 DHL2005782555 120050317A5330 SKIN BOEING727 727227 1384078NM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 ACCOMPLISH IDENTIFICATION OF EXISTING REPAIR ON FUSELAGE SKIN AT A/C STA 406 STRINGER 24R PER ASTAR J/C NR FCD500001-001B. EXISTING REPAIR FOUND TO BE NON-COMPLIANCE IAW 727 SRM 53-30-3 FIG 1. REMOVED PREVIOUS REPAIR IAW 727 SRM 51-30-2. FABRICATED NEW DOUBLER FROM 2024 T3 .050 PO NR 9002012 DIM 10 7/16" BY 8 1/4" IAW 727 SRM 53-30-2 FIG 1 AND 53-30-3 FIG 1. TREATED AND PRIMED IAW 727 SRM 51-10-2. INSTALLED REPAIR DOUBLER IAW 727 SRM 51-30-2. 2L73 4F A3WE 20050408000032005040800003NM 2005 4 8 ASMF200504001 120050402A21335653732 HOUSING DOUG MD88 MD88 3023688NM OUTFLOW VALVE FAILED W ASMFA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW23169PL 53175 AIRCRAFT PERFORMED AN UNSCHEDULED LANDING AS A CONSEQUENCE OF BOTH CABIN PRESSURE CONTROL VALVES WERE OUT SERVICE AND CABIN ALTITUDE ROSE TO 9500. IT WAS NECESSARY TO CONTROL PRESSURE IN MANUAL DUE TO AN OBSTRUCTION OF WHEEL CONTROL. IN GROUND, BOTH SYSTEM WERE CHECKED AND WORKED NORMAL IAW MM 21-32-03. DURING OVERNIGHT SERVICE, THE OUTFLOW VALVES BODY WAS REPLACED, ADJUSTED AND TESTED. RIGGING WAS PERFORMED TO CABLES 119-B AND 120-B IAW MM 21-32-05, TESTED CORRECT. A PRESSURIZATION TEST WAS PERFORMED 3 TIMES IN MANUAL AND AUTOMATIC, ALL CORRECT. 2L72 4F RTA6WE 20050408000042005040800004NM 2005 4 8 QXEA200500494 120050309A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09366PH 510 PDX - NR 4 SEAT TRACK HAS PITTING CORROSION THAT IS BEYOND BLENDABLE LIMITS. REPLACED IAW RD 8-53-4473, 8-51-102 AND 8-53-1102. 2H72 4T RTA13NM 20050408000072005040800007NM 2005 4 8 QXEA200500490 120050311A5412 FIREWALL DHAV DHC8 DHC8202 2809007NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09366PH 510 PDX - NR 1 ENGINE NACELLE, AFT FIREWALL INBOARD SIDE POSSIBLE CRACK AT STATION XN125/YW142/ZN9.5. REPAIRED IAW HORIZON AIR EA 2-54-223. 2H72 4T RTA13NM 20050408000082005040800008NM 2005 4 8 QXEA200500492 120050312A5330 SKIN DHAV DHC8 DHC8202 2809007NM ZONE 100 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09366PH 510 PDX - STATION X320 Z95 DENT IN FUSELAGE SKIN. REPAIRED IAW HORIZON AIR EA 2-53-611. 2H72 4T RTA13NM 20050408000102005040800010NM 2005 4 8 DHL2005782563 120050323A5330 SKIN BOEING727 727227 1384078NM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 REMOVED AND REPLACED FASTENER ON NR NR 82194, BELOW STA 19R SAT 680 NEED TO EVALUATE MATERIAL LOSS FROM BLEND OUT. MEASURED BLEND OUT AT STA 680 STR 19R AND FOUND OUT OF LIMITS A.6/Y.028=21.4 IAW B727 SRM 53-30-1 FIG 1. FABRICATED DOUBLER MATERIAL IDENTIFICATION 53-30-2 FIG 2 FROM MATERIAL 2024T3 .071 PIO NR 9001737 DIMENSION 10 1/4" BY 8 1/4" AND FILLER FROM MATERIAL 2024T3 .063 PO NR 9001978 DIMENSION 5 3/4 BY 3 3/4 IAW B727 SRM 53-30-3. CUT OUT DAMAGED AREA 5 3/4" BY 3 3/4 IAW B727 SRM 53-30-3 FIG 3A ALODINE AND PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED DOUBLER AND FILLER IAW B727 SRM 53-30-3 FIG 3A. THIS REPAIR IS A CATEGORY "A". 2L73 4F A3WE 20050408000112005040800011NM 2005 4 8 DHL2005782564 120050324A5330 SKIN BOEING727 727227 1384078NM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 INSTALL B727 GPS ANTENNA DOUBLER AT BS 360-380 BETWEEN STR 1 AND 2R PER DECRANE AIRCRAFT EO NR 2757-3460-150 REV A. INSTALLED B727 GPS ANTENNA DOUBLER AT BS 370 BETWEEN STRINGERS 1 AND 2R PER DECRANE AIRCRAFT EO NR 2757-3460-150 IAW DWG NO 2757-3460-1045 REV A DOUBLER PN 40503-03 DIM 6.88"BYX 5.25". 2L73 4F A3WE 20050408000122005040800012NM 2005 4 8 DHL2005782562 120050322A5754 SKIN BOEING727 727227 1384078NM NR 2 SLAT DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 NR 2 LE SLAT EXTERNAL SKIN HAS DENT WS 684.3 (AREA MARKED). DENT AT WS 684.3 ON NR 2 SLAT SKIN OUT OF LIMITS A.9/Y.032=28.1 IAW B727 SRM 57-50-1 FIG 1. CUT OUT DAMAGE AREA SIZE 1" BY 1" IAW B727 SRM 57-50-1. FABRICATED DOUBLER REPAIR USING 2024T3 .080 PO NR 9002012 DIM 6" BY 5" IAW B727 SRM 57-50-3 FIG 1. ALODINED AND PRIMED DOUBLER IAW B727 SRM 51-10-2. INSTALLED DOUBLER AT WS 684.3 #2 SLAT OUTER SKIN IAW B727 57-50-3 FIG 1 2L73 4F A3WE 20050408000132005040800013NE 2005 4 8 MASA200500108 220050212A73206078T55P26 FUEL CONTROL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 1 ENGINE FLUCTUATES A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0717358468 7358 ASH 6108 PHX TO PSP, RETURNED TO THE FIELD WITH NR 1 ENGINE FUEL FLOW, ITT, AND OVERSPEED SITUATION. MAINTENANCE IS IN WORK. 2/13/05 MAINTENANCE REMOVED AND REPLACED NR 1 FCU, OPS CHKD GOOD. 2L72 4F4 FRTA21EA E15NE 20050408000152005040800015NM 2005 4 8 MASA200500261 120050330A2913570347 PUMP DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE NR 2 ENGINE FAILED A MASAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 SW07456YV7184 3753 456 TMAG0006 ASH 7059 DEN-GUC - THE AIRCRAFT RETURNED TO FIELD WITH NR 2 ENGINE HYD PUMP AND ROLL SPOILER HYD CAUTION LIGHTS. MAINTENANCE FOUND THE NR 2 ENGINE PUMP BAD AND CHANGED THE PUMP. 2H72 4T4 TRTA13NM E20NE 20050408000162005040800016NM 2005 4 8 DHL2005782560 120050322A5522 SKIN BOEING727 727227 1384078NM RT ELEVATOR DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 ACCOMPLISH IDENTIFICATION OF EXISTING REPAIR ON RT ELEVATOR LOWER SKIN AT STAB STA 106 PER ASTAR J/C NR FCD500001-001B. REPAIR ON RT ELEVATOR LWR SKIN AT STAB STA 106 FOUND TO BE IN NON-COMPLIANCE IAW 727 SRM 55-20-3 FIG 5. REMOVED REPAIRS 2 EA FOR INCORPARATION IAW 727 SRM 51-30-2. FABBED NEW DOUBLER FROM 2024-T3 /032 PO NR 9002034 DIM 10 INCH BY 9 1/4 INCH IAW 727 SRM 55-20-3 FIG 5. DOUBLER TREATED PRIMED AND INSTALLED IAW 727 SRM 51-10-2 AND 55-20-3 FIG 5. CALCULATED ELEVATORS NEW MOMENT OF 121.06 IS WITHIN THE LIMITS 120+- 20 POUND-INCHES, NO FURTHER ACTION REQUIRED IAW 727 SRM 51-80-7. 2L73 4F A3WE 20050408000172005040800017NM 2005 4 8 DHL2005782565 120050326A5720 WEB BOEING727 727227 1384078NM RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 RT WING TIP WEB CRACKED AT THE UPPER AND LWR FLANGES. ON RT WING TIP REMOVED CRACKED WEB IAW B727 SRM 51-30-2. FAB NEW WEB FROM 7075T6 .040 PO NR 9001068 14" BY 9" IAW B727 SRM 57-20-2 FIG 3. TREATED AND PRIMED IAW B727 SRM 51-10-2 INST IAW B727 SRM 51-30-2. 2L73 4F A3WE 20050408000212005040800021WP 2005 4 8 IXXA0500061O 120050406A793142D391C TRANSMITTER DOUG DC8 DC862F 3021972WP PWA JT3D JT3D7 52039NE OIL PRESSURE BROKEN A IXXAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW1171CX 663392633 45961 644664 AFTER TAKEOFF FROM TAPA NR 1 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED. CREW PERFORMED ENGINE SHUTDOWN CHECK LIST AND CREW RETURNED AIRCRAFT TO TAPA AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE DIFFERENTIAL TRANSMITTER PER ALL APPLICABLE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F4 F 4A25 1E8 20050408000242005040800024WP 2005 4 8 DHL2005805001 120050407A33505708458505 RELAY DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01805DH 46125 DURING PREFLIGHT INSPECTION, THE EMERGENCY LIGHTS DID NOT ILLUMINATE DURING BATTERY CHECK. REMOVED AND REPLACED EMERGENCY BATTERY RELAY UNIT IAW DC-8 M/M 33-50-1. OKAY FOR SERVICE. 2L74 4F RT4A25 20050408000262005040800026NE 2005 4 8 ASMF200503019 220050326A73201853MB3P06 EEC BOEING737 737724 13844BYNM CFMINTCFM567CFM567B22 13802NE RIGHT FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23997AM 30283 889997 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF RIGHT ENGINE, N2 AND OIL PRESS WARNINGS TURNED ON. DURING CHECK, THERE WERE DETECTED RECENT FAULTS IN CDU WITH LEGENDS EEC NR 2 SUPPLY AND 73-21282-FAIL CODE. ENGINE WAS RESTARTED, SHUTTING DOWN AUTOMATICALLY AT 21 PERCENT OF N2. BOTH EEC SWITCHES WERE PUTTED ON P5 ALTERNATE MODE AND ENGINES WERE STARTED NORMALLY. REPORT WAS DEFERRED IAW MM 73-11-1. DURING OVERNIGHT SERVICE, EEC WAS REPLACED IAW MM 73-21-60. 2L72 4F4 FRTA16WE E00055EN 20050408000272005040800027NM 2005 4 8 ASMF200503020 120050327A7160A648475 INLET GUIDE VANE BOEING757 7572Q8 1384972NM LT ENGINE FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23806AM5925 26273 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF CAPTAIN REPORTED APU PNEUMATIC PRESSURE DOWN TO 8 PSI WHEN LEFT ENGINE STARTED INSULATION VALVE WAS OPENED. ENGINES WERE STARTED WITH A GPU AND REPORT WAS DEFERRED IAW MEL 49-11-01. DURING OVERNIGHT SERVICE, ECU WAS CHECKED AND IT HAD FAIL CODE OF IGV ACTUATOR. IT WAS REPLACED IAW MM 49-52-02, TESTED CORRECT. 2L72 4F RTA2NM 20050408000282005040800028WP 2005 4 8 ASMF200503021 120050330A7711LG80E1 TRANSMITTER DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE LT ENGINE EPR FAILED W ASMFD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SW23754RA19536 49641 726174 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF LEFT ENGINE EPR'S WERE IN 1.2. EPR INDICATOR EGG WERE REPLACED IAW MM 77-11-01 AND 77-11-02 RESPECTIVELY, TESTED CORRECT. ENGINE WAS TESTED IAW MM 71-00-00, ALL CORRECT. 2L72 4F4 FRTA6WE E9NE 20050408000292005040800029NM 2005 4 8 QXEA200500496 120050328A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09366PH 510 PDX - RIGHT OUTBOARD SEAT TRACK NR 11 HAS CORROSION IN TRACK GROOVE BETWEEN STATION X435 AND X438. REPAIRED IAW DHC-8 200 SRM 51-40-00 AND SRM 51-40-11. 2H72 4T RTA13NM 20050408000302005040800030EU 2005 4 8 05FDEA00829 120050404A7830 LATCH AIRBUS310 A310 EU THRUST REVERSER DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 REPAIR NEEDS EVALUATION FOR FAA APPROVED DATA AND MAJOR OR MINOR CLASSIFICATION. NR 2 ENGINE NACELLE O/B T/R BELOW AFT UPPER LATCH. (ITEM NR 51 OF LIST) REMOVED EXISTING REPAIR DOUBLER PER A310 SRM 51-40-21 AND COMPLIED WITH FEDEX EA # 6-7830-87224, THIS REPAIR IS CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100. 2L72 4F RTA35EU 20050408000312005040800031EU 2005 4 8 05FDEA00830 120050404A5531 RIB AIRBUS310 A310 EU VERTICAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 VERTICAL STAB RT SIDE 6" BELOW RIB 21 TO RIB 1 HAS CORROSION ON REAR CHORD SPAR CHORD FLANGE IN FASTERNER HOLES, AROUND FASTERNER HOLE AREA EXTENDING TO STAB SKIN AS MARKED. REMOVED NUPLATES IAW A310-200 SRM 51-40-21. REMOVED CORROSION IAW A310-200 SRM 51-74-10. CHECKED LIMITS IAW A310-200 SRM 55-30-00 TABLE 101. ALL AREAS ARE IN LIMITS EXCEPT FOR HOLE NR 15,18, 25 IAW SRM 55-30-00. HOLES 15,18 25 ARE IN LIMITS IAW OE-345-03-05-023. TREATED, PRIMED TOP COATED IAW SRM 51-23-20 51-75-10. REINSTALLED NUT PLATES IAW A310-200 SRM 51-40-21. COMPLIED WITH EA6-5510-87215. 2L72 4F RTA35EU 20050408000322005040800032NM 2005 4 8 05FDEA00869 120050406A5740651621813 FITTING BOEING727 727227 1384078NM WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 BLENDED DAMAGE IN WING TERMINAL FITTING OUT OF LIMITS. REPAIRED LEFT WING BODY FITTING PER FED EX EA 7-5340-86266. 2L73 4F A3WE 20050408000332005040800033NM 2005 4 8 05FDEA00870 120050406A5340651621813 FITTING BOEING727 727227 1384078NM WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 WING FITTING REQUIRED RESLEEVING DUE TO BLENDED DAMAGE OUT OF LIMITS. SO, THE BODY FITTING ALSO NEED TO BE RESLEEVED. REPAIRED LT 740 WING TERMINAL FITTING PER FED EX EA 7-5710-86260. 2L73 4F A3WE 20050408000352005040800035NM 2005 4 8 QXEA200500498 120050309A5730 SKIN DHAV DHC8 DHC8202 2809007NM ZONE 600 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09366PH 510 PDX - 623AT HAS FRETTING CORROSION IN COUNTER SINKS. REPAIRED IAW DHC-8 200 RD 8-57-1715. 2H72 4T RTA13NM 20050408000362005040800036 2005 4 8 MASA200500150 420050223A34971796002030016 WIRE HARNESS DHAV DHC8 DHC8202 2809007NM FMS BURNED A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW07444YV116 444 ASH 7063 EGE-DEN - AFTER SHUTDOWN CREW REPORTED AN ELECTRICAL SMELL IN THE COCKPIT. DEN MAINTENANCE RAN A/C AND FOUND WIRE BUNDLE INSIDE OF FMS BOX CAUSING SHORT AND POPPING CB'S. 3/3 MX REMOVED AND REPLACED FMS. 2H72 4T RTA13NM 20050408000372005040800037NM 2005 4 8 DHL2005782558 120050318A2760 HINGE BOEING727 727227 1384078NM NR 3 SPOILER CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 L/WING T/E SURFACE CRACKED AT NR 3 SPOILER HINGE CUTOUT (3RD). REMOVED NR 3 SPOILER TO FACILITATE S/M WORK IAW 7727-61-0 STOP DRILL CRACK IAW B727 SRM 51-10-1. FABRICATED DOUBLER USING7075 T6 .071 PO NR 9001737 DIM 6 1/4" BY 4" IAW B727 SRM 57-30-04 FIG 10. TREATED AND PRIMED PART IAW B727 SRM 51-10-2. INSTALLED DOUBLER IAW B727 SRM 57-30-04 FIG 10. 2L73 4F A3WE 20050408000382005040800038GL 2005 4 8 CHQA200500065 220050329A7200 ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 2 FAILED A CHQAEA ENGINE SHUTDOWN UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 GL11370SK1026910269 145515 CAE311655 CLIMBING, BOOM HEARD FROM RT SIDE OF A/C. LOOKED AT INSTRU ON NR 2, ITT TO RED. THRUST LEVER TO IDLE. ENG 2 OUT ON EICAS & DECLARED EMERGENCY. PROCEEDED W/E-2 OUT ABNORM CHKLST. ENG SHUTDOWN CHKLST. DISPATCH CONTACTED & DIVERT TO KBDL. CHKD ENG INSTS, & OIL QTY 10 QTS. ENG AIRSTART CHKLST W/APU ASSIST START. DURING START, NO ITT RISE. SHUTDOWN AGAIN. OEI APPROACH & LANDING W/OEI GO ROUND CHKLST COMPLETE. NORM DESCENT, APPROACH & LANDING, LANDING CHKLST COMPLETE. EICAS MESSAGES NOT NORMAL. E2 EXCEED, E2 NO DISP & E2 SHORT DISP. RAN AFTER LANDING CHKLST & NO EVAC OR EMERG VEHICLE ASSIST. MX INSPECT ENG & FOUND METAL IN EXHAUST. R / R NR 2 ENG, PERFORMED ENG RUNS. OPS & LEAK CHECK GOOD. 2L72 4T4 FRTT00011ATTE6CH 20050408000392005040800039NM 2005 4 8 ASMF200503023 120050331A3411 PITOT LINE DOUG MD80 MD83 3023681NM AIR SPEED MISUSED W ASMFC ABORTED TAKEOFF WJ INADEQUATE Q C WARNING INDICATION TOTAKEOFF 1 SW23881LF 53051 AIRCRAFT REJECTED TAKEOFF AND RETURNED TO PLATFORM AS A CONSEQUENCE OF AT 80 KTS, THE AUXILIARY AIR SPEED INDICATOR SHOWS O KTS. DURING CHECK, MAINTENANCE PERSONNEL DETECTED THAT THE PITOT PNEUMATIC LINE WAS WRONGLY CONNECTED AND LOOSED. ADDITIONALLY THE STATIC PRESS LINE CONNECTOR AND THE NIPPLE TO JOINT THE STATIC PITOT TUBE TO THE INDICATOR WERE WITH SEVERAL DAMAGES. BOTH CONSUMABLE ITEMS WERE REPLACED AND AUXILIARY PITOT TUBE LEAK TEST AND SPEED INDICATION TEST WERE PERFORMED IAW MM 34-13-02, ALL CORRECT. 2L72 4F RT 20050408000402005040800040SO 2005 4 8 SWIA200514647 120050225A2731 TRIM SWITCH EMB 120 EMB120ER 3260203SO COCKPIT INOPERATIVE A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07221SW 120290 ELECTRIC TRIM SWITCH INOPERATIVE ON CAPTAINS SIDE. REPLACED CAPTIANS TRIM SWITCH. OPERATIONAL CHECK GOOD IAW MM 22-10-00. 2L72 4T RTA31SO 20050408000422005040800042SO 2005 4 8 SWIA200514649 120050224A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT INTERMITTENT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07569SW8571 8571 120344 FA REPORTS EMERGENCY LIGHTS FROM ROW 9 AFT WORK INTERMITTENTLY. REPLACED AFT CABIN EMERGENCY LIGHT BATTERY PACK. 2L72 4T RTA31SO 20050408000452005040800045NE 2005 4 8 EGRA2005212 120050122A67107630103901102 ACTUATOR SKRSKYS76 S76 8143010NE ALLSN 250C 250C30 03013GL AFCS FROZEN E EGRAA UNSCHED LANDING F FLT CONT AFFECTED HOHOVERING 1 EA17764MH 760181 AIRCRAFT WAS LIFTED TO HOVER PRIOR TO FLIGHT. CONTROL INPUTS SEEMED SLUGGISH AS IF AFCS WAS OFF. AIRCRAFT WAS IMMEDIATELY LANDED, AFCS SYSTEM WAS CONFIRMED ON. FUNCTION CHECK PERFORMED AND ALL AFCS CHANNELS NOTED TO BE EITHER SLUGGISH OR INOP. HEAT WAS APPLIED TO ROLL AND PITCH ACTUATORS. GROUND RUN AIRCRAFT. OPERATIONAL CHECK OK. 1G72 3U3 U H1NE E1GL 20050408000462005040800046CE 2005 4 8 45165021505 120050215A29104529101088001 LINE LEAR 45 45LEAR 5170805CE HYD SYS LEAKING E J7SAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SW05429FX 165 CREW REPORTED "MAIN HYD QTY LOW" WHITE CAS FOLLOWED BY "LEFT HYD PUMP LOW", FOLLOWED BY "RIGHT HYD PUMP LOW", FOLLOWED BY AMBER "MAIN HYD PRESS" CAS MESSAGES. CREW DECLARED EMERGENCY AND LANDED AT DESTINATION AIRPORT WITHOUT INCIDENT. AFTER LANDING FOUND HYD FLUID COVERING RT ENGINE COWL. MAINTENANCE FOUND HYD PRESS LINE IN CONTACT WITH RETURN LINE RESULTING IN CHAFFING AND SUBSEQUENT LINE FAILURE. LINES REPLACED AND OPS CHECKS PERFORMED SATISFACTORILY. SECOND INCIDENT OF IDENTICAL PROBLEM WITHIN ONE MONTH. 2L72 4F RTT00008WI 20050408000532005040800053NM 2005 4 8 TSAA0527016 120050312A2751 SENSOR BOEING737 73773A 1384606NM TE FLAPS INTERMITTENT A TSAAO OTHER N FALSE WARNING APAPPROACH 1 WP13738AL 28499 ON APPROACH, FLAPS STUCK AT 5 DEGREES. NO OTHER WARNING INDICATIONS. SET FLAPS USING ALTERNATE FLAP UNIT. UNEVENTFUL LANDING AT ONT. MAINTENANCE PERFORMED FSEU BITE CHECK PER AMM 27-51-00-810-802. NO EXISTING FAULTS NOTED. FAULT HISTORY SHOWS TE FLAP SENSOR LEFT INTERMITTENT FAULT. PERFORMED TE FLAP OPS CHECK PER AMM 27-51-00-810-836. OPS CHECK OK. FLIGHT VERIFICATION, FLAPS CYCLED TO 40 DEGREES ON LANDING. FLAPS CYCLED OKAY. NOTED BY MAINTENANCE. FLIGHT VERIFICATION ACCOMPLISHED. 2L72 4F RTA16WE 20050408000542005040800054EA 2005 4 8 COMA0570025 120050308A532067053110522 WEB CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01641CA3959 10122 FS 280 - LT AND RT BULKHEADS AND TRANSVERSE BEAM HAVE MAJOR CORROSION ON AFT SIDE ALONG THE BOTTOM EDGES. REPLACED LOWER WEBS AT FS 280 BULKHEAD I/A/W BOMBARDIER INC REO 670-53-11-052, REV A AND BRAS EO 601R-53-6066. REPLACED TRANSVERSE BEAM I/A/W BOMBARDIER INC REO 670-53-11-047 REV A AND BRAS EO 601R-53-6066. 2L72 4F RTA21EA 20050408000552005040800055EA 2005 4 8 COMA0570026 120050308A53106753110471 BEAM CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01641CA3959 10122 FS 280 LT AND RT BULKHEADS AND TRANSVERSE BEAM HAVE MAJOR CORROSION ON AFT SIDE ALONG THE BOTTOM EDGES. REPLACED LOWER WEBS AT FS 280 BULKHEAD IAW BOMBARDIER, INC. REO 670-53-11-052, REV A REPAIR NR 2 AND BRAS E.O. 601R-53-6066. REPLACED TRANSVERSE BEAM I/A/W BOMBARDIER INC REO 670-53-11-047 REV A AND BRAS EO 601R-53-6066. 2L72 4F RTA21EA 20050408000562005040800056NM 2005 4 8 05FDEA00575 120050316A5230 DOOR FRAME BOEING727 727200 138407ENM CARGO DOOR GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 MAIN CARGO DOOR AFT SIDE FRAME PREVIOUS REPAIR GOUGED 18 INCHES FROM BOTTOM OF DOOR. REMOVED AND REPLACED REPAIR ON MCD AFT SIDE FRAME PER SRM 51-20-1. 2L73 4F RTA3WE 20050408000572005040800057NM 2005 4 8 DHL2005782508 120050310A5210 SKIN BOEING727 727227 1384078NM PAX DOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 FWD ENTRY DOOR OUTBOARD SIDE TOP RT CORNER SKIN DENTED. STOP DRILLED CRACK SIZE .250 IAW B727 SRM 51-10-1. FABRICATED DOUBLER REPAIR USING 2024T3 .050 PO NR 9001873 SIZE 5 3/4" BY 4 3/4" IAW B727 SRM 52-10-1 FIG 1AND 52-00-3 FIG 3. TREATED AND PRIMED AREA AND PART IAW B727 SRM 51-10-2. ACCOMPLISHED 727 HFEC INSPECTION 51-00-00 FIG 4. CRACK CONTAIN CONFIRMED INSTALLED DOUBLER REPAIR IAW B727 SRM 51-30-2. 2L73 4F A3WE 20050408000582005040800058 2005 4 8 05FDEA00767 420050331A2311A23190201200 SPAR AIRBUS310 A310 EU VERTICAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 VERT STAB FRONT SPAR ANTENNA HAS PITTING CORROSION IN SEVERAL AREAS. REMOVED AND REPLACED 1 EA ANTENNA IAW A310-200 AMM 23-11-11-4. OPS CHECK NOT REQUIRED HF SYSTEM IS DEACTIVATED. 2L72 4F RTA35EU 20050408000612005040800061NM 2005 4 8 2005UALA00097 120050125A55126573783 SKIN BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE HORIZONTAL STAB DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29905UA 25005 LEFT HORIZONTAL STABILIZER HAS A DENT IN THE LEADING EDGE, FOUND DENT APPROX 4 FT OUTBD ON L/E HORZ STAB. DIMENSIONS ARE 3 INCH BY 2 INCH BY .25 INCH DEEP WITHIN 1 INCH OF FASTENERS. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INTERIM DOUBLER REPAIR REPLACED WITH PERMANENT FLUSH REPAIR. 2L72 4F4 FRTA16WE E2GL 20050408000622005040800062NM 2005 4 8 2005UALA00098 120050125A55126573783 SKIN BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE HORIZONTAL STAB DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29907UA 25007 LT HORIZ STAB LEADING EDGE IS DENTED APROX 4' FROM FUSE. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REMOVED DENT DAMAGE AND INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20050408000642005040800064CE 2005 4 8 021705N308CS1 120050217A783053ND783041 SWITCH CESSNA500 550 2076604CE THRUST REVERSER OUT OF TOLERANCEE Z5FAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NE03308CS 5500976 THRUST REVERSER UNLOCK LIGHT ILLUMINATED AFTER TAKEOFF. PILOT PERFORMED EMERGENCY PROCEDURES CHECKLIST AND LANDED AIRCRAFT BACK AT DEPARTURE FIELD (TEB). MAINTENANCE PERFORMED OVERWEIGHT LANDING INSPECTION AND TROUBLESHOOT FAULT TO INDICATION PROBLEM. REPLACED BOTH STOW SWITCHES. 1L72 4F A22CE 20050408000652005040800065NM 2005 4 8 DHL2005782507 120050309A5330 SKIN BOEING727 727227 1384078NM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 REMOVED 2EA RIVETS BS 500-520 STR 24-25R [MS20470 AD-8] AND INSTALL B727 SRM 53-30-3 FIG 23. REPAIR PER ASTAR J/C MSI53300277-001-B. REMOVED 2EA MS20470D-8 FASTENERS IAW 727 SRM 51-30-2. FABBED REPAIR DOUBLER FROM 2024T3 .080 PO NR 9002012 DIM 63 3/4 INCH BY 30 INCH IAW 727 SRM 53-30-2 FIG1 AND 53-30-3 FIG 23. DOUBLER TREATED PRIMED AND INSTALLED IAW 727 SRM 51-10-2 AND 53-30-3 FIG 23. 2L73 4F A3WE 20050408000662005040800066NM 2005 4 8 WRLA2005030 120050220A5512 SKIN DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST LT BARREL NUT HOLE NR 33. 2L73 4F4 FRTA22WE E24NE 20050408000672005040800067NM 2005 4 8 WRLA2005033 120050218A5512 SKIN DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST RT BARREL NUT HOLE NR 16. 2L73 4F4 FRTA22WE E24NE 20050408000682005040800068NM 2005 4 8 WRLA2005034 120050218A5512 SKIN DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST RT BARREL NUT HOLE NR 20. 2L73 4F4 FRTA22WE E24NE 20050408000702005040800070 2005 4 8 AALA20050139 420050222A3417 ADC AIRBUS300 A300B4605R 3930308EU COCKPIT INOPERATIVE A AALAA UNSCHED LANDING O OTHER CLCLIMB 1 SW2170074 517 MIA - INFLIGHT T2177/22 - AFTER TAKEOFF, THE NUMBER TWO AIR DATA COMPUTER FAULTED. LANDING GEAR WOULD NOT RETRACT IN POSITION NUMBER TWO. NUMBER TWO AIR DATA COMPUTER FAILURE. AUTOTHROTTLE FAILURE AND CABIN PRESSURE REGULATOR NUMBER TWO FAULT. ACCOMPLISHED BITE ON PROXIMITY DETECTOR PROCESSING UNIT AND FOUND FAULT AND BOX LIGHTS ON WITH FAULT CODES 04, 30 AND 31. REPLACED PROXIMITY DETECTOR PROCESSING UNIT. PROXIMITY BITE THEN SHOWED NOSE WHEEL CENTERED SENSOR FAULT. REPLACED SENSOR 82GB. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20050408000712005040800071WP 2005 4 8 AALA20050137 120050222A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW2176202 53292 DFW - FIRST CLASS CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FIRST CLASS CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050408000772005040800077EA 2005 4 8 QXEA200500232 120050218A3250 SWITCH CNDAIRCL600 CL6002C10 1390015EA ZONE 700 FAILED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09614QX7213 10049 SEA - FLIGHT 2467 - THE FLIGHT RETURNED TO THE GATE AFTER RECEIVING A STEERING INOP CAUTION MESSAGE. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE STEERING ARMING SWITCH. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20050408000822005040800082 2005 4 8 0500303243 420050302A256560592101 CABLE AIRBUS320 A320212 3930322EU ESCAPE SLIDE BROKEN A NWAAK NONE O OTHER ININSP/MAINT 1 GL01343NW359178495 387 DURING LIGHT CHECK, FOUND RIGHT OVERWING SLIDE RELEASE CABLE BROKEN BETWEEN COUPLING AND SLIDE INFLATION BOTTLE. REPLACED SLIDE INFLATION BOTTLE ASSEMBLY WITH CABLE PER AMM. 2L72 4F RTA28NM 20050408000832005040800083NM 2005 4 8 2005UALA00248 120050315A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29583UA 26705 EXTERNAL FUSELAGE SKIN IS DENTED AT 5 AREAS AT FUSELAGE STA 600 TO 625 BETWEEN STR 15LT AND 17LT. 2L72 4F4 FRTA2NM E17NE 20050408000842005040800084NM 2005 4 8 2005UALA00249 120050315A5310 TEAR STRAP BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSLEAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29583UA 26705 TEAR STRAP AT STA 1400 BETWEEN STR 27L AND 28L IS CORRODED. DAMAGE CAUSED BY TYPICAL CORROSION. TEAR STRAP REPAIR AND EXTERNAL DOUBLER WAS INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050408000852005040800085NM 2005 4 8 2005UALA00250 120050315A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE GOUGED A UALAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP29583UA 26705 AFT PIT FUSELAGE FRAME GOUGED IN 6 PLACES BS 1520 STR 22R TO 25R. DAMAGE TO FRAMES IN AFT PIT DUE TO NORMAL CARGO LOADING. DAMAGE WAS REMOVED AND REPAIR ANGLE FABRICATED TO REPAIR FRAME. 2L72 4F4 FRTA2NM E17NE 20050408000862005040800086CE 2005 4 8 20030801 120050222A5260 DOOR BEECH 1900 1900D 1154162CE AIRSTAIR CORRODED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03153GL UE153 ON ROUTINE STRUCTURAL INSPECTION, THE AIRSTAIR DOOR HAS CORROSION ON INNER SKIN NEAR HANDLE. AFFECTED AREA IS APPROX 5.75" TO 7.5" IN DIA. DOOR REPAIRED, AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA24CE 20050408000872005040800087NM 2005 4 8 2005UALA00251 120050315A2612 FIRE LOOP BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE NR 2 ENGINE MALFUNCTIONED A UALAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29912UA 25290 DIVERTED TO LNK DUE TO NR 2 ENGINE OVERHEAT INDICATION. SHUTDOWN NR 2 ENGINE AND BLEW BOTH FIRE BOTTLES. THERE WERE NO EVIDENCE OF FIRE OR OVERHEAT ON POST FLT INSP. REPLACED UPPER FAN OVERHEAT DETECTOR LOOP M1120. ENGINE OVERHEAT DETECTION SYSTEM TESTED NORMAL AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA16WE E2GL 20050408000902005040800090EA 2005 4 8 COMA0570027 120050308A532067053110475 BEAM CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01641CA3959 10122 FS 280 LT AND RT BULKHEADS AND TRANSVERSE BEAM HAVE MAJOR CORROSION ON AFT SIDE ALONG THE BOTTOM EDGES. REPLACED LOWER WEBS AT FS 280 BULKHEAD I/A/W BOMBARDIER INC REO 670-53-11-052, REV A. REPAIR NR 2 AND BRAS EO 601R-53-6066. REPLACED TRANSVERSE BEAM I/A/W BOMBARDIER INC REO 670-53-11-047 REV A AND BRAS EO 601R-53-6066. 2L72 4F RTA21EA 20050408000912005040800091CE 2005 4 8 DJFA2005067 120050221A551145A211465 RIB BEECH MU300 400A 1155402CE HORIZONTAL STAB CRACKED E DJFAK NONE O OTHER ININSP/MAINT 1 EA23718TA RK195 RK195 DURING A ROUTINE MAINTENANCE VISIT WHILE PERFORMING PHASE A AND PHASE B INSPECTIONS A CRACKED RIB WAS DISCOVERED ON THE LEFT HORIZONTAL STABILIZER AT THE LEFT ROLLER ASSEMBLY. THE RIB WAS REPLACED ALONG WITH SUPPORT BRACKETS. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4F RTA16SW 20050408000992005040800099SO 2005 4 8 C2XA05SH009 120050214A53302024T3ALCLAD SKIN EMB 145 EMB145ER 3260211SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714940 145033 SHV - DURING C-CHECK, GOUGES WERE FOUND ON THE EXTERNAL FUSELAGE SKIN AT FRAME 40. 2L72 4F RTT00011AT 20050408001002005040800100EU 2005 4 8 05FDEA00745 120050331A5420A545150675000 BRACKET AIRBUS310 A310 EU ZONE 400 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 NR 1 PYLON AFT END AT APPROX RIB 18 1 BRACKET IS CRACKED. REMOVED AND REPLACED BRACKET IAW A310-200 SRM 51-72-10. 2L72 4F RTA35EU 20050408001012005040800101EU 2005 4 8 05FDEA00746 120050331A54202241348502 BRACKET AIRBUS310 A310 EU ZONE 400 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 NR 2 ENGINE RT CORE COWL DOOR HOLD OPEN ROD SUPPORT BRACKET ON ENGINE IS WORN. REMOVED AND REPLACED BRACKET, INSTALLING IAW A310-200 AMM 20-21-12. 2L72 4F RTA35EU 20050408001042005040800104EU 2005 4 8 05FDEA00750 120050331A5311 FRAME AIRBUS310 A310 EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 AREA BEHIND AFT CARGO COMPARTMENT FRAME 77 LEFT SIDE APPROX STR 49L STR HAS 5 SQ INCHES OF CORROSION. REMOVED CORROSION AT FRAME 77 FOUND TO BE OUT OF LIMITS IAW A310-200 SRM 53-10-00 FIG 104 TABLE 102. REMOVED AND REPLACED STRINGER SECTION WITH NEW 48L FR 72-78 IAW A310-200 SRM 53-10-14. 2L72 4F RTA35EU 20050408001062005040800106EU 2005 4 8 05FDEA00752 120050331A5313 STRINGER AIRBUS310 A310 EU FUSLEAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 AREA BEHIND BULK CARGO BETWEEN FRAME 75 AND 76 APPROX AREA STR 49L, STRINGER HAS 5 SQ INCHES OF CORROSION. REMOVED CORROSION AFT OF FRAME 75 FOUND TO BE OUT OF LIMITS IAW A310-200 SRM 53-10-00 FIG 104, TABLE 102. REMOVED AND REPLACED STRINGER SECTION WITH NEW 48L FR 72 TO 78 IAW A310-200 SRM 53-10-14. 2L72 4F RTA35EU 20050408001092005040800109EA 2005 4 8 QXEA200500167 120050115A5310 DOOR FRAME CNDAIRCL600 CL6002C10 1390015EA ZONE 200 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - FORWARD FUSELAGE AT PILOT ESCAPE HATCH CUTOUT, FORWARD RIGHT CORNER HAS GOUGE ON OUTER SKIN 1" LONG. REPAIRED IAW HORIZON AIR EA R-53-256 AND CRJ REO 670-53-11-059. 2L72 4F RTA21EA 20050408001102005040800110EA 2005 4 8 QXEA200500168 120050120A5315 FLOORBEAM CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - FUSELAGE STATION 280 LEFTHAND SIDE FLOORBEAM ASSEMBLY IS CORRODED ALONG TOP FLANGE FROM BL-0 TO LBL 40. REPLACED IAW REO 670-53-11-047. 2L72 4F RTA21EA 20050408001122005040800112NM 2005 4 8 WRLA2005031 120050218A5513 SPAR CAP DOUG MD11 MD11F 3023600NM CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST LT BARREL NUT HOLE NR 36. 2L73 4F RTA22WE 20050408001152005040800115NM 2005 4 8 WRLA2005035 120050206A5513 SPAR CAP DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST RT BARREL NUT HOLE NR 36. 2L73 4F4 FRTA22WE E24NE 20050408001172005040800117WP 2005 4 8 WX0500013 120050131A33500105607001 LENS DOUG DC9 DC983 3022083WP EMERGENCY LIGHT DAMAGED A WX0AK NONE O OTHER ININSP/MAINT 1 WP19860GA 49786 LAS - CREW REPORTED EMERGENCY LIGHT FLOOR TRACK BROKEN AT ROW 30. MAINTENANCE REMOVED AND REPLACED FLOOR TRACK COVER AT ROW 30DEF. SYSTEM OPERATIONALLY CHECKED GOOD IAW MM 33-53-01. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050408001182005040800118EA 2005 4 8 QXEA200500475 120050228A5410 ACCESS PANEL CNDAIRCL600 CL6002C10 1390015EA ZONE 400 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - LEFT HAND COWL LATCH ACCESS PANEL 433AL HAS FRETTING CORROSION AT INTERNAL EDGE. REPAIRED IAW CRJ700 SRM 54-21-00-101-001-A01, SRM 51-12-00-001-001-A01, AND SRM 51-25-06-001-001-A01. 2L72 4F RTA21EA 20050408001192005040800119EA 2005 4 8 QXEA200500470 120050302A1430 FASTENER CNDAIRCL600 CL6002C10 1390015EA ZONE 800 LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - LEFT HAND WING UPPER SURFACE TRAILING EDGE HAS LOOSE FASTENERS AT STATION 170 AND 232. REPAIRED IAW CRJ7, SRM 51-25-01-001-001-A01 AND SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20050408001222005040800122NM 2005 4 8 AT0500013 120050328A323359567435501 ACTUATOR BOEING717 717200 1383700NM RT MLG DOOR INOPERATIVE A ZZDAB EMER. DESCENT J WARNING INDICATION APAPPROACH 1 SO15915AT 55085 PUT THE GEAR HANDLE DOWN AND GOT 3 GREEN AND GEAR DOOR OPEN ALERT. FOLLOWED QRH. LANDED WITH GEAR DOORS OPEN. REMOVED AND REPLACED MLG DOOR ACTUATOR IAW MM 32-34. LEAK AND OPS CHECK GOOD. 2L72 4F TRA6WE 20050408001242005040800124NM 2005 4 8 QXEA200500493 120050311A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09366PH 510 PDX - NR 1 SEAT TRACK HAS AREAS WITH PITTING CORROSION THAT ARE BEYOND BLENDABLE LIMITS. REPLACED IAW DHC-8200 SRM 51-40-00 AND 5140-11. 2H72 4T RTA13NM 20050408001252005040800125SO 2005 4 8 CHQA200500071 120050404A33501317 BULB EMB 145 EMB145MP 3260216SO EMERGENCY LIGHT BURNED OUT A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11976RP 145322 EMERGENCY EXIT LIGHT IS INOP OVER RIGHT HAND WING. REMOVED AND REPLACED EMERGENCY LIGHT BULB OVER RIGHT HAND WING FAIRING IAW EMB 145 MM 33-50-10. OPS CHECK GOOD AT THIS TIME AND DATE. 2L72 4F RTT00011AT 20050407001092005040700109NM 2005 4 7 ASAA0540087 120050203A532065414737 SHEAR WEB BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - DAMAGED FLOOR SHEAR WEB AT 500D-500E, LBL 36, WL 152. REMOVED AND REPLACED. (K) 2L72 4F4 FRTA16WE E21EU 20050407001182005040700118NM 2005 4 7 ASAA0540077 120050202A52416545849171 DOOR FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU AFT GALLEY DOOR GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - AFT GALLEY DOOR FWD SLIDE GOUGED ADJACENT TO UPPER LATCH CRANK. REMOVED AND REPLACED AFT GALLEY DOOR SIDE FRAME. (K) 2L72 4F4 FRTA16WE E21EU 20050407001412005040700141NM 2005 4 7 AWXA200500396 120050228A5320654795711 STRAP BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 MCN - MAJOR REPAIR - DURING C-16 CHECK GALVANIC CORROSION WAS FOUND IN MULTIPLE PLACES ON FLOOR STRAP AT AFT CARGO COMPARTMENT DOOR THRESHOLD BETWEEN BS 787 AND BS 867, RBL 22. MAINTENANCE REMOVED CORRODED FLOOR STRAP AT AFT CARGO DOOR THRESHOLD FROM BS 787 TO BS 867, RBL 22; FABRICATED A NEW REPLACEMENT STRAP PER DWG 65-47957; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050407001442005040700144NM 2005 4 7 AWXA200500398 120050301A5311654795961 FRAME BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 MCN - MAJOR REPAIR - DURING C-16 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT SIDE OF FRAME BETWEEN STR 25 RT AND STR 26 RT. MAINTENANCE BLENDED OUT CORROSION ON AFT SIDE OF FRAME AT BS 794, BETWEEN STR 25 RT AND STR 26 RT; FABRICATED 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW ER 03-5311-05081-RA4. 2L72 4F RTA16WE 20050407001452005040700145NM 2005 4 7 ASAA0540119 120050206A53226546548110 SHEAR TIE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - CORRODED SHEAR TIE AT BS 747, LBL 12.5 TO RBL 24. WI 148. REPAIRED SHEAR TIE BS 747, LBL8-13. (K) 2L72 4F4 FRTA16WE E21EU 20050407001532005040700153NM 2005 4 7 ASAA0540113 120050206A531265C33896145 PRESSURE PANEL BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - LT MAIN WHEEL WELL CUTOUT VERTICAL WEB CHAFED AT LBL 45. REPAIRED LT MAIN WHEEL WELL CUTOUT VERTICAL WEB AT BS 700 WL, 140 LBL 45. (K) 2L72 4F4 FRTA16WE E21EU 20050407001562005040700156EA 2005 4 7 COMA0560232 120050404A3260 PROXIMITY SWITCH CNDAIRCL600 CL6002B19 1900309EA MLG OUT OF ADJUST A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01959CA 7116 FLIGHT 5202 RECEIVED A RED NOSE LANDING GEAR DISAGREE CAUTION ON APPROACH INTO CVG, ABORTED 1ST APPROACH THEN LANDED WITHOUT INCIDENT ON 2ND ATTEMPT AFTER FOLLOWING QRH PROCEDURE. SERVICED THE NOSE STRUT AND ADJUSTED THE UPLOCK PIN AND PROXIMITY SWITCH CLEARANCE. 2L72 4F RTA21EA 20050407001582005040700158EA 2005 4 7 COMA0560239 120050404A335020131A BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT FAULTY A COMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SO01477CA 7670 FLIGHT 5358 DURING TEST OF THE LIGHTING SYSTEM THE FLOOR TRACK EMERGENCY LIGHTS AT ROWS 1 THROUGH 5 FAILED TO ILLUMINATE. REPLACED THE EMERGENCY BATTERY PACK. 2L72 4F RTA21EA 20050407001632005040700163CE 2005 4 7 DXTA200500658 120050402A261172111211102 SMOKE DETECTOR CESSNA750 750 2076810CE INOPERATIVE E DXTAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL07912QS5552 7500012 BAGGAGE SMOKE MASTER WARNING CYCLED ON AND OFF ON THE TAXI OUT (MASTER WARNING AND EICAS). REPLACED SMOKE DETECTOR IAW CE 750 MM 26-14-00. OPS CHECKED NORMAL. 2L72 4J RTT00007WI 20050407001672005040700167NM 2005 4 7 ASAA0540095 120050204A532265465553 SHEAR TIE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - AFT CARGO BAY CORROSION ON SHEAR TIE (FRAME). REPAIRED SHEAR TIE IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050407002292005040700229NM 2005 4 7 ASAA0540037 120050118A575465C26686 WEDGE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU L/E SLAT DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 OKC - RT WING NR 5 LE SLAT TRAILING EDGE WEDGE HAS SMALL AREA OF DELAMINATION AND DETERIORATED EDGE POTTING ON OB EDGE. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER AND REPORTED IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050407002852005040700285NM 2005 4 7 AWXA200500047 120050102A5330654577566 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK A 3 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT BS 727D + 17 INCHES, STR 24 RT. MAINTENANCE CUTOUT CRACKED SECTION OF FUSELAGE SKIN AT BS 727D + 17 INCH, STR 24 RT; FABRICATED A FILLER, DOUBLER AND TRIPLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-01, FIG 229. 2L72 4F RTA16WE 20050407002862005040700286NM 2005 4 7 TSAA0527002 120050116A2781189915 SENSOR BOEING737 737282 13844ATNM NR 4 SLAT DEFECTIVE A TSAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP13824AL 23045 FLT 278, HNL-KOA: ON INITIAL TAKEOFF ROLL, THE LEADING EDGE FLAP TRANSIT LIGHT ILLUMINATED (NR 4 SLAT) WITH THE CONFIGURATION WARNING HORN. ABORTED TAKEOFF AND RETURNED TO GATE. REMOVED AND REPLACED THE NR 4 LEADING EDGE FLAP EXTEND SENSOR. OPS CHECK OK PER MM 27-88-44. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA16WE 20050407003182005040700318NM 2005 4 7 05FDEA00847 120050405A5330 SKIN BOEING727 727233 138408ANM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25272FE 22037 CRACKED EXTERNAL SKIN FWD ENTRY DOOR UPPER HINGE CUTOUT. REPAIRED CRACK PER FED-EX EA 7-5330-86273. 2L73 4F RTA3WE 20050408000052005040800005NM 2005 4 8 QXEA200500495 120050308A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09366PH 510 PDX - NR 10 SEAT TRACK HAS AREAS WITH PITTING CORRSION BEYOND BLENDABLE LIMITS. REPLACED IAW SRM 51-40-00 AND SRM 51-40-11. 2H72 4T RTA13NM 20050408000092005040800009NM 2005 4 8 QXEA200500486 120050308A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09366PH 510 PDX - NR 7 SEAT TRACK HAS PITTING CORROSION OUT OF LIMITS AT X219. REPAIRED IAW EO 4473, 8-51-102 AND 8-53-1102. 2H72 4T RTA13NM 20050408000342005040800034NM 2005 4 8 QXEA200500497 120050311A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09366PH 510 PDX - LEFT OUTBOARD SEAT TRACK NR 2 HAS CORROSION BETWEEN STATION X499 AND X503. REPAIRED IAW DHC-8 200 SRM 51-40-00 AND SRM 51-40-11. 2H72 4T RTA13NM 20050408000432005040800043CE 2005 4 8 DELA200500004 120050215A750032144801 MIXING VALVE LEAR 55 55LEAR 5170702CE BLEED SYSTEM MALFUNCTIONED E DELAO OTHER J WARNING INDICATION CRCRUISE 1 CE03903JC 081 RIGHT ENGINE FIRE WARNING ILLUMINATED ABOVE FL400. AFM PROCEDURES FOLLOWED AND WARNING CEASED. WARNING DID NOT ILLUMINATED BELOW FL380. MAINTENANCE FOUND THE LEFT BLEED MIXING VALVE STUCK IN LOW CAUSING THE RIGHT SIDE TO OVERHEAT THE FIRE DETECTION LOOP. LEFT MIXING VALVE REPLACED WITH OVERHAULED UNIT. GROUND TESTING SATISFACTORY. MAINTENANCE CHECK FLIGHT CONDUCTED. R/H FIRE WARNING AT ALTITUDE OCCURRED ONLY WITH R/H BLEED SWITCH ON. R/H ENGINE REMOVED, ALL ACCESSIBLE BLEED SYSTEM SEALS REPLACED AND HOT SECTION FIRE LOOP REPLACED. FOLLOW-UP CHECK FLIGHT SHOWED NO FIRE WARNING. 2L72 4F A10CE 20050408000502005040800050EU 2005 4 8 05FDEA00563 120050315A5320 ANGLE AIRBUS310 A310 EU FUSELAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25419FE 345 FRAME 86 JUST ABOVE THS JACKSCREW 1 AREA OF CORROSION BETWEEN 2EA FASTENERS ON L-ANGLE. REMOVED CORROSION IAW A310 SRM 51-73-10. EVALUATED AREA AND FOUND IT TO BE OUT OF LIMITS IAW A310 SRM 53010-00. REMOVED AND REPLACED L-ANGLE IAW A310 SRM 51-40-21. TREATED BARE METAL IAW A310 SRM 51-75-10. (SEE JPF) 2L72 4F RTA35EU 20050408000522005040800052 2005 4 8 VW3R20050010 420050211A2565D29601103 GIRT BAR AIRCRUISERS AIRBUS330 A300* EU ESCAPE SLIDE DEFECTIVE B VW3RK NONE W INADEQUATE Q C ININSP/MAINT 1 WP09ALL 0451 ALL GIRT EXTENSION DOES NOT FIT PROPERLY ON GIRT BAR. GIRT EXTENSION PADS RIDE UP ON CAVITY RIDGE OF GIRT BAR. PLEASE NOTE THIS EVACUATION SLIDE IS ALSO USED ON A310 AIRCRAFT. 2L72 4F RTA26NM 20050408000592005040800059EA 2005 4 8 COMA0560193 120050321A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01494CA 7765 RIGHT HAND ENGINE SUPPORT BEAM HAS CRACK. REPAIRED IAW REO 601R-53-61-366. 2L72 4F RTA21EA 20050408000692005040800069WP 2005 4 8 AALA20050143 120050224A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217519A 49896 AUS - EXTERIOR EMERGENCY LIGHTS IN CABIN. REPLACED BATTERY PACK FOR EXTERIOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050408000782005040800078NM 2005 4 8 QXEA200500204 120050208A2611 WARNING LIGHT DHAV DHC8 DHC8202 2809007NM CARGO SMOKE FALSE ACTIVATIONA QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09352PH 494 PDX - FLIGHT 2058 - THE SMOKE AND MASTER WARNING LIGHT FLICKERED ON VERY BRIEFLY AND THEN TURNED BACK OFF. THE FLIGHT ATTENDANT OPENED THE BACK ACCESS DOOR AND FOUND NO SIGNS OF SMOKE. THE WARNINGS LIGHTS DID NOT COME ON AGAIN. MAINTENANCE CHECKED BOTH CARGO COMPARTMENT SMOKE DETECTORS CONNECTORS. C/W TEST PER AMM TASK 26-15-00-710-801. BOTH DETECTORS TESTED NORMAL. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050408000812005040800081EA 2005 4 8 QXEA200500185 120050123A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - LEFT OUTBOARD SIDE FACING SEAT RAIL AT STATION X645 TO X661, HAS PITTING CORROSION ON MOST INBOARD SURFACE. REPAIRED IAW CRJ-700 SRM 51-21-06-001-001-A01, REO 670-53-00-060. REV B AND HORIZON AIR EA R-53-266. 2L72 4F RTA21EA 20050408000892005040800089NM 2005 4 8 72300002 120050201A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CRACKED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 .75 INCH CRACK IN SHEAR TIE LOWER RADIUS. 2L73 4F4 FRTA3WE E2EA 20050408000972005040800097EU 2005 4 8 05FDEA00765 120050331A5347 SEAT TRACK AIRBUS310 A310 EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 SEAT TRACK '0' AT FR 75A AND 76 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK. REINSTALLED FLOORBOARDS IAW A310-200 SRM 51-72-10 AND 51-40-21. 2L72 4F RTA35EU 20050408000982005040800098EU 2005 4 8 05FDEA00766 120050331A5414A5461135700200 PANEL AIRBUS310 A310 EU ZONE 400 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 OFF AIRCRAFT PART, NR 1 PYLON ACCESS PANEL NR 413BL HAS MODERATE CORROSION AROUND ALL FASTENERS HOLES INTERIOR SIDE OF PANEL. REPLACED PANEL ASSY IAW A310-200 SRM 51-72-10. 2L72 4F RTA35EU 20050408001082005040800108NM 2005 4 8 P5CA0501329 120050313A32501171188 SWITCH BOEING747 74746NF 13848BTNM NLG STEERING INOPERATIVE A P5CAH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION ININSP/MAINT 1 EA15454PA 30812 BODY GEAR STEERING IND SYSTEM INOP. DEFERRED BODY GEAR SYSTEM PER MEL 32-52-2 ON DMI NR 33945. REMOVED AND REPLACED PRIMARY SWITCH ON LT BODY GEAR RT ACTUATOR PER MM 32-53-16. OPS CHK OK. 2L74 4F RTA20WE 20050408001132005040800113NE 2005 4 8 MASA200500125 220050216A72106014T81G27 GEARBOX CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 2 ENGINE MAKING METAL A MASAE ENGINE SHUTDOWN YJ ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 SW07759958138 7361 872634 ASH 7169 IAD-GSP- E2 SHUTDOWN AT 11OOO FEET IN LEVEL CRUISE. CAPTAIN DECLARED AN EMERGENCY AND LANDED WITH ONE ENGINE. MAINTENANCE IS TROUBLESHOOTING 2/18/05 MAINTENANCE CHANGED THE AGB. 2L72 4F4 FRTA21EA E15NE 20050408001142005040800114NM 2005 4 8 WRLA2005032 120050217A5513 SPAR CAP DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST RT BARREL NUT HOLE NR 01. 2L73 4F4 FRTA22WE E24NE 20050408001162005040800116EA 2005 4 8 QXEA200500473 120050302A5753 VANE CNDAIRCL600 CL6002C10 1390015EA ZONE 500 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - LEFT HAND WING INBOARD FLAP VANE, INBOARD LEADING EDGE PANEL 584ET HAS CHAFED MARK. REPAIRED IAW CRJ700 SRM 57-52-02-101-001-A01 AND SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050408001202005040800120 2005 4 8 VW3R20050006 420050211A2565D29601103 GIRT BAR AIRBUS330 A300* EU CABIN DEFECTIVE B VW3RK NONE W INADEQUATE Q C ININSP/MAINT 1 WP09ALL ALL GIRT EXTENSION DOES NOT FIT PROPERLY ON GIRT BAR. GIRT EXTENSION PADS RIDE UP ON CAVITY RIDGE OF GIRT BAR. PLEASE NOTE THIS EVACUATION SLIDE IS ALSO USED ON A310 AIRCRAFT. 2L72 4F RTA26NM 20050408001262005040800126WP 2005 4 8 0500429755 120050228A5315 FLOORBEAM DOUG DC9 DC941 302207NWP FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01755NW 47178 DURING H-CHECK FOUND CORROSION ON FLOORBEAM AT BS 794 RBL 57 TO RBL 60. REPAIRED PER EA 97-202515. 2L72 4F A6WE 20050408001272005040800127SO 2005 4 8 CHQA200500069 120050331A33501317 BULB EMB 135 EMB135KL 3260302SO EMERGENCY LIGHT BURNED OUT A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11376SK 145578 LEFT HAND FORWARD EMERGENCY EXIT LIGHT IS INOPERATIVE. RELAMPED LEFT HAND FORWARD EMERGENCY EXIT LIGHT IAW EMB 140 AMM 33-50-07. OPS CHECK GOOD. 2L72 4F RTT00011AT 20050408001292005040800129NM 2005 4 8 SWAA050999 120050404A335065C27095 CHARGER BOEING737 7373K2 13844BANM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29340LV 23738 DURING SCHEDULED SERVICE CHECK, FOUND L1 & R1 DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM. 2L72 4F RTA16WE 20050408001322005040800132NM 2005 4 8 372PA0080 120050324A3350 LIGHT BOEING737 737306 13844BGNM BULL NOSE INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05372PA 23546 RIGHT BULL NOSE EMERGENCY LIGHT (OVERHEAD BAGGAGE BIN) INOP. REPLACED EXIT LIGHT, OPS CHECKS GOOD. 2L72 4F RTA16NE 20050408001362005040800136 2005 4 8 SWAA051005 420050405A256565C168209 HOOK BOEING737 7373H4 1384600NM L2 DOOR GIRT BAROUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29633SW 27936 L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOKS OUT OF POSITION. REPOSITIONED HOOKS PER MM. 2L72 4F RTA16WE 20050408001412005040800141SO 2005 4 8 MASA200500255 120050325A335078241 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07836MJ 145359 ASH 2604 CLT TO MKE EMERGENCY EXIT SIGN AT RIGHT HAND EMERGENCY EXIT INOP. MAINTENANCE REPLACED THE EMERGENCY LIGHT INVERTER. 2L72 4T RTT00011AT 20050411000012005041100001NM 2005 4 11 HNAA0500029 120050330A3220 LOCK DHAV DHC8 DHC8102 2809003NM NLG ENGAGED A HNAAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 EA07907H 011 NOSE GEAR RED INDICATION WITH GEAR SELECTED UP. FOUND NOSE GEAR LOCK ENGAGED. STOWED LOCK INSPECTED GEAR, NO DEFECTS NOTED. 2H72 4T RTA13NM 20050411000042005041100004SO 2005 4 11 LR7A05041 120050405A5512 SKIN LKHEED382 382G 526414USO HORIZONTAL STAB CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 86 4606 DURING SCHEDULED A1 INSPECTION PER JOB CARD HA1201 FOUND LT HORIZONTAL STABILIZER UPPER SKIN CRACKED 2 INCHES AT FS 1093, LT HSS 219. REPAIRED SKIN IAW SMP583 FIG 55-20-06. 2H74 4T A1SO 20050411000052005041100005CE 2005 4 11 DXTA200500653 120050331A3000S100420PG SENSOR CESSNA750 750 2076810CE STAB FAILED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07908QS4979 7500108 ON TAKEOFF ROLL, FULL POWER, ABOUT 70-80 KTS THE RED STAB BLD LEAK L CAS MESSAGE ILLUMINATED. INSTALLED NEW STABILIZER TEMP SENSOR. OPS CHECKED GOOD IAW 750 MM CHAPTER 30-14-00. 2L72 4J RTT00007WI 20050411000072005041100007EU 2005 4 11 WRNA200500009 120050210A3240286467100 SERVO VALVE AIRBUS300 A300B4203 3930306EU MLG BRAKES UNSERVICEABLE A WRNAO OTHER J WARNING INDICATION LDLANDING 1 SO05502TA 075 NR 7 BRAKE OVER 700 DEGREES CELSIUS AFTER LANDING. NR 7 TIRE DEFLATED DUE TO FUSEABLE PLUG MELTING. NR 7 & NR 8 TIRE ASSY'S REPLACED IAW 12-37-32, NR 7 BRAKE DE-ACTIVATED- MEL'D IAW 32-42-09. AIRCRAFT RETURNED TO SERVICE. 2-12-05 REMOVED AND REPLACED AFT AXLE ASSY IAW CMM 32-14-23, REMOVED AND REPLACED NR 7 BRAKE ASSY IAW 32-42-27. 2-17-05 REMOVED AND REPLACED BRAKE SERVO VALVE ASSY IAW 32-42-48. ALL FUNCTION TESTS SATISFACTORY, CLEARED MEL. AIRCRAFT OK FOR SERVICE. 2L72 4F RTA35EU 20050411000102005041100010WP 2005 4 11 WX0500035 120050324A3350 BATTERY DOUG DC9 DC983 3022083WP FLASHLIGHT DISCHARGED A WX0AK NONE O OTHER ININSP/MAINT 1 WP19891GA 49423 LAS - CREW REPORTED SHIPS FLASHLIGHT BATTERIES DEAD. MAINTENANCE REPLACED FLIGHT DECK FLASHLIGHT BATTERIES REF MM 25-60-00. FLASHLIGHT OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050411000122005041100012WP 2005 4 11 WX0500037 120050328A2160SYLZ9885 THERMOSWITCH DOUG DC9 DC983 3022083WP RT A/C PACK FAILED A WX0AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP19862GA 49556 LAS TO BLI - CREW REPORTED RT A/C PACK DROPPED TO ZERO PRESSURE CLIMBING THROUGH ABOUT 20,000 FT AND REMAINED AT ZERO PRESSURE IN THE DESCENT TO ABOUT 18,000 FT AFTER SELECTION OF MANUAL, HOT ON THE CABIN TEMP CONTROL KNOB. AIRCRAFT RETURNED TO LAS AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE CABIN TEMP CONTROL ELECTRONIC THERMOSWITCH FAILED. MAINTENANCE REMOVED AND REPLACED CABIN TEMP CONTROL SWITCH IAW MM 21-60-00. SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050411000132005041100013WP 2005 4 11 ARWA20050305 120050331A27505751152503N LINK DOUG DC8 DC863F 302198FWP TE FLAPS DAMAGED A ARWAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO19661AV 45969 WHEN FLAPS SELECTED, 10 SPLIT WITH NO CONTROL PROBLEMS. REPLACE FLAP LINK FITTING AT STA 98. OPERATIONAL CHECK SATISFACTORY IN ACCORDANCE WITH DC8 M/M 37-51-41. 2L74 4F 4A25 20050411000142005041100014WP 2005 4 11 ARWA20050402 120050405A2910 LINE DOUG DC10 DC1030 3023501WP HYD SYSTEM BROKEN A ARWAD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SO19526MD 46998 DURING TAXI, TOTAL LOSS OF HYDRAULIC SYSTEM NR 3 FLUID. T/S FOUND BROKEN LINE FROM NR 3 SYSTEM IN CENTER WHEEL WELL. REPAIRED LINE IN ACCORDANCE WITH DC-10 M/M 20-10-01. SERVICED NR 3 HYDRAULIC SYSTEM IN ACCORDANCE WITH M/M 12-13-02. NO LEAKS NOTED. 2L73 4F A22WE 20050411000152005041100015 2005 4 11 SWIA200514832 420050406A3418 COMPUTER CNDAIRCL600 CL6002B19 1900309EA STALL WARNING MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07439SW 7578 STALL FAIL MSG IN FLIGHT. REPLACED STALL COMPUTER IAW 27-34-00 AND REPLACED LEFT AOA IAW 27-35-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050411000182005041100018SO 2005 4 11 SWIA200514835 120050405A3397 WIRE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07232SW 120306 FORWARD BULB INOPERATIVE ON EMERGENCY TRACK LIGHTING. REPAIRED BROKEN WIRE AS REQUIRED. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050411000202005041100020EA 2005 4 11 SWIA200514837 120050405A5610 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAO OTHER O OTHER CRCRUISE 1 NM07903SW 7425 CAPTAIN'S WINDSHIELD SHATTERED WHILE AT FL340. REPLACED CAPTAIN'S WINDSHIELD ASSY PER CRJ MM 56-00-00, 56-11-01, 56-12-01. OPERATIONAL CHECK GOOD. P/N NP139321-11, S/N OFF 01043H9715. 2L72 4F RTA21EA 20050411000212005041100021EA 2005 4 11 SWIA200514838 120050401A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLT SPOILER MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07443SW3705 3705 7638 SPOILERON FAULT STATUS MESSAGE. REPLACED LEFT SPOILERON INBOARD PCU IAW MM 27-62-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050411000222005041100022EA 2005 4 11 SWIA200514839 120050404A27604916405 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07710BR 7852 SPOILERON FAULT STATUS MSG. REPLACED NR 2 SECU IAW CRJ200 MM 27-61-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050411000272005041100027CE 2005 4 11 DXTA200500656 120050401A282099144751 FLAPPER VALVE CESSNA750 750 2076810CE FUEL SYSTEM LEAKING E DXTAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL07958QS 7500158 WING TANK O-FILL-R CAS MESSAGE ILLUMINATED IN FLIGHT. FUEL VENTED OVERBOARD, THEN STOPPED. CAS MESSAGE WENT OUT BUT CAME ON AGAIN SHORTLY THEREAFTER, CAS MESSAGE THEN WENT OUT. REMOVED FLAPPER VALVE DUE TO MALFUNCTION. INSTALLED NEW FLAPPER VALVE IAW CE750 M/M CHAP 28-10-05. FUNCTIONAL/LEAK CHECK GOOD. 2L72 4J RTT00007WI 20050411000292005041100029SO 2005 4 11 MASA200500153 120050224A3260355022022MOD CONTROL UNIT EMB 145 EMB145LR 3260212SO MLG INOPERATIVE A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07843MJ6852 145478 ASH 2641 ACK TO CLT THE AIRCRAFT RETURNED TO THE FIELD DUE TO THE LANDING GEAR AIR GROUND FAIL GEAR WILL NOT RETRACT. MAINTENANCE IS TROUBLESHOOTING, 2/24/05 MAINTENANCE REPLACED THE LANDING GEAR ELECTRONIC CONTROL UNIT AND PROX SENSOR SWITCH P/N 8-527-01, S/N 20939. 2L72 4T RTT00011AT 20050411000302005041100030SO 2005 4 11 CHQA200500068 120050331A33501317 BULB EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT BURNED OUT A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11841RP 145737 RIGHT HAND REAR EMERGENCY EXIT LIGHT IS INOPERATIVE. REMOVED AND REPLACED RIGHT HAND EMERGENCY EXIT LIGHT BULB IAW EMB 135 AMM 33-50-10. OPS CHECK GOOD. LEFT HAND EMERGENCY OVERWING EXIT LIGHT IS INOPERATIVE. REMOVED AND REPLACED LEFT HAND OVERWING EMERGENCY EXIT LIGHT BULB IAW EMB 135 AMM 33-50-10. OPS CHECK GOOD. 2L72 4F RTT00011AT 20050411000312005041100031NM 2005 4 11 SWAA051008 120050406A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND CORROSION ON CABIN FLOORBEAM UPPER CHORD AT BS 328, LBL 16. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20050411000322005041100032NM 2005 4 11 SWAA051009 120050406A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND CORROSION ON CABIN FLOORBEAM UPPER CHORD AT BS 344, BETWEEN RBL 8 TO LBL 35. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20050411000332005041100033 2005 4 11 SWAA051010 420050406A25656557463 FITTING BOEING737 7373H4 1384600NM L1 DOOR SLIDE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE, FWD & AFT GIRT BAR FLOOR FITTINGS CORRODED. REMOVED AND REPLACED FLOOR FITTINGS PER SRM. 2L72 4F RTA16WE 20050411000342005041100034NM 2005 4 11 SWAA051011 120050406A53306545890 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29333SW 23697 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 312, STR 20R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050411000362005041100036NM 2005 4 11 SWAA051013 120050406A5610141A481016 WINDOW BOEING737 7377H4 1384404NM COCKPIT ARCED A SWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW29414WN 29820 R2 COCKPIT WINDOW ARCED & CRACKED. REMOVED AND REPLACED R2 WINDOW & WINDOW HEAT CONTROLLER. 2L72 4F RTA16WE 20050411000372005041100037EA 2005 4 11 MASA200500233 120050319A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A MASAK NONE O OTHER ININSP/MAINT 1 SW0717217 7217 ASH 7132 FROM CLT TO IAD, CREW FOUND TWO ADJACENT STRIPS OF EMERGENCY FLOOR LIGHTING INOP. CLT MX IN PROCESS OF TROUBLESHOOTING. MAINTENANCE RESECURED, OPS CHECKED GOOD. 2L72 4F RTA21EA 20050411000382005041100038SO 2005 4 11 MASA200500247 120050322A3397 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY SIGN LOOSE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07826MJ 145214 ASH 2647 CLT, CREW REPORTED THE RT OVERWING EMERGENCY EXIT SIGN LIGHTS WERE INOP. MAINTENANCE RESECURED THE CONNECTOR AND THE SIGN, OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050411000392005041100039SO 2005 4 11 MASA200500251 120050324A3397 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT UNSECURE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07826MJ 145214 ASH 2712 CLT TO YYZ HAD THE RT OVERWING EXIT EMERGENCY EXIT LIGHT INOP. MAINTENANCE SECURED THE LIGHT CONNECTOR AND IT OPERATED NORMALLY. AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. 2L72 4T RTT00011AT 20050411000402005041100040EA 2005 4 11 MASA200500253 120050325A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07570ML 7206 ASH 2706 IN PHL REPORTED ALL EMERGENCY EXIT FLOOR PATH LIGHTING INOP. MAINTENANCE RESET THE SYSTEM AND COULD NOT DUPLICATE THE PROBLEM. 2L72 4F RTA21EA 20050411000422005041100042EA 2005 4 11 HNAA050034 120050405A2910DSC252B40124 LINE DHAV DHC8 DHC8311 1386006EA HYDRAULIC SYS LEAKING A HNAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 EA07336EN2890628906 336 ON GEAR RETRACTION NOSE GEAR DID NOT RETRACT, NR 2 HYDRAULIC QUANTITY DROPPED TO .5 QUARTS. CREW PERFORMED EMERGENCY EXTENSION. FOUND PRESSURE LINE TO NOSE GEAR DRAG STRUT ACTUATOR LEAKING. REMOVED AND REPLACED LINE AND COMPLIED WITH GEAR SWINGS. 2H72 4T RTA13NM 20050411000452005041100045 2005 4 11 DXTA200500650 420050330A3410 DISPLAY CESSNA750 750 2076810CE COCKPIT LOOSE E DXTAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 GL07923QS 7500023 ON TAKEOFF ROLL PILOT'S PFD (DU NR 1) FAILED AT 40 KTS. EICAS MESSAGE CHECK DU NR 1 MESSAGE ILLUMINATED. TAKEOFF WAS ABORTED. INSPECTED AND FOUND PFD LOOSE IN SLOT. RESECURED PFD PER M/M 31-50-01 PFD OP CHECKS NORMAL, A/C OK FOR SERVICE. 2L72 4J RTT00007WI 20050411000462005041100046 2005 4 11 ARWA20050401 420050403A3414 WIRE DOUG DC10 DC1010 3022110WP AIRSPEED IND BROKEN A ARWAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO1968041 46900 DURING INITIAL TAKEOFF ROLL, NO AIR SPEED INDICATION ON CAPTAIN'S SIDE, ABORTED TAKEOFF AT 90 KNOTS. REPAIRED BROKEN WIRE AT CAPTAIN'S AIRSPEED INDICATION CONNECTOR (P1-102T) IN ACCORDANCE WITH M/M 20-30-00. PERFORMED DADC BITE TEST IN ACCORDANCE WITH M/M 34-13-00, FOUND NORMAL. 2L73 4F A22WE 20050411000472005041100047 2005 4 11 252TR0037 420050328A22104084042911 COUPLER BOEING737 737228 13844AGNM YAW DAMPER DAMAGED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05252TR 23001 YAW DAMPER IS INOP. PLACED ON MEL 22-3. REPLACED YAW DAMPER COUPLER PER MM 22-11-141. OPS AND BITE CHECK OK. 2L72 4F RTA16WE 20050411000482005041100048CE 2005 4 11 DXTA200500649 120050329A3244164F032 TIRE CESSNA750 750 2076810CE MLG DEFECTIVE E DXTAD RETURN TO BLOCK E VIBRATION/BUFFET TOTAKEOFF 1 GL07923QS1395 7500023 DURING T/O ROLL BETWEEN 40 KTS - 80 KTS NOSE WHEEL VIBRATION REACHED EXCESSIVE LEVEL, PILOTS SIDE PFD NR 1 KICKED OFF. T/O WAS ABORTED AT 80 KTS. REMOVED AND REPLACED NR 1 AND NR 2 NOSE WHEEL ASSY IAW CE750 MM 32-41-01 (SQK NR 1). REMOVED AND REPLACED NR 1 NOSE WHEEL ASSY P/N OFF 3-1538-1, S/N 0537, P/N ON 3-1538-1, S/N 0690. REMOVED AND REPLACED NR 2 NOSE WHEEL ASSY P/N 3-1538-1 OFF, S/N 0387, P/N ON 3-1538-1, S/N 0688, PER LMCC ALL WORK DONE IAW CE750 MM 32-41-01. 2L72 4J RTT00007WI 20050411000492005041100049SO 2005 4 11 RAIA00503014 120050328A32348271013 HANDLE EMB 145 EMB145 3260210SO MLG INOPERATIVE A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03802HK15843 145066 FLT 3510 - RIC - LANDING GEAR WILL NOT RETRACT. MAINTENANCE REMOVED A NDREPLACED LANDING GEAR HANDLE. 2L72 4F RTT00011AT 20050411000502005041100050 2005 4 11 PIDA2005002 420050403A22104051601932 CONTROL PANEL BOEING737 7373G7 1384595NM AUTOPILOT FAILED A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05370WL 24011 FIRST OFFICER'S COURSE SELECTOR WILL NOT TUNE IN COURSE. PLACED ON MEL 22-16-E. 04/03/2005: REPLACED AUTO PILOT MODE CONTROL PANEL AND OPS CHECKED PER MM 22-11-34. 2L72 4F RTA16WE 20050411000512005041100051EA 2005 4 11 SWIA200514840 120050402A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07926SW 7687 EMERGENCY LIGHT (FLOOR LEVEL) WILL NOT ILLUMINATE AT SEAT 8A. REPLACED FLOOR EMERGENCY FLOOR LIGHTS LUMINESCENT STRIP REF CRJ MM 33-51-01. 2L72 4F RTA21EA 20050411000522005041100052NM 2005 4 11 SWAA050984 120050401A3350311500 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29329SW 23693 EMERGENCY BULLNOSE LIGHT LENS MISSING AT ROW 19 DEF. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20050411000542005041100054 2005 4 11 SWAA050986 420050401A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29399WN 27693 DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050411000552005041100055NM 2005 4 11 SWAA050987 120050403A335007912 COVER BOEING737 7377H4 1384404NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29409WN 27896 DURING SCHEDULED MV2 CHECK, FOUND FWD END OF EEPLS STRIP COVER BROKEN. REMOVED AND REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20050411000562005041100056NM 2005 4 11 SWAA050988 120050403A335057771 CAP BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29433LV 33716 EEPLS FWD END CAP MISSING. INSTALLED EEPLS END CAP PER MM. 2L72 4F RTA16WE 20050411000572005041100057NM 2005 4 11 390WL0002 120050328A3350 LIGHT BOEING737 7373G7 1384595NM SEAT 21 ABC BROKEN A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05390WL 23219 EMERGENCY OVERHEAD LIGHT AT SEAT 21 ABC IS BROKEN. PLACED OVERHEAD LIGHT ON MEL 33-15-3. REPLACED BROKEN RETAINER ON LIGHT FIXTURE AND RETURNED LIGHT TO NORMAL. OPS CHECKS GOOD. 2L72 4F RTA16WE 20050411000582005041100058 2005 4 11 P5CA0501334 420050402A342096501840001 COMPUTER BOEING747 747230B 1384889NM ALTITUDE INOPERATIVE A P5CAK NONE O OTHER ININSP/MAINT 1 EA15509MC 21221 ALTITUDE ALERT SYSTEM INOP. REPLACED ALTITUDE ALERT COMPUTER AND TESTED OK PER MM 34-16-00. 2L74 4F A20WE 20050411000592005041100059NM 2005 4 11 SWAA050981 120050331A551265C25727 SKIN BOEING737 7373G7 1384595NM HORIZONTAL STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29670SW 23784 DURING SCHEDULED C1 CHECK, FOUND LT HORIZONTAL STAB LOWER SKIN CRACKED AT INBOARD BALANCE BAY. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050411000662005041100066 2005 4 11 UPS05544232 420050401A2210 COMPUTER BOEING757 75724APF 1384969NM NR 1 INOPERATIVE A IPXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01425UP 25370 EMERGENCY DECLARED. ON CLIMBOUT APPROX 20,000 FT CAPT'S AIRSPEED, ALT & VSI FAILED. CAPT SWITCHED TO ALT AIR DATA SWITCH, ALL CORRECTED AT APPROX 25,000 FT, BEGAN TO RECEIVE OVERSPEED WARNINGS (FAST/SLOW). AT 41,000 AUTOTHROTTLE COULD NOT MAINTAIN PROPER AIRSPEED. A/T WERE DISCONNECTED IN ATTEMPT TO SOLVE PROBLEM. TEN MIN LATER MACH TRIM & RUDDER RATIO & O/S WARNING WENT OFF. FIFTEEN MIN LATER CAPT PRIMARY ALT FAILED. *S/D* REMOVED AND REPLACED L/ADC & L ALT. OPS CHECK OK PER MM 34-12-01 & 34-13-01. FOUND WIRE W4471-0102-24 SHORTING TO GROUND INTERMITTENT CAUSING L/ADC TO GO INTO TEST MODE. REMOVED AND REPLACED WIRE PER WDM 34-12-12. L ADC OPS CHECKS NORMAL. 2L72 4F RTA2NM 20050411000672005041100067NM 2005 4 11 SWAA051015 120050406A21210802032501 TRU BOEING737 7375H4 138449DNM COOLING FAN FAULTY A SWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW29505SW 24182 DIVERSION/DECLARED EMERGENCY. LOST CABIN PRESSURE, NR 1 TRANSFORMER RECTIFIER & EQUIPMENT COOLING FAN INOP. REMOVED AND REPLACED NR 1 TRANSFORMER RECTIFIER & NR 1 ENGINE GENERATOR PER MM. 2L72 4F RTA16WE 20050411000682005041100068NM 2005 4 11 SWAA051016 120050406A256010C801 LATCH BOEING737 7373H4 1384600NM FWD CABIN OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29643SW 27716 DURING SCHEDULED SERVICE CHECK, FOUND F/O'S EMERGENCY ESCAPE ROPE DOOR LATCH OUT OF ADJUST. ADJUSTED DOOR LATCH PER MM. 2L72 4F RTA16WE 20050411000692005041100069 2005 4 11 SWAA051017 420050406A34174061100901 COMPUTER BOEING737 7373H4 1384600NM FWD CABIN FAULTY A SWAAO OTHER O OTHER NRNOT REPORTED 1 SW29655WN 28400 AIR TURNBACK. CAPTAIN'S AIRSPEED, ALTIMETER, VSI & CABIN PRESSURE CONTROL SYSTEM INOP. REMOVED AND REPLACED NR 1 DADC PER MM. 2L72 4F RTA16WE 20050411000702005041100070NM 2005 4 11 SWAA051018 120050406A53306545777 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050411000722005041100072NM 2005 4 11 SWAA051020 120050406A57536546486 WEDGE BOEING737 7377H4 1384404NM LT WING TE FLAPSDELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29788SA 30603 DURING SCHEDULED HC2 CHECK, FOUND LT WING INBOARD MAIN FLAP OUTBOARD T/E WEDGE DELAMINATED. REPAIRED WEDGE PER SWA EA. 2L72 4F RTA16WE 20050411000752005041100075NM 2005 4 11 PIDA2005047 120050401A3350 BULB BOEING737 737317 138447PNM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05375PA 23812 L1 OUTSIDE EMERGENCY LIGHT INOP. REPLACED L1 EMERGENCY LIGHT BULB. OPS CHECKS GOOD. 2L72 4F RTA16WE 20050411000792005041100079NM 2005 4 11 SWAA050977 120050331A53306545775 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29501SW 24178 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT CARGO DOOR CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050411000802005041100080NM 2005 4 11 SWAA050978 120050331A531265C35740 PANEL BOEING737 7375H4 138449DNM NLG W/W CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29501SW 24178 DURING SCHEDULED 1/2D CHECK, FOUND NLG W/W CEILING PANEL CRACKED AT LT & RT BRAKE MOUNT PADS. REPAIRED PER SWA EA & SRM. 2L72 4F RTA16WE 20050411000822005041100082NM 2005 4 11 SWAA050980 120050331A57536546431280 SKIN BOEING737 7373G7 1384595NM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29670SW 23784 DURING SCHEDULED C1 CHECK, FOUND RT WING OUTBOARD T/E FOREFLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM. 2L72 4F RTA16WE 20050411000832005041100083NM 2005 4 11 SWAA050989 120050401A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29477WN 33988 EEPLS FWD END STRIP LOOSE. SECURED EEPLS STRIP PER MM. 2L72 4F RTA16WE 20050411000842005041100084NM 2005 4 11 ABXA050086 120050401A79318D1415 PRESSURE SWITCH BOEING767 767231 1385131NM PWA JT9 JT9D* NE RT ENGINE DEFECTIVE A ABXAE ENGINE SHUTDOWN YJ ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 GL23708AX260 22571 709677 IN FLIGHT, RIGHT OIL FILTER LIGHT DID NOT GO OUT WITH TRUST REDUCTION. RT ENGINE WAS SHUT DOWN. WINDMILLED FOR 31 MINUTES, OIL PRESSURE UNKNOWN. FOUND THE RIGHT OIL FILTER DIFFERENTIAL PRESSURE SWITCH DEFECTIVE. REPLACED THE SWITCH. COMPLIED WITH NR 2 ENGINE WINDMILL AND BOROSCOPE INSPECTION. NO DEFECTS WERE FOUND. 2L72 4F4 FRTA1NM E20EA 20050411000862005041100086NM 2005 4 11 UPS05544237 120050402A2560 PBE BOEING757 75724APF 1384969NM COCKPIT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01464UP 28268 A/C PBE UNIT VACUUM LOST. REMOVED AND REPLACED A/C PBE UNIT. 2L72 4F RTA2NM 20050411000902005041100090NM 2005 4 11 SWAA050991 120050402A291065C26839 LINE BOEING737 7375H4 138449DNM HYD SYSTEM CHAFED A SWAAC ABORTED TAKEOFF KJ FLUID LOSS WARNING INDICATION TOTAKEOFF 1 SW29520SW 25319 AIR TURNBACK, DECLARED EMERGENCY. LOST B-HYDRAULIC SYSTEM ON TAKEOFF. REMOVED AND REPLACED HYDRAULIC LINES FROM B-SYSTEM PUMP TO B-SYSTEM CONTROL MODULE & B-SYSTEM PUMP CASE DRAIN TO T-FITTING PER MM. 2L72 4F RTA16WE 20050411000912005041100091 2005 4 11 SWAA050992 420050402A2565D31354433 SLIDE BOEING737 7375H4 138449DNM R2 DOOR DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29526SW 26568 DURING SCHEDULED A1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATING LOW. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20050411000952005041100095NM 2005 4 11 375PA0044 120050221A5230 SKIN BOEING737 73739A 138447PNM CARGO DOOR CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05375PA 23812 AFT CARGO DOOR INNER SKIN CRACKED AROUND LIGHTENING HOLE NEAR CENTER OF DOOR. REPAIRED PER SRM 51-70-13. 2L72 4F RTA16WE 20050411000962005041100096NM 2005 4 11 375PA0047 120050401A3350 BULB BOEING737 737317 138447PNM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05375PA 23812 L1 OUTSIDE EMERGENCY LIGHT INOP. REPLACED L1 EMERGENCY LIGHT BULB. OPS CHECKS GOOD. 2L72 4F RTA16WE 20050411000972005041100097SO 2005 4 11 RAIA00503015 120050330A5270 WARNING SYSTEM EMB 145 EMB145 3260210SO SERVICE DOOR MALFUNCTIONED A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03801HK 145053 FLT 3562 - BNA - SERVICE DOOR WARNING LIGHT ILLUMINATED. DEFERRED SERVICE DOOR WARNING SYSTEM PER MEL. 2L72 4F RTT00011AT 20050411000982005041100098SO 2005 4 11 RAIA00503013 120050325A361014538590402 TUBE EMB 145 EMB145ER 3260211SO NR 2 ENG BLEED LEAKING A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03808HK 145157 FLT 3588 - RIC - ENGINE NR 2 FIRE WARNING. MAINTENANCE REMOVED AND REPLACED NR 2 HP BLEED TUBE. 2L72 4F RTT00011AT 20050411000992005041100099NM 2005 4 11 249TR0105 120050324A771410619911 INDICATOR BOEING737 7372K5 138448XNM PWA JT8 JT8D15A 52051NE N1 TACH MALFUNCTIONED A PIDAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO05249TR 22598 717107 RIGHT ENGINE N1 GAUGE WENT TO 80 PERCENT AND STOPPED. ABORTED TAKEOFF PRIOR TO 60 KNOTS. MINIMUM BREAKING APPLIED. REPLACED N1 TACH AND OPS CHECKED PER MM 77-12-0 AND 31-00-11. 2L72 4F4 FRTA16WE E2EA 20050411001002005041100100NM 2005 4 11 SWAA050942 120050328A53106547978 CREASE BEAM BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29501SW 24178 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE CREASE BEAM WEB CRACKED AT BS 616, RBL 64. REPAIRED WEB PER SWA EA & SRM. 2L72 4F RTA16WE 20050411001012005041100101NM 2005 4 11 SWAA050943 120050328A53106547978 CREASE BEAM BOEING737 7375H4 138449DNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29501SW 24178 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE CREASE BEAM WEB CORRODED AT BS 638, RBL 65. REPAIRED WEB PER SWA EA & SRM. 2L72 4F RTA16WE 20050411001032005041100103SO 2005 4 11 CHQA200500070 120050401A335066368 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11266SK 145241 EMERGENCY FLOOR PROXIMITY EXIT LIGHT STRIPS ARE INOP AT ROW 7 AND 8. REMOVED AND REPLACED NR 7 AND NR 8 EMERGENCY FLOOR PROXIMITY LIGHT STRIPS IAW EMB 145 AMM 33-50-12. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050411001042005041100104SO 2005 4 11 CHQA200500066 120050330A3350MS25231316 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11270SK 145304 MAIN ENTRANCE DOOR EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED MAIN ENTRY DOOR EMERGENCY EXIT LIGHT IAW EMB 145 MM 33-50-10. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050411001072005041100107NM 2005 4 11 SWAA050959 120050329A3350071701100 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29735SA 27867 DURING SCHEDULED RON CHECK, FOUND EMERGENCY EXIT LIGHT INOP ON LT OVERWING DOOR & CENTER AISLE. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20050411001082005041100108NM 2005 4 11 SWAA050951 120050328A551265C25727 SKIN BOEING737 7373H4 1384600NM HORIZONTAL STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29338SW 23960 DURING SCHEDULED C2 CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED AT STA 135. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050411001102005041100110NM 2005 4 11 2005UALA00265 120050325A2932 WARNING LIGHT AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE NR 2 ENG PUMP MALFUNCTIONED A UALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 WP29834UA 1420 ENGINE 2 PUMP LO PRESSURE DISPLAYED ON UPPER ECAM. REPLACED NR 2 ENG. HYDRAULIC PRESS. SWITCH, RAN ENG. LEAK CHECKS GOOD. 2L72 4F4 FRTA28NM E40NE 20050411001112005041100111EU 2005 4 11 2005UALA00266 120050325A3610 DUCT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE LT WING LOOSE A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29404UA 450 LEFT WING LEAK DISPLAYED ON UPPER ECAM. FOUND DUCT LOOSE AT FIRST CLAMP AFT OF THE GROUND AIR CONNECTOR. REPOSITIONED DUCT AND RESECURED CLAMPS. 2L72 4F4 FRTA28NM E40NE 20050411001122005041100112EA 2005 4 11 SWIA200514829 120050328A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY MALFUNCTIONED A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07960SW 7853 CARGO SMOKE MESSAGE ILLUMINATED AT GATE. REPLACED AFT CARGO SMOKE DETECTOR. OPERATIONAL CHECK GOOD. P/N 473597-19, S/N OFF 2779. 2L72 4F RTA21EA 20050411001172005041100117SO 2005 4 11 SWIA200514808 120050328A27115301 ACTUATOR EMB 120 EMB120ER 3260203SO AILERON TRIM TABMALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07284YV 120284 AILERON TRIM VERY STIFF IN FLIGHT. REMOVED AND REPLACED AILERON TRIM TAB ACTUATOR ASSY IAW EMB 120 MM 27-12-01. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050411001182005041100118SO 2005 4 11 SWIA200514809 120050323A3350 BATTERY EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT DISCHARGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07560SW 120334 EMERGENCY LIGHTS INOPERATIVE. INSTALLED SERVICEABLE BATTERIES FOR EMERGENCY LIGHTS. OPERATIONALCHECK GOOD. P/N D366-04-001; S/N OFF 1120, P/N D366-04-001; S/N OFF 1238, P/N D366-04-001; S/N OFF 312. 2L72 4T RTA31SO 20050411001232005041100123EA 2005 4 11 COMA0560224 120050403A30205399111 VALVE CNDAIRCL600 CL6002B19 1900309EA ENGINE FAULTY A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01785CA14638 7326 FLT 5372 RECEIVED A LT ENGINE COWL CAUTION DURING CRUISE FLIGHT (IND-JFK), AIRCRAFT DIVERTED TO CVG. REPLACED THE LT ENGINE ANTI-ICE COWL VALVE. 2L72 4F RTA21EA 20050411001252005041100125EA 2005 4 11 VTZA200500043 120050401A5320601R311719 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27638BR 7311 INTERCOSTAL CRACKED AT .250 INCH IN LENGTH ON RIGHT INBOARD SIDE AT FS 484 AT BL 36.00. 2L72 4F RTA21EA 20050411001272005041100127EA 2005 4 11 VTZA200500045 120050402A2750 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A VTZAL ABORTED APPROACH F FLT CONT AFFECTED APAPPROACH 1 EA27653BR 7438 FLAP FAIL AT 8 DEGREES ON APPROACH. RECORDED FECU FAULTS AND RESET IAW FIM 27-50-00. MSGS CLEARED FLAPS OPERATE NORMALLY. NO RECENT HISTORY NOTED. 2L72 4F RTA21EA 20050411001282005041100128EA 2005 4 11 VTZA200500046 120050401A3411 PITOT LINE CNDAIRCL600 CL6002B19 1900309EA AIRSPEED OBSTRUCTED A VTZAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 EA27625BR 7214 NO STANDBY AIRSPEED INDICATION ON TAKEOFF ROLL. PURGED STANDBY PITOT SYSTEM WITH NITROGEN. REF AMM 34-11-00. PERFORMED OPS CHECK ON STANDBY AIRSPEED, OPS CHECK GOOD. REF AMM 34-12-01. 2L72 4F RTA21EA 20050411001292005041100129WP 2005 4 11 ABXA050081 120050321A541299122432 BULKHEAD DOUG DC9 DC941 302207NWP LT PYLON CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23975AX 47512 WEB ON LEFT PYLON BULKHEAD WAS OIL CANNED AND CRACKED AT LOWER INBOARD LIGHTNING HOLE. REPAIRED AREA IAW DC-9 SRM 53-01. 2L72 4F A6WE 20050411001332005041100133CE 2005 4 11 20030815 120050405A27201295240835 ROD END BEECH 1900 1900D 1154162CE RUDDER BELLCRANKBROKEN A GLBAK NONE O OTHER ININSP/MAINT 1 NM03208GL UE208 DURING NON-ROUTINE INSPECTION, MAINTENANCE DISCOVERED LT RUDDER PEDAL INTERCONNECT ROD END WAS BROKEN AT RUDDER BELLCRANK. RODEND REPLACED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA24CE 20050411001342005041100134NM 2005 4 11 QXEA200500538 120050321A5730 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 600 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09416QX 4083 PDX - RIGHT WING LOWER SKIN IS CHAFED BY WING TO FUSELAGE FAIRING STRUCTURE, AFT OF LEADING EDGE SPAR. REPAIRED IAW SRM 57-10-30 AND SRM 51-21-10. 2H72 4T RTA13NM 20050411001352005041100135NM 2005 4 11 QXEA200500539 120050321A5420 DIAPHRAGM BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09416QX 4083 PDX - RIGHT OUTBOARD NACELLE DIAPHRAM CRACKED. REPAIRED IAW DHC-8-400 SRM 51-42-05, SRM 51-40-15 AND RD 8/4-31-155. 2H72 4T RTA13NM 20050411001392005041100139EA 2005 4 11 QXEA200500545 120050322A5530 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 300 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - VERTICAL STABILIZER, SKIN BELOW BOTTOM AFT CORNER OF PANEL 325FR IS GOUGED IN TWO PLACES. REPAIRED IAW CRJ700 SRM 51-25-01-001-01-A01. 2L72 4F RTA21EA 20050411001412005041100141EA 2005 4 11 QXEA200500547 120050321A5340 RAIL CNDAIRCL600 CL6002C10 1390015EA ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FORWARD FUSELAGE, FORWARD CARGO COMPARTMENT CARGO RETRIEVAL BIN RAILS, FORWARD LEFTHAND INBOARD ANODIZED COATING COMING OFF. REPAIRED IAW CRJ700 SRM 51-21-11-001-001-A01 AND SRM 51-21-06-001-001-A01. 2L72 4F RTA21EA 20050411001442005041100144NM 2005 4 11 AWXA200500401 120050303A531369353501 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 DURING C-16 CHECK A .375 INCH CRACK WAS FOUND IN STRINGER TIE CLIP ON FWD SIDE OF BS 727A, STR 27 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 727A, STR 27 LT; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER DWG 69-35350; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050411001452005041100145NM 2005 4 11 AWXA200500402 120050405A3397BMS13311122 WIRE BOEING737 7373G7 1384595NM SEAT ROW 21 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 PHX - EEL - DURING 4-DAY CHECK, FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 21 LT INOPERATIVE. MAINTENANCE REPAIRED A BROKEN EMERGENCY ESCAPE PATH LIGHT WIRE UNDER SEAT AT SEAT ROW 21 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050411001472005041100147NM 2005 4 11 AWXA200500404 120050311A5315654681143 FLOORBEAM BOEING737 737375 13844BNNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 MCN - MAJOR REPAIR - DURING C-05 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOORBEAM UPPER CHORD AT BS 986, BETWEEN LBL 3 AND LBL 40. MAINTENANCE REMOVED CORRODED SECTION OF FLOORBEAM UPPER CHORD AT BS 986, FROM LBL 3 TO LBL 40; FABRICATED A NEW REPLACEMENT SECTION OF FLOORBEAM UPPER CHORD; INSTALLED REPAIR PART IAW B737-300 SRM 53-60-51, FIG. 202. 2L72 4F RTA16WE 20050411001492005041100149NM 2005 4 11 AWXA200500406 120050318A5743656717217 FITTING BOEING737 737375 13844BNNM LT WING CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 DURING C-05 CHECK CORROSION WAS FOUND ON LT MAIN LANDING GEAR STABILIZER BEAM AFT ATTACH FITTING WHERE IT CONNECTS TO LOWER WING AT RS 197. MAINTENANCE REMOVED AND REPLACED LT MAIN LANDING GEAR STABILIZER BEAM AFT ATTACH FITTING IAW SOPM 20-50-01. 2L72 4F RTA16WE 20050411001502005041100150NM 2005 4 11 AWXA200500407 120050311A5320654681282 WEB BOEING737 737375 13844BNNM FUSLEAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 DURING C-05 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF LT AFT OUTBOARD WEB BETWEEN BS 995 AND BS 1015, LBL 38 AND LBL 42. MAINTENANCE REMOVED CORRODED LT AFT OUTBOARD WEB FROM BS 995 TO BS 1015, LBL 38 TO LBL 42; FABRICATED A NEW REPLACEMENT WEB PER DWG 65-46812; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050411001512005041100151NM 2005 4 11 AWXA200500408 120050313A532069417579 INTERCOSTAL BOEING737 737375 13844BNNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 DURING C-05 CHECK EXFOLIATION CORROSION WAS FOUND ON FORWARD CARGO COMPARTMENT INTERCOSTAL AT FORWARD SIDE OF BS 500D, STR 26 LT. MAINTENANCE REMOVED CORRODED INTERCOSTAL AT BS 500D, STR 26 LT; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER DWG 69-41757; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050411001522005041100152EA 2005 4 11 QXEA200500543 120050320A1430 RIVET CNDAIRCL600 CL6002C10 1390015EA ZONE 200 SMOKE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE EXTERIOR HAS SMOKING RIVET AT FUSELAGE STATION 485. REPAIRED IAW CRJ700 SRM 51-25-001-001-A01. 2L72 4F RTA21EA 20050411001532005041100153SO 2005 4 11 20030811 120050330A5297 WIRE EMB 120 EMB120ER 3260203SO CONTROL SWITCH LOOSE A GLBAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 NM03293UX 120293 FORWARD CABIN DOOR WOULD NOT OPEN WITHOUT USING DOOR ACTUATOR BYPASS SWITCH. AIRCRAFT WAS FERRIED TO MAINTENANCE BASE AND INVESTIGATION REVEALED SOLDER JOINTS NEEDED REPAIR ON FWD DOOR CONTROL SWITCH S0026. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA31SO 20050411001572005041100157NM 2005 4 11 AWXA200500409 120050323A531369402342 GUSSET BOEING737 737375 13844BNNM STRINGER CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 DURING C-05 CHECK CORROSION WAS FOUND ON RT STRINGER GUSSET AT BS 1088, STR 20 RT. MAINTENANCE REMOVED CORRODED RT STRINGER GUSSET AT BS 1088, STR 20 RT; FABRICATED A NEW REPLACEMENT GUSSET PER DWG 69-40234; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050411001582005041100158NM 2005 4 11 AWXA200500410 120050313A5320652072642 WEB BOEING737 737375 13844BNNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 DURING C-05 CHECK CORROSION WAS FOUND ON FORWARD CARGO COMPARTMENT THRESHOLD INBOARD WEB SILL BETWEEN BS 440 AND BS 492, STR 25 RT. MAINTENANCE REMOVED CORRODED WEB FROM BS 440 TO BS 492, STR 25 RT; FABRICATED A NEW REPLACEMENT WEB PER DWG 65-20726; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 8 AND 12. 2L72 4F RTA16WE 20050411001592005041100159NM 2005 4 11 AWXA200500411 120050311A534069427477 BRACKET BOEING737 737375 13844BNNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 DURING C-05 CHECK CORROSION WAS FOUND ON L-2 DOOR SILL FWD ATTACH CLIP (BRACKET) AT BS 956, LBL 51. MAINTENANCE REMOVED CORRODED BRACKET AT BS 956, LBL 51; FABRICATED A NEW REPLACEMENT BRACKET PER DWG 69-42747; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050411001602005041100160NM 2005 4 11 AWXA200500412 120050310A532066221871 CHANNEL BOEING737 737375 13844BNNM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 DURING C-05 CHECK A 11/16 INCH CRACK WAS FOUND ON INBOARD SIDE OF SUPPORT CHANNEL LOCATED ON AFT SIDE OF BS 520 FLOORBEAM AT RBL 24.75. MAINTENANCE REMOVED CRACKED SUPPORT CHANNEL AT BS 520. RBL 24.75; FABRICATED A NEW REPLACEMENT CHANNEL PER DWG 66-22187; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050411001612005041100161NM 2005 4 11 QXEA200500534 120050327A5310 STRUCTURE BOMBDRDHC8 DHC8401 1390041NM ZONE 700 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09416QX 4083 PDX - SHEET METAL PIECE JUST AFT OF LEFTHAND FORWARD NOSE LANDING GEAR DOOR ON NOSE LANDING GEAR SIDEWALL IS PUSHED UP AND CRUMPLED. REPAIRED IAW DHC-8-400 SRM 51-42-05. 2H72 4T RTA13NM 20050407002622005040700262EU 2005 4 7 AWXA200500044 120050111A5315D5347209800 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28621AW 053 SAL - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM Y920 AT FR 66 + 4". MAINTENANCE REMOVED DAMAGED FLOORBEAM Y920 FROM FS 66 TO FS 70; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050407002982005040700298EU 2005 4 7 MALA050122 120050108A53477253721495 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15425XJ 340B425 DURING 4Y/2Y CHECK IN BNA, GALLEY SEAT TRACK PROFILE PN 7253721-495 IS CORRODED OUT OF LIMITS AT FS 272. DAMAGED PART WILL BE REMOVED AND REPLACED IAW SRM NR 514021. REFER EAMS WO NR 211363, TASK 1514 FOR ADDITIONAL INFORMATION. AIRCRAFT WAS RELEASED 1/11/05. 2L72 4T RTA52EU 20050407003012005040700301EU 2005 4 7 MALA050127 120050111A53207253721439 STIFFENER SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15366PX 340B267 DURING 4Y/2Y INSPECTION IN BNA, WEB REINFORCEMENT PN 7253721-439 IS CORRODED OUT OF LIMITS. THE DAMAGED AREAS HAVE BEEN REPAIRED IAW SRM REFER EAMS WO NR 211360, TASK 2503 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 1/15/05. 2L72 4T RTA52EU 20050407003132005040700313EU 2005 4 7 05FDEA00851 120050405A5315 FLOORBEAM AIRBUS310 A310 EU FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 REPAIR NEEDS EVALUATION FOR FAA APPROVED DATA AND MAJOR OR MINOR CLASSIFICATION. FLOORBEAM NR 35 C R OF CENTER LINE. COMPLIED WITH FEDEX EA NR 6-5310-87772 AND CLASSIFIED AS A MINOR REPAIR PER FEDEX EA NR 6-5310-87772 AND FEDEX GMM 6-2-100. 2L72 4F RTA35EU 20050407003202005040700320NM 2005 4 7 05FDEA00853 120050405A5514 STRUCTURE DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT UPPER FORWARD SKIN PLANK NR 2L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82939. 2L73 4F RTA22WE 20050407003212005040700321NM 2005 4 7 SWAA050931 120050327A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29341SW 24091 DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 925, STR 20R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050407003242005040700324NM 2005 4 7 SWAA050933 120050328A52406969854 FRAME BOEING737 7375H4 138449DNM R1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29501SW 24178 DURING SCHEDULED 1/2D CHECK, FOUND R1 DOOR LOWER AFT FRAME CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20050407003252005040700325NM 2005 4 7 05FDEA00788 120050401A5514 STRUCTURE DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZONTAL STAB RT UPPER CENTER SKIN PLANK NR 16R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82953. 2L73 4F RTA22WE 20050407003292005040700329EU 2005 4 7 05FDEA00565 120050315A5330 SKIN AIRBUS310 A310 EU FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 REPAIR NEEDS EVALUATION FOR FAA APPROVED DATA AND MAJOR OR MINOR CLASSIFICATION. ITEM NR 20 OF LIST FUSELAGE DOUBLER LOWER LT SIDE AFT OF LT MLG DOOR OPENING. FUSELAGE DOUBLER FOUND TO BE IN CONFORMANCE WITH AIRBUS DWG A538-12568 LOWER LT SIDE AFT OF LT MLG DOOR. 2L72 4F RTA35EU 20050408000012005040800001 2005 4 8 P5CA0501335 420050403A3457 DATA CARD BOEING747 747283B 1384867NM GPS FAILED A P5CAK NONE O OTHER ININSP/MAINT 1 EA15921FT 21575 GPS DATA CARD FAILED. TRANSFERRED TO DMI 34058 PER MEL 34-27-2S. 2L74 4F A20WE 20050408000062005040800006NM 2005 4 8 QXEA200500487 120050312A5330 SKIN DHAV DHC8 DHC8202 2809007NM ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09366PH 510 PDX - FUSELAGE SKIN AT STATION 302 TO STATION 333 BETWEEN STRINGERS 29R AND 30R HAS SEVERAL SMALL IMPACT GOUGES. REPAIRED IAW HORIZON AIR EA 2-53-611. 2H72 4T RTA13NM 20050408000182005040800018 2005 4 8 ASMF200503018 420050324A23126223255001 CONNECTOR DOUG DC9 DC982 3022082WP NR 1 VHF SYSTEM FAILED W ASMFC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW231003Y7892 48068 AIRCRAFT WAS RECEIPT AT GDL WITH CAPTAIN REPORT "VHF 1 OUT OF SERVICE", AS A CORRECTIVE ACTION BOTH VHF WERE REPLACED AN TESTED, ALL CORRECT. AIRCRAFT RETURNED OF FLIGHT AS A CONSEQUENCE OF VHF FAILURE CONTINUED. COAXIAL CABLE AND VHF NR 1 WERE CHECKED IAW MM 34-51-01, TESTED CORRECT. AS A PRECAUTIONARY ACTION, VHF NAV NR 1 CONNECTOR WAS REPLACED AND TESTED IAW MM 34-32-00. 2L72 4F A6WE 20050408000202005040800020EA 2005 4 8 MASA200500156 120050225A2410820465 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA ADG FAILED A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW077727828126 7278 ASH 6332 AUS-PHX . PILOT RETURNED THE AIRCRAFT TO THE FIELD DUE TO AN ADG DEPLOYMENT ON ROTATION. CONTRACT MAINTENANCE SECURED THE ADG CLOSED AND THE AIRCRAFT WAS FERRIED TO PHX FOR MAINTENANCE. MAINTENANCE REPLACED ADG CONTROLLER, OPS CHK GOOD. 2L72 4F RTA21EA 20050408000232005040800023NM 2005 4 8 DHL2005782556 120050317A5500 RIB BOEING727 727227 1384078NM PANEL GOUGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 RT NR 5 BALANCE PANEL I/B RIB GOUGED. REMOVED RT NR 5 BALANCE BAY I/B SEAT PLATED FOR ACCESS IAW 727 SRM 51-30-2. EVALUATED DAMAGED TO BE OUT OF LIMITS IAW SRM 55-10-1 FIG 1. REMOVED RT NR 5 BALANCE PANEL I/B RIB IAW B727 SRM 51-30-2 AND INSTALLED NEW RIB PN 65-17-442-3 PO NR 503085 IAW S/B 727-55A091 REV FIG 8 AND REINSTALLED SEAL PLATE IAW B727 SRM 51-30-2. 2L73 4F A3WE 20050408000252005040800025WP 2005 4 8 DHL2005805002 120050407A33505708458505 BATTERY PACK DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01805DH 46125 ON CREW PRE-FLIGHT, EMERG EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY ASSY, OPS CHECK GOOD PER MM 33-50-2. 2L74 4F RT4A25 20050408000512005040800051NE 2005 4 8 ASMF200501016 220050127A73207791005 FUEL CONTROL BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE RT ENGINE MALFUNCTIONED W ASMFD RETURN TO BLOCK YJ ENGINE STOPPAGE WARNING INDICATION TXTAXI/GRND HDL 1 SW23703AM197 27203 726736 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING TAXING AND AFTER RIGHT ENGINE STARTING AUTO-SHUTDOWN WITHOUT ANY APPARENT CAUSE. CAPTAIN PERFORMED CLEANING PROCEDURE FOR ENGINE REVISION. ENTRANCE, EXHAUST AND MASTER CHIP DETECTOR OF RIGHT ENGINE WERE CHECKED, BEING CORRECT. UNITS WERE CHECKED BY CONDITION, ALL CORRECT. CLEANING PROCEDURE WAS APPLIED AND ENGINE WAS RESTARTED WITH ALL PARAMETERS WERE NORMAL AND EGT'S STABILIZED AT 339 GRADES. DURING OVERNIGHT SERVICE, RIGHT ENGINE FCU WAS REPLACED IAW MM 73-21-00 AND ENGINE WAS TESTED IAW MM 71-00-00, ALL CORRECT. 2L72 4F4 FRTA2NM E17NE 20050408000602005040800060NM 2005 4 8 QXEA200500203 120050209A3230574205A SELECTOR VALVE DHAV DHC8 DHC8202 2809007NM MLG INOPERATIVE A QXEAO OTHER O OTHER APAPPROACH 1 NM09353PH7599 7599 496 SEA - FLIGHT 2039 - ON APPROACH, THE GEAR HANDLE WAS PUT DOWN BUT THE GEAR DID NOT COME DOWN AND THREE RED LIGHTS WERE ILLUMINATED. NORMAL HYDRAULIC PRESSURE AND QUANTITY WERE NOTED. THE GEAR EVENTUALLY CAME DOWN USING THE ALT EXTENSION METHOD. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR SELECTOR VALVE IAW AMM 32-33-11. OPS CHECKS GOOD. 2H72 4T RTA13NM 20050408000722005040800072WP 2005 4 8 AALA20050138 120050222A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21470AA 49600 SAT - OVERHEAD EMERGENCY LIGHTS FROM ROWS 22 TO 27 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS FROM ROWS 22 TO 27. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050408000742005040800074NM 2005 4 8 AALA20050146 120050224A3350 LIGHT BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE O OTHER ININSP/MAINT 1 SW21379AA 25448 DFW - EMERGENCY LIGHT AT SEAT 36B INOPERATIVE. SECURED LOOSE CONNECTION FOR EMERGENCY LIGHT AT SEAT 36B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050408000752005040800075EU 2005 4 8 AALA20050141 120050224A3350 BATTERY PACK AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217055A 462 JFK - EMERGENCY LIGHTS AT RIGHT NUMBER ONE DOOR, FORWARD STRIP LIGHTS, AFT STRIP LIGHTS AND EXIT STRIP LIGHTS INOPERATIVE. REPLACED BATTERY PACK 11OWL2 FOR EMERGENCY LIGHTS AT RIGHT NUMBER ONE DOOR, FORWARD STRIP LIGHTS, AFT STRIP LIGHTS AND EXIT STRIP LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20050408000762005040800076EA 2005 4 8 QXEA200500182 120050122A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - LEFT OUTBOARD SIDE FACING SEAT RAIL, AT STATION X753, HAS PITTING CORROSION ON INNER AND MOST INBOARD SURFACES. REPAIRED IAW CRJ SRM 51-21-06-001-001-A01 AND HORIZON AIR EA R-53-266. 2L72 4F RTA21EA 20050408000792005040800079EA 2005 4 8 QXEA200500183 120050124A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - LEFT OUTBOARD SIDE FACING SEAT RAIL AT STATION X708, HAS PITTING CORROSION ON MOST INBOARD SURFACE. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01, HORIZON AIR EA R-53-266 AND REO 670-53-00-060, REV B. 2L72 4F RTA21EA 20050408000922005040800092NM 2005 4 8 72300003 120050202A5340 STRINGER CLIP BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 APPROX 2 INCH BY 2 INCH AREA OF CORROSION ON CLIP. 2L73 4F4 FRTA3WE E2EA 20050408000962005040800096NE 2005 4 8 HNAA0500011 220050216A73207898426009 EEC DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE INOPERATIVE A HNAAD RETURN TO BLOCK R PARTIAL RPM/PWR LOSS CLCLIMB 1 EA07824EX 387 ON CLIMB-OUT AT 500 FEET, NR 2 TORQUE WAS FLUCTUATING 70 TO 100 PERCENT AND PROP WAS FLUCTUATING 900 TO 1200. REMOVED AND REPLACED NR 2 ENGINE EEC. OPS CHECK GOOD. 2H72 4T4 TRTA13NM E20NE 20050408001032005040800103EU 2005 4 8 05FDEA00748 120050331A5313 STRINGER AIRBUS310 A310 EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 AFT OF BULK CARGO BILGE AREA STGR 53 LT HAS 2 AREAS OF CORROSION BETWEEN FR 70-71. REMOVED REQUIRED FASTENERS AND REMOVED CORROSION IAW A310-200 SRM 51-40-21 AND SRM 51-74-10. MATERIAL LOSS AFTER CORROSION REMOVAL WENT OUT OF LIMITS IAW A310-200 SRM 53-10-00. CUT OUT DAMAGED STRINGER SECTION AND FABBED REPAIR STRINGER AND SPLICE IAW A310-200 SRM 53-10-14. RESTORED SURFACE PROTECTIVE COATING IAW A310-200 SRM 51-21-10. INSTALLED STRINGER REPAIR IAW A310-200 SRM 53-10-14. 2L72 4F RTA35EU 20050408001282005040800128NM 2005 4 8 SWAA050998 120050404A335065C27093 LIGHT BOEING737 7373A4 1384585NM R2 DOOR BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 R2 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY & BATTERY PACK PER MM. 2L72 4F RTA16WE 20050408001392005040800139NM 2005 4 8 WRNA200500008 120050403A5220 FITTING BOEING747 747200 1384847NM ESCAPE HATCH OUT OF ADJUST A WRNAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO05524UP 21446 UPPER DECK ESCAPE HATCH MADE A LOUD BANG AT 23,000 FT. UNABLE TO HEAR DUE TO ESCAPING AIR. AIRCRAFT RETURNED TO AIRFIELD. LANDING NORMAL. ADJUSTED BAYONET FITTING ON THE HATCH. INSPECTED HATCH INTERIOR AND EXTERIOR IAW 52-21-00. ALL CHECKS SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. 2L74 4F RTA20WE 20050408001432005040800143SO 2005 4 8 MASA200500264 120050401A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSBURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07860MJ 145773 LEFT HAND OVERWING EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT. 2L72 4T RTT00011AT 20050408001442005040800144EA 2005 4 8 MASA200500267 120050402A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSBURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0727172 7172 ASH 2601 MCI TO PHL, THE PILOT REPORTED THE CABIN CEILING EMERGENCY FLOOD LIGHT JUST FORWARD OF THE MOST AFT EMERGENCY LIGHT WAS INOPERATIVE. THE LIGHT WAS PLACED ON DEFERRAL WITH THE CAPTAIN. 4/3/05 MX RELAMPED, OPS CHECK GOOD. 2L72 4F RTA21EA 20050411000112005041100011WP 2005 4 11 WX0500036 120050327A49203732052 PRESSURE SWITCH DOUG DC9 DC983 3022083WP APU FAILED A WX0AA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP19861GA 49557 LAS TO FNL - CREW REPORTED APU AUTO SHUTDOWN DUE TO LOW OIL PRESSURE IN FLIGHT. AIRCRAFT RETURNED TO LAS AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED OIL PRESSURE LOW SWITCH IAW MM 49-90-03. APU OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050411000172005041100017EA 2005 4 11 SWIA200514834 120050406A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLT SPOILER MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CRCRUISE 1 NM07927SW 7693 SPOILERON FAULT STATUS MESSAGE EN ROUTE. REPLACED RIGHT SPOILERON OUTBOARD PCU IAW CRJ MM 27-62-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050411000892005041100089NM 2005 4 11 SWAA050990 120050403A3350101073 LENS BOEING737 7375H4 138449DNM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29501SW 24178 DURING SCHEDULED 1/2D CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE AT FWD GALLEY. SECURED LENS PER MM. 2L72 4F RTA16WE 20050411000922005041100092NM 2005 4 11 SWAA050993 120050401A2560P4010021 BATTERY BOEING737 7373H4 1384600NM FLASHLIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29617SW 27700 FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2L72 4F RTA16WE 20050411001162005041100116EA 2005 4 11 SWIA200514807 120050326A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN DOOR INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07408SW 7055 EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT AT CABIN DOOR, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050411001192005041100119NE 2005 4 11 WRNA200500006 220050318A7200CF650C2 ENGINE AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE NR 2 UNSERVICEABLE A WRNAJA DUMP FUEL UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO05501TR379565540 53 517898 DURING CLIMBOUT NR 2 ENGINE EXCEEDED EGT LIMITS. WHEN LIMITS WERE IN NORM OPERATING RANGE NO RESPONSE WAS SEEN WHEN THROTTLES WERE ADVANCED. FUEL DUMP PROCEDURES FOLLOWED, AIRCRAFT RETURNED TO AIRPORT, LANDING NORMAL. REMOVED AND REPLACED NR 2 ENGINE IAW A300-71-007. RUN UP CHECKS AND LEAK CHECKS ALL SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA35EU E23EA 20050411001222005041100122NM 2005 4 11 AWXA200500385 120050311A53206545855522 WEB BOEING737 737375 13844BNNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 MCN - MAJOR REPAIR - DURING C-05 CHECK EXFOLIATION CORROSION WAS FOUND ON RIGHT AFT OUTBOARD WEB BETWEEN BS 996 AND BS 1016, RBL 44 AND RBL 46. MAINTENANCE REMOVED DAMAGED RIGHT AFT OUTBOARD WEB FROM BS 996 TO BS 1016, RBL 44 TO RBL 46; FABRICATED A NEW REPLACEMENT WEB PER DWG 65-45855; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050411001262005041100126EA 2005 4 11 VTZA200500044 120050401A5320601R3117117 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27638BR 7311 INTERCOSTAL CRACKED AT .250 INCH IN LENGTH ON LEFT INBOARD SIDE AT FS 484 AT BL 36.00. 2L72 4F RTA21EA 20050411001302005041100130NE 2005 4 11 QXEA200500639 220050406A732079821330007 EEC DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE NR 2 ENGINE MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09359PH119922900 514 PCEAG0061 SEA FLIGHT NR 2156 CLIMB TORQUE WAS APPROXIMATELY 107 PERCENT, NR 2 ENGINE MANUAL CAUTION LIGHT ON CLIMB-OUT, TORQUE INDICATED 124 PERCENT UPON CAUTION LIGHT PULLED POWER BACK IMMEDIATELY. RAN NR 2 ENGINE MANUAL CHECKLIST. CAUTION LIGHT EXTINGUISHED, TORQUE BUG RESTORED MOMENTARILY THEN DROPPED BACK DOWN. ENGINE RAN NORMALLY. MAINTENANCE REPLACED THE EEC UNIT AND T1 SENSOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20050411001372005041100137EA 2005 4 11 QXEA200500551 120050324A5320 ANGLE CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE INTERIOR, FUSELAGE STATION 280 AT LBL9 AND RBL9 TEE ANGLES ARE CRACKED. REPAIRED IAW CRJ700 SRM 51-42-20-001-001-A01 AND SRM 51-40-11-001-001-A01. 2L72 4F RTA21EA 20050411001422005041100142CE 2005 4 11 20030808 120050326A5511 SPAR BEECH 1900 1900D 1154162CE HORIZONTAL STAB CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03251GL UE251 HORIZONTAL STAB MAIN SPAR CENTER WEB SKIN CRACKED AT DEICE HOLE IN FOUR PLACES APPROX 1 INCH LONG. REPAIRED PER EO. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA24CE 20050411001462005041100146NM 2005 4 11 AWXA200500403 120050311A53136552928604 STRINGER BOEING737 737375 13844BNNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 DURING C-05 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER 27 LT AT BS 986. MAINTENANCE CUTOUT DAMAGE IN STRINGER 27 LT AT BS 986; FABRICATED A CHANNEL AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-03, FIG 201. 2L72 4F RTA16WE 20050411001632005041100163NM 2005 4 11 QXEA200500536 120050322A5320 SILL BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09416QX 4083 PDX - LIGHT CORROSION AROUND NUT PLATES AND SCREW HOLES ON TOP AND UNERSIDE OF MAIN CABIN DOOR DOOR SILL. REPAIRED IAW SRM TASK 51-21-00-350-801 AND SRM 51-25-10. 2H72 4T RTA13NM 20050411001672005041100167WP 2005 4 11 ASMF200502006 120050206A275039177785503 VALVE DOUG DC9 DC987 3022087WP FLAP DAMAGED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23751RA373571517 49779 DURING TRANSIT OVERNIGHT SERVICE, IT WAS DETECTED THAT OCCASIONALLY THE FLAPS DID NOT RETRACT COMPLETELY AND, IF THEY WERE DOWN AND UP DID NOT STORE TOTALLY. AIRCRAFT WAS SENT TO THE HANGAR AND THE TWO SPEED VALVES AND PTU WERE REPLACED, IAW MM 27-52-01. ACTUATORS AND FLAPS CONTROL VALVE WERE REPLACED CONTINUING FAILURE. FLAPS ADJUSTMENT AND TESTED WERE PERFORMED IAW MM 27-50-00, ALL CORRECT. 2L72 4F RTA6WE 20050411001682005041100168WP 2005 4 11 WX0500014 120050204A2170 COALESCER BAG DOUG DC9 DC983 3022083WP ACM CONTAMINATED A WX0AC ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 WP19865GA 49998 IFP - ABORTED TAKEOFF (HIGH SPEED 110-115 KNOTS) DUE TO STRONG AND PRONOUNCED ACRID/RUBBERY SMELL. MAINTENANCE INSPECTED ACM’S, WATER SEPARATORS, DRAINS AND ANTI-ICE SCREENS WITH NO DEFECTS NOTED. MAINTENANCE CLEANED COALESCER BAGS. SYSTEM OPERATIONALLY CHECKED GOOD IAW MM 21-20-02. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050411001702005041100170 2005 4 11 45101012005 420050120A3418 COMPUTER LEAR 45 45LEAR 5170805CE STALL WARNING MALFUNCTIONED E J7SAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW05410FX 101 DURING TAKEOFF ROLL, AMBER LEFT STALL WARN FAIL CAS ANNUNCIATED AT 80 KIAS. CREW ABORTED TAKEOFF WITHOUT INCIDENT. CREW NOTED THAT STALL WARNING TESTED CORRECTLY AND THAT THE AOA INDICATOR REMAINED AT 12 O'CLOCK POSITION WITH VANES BEING MOVED BY HAND. PERFORMED FSR RECOMMENDATIONS: 1. SWAP STALL WARNING COMPUTERS AND RETEST. IF AOA VANES CONTINUE NOT TO MOVE. VIA MCOS - STALLS, VIEW VANE AOA DATA AND NOTE POSITION CHANGE WITH ACTUAL VANE MOVEMENT. NOTE ANY CURRENT OR STORED FAULTS. MX PULLED THE ACFT INSIDE AND LET IT SIT FOR ABOUT 3 HOURS AND NOW THE STALL TEST WORKS. MX REPLACED THE STALL WARNING COMPUTER. OPS CHECK NORMAL. AIRCRAFT HAS BEEN PARKED OUTSIDE IN TEMPS REACHING -45 DEGREES FOR PAST TW2L72 4F RTT00008WI 20050411001712005041100171CE 2005 4 11 452004012705 120050127A3297 ELEC CONNECTOR LEAR 45 45LEAR 5170805CE MLG CONTAMINATED E J7SAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW05605FX 2004 LANDING GEAR FAILED TO RETRACT, FOUND A70P1 CONNECTOR ON LANDING GEAR CONTROL MANIFOLD CONTAMINATED WITH HYD FLUID, CLEANED AND REINSTALLED. F/T GOOD. AFTER APPROX 50 CYCLES OF LANDING GEAR SYSTEM, NO DEFECTS NOTED. HYD FLUID CONTAMINATION ON ELECTRICAL CONNECTOR INTERFERING WITH CONTROL MANIFOLD RETRACT SIGNAL. 2L72 4F RTT00008WI 20050411001722005041100172NM 2005 4 11 DHL2005781517 120050212A5344 HINGE BOEING727 727227 1384078NM CARGO DOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A "C" CHECK, MAIN CARGO DOOR, LT AFT HINGE CRACKED. REMOVED AFT HINGE SECTION AT MCD IAW B727 SRM 51-30-2, DRILLED NEW HINGE P/N MS20001-16-7200 PO 9001289 DIM.18 INCH BY 2 INCH AND 12 INCH BY 2 INCH IAW S/B AEJ 01-01,TREATED AND PRIMED HINGE AND AREA IAW B727 SRM 51-10-2. INSTALLED HINGE IAW S/B AEIO1-01 REV B. 2L73 4F A3WE 20050411001732005041100173EU 2005 4 11 249 120050308A2913 PUMP SAAB SF340 SF340A 7850100EU HYD SYSTEM MALFUNCTIONED A UHLAD RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL17158SD 158SD ON 3-08-2005, FLIGHT NR 7883 FROM IAD TO DAY, ON TAKEOFF AIRCREW REPORTED THAT THEY WERE RECEIVING THE GEAR INTRANSIT LIGHT AND THAT THE HYD PUMP WAS CONTINUING TO OPERATE. ASKED AIRCREW TO CYCLE THE GEAR TO GET IT UP AND LOCK-- NO FIX. AIRCRAFT RETURNED TO IAD WITH NO FURTHER ISSUES. 2L72 4T RTA52EU 20050411001742005041100174NM 2005 4 11 DHL2005781521 120050213A5720 ANGLE BOEING727 727227 1384078NM RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A "C" CHECK: RT WING LEADING EDGE COVE PANEL INBD SUPPORT ANGLE IS CRACKED AT WS 130. REMOVED R/W L/E COVE PNL SUPPORT ANGLE AND FABBED NEW FROM 2024-T3 .050 PO NR 9001417 DIM 17 1/2 INCH BY 1 1/2 INCH IAW 727 SRM 57-20-2 FIG 1. NEW ANGLE TREATED AND PRIMED AND INSTALLED IAW 727 SRM 51-10-2 AND 51-30-2. 2L73 4F A3WE 20050411001762005041100176NM 2005 4 11 DHL2005782503 120050310A5330 SKIN BOEING727 727227 1384078NM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 BULGE L/SIDE FUSELAGE SKIN AFT OF STA 580 BELOW STR 24L. DAMAGE FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-30-1 FIG 1. CUT OUT DAMAGE AREA FABBED FILLER FROM 2024 T3 .050 PO NR 9001684 DIM 1 1/2 INCH BY 1 1/2 INCH AND DOUBLER FROM 2024 T3 .063 PO NR 9001634 DIM 7 1/2 BY 6 1/2 IAW B727 SRM 53-30-2 FIG 2 53-30-3 FIG 2. TREATED AND PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED REPAIR IAW B727 SRM 53-30-3 PG2. 2L73 4F A3WE 20050411001782005041100178EA 2005 4 11 MASA200500005 120050103A323046193 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA MLG SLOW A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07400MJ1 7309 ASH 2799 FROM PHL TO CHS RETURNED TO THE FIELD AFTER GETTING A GEAR DISAGREE AFTER TAKEOFF. MAINTENANCE REPLACED THE PRIORITY VALVE. 2L72 4F RTA21EA 20050411001792005041100179NM 2005 4 11 F3LA200500004 120050127A5315 FLOORBEAM BOEING737 73736Q 1384409NM FUSELAGE BROKEN A F3LAK NONE O OTHER ININSP/MAINT 1 NM03307FL 4290 28760 DURING C-7 CHECK, INSPECTION REPORTED FLOORBEAM AND WEB BROKEN AT STA 685 FROM LT FRAME TO SEAT TRACK BEAM. REPLACED L STUB FRAME PER SRM 51-40-02 AND 51-10-02. 2L72 4F RTA16WE 20050411001822005041100182NM 2005 4 11 ASMF200503024 120050331A4950 APU DOUG MD80 MD83 3023681NM MALFUNCTIONED W ASMFD RETURN TO BLOCK MJ OVER TEMP WARNING INDICATION TXTAXI/GRND HDL 1 SW23945AS 49643 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF AFTER PUSH BACK, THE RIGHT ENGINE HAD A HOT STARTING PROMOTED BY LOW PRESS FORM THE APU. ENGINES WERE STARTED WITH A GPU AND APU WAS DEFERRED IAW MEL 49-1-2. DURING OVERNIGHT SERVICE, APU WAS TESTED IN BOTH MODES IAW MM 49-00-00, ALL CORRECT. DEFERRED REPORT WAS CLOSED. 2L72 4F RT 20050411001942005041100194SO 2005 4 11 C2XA05SH018 120050320A532014521713003 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715910 145455 SHV-DURING C-CHECK, THE CENTER OMEGA BEAM AT FRAME 20 CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED REPAIR IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050411001952005041100195SO 2005 4 11 C2XA05SD016 120050318A2611 ENGINE EMB 145 EMB145XR 3260214SO ALLSN AE300 AE3007A GL NR 2 MALFUNCTIONED A C2XAO OTHER J WARNING INDICATION CLCLIMB 1 SW27141175930 145674 CAE312307 SDF - LOG PAGE 1033424 - LAV SMOKE INDICATION CAME ON IN FLIGHT AT 13,500 FT FOR A COUPLE OF MINUTES. REMOVED AND REPLACED NR 2 ENGINE. OPS AND LEAK CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE. 2L72 4F4 FRT TE6CH 20050411001962005041100196SO 2005 4 11 C2XA05IA048 120050321A32348271013 HANDLE EMB 145 EMB145LR 3260212SO MLG INOPERATIVE A C2XAO OTHER O OTHER NRNOT REPORTED 1 SW27165591024610246 145603 ZIH - FLIGHT 2870, THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT EXTEND WITH THE GEAR HANDLE, AND NO WARNING WAS PRESENTED WITH THE FAILURE. THE AIRCRAFT LANDED IN ZIH WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FERRIED IT TO IAH WHERE IAH MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR HANDLE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050411001992005041100199NM 2005 4 11 05FDEA00728 120050331A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZ STAB LT UPPER FWD SKIN PLANK NR 9L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82939. 2L73 4F RTA22WE 20050411002012005041100201EA 2005 4 11 QXEA200500169 120050120A5315 FLOORBEAM CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - FUSELAGE STATION 280 RIGHT FLOORBEAM IS CORRODED ALONG TOP FLANGE FROM BL-0 TO RBL40. REPAIRED IAW REO 670-53-11-047. 2L72 4F RTA21EA 20050411002042005041100204NM 2005 4 11 2005000001 120050102A2750 WARNING LIGHT BOEING757 757* NM TE FLAPS ILLUMINATED A CNMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SW07549AX 24528 TRAILING EDGE FLAP DISAGREE EICAS MESSAGE ON APPROACH WHEN FLAPS 20 WERE SELECTED SPEED APPROX 190 KIAS. INDICATOR SHOWED 17 DEGREES WHEN LIGHT CAME ON. APPROACH WAS DISCONTINUED DECLARED EMERGENCY AND ADVISED ATC OF NATURE OF PROBLEM. 2L72 4F RTA2NM 20050411002062005041100206NM 2005 4 11 DHL2005770004 120050401A2797 CONNECTOR BOEING727 7272B7 138407LNM TE FLAPS DIRTY A DHLAB EMER. DESCENT J WARNING INDICATION APAPPROACH 1 SO01770AT 21953 WHEN FLAPS SELECTED TO 2DEG INBD FLAP ASSYMETRIC PERFORMED ABNORMAL PROCEDURE ISOLATING INBD FLAP MOTOR CONTROL WHEN FLAP SELECTED 5 DEG ASSYMETRIC INBD FLAP LOWERED TO 5 DEG AND OUTBDS LOCKED OUT. ADJUSTED IND AND OUT FLAP XMITTERS AND CLEANED CONNECTORS, OPS CK GOOD IAW MM 27-52-13. OPS CK GOOD SEE ITEM 2 P FOR CORRECIVE ACTION, NO DEFECT NOTED IAW MM 27-52-13. 2L73 4F A3WE 20050411002122005041100212SO 2005 4 11 C2XA05IA025 120050209A3260852701 PROXIMITY SENSOR EMB 145 EMB145 3260210SO NLG INOPERATIVE A C2XAO OTHER E VIBRATION/BUFFET CLCLIMB 1 SW27199661367513675 145131 IAH - FLIGHT 3347- THE CREW REPORTED A LOUD RUMBLE NOISE PASSING THROUGH 19K COMING FROM THE NOSE, AND DIFFICULTY MAINTAINING 1000 FPM CLIMB AT 23K TO 24K. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NOSE THIRD UPLOCK PROXIMITY SWITCH. OPERATIONALLY CHECKED WITH NO DEFECTS. THE AIRCRAFT WAS TEST FLOWN SATISFACTORILY, AND WAS THEN APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050411002132005041100213NM 2005 4 11 P9RA20050070 120050217A5270834501 PROXIMITY SWITCH BOEING757 757236 1384971NM CARGO DOOR CONTAMINATED A P9RAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO11958PG 24118 CVG - LOW SPEED REJECTED TAKE OFF AT 70KTS FOR AFT CARGO DOOR INDICATION. PLACED DOOR INDICATION ON MEL 52-71-1. MAINTENANCE PROCEDURES COMPLIED WITH. ITEM CLEARED 2/19/2005; SYR MAINTENANCE ENTRY. TROUBLESHOT INDICATION SYSTEM PER FIM. SWITCH FOUND TO BE ADJUSTED PROPERLY. CMEL CLEARED. 2L72 4F RTA2NM 20050411002152005041100215SO 2005 4 11 C2XA05TY014 120050208A533014564093001 SKIN EMB 145 EMB145ER 3260211SO FUSELAGE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713936 145025 TYS, DURING A SCHEDULED INSPECTION, THE FUSELAGE SKIN WAS FOUND CRACKED AT FS 75. MAINTENANCE MEASURED DAMAGED AREA, CUT OUT, FABRICATED A DOUBLER AND INSTALLED I/A/W-EC5310-01320 AND IC2005-145/0271. 2L72 4F RTT00011AT 20050411002182005041100218NM 2005 4 11 05FDEA00326 120050302A5532652066024 PANEL BOEING727 727227 1384078NM VERTICAL STAB DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25496FE 21670 RT HORIZ STAB NR 5 BALANCE BAY UPPER SKIN PANEL HAS A SHARP PROTRUSION ON THE OTBD END. THE PANEL HAS CREASE ON O/B END. THE SRM REPAIRS FOR THIS PANEL ARE FOR CRACKS AND NOT DAMAGE OF THIS SIZE. (APPROX 3 INCH BY 1 1/2 INCH). FED-EX DRAWING SR27-55-0004 ALLOWS US TO FABRICATE A SIMILAR PANEL AT A DIFFERENT STAB LOCATION. REMOVED, FABRICATED AND INSTALLED RT HORIZONTAL STAB NR 5 BALANCE BAY PANEL IAW 7- 5510-86202. 2L73 4F A3WE 20050412000012005041200001NM 2005 4 12 ANCF200400042 120050322A2497 WIRE BOEING767 767284 1385184NM PWA 4060 PW4060 52119NE GENERATOR DRIVE CHAFED W ANCFO OTHER J WARNING INDICATION CRCRUISE 1 SO23988AN 24742 EICAS MSG L GEN DRIVE DISPLAYED GEN DRIVE LIGHT ILLUMINATED GEN DRIVE DISCONECTED IAW FIM 24-30-00 FIG 107 BLOCKS 1-2-11. PROCEDURE WAS PERFORMED AND FOUND CHAFING BETWEEN LINES 4-5 IN CONNECTOR D10964. IT WAS REPAIRED IAW WDM 24-11-21. 2L72 4F4 FRTA1NM E24NE 20050412000042005041200004EA 2005 4 12 COMA0560205 120050327A2613355924400 SENSOR CNDAIRCL600 CL6002B19 1900309EA RT PYLON FAULTY A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01435CA 7473 FLIGHT 5184 RECEIVED A RT 14TH STAGE DUCT MESSAGE DURING CLIMB OUT OF CVG. AIRCRAFT RETURNED TO THE FIELD. REPLACED THE 14TH STAGE HEAT SENSING ELEMENT. 2L72 4F RTA21EA 20050412000452005041200045NE 2005 4 12 ANCF200400043 220050319A7200 ENGINE DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE RIGHT BIRD INGESTION W ANCFO OTHER C F.O.D. TOTAKEOFF 1 SO23593AN 53093 P728105D DURING ROTATION THE RT ENGINE WAS IMPACTED WITH A BIRD. ALL ENGINE PARAMETERS WENT DOWN TO IDLE AND RETURNED SLOWLY TO NORMAL PARAMETERS IAW AMM 05-51-08 PAGE 601 BIRD STRIKE CONDITION. CHECK WAS ACCOMPLISHED AND NOT FOUND DAMAGE IN THE ENGINE AREAS. 2L72 4F4 FRT E9NE 20050412000672005041200067SO 2005 4 12 SIMA200508202 120050323A3397 CONNECTOR EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT MISINSTALLED A SIMAO OTHER W INADEQUATE Q C TXTAXI/GRND HDL 1 SO27718AE 145275 CREW REPORTED THE EMERGENCY FLOOR LIGHT EXIT LOCATOR TO BE INOPERATIVE. MAINTENANCE FOUND THE CONNECTOR NOT CORRECTLY CONNECTED. THE CANNON PLUG WAS RESECURED AND AN OPERATIONAL CHECK WAS COMPLIED WITH. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050412000692005041200069NM 2005 4 12 CALA0500099 120050408A55106575563 BEAM BOEING737 7373T0 1384582NM HORIZONTAL STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717326 23456 INSPECTION FOUND TOP AFT MID SECTION OF LT HORIZONTAL STABILIZER CORRODED AT AFT T/E STRAP AROUND SUPPORT RETAINER HOLES AT STAB STA 176.4 ON TOP SIDE OF T/E BEAM AT HINGE ATTACH POINT. A TRAILING EDGE BEAM REPAIR WAS INSTALLED IAW SRM 55-10-13, FIGURE 203, PAGE 207. 2L72 4F RTA16WE 20050412000852005041200085EU 2005 4 12 05FDEA00868 120050406A5730 SKIN AIRBUS310 A310 EU ZONE 600 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 WHILE WORKING EO 6-5710-7-5004 PT 4, RT WING FOR LANDING ASSY FOR PANEL 675CB, 2 EA HOLES NOTED ARE LARGER THAN DRAWING SIZE. THIS IS AN INCOMING CONDITION. HOLE NR 10 .390", EDGE MARGIN RIB .610", PLANK .760", NR 17 .390", EDGE MARGIN RIB .570", PLANK .840". HOLE SIZE SHOULD BE .310". REPAIRED HOLES IAW EA 6-5730-79121 2L72 4F RTA35EU 20050412000872005041200087NM 2005 4 12 05FDEA00866 120050406A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT UPPER AFT SKIN PLANK NR 36L BARREL NUT BORE FOUND EXCEEDED LIMITS. REWORK/REPAIR - 1-5510-7-5000 HAS BEEN COMPLIED WITH. 2L73 4F RTA22WE 20050412000892005041200089NM 2005 4 12 05FDEA00863 120050406A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT NR 2R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-83000. 2L73 4F RTA22WE 20050412000912005041200091NM 2005 4 12 05FDEA00861 120050406A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT NR 8R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-83000. 2L73 4F RTA22WE 20050412000932005041200093NM 2005 4 12 05FDEA00858 120050405A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT UPPER FORWARD SKIN PLANK NR 13L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82991. 2L73 4F RTA22WE 20050412000952005041200095NM 2005 4 12 05FDEA00856 120050405A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT UPPER FORWARD SKIN PLANK NR 11L BARREL NUT FOUND EXCEEDED LIMIT. REPAIRED IAW FEDEX EA 1-5510-82991. 2L73 4F RTA22WE 20050412000992005041200099NM 2005 4 12 05FDEA00842 120050405A5753 STRAP DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LEFT WING, OUTBOARD FLAP INBOARD HINGE TENSION STRAP SUPPORT CRACKED, FOUND ON THE SPOTFACE OF THE UPPER BOLT HOLE AT 3 O'CLOCK AND LOWER BOLT HOLE AT 6 O' CLOCK POSITIONS (VIEW LOOKING INBOARD) WITH CRACK. LENGTH APPROXIMATELY ONE-FOURTH (1/4) INCH AND ONE-EIGHTH (1/8) INCH RESPECTIVELY. KIT P/N 1575075004-03. REPLACED PER FEDEX EO 1-5750-7-5004 PART 1. 2L73 4F RTA22WE 20050412001002005041200100NM 2005 4 12 05FDEA00843 120050405A5753 STRAP DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25583FE 48421 RT WING, OUTBOARD FLAP INBOARD HINGE, TENSION STRAP SUPPORT FOUND CRACKED. KIT P/N 1575075004-0. REPLACED PER FEDEX EO 1-5750-7-5004 PART 2. 2L73 4F RTA22WE 20050412001012005041200101NM 2005 4 12 05FDEA00839 120050404A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON NR 26R BARREL NUT BORE FOUND EXCEEDED LIMITS. REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20050412001022005041200102NM 2005 4 12 05FDEA00838 120050404A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON NR 14R BARREL NUT BORE FOUND EXCEEDED LIMITS. REMOVED AND REPLACED IAW SRM 51-33-01 VOLUME II. 2L73 4F RTA22WE 20050412001032005041200103NM 2005 4 12 05FDEA00837 120050404A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 MAIN DECK CARGO SEAT TRACK FOUND CRACKED AT STA 1581 LBL 8. CUT AND REMOVED IAW SRM 53-70-00 FIG 1 VOL I. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-70-00 FIG 1 VOL I. 2L73 4F RTA22WE 20050412001042005041200104NM 2005 4 12 05FDEA00836 120050404A5347 SEAT TRACK DOUG MD11 MD11F 3023600NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 MAIN DECK CARGO SEAT TRACK FOUND CRACKED AT STA 1581 RBL 8. CUT AND REMOVED IAW SRM 53-70-00 FIG 1 VOL I. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-70-00 FIG 1 VOL I. 2L73 4F RTA22WE 20050412001052005041200105NM 2005 4 12 05FDEA00835 120050404A5347 SEAT TRACK DOUG MD11 MD11F 3023600NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 MAIN DECK CARGO SEAT TRACK FOUND CRACKED AT STA 1686 RBL 28. CUT AND REMOVED IAW SRM 53-70-00 FIG 1 VOL I. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-70-00 FIG 1 VOL I. 2L73 4F RTA22WE 20050412001062005041200106NM 2005 4 12 DHL2005782561 120050323A5753 SKIN BOEING727 727227 1384078NM TE FLAPS DELAMINATED A DHLAO OTHER O OTHER ININSP/MAINT 1 SO01782DH 21998 LT WING OB AFT FLAP OB TE CORNER DELAMINATED. REMOVED PREVIOUS REPAIR AND CUT OUT DELAMINATED AREA OF LOWER SKIN APPROX 7" BY 5" AT O/B CORNER AND VACUUM BAGGED FOR MOISTURE REMOVAL IAW B727 SRM 51-40-20 FIG 31. FABRICATED REPLACEMENT SKIN APPROX 7" BY 5" AND EXTERNAL DOUBLER APPROX 8 1/2" BY 6 1/2" FROM 2024 T3 .016 PO NR 9001660 IAW B727 SRM 57-50-2 FIG 4 CLEANED PREPPED APPLIED ADHESIVE PRIMER AND ADHESIVE TO REPAIR PARTS AND SURFACES AND VACUUM BAGGED FOR BONDING IAW B727 SRM 51-40-20 FIG 31. BONDED CLEANED TREATED PRIMED AND SEALED REPAIR IAW B727 SRM 51-40-20-FIG 31. 2L73 4F A3WE 20050412001072005041200107NM 2005 4 12 DHL2005782559 120050318A5753 SKIN BOEING727 727227 1384078NM TE FLAP DEBONDED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 LT I/B T/E FOREFLAP DISBONDED AT T/E. CUT OUT DISBONDED AREA AT TE APPROX 4 1/2" BY 1 3/4". REMOVED DAMAGED CORE APPROX 4 1/2" BY 1 3/4" AND VACUUM BAGGED FOR MOISTURE REMOVAL FABRICATED REPLACEMENT SKIN APPROX 4 1/2" BY 1 3/4" EXTERNAL DOUBLER APPROX 3 1/2" BY 7 1/2" FROM 2024 T3 .016 PO NR 9001660 AND REPLACEMENT CORE APPROX 4 1/2" BY 1 3/4" FROM DUR-5052-4.4-3/16-N-.050 PO NR 9911139. CLEANED PREPPED APPLIED ADHESIVE PRIMER AND ADHESIVE TO REPAIR PARTS AND SURFACES. VACUUM BAGGED FOR BONDING. BONDED CLEANED TREATED PRIMED AND SEALED REPAIR ALL MAINTENANCE ACTIONS ACCOMPLISHED IAW B727 SRM 57-50-2 FIG 3 AND 51-40-20 FIG 32. 2L73 4F A3WE 20050412001082005041200108NM 2005 4 12 DHL2005782557 120050318A5730 SKIN BOEING727 727227 1384078NM LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 L/WING T/E SURFACE CRACKED AT NR 4 SPOILER HINGE CUTOUT (3RD). STOP DRILLED CRACK SIZE .250 IAW B727 SRM 51-10-1. REMOVED NR 4 SPOILER IAW B727 MM 27-61-0. NDT AREA IAW B727 NDTM PART 6 51-00-00 FIG 23 CRACK TERMINATES AT STOP DRILL HOLE, FABRICATE DOUBLER USING 7075 T6 .071 PO NR 9001737 DIM 6" BY 4 1/2" IAW B727 SRM 57-30-4 FIG 10. TREATED AND PRIMED AREA IAW B727 SRM 51-10-2. INSTALLED DOUBLER IAW B727 SRM 51-30-2. 2L73 4F A3WE 20050412001092005041200109WP 2005 4 12 DHL2005802006 120050402A5297 WIRE DOUG DC8 DC873 302199CWP DOOR SWITCH SHORTED A DHLAO OTHER N FALSE WARNING TOTAKEOFF 1 SO01802DH 46076 LEFT GEAR DOOR UNSAFE LIGHT ILLUMINATED AFTER GEAR RETRACTION. JACKED PLANE PER DACO M/M 7-11-0. PERFORMED GEAR DOOR CHECKOUT PER DACO M/M 32-31-4. FOUND SHORTED POWER WIRE PIN 1 JUST FWD OF DOOR SWITCH. REPAIRED PER DACO M/M 20-50-1. DOOR CHECKS SERV. 2L74 4F RT4A25 20050412001102005041200110NM 2005 4 12 DHL2005764001 120050405A2780 CONTROL BOX BOEING727 727264 138408MNM LE FLAPS MALFUNCTIONED A DHLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01764AT 22984 LE FLAPS AMBER LIGHT CAME ON AFTER TAKEOFF WITH FLAPS 15. NR 1 LE DEVICE. NO INDICATION. C/W ABNORMAL PROCEDURE. ON APPROACH WHEN GEAR EXTENDED LIGHT NORMAL. REMOVED AND REPLACED L/E CONTROL BOX IAW MM 27.82.31. OPS CK SERVICEABLE. 2L73 4F A3WE 20050412001112005041200111NM 2005 4 12 DHL2005782552 120050316A5313 STRINGER BOEING727 727227 1384078NM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 FUSELAGE STRINGER 21 R CORRODED BS 441-490. CORROSION ON STR 21R BS 440 TO 490 OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 1. REMOVED STR 21R BS 440 TO 490 IAW B727 SRM 51-30-2. FABBED NEW FROM BAC 1498-142 PO NR 9001078 DIM 48 INCH LONG IAW B727 SRM 53-10-2 FIG9. NEW STR TREATED AND PRIMED IAW B727 SRM 51-10-2 AND INSTALLED IAW B727 SRM 51-30-2 AND 53-10-3 FIG 1. 2L73 4F A3WE 20050412001122005041200112NM 2005 4 12 DHL2005782551 120050316A5322 SHEAR TIE BOEING727 727227 1384078NM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 SHEAR TIE AFT STA 1166 BETWEEN STR 18-19R CORRODED. REMOVED SHEAR TIE IAW B727 SRM 51-30-2 CUT OUT DAMAGE ON FRAME SIZE 2 1/2 INCH BY 2 INCH IAW B727 SRM 53-10-1. FABRICATED FILLER SIZE 2 1/2 BY 2 INCH MAT USED 7075 T6 .063 PO NR 900860 AND DOUBLER MAT USED 7075 T6 .071 PO NR 900242 IAW B727 53-10-4 FIG 14 SIDE OF DOUBLER 6 1/4 INCH BY 4 INCH TREATED ALODINE AND PRIMED IAW B727 SRM 51-10-2. INSTALLED FILLER AND DOUBLER REPAIR IAW B727 SRM 53-10-4 AND FIG 14. 2L73 4F A3WE 20050412001132005041200113NM 2005 4 12 DHL2005782550 120050316A5311 FRAME BOEING727 727227 1384078NM FUSELAGE BENT A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 FRAME AT STR 26 R STA 1110 BENT. CUT OUT DAMAGE AREA IAW B727 SRM 53-10-1 SIZE 2" BY 1". FABRICATED FRAME DOUBLER USING 7075 T6 .071 PO NR 9001298 DIM 10" BY 4" IAW B727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1. ALODINE AND PRIMED IAW B727 SRM 51-10-2. INSTALLED FRAME REPAIR IAW B727 SRM 51-30-2 AND 51-40-3 FIG 1. 2L73 4F A3WE 20050408000142005040800014NM 2005 4 8 DHL2005782566 120050331A5320 WEB BOEING727 727227 1384078NM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 AFT AIRSTAIR AREA, FUSELAGE STA 12 30 WEB IS CRACKED. CUT OUT DAMAGE AREA AT AFT AIRSTAIR STA 1230 DIM 5" BY 3 1/4" IAW B727 SRM 51-40-2 FIG 1. FABRICATED DOUBLER REPAIR-MAT-USED 7075-T6 .040 PO NR 9001777 DIM 8" BY 6 1/4" IAW B727 SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1. ALODINE AND PRIMED PART IAW B727 SRM 51-10-2. INSTALLED DOUBLER REPAIR IAW B727 SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1. 2L73 4F A3WE 20050408000192005040800019NE 2005 4 8 ASMF200503017 220050323A732176960613 FCU DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE LT ENGINE FAILED W ASMFE ENGINE SHUTDOWN J WARNING INDICATION NRNOT REPORTED 1 SW23751RA278225994 49779 718106 DURING LEFT ENGINE STARTING, EGT INCREASED UNTIL 512 GRADES SHUTTING DOWN THE ENGINE. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE LEFT ENGINE FUEL CONTROL UNIT WAS REPLACED IAW MM 73-20-01 AND ENGINE WAS TESTED IAW MM 71-00-00, ALL CORRECT. 2L72 4F4 FRTA6WE E9NE 20050408000412005040800041EA 2005 4 8 SWIA200514648 120050227A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07448SW 7678 CEILING EMERGENCY LIGHT AT ROW 5 INOPERATIVE. RELAMPED LIGHT AT ROW 5. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050408000442005040800044SO 2005 4 8 C2XA05IA023 120050209A326080069425 WARNING SYSTEM EMB 135 EMB135LR 3260305SO FUSELAGE INOPERATIVE A C2XAO OTHER N FALSE WARNING DEDESCENT 1 SW27245173353 2978 145332 IAH - FLIGHT 2373, ON DESCENT THE CREW REPORTED A GPWS WARNING AND A LANDING GEAR WARNING. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE AURAL WARNING UNIT, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050408000472005040800047EA 2005 4 8 COMA0560184 120050318A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01466CA 7627 FLIGHT 5379 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2L72 4F RTA21EA 20050408000732005040800073WP 2005 4 8 AALA20050145 120050224A33506011779 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21962TW 53612 DFW - OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050408000802005040800080EA 2005 4 8 QXEA200500184 120050121A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - LEFT OUTBOARD SIDE FACING SEAT RAIL, AT STATION X676 TO X692, HAS PITTING CORROSION ON MOST INBOARD SURFACE. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01, REO 670-53-00-060, REV B AND HORIZON AIR EA R-53-266. 2L72 4F RTA21EA 20050408000882005040800088EU 2005 4 8 2005UALA00252 120050317A5230 SEAL AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CARGO DOOR LEAKING A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29425UA 508 CABIN PRESSURE INCREASED RAPIDLY DURING CLIMB FROM FL300-370. PRESSURIZED AIRCRAFT AND FOUND FWD CARGO DOOR LEAKING. REPLACED FWD CARGO DOOR SEAL AND PRESSURIZED AIRCRAFT, NO LEAKS NOTED. 2L72 4F4 FRTA28NM E40NE 20050408001022005040800102EU 2005 4 8 05FDEA00747 120050331A5313 STRINGER AIRBUS310 A310 EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 AFT OF BULK CARGO AT BILGE AREA, STRINGER 56 LT HAS NUMEROUS CORROSION ON STRINGER'S. RUNS THROUGH FRAME 70-71 AND FRAME 72, AS MARKED. REMOVED FASTENERS ON STR 56 LT AT FR 70-71 AND 72 IAW A310-200 SRM 51-40-21. REMOVED CORROSION IAW A310-200 SRM 51-74-10. MATERIAL LOSS OUT OF LIMITS. REMOVED STR 56 LT AT FR 69.5 TO FR 72 IAW A310-200 SRM 51-40-21. MATERIAL ID FOR REPAIR PARTS VERIFIED IAW A310-200 SRM 53-17-14. FABRICATED REPAIR PARTS IAW A310-200 SRM 53-10-14. TREATED, PRIMED AND TOP COATED REPAIR PARTS IAW A310-200 SRM 51-74-10. INSTALLED REPAIR PARTS IAW A310-200 SRM 51-40-21. 2L72 4F RTA35EU 20050408001052005040800105EU 2005 4 8 05FDEA00751 120050331A5313 STRINGER AIRBUS310 A310 EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 AREA BEHIND BULK CARGO BETWEEN FRAMES 72-74 LEFT SIDE AT STRINGER 48 HAS 15 SQ INCHES OF CORROSION. REMOVED CORROSION FR 72-74 FOUND TO BE OUT OF LIMITS IAW A310-200 SRM 53-10-00 FIG 104. REMOVED AND REPLACED STRINGER SECTION 48L FR 72 TO 78 IAW A310-200 SRM 53-10-14. 2L72 4F RTA35EU 20050408001112005040800111NE 2005 4 8 WRNA200500001 220050220A7261 CAP BOEING747 747200 1384847NM PWA JT9 JT9D7J 52054NE NR 1 ENGINE OIL LOOSE A WRNAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO05524UP 21446 702000 ON CLIMB-OUT FROM MIA, NR 1 OIL QTY STARTED TO DECREASE RAPIDLY. DID A PRECAUTIONARY ENG SHUTDOWN OF NR 1 ENGINE FOR OIL QTY LOSS. RETURNED TO AIRFIELD, LANDING NORMAL. MAINTENANCE INSPECTED NR 1 ENG AND FOUND OIL TANK CAP NOT IN CLOSE POSITION. SERVICED ENGINE TO PROPER AMOUNT AS REQUIRED. RESECURED ENGINE TANK OIL CAP. RUN UP CHECK ACCOMPLISHED, NO LEAKS NOTED, ENGINE OP'S CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L74 4F4 FRTA20WE E20EA 20050408001212005040800121NM 2005 4 8 SWAA050997 120050404A53306545776 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29503SW 24180 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 887, STR 25R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050408001232005040800123NM 2005 4 8 QXEA200500491 120050312A5330 SKIN DHAV DHC8 DHC8202 2809007NM ZONE 100 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09366PH 510 PDX - STATION X320/Z88 DENT IN FUSELAGE SKIN. REPAIRED IAW HORIZON AIR EA 2-53-611. 2H72 4T RTA13NM 20050408001302005040800130NM 2005 4 8 SWAA051000 120050404A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29410WN 27897 EEPLS COVER BROKEN AT FWD LT SIDE. REMOVED AND REPLACED COVER PER MM. 2L72 4F RTA16WE 20050408001332005040800133 2005 4 8 SWAA051002 420050405A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. INSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20050408001372005040800137NM 2005 4 8 SWAA051006 120050405A52106545776 SKIN BOEING737 737301 1384611NM L2 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER AFT CUTOUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050408001422005040800142EA 2005 4 8 MASA200500260 120050330A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSBURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0717175 7175 ASH 7133 IN IAD REPORTED A CABIN OVERHEAD CEILING EXIT LIGHT INOP. THE CREW COMPLIED WITH THE MEL. 3/30/05 MAINTENANCE RELAMPED, OPS GOOD. 2L72 4F RTA21EA 20050411000022005041100002SO 2005 4 11 MASA200500268 120050402A3397 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT LOOSE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07836MJ 145359 ASH FLT 2688 CLT TO ILM, FLOOR EMERGENCY EXIT LIGHTS ROW 3-7 WOULD NOT ILLUMINATE. MAINTENANCE SECURED LOOSE ELECTRICAL CONNECTOR AND PERFORMED OPERATIONAL TEST OF THE EMERGENCY LIGHTS. NO FURTHER DEFECTS NOTED. 2L72 4T RTT00011AT 20050411000032005041100003SO 2005 4 11 MASA200500273 120050403A3397 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT UNSECURE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07832MJ 145310 ASH 2640 CLT HAD THE FWD EMERGENCY EXIT PROX LIGHTING INOP. MAINTENANCE SECURED THE CONNECTION TO THE PROX LIGHTING ASSEMBLY. 2L72 4T RTT00011AT 20050411000062005041100006NM 2005 4 11 DHL2005753002 120050406A2120 A/C PACK BOEING727 727223 1384074NM LEFT NOISY A DHLAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO01753DH 22468 ABORTED T/O DUE TO SQUEAL AND AIRFLOW NOISE FROM LEFT PACK IN COCKPIT AREA, LOW SPEED ABORT AUTO PACK DID NOT ARM. TRANSFERRED TO MEL 21-1-2 REF DMI 20391. 2L73 4F A3WE 20050411000082005041100008NM 2005 4 11 HNAA00033 120050405A3230574205A SELECTOR VALVE DHAV DHC8 DHC8102 2809003NM MLG FAILED A HNAAO OTHER J WARNING INDICATION APAPPROACH 1 EA07810 3310433104 308 WHEN GEAR WAS SELECTED DOWN ALL GEAR SHOWED UNSAFE INDICATION (THREE RED). MAIN GEAR EXTENDED USING ALTERNATE EXTENSION. NOSE GEAR WOULD NOT EXTEND ON FIRST PULL OF ALT EXTENSION CABLE. FORCEFUL SECOND PULL DID EXTEND THE NOSE GEAR. REMOVED AND REPLACED THE LANDING GEAR SELECTOR VALVE, SERVICED AND BLED SYSTEM PERFORMED GEAR SWINGS GEAR EXTENDED NORMALLY USING ALTERNATE EXTENSION. 2H72 4T RTA13NM 20050411000162005041100016SO 2005 4 11 SWIA200514833 120050406A27513471001001 ANNUNCIATOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07561SW 120335 RETRACTED FLAPS AND RECEIVE A FLAP AND ADVANCED SWS ON MAP. REMOVED AND REPLACED THE FLAP ANNUNCIATOR IAW AMM 27-50-05. OPERATIONAL CHECK GOOD. P/N 347100-1001, S/N OFF 0214. 2L72 4T RTA31SO 20050411000232005041100023CE 2005 4 11 DXTA200500655 120050331A321067421801 BARREL CESSNA750 750 2076810CE MLG SCORED E DXTAO OTHER J WARNING INDICATION CLCLIMB 1 GL07936QS6801 7500036 DURING CLIMBOUT HEARD A THUMP FROM THE NOSE GEAR. NOTICED THE UNLOCK LIGHT ILLUMINATED. THE UNLOCK LIGHT STAYED ON FOR THE DURATION OF THE FLIGHT UNTIL DESCENT PASSING THROUGH 11700; IN WHICH A SECOND THUMP WAS HEARD. FOUND STRUT EXTENSION OUT OF LIMIT. REMOVED & REPLACED UPPER & LOWER BARREL ASSY WITH A RENTAL UNIT. OPS CHECK AND LEAK CHECK GOOD. STEERING TRAVEL CHECK GOOD. GEAR SWING CHECK GOOD IAW 750 M/M CHP 32-30-05. 2L72 4J RTT00007WI 20050411000282005041100028CE 2005 4 11 DXTA200500648 120050330A3700 LINE CESSNA750 750 2076810CE VACCUM SYSTEM CONTAMINATED E DXTABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL07970QS 7500070 BAGGAGE SEAL CAS MESSAGE CAME ON AT FL 430 (CABIN PRESS OK), APPROX 1 HOUR LATER BAGGAGE ALTITUDE MESSAGE APPEARED AND CABIN PRESS STARTED CLIMBING AT 1000 FPM. DESCENDED TO 32000 AND CLOSED BAGGAGE ISOLATION VALVE PER CHECKLIST. CABIN PRESS STABILIZED AT 3500 PRESS ALT. PERFORMED VACCUM EJECTOR TRAP CLEANING IAW CE-750 MM TASK 36-15-00-900, PURGED ALL MOISTURE FROM LINES WITH DRY N2. OPS CHECK OF BAGGAGE DOOR SEAL GOOD IAW CE-750 MM CHAPT 36-1-00. PERFORMED BAGGAGE COMP ISOLATION CHECK IAW CE-750 MM TASK 21-30-00-711. NO DEFECTS NOTED. 2L72 4J RTT00007WI 20050411000352005041100035NM 2005 4 11 SWAA051012 120050406A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29333SW 23697 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 727D + 2, STR 19R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050411000412005041100041SO 2005 4 11 MASA200500278 120050404A335066367 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07829MJ 145228 ASH 2715 CLT HAD THE EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE BETWEEN ROW 3 AND ROW 7. MAINTENANCE REPLACED THE LIGHTING ASSEMBLY. 2L72 4T RTT00011AT 20050411000432005041100043CE 2005 4 11 DXTA200500651 120050330A3240 BRAKE CESSNA500 560CESSNA 2076750CE MLG MALFUNCTIONED E DXTAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL07398QS 5600522 CO-PILOT LEFT BRAKE PEDAL EXCESSIVE TRAVEL & SPONGY. CHECKED BRAKE ASSEMBLIES, ALL VISIBLE BRAKE LINES, MASTER CYLINDERS, & RESERVOIR FOR LEAKS, NONE FOUND. CHECKED BRAKE LINE FITTINGS FOR LOOSENESS FITTINGS FOUND SATISFACTORY. WORK PERFORMED IAW 560 M/M 32-42-01 & 32-42-02. 2L72 4F RTA22CE 20050411000532005041100053NM 2005 4 11 SWAA050985 120050403A3350300432 LIGHT BOEING737 7373H4 1384600NM L1 DOOR INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29370SW 26597 L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20050411000612005041100061WP 2005 4 11 0500449943 120050402A2170 BOOT DOUG DC9 DC931 3022065WP WATER SEPARATOR BLOWN A NWAAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 GL011308T 47315 WHILE CRUISING AT FL330, THE RED CABIN PRESS ANNUNCIATOR LIGHT ILLUMINATED AS THE CABIN WAS CLIMBING THROUGH 11,000 FEET. AN EMERGENCY DESCENT WAS EXECUTED AND COMPLIED WITH COM PROCEDURES. FLIGHT DIVERTED TO DTW AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE DID BITE CHECK THE DCPC AND NO CURRENT FAULTS DISPLAYED. THE RIGHT SIDE WATER SEPARATOR BOOT WAS DISCONNECTED AND THE LEFT SIDE RAM AIR BOOT WAS LOOSE. THE RAM AIR BOOT WAS RESECURED AND THE WATER SEPARATOR BOOT WAS REPAIRED AND RECONNECTED. ALL CHECKS WERE GOOD AND THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20050411000622005041100062EA 2005 4 11 SWIA200514841 120050331A274070623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TRIM MOTOR FAILED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07944SW2192 2192 7764 ON ORIGINATING CHECK STAB CH 2 WILL NOT ENGAGE. INSTALLED SERVICEABLE MOTOR CONTROL UNIT IAW CRJ 200 MM 27-42-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050411000732005041100073NM 2005 4 11 SWAA050982 120050331A3350D71702001 BATTERY PACK BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29794SW 30605 DURING SCHEDULED HC1 CHECK, CABIN EMERGENCY LIGHTING BATTERY PACKS FAILED TEST. REMOVED AND REPLACED 7 EACH BATTERY PACKS PER MM. 2L72 4F RTA16WE 20050411000742005041100074NM 2005 4 11 SWAA050983 120050331A53306545774 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29670SW 23784 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 19. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050411000942005041100094 2005 4 11 SWAA050995 420050402A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29704SW 27838 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. INSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20050411001052005041100105SO 2005 4 11 CHQA200500067 120050330A3397 WIRE EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BROKEN A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11268SK 145270 EMERGENCY EXIT LIGHT IDENTIFIER IS INOPERATIVE. TROUBLESHOT PROBLEM TO A BROKEN WIRE AT W192-8588-22 PRIOR TO SPLICE SP9048 REF EMB AWM 33-50-50. REQUIRED REWIRE IAW EMB 145AMM 20-31-00. OPS CHECK GOOD IAW CHQ JC E33-50-00-710-001. 2L72 4T RTT00011AT 20050411001132005041100113EA 2005 4 11 SWIA200514830 120050331A27604916406 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07935SW 7725 DURING FLIGHT CONTROL CHECK RIGHT SPOILERON DEPLOYS 1/4 SCALE DURING LEFT FULL AILERON INPUT, THEN A SPOILERON FAULT STATUS MSG ILLUMINATED. REMOVED AND REPLACED NR 1 AND NR 2 SECU IAW 27-61-05. OPERATIONAL CHECK GOOD. P/N 49-164-06; S/N OFF 01717. 2L72 4F RTA21EA 20050411001322005041100132CE 2005 4 11 20030814 120050405A27201295240835 ROD END BEECH 1900 1900D 1154162CE RUDDER PEDALS BROKEN A GLBAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 NM03150GL UE150 ON TAKEOFF, AS SOON AS THE NOSEWHEEL LEFT THE GROUND THE CAPTAIN SIDE RUDDER PEDALS LOST EFFECTIVENESS. FO'S CONTROLS WERE WORKING NORMALLY AND CONTROL WAS TRANSFERRED AND AIRCRAFT LANDED SAFELY. MAINTENANCE DISCOVERED RUDDER PEDAL INTERCONNECT RODEND WAS BROKEN AT RUDDER BELLCRANK ATTACH. INTERCONNECT RODEND WAS REPLACED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA24CE 20050411001402005041100140EA 2005 4 11 QXEA200500546 120050324A5743 ATTACH FITTING CNDAIRCL600 CL6002C10 1390015EA ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - LT WING FORWARD MAIN LANDING GEAR ATTACHMENT POINT AREA SURFACE CORROSION ON RIVET HEADS/SURROUNDINGS. REPAIRED IAW CRJ700 SRM 51-21-00-001-001-A01, PARAGRAPH 6 AND SRM 51-25-00-001-001-A01. 2L72 4F RTA21EA 20050411001432005041100143NM 2005 4 11 TSAA0549006 120050202A4900 APU BOEING737 73776N 13844CHNM APU BAY NOISY A TSAAE ENGINE SHUTDOWN E VIBRATION/BUFFET CRCRUISE 1 WP13748AL 30050 LOUD THUNDERING SOUND BENEATH THE AFT RIGHT FLIGHT ATTENDANTS SEAT. THE NOISE WAS INTERMITTENT AFTER 2 HOURS. THE APU ELECT METER INDICATED BLANK CPS 4 +00 INTO FLT. APU GEN OFF BUSS LIGHT ILLUMINATED. APU EGT AS 360 DEG; AMPS & VOLTS = 0. APU SHUTDOWN MANUALLY. 1+00 HOURS REMAINING AT CRUISE. INSP AFT GALLEY, AFT CARGO PIT, EXT DOORS, OUTFLOW VALVE. UNABLE TO VERIFY SOUND ON GROUND. VERIFY FLT REQ’D. BITE CHK OF METERS PANEL OK. PUT HIGH ELECTR LOAD ON APU GEN-OK. ALL ANNUNCIATORS EXTINGUISHED. INDICATION NORMAL. IN FLT VERIF REQ’D. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA16WE 20050411001482005041100148NM 2005 4 11 AWXA200500405 120050313A5340652072615 ATTACH ANGLE BOEING737 737375 13844BNNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 DURING C-05 CHECK CORROSION WAS FOUND ON UPPER ATTACH ANGLE FOR INTERCOSTAL AT FORWARD CARGO COMPARTMENT THRESHOLD BS 460, STR 25 RT. MAINTENANCE REMOVED CORRODED ATTACH ANGLE AT BS 460, STR 25 RT; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 65-20726; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050411001552005041100155EA 2005 4 11 QXEA200500548 120050321A5347 CARGO TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FORWARD FUSELAGE, FORWARD CARGO COMPARTMENT RETREVIAL TRAY RAILS, FORWARD RIGHTHAND INBOARD RAIL HARD ANODIZED COATING COMING OFF. REPAIRED IAW CRJ700 SRM 51-21-11-001-001-A01 AND SRM 51-21-06-001-00-A01. 2L72 4F RTA21EA 20050411001642005041100164 2005 4 11 VW3R20050007 420050211A2565D29601103 EXTENSION AIRCRUISERS AIRBUS330 A300* EU GIRT BAR DEFECTIVE B VW3RK NONE W INADEQUATE Q C ININSP/MAINT 1 WP09ALL 0468 ALL GIRT EXTENSION DOES NOT FIT PROPERLY ON GIRT BAR. GIRT EXTENSION PADS RIDE UP ON CAVITY RIDGE OF GIRT BAR. PLEASE NOTE THIS EVACUATION SLIDE IS ALSO USED ON A310 AIRCRAFT. 2L72 4F RTA26NM 20050411001652005041100165 2005 4 11 VW3R20050008 420050211A2565D29601103 EXTENSION AIRCRUISERS AIRBUS330 A300* EU GIRT BAR DEFECTIVE B VW3RK NONE W INADEQUATE Q C ININSP/MAINT 1 WP09ALL 0407 ALL GIRT EXTENSION DOES NOT FIT PROPERLY ON GIRT BAR. GIRT EXTENSION PADS RIDE UP ON CAVITY RIDGE OF GIRT BAR. PLEASE NOTE THIS EVACUATION SLIDE IS ALSO USED ON A310 AIRCRAFT. 2L72 4F RTA26NM 20050411001662005041100166 2005 4 11 VW3R20050009 420050211A2565D29601103 EXTENSION AIRCRUISERS AIRBUS310 A310 EU GIRT BAR DEFECTIVE B VW3RK NONE W INADEQUATE Q C ININSP/MAINT 1 WP09ALL 0469 ALL GIRT EXTENSION DOES NOT FIT PROPERLY ON GIRT BAR. GIRT EXTENSION PADS RIDE UP ON CAVITY RIDGE OF GIRT BAR. PLEASE NOTE THIS EVACUATION SLIDE IS ALSO USED ON A310 AIRCRAFT. 2L72 4F RTA35EU 20050411001802005041100180NM 2005 4 11 HNAA0500006 120050129A531385320056107 STRINGER DHAV DHC8 DHC8102 2809003NM FUSELAGE CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07936HA 145 DURING C CHECK, FOUND WIDESPREAD CORROSION ON STR 31S. DUE TO WIDE SPREAD DAMAGE, DECISION WAS MADE TO REMOVE ENTIRE STR SECTION FROM X182 TO F /SPAR FS (X387) FOR CONVENIENCE. THIS IS A MAJOR REPAIR. REPAIR DONE IAW PIEDMONT E0 8-53-05-0023. 2H72 4T RTA13NM 20050411001832005041100183CE 2005 4 11 20030789 120050205A5511 SPAR BEECH 1900 1900D 1154162CE HORIZONTAL STAB CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03253GL UE253 DURING ROUTINE STRUCTURAL "I" INSPECTION, FOUR CRACKS WERE IDENTIFIED EMANATING FROM THE DE-ICE HOLE ON THE HORIZONTAL CENTER MAIN SPAR CENTER WEB SKIN APPROX 1" LONG EACH UNDER PANEL 332 ATC. REPAIR WAS MADE AND AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA24CE 20050411002002005041100200EA 2005 4 11 COMA0560185 120050320A2750860D10018 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION CRCRUISE 1 SO01466CA8073 7627 FLIGHT 5465- FLAP FAIL CAUTION. REPLACED THE FECU. 2L72 4F RTA21EA 20050411002072005041100207WP 2005 4 11 ASMF200502008 120050211A2910AC7031H8K1 HOUSING DOUG DC9 DC983 3022083WP HYD FILTER CRACKED W ASMFK NONE K FLUID LOSS TXTAXI/GRND HDL 1 SW23838AM55892 49397 CAPTAIN REPORTED THAT QUANTITY AND PRESSURE WERE LOOSE ON LEFT HYDRAULIC SYSTEM. DURING ENGINE RUNNING, A LEAK WAS DETECTED IN THE HOUSING OF THE HYDRAULIC PUMP FILTER. THE MODE FILTER HYDRAULIC LEFT SIDE PUMP ENGINE DRIVE WAS REPLACED IAW MM 29-10-14, TESTED CORRECT. PER STRONG HYDRAULIC FLUID SMELL, LEFT AIR CONDITIONING SYSTEM WAS DEFERRED IAW MEL 21-1. ADDITIONALLY AIR CONDITIONING WATER SEPARATOR WAS REPLACED IAW MM 21-20-02, TESTED CORRECT. 2L72 4F RTA6WE 20050411002112005041100211SO 2005 4 11 C2XA05TY016 120050208A533014520568005 SKIN EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713936 145025 TYS, DURING A SCHEDULED INSPECTION THE FUSELAGE SKIN INSIDE SURFACE AT THE POTABLE WATER MANIFOLD MOUNT, CORRODED. REMOVED THE CORROSION, ALODINED, FABRICATED NEW REPAIR DOUBLER AND INSTALLED, PAINTED AND PRESSURE CHECKED I/A/W-EC5330-01435. 2L72 4F RTT00011AT 20050411002142005041100214SO 2005 4 11 C2XA05TY010 120050203A571114567014003 SPAR EMB 145 EMB145ER 3260211SO WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717928 145007 TYS DURING THE ACCOMPLISHMENT OF A NDI TASK(57-28-00) A CRACK INDICATION WAS DISCOVERED. MAINTENANCE FAB`D AND INSTALLED A REPAIR DOUBLER IAW EA5710-01041. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20050411002172005041100217NM 2005 4 11 SB05043 120050331A335020121 POWER SUPPLY BOEING737 7374B7 1384702NM EMERGENCY LIGHT FAILED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US 24781 BDL - MAINTENANCE REPORTED ALL THE EMERGENCY LIGHTS CONTROLLED BY POWER SUPPLY M1479 WERE EXTREMELY DIM. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY M1479. OPERATIONAL CHECK OF LIGHTS GOOD. 2L72 4F RTA16WE 20050412000662005041200066SO 2005 4 12 SIMA200508705 120050322A532014521721009 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SO27707EB 145195 ABI - THE GALLEY FORWARD DIGITAL WAS FOUND CORRODED. REMOVED EXISTING DIGITAL AND INSTALLED SERVICEABLE DIGITAL IAW EMB 145 SRM, SRM EMB-145/1142 REV 28 CHAPTER 51-40-02. (M) 2L72 4F RTT00011AT 20050412000702005041200070NM 2005 4 12 QXEA200500530 120050330A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09367PH 511 PDX - LEFTHAND OUTBOARD SEAT TRACK HAS CORROSION PIT AT FUSELAGE STATION 436, INSIDE CHANNEL. REPAIRED IAW DHC-8-200 SRM 51-40-00 AND SRM 51-40-11. 2H72 4T RTA13NM 20050412000722005041200072EA 2005 4 12 QXEA200500511 120050317A5210 PLATE CNDAIRCL600 CL6002C10 1390015EA ZONE 800 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09613QX 10045 PDX - MAIN CABIN DOOR FORWARD SACRIFICAL PLATE DENTED. REPAIRED IAW CRJ 700 REO 670-53-22-001. 2L72 4F RTA21EA 20050412000742005041200074EA 2005 4 12 QXEA200500509 120050317A5320 WEB CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09613QX 10045 PDX - LEFTHAND WEB CORRODED IN AND AROUND FLOORBEAM FS 280.0, WL 72.50. REPAIRED IAW CRJ 700 SRM 51-42-06 AND REO 670-53-11-052. 2L72 4F RTA21EA 20050412000762005041200076 2005 4 12 AWXA200500422 420050322A2565D31041147 SLIDE BOEING757 757225 1384959NM R-3 DOOR WILL NOT TEST A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28914AW404413309 22208 DURING SCHEDULED DEPLOYMENT OF THE R-3 DOOR SLIDE, THE SLIDE EXCEEDED INFLATION TIME FAILING THE TEST, SLIDE TOOK 13 SECONDS TO BECOME FULLY INFLATED. MAINTENANCE REMOVED AND REPLACED THE R-3 DOOR SLIDE ASSEMBLY. FOUND NO OBVIOUS REASON WHY SLIDE EXCEEDED DEPLOYMENT TIME. TWO SMALL HOLES WERE FOUND AND PATCHED, SLIDE WAS OVERHAULED AND A HYDRO TEST WAS ACCOMPLISHED ON HOSE AND CYLINDER, NO DEFECTS NOTED. PERFORMED OPS TEST OF SLIDE ON FLAT STAND, TEST WAS GOOD PER CMM 25-66-03, REV. 4. 2L72 4F RTA2NM 20050412000782005041200078NM 2005 4 12 AWXA200500420 120050311A53226546812171 FLOOR SUPPORT BOEING737 737375 13844BNNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 DURING C-05 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF FLOOR SUPPORT BETWEEN BS 1009 AND BS 1012, AT RBL 38. MAINTENANCE CUTOUT DAMAGE IN FLOOR SUPPORT AT RBL 38 FROM BS 1009 AND BS 1012; FABRICATED -1 AND -2 REPAIR PLATES; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-12, FIG. 1. 2L72 4F RTA16WE 20050412000802005041200080NM 2005 4 12 AWXA200500418 120050318A53136546579552 STRINGER BOEING737 737375 13844BNNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 DURING C-05 CHECK CORROSION WAS FOUND ON RT TORQUE BOX STRINGER BETWEEN BS 1105 AND 1117, STR 16 RT. MAINTENANCE REMOVED CORRODED RT TORQUE BOX STRINGER FROM BS 1105 TO 1117, STR 16 RT; INSTALLED NEW REPLACEMENT STRINGER IAW B737-300 SRM 51-40-02, FIG 3 AND 8. 2L72 4F RTA16WE 20050412000822005041200082NM 2005 4 12 AWXA200500416 120050318A53136546574595 STRINGER BOEING737 737375 13844BNNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 DURING C-05 CHECK CORROSION WAS FOUND ON RT TORQUE BOX STRINGER BETWEEN BS 1105 AND BS 1117, STR 13 RT. MAINTENANCE REMOVED CORRODED RT TORQUE BOX STRINGER FROM BS 1105 TO BS 1117, STR 13 RT; INSTALLED NEW REPLACEMENT STRINGER IAW B737-300 SRM 51-40-02, FIG 3 AND 8. 2L72 4F RTA16WE 20050412000842005041200084NM 2005 4 12 AWXA200500414 120050311A53206546812171 CHANNEL BOEING737 737375 13844BNNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 DURING C-05 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF WEB SUPPORT CHANNEL BETWEEN BS 995 AND BS 1001, RBL 41, WL 207. MAINTENANCE CUTOUT DAMAGE ON LOWER SURFACE OF WEB SUPPORT CHANNEL FROM BS 995 TO BS 1001, AT RBL 41; FABRICATED A FILLER AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-12. 2L72 4F RTA16WE 20050412001142005041200114NM 2005 4 12 DHL2005782549 120050316A5311 FRAME BOEING727 727227 1384078NM FUSELAGE BENT A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 FRAME BETWEEN STR 25-26 R AT STA 1050 BENT. CUT OUT DAMAGE AREA SIZE 1 1/2 INCH BY 1 INCH IAW B727 SRM 53-10-1. FABRICATED FRAME REPAIR USING 7075-T6 .071 PO NR 9002012 DIM 8 INCH BY 4 INCH IAW B727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1. ALODINE AND PRIMED PART AND AREA IAW B727 SRM 51-10-2. INSTALLED FRAME REPAIR IAW B727 SRM 53-10-2 FIG 5 AND 51-40-3. 2L73 4F A3WE 20050412001152005041200115NM 2005 4 12 DHL2005782548 120050316A5530 BRACKET BOEING727 727227 1384078NM VERTICAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 VERT STAB FRAME CLIP CRACKED FIN STA 157.2 BETWEEN STR 8L AND 9L. REMOVED DAMAGED CLIP AT FIN STA 157.2 BETWEEN STR 8-9L IAW 727 SRM 51-30-2. FABBED NEW FROM 7075 T6 .050 PO NR 90014147 DIM 6 5/8" BY 3" IAW 727 SRM 55-30-2 FUG 2 NEW CLIP TREATED PRIMED AND INSTALLED IAW 727 SRM 51-10-2 AND 51-30-2. 2L73 4F A3WE 20050412001162005041200116NM 2005 4 12 DHL2005782547 120050316A5531 STRINGER BOEING727 727227 1384078NM VERTICAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 VERT STAB STR 6L CRACKED AT FIN STA 180.6. REMOVED FASTENERS CUT OUT DAMAGED AREA FABBED NEW STIFFENER FROM BAC 1517-1367 PO NR 501953 DIM 5 1/8" BY 3 INCH SPLICE FROM AND 10133-1401 PO NR 501952 DIM 21 3/8" BY 2" SPLICE FROM AND 10134-1201 PO NR 501952 DIM 21 3/8" BY 2" FILLER FROM 7075 T6 .080 PO NR 9002012 DIM 21 3/8" BY 1" FILLER FROM 7075 T6 .100 PO NR 9911580 DIM 21 3/8" BY 3/4" AND CLIP FROM AND 10133-1401 PO NR 501952 DIM 2" BY 2" IAW 727 SRM 55-30-11 FIG 1. REPAIR PARTS TREATED PRIMED AND INSTALLED IAW 727 SRM 51-10-2 AND 55-30-4 FIG 1. 2L73 4F A3WE 20050412001182005041200118NM 2005 4 12 DHL2005782545 120050315A5754 SKIN BOEING727 727227 1384078NM NR 6 SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 NR 6 SLAT IB TRACK SEAL CUTOUT CRACKED WS474 R/W L/E. REMOVED NR 6 SLAT ASSY TO FROM IAW B727 W/W 27-81-41. REMOVED FASTENERS AT NR 6 SLAT I/B TRACK SEAL WS 474 R/W L/E FOR ACCESS IAW B727 SRM 51-30-2. STOP DRILL CRACK IAW B727 SRM 51-10-1. HFEC INSP PER NDT 727 PT 6 51-00-00 FIG 23. CRACK ENDS IN STOP HOLE FABRICATED DOUBLER FROM MAT USED 2024T3 .063 PO NR 9001930 DIMS 7 1/4 BY 6" IAW B727 SRM 57-30-4 FIG 11. ALODINED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED DOUBLER REPAIR IAW B727 SRM 57-30-4 FIG 11. 2L73 4F A3WE 20050412001192005041200119NM 2005 4 12 DHL2005782544 120050315A5530 WEB BOEING727 727227 1384078NM VERTICAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 CRACKS IN WEBBING OF RIB LOCATED INSIDE THE BOTTOM END OF THE VERTICAL FIN BS 1303 (MARKED IN RED). JFEC INSPECTED WEB CRACK TERMINATED AT 1ST FASTENER HOLE IAW B727 NDT MAN PT 6 51-00-00 IIS 23, FABRICATED NEW DOUBLER REPAIR MATERIAL USED 7050 T6 .050 PO NR 9001417 DIM 5 1/2" BY 3 3/8" IAW B727 SRM 55-30-2/IS 2 AND 51-40-2. TREATED AND PRIMED WEB REPAIR IAW B727 SRM 51-10-2. INSTALLED DOUBLER REPAIR IAW B272 SRM 51-40-2. 2L73 4F A3WE 20050412001212005041200121NM 2005 4 12 DHL2005782542 120050314A5531 STRINGER BOEING727 727227 1384078NM VERTICAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 STRINGER 9R CRACKED AT FIN STA 157.2 INSIDE VERTICAL FIN. REMOVED FASTENERS CUT OUT DAMAGED AREA FABBED NEW STIFFENER FROM BAC 1517-1387 PO NR 501953 DIM 4 3/8 INCH BY 3 INCH SPLICE FROM AND 10133-1401 PO NR 501952 DIM 17 3/8" BY 2" SPLICE FROM AND 10134-1201 PO NR 501952 DIM 17 3/8" BY 2" FILLER FROM 7075 T8 .080 PO #9002012 DIM 17 3/8" BY 1" FILLER FROM 7075 T8 .100 PO #9911586 DIM 17 3/8" BY 3/4" AND CLIP FROM AND 10133-1401 PO NR 501952 DIM 2" BY 2" IAW 727 SRM 55-30-4 FIG 1 REPAIR PARTS TREATED, PRIMED AND INSTALLED IAW 727 SRM 51-10-2 AND 55-30-4 FIG 1. 2L73 4F A3WE 20050412001232005041200123NM 2005 4 12 DHL2005782540 120050314A5754 SKIN BOEING727 727227 1384078NM NR 7 SLAT DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 4 DENTS ON NR 7 SLAT EXTERNAL SKIN (MARKED). MEASURED 4 DENTS ON NR 7 SLAT IAW B727 SRM 53-30-1 FIG 1 AND FOUND 3 MOST INBOARD DENTS WITHIN LIMITS, A.4/Y.013=30.7, A.2/Y.003=66.6, A.2/Y.002=100 AND OUTBOARD DENT OUT OF LIMITS A.4/Y.O41=9.7. CUT OUT DAMAGED AREA SIZE 1 3/4" BY 1 1/4" IAW B727 SRM 57-50-3. FABRICATED DOUBLER MATERIAL USED 2024 T3 -.080 PO NR 9002012 SIZE 5 1/4 BY 4 1/4" IAW SRM 57-50-3 FIG 1. ALODINED AND PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED DOUBLER IAW B727 SRM 57-50-3 FIG 1. 2L73 4F A3WE 20050412001242005041200124WP 2005 4 12 DHL2005782538 120050313A5311 FRAME DHAVXXDH82 DH82AROBRTSN2801002WP FUSELAGE BENT A DHLAK NONE O OTHER ININSP/MAINT 1 SO015300 T5703 AFT CARGO BENT FRAME STA 1070 RIGHT AROUND STR 27R. REMOVED DAMAGED AREA, FABRICATED DOUBLER REPAIR FROM 7075-T6,0. .063 PO NR 9001660 DIMENSIONS 3 1/4' X 8 1/2', FILLER REPAIR FROM 7075-T6 0.063 PO #9001660 DIMENSIONS 1 3/8' BY 1 3/4' AND SHIM FROM 7075-T6 0.090 PO NR 9001777 DIMENSIONS 11/16' BY 8 1/2' IAW B727 SRM 51-40-3 FIG 1 AND 53-10-2 FIG 5. TREATED AND PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED PARTS IAW B727 SRM 51-40-3 FIG 1. 1Q71 3I A8EU 20050412001262005041200126WP 2005 4 12 05FDEA00826 120050404A5330 SKIN DOUG DC10 DC1010 3022110WP FUSELAGE DAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25571FE 47830 DURING INSPECTION FOUND 3 EXISTING REPAIRS AT STA 835- STA 855 REF LOG 48-44 LT SIDE. REMOVED EXISTING REPAIR PER SRM 53-20-00 FIG 6 SHT 5, PERFORMED NEW REPAIR PER SRM 53-20-00 FIG 6 SHEET 5. (OPEN) 2L73 4F A22WE 20050412001272005041200127NM 2005 4 12 05FDEA00825 120050404A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT UPPER AFT SKIN PLANK NR 27R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82942. 2L73 4F RTA22WE 20050412001292005041200129NM 2005 4 12 05FDEA00823 120050404A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT UPPER CENTER SKIN PLANK NR 17R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82953. 2L73 4F RTA22WE 20050412001312005041200131NM 2005 4 12 05FDEA00821 120050404A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT UPPER FORWARD SKIN PLANK NR 13R BARREL NUT BORE FOUND EXCEEDED LIMITS. REWORK/REPAIR - 1-5510-7-5000 HAS BEEN COMPLIED WITH. 2L73 4F RTA22WE 20050412001332005041200133NM 2005 4 12 05FDEA00817 120050404A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT HAND UPPER CENTER SKIN PLANK NR 24L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82940. 2L73 4F RTA22WE 20050412001352005041200135NM 2005 4 12 05FDEA00815 120050404A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT UPPER CENTER SKIN PLANK NR 20L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82940. 2L73 4F RTA22WE 20050412001372005041200137NM 2005 4 12 05FDEA00813 120050404A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT HAND UPPER CENTER SKIN PLANK NR 26L BARREL NUT BORE FOUND EXCEEDED LIMITS. REMOVED AND REPLACED IAW SRM 51-33-01, VOL II. 2L73 4F RTA22WE 20050412001392005041200139NM 2005 4 12 05FDEA00811 120050404A3230 TRUNNION DOUG MD11 MD11 3023602NM ZONE 700 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25583FE 48421 CENTER LANDING GEAR, RT TRUNNION SUPPORT FITTING MATING SURFACE FOUND CORRODED AND EXCEED LIMIT AREA OF 10 PERCENT PER SRM 53-40-00 FIGURE 15, SHEET 4. (FOR LOCAL BLEND OPTIONS) AEA7051-502. REPAIR CARRIED OUT IAW FEDEX EA 1-5340-82950. 2L73 4F RTA22WE 20050412001412005041200141NM 2005 4 12 05FDEA00806 120050404A5713 STRINGER DOUG MD11 MD11 3023602NM LT WING CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25583FE 48421 LEFT WING STRINGER 13 END SUSPECTED CRACKED. REPAIR CARRIED OUT IAW SRM 57-20-00 VOLUME I, FIGURE 10. 2L73 4F RTA22WE 20050412001432005041200143NM 2005 4 12 05FDEA00804 120050404A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RT WING STRINGER 9 END SUSPECTED CRACKED ARB7509-2. REPAIR CARRIED OUT IAW SRM 57-20-00 VOLUME I, FIGURE 10 AND FEDEX EA 1-5710-83090. 2L73 4F RTA22WE 20050412001452005041200145NM 2005 4 12 05FDEA00802 120050404A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RIGHT WING STRINGER 11 END SUSPECTED CRACKED ARB7511-2. REPAIR CARRIED OUT IAW SRM 57-20-00 VOLUME I, FIGURE 10 AND FEDEX EA 1-5710-83090. 2L73 4F RTA22WE 20050412001472005041200147NM 2005 4 12 05FDEA00800 120050403A5310 BEAM DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 AFT FUSELAGE COMPT STA 2007 RT BEAM APPROX X=20 FOUND VERTICAL L-ANGLE BRACKET SUSPECT CRACK AT THE TOP MOST EDGE AS MARKED. REPAIRED AS PER FEDEX EA 1-5310-83088. 2L73 4F RTA22WE 20050412001492005041200149EU 2005 4 12 05FDEA00797 120050402A5410A5461256100000 DOOR AIRBUS310 A310 EU ZONE 400 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 NR 1 PYLON PANEL 416AR HAS AREA AROUND SCOOP AND EXTENDING UNDER SCOOP WITH CORROSION. REMOVED AND REPLACED DOOR ASSY PER A310-200 AMM 54-50-00-4, DUE TO CORROSION OUT OF LIMITS PER A310-200 SRM 54-50-00 TABLE 102, SHEET 2. 2L72 4F RTA35EU 20050412001502005041200150NM 2005 4 12 05FDEA00796 120050401A5511 SPAR CAP DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZ STAB RT UPPER AFT SPAR CAP NR 36R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82959. 2L73 4F RTA22WE 20050412001512005041200151NM 2005 4 12 05FDEA00795 120050401A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZ STAB RT UPPER AFT SKIN PLANK NR 32R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82942. 2L73 4F RTA22WE 20050412001522005041200152NM 2005 4 12 05FDEA00794 120050401A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZ STAB RT UPPER AFT SKIN PLANK NR 30R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82942. 2L73 4F RTA22WE 20050412001532005041200153NM 2005 4 12 05FDEA00793 120050401A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZ STAB RT UPPER CENTER SKIN PLANK NR 28R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82942. 2L73 4F RTA22WE 20050412001552005041200155NM 2005 4 12 05FDEA00791 120050401A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZ STAB RT UPPER CENTER SKIN PLANK NR 22R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82953. 2L73 4F RTA22WE 20050412001572005041200157NM 2005 4 12 05FDEA00789 120050401A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZ STAB RT UPPER CENTER SKIN PLANK NR 18R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82953. 2L73 4F RTA22WE 20050412001592005041200159NM 2005 4 12 05FDEA00786 120050401A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZ STAB LT UPPER AFT SKIN PLANK NR 33L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82941. 2L73 4F RTA22WE 20050412001612005041200161NM 2005 4 12 05FDEA00784 120050401A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZ STAB LT UPPER AFT SKIN PLANK NR 29L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82941. 2L73 4F RTA22WE 20050412001622005041200162NM 2005 4 12 05FDEA00783 120050401A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZ STAB LT UPPER AFT SKIN PLANK NR 27L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82941. 2L73 4F RTA22WE 20050412001632005041200163NM 2005 4 12 05FDEA00782 120050401A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZ STAB LT UPPER CENTER SKIN PLANK NR 25L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82940. 2L73 4F RTA22WE 20050412001642005041200164NM 2005 4 12 05FDEA00781 120050401A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZ STAB LT UPPER CENTER SKIN PLANK NR 23L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82940. 2L73 4F RTA22WE 20050412001652005041200165NM 2005 4 12 05FDEA00780 120050401A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZ STAB LT UPPER CENTER SKIN PLANK NR 21L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82940. 2L73 4F RTA22WE 20050412001662005041200166NM 2005 4 12 BB05025 120050330A3397 WIRE BOEING767 767201 1385125NM EMERGENCY LIGHT LOOSE A USAAK NONE O OTHER ININSP/MAINT 1 EA19649US 23901 PIT - FOUND FIRST FOUR FLOOR EMERGENCY LIGHTS ON THE RIGHT SIDE INOPERATIVE. MAINTENANCE SECURED A LOOSE CONNECTION ON THE FOURTH EMERGENCY LIGHT. 2L72 4F RTA1NM 20050412001672005041200167NM 2005 4 12 DHL2005782536 120050312A5753 SKIN BOEING727 727227 1384078NM TE FLAP CHAFED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 RT IB FOREFLAP LOWER OB END CHAFFED THROUGH REPAIR PATCH. REMOVED FASTENERS AND PREVIOUS REPAIR FOR ACCESS IAW 727 SRM 51-30-2. HFEC INSPECTED AREA WITH NO CRACKS NOTED IAW B727 NDT MAN. PT. 6 51-00-00 FIG 23. FABRICATED REPAIR DOUBLER FROM 2024T3 .071 PO NR 9001978 (6' BY 6')(1' BY 4') FILLER IAW 727 SRM 57-50-2 FIG 3, 57-50-4 FIG 1. REPAIR DOUBLER AND BARE METAL TREATED AND PRIMED IAW 727 SRM 51-10-2. REMOVED RT INBD FOREFLAP FOR S/M ACCESS IAW 727 MM 27-51-03. INSTALLED DOUBLER IAW 727 SRM 57-50-4 FIG 1 2L73 4F A3WE 20050412001682005041200168NM 2005 4 12 DHL2005782535 120050313A5410 SKIN BOEING727 727227 1384078NM NOSE COWL DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 NR 3 ENG NOSE COWL, EXTERIOR SKIN AT 3 O'CLOCK AFT SKIN SURFACE EDGE IS DENTED, ERODED AND SEPARATING. DAMAGE ON NR 3 ENG NOSE COWL EXTERIOR SKIN 3 O'CLOCK AFT SKIN FOUND TO BE OUT OF LIMITS IAW 727 SRM 54-30-1 FIG 1. CUT OUT DAMAGED AREA, FABBED FILLER FROM 2024 T3 .040 PO NR 9001938 DIM 9' BY 1' AND DOUBLER FROM 2024T3 .050 PO#9002093 DIM 17' BY 3' IAW 727 SRM 51-40-2, 54-30-2 FIG 1 AND 54-30-3 FIG 3A. REPAIR PARTS TREATED, PRIMED AND INSTALLED IAW 727 SRM 51-10-2 AND 51-40-2 FIG 1. 2L73 4F A3WE 20050412001692005041200169NM 2005 4 12 DHL2005782534 120050308A5260 SKIN BOEING727 727227 1384078NM AIRSTAIR DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 AFT AIRSTAIR EXTERIOR SKIN AT STA 1303 IS DENTED. REMOVED FASTENER DOOR S/M. REPAIR AT AFT AIRSTAIR EXT SKIN IAW B727 SRM 51-10-2 FIG 4. FABRICATED FILLER SKIN MAT USED 2024T3 040 PO NR 9002012 DIMENSION 61 1/2' BY 42' AND 1 EA STRAP MAT USED 2024T3 0.40 PO NR 9002012 DIMENSION 42' X 4' IAW B727 SRM 52-10-2 FIG 4. ALODINE AND PRIME IAW B727 SRM 51-10-2. INSTALLED DOUBLER IAW B727 SRM 52-10-2 FIG NR .4 2L73 4F A3WE 20050412001702005041200170NM 2005 4 12 DHL2005782517 120050310A5330 SKIN BOEING727 727227 1384078NM FUSELAGE BULGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 BULGE L/SIDE FUSELAGE SKIN AFT OF STA 580 BELOW STA 24L. DAMAGED FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-30-1 FIG 1. CUTOUT DAMAGE AREA FABBED FILLER FROM 2024T3 .050 PO NR 9001684 DIM 7 1/2 INCH BY 6 1/2 INCH IAW B727 SRM 53-30-2 FIG2 53-30-3 FIG 2. TREATED AND PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B727 53-30-3 FIG 2. 2L73 4F A3WE 20050412001712005041200171EU 2005 4 12 SA05037 120050403A3350321431 BATTERY AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT INSTALLED A USAAK NONE O OTHER ININSP/MAINT 1 EA19763US 1360 DCA - FOUND AN EPSU BATTERY (13WLA) WHICH NEEDED TO BE REPLACED. MAINTENANCE REPLACED THE EPSU BATTERY. 2L72 4F RTA28NM 20050412001732005041200173NM 2005 4 12 DHL2005782533 120050313A5410 NOSE COWL BOEING727 727227 1384078NM NR 3 ENGINE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 NR 3 ENGINE NOSE COWL, EXTERIOR SKIN AT 9 O'CLOCK FWD OF LOWER LATCH HANDLE, SKIN IS DENTED. DAMAGE ON NR 3 ENGINE NOSE COWL EXTERIOR SKIN AT 9 O'CLOCK FWD OF LOWER LATCH HANDLE OUT OF LIMITS IAW 727 SRM 54-30-1 FIG 1. CUTOUT DAMAGED AREA DIM 1 INCH BY 3/4 INCH AND FABBED REPAIR DOUBLER FROM 2024T3 .050 PO NR 9001873 DIM. 10 1/2 INCH BY 5 7/8 INCH IAW 727 SRM 54-30-2 FIG 1 AND 54-30-3 FIG 8. DOUBLER TREATED AND PRIMED IAW 727 SRM 51-10-2 AND INSTALLED IAW 727 SRM 54-30-3 FIG 8. 2L73 4F A3WE 20050412001742005041200174NM 2005 4 12 DHL2005782531 120050312A5753 SKIN BOEING727 727227 1384078NM FLAP DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 RT IB T/E FLAP IS DELAMINATED ON THE UPPER SURFACE OF THE AFT FLAP INBOARD EDGE CORRECTIVE ACTION: CUT OUT DELAM AREAS 3 APPROX 3 INCH DIAM, 2 INCH DIAM AND 2 INCH BY 4 1/4 AND CUT OUT PUNCTURED SKIN APPROX 2 INCH IAW B727 SRM 51-40-20 FIG 30. FABBED 2 FILLERS APPROX 2 INCH DIAM, 3 INCH DIAM AND 2 INCH BY 4 1/2 DOUBLER APPROX 7 1/2 INCH BY 5 INCH AND DOUBLER APPROX 10 1/2" BY 7 1/2' USING 2024T3 .016 PO#9001660 IAW B727 SRM 57-50-2 FIG 3. CLEANED, PREPARED ALL SURFACES APPLIED ADHESIVE PRIMER AND ADHESIVE TO ALL REPAIR SURFACES INST PAETS AND BAGGED FOR BONDING IAW B727 SRM 57-40-20 FIG30. CURED REPAIRS SANDED CLEANED AND PERFORMED POST BOND INSP WITH NO DELAM NOTED IAW B727 SRM 51-40-20 PARA0. TREATED PRIM2L73 4F A3WE 20050412001752005041200175NM 2005 4 12 DHL2005782532 120050311A5753 SKIN BOEING727 727227 1384078NM LT TE FLAP DEBONDED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 LT OB AFT FLAP IB UPPER SURFACE WBL 300 HAS DISBOND AT EDGE OF EXISTING REPAIR. FOUND 2 EACH DISBONDED AREA OF LOWER SKIN, ALSO REMOVED PREVIOUS REPAIR FROM LOWER SKIN AND CUTOUT DAMAGED AREA APPROX 48 SQ IN IAW B727 SRM 51-40-20 FIG 31. FABRICATED ON FILLER APPROX 48 SQ IN AND ONE DOUBLER APPROX 9 INCH BY 9 1/2 INCH USING 2024T3 .016 PO NR 9912184 IAW SRM 57-50-2 FIG.4. CLEANED, PREPPED, APPLIED ADHESIVE PRIME & ADHESIVE TO ALL REPAIR SURFACES INCLUDING UPPER SKIN, INSTALLED PARTS & BAGGED FOR BONDING IAW B727 SRM 51-40-20 FIG.31. CURED REPAIR, CLEANED,& PERFORMED POST BOND INSP. TO UPPER AND LOWER SURFACES WITH NO DELAM. NOTED IAW B727 SRM 51-40-20 PARA 0. TREATED, PRIMED, & SEALED REPAIR IAW B727 SRM 51-402L73 4F A3WE 20050412001762005041200176NM 2005 4 12 DHL2005782530 120050311A5730 SKIN BOEING727 727227 1384078NM RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 R/WING UPPER SURFACE CRACKED AT NR 12 SPOILER HINGE CUTOUT. STOP DRILLED CRACK SIZE .250 IAW B72 SRM 51-10-1. FABRICATED DOUBLER REPAIR USING 7075T6 .071 PO# 9002012 DIM. 6" BY 3 3/4" IAW B727 SRM 57-30-4 FIG 10. ALODINE AND PRIMED PART AND AREA IAW B727 51-10-2. INSTALLED DOUBLER IAW B727 SRM 57-30-4 FIG 10 AND 51-30-2. 2L73 4F A3WE 20050412001782005041200178NM 2005 4 12 DHL2005782526 120050311A5753 SKIN BOEING727 727227 1384078NM LT TE FLAP GOUGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 LT OB FORE FLAP L/E IB AT WBL 314 HAS GOUGES IN REPAIR DOUBLER SURFACE. REMOVED DOUBLER IAW B727 SRM 51-30-2. FABRICATED NEW DOUBLER USING 2024T3 .063 PO# 9001978 DIM. 7 1/2" BY 3 1/2" IAW B727 SRM 57-50-2 FIG 3 AND 57-30-4 FIG 1. ALODINE AND PRIMED PART AND DOUBLER IAW B727 SRM 51-10-2. INSTALLED DOUBLER IAW B727 57-50-2 FIG 3 AND 57-50-4 FIG 1. 2L73 4F A3WE 20050412001802005041200180NM 2005 4 12 DHL2005782528 120050311A5522 SKIN BOEING727 727227 1384078NM ELEVATOR SCRATCHED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 LT ELEV INBD BOTTOM SIDE HAS ALONG SCRATCH MARK. BURNISHED AREA ON LT ELEV I/B LOWER SKIN AND FOUND AREA CRACKED AND OUT OF LIMITS IAW 727 SRM 55-20-1 FIG 1. CUT OUT DAMAGED AREA DIM 5/8" AND 1/2" AND FABBED DOUBLER FROM 2024T3 .032 PO NR 9002034 DIM 2 1/2" BY 2 1/4" IAW 727 SRM 55-20-3 FIG 1. DOUBLER TREATED PRIMED AND INSTALLED IAW 727 SRM 51-10-2 AND 55-20-3 FIG 1. CALCULATED ELEVATORS NEW MOMENT OF 118.705 ITS WITHIN THE LIMITS 120+-20 POUND-INCHES. NO FURTHER ACTION REQUIRED IAW 727 SRM 51-80-7. 2L73 4F A3WE 20050412001822005041200182NM 2005 4 12 DHL2005782525 120050311A5522 SKIN BOEING727 727227 1384078NM LT ELEVATOR DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 LT ELEV IB BOTTOM AFT HAS 2 DENTS. EVALUATED 2 DENTS 1ST A/Y=1/.02=50 AND WITHIN LIMITS, 2ND IS OUT OF LIMITS IAW 727 SRM 55-20-1 FIG 1. CUT OUT DAMAGED AREA DIM 5/8" BY 1/2"AND FABBED DOUBLER FROM 2024T3 .032 PO NR 9002034 DIM 2 1/2" BY 2 1/4" IAW 727 SRM 55-20-3 FIG 1. DOUBLER TREATED, PRIMED, AND INSTALLED IAW 727 SRM 51-10-2 AND 55-20-3 FIG 1. CALCULATED ELEVATOR NEW MOMENT OF 118.2075 IS WITHIN THE LIMITS 120 +- 20 POUNDS-INCHES, NO FURTHER ACTION REQUIRED IAW 727 SRM 51-80-7. 2L73 4F A3WE 20050412001842005041200184NM 2005 4 12 DHL2005782522 120050310A5712 RIB BOEING727 727227 1384078NM RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 RIB CRACKED ON FWD BOTTOM EDGE, RT WING LE WS 130. REMOVED NR 4 K-FLAP FOR ACCESS IAW B727 MM 27-81-01. STOP DRILLED CRACK IAW 727 SRM 51-10-1 AND FABBED REPAIR ANGLE FROM 7075T6 .063 PO NR 900861 DIM. 6" BY 1 3/4" IAW 727 SRM 57-20-2 FIG 1 AND 51-40-3 FIG 1. REPAIR ANGLE TREATED, PRIMED, AND INSTALLED IAW 727 SRM 51-10-2 AND 51-40-3 FIG 1. 2L73 4F A3WE 20050412001862005041200186SW 2005 4 12 ALGA099111 120050122A6710406310405101 PITCH LINK BELL 407 407 1182206SW MAIN ROTOR WORN B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03587AL325 53248 AXIAL PLAY BEYOND MAX AND RATCHETY. REPLACED WITH NEW BY FIELD MAINTENANCE. 1G71 3U O H2SW 20050412001882005041200188EU 2005 4 12 ALGA099103 120050125A6220 BUSHING UROCOPEC120 EC120B 8680987EU MAIN ROTOR MIGRATED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03512AL2428 1148 AT 500HR INSP FOUND BUSHING SLID OUT OF PLACE. POSSIBLE MANUFACTURER DEFECT. REPLACED WITH NEW OR SERVICEABLE PART BY O/H SHOP. 1G72 3U NCR0001RD 20050412001892005041200189EU 2005 4 12 ALGA099525 120050213A6410C642A0300103 BLADE UROCOPEC120 EC120B 8680987EU TAIL ROTOR CHIPPED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03516AL492 1157 CHROME MONOXIDE SURFACE CHIPPED BEYOND LIMITS. SEND TO AMERICAN EUROCOPTER FOR WARRANTY CONSIDERATION. 1G72 3U NCR0001RD 20050412001902005041200190SW 2005 4 12 ALGA099876 120050222A6710406310405101 PITCH LINK BELL 407 407 1182206SW MAIN ROTOR WORN B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03XAADL624 53447 RATCHEY, BINDING, AXIAL PLAY BEYOND MAX / REPLACED WITH NEW BY FIELD MAINTENANCE 1G71 3U O H2SW 20050412001922005041200192SW 2005 4 12 ALGA100000 120050321A6710406310405101 PITCH LINK BELL 407 407 1182206SW MAIN ROTOR WORN B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03687AL197 53366 BINDING; AXIAL PLAY BEYOND LIMITS; ROUGH / REPLACED WITH NEW PART BY FIELD MAINT. 1G71 3U O H2SW 20050412001932005041200193SW 2005 4 12 ALGA100083 120050205A6220 BEARING BELL 412 412 1182202SW M/R SPINDLE DEBONDED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW035NBGS4199 A1003 33186 ELASTOMERIC BEARING COMPLETELY UNBONDED FROM SPINDLE / REPLACED WITH NEW/SERVICEABLE PART BY FIELD MAINTENANCE. 1G72 4U H4SW 20050412001942005041200194EA 2005 4 12 COMA0560068 120050119A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS UNRELIABLE A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01442CA10226 7483 FLIGHT 5262 - FLAPS FAIL CAUTION MESSAGE. REPLACED THE LT BPSU. 2L72 4F RTA21EA 20050412001952005041200195EA 2005 4 12 COMA0560069 120050119A2750860D10018ABCD CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01966CA8559 7132 FLIGHT 5330 - FLAPS FAILED AT "O". REPLACED THE FECU. 2L72 4F RTA21EA 20050412001962005041200196EA 2005 4 12 COMA0560070 120050120A3080601970977 VALVE CNDAIRCL600 CL6002B19 1900309EA LT ENGINE FAULTY A COMAO OTHER J WARNING INDICATION CLCLIMB 1 SO01797CA1150 7344 FLIGHT 4983, DURING CLIMB-OUT OF ATL, RECEIVED A LEFT COWL ANTI-ICE CAUTION, FLIGHT DIVERTED BACK TO ATL. REPLACED THE ANTI-ICE VALVE. 2L72 4F RTA21EA 20050412001972005041200197EA 2005 4 12 COMA0560072 120050122A2910 HYDRAULIC SYSTEM CNDAIRCL600 CL6002B19 1900309EA NR 3 LOW A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01528CA 7841 FLIGHT 5045 - DURING APPROACH TO BOS, RECEIVED A GEAR DISAGREE FOLLOWED BY A HYDRAULIC NR 3 LOW PRESSURE CAUTION, CREW DECLARED AN EMERGENCY, FOLLOWED QRH AND LANDED WITHOUT INCIDENT. SERVICED THE NR 3 HYDRAULIC SYSTEM. 2L72 4F RTA21EA 20050412001982005041200198EA 2005 4 12 COMA0570022 120050224A3250523505 ACTUATOR CNDAIRCL600 CL6002C10 1390015EA NLG STEERING FAULTY A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01379CA5139 10102 FLIGHT 5307 - AFTER TAKEOFF FROM JAX RECEIVED A STEERING INOP CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND DIVERTED TO BWI. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE STEERING ACTUATOR. 2L72 4F RTA21EA 20050412001992005041200199NE 2005 4 12 COMA0560141 220050226A7200CF343A1 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE RIGHT MALFUNCTIONED A COMAD RETURN TO BLOCK MJ OVER TEMP WARNING INDICATION TXTAXI/GRND HDL 1 SO01807CA919 7364 807593 FLIGHT 5121 DURING TAXI OUT WITH BOTH ENGINES OPERATING CREW RECEIVED AN EICAS "COMP MON" MESSAGE LOOSING ALL NR 2 ENGINE INDICATIONS. WHEN INDICATIONS RETURNED 15 SECONDS LATER, ENGINE NR 2 ITT INDICATED 990C WITH ABNORMAL N1 AND N2 INDICATIONS. THE CREW NOTED A SMOKE SMELL, ENGINE WAS SHUT DOWN AND DECLARED AN EMERGENCY, AIRCRAFT RETUREND TO THE GATE. REPLACED THE RIGHT ENGINE ASSEMBLY. 2L72 4F4 FRTA21EA E15NE 20050412002002005041200200EA 2005 4 12 COMA0560142 120050226A2410 IDG CNDAIRCL600 CL6002B19 1900309EA FAILED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01963CA 7127 FLIGHT 5082 - DURING TAKEOFF ROLL AT 60 KNOTS RECEIVED AN IDG CAUTION MESSAGE, ABORTED TAKEOFF AND RETURNED TO THE GATE. DEFERRED FAILED IDG PER MEL 24-11-01-1. 2L72 4F RTA21EA 20050412002012005041200201EA 2005 4 12 COMA0560144 120050225A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01966CA 7132 FLIGHT 5792 RECEIVED A FLAP FAIL CAUTION AFTER DEPARTING CVG, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. AIRCRAFT LANDED WITHOUT INCIDENT. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION, PARAGRAPH (B) 1,2,3, (A,B,C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2L72 4F RTA21EA 20050412002022005041200202EA 2005 4 12 COMA0560145 120050225A2750856D1007 PDU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAULTY A COMAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 SO01966CA10814 7132 FLIGHT 5792 - RECEIVED A FLAP FAIL CAUTION DURING YYZ APPROACH, CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED THE RIGHT POWER DRIVE UNIT. 2L72 4F RTA21EA 20050412002032005041200203EA 2005 4 12 COMA0560161 120050308A3231 LANDING GEAR CNDAIRCL600 CL6002B19 1900309EA NOSE MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01981CA 7163 FLIGHT 5807 - GEAR DISAGREE WARNING. COULD NOT DUPLICATE EXTENSION AND RETRACTION CHECKS SATISFACTORY. REPLACED THE NLG UPLOCK FOR TROUBLE SHOOTING. 2L72 4F RTA21EA 20050412002042005041200204EA 2005 4 12 COMA0560186 120050320A339764643 POWER CABLE CNDAIRCL600 CL6002B19 1900309EA EMERGENC LIGHT FAILED A COMAO OTHER O OTHER NRNOT REPORTED 1 SO01937CA 7044 FLIGHT 5377 - EMERGENCY FLOOR PATH LIGHTING IS INOP BETWEEN ROWS 2 TO 5. REPLACED POWER STRIP. 2L72 4F RTA21EA 20050412002052005041200205EA 2005 4 12 COMA0560187 120050320A5270 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA PAX DOOR ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01708CA 7235 FLIGHT 5311 - CABIN DOOR OUTER HANDLE MESSAGE. DEFERRED MAINTENANCE ON DOOR WARNING SYSTEM PER MEL. 2L72 4F RTA21EA 20050412002062005041200206EA 2005 4 12 COMA0560188 120050321A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01494CA 7765 LEFT HAND INTERCOSTALS AT FS 484.00 OUTBOARD CRACKED. REPAIRED IAW REO 601R-53-41-059. 2L72 4F RTA21EA 20050412002072005041200207EA 2005 4 12 COMA0560189 120050321A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01494CA 7765 LEFT HAND 621.00 FRAME CRACKED. REPAIRED IAW REO 601R-53-61-117. 2L72 4F RTA21EA 20050412002082005041200208EA 2005 4 12 COMA0560191 120050321A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSLEAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01494CA 7765 RIGHT HAND INTERCOSTALS AT FS 484.00 OUTBOARD CRACKED. REPAIRED IAW REO 601R-53-41-059. 2L72 4F RTA21EA 20050412002092005041200209EA 2005 4 12 COMA0560192 120050321A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01494CA 7765 RIGHT HAND 621.00 FRAME CRACKED. REPAIRED IAW REO 601R-53-61-117. 2L72 4F RTA21EA 20050412002102005041200210EA 2005 4 12 COMA0560194 120050321A5210 CABLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR DAMAGED A COMAK NONE O OTHER ININSP/MAINT 1 SO01494CA 7765 PAX DOOR ICE BREAK CABLE DAMAGED. REMOVED AND REPLACED PER CRJ MM 52-11-15. 2L72 4F RTA21EA 20050412002112005041200211EA 2005 4 12 COMA0570032 120050317A3234533407 SELECTOR VALVE CNDAIRCL600 CL6002C10 1390015EA MLG UNRELIABLE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01641CA5000 3409 10122 FLIGHT 5221 - GEAR DISAGREE WARNING. REPLACED THE LANDING GEAR SELECTOR VALVE. 2L72 4F RTA21EA 20050412002122005041200212EA 2005 4 12 COMA0560242 120050405A339764641 CABLE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT FAILED A COMAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO01805CA 7354 FLIGHT 5483 DURING TEST OF LIGHTING SYSTEM THE EMERGENCY FLOOR TRACK LIGHT FAILED TO ILLUMINATED AT ROW 1C. REPLACED FLOOR EMERGENCY TRACK CABLE AT 1C. 2L72 4F RTA21EA 20050412002132005041200213EA 2005 4 12 COMA0560243 120050404A339764643 CABLE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT FAILED A COMAD RETURN TO BLOCK L NO TEST TXTAXI/GRND HDL 1 SO01966CA 7132 FLIGHT 5318 DURING TEST OF LIGHTING SYSTEM THE EMERGENCY LIGHT FROM ROWS 2 THROUGH 5 FAILED TO ILLUMINATE. REPLACED CABLE ASSEMBLY AT ROWS 2 THROUGH 5. 2L72 4F RTA21EA 20050412002142005041200214EA 2005 4 12 COMA0560244 120050407A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA MAIN PAX OPEN A COMAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 SO01938CA 7046 FLIGHT 5198 DURING CLIMBOUT OF DTW THE CABIN FAILED TO PRESSURIZE ASSOCIATED WITH CABIN DOOR NOISE, CREW DECLARED EMERGENCY AND RETURNED TO THE FIELD LANDING WITHOUT INCIDENT. INSPECTED CABIN DOOR SEAL AND FRAME, CLOSED DOOR AND VERIFIED ALIGNMENT MARKS, PERFORMED PRESSURIZATION CHECK, DISCREPANCY COULD NOT BE DUPLCIATED BY MAINTENANCE. 2L72 4F RTA21EA 20050412002152005041200215EA 2005 4 12 COMA0560245 120050407A2750 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A COMAO OTHER J WARNING INDICATION CLCLIMB 1 SO01721CA 7259 FLIGHT 5315 DURING CLIMBOUT OF CVG WITH FLAPS RETRACTED THE STAB AND MACH TRIM MASTER CAUTION MESSAGES ACTIVATED, CREW FOLLOWED QRH PROCEDURES, RE-ENGAGED STAB/MACH TRIM AND LANDED AT SAV WITHOUT INCIDENT. CLEANED STAB/MACH TRIM ENGAGE PANEL SWITCHES AND RE-RACKED HSTCU. PERFORMED GROUND FUNCTIONAL CHECK WITH NO FURHTER DEFECTS NOTED. 2L72 4F RTA21EA 20050408001312005040800131NM 2005 4 8 SWAA051001 120050404A5313BAC1498 STRINGER BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON FUSELAGE STRINGER BETWEEN BS 967 TO BS 1016, STR 25L. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20050408001342005040800134NM 2005 4 8 SWAA051003 120050405A3397 WIRE BOEING737 7373H4 1384600NM EMERGENCY LIGHT DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED C1 CHECK, FOUND FWD EMERGENCY EXIT BULLNOSE LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY WIRE CONNECTORS PER MM. 2L72 4F RTA16WE 20050408001352005040800135NM 2005 4 8 SWAA051004 120050405A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29433LV 33716 DURING SCHEDULED HC2 CHECK, FOUND SEVERAL EEPLS COVERS CRACKED. REMOVED AND REPLACED EEPLS COVERS PER MM. 2L72 4F RTA16WE 20050408001382005040800138NM 2005 4 8 SWAA051007 120050405A53306545776 SKIN BOEING737 737301 1384611NM R2 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050408001402005040800140SO 2005 4 8 MASA200500254 120050325A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSBURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07828MJ 145218 ASH 2816 FROM CAE TO CLT HAD THE OVERWING EMERGENCY EXIT SIGN AT ROW 12F INOP. MAINTENANCE RELAMPED AND IT OPERATED NORMALLY. A/C DEPARTED WITHOUT FURTHER INCIDENT. 2L72 4T RTT00011AT 20050411000092005041100009CE 2005 4 11 DXTA200500646 120050328A3260 UPLOCK SWITCH CESSNA750 750 2076810CE NLG OUT OF ADJUST E DXTAO OTHER O OTHER CLCLIMB 1 GL07978QS 7500187 NOSE GEAR REPEATEDLY RAISING INTO WHEEL WELL AT 13,000, 17,000, 23,000 FT CAUSING A LOUD BANGING NOISE. DID NOT NOTICE UNLOCK LIGHT ILLUMINATING. SERVICED NOSE GEAR OLEO IAW CE 750 MM CHPT 12-10-38. ACCOMPLISHED NOSE GEAR UPLOCK SWITCH RIG CHECK, RIG CHECK GOOD IAW CE 750 MM 32-30-05, ACCOMPLISHED LT & RT MAIN GEAR UPLOCK SWITCH CHECK, CHECKS GOOD IAW CE 750 MM CHPT 32-30-05, ACCOMPLISHED NOSE GEAR ROLLER UPLOCK RIG CHECK, CHECKS GOOD IAW CE750 MM CHPT 32-30-05. ACCOMPLISHED GEAR SWING & COLD SOAK CHECK, CHECKS GOOD IAW CE750 MM CHPT 32-30-05. NO PROBLEMS NOTED. 2L72 4J RTT00007WI 20050411000192005041100019 2005 4 11 SWIA200514836 420050402A3418 CONTROL PANEL EMB 120 EMB120ER 3260203SO STALL WARNING INOPERATIVE A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07216SW 120285 STALL PANEL INOPERATIVE. REPLACED STALL PANEL. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050411000442005041100044EU 2005 4 11 0500413218 120050329A2910MS21902D8 FITTING AIRBUS320 A320211 3930320EU HYD SYSTEM BROKEN A NWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL01318US 206 AFTER TAKEOFF FROM MEM PRIOR TO FLAP RETRACTION, RECEIVED ECAM CAUTION HYD Y RSVR LO LVL. FOLLOWED COM PROCEDURES, RETURNED TO MEM, AND LANDED UNEVENTFULLY. ENGINE DRIVEN PUMP CAVITATED FOR ABOUT 30 SECONDS. FOUND UNION FITTING BROKEN OFF OF BRAKE DUAL DISTRIBUTION VALVE, REPLACED UNION FITTING AND O-RING. SERVICED YELLOW HYDRAULIC SYSTEM. PERFORMED HYDRAULIC SYSTEM CHECKS REQUIRED AFTER ENGINE DRIVEN PUMP CAVITATION. LEAK AND OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA28NM 20050411000602005041100060WP 2005 4 11 0500439943 120050402A2130 LINE DOUG DC9 DC931 3022065WP FLOW CONTROL LOOSE A NWAAB EMER. DESCENT O OTHER CRCRUISE 1 GL011308T 47315 DURING CRUISE AT FL350, THE RED CABIN PRESS ANNUNCIATOR LIGHT ILLUMINATED. CREW COMPLIED WITH COM AND PERFORMED AN EMERGENCY DESCENT AND DIVERTED TO A NORMAL SAFE LANDING AT DFW. MASKS DID NOT DEPLOY. MAINTENANCE BITE OF THE SYSTEM SHOWED NR 2 CONTROLLER FAULT CODE 5 AND FOUND A LOOSE SENSE LINE TO THE RIGHT FLOW CONTROL VALVE. LINE WAS SECURED AND PRESSURIZATION WAS CHECKED WITH AN ENGINE RUN-UP. ALL CHECKS WERE GOOD AND THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20050411000632005041100063 2005 4 11 P5CAO501333 420050328A2200 CONNECTOR BOEING747 747230B 1384889NM TAWS INDICATOR LOOSE A P5CAK NONE N FALSE WARNING ININSP/MAINT 1 EA15509MC 21221 TAWS SYSTEM GIVES ERRONEOUS INFORMATION CALL OUTS TERRAIN. FOUND P-3 CONNECTOR LOOSE AT TAWS INDICATOR. FOUND NO POWER AT PIN 63 ON NR 1 CADC RACK PLUG. RESTORED 26V PER WDM 34-12-12. ALL OPS & LEAK CHECK OK. 2L74 4F A20WE 20050411000642005041100064NM 2005 4 11 P5CA0501332 120050321A528065B11669 DOOR BOEING747 74746NF 13848BTNM MLG DELAMINATED A P5CAK NONE C F.O.D. ININSP/MAINT 1 EA15452PA 30810 RIGHT WING GEAR DOOR O/B HAS DELAMINATION ON AFT LWR EDGE. DOOR REMOVED AND REPAIR ACCOMPLISHED. REINSTALLED DOOR (SERVICEABLE) PER MM 32-12-07. 2L74 4F RTA20WE 20050411000652005041100065NM 2005 4 11 SWAA051014 120050406A3350207377 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29423WN 29827 DURING SCHEDULED MV2 CHECK, FOUND FWD END OF EEPLS LENS BROKEN. REMOVED AND REPLACED LENS PER MM. 2L72 4F RTA16WE 20050411000712005041100071NM 2005 4 11 SWAA051019 120050406A53306545777 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER AFT CUTOUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050411000762005041100076NM 2005 4 11 SWAA050974 120050330A3350101073 LENS BOEING737 7373H4 1384600NM R1 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EMERGENCY EXIT LOWER LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT ASSY. 2L72 4F RTA16WE 20050411000772005041100077NM 2005 4 11 SWAA050975 120050331A57536546430182 SKIN BOEING737 7373H4 1384600NM RT WING FLAP PEELING A SWAAK NONE O OTHER TXTAXI/GRND HDL 1 SW29396SW 27690 RIGHT WING INBOARD T/E FOREFLAP PREVIOUS REPAIR PEELING. TEMP REPAIRED PER SWA EA, THEN LATER AT PHX, REMOVED AND REPLACED FOREFLAP PER MM. 2L72 4F RTA16WE 20050411000782005041100078NM 2005 4 11 SWAA050976 120050331A3350101114 BULB BOEING737 7377H4 1384404NM R1 DOOR INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29477WN 33988 DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050411000812005041100081NM 2005 4 11 SWAA050979 120050331A53306545857 BEAR STRAP BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON FUSELAGE SKIN BEAR STRAP BETWEEN BS 947 TO BS 967, BETWEEN STR 23L TO STR 27R. REPAIRED BEAR STRAP SECTION PER SRM. 2L72 4F RTA16WE 20050411000852005041100085NM 2005 4 11 DXTA200500644 120050328A2760MS272407 POSITION SWITCH GULSTM200 200 4500308NM SPEED BRAKE SHORTED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07707QS1378 066 T/O UNSAFE EICAS ILLUMINATED DURING TAKEOFF ROLL. ABORTED AT 120 KNOTS. ATTEMPTED TO DUPLICATE INDICATION IN HANGER WITH EXTERNAL POWER SUPPLIED, COULD NOT DUPLICATE. INSPECTED ALL 8 AIRBRAKE SWITCHES VISUALLY FOR OBVIOUS DEFECTS, NONE NOTED. RANG OUT AIRBRAKE SWITCHES FROM CONNECTOR 364P AND FOUND INTERMITTANT SHORT TO GROUND AT PIN BB. ISOLATED SHORT TO PIN 2 AT TB 112. FOUND SHORT TO EXIST ON WIRE 2-20 OF AIRBRAKE SWITCH 48C. REMOVED AIRBRAKE SWITCH P/N MS27240-7 NSN AND INSTALLED NEW AIRBRAKE SWITCH P/N MS27240-7, NSN AS NEEDED. WORK ACCOMPLISHED IAW G200 M/M 27-60-20. 2L72 4F RTA53NM 20050411000872005041100087NM 2005 4 11 HNAA0500032 120050404A7997MS3474L2039P CONNECTOR DHAV DHC8 DHC8102 2809003NM NR 1 ENG OIL SHORTED A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07936HA4229442294 145 NR 1 ENGINE OIL PRESSURE WARINING LIGHT ILLUMINATED ON CLIMBOUT. OIL PRESSURE WAS CONFIRMED NORMAL. MAINTENANCE CLEANED MOISTURE FROM WING ROOT CANNON PLUG, OPS CHECK GOOD. 2H72 4T RTA13NM 20050411000882005041100088NM 2005 4 11 HNAA0500031 120050403A5270864202 SENSOR DHAV DHC8 DHC8102 2809003NM MLG DOOR MISRIGGED A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07815EX3286432864 321 JUST AFTER TAKEOFF THE RIGHT SIDE FORWARD GEAR DOOR CAME OPEN. CREW ELECTED TO RETURN BACK TO MDT. DID NOT DECLARE AN EMERGENCY. FOUND PROXIMITY SWITCH OUT OF RIG, RE-RIGGED, OP'S CHECK GOOD. 2H72 4T RTA13NM 20050411000932005041100093NM 2005 4 11 SWAA050994 120050402A3350101331 LENS BOEING737 7373G7 1384595NM EMERGNECY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29671SW 23785 DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS COVER PER MM. 2L72 4F RTA16WE 20050411001022005041100102CE 2005 4 11 DXTA200500647 120050328A282123061826 FILTER CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL FUEL SYSTEM OBSTRUCTED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07960QS399 399 7500160 CAE330338 AMBER FUEL FILTER BYPASS RT CAME ON DURING TAKEOFF JUST AFTER MAXIMUM POWER. ABORTED TAKEOFF. CAS MESSAGE REMAINED ILLUMINATED DURING TAXI TO RAMP. REPLACED RT ENG FUEL FILTER WITH A NEW FILTER KIT. LEAK CHECK SATISFATORY. NO FURTHER DEFECTS NOTED. 2L72 4J4 FRTT00007WITE6CH 20050411001062005041100106CE 2005 4 11 DXTA200500645 120050328A324099123882 VALVE CESSNA500 560CESSNA 2076750CE MLG FAILED E DXTAO OTHER O OTHER LDLANDING 1 GL07333QS8533 5600333 BRAKES LOCKED UP AT END OF LANDING ROLL AND WOULD NOT RELEASE AFTER STOPPING. REMOVED AND REPLACED LT MAIN WHEEL ASSY P/N ON/OFF 3-1490-1, S/N ON 2298 AND 3887P S/N OFF 3522. REMOVED AND REPLACED RT MAIN WHEEL ASSY, P/N ON/OFF 3-1490-1, S/N ON 2642, S/N OFF 3272. REMOVED AND REPLACED LT BRAKE ASSY P/N ON/OFF 2-1529-7, S/N ON 2401, S/N OFF 2281. REMOVED AND REPLACED RT BRAKE ASSY P/N OFF 2-1529-7, S/N ON 2779, S/N OFF 1692. REMOVED AND REPLACED PARKING BRAKE VALVE P/N ON/OFF 9912388-2, S/N ON 1568A, S/N OFF 0287A. REMOVED AND REPLACED PARK BRAKE CABLE, CE 560 M/M CHA 32-41-01, 32-40-00, 32-42-03, 12-12-02, 12-13-03. 2L72 4F RTA22CE 20050411001092005041100109NM 2005 4 11 SWAA050952 120050329A5310573149 POST BOEING737 7373H4 1384600NM COCKPIT WINDOW CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29364SW 26575 DURING SCHEDULED 1/4D CHECK, FOUND R1 COCKPIT WINDOW POST CRACKED AT UPPER OUTBOARD CORNER. REPAIRED WINDOW POST PER SRM. 2L72 4F RTA16WE 20050411001142005041100114EA 2005 4 11 SWIA200514831 120050329A492038004883 APU CNDAIRCL600 CL6002B19 1900309EA APU BAY SMOKE A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM07952SW4478 4478 7805 ON TAXI, F/A REPORTED SMOKE IN CABIN. REPLACED THE APU ASSY IAW MM 49-10-00. PACKS OPERATING NORMALLY AT THIS TIME IAW CRJ AMM REF CHAP 21-00-00. 2L72 4F RTA21EA 20050411001202005041100120NM 2005 4 11 HNAA0500030 120050402A7997 WIRE DHAV DHC8 DHC8201 2809001NM ENGINE INDICATORSHORTED A HNAAO OTHER N FALSE WARNING APAPPROACH 1 EA07969HA1408114081 468 ON APPROACH INTO CLT THE NR 1 LOW OIL PRESSURE CAUTION LIGHT ILLUMINATED. NO INDICATION OF OIL QUANTITY LOW. THE CREW DECLARED AN EMERGENCY AND CONTINUED TO LAND WITHOUT INCIDENT. FOUND WIRE SEGMENT 7932-103, SHORTED BETWEEN CONDUCTOR AND SHIELD. SHORTED AT FIREWALL CONNECTOR 9811-P29, REPLACED CONNECTOR. 2H72 4T RTA13NM 20050411001212005041100121NM 2005 4 11 SWAA050996 120050402A2560P4010021 BATTERY BOEING737 7377H4 1384404NM FLASHLIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29749SW 29801 FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2L72 4F RTA16WE 20050411001242005041100124EA 2005 4 11 VTZA200500042 120050401A5320601R311719 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27638BR 7311 INTERCOSTAL CRACKED AT .250 INCH IN LENGTH ON RIGHT OUTBOARD SIDE AT FS 484 AT BL 27.00. 2L72 4F RTA21EA 20050411001312005041100131NM 2005 4 11 QXEA200500537 120050325A5753 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09416QX 4083 PDX - LEFT WING OUTBOARD FLAP, UPPER SURFACE IS CHAFED BETWEEN YW222 AND YW285. REPAIRED IAW HORIZON AIR EA 6-57-325. 2H72 4T RTA13NM 20050411001362005041100136NM 2005 4 11 QXEA200500532 120050322A5420 BRACKET BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09416QX 4083 PDX - NR 2 ENGINE SPINE COWL FORWARD RIGHT BRACKETS CRACKED. REPAIRED IAW RD 8/4-71-032 AND DHC-8-400 SRM 51-42-05. 2H72 4T RTA13NM 20050411001382005041100138EA 2005 4 11 QXEA200500544 120050321A7830 STRUCTURE CNDAIRCL600 CL6002C10 1390015EA THRUST REVERSER WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - RIGHT ENGINE, UPPER AND LOWER THRUST REVERSER COWLS HAVE WEAR ON STOW RAMP AND STRIKER PLATES AS FOLLOWS UPPER, 3 EACH INBOARD, LOWER 1 EACH INBOARD. REPAIRED IAW HORIZON AIR EA R-78-24M R-78-25 ABD REO 670-78-34-351. 2L72 4F RTA21EA 20050411001542005041100154NM 2005 4 11 QXEA200500529 120050330A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09367PH 511 PDX - RIGHT OUTBOARD SEAT TRACK CORROSION PITS IN BOTTOM CHANNEL AT STATION X424. REPAIRED IAW DHC-8-200 SRM 1-40-00 AND SRM 51-40-11. 2H72 4T RTA13NM 20050411001562005041100156EA 2005 4 11 QXEA200500552 120050322A5751 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 600 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - RT WING AILERON UPPER LEADING EDGE SURFACES HAVE CHAFE MARKS. REPAIRED IAW CRJ700 SRM 51-41-02-001-001-A01. 2L72 4F RTA21EA 20050411001692005041100169NM 2005 4 11 AWXA200500378 120050330A3397BMS13311122 WIRE BOEING737 73733A 1384673NM SEAT ROW 14 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 PHX - EEL - DURING 4-DAY CHECK, FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 14 LT INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE AT PIN FOR CONNECTOR, RETERMINATED WIRE AT PIN AT SEAT ROW 14 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050411002022005041100202EA 2005 4 11 QXEA200500442 120050302A5210 STIFFENER CNDAIRCL600 CL6002C10 1390015EA ZONE 800 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - PASSENGER DOOR INTERNAL Z STIFFENER CRACKED BELOW ASSIST MOTOR OUTER BOTTOM BOLT. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20050411002082005041100208NM 2005 4 11 WRLA2005036 120050207A5512 SKIN DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST RT BARREL NUT HOLE NR 33. 2L73 4F4 FRTA22WE E24NE 20050411002092005041100209NM 2005 4 11 AWXA200500413 120050313A532069167832 INTERCOSTAL BOEING737 737375 13844BNNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 DURING C-05 CHECK CORROSION WAS FOUND ON FORWARD CARGO COMPARTMENT THRESHOLD INTERCOSTAL WEB AT BS 474, STR 25 RT. MAINTENANCE REMOVED CORRODED INTERCOSTAL WEB AT BS 474, STR 25 RT; FABRICATED A NEW REPLACEMENT WEB PER DWG 69-16783; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG. 8 & 12. 2L72 4F RTA16WE 20050411002162005041100216EA 2005 4 11 COMA0560147 120050225A2760 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA SPOILER ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01478CA 7671 FLIGHT 5845 - RECEIVED A FLIGHT SPOILER CAUTION MESSAGE DURING FLIGHT, AIRCRAFT DIVERTED TO SYR AND LANDED WITHOUT INCIDENT. PERFORMED A RESET OF THE SPOILER SYSTEM. 2L72 4F RTA21EA 20050412000682005041200068SO 2005 4 12 SIMA200508701 120050309A532014525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO FRAME 20 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SO27700LE 145156 THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED THE CORRODED SECTION. FABRICATED A FILLER, EXTERNAL ANGLE, SHIM AND PLATE. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 28, CHAPTER 53-21-10. (M) 2L72 4F RTT00011AT 20050412000712005041200071EA 2005 4 12 QXEA200500512 120050317A5210 PLATE CNDAIRCL600 CL6002C10 1390015EA ZONE 800 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09613QX 10045 PDX - MAIN CABIN DOOR AFT SACRIFICIAL PLATE DENTED. REPAIRED IAW REO 670-53-22-001. 2L72 4F RTA21EA 20050412000732005041200073EA 2005 4 12 QXEA200500510 120050320A5315 FLOORBEAM CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09613QX 10045 PDX - FLOORBEAM FS280.0 CORRODED WL72.50 FROM BLL 22.0 - BLR25.0 AND CRACK AT FS280.0, WL 72.50, BLL 12.0. REPAIRED IAW CRJ 700 REO 670-53-11-045 AND CRJ 700 SRM 51-42-06 2L72 4F RTA21EA 20050412000752005041200075EA 2005 4 12 QXEA200500508 120050317A5320 WEB CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09613QX 10045 PDX - RIGHTHAND WEB CORRODED IN AND AROUND FLOORBEAM FS 280.0, WL 72.50, BLR25.0. REPAIRED IAW CRJ SRM 51-42-06 AND REO 670-53-11-052. 2L72 4F RTA21EA 20050412000772005041200077NM 2005 4 12 AWXA200500421 120050312A5320654795710 CHANNEL BOEING737 737375 13844BNNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 DURING C-05 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT DOOR CUTOUT SILL WEB CLOSE OUT "U" CHANNEL BETWEEN BS 794 AND BS 847, AT RBL 28. MAINTENANCE REMOVED CORRODED "U" CHANNEL FROM BS 794 TO BS 847, AT RBL 28; FABRICATED A NEW REPLACEMENT SECTION OF CHANNEL PER DWG 65-47957; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050412000792005041200079NM 2005 4 12 AWXA200500419 120050318A53206546572515 STIFFENER BOEING737 737375 13844BNNM BULKHEAD CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 DURING C-05 CHECK CORROSION WAS FOUND ON VERTICAL STIFFENER ON FORWARD FACE OF BULKHEAD BS 1088, RBL 33, BETWEEN WL 210 AND WL 220. MAINTENANCE REMOVED CORRODED VERTICAL STIFFENER AT BS 1088, RBL 33, FROM WL 210 TO WL 220; FABRICATED A NEW REPLACEMENT STIFFENER PER DWG 65-46572; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 3 AND 8. 2L72 4F RTA16WE 20050412000812005041200081NM 2005 4 12 AWXA200500417 120050318A53206546579531 STIFFENER BOEING737 737375 13844BNNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 DURING C-05 CHECK CORROSION WAS FOUND ON RT TORQUE BOX STIFFENER AT BS 1116, STR 15 RT. MAINTENANCE REMOVED CORRODED RT TORQUE BOX STIFFENER AT BS 1116, STR 15 RT; INSTALLED NEW REPLACEMENT STIFFENER IAW B737-300 SRM 51-40-02, FIG 3 & 8. 2L72 4F RTA16WE 20050412000832005041200083NM 2005 4 12 AWXA200500415 120050318A53206940355502 STIFFENER BOEING737 737375 13844BNNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 DURING C-05 CHECK CORROSION WAS FOUND ON RT TORQUE BOX ANGLE AT BS 1104, STR 14 RT. MAINTENANCE REMOVED CORRODED RT TORQUE BOX ANGLE AT BS 1104, STR 14 RT; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 69-40355; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050412000862005041200086WP 2005 4 12 05FDEA00867 120050406A5320 WEB DOUG DC10 DC1010 3022110WP FUSELAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25571FE 47830 DURING INSPECTION, FOUND AT STA 330 X= 15 WITH CORROSION ON THE WEB FLIGHT COMPARTMENT FLOOR LINE. REMOVED CORROSION PER SRM 51-21-01 PAGE 28 (OUT LIMITS). DURING CONTROL CORROSION FOR LIMITS FOUND EA 2 CRACKS 2". REMOVED MEMBRANE IAW SRM 51-35-01 PG 1/13. REPLACED MEMBRANE IAW SRM 51-35-01 PG 1/13. (OPEN) 2L73 4F A22WE 20050412000882005041200088NM 2005 4 12 05FDEA00865 120050406A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT UPPER FORWARD SKIN PLANK NR 1R BARREL NUT BORE FOUND EXCEEDED LIMITS. REWORK/REPAIR 1-5510-7-5000 HAS BEEN COMPLIED WITH. 2L73 4F RTA22WE 20050412000902005041200090NM 2005 4 12 05FDEA00862 120050406A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT NR 4R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-83000. 2L73 4F RTA22WE 20050412000922005041200092NM 2005 4 12 05FDEA00859 120050405A5512 SKIN DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT UPPER FORWARD SKIN PLANK NR 7L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82991. 2L73 4F RTA22WE 20050412000942005041200094NM 2005 4 12 05FDEA00857 120050405A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON HORIZ STAB LT UPPER FWD SKIN PLANK NR 9L BARREL NUT BORE, FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA1-5510-82991. 2L73 4F RTA22WE 20050412000962005041200096NM 2005 4 12 05FDEA00855 120050405A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT UPPER AFT SKIN PLANK NR 33R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82942. 2L73 4F RTA22WE 20050412000972005041200097NM 2005 4 12 05FDEA00854 120050405A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT UPPER FORWARD SKIN PLANK NR 4L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82939. 2L73 4F RTA22WE 20050412000982005041200098EU 2005 4 12 05FDEA00849 120050405A5522 SKIN AIRBUS310 A310 EU LT ELEVATOR DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 REPAIR NEEDS EVALUATION FOR FAA APPROVED DATA AND MAJOR OR MINOR CLASSIFICATION. LT ELEVATOR UPPER SURFACE T/E 6' O/B FROM I/B END (ITEM 35 OF LIST). REPAIRED ELEVATOR IAW E NR #6-5520-87201. REPAIR IS CLASSIFIED AS MINOR AS PER EA6-5520-87201 AND FEDEX GMM 6-2-100. 2L72 4F RTA35EU 20050412001172005041200117NM 2005 4 12 DHL2005782546 120050318A5531 STRINGER BOEING727 727227 1384078NM VERTCIAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 VERT STAB STR 8L CRACKED AT FIN STA 180.6. REMOVED FASTENERS CUT OUT DAMAGED AREA FABBED NEW STIFFENER FROM BAC 1517-1367 PO NR 501953 DIM 4 5/8" BY 3" SPLICE FROM AND 10133-1401 PO NR 501952 DIM 19 1/8" BY 2" SPLICE FROM AND 10134-1201 PO NR 501952 DIM 19 1/8" BY 2" FILLER FROM 7075 T 6 .080 PO NR 9002012 DIM 19 1/8" BY 1" FILLER FROM 7075 T6 .100 PO NR 9911585 DIM 19 1/8" BY 3/4" AND CLIP FROM AND 10133-1401 PO NR 501952 DIM 2" BY 2" IAW 727 SRM 55-30-4 FIG 1. REPAIR PARTS TREATED, PRIMED AND INSTALLED IAW 727 SRM 51-10-2 AND 55-30-4 FIG 1. 2L73 4F A3WE 20050412001722005041200172NM 2005 4 12 DHL2005782506 120050308A5320 WEB BOEING727 727227 1384078NM FUSEAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 STA 1243 RT LOWER TORQ BOX WEB IS CRACKED. STOP DRILLED CRACK IAW B727 SRM 51-10-1. HFEC PER NDT PT 6 51-00-00 FIG 23 CRACK ENDS AT STOP DRILL. FABRICATED DOUBLER REPAIR USING 7075 T6 .032 PO NR 900573 DIM 4 3/4 INCH BY 2 1/2 INCH IAW B727 SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1. ALODINED AND PRIMED DOUBLER IAW B727 SRM 51-10-2. INSTALLED DOUBLER IAW B727 SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1. 2L73 4F A3WE 20050412001772005041200177NM 2005 4 12 DHL2005782529 120050311A5730 SKIN BOEING727 727227 1384078NM RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 R/WING UPPER SURFACE CRACKED OUT AT NR 11 SPOILER HINGE CUTOUT. REMOVED SPOILER PANEL FOR ACCESS IAW 727 MM 27-61-1. STOPPED DRILLED CRACK IAW 727 SRM 51-10-1. FABBED DOUBLER FROM 7075T6 .071 PO NR 9001737 DIM 5" BY 4" IAW 727SRM 57-30-4 FIG10. DOUBLER TREATED PRIMED INSTALLED IAW727 SRM 51-10-2 AND 57-30-4 FIG 1. REINSTALLED NR 1 SPOILER PNL IAW 727 MM 27-61-01. 2L73 4F A3WE 20050412001792005041200179NM 2005 4 12 DHL200578228 120050311A5753 SKIN BOEING727 727227 1384078NM LT TE FLAP GOUGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 LT OB FORE FLAP L/E IB AT WBL 314 HAS 2 GOUGES IN REPAIR DOUBLER SURFACE. REMOVED DOUBLER IAW B727 SRM 51-30-2 FABRICATED NEW DOUBLER USING 2024T3 .063 PO NR 9001978 DIM 7 1/2" BY 3 1/2" IAW B727 SRM 57-50-2 FIG 3 AND 57-30-4 FIG 1. ALODINE AND PRIMED PART AND DOUBLER IAW B727 SRM 51-10-2. INSTALLED DOUBLER REPAIR IAW B727 SRM 57-50-2 FIG 3 AND 57-50-4 FIG 1. 2L73 4F A3WE 20050412001812005041200181NM 2005 4 12 DHL2005782527 120050311A5522 SKIN BOEING727 727227 1384078NM LT ELEVATOR DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 LT ELEV STA 136 HAS 3 DENTS EACH. EVALUATED DENTS AT LT ELEVATOR STA 136 1ST A/Y=1.25/.017=73, 2ND 2.75/.03=91, WITHIN LIMITS AND 3RD OUT OF LIMITS IAW 727 SRM 55-20-1 FIG 1. CUT OUT DAMAGED AREA DIM 5/8" BY 1/2" AND FABBED DOUBLER FROM 2024T3 .032 PO AND 9002034 DIM. 2 1/2"X 2 1/4"IAW SRM 55-20-3 FIG 1. DOUBLER TREATED, PRIMED, AND INSTALLED IAW 727 SRM 51-10-2 AND 55-20-3 FIG 1. CALCULATED ELEVATORS NEW MOMENT OF 119.545 IT IS WITHIN LIMIS 120 +- 20 POUND INCHES NO FURTHER ACTION REQUIRED IAW 727 SRM 51-80-7. 2L73 4F A3WE 20050412001832005041200183NM 2005 4 12 DHL2005782523 120050310A5754 SKIN BOEING727 727227 1384078NM NR 5 SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 SKIN CRACKED ON UPPER SKIN CUT OUT FOR NR 5 SLAT IB TRACK, RT WING LE WS 375. STOP DRILLED CRACK SIZE 1/4 AT UPPER SKIN CUT OUT NR 5 SLAT IB TRACK RT WING LE IAW B727 SRM 51-10-1. FABRICATE DOUBLER REPAIR USING 2024T3 .063 PO NR 9001634 SIZE 7 1/2 INCH BY 6.5 INCH IAW B727 SRM 57-30-4 FIG 11. ALODINE AND PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED DOUBLER REPAIR IAW B727 SRM 57-30-4 FIG 11 AND 51-30-2. 2L73 4F A3WE 20050412001852005041200185NM 2005 4 12 DHL2005782521 120050310A5330 SKIN BOEING727 727227 1384078NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 SEVERAL DENTS RT SIDE FUSELAGE SKIN AFT OF STA 178 BELOW RADOME. CUT OUT DAMAGE AREA IAW B727 SRM 1 1/2" BY 1 1/2" IAW B727 SRM 53-30-2. FABRICATED DOUBLER USING 2024T3 .050 PO NR 9002093 DIM. 10" BY 8" IAW B727 SRM 53-30-2 FIG. 1 AND 53-30-3 FIG. 1. ALODINE AND PRIMED PART AND AREA IAW B727 SRM 51-10-2. INSTALLED DOUBLER IAW 53-30-2 FIG 1 AND 53-30-3 FIG 1. 2L73 4F A3WE 20050412001872005041200187SW 2005 4 12 ALGA099112 120050123A6710406310405101 PITCH LINK BELL 407 407 1182206SW MAIN ROTOR WORN B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03627AL807 53284 AXIAL PLAY BEYOND MAX AND ROUGH. REPLACED WITH NEW BY FIELD MAINTENANCE. 1G71 3U O H2SW 20050412001912005041200191NE 2005 4 12 ALGA100035 120050226A632023077527 GEARBOX SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL MAIN ROTOR MAKING METAL B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03522AL395 760236 CAE890416S FOUND METAL ON BOTH CHIP PLUGS. FOUND MAIN CAUSE TO BE PINION GEAR / REPAIRED G/BOX, REPLACED PINION GEAR,TORQUE METER GEAR,PTO GEARSHAFT. 1G72 3U3 U H1NE E1GL 20050412002162005041200216EA 2005 4 12 COMA0560246 120050407A2750860D10018ABC FCU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAULTY A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01941CA25642 7050 FLIGHT 5142 RECEIVED A FLAP FAIL CAUTION WHILE PARKED AT THE GATE. REPLACED THE FLAP ELECTRONIC CONTROL UNIT. 2L72 4F RTA21EA 20050412002172005041200217EA 2005 4 12 COMA0560247 120050405A4970 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA APU BAY ILLUMINATED A COMAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO01979CA 7159 FLIGHT 5106 DURING CRUISE FLIGHT RECEIVED AN APU OIL TEMPERATURE CAUTION MESSAGE, EXECUTED QRH PROCEDURE AND DIVERTED TO CMH. INTERROGATED APU ECU, INSPECTED OIL LEVEL AND CHECKED FOR LEAKS, OPERATED APU WITH NO FAULTS. 2L72 4F RTA21EA 20050412002182005041200218EA 2005 4 12 COMA0560248 120050406A5270 TARGET CNDAIRCL600 CL6002B19 1900309EA MAIN PAX DOOR OUT OF ADJUST A COMAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO01977CA 7157 FLIGHT 5815 DURING CRUISE FLIGHT (CID/CVG) RECEIVED A CABIN DOOR WARNING MESSAGE, AIRCRAFT DIVERTED TO MLI. PERFORMED BITE TEST ON PSEU AND INSPECTED CABIN DOOR TARGETS, FOUND NO DISCREPANCIES. 2L72 4F RTA21EA 20050412002192005041200219EA 2005 4 12 COMA0560249 120050406A32604622 VALVE CNDAIRCL600 CL6002B19 1900309EA NLG FAULTY A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01420CA11714 7451 FLIGHT 5846 DURING APPROACH INTO XNA RECEIVED A NOSE GEAR DISAGREE CAUTION, CREW DECLARED AN EMERGENCY AND ABORTED 1ST APPROACH, THEN LANDED WITHOUT INCIDENT ON 2ND ATTEMPT. REPLACED THE NOSE LANDING GEAR PRIORITY VALVE. 2L72 4F RTA21EA 20050412002202005041200220EA 2005 4 12 COMA0570038 120050404A5270 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA E/E BAY DOOR ILLUMINATED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01368CA 10075 FLIGHT 5286 DURING TAKEOFF RECEIVED AN AVIONICS BAY DOOR CAUTION MESSAGE, ABORTED TAKEOFF AND RETURNED TO THE GATE. DEFERRED DOOR INDICTION PER MEL. 2L72 4F RTA21EA 20050412002212005041200221EA 2005 4 12 COMA0570039 120050402A5270 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA PAX DOOR FALSE ACTIVATIONA COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01331CA 10061 FLIGHT 5493 DURING CLIMBOUT OF JAX RECEIVED A CABIN DOOR WARNING, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. AIRCRAFT FERRIED TO CVG, CHECKED SENSOR PX27 FOR GAP, PRESSURIZED AIRCRAFT, DISCREPANCY COULD NOT BE DUPLICATED BY MAINTENANCE. 2L72 4F RTA21EA 20050412002222005041200222EA 2005 4 12 COMA0570040 120050404A284073811812 COMPUTER CNDAIRCL600 CL6002C10 1390015EA AVIONIC BAY FAULTY A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01659CA2292 10153 FLIGHT 5230 DURING CRUISE FLIGHT (CVG/PHL) RECEIVED A FUEL CHANNEL NR 2 FAIL STATUS MESSAGE, AIRCRAFT DIVERTED TO PIT AND LANDED WITHOUT INCIDENT. AIRCRAFT FERRIED TO CVG FOR REPLACEMENT OF THE FUEL SYSTEM COMPUTER (FSCU). 2L72 4F RTA21EA 20050412002252005041200225WP 2005 4 12 05FDEA00321 120050301A5320ADA0152 FITTING DOUG MD10 MD1010F 3022112WP FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25361FE 48260 CRACKED LONGERON END FITTING ON LONGERON 47 RIGHT IN FRONT OF PRESSURE BULKHEAD AT FUSETAGE STATION 1129. COMPLIED WITH EA 8-5340-83987, FUSELAGE- LONGERON 47 RIGHT STATION 1129, CRACK, REPAIR. REFERENCE NON-ROUTINE N00242. 2L73 4F RTA22WE 20050412002292005041200229WP 2005 4 12 GTIA050075 120050319A5610 LATCH DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE COCKPIT BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23827NK 49793 F/O CLEARVIEW WINDOW JAMS WHEN OPENING, WINDOW UNLATCHES BUT IS JAMMED THUS NOT ABLE TO SLIDE AFT IN TRACKS. AIRCRAFT TAIL SWAP WITH 822NK. REPLACED BROKEN UPPER LATCH BAR ON F/O`S CLEARVIEW WINDOW. OPS CHECKED GOOD. (K) 2L72 4F4 FRTA6WE E9NE 20050412002312005041200231WP 2005 4 12 GTIA050060 120050218A5330 SKIN DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FLUSH REPAIR FS 622 LONGERON 22R-24R HAS NO FINGER DOUBLER. REMOVED TEMP REPAIR. FABRICATED PERMANENT REPAIR PARTS. TREATED AND PRIMED ON FINAL REPAIR. INSTALLED REPAIR IAW SRM. (K) 2L72 4F4 F A6WE E9NE 20050412002332005041200233WP 2005 4 12 GTIA050054 120050215A5330 SKIN DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FUSELAGE EXTERIOR STA 1485 CANT. LT LOWER SKIN CRACKED. CUT OUT DAMAGED AREA 2 INCH X 4.8 INCH AT STA 1485. FABED FINGER DOUBLER, TREATED AND PRIMED. INSTALLED REPAIR ON LT LOWER SKIN, STA 1485 CANT IAW SRM. (K) 2L72 4F4 F A6WE E9NE 20050412002352005041200235WP 2005 4 12 GTIA050056 120050220A5320 SUPPORT ANGLE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 THRESHOLD SUPPORT ANGLE, STA 1212, ON DOOR JAMB BEAM IS CORRODED. REMOVED CORROSION AT SUPPORT ANGLE. MATERIAL LOSS OUT OF LIMITS. REMOVED SUPPORT ANGLE AT STA 1212. FABRICATED NEW SUPPORT ANGLE, HEAT TREATED REPAIR PART. INSTALLED SUPPORT ANGLE AT STA 1212 IAW SRM. (K) 2L72 4F4 F A6WE E9NE 20050412002362005041200236WP 2005 4 12 GTIA050059 120050313A3260 PROXIMITY SENSOR DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE NLG FAULTY A GTIAO OTHER N FALSE WARNING CLCLIMB 1 GL23803NK 48087 ON TAKEOFF, THE GEAR RETRACTED BUT THE NOSE (RED) UNSAFE LIGHT REMAINED ON, AIRCRAFT TAIL SWAP WITH 819NK. T/S FOUND NOSE GEAR DOWNLOCK PROX SENSOR AT MAX CLEARANCE. REMOVED AND REPLACED PROXIMITY SENSOR AND RESHIMMED PROXIMITY SWITCH FOR DESIRED TARGET SENSOR CLEARANCE - PERFORMED BITE CHECK ON NLG. (K) 2L72 4F4 F A6WE E9NE 20050412002412005041200241WP 2005 4 12 GTIA050058 120050310A5751 COVER DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE LT AILERON DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 LT AILERON IB UPPER ATTACH FITTING COVER DAMAGED, AIRCRAFT TAIL SWAP WITH 819NK. INSTALLED LT AILERON IB UPPER ATTACH FITTING COVER. (K) 2L72 4F4 F A6WE E9NE 20050412002422005041200242WP 2005 4 12 GTIA050062 120050216A5230 ANGLE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE MID CARGO DOOR CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 MID PIT DOOR INTERNAL ANGLE CRACKED AT LOWER CENTER EDGE. REMOVED INTERNAL ANGLE FROM MID CARGO DOOR LOWER CENTER EDGE. LOCATED AND DRILLED NEW INTERNAL ANGLE (FITTING), INSTALLED NEW FITTING IAW SRM. (K) 2L72 4F4 F A6WE E9NE 20050412002442005041200244WP 2005 4 12 GTIA050066 120050215A5753 SKIN DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE FLAP VANE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 RT WING OB FLAP MID FIXED VANE DAMAGED. REMOVED DAMAGED SKIN AND CORE TO OB FLAP VANE, FABRICATED REPAIR DOUBLER AND HONEYCOMB CORE. TREATED METAL, BONDED CORE AND DOUBLER. INSTALLED REPAIRED CORE AND SKIN IAW SRM. (K) 2L72 4F4 F A6WE E9NE 20050412002462005041200246NE 2005 4 12 GTIA050049 220050304A7200 ENGINE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE LEFT MALFUNCTIONED A GTIAE ENGINE SHUTDOWN KMJFLUID LOSS OVER TEMP WARNING INDICATION DEDESCENT 1 GL23814NK 49619 LOST OIL IN LT ENGINE, QTY 0, PRESSURE 40 PSI, TEMP RISING, SHUT DOWN LT ENGINE BEFORE LOSING ALL OIL PRESSURE, OIL PRESSURE BELOW 10 PSI WHILE WINDMILLING. REMOVED AND REPLACED NR1 ENGINE. (K) 2L72 4F4 FRTA6WE E9NE 20050412002472005041200247WP 2005 4 12 GTIA050038 120050223A7711 LINE DOUG DC9 DC981 3022081WP PWA JT8 JT8D217C 52053NE EPR BROKEN A GTIAO OTHER O OTHER ININSP/MAINT 1 GL23811NK 48017 ENGINE INDICATIONS DO NOT MATCH OBSERVED ENGINE PERFORMANCE WHEN OPERATING AT T/O POWER AND CRUISE, NR1 EPR IS BELOW EXPECTED. AIRCRAFT TAIL SWAP WITH 833. T/S NR 1 ENGINE AND FOUND NO LEAKS, PROBLEM SEEMS TO BE ON NR 2 ENGINE PT2 AND PT7 LINES, CHECKED OKAY, BLEW OUT PT2 PORT FOR OBSTRUCTION, NONE FOUND. NR 2 ENGINE READING LOW DUE TO A BROKEN PT2 FLEX LINE ON THE EPR TRANSMITTER, REMOVED AND REPLACED EPR TRANSMITTER. OPS CHECK AND ENGINE RUN-UP NORMAL. (K) 2L72 4F4 F A6WE E9NE 20050412002482005041200248 2005 4 12 GTIA050039 420050225A3425 INDICATOR DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE NR 2 ADI FAILED A GTIAK NONE O OTHER TOTAKEOFF 1 GL23825NK 53012 F/O`S ADI WENT BLANK THEN SHOWED FAIL ON TAKEOFF ROLL, TAIL SWAP WITH AC 833. REMOVED AND REPLACED NR2 ADI, OPS CHECK NORMAL. (K) 2L72 4F4 FRTA6WE E9NE 20050412002492005041200249 2005 4 12 GTIA050041 420050228A3423 RACK DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE NR 1 & NR 2 DEFECTIVE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 DURING RTS CHECK FOR LMP UPGRADE, FOUND CAPT`S RMI SYNC INDICATION NOT MOVING, COMPASS CARD DOES NOT MOVE BACK TO COMPASS HEADING, TAIL SWAP WITH AC 808. REMOVED AND REPLACED COMPASS RACK FOR CAPT`S COMPASS SYSTEM. (NR 2) NO HELP, INSTALLED NEW DG. NO HELP, RE-INSTALLED ORIGINAL COMPASS RACK AND DG. SWAPPED CAPT`S AND F/O`S RMI`S. NO HELP, SWAPPED BACK TO ORIGINAL POSITIONS. INSTALLED NEW FLUX VALVE. NO HELP, REMOVED AND REPLACED F/O`S COMPASS RACK, BOTH NR 1 AND NR 2 COMPASS SYSTEMS. OPS CHECK OK. (K) 2L72 4F4 F A6WE E9NE 20050412002502005041200250WP 2005 4 12 GTIA050046 120050117A5320 DOUBLER DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 AFT PIT FS 1338 APB FWD SIDE STIFFNER LOWER DOUBLER CORRODED L30. REMOVED CORROSION AND FOUND EVIDENCE OF CORROSION BETWEEN DOUBLER AND APB. REMOVED DOUBLER, REMOVED LONGERON END FITTING STA 1338 L28R, L29R, L28L AND L29L, REMOVED WEB STIFFNER ON FALSE BULKHEAD L29R TO L29L. DRILLED AND LOCATED HOLES IN SHEARTIE DOUBLER, TREATED, PRIMES AND INSTALLED REPAIR ANGLES, DOUBLERS AND END SPLICES. (K) 2L72 4F4 F A6WE E9NE 20050412002512005041200251NM 2005 4 12 GTIA050036 120050301A2781 PROXIMITY SENSOR DOUG MD80 MD83 3023681NM PWA JT8 JT8D217C 52053NE LT L/E SLAT DEFECTIVE A GTIAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 GL23828NK 49823 UPON RETRACTION OF SLATS AND FLAPS, SLAT DISAGREE LIGHT CAME ON AND REMAINED ON UNTIL SLATS RE-SELECTED. AFTER LANDING LIGHT CAME BACK ON WHEN SLAT/ FLAP SELECTED TO UP/RETRACT, AIR RETURN. INSPECTED PROXIMITY SWITCHES AND FOUND SWITCH ON NR 1 SLAT (C) SENSOR, CLEANED AND LUBED NR 1 SLAT PROXIMITY SENSOR AND PERFORMED OPS CHECK- GOOD. T/S FOUND LT WING SENSOR (CT) TARGET BAD, REMOVED AND REPLACED SENSOR AND PERFORMED TEST OF PROX BOX, NORMAL. (K) 2L72 4F4 FRT E9NE 20050412002562005041200256WP 2005 4 12 GTIA050064 120050220A5330 SKIN DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE FUSELAGE DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FUSELAGE SKIN DENTED AT FS 304 BETWEEN LONGERON 28L-29L. (D=0.5 INCH, X=0.015 INCH D/X= 33.3). DENT WAS FOUND TO BE LESS THAN 1.0 INCH FROM FRAME REQ A CUT OUT REPAIR. CUT OUT DAMAGED SKIN AT FS 304 BETWEEN LONGERON 28L-29L. FABED NEW SKIN SECTION, REPAIR DOUBLER AND FABED NEW 4 EA STRAPS. TREATED, PRIMED AND INSTALLED AT FS 304 BETWEEN 28L-29L. (K) 2L72 4F4 F A6WE E9NE 20050412002582005041200258WP 2005 4 12 GTIA050043 120050219A7920 OIL FILTER DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE NR 2 ENGINE CLOGGED A GTIAO OTHER J WARNING INDICATION DEDESCENT 1 GL23835NK 53044 725701 NR2 ENGINE OIL STRAINER CLOGGING LIGHT CAME ON DURING DESCENT, FOLLOWED QRH PROCEDURE REDUCED THRUST AND LIGHT WENT OUT, TURNING ONTO FINAL APPROACH LIGHT, CAME BACK ON WITH THROTTLE AT IDLE, LIGHT REMAINED ON, SHUT ENGINE DOWN. REMOVED AND REPLACED NR2 ENGINE MAIN OIL FILTER, PERFORMED ENGINE RUN AND LEAK CHECK, NO OIL STRAINER CLOGGING LIGHT AND NO LEAKS DETECTED. FOUND CARBON DEPOSITS IN NR 2 ENGINE OIL FILTER. (K) 2L72 4F4 FRTA6WE E9NE 20050412002612005041200261WP 2005 4 12 GTIA050073 120050321A2120 SMOKE DOUG DC9 DC983 3022083WP PWA JT8 JT8D1 52044NE CABIN DETECTED A GTIAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL23836NK 53045 DURING TAXI, AFT FLIGHT ATTENDANT REPORTED SMOKE IN THE AFT CABIN, ENTIRE AIRCRAFT SMELLED LIKE AN OVERHEATED PACK, GATE RETURN. OPS CHECKED RT AUTO-TEMP. NO DEFECTS NOTED, OPS CHECKED GOOD. (K) 2L72 4F4 FRTA6WE E2EA 20050412002622005041200262WP 2005 4 12 GTIA050077 120050326A2450 KNOB DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE COCKPIT DEFECTIVE A GTIAO OTHER O OTHER ININSP/MAINT 1 GL23829NK 49931 AC VOLT/FREQ SELECTOR KNOB DOES NOT ROTATE TO ANY POSITION, AIRCRAFT TAIL SWAP TO 825NK. REMOVED AND REPLACED VOLT/FREQ DEFLECTOR KNOB. OPS CHECK GOOD. (K) 2L72 4F4 F A6WE E2EA 20050412002642005041200264WP 2005 4 12 GTIA050069 120050218A5230 SKIN DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE AFT CARGO DOOR DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 DENT ON AFT CARGO DOOR AT STA 1165, 13 INCHES FROM FORWARD EDGE, 14 INCHES FROM UPPER EDGE (D=2.0, X=0.05, D/X=40). FOUND DENT TO BE COND. 1B. PERFORMED COLD WORK AREA BACK TO ORIGINAL CONTOUR. DYE PENETRANT PERFORMED FOR CRACKS. FABRICATED DOUBLER. TREAT AND PRIMED DOUBLER AND SKIN. INSTALLED DOUBLER IAW SRM. (K) 2L72 4F4 F A6WE E9NE 20050412002652005041200265WP 2005 4 12 GTIA050065 120050218A5330 SKIN DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE FUSELAGE DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FUSELAGE SKIN DENTED AT FS 310, LONGERON 29L-28L. (D=0.5 INCH, X=0.010 INCH, D/X=50). DENT WAS FOUND TO BE LESS THAN 1.0 INCH AND REQ A CUT OUT REPAIR. FAB`D NEW SKIN SECTION, REPAIR DOUBLER, FINGER DOUBLER, FABED (4 EA) STRAPS. TREATED, PRIMED AND TOP COATED REPAIRED PARTS. INSTALLED REPAIRED SKIN FILLER, FINGER DOUBLER, AND (4 EA) STRAPS PART AT FS 304, L28L-29L IAW SRM. (K) 2L72 4F4 F A6WE E9NE 20050412002662005041200266WP 2005 4 12 GTIA050067 120050214A5230 SKIN DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE MID CARGO DOOR DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 (1EA) MINOR DENT ON MID CARGO DOOR EXTERNAL SKIN AT LOWER L/R MARKED. DENT MEASURE IS OUT OF LIMITS CONDITION. 2(D=0.25, X=0.75). REMOVED CARGO DOOR FOR FOM, APPLIED DYE PENETRANT FOR CRACKS. FABED (3 SHIMS) AND REPAIR DOUBLER. TREATED SKIN, SHIMS AND DOUBLER IAW SRM. INSTALLED MID CARGO DOOR. (K) 2L72 4F4 F A6WE E9NE 20050412002672005041200267NE 2005 4 12 GTIA050074 220050318A7200 ENGINE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE NR 1 VIBRATION A GTIAO OTHER E VIBRATION/BUFFET TXTAXI/GRND HDL 1 GL23827NK 49793 NR 1 ENGINE HAS VIBRATION AT IDLE ON GROUND AND IN FLIGHT, AIRCRAFT TAIL SWAP WITH 819NK. PERFORMED ENGINE VIBRATION TEST ON NR 1 ENGINE AND NO DEFECTS NOTED, WITHIN LIMITS. INSPECTED INLET AND EXHAUST AREAS, INSPECTED CSD, GEAR BOX MAG PLUGS AND OIL FILTER, NO DEFECTS NOTED. (K) 2L72 4F4 FRTA6WE E9NE 20050412002682005041200268EA 2005 4 12 A6WA200540120 120050319A5743601R572100323 BUSHING CNDAIRCL600 CL6002B19 1900309EA LT WING OUT OF POSITION A A6WAK NONE O OTHER ININSP/MAINT 1 GL31413AW 7585 LEFT AFT MLG TRUNNION BUSHING MIGRATED .006. REMOVED AND REPLACED LEFT AFT MLG TRUNNION BUSHING WITH 2ND OVERSIZED BUSHING P/N 601R-57-21-003-23 IAW BOMARDIER REO 601R-57-21-0003 REV B. (M) 2L72 4F RTA21EA 20050412002722005041200272NM 2005 4 12 ASAA0540070 120050131A52416545849171 DOOR FRAME BOEING737 7374Q8 138447QNM GALLEY DOOR GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - FOUND AFT GALLEY DOOR FORWARD SIDE FRAME GOUGED ADJACENT TO UPPER LATCH CRANK. REMOVED AND REPLACED AFT GALLEY DOOR SIDE FRAME. (M) 2L72 4F RTA16WE 20050412002732005041200273NM 2005 4 12 ASAA0540143 120050224A5320654587512 SUPPORT BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02791AS 28886 PAE - FOUND CORROSION ON RIGHT ENTRY DOOR CUTOUT, BS 297-328 RBL 62, WL 208 LOWER FRAME INBOARD THRESHOLD SUPPORT HAS CORROSION. REMOVED AND REPLACED. (M) 2L72 4F RTA16WE 20050412002742005041200274NM 2005 4 12 ASAA0540134 120050219A531265465682 BULKHEAD BOEING737 737490 1384715NM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02791AS 28886 PAE - FOUND DENT ON 1016 BULKHEAD. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA16WE 20050412002762005041200276NM 2005 4 12 ASAA0540136 120050218A532069434477U2 SUPPORT BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02791AS 28886 PAE - FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT. INSTALLED NEW SUPPORT. (M) 2L72 4F RTA16WE 20050412002772005041200277NM 2005 4 12 ASAA0540151 120050227A5320 SUPPORT BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02791AS 28886 PAE - FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT BS 727-727E PLUS 10 INCHES, LBL 22, WL 156. REMOVED AND REPLACED SIDEWALL SUPPORT. (M) 2L72 4F RTA16WE 20050412002782005041200278NM 2005 4 12 ASAA0540153 120050227A532065176887180 SILL BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02791AS PAE - FOUND CORROSION ON LT ENTRY DOOR CUTOUT MOPSILL BS 303 TO 360, LBL 60, WL 208. REPLACED MOPSILL. (M) 2L72 4F RTA16WE 20050412002802005041200280NM 2005 4 12 ASAA0540146 120050225A53206547957UL INTERCOSTAL BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02791AS 28886 PAE - FOUND CORROSION ON INTERCOSTAL AT BS 858 RBL 20 WL 163. REMOVED AND REPLACED INTERCOSTAL. (M) 2L72 4F RTA16WE 20050412002842005041200284EA 2005 4 12 ASOA05248 120050319A33506100976 LIGHT CNDAIRCL600 CL6002C10 1390015EA CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM02709EV 10068 FLT 4818 - DURING A GROUND INSPECTION IN SLC, THE EMERGENCY CEILING FLOODLIGHTS AT ROWS 10/17 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMPS IN THE EMERGENCY CEILING FLOOD LIGHT AT ROWS 10 AND 17. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050412002852005041200285NM 2005 4 12 ASAA0540152 120050227A532065317875 SUPPORT BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02791AS 28886 PAE - FOUND CORROSION ON LT ENTRY DOOR CUTOUT BS 312-344, LBL 62, SL 208 LOWER FRAME THRESHOLD SUPPORT. REPLACED SUPPORT. (M) 2L72 4F RTA16WE 20050412002862005041200286NM 2005 4 12 ASAA0540064 120050126A52476550904 DOOR BOEING737 7374Q8 138447QNM APU GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - APU DOOR HAS A GOUGE 3 INCHES AFT FROM HATCH. REPAIRED PER SRM 51-70-13. (M) 2L72 4F RTA16WE 20050412002902005041200290NM 2005 4 12 ASAA0540053 120050126A5320654769012 SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - AFT CARGO BAY CORROSION ON FLOOR TO SIDEWALL SUPPORT. AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT BS 727B PLUS 8 INCHES TO 727F PLUS 7 INCHES, RBL 23 WL 156 WILL BE REPLACED ON 4879144. (M) 2L72 4F RTA16WE 20050412002912005041200291NM 2005 4 12 ASAA0540063 120050127A5320655572615 ANGLE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - CORROSION OF FLOOR TO SIDEWALL L-ANGLE TIE. REMOVED, FABRICATED AND INSTALLED PART PER SRM 53-60-53, 51-20-01 AND 51-40-02. (M) 2L72 4F RTA16WE 20050412002922005041200292NM 2005 4 12 ASAA0540059 120050126A5320654659244 FLOOR SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - AFT CARGO BAY CORROSION ON UPPER SURFACE OF FLOOR SUPPORT AT FLOORBOARD SUPPORT STRAP TOGGLE. REPAIRED PER SRM 53-00-53 AND EA 5320-01378. (M) 2L72 4F RTA16WE 20050412002942005041200294NM 2005 4 12 ASAA0540061 120050127A532069434961 SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - AFT CARGO BAY CORROSION ON FLOOR TO SIDEWALL SUPPORT. REMOVED AND REPLACED DAMAGED FLOOR TO SIDEWALL SUPPORT PER SRM 51-40-02, AND 53-60-53. (M) 2L72 4F RTA16WE 20050412002982005041200298NM 2005 4 12 ASAA0540055 120050126A5320654659237 FLOOR SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - AFT CARGO BAY FLOOR SUPPORT DAMAGED BS 727F PLUS 7 INCHES TO 727G PLUS 13 INCHES RBL 3, WL 156. COMPLETION ON THIS CARD WILL BE ACCOMPLISHED ON CARD NR 4879499. (M) 2L72 4F RTA16WE 20050412002992005041200299NM 2005 4 12 ASAA0540062 120050127A532069434961 FLOOR SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - AFT CARGO BAY FLOOR SUPPORT DAMAGED AT BS 727D PLUS 17. REPAIRED FLOOR SUPPORT PER SRM 53-00-53 FIG 201. (M) 2L72 4F RTA16WE 20050412003002005041200300NM 2005 4 12 ASAA0540065 120050131A5320657374337 SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - FOUND FORWARD CARGO BAY, CORROSION ON FLOOR TO SIDEWALL SUPPORT, BS 500A PLUS 15 INCHES TO 500D PLUS 10 INCHES RBL 23 WL 156. CORROSION OUT OF LIMITS. REMOVED, FABRICATED AND INSTALLED NEW FLOOR TO SIDEWALL SUPPORT BS 500A TO 500G RBL 23 WL 156. (M) 2L72 4F RTA16WE 20050412003022005041200302NM 2005 4 12 ASAA0540056 120050125A532165338598 FLOORBOARD BOEING737 7374Q8 138447QNM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - AFT CARGO BAY FLOORBOARD NR 4 GOUGED AT RT FORWARD TIE DOWN CUTOUT. REMOVED GOUGED BY .25 INCH BY 1 INCH, FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53 FIG 101 DETAIL V. FABRICATED, ALODINED AND PRIMED ACB NR 4 FLOORBOARD IAW 51-40-2 STEP 8B AND AMM 51-21-21 STEP 3 MADE OUT OF 2024 T3 .071 INCH LOT 586654 IAW SRM 53-60-95 FIG 1, SH 4, DETAIL NR. (M) 2L72 4F RTA16WE 20050412003032005041200303NM 2005 4 12 ASAA0540057 120050126A5320654659249 FLOOR SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - AFT CARGO BAY CORROSION ON UPPER SURFACE OF FLOOR SUPPORT AT FLOORBOARD SUPPORT STRAP. REPAIRED PER SRM 53-00-53 AND EA 5320-01378. (M) 2L72 4F RTA16WE 20050412003042005041200304NM 2005 4 12 ASAA0540067 120050130A5320654659242 FLOOR SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - FOUND CORROSION AFT CARGO BAY, CORROSION ON FLOOR SUPPORT. REPLACED FLOOR SUPPORT, CUTTING OUT SECTIONS AND SPLICING IN NEW SECTION BS 727E PLUS 10 INCHES TO 727G PLUS 10 INCHES. (M) 2L72 4F RTA16WE 20050412003052005041200305NM 2005 4 12 ASAA0540158 120050303A532065C27308105 SUPPORT BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02791AS 28886 PAE - FOUND CORROSION ON SIDEWALL SUPPORT. REPLACED WITH NEW SIDEWALL SUPPORT. (M) 2L72 4F RTA16WE 20050412003062005041200306NM 2005 4 12 ASAA0540144 120050224A5311654654997 FRAME BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02791AS 28886 PAE - FOUND CORROSION AFT CARGO BAY ON FRAME BS 767 STRINGER 25R AND 27R FORWARD SIDE OF FRAME. REMOVED AND REPLACED FRAME. (M) 2L72 4F RTA16WE 20050412003072005041200307NM 2005 4 12 ASAA0540140 120050222A532065317875 SUPPORT BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02791AS 28886 PAE - FOUND CORROSION ON LT ENTRY DOOR CUTOUT BS 312, LBL 62, WL 208. LOWR FRAME INBOARD THRESHOLD SUPPORT HAS CORROSION. REPLACED SUPPORT. (M) 2L72 4F RTA16WE 20050412003082005041200308NM 2005 4 12 ASAA0540150 120050228A532065476903 SUPPORT BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02791AS 28886 PAE - FOUND CORROSION ON SIDEWALL SUPPORT PLATE, BS 837-947, LBL 22, WL 156. REMOVED AND REPLACED SIDEWALL SUPPORT PLATE. (M) 2L72 4F RTA16WE 20050412003092005041200309NM 2005 4 12 ASAA0540068 120050130A5320654175710 WEB BOEING737 7374Q8 138447QNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - FOUND DAMAGED FLOOR SUPPORT SHEAR WEB AT BS 500F-500G RBL 36 WL 152. REMOVED, FABRICATED AND INSTALLED NEW SHEAR WEB. (M) 2L72 4F RTA16WE 20050412003112005041200311EA 2005 4 12 ASOA05238 120050316A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27905EV 7632 DURING A C-CHECK IN MCN, THE FS 625 LT/RT CLIPS WERE FOUND TO BE CRAKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FS 625 LT/RT CLIPS. (M) 2L72 4F RTA21EA 20050412001202005041200120NM 2005 4 12 DHL2005782543 120050315A5532 SKIN BOEING727 727227 1384078NM VERTICAL STAB DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 REPLACE INTERIM REPAIR LOCATED ON THE RT VERTICAL STABILIZER BY REPLACING THE PANEL AFT OF THE REAR SPAR WITH A SERVICEABLE PANEL. REMOVED AND REPLACED VERTICAL STAB SKIN PANEL RT AFT OF THE REAR SPAR PN 6517561-234 PO NR 503010 IAW 727 SRM 51-30-2. 2L73 4F A3WE 20050412001222005041200122NM 2005 4 12 DHL2005782541 120050314A5754 SKIN BOEING727 727227 1384078NM NR 8 SLAT DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 DENT ON NR 8 SLAT EXTERNAL SKIN (MARKED). CUT OUT DAMAGE AREA SIZE 1 INCH BY 1 1/2 INCH IAW B727 SRM 57-50-1 FIG 2. FABRICATED DOUBLER REPAIR USING 2024 T3 .080 PO NR 90020125126 DIMENSIONS 6" BY 5" IAW B727 SRM 57-50-2 FIG 2 AND 57-50-3 FIG 1. ALODINE AND PRIMED PART AND AREA IAW B727 SRM 51-10-2. INSTALLED DOUBLER REPAIR IAW B727 SRM 57-50-2 FIG 2 AND 57-50-3 FIG 1. 2L73 4F A3WE 20050412001252005041200125WP 2005 4 12 05FDEA00827 120050404A5320 WEB DOUG DC10 DC1010 3022110WP FUSELAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25571FE 47830 DURING INSPECTION, FOUND AT STA 312 X=-45 WITH CORROSION ON THE WEB FLIGHT COMPARTMENT FLOOR LINE. REMOVED CORROSION PER SRM 51-21-01 PAGE 28 (WITHIN LIMITS). DURING CONTROL CORROSION FOR LIMITS, FOUND CRACK .50 INCH, CUT OUT DAMAGE IAW SRM 53-00-0. REPAIRED AREA IAW SRM 53-00-01 FIG 4 SHT 2. 2L73 4F A22WE 20050412001282005041200128NM 2005 4 12 05FDEA00824 120050404A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT UPPER CENTER SKIN PLANK NR 23R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82953. 2L73 4F RTA22WE 20050412001302005041200130NM 2005 4 12 05FDEA00822 120050404A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT UPPER FORWARD SKIN PLANK NR 15R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82953. 2L73 4F RTA22WE 20050412001322005041200132NM 2005 4 12 05FDEA00820 120050404A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT UPPER FORWARD SKIN PLANK NR 5R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82943. 2L73 4F RTA22WE 20050412001342005041200134NM 2005 4 12 05FDEA00816 120050404A5512 SKIN DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT UPPER CENTER SKIN PLANK NR 22L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82940. 2L73 4F RTA22WE 20050412001362005041200136NM 2005 4 12 05FDEA00814 120050404A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT UPPER CENTER SKIN PLANK NR 16L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82940. 2L73 4F RTA22WE 20050412001382005041200138NM 2005 4 12 05FDEA00812 120050404A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT HAND UPPER FORWARD SKIN PLANK NR 14L BARREL NUT BORE FOUND EXCEEDED LIMITS. REMOVED AND REPLACED IAW SRM 51-33-01, VOL II. 2L73 4F RTA22WE 20050412001402005041200140NM 2005 4 12 05FDEA00809 120050404A3210 TRUNNION DOUG MD11 MD11 3023602NM ZONE 700 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25583FE 48421 CENTER LANDING GEAR, LT TRUNNION SUPPORT FITTING MATING SURFACE FOUND CORRODED AND EXCEED LIMIT AREA OF 10 PERCENT PER SRM 53-40-00 FIGURE 15, SHEET 4, (FOR LOCAL BLEND OPTIONS) AEA7051-501. REPAIRED IAW FEDEX EA 1-5340-82950. 2L73 4F RTA22WE 20050412001422005041200142NM 2005 4 12 05FDEA00805 120050404A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LEFT WING STRINGER 11 END SUSPECTED CRACKED ARB7514-1. REPAIR CARRIED OUT IAW SRM 57-20-00 VOLUME I, FIGURE 10 AND FEDEX EA 1-5710-83090. 2L73 4F RTA22WE 20050412001442005041200144NM 2005 4 12 05FDEA00803 120050404A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RIGHT HAND WING STRINGER 10 END SUSPECTED CRACKED ARB7510-2. REPAIR CARRIED OUT IAW SRM 57-20-00 VOLUME I, FIGURE 10 AND FEDEX EA 1-5710-83090. 2L73 4F RTA22WE 20050412001462005041200146WP 2005 4 12 05FDEA00801 120050401A3213 STRUT DOUG DC10 DC1030 3023501WP MLG DAMAGED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25316FE 48314 ON TAKEOFF FROM MEM, CENTER GEAR INDICATED UNSAFE UP. BOTH DISPLAYS SHOWED UNSAFE UP. COMPLIED WITH ALL CHECKLISTS AND LANDED KMEM 36C. REMOVED CENTER LANDING GEAR SHOCK STRUT, PER FEDEX WORK CARD 32T7101. REMOVED THE CTR LDG AFT W/W LT AND RT GEAR DOORS IN REF TO THE MD-10-30 M/M 32-14-04-2. CLG INST IS HANDLED ON WORKCARD 32T7701 AND IS C/W UP TO AND INCLUDING STEP 8J.COMPLETED FEDEX WORKCARD 32T7701 CENTER LANDING GEAR SHOCK STRUT INST.ALL STEPS COMPLETED ALL OPS CHECKS AND LEAK CHECKS O.K. PER WORKCARD. 2L73 4F A22WE 20050412001482005041200148NM 2005 4 12 05FDEA00798 120050402A5320AEA0526U2 DOUBLER DOUG MD11 MD11 3023602NM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 FOUND WELL INTERIOR FWD RT SIDE WEB WITH DOUBLER CUT OUT. CRACKED AT LOWER FASTENERS HOLE LOCATION AS MARKED. REMOVED AND REPLACED IAW SRM 51-33-01 VOLUME II. 2L73 4F RTA22WE 20050412001542005041200154NM 2005 4 12 05FDEA00792 120050401A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZ STAB RT UPPER CENTER SKIN PLANK NR 24R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82953. 2L73 4F RTA22WE 20050412001562005041200156NM 2005 4 12 05FDEA00790 120050401A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZ STAB RT UPPER CENTER SKIN PLANK NR 20R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82953. 2L73 4F RTA22WE 20050412001582005041200158NM 2005 4 12 05FDEA00787 120050401A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZ STAB LT UPPER AFT SKIN PLANK NR 35L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82941. 2L73 4F RTA22WE 20050412001602005041200160NM 2005 4 12 05FDEA00785 120050401A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZ STAB LT UPPER AFT SKIN PLANK NR 31L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82941. 2L73 4F RTA22WE 20050412002302005041200230WP 2005 4 12 GTIA050057 120050217A5313 LONGERON DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 LONGERON 28R STA 1140 HAS CORROSION AROUND FASTENERS THROUGH SKIN IN AFT PIT. REMOVED FASTENERS THROUGH SKIN AND REMOVED CORROSION. LONGERON 28R AT STA 1140 IS OUT OF LIMITS. LOCATED AND DRILLED FABED LONG SECTION AND SPLICE. TREAT AND PRIMED, INSTALLED LONG. SECTION AND REPAIR SPLICE 28R IAW 51-30-5. (K) 2L72 4F4 F A6WE E9NE 20050412002322005041200232WP 2005 4 12 GTIA050053 120050219A5330 SKIN DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE FUSELAGE DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 DENT AT FS 245, LONGERON 18L (D=1.250 INCH, X=0.054 D/X=23.14). REMOVED AIRCRAFT SKIN AT STA FS 245, LONGERON 18L (20 INCHES X 14 INCHES). FABRICATED REPAIR PARTS IAW SRM. INSTALLED, REPAIR AT FS STA 245 LONGERON 18L. (K) 2L72 4F4 F A6WE E9NE 20050412002572005041200257NE 2005 4 12 GTIA050040 220050225A7200 ENGINE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE NR 1 MALFUNCTIONED A GTIAK NONE O OTHER TXTAXI/GRND HDL 1 GL23834NK 49847 NR 1 ENGINE SLOW TO SPOOL, TAIL SWAP WITH AIRCRAFT 810. REMOVED AND REPLACED NR 1 ENGINE. (K) 2L72 4F4 FRTA6WE E9NE 20050412002592005041200259WP 2005 4 12 GTIA050048 120050216A5320 ANGLE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 DOOR FRAME TO SKIN CORNER ANGLES STA 1155 AND 1212 AT DOOR JAMB BEAM ARE CORRODED IN AFT PIT. REMOVED CORROSION ON DOOR FRAME TO SKIN CORNER ANGLES AND DOOR JAMB. MATERIAL LOSS OUT OF LIMITS. DRILLED AND LOCATED NEW ANGLE, TREATED, PRIMED AND INSTALLED NEW ANGLE. (K) 2L72 4F4 F A6WE E9NE 20050412002712005041200271NM 2005 4 12 ASAA0540139 120050222A5347655384416 CARGO TRACK BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02791AS 28886 PAE - FOUND CORROSION ON TIE DOWN TRACK. REMOVED AND REPLACED. (M) 2L72 4F RTA16WE 20050412002752005041200275NM 2005 4 12 ASAA0540135 120050219A5320654769013 SUPPORT BOEING737 737490 1384715NM CARGO BAY CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02791AS 28886 PAE - FOUND CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT, BLENDED OUT OF LIMITS. REPLACED WITH NEW PART. (M) 2L72 4F RTA16WE 20050412002812005041200281NM 2005 4 12 ASAA0540148 120050225A53206520726037 SUPPORT BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02791AS 28886 PAE - FOUND CORROSION ON SIDEWALL SUPPORT PLATE, BS 500 PLUS 6 INCHES, WL 156, RBL 25. REMOVED AND REPLACED SIDEWALL SUPPORT PLATE. (M) 2L72 4F RTA16WE 20050412002822005041200282NM 2005 4 12 ASAA0540147 120050225A532069434961 SUPPORT BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02791AS 28886 PAE - FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT BS 847-867. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT. (M) 2L72 4F RTA16WE 20050412002882005041200288NM 2005 4 12 ASAA0540051 120050125A5320657374337 SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - FOUND FORWARD CARGO BAY 1 INCH CRACK ON FLOOR TO SIDEWALL SUPPORT BS 500B RBL 23 WL 156. FLOOR-TO-SIDEWALL SUPPORT TO BE REPLACED ON CARD 478974 BECAUSE OF ADDITIONAL OUT OF LIMITS DISCREPANCIES. (M) 2L72 4F RTA16WE 20050412002892005041200289NM 2005 4 12 ASAA0540052 120050125A5320657374337 SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - FOUND FORWARD CARGO BAY AREAS OF CORROSION ON FLOOR TO SIDEWALL SUPPORT AT BS 500D PLUS 10 INCHES TO 500G RBL 23 WL 156. FLOOR TO SIDEWALL SUPPORT OUT OF LIMITS THROUGHOUT ENTIRE LENGTH, TO BE REPLACED ON 4878974. (M) 2L72 4F RTA16WE 20050412002952005041200295NM 2005 4 12 ASAA0540066 120050201A5320652072619 SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - FORWARD CARGO BAY, AREAS OF CORROSION ON FLOOR TO SIDEWALL SUPPORT BS 420 TO 440 RBL 23, WL 156. REMOVED AND REPLACED PER 53-30-15, 51-40-02. (M) 2L72 4F RTA16WE 20050412003012005041200301NM 2005 4 12 ASAA0540054 120050125A532065452965 RETAINER BOEING737 7374Q8 138447QNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - AFT CARGO BAY TO FLOOR TO SIDEWALL SUPPORT, HAS EXTRA HOLE IN RETAINER STRIP. REMOVED DAMAGED PART, FABRICATED NEW RETAINER STRIP USING 2024-T3 .063 LOT NR 593315. (M) 2L72 4F RTA16WE 20050413000012005041300001EU 2005 4 13 ASOA05181 120050204A5311S53671311242 FRAME AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27633AS 344 DURING A C-CHECK IN YUL, THE FRAME 37 RT, STRINGER 14 ON THE AFT SIDE WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE FRAME 37 RT, STRINGER 14 IAW ASA EO 72-53-0162. (M) 2H72 4T RTA53EU 20050413000072005041300007EA 2005 4 13 ASOA05176 120050302A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27880AS 7606 DURING A C-CHECK IN MCN, THE LEFT INBOARD FS 280 CLIP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT INBOARD FS 280 CLIP IAW SRM 51-42-06. (M) 2L72 4F RTA21EA 20050413000262005041300026EA 2005 4 13 ASOA05175 120050302A5320 SUPPORT ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27880AS 7606 DURING A C-CHEC IN MCN, THE FLOOR SUPPORT ANGLES AT FS 621 LT/RT WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FLOOR SUPPORT ANGLES AT FS 621 LT/RT IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20050413000292005041300029EA 2005 4 13 2005F00058 120050228A3350BR9279106 LENS CNDAIRCL600 CL6002B19 1900309EA CABIN CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27880AS 7606 DURING A -CHECK IN MCN, THE EMERGENCY EXIT LIGHT BASE AND LENS BY THE SERVICE DOOR WERE FOUND TO BE CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE EMERGENCY EXIT LIGHT ASSEMBY BY THE SERVICE DOOR. (M) 2L72 4F RTA21EA 20050413000372005041300037EA 2005 4 13 ASOA05243 120050317A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27905EV 7632 DURING A C-CHECK IN MCN, THE FS 280 RIGHT CLIPS INBOARD AND OUTBOARD AT RBL 9 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FS 280 RT CLIPS INBOARD AND OUTBOARD AT RBL. (M) 2L72 4F RTA21EA 20050413000412005041300041EA 2005 4 13 ASOA05237 120050316A5320 SUPPORT ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27905EV 7632 DURING A C-CHECK IN MCN, THE FLOOR SUPPORT ANGLE AT FS 621 WAS FOUND TO BE CRACKED ON THE LEFT AND RIGHT CORNERS BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FLOOR SUPPORT ANGLE AT FS 621 IAW WITH ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20050413000422005041300042EA 2005 4 13 ASOA05227 120050312A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA EXTERIOR INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27866AS 7517 DURING AN A-CHECK IN BTR, THE AFT EXTERIOR EMERGENCY LIGHT ON THE LEFT SIDE WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE AFT EXTERIOR EMERGENCY LIGHT ON THE LEFT SIDE. OPERATIONAL CHECKS GOOD. (M) 2L72 4F RTA21EA 20050413000432005041300043EA 2005 4 13 ASOA05235 120050315A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27925EV 7831 DURING A C-CHECK IN MCN, THE RIGHT OUTBOARD FS 280 CLIP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE RIGHT OUTBOARD FS 280 CLIP. (M) 2L72 4F RTA21EA 20050413000462005041300046EU 2005 4 13 ASOA05231 120050313A33507012210 LIGHT AEROSPATR72 ATR72212 8680945EU CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27633AS 344 DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY LIGHT ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20050413000562005041300056EU 2005 4 13 ASOA05220 120050309A3350 LIGHT AEROSPATR72 ATR72 EU CABIN MALFUNCTIONED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27631AS 362 FLT 4708 - DURING A GROUND INSPECTION IN ATL, THE RIGHT FORWARD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE OPERATED THE EMERGENCY LIGHT ARM SWITCH SEVERAL TIMES WITH THE RIGHT FORWARD EMERGENCY EXIT LIGHT ILLUMINATING PROPERLY DURING EACH TEST. NO DEFECTS WERE NOTED. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20050413000682005041300068SO 2005 4 13 SIMA200507502 120050313A5610163500112 WINDSHIELD EMB 135 EMB135KL 3260302SO COCKPIT MALFUNCTIONED A SIMAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SW21825AE 145589 ON APPROACH, ENTERED ICING AND THEN NOTED SMOKE COMING UP BETWEEN THE TWO FORWARD WINDSHIELDS WHEN THE AI SYSTEM CAME ON. CREW DECLARED AN EMERGENCY AND AIRCRAFT WAS LANDED SAFELY WITH NO INCIDENTS REPORTED. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS WINDSHIELD AND CABLE TERMINAL END IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050413000822005041300082SO 2005 4 13 SIMA200507904 120050318A34110856NF PITOT TUBE EMB 135 EMB135LR 3260305SO RIGHT MALFUNCTIONED A SIMAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 SW21717AE 145272 ABI - FLT 9806 - CREW REPORTED THE STANDBY ALTIMETER OFF BY 200 FEET FROM PRIMARY AT 10,000 FEET AND BACKLIGHTING ON THE THRUST RATING PANEL IS BLINKING ON AND OFF. AIRCRAFT RETURNED TO ABI AND LANDED SAFELY WITH NO FURTHER INCIDENTS REPORTED. MAINTENANCE REMOVED AND REPLACED THE RIGHT PTITO TUBE IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050414000012005041400001NM 2005 4 14 UPS05444200 120050312A5730 PANEL BOEING747 747121 1384871NM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 RT WING L/E CAVITY AT FSSI 998 L/E MOST FWD D-SECTION ATT PANEL AND UPPER EDGE CHORD FOUND CRACKED, AFT OF NR 20 VC FLAP, CRACK LENGTH 1 INCH. PANELS AND CHORD REPAIRED AS PER SRM 57-20-03 FIG 7. 2L74 4F A20WE 20050414000052005041400005NM 2005 4 14 UPS05444204 120050310A5330 SKIN BOEING747 747121 1384871NM EMPENNAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 TAIL FUSELAGE STA 2685 - 2705 WL 297 TO WL 334 LT MIDDLE AREA FOUND SKIN CRACKED, CRACK LENGTH 2.5 INCH. SKIN REPAIRED AS PER SRM 53-30-03 FIG 1A. 2L74 4F A20WE 20050414000102005041400010WP 2005 4 14 UPS05844243 120050321A57404653423U FITTING DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE:C2 RT WING FLAP WELL STA 230 UPPER AREA HAS CRACKED WEB TO INTERCOSTAL ATTACH FITTING. REMOVED AND REPLACED ATTACH FITTING IAW DC-8 SRM 51-1-21D. 2L74 4F RT4A25 20050414000142005041400014WP 2005 4 14 UPS05844248 120050319A5712 RIB DOUG DC8 DC873F 302199FWP LH LE STA CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE: C2, LT L/E UPPER RIB CRACKED .25 INCH LONG AT STA 782. REPAIRED LEFT L/E UPPER RIB IAW DC-8 SRM 57-2-0 FIG 2 AND SRM 51-1-20D. 2L74 4F RT4A25 20050414000242005041400024WP 2005 4 14 UPS05844262 120050319A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE: C2, EXTERIOR FUSELAGE LT APPROX. STA 1735 LONGERON 16 HAS ONE SMALL CRACK ( APPROX. .25" ) EXTENDING FROM FASTENER. REPAIRED CRACK IAW DC-8 SRM 53-2-1, 51-1-26, 51-1-21, & 51-1-20D. 2L74 4F RT4A25 20050414000272005041400027WP 2005 4 14 UPS05844265 120050319A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE: C2, LONGERON 15R IS CRACKED AT F/S 1730 & F/S 1750 AT CANTED FRAMES. REMOVED AND REPLACED LONGERON SECTION IAW DC-8 SRM53-2-2 FIG. 10, 51-1 -21, & 51-1-20D. 2L74 4F RT4A25 20050414000282005041400028EU 2005 4 14 UPS05844270 220050412A7200 ENGINE DOUG DC8 DC873F 302199FWP CFMINTCFM56 CFM563C 13802EU NR 4 FLAMED OUT A IPXAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 SO01809UP 46109 NR 4 ENGINE FLAME OUT IN CRUISE FLT ENROUTE TO PHL. RESTART UNSUCCESSFUL. FUEL PRESSURE ON S/O PANEL DROPPED FROM 35 PSI TO 20 OIL TEMP & QTY NORMAL OIL PRESS DROPPED TO 18 PSI AFTER FLAMEOUT. R&R NR 4 ENGINE, MAIN ENGINE CONTROL (MEC) IAW MM 73-20-01-4. PERFORMED MEC ADJ AND TEST IAW 73-30-01-5. LEAK CK AND ENG RUN CHECK GOOD. (CLOSED) 2L74 4F4 FRT4A25 E21EU 20050414000372005041400037NM 2005 4 14 ASMF200502007 120050207A7400 IGNITION UNIT BOEING737 73776N 13844CHNM LT ENGINE FAILED W ASMFD RETURN TO BLOCK HJ ELECT. POWER LOSS-50 PC WARNING INDICATION TXTAXI/GRND HDL 1 SW23997AM 30283 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF RIGHT IGNITION SYSTEM FAILED IN LEFT ENGINE. DURING MAINTENANCE REVISION, THE C485 BREAKER LOCATED AT THE P18-2 A1 PANEL WAS THROWN AWAY. THE C485 BREAKER WAS REPOSITIONED IAW MM 74-00-00, TESTED CORRECT. 2L72 4F RTA16WE 20050414000482005041400048 2005 4 14 ASMF200504004 420050408A34189650449002 COMPUTER DOUG MD80 MD83 3023681NM STALL WARNING FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23861LF13797 49826 DURING TRANSIT CHECK, THE STALL SYSTEM TEST WAS INOPERATIVE. DURING REVISION WAS DETECTED SIF LIGHT AT ANNOUNCED PANEL AND STALL WARNING IN COMPUTER NUMBER 1. THE STALL WARNING COMPUTER NUMBER 1 WAS REPLACED IAW MM 34-19-02, TESTED CORRECT. LATER, AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING TAXING APPEARED THE SAME FAILURE. AIRCRAFT WAS SENT TO THE HANGAR AND RELAY R2-58 WAS REPLACED IAW WDM 34-11-00 AND FLAP POSITION TRANSMITTER WAS REPLACED IAW MM 27-54-01, TESTED CORRECT. 2L72 4F RT 20050414000862005041400086NM 2005 4 14 2005UALA00069 120050117A5313 STRINGER BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29905UA 25005 STR 16 RT HAS A CRACK AT STA 498B JUST AFT OF LIGHT ASSY. SUPPLEMENTAL DATA UPDATE, MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SECTION FROM STRINGER AND INSTALLED SPLICE REPAIR. 2L72 4F4 FRTA16WE E2GL 20050414000882005041400088 2005 4 14 2005UALA00071 420050115A256120131 BATTERY BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE LIFE VEST INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29672UA 30027 SQUIB TEST 1 LEFT INOP. REPLACED BATTERY AND CHECKS OK. 2L72 4F4 FRTA1NM E24NE 20050414000922005041400092NM 2005 4 14 2005UALA00075 120050119A5315 FLOORBEAM BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29905UA 25005 STA 294 FLOORBEAM UPPER CAP HAS MATERIAL LOSS FROM CORROSION REMOVAL AT RBL 39 TO RBL 52. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. CUTOUT DAMAGED SECTION AND INSTALLED DOUBLE FLANGE REPAIR. 2L72 4F4 FRTA16WE E2GL 20050414000932005041400093NM 2005 4 14 2005UALA00076 120050119A5312 PRESSURE PANEL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29302UA 23643 STA 664 PRESSURE DECK HAS 2 CRACKS AT LBL 30. CUT-OUT WEB AND INSTALLED SPLICE REPAIR. 2L72 4F4 FRTA16WE E2GL 20050414000952005041400095NM 2005 4 14 05FDEA00176 120050126A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25235FE 21329 FRAME HAS TWO DENTS WITHIN 10 INCHES OF EACH OTHER BS 1110 BELOW STR 25R AND AT STR 26R. REPAIRED PER SRM 53-40-2 2L73 4F RTA3WE 20050414000962005041400096NM 2005 4 14 05FDEA00177 120050126A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25235FE 21329 DENT IN FRAME BS 1070 JUST BELOW STR 25R. REPAIRED PER SRM 53-10-2 2L73 4F RTA3WE 20050414000982005041400098WP 2005 4 14 DXTA200500573 220050202A7261 SEAL CESSNA650 650 2076802CE GARRTTTFE731TFE7314R 01518WP ENGINE LEAKING E DXTAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 GL07797QS 6507097 P102308 LEFT ENGINE OIL PRESS LOW ANNUNCIATOR CAME ON DURING DESCENT. OIL PRESSURE GAUGE WAS FLUCTUATING BETWEEN 25 - 40 PSI. AFTER LANDING, ENGINE HAD NO OIL LEFT IN IT. ENG INSPECTED & RESERVICED WITH OIL & CHECKED CHIP DETECTOR ALL GROUND RUN NO DEFECTS, ALL GEARBOX SUMP PRESSURE CHECKS IAW 731-9R CMM ALL OK. REPAIRED ACCY GEARBOX LEAK BY REPLACING FWD 3 EA CARBON & GARLOC SEALS. REPLACED WORN HYD PUMP DRIVE GEARSHAFT IN ACCY GEARBOX IAW 731-4R M/M & GARRETT MM. 2L72 4F4 F A9NM E6WE 20050414000992005041400099CE 2005 4 14 DXTA200500574 120050202A3260602751 PROXIMITY SWITCH CESSNA750 750 2076810CE MLG MALFUNCTIONED E DXTAO OTHER J WARNING INDICATION APAPPROACH 1 GL07958QS 7500158 LEFT MAIN LANDING GEAR DID NOT EXTEND NORMALLY. USED MANUAL BLOW DOWN PER CHECKLIST TO EXTEND LT MAIN. FOUND LT MLG GEAR DOWN LOCK SWITCH HAD ERRONEOUS RESISTANCE VALVE WHEN SWITCH IS FROZEN, 0.0 TO 5.8 OHM. REMOVED LT MLG GEAR DOWN LOCK SWITCH, AND INSTALLED A NEW SWITCH OF SAME P/N. PERFORMED LANDING GEAR FUNCTIONAL TEST. OPS TEST CHECKS GOOD. ALL WORK ACCOMPLISHED IAW CE-750 MM CHAPTER 32-00-01. 2L72 4J RTT00007WI 20050414001012005041400101NM 2005 4 14 05FDEA00022 120050105A7830683L221G04 THRUST REVERSER DOUG MD11 MD11 3023602NM ZONE 400 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25605FE 48514 NR 3 ENGINE, RT THRUST REVERSER, TRANSLATING COWL, UPPER TRACK, MOST AFT END FOUND WITH CRACKED. THRUST REVERSER P/N 683L221G04, S/N R592-084. NR 3 ENGINE, RT THRUST REVERSER REMOVED AND REPLACED PER AMM 78-33-01-4. THRUST REVERSER DOOR ADJUSTMENT AND CHECK PER AMM 78-33-01-700-807. FUCTIONAL TEST CARRIED OUT PER AMM 78-30-00-700-801. COMPLIED WITH ROUTINE WORKCARD NOS.: 78T3003-R AND 78T3903-R 2L73 4F RTA22WE 20050414001092005041400109NE 2005 4 14 05003 220050107A7210 GEARBOX BOEING747 7472B4B 138481BNM PWA JT9 JT9D7J 52054NE NR 4 ENGINE DAMAGED A KCSAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL23710CK45453 21097 662495 NR 4 ENG SLOW/STEADY OIL LEAK FROM 5.6 GALS DOWN TO 0.6 GALS. OIL TEMP CONSTANT AT 75 TO 79C AND OIL PRESS STEADY AT 47 TO 49 PSI. ACCOMPLISHED PRECAUTIONARY ENG SHUTDOWN IAW AOM VOL I, LOW OIL QTY PG 3-109, IN FLT ENG SHUTDOWN PG 3-97 AND WINDMILLING ENG PROCEDURES PG 3-114. ENG RESTARTED IAW IN-FLIGHT START PROCEDURES P 3-98 FOR NORMAL DESCENT, APPROACH AND LANDING. REMOVED AND REPLACED MAIN GEARBOX IAW P/W E/M 72-00-00. ENGINE TEST RUN PERFORMED IAW P/W E/M 72-00-00, TESTING 02. NO OIL USAGE NOTED AT THIS TIME. 2L74 4F4 FRTA20WE E20EA 20050414001102005041400110CE 2005 4 14 200501309 120050124A5310612826 RACK CESSNA172 172RG 2072438CE LYC O360 O360* 41514EA FUSELAGE TORN B HJBRK NONE O OTHER ININSP/MAINT 1 AL056407V 172RG0669 FOUND TRAY HAD STRESS TEARS IN THE CORNERS OF THE THUMBSCREW CUTOUT AT THE BEND RADII FOLLOWING INSPECTION IAW SIL-012. 1H71 3O3 O 3A17 E286 20050414001172005041400117 2005 4 14 TXER099080 420050115A2562S182150202 ELT UROCOPEC155 EC155B 8681000EU CABIN WILL NOT TEST B TXERO OTHER O OTHER NRNOT REPORTED 1 SW99588CF 6662 ELT FAILS TEST MODE. 1G72 3U H10EU 20050414001192005041400119 2005 4 14 TXER099082 420050101A3120B1894532281AG CLOCK UROCOPEC155 EC155B 8681000EU COCKPIT INOPERATIVE B TXERO OTHER O OTHER NRNOT REPORTED 1 SW09588CF 6662 CLOCK INOP. 1G72 3U H10EU 20050414001232005041400123NM 2005 4 14 S05432042 120050122A323365B015709 ACTUATOR BOEING747 747400 NM PWA 4056 PW4056 NE RT MLG DAMAGED W SAJFK NONE O OTHER ININSP/MAINT 1 WP03 36975 28709 9A CHECK FOUND RT WING GEAR RETRACT ACTUATOR ROD END SLEEVE WORN OUT. ROD END BEARING SLEEVE WORN OUT. ACTUATOR REPLACED AND FUNCTION TEST NORMAL. IAW 744 AMM 32-32-01 P.407 AND IPC 32-11-01 FIG.1. WASHERS AND SPACERS SHOULD BE INSTALLED ON BOTH SIDE OF ROD END. SHORT INSTALLATION OF SPACERS AND WASHERS WILL LEAD TO DISLOCATION BETWEEN BEARING AND ROD END. ROOT CAUSE OF THIS EVENT IS ATTRIBUTED TO "NOT COMPLY WITH MANUAL" 2L74 4F4 FRTA20WE E24NE 20050415000432005041500043WP 2005 4 15 WX0500012 120050131A3350 BULB DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A WX0AK NONE O OTHER ININSP/MAINT 1 WP19891GA 49423 LAS - MAINTENANCE REPORTED OVERHEAD EMERGENCY LIGHT BETWEEN SEAT ROW 26 INOPERATIVE. MAINTENANCE REPLACED BULB IN OVERHEAD EMERGENCY LIGHT BETWEEN SEAT ROW 26. SYSTEM OPERATIONALLY CHECKED GOOD IAW MM 33-53-01. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050415000462005041500046NM 2005 4 15 C8GA20050005 120050203A3297 WIRE BOEING727 727223 1384074NM NLG POS SWITCH BROKEN A C8GAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO15715AA56632 22470 FLT 202 FROM SDQ TO MIA, ON APPROACH TO MIA, WITH GEAR EXTENDED, NOSE GEAR RED WARNING LIGHT ILLUMINATED WITH NO GREEN OR AURAL WARNING. RECYCLED GEAR NO HELP. EXECUTED MISSED APPROACH AND COMPLETED ABNORMAL CHECKLIST. F/E VISUALLY CONFIRMED NOSE GEAR DOWN AND LOCKED WITH CONFIRMATION FROM TOWER THAT ALL GEAR WERE DOWN AND VISIBLE. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND BROKEN WIRE AT NOSE GEAR POSITION SWITCH. REPAIRED WIRE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE 2L73 4F A3WE 20050415000472005041500047NM 2005 4 15 WRLA2005008 120050201A5753 SKIN DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE FLAP VANE DAMAGED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11273 48519 ITEM: DURING "C2" CHECK IN TPE, FOUND RIGHT WING INBD FLAP VANE SKIN DISBAND. CUT OUT DAMAGED SKIN AREA WITH 0.5" MIN RADIUS PER MD11 SRM 57-90-00 VOL I AND FAA FORM 8100-9 DATED 01/27/05. ACCOMPLISHED CO-CURE REPAIR USING FM300-2 AT 250DEG "F" FOR 90 TO 100 MINUTES. CONDITION CHECK SATISFACTORY. 2L73 4F4 FRTA22WE E24NE 20050415000482005041500048NM 2005 4 15 C8GA20050006 120050203A2910BACH8C06NN0237T LINE BOEING727 7272A1 138407FNM HYDRAULIC SYS RUPTURED A C8GAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO15287SC53662 21345 FLT 721 FROM FLL TO RDU, AFTER TAKEOFF, BOTH "A" HYDRAULIC PRESSURE LOW LIGHTS ILLUMINATED FOLLOWED BY LOSS OF SYSTEM PRESSURE AND QUANTITY. AIRCRAFT RETURNED TO FLL AND LANDED WITHOUT FURTHER INCIDENT. FOUND RUPTURED FLEXIBLE HYDRAULIC LINE TO NOSE GEAR ACTUATOR. REPLACED LINE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L73 4F A3WE 20050415000522005041500052NM 2005 4 15 DL75K050071 120050201A2910 LINE BOEING757 757232 1384965NM HYD SYSTEM LEAKING A DALAC ABORTED TAKEOFF KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO27644DL UNK 23998 AIR TURN BACK RT GEAR WOULD NOT RETRACT AFTER TAKEOFF. REPLACED HYDRAULIC LINE TO TRUCK POSITION ACTUATOR. 2L72 4F RTA2NM 20050415000542005041500054NM 2005 4 15 DL75A050077 120050201A5330143N31311 SKIN BOEING757 757212 1384951NM FUSELAGE TOOL DAMAGE A DALAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO27752AT 23128 TOOLING DAMAGE TO THE FUSELAGE SKIN AT STATION 631 AND STR 4L. 2L72 4F RTA2NM 20050415000552005041500055NM 2005 4 15 DLM88050078 120050202A8000809101012 B-NUT DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 ENGINE CRACKED A DALAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO27980DL 53267 718217 RT START VALVE WOULD NOT OPEN. REPLACED START DUCT AND SECURED LOOSE B-NUT. 2L72 4F4 FRTA6WE E9NE 20050415000562005041500056NE 2005 4 15 DLM88050079 220050202A731438430110 SHAFT DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 FUEL PUMP SHEARED A DALAE ENGINE SHUTDOWN XJ ENGINE FLAMEOUT WARNING INDICATION DEDESCENT 1 SO27926DL32912 725812 49713 725812 STARTING DOWN AT FL230, AROUND FL210 RT ENG FAILED GOOD HYD PRESS/OIL PRESS C/W ENG FAILURE W/QRH DURING FAILURE POWER WAS 55-60 N1 DUE TO 1 A/C PACK, APPROX TIME OF SHUTDOWN 2345Z LANDING AT 0009Z. REPLACED RIGHT ENGINE FUEL CONTROL AND PUMP. FUEL PUMP SHAFT SHEARED. 2L72 4F4 FRTA6WE E9NE 20050415000572005041500057NM 2005 4 15 DL767050080 120050203A2910 LINE BOEING767 767232 1385132NM RT ENGINE LEAKING A DALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO27102DA 22214 RT HYD SYS FAILURE. RT HYD SYS QTY DROPPED QUICKLY SUGGESTING A LEAK. FOUND RT ENGINE PRESSURE LINE CHAFED THROUGH, REPLACED SAME. 2L72 4F RTA1NM 20050415000582005041500058NM 2005 4 15 DLM88050081 120050201A533029525581 SKIN DOUG MD88 MD88 3023688NM FUSLAGE GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27911DE 49967 FUSELAGE SKIN DENTED AND GOUGED AT STATION 646 AND LONGERON 30. REPAIRED IAW ERA 096160-14. 2L72 4F RTA6WE 20050415000592005041500059NM 2005 4 15 DLM88050082 120050202A5311992340614 FRAME DOUG MD88 MD88 3023688NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27912DL 49543 FUSELAGE OVERWING FRAME AT STATION 886 FOUND CRACKED AT LONGERON 18L. FRAME REPLACED I/A/W ERA 096171-14. 2L72 4F RTA6WE 20050415000612005041500061 2005 4 15 DL76S050087 420050205A2330250008632 PROJECTOR BOEING767 767332 1382001NM NR 3 FAILED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27129DL 24079 PROJECTOR AT SCREEN 3 FAILED ACCOMPANIED WITH ELECTRICAL ODOR. SHUT OFF SYSTEM PULLED C/B T8 ON OVERHEAD, ODOR DISSIPATED. REPLACED PROJECTOR. 2L72 4F RTA1NM 20050415000652005041500065NM 2005 4 15 WRLA2005012 120050131A5347 SEAT TRACK DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11273 48519 DURING "C2" CHECK, FOUND SEAT TRACK CORROSION BETWEEN STA 1371 AND STA 1521 X=-75.25. CUTOUT AND REMOVED CORRODED SECTION BETWEEN STA 1371 AND 1531 X=-75.25, FABRICATED AND INSTALLED NEW SEAT TRACK SECTION AND SPLICE HAT. CONDITION CHECK SATISFACTORY REF MD11 SRM 53-70-00 FIG REV 36 VOL I. 2L73 4F4 FRTA22WE E24NE 20050415000712005041500071NM 2005 4 15 WRLA2005017 120050201A5330 SKIN DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11273 48519 ITEM: DURING "C2" CHECK INSPECTION, FOUND CORROSION AT BARREL NUT HOLE NR 36 RT. CLEANED CORROSION AND OVERSIZED BARREL NUT HOLE TO 2.587" DIA, PER SECTION 7 OF E/O 02-5510-098 REV 03 AND FABRICATED REPAIR BUSHING PER SECTION 12 OF SAME E/O. CLEANED AND REINSPECTED BOLT AND BARREL NUT, REINSTALLED BARREL NUT WITH NEW PL1 WASHER. CONDITION CHECK SATISFACTORY. 2L73 4F4 FRTA22WE E24NE 20050415000722005041500072NM 2005 4 15 WRLA2005018 120050131A5347 SEAT TRACK DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11273 48519 DURING "C2" CHECK, FOUND CABIN SEAT TRACK CORROSION BETWEEN STA 858 AND STA 873 X=27.5. CUT AND REMOVED CORRODED SECTION BETWEEN STA 816 AND 909 X=75.25, FABRICATED AND INSTALLED NEW SEAT TRACK SECTION AND SPLICE HAT. CONDITION CHECK SATISFACTORY REF MD11 SRM 53-70-00 FIG 1 REV 36 VOL I. 2L73 4F4 FRTA22WE E24NE 20050415000762005041500076EA 2005 4 15 HNAA0500008 120050208A2797 PIN DHAV DHC8 DHC8311 1386006EA CONNECTOR DAMAGED A HNAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA07335EX 375 OUTBD ROLL SPLR CAUTION LIGHT ILLUMINATED ON T/O LIGHT WENT OUT ON TOUCH DOWN. MX DUPLICATED PROBLEM ON GROUND USING PITOT PRESSURE. FOUND PIN A ON C/P 9811-J31, NOT SEATED PROPERLY IN PLUG. REMOVED AND REPLACED PIN A. OPS CHECK GOOD. CND AFTER REPINNING. 2H72 4T RTA13NM 20050415000782005041500078EU 2005 4 15 EGRA2005211 120050210A3310 PANEL BOLKMS117 BK117A3 5626015EU LYC LTS101LTS101650C2 41560NE COCKPIT FIRE E EGRAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA17135CP S7014 PILOT REPORTED MOMENTARY SMOKE, SPARKS, AND POSSIBLE FLAMES IN OVERHEAD CIRCUIT BREAKER PANEL. CIRCUIT BREAKER FOR PILOT INSTRUMENT LIGHTS POPPED AND SMOKE AND SPARKS STOPPED. THIS OCCURRED BETWEEN LOM (WINGS FIELD) AND NO2 (KEYSTONE HELIPORT). NO PATIENT ONBOARD. FLIGHT CONTINUED TO ORIGINAL DESTINATION. NO CAUSE IDENTIFIED AT THIS TIME. 1G72 3U3 U H13EU E5NE 20050415000802005041500080NM 2005 4 15 WRLA2005021 120050202A5313 LONGERON DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "4C" CHECK FOUND CORROSION IN CENTER CARGO LONGERON AT STA 5-120 L44R. 2L73 4F4 FRTA22WE E24NE 20050415000812005041500081NM 2005 4 15 WRLA2005022 120050202A5313 LONGERON DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "4C" CHECK FOUND CORROSION IN CENTER CARGO LONGERON AT STA 5-120 L45R. 2L73 4F4 FRTA22WE E24NE 20050415000822005041500082NM 2005 4 15 WRLA2005023 120050202A5343 SUPPORT FITTING DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE MLG WW CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "4C" CHECK, FOUND CORROSION IN CENTER L/G W/W LT TRUNNION SUPPORT FITTING BOOT STRAP AT STA Y=1471. 2L73 4F4 FRTA22WE E24NE 20050415000832005041500083 2005 4 15 VW3R20050003 420050208A2565D29601103 GIRT BAR AIRCRUISERS AIRBUS330 A300* EU ESCAPE SLIDE DEFECTIVE B VW3RK NONE W INADEQUATE Q C ININSP/MAINT 1 WP09ALL 0430 ALL GIRT EXTENSION DOES NOT FIT PROPERLY ON GIRT BAR. GIRT EXTENSION PADS RIDE UP ON CAVITY RIDGE OF GIRT BAR. PLEASE NOTE THIS EVACUATION SLIDE IS ALSO USED ON A310 AIRCRAFT. 2L72 4F RTA26NM 20050415000872005041500087WP 2005 4 15 WX0500019 120050208A3397 CONNECTOR DOUG DC9 DC983 3022083WP EMERGENCY LIGHT LOOSE A WX0AK NONE O OTHER ININSP/MAINT 1 WP19860GA 49786 LAS - MAINTENANCE REPORTED NUMEROUS FLOOR EMERGENCY EXIT LIGHTS INOPERATIVE AND L2 DOOR EMERGENCY EXIT SIGN LIGHTS INOPERATIVE. MAINTENANCE RECONNECTED EMERGENCY EXIT FLOOR LIGHT AT SEAT 6DEF. ALL LIGHTS OPERATIONALLY CHECK GOOD IAW 33-53-01. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050415000892005041500089WP 2005 4 15 WX0500017 120050206A3260 UPLOCK SENSOR DOUG DC9 DC983 3022083WP MLG OUT OF ALIGNMENTA WX0AA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 WP19862GA 49556 LAS TO ICT- CREW REPORTED NOSE UNSAFE LIGHT ILLUMINATED IN CRUISE FLIGHT. AIRCRAFT RETURNED TO LAS AND LANDED WITHOUT INCIDENT. AIRCRAFT WAS FERRIED TO GYR FOR MAINTENANCE. MAINTENANCE SHIMMED UPLOCK PROXIMITY SWITCH IAW MM 32-60-05. MAINTENANCE COMPLETED GEAR SWING IAW MM 32-60-00. UPLOCK SWITCH OPERATIONALLY CHECKS GOOD ON GROUND. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050415000932005041500093NM 2005 4 15 2005UALA00121 120050205A5322 SHEAR TIE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29578UA 26694 SHEAR TIE HAS ELONGATED HOLES STA 620, BETWEEN STR 16L AND 17L. SUPPLEMENTAL DATA UPDATE SHEAR TIE FOUND DAMAGED DURING REPLACEMENT OF PREVIOUS REPAIR IN THE AREA. MAJOR REPAIR ACCOMPLISHED. SHEAR TIE REPLACEMENT WAS FABRICATED AND INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050415000952005041500095NM 2005 4 15 2005UALA00123 120050205A5312 PRESSURE PANEL BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29578UA 26694 AFT PRESSURE DECK HAS DAMAGE AT STA 1681 TO 1691, RBL 29 TO RBL 56. SUPPLEMENTAL DATA UPDATE DAMAGE CAUSED BY TYPICAL FLOOR CORROSION UNDER THE GALLEY AREA. MAJOR REPAIR ACCOMPLISHED. REMOVED EXISTING REPAIRS AND INSTALLED NEW DOUBLERS ON THE AFT PRESSURE DECK WEB. 2L72 4F4 FRTA2NM E17NE 20050415000962005041500096NM 2005 4 15 2005UALA00124 120050205A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29581UA 26701 CABIN FLOORBEAM STA 365 HAS CORROSION RBL 3 TO RBL 26 UPPER T-CAP. SUPPLEMENTAL DATA UPDATE DAMAGE CAUSED BY TYPICAL FLOORBEAM CORROSION. MAJOR REPAIR ACCOMPLISHED. DAMAGE TO THE T-CAP REMOVED. T-CAP REPLACEMENT SECTION FABRICATED AND INSTALLED USING SPLICE ANGLES. 2L72 4F4 FRTA2NM E17NE 20050412002232005041200223NM 2005 4 12 05FDEA00327 120050302A5314 KEELBEAM BOEING727 727227 1384078NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25496FE 21670 FWD CARGO BAY RT KEEL BEAM HAS CORROSION AT NUTPLATES FROM BS 720C PLUS 5 TO PLUS 9, RBL 5, WL 149. REMOVED CORROSION FROM RT KEEL BEAM, FOUND TO BE OUT OF LIMITS, REPAIRED IAW FED EX EA 7-5310-86203. 2L73 4F A3WE 20050412002272005041200227WP 2005 4 12 GTIA050061 120050226A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE FUSELAGE BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FLOOR SUPPORT STA 1136 BROKEN AFT PIT 28R-28L. REMOVED FLOOR SUPPORT AND LOCATED NEW FLOOR SUPPORT AT STA 1136, 28R-28L. INSTALLED FLOOR SUPPORT FS 1136, 28R-28L, AFT PIT IAW SRM. (K) 2L72 4F4 F A6WE E9NE 20050412002282005041200228WP 2005 4 12 GTIA050070 120050218A5230 DOOR DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE AFT CARGO DOOR DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 DENT ON AFT CARGO DOOR AT STA 1183, 14 INCHES FROM UPPER EDGE/ 23 INCHES FROM AFT EDGE (D=1.0, X=0.015, D/X=66.7). REMOVED AFT CARGO DOOR TO FOM DENT FOUND TO BE COND 1B. COLD WORK PERFORMED TO ORIGINAL CONTOUR. DYE PENETRANT PERFORMED FOR CRACKS. FABRICATED REPAIR DOUBLER. TREATED AND PRIMED REPAIR DOUBLER. INSTALLED DOUBLER IAW 53-04, FIG 38. INSTALLED AFT CARGO DOOR IAW 52-31-00. (K) 2L72 4F4 F A6WE E9NE 20050412002392005041200239NE 2005 4 12 GTIA050042 220050218A7230 COMPRESSOR AIRBUSA321 A321211 3930370EU IAE V2500 V2500A1 NE NR 2 ENGINE STALLED A GTIAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS CRCRUISE 1 GL23586NK 1794 NR2 ENGINE COMPRESSOR STALL AT 10,000 LEVEL FLIGHT, PERFORMED QRH REST ENGINE TO MATCH NR1 AND ENGINE STALLED AGAIN, DIVERTED. REMOVED AND REPLACED NR2 ENGINE, PERFORMED IDLE LEAK CHECK, OPS CHECK GOOD. (K) 2L72 4F4 FRTA28NM E311NE 20050412002432005041200243WP 2005 4 12 GTIA050063 120050215A5320 ANGLE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 DOOR FRAME TO SKIN CORNER ANGLES STA 1155 AND 1212 AT DOOR JAMB BEAM ARE CORRODED IN AFT PIT. REMOVED CORROSION ON DOOR FRAME SKIN, CORNER ANGLES STA 1155 AND 1212 AT DOOR JAMB BEAM. CORNER ANGLE IS OUT OF LIMITS STA 1212 AND LOCATED NEW ANGLE, INSTALLED ANGLE AT STA 1212. CORNER ANGLE AT STA 1155 WITHING LIMITS IAW 53-01. (K) 2L72 4F4 F A6WE E9NE 20050412002452005041200245WP 2005 4 12 GTIA050045 120050215A5310 BEAM DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 AFT PIT LOWER DOOR JAMB BEAM CORRODED AND HAS BARE METAL. REMOVED CORROSION, FABRICATED REPAIR IAW SRM. OK TO TREAT, PRIME AND TOPCOAT REPAIR. LOCATED AND DRILLED 2 DOOR STOP FITTINGS AND INSTALLED DOOR JAMB BEAM REPAIR. (K) 2L72 4F4 F A6WE E9NE 20050412002602005041200260WP 2005 4 12 GTIA050071 120050303A5330 SKIN DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE FUSELAGE DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 SKIN DENT AT STA 1174, BETWEEN LONGERON 17L AND 18L. REMOVED SAF-T-GLO, GALLEY 4 AND SIDE WALL PANEL TO FOM AT LT FS 1184. FOUND DENT TO BE (D=1.5 INCH, X=0.050, D/X=30) COND 2. REFORMED DENT AREA TO ORIGINAL CONTOUR. INSTALLED DOUBLER IAW SRM 53-04, FIG 38. INSTALLED SIDE WALL PANEL, G4 GALLEY AND SAF-T-GLO IAW MM. (K) 2L72 4F4 F A6WE E9NE 20050412002632005041200263WP 2005 4 12 GTIA050068 120050218A5753 WEDGE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE T/E FLAP DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 LT WING, IB FLAP, OB T/E WEDGE HAS TEMPORARY REPAIR LOWER SIDE IB. REMOVED TEMP REPAIR, REMOVED DAMAGED AREA (2 INCH DIA) FABRICATE DOUBLER AND FILLER, TREATED, PRIMED DOUBLER AND FILLER. INSTALLED REPAIRED DOUBLER AND FILLER IAW SRM. (K) 2L72 4F4 F A6WE E9NE 20050412002692005041200269EA 2005 4 12 A6WA200540119 120050314A5720 ANGLE CNDAIRCL600 CL6002B19 1900309EA WING CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31413AW 7585 RT FS 625 OBLIQUE ANGLE IS CRACKED. REMOVED AND REPLACED RT 621-00 ANGLE AT STRINGER 14 IAW CRJ SRM 57-42-06. (M) 2L72 4F RTA21EA 20050412003122005041200312EA 2005 4 12 ASOA05236 120050316A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27905EV 7632 DURING A C-CHECK IN MCN, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 WAS FOUND TO CRACKED UNDER THE FIRE LOOP CLIP BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW ASA EO 600-53-0072B. (M) 2L72 4F RTA21EA 20050413000042005041300004EU 2005 4 13 ASOA05179 120050204A5320 INTERCOSTAL AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27633AS 344 DURING A C-CHECK IN YUL, THE INTERCOSTAL BETWEEN FRAME 38-39 LEFT WAS FOUND TO BE CORRODED ON THE LOWER FLANGE BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTAL BETWEEN FRAME 38-39 LEFT IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20050413000052005041300005EU 2005 4 13 ASOA05178 120050204A5320 INTERCOSTAL AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27633AS 344 DURING A C-CHECK IN YUL, THE INTERCOSTAL BETWEEN FRAME 36 AND 38 RT, STRINGER 16 AND 17 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTAL BETWEEN FRAME 36/38, RT, STRINGER 16/17 IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20050413000162005041300016EA 2005 4 13 ASOA05174 120050302A5260601R3198045 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27830AS 7236 DURING HANGAR MAINTENANCE IN MCN, THE TOP STEP ON THE PASSENGER DOOR WAS FOUND CRACKED AT BOTH OUTBOARD CORNERS. MAINTENANCE REMOVED AND REPLACED THE TOP STEP ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20050413000302005041300030EA 2005 4 13 ASOA05241 120050316A5320601R53611001 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27925EV 7831 DURING A C-CHECK IN MCN, THE FS 625 LEFT CLIP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FS 625 LT CLIP IAW CRJ-200 SRM 51-42. (M) 2L72 4F RTA21EA 20050413000332005041300033EA 2005 4 13 ASOA05255 120050321A3350BR9279106 LENS CNDAIRCL600 CL6002B19 1900309EA CABIN CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27902EV 7620 DURING A C-CHECK IN MCN, THE LENS COVER ON THE EMERGENCY EXIT LIGHT AT THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE EMERGENCY EXIT LIGHT ASSEMBLY AT THE SERVICE DOOR. (M) 2L72 4F RTA21EA 20050413000442005041300044EA 2005 4 13 ASOA05229 120050306A5312670531105212 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27702EV 10035 DURING HANGAR MAINTENANCE IN CKB, THE LEFT AND RIGHT LOWER BULKHEAD WEBS AT FS 280 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT LOWER BULKHEAD WEBS AT FS 280 IAW BOMBARDIER REO 670-53-11-052. (M) 2L72 4F RTA21EA 20050413000572005041300057SO 2005 4 13 SIMA200507506 120050313A531314533888001 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21652RS 145432 ABI - DURING INSPECTION, FOUND STRINGER 19L WAS FOUND TO BE CHAFED AT AFT FAIRING CUT OUT. BLENDED THE CHAFE AND PERFORMED EDDY CURRENT INSPECTION WITH NO CRACKS NOTED. FABRICATED A DOUBLER, TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 28, CHAPTER 53-24-02. (M) 2L72 4T RTT00011AT 20050413000582005041300058SO 2005 4 13 SIMA200507902 120050318A27403621005009 CONTROL UNIT EMB 145 EMB145 3260210SO E/E BAY FAILED A SIMAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 SW21611AE 145074 YUL - FLT 4759 - DURING APPROACH CREW REPORTED A MAIN AND BACKUP PITCH TRIM FAIL ON EICAS. SYSTEM WAS RESET AS PER THE MANUAL AND AICRAFT WAS LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT IAW EMB MM. OPERATIONAL CHECKS WERE SATISACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050413000652005041300065SO 2005 4 13 SIMA200507515 120050311A532014522178005 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21652RS 145432 ABI - DURING INSPECTION OF AIRCRAFT, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED CENTER SILL. INSTALLED SERVICEABLE SILL IAW EMB SRM, SRM EMB 145/1142 REV 28 CHAPTERS 51-20-01, 51-20-03, 51-40-02, 51-40-04 AND 51-40-06. (M) 2L72 4T RTT00011AT 20050413000812005041300081SO 2005 4 13 SIMA200507514 120050311A532014521725615 SILL EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21700LE 145156 ABI - DURING INSPECTION OF AIRCRAFT, THE SERVICE DOOR AFT SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED AFT SILL. INSTALLED NEW SILL IAW EMB SRM, SRM 145/1142 REV 28, CHAPTERS 51-20-03 AND 51-40-02. (M) 2L72 4F RTT00011AT 20050413000852005041300085SO 2005 4 13 SIMA200507001 120050310A143014569390001 BOLT EMB 135 EMB135KL 3260302SO RT AILERON BROKEN A SIMAK NONE F FLT CONT AFFECTED TXTAXI/GRND HDL 1 SW21803AE 145483 DURING PHASE 2A INSPECTION, FOUND RIGHT AILERON DAMPER ROD END BOLT BROKEN. REMOVED AND REPLACED BOLT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050413000872005041300087SO 2005 4 13 SIMA200508702 120050318A532014525381003 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21636AE 145160 THE LEFT OMEGA BEAM AFT OF FRAME 24 WAS FOUND CORRODED. PERFORMED A NINE INCH CUT OUT OF THE OMEGA BEAM TO REMOVE THE CORROSION. FABRICATED A FILLER, EXTERNAL ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2005-145/1180 PARA 1 DATED MARCH 15, 2005. (M) 2L72 4T RTT00011AT 20050413000972005041300097EU 2005 4 13 USAA050007 120050101A21404E33621 ELEMENT AIRBUS330 A330323 3930335EU CABIN CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW22421 0315 BFM - FOUND HEATED FLOOR PANEL ELEMENT WITH CORROSION, BETWEEN FRAME 33-354, Y+-1456-2462. FABRICATED REPLACEMENT SKIN PER EA 961140 REV A. (M) 2L72 4F RTA46NM 20050414000252005041400025WP 2005 4 14 UPS05844263 120050319A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE: C2, EXTERIOR FRUSLAGE SKIN LT APROX. STA 1746 LONGERON 14 HAS TWO SMALL CRACKS ( APROX. .25 ) EXTENDING FROM FASTENER. REPAIRED CRACKS IAW DC-8 SRM 53-2-1, 51-1-20D, & 51-1-21. 2L74 4F RT4A25 20050414000292005041400029 2005 4 14 ASMF200501007 420050113A3430285A12001 CONTROL UNIT BOEING737 73776N 13844CHNM E/E BAY FAILED W ASMFK NONE G MULTIPLE FAILURE APAPPROACH 1 SW23997AM27 30283 DURING APPROACH, ATS DID NOT MAINTAIN SPEED, SPEED BRAKES DID NOT ARM, LIGHT TURNED ON, CAPT FLT DIRECTOR TURNED OFF, ALL ALERTS SOUND TURNED OFF, ILS WAS IN PARALLEL TO THE LOCALIZER AND PWS LIGHT TURNED ON. VERIFICATION FLIGHT WAS PERFORMED CONFIRMING FAILURE IN AUTOMATIC PILOT SYSTEM A. DURING OVERNIGHT SERVICE, RADIO ALTIMETERS 3 AND 4, FSEU AND CONTROL MODULE WERE REPLACED IAW MM, RESPECTIVELY. ILS WAS TESTED IAW MM, ALL CORRECT. AUTOMATIC PILOT "A" SYSTEM WAS DEFERRED IAW MEL 22-1. DURING OVERNIGHT SERVICE 14/15 FCC "A" AND "B" AND MCP WERE REPLACED IAW MM, ALL CORRECT. DFG SYSTEM WAS TESTED IAW 22-11-00 AND 22-31-00, ALL CORRECT AND DEFERRED REPORT WAS CLOSED. 2L72 4F RTA16WE 20050414000402005041400040NM 2005 4 14 ASMF20050301 120050301A5220 DOOR DOUG MD88 MD88 3023688NM EMERGENCY EXIT OPEN W ASMFA UNSCHED LANDING WP INADEQUATE Q C NO WARNING INDICATION CLCLIMB 1 SW23169PL 53175 AIRCRAFT RETURNED OF FLIGHT AS A CONSEQUENCE OF PRESSURIZATION LEAK IN RIGHT FORWARD EMERGENCY EXIT. DURING CHECK WAS DETECTED RIGHT FORWARD EMERGENCY DOOR PARTIALLY OPENED. THE RIGHT FORWARD EMERGENCY DOOR WAS INSTALLED CORRECTLY IAW MM 52-21-10, PRESSURIZATION TEST WAS PERFORMED IAW MM 21-32-00 AND THE HARD LANDING INSPECTION WAS PERFORMED IAW MM 05-51-04, TESTED CORRECT. 2L72 4F RTA6WE 20050414000432005041400043NM 2005 4 14 ASMF200503006 120050308A27515955401501 SKIN DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE AILERON DAMAGED W ASMFK NONE F FLT CONT AFFECTED ININSP/MAINT 1 SW23946AS 49658 DURING TRANSIT CHECK WAS DETECTED HIT IN LT AILERON. DURING REVISION WAS DETECTED DAMAGED THE AILERON FITTING PN 44938931-507. THE LT AILERON WAS REPLACED AND TESTED IAW MM 27-10-0 AND MM 27-10-00. TEST FLIGHT WAS PERFORMED IAW GMM CHAPTER 4-10-6, NOTE 2 AND 4, ALL CORRECT. 2L72 4F4 FRT E9NE 20050414000442005041400044NM 2005 4 14 ASMF200503012 120050313A3600 PNEUMATIC SYSTEM BOEING737 737* NM GE CFM56 CFM56* 13802NE MALFUNCTIONED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23904AM 28262 AIRCRAFT RETURNED TO PLATFORM DURING PUSH BACK, THE PNEUMATIC WAS NOT ENOUGH TO START THE ENGINES. THE ENGINES WERE STARTED WITH EXTERNAL PNEUMATIC PLANT IAW MM 49-50-00, TESTED CORRECT AND THE PNEUMATIC AUXILIARY POWER UNIT WAS DEFERRED IAW MEL 49-7. DURING TRANSIT SERVICE, OPERATIONAL TEST WAS PERFORMED TO PNEUMATIC AUXILIARY POWER UNIT WAS PERFORMED IAW MM 49-11-00, TESTED CORRECT, DEFERRED REPORT WAS CLOSED. 2L72 4F4 FRTA16WE E2GL 20050414000512005041400051WP 2005 4 14 ASMF200504007 120050408A2410696233B CSD DOUG DC9 DC987 3022087WP RIGHT ENGINE FAILED W ASMFK NONE J WARNING INDICATION ININSP/MAINT 1 SW23205AM3630510851 49405 AIRCRAFT ARRIVED WITH DEFERRED REPORT OF RIGHT CSD OIL PRESSURE LOW LIGHT TURNED ON AND BEFORE TO ENGINES STARTED, THE APU OIL TEMPERATURE HIGH LIGHT TURNED ON. ABNORMAL PROCEDURE WAS PERFORMED AND LIGHT CONTINUED ON. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE, THE RIGHT CSD AND OIL COOLER WERE REPLACED IAW 24-10-01 / 03 RESPECTIVELY AND THE APU WAS REPLACED TOO IAW MM 49-10-00, TESTED CORRECT. 2L72 4F RTA6WE 20050414000872005041400087 2005 4 14 2005UALA00070 420050117A2565131W1813 GIRT BAR BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29223UA13204 30224 DOOR 1 RT GIRT BAR SUPPORT FITTING AFT SIDE OF DOOR BROKEN. SUPPLEMENTAL DATA UPDATE THE GIRT BAR SUPPORT FITTING WAS FOUND TO BE CRACKED. THE FAILURE WAS DUE TO CONTACT WITH A SERVICE VEHICLE RAMP. THE CRACKED FITTING WAS REMOVED AND REPLACED. 2L72 4F4 FRTT0001SE E46NE 20050414001002005041400100EU 2005 4 14 DXTA200500576 120050203A2701 CONTROL CABLE BRAERO1000 HAWKER1000 7450005EU CONTROL COLUMN OUT OF ADJUST E DXTAO OTHER F FLT CONT AFFECTED CRCRUISE 1 GL07545QS 259045 CONTROLS ARE BINDING. WHILE MOVING THE CONTROLS LT & RT THERE IS A NOISE AND FEELING OF BINDING IN PILOT CONTROL COLUMN. AT HIGHER SPEED MORE PRONOUNCED, AT SLOWER SPEED LESS PRONOUNCED. AFTER PERFORMING DETAIL INSPECTION DETERMINE THAT SLIGHT RATCHETING MOVEMENT IS INTERNAL OF PILOT'S CONTROL COLUMN. PERFORM ONE TIME INSPECTION OF AIRCRAFT FOR THE PURPOSE OF A FERRY FLIGHT FROM BWI TO ACY, AT ACY ADJUSTED CABLES ON PILOT'S CONTROL COLUMN IAW HAWKER 1000 MM CH 27-10-00, NO BINDING FELT ON EITHER CONTROL COLUMN. 2L72 4F RTA3EU 20050414001142005041400114NM 2005 4 14 2090405 120050121A2701 YOKE BOEING737 737724 13844BYNM COCKPIT DETACHED Z O OTHER F FLT CONT AFFECTED TOTAKEOFF 1 EA15VPBBT 29089 BERMUDA (BD) - JUST AFTER TAKEOFF, THE CAPTAIN'S CONTROL YOKE CAME OUT AND FELL TO THE GROUND. AT A SAFE HEIGHT THE CONTROL YOKE PIN WAS PUT BACK IN PLACE. THIS RESULTED IN A MOMENTARY LOSS OF AILERON AND RUDDER CONTROL. PENDING ENGINEERING INVESTIGATION REPORT. 2L72 4F RTA16WE 20050415000492005041500049NM 2005 4 15 WRLA2005009 120050131A5753 SKIN DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE RT WING TE FLAP CANNING A WRLAK NONE O OTHER ININSP/MAINT 1 SO11273 48519 DURING "C2" CHECK FOUND RIGHT INBD FLAP UPPER SKIN HAVE ONE OIL-CANNING AT XIFH 286 ABOVE T/E 24" L=3" W=3". CUTOUT DAMAGED SKIN AND REPAIRED WITH EXTERNAL DOUBLER (2024-T3 .050 CLAD, L=5.625" W=5") AND RIVET (CR32245-4) REF MD11 SRM 57-20-00 VOL I REV 36 FIG 6. 2L73 4F4 FRTA22WE E24NE 20050415000502005041500050NM 2005 4 15 WRLA2005010 120050131A5753 SKIN DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE RT WING TE FLAP DENTED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11273 48519 DURING "C2" CHECK, FOUND DENT LOCATED AT RT INBD FLAP LOWER SKIN XIFH193 ABOVE T/E 9" L=1.5" W=0.066". CUTOUT AREA 2 INCH BY 1 INCH AND REPAIRED DAMAGE AREA WITH DOUBLER (2024-T3 .050 ALU SHEET) AND RIVET(CR3224-5). CONDITION CHECK SATISFACTORY REF MD11 SRM 57-10-00 FIG 6 VOL I REV 36. 2L73 4F4 FRTA22WE E24NE 20050415000532005041500053NM 2005 4 15 DL757050072 120050201A3350 FUSE BOEING757 757232 1384965NM EMERGENCY LIGHT FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27628DL 22918 IR- ON L/O FOUND EMERGENCY EXIT SIGN ABOVE 4L DOOR INOP. RELAMPED, NO HELP. REMOVED AND REPLACED SIGN, NO HELP. INSTALLED ORG. T/S PER WDM 33-51-11, FOUND PWR SUPPLY M737 FUSE BURNED OUT. REPLACED FUSE, OPS CK OK. 2L72 4F RTA2NM 20050415000602005041500060NM 2005 4 15 DLM88050083 120050204A25304110001137 COFFEEMAKER DOUG MD88 MD88 3023688NM FWD GALLEY SMOKE A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27915DE 53420 SMOKE IN FWD CABIN AND COCKPIT. UPON INSPECTION, DETERMINED FWD GALLEY COFFEEMAKER TO BE SOURCE. REPLACED SAME. 2L72 4F RTA6WE 20050415000642005041500064NM 2005 4 15 WRLA2005011 120050131A5753 SKIN DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE RT WING TE FLAP DENTED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11273 48519 DURING "C2" CHECK, FOUND RT INBD FLAP LOWER SKIN DENT AT XIFH 139 ABOVE T/E 58" L=0.5" W=0.75" D=0.065". CUTOUT DENT AREA 1.5' BY 1", FABRICATED REPAIR DOUBLER 6" BY 6" (2024-T3 .063" ALU SHEET) AND USED RIVET CR3224-5 TO REPAIR THE DENT. CONDITION CHECK SATISFACTORY REF SRM 57-10-00 FIG 34 REV 36 VOL I. 2L73 4F4 FRTA22WE E24NE 20050415000672005041500067CE 2005 4 15 20030787 120050204A3220 SWITCH BEECH 1900 1900D 1154162CE NLG INOPERATIVE A GLBAL ABORTED APPROACH P NO WARNING INDICATION DEDESCENT 1 NM03153GL UE153 UPON APPROACH, LANDING GEAR WAS SELECTED DOWN AND CREW NOTED THAT NOSE GEAR SHOWED NO INTRANSIT OR GREEN DOWN AND LOCKED INDICATION. CREW PERFORMED CHECKLIST AND HAD GEAR VERIFIED BY TOWER GEAR DOWN. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE DISCOVERED INTERNAL SWITCH IN NOSE LANDING GEAR INOPERATIVE. NOSE GEAR REMOVED AND REPLACED, OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA24CE 20050415000682005041500068NM 2005 4 15 WRLA2005014 120050131A5347 SEAT TRACK DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11273 48519 DURING "C2" CHECK FOUND CABIN SEAT TRACK CORROSION BETWEEN STA 840 AND STA 860 X=-44.5. CUT AND REMOVED CORRODED SECTION BETWEEN STA 832 AND 909 X=-44.5, FABRICATED AND INSTALLED NEW SEAT TRACK SECTION AND SPLICE HAT. CONDITION CHECK SATISFACTORY REF MD11 SRM 53-70-00 FIG 1 REV 36 VOL I. 2L73 4F4 FRTA22WE E24NE 20050415000752005041500075SW 2005 4 15 47518011705 120050117A291070012H000Y210 LINE BELL 222 222UT 1182148SW LYC LTS101LTS101750C1 41560NE HYD SYSTEM RUPTURED E A1UAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 CE03419MA 47518 47215 THE NR 1 HYD SYSTEM CAUTION LIGHT CAME ON. PRESSURE CHECKED AND WAS CONFIRMED TO BE AT ZERO. CYCLED SWITCH, MOVED PEDALS AND VERIFIED ACTUAL FAILURE, SO TURNED HYD SYSTEM #1 OFF, PROCEEDED TO FULLERTON AIRPORT AND MADE LANDING FROM A HOVER TO HELIPAD, NO PROBLEM. FOUND THAT THE NR 1 HYDRAULIC PRESSURE LINE FROM THE FILTER MODULE HAD RUPTURED. 1G72 3U3 U H9SW E5NE 20050415000902005041500090WP 2005 4 15 WX0500016 120050204A3260833605 PROXIMITY SWITCH DOUG DC9 DC983 3022083WP MLG OUT OF ADJUST A WX0AO OTHER N FALSE WARNING CRCRUISE 1 WP19862GA 49556 BLI TO LAS - CREW REPORTED NOSE GEAR RED LIGHT ILLUMINATED IN CRUISE. CHECKLIST PROCEDURE PERFORMED. LIGHT REMAINED ILLUMINATED. AIRCRAFT LANDED AS SCHEDULED LAS WITHOUT INCIDENT. MAINTENANCE SHIMMED THE SENSOR AND REMOVED AND REPLACED THE PROXIMITY SWITCH UNIT, PERFORMED MULTIPLE GEAR SWINGS, SYSTEM OPERATIONALLY CHECKED GOOD IAW MM 32-30-00, 32-60-04 AND 32-60-05. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050415000972005041500097NM 2005 4 15 2005UALA00125 120050204A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29526UA 24994 FUSELAGE SKIN AT STA 1600 STR 14R IS DAMAGED. SUPPLEMENTAL DATA UPDATE DENT DAMAGE CAUSED BY IMPACT WITH FUSELAGE SKIN. MAJOR REPAIR ACCOMPLISHED. SKIN DAMAGE WAS CUTOUT AND REPAIR DOUBLER AND STRUCTURAL FILLER INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050415001002005041500100EU 2005 4 15 2005UALA00131 120050208A2840 INDICATION SYS AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUEL QTY FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29436UA 638 LOST ALL FUEL QUANTITY INDICATIONS. REVIEW OF THE POST FLIGHT REPORT RESULTED IN THE INDICATION OF BOTH THE FQIC 3QT AND FWC1 AS BEING FAULTED. FURTHER TROUBLESHOOTING ALONG WITH SOME ADDITIONAL WIRING CHECKS CONFIRMED NO DATA WAS AVAILABLE FOR CHANNEL 1A OR 1B WITHIN THE FQIC 3QT. FQIC 3QT AND FWC1 WERE REPLACED AS REQUIRED. SHOP FINDINGS WERE REPORTED AS BOTH UNITS DID CONTAIN FAILURES. 2L72 4F4 FRTA28NM E40NE 20050415001012005041500101NM 2005 4 15 2005UALA00138 120050210A3350 LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE EMERGENCY SLIDE INOPERATIVE A UALAO OTHER O OTHER NRNOT REPORTED 1 WP29507UA 24743 EMERGENCY SLIDE LIGHT ON EXTERIOR OF AIRCRAFT AFT OF LT WING INOP. RELAMPED PER AMM 33-51-06-201 2L72 4F4 FRTA2NM E17NE 20050415001022005041500102NM 2005 4 15 P9RA20050067 120050213A33501102833 LIGHT BOEING737 737231 1384079NM AIRSTAIR INOPERATIVE A P9RAK NONE L NO TEST ININSP/MAINT 1 SO1154344 21631 AIRCRAFT IN MAINTENANCE, ATL. AFT AIRSTAIR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED AIRSTAIR EMERGENCY LIGHT IAW MM. 2L72 4F RTA16WE 20050415001042005041500104 2005 4 15 I05R099334 420050202A34215040111932 INDICATOR SNIAS 350 AS350* EU ARTI HORIZON PRECESSES E I05RO OTHER O OTHER NRNOT REPORTED 1 WP0529LB 3500 3560 INDICATOR WHEN CAGED WILL RETURN TO A PRECESSED CONDITION. 1G71 3U H9EU 20050415001052005041500105GL 2005 4 15 YTRR099159 220050128A732123070613 FUEL CONTROL BELL 206 206L1 1182107SW ALLSN 250C 250C20 03013GL ENGINE INOPERATIVE B YTRAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 SW03518RL 45183 FUEL CONTROL UNIT WOULD NOT MAINTAIN IDLE OF THE AIRCRAFT. THE UNIT HAD BEEN PREVIOUSLY REPAIRED 91.3 HRS AGO FOR THE SAME EXACT PROBLEM. 1G71 3U3 U H2SW E4CE 20050415001082005041500108SW 2005 4 15 YTRR099231 120050104A7712222375077119 TRANSDUCER BELL 407 407 1182206SW ENGINE TORQUE FAILED B YTRAO OTHER O OTHER NRNOT REPORTED 1 SW03594RL483 53594 ENGINE TORQUE TRANSDUCER FAILED. 1G71 3U O H2SW 20050415001092005041500109SW 2005 4 15 YTRR099234 120050208A6510407340339107 BEARING BELL 407 407 1182206SW TAIL ROTOR VIBRATION B YTRAO OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 SW03594RL1152 53594 NR 1 AND 2 TAIL ROTOR HANGAR BEARING CAUSING HI FREQUENCY VIBRATION IN AIRCRAFT 1G71 3U O H2SW 20050415001102005041500110NM 2005 4 15 QXEA200500217 120050213A5230502213 SEAL BOMBDRDHC8 DHC8401 1390041NM AFT CARGO DOOR MISALIGNED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09402QX8936 4032 SMF - FLIGHT 2303 - THE EMERGENCY/ABNORMAL CHECKLIST WAS COMPLIED WITH WHEN THE CREW RECEIVED A CABIN PRESSURE CAUTION LIGHT WHILE AT CRUISE ALTITUDE. AFTER SELECTING THE BLEEDS TO MAX, THE LIGHT EXTINGUISHED AND THE SYSTEM PERFORMED NORMALLY. MAINTENANCE FOUND THE LOWER PORTION OF THE AFT CARGO DOOR SEAL NOT IN THE TRACK. THE SEAL WAS REINSTALLED AND OPERATIONAL CHECKS WERE PERFORMED. THE CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050415001112005041500111EA 2005 4 15 QXEA200500170 120050117A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - FUSELAGE STATION 280 BULKHEAD Z10009 IS CORRODED AT FLOOR LINE FROM RBL 11 TO RBL 30. REPAIRED IAW REO 670-53-11-052. 2L72 4F RTA21EA 20050415001122005041500112EA 2005 4 15 QXEA200500171 120050120A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - AFT FUSELAGE AT STATION 974.75, STRINGER 27, LOWER SKIN GOUGED BY FAIRING STIFFENER. REPAIRED IAW HORIZON AIR EA R-53-264 AND REO 670-53-61-143. 2L72 4F RTA21EA 20050415001132005041500113EA 2005 4 15 QXEA200500172 120050116A5320 SILL CNDAIRCL600 CL6002C10 1390015EA ZONE 100 WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - FUSELAGE AFT CARGO COMPARTMENT LOWER THRESHOLD STRUCTURE SILL HAS WEAR DAMAGE FROM FLOOR SILL COVER. REPAIRED IAW REO 670-53-61-141 AND SRM 51-21-16. 2L72 4F RTA21EA 20050415001142005041500114EA 2005 4 15 QXEA200500173 120050119A5320 PLATE CNDAIRCL600 CL6002C10 1390015EA ZONE 200 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - FUSELAGE AFT CARGO COMPARTMENT DOOR SURROUND STRUCTURE LOWER STRIP PLATE FOR DOOR SEAL, HAS SCRATCHES FORWARD AND AFT. REPAIRED IAW HORIZON AIR EA R-53-263 AND REO 670-53-61-142. 2L72 4F RTA21EA 20050415001162005041500116EA 2005 4 15 QXEA200500175 120050121A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - RIGHT OUTBOARD SIDE FACING SEAT RAIL AT STATION X524 HAS PITTING CORROSION ON MOST INBOARD SURFACE. REPAIRED IAW HORIZON AIR EA R-53-266 AND REO 670-53-00-060, REV B. 2L72 4F RTA21EA 20050415001192005041500119WP 2005 4 15 AALA20050103 120050210A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217514A 49891 DFW - OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050415001202005041500120WP 2005 4 15 AALA20050106 120050212A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21492AA 49730 TUL - OVERWING EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050415001232005041500123WP 2005 4 15 AALA20050116 120050215A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21233AA 49180 DFW - EMERGENCY LIGHTS AT L2 615, L2 671 AND L2 694 INOPERATIVE. RESTORED CONNECTION IN THE CLIPS OF BATTERY PACK ASSEMBLY B5 27 FOR EMERGENCY LIGHTS AT L2 615, L2 671, AND L2 694. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050415001262005041500126NM 2005 4 15 HNAA0500009 120050208A273051608003 CONTROL UNIT DHAV DHC8 DHC8102 2809003NM ELEVATOR FAILED A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07907HA 011 RT AC BUSS, TRU STALL WARN, ELEVATOR HORN HTR IN FLT. REMOVED AND REPLACED NR 2 AC GND RUN. OPS CK GOOD. LEFT VARIABLE AC BUS ZERO VOLTS AND LOADS. REMOVED AND REPLACED GCU AND CURRENT LIMITER. REMOVED AND REPLACED R AC GCU AND CURRENT LIMITER. 2H72 4T RTA13NM 20050415001282005041500128NM 2005 4 15 QXEA200500234 120050221A335061047811 BATTERY PACK DHAV DHC8 DHC8202 2809007NM ZONE 200 INOPERATIVE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09358PH11241476 506 PDX - NUMEROUS EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED ALL SIX BATTERY PACKS. S/N'S ARE: 010628, 9707245, 9801191, 9807015, 9811181, AND THE LAST ONE SEE BELOW. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050415001292005041500129NM 2005 4 15 RYNA200500005 120050220A274132EM214 SWITCH BOEING737 737800* NM STAB TRIM DEFECTIVE A RYNAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 CE07DIT 28621 DURING CRUISE AT FL370, AUTOPILOT ENGAGED, THE STABILIZER OUT OF TRIM LIGHT ILLUMINATED. CHECKLIST PROCEDURES WERE FOLLOWED AND AUTOPILOT DISENGAGED TO RETRIM AIRCRAFT. THE ELECTRIC TRIM IN THE NOSE UP POSITION WOULD NOT WORK AND MANUAL TRIMMING WAS HARDER THAN NORMAL AND FELT LIKE IT WAS BINDING. NOSE DOWN TRIM WORKED NORMALLY IN BOTH ELECTRIC AND MANUAL MODES. AN EMERGENCY WAS DECLARED AND AIRCRAFT DIVERTED TO AND LANDED AT DFW WITHOUT INCIDENT. REMOVED AND REPLACED THE UP STABILIZER SWITCH. GROUND OPERATIONAL CHECK NORMAL. 2L72 4F RTA16WE 20050415001312005041500131NM 2005 4 15 WRLA2005038 120050215A5512 SKIN DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST RT BARREL NUT HOLE NR 29. 2L73 4F4 FRTA22WE E24NE 20050415001322005041500132NM 2005 4 15 WRLA2005040 120050213A5512 SKIN DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST RT BARREL NUT HOLE NR 25. 2L73 4F4 FRTA22WE E24NE 20050415001342005041500134NM 2005 4 15 WRLA20050420 120050214A5512 SKIN DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST RT BARREL NUT HOLE NR 18. 2L73 4F4 FRTA22WE E24NE 20050415001352005041500135NM 2005 4 15 WRLA2005043 120050213A5512 SKIN DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST RT BARREL NUT HOLE NR 13. 2L73 4F4 FRTA22WE E24NE 20050415001372005041500137NM 2005 4 15 WRLA2005046 120050213A5512 SKIN DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST RT BARREL NUT HOLE NR 07. 2L73 4F4 FRTA22WE E24NE 20050415001382005041500138NM 2005 4 15 WRLA2005047 120050207A5512 SKIN DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST RT BARREL NUT HOLE NR 05. 2L73 4F4 FRTA22WE E24NE 20050415001392005041500139NM 2005 4 15 WRLA2005048 120050213A5512 SKIN DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST LT BARREL NUT HOLE NR 34. 2L73 4F4 FRTA22WE E24NE 20050415001402005041500140NM 2005 4 15 WRLA2005049 120050211A5512 SKIN DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST LT BARREL NUT HOLE NR 29. 2L73 4F4 FRTA22WE E24NE 20050415001412005041500141NM 2005 4 15 WRLA2005050 120050213A5512 SKIN DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST LT BARREL NUT HOLE NR 25. 2L73 4F4 FRTA22WE E24NE 20050415001432005041500143NM 2005 4 15 WRLA2005052 120050211A5512 SKIN DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST LT BARREL NUT HOLE NR 19. 2L73 4F4 FRTA22WE E24NE 20050415001462005041500146NM 2005 4 15 WRLA2005055 120050207A5512 SKIN DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST LT BARREL NUT HOLE NR 09. 2L73 4F4 FRTA22WE E24NE 20050415001472005041500147NM 2005 4 15 WRLA2005056 120050215A5512 SKIN DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST LT BARREL NUT HOLE NR 08. 2L73 4F4 FRTA22WE E24NE 20050415001512005041500151NM 2005 4 15 WRLA2005061 120050213A5347 SEAT TRACK DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK INSPECTION, FOUND CORROSION IN MAIN DECK CARGO SEAT TRACK AT STA 880, X=8.5. 2L73 4F4 FRTA22WE E24NE 20050415001522005041500152NM 2005 4 15 WRLA2005063 120050213A5347 SEAT TRACK DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK INSPECTION, FOUND CORROSION IN MAIN DECK CARGO SEAT TRACK AT STA 877, X=27.5. 2L73 4F4 FRTA22WE E24NE 20050415001532005041500153NM 2005 4 15 WRLA2005064 120050212A5320 FLOOR SUPPORT DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK INSPECTION, FOUND CORROSION IN MAIN DECK CARGO FLOOR PANEL SUPPORT AT STA 1966, X=-53.5. 2L73 4F4 FRTA22WE E24NE 20050415001542005041500154NM 2005 4 15 WRLA2005065 120050212A5320 FLOOR SUPPORT DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK INSPECTION, FOUND CORROSION IN MAIN DECK CARGO FLOOR PANEL SUPPORT AT STA 2007, X=-27.5. 2L73 4F4 FRTA22WE E24NE 20050415001562005041500156NM 2005 4 15 WRLA2005067 120050205A5313 LONGERON DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK INSPECTION, FOUND CORROSION IN CENTER CARGO LONGERON AT STA 5-120 L44R. 2L73 4F4 FRTA22WE E24NE 20050415001592005041500159NM 2005 4 15 WRLA2005070 120050202A5343 STRAP DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE SUPPORT FITTING CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK INSPECTION, FOUND CORROSION IN CENTER LANDING GEAR W/W LT TRUNNION SUPPORT FITTING BOOT STRAP AT STA Y=1470. 2L73 4F4 FRTA22WE E24NE 20050415001612005041500161NM 2005 4 15 AALA20050135 120050221A3350BPS73 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21647AM 24605 MIA - FIRST CLASS EMERGENCY LIGHTS AT RIGHT 1 AND LEFT 1 DOOR EXIT SIGNS INOPERATIVE. REPLACED FRONT EMERGENCY LIGHT MODULE BATTERY PACK FOR THE FIRST CLASS EMERGENCY LIGHTS AT RIGHT 1 AND LEFT 1 DOOR EXIT SIGNS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050415001632005041500163NM 2005 4 15 AALA20050132 120050221A3350 LIGHT BOEING767 767323 1385205NM SEAT 34B INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21363AA 24044 GRU - EMERGENCY ESCAPE PATH LIGHT AT 34B INOPERATIVE. REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT 34B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050415001652005041500165WP 2005 4 15 AALA20050134 120050222A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217533A 49987 DFW - EMERGENCY EXIT SIGNS AT AFT OVERWING INOPERATIVE. REPLACED BATTERY AND CHARGER ASSEMBLY FOR EMERGENCY EXIT SIGNS AT AFT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050415001672005041500167NM 2005 4 15 RYNA200500006 120050218A2612285T003430 CIRCUIT CARD BOEING757 757200 1384950NM FIRE WARNING DIRTY A RYNAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE07151GX 24451 DURING CLIMB AT FL400, THE AURAL FIRE WARNING HORN SOUNDED. THERE WAS NO SIGN OF FIRE OR SMOKE IN THE CABIN AND NO LIGHTS ASSOCIATED WITH THE WARNING HORN. AN EMERGENCY WAS DECLARED AND AIRCRAFT RETURNED TO CUN AND LANDED WITHOUT INCIDENT. CLEANED AND RESEATED AURAL WARNING HORN CIRCUIT CARD. OPERATIONAL CHECK NORMAL. 2L72 4F RTA2NM 20050415001682005041500168NM 2005 4 15 05FDEA00316 120050224A3411 PITOT LINE DOUG MD11 MD11F 3023600NM FIRST OFFICERS OBSTRUCTED A FDEAJA DUMP FUEL UNSCHED LANDING GJ MULTIPLE FAILURE WARNING INDICATION CRCRUISE 1 SO25599FE 48598 FL 340 CLR AIR, A/P DISCON, NEITHER A/P AVBL, IAS COMPARATOR F/O A/S INDICATED UPPER FOOT, RAN QRH AIRSPEED LOST, SUSPECT, ERRATIC CHECKLIST, DETERMINED F/O'S A/S ERRONEOUS BY 25 KIAS. F/O SELECTED ALT STATIC SOURCE IAS COMPARATOR DISAPPEARED AND A/S MATCHED. DUMPED 10,000 LBS OF FUEL. DIVERTED TO OAK. INSPECTED FIRST OFFICERS PITOT TUBE AND FOUND PITOT DRAIN HOLE BLOCKED. REMOVED BLOCKAGE AND APPLIED DRY NITROGEN CLEANING OUT LINE MM 34-11-00-2. PERFORMED PITOT STATIC SYS TEST ON F/O AND STBY AIRSPEED INDICATOR. ALL INDICATIONS WITHIN LIMITS. PERFORMED RTS OF MSC AIR DATA HEATERS TEST PASSED. A/C OK TO CONTINUE. 2L73 4F RTA22WE 20050415001702005041500170NM 2005 4 15 TSAA0529008 120050223A3233 LINE BOEING737 7372T4 1384492NM MLG ACTUATOR LEAKING A TSAAO OTHER KJ FLUID LOSS WARNING INDICATION LDLANDING 1 WP13808AL 23445 FLT 89, KOA-HNL: A SYSTEM HYDRAULICS FAILED ON SHORT FINAL. LEFT MAIN GEAR LEAKING. FOUND THE LEFT HAND MAIN LANDING GEAR ACTUATOR UP PRESSURE HOSE ASSEMBLY LEAKING. REMOVED AND REPLACED THE HYDRAULIC PRESSURE HOSE ASSEMBLY AND SERVICED THE HYDRAULIC RESERVOIR. OPS AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A16WE 20050415001712005041500171CE 2005 4 15 DELA200500005 120050215A216054196501 ADAPTER LEAR 55 55LEAR 5170702CE RAM AIR CRACKED E DELAO OTHER S AFFECT SYSTEMS CRCRUISE 1 CE03903JC11923 081 HOT AIR DELIVERED TO CABIN EVEN WITH CABIN TEMPERATURE CONTROLS SET TO COOL. INVESTIGATION REVEALED A RUPTURED AREA OF THE RAM AIR ADAPTER ASSEMBLY DUE TO CRACKING. SUBSEQUENT HOLE IN ADAPTER ALLOWED RAM AIR TO BYPASS HEAT EXCHANGER. 2L72 4F A10CE 20050415001732005041500173EA 2005 4 15 QXEA200500179 120050121A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - RT OUTBOARD SIDE FACING SEAT RAIL, AT STATION X785 TO X797, HAS PITTING CORROSION ON MOST INBOARD SURFACE. REPAIRED IAW CRJ REO 670-53-00-060, REV B AND HORIZON AIR EA R-53-266. 2L72 4F RTA21EA 20050415001752005041500175NM 2005 4 15 QXEA200500292 120050223A2751 WARNING LIGHT BOMBDRDHC8 DHC8401 1390041NM TE FLAPS FALSE ACTIVATIONA QXEAO OTHER N FALSE WARNING APAPPROACH 1 NM09414QX7882 4061 LAX - FLIGHT 2428 - THE FLAP POWER CAUTION LIGHT ILLUMINATED WHILE ON APPROACH AND THE CREW C/W THE CHECKLIST. MAINTENANCE INSPECTED THE AIRCRAFT AND ACCOMPLISHED THE FLAP POWER NUISANCE CAUTION LIGHT RESET PROCEDURE. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050415001772005041500177EU 2005 4 15 SA05021 120050212A3242466191 SENSOR AIRBUSA319 A319112 3930323EU LT MLG BRAKE FAULTY A USAAO OTHER N FALSE WARNING CLCLIMB 1 EA19733UW 1205 CLT - FLT 458 EN-ROUTE LIR - CLT. AFTER TAKEOFF, THE NR ONE MAIN BRAKE INDICATED INTERMITTENT OVERHEAT, FROM 200 - 800 DEGREE CELSIUS. THE CREW LOWERED THE GEAR TO COOL THE BRAKES. WHEN THE TEMPERATURES STABILIZED TO 135 DEGREE CELSIUS, THE CREW RAISED THE GEAR AND CONTINUED THE FLIGHT TO CLT. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PLACED THE NUMBER 1 BRAKE TEMP INDICATION ON MEL. MAINTENANCE REPLACED THE NR 1 BRAKE TEMPERATURE SENSOR AND REMOVED THE MEL. OK FOR SERVICE. 2L72 4F RTA28NM 20050415001792005041500179EA 2005 4 15 QXEA200500187 120050121A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - LEFT OUTBOARD SIDE FACING SEAT RAIL, AT STATION X581 TO X597, HAS PITTING CORROSION ON MOST INBOARD SURFACE. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01. REO 670-53-00-060, REV B, AND HORIZON AIR EA R-53-266. 2L72 4F RTA21EA 20050415001842005041500184NM 2005 4 15 05FDEA00318 120050226A3260694710566 MODULE BOEING727 727233 138408ANM MLG INDICATOR FAILED A FDEAO OTHER P NO WARNING INDICATION CLCLIMB 1 SO25222FE 20933 WHEN GEAR HANDLE IS UP, RIGHT GEAR SAFE GREEN LIGHT WILL NOT TEST. REPLACED BULBS CYCLED CBS. SWAPPED RIGHT GEAR AND LEFT GEAR LIGHTS IN LEFT POSITION, RIGHT LIGHT WORKED IN RIGHT POSITION, LEFT LIGHT DID NOT WORK. CK'D CONTINUITY THROUGH WARN LIGHT PUSH TO TEST CIRCUIT. L808 FOR RT MLG. FOUND NO CONTINUITY. CK'D NEW PANEL ASSY. LIGHT L808 FOR CONTINUITY FOUND GOOD CONTINUITY. INSTALLED NEW L/G LIGHT MODULE, OPS CK GOOD. REF 727-200 WDM 32-64-01. 2L73 4F RTA3WE 20050415001852005041500185EU 2005 4 15 05FDEA00319 120050226A5610 WINDSHIELD AIRBUS300 A300B4605R 3930308EU COCKPIT FAILED A FDEAA UNSCHED LANDING O OTHER CLCLIMB 1 SO25668FE 772 FO'S WINDSHIELD SHATTERED. DECLARED EMERGENCY. NO OVERWEIGHT LANDING. MEM R CHECK RESISTANCE VALUES ON NEW WINDSHIELD AND ALL CHECK GOOD PER AIRBUS TSM 30-42-00. REMOVED AND REPLACED F/O'S_WINDSHIELD IN REFERENCE T TO A300 AMM 56-11-11-4. OPS CHECKED GOOD AT THIS TIME. SEALANT APPLIED 19:25. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION OFF MFG NP175201-4, POS ONL SRL 98071H9632, TAG 3A0236 ON MFG NP175201-6 SRL 04261H6378, TAG 662105. 2L72 4F RTA35EU 20050415001912005041500191EU 2005 4 15 AWXA200500268 120050215A5315D5347209300000 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28647AW 762 MCN - MAJOR REPAIR - DURING 8-DAY CHECK, CORROSION WAS FOUND ON FLOORBEAM Y29 FORWARD OF FR 68. MAINTENANCE REMOVED CORRODED FLOORBEAM Y29 AT FS 68; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-49-00. 2L72 4F RTA28NM 20050415001932005041500193EU 2005 4 15 AWXA200500271 120050217A5315D5347213320000 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28647AW 762 MCN - MAJOR REPAIR - DURING 8-DAY CHECK, CORROSION WAS FOUND ON FLOORBEAM -Y50 AT FS 66. MAINTENANCE REMOVED CORRODED FLOORBEAM -Y50 AT FS 66; FABRICATED A NEW REPLACEMENT FLOORBEAM, INSTALLED REPAIR PART IAW A320 SRM 51-42-11. 2L72 4F RTA28NM 20050415001952005041500195EU 2005 4 15 AWXA200500273 120050217A5320D53471124200 PLATE AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28647AW 762 MCN - MAJOR REPAIR - DURING 8-DAY CHECK, CORROSION WAS FOUND ON SHEAR PLATE Y50 BETWEEN FS 69 AND FS 70. MAINTENANCE REMOVED CORRODED SHEAR PLATE Y50 FROM FS 69 TO FS 70; FABRICATED A NEW REPLACEMENT SHEAR PLATE, INSTALLED REPAIR PART IAW A320 SRM 51-42-11. 2L72 4F RTA28NM 20050415001982005041500198EU 2005 4 15 AWXA200500276 120050217A5321D5367175400000 FLOOR PANEL AIRBUS320 A320232 3930326EU FUSELAGE DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28647AW 762 MCN - MAJOR REPAIR - DURING 8-DAY CHEC, FOUND AFT GALLEY FLOOR PANEL 261QF DELAMINATED. MAINTENANCE REMOVED DELAMINATED AFT GALLEY FLOOR PANEL 261QF, FABRICATED AND INSTALLED NEW REPLACEMENT FLOOR PANEL IAW DWG D53671754. 2L72 4F RTA28NM 20050415002012005041500201NM 2005 4 15 AWXA200500279 120050220A5315D5347209001100 FLOORBEAM AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28812AW 1178 SAL - MAJOR REPAIR - DURING BC-4 CHECK, EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM -Y1292 AT FS 66+3". MAINTENANCE REMOVED CORRODED FLOORBEAM -Y1292 FROM FS 64" TO FS 66+5", FABRICATED A NEW REPLACEMENT FLOORBEAM, INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050415002032005041500203NM 2005 4 15 AWXA200500281 120050220A5315D5347218420400 FLOORBEAM AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28812AW 1178 SAL - MAJOR REPAIR - DURING BC-4 CHECK, EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM Y1190 AT FS 68. MAINTENANCE REMOVED CORRODED FLOORBEAM Y1190 FROM FS 67 -5" TO FS 68 +3". FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050415002042005041500204EU 2005 4 15 AALA20050140 120050224A3397 CONNECTOR AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHTSDISCONNECTED A AALAK NONE O OTHER ININSP/MAINT 1 SW217055A 462 JFK - EMERGENCY LIGHTS AT SEAT 27G INOPERATIVE. SECURED CONNECTOR AT SEAT 27G FOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20050415002052005041500205EU 2005 4 15 AALA20050142 120050224A3350P4010049 BATTERY PACK AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217055A 462 JFK - EMERGENCY LIGHTS AT 1G TO 5G INOPERATIVE. REPLACED BATTERY PACK 110WL2 FOR EMERGENCY LIGHTS AT 1G TO 5G. SYSTEM GROUND CHECKED NORMAL OPERATIONS. 2L72 4F RTA35EU 20050415002062005041500206WP 2005 4 15 AALA20050144 120050224A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21473AA 49648 BOS - COCKPIT AND FORWARD ENTRY DOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK B5 23 FOR COCKPIT AND FORWARD ENTRY DOOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050415002072005041500207EU 2005 4 15 MALA050200 120050130A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15422XJ 340B422 GALLEY SEAT TRACK AND PROFILE PN 7253721-459 AND 7253721-495 ARE CORRODED OUT OF LIMITS AND HAVE BEEN REPLACED WITH NEW PARTS IAW SRM 51-40-21 AND SRM 51-40-27. REF EAMS WORK ORDER 211546 TASK 1507, FOUND DURING 4Y/2Y CHECK IN BNA. 2L72 4T RTA52EU 20050415002082005041500208EU 2005 4 15 MALA050211 120050106A33506122751 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU EMERGENCY LIGHT DISCHARGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15501XJ E2208 BATTERY PACK PN 61-2275-1 SN 9812852 FAILED SCHEDULED CAPACITY CHECK. REPLACED BATTERY ASSEMBLY PN 61-2274-1. UNIT PASSES CMM CHECKS RTS 1/9/05. 2H74 4F RTA49EU 20050415002092005041500209 2005 4 15 MALA050212 220050126A7200 PROCESSOR BAC 146 AVRO146RJ85A1500097EU NR 1 ENGINE MALFUNCTIONED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15502XJ E2307 AFTER ENGINE START NR 1 LOW OIL PRESSURE LIGHT CAME ON. OIL PSI SHOWED BETWEEN 40 AND 50 PSI (GREEN ARC). OIL PRESSURE GOOD 80 PSI WHEN ENGINE NR 1 AT 80 PERCENT. NR 2 OIL PRESSURE LIGHT NEVER WENT OUT, RETURNED TO GATE. AIRCRAFT TO BE FERRIED TO MSP FOR REPAIRS. REPLACED PROCESSOR PN 2-303-864-02 SN OFF 03013070045 SN ON 040130700515. GROUND RAN A/C, NR 1 OIL PRESS WARNING CHECKS GOOD. 2H74 4F RTA49EU 20050415002102005041500210EU 2005 4 15 MALA050213 120050103A3350 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU EMERGENCY LIGHT DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15502XJ E2307 BATTERY PACK PN 61-2275-1 SN 0006353 REPORTED DEAD. REPLACED BATTERY ASSY PN 61-2274-1. UNIT PASSES CMM CHECKS RTS 1/9/05. 2H74 4F RTA49EU 20050415002112005041500211EU 2005 4 15 MALA050214 120050124A2760 SWITCH BAC 146 AVRO146RJ85A1500097EU SPOILER MALFUNCTIONED A MALAO OTHER J WARNING INDICATION CLCLIMB 1 GL15508XJ E2318 MWS DIMMING INOP ON TAKEOFF ROLL. REPLACED LIFT SPOILER SWITCH. 2H74 4F RTA49EU 20050415002132005041500213EU 2005 4 15 MALA050218 120050121A2611 SMOKE DETECTOR BAC 146 AVRO146RJ85A1500097EU LAVATORY MALFUNCTIONED A MALAO OTHER N FALSE WARNING CLCLIMB 1 GL15522XJ E2347 DURING CLIMB-OUT OF DTW, THE FWD LAV SMOKE DETECTOR WENT OFF. THE FWD FA INVESTIGATED AND FOUND NO SMOKE IN LAV AND SMOKE DETECTOR STOPPED AND NEVER WENT OFF AGAIN. THE AFT FA REPORTED SEEING A HAZE IN FWD CABIN AND THEN IT DISSIPATED QUICKLY. NO ONE REPORTED ANY SMELL OF ANY KIND (CREW OR PASSENGERS). A/C RETURNED TO DTW FOR PRECAUTIONARY REASONS. GROUND RAN AC FOR 20 MIN WITH ALL SYSTEMS ONLINE GENS, HYD, AIR ECT. NOTED NO DISTINCTIVE ODOR OR VISUAL HAZE IN CABIN OR FLT DECK. INSPECTED LAV BOTTLES AND ALL CABIN EMERGENCY EQUIPMENT. ALL CHECKS GOOD. FOR PRECAUTIONARY MEASURES REPLACED FWD LAV SMOKE DETECTOR 2H74 4F RTA49EU 20050415002142005041500214EU 2005 4 15 MALA050203 120050130A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15422XJ 340B422 DURING 4Y/2Y CHECK IN BNA, FOUND SEAT TRACK AT BLO IS CORRODED OUT OF LIMITS FROM FS 294 TO FS 319 AND HAS BEEN REPAIRED IAW SRM 53-70-60. REF EAMS WORK ORDER 211546 TASK 1515. 2L72 4T RTA52EU 20050415002162005041500216EU 2005 4 15 MALA050204 120050130A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15422XJ 340B422 DURING 4Y/2Y CHECK IN BNA, FOUND SEAT TRACK AT LBL 18.3 IS CORRODED FROM FS 294 TO FS 319. DAMAGED AREAS HAVE BEEN REPAIRED IAW SRM 53-70-60 REF. EAMS WORK ORDER 211546 TASK 1516. 2L72 4T RTA52EU 20050415002172005041500217EU 2005 4 15 MALA050205 120050130A53207253711245 STRUCTURE SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15422XJ 340B422 DURING 4Y/2Y CHECK IN BNA, FOUND LT WRAP AROUND PN 7253711-245 IS CORRODED OUT OF LIMITS AND HAS BEEN REPLACED WITH A NEW PART IAW SRM 51-40-21. REF EAMS WORK ORDER 211546 TASK 1516. 2L72 4T RTA52EU 20050415002192005041500219EU 2005 4 15 MALA050198 120050123A2611 SMOKE DETECTOR SAAB SF340 340B 7860101EU CARGO BAY MALFUNCTIONED A MALAO OTHER N FALSE WARNING NRNOT REPORTED 1 GL15410XJ 340B410 AFTER STARTING NR 2 ENGINE CREW NOTED CARGO SMOKE LIGHT WAS ILLUMINATED. FA INVESTIGATED. NO SMOKE FOUND. CREW HAD RAMP AGENTS CHECK CARGO BAY AND NO SMOKE WAS FOUND IN CARGO BAY. LIGHT STAYED ON WITH NO SMOKE IN CARGO BAY. REPLACED NR 2 CARGO BIN SMOKE DETECTOR IAW SF340 MM. ALL CHECKS GOOD AT THIS TIME. 2L72 4T RTA52EU 20050415002212005041500221EU 2005 4 15 MALA050206 120050131A5320 FLOOR SUPPORT SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15422XJ 340B422 DURING 4Y/2Y CHECK IN BNA, FOUND FLOOR SUPPORT FLANGE AT PAX DOOR THRESHOLD IS CORRODED OUT OF LIMITS. DAMAGE IS ACCEPTABLE PER EMAIL FROM MESABA ENGINEER, KEN SEVERSON, DATED 2/1/05. REF EAMS WORKORDER 211546 TASK 1517. 2L72 4T RTA52EU 20050415002222005041500222EU 2005 4 15 MALA050207 120050207A3020 DUCT SAAB SF340 340B 7860101EU LT ENGINE BURNED A MALAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL15439XJ 340B439 LEFT INTAKE CAUTION LIGHT ON AND CYCLED OFF. ODOR NOTED ABOUT 5 MN LATER IN FLT DECK. ON POST FLT NOTED DAMAGE TO LEFT INTAKE. REMOVED AND REPLACED BURNED LEFT LOWER INTAKE DUCT, SN OFF L169235 SN ON L198068. ALL CHECKS GOOD. 2L72 4T RTA52EU 20050415002232005041500223EU 2005 4 15 MALA050208 120050124A3150 MONITOR SAAB SF340 340B 7860101EU COCKPIT MALFUNCTIONED A MALAO OTHER N FALSE WARNING CRCRUISE 1 GL15446XJ 340B446 LEFT PITOT LIGHT ILLUMINATED IN FLIGHT. QRH COMPLETED. RETURNED TO DTW. REMOVED AND REPLACED 5HG CURRENT MONITOR, PN ON/OFF 006WS00 SN 1581, SN OFF 1627. LEFT PITOT TUBE PN ON/OFF 856ML3, SN ON 214837, SN OFF 215686. ALL CHECKS GOOD IAW SF 340 M/M CH 31 AND 34. 2L72 4T RTA52EU 20050415002252005041500225EU 2005 4 15 MALA050219 120050126A3610 WARNING LIGHT BAC 146 AVRO146RJ85A1500097EU NR 3 ENGINE ILLUMINATED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15523XJ E2348 ENG NR 3 AIR FAULT OCCURED DURING AIR SWITCH OVER ON DEPARTURE. EITHER OVER TEMP OR OVER PRESSURE INDICTION REST, RESECURED. AIR TURNBACKPERFORMED OPS CHECK OF NR 3 ENG AIR VALVE IAW AMM 36-11-11. COULD NOT DUPLICATE. 2H74 4F RTA49EU 20050415002272005041500227EU 2005 4 15 MALA050222 120050128A2710 TAB BAC 146 AVRO146RJ85A1500097EU ELEVATOR SERVO LOOSE A MALAO OTHER E VIBRATION/BUFFET CRCRUISE 1 GL15513XJ E2329 YOKE VIBRATED BACK AND FORTH AT SPEEDS OF 250KTS AND GREATER. AS THE SPEED INCREASED THE VIBRATION INCREASED. RETURNED TO DTWUPON INSPECTION FOUND MISSING HARDWARE ON LT ELEVATOR SERVO TAB CAUSING PLAY. REPLACED MISSING HARDWARE. ALL CHECKS GOOD. ALL WORK DONE IAW AVRO MM CHP 27. 2H74 4F RTA49EU 20050413000112005041300011EA 2005 4 13 ASOA05251 120050321A5260601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 DURING AN A-CHECK IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050413000382005041300038EU 2005 4 13 ASOA05232 120050313A7712311649902 SENSOR AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE NR 2 MALFUNCTIONED A ASOAK NONE J WARNING INDICATION CRCRUISE 1 SO27632AS 338 127029 FLT 9953 - DURING CRUISE INTO ATL FROM MCN, JUST PRIOR TO INITIATION OF DESCENT THE CREW NOTICED THE RIGHT ENGINE BEGAN SURGING. THE CREW OBSERVED THE TORQUE NEEDLE RISE TO AT LEAST 120 PERCENT WHILE THE DIGITAL TORQUE INDICATION READ BETWEEN 0 PERCENT TO 40 PERCENT. DURING TH SURGES, THE CREW OBSERVED ITT LIGHT ILLUMINATE AND FELT A MOMENTARY YAW. THE SURGES CONTINUED INTERMITTENTLY AFTER THE POWER LEVER WAS RETARDED. THE QRH WAS COMPLIED WITH AND THE CREW SHUTDOWN THE RIGHT ENGINE AS A PRECAUTION. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE NR 2 TORQUE MONITOR SENSOR ON THE RIGHT ENGINE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T4 TRTA53EU E20NE 20050413000472005041300047EA 2005 4 13 ASOA05230 120050307A5320 SILL CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27702EV 10035 DURING HANGAR MAINTENANCE IN CKB, THE RIGHT OUTBOARD FLOOR SILL PLATE AT FS 280 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THR RIGHT OUTBOARD FLOOR SILL PLATE AT FS 280 IAW BOMBARDIER REO 670-53-21-086. (M) 2L72 4F RTA21EA 20050413000482005041300048EA 2005 4 13 ASOA05245 120050317A78302285074115 SWITCH CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER OUT OF RIG A ASOAK NONE N FALSE WARNING CRCRUISE 1 SO27854AS 7832 FLT 9953 - DURING A HOLDING PATTERN OVER ATL FROM MOB WITH THE RIGHT THRUST REVERSER DEFERRED IAW MEL NR 78-30-01, THE CREW RECEIVED A RT REVERSE UNLOCKED MSG. THE REFERENCED MEL STATES THIS TYPE CAUTION MESSAGE CAN OCCUR CONTINUOUSLY OR INTERMITTENTLY DURING AIRCRAFT OPERATIONAL. BECAUSE OF THE CREWS CONCERN OVER THE EXTENDED HOLDING PATTERN AND THE CAUTION MESSAGE RECEIVED, THE CREW DECLARED AN EMERGENCY. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE RERIGGED THE STOW SWITCH ON THE RIGHT ENGINE THRUST REVERSER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050413000512005041300051EA 2005 4 13 ASOA05223 120050310A5260601R3198045 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27830AS 7236 FLT 4213 - DURING A GROUND INSPECTION IN ATL, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050413000602005041300060SO 2005 4 13 SIMA200507513 120050311A5320145217725613 SILL EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21700LE 145156 ABI - DURING INSPECTION OF AIRCRAFT, THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED FORWARD SILL. INSTALLED SERVICEABLE SILL IAW EMB 145 (SRM-145/1142 REV 28, CHAPTERS 51-20-03, 51-40-06 AND 51-40-02. (M) 2L72 4F RTT00011AT 20050413000632005041300063SO 2005 4 13 SIMA200507002 120050310A335020131A POWER SUPPLY EMB 145 EMB145LR 3260212SO CABIN DISCHARGED A SIMAK NONE L NO TEST TXTAXI/GRND HDL 1 SW21617AE 145093 AFT TWO EMERGENCY LIGHTING STRIPS WILL NOT ILLUMINATE DURING TEST. REPLACED THE NR 4 EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20050413000712005041300071SO 2005 4 13 SIMA200507510 120050306A532014525381003 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21655AE 145452 ABI - DURING INSPECTION OF AIRCRAFT, THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED THE CORROSION BY MAKING A CUTOUT. FABRICATED AN EXTERNAL DOUBLER, FILLER, THREE SHIMS AND PLATE. REPAIR DONE IAW EMB SRM, SRM EMB-145/1142 REV 28, CHAPTER 53-21-10. (M) 2L72 4T RTT00011AT 20050413000732005041300073SO 2005 4 13 SIMA200507511 120050308A53302024T3 SKIN EMB 145 EMB145LR 3260212SO FUSELAGE DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21665BC 145783 ABI - DURING A DROP IN REPAIR, AIRCRAFT ARRIVED FOR REPAIR OF ACCIDENTAL DAMAGE ON THE RT AFT FUSELAGE BETWEEN FRAMES 71 AND 73 AND BETWEEN STRINGERS 15R AND 17R. PERFORMED A CUTOUT OF THE SKIN TO REMOVE THE DAMAGE. FABRICATED A FILLER, DOUBLER, FAIL/SAFE STRAP AND SHEAR CLIP. REPAIR DONE IAW EMB REPAIR SATEMENT IC2005-145/1186 DATED MARCH 5, 2005 AND IC2005-145/1208 DATED MARCH 7, 2005. (M) 2L72 4T RTT00011AT 20050413000772005041300077SO 2005 4 13 SIMA200507523 120050310A532013500437003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21705AE 145184 SAW - DURING CPCP INSPECTION FOUND, CENTER OMEGA HAS CORROSION UNDER CROSS BEAM AT FRAME 29. REMOVED AND REPLACED OMEGA BEAM, IAW EMB 135 SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050413000832005041300083SO 2005 4 13 SIMA200506609 120050307A335020131A BATTERY PACK EMB 135 EMB135KL 3260302SO CABIN DISCHARGED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21816AE 145552 ALB - FLT 4155 - CREW REPORTED THE FIRST THREE STRIPS OF FLOOR PROXIMITY EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED FOUR BATTERY PACKS IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050413000842005041300084SO 2005 4 13 SIMA200507517 120050307A532014521725013 SILL EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21705AE 145184 SAW - DURING CPCP INSPECTION, FOUND SERVICE DOOR FORWARD HAS AREAS OF CORROSION. RAI'D SILL IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050413000862005041300086SO 2005 4 13 SIMA200507516 120050307A532014521721005 STRUCTURE EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21705AE 145184 DURING CPCP INSPECTION, FOUND DIGITAL FORWARD OF FRAME 15 IS CORRODED. RAI'D DIGITAL FORWARD OF FRAME 15 IAW SRM 53-21-10. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050413000912005041300091SO 2005 4 13 SIMA200507518 120050307A5320 DOUBLER EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21705AE 145184 SAW - DURING CPCP INSPECTION, FOUND LEFT OMEGA BEAM AT FRAME 20 HAS CORRODED REPAIR DOUBLER. REMOVED, FABRICATED AND INSTALLED NEW DOUBLER IAW EMB SRM 53-21-10. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050413000932005041300093NM 2005 4 13 USAA050371 120050311A5347 SEAT TRACK BOEING767 767201 1385125NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19648US68950 23900 BFM - FOUND SEAT TRACK CORRODED 1.40 INCH LONG BY .70 INCH WIDE BY .085 INCH DEEP AND 1.30 INCH LONG BY .071 INCH, BS 257 RBL 30, 52.5, 59 FLOOR LEVEL MAIN CABIN. T-CAP REPAIR, 4 STRAPS, 2 ANGLES. (M) 2L72 4F RTA1NM 20050414000062005041400006 2005 4 14 UPS05144240 420050406A2565 HANDLE AIRBUSA300 A300F4622R 3930360EU ESCAPE SLIDE STUCK A IPXAK NONE O OTHER ININSP/MAINT 1 SO01127UP 0811 UNABLE TO DISARM SLIDE. LUBRICATED ARMING HANDLE, ARMED & DISARMED SLIDE SEVERAL TIMES. CHECKED ESCAPE SLIDE IAW MM 25-61-20-6, FOUND SATISFACTORY. 2L72 4F RTA35EU 20050414000072005041400007WP 2005 4 14 UPS05844238 120050406A5230 LATCH DOUG DC8 DC873F 302199FWP MAIN CARGO DOOR DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 INSPECTION TYPE:N/A ON MAIN CARGO DOOR LATCH ACTUATING BEAM BOLT HOLE ELONGATED 3RD AFT. ACCOMPLISHED MAIN CARGO DOOR LATCH WALKING BEAM REPAIR AS PER EO DC8-5230-1803-M. DOOR OPERATES NORMAL. 2L74 4F RT4A25 20050414000092005041400009NM 2005 4 14 UPS05M44250 120050408A2560 SMOKE GOGGLES DOUG MD11 MD11 3023602NM COCKPIT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP 48579 INSPECTION TYPE:N/A, F/O'S SMOKE GOGGLES ARE CRACKED. REPLACED SMOKE GOGGLES. 2L73 4F RTA22WE 20050414000182005041400018WP 2005 4 14 UPS05844254 120050317A53403750497 FITTING DOUG DC8 DC873F 302199FWP KEELBEAM CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE: C2, FWD ACCESSORY COMPT FS 660 LT KEELBEAM ATTACH FITTING HAS 2.50 INCH CRACK ON VERTICAL FLANGE BETWEEN ATTACH BOLTS HEADS. REMOVED CRACKED ATTACHMENT FITTING, FABRICATED REPLACEMENT FITTING IAW DWG 3750497 AND INSTALLED IAW DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20050414000192005041400019WP 2005 4 14 UPS05844256 120050324A53403755847U1 FITTING DOUG DC8 DC873F 302199FWP DOOR FRAME CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE: C2, AFT CARGO DOOR -C- LOWER DOOR JAMB CUTOUT AFT REAR LOWER CORNER CORRODED. REMOVED CORROSION FOUND OUT OF LIMITS IAW DC-8 SRM 53-2-0 FIG 1F. REMOVED AND REPLACED FITTING IAW DC-8 SRM 53-1-0, 51-3-2, 51-1-20D, 51-1- 21, & 51-3-0. 2L74 4F RT4A25 20050414000332005041400033NM 2005 4 14 ASMF200502001 120050203A291079138605505 RELIEF VALVE DOUG MD80 MD83 3023681NM HYD SYSTEM FAILED W ASMFD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SW23831LF14761 53050 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING PUSH BACK, CAPTAIN REPORTED LOST OF HYDRAULIC PRESSURE AND QUANTITY. DURING CHECK WAS DETECTED A LEAK FROM THE LEFT HYDRAULIC RELIEF VALVE, IT WAS REPLACED IAW MM 29-10-12, TESTED CORRECT. 2L72 4F RT 20050414000352005041400035WP 2005 4 14 ASMF200502003 120050206A2910 VALVE DOUG DC9 DC982 3022082WP HYD SYSTEM LEAKING W ASMFK NONE KJ FLUID LOSS WARNING INDICATION ININSP/MAINT 1 SW231003Y 48068 DURING TRANSIT CHECK WERE DETECTED HYDRAULIC LEAK AT RIGHT MAIN LANDING GEAR IN VALVE LOCKOUT. THE VALVE LOCKOUT WAS REPLACED IAW MM 32-42-06, TESTED CORRECT. CORRECT, DEFERRED REPORT WAS CLOSED 2L72 4F A6WE 20050414000412005041400041NM 2005 4 14 ASMF200503003 120050304A2450 CIRCUIT BREAKER DOUG MD88 MD88 3023688NM COCKPIT TRIPPED W ASMFK NONE H ELECT. POWER LOSS-50 PC ININSP/MAINT 1 SW23160PL 49763 CAPTAIN REPORTED THAT PEDESTAL OF INTEGRAL LIGHTS WAS OUT SERVICE. THE SYSTEM WAS VERIFIED WITH OTHER CONTROL PANEL AND FAIL CONTINUED. THE CIRCUIT BREAKERS B1-309, B1-310 AND B1-311 WERE ADJUSTED AND FAIL CONTINUED. THE FEEDING LINES AND VOLTAGES IN CIRCUIT BREAKERS WERE VERIFIED AND THE CIRCUIT BREAKER B1-311 WAS DETECTED OPEN. THE CIRCUIT BREAKER B1-311 WAS REPLACED IAW WDM 33-16-06, TESTED CORRECT. 2L72 4F RTA6WE 20050414000472005041400047NE 2005 4 14 ASMF200504003 220050405A732176960615 FUEL CONTROL DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE RIGHT ENGINE FAILED W ASMFD RETURN TO BLOCK RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SW23755RA364835297 49727 725614 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING RIGHT ENGINE STARTED, ACCELERATION INCREASED SLOWLY. THE RIGHT ENGINE WAS VERIFIED AND FOUND ALL CORRECT. THE FCU WAS REPLACED IAW MM 73-20-01 AND ACCELERATION CHECK WAS PERFORMED IAW 71-00-00, ALL CORRECT. DUE TO THE TYPE OF FAILURE, RIGHT ENGINE WAS REPLACED IAW 71-00-02, TESTED CORRECT. 2L72 4F4 FRTA6WE E9NE 20050414000492005041400049WP 2005 4 14 ASMF200504005 120050408A801138334211 STARTER DOUG DC9 DC987 3022087WP RT ENGINE FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23755RA3963016494 49727 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING RIGHT ENGINE STARTED, THE A AND B IGNITION SYSTEM DID NOT HAVE ROTATION IN N1 AND N2 AND HYDRAULIC PRESSURE DID NOT INCREASE. DURING REVISION, THE RIGHT ENGINE WAS STARTED WITH NEGATIVES RESULTS, STARTER VALVE LIGHT TURNED ON AND OSCILLATION OF PNEUMATIC PRESSURE WITHOUT ROTATION. THE ENGINE AIR TURBINE STARTER WAS REPLACED IAW MM 80-10-01, TESTED CORRECT. 2L72 4F RTA6WE 20050414000912005041400091NM 2005 4 14 2005UALA00074 120050115A5330 SKIN BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29907UA 25007 DENT FOUND AT LT SIDE OF FUSELAGE 3 FT AFT OF DOOR 1L SILL. CUT-OUT DAMAGE AND INSTALLED DOUBLER AND TRIPLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20050414001182005041400118 2005 4 14 TXER099081 420050115A2562182051309 ELT UROCOPEC155 EC155B 8681000EU CABIN INOPERATIVE B TXERO OTHER O OTHER NRNOT REPORTED 1 SW09588CF 6662 ELT FAILS TEST MODE. 1G72 3U H10EU 20050414001202005041400120 2005 4 14 TXER099084 420050102A34231007KCA1 COMPASS UROCOPEC155 EC155B 8681000EU COCKPIT BROKEN B TXERO OTHER O OTHER NRNOT REPORTED 1 SW09588CF 6662 COMPASS MOUNT FLANGE BROKEN. 1G72 3U H10EU 20050415000512005041500051NM 2005 4 15 DLM88050070 120050131A21308597221 CONTROL VALVE DOUG MD88 MD88 3023688NM RT A/C PACK FAILED A DALAB EMER. DESCENT J WARNING INDICATION DEDESCENT 1 SO27930DL 49717 LOST ALL CABIN PRESSURIZATION DESCENDING THRU FL260, ON INITIAL DESCENT MASKS DROPPED CABIN ALTITUDE REACHED 14500 FT. CREW USED CREW OXYGEN. FLIGHT ATTENDANT REPORTED HUGE GAP IN 2L DOOR SEAL AND THE SOUND OF RUSHING AIR. REPLACED BROKEN SENSE LINE ON RT PACK FLOW CONTROL VALVE. 2L72 4F RTA6WE 20050415000622005041500062NM 2005 4 15 DL76G050088 120050205A7830681L270G08 THRUST REVERSER BOEING767 7673P6 1385105NM NR 2 ENGINE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27153DL 24985 0 WHILE T/S NBR 2 ENG T/R NOT STOWING, FOUND DAMAGE TO RIGHT T/R COWL. REPLACED REVERSER. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS. 2L72 4F RTA1NM 20050415000662005041500066NM 2005 4 15 WRLA2005013 120050131A5347 SEAT TRACK DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11273 48519 DURING "C2" CHECK, FOUND CABIN SEAT TRACK CORROSION BETWEEN STA 865 AND STA 880 X=-8.5. CUT AND REMOVED SECTION BETWEEN STA 832 AND 929 X=-8.5, FABRICATED AND INSTALLED NEW SEAT TRACK SECTION AND SPLICE HAT. CONDITION CHECK SATISFACTORY REF MD11 SRM 53-70-00 FIG 1 REV 36 VOL I. 2L73 4F4 FRTA22WE E24NE 20050415000742005041500074CE 2005 4 15 DGCA05020 120050210A2430A2017 CONTROL BOX RKWELLNA265 NA26565 7630107CE MALFUNCTIONED E DGCAA UNSCHED LANDING GJ MULTIPLE FAILURE WARNING INDICATION CLCLIMB 1 CE03265M 1301313013 46531 DC VOLTAGE "SPIKE", CAUSING MULTIPLE COMPONENT/SYSTEM FAILURES, CIRCUIT BREAKERS POPPING. 2L72 4J A2WE 20050415000792005041500079 2005 4 15 2005F00059 420050211A3445066011460101 PROCESSOR LEAR 35 31A 5170531CE TCAS INCORRECT E K NONE W INADEQUATE Q C NRNOT REPORTED 1 SW1331MW 171 FAR 91, APPENDIX G, SECTION 2 REQUIRES THAT FOR AN AIRCRAFT TO USE TCAS II IN RVSM AIRSPACE, THE SYSTEM MUST BE "VERSION 7.0" WHICH IS IN COMPLIANCE WITH TSO C 119B. ALTHOUGH TCAS II IS NOT REQUIRED FOR RVSM COMPLIANCE, IF IT IS INSTALLED, IT MUST BE UPDATED TO THE CORRECT VERSION. THIS AIRCRAFT IS RVSM COMPLIANT AND APPROVED, BUT DID NOT HAVE THE TCAS PROCESSOR UPDATED AT THAT TIME. THE RULE IN PART 91 IS RATHER OBSCURE AND HAS GENERATED SOME CONFUSION AS TO WHAT IS REQUIRED. I SUGGEST THAT THIS DETAIL BE PRESENTED MORE CLEARLY TO THOSE INVOLVED WITH THOSE COMPLYING WITH RVSM REQUIREMENTS AND ALSO TO THE FAA PERSONNEL APPROVING THOSE AIRCRAFT. 2L72 4F RTA10CE 20050415000862005041500086 2005 4 15 P9RA20050068 420050212A2565284N14201 PROXIMITY SENSOR BOEING757 757236 1384971NM GIRT BAR DIRTY A P9RAO OTHER P NO WARNING INDICATION NRNOT REPORTED 1 SO11522NA 25133 CANCUN - AFTER LANDING, FLIGHT ATTENDANT NOTICED R1 DOOR SLIDE LIGHT WAS NOT ILLUMINATED. ITEM DEFERRED PER MEL 25-66-5. INSPECTED, CLEANED GIRT BAR PROXIMITY SWITCHES. OPS CHECKED GOOD. CLEARED MEL 25-66-5. 2L72 4F RTA2NM 20050415000882005041500088WP 2005 4 15 WX0500018 120050208A339758791 WIRE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT BROKEN A WX0AK NONE O OTHER ININSP/MAINT 1 WP19863GA 49911 DEN - MAINTENANCE REPORTED EMERGENCY FLOOR LIGHTS INOPERATIVE FROM SEAT ROW 10 TO 19. RIBBON WIRE BROKEN IN SEAT TRACK AT ROW 11. MAINTENANCE REPLACED LEAD WIRE ASSEMBLY AND INSTALLED FLEXIBLE LAMP. SYSTEM OPERATIONALLY CHECKED GOOD IAW 33-53-01. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050415000922005041500092NM 2005 4 15 2005UALA00120 120050205A5322 SHEAR TIE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29578UA 26694 FUSELAGE AT FRAME STA 640, FWD SHEAR TIE IS CRACKED AT STR 16L. SUPPLEMENTAL DATA UPDATE SHEAR TIE CRACKED DUE TO IMPACT DAMAGE. MAJOR REPAIR ACCOMPLISHED. SHEAR TIE WAS FABRICATED AND REPLACED. 2L72 4F4 FRTA2NM E17NE 20050415001032005041500103NM 2005 4 15 TSAA0526005 120050211A269787858201 CONNECTOR BOEING737 737209 13844AENM FIRE DETECTOR DEFECTIVE A TSAAE ENGINE SHUTDOWN N FALSE WARNING LDLANDING 1 WP13827AL 23913 FLT 71, HNL-OGG - THE NR 2 ENGINE FIRE WARNING LIGHT CAME ON INTERMITTENTLY DURING FLIGHT. DECIDED TO RETURN TO HNL. THE NR 2 ENGINE FIRE WARNING LIGHT CAME ON STEADY AT TOUCHDOWN. ENGINE SHUTDOWN. BOTTLE DISCHARGED. REPLACED THE NR 2 ENGINE FIRE DETECTOR SENSOR CONNECTORS. SYSTEM TEST WITH ENGINE RUN FOUND NORMAL. OK FOR SERVICE. REPLACED THE FORWARD AND AFT POSITION ENGINE FIRE EXTINGUISHER BOTTLES PER MM 26-21-11. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA16WE 20050415001222005041500122WP 2005 4 15 AALA20050094 120050207A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21489AA 49682 DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT 14D. REPLACED SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT 14D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050415001252005041500125CE 2005 4 15 2003795 120050214A5344129440493 HINGE BEECH 1900 1900D 1154162CE CARGO DOOR SHEARED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03179GL UE179 DURING ROUTINE STRUCTURAL INSPECTION, CARGO DOOR HINGE HAD SHEARED RIVIT AND BROKEN LUG. CARGO DOOR HINGE WAS REPLACED, AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA24CE 20050415001302005041500130NM 2005 4 15 WRLA2005037 120050211A5513 SKIN DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST RT BARREL NUT HOLE NR 31. 2L73 4F4 FRTA22WE E24NE 20050415001452005041500145NM 2005 4 15 WRLA2005054 120050214A5512 SKIN DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST LT BARREL NUT HOLE NR 12. 2L73 4F4 FRTA22WE E24NE 20050415001552005041500155NM 2005 4 15 WRLA2005066 120050207A5714 SKIN DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE CENTER WING CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK INSPECTION, FOUND CORROSION IN CENTER WING SECTION UPPER SURFACE AT S-15 STR X=47.5 TO X=-47.5. 2L73 4F4 FRTA22WE E24NE 20050415001602005041500160NM 2005 4 15 WRLA2005042 120050214A5512 SKIN DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST RT BARREL NUT HOLE NR 18. 2L73 4F4 FRTA22WE E24NE 20050415001722005041500172EA 2005 4 15 QXEA200500177 120050121A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - RIGHT HAND OUTBOARD SIDE FACING SEAT RAIL AT STATION X739, HAS PITTING CORROSION ON MOST INBOARD SURFACE. REPAIRED IAW CRJ 700 SRM 51-21-06-001-001-A01 AND HORIZON AIR EA R-53-266. 2L72 4F RTA21EA 20050415001762005041500176NM 2005 4 15 QXEA200500293 120050224A2751 WARNING LIGHT BOMBDRDHC8 DHC8401 1390041NM TE FLAPS FALSE ACTIVATIONA QXEAO OTHER N FALSE WARNING APAPPROACH 1 NM09414QX7889 4061 LAX - FLIGHT 2343 - THE CHECKLIST WAS COMPLIED WITH WHEN ON APPROACH THE FLAP POWER CAUTION LIGHT ILLUMINATED. MAINTENANCE INSPECTED THE AIRCRAFT AND ACCOMPLISHED THE FLAP POWER NUISANCE CAUTION LIGHT RESET PROCEDURE. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050415001802005041500180EA 2005 4 15 QXEA200500188 120050124A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - RIGHT INBOARD SEATRAIL, AT STATION X349 TO X379, HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01, REO 670-53-00-060, REV B AND HORIZON AIR EA R-53-266, SECTION 1. 2L72 4F RTA21EA 20050415001812005041500181NM 2005 4 15 HNAA0500015 120050223A792128E998 OIL COOLER DHAV DHC8 DHC8102 2809003NM NR 1 ENGINE LEAKING A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07906HA 9 NR 1 ENGINE OIL PRESSURE WARNING LT ILLUMINATED ON CLIMB-OUT. POWER REDUCED AND ENGINE S/D AT 40 PSI. REMOVED AND REPLACED ENGINE OIL COOLER. FERRIED TO MDT FOR ENGINE REMOVED AND REPLACED. 2H72 4T RTA13NM 20050415001832005041500183NM 2005 4 15 05FDEA00317 120050225A3240 WARNING LIGHT DOUG MD11 MD11 3023602NM MLG BRAKES FALSE ACTIVATIONA FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25580FE 48471 BRAKE OVERHEAT ALERT ON T/O. PUT GEAR BACK DOWN LIGHT WENT OUT. BRAKE NR 9 INITIALLY BLANK THEN 130 DEGREES WHEN LIGHT WENT OUT. T/O ROLL WAS NORMAL. NO CURRENT FAULT SHOWN IN BTMTP. PERFORMED RTS OF BTMTPI IAW MM 32-46-00-700,TEST PASSED. PERFORMED VISUAL INSPECTION OF BRAKE NR 9 IAW MM 32-43-20. NO DAMAGE FOUND. 2L73 4F RTA22WE 20050415001962005041500196EU 2005 4 15 AWXA200500274 120050217A5315D5347209200000 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28647AW 762 MCN - MAJOR REPAIR - DURING 8-DAY CHECK, CORROSION WAS FOUND ON FLOORBEAM Y29 AT FS 68. MAINTENANCE REMOVED CORRODED FLOORBEAM Y29 AT FS 68; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11. 2L72 4F RTA28NM 20050415001992005041500199EU 2005 4 15 AWXA200500277 120050211A5315D5347229800000 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28647AW 762 MCN - MAJOR REPAIR - DURING 8-DAY CHECK, CORROSION WAS FOUND AROUND MOUNT HOLE OF FLOORBEAM -Y18 BETWEEN FS 68 AND FS 69. MAINTENANCE REMOVED CORRODED FLOORBEAM -Y18 FROM FS 68 TO FS 69; FABRICATED A NEW REPLACEMENT FLOORBEAM, INSTALLED REPAIR PART IAW A320 SRM 51-42-11. 2L72 4F RTA28NM 20050415002022005041500202NM 2005 4 15 AWXA200500280 120050220A5315D53472188204 FLOORBEAM AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28812AW 1178 SAL - MAJOR REPAIR - DURING BC-4 CHECK, EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM Y1292 AT FR 68 -3". MAINTENANCE REMOVED CORRODED FLOORBEAM Y1292 FROM FS 68 -3" TO FS 69. FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050415002202005041500220EU 2005 4 15 MALA050199 120050127A3350 POWER SUPPLY SAAB SF340 340B 7860101EU EMERGENCY LIGHT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15412XJ 340B412 EMERGENCY POWER SUPPLY 20LN FAILED CAPACITY CHECK IAW JOB CARD 335003. 2L72 4T RTA52EU 20050415002242005041500224EU 2005 4 15 MALA050210 120050122A2160 SENSOR SAAB SF340 340B 7860101EU RT DUCT TEMP MALFUNCTIONED A MALAO OTHER N FALSE WARNING CRCRUISE 1 GL15454XJ 340B454 IN FLIGHT RT BLEED FAULT ILLUMINATED WITH RT DUCT OVERTEMP. RAN QRH AND THEY CAME BACK ON. RETURNED TO MEM. REMOVED AND REPLACED RT DUCT TEMP SENSOR PN 754691-1 AND TEMP SWITCH PN M2035-501 IAW AMM CH 21. OPS CHECK GOOD. 2L72 4T RTA52EU 20050415002262005041500226EU 2005 4 15 MALA050221 120050224A3010 DEICE SYSTEM SAAB SF340 340B 7860101EU TAIL INOPERATIVE A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15438XJ 340B438 AIR RETURN DUE TO TAIL DEICE INOP. NO FURTHER INFORMATION AT THIS TIME. 2L72 4T RTA52EU 20050415000632005041500063NM 2005 4 15 DL76S050090 120050206A2560 STRAP BOEING767 767332 1382001NM FLASHLIGHT BROKEN A DALAK NONE O OTHER ININSP/MAINT 1 SO27127DL 24077 AFT LEFT FA JUMPSEAT EMERGENCY FLASHLIGHT STRAP BROKEN. REPLACED FLASHLIGHT AND STRAP. 2L72 4F RTA1NM 20050415000692005041500069NM 2005 4 15 WRLA2005015 120050131A5347 SEAT TRACK DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11273 48519 DURING "C2" CHECK FOUND CABIN SEAT TRACK CORROSION BETWEEN STA 840 AND STA 870 X=-27.5. CUT AND REMOVED CORRODED SECTION BETWEEN STA 832 AND 869 X=-27.5, FABRICATED AND INSTALLED NEW SEAT TRACK SECTION AND SPLICE HAT PER MD11 SRM 53-70-00 FIG 1 REV 36 VOL I. CONDITION CHECK SATISFACTORY. 2L73 4F4 FRTA22WE E24NE 20050415000702005041500070NM 2005 4 15 WRLA2005016 120050201A5512 SKIN DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11273 48519 DURING "C2" CHECK INSPECTION, FOUND CORROSION AT BARREL NUT HOLE NR 1 RT. REAMED SUBJECT BARREL NUT HOLE TO 1.594" DIA, PER SECTION 7 OF E/O 02-5510-098 REV 03 AND FABRICATED REPAIR BUSHING PER SECTION 12 OF SAME E/O. CLEANED AND REINSPECTED BOLT AND BARREL NUT, REINSTALLED BARREL NUT WITH NEW PL1 WASHER. CONDITION CHECK SATISFACTORY. 2L73 4F4 FRTA22WE E24NE 20050415000912005041500091WP 2005 4 15 WX0500015 120050204A2170 COALESCER BAG DOUG DC9 DC983 3022083WP CABIN AIR CONTAMINATED A WX0AA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP19865GA 49998 RNO TO YKM - CREW REPORTED STRONG SULPHURIC SMELL COMING OUT OF THE VENTS ON CLIMB-OUT. AIRCRAFT RETURNED TO RNO WHERE CREW REPORTED RUBBER/ACRID SMELL ON FINAL DESCEND. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND DIRTY COALESCER BAGS, MAINTENANCE REMOVED AND REPLACED COALESCER BAGS IAW MM 21-20-02. PERFORMED HIGH POWER RUNS AND COULD NOT DUPLICATE SMELL. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050415000942005041500094NM 2005 4 15 2005UALA00122 120050205A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29578UA 26694 FLOORBEAM T-CAP IS DAMAGED AT STA 1640, BL-0 TO RBL 61. SUPPLEMENTAL DATA UPDATE EXISTING REPAIR REQUIRED MODIFICATION. ORIGINAL DAMAGE CAUSED BY TYPICAL FLOORBEAM CORROSION. MAJOR REPAIR ACCOMPLISHED. REMOVED EXISTING REPAIR AND INSTALLED NEW T-CAP SECTION WITH SPLICE ANGLES AND STRAPS. 2L72 4F4 FRTA2NM E17NE 20050415000982005041500098NM 2005 4 15 2005UALA00126 120050207A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29578UA 26694 FLOORBEAM UPPER CAP IS CORRODED AT STA 365, RBL 16-73. SUPPLEMENTAL DATA UPDATE TYPICAL FLOORBEAM CORROSION DAMAGE. MAJOR REPAIR ACCOMPLISHED. REPAIRED USING NEW T-CAP SECTION AND SPLICE ANGLES. 2L72 4F4 FRTA2NM E17NE 20050415001152005041500115EA 2005 4 15 QXEA200500174 120050120A5753 FITTING CNDAIRCL600 CL6002C10 1390015EA ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - LEFT OUTBOARD FLAP INBOARD GUIDE ROLLER FITTING HAS FRETTING CORROSION AND GOUGED. REPAIED IAW HORIZON AIR EA R-57-93 AND REO 670-57-53-017. 2L72 4F RTA21EA 20050415001172005041500117EA 2005 4 15 QXEA200500176 120050121A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - RIGHT OUTBOARD SIDE FACING SEAT RAIL AT STATION X708, HAS PITTING CORROSION ON MOST INBOARD SURFACE. REPAIRED IAW HORIZON AIR EA R-53-266 AND REO 670-53-00-060, REV B. 2L72 4F RTA21EA 20050415001182005041500118WP 2005 4 15 AALA20050102 120050210A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217514A 49891 DFW - CEILING EMERGENCY LIGHTS AT ROWS 19 TO 21 AND BETWEEN AFT LAVATORY INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROWS 19 TO 21 AND BETWEEN AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050415001212005041500121WP 2005 4 15 AALA20050110 120050214A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21451AA 49477 DFW - EMERGENCY ESCAPE PATH LIGHTS AT SEATS 13B AND 18D INOPERATIVE. REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY FOR SEATS 13B AND 18D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050415001242005041500124CE 2005 4 15 2003794 120050214A5311 FRAME BEECH 1900 1900D 1154162CE FUSELAGE CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03179GL UE179 DURING ROUTINE STRUCTURAL INSPECTION, A 1.3 INCH FRAME CRACK WAS DISCOVERED AT FS 450 STRINGER 10R. REPAIRED CRACKED FRAME AREA, AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA24CE 20050415001422005041500142NM 2005 4 15 WRLA2005051 120050211A5512 SKIN DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST LT BARREL NUT HOLE NR 23. 2L73 4F4 FRTA22WE E24NE 20050415001492005041500149NM 2005 4 15 WRLA2005060 120050213A5347 SEAT TRACK DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK INSPECTION, FOUND CORROSION IN MAIN DECK SEAT TRACK AT STA 445, X=-87. 2L73 4F4 FRTA22WE E24NE 20050415001502005041500150NM 2005 4 15 WRLA2005062 120050213A5347 SEAT TRACK DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK INSPECTION, FOUND CORROSION IN MAIN DECK CARGO SEAT TRACK AT STA 838, X=75. 2L73 4F4 FRTA22WE E24NE 20050415001622005041500162WP 2005 4 15 AALA20050136 120050222A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT PINCHED A AALAK NONE O OTHER ININSP/MAINT 1 SW21483A 49676 RDU EMERGENCY ESCAPE PATH LIGHT IN AFT CABIN INOPERATIVE. FOUND PINCHED WIRE ON OUTBOARD SEAT TRACK. REPAIRED WIRE FOR EMERGENCY ESCAPE PATH LIGHT IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050415001862005041500186NM 2005 4 15 RYNA200500008 120050217A3150285T003430 CIRCUIT CARD BOEING757 757200 1384950NM WARNING SYSTEM DIRTY A RYNABA EMER. DESCENT UNSCHED LANDING P NO WARNING INDICATION CRCRUISE 1 CE07151GX 24451 AURAL WARNING BELLS SOUNDED, (NO FIRE WARNING LIGHTS). THE AIRCRAFT PERFORMED AN AIRTURNBACK AND LANDED SAFELY AT CUN AND THE AURAL WARNING CIRCUIT CARD WAS CLEANED, RESEATED AND OPERATIONALLY CHECKED NORMAL. 2L72 4F RTA2NM 20050415001892005041500189EU 2005 4 15 AWXA200500266 120050217A5315D534721892000 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28647AW 762 MCN - MAJOR REPAIR - DURING 8-DAY CHECK, CORROSION WAS FOUND ON FLOORBEAM -Y50 BETWEEN FS 68 AND FS 69. MAINTENANCE REMOVED CORRODED FLOORBEAM -Y50 FROM FS 68 TO FS 69; FABRICATED A NEW REPLACEMENT FLOORBEAM, INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050415001972005041500197EU 2005 4 15 AWXA200500275 120050215A5315D5347218820200 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28647AW 762 MCN - MAJOR REPAIR - DURING 8-DAY CHECK, CORROSION WAS FOUND AROUND FASTENER HOLES ON FLOORBEAM Y44 JUST FORWARD OF FS 68. MAINTENANCE REMOVED CORRODED FLOORBEAM Y44 AT FS 68; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11. 2L72 4F RTA28NM 20050415002002005041500200NM 2005 4 15 AWXA200500278 120050220A5315D53472172202 FLOORBEAM AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28812AW 1178 SAL - MAJOR REPAIR - DURING BC-4 CHECK, EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM Y1292 AT FS 67+3". MAINTENANCE REMOVED CORRODED FLOORBEAM Y1292 FROM FS 67+3" TO FS 68, FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050415002182005041500218EU 2005 4 15 MALA050196 120050129A3030 WARNING LIGHT SAAB SF340 340B 7860101EU LT ALPHA ILLUMINATED A MALAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL15368PX 340B274 LT "ALPHA" LIGHT AFTER T/O. AIR RETURN TO MEMPHIS DUE TO ICE RESTRICTION. 2L72 4T RTA52EU 20050415002372005041500237NE 2005 4 15 PCSA05041401 220050414A7210 HOUSING BOEING727 727212 138407GNM PWA JT8 JT8D17 52049NE GEARBOX STRIPPED A PCSAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SO29598AJ407673757 21947 688418 FLT 8414 ON APPROACH TO MIA CREW REPORTED NR 1 ENGINE LOST OIL, ENG. NR 1 WAS SHUTDOWN AS A PRECAUTION. A/C LANDED AT INTENDED DESTINATION WITHOUT FURTHER INCIDENT. MX INSPECTION OF THE NR 1 ENGINE FOUND OIL FILTER & GEARBOX CHIP DETECTORS HAD NO METAL, INSPECTION OF MAGNETIC CHIP DETECTORS IAW MM79-20-12. FOUND OIL PRESSURE TUBE AT MAIN OIL FILTER HOUSING LEAKING, REPLACED TORN O-RING, REPLACED MAIN OIL FILTER & O-RINGS & ACCOMPLISHED HELICOIL INSERT REPAIR ON GEARBOX PER PWC MM 72-61-01, RAN NR 1 ENGINE TO TAKE-OFF POWER 2.19 EPR, LEAK CHECK GOOD IAW MM 79-20-11, OIL PRESSURE 50 PSI ALL PARAMETERS NORMAL IAW AMERIJET FORM B-41, NR 1 ENG. OIL SAMPLE WAS TAKEN FOR SOAP TEST. AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 20050628001312005062800131EA 2005 6 28 ASOA05353 120050418A335020131A POWER SUPPLY CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE EMERGENCY LIGHTSDISCHARGED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27706EV 10054 DURING A GROUND INSPECTION, THE EMERGENCY LIGHTS WOULD NOT OPERATE WHEN SELECTED TO THE ON POSITION. MAINTENANCE CHARGE THE BATTERY PACKS. OPERATION CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA EOOO63EN 20050418001622005041800162EU 2005 4 18 USAA050271 120050205A5347DAN2001179511 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19671UW 0323 BFM - FOUND SEAT TRACK CORRODED, 3 INCH BY 1.5 INCH BY .026 INCH DEEP, CABIN FRAME 30-33, -Y953. CORROSION LEVEL 2, TASK C532134-01. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER SRM 53-00-15, FIG 202, FIG 101. (M) 2L72 4F RTA46NM 20050418001662005041800166EU 2005 4 18 USAA050008 120050101A21404E33592 ELEMENT AIRBUS330 A330323 3930335EU FLOOR PANEL CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW 0315 BFM - FOUND HEATED FLOOR PANEL ELEMENT WITH CORROSION FRAME 13A-16A, Y=-953 THROUGH -1456. FABRICATED REPLACED SKIN PER EA 96114 REV A. (M) 2L72 4F RTA46NM 20050418001672005041800167EU 2005 4 18 USAA050013 120050101A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW22421 0315 BFM - FOUND SEAT TRACK CORRODED .750 INCH LENGTH BY .500 INCH WIDE BY .035 INCH DEEP AREA, -Y450 FROM FRAME 68-72. CORROSION LEVEL 2, TASK NR J7-200-258OC. REMOVED AND REPLACED SEAT TRACK PER SRM 53-00-15, 51-42-11, 51-44-11, 51-21-11. (M) 2L72 4F RTA46NM 20050418001682005041800168EU 2005 4 18 USAA050014 120050101A5347F53476114201 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW22421 0315 BFM - FOUND SEAT TRACK APPROX 27 SQUARE INCH 18 LOCATIONS, FRAME 54-68, +Y450, MAIN CABIN SEAT TRACK. REMOVED AND REPLACED SEAT TRACKS PER SRM 53-00-15. CORROSION LEVEL 2, TASK NR J7-200-258OC. (M) 2L72 4F RTA46NM 20050418001722005041800172EU 2005 4 18 USAA050388 120050304A5347F5327563920000 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW22938 0337 BFM - FOUND SEAT TRACK CORRODED Y-1550 AT FRAME 32 AND FRAME 34. CORROSION LEVEL 2, TASK C532134-01. REMOVED AND REPLACED PER SRM 51-42-11. (M) 2L72 4F RTA46NM 20050418001732005041800173EU 2005 4 18 USAA050389 120050304A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW22938 0337 BFM - FOUND SEAT TRACK CORRODED 1.3 INCH WIDE BY 1.15 INCH LONG BY .032 INCH DEEP, 14.6 INCH WIDE BY 1.15L BY .003, BETWEEN FRAME 32-36 Y-950. CORROSION LEVEL 2, TASK C532134-01. FABRICATED NEW TRACK SECTION AND SPLICES PER SRM 53-00-15, FIG 204, SHEET 1 AND 2. (M) 2L72 4F RTA46NM 20050418001752005041800175NM 2005 4 18 USAA050367 120050311A5347143T52156 SEAT TRACK BOEING767 767201 1385125NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19648US68950 23900 BFM - FOUND SEAT TRACK CORRODED, 2 INCH BY 1 INCH BY .037 INCH AREA, STATION 412-740 LBL 88.50 CABIN FLOOR. (M) 2L72 4F RTA1NM 20050418001772005041800177NM 2005 4 18 USAA050373 120050311A5347145T521344 SEAT TRACK BOEING767 767201 1385125NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19648US68950 23900 BFM - FOUND SEAT TRACK CORRODED 1.5 INCH BY .7 INCH BY .035 INCH AND 1 INCH BY .5 INCH BY .033 INCH, CABIN FLOORBEAM STATION 785.9-830, RBL 88.5. INSTALLED NEW SEAT TRACK AND SPLICE REPAIR PER SRM 53-00-52 DWG 145T5213, SRM 53-00-52 FIG 203. (M) 2L72 4F RTA1NM 20050418001792005041800179EU 2005 4 18 USAA050380 120050306A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW22938 0337 BFM - FOUND SEAT TRACK CORRODED 4 INCH BY 1 INCH BY .050 INCH DEEP, FRAME 37, Y450, MAIN CABIN FLOOR. REMOVED DAMAGED SECTION, FABRICATED REPAIR SECTION AND SPLICES, INSTALLED REPAIR PARTS PER SRM 53-00-15. (M) 2L72 4F RTA46NM 20050418001802005041800180EU 2005 4 18 USAA050009 120050101A21404E33691 ELEMENT AIRBUS330 A330323 3930335EU FLOOR PANEL CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW 0315 BFM - FOUND HEATED FLOOR PANEL ELEMENT CORRODED, BETWEEN FRAME 53.5 - 53.7A, Y=1456-1959. FABRICATED REPLACEMENT SKIN PER EA 96114 REV A. (M) 2L72 4F RTA46NM 20050418001812005041800181EU 2005 4 18 USAA050010 120050101A21404E33681 ELEMENT AIRBUS330 A330323 3930335EU FLOOR PANEL CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW22421 0315 BFM - FOUND HEATED FLOOR PANEL ELEMENT CORRODED, FS 53.5-53.7A, Y=1959 - 2462. CORROSION LEVEL 1, TASK NR J7-270-53100-002. FABRICATED REPLACEMENT SKIN PER EA 96114 REV A. (M) 2L72 4F RTA46NM 20050418001822005041800182EU 2005 4 18 USAA050015 120050101A5347F53477214201 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW22421 0315 BFM - FOUND SEAT TRACK CORROSION .075 INCH LONG BY .5 INCH WIDE BY .036 INCH DEEP, FRAME 58-59, -Y450, -Z240. CORROSION LEVEL 2, TASK NR J7-200-2580C. REMOVED AND REPLACED SEAT TRACK PER SRM 51-74-00, 53-00-15. (M) 2L72 4F RTA46NM 20050418001842005041800184EU 2005 4 18 USAA050016 120050101A5347F5331140220001 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW22421 0315 BFM - FOUND SEAT TRACK CORRODED .017D BY .25W BY .5L AREA, BETWEEN FRAME 52-53, Y=-450 SEAT TRACK. CORROSION LEVEL 2, TASK J7-200-2578C. REMOVED AND REPLACED PER SRM 53-31-15, FIG 101 SH 8. (M) 2L72 4F RTA46NM 20050418001852005041800185EU 2005 4 18 USAA050017 120050101A5347F5347721020600 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW22421 0315 BFM - SEAT TRACK FOUND CORRODED .046 INCH DEEP BY .36 INCH WIDE BY 1.46 INCH LONG, FRAME 62-72, Y= -2462. CORROSION LEVEL 2, TASK NR J7-200-2580C. REMOVED AND REPLACED PER SRM 53-00-15 FIG 101 SHEET 2. (M) 2L72 4F RTA46NM 20050418001862005041800186NM 2005 4 18 USAA050391 120050323A5320 ANGLE BOEING767 7672B7 1385107NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19652US63776 24765 FOUND CHORD ANGLE CRACKED .0750 INCH, BS 287, LBL 25, 11.5 INCH BELOW CEILING. INSTALLED EXTRUDED SECTION REPAIR PER SRM 51-70-12. (M) 2L72 4F RTA1NM 20050418001892005041800189NM 2005 4 18 USAA050365 120050304A5347145T521344 SEAT TRACK BOEING767 767201 1385125NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19648US68950 23900 BFM - FOUND SEAT TRACK CORRODED 2.5 INCH BY .80 INCH WIDE BY .040 INCH DEEP, MAIN CABIN FLOOR, BS 855, RBL 88.5. CORROSION LEVEL 2, TASK C53-242-02. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER SRM 53-00-52, FIG 203/SRM 51-40-02. (M) 2L72 4F RTA1NM 20050418001912005041800191NM 2005 4 18 USAA050366 120050311A5347141T512169 SEAT TRACK BOEING767 767201 1385125NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19648US 23900 PIT - FOUND SEAT TRACK CORRODED 4 INCH BY 4 INCH BY .080 INCH AREA, CABIN FLOORBEAM STATION 355-422 RBL 54.75. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER SRM 53-00-52 PAGE 101, FIG 101 AND 206. (M) 2L72 4F RTA1NM 20050418001922005041800192NM 2005 4 18 USAA050447 120050310A5311 FRAME BOEING767 767201 1385125NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19648US68950 23900 BFM - FOUND FLOOR FRAME CORRODED 2 INCH LONG BY 1 INCH WIDE BY .050 INCH DEEP AREA, STATION 1109 RBL 14.5-RBL 45. REMOVED AND REPLACED CHORD SECTION, ADDING CHANNEL AND STRAP PER 53-00-07. (M) 2L72 4F RTA1NM 20050418001962005041800196EU 2005 4 18 USAA050018 120050101A5347F331140220001 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW22421 0315 BFM - FOUND SEAT TRACK CORRODED .018 INCH DEEP BY .25 INCH DEEP WIDE BY .5 INCH LONG AREA, FR 51, Y = -450 SEAT TRACK. CORROSION LEVEL 2, TASK NR J7-200-2578X. REMOVED AND REPLACED PER SRM 53-31-15 FIG 101 SHEET 8. (M) 2L72 4F RTA46NM 20050418002002005041800200EU 2005 4 18 USAA050274 120050129A5347F53275847200 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19671UW22760 0323 BFM - FOUND TRACK CORRODED 4 AREAS, TOTAL 8.5 SQUARE INCH, MAX D .060 INCH, FRAME 31-36, Y1959, MAIN CABIN FLOOR SEAT TRACK. REMOVED AND REPLACED SEAT TRACK PER SRM 53-00-15. (M) 2L72 4F RTA46NM 20050418002012005041800201EU 2005 4 18 USAA050260 120050205A5347F5347801100500 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19671UW22760 0323 BFM - FOUND SEAT TRACK BEAM CORRODED 2.5 INCH BY 1.5 INCH BY .040 INCH AREA, FRAME C75 AND FRAME C76 AT -Y450 MAIN CABIN FLOOR. REPLACED WITH NEW SUPPORT BEAM PER SRM 53-00-15. (M) 2L72 4F RTA46NM 20050418002042005041800204EU 2005 4 18 USAA050261 120050209A5315F53478222207 FLOORBEAM AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19671UW 0323 BFM - FOUND FLOORBEAM CORRODED 1 INCH BY .65 INCH BY .035 AND 1.5 BY .75 BY .037 INCH AREA, FRAME C76 -Y1470--Y1840 MAIN CABIN FLOOR. REPLACED WITH NEW BEAM PER SRM 53-41-14. (M) 2L72 4F RTA46NM 20050418002122005041800212EU 2005 4 18 USAA050385 120050306A5320F5347823420000 BEAM AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW22938 0337 BFM - FOUND BEAM CORRODED 1.5 INCH BY 1 INCH BY .022 INCH DEEP, FRAME 75, Y445, MAIN CABIN FLOOR. REMOVED AND REPLACED BEAM PER SRM 51-72-11. (M) 2L72 4F RTA46NM 20050418002132005041800213EU 2005 4 18 USAA050395 120050308A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW 0337 BFM - FOUND SEAT TRACK CORRODED 4 INCH BY 1.5 INCH AREA, FRAME 65 AT Y-1959. CORROSION LEVEL 2, TASK C534159-01. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR TRACK PER SRM 53-00-15, 51-23-11, 53-23-11. (M) 2L72 4F RTA46NM 20050418002142005041800214EU 2005 4 18 USAA050424 120050317A5347F53111701200 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW22938 0337 BFM - FOUND SEAT TRACK CORRODED 2.5 INCH LONG BY .75 INCH WIDE BY .040 INCH DEEP, MAIN CABIN SEAT TRACK Y450 FRAME 15-17. CORROSION LEVEL 2, TASK C531172-01. REPLACED SEAT TRACK PER SRM 53-00-15. (M) 2L72 4F RTA46NM 20050418002152005041800215EU 2005 4 18 USAA050418 120050308A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW22938 0337 FOUND SEAT TRACK CORRODED 3.2 INCH BY .70 INCH BY .065 INCH DEEP, Y 1963 FRAME 53.2 - 53.5 Z-240. FABRICATED NEW SEAT TRACK SECTION PER SRM 53-31-15 FIG 201 SH 2, 53-31-15 FIG 101 SH 8. (M) 2L72 4F RTA46NM 20050418002172005041800217EU 2005 4 18 USAA050399 120050307A5347A5327400SDAN2001SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW22938 0337 BFM - FOUND SEAT TRACK SECTION CORRODED 4 INCHES LONG BY 1 INCH WIDE BY .050 INCH DEEP, -Y450 BETWEEN FRAME 36-37.1 -Z240. CUT OUT DAMAGED AREA AND REPLACED WITH NEW SECTION PER SRM 53-00-15 FIG 204 SHEET 1. (M) 2L72 4F RTA46NM 20050418002202005041800220EU 2005 4 18 USAA050402 120050311A5347F5327584720000 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW22938 0337 BFM - FOUND SEAT TRACK CORRODED 4.95 INCH BY 1.15 INCH BY .043 INCH, 5.48 INCH BY 1.15 INCH BY .034 INCH, FRAME 32-35, -Y1950 MAIN CABIN FLOOR. REMOVED AND REPLACED SEAT TRACK PER SRM 53-00-15 2L72 4F RTA46NM 20050418002212005041800221EU 2005 4 18 USAA050403 120050310A5347F5347621120000 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW22938 0337 BFM - FOUND SEAT TRACK CORRODED, 3.1 INCH LONG BY .600 INCH WIDE BY .051 INCH DEEP, Y1959 FRAME 55-60 -Z240. REMOVED AND REPLACED WITH NEW SEAT TRACK AND TRACK SECTION PER SRM 53-00-15 FIG 204. (M) 2L72 4F RTA46NM 20050418002232005041800223EU 2005 4 18 USAA050406 120050308A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW22938 0337 BFM - FOUND SEAT TRACK CORRODED 1 INCH LONG BY .300 INCH WIDE BY -.045 INCH DEEP, -Y2462 BETWEEN FS 62-72 -Z240. CUT OUT DAMAGED AREA, REPLACED WITH NEW SEAT TRACK SECTION PER SRM 53-00-15 PAGE 233. CORROSION LEVEL 2, TASK C534159-01. (M) 2L72 4F RTA46NM 20050418002242005041800224EU 2005 4 18 USAA050423 120050312A5347F5327591620000 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW22938 0337 BFM - FOUND SEAT TRACK CORRODED, 1.9 INCH LONG BY 1.15 INCH WIDE BY .034 INCH DEEP, Y-1550 AT FS 34-35.5. FABRICATED SEAT TRACK SPLICE PER SRM 53-00-15. CORROSION LEVEL 2, TASK NR C532134-01. CORROSION LEVEL 2, TASK NR C532134-01. (M) 2L72 4F RTA46NM 20050418002262005041800226EU 2005 4 18 USAA050400 120050306A5347F5347821420100 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW22938 0337 BFM - FOUND SEAT TRACK CORRODED 1 INCH LONG BY .500 INCH WIDE BY .071 INCH DEEP, -Y450 BETWEEN FRAME 72-75 -Z240. REMOVED AND REPLACED WITH NEW SEAT TRACK PER SRM 53-00-15, 51-42-11. (M) 2L72 4F RTA46NM 20050418002272005041800227EU 2005 4 18 USAA050401 120050308A5347F5347621420000 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW22938 0337 BFM - FOUND SEAT TRACK CORRODED 2 INCHES BY .045 INCH BY .040 INCH AREA, Y450 FRAME 55-58 Z-240. CORROSION LEVEL 2, TASK C534159-01. INSTALLED NEW SEAT TRACK PER SRM 53-00-15 FIG 101 SHEET 2. (M) 2L72 4F RTA46NM 20050418002292005041800229EU 2005 4 18 USAA050444 120050317A5320F53315373200 FLOOR SUPPORT AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW22938 0337 BFM - FOUND PANEL SUPPORT CORRODED 1 INCH LONG BY 1.1 INCH WIDE BY .040 INCH DEEP, FS 40.2 TO 44 LOWER FUSELAGE Y0. REPLACED PANEL SUPPORT PER SRM 51-72-11. (M) 2L72 4F RTA46NM 20050418002302005041800230EU 2005 4 18 USAA050383 120050303A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW22938 0337 BFM - FOUND SEAT TRACK CORRODED .37 INCH DEEP BY .04 INCH WIDE BY 1 INCH LONG AREA, BETWEEN FRAME 73-74 Y = +1137.1. CORROSION LEVEL 2, TASK C534159-01. REMOVED AND REPLACED SEAT TRACK PER SRM 53-00-15, SRM 57-44-11. (M) 2L72 4F RTA46NM 20050418002312005041800231EU 2005 4 18 USAA050445 120050311A5320F5331532920000 SUPPORT AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW22938 0337 FOUND TEE CORRODED 1 INCH BY 1 INCH BY .040 INCH DEEP, LOWER WING TO BODY FAIRING SUPPORT TEE BELOW OZONE, FILTER 5511HB. REMOVED AND REPLACED SUPPORT TEE. (M) 2L72 4F RTA46NM 20050418002322005041800232EU 2005 4 18 USAA050446 120050319A5321 FLOOR PANEL AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW22938 0337 BFM - FOUND FLOOR PANEL CORRODED GREATER THAN 10 PERCENT, HEAT FLOOR PANEL AT L2. FABRICATED NEW FLOOR PANEL PER TYPICAL REPAIR 53-002-01. (M) 2L72 4F RTA46NM 20050418002342005041800234EU 2005 4 18 USAA050258 120050202A5347F53275664200 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19671UW 0323 BFM - FOUND SEAT TRACK CORRODED, 3 FT BY 2 INCHES BY .047 INCH DEEP, BETWEEN FS 32-33, Y1456, MAIN CABIN FLOOR. FABRICATED SEAT TRACK SPLICES, NEW SECTION OF SEAT TRACK, INSTALLED REPAIR PARTS PER SRM 53-00-15. (M) 2L72 4F RTA46NM 20050418002362005041800236EU 2005 4 18 USAA050265 120050203A5347F53478209203 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19671UW22760 0323 BFM - FOUND SEAT TRACK CORRODED 1.4 INCH LONG BY 1.2 INCH WIDE BY .050 INCH DEEP, FRAME C 64, -Y 1560 MAIN CABIN FLOOR. REMOVED AND REPLACED SEAT TRACK PER SRM 53-41-15 FIG 101, SRM 51-42-11. (M) 2L72 4F RTA46NM 20050418002372005041800237EU 2005 4 18 USAA050266 120050204A5347F5331089820000 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19671UW22760 0323 BFM - FOUND SEAT TRACK CORRODED 2 INCHES LONG BY .5 INCHES WIDE BY .036 INCH DEEP AND 1 INCH LONG BY .5 INCH WIDE BY .029 DEEP, FRAME 37 PLUS Y450 MAIN CARGO FLOOR. CORROSION LEVEL 2, TASK C533170-01. SPLICED IN SECTION OF SEAT TRACK PER SRM 53-31-15, 53-00-15 FIG 204 SHT 1. (M) 2L72 4F RTA46NM 20050418002382005041800238EU 2005 4 18 USAA050272 120050205A5347R53204902000 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19671UW22760 0323 BFM - FOUND SEAT TRACK CORRODED 3.5 ICH LONG BY .85 INCH WIDE BY .040 INCH DEEP, CABIN FRAME 30-34, -Y1959. CORROSION LEVEL 2, TASK C53213401. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER SRM 53-00-15, FIG 204 FIG 101. (M) 2L72 4F RTA46NM 20050418002412005041800241EU 2005 4 18 USAA050413 120050309A5320F5347968200100 WEB AIRBUS330 A330323 3930335EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW22938 0337 BFM - FOUND WEB CRACKED 1 INCH, Y -1447.8 AT FRAME 78-79. REMOVD AND REPLACED WEB PER SRM 51-42-11. (M) 2L72 4F RTA46NM 20050418002422005041800242EU 2005 4 18 USAA050440 120050310A5320F5327584620000 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW 0337 BFM - FOUND SEAT TRACK CORRODED, Y-1450 AT FRAME 30 AND 34. REMOVED AND REPLACED SEAT 3.20 BY .40 BY .010 INCH AREA. REMOVED AND REPLACED SEAT TRACK PER SRM 53-00-15. (M) 2L72 4F RTA46NM 20050418002462005041800246EU 2005 4 18 USAA050433 120050311A5321F53672338000000 FLOOR PANEL AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW 0337 BFM - FOUND FLOOR PANEL DELAMINATED AND CORRODED, MAIN CABIN HEATED FLOOR PANEL 271JF. FABRICATED NEW FLOOR PANEL PER TYPICAL REPAIR 53-02-01. (M) 2L72 4F RTA46NM 20050418002472005041800247EU 2005 4 18 USAA050434 120050311A5321F5367233700300 FLOOR PANEL AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW 0337 BFM - FOUND FLOOR PANEL DELAMINATED AND CORRODED GREATER THAN 10 PERCENT, MAIN CABIN HEATED FLOOR PANEL 272 KF. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F RTA46NM 20050418002492005041800249EU 2005 4 18 USAA050419 120050308A5347F5932671120400 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW22938 0337 BFM - FOUND SEAT TRACK CORRODED 3 INCH BY 2 INCH BY .056 INCH AND 4 INCH BY 2 INCH BY .060 INCH, Y-450 FRAME 53.2 - 53.5 Z-240. INSTALLED NEW SEAT TRACK PER SRM 53-31-15 FIG 101 SHEET 1/8. (M) 2L72 4F RTA46NM 20050419000592005041900059EU 2005 4 19 AALA20050264 120050413A2934 TRANSMITTER AIRBUS300 A300B4605R 3930308EU HYDRAULIC SYS MALFUNCTIONED A AALAO OTHER N FALSE WARNING DEDESCENT 1 SW2170072 515 MIA - GREEN HYDRAULIC SYSTEM QUANTITY LOSS DURING DESCENT. ECAM AND GAUGE ON OVERHEAD PANEL BOTH SHOWED HYDRAULIC LEVEL IN YELLOW BAND. PERFORMED MANUAL GEAR EXTENSION AND LANDED MIA WITHOUT INCIDENT. REPLACED GREEN SYSTEM RESERVOIR QUANTITY TRANSMITTER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20050419000632005041900063NM 2005 4 19 AALA20050233 120050331A3350 CONNECTOR BOEING757 757223 1384957NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21198AA 32392 RNO - EMERGENCY LIGHTS AT ROWS 26 TO 33 INOPERATIVE. FOUND LOOSE PLUG AT SEAT 29. SECURED PLUG AT SEAT 29 FOR EMERGENCY LIGHTS AT ROWS 26 TO 33. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050419000662005041900066NM 2005 4 19 AALA20050238 120050404A3350 LIGHT BOEING767 767323 1385205NM COCKPIT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21388AA 27448 DFW - EMERGENCY LIGHT IN COCKPIT OVER COCKPIT DOOR INOPERATIVE. REPLACED EMERGENCY LIGHT IN COCKPIT OVER COCKPIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050419000702005041900070WP 2005 4 19 AALA20050236 120050403A3350 MODULE DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21418AA 49329 DTW - EMERGENCY EXIT LIGHTS FROM SEAT 21 TO AFT OF CABIN INOPERATIVE. REPLACED MODULE AT ROW 20 FOR EMERGENCY EXIT LIGHTS FROM SEAT 21 TO AFT OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050419000722005041900072WP 2005 4 19 AALA20050237 120050404A3397 WIRE DOUG DC9 DC982 3022082WP CABIN DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21255AA 49287 DFW - ENTRY AISLE EMERGENCY LIGHT ASSEMBLY ON FORWARD GALLEY WALL NEAR FLOOR WITH DOUBLE ARROW IS INOPERATIVE. REPAIRED DAMAGED WIRES AT THE BASE OF THE WINDSCREEN FORWARD OF SEAT 3EF WITH ENVIRONMENTAL SPLICES FOR ENTRY AISLE EMERGENCY LIGHT ASSEMBLY ON FORWARD GALLEY WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050419000732005041900073WP 2005 4 19 AALA20050235 120050401A3350 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW217519A 49896 TUL - OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK AT STATION 1050 LEFT FOR OVERWING EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050415000992005041500099NM 2005 4 15 2005UALA00127 120050207A2612 WARNING SYSTEM BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE LT ENGINE ACTIVATED A UALAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29793UA 26946 LT ENG FIRE LOOP AND LT ENG OVERHT DETECT EICAS MESSAGES. OIL QTY AND OIL PRESSURE DROPPED. ENGINE SHUTDOWN. EMERGENCY DECLARED. ENGINE REPLACED. FOUND ONE HPT STG-2 BLADE FAILED AT AIRFOIL MID-SPAN AS A RESULT OF INTERNAL SULFIDATION. ANOTHER BLADE FAILED NEAR THE AIRFOIL PLATFORM, AS A RESULT OF CONTACT WITH DEBRIS FROM 1ST BLADE. RESULTED IN VIBRATION. OVER TIME, CAUSED FAILURE OF THE FIRE/OVERHEAT LOOPS, & RESULTED IN CRACKING OF OIL PRESSURE LINE BETWEEN SERVO FUEL HEATER & AIR OIL HEAT EXCHANGER. CAUSE OF BLADE SULFIDATION CONTAMINATION OF COOLING PASSAGES WITH TURBO-TIP COATING. PWA HAS CHANGED COATING PROCESS TO PRECLUDE FUTURE CONTAMINATION. 2L72 4F4 FRTT0001SE E46NE 20050415001062005041500106EU 2005 4 15 S9HA099198 120050204A7931704A37642043 TRANSMITTER AEROSPAS355 AS355* EU OIL PRESSURE DEFECTIVE B S9HAO OTHER O OTHER NRNOT REPORTED 1 WP19352NT45 2553 NO OIL PRESSURE INDICATION. ENGINE PRESSURE LIGHT NOT ILLUMINATED. REPLACED TRANSMITTER WITH NEW TRANSMITTER. CHECK GOOD. 1G72 3U H11EU 20050415001332005041500133NM 2005 4 15 WRLA2005041 120050216A5512 SKIN DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST RT BARREL NUT HOLE NR 23. 2L73 4F4 FRTA22WE E24NE 20050415001362005041500136NM 2005 4 15 WRLA2005044 120050211A5512 SKIN DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST RT BARREL NUT HOLE NR 11. 2L73 4F4 FRTA22WE E24NE 20050415001442005041500144NM 2005 4 15 WRLA2005053 120050214A5512 SKIN DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST LT BARREL NUT HOLE NR 15. 2L73 4F4 FRTA22WE E24NE 20050415001482005041500148NM 2005 4 15 WRLA2005059 120050213A5347 SEAT TRACK DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK INSPECTION, FOUND CORROSION IN MAIN DECK SEAT TRACK AT STA 847, X=44. 2L73 4F4 FRTA22WE E24NE 20050415001572005041500157NM 2005 4 15 WRLA2005068 120050205A5313 LONGERON DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK INSPECTION, FOUND CORROSION IN CENTER CARGO LONGERON AT STA 5-120 L45R. 2L73 4F4 FRTA22WE E24NE 20050415001582005041500158NM 2005 4 15 WRLA2005069 120050205A5312 STRUCTURE DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE BULKHEAD CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK INSPECTION, FOUND CORROSION IN T CHORD IN AFT CARGO PRESSURE BULKHEAD L27 AND STA 2007, X=-27.5. 2L73 4F4 FRTA22WE E24NE 20050415001642005041500164WP 2005 4 15 AALA20050133 120050222A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217533A 49987 DFW - CEILING EMERGENCY LIGHTS AT ROWS 8 TO 17 INOPERATIVE. REPLACED BATTERY AND CHARGER ASSEMBLY FOR CEILING EMERGENCY LIGHTS FOR ROWS 8 TO 17. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050415001742005041500174EA 2005 4 15 QXEA200500178 120050121A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - RIGHT OUTBOARD SIDE FACING SEAT RAIL, AT STATION X753, HAS PITTING CORROSION ON MOST INBOARD SURFACE. REPAIRED IAW CRJ REO 670-53-00-060, REV B AND HORIZON AIR EA R-53-226. 2L72 4F RTA21EA 20050415001782005041500178EA 2005 4 15 QXEA200500186 120050122A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - LEFT OUTBOARD SIDE FACING SEAT RAIL, AT STATION X613 TO X629, HAS PITTING CORROSION ON MOST INBOARD SURFACE. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01, REO 670-53-00-060, REV B AND HORIZON AIR EA R-53-266. 2L72 4F RTA21EA 20050415001882005041500188EU 2005 4 15 AWXA200500265 120050217A5320D53471124200 PLATE AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28647AW 762 MCN - MAJOR REPAIR - DURING 8-DAY CHECK, CORROSION WAS FOUND ON SHEAR PLATE -Y50 BETWEEN FS 64 AND FS 70. MAINTENANCE REMOVED CORRODED SHEAR PLATE -Y50 FROM FS 64 TO FS 70; FABRICATED A NEW REPLACEMENT SHEAR PLATE, INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050415001902005041500190NM 2005 4 15 AWXA200500267 120050131A143069702514 BOLT BOEING737 7373G7 1384595NM VERTICAL STAB CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 MCN - MAJOR REPAIR - DURING C-16 CHECK, CORROSION WAS FOUND ON RT OUTBOARD VERTICAL STABILIZER ATTACH BOLT AND WASHERS BS 1016, STR 2 RT. MAINTENANCE REMOVED AND REPLACED CORRODED RT OUTBOARD VERTICAL STABILIZER ATTACH BOLT AND WASHERS IAW BMM 55-30-00. 2L72 4F RTA16WE 20050415001922005041500192EU 2005 4 15 AWXA200500270 120050217A5315D5347217220390 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28647AW 762 MCN - MAJOR REPAIR - DURING 8-DAY CHECK, CORROSION WAS FOUND ON FLOORBEAM -Y50 BETWEEN FS 66 AND FS 68. MAINTENANCE REMOVED CORRODED FLOORBEAM -Y50 FROM FS 66 TO FS 68; FABRICATED A NEW REPLACEMENT FLOORBEAM, INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050415001942005041500194EU 2005 4 15 AWXA200500272 120050217A5315D5347213320200 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28647AW 762 MCN - MAJOR REPAIR - DURING 8-DAY CHECK, CORROSION WAS FOUND ON FLOORBEAM -Y29 BETWEEN FS 64 AND FS 66. MAINTENANCE REMOVED CORRODED FLOORBEAM -Y29 FROM FS 64 TO FS 66; FABRICATED A NEW REPLACEMENT FLOOR BEAM, INSTALLED REPAIR PART IAW A320 SRM 51-49-00. 2L72 4F RTA28NM 20050415002122005041500212EU 2005 4 15 MALA050216 120050121A33506122751 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU EMERGENCY LIGHT DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15517XJ E2335 BATTERY PACK PN 61-2275-1 SN 9803381, REMOVED FOR CAPACITY CHECK. CAPACITY CHECK FAILED. REPLACED BATTERY ASSY PN 61-2274-1. UNIT PASSES CMM CHECKS, RTS 1/23/05. 2H74 4F RTA49EU 20050415002152005041500215EU 2005 4 15 MALA050209 120050108A2611 SMOKE DETECTOR SAAB SF340 340B 7860101EU LAVATORY MALFUNCTIONED A MALAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL15451XJ 340B451 LAV SMOKE DETECTOR LIGHT ILLUMINATED ON TAKEOFF ROLL. RETURNED TO GATE. REPLACED DETECTOR 2L72 4T RTA52EU 20050418001592005041800159NM 2005 4 18 C7WA200300078 120050113A2197 WIRE BOEING727 7272M7 138407SNM A/C SYSTEM SHORTED A C7WAO OTHER O OTHER CLCLIMB 1 SO17742RW 21952 NR 1 PACK VALVE CIRCUIT BREAKER POPPED ON CLIMB-OUT, CIRCUIT BREAKER WOULD NOT RESET. TROUBLESHOOTING PERFORMED BY WD 21-61-02, FOUND WIRE SHORTED. ACCOMPLISHED REPAIR BY WIRE SPLICE, AIR COND SYSTEM. TESTED WITH BOTH PACKS ON TESTED GOOD. (M) 2L73 4F A3WE 20050418001602005041800160NM 2005 4 18 C7WA200300077 120050115A2780 CONNECTOR BOEING727 727222 1384073NM L/E SLAT DIRTY A C7WAO OTHER F FLT CONT AFFECTED CLCLIMB 1 SO177640U 19913 AIR RETURN, UPON FLAP RETRACTION ON CLIMB-OUT, NR 1 SLAT FAILED TO RETRACT. CLEANED CONNECTOR IAW 20-80-01, OPS CHECKED FLAPS AND SLATS PER MM 27-80-0. ALL INDICATIONS NORMAL. OK FOR CONTINUED SERVICE. (M) 2L73 4F A3WE 20050418001642005041800164EU 2005 4 18 USAA050019 120050101A5347F5347820720000 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW22421 0315 BFM - FOUND SEAT TRACK CORRODED, 1 INCH BY .75 INCH BY .035 INCH DEEP, FRAME 74, Y 1202 CM, MAIN CABIN SEAT TRACK. REMOVED AND REPLACED SEAT TRACK PER SRM 53-00-15. CORROSION LEVEL 2, TASK NR J7-270-53500. (M) 2L72 4F RTA46NM 20050418001692005041800169EU 2005 4 18 USAA050021 120050101A5347F31170220000 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW22421 0315 BFM - FOUND TRACK CORRODED 1.5 INCH BY 1.5 INCH BY .040 INCH DEEP, MAIN DECK FLOORBEAM, FRAME 13-13A AT Y953. CORROSION LEVEL 2, TASK NR J7-220-53500. REMOVED AND REPLACED BEAM TRACK PER STM 53-11-15. (M) 2L72 4F RTA46NM 20050418001712005041800171EU 2005 4 18 USAA050386 120050305A5320F5347823420100 RAIL AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW22938 0337 BFM - FOUND RAIL CORRODED 1 INCH BY 1.75 INCH BY .010 INCH DEEP, FRAME 79, -Y445, MAIN CABIN. REMOVED AND REPLACED RAIL PER SRM 53-00-15 FIG 101. (M) 2L72 4F RTA46NM 20050418001742005041800174NM 2005 4 18 USAA050369 120050308A5311 FRAME BOEING767 767201 1385125NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19648US68950 23900 PIT - FOUND FLOOR FRAME CORRODED 2.5 INCH LONG BY 2 INCH WIDE BY .15 INCH DEEP, MAIN CABIN FLOOR BS 347, RBL 54.75. ACCOMPLISHED T-CAP REPAIR PER 53-00-51 FIG 201 SHT 1. (M) 2L72 4F RTA1NM 20050418001762005041800176NM 2005 4 18 USAA050372 120050312A5347146T52162 SEAT TRACK BOEING767 767201 1385125NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19648US68950 23900 BFM - FOUND SEAT TRACK CORRODED 6 INCH BY .80 INCH BY .060 INCH AREA, CABIN FLOOR STATION 1120 TO 1126 RBL 88.5 INCH. ACCOMPLISHED SEAT TRACK REPAIR PER SRM 53-00-52 FIG 203. (M) 2L72 4F RTA1NM 20050418001902005041800190NM 2005 4 18 USAA050370 120050312A5347 SEAT TRACK BOEING767 767201 1385125NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19648US 23900 BFM - FOUND SEAT TRACK CORRODED 3 INCH LONG BY .05 INCH WIDE BY .10 INCH DEEP AND 1 INCH LONG BY .05 INCH WIDE BY .092, RBL 88.5 AND BS 611-644. FABRICATED NEW SEAT TRACK PER SRM 53-00-52 FIG 203. (M) 2L72 4F RTA1NM 20050418001952005041800195NM 2005 4 18 USAA050374 120050303A5347146T52156 SEAT TRACK BOEING767 767201 1385125NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19648US68950 23900 BFM - FOUND SEAT TRACK ASSEMBLY CORRODED 4.5 INCH LONG BY .80 INCH WIDE BY .032 INCH DEEP, MAIN CABIN FLOOR, BS 1373-1481, LBL 88.5. CORROSION LEVEL 2, TASK C53-252-01. REMOVED AND REPLACED ENTIRE SEAT TRACK ASSEMBLY PER SRM 51-40-02, 53-00-52, 51-30-02, DWG NR 146T5215, SHT 2. (M) 2L72 4F RTA1NM 20050418002022005041800202EU 2005 4 18 USAA050264 120050203A5320F53478236204 FLOOR SUPPORT AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19671UW22760 0323 BFM - FOUND FLOOR SUPPORT CORRODED .50 INCH LONG BY .50 INCH WIDE BY .037 INCH DEEP, FRAME 73 PLUS Y 1190 MAIN CABIN FLOOR. REMOVED AND REPLACED FLOOR SUPPORT. CORROSION LEVEL 2, TASK C53415901. (M) 2L72 4F RTA46NM 20050418002072005041800207EU 2005 4 18 USAA050408 120050310A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW22938 0337 BFM - FOUND SEAT TRACK CORRODED .40 INCH LONG BY .095 INCH WIDE BY .090 INCH DEEP AREA, Y1959 AT FRAME 53.2 TO 53.5. FABRICATED SEAT TRACK SECTION PER SRM 53-31-15, 53-00-15. (M) 2L72 4F RTA46NM 20050418002092005041800209EU 2005 4 18 USAA050421 120050308A5347F5332561620000 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW 0337 BFM - FOUND SEAT TRACK CORRODED 5.30 INCH BY 1.15 INCH BY .045 INCH, Y-1959, FRAME 39.2-40 Z-240. INSTALLED NEW SEAT TRACK PER SRM 53-31-15 FIG 101 SHT 1/8. (M) 2L72 4F RTA46NM 20050418002162005041800216EU 2005 4 18 USAA050443 120050314A5315F5311198520600 FLOORBEAM AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW22938 0337 BFM - FOUND FLOORBEAM CORRODED 2 INCHES LONG BY 1 INCH WIDE BY .016 INCH DEEP, FRAME 16A-Y1450 -Z240. REPLACED FLOORBEAM PER SRM 53-11-14 FIG 101, 51-42-11. (M) 2L72 4F RTA46NM 20050418002222005041800222EU 2005 4 18 USAA050405 120050309A5320F53478216200 FLOOR SUPPORT AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW 0337 BFM - FOUND FLOOR SUPPORT CORRODED 1.7 BY 1.7 BY .047 INCH AREA, Y 0 AT FS 73-75. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 53-41-14, 51-42-11. CORROSION LEVEL 2, TASK C534159-01. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 53-41-14, 51-42-11. (M) 2L72 4F RTA46NM 20050418002252005041800225EU 2005 4 18 USAA050394 120050304A5320F5347821620200 BEAM AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW22938 0337 BFM - FOUND LONGERON BEAM CORRODED .080 INCH LONG BY 1.20 WIDE BY .070 INCH DEEP, BETWEEN FRAME 78-79, Y=0 REPLACED PART WITH IDENT PART PER 51-42-11, 51-72-11. (M) 2L72 4F RTA46NM 20050418002282005041800228EU 2005 4 18 USAA050384 120050306A5320F5347801100400 BEAM AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW22938 0337 BFM - FOUND BEAM CORRODED 1.6 INCH BY .80 INCH BY .055 INCH DEEP, FRAME 75, Y459, MAIN CABIN FLOOR. REMOVED AND REPLACED BEAM PER SRM 51-72-11. (M) 2L72 4F RTA46NM 20050418002402005041800240EU 2005 4 18 USAA050263 120050203A5320F53478017007 FLOOR SUPPORT AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19671UW 0323 BFM - FOUND FLOOR SUPPORT CORRODED 4 AREAS, 1 INCH LONG BY 6 INCH WIDE BY .005 INCH DEEP, 2 INCHES LONG BY 1 INCH WIDE BY .006 DEEP, 1 INCH WIDE BY 1.1 INCH LONG BY .017 DEEP, FRAME C73, -Y1680 - -Y2040 MAIN CABIN FLOOR. REMOVED AND REPLACED FLOOR SUPPORT. (M) 2L72 4F RTA46NM 20050419000612005041900061WP 2005 4 19 AALA20050263 120050412A3244 TIRE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE NR 4 SEPARATED A AALAA UNSCHED LANDING SR AFFECT SYSTEMS PARTIAL RPM/PWR LOSS TOTAKEOFF 1 SW21983TW 53633 717879 DFW - RIGHT ENGINE COMPRESSOR STALL ON TAKEOFF DUE TO THREAD SEPARATION OF NUMBER FOUR TIRE RESULTING IN FOD DAMAGE TO RIGHT HAND ENGINE. SHUTDOWN RIGHT ENGINE. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. AIRCRAFT OUT OF SERVICE FOR EVALUATION AND REPAIRS. 2L72 4F4 FRTA6WE E9NE 20050419000652005041900065WP 2005 4 19 AALA20050234 120050401A3350 BATTERY DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21416AA 49327 SFO - EMERGENCY LIGHT ON LEFT AND RIGHT OVERWING EXIT DOORS INOPERATIVE. LEFT EMERGENCY LIGHT SYSTEM IN ARM TO CHARGE LEFT AND RIGHT OVERWING EXIT DOOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050419000682005041900068NM 2005 4 19 AALA20050232 120050330A3350BPS73 BATTERY PACK BOEING767 767323 1385205NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW2139365 24046 JFK - RIGHT AFT CABIN SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR RIGHT AFT CABIN SEAT MOUNTED EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050419000742005041900074NM 2005 4 19 AALA20050239 120050403A3350 CONNECTOR BOEING767 767323 1385205NM CABIN DISCONNECTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21345AN 33084 MIA - EMERGENCY LIGHT AT ROWS 20H AND 21H INOPERATIVE. RECONNECTED CONNECTION FOR EMERGENCY LIGHTS AT ROWS 20H AND 21H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050419000772005041900077NE 2005 4 19 AALA20050240 220050404A7230 SPOOL DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE NR 1 ENGINE MALFUNCTIONED A AALAA UNSCHED LANDING Y ENGINE STOPPAGE CLCLIMB 1 SW21223AA 49173 709827 DFW - DURING CLIMBOUT AT FL200 LEFT ENGINE FAILED. N2 SPOOL READ ZERO. OIL PRESSURE READ ZERO. N1 SPOOL READ 20. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. PER ENGINEERING REIVEW OF DFDR N2 SPOOL UNCOUPLED FROM GEARBOX. REPLACED NUMBER ONE ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 F A6WE E9NE 20050419000892005041900089WP 2005 4 19 AALA20050259 120050411A4990 SEAL DOUG DC9 DC982 3022082WP APU LEAKING A AALAA UNSCHED LANDING KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW217547A 53029 SJC - CABIN BEGAN FILLING WITH SMOKE SHORTLY AFTER TAKEOFF. RETURNED TO SJC AND LANDED WITHOUT INCIDENT. FOUND APU OIL COOLER SEAL LEAKING. REPLACED APU OIL COOLER SEAL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050420000362005042000036CE 2005 4 20 2005F00061 120050307A5730310R SKIN CESSNA310 310A 2074204CE RT WING CRACKED E K NONE O OTHER ININSP/MAINT 1 GL11134J 7073 1100 DURING MAINTENANCE WORK ON THE RIGHT CENTER WING LOCKER BAY COMPARTMENT FUEL TANK, MAINTENANCE FOUND TWO WING SKIN .5 INCH SURFACE CRACKS AT APPROX WING STATION 60.0 AND FUSELAGE STATION 54.0. SIMILAR DAMAGE WAS FOUND IN THE LEFT WING SAME LOCATION. A DAMAGE REPORT WAS SENT TO CESSNA ENGINEERING BY THE OPERATOR. NO PREVIOUS REPAIRS OR MODIFICATION TO THE AFFECTED AREA. 1L72 3O 3A10 20050420000372005042000037WP 2005 4 20 0656 120050305A3260 UPLOCK DOUG DC8 DC863F 302198FWP RT MLG OUT OF RIG A U2RAO OTHER N FALSE WARNING CLCLIMB 1 GL23865F 77744822 46088 AFTER MAIN LANDING GEAR RETRACTION GEAR HANDLE IN THE UP POSITION, DOOR NOT LATCH LIGHT REMAINS ON. POSITION GEAR HANDLE IN THE UP-LATCH CHECK POSITION, DOOR NOT LATCHED LIGHT, GEAR NOT LATCHED LIGHT AND ALTERNATE RIGHT HAND DOOR NOT LATCHED LIGHT REMAINS ON, PUT FLAPS TO 23 DEGREES POSITION AND GEAR HANDLE IN THE UP POSITION, ALL LIGHTS OUT. 2L74 4F 4A25 20050420000392005042000039WP 2005 4 20 050301 120050206A531059217181 BEAM DOUG DC9 DC915F 3022037WP CARGO DOOR FRAMECRACKED A MJYAK NONE O OTHER ININSP/MAINT 1 SW07785TW 47015 FORWARD CARGO COMPARTMENT, DOOR JAMB, STUB BEAM SHORT FLANGE IS CRACKED. 2L72 4F A6WE 20050420000402005042000040CE 2005 4 20 DELA200500006 120050308A561066003942 WINDSHIELD LEAR 60 60LEAR 5170707CE COCKPIT MELTED E DELAO OTHER MP OVER TEMP NO WARNING INDICATION CRCRUISE 1 CE03188TG2614 078 SELECTED WINDSHIELD DEFOG CLIMBING FL200, 45 MIN LATER LEVEL CRUISE FL400 F/O NOTICED RT WINDSHIELD APPEARED TO HAVE BUBBLE FORMING I/B HEATING BUS BAR, SURFACE HOT TO TOUCH. W/S DEFOG SYS SELECTED OFF. W/S DEFOG ANNUNCIATOR HAD NOT ILLUMINATED AFTER INITIAL UNDER TEMP INDICATION EXTINGUISHED. NORMAL OPS OF ANNUNCIATOR IS ILLUMINATION WHEN W/S DEFOG SELECTED TO OPERATE, W/S IS EITHER UNDER 85 DEG OR OVER 150 DEG. CONSULTED AFM & MEL, SECURED RT W/S DEFOG CIRCUIT BREAKER & USED W/S ANTI-ICE SYS TO PREVENT FOGGING ON DESCENT. MELTING OF HEATED PLY, SMALL AREAS OF DELAMINATION, SURFACE DEFORMATION ON INNER & OUTER PLIES. DAMAGE BEYOND LIMITS. W/S REMOVED & REPLACED. W/S DEFOG ELECTRICAL SYS BEING TESTED. 2L72 4F RTA10CE 20050420000412005042000041NM 2005 4 20 C8GA20050008 120050311A2424939D1502 VOLT REGULATOR BOEING727 7272A1 138407FNM NR 2 GENERATOR INOPERATIVE A C8GAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO15286SC52514 21601 FLT 738 FROM MMIO TO MGDL. AFTER V1, NR 2 GENERATOR 3 LIGHT TRIP. COULD NOT RE-ESTABLISH BUS TIE BREAKER. RETURNED TO MMIO AND LANDED WITHOUT FURTHER INCIDENT. PLACED NR 2 GENERATOR/CSD ON MEL. AIRCRAFT RETURNED TO SERVICE. ON 3/13/05, REMOVED AND REPLACED VOLTAGE REGULATOR AND GENERATOR CONTROL PANEL. OPS CHECK GOOD. MEL CLEARED. 2L73 4F A3WE 20050420000452005042000045SW 2005 4 20 2005F00062 120050323A2910SS1008F000E090Y HOSE SWRNGNSA227 SA227AC 8780603SW HYD SYSTEM RUPTURED E DUFAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL27371PH AC576 WHILE EN ROUTE FROM SIOUX FALLS, SD TO RAPID CITY, SD THE PILOT NOTICED THE HYDRAULIC PRESSURE WAS FLUCTUATING ON THE LEFT HAND ENGINE. SHORTLY THEREAFTER THE RIGHT HAND PRESSURE BEGAN TO FLUCTUATE. THE PILOT REQUESTED CLEARANCE TO RETURN TO SIOUX FALLS WHICH WAS GRANTED. EMERGENCY VEHICLES WERE DISPATCHED AS A PRECAUTION AND AN UNEVENTFUL LANDING WAS PERFORMED. INVESTIGATION REVEALED THAT A HYDRAULIC PRESSURE LINE HAD RUPTURED. 2L72 4T RTA8SW 20050420000482005042000048NM 2005 4 20 SROM200500007 120050324A335030043211 LIGHT BOEING737 737205 1384456NM ESCAPE SLIDE CORRODED C SROMK NONE L NO TEST ININSP/MAINT 1 AL03733PA 6 23466 EXTERIOR EMERGENCY LIGHT BY L2 DOOR INOP. CLEANED CORROSION FROM EMERGENCY ESCAPE SLIDE LIGHTS, REINSTALLED LAMP ASSEMBLY AND TESTED GOOD IAW B737 MM33-51-61. 2L72 4F RTA16WE 20050420000502005042000050SW 2005 4 20 PNSA050302 120050325A7712 INDICATOR SWRNGNSA227 SA227AC 8780603SW NR 1 TORQUE INACCURATE A PNSAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 AL032719H AC713B PILOT REPOTED ON TAKEOFF ROLL THE NR 1 ENGINES POWER WAS LOW. TAKEOFF WAS ABORTED. MX FOUND THAT THE NR 1 TORQUE GAUGE WAS READING WRONG. ALSO FOUND THE NR 1 ENGINE WAS FUEL LIMITED. THE TORQUE GAUGE WAS REPLACED AND THE FUEL FLOW WAS ADJUSTED AS NEEDED. 2L72 4T RTA8SW 20050420000522005042000052SO 2005 4 20 101 220050328A731464936827A1 PUMP PIPER PA34 PA34200T 7103406SO CONT O360 LTSIO360EB 17025SO RT ENGINE FUEL INOPERATIVE B FFKRK NONE O OTHER ININSP/MAINT 1 SO0521407261 261 347870435 807968 PILOT SQUAWKED THAT THE FUEL FLOW FOR THE RIGHT ENGINE WAS LOW AND ERRATIC IN-FLIGHT. MAINTENANCE INSPECTED AND TRIED TO ADJUST THE FUEL SYSTEM, REPLACED FUEL PUMP. NO FURTHER ACTION NEEDED. 1L72 3O3 O A7SO E9CE 20050420000532005042000053NM 2005 4 20 C1HA200585001 120050326A2170 O-RING BOEING727 7272S7 138407ZNM WATER SEPARATOR FAILED A C1HAA UNSCHED LANDING SJ AFFECT SYSTEMS WARNING INDICATION CRCRUISE 1 GL15685CA 22492 EXPERIENCED RAPID DECOMPRESSION AT FLT 310, RAN COM RAPID DECOMPRESSION AND DESCENT CHECK LIST. CABIN STABILIZED AT 17,000 FT, FOUND LT FWD CLAMP LOOSE ON WATER SEPARATOR. REMOVED AND INSPECTED CLAMP, FOUND SERVICEABLE. INSTALLED NEW O-RINGS, REINSTALLED LT FWD CLAMP IAW 21-55-41 AND 21-55-51. OPS AND LEAK CHECKED NORMAL. SECURED ACCESS PANELS. 2L73 4F A3WE 20050420000562005042000056NM 2005 4 20 MWEA050029 120050330A5270 PROXIMITY SENSOR BOEING717 717200 1383700NM ACCESS DOOR OUT OF TOLERANCEA MWEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL31913ME 55176 ACCESS COMPARTMENT DOOR ANNUNCIATOR ILLUMINATED. INSPECTED DOOR FOUND TARGET AND PROXIMITY SENSOR TO BE OUT OF TOLERANCE DUE TO FAULT. REOPENED, RESEATED AND RESECURED DOOR, ALL WORK DONE, OK FOR SERVICE. 2L72 4F TRA6WE 20050420000572005042000057EU 2005 4 20 166921 120050331A3230D49410001 CONTROL MODULE SAAB SF340 SF340A 7850100EU MLG MALFUNCTIONED A UHLAL ABORTED APPROACH J WARNING INDICATION DEDESCENT 1 GL17118SD 118 NO NOSE WHEEL DOWN AND LOCKED INDICATION WHEN SELECTED IN THE DOWN AND LOCKED POSITION. REMOVED AND REPLACED LANDING GEAR CONTROL ASSEMBLY. 2L72 4T RTA52EU 20050420000582005042000058EU 2005 4 20 248301 120050328A2120 ODOR SAAB SF340 SF340A 7850100EU COCKPIT DETECTED A UHLAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL1714XS 340A014 AIRCREW CALLED INTO REPORT SMELL OF SMOKE IN THE CABIN AND COCKPIT SOON AFTER BLEEDS TURNED ON. AIRCRAFT RETURNED SAFELY TO DAY. 2L72 4T RTA52EU 20050420000642005042000064EU 2005 4 20 TCA003 120050405A2824 TRANSFER VALVE AMD FALC20FALCON 2720302EU LT TANK MALFUNCTIONED E E18ABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL23326VW 27 THE LT FEEDER TANK STARTED OVER FILLING IN THE AIR AND FILLED UP TO YELLOW ARCON THE INDICATOR. 2L72 4F A7EU 20050420000672005042000067EU 2005 4 20 200504051 120050405A7931 WARNING LIGHT SAAB SF340 SF340A 7850100EU RT PROP OIL ILLUMINATED A UHLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL17121CQ 121 LOSS OF RIGHT PROP OIL PRESSURE. AIRCRAFT DECLARED EMERGENCY AND SAFELY RETURNED TO IAD. 2L72 4T RTA52EU 20050420000712005042000071NM 2005 4 20 FRISBY05004 120050313A292041022021 HOUSING DOUG MD80 MD83 3023681NM DRAIN PORT CRACKED B A UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 SO05 315C 1693 DURING T/O, EXPERIENCED TOTAL LOSS OF PRESSURE IN LT HYD SYS & A LOSS (5 PSI REMAINING) OF RT HYD SYSTEM. FLT CREW REPORTED NO HYD PRESSURE WHEN SELECTING GEAR UP. SELECTED GEAR HANDLE DOWN & STARTED WITH EMERGENCY CHECK LISTS. RETURNED TO ARLANDA (STOCKHOLM) & MADE A FLAP 11 LANDING. STOPPED AT RUNWAY END, UNABLE TO TURN OFF. MX REVEALED DRAIN PORT HOUSING, P/N 4102202-1, INSTALLED PTU, P/N 4100310-6, S/N 315C, HAD CRACKED COMPLETELY AROUND CIRCUMFERENCE. PTU REPORTED TO HAVE 42,254 BUT THE TIME ON THE FAILED DRAIN PORT HOUSING, SINCE INSTALLATION IAW SB 4100310-29-0031 (AD 94-22-03) WAS NOT REPORTED. FRISBY AEROSPACE HAS REQUESTED THIS FAILED DRAIN PORT HOUSING BE RETURNED FOR FAILURE INVESTIGATION. 2L72 4F RT 20050420000722005042000072NM 2005 4 20 TSAA0524018 120050404A2460941D3352 CIRCUIT BREAKER BOEING737 73725A 1384481NM GENERATOR DAMAGED A TSAAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 WP13819AL 23791 CREW REPORTED SMOKE IN THE COCKPIT. SMOKE FROM CB PANEL BEHIND F/O. SLIDING WINDOW OPENED TO VENT SMOKE. RETURNED TO GATE. REMOVED AND REPLACED THE APU GCU. DID NOT CURE PROBLEM. FOUND B-LEG ON APU GENERATOR DEAD. DEFER PER MEL 24-2. PLACARDS INSTALLED. AIRCRAFT RETURNED TO SERVICE. NOISE COMING FROM BEHIND F/O CIRCUIT BREAKER PANEL. REPLACED APU GCU & APU GEN BREAKER. OPS CHECK OK WITH EXTERNAL POWER APPLIED & APU SUPPLYING PNEUMATIC. ALSO OPS CHECK OK WITH NR 1 & NR 2 ENGINE GEN ON LINE. APU NOT ACCEPTING GROUND POWER. REMOVED AND REPLACED NR 1 BT BREAKER. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA16WE 20050420000732005042000073NM 2005 4 20 LOFR200500001 120050407A324626113555 WHEEL BOEING747 747200 1384847NM MLG CRACKED B Q2SAK NONE O OTHER ININSP/MAINT 1 AL03 CRACKED KEY BOSS IDENTIFIED PER HONEYWELL CMM 32-45-12, APPENDIX A, KEY BOSS NDT INSPECTION AREA. CRACK IDENTIFIED USING EDDY CURRENT METHOD. 2L74 4F RTA20WE 20050420000742005042000074NM 2005 4 20 LOFR200500002 120050407A32462609113 WHEEL BOEING747 747200 1384847NM MLG CRACKED B Q2SAK NONE O OTHER ININSP/MAINT 1 AL03 CRACKED SPOKES IDENTIFIED DURING VISUAL INSPECTION. 2L74 4F RTA20WE 20050420000752005042000075CE 2005 4 20 DXTA200500659 120050403A322067940624 LANDING GEAR CESSNA750 750 2076810CE NOSE WORN E DXTAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 GL07930QS3432 7500130 ON TAKEOFF LANDING GEAR HANDLE JAMMED IN DOWN POSITION. JACKED AIRCRAFT, NOTED NOSE GEAR DID NOT FULLY EXTEND. UPPER CHAMBER WAS SERVICED TO 375 PSI, LOWER CHAMBER WAS SERVICED TO -0- PSI. NEED TO INSTALL RENTAL NOSE GEAR. JACKED AIRCRAFT REMOVED RT & LT NOSE LANDING GEAR WHEELS. REMOVED UPPER & LOWER BARREL ASSEMBLY & INSTALLED A REPAIRED UNIT. UNIT REPAIRED BY CESSNA, WORK PERFORMED IAW CESSNA 750 CMM 32-20-02. 2L72 4J RTT00007WI 20050420000772005042000077CE 2005 4 20 DXTA200500662 120050406A3297 WIRE CESSNA500 560CESSNA 2076750CE MLG INDICATOR BROKEN E DXTAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL07317QS 5600317 UPON GEAR EXTENSION, RIGHT MAIN GEAR INDICATOR LIGHT WOULD NOT ILLUMINATE. EMERGENCY GEAR EXTENSION CHECKLIST WAS ACCOMPLISHED; GEAR EXTENDED MANUALLY. EMERGENCY DECLARED. TROUBLESHOT RT GEAR INDICATION FOUND A BROKEN WIRE J64 & S82 OFF OF PIN A REPAIRED WIRE IAW CESSNA 560 WIRING MANUAL CHAPTER 20-00-00 INDICATOR OPS CHECK SATISFACTORY PERFORMED GEAR RETRACTION BLED SYSTEM IAW CESSNA 560 MAINTENANCE MANUAL CHAPTER 32-30-00. SERVICED EMERGENCY GEAR BOTTLE IAW CESSNA 560 MAINTENANCE MANUAL 12-13-01. GEAR SYSTEM CHECKS SATISFACTORY. 2L72 4F RTA22CE 20050420000792005042000079NM 2005 4 20 HNAA0500037 120050407A7932 WARNING LIGHT DHAV DHC8 DHC8102 2809003NM NR 1 ENGINE ILLUMINATED A HNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA07930HQ 126 NR 1 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED ON TAKEOFF, AT ROTATION, OIL PRESSURE WAS AT 40 PSI. 2H72 4T RTA13NM 20050420000802005042000080CE 2005 4 20 DTA200500663 120050407A2120 SMOKE CESSNA750 750 2076810CE COCKPIT DETECTED E DXTAC ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 GL07910QS 7500110 WHITE SMOKE FILLED CABIN ON GROUND. SECURED APU BLEED AND SMOKE DISSIPATED. TURNED BLEED ON, PACS OFF. NO SMOKE, SMELLS OILY. 2L72 4J RTT00007WI 20050420000812005042000081CE 2005 4 20 DXTA200500665 120050204A291099146371 MANIFOLD CESSNA750 750 2076810CE HYD SYSTEM BYPASSING E DXTAK NONE JE WARNING INDICATION VIBRATION/BUFFET DEDESCENT 1 GL07964QS1541 7500164 ON DESCENT THROUGH 17,000 AND 330 KTS IAS, GEAR UNLOCK LIGHT ILLUMINATED FOLLOWED BY THE GREEN NOSE GEAR LIGHT THEN BOTH EXTINGUISHED. THUD WAS FELT AND HEARD BY CREW. TROUBLESHOT DISCREPANCY TO A INTERMITTENLY FAILING LANDING GEAR CONTROL VALVE. REMOVED VALVE AND REPLACED IT WITH A MODIFIED VALVE OPS CHECK GOOD. WORK PERFORMED IAW CHAPTER 32-30-02 AND CHAPTER 32-00-01 OF THE CITATION 750 MM. 2L72 4J RTT00007WI 20050420000842005042000084EA 2005 4 20 QXEA200500505 120050321A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 200 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09613QX 10045 PDX - FUSELAGE SKIN HAS TWO ADJACENT GOUGES RIGHTHAND SIDE FS 357 WL 92.5. REPAIRED IAW CRJ 700 SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050418001702005041800170EU 2005 4 18 USAA050387 120050304A5347F5347821720000 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW22938 0337 BFM - FOUND SEAT TRACK CORRODED 4 INCH BY 1 INCH AREA, Y450 FROM FRAME 72-75. CORROSION LEVEL 2, TASK C534159-01. REMOVED AND REPLACED TRACK PER SRM 51-42-11. (M) 2L72 4F RTA46NM 20050418001972005041800197EU 2005 4 18 USAA050435 120050311A5321F5367233800100 FLOOR PANEL AIRBUS330 A330323 3930335EU FUSELAGE DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW22038 0337 BFM - FOUND FLOOR PANEL DELAMINATED AND CORRODED GREATER THAN 10 PERCENT, MAIN CABIN HEAT FLOOR PANEL 272JF. FABRICATED NEW FLOOR PANEL PER TYPICAL REPAIR 53-02-01. (M) 2L72 4F RTA46NM 20050418001982005041800198EU 2005 4 18 USAA050273 120050129A5347F53477214201 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19671UW22760 0323 BFM - FOUND TRACK CORRODED 11 AREAS TOTAL OF 14 SQUARE INCH MAX D .055 INCH, -Y 450, FRAME 58-68 MAIN CABIN FLOOR SEAT TRACK. REMOVED AND REPLACED SEAT TRACK PER SRM 53-00-15. (M) 2L72 4F RTA46NM 20050418002032005041800203EU 2005 4 18 USAA050269 120050204A5320F53479046005 FLOOR SUPPORT AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19671UW22760 0323 BFM - FOUND FLOOR SUPPORT BEAM CORRODED, .038 INCH DEEP BY .50 INCH LONG BY .50 INCH WIDE, FRAME 75-76, -Y1850 MAIN CABIN FLOOR. REMOVED AND REPLACED FLOOR SUPPORT BEAM PER SRM 53-41-14, 57-42-11. CORROSION LEVEL 2, TASK C534159-01. (M) 2L72 4F RTA46NM 20050418002192005041800219EU 2005 4 18 USAA050397 120050307A5347F5347621420100 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW22938 0337 BFM - FOUND SEAT TRACK CORRODED .8 INCH LONG BY .3 INC WIDE BY .058 INCH DEEP, -Y450 BETWEEN FRAME 55-58. REMOVED AND REPLACED WITH NEW SEAT TRACK SECTION PER SRM 51-74-00 AND 53-00-15 FIG 1 SHEET 2. (M) 2L72 4F RTA46NM 20050418002352005041800235EU 2005 4 18 USAA050262 120050207A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19671UW22760 0323 BFM - FOUND SEAT TRACK CORRODED 7 INCH BY 3.5 INCH BY .030 INCH DEEP, FRAME 32-33, -Y450, MAIN CABIN FLOOR. FABRICATED NEW TRACK SECTION AND SPLICES, INSTALLED REPAIR PARTS PER SRM 53-00-15, FIG 204. (M) 2L72 4F RTA46NM 20050418002442005041800244EU 2005 4 18 USAA050442 120050315A5320F5311889200 WEB AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW22938 0337 BFM - FOUND WEB CORRODED 1.9 INCH LONG BY .85 INCH WIDE BY .030 INCH DEEP, Y953 FRAME 12-12A. CORROSION LEVEL 2, TASK C531123-01. REMOVED AND REPLACED WITH NEW WEB PER SRM 51-74-00 AND 51-72-11. (M) 2L72 4F RTA46NM 20050418002452005041800245EU 2005 4 18 USAA050432 120050330A5347F5711057120400 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE NICKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW22938 0337 BFM - FOUND SEAT TRACK NICKED AND GOUGED 7 INCH BY 7 INCH AREA, Y 1959 AT FRAME 40-47. REMOVED AND REPLACED SEAT TRACK. (M) 2L72 4F RTA46NM 20050418002482005041800248EU 2005 4 18 USAA050407 120050312A5347F571105722020000SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW 0337 BFM - FOUND SEAT TRACK CORRODED .90 INCH LONG BY .10 WIDE BY .030 DEEP, Y2462 FROM FS 46-47. FABRICATED SEAT TRACK SPLICE PER SRM 53-31-15. (M) 2L72 4F RTA46NM 20050419000882005041900088WP 2005 4 19 AALA20050247 120050408A49905940405503 OIL CAP DOUG DC9 DC982 3022082WP APU UNSECURE A AALAA UNSCHED LANDING KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21490AA 49683 AUS - ON ROTATION BURNING OIL SMELL IN COCKPIT. AT ABOUT 2000 FEET FLIGHT ATTENDANT CALLED TO REPORT SMOKE IN CABIN THAT ALSO SMELLED LIKE BURNING OIL. RETURNED TO AUS AND LANDED WITHOUT INCIDENT. PLACARD APU FOR OIL LEAK. REPLACED COALESCER BAGS AND ACCOMPLISHED PACK BURN. ACCOMPLISHED FUNCTIONAL CHECK FLIGHT FERRY TO DFW. FOUND OIL CAP NOT SECURE. CLEANED RESIDUE OIL FROM APU AND RAN APU WITH PACKS. NO SMOKE OR OIL SMELL. 2L72 4F A6WE 20050420000352005042000035CE 2005 4 20 Z4TA20050001 120050303A7933MS280341 ELEMENT BEECH 58 58 1152740CE CONT O550 IO550C SO RT ENGINE SHORTED E Z4TAK NONE O OTHER ININSP/MAINT 1 SO0595KM TH1315 810485 DURING GROUND RUN, DISCOVERED RIGHT ENGINE OIL TEMP WOULD NOT REACH GREEN RANGE. REPLACED OIL TEMP SENDER AND SYSTEM OPS CK OK. OIL TEMP SENDER BULB ALLOWED OIL TO LEAK INTO ELECTRICAL CONNECTION CAVITY, THUS SHORTING THE CONNECTION. 1L72 3O3 O 3A16 E3SO 20050420000382005042000038WP 2005 4 20 0657 120050305A3297DC26A1415S CONNECTOR DOUG DC8 DC863F 302198FWP LT MLG DIRTY A U2RAO OTHER N FALSE WARNING CLCLIMB 1 GL23865F 77744822 46088 LEFT MAIN GEAR DOWN AND LOCK SAFE LIGHTS DID NOT COME ON. PERFORMED ABNORMAL CHECKLIST. AFTER LANDING LIGHT CAME ON. 2L74 4F 4A25 20050420000442005042000044NM 2005 4 20 FX7A200500003 120050318A3600320115 SHUTOFF VALVE BOEING727 727224 1384076NM PWA JT8 JT8D15 52051NE NR 1 ENGINE DEFECTIVE A FX7AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO1979749 22451 DURING CLIMB ENGINE NR 1 STRUT OVER HEAT LIGHT ILLUMINATED. 2L73 4F4 F A3WE E2EA 20050420000542005042000054 2005 4 20 F3LA200500016 420050328A3460 COMPUTER AIRBUSA319 A319111 3930336NM FLT MANAGEMENT MALFUNCTIONED A F3LAO OTHER J WARNING INDICATION APAPPROACH 1 NM03932FR 2258 AUTOPILOT APPEARED TO ENTER A HARDOVER CONDITION, DISCONNECTED A/P AS ACFT ATTEMPTED TO ROLL RIGHT PAST 30" ADB. PERFORMED AFS TEST, TESTED OK. PERFORMED LAND CAT 3 TEST, TESTED OK. ACCOMPLISHED MEL 02-60-01A. PERFORMED DOWNLOAD OF FLT DATA RECORDER, NO TURBULENCE OR PILOT ERROR. ROLL ANGLE DIFFERENTIAL LIGHT DID NOT INDICATE ANY ANOMALIES. BOTH FMGC'S WERE REPLACED AS PRECAUTIONARY. BOTH UNITS HAVE BEEN QUARANTINED FOR EVALUATION BY AIRBUS. IN DEN, PERFORMED ANOTHER AFS TEST & LAND CAT IIIB TEST, OPS TEST CHECK GOOD. UPGRADED CAT IIIB, REMOVED MEL. 1ST OCCURRENCE ON F9 FLEET, PER AIRBUS, VERY RARE. OEB JANUARY, 2005, INDICATES SOFTWARE ISSUE. PER AIRBUS, NEW SOFTWARE WILL BE DESIGNED THIS SUMMER. 2L72 4F RTA28NM 20050420000592005042000059CE 2005 4 20 03032905 120050329A2120 SHUTOFF VALVE CESSNA208 208B 2073701CE CABIN AIR CONTAMINATED E HSYAA UNSCHED LANDING O OTHER CLCLIMB 1 NM05851FE 208B0166 DURING CLIMBOUT, OBSERVED A MIST OR CONDENSATION IN COCKPIT & INSIDE OF WINDSCREEN. PILOT SELECTED WINDSHIELD DEFROST WHICH ACCELERATED RATE OF CONDENSATION. DESELECTED DEFROST, CABIN HEAT & DONNED EMERGENCY O2. DECLARED EMERGENCY DUE TO SUSPECTED SMOKE & RETURNED. STANDING WATER IN CABIN HEATER BOX. AIRCRAFT OPERATED IN HEAVY WIND & RAINY CONDITIONS DURING BOTH GROUND & FLIGHT TIME. SERVICEABLE AFTER DRYING WITH COMPRESSED AIR. MAINTENANCE FOUND WATER IN FWD/AFT DISTRIBUTION BOX & DRIED WITH COMPRESSED AIR. PERFORMED GROUND RUNS AT MAX HEAT. NO FURTHER DISCREPANCIES NOTED. SUSPECT WATER MAY HAVE ENTERED CABIN DURING GROUND TIME (MAIN DOOR OPEN) AND ACCUMULATED IN LEFT & RIGHT PLENUN. 1H71 3T A37CE 20050420000762005042000076EU 2005 4 20 DXTA200500660 120050403A3260 WARNING LIGHT BRAERO1000 HAWKER1000 7450005EU MLG ILLUMINATED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07503QS 259003 ON CLIMBOUT, AFTER GEAR SELECTED UP, THREE RED UNSAFE LIGHTS SHOWED (LM, NOSE, RM) AS WELL AS THE GREEN RIGHT MAIN LIGHT. RETURNED FOR LANDING GEAR SELECTED DOWN THREE GREEN INDICATED AS WELL AS BOTH GREEN STANDBY LIGHTS AND NOSE GEAR PIN WAS EXTENDED FOR A SHORT WHILE THE RM RED UNSAFE REMAINED ON BUT THEN EXTINGUISHED. CYCLED LANDING GEAR NUMEROUS TIMES AFTER SHIMMING SIDESTAYS. ALL GEAR LIGHTS INDICATED NORMAL OPERATIONS. COULD NOT DUPLICATE SQK WORK DONE IAW HAWKER 1000 AMM 32-60-00. 2L72 4F RTA3EU 20050421000052005042100005NM 2005 4 21 05FDEA00331 120050302A27824059005901 ACTUATOR DOUG MD11 MD11F 3023600NM SLATS MALFUNCTIONED A FDEAJA DUMP FUEL UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SO25607FE 48547 FLAP DISAGREE ALERT AFTER TAKEOFF AT WSSS. CONFIG PAGE SHOWED SLATS EXT L22/25, R24/23. DID QRH PROCEDURE. DUMPED FUEL TO RETURN TO WSSS. REMOVED AND REPLACED FLAP DUPLEX ACTUATOR AND ALL 4 INBD FLAP CONTROL VALVE RESTRICTORS. 2L73 4F RTA22WE 20050421000072005042100007CE 2005 4 21 DXTA200500577 120050204A3260 WARNING SYSTEM CESSNA560 560XL 2076702CE COCKPIT MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL07635QS 5605358 WHILE IN DESCENT THE LT GREEN LANDING LIGHT CAME ON ALONG WITH THE "LO BRAKE PRESS" AND "ANTISKID INOP" ANNUNCIATORS & MASTER CAUTION. ALL LIGHTS WENT OUT AFTER A COUPLE OF MINUTES AND LANDING WAS NORMAL. COULD NOT DUPLICATE AT THIS TIME. JACKED ACFT, PERFORM FUNCTIONAL CHECKS OF GEAR SYSTEM. INSPECTED AND CLEANED CONNECTORS, FROZE UPLOCKS SWITCHES. MEGA OHM CHECKED WIRING. ALL CHECKED GOOD. ALL WORK COMPLIED WITH REF CE560XL M/M 32-61-00. 2L72 4F RTA22CE 20050421000082005042100008 2005 4 21 DXTA200500580 420050205A2210 AUTOPILOT SYS CESSNA750 750 2076810CE COCKPIT MALFUNCTIONED E DXTAO OTHER E VIBRATION/BUFFET CRCRUISE 1 GL07933QS 7500133 DURING CRUISE, AUTOPILOT INPUTS FOR AILERON & UPPER RUDDER CONTROL OSCILLATES CONTINUOUSLY. TURBULENCE INCREASES THE INTENSITY & FREQUENCY OF OSCILLATIONS. APPLIED PRESSURE ON FLT CONTROLS (AILERON & RUDDER PRESSURE). ON CONTROL PANEL SYNOPTIC AILERON MOVES FROM NEUTRAL TO 1/3 "UP" AILERON POSITION. RESET RUDDER TRIM ACT. IAW 27-26-00. RESET LINK TO YAW DAMPENER TO NEUTRAL POSITION 7 PUSH PULL ROD TO RUDDER SUMMING LINK OUT PUT TO NEUTRAL. RESET RUDDER COMMAND BUNGEE TO NEUTRAL IAW 750 MM 27-20-00. RESET UPPER "B" RUDDER RTV TO NEUTRAL IAW 750 MM 27-24-01. RESET TRIM INDICATOR TO NEUTRAL IAW 750 M/M CHAP. 27-14-01. ACCOMPLISHED RUDDER RIG CHECK IAW MM 27-00-00. CHECKS GOOD. 2L72 4J RTT00007WI 20050421000102005042100010NM 2005 4 21 SB05026 120050211A33501012621 LIGHT BOEING737 737301 1384611NM SEAT ROW 9 INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19340US 23237 PILOT REPORTED THE FLOOR LEVEL EMERGENCY LIGHT AT SEAT ROW 9 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050421000112005042100011NM 2005 4 21 2005UALA00132 120050125A2830 CONNECTOR BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUEL PUMP MISPINNED A UALAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 WP29662UA 27159 FUEL JETTISON SYSTEM FAILED. THE JETTISON SYSTEM FAULT LIGHT ILLUMINATED AND THE LH JET PUMP EICAS MESSAGE APPEARED WHEN THE LH JETTISON PUMP FAILED TO GENERATE SUFFICIENT PRESSURE TO SET THE PRESSURE SWITCH. THIS WAS A RESULT OF THE PUMPS SHIP SIDE ELECTRICAL CONNECTOR BEING PINNED INCORRECTLY. TWO OF THE THE AC PHASE LEADS AT CONNECTOR D12188 WERE SWAPPED. REPINNED ELECTRICAL CONNECTOR D12188 PER 767 WDM 28-31-21. 2L72 4F4 FRTA1NM E24NE 20050421000132005042100013NM 2005 4 21 2005UALA00134 120050206A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29598UA 28751 AREA 20 INCHES AFT OF DOOR 3 RIGHT IS DAMAGED. SKIN WAS HFEC INSPECTED FOR CRACKS AND A DOUBLER REPAIR WAS INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050421000152005042100015NM 2005 4 21 2005UALA00137 120050210A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29598UA 28751 AFT PIT STA 1460 AND STR 25L, FRAME IS DENTED ON THE INBD FLANGE. INSTALLED NESTED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20050421000182005042100018NE 2005 4 21 HNAA0500010 220050215A7320324485318 FUEL CONTROL DHAV DHC8 DHC8201 2809001NM PWA 120 PW120 NE NR 1 ENGINE MALFUNCTIONED A HNAAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 EA07985HA 479 AG0013 AFTER T/O NR 1 ENGINE HAD NO RESPONSE TO POWER LEVER MOVEMENT. CYCLING ECU W/ PWR LEVER MOVEMENT HAD NO CHANGE TO RESPONSE. DURING THIS SEQ, TQ HAD DROPPED FROM 105 TO 52 PERCENT AND STAYED UNCHANGED. ON APPROACH ENGINE RETURNED TO NORMAL OPS. REMOVED AND REPLACED MFC. LEAK AND OPS CHECK GOOD. 2H72 4T4 TRTA13NM E20NE 20050421000192005042100019NM 2005 4 21 UPS05543911 120050218A2560 SMOKE GOGGLES BOEING757 75724APF 1384969NM CABIN INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01452UP 25473 SMOKE GOGGLES MISSING UNDER JUMPSEAT. INSTALLED SERV SMOKE GOGGLES. 2L72 4F RTA2NM 20050421000202005042100020SO 2005 4 21 C2XA05SH011 120050121A3350RPSIB BATTERY PACK EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714940 145033 DURING SERVICE ROUTINE, LT OVERWING EMERGENCY LIGHT AND 3RD CEILING PANEL EMERGENCY LIGHT DO NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED NR 1 BATTERY AND BATTERY PACK FOR EMERGENCY LIGHT ON LT FWD OVERWING AND 3RD CEILING PANEL IAW EMB 145 AMM 33-50-11. OPS CHECK GOOD. 2L72 4F RTT00011AT 20050421000212005042100021NM 2005 4 21 SB05028 120050219A335071080201 POWER UNIT AIRCRUISERS BOEING737 7373B7 1384580NM ESCAPE SLIDE DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19426US 1246 24548 DURING ANNUAL OPERATIONAL CHECK OF THE AFT LEFT ENTRY DOOR ESCAPE SLIDE, THE SLIDE DEPLOYED NORMALLY BUT THE SLIDE MOUNTED EMERGENCY LIGHTS FAILED TO ILLUMINATE. SLIDE OPERATIONAL CHECK FAILED. MAINTENANCE FOUND THE POWER UNIT ASSEMBLY FOR THE ESCAPE SLIDE MOUNTED LIGHTS HAD FAILED. MAINTENANCE REMOVED AND REPLACED THE AFT LEFT ENTRY DOOR ESCAPE SLIDE ASSEMBLY. TWO ADDITIONAL OPERATIONAL CHECKS ARE SCHEDULED TO BE CONDUCTED AT THE AFT LEFT ENTRY DOOR POSITION PER US AIRWAYS POLICY AND PROCEDURES. 2L72 4F RTA16WE 20050421000222005042100022EU 2005 4 21 05FDEA00307 120050218A2910 LINE AIRBUS300 A300F4605R 3930327EU HYD SYSTEM LEAKING A FDEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO25659FE 757 AFTER SLAT RETRACTION LOST YELLOW SYS HYD PUMP, FOLLOWED BY LOW PRESSURE. ONE MINUTE LATER LOST YELLOW SYS QUANTITY. APPROX 1 MIN PUMP WAS RUNNING. FOUND LEAK AT FLEX LINE JUST BEHIND TOP OF LT MAIN GEAR LEG. ADDED MPN A2714201300000, CPN 2713423 QTY 1, ADDED MPN 190L0F21D, CPN 0021528 QT. REPLACED LEAKING HYD LINE WITH NEW LINE P/N A2714201. 300000 PER SMP. SERVICED YELLOW HYD RESEVOIR IAW MM 12-12-29-0. PERFORMED CHECK OF YELLOW HYDRAULIC SYS AND YELLOW ENGINE DRIVEN HYD PUMP, AND WHOLE SYSTEM CHECKED GOOD. 2L72 4F RTA35EU 20050421000232005042100023NE 2005 4 21 UPS05143914 220050220A7200 ENGINE AIRBUSA300 A300F4622R 3930360EU PWA 4158 PW4158 NE NR 1 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01160UP 0005 NR 1 ENGINE INLET SKIN CRACKS. R&R LT ENGINE NOSE COWL IAW A300 MM THRU STEP 3B (10). INSTALLED LT NOSE COWL LEAK CHECK GOOD REF MM. THIS CLEARS D296652 INSPECTION. 2L72 4F4 FRTA35EU E24NE 20050421000252005042100025EU 2005 4 21 EM05003 120050216A3350 BATTERY EMB ERJ170ERJ170100 EU EMERGENCY LIGHT INOPERATIVE A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19814MD 000033 FLIGHT 1834, DFW TO DCA, EMERGENCY LIGHT BATTERY FAULT AFTER POWER UP ON APU, COULD NOT EXTINGUISH AFT EXIT SIGNS. MAINTENANCE, AIRCRAFT FERRIED TO DCA. PERFORMED OPERATIONAL CHECK OF LIGHTS IAW AMM 33-50-00-710-801-A, CHECK IS GOOD. MTSI, AS A PRECAUTIONARY ACTION, NEXT MAINTENANCE OPPORTUNITY, CHANGE THE AFT EMERGENCY LIGHT POWER UNIT. 2L74 4F RTA56NM 20050421000282005042100028EA 2005 4 21 SWIA200514616 120050219A3320 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN SMOKE A SWIAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 NM07903SW 7425 ON CLIMBOUT SMOKE TOILET CAUTION MESSAGE ILLUMINATED. SMOKE ALARM SOUNDED AND SMOKE VISIBLE IN LAV AREA. RETURNED TO KCRW. REPLACED LAV OVERHEAD LIGHT ASSY PER CRJ MM CH 33. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050421000292005042100029SO 2005 4 21 WRLA2005058 120050215A5311 SPAR CAP PIPER PA32 PA32R300 7103213SO CENTER W/W CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 32R7680095 DURING "C04" CHECK INSPECTION, FOUND CORROSION IN CENTER W/W UPPER SURFACE, UPPER CAP AND SUPPORT FITTING SLANT PRESSURE PANEL STRUCTURE, AROUND FASTENER HEAD AT STA 1376 X=-8, X=-16, X=-31 TTL 6 LOCATIONS. 1L71 3O A3SO 20050421000312005042100031NM 2005 4 21 SB05032 120050223A2450BACC18AE25 CIRCUIT BREAKER BOEING737 7373B7 1384580NM COCKPIT BURNED A USAAF ACTIVATE FIRE EXT. BA SMOKE/FUMES/ODORS/SPARKS FLAME/FIRE TXTAXI/GRND HDL 1 EA19394US 23316 AFTER LANDING CREW STOPPED A/C ON TAXIWAY & REPORTED TO INBOUND RAMP, FIRE & SMOKE IN COCKPIT. CREW STATED, "ON TAXI-IN, FIRE ERUPTED FROM F/O LWR C/B PNL. USED PORTABLE HALON FIRE EXTINGUISHER & EVACUATED A/C. ENG 1 & 2 & APU FIRE EXTINGUISHER BOTTLES DISCHARGED. ALL 4 ESCAPE SLIDES ACTIVATED FOR EVACUATION." PAX`S & CREW EVACUATED A/C W/O INCIDENT. DURING APPROACH, NORMAL EQUIP COOLING C/B POPPED. MX FOUND TERMINAL END ON C-PHASE LUG C/B C813 BURNED. REPLACED C/B C813 & TERMINAL END. CHECKED ALL WIRING FOR SHORTS TO GROUND. NO FAULTS FOUND. ALL CIRCUITS CHK GOOD, OPS CHK NORM, BLOWER FAN GOOD. 2L72 4F RTA16WE 20050421000332005042100033 2005 4 21 UPS05243938 420050222A2564 LIFE RAFT BOEING727 72722C 138400FNM AFT OF LAV MALFUNCTIONED A IPXAO OTHER O OTHER CRCRUISE 1 SO01942UP 19101 LIFE RAFT LOCATED AFT OF LAV EXPERIENCED AN UNCOMMANDED INFLATION. NO DAMAGE TO THE A/C WAS NOTICED. A/C NOW IN HEAVY MAINTENANCE IN SNN. INSTALLED SERVICEABLE LIFE RAFT MM 25-60-00 LOG PAGE 333531 THIS WAS TRANSFERRED TO NRC768041 AT SNN. 2L73 4F A3WE 20050421000352005042100035NM 2005 4 21 SB05033 120050226A3397 WIRE BOEING737 7373B7 1384580NM SEAT 19ABC BROKEN A USAAK NONE O OTHER ININSP/MAINT 1 EA19527AU 23862 PHL - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT AT SEAT 19ABC INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRES. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050421000362005042100036NM 2005 4 21 USAA040081A 120050101A5300 FLANGE BOEING737 7373B7 1384580NM RT PYLON CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 SW99522AU48282 23857 FOUND FLANGE CRACKED .5 INCH,PANEL 582-8R OPENING IN RT PYLON. STOP DRILLED THE CRACK, INSTALLED DOUBLER PER TYPICAL REPAIR 54-30-07. (M) 2L72 4F RTA16WE 20050422000012005042200001GL 2005 4 22 05FDEA00332 220050302A7530 ENGINE DOUG DC10 DC1010F 3022111WP GE CF6 CF66D 30020GL NR 1 STALLED A FDEAO OTHER RXJPARTIAL RPM/PWR LOSS ENGINE FLAMEOUT WARNING INDICATION DEDESCENT 1 SO25370FE49091 46608 451428 ON DESCENT FROM 36,000 TO 35,000 AND AGAIN DESCENT TO 34,000 FT NR 1 ENGINE COMPRESSOR STALLED AND N1, N2 WENT TO LESS THAN IDLE, RESTARTED EACH TIME AND HAD MUCH COMPRESSOR STALLS. ENGINE WAS THEN SHUT DOWN. BOROSCOPE INSPECTED NR 1 ENGINE FOR STALLS, FOUND DAMAGE IN 1ST STAGE HPC BLADES HAS TEARS AND EVIDENCE OF RUBBING ON LEADING EDGES, 3RD STAGE HAS TORN BLADE, 4TH STAGE HAS SEVERE TIP CLANG, ALSO 5TH STAGE HAS SEVERE TIP CLANG. REQUIRES ENG CHANGE. INFO 02MAR05 APPROVED THIS ENGINE FOR CHANGE DUE TO THE DAMAGE AND TIP CLANG. 2L73 4F4 F A22WE E23EA 20050422000032005042200003NM 2005 4 22 05FDEA00336 120050302A5313 STRINGER BOEING727 727227 1384078NM FUSELAGE TOOL DAMAGE A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25481FE 21463 TOOLING DAMAGE AT BS 1010 STRINGER 7L IN STRINGER CLIP AND STRINGER SPLICE. REPAIRED PER SRM 53-10-2. 2L73 4F A3WE 20050422000052005042200005NM 2005 4 22 05FDEA00346 120050303A534065453136 STRINGER CLIP BOEING727 727227 1384078NM FUSELAGE MISDRILLED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 BONUS HOLES IN STRINGER CLIP AT BS 950F STR 7L. REPLACED PER SRM 51-30-2 2L73 4F A3WE 20050422000082005042200008NM 2005 4 22 2005UALA00140 120050213A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSLAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29578UA 26694 AFT PIT STA 1480 FRAME IS DENTED ON INBD FLANGE AT STR 26L. INSTALLED NESTED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20050422000092005042200009NM 2005 4 22 2005UALA00141 120050213A5340146N38108200 SPLICE BOEING757 757222 1384956NM PWA 2037 PW2037 NE CIRCUMFERENTIAL CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29578UA 26694 AFT PIT STA 1400 LBL 18 CIRCUMFERENTIAL SPLICE IS CORRODED. DAMAGE CAUSED BY TYPICAL STA 1400 PIT CORROSION. FABRICATED CIRCUMFRENTIAL SPLICE STRAP AND REPLACED CORRODED STRAP. 2L72 4F4 FRTA2NM E17NE 20050422000102005042200010NM 2005 4 22 2005UALA00142 120050213A5322146N10846 SHEAR TIE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSLEAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29578UA 26694 AFT PIT FRAME SHEAR TIE IS CORRODED AT STA 1400 BETWEEN STRINGERS 27L AND 28L. DAMAGE CAUSED BY TYPICAL STA 1400 PIT CORROSION. REPLACED SHEAR TIE. 2L72 4F4 FRTA2NM E17NE 20050422000112005042200011NM 2005 4 22 2005UALA00143 120050213A5322146N16021 SHEAR TIE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29578UA 26694 AFT PIT FRAME SHEAR TIE IN BILGE AREA IS CORRODED AT STA 1400 BETWEEN STR 28L AND 29L. DAMAGE CAUSED BY TYPICAL STA 1400 PIT CORROSION. REPLACED SHEAR TIE. 2L72 4F4 FRTA2NM E17NE 20050422000122005042200012NM 2005 4 22 2005UALA00144 120050213A5322 SHEAR TIE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29578UA 26694 AFT CARGO PIT SHEAR TIE CORRODED AT BS 1340 AND RBL 27. DAMAGE CAUSED BY TYPICAL AFT PIT CORROSION. REPLACED SHEAR TIE. 2L72 4F4 FRTA2NM E17NE 20050422000132005042200013NM 2005 4 22 2005UALA00145 120050213A5322146N542645 SHEAR TIE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29578UA 26694 STA 1400 SHEAR CLIP SEVERELY CORRODED. DAMAGE CAUSED BY TYPICAL STA 1400 PIT CORROSION. REPLACED SHEAR TIE. 2L72 4F4 FRTA2NM E17NE 20050422000212005042200021NM 2005 4 22 2005UALA00154 120050213A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29578UA 26694 AFT PIT STA 1620 FRAME IS DENTED ON INBD FLANGE AT STR 25R. INSTALLED NESTED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20050422000232005042200023NM 2005 4 22 2005UALA00157 120050213A5315 STIFFENER BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FLOORBEAM CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29652UA 25390 FLOORBEAM AT STA 246 HAS A CRACKED VERTICAL STIFFENER ON FWD FACE OF BEAM AT APPROX LBL 26. REPLACED CRACKED STIFFENER. 2L72 4F4 FRTA1NM E24NE 20050422000312005042200031NM 2005 4 22 2005UALA00165 120050220A5310143N832253 CREASE BEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29581UA 26701 CABIN LT CREASE BEAM AT STA 670-680, LBL 64 HAS CORROSION. DAMAGE CAUSED BY TYPICAL FLOOR AREA CORROSION AT DOOR SILL LOCATIONS. ANGLE WHICH IS PART OF THE LOWER DOOR SILL INSTALLATION WAS REMOVED AND REPLACED TO ADDRESS THE OUT OF LIMITS CORROSION. 2L72 4F4 FRTA2NM E17NE 20050422000332005042200033NM 2005 4 22 2005UALA00167 120050220A5322140N2002215 SHEAR TIE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29581UA 26701 AFT PIT SHEAR TIE HAS CORROSION AT BS 1480 BETWEEN STR 28L AND 28R. DAMAGE CAUSED BY TYPICAL AFT PIT CORROSION. SHEAR TIE REMOVED AND REPLACED TO ADDRESS CORROSION. 2L72 4F4 FRTA2NM E17NE 20050422000352005042200035NM 2005 4 22 2005UALA00172 120050220A53119638203000 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE BULKHEAD DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29934UA 26662 178 BULKHEAD UPPER FRAME ANGLE LT SIDE AT SPLICE HAS 2 EACH HOLES WITH NO EDGE DISTANCE. TRIMMED THE DISCREPANT FRAME, FABRICATED AND INSTALLED REPAIR FRAME SPLICE ANGLE. 2L72 4F4 FRTA16WE E2GL 20050422000362005042200036NM 2005 4 22 2005UALA00173 120050222A5310 SHEAR WEB BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29581UA 26701 AFT CABIN FLOOR, SHEAR WEB CORRODED AT BS 1681 RBL38. AFT PRESSURE DECK SHEAR WEB DAMAGE CAUSED BY TYPICAL GALLEY AREA CORROSION. CORROSION WAS REMOVED AND DECK WEB WAS REPAIRED USING DOUBLERS AND SHIMS. 2L72 4F4 FRTA2NM E17NE 20050422000372005042200037NM 2005 4 22 2005UALA00174 120050222A5230 SKIN BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE CARGO DOOR DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29667UA 29239 BULK CARGO DOOR OUTER SKIN IS DENTED, AFT END MID SECTION. REPAIRED DOOR SKIN WITH DOUBLER AND FILLERS PER SRM 52-30-01. 2L72 4F4 FRTA1NM E24NE 20050422000432005042200043NM 2005 4 22 2005UALA00181 120050223A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29581UA 26701 AFT PIT STA 1460 LT FRAME DENTED AT STR 25L ON INBD FLANGE.TYPICAL PIT FRAME UPPER INNER FRAME CAP DAMAGE. FRAME REPAIRED USING NESTED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20050422000442005042200044NM 2005 4 22 2005UALA00182 120050223A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29581UA 26701 AFT PIT STA 1480 FRAME DENTED ON INBD FLANGE AT STR 26L. TYPICAL PIT FRAME UPPER INNER FRAME CAP DAMAGE. FRAME REPAIRED USING NESTED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20050422000452005042200045NM 2005 4 22 2005UALA00183 120050223A5315 FLOORBEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29305UA 23666 CORROSION ON FWD LT CABIN FLOORBEAM AT STA 294.5 LBL 37-53. ACCOMPLISHED. BLENDED OUT DAMAGE AND INSTALLED ANGLE/STRAP REPAIR. 2L72 4F4 FRTA16WE E2GL 20050422000462005042200046NM 2005 4 22 2005UALA00184 120050223A5312 PRESSURE PANEL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29305UA 23666 STA 664 PRESSURE DECK IS CRACKED AT APPROXIMATELY LBL 30. ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20050422000492005042200049NM 2005 4 22 2005UALA00199 120050221A2621233N6203 CONTROL PANEL BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE COCKPIT FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29647UA 25284 NR 2 CARGO FIRE SQUIB DOES NOT TEST. FOUND 757 TYPE APU/CARGO FIRE CONTROL PANEL INSTALLED. WITH THAT PANEL INSTALLED, THE NO. 2 CARGO SQUIB TEST LAMP WILL NOT LIGHT DUE TO DIFFERENT INTERNAL CIRCUITRY IN THE PANEL, PANEL WAS REPLACED WITH 767-322 TYPE APU/CARGO FIRE CONTROL PANEL. 2L72 4F4 FRTA1NM E24NE 20050422000542005042200054CE 2005 4 22 DXTA200500616 120050306A21301173T421 THERMAL SWITCH CESSNA500 560CESSNA 2076750CE CABIN PRESSURE FAILED E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL07342QS5983 5600324 AFTER TAKEOFF CABIN PRESSURE DUMPED SUDDENLY AND EMERGENCY PRESSURE CAME ON. RETURNED TO FIELD BECAUSE OF BURNING SMELL. TROUBLESHOT FOUND ACM 450 DEG SWITCH FAILED IN OPEN POSITION. REMOVED AND REPLACED SWITCH WIT A NEW SWITCH IAW CE 560 MM 21-51-00. OPS CHECK GOOD. 2L72 4F RTA22CE 20050422000552005042200055 2005 4 22 380WL0002 420050307A3454 INDICATOR BOEING737 7373G7 1384595NM VOR/ILS SYSTEM MALFUNCTIONED A PIDAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO05380WL 23218 NR 2 NAV-ILS, FLAGS WHEN IN VOR/ILS/AP MODE. PLACED ON MEL 22-15-7 AND 8. PERFORMED TROUBLE-SHOOTING PROCEDURE FOR VOR/ILS SYSTEM PER MM 34-31-00. NO DEFECTS NOTED. CLEARED MEL. 2L72 4F RTA16WE 20050422000572005042200057NM 2005 4 22 2005UALA00197 120050301A5315 FLOORBEAM BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29117UA 28810 AFT PIT FLOOR TEE CHORD FLANGE DENTED AT STA 1780 AND RBL 48. DENT MEASURES 0.5 LONG BY 0.5 WIDE BY 0.06 5 INCH DEEP. 2L74 4F4 FRTA20WE E24NE 20050422000582005042200058NM 2005 4 22 2005UALA00210 120050303A5320 FLANGE BOEING747 747422 1384935NM PWA 4056 PW4056 NE EXT POWER DOOR DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29177UA 24384 EXTERNAL POWER RECEPTICLE DOOR FLANGE HAS AN AREA APPROX 0.5 INCH IN DIA, BURNED AWAY FROM HEAVY ARCHING ON LOWER EDGE. SOURCE OF DAMAGE UNCERTAIN. ROUTINE INSPECTION DISCOVERED DAMAGE. REPAIR PROVIDED BY ENGINEERING. 2L74 4F4 FRTA20WE E24NE 20050422000592005042200059NM 2005 4 22 05FDEA00390 120050307A5347ACA7104523 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA Y= 635, X= -27 FOUND WITH APPROX 4 INCHES LONG CRACKED. TRIMMED PER SRM 53-70-00 VOLUME I, FIGURE 1. REWORKED SEAT TRACK AND SPLICES INSTALLED PER SRM 53-70-00 VOLUME I, FIGURE 1. 2L73 4F RTA22WE 20050422000602005042200060NM 2005 4 22 05FDEA00391 120050307A5347ACA7104523 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA Y= 635, X= -8.5 FOUND WITH APPROXIMATELY 4 INCHES LONG CRACKED. REWORK SEAT TRACK INSTALLED PER SRM 53-70-00 VOLUME I, FIGURE1 2L73 4F RTA22WE 20050422000612005042200061NM 2005 4 22 05FDEA00392 120050307A5347A5A70821 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA Y= 5-83, X= -8.5 FOUND WITH CORROSION. REWORKED TRACK INSTALLED PER SRM 53-70-00 VOLUME I FIGURE 1. 2L73 4F RTA22WE 20050422000632005042200063SO 2005 4 22 C2XA05TY026 120050306A712014532835001 MOUNT EMB 145 EMB145LR 3260212SO NR 2 ENGINE WORN A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714952 145067 TYS DURING A SCHEDULED 4C INSPECTION THE NR 2 ENGINE MOUNT FORWARD UPPER WAS FOUND MIGRATED. MAINT REMOVED, CLEANED AND MEASURED THE DEFECT, FAB A NEW BUSHING AND INSTALL, TORQUE AND SAFTIED MOUNT BOLTS IAW AMM71-20-00. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20050418001612005041800161EU 2005 4 18 USAA050270 120050205A5320F53478242203 SUPPORT BEAM AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19671UW 0323 BFM - FOUND SUPPORT BEAM CORRODED, 2.5 INCH BY 2 INCH BY .060 INCH DEEP, FRAME 80-81, -Y390 -Z240. REMOVED AND REPLACED WITH NEW PART PER SRM 53-00-15. CORROSION LEVEL 2, TASK C534159-01. (M) 2L72 4F RTA46NM 20050418001782005041800178NM 2005 4 18 USAA050368 120050311A5347143T52186 SEAT TRACK BOEING767 767201 1385125NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19648US 23900 BFM - FOUND SEAT TRACK CORRODED 1 INCH BY .5 INCH BY .052 INCH AREA, CABIN FLOORBEAM STATION 664-752 RBL 88.5. INSTALLED NEW SEAT TRACK AND SPLICE REPAIR PER SRM 53-00-52 DWG NR 143T5218. (M) 2L72 4F RTA1NM 20050418001832005041800183EU 2005 4 18 USAA050381 120050306A5320F5331533220000 FLANGE AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW22938 0337 BFM - FOUND FLANGE CORRODED 1 INCH BY 1 INCH BY .050 INCH DEEP AREA, FRAME 40.2, Y10 LOWER BELLY FAIRING SUPPORT. REMOVED AND REPLACED FLANGE PER SRM 51-72-11, 51-42-11. (M) 2L72 4F RTA46NM 20050418001932005041800193EU 2005 4 18 USAA050417 120050308A5347F5347721420200 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW22938 0337 BFM - FOUND SEAT TRACK CORRODED 1 INCH BY .500 INCH BY .01 INCH BY 1 INCH BY .500 INCH BY .035 INCH, Y 450 FS 68-72 -Z240. REPLACED WITH NEW SEAT TRACK PER SRM 53-00-15 FIG 101 SHEET 1. (M) 2L72 4F RTA46NM 20050418001942005041800194EU 2005 4 18 USAA050426 120050314A5347F5311170220000 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW22938 0337 BFM - FOUND SEAT TRACK CORRODED 1 INCH LONG BY 1 INCH WIDE BY 0.025 INCH DEEP, Y953 FRAME 13 -Z -240. CORROSION LEVEL 2, TASK C53117201. REMOVED AND REPLACED WITH NEW SEAT TRACK PER SRM 51-74-00, AND 53-11-15. (M) 2L72 4F RTA46NM 20050418001992005041800199EU 2005 4 18 USAA050412 120050310A5320F5347968620000 WEB AIRBUS330 A330323 3930335EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW 0337 BFM - FOUND CUSP WEB CRACKED 1 INCH, Y 1447.8 AT FS 78-79. REMOVED AND REPLACED WEB PER SRM 51-42-11. (M) 2L72 4F RTA46NM 20050418002052005041800205EU 2005 4 18 USAA050420 120050308A5347F5347721420000 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW 0337 BFM - FOUND SEAT TRACK CORRODED 1.5 INCH BY 1 INCH BY .50 INCH AREA, Y450 FRAME 58-67 -240. INSTALLED NEW SEAT TRACK PER SRM 53-00-15 FIG 101 SHT 2. (M) 2L72 4F RTA46NM 20050418002062005041800206EU 2005 4 18 USAA050422 120050314A5347F5711057120401 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW 0337 BFM - FOUND SEAT TRACK CORRODED 1.5 INCHES LONG BY .7 INCHES BY .025 INCH DEEP, -Y1959 FRAME 40-47 -Z240. REMOVED AND REPLACED WITH NEW SEAT TRACK PER SRM 51-74-00, 53-31-15 FIG 101 SHT 8. (M) 2L72 4F RTA46NM 20050418002082005041800208EU 2005 4 18 USAA050396 120050307A5347F5347721010400 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW22938 0337 BFM - FOUND SEAT TRACK CORRODED .70 INCH LONG BY .085 INCH WIDE BY .030 INCH DEEP, -Y2462 BETWEEN FRAME 58-62 -Z240. REMOVED AND REPLACED WITH NEW SEAT TRACK PER SRM 51-74-00, 53-00-15 FIG 101 SHT 2. (M) 2L72 4F RTA46NM 20050418002102005041800210EU 2005 4 18 USAA050425 120050317A5347F5311170420000 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAO OTHER O OTHER ININSP/MAINT 1 EA19673UW 0337 BFM - FOUND SEAT TRACK CORRODED, FS 18 -Y950-Z240. REPLACED SEAT TRACK PER SRM 53-00-15 FIG 101, 51-72-11, 51-42-11. (M) 2L72 4F RTA46NM 20050418002112005041800211EU 2005 4 18 USAA050404 120050312A5320F5311171720100 FLOOR SUPPORT AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW22938 0337 BFM - FOUND FLOOR SUPPORT CORRODED 1.5 FT BY .5 INCH WIDE BY .025 INCH DEEP, Y-2500 LATERAL FLOOR SUPORT. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 53-11-14. CORROSION LEVEL 2, TASK C53213401. (M) 2L72 4F RTA46NM 20050418002182005041800218EU 2005 4 18 USAA050414 120050311A5347F53477214201 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW 0337 BFM - FOUND SEAT TRACK CORRODED, 20 INCHES LONG BY .50 INCH WIDE BY .020 INCH DEEP, Y-450 FROM 59-67. REMOVED AND REPLACED SEAT TRACK PER SRM 53-00-15, 51-42-11, 51-44-11, 51-23-11. (M) 2L72 4F RTA46NM 20050418002332005041800233EU 2005 4 18 USAA050259 120050202A5315F5311170420000 FLOORBEAM AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19671UW22760 0323 BFM - FOUND RAIL CORRODED 3 INCH BY 2 INCH BY .030 INCH DEEP, FRAME 14, -Y953 MAIN CABIN FLOOR. REMOVED AND REPLACED FLOORBEAM PER SRM 53-11-15. (M) 2L72 4F RTA46NM 20050418002392005041800239EU 2005 4 18 USAA050267 120050204A5347F53111701200 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19671UW22760 0323 BFM - FOUND SEAT TRACK CORRODED, 2 INCHES LONG BY .25 INCHES WIDE BY .067 INCH DEEP, FRAME 17 PLUS Y450 MAIN CABIN FLOOR. REMOVED AND REPLACED SEAT TRACK PER SRM 53-11-15 FIG 101 SH 7, 51-42-11. (M) 2L72 4F RTA46NM 20050418002432005041800243EU 2005 4 18 USAA050441 120050311A5321F5367233700200 FLOOR PANEL AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW 0337 BFM - FOUND FLOOR PANEL DELAMINATED AND CORRODED MORE THAN 10 PERCENT, MAIN CABIN HEATED FLOOR PANEL 271KF. FABRICATED NEW FLOOR PANEL PER TYPICAL REPAIR 53-02-01. (M) 2L72 4F RTA46NM 20050419000912005041900091WP 2005 4 19 AALA20050255 120050410A3350 SOCKET DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW213507A 49801 DFW - EMERGENCY LIGHT AT SEAT 25D INOPERATIVE. REPLACED SOCKET AT SEAT 25D FOR EMERGENCY SEAT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050419000932005041900093NM 2005 4 19 AALA20050253 120050410A3350 LIGHT BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21373AA 25200 MIA - EMERGENCY LIGHT EXIT SIGN BY SEAT 20G BROKEN. REPLACED EMERGENCY LIGHT ASSEMBLY FOR EMERGENCY LIGHT EXIT SIGN AT SEAT 20G. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA1NM 20050420000422005042000042CE 2005 4 20 03132005 120050313A7810 EXHAUST DUCT CESSNA500 550 2076604CE PWA JT15 JT15D4 52112NE NR 1 ENGINE DAMAGED E STZAK NONE O OTHER ININSP/MAINT 1 AL0388NM 5500590 PCE70376 PILOTS REPORT THAT WHILE EN ROUTE FROM MERRILL FIELD TO ANCHORAGE INTL, HEARD AN UNUSUAL NOISE AND FEEL A LOW FREQUENCY VIBRATION. ALL SYSTEM AND ENGINE INDICATIONS WERE NORMAL. POST FLIGHT INSPECTION REVEILED DAMAGE ON THE NR 1 ENGINE TURBINE WHEEL AND REAR EXHAUST DUCT ASSEMBLY. LARGE PIECES OF THE EXHAUST DUCT WERE MISSING AND IMPACT DAMAGES IS EVIDENT ON THE TURBINE WHEEL. ENGINE ROTATES FREELY, HOWEVER IT ALWAYS ROTATES BACK TO THE SAME POSITION INDICATING A SEVERE IMBALANCE IN THE ROTATING GROUP. NO EVIDENCE OF IMPACT OR FOD DAMAGE TO THE FAN OR COMPRESSOR SECTION AT THIS TIME. FURTHER INFORMATION MAY BE AVALIABLE POST ENGINE TEARDOWN. 1L72 4F4 F A22CE E1NE 20050420000462005042000046NE 2005 4 20 T48R200500002 220050328A7532UNKNOWN BLEED VALVE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE ENGINE MISSING B GTIAO OTHER O OTHER NRNOT REPORTED 1 GL09835NK 53044 725704 ENGINE WAS REMOVED FOR DELAMINATION OF THE DIFFUSER OUTER DUCT SOUND ABSORBING LINER. DISASSEMBLY SHOWED A MISSING 6TH STAGE BLEED VALVE WHICH RESULTED IN AIR LEAKAGE DAMAGING THE OUTER SOUND ABSORBING LINERS. 2L72 4F4 FRTA6WE E9NE 20050420000632005042000063NM 2005 4 20 C8GA20050009 120050329A7714652185723 LINE BOEING727 727200 138407ENM EPR PROBE BROKEN A C8GAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO15713AA55645 22469 FLT 712 FROM DEN TO SAN. ON TAKEOFF ROLL, NR 2 EPR WOULD NOT INCREASE ABOVE 1.8. ABORTED TAKEOFF WITHOUT FURTHER INCIDENT. TAXIED AIRCRAFT TO ENGINE RUN-UP AREA. CONFIRMED NR 2 EPR WOULD NOT INCREASE ABOVE 1.84. ALL OTHER ENGINE PARAMETERS GOOD. PLACED NR 2 EPR GAUGE ON MEL. AIRCRAFT RELEASED FOR SERVICE. ON 4/01/05, FOUND PT 7 LINE BROKEN BETWEEN NR 3 AND NR 4 EPR PROBE. REPLACED BROKEN LINE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L73 4F RTA3WE 20050421000032005042100003WP 2005 4 21 05FDEA00330 120050302A5310AFA3248 DRAIN DOUG DC10 DC1010F 3022111WP ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25369FE 46607 COMPLY WITH EA 8-5310-55454, FUSELAGE MAIN FRAME BULK CARGO DOOR LWR JAMB SILL CORROSION REPAIR (P/N AFA3248). CLOSING ACTION ON 02/28/05. ON N/R S00015, COMPLIED WITH EA8-5310-55454. 2L73 4F A22WE 20050421000042005042100004CE 2005 4 21 5285002 120050301A326065430087 UPLOCK SWITCH CESSNA560 560XL 2076702CE RT MLG DEFECTIVE E ERYAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE07422AB1068 5605285 AFTER DEPARTURE FROM FSM, LANDING GEAR UNLOCK LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. EXTENDED GEAR SUCCESSFULLY, RETURN TO FSM UNEVENTFUL. FOUND FAULTY UPLOCK SWITCH. 2L72 4F RTA22CE 20050421000172005042100017NM 2005 4 21 SWAA050437 120050215A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 DURING SCHEDULED A1 CHECK, FOUND 3 EACH FUSELAGE SKIN CRACKS AT BS 727E, STRINGER 23L AND STRINGER 19R, BS 867, STRINGER 24R. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20050421000322005042100032 2005 4 21 BB05012 420050224A2565140N297611 ATTACH BRACKET BOEING757 7572B7 1384964NM R1 DOOR SLIDE LOOSE A USAAO OTHER O OTHER CRCRUISE 1 EA19614AU 27145 TPA - IN-FLIGHT, THE GIRT BAR ENGAGEMENT LIGHT EXTINGUISHED AT THE R1 DOOR. MAINTENANCE SECURED A LOOSE GIRT BAR ATTACH BRACKET. 2L72 4F RTA2NM 20050422000022005042200002NM 2005 4 22 05FDEA00335 120050302A5753652163249 SKIN BOEING727 727227 1384078NM TE FLAPS GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 LT IB MID FLAP UPPER SURFACE IS GOUGED AT OB END 13 INCHES FROM LE. BLENDED GOUGE ON LT IB MIDFLAP OB END PER FEDEX EA 7-5710-86252 2L73 4F A3WE 20050422000042005042200004NM 2005 4 22 05FDEA00337 120050302A5313 STRINGER BOEING727 727227 1384078NM FUSELAGE TOOL DAMAGE A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25481FE 21463 TOOLING DAMAGE AT BS 1010 STRINGER 7L IN STRINGER CLIP AND STRINGER SPLICE. REPAIRED PER SRM 53-10-2 (DUPLICATE ENTRY TO TRACKING NR 05-0336) 2L73 4F A3WE 20050422000152005042200015NM 2005 4 22 2005UALA00148 120050213A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29578UA 26694 CREASE NEAR BELLY CENTERLINE AT BS 1385 (EXTERIOR). SKIN DOUBLER REPAIRS AND STRINGER REPAIRS WERE ACCOMPLISHED. 2L72 4F4 FRTA2NM E17NE 20050422000272005042200027NM 2005 4 22 2005UALA00161 120050216A5322 SHEAR TIE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29581UA 26701 AFT PIT SHEARTIE HAS CORROSION STA 1460, BETWEEN STR 28L AND 28R. REPLACED SHEAR TIE. 2L72 4F4 FRTA2NM E17NE 20050422000302005042200030 2005 4 22 2005UALA00164 420050116A256560461101 ASPIRATOR AIRCRUISERS D31042205 BOEING757 757222 1384956NM PWA 2037 PW2037 NE ESCAPE SLIDE DISTORTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29513UA 0648 24810 FOUND ASPIRATOR FLATTENED DURING INSPECTION FOR OVERHAUL. ASPIRATOR MIXING TUBE WAS DISTORTED AT DISCHARGE END. IT IS SUSPECTED THAT ASPIRATOR HAD BEEN DAMAGED DURING THE LAST PACKING PROCESS. NO OTHER DAMAGE WAS OBSERVED. ASPIRATOR WAS REPLACED. 2L72 4F4 FRTA2NM E17NE 20050422000392005042200039 2005 4 22 2005UALA00177 420050222A2564644831 INDICATOR AIRCRUISERS BOEING757 757222 1384956NM PWA 2037 PW2037 NE RAFT BOTTLE LEAKING A UALAK NONE O OTHER ININSP/MAINT 1 WP29587UA 122151292 26713 LOW BOTTLE PRESSURE. PRESSURE LOSS WAS DUE TO LEAKAGE FROM PRESSURE GAUGE WINDOW. PRESSURE GAUGE WAS REPLACED. 2L72 4F4 FRTA2NM E17NE 20050422000402005042200040NM 2005 4 22 2005UALA00178 120050223A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29581UA 26701 FWD PIT STA 600 FRAME DENTED AT STR 24L ON INBD FLANGE. TYPICAL PIT FRAME UPPER INNER FRAME CAP DAMAGE. FRAME REPAIRED USING NESTED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20050422000412005042200041NM 2005 4 22 2005UALA00179 120050223A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29581UA 26701 FWD PIT STA 640 FRAME DENTED ON INBD FLANGE AT STR 25R. TYPICAL PIT FRAME UPPER INNER FRAME CAP DAMAGE. FRAME REPAIRED USING NESTED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20050422000522005042200052NM 2005 4 22 DHL2005754002 120050304A324026011825 BRAKE ASSY BOEING727 727223 1384074NM MLG CHATTERING A DHLAD RETURN TO BLOCK E VIBRATION/BUFFET TXTAXI/GRND HDL 1 SO01754DH 22008 BRAKES CHATTER WHEN APPLIED. REPLACED NR 3 & 4 MAIN BRAKE ASSY'S PER 727 MM 32-41-32, TAXIED A/C PER JRH, BRAKES OPS CHECKS NORMAL. 2L73 4F A3WE 20050422000682005042200068EU 2005 4 22 05FDEA00425 120050308A5712 RIB AIRBUS310 A310 EU RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 RT WING 4 IN IB OF RIB 30 L/E AREA AFT PANEL LANDING IS CRACKED REF N00636. REMOVED AND REPLACED LANDING IAW SRM 51-40-21 AND 51-72-10 AND DRW A57243955. 2L72 4F RTA35EU 20050422000692005042200069NM 2005 4 22 05FDEA00427 120050308A5322 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 CORROSION ON SHEAR TIE BS 970 STR 29R -30R OUT OF LIMITS. REMOVED CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 REPARIED PER SRM 53-10-4 2L73 4F RTA3WE 20050422000702005042200070NM 2005 4 22 05FDEA00428 120050308A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 BS 592 STR 23 LT IS DENTED. REPAIRED PER SRM 53-10-3 2L73 4F RTA3WE 20050422000712005042200071NM 2005 4 22 05FDEA00429 120050308A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 BS 592 STR 25 LT IS GOUGED. REPAIRED IAW SRM 53-10-3 2L73 4F RTA3WE 20050422000722005042200072NM 2005 4 22 05FDEA00430 120050308A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 FRAME IS DENTED ON I/B FLANGE AT BS 660 BETWEEN STR'S 23 LT AND 25 LT. REPAIRED PER SRM 51-40-3 2L73 4F RTA3WE 20050422000732005042200073NM 2005 4 22 05FDEA00431 120050308A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 FRAME IS DENTED ON I/B FLANGE AT BS 560 BETWEEN STR'S 24 LT AND 25 LT. REPAIRED PER SRM 51-40-3, 51-10-2, MM 51-20-151-7 AND SRM 51-30-2 2L73 4F RTA3WE 20050422000792005042200079NM 2005 4 22 05FDEA00460 120050308A5753NRC67622 VANE DOUG MD11 MD11 3023602NM ZONE 600 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 RIGHT HAND WING, INBOARD FLAP VANE, LEADING EDGE, ABOUT 25 INCHES (FROM OUTBOARD TO INBOARD). FOUND WITH CHAFFING DAMAGE OF 3 INCHES DIAMETER. REMOVED AND REPLACED PER AMM 27-50-22-02. ADJUSTMENT AND TEST CARRIED OUT PER AMM 27-50-22-05. 2L73 4F RTA22WE 20050419000762005041900076NE 2005 4 19 AALA20050241 220050403A7321 FUEL CONTROL AIRBUS300 A300B4605R 3930308EU GE CF6 CF680C2A5 NE ENGINE INOPERATIVE A AALAA UNSCHED LANDING O OTHER CRCRUISE 1 SW2140064 507 MCO - INABILITY TO FEED FORWARD TO ENGINES FROM INNER FUEL TANKS. ALL PUMPS OPERATE OK. REPLACED FUEL QUANTITY CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA35EU E13NE 20050419000902005041900090WP 2005 4 19 AALA20050257 120050411A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21464AA 49594 SAT - FORWARD GALLEY AND COCKPIT EMERGENCY ESCAPE LIGHT AND AFT CABIN OVERHEAD EMERGENCY LIGHTS FROM ROW 18 BACK INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD GALLEY AND COCKPIT EMERGENCY ESCAPE LIGHTS AND AFT CABIN OVERHEAD EMERGENCY LIGHTS FROM ROW 18 BACK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050419000922005041900092WP 2005 4 19 AALA20050245 120050407A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21572AA 49458 ORD - EMERGENCY LIGHTS IN CEILING ABOVE SEATS 19, 20, AND 21DEF INOPERATIVE. REPLACED BATTERY PACK B5104 FOR EMERGENCY LIGHTS IN CEILING ABOVE SEATS 19, 20, 21DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050420000492005042000049CE 2005 4 20 BSYA200500006 120050329A29102307006112 HOSE LEAR 35 35LEAR 5170600CE NR 3 BRAKE ASSY.LEAKING E BSYAO OTHER K FLUID LOSS APAPPROACH 1 GL074358N1516 065 NR 3 BRAKE HOSE LEAKED DEPLEATING HYD RES. GEAR WOULD NOT CYCLE DOWN, DECLARED AN A EMERGENCY AT CMH, GEAR DID COME DOWN AND LOCK WITH AUX HYD PUMP. LANDED NO PROBLEMS. FOUND NR 3 BRAKE FLEX LINE LEAKING. REMOVED AND REPLACED LINE, CHANGED BOTH ENGINE DRIVEN HYD PUMPS AND FILTERS, SWUNG GEAR SEVERAL TIMES, OPS CHECKS GOOD. 2L72 4F A10CE 20050420000512005042000051SO 2005 4 20 100 220050316A731464936826A1 PUMP PIPER PA34 PA34200T 7103406SO CONT O360 LTSIO360EB 17025SO LT ENGINE FUEL INOPERATIVE B FFKRK NONE O OTHER ININSP/MAINT 1 SO056935C 347870167 826972 INSTALLED A FACTORY REMANUFACTURED ENGINE FROM CONTINENTAL THAT CAME WITH A NEW FUEL PUMP. UPON DOING THE ENGINE GROUND RUNS AND INITIAL ENGINE SET UP THE FUEL PUMP WOULD NOT SHUT OFF THE FUEL AFTER THE MIXTURE HAD BEEN PULLED BACK. INSPECTED SYSTEM FOUND TO HAVE A DEFECTIVE FUEL PUMP, REPLACED FUEL PUMP WITH A FACTORY NEW PUMP FROM CONTINENTAL. NO FURTHER ACTION NEEDED. 1L72 3O3 O A7SO E9CE 20050420000552005042000055 2005 4 20 TSAA0534017 420050327A3416S231A1211 INDICATOR BOEING737 73776N 13844CHNM STDBY ALTIMETER MALFUNCTIONED A TSAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP13741AL 28641 STANDBY ALTITUDE INDICATOR FAILED AT 30,000 FEET ON CLIMBOUT. DIVERTED TO HNL FOR UNEVENTFUL LANDING. LANDED AT 143,600 LBS AND LESS THAN 100 FPM. BRAKES APPLIED AT 90 KIAS, ONLY SLIGHT BRAKING APPLIED. REPLACED THE STANDBY ALTITUDE INDICATOR. OPS CHECK OK IAW AMM 34-24-01-4. PERFORMED AN OVERWEIGHT LANDING CHECK IAW AMM 05-51-35-2. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. VERIFICATION FLIGHT CHECKED OK. 2L72 4F RTA16WE 20050420000782005042000078NE 2005 4 20 T48R200500003 220050408A72305005888021 COMPRESSOR DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE NR 2 ENGINE DAMAGED B GTIAC ABORTED TAKEOFF C F.O.D. TOTAKEOFF 1 GL09804NK 49104 696383 ENGINE WAS REMOVED NR 2 POSITION FOR COMPRESSOR SURGE AT TAKEOFF. TEARDOWN AND INSPECTION REVEALED IMPACT DAMAGE STARTING AT THE 8TH STAGE OF THE N2 COMPRESSOR. ONE EACH VANE WAS MISSING FROM THE C-8 STATOR WITH INCREASING LEVELS OF DAMAGE REARWARD OF THE MISSING VANE. 2L72 4F4 F A6WE E9NE 20050420000822005042000082NM 2005 4 20 DHL2005780002 120050408A2560 DOOR BOEING727 727223 1384074NM ESCAPE ROPE DAMAGED A DHLAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01780DH 22006 EMERGENCY ESCAPE ROPE DOOR ON F/O'S SIDE DOES NOT STAY CLOSED DURING TAXI AND TURBULENCE. THE CEILING PANEL WHERE DOOR LATCHES IS CRACKED. APPLIED TAPE P/N 225FR TO CRACKED OVERHEAD PANEL ON F/O'S SIDE AND DEFERRED PER GMM 3.5 CAT 2 ASSIGNED DMI 20427E PLACARD INSTALLED. 2L73 4F A3WE 20050420000832005042000083 2005 4 20 YENA200526 420050404A23303042865102 ELECTRICAL BOX AIRBUS320 A320232 3930326EU UNKNOWN A YENAK NONE B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA15592JB2238 2259 SMOKE SMELL ROW 8 RT SIDE. ACCOMPLISHED INFO NOTICE 2004-T023TR, OPS CHECKED NO FAULTS FOUND. REMOVED AND REPLACED SEB AT 8E AS PRECAUTIONARY AS STATED IN INFO NOTICE. 2L72 4F RTA28NM 20050421000022005042100002CE 2005 4 21 20030803 120050302A6123 AUTOFEATHER SYS BEECH 1900 1900D 1154162CE LEFT MALFUNCTIONED A GLBAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM03245GL UE245 THE LT AUTO FEATHER AFX ANNUNCIATOR STARTED FLICKERING THEN EXTINGUISHED COMPLETELY AND THEN EVEN PRESS TO TEST WOULD NOT FUNCTION. PERFORMED AIR RETURN WITHOUT FURTHER INCIDENT. MAINTENANCE COULD NOT DUPLICATE AND SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA24CE 20050421000242005042100024 2005 4 21 UPS05143915 420050219A2565 SLIDE AIRBUSA300 A300F4622R 3930360EU CREW DOOR INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01133UP 0816 CREW ENTRY DOOR DOES NOT INDICATE "SLIDE ARMED" ON ECAM DOOR PAGE AFTER ARMING DOOR LEVER. DEFERRED PER MEL 52-30-04. PERFORMED TEST OF ENTRY DOOR LIMIT SW. IAW 52-73-13-5. SYSTEM OPS CK GOOD SEVERAL TIMES. NO HISTORY NOTED A/C OK TO CONTINUE THIS CLEARS M297414. PLACARD REMOVED. 2L72 4F RTA35EU 20050421000262005042100026NM 2005 4 21 375PA0026A 120050221A3610 PRECOOLER BOEING737 737317 138447PNM RT ENGINE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05375PA 23812 RIGHT ENGINE PRECOOLER CRACKED IN O/B UPPER FORWARD CORNER. WELDED PER BAC SPEC 5975. 2L72 4F RTA16WE 20050422000072005042200007NM 2005 4 22 2005UALA00139 120050212A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29598UA 28751 FRAME FLANGE AT BS 1540 AND STR 25L DENTED. INSTALLED NESTED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20050422000142005042200014NM 2005 4 22 2005UALA00146 120050213A5322 SHEAR TIE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29578UA 26694 STA 1400 FRAME SHEAR TIE BETWEEN STR 29R AND 30R IS SEVERELY CORRODED. DAMAGE CAUSED BY TYPICAL STA 1400 PIT CORROSION. REPLACED SHEAR TIE. 2L72 4F4 FRTA2NM E17NE 20050422000172005042200017NM 2005 4 22 2005UALA00150 120050213A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29578UA 26694 AFT PIT STA 1580 AT STR 26L FRAME IS DENTED ON INBD FLANGE. INSTALLED NESTED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20050422000192005042200019NM 2005 4 22 2005UALA00152 120050213A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29578UA 26694 AFT PIT STA 1560 AT STR 26L FRAME IS DENTED ON INBD FLANGE. INSTALLED NESTED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20050422000292005042200029EU 2005 4 22 2005UALA00163 120050216A3010D3615000300061 DUCT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE LT WING CHAFED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29423UA35217 504 LEFT WING BLEED LEAK MESSAGE AFTER TAKEOFF. A SMALL HOLE WAS FOUND IN A WING-ANTI ICE DUCT FLANGE. THE HOLE WAS CAUSED BY A CLAMP CHAFING THE DUCT FLANGE. THE DEFECTIVE DUCT WAS REPLACED AND A NEW CLAMP INSTALLED. 2L72 4F4 FRTA28NM E40NE 20050422000382005042200038 2005 4 22 2005UALA00176 420050223A2565B142681 DISC BOEING757 757222 1384956NM PWA 2037 PW2037 NE SLIDE BOTTLE RUPTURED A UALAK NONE O OTHER ININSP/MAINT 1 WP29506UA 24627 LOW BOTTLE PRESSURE. RUPTURE DISC LEAKING. REPLACED RUPTURE DISC. 2L72 4F4 FRTA2NM E17NE 20050422000422005042200042NM 2005 4 22 2005UALA00180 120050223A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29581UA 26701 FWD PIT FRAME DENTED ON INBD FLANGE AT BS 660 AND STR 24L. TYPICAL PIT FRAME UPPER INNER FRAME CAP DAMAGE. FRAME REPAIRED USING NESTED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20050422000482005042200048NM 2005 4 22 2005UALA00186 120050224A5320 SILL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29303UA 23644 AFT PIT SIL BEAM UPPER STRAP HAS CORROSION FROM STA 847-787. REPLACED STRAP. 2L72 4F4 FRTA16WE E2GL 20050422000652005042200065 2005 4 22 UPS05144034 420050308A2565 INDICATOR AIRBUSA300 A300F4622R 3930360EU ENTRY DOOR SLIDEINOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01133UP 0816 NO ENTRY DOOR SLIDE ECAM IND WHEN DOOR ARMED. DEFERRED PER MEL 52-30-04. PLACARD INSTALLED M298435. R&R SWITCH 13WN OPS CK. NORMAL REF MM 52-73-13-4 THIS CLEARS M298435 2L72 4F RTA35EU 20050422000742005042200074NM 2005 4 22 05FDEA00432 120050308A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 FRAME IS DENTED ON I/B FLANGE AT BS 680 BETWEEN STR'S 23 LT AND 25 LT. REPAIRED PER SRM 51-40-3 2L73 4F RTA3WE 20050422000762005042200076NM 2005 4 22 05FDEA00435 120050308A5340 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 MECHANICAL DAMAGE ON STRINGER CLIP AT BS 660, STR 13L. REPLACED PER SRM 51-30-2. 2L73 4F RTA3WE 20050422000782005042200078EU 2005 4 22 05FDEA00439 120050308A5730 PANEL AIRBUS310 A310 EU RT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 RT WING PANEL 650JB HAS 4 EA ELONGATED REF N00522. REPAIRED PANEL 650JB IAW EA 6-5710-86051. 2L72 4F RTA35EU 20050425001712005042500171NM 2005 4 25 2005UALA00155 120050213A5712 RIB BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE RT WING CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29652UA 25390 RT WING L-E CAVITY AT FSS 512, UPPER RIB LOWER CHORD PREVIOUS REPAIR CRACKED AT AFT END-OUTBD OF NR 8 SLAT OUTBD ACTUATOR. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. RIB REPAIRED WITH ANGLE DOUBLER. 2L72 4F4 FRTA1NM E24NE 20050425001752005042500175NM 2005 4 25 2005UALA00130 120050208A5210 DOOR BOEING747 747422 1384935NM PWA 4056 PW4056 NE 4L NOISY A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29174UA 24381 AFTER TAKEOFF, LOUD NOISE FROM DOOR 4L. ALSO, EICAS MESSAGE FOR DOOR. EXAMINATION OF THE DOOR DID NOT REVEAL ANY DISCREPANCIES. THE DOOR WAS OPERATED SEVERAL TIMES EACH TIME SATISFACTORILY. 2L74 4F4 FRTA20WE E24NE 20050425001762005042500176NM 2005 4 25 2005UALA00136 120050208A3260KD4L036 RELAY BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE MLG FAILED A UALAO OTHER J WARNING INDICATION CLCLIMB 1 WP29377UA 24642 AFTER TAKEOFF GEAR HANDLE WOULD NOT GO UP AND TAKEOFF WARNING HORN SOUNDING. REPLACED R276 RELAY AND ADJUSTED SAFETY SENSOR TARGET. PERFORMED EXTENSION AND RETRACTION CHECK OF THE LANDING GEAR. OPERATIONS CHECK GOOD. 2L72 4F4 FRTA16WE E2GL 20050425001782005042500178WP 2005 4 25 05FDEA00347 120050303A5753ARC2155 PANEL DOUG MD10 MD1010F 3022112WP ZONE 600 DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25361FE 48260 RIGHT OUTBOARD FLAP PANEL 635 HL HAS LARGE AREA OF DELAMINATION. REPAIRED IAW EA 8-5710-83085, COVER ASSY ACCESS, LOWER INBOARD FLAP, REPAIR. REFERENCE NON-ROUTINE N01042. 2L73 4F RTA22WE 20050425001822005042500182EA 2005 4 25 SWIA200514650 120050302A2721 SWITCH CNDAIRCL600 CL6002C10 1390015EA RUDDER TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07705SK 10145 RUDDER TRIM SWITCH DOES NOT RESPOND NORMALLY TO THE RIGHT. REPLACED RUDDER TRIM PANEL IN REFERENCE TO CRJ700 MM27-12-10. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050425001832005042500183 2005 4 25 SWIA200514651 420050302A34178220372445 COMPUTER CNDAIRCL600 CL6002B19 1900309EA AIR DATA MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION APAPPROACH 1 NM07406SW2536 2536 7030 ON APPROACH WITH FLAP PAST 20 DEGREES FLAP OVERSPEED CLACKER OCCURRED. REMOVED AND REPLACED ADC IAW MM 34-13-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050425001842005042500184EA 2005 4 25 SWIA200514655 120050301A2422 INVERTER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07928SW 7664 EMERGENCY FLOOR LIGHTING STRIPS BETWEEN ROWS 5-8 WILL NOT ILLUMINATE. REMOVED AND REPLACED NR 3 INVERTER FOR EMERGENCY LIGHTS IAW CRJ MM 33-51-04, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050425001852005042500185EA 2005 4 25 QXEA200500264 120050217A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 200 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - FUSELAGE EXTERIOR, CROWN FUSELAGE SKIN UNDER TCAS ANTENNA HAS AREAS OF SCRATCHES AT STATION 350 AND STRINGER 0. REPAIRED IAW HORIZON AIR EA R-53-271, REO 670-53-21-071 AND CRJ-700 AMM TAXK 34-43-00-802-A01 AND 34-43-00-710-801. 2L72 4F RTA21EA 20050425001882005042500188EA 2005 4 25 QXEA200500266 120050212A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 200 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - FUSELAGE EXTERIOR CROWN AT STATION 1000 AND STRINGER 3R HAS NICK ON FUSELAGE SKIN. REPAIRED IAW CRJ700 SRM 51-26-00-001-001-A01, 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050425001902005042500190EA 2005 4 25 QXEA200500269 120050207A5230 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - AFT BAGGAGE DOOR OUTER SKIN IS GOUGED AT THE UPPER EDGE OF THE DOOR HANDLE CUTOUT. REPAIRED IAW CRJ700 SRM 52-31-01-001-001-A01 AND 53-00-01-101-001-A01, PARAGRAPH 3A. 2L72 4F RTA21EA 20050425001912005042500191EA 2005 4 25 QXEA200500270 120050211A5751 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 600 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - RIGHT AILERON UPPER SKIN JUST AFT OF LEADING EDGE IS CHAFED AT STATION 290, 340 AND 323. REPAIRED IAW CRJ700 SRM 51-41-02-001-001-A01, 57-61-01-101-001-A01, 51-12-00-001-001-A01, 51-25-00-001-001-A01, 51-25-01-001-001-A01 AND 51-41-02-001-001-A01. 2L72 4F RTA21EA 20050425001922005042500192NM 2005 4 25 C8GA20050007 120050301A302065189221 OVERHEAT SENSOR BOEING727 727223 1384074NM ANTI ICE DUCT INOPERATIVE A C8GAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO15715AA56746 22470 AFTER TAKEOFF, AT 4500 FT, ANTI-ICE DUCT OVERHEAT LIGHT ILLUM. LOWER CARGO FIRE LIGHT ILLUM WITH FIRE WARNING BELL. MX DISPLAY ANNUNCIATOR READING "AFT CARGO". CREW DECLARED AN EMERGENCY, DUMPED FUEL, & RETURNED TO MOTTO. DURING FUEL DUMP, BOTH WARNING LIGHTS EXTINGUISHED. ON FINAL, BOTH WARNING LIGHTS ILLUMINATED & WARNING BELL SOUNDED. AT 1000 FT GAL, ALL WARNING LIGHTS EXTINGUISHED. CREW COMPLETED EMERGENCY & NORMAL CHECKLISTS & LANDED WITHOUT FURTHER INCIDENT. FOUND THERMAL ANTI-ICE OVERHEAT SENSOR INOP. REPLACED SENSOR. OPS CHK GOOD. PERFORMED INSP OF LOWER CARGO BAY. NO EVIDENCE OF FIRE OR OVERHEAT NOTED. LOWER CARGO FIRE DETECTION SYS OPS CHK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L73 4F A3WE 20050425001962005042500196NM 2005 4 25 HNAA0500017 120050302A3040 HEATER DHAV DHC8 DHC8102 2809003NM WINDSHIELD INOPERATIVE A HNAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA07975HA 1136F 176 LEFT WINDSHIELD HOT CAUTION LIGHT ILLUMINATED IN FLIGHT (COOL TO THE TOUCH). A/C DIVERTED TO MDT RATHER THAN LANDING ELM, BECAUSE IT WAS SNOWING THERE. REMOVED AND REPLACED WINDSCREEN HEAT CONTROLLER. 2H72 4T RTA13NM 20050425001972005042500197NE 2005 4 25 HNAA0500016 220050228A7320324485318 FUEL CONTROL DHAV DHC8 DHC8311 1386006EA PWA PW120 PW123 NE ENGINE INOPERATIVE A HNAAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 EA07328EN 281 AE0076 ENGINE SHUT DOWN IN FLIGHT AND RETURNED TO GATE. REMOVED AND REPLACED MFC, OPS AND LEAK CHECK GOOD C/W WORKCARD 76-00-02Q AND TRIMMED ENGINE PER DASH 8 RUNUP MANUAL. 2H72 4T4 TRTA13NM E20NE 20050425002022005042500202NM 2005 4 25 TSAA0538010 120050228A3800 HANDLE BOEING737 73773A 1384606NM POTABLE WATER UNKNOWN A TSAAA UNSCHED LANDING O OTHER CLCLIMB 1 WP13739AL 28500 NO WATER PRESSURE AVAILABLE. RETURNED TO OGG. OVERWEIGHT LANDING MADE AT 142,000 LBS. SMOOTH LANDING. MAINTENANCE RESET THE POTABLE WATER SERVICE HANDLE AT THE SERVICE ACCESS. OPS CHECK NORMAL. PERFORMED OVERWEIGHT LANDING CONDITIONAL INSPECTION PER MM 5-51-35-2. NO HARD LANDING INSPECTION REQUIRED. RETURN TO SERVICE. 2L72 4F RTA16WE 20050425002052005042500205NM 2005 4 25 DHL2005781510 120050213A5730 SKIN BOEING727 727227 1384078NM RT WING GOUGED A DHLAO OTHER O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A "C" CHECK, RT WING TIP LOWER INBD EDGE IS GOUGED BY NR 8 SLAT AND WEB IS DENTED SLAT STA 434.5. REMOVED R/WING TIP AND WEB SLAT STA 434.5 IAW B727 SRM 51-30-2. REMOVED AREA TO ORIGINAL CONTOUR IAW B727SRM 51-40-1. ACCOMPLISHED NOT HFEC AT REMOVED AREA IAW NDT MAT PART 6, 51-00-00 FIG 23. NO CRACKS NOTED, FABRICATED SKIN AT R/WING TIP SLAT MAT USED 7075T6 .040 PO NR 900920 DIM 44 INCH BY 16 INCH IAW B727 SRM 57-30-2 FIG 3 AND 51-20-1. ALODINED AND PRIMED PART IAW B727 SRM 51-10-2. INSTATED NEW SRM IAW B727 SRM 57-30-2 FIG 3. 2L73 4F A3WE 20050425002062005042500206NM 2005 4 25 DHL2005781511 120050215A5753 SKIN BOEING727 727227 1384078NM LT WING FORFLAP GOUGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A "C" CHECK, LT WING INBD FOREFLAP GOUGED ABOVE NR 3 FLAP CARRIAGE (MARKED). REMOVED PREV REPAIR ON L/WING I/B FOREFLAP IAW B727 SRM 51-30-2. FABRICATED REPAIR DOUBLER FROM 2024-T3 .063 IS 8.2 BY 6.4 PO 9001634 IAW B727 SRM 57-50-4 FIG 1 57-50-2 FIG 3. TREAT AND PRIME AREA DOUBLER AND INSTALLED THEM IAW B727 SRM 51-10-2, 57-50-4 FIG 1. 2L73 4F A3WE 20050425002082005042500208NM 2005 4 25 RYNA200500009 120050223A2130S417A2042001 LINE BOEING737 737800* NM POTABLE WATER LEAKING A RYNAB EMER. DESCENT O OTHER CRCRUISE 1 CE07DGZ 28624 DURING CRUISE FLT AT FL350, AUTO PRESSURE FAIL LIGHT ILLUMINATED. SWITCHED PRESSURE MODE CONTROL TO ALTN & LIGHTS REMAINED ON & DIFF PRESSURE BEGAN TO RISE. DIFF PRESSURE REACHED 8.7 PSI, PRESSURE MODE CONTROL SWITCHED TO MANUAL & SLIGHTLY OPENED OUTFLOW VALVE DIFF PRESSURE BEGAN TO DESCEND & CABIN ALT TO RISE. ATTEMPTED TO CLOSE OUTFLOW VALVE, VALVE WOULD NOT CLOSE FULLY, CABIN ALT BEGAN TO RISE. ATC CONTACTED FOR EMERGENCY DESCEND & LANDED W/OUT INCIDENT. INSP OF CURRENT ACRFT ACTIVITY & PAST FAULT REPORTS BY ENGINEERS INDICATED A REAR GALLEY WATER LINE LEAKED. R/R`D REAR GALLEY WATER LINE & OUTFLOW VALVE. GROUND AND FLT TESTS WERE ACCOMP SUCCESSFULLY & A/C DETERMINED READY FOR RETURN TO SERVICE. 2L72 4F RTA16WE 20050425002092005042500209NM 2005 4 25 DHL2005781513 120050217A5754 SKIN BOEING727 727227 1384078NM NR 7 SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A "C" CHECK, CRACKED PANEL SURROUNDING NR 7 SLAT I/B UPSTOP BOLT STOP PAD. REMOVED CRACKED PANEL IAW B727 SRM 51-30-2. FABRICATED PANEL SURROUNDING NR 7 SLAT I/B UPSTOP BOLT STOP PAD MAT USED 2024T3 .050 PO NR 9001684 DIM 18 3/4 INCH BY 8 1/4 INCH IAW B727 SRM 57-50-2 FIG 1 AND 51-20-1. ALOINED AND PRIMED PART IAW B727 SRM 51-10-3. INSTALLED PANEL IAW B727 SRM 727 SRM 57-50-2 FIG 1. 2L73 4F A3WE 20050425002182005042500218NM 2005 4 25 UPS05444348 120050408A532065B05000157 STRAP BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 INSPECTION TYPE:C LT BS 2231 FRAME INNER CHORD AREA FOUND 1EA FASTENER HOLE AT STR 25L CRACKED AT STRAP. ( CRACK LENGTH 0.040 INCH). STRAP REPLACED AS PER SRM 51-10-01 PG 9 2L74 4F RTA20WE 20050425002192005042500219NM 2005 4 25 UPS05444349 120050409A532069B107861 CLIP BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 INSPECTION TYPE:C M/D BS 400 S14L INTERCOSTAL AFT SUPPORT CLIP FOUND CRACKED ( CRACK LENGTH .125 INCH). M/D BS 400 STR 14L INTERCOSTAL AFT SUPT CLIP REPLACED AS PER SRM 51-10-01 PG 9 2L74 4F RTA20WE 20050425002222005042500222NM 2005 4 25 UPS05444303 120050415A5312 PRESSURE PANEL BOEING747 747121 1384871NM NLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE:SV NW-LT SIDE WALL WEB CRACK AT 4 EA HOLE LOCATION AT BS 280 - 300 WL 170 AREA. CRACK LENGTH 4 INCHES. NW-LT SIDE WALL WEB CRACK AREA REPAIR AS PER EO B747-5310-20502 APPENDIX C ITEM 6 INSTRUCTION & SRM 53-10-04 FIGURE 116. 2L74 4F A20WE 20050425002242005042500224NM 2005 4 25 UPS05444305 120050416A5312 PRESSURE PANEL BOEING747 747121 1384871NM NOSE WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE:SV NOSE WHEEL WELL LT SIDE PANEL FROM BS 280-300 WL 160 CRACK AT NR 12 TO NR 14 & NR 16 FASTENER AREA. CRACK LENGTH 5 INCH. CRACKED SIDE PANEL REPAIRED AS PER EO B747-5310-20502 APPENDIX C ITEM (6) INSTRUCTION AND SRM 53-10-04 FIGURE 116. 2L74 4F A20WE 20050425002262005042500226NM 2005 4 25 UPS05444307 120050416A5312 PRESSURE PANEL BOEING747 747121 1384871NM NLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE:SV NOSE WHEEL WELL RT SIDE PANEL FROM BS 280-300 WL 170 CRACK INDICATION FOUND AT FASTENER LOCATION NR 6, 10, 12 AT WEB. CRACK LENGTH 3 INCHES. CRACKED WEB REPAIRED AS PER EO B747-5310-20502-C ITEM (6) INSTRUCTION AND SRM 53-10-04 FIGURE 116. 2L74 4F A20WE 20050425002322005042500232WP 2005 4 25 UPS05844291 120050320A5711 SPAR DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE:C2 POSSIBLE CRACK BETWEEN VERTICAL FASTENERS ON RT WING REAR SPAR LOWER T-CAP RIGHT W/W STA 857 RBL 28-32. NDT DETECTED A 4 INCH CRACK PER NDT SPM 06-10-01.001. STOP DRILLED CRACK PER DWG SRO8570009. REPAIRED REAR SPAR LOWER T-CAP PER DWG SRO8570009. 2L74 4F RT4A25 20050425002332005042500233WP 2005 4 25 UPS05844292 120050318A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE:C2 LEFT WING L/E LWR DRAIN HOLE HAS 2 INCH CRACK AT STA XFS 585. REMOVED DAMAGE, FABRICATED DOUBLER & FILLER, AND INSTALLED IAW DC-8 SRM 57-3-0, 57-2-0 FIG 6, 51-1-21, AND 51-1-20D. 2L74 4F RT4A25 20050425002342005042500234WP 2005 4 25 UPS05844293 120050320A5753 RIB DOUG DC8 DC873F 302199FWP T/E FLAP DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE:C2 RIGHT STA 3 AFT LINK TO FLAP HINGE BOLT FROZEN & NUT PLATE BROKEN. REMOVED DAMAGED RIB, REMOVED AND REPLACED NUT PLATE, AND FABRICATED & INSTALLED REPLACEMENT RIB PER EO DC8-5750-16293-A AND DWG DC8-57-009. 2L74 4F RT4A25 20050425002392005042500239WP 2005 4 25 AALA20050249 120050409A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW217541A 49995 BOS - EMERGENCY TRACK LIGHTING FROM SEAT 20DEF FORWARD INOPERATIVE. REPLACED BATTERY PACK ABOVE SEAT 20DEF AND IN FIRST CLASS GALLEY AND SPLICED TWO CHAFED WIRES FOR EMERGENCY TRACK LIGHTING FROM SEAT 20DEF FORWARD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050425002402005042500240WP 2005 4 25 AALA20050246 120050407A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW217542A 49996 SFO - AFT OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT STATION 909R FOR AFT OVERWING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050425002442005042500244WP 2005 4 25 AALA20050252 120050409A2130 SWITCH DOUG DC9 DC983 3022083WP RIGHT & LEFT INOPERATIVE A AALABG EMER. DESCENT O2 MASK DEPLOYED O OTHER CRCRUISE 1 SW21599AA 53289 DFW - PRESSURIZATION LOSS AT CRUISE (34,000). BOTH PACKS WENT TO ZERO FLOW. STARTED DESCENT PERFORMED PROCEDURES BUT NO HELP. DROPPED 02 MASKS IN BACK. PACKS BEGAN TO WORK AGAIN BETWEEN 8000 AND 6000 FEET. FLOW ON METERS BEFORE CABIN PRESSURIZED DOWN TO AROUND 4000 THEN THE LEFT FLOW BEGAN TO BACK OFF TO MATCH ON THE RIGHT SIDE. REPLACED BOTH RIGHT AND LEFT ENGINE SINGLE ENGINE CLIMB SWITCH. PERFORMED SPECIAL ITEM CARD 4354. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050425002452005042500245WP 2005 4 25 AALA20050251 120050408A33970201975005 WIRE HARNESS DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21579AA 53156 LGA - EMERGENCY EGRESS LIGHTING AT SEAT 27D INOPERATIVE. REPLACED SEAT HARNESS AT SEAT 27D FOR EMERGENCY EGRESS LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050425002472005042500247WP 2005 4 25 AALA20050244 120050406A3397 WIRE DOUG DC9 DC982 3022082WP CABIN DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW217541A 49995 EWR - EMERGENCY LIGHTING FROM ROWS 1 TO 20 INOPERATIVE. REPAIRED WIRING AT SEAT ROW 1 FOR EMERGENCY LIGHTING FROM ROWS 1 TO 20. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050425002482005042500248WP 2005 4 25 AALA20050254 120050409A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21578AA 53155 LAX - EMERGENCY LIGHTS AT AFT CABIN CEILING INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT AFT CABIN CEILING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050425002492005042500249NM 2005 4 25 AALA20050270 120050415A3397 WIRE BOEING767 767323 1385205NM CABIN DISCONNECTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW2139365 24046 SFO - EMERGENCY LIGHTING AT SEATS 32H TO 41H INOPERATIVE. RECONNECTED SOCKET WIRES AT ROW 35 FOR EMERGENCY LIGHTING AT SEATS 32H TO 41H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050425002502005042500250 2005 4 25 AALA20050266 420050413A2565 PIN DOUG DC9 DC982 3022082WP EVAC SLIDE MIGRATED A AALAK NONE O OTHER ININSP/MAINT 1 SW21459AA 49564 RDU - PINS MIGRATED OUT OF EMERGENCY SLIDE AT LEFT NUMBER ONE DOOR. REPLACED LEFT NUMBER ONE EMERGENCY SLIDE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050425002512005042500251 2005 4 25 AALA20050267 420050413A2565 SLIDE BOEING737 737823 13844BZNM L1 DOOR OUT OF POSITION A AALAK NONE O OTHER ININSP/MAINT 1 SW21910AN 29512 RDU - EMERGENCY ESCAPE SLIDE AT LEFT NUMBER ONE DOOR FELL OFF. INSPECTED AND REPLACED EMERGENCY ESCAPE SLIDE AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20050425002522005042500252NM 2005 4 25 AALA20050268 120050413A2150 ACM BOEING737 737823 13844BZNM A/C BAY FAILED A AALAGA O2 MASK DEPLOYED UNSCHED LANDING O OTHER CRCRUISE 1 SW21930AN 29529 MIA - AT FLIGHT LEVEL 390 RAPID DECOMPRESSION OCCURRED AND OXYGEN MASKS DEPLOYED. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. FLIGHT DATA RECORDER SHOWED RIGHT HAND PACK WAS OFF (FLOW CONTROL VALVE) CLOSED UNTIL BOTTOM OF DESCENT. FLIGHT DATA RECORDER ALSO SHOWED LEFT HAND PACK IN HIGH MODE. REPLACED LEFT HAND AIR CYCLE MACHINE AND HEAT EXCHANGER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20050425002542005042500254NM 2005 4 25 AALA20050265 120050402A3350BPS73 BATTERY PACK BOEING757 757223 1384957NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21184AN 29594 DFW - EMERGENCY LIGHTS ABOVE RIGHT OVERWING EXIT DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERWING EXIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050425002552005042500255WP 2005 4 25 ABXA050087 120050407A5320991050131 CUSP WEB DOUG DC9 DC932 3022066WP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23903AX 47427 CUSP WEB CORRODED AT FS 200, BETWEEN SEAT TRACKS, RBL 44.5 - RBL 54.5. CUT OUT CORRODED SECTION OF CUSP WEB AT FS 200 RBL 49. INSTALLED REPAIR DOUBLER IAW DC-9 SRM 53-01 AND 51-30-5. 2L72 4F A6WE 20050425002572005042500257WP 2005 4 25 ABXA050089 120050407A53205917497501 FITTING DOUG DC9 DC941 302207NWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23973AX 47511 DURING ROUTINE LINE MAINTENANCE, FOUND THE AFT FUSELAGE JACK PAD FITTING CORRODED BEYOND LIMITS. REPLACED FITTING IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20050425002592005042500259NM 2005 4 25 AWXA200500482 120050416A5320652981818 BRACKET BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCN - MAJOR REPAIR - DURING C-19 CHECK 2 INCH CRACK WAS FOUND AT FASTENER HOLE AND A 1 INCH CRACK WAS FOUND IN INBOARD FLANGE RADIUS OF GUSSET BRACKET AT FR 335, BETWEEN STR 17 LT AND STR 18 LT. MAINTENANCE REMOVED DAMAGED GUSSET BRACKET AT FR 335, BETWEEN STR 17 LT AND STR 18 LT; FABRICATED A NEW REPLACEMENT BRACKET PER DWG 65-29818; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050425002642005042500264NM 2005 4 25 AWXA200500427 120050311A53205804119 WEB BOEING737 737375 13844BNNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 MCN - MAJOR REPAIR - DURING C-05 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF RT AFT OUTBOARD WEB BETWEEN BS 996 AND BS 1016, RBL 44 AND RBL 46. MAINTENANCE BLENDED OUT CORROSION ON UPPER SURFACE OF RT AFT OUTBOARD WEB FROM BS 996 TO BS 1016, RBL 44 TO RBL 46 AND FOUND MATERIAL LOSS OUT OF LIMITS BETWEEN BS 1006 AND BS 1016, RBL 44 AND RBL 46. REMOVED CORRODED AREA OF WEB FROM BS 1006 TO BS 1016, RBL 44 TO RBL 46; FABRICATED A NEW SECTION OF WEB PER DWG 65-45855; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050425002652005042500265NM 2005 4 25 AWXA200500428 120050310A551069730963 PIN BOEING737 737375 13844BNNM HORIZ STAB CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 MCN - FLIGHT CONTROL - DURING C-05 CHECK CORROSION WAS FOUND ON LT HORIZONTAL STABILIZER INNER HINGE PIN. MAINTENANCE REMOVED AND REPLACED THE LT HORIZONTAL STABILIZER INNER HINGE PIN IAW T/C E6C55102. 2L72 4F RTA16WE 20050425002662005042500266NM 2005 4 25 AWXA200500429 120050313A5320652072613 ATTACH ANGLE BOEING737 737375 13844BNNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 MCN - MAJOR REPAIR - DURING C-05 CHECK EXFOLIATION CORROSION WAS FOUND ON FORWARD CARGO DOOR LOWER SILL, LOWER AFT ATTACH ANGLE AT BS 491, RBL 23. MAINTENANCE REMOVED CORRODED LOWER AFT ATTACH ANGLE AT BS 491, RBL 23; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 65-20726; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050425002672005042500267NM 2005 4 25 AWXA200500430 120050326A53206546579510 STIFFENER BOEING737 737375 13844BNNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 MCN - MAJOR REPAIR - DURING C-05 CHECK CORROSION WAS FOUND ON U-CHANNEL (STIFFENER) AT BS 1113 ON RT SIDE 3.5 INCH FROM BOTTOM, STR 17 RT. MAINTENANCE REMOVED CORRODED STIFFENER AT BS 1113, STR 17 RT; FABRICATED A NEW REPLACEMENT STIFFENER PER DWG 65-46579; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050425002692005042500269NM 2005 4 25 AWXA200500466 120050401A5315654681138 FLOORBEAM BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - DURING C-19 CHECK CORROSION WAS FOUND ON TRANSVERSE FLOORBEAM UPPER CHORD AT BS 986 BETWEEN RBL 18 AND RBL 43, WL 208. MAINTENANCE BLENDED OUT CORROSION ON TRANSVERSE FLOORBEAM UPPER CHORD AT BS 986 BETWEEN RBL 18 AND RBL 43; FABRICATED A REPAIR STRAP; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-51 FIG 203. 2L72 4F RTA16WE 20050426000012005042600001NM 2005 4 26 P5CA0501325 120050303A7830 WARNING LIGHT BOEING747 747283B 1384867NM THRUST REVERSER ILLUMINATED A P5CAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA15921FT 21575 NR 2 ENGINE THRUST REVERSER LIGHT CAME ON FLASHING AS ENGINE APPROACHED TAKE OFF EPR. DEFERRED T/R PER MEL NR 78-3-1B. 2L74 4F A20WE 20050426000022005042600002EU 2005 4 26 WRNA200500002 120050306A3234221TS02Y02 SELECTOR AIRBUS300 A300B4203 3930306EU MLG UNSERVICEABLE A WRNAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO05820SC 154 LANDING GEAR CANNOT BE RAISED AFTER TAKEOFF. AIRCRAFT RETURNED TO AIRPORT. LANDING NORMAL. DURING TROUBLESHOOTING FOUND LANDING GEAR NORMAL CONTROL SWITCH READS NO CONTINUITY BETWEEN PINS H AND K. REMOVED AND REPLACED LANDING GEAR SELECTOR UNIT. OPS CHECK GOOD I/A/W 32-31-11. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA35EU 20050426000032005042600003 2005 4 26 P5CA0501326 420050306A2312 CONTROL PANEL BOEING747 74746NF 13848BTNM VHF COMMS FAILED A P5CAK NONE O OTHER ININSP/MAINT 1 EA15454PA 30812 ALL VHF COMMUNICATIONS FAILED, NO TRANSMIT OR RECEIVE ON ANY RADIO. SWAPPED F/O'S FREQUENCY SELECT PANEL WITH CENTER POSITION AND DEFERRED PER MEL 23-24-1. 2L74 4F RTA20WE 20050426000042005042600004EU 2005 4 26 WRNA200500003 120050305A2710VL35B1 ACTUATOR AIRBUS300 A300B4203 3930306EU LWSPD AILERON UNSERVICEABLE A WRNAJA DUMP FUEL UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO05501TR 53 LT LOW SPEED AILERON FAILED TO DISCONNECT UPON SLAT RETRACTION. FUEL DUMP PROCEDURES FOLLOWED, AIRCRAFT RETURNED TO AIR FIELD, LANDING NORMAL. MANUALLY DISCONNECT LOW SPEED AILERON. LOCK OUT ACTUATOR I/A/W 27-00-00, VERIFIED ROD IS RETRACTED AND IN DISCONNECT MODE MEL 27-11-01 CAT "C" EXP 3-15-05 PLACARD INSTALLED. AIRCRAFT RETURNED TO SERVICE. FOUND LT LOW SPEED AILERON ACTUATOR AT FAULT. REMOVED AND REPLACED LT LOW SPEED AILERON ACTUATOR. SYSTEMS OP'S CHECK GOOD I/A/W 27-11-43, PLACARED REMOVED MEL CLEARED. AIRCRAFT OK FOR SERVICE. 2L72 4F RTA35EU 20050426000052005042600005NM 2005 4 26 DHL2005781514 120050210A5330 SKIN PANEL BOEING727 727227 1384078NM FUSELAGE SCRATCHED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A "C" CHECK, THREE SCRATCHES EXTERIOR SURFACE AT STA 460, STR 5 RIGHT. REMOVED PAINT AFFECTED AREA BS 440 TO BS 460 AT STR 3 TO STR 6 RT SIDE IAW B727 M/M 51-20-1, SCRATCHED AREA FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA AT BS 445 TO BS 455 STR 4 AND 5 RT IAW B727 SRM 53-30-3 FIG 24 DIM 10 BY 3 5/8 FAB. REPAIR DOUBLER FROM 2024 T3 .063 PO 9001387 DIM. 20 1/8 BY 13 1/2, AND FILLER FROM MAT'L 2024 T3 .063 PO 9001387 DIM 22 1/8 BY 10 1/2, IAW B727 SRM 53-30-3 FIG 24 AND 53-30-2, PARTS PAINTED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED IAW B727 SRM 51-30-2. 2L73 4F A3WE 20050426000062005042600006NM 2005 4 26 DHL2005781516 120050211A5754 SKIN BOEING727 727227 1384078NM NR 4 SLAT DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A "C" CHECK, LT L/E SKIN DENTED 15 INCH I/B OF NR 4 SLAT I/B TRACK. CUT OUT DAMAGED AREA AT LT WING L/E SKIN I/B NR 4 SLAT, I/B TRACK DIM.3/4 BY 3/4 IAW B727 SRM 57-30-4 FIG.1. FABRICATED DOUBLER REPAIR MAT'L 2024 T3 .050 PO 9001873 DIM 3 1/4 BY 3 3/4 IAW B727 SRM 57-30-2 FIG 3 AND 57-30-1 FIG 1. TREATED, ALODINE AND PRIMED IAW B727 SRM 51-10-. INSTALLED REPAIR DOUBLER AT LT WING L/E SKIN I/B OF NR 4 SLAT I/B TRACK IAW B727 SRM 51-30-2. 2L73 4F A3WE 20050426000072005042600007NM 2005 4 26 DHL2005781518 120050213A5330 SKIN BOEING727 727227 1384078NM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A "C" CHECK, L1 DOOR UPPER HINGE CUTOUT IS CRACKED AT BS 303. REMOVED EXISTING FASTENERS, CUT OUT DAMAGED AREA DIM 1.5 X .5. ACCOMPLISHED NDT INSPECTION AROUND CUTOUT, NO CRACK NOTED. FABRICATED DOUBLER FROM 301 CRESS 1/2 HARD .063, PO 900125 DIM. 16 1/8 BY 6 FILLERS FROM 2024 T3 .080 PO 9001011 DIM. 7 1/2 BY 6 3/4 AND 1 1/2 BY 1 1/4 TREATED AND PRIMED IAW B727 SRM. INSTALLED REPAIR PARTS IAW B727 S/B 727-53 A0198, REV 2 AND SRM 51-30-2 AND 51-10-2. 2L73 4F A3WE 20050426000092005042600009NM 2005 4 26 DHL2005781520 120050213A5311 FRAME BOEING727 727227 1384078NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A "C" CHECK, AFT CARGO DENT FRAME STA 1110 AT STA 23 LT. REMOVED FASTENERS FOR ACCESS AT AFT CARGO STA 1110 AT STA 23 LT IAW B727 SRM 51-30-2. CUT OUT DAMAGE AREA DIMENSION 2 INCH BY 1 INCH IAW B727 SRM 51-40-3 FIG 1. FABRICATED FRAME REPAIR MAT USED 7075-T6 .071 PO NR 900573 DIMENSION 18 INCH BY 5 1/4 INCH IAW B727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1. ALODINED AND PRIMED AREA AND PART IAW B727 SRM 51-10-2. INSTALLED FRAME REPAIR IAW B727 SRM 51-40-3 FIG 1. 2L73 4F A3WE 20050426000132005042600013NM 2005 4 26 RYNA200500007 120050223A2133 OUTFLOW VALVE BOEING737 737800* NM CABIN PRESSURE MALFUNCTIONED A RYNAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 CE07DGZ 28624 DURING CRUISE AT FL350, THE AUTO PRESSURE FAIL LIGHT ILLUMINATED. SWITCHED THE PRESSURE MODE CONTROL TO ALTN AND THE LIGHTS REMAINED ON AND DIFFERENTIAL PRESSURE BEGAN TO RISE. WHEN THE DIFFERENTIAL PRESSURE REACHED 8.7 PSI, THE PRESSURE MODE CONTROL WAS SWITCHED TO MANUAL AND THE SLIGHTLY OPENED THE OUTFLOW VALVE. THE DIFFERENTIAL PRESSURE BEGAN TO DESCEND AND CABIN ALT TO RISE. WHEN ATTEMPTED TO CLOSE THE OUTFLOW VALVE, THE VALVE WOULDN'T CLOSE FULLY, SO THE CABIN ALT BEGAN TO RISE. CONTACTED ATC FOR AN EMERGENCY DESCEND INTO KMCO. AIRCRAFT LANDED WITHOUT INCIDENT. 2L72 4F RTA16WE 20050426000182005042600018NM 2005 4 26 F3LA20050006 120050308A2750786A000012 PCU AIRBUSA319 A319111 3930336NM TE FLAPS FAILED A F3LAO OTHER F FLT CONT AFFECTED APAPPROACH 1 NM03912FR8944 819 1803 UPON APPROACH SELECTED FLAPS 2, ECAM: FLT CTL FLAPS STUCK AT 0 DEG. RAN CHECK LISTS. FLIGHT CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. SLATS EXTENDED VAPP 155. PERFORMED TROUBLESHOOTING PER TSM 27-51-00-810-810. REPLACED FLAP PCU PER AMM 27-54-51PB401. FLAP SYSTEM OPERATION NORMAL. 2L72 4F RTA28NM 20050426000212005042600021NE 2005 4 26 EM05004 220050306A73144120T04P05 PUMP EMB ERJ170ERJ170100 EU GE CF34 CF348E5 30015NE LT ENGINE UNSERVICEABLE A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19802MD2337 17000013 GEE193130 ENGINE NR 1 NO DISPATCH FAULT MESSAGE. MAINTENANCE, TROUBLESHOT SYSTEM IAW GE EM 72-00-00 FAULT CODES. REMOVED AND REPLACED FADEC, FAULT REMAINED. REMOVED AND REPLACED FUEL METERING UNIT, FAULT REMAINED. REMOVED AND REPLACED FUEL PUMP, FAULT CLEARED. SYSTEM OPERATIONAL CHECK AND LEAK CHECK IS GOOD DURING GROUND ASSURANCE ENGINE RUN UP. 2L74 4F4 FRTA56NM E00063EN 20050426000312005042600031SW 2005 4 26 47518022205 120050222A6330222031605109 FLEXURE BELL 222 222UT 1182148SW LYC LTS101LTS101750C1 41560NE LEFT DELAMINATED E A1UAA UNSCHED LANDING E VIBRATION/BUFFET NRNOT REPORTED 1 CE03419MA9492 47518 4721547041 SHORTLY AFTER TAKEOFF WHILE ACCELERATING THROUGH 40-50 KTS A MODERATE 1/1 WAS NOTED. IT CONTINUED TO WORSEN WITH AIR SPEED. I TURNED AROUND AT ABOUT 100 KTS. LOWERED COLLECTIVE, AND RETURNED TO BASE. THE SEVERITY OF THE VIBRATION LESSENED WITH LOWER COLLECTIVE SETTINGS. DURING INSPECTION OF AIRCRAFT, FOUND THAT THE LT FLEXURE ASSEMBLY WAS DELAMINATING. REMOVED AND REPLACED FLEXURE ASSEMBLY AND CONTINUED OPERATION CHECK FLIGHT. AIRCRAFT RETURNED TO SERVICE. 1G72 3U3 U H9SW E5NE 20050426000322005042600032EU 2005 4 26 05FDEA00441 120050308A5553 ATTACH FITTING AIRBUS310 A310 EU VERTICAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 VERTICAL STAB UPPER EDGE LEFT AND RIGHT FORE TO AFT HAS CORROSION AROUND CAP ATTACH FASTENER HOLES REF N00734. REMOVED AND REPLACED RT CHORD IAW SRM 51-40-21 AND DRW A55371360 AND REPAIRED LT CHORD IAW SRM 51-74-40 FIG 201 2L72 4F RTA35EU 20050426000332005042600033EU 2005 4 26 05FDEA00442 120050308A5753 SKIN AIRBUS310 A310 EU RT WING TE FLAP PUNCTURED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 RT WING I/B FLAP UPPER SURFACE 3.9 IN FROM T/E AND 30 IN FROM I/B END SKIN PUNCTURED REF N00914. REPAIRED FLAP IAW SRM 57-52-12 FIG 4D. 2L72 4F RTA35EU 20050426000372005042600037EU 2005 4 26 05FDEA00446 120050308A5330 SKIN AIRBUS310 A310 EU FUSLEAGE LIGHTNING STRIKEA FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 LT FUSELAGE FRAME 11A APPROX AT STR 18L HAS A LIGHTNING STRIKE. BLENDED OUT AREA IAW SRM 51-73-10 AND 53-10-12 FIG 220 SH 1. 34 PERCENT MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW SRM 53-12-12 DIA 104. REPAIRED SKIN WITH DOUBLER AND FILLER ONLY PER SRM 53-12-12 FIG 202 SH 1 FRAME WAS NOT DAMAGED. 2L72 4F RTA35EU 20050426000392005042600039EU 2005 4 26 05FDEA00449 120050308A5322 SHEAR TIE AIRBUS310 A310 EU FUSELAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25446FE 224 BULK PIT UNDER FLOOR STG 53R FROM 1 INCH FWD OF 66 TO FR 67 HAS CORROSION EXTENDING UNDER SHEAR TIE AT FR 66 AND EXTENDING UNDER FASTENERS IN SEVERAL AREAS. REMOVED CORROSION, CHECK LIMITS MAT'L LOSS EXCEEDED LIMITS IAW A310-200 SRM 53-10-00 FIG 104. REMOVED CORROSION STG SECTION AND FAB REPAIR IAW A310-200 SRM 53-10-14 AND INSTALLED IAW A310-200 SRM 51-40-21. 2L72 4F RTA35EU 20050426000412005042600041EU 2005 4 26 05FDEA00451 120050308A5315 FLOORBEAM AIRBUS310 A310 EU FUSELAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25446FE 224 AFT PIT FLOOR FS 66 10 INCH TO RT OF CTR HAS A 5 INCH BY 2 INCH AREA OF CORROSION. REMOVED CORROSION PER A310-200 SRM 51-74-10. CORROSION OUT OF LIMITS PER SRM 51-10-00. REMOVED CORRODED FLOORBEAM AND INSTALLED NEW BEAM PER A310-200 SRM 51-72-10. REPROTECTED FASTENER HEADS AND TAILS PER A310-200 SRM 53-21-10. SCRAPPED OLD PART PER QC5-0025. 2L72 4F RTA35EU 20050422000642005042200064WP 2005 4 22 DHL2005802001 120050309A323357740355507 ACTUATOR DOUG DC8 DC873 302199CWP MLG LEAKING A DHLAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO01802DH 46076 ON GEAR RETRACTION LOST HYDRAULIC FLUID TO AUX LEVEL. FOUND LT GEAR ACTUATOR LEAKING. REPLACED LT GEAR ACTUATOR PER DC-8 M/M 32-32-2 OPS CHECKS NORMAL 2L74 4F RT4A25 20050425000712005042500071WP 2005 4 25 UPS05843641 120050111A3350 LIGHT DOUG DC8 DC873F 302199FWP COCKPIT INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE:N/A, F/O UNDERGLARE SHIELD EMERGENCY LIGHT INOP. RELAMPED WITH NEW LAMPS. OPS CHECK NORMAL. 2L74 4F RT4A25 20050425001702005042500170NM 2005 4 25 2005UALA00129 120050206A5330143W2331 SKIN BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29224UA11175 30225 FUSELAGE SKIN HAS 2 DENTS AFT OF STA 655 BUTT JOINT BETWEEN S-26L AND S-27L. ONE DENT IS 3.0 INCHES LONG AND 2.75 INCHES WIDE AND 0.028 INCHES DEEP LOCATED 0.5 INCHES AFT OF STA 655 IS DIRECTLY OVER 3 BUTT JOINT FASTENERS, 3 ROWS ABOVE S-27L. OTHER DENT IS IN BAY 6 INCHES AFT OF STA 655 AND 3 INCHES BELOW S-26L, MEASURES 3.0 INCHES LONG BY 2.0 INCHES WIDE BY 0.040 INCHES DEEP. DAMAGE WAS TRIMMED OUT AND EXTERNAL DOUBLERS INSTALLED AS CATEGORY 'B' REPAIR PER EVA ORD-6136 A. 2L72 4F4 FRTT0001SE E46NE 20050425001742005042500174NM 2005 4 25 2005UALA00128 120050207A5310 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CARGO DOOR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29377UA 24642 FWD CARGO DOOR CUTOUT FRAME CRACKED AT FWD LOWER STOP. MANUFACTURED AND INSTALLED REPAIR ANGLE DOUBLER. 2L72 4F4 FRTA16WE E2GL 20050425001862005042500186EA 2005 4 25 QXEA200500262 120050210A5753 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 500 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - LEFT INBOARD FLAP LOWER SKIN, INBOARD SECTION, HAD FOD IMPACT DAMAGE. REPAIRED IAW CRJ700 SRM 57-52-01-101-001-A01 AND 51-12-00-001-001-A01. 2L72 4F RTA21EA 20050425001892005042500189EA 2005 4 25 QXEA200500267 120050212A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - FUSELAGE EXTERIOR AFT LOWER STATION 979, BL 0, SKIN PANEL HAS A GOUGE ADJACENT TO FASTENER HEAD. REPAIRED IAW CRJ700 SRM 51-42-21-001-001-A01, 51-12-00-001-001-A01, 51-41-21-001-001-A01, HORIZON AIR EA R-53-268, AND REO 670-53-61-147. 2L72 4F RTA21EA 20050425002012005042500201NM 2005 4 25 DHL2005781507 120050215A5320 TORQUE BOX BOEING727 727227 1384078NM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A "C" CHECK, CRACK AT LIGHTENING HOLE LOWER TORQUE BOX L/SIDE AFT OF STA 1223 (MARKED). STOP DRILL CRACK AT LIGHTENING HOLE LOWER TORQUE BOX LT SIDE AFT OF STA 1223, .250 TERMINATED AT END OF CRACK IAW B727 SRM 51-10-1 ACCOMPLISHED 727 HFEC 51-00-00 FIG 1 END OF CRACK FOUND, FABRICATED DOUBLER IAW 53-10-25 FIG IAW MAT 7075T6 .040 PO NR 9001065 DIM 4 1/2 INCH BY 4 INCH IAW B727 SRM 51-40-2 FIG 1 ALODINED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED DOUBLER REPAIR IAW B727 SRM 51-40-2 FIG 1. 2L73 4F A3WE 20050425002042005042500204NM 2005 4 25 DHL2005781509 120050214A5753 SKIN BOEING727 727227 1384078NM RT WING TE FLAP DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A "C" CHECK, RT WING OUTBD MID FLAP INBD END IS DELAMINATED AT TRAILING EDGE, WBL 300. REMOVED RT O/B MID FLAP I/B FAIRING TO F.D.M IAW B727 SRM 51-30-2. CUT OUT DELAM AREA UPPER SKIN AT T/E APPROX 7 INCH BY 3 1/2 INCH IAW B727 SRM 51-40-20 FIG 30. FABRICATED ONE SKIN REPLACEMENT APPROX 7 INCH BY 3 1/2 INCH AND ONE SPLICE APPROX 3 1/2 INCH BY 3 INCH USING 2024-T3 .016 PO NR 9001660 IAW B727 SRM 57-05-2 FIG 3. CLEANED, PREPPED, APPLIED ADHESIVE TO ALL SURFACES AND BAGGED FOR BONDING IAW B727 SRM 51-40-20 FIG 30. CURED REPAIR SANDED CLEANED AND PERFORMED POST BOND INSP WITH DELAM NOTED IAW B727 SRM 51-40-20 PARA 0. TREATED, PRIMED AND SEALED REPAIR IAW B727 SRM 51-40-20 PARA P. RE-INSTALLED RT O/B 2L73 4F A3WE 20050425002072005042500207NM 2005 4 25 DHL2005781512 120050215A5753 SKIN BOEING727 727227 1384078NM LT WING FORFLAP GOUGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A"C" CHECK, LEFT O/B FOREFLAP I/B UPPER L/E GOUGED. REMOVED PREV REPAIR LEFT O/B FOREFLAP I/B UPPER LT IAW B727 SRM 51-30-2. FABRICATE DOUBLER METAL IS 2024-T3 .063 5.0 BY 4.75 PO 9001634 IAW B727 SRM 57-50-2 FIG 4 57-50-4M FIG 1. TREAT PRIME AREA DOUBLER IAW B727 SRM 51-10-2. INSTALL REPAIR DOUBLER IAW B727 SRM 57-50-4 FIG 1. 2L73 4F A3WE 20050425002162005042500216NM 2005 4 25 UPS05444346 120050414A5330 SKIN BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 INSPECTION TYPE:C LT BS 1480 BHD NR 11 HOLE FOUND CRACK AT FUSELAGE SKIN THROUGH THICKNESS RUNNING FWD ( CRACK LENGTH 0.325 INCH ). BS 1480 LT STR 32 TO STR 34 AREA SKIN REPAIRED AS PER SB 747-53A2390 FIG 28 2L74 4F RTA20WE 20050425002282005042500228NM 2005 4 25 UPS05444308 120050416A5312 PRESSURE PANEL BOEING747 747121 1384871NM NLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE:SV NOSE W/W LEFT SIDE PANEL FROM BS 260-280 AT WL 170 CRACK INDICATED FOUND AT THE LOCATION FASTENER NR 7 TO 15. CRACK LENGTH 9 INCHES. WEB REPAIRED AS PER EO B747-5310-20502-C ITEM (6) INSTRUCTION AND SRM 53-10-04 FIGURE 116. 2L74 4F A20WE 20050425002362005042500236WP 2005 4 25 UPS05844297 120050402A5320 ATTACH FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 INSPECTION TYPE:C1 FRAME TO INTERCOSTAL ATTACH FITTING CRACKED 1 FT LONG AT STA 837 FWD L13R. REMOVED, FABRICATED AND INSTALLED FITTING IAW SRM 51-1-20D. 2L74 4F RT4A25 20050425002602005042500260NM 2005 4 25 AWXA200500432 120050310A551069730963 PIN BOEING737 737375 13844BNNM HORIZ STAB CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 MCN - FLIGHT CONTROL - DURING C-05 CHECK CORROSION WAS FOUND ON RT HORIZONTAL STABILIZER INNER HINGE PIN. MAINTENANCE REMOVED AND REPLACED THE RT HORIZONTAL STABILIZER INNER HINGE PIN IAW T/C E6C55102. 2L72 4F RTA16WE 20050425002612005042500261NM 2005 4 25 AWXA200500423 120050318A53206546579513 STIFFENER BOEING737 737375 13844BNNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 MCN - MAJOR REPAIR - DURING C-05 CHECK CORROSION WAS FOUND ON RT TORQUE BOX STIFFENER AT BS 1106, STR 17 RT. MAINTENANCE REMOVED CORRODED RT TORQUE BOX STIFFENER AT BS 1106, STR 17 RT; FABRICATED A NEW REPLACEMENT STIFFENER PER DWG 65-46579; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050425002702005042500270NM 2005 4 25 AWXA200500467 120050328A52105079454 SKIN BOEING737 737301 1384611NM L1 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - DURING C-19 CHECK A .25 INCH CRACK WAS FOUND ON L-1 DOOR INNER WEB SKIN ON AFT SIDE, AT 5TH DOOR STOP FROM TOP BS 344, STR 13 LT. MAINTENANCE CUT OUT DAMAGED L-1 DOOR INNER WEB SKIN AT 5TH DOOR STOP FROM TOP BS 344, STR 13 LT; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 51-70-13. 2L72 4F RTA16WE 20050425002712005042500271NM 2005 4 25 AWXA200500468 120050329A52105079454 SKIN BOEING737 737301 1384611NM L1 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - DURING C-19 CHECK A .25 INCH CRACK WAS FOUND ON L-1 DOOR INNER WEB SKIN ON AFT SIDE, AT 6TH DOOR STOP FROM TOP BS 344, STR 14 LT. MAINTENANCE CUT OUT DAMAGED L-1 DOOR INNER WEB SKIN AT 6TH DOOR STOP FROM TOP BS 344, STR 14 LT; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 51-70-13. 2L72 4F RTA16WE 20050426000152005042600015NM 2005 4 26 DHL2005745004 120050309A5270 SWITCH BOEING727 727224 1384076NM MLG DOOR DIRTY A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01745DH 20665 ON CLIMB-OUT WITH GEAR HANDLE OFF, RED GEAR DOOR LIGHT REMAINED ILLUMINATED. AFTER ABNORMAL PROCEDURE PERFORMED, LIGHT STAYED OUT WITH GEAR HANDLE UP. DUPLICATED DISCREPANCY RT GEAR DOOR NOT RETRACTING, INTERMITTENT. CLEANED DEBRIS FROM DOOR MECHANISM CLEANED SWITCHES PERFORMED PWR OFF RERACK OF LAND GEAR ACCY UNIT, OPS CHECK GOOD PER MM 32-11. 2L73 4F A3WE 20050426000192005042600019NM 2005 4 26 DHL2005743001 120050308A2150 ODOR BOEING727 727225 1384077NM COCKPIT DETECTED A DHLAC ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SO01743DH 22438 ON CLIMBOUT IMMEDIATELY AFTER TAKEOFF THRU 10,000 FEET, ACRID ODOR SMELL IN COCKPIT. (ELECTRICAL SMELL) RAN GASPER PLUS PACKS FOR 1 HOUR. NO UNUSUAL SMELL NOTED 21-51-00. SEE LOG PAGE 032025 ITEM 1P FOR ORIGINAL ITEM. (ACRID ODOR SMELL IN COCKPIT AFTER TAKE OFF). ALSO CHECKED COCKPIT, E/E BAYS FOR EVIDENCE OF BURNT WIRING ETC. NO DEFECTS NOTED. FOUND EVIDENCE OF RESIDUAL GLYCOL IN LT WHEEL WELL AREA. CHECKED OIL LEVELS IN ALL 3 ACM'S INSPECTED WIRING AND GASPER FAN A. 2L73 4F A3WE 20050426000912005042600091CE 2005 4 26 DELA200500007 120050318A21303203353 CONTROL VALVE LEAR 55 55LEAR 5170702CE CABIN PRESSURE INOPERATIVE E DELAA UNSCHED LANDING O OTHER CLCLIMB 1 CE03273MG 119 DURING CLIMBOUT, CABIN PRESSURIZATION SYSTEM DID NOT SCHEDULED ALTITUDE OF DIFFERENTIAL PRESSURE. AN UNSCHEDULED/PRECAUTIONARY LANDING WAS MADE. TROUBLESHOOTING INDICATED FAULTY PRESSURIZATION FLOW CONTROL VALVE. VALVE WAS REPLACED WITH OVERHAULED UNIT. GROUND CHECKS AND SUBSEQUENT FLIGHT CHECK WERE SATISFACTORY. 2L72 4F A10CE 20050426000922005042600092NE 2005 4 26 PCAO501328 220050303A731438690114 PUMP BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE NR 4 ENGINE MALFUNCTIONED A P5CAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 EA15920FT 22237 7002269 CREW REPORTED NR 4 ENGINE WOULD NOT MAKE TAKEOFF POWER. ENGINE COULD ONLY MAKE 1.24 EPR. REPLACED FUEL PUMP. PERFORMED TRIM RUN, ALL NORMAL PER 73-21-01 AND 73-11-01. 2L74 4F4 F A20WE E3NE 20050426001012005042600101 2005 4 26 SWAA051034 420050408A25651061323478 SLIDE BOEING737 7373H4 1384600NM L1 DOOR UNSERVICEABLE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29360SW 26571 DURING SCHEDULED A2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATING LOW. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20050426001022005042600102NM 2005 4 26 SWAA051035 120050410A53116546546 BELTFRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29366SW 26577 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON BELT FRAME AT BS 787, RBL 8. REPAIRED BELT FRAME PER SRM. 2L72 4F RTA16WE 20050426001122005042600112SW 2005 4 26 AC2A099727 120050215A2432RG206 BATTERY BELL 206 206B3 1181506SW MASTER LEAKING B AC2AK NONE K FLUID LOSS ININSP/MAINT 1 SO077131U423 4111 PART LEAKS ACID REMOVED BATTERY FROM SERVICE. SENT TO CONCORDE BATTERY CORP FOR EVALUATION. 1G71 3U H2SW 20050426001162005042600116SW 2005 4 26 AC2A099722 120050126A63203VX500K BELT BELL 427 427 1182207SW XMSN FAN FAILED B AC2AO OTHER O OTHER NRNOT REPORTED 1 SO07427CK152 56043 BELT WAS UNSERVICABLE AFTER 152.3 HOURS OF FLIGHT TIME SINCE NEW. REPLACED BELT WITH NEW PART. 1G71 3U R00001RC 20050427000022005042700002GL 2005 4 27 YTRR099528 220050225A732223070606 FUEL CONTROL BELL 206 206B3 1181506SW ALLSN 250C 250C20 03013GL ENGINE MALFUNCTIONED B YTRAO OTHER O OTHER NRNOT REPORTED 1 SW0321RT 2659 UNABLE TO ADJUST START PROPERTIES OF FUEL CONTROL AFTER 443.8 TSO 1G71 3U3 U H2SW E4CE 20050427000062005042700006WP 2005 4 27 WX0500021 120050212A5310 STRUCTURE DOUG DC9 DC983 3022083WP UNKNOWN VIBRATION A WX0AA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 WP19866GA 49910 ENROUTE LAS TO ICT A/C ENCOUNTERED POCKET OF SEVERE TURBULENCE AND ON RETURN FLT ICT TO LAS CREW REPORTED MODERATE AIRFRAME VIBRATION STRONGEST IN FWD FUSELAGE, SIMILAR TO HAVING FULL SPOILER DEFLECTION AND LANDING LIGHTS EXTENDED IN CRUISE FLT. THROTTLE SETTINGS WERE CHECKED AND AT 80 TO 87 PERCENT N1, VIBRATION WAS MAX. FLT WAS DIVERTED TO DEN AND LANDED W/O INCIDENT. MX INSPECTED A/C AND FOUND NO DEFECTS, PERFORMED HIGH POWER ENGINE RUNS WITH NO VIBRATION NOTED AND OBSERVED NOSE BULLETS FOR OSCILLATIONS WITH NONE NOTED. A/C WAS FERRIED TO LAS AND MX COMPLETED THE TURBULENCE INSPECTION IAW MM 05-51-02 SCHEDULE A WITH NO DAMAGE NOTED. MX PERFORMED AN INSPECTION OF THE NR 2 FLT SPOILER IAW MM 27-60-00 WIT2L72 4F RTA6WE 20050427000072005042700007WP 2005 4 27 WX0500022 120050218A3397 WIRE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT DISCONNECTED A WX0AO OTHER O OTHER TXTAXI/GRND HDL 1 WP19860GA 49786 CREW REPORTED EMERGENCY FLOOR LIGHT COVER PULLED LOOSE, WIRES DISCONNECTED AND EMERGENCY LIGHTS INOPERATIVE. MX CONNECTED THE WIRES AND SECURED THE COVERS. SYSTEM OPERATIONALLY CHECKED GOOD IAW AMM 33-53-00. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050427000082005042700008WP 2005 4 27 WX0500023 120050220A324142807 CONTROL UNIT DOUG DC9 DC983 3022083WP ANTI SKID MALFUNCTIONED A WX0AC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP19864GA 49912 MSN TO LAS - WHEEL NOT TURNING LIGHT ILLUMINATED ON TAKEOFF AT 60 KNOTS, ABORTED TAKEOFF. MAINTENANCE REMOVED AND REPLACED ANTI-SKID CONTROL UNIT SYSTEM OPERATIONALLY CHECKED GOOD IAW AMM 32-43-04. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050427000092005042700009WP 2005 4 27 WX0500020 120050212A3350 BATTERY DOUG DC9 DC983 3022083WP EMERGENCY LIGHT DISCHARGED A WX0AK NONE O OTHER ININSP/MAINT 1 WP19862GA 49556 MAINTENANCE REPORTED OVERHEAD EMERGENCY LIGHTS INOPERATIVE ROW 31 TO ROW 36 AND AFT SERVICE DOOR . MAINTENANCE INSTALLED CHARGED BATTERIES IN POWER PACK AS REQUIRED. ALL LIGHTS OPERATIONALLY CHECK GOOD IAW 33-50-00. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050427000102005042700010WP 2005 4 27 WX0500025 120050224A3350 LIGHT DOUG DC9 DC983 3022083WP CABIN CONTAMINATED A WX0AK NONE O OTHER ININSP/MAINT 1 WP19891GA 49423 LAS - MAINTENANCE REPORTED EMERGENCY FLOOR LIGHT TRACK FROM ROW 1 TO ROW 10 INOPERATIVE. MAINTENANCE CLEANED MOISTURE FROM THE LIGHT STRIPS, SYSTEM OPERATIONALLY CHECKS GOOD IAW AMM 33-53-01. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050427000142005042700014WP 2005 4 27 WX0500024 120050223A3397 CONNECTOR DOUG DC9 DC983 3022083WP EMERGENCY LIGHT LOOSE A WX0AK NONE O OTHER ININSP/MAINT 1 WP19863GA 49911 MAINTENANCE REPORTED FLOOR LIGHT STRIP AT ROW 23 INOPERATIVE. MAINTENANCE DEFERRED SYSTEM IAW MEL 33-24. MAINTENANCE FOUND CONNECTOR LOOSE. MAINTENANCE SECURED THE CONNECTOR. EMERGENCY LIGHT STRIP OPERATIONALLY CHECKED GOOD IAW AMM 33-53-00. DEFERRAL CLEARED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050427000242005042700024 2005 4 27 P9RA20050071 420050312A2565146N61501 GIRT BAR BOEING757 757231 1384950NM L4 DOOR STICKING A P9RAO OTHER O OTHER NRNOT REPORTED 1 SO11708TW 28480 AIRCRAFT AT GATE; CANCUN, L4 DOOR SLIDE GIRT WOULD WOULD NOT ENGAGE. CLEANED AND LUBRICATED GIRT BAR. GIRT BAR ENGAGED PROPERLY. 2L72 4F RTA2NM 20050427000332005042700033EU 2005 4 27 05FDEA00514 120050315A7931 REGULATOR VALVE AIRBUS310 A310 EU PWA JT9 JT9D* NE NR 1 OIL PRESS MALFUNCTIONED A FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25455FE 331 707703 APPROX 80-90 KNOTS GOT ECAM RED LIGHT FOR "HIGH OIL PRESS" NR 1 ENG DID RTO LIGHT WENT OUT. AT IDLE NR 1 ENG = 54 PSI, NR 2 ENG = 44 PSI. REMOVED AND REPLACED NR 1 OIL PRESS REGULATOR VALVE PER AMM 79-21-04-4. PERFORMED ENG RUN PER JRH. ALL PARAMETERS NORMAL. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION OFF MFG 793739 POS 1 SRL A28440 TAG A28440 ON MFG 793739 SRL MG9205 TAG 939367. 2L72 4F4 FRTA35EU E20EA 20050427000342005042700034 2005 4 27 05FDEA00519 420050315A3417 ADC BOEING727 727233 138408ANM COCKPIT MALFUNCTIONED A FDEAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 SO25275FE 22040 REJECTED TO AT 80 KTS. RAN RTO CHECKLIST. NO AIRSPEED ON CAPT'S AIRSPEED INDICATOR. REMOVED AND REPLACED AIR DATA COMPUTER IAW MM 34-12-011-4. A/C DOWN GRADED TO NOT CAT II. A/P NR 1 CK CAT II A/P NR 2 CK CAT II. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION OFF MFG HG480B13. 2L73 4F RTA3WE 20050427000352005042700035 2005 4 27 05FDEA00520 420050315A3417HG480B13 ADC BOEING727 727233 138408ANM COCKPIT MALFUNCTIONED A FDEAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 SO25275FE7238 7238 22040 REJECTED TAKEOFF. REMOVED AND REPLACED AIR DATA COMPUTER IAW MM 34-12-011-4. GRD CK OK. A/C DOWN GRADED TO NOT CAT II. A/P NR 1 CK CAT II A/P NR 2 CK CAT II PREMATURE REMOVAL/INSTALLATION OFF MFG HG480B13. 2L73 4F RTA3WE 20050427000412005042700041EU 2005 4 27 DHL2005362005 120050317A3240355511011 CONTROL UNIT AIRBUS300 A300B4203 3930306EU AUTOBRAKE SYS MALFUNCTIONED A DHLAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01362DH 84 PRIOR TO TAKEOFF, ATTEMPTED TO ARM AUTOBRAKE SYSTEM. WHEN THE MAX BUTTON WAS PUSHED, THE BRAKES LOCKED UP. ANTI-SKID SYSTEM OPERATED NORMALLY. DEFERRED PER MEL NR 32-42-07 DMI CONTROL NR 20126 TS PLAC INSTALLED, MXC NOTIFIED. DSMER 8973. DMI NR 20126 AUTO BRAKES WOULD NOT ARM. REMOVED AND REPLACED AUTO BRAKE CONTROL UNIT AND PERFORMED OPS TEST IAW 32-42-54. CKS NORMAL. DMI 20126 CLEARED. PLACARD REMOVED. 2L72 4F RTA35EU 20050427000462005042700046NM 2005 4 27 DHL2005781551 120050216A5531 FRAME BOEING727 727227 1384078NM VERTICAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A C-CHECK, VERT STAB AT FIN STA 157 STR 9 LT IS CRACKED AT FRAME ATTACH BOLT. REMOVED FASTENERS FOR ACCESS, CUT OUT DAMAGED 6 X 3 INCHES STIFFENER & REMOVED FILLER IAW B727 SRM 55-30-4 FIG 1, FABRICATED STIFFENER REPAIR PN BAC1517-1367, PO NR 501953 DIM 6 X 3 INCHES SPLICE P/N AND10134-1201 PO 501952 DIM 20 X 2.250 INCHES FILLER P/N 7075T6 .100 PO 9001777 DIM. 20 X .50" SPLICE P/N AND 10133-1401 PO 501952 DIM 20 X 2 INCHES, FILLER PN 7075-T6 .090 PO 501952 DIM 20 X .5 INCHES DIA P/N AND10133-1401 PO NR 501952 DIM 2 X 2 INCHES IAW B727 SRM 55-30-4 FIG 1. TREATED AND PRIMED STIFFENER REPAIR IAW B727 SRM 51-10-2. INSTALLED STIFFENER REPAIR AT VERT STAB FIN STA 157 STR 9 LT IAW B727 SRM 55-30-4 FIG 1. 2L73 4F A3WE 20050427000472005042700047NM 2005 4 27 DHL2005781553 120050216A5531 FRAME BOEING727 727227 1384078NM VERTICAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A C-CHECK, VERT STAB FIN STA 133 STR 7 LT IS CRACKED AT FRAME ATTACH BOLT. REMOVED FASTENERS FOR ACCESS, CUT-OUT DAMAGED STIFFENER IAW B727 SRM 55-30-4 FIG 1 (4 X 5 INCHES). FABRICATED REPAIR STIFFENER. INSTALLED REPAIR STIFFENER IAW B727 SRM 55-30-4 FIG 1. 2L73 4F A3WE 20050427000502005042700050NM 2005 4 27 DHL2005781556 120050217A5311 FRAME BOEING727 727227 1384078NM CARGO BAY CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A C-CHECK, AFT PIT FRAME DENTED BS 1130 STR 26 RT. CUT OUT DAMAGED AREA FROM FRAME BS 1130 STR 26 RT IAW 727 SRM 53-10-1 FIG 1. FABRICATED DOUBLER FROM 7075-T6 .063 PO NR 9001660 8.5 X 3 INCHES & STRIP FROM 7075T6 .063 PO NR 9001660 8.5 X 1 INCHES AND FILLER FROM 7075T6 .063 PO NR 9001660 1.25 X 1 INCHES IAW 727 SRM 53-10-3 FIG 1 AND 51-40-3 FIG 1. TREATED AND PRIMED PARTS AND BARE METAL IAW 727 SRM 51-10-2. INSTALLED DOUBLER IAW 727 SRM 53-10-1. 2L73 4F A3WE 20050427000512005042700051NM 2005 4 27 DHL2005781557 120050224A5531 FRAME BOEING727 727227 1384078NM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING C-CHECK, VERT STAB FIN STA 55.8 STR 3 LT IS CRACKED AT FRAME ATTACH BOLT. REMOVED FRAME CLIP BS 55.8 STR 3 LT IAW B727 SRM 51-30-2. FABRICATED CLIP MATERIAL USED 7075-T6 .050 PO NR 9001777 DIM .750 INCH 2.5 INCH X 5 INCHES IAW B727 SRM 55-30-2 FIG 2 AND 51-20-1 FIG 7. TREATED AND PRIMED CLIP IAW B727 SRM 51-10-2. INSTALLED FRAME CLIP BS 55.8 STR 3 LT IAW B727 SRM 51-30-2. 2L73 4F A3WE 20050427000532005042700053NM 2005 4 27 DHL2005781559 120050224A5531 FRAME BOEING727 727227 1384078NM VERTICAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING C-CHECK, VERT STAB FIN STA 133 AT STR 9LT HAS 1 FRAME CLIP CRACKED. REMOVED FRAME CLIP AT VERT STAB FIN STA 133 AT STR 9 LT IAW B727 SRM 51-30-2. FABRICATED NEW CLIP MATERIAL USED 7075T6 .050 PO NR 9001777 DIM 7/8" BY 2.50 BY 5.50 IAW B727 SRM 55-30-2 FIG 2 AND 51-20-1 FIG 7. TREATED AND PRIMED CLIP IAW B727 SRM 51-10-2. INSTALLED FRAME CLIP IAW B727 SRM 51-30-2. 2L73 4F A3WE 20050427000552005042700055NM 2005 4 27 DHL2005781561 120050227A5755 SKIN BOEING727 727227 1384078NM SPOILER DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A C-CHECK, NR 9 SPOILER HAS TWO SPOTS OF DELAMINATION ON UPPER SURFACE AT TRAILING EDGE AND PHENOLIC RUB STRIP AT BOTTOM TRAILING EDGE IS LOOSE. REMOVED NR 9 SPOILER FOR REPAIR IAW B727 MM. REMOVED PREVIOUS REPAIR AND CUT OUT DAMAGE AREA APROX 30.5 BY 6 INCHES BAGGED FOR MOISTURE REMOVAL IAW B727 SRM. CLEANED PREPPED & INSTALLED RESIN IMPREGNATED FIBERGLASS OVERLAY REPAIR & BAGGED FOR BONDING IAW B727 SRM. CURED REPAIR, SANDED, CLEANED AND INSTALLED FIBERGLASS SEALANT COMPOUND IAW B727 SRM. CURED SEALANT COMPOUND, SANDED SMOOTH, CLEANED, PRIMED & INSTALLED T/E TACK RIVETS IAW B727 SRM. REBONDED T/E RUB STRIP IAW B727 SRM. INSTALLED NR 9 SPOILER PANEL IAW 727 MM. OP CHECK PERFORMED GOOD IAW 727 MM. 2L73 4F A3WE 20050427000602005042700060WP 2005 4 27 DHL2005801004 120050318A5270H2024B SWITCH DOUG DC8 DC873F 302199FWP RT MLG DOOR MALFUNCTIONED A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01801DH 46033 DURING GEAR RETRACTION, RT DOOR UNSAFE LIGHT REMAINED ILLUMINATED. PERFORMED ABNORMAL PROCEDURE. LIGHT REMAINED EXTINGUISHED. STAYED OUT. REMOVED AND REPLACED RT GEAR DOOR SWITCH. ALSO, REPAIRED BROKEN WIRE AT SAME C/P SYSTEM CKD NORMAL IAW 32-60-0 P/N H20-24B. 2L74 4F RT4A25 20050427000622005042700062GL 2005 4 27 YTRR099851 220050311A73232524676914 GOVERNOR BELL 206 206B3 1181506SW ALLSN 250C 250C20B 03013GL ENGINE MALFUNCTIONED B YTRAO OTHER R PARTIAL RPM/PWR LOSS NRNOT REPORTED 1 SW09209RA 2091 ENGINE WOULD DROOP WHEN POWER WAS APPLIED AND NOT RECOVER 1G71 3U3 U H2SW E4CE 20050427000702005042700070WP 2005 4 27 05FDEA00604 120050318A7714 SENSOR DOUG MD10 MD1010F 3022112WP NR 1 FAN SPEED MALFUNCTIONED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO2568050 47804 CLIMB-OUT PASSING 3000 FT ENG 1 EXCEEDANCE N1 168.6. PULL THROTTLE NR 1 BACK. ALSO ATS OFF. ALL OTHER INST NORM, NO VIB. REENGAGED ATS AS SOON AS NR 1 WAS CLIMB POWER IMMEDIATELY JUMPED TO RED EXCEED OF 168.6 AND DISCONNECTED ATS. NR 1 THROTTLE BACK TO IDLE AND LAND AT OAK. INSPECTION FAN INLET COWL, FAIRINGS, FAN CASE, ACOUSTICAL PANELS, FAN BLADES, SPINNER AND ADJACENT AREAS. NO DEFECTS NOTED. REMOVED AND REPLACED FAN SPEED SENSOR REF MD-10 MM 77-11-01- 2. VIA 1,2 AND 3, SHOWED N1 SPIKES WAY OUT OF RANGE AND N2 AND EGT INDICATIONS WERE IN LIMITS PER JRHCH4. RAN NR 1 ENGINE PER JRH CH5,4 AND 6. ALL INDICATIONS FROM IDLE TO MAX POWER IN NORMAL RANGE, NO SPIKES. A/C OK FOR SERVICE. 2L73 4F RTA22WE 20050427000922005042700092NM 2005 4 27 AWXA200500352 120050311A5320654585567 WEB BOEING737 737375 13844BNNM FUSLEAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 MCN - MAJOR REPAIR - DURING C-05 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF R-2 DOOR SILL (WEB) BETWEEN BS 953 AND BS 985, RBL 48, WL 208. MAINTENANCE REMOVED CORRODED R-2 DOOR SILL FROM BS 947 TO BS 986.5, RBL 48; FABRICATED A NEW REPLACEMENT WEB PER DWG 65-45855; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050427000942005042700094NM 2005 4 27 72300026 120050117A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 CORROSION ON STRINGER 27R. 2L73 4F4 FRTA3WE E2EA 20050427001082005042700108NM 2005 4 27 72300016 120050125A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 DAMAGED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 LOWER FLANGE OF SHEAR TIE HAS DAMAGED FASTENER HOLES. 2L73 4F4 FRTA3WE E2EA 20050427001092005042700109NM 2005 4 27 72300017 120050114A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 DAMAGED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 LOWER FLANGE OF SHEAR TIE HAS DAMAGED FASTENER HOLES. 2L73 4F4 FRTA3WE E2EA 20050427001112005042700111NM 2005 4 27 72300020 120050201A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 1 INCH BY 3 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050427001132005042700113NM 2005 4 27 72300022 120050201A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 .75 INCH BY 1.5 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050427001152005042700115NM 2005 4 27 72300024 120050114A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 GOUGED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 APPROX (3) .1875 INCH GOUGES IN SHEAR TIE FLANGE. 2L73 4F4 FRTA3WE E2EA 20050427001222005042700122EU 2005 4 27 05FDEA00526 120050315A5200 SKIN AIRBUS310 A310 EU ACCESS DOOR DAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25451FE 303 REPAIR AT STN 2135 FS 38.1 STN 2188 FS 38.2 STR 49 LT, AIR CONDITION ACCESS DOOR. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-72-10 AND 51-40-21. 2L72 4F RTA35EU 20050427001232005042700123NM 2005 4 27 05FDEA00629 120050322A5347 SEAT TRACK BOEING727 727233 138408ANM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25271FE 22036 SEAT TRACK, STA. 344 - 480, LBL 24 HAS CORROSION AND EXISTING BLEND REPAIRS AND REQUIRES REPLACEMENT PER 7-5340-7-5002. REMOVED DAMAGED SEAT TRACK IAW SRM 51-30-2 - MAT ID BAC 1520-792 IAW SRM 51-10-2 FIG 7. NEW EXTRUSION SCALLOPED ON TRAV NR T5/501341. INSTALLED NEW SEAT TRACK IAW SRM 51-30-2. 2L73 4F RTA3WE 20050427001502005042700150EU 2005 4 27 KBM2005F00042 120050312A7931704A37642043 TRANSMITTER SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1D NE ENG OIL PRESS INOPERATIVE E KBMAK NONE O OTHER ININSP/MAINT 1 WP1953SH 327 2009 OIL TRANSMITTER, ENGINE OIL PRESSURE INOPERATIVE. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050427001522005042700152WP 2005 4 27 DHL2005802004 120050329A3260 UPLOCK DOUG DC8 DC873 302199CWP MLG OUT OF ADJUST A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01802DH 46076 DOOR NOT LATCHES LIGHT ILLUMINATED AFTER TAKEOFF. PERFORMED ABNORMAL PROCEDURE. LEFT AND RIGHT DOOR UNSAFE LIGHT ILLUMINATED. PERFORMED ADJUSTED/TET AT MAIN GEAR DOOR UPLATCH MECHANISM IAW 32-21-4, OPS CKD NORMAL. 2L74 4F RT4A25 20050427001602005042700160EA 2005 4 27 QXEA200500434 120050303A5751 SKIN CNDAIRCL600 CL600* EA ZONE 500 WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - LEFT AILERON, UPPER INBOARD LEADING EDGE HAS TWO AREAS OF WEARING FROM TRAILING EDGE SEALS. REPAIRED IAW CRJ700 SRM 57-61-01-101-001-A01 AND SRM 51-12-00-001-001-A01. 2L72 4F RTA21EA 20050427001622005042700162WP 2005 4 27 DHL2005805532 120050314A5751 SKIN DOUG DC8 DC873F 302199FWP RT WING AILERON WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 RT WING INBD AILERON UPPER SKIN WORN 2.000M XA 474.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PAGE 1, SRM 57-8-1 FIG 1. REMOVED DAMAGED PLATING IAW SRM 51-1-21 PAGE 1, SRM 51-3-0 PAGE 1. FABRICATED NEW PLATING (AL 2024-T3 0.040) IAW SRM 57-8-1 FIG 1 ITEM E. CLEANED, TREATED AND PRIMED AREA AND NEW PLATING INTERNAL PART IAW SRM 51-1-8B. INSTALLED NEW PLATING IAW SRM 51-1-21 PAGE 1, SRM 51-3-0 PAGE 1. TORQUED IAW SRM 51-3-1. PERFORMED BALANCE TO RT INBD AILERON IAW SRM 51-4-1 PAGES 1-4. INSTALLED WEIGHT (PN 5706734-41), STA 555.000. FOUND WITHIN TOLERANCE. MOMENT 3326.64 20 LBS. 2L74 4F RT4A25 20050427001642005042700164WP 2005 4 27 DHL2005805561 120050320A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME WORN STA 460.000, L-10R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-04-05, EO NR AST 050217 DATE 03-03-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLE WITH RIVETS (MS20470AD) IAW EO NR AST 050217, SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050427001662005042700166WP 2005 4 27 DHL2005805598 120050320A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME MISDRILLED HOLE OF 0.15625 AT STA 880.000 L-12L TO L-13L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 02-25-05 EO NR AST 050202 DATED 02-17-05. PERFORMED DETAIL VISUAL INSP. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLE WITH RIVET (MS20470AD) IAW EO NR AST 050202 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050427001682005042700168WP 2005 4 27 DHL2005805530 120050318A5310 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBD FLANGE HOLES (2EA) MISDRILLED AT STA 1420.000 L-12 AND L-13L. PERFORMED MAJOR REPAIR IAWW FAA FORM 8110-3 DATE 03-05-05, EO NR AST050205 DATE 02-21-05. CLEANED, TREATED AND PRIMED (AREA) MISDRILLED HOLES IAW SRM 51-1-8B. PERFORMED VISUAL INSPECTION (DETAILED). NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD6-4) IAW EO NR AST050205 IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050427001702005042700170WP 2005 4 27 DHL2005805540 120050320A5311 FRAME DOUG DC8 DC873F 302199FWP FUSLEAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME MISDRILLED HOLES VERTICAL FLANGE (STA 100.000-1560.000, BETWEEN L-19L AND L-19R) (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-16-05, EO NR AST 050223 DATED 02-24-05. PERFORMED DETAIL VISUAL INSP. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO NR AST050223, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050427001722005042700172WP 2005 4 27 DHL2005805538 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBD FLANGE (1EA) MISDRILLED HOLE, STA 240.000 L-12.5R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-07-05 EO NR AST-050201 DATED 02-17-05. PERFORMED DETAIL VISUAL INSP. NO CRACK FOUND. PERFORMED CLEANING, TREATING AND PRIMING OF MISDRILLED HOLE AREA AT STA 240.000 L-12.5R IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLE WITH RIVET (MS20470AD) IAW EO NR AST-050201, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050427001742005042700174WP 2005 4 27 DHL2005805542 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT INBD FLANGE "Z" FRAME HOLES (2EA) MISDRILLED AT STA 220.000 L-10R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-07-05, EO NR AST 050201 DATE 02-17-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED AREA (MISDRILLED HOLES) IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO NR AST 050201, SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050427001762005042700176WP 2005 4 27 DHL2005805569 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT INBD FLANGE "Z" FRAME HOLES (2EA) MISDRILLED AT STA 300.000 L-10R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-07-05 EO NR AST 050201 DATE 02-17-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED AREA (MISDRILLED HOLES) IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO NR AST050201, SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050427001782005042700178WP 2005 4 27 DHL2005805604 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME (2EA) MISDRILLED HOLES AT STA 540.000 L-10L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-05-05 EO NR AST 050205 DATED 02-21-05. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. PERFORMED DETAIL VISUAL INSP. NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD5-6) IAW EO NR AST 050205 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050427001802005042700180WP 2005 4 27 DHL2005805646 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBD FLANGE (1EA) HOLE MISDRILLED STA 520.000 L-12R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-07-05 EO NR AST 050201 DATE 02-17-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLE WITH RIVET (MS20470AD) IAW EO NR AST 050201 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050427001822005042700182WP 2005 4 27 DHL2005805669 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME HOLES (2EA) MISDRILLED STA 960.000 L-10R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 02-25-05 EO NR AST 050203 DATE 02-18-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVET (MS20470AD6-5) IAW EO NR AST 050203 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050427001832005042700183WP 2005 4 27 DHL2005805683 120050324A52109751065 FITTING DOUG DC8 DC873F 302199FWP PAX DOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT AFT PASSENGER DOOR FITTING CRACKED 1.000 STA 620.000 L-13L (INNER SKIN) (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-22-05 EO NR AST 050225 DATE 03-22-05. REMOVED CRACKED FITTING IAW SRM 51-1-20D PAGE 21, SRM 51-1-21 PAGE 1, SRM 51-3-0 PAGE 1. FABRICATED NEW FITTING (AL7075-T651) IAW EO NR AST050225. PERFORMED HEAT TREATMENT IAW SRM 51-1-1 PAGE 1-13-17. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02 TO 07. CLEANED, TREATED AND PRIMED AREA AND FITTING (NEW) IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PAGE 9. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050427001852005042700185WP 2005 4 27 DHL2005805649 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBD FLANGE (1EA) MISDRILLED HOLE, STA 460.000 L-12.5R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-07-05 EO NR AST 050201 DATE 02-17-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLE WITH RIVET (MS20470AD) IAW EO NR AST 050201 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050427001872005042700187WP 2005 4 27 DHL2005805681 120050320A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CABIN INTERIOR "Z" FRAME INBD FLANGE HOLE MISDRILLED STA 1000.000 L-6R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 02-25-05 EO NR AST 050204 DATE 02-18-05. PERFORMED NDT INSPECTION TO AREA IAW NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER ANGLE (AL7075"0" 0.080) IAW EO NR AST 050204, SRM 51-1-4 PAGE 1. PERFORMED HEAT TREATMENT IAW SRM 51-1-1 PAGES 1-13-17. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA, REPAIR DOUBLER ANGLE IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLE WITH RIVET (NAS1097AD). INSTALLED REPAIR DOUBLER ANGLE IAW EO NR AST 050204 SRM 51-1-21 PAGE 1. TRANSFERRED ITEM FROM NR 028433 2L74 4F RT4A25 20050427001892005042700189WP 2005 4 27 DHL2005805677 120050321A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 RT WING OUTBD L/E UPPER SKIN HOLES ELONGATED STA XFS 560.000.(MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-16-05 DWG X83-R01 REV IR DATED 02-21-05. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. CUT OUT DAMAGED SECTION IAW DWG X83-R01. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER (AL7075T6 0.063) FILLER (AL7075T6 0.050) IAW DWG X83-R01. CLEANED, TREATED AND PRIMED AREA AND INNER SIDE OF REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW DWG X83-R01, SRM 51-1-21 PG 1 SRM 51-3-0 PG1 SRM 51-1-20D PG 9. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050425002032005042500203NM 2005 4 25 DHL2005781508 120050215A5320 TORQUE BOX BOEING727 727227 1384078NM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A "C" CHECK, CRACK AT LIGHNING HOLE TORQUE BOX L/SIDE AFT OF STA 1323. REMOVED FASTENERS AT LIGHTENING HOLE LOWER TORQUE BOX L/SIDE AFT OF STA 1323 IAW B727 SRM 51-30-2. STOP DRILL CRACK .250 TERMINATED AT END OF CRACK IAW B727 SRM 51-10-1. FABRICATED DOUBLER REPAIR MAT IAW 53-10-2 FIG 6 FROM MAT 7075T6.040 PO NR 9001688 DIM 2 1/2 INCH BY 3 INCH IAW B727 SRM 51-40-2 FIG 1. ACCOMPLISHED 727 HFEC INSPECTION 51-00-00 FIG 4 END OF CRACK FOUND ALODINED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED DOUBLER REPAIR IAW B727 SRM 51-40-2 FIG 1. 2L73 4F A3WE 20050425002142005042500214WP 2005 4 25 UPS05844280 120050401A5313S2645716 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 C1 LONGERON CRACKED .25 INCH LONG AT STA 1746 L14R. REPAIRED BY CUTTING OUT DAMAGE AND INSTALLING FILLER AND DOUBLER IAW SRM 53-02-02 FIG 11 AND 51-1-20D AND 51-3-0. 2L74 4F RT4A25 20050425002152005042500215NM 2005 4 25 UPS05444345 120050424A3350S135610A BATTERY BOEING747 747SR46 1384816NM CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01680UP 20923 INSPECTION TYPE:6A EMERGENCY LIGHT AT STA 2280 L/H HAS A BAD BATTERY. LIGHT FLASHES ON A AND THEN OFF WHEN TURNED ON. REPLACED BATTERY PACK. EMERGENCY LIGHT OPERATION CHECKS OKAY I.A.W. B 747 MM 33-51-00 ADJ/TEST. 2L74 4F RTA20WE 20050425002212005042500221NM 2005 4 25 UPS05444302 120050416A5312 PRESSURE PANEL BOEING747 747121 1384871NM NLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE:SV NOSE WHEEL WELL TOP PANEL FROM BS 300 TO 320 AT LBL 20 CRACK INDICATION FOUND AT FASTENER NR 8, 9, 14, 15 & 16. CRACK LENGTH 5 INCHES. CRACKED TOP PANEL REPAIRED AS PER HX RS R53-10-35292 & UPS EO B747-5310-22075-A. 2L74 4F A20WE 20050425002232005042500223NM 2005 4 25 UPS05444304 120050416A5312 PRESSURE PANEL BOEING747 747121 1384871NM NLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE:SV NOSE WHEEL WELL RT SIDE PANEL FROM BS 260 - 280 WL 170 CRACK INDICATION FOUND AT FASTENER NR 8 AT WEB AREA. CRACK LENGTH 1 INCH. CRACKED WEB REPAIRED AS PER EO B747-5310-20502-C ITEM 6 INSTRUCTION AND SRM 53-10-04 FIGURE 116. 2L74 4F A20WE 20050425002252005042500225NM 2005 4 25 UPS05444306 120050416A5312 PRESSURE PANEL BOEING747 747121 1384871NM NLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE:SV NOSE WHEEL WELL LT SIDE PANEL FROM BS 260-280 WL 150 CRACK INDICATION FOUND BETWEEN NR 8, 13 AT WEB AREA. CRACK LENGTH 6 INCHES. CRACKED WEB REPAIRED AS PER EO B747-5310-20502 APPENDIX C ITEM (6) INSTRUCTION AND SRM 53-10-04 FIGURE 116. 2L74 4F A20WE 20050425002292005042500229NM 2005 4 25 UPS05544295 120050416A2560 SMOKE GOGGLES BOEING757 75724APF 1384969NM COCKPIT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01417UP 23904 INSPECTION TYPE:N/A 2ND OBS SEAT SMOKE GOGGLE CRACKED. REMOVED AND REPLACED 2ND OBS SMOKE GOGGLES. 2L72 4F RTA2NM 20050425002312005042500231NM 2005 4 25 UPS05544313 120050417A2560 SMOKE GOGGLES BOEING757 75724APF 1384969NM COCKPIT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01432UP 25463 INSPECTION TYPE:N/A F/O SMOKE GOGGLES CRACKED. REMOVED AND REPLACED F/O SMOKE GOGGLES AS REQUIRED. 2L72 4F RTA2NM 20050425002372005042500237WP 2005 4 25 AALA20050260 120050412A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21505AA 49799 LAX - FORWARD DOOR OVERWING EXIT SIGNS INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD DOOR OVERWING EXIT SIGNS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050425002422005042500242NM 2005 4 25 AALA20050250 120050408A3350BPS73 BATTERY PACK BOEING757 757223 1384957NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21629AA 24587 MIA - EMERGENCY EXIT LIGHT AT DOOR RIGHT ONE INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHT AT DOOR RIGHT ONE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050425002432005042500243WP 2005 4 25 AALA20050262 120050414A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW217517A 49894 DFW - PORTABLE EMERGENCY LIGHT AT LEFT ONE DOOR AND EXTERIOR OVERWING EMERGENCY LIGHTS ON LEFT AND RIGHT SIDE INOPERATIVE. REPLACED PORTABLE EMERGENCY LIGHT AT LEFT ONE DOOR AND REPLACED BATTERY PACK FOR EXTERIOR OVERWING EMERGENCY LIGHTS ON LEFT AND RIGHT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050425002532005042500253WP 2005 4 25 AALA20050269 120050415A335060030451 BATTERY DOUG DC9 DC982 3022082WP CABIN NOT SEATED A AALAK NONE L NO TEST ININSP/MAINT 1 SW217547A 53029 SFO - OVERHEAD EMERGENCY LIGHTS AT ROWS 8 TO 11 INOPERATIVE. RESEATED BATTERIES IN PACKS FOR OVERHEAD EMERGENCY LIGHTS FOR ROWS 8 TO 11. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050425002622005042500262NM 2005 4 25 AWXA200500424 120050312A532069432331 ATTACH ANGLE BOEING737 737375 13844BNNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 MCN - MAJOR REPAIR - DURING C-05 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE AFT CARGO DOOR CUTOUT SILL WEB TO FRAME ATTACH ANGLE AT BS 794, BETWEEN STR 26 RT & STR 27 RT. MAINTENANCE REMOVED CORRODED SILL WEB TO FRAME ATTACH ANGLE AT BS 794, BETWEEN STR 26 RT & STR 27 RT; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 65-47957; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050425002632005042500263NM 2005 4 25 AWXA200500425 120050318A53206546572502 STIFFENER BOEING737 737375 13844BNNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 MCN - MAJOR REPAIR - DURING C-05 CHECK CORROSION WAS FOUND ON HORIZONTAL STIFFENER ANGLE AT FORWARD FACE OF BULKHEAD AT BS 1088, BETWEEN RBL 23 AND RBL 33. MAINTENANCE REMOVED CORRODED HORIZONTAL STIFFENER ANGLE AT FORWARD FACE OF BULKHEAD AT BS 1088, FROM RBL 23 TO RBL 33; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 65-46572; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050426000142005042600014NM 2005 4 26 DHL2005781522 120050213A5754 RIB BOEING727 727227 1384078NM RT WING SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A "C" CHECK, RT WING LEADING EDGE RIB AT SLAT, STA 260 IS CRACKED. REMOVED AT RT WING LEADING EDGE RIB AT STA 260 FOR FAB IAW B727 SRM 51-30-2, FABRICATED NEW RIB, MAT'L USED 2024-T3 .050 PO NR 9001873,DIM.15 INCH BY 1 1/2 INCH IAW B727 SRM 57-20-2 FIG 1 AND 51-10-2, ALODINE AND PRIMED IAW B727 SRM 51-10-2. INSTALLED NEW RIB IAW B727 SRM 51-30-2. 2L73 4F A3WE 20050426000222005042600022EU 2005 4 26 249132 120050308A2913 PUMP SAAB SF340 SF340A 7850100EU HYD SYSTEM MALFUNCTIONED A UHLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL17158SD 158SD ON TAKEOFF AIRCREW REPORTED THAT THEY WERE RECEIVING THE GEAR INTRANSIT LIGHT AND THAT THE HYD PUMP WAS CONTINUING TO OPERATE. ASKED AIRCREW TO CYCLE THE GEAR TO GET IT UP AND LOCK-- NO FIX. AIRCRAFT RETURNED TO IAD WITH NO FURTHER ISSUES. 2L72 4T RTA52EU 20050426000242005042600024NM 2005 4 26 0500295521 120050214A5347 SEAT TRACK BOEING757 757251 1384970NM FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01521US 23209 DURING "M" CHECK, FOUND CORROSION ON SEAT TRACK AT BS 1640 LBL 24. REPAIRED PER EA 55-202017. 2L72 4F RTA2NM 20050426000872005042600087NE 2005 4 26 P5CAO501327 220050303A73217800001 FUEL CONTROL BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE NR 4 ENGINE MALFUNCTIONED A P5CAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 EA15920FT 22237 702269 CREW REPORTED NR 4 ENGINE WOULD NOT MAKE TAKEOFF POWER. ENGINE COULD ONLY MAKE 1.24 EPR. REPLACED FUEL CONTROL. PERFORMED TRIM RUN, ALL NORMAL PER 73-21-01 AND 73-11-01. 2L74 4F4 F A20WE E3NE 20050426001032005042600103NM 2005 4 26 SWAA051036 120050410A53226546529 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29366SW 26577 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON SHEAR TIE AT BS 500, BL 0. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050427000032005042700003SW 2005 4 27 YTRR099530 120050307A2821222366621103 FUEL FILTER BELL 407 407 1182206SW ALLSN 250C 250C47B GL ENGINE FAILED B YTRAO OTHER O OTHER NRNOT REPORTED 1 SW03595RL660 53595 FUEL FILTER HEAD ASS'Y WAS INSTALLED ON THIS AIRCRAFT NEW FROM BHT. IT FAILED AFTER 659.6 HRS TIME IN SERVICE. 1G71 3U3 UO H2SW E1GL 20050427000112005042700011 2005 4 27 WX0500027 420050303A3417HG280D80 ADC DOUG DC9 DC983 3022083WP COCKPIT MALFUNCTIONED A WX0AC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP19862GA 49556 LAS - DURING TAKEOFF ROLL AT 50 KNOTS, RIGHT INSTRUMENT PANEL ALL INSTRUMENTS DISPLAYED FLAGS. CAPTAIN’S INSTRUMENT PANEL NORMAL. TAKEOFF ABORTED. ONCE CLEAR OF RUNWAY RIGHT INSTRUMENTS DISPLAYED NORMAL. MAINTENANCE REMOVED AND REPLACED NR 2 AIR DATA COMPUTER IAW MM 34-16-01. OPERATIONAL CHECK GOOD. PERFORMED RTS IAW MM 22-01-03, NO FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE 2L72 4F RTA6WE 20050427000122005042700012WP 2005 4 27 WX0500028 120050308A3350 LAMP DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A WX0AK NONE O OTHER ININSP/MAINT 1 WP19866GA 49910 LAS - MAINTENANCE REPORTED LEFT SIDE EXTERIOR EMERGENCY OVERWING LIGHT INOPERATIVE. MAINTENANCE RELAMPED EMERGENCY LIGHT. SYSTEM OPERATIONALLY CHECKS GOOD IAW MM 33-53-00. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050427000372005042700037NM 2005 4 27 ANCF200400041 120050315A2613 OVERHEAT SENSOR DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE TAIL DIRTY W ANCFA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO23583AN 53093 AFTER TAKEOFF, TAIL COMP TEMP LIGHT CAME ON. ABNORMAL CHECK LIST WAS PERFORMED AFTER LT ENGINE WAS REDUCED, 1.5 MIN LATER THE LIGHT WENT OFF, LT PACK WAS SWITCHED TO OFF AND LT ENG POWER RESTRICTED. IAW AMM 36-20-02 PAGE 201, TAIL COMPARTMENT OVERHEAT SENSOR, LT SIDE WAS CLEANED AND ADJUSTED. 2L72 4F4 FRT E9NE 20050427000562005042700056NM 2005 4 27 DHL2005781563 120050303A5754 RIB BOEING727 727227 1384078NM NR 6 SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A C-CHECK, RT WING NR 6 SLAT I/B RIB AT ACTUATOR ROD ATTACH POINT IS CRACKED. REMOVED DAMAGED RIB IAW B727 SRM 51-30-2, FABRICATED NEW RIB, MATERIAL USED 2024 T3, .040 PO 9002012 DIM 15 BY 5.50 INCHES IAW B727 SRM 57-50-2 FIG 2 AND 51-20-1 FIG 7. ALODINE AND PRIMED RIB AND AREA IAW B727 SRM 51-10-2. INSTALLED NEW RIB AT RIGHT WING NR 6 SLAT IAW B727 SRM 51-30-2. OPS CHECK/LEAK CHECK GOOD IAW B727 MM 27-81-00. LATE ENTRY, REMOVAL AND REINSTALLATION OF NR 6 SLAT ACTUATOR IS DOCUMENTED ON THE BACK OF NON-ROUTINE 95554. REINSTALLED NR 6 SLAT IAW B727 MM 27-81-11. ALL CHECK GOOD. 2L73 4F A3WE 20050427000682005042700068EU 2005 4 27 05FDEA00523 120050315A5330 SKIN AIRBUS310 A310 EU FUSELAGE DAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25451FE 303 MOD TYPE Y MOD NR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR). COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. FUSELAGE - REPAIR AT FR 15/16 BELOW R1 DOOR (PLEASE EVALUATE). REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 53-12-12, FIG 201, SHEET 1 AND 51-40-21. 2L72 4F RTA35EU 20050427000772005042700077WP 2005 4 27 DHL2005809001 120050322A3350 CONNECTOR DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT DISCONNECTED A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01809DH 46047 EMERGENCY LIGHTS WOULD NOT TEST DURING PREFLIGHT. RESECURED CONNECTOR TO EMERGENCY LIGHT RELAY PAC, OPS NORMAL PER MM 33-50-1. 2L74 4F RT4A25 20050427001562005042700156EA 2005 4 27 QXEA200500433 120050227A5320 PLATE CNDAIRCL600 CL6002C10 1390015EA ZONE 800 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - GALLEY SERVICE DOOR CUTOUT INNER PROTECTOR PLATE HAS CORROSION ON UNDERSIDE. REPAIRED IAW CRJ700 SRM 51-21-23-101-002-A01 AND SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050427001582005042700158EA 2005 4 27 QXEA200500431 120050303A5230 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 800 TOOL DAMAGE A QXEAK NONE W INADEQUATE Q C ININSP/MAINT 1 NM09605QX 10022 YYC - CENTER FUSELAGE, FORWARD BAGGAGE BAY DOOR, DOOR SKIN PANEL HAS TOOLING MARK. REPAIRED IAW REO-679-52-35-059 AND HORIZON AIR EAR-52-225. 2L72 4F RTA21EA 20050427001842005042700184WP 2005 4 27 DHL2005805684 120050320A5311 FRAME DOUG DC8 DC873F 302199FWP FUSLEAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME HOLE (1EA) MISDRILLED 0.1875 STA 700.000 L-11 L-12L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 02-25-05 EO NR AST 050210 DATE 02-21-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED AREA (MISDRILLED HOLES) IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLE WITH RIVET (MS20470AD) IAW EO NR AST 050210 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050427001862005042700186WP 2005 4 27 DHL2005805675 120050321A2120 HEAT EXCHANGER DOUG DC8 DC873F 302199FWP RT PRIMARY CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 0.500 CRACK IN SKIN OF RT PRIMARY HEAT EXCHANGER AFT LWR CORNER STA -12.000 L-27R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-16-05 DWG X83-R05, REV IR DATED 03-01-05. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. CUT OUT DAMAGED SECTION IAW DWG X83-R07. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER (AL2024-T3 0.050) REPAIR TRIPLER (AL2024-T3 0.063) AND FILLER (AL2024T3 0.100) IAW DWG X83-R05. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW DWG X83-R05 SRM 51-1-20D PG 9, SRM 51-1-21 PG 1, SRM 51-3-0 PG 1, SRM 51-1-26. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050427001882005042700188WP 2005 4 27 DHL2005805674 120050321A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 FUSELAGE EXTERIOR INTERIM REPAIR ON HOLD OPEN LATCH BUMPER ASSEMBLY SKIN AT STA 20.000 L-15L TO L-16L ( MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-16-05 DWG X83-R06 REV IR DATED 03-01-05. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. CUT OUT DAMAGED SECTION IAW DWG X83-R06. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER (AL7075-T60.071) AND (2EA) INTERNAL FINGER DOUBLER (AL7075-T6 0.032) AND FILLER (AL7075-T6 0.050) IAW DWG X83-R06. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW DWG X83-R06, SRM 51-1-21 PG.1, SRM 51-3-0 PG1, SRM 51-1-20D PG 9. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050427001902005042700190WP 2005 4 27 DHL2005805658 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBD FLANGE HOLE MISDRILLED STA 460.000 L-12R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-07-05 EO NR AST 050201 DATE 02-17-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLE WITH RIVET (MS20470AD) IAW EO NR AST 050201 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050427001912005042700191WP 2005 4 27 DHL2005805661 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT INBD FLANGE "Z" FRAME HOLES (2EA) MISDRILLED AT STA 240.000 L-10R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-07-05 EO NR AST 050201 DATE 02-17-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO NR AST 050201 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050427001922005042700192WP 2005 4 27 DHL2005805634 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBD FLANGE (1EA) MISDRILLED HOLE AT STA 220.000 L-18R L-19R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-07-05 EO NR AST 050201 DATED 02-17-05. PERFORMED DETAIL VISUAL INSP. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLE WITH RIVET (MS20470AD) IAW EO NR AST 050201 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050427001932005042700193WP 2005 4 27 DHL2005805647 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBD FLANGE (2EA) MISDRILLED HOLES STA 1320.000 L-10R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-07-05 EO NR AST 050201 DATE 02-17-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO NR AST 050201 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050427001942005042700194WP 2005 4 27 DHL2005805657 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBD FLANGE (2EA) HOLES MISDRILLED STA 1480.000 L-10R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-07-05 EO NR AST 050201 DATE 02-17-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO NR AST 050201 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050427001952005042700195WP 2005 4 27 DHL2005805660 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME (2EA) MISDRILLED HOLES AT STA 620.000 L-10R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-07-05 EO NR AST 050201 DATE 02-17-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO NR AST 050201 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050427001962005042700196WP 2005 4 27 DHL2005805628 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME (2EA) MISDRILLED HOLES AT STA 620.000 L-12L T L-13L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-05-05 EO NR AST 050205 DATED 02-21-05. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA AT STA 620.000 L-12L TO L-13L IAW SRM 51-1-8B. PERFORMED DETAIL VISUAL INSP. NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD6-5) IAW EO NR AST 050205 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050427001972005042700197WP 2005 4 27 DHL2005805631 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT "J" FRAME INBD FLANGE (1EA) HOLE MISDRILLED AT STA 1020.000 L-10L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 02-25-05 EO NR AST 050203 DATE 02-18-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO NR AST 050203 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050427001982005042700198WP 2005 4 27 DHL2005805610 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT INBD FLANGE "Z" FRAME HOLES 1EA MISDRILLED AT STA 100.000 L-19L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-05-05 EO NR AST 050205 DATE 02-21-05. CLEANED, TREATED AND PRIMED (AREA) MISDRILLED HOLES IAW SRM 51-1-8B. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS MS20470AD5-6 IAW EO NR AST050205 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050427001992005042700199WP 2005 4 27 DHL2005805635 120050314A5753 PLATE DOUG DC8 DC873F 302199FWP LT WING TE FLAP CRACKED A DHLAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SO01805DH80855 46125 LT INBD FLAP LWR PLATING (2EA) DENTS AND 0.250 CRACK (STA XF 30.000- 40.000) (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 02-28-05 EO NR AST 050209 DATED 02-25-05. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. CUT OUT DAMAGED SKIN SEGMENT IAW EO NR AST 050209. PERFORMED DETAIL VISUAL INSP. NO CRACK FOUND. FABRICATED NEW SKIN SEGMENT (AL2024T3 0.032) INNER BONDED DOUBLER (AL2024T30.020) SPLICE STRAP (AL2024T3 0.063) AND FILLER (AL2024T3 0.020) IAW EO NR AST 050209. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS AND NEW FASTENERS IAW EO NR AST 050209, SRM 51-1-9 PG 1 SRM 51-1-9A PG 1, SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050427002002005042700200WP 2005 4 27 DHL2005805638 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT INBD FLANGE "Z" FRAME (1EA) HOLE MISDRILLED AT STA 260.000 L-10R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-07-05 EO NR AST 050201 DATE 02-17-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLE WITH RIVET (MS20470AD) IAW EO NR AST 050201 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050427002012005042700201WP 2005 4 27 DHL2005805648 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME (2EA) MISDRILLED HOLES AT STA 440.000 L-10R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-07-05 EO NR AST 050201 DATE 02-17-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVET (MS20470AD) IAW EO NR AST 050201 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050427002022005042700202WP 2005 4 27 DHL2005805611 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT "Z" FRAME INBD FLANGE HOLES (2EA) MISDRILLED AT STA 1160.000 L-12L L-13L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-05-05 EO NR AST 050205 DATE 02-21-05. CLEANED, TREATED AND PRIMED AREA MISDRILLED HOLES IAW SRM 51-1-8B. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD6-4) IAW EO NR AST050205, SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050427002032005042700203WP 2005 4 27 DHL2005805629 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBD FLANGE (2EA) MISDRILLED HOLES AT STA 1180.000 L-10R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-07-05 EO NR AST 050201 DATED 02-17-05. PERFORMED DETAIL VISUAL INSP. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO NR AST 050201 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050427002042005042700204WP 2005 4 27 DHL2005805607 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT INBD FLANGE "Z" FRAME HOLES (3EA) MISDRILLED STA 300.000 L-14L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-05-05 EO NR AST 050205 DATE 02-21-05. CLEANED, TREATED AND PRIMED (AREA) MISDRILLED HOLES IAW SRM 51-1-8B. PERFORMED VISUAL INSPECTION DETAILED. NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD5-6) IAW EO NR AST 050205 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050427002052005042700205WP 2005 4 27 DHL2005805592 120050320A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME HOLE MISDRILLED 0.1875 STA 902.000 L-12 L-13L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 02-25-05 EO NR AST 050210 DATE 02-21-05. PERFORMED NDT INSPECTION (DETAILED). NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO NR AST 050210 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050427002062005042700206WP 2005 4 27 DHL2005805593 120050320A5320 CLIP DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT CLIP HOLES (2EA) MISDRILLED 0.15625 STA 834.000 L-13R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-13-05 EO NR AST 050220 DATE 03-08-05. REMOVED DAMAGED CLIP IAW SRM 51-1-21 PAGE 1. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. FABRICATED NEW CLIP (AL7075-T6 0.063) IAW EO NR AST 050220. CLEANED, TREATED AND PRIMED AREA AND NEW CLIP IAW SRM 51-1-8B. INSTALLED NEW CLIP IAW EO NR AST 050220 SRM 51-1-21 PAGE 1. (MS20470AD) 2L74 4F RT4A25 20050427002072005042700207WP 2005 4 27 DHL2005805596 120050320A5311 FRAME DOUG DC8 DC873F 302199FWP FUSLEAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME (1EA) ANGLE CRACKED STA 480.000 L-8R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-14-05 EO NR AST 050222 DATED 03-09-05. REMOVED CRACKED SUPPORT ANGLE IAW SRM 51-1-21 PG 1. PERFORMED DETAIL VISUAL INSP. NO CRACK FOUND. FABRICATED NEW SUPPORT ANGLE (EXTRUSION 7075T6 0.063) IAW EO NR AST 050222. CLEANED, TREATED AND PRIMED AREA AND SUPPORT ANGLE IAW SRM 51-1-8B. INSTALLED NEW SUPPORT ANGLE IAW EO NR AST 050222, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050427002082005042700208WP 2005 4 27 DHL2005805659 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBD FLANGE (1EA) HOLE MISDRILLED STA 600.000 L-12R. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-07-05 EO NR AST 050201 DATE 02-17-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLE WITH RIVET (MS20470AD) IAW EO NR AST 050201 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050427002102005042700210WP 2005 4 27 DHL2005805586 120050320A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME SUPPORT ANGLE CRACKED AT STA 700.000 L-10R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-14-05 EO NR AST 050222 DATE 03-09-05. REMOVED DAMAGED SUPPORT ANGLE IAW SRM 51-1-21 PG 1. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. FABRICATED NEW SUPPORT ANGLE (EXTRUSION 7075-T6 0.090) IAW EO NR AST 050222. CLEANED, TREATED AND PRIMED AREA AND SUPPORT ANGLE IAW SRM 51-1-8B. INSTALLED NEW SUPPORT ANGLE IAW EO NR AST 050222 SRM 51-1-21 PG1. 2L74 4F RT4A25 20050427002122005042700212WP 2005 4 27 DHL2005805633 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT "J" FRAME INBD FLANGE (2EA) MISDRILLED HOLES AT STA 980.000 L-10R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 02-25-05 EO NR AST 050203 DATED 02-18-05. PERFORMED DETAIL VISUAL INSP. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA AT STA 980.000 L-10R IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO NR AST 050203 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050427002142005042700214WP 2005 4 27 DHL2005805591 120050320A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT "Z" FRAME INBD FLANGE (4EA) MISDRILLED HOLES AND WEAR AT STA 80.000 BETWEEN L-14R AND L-17R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FA FORM 8110-3 DATED 03-15-05, EO NR AST 050219 DATED 03-07-05. PERFORMED DETAIL VISUAL INSP. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. FABRICATED ANGLE DOUBLER (AL7075:O: 0.100) IAW EO NR AST 050219, SRM 51-1-4 PG.1. HEAT TREATED IAW SRM 51-1-1 PG 1-13-17. CLEANED, TREATED AND PRIMED ANGLE DOUBLER IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (NAS1097AD) IAW EO NR AST050219, SRM 51-1-21 PG 1. INSTALLED ANGLE DOUBLER WITH RIVETS (MS20470AD) IAW EO NR AST050219, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050427002162005042700216WP 2005 4 27 DHL2005805630 120050320A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT (8EA) MISDRILLED HOLES IN L-12L (STA 600.000 - 620.000) (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-15-05 EO NR AST 050216 DATED 03-02-05. PERFORMED DETAIL VISUAL INSP. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO NR AST 050216, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050427002172005042700217WP 2005 4 27 DHL2005805636 120050321A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 LT OUTER WING INBD L/E HOLE ELONGATED AT STA XFS 710.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-16-05 DWG X83-R02 REV IR DATE 02-23-05. REMOVED FASTENERS FROM AREA (REPAIRED) IAW SRM 51-1-21 PAGE 1, SRM 51-3-0 PAGE 1, SRM 51-1-20D PAGE 21. TRIMMED OUT DAMAGED AREA IAW DWG X83-R02. PERFORMED NDT INSPECTION TO AREA IAW NDT SPM PART 06-10-01-001. FABRICATED FILLER (AL7075T6 0.050) REPAIR DOUBLER (AL7075T6 0.063) IAW DWG X83-R02. CLEANED, TREATED AND PRIMED AREA, FILLER, REPAIR DOUBLER INTERNAL PART IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW DWG X83-R02, SRM 51-1-21 PAGE 1, SRM 51-3-0 PAGE 1, SRM 51-1-20D PAGE 9. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050427002292005042700229WP 2005 4 27 DHL2005805556 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBD FLANGE HOLES (2EA) MISDRILLED AT STA 1500.000 L-10R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-07-05 EO NR AST050201 DATE 02-17-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO NR AST050201, SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050427002312005042700231WP 2005 4 27 DHL2005805574 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME HOLES (2EA) MISDRILLED, STA 717.000 L-10R. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 02-25-05, EO NR AST 050203 DATE 02-18-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED AREA (MISDRILLED HOLES ) IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD5-4) IAW EO NR AST050203, SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050427002332005042700233WP 2005 4 27 DHL2005805671 120050225A5310 DOOR FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 AFT PASSENGER DOOR AFT UPPER JAMB CORNER HAS CRACKS 0.250, 0.750 STA 1660.000 BETWEEN L-9 AND L-10L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 18 TR NR 53-134, TR NR 53-199 DWG SR 08530021 DWG 5750776. REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1. TRIMMED OUT DAMAGED AREA AND FABRICATED REPAIR DOUBLER (AL7075T6 0.090) REPAIR TRIPLER (AL7075T6 0.125) FILLER (AL7075-T6 0.080) IAW SRM 53-2-0 FIG 18 SHEET 3 SHEET 1 VIEW D ( TR 53 TR 154) SHEET 5-6-7-8 (TR53-199) IAW SRM 51-1-4 PAGE 1. PERFORMED NDT INSPECTION TO AREA IAW DC8 NDT SPM PART 06-10-01-001. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SRM 53-2-0 FIG 18 TR 53-134 TR 53-199 SR08530021. TORQ2L74 4F RT4A25 20050427002352005042700235WP 2005 4 27 DHL2005805552 120050320A5340 CLIP DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT CLIP HAS A MISDRILLED HOLE OF 0.1875 AT STA 834.000 L-17L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-13-05, EO NR AST 050220 DATED 03-08-05. REMOVED DAMAGED CLIP IAW SRM 51-1-21 PG 1. PERFORMED DETAIL VISUAL INSP. NO CRACK FOUND. FABRICATED NEW CLIP (AL7075T60.063) IAW EO NR AST050220. CLEANED, TREATED AND PRIMED AREA AND NEW CLIP IAW SRM 51-1-8B. INSTALLED NEW CLIP IAW EO NR AST050220, SRM 51-1-21 PG 1 (MS20470AD). 2L74 4F RT4A25 20050427002372005042700237WP 2005 4 27 DHL2005805550 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT INBD FLANGE "Z" FRAME HOLES (2EA) MISDRILLED AT STA 280.000 L-10R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-07-05, EO NR AST050201 DATE 02-17-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO NR AST050201, SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050427002392005042700239WP 2005 4 27 DHL2005805549 120050320A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT. "Z" FRAME INBD FLANGE HOLES (2EA) MISDRILLED STA 980.000 L-12 - L-13L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 02-25-05, EO NR AST050202 DATE 02-17-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED AREA (MISDRILLED HOLES) IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO NR AST050202, SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050427002712005042700271EA 2005 4 27 QXEA200500522 120050302A5753 VANE CNDAIRCL600 CL6002C10 1390015EA ZONE 600 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - RIGHT HAND INBOARD FLAP VANE INBOARD LEADING EDGE PANEL 684ET HAS CHAFED MARK. REPAIRED IAW CRJ700 SRM 57-52-02-101-001-A01 AND SRM 51-12-00-001-001-A01. 2L72 4F RTA21EA 20050427002732005042700273EA 2005 4 27 QXEA200500520 120050303A5753 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 600 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - RIGHT HAND INBOARD FLAP LOWER SURFACE HAS GRAVEL DAMAGED. REPAIRED IAW CRJ700 SRM 57-52-01-101-001-A01, SRM 51-12-00-001-001-A01, AND SRM 51-25-16-001-001-A01. 2L72 4F RTA21EA 20050427002752005042700275EA 2005 4 27 QXEA200500518 120050301A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - FUSELAGE INTERIOR FS 280 BULKHEAD RIGHT HAND LOWER WEB IS CORRODED ALONG FLOOR LEVEL. REPAIRED IAW REO 670-53-11-052. 2L72 4F RTA21EA 20050427002802005042700280EA 2005 4 27 MASA200500008 120050104A32304622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA MLG INOPERATIVE A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0717358 7358 ASH 6152 FROM DSM TO PHX RETURNED TO THE FIELD DUE TO A GEAR DISAGREE AFTER TAKEOFF. WAITING FOR WEATHER TO IMPROVE BEFORE FERRYING THE AIRCRAFT. 1/6/04 MAINTENANCE REPLACED PRIORITY VALVE, NLG SELECTOR VALVE P/N 750006000, PROX SENSOR P/N 8-642-02 AND A CABLE HARNESS P/N 17300-205. 2L72 4F RTA21EA 20050427002812005042700281EA 2005 4 27 MASA200500015 120050106A2410 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA NR 1 IDG ILLUMINATED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW0717275 7275 ASH 6370 YUM TO PHX ABORTED TAKEOFF, DUE TO NR 1 IDG MESSAGE ON TAKEOFF ROLL. MAINTENANCE COMPLIED WITH MEL PROCEDURES. 1/6 04 MAINTENANCE SERVICED IDG, OPS CHECKED GOOD. 2L72 4F RTA21EA 20050427002832005042700283EA 2005 4 27 MASA200500022 120050108A3260 PROXIMITY SWITCH CNDAIRCL600 CL6002B19 1900309EA MLG OUT OF ADJUST A MASAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW0717358 7358 ASH 6239 PHX - SBA - PILOT RETURNED TO THE FIELD WITH A GEAR DISAGREE MESSAGE AFTER TAKOFF. MAINTENANCE ADJUSTED AND CENTERED THE PROX SWITCH. 2L72 4F RTA21EA 20050427002852005042700285EA 2005 4 27 MASA200500030 120050112A3230750006000 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA NLG FAILED A MASAO OTHER J WARNING INDICATION APAPPROACH 1 SW07372183563 2604 7218 ASH 6531 FROM LAS TO ONT HAD A GEAR DISAGREE AND NOSE GEAR DOOR OPEN MESSAGE UPON GEAR EXTENSION. AIRCRAFT WAS FERRIED TO PHX FOR TROUBLESHOOTING AND REPAIR. MAINTENANCE REPLACED NLG SELECTOR VALVE. 2L72 4F RTA21EA 20050427002862005042700286SO 2005 4 27 MASA200500227 120050317A3397 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT UNSECURE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07826MJ 145214 ASH 2849 FROM CLT TO GSO, HAD THE RT OVERWING EXIT EMERGENCY EXIT LIGHT INOP. MAINTENANCE SECURED THE LIGHT CONNECTOR AND IT OPERATED NORMALLY. A/C DEPARTED WITHOUT FURTHER INCIDENT. 2L72 4T RTT00011AT 20050427002882005042700288SO 2005 4 27 MASA200500237 120050319A335020131A BATTERY PACK EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07837MJ7138 145367 ASH 2987 BHM HAD THE AFT HALF OF THE EMERGENCY EXIT FLOOR PATH LIGHTING INOP. THE A/C WAS FERRIED TO CLT WHERE THE NR 3 AND NR 4 POWER SUPPLIES WERE REPLACED. 2L72 4T RTT00011AT 20050427002902005042700290EA 2005 4 27 MASA200500040 120050116A5210601R386493 PUSHROD CNDAIRCL600 CL6002B19 1900309EA PAX DOOR VENT DAMAGED A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07154SF 7154 ASH 2686 PHL TO GSO RETURNED TO THE FIELD DUE TO CABIN ALT MSG IN FLIGHT AND THE AIRCRAFT WOULD NOT PRESSURIZE. MAINTENANCE REPLACED THE PAX DOOR VENT FLAP ROD. 2L72 4F RTA21EA 20050427002922005042700292WP 2005 4 27 05FDEA00707 120050330A5753ARC25121 HINGE DOUG MD10 MD1010F 3022112WP ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2510060 46970 LEFT WING INBOARD FLAP, OUTBOARD SUPPORT, PIVOT ATTACH POINT INBOARD BORE CORRODED. REMOVED CORROSION FROM BORE IAW DAC CMM 57-52-01, ALODINE AND PRIMED BORE IAW DC19-10 SRM 51-21-01 VOL 2. FABRICATED AND INSTALLED AND FINAL HONED NEW OVERSIZED BUSHING TO 0.9995-1,0005 INCHES IAW DAC CMM 57-52-01 AND EA 8-5750-83998, WINGS-LEFT INBOARD FLAP, OUTBOARD HINGE BRACKET OVERSIZE PIVOT BORES AND STRAP-REPAIR. 2L73 4F RTA22WE 20050427002942005042700294NM 2005 4 27 05FDEA00724 120050331A5511 SPAR CAP DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZ STAB LT FWD SPAR CAP NR 1L BARREL NUT BORE FOUND EXCEEDED LIMITS. REWORK/REPAIR - 1-5510-7-5000 HAS BEEN COMPLIED WITH. 2L73 4F RTA22WE 20050427002962005042700296NM 2005 4 27 05FDEA00726 120050331A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZ STAB LT UPPER FWD SKIN PLANK NR 7L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82939. 2L73 4F RTA22WE 20050427002982005042700298NM 2005 4 27 05FDEA00729 120050331A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZ STAB LT UPPER FWD SKIN PLANK NR 11L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82939. 2L73 4F RTA22WE 20050427003002005042700300NM 2005 4 27 05FDEA00731 120050331A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HOR STAB LT UPPER CENTER SKIN PLANK NR 15L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82940. 2L73 4F RTA22WE 20050427003022005042700302NM 2005 4 27 05FDEA00733 120050331A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZ STAB RT UPPER FWD SKIN PLANK NR 10R BARREL NUT BORE FOUND EXCEEDED LIMITS. REWORK/REPAIR 1-5510-7-5000 HAS BEEN COMPLIED WITH. 2L73 4F RTA22WE 20050427003042005042700304WP 2005 4 27 DHL2005802005 120050331A5270 CONNECTOR DOUG DC8 DC873 302199CWP MLG DOOR DIRTY A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01802DH 46076 DOORS NOT LATCHED AND LEFT DOOR UNSAFE LIGHT ILLUMINATED AFTER GEAR RETRACTED LIGHT WENT OUT APPROX ONE 1/2 MINUTES AFTER RETRACTION. CLEANED AND RESECURED CONNECTOR ON LT DOOR SW. OPS CK GOOD PER MM 32-60-0. 2L74 4F RT4A25 20050427003072005042700307NM 2005 4 27 DHL2005770005 120050401A2750 CONTROL SYSTEM BOEING727 7272B7 138407LNM TE FLAPS MALFUNCTIONED A DHLAO OTHER E VIBRATION/BUFFET CRCRUISE 1 SO01770AT 21953 AT FL 340 .80 MACH FLUTTER OR VIBRATION FELT IN AIRFRAME EXTEND SPOILER (CRACK) FLUTTER ELIMINATED. STOW SPOILER AND FLUTTER RETURNS AT SPEED BELOW .79 MACH FLUTTER ELIMINATED, RETURNS ABOVE. ADJUSTED LEFT OUTBOARD FLAP ECCENTRICS, CK OK IAW MM 27-51-00 (TRAILING EDGE FLAP) 2L73 4F A3WE 20050427003312005042700331NM 2005 4 27 05FDEA00463 120050309A5322 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 CORROSION OF SHEAR TIE FWD SIDE BS 1050, AT STR 27, AFT CARGO BAY. REPAIRED PER SRM 53-10-4. 2L73 4F RTA3WE 20050427003322005042700332NM 2005 4 27 05FDEA00481 120050309A5347ABA7680505 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25592FE 48550 MAIN DECK CARGO, SEAT TRACK CORRODED AT STA 461-470 LBL 90. REPLACED IAW SRM 51-33-01 VOL 2. 2L73 4F RTA22WE 20050427003342005042700334EU 2005 4 27 05FDEA00447 120050308A5330 SKIN AIRBUS310 A310 EU FUSELAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25446FE 224 BULK PIT UNDER FLOOR AREA FS 69 STR 48 LT HAS AN AREA THAT EXTEND 2 INCHES FWD OF FS 69 OF CORROSION EXTENDING UNDER SHEAR TIE. REMOVED SHEAR TIE AND STRINGER SECTION IAW A310-200 SRM 53-10-14. INSTALLED SHEAR TIE AND STRINGER SECTION IAW A310-200 SRM 53-10-14. 2L72 4F RTA35EU 20050427003352005042700335WP 2005 4 27 AALA20050170 120050304A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21234AA 49181 SFO - LEFT AND RIGHT FUSELAGE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR LEFT AND RIGHT EMERGENCY LIGHT. LEFT EMERGENCY LIGHT WORKS. RIGHT EMERGENCY LIGHT STILL INOPERATIVE. REPLACED BULB IN RIGHT EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (SUPP. CLOSED) 2L72 4F A6WE 20050427003372005042700337WP 2005 4 27 AALA20050181 120050310A2120 CLAMP DOUG DC9 DC982 3022082WP APU BROKEN A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21585AA 53248 DFW - ON CLIMBOUT NOTICED HOT SMELL. FLIGHT ATTENDANT REPORTED SMOKE IN CABIN. LEFT HAND PACK WAS IN MANUAL PER MEL. TURNED OFF LEFT HAND PACK AND REQUESTED RETURN TO DFW. NEVER GOT OVER 13K FEET. DID AIRCRAFT SMOKE IN CABIN CHECK LIST PULLED CIRCUIT BREAKER FOR RECIRCULATION FAN. FLIGHT ATTENDANT REPORTED SMOKE WAS GETTING BETTER/IMPROVING. TAXIED TO GATE NO SMOKE AT ANYTIME IN COCKPIT. APU WAS NOT RUNNING. REPLACED LEFT TEMPERATURE CONTROL VALVE AND BROKEN CLAMP. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F A6WE 20050427003382005042700338NM 2005 4 27 05FDEA00488 120050310A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 BS 480, STRINGER 26 RT IS CORRODED. REMOVED CORROSION, OUT OF LIMITS PER SRM, REPLACED STR 26 RT AT BS 480 TO BS 510, IAW SRM 53-10-3 AND 51-30-2. 2L73 4F RTA3WE 20050427003392005042700339NM 2005 4 27 05FDEA00496 120050311A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 BS 585 STR 24 LT IS DENTED AND GOUGED. REPAIRED STR 24 LT, BS 585 PER SRM 53-10-1, SRM 53-10-3 AND MM 51-20-151. 2L73 4F RTA3WE 20050427003402005042700340NM 2005 4 27 05FDEA00498 120050311A5322 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 CORROSION ON SHEAR TIE, FWD SIDE, BS 1110, AT STR 28L AFT CARGO BAY. REPAIRED PER SRM 53-10-4 AND 51-30-2. 2L73 4F RTA3WE 20050427003412005042700341NM 2005 4 27 05FDEA00499 120050311A5513 SPLICE BOEING727 727200 138407ENM STRINGER CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 CORROSION ON STRINGER SPLICE AT BS 678 STRINGER 28L. INSTALLED NEW STRINGER SPLICE AT BS 678, STR 28L IAW SRM 51-30-2 & SRM 51-10-2. 2L73 4F RTA3WE 20050427003422005042700342NM 2005 4 27 BB05016 120050311A2597R071014A7SNL CONNECTOR BOEING767 767201 1385125NM RT WING CONTAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19650US 23902 SJU - THE RIGHT SPOILER BLOW DOWN SQUIB LIGHT FAILED TO ILLUMINATE DURING TEST. MAINTENANCE FOUND GLYCOL PRESENT IN THE SQUIB CONNECTOR AND SOME BENT PINS. STRAIGHTENED PINS AND REPLACED CONNECTOR D1166. 2L72 4F RTA1NM 20050427003452005042700345CE 2005 4 27 DXTA200500625 120050312A2120 ODOR CESSNA500 560CESSNA 2076750CE COCKPIT DETECTED E DXTAB EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07354QS 5600356 SMELL OF SMOKE IN COCKPIT AFTER APPROX 1 HOUR AT FL400. AIRCRAFT RUN WITH FULL ELECTRICAL LOAD, NO SMELL/DEFECTS NOTED. RT & LT CB PANELS LOWERED TO INSPECT CB PANEL REAR, NO DEFECTS NOTED. FREON AIR CON UNIT RUN FOR OVER 30 MINUTES NO DEFECTS/SMELL NOTED. INSP OVERHEAD BLOWER AS PER 21-21-04, NO DEFECTS NOTED INSP DEFOG. FAN BLOWER PER 21-21-01 NO DEFECTS NOTED. REMOVED, INSP, & CLEANED COALESCER SOCK PER 21-70-00. NO ODOR NOTED. ACCOMP ENG RUN, RUN ACH FULL HOT / FULL COLD FOR OVER 45 MIN NO SMELL / DEFECTS NOTED. RAN OVERHEAD BLOWER / DEFOG FAN FOR OVER 30 MIN NO SMELL / DEFECTS NOTED. NO ODOR, NO SMOKE, NO DEFECTS NOTED AT THIS TIME. COULD NOT DUPLICATE WRITE UP ON GROUND. 2L72 4F RTA22CE 20050427003462005042700346EU 2005 4 27 SA05028 120050314A3397 CONNECTOR AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT MISWIRED A USAAK NONE O OTHER ININSP/MAINT 1 EA19706US 946 CLT - EMERGENCY LIGHTING INOPERATIVE AT FORWARD STOWAGE COMPARTMENT IN THE FORWARD GALLEY. MAINTENANCE FOUND CONNECTORS 7441VS-A AND 7443VS-A SWAPPED AND RECONNECTED THEM PROPERLY. 2L72 4F RTA28NM 20050427003472005042700347NE 2005 4 27 05FDEA00501 220050312A7261 OIL FILTER BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE NR 1 ENGINE BYPASSING A FDEAE ENGINE SHUTDOWN J WARNING INDICATION DEDESCENT 1 SO25240FE 20978 DESCENDING THROUGH 20,000 FEET, THE NR 1 LOW OIL PRESSURE/FILTER BYPASS LIGHT ILLUMINATED; ENGINE OIL PRESSURE READ 45 PSI (MATCHED NR 2 AND NR 3). SHUT DOWN NR 1 ENGINE IAW QRH PROCEDURES. NO OTHER PROBLEMS NOTED. 2L73 4F4 FRTA3WE E2EA 20050427003482005042700348WP 2005 4 27 05FDEA00504 120050310A5330071X48X722024T SKIN DOUG DC10 DC1010 3022110WP ZONE 100 TORN A FDEAO OTHER O OTHER TXTAXI/GRND HDL 1 SO2568058 46705 INSPECTED DAMAGED AREA, FOUND A LARGE TEAR IN SKIN APPROX 16 X 6 INCH FWD OF FR959 L AND ABOVE STRINGER 41L. STOP DRILLED TEARS AND CUT OUT DAMAGE PER DC10 SRM 53-20-00 VOL 1 FIG 6 SHEET 7. UPON REMOVAL OF SKIN FOUND TEAR STRIP AT FR 959L/ STRINGER 41L CRACKED. REMOVED ADDITIONAL SKIN IN ORDER TO CUT THE DAMAGED SECTION OF TEAR STRIP. REMOVED DAMAGE SECTION OF TEAR STRIP PER DC10 SRM 53-20-00 VOL 1 FIG 18. REPAIR IS A CLASS 2 REPAIR AS PER SRM 53-20-0 FIG 6 SHEET 7, AND REQUIRES AN INITIAL INSPECTION AT 15,000 CYCLES, A REPETITIVE AT 9,800 AND REPLACEMENT AT 37,450 CYCLES. 2L73 4F A22WE 20050427003492005042700349NM 2005 4 27 05FDEA00505 120050314A2822 PUMP BOEING727 727200 138407ENM FUEL BOOST MALFUNCTIONED A FDEAC ABORTED TAKEOFF GJ MULTIPLE FAILURE WARNING INDICATION TOTAKEOFF 1 SO25218FE 21101 ON TAKEOFF ROLL, NR 2 FUEL TANK LEFT FORWARD BOOST PUMP CIRCUIT BREAKER POPPED; 3 SECONDS LATER, RIGHT AFT BOOST PUMP CIRCUIT BREAKER POPPED. NOTE: USING GEN 1 FOR ESSENTIAL POWER. CHECKED PER 24-09-100-2 FOUND OK. CHECKED PER 28-22-000-1 FOUND OK. REMOVED & REPLACED NR 2 LEFT FORWARD B/P CIRCUIT BREAKER. RAN NR 2 ENGINE PER JRH. NO CIRCUIT BREAKERS POPPED. OK FOR SERVICE. 2L73 4F RTA3WE 20050427003502005042700350CE 2005 4 27 70122 120050404A3242 BRAKE BEECH 1900 1900D 1154162CE MLG DIRTY A AMWAK NONE O OTHER NRNOT REPORTED 1 CE07176YV UE176 AFTER ARRIVING AT GATE IN DFW, CREW REPORTED LEFT BRAKE WEAK. MAINTENANCE CLEANED THE BRAKES. THEREFORE NO PARTS WERE USED. 2L72 4T RTA24CE 20050427003522005042700352NM 2005 4 27 AWXA200500426 120050311A5330654577683 SKIN BOEING737 737375 13844BNNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 MCN - MAJOR REPAIR - DURING C-05 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF BILGE SKIN BETWEEN BS 988 AND BS 1005, STR 26 LT AND STR 27 RT. MAINTENANCE CUT OUT CORRODED SKIN FROM BS 988 TO BS 1005, STR 26 LT TO STR 27 RT; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-01 FIG 226. 2L72 4F RTA16WE 20050427003532005042700353NM 2005 4 27 QXEA200500540 120050323A7110 BRACKET BOMBDRDHC8 DHC8401 1390041NM NR 1 COWLING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09416QX 4083 PDX - NR 1 ENGINE RIGHTHAND FORWARD SPINE COWL BRACKET IS CRACKED. REPAIRED IAW RD 8/4-71-032 AND DHC-8-400 SRM 51-42-05. 2H72 4T RTA13NM 20050427003552005042700355NM 2005 4 27 QXEA200500542 120050327A7110 STIFFENER BOMBDRDHC8 DHC8401 1390041NM COWLING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09416QX 4083 PDX - 412AB LOWER COWL FRAME ASSEMBLY SUPPORT STIFFENER IS CRACKED. REPLACED IAW RD 8/4-71-016. 2H72 4T RTA13NM 20050427003562005042700356NM 2005 4 27 QXEA200500533 120050325A5542 SKIN BOMBDRDHC8 DHC8401 1390041NM RUDDER DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09416QX 4083 PDX - CREASE IN FORE RUDDER, RIGHTHAND SIDE, JUST ABOVE THE 4TH RIB FROM THE TOP. REPAIRED IAW RD 8/4-55-001 AND HORIZON AIR EA 6-55-111. 2H72 4T RTA13NM 20050427003572005042700357EA 2005 4 27 QXEA200500549 120050316A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE INTERIOR, FUSELAGE STATION 280 BULKHEAD RIGHTHAND LOWER WEB IS CORRODED ALONG THE FLOOR CROSSBEAM. REPAIRED IAW REO 670-53-11-052, REV A. 2L72 4F RTA21EA 20050427003612005042700361EA 2005 4 27 QXEA200500628 120050324A1430 FASTENER CNDAIRCL600 CL6002C10 1390015EA RT WING CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - RIGHTHAND WING LOWER SURFACE INBOARD MAIN LANDING GEAR DOUBLER PLATE ATTACHMENT FASTENERS ARE RUSTY. REPAIRED IAW CRJ700 SRM 51-21-00-001-001-A01 AND SRM 51-25-00-001-001-A01. 2L72 4F RTA21EA 20050427003622005042700362EA 2005 4 27 QXEA200500624 120050323A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA FUSELAGE GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - CENTER FUSELAGE, LOWER FUSELAGE SKIN GOUGED AT FUSELAGE STATION 975.00 AND STRINGER 27.0. REPAIRED IAW CRJ700 SRM 51-21-16-001-001-A01 AND HORIZON AIR EA R-53-787. 2L72 4F RTA21EA 20050427003642005042700364NM 2005 4 27 QXEA200500684 120050401A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09367PH 511 PDX - LEFTHAND INBOARD SEAT TRACK HAS SURFACE CORROSION ALONG 10 INCH AREA ON INBOARD FLANGE AT STATION 580. REPAIRED IAW RD 8-53-784. 2H72 4T RTA13NM 20050427003672005042700367NM 2005 4 27 QXEA200500678 120050401A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09367PH 511 PDX - LEFTHAND INBOARD SEAT TRACK HAS CORROSION INSIDE CHANNEL AT STATION 468. REPAIRED IAW RD 8-53-1339. 2H72 4T RTA13NM 20050427003682005042700368NM 2005 4 27 QXEA200500682 120050401A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09367PH 511 PDX - LEFTHAND INBOARD SEAT TRACK HAS CORROSION ON TOP OF CHANNEL AT STATION X516. REPAIRED IAW RD 8-53-1339. 2H72 4T RTA13NM 20050426000622005042600062EU 2005 4 26 05FDEA00474 120050309A5347 SEAT TRACK AIRBUS310 A310 EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 REF SNRM# N00536 MDCC ZONE 241 RT SEAT TRACK NR 5 FR 5.5 FR50 FR50.5 FR53 FR54 CORROSION INSIDE SCALLOPED HOLES 5-AREAS. REMOVED CORROSION IAW SRM 51-74-10 OUT OF LIMITS IAW SRM 53-10-16 FIG 101. REMOVED BAD SECTION OF TRACK FABBED REPAIR SPLICES AND TRACK INSTALLED NEW REPAIR SPLICES AND TRACK IAW SRM 53-10-16 FIG 205. 2L72 4F RTA35EU 20050426000892005042600089EA 2005 4 26 QXEA200500504 120050320A5315 FLOORBEAM CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09613QX 10045 PDX - FLOORBEAM AT FUSELAGE STATION 280.00 CORRODED WL 72.50 FROM LBL 22.0 - RBL 25.0 AND CRACK AT FS 280.0 WL 72.50 BLL 12.0. REPAIRED IAW REO 670-53-11-045. 2L72 4F RTA21EA 20050426000942005042600094NM 2005 4 26 SWAA051027 120050409A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED C4 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS BETWEEN BS 312 & BS 317, BETWEEN STR 18R & STR 19R. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050426000952005042600095NM 2005 4 26 SWAA051028 120050408A575465C26685 SKIN BOEING737 7373H4 1384600NM L/E SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED C4 CHECK, FOUND RT WING NR 4 L/E SLAT INBOARD & OUTBOARD AUX TRACK CUTOUTS CRACKED. REPAIRED SLAT PER SWA EA & SRM. 2L72 4F RTA16WE 20050426000972005042600097NM 2005 4 26 SWAA051030 120050408A575565C2525121A SPOILER BOEING737 7373H4 1384600NM RT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED C4 CHECK, FOUND RT WING NR 8 SPOILER DELAMINATED. REMOVED AND REPLACED NR 8 SPOILER PER MM. 2L72 4F RTA16WE 20050426001002005042600100NM 2005 4 26 SWAA051033 120050410A33506128251 CHARGER BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29321SW 23342 DURING SCHEDULED RON CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM. 2L72 4F RTA16WE 20050426001112005042600111SW 2005 4 26 AC2A099721 120050110A2432RG222 BATTERY BELL 206 206L3 1182108SW MASTER WEAK B AC2AO OTHER O OTHER NRNOT REPORTED 1 SO0717238674 51492 BATTERY IS WEAK. BATTERY FAILED TWO CAPACITY CHECKS EVEN AFTER ONE CONDITIONING CHARGE. REPLACED BATTERY. 1G71 3U H2SW 20050426001132005042600113SW 2005 4 26 AC2A099729 120050221A2432RG407A1 BATTERY BELL 430 430 1182150SW MASTER WEAK B AC2AO OTHER O OTHER NRNOT REPORTED 1 SO07430CV236 49072 BATTERY IS WEAK. CHARGED AND TESTED. FAILED FIRST CHECK. CHARGED WITH CONDITIONING CHARGE AND RETESTED, FAILED SECOND CHECK. RECHARGED BATTERY AND APPLIED FOR WARRANTY, S/O NR S3034. 1G72 3U RTH9SW 20050426001172005042600117SW 2005 4 26 AC2A099730 120050221A3246427036123101 SKID SHOE BELL 427 427 1182207SW MLG BROKEN B AC2AK NONE O OTHER ININSP/MAINT 1 SO07427CK198 56043 SKID SHOE IS BROKEN OUT AT ATTACHMENT HOLES. REPLACED WITH NEW SKID SHOE ASSEMBLY. 1G71 3U R00001RC 20050427003692005042700369NM 2005 4 27 QXEA200500675 120050401A5330 SKIN DHAV DHC8 DHC8202 2809007NM FUSELAGE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09367PH 511 PDX - THERE IS CHAFING DAMAGE ON FUSELAGE SKIN, AT FORWARD TOP CORNER AREA OF FUSELAGE SURROUND. REPAIRED IAW HORIZON AIR EA 2-53-615 AND 51-12-00. 2H72 4T RTA13NM 20050427003712005042700371NM 2005 4 27 QXEA200500692 120050414A5320 SILL DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - MAIN CABIN DOOR SILL CORRODED ON TOP SIDE AT AFT END FLOOR SUPPORT TAB. REPAIRED IAW DHC-8 200 SRM 51-40-00 AND SRM 51-40-11. 2H72 4T RTA13NM 20050427003752005042700375NM 2005 4 27 QXEA200500665 120050410A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - LEFTHAND INBOARD SEAT TRACK HAS SURFACE CORROSION BETWEEN STATION X240.0 AND X252.0 IN TWO LOCATIONS. REPLACED NR 4 SEAT TRACK. 2H72 4T RTA13NM 20050427003772005042700377NM 2005 4 27 QXEA200500662 120050410A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - RIGHTHAND INBOARD SEAT TRACK , TOP OF TRACK CORRODED IN CENTER IN TWO LOCATION BETWEEN X182 AND X201. REPLACED SEAT TRACK. 2H72 4T RTA13NM 20050427003822005042700382NM 2005 4 27 QXEA200500702 120050413A5711 SPAR DHAV DHC8 DHC8202 2809007NM LT WING CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - LEFTHAND WING FORWARD SPAR LOWER FLANGE IS CHAFED AT WING STATION YW130 - YW138. REPAIRED IAW DHC-8 200 SRM 51-40-11 AND RD 8-57-1150. 2H72 4T RTA13NM 20050427003832005042700383NM 2005 4 27 QXEA200500704 120050413A5521 RIB DHAV DHC8 DHC8202 2809007NM LT ELEVATOR CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - LEFT ELEVATOR HORN, INBOARD CLOSING RIB HAS CHAFE DAMAGE AT TOP AND BOTTOM. REPAIRED IAW DHC-8 200 SRM 51-20-11, 51-20-16 AND SRM 51-20-57. 2H72 4T RTA13NM 20050427003852005042700385NM 2005 4 27 QXEA200500705 120050413A5521 RIB DHAV DHC8 DHC8202 2809007NM RT ELEVATOR CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - RIGHTHAND ELEVATOR HORN, INBOARD CLOSING RIB HAS CHAFE DAMAGE ON TOP SURFACE. REPAIRED IAW DHC-8 200 SRM 51-00-02, 51-20-36 AND SRM 51-20-51. 2H72 4T RTA13NM 20050427003882005042700388NM 2005 4 27 QXEA200500698 120050413A5753 SKIN DHAV DHC8 DHC8202 2809007NM T/E FLAP CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - RIGHTHAND WING, OUTBOARD FLAP, CHAFE ON TOP SURFACE 2.25 INCH FROM INBOARD EDGE X20 AND 20 1/4 INCH UP FROM TRAILING EDGE. REPAIRED IAW RD 8-57-1734. 2H72 4T RTA13NM 20050427003892005042700389NM 2005 4 27 QXEA200500695 120050413A5330 SKIN DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - FUSELAGE SKIN UNDER THE NR 2 DME ANTENNA HAS EVIDENCE OF CORROSION. REPAIRED IAW DHC-8 200 SRM 51-20-16. 2H72 4T RTA13NM 20050427003942005042700394NM 2005 4 27 QXEA200500687 120050413A1430 RIVET DHAV DHC8 DHC8202 2809007NM FUSELAGE LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - FOUR RIVETS SMOKING/PULLING THROUGH SKIN UNDER WING FAIRING, APPROXIMATELY X424, LEFT SIDE WHERE LOWER END OF FAIRING MEETS FUSELAGE. REPAIRED IAW DHC-8 200 SRM 51-40-00, PAGE 1-6. 2H72 4T RTA13NM 20050427003962005042700396EA 2005 4 27 QXEA200500619 120050327A5330 BUTT JOINT CNDAIRCL600 CL6002C10 1390015EA FUSELAGE LEAKING A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE EXTERIOR, HAS AREAS OF SUSPECT PRESSURE LEAKS ON BUTT JOINT FUSELAGE STATION 669, STRINGER 15R TO 15L. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-23-03-001-001-A01. 2L72 4F RTA21EA 20050427003972005042700397EA 2005 4 27 QXEA200500600 120050319A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE INTERIOR, RIGHTHAND INBOARD SEAT RAIL, AT STATION X417, HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01, REO 670-53-00-013 AND CRJ700 SRM 51-21-16, CODE A044. 2L72 4F RTA21EA 20050427003992005042700399EA 2005 4 27 QXEA200500609 120050317A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE INTERIOR, LEFTHAND INBOARD SEAT RAIL AT STATION X460 HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW REO 670-53-00-013 AND CRJ700 SRM 51-21-16, CODE A044. 2L72 4F RTA21EA 20050427004002005042700400EA 2005 4 27 QXEA200500599 120050324A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE INTERIOR, RIGHTHAND INBOARD SEAT RAIL AT STATION X350 TO X402, HAS MODERATE TO SEVERE PITTING CORROSION ON TOP AND INSIDE SURFACES. REMOVED AND REPLACED IAW CRJ700 SRM 51-41-02-001-001-A01 AND SRM 53-00-49-400-801-A02. 2L72 4F RTA21EA 20050427004032005042700403EA 2005 4 27 QXEA200500593 120050317A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE INTERIOR, RIGHTHAND OUTBOARD SEAT RAIL AT STATION X708 HAS PITTING CORROSION ON MOST INBOARD SURFACE. REPAIRED IAW CRJ700/900 SRM 51-21-06-001-0101-A01, PARAGRAPH 3E AND SRM 51-21-16, CODE A044. 2L72 4F RTA21EA 20050427004042005042700404EA 2005 4 27 QXEA200500595 120050317A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE INTERIOR, RIGHT HAND OUTBOARD SEAT RAIL AT STATION X739, HAS PITTING CORROSION ON MOST INBOARD SURFACE. REPAIRED IAW CRJ700/900 SRM 51-21-06-001-001-A01, PARAGRAPH A 3E AND CRJ700 SRM 51-21-16, CODE A044. 2L72 4F RTA21EA 20050427004052005042700405EA 2005 4 27 QXEA200500596 120050317A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE INTERIOR, RIGHTHAND OUTBOARD SEAT RAIL AT STATION 753, HAS PITTING CORROSION ON MOST INBOARD SURFACE. REPAIRED IAW CRJ700/900 SRM 51-21-06-001-001-A01, PARAGRAPH 3E AND CRJ700 SRM 51-21-16, CODE A044. 2L72 4F RTA21EA 20050427004072005042700407EA 2005 4 27 QXEA200500604 120050317A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE INTERIOR, RIGHTHAND INBOARD SEAT RAIL, AT STATION X523 HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW CRJ700/900 SRM 51-21-06-001-001-A01, PARAGRAPH 3E, REO 670-53-013 AND CRJ700 SRM 51-21-16, CODE A044. 2L72 4F RTA21EA 20050427004102005042700410NM 2005 4 27 QXEA200500643 120050408A2751 WARNING LIGHT BOMBDRDHC8 DHC8401 1390041NM COCKPIT ILLUMINATED A QXEAO OTHER J WARNING INDICATION APAPPROACH 1 NM09403QX 4037 BOI - FLAP POWER CAUTION LIGHT WHEN FLAPS SELECTED FOR APPROACH. COMPLIED WITH E&A CHECKLIST RESET PROCEDURE. FLAP POWER CAUTION EXTINGUISHED AND FLAPS OPERATED NORMAL FOR REMAINDER OF FLIGHT. MAINTENANCE COMPLIED WITH DH8-400-SL-27-002A, CAUTION CLEARED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050427004122005042700412EA 2005 4 27 QXEA200500563 120050321A2550 RAIL CNDAIRCL600 CL6002C10 1390015EA CARGO BAY DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FORWARD FUSELAGE, FORWARD CARGO COMPARTMENT, RETRIEVAL TRAY RAILS, CENTER AFT RAIL HAD ANODIZED COATING COMING OFF. REPAIRED IAW CRJ700 SRM 51-21-11-001-001-A01. 2L72 4F RTA21EA 20050427004152005042700415EA 2005 4 27 QXEA200500553 120050324A5753 SKIN CNDAIRCL600 CL6002C10 1390015EA T/E FLAP DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - LEFTHAND INBOARD FLAP LOWER SURFACE GRAVEL DAMAGED. REPAIRED IAW CRJ 700 SRM 51-25-01-001-A01. 2L72 4F RTA21EA 20050427004182005042700418NM 2005 4 27 QXEA200500668 120050412A5230 SKIN DHAV DHC8 DHC8202 2809007NM CARGO DOOR GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - CARGO DOOR INNER SKIN GOUGED AT SCREW HOLE UPPER AFT CORNER X591, Z151. REPAIRED IAW DHC-8 200 SRM 51-20-11, 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20050427004252005042700425EA 2005 4 27 QXEA200500635 120050319A5320 FLOOR SUPPORT CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE INTERIOR FLOOR SUPPORT CROSSBEAM AND FUSELAGE STATION 280 IS CORRODED ALONG UPPER FLANGE. REPAIRED IAW CRJ700 SRM 51-26-21-001-001-A01 AND REO 670-53-11-047. 2L72 4F RTA21EA 20050427004262005042700426EA 2005 4 27 QXEA200500613 120050317A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE INTERIOR, LEFTHAND INBOARD SEAT RAIL AT STATION X678 HAS PITTING CORROSION ON TOP SURFACE. REPAIRED IAW CRJ700/900 SRM 51-21-06-001-001-A01, PARAGRAPH 3E, REO 670-53-00-013 AND CRJ700 SRM 51-21-16, A044. 2L72 4F RTA21EA 20050427004272005042700427EA 2005 4 27 QXEA200500638 120050329A1430 FASTENER CNDAIRCL600 CL6002C10 1390015EA HORIZ STAB LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - HORIZONTAL STABILIZER CENTERING TRACK ALL ATTACHED FASTENERS LOOSE. REPAIRED IAW HORIZON AIR EA R-55-32A AND REO 670-55-31-004. 2L72 4F RTA21EA 20050427004282005042700428EA 2005 4 27 QXEA200500634 120050325A5350 STIFFENER CNDAIRCL600 CL6002C10 1390015EA FUSELAGE FAIRINGDAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - CENTER FUSELAGE, LOWER FAIRING PANEL, PANEL STIFFENER REQUIRES REWORK DUE TO CONTACT WITH FUSELAGE SKIN. REPAIRED IAW HORIZON AIR EA R-53-287 AND MOD SUM 1S67053820021, REV A-1. 2L72 4F RTA21EA 20050427004332005042700433EA 2005 4 27 QXEA200500564 120050319A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE INTERIOR, LEFTHAND OUTBOARD SEAT RAIL AT STATION X709 HAS PITTING CORROSION ON INSIDE AND MOST INBOARD SURFACES. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01 AND SRM 51-21-16. 2L72 4F RTA21EA 20050427004372005042700437EA 2005 4 27 QXEA200500566 120050326A5754 SLAT CNDAIRCL600 CL6002C10 1390015EA LT WING GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - LEFTHAND WING LEADING EDGE SLAT NR 1 TRAILING EDGE IS GOUGED AT SS60. REPAIRED IAW HORIZON AIR EA R-57-100 AND REO 690-57-42-001. 2L72 4F RTA21EA 20050427004382005042700438EA 2005 4 27 QXEA200500567 120050323A3222 CYLINDER CNDAIRCL600 CL6002C10 1390015EA NLG CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - CORROSION FOUND ON NOSE LANDING GEAR OUTER CYLINDER. REPAIRED IAW HORIZON AIR EA R-32-184 AND REO 670-32-21-0041. 2L72 4F RTA21EA 20050427004392005042700439EA 2005 4 27 QXEA200500627 120050324A5753 SKIN CNDAIRCL600 CL6002C10 1390015EA T/E FLAP DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - RIGHTHAND INBOARD FLAP LOWER SURFACE HAS GRAVEL DAMAGE. REPAIRED IAW CRJ700 SRM 51-26-00-001-001-A01, SRM 51-12-00-001-001-A01, SRM 51-25-01-001-001-A01 AND SRM 57-52-01-101-001-A01. 2L72 4F RTA21EA 20050427004402005042700440NM 2005 4 27 QXEA200500683 120050401A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09367PH 511 PDX - LEFTHAND INBOARD SEAT TRACK HAS CORROSION INSIDE CHANNEL AT STATION 541. REPAIRED IAW RD 8-53-3644. 2H72 4T RTA13NM 20050427004472005042700447EA 2005 4 27 QXEA200500602 120050317A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE INTERIOR, RIGHTHAND INBOARD SEAT RAIL AT STATION X448 HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW CRJ700/900 SRM 51-21-06-001-001-A01, PARAGRAPH 3E, REO 670-53-00-013 AND CRJ700 SRM 51-21-16, CODE A044. 2L72 4F RTA21EA 20050428000042005042800004EU 2005 4 28 05FDEA00530 120050315A5730 SKIN AIRBUS310 A310222 3930315EU LT WING MISREPAIRED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25451FE 303 COMPLY WITH AGING 9 - AGING INSPECTION, LT WING - REPAIRS (2) AT LT WING LWR SURFACE (ALL SPEED AILERON) PLEASE EVALUATE. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 57-61-12. 2L72 4F RTA35EU 20050428000052005042800005EU 2005 4 28 05FDEA00532 120050315A5753 SKIN AIRBUS310 A310222 3930315EU LT WING TE FLAP MISREPAIRED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25451FE 303 COMPLY WITH AGING 9 - AGING INSPECTION, LT WING - REPAIR AT LT INBOARD FLAP TRAILING EDGE, UPPER SURFACE (PLEASE EVALUATE). REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED IN ACCORDANCE WITH FEDEX ENGINEERING AUTHORIZATION 6- 5710-84099. 2L72 4F RTA35EU 20050428000082005042800008EU 2005 4 28 05FDEA00536 120050315A5350 FAIRING AIRBUS310 A310222 3930315EU TAIL CONE MISREPAIRED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25451FE 303 COMPLY WITH AGING 9 - AGING INSPECTION, REPAIR AT TAIL CONE EXHAUST AREA (PLEASE EVALUATE). REPLACED THIS FAIRING IAW AMM 52-41-18. 2L72 4F RTA35EU 20050428000092005042800009EU 2005 4 28 05FDEA00538 120050315A5100 REPAIR AIRBUS310 A310222 3930315EU PRECOOLER UNKNOWN A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25451FE 303 COMPLY WITH AGING 9 - AGING INSPECTION, NR 2 PYLON - FERRULE PRECOOLER AT AFTER SIDE OF UPPER SIDE WITH REPAIR (PLEASE EVALUATE). REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 54-51-11, CONFIG 2, FIG 201 AND 51-40-21. 2L72 4F RTA35EU 20050428000102005042800010EU 2005 4 28 05FDEA00540 120050315A5730 SKIN AIRBUS310 A310222 3930315EU RT WING MISREPAIRED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25451FE 303 COMPLY WITH AGING 9 - AGING INSPECTION, RT WING - REPAIR ON UPPER SKIN SURFACE BETWEEN TRAILING EDGE AND REAR SPAR AND BETWEEN RIB 2 AND TRACK 3. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED IN ACCORDANCE WITH FEDEX ENGINEERING AUTHORIZATION EA 6-5710-84101. 2L72 4F RTA35EU 20050428000112005042800011EU 2005 4 28 05FDEA00539 120050315A5730 SKIN AIRBUS310 A310222 3930315EU RT WING MISREPAIRED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25451FE 303 COMPLY WITH AGING 9 - AGING INSPECTION, RT WING - REPAIR ON LWR SKIN SURFACE BETWEEN FRONT SPAR AND MAIN, AND BETWEEN RIB 3 AND RIB 4. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 57-53-12. 2L72 4F RTA35EU 20050428000132005042800013NE 2005 4 28 UPS05M44132 220050317A7261 ENGINE DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE NR 1 LEAKING A IPXAEJA ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING KMJFLUID LOSS OVER TEMP WARNING INDICATION CRCRUISE 1 SO01252UP 48768 NR 1 ENGINE SHUTDOWN IN FLIGHT DUE TO LOW OIL QTY. ATB. ONE AUTO FUEL CHANNEL WLD NOT MAINTAIN FUEL BALANCE. SECOND AUTO FUEL CHANNEL MAINTAINED BALANCE. DUMPED FUEL T O MAINTAIN BALANCE. PERFORMED FSC R-T-S SYSTEM TEST PASSED ON GROUND. NO MSG AND FAULT FOU ND OK TO SERVICE. 2L73 4F4 FRTA22WE E13NE 20050428000152005042800015NM 2005 4 28 05FDEA00616 120050321A5310 SHEAR WEB BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 CORROSION ON SHEAR WEB WITH 100 PERCENT MATERIAL LOSS AT BS 1140-1145, LBL 57-62, WL 208. REPLACED SHEAR WEB PER SRM 51-40-2 2L73 4F RTA3WE 20050428000162005042800016NM 2005 4 28 05FDEA00617 120050321A5315BAC1518338 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 CORROSION SPOTS UNDER FLOORBEAM LOWER SURFACE AROUND NUT CLIP HOLES AT BS 1070 FROM LBL 42 TO RBL 21, WL 200 IN THE AFT CARGO BAY. BLENDED CORROSION ON LOWER SURFACE OF BS 1070 FLOORBEAM LOWER CHORD FROM RBL 21- LBL 42 WL 200, FOUND AREA RBL 21-LBL 4 TO BE WITHIN LIMITS PER SRM 53-10-1 FIG 4 AND AREA LBL 4.5- 42 TO BE OUT OF LIMITS PER SRM 53-10-1 FIG 4, REMOVED DAMAGED SECTION OF BS 1070 FLOORBEAM LBL 3-42 WL 200 FABRICATED REPAIR LWR CHORD FROM 60-3251, 7075T6511 EXT LOT 617089 AND INSTALLED REPAIR TO BS 1070 LWR CHORD FLOORBEAM RBL 3 - LBL 42 WL 200, ALL WORK ACCOMPLISHED PER FEDEX SR27-53-034E. 2L73 4F RTA3WE 20050428000192005042800019NM 2005 4 28 2005UALA00238 120050314A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29583UA 26705 AFT PIT STA 1440, STR 26L FRAME INBD FLANGE DENTED. FABRICATED AND INSTALLED NEW PRODUCTION SPLICE ANGLE EXTENDED TO ACCOMODATE REPAIR TO THE DAMAGED FRAME. 2L72 4F4 FRTA2NM E17NE 20050428000202005042800020NM 2005 4 28 2005UALA00239 120050314A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29583UA 26705 AFT PIT STA 1540, STR 27R, FRAME INBD FLANGE IS DENTED. FABRICATED AND INSTALLED NEW PRODUCTION SPLICE ANGLE EXTENDED TO ACCOMODATE REPAIR TO THE DAMAGED FRAME. 2L72 4F4 FRTA2NM E17NE 20050428000232005042800023NM 2005 4 28 05FDEA00630 120050323A5347S4929148 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 STA 939 TO 969 RT MOST OUTBOARD SEAT TRACK AREAS FOUND CHAFED MARKS. FABRICATED & REPAIRED AS PER SRM 53-70-00 FIG 1 VOL I. 2L73 4F RTA22WE 20050428000242005042800024NM 2005 4 28 05FDEA00632 120050324A5322 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25272FE 22037 CORROSION ON SHEAR TIE FWD SIDE AT BS 1030, JUST OB OF STR 28 LT, AFT CARGO BAY. REPAIRED PER SRM 53-10-4. 2L73 4F RTA3WE 20050428000262005042800026NM 2005 4 28 05FDEA00634 120050324A5320 INTERCOSTAL BOEING727 727227 1384078NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 WHILE WORKING BARRIER MOD FOUND STR 16 LT INTERCOSTAL CRACKED AT BS 354. REPAIRED PER SRM 51-40-3. 2L73 4F A3WE 20050428000292005042800029WP 2005 4 28 ARWA20050303 120050322A2130TA0603 RESISTOR DOUG DC8 DC863F 302198FWP CLIMATE CONTROL FAILED A ARWAJA DUMP FUEL UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO19906R 46087 ON TOP OF CLIMB, A BURNING ODOR & SMOKE APPEARED IN COCKPIT, REPEATEDLY PERFORMED APPROPRIATE CHECKLIST; PERFORMED FUEL DUMPING PER ABNORMAL CHECKLIST; PULLED CUR. C/B PER EMERGENCY CHECKLIST. SMOKE SOURCE IDENTIFIED AT LOW BLOW FAN RESISTOR "COCKPIT CLIMATE CONTROL"; REMOVED & WIRING STOWED HI-BLOW; OPS NORMAL IAW TECH AIR MM ON STC NR ST145CH, SEE 4-M LOW BLOW; INSPECTED FUEL DUMP SYSTEM AND DUMP CHUTES AND RETRACTED AND SAFETY IAW MM 28-38-00; RESET C/B SYS, OPS NORMAL IAW MM 23-70-0; ENTERED ON DMI NR 19078 AS PER MEL 21-61-C CAT C . R & R CLIMATE CONTROL LOW SENSOR; SYS GROUND TEST NORMAL IAW MM STC ST14SCH. THIS CLEAR DMI 19078. 2L74 4F 4A25 20050428000302005042800030NM 2005 4 28 F3LA200500015 120050327A534469203212 HINGE FITTING BOEING737 7373S1 138447SNM R1 DOOR CRACKED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03311FL 3157 24856 INSPECTION REPORTED R1 DOOR UPPER HINGE ARM FITTING CRACKED. DOOR FRAME CRACKED AT HINE ARM CUTOUT. REPLACED R1 DOOR UPPER HINGE CASTING PER SRM 51-40-02 AND 51-10-02 2L72 4F RTA16WE 20050607001512005060700151EA 2005 6 7 QXEA200500935 120050503A7830 PLATE CNDAIRCL600 CL6002C10 1390015EA ZONE 400 WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - RIGHT ENGINE UPPER AND LOWER TRANS COWL STOWED RAMPS AND TORQUE BOX STOW RAMP STRIKE PLATES ARE WORN. REPAIRED IAW REO 670-78-33-333. 2L72 4F RTA21EA 20050607001522005060700152EA 2005 6 7 QXEA200500936 120050509A3213 STRUT CNDAIRCL600 CL6002C10 1390015EA ZONE 700 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - NOSE LANDING GEAR PISTON ASSEMBLY HAS SEVERAL SCRATCHES AFT FACE OF CHROME. REPAIRED IAW HORIZON AIR EA R-32-188 AND REO 670-32-21-0051. 2L72 4F RTA21EA 20050428000462005042800046NM 2005 4 28 05FDEA00892 120050407A5514 STRUCTURE DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 STABILIZERS - HORIZONTAL STABILIZER BARREL NUT BORES, CORROSION REMOVAL, COMPLY WITH EA 1-5510-71839. COMPLIED WITH EA 1-5510-71839. 2L73 4F RTA22WE 20050428000502005042800050NM 2005 4 28 05FDEA00896 120050408A5315FX7532155461 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25204FE 22926 COMPLY WITH EA 7-5321-55461 FUSELAGE - FLOORBEAM LOWER CHORD REPAIR, STA 720 AT RBL 13.0. COMPLIED WITH EA 7-5321-55461. 2L73 4F RTA3WE 20050428000512005042800051NM 2005 4 28 05FDEA00897 120050408A5514 STRUCTURE DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 RT HORIZONTAL STABILIZER UPPER BARREL NUT NR 11 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133. 2L73 4F RTA22WE 20050428000522005042800052NM 2005 4 28 05FDEA00898 120050408A5514 STRUCTURE DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 RT HORIZONTAL STABILIZER UPPER BARREL NUT NR 13 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133. 2L73 4F RTA22WE 20050428000532005042800053NM 2005 4 28 05FDEA00899 120050408A5514 STRUCTURE DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 RT HORIZONTAL STABILIZER UPPER BARREL NUT NR 17 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133. 2L73 4F RTA22WE 20050428000542005042800054NM 2005 4 28 05FDEA00900 120050408A5514 STRUCTURE DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 RT HORIZONTAL STABILIZER UPPER BARREL NUT NR 19 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133. 2L73 4F RTA22WE 20050428000562005042800056NM 2005 4 28 05FDEA00902 120050408A2710 STUD DOUG MD11 MD11 3023602NM RT AILERON CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 RIGHT WING O/B AILERON ACTUATOR MOUNTING UPPER O/B STUD FOUND CORRODED. REMOVED AND REPLACED ON THE RT WING O/B AILERON ACTUATOR MOUNTING UPPER O/B STUD AS PER MM 20-50-02. 2L73 4F RTA22WE 20050428000572005042800057NM 2005 4 28 05FDEA00903 120050408A2710 STUD DOUG MD11 MD11 3023602NM RT AILERON CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 RIGHT WING O/B AILERON ACTUATOR MOUNTING LWR I/B & O/B MOUNTING STUDS FOUND CORRODED. RT WING O/B AILERON ACTUATOR MOUNTING LWR I/B & O/B MOUNTING STUDS REMOVED AND REPLACED STUDS AS PER MM20-50-02. 2L73 4F RTA22WE 20050428000592005042800059NM 2005 4 28 05FDEA00905 120050408A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 RIGHT WING O/B FLAP MOUNTED HINGE PIVOT HOLE EVIDENT OF CORROSION. CORROSION REMOVED AS PER CMM 20-11-00. 2L73 4F RTA22WE 20050428000602005042800060NM 2005 4 28 05FDEA00906 120050408A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 LEFT WING O/B FLAP, I/B FLAP MOUNTED HINGE ACTUATOR HOLE EVIDENT OF CORROSION. REMOVAL & REPAIR. REFER TO EO E1-5750-7-5002 CI. PT 1. 2L73 4F RTA22WE 20050428000652005042800065NM 2005 4 28 05FDEA00911 120050408A5514 STRUCTURE DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT HAND UPPER AFT SKIN PLANK NR 34L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82941. 2L73 4F RTA22WE 20050428000702005042800070SO 2005 4 28 CHQA200500076 120050407A2770 WARNING SYSTEM EMB 135 EMB135KL 3260302SO COCKPIT FALSE INDICATIONA CHQAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL11295SK 145513 WHILE CRUISING AT FL350 BOTH AMBER GUST LOCK WARNING LIGHTS ILLUMINATED. THE QRH PROCEDURES WERE RUN, WHICH AT THE END STATED TO LAND AT THE NEAREST SUITABLE AIRPORT. DISPATCH AND MAINTENANCE CONTROL WERE CONTACTED ABOUT THE PROBLEM AND ADVISED THEM ABOUT THE DIVERT TO IND. AN UNEVENTFUL APPROACH AND LANDING AT IND WAS COMPLETED. IN ADDITION TO WRITING UP THE GUST LOCK PROBLEM, THE OVERWEIGHT LANDING WAS ALSO WRITTEN UP. MAINTENANCE PERFORMED OPERATIONAL CHECK OF ELECTROMECHANICAL GUST LOCK SYSTEM. OPS CHECK GOOD IAW EMB 140 MM 77-71-00-2. 2L72 4F RTT00011AT 20050428000742005042800074SO 2005 4 28 MASA200500250 120050323A2750 FLAP EMB 145 EMB145LR 3260212SO WING MALFUNCTIONED A MASAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 SW07837MJ 145367 A FLAP FAIL ON APPROACH. CONTRACT MAINTENANCE WAS ABLE TO RESET AND PERFORM OPERATIONAL TEST OF FLAP SYSTEM WITH NO DEFECTS NOTED. 2L72 4T RTT00011AT 20050428000802005042800080NM 2005 4 28 72300150 120050408A5320 FITTING BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 1 INCH AREA OF CORROSION ON STRINGER END FITTING. 2L73 4F4 FRTA3WE E2EA 20050428000822005042800082NM 2005 4 28 72300152 120050408A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CRACKED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A .5 INCH CRACK COMING FROM HOLE TO OUTER EDGE OF STRINGER FLANGE. 2L73 4F4 FRTA3WE E2EA 20050428000842005042800084NM 2005 4 28 72300154 120050408A5311 FRAME BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 4 X 1 INCH AREA OF CORROSION ON FRAME WEB. 2L73 4F4 FRTA3WE E2EA 20050428000852005042800085NM 2005 4 28 05FDEA00641 120050325A5322 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 REPAIR SHEAR TIE BS 380 BETWEEN STR 14L & 15L TO ACCOMPLISH 9G MOD. REPAIRED SHEAR TIE AT BS 380 BETWEEN STR 14L & 15L PER SRM 53-10-4. 2L73 4F RTA3WE 20050428000872005042800087NM 2005 4 28 05FDEA00643 120050325A575365192497 FLAP TRACK BOEING727 727200 138407ENM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 NR 3 FLAP TRACK AFT MOUNTING PAD CORRODED. REPLACED NR 3 FLAP TRACK PER FED EX W/C 27X5705-03. 2L73 4F RTA3WE 20050428000892005042800089NM 2005 4 28 05FDEA00646 120050326A5240NAA605663 DOOR DOUG MD11 MD11 3023602NM ZONE 100 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25592FE 48550 FUSELAGE CAC DOOR UNABLE TO OPEN AFTER CABIN PRESSURIZATION TEST. CAC DOOR REPLACED AS PER AMM 52-43-01-4. ADJUSTMENT, TEST ON CAC DOOR CARRIED OUT AS PER AMM 52-43-01-5. 2L73 4F RTA22WE 20050428000922005042800092EA 2005 4 28 SWIA200514842 120050407A2740 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA COCKPIT STICKS A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07905SW 7437 TRIM SWITCH ON PILOT SIDE STICKS. REPLACED THE CAPTAIN'S SIDE STAB TRIM SWITCH. OPERATIONAL CHECK GOOD IAW MM 27-41-00. 2L72 4F RTA21EA 20050428000932005042800093SO 2005 4 28 SWIA200514843 120050406A3350 LIGHT EMB 120 EMB120ER 3260203SO CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07218SW 120287 AFT OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LAMP. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050428000942005042800094NM 2005 4 28 05FDEA00715 120050330A3210AYG72331 BLOCK DOUG MD11 MD11 3023602NM ZONE 700 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 CENTER LANDING GEAR, LEFT HAND AND RIGHT HAND PILLOW BLOCKS, FOUND EMITTED WITH RUST. LEFT HAND AND RIGHT HAND PILLOW BLOCKS REMOVED AND REPLACED PER CMM 32-15-01. CENTER LANDING GEAR ASSEMBLY REINSTALLED PER WIC 32T9004. 2L73 4F RTA22WE 20050428000952005042800095EA 2005 4 28 SWIA200514844 120050405A2611 SMOKE WARNING CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A SWIAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 NM07935SW 7725 CARGO SMOKE MESSAGE ON PUSHBACK. INSPECTED CARGO COMPARTMENT. NO DEFECTS NOTED. PERFORMED ENGINE RUNS WITH CREW. NO DEFECTS NOTED. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050428000972005042800097NM 2005 4 28 SB05042 120050330A335020131A BATTERY PACK BOEING737 7373B7 1384580NM EMERGENCY LIGHT FAULTY A USAAK NONE O OTHER ININSP/MAINT 1 EA19393US 23315 MAINTENANCE REPORTED THE EMERGENCY LIGHTS IN THE AFT CABIN WOULD NOT TURN OFF. MAINTENANCE REMOVED AND REPLACED THE AFT CABIN EMERGENCY LIGHT BATTERY PACKS. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050428000992005042800099EA 2005 4 28 SWIA200514845 120050405A335020131A BATTERY PACK CNDAIRCL600 CL6002C10 1390015EA CABIN DISCHARGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07705SK3979 3979 10145 NR 4 OVERHEAD EMERGENCY LIGHT POD AND SIGN ON OVERWING EXIT WILL NOT ILLUMINATE. REPLACED NR 2 OVERHEAD BATTERY PACK IAW MM 33-60-00. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050428001012005042800101EU 2005 4 28 05FDEA00764 120050331A5347 ADAPTER AIRBUS310 A310 EU FUSELAGE BROKEN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 CLS ADAPTER AT FS 74 TRACK L4 HAS BROKEN CLEVIS. REMOVED AND REPLACED CLS ADAPTER IAW A310-200 SRM 51-72-10. 2L72 4F RTA35EU 20050428001022005042800102NM 2005 4 28 AWXA200500435 120050318A53206546572515 STIFFENER BOEING737 737375 13844BNNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 MCN - MAJOR REPAIR - DURING C-05 CHECK CORROSION WAS FOUND ON VERTICAL STIFFENER AT FORWARD FACE OF BULKHEAD AT BS 1088, RBL 23, BETWEEN WL 210-220. MAINTENANCE REMOVED CORRODED VERTICAL STIFFENER AT FORWARD FACE OF BULKHEAD BS 1088, RBL 23, FROM WL 210 TO WL 220; FABRICATED A NEW REPLACEMENT STIFFENER PER DWG 65-46572; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050428001042005042800104NM 2005 4 28 AWXA200500436 120050314A53206546572545 STRAP BOEING737 737375 13844BNNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 MCN - MAJOR REPAIR - DURING C-05 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT TAIL COMPARTMENT LOWER STRAP AT BS 1088, BETWEEN STR 19 RT AND STR 20 RT. MAINTENANCE REMOVED CORRODED STRAP AT BS 1088, FROM STR 19 RT TO STR 20 RT; FABRICATED A NEW REPLACEMENT STRAP PER DWG 65-46572; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050428001052005042800105NM 2005 4 28 AWXA200500437 120050330A53226546579514 CLIP BOEING737 737375 13844BNNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 MCN - MAJOR REPAIR - DURING C-05 CHECK CORROSION WAS FOUND ON LOWER ATTACH CLIP AT BS 1129, BETWEEN STR 15 RT AND STR 16 RT. MAINTENANCE REMOVED CORRODED LOWER ATTACH CLIP AT BS 1129, BETWEEN STR 15 RT AND STR 16 RT; ORDERED & RECEIVED A NEW REPLACEMENT CLIP; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050428001062005042800106NM 2005 4 28 AWXA200500438 120050330A53226546579508 CLIP BOEING737 737375 13844BNNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 MCN - MAJOR REPAIR - DURING C-05 CHECK CORROSION WAS FOUND ON LOWER ATTACH CLIP AT BS 1105, BETWEEN STR 15 RT AND STR 16 RT. MAINTENANCE REMOVED CORRODED ATTACH CLIP AT BS 1105, BETWEEN STR 15 RT AND STR 16 RT; FABRICATED A NEW REPLACEMENT CLIP PER DWG 65-46579; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050428001072005042800107NM 2005 4 28 AWXA200500439 120050330A53226546579575 CLIP BOEING737 737375 13844BNNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 MCN - MAJOR REPAIR - DURING C-05 CHECK CORROSION WAS FOUND ON UPPER ATTACH CLIP AT BS 1129, BETWEEN STR 15 RT AND STR 16 RT. MAINTENANCE REMOVED CORRODED UPPER ATTACH CLIP AT BS 1129, BETWEEN STR 15 RT AND STR 16 RT; ORDERED & RECEIVED A NEW REPLACEMENT CLIP; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050428001082005042800108NM 2005 4 28 AWXA200500440 120050313A534065465648 SHEAR TIE BOEING737 737375 13844BNNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 MCN - MAJOR REPAIR - DURING C-05 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT LOWER FUSELAGE FRAME SHEAR TIE AT BS 986.5, STR 25 RT. MAINTENANCE REMOVED CORRODED SHEAR TIE AT BS 986.5, STR 25 RT; FABRICATED A NEW REPLACEMENT SHEAR TIE PER DWG 65-46564; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050428001092005042800109NM 2005 4 28 AWXA200500441 120050313A53206520726505 SILL BOEING737 737375 13844BNNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 MCN - MAJOR REPAIR - DURING C-05 CHECK CORROSION WAS FOUND ON LOWER SURFACE OF FORWARD CARGO DOOR LOWER SILL WEB BETWEEN BS 447 AND BS 488, AT RBL 28. MAINTENANCE REMOVED CORRODED FORWARD CARGO DOOR LOWER SILL WEB FROM BS 447 TO BS 488, AT RBL 28; FABRICATED A NEW REPLACEMENT SILL WEB PER DWG 65-20726; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050428001102005042800110NM 2005 4 28 AWXA200500442 120050406A335020131A BATTERY PACK BOEING737 737375 13844BNNM CABIN DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 MCN - EEL - DURING C-05 CHECK FUNCTIONAL TEST OF EMERGENCY LIGHT SYSTEM THE LT FORWARD ENTRYWAY EMERGENCY LIGHT BATTERY PACK WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT FORWARD ENTRYWAY EMERGENCY LIGHT BATTERY PACK, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050428001112005042800111NM 2005 4 28 AWXA200500443 120050324A33503404302 CONNECTOR BOEING737 737375 13844BNNM CABIN BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 MCN - EEL - DURING C-05 CHECK FOUND EMERGENCY ESCAPE PATH LIGHT HOOK-UPS DAMAGED THROUGHOUT CABIN ON BOTH THE HARNESS AND AIRCRAFT SIDE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT HOOK-UPS, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050428001172005042800117NM 2005 4 28 05FDEA00808 120050404A5720ARB293347 SUPPORT DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 LEFT WING, FIXED LEADING EDGE ACCESS PANEL FORWARD SUPPORT AT STA XOR 450 FOUND CRACKED. REMOVED CRACKED SUPPORT AS PER SRM 51-31-01 VOLUME II AND FABRICATED NEW SUPPORT DOUBLER AS PER DRAWING ARB2933. INSTALLED NEW SUPPORT DOUBLER AT LEFT WING FIXED LEADING EDGE ACCESS PANEL FORWARD AT STA XOR 450 AS PER SRM 51-35-01 VOLUME II AND SRM 51-33-01 VOLUME II. 2L73 4F RTA22WE 20050428001192005042800119NM 2005 4 28 05FDEA00810 120050404A5720ARB293348 SUPPORT DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 RIGHT WING FIXED LEADING EDGE ACCESS PANEL FORWARD SUPPORT AT STA XOR 450 FOUND CRACKED. REMOVED CRACKED SUPPORT AS PER SRM 51-31-01 VOLUME II AND FABRICATED NEW SUPPORT DOUBLER AS PER DRAWING ARB2933. INSTALLED NEW SUPPORT DOUBLER AT RIGHT WING FIXED LEADING EDGE ACCESS PANEL FORWARD AT STA XOR 450 AS PER SRM 51-35-01 VOLUME II AND SRM 51-33-01 VOLUME II. 2L73 4F RTA22WE 20050428001202005042800120NE 2005 4 28 DLM88050174 220050319A7200JT8D219 ENGINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 LEAKING A DALAA UNSCHED LANDING KBJFLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SO27920DL40080 49644 725416 ON CLIMB JUST AFTER TAKEOFF BOTH AFT LAV SMOKE DETECTORS SOUNDED FOLLOWED BY VISIBLE SMOKE IN THE CABIN. REPLACED RT ENGINE FOR INTERNAL OIL LEAKAGE. 2L72 4F4 FRTA6WE E9NE 20050428001212005042800121NM 2005 4 28 DL738050175 120050320A2120 SMOKE BOEING737 737832 13844CFNM CFMINTCFM56 CFM562AFR 13802EU COCKPIT DETECTED A DALAC ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SO273750D 32375 P5982 REJECTED TAKEOFF AT 125 KTS WITH SMOKE IN COCKPIT. USED APU FOR NO BLEED TAKEOFF AND LEFT PACK. PERFORMED DUCT BURN OUT FROM GROUND AIR CONNECTION FOR APU AND ENGINES. RAN PACKS NO EVIDENCE OF ELECTRICAL OR GLYCOL SMELL. 2L72 4F4 FRTA16WE E21EU 20050428001222005042800122EU 2005 4 28 DHL2005367500 120050325A55405547067020692 FITTING AIRBUS300 A300B4203 3930306EU RUDDER CRACKED A DHLAO OTHER O OTHER ININSP/MAINT 1 SO01367DH 444 265 DURING "C" CHECK INSPECTION, RUDDER HINGE AND HYDRAULIC ACTUATOR FITTING ATTACHMENT TO RUDDER AT RIB 19 (UPPER ACTUATOR ) AREA CRACKED (MKD). 2L72 4F RTA35EU 20050428001232005042800123NM 2005 4 28 DLM88050176 120050320A2421976J2528 GENERATOR DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 1 ENGINE FAILED A DALAA UNSCHED LANDING O OTHER CLCLIMB 1 SO27950DL 49881 725534 ON DEPARTURE FROM DCA LEFT GENERATOR FAILED WITH NO VOLTS OR FREQS CAUSING CROSSTIE LOCKOUT. REPLACED LEFT CSD AND GENERATOR. 2L72 4F4 FRTA6WE E9NE 20050428001242005042800124NM 2005 4 28 DLM88050177 120050320A2740R2014 RELAY DOUG MD88 MD88 3023688NM TRIM SYSTEM FAILED A DALAA UNSCHED LANDING F FLT CONT AFFECTED TOTAKEOFF 1 SO27982DL 53273 AFTER T/O HIGH SPEED TRIM MOTORS WOULD NOT WORK ON BOTH YOKES, ALSO SLOW SPEED TRIM INTERMITTENT. AUTO-PILOT TRIM ALSO WOULD NOT WORK. REPLACED BRAKE RELAY. 2L72 4F RTA6WE 20050428001252005042800125NM 2005 4 28 DL76G050178 120050320A2750271003372 PSEU BOEING767 7673P6 1385105NM E/E BAY FAILED A DALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO27153DL 24985 AT APPROX 96 KNOTS CREW RECEIVED T/O CONFIG WARNING MESSAGE T/O WAS ABORTED A/C RETURNED TO GATE FOR REPAIRS. REPLACED PSEU M162 WAS AND FSPM M839. 2L72 4F RTA1NM 20050429000032005042900003NM 2005 4 29 05FDEA00864 120050406A5347AEA732515 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA 1179 TO 1239, WL 75 FOUND WITH CORROSION AEA7325-15. 2L73 4F RTA22WE 20050429000052005042900005CE 2005 4 29 DXTA200500654 120050331A2120 ODOR CESSNA500 560CESSNA 2076750CE CABIN/COCKPIT DETECTED E DXTAC ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 GL07345QS 5600445 UPON TAKEOFF ROLL RANCID BURNING OIL SMELL WAS EMITTING FROM GASPERS & VENTS. 2L72 4F RTA22CE 20050429000062005042900006CE 2005 4 29 DXTA200500661 120050404A5514 STRUCTURE CESSNA500 560CESSNA 2076750CE HORIZONTAL STAB BIRD STRIKE E DXTAC ABORTED TAKEOFF C F.O.D. TOTAKEOFF 1 GL07340QS 5600514 BIRD STRIKE ON TAKEOFF. DAMAGE TO RIGHT HORIZONTAL STAB APPROX 8 INCHES WIDE & 2 INCHES DEEP. 2L72 4F RTA22CE 20050429000082005042900008NM 2005 4 29 05FDEA00872 120050406A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CROWN LIGHTNING STRIKEA FDEAK NONE O OTHER ININSP/MAINT 1 SO25272FE 22037 LIGHTNING STRIKE ON CROWN BS 588 BETWEEN STR 1 AND STR 2L. FOUND TO BE OUT OF LIMITS. REPAIRED SKIN IAW FED EX EA 7-5330-866368. 2L73 4F RTA3WE 20050429000092005042900009NM 2005 4 29 05FDEA00874 120050406A5343AEA7051 FITTING DOUG MD11 MD11 3023602NM ZONE 700 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 CENTER LANDING GEAR, LEFT HAND TRUNNION SUPPORT FITTING SHEAR PIN HOLES FOUND CORRODED. REPAIR CARRIEDOUT AS PER FEDEX EA 1-5340-82950. 2L73 4F RTA22WE 20050429000102005042900010NM 2005 4 29 05FDEA00875 120050406A5343AEA7051 FITTING DOUG MD11 MD11 3023602NM ZONE 700 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 CENTER LANDING GEAR, RIGHT HAND TRUNNION SUPPORT FITTING SHEAR PIN HOLES FOUND CORRODED. REPAIR CARRIED OUT AS PER FEDEX EA 1-5340-82950. 2L73 4F RTA22WE 20050502000032005050200003EU 2005 5 2 05FDEA00754 120050331A5313 STRINGER AIRBUS310 A310 EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 AREA BEHIND BULK CARGO AT FRAME 72 LEFT SIDE APPROX STR 41L, STRINGER HAS 5 SQ INCHES OF CORROSION. REMOVED CORROSION, AREA OUT OF LIMITS, REMOVED DAMAGED STRINGER SECTION AND REPLACED WITH NEW SECTION PER A310-200 SRM 51-74-10 AND 53-10-14. 2L72 4F RTA35EU 20050502000042005050200004EU 2005 5 2 05FDEA00755 120050331A5315 FLOORBEAM AIRBUS310 A310 EU FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 FLOORBEAM IS CRACKED 66 INCH RIGHT OF CENTER LINE AT FRAME 54.3 UNDER CEILING PANEL 152BC IN AFT CARGO, (PANEL NOT REMOVED FOR C-CHECK). REMOVED FLOOR PANEL 252DF AND CEILING PANEL 152BC FOR ACCESS IAW A310-200 SRM 51- 40-21. CUT OUT DAMAGED AREA, FABRICATED REPAIR ANGLES AND INSTALLED ANGLES ON AIRCRAFT IAW A310-200 SRM 53-10-15 FIG 201. REINSTALLED FLOOR AND CEILING PANELS IAW A310-200 SRM 51-40-21 AND AMM 53-10-25-4. 2L72 4F RTA35EU 20050502000072005050200007EU 2005 5 2 05FDEA00758 120050331A5313 STRINGER AIRBUS310 A310 EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 CORROSION ALONG STRINGER 52L BETWEEN FRAMES 60 AND 61, AFT CARGO UNDER FLOOR. REMOVED CORROSION IAW A310-200 SRM 51-74-10. MATERIAL THICKNESS AFTER WENT OUT OF LIMITS IAW A310-200 SRM 51-10-04. CUT AND SPLICED STRINGER 52L AT FRAMES 60 AND 61 IAW A310-200 SRM 53-10-14. RESTORED PROTECTIVE COATING IAW A310-200 SRM 51-21-10. 2L72 4F RTA35EU 20050502000092005050200009EU 2005 5 2 05FDEA00760 120050331A5313 STRINGER AIRBUS310 A310 EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 AFT CARGO COMPT, AFT OF FS 54 ON R-STRINGER 51 HAS AREA OF CORROSION. REMOVED STRINGER END FITTING AT FS 54 ON STRINGER 51R IAW A310-200 SRM 51-74-21. REMOVED CORROSION FROM STRINGER 51 AFT OF FS 54 IAW A310-200 SRM 51-74-10. VERIFIED ALLOWABLE LIMITS AND MATERIAL LOSS IAW A310-200 SRM 53-10-00 AND FOUND TO BE OUT OF LIMITS. FABRICATED NEW SPLICE ANGLE AND STRINGER SECTION IAW A310-200 SRM 53-10-14. INSTALLED END FITTING, SPLICE ANGLE AND NEW STRINGER 51 SECTION IAW A310-200 SRM 51-40-21 AND 53-10-14. 2L72 4F RTA35EU 20050502000102005050200010EU 2005 5 2 05FDEA00761 120050331A7110 ANGLE AIRBUS310 A310 EU THRUST REVERSER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 NR 1 ENGINE OUTBD T/R COWL LOWER FWD CORNER ANGLE IS CRACKED. REMOVED RIVETS IAW A310-200 SRM 51-40-21. CUTOUT CRACKED FLANGE IAW ROHR CF6-80A SRM 54-05-02. VERIFIED REPAIR FILLER AND ANGLE IAW ROHR CF6-80A SRM 54-05-02. FABBED FILLER AND REPAIR IAW ROHR CF6-80A SRM 54-05-02. APPLIED PROTECTIVE COATING IAW A310-200 SRM 51-21-10. INSTALLED REPAIR ANGLE AND FILLER IAW ROHR CF6-80A SRM 54-05-02 FIG 1. 2L72 4F RTA35EU 20050502000142005050200014NM 2005 5 2 QXEA200500527 120050331A2611 SMOKE WARNING DHAV DHC8 DHC8202 2809007NM COCKPIT FALSE ACTIVATIONA QXEAK NONE N FALSE WARNING APAPPROACH 1 NM09360PH6505 3959 515 PSC - ON FLIGHT NUMBER 2096, SMOKE WARNING AND MASTER WARNING ILLUMINATED INTERMITTENTLY. NO AUDIBLE OR VISUAL INDICATION AND NO SMOKE NOTICED. MAINTENANCE INSPECTED AND FOUND NO EVIDENCE OF SMOKE, C/W OPERATIONAL TEST OF BAGGAGE COMPARTMENT SMOKE DETECTION SYSTEM. OPERATIONAL TESTS GOOD. REMOVED AND REPLACED SMOKE DETECTOR AS PRECAUTIONARY MEASURES. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050502000152005050200015NM 2005 5 2 QXEA200500526 120050330A2910 HYDRAULIC LINE DHAV DHC8 DHC8202 2809007NM HYDRAULIC SYS LEAKING A QXEAK NONE KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM09354PH 498 YKM-ON FLIGHT NUMBER 2002, AFTER LANDING AND PARKING NOTICED A STRANGE ODOR AND BOTH PILOTS STARTED COUGHING, COULD SEE MIST/SMOKE IN THE COCKPIT. AFTER SHUTDOWN NOTICED FLUID LEAKING FROM BELLY OF AIRCRAFT UNDER COCKPIT. MAINTENANCE INSPECTED AND FOUND HYDRAULIC LINE LEAK UNDER LAV. REPAIRED THE GEAR DOWN HYDRAULIC LINE USING CORROSION RESISTANT STEEL TUBING. SERVICE AND BLEED SYSTEM. GROUND RAN ENGINES. NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050502000162005050200016NM 2005 5 2 ANCF200400044 120050329A3241 CONNECTOR BOEING767 7673Y0 NM ANTI-SKID SYS DAMAGED W ANCFA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO23948AV 24948 EICAS MSG NORM ANTI-SKID ALTN ANTI-SKID DISPLAYED AND AMBER ANTI-SKID LIGHT ILLUM AFTER LIFTOFF. AS PER A-M-M 32-42-01 PAGE 406 WAS PERFORMED PROCEDURE BITE ANTI-SKID SYSTEM CHANNEL 7 SHOWING FAIL AS PER MEL 32-42-1-1 CAT C DMI NBR 37.IT WAS ACCOMPLISHED PROCEDURE MEL A/P 2591772 AS PER WDM 32-42-02 PAGE 101 SHEET THE LINE IN CONNECTOR D2024 WAS REPAIRED TEST OK. 2L72 4F RTA1NM 20050502000232005050200023NM 2005 5 2 DHL2005782516 120050310A5330 SKIN BOEING727 727227 1384078NM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 CREASE LT SIDE FUSELAGE SKIN STA 1148 STR 26L. REMOVED INTERCOSTAL IAW B727 SRM 51-30-2. CUT OUT DAMAGED AREA SIZE 2 INCHES BY 1 9/16 INCH IAW B727 SRM 53-30-3 FIG 24. FABBED FILLER SIZE 2 INCHES BY 1 9/16 INCH USING 2024T3 .100 PO NR 9001576 STRUCTURE FILLER USING 2024T3 .063 PO NR 9002039 SIZE 13 1/2 INCH BY 7 3/4 INCH DOUBLER 11 1/8 INCH BY 11 5/8 INCH USING 2024 T3 .125 PO# 9001673 IAW B727 SRM 53-30-3 FIG 24. TREATED AND PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED INTERCOSTAL IAW B727 53-30-3 FIG 24. THIS REPAIR IS A CAT B. 2L73 4F A3WE 20050502000252005050200025NM 2005 5 2 DHL2005782519 120050310A5330 SKIN BOEING727 727227 1384078NM FUSELAGE BULGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 BULGE UNDERNEATH FUSELAGE SKIN FWD OF STA 1050 STR 29R. DAMAGE FOUND TO BE OUT OF LIMITS IAW 727 SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREAS DIM 3 3/4 INCH BY 1 7/8 INCH AT BS 1040 STR 29R AND 3 1/8 INCH BY 3 3/4 INCH ATBS 1040 STR 29L. FABBED 2 FILLERS FROM 2024T3 .071 PO NR 9001978 DIM 3 1/2 INCH BY 1 INCH AND 3 3/4 INCH BY 1 INCH AND DOUBLER FROM 2024T3 .080PO NR 9002012 DIM 21 5/8 INCH BY 18 3/4 INCH IAW 727 SRM 53-30-3 FIG3 AND 53-30-2 FIG2. REPAIR PARTS TREATED, PRIMED AND INSTALLED IAW 727 SRM 51-10-2 AND 53-30-3 FIG 3. 2L73 4F A3WE 20050502000262005050200026NM 2005 5 2 DHL2005782520 120050310A5754 SKIN BOEING727 727227 1384078NM L/E SLAT DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 NR 2 SLAT EXTERNAL SKIN DENTED (3) PLACES. MEASURED DENT AT WS 656.3 ON NR 2 SLAT AND FOUND IN LIMITS A.2/Y.005=40 IAW SRM 53-30-1 FIG 1. MEASURED DENT AT WS 684.3 ON NR 2 SLAT AND FOUND TO BE OUT OF LIMITS A.4/Y.32=28.1 IAW B727 SRM 53-30-1 FIG 1 AND REPAIRED ON NR 82240. MEASURED DENT AT WS 661.3 ON NR 2 SLAT AND FOUND TO BE OUT OF LIMITS A.6/Y.028=21.4 IAW B727 SRM 53-30-1 FIG1. CUT OUT DAMAGED AREA AT WS 661.3 ON NR 2 SLAT SIZE 1 INCH BY 3/4 INCH IAW B727 SRM 57-50-3. FABBED NEW DOUBLER USING 2024T3 .080 PO#9002012 SIZE 4 1/2 INCH BY 4 1/2 INCH IAW B727 SRM 57-50-3 FIG 1. TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED DOUBLER IAW B727 SRM 57-50-3. 2L73 4F A3WE 20050502000322005050200032 2005 5 2 RYNA200500010 420050402A2210 AUTOPILOT SYS BOEING737 737201 1384454NM COCKPIT MALFUNCTIONED A RYNAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 CE07225US 21667 IMMEDIATELY AFTER TAKEOFF FROM TUS, THE AUTOPILOT PORPOISED IN PITCH. THE AIRCRAFT WAS RETURNED TO TUS AND LANDED WITHOUT INCIDENT. AMENDMENT TO BE FILED UPON COMPLETION OF TROUBLESHOOTING AND CORRECTIVE ACTION. 2L72 4F A16WE 20050502000352005050200035NM 2005 5 2 SWAA051038 120050408A256065C16820 HOOK BOEING737 7373H4 1384600NM L1 DOOR SHEARED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29369SW 26580 DURING SCHEDULED RON CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK SHEARED OFF. RE-INSTALLED HOOK PER MM. 2L72 4F RTA16WE 20050502000372005050200037NM 2005 5 2 SWAA051040 120050408A3350BR2013 LENS BOEING737 7377H4 1384404NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29406WN 27894 EEPLS TRACK LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20050502000392005050200039NM 2005 5 2 SWAA051042 120050411A3350101331 LENS BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29322SW 23343 LT OVERWING EMERGENCY EXIT SIGN LENS LOOSE. SECURED LENS PER MM. 2L72 4F RTA16WE 20050502000412005050200041NM 2005 5 2 SWAA051044 120050411A33506104789 BATTERY PACK BOEING737 7373H4 1384600NM CABIN DISCHARGED A SWAAK NONE O OTHER TXTAXI/GRND HDL 1 SW29332SW 23696 L2 & R2 DOOR EMERGENCY EXIT SIDE LIGHTS INTERMITTANT. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050502000432005050200043NM 2005 5 2 SWAA051046 120050411A256065C168209 HOOK BOEING737 7377H4 1384404NM L1 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29424WN 29828 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT HOOK LOOSE. SECURED HOOK PER MM. 2L72 4F RTA16WE 20050502000442005050200044NM 2005 5 2 SWAA051047 120050411A5320672056 BEAM BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29505SW 24182 DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEB CRACKED AT BS 180, WL 180, LBL 5.7. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050502000462005050200046NM 2005 5 2 SWAA051049 120050411A3350D71702001 BATTERY PACK BOEING737 7373G7 1384595NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29670SW 23784 DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050502000472005050200047NM 2005 5 2 SWAA051050 120050411A5210141A60741 GUIDE ARM BOEING737 7377H4 1384404NM L1 DOOR OUT OF ADJUST A SWAAA UNSCHED LANDING O OTHER CLCLIMB 1 SW29716SW 27850 AIR TURNBACK, CABIN WOULD NOT PRESSURIZE. FOUND L1 DOOR GUIDE ARM OUT OF ADJUSTMENT. ADJUSTED GUIDE ARM PER MM. 2L72 4F RTA16WE 20050502000492005050200049 2005 5 2 SWAA051052 420050412A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 & R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 R1 & R2 DOOR EMERGENCY EVAC SLIDES OUT OF ADJUST. ADJUSTED SLIDES PER MM. 2L72 4F RTA16WE 20050502000512005050200051NM 2005 5 2 SWAA051054 120050412A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 294, STR 13L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050502000522005050200052NM 2005 5 2 SWAA051055 120050412A53156545410 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 662, RBL 25, WL 207. REPAIRED BEAM PER SB & PAE ER. 2L72 4F RTA16WE 20050502000532005050200053NM 2005 5 2 SWAA051056 120050412A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 578, STR 8L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050502000542005050200054NM 2005 5 2 SWAA051057 120050412A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND 2 EA FUSELAGE STRINGER CLIPS CRACKED AT BS 597, STR 8L & STR 9L. REMOVED AND REPLACED CLIPS PER SRM. 2L72 4F RTA16WE 20050426000992005042600099 2005 4 26 SWAA051032 420050408A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050502000552005050200055NM 2005 5 2 USAA050375 120050316A5330 SKIN BOEING737 737301 1384611NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19587US53011 23932 CLT - RON - SKIN, 1.75 INCHES, CRACKED, STA 727E, STR 18L. INSTALLED DOUBLER IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050502000562005050200056NM 2005 5 2 USAA050376 120050316A5311 FRAME BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19442US40275 24841 CLT - Q6 - FRAME, .125 INCH, CRACKED, STA 787, STR8/9L. INSTALLED DOUBLER IAW TR 53-10-20B. INSTALLED DOUBLER IAW TR. (K) 2L72 4F4 FRTA16WE E21EU 20050502000572005050200057NM 2005 5 2 USAA050377 120050316A5320 TIE CLIP BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19442US 24841 CLT - Q6 - TIE CLIP, SRM 51-10-02, CRACKED, STA 787, STR 24R. REPLACED TIE CLIP. (K) 2L72 4F4 FRTA16WE E21EU 20050502000582005050200058NM 2005 5 2 USAA050364 120050315A5330 SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19517AU 23703 PIT - RON - SKIN, 4.500 INCH CRACK, STA 727A, 727B, STR 22R. INSTALLED DOUBLER IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050502000592005050200059NM 2005 5 2 USAA050363 120050310A5310 FORGING BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19527AU 23862 CLT - C5 - FORGING, .3 INCH, CRACKED, FWD SERVICE DOOR CUTOUT UPPER FWD UPPER CORNER. REMOVED CRACKED REVEL AND REPLACED IAW DWG NR 65-55878. (K) 2L72 4F4 FRTA16WE E21EU 20050502000602005050200060NM 2005 5 2 USAA050362 120050315A5311 FRAME BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19442US40275 24841 CLT - Q6 - FRAME, .250 INCH CRACK, STA 867, STR 8/9L. INSTALLED DOUBLER REPAIR IAW TR. (K) 2L72 4F4 FRTA16WE E21EU 20050502000612005050200061NM 2005 5 2 USAA050361 120050315A5320 TIE CLIP BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19442US40275 24841 CLT - Q6 - TIE CLIP, .250 INCH CRACK, STR 10L, BS 685. REPLACED TIE CLIP IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050502000622005050200062NM 2005 5 2 USAA050360 120050315A5320 TIE CLIP BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19442US 24841 CLT - Q6 - TIE CLIP, .250 INCH CRACK, STR 4R, BS 867. REPLACED TIE CLIP IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050502000642005050200064NM 2005 5 2 AMTA200500252 120050311A3350 LIGHT BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE CABIN DISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11522AT 29330 EGRESS LIGHT TRACK AT SEAT 28DEF, HAS 2 LIGHTS INOPERATIVE. FOUND LIGHTS UNPLUGGED. PLUGGED LIGHTS IN IAW MM. OPS CHECK GOOD. (K) 2L72 4F4 FRTA2NM E12EU 20050502000672005050200067NM 2005 5 2 AMTA200500287 120050320A2613S332T301240 OVERHEAT LOOP BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE LT ENGINE DEFECTIVE A AMTAK NONE N FALSE WARNING CRCRUISE 1 GL11557TZ 32591 EICAS STATUS MSG: L ENG OH LP2 DISPLAYED. REMOVED AND REPLACED LT ENG LOOP 2 OVERHEAT DETECTOR. REF; AMM 26-11-01. SYSTEM OPS CHECKED OK. (K) 2L72 4F4 FRTA2NM E12EU 20050502000682005050200068NM 2005 5 2 AMTA200500284 120050319A3397 WIRE BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE CABIN DAMAGED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11514AT 27971 EGRESS TRACK LIGHTS INOPERATIVE BETWEEN SEAT ROW 10 DEF AND SEAT ROW 12 DEF. REPAIRED WIRES REF STAND PRACT. OK FOR SERVICE. (K) 2L72 4F4 FRTA2NM E12EU 20050502000712005050200071EA 2005 5 2 A6WA200540094 120050313A2913848847 PUMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE HYDRAULIC SYS FAILED A A6WAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 GL31403AW5554 7288 UPON FINAL APPROACH EXTENDED GEAR RECEIVED HYD 3 LO PRESSURE CAUTION MESSAGE. ASSOC WITH GEAR DISAGREE AND NOSE DOOR OPEN WARNING MESSAGE. EXECUTED GO AROUND. GEAR CAME UP AFTER ABOUT A MINUTE. RAN ASSOCIATED QRH PUT GEAR DOWN. ALL NORMAL. REMOVED AND REPLACED ENGINE DRIVEN MOTOR PUMP 3B. (K) 2L72 4F4 FRTA21EA E15NE 20050810002322005081000232EA 2005 8 10 A6WA200540113 120050318A4920380004883 APU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE APU MAKING METAL A A6WAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 GL31419AW 7633 APU FAULT CONDITION IN FLIGHT. SMOKE APPEARED IN CABIN. CLOSED PACKS AND SHUTDOWN APU. INSPECTED APU COMPARTMENT, NO FUEL OR OIL LEAKS NOTED CHECKED BOTH ACM`S IAW AMM. OIL LEVEL CHECK GOOD. CHECKED APU OIL LEVEL IAW AMM. OIL LEVEL GOOD. FOUND METAL INSIDE APU, REMOVED AND REPLACED APU. OPS CHECK AND LEAK CHECK GOOD. (K) 2L72 4F4 FRTA21EA E15NE 20050502000782005050200078NM 2005 5 2 GAIA05016OP 120050325A3350GR062 BATTERY PACK BOEING727 7272J0 138407ENM PWA JT8 JT8D15 52051NE CABIN DISCHARGED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07284KH 21108 DURING PREFLIGHT, FOUND L1 DOOR AND COCKPIT ENTRY DOOR EMERGENCY BATTERY PACKS DRAINED TO DIM ILLUMINATION. REPLACED BATTERY PACKS (2 EA). OPERATED EMERGENCY LIGHTS SYSTEM AND FOUND OPERATING NORMALLY. OK FOR SUBSEQUENT FLIGHT. AC WAS RETURNED TO SERVICE. (K) 2L73 4F4 FRTA3WE E2EA 20050503000682005050300068 2005 5 3 DLM88050193 420050330A3417HG280D80 ADC DOUG MD88 MD88 3023688NM NR 1 MALFUNCTIONED A DALAA UNSCHED LANDING G MULTIPLE FAILURE TOTAKEOFF 1 SO27993DL 53345 ABOUT 100 KIAS ON T/O ROLL THROTTLES KICKED OFF AND CAPT LOST AIRSPEED, ALT, AND VSI. ALSO HAD GPWS WARNING. ALTI WINDOW WAS BLANK ON DFGC PANEL. FOUND PITOT AND STATIC LINE NOT SECURED ON NR 1 CADC. REPLACED NR 1 CADC PER MM 34-16-01-201 AS A PRECAUTION. PERFORMED RTS, BOTH NR 1 AND NR 2 DFGC GOOD. CADC FUNCTIONS NORMAL. 2L72 4F RTA6WE 20050503000722005050300072NM 2005 5 3 DLM88050195 120050331A4920 INLET DOUG MD88 MD88 3023688NM PWA JT8 JT8D NE APU CONTAMINATED A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27991DL15085 53343 P80411 BURNING OIL SMELL IMMEDIATELY AFTER TAKEOFF LASTED ONLY A FEW MINUTES. FOUND SMALL AMOUNT OF HYD FLUID IN APU INLET. CLEANED APU INLET, PERFORMED ALTERNATE DUCT BURN OPN 5090. REPLACED WATER SEPARATOR BAGS, NO FURTHER ODOR NOTED. 2L72 4F4 FRTA6WE E2EA 20050503000802005050300080NM 2005 5 3 DL733050197 120050402A2612 FIRE LOOP BOEING737 737347 1384647NM CFMINTCFM56 CFM562AFR 13802EU APU FAULTY A DALAFA ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27304WA39011 23345 35523C APU FIRE WARNING LIGHT/ALARM BELL IN FLIGHT APPROX 1 TO 2 MINS AFTER APU SHUTDOWN IN FLIGHT AT 10 TO 12,000 FT ALT FIRE BOTTLE USED. REMOVED APU SHROUD, APU INSPECTED FOUND NO EVIDENCE OF FIRE. REPLACED AFT DETECTOR LOOP. 2L72 4F4 FRTA16WE E21EU 20050503000902005050300090NM 2005 5 3 DLM88050200 120050404A4910 FLUID DOUG MD88 MD88 3023688NM APU BAY DETECTED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27957DL 49976 AFTER TAKEOFF FLIGHT ATTENDANTS REPORTED SMOKE/FUMES AFT CABIN. FOUND FLUID IN APU COMP. CLEANED SAME, PERFORMED DUCT BURNOUT. 2L72 4F RTA6WE 20050503000932005050300093NM 2005 5 3 DLM88050201 120050404A2410696233B CSD DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 1 ENGINE FAILED A DALAH DEACTIVATE SYST/CIRCUITS G MULTIPLE FAILURE CRCRUISE 1 SO27907DL 49538 726905 LT CSD TEMP STABILIZED IN EXCESS OF THE RED BAND. REPLACED CSD, GEN AND OIL COOLER. 2L72 4F4 FRTA6WE E9NE 20050503000952005050300095NM 2005 5 3 DL73S050202 120050405A2612 FIRE LOOP BOEING737 737232 1384475NM MLG WW FAILED A DALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27311DL 23083 CLIMBING THRU 18,000 FT WHEEL WELL FIRE INDICATION. LOWERED GEAR AND INDICATION REMAINED ON. REPLACED DETECTOR LOOP. 2L72 4F RTA16WE 20050503000962005050300096 2005 5 3 DL757050203 420050405A2565D31393110 SLIDE BOEING757 757232 1384965NM RT OVERWING DEPLOYED A DALAK NONE O OTHER ININSP/MAINT 1 SO27617DL 22907 RT OVERWING SLIDE DEPLOYMENT OCCURRED WHILE ORF POLICE SWAT TEAM WAS TRAINING ON BOARD A/C. DEPLOYMENT WAS SUCCESSFUL. 2L72 4F RTA2NM 20050503001022005050300102NM 2005 5 3 DL777050208 120050409A3350 FUSE BOEING777 777232 1385232NM POWER SUPPLY BLOWN A DALAK NONE L NO TEST ININSP/MAINT 1 SO27862DA 29734 EMERGENCY LIGHTS OUT ON MIDDLE ROW AT 45 THRU 56. REPLACED FUSE IN POWER SUPPLY. 2L72 4F RTT00001SE 20050503001032005050300103NM 2005 5 3 DL73S050211 120050408A53126546568515 BULKHEAD BOEING737 737247 138448DNM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27382DL 23609 THE AFT PRESSURE P-DOME WEB WAS FOUND WITH CRACKS AS FASTENER HOLES COMMON TO THE Y-CHORD AT STRINGER 6L. THE CRACKS ARE TYPICAL OF AD 99-08-23. THE CRACKS WERE REMOVED WITH A CUTOUT AND REPAIRED WITH ALUMINUM DOUBLERS PER B737 SRM AND PER ER/A 097892-14AD. 2L72 4F A16WE 20050503001052005050300105NM 2005 5 3 DL733050214 120050411A2460 CIRCUIT BREAKER BOEING737 737347 1384647NM COCKPIT TRIPPED A DALAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CLCLIMB 1 SO27309WA 23442 ON CLIMBOUT, BATTERY ON DC- IRS LIGHTS ILLUMINATED. BATTERY VOLTS ZERO. RETURNED TO SLC. MTC IN WORK. FOUND HOT BATTERY BUS C/B POPPED P18 PNL. RESET C/B. PERFORMING DC POWER CHECK. 2L72 4F RTA16WE 20050503001072005050300107EU 2005 5 3 05FDEA00960 120050409A7830 SWITCH AIRBUS310 A310222 3930315EU THRUST REVERSER FAILED A FDEAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO25450FE 162 REJECT TAKEOFF AT APPROX 100 KNOTS DUE TO NR 1 ENG REVERSE UNLOCK LIGHT ON. REMOVED & REPLACED NR 1 ENG RT TRANSLATING SLEEVE STOW SWITCH, RAN REVERSER SEVERAL TIMES OPS CK'D GOOD PER 78-31-18-4-A. CK'D RIGGING OPS CK'D GOOD PER MM 78-31-38-2-A. COMP STALL NR 2 ENG. PERFORMED BOROSCOPE AND VISUAL FUNCTIONAL CHECKS. NO DAMAGE FOUND PER EA 6-7200-87936. 2L72 4F RTA35EU 20050503001092005050300109NM 2005 5 3 05FDEA00954 120050411A5320 STRUCTURE DOUG MD11 MD11 3023602NM FUSELAGE DAMAGED A FDEAO OTHER O OTHER UKUNKNOWN 1 SO25628FE 48447 DURING AIRPLANE'S CONVERSION FROM P TO F FOUND: REPAIR AT STA 1960, STR 40-42 LT REQUIRES ENGINEERING EVALUATION TO DETERMINE WHETHER REPAIR IS MAJOR OR MINOR AND CONFORM TO APPLICABLE DATA. NO ACTION REQUIRED: REPAIR IS CONFORMED IAW SRE 53-50-00 FIG 16. 2L73 4F RTA22WE 20050503001112005050300111NM 2005 5 3 05FDEA00956 120050411A5320 STRUCTURE DOUG MD11 MD11 3023602NM FUSELAGE DAMAGED A FDEAO OTHER O OTHER UKUNKNOWN 1 SO25628FE 48447 DURING AIRPLANE'S CONVERSION FROM P TO F FOUND: REPAIR AT STA 635, STR 43-46 LT REQUIRES ENGINEERING EVALUATION TO DETERMINE WHETHER REPAIR IS MAJOR OR MINOR AND CONFORM TO APPLICABLE DATA. NO ACTION REQUIRED: REPAIR IS CONFORMED IAW SRE 5320-00 FIG 2 SHEET 3. 2L73 4F RTA22WE 20050503001172005050300117NM 2005 5 3 05FDEA00917 120050406A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER TXTAXI/GRND HDL 1 SO25216FE 22937 DURING LIFT TRUCK POSITIONING STRUCK A/C ON LT SIDE AND CAUSED HORIZONTAL SCRATCH/HOLES APPROXIMATELY 14 INCHES IN LENGTH AT BS 300 TO 314 AND 18 INCHES BELOW WL 208 CHORD (FLOORBEAM). REPAIRED NOTED DAMAGE PER BOEING 727 SRM 53-30-3. THIS REPAIR WAS DEEMED A CAT-B IN REF TO SRM 53-30-3 PAGE 6. THE SKIN THICKNESS DID NOT MEET THIS CRITERIA AND THEREFORE CAUSED THE REPAIR TO BE A CATAGORY B REPAIR, FEDEX SRM 53-30-3. 2L73 4F RTA3WE 20050503001202005050300120NM 2005 5 3 05FDEA00920 120050410A5531 RIB BOEING727 727200 138407ENM VERTICAL STAB CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25272FE 22037 VERTICAL STAB T/E CAVITY RIB WEB IS CHAFED AT UPPER SURFACE, FIN STA 180, 5 RBL, THROUGH ACCESS PNL 9510. REPAIRED THE CHAFED RIB WEB, VERTICAL STAB T/E CAVITY AT UPPER SURFACE FIN STA 180, 5 RBL IAW FEDEX EA 7-5530-86275. 2L73 4F RTA3WE 20050503001252005050300125NM 2005 5 3 05FDEA00921 120050410A5753 SKIN BOEING727 727200 138407ENM RT MID FLAP DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25272FE 22037 RIGHT WING O/B MID FLAP UPPER SKIN FWD EDGE IS GOUGED AND BENT AT NR 7 CARRIAGE. REPAIRED RIGHT WING O/B MID FLAP UPPER SKIN FWD EDGE AT NR 7 FLAP CARRIAGE PER EA 7-5710-86274. 2L73 4F RTA3WE 20050503001272005050300127NM 2005 5 3 05FDEA00940 120050411A5514 STRUCTURE DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON HORIZONTAL STABILIZER LEFTHAND BORE NR 8L FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82991. 2L73 4F RTA22WE 20050503001322005050300132NM 2005 5 3 05FDEA00943 120050411A5514 STRUCTURE DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT HAND UPPER CENTER SKIN PLANK NR 1L BARREL NUT BORE FOUND EXCEEDED LIMIT. REPAIRED IAW FEDEX EA 1-5510-82998. 2L73 4F RTA22WE 20050503001352005050300135NM 2005 5 3 05FDEA00945 120050411A5514 STRUCTURE DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON HORIZONTAL STABILIZER LEFTHAND BORE NR 10L, FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82991. 2L73 4F RTA22WE 20050503001382005050300138SO 2005 5 3 C2XA05IA052 120050401A32347455503 CONTROL LEVER EMB 145 EMB145XR 3260214SO COCKPIT DEFECTIVE A C2XAK NONE O OTHER CLCLIMB 1 SW27131325593 655 145708 DURING CLIMB THE LANDING GEAR LEVER WOULD NOT MOVE TO THE UP POSITION. THE CREW PERFORMED A MANUAL OVERRIDE TO RETRACT THE GEAR. THE AIRCRAFT LANDED WITHOUT INCIDENT AT IAH WHERE MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL LEVER. THE GEAR OPERATIONALLY TESTED GOOD AND THE AIRCAFT WAS RETURNED TO SERVICE. 2L72 4F RT 20050503001512005050300151NM 2005 5 3 05FDEA00948 120050411A5514 STRUCTURE DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT HAND BORE NR 22L FOUND EXCEEDED LIMIT. REPAIRED IAW FEDEX EA 1-5510-82952. 2L73 4F RTA22WE 20050503001552005050300155NM 2005 5 3 05FDEA00949 120050411A5320 STRUCTURE DOUG MD11 MD11 3023602NM FUSELAGE DAMAGED A FDEAO OTHER O OTHER UKUNKNOWN 1 SO25628FE 48447 DURING AIRPLANE'S CONVERSION FROM P TO F FOUND: EXISTING REPAIR AT FWD CARGO, FROM STA 775 TO STA 791, Z19, X= -117 LOWER FLOOR. NO ACTION REQUIRED: REPAIR IS IAW SRM 53-00-01, FIG 8, SHEET 5. 2L73 4F RTA22WE 20050503001572005050300157WP 2005 5 3 MWEA050030 120050407A57309937498502 SKIN DOUG DC9 DC982 3022082WP RT WING CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 RIGHT WING LEADING EDGE SKIN CRACKED AT STATION X15 = 136.421 AT SLAT TRACK. INSTALLED DOUBLER AND TRIPLER. 2L72 4F A6WE 20050503001592005050300159NE 2005 5 3 MWEA050031 220050408A7200720000025 ENGINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE LEFT FAILED A MWEAC ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 GL31701ME 49760 CREW HEARD A LOUD NOISE FROM THE LEFT SIDE AND NOTED POWER LOSS AND OIL PRESSURE ON THE NUMBER ONE ENGINE. REMOVED AND REPLACED LEFT ENGINE. 2L72 4F4 FRTA6WE E9NE 20050503001622005050300162NM 2005 5 3 05FDEA00953 120050411A5312 BULKHEAD DOUG MD11 MD11 3023602NM FUSELAGE DAMAGED A FDEAO OTHER O OTHER UKUNKNOWN 1 SO25628FE 48447 DURING AIRPLANE'S CONVERSION FROM P TO F FOUND: EXISTING REPAIR ON BULKHEAD, AT STA 595, X=56 LT SIDE. NO ACTION REQUIRED. REPAIR IS IAW SRM 53-20-00 FIG 6 SHEET 5. 2L73 4F RTA22WE 20050503001632005050300163NE 2005 5 3 2005UALA00277 220050401A7230 BLADE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 2 ENG COMPRESFAILED A UALACF ABORTED TAKEOFF ACTIVATE FIRE EXT. A FLAME/FIRE TOTAKEOFF 1 WP29432UA 587 ABORTED INITIAL TAKEOFF ROLL DUE TO COMPRESSOR STALL AND REPORTED FLAMES FROM NR 2 ENGINE. ENGINE TEARDOWN CONFIRMED A HPC STAGE 3 BLADE FAILURE. THIS FAILURE MODE IS AN INDUSTRY KNOWN PROBLEM AS A RESULT OF WEAR ON THE BLADE MIDSPAN SHROUD. A PROGRAM IS IN PLACE TO BORESOPE HIGH TIME COMPRESSOR BLADES SUSCEPTIBLE TO INCREASE MIDSPAN SHROUD WEAR. IAE HAS RECENTLY ISSUED A SERVICE BULLETIN WITH A NEW DESIGN TO REDUCE MIDSPAN SHROUD WEAR. 2L72 4F4 FRTA28NM E40NE 20050503001842005050300184 2005 5 3 2005UALA00282 420050318A2565A29011 ASPIRATOR BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE SLIDE/RAFT LEAKING A UALAK NONE O OTHER ININSP/MAINT 1 WP29657UA PA0656 27112 THE ASPIRATOR LEAKING BY BARREL. REPLACED ASPIRATOR. 2L72 4F4 FRTA1NM E24NE 20050503001872005050300187 2005 5 3 2005UALA00293 420050404A2565 ASPIRATOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE SLIDE/RAFT CRUSHED A UALAK NONE O OTHER ININSP/MAINT 1 WP29537UA 25157 FOUND LOWER TUBE ASPIRATOR CRUSHED. SLIDE WAS REMOVED FROM AIRCRAFT AT NORMAL MAINTENANCE INTERVAL. DAMAGED ASPIRATOR WAS OBSERVED DURING SHOP MAINTENANCE. THE EXACT CAUSE OF THE DAMAGE TO THE ASPIRATOR COULD NOT BE DETERMINED. 2L72 4F4 FRTA2NM E17NE 20050503001902005050300190NM 2005 5 3 2005UALA00299 120050405A2150 A/C PACK BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE A/C BAY MALFUNCTIONED A UALABA EMER. DESCENT UNSCHED LANDING O OTHER CRCRUISE 1 WP29647UA 25284 LOSS OF BOTH PACKS CAUSED RESULTANT PRESSURIZATION PROBLEM. ALTHOUGH RT PACK WAS DEFERRED IN STANDBY MODE PER MEL AT THE TIME OF THE EVENT, THERE IS NO RECORD OF ANY DEFECT OR MAINTENANCE ACTIVITY AGAINST THE LT PACK, PRIOR TO OR AFTER THE EVENT. RT PACK COMPRESSOR OUTLET TEMP SENSOR AND RT PACK RAM AIR INLET ACTUATOR WERE BOTH REPLACED. MAINTENANCE ALSO REPLACED LT BLEED ISOLATION VALVE DUE TO DAMAGED BUTTERFLY SEAL. HOWEVER, NONE OF THE AVAILABLE DATA EXPLAINS LOSS OF CABIN PRESSURIZATION. 2L72 4F4 FRTA1NM E24NE 20050503002022005050300202NE 2005 5 3 2005UALA00306 220050406A75301685MK6 ACTUATOR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 1 ENGINE FAILED A UALAE ENGINE SHUTDOWN MJ OVER TEMP WARNING INDICATION DEDESCENT 1 WP29433UA16985 589 V10617 NUMBER 1 ENGINE SHUT DOWN DUE TO ECAM WARNING FOR COMPRESSOR VANE, STALL AND EGT OVER LIMIT. REPLACED VSV ACTUATOR AND ACCOMPLISHED POWER ASSURANCE TEST. HISTORY SHOWED CLASS 2 FAULT MESSAGE ON VSV ACTUATOR FUNCTIONING ON ONE CHANNEL. A SUBSEQUENT STALL WAS DUE TO 10TH STAGE SOLENOID VALVE 4023KS FOUND FAILED WITH A CRACK. PART WAS REPLACED. 2L72 4F4 FRTA28NM E40NE 20050503002052005050300205SO 2005 5 3 RAI00503016 120050330A32608005701 PROXIMITY SWITCH EMB 145 EMB145 3260210SO NLG DEFECTIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03804HK 145082 PIT - LOUD BANGING NOISE COMING FROM NOSE GEAR WHILE TAXIING. MAINTENANCE REMOVE AND REPLACED NOSE LANDING GEAR DOWNLOCK PROX SWITCH. 2L72 4F RTT00011AT 20050503002062005050300206EU 2005 5 3 HE66099998 120050324A243523081002 STARTER GEN BOLKMS105 BO105LSA1 5626021EU ALLSN 250C 250C28 03013GL NR 2 ENGINE UNSERVICEABLE B HEEAO OTHER S AFFECT SYSTEMS NRNOT REPORTED 1 SW03202LF 2014 CAE280056 NR 2 ENG FAILED TO START. STARTER GENERATOR UNSERVICEABLE. 1G72 3U3 U H3AU E1GL 20050503002082005050300208EU 2005 5 3 RAI00504002 120050403A3222AIR860122 STRUT JETAIRJETSTMJETSTM4101 1500501EU NLG FAULTY A RAIAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 CE03573HK12934 41092 STL - ON TAKEOFF NOSE GEAR PULLED HARD TO THE RIGHT TRIED TO BRING NOSE GEAR BACK TO THE LEFT BUT STILL PULLED RIGHT. MAINTENANCE REMOVED AND REPLACED NOSE GEAR STRUT. 2L72 4T RTA41NM 20050503002112005050300211SO 2005 5 3 RAI00504005 120050405A2612 CONNECTOR EMB 145 EMB145LR 3260212SO NR 1 PYLON DIRTY A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03829HK 145281 PIT - ENGINE NR 1 FIRE DETECTION FAIL. MAINTENANCE INSPECTED SYSTEM, FOUND DEBRIS IN PYLON LOOP CONNECTOR. CLEANED DEBRIS AND RESECURED. 2L72 4T RTT00011AT 20050503002122005050300212EU 2005 5 3 RAI00504006 120050406A3297 WIRE AEROSPATR72 ATR72202 8680940EU AOG SWITCH DAMAGED A RAIAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 CE03723TE 283 STL - AFTER TAKEOFF GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. MAINTENANCE REPAIRED WIRING IN AOG SWITCH, OPS CHECKED GOOD. 2H72 4T RTA53EU 20050503002132005050300213GL 2005 5 3 RAI00504007 320050407A6110B5JFR36C1103E PROPELLER JETAIRJETSTMJETSTM4101 1500501EU MCAULY5JFR B5JFR36C1101GL LEFT DEFECTIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03560HK15913 41076 020993 STL - LEFT PROP HEAT FAULTS IN LONG AND SHORT CYCLES. MAINTENANCE REMOVED AND REPLACED LEFT PROP. 2L72 4T RTA41NM 5 CP15WE 20050503002172005050300217CE 2005 5 3 04052005 120050405A3260602EN556B UPLOCK SWITCH CESSNA402 402C 207590RCE NLG INOPERATIVE G HYIAK NONE O OTHER TOTAKEOFF 1 NE02548GA 402C0653 AIRCRAFT HAD THE HYDRAULIC LIGHT REMAIN ILLUMINATED AFTER GEAR RETRACTION. MAINTENANCE WAS UNABLE TO DUPLICATE, THE LT DOWNLOCK SWITCH WAS RESEALED AND LUBRICATED, FLIGHT CHECK UNSATISFACTORY, STILL UNABLE TO DUPLICATE ON GROUND, REPLACED NOSE UPLOCK SWITCH AND ADJUSTED LT UPLOCK SWITCH AND FLIGHT CHECKED GOOD. 1L72 3O A7CE 20050503002202005050300220NM 2005 5 3 SB05044 120050405A3397 WIRE BOEING737 7373B7 1384580NM EMERGENCY LIGHT BROKEN A USAAK NONE O OTHER ININSP/MAINT 1 EA19393US 23315 BOS COCKPIT EMERGENCY LIGHT SWITCH NOT WORKING PROPERLY. MAINTENANCE REPAIRED A BROKEN WIRE ABOVE ROW 20ABC. 2L72 4F RTA16WE 20050503002262005050300226SO 2005 5 3 2005F00073 220050406A8530 CYLINDER CESSNA206 U206F 2073333CE CONT O520 IO520F 17032SO MCAULYD3A34 D3A34C401 GL NR 2 CRACKED A HXRAK NONE O OTHER ININSP/MAINT 1 AL058295Q U20603156 814823R 022477 TCM CYLINDER CASE CRACKED NEAR NR 2 CYLINDER. 1H71 3O3 O A4CE E5CE 5 CP47GL 20050503002272005050300227EU 2005 5 3 A109040705DG 120050407A6510 DRIVE ASSY AGUSTAA109 A109 0260109EU TAIL ROTOR DAMAGED B JBZAO OTHER O OTHER NRNOT REPORTED 1 WP2722RX 7155 UPON UNCOWLING FOR A ROUTINE 600 HOUR INSPECTION, THE MAINTENANCE STAFF NOTED THE REMAINS OF A TAIL ROTOR DRIVE SHAFT RUBBER COLLAR (P/N: 109-0425-08-1) LAYING ON THE DECK BELOW ITS RESPECTIVE BEARING HANGAR. THE RUBBER COLLAR APPEARS HEAT DAMAGED AND BRITTLE, THE BEARING APPEARS TO HAVE EXCESSIVE DRAG. THE DRIVE SHAFT SHOWS INDICATIONS OF THE DRIVESHAFT SPINNING INSIDE THE COLLAR AND CAUSING EXCESSIVE WEAR. THIS BEARING ASSEMBLY IS DIFFICULT TO VISUALIZE ON DAILY INSPECTIONS BECAUSE OF ITS LOCATION. 1G72 3U H7EU 20050503002292005050300229CE 2005 5 3 GUU2005F00008 120050305A55101016200111 HINGE BRACKET BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE LT STABILIZER CORRODED A GUUAK NONE O OTHER ININSP/MAINT 1 SO178755217574 UE216 AT SCHEDULED ROUTINE MAINTENANCE, LT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED LT OB ELEVATOR HINGE BRACKET. (K) 2L72 4T4 TRTA24CE E26NE 20050503002312005050300231SO 2005 5 3 TZR2005F00002 220050103A8530T15T712BCA CYLINDER CESSNA401 401 207590CCE CONT O520 TSIO520* 17040SO EXHAUST VALVE CRACKED E TZRAK NONE O OTHER ININSP/MAINT 1 SW05401TE94 4010180 275395R CYLINDER CRACKED FROM EXHAUST VALVE TO SPARK PLUG HOLE. (K) 1L72 3O3 O A7CE E8CE 20050503002322005050300232SO 2005 5 3 TZR2005F00003 220050103A8530T1ST712BCN01 CYLINDER CESSNA401 401 207590CCE CONT O520 TSIO520* 17040SO NR 1 CRACKED E TZRAK NONE O OTHER ININSP/MAINT 1 SW05401TE601 4010180 CYLINDER CRACK FROM EXHAUST VALVE TO SPARK PLUG. (K) 1L72 3O3 O A7CE E8CE 20050503002332005050300233SO 2005 5 3 TZR2005F00004 220050321A8530T1ST712BCA01 CYLINDER CESSNA401 401 207590CCE CONT O520 TSIO520* 17040SO NR 4 CRACKED E TZRAK NONE O OTHER ININSP/MAINT 1 SW05405TE605 4010121 CYLINDER CRACKED FROM EXHAUST VALVE TO TOP SPARK PLUG HOLE. (K) 1L72 3O3 O A7CE E8CE 20050503002342005050300234SO 2005 5 3 TZR2005F00005 220050321A8530T1ST712BCA01 CYLINDER CESSNA401 401 207590CCE CONT O520 TSIO520* 17040SO NR 3 CRACKED E TZRAK NONE O OTHER ININSP/MAINT 1 SW05405TE605 4010121 14590271E CYLINDER CRACK FROM EXHAUST VALVE. (K) 1L72 3O3 O A7CE E8CE 20050503002352005050300235SO 2005 5 3 TZR2005F00006 220050129A8530T1ST712BCA01 CYLINDER HEAD CESSNA401 401 207590CCE CONT O520 TSIO520* 17040SO NR 3 CRACKED E TZRAK NONE O OTHER ININSP/MAINT 1 SW05405TE1338 4010121 275439R CYLINDER CRACKED AT HEAD. (K) 1L72 3O3 O A7CE E8CE 20050503002362005050300236SO 2005 5 3 TZR2005F00007 220050114A8530T1ST712BCA01 CYLINDER CESSNA401 401 207590CCE CONT O520 TSIO520* 17040SO NR 6 CRACKED E TZRAK NONE O OTHER ININSP/MAINT 1 SW05405TE1068 4010121 CYLINDER CRACKED FROM EXHAUST VALVE. (K) 1L72 3O3 O A7CE E8CE 20050503002372005050300237SO 2005 5 3 TZR2005F00008 220050112A8530T1ST712BCA01 CYLINDER CESSNA401 401 207590CCE CONT O520 TSIO520* 17040SO NR 3 CRACKED A TZRAK NONE O OTHER ININSP/MAINT 1 SW05405TE432 4010121 14590271E CYLINDER CRACKED AT SPARK PLUG HOLE. (K) 1L72 3O3 O A7CE E8CE 20050503002382005050300238SO 2005 5 3 TZR2005F00009 220050222A8530T1ST712BCA01 CYLINDER CESSNA401 401 207590CCE CONT O520 TSIO520* 17040SO NR 5 CRACKED E TZRAK NONE O OTHER ININSP/MAINT 1 SW05405TE515 4010121 CYLINDER CRACKED VALVE TO VALVE. (K) 1L72 3O3 O A7CE E8CE 20050503002402005050300240SO 2005 5 3 TZR2005F00011 220050302A8530T1ST712BCA01 CYLINDER CESSNA402 402B 207590PCE CONT O520 TSIO520* 17040SO NR 5 CRACKED A TZRAK NONE O OTHER ININSP/MAINT 1 SW05404TE876 402B0834 1655858E CYLINDER CRACKED FROM EXHAUST VALVE. (K) 1L72 3O3 O A7CE E8CE 20050503002422005050300242SO 2005 5 3 TZR2005F00013 220050110A8530T15ST712BCA01 CYLINDER CESSNA401 401 207590CCE CONT O520 TSIO520* 17040SO NR 5 DAMAGED E TZRAK NONE O OTHER ININSP/MAINT 1 SW05403TE1068 4010008 182946R CYLINDER COMPRESSION BELOW MINIMUMS. (K) 1L72 3O3 O A7CE E8CE 20050630000202005063000020 2005 6 30 QXEA200501035 420050610A3418 STALL WARNING BOMBDRDHC8 DHC8402 1390042NM COCKPIT FALSE ACTIVATIONA QXEAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 NM09405QX 4047 PUSHER SYSTEM FAIL LIGHT ON TAXI. WILL NOT CLEAR WITH ABNORMAL CHECKLIST. MX INTERROGATED CDS FOR FAULTS. NONE FOUND. COMPLIED WITH FIM TASK 27-33-00-810-829. COMPLIED WITH PUSHER SYSTEM FUNCTION TEST PER AMM 27-33-00-720-801. OPS CHECK GOOD. NO FAULTS IN CDS. NO PARTS REPLACED. ACFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050630000352005063000035EA 2005 6 30 SWIA200515127 120050323A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07958SW 7833 OUTBOARD CLIP CRACKED AT FS 280.00 AND RBL 9, ITEM FOUND AT C-CHECK INSP. CLIP REPLACED AT FS 280.00 AND RBL 9 IAW CRJ SRM 51-42-06 AND 51-42-21. 2L72 4F RTA21EA 20050630000432005063000043NM 2005 6 30 DHL2005741563 120050421A5315 FLOORBEAM BOEING727 7272Q9 138448MNM FUSELAGE DEFECTIVE A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 FOUND REPLACE TEE ANGLE AT BS RBL 60-LBL 60 FOR 9-G BARRIER INSTALLATION. REMOVED TEE ANGLE BS 344 FROM LBL 60 -LBL 60. LOCATED AND DRILLED HOLES IN REPLACEMENT PART IAW B727 SRM 51-30-2 FIG 1. TREATED AND PRIMED PART IAW B727 SRM 51-10-2. INSTALLED REPLACEMENT PART NR BAC 1505-29222 PO NR 9002149 (12FT) FROM LBL 60 -LBL 60 IAW B727 SRM 51-30-2 AND STC ST0088LA. 2L73 4F RTA3WE 20050630000482005063000048WP 2005 6 30 UPS05844696 120050525A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 RT CENTER WING L/E PNEUMATIC DUCT ATTACH POINT UPPER RIB CRACKED 3 INCH LONG AT XFS 304. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2 -0 FIG 2, 51-1-15, AND 51-1-20D. 2L74 4F RT4A25 20050630000502005063000050WP 2005 6 30 UPS05844698 120050527A532037592221N SPLICE DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 LONGERON SPLICE FITTING CRACKED AT STA 1260 TO 1280 L36. REMOVED AND REPLACED LONGERON SPLICE FITTING IAW DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20050630000882005063000088EA 2005 6 30 MASA200500340 120050507A5210 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR STICKING A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0747239 7239 CREW REPORTED A MAIN PASSENGER DOOR THAT WAS STICKING. MX LUBED AND ADJUSTED THE INNER DOOR STOW HANDLE. 2L72 4F RTA21EA 20050630000912005063000091NE 2005 6 30 MASA200500354 220050514A7261 OIL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF341A NE RT ENGINE LOW A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07652ML 7036 CREW RETURNED TO FIELD FOR RT ENGINE OIL LOW PRESSURE. CREW DID NOT SHUT DOWN ENGINE. MX SERVICED ENGINE OIL. 2L72 4F4 FRTA21EA E15NE 20050630001142005063000114SO 2005 6 30 RTE2005F00000 120050404A2823491947 SELECTOR PIPER PA28 PA28181 7102807SO LYC O360 O360A4M 41514EA SNSNCH76E 76EM8 EA FUEL SYSTEM INTERMITTENT E RTEAO OTHER O OTHER TXTAXI/GRND HDL 1 NM019279J416 2843068 L3522836A 31066K DURING GROUND RUNUP, FOUND FUEL SELECTOR OPERATION INTERMITTENT. INSP, FOUND UNIT EXTERIOR COVERED IN FINELY GROUND METAL SHAVINGS. UPON DISASSEMBLY, FOUND INTERNAL WALL SCORED BY SELECTOR DETENT MECHANISM. AFTER ANALYSIS OF FUEL SELECTOR INSTALL, WHICH IS PRESUMED TO HAVE BEEN DONE AT FACTORY DURING MFG DUE TO LACK OF MAINT ENTRIES CONCERNING FUEL SELECTOR. COVER PLATE MOUNTING SCREWS HAD BEEN WORKING WHERE THEY PASS THROUGH AIRFRAME SUPPORT STRUCTURE. THIS IS WHAT PRODUCE METAL SHAVINGS. WHICH THEN WORKED THEIR WAY INTO THE SELECTOR BODY THROUGH DETENT STOP HOLES. SCREWS IN QUESTION WERE FOUND SAFTIED WITH STAINLESS STEEL SAFETY WIRE. REMOVE SAFETY WIRE, RETORQUE SCREWS AND RESAFETY. (K) 1L71 3O3 O 2A13 E286 5 NP4EA 20050701000222005070100022SO 2005 7 1 C2XA05RI013 120050626A793223073345 PRESSURE VALVE EMB 145 EMB145XR 3260214SO ALLSN AE300 AE3007A GL NR 1 ENGINE OIL FAILED A C2XAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW2717108 145655 CAE312276 FLIGHT 2567 - EWR TO FPO - DURING CRUISE, ENGINE NR 1 OIL QUANTITY DROP FROM 8 QTS TO 5 QTS IN A LITTLE OVER ONE HOUR. CREW DIVERTED FLIGHT TO RIC. RIC MAINTENANCE REMOVED AND REPLACED OIL PRESS RELIEF VALVE AND SERVICE ENGINE NR 1. OPERATIONAL CHECK AND LEAK TEST WERE PERFORMED SUCCESFULLY. ACFT WAS APPROVED TO RETURN TO FLIGHT. 2L72 4F4 FRT TE6CH 20050701000322005070100032EA 2005 7 1 SWIA200515191 120050626A2740 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07720SW 7297 CAPTAIN'S TRIM SWITCH STICKING. REPLACED CAPTAIN'S TRIM SWITCH IAW MM 27-41-00. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050701000352005070100035EA 2005 7 1 SWIA200515194 120050620A2120 SMOKE CNDAIRCL600 CL6002B19 1900309EA COCKPIT DETECTED A SWIAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 NM07975SW 7951 SMELLED SMOKE IN COCKPIT AND CABIN. GROUND RAN ENGINES WITH PACKS ON AND INSPECTED BEHIND ALL ACCESSIBLE PANELS IN FLIGHT DECK. COULD NOT DUPLICATE DISCREPANCY. 2L72 4F RTA21EA 20050701000362005070100036EA 2005 7 1 SWIA200515195 120050625A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07913SW 7597 AFT EMERGENCY CEILING FLOOD LIGHT INOP. RELAMPED AFT EMERGENCY CEILING LIGHT AS REQUIRED. OPERATIONAL CHECK GOOD. ALL IAW 33-31-16. 2L72 4F RTA21EA 20050701000412005070100041EA 2005 7 1 A6WA200540210 120050621A2150 A/C PACK CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RIGHT SMOKE A A6WAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL31404AW 7294 RT PACK HIGH TEMP MESSAGE, PACK SHUTDOWN, SMOKE IN CABIN AND COCKPIT. (K) 2L72 4F4 FRTA21EA E15NE 20050701000712005070100071EU 2005 7 1 SF20050622 120050622A6123 CONNECTOR SAAB SF340 SF340A 7850100EU GE CT7TS CT71 30030NE AUTOCOARSEN LOOSE A UHLAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 GL1714XS 340A014 AUTOCOARSEN FAILED ON TAKEOFF ROLL. ABORTED TAKEOFF AT LESS THEN 40 KTS. FOUND NR 1 P3 SWITCH CONNECTOR TO BE LOOSE. TIGHTENED AS REQUIRED, OPS CK GOOD IAW AMM 61-22-00-5. 2L72 4T4 URTA52EU E8NE 20050701000752005070100075WP 2005 7 1 ASMF200506023 120050621A2530 VALVE DOUG DC9 DC987 3022087WP PWA JT8 JT8D* NE COFFEEMAKER LEAKING W ASMFD RETURN TO BLOCK K FLUID LOSS TXTAXI/GRND HDL 1 SW23755RA 49727 AIRCRAFT RETURNED TO PLATFORM, WATER LEAK IN THE COFFEE MAKER OF AFT GALLEY. DURING REVISION WAS DETECTED THE FEEDING WATER VALVE LOOSEN. THE FEEDING WATER VALVE WAS REPRESSED IAW MM 20-30-02, ALL CORRECT. DURING OVERNIGHT SERVICE, THE TORQUE IN COFFEE MAKER CONNECTORS OF AFT GALLEY WAS VERIFIED IAW MM 20-30-02, ALL CORRECT. 2L72 4F4 FRTA6WE E2EA 20050701000782005070100078CE 2005 7 1 DXTA200500809 120050628A2720666000266 CONTROL CABLE CESSNA560 560XL 2076702CE PWA 545 PW545A NE RUDDER SHEARED E DXTAA UNSCHED LANDING F FLT CONT AFFECTED NRNOT REPORTED 1 GL07695QS192 5605293 LT RUDDER PEDAL WILL NOT MOVE RUDDER. RT RUDDER PEDAL WILL MOVE RUDDER. LT RUDDER PEDAL MOVES FREELY WITH NO RESISTANCE. ALSO NOTED RUDDER CABLE BOWS BEHIND PEDAL AND FIREWALL. FOUND RUDDER CONTROL CABLE ASSY (UPPER) BROKEN AT 9 O' CLOCK POSITION. REPLACED RUDDER CONTROL CABLE ASSY AND CHECKED RIG, CABLE TENSIONS IAW CE560XL MM CH 27-20-00. 2L72 4F4 FRTA22CE E00059EN 20050701000792005070100079CE 2005 7 1 DXTA200500810 120050629A3240 BRAKE ASSY CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE MLG MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07367QS 5600367 ON TAXI ZERO BRAKING FOR SEVERAL SECONDS, THEN BRAKES GRABBED. ITEM IS UNDER INVESTIGATION. 2L72 4F4 FRTA22CE E25EA 20050701000802005070100080EU 2005 7 1 EGRR101267 120050609A7800N5205 DAMPER AGUSTAA109 A109E 0260119EU PWA PW206 PW206A NE LT ENGINE DETERIORATED B EGRRK NONE O OTHER ININSP/MAINT 1 EA1715MV 829 11025 DURING AIRCRAFT INSPECTION, FOUND LT ENGINE EXHAUST SADDLE CHAFING ON ENGINE FIRE EXTINGUISHER BOTTLE UPPER ACTIVATION CARTRIDGE ELECTRICAL WIRE CONNECTING POINT. THE RUBBER NIPPLE WAS CHAFED THROUGH AND THE SADDLE WAS SITTING DIRECTLY ON THE STUD. REPLACED 2 EA RUBBER DAMPERS P/N N5205 WITH NEW. CLEARANCE BETWEEN SADDLE AND ELECTRICAL CONNECTION IS NOW APPROX .1875. 1G72 3U3 URTH7EU E42NE 20050701000822005070100082SW 2005 7 1 ALGA104357 120050501A6410206101733003 SLEEVE BELL 206 206L4 1182110SW ALLSN 250C 250C30 03013GL TAIL ROTOR WORN E ALGAK NONE O OTHER ININSP/MAINT 1 SW03176AL385 52146 BEARING AXIAL PLAY BEYOND MAX. INSTALLED NEW BEARINGS AND SLEEVES BY O/H SHOP. 1G71 3U3 UNCH2SW E1GL 20050705000152005070500015EU 2005 7 5 USAA050697 120050522A5320D5347217220400 FLOOR SUPPORT AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19717UW17895 1069 PIT - FOUND FLOOR SUPPORT CORRODED 2 INCHES BY 10 INCHES, Y1292 FLOOR SUPPORT FROM C-66 TO C-70. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-72-11 AND DWG D53472815. (M) 2L72 4F RTA28NM 20050705000192005070500019NM 2005 7 5 USAA050708 120050601A5340 STRINGER CLIP BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19445US40360 24863 CLT - FOUND TIE CLIP CRACKED .6 INCH, STRINGER TIE CLIP STATION 294.5 STRINGER 13L. FABRICATED AND INSTALLED NEW TIE CLIP IAW BOEING DRAWING 62-01633. (M) 2L72 4F RTA16WE 20050705000352005070500035SO 2005 7 5 C2XA05SH053 120050618A532014521713005 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713903 145479 DURING C-CHECK, CENTER OMEGA BEAM HAS CORROSION AT FS 20. MX REMOVED AND REPLACED CENTER OMEGA BEAM AT FS 18 TO FS 23 IAW EMB 145 SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050705000392005070500039NM 2005 7 5 CALA0500201 120050617A5330BACR15FV6 SKIN BOEING767 767424ER 1385270NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776054 29449 INSP FOUND 2.5 INCH CRACK IN FUSELAGE SKIN JUST FORWARD OF L-2 DOOR AT STA 654, S20L. INTERIM REPAIR PERFORMED IAW ECRA 5330-03448 AND A DIP WAS INITIATED TO PERFORM PERMANENT REPAIR WITHIN 12 MONTHS. 2L72 4F RTA1NM 20050705000402005070500040NM 2005 7 5 CALA0500202 120050618A5347143A5310 SEAT TRACK BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714214 28774 INSP FOUND LT I/B SEAT TRACK CORRODED BETWEEN STA 360 AND 380, LBL 24.75. NEW SEAT TRACK INSTALLED IAW SRM 51-40-02. 2L72 4F RTA16WE 20050705000412005070500041NM 2005 7 5 CALA0500203 120050618A531565C339502 FLOORBEAM BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716618 27331 INSP FOUND UPPER SURFACE OF FLOORBEAM CORRODED AT STA 986.5, LBL 45 TO RBL 45. REPAIRED FLOORBEAM IAW ECRA 5310-04472. 2L72 4F RTA16WE 20050705000452005070500045EU 2005 7 5 AWXA200500716 120050618A3350321430 BATTERY AIRBUS320 A320231 3930325EU EMERGENCY LIGHTSINOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28634AW 091 DURING 8 DAY CHECK EMERGENCY EXIT LIGHTS FAILED CIDS TEST PANEL (INT LEADS EMER L). MX REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT IAW TASK CARD R1C33303. ALSO, REMOVED AND REPLACED EMERGENCY LIGHT BATTERY IAW TASK CARD A1C33302. OPS TEST FROM CIDS PANEL GOOD. 2L72 4F RTA28NM 20050705000502005070500050 2005 7 5 AWXA200500721 420050619A34187705401 RELAY BOEING757 7572S7 1384962NM STALL WARNING MALFUNCTIONED A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28901AW 23321 DURING TAKEOFF BELOW 60 KNOTS REJECTED TAKEOFF FOR LT AOA PROBE EICAS MESSAGE. MESSAGE EXTINGUISED AFTER ABOUT 10 SECONDS. LT AOA WAS MEL'D. MX REMOVED AND REPLACED LT AOA CURRENT SENSING RELAY K401 IAW BOEING 757 MM 30-32-00-5, OPS CHECKS WERE GOOD. MEL WAS CLEARED. 2L72 4F RTA2NM 20050705000602005070500060EU 2005 7 5 MALA050485 120050606A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE GOUGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15453XJ 340B453 LT FUSELAGE SKIN GOUGED JUST AFT OF LOWER AFT CORNER OF PAX DOOR. DAMAGE IS ACCEPTABLE IAW MESABA EO NR S53304 DATED 6/15/05. REF EAMS WORK ORDER 212404 TASK 1501. 2L72 4T RTA52EU 20050705000622005070500062NM 2005 7 5 WRLA20051040 120050614A5511 RIB DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C-04 CHECK, WHILE PERFORMING INSP PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE NR 14. 2L73 4F4 FRTA22WE E24NE 20050705000682005070500068EA 2005 7 5 SWIA200515160 120050603A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07710BR 7852 FS 280 FLOORBEAM LBL 9.0 OUTBOARD ATTACH ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-00, 51-42-13, 51-23-00. 2L72 4F RTA21EA 20050705000692005070500069EA 2005 7 5 SWIA200515161 120050603A2560 ESCAPE HATCH CNDAIRCL600 CL6002B19 1900309EA EMERGENCY EQUIP FAILED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07710BR 7852 CREW ESCAPE HATCH FAILED FUNCTIONAL TEST. ITEM FOUND AT C-CHECK INSPECTION. LUBRICATED CREW ESCAPE HATCH IAW AMM 12-20-52-640-803. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050705000712005070500071EA 2005 7 5 SWIA200515163 120050603A5340 STRINGER CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07710BR 7852 RT FS 625 CLIP CRACKED AT STR 14R. ITEM FOUND AT C-CHECK INSPECTION. CLIP REPLACED IAW CRJ SRM 51-40-11, 51-42-06 AND 51-25-16. 2L72 4F RTA21EA 20050705000732005070500073EA 2005 7 5 SWIA200515165 120050528A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07965SW 7871 FS 280 AT RBL 9.0 INBOARD AND OUTBOARD FLOORBEAM ATTACH ANGLES CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REMOVED AND REPLACED ANGLES IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-21-11, 51-25-16, 51-23-00 . 2L72 4F RTA21EA 20050705001062005070500106EU 2005 7 5 DHL2005363004 120050618A3260141FL01D3 SWITCH AIRBUS300 A300B4203 3930306EU NLG MALFUNCTIONED A DHLAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01363DH 85 ON SHORT FINAL AFTER LANDING, GEAR EXTENSION, NOSE GEAR UNSAFE LIGHT (RED) ILLUMINATED ON PILOTS FRONT PANEL. ELECTED TO GO AROUND AND ACCOMPLISHED ABNORMAL PROCEDURE. RETURNED TO LANDING. NO COMPLICATIONS. SECOND OFFICERS GEAR LIGHTS OPERATE NORMALLY. REPLACED NLG SWITCH 40GB (P/N 141FL01D3) AND NLG RT TELESCOPIC DRAG STRUT ROCKER ARM PER MM 32-31-24. OPS CKS GOOD. 2L72 4F RTA35EU 20050705001122005070500112NM 2005 7 5 USAA050503 120050414A5420300N05019 SHIM BOEING757 7572B7 1384964NM NR 1 PYLON MIGRATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19611AU40729 27123 FOUND SHIM MIGRATION GREATER THAN .030 INCH, NR 1 PYLON MID BULKHEAD UPPER ATTACH AREA BETWEEN THREAD FITTING. REPLACED SHIMS PER EO 5402R022A SECT IV PART 2/6, EA 96212. (M) 2L72 4F RTA2NM 20050705001152005070500115NM 2005 7 5 USAA050475 120050407A5415 ATTACH FITTING BOEING757 7572B7 1384964NM RT PYLON DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19611AU 27123 CLT - FOUND FITTINGS DAMAGED, FORWARD OUTBOARD MID BULKHEAD AND UPPER ATTACH FITTING HOLES, RT PYLON FORWARD OUTBOARD MID AND UPPER ATTACH FITTING HOLES. REPAIRED OVERSIZED HOLES AND FABRICATED REPAIR BUSHINGS IAW EA 96400. (M) 2L72 4F RTA2NM 20050705001172005070500117NM 2005 7 5 USAA050480 120050406A5415 FITTING BOEING757 7572B7 1384964NM NR 2 PYLON GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19626AU 27303 PIT - FOUND GOUGED .4 INCH BY .4 INCH BY .020 INCH, AFT BOLT HOLE, NR 2 PYLON, INBOARD MID BULKHEAD. REAMED HOLE, FLAP PEEN, RE-SLEEVE AND BUSH PER EA 96439 AND 96450. (M) 2L72 4F RTA2NM 20050705001222005070500122EU 2005 7 5 USAA050637 120050502A5340 TEE FITTING AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA01672UW 0333 BFM - FOUND LOWER TEE FITTING CORRODED 2 INCHES LONG BY 2 INCHES WIDE BY .021 INCHES DEEP, AT FRAME 40. FABRICATED AND INSTALLED REPAIR WASHER PER EA 96536, SRM 51-74-00- 41-23-11. (M) 2L72 4F RTA46NM 20050705001232005070500123EU 2005 7 5 USAA050636 120050502A5330 SKIN AIRBUS330 A330323 3930335EU FUSELAGE DENTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW24199 0333 BFM - FOUND SKIN DENTED 2.239 INCH LONG BY 2.1175 INCH WIDE BY .107 INCH DEEP, FUSELAGE EXT SKIN AT FRAME 36, STRINGER 33 RT. INSTALLED DOUBLER REPAIR PER EA 75686E AND SRM 53-00-11 FIG 202. (M) 2L72 4F RTA46NM 20050705001262005070500126EU 2005 7 5 USAA050633 120050422A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW 0333 BFM - FOUND SEAT TRACK CORRODED 6 INCHES BY .50 INCH BY .060 INCH DEEP, AT Y450, FRAME 73 AND 74. CORROSION LEVEL 2, TASK C53415901. REMOVED AND REPLACED SEAT TRACK PER SRM 51-74-00, 53-00-15, 51-42-11. (M) 2L72 4F RTA46NM 20050705001292005070500129EU 2005 7 5 USAA050630 120050420A5347F5347821720100 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW24199 0333 BFM - FOUND SEAT TRACK CORRODED 1.5 INCH BY 1.4 INCH WIDE BY .080 INCH DEEP, FRAME 73 AND 74 Y=-450. CORROSION LEVEL 2, TASK C534159-01. REMOVED AND REPLACED SEAT TRACK PER SRM 53-00-15, 51-42-11. (M) 2L72 4F RTA46NM 20050705001332005070500133EU 2005 7 5 USAA050626 120050422A5347F5347820720100 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW24199 0333 BFM - FOUND SEAT TRACK CORRODED, 1 INCH LONG BY .5 INCH WIDE BY .050 INCH DEEP, Y-1337.1 FRAME 74. REMOVED AND REPLACED SEAT TRACK PER SRM 51-74-00, 53-00-15. (M) 2L72 4F RTA46NM 20050705001392005070500139EU 2005 7 5 USAA050620 120050429A5320 FLOOR SUPPORT AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW 0333 BFM - FOUND FLOOR SUPPORT CORRODED 1.2 INCHES LONG BY .400 INCHES WIDE BY .035 INCHES DEEP, Y450 AT FRAME 31-34. FABRICATED AND INSTALLED REPAIR SPLICE PER SRM 51-74-00, 53-00-15, 51-40-01. (M) 2L72 4F RTA46NM 20050705001402005070500140EU 2005 7 5 USAA050619 120050505A5320F533153742000 FLANGE AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW24199 0333 BFM - FOUND FLANGE CORRODED 3 INCH BY 2 INCH BY .030 INCH, .024 INCH, .008 INCH, .032 INCH, FRAME 44, 24 INCHES RIGHT OF CENTER. REPLACED WITH NEW FLANGE PER SRM 51-42-11, 51-44-11. (M) 2L72 4F RTA46NM 20050705001412005070500141EU 2005 7 5 USAA050618 120050428A5320 FLOOR SUPPORT AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW 0333 BFM - FOUND FLOOR SUPPORT CORRODED 2 INCHES BY 1.72 INCH BY.040 INCH, Y0 AT FRAME 13B. REMOVED AND REPLACED SUPPORT PER SRM 53-11-14. (M) 2L72 4F RTA46NM 20050705001502005070500150EU 2005 7 5 USAA050609 120050427A5313 STRINGER AIRBUS330 A330323 3930335EU FUSLEAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW24199 0333 BFM - FOUND ANGLE CRACKED .750 INCH LONG, FRAME 80 AT Y-1447.8. REMOVED AND REPLACED STRINGER PER SRM 53-00-13, 51-21-11, 51-23-11, 51-43-11, 51-42-11, 51-73-12. (M) 2L72 4F RTA46NM 20050705001552005070500155EU 2005 7 5 USAA050604 120050427A5340 ANGLE AIRBUS330 A330323 3930335EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW24199 0333 BFM - FOUND ANGLE CRACKED .750 INCH, FRAME 80 AT Y1447.8. REMOVED AND REPLACED CUSP ANGLE PER SRM 51-42-11, 53-00-13, 51-21-11, 51-23-11, 51-42-11. (M) 2L72 4F RTA46NM 20050706000012005070600001EU 2005 7 6 USAA050658 120050502A5347D5311282600101 TRACK AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19105UW13610 0868 PIT - FOUND TRACK CORRODED .5 INCH AREA, AT FRAME 16 Y503. REPLACED WITH IDENT PART. (M) 2L72 4F RTA28NM 20050706000032005070600003EU 2005 7 6 USAA050654 120050503A53151161201 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19715UW17968 1051 PIT - FOUND FLOORBEAM CORRODED .5 INCH WIDE BY 6 INCHES LONG, TOP SURFACE FLOORBEAM, FRAME STATION 66, 30 INCHES RIGHT OF CENTER LINE. REPLACED PER AIRBUS DWG D54372815 AND SRM 51-72-11. (M) 2L72 4F RTA28NM 20050706000102005070600010EU 2005 7 6 USAA050681 120050523A5310D5347209001100 BEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19716UW18358 1055 PIT - FOUND BEAM CORRODED BETWEEN FRAME 64-66 AT - Y 52 INCHES. REMOVED AND REPLACED BEAM PER SRM 51-72-11. (M) 2L72 4F RTA28NM 20050706000202005070600020NM 2005 7 6 USAA050651 120050515A5330 SKIN BOEING737 737401 1384701NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19423US44823 23990 CLT - FOUND SKIN CRACKED .5 INCH, AFT SERVICE DOOR LOWER HINGE CUTOUT, BS 957.5. INSTALLED DOUBLER AND TRIPLER IAW SRM 53-60-01. (M) 2L72 4F RTA16WE 20050706000232005070600023NM 2005 7 6 USAA050663 120050511A5315BAC150510024618 FLOORBEAM BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19574US50136 23739 BFM - FOUND CAP CORRODED 2 INCH BY 51.5 INCH BY .025 INCH AND .018 INCH, STATION 344 LBL 20 - RBL 20. REMOVED FLOORBEAM CAP, APPROX 51.5; FABRICATED NEW CAP AND INSTALLED PER SRM 53-10-51, 51-20-01, 51-40-02. (M) 2L72 4F RTA16WE 20050706000272005070600027NM 2005 7 6 USAA050667 120050520A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19373US56099 22952 CLT - FOUND SKIN CRACKED .750 INCH, STATION 330, STRINGER 17R. FABRICATED AND INSTALLED SKIN DOUBLERS PER SRM 53-10-01. (M) 2L72 4F RTA16WE 20050706000312005070600031NM 2005 7 6 USAA050671 120050520A5340 STRINGER CLIP BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19445US40360 24863 CLT - FOUND TIE CLIP CRACKED .250 INCH, STATION 500F STRINGER 9R. REPLACED TIE CLIP IAW SRM 51-10-02. (M) 2L72 4F RTA16WE 20050706000442005070600044NE 2005 7 6 06252005 220050625A7200 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RIGHT FAILED A NSVAO OTHER Y ENGINE STOPPAGE APAPPROACH 1 EA27242CJ 242 785379 RIGHT ENGINE FAILED INFLIGHT. 2L72 4T4 TRTA52EU E8NE 20050706000562005070600056NM 2005 7 6 P5CA0501371 120050622A5414 SKIN BOEING747 747230B 1384889NM NR 3 NACELLE WORN A P5CAK NONE O OTHER ININSP/MAINT 1 EA15509MC 21221 WORN/CHAFING NR 3 NACELLE STRUT SKIN AROUND CUTOUT NR 12. NR 3 NACELLE STRUT SKIN AROUND CUTOUT REPAIRED PER BOEING INSTRUCTIONS 1-1MNB95 AND FAA FORM 8100-9. 2L74 4F A20WE 20050706000762005070600076SO 2005 7 6 TZR2005F00022 220050610A8530ACE520T101 CYLINDER CESSNA401 401A 207590DCE CONT O520 GTSIO520C 17032SO RT ENGINE CRACKED E TZRAO OTHER O OTHER NRNOT REPORTED 1 SW05409TE455 401A0118 CRACK IS TYPICAL FOR THESE CYLINDERS. RT NR 4. (SW05200509363). (K) 1L72 3O3 O A7CE E7CE 20050706000822005070600082NM 2005 7 6 DHL2005783002 120050630A3260 UPLOCK SENSOR BOEING727 727227 1384078NM PWA JT8 JT8D17 52049NE RT MLG MALFUNCTIONED A DHLAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO01783DH 21999 FOUND RT MLG RED LIGHT ILLUMINATED. CLEANED CONTACTS ON RT MLG DOWNLOCK SWITCHS SYS OPS CHECKED BAD ON GROUND IAW B727 M/M R & R RT MAIN GEAR UPLOCK SENSOR OPS CHECK OK IAW MM 32-61-81. P/N 1-899-29. 2L73 4F4 F A3WE E2EA 20050706000892005070600089NM 2005 7 6 USAA050699 120050514A5523 SKIN BOEING737 737301 1384611NM TRIM TAB CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA01574US50136 23739 BFM - FOUND TRIM TAB WEB SKIN CRACKED .20 INCH, RT ELEV TRIM TAB HINGES NR 1 AND 3. BONDED FLIES REPAIR ON TRIM TAB PER SRM 51-70-17 AND TYP REPAIR 55-20-03. (M) 2L72 4F RTA16WE 20050706001002005070600100NM 2005 7 6 05FDEA01730 120050628A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25619FE 48770 LT BARREL NUT HOLE NR 30L FOUND OUT OF LIMIT AFTER CORROSION REMOVAL. REPAIRED AS PER FEDEX EA 1-5510-83022. 2L73 4F RTA22WE 20050706001022005070600102 2005 7 6 05FDEA01722 420050628A34535221837000 ANTENNA BOEING727 727200 138407ENM NR 1 ADF DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25203FE 22925 NR 1 ADF LOOP ANTENNA IS DELAMINATED. REMOVED AND REPLACED NR 1 ADF ANTENNA IAW MM 34-37-012-4. OPS CHECKED GOOD IAW M/M 34-37-001-5 2L73 4F RTA3WE 20050706001032005070600103NM 2005 7 6 05FDEA01723 120050628A7830HA6006310 COVER BOEING727 727200 138407ENM THRUST REVERSER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25203FE 22925 PANEL RACK NR 1 ENGINE UPPER AFT THRUST REVERSER PANEL CRACKED AND GOUGED AT BOTH ENDS. REPLACED PART TO BE INSTALLED DURING C-CHECK. 2L73 4F RTA3WE 20050706001062005070600106NM 2005 7 6 05FDEA01726 120050628A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25619FE 48770 RT BARREL NUT HOLE NR 31R FOUND OUT OF LIMIT AFTER CORROSION REMOVAL. REPAIRED AS PER FEDEX EA 1-5510-83026. 2L73 4F RTA22WE 20050706001142005070600114NM 2005 7 6 05FDEA01743 120050629A5754ARB126823 PANEL DOUG MD11 MD11 3023602NM ZONE 500 SEPARATED A FDEAO OTHER D INFLIGHT SEPARATION NRNOT REPORTED 1 SO25623FE 48794 LOST PANEL L WING COVERS OUTBD SLAT MECHANISM. LT WING PANEL NO.518FB REPLACED AS PER AMM 20-50-02 AND HINGE FILLERS REMOVED AND REPLACED AS PER SRM 51-35-01 VOL II. 2L73 4F RTA22WE 20050706001202005070600120NM 2005 7 6 05FDEA01749 120050630A5730ARB2886503 SKIN DOUG MD11 MD11 3023602NM ZONE 500 PUNCTURED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 LT WING FIXED LE FOUND PUNCTURED AT XORS 402. PUNCTUREED SKIN ON LT WING FIXED L/E AT XORS402 TRIMMED OUT AND REPAIRED AS PER SRM 57-10-00, FIG 14, VOL 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (OPEN) 2L73 4F RTA22WE 20050706001222005070600122NM 2005 7 6 05FDEA01751 120050630A2612 WARNING LIGHT BOEING727 727200 138407ENM APU FIRE HANDLE FALSE INDICATIONA FDEAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO25461FE 22548 DURING CLIMBOUT AT FL 220 HAD INTERMITTENT MASTER FIRE WARNING LIGHT AND TESTED ENGINE AND CARGO FIRE SYSTEMS, ALL TESTED OK. DURING CRUISE AT 330 ABOUT 30 MINS LATER, APU FIRE LIGHT ILLUMINATED. NO WARNING BELL JUST THE LIGHT IN THE HANDLE. RAN RED TABS PULLED FIRE HANDLE AND PUSHED DISCHARGE BUTTON. (OPEN) 2L73 4F RTA3WE 20050706001232005070600123WP 2005 7 6 05FDEA01753 120050629A2611 SMOKE DETECTOR DOUG MD10 MD1010F 3022112WP CARGO BAY INOPERATIVE A FDEAF ACTIVATE FIRE EXT. N FALSE WARNING LDLANDING 1 SO25570FE 47829 ON SHORT FINAL, RECEIVED LEVEL 3 CARGO FIRE LOWER FWD ALERT. PERFORMED PHASE 1, ALERTED TOWER, LANDED AND EXITED RWY. ALERT OFF AFTER APPROX 2 MIN DURING LANDING ROLL ONLY FIRED ONE BOTTLE. AFTER 20 MINUTES ALL CLEAR GIVEN 'MEL 26-22-01-02-A: FIRE EXT CYLINDER NR 1, INOPERATIVE DURING INSPECTION OF CARGO FIRE ALERT. FOUND NR 3 SMOKE DETECTOR FWD LOWER CARGO BAY INOPERATIVE DEFERED NR 3 DETECTOR 2L73 4F RTA22WE 20050706001252005070600125NM 2005 7 6 05FDEA01756 120050630A5310 DOOR FRAME DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 NR 3 LT MAIN ENTRY DOOR AFT JAMB CUTOUT BETWEEN LONGERONS 24L AND 25L , LOWER INTERNAL DOUBLER (AEA7539) FOUND WITH CORROSION. REPAIRED PER SRM VOLUME I, FIGURE 17 (SHEET 3) PAGE 62. (OPEN) 2L73 4F RTA22WE 20050706001282005070600128NM 2005 7 6 05FDEA01422 120050524A5313ADA80901 LONGERON DOUG MD11 MD11 3023602NM FUSLEAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25631FE 48454 FWD INTERMEDIATE FUSELAGE STA 1019 LONG 52 EXISITNG REPAIR ON CRACKED LONGERON. LONGERON REPAIR AT STA 1019 LONG 52 FORWARD INTERMEDIATE FUSELAGE EVALUATED FOUND REPAIR CARRIED OUT IAW SRM 53-10-00 FIG 1 AND FIG 2 VOL I. EO 1-5100-7-5001 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2L73 4F RTA22WE 20050706001292005070600129NM 2005 7 6 05FDEA01731 120050629A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 DURING ACCOMPLISHMENT OF EA 1-5750-87541. LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) OUTBOARD MID BOLT HOLE FOUND CORRODED. REMOVED AND REPLACED PER AMM 27-50-30-4. (CLOSED) 2L73 4F RTA22WE 20050706001302005070600130NM 2005 7 6 05FDEA01732 120050629A5710 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 DURING ACCOMPLISHMENT OF EA 1-5750-87541. LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) OUTBOARD AFT BOLT HOLE FOUND CORRODED. REMOVED AND REPLACED PER AMM 27-50-30-4. FLAP RIGGING CARRIED OUT PER AMM 27-50-30-5. 2L73 4F RTA22WE 20050706001332005070600133NM 2005 7 6 05FDEA01735 120050629A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) AFT HINGE FITTING FORWARD BOLT HOLE FOUND CORRODED. REMOVED AND REPLACED PER AMM 27-50-30-4. 2L73 4F RTA22WE 20050706001342005070600134NM 2005 7 6 05FDEA01737 120050629A5347 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 AT STATION 1964 LBL 78 SEAT TRACK CROWN, BASE AND FLANGE FOUND CORRODED. REMOVED AND REPAIRED IAW SRM 53-70-00. [CLOSED] 2L73 4F RTA22WE 20050706001382005070600138NM 2005 7 6 05FDEA01710 120050628A5753 HINGE FITTING DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) AFT HINGE FITTING FORWARD STRUT HOLE FOUND CORRODED STRUT. COMPLIED WITH FEDEX EA 1-5750-87545. (CLOSED) 2L73 4F RTA22WE 20050706001462005070600146CE 2005 7 6 DXTA200500785 120050619A2750 CONVERTER CESSNA750 750 2076810CE TE FLAPS MALFUNCTIONED E DXTAA UNSCHED LANDING JF WARNING INDICATION FLT CONT AFFECTED CRCRUISE 1 GL07958QS 7500158 "FLAPS FAIL" CAS MESSAGE DISPLAYED IN CRUISE AND RESET PER CHECKLIST WHEN FLAPS WERE DEPLOYED FROM 5-15 DEGREES, A MOMENTARY ROLL OCCURRED. FLAPS EXTENDED NORMALLY BEYOND 15 DEGREES. OPS CHECKED FLAPS WITH FLAP BREAKOUT BOX. TESTED AT DIFFERENT FLAP ANGLES WITH AND WITHOUT RESOLVERS COLD SOAKED. CLEANED FLAP HANDLE ASSEMBLY. TESTED WITH AND WITHOUT BOTH CONVERTERS COLD SOAKED. REMOVED FLAP BREAKOUT BOX. FLAP OPERATIONAL CHECKS WERE GOOD. NO DEFECTS WERE NOTED. REF: 750 M/M 27-50-00. 2L72 4J RTT00007WI 20050706001522005070600152CE 2005 7 6 DXTA200500790 120050619A27403094338 LIMIT SWITCH CESSNA750 750 2076810CE TRIM SYSTEM INOPERATIVE E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07960QS 7500160 AMBER TRIM SWITCH FAIL ILLUMINATED DURING CLIMB-OUT (FL180-FL200). TROUBLE SHOT AND FOUND FAULTY TRIM SWITCH ON PILOT CONTROL WHEEL. REMOVED & REPLACED SWITCH SWITCH OPS CHECKS GOOD IAW 750 M/M 27-40-00. 2L72 4J RTT00007WI 20050706001542005070600154NM 2005 7 6 DHL2005741586 120050429A5542 SKIN BOEING727 7272Q9 138448MNM RUDDER DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 UPPER RUDDER T/E DENTED 3 IN. ABOVE NR 6 TAB HINGE RT SIDE. CUT OUT DAMAGED AREA 2EA PLACES IAW B727 SRM 51-40-2 FIG 1. FABRICATED REPAIR DOUBLER IAW B727 SRM 55-40-2 FIG 2 AND SRM 51-40-2 FIG 1. TREATED AND PRIMED PART AND AREA IAW B727 SRM 51-10-2. INSTALLED REPAIR IAW B727 SRM 51-40-2 FIG 1. 2L73 4F RTA3WE 20050706001552005070600155NE 2005 7 6 MALA050498 220050622A7200 ENGINE BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE NR 3 VIBRATION A MALAE ENGINE SHUTDOWN E VIBRATION/BUFFET NRNOT REPORTED 1 GL15508XJ E2318 CREW SHUT DOWN NR 3 ENGINE DUE TO ENGINE VIBRATION. NO EMERGENCY DECLARED AND FLIGHT LANDED WITHOUT FURTHER INCIDENT. 2H74 4F4 FRTA49EU E6NE 20050706001562005070600156EU 2005 7 6 MALA050499 120050616A2432 BATTERY BAC 146 AVRO146RJ85A1500097EU DC GEN SYS FAILED A MALAK NONE O OTHER ININSP/MAINT 1 GL15531XJ E2365 BATTERY FAILED CAPACITY CHECK. 2H74 4F RTA49EU 20050706001582005070600158EU 2005 7 6 MALA050501 120050623A2432 BATTERY BAC 146 AVRO146RJ85A1500097EU DC GEN SYS FAILED A MALAK NONE O OTHER ININSP/MAINT 1 GL15519XJ E2344 BATTERY FAILED CAPACITY CHECK. 2H74 4F RTA49EU 20050706001602005070600160WP 2005 7 6 IXXA05SMN03S 120050427A5320 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX834963359 45993 DURING ROUTINE C-CHECK INSP, FWD CARGO COMPARTMENT INTERIOR, SPLICE FITTING CRACKED 3 IN, STA 440.000 - STA 460.000 L-35L. REMOVED CRACKED FITTING IAW DC-8 SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING IAW DWG 3750330. PERFORMED NDT INSPECTION TO FITTING IAW NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED AREA AND NEW FITTING IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO IAW DC-8 SRM 51-1-11 PAGE 9. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D PAGE 9. TORQUED IAW DC-8 RM 51-3-1. 2L74 4F RT4A25 20050706001652005070600165WP 2005 7 6 IXXA05SMN10S 120050429A5342 FITTING DOUG DC8 DC871F 302199DWP HORIZONTAL STAB CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX834963359 45993 DURING ROUTINE C-CHECK INSPECTION, LT HORIZONTAL STABILIZER FITTING CRACKED 1 IN., XFS 47.000 - XFS 60.000 (LWR PART). REMOVED CRACKED FITTING IAW DC-8 SRM 51-1-20D PAGE 21. CLEANED, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8B. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D PAGE 9, DC-8 SRM 51-1-21 PAGE 1. TORQUED IAW DC-8 RM 51-3-1. 2L74 4F RT4A25 20050706001672005070600167WP 2005 7 6 IXXA05SMN12S 120050429A5345 MOUNT DOUG DC8 DC871F 302199DWP ANTENNA CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX834963359 45993 DURING ROUTINE C-CHECK INSPECTION, 2 CRACKS ON DOPPLER ANTENNA FRAME, STA -99.000 TO STA -131.000. REMOVED CRACKED CAP IAW DC-8 SRM 53-1-0 PAGE 1, DC-8 SRM 51-1-21 PAGE 1, IAW DWG 5616101. PERFORMED HEAT TREATMENT IAW DC-8 SRM 51-1-1 PAGES 1, 13, 17. CLEANED, TREATED, PRIMED AREA AND NEW CAP IAW DC-8 SRM 51-1-8B. INSTALLED NEW CAP IAW DC-8 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050706001682005070600168WP 2005 7 6 IXXA05SMN13S 120050429A5751 SKIN DOUG DC8 DC871F 302199DWP RT WING AILERON CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX834963359 45993 RT WING INBD AILERON UPPER SKIN CRACKED 0.5 IN., STA. XA 610.000. MAJOR REPAIR IAW DC-8 SRM 57-1-0 PAGE 1 IAW DC-8 SRM 57-8-1 FIG 1, DWG DACO 5705334. REMOVED DAMAGED PANEL IAW DC-8 SRM 57-1-0 PAGE 1, DC-8 SRM 51-1-21 PAGE 1. REMOVED DAMAGED AREA IAW DC-8 SRM 57-2-5 FIG 1 SHEET 2. FABRICATED NEW PANEL AND FINGER DOUBLER IAW DC-8 SRM 57-8-1 FIG 1 ITEM B, K, DWG DACO 5705334. BONDED FINGER DOUBLER ON NEW PANEL IAW DC-8 SRM 51-1-9 PAGE 1, DC-8 SRM 51-1-9D PAGE 1, DPS 1.950, REV. AR R-1. CLEANED, TREATED, PRIMED AREA AND NEW PANEL INTERNAL PART IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11 PAGE 9, DPS 2.50 REV BB. INSTALLED NEW PANEL IAW DACO 5705334, DC-8 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050706001712005070600171WP 2005 7 6 IXXA05SMN35S 120050429A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX834963359 45993 EXT FUSELAGE RT FUSELAGE CTR SECTION PLATING TCAS DOUBLER MOD CORRODED. ELONGATED HOLES AND DENT DAMAGE (STA 220.000 - 260.000, L-29R TO L-31R). PERFORMED MAJOR REPAIR IAW FAA 8110-3 NR 05168, SEMAN DWG ED-3951. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FOUND OUT OF LIMITS IAW DC-8 SRM 53-2-0. REMOVED EXISTING DOUBLER DC-8 SRM 51-1-21. DC-8 SRM 51-1-20D. REMOVED DAMAGED AREA IAW SEMAN DWG ED-3951. PERFORMED NDT INSP IAW DC-8 NDT SPM PART 06-10-01-001. FAB NEW SEGMENT OF SKIN, EXT SPLICE DOUBLER, INT FINGER DOUBLERS, FINGER DOUBLER, FILLER , AND INT DOUBLER M STRAPS IAW SEMAN DWG ED-3951. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO SURFACES IAW DC-8 SRM 51-1-11. 2L74 4F RT4A25 20050706001732005070600173 2005 7 6 SA05074 420050617A256561639103 BOTTLE AIRBUSA321 A321211 3930370EU L-2 DOOR SLIDE DISCHARGED A USAAO OTHER J WARNING INDICATION NRNOT REPORTED 1 EA19161UW9946 1403 CIDS PANEL CAUTION LIGHT ILLUMINATED IN FLIGHT AND ON LANDING. MAINTENANCE FOUND L-2 DOOR SLIDE INFLATION BOTTLE PRESSURE LOW. MAINTENANCE REPLACED L-2 DOOR SLIDE INFLATION BOTTLE. OK FOR SERVICE. 2L72 4F RTA28NM 20050706001752005070600175NM 2005 7 6 DHL2005741583 120050429A5542 SKIN BOEING727 7272Q9 138448MNM RUDDER DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 UPPER RUDDER T/E DENTED 2 IN. BELOW NR 3 TAB HINGE RT SIDE. CUT OUT DAMAGED AREA IAW B727 SRM 51-40-2 FIG 1. FABRICATED REPAIR DOUBLER IAW B727 SRM 55-40-2 FIG 2 AND SRM 51-40-2 FIG . TREATED AND PRIMED PART AND AREA IAW B727 SRM 51-10-2. INSTALLED REPAIR DOUBLER IAW B727 SRM 51-40-2 FIG 1. 2L73 4F RTA3WE 20050706001772005070600177NM 2005 7 6 DHL2005741576 120050426A5311 FRAME BOEING727 7272Q9 138448MNM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741 21931 FRAME CORRODED AT STA 1166 AT STR 29R. FRAME AT BS 1166 FROM STR 25L-STR 25R IS CORRODED BEYOND ALLOWABLE LIMITS. CUT OUT DAMAGE SECTION FROM 25L- STR 25R IAW B727 SRM 53-10-4 FIG 13. FABRICATED NEW SECTION FROM 25L TO 25R 76 BY 10 IN. 7075-T6 .063 PO NR 5096262 IAW B727 SRM 53-10-2 FIG 5. LOCATED AND DRILLED FASTENER HOLES IN FRAME IAW B727 SRM 51-30-2 FIG 1. DRILLED AND LOCATED FASTENER HOLES IN NEW SHEAR TIE SECTION PN 65-16349-99 PO NR 5096122 IAW B727 SRM 51-30-2 AND 53-10-2 FIG 5. TREATED AND PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED PARTS PER B727 SRM 51-30-2. 2L73 4F RTA3WE 20050706001782005070600178 2005 7 6 MALA050496 420050615A3418 VANE SAAB SF340 340B 7860101EU STALL WARNING MALFUNCTIONED A MALAO OTHER N FALSE WARNING CLCLIMB 1 GL15429XJ 340B429 DURING CLIMB LT STALL CAUTION LIGHT ILLUMINATED. RETURNED TO MSP. REMOVED AND REPLACED RT STALL VANES. 2L72 4T RTA52EU 20050706001802005070600180EU 2005 7 6 MALA050490 120050620A53477253721459 GALLEY TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15421XJ 340B421 DURING 4K INSP, FOUND GALLEY TRACK AND PROFILE 7253721-495 CORRODED AND WILL BE REPLACED IAW SRM 51-40-21/22/27. RE:EAMS WORK ORDER 212304 TASK 2576. 2L72 4T RTA52EU 20050706001812005070600181EU 2005 7 6 MALA050495 120050620A53207253710243 PLATE SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15421XJ 340B421 DURING 4K INSPECTION, FOUND RT WRAP AROUND CORRODED AND HAS BEEN REPLACED IAW SRM 51-40-21. 2L72 4T RTA52EU 20050706001842005070600184EU 2005 7 6 MALA050494 120050620A5347 SEAT TRACK SAAB SF340 340B 7860101EU CABIN CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15421XJ 340B421 DURING 4K INSPECTION, FOUND SEAT TRACK AT BL 0 IS CORRODED AND HAS BEEN REPAIRED IAW SRM 53-70-60 BETWEEN FS 297 AND 304. 2L72 4T RTA52EU 20050706001872005070600187SO 2005 7 6 C2XA05CL050 120050619A49004504113 APU EMB 145 EMB145ER 3260211SO APU BAY ODOR A C2XAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW27149334993 4989 145018 DURING ROUTINE MAINTENANCE, OIL ODOR IN CABIN WAS NOTED WHEN APU BLEED WAS SELECTED. MX RELEASED ACFT IAW MEL 49-00-00. MX REPLACED APU. OPS CHECKS WERE GOOD. 2L72 4F RTT00011AT 20050706001882005070600188GL 2005 7 6 C2XA05RI012 220050619A7310P1081 FUEL FILTER EMB 145 EMB145ER 3260211SO ALLSN AE300 AE3007A GL NR 1 ENGINE CLOGGED A C2XAO OTHER J WARNING INDICATION CRCRUISE 1 SW2713936 145025 CAE310025 E1 FUEL IMPENDING BYPASS MESSAGE ILLUMINATED IN FLIGHT. CREW DIVERTED FLIGHT. MX REMOVED AND REPLACED ENGINE 1 FUEL FILTER. OPERATIONAL TEST WAS SUCCESSFULLY PERFORMED. ACFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20050706001892005070600189SO 2005 7 6 C2XA05SH056 120050622A491014547494403 FIREWALL EMB 145 EMB145LR 3260212SO APU CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714904 145477 DURING C-CHECK, APU FIREWALL HAS SEVERAL CHAFE MARKS AT BOTTOM EDGE. MX REMOVED DAMAGED AREA ON APU FIREWALL BOTTOM EDGE IAW EC 5310-01339. ACFT APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050706001912005070600191EA 2005 7 6 COMA0560357 120050616A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERS LEAKING A COMAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO01797CA15403 7344 RECEIVED HYDRAULIC NR 2 LOW PRESSURE CAUTION MESSAGE. CREW DECLARED AN EMERGENCY AND DIVERTED TO IAD. ACFT LANDED WITHOUT INCIDENT. REPLACED LEAKING FLIGHT SPOILER PCU. 2L72 4F RTA21EA 20050706001932005070600193NM 2005 7 6 DHL2005741592 120050511A5313 STRINGER BOEING727 7272Q9 138448MNM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 AFT PIT AT BS 1166 STR 30 IS CORRODED. REMOVED DAMAGED STR 30 FROM 1138-1183 IAW B727 SRM 53-10-3 FIG 1. FABRICATED STR 30. REPAIR PARTS FILLER BAC1498-147 PO3345302 DIM 42 IN. FROM BS 1138-1183 SPLICE BAC 1498-131 PO9001233 12 IN. AT BS 1138 IAW B727 SRM 53-10-3 FIG 1. TREATED AND PRIMED PARTS AND IAW B727 SRM 51-10-2. INSTALLED NEW STR 30 REPAIR FROM BS 1138-1183 IAW B727 SRM 53-10-3 FIG 1. 2L73 4F RTA3WE 20050706001942005070600194NM 2005 7 6 DHL2005741589 120050530A5230 WEB BOEING727 7272Q9 138448MNM CARGO DOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 WEB CRACKED AT AFT ATTACH BRACKET HOLE OF C2 DOOR SNUBBER. ROUTED OUT CRACK ON WEB BY INSP HOLE ON INNER SKIN OF C-2 DOOR SNUBBER AREA IAW B727 SRM 51-40-2 FIG 1. FABRICATED REPAIR DOUBLER IAW B727 SRM 51-10-2. INSTALLED REPAIR DOUBLER TO INNER WEB OF C-2 DOOR IAW B727 SRM 51-40-2 FIG 11. 2L73 4F RTA3WE 20050706001952005070600195NM 2005 7 6 DHL2005741581 120050429A5542 SKIN BOEING727 7272Q9 138448MNM RUDDER DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 UPPER RUDDER T/E DENTED 3 INCH ABOVE NR 5 TAB HINGE LT SIDE MARKED. CUT OUT DAMAGED AREA 2 EA PLACES IAW B727 SRM 51-01-2 FIG 1. FABRICATED REPAIR DOUBLER IAW B727 SRM 55-40-2 FIG 2 AND SRM 51-40-2 FIG 1. TREATED AND PRIMED PART AND AREA IAW B727 SRM 51-10-2. INSTALLED REPAIR PART IAW B727 SRM 51-40-2 FIG 1. 2L73 4F RTA3WE 20050706001962005070600196NM 2005 7 6 DHL2005741584 120050429A5542 SKIN BOEING727 7272Q9 138448MNM RUDDER DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 UPPER RUDDER T/E DENTED 4 INCH ABOVE NR 3 TAB HINGE RT SIDE. CUT-OUT DAMAGED AREA UPPER RUDDER T/E ABOVE NR 3 HINGE IAW B727 SRM 55-40-2 FIG 1 AND SRM 51-40-2 FIG 1. FABRICATED REPAIR " IAW B727 SRM 55-40-2 AND SRM 51-40-2 FIG 1. TREATED AND PRIMED PART AND AREA IAW B727 SRM 51-10-2. INSTALLED REPAIR IAW B727 SRM 51-40-2 FIG 1. 2L73 4F RTA3WE 20050706001972005070600197NM 2005 7 6 DHL2005741578 120050429A5330 LAP JOINT BOEING727 7272Q9 138448MNM FUSELAGE CHAFED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 LAP SPLICE AT BS 720D STR 19R CHAFED. DAMAGED AREA OUT OF LIMITS IAW 727 SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA DIM 4.625 BY 2.75 IN. FABRICATED DOUBLER FROM 2024T3 .071 PO 9002193 DIM 13.125 BY 11.25 AND STRUCTURAL FILLER FROM 2024T3 .063 PO9001684 DIM 15.5 BY 7.875 IAW 727 SRM 53-30-3 FIG 5. REPAIR PARTS TREATED PRIMED AND INSTALLED IAW 727 SRM 51-10-2 AND 53-30-3 FIG 5. 2L73 4F RTA3WE 20050706001982005070600198NM 2005 7 6 DHL2005741585 120050429A5542 SKIN BOEING727 7272Q9 138448MNM RUDDER DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 UPPER RUDDER T/E DENTED 4 INCHES ABOVE 4 TAB HINGE RT. CUT OUT DAMAGED AREA IAW B727 SRM 51-40-2 FIG 1. FABRICATED REPAIR DOUBLER IAW B727 SRM 55-40-2 FIG 2 AND SRM 51-40-2 FIG 1. TREATED AND PRIMED PART AND AREA IAW B727 SRM 51-10-2. INSTALLED REPAIR DOUBLER IAW B727 SRM 51-40-2 FIG 1. 2L73 4F RTA3WE 20050706001992005070600199EA 2005 7 6 COMA0570070 120050617A5755CC670171135 HINGE FITTING CNDAIRCL600 CL6002C10 1390015EA SPOILERS CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01340CA7435 10062 RT MULTI-FUNCTION SPOILER CENTER HINGE FITTING CRACKED IN HALF. REMOVED CRACKED FITTING AND INSTALLED NEW FITTING P/N CC670-17113-5 IAW CRJ AMM 57-73-27-400-801-A01. 2L72 4F RTA21EA 20050706002002005070600200WP 2005 7 6 IXXA05SMN01S 120050427A1430 SCREW DOUG DC8 DC871F 302199DWP RT WING CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX834963359 45993 DURING ROUTINE C CHECK INSPECTION, RT WING, L/E INBD STUB WING UPPER SURFACE SCREWS OXIDIZED, XW 257.000. REMOVED OXIDIZED SCREWS IAW DC-8 SRM 51-3-0 PAGE 1. INSTALLED NEW SCREWS ON RT L/E INBD STUD WING UPPER SURFACE, XW 257.000 IAW DC-8 SRM 51-3-0 PAGE 1. TORQUED FASTENERS IAW DC-8 SRM 51-3-1. 2L74 4F RT4A25 20050706002012005070600201EU 2005 7 6 MALA050482 120050618A2612 FIRE WARNING BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE NR 2 ENGINE ACTIVATED A MALAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 GL15515XJ E2333 CREW REPORTED ENGINE FIRE ILLUMINATION EN ROUTE APPROX 15 MINUTES AFTER TAKEOFF. FLIGHT CREW SHUT ENGINE DOWN AND LIGHT EXTINGUISHED. DIDN'T BLOW FIRE BOTTLES. RETURNED TO AIRPORT. NO FURTHER INFORMATION AVAILABLE AT THIS TIME. REPLACED NR 2 ENGINE LT AND RT FUEL MANIFOLDS. LT FAN DUCT DOOR, AND RT FAN DUCT DOOR SEAL. 2H74 4F4 FRTA49EU E6NE 20050706002022005070600202EA 2005 7 6 COMA0560361 120050620A5240 DOOR CNDAIRCL600 CL6002B19 1900309EA 02 SERVICE OPEN A COMAA UNSCHED LANDING WN INADEQUATE Q C FALSE WARNING CLCLIMB 1 SO01488CA 7730 STALL FAIL CAUTION. FOUND O2 SERVICE DOOR OPEN, CLOSED DOOR. 2L72 4F RTA21EA 20050706002032005070600203EU 2005 7 6 SA05076 120050621A2597 WIRE HARNESS AIRBUSA321 A321211 3930370EU ESCAPE SLIDE MISROUTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19180US 1525 DURING INSPECTION OF RT AFT DOOR ESCAPE SLIDE, LIGHT WIRE HARNESS FOUND MIS-ROUTED. MAINTENANCE CORRECTLY ROUTED LIGHT WIRE HARNESS. OK FOR SERVICE. 2L72 4F RTA28NM 20050706002042005070600204 2005 7 6 SA05077 420050621A2565 LINE AIRBUS320 A320214 3930316EU ESCAPE SLIDE MISINSTALLED A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19108UW 1061 DURING INSPECTION OF AFT LT DOOR ESCAPE SLIDE, GREEN MOORING LINE FOUND INCORRECTLY INSTALLED. MAINTENANCE CORRECTLY INSTALLED GREEN MOORING LINE. 2L72 4F RTA28NM 20050706002052005070600205 2005 7 6 SA05078 420050621A2565 CABLE AIRBUS320 A320214 3930316EU ESCAPE SLIDE MISINSTALLED A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19108UW 1061 DURING INSPECTION OF RT FRONT DOOR ESCAPE SLIDE ASSEMBLY, CABLE FOUND INCORRECTLY INSTALLED. MAINTENANCE INSTALLED CABLE CORRECTLY. 2L72 4F RTA28NM 20050706002062005070600206WP 2005 7 6 AALA20050391 120050616A2913 PUMP DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE RT ENGINE INOPERATIVE A AALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW21460AA 49565 AT FL 230 RT HYDRAULIC PRESSURE BEGAN TO FLUCTUATE VERY RAPIDLY AND FOLLOWED SHORTLY BY RT HYDRAULIC PRESSURE LOW ANNUCIATOR AND RAPIDLY DECREASING HYDRAULIC QUANTITY. TURNED OFF RT ENGINE PUMP AND STOPPED QUANTITY LOSS AT 8. USED MANUAL LANDING GEAR EXTENSION AND LANDED NORMAL WITH GEAR DOORS EXTENDED FOR LANDING. REPLACED RT ENGINE PUMP AND FILTER AND REPLACED PRESSURE LINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 F A6WE E9NE 20050706002082005070600208EU 2005 7 6 AALA20050393 120050618A3350BR964814 LIGHT AIRBUS300 A300B4605R 3930308EU CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2170079 619 EMERGENCY PATH LIGHT AT SEAT 17C INOPERATIVE. REPLACED EMERGENCY PATH LIGHT ASSY FOR SEAT 17C. SYSTEM GROUND CHECKED. NORMAL OPERATION. 2L72 4F RTA35EU 20050706002102005070600210NM 2005 7 6 AALA20050390 120050617A3350BPS73 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21199AN 32393 RT AFT GALLEY DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR RT AFT GALLEY DOOR EMERGENCY LIGHT. SYSTEM GROUND CHECKED. NORMAL OPERATION. 2L72 4F RTA2NM 20050706002122005070600212WP 2005 7 6 AALA20050397 120050620A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21555AN 53085 CEILING EMERGENCY LIGHTS FROM 8DEF TO 16DEF AND ROWS 22 TO 26 INOPERATIVE. REPLACED BATTERY PACK B5101, B5102, AND B5106 FOR CEILING EMERGENCY LIGHTS FROM 8DEF TO 16DEF AND ROWS 22 TO 26. SYSTEM GROUND CHECKED. NORMAL OPERATION. 2L72 4F A6WE 20050706002142005070600214NM 2005 7 6 AALA20050400 120050614A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21907AN 29509 EMERGENCY LIGHTS AT SEAT 19ABC INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT 19ABC. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20050706002162005070600216NM 2005 7 6 AALA20050399 120050610A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21917AN 29518 ALL EMERGENCY LIGHTS IN CABIN FAILED BLEED DOWN TEST. REPLACED BATTERY PACKS FOR ALL EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20050706002172005070600217NM 2005 7 6 DHL2005741591 120050507A5753 SKIN BOEING727 7272Q9 138448MNM TE FLAPS DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 RT I/B FOREFLAP AT I/B HAS DELAMINATED AT CHAFE STRIP. REMOVED CHAFE STRIP ON UPPER IB SURFACE. CUT OUT DELAMINATED AREA AND EXTERNAL DOUBLER FROM 2024T3 .016 PO9001660. CLEANED, PREPPED, APPLIED PRIMER AND ADHESIVE TO REPAIR PARTS AND SURFACE. VACUUM BAGGED FOR BONDING. BONDED, CLEANED, TREATED, PRIMED AND SEALED REPAIR BONDED REPLACEMENT CHAFE STRIP IAW B727 SRM 51-40-20 FIG 30 57-50-2 FIG 3 MM 51-51-11. 2L73 4F RTA3WE 20050706002182005070600218NM 2005 7 6 DHL2005741757 120050426A5322 SHEAR TIE BOEING727 7272Q9 138448MNM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 FRAME SHEAR TIE CORRODED AT STA 1148 FROM STR 28L-27R. REMOVED INTERCOASTAL AT BS 1148 STR 29 R CUT OUT DAMAGED SHEAR TIE FROM STR 28R - STR 30 IAW B727 SRM 53-10-4 FIG NR 13. FABRICATED 4EA SHEAR TIE SECTION 7075-T6 .071 PO9001298 DIM 4 BY 3 IN. IAW B727 SRM 53-10-4 FIG 13. ALODINE AND PRIMED 4EA SHEAR TIE SECTION IAW B727 SRM 51-10-2. REMOVED CORROSION BS 1148 AT STR 27L-29L AND 27R MAX MAT'L LOSS .005 AND IS WITHIN THE ALLOWABLE LIMITS OF 10% IAW B727 SRM 53-10-1 FIG 1. INSTALLED NEW SHEAR TIE ANGLE REPAIR IAW B727 SRM 53-10-4 FIG 13. 2L73 4F RTA3WE 20050706002202005070600220EA 2005 7 6 COMA0560358 120050619A3320BC10059001 LIGHT CNDAIRCL600 CL6002B19 1900309EA GALLEY MELTED A COMAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO01971CA 7145 BURNING ODOR IN COCKPIT. REPLACED GALLEY OVERHEAD LAMP ASSEMBLY. 2L72 4F RTA21EA 20050706002222005070600222EA 2005 7 6 COMA0560362 120050621A261347259701 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA DETECTION SYS MALFUNCTIONED A COMAE ENGINE SHUTDOWN N FALSE WARNING APAPPROACH 1 SO01781CA15817 7312 RT JET PIPE OVERHEAT AND APU FIRE FAIL CAUTION. CREW DECLARED EMERGENCY AND SHUTDOWN RT ENGINE. ACFT LANDED WITHOUT INCIDENT. REPLACED FIRE OVERHEAT CONTROLLER. 2L72 4F RTA21EA 20050706002242005070600224NM 2005 7 6 AWXA200500729 120050607A5320146N85614 THRESHOLD BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28905AW 23567 DURING C-10 CHECK, FOUND CORROSION IN AFT CARGO BAY ON UPPER SURFACE OF CARGO FLOOR AT THRESHOLD PLATE BETWEEN STA 1380 TO STA 1440, WL 142, STRINGER 27R. MX REMOVED CORRODED THRESHOLD PLATE BETWEEN STA 1380 TO STA 1440, WL 142, STRINGER 27R AND INSTALLED NEW THRESHOLD PLATE IAW BOEING 757 SRM 53-00-53, 51-70-01, AND 51-40-02. 2L72 4F RTA2NM 20050706002262005070600226NM 2005 7 6 AWXA200500731 120050608A53156546812186 FLOORBEAM BOEING737 7373B7 1384580NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28328AW 23377 DURING C-13 CHECK, FOUND CORROSION ON FLOORBEAM FROM BS 986.5 TO BS 1006, WL 204, BL 16R. OUT OF LIMITS IAW BOEING 737-300 SRM 56-60-51 FIG 101. REMOVED CORRODED BEAM AT BS 986.5 TO BS 1006, WL 204, BL 16R IAW BOEING 737-300 SRM 53-60-51-1. INSTALLED NEW BEAM FROM BS 986.5 TO BS 1006, WL 204, BL 16R IAW BOEING 737-300 SRM 51-40-02-0 FIG 12. 2L72 4F RTA16WE 20050706002282005070600228NM 2005 7 6 AWXA200500733 120050609A53156545834256 STIFFENER BOEING737 7373B7 1384580NM FLOORBEAM CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28328AW 23377 DURING C-13 CHECK, FOUND GALVANIC CORROSION ON FLOORBEAM STIFFENER LOCATED AT BS 325, BL 12R, WL 208. MX REMOVED CORROSION AT BS 325, BL 12R, WL 208 IAW BOEING 737-300 SRM 51-10-02 AND DETERMINED CORROSION TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-10-51-1 FIG 101. REMOVED FLOORBEAM STIFFENER AT BS 325, BL 12R, WL 208 AND INSTALLED NEW FLOORBEAM STIFFENER IAW BOEING 737-300 SRM 51-40-02-2 FIG 12. 2L72 4F RTA16WE 20050706002302005070600230NM 2005 7 6 DHL2005741 120050502A5330 SKIN BOEING727 7272Q9 138448MNM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 AFT CARGO INNER FUSELAGE SKIN AT BS 154 O/B OF STR 28R IS CORRODED. REMOVED FASTENER AT DAMAGED AREA FROM BS 1148 TO BS 1166 IAW B727 SRM 53-30-3 FIG 1. DAMAGE BEYOND ALLOWABLE LIMITS IAW B727 SRM 53-30-1 FIG 1. FABRICATED FILLER AND DOUBLER IAW B727 SRM 53-30-3 FIG 1. TREATED AND PRIMED REPAIR PARTS IAW B727 SRM 51-10-2. INSTALLED REPAIR FILLER AND DOUBLER IAW B727 SRM 53-30-3 FIG 1. 2L73 4F RTA3WE 20050706002322005070600232NM 2005 7 6 SB05074 120050620A21337207375 OUTFLOW VALVE BOEING737 737301 1384611NM CABIN PRESSURE FAULTY A USAAO OTHER J WARNING INDICATION CRCRUISE 1 EA19575US61 61 23740 AT FL330, CREW REPORTED CABIN BEGAN A 6,000 FPM CLIMB. AUTO FAIL LIGHT ILLUMINATED ALONG WITH STANDBY ON LIGHT. CREW SWITCHED TO MANUAL AC/DC PRESSURIZATION MODE AND CONFIRMED OUTFLOW VALVE FULLY CLOSED. CREW APPLIED THRUST ON ENGINES AND DESCENDED TO LOWER ALTITUDE TO CONTROL CABIN. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED BOTH CABIN PRESSURE SAFETY RELIEF VALVES PER MM 21-32-21. OPERATIONAL CHECK AND LEAK CHECK GOOD. PERFORMED SATISFACTORY TEST FLIGHT. AIRCRAFT OK FOR SERVICE. 2L72 4F RTA16WE 20050706002332005070600233EA 2005 7 6 COMA0560355 120050616A2910AE2460010H0264 LINE CNDAIRCL600 CL6002B19 1900309EA NR 2 HYD SYS LEAKING A COMAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO01797CA 7344 RECEIVED A HYDRAULIC NR 2 LOW PRESSURE CAUTION MESSAGE. CREW DECLARED EMERGENCY AND DIVERTED TO IAD. ACFT LANDED WITHOUT INCIDENT. REPLACED LEAKING NR 2 EDP PRESSURE LINE. 2L72 4F RTA21EA 20050706002352005070600235WP 2005 7 6 IXXA05SMN37S 120050429A5340 FITTING DOUG DC8 DC871F 302199DWP FWD CARGO BAY BROKEN A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX834963359 45993 DURING ROUTINE C-CHECK INSPECTION, FWD CARGO COMPARTMENT FITTING BROKEN, 70.000 L-31L. REMOVED BROKEN FITTING IAW DC-8 SRM 51-120D PAGE 21. CLEANED, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8B. INSTALLED NEW FITTING DC-8 SRM 51-1-20D PAGE 9. TORQUED IAW DC-8 SRM 51-3-1. 2L74 4F RT4A25 20050706002362005070600236EA 2005 7 6 COMA0570072 120050617A531267053110521 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01340CA7435 10062 LT AND RT LOWER WEBS BELOW FLOOR AT FS 280 ARE CORRODED FROM LBL36 TO RBL36. REMOVED CORRODED WEBS AND INSTALLED NEW WEBS IAW REO 6670-53-11-052 REV A. 2L72 4F RTA21EA 20050706002372005070600237EA 2005 7 6 COMA0570073 120050620A5753 VANE CNDAIRCL600 CL6002C10 1390015EA TE FLAPS CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01340CA7435 10062 RT OUTBOARD FLAP VANE IS CRACKED. REPAIRED RT OUTBOARD FLAP VANE UPPER SKIN IAW BRAS EO 601R-52-6696. 2L72 4F RTA21EA 20050706002382005070600238SO 2005 7 6 C2XA05CL052 120050620A521014532437003 LEVER EMB 145 EMB145LR 3260212SO MAIN CABIN DOOR BENT A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713988 145265 CREW REPORTED MAIN CABIN DOOR DIFFICULT TO SHUT AND NOT INDICATING CLOSED. MX INSPECTED AND REPLACED SPRING LEVER ON FOLDING FLAP ACTUATING CAM. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20050706002392005070600239NM 2005 7 6 DHL2005741575 120050425A5347 SEAT TRACK BOEING727 7272Q9 138448MNM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741 21931 SEAT TRACK 24L AT BS 760 TO 848 CORROSION. REMOVED SEAT TRACK AT BS 760-848 LBL 24 IAW B727 RSM 51-30-2 FIG 7. REPLACED, LOCATED AND DRILLED FASTENER HOLES IN PN BAC 1520-841 PO NR 9002155 (8FT) IAW B727 SRM 51-30-2. TREATED AND PRIMED AREA AND PART IAW B727 SRM 51-10-2. INSTALLED SEAT TRACK IAW B727 SRM 51-30-2 FIG 15 AND 53-10-5 FIG 1. 2L73 4F RTA3WE 20050706002402005070600240WP 2005 7 6 IXXA05SMN38S 120050429A5330 SKIN DOUG DC8 DC871F 302199DWP OVERWING EXIT CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX834963359 45993 FUSELAGE EXTERIOR SKIN LOCAL CORROSION, STA 700.000 STA 708.000, L-32R. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05163 DATE 04-28-05; SEMAN DWG ED-3961 DATED 04-20-05. REMOVED DAMAGED PLATING SEGMENT IAW SEMAN DWG ED-3961. PERFORMED NDT INSPECTION IAW DC-8 NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER STRAP (ALCLAD 7075 T6 0.090”), REPAIR TRIPLER STRAP (ALCLAD 7075 T6 0.100”), PLATING SEGMENT (ALCLAD 7075 T6 0.125”) IAW SEMAN DWG ED-3961. CLEANED, TREATED AND PRIMED REPAIR PARTS IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11 PAGE 9. INSTALLED REPAIR PARTS IAW SEMAN DWG ED-3961, DC-8 SRM 51-1-20D PAGE 9, DC-8 SRM 51-3-1 PAGE 1, DC-8 SRM 51-3-0 PAGE 1. 2L74 4F RT4A25 20050706002412005070600241WP 2005 7 6 IXXA05SMN39S 120050429A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX834963359 45993 FUSELAGE SKIN CORRODED STA 700.00 STA 708.000 L-32L. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05163 DATE 04-28-05; SEMAN DWG ED-3961 DATED 04-20-05. REMOVED DAMAGED PLATING SEGMENT IAW SEMAN DWG ED-3961. PERFORMED NDT INSPECTION IAW DC-8 NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER STRAP (ALCLAD 7075 T6 0.090”), REPAIR TRIPLER STRAP (ALCLAD 7075 T6 0.100”), PLATING SEGMENT (ALCLAD 7075 T6 0.125”) IAW SEMAN DWG ED-3961. CLEANED, TREATED AND PRIMED REPAIR PARTS IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11 PAGE 9. INSTALLED REPAIR PARTS IAW SEMAN DWG ED-3961, DC-8 SRM 51-1-20D PAGE 9, DC-8 SRM 51-3-1 PAGE 1, DC-8 SRM 51-3-0 PAGE 1. 2L74 4F RT4A25 20050706002422005070600242WP 2005 7 6 IXXA05SMN40S 120050429A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX834963359 45993 DURING ROUTINE C-CHECK INSPECTION, FUSELAGE L-35L CORRODED, STA 690.000 STA 781.000. REMOVED LEVEL I CORROSION IAW DC-8 SRM 51-1-8 PAGES 17-18. PERFORMED BLEND OUT 0.003”. MATERIAL THICKNESS 0.160”, REMAINING MATERIAL 0.157 FOUND WITHIN ALLOWABLE LIMITS IAW DC-8 SRM 53-2-0 FIG 11 SHEET 3 PAGE 2P. CLEANED, TREATED AND PRIMED IAW DC-8 SRM 51-1-8B. 2L74 4F RT4A25 20050810002822005081000282EA 2005 8 10 A6WA200540266 120050724A5510600214021 FITTING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LOOSE A A6WAK NONE O OTHER ININSP/MAINT 1 GL31420AW 7640 HORIZONTAL STABILIZER FORWARD STEADY FITTING HAS 3 LOOSE MOUNT BOLTS ON LT SIDE OF FITTING. REMOVED BOLTS, VISUALLY INSPECTED HARDWARE AND HOLES, REINSTALLED BOLTS AND TORQUED IAW AMM. (K) 2L72 4F4 FRTA21EA E15NE 20050810002852005081000285SO 2005 8 10 SIM2005F00009 120050720A573014566209007 SKIN EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL LT WING DAMAGED A SIMAO OTHER O OTHER ININSP/MAINT 1 SW21925AE 14500908 LT AILERON AND WING WERE DAMAGED BY A CATERING TRUCK. MAINTENANCE REPLACED LT WING SPAR SEGMENT AND WING SKIN. REPLACED LT AILERON IAW EO. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4T4 FRTT00011ATTE6CH 20050810002892005081000289EA 2005 8 10 A6WA200540268 120050724A5551600214021 FITTING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE HZ STAB LOOSE A A6WAK NONE O OTHER ININSP/MAINT 1 GL31405AW 7362 HORIZONTAL STABILIZER FORWARD STEADY FITTING HAS 6 LOOSE MOUNT BOLTS. REMOVED BOLTS, VISUALLY INSPECTED HARDWARE AND HOLES, REINSTALLED BOLTS AND TORQUED IAW AMM. (K) 2L72 4F4 FRTA21EA E15NE 20050810002952005081000295SO 2005 8 10 SIMA200520605 120050720A5330AL2027T3 SKIN EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FR 10,11 DAMAGED A SIMAO OTHER O OTHER NRNOT REPORTED 1 SW21811AE8528 145529 LOWER FUSELAGE SKIN WAS DAMAGED BETWEEN FRAMES 10, 11 AND STRINGERS 20R AND 21R. REMOVED THE DAMAGED SKIN BY MAKING A CUT OUT. FABRICATED A FILLER AND DOUBLER. REPAIR DONE IAW SRM. (K) 2L72 4F4 FRTT00011ATTE6CH 20050810003062005081000306NM 2005 8 10 DHL2005746523 120050705A5310 CROSSBEAM BOEING727 727224 1384076NM CRACKED A DHLAO OTHER O OTHER ININSP/MAINT 1 SO01746DH 22252 E&E DOORS AFT CROSS MEMBER IN ENTRYWAY CRACKED INSIDE LIP 4.5 INCHES OFF CENTER RT SIDE (MARKED). REMOVED FASTENERS AND FRAME IAW B727 SRM 51-30-2. FABBED NEW FRAME 7075 T6 PO9001873 1050 24"X6" IAW B727 SRM 53-10-2 FIG 1. TREATED AND PRIMED PART IAW B727 SRM 51-10-2. INSTALLED NEW FRAME AFT OF E&E DOOR IAW B727 SRM 51-30-2. 2L73 4F A3WE 20050810003092005081000309NM 2005 8 10 DHL2005746529 120050807A5320 SUPPORT BOEING727 727224 1384076NM AIRSTAIR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01746DH 22252 AFT AIRSTAIR RT LWR TORQUE BOX HORIZONTAL SUPPORT IS CRACKED AT STA 1263 RBL 18 NDT VERIFIED. REMOVED CRACKED EXISTING REPAIR IAW B727 SRM 51-30-2. FABBED NEW ANGLE REPAIR MAT 15-5 PH SS .063 PO 315722 8"X 3 1/2" IAW B727 SRM 53-10-2 FIG 1, S/B 727-53-0129 & SRM 51-40-3 FIG 1. TREATED AND PRIMED PART IAW B727 SRM 51-10-2. INSTALLED REPAIR ANGLE IAW B727 SRM 51-40-3 FIG 1 AND S/B 727-53-0129. 2L73 4F A3WE 20050810003162005081000316NM 2005 8 10 DHL2005746517 120050703A5320 WEB BOEING727 727224 1384076NM TORQUE BOX CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01746DH 22252 C-CHECK POSSIBLE CRACK IN UPPER TORQUE BOX WEB BS 1303 AT LWR LT CORNER ACCESS BY PNL 9504 (MARKED IN RED). STOP DRILLED IAW B727 SRM 51-10-1, HFEC VERFIED STOP DRILLED IAW B727 NDT MAN.PH.4 51-00-00 FIG 23. C/W COTNEY AEROSPACE EAZ04.3 DATED 7/26/05. 2L73 4F A3WE 20050810003472005081000347WP 2005 8 10 ASAA0580258 120050515A534759305471 SEAT TRACK DOUG DC9 DC983 3022083WP FS 218-237 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - DURING C-CHECK, FOUND CABIN SEAT TRACK BL 44 STATION 218-237 IS CORRODED. REMOVED AND REPLACED DAMAGED SECTION OF TRACK. (M) 2L72 4F RTA6WE 20050810003572005081000357WP 2005 8 10 ASAA0580316 120050613A5320993656435 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FS 180 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - DURING HV-CHECK, FOUND CABIN FLOOR PANEL SUPPORT CORRODED. REPLACED FLOOR PANEL SUPPORT. (M) 2L72 4F RTA6WE 20050810003582005081000358WP 2005 8 10 ASAA0580313 120050613A532199365533 FLOOR PANEL DOUG DC9 DC983 3022083WP FS 200-256 BROKEN A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - DURING HV-CHECK, FOUND CABIN FLOOR PANEL BROKEN. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050810003622005081000362WP 2005 8 10 ASAA0580318 120050613A53209936534165 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FS 160-200 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - DURING HV-CHECK, FOUND CABIN FLOOR PANEL SUPPORT CORRODED. REPLACED FLOOR PANEL SUPPORT. (M) 2L72 4F RTA6WE 20050810003652005081000365NM 2005 8 10 DHL2005746518 120050703A5330 SKIN BOEING727 727224 1384076NM BS 1123 DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01746DH 22252 C-CHECK DENT RT SIDE FUSELAGE SKIN STA 1123 ABOVE STR 27R (MARKED). CUT OUT DAMAGE AREA OF SKIN AT STA 1123 ABOVE STR 27R DIMENSIONS 2.5"X 1", FABBED REPAIR DOUBLER FROM .063 2024T3 PO 9002199 IAW B727 SRM 53-30-2 FIG 2 & 53-30-3 FIG 1, DIMENSIONS 11.25"X 7.5", TREATED AND PRIME IAW B727 SRM 51-10-2, INSTALLED REPAIR IAW B727 SRM 53-30-3 FIG 1 AND 51-30-2. THIS IS A CAT-A REPAIR. 2L73 4F A3WE 20050810003702005081000370WP 2005 8 10 05FDEA02358 120050809A5754 RIB DOUG MD10 MD1010F 3022112WP ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25564FE 46984 SLAT 2 R O/B SIDE ON RIB FOUND 1EA CRACK 2" LONG. REPAIR PER SRM 57-00-01 VOL 1 FIG 10 SHT 2 AND SRM 51-35-01 PAR 1-5 VOL 2. 2L73 4F RTA22WE 20050811000022005081100002NM 2005 8 11 UPS05445141 120050723A531165B0434069 FRAME BOEING747 747121 1384871NM M/D CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE:C M/D BS 2060 BETWEEN STR 25-26L FRAME FOUND CRACKED (CRACK LENGTH .375 INCH). M/D BS 2060 BETWEEN STR 26L - 26L FRAME REPAIRED AS PER HX RS R53-62-35347 & UPS EO B747-5310-22631-A7. 2L74 4F A20WE 20050811000082005081100008WP 2005 8 11 05FDEA02335 120050809A5720 ANGLE DOUG DC10 DC1010 3022110WP LT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25564FE 46984 LEFT WING FWD INT L/E XOS 667 EXISTING REPAIR ANGLE ON INTERNAL STIFFENER. REPAIR IS IN COMPLIANCE WITH SRM 51-00-01 FIG 100 VOL 1. 2L73 4F A22WE 20050811000112005081100011WP 2005 8 11 05FDEA02338 120050809A5311 FRAME DOUG DC10 DC1010 3022110WP FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25564FE 46984 RT SIDE AT STA 1119 FROM L NR 44 TO 50 FOUND 1EA NEW FRAME ABOUT 33 INCHES LONG WITH TWO SPLICE ANGLES. ACCOMPLISH REPAIR PER EA 8-5310-87669. 2L73 4F A22WE 20050811000122005081100012WP 2005 8 11 05FDEA02349 120050809A5754 ANGLE DOUG DC10 DC1010 3022110WP ZONE 500 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25564FE 46984 LT WING SLAT 2 XDLE 309 EXISTING REPAIR ANGLE ON CLOSURE ANGLE. REPLACE REPAIR PER SRM 57-00-01 FIG 10 VOL 1. 2L73 4F A22WE 20050811000202005081100020WP 2005 8 11 05FDEA02343 120050809A5754 SKIN DOUG MD10 MD1010F 3022112WP NR 1 SLAT DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25564FE 46984 RIGHT WING SLAT NR 1 XCW 118 EXISTING 1 EA REPAIR DOUBLER ON UPPER SKIN. REPLACED REPAIR PER SRM 57-10-00 FIG 84 SHEET 2 VOL 1. 2L73 4F RTA22WE 20050811000212005081100021WP 2005 8 11 05FDEA02344 120050809A5311 FRAME DOUG MD10 MD1010F 3022112WP RT DROOP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25564FE 46984 RIGHT DROOP L/E INTERNAL SIDE FOUND CRACKED FORMER ON UPPER EDGE AT XORS 299. REPAIR PER SRM 53-00-01 FIG 8 SHEET 1, 3, 4. 2L73 4F RTA22WE 20050811000362005081100036WP 2005 8 11 05FDEA02355 120050809A5710 BULKHEAD DOUG MD10 MD1010F 3022112WP ZONE 600 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25564FE 46984 RIGHT WING XORS 372 FWD OF STR 12 BULKHEAD CAP CRACKED BETWEEN FASTENERS. REPAIR PER EA 8-5710-84863. 2L73 4F RTA22WE 20050811000372005081100037WP 2005 8 11 05FDEA02356 120050809A5330 SKIN DOUG MD10 MD1010F 3022112WP ZONE 100 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25564FE 46984 LWR FUSELAGE AT STA 1781 BETWEEN L38-41 RT EXISTING TWO EXTERNAL REPAIR DOUBLER ON SKIN. INSTALLED REPAIR DOUBLER PER SRM 53-50-00 FIG 26 VOL 1. 2L73 4F RTA22WE 20050811000582005081100058CE 2005 8 11 DXTA200500871 120050727A3240 LINE CESSNA560 560XL 2076702CE HYDRAULIC SYS LEAKING E DXTAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07625QS 5605319 PILOT AND COPILOT BRAKES SPONGY. INSPECTED LT AND RT MAIN BRAKES WEAR INDICATORS ARE WITHIN LIMITS. CHECKED BRAKE ACCUMULATOR AND BRAKE RESERVOIR ARE GOOD. BLEED LEFT AND RT MAIN BRAKE IAW CITATION 560 M/M CH 32-42-00. TAXIED AIRCRAFT AND BRAKE CHECK WAS GOOD. 2L72 4F RTA22CE 20050811000602005081100060CE 2005 8 11 DXTA200500876 120050731A3297 WIRE CESSNA500 560CESSNA 2076750CE LT MLG BROKEN E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07341QS 5600341 LEFT MAIN GEAR WOULD NOT RETRACT ON GEAR RETRACTION (CYCLED GEAR DOWN) 3 GREEN INDICATED. PUT AIRCRAFT ON JACKS, SWUNG GEAR 10 TIMES NO PROBLEMS. FOUND ON 11TH GEAR SWING, GEAR CAME UP BUT GOT GEAR UNSAFE LIGHT WITH GEAR DOWN. FOUND BROKEN WIRE TO LT MAIN GEAR DOWN LOCK SWITCH REPAIRED WIRE AND PERFORMED SWINGS OF SYSTEM NO PROBLEMS FOUND PERFORMED GEAR OPERATIONAL CHECKS IAW CESSNA 560 MM CH 32-00-00 AND 32-31-04. 2L72 4F RTA22CE 20050811000772005081100077WP 2005 8 11 ASAA0580331 120050613A5313591143289 LONGERON DOUG DC9 DC983 3022083WP FS 1429-1430 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - DURING HV CHECK, FOUND LONGERON 2L CRACKED. REPLACED DAMAGED SECTION OF LONGERON. (M) 2L72 4F RTA6WE 20050811001162005081100116WP 2005 8 11 UPS05845111 120050711A53403779762U1 FITTING DOUG DC8 DC873F 302199FWP STA 690 L4L CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C1, LONGERON END FITTING CRACKED AT STA 690 L4L. REMOVED CRACKED END FITTING AT STA 690 L4L IAW SRM 53-2-2. REPLACED END FITTING AT STA 690 L4L IAW SRM 51-1-20 AND 51-3-0. 2L74 4F RT4A25 20050811001172005081100117WP 2005 8 11 UPS05845123 120050711A5310 FITTING DOUG DC8 DC873F 302199FWP FS1770 L17L CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE:C1 60 COMPT L17L AT 1770 HAS 6 INCH CRACK AT END FITTING. REMOVED FITTING AND SUPPORT FROM STA 1770 L17L IAW SRM 51-1-20D, FABRICATED AND INSTALLED LONGERON END SPLICE FITTING AT STA 1170 1793 IAW DWG S-1616757 AND SRM 51-1-8. 2L74 4F RT4A25 20050811001332005081100133NM 2005 8 11 UPS05445126 120050721A5350 SUPPORT BOEING747 747121 1384871NM FAIRING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE:C AIR CONDITIONING BAY BODY FAIRING SUPPORT FOUND CORRODED AT BS 1155 LBL 65. CORROSION BLEND OUT 0.043" X 1" X 1.5" EXCEED SRM 53-50-01 FIG 5 LIMITS, SUPPORT REPAIRED AT LBL 65" AS PER SRM 51-40-04 FIG 1. 2L74 4F A20WE 20050811001432005081100143SO 2005 8 11 CHQA200500138 120050806A33501317 BULB EMB 145 EMB145LR 3260212SO CABIN BURNED OUT A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11573RP 14500837 EMERGENCY LIGHTS IN ENTRY ARE INOP. BULB APPEARS BURNED OUT. RELAMPED PASSENGER DOOR EMERGENCY EXIT LIGHT IAW EMB 145 AMM 33-50-09. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050811001442005081100144CE 2005 8 11 DXTA200500886 120050808A3260387 LIGHT CESSNA560 560XL 2076702CE INIDCATOR BURNED E DXTAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL07659QS 5605359 LEFT LANDING LIGHT INDICATOR WOULD NOT ILLUMINATE, HAD TO FOLLOW THE EMERGENCY GEAR EXTENSION PROCEDURE, BLEW GEAR DOWN. T/S INDICATOR. RESET GEAR BLOW DOWN BOTTLE. SERVICED BOTTLE. CYCLED GEAR. FOUND BOTH BULBS IN LT DOWN AND LOCKED INDICATOR BURNED OUT. REMOVED AND REPLACED BOTH BULBS. OPS CHECK GOOD IAW CE 560XL M/M. 2L72 4F RTA22CE 20050811001502005081100150CE 2005 8 11 DXTA200500890 120050809A3240 BRAKE CESSNA750 750 2076810CE LEFT STICKING E DXTAD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07999QS 7500203 WHILE TAXIING, DURING BRAKE TEST, THE LEFT MAIN BRAKES SEEMED TO BE STICKING, AN ABRUPT PULLING TO THE LEFT, COULD NOT HOLD A/C STRAIGHT EVEN WITH DIFFERENTIAL BRAKING . HYDRAULIC PRESSURE NORMAL. 2L72 4J RTT00007WI 20050811001532005081100153NM 2005 8 11 UPS05445089 120050723A532265B04332175 SHEAR TIE BOEING747 747121 1384871NM M/D CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 BS 1900 S23-24R STRINGER SHEAR TIE FOUND CRACKED, CRACK LENGTH 7/16". BS 1900 STR 23-24R STRINGER SHEAR TIE REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050811001662005081100166EA 2005 8 11 ASOA05630 120050724A5312 PRESSURE PANEL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27833AS 7246 DURING A C-CHECK, CORROSION WAS FOUND BEYOND LIMIT ON THE PRESSURE FLOOR SKIN LT SIDE BETWEEN 409 AND 128 TO 559 RBL 36 AND 45. MAINTENANCE HAS SUBMITTED A DAMAGE REPORT AND IS AWAITING AN REO FOR REPAIR. THIS MRR WILL REMAIN OPEN UNTIL THE PROPER DOCUMENTATION IS OBTAINED AND THE REPAIR CAN BE COMPLIED WITH. (K) 2L72 4F4 FRTA21EA E15NE 20050811001672005081100167EA 2005 8 11 ASOA05632 120050724A5210601R3807413 ANCHOR FITTING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PASSENGER DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27886AS 7531 DURING HANGAR MAINTENANCE, THE AFT ANCHOR FITTING ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE COMPLIED WITH REO, A TEMPORARY REPAIR VALID FOR 100 FLIGHT HOURS FROM DATA OF INCORPORATION. THIS MRR WILL REMAIN OPEN PENDING COMPLETION OF PERMANENT REPAIR. (K) 2L72 4F4 FRTA21EA E15NE 20050811001682005081100168EA 2005 8 11 ASOA05634 120050725A3350362624 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27847AS 7335 DURING INSPECTION, THE GREEN EMERGENCY LIGHTING FORWARD OF ROW 5 WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE INOPERATIVE SECTION OF EMERGENCY FLOOR STRIP LIGHTING. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050811001822005081100182NM 2005 8 11 UPS05M45102 120050607A5311 FRAME DOUG MD11 MD11F 3023600NM AIR CON SYS NR 1CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01255UP 48404 INSPECTION TYPE:C-CHECK AIR-CON SYS NR 1 COMPT O/B OF EXHAUST RAM AIR DOOR CORROSION FOUND ON FR FRAME AS MARKED. CORROSION REMOVED AND TREATED AS PER SRM 51-21-01 VOL II REV 37, FOUND WITHIN LIMIT AS PER SRM 53-00-01 VOL I REV 37. 2L73 4F RTA22WE 20050811001832005081100183NM 2005 8 11 UPS05M45103 120050608A5313 LONGERON DOUG MD11 MD11F 3023600NM CTR CGO COMPT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01255UP 48404 INSPECTION TYPE:C-CHECK CTR CARGO COMPT AT STA 1701 LONGERON 51LT TO 51RT FOUND TRANSVERSE WITH CORROSION. CORROSION REMOVED AS PER SRM 53-30-00 VOL I FIG 7 REV 37 ON CTR CARGO AT STA 1701 LONGERON 51LT TO 51RT TRANSVERSE AND FOUND WITHIN LIMIT AS PER SRM 53-00-01 VOL I FIG 1A REV 37 AND REWORKED AREA REPROTECTED AS PER SRM 51-21-01 VOL II REV 37. 2L73 4F RTA22WE 20050811001842005081100184NM 2005 8 11 UPS05M45104 120050608A5313 LONGERON DOUG MD11 MD11F 3023600NM CTR CGO COMPT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01255UP 48404 INSPECTION TYPE:C-CHECK CTR CARGO COMPT AT STA 1801 LONGERON 51 LT TO 51 RT TRANSVERSE AREA WITH CORROSION AS MARKED. CORROSION REMOVED AS PER SRM 53-30-01 VOL 1 FIG 7 REV 37 ON CTR CARGO AT STA 1801 LONGERON 51 LT TO 51 RT TRANSVERSE AREA AND FOUND WITHIN LIMIT AS PER SRM 51-00-01 VOL 1 FIG 1A REV 37, REWORKED AREA REPROTECTED AS PER SRM 51-21-01 VOL II REV37. 2L73 4F RTA22WE 20050811001862005081100186NM 2005 8 11 UPS05M45106 120050608A5321 FLOOR PANEL DOUG MD11 MD11F 3023600NM CTR CGO COMPT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01255UP 48404 INSPECTION TYPE:C-CHECK CTR CARGO COMPT AT STA 1701 CENTERLINE FLOOR PANEL SUPPORT TOPP SURFACE WITH SLIGHT CORROSION AS MARKED. CORROSION REMOVED AS PER SRM 53-00-01 VOL I FIG 1A REV 37 ON CTR CARGO AT STA 1701 CENTERLINE FLOOR SUPPORT SURFACE AND FOUND WITHIN LIMIT AS PER SRM 53-00-01 VOL I REV 37 AND REPROTECTED AS PER SRM 51-21-01 VOL II REV 37. 2L73 4F RTA22WE 20050811001892005081100189NM 2005 8 11 UPS05M45109 120050613A5313 LONGERON DOUG MD11 MD11F 3023600NM CAC COMPT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01255UP 48404 INSPECTION TYPE:C-CHECK CAC COMPT STA 1156 LONG 52 CORROSION FOUND AS MARKED. CORROSION REMOVED & TREATED AS PER SRM 51-21-01 VOL II REV 37 FOUND WITHIN LIMIT AS PER SRM 53-00-01 REV 37. 2L73 4F RTA22WE 20050811001922005081100192NM 2005 8 11 UPS05445134 120050722A531165B0172545 FRAME BOEING747 747121 1384871NM M/D CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE:C M/D BS 640 LT STR 24L & 25L FRAME FOUND CRACKED (CRACK LENGTH 1/2" & 0.75"). M/D BS 640 LT STR 23 TO STR 26 AREA FRAME REPAIRED AS PER HX RS R53-22-35339 & UPS EO B747-5310-22627-A. 2L74 4F A20WE 20050811001962005081100196NM 2005 8 11 UPS05445138 120050723A531165B041726 FRAME BOEING747 747121 1384871NM FWD CARGO CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE:C FWD CARGO RT STA 760 FRAME UPPER FLANGE AT RBL 60 FOUND CRACKED (CRACK LENGTH 1/2", 5/8", 1.125"). FRAME REPAIRED AS PER HX RS R53-22-35341 & UPS EO B747-5310-22629-A. 2L74 4F A20WE 20050811002002005081100200WP 2005 8 11 IXXA05SMN115S 120050627A5730 SKIN DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE XF 226.000 NICKED B IXXAO OTHER O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSP, LT OB FLAP L/E NICKED, XF 226.000 (UPPER PART) PERFORMED MAJOR REPAIR, DWG NR ED 3987 DATE 06-20-05, EO. REMOVED FASTENERS IAW SRM. REMOVED DAMAGED PLATING SEGMENT IAW DWG ED 3987. PERFORMED NDT INSP IAW SPM. NO CRACK, CORROSION FOUND. FABRICATED NEW PLATING SEGMENT (ALCLAD 2024 T3 0.071) + INTERNAL SPLICE (ALCLAD 2024 T3 0.080) + (02 EA) EXTERNAL DOUBLERS (ALCLAD 2024 T3 0.071”) IAW DWG ED 3987, SRM. CLEANED, TREATED AND PRIMED AREA + REPAIR PARTS (INTERNAL PART) IAW SRM. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PAGE 9. INSTALLED REPAIR PARTS IAW SEMAN DWG ED 3987, SRM 51-1-21 PAGE 1, SRM 51-3-0 PAGE 1, SRM 51-1-20D PAGE 9. TORQUED IAW SRM 51-3-1. 2L74 4F4 FRT4A25 E2GL 20050811002042005081100204WP 2005 8 11 IXXA05SMN156S 120050706A5730 SKIN DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE XS250.089 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, RT WING IB L/E UPPER PART EXTERNAL SKIN CORRODED XS 250.089. PERFORMED MAJOR REPAIR IAW SRM, TR NR 57-85, EO SEMAN NR 2005984 DATE 06-18-05. REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1, SRM. REMOVED CORROSION IAW SRM. FOUND OUT OF LIMITS IAW SRM. REMOVED CORRODED AREA IAW SRM 57-2-1 FIG. 38. PERFORMED VISUAL INSPECTION NO CRACK, CORROSION FOUND. FABRICATED DOUBLER (ALCLAD 7075 T6 0.071) + FILLER (ALCLAD 7075 T6 0.063) IAW SRM 57-2-1 FIG. 38, SRM 57-3-1 FIG. 3. CLEANED, TREATED AND PRIMED AREA + REPAIR PART INTERNAL PART IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PAGE 9. INSTALLED REPAIR PARTS WITH NEW FASTENERS IAW SRM, TORQUED IAW SRM 51-3-1. 2L74 4F4 FRT4A25 E2GL 20050811002142005081100214EU 2005 8 11 08022005A 120050802A2161 CONTROLLER SAAB SF340 340B 7860101EU GE CT7TS CT71 30030NE TEMP MALFUNCTIONED A NSVAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA27307CE 204 LT AND RT TEMP CONTROLLERS UNCONTROLLABLE IN BOTH MODES. RAN A/C LT OPS CHECK GOOD, MEL'D RT ACM. 2L72 4T4 URTA52EU E8NE 20050811002172005081100217EU 2005 8 11 ALGA105168 120050729A6510C651A2001101 COUPLING UROCOPEC120 EC120B 8680987EU CRACKED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03510AL2162 1251 CRACKED LAMINATE / REPLACED WITH NEW BY FIELD MAINTENANCE. 1G72 3U NCR0001RD 20050811002192005081100219NM 2005 8 11 HNAA0500074 120050808A2761 ACTUATOR DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE SPOILER LEAKING A HNAAO OTHER K FLUID LOSS LDLANDING 1 EA07907HA 011 ON TOUCHDOWN, LOST NORMAL BRAKING, DUE TO LOSS OF NR 1 HYDRAULIC QUANTITY (NR 1 ISO VALVE CAUTION LIGHT ILLUMINATED) INSPECTED CASE DRAIN NO CONTAMINANTS FOUND, REMOVED AND REPLACED FILTER AND SERVICED HYDRAULICS. REMOVED AND REPLACED LT IB SPOILER ACTUATOR (HOUSING CRACKED). 2H72 4T4 TRTA13NM E20NE 20050812000042005081200004SO 2005 8 12 C2XA05SH094 120050807A532014530643401 FLOOR SUPPORT EMB 145 EMB145 3260210SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713958 145085 SHV - DURING C-CHECK MAINTENANCE FOUND CORROSION ON THE CENTER OMEGA BEAM AT FRAME 25-29. MAINTENANCE REPAIRED CENTER OMEGA BEAM AT FRAME 29 IAW EMB 145 SRM 53-00-10, SECTION 4, FIGURE 203, SHEET 2. INSTALLED NUT PLATES IAW EC 5320-01137. PAINTED REPAIR AREA IAW EC 5320-01140. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050815000022005081500002EU 2005 8 15 05FDEA02382 120050810A2780 SWITCH AIRBUS310 A310203 3930313EU LE K FLAPS MALFUNCTIONED A FDEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO25430FE 394 AFTER T/O TRIED TO RETRACT FLAPS BUT GOT A KRUGER LIGHT. RECYCLED 2 TIMES RAN QRH. KRUGER REMAINED EXTENDED. RETURNED TO OAK AND AFTER LANDING KRUGERS RETRACTED. FOUND FAULT BALL SHOWS ON SFCC 1, LT RETRACT SW. REMOVED AND REPLACED LT RETRACT SWITCH PER MM 27 89 12 4, OPS CHECK FOUND NORMAL, RAN ENGINE 2 PER JRH AND RAN FLAPS SLATS UP AND DOWN COUPLE OF TIMES KRUEGER FLAPS WORKED NORMALLY. 2L72 4F RTA35EU 20050815000032005081500003WP 2005 8 15 05FDEA02383 120050810A3233 VALVE DOUG DC10 DC1010 3022110WP MLG DOWNLOCK MALFUNCTIONED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO2568054 47808 AFTER TAKEOFF DURING GEAR RETRACTION, RT MLG RED LIGHT FRONT AND REAR PANEL REMAINED ILLUMINATED. QRH COMPLIED W/ RECYCLED GEAR AT 180 KNOTS. LIGHTS REMAINED ILLUMINATED AND EVENTUALLY EXTINGUISHED IN APPROX 5 MINUTES. CHECKED PROX SENSORS AND WIRING, ALL LOOK OK. PERFORMED BITE TEST ON PROX ELECTRONIC UNIT NO FAULTS. CHECKED SENSOR GAP PER M/M 32-34-03-02, ALL WITHIN LIMITS. INSTALLED GEAR PINS, REMOVED TARGET SENSOR FROM RLG DOWN LOCK, SIMULATED FLIGHT CONDITIONS WITH GEAR UP. PER TAFI 32-30-00 CODE "AL" PRESSURIZED HYDRAULIC SYSTEM AND CHECKED ALL COMPONENTS FOR BYPASSING OR INTERNAL LEAKAGE. ALL CHECK OK. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR DOWNLOCK ACTUATOR RESTRICTOR VALVE PER MM 322L73 4F A22WE 20050815000122005081500012WP 2005 8 15 05FDEA02394 120050811A5310 DOOR FRAME DOUG MD10 MD1010F 3022112WP CARGO BAY DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25564FE 46984 AFT CARGO COMPT LOWER SIDE DOOR JAMB STA 1821 FOUND DOUBLER REPAIR ON WEB. REPLACED REPAIR BY NEW DOUBLER IAW SRM 53-50-00 FIG 12 VOL 1 AND EA 8-5310-87666. 2L73 4F RTA22WE 20050815000142005081500014WP 2005 8 15 05FDEA02396 120050811A5730 SKIN DOUG DC10 DC1010 3022110WP LT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25564FE 46984 LT WING UPPER SIDE INTERNAL L/E XORS=778 EXISTING REPAIR DOUBLER ON EXT SKIN. REMOVED AND REPLACE EXISTING REPAIR WITH NEW ONE IAW SRM 57-10-00 FIGURE 68 VOL 1. 2L73 4F A22WE 20050815000212005081500021NM 2005 8 15 05FDEA02403 120050811A5330 SKIN BOEING727 727227 1384078NM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 EXTERNAL FUSELAGE SKIN GOUGED STA 1183 2" ABOVE STR 15L. REPAIRED SKIN AT BS 1183 2" ABOVE STR 15L PER SRM 53-30-3 2L73 4F A3WE 20050815000242005081500024NM 2005 8 15 05FDEA02406 120050811A5100 NONE DOUG MD11 MD11 3023602NM NONE NONE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25624FE 48443 IAW DWG SR11340052 SHT 10, 307.203, 307.204, THERE IS ALL WIRE INSTALLED. ACCOMPLISH EA 1-3431-82825. 2L73 4F RTA22WE 20050815000272005081500027NM 2005 8 15 AWXA200500942 120050715A53206517684638 WEB BOEING737 7373S3 1384711NM L1 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 DURING C18 CHECK DISCOVERED L1 DOOR CUTOUT WEB CRACKED, .5 INCHES IN LENGTH, AT THE FORWARD INBOARD SIDE AT BS 294.5, STRINGER 12L. MAINTENANCE REMOVED THE L1 DOOR CUTOUT AT BS 294.5, STRINGER 12L WEB IAW BOEING 737-300 SRM 51-40-02-0. FABRICATED NEW INTERCOSTAL WEB IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5312-05215-SS2. INSTALLED FABRICATED REPAIR PARTS AT BS 294.5, STRINGER 12L IAW AWA ER 03-5312-05215-SS2. 2L72 4F RTA16WE 20050815000312005081500031NM 2005 8 15 AWXA200500947 120050726A5753 SKIN BOEING737 7373Y0 1384671NM FOREFLAP DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28334AW 1353 23747 DURING C16 CHECK DISCOVERED DISBOND ARE ON THE UPPER SURFACE OF THE RT OUTBOARD FORE FLAP 119 INCHES FROM INBOARD END. MAINTENANCE CUT OUT DISBOND AREA ON THE UPPER SURFACE OF THE RT OUTBOARD FORE FLAP IAW BOEING 737-300 SRM 51-70-10-0 FIG 9. FABRICATED REPAIR DOUBLER, SEPTUM AND REPAIR CORE IAW BOEING 737-300 SRM 51-70-10-0 FIG 9. BONDED AND SEALED REPAIR PARTS TO THE UPPER SURFACE OF THE RT OUTBOARD FORE FLAP 119 INCHES FROM INBOARD END IAW BOEING 737-300 SRM 51-70-10-0. 2L72 4F RTA16WE 20050815000322005081500032NM 2005 8 15 AWXA200500948 120050725A5754 WEDGE BOEING737 7373Y0 1384671NM NR 4 SLAT DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28334AW 262 23747 MCN - DURING C16 CHECK DISCOVERED TWO DISBOND AREA'S ON THE NR 4 SLAT WEDGE AT SS 12.75 TO SS 18.25 AND FROM 120.27 TO SS 124.27. MAINTENANCE REMOVED DISBOND AREAS ON THE NR 4 SLAT WEDGE IAW BOEING 737-300 SRM 51-70-10-0. FABRICATED FILLER AND DOUBLER IAW BOEING 737-300 SRM 51-70-10-0. BONDED REPAIR PARTS TO THE NR 4 SLAT WEDGE AT SS 12.75 TO SS 18.25 AND FROM 120.27 TO SS 124.27 IAW BOEING 737-300 51-70-10-0. 2L72 4F RTA16WE 20050815000342005081500034EA 2005 8 15 QXEA200501165 120050809A2840 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA PUMP ILLUMINATED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09607QX 10024 SEA- ON FLIGHT 2453, DURING TAXI OUT, RECEIVED A CROSSFLOW PUMP CAUTION MESSAGE. RETURNED TO THE GATE. MAINTENANCE CLEARED THE MESSAGE PER THE SERVICE LETTER 28-007. OPERATIONAL CHECKS GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20050815000352005081500035EA 2005 8 15 QXEA200501166 120050810A2620 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA NR 2 FIRE EXTINGILLUMINATED A QXEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM09606QX 10023 SEA - NR 2 ENGINE FIRE EXTINGUISHER FAIL CAUTION MESSAGE RECEIVED. MAINTENANCE CLEANED THE CONNECTOR ON THE FIRE EXTINGUISHER BOX. OPERATIONAL CHECKS GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20050815000362005081500036 2005 8 15 QXEA200501162 420050808A3417 ADC CNDAIRCL600 CL6002C10 1390015EA COCKPIT MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09609QX 10031 TUL- ON FLIGHT 4207, RECEIVED A EFIS COMP MON CAUTION MESSAGE WITH A DISCREPANCY NOTED IN THE ALTIMETERS. PERFORMED CHECKLIST AND DETERMINED THAT IT WAS A CAPTAIN'S AIR DATA PROBLEM. DISCONTINUED RVSM OPERATIONS. MAINTENANCE CYCLED AIRCRAFT POWER, AND PERFORMED ADC BITE TESTS. BITE TESTS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2L72 4F RTA21EA 20050815000372005081500037SO 2005 8 15 RAIA00508010 120050808A2131 CONTROLLER EMB 145 EMB145LR 3260212SO CABIN PRESSURE MALFUNCTIONED A RAIAA UNSCHED LANDING O OTHER CLCLIMB 1 CE03813HK 145044 FLT 5559 - STL - CREW REPORTED, COULD NOT CONTROL CABIN ALTITUDE IN AUTO OR MANUAL. MAINTENANCE CYCLED POWER AND OPS CHECKED OK. 2L72 4T RTT00011AT 20050815000392005081500039SO 2005 8 15 RAIA00508012 120050809A7720 CONNECTOR EMB 145 EMB145LR 3260212SO LT ENGINE UNSECURE A RAIAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 CE03825HK 145510 FLT 5502 - DEN - LEFT ENGINE ITT WENT TO 948C. MAINTENANCE RESEATED CONNECTOR AT NR 1 TRIM PLUG PERFORMED ENGINE GRN PENALTY RUN ALL INDICATIONS OK. 2L72 4T RTT00011AT 20050815000412005081500041SO 2005 8 15 RAIA00508014 120050810A2741 WARNING LIGHT EMB 145 EMB145 3260210SO PITCH TRIM ILLUMINATED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03820HK 145064 FLT 5569 - STL - PITCH TRIM MAIN AND BACKUP INOP WARNING INDICATION. MAINTENANCE CYCLED POWER AND GROUND CK OK. 2L72 4F RTT00011AT 20050815000422005081500042NM 2005 8 15 SWAA052352 120050808A53156546811 FLOORBEAM BOEING737 7373Q8 1384670NM CABIN CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29317WN 24068 DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 986, RBL 45. REPAIRED FLOORBEAM PER BFG ER. 2L72 4F RTA16WE 20050815000442005081500044NM 2005 8 15 SWAA052354 120050808A53306545776 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29317WN 24068 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050815000452005081500045 2005 8 15 SWAA052355 420050807A25651061323478 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF LIMITS A SWAAK NONE O OTHER ININSP/MAINT 1 SW29364SW 26575 R1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATES OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20050815000482005081500048 2005 8 15 SWAA052358 420050807A256565C16820 HOOK BOEING737 7373H4 1384600NM R1 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29610WN 27696 DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED HOOK PER MM. 2L72 4F RTA16WE 20050815000502005081500050NM 2005 8 15 SWAA052360 120050808A3350MS155721 BULB BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29633SW 27936 DURING SCHEDULED RON CHECK, FOUND BULLNOSE EMERGENCY LIGHT INOP AT ROW 13 ABC. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050815000512005081500051NM 2005 8 15 SWAA052361 120050807A3350MS155721 BULB BOEING737 7373Y0 1384671NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29664WN 23495 DURING SCHEDULED SERVICE CHECK, FOUND LT FUSELAGE EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050815000522005081500052NM 2005 8 15 SWAA052362 120050808A53126516300 BULKHEAD BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29696SW 23064 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE WEB CRACKS AT BS 178 BULKHEAD, RBL 5 & LBL 5, WL 200. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050815000532005081500053NM 2005 8 15 SWAA052363 120050807A534465C346701 HINGE FITTING BOEING737 7373H4 1384600NM L1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29610WN 27696 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR UPPER HINGE BOX FITTING CRACKED. REMOVED AND REPLACED UPPER HINGE BOX PER SRM. 2L72 4F RTA16WE 20050815000542005081500054NM 2005 8 15 SWAA052364 120050808A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050815000572005081500057NM 2005 8 15 SWAA052367 120050809A335020121 BATTERY PACK BOEING737 7373H4 1384600NM EMERGENCY LIGHT FAILED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29353SW 24889 RIGHT CABIN EMERGENCY EXIT LIGHTS FAILED TEST. REMOVED AND REPLACED RIGHT FWD BATTERY PACK PER MM. 2L72 4F RTA16WE 20050815000612005081500061NM 2005 8 15 SWAA052371 120050809A323469382005 HANDLE BOEING737 7373H4 1384600NM MLG FAULTY A SWAAO OTHER O OTHER APAPPROACH 1 SW29605SW 27956 DURING MLG EXTENTION, 3 GREEN & 3 RED LIGHTS ILLUMINATED. RECYCLED GEAR HANDLE, RED LIGHTS EXTINGUISHED. LUBED GEAR HANDLE PER MM. OPS CHECKED OK. 2L72 4F RTA16WE 20050815000632005081500063EA 2005 8 15 VNAA0508003 120050801A29136619003 PUMP CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE RT HYD SYSTEM LEAKING A VNAAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 GL05710PS1138 10167 ON SHORT FINAL THE HYD EDP 2A MESSAGE ILLUMINATED AND NR 2 HYDRAULIC SYSTEM QUANTITY INDICATED 0 PERCENT. THE CREW MADE AN UNEVENTFUL LANDING. MAINTENANCE FOUND THE RT ENGINE DRIVEN HYDRAULIC PUMP LEAKING. THE RT EDP WAS REMOVED & REPLACED IAW CRJ700 AMM 29-11-01-000(400)-801-A01. THE NR 2 HYDRAULIC SYSTEM WAS SERVICED. OPERATIONAL AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050815000642005081500064EA 2005 8 15 VNAA0507024 120050730A2150 A/C PACK CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LEFT MALFUNCTIONED A VNAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL05237PS 7906 DURING CRUISE, WITH THE LT PACK DEFERRED, THE RT PACK HIGH PRESS CAUTION MESSAGE ILLUMINATED. THE CREW RETURNED TO CLT. MAINTENANCE OPERATIONALLY TESTED THE AIR CONDITIONING SYSTEM IAW CRJ200 AMM 21-51-00-710-801. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050815000652005081500065EA 2005 8 15 VNAA0508001 120050801A5710 STRUCTURE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT WING LIGHTNING STRIKEA VNAAK NONE O OTHER ININSP/MAINT 1 GL05213PS 7879 EVIDENCE OF LIGHTNING DAMAGE ON THE RIGHT WINGLET WAS FOUND DURING THE SERVICE CHECK. MAINTENANCE COMPLIED WITH LIGHTNING STRIKE INSPECTIONS IAW CRJ200 AMM 05-51-05-220-803. NO OTHER DEFECTS WERE FOUND. THE WINGLET WAS TEMP REPAIRED IAW BOMBARDIER REO 601R-57-30-001. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050815000672005081500067CE 2005 8 15 DJFA2005127 120050807A2910AE1009196G0124 LINE BEECH MU300 400A 1155402CE LT HYD SYSTEM RUPTURED E DJFAO OTHER KJ FLUID LOSS WARNING INDICATION LDLANDING 1 EA23708TA RK178 ON LANDING ROLL AS THE A/C SLOWED THROUGH 55 KTS BRAKE PRESSURE WAS LOST AND THE THRUST REVERSERS WOULD NOT DEPLOY. THE EMERGENCY BRAKES WERE APPLIED TO STOP THE A/C. AT THAT POINT, THE HYD PRESSURE WAS INDICATING ZERO. WHILE AWAITING PARKING INSTRUCTIONS, THE HYD AND NITROGEN PRESSURE RETURNED TO NORMAL. DURING A POSTFLIGHT INSPECTION THE CREW DISCOVERED THE LEFT AFT SECTION OF THE A/C WAS COVERED IN HYD FLUID. MX DISCOVERED THE PRESSURE LINE TO THE LEFT THRUST REVERSER HAD RUPTURED. THE PRESSURE AND RETURN LINES LEADING TO THE NR 1 ENG THRUST REVERSER WERE REPLACED. NORMAL AND EMERGENCY SYSTEMS FOR THE BRAKES WERE BLED. BOTH LT AND RT ENGINE DRIVEN HYD PUMPS WERE REPLACED AS A PRECAUTION. THE A/C WAS2H72 4F RTA16SW 20050815000702005081500070EA 2005 8 15 VNAA0508004 120050802A27413094334 SWITCH CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE STAB TRIM FAILED A VNAAO OTHER F FLT CONT AFFECTED CRCRUISE 1 GL05246PS 7920 DURING CRUISE THE STAB TRIM CAUTION MESSAGE ILLUMINATED. THE CREW SUCCESSFULLY RE-ENGAGED THE SYSTEM AND CONTINUED TO DTW. MAINTENANCE REMOVED & REPLACED THE CAPTAIN'S PITCH TRIM DISCONNECT SWITCH IAW CRJ200 AMM 27-41-30-000(400)-802. OPERATIONAL CHECKS WERE GOOD. A SATISFACTORY OPERATIONAL CHECK FLIGHT WAS PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050815000712005081500071EA 2005 8 15 VNAA0507025 120050730A3250530133 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE NLG STEERING FAILED A VNAAO OTHER O OTHER APAPPROACH 1 GL05712PS1348 10168 UPON LANDING GEAR DEPLOYMENT THE STEERING INOP CAUTION MESSAGE ILLUMINATED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED & REPLACED THE STEERING HAND WHEEL CONTROL UNIT IAW CRJ200 AMM 32-51-01-400-801-A01. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050815000722005081500072NM 2005 8 15 PIDA20050063 120050809A3350 LAMP BOEING737 737306 13844BGNM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05372PA 23546 L1 DOOR EMERGENCY LIGHT ON EXTERIOR OF FUSELAGE INOP. RELAMPED L1 DOOR EXTERIOR LIGHT PER MM 33-50. OPS CHECKS GOOD. 2L72 4F RTA16NE 20050815000732005081500073EA 2005 8 15 VNAA0508006 120050802A2133 OUTFLOW VALVE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN PRESSURE MALFUNCTIONED A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL05253PS 7934 DURING CLIMBOUT THE OVERBOARD COOL CAUTION MESSAGE ILLUMINATED AND THE CABIN DID NOT PRESSURIZE. THE CREW RETURNED TO DAY. MAINTENANCE FOUND THE OVERBOARD EXHAUST SHUTOFF VALVE OPEN. THE SOV WAS SECURED CLOSED IAW CRJ200 AMM 21-24-00-040-806 AND MEL 21-24-06. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050815000742005081500074WP 2005 8 15 IXXA0500093O 120050812A772265016003 INDICATOR DOUG DC8 DC873F 302199FWP EGT READS HIGH A IXXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW11605AL953701792 46106 DURING CLIMB-OUT FROM KLRD TO KMEM, NR 1 EGT INDICATED TO 912 DEGREES. TEMP DECREASED AS THROTTLE WAS PULLED BACK. TEMP WAS AT 912 FOR APPROX 5 SECONDS, OAT WAS 34 DEGREES C, N1 SETTING 91.3% AND THE INDICATOR WAS FLASHING 912 DEGREES. THE CREW DIVERTED A/C DIRECTLY TO KTOL WERE IT LANDED W/O INCIDENT. MX PERFORMED AN INSPECTION OF THE NR 1 ENGINE AND NO DEFECTS WERE NOTED. ALSO, CHECKED EGT HARNESS AND IT CHECKED GOOD. MX ALSO PERFORMED A POWER ASSURANCE CHECK AND FOUND NR 1 EGT READING HIGH. REMOVED AND REPLACED NR 1 EGT INDICATOR. RAN POWER ASSURANCE CHECK AND THE EGT TEST WAS GOOD IN ACCORDANCE WITH THE ERH AND CFM MANUALS. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20050815000762005081500076EA 2005 8 15 VNAA0508008 120050805A5350 RADOME CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE FUSELAGE LIGHTNING STRIKEA VNAAO OTHER O OTHER CRCRUISE 1 GL05709PS 10165 THE CREW REPORTED A LIGHTNING STRIKE TO THE RADOME. MAINTENANCE COMPLIED WITH EN ROUTE & DETAILED LIGHTNING STRIKE INSPECTIONS IAW CRJ700 AMM 05-51-07-210-801-A01 & AMM 05-51-07-220-801-A01. MINOR BURN DAMAGE TO BOTH WINGLET TIPS WAS REPAIRED IAW BOMBARDIER REO 690-57-31-002. NO OTHER DEFECTS WERE FOUND. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050815000782005081500078NM 2005 8 15 SWAA052374 120050805A53126545819 PRESSURE PANEL BOEING737 7373H4 1384600NM NLG WW CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED SERVICE CHECK, FOUND NLG W/W RT FWD UPPER ACCESS CUTOUT, AFT INBD CORNER CRACKED AT BS 251.6, LBL 2.0. REPAIRED WEB PER SWA EA. 2L72 4F RTA16WE 20050815000812005081500081NM 2005 8 15 SWAA052377 120050810A326065C367251 SWITCH BOEING737 7373H4 1384600NM FWD E/E BAY FAULTY A SWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW29353SW 24889 AIR TURNBACK, LANDING GEAR HANDLE MOVED TO UP POSITION, HORN SOUNDED AND ALL THREE RED UNSAFE LIGHTS ILLUMINATED. ALL 3 RED LIGHTS STILL ILLUMINATED WITH GEAR HANDLE IN OFF POSITION. REMOVED AND REPLACED LT AUTOTHROTTLE SWITCH PACK PER MM. 2L72 4F RTA16WE 20050815000832005081500083NM 2005 8 15 SWAA052379 120050809A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29448WN 33721 DURING SCHEDULED MV2 CHECK, FOUND EEPLS TRACK COVER MISSING AT ROW 13 ABC. INSTALLED COVER PER MM. 2L72 4F RTA16WE 20050815000842005081500084NM 2005 8 15 SWAA052380 120050810A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29612SW 27930 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727A, STR 19L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050815000862005081500086NM 2005 8 15 SWAA052382 120050810A53116520722 FRAME BOEING737 7373H4 1384600NM FWD CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29612SW 27930 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 440, STR 23R TO STR 25R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050815000872005081500087NM 2005 8 15 SWAA052383 120050810A53116546550 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29612SW 27930 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 787 AND BS 867, STR 8L TO STR 9L. REPAIRED FRAMES PER SRM. 2L72 4F RTA16WE 20050815000882005081500088NM 2005 8 15 SWAA052384 120050810A53116546550 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29612SW 27930 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 787 AND BS 867, STR 8R TO STR 9R. REPAIRED FRAMES PER SRM. 2L72 4F RTA16WE 20050815000902005081500090GL 2005 8 15 SWAA052386 220050809A72103353000110 GEARBOX BOEING737 7373H4 1384600NM CFMINTCFM56 CFM563B1US GL NR 2 ENGINE MAKING METAL A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 DURING SCHEDULED A1 CHECK, FOUND METAL CHIPS IN NR 2 ENGINE FWD OIL MAGNETIC CHIP DETECTOR. REMOVED AND REPLACED NR 2 TRANSFER GEARBOX ASSY PER MM. 2L72 4F4 FRTA16WE E2GL 20050815000912005081500091NM 2005 8 15 SWAA052387 120050809A3350MS155721 BULB BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29623SW 27933 DURING SCHEDULED C4 CHECK, FOUND EMERGENCY BULLNOSE LIGHT INOP AT ROW 17 ABC. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050815000922005081500092NM 2005 8 15 SWAA052388 120050810A53306545774 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29690SW 23783 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727C + 5, STR 10L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050815000942005081500094NM 2005 8 15 SWAA052390 120050810A534065C27314 STRINGER CLIP BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29696SW 23064 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 360, STR 13L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050815000962005081500096NM 2005 8 15 SWAA052392 120050810A53106517582 VERTICAL BEAM BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29696SW 23064 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 181, RBL 17.1, WL 181. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050815000972005081500097 2005 8 15 SWAA052393 420050809A256563550 SLIDE BOEING737 7377H4 1384404NM FWD GALLEY OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29739GB 29275 DURING SCHEDULED HC2 CHECK, FOUND L1 AND R1 DOOR EMERGENCY EVAC SLIDES OUT OF ADJUST. ADJUSTED SLIDES PER MM. 2L72 4F RTA16WE 20050825000032005082500003NM 2005 8 25 SWAA052538 120050823A53116520723 FRAME BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29317WN 24068 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 492, STR 24R. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20050825000042005082500004NM 2005 8 25 SWAA052509 120050819A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29617SW 27700 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 807, LBL 19. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050825000072005082500007NM 2005 8 25 SWAA052512 120050819A53306545768 SKIN BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CORRODED BETWEEN BS 259 TO BS 312, STR 14L. REPAIRED SKIN PER BFG ER. 2L72 4F RTA16WE 20050825000082005082500008NM 2005 8 25 SWAA052513 120050820A335020121 BATTERY PACK BOEING737 7373G7 1384595NM AFT CABIN FAILED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29683SW 24008 DURING SCHEDULED SERVICE CHECK, AFT CABIN EMERGENCY LIGHTS FAILED TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050825000092005082500009CE 2005 8 25 DXTA200500910 120050820A2150 A/C PACK CESSNA750 750 2076810CE LEFT OVERTEMP E DXTAH DEACTIVATE SYST/CIRCUITS BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 GL07943QS 7500043 LEFT PACK TEMP 120 DEGREES AND RISING UNCONTROLLABLE BOTH MANUAL OR AUTO FOLLOWED BY BLUE SMOKE IN THE COCKPIT COMING FROM AIR VENTS. ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20050825000132005082500013 2005 8 25 DXTA200500907 420050819A22108221019213 CIRCUIT CARD BEECH MU300 400A 1155402CE FCC MALFUNCTIONED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07108QS RK382 DURING T/O ROLL AT 70-80 KIAS OVERSPEED TONE ACTIVATED MOMENTARILY. REMOVED AND REPLACED NR 2 FCC CARD IAW HAWKER 400XP MM CH 22-13-00. 2H72 4F RTA16SW 20050825000142005082500014CE 2005 8 25 DXTA200500906 120050819A3240 CONTROL SYSTEM CESSNA500 560CESSNA 2076750CE RUDDER STUCK E DXTAD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07806QS 5600614 UPON TAXI OUT THE CO-PILOT APPLIED FULL RT RUDDER AND HAD NO RT BRAKE. THE CAPT APPLIED RT BRAKE WHICH WORKED BUR THE RT BRAKE AND RUDDER PEDAL MADE A LOUD CATCHING NOISE AND STUCK TO THE FLOOR (IN FULL BRAKING MODE). STOMPED ON THE LT PEDAL TO RELEASE THE RT SIDE. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20050825000162005082500016NM 2005 8 25 SWAA052515 120050818A5313BAC1498 STRINGER BOEING737 7373T5 1384608NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29696SW 23064 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 991.5, STR 24R. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20050825000172005082500017NM 2005 8 25 SWAA052516 120050820A33506042221 LIGHT BOEING737 7377H4 1384404NM FWD GALLEY BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29705SW 27839 R1 DOOR LOWER EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20050815001072005081500107NM 2005 8 15 05FDEA02430 120050811A5330 SKIN BOEING727 727227 1384078NM FUSELAGE UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 PREVIOUS REPAIR AT STA 243 TO 280 BTWN STR 21L AND 23L IS IAW SRM 53-30-3 AND IS A MAJOR REPAIR. 2L73 4F A3WE 20050815001092005081500109NM 2005 8 15 05FDEA02433 120050811A5512 SKIN DOUG MD11 MD11 3023602NM HORIZONTAL STAB DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 LT HORIZONTAL STABILIZER HAS UPPER TRAILING EDGE PANEL WITH DELAMINATION, BETWEEN INBOARD AND OUTBOARD ELEVATOR ACTUATOR FORWARD ACCESS PANELS, STA XE 160. REPAIRED IAW CHP 51-62-01. 2L73 4F RTA22WE 20050815001102005081500110NM 2005 8 15 05FDEA02434 120050811A3210 SLEEVE DOUG MD11 MD11 3023602NM ZONE 700 MISSING A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT MAIN GEAR, TRUCK BEAM AFT OUTBOARD LUBE HOLE FOUND PIVOT BORE SLEEVE CHIPPED OFF. REMOVED AND RE-INSTALLED AS PER MM 32-12-20-4 AND RE-INSPECTED LEFT HAND TRUCK BEAM AFT OUTBOARD PIVOT BORE SLEEVE AREA FOUND THE CHIPPED OUT IS ACTUALLY GREASE AS PER DRAWING ARG7029. 2L73 4F RTA22WE 20050815001112005081500111NM 2005 8 15 05FDEA02435 120050811A3210 SLEEVE DOUG MD11 MD11 3023602NM MLG DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT MAIN GEAR, TRUCK BEAM AFT INBOARD LUBE HOLE FOUND PIVOT BORE SLEEVE CHIPPED OFF. REMOVED AND RE-INSTALLED AS PER MM 32-12-20-4 AND RE-INSPECTED RIGHT HAND TRUCK BEAM AFT INBOARD PIVOT BORE SLEEVE AREA FOUND THE CHIPPED OFF IS ACTUALLY A GREASE GROOVE AS PER DRAWING ARG7029. 2L73 4F RTA22WE 20050815001122005081500112NM 2005 8 15 05FDEA02437 120050812A5320 INTERCOSTAL DOUG MD11 MD11 3023602NM CABIN CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 CABIN, STA 1441 TO 1461 LONGERON L-9 RT INTERCOSTAL FOUND CRACKED AS MARKED. REMOVED AND FABRICATED IAW DWG AEA 7685. INSTALLED IAW SRM 51-35-01. 2L73 4F RTA22WE 20050815001132005081500113NM 2005 8 15 05FDEA02438 120050812A5320 INTERCOSTAL DOUG MD11 MD11 3023602NM CABIN CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 CABIN, STA 5-53 TO 5-73 LONGERON L-7 RT INTERCOSTAL FOUND CRACKED AS MARKED. INTERCOSTAL REMOVED AND FABRICATED IAW DWG A5A 7071. INSTALLED IAW SRM 51-35-01 2L73 4F RTA22WE 20050815001142005081500114NM 2005 8 15 05FDEA02439 120050812A5240 BRACKET DOUG MD11 MD11 3023602NM DOOR R3 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 MAIN DECK, R3 DOOR LOWER STOP FORWARD BRACKET FOUND CRACKED. REMOVED AND REPLACED PER SRM 51-31-01 VOLUME II. 2L73 4F RTA22WE 20050815001162005081500116NM 2005 8 15 05FDEA02441 120050812A5315 FLOORBEAM BOEING727 727227 1384078NM CABIN UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 REPAIR ON FLOORBEAM AT STA 1130 BL 0 THRU RBL 18, PREVIOUS REPAIR AT STA 1130 , BL 0 TO RBL 18 NEEDS ENG EVALUATION TO DETERMINE IF MAJOR OR MINOR AND IF REPAIR IS IAW FAA APPROVED DATA. NO ENGINEERING NEEDED. THE REPAIR IS WAS INSTALLED IAW SRM 53-10-8 AND IS A MAJOR REPAIR IAW GMM 6-2-100. 2L73 4F A3WE 20050815001172005081500117NM 2005 8 15 05FDEA02442 120050812A5330 SKIN BOEING727 727227 1384078NM UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 REPAIR LOCATED AT APPROX BS 1140 TO 1183 STR 21L TO 23L, PREVIOUS REPAIR AT STA 1140 TO 1183 STR 21L TO 23L NEEDS ENG EVALUATION TO DETERMINE IF MAJOR OR MINOR AND IF REPAIR IS IAW FAA APPROVED DATA. NO ENGINEERING EVALUATION REQUIRED. REPAIR HAS BEEN COMPLIED WITH IAW SRM 53-30-3 FIG 3A, THIS IS A MAJOR REPAIR IAW GMM 6-2-100. 2L73 4F A3WE 20050815001182005081500118NM 2005 8 15 05FDEA02443 120050812A5330 SKIN BOEING727 727227 1384078NM UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 REPAIR LOCATED ON FUSELAGE AT NR 1 ENGINE, PREVIOUS REPAIR AT FS 1243 BELOW NR 1 PYLON NEEDS ENG EVALUATION TO DETEMINE IF MAJOR OR MINOR AND IF REPAIR IS IAW FAA APPROVED DATA. NO ENGINEERING NEEDED. THIS IS A MODIFICATION INSTALLED IAW DRAWING B27-53-020. THIS IS A MAJOR MODIFICATION IAW GMM 6-2-100. 2L73 4F A3WE 20050815001192005081500119NM 2005 8 15 05FDEA02444 120050812A5330 SKIN BOEING727 727227 1384078NM UNKNOWN A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25479FE 21461 REPAIR LOCATED ON FUSELAGE AT NR 3 ENG, PREVIOUS REPAIR AT STA 1243 BELOW NR 3 PYLON NEEDS ENG EVALUATION TO DETERMINE IF MAJOR OR MINOR AND IF REPAIR IS IAW FAA APPROVE DATA. NO ENGINEERING NEEDED. THIS IS A MODIFICATION COMPLETED BY DRAWING B27-53-020 REV D. THIS IS A MAJOR MODIFICATION IAW GMM 6-2-100. 2L73 4F A3WE 20050815001202005081500120NM 2005 8 15 05FDEA02445 120050812A5330 SKIN BOEING727 727227 1384078NM UNKNOWN A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25479FE 21461 REPAIR LOCATED ON FUSELAGE AT NR 3 ENG, PREVIOUS REPAIR AT STA 1243 BELOW NR 3 PYLON NEEDS ENG EVALUATION TO DETERMINE IF MAJOR OR MINOR AND IF REPAIR IS IAW FAA APPROVE DATA. 2L73 4F A3WE 20050815001232005081500123EU 2005 8 15 UPS05145163 120050729A5754A5724199320200 DOUBLER AIRBUSA300 A300F4622R 3930360EU LT WING K FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01124UP 0808 LEFT WING KRUGER BOX AREA, CURVED DOUBLER ON 2ND RIB FROM FUSELAGE HAS APPROX 4" CRACK. REMOVED AND REPLACED REINFORCING ANGLE IAW SRM 51-40-00. 2L72 4F RTA35EU 20050815001242005081500124NM 2005 8 15 UPS05445165 120050722A531165B01732109 FRAME BOEING747 747121 1384871NM M/D CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 BS 780 STR 20-22R FRAME FWD FACE FOUND CRACK. CRACK LENGTH 1.75" CORROSION BLEND OUT. M/DECK BS 780 BETWEEN STR 20R-22R FRAME REPAIRED AS PER HX RS R53-22-35346 AND UPS EO B747-5310-22632-A. 2L74 4F A20WE 20050815001272005081500127NM 2005 8 15 UPS05445168 120050723A532265B01736171 SHEAR TIE BOEING747 747121 1384871NM M/D CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 M/DECK BS 860 RT FRAME BTN STR 12-13R SHEAR TIE FOUND CRACKED, CRACK LENGTH 5/8". M/DECK BS 860 BETWEEN STR 12R-13R SHEAR TIE REPAIRED AS PER HX RS R53-22-35349 AND UPS EO B747-5310-22630-A. 2L74 4F A20WE 20050815001292005081500129NM 2005 8 15 UPS05445170 120050723A531165B041793 FRAME BOEING747 747121 1384871NM FWD CARGO CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 FWD CARGO LT STA 920 LBL 60" FRAME UPR FLANGE FOUND CRACKED, CRACK LENGTH 3". FWD CARGO COMPT BS 920 LBL 60" FRAME REPAIRED AS PER HX RS R53-22-35342 AND UPS EO.B747-5310-22635-A. 2L74 4F A20WE 20050815001322005081500132NM 2005 8 15 UPS05445174 120050723A5313 STRINGER BOEING747 747121 1384871NM M/D CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 M/D BS 1740-1760 S3R STRINGER END FOUND CRACKED, CRACK LENGTH 1.5". M/D BS 1740-1760 STR 3R STRINGER END REPAIRED AS PER HX RS R53-61-35355. FOLLOW UP INSPECTION FOR THIS REPAIR IS REQUIRED AS PER HX RS R53-61-35355 AND UPS EO.B747-5310-22662-A. 2L74 4F A20WE 20050815001352005081500135NM 2005 8 15 UPS05445177 120050727A5310 DOOR FRAME BOEING747 747121 1384871NM CARGO BAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 BULK CARGO DOOR CUTOUT AFT FRAME AREA AT BS 2034 STR 35-37 FOUND 2EA HOLE CRACK, CRACK LENGTH 0.020" AND 0.030". BULK CARGO DOOR CUTOUT AFT AREA BS 2034 BETWEEN STR 34/35R TO STR 37/38R AREA REPAIRED AS PER HX RS R-53-61-35359. REF NRC 6801 FOR DETAIL AND C/OUT CONTINUE INSPECTION PER HX RS R-53-61-35359. 2L74 4F A20WE 20050815001362005081500136NM 2005 8 15 UPS05445178 120050727A5310 DOOR FRAME BOEING747 747121 1384871NM CARGO BAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 BULK CARGO DOOR CUTOUT AFT FRAME AT BS 2034 STR 35-37 FOUND 7EA HOLE CRACK AT FRAME OUTER CHORD, CRACK LENGTH 0.020"/0.030". BULK CARGO DOOR CUTOUT AFT AREA BS 2034 BETWEEN STR 34/35R TO STR 37/38R AREA REPAIRED AS PER HX RS R-53-61-35359 AND C/OUT CONTINUE INSPECTION PER HX RS R-53-61-35359. 2L74 4F A20WE 20050815001382005081500138NM 2005 8 15 UPS05445180 120050726A521065B0183658 TORQUE BOX BOEING747 747121 1384871NM M/D CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 1R DOOR LATCH TORQUE BOX CUTOUT LWR BEAM CRACKED AND ATT 'T' BRACKET DEFORMED, CRACK LENGTH 5/16". SUPPORT BEAM AND BRACKET REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050815001402005081500140WP 2005 8 15 UPS05845146 120050729A534046143972N FITTING DOUG DC8 DC873F 302199FWP FS 160 L31L CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 WHILE WORKING N/R 859104 FOUND LONG 31L END FITTING CRACKED. REMOVED AND REPLACED LONG END FITTING AT STA 106 IAW SRM 51-3-0 51-1-21, AND SRM 51-1-20D. 2L74 4F RT4A25 20050815001432005081500143WP 2005 8 15 UPS05845150 120050725A5330 SKIN DOUG DC8 DC873F 302199FWP FS 1746 L15R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 FUSELAGE EXTERIOR SKIN CRACKED 1/2" LONG AT STA 1746 L15R. REMOVED DAMAGED SECTION OF SKIN, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 53-2-1 FIG 7. 2L74 4F RT4A25 20050815001442005081500144WP 2005 8 15 UPS05845151 120050726A5730 SKIN DOUG DC8 DC873F 302199FWP XCW 98 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 R/W UPPER SURFACE 6" AFT OF FRONT SPAR AT FUEL PROBE NR 12 HAS A 1" CRACK AT FASTENER HOLE. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57- 2-1 FIG 10. 2L74 4F RT4A25 20050815001452005081500145WP 2005 8 15 UPS05845153 120050728A5311 FRAME DOUG DC8 DC873F 302199FWP FS 1700 L20L CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 MAIN CABIN FRAME CRACKED 1" LONG AT STA 1700 L20L. TRIMMED OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW EO DC8-5310 -11728-B AND DWG DC8-53A-011-A. 2L74 4F RT4A25 20050815001462005081500146WP 2005 8 15 UPS05845154 120050727A53403779874501 FITTING DOUG DC8 DC873F 302199FWP FS 700 L18L CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 STA 700 LONG 18L INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED APPROX 3" LONG. REMOVED AND REPLACED ATTACH FITTING IAW DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20050815001472005081500147WP 2005 8 15 UPS05845155 120050727A53403779659U501 FITTING DOUG DC8 DC873F 302199FWP FS 902 L5R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 STA 902 L5R LONGERON FITTING CRACKED 2" LONG. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D AND 51-1-21. 2L74 4F RT4A25 20050815001482005081500148WP 2005 8 15 UPS05845156 120050727A53404750418U1 FITTING DOUG DC8 DC873F 302199FWP FS 1160 L19R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 STA 1160 L19R FITTING CRACKED 1" LONG. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20050815001492005081500149WP 2005 8 15 UPS05845157 120050727A53404750419U501 FITTING DOUG DC8 DC873F 302199FWP FS 1220 L20R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 MAIN CABIN STA 1220 L20R FRAME ATTACH FITTING CRACKED 1/2" LONG. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20050815001502005081500150WP 2005 8 15 UPS05845158 120050728A5310 FINGER DOUBLER DOUG DC8 DC873F 302199FWP FS879-902 LBL65 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 CENTER WING BOX AT STA 879 TO 902 LBL 65 FINGER DOUBLER HAS SEVERAL SHEARED FASTENER HEADS AND HEAVY CORROSION UNDER THE FINGER DOUBLER. REMOVED FINGER DOUBLER AND FOUND OUT OF LIMITS IAW DC-8 SRM 53-2-0 FIG 1F. AREA UNDER FINGER DOUBLER FOUND IN LIMITS IAW DC-8 SRM 53-2-0 FIG 1F. FABRICATED AND INSTALLED FINGER DOUBLER IAW DWG 5645332 AND SRM 53-7-3 FIG 4 AND 51-1-20D. 2L74 4F RT4A25 20050815001522005081500152WP 2005 8 15 UPS05845160 120050801A534037558272 FITTING DOUG DC8 DC873F 302199FWP STA 280 L29R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 "A" PIT STA 280 L29R ZEE FITTING CRACKED 1/2" LONG. REMOVED AND REPLACED "Z" FITTING IAW DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20050815001532005081500153WP 2005 8 15 UPS05845161 120050801A5310559799213 STIFFENER DOUG DC8 DC873F 302199FWP FS -109 LBL36 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 HEAVY CORROSION ON BASE OF DIAGONAL STIFFENER IN COCKPIT SUB FLOOR BELOW PILOTS LT RUDDER PEDAL. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT GUSSET IAW DWG 5597992 AND SRM 51-1-20D. 2L74 4F RT4A25 20050815001582005081500158EU 2005 8 15 XN0A1251 120050805A2420 CSD AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE NR 1 DISCONNECTED A XN0AD RETURN TO BLOCK O OTHER NRNOT REPORTED 1 GL23371PC 157 NR 1 GENERATOR TRIP OFF. NO VOLT AND FREQ. ITEM TRANSFER TO DMI NR 5616 IAW MEL 24-11-01 CAT - (B), NR 1 CSD DISCONNECTED. (ORIG/OPEN) 2L72 4F4 FRTA35EU E23EA 20050811000172005081100017WP 2005 8 11 05FDEA02340 120050809A5310AFA38733 FRAME DOUG MD10 MD1010F 3022112WP CARGO DOOR CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25564FE 46984 CTR CARGO COMPT STA 1710 X=-65 JAMB DOOR FWD, AFTER REMOVED RAIL FOUND SEVERE CORROSION WITH EXFOLIATION. REMOVED CORROSION PER SRM 53-00-01 VOL 1 FIG 1B AND REPLACED FRAME PER SRM 51-32-01 PG 59/68, SRM 51-35-01 PG 1/13, SRM 51-33-01 PG 34/47 VOL 2 AND DWG AFAQ3873. 2L73 4F RTA22WE 20050811000242005081100024WP 2005 8 11 05FDEA02347 120050809A5522 SKIN DOUG MD10 MD1010F 3022112WP RT ELEVATOR DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25564FE 46984 RIGHT STAB I/B ELEV XE 61.875 EXISTING 1EA EXT REPAIR DOUBLER ON UPPER DETACHABLE SKIN. REPLACED REPAIR PER SRM 55-00-01 VOL 1 FIG 3 SHT 2 AND SRM 55-00-01 PG 2A, 2B VOL 1. 2L73 4F RTA22WE 20050811000382005081100038 2005 8 11 IXXA0500090O 420050810A3420 INDICATOR DOUG DC8 DC873F 302199FWP COCKPIT INOPERATIVE A IXXAA UNSCHED LANDING O OTHER CLCLIMB 1 SW11604BX8499521 46046 DURING CLIMB-OUT FROM KTOL, PILOT'S HSI/ADHI WAS INOP. LOST ATTITUDE AND HEADING INFORMATION. CREW RETURNED AIRCRAFT TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET EADI AND EHSI CIRCUIT BREAKERS. THE SYSTEM RETURNED TO NORMAL AND THE OPERATIONAL CHECK WAS GOOD PER ALL APPLICABLE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20050811000432005081100043GL 2005 8 11 DXTA200500881 220050803A739723051442 WIRE HARNESS CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL RT ENGINE INOPERATIVE E DXTAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL07964QS 7500164 FUEL FILTER BYPASS LIGHT (R) ILLUMINATED ON T/O ROLL. LOW SPEED ABORT AT 40KTS. REMOVED AND REPLACED RT ENGINE HARNESS IAW RR 30007 MM 73-13-10. REMOVED PN 23051442 S/N OFF NX0466. 2L72 4J4 FRTT00007WITE6CH 20050811000462005081100046CE 2005 8 11 DXTA200500883 120050804A2120 SMOKE CESSNA650 650 2076802CE COCKPIT DETECTED E DXTAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL07791QS 6507091 ON THE GROUND WITH APU RUNNING THE COCKPIT FILLED WITH BLUE SMOKE AND THE COCKPIT SUPPLY AIR TEMPERATURE WAS 170 DEGREES AND CLIMBING WITH THE TEMPERATURE CONTROL IN FULL COLD. 2L72 4F A9NM 20050811000502005081100050EU 2005 8 11 05FDEA02327 120050808A5420 FAIRING AIRBUS300 A300B4605R 3930308EU NR 1 PYLON DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25671FE 778 NR 1 PYLON AFT FAIRING 473EL DELAMINATED. 2L72 4F RTA35EU 20050811000712005081100071WP 2005 8 11 ASAA0580325 120050613A53105936038501 BEAM DOUG DC9 DC983 3022083WP FS 1117-1250 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - DURING HV CHECK, FOUND AFT CARGO BAY DOOR JAMB LOWER BEAM CORRODED. REPLACED BEAM. (M) 2L72 4F RTA6WE 20050811000752005081100075NM 2005 8 11 ASAA0580340 120050613A5347SR095301157001 SEAT TRACK DOUG MD80 MD83 3023681NM FS 200-265 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - DURING HV-CHECK, FOUND SEAT TRACK CORRODED. REPLACED DAMAGED SEAT TRACK SECTION. (M) 2L72 4F RT 20050811000812005081100081WP 2005 8 11 ASAA0580333 120050613A532059360717 INTERCOSTAL DOUG DC9 DC983 3022083WP FS 1212-1231 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - DURING HV CHECK, FOUND INTERCOSTAL CORRODED. REPLACED DAMAGED INTERCOSTAL. (M) 2L72 4F RTA6WE 20050811000822005081100082NM 2005 8 11 ASAA0580339 120050613A5347SR095301157003 SEAT TRACK DOUG MD80 MD83 3023681NM FS 200-247 GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - HV-CHECK, FOUND SEAT TRACK GOUGED. REPLACED DAMAGED SEAT TRACK SECTION. (M) 2L72 4F RT 20050811000862005081100086WP 2005 8 11 ASAA0580329 120050613A532099365807 INTERCOSTAL DOUG DC9 DC983 3022083WP FS 769-785 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - DURING HV CHECK, CABIN FLOOR INTERCOSTAL CRACKED. REPLACED DAMAGED INTERCOSTAL. (M) 2L72 4F RTA6WE 20050811000932005081100093EA 2005 8 11 ASOA05589S 120050710A3297491039 WIRE HARNESS CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE LT MLG PROX SENSINOPERATIVE A ASOAO OTHER J WARNING INDICATION DEDESCENT 1 SO27730EV3705 MA0144 10141 DURING DESCENT, AT APPROX 18,000 FT, THE CREW RECEIVED A BRAKE OVERHEAT WARNING MESSAGE ON EICAS WITH THE LT OB BRAKE INDICATOR GOING TO TWENTY AND FLUCTUATED ERRATICALLY. AFTER COMPLYING WITH THE QRH, ALL INDICATIONS RETURNED TO NORMAL. UPON LOWERING THE GEAR FOR FINAL APPROACH, THE OVERHEAT MESSAGE ACTIVATED AGAIN WITH THE LT OB MAIN BRAKE INDICATOR SHOWING RED AND AL OTHER SHOWING GREEN AND THE TEMP INDICATOR SHOWING ONE. EMERGENCY VEHICLES WERE REQUESTED AS PRECAUTION. AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE LT OB PROXIMITY SENSOR HARNESS ASSEMBLY. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA EOOO63EN 20050811000952005081100095EA 2005 8 11 ASOA05618 120050710A5210 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PASSENGER DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27852AS 7367 7369 DURING A C-CHECK, THE PASSENGER DOOR INTERCOSTAL AND INNER SKIN WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE PASSENGER DOOR INTERCOSTAL AND INNER SKIN IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050811001082005081100108EA 2005 8 11 ASOA05613 120050721A5240 DOOR CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE SERVICE STIFF A ASOAK NONE O OTHER ININSP/MAINT 1 SO27748EV 10158 DURING A GROUND INSPECTION, THE SERVICE DOOR WAS FOUND HARD TO OPEN AND CLOSE. MAINTENANCE INSPECTED THE SERVICE DOOR WITH NO DEFECTS FOUND. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA EOOO63EN 20050811001132005081100113EA 2005 8 11 ASOA05624 120050722A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX STIFF A ASOAK NONE O OTHER ININSP/MAINT 1 SO27833AS 7246 DURING A C-CHECK, THE PASSENGER DOOR WAS FOUND HARD TO OPEN FROM THE INSIDE AND OUTSIDE. MAINTENANCE RE-RIGGED THE PASSENGER DOOR OUTER HANDLE IAW MM. OPS CHECK GOOD. (K) 2L72 4F4 FRTA21EA E15NE 20050811001192005081100119NM 2005 8 11 UPS05M45081 120050610A5320 RAIL DOUG MD11 MD11F 3023600NM FWD CARGO COMPT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01255UP 48404 INSPECTION TYPE:C-CHECK, FWD CARGO COMPT AT STATION 715, 775, 791, 824 AND 879 RT Z-TYPE SIDE RAIL GUIDE UPPER SURFACE WITH CORROSION AS MARKED. CORROSION REMOVED AND TREATED AS PER SRM 51-21-01 VOL II REV 37 AND FOUND WITHIN LIMIT AS PER SRM 53-00-01 VOL I REV 37. 2L73 4F RTA22WE 20050811001302005081100130NM 2005 8 11 UPS05445088 120050722A5730 SKIN BOEING747 747121 1384871NM RT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE:C RIGHT WING UPPER SURFACE RABBIT AREA FOUND BULGED BETWEEN WS 1375 AND WS 1395 (AFT NR 24 VC FLAP). CORROSION BLEND OUT 0.127" X 1.625" X 6" EXCEED SRM 57-30-01 FIG 1 LIMITS. RIGHT WING UPPER SURFACE RABBIT AREA REPAIRED AFTER CORROSION BLENDED OUT AS PER HX RS R57-25-35358 & UPS ENGINEERING FILE 747-57-20079. 2L74 4F A20WE 20050811001342005081100134NM 2005 8 11 UPS05445127 120050724A5720 WEB BOEING747 747121 1384871NM LHW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE:C LEFT WING UPPER WING L/E CAVITY NOSE L/E WEB CRACK AT WS 670-680 ABOVE NR 2 PYLON AREA, (CRACK LENGTH 1.25"). WEB FABRICATED & INSTALLED AS PER SRM 57-20-03 FIG 7. 2L74 4F A20WE 20050811001522005081100152WP 2005 8 11 0501239618 120050806A213110256861 CONTROLLER DOUG DC9 DC932 3022066WP CABIN PRESSURE MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01618NW1576812763 47433 AT FL270 CABIN BEGAN TO CLIMB 2000 FPM. FOLLOWED COM AND RAPID DESCENT TO 10000 FT. MASKS DID NOT DEPLOY. FLT CONTINUED TO MCO AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED CABIN PRESSURE CONTROLLER. OPERATION CHECKS GOOD. 2L72 4F A6WE 20050811001612005081100161NM 2005 8 11 ASAA0580341 120050613A53209936534139 TRACK DOUG MD80 MD83 3023681NM FS 148.5-200 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - DURING HV CHECK, CABIN FLOOR FALSE TRACK CORRODED. REPLACED FALSE TRACK. (M) 2L72 4F RT 20050811001622005081100162NM 2005 8 11 USAA050896 120050718A5340415N400217 SUPPORT BOEING757 7572B7 1384964NM FS 398 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19628AU 27806 BFM - FOUND GAL SUPPORT CORRODED, 2.5 INCHES BY 1 INCH BY .05 INCH, MAIN CABIN STATION 398 RBL 12. REMOVED AND REPLACED WITH NEW PART PER SRM 53-00-51, 51-40-02. (M) 2L72 4F RTA2NM 20050811001802005081100180NM 2005 8 11 UPS05M45100 120050606A5320 SPLICE DOUG MD11 MD11F 3023600NM CTR CARGO COMPT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01255UP 48404 INSPECTION TYPE:C-CHECK CENTER CARGO RT TUNNEL AT STA 5-123 LONGERON 33RT SPLICE FOUND WITH CORROSION AS MARKED. CORROSION REMOVED AND TREATED AS PER SRM 51-21-01 VOL II REV 37 FOUND WITHIN LIMIT AS PER SRM 53-00-01 VOL I REV 37. 2L73 4F RTA22WE 20050811001982005081100198EU 2005 8 11 DHL2005367003 120050810A3350312101 BATTERY PACK AIRBUS300 A300B4203 3930306EU GE CF6 CF650* 30018NE EMERGENCY LIGHT INOPERATIVE A DHLAK NONE O OTHER ININSP/MAINT 1 SO01365DH 149 L1 EMRG LT INOP. REMOVED AND REPLACED, L1 EMERG LT BATT PACK IAW 33-51-13. 2L72 4F4 FRTA35EU E23EA 20050811001992005081100199EA 2005 8 11 HNAA0500075 120050809A7922 ENGINE DHAV DHC8 DHC8311 1386006EA PWA PW120 PW123 NE NR 2 OVERTEMP A HNAAC ABORTED TAKEOFF MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 EA07327EN 261 NR 2 ENGINE OIL TEMP WENT INTO RED ON TAKEOFF, REDUCED POWER AND STABILIZED IN YELLOW. REMOVED AND REPLACED THE OIL FUEL HEATER. 2H72 4T4 TRTA13NM E20NE 20050811002072005081100207WP 2005 8 11 IXXA05SMN122S 120050629A5340 FITTING DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE 1690.000 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, AFT ACCESSORY COMPARTMENT BATHTUB FITTING, CRACKED STA 1690.000 L-34L. REMOVED CRACKED BATHTUB FITTING IAW SRM 51-1-20D PAGE 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW BATHTUB FITTING IAW SRM 51-1-20D PAGE 1. TORQUED IAW SRM 51-3-1. 2L74 4F4 FRT4A25 E2GL 20050811002112005081100211NM 2005 8 11 TSAA0549035 120050807A361014A495 CONNECTOR BOEING737 737230 1384401NM PWA JT8 JT8D* NE BLEED AIR DAMAGED A TSAAF ACTIVATE FIRE EXT. N FALSE WARNING TXTAXI/GRND HDL 1 WP13821AL 23155 NON-ETOPS ON TAXI AFTER LANDING THE CREW GOT AN APU FIRE WARNING LIGHT, COMPLETED APU FIRE CHECK LIST, SHUTDOWN APU AND DISCHARGED APU FIRE BOTTLE. FIRE WARNING LIGHT EXTINGUISHED. AIRCRAFT TAXIED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED APU FIRE BOTTLE AND FOUND NO EVIDENCE OF FIRE. FOUND A LEAK IN THE BLEED AIR DUCT CONNECTOR. THE CONNECTOR WAS REPLACED AND LEAK CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA16WE E2EA 20050812000062005081200006SO 2005 8 12 C2XA05IA096 120050807A2611FDS765A2 SMOKE DETECTOR EMB 145 EMB145LR 3260212SO LAVATORY INOPERATIVE A C2XAA UNSCHED LANDING BN SMOKE/FUMES/ODORS/SPARKS FALSE WARNING NRNOT REPORTED 1 SW2714570133 133 145632 IAH - FLIGHT 2596, THE CREW REPORTED A LAV SMOKE MASTER WARNING WITH WHITE SMOKE IN THE CABIN AND RETURNED TO IAH WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE LAV SMOKE DETECTOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050812000092005081200009SO 2005 8 12 C2XA05SH096 120050809A491014526850401 FIREWALL EMB 135 EMB135LR 3260305SO APU BAY CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715527 145413 SHV - DURING C-CHECK APU FIRE WALL CRACK AROUND NUT PLATE FASTENERS AT 3 O`CLOCK POSITION. MAINTENANCE REPAIRED APU FIREWALL AT 3 O`CLOCK POSITION IAW EC 5330-01483. THE AIRCRAFT WAS APPROVED TO CONTINUED FOR SERVICE. 2L72 4F RTT00011AT 20050812000152005081200015SO 2005 8 12 C2XA05SH097 120050810A532014532636401 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711535 145518 SHV - DURING C-CHECK THE LT OMEGA BEAM HAS CORROSION I/B SIDE AT FR 23-24. MAINTENANCE REPAIRED LT OMEGA BEAM AT FR 23-24 IAW EC 5320-01256. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2L72 4T RTT00011AT 20050812000212005081200021NM 2005 8 12 QXEA200501164 120050810A3060 WARNING SYSTEM BOMBDRDHC8 DHC8402 1390042NM DE ICE SYSTEM ACTIVATED A QXEAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM09404QX 4046 SEA FLIGHT NR 2350: AFTER PUSHBACK, NOTICED PROP DE-ICE CAUTION LIGHT WAS ILLUMINATED. FOLLOWED PROP DE-ICE CAUTION CHECKLIST. LIGHT REMAINED ILLUMINATED. MAINTENANCE FOUND NO FAULTS IN CDS. CLEARED NVM ON NR 1 AND NR 2 PROP DE-ICE. CAUTION LIGHT EXTINGUISHED. TESTED NR 1 AND NR 2 PROP DE-ICE IAW DHC-400 MM 30-61-00-720-801 NUMEROUS TIMES. NO FURTHER FAULTS NOTED. OPS CHECK ALWAYS GOOD DURING TESTING. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050812000252005081200025NM 2005 8 12 05FDEA02379 120050810A5315 FLOORBEAM BOEING727 727227 1384078NM INTERFERENCE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 BS 344 FLOORBEAM SPLICE INTERFER'S WITH BL O SEAT TRACK TO COMPLY WITH BARRIER MOD. 2L73 4F A3WE 20050815000172005081500017NM 2005 8 15 05FDEA02399 120050811A5230 FRAME BOEING727 727227 1384078NM CARGO DOOR GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 MAIN CARGO DOOR AFT SIDE FRAME GOUGED, CENTER OF FRAME. REPAIRED PER SRM 53-30-2. 2L73 4F A3WE 20050815000192005081500019NM 2005 8 15 05FDEA02401 120050811A5330 SKIN BOEING727 727227 1384078NM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 FUSELAGE SKIN HAS A DENT AT BS 1186, 1 INCH BELOW STRINGER 23L. REPAIRED SKIN AT BS 1186 PER SRM 53-30-3. 2L73 4F A3WE 20050815000382005081500038 2005 8 15 RAIA00508011 420050809A34607014300901 FMC EMB 145 EMB145LR 3260212SO NR 1 FAILED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03824HK53 145498 FLT 5493 - STL - PRIMARY FLIGHT DIRECTOR NR 1 FAILED. MAINTENANCE REPLACED NR 1 PFD. 2L72 4T RTT00011AT 20050815000492005081500049 2005 8 15 SWAA052359 420050807A2565D31354 SLIDE BOEING737 7373H4 1384600NM AFT CABIN OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29613SW 27931 DURING SCHEDULED C2 CHECK, FOUND R2 & L2 DOOR EMERGENCY EVAC SLIDES OUT OF ADJUST. ADJUSTED SLIDES PER MM. 2L72 4F RTA16WE 20050815000552005081500055 2005 8 15 SWAA052365 420050808A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050815000582005081500058NM 2005 8 15 SWAA052368 120050808A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LGIHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29413WN 29819 DURING SCHEDULED HC2 CHECK, FOUND SEVERAL EEPLS TRACK COVERS CRACKED. REMOVED AND REPLACED COVERS PER MM. 2L72 4F RTA16WE 20050815000592005081500059NM 2005 8 15 SWAA052369 120050809A335010107451 LIGHT BOEING737 7377H4 1384404NM AFT GALLEY BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29421LV 32452 R2 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20050815000792005081500079NM 2005 8 15 SWAA052375 120050810A53116516301 FRAME BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29317WN 24068 DURING SCHEDULED D CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 188, LT SIDE, WL 208. REMOVED AND REPLACED STUB FRAME PER SRM. 2L72 4F RTA16WE 20050815000822005081500082NM 2005 8 15 SWAA052378 120050810A3350101073 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29362SW 26573 L1 DOOR LOWER EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20050815001002005081500100NM 2005 8 15 05FDEA02429 120050811A5330 SKIN BOEING727 727227 1384078NM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 PREVIOUS REPAIR AT STA 460 TO 470 STR 10L TO 11L IS IAW SRM 53-30-3 AND IS A MAJOR REPAIR. 2L73 4F A3WE 20050825000112005082500011CE 2005 8 25 DXTA200500909 120050819A3246315381 WHEEL CESSNA750 750 2076810CE NLG VIBRATES E DXTAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 GL07999QS970 7500203 DURING T/O ROLL, NOSE STRUT VIBRATES EXCESSIVELY. REMOVED AND REPLACED LT AND RT NOSE GEAR TIRE ASSYS IAW 750 MM 32-41-01. 2L72 4J RTT00007WI 20050825000192005082500019 2005 8 25 SWAA052518 420050820A256563550101 SLIDE BOEING737 7377H4 1384404NM R1 DOOR DEPLOYED A SWAAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW29775SW 30590 DURING SCHEDULED RON CHECK, R1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20050815001152005081500115NM 2005 8 15 05FDEA02440 120050812A5311 FRAME BOEING727 727227 1384078NM UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 REPAIR LOCATED AT APPROX BS 1010 TO 1016 BETWEEN 23L AND 24L, PREVIOUS REPAIR AT STA 1010 TO 1016 BETWEEN STR 23L AND 24L NEEDS ENG EVALUATION TO DETERMINE IF MAJOR OR MINOR AND IF REPAIR IS IAW WITH FAA APPROVED DATA. NO ENGINEERING NEEDED. THIS REPAIR WAS COMPLETED IAW SRM 53-10-4, THIS IS A MAJOR REPAIR IAW GMM 6-2-100. 2L73 4F A3WE 20050815001262005081500126NM 2005 8 15 UPS05445167 120050725A571265B078455 RIB BOEING747 747121 1384871NM LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 LT WING NR 2 VC FLAP I/B ARM I/B SUPT RIB TWO VERTICAL O/B FLANGE UPPER FASTENER HOLE CRACKED, CRACK LENGTH 3/8". SUPPORT RIB REPAIRED AS PER HX RS R-57-41-35350 AND C/OUT REPEAT INSPECTION PER UPS EO.B747-5740-22636-A. 2L74 4F A20WE 20050815001282005081500128NM 2005 8 15 UPS05445169 120050723A531165B017426 FRAME BOEING747 747121 1384871NM M/D CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 M/D BS 980 BETWEEN S20-22R FRAME FWD FACE FOUND CRACK, CRACK LENGTH 0.5" AND 0.75". M/DECK BS 980 BTWEEN STR 20-22R FRAME REPAIRED AS PER HX RS R53-22-35344 AND UPS EO.B747-5310-22630-A. 2L74 4F A20WE 20050815001302005081500130NM 2005 8 15 UPS05445172 120050722A531165B0172245 FRAME BOEING747 747121 1384871NM M/D CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 M/DECK BS 580 LT STR 24L FRAME FOUND CRACKED, CRACK LENGTH 1". M/DECK BS 580 LT STR 23L TO 25L FRAME REPAIRED AS PER HX RS R53-22-35338 AND UPS EO.B747-5310-22626-A. 2L74 4F A20WE 20050815001422005081500142WP 2005 8 15 UPS05845149 120050725A5330 SKIN DOUG DC8 DC873F 302199FWP FS 1746 L15L CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 FUSELAGE EXTERIOR SKIN CRACKED 1/2" LONG AT STA 1746 L15L. CUT OUT DAMAGED SECTION OF SKIN AT STA 1746 AND L15L. FABRICATED, AND IN STALLED REPAIR IAW DC-8 SRM 53-2-1 FIG 7. 2L74 4F RT4A25 20050815001512005081500151WP 2005 8 15 UPS05845159 120050730A534037798741 FITTING DOUG DC8 DC873F 302199FWP FS 834 L18R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 MAIN CABIN STA 834 L18R FRAME TO INTERCOSTAL FITTING CRACKED 1/2" LONG. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20050815001542005081500154WP 2005 8 15 UPS05845162 120050802A53403755842U1 FITTING DOUG DC8 DC873F 302199FWP FS1200 L29L-L28LCORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 "C" PIT BATHTUB FITTING CORRODED AT STA 1200 BETWEEN L29L AND L28L. REMOVED AND REPLACED BATHTUB FITTING IAW DC-8 SRM 53-2-0 FIG 2D AND 51-1-20D. 2L74 4F RT4A25 20050815001592005081500159EU 2005 8 15 05FDEA02326 120050808A5420 SUPPORT BRACKET AIRBUS330 A300* EU GE CF6 CF680C2A5 NE NR 1 PYLON CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25671FE 778 NR 1 ENG HYDRAULIC CASE DRAIN LINES SUPPORT BRACKET CRACKED ACCESS THRU 473CL PNL. 2L72 4F4 FRTA26NM E13NE 20050815001602005081500160WP 2005 8 15 IXXA05SMN143S 120050630A5710 PAN DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE XFS 520.168 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, RT WING. CTR L/E ZEE PAN CRACKED 2 INCHES, XFS 520.168. REMOVED AND REPLACED ZEE PAN ON RT WING CTR. L/E XFS 520.168 IAW SRM 51-1-21, SRM 51-1-20 PAGE 9, 21. 2L74 4F4 FRT4A25 E2GL 20050815001612005081500161EA 2005 8 15 COMA0560419 120050801A3260100865 TARGET CNDAIRCL600 CL6002B19 1900309EA RT MLG UPLOCK LOOSE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01912CA 7011 FLIGHT 5071 - GEAR DISAGREE WARNING, RT MLG INDICATED INTRANSIT. TIGHTENED LOOSE PROX SENSOR TARGET ON RT MLG UPLOCK. 2L72 4F RTA21EA 20050815001642005081500164NM 2005 8 15 CALA0500261 120050811A5320147A57051 INTERCOSTAL BOEING737 737724 13844BYNM STA 986.5-1016 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2724706 28767 INSPECTION FOUND INTERCOSTAL CORRODED AT STA 986.5-1016, LBL 33. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW ECRA 5321-01268. 2L72 4F RTA16WE 20050815001662005081500166NM 2005 8 15 CALA0500263 120050811A5320147A56603 STRUCTURE BOEING737 737724 13844BYNM STA 992.8-1040 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2724706 28767 INSPECTION FOUND CHORD AT R-2 DOOR CORRODED AT STA 992.8 TO 1040, LBL 63. THE CHORD WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND BOEING DRAWING 147A8540. 2L72 4F RTA16WE 20050815001672005081500167NM 2005 8 15 CALA0500264 120050811A5320147A5660YZ INTERCOSTAL BOEING737 737724 13844BYNM STA 947-967 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2724706 28767 INSPECTION FOUND INTERCOSTAL CORRODED AT STA 947-967, RBL 36. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20050815001682005081500168NM 2005 8 15 SWAA052394 120050810A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727B, STR 19L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050815001692005081500169NM 2005 8 15 SWAA052395 120050810A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29362SW 26573 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 530, STR 10R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050815001722005081500172 2005 8 15 SWAA052398 420050811A2565D31354 SLIDE BOEING737 7375H4 138449DNM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29507SW 24184 DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050815001792005081500179NM 2005 8 15 SWAA052405 120050811A53106935366 CREASE BEAM BOEING737 7373H4 1384600NM CABIN FLOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29612SW 27930 DURING SCHEDULED D CHECK, FOUND FUSELAGE CREASE BEAM WEB CORRODED BETWEEN BS 500A AND BS 500B, RBL 60. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050815001812005081500181NM 2005 8 15 SWAA052407 120050811A53156546811 FLOORBEAM BOEING737 7373H4 1384600NM CABIN FLOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29612SW 27930 DURING SCHEDULED D CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 986, BETWEEN LBL 52 TO RBL 52. REPAIRED FLOORBEAM PER BFG ER. 2L72 4F RTA16WE 20050815001832005081500183NM 2005 8 15 SWAA052409 120050811A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM AFT CARGO BAY CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29612SW 27930 DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, RBL 7 TO RBL 10. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050815001842005081500184NM 2005 8 15 SWAA052410 120050811A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM AFT CARGO BAY CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29612SW 27930 DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 767, RBL 7 TO RBL 10. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050815001862005081500186 2005 8 15 SWAA052412 420050810A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29618WN 28034 DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050815001872005081500187NM 2005 8 15 SWAA052413 120050810A335065C3330486 LIGHT BOEING737 7373H4 1384600NM FWD GALLEY MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29618WN 28034 DURING SCHEDULED C2 CHECK, FOUND FWD GALLEY SIDEWALL EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20050815001882005081500188NM 2005 8 15 SWAA052414 120050811A534065C27314 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29690SW 23783 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 520, STR 16L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050815001892005081500189 2005 8 15 SWAA052415 420050811A256565659723 FITTING BOEING737 7373T5 1384608NM GIRT BAR BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29696SW 23064 DURING SCHEDULED 1/4D CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT FLOOR FITTING BROKEN. REMOVED AND REPLACED FITTING PER MM. 2L72 4F RTA16WE 20050815001902005081500190NM 2005 8 15 SWAA052416 120050811A561058935841 WINDOW BOEING737 7377H4 1384404NM COCKPIT CRACKED A SWAAA UNSCHED LANDING O OTHER CLCLIMB 1 SW29707SA 27841 AIR TURNBACK/DECLARED EMERGENCY, L5 COCKPIT WINDOW CRACKED AND SEPARATED FROM AIRCRAFT. REMOVED AND REPLACED R L5 COCKPIT WINDOW PER MM. 2L72 4F RTA16WE 20050815001922005081500192WP 2005 8 15 IXXA05SMN144S 120050630A5730 SKIN DOUG DC8 DC871F 302199DWP CFMINTCFM56 CFM563C 13802EU XFS520.168 IMPROPER B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, RT WING. CTR L/E SKIN FWD PART HAS NON STANDARD REPAIR. PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PAGE 1, SRM 57-3-1 FIG. 5 SHEET 1, EO SEMAN NR 2005910 DATE 06-18-05. REMOVED DAMAGED PLATING WITH INTERIM REPAIR IAW SRM 51-1-21 PAGE 1. FABRICATED NEW PLATING (ALCLAD 7075 T6 0.063”) IAW SRM 57-3-1 FIG. 5 SHEET 1 ITEM (G). CLEANED, TREATED AND PRIMED AREA AND NEW PLATING INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PAGE 1. INSTALLED NEW PLATING IAW SRM 51-1-21 PAGE 1, SRM 51-3-0 PAGE 1, SRM 51-1-20D. TORQUED IAW SRM 51-3-1. 2L74 4F4 FRT4A25 E21EU 20050815001962005081500196NM 2005 8 15 05FDEA02387 120050810A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 BS 277, LBL 14, WL 208 CORROSION ON FLOORBEAM. INSTALLED REPAIR PER SRM 51-40-4, THIS REPAIR IS MAJOR 2L73 4F RTA3WE 20050815001972005081500197NM 2005 8 15 05FDEA02393 120050811A5720 PANEL DOUG MD11 MD11 3023602NM WING BOX CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25624FE 48443 CENTRAL WING BOX FOUND SEVERAL CORROSION ON PANEL AT STA 1219 X=104. PERFORMED REPAIR IAW E.A. 1-5720-88880 PT.1. 2L73 4F RTA22WE 20050815001982005081500198WP 2005 8 15 IXXA05SMN146S 120050630A5720 ANGLE DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE XFS17.500 -11.00DEFORMED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, LT WING INTERIOR ANGLE DEFORMED, STA XFS -17.500 TO XFS -11.000. PERFORMED MAJOR REPAIR, EO MFG NR 2005948 DATE 06-24-05. REMOVED FASTENERS IAW SRM. REMOVED DAMAGED AREA IAW DWG NR ED 4016, PERFORMED NDT INSPECTION. IAW NDT. FABRICATED NEW LWR. STANT PANEL SEGMENT (PLATE 7075 T6 51) + (04 EA) ANGLE REPAIR DOUBLERS (PLATE 7075 T6 51) + (01 EA) REPAIR ANGLE DOUBLER (TITANIUM 651-4V 0.032”) + EXTERNAL REPAIR DOUBLER (ALCLAD 7075 T6 0.071”) +(02 EA) + CLIP (EXTRUSION 7075 T6 51) + SHIM (ALCLAD 7075 T6) IAW DWG ED 4016. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM. INSTALLED REPAIR PARTS AND TORQUED IAW SRM. 2L74 4F4 FRT4A25 E2GL 20050825000202005082500020 2005 8 25 SWAA052519 420050820A256565C16820 HOOK BOEING737 7377H4 1384404NM R1 DOOR SLIDE BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29775SW 30590 DURING SCHEDULED RON CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK BROKEN. REMOVED AND REPLACED HOOK PER MM. 2L72 4F RTA16WE 20050816000012005081600001NM 2005 8 16 QXEA200501168 120050810A2730 WARNING LIGHT BOMBDRDHC8 DHC8402 1390042NM PITCH TRIM ILLUMINATED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09412QX 4059 PDX FLIGHT: PITCH TRIM CAUTION LIGHT ILLUMINATED DURING TAXI OUT. RETURNED TO GATE. MAINTENANCE REINITIALIZED PITCH TRIM SYSTEM VIA CYCLING SHIP'S POWER. POWER-UP SELF-TEST NORMAL. PITCH TRIM CAUTION LIGHTS OUT. PITCH TRIM OPERATION NORMAL. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050816000032005081600003EU 2005 8 16 AWXA200500949 120050721A5313D53470425200 STRINGER AIRBUS320 A320231 3930325EU CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28627AW 66 MCN - MAJOR REPAIR - DURING C4 CHECK DISCOVERED CORROSION IN SEVERAL LOCATION ON STRINGER 42R, FROM FR 54 + 16" TO FR 58 + 6". MAINTENANCE REMOVED CORROSION ON STRINGER 42R, FROM FR 54 + 16" TO FR 58 + 6", IAW AIRBUS 320 SRM 51-74-00. NO ALLOWABLE DAMAGE LIMITS ARE AVAILABLE IN THE AIRBUS A320 SRM. MAINTENANCE REMOVED DAMAGED SECTION FROM STRINGER 42R IAW AMERICA WEST AIRLINES ENGINEERING REPAIR 26-5341-05215-SS1. FABRICATED ANGLE IAW AWA ER 26-5341-05215-SS1. PREPARED ANGLE, STRINGER, CLIPS FOR INSTALLATION IAW AWA ER 26-5341-05215-SS1. INSTALLED REPAIR PART ON STRINGER 42R. FROM FR 54 + 16" TO FR 58 + 6" IAW AWA ER 26-5341-05215-SS1. 2L72 4F RTA28NM 20050816000092005081600009EA 2005 8 16 SWIA200515407 120050808A274183963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07909SW5892 5892 7558 STAB TRIM CH 2 WILL NOT ENGAGE. REMOVED AND REPLACED HSTCA AND MOTOR CONTROL UNIT IAW MM 27-40-00, 27-42-01, 27-42-05. OPERATIONAL CHECK GOOD, P/N: 7062-3, S/N OFF: 9911. 2L72 4F RTA21EA 20050816000132005081600013SO 2005 8 16 SWIA200515411 120050731A5210 SEAL EMB 120 EMB120ER 3260203SO PAX DOOR DIRTY A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07584SW 120352 MAIN CABIN DOOR IS DIFFICULT TO OPEN OR CLOSE. REMOVED FOD FROM AROUND DOOR SEAL. NO OTHER DEFECTS FOUND. CYCLED DOOR SEVERAL TIMES. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050816000152005081600015SO 2005 8 16 SWIA200515413 120050802A3350D36604001 BATTERY EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT DISCHARGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07291SW8561 8561 120318 FOUR CONSECUTIVE WHITE EMERGENCY FLOOR LIGHTS INOP. REPLACED EMERGENCY LIGHT BATTERY. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050816000162005081600016EA 2005 8 16 SWIA200515414 120050803A274070623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07976SW 7952 STAB CH1 INOP, STATUS MSG. REPLACED HORIZONTAL STAB MOTOR CONTROL UNIT. OPERATIONAL CHECK GOOD IAW CRJ 200 MM 27-42-05. 2L72 4F RTA21EA 20050816000172005081600017EA 2005 8 16 SWIA200515415 120050810A2741 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA VERTICAL STAB INOPERATIVE A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07459SW 7782 STAB NR 2 CHANNEL WILL NOT ENGAGE. REPLACED FOS TRIM SWITCH IAW MM 27-41-05. OPERATIONAL CHECK GOOD IAW AMM 27-44-00. 2L72 4F RTA21EA 20050816000182005081600018WP 2005 8 16 ARWA20050802 120050812A2612 ENGINE DOUG DC10 DC1030 3023501WP NR 1 FIRE A ARWAA UNSCHED LANDING AJ FLAME/FIRE WARNING INDICATION CLCLIMB 1 SO19526MD 46998 ON CLIMBOUT, NR 1 ENGINE FIRE LIGHT AND BELL. ENGINE FIRE SEVERE DAMAGE CHECK COMPLIED WITH. REMOVED AND REPLACED NR 1 ENGINE LOWER FIRE DETECTOR TUBE ASSEMBLY AND "A" SENSING FIRE LOOP/GROMMETS IN ACCORDANCE WITH M/M 26-11-01 AND INSPECTED FOR ANY LEAKS PNEUMATICS FOUND NORMAL IN ACCORDANCE WITH M/M 36-00 AND M/M 71-00-00; PERFORMED ENGINE RUN-UP AT TAKE OFF POWER ON ENGINE NR 1 IN ACCORDANCE WITH MM 71-00-00, FOUND NORMAL, NO DISCREPANCIES NOTED. 2L73 4F A22WE 20050816000192005081600019WP 2005 8 16 ARWA20050801 120050809A2997 WIRE HARNESS DOUG DC10 DC1030F 3023504WP NR 1 AUX PUMP BURNED A ARWAO OTHER J WARNING INDICATION CRCRUISE 1 SO19478CT 47819 NR 1 AUXILIARY PUMP POPS C/B. T/S FOUND WIRE BUNDLE IN RT WHEEL WELL BURNED AT STA. 1381 FORWARD BULKHEAD; REROUTED WIRE BUNDLE RT WHEEL WELL FORWARD BULKHEAD STATION 1381 IN ACCORDANCE WITH 20-50-02; AUXILIARY PUMP CHECKED NORMAL IN ACCORDANCE WITH M/M 29-21-01 AND M/M 29-22-04. 2L73 4F RTA22WE 20050816000222005081600022WP 2005 8 16 AALA20050513 120050809A3242 BRAKE DOUG DC9 DC982 3022082WP MLG OVERHEATED A AALAC ABORTED TAKEOFF MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 SW21484AA 49677 PIT - ABORTED TAKEOFF DUE TO RIGHT HAND COMPRESSOR STALL. UPON ABORT BRAKES OVERHEATED AND TIRE LOST PRESSURE. REPLACED TIRES AND BRAKES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050816000242005081600024WP 2005 8 16 IXXA05RNG032S 120050721A5753XF976090 SUPPORT FITTING DOUG DC8 DC862F 3021972WP TE FLAP CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW1171CX 670243317 45961 DURING ROUTINE "C" CHECK, CRACK 0.385" LONG WAS FOUND ON THE LEFT WING INBOARD FLAP AT FITTING LOCATED AROUND STATION XF 97-6090 INBOARD. LEFT WING OUTBOARD FLAP SUPPORT FITTING WAS REPAIRED IAW EWO ATI 57-022 AND EO ATI-070805. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR. 2L74 4F 4A25 20050816000252005081600025WP 2005 8 16 IXXA05RNG033S 120050721A5753 SUPPORT FITTING DOUG DC8 DC862F 3021972WP TE FLAP CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW1171CX 670243317 45961 DURING ROUTINE "C" CHECK, CRACK 0.2740" LONG WAS FOUND ON THE LEFT WING OUTBOARD FLAP AT FITTING LOCATED AROUND STATION XF 339.7232 INBOARD. LEFT WING INBOARD FLAP SUPPORT FITTING WAS REPAIRED IAW EWO-ATI-57-023 AND EO ATI-070905. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR. 2L74 4F 4A25 20050816000262005081600026WP 2005 8 16 IXXA05RNG034S 120050721A5753 SUPPORT FITTING DOUG DC8 DC862F 3021972WP PWA JT3D JT3D* 52039NE TE FLAP CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW1171CX 670243317 45961 DURING ROUTINE "C" CHECK, CRACK 0.5220" LONG WAS FOUND ON THE LEFT WING OUTBOARD FLAP AT FITTING LOCATED AROUND STATION XF 339.7232 OUTBOARD. LEFT WING OUTBOARD FLAP SUPPORT FITTING WAS REPAIRED IAW EWO ATI 57-024 AND EO ATI-071005. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR. 2L74 4F4 F 4A25 1E8 20050816000272005081600027WP 2005 8 16 IXXA05RNG036S 120050718A5730 SKIN DOUG DC8 DC862F 3021972WP LT WING CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW1171CX 670243317 45961 DURING INSPECTION CHECK, SKIN CORROSION DAMAGE WAS FOUND ON THE LEFT INNER WING AT OUTBOARD EXTENDED LEADING EDGE SLOT AROUND L/E STATION XFS 207.00. REMOVED CORROSION AND ACCOMPLISHED REPAIR "DOUBLER" IAW EWO ATI 57-028 AND EO ATI-071205. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR. 2L74 4F 4A25 20050816000292005081600029WP 2005 8 16 IXXA05RNG038S 120050719A5730 SKIN DOUG DC8 DC862F 3021972WP PWA JT3D JT3D* 52039NE RT WING CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW1171CX 670243317 45961 DURING A "C" CHECK INSPECTION, FOUND SKIN CORROSION DAMAGE ON THE RIGHT OUTER WING AT THE INBOARD EXTENDED L/E STA XFS 653.750. RT WING L/E UPPER SKIN WAS REPAIRED IAW EWO ATI 57-030 AND EO ATI-071305. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR. 2L74 4F4 F 4A25 1E8 20050816000312005081600031WP 2005 8 16 IXXA05RNG042S 120050719A5730 SKIN DOUG DC8 DC862F 3021972WP RT WING CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW1171CX 670243317 45961 DURING A ROUTINE C CHECK INSPECTION, FOUND CORROSION OVER EXISTING REPAIR ON WING ON INNER OUTBOARD EXTENDED L/E SLAT STA XFS 207-XILD42. CORROSION ON RT WING LEADING EDGE UPPER SKIN WAS REMOVED AND REPAIR "DOUBLER' WAS INSTALLED IAW EWO ATI 57-034 AND SRM 57-2-1 FIG 44. 2L74 4F 4A25 20050816000322005081600032WP 2005 8 16 IXXA05RNG035S 120050721A5753 SUPPORT FITTING DOUG DC8 DC862F 3021972WP TE FLAP CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW1171CX 670243317 45961 DURING ROUTINE "C" CHECK, CRACKS 2.023" AND 0.521" LONG WERE FOUND ON THE LEFT WING OUTBOARD FLAP AT FITTING STA XF 409.6675 OUTBOARD. FITTING WAS REPAIRED IAW EWO ATI 57-025 AND EO ATI-071105. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR. 2L74 4F 4A25 20050816000352005081600035NM 2005 8 16 DHL2005747500 120050712A5320 WEB BOEING727 727224 1384076NM CARGO BAY CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01747DH 22253 CORROSION ON WEB AFT CARGO BIN FS 950 TO FS 950A AT STR 27R. REMOVED CORROSION ON WEB IN AFT CARGO BIN FS 950 TO 950A AT STR 27R. FOUND OUT OF LIMITS. OPEN PANEL NR 3622 FOR ACCESS. REMOVED FLOOR SUPPORT SPLICE ANGLE SAT 950A TO 950B LONGERON 27R. REMOVED OUT OF LIMITS WEB. FOUND WEB STIFFENER ANGLE CRACKED. LOCATED AN DRILLED NEW -6 CLIP, -14 WEB AN INSTALLED. INSTALLED FLOOR SUPPORT SPLICE ANGLE. CLOSED PANEL NR 3622 IAW B-727 SRM 51-30-2, 53-10-1 AND 51-30-3. 2L73 4F A3WE 20050816000362005081600036NM 2005 8 16 DHL2005747501 120050710A5753 SKIN BOEING727 727224 1384076NM TE FLAP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01747DH 22253 CRACK IN T/E FLAP SHIM AT NR 2 ATTACH CUT OUT I/B SIDE LOWER SIDE LEFT WING. FABRICATED REPAIR DOUBLER, CHEM TREATED AN PRIMED AN INSTALLED REPAIR DOUBLER IAW B-727 SRM 57-50-4,51-10-2 AND 51-20-0 PG 1 OF B727 MM, AT T/E FLAP SKIN AT NR 2 ATTACH CUT OUT I/B LOWER SIDE LT WING. 2L73 4F A3WE 20050816000372005081600037NM 2005 8 16 DHL2005747502 120050727A5753 WEDGE BOEING727 727224 1384076NM TE FLAP DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01747DH 22253 LEFT WING INBD MID FLAP T/E WEDGE APPROX 61" FROM INBD END HAS AREA OF DELAMINATION ON BOTTOM SKIN. REPAIRED LEFT INBD MID FLAP T/E INNER BOTTOM SKIN AT APPROX 61" FROM INBD END IAW B-727 SRM 51-40-20 PAR 20-22 BY INSTALLING DOUBLER REPAIR. 2L73 4F A3WE 20050816000402005081600040NM 2005 8 16 05FDEA02425 120050811A3411 PITOT LINE BOEING727 72722 1384002NM AIRSPEED OBSTRUCTED A FDEAA UNSCHED LANDING O OTHER CLCLIMB 1 SO25192FE 19085 AFTER TAKE F/O NOTED AIRSPEED INDICATOR STOPPED ACCELERATING BEYOND 140 KTS AS CAPTAIN LEVEL AT 3000, F/O ALTIMETER READ 2000 F/O AIRSPEED INOP FLAG CAME INTO VIEW. NO C/B'S OUT. F/O SELECTED ALTERNATE STATIC SOURCE THEN F/O'S A.S AND ALTIMETER THEN MATCHED CAPTAINS. BLEW NITROGEN FORWARD THROUGH TUBE. RETRIEVED REMNANTS OF BUG. PERFORMED PITOT/STATIC SYS TEST IN FO SIDE IAW MM 34-11-000-5, PITOT PASSED BUT STATIC TEST, FAILED. ISOLATED F/O'S STATIC LEAK TO THE NR 2 PNEUMATIC MACH AIRSPEED WARNING SWITCH, REPLACED SAME REF MM 34-14-012-4. ACCOMPLISHED ADJ/TEST 34-11-000-5. LEAK CKS AND INDICATIONS NORMAL. 2L73 4F A3WE 20050816000422005081600042WP 2005 8 16 05FDEA02449 120050812A5714 STRUCTURE DOUG DC10 DC1010 3022110WP GE CF6 CF66K 30020NE ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25564FE 46984 CTR WING LWR BARREL STA 1216 LONGERON 48 REWORK OF CORROSION 40 PERCENT. MATERIAL LOSS TO STANDING LEG. CUT OUT CORRODED SECTION OF LONGERON IAW SRM 53-00-01 FIG 7 VOL I GN 16. 2L73 4F4 F A22WE E23EA 20050816000442005081600044SO 2005 8 16 C2XA05RI015 120050714A3350 LIGHT EMB 145 EMB145 3260210SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716963 145116 RIC - DURING ACFT ROUTINE INSPECTION, LT FWD EMERGENCY LIGHT OVER THE WING DID NOT ILLUMINATE. SYSTEM WAS MEL'D. ACFT WAS RELEASED FOR FLT. (OPEN) 2L72 4F RTT00011AT 20050816000452005081600045SO 2005 8 16 C2XA05IA088 120050713A335078241 INVERTER EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2711121 145683 MCI - DURING SCHEDULED MAINTENANCE, THE RIGHT OVERWING EMERGENCY EXIT MARKER WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 INVERTER, OPERATIONALLY TESTED THE EMERGENCY LIGHTING SYSTEM, AND CLEARED THE DISCREPANCY. 2L72 4F RT 20050816000462005081600046SO 2005 8 16 C2XA05IA089 120050714A3350 SIGN EMB 145 EMB145LR 3260212SO SERVICE DOOR MALFUNCTIONED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2711565 145621 ORF - DURING PREFLIGHT INSPECTION, THE FLIGHT CREW REPORTED THE SERVICE DOOR EXIT SIGN NOT ILLUMINATING WHEN TESTED. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY EXIT LIGHTING SYSTEM AND THE SERVICE DOOR EXIT SIGN OPERATED NORMALLY WITHOUT ANY DEFECTS NOTED. MAINTENANCE THEN CLEARED THE DISCREPANCY. 2L72 4T RTT00011AT 20050816000482005081600048SO 2005 8 16 C2XA05BT049 120050719A3350RPS1B BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT FAULTY A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713955 145075 BTV---CO2874, DURING SERVICE AND ROUTINE CHECK MAINTENANCE, FOUND THE SERVICE DOOR EMERGENCY LIGHT TO NOT BE WORKING. REMOVED AND REPLACED NR 2 BATTERY CHARGER IAW EMB145 AMM NR 33-50-05, OPS CHECK GOOD. 2L72 4T RTT00011AT 20050816000512005081600051NM 2005 8 16 05FDEA02453 120050812A5315651759393 FLOORBEAM BOEING727 727200 138407ENM MAIN CARGO BAY CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 MAIN CARGO DECK FLOORBEAM STA 312 LBL 32 SUPPORT IS CRACKED. REMOVED AND REPLACED SUPPORT IAW SRM 51-30-2. 2L73 4F RTA3WE 20050816000522005081600052SO 2005 8 16 C2XA05BT050 120050719A3397 WIRE EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BROKEN A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713955 145075 BTV---CO2874, DURING SERVICE AND ROUTINE CHECK, MAINTENANCE FOUND THE FLOOR EMERGENCY AISLE PATH STRIP HAD A BROKEN WIRE. REMOVED AND REPLACED EMERGENCY LIGHT STRIP IAW EMB145 AMM NR 33-50-12, OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050816000542005081600054NM 2005 8 16 05FDEA02454 120050812A5754 SKIN BOEING727 727200 138407ENM NR 2 SLAT UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 LEFT SLAT NR 2 HAS PREVIOUS REPAIR ON LWR SURFACE THAT IS A MAJOR REPAIR IAW SRM 57-50-3 FIG 1. 2L73 4F RTA3WE 20050816000562005081600056SO 2005 8 16 C2XA05IA092 120050724A335078812 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713988 145265 CRP - DURING MAINTENANCE INSPECTION, THE NUMBER THREE EMERGENCY FLOOR PROXIMITY LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050816000602005081600060NM 2005 8 16 05FDEA02459 120050813A5414B277101801 SKIN BOEING727 727200 138407ENM NR 1 NACELLE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 NR 1 ENGINE UPPER COWL INNER AND OUTER SKIN IS CRACKED. REPLACED UPPER COWL TO BE INST ON WC 74C101-01. 2L73 4F RTA3WE 20050816000642005081600064NM 2005 8 16 05FDEA02463 120050813A5312 BULKHEAD BOEING727 727200 138407ENM CARGO BAY UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 PREVIOUS REPAIR AFT PIT AT 1183 BULKHEAD IS A MAJOR REPAIR IAW EO 7-5310-7-2344. 2L73 4F RTA3WE 20050816000662005081600066NM 2005 8 16 DHL2005747504 120050710A5753 SKIN BOEING727 727224 1384076NM TE FLAP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01747DH 22253 CRACK IN T/E FLAP LWR SKIN AT NR 3 ATTACH CUT OUT I/B SIDE LT WING. FABRICATED REPAIR DOUBLER, CHEM TREATED AND PRIMED AND INSTALLED REPAIR DOUBLER IAW B727 SRM 57-50-4,51-10-2 AN 51-20-0 PG 1 OF MM AT T/E FLAP LOWER SKIN NR 3 ATTACH CUTOUT I/B SIDE OF LT WING. 2L73 4F A3WE 20050816000682005081600068EU 2005 8 16 0501243303 120050712A324226122023 BRAKE AIRBUS330 A330323 3930335EU MLG CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01803NW8383 00542 DURING LINE CHECK FOUND NR 6 BRAKE COMPROMISED. REMOVED AND REPLACED BRAKE 33-3240-9-0001, S/N 00047 AND BRAKE WAS SENT TO HONEYWELL FOR REPAIR. VENDOR TEARDOWN FINDINGS BRAKE S/N 00047 WAS FOUND WITH THERMAL OXIDATION, PRESSURE PLATE WAS MISSING, WITH WEAR PINS HANGING OFF OF BRAKE HOUSING, ROTOR NR 1 HAS GROOVE WORN IN IT FROM PISTONS, ROTOR NR 2 CHIPPING INSIDE EDGE, ROTORS NR 3, 4, AND 5 LOOKED GOOD. ALL STATORS WERE MISSING LUGS AND CRUMBING, BACK PLATE CHIPPING ON EDGES. 2L72 4F RTA46NM 20050816000692005081600069NM 2005 8 16 SB05093 120050815A335020131A BATTERY PACK BOEING737 7373B7 1384580NM EMERGENCY LIGHT DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19389US 23311 CLT - MAINTENANCE REPORTED THE AFT LEFT-HAND INTERIOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT STATION 753L. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050816000712005081600071NM 2005 8 16 SWAA052428 120050813A335007912 COVER BOEING737 7377H4 1384404NM CABIN DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29474WN 33861 DURING SCHEDULED MV3 CHECK, FOUND EEPLS TRACK COVER DAMAGED AT ROW 22 ABC. REMOVED AND REPLACED COVER PER MM. 2L72 4F RTA16WE 20050816000732005081600073NM 2005 8 16 SWAA052430 120050812A53306545765 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29512SW 24189 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 10R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050816000742005081600074NM 2005 8 16 SWAA052431 120050811A3350101073 LENS BOEING737 7375H4 138449DNM AFT GALLEY BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29524SW 26566 DURING SCHEDULED SPECIAL VISIT, FOUND L2 DOOR EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER SRM. 2L72 4F RTA16WE 20050816000752005081600075NM 2005 8 16 SWAA052432 120050812A53306545765 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29525SW 26567 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 11R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050816000762005081600076NM 2005 8 16 SWAA052433 120050812A534065C27314 CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29612SW 27930 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727A, STR 19L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050816000772005081600077NM 2005 8 16 SWAA052434 120050813A3350207377 LENS BOEING737 7373H4 1384600NM MID CABIN DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 RIGHT OVERWING EMERGENCY EXIT LIGHT LENS FELL OFF. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20050816000852005081600085NM 2005 8 16 SWAA052420 120050810A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29329SW 23693 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 16R. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050816000862005081600086NE 2005 8 16 SWAA052418 220050811A7200CFM567B ENGINE BOEING737 7377H4 1384404NM CFMINTCFM567CFM567B22 13802NE RT PYLON FAILED A SWAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW29207WN 34012 892187 INFLIGHT SHUTDOWN/AIR TURNBACK/DECLARED EMERGENCY. LOST OIL QUANTITY & OIL PRESSURE ON NR 2 ENGINE. REMOVED AND REPLACED NR 2 ENGINE PER MM. 2L72 4F4 FRTA16WE E00055EN 20050816000872005081600087 2005 8 16 SWAA052419 420050811A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050816000882005081600088NM 2005 8 16 SWAA052424 120050811A53306545775 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29354SW 25219 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 847, BETWEEN STR 23R & STR 24R. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050816000892005081600089NM 2005 8 16 SWAA052425 120050811A53306545775 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29354SW 25219 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 827, STR 22L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050816000912005081600091NM 2005 8 16 SWAA052427 120050812A335010107451 SIGN BOEING737 7377H4 1384404NM MID CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29472WN 33831 RIGHT MID CABIN EMERGENCY EXIT SIGN MISSING. INSTALLED SIGN PER MM. 2L72 4F RTA16WE 20050816000942005081600094NM 2005 8 16 SWAA052426 120050813A3350207377 LENS BOEING737 7377H4 1384404NM AFT CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29453WN 29847 DURING SCHEDULED RON CHECK, FOUND EEPLS TRACK LENS MISSING AT ROW 22 ABC. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20050816000982005081600098NM 2005 8 16 SWAA052449 120050814A33506042221 LIGHT BOEING737 7377Q8 1384418NM FWD GALLEY BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29799SW 28209 L1 DOOR LOWER EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20050816001002005081600100NM 2005 8 16 SWAA052436 120050814A53306545765 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29690SW 23783 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C + 4, STR 10L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050816001012005081600101NM 2005 8 16 SWAA052437 120050814A53306545765 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29690SW 23783 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D + 18, STR 12L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050816001022005081600102NM 2005 8 16 SWAA052438 120050814A5510BAC1506 STIFFENER BOEING737 7373G7 1384595NM HORIZONTAL STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29690SW 23783 DURING SCHEDULED 1/4D CHECK, FOUND LT HORIZONTAL STAB ANGLE CRACKED AT STA 213, AFT SPAR UPPER CORNER. REMOVED AND REPLACED VERTICAL STIFFENER PER SRM. 2L72 4F RTA16WE 20050816001032005081600103NM 2005 8 16 SWAA052439 120050814A53126546568 BULKHEAD BOEING737 7373G7 1384595NM BS 1016 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29690SW 23783 DURING SCHEDULED 1/4D CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT STR 7L. REPAIRED WEB PER SWA EA. 2L72 4F RTA16WE 20050816001052005081600105NM 2005 8 16 SWAA052441 120050814A53306545765 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29696SW 23064 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 10L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050816001062005081600106NM 2005 8 16 SWAA052442 120050814A53406551698 SPLICE BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29696SW 23064 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER SPLICE CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20050816001072005081600107NM 2005 8 16 SWAA052443 120050814A534065C27314 CLIP BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29696SW 23064 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 520, STR 16L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050816001082005081600108NM 2005 8 16 SWAA052444 120050814A534065C27314 CLIP BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29696SW 23064 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 500D, STR 7L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050811001472005081100147CE 2005 8 11 DXTA200500885 120050805A3150 COMPUTER CESSNA750 750 2076810CE INOPERATIVE E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07941QS 7500141 TAKEOFF ABORTED FOR AMBER MESSAGE WITH CAUTION LIGHT, MACH TRIM INOP, YAW INOP, ALSO HAD CYAN FGC A INOP. PERFORMED OPS CHECKS ON BOTH FGC'S IAW PRIMUS 2000 INTEGRATED AVIONICS SYSTEMS TEST AND FAULT MANUAL, OPS CHECKS SERVICEABLE. 2L72 4J RTT00007WI 20050811001482005081100148CE 2005 8 11 DXTA200500887 120050808A2720 RUDDER CESSNA750 750 2076810CE OSCILLATES E DXTAO OTHER F FLT CONT AFFECTED CRCRUISE 1 GL07912QS 7500012 UPPER RUDDER OSCILLATING FULL DEFLECTION WITH IN GREEN ARC AT HIGH SPEED LIMITS CHANGED FGC WITH NO CHANGE. 2L72 4J RTT00007WI 20050811001512005081100151CE 2005 8 11 DXTA200500892 120050808A2820651631155 PIPE CESSNA500 560CESSNA 2076750CE FUEL SYS CHAFED E DXTAK NONE O OTHER ININSP/MAINT 1 GL07800QS 5600598 MCC REQUEST TO INSPECT LINE ASSY, (REFUEL/DEFUEL FLOW) P/N 6516311-55 (IPC 28-22-00 ITEM #156) FOR CHAFING BY FLAP CROSS OVER CABLE. REMOVED PANELS 171BB AND 172BB FOR VISUAL ACCESS NR FOUND CHAFING IN ACCESS PNL 172BB ON SP FUELING LINE. MEASURED CHAFFING TO BE AT .003 ". INSTALLED NEW LINE IAW 560 MM 28-22-008, LEAK DUE LEAK CHECK GOOD. 2L72 4F RTA22CE 20050811001602005081100160NM 2005 8 11 ASAA0580344 120050613A533059101573 SKIN DOUG MD80 MD83 3023681NM FS 1174-1193 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - DURING HV CHECK, AFT CARGO BAY DOOR SKIN DENTED. RECONTOURED SKIN AND INSTALLED REPAIR DOUBLER. (M) 2L72 4F RT 20050811001652005081100165EA 2005 8 11 ASOA05631 120050724A325016735107 SWITCH CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NLG STEERING INOPERATIVE A ASOAO OTHER O OTHER APAPPROACH 1 SO27915EV 7754 ON APPROACH, THE CREW RECEIVED A STEERING INOP CAUTION MESSAGE WHEN THE GEAR WAS SELECTED TO THE DOWN POSITION. THE CREW TRIED TO RESET THE NOSE WHEEL STEERING SWITCH, BUT THE SWITCH WOULD NO RESET. THE QRH WAS FOLLOWED. AN EMERGENCY WAS NOT DECLARED, BUT EMERGENCY TRUCKS WERE ROLLED OUT AS A PRECAUTION. AIRCRAFT LANDED AND TAXIED TO THE GATE WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LT FEEDBACK RVDT AND ADJUSTED THE RT RVDT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050811001722005081100172WP 2005 8 11 UPS05845116 120050710A5340 FITTING DOUG DC8 DC873F 302199FWP FS 1756 L14L CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE:C1 LEFT AFT MAIN CABIN FS 1756 LONG 14L UPPER FLANGE AT FRAME INTERSECTION CRACKED .500" LONG. REMOVED LONG SECTION AT STA 1756 LONG 14L IAW SRM 51-1-21. FABRICATED AND INSTALLED REPAIR SPLICE AT STA 1756-1764 L14L IAW SRM 53-02-02 FIG 11 AND SRM 51-1-20D. 2L74 4F RT4A25 20050811001782005081100178WP 2005 8 11 UPS05845122 120050711A5320 INTERCOSTAL DOUG DC8 DC873F 302199FWP FS1473 L34R CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE:C1 D-PIT FS 1473 LONG 34R LWR RETURN FLANGE ON INTERCOSTAL IN LONGERON HAS HEAVY EXFOLIATION 4.00". REMOVED INTERCOSTAL ATTACH ANGLE AT STA 1473 LONG 34R IAW SRM 51-1-20D. FABRICATED AND INSTALLED INTERCOSTAL ATTACH ANGLE AT STA 1473 LONG 34R IAW SRM 51-1-20D AND DWG 5616674. 2L74 4F RT4A25 20050811001932005081100193NM 2005 8 11 UPS05445135 120050722A531165B0172450 FRAME BOEING747 747121 1384871NM M/D CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE:C M/D BS 620 LT STR 25 FRAME FOUND CRACKED (CRACK LENGTH 5/8"). M/D BS 620 LT STR 24 TO STR 26 AREA FRAME REPAIRED AS PER HX RS R53-22-35340 & UPS EO B747-5310-22628-A. 2L74 4F A20WE 20050811001952005081100195NM 2005 8 11 UPS05445137 120050722A531165B0171815 FRAME BOEING747 747121 1384871NM M/D CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE:C M/D BS 940 S25L FRAME FOUND CRACKED (CRACK LENGTH 0.50"). M/D BS 940 STR 24L TO 26L AREA FRAME REPAIRED AS PER HX RS R53-22-35340 & UPS EO B747-5310-22628-A. 2L74 4F A20WE 20050811001972005081100197NM 2005 8 11 UPS05445139 120050729A531165B04346160 FRAME BOEING747 747121 1384871NM M/D CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE:C M/D BS 2180 FRAME WEB S24R STR CUTOUT FOUND CRACK (CRACK LENGTH 0.75" & 0.5"). M/D BS 2180 STR 23R TO STR 26R FRAME REPAIRED AS PER HX RS R53-62-35345 & UPS EO B747-5310-22631-A. 2L74 4F A20WE 20050811002132005081100213NM 2005 8 11 SB05090 120050808A3260655825029 CIRCUIT CARD BOEING737 737301 1384611NM GE CFM56 CFM56* 13802NE E11 LOGIC SHELF FAULTY A USAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19558AU 23512 AFTER TAKEOFF, ENROUTE, CAPTAIN REPORTED THE RT MLG RED UNSAFE LIGHT ILLUMINATED. CREW RECYCLED THE GEAR AND LIGHT EXTINGUISHED. CAPTAIN ELECTED TO RETURN TO FIELD WHERE THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. NORMAL GEAR INDICATION OF 3 GREEN LIGHTS WERE OBSERVED AFTER GEAR EXTENSION. NO EMERGENCY WAS DECLARED. AIRCRAFT WAS THEN MAINTENANCE FERRIED. MAINTENANCE ACCOMPLISHED TROUBLESHOOTING TASK IAW MM 32-61-00. REMOVED AND REPLACED MAIN GEAR RED LIGHT CIRCUIT CARD M986. LANDING GEAR POSITION INDICATING AND WARNING SYSTEM OPERATIONAL CHECK NORMAL IAW MM 32-61-00 AND MM 32-09-20-844-030. 2L72 4F4 FRTA16WE E2GL 20050812000082005081200008SO 2005 8 12 C2XA05BT056 120050805A2120 ODOR EMB 145 EMB145LR 3260212SO CABIN DETECTED A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW2714993 145289 CREW REPORTED, VERY STRONG FUEL OR EXHAUST ODOR IN GALLEY AND GALLEY CLOSETS. RAN NR 1 AND NR 2 ENGINES, OPS CHECK OF ENGINE BLEED SYSTEMS CHECKS GOOD, VISUAL INSPECTION OF FORWARD CABIN AREA [GALLEYS, CLOSETS, SPACES] NO DEFECTS, NO ODORS NOTED IAW EMB145 AMM 71-00-01, 36-11-01, AND 05-20-18. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20050812000142005081200014SO 2005 8 12 C2XA05SH098 120050809A491014526850401 FIREWALL EMB 145 EMB145LR 3260212SO APU BAY CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711535 145518 SHV - DURING C-CHECK APU FIREWALL CRACKED AROUND FASTENER 2 3 O`CLOCK POSITION. MAINTENANCE REPAIRED APU FIREWALL AT 3 O`CLOCK POSITION IAW EC 5330-01483. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2L72 4T RTT00011AT 20050812000172005081200017NM 2005 8 12 CALA0500260 120050728A5230143A61109 SKIN BOEING737 737824 13844BZNM CARGO DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718243 28806 INSPECTION FOUND A 1.5" CRACK AT THE FORWARD LOWER CORNER OF THE FORWARD CARGO DOOR SKIN. REPAIRED IAW ECRA 5230-01748. 2L72 4F RTA16WE 20050812000182005081200018NM 2005 8 12 BB05065 120050810A2611 SMOKE WARNING BOEING757 7572B7 1384964NM LAVATORY ACTIVATED A USAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA19608AU 22204 FLT 310 - EN ROUTE BWI TO CLT - IN FLIGHT, THE MID LAVATORY SMOKE DETECTOR BEGAN ALARMING. CREW NOTICED AN OIL ODOR IN FLIGHT. FLIGHT CONTINUED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PLACED THE LEFT PACK ON MEL. PERFORMED A SATISFACTORY PACK TEMPERATURE CONTROLLER BITE CHECK. NO FAULTS WERE FOUND. OPERATIONALLY CHECKED THE LEFT PACK WITH THE ENGINES RUNNING. NO ODORS WERE DETECTED AND THE FLOW/COOLING WAS NORMAL. REMOVED THE MEL. OK FOR SERVICE. 2L72 4F RTA2NM 20050812000222005081200022NM 2005 8 12 05FDEA02376 120050809A54136519647220 LONGERON BOEING727 727227 1384078NM NR 2 NACELLE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 NR 2 ENG RT AFT COWL AFT LOWER CORNER IS CRACKED. REMOVED AND REPLACED FRAME IAW SRM 51-30-2. 2L73 4F A3WE 20050815000082005081500008NM 2005 8 15 05FDEA02389 120050811A5714 STRUCTURE DOUG MD11 MD11 3023602NM WING BOX UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25624FE 48443 REPAIR ASSESSMENT (EO 1-5100-7-5001) FOUND EXT DOUBLER LOCATED ON CTR WING BOX RT SIDE LOWER STA 1235. REPAIR IS IN COMPLIANCE WITH FAA FORM 8100-9. 2L73 4F RTA22WE 20050815000282005081500028NM 2005 8 15 AWXA200500944 120050726A532065528941 ANGLE BOEING737 7373Y0 1384671NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28334AW 23747 DURING C16 CHECK DISCOVERED ANGLE CRACKED AT BS 540, BL 2L AND WL 208. MAINTENANCE REMOVED ANGLE AT BS 540, BL 2L, WL 208 IAW BOEING 737-300 SRM 51-40-02. RECEIVED NEW ANGLE AND PREPARED FOR INSTALLATION IAW BOEING 737-300 SRM 5140-05-0 FIG 2. INSTALLED REPAIR PARTS AT BS 540, BL 2L, WL 208 IAW BOEING 737-300 SRM 51-40-02-0. 2L72 4F RTA16WE 20050815000302005081500030NM 2005 8 15 AWXA200500946 120050725A52106545871523 SKIN BOEING737 7373Y0 1384671NM R1 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28334AW 23747 DURING C16 CHECK, DISCOVERED R1 DOOR LOWER HINGE CUTOUT ON DOOR CRACKED, .3 INCHES IN LENGTH, AT THE AFT LOWER CORNER, BS 300, STRINGER 14R. MAINTENANCE REMOVED AREA ON SKIN AT IAW AMERICA WEST AIRLINES ENGINEERING REQUEST 03-5241-05208-ES3. FABRICATED REPAIR DOUBLER IAW AWA ER 03-5241-05208-ES3. INSTALLED REPAIR PARTS IAW AWA ER 03-5341-05108-ES3. 2L72 4F RTA16WE 20050815000332005081500033NE 2005 8 15 QXEA200501160 220050807A73204120T02P03 ACTUATOR CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 30049NE VARIABLE SLAVE MALFUNCTIONED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09612QX 10042 GEE965230 PDX - FUEL LEAK NOTED ON NR 1 ENGINE. MAINTENANCE REPLACED THE VARIABLE SLAVE ACTUATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E00063EN 20050815000402005081500040SO 2005 8 15 RAIA00508013 120050809A3242 CONNECTOR EMB 145 EMB145LR 3260212SO MLG BRAKE UNSECURE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03834HK 145269 FLT - 7997 - IAD - BRAKE DEGRADE WARNING INDICATION. MAINTENANCE RE-SECURED LEFT INBD BRAKE TRANSDUCER CANNON PLUG AND OPS CK OK. 2L72 4T RTT00011AT 20050815000432005081500043NM 2005 8 15 SWAA052353 120050808A53116546554 FRAME BOEING737 7373Q8 1384670NM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29317WN 24068 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 847, RBL 21. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050815000462005081500046NM 2005 8 15 SWAA052356 120050808A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29402WN 29814 EEPLS TRACK LOOSE AT ROW 1 ABC. SECURED EEPLS PER MM. 2L72 4F RTA16WE 20050815000472005081500047NM 2005 8 15 SWAA052357 120050808A3350D71701100 BATTERY PACK BOEING737 7377H4 1384404NM EMERGENCY LIGHT FAILED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29416WN 32453 CABIN EMERGENCY EXIT LIGHT SYSTEM FAILED TEST. REMOVED AND REPLACED LT & RT FWD BATTERY PACKS PER MM. 2L72 4F RTA16WE 20050815000622005081500062NM 2005 8 15 SWAA052372 120050808A3350311500 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED C2 CHECK, FOUND FWD CABIN BULLNOSE EMERGENCY EXIT LENS WORN. REMOVED AND REPLACED LENS PER MM. 2L72 4F RTA16WE 20050815000662005081500066NE 2005 8 15 VNAA0508002 220050801A72004071T72P01 SENSOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 2 ENG TEMP FAILED A VNAAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 GL05230PS3087 7904 NR 2 ENGINE N1 STARTED FLUCTUATING +/-10% WHILE CLIMBING THROUGH 21,000 FT. THE AIRCRAFT RETURNED TO PHL WHERE MAINTENANCE REMOVED AND REPLACED THE T2C COMPRESSOR INLET TEMPERATURE SENSOR IAW CRJ200 AMM 73-21-09-000(400)-801. ALL GROUND OPERATIONAL CHECKS WERE GOOD. A SATISFACTORY OPERATIONAL CHECK FLIGHT WAS PERFORMED. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050815000682005081500068 2005 8 15 IXXA0500091O 420050810A34231428302001 FIBER OPTIC GYRO DOUG DC8 DC873F 302199FWP ADHI INOPERATIVE A IXXAA UNSCHED LANDING O OTHER CLCLIMB 1 SW11604BX8499521 46046 DURING CLIMB-OUT FROM KTOL PILOTS HSI/ADHI WAS INOP, INFORMATION WAS LOST. AFTER CREW RESET CIRCUIT BREAKERS ADHI RETURNED THEN WENT BLANK. CREW RETURNED AIRCRAFT TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 FOG. PERFORMED A SHAKEDOWN OF WIRES BEHIND THE NR 1 EADI NR 1 FOG. ALSO, REPLACED NR 1 INSTRUMENT AMP. THE OPERATIONAL CHECK WAS GOOD PER ALL APPLICABLE MANUALS AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20050815000692005081500069EA 2005 8 15 VNAA0508005 120050802A3250 STEERING SYS CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE NLG INTERMITTENT A VNAAO OTHER O OTHER LDLANDING 1 GL05720PS 10178 THE CREW REPORTED THE NOSE WHEEL STEERING INOPERATIVE ON LANDING. MAINTENANCE COMPLIED WITH STEERING RESET PROCEDURES IAW BOMBARDIER CRJ700 SERVICE LETTER SL-32-019. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050815000752005081500075EA 2005 8 15 VNAA0508007 120050804A7603BLC3BC09SL5C4 PIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE THRUST LEVER FAILED A VNAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL05259PS 7945 DURING CLIMBOUT THE CREW REPORTED THAT THE LT ENGINE THRUST LEVER WOULD NOT RETARD BELOW 93 PERCENT. THE AIRCRAFT DIVERTED TO DAY, FOLLOWED THE QRH, AND LANDED SAFELY. MAINTENANCE FOUND THE UPPER CORE COWL SUPPORT STRUT UNSECURED AND INTERFERING WITH THROTTLE MOVEMENT. THE STRUT STOWAGE PIN LOCKING MECHANISM WAS FOUND INOPERATIVE. THE SUPPORT STRUT WAS STOWED IAW CRJ200 AMM 71-12-01-410-802 AND THE PIN WAS TEMPORARILY SECURED. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050815000802005081500080NM 2005 8 15 SWAA052376 120050810A53116520723 FRAME BOEING737 7373Q8 1384670NM FWD CARGO CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29317WN 24068 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 492, STR 24R. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20050815000852005081500085NM 2005 8 15 SWAA052381 120050810A53116520723 FRAME BOEING737 7373H4 1384600NM FWD CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29612SW 27930 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 492.4, RBL 28. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050815001012005081500101NM 2005 8 15 05FDEA02428 120050811A5330 SKIN BOEING727 727227 1384078NM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 PREVIOUS REPAIR AT STA 251 TO 267 STR 17L TO 18L IAW SRM 53-30-3 IS A MAJOR REPAIR. 2L73 4F A3WE 20050815001032005081500103NM 2005 8 15 05FDEA02436 120050812A5320 INTERCOSTAL DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 CABIN, AT STA 1986 FRAME TO LONGERON 27L INTERSECTION, INTERCOSTAL FOUND CORRODED. WEB REMOVED, NEW WEB FABRICATED. INSTALLED AS PER SRM 51-31-01. 2L73 4F RTA22WE 20050815001042005081500104EU 2005 8 15 05FDEA02418 120050811A5753 SKIN AIRBUS300 A300F4605R 3930327EU FLAP DENTED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25671FE 778 LT I/B T/E FLAP, LWR SURFACE SKIN DENTED/GOUGED BEHIND NR 2 LT FLAP JACK SCREW. MEASURED DEPTH OF DENT AT .162 OUT OF LIMITS IAW SRM 57-50-00 FIG 101. INSTALLED REPAIR IAW SRM 57-52-12. REVIEW OF REPAIR REVEALS IT AS UNSAT DUE TO UNAPPLICABLE SRM SCHEME. SEE NR N00768 FOR REWORK. REPAIR AFFECTED ON NR N00759 FOUND UNSAT. SRM REQUIRES AREA BE BOUNDED BY RIBS AND STRINGERS. IT IS NOT. REPAIR REFERENCE IS N/A. COMPLIED WITH EA 6-5750- 82120 WING INBD FLAP LOWER SKIN REPAIR ON S00013. COMPLY WITH EA 6-5750-82120 WING-INBD FLAP-LOWER SKIN REPAIR. COMPLIED WITH EA 6-5750-82120 WING-FLAP-LOWER SKIN REPAIR. 2L72 4F RTA35EU 20050815001052005081500105NM 2005 8 15 05FDEA02423 120050811A7711 TRANSMITTER BOEING727 727225 1384077NM NR 2 EPR MALFUNCTIONED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25466FE 21292 ON TAKEOFF ROLL, NR 2 EPR WOULD NOT ADVANCE PAST 1.4. ALL OTHER ENG INDICATIONS WERE NORMAL. REMOVED AND REPLACED NR 2 ENGINE EPR TRANSMITTER IAW AMM 77-11-011-4. NO HELP. RAN NR 2 ENG TO MAX PWR AND EPR INDICATION WOULD GO TO 1.6 EPR AND DROP TO 1.4 EPR WITH PWR ADVANCED. CONNECTED NR 3 EPR WIRING TO NR 2 EPR XMITTER. ENG CKS GOOD. WITH NR 3 ENG CONNECTED TO NR 2 WIRING GOT NO EPR INDICATION. WIRING IS SUSPECTED PROBLEM BETWEEN NR 2 EPR XMITTER AND NR 2 EPR INDICATOR. 2L73 4F A3WE 20050815001062005081500106NM 2005 8 15 05FDEA02426 120050811A5315 FLOORBEAM BOEING727 727227 1384078NM CABIN DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 FLOORBEAM WEB DAMAGED AT BS 328, LBL 31, WL 207. REPAIRED DAMAGED FLOOR BEAM WEB PER SRM 51-10-1, 53-10-1, 51-40-2 2L73 4F A3WE 20050815001082005081500108NM 2005 8 15 05FDEA02431 120050811A5315 FLOORBEAM BOEING727 727227 1384078NM MAIN CARGO DECK CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 PREVIOUS REPAIR AT STA 1070 BL 0 TO RBL 65 ON FLOORBEAM IS IAW SRM 53-10-8 AND IS A MAJOR REPAIR. 2L73 4F A3WE 20050815001312005081500131NM 2005 8 15 UPS05445173 120050723A5313 STRINGER BOEING747 747121 1384871NM M/D CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 BS 1740-1760 S2R STRINGER END FOUND CRACK, CRACK LENGTH 2". M/DECK BS 1740-1760 STR 2R STRINGER END REPAIRED AS PER HX RS R53-61-35355 AND UPS EO.B747-5310-22662-A. 2L74 4F A20WE 20050815001332005081500133NM 2005 8 15 UPS05445175 120050722A531165B0173121 FRAME BOEING747 747121 1384871NM M/D CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 BS 760 LT STR-14 FRAME FOUND CRACKED, CRACK LENGTH 3/4". FRAME REPAIRED AS PER HX RS R-53-22-35348 AND UPS EO. B747-5310-22632-A. 2L74 4F A20WE 20050815001342005081500134NM 2005 8 15 UPS05445176 120050723A5230 SKIN BOEING747 747121 1384871NM CARGO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 BULK CARGO DOOR CUTOUT FX SKIN EXTERNAL REPAIR PATCH AT BS 2034 STR 35R-37R REQUEST REMOVAL FOR ASSESSMENT PER BOEING MESSAGE 1-109528471-2. BULK CARGO DOOR CUTOUT AFT AREA BS 2034 BTN STR 34/35R TO STR 37/38R AREA REPAIRED AS PER HX RS R-53-61-35359. REF NRC 6801 FOR WORKING DETAIL AND C/OUT CONTINUE INSPECTION PER HX RS R-53-61-35359. 2L74 4F A20WE 20050815001372005081500137NM 2005 8 15 UPS05445179 120050726A531565B1795119 FLOORBEAM BOEING747 747121 1384871NM M/D CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 BS 1918 LBL 100 FLOOR SUPPORT CORROSION. CORROSION BLEND OUT 0.103" BY 1" BY 2". FLOOR SUPPORT REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050815001412005081500141WP 2005 8 15 UPS05845148 120050724A534736575041 SEAT TRACK DOUG DC8 DC873F 302199FWP COCKPIT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 FE'S AFT SEAT TRACK STOP HOLES WORN AND HEAVY CORROSION AROUND COUNTER SUNK ATTACH SCREWS. REMOVED AND REPLACED FE'S AFT SEAT TRACK IAW DC-8 SRM 51-1-21, 51-3-2, AND 51-3-0. 2L74 4F RT4A25 20050815001622005081500162EA 2005 8 15 COMA0560420 120050801A3230601R751605 BYPASS VALVE CNDAIRCL600 CL6002B19 1900309EA MLG MALFUNCTIONED A COMAO OTHER J WARNING INDICATION CLCLIMB 1 SO01416CA12685 7450 FLIGHT 4981 - GEAR DISAGREE WARNING. REPLACED THE MLG RUNAROUND AND BYPASS VALVE. 2L72 4F RTA21EA 20050815001772005081500177NM 2005 8 15 SWAA052403 120050811A53116517684 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29612SW 27930 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303.9, LBL 58, WL 216. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20050815001782005081500178 2005 8 15 SWAA052404 420050811A256565659723 FITTING BOEING737 7373H4 1384600NM GIRT BAR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29612SW 27930 DURING SCHEDULED D CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD AND AFT FLOOR FITTINGS CORRODED. REMOVED AND REPLACED FLOOR FITTINGS PER SRM. 2L72 4F RTA16WE 20050815001852005081500185NM 2005 8 15 SWAA052411 120050811A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29612SW 27930 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 947, STR 25R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050815001932005081500193WP 2005 8 15 IXXA05SMN145S 120050630A5330 GATE DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE FS 55.000 L-29L IMPROPER B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, EXTERNAL FUSELAGE. FREON SYSTEM EXHAUST GATE NON STANDARD REPAIR FS 55.000 L-29L. PERFORMED MAJOR REPAIR IAW SRM, EO SEMAN NR 2005946 DATE 06-21-05. REMOVED EXISTING REPAIR DOUBLER IAW SRM. FABRICATED REPAIR DOUBLER (ALCLAD 2024 T3 0.071), FILLER (ALCLAD 2024 T3 0.063) IAW SRM SHEET. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM. INSTALLED REPAIR PARTS AND TORQUED IAW SRM. 2L74 4F4 FRT4A25 E2GL 20050816000042005081600004EA 2005 8 16 SWIA200515402 120050809A5230 DOOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY OUT OF ADJUST A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07923SW 7664 MCD WON'T OPEN. CHECKED RIGGING AND ADJUSTED IAW AMM 52-11-02. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050816000052005081600005EA 2005 8 16 SWIA200515403 120050809A2750860D10018 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07923SW7579 7579 7664 FLAP 1/2 SPEED MESSAGE AND FLAP FAIL. REPLACED FECU IAW AMM TASK 27-51-05. OPERATIONAL CHECK GOOD. FLAPS HALFSPEED. 2L72 4F RTA21EA 20050816000062005081600006SO 2005 8 16 SWIA200515404 120050804A3397 WIRE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07567SW 120342 "EXIT" LIGHT AT ROW 9BC INOP. REPAIRED BROKEN WIRE. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050816000072005081600007SO 2005 8 16 SWIA200515405 120050809A3350 RECEPTACLE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT LOOSE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07218SW 120287 FA REPORTS OVERHEAD EMERGENCY LIGHT BY ROW 9 EXIT ROW INOP. RESECURED TERMINAL AT LIGHT RECEPTICAL. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050816000122005081600012SO 2005 8 16 SWIA200515410 120050805A2611 SMOKE WARNING EMB 120 EMB120ER 3260203SO COCKPIT FALSE ACTIVATIONA SWIAO OTHER N FALSE WARNING CRCRUISE 1 NM07584SW 120352 "SMOKE" LIGHT ON THE MAP ILLUMINATED DURING FLIGHT AS WELL AS THE SMOKE LIGHT AND ALARM IN THE REAR OF THE CABIN. ALL LIGHTS AND ALARMS CEASED AFTER ABOUT 4 MINUTES. FLIGHT ATTENDANT REPORTED NO ODOR OF SMOKE OR FIRE INDICATION IN THE LAV OR CABIN AREA. NO SMOKE DETECTED IN THE COCKPIT. OPERATIONAL CHECK LAV SMOKE DETECTOR WITH NO DEFECTS. 2L72 4T RTA31SO 20050816000202005081600020WP 2005 8 16 AALA20050511 120050802A4920 APU DOUG DC9 DC983 3022083WP ODOR A AALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW21976TW 53626 DFW - DURING TAXI WHEN APU WAS TURNED ON, CAUSED SMOKE IN CABIN AND COCKPIT. AN EMERGENCY EVACUATION OCCURRED. TAIL CONE SLIDE DEPLOYED. REPLACED SLIDE AND TAIL CONE. REPLACED APU DUE TO SKYDROL INGESTION CAUSING SMOKE AND ODOR IN CABIN AND COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050816000232005081600023NE 2005 8 16 AALA20050512 220050807A7313 NOZZLE BOEING757 757223 1384957NM RROYCERB211 RB211535E4 54555NE ZONE 600 INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21687AA 25695 31053 BWI - INFLIGHT RIGHT HAND ENGINE SURGE AT TAKEOFF. ENGINE PRESSURE RATIO N1 N2 AND N3 FLUCTUATION DURING TAKEOFF ROLL AND CLIMB. REPLACED RIGHT HAND ENGINE LEFT HAND PF RAKE NOZZLES AT 5 O`CLOCK POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA2NM E12EU 20050816000282005081600028WP 2005 8 16 IXXA05RNG037S 120050719A5730 SKIN PANEL DOUG DC8 DC862F 3021972WP RT WING CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW1171CX 670243317 45961 DURING INSPECTION CHECK CORROSION WAS FOUND ON PANEL AT WING OUTER INBOARD EXTENDED LEADING EDGE PLATING STA XFS 710.0, RT. CORROSION ON RT WING LEADING EDGE UPPER SKIN WAS REMOVED AND REPAIR "DOUBLER" WAS INSTALLED IAW EWO ATI 57-029 AND EO ATI-071505. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR. 2L74 4F 4A25 20050816000382005081600038NM 2005 8 16 DHL2005747503 120050712A5753 SKIN BOEING727 727224 1384076NM TE FLAP DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01747DH 22253 LT WING INBD MID-FLAP T/E APPROX 61" FROM INBD END HAVE DELAMINATION. REPAIRED LT INBD MID FLAP T/E AT APPROX 61" FROM INBD END IAW B-727 SRM 51-40-20 PAR 20-22 BY INSTALLING DOUBLER REPAIR. 2L73 4F A3WE 20050816000392005081600039NM 2005 8 16 05FDEA02424 120050811A56105893543130 WINDOW BOEING727 7272S2F 1384O81NM R1 DELAMINATED A FDEAA UNSCHED LANDING O OTHER CRCRUISE 1 SO25204FE 22926 UPPER PORTION OF WINDOW R1 IS DELAMINATING, AND A BUBBLING FLUID IS PRESENT INSIDE THE DELAM, R1 OUTER PANE CRACKED. REMOVED AND REPLACED RT NR 1 WINDSHIELD PER MM 56-11-011-4. REMOVED AND REPLACED WINDOW HEAT CONTROLLER PER MM 30-41-02, PRECAUTIONARY R/I. PREMATURE REMOVAL/INSTALLATION OFF MFG 5-89354-3130, POS RT SRL 01346R5016, TAG 61A952 ON MFG 5-89354-3136 SRL 03077R9056, TAG 794227 R/I. PREMATURE REMOVAL/INSTALLATION OFF MFG 231-3, POS 3 SRL 5511 TAG A62037 ON MFG 231-3 SRL 3923, TAG 5A6658. INSTALLED TRIM PIECES INSTALLATION COMPLETE. WINDSCREEN HEAT OPS NORMAL PER MM 30-41-02. 2L73 4F A3WE 20050816000412005081600041WP 2005 8 16 05FDEA02448 120050812A5714 FLANGE DOUG MD10 MD1010F 3022112WP GE CF6 CF66D 30020GL ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25564FE 46984 CTR WING LWR BARREL AT STA 1216 REWORK TO STR 47 BASE FLANGE TO REMOVE CORROSION MATERIAL PLUS 50 PERCENT. REPAIRED LONGERON IAW SRM 53-00-01 FIG 9 VOL I. 2L73 4F4 FRTA22WE E23EA 20050816000432005081600043EU 2005 8 16 05FDEA02450 120050812A5311A5381231220001 FRAME AIRBUS300 A300B4622R 3930312EU CABIN CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25718FD 365 MAIN CABIN AT FRAME 46 LT CRACKED APPROX 4 INCHES. 2L72 4F RTA35EU 20050816000472005081600047SO 2005 8 16 C2XA05BT046 120050719A335078241 INVERTER EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT FAULTY A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2728529 145512 EWR---CO2352, CREW REPORTED, BULKHEAD EMERGENCY EXIT SIGN DOES NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED INVERTER BY GALLEY DOOR. OPS CHECK GOOD IAW EMB145 MM 33-50-11. 2L72 4F RTT00011AT 20050816000502005081600050NM 2005 8 16 05FDEA02452 120050812A5315 FLOORBEAM BOEING727 727200 138407ENM CABIN UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 EVALUATE TO DETERMINE IF REPAIR IS MAJOR OR MINOR AND IF REPAIR IS IN ACCORDANCE WITH FAA APPROVED DATA, (FLOORBEAM REPAIR AT BS 380, RBL 52-63). EMOVED EXISTING REPAIR B/S 380 RBL 52-63 FABRICATED & INSTALLED NEW REPAIR IAW FED EX SR DRW 52-034E THIS IS A MAJOR REPAIR 2L73 4F RTA3WE 20050816000622005081600062NM 2005 8 16 05FDEA02461 120050813A5720652165829 CHANNEL BOEING727 727200 138407ENM RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 RIGHT WING LOWER T/E PANEL SUPPORT BRACKET CRACKED AT WS 519. REMOVED AND REPLACED CHANNEL IAW SRM 51-30-2. 2L73 4F RTA3WE 20050816000652005081600065NM 2005 8 16 05FDEA02464 120050814A5753 VANE DOUG MD11 MD11 3023602NM ZONE 500 DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LT WING - DELAMINATION FOUND AT LOWER SURFACE, INBOARD FLAP VANE 17 INCHES FROM INBOARD FLAP, CENTER TRACK. COMPLIED WITH FEDEX EA 1-5750-89965 2L73 4F RTA22WE 20050816000962005081600096NM 2005 8 16 SWAA052422 120050813A27506573271 TORQUE TUBE BOEING737 7373H4 1384600NM RT WING TE FLAP WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 DURING SCHEDULED SERVICE CHECK, FOUND NR 5 T/E FLAP TRANSMISSION TORQUE TUBES WORN. REMOVED AND REPLACED TORQUE TUBES PER MM. 2L72 4F RTA16WE 20050816000972005081600097 2005 8 16 SWAA052423 420050814A256565C16820 HOOK BOEING737 7373H4 1384600NM R2 DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29339SW 24090 R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOKS OUT OF POSITION. REPOSITIONED HOOKS PER MM. 2L72 4F RTA16WE 20050816000992005081600099NM 2005 8 16 SWAA052447 120050814A5315BAC1509 FLOORBEAM BOEING737 7377H4 1384404NM CABIN FLOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29781WN 30601 DURING SCHEDULED 5Y CHECK, FOUND LONGITUDINAL FLOORBEAMS CORRODED AT BS 727D, LBL 3 & BS 772 TO BS 774, LBL 17. REPAIRED FLOORBEAMS PER SWA EA. 2L72 4F RTA16WE 20050816001582005081600158EA 2005 8 16 VNAA0508009 120050810A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT WING LIGHTNING STRIKEA VNAAO OTHER O OTHER NRNOT REPORTED 1 GL05229PS 7898 AFTER LANDING THE CREW REPORTED POSSIBLE LIGHTNING DAMAGE ON THE LEFT WINGLET TRAILING EDGE. MAINTENANCE COMPLIED WITH EN ROUTE & DETAILED LIGHTNING STRIKE INSPECTIONS IAW CRJ200 AMM 05-51-05-210-801, AMM 05-51-05-220-801, AND AMM 05-51-05-220-803. THE LT WINGLET WAS REPAIRED IAW BOMBARDIER REO 601R-57-30-001. MINOR DAMAGE TO THE NR 5 OUTBOARD TRAILING EDGE FLAP FAIRING WAS REPAIRED IAW CRJ200 SRM 57-50-00. NO OTHER DEFECTS WERE FOUND. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050816001602005081600160NM 2005 8 16 0501265507 120050813A2530 OVEN BOEING757 757251 1384970NM GALLEY SMOKE A NWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL01507US 23196 SMOKE COMING FROM 1ST CLASS GALLEY OVEN, SUBSIDED WHEN OVEN WAS TURNED OFF. THERE WAS NO FIRE AND THE SMOKE WAS NOT FOOD RELATED PER FLIGHT ATTENDANT. OVEN WAS REMOVED AND REPLACED, AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA2NM 20050816001642005081600164SO 2005 8 16 LR7A05104 120050813A5330 SKIN LKHEED382 382G 526414USO FS 900 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 647 4763 DURING SCHEDULED B2 INSPECTION PER JOB CARD HB5301 FOUND FS 900 FUSELAGE SKIN CRACKED AT RBL 59, WL 215. REPAIRED IAW SRM SMP 583 51-140-12. 2H74 4T A1SO 20050816001662005081600166SO 2005 8 16 LR7A05105 120050813A5330 SKIN LKHEED382 382G 526414USO FS 105 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 647 4763 DURING SCHEDULED B2 INSPECTION PER JOB CARD HB5303 FOUND FS 105 FUSELAGE SKIN CRACKED AT CO-PILOTS DV WINDOW APERTURE, RBL 60, WL 231. REPAIRED IAW LAC MEA 382-53-05-065. 2H74 4T A1SO 20050816001682005081600168SO 2005 8 16 LR7A05106 120050813A5542 FAIRING LKHEED382 382G 526414USO FS 1128 LIGHTNING STRIKEA LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 647 4763 DURING SCHEDULED B2 INSPECTION PER JOB CARD HB2703 FOUND EVIDENCE OF LIGHTNING STRIKE AT RUDDER FAIRING TIP, FS 1128, VSS 277. REPAIRED IAW LAC MEA 382-53-05-062. 2H74 4T A1SO 20050816001712005081600171EU 2005 8 16 XN0A1256 120050815A5330 ACCESS PANEL AIRBUS300 A300B4203 3930306EU LEFT INFLT SEPARATIONA XN0AA UNSCHED LANDING D INFLIGHT SEPARATION CLCLIMB 1 GL23473AS 203 LEFT ACCESS PANEL (AC) DEPARTED AIRCRAFT ON T/O. ATC REPORTED SEEING PANEL FULL, TURNED BACK. PERFORMED L INSPECTION OF WHEEL WELL AREA, LOWER SURFACE WINES, FUSELAGE EMPENNAGE, NO DAMAGE NOTED. INSPECTED LT & RT MLG, NO DAMAGE NOTED. INSTALLED SERVICEABLE PANEL IAW A300 MM 53-15-00. NO DEFECT NOTED. 2L72 4F RTA35EU 20050816001732005081600173EU 2005 8 16 MALA050636 120050807A5311 FRAME SAAB SF340 340B 7860101EU CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15403XJ 340B403 IRREGULAR ROUTING DUE TO AIRFRAME CORROSSION NOTED DURING ROUTINE MAINTENANCE. NO FURTHER INFORMATION AT THIS TIME. 2L72 4T RTA52EU 20050816001812005081600181NM 2005 8 16 SB05091 120050811A2120 ODOR BOEING737 7373B7 1384580NM CABIN DETECTED A USAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA19517AU 23703 DCA FLT1285 DUE TO AN INOPERATIVE APU, A GROUND AIRSTART WAS ACCOMPLISHED PRIOR TO DEPARTURE IN SYR. AN OBNOXIOUS ODOR BECAME PRESENT IN THE COCKPIT AND CABIN SHORTLY THEREAFTER. AFTER DEPARTURE, THE CAPTAIN SENT AN ACAR'S MESSAGE STATING THE ODOR CLEARED IN THE COCKPIT BUT COMPLAINTS OF THE ODOR IN THE CABIN CONTINUED. (CAPTAIN THOUGHT THE ODOR WOULD CLEAR WHILE AIRBORNE.) FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT IN DCA. MAINTENANCE DETERMINED THAT AN AIRSTART CART INSTEAD OF AN AIR CONDITIONING CART WAS USED TO COOL THE AIRCRAFT WHILE AT SYR. THIS IS WHAT MAINTENANCE DETERMINED/CAUSED THE ODOR. 2L72 4F RTA16WE 20050816001832005081600183NM 2005 8 16 SB05092 120050811A2120 ODOR BOEING737 737301 1384611NM CABIN DETECTED A USAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA19589US 23934 CREW REPORTED A SLIGHT ELECTRICAL/BURNING ODOR IN THE AFT GALLEY. CREW TURNED GALLEY POWER OFF AND ODOR DISSIPATED. MAINTENANCE TURNED GALLEY POWER ON AND INVESTIGATED PROBLEM. COULD NOT VERIFY OR FIND ANY SOURCE OF THE ODOR. AIRCRAFT OK FOR SERVICE. 2L72 4F RTA16WE 20050816002012005081600201 2005 8 16 RAIA00508005 420050805A34257003360948 AHRS JETAIRJETSTMJETSTM4101 1500501EU COCKPIT INOPERATIVE A RAIAA UNSCHED LANDING O OTHER CLCLIMB 1 CE03562HK20585 41078 FLT 3663 - RIC, AHRS NR 1 ROLLED OVER IN FLIGHT. MAINTENANCE REMOVED AND REPLACED NR 1 AHRS. 2L72 4T RTA41NM 20050816002022005081600202NM 2005 8 16 DHL05780001 120050813A3150 WARNING HORN BOEING727 727223 1384074NM TE FLAPS ACTIVATED A DHLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01780DH 22006 AT BEGINING OF T/O ROLL TAKE OFF WARNING HORN SOUNDED AND COULD NOT BE SILENCED. RESET FLAPS AND TRIM, NO HELP. T/O WAS REJECTED AT AERO FORWARD AIRSPEED. T/S FOUND 31 FLAP POSITION SWITCH LOOSE, TIGHTENED, SECURED SWITCH AND OPS CKS GD. NO HIGH ENERGY INSP REQ PER RTO EVAL FORM 080, NO DEFECTS NOTED. 2L73 4F A3WE 20050816002042005081600204NM 2005 8 16 DHLA05740015 120050810A3260 SWITCH BOEING727 7272Q9 138448MNM NLG DOOR OUT OF ADJUST A DHLAO OTHER N FALSE WARNING DEDESCENT 1 SO01740DH NOSE GEAR DOOR LIGHT ILLUMINATED DURING DECENT. ABNORMAL PROCEDURE WAS ACCOMPLISHED LIGHT WENT OUT WITH GEAR LEVER IN UP POSITION. ADJUSTED NOSEGEAR DOOR WARNING SWITCH IAW M/M 32-62-0 OPS CK NORMAL 2L73 4F RTA3WE 20050816002082005081600208NM 2005 8 16 MZZA0500001 120050318A2560 BATTERY BOEING737 737823 13844BZNM FLASHLIGHT DISCHARGED A MZZAL ABORTED APPROACH O OTHER NRNOT REPORTED 1 WP1335236 28801 TWO AFT GALLEY FLASHLIGHTS INOPERATIVE. FLASHLIGHT BATTERIES REPLACED IAW MM 25-65-00. 2L72 4F RTA16WE 20050816002102005081600210NM 2005 8 16 MZZA0500003 120050721A36101324M12P10 ACTUATOR BOEING737 737823 13844BZNM NR 1 ENGINE LEAKING A MZZAB EMER. DESCENT O OTHER LDLANDING 1 WP132724620877 28956 A FUEL ODOR WAS NOTICED THOUGHOUT THE CABIN DURING LANDING AT GUM. THE FIRE TRUCKS WERE REQUESTED. MX FOUND NR 1 ENGINE VSV ACTUATOR LEAKING AT ENGINE VENT. THE NR 1 ENGINE RT VSV ACTUATOR WAS REMOVED AND REPLACED IAW MM. NR 1 ENGINE WAS RUN, OPS AND LEAKED CHECKED WERE GOOD. 2L72 4F RTA16WE 20050816002132005081600213SW 2005 8 16 ALGA105220 120050807A6220407010101101 YOKE BELL 407 407 1182206SW MAIN ROTOR HEAD CRACKED B ALGAK NONE O OTHER ININSP/MAINT 1 SW03647AL3676 LK7 53357 M/R YOKE CRACKED (RED) ARM / REPLACED WITH SERVICEABLE YOKE 1G71 3U O H2SW 20050816002212005081600221EU 2005 8 16 USAA050888 120050718A53151160826 FLOORBEAM AIRBUS320 A320214 3930316EU FS 66-68 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19109UW19030 1065 FOUND FLOORBEAM CORRODED 1 INCH BY 1.5 INCH, 1 INCH BY 3 INCH, FRAME 66-68. CORROSION LEVEL 1. DEFECTIVE PART REPLACED WITH IDENTICAL PART IAW JA-260-53500. (M) 2L72 4F RTA28NM 20050816002232005081600223WP 2005 8 16 IXXA05SMN116S 120050627A5753 FLAP DOUG DC8 DC871F 302199DWP XF 333.000 IMPROPER A IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, LT OB FLAP L/E REPAIR IMPROPER, XF 333.000 (UPPER PART) PERFORMED MAJOR REPAIR IAW NR 05259 DATE 06-24-05, DWG NR ED 3988, EO NR 2005855 DATE 06-24-05. REMOVED FASTENERS IAW SRM. REMOVED DAMAGED PLATING SEGMENT IAW DWG ED 3988. PERFORMED NDT INSPECTION IAW SPM. NO CRACK, CORROSION FOUND. FABRICATED NEW PLATING SEGMENT (ALCLAD 2024 T3 0.071”) + INTERNAL SPLICE (ALCLAD 2024 T3 0.080”) + (02 EA) EXTERNAL DOUBLERS (ALCLAD 2024 T3 0.071) IAW DWG ED 3988, SRM. CLEANED, TREATED AND PRIMED REPAIR PARTS (INTERNAL PART) + AREA IAW SRM. APPLIED SEALANT TO FAYING SURFACES IAW SRM. INSTALLED REPAIR PARTS IAW DWG ED 3988, SRM. TORQUED IAW SRM. 2L74 4F RT4A25 20050817000082005081700008NM 2005 8 17 QXEA200501169 120050810A5240 LINKAGE BOMBDRDHC8 DHC8402 1390042NM GALLEY DOOR FROZEN A QXEAO OTHER O OTHER TXTAXI/GRND HDL 1 NM09415QX 4081 PDX FLIGHT NR 2361 - GALLEY SERVICE DOOR COULD NOT BE OPENED. MAINTENANCE FOUND VENT DOOR LINKAGE FROZEN. CLEANED AND LUBED DOOR LINKAGE. OPS CHECK SHOWED DOOR OPERATION NORMAL. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050817000092005081700009NM 2005 8 17 QXEA200501170 120050813A5240 DOOR BOMBDRDHC8 DHC8402 1390042NM GALLEY LACK OF LUBE A QXEAO OTHER O OTHER TXTAXI/GRND HDL 1 NM09415QX 4081 PDX FLIGHT NR 2360: GALLEY DOOR WAS UNABLE TO BE OPENED FROM THE INSIDE. MAINTENANCE CLEANED AND LUBED AFT GALLEY SERVICE DOOR AS REQUIRED. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050817000122005081700012WP 2005 8 17 MWEA050075 120050812A5320 SUPPORT DOUG DC9 DC981 3022081WP NLG WW CHAFED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 NOSE WHEEL WELL OVER CENTER LINK BOLT COTTER PIN IS CHAFING, LEFT BUNGEE SUPPORT. FABRICATED AND INSTALLED WEB REPAIR DOUBLER. 2L72 4F A6WE 20050817000142005081700014WP 2005 8 17 MWEA050079 120050815A5347593056677 SEAT TRACK DOUG DC9 DC981 3022081WP CABIN CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 LEFT SIDE SEAT TRACK INBOARD SIDE BETWEEN STATION 1126 AND 1260 REQUIRES SPLICING DUE TO OUT OF LIMITS MATERIAL REMAINING AFTER CORROSION REMOVAL. FABRICATED AND INSTALLED SEAT TRACK. 2L72 4F A6WE 20050817000152005081700015WP 2005 8 17 MWEA050080 120050815A534049125671 ATTACH ANGLE DOUG DC9 DC981 3022081WP SEAT TRACK CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 MAIN CABIN, LEFT INBOARD SEAT TRACK ATTACH ANGLE AT STATION 1174 BROKEN AND CORRODED. REMOVED AND REPLACED CLIP. 2L72 4F A6WE 20050427000132005042700013WP 2005 4 27 WX0500026 120050301A3350 LAMP DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A WX0AK NONE O OTHER ININSP/MAINT 1 WP19866GA 49910 LAS - MAINTENANCE REPORTED EMERGENCY OVERHEAD LIGHT INOPERATIVE AT ROW 14. MAINTENANCE RELAMPED THE EMERGENCY OVERHEAD LIGHT, SYSTEM OPERATIONALLY CHECKS GOOD IAW AMM 33-53-01. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050427000312005042700031CE 2005 4 27 DJFA2005066 120050315A3260 BULB BEECH MU300 400A 1155402CE NLG INDICATOR INOPERATIVE E DJFAL ABORTED APPROACH P NO WARNING INDICATION APAPPROACH 1 EA23739TA RK257 CREW REPORTED THAT WHILE ON APPROACH TO KVNY, AFTER LOWERING THE LANDING GEAR, THE NOSE GEAR DID NOT INDICATE GREEN. THE RED GEAR HANDLE LIGHT WAS EXTINGUISHED. THE LANDING GEAR WAS CYCLED AND CREW RECEIVED THE SAME INDICATION. A MASTER LIGHT TEST INDICATED ALL LIGHTS WERE WORKING EXCEPT FOR THE NOSE GEAR. ALL GEAR APPEARED TO BE DOWN AFTER PERFORMING A FLY-BY PAST THE TOWER. AN EMERGENCY WAS DECLARED AND AIRCRAFT MADE AN UNEVENTFUL LANDING. MAINTENANCE REPLACED THE LIGHT BULB IN THE NOSE GEAR CAPSULE. OPERATIONAL CHECK OF THE LIGHT WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4F RTA16SW 20050427000322005042700032EU 2005 4 27 05FDEA00513 120050315A7931 TRANSMITTER AIRBUS310 A310 EU PWA JT9 JT9D* NE OIL PRESSURE MALFUNCTIONED A FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25455FE 331 707703 RTO RPLB RWY 25 AT 95 KTS WITH A OIL PRESSURE HIGH INDICATION ON LOWER FORWARD INSTRUMENT PANEL. LIGHT OUT AFTER SEVERAL SECONDS. DRAINED ENG NR 1 OIL TANK PERFORMED SNIFF CHECK, NO FUEL CONTAMINATION NOTED. REMOVED AND REPLACED OIL PRESS TRANSMITTER PER AMM 79-33-11-4. RAN NR 1 ENGINE PER A310 JRH AT TAKEOFF POWER, EPR = 1.27 AT 24 DEG C, ALL PARAMETERS NORMAL; NO HIGH OIL PRESSURE WARNING LIGHTS, ILLUMINATED. A/C OK FOR SERVICE. AMT'S 354575, 366556, 472875 AND 559576. PREMATURE REMOVAL/INSTALLATION OFF MFG VT0304S POS P1 SRL 480 TAG A41053 ON MFG VT0304S SRL 671 TAG 787111. 2L72 4F4 FRTA35EU E20EA 20050427000492005042700049NM 2005 4 27 DHL2005781555 120050216A5531 FRAME BOEING727 727227 1384078NM VERTICAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A C-CHECK, VERT STAB FIN STA 133 STR 9 LT IS CRACKED AT FRAME ATTACH BOLT. REMOVED FASTENERS FOR ACCESS, CUT-OUT DAMAGED DIM 4.5 X 3 INCHES STIFFENER AND REMOVED FILLER IAW B727 SRM 55-30-4 FIG 1. FABRICATED STIFFENER REPAIR. INSTALLED STIFFENER REPAIR AT VERT STAB FIN STA 133 STRINGER 9L IAW B727 SRM 55-30-4 FIG 1. 2L73 4F A3WE 20050427000572005042700057NM 2005 4 27 DHL2005781565 120050216A5542 SKIN BOEING727 727227 1384078NM RUDDER DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A C-CHECK, ACCOMPLISH IDENTIFICATION OF EXISTING REPAIR ON UPPER RUDDER RT SKIN AT STA 156 PER ASTAR J/C FCD500001-010-B. DISCONNECTED UPPER RUDDER ACTUATOR ROD END THROUGH BOLT FOR S/M ACCESS IAW B727 MM 27-20-14. REMOVED PREVIOUS REPAIR NOT COMPLIANT TO SRM 55-20-3,FIG 1. DIM PROVIDING CUT OUT 2.5 BY 4 INCHES, FABRICATED DOUBLER REPAIR MAT, USED 2024 T3 .032 PO NR 90001777 DIM. 12 BY 10 INCHES IAW B727 SRM 55-20-3 FIG 1. ALODINE AND PRIMED IAW B727 SRM 51-10-2. INSTALLED DOUBLER REPAIR IAW B727 SRM 55-20-3 FIG 1. RECONNECTED UPPER RUDDER ACT ROD END BOLT IAW B727 NMM/27-20-141. 2L73 4F A3WE 20050427000592005042700059NM 2005 4 27 0500345647 120050315A21503508806 PUMP BOEING757 757251 1384970NM LT ENGINE LEAKING A NWAAH DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 GL01547US325962395 26494 AFTER TAKEOFF, RECEIVED "L ENG HYD OVHT" AND PUMP WAS SHUT DOWN. LT HYDRAULIC SYSTEM WAS LOSING FLUID. ON APPROACH, LOST HYDRAULIC PRESSURE AND DECLARED AN EMERGENCY, LANDING WAS UNEVENTFUL. FOUND LT ENGINE DRIVEN HYDRAULIC PUMP LEAKING. REPLACED LEFT ENGINE HYDRAULIC PUMP. OPERATIONAL CHECK GOOD. 2L72 4F RTA2NM 20050427000762005042700076NM 2005 4 27 DHL2005765001 120050322A33501000677 BATTERY PACK BOEING727 727264 138408MNM EMERGENCY LIGHT INOPERATIVE A DHLAK NONE O OTHER ININSP/MAINT 1 SO01765AT 23014 WHEN PERFORMING STBY POWER AND BATTERY CHECK, OBSERVED THAT EMERGENCY EXIT LIGHT OVER COCKPIT ENTRY DOOR INOP. REMOVED AND REPLACED BATTERY PACK AND CHARGER. OPS CK GOOD MM 33 10 00. 2L73 4F A3WE 20050427000782005042700078CE 2005 4 27 DJFA2005068 120050319A2140 HEATER BEECH MU300 400A 1155402CE CABIN CONTAMINATED E DJFAH DEACTIVATE SYST/CIRCUITS CB F.O.D. SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA23477LX RK377 CREW REPORTED THAT THEY NOTICED A HAZE AND A BURNING SMELL IN THE CABIN. THE CREW BELIEVED THAT SOMETHING MAY HAVE BEEN PLACED INTO A HEATER VENT THAT WAS CAUSING THE SMOKE. THE HEAT WAS THEN TURNED OFF AND THE HAZE HAD DISSIPATED. WHEN THE HEAT WAS TURNED BACK UP THE SMOKE CAME BACK. THE AIRCRAFT CABIN WAS INSPECTED TO ASSURE NOTHING WAS BURNING. THE FLIGHT WAS COMPLETED WITHOUT FURTHER INCIDENT. MAINTENANCE DISCOVERED A MELTED CRAYON AND CANDY IN THE RIGHT SIDE TRAY TABLE HOUSING. THE DEBRIS WAS REMOVED FROM THE TRAY TABLE HOUSING AND THE AIRCRAFT WAS RAN. NO FURTHER DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4F RTA16SW 20050427000912005042700091EU 2005 4 27 AWXA200500351 120050321A3350321452 EPSU AIRBUS320 A320231 3930325EU ZONE 263 FAILED A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28637AW48476 099 LAS - EEL - FLIGHT CREW REPORTED THE EMERGENCY EXIT LIGHTS OVER L-2 AND R-2 DOOR DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED AFT LT EMERGENCY POWER SUPPLY UNIT (13WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050427001122005042700112NM 2005 4 27 72300021 120050201A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 1.25 INCH BY 2 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050427001142005042700114NM 2005 4 27 72300023 120050201A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 1 INCH BY 3 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050427001162005042700116NM 2005 4 27 72300025 120050201A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CRACKED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 APPROX 1 INCH CRACK IN SHEAR TIE RADIUS. 2L73 4F4 FRTA3WE E2EA 20050427001202005042700120NM 2005 4 27 72300018 120050114A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSLEAGE DAMAGED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 LOWER FLANGE OF SHEAR TIE HAS DAMAGED FASTENER HOLES. 2L73 4F4 FRTA3WE E2EA 20050427001242005042700124NM 2005 4 27 05FDEA00631 120050324A2612 LAMP BOEING727 727* NM INDICATOR MALFUNCTIONED A FDEAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO25258FE 20940 LOWER CARGO SMOKE LIGHT ILLUMINATED ON T/O AT 90 KTS, RTO- NO OTHER INDICATION ON CARGO PANEL OR BELL. BOTH FWD AFT COMPARTMENTS CHECK CLEAR. RELAMPED INDICATOR OPS TEST NORMAL IAW MM 26-17-012-2 OK FOR SERVICE. 2L73 4F RTA3WE 20050427001452005042700145NM 2005 4 27 DHL2005745008 120050326A2150 ODOR BOEING727 727224 1384076NM A/C PACK DETECTED A DHLAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO01745DH 20665 DURING DESCENT, ODOR CAN BE SMELLED COMING FROM PACKS. RAN PACKS FOR APPROX 1 HR WHILE OCCUPYING COCKPIT. NO ODORS OR SMOKE DETECTED AT THIS TIME, PACK DISTRIBUTION SYSTEM. OPS CK GOOD IAW BMM CH 21-20-01. 2L73 4F A3WE 20050427001462005042700146NM 2005 4 27 USAA050336 120050302A5340 STRINGER CLIP BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19442US40275 24841 CLT - Q6 - STRINGER CLIP, .5 INCH CRACK, STATION 706, STRINGER 11R. REPLACED TIE CLIP IAW SRM 51-10-02. 2L72 4F4 FRTA16WE E21EU 20050427001472005042700147NM 2005 4 27 USAA050341 120050304A5310 STRINGER CLIP BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19442US40275 24841 CLT - Q6 - STRINGER CLIP, .5 INCH CRACK, STATION 500A, STRINGER 16R. REPLACED WITH FABRICATED CLIP IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050427001482005042700148SO 2005 4 27 20030810 120050322A5512 SKIN EMB 120 EMB120ER 3260203SO STAB CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03293UX 120293 DURING ROUTINE INSPECTION A 1 INCH CRACK WAS FOUND ON RT FUSELAGE TO STABILIZER SKIN AREA AT FS16144.9 BETWEEN RIVETS 15 AND 16. PERFORMED DOUBLER SKIN PATCH REPAIR. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA31SO 20050427001492005042700149SW 2005 4 27 KBM2005F00039 120050313A770012444412 INDICATOR BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL TOT INOPERATIVE E KBMAK NONE O OTHER ININSP/MAINT 1 WP19188TV 2704 TOT GAUGE, INOPERATIVE. REMOVED AND REPLACED. (K) 1G71 3U3 U H2SW E4CE 20050427001572005042700157EA 2005 4 27 QXEA200500432 120050225A5414 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 400 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - LEFT HAND NACELLE LIP SKIN GOUGED BETWEEN 7 AND 8 O'CLOCK POSITION. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01 AND SRM 54-11-05-101-001-A01. 2L72 4F RTA21EA 20050427001592005042700159EA 2005 4 27 QXEA200500435 120050303A5751 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 600 WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - RIGHT HAND AILERON, UPPER LEADING EDGE HAS THREE AREAS OF WEARING FROM TRAILING EDGE SEALS. REPAIRED IAW CRJ700 SRM 57-61-01-101-001-A01 AND SRM 51-12-00-001-001-A01. 2L72 4F RTA21EA 20050427001612005042700161WP 2005 4 27 DHL2005805528 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBD FLANGE (2EA) HOLES MISDRILLED AT STA 1480.000 L-13L L-12L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-05-05, EO NR AST 050205 DATE 02-21-05. CLEANED, TREATED AND PRIMED (AREA) MISDRILLED HOLES IAW SRM 51-1-8B. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD6-4) IAW EO NR AST050205, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050427001632005042700163WP 2005 4 27 DHL2005805537 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT INBD FLANGE "Z" FRAME HOLES (2EA) MISDRILLED AT STA 300.000 L-12 L-13L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-05-05, EO NR AST 050205 DATE 02-21-05. CLEANED, TREATED AND PRIMED AREA MISDRILLED HOLES IAW SRM 51-1-8B. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD6-5) IAW EO NR AST 050205, SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050427001652005042700165WP 2005 4 27 DHL2005805580 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBD FLANGE (2EA) MISDRILLED HOLES, STA 1340.000 L-9L - L-10L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-05-05, EO NR AST 050205 DATED 02-21-05. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA AT STA 1340.000 L-10L IAW SRM 51-1-8B. PERFORMED DETAIL VISUAL INSP. NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD5-5) IAW EO NR AST050205, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050427001672005042700167WP 2005 4 27 DHL2005805535 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 ITEM REF. NR. 028600: MAIN CARGO COMPT FRAME INBD FLANGE HOLES MISDRILLED (2EA) STA 1160.000 L-10L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-05-05 EO NR AST 050205 DATE 02-21-05. CLEANED, TREATED AND PRIMED (AREA) MISDRILLED HOLES IAW SRM 51-1-8B. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD5-4) IAW EO NR AST050205, SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050427001692005042700169WP 2005 4 27 DHL2005805534 120050320A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME HOLES (2EA) MISDRILLED 0.15625, STA 920.000 L-12L L-13L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FORM 8110-3 DATE 02-28-05, EO NR AST050206 DATE 02-24-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. FABRICATED NEW CLIP (AL 7075-T6 0.080) IAW EO NR AST050206. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA AND NEW CLIP IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (NAS 1097AD). INSTALLED NEW CLIP IAW EO NR AST 050206, SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050427001712005042700171WP 2005 4 27 DHL2005805541 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBD FLANGE (1EA) MISDRILLED HOLE, STA 220.000 L-12.5R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-07-05, EO NR AST 050201 DATED 02-17-05. PERFORMED DETAIL VISUAL INSP. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA AT STA 220.000 L-12.5R IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLE WITH RIVET (MS20470AD) IAW EO NR AST-050201, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050427001732005042700173WP 2005 4 27 DHL2005805536 120050305A5310 DOUBLER DOUG DC8 DC873F 302199FWP DOOR FRAME DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 EXTERNAL FUSELAGE RT NR 6 ACCESS DOOR JAMB HAS INTERIM REPAIR ON INTERNAL DOUBLER (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PAGE 1, SRM 53-3-3 FIG 1. REMOVED EXISTING REPAIR DOUBLER (EXT) AND INTERNAL DOUBLER WITH INTERIM REPAIR IAW SRM 51-1-21 PAGE 1. FABRICATED NEW INTERNAL DOUBLER (AL7075-T6 0.063) IAW SRM 53-3-3 FIG 1 ITEM K, SRM 51-9-0 FIG 68A. CLEANED, TREATED AND PRIMED AREA, INTERNAL DOUBLER AND REPAIR DOUBLER (EXISTING) IAW SRM 51-1-8B. INSTALLED INTERNAL DOUBLER (NEW) AND REINSTALLED EXISTING REPAIR DOUBLER (EXT) IAW SRM 51-1-21 PAGE 1, SRM 51-1-20D PAGE 9. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050427001752005042700175WP 2005 4 27 DHL2005805547 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBD FLANGE (2EA) MISDRILLED HOLES, STA 1420.000 L-10R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-07-05, EO NR AST050201 DATED 02-17-05. PERFORMED DETAIL VISUAL INSP. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO NR AST050201, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050427001772005042700177WP 2005 4 27 DHL2005805585 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBD FLANGE (2EA) MISDRILLED HOLE AT STA 440.000 L-12.5R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-07-05 EO NR AST 050201 DATED 02-17-05. PERFORMED DETAIL VISUAL INSP. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA AT STA 440.000 L-12.5R SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLE WITH RIVET (MS20470AD) IAW EO NR AST 050201, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050427001792005042700179WP 2005 4 27 DHL2005805627 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME (2 EA) MISDRILLED HOLES AT STA 600.000 L-12L TO L-13L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-05-05 EO NR AST 050205 DATED 02-21-05. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA AT STA 600.000 L-12L TO L-13L IAW SRM 51-1-8B. PERFORMED DETAIL VISUAL INSP. NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD6-5) IAW EO NR AST 050205 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050427001812005042700181WP 2005 4 27 DHL2005805656 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBD FLANGE (1EA) HOLE MISDRILLED STA 540.000 L-12.5R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-07-05 EO NR AST 050201 DATE 02-17-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLE WITH RIVET (MS20470AD) IAW EO NR AST 050201 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050427002092005042700209WP 2005 4 27 DHL2005805594 120050320A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT "Z" FRAME INBD FLANGE HOLES (2EA) MISDRILLED AT STA 1100.000 L-8R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-04-05 EO NR AST 050213 DATE 03-02-05. PERFORMED DETAILED VISUAL INSPECTION TO AREA. NO CRACK FOUND. FABRICATED DOUBLER ANGLE (AL7075O0.100) IAW EO NR AST 050213, SRM 51-1-4 PAGE 1, SRM 51-1-1 PAGES 1,13,17.(HEAT TREATMENT). CLEANED, TREATED AND PRIMED AREA (MISDRILLED HOLES) AND DOUBLER ANGLE IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (NAS 1097AD). INSTALLED DOUBLER ANGLE IAW EO NR AST 050213 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050427002112005042700211WP 2005 4 27 DHL2005805588 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBD FLANGE (2EA) MISDRILLED HOLES AT STA 1340.000 L-12R TO L-13R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-07-05 EO NR AST 050201 DATED 02-17-05. PERFORMED DETAIL VISUAL INSP. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO NR AST 050201 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050427002132005042700213WP 2005 4 27 DHL2005805637 120050323A534037532351 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 AFT CARGO COMPT FITTING CRACKED 1.000 STA 980.000 L-22R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PAGE 1. REMOVED DAMAGED FITTING IAW SRM 51-1-20D PAGE 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING (PN 3753235-1) IAW SRM 51-1-20D PAGE 9. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050427002152005042700215WP 2005 4 27 DHL2005805605 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME HOLES (2EA) MISDRILLED STA 460.000 L-10R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-07-05 EO NR AST 050201 DATE 02-17-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MSIDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO NR AST 050201 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050427002182005042700218WP 2005 4 27 DHL2005805576 120050320A5340 CLIP DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO BAY CLIP HAS A MISDRILLED HOLE OF 0.1875 AT STA 834.000 L-14L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-13-05, EO NR AST050220 DATED 03-08-05. REMOVED DAMAGED CLIP IAW SRM 51-1-21 PG 1. PERFORMED DETAIL VISUAL INSP. NO CRACK FOUND. FABRICATED NEW CLIP (AL7075T60.063) IAW EO NR AST050220, SRM 51-1-21 PG 1. (MS20470AD). 2L74 4F RT4A25 20050427002192005042700219WP 2005 4 27 DHL2005805587 120050320A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBD FLANGE (1EA) MISDRILLED HOLE STA 1460.000 L-17R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-04-05 EO NR AST 050217 DATED 03-03-05. PERFORMED DETAIL VISUAL INSP. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLE WITH RIVET (MS20470AD) IAW EO NR AST 050217, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050427002202005042700220WP 2005 4 27 DHL2005805589 120050323A5740565122113 FITTING DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 LT WING T/E ZEE CRACKED 1.000 XW -3125.000. REMOVED CRACKED ZEE IAW SRM 57-1-0 PAGE 1, SRM 51-1-20D PAGE 1, SRM 51-1-21 PAGE 1. FABRICATED NEW ZEE (AL2024.0 0.050) IAW EA572000555, DWG 5651221. PERFORMED HEAT TREATMENT IAW SRM 51-1-1 PAGES 1, 13, 17. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02 TO 07. CLEANED, TREATED AND PRIMED AREA AND NEW ZEE IAW SRM 51-1-8B. INSTALLED NEW ZEE IAW SRM 51-1-20D PAGE 9. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050427002212005042700221WP 2005 4 27 DHL2005805597 120050326A57403654648 BRACKET DOUG DC8 DC873F 302199FWP FUEL PUMP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 NR 2 MAIN TANK FEED PUMP FWD BRACKET CRACKED (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-22-05, EO NR AST 050226 DATE 03-22-05. REMOVED CRACKED BRACKET IAW SRM 51-1-20D PAGE 21. FABRICATED NEW BRACKET (AL7075-T651) IAW EO NR AST 050226. PERFORMED HEAT TREATMENT IAW SRM 51-1-1 PAGES 1,13,17. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02 TO 07. CLEANED, TREATED AND PRIMED AREA AND NEW BRACKET IAW SRM 51-1-8B. INSTALLED NEW BRACKET IAW SRM 51-1-20D PAGE 9. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050427002222005042700222WP 2005 4 27 DHL2005805570 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBD FLANGE HOLES (2EA) MISDRILLED AT STA 1060.000 L-10R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-07-05 EO NR AST050201 DATE 02-17-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO NR AST050201, SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050427002232005042700223WP 2005 4 27 DHL2005805573 120050324A57205615767502 CAP DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 RT WING LWR CAP CRACKED BETWEEN CTR AND FRONT SPAR, STA XRS 238.000 CANT (NR 3 MAIN TANK) (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-09-05, EO NR AST050214 EO AST 050215, DWG 5615767. REMOVED DAMAGED BULKHEAD LWR CAP IAW SRM 51-1-20D PG 21, SRM 51-3-0 PAGE 1. FABRICATED NEW BULKHEAD LWR CAP (AL7075T6511) EO NR AST 050214, DWG 5615767. PERFORMED HEAT TREATMENT IAW SRM 51-1-1 PAGES 1, 13, 17. PERFORMED NDT INSPECTION IAW ND SPM PART 08-00-02-07. CLEANED, TREATED AND PRIMED AREA AND NEW CAP IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PAGE 9. INSTALLED BULKHEAD LWR CAP IAW EO AST 050215, SRM 51-1-20D PAGE 9, SRM 51-3-0 PAGE 1. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050427002242005042700224WP 2005 4 27 DHL2005805554 120050324A5313 SPLICE DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 L-1 SPLICE FITTING CRACKED 1.000 STA 587.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EA NR 534000556, DWG 4750521, SRM 53-1-0 PG 1. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-20D PG 21. FABRICATED NEW SPLICE FITTING (7075T651) IAW DRAWING NR 4750521. PERFORMED NDT INSP IAW NDT SPM PART 08-00-02-07. INSTALLED NEW SPLICE FITTING IAW SRM 51-1-20D PG 9. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050427002252005042700225WP 2005 4 27 DHL2005805558 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBD FLANGE (2EA) MISDRILLED HOLES, STA 1420.000 L-9 L-10L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-05-05 EO NR AST 050205 DATED 02-21-05. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA AT STA 1420.00 L-9L TO L-10L IAW SRM 51-1-8B. PERFORMED DETAIL VISUAL INSP. NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD6-4) IAW EO NR AST 050205, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050427002262005042700226WP 2005 4 27 DHL2005805590 120050323A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT "Z" FRAME INBD FLANGE CRACKED 2.000 STA 80.000 L-20.5R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 2 SHEET 2, 6 TR NR 53-110, SRM 53-4-1 FIG 40. REMOVED FASTENERS IAW SRM 51-1-20D PAGE 21, SRM 51-1-21 PAGE 1. TRIMMED OUT DAMAGED AREA, FABRICATED NEW FRAME SEGMENT (AL7075-T6 BAR) SPLICES (2EA) (AL70750 0.080) IAW SRM 53-2-0 FIG 2 SHEET 2, 7, 8, SRM 53-4-1 FIG 40, SRM 51-1-4 PAGE 1. PERFORMED HEAT TREATMENT IAW SRM 51-1-1 PAGES 1, 13, 17. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SRM 53-2-0 FIG 2 SHEET 2, 6, 7, 8 SRM 51-1-21 PAGE 1, SRM 51-1-20D PAGE 9. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050427002272005042700227WP 2005 4 27 DHL2005805606 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBD FLANGE (2EA) MISDRILLED HOLES AT STA 1140.000 L-12R TO L-13R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-07-05 EO NR AST 050201 DATED 02-17-05. PERFORMED DETAIL VISUAL INSP. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO NR AST 050201, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050427002282005042700228WP 2005 4 27 DHL2005805609 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME (1EA) MISDRILLED HOLE AT STA 460.000 L-12L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-05-05 EO NR AST 050205 DATED 02-21-05. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA AT STA 460.000 L-12L IAW SRM 51-1-8B. PERFORMED DETAIL VISUAL INSP. NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD6-5) IAW EO NR AST 050205 AND SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050427002302005042700230WP 2005 4 27 DHL2005805560 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBD FLANGE HOLE MISDRILLED STA 520.000 L-15R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-07-05, EO NR AST050201 DATE 02-17-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLE WITH RIVET (MS20470AD) IAW EO NR AST050201, SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050427002322005042700232WP 2005 4 27 DHL2005805575 120050325A57305643321 SEAL DOUG DC8 DC873F 302199FWP RT WING SKIN CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 RT WING T/E UPPER SKIN STEEL SEAL CRACKED XRS 9.000 - XRS 15.000. REMOVED CRACKED SEAL FITTING IAW SRM 57-1-0 PAGE 1, SRM 51-1-21 PAGE 1. FABRICATED NEW SEAL FITTING (STEEL SHEET 301CRES 0.500 HARD 0.012) IAW FAA FORM 8110-3 DATE 03-23-05 EO NR AST050227 DATE 03-23-05. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02 TO 07. CLEANED, TREATED AND PIRMED AREA IAW SRM 51-1-8B. INSTALLED NEW SEAL FITTING IAW SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050427002342005042700234WP 2005 4 27 DHL2005805548 120050323A5313 SPLICE DOUG DC8 DC873F 302199FWP STRINGER CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 LONGERON END FITTING AFTER SPLICE FITTING CRACKED 3.000, STA 902.000 L-1 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EA534000554, DWG 4750521, SRM 53-1-0 PAGE 1. REMOVED DAMAGED SPLICE FITTING IAW SRM 51-1-20D PAGE 21. FABRICATED SPLICE FITTING (AL7075T651) IAW DWG 4750521. PERFORMED NDT INSPECTION TO SPLICE FITTING IAW NDT SPM PART 08-00-02-07. INSTALLED NEW SPLICE FITTING IAW SRM 51-1-20D PAGE 9. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050427002362005042700236WP 2005 4 27 DHL2005805559 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBD FLANGE HOLE MISDRILLED STA 520.000 L-12.5R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-07-05, EO NR AST 050201 DATE 02-17-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED AREA (MISDRILLED HOLES) IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLE WITH RIVET (MS20470AD) IAW EO NR AST 050201, SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050427002382005042700238WP 2005 4 27 DHL2005805551 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME (2EA) MISDRILLED HOLES AT STA 600.000 L-10R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-07-05, EO NR AST 050201 DATED 02-17-05. PERFORMED DETAIL VISUAL INSP. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGE AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO NR AST050201, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050427002402005042700240WP 2005 4 27 DHL2005805577 120050320A5340 CLIP DOUG DC8 DC873F 302199FWP FUSELAGE FRAME WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME CLIP WORN, STA 580.000 L-11L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-15-05, EO NR AST 050220 DATED 03-08-05. REMOVED DAMAGED CLIP IAW SRM 51-1-21 PG 1. PERFORMED DETAIL VISUAL INSP. NO CRACK FOUND. FABRICATED NEW CLIP (AL7075-T6 0.080) IAW EO NR AST 050220. CLEANED, TREATED AND PRIMED AREA AND NEW CLIP IAW SRM 51-1-8B. INSTALLED NEW CLIP IAW EO NR AST 050220, SRM 51-1-21 PG 1. (MS20470AD) 2L74 4F RT4A25 20050427002412005042700241EA 2005 4 27 QXEA200500440 120050304A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 200 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - FUSELAGE EXTERIOR FORWARD BAY DOOR CUTOUT, HAS SCRATCHES ON FORWARD EDGE OF DOOR CUTOUT FS 310, WL 80. REPAIRED IAW REO 670-53-21-081 AND HORIZON AIR EA R-53-276 AND CRJ700 SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050427002432005042700243EA 2005 4 27 QXEA200500436 120050224A5320 PLATE CNDAIRCL600 CL6002C10 1390015EA ZONE 200 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - CENTER UPPER FUSELAGE, OVERWING EXITS, RIGHT HAND OVERWING EXIT LOWER SILL PLATE GOUGED. REPAIRED IAW CRJ700 SRM 53-41-06-101-003-A01, SRM 51-12-00-001-001-A01, AND SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050427002822005042700282 2005 4 27 MASA200500018 420050106A34177858062 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA NR 2 AIR DATA MALFUNCTIONED A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW077730210554 7302 ASH 6164 PHX TO SAT, RETURNED TO THE FIELD DUE TO A RT TAT, PITOT AND AOA HEAT CAUTION MESSAGE. MAINTENANCE REPLACED THE AIR DATA SENSOR CONTROLLER IN THE NR 2 POSITION. 2L72 4F RTA21EA 20050427002842005042700284EA 2005 4 27 MASA200500029 120050112A3260 PROXIMITY SWITCH CNDAIRCL600 CL6002B19 1900309EA MLG OUT OF ADJUST A MASAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW07715SF 7115 ASH 2669 FROM PHL TO GRR, DIVERTED TO PIT DUE TO A LT MAIN LANDING GEAR DISAGREE MESSAGE AFTER TAKEOFF. AIRCRAFT FERRIED TO PHL AND MX ADJUSTED THE UPLOCK PROXIMITY SWITCHES. AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. 2L72 4F RTA21EA 20050427002872005042700287EA 2005 4 27 MASA200500232 120050318A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA EMERGENCY EXIT MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0777331 7331 ASH 7197 IAD TO ATL- LT EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE. MX PERFORMED OPERATIONAL TEST OF THE EMERGENCY LIGHTS AND COULD NOT DUPLICATE. 2L72 4F RTA21EA 20050427002912005042700291WP 2005 4 27 05FDEA00706 120050330A5753 SKIN DOUG DC10 DC10* WP ZONE 600 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25060 46970 RIGHT WING INBOARD FLAP, INCORRECT REPAIR ON UPPER SKIN, INBOARD WEDGE. REMOVED DOUBLER, FABRICATED NEW SKIN, FINGER DOUBLERS AND DOUBLER AND BONDED IAW FEDEX EA 8- 5710-84001 AND TPS 1001 REV E AND DC10 SRM 51-21-01 VOL 2 AND DC10 SRM 51-31-01 VOL 2. REFERENCE NON-ROUTINE N00788. 2L73 4F A22WE 20050427002932005042700293WP 2005 4 27 05FDEA00708 120050330A5753ARC25121 HINGE DOUG DC10 DC10* WP ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2510060 46970 LEFT WING INBOARD FLAP, OUTBOARD SUPPORT, PIVOT ATTACH POINT OUTBOARD BORE CORRODED. REMOVED CORROSION FROM BORE IAW DAC CMM 57-52-01. ALODINED AND PRIMED BORE IAW DC10-10 SRM 51-21-01 VOL 2, FABRICATED AND INSTALLED FINAL HONED NEW OVERSIZED BUSHING TO 0.9995-1.0005 IAW DAC CMM 57-52-01 AND EA 8-5750-83998, WINGS LEFT INBOARD FLAP, OUTBOARD HINGE BRACKET OVERSIZE PIVOT BORES AND STRAP REPAIR. REFERENCE NON-ROUTINE N00468. 2L73 4F A22WE 20050427002952005042700295NM 2005 4 27 05FDEA00725 120050331A5512 SKIN DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZ STAB LT UPPER FWD SKIN PLANK NR 5L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82939. 2L73 4F RTA22WE 20050427002972005042700297NM 2005 4 27 05FDEA00727 120050331A5210 SKIN DOUG MD11 MD11 3023602NM ZONE 200 DEFORMED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 FWD CABIN, L1 DOOR SKIN UPPER EDGE FOUND DEFORMED. REPAIRED IAW EA 1-5210-83093. 2L73 4F RTA22WE 20050427002992005042700299NM 2005 4 27 05FDEA00730 120050331A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZ STAB LT UPPER FWD SKIN PLANK NR 13L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82939. 2L73 4F RTA22WE 20050427003012005042700301NM 2005 4 27 05FDEA00732 120050331A5512 SKIN DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZ STAB LT UPPER CENTER SKIN PLANK NR 17L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82940. 2L73 4F RTA22WE 20050427003032005042700303WP 2005 4 27 DHL2005801005 120050331A5270 SWITCH DOUG DC8 DC873F 302199FWP MLG DOOR DIRTY A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01801DH 46033 AFTER TAKEOFF GEAR DOOR NOT LATCHED LIGHT ILLUMINATED, PERFORMED UPLATCH CHECK, LIGHT WENT OUT. INSPECTED RT MAIN DOOR SWITCH. PERFORMED OPS CHECK OF UP LATCH SYSTEM. CLEAN RT DOOR SWITCH, OPS CHECK GOOD PER 32-60-00 DC8 MM. 2L74 4F RT4A25 20050427003052005042700305CE 2005 4 27 032805N152CS1 120050328A273155657562 TRIM SCALE CESSNA525 525 2076601CE COCKPIT BROKEN E Z5FAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 NE03152CS 5250539 UPON ROTATION AIRCRAFT REQUIRED EXCESSIVE BACK PRESSURE ON YOKE TO MAINTAIN CLIMB PITCH AND UNABLE TO CLIMB TO ASSIGNED ALTITUDE. DECLARED EMERGENCY AND RETURNED TO AIRPORT FOR UNEVENTFUL LANDING. REPAIR TO AIRCRAFT INVOLVED REPLACEMENT OF ELEVATOR TRIM WHEEL AND TRIM POINTER, COMPLETE CHECK OF ELEVATOR CONTROL SYSTEM, AND OPERATIONAL CHECK FLIGHT. AIRCRAFT RETURNED TO SERVICE WITH NO PROBLEMS SINCE EVENT. 1L72 4F RTA1WI 20050427003332005042700333NM 2005 4 27 05FDEA00483 120050307A5320 STIFFENER BOEING727 727100 1384036NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 DURING B-CHECK, STIFFENER FITTING BELOW "S" DUCT CRACKED AND FRAMING STRUCTURE FOR "S" DUCT CORRODED, BOTH AT BS 1342 BOTH ON RT SIDE REF EA NR7-5310-87123 FOR FERRY FLT APPROVAL. 2L73 4F RTA3WE 20050427003362005042700336WP 2005 4 27 AALA20050180 120050309A32404920750U1 RIVET DOUG DC9 DC982 3022082WP BRAKE SHEARED A AALAO OTHER O OTHER TXTAXI/GRND HDL 1 SW21494AA 49732 BNA - AIRCRAFT WOULD NOT TAXI FORWARD AFTER PUSHOUT. LEFT HAND BRAKES LOCKED. FOUND RIVET SHEARED ON LEFT HAND BRAKE PAW ASSEMBLY ON CAPTAINS LEFT HAND BRAKE PEDAL LINKAGE. REPLACED RIVET ON LEFT HAND BRAKE PAW ASSEMBLY ON CAPTAINS LEFT HAND BRAKE PEDAL LINKAGE. SYSTEM GROUND CHECKED NORMAL OPERATION. (SUPP. CLOSED) 2L72 4F A6WE 20050427003512005042700351CE 2005 4 27 70056 120050330A3260 ANNUNCIATOR BEECH 1900 1900D 1154162CE COCKPIT DEFECTIVE A AMWAB EMER. DESCENT N FALSE WARNING APAPPROACH 1 CE07140ZV UE140 ON APPROACH FOR LANDING IN ART WITH GEAR EXTENDED CREW NOTED NOSE GEAR DIDN'T INDICATE DOWN AND LOCKED. THEN PERFORMED EMERGENCY CHECKLIST AND PUMPED GEAR DOWN BY HAND. STILL NOSE DIDN'T INDICATE DOWN AND LOCKED. CREW DID FLYBY OF FIELD AND WERE REPORTED NOSE GEAR WAS DOWN. CREW THEN LANDED SAFELY WITH NO FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ANNUNICATOR ASSEMBLY. 2L72 4T RTA24CE 20050427003542005042700354NM 2005 4 27 QXEA200500541 120050324A7110 FITTING BOMBDRDHC8 DHC8401 1390041NM NR 1 COWLING CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09416QX 4083 PDX - FORWARD LOWER COWL ATTACHMENT LUG CHAFED ON NR 1 ENGINE RIGHTHAND FORWARD LOWER LUG. REPAIRED IAW HORIZON AIR EA 6-54-346. 2H72 4T RTA13NM 20050427003592005042700359EA 2005 4 27 QXEA200500620 120050320A1430 RIVET CNDAIRCL600 CL6002C10 1390015EA FUSELAGE LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE UPPER EXTERIOR HAS SEVERAL SMOKING RIVETS AT STRINGER 7L, BETWEEN FUSELAGE STATION 893 TO 939. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01 AND SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050427003602005042700360EA 2005 4 27 QXEA200500621 120050320A1430 RIVET CNDAIRCL600 CL6002C10 1390015EA FUSELAGE LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE UPPER EXTERIOR HAS SEVERAL SMOKING RIVETS AT STRINGER 3L AND BETWEEN FUSELAGE STATION 345 TO 379. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01 AND SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050427003662005042700366NM 2005 4 27 QXEA200500680 120050401A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09367PH 511 PDX - LEFTHAND INBOARD SEAT TRACK HAS 14 INCH LONG CHAFE MARK INSIDE CHANNEL AT STATION 504. REPAIRED IAW RD 8-53-1339. 2H72 4T RTA13NM 20050427003702005042700370NM 2005 4 27 QXEA200500688 120050416A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - RIGHTHAND INBOARD SEAT TRACK IS CORRODED IN NUMEROUS LOCATION ON TOP BETWEEN X201 AND X222.7. REPAIRED IAW DHC-8 200 SRM 51-40-11 AND RD 8-53-4473. 2H72 4T RTA13NM 20050427003722005042700372NM 2005 4 27 QXEA200500696 120050413A5330 SKIN DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - FUSELAGE SKIN UNDER THE NR 1 ATC ANTENNA HAS EVIDENCE OF CORROSION. REPAIRED IAW HORIZON AIR EA 2-53-618 AND RD 8-53-8473. 2H72 4T RTA13NM 20050427003742005042700374NM 2005 4 27 QXEA200500700 120050415A5420 STRUCTURE DHAV DHC8 DHC8202 2809007NM NACELLE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - LEFTHAND MAIN LANDING GEAR CHAFE ABOVE DRAG STRUT ASSEMBLY LEFT SIDE. REPAIRED IAW RD 8-54-2000 AND HORIZON AIR EA 2-54-227. 2H72 4T RTA13NM 20050427003762005042700376NM 2005 4 27 QXEA200500674 120050412A5230 SKIN DHAV DHC8 DHC8202 2809007NM CARGO DOOR GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - CARGO DOOR INNER SKIN GOUGED AT SCREW HOLE, MIDDLE FORWARD OF DOOR, X554, Z130. REPAIRED IAW DHC-8 200 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20050427003782005042700378NM 2005 4 27 QXEA200500666 120050412A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - CORROSION IN AND AROUND SCREW HOLES ON NR 6 SEAT TRACK INBOARD FLANGE AT STATION X264 AND X580. REPAIRED IAW DHC-8 200 SRM 51-40-11 AND RD 8-53-784. 2H72 4T RTA13NM 20050427003802005042700380NM 2005 4 27 QXEA200500701 120050416A5753 DOUBLER DHAV DHC8 DHC8202 2809007NM T/E FLAP CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - LEFTHAND OUTBOARD FLAP HAS .5 INCH CHAFE MARK ON PREVIOUS REPAIR PATCH ON TOP EXTERIOR SKIN AT WS YW 176.000, 20 INCH FORWARD OF TRAILING EDGE AND 2 INCH INBOARD FROM FLAP EDGE. REPAIRED IAW DHC-8 200 SRM 51-20-16, SRM 51-20-36 AND SRM 51-40-00. 2H72 4T RTA13NM 20050427003812005042700381NM 2005 4 27 QXEA200500712 120050421A2750C1486561 POWER UNIT BOMBDRDHC8 DHC8401 1390041NM T/E FLAP FAILED A QXEAL ABORTED APPROACH FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 NM09410QX6177 2199 4053 PDX - FLIGHT 2310 - FLAP POWER CAUTION. CREW ABORTED LANDING DUE TO THE FLAPS REMAINING UP WHEN SELECTED TO 5 DEGREES. THE FLAP CONTROL CIRCUIT BREAKER WAS RESET IAW THE EMERGENCY CHECKLIST. THE FLAP POWER CAUTION CAME BACK AND THE FLIGHT MADE A ZERO FLAP LANDING. MAINTENANCE INTERROGATED CDS AND FOUND A LOSS OF HYDRAULIC POWER FAULT. MAINTENANCE REMOVED AND REPLACED THE FLAP POWER UNIT PER Q400 MM TASKS 27-52-01-000-801 AND 27-52-01-400-801. MAINTENANCE PERFORMED A FUNCTIONAL TEST OF THE FLAP DRIVE SYSTEM. FUNCTIONAL CHECK AND LEAK CHECK GOOD. NO FURTHER DETECTS NOTED. 2H72 4T RTA13NM 20050427003872005042700387NM 2005 4 27 QXEA200500693 120050414A5320 SILL DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - MAIN CABIN DOOR SILL TOP SIDE CORRODED AROUND MIDDLE NUT PLATE. REPAIRED IAW DHC-8 200 SRM 51-40-00 AND SRM 51-40-11. 2H72 4T RTA13NM 20050427003902005042700390NM 2005 4 27 QXEA200500689 120050416A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - LEFTHAND INBOARD SEAT TRACK HAS SURFACE CORROSION BETWEEN STATION 222.7 AND STATION 240.0 IN FIVE LOCATIONS. REPAIRED IAW DHC-8 200 SRM 51-40-11 AND RD 8-53-4473. 2H72 4T RTA13NM 20050427003922005042700392NM 2005 4 27 QXEA200500690 120050415A5312 BULKHEAD DHAV DHC8 DHC8202 2809007NM FUSELAGE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - UPPER CENTER RADOME SCREW HAS CHAFED BULKHEAD AT STATION X66, Z120. REPAIRED IAW HORIZON AIR EA 2-53-620. 2H72 4T RTA13NM 20050427004012005042700401EA 2005 4 27 QXEA200500606 120050317A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE INTERIOR, RIGHTHAND INBOARD SEATRAIL, AT STATION X584, HAS PITTING CORROSION ON TOP SURFACE. REPAIRED IAW CRJ700/900 SRM 51-21-06-001-001-A01, PARAGRAPH 3E, REO 670-53-00-013 AND CRJ700 SRM 51-21-16, CODE A044. 2L72 4F RTA21EA 20050427004022005042700402EA 2005 4 27 QXEA200500568 120050321A5414 SKIN CNDAIRCL600 CL6002C10 1390015EA RT NACELLE GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - RIGHTHAND NACELLE LIPSKIN GOUGED BETWEEN 3 AND 5 O'CLOCK POSITIONS. REPAIRED IAW CRJ700 SRM 51-21-11-001-A01. 2L72 4F RTA21EA 20050427004092005042700409NM 2005 4 27 QXEA200500642 120050408A2751 WARNING LIGHT BOMBDRDHC8 DHC8401 1390041NM COCKPIT ILLUMINATED A QXEAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM09403QX 4037 PDX - FLAP POWER CAUTION LIGHT. COMPLIED WITH RESET OF FLAPS CONTROL CIRCUIT BREAKER PER CHECKLIST. MAINTENANCE COMPLIED WITH DH8-400-SL-27-002A, CAUTION CLEARED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050427004132005042700413EA 2005 4 27 QXEA200500570 120050323A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA FUSELAGE SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FORWARD LOWER FUSELAGE SKIN AT STATION 260 AND RBL 6.0 HAS A TWO INCH LONG SCRATCH. REPAIRED IAW CRJ700 SRM 51-25-01-001-A01. 2L72 4F RTA21EA 20050427004142005042700414EA 2005 4 27 QXEA200500561 120050321A2550 RAIL CNDAIRCL600 CL6002C10 1390015EA CARGO BAY DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FORWARD FUSELAGE, FORWARD CARGO COMPARTMENT RETRIEVAL TRAY RAILS, FORWARD RIGHTHAND OUTBOARD SEVERAL SMALL AREAS OF HARD ANODIZED SURFACE COMING OFF. REPAIRED IAW CRJ700 SRM 51-21-11-001-001-A01 AND 51-21-06-001-001-A01. 2L72 4F RTA21EA 20050427004162005042700416EA 2005 4 27 QXEA200500554 120050323A5751 SKIN CNDAIRCL600 CL6002C10 1390015EA LT AILERON WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - LEFTHAND AILERON HAS SEVERAL AREAS OF WEAR ON TOP AND LOWER LEADING EDGE SKIN. REPAIRED IAW CRJ 700 SRM 51-41-02-001-001-A01. 2L72 4F RTA21EA 20050427004212005042700421EA 2005 4 27 QXEA200500559 120050326A5730 PANEL CNDAIRCL600 CL6002C10 1390015EA RT WING CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - RIGHTHAND WING FUEL LID REBATE PANEL 641BB HAS MINOR FRETTING CORROSION. REPAIRED IAW CRJ700 SRM 51-21-16-001-001-A01 AND TASK 51-80-00-760-802-A01. 2L72 4F RTA21EA 20050427004232005042700423EA 2005 4 27 QXEA200500614 120050325A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA FUSELAGE SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE EXTERIOR HAS SCRATCH AT STATION 1031 AND STRINGER 5R. REPAIRED IAW CRJ700 SRM 51-25-01-001-001-A01 AND CRJ700 SRM 53-61-01-101-A01. 2L72 4F RTA21EA 20050427004422005042700442NM 2005 4 27 QXEA200500710 120050416A2612JD4N RELAY BOMBDRDHC8 DHC8401 1390041NM APU FIRE WARNINGINOPERATIVE A QXEAO OTHER N FALSE WARNING CRCRUISE 1 NM09403QX 4037 PDX - FLIGHT 403QX - THE MASTER WARNING AND CHECK FIRE DETECTION LIGHTS ILLUMINATED IN FLIGHT. THE APU FIRE BOTTLE LOW LIGHT WAS ALSO ILLUMINATED AND STEADY AFTER RUNNING CHECK LIST. THE BOTTLE LOW AND MASTER WARNING ILLUMINATED OFF AND ON FOR A WHILE AND THEN STAYED OFF. UPON LANDING THE APU FIRE WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED THE APU FIRE CONTROL RELAY AND PERFORMED OPERATIONAL TESTS OF THE APU FIRE DETECTION SYSTEM IAW 8-400 MM TASK 26-13-00-710-801. OPS CHECK GOOD. MTX ALSO CHECKED CONNECTORS ON APU FIRE BOTTLES, APU FADE AND RELAY BOX. ALL CONNECTORS SECURE AND APU FIRE BOTTLE INDICATOR SHOWS GREEN LIGHT. OK FOR SERVICE. 2H72 4T RTA13NM 20050427004442005042700444EA 2005 4 27 QXEA200500556 120050329A7110 SKIN CNDAIRCL600 CL6002C10 1390015EA LT COWLING DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - LEFT LOWER TRANSCOWL HAS A DENT 9 INCHES AFT OF FORWARD EDGE AT BOTTOM OF COWL. REPAIRED IAW REO 670-54-21-350 AND CRJ 700 SRM 51-25-16-001-001-A01. 2L72 4F RTA21EA 20050427004492005042700449EA 2005 4 27 QXEA200500610 120050317A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE INTERIOR, LEFTHAND INBOARD SEAT RAIL AT STATION X479 HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW REO 670-53-00-013 AND CRJ700 SRM 51-21-16, CODE A044. 2L72 4F RTA21EA 20050428000032005042800003EU 2005 4 28 05FDEA00527 120050315A5753 SKIN AIRBUS310 A310222 3930315EU TE FLAP MISREPAIRED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25451FE 303 COMPLY WITH AGING 9 - AGING INSPECTION, RT WING - REPAIR AT RT INBOARD FLAP LOWER TRAILING EDGE. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 57-52-12. 2L72 4F RTA35EU 20050428000062005042800006EU 2005 4 28 05FDEA00533 120050315A5230 HOOK AIRBUS310 A310222 3930315EU CARGO DOOR DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25451FE 303 COMPLY WITH AGING 9 - AGING INSPECTION, FUSELAGE - REPAIR AT REAR LOWER CARGO DOOR AT FWD LOCK HOOK (PLEASE EVALUATE). REMOVED/INSTALLED AFTER REPAIR PER AMM 52-30-21. REPAIRED PER SRM 51-73-10. PAINTED PER SRM 51-75-10-08. CONFORMS TO SRM 51-73-10. 2L72 4F RTA35EU 20050428000212005042800021NM 2005 4 28 DHL2005742003 120050323A56105893543130 WINDOW BOEING727 727225 1384077NM COCKPIT FIRE A DHLAFB ACTIVATE FIRE EXT. EMER. DESCENT BA SMOKE/FUMES/ODORS/SPARKS FLAME/FIRE CRCRUISE 1 SO01742DH 21290 SMOKE AND FIRE NOTED FROM R1 WINDSHIELD CONNECTION. COMPLETED CHECK LIST AND NOTED C/B HAD TRIPPED. FIRE EXTINGUISHER HAS BEEN DISCHARGED. INSPECTED WIRING PER SWPM CH-20-10-06. NO DEFECTS NOTED. R & R R2 WINDOW ASSY IAW B727 M/M 56-11-11. PERFORMED OPS CHECK IAW 30-41-12. OPS CHECK SERVICEABLE. 2L73 4F A3WE 20050428000222005042800022WP 2005 4 28 DHL2005809002 120050323A3350 LIGHT DOUG DC8 DC873F 302199FWP CABIN INOPERATIVE A DHLAK NONE O OTHER ININSP/MAINT 1 SO01809DH 46047 DEMERGENCY EXIT LIGHTS INOP. PERFORMED OPS CHECKS OF EMERGENCY LIGHTS SYSTEM OPS CKS OK IAW MM 33-50-0 2L74 4F RT4A25 20050428000252005042800025NM 2005 4 28 05FDEA00633 120050324A5315BAC1518338 FLOORBEAM BOEING727 727227 1384078NM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25493FE 21531 WHILE ACCESSING FOR BARRIER MOD FOUND REPAIR ON FLOORBEAM BL 0 NEEDS REWORK TO ACCOMPLISH INSTALLATION OF EXTENDED SEAT TRACK. REPAIRED PER SRM 53-10-8 2L73 4F A3WE 20050428000272005042800027EU 2005 4 28 SA05033 120050324A33501012881 LIGHT AIRBUSA319 A319112 3930323EU CABIN DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19108UW 1061 CLT - THE ROW 5C EMERGENCY EXIT LIGHT HOUSING WAS FOUND DAMAGED. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY AT SEAT ROW 5C. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20050428000282005042800028GL 2005 4 28 DJFA2005070 220050324A7310 WARNING LIGHT CESSNA525 525 2076601CE WILINTFJ44 FJ441A GL ENGINES ILLUMINATED E DJFAO OTHER J WARNING INDICATION CRCRUISE 1 EA23288CW 5250218 DURING CRUISING, APPROX 1 HR AFTER TAKING OFF WITH FULL FUEL, RT FUEL FILTER BY-PASS & MASTER CAUTIONS ILLUMINATED. RT BOOST PUMP TURNED ON. 10 MINS LATER, LT FUEL FILTER BY-PASS ILLUMINATED. LT BOOST PUMP TURNED ON & AN EMERGENCY DECLARED. DURING DESCENT, HEARD WHAT SOUNDED LIKE A MILD COMPRESSOR STALL FROM 1 OF ENGS. ENG INSTRUMENTS INDICATED NORMAL. A/C MADE AN UNEVENTFUL LANDING. MX REPLACED FUEL FILTERS. FUEL FILTERS & SAMPLES SENT FOR ANALYSIS. FILTERS & FUEL FROM BOWL SENT TO BE TESTED. DRAINS SUMPED, & ENGS RAN. FUEL FILTERS REPLACED & DRAINS SUMPED FOLLOWING ENG RUN. FILTERS REMOVED ALONG WITH FUEL FROM BOWL SENT FOR TESTING OF WATER & CONTAMINANTS. TESTS NEGATIVE. A/C RETURNED TO SERVICE. 1L72 4F4 FRTA1WI E3GL 20050428000322005042800032NM 2005 4 28 DHL2005782567 120050310A5532 PANEL BOEING727 727227 1384078NM VERTICAL STAB DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 DURING AN A-CHECK, THE FOLLOWING DISCREPANCES WERE NOTED LWR VERTICAL PNL LT SIDE HAS 2 EA DENTS. CUT OUT DAMAGED AREAS APPROX 1 INCH ROUND AND 2 INCHES ROUND IAW B727 SRM 51-40-2 FIG 30, FABRICATED ONE FILLER 1 INCH ROUND AND ONE FILLER 2 INCHES ROUND AND ONE DOUBLER 4 INCHES ROUND AND ONE DOUBLER 5 INCHES ROUND, USING 2024-T3 .016 PO 9001660 IAW B727 SRM 55-30-2 FIG 1. CLEANED, PREPPED, AND APPLIED PRIMER AND ADHESIVE TO ALL REPAIR SURFACES AND BAGGED FOR BONDING IAW B727 SRM 51-40-2 FIG 30. CURED REPAIR, CLEANED AND PERFORMED POST-BOND INSP WITH NO DEFECTS NOTED IAW B727 SRM 51-40-2 PARA 0. TREATED SEALED AND PRIMED REPAIR IAW B727 SRM 51-40-2 PARAGRAPH-P. 2L73 4F A3WE 20050428000342005042800034NM 2005 4 28 05FDEA00876 120050406A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 RIGHT WING O/B FLAP I/B FLAP MOUNTED HINGE PIVOT HOLE EVIDENT OF CORROSION. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F RTA22WE 20050428000372005042800037NM 2005 4 28 05FDEA00882 120050406A5347FXMACH7248 SEAT TRACK BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25271FE 22036 MAIN CARGO COMPT SEAT TRACK FS 1110 - 1130, BL 0, HAS DAMAGED AREAS. REMOVED DAMAGED AREA ON SEAT TRACK IAW SRM 53-10-1 FIG 3 DETAIL 6. RE-EVALUATED AREA FOUND TO BE OUT OF LIMIT IAW SRM 53-10-1 FIG 3 DETAIL 6. REMOVED FASTENER ON LOWER LEG OF SEAT TRACK BL 0, FS 1110-1130 IAW SRM 51-30-2. REMOVED REMAINING FASTENERS AND CUT SEAT TRACK IAW SRM 53-10-5 FIG 1. FABRICATED SEAT TRACK REPAIR SECTION IAW SRM 53-10-5 FIG 1. LOCATED AND DRILLED REPAIR PARTS IAW SRM 51-30-5. INSTALLED SEAT TRACK SECTION IAW SRM 51-30-2 AND SRM 53-10-5 FIG 1. 2L73 4F RTA3WE 20050428000392005042800039EU 2005 4 28 05FDEA00884 120050407A2170 COALESCER BAG AIRBUS310 A310203 3930313EU A/C BAY CONTAMINATED A FDEAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SO25427FE 362 ON TAKEOFF ROLL JUST PRIOR TO V1, ODOR NOTED, THEN AT 300 FEET, MAIN DECK CARGO DET ILLUMINATED WITH APPROPRIATE ECAM. ATB KMEM 18R, CLEARED RWY. EMERGENCY GROUND PERSONNEL NOTED STRONG ELECTRICAL ODOR NO FUMES. DURING DEBRIEF, CREW REPORTED ECAM MESSAGE TO TURN NR 2 PACK OFF, MAIN DECK ISOL VALVE OFF, AND HOT AIR SUPPLY VALVE OFF. AFTER DOING SO, MAIN DECK CARGO DET LIGHTS WENT OUT. PERFORMED ADJUSTMENT TEST OF MAIN CARGO SMOKE DETECTION SYS. REMOVED AND REPLACED THE AFT MAIN, MID1 AND MID2 CONTROL UNITS AS PRECAUTIONARY. ENG RAN BOTH PACKS NOTICED ODOR CHECKED NR 1 AND 2 COALESCER BAGS, FOUND BAGS HEAVILY CONTAMINATED. REMOVED AND REPLACED NR 1 AND NR 2 COALESCER BAGS. RAN BOTH PACKS WITH NR 1, 2 ENG2L72 4F RTA35EU 20050428000402005042800040WP 2005 4 28 05FDEA00885 120050407A2781 SENSOR DOUG DC10 DC1030 3023501WP L/E SLAT FAULTY A FDEAK NONE N FALSE WARNING APAPPROACH 1 SO25320FE 47835 SLAT DISAGREE LIGHT ILLUMINATED WITH FLAP EXTENSION FROM 22 TO 35 AND REMAINED ON. PERFORMED RED TABS. LANDED WITH 22/EXT CONFIGURATION. ACCOMPLISHED DETAILED VISUAL INSPECTION OF THE SLAT CABLES BOTH LEFT AND RIGHT WING, PERFORMED PCU BITE TEST ALL CHANNELS PASS, PERFORMED SLAT TIMING TEST REF: 27-80-00-5-1 PASSED TEST. PERFORMED SLAT POSITION TEST PANEL CHECK REF: 27-80-00-6 PANEL PASSED TEST. CLEANED INBOARD SLAT SENSOR AND TARGET (MASSIVE AMOUNT OF GREASE ON TARGET & SENSOR). REMOVED AND REPLACED LEFT AND RIGHT NR 4 SLAT SENSOR BOTH A & B CHANNELS, PERFORMED ANOTHER PCU BITE TEST ALL CHANNELS PASSED. 2L73 4F A22WE 20050606000942005060600094CE 2005 6 6 DXTA200500745 120050529A3230 CABLE CESSNA750 750 2076810CE MLG OUT OF ADJUST E DXTAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 GL07924QS 7500124 25 MINS INTO THE FLIGHT JUST LEVELING OFF AT FL 410, FELT AND HEARD THE LANDING GEAR UNLOCK AND RETRACT TWICE. THE GEAR "UNLOCK" LIGHT REMAINED ILLUMINATED FOR 42 MINS UNTIL DESCENDING THRU FL310 WHEN FELT AND HEARD THE LANDING GEAR UNLOCK AND RETRACT ONCE AND THE LIGHT EXTINGUISHED. TROUBLESHOT NOSE LANDING GEAR BUMP PROBLEM IAW CESSNA MODEL 750 MM 32-30-00. FOUND EMERGENCY GEAR EXTEND CABLE TO BE TIGHT WITH NO SLACK AT ALL. ADJUSTED UPLOCK RELEASE CABLE IAW CMM MODE 750 32-30-06. 2L72 4J RTT00007WI 20050428000422005042800042NM 2005 4 28 05FDEA00888 120050407A5347 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 MAIN DECK, ALONG STA 1331 TO STA 1351 RBL 107.25 SEAT TRACK FOUND CORRODED. SEAT TRACK REPAIRED AS PER SRM 53-70-00 FIG. 1 VOL I. REPAIR SEAT TRACK FABRICATED AS PER DRAWING AEA 7532. MAJOR REPAIR PER GMM 6-2-100. 2L73 4F RTA22WE 20050428000432005042800043NM 2005 4 28 05FDEA00889 120050407A5312 BULKHEAD DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 CENTER CARGO HAS CRACK ON BULKHEAD AT STA 184 X=5. REPAIRED AS PER SRM 53-00-01, VOL I, FIG. 10. 2L73 4F RTA22WE 20050428000482005042800048NM 2005 4 28 05FDEA00894 120050407A5347FX601045218 SEAT TRACK BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25271FE 22036 MAIN CARGO COMPT SEAT TRACK FS 1160 - 1183 HAS DAMAGED AREAS ALONG BL 0. REMOVED & REPLACED SEAT TRACK SECTION STA 1138 - 1183 BL 0 IAW SRM 51-30-2. NEW TRACK FABBED ON TRAVELER T5/503663. 2L73 4F RTA3WE 20050428000492005042800049NM 2005 4 28 05FDEA00895 120050407A5347FX1520792 SEAT TRACK BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25271FE 22036 SEAT TRACK STA 480 TO 690, LBL 45 HAS CORROSION AND EXISTING BLEND REPAIRS AND REQUIRES REPLACEMENT PER 7-5340-7-5002. REMOVED SEAT TRACK IAW SRM 51-30-2. NEW SEAT TRACK FABBED ON TRAVELER T5/512298, CUT OUT SECTION OF TRACK AT 480 - 510 IAW SRM 53-10-5 FIG 1. FABRICATED REPAIR PARTS FROM 60-6549/24 BATCH 30754-1, FROM 60-338/24 BATCH 869734, FROM 7075 T-6 250C BATCH 555535 IAW SRM 53-10-5 FIG 1. LOCATED AND DRILLED HOLES IAW SRM 51-10-2, INSTALLED SEAT TRACK IAW SRM 51-30-2, STA 480 - 690. PERFORMED J-VIEW OF DWG 2902. 2L73 4F RTA3WE 20050428000552005042800055NM 2005 4 28 05FDEA00901 120050408A5514 STRUCTURE DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 RT HORIZONTAL STABILIZER UPPER BARREL NUT NR 25 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133. 2L73 4F RTA22WE 20050427000482005042700048NM 2005 4 27 DHL2005781554 120050216A5531 FRAME BOEING727 727227 1384078NM VERTICAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A C-CHECK, VERT STAB FIN STA 133 STR S-8LT IS CRACKED AT FRAME ATTACH BOLT. REMOVED FASTENERS FOR ACCESS, CUT OUT DAMAGED DIM 4.50 X 3 INCHES STIFFENER AND REMOVED FILLER IAW B727 SRM 55-30-4 FIG 1. FABRICATED STIFFENER REPAIR. INSTALLED STIFFENER REPAIR AT VERT STAB FIN STA 133 STRG 8 LT IAW B727 SRM 55-30-4 FIG 1. 2L73 4F A3WE 20050427000522005042700052NM 2005 4 27 DHL2005781558 120050224A5531 FRAME BOEING727 727227 1384078NM VERTICAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A C-CHECK, THE FOLLOWING DISCREPANCY WAS NOTED: VERT STAB FIN STA 133 AT STR 8 LT HAS 1 FRAME CLIP CRACKED. REMOVED FRAME CLIP AT VERT STAB FIN STA 133 AT STR 8 LT IAW B727 SRM 51-30-2. FABRICATED NEW CLIP MATERIAL USED 7075T6 .050 PO NR 9001777 DIM 7/8 INCH BY 2.5 INCH BY 5.5 INCH IAW B727 SRM 55-30-2 FIG 2 AND 51-20-1 FIG 7. TREATED AND PRIMED CLIP IAW B727 SRM 51-10-2. INSTALLED FRAME CLIP IAW B727 SRM 51-30-2. 2L73 4F A3WE 20050427000542005042700054NM 2005 4 27 DHL2005781560 120050224A5531 CLIP BOEING727 727227 1384078NM VERTICAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING C-CHECK, VERT STAB FIN STA 157 AT STR 9 LT HAS 2 FRAME CLIPS CRACKED. REMOVED FRAME CLIP BS 157 STR 9 LT IAW B727 SRM 51-30-2. FABRICATED (2 EA) FRAME CLIP MATERIAL USED 7075T6 .050 PO NR 9001777 DIM .750 BY 2.50 BY 5 INCHES IAW B727 SRM 55-30-2 FIG 2 AND 51-20-1 FIG 7. TREATED AND PRIMED CLIP IAW B727 SRM 51-10-2. INSTALLED FRAME CLIP BS 157 TO STR NR 9 LT IAW B727 SRM 51-30-2. 2L73 4F A3WE 20050427000612005042700061EU 2005 4 27 TXER099790 120050303A2435524031 STARTER GEN UROCOPEC155 EC155B 8681000EU ENGINE INOPERATIVE B TXERO OTHER O OTHER NRNOT REPORTED 1 SW09155EW596 6660 STARTER GEN WILL NOT MAINTAIN VOLTAGE / AMPS AT LOAD. 1G72 3U H10EU 20050427001362005042700136WP 2005 4 27 XV62005F00002 220050214A72618941172 ADAPTER DORNERDO228 DO228202 2992030EU GARRTTTPE331TPE33110T WP NR 2 ENG OIL FILCRACKED E XV6AK NONE O OTHER ININSP/MAINT 1 WP19405VA 2664 8144 P101261C OIL FILTER ADAPTER CRACKED AT MOUNTING PLATE. (WP19200505213) (K) 2H72 4T4 TRTA16EU E4WE 20050427001382005042700138SW 2005 4 27 YTRR099951 120050322A6420206011810153 HUB BELL 206 206B3 1181506SW TAIL ROTOR LOOSE B YTRAO OTHER O OTHER NRNOT REPORTED 1 SW09209RA455 2091 TAIL ROTOR HUB ASS'Y TRUNNION WAS FOUND LOOSE IN THE PILLOW BLOCKS. ON INSPECTION FOUND THE THRUST PLUGS COMPRESSED. TAIL ROTOR HUB ASS'Y WAS PURCHASED NEW. 1G71 3U H2SW 20050427001392005042700139SW 2005 4 27 YTRR099952 120050322A6210206010200133 BLADE BELL 206 206B3 1181506SW MAIN ROTOR DELAMINATED B YTRAO OTHER O OTHER NRNOT REPORTED 1 SW09209RA455 2091 ON ROUTINE INSPECTION FOUND THE 5TH FINGER FROM THE ROOT END DELAMINATED APPROXIMATLEY 1 - 2 INCHES. BLADE RETURNED TO BHT FOR INSPECTION 1G71 3U H2SW 20050427001402005042700140SW 2005 4 27 AC2A099569 120050308A2842427366101101 PROBE BELL 427 427 1182207SW FUEL QTY MALFUNCTIONED B AC2AO OTHER S AFFECT SYSTEMS CRCRUISE 1 SO07427CK231 56043 PROBE GIVING ERRATIC FUEL QUANTITY READINGS 1G71 3U R00001RC 20050427001412005042700141SW 2005 4 27 AC2A099570 120050308A3246427036123101 SKID SHOE BELL 427 427 1182207SW MLG BENT B AC2AK NONE O OTHER ININSP/MAINT 1 SO07427CK232 56043 SKID SHOES WERE BENT AND DEFORMED DUE TO NORMAL USAGE. 1G71 3U R00001RC 20050427001422005042700142CE 2005 4 27 20030809 120050325A5330 SKIN BEECH 1900 1900D 1154162CE FUSELAGE CORRODED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03153GL UE153 DURING ROUTINE INSPECTION, UNDER FUSELAGE SKIN CORROSION WAS FOUND WHERE SKIN BONDS TO AIRCRAFT STRUCTURE FS 243-249 AT STRINGER 16, WL75. ALL AFFECTED SKIN AND CORROSION WAS REMOVED AND REPAIRED PER EO. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA24CE 20050427002422005042700242EA 2005 4 27 QXEA200500437 120050226A1430 RIVET CNDAIRCL600 CL6002C10 1390015EA ZONE 200 LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - FUSELAGE EXTERIOR HAS LOOSE RIVETS AT FS800 BETWEEN STRINGER 16 LT AND STRINGER 17 LT, AT WING TO BODY FAIRING ATTACH. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20050427002492005042700249EA 2005 4 27 QXEA200500449 120050304A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - RIGHT HAND INBOARD SEAT RAIL AT STATION X399 HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01 AND REO 670-53-00-013. 2L72 4F RTA21EA 20050427002502005042700250EA 2005 4 27 QXEA200500447 120050304A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - RIGHT HAND INBOARD SEAT RAIL AT STATION X350 TO X355 HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01 REO 670-53-00-013. 2L72 4F RTA21EA 20050427002512005042700251EA 2005 4 27 QXEA200500445 120050304A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - RIGHT HAND OUTBOARD SEAT RAIL AT STATION X421 TO X426 HAS PITTING CORROSION ON MOST INBOARD SURFACE. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01 AND REO 670-53-00-013. 2L72 4F RTA21EA 20050427002522005042700252EA 2005 4 27 QXEA200500453 120050303A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - RIGHT HAND INBOARD SEAT RAIL AT STATION X603 HAS PITTING CORROSION ON TOP SURFACE. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01 AND HORIZON AIR EA R-53-285. 2L72 4F RTA21EA 20050427002532005042700253EA 2005 4 27 QXEA200500450 120050304A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - RIGHT HAND INBOARD SEAT RAIL AT STATION X430 HAS PITTING CORROSION AND WEARING MARKS ON TOP AND INSIDE SURFACES. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01 AND REO 670-53-00-013. 2L72 4F RTA21EA 20050427002542005042700254EA 2005 4 27 QXEA200500456 120050303A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - LEFT HAND INBOARD SEAT RAIL AT STATION X461 HAS PITTING CORROSION ON TOP SURFACE. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01 AND HORIZON AIR EA R-53-282. 2L72 4F RTA21EA 20050427002582005042700258EA 2005 4 27 QXEA200500462 120050303A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - FUSELAGE EXTERNAL BELLY SKIN HAS A GOUGE FROM FAIRING SCREW AT FS 983 AND LBL 1.5 AND A DAMAGED HILITE FASTENER AT STRINGER 27. REPAIRED IAW REO 670-53-61-155 AND HORIZON AIR EA R-53-284. 2L72 4F RTA21EA 20050427002632005042700263EA 2005 4 27 VTZA200500029 120050328A5320601R311719 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27657BR 7491 INTERCOSTAL CRACKED AT .25 INCH IN LENGTH ON RT OUTBD SIDE AT FS 484 BETWEEN RBL 27.00. 2L72 4F RTA21EA 20050427002642005042700264EA 2005 4 27 QXEA200500517 120050301A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - FUSELAGE INTERIOR FS 280 BULKHEAD LEFT HAND LOWER WEB IS CORRODED AT FLOOR LEVEL. REPAIRED IAW REO 670-53-11-052. 2L72 4F RTA21EA 20050427002652005042700265EA 2005 4 27 QXEA200500481 120050228A5753 ACCESS PANEL CNDAIRCL600 CL6002C10 1390015EA ZONE 600 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - RIGHT HAND INBOARD FLAP LOWER ACCESS PANEL 684BB HAS CHAFFED MARK FROM HINGE FAIRING. REPAIRED IAW CRJ700 SRM 51-25-01-001-001-A01 AND SRM 57-52-01-101-001-A01. 2L72 4F RTA21EA 20050427002662005042700266EA 2005 4 27 QXEA200500482 120050305A5313 STRINGER CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - FUSELAGE INTERIOR STRINGER AT FS 280 TO FS 333 STRINGER 25R HAS SEVERAL SPOTS OF CORROSION ALONG RIVET ROW. REPAIRED IAW CRJ700 SRM 53-21-03-101-002-AA1, SRM 51-42-06-001-001-A01, AND SRM 51-42-21-001-001-A01. 2L72 4F RTA21EA 20050427002672005042700267EA 2005 4 27 QXEA200500476 120050303A5414 PANEL CNDAIRCL600 CL6002C10 1390015EA ZONE 400 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - LEFT HAND PYLON PANEL 412JB END EDGE HAS CHAFE MARK. REPAIRED IAW CRJ700 SRM 51-21-16-001-001-A01, REO 670-54-52-013 AND HORIZON AIR EA R-54-76. 2L72 4F RTA21EA 20050427002682005042700268EA 2005 4 27 QXEA200500513 120050226A5414 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 400 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - LEFT HAND NACELLE AFT CORE COWL SCRATCHED ON OUTBOARD SIDE. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01, SRM 54-13-00-101-001-A01, AND SRM 51-21-11-001-001-A01. 2L72 4F RTA21EA 20050427002692005042700269EA 2005 4 27 QXEA200500515 120050301A5310 CROSSBEAM CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - FUSELAGE INTERIOR FLOOR SUPPORT CROSSBEAM AT FS280 IS CORRODED. REPAIRED IAW REO 670-53-11-047. 2L72 4F RTA21EA 20050427002702005042700270EA 2005 4 27 QXEA200500474 120050302A5753 VANE CNDAIRCL600 CL6002C10 1390015EA ZONE 500 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - LEFT HAND WING INBOARD FLAP VANE HAS CHAFFED MARK AT LEADING EDGE MID SECTION. REPAIRED IAW CRJ700 SRM 57-52-02-101-001-A01 AND SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050427002722005042700272EA 2005 4 27 QXEA200500519 120050226A5755 FASTENER CNDAIRCL600 CL6002C10 1390015EA ZONE 600 LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - RIGHT HAND WING UPPER SURFACE TRAILING EDGE HAS LOOSE FASTENERS AT STATION WS 170 INBOARD OF MULTIFUNCTION SPOILERS. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01, SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050427002742005042700274EA 2005 4 27 QXEA200500521 120050303A5753 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 600 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - RIGHT HAND FLAP LOWER SURFACE INBOARD HINGE AREA HAS CHAFED MARKS FROM FAIRING. REPAIRED IAW CRJ700 SRM 57-52-01-101-001-A01, SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050427003432005042700343NM 2005 4 27 BB05015 120050314A3397 CONNECTOR BOEING767 7672B7 1385107NM ROWS 27 AND 29 DISCONNECTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19653US 24894 MAN - FOUND FLOOR EMERGENCY LIGHTING INOPERATIVE AFT FROM ROW 27 RIGHT. MAINTENANCE FOUND THE LIGHTING CABLE DISCONNECTED AT SEATS 27FG AND 29FG. CABLE WAS RECONNECTED. 2L72 4F RTA1NM 20050427003442005042700344EU 2005 4 27 SA05027 120050312A3260848401 PROXIMITY SENSOR AIRBUSA319 A319112 3930323EU LT MLG FAILED A USAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19767UW 1382 CLT FL 319 - AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT. CREW CYCLED THE GEAR, AND THE GEAR RETRACTED. DURING THE SUBSEQUENT RADIO REPORT TO COMPANY MAINTENANCE, THE AIRCRAFT EXPERIENCED OTHER NON-GEAR RELATED DIFFICULTIES. THE FLIGHT RETURNED TO CLT FOR MAINTENANCE CONSIDERATIONS. MAINTENANCE REPLACED THE 23GA PROXIMITY SENSOR ON THE LEFT MAIN LANDING GEAR. 2L72 4F RTA28NM 20050427003582005042700358EA 2005 4 27 QXEA200500550 120050316A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE INTERIOR, FUSELAGE STATION 280 BULKHEAD LEFTHAND LOWER WEB IS CORRODED ALONG THE FLOOR CROSSBEAM. REPAIRED IAW REO 670-53-110-052, REV A. 2L72 4F RTA21EA 20050427003652005042700365NM 2005 4 27 QXEA200500679 120050401A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09367PH 511 PDX - LEFTHAND INBOARD SEAT TRACK HAS 12 FT LONG CHAFE MARK INSIDE CHANNEL AT STATION X473. REPAIRED IAW RD 8-53-1339. 2H72 4T RTA13NM 20050427003732005042700373NM 2005 4 27 QXEA200500699 120050413A5753 SKIN DHAV DHC8 DHC8202 2809007NM T/E FLAP CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - RIGHTHAND WING, OUTBOARD FLAP, CHAFE ON TOP SURFACE STARTING 32.5 INCH FROM INBOARD END AND RUNNING OUTBOARD TO 83.5 INCH FROM INBOARD END. REPAIRED IAW RD 8-57-1022. 2H72 4T RTA13NM 20050427003842005042700384 2005 4 27 QXEA200500697 420050413A3445 STRUCTURE DHAV DHC8 DHC8202 2809007NM TCAS ANTENNA CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - EVIDENCE OF CORROSION AT THE FORWARD RIGHTHAND FASTENER HOLE OF THE UPPER TCAS ANTENNA. REPAIRED IAW DHC-8 200 SRM 51-20-16. 2H72 4T RTA13NM 20050427003912005042700391NM 2005 4 27 QXEA200500703 120050413A5711 SPAR DHAV DHC8 DHC8202 2809007NM LT WING CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - LEFTHAND WING FORWARD SPAR LOWER FLANGE IS CHAFED AT WING STATION YW 48.000. REPAIRED IAW RD 8-57-811. 2H72 4T RTA13NM 20050427003932005042700393NM 2005 4 27 QXEA200500694 120050413A5551 FITTING DHAV DHC8 DHC8202 2809007NM HORIZ STAB SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - HORIZONTAL STABILIZER LEFT HAND AND RIGHT HAND FORWARD ATTACH POINT LUGS ARE SCRATCHED ALONG OUTBOARD FACES. REPAIRED IAW RD 8-55-847. 2H72 4T RTA13NM 20050427003952005042700395NM 2005 4 27 QXEA200500691 120050413A5320 SILL DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - MAIN CABIN DOOR SILL CORRODED ON BOTTOM AROUND NUT PLATES. REPAIRED IAW DHC-8 200 SRM 51-40-00 AND SRM 51-40-11. 2H72 4T RTA13NM 20050427004062005042700406EA 2005 4 27 QXEA200500597 120050317A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE INTERIOR, RIGHTHAND OUTBOARD SEAT RAIL AT STATION X785, HAS PITTING CORROSION ON MOST INBOARD SURFACE. REPAIRED IAW CRJ700/900 SRM 51-21-06-001-001-A01, PARAGRAPH 3E, REO 670-53-00-013 AND CRJ700 SRM 51-21-16, CODE A044. 2L72 4F RTA21EA 20050427004112005042700411EA 2005 4 27 QXEA200500569 120050321A5420 STRUCTURE CNDAIRCL600 CL6002C10 1390015EA RT NACELLE SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - RIGHTHAND NACELLE, AFT CORE COWL SCRATCHED ON OUTBOARD. REPAIRED IAW CRJ700 SRM 51-21-11-001-001-A01. 2L72 4F RTA21EA 20050427004242005042700424EA 2005 4 27 QXEA200500629 120050322A5320 STRIKER CNDAIRCL600 CL6002C10 1390015EA FUSELAGE GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE PASSENGER DOOR SEAL STRIKE GOUGED BESIDE FORWARD TOP PRESSURE STOP. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01, SRM 51-21-16-001-001-A01 AND SRM 53-21-23-101-001-A01. 2L72 4F RTA21EA 20050427004312005042700431NM 2005 4 27 QXEA200500673 120050412A5230 SKIN DHAV DHC8 DHC8202 2809007NM CARGO DOOR GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - CARGO DOOR INNER SKIN GOUGED AT SCREW HOLE UPPER FORWARD CORNER X554, Z151. REPAIRED IAW DHC-8 200 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20050427004322005042700432NM 2005 4 27 QXEA200500664 120050410A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - LEFTHAND INBOARD SEAT TRACK HAS SURFACE CORROSION BETWEEN STATION 201.0 AND 222.7. REPLACED NR 4 SEAT TRACK. 2H72 4T RTA13NM 20050427004342005042700434EA 2005 4 27 QXEA200500565 120050326A7110 TORQUE BOX CNDAIRCL600 CL6002C10 1390015EA RT COWLING CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - RIGHTHAND ENGINE LOWER FAN COWL HAS CHAFE DAMAGE IN THE TORQUE BOX AT THE 4 O'CLOCK AND 7 O'CLOCK POSITIONS. REPAIRED IAW REO 670-78-34-355 AND HORIZON AIR EA R-78-31. 2L72 4F RTA21EA 20050427004482005042700448EA 2005 4 27 QXEA200500608 120050317A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE INTERIOR, RIGHTHAND INBOARD SEAT RAIL AT STATION X616 HAS PITTING CORROSION ON TOP SURFACE. REPAIRED IAW CRJ700/900 SRM 51-21-06-001-001-A01, PARAGRAPH 3E, REO 670-53-00-013 AND CRJ700 SRM 51-21-16, CODE A044. 2L72 4F RTA21EA 20050428000072005042800007EU 2005 4 28 05FDEA00534 120050315A5522 SKIN AIRBUS310 A310222 3930315EU RT ELEVATOR MISREPAIRED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25451FE 303 COMPLY WITH AGING 9 - AGING INSPECTION, HORIZONTAL STAB - REPAIR AT RT ELEVATOR INBOARD TRAILING EDGE. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 55-21-11. 2L72 4F RTA35EU 20050428000142005042800014NM 2005 4 28 05FDEA00605 120050318A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 CORROSION ON SKIN BS 698 BETWEEN STRINGERS 28 LT & 28 RT. REPAIRED SKIN AT BS 698 BETWEEN STRINGERS 28 LT AND 29 RT PER SRM 53-30-3. 2L73 4F RTA3WE 20050428000182005042800018EU 2005 4 28 2005UALA00237 120050311A2133VFT300 OUTFLOW VALVE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CABIN PRESSURE OUT OF ADJUST A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29442UA 780 UNABLE TO PRESSURIZE THE CABIN. PFR SHOWED THE AVIONICS SKIN AIR OUTLET VALVE FAILED. ADJUSTED VALVE DOOR 3 QUARTER TURN TO FULL OPEN STOP. 2L72 4F4 FRTA28NM E40NE 20050428000332005042800033WP 2005 4 28 05FDEA00873 120050406A3411 PITOT TUBE DOUG MD10 MD1010F 3022112WP NR 1 CLOGGED A FDEAA UNSCHED LANDING GS MULTIPLE FAILURE AFFECT SYSTEMS TOTAKEOFF 1 SO25383FE 46616 ON TAKEOFF ROTATION CADC NR 1 FAILURE, LOST CAPT A/S, ALT, F/D, AP, ATS. COMPLIED WITH QRH. REPEAT WRITE UP. CONFIRMED NR 1 PITOT TUBE WAS CLOGGED FOUND WATER PITOT TUBES AND DRAIN HOLES CLOGGED. ALSO PURGED PITOT SYSTEM IAW MD-10 MM 34-11-00. SYSTEM OP'S CHECKS GOOD IAW MD-10 MM 34-11-00, NO FAULTS NOTED. 2L73 4F RTA22WE 20050428000412005042800041NM 2005 4 28 05FDEA00886 120050407A5411 SPAR CAP DOUG MD11 MD11 3023602NM NR 2 PYLON CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 NACELLES/PYLONS - PYLON STRUCTURE - CRACK ON NR 2 ENGINE PYLON UPPER SPAR CAP COMPLY WITH EA 1-5450-76453. COMPLIED NR 2 ENG UPPER SPAR REPAIR PER EA 1-5450-81683. 2L73 4F RTA22WE 20050428000582005042800058NM 2005 4 28 05FDEA00904 120050408A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 RIGHT WING O/B FLAP MOUNTED HINGE ACTUATOR HOLE EVIDENT OF CORROSION. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F RTA22WE 20050428000622005042800062NM 2005 4 28 05FDEA00908 120050408A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 LT WING O/B FLAP, O/B FLAP MOUNTED HINGE PIVOT HOLE EVIDENT OF CORROSION. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F RTA22WE 20050428000632005042800063NM 2005 4 28 05FDEA00909 120050408A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 LEFT WING O/B FLAP, O/B FLAP MOUNTED HINGE ACTUATOR HOLE EVIDENT OF CORROSION. CORROSION REMOVED AS PERCMM 20-11-02. 2L73 4F RTA22WE 20050428000662005042800066SO 2005 4 28 CHQA200500072 120050405A33503025103 LIGHT EMB 145 EMB145LR 3260212SO EXTERIOR INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11273SK 145331 THE RIGHT OVERWING EMERGENCY EXIT LIGHT IS INOPERATIVE. REMOVED AND REPLACED RIGHT HAND REAR EXTERNAL EMERGENCY EXIT LIGHT IAW EMB 145 AMM 33-50-10. OPS CHECK OF EMERGENCY LIGHTS IS GOOD. 2L72 4T RTT00011AT 20050428000682005042800068SO 2005 4 28 CHQA200500074 120050407A2611FDS765A2 SMOKE DETECTOR EMB 135 EMB135KL 3260302SO LAVATORY FAULTY A CHQAH DEACTIVATE SYST/CIRCUITS N FALSE WARNING CLCLIMB 1 GL11373SK 145543 LAV SMOKE TRIPLE CHIME AND EICAS MESSAGE WHILE CLIMBING THROUGH 7,800 FEET. REFERENCED QRH AND PULLED CB E11 AND E12, MESSAGE WENT AWAY BEFORE PULLING THE CIRCUIT BREAKERS. FLIGHT ATTENDANT REPORTED NO SIGNS OF SMOKE OR FIRE. MAINTENANCE REMOVED AND REPLACED THE LAVATORY SMOKE DETECTOR. PERFORMED LAV SMOKE DETECTION SYSTEM TEST. OPS CHECK GOOD IAW EMB 140 AMM 26-14-00. 2L72 4F RTT00011AT 20050428000712005042800071SO 2005 4 28 MASA200500184 120050305A3610S2U226 COUPLING EMB 145 EMB145LR 3260212SO CARGO BAY BLOWN A MASAFA ACTIVATE FIRE EXT. UNSCHED LANDING JS WARNING INDICATION AFFECT SYSTEMS CRCRUISE 1 SW07851MJ 145572 LOUD BANG IN FLIGHT. CREW RETURNED TO THE FIELD AND REPORTED A LOUD BANG IN THE AFT AREA OF THE AIRCRAFT, A BAGGAGE SMOKE INDICATION AND F/O SIDE HAS NO VOR OR LOCALIZER INDICATION. CREW BLEW THE CARGO FIRE BOTTLE IN RESPONSE TO THE SMOKE DETECTION. CONTRACT MX OPENED THE CARGO COMPARTMENT FLOORBOARDS AND REPORTED THE FORWARD COUPLING AREA WAS BLOWN AND A FLIGHT CONTROL PULLEY WAS MELTED. INSPECTED THE VOR COAX CABLE BUT SAW NO VISIBLE EVIDENCE OF DAMAGE BUT BELIEVED IT TO BE HEAT DAMAGED AS WELL. MOST LIKELY STRATEGY IS TO REPAIR THE PULLEY AND BLEED DUCT AND PREPARE THE AIRCRAFT FOR FERRY TO CLT. MX REPLACED O-RING AND RECONNECTED COUPLING, LEAK CHECK GOOD. 2L72 4T RTT00011AT 20050428000732005042800073SO 2005 4 28 MASA200500234 120050319A49204501968C APU EMB 145 EMB145LR 3260212SO APU BAY FAILED A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW07827MJ7312 145217 SMOKE IN THE CABIN PRIOR TO THE FIRST FLIGHT OF THE DAY. MX TROUBLESHOT FAULT AND OPERATED ENG NR 2 WITH BOTH PACKS AND FOUND THAT THE SMOKE WAS CAUSED BY THE APU. MX RE-OPENED THE MEL FOR THE APU 3/23/05. MAINTENANCE REPLACED THE APU. 2L72 4T RTT00011AT 20050428000752005042800075SO 2005 4 28 MASA200500256 120050325A27503631001009 CONTROL UNIT EMB 145 EMB145LR 3260212SO T/E FLAP FAILED A MASAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TOTAKEOFF 1 SW07860MJ3084 145773 A FLAP HALF SPEED ON TAKEOFF. FLIGHT CREW CONTINUED TO CLT. CHANNEL 1 C/B POPPED AND WOULD NOT RESET CAUSING AN SPS ADVANCE CAUTION MESSAGE WHICH DEFERRAL OF THE FLAP SYSTEM. MAINTENANCE REPLACED THE FLAP ELECTRONIC CONTROL UNIT. NO FURTHER DEFECTS NOTED. 2L72 4T RTT00011AT 20050428000772005042800077CE 2005 4 28 DXTA200500666 120050330A2750NPN FLAP RAYTHNDH125 HAWKER800XP 7150012CE WING MALFUNCTIONED E DXTAA UNSCHED LANDING O OTHER APAPPROACH 1 GL07873QS 258573 FLAPS STOPPED MOVING AT APPROX 5 DEGREE POSITION (BOTH SIDES AT 5 DEGREE) DURING APPROACH INTO RIL WITH INTERMITTENT LIGHT ICING CONDITION, THEN WOULD NOT EXTEND FURTHER NOR RETRACT. FLAPS RETRACTED BY THEMSELVES AFTER LANDING. LEVER POSITION WAS 0 DEGREES, CYCLED FLAPS THROUGH FULL TRAVEL 20 TIMES. COULD NOT DUPLICATE SQK. FLAPS OPS CHECKED GOOD IAW HAWKER 800XP MM CH 27-50-02. 2L72 4F RTA3EU 20050428000792005042800079 2005 4 28 DXTA200500667 420050408A22107003974729 AUTOPILOT SYS CESSNA650 650 2076802CE COCKPIT MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL07795QS 6507095 WHEN AUTOPILOT A-SIDE ENGAGED SYSTEM FLAGGED FAIL CYCLED TO B-SIDE, AND DEFECTED RIGHT RUDDER INPUTS RUDDER INPUTS BECAME INCREASINGLY AGGRESSIVE PIC AND SIC COMMAND BARS SHOWED 2-3 DEGREES TO BANK DISAGREEMENT. RAN AUTOPILOT TEST IAW CE650 MM 22-10-00; NO DEFECTS NOTED. PERFORMED GROUND CHECK OF THE SPZ-8000 SYSTEM IAW HONEYWELL TECH PUB A15-1146-058 CHAPTER 22-05-07, FOUND NO ERRORS. NO FAULTS STORED IN FLIGHT FAULT SUMMARY. SWAPPED FGC'S & PERFORMED OPS CHECKS. OPS CHECKED GOOD PER ABOVE REFERENCES. 2L72 4F A9NM 20050428000812005042800081NM 2005 4 28 72300151 120050408A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 6 X 3 INCH AREA OF CORROSION ON STRINGER. 2L73 4F4 FRTA3WE E2EA 20050428000832005042800083NM 2005 4 28 72300153 120050408A5311 FRAME BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE DAMAGED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 DAMAGED FASTENER HOLES IN UPPER CHORD. 2L73 4F4 FRTA3WE E2EA 20050428000862005042800086NM 2005 4 28 05FDEA00642 120050325A5322 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 REPAIR SHEAR TIE BS 380 BETWEEN STR 15L & 16L TO ACCOMPLISH 9G MOD. REPAIRED SHEAR TIE AT BS 380 BETWEEN STR 15L & 16L PER SRM 53-10-4. 2L73 4F RTA3WE 20050428000882005042800088NM 2005 4 28 05FDEA00644 120050325A575365192507 FLAP TRACK BOEING727 727200 138407ENM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 NR 1 FLAP TRACK FWD I/B ATTACH LUG CORRODED. REPLACED PER FED EX W/C 27X5707-03. 2L73 4F RTA3WE 20050428000902005042800090NM 2005 4 28 05FDEA00662 120050328A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25272FE 22037 EXTERNAL FUSELAGE SKIN HAS FOD/GRAVEL DAMAGE, BS 480-520, STR 22R-27L ALONG BELLY SKIN. RVSM CRITICAL AREA. REPAIRED SKIN BS 496-501 AT STR 27R PER SRM 53-30-3. 2L73 4F RTA3WE 20050428000912005042800091 2005 4 28 ASAA04801AA 420050216A25653961896501 LANYARD DOUG DC9 DC983 3022083WP L1 DOOR SLIDE DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM02977AS 53453 SEA - PREFLIGHT CHECK, FORWARD PAX L1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M) 2L72 4F RTA6WE 20050428000962005042800096NM 2005 4 28 05FDEA00716 120050330A7830683L221G04 SLIDING SLEEVE DOUG MD11 MD11 3023602NM ZONE 400 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 NR 2 ENGINE RIGHT THRUST REVERSER COWL UPPER SLIDER TRACK END CRACKED. THRUST REVERSER COWL REMOVED AS PER FEDEX WORKCARD 78T3002-R AND REPLACED AS PER FEDEX WORKCARD 78T3902-R. 2L73 4F RTA22WE 20050428000982005042800098NM 2005 4 28 BB05027 120050401A33501000679 LIGHT BOEING767 7672B7 1385107NM COCKPIT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19656US 26847 FOUND FLIGHT DECK EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. 2L72 4F RTA1NM 20050428001002005042800100NM 2005 4 28 AWXA200500434 120050408A2560P4010021 BATTERY BOEING737 7373G7 1384595NM FLASHLIGHT DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28322AW 25400 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050428001032005042800103NM 2005 4 28 05FDEA00768 120050329A5740NRC6753503 FLAP DOUG MD11 MD11 3023602NM ZONE 500 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE47889 48420 LEFTHAND OUTBOARD FLAP; INBOARD HINGE ATTACH FITTING HAS 2.25 INCH CRACK ADJACENT TO ATTACH POINT. ACCESSED THRU PANEL 557GT. REMOVED & INSTALLED NEW FLAP P/N NRC6753-503,S/N LS0205 IAW MM 27-50-30-4. CHECKED & ADJUSTED O/B FLAP & VANE INW MM 27-50-32/27-50-30. REFER N/R N00150. 2L73 4F RTA22WE 20050428001122005042800112NM 2005 4 28 AWXA200500444 120050405A5411BAC312N582712 SPAR BOEING757 7572S7 1384962NM NR 2 PYLON CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28901AW 23321 SAL - MAJOR REPAIR - DURING ACCOMPLISHMENT OF SB 757-54A0039 A 1.375 INCH CRACK WAS FOUND ON NR 2 ENGINE PYLON UPPER SPAR WEB. MAINTENANCE STOP DRILLED CRACK ON NR 2 ENGINE PYLON UPPER SPAR WEB; PERFORMED HFEC INSPECTION TO VERIFY CRACK CONTAINED; FABRICATED 2 EACH DOUBLERS; INSTALLED REPAIR PARTS IAW ER 19-5450-05099-HF2. 2L72 4F RTA2NM 20050428001152005042800115NM 2005 4 28 DL76G050171 120050318A2421 IDG BOEING767 767332 1382001NM RT ENGINE FAILED A DALAC ABORTED TAKEOFF HJ ELECT. POWER LOSS-50 PC WARNING INDICATION TOTAKEOFF 1 SO271609 30574 T/O ABORT AT 70 KTS FOR RT GEN DRIVE LIGHT EICAS MSG. REPLACED IDG. 2L72 4F RTA1NM 20050428001182005042800118NM 2005 4 28 DLM88050173 120050318A2421249001278 GENERATOR DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 ENGINE FAILED A DALAK NONE O OTHER CRCRUISE 1 SO27911DE 49967 718104 NUMBER 2 ENGINE GENERATOR FAILED IN FLIGHT. REPLACED GENERATOR AND CSD. 2L72 4F4 FRTA6WE E9NE 20050428001262005042800126NM 2005 4 28 DL757050179 120050321A5753113N200346 SPAR BOEING757 757232 1384965NM RT T/E FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27670DN 25331 DURING SHOP VISIT, IMPACT DAMAGE WAS FOUND ON THE RT INBOARD MAIN FLAP. THE IMPACT CAUSED DAMAGE TO THE REAR SPAR LOWER CHORD, WHICH WAS SPLICE REPAIRED BETWEEN STA 117 AND 127. REPAIRED PER DELTA ERA 097596-14. 2L72 4F RTA2NM 20050428001272005042800127NM 2005 4 28 DL73S050180 120050322A2710654476115 PCU BOEING737 737232 1384475NM AILERON MALFUNCTIONED A DALAB EMER. DESCENT K FLUID LOSS APAPPROACH 1 SO27303DL 23075 AFTER MOVING FLAPS TO 5 DEGREES SYS-A HYD QTY DROPPED TO ZERO. REPLACED LOWER A-SYSTEM AILERON PCU FOR LEAKING. 2L72 4F RTA16WE 20050428001292005042800129NM 2005 4 28 DLM90050182 120050319A2530259002018 OVEN DOUG MD90 MD9030 3023690NM FWD GALLEY MALFUNCTIONED A DALAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27911DA 53391 FORWARD GALLEY OVEN SMOKED WHEN TURNED ON. SMOKE DISSIPATED WHEN OVEN WAS SELECTED OFF. REPLACED OVEN. 2L72 4F RTA6WE 20050428001312005042800131NM 2005 4 28 DL76L050184 120050322A2120 ODOR BOEING767 767332 1382001NM LAVATORY DETECTED A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27171DN 24759 SMELLED SMOKE/ELECTRICAL BURNING SMELL IN 2L LAVATORY. INSPECTED LAV AREA, NO DEFECTS FOUND. 2L72 4F RTA1NM 20050428001332005042800133NM 2005 4 28 DLM88050186 120050323A3150 WARNING SYSTEM DOUG MD88 MD88 3023688NM COCKPIT MALFUNCTIONED A DALAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO27909DL 49540 DISCONTINUED TAKEOFF, TAKEOFF WARNING. ALL CHECKED GOOD. CONTACTED MTC, CYCLED FLAPS, NO WARNING FLAPS. SYSTEM CHECKS OK. NO TROUBLE FOUND. CLEANED FLAP THUMBWHEEL POSITION SWITCH S1-492 AS PRECAUTION. 2L72 4F RTA6WE 20050428001362005042800136 2005 4 28 DL764050189 420050326A23301301851100 MONITOR BOEING767 767432ER 1385134NM CABIN MALFUNCTIONED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO27833MH 29706 PRIOR TO BOARDING, ELECTRICAL SMELL AND SLIGHT SMOKE IN CABIN. MID CABIN MORE PREVALENT OF SMOKE. REPLACED MONITOR. 2L72 4F RTA1NM 20050428001382005042800138NM 2005 4 28 DL764050192 120050326A2120 ODOR BOEING767 767432ER 1385134NM CABIN/COCKPIT DETECTED A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO27831MH 29702 ON DESCENT AFTER ADDING POWER FROM IDLE A BURNING SMELL LIKE BURNING POPCORN / RUBBER WAS NOTICED IN THE COCKPIT. AFTER LANDING GOING FROM IDLE TO REVERSE THE SMELL RETURNED AND WAS ALSO NOTICED IN FIRST CLASS BUT NOT IN THE MAIN CABIN. INSPECTED ENG INLETS FOR OIL. NO OIL FOUND. OIL CONSUMPTION WITHIN LIMITS. RAN APU PNEUMATICS AND PACKS. NO SMELLS NOTED. IFE SYSTEM ON AND NO SMELLS OR STATUS MSG. OPERATED GALLEY EQUIPMENT, NO SMELLS NOTED. 2L72 4F RTA1NM 20050429000012005042900001NM 2005 4 29 05FDEA00834 120050404A5340 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25272FE 22037 CORROSION C53-113-01 (1) UNDER LEVELING COMPOUND BS 660 STR 28R. FOUND CORROSION TO BE 100 PERCENT MATERIAL LOSS, REPAIRED DOUBLER, SHEAR TIE PER SRM 53-10-4, 53-30-3. 2L73 4F RTA3WE 20050429000022005042900002NE 2005 4 29 05FDEA00848 220050405A7323 ENGINE BOEING727 7272S2F 1384O81NM PWA JT8 JT8D17 52049NE NR 1 MALFUNCTIONED A FDEAE ENGINE SHUTDOWN O OTHER DEDESCENT 1 SO25205FE15252 22927 726133 DURING DESCENT FOR APPROACH FROM 8000-4000 FT., REDUCED THROTTLES TO IDLE NR 1 ENG DID NOT RESPOND APPROPRIATELY. NR 1 ENG PARAMETERS WERE 1.09 EPR, N1 46.8, EGT 450, N2 72.5, FF 2000 PPH. RAN RED TABS FOR LOSS OF THROTTLE CONTROL. ENGINE WOULD ACCELERATE BUT WOULD NOT COME DOWN TO NORMAL IDLE. TAT 19.2. SHUTDOWN ENGINE IAW QRH AND LANDED. REMOVED AND REPLACED APPROACH IDLE SOLENOID VALVE PER B727-200 (JT8D-217C) NR 1 ENG. OPS CHECK GOOD, OK FOR SERVICE. 2L73 4F4 F A3WE E2EA 20050429000072005042900007 2005 4 29 AALA20050242 420050401A2220 COMPUTER BOEING737 737823 13844BZNM FLT CONTROLS INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21908AN 29510 AFTER TAKEOFF GOT MASTER CAUTION FOLLOWED BY FLIGHT CONTROL AND SPEED TRIM FAIL LIGHT AND WITH AUTO PILOT PITCH ON GOT STABILIZER OUT OF TRIM LIGHT. REPLACED FLIGHT CONTROL COMPUTER SYSTEM A. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA16WE 20050429000112005042900011NM 2005 4 29 05FDEA00878 120050406A5350AKC76055 RIB DOUG MD11 MD11 3023602NM TAIL CONE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 EMPENNAGE, EXTENDED TAIL CONE AFT INTERIOR RIB FRAME FOUND CRACKED. REMOVED PER SRM 51-35-01 VOLUME II. NEW RIB AND SPLICES FABRICATED PER DWG AKC7605 AND PART MARKED PER GMM 7-0-1001. NEW RIB AND SPLICES INSTALLED PER SRM 51-35-01 VOLUME II. 2L73 4F RTA22WE 20050429000122005042900012GL 2005 4 29 05FDEA00912 220050408A7530 ENGINE DOUG MD10 MD1010F 3022112WP GE CF6 CF66D 30020GL NR 2 STALLED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25394FE77010204 46628 451412 ENGINE NR 2 COMPRESSOR STALLS (SIGNIFICANT BANG-BANG) UPON THROTTLE REDUCTION, FL280- PERFORMANCE ENG SHUTDOWN PER QRH. 2L73 4F4 FRTA22WE E23EA 20050429000132005042900013CE 2005 4 29 DXTA200500663 120050407A2120 ODOR CESSNA750 750 2076810CE CABIN DETECTED E DXTAC ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 GL07910QS 7500110 WHITE SMOKE FILLED CABIN ON GROUND. SECURED APU BLEED AND SMOKE DISSIPATED. TURNED BLEED ON, PACS OFF. NO SMOKE, OILY ODORS. RAN ACFT & ISOLATED COCKPIT PRE & CAD PAC. WITH COCKPIT PRE RUNNING FOR SEVERAL MINUTES THERE WAS NORMAL OPS & NO OILY ODOR. WITH CAP PAC RUNNING THERE WAS A STRONG OIL ODOR. REMOVED BOTH WATER EVAPERATOR CAPS & FOUND METAL CHIPS IN CAP PAC WATER EVAPORATOR. CLEANED BOTH SOCKETS IN REF TO 750 MM. OK TO INSTALL SOCKS. INSTALLED SOCKS. & EVAPORATOR CAPS IN REF TO 750 MM. REMOVED FWD ACM IN REF TO 750 MM. OK TO INSTALL ACM 4/8 SERVICED ACM OIL LEVEL AND INSTALLED NEW ACM ON A/C IAW 750 MM. 2L72 4J RTT00007WI 20050429000142005042900014 2005 4 29 DXTA200500670 420050410A34577003110901 DISPLAY RAYTHNDH125 HAWKER800XP 7150012CE COCKPIT SHORTED E DXTAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07874QS 258474 IN FLIGHT MFD (PREVIOUSLY MEL'S) GLOWED BRIGHTLY THEN EXTINGUISHED ACCOMPANIED BY ELECTRIC SMELL IN COCKPIT. GPWS TERRAIN NOT ILLUMINATED AND NR 1 HF R/T CIRCUIT BREAKER POPPED. REMVOVED MFD UNIT AND INSTALLED REPAIRED UNIT FROM HONEYWELL, SYSTEM OPS CHECKED GOOD. 2L72 4F RTA3EU 20050502000012005050200001CE 2005 5 2 DXTA200500669 120050410A2120 ODOR CESSNA500 560CESSNA 2076750CE CABIN DETECTED E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07382QS 5600382 AIRCRAFT FREON AIR CONDITIONING INOP. FIRST OFFICER WAS SITTING IN AIRCRAFT AND NOTICED THE CABIN GETTING WARM WENT BACK TO LOOK IN THE HELL HOLE AND NOTICED A VERY STRONG ELECTRICAL SMOKE ODOR. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20050502000022005050200002NM 2005 5 2 DHL2005782501 120050310A5754 SKIN BOEING727 727227 1384078NM L/E SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 CRACK ON NR 4 SLAT SKIN AT I/B UP STOP BLOCK FASTENER. STOP DRILLED CRACK AT NR 4 SLAT SKIN AT I/B UPSTOP IAW B727 SRM 51-10-1. ACCOMPLISHED 727 HFEC INSPECTION 51-00-00 CRACK CONTIMENT CONFIRMED. FABRICATED REPAIR DOUBLER MAT USED 2024-T3 .80 DIMENSION 11 INCHES BY 5 INCHES PO NR 9001811 IAW B727 SRM 57-50-3 FIG 1. TREATED ALODINED AT DOUBLER REPAIR IAW B727 SRM 51-10-2. INSTALLED DOUBLER REPAIR IAW B727 SRM 57-50-3 FIG 1 AND 57-50-2. 2L73 4F A3WE 20050502000052005050200005EU 2005 5 2 05FDEA00756 120050331A5753 WEDGE AIRBUS310 A310 EU T/E FLAP DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 REPAIR NEEDS EVALUATION FOR FAA APPROVED DATA AND MAJOR OR MINOR CLASSIFICATION, LT WING COMPOSITE REPAIR LOWER SURFACE INBD T/E FLAP WEDGE 5 INCH FWD OF AFT EDGE AND 28 INCH O/B OF I/B EDGE. COMPLIED WITH EA6-5750-87746 PT1 NO ANOMALIES NOTED AS PER FEDEX GMM 6-2-100, FIG 1. THIS REPAIR IS CLASSIFIED AS MINOR. 2L72 4F RTA35EU 20050502000062005050200006EU 2005 5 2 05FDEA00757 120050331A5320A2557217220200 ATTACH BRACKET AIRBUS310 A310 EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 BULK CARGO COMPT, BETWEEN FR 64 AND 65 ABOUT RT STRINGER 46 FLOOR PANEL ATTACH BRACKET HAS 3 SCREW HOLE CORRODED BENEATH NUTPLATE AREA. REMOVED AND REPLACED PROFILE IAW A310-200 SRM 51-72-10. 2L72 4F RTA35EU 20050502000082005050200008EU 2005 5 2 05FDEA00759 120050331A5313 STRINGER AIRBUS310 A310 EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 BULK CARGO COMPT, JUST AFT FS 63 ON R STRINGER 53 1 AREA OF CORROSION. REMOVED DISCREPANT SECTION OF STRINGER AND REPLACED PER A310-200 SRM 51-10-14 IN BULK CARGO COMPARTMENT AFT OF FRAME 63 ON R STRINGER 53. 2L72 4F RTA35EU 20050502000112005050200011EU 2005 5 2 05FDEA00762 120050331A5320A5361087322290 STIFFENER AIRBUS310 A310 EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 AVIONICS COMPARTMENT LEFT SIDE AT FRAME 12 TO 12A AT FLOOR BOARD LEVEL, AREA HAS CORROSION APPROX 8 INCHES BY 8 INCHES ON RIBS AND STRINGER, STR 44L. REMOVED SKIN STIFFENER AT LT AVIONICS COMPARTMENT BETWEEN FR 12 AND 12A STR 44L IAW A310-200 DRAWING A536-10873. INSTALLED REPLACEMENT STIFFENER IAW A310-200 DRAWING A536-10873. 2L72 4F RTA35EU 20050502000122005050200012EU 2005 5 2 05FDEA00763 120050331A5753 STRUCTURE AIRBUS310 A310 EU T/E FLAP DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 REPAIR NEEDS EVALUATION FOR FAA APPROVED DATA AND MAJOR AND MINOR CLASSIFICATION. RT WING RT I/B T/E LOWER SURFACE AFT OF NR 2 FLAP TRACK BEAM. COMPLIED WITH EA 6-5750-87747 PART 1. NO DEFECTS NOTED PER NTM 51-10-08. REPAIR IS CLASSIFIED AS A MINOR REPAIR PER FEDEX GMM 6-2-100. 2L72 4F RTA35EU 20050502000132005050200013EU 2005 5 2 05FDEA00778 120050401A3020 ANTI-ICE VALVE AIRBUS310 A310 EU NR 2 ENGINE MALFUNCTIONED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25423FE 281 NR 2 ENG ANTI-ICE FAULT WHEN ENG NR 2 ANTI-ICE TURNED ON. PULLED AND RESET C/B. NO JOY. RELEASED FOR SERVICE PER MEL/CDL: 30-21-01-C CATEGORY: C EXPIRATION: 11APR05 "MEL 30-21-01-C: ENGINE 2 ANTI-ICE VALVE INOP. ENGINE NACELLE VALVE SECURED OPEN." NO TIME TO TROUBLESHOOT DUE TO HISTORY. ITEM DEFERRED PER MEL 30-21-01-C. 2L72 4F RTA35EU 20050502000182005050200018NM 2005 5 2 DHL2005782509 120050310A5330 SKIN BOEING727 727227 1384078NM FUSELAGE BULGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 BULGE R/SIDE FUSELAGE SKIN FWD OF STA 1050 BETWEEN STR 27R AND 26R. DAMAGED FOUND TO BE OUT OF LIMITS IAW 727 SRM 53-30-1 FIG1. CUTOUT DAMAGED AREA DIM 2 1/4 INCH BY 1 7/8 INCH IAW B727 SRM 53-30-3 FIG 3. FABRICATED DOUBLER FROM 2024T3 .071 PO NR 7001978 DIM 11 1/2 INCH BY 12 3/4 INCH AND STRUCTURAL FILLER FROM 2024T3 .063 PO NR 9001765 DIM 12 1/2 INCH BY 10 IAW B727 SRM 53-30-3 FIG24. TREATED AND PRIMED IAW B727 SRM 51-10-2 ND. INSTALLED DOUBLER AND STRUCTURAL FILLER ON FUSELAGE SKIN FWD OF STA 1050 IAW B727 SRM 53-30-3 FIG 24. 2L73 4F A3WE 20050502000202005050200020NM 2005 5 2 DHL2005782512 120050310A5330 SKIN BOEING727 727227 1384078NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 SEVERAL DENTS R/SIDE FUSELAGE SKIN WITHIN 1INCH OF AECH OTHER FWD OF STA 1263 ABOVE STR 21R. REMOVED FASTENERS FOR ACCESS AT RT SIDE FUSELAGE SKIN STA 1263 STR 21R IAW B727 SRM 51-30-2. CUT OUT DAMAGE AREA DIMENSION 1 7/8 INCH BY 3 INCHES IAW B727 SRM 53-30-3 FIG 3. FABRICATED DOUBLER REPAIR MAT USED 2024T3 .063 PO NR 9001978 DIMENSION 11 1/8 INCH BY 9 3/4 IAW B727 SRM 53-30-3 FIG 3 AND 53-30-2 FIG 3. ALODINED AND PRIMED AREA AND PART IAW B272 SRM 51-10-2. INSTALLED DOUBLER IAW B727 SRM 53-30-3 FIG 3 AND 51-30-2. 2L73 4F A3WE 20050502000222005050200022NM 2005 5 2 DHL2005782515 120050310A5330 SKIN BOEING727 727227 1384078NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 DENT R/SIDE FUSELAGE SKIN AFT OF STA 1110 ABOVE STR 20. DAMAGED FOUND TO BE OUT OF LIMITS IAW 727 SRM 53-30-1 FIG 1. REMOVED 2 EA EXISTING REPAIRS FOR INCORPORATION INTO 1 BS 1130 STR 20R CUT OUT 2 3/4 INCH BY 1 1/2 INCH BY 2 : BS 1110-1130 STR 21 CUT OUTS 3 1/4 INCH BY 1 INCH BY 1/2 DIA IAW 727 SRM 53-30-3 FIG 5. FABBED DOUBLER FROM 2024T3 .071 PO NR 900978 DIM 34 1/2 INCH BY 20 1/2: AND STRUCTURAL FILLER 2024T3 .063 PO NR 9001765 DIM 36 INCHES BY 12 3/4 INCH 3/4 INCH IAW 727 SRM 53-30-3 FIG 5 AND 53-30-2 FIG 7. REPAIR PARTS TREATED AND PRIMED AND INSTALLED IAW 727 SRM 51-10-2 AND 53-30-3 FIG 5. 2L73 4F A3WE 20050502000242005050200024NM 2005 5 2 DHL2005782518 120050310A5330 SKIN BOEING727 727227 1384078NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 DENT RT SIDE FUSELAGE SKIN FWD OF STA 480 BELOW STR 21R. DAMAGE FOUND ON PREVIOUS REPAIR FILLER AND OUT OF LIMITS IAW 727 SRM. REMOVED DAMAGED FILLER AND FABBED NEW FROM 2024T3 .040 PO NR 9001417 DIM 43.5 INCH BY 23 INCH IAW 727 SRM 53-30-2 FIG 1 AND COTNEY AEROSPACE ERES44-2 REV. IR. FILLER TREATED AND PRIMED IAW 727 SRM 51-10-2 AND INSTALLED IAW 727 SRM 51-30-2 AND COTNEY AEROSPACE ERE S44-2 REV. IR WITH 8110-3 DATED 2/20/03. THIS REPAIR IS CAT B. 2L73 4F A3WE 20050502000272005050200027CE 2005 5 2 DJFA2005074 120050313A3230 LANDING GEAR MTSBSIMU300 MU300 5780602CE NLG MALFUNCTIONED E DJFAO OTHER O OTHER CLCLIMB 1 EA23507CW A007SA KDAL - KBGM TRIP ID NR 797353 CREW REPORTED THAT AFTER GEAR RETRACTION FOLLOWING A FUEL STOP AT KLEX THE NOSE LANDING GEAR DROPPED AND LOCKED. GEAR WAS CYCLED TWO ADDITIONAL TIMES TO KEEP IT UP AND LOCKED. AIRCRAFT LANDED IN KBGM WITHOUT FURTHER INCIDENT. 2H72 4F RTA14SW 20050502000282005050200028NM 2005 5 2 P9RA20050075 120050326A56206556703 WINDOW BOEING727 727231 1384079NM CABIN CRACKED A P9RAI CABIN DEPRESSURIZATION O OTHER CRCRUISE 1 SO1154344 21631 CRUISE FLT 270, ATL-SFB. F/A CALLED FORWARD AND ADVISED A PASSENGER CABIN WINDOW AT 18A HAD CRACKED. F/E RAISED CABIN DIFFERENTIAL TO 0 PSID. CREW REQUESTED NORMAL DESCENT TO 10,000 FEET. FLIGHT CONTINUED NORMALLY TO SFB. NO PRIORITY OR EMERGENCY HANDLING REQUESTED. REMOVED AND REPLACED PASSENGER WINDOW IAW M/M. 2L73 4F A3WE 20050502000292005050200029CE 2005 5 2 DJFA2005075 120050330A3241 LINE BEECH MU300 400A 1155402CE LT & RT BRAKE REVERSED E DJFAO OTHER W INADEQUATE Q C LDLANDING 1 EA23718TA5904 RK195 KTEB - KBWI TRIP ID NR 807676 CREW REPORTED THAT WHILE ON LANDING ROLL OUT AT APPROXIMATELY 60 KTS, WHEN THE BRAKES WERE APPLIED THEY WOULD CATCH AND THE AIRCRAFT WOULD MOVE LEFT AND RIGHT OF THE CENTERLINE. WHILE AT TAXI SPEEDS THE AIRCRAFT WAS REPORTED AS HARD TO CONTROL WHEN USING THE BRAKES. MAINTENANCE FOUND THE LEFT AND RIGHT BRAKE LINES ON THE POWER BRAKE ANTI-SKID CONTROL VALVE TO BE REVERSED. THE LINES WERE CORRECTLY INSTALLED AND THE BRAKE/ANTI-SKID SYSTEM WAS BLED. BRAKING SYSTEMS OPERATIONALLY TESTED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4F RTA16SW 20050502000302005050200030NE 2005 5 2 20053 220050330A7200 ENGINE DHAV DHC8 DHC8103 1386005NM PWA 120 PW120A NE NR 2 MALFUNCTIONED A KPVAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CLCLIMB 1 WP13808WP 22 026 PCE120166 AFTER T/O APPROX 500FT AGL, NR 2 ENGINE TQ DROPPED TO 11 PERCENT, ALL OTHER INSTRUMENTS INDICATING NORMAL. ENGINE BEGAN TO SURGING AND UNABLE TO CONTROL WITH THRUST LEVERS. COMMENCED WITH ENGINE SHUTDOWN PROCEDURES. DECLARED EMERGENCY WITH APPROACH. LEVELED OFF AT 1000 FT MSL TO STAY VFR, LANDED WITHOUT INCIDENT. 2H72 4T4 TRTA13NM E20NE 20050502000312005050200031CE 2005 5 2 4502603292005 120050329A7110 COWLING LEAR 45 45LEAR 5170805CE RT ENGINE UNSECURE E J7SABA EMER. DESCENT UNSCHED LANDING WE INADEQUATE Q C VIBRATION/BUFFET CLCLIMB 1 SW05405FX 026 AFTER TAKEOFF CREW HEARD LOUD "BANG" FOLLOWED BY BUFFETING OF AIRCRAFT, AIRCRAFT CONTROL AFFECTED. ON LANDING, CREW OBSERVED ENGINE COWLING ON RT ENGINE HAD COME OFF FROM TOP/INBOARD FASTENING POSITION AND HAD BEAT ITSELF AGAINST FUSELAGE. DETERMINED THAT MX PERSONNEL FROM PREVIOUS EVENT HAD FAILED TO PROPERLY FASTEN 16 CAMLOCS AT AFFECTED POSITION. QC INADEQUATE. LOCAL FSDO HAS TAKEN APPROPRIATE ACTION AGAINST FACILITY INVOLVED. 2L72 4F RTT00008WI 20050502000332005050200033NM 2005 5 2 RYNA200500011 120050402A5210 SEAL BOEING737 737201 1384454NM L1 DOOR OUT OF ADJUST A RYNAA UNSCHED LANDING O OTHER CLCLIMB 1 CE07225US 21667 AFTER TAKEOFF FROM TUS, A LOUD SQUEAL AND PRESSURIZATION LEAK WAS DETECTED AT THE L-1 DOOR. THE AIRCRAFT WAS RETURNED TO TUS AND LANDED WITHOUT INCIDENT. ADJUSTED L-1 DOOR SEAL. LEAK CHECK GOOD DURING FLIGHT TEST. 2L72 4F A16WE 20050502000342005050200034NM 2005 5 2 SWAA051037 120050410A53306545777 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29366SW 26577 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR FWD LOWER CUTOUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050502000362005050200036NM 2005 5 2 SWAA051039 120050409A56105893543130 WINDOW BOEING737 7377H4 1384404NM COCKPIT CRACKED A SWAAK NONE B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 SW29401WN 29813 R1 COCKPIT WINDOW ARCED & OUTER PANE SHATTERED. REMOVED AND REPLACED R1 WINDOW & HEAT CONTROLLER PER MM. 2L72 4F RTA16WE 20050502000382005050200038NM 2005 5 2 SWAA051041 120050409A53306545776 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29671SW 23785 DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 940, STR 23L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050502000402005050200040NM 2005 5 2 SWAA051043 120050411A215020405011 ACM BOEING737 7373H4 1384600NM A/C BAY MALFUNCTIONED A SWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW29325SW 23689 AIR TURNBACK / DECLARED EMERGENCY. BURNING SMELL IN CABIN & COCKPIT. REMOVED AND REPLACED RT AIR CYCLE MACHINE PER MM. 2L72 4F RTA16WE 20050502000422005050200042 2005 5 2 SWAA051045 420050411A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29389SW 26592 R2 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20050502000482005050200048NM 2005 5 2 SWAA051051 120050411A57536546435 SKIN BOEING737 7377H4 1384404NM T/E FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29769SW 30588 DURING SCHEDULED 5Y CHECK, FOUND RIGHT WING INBOARD AFT T/E FLAP LOWER SURFACE DELAMINATED. REPAIRED FLAP PER SRM. 2L72 4F RTA16WE 20050502000502005050200050NM 2005 5 2 SWAA051053 120050412A53116546539 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, RBL 65, WL 202. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050502000632005050200063NM 2005 5 2 USAA050378 120050318A5415 ATTACH FITTING BOEING757 7572B7 1384964NM CFMINTCFM56 CFM563B2 13802EU RT PYLON DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19611AU40542 27123 CLT - DROP IN FITTING, .020 INCH, ELONGATED. RT PYLON MID BULKHEAD UPPER LINK ATTACH FITTING. REWORKED HOLES IAW EA. (K) 2L72 4F4 FRTA2NM E21EU 20050502000652005050200065NM 2005 5 2 AMTA200500297 120050321A3150 WARNING SYSTEM BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE COCKPIT ACTIVATED A AMTAK NONE J WARNING INDICATION ININSP/MAINT 1 GL11557TZ 32591 EICAS STATUS MSG L ENG OH LP2 DISPLAYED. DEFERRED IAW MEL 26-11-10, AUTH NR: D26MA21-1005.31 MAR 05. (K) 2L72 4F4 FRTA2NM E12EU 20050502000662005050200066NM 2005 5 2 AMTA200500288 120050320A2613 WARNING SYSTEM BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE COCKPIT INTERMITTENT A AMTAK NONE N FALSE WARNING CRCRUISE 1 GL11557TZ 32591 EICAS STATS MSG: L ENG OH LB2 DISPLAYED INTERMITTENT. PERFORMED BITE PROCEDURE IAW FIM 26-11-00. LT ENG FIRE DETECTION SYS OPS CHECKS NORMALLY. NO STATUS MSG. DISPLAYED. OK FOR SERVICE. (K) 2L72 4F4 FRTA2NM E12EU 20050502000692005050200069EA 2005 5 2 A6WA200540108 120050316A5320 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL13415AW 7593 FOUND FS 280, FRAME RBL 9, ATTACHMENT ANGLE TO BE CRACKED APPROX 1 INCH LENGTH. 2L72 4F4 FRTA21EA E15NE 20050502000702005050200070EA 2005 5 2 A6WA200540112 120050316A5712 RIB CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT WING CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31415AW 7593 LT MLG WHEEL WELL AT WS 48.30 FS 523.8 BATT RIB IS CRACKED APPROX 1 INCH. 2L72 4F4 FRTA21EA E15NE 20050502000722005050200072EA 2005 5 2 A6WA200540087 120050304A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31407AW 7424 RT FS 625 OBLIQUE ANGLE CRACKED IN RADIUS .3750 INCH LONG. REMOVED CRACKED ANGLE, INSTALLED NEW ANGLE IAW SRM. (K) 2L72 4F4 FRTA21EA E15NE 20050427003792005042700379NM 2005 4 27 QXEA200500667 120050413A5320 CLIP DHAV DHC8 DHC8202 2809007NM FUSELAGE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - MAIN CABIN DOOR SILL HAS A CRACKED CLIP ON BOTTOM AT STATION X240. REPAIRED IAW DHC-8 200 SRM 51-40-11. 2H72 4T RTA13NM 20050427003862005042700386NM 2005 4 27 QXEA200500706 120050413A5210 DOOR FRAME DHAV DHC8 DHC8202 2809007NM PAX DOOR CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - MAIN CABIN DOOR FORWARD LOWER SIDE IS CRACKED IN RADIUS. REPAIRED IAW DHC-8 200 SRM 51-40-11. 2H72 4T RTA13NM 20050427003982005042700398EA 2005 4 27 QXEA200500607 120050317A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE INTERIOR, RIGHTHAND INBOARD SEAT RAIL AT STATION X603 HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW CRJ700/900 SRM 51-21-06-001-001-A01, PARAGRAPH 3E, REO 670-53-00-013 AND CRJ700 SRM 51-21-16, CODE A044. 2L72 4F RTA21EA 20050427004082005042700408EA 2005 4 27 QXEA200500611 120050317A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE INTERIOR, LEFTHAND INBOARD SEAT RAIL AT STATION X647 HAS PITTING CORROSION ON TOP SURFACE. REPAIRED IAW CRJ700/900 SRM 51-21-06-001-001-A01, PARAGRAPH 3E, REO 670-53-00-013 AND CRJ700 SRM 51-21-16, CODE A044. 2L72 4F RTA21EA 20050427004172005042700417EA 2005 4 27 QXEA200500555 120050322A7110 HINGE CNDAIRCL600 CL6002C10 1390015EA FAN COWLING GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - RIGHTHAND NACELLE FAN COWL DOOR HINGES, UPPER AND LOWER, ARE GOUGED AT STATION 1069.75 ON HINGE LUGS. REPAIRED IAW CRJ 700 SRM 51-12-001-001-A01 AND HORIZON AIR EA R-78-23. 2L72 4F RTA21EA 20050427004192005042700419NM 2005 4 27 QXEA200500669 120050412A5230 SKIN DHAV DHC8 DHC8202 2809007NM CARGO DOOR GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - CARGO DOOR INNER SKIN GOUGED AT SCREW HOLE LOWER AFT CORNER X591, Z109. REPAIRED IAW DHC-8 200 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20050427004202005042700420NM 2005 4 27 QXEA200500670 120050412A5230 SKIN DHAV DHC8 DHC8202 2809007NM CARGO DOOR GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - CARGO DOOR INNER SKIN GOUGED AT SCREW HOLE, CENTER AFT OF DOOR, X570, Z130. REPAIRED IAW DHC-8 200 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20050427004222005042700422NM 2005 4 27 QXEA200500663 120050410A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - RIGHTHAND INBOARD SEAT TRACK IS CORRODED IN NUMEROUS LOCATIONS ON TOP BETWEEN X227.7 AND 240. REPLACED NR 7 SEAT TRACK. 2H72 4T RTA13NM 20050427004292005042700429NM 2005 4 27 QXEA200500671 120050412A5230 SKIN DHAV DHC8 DHC8202 2809007NM CARGO DOOR GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - CARGO DOOR INNER SKIN GOUGED AT SCREW HOLE UPPER MIDDLE OF DOOR, X570, Z151. REPAIRED IAW DHC-8 200 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20050427004302005042700430NM 2005 4 27 QXEA200500672 120050412A5230 SKIN DHAV DHC8 DHC8202 2809007NM CARGO DOOR GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - CARGO DOOR INNER SKIN GOUGED AT SCREW HOLE LOWER MIDDLE OF DOOR, TWO LOCATIONS, X570, X575, Z109. REPAIRED IAW DHC-8 200 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20050427004352005042700435EA 2005 4 27 QXEA200500571 120050323A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA FUSELAGE NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FORWARD FUSELAGE LOWER SKIN FROM STATION 295-310 AND STRINGER 25P TO 27 HAS SMALL NICKS IN SKIN. REPAIRED IAW CRJ700 SRM 51-25-01-001-001-A01, 51-12-00-001-A01. 2L72 4F RTA21EA 20050427004362005042700436EA 2005 4 27 QXEA200500572 120050323A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA FUSELAGE NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FORWARD FUSELAGE LOWER SKIN FROM STATION 310 TO 319.7 AND STRINGER 25P TO 26P HAS FOUR SMALL NICKS IN SKIN. REPAIRED IAW CRJ700 SRM 51-12-001-001-A01 AND SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050427004412005042700441NM 2005 4 27 QXEA200500708 120050417A5230 HANDLE BOMBDRDHC8 DHC8401 1390041NM CARGO DOOR NOT SEATED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09404QX 4046 BUR- ON FLIGHT 2502, WHILE ON CLIMBOUT, THE FORWARD BAGGAGE DOOR WARNING ILLUMINATED. AIRCRAFT RETURNED TO BUR AND ACCOMPLISHED A UNEVENTFUL LANDING. CFR WAS NOT CALLED. FOUND LATCH HANDLE .25 INCH FROM FLUSH. RESEATED HANDLE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2H72 4T RTA13NM 20050427004432005042700443NM 2005 4 27 QXEA200500711 120050421A2611473054 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM CARGO BAY DEFECTIVE A QXEAK NONE N FALSE WARNING APAPPROACH 1 NM09366PH132662081 510 SEA - FLIGHT 2062 - THE CREW REPORTED AN INTERMITTANT SMOKE WARNING INDICATION TWICE ON THE GROUND IN EUGENE AND ONCE ON APPROACH IN SEATTLE. THE INDICATION ONLY LASTED FOR A FEW SECONDS AND THEN EXTINGUISHED. MAINTENANCE REMOVED AND REPLACED THE CARGO COMPARTMENT CEILING NR 1 SMOKE DETECTOR. OPS CHECKS GOOD IAW 8 AMM 26-15-00 P 501. DEFERRED THE BULKHEAD NR 2 SMOKE DETECTOR IAW MEL REF 26-8. 2H72 4T RTA13NM 20050427004452005042700445EA 2005 4 27 QXEA200500557 120050322A7110 COWLING CNDAIRCL600 CL6002C10 1390015EA LT ENGINE WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - LEFT HAND ENGINE AFT ENGINE OF FAN COWL STATION, ENGINE STATION 157.00 HAS WEAR MARKS FROM TRANS COWL AT 2 O'CLOCK AND 4 O'CLOCK POSITION. REPAIRED IAW REO 670-78-33-347 2L72 4F RTA21EA 20050427004462005042700446EA 2005 4 27 QXEA200500558 120050326A5730 PANEL CNDAIRCL600 CL6002C10 1390015EA RT WING CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - RIGHT HAND WING FUEL LID PANEL 641BB HAS FRETTING CORROSION. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01 AND REO 670-57-12-002, ISSUE 1. 2L72 4F RTA21EA 20050428000122005042800012EU 2005 4 28 MALA050235 120050214A3260 WARNING LIGHT SAAB SF340 340B 7860101EU MLG INTERMITTENT A MALAO OTHER N FALSE WARNING CRCRUISE 1 GL15366PX 340B267 MSP TO YQT, DIVERT TO DLH. INTERMITTENT GEAR INTRANSIT LIGHT IN CRUISE. FERRIED TO MSP AND INSPECTED GEAR SWITCHES. NO DISCREPANCIES NOTED. ALL CHECKS GOOD. 2L72 4T RTA52EU 20050428000172005042800017NM 2005 4 28 BB05018 120050321A335020121 CHARGER BOEING767 767201 1385125NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19648US 23900 PHL - FOUND LEFT AFT SERVICE DOOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER (M1210). 2L72 4F RTA1NM 20050428000312005042800031EU 2005 4 28 245291 120050409A7931 INDICATOR SAAB SF340 SF340A 7850100EU COCKPIT MALFUNCTIONED A UHLAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL17121CQ 121 LT PROP OIL PRESSURE FLUX BETWEEN 10-80 PSI. REMOVED AND REPLACED LEFT PROP OIL PRESSURE IND, OPS CHECK NORMAL. 2L72 4T RTA52EU 20050428000352005042800035NM 2005 4 28 05FDEA00877 120050406A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 RIGHT WING O/B FLAP I/B FLAP MOUNTED HINGE ACTUATOR HOLE EVIDENT OF CORROSION. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F RTA22WE 20050428000362005042800036NM 2005 4 28 05FDEA00881 120050406A5347 SEAT TRACK BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25271FE 22036 MC DECK SEAT TRACK RBL 24 BETWEEN STA 720E TO 8 INCHES AFT OF 720F CORROSION AND HAS EXISTING BLEND REPAIRS AND REQUIRES REPLACEMENT PER EO 7-5340-7-5002. REMOVE SEAT TRACK IAW SRM 51-30-02, SEAT TRACK FABRICATED ON TRAVELER T5/506089 PER SRM 53-10-02 / 53-10-05. LOCATED AND DRILLED SEAT TRACK IAW SRM 51-30-02. TREATED AND PRIMED SEAT TRACK IAW SRM 51-10-02. INSTALLED SEAT TRACK IAW SRM 51-30-02. 2L73 4F RTA3WE 20050428000382005042800038NM 2005 4 28 05FDEA00883 120050406A5347FX1520792 SEAT TRACK BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25271FE 22036 SEAT TRACK BL 0, STA 510 HAS AN EXISTING REPAIR THAT INTERFERES WITH THE INSTALLATION OF MOD PARTS PER 7-5340-7-5002. REMOVED SEAT TRACK DAMAGED FROM STA 480 TO 600 IAW SRM 51-30-2. SCALLOPED NEW SEAT TRACK IAW SRM 51-30-5. TREATED AND PRIMED TRACK IAW SRM 51-10-2, INSTALLED NEW SEAT TRACK IAW SRM 51-30-2. 2L73 4F RTA3WE 20050428000442005042800044NM 2005 4 28 05FDEA00890 120050407A5514 STRUCTURE DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 RT HORIZONTAL STABILIZER UPPER BARREL NUT NR 23 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133. 2L73 4F RTA22WE 20050428000452005042800045NM 2005 4 28 05FDEA00891 120050407A5514 STRUCTURE DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25582FE 48420 STABILIZERS - HORIZONTAL STABILIZER BARREL NUT BORES, CORROSION REMOVAL COMPLY WITH EA 1-5510-71838. COMPLIED WITH EA 1-5510-71838. 2L73 4F RTA22WE 20050428000472005042800047NM 2005 4 28 05FDEA00893 120050407A5320FX69436951 ANGLE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25204FE 22926 STA 740 AFT PRESSURE BULKHEAD AFT FACE LOWER SPAR CAP AREA CORROSION RUNNING INTO SUPPORT ANGLE ON LT SIDE OF DELTA KEEL BEAM. ACCESSED AREA TO GAIN ACCESS TO REPAIR AREA, FOUND ANGLE P/N 69-43695-1 CORRODED WITH 100 PERCENT MATERIAL LOSS. REMOVED ANGLE IAW SRM 51-30-2. FABRICATED NEW ANGLE ON MAE TRAVELER T5/498923. LOCATED & DRILLED IAW SRM 51-30-5. INSTALLED ANGLE IAW SRM 51-30-2. REINSTALLED ITEMS, REMOVED FOR ACCESS IAW SRM 51-30-2, MM 20-10-005-4. CORROSION WAS ON ANGLE P/N 69-43695-1 ONLY. NO OTHER CORROSION NOTED. 2L73 4F RTA3WE 20050428000612005042800061NM 2005 4 28 05FDEA00907 120050408A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 LT WING O/B FLAP, I/B FLAP MOUNTED HINGE PIVOT HOLE EVIDENT OF CORROSION. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F RTA22WE 20050428000642005042800064NM 2005 4 28 05FDEA00910 120050408A5514 STRUCTURE DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT HAND UPPER AFT SKIN PLANK NR 34R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82942. 2L73 4F RTA22WE 20050428000672005042800067SO 2005 4 28 CHQA200500075 120050407A33501317 BULB EMB 145 EMB145LR 3260212SO CABIN LOOSE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11271SK 145305 AFT CEILING EMERGENCY LIGHT IS INOP. FOUND BULB LOOSE IN SOCKET. REPLACED BULB WITH NEW. OPS CHECK GOOD IAW EMB 145 AMM 33-50-09. 2L72 4T RTT00011AT 20050428000692005042800069SO 2005 4 28 CHQA200500077 120050409A2460 RELAY EMB 145 EMB145LR 3260212SO COCKPIT FAILED A CHQAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL11294SK 145497 A STRONG ELECTRICAL BURNING ODOR WAS NOTED DURING CLIMB FROM 520 FT TO 11,000 FT. CAPTAIN AND FIRST OFFICER DONNED O2 MASKS AND COMPLETED CABIN FIRE/SMOKE QRH CHECKLIST. AN EMERGENCY WAS DECLARED WITH POTOMAC APPROACH AND THE AIRCRAFT LANDED UNEVENTFULLY. MAINTENANCE FOUND A FAULTY RELAY. REMOVED AND REPLACED RELAY K0285 ON CB PANEL 0093. OPS CHECK GOOD IAW EMB 145 AMM 24-65-00 AND 24-31-00. NO DEFECTS NOTED. 2L72 4T RTT00011AT 20050428000722005042800072SO 2005 4 28 MASA200500187 120050306A2621 WARNING SYSTEM EMB 145 EMB145LR 3260212SO COCKPIT MALFUNCTIONED A MASAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SW07842MJ8540 145457 AIRCRAFT RETURNED TO THE GATE. CREW REPORTED A BAGGAGE COMPARTMENT FIRE EXTINGUISHER INOP MESSAGE. MAINTENANCE FOUND BOTH BOTTLES DISCHARGED, REPLACED THEM AND RETURNED THE AIRCRAFT TO SERVICE. A FEW MOMENTS LATER, THE CREW CALLED IN THE SAME MESSAGE AGAIN. MAINTENANCE FOUND THAT THE BOTTLES HAD NOT DISCHARGED THIS TIME. MX SWAPPED THE DAU AND THE FIRE SYSTEM CONTROL PANEL BUT THE FAULT DID NOT CLEAR. TROUBLESHOOTING AT THIS TIME. MX REPLACED FIREX BOTTLES P/N 33700027-1, S/N 42676D1 AND P/N 34600073-1, S/N 19943F1. 2L72 4T RTT00011AT 20050428000762005042800076 2005 4 28 MASA200500285 420050405A31407013348940 DAU EMB 145 EMB145LR 3260212SO NR 1 OVERHEATED A MASAA UNSCHED LANDING MBJOVER TEMP SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NRNOT REPORTED 1 SW07833MJ8244 145327 AIRCRAFT RETURNED TO THE FIELD. CREW REPORTED A DU1 OVERHEAT MESSAGE AND SPS ADVANCE MESSAGE WITH STRONG ELECTRICAL SMOKE ODOR IN THE FLIGHT DECK AND CABIN. MAINTENANCE FOUND THE DAU 1 BAD AND REPLACED IT AND PERFORMED THE SYSTEM OPERATIONAL CHECKS. 2L72 4T RTT00011AT 20050428001132005042800113NM 2005 4 28 DL73S050170 120050315A53209078223 GUSSET BOEING737 737247 138448DNM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27374DL 23521 THE GUSSET SURROUNDING THE LOWER HINGE CUTOUT FOR THE FWD FRAME ASSEMBLY OF THE L1 DOOR CUTOUT WAS FOUND WITH A SMALL CRACK IN THE RADIUS OF THE GUSSET. THE CRACK WAS ROUTED OUT AND REPAIRED WITH A TITANIUM DOUBLER PER ER/A 097525-14. 2L72 4F A16WE 20050428001142005042800114NM 2005 4 28 05FDEA00779 120050401A52301036541 HOUSING BOEING727 727233 138408ANM CARGO DOOR GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25272FE 22037 NR 3 LOWER CARGO DOOR, HANDLE HOUSING GOUGED BY HANDLE STUD. REMOVED AND REPLACED #3 LWR CARGO DOOR HANDLE PER SRM 51-30-02. 2L73 4F RTA3WE 20050428001162005042800116NM 2005 4 28 DL76L050172 120050319A3840381702030 COMPRESSOR BOEING767 767332 1382001NM WATER PRESSURE MALFUNCTIONED A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27189DN 25990 SMELL OF SMOKE ELEC FROM AROUND ROW 38. REPLACED WATER COMPRESSOR. 2L72 4F RTA1NM 20050428001282005042800128NM 2005 4 28 DL733050181 120050319A492085129E APU BOEING737 737347 1384647NM CFMINTCFM56 CFM562AFR 13802EU APU BAY DEFECTIVE A DALAE ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27305WA14837 23346 60550 SMOKE SMELL IN CABIN WITH APU AIR. REPLACED APU. 2L72 4F4 FRTA16WE E21EU 20050428001302005042800130 2005 4 28 DL757050183 420050322A2213622459512 COMPUTER BOEING757 757232 1384965NM E/E BAY FAILED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27631DL 23612 SMOKE SMELL NOTICED BY FLIGHT AND CABIN CREW. REPLACED CENTER FCC. 2L72 4F RTA2NM 20050428001322005042800132NM 2005 4 28 DL757050185 120050322A3397 WIRE BOEING757 757232 1384965NM CABIN DAMAGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27608DA 22815 EMERGENCY EXIT LIGHT AT SEAT 2CD INOP. REPAIRED WIRE. 2L72 4F RTA2NM 20050428001342005042800134NM 2005 4 28 DL73G050187 120050323A5330 SKIN BOEING737 737330 13844BJNM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27242DL 23834 MAJOR REPAIR INSTALLED. INSTALLED DOUBLER BETWEEN STR 28L & 28R STA 380 IAW SRM 53-30-01D. 2L72 4F RTA16WE 20050428001352005042800135NM 2005 4 28 DL76L050188 120050325A2520 SUPPORT BRACKET BOEING767 767332 1382001NM SEAT BROKEN A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27185DN 27961 CREW REST SEAT RECLINE ACTUATOR SPARKING WHEN OPERATED. MTC FOUND SUPPORT BRACKET BROKEN WHICH CAUSE DAMAGE THE ACTUATOR WIRING. REPLACED SEAT. 2L72 4F RTA1NM 20050428001372005042800137NM 2005 4 28 DLM88050191 120050327A2910AS15508K024 HYDRAULIC LINE DOUG MD88 MD88 3023688NM A/C BAY WORN A DALAO OTHER K FLUID LOSS DEDESCENT 1 SO27956DL 49887 LEFT HYD QTY DROPPED PRESSURE FAILED TO ZERO. REPLACED ENG HYD PRESSURE LINE IN TAIL COMPARTMENT. 2L72 4F RTA6WE 20050429000042005042900004EU 2005 4 29 YENA200525 120050403A3350321430 BATTERY PACK AIRBUS320 A320232 3930326EU EMERGENCY LIGHT FAILED A YENAK NONE O OTHER ININSP/MAINT 1 EA15524JB15011 1528 EMERGENCY LIGHT BATTERY PACK FAILED TEST. REPLACED 12WL BATTERY PACK. 2L72 4F RTA28NM 20050429000152005042900015CE 2005 4 29 DXTA200500671 120050410A3210 LANDING GEAR CESSNA750 750 2076810CE NOISY E DXTAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL07910QS 7500110 LOUD KLUNKING NOISE COMING FROM NOSE GEAR AT 10,000 FT AND 250 KTS. PERFORMED GEAR BUMP TROUBLESHOOTING CHECK LIST IAW CE750 M/M CH 32-30-00. OPERATIONAL CHECKS GOOD. NO DEFECTS WERE NOTED. 2L72 4J RTT00007WI 20050502000172005050200017NM 2005 5 2 DHL2005782505 120050314A5534 CLIP BOEING727 727227 1384078NM VERTICAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 ANGLED SHEAR TIE CRACKED JUST BELOW STRINGER 9L AT FIN STA 180.6 INSIDE VERTICAL FIN. REMOVED DAMAGED CLIP AT FIN STA 180.6 BELOW STR 9L IAW 727 SRM 51-30-2. FABBED NEW CLIP FROM 7075 T6 .050 PO NR 9001417 DIM 5 3/4 INCH BY 3 INCHES IAW 727 SRM 727 55-30-2 FIG 2. FABRICATED CLIP TREATED PRIMED AND INSTALLED IAW 727 SRM 51-10-2 AND 51-30-2. 2L73 4F A3WE 20050502000192005050200019NM 2005 5 2 DHL2005782510 120050310A5330 SKIN BOEING727 727227 1384078NM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 CREASE R/SIDE FUSELAGE SKIN AT STA 1342.2 BELOW 21R. CUT OUT DAMAGED AREA AT FUSELAGE SKIN AT STA 1342 IAW B727 SRM 54-30-1 SIZE 1/2 INCH BY 2 INCH. FABRICATED DOUBLER REPAIR USING 2024T3 .063 PO NR 9001978 SIZE 10 INCH BY 9 INCH IAW B727 SRM 54-30-2 FIG 4AND 54-30-3 FIG 7. ALODINED AND PRIMED PART AND AREA IAW B727 SRM 51-10-2 AND INSTALLED ANGLE IAW B727SRM 54-30-3 FIG 7. 2L73 4F A3WE 20050502000212005050200021NM 2005 5 2 DHL2005782514 120050310A5330 SKIN BOEING727 727227 1384078NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 DENT LT SIDE FUSELAGE SKIN ABOVE STR 17L, AFT OF STA 1324.4. CUTOUT DAMAGED AREA IAW B727 SRM 54-30-1 FIG 1. FABRICATED DOUBLER REPAIR USING 2024T3 .063 PO NR 9001978 DIMENSION 15 INCHES BY 5 5/8 INCH IAW B727 SRM 54-30-2 FIG 7. ALODINED AND PRIMED PART IAW SRM 51-10-2. INSTALLED DOUBLER IAW B727 SRM 54-30-2 FIG 1 AND 54-30-3 FIG 7. 2L73 4F A3WE 20050502000452005050200045NM 2005 5 2 SWAA051048 120050411A5753654643489 FLAP BOEING737 7373H4 1384600NM LT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29634SW 27937 DURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM. 2L72 4F RTA16WE 20050502000732005050200073EA 2005 5 2 A6WA200540114 120050320A21707536893 COALESCER BAG CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE A/C BAY DIRTY A A6WAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL31469AW 7917 STRONG FUEL SMELL IN COCKPIT AT CRUISE. SMELL INCREASED WITH TEMP SELECTED IN MANUAL MODE. SELECTED LT PACK OFF, SMELL WENT AWAY. INSPECTED APU AREA, PACK NR 1 AND NR 2, NO LEAKS NOTED. NO EVIDENCE OF FUEL AROUND ENGINES OR APU. REAM ENGINE AND BOTH PACKS, NO SMELL OF FUEL ON RUNS. SUSPECT DIRTY LT COALESCER BAG ON LT PACK. PLACED ON MEL. (K) 2L72 4F4 FRTA21EA E15NE 20050502000742005050200074EA 2005 5 2 A6WA200540115 120050320A2700 UNKNOWN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE WING MALFUNCTIONED A A6WAK NONE F FLT CONT AFFECTED APAPPROACH 1 GL31426AW 7669 DURING APPROACH, WHEN SELECTING FLAPS FROM 30 TO 45 AIRCRAFT STARTED ROLLING LT, REQUIRED HALF AVAILABLE AILERON TRIM AND RT CONTROL WHEEL INPUT TO KEEP WINGS LEVEL. FLAP TRAVEL APPEARS UNEVEN. PERFORMED FLAP RIG CHECK, OPS CHECK GOOD. SPOILER SYSTEMS OPS CHECK GOOD. INSPECTED FLAPS RUB STRIP, RUB STRIPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. (K) 2L72 4F4 FRTA21EA E15NE 20050502000752005050200075EA 2005 5 2 A6WA200540116 120050321A2421755469E IDG CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT ENGINE LACK OF LUBE A A6WAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL31436AW2721 7734 IDG NR 2 CAS MESSAGE ON TAKEOFF, ABORTED TAKEOFF, BELOW 60 KNOTS TO 70 KNOTS, TOTAL WEIGHT 47000. ALL BRAKES IN GREEN LT TO RT 4,3,3,4 AND CONFIG WARNING ILLUMINATED. SERVICED IDG NR 2 IAW 24-12-00. OPS CHECK GOOD AT THIS TIME. BTMS CHECKS NORMAL AT THIS TIME, NO INDICATION OF CONFIG WARNING AT THIS TIME. OPS CHECK GOOD, OPS CHECK CONTROL SURFACES HES PROCEDURE NOT REQUIRED. (K) 2L72 4F4 FRTA21EA E15NE 20050502000772005050200077NM 2005 5 2 GAIA05015OP 120050322A33501000679 LIGHT BOEING727 727223 1384074NM PWA JT8 JT8D9A 52048NE CABIN INOPERATIVE A GAIAK NONE L NO TEST ININSP/MAINT 1 SW07856AA 20997 DURING PREFLIGHT, FOUND COCKPIT EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT IAW MM. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L73 4F4 F A3WE E2EA 20050502000792005050200079NM 2005 5 2 GAIA05017OP 120050408A3350 BATTERY PACK BOEING727 727223 1384074NM PWA JT8 JT8D9A 52048NE CABIN DISCHARGED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07856AA 20997 DURING PREFLIGHT, FOUND L-1 DOOR AND COCKPIT ENTRY DOOR EMERGENCY BATTERY PACKS DRAINED TO DIM ILLUMINATION. REPLACED BATTERY PACKS (2 EA). OPERATED EMERGENCY LIGHT SYSTEM AND FOUND OPERATING NORMALLY. OK FOR SUBSEQUENT FLIGHT. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L73 4F4 F A3WE E2EA 20050503000672005050300067 2005 5 3 DLM88050190 420050327A3417HG280D80 ADC DOUG MD88 MD88 3023688NM NR 2 FAILED A DALAA UNSCHED LANDING G MULTIPLE FAILURE CLCLIMB 1 SO27960DL 49979 AIRBORNE A/T CLICKED OFF, DFGS ALT WINDOW BLANKED, AND FMS SCRATCH PAD SHOWED CADC NR 1 FAILED. USED CADC FAIL CHECKLIST. ON LEVEL OFF NR 1 ALT WAS 600 FT HIGHER THAN STBY. BECAUSE OF INDICATION IF INTERMITTENT FAILURE FROM BOTH CADC COMP, RETURNED TO CVG. REPLACED CADC NR 1 AND CADC NR 2. OPS AND LEAK CHECKED SYS PER AMM 34-11-00-201-1. RAN RT 1 AND 2, BOTH OK. 2L72 4F RTA6WE 20050503000762005050300076NM 2005 5 3 DL757050196 120050401A4920 SEAL BOEING757 757232 1384965NM PWA JT8 JT8D NE APU LEAKING A DALAK NONE KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27629DL10913 P2432 22919 P2432 MUSTY SMELL IN COCKPIT. FOUND COCKPIT AND FWD CABIN TO HAVE SMELL OF BURNED OIL. FOUND APU LOAD COMPRESSOR SEAL LEAKING. PERFORMED DUCT BURNOUT. APU WILL NEED REPLACEMENT. FWD APU TO MCO AND PLAC. 2L72 4F4 FRTA2NM E2EA 20050503000842005050300084NM 2005 5 3 DL764050198 120050326A2120 ODOR BOEING767 767432ER 1385134NM COCKPIT DETECTED A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO27831MH 29702 ON DESCENT WITH THRUST LEVERS AT IDLE STRANGE SMELL PERMEATED COCKPIT. REFERENCE PREVIOUS WRITE UP. RAN ENGINES AT TAKEOFF PWR FOR 5 MINS WITH BOTH PACKS OPERATING. ALSO RAN EACH ENGINE INDIVIDUALLY AT TAKEOFF WITH CORRESPONDING PACK OPERATING. NO SMELL NOTED. RAN EACH ENGINE IN REVERSE THRUST. NO SMELL NOTED. CANNOT DUPLICATE PROBLEM. 2L72 4F RTA1NM 20050503000862005050300086NM 2005 5 3 DL76G050199 120050403A3350 FUSE BOEING767 7673P6 1385105NM POWER SUPPLY BLOWN A DALAK NONE L NO TEST ININSP/MAINT 1 SO27152DL 24984 EMERGENCY EXIT LIGHTS ON RT SIDE FROM MID GALLEY TO ROW 19 INOP. FOUND FUSE ON BATTERY PWR SUPPLY BLOWN. REMOVED AND REPLACED SAME, CHECKS GOOD. 2L72 4F RTA1NM 20050503000982005050300098NM 2005 5 3 DLM88050204 120050406A4940 STARTER DOUG MD88 MD88 3023688NM APU FAILED A DALAK NONE A FLAME/FIRE TXTAXI/GRND HDL 1 SO27909DE 80539 53418 80539 WHILE WORKING AN MCO FOR AN APU REPORT TO NOT START, IT WAS FOUND THAT THE APU STARTER HAD EITHER BURNT, OVERHEATED OR CAUGHT FIRE. THE STARTER CABLES WERE BURNT, AS WERE THE GENERATOR CABLES. THE STARTER ITSELF WAS CHARRED AND DISCOLORED, AS WAS NUMEROUS WIRES AND WIRING HARNESSES. REPLACED STARTER, CABLES, BATTERY CONTACTOR, AND AUX POWER RELAYS 2L72 4F RTA6WE 20050503001002005050300100NM 2005 5 3 DL76G050205 120050407A324226124121A BRAKE BOEING767 767332 1382001NM RT MLG BROKEN A DALAD RETURN TO BLOCK K FLUID LOSS TXTAXI/GRND HDL 1 SO271611B 30595 A/C RETURNED TO GATE DUE TO REPORTS OF FLUID LEAKING FROM RT MAIN LANDING GEAR. ON INSPECTION FOUND NUMBER 7 AND NUMBER 8 STATOR/PRESSURE PLATES BREAKING UP ALLOWING PISTON OVER EXTENSION WHICH CAUSED A FLUID LEAK. BRAKE UNIT S/N DL2073, REMOVED FROM POSITION NUMBER 8. BRAKE UNIT S/N DL2072, REMOVED FROM POSITION NUMBER 7. 2L72 4F RTA1NM 20050503001012005050300101NM 2005 5 3 DL764050207 120050409A3350 LIGHT BOEING767 767432ER 1385134NM CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27837MH 29710 THE 2L/2R/3L EMERGENCY EXIT LIGHTS INOP. RELAMPED ALL. 2L72 4F RTA1NM 20050503001042005050300104NE 2005 5 3 DL76L050212 220050411A7200 ENGINE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 2 MAKING METAL A DALAO OTHER O OTHER ININSP/MAINT 1 SO27197DN34663 28454 724844 NR 2 ENGINE REPLACED DUE METAL FOUND IN NR 3 MCD. 2L72 4F4 FRTA1NM E24NE 20050503001062005050300106NM 2005 5 3 DL777050215 120050411A3350D71702001 POWER SUPPLY BOEING777 777232 1385232NM CABIN FAILED A DALAK NONE O OTHER DEDESCENT 1 SO27862DA 29734 FLT ATTENDANT ADVISE, ON DESCENT ALL EMERGENCY LIGHTS CAME ON. AFT CABIN FLOOR PROX LIGHTS NOT ON. VERIFIED AFT CABIN ZONE SEAT PROX LIGHTS INOP. FOUND EMERGENCY LIGHTS PWR SUPPLY M33401 AT DOOR 3R BAD. REPLACED M33401 PWR SUPPLY AND BATTERY PACK. LOANED PART FROM JAPAN AIRLINES AT NRT 04/12/05. LIGHTS NOW OKAY. 2L72 4F RTT00001SE 20050503001082005050300108NM 2005 5 3 05FDEA00916 120050410A5347AEA7325501 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 MAIN DECK, RIGHT HAND SEAT TRACK AT STA Y= 1361 - Y= 1481, -X= 47 FOUND WITH CORROSION. MAIN DECK, RIGHT HAND SEAT TRACK CUT AND REMOVED FROM STA Y= 1351 - Y= 1481 -X= 47 PER SRM 51-31-01 VOLUME II. REPAIR SEAT TRACK AND SPLICE FABRICATED PER SRM 53-70-00 VOLUME I, FIGURE 1 AND INSTALLED PER SRM 51-3102 VOLUME II. 2L73 4F RTA22WE 20050503001102005050300110NM 2005 5 3 05FDEA00955 120050411A5320 STRUCTURE DOUG MD11 MD11 3023602NM FUSELAGE DAMAGED A FDEAO OTHER O OTHER UKUNKNOWN 1 SO25628FE 48447 DURING AIRPLANE'S CONVERSION FROM P TO F FOUND: REPAIR AT STA 5-53, STR 50-51 LT REQUIRES ENGINEERING EVALUATION TO DETERMINE WHETHER REPAIR IS MAJOR OR MINOR AND CONFORM TO APPLICABLE DATA. NO ACTION REQUIRED: REPAIR IS CONFORMED IAW SRE 53-20-00 FIG 6, SHEET 7, VOL 1. 2L73 4F RTA22WE 20050503001122005050300112NM 2005 5 3 05FDEA00957 120050411A5320 STRUCTURE DOUG MD11 MD11 3023602NM FUSELAGE DAMAGED A FDEAO OTHER O OTHER UKUNKNOWN 1 SO25628FE 48447 DURING AIRPLANE'S CONVERSION FROM P TO F FOUND: REPAIR AT STA 990, STR 40-42 RT REQUIRES ENGINEERING EVALUATION TO DETERMINE WHETHER REPAIR IS MAJOR OR MINOR AND CONFORM TO APPLICABLE DATA. NO ACTION REQUIRED: REPAIR IS CONFORMED IAW SRE 53-50-00 FIG 7A. 2L73 4F RTA22WE 20050503001132005050300113NM 2005 5 3 05FDEA00964 120050411A5534 BUSHING BOEING727 727200 138407ENM VERTICAL STAB LOOSE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25272FE 22037 BUSHINGS LOOSE ON UPPER CLEVIS FOR THE PCU ROD END. REPAIRED UPPER RUDDER CLEVIS BUSHINGS FOR THE PCU RODEND IAW FED EX EA 7-5530- 86276. 2L73 4F RTA3WE 20050503001292005050300129NM 2005 5 3 05FDEA00941 120050411A5320 BRACKET DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 AFT FUSELAGE COMPARTMENT STATION 2007 RIGHT HAND BEAM APPROX X=20 FOUND VERTICAL L-ANGLE BRACKET SUSPECT CRACK AT THE TOP MOST EDGE. REPAIRED AS PER FEDEX EA 1-5310-83088. 2L73 4F RTA22WE 20050503001302005050300130NM 2005 5 3 05FDEA00942 120050411A5514 STRUCTURE DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT HAND UPPER CENTER SKIN PLANK NR 36R BARREL NUT BORE FOUND EXCEEDED LIMIT. REPAIRED IAW FEDEX EA 1-5510-82996. 2L73 4F RTA22WE 20050503001342005050300134NM 2005 5 3 05FDEA00944 120050411A5514 STRUCTURE DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT HAND BORE NR 6L FOUND EXCEEDED LIMIT. REPAIRED IAW FEDEX EA 1-5510-82991. 2L73 4F RTA22WE 20050503001372005050300137NM 2005 5 3 05FDEA00946 120050411A5514 STRUCTURE DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON HORIZONTAL STABILIZER LEFTHAND BORE NR 18L, FOUND EXCEEDED LIMIT. REPAIRED IAW FEDEX EA 1-5510-82952. 2L73 4F RTA22WE 20050503001472005050300147SO 2005 5 3 C2XAO5SH021 120050405A5522BRRFZ5AD4 SKIN EMB 145 EMB145LR 3260212SO LT ELEVATOR CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716951 145063 SHV - DURING C-CHECK LT ELEVATOR ACCESS PANEL 335 HB, CUTOUT BENT. MAINTENANCE ON FURTHER EVALUATION FOUND LT ELEVATOR ACCESS PNL (CUTOUT)CRACKED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED REPAIR IAW EC5520-01070. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050503001502005050300150NM 2005 5 3 05FDEA00947 120050411A5514 STRUCTURE DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON HORIZONTAL STABILIZER LEFTHAND BORE NR 16L, FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82952. 2L73 4F RTA22WE 20050503001562005050300156NM 2005 5 3 CALA0500100 120050411A531565C33948 FLOORBEAM BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716617 27330 INSPECTION FOUND MAIN CABIN FLOORBEAM BEAM CORRODED AROUND SCREW HOLES AT STA 947.5, LBL 17 TO RBL 17. A REPAIR WAS INSTALLED IAW ECRA 5310-04049. 2L72 4F RTA16WE 20050503001662005050300166EU 2005 5 3 2005UALA00280 120050329A2560 INSERT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE EVAC SLIDE MISSING A UALAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP29422UA 503 LT OFFWING SLIDE, METAL INSERTS IN ENCLOSURE FOR MOUNTING STUDS ARE MISSING IN 4 HOLES, ALLOWING MOUNTING STUDS TO CRUSH ENCLOSURE AGAINST MOUNTING PLATE. INSERTS COULD GET FOULED UP AND GETTING LOST DURING ENCLOSURE REMOVAL AND/OR TRANSPORT. THE SHOP DOCUMENT (CE-40-25-61-01-JD AND OEM CMM) REQUIRE THE SHOP TO PROVIDE THESE EXPENDABLE HARDWARE. THE REPAIR LIMITS ARE ALSO SPECIFIED IN THE CMM. 2L72 4F4 FRTA28NM E40NE 20050503001732005050300173 2005 5 3 2005UALA00281 420050328A2565 FLAPPER VALVE BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE ASPIRATOR DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29229UA 30557 DAMAGED ASPIRATOR FLAPPER VALVE. SLIDE/RAFT WAS REMOVED FROM AIRCRAFT AT NORMAL MAINTENANCE INTERVAL. DAMAGED ASPIRATOR FLAPPER VALVE WAS OBSERVED DURING SLIDE/RAFT MAINTENANCE. THE EXACT CAUSE OF THE DAMAGE COULD NOT BE DETERMINED. 2L72 4F4 FRTT0001SE E46NE 20050503001852005050300185 2005 5 3 2005UALA00283 420050311A2565 O-RING BOEING757 757222 1384956NM PWA 2037 PW2037 NE EVAC SLIDE LEAKING A UALAK NONE O OTHER ININSP/MAINT 1 WP29553UA 25277 LOW BOTTLE PRESSURE. RESERVOIR/VALVE ASSEMBLY SHAFT O-RING LEAKING. REPLACED SHAFT O-RING AND BACK-UP O-RING. 2L72 4F4 FRTA2NM E17NE 20050503001912005050300191 2005 5 3 2005UALA00304 420050216A2565 CELL AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE SLIDE/RAFT SEPARATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29806UA 788 AFTER INFLATION AND PRESSURIZING TO 2.5 PSI FOR AR, CHAMBERS SEPARATED. ADHESIVE FAILURE, RESULTED IN AIR CHAMBERS TO SEPARATE DURING PRESSURIZATION OF ASSEMBLY. UNIT WAS SENT TO OEM FOR REPAIR/DISPOSITION. 2L72 4F4 FRTA28NM E40NE 20050810000032005081000003NM 2005 8 10 DHL2005746507 120050630A5347 SEAT TRACK BOEING727 727224 1384076NM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01746DH 22252 SEAT TRACK DAMAGED AT BS 520 TO 560 RBL 24.75. REMOVED SEAT TRACK AT BS 480 TO 550 RBL 24.75 IAW B727 SRM 51-30-2, FABBED NEW SEAT TRACK MAT P/N BAC 1520-792 PO 9001320 SIZE 70" IAW B727 SRM 53-10-5 FIG 1 AND SRM 53-10-2 FIG 1, TREATED AND PRIMED SEAT TRACK IAW B727 SRM 51-10-2, INSTALLED SEAT TRACK IAW B727 53-10-5 FIG 1. 2L73 4F A3WE 20050503002552005050300255NE 2005 5 3 WRLA2005084 220050407A7300 FUEL SYS DOUG DC10 DC1030 3023501WP GE CF6 CF650C2 30018NE NR 3 LEAKING A WRLAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO1114075 46922 455894 DIVERSION DUE TO 1+20HR INTO FLIGHT NR 3 FUEL FLOW STARTED TO INDICATE 15,000 LBS PER HOUR ON THE NEEDLE, 29,320 ON DIGITAL. FUEL USED ON NR 3 ROSE TO OVER 5,000 LBS MORE THAN 1 AND 2. ENGINE SHUTDOWN PER PROCEDURES. FUEL PRESSURE ON NR 3 STILL INDICATES 80 PSI AND FUEL FLOW INDICATED 2,500 LBS PER HOUR. FIRE HANDLE WAS PUT DOWN AND FUEL FLOW DROPPED. FLEW 45 MINUTES WITH FIRE HANDLE DOWN AND ENGINE SHUT DOWN. INSPECTED ENGINE, FOUND NO FUEL LEAKS STATIC OR WITH PUMPS. ENGINE IDLE RUN FOUND NO LEAKS. REINSPECTED AFTER ENGINE RUN. NO LEAKS NOTED. HIGH POWER ENGINE RUN ALL PARAMETERS NORMAL (EGT, N1, N2, FUEL FLOW, FUEL PRESSURE) NO LEAKS NOTED. AIRCRAFT DETERMINED TO BE OK FOR SERVICE. 2L73 4F4 F A22WE E23EA 20050503002572005050300257EA 2005 5 3 DAT2005F00001 220050322A7261 ENGINE STBROSSD3 SD330 8100602EU PWA PT6 PT6A45R 52043EA RIGHT LEAKING E DATAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL1358DD 187983245 SH3008 PCE84125 ON FINAL FLT OF DAY, CREW EXPERIENCED PROBLEMS WITH RT ENGINE. PRIOR TO CRUISING ALTITUDE IT WAS NOTICED THE OIL R LIGHT WAS FLICKERING, WHILE OIL PRESSURE GAUGE WAS OSCILLATING BETWEEN 90 PSI AND 135 PSI. GAUGE CONTINUED WITH ITS OSCILLATIONS, BUT THE RANGE LOWERED TO 80 PSI AND 120 PSI. TREND CONTINUED DOWN, SHUT DOWN ENG WHEN PSI DROPPED BELOW 60PSI. LANDED SAFELY. MECHANICS DISPATCHED, OIL WAS ADDED, DISCREPANCY WAS NOT CORRECTED. SERVICEABLE ENG WAS INSTALLED. OPS CHECKED GOOD. AC RETURNED TO SERVICE. 2H72 4T4 T A41EU E4EA 20050503002622005050300262EA 2005 5 3 VNAA0503009 120050320A3150 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE ANTI-ICE SYSTEM MALFUNCTIONED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL05242JS 7911 DURING TAKEOFF ROLL AT DAY THE CREW RECEIVED ANTI-ICE DUCT WARNING MESSAGES. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. PSA MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE WING ANTI-ICE CONTROL & INDICATION SYSTEM IAW CRJ 200 AMM 30-12-00-710-801. THE SYSTEM CHECKED GOOD AND NO DEFECTS WERE NOTED. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050503002662005050300266NM 2005 5 3 DHL2005782568 120050313A5414 SKIN BOEING727 727227 1384078NM NR 1 PYLON DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 C-CHECK, DENT NR 1 ENGINE PYLON SKIN UPPER SURFACE 7 INCHES AFT OF STA 1303 STR 14L. DENT IS CREASED, FOUND TO BE OUT OF LIMITS ON PYLON NR 1 UPPER SKIN SURFACE 7 INCHES AFT OF STA 1303 STR 14L IAW B727 SRM 54-10-1 FIG 1. CUT OUT DAMAGE AREA SIZE .75 INCH X .75 INCH IAW B727 SRM 54-10-3 FIG 5, FAB REPAIR DOUBLER FROM 2024T3 .050 SIZE 4 X 4 INCH PO 9001873 IAW B727 SRM 54-10-3 FIG 5, TREATED AND PRIMED PART AND AREA IAW B727 SRM 51-10-2, INSTALLED REPAIR DOUBLER IAW B727 SRM 54-10-3 FIG 5. 2L73 4F A3WE 20050503002682005050300268EA 2005 5 3 QXEA200500560 120050319A1430 RIVET CNDAIRCL600 CL6002C10 1390015EA FUSELAGE PULLED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - CENTER FUSELAGE AT STATION 770.0, WL 725, RBL 9.0-17.0 HAS RIVETS PULLED ON FLAT STRAP. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20050503002702005050300270WP 2005 5 3 0500479611 120050401A5310 DOOR FRAME DOUG DC9 DC932 3022066WP FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01611NA 47435 DURING M-CHECK FOUND CRACK IN LT SIDE AFT ENTRY DOOR JAMB FRAME. REPAIRED PER EA 96-203207. 2L72 4F A6WE 20050503002722005050300272WP 2005 5 3 0500519877 120050222A5320 CHANNEL DOUG DC9 DC951 3022051WP FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01786NC 48148 DURING H-CHECK FOUND CRACK IN BULKHEAD HAT CHANNEL AT BS 855. REPAIRED PER EA 98-202509. 2L72 4F RTA6WE 20050503002742005050300274WP 2005 5 3 0500499870 120050225A5315 FLOORBEAM DOUG DC9 DC951 3022051WP FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01779NC 48101 DURING H-CHECK FOUND CRACK IN FLOORBEAM AT BS 674 LBL 5. REPAIRED PER EA 98-202520. 2L72 4F RTA6WE 20050503002772005050300277EA 2005 5 3 VTZA200500047 120050413A2740 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA COCKPIT JAMMED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27658BR 7500 STABILIZER CHANNEL 1 FAILURE. LABEL 270 BIT 12 SHOWED 1 (CO-PILOTS TRIM SWITCH JAMMED). 2L72 4F RTA21EA 20050503002782005050300278NM 2005 5 3 P9RA20050077 120050410A335085 BULB BOEING757 757236 1384971NM EMERGENCY LIGHT INOPERATIVE A P9RAK NONE L NO TEST ININSP/MAINT 1 SO11962PG 24119 AIRCRAFT IN MAINTENANCE ORD; MID CABIN BULLNOSE EMERGENCY LIGHT INOP. RELAMPED MID CABIN EMERGENCY LIGHT IAW MM. 2L72 4F RTA2NM 20050503002802005050300280SO 2005 5 3 C2XA05CL019 120050404A21332099L01110 OUTFLOW VALVE EMB 145 EMB145ER 3260211SO CABIN PRESSURE FAILED A C2XAB EMER. DESCENT O OTHER CRCRUISE 1 SW271294614539 145052 CLE - THE CREW REPORTED, LOST ALL PRESSURIZATION WHILE CRUISING AT 22,000 FT. THE CREW MADE AN EMERGENCY DESCENT. THE CREW WAS ABLE TO REGAIN CONTROL OF PRESSURIZATION USING MANUAL CONTROL, AND LANDED IN CLE WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE PNEUMATIC OUTFLOW VALVE. A SATISFACTORY TEST FLIGHT WAS PERFORMED AND THE ACFT WAS RELEASED TO SERVICE. 2L72 4F RTT00011AT 20050503002812005050300281NE 2005 5 3 ANCF200400045 220050405A7230 BLADE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE ENGINE CRACKED B ANCFK NONE O OTHER ININSP/MAINT 1 SO23190AN 53190 718035 DURING OVERNIGHT SERVICE WAS ACCOMPLISHED EO 83-72-007 BORESCOPE INSPECTION FIRST AND SECOND STAGE TURBINE BLADES AND FOUND ON LT ENGINE ONE BLADE WITH CRACK ON TRAILING EDGE CONCAVE SIDE OF FIRST STAGE TURBINE. THE ENGINE HAS BEEN REMOVED IAW AMM 72-00-00, 71-00-00 AND WILL BE SENT TO THE SHOP. THAT ENGINE WAS PREVIOUSLY REPAIRED ON IAI (ISRAEL AIRCRAFT INDUSTRIES) SHOP AND HAD 824.66 HRS OF OPERATION. 2L72 4F4 FRTA6WE E9NE 20050503002842005050300284CE 2005 5 3 DJFA2005078 120050408A3260MS243311 SWITCH BEECH MU300 400A 1155402CE RT MLG NO INDICATION E DJFAO OTHER P NO WARNING INDICATION APAPPROACH 1 EA23477LX RK377 KDAL TRIP ID NR 813053, CREW REPORTED THAT THEY RECEIVED A UNSAFE GEAR INDICATION FOR THE RIGHT MAIN GEAR WITH NO GREEN LIGHT ILLUMINATING. THE GEAR HANDLE LIGHT WAS EXTINGUISHED. GEAR WAS CYCLED ONCE WITH NO CHANGE IN GEAR DOWN INDICATION. AN ALTERNATE GEAR EXTENSION, AND AIRCRAFT MANEUVERS WERE PERFORMED WITH NO IMMEDIATE CHANGE IN INDICATION. THE GEAR INDICATION ILLUMINATED ON THE 2 MILE FINAL APPROACH AND AN UNEVENTFUL LANDING WAS MADE. MAINTENANCE REPLACED THE RIGHT MAIN GEAR DOWN LOCK SWITCH. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4F RTA16SW 20050503002852005050300285SO 2005 5 3 C2XA05TY032 120050413A532014532636401 FLOOR SUPPORT EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712957 145080 TYS, DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT OMEGA BEAM BETWEEN FRAMES 23 + 30. MAINTENANCE REMOVED AND REPLACED THE OMEGA BEAM IAW EMB 135/145 SRM-51-40-02. 2L72 4F RTT00011AT 20050503002882005050300288 2005 5 3 DXTA200500672 420050411A2210 AUTOPILOT SYS CESSNA650 650 2076802CE COCKPIT MALFUNCTIONED E DXTAA UNSCHED LANDING O OTHER CLCLIMB 1 GL07715QS 6507105 AFTER TAKEOFF FROM KBAZ THE YAW DAMP AND AUTOPILOT FAILED TO ENGAGE. BOTH LEFT & RIGHT AP CHANNELS WERE ATTEMPTED WITH NO RESULTS. FLIGHT DIRECTOR FUNCTIONED NORMALLY. OPS CHECK A/P SYSTEM CHECK IS GOOD, POWER UP A/C FOR SEVERAL HRS CHECKING A/P OPS CHECK GOOD, ACCESS MAINT MODE ALL SYSTEMS PASSED. C/W GROUND MAINTENANCE TEST ON SP2-8000 SYSTEM ALL TEST PASSED, COULD NOT DUPLICATE MALFUNCTION SYSTEM, OPS CHECKS GOOD IAW 650 MM CH 34-21-01. 2L72 4F A9NM 20050503003022005050300302 2005 5 3 SWAA051069 420050411A2565D31354 SLIDE BOEING737 7373T0 1384582NM L1 DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29684WN 23941 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER UPON DOOR OPENING. SLIDE DID NOT DEPLOY. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20050503003042005050300304NM 2005 5 3 SWAA051071 120050412A534065C27314 STRINGER CLIP BOEING737 7373TO 138447GNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29697SW 23838 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727, BL 0. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050504000042005050400004NM 2005 5 4 05FDEA00926 120050410A5320ABA83561 SUPPORT BRACKET DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 FLOOR PANEL SUPPORT BRACKET AT STA 457 LBL 82 FOUND CORRODED. REMOVED IAW SRM 51-35-01 VOL II. FABRICATED NEW SUPPORT IAW DRAWING NR ABA8356 AND INSTALLED IAW SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20050504000062005050400006NM 2005 5 4 2005UALA00278 120050402A5754 SKIN BOEING BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 6 SLAT DELAMINATED A UALAO OTHER ED VIBRATION/BUFFET INFLIGHT SEPARATION DEDESCENT 1 WP29524UA A20316 24977 SLAT NR 6 TRAILING EDGE WEDGE DEPARTED THE AIRCRAFT. LEADING EDGE PANELS DAMAGED AFT OF THE NR 6 SLAT. DELAMINATION OF SLAT'S TRAILING WEDGE (INDUSTRY PROBLEM). WEDGE DAMAGED LEADING EDGE PANELS PRIOR TO DEPARTURE. NEW NR 6 LEADING EDGE SLAT INSTALLED. LEADING EDGE PANELS REPAIRED. 2L72 4F4 FRTA2NM E17NE 20050504000072005050400007NM 2005 5 4 2005UALA00279 120050403A3350 WIRE BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29179UA 25158 FIRST CLASS ALL LT EELS INOP. REPAIRED WIRING. 2L74 4F4 FRTA20WE E24NE 20050504000102005050400010NM 2005 5 4 2005UALA00288 120050401A5340 STRINGER CLIP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29309UA 23670 STATION 727A STRINGER CLIP IS CRACKED AT STR 20R. REPLACED STRINGER CLIP. 2L72 4F4 FRTA16WE E2GL 20050504000112005050400011NM 2005 5 4 2005UALA00289 120050401A5310 CREASE BEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29308UA 23669 CABIN CREASE BEAM CORRODED AT STA 294.5 RIGHT TO STA 328 RIGHT WL 207, RBL 60. REPLACED CREASE BEAM. 2L72 4F4 FRTA16WE E2GL 20050504000132005050400013NM 2005 5 4 2005UALA00291 120050401A5315 FLOORBEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29308UA 23669 AFT CABIN FLOORBEAM HAS EXCESSIVE MATERIAL LOSS OF 15 PERCENT TO 88 PERCENT STA 947 LBL 43 TO RBL 52. REPLACED T-CAP. 2L72 4F4 FRTA16WE E2GL 20050504000142005050400014NM 2005 5 4 2005UALA00292 120050401A5315 FLOORBEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29308UA 23669 FLOORBEAM HAS LIGHT SURFACE CORROSION LOCATED STA 294.5 RT RBL 38. REPLACED HAT CHANNEL. 2L72 4F4 FRTA16WE E2GL 20050504000162005050400016NM 2005 5 4 2005UALA00295 120050404A335058781 WIRE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29301UA 23642 EMERGENCY LIGHT DIM FROM ROW 13ABC TO AFT GALLEY. REPLACED POWER CABLE. 2L72 4F4 FRTA16WE E2GL 20050504000182005050400018NM 2005 5 4 2005UALA00297 120050403A5330 BEAR STRAP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29309UA 23670 AFT CARGO DOOR CUTOUT HAS PRE-EXISTING CUTOUT IN BEAR STRAP FOR REPAIR. AFTER AFT FUSELAGE SKIN REPLACEMENT, INSTALLED DOUBLER/TRIPLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20050504000202005050400020NM 2005 5 4 2005UALA00301 120050405A335020131 BATTERY PACK BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29925UA 26646 EEL FLOOR LIGHTS INOP ROWS 3-11 ABC. REPLACED BATTERY PACK M1134 . 2L72 4F4 FRTA16WE E2GL 20050504000222005050400022NM 2005 5 4 2005UALA00305 120050406A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE AFT CARGO DR CUTDAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29308UA 23669 AFT CARGO DOOR CUTOUT FWD EDGE 20 INCHES FROM LOWER DOOR SILL, SUSTAINED DAMAGE MEASURING .2187 INCHES DEEP BY 4 INCHES LONG. INSTALLED TRIPLER EXT FUSE SKIN REPAIR 20" X 8". 2L72 4F4 FRTA16WE E2GL 20050504000242005050400024NM 2005 5 4 2005UALA00308 120050405A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29584UA 26706 AFT PIT STA 1580 AT STR 26L FRAME DENTED. FRAME DENT DAMAGE WAS TRIMMED AND A DOUBLER REPAIR WAS INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050504000262005050400026NM 2005 5 4 2005UALA00310 120050405A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29585UA 26709 AFT CABIN FLOORBEAM IS CORRODED AROUND FASTENERS AT APPROXIMATELY BS 1661 RBL 58. DAMAGE CAUSED BY FLOORBEAM CORROSION IN WET AREAS OF THE CABIN. NEW T-CAP WAS FABRICATED AND INSTALLED TO REPLACE THE DAMAGED PORTION OF THE FLOORBEAM. 2L72 4F4 FRTA2NM E17NE 20050504000282005050400028NM 2005 5 4 2005UALA00312 120050407A5330143N33206 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE GOUGED A UALAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP29594UA 28145 FUSELAGE SKIN ON LT SIDE BETWEEN STA 598 AND 604 AT STR 17L IS GOUGED. DAMAGE CAUSED BY CONTACT WITH GROUND EQUIPMENT. DAMAGE WAS CUTOUT AND DOUBLER WAS INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050504000302005050400030NM 2005 5 4 2005UALA00315 120050408A5330143N33206 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP29594UA 28145 LT FUSELAGE STA 599 TO 618 STRINGER 16L TO 17L. DAMAGE CAUSED BY CONTACT WITH GROUND EQUIPMENT. DAMAGE WAS CUTOUT AND DOUBLER REPAIR INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050504000312005050400031EA 2005 5 4 A6WA200540A 120050323A2150 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN COOLING CONTAMINATED A A6WAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL31404AW 7294 OVERBOARD COOL CAUTION AND IB COOL STATUS MESSAGE. INSPECTED DOOR AND FOUND CONNECTOR INSIDE DOOR WET. CLEANED AND DRIED CONNECTOR PLUG. OPS CHECK GOOD. (K) 2L72 4F4 FRTA21EA E15NE 20050504000322005050400032CE 2005 5 4 DJFA2005080 120050411A291045AS6502223 VALVE BEECH MU300 400A 1155402CE HYD SYSTEM MALFUNCTIONED E DJFAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA23484CW3203 RK334 KTEB TRIP ID NR814487 CREW REPORTED THAT AFTER TAKEOFF WHILE ATTEMPTING TO RETRACT THE LANDING GEAR, THE GEAR UNSAFE LIGHT REMAINED ILLUMINATED. AN ALTERNATE GEAR EXTENSION WAS INITIATED, AND THREE GREEN AND NO RED INDICATIONS WERE RECEIVED. A FLY-BY PAST THE TOWER WAS PERFORMED TO VERIFY GEAR POSITION. AN EMERGENCY WAS DECLARED AND AIRCRAFT LANDED IN KTEB WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE MAIN HYDRAULIC VALVE PACKAGE. ALTERNATE GEAR EXTENSION SYSTEM WAS BLED AND RETURNED TO IT'S NORMAL CONFIGURATION. OPERATIONAL AND LEAK CHECKS WERE GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4F RTA16SW 20050504000332005050400033NM 2005 5 4 AALA20050BB 120050410A3350 LIGHT BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21622AA 24580 DFW SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT 9D AND FORWARD INOPERATIVE. REPLACED THE FORWARD SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA2NM 20050504000382005050400038EU 2005 5 4 2005F00072 120050406A5343NB400075 ATTACH BRACKET BNORM BN2 BN2A26 1520226EU MLG STRUT BROKEN G O OTHER O OTHER LDLANDING 1 AL05298849172 101 847 GEAR LEFT HAND OLEO ATTACHMENT BRACKET FAILED DURING LANDING. A/C NOSED INTO THE MUD CAUSING MAJOR DAMAGE. PN NB-40-0075 IS COVERED UNDER AD2002-02-11 AND HAD 217 LANDINGS AND 101 HOURS SINCE LAST INSPECTION PER PAR (D)(1) OF AD. 1H72 3O A17EU 20050504000392005050400039NM 2005 5 4 FDE2005F00000 120050404A5347AEA732515 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 MAIN DECK - SEAT TRACK AT RIGHT HAND STA Y= 1371 TO Y= 1500, X= -75 CORRODED. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG.1 VOL. I. 2L73 4F RTA22WE 20050504000412005050400041NM 2005 5 4 05FDEA00914 120050410A5347AEA73256 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RT SEAT TRACK AT STA Y= 1361 - Y= 1381, X= -29, FOUND WITH CORROSION. MAIN DECK, RIGHT SEAT TRACK AT STA Y= 1351 - Y= 1381, X= -29 CUT AND REMOVED PER SRM 53-70-00 VOLUME I, FIGURE 1 AND SRM SRM 51-31-01 VOLUME II. REPAIR SEAT TRACK AND SPLICE FABRICATED PER SRM 53-70-00 VOLUME I FIGURE 1. REPAIR SEAT TRACK AND SPLICE INSTALLED PER SRM 53-70-00 VOLUME I, FIGURE 1 AND SRM 51-31-01 VOLUME II. 2L73 4F RTA22WE 20050609000022005060900002WP 2005 6 9 ASMF200505026 120050522A2760 CONTROL BOX DOUG DC9 DC981 3022081WP AUTO SPOILERS MALFUNCTIONED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23501AM 49188 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF AUTO SPOILERS FAILURES, SHUTTING DOWN THE ENGINES. THE CONTROL BOX WAS RESEATED, ENGINE ACTUATOR CONNECTOR WAS CHECKED AND OPERATIONAL TESTS WERE PERFORMED IAW MM 27-60-00. DURING OVERNIGHT SERVICE, ARMED AND AUTO SPOILER SHUTOFF TESTS WERE PERFORMED IAW MM 27-60-00, ALL CORRECT. 2L72 4F A6WE 20050504000432005050400043NM 2005 5 4 05FDEA00967 120050412A5711 SPAR DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE RT WING O/B FLAP I/B REAR SPAR MOUNTED HINGE ACTUATOR HOLE HAS EVIDENCE OF CORROSION. CORROSION REMOVED & FOUND I/B & O/B LUG HOLES EXCEED LIMITS PER CMM 57-44-08. 2L73 4F RTA22WE 20050504000452005050400045NM 2005 5 4 05FDEA00970 120050412A5711 SPAR DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE RT WING O/B FLAP O/B REAR SPAR MOUNTED HINGE ACTUATOR HOLE EVIDENT OF CORROSION. CORROSION REMOVED & FOUND I/B AND O/B LUG HOLES EXCEED LIMITS AS PER CMM 57-44-09. 2L73 4F RTA22WE 20050504000462005050400046NM 2005 5 4 05FDEA00922 120050410A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE RT HORIZONTAL STABILIZER UPPER BARREL NUT NR 01 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133. 2L73 4F RTA22WE 20050504000512005050400051EU 2005 5 4 SA05038 120050408A335032145410 EPSU AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT FAULTY A USAAK NONE L NO TEST ININSP/MAINT 1 EA19717UW3977 1069 THE LEFT CENTER EMERGENCY POWER SUPPLY UNIT WOULD NOT TEST. MAINTENANCE REPLACED THE LEFT CENTER EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20050504000542005050400054WP 2005 5 4 ABXA050090 120050411A7931M057281 INDICATOR DOUG DC8 DC861 3021952WP PWA JT3D JT3D3 52039NE ENG OIL PRES DEFECTIVE A ABXAE ENGINE SHUTDOWN Y ENGINE STOPPAGE CLCLIMB 1 GL23847AX383 46031 671216 ON TAKEOFF AND CLIMB, NR 3 ENGINE OIL PRESSURE CLIMBED TO 75 - 80 PSI. TOOK THROTTLE TO IDLE, PRESSURE WENT TO 60 PSI. SECURED NR 3 ENGINE. AIR TURN BACK. AFTER SECURING THE ENGINE, THE PRESSURE READ 14 PSI STATIC ON TAXI. REPLACED NR 3 ENGINE OIL PRESSURE INDICATOR. OPS CHECKED GOOD. 2L74 4F4 F 4A25 1E8 20050504000552005050400055NE 2005 5 4 T48R20050007 220050412A7200500094701 TURBINE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE NR 2 ENGINE SEPARATED B GTIAE ENGINE SHUTDOWN Y ENGINE STOPPAGE NRNOT REPORTED 1 GL09827NK283495128 49793 725674 ENGINE WAS REMOVED FROM N827NK NR 2 POSITION FOR IN FLIGHT SHUTDOWN. DISASSEMBLY AND INSPECTION REVEALED EVIDENCE OF A POSSIBLE INTERNAL OIL FIRE RESULTING IN THE HIGH PRESSURE TURBINE SHAFT FRACTURING. THE REAR TURBINE SECTION WAS SEVERELY DAMAGED WITH NO PENETRATION OF EXTERIOR CASES. 2L72 4F4 FRTA6WE E9NE 20050504000572005050400057EA 2005 5 4 AJC2005F00003 120050327A323175006000 SELECTOR VALVE CNDAIRCL600 CL6002B16 1900305EA GE CF34 CF34* NE NLG DOOR SHORTED E AJCAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA25601AD1190 5186 DEPARTED, ENROUTE, UPON GEAR RETRACTION THE NOSE GEAR DOOR OPEN LIGHT STAYED ILLUMINATED. THE CREW CYCLED THE GEAR BUT THE LIGHT REMAINED ILLUMINATED. THE AIRCRAFT RETURNED TO DEPARTURE WHERE IT LANDED SAFELY. TROUBLESHOOTING REVEALED NOSE GEAR SELECTOR VALVE INTERNALLY SHORTED. SELECTOR VALVE WAS REMOVED AND REPLACED. SERVICED NR 3 HYDR SYSTEM. PERFORMED GEAR SWING TEST IAW MM. AC RETURNED TO SERVICE. (K) (EA25200507171) 2L72 4F4 FRTA21EA E15NE 20050504000592005050400059EA 2005 5 4 AJC2005F00004 120050401A274056417005 CONTROL UNIT CNDAIRCL600 CL6002B16 1900305EA GE CF34 CF34* NE HORZ STAB TRIM FAILED E AJCAA UNSCHED LANDING G MULTIPLE FAILURE CLCLIMB 1 EA25601AD 5186 DURING CLIMB OUT, THE CREW REPORTED LOOSING THE NR1 AND NR2 PITCH TRIM CHANNELS. BOTH FAIL LIGHTS ILLUMINATED. THE AUTO PILOT DISENGAGED. THE AC DIVERTED WHERE IT LANDED SAFELY, CREW DID NOT DECLARE EMERGENCY. TROUBLESHOOTING REVEALED THAT THE HORIZ STABILIZER TRIM CONTROL UNIT (HSTCU) FAILED 2 CHANNELS. HSTCU WAS REMOVED AND REPLACEDAND A SATISFACTORY OPS CHECK WAS PERFORMED IAW MM. AIRCRAFT WAS RETURNED TO SERVICE. (EA25200507339) (K) 2L72 4F4 FRTA21EA E15NE 20050504000612005050400061EA 2005 5 4 VNAA0503011 120050321A7830 PISTON CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE THRUST REVERSER DAMAGED A VNAAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL05241PS 7909 IN FLIGHT (CLT TO ROC) THE L REV UNLOCKED CAUTION MESSAGE ILLUMINATED. THE CREW OF FLIGHT 2532 FOLLOWED THE QRH, RETURNED TO CLT, AND MADE AN UNEVENTFUL LANDING. PSA MAINTENANCE DEFERRED THE LT THRUST REVERSER AND C/W THE M FUNCTION IAW CRJ 200 MEL 78-30-01 B. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. ON 25MAR05 AFTER TROUBLESHOOTING, THE MEL WAS CLEARED BY LUBRICATING THE LT THRUST REVERSER PDU LOCK PISTON IAW CRJ 200 AMM 12-20-78-640-805. OPERATIONAL CHECKS WERE GOOD IAW CRJ 200 AMM 78-30-00-720-809. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050504000632005050400063 2005 5 4 VNAA0503013 420050327A3418 STALL WARNING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE MALFUNCTIONED A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL05209PS 7874 ON CLIMBOUT (PHL TO YOW) THE STALL FAIL CAUTION MESSAGE ILLUMINATED. THE CREW OF FLIGHT 2566 RETURNED TO PHL AND LANDED WITHOUT INCIDENT. PSA MAINTENANCE RESET POWER AND OPERATIONALLY TESTED THE STALL PROTECTION SYSTEM IAW CRJ 200 AMM 27-35-01-750-802. THE STALL SYSTEM TESTED GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050504000642005050400064EA 2005 5 4 VNAA0504001 120050402A3110 DISPLAY CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE COCKPIT FAILED A VNAAO OTHER O OTHER NRNOT REPORTED 1 GL05223JS 7892 DURING FLIGHT 2491 (CLT TO PIT) THE CAPTAIN'S DISPLAY CONTROL PANEL FAILED. THE CREW FOLLOWED THE QRH, TRANSFERRED CONTROLS, AND MADE AN UNEVENTFUL LANDING AT DESTINATION. MAINTENANCE FOUND CIRCUIT BREAKER C9 ON PANEL 4 OPEN. THE CIRCUIT BREAKER WAS CLOSED AND THE DISPLAY CONTROL PANEL WAS OPERATIONALLY TESTED IAW CRJ 200 AMM 34-25-04-710-801. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050504000652005050400065CE 2005 5 4 AJC2005F00005 120050326A3244M13701 TIRE BEECH 50 L23D 1152526CE LYC O480 GO480* 41527EA MLG FAILED E AJCAC ABORTED TAKEOFF C F.O.D. TOTAKEOFF 1 EA25102SF RLH62 AIRCRAFT`S LT MAIN TIRE FAILED DURING ITS TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AT APPROX 40 KNOTS WITHOUT INCIDENT. ADDITIONAL DAMAGE WAS DONE TO THE NOSE WHEEL AND RT MAIN TIRE DURING REMOVAL OF THE AC FRO THE RUNWAY BY THE AIRPORT AUTHORITY. MAINT WAS DISPATCHED TOT THE AIRCRAFT. EVALUATED THE DAMAGE AND REMOVED AND REPLACED THE NOSE WHEEL AND BOTH LT AND RT MAIN WHEEL ASSY AND THE LT MAIN AUX BRAKE LINE. AS A PRECAUTIONARY MEASURE A FERRY PERMIT WAS REQUESTED AND GRANTED. INSPECTED THE AC AND DEEMED IT SAFE FOR THE FERRY FLIGHT. AC WAS FERRIED, GEAR DOWN. AIRCRAFT WAS RETURNED TO SERVICE. (EA25200507343) (K) 1L72 3O3 O 5A4 E275 20050504000672005050400067NM 2005 5 4 UIEA200500041 120050328A5414 SKIN BOEING747 747271C 1384869NM GE CF6 CF650E2 30018NE NR 4 NACELLE CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15537MC 22403 D-CHECK, DURING SCHEDULE INSPECTION. THE STRUT SKIN ASSY EDGE ADJACENT TO THE PRECOOLER EXHAUST CUTOUT WAS FOUND CRACKED. SKIN ASSY INSPECTION CONFIRMED THAT CRACKS TERMINATED IN EXISTING FASTENER HOLES. NR3 STIFFENER WAS REINFORCED WITH A STEEL LOWER REPAIR ANGLE FROM STA 237 TO STA 254. EXISTING REINFORCED RIB INSTALLED AT NAC STA 248 WAS MODIFIED TO ACCOMMODATE REPAIR ANGLE INSTALLED NO NR 3 STIFFENER. DETAIL VISUAL INSPECT ALUMINUM SKIN ASSY INNER SURFACE AREA, BELOW NR3 STIFFENER FLANGE, FOR ABSENCE OF ANY CRACKS AND LOOSE FASTENERS EVERY C-CHECK, NOT TO EXCEED 18 MONTHS. EO ISSUED TO ACCOMPLISH THE INSPECTION. (K) 2L74 4F4 F A20WE E23EA 20050504000742005050400074NM 2005 5 4 UIEA200500043 120050330A5310 BEAM BOEING747 747271C 1384869NM GE CF6 CF650E2 30018NE FUSELAGE CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15537MC 22403 D-CHECK, DURING SCHEDULED INSPECTION, CRACKS WERE FOUND AT THE NOSE GEAR WELL ON THE VERTICAL BEAM WEBS AT LHS BS 280L, 300L, 320L AND 320R. DAMAGED PORTION OF THE VERTICAL BEAM WEB WAS TRIMMED OUT AND A NEW SECTION OF THE WEB WAS SPLICED IN. NOTE: THESE REPAIRS ARE SUBJECT TO CONTINUED INSP IAW SB. (K) 2L74 4F4 F A20WE E23EA 20050504000762005050400076EU 2005 5 4 USAA050020 120050101A5320 ANGLE AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW22421 0315 BFM - FOUND T-CAP CORRODED THREE AREAS, 5.5 SQUARE INCH TOTAL, .021 INCH DEEP, FRAME 44, LOWER BELLY T-CAP BETWEEN Y 130- Y 380. CORROSION LEVEL 2, TASK NR J7-190-5310C. REMOVED CORROSION, INSTALLED REPAIR ANGLE AND FILLERS PER EA 96112. (M) 2L72 4F RTA46NM 20050504000872005050400087CE 2005 5 4 20030825 120050311A56301294300433 WINDOW BEECH 1900 1900D 1154162CE EMERGENCY EXIT CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03184UX UE184 DURING ROUTINE INSPECTION, EMERGENCY EXIT 4C WINDOW PAN FOUND CRACKED AT RADIUS. REPLACED WINDOW PAN IAW EO. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA24CE 20050504000892005050400089CE 2005 5 4 20030824 120050310A5312 BULKHEAD BEECH 1900 1900D 1154162CE FUSELAGE CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03184UX UE184 DURING ROUTINE INSPECTION, BULKHEAD AT FRAME STATION 492.75 FOUND TO BE CRACKED WHERE IT ATTACHES TO TOP OF CARGO DOOR FRAME. REPAIRED IAW EO. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA24CE 20050504000912005050400091CE 2005 5 4 GUU2005F00009 120050413A55201016200131 BRACKET BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE RT ELEVATOR CORRODED A GUUAK NONE O OTHER ININSP/MAINT 1 SO294754218686 UE198 AT SCHEDULED ROUTINE MAINTENANCE, RT CENTER ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RT CENTER ELEVATOR HINGE BRACKET. (K) 2L72 4T4 TRTA24CE E26NE 20050504000942005050400094NE 2005 5 4 NACA20050007 220050303A8500R2800CB3 ENGINE DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE NR 3 MAKING METAL A NACAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CRCRUISE 1 AL032907F1132 1132 533265 P28443 NR 3 ENGINE SHUT DOWN DUE TO DOUBLE SHORTED SECONDARY ON NR 10 CYLINDER. PRELIMINARY INSPECTION FOUND INTERNAL FAILURE OF THE NR 3 ENGINE. NR 3 ENGINE REPLACED. 2L74 4R4 R A781 5E8 20050504000952005050400095EU 2005 5 4 USAA050183 120050117A53214E33691 FLOOR PANEL AIRBUS330 A330323 3930335EU PWA 4168 PW4168A NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW 0342 BFM - S1 CK - HEATED FLOOR PANEL, (12 INCHES X 1.5 INCH X 0.60 INCH AREA), CORROSION; LEVEL 2; TASK J7-270-53100, FR74-75, Y-1456, Z-240, PANEL NR 272JF. REPLACED ALUMINUM SKIN IAW TYP REP, SRM. (K) 2L72 4F4 FRTA46NM 20050504000962005050400096EU 2005 5 4 USAA050184 120050117A5347F5332371120400 SEAT TRACK AIRBUS330 A330323 3930335EU PWA 4168 PW4168A NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW21927 0342 BFM - S1 CHECK - SEAT TRACK, (3.0 X 0.50 X 0.03 AND 0.03 X 0.50 X 0.04); CORROSION; LEVEL 2; TASK J7-200-2580C SEAT TRACK, Y450, FR 53.7-55, Z240 MAIN CABIN FLOOR. INSTALLED NEW SEAT TRACK SECTION AND SPLICES IAW SRM. (K) 2L72 4F4 FRTA46NM 20050504000972005050400097EU 2005 5 4 USAA050185 120050117A53214E33711 FLOOR PANEL AIRBUS330 A330323 3930335EU PWA 4168 PW4168A NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW 0342 BFM - S1 CHECK - FLOOR PANEL HEATED, (12 INCHES X 36 INCHES X 0.50) CORROSION AND DELAM. FR 74-75, Y1456, X240 PANEL NR 271JF. REPLACED ALUNIMUM SKIN IAW TYP REP, SRM. (K) 2L72 4F4 FRTA46NM 20050504000982005050400098NM 2005 5 4 NACA20050010 120050411A291355097 PUMP BOEING727 72722C 138400FNM PWA JT8 JT8D7B 52053NE HYD SYSTEM LEAKING A NACAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 AL03792A 13 19195 654518 LOSS OF "A" SYS HYDRAULIC QUANTITY UPON GEAR RETRACTION AT TAKEOFF. REPLACED NR 2 A-SYSTEM HYDRAULIC PUMP. LEAK AND OP CHECK GOOD. 2L73 4F4 F A3WE E2EA 20050504001022005050400102EU 2005 5 4 USAA050393 120050322A5230 SKIN AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE CARGO DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19107US 1052 PIT - RON - AFT CARGO DOOR INNER, .7500 INCH CRACK, INNER SKIN LOWER FWD CORNER. CUT OUT DAMAGE, INSTALLED DOUBLER EA. (K) 2L72 4F4 FRTA28NM E38NE 20050504001032005050400103NM 2005 5 4 USAA050392 120050323A5330 SKIN BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19384US54179 22957 PIT - RON - SKIN, (2 INCH CRACK), 6.5 INCHES AFT OF BS 727D, JUST ABOVE S-24L. CUT OUT DAMAGE, INSTALLED DOUBLER IAW SRM. (K) 2L72 4F4 FRTA16WE E2GL 20050504001042005050400104NM 2005 5 4 USAA050398 120050324A5330 SKIN BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19384US 22957 PIT - RON - SKIN, (2 INCH CRACK), 6.5 INCHES AFT OF BS 727D JUST ABOVE S24L. CUTOUT DAMAGE INSTALLED DOUBLER IAW SRM. (K) 2L72 4F4 FRTA16WE E2GL 20050504001062005050400106NM 2005 5 4 USAA050431 120050330A5315 FLOORBEAM BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19440US39307 24811 CLT - Q4 - FLOORBEAM, (.5 INCH) CORROSION. STA 312, BL 0 TO RBL 10. SPLICED IN NEW T-CAP IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050504001072005050400107NM 2005 5 4 USAA050410 120050312A5330 SKIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19442US40275 24841 CLT - Q6 - FUSELAGE SKIN, (.5 INCH) CRACK., RT WW BEADED PRESSURE DECK STA 664RBL 40. INSTALLED FILLERS AND TRIPLER IAW TR. (K) 2L72 4F4 FRTA16WE E21EU 20050504001082005050400108NM 2005 5 4 USAA050390 120050324A5712 RIB BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19442US40275 24841 CLT - Q6 - RIB, (1.5 AND .3750 INCH) CRACK; H WING, ROB AT WS 505 UPPER FLANGE RADIUS 20 INCH FROM L/E OF RIB. INSTALLED REPAIR DOUBLER IAW EA. (K) 2L72 4F4 FRTA16WE E21EU 20050504001092005050400109NM 2005 5 4 USAA050411 120050310A5712 RIB BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU LT WING CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19442US40275 24841 CLT - Q6 - RIB, (2 EA- 1.5 INCH AND .3750 INCH) CRACK. LT WING RIB AT WS 505 UPPER FLANGE RADIUS 20 INCHES FROM L/E OF RIB. FABRICATED REPAIR DOUBLER IAW EA. (K) 2L72 4F4 FRTA16WE E21EU 20050504001102005050400110NM 2005 5 4 USAA050428 120050329A52306546921225XE SKIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU CARGO DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19442US40275 24841 CLT - Q6 - EXTERNAL SKIN, 1 INCH, CRACKED, FWD CARGO DOOR HANDLE CUTOUT. (K) 2L72 4F4 FRTA16WE E21EU 20050504001112005050400111NM 2005 5 4 USAA050436 120050331A5340 STRINGER CLIP BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19442US 24841 CLT - Q6 -TIE CLIP, (.5 INCH CRACK), STATION 578.0991, STRINGER 8R. REPLACED TIE CLIP IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050504001122005050400112EU 2005 5 4 BA05008 120050412A3350321431 BATTERY AIRBUS330 A330323 3930335EU EMERGENCY LIGHT DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW 315 PHL THE 2L DOOR EPSU BATTERY FAILED THE OPERATIONAL TEST. MAINTENANCE REPLACED THE EMERGENCY BATTERY ON DOOR 2L. OPERATIONALLY CHECKS OK. 2L72 4F RTA46NM 20050504001152005050400115NM 2005 5 4 USAA050429 120050328A5230 SKIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU CARGO DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19442US40275 24841 CLT - Q6 - EXTERNAL SKIN, (1 INCH CRACK), AFT CARGO DOOR HANDLE CUTOUT. INSTALLED DOUBLER. (K) 2L72 4F4 FRTA16WE E21EU 20050504001172005050400117NM 2005 5 4 USAA050438 120050331A5313 STRINGER BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19442US 24841 CLT - Q6 - STRINGER, (.250 INCH CRACK), STRINGER 4L, STATION 908.0906. INSTALLED SPLICE IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050504001202005050400120EU 2005 5 4 USAA050415 120050307A5347A53274005DAN2001SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW22938 0337 BFM - FOUND SEAT TRACK CORRODED 1.5 INCHES LONG BY 1 INCH WIDE BY .039 INCH DEEP, Y1959 BETWEEN FRAME FRAME 53.1-53.2. CUT OUT DAMAGED AREA AND REPLACED WITH NEW SEAT TRACK SECTION PER SRM 53-00-15 FIG 102 SH 2, 53-00-15. (M) 2L72 4F RTA46NM 20050504001212005050400121EU 2005 5 4 USAA050416 120050310A5347F5347721420300 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW22938 0337 BFM - FOUND SEAT TRACK CORRODED 2 INCH BY .5 INCH BY .030 INCH AND 2 INCH BY 1.5 INCH BY .041 INCH, Y-450 FRAME 68 - 72 Z-240. INSTALLED NEW SEAT TRACK PER SRM 53-00-15 FIG 101 SHEET 1. (M) 2L72 4F RTA46NM 20050505000042005050500004EA 2005 5 5 A6WA200540126 120050325A2840 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CAS SYS ILLUMINATED A A6WAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL31438AW 7748 AT 32,000 FT, A FUEL IMBALANCE CAS MESSAGE APPEARED ON EICAS. THE PROBLEM WAS NOT CORRECTABLE USING AUTO, MANUAL OR GRAVITY CROSSFLOW. LT WING HEAVY AT LANDING AN IMBALANCE 1700 LBS C/W QRH. SHUTDOWN ENG NR 2, LANDING WEIGHT WAS NOT EXCEEDED. PERFORMED SYSTEM OPS CHECK OF FUEL CROSS FLOW, NO FAULTS FOUND, ALSO PERFORMED GRAVITY CROSSFLOW, NO FAULTS FOUND. REMOVED AND REPLACED FUEL COMPUTER SYSTEM, OPS CHECK GOOD. (K) 2L72 4F4 FRTA21EA E15NE 20050505000052005050500005EA 2005 5 5 A6WA200540127 120050327A2910601R752863 LINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE HYDRAULIC SYS CHAFED A A6WAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL31414ZW 7586 HYDRAULIC NR 1 LOW PRESSURE MESSAGE INFLIGHT ON CLIMBOUT. QUANTITY INDICATES ZERO. REMOVED AND REPLACED HYDRAULIC SUPPLY LINE TO CASE DRAIN ASSY REF 29-11-02, RAN ENGINE LEAK CHECK. OPS CHECK GOOD. (K) 2L72 4F4 FRTA21EA E15NE 20050505000092005050500009EA 2005 5 5 A6WA200540128 120050404A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FLOOR SUPPORT CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31416AW 7603 FLOOR SUPPORT BEAM CLIP AS FS280, LBL 9.0, OB IS CRACKED IN RADIUS APPROX 0.30. REMOVED AND REPLACED ANGLE P/N 601R31113-57 IAW CRJ 200 SRM 51-42-06, 51-42-21 AND BRAS EO 601R-53-6212. (M) 2L72 4F4 FRTA21EA E15NE 20050505000112005050500011WP 2005 5 5 ARWA20050503 120050412A2421 GENERATOR DOUG DC8 DC863F 302198FWP NR 4 TRIPPED A ARWAD RETURN TO BLOCK HJ ELECT. POWER LOSS-50 PC WARNING INDICATION TXTAXI/GRND HDL 1 SO19906R 46087 ON TAXI OUT, NR 4 GENERATOR TRIPPED OFF. 2L74 4F 4A25 20050505000132005050500013EA 2005 5 5 A6WA200540132 120050404A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FLOOR SUPPORT CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31416AW 7603 FLOOR SUPPORT BEAM CLIP AT FS 280, RBL 9 OB IS CRACKED IN RADIUS APPROX 0.52 INCH. (K) 2L72 4F4 FRTA21EA E15NE 20050505000142005050500014EA 2005 5 5 A6WA200540133 120050404A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FLOOR SUPPORT CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31416AW 7603 FLOOR SUPPORT BEAM CLIP AT FS484, LBL 36, IS CRACKED FROM TOP RIVET HOLE TO EDGE APPROX. (0.30 INCH). (K) 2L72 4F4 FRTA21EA E15NE 20050505000352005050500035CE 2005 5 5 DXTA200500675 120050411A323099147282 LOGIC CARD CESSNA750 750 2076810CE NLG FAILED E DXTAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL07984QS3714 7500084 NOSE GEAR BUMPS DURING CLIMB-OUT AT MID TO UPPER 20,000 FT 300KTS INDICATED (CREW STATES NO CHANGE IN GEAR UP INDICATION). REMOVED AND REPLACED LOGIC CARD NC002 IAW 750MM 24-53-00. COMPLIED WITH GEAR BUMP TROUBLESHOOTING IAW 750MM 32-30-00. 2L72 4J RTT00007WI 20050505000402005050500040NM 2005 5 5 SWAA051074 120050412A335008163 LIGHT BOEING737 7377H4 1384404NM AFT CABIN DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29747SA 29799 DURING SCHEDULED MV3 CHECK, FOUND AFT CABIN EEPLS STRIP DELAMINATED. REMOVED AND REPLACED EEPLS STRIP PER MM. 2L72 4F RTA16WE 20050505000412005050500041NE 2005 5 5 637041005 220050410A73211501KDC05010 FUEL CONTROL GULSTMGV GULFSTREAMGV3980116SO RROYCEBR700 BR700710A110 NE ENGINE FAILED E N93AA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO13509QS3947 637 ENG MAINT AMBER CAS MESSAGE. 2L72 4F4 FRTA12EA E00057EN 20050505000422005050500042NM 2005 5 5 72300155 120050411A5330 SKIN BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 10.5 X 25 INCH AREA OF CORROSION ON SKIN INTERIOR. 2L73 4F4 FRTA3WE E2EA 20050505000512005050500051SO 2005 5 5 SIMA7330791S 120050320A4900M450443A APU EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL APU BAY FAILED A SIMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21733KR 145368 CREW NOTED JUST AFTER TAKEOFF AND IN CRUISE FLT THEY STARTED GETTING A BAD ODOR IN THE CABIN, SO THEY RETURNED TO DEPARTURE FOR MAINTENANCE. THEY LANDED SAFELY BUT DID A EMERGENCY EVAC AC ON TAXIWAY. MAINTENANCE PERFORMED INSPECTIONS OF DUCTING AND SEVERAL COMPARTMENTS. COULD NOT FIND EVIDENCE OF FLUIDS OR ODOR. ISSUED MEL FOR APU. INSPECTED APU COMPARTMENT, ECS COMPARTMENT, ENG COWLING, AND PERFORMED OPS CHECK OF APU. RAI APU IAW MM WORKCARD NR 49-800-05. (K) 2L72 4F4 FRTT00011ATTE6CH 20050505000522005050500052EA 2005 5 5 COMA0560250 120050412A3260 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA MLG ILLUMINATED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01819CA 7415 FLIGHT 5420 GEAR DISAGREE WARNING IN TURBULENCE WITH FLAPS AT -0-. SECOND ATTEMPT WITH FLAPS AT 8 DEGREES WAS NORMAL. SYSTEM OPERATION NORMAL PER AFM, NO MAINT REQUIRED. 2L72 4F RTA21EA 20050505000532005050500053SO 2005 5 5 SIMA200507003 120050320A4900M450443A APU EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL TAIL LEAKING A SIMAA UNSCHED LANDING KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21733KR6122 147 145368 CREW REPOARTED DURING CRUISE FLIGHT GETTIG A BAD ODOR IN THE CABIN. AIRCRAFT WAS RETURNED TO DEPARTURE. AIRCRAFT WAS LANDED SAFELY AND AN EMERGENCY EVACUATION WAS DONE ON THE TAXIWAY. REPLACED APU IAW WORK CARD 49-800-05. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (K) 2L72 4F4 FRTT00011ATTE6CH 20050505000542005050500054EA 2005 5 5 COMA0560251 120050411A7930 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA OIL SYSTEM ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01498CA 7792 FLIGHT 5837 ENGINE OIL PRESSURE WARNING. INSPECTED ENGINE OIL SYSTEM, NO DEFECTS FOUND, GROUND RIMS WERE SATISFACTORY. COULD NOT DUPLICATE. 2L72 4F RTA21EA 20050505000572005050500057EA 2005 5 5 COMA0560252 120050411A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01409CA 7441 FLIGHT 5811 FLAPS FAIL CAUTION. INSPECTED FLAP SYSTEM IAW AD 98-20-01. NO DEFECTS FOUND. COULD NOT DUPLICATE. 2L72 4F RTA21EA 20050505000582005050500058SO 2005 5 5 SIMA200509101 120050325A532014525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21702AE11700 145164 THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 24-25. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED A DOUBLER, FILLER, AND 2 SHIMS. REPAIR DONE IAW SRM. (SW21200504814) (K) 2L72 4F4 FRTT00011ATTE6CH 20050505000592005050500059EA 2005 5 5 COMA0560253 120050411A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCONNECTED A COMAK NONE O OTHER ININSP/MAINT 1 SO01494CA 7765 FLIGHT 5595 LT FWD CABIN EMERGENCY LIGHT AT ROW 1 IS INOP. FOUND THE WIRING DISCONNECTED, RECONNECTED WIRING. 2L72 4F RTA21EA 20050503001862005050300186 2005 5 3 2005UALA00284 420050315A2565 O-RING BOEING757 757222 1384956NM PWA 2037 PW2037 NE EVAC SLIDE LEAKING A UALAK NONE O OTHER ININSP/MAINT 1 WP29583UA 26705 LOW BOTTLE PRESSURE. RESERVOIR/VALVE ASSEMBLY PRESSURE GAGE O-RING LEAKING. REPLACED O-RING. 2L72 4F4 FRTA2NM E17NE 20050503001882005050300188NM 2005 5 3 2005UALA00298 120050406A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29594UA 28145 FUSELAGE SKIN DENTED OVER FRAME AT STA 560 BETWEEN STRINGERS 16L AND 17L. DENT IS .070 INCH DEEP. DENT WAS CUTOUT AND THE FUSELAGE SKIN REPAIRED USING A DOUBLER. 2L72 4F4 FRTA2NM E17NE 20050503002042005050300204NM 2005 5 3 2005UALA00313 120050407A3620 WARNING SYSTEM BOEING757 757222 1384956NM PWA 2037 PW2037 NE COCKPIT ACTIVATED A UALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP29573UA 26685 CREW ABORTED TAKEOFF AT APPROXIMATELY 105 KNOTS NECESSARY TO LOCK OUT LEFT HIGH STAGE VALVE. PRIMARY CAUSE OF FAILURE WAS PRESSURE REGULATOR. REPLACED HIGH STAGE PILOT. 2L72 4F4 FRTA2NM E17NE 20050503002072005050300207EU 2005 5 3 RAI00504001 120050401A5270 WARNING SYSTEM JETAIRJETSTMJETSTM4101 1500501EU COCKPIT ACTIVATED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03557HK 41074 SYR - POD DOOR WARNING LIGHT ILLUMINATED. MAINTENANCE DEFERRED POD DOOR PER MEL 52-4 CAT C. 2L72 4T RTA41NM 20050503002092005050300209SO 2005 5 3 RAI00504003 120050404A3150 WARNING SYSTEM EMB 145 EMB145LR 3260212SO COCKPIT MALFUNCTIONED A RAIAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 CE03850HK 145003 MDT- NO TAKEOFF CONFIG AND TRIM WARNING ON TAKEOFF. MAINTENANCE PERFORMED TAKEOFF CONFIG TEST. NO DEFECTS NOTE. 2L72 4T RTT00011AT 20050503002102005050300210SO 2005 5 3 RAI00504004 120050404A4930 PRESSURE SWITCH EMB 145 EMB145ER 3260211SO APU LEAKING A RAIAA UNSCHED LANDING KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 CE03808HK 145157 DAY - STRONG FUEL SMELL IN THE COCKPIT, AFTER TAKEOFF. MAINTENANCE INSPECTED AIRCRAFT FOUND APU FUEL PRESS SWITCH LEAKING. DEFERRED APU PER MEL 49-00-00. 2L72 4F RTT00011AT 20050503002212005050300221NM 2005 5 3 SB05045 120050405A335030043211 LIGHT BOEING737 7373B7 1384580NM AFT GALLEY INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19353US 23556 PIT LEFT AFT GALLEY EMERGENCY LIGHT FOUND INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. 2L72 4F RTA16WE 20050503002252005050300225NM 2005 5 3 UALA200504AA 120050406A5330 SKIN BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE DENTED D UALAK NONE O OTHER ININSP/MAINT 1 SO15953UA 26700 FOUND FUSELAGE EXTERNAL SKIN HAS A GROUP OF DENTS FROM BS 380-400 BETWEEN STR. 15L-17L. S/O 269010, N/R 22034 2L72 4F4 FRTA16WE E21EU 20050503002462005050300246SO 2005 5 3 RAI00504008 120050408A3242 BRAKE EMB 145 EMB145 3260210SO MLG MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03806HK 145112 PIT - OUTBOARD BRAKE MESSAGE INOP. MAINTENANCE INSPECTED AND RESET OUTBOARD BRAKES. NO EICAS MESSAGE NOTED. 2L72 4F RTT00011AT 20050503002492005050300249EU 2005 5 3 RAI00504009 120050409A3250 STEERING SYS JETAIRJETSTMJETSTM4101 1500501EU NLG MALFUNCTIONED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03567HK 41085 STL - NOSE WHEEL STEERING OFF RACK. MAINTENANCE RERACKED NOSE WHEEL STEERING, AND PERFORMED TEST OF NOSE WHEEL STEERING. 2L72 4T RTA41NM 20050503002502005050300250GL 2005 5 3 RAI00504010 320050409A6110B5JFR36C1103 PROPELLER JETAIRJETSTMJETSTM4101 1500501EU MCAULY5JFR36B5JFR36C1103GL NR 1 MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03563HK15198 41079 001337 RIC - PROP HEAT FAULTED. MAINTENANCE REMOVED AND REPLACED NR 1 PROP, LEAK CHECKS GOOD. 2L72 4T RTA41NM 6 CP15NE 20050503002522005050300252SO 2005 5 3 RAI00504011 120050410A2120 SMOKE EMB 145 EMB145 3260210SO COCKPIT DETECTED A RAIAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CE03806HK 145112 PIT - SMOKE IN COCKPIT AFTER STARTING ENGINE NR 1. MAINTENANCE RAN NR 1 ENGINE, NO SMOKE DETECTED. INSPECTED ELECTRICAL SYSTEM. 2L72 4F RTT00011AT 20050503002532005050300253SO 2005 5 3 RAI00504012 120050407A243430086011 GENERATOR EMB 145 EMB145LR 3260212SO NR 1 FAILED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03834HK7537 145269 STL - GENERATOR NR 1 OFF BUS AFTER START. RESET GENERATOR NR 1 SWITCH, STILL NO GENERATOR AMPS. MAINTENANCE REMOVED AND REPLACED NR 1 GENERATOR. 2L72 4T RTT00011AT 20050503002542005050300254SO 2005 5 3 RAIOO504013 120050409A2913MPEV30086 PUMP EMB 145 EMB145LR 3260212SO HYDRAULIC SYS FAILED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03813HK10493 145044 STL - HYD PUMP INOP. MAINTENANCE REMOVED AND REPLACED NR 1 ELECTRIC HYD PUMP. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050503002562005050300256WP 2005 5 3 91500002 120050412A5320 DOUBLER DOUG DC9 DC915F 3022037WP PWA JT8 JT8D9A 52048NE FUSELAGE CRACKED A K11AK NONE O OTHER ININSP/MAINT 1 GL23915CK 47086 A 1.375 INCH LONG CRACK IN ACCESS DOOR DOUBLER. 2L72 4F4 F A6WE E2EA 20050503002592005050300259WP 2005 5 3 0500451233 120050409A7810NWSA7810010242 NOZZLE DOUG DC10 DC1030 3023501WP GE CF6 CF650C 30018GL NR 2 ENGINE DEPARTED A NWAAK NONE D INFLIGHT SEPARATION CLCLIMB 1 GL01233NW2661617436 46640 517700 AFTER TAKEOFF FROM MSP, THE NR 2 ENGINE EXHAUST NOZZLE DEPARTED FROM THE AIRCRAFT. THERE WERE NO ABNORMAL AIRCRAFT OR ENGINE INDICATIONS SO THE CREW WAS UNAWARE OF THE CONDITION. THE FLIGHT CONTINUED TO HNL WITHOUT INCIDENT. MAINTENANCE INSTALLED A REPLACEMENT EXHAUST NOZZLE IN HNL. OPERATIONAL CHECK GOOD. 2L73 4F4 F A22WE A23EA 20050503002652005050300265EA 2005 5 3 VNAA0503012 120050309A2740 TRIM SYSTEM CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE HORIZ STAB MALFUNCTIONED A VNAAK NONE FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 GL05706PS 10150 THE STAB TRIM CAUTION MESSAGE ILLUMINATED IN FLIGHT. THE CREW OF FLIGHT 2239 FOLLOWED THE QRH, CONTINUED TO DESTINATION, AND MADE AN UNEVENTFUL LANDING. MAINTENANCE RESET THE STAB TRIM SYSTEM IAW CRJ 700 SERVICE LETTER SL-27-028. THE MESSAGE CLEARED AND THE STAB TRIM SYSTEM OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050503002672005050300267EA 2005 5 3 QXEA200500562 120050321A2550 RAIL CNDAIRCL600 CL6002C10 1390015EA CARGO BAY DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FORWARD FUSELAGE, FORWARD CARGO COMPARTMENT RETRIEVAL TRAY RAILS, RIGHTHAND AFT INBOARD RAIL HAS ANODIZED COATING COMING OFF. REPAIRED IAW CRJ700 SRM 51-21-11-001-001-A01 AND SRM 51-21-06-001-001-A01. 2L72 4F RTA21EA 20050503002692005050300269SO 2005 5 3 C2XA05SH023 120050407A33503025101 LIGHT EMB 145 EMB145ER 3260211SO EXTERIOR INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714940 145033 SHV - DURING A SERVICE/ROUTINE CHECK THE RIGHT EXTERNAL OVERWING EMERGENCY LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY IAW EMB 145 AMM 33-50-10. THE ENSUING OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050503002712005050300271WP 2005 5 3 0500469954 120050329A5311 FRAME DOUG DC9 DC931 3022065WP FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01921RW 47164 DURING M-CHECK FOUND CORROSION ON FRAME AT BS 996. REPAIRED PER EA 99-203328. 2L72 4F A6WE 20050503002732005050300273WP 2005 5 3 0500489611 120050401A5711 SPAR CAP DOUG DC9 DC932 3022066WP RT WING CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01611NA 47435 DURING M-CHECK FOUND CRACK IN RT WING REAR SPAR CAP AT XRS 267. REPAIRED PER EA 96-201450. 2L72 4F A6WE 20050503002752005050300275WP 2005 5 3 0500509602 120050309A5320 STIFFENER DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01602NW 47046 DURING M-CHECK FOUND CRACK IN BULKHEAD VERTICAL STIFFENER AT BS 756 L28R. REPAIRED PER EA 96-202516. 2L72 4F A6WE 20050503002792005050300279CE 2005 5 3 DJFA2005076 120050407A793030714374 CHIP DETECTOR CESSNA650 650 2076802CE GARRTTTFE731TFE7313 01518WP RT ENGINE FALSE ACTIVATIONE DJFAE ENGINE SHUTDOWN N FALSE WARNING APAPPROACH 1 EA23359CW 6500159 P87109 KTEB - KBOS TRIP ID NR 781356 CREW REPORTED THEY RECEIVED A RIGHT ENGINE CHIP DETECTOR LIGHT WHILE ON APPROACH. THE RIGHT ENGINE WAS SECURED AND AN UNEVENTFUL LANDING WAS MADE IN KBOS. MAINTENANCE INSPECTED THE RIGHT ENGINE OIL CHIP DETECTOR AND FOUND NO DISCERNABLE CONTAMINATION. THE CHIP DETECTOR WAS CLEANED AND INSTALLED INTO THE LEFT ENGINE. THE LEFT ENGINE CHIP DETECTOR WAS INSTALLED INTO THE RIGHT ENGINE FOR TROUBLESHOOTING. A GROUND ENGINE RUN WAS PERFORMED FOR 25 MINUTES WITH NO CHIP DETECTOR LIGHT ILLUMINATING. THE SUSPECT CHIP DETECTOR WAS REMOVED FROM THE LEFT ENGINE WAS REPLACED. AIRCRAFT WAS RETURNED TO SEVICE. 2L72 4F4 F A9NM E6WE 20050503002822005050300282NE 2005 5 3 ANCF200400046 220050405A7200 BLADE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE ENGIEN DAMAGED B ANCFK NONE O OTHER ININSP/MAINT 1 SO23190AN 53190 726846 DURING OVERNIGHT SERVICE WAS ACCOMPLISHED EO 83-72-007 BORESCOPE INSPECTION FIRST AND SECOND STAGE TURBINE BLADES AND FOUND ON RT ENGINE TWO BLADES WITH CRACKS ON TRAILING EDGE CONCAVE SIDE OF FIRST STAGE TURBINE. THE ENGINE HAS BEEN REMOVED IAW AMM 72-00-00, 71-00-00 AND WILL BE SENT TO THE SHOP. THAT ENGINE WAS PREVIOUSLY REPAIRED ON IAI (ISRAEL AIRCRAFT INDUSTRIES) SHOP AND HAD 1924.39 HRS OF OPERATION 2L72 4F4 FRTA6WE E9NE 20050503002932005050300293NM 2005 5 3 AWXA200500450 120050310A533065C337568 SKIN BOEING737 737375 13844BNNM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 MCN - MAJOR REPAIR - DURING C-05 CHECK A .625 INCH CRACK WAS FOUND IN SKIN AT R-1 DOOR FRAME CUTOUT IN LOWER AFT CORNER ABOVE STR 17 RT, BS 328. MAINTENANCE CUT OUT CRACK IN SKIN AT R-1 DOOR FRAME CUTOUT LOWER AFT CORNER STR 17 RT, BS 328. FABRICATED OUTER, INNER, & MIDDLE PLATES, 2 EACH FILLERS, AND A TAPERED FILLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-01, FIG 202. 2L72 4F RTA16WE 20050503002942005050300294NM 2005 5 3 SWAA051061 120050412A5311BAC1489 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME U-CHANNEL CRACKED AT BS 360, STR 14L. REPAIRED U-CHANNEL PER SRM. 2L72 4F RTA16WE 20050503002952005050300295 2005 5 3 SWAA051062 420050412A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29320SW 23341 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20050503002962005050300296NM 2005 5 3 SWAA051063 120050411A3350101073 LENS BOEING737 7373H4 1384600NM R2 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29330SW 23694 DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2L72 4F RTA16WE 20050503002972005050300297NM 2005 5 3 SWAA051064 120050412A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29336SW 23940 DURING SCHEDULED RON CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS AT BS 747 & BS 727 E, STR 16R. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050503002982005050300298NM 2005 5 3 SWAA051065 120050412A335007912 COVER BOEING737 7377H4 1384404NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29478WN 33989 DURING SCHEDULED MV2 CHECK, FOUND FWD END OF EEPLS COVER CRACKED. REMOVED AND REPLACED COVER PER MM. 2L72 4F RTA16WE 20050503002992005050300299NM 2005 5 3 SWAA051066 120050412A3397 WIRE BOEING737 7373H4 1384600NM COCKPIT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED SERVICE CHECK, FOUND COCKPIT EMERGENCY LIGHT INOP. REPAIRED BROKEN WIRE PER MM. 2L72 4F RTA16WE 20050503003002005050300300NM 2005 5 3 SWAA051067 120050412A3350612825 BATTERY BOEING737 7373A4 1384585NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20050503003012005050300301 2005 5 3 SWAA051068 420050412A2565D31354 SLIDE BOEING737 7373Y0 1384671NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050503003032005050300303NM 2005 5 3 SWAA051070 120050412A53126546568 BULKHEAD BOEING737 7373TO 138447GNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29697SW 23838 DURING SCHEDULED 1/4D CHECK, FOUND 2 EA CRACKS AT BS 1016 BULKHEAD WEB DOME CAP, 12 O'CLOCK POSITION. REPAIRED PER SWA EA. 2L72 4F RTA16WE 20050503003052005050300305NM 2005 5 3 SWAA051072 120050412A53406546529 SHEAR TIE BOEING737 7373TO 138447GNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29697SW 23838 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON SHEAR TIE AT BS 520, STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050504000022005050400002 2005 5 4 05FDEA00959 420050408A3460 COMPUTER AIRBUS310 A310222 3930315EU FLT DIRECTOR FAILED A FDEAA UNSCHED LANDING JG WARNING INDICATION MULTIPLE FAILURE CLCLIMB 1 SO25455FE 331 AFTER TAKEOFF THE FMS'S WENT INTO INDEPENDENT OPERATION COMPLIED WITH QRH WITHOUT SUCCESS. F/O FLT DIR NR 2 LOST 34-73/3234. F/O LOST EFIS/SGU, DIA LINE ON NA & PFD. REPLACED AND CORRECTION FOR ALL 3 WRI'S. PERFORMED ADJ/TEST PER RELATED AMM WDM 34-73-01, 34-65,01 FOUND CHAFFING AT 22XU TRANSFORMER CURRENT GEN. 2 REPAIRED CHAFING PER SMP AND "A" REPLACED BURNED PIN & CONNECTOR ON IDG FEEDER CABLE AT PYLON CONNECTION OPS CHECK ALL SYSTEMS ON ENGINE RUN. 2L72 4F RTA35EU 20050504000032005050400003NM 2005 5 4 05FDEA00958 120050411A5330 DOUBLER BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 REPAIR AT EXTERNAL DOUBLER BS 990 TO BS 1000 BL 0 WL 148, 18 INCHES BY 18.5 INCHES NEEDS EVALUATION TO DETERMINE PER SRM OR APPROVED DATA. REPAIRED DOUBLER PER FED EX EA 7-5330-86271 2L73 4F RTA3WE 20050504000052005050400005NM 2005 5 4 05FDEA00939 120050411A5512ALC8101501 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT HAND UPPER FORWARD SKIN PLANK NR 3L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82939 2L73 4F RTA22WE 20050504000122005050400012NM 2005 5 4 2005UALA00290 120050401A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29308UA 23669 AFT FUSELAGE DENT AT STA 996 FOUR INCHES ABOVE STR 14L. REMOVED DAMAGED AREA AND INSTALLED DOUBLER. 2L72 4F4 FRTA16WE E2GL 20050504000152005050400015NM 2005 5 4 2005UALA00294 120050404A5310 DOOR FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29308UA 23669 DOOR 1R LOWER FRAME CRACKED (LOWER AFT CORNER). REPLACED FRAME. 2L72 4F4 FRTA16WE E2GL 20050504000172005050400017NM 2005 5 4 2005UALA00296 120050404A275118196917 SENSOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE RT OUTBRD FLAP FAILED A UALAO OTHER N FALSE WARNING DEDESCENT 1 WP29581UA 26701 UPON DESCENT, CREW RETRACTED FLAPS AND RECEIVED A FLAP TRAILING EDGE SYS INDICATION. A FAILED FLAP POSITION SENSOR INITIATED A FAILURE PROTECTION SHUTDOWN OF TE FLAP SYSTEM BY THE FLAP SLAT ELECTRONICS UNIT (FSEU NR 1 AND 2), WHICH IN TURN ILLUMINATED TE MASTER CAUTION LIGHT WITH A TE DISAGREE MESSAGE ON EICAS. REPLACED TRANSMITTER. 2L72 4F4 FRTA2NM E17NE 20050504000252005050400025NM 2005 5 4 2005UALA00309 120050407A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29584UA 26706 DENT WAS FOUND AT BS 1708 STR 17R APPROX 2 INCHES LONG. DENT DAMAGE ON FUSELAGE SKIN CAUSED BY IMPACT. DAMAGE TO THE SKIN WAS CUTOUT AND A DOUBLER, TRIPLER, AND FILLER REPAIR STACKUP WAS INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050504000272005050400027NM 2005 5 4 2005UALA00311 120050407A5330141N33319 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP29594UA 28145 FUSELAGE SKIN ON LT SIDE BETWEEN STA 418 AND 435 AT STR 17L IS DAMAGED. DAMAGE CAUSED FROM CONTACT WITH GROUND EQUIPMENT. DAMAGE WAS CUTOUT AND A REPAIR DOUBLER INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050504000292005050400029NM 2005 5 4 2005UALA00314 120050407A5330143N33206 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP29594UA 28145 LT FUSELAGE STATION 440 TO 475, STRINGER 16L TO 17L. DAMAGE CAUSED BY CONTACT WITH GROUND EQUIPMENT. DAMAGE SKIN WAS CUTOUT AND DOUBLER REPAIR INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050504000562005050400056 2005 5 4 AJC2005F00002 420050327A34256229336400 AHRS ISRAEL1125 ASTRASPX 4500205EU PWA JT8 JT8D9A 52048NE NR 1 INTERMITTENT E AJCAO OTHER O OTHER LDLANDING 1 EA25387PA847 145 ON APPROACH THE NR 1 AHRS (ATTITUDE HEADING REFERENCE SYS) UNIT OPERATED INTERMITTENTLY, THE UNIT RED FLAGGED THE HEADING AND WAS UNABLE TO ENGAGE THE FLIGHT DIRECTOR. THE CREW WAS UNABLE TO SWITCH THE NR 2 AHRS TO DRIVE THE NR 1 SIDE. AC PROCEEDED AND LANDED SAFELY WITHOUT INCIDENT, DID NOT DECLARE AN EMERGENCY. TROUBLESHOT SYSTEM AND FOUND THE NR 1 AHRS AHC-85E COMPUTER WAS AT FAULT. REMOVED AND REPLACED UNIT. COMPLIED WITH AHRS ADJUSTMENT/ TEST IAW MM. OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (K) (EA25200507108) 2L72 4F4 FRTA16NM E2EA 20050504000602005050400060EA 2005 5 4 VNAA0503010 120050321A3000 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE ANTI ICE SYS ACTIVATED A VNAAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL05242JS 7911 MULTIBLE TIMES DURING THE FLIGHT THE CREW RECEIVED ANTI-ICE DUCT WARNING MESSAGES. THE CREW OF FLIGHT 2471 FOLLOWED THE QRH AND MADE AN UNEVENTFUL LANDING AT DESTINATION. MAINTENANCE PERFORMED AN OPERATIONAL TEST OF THE BLEED-AIR LEAK DETECTION AND WARNING SYSTEM IAW CRJ-200 AMM 36-21-00-710-801. ALL TESTS WERE GOOD. NO DEFECTS WERE NOTED AT THIS TIME. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050504000622005050400062EA 2005 5 4 VNAA0503014 120050327A2740 WARNING SYSTEM CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE STAB TRIM ACTIVATED A VNAAO OTHER O OTHER DEDESCENT 1 GL05719PS 10177 DURING DESCENT THRU 17000 (CLT TO CLE) THE MACH TRIM & STAB TRIM CAUTION MESSAGES ILLUMINATED. THE CREW OF FLIGHT 2239 DECLARED AN EMERGENCY AND MADE A SUCCESSFUL REDUCED FLAP LANDING IN CLE. MAINTENANCE CYCLED POWER AND OPERATIONALLY CHECK THE MACH TRIM & STAB TRIM SYSTEMS IAW CRJ 700 SL-27-028. THE SYSTEMS OPS CHECKED GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050504000662005050400066NM 2005 5 4 UIEA200500020 120050315A3260 PROXIMITY SENSOR BOEING747 74747UF 1384949NM GE CF6 CF680C2* GL MLG DOOR MALFUNCTIONED A UIEAO OTHER EN VIBRATION/BUFFET FALSE WARNING CLCLIMB 1 EA15493MC 29254 AFTER TAKEOFF GEAR CLOSED NORMALLY; INDICATED CLOSED GEAR LEVER SELECTED TO OFF; VIBRATION FELT, EICAS MSG (GEAR DOOR) AND SYNOPTIC INDICATED LT BODY GEAR DOOR NOT CLOSED. NNC 14.5 ACCOMPLISHED AND FLIGHT CONTINUED WITH GEAR LEVER IN UP POSITION. PERFORMED VISUAL CHECK ON LT BODY GEAR DOOR PROX SENSOR. NO DEFECT. PERFORMED PSEU GROUND TEST IAW MM. PERFORMED INSPECTION CK IAW MM NO DEFECT FOUND. 2L74 4F4 FRT1384945 E23EA 20050504000682005050400068NM 2005 5 4 UIEA200500042 120050329A541465B940533 SKIN BOEING747 747271C 1384869NM GE CF6 CF650E2 30018NE NR 3 PYLON CRACKED E UIEAK NONE O OTHER ININSP/MAINT 1 EA15537MC 22403 D-CHECK, DURING SCHEDULE INSPECTION, NR 3 PYLON, A 2.25 INCH CRACK WAS FOUND AT THE TOP EDGE OF SKIN ASSY AT NAC WL147.8, JUST FORWARD OF THE NAC STA 286. CRACK IN THE SKIN ASSY WAS CONTAINED WITH A 1.0 INCH DIAMETER HOLE AT THE CRACK TIP. REPAIR AREA WAS NDT INSP, INCLUDING HFEC INSPECTION OF THE SKIN ASSY TRIMMED EDGES AND ALL REPAIR FASTENER HOLES. SKIN ASSY WAS REINFORCED AT THE CRACK LOCATION WITH 2 LAYERS IF STAGGERED EXTERIOR ALUMINUM REPAIR DOUBLERS. REPAIR AREA IS TO BE GIVE A DETAILED VISUAL EVERY C-CHECK OR 18 MONTHS, TO ENSURE ABSENCE OF LOOSE FASTENERS, CRACKS, CORROSION AND ANY OTHER DAMAGE. EO ISSUED TO ACCOMPLISH INSPECTION. (K) 2L74 4F4 F A20WE E23EA 20050504000792005050400079EU 2005 5 4 USAA050178 120050125A5347F53477214200 SEAT TRACK AIRBUS330 A330323 3930335EU PWA 4168 PW4168A NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW21927 0342 BFM - S1 - SEAT TRACK, (1.0, 1.0, 0.32 INCH D; 1.5, 1.0, .040 D), CORROSION; LEVEL 2; TASK J7-200-2580C, Y450, FR 58 TO 67. INSTALLED NEW SEAT TRACK IAW SRM. (K) 2L72 4F4 FRTA46NM 20050504000812005050400081EU 2005 5 4 USAA050180 120050114A5310F53478017009 SUPPORT BEAM AIRBUS330 A330323 3930335EU PWA 4168 PW4168A NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW21927 0342 BFM - S1 CHECK- AUX BEAM SUPPORT - (1.5 INCH L X 1.5 INCH W X .060 INCH D); CORROSION; LEVEL 2; TASK J7-900-09000-043, FR71.8 - Y1400 - Z240. REMOVED AND REPLACED WITH NEW PORT SRM. (K) 2L72 4F4 FRTA46NM 20050504000842005050400084EU 2005 5 4 USAA050182 120050117A53214E33621 FLOOR PANEL AIRBUS330 A330323 3930335EU PWA 4168 PW4168A NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW21927 0342 BFM - S1 CK - HEATED FLOOR PANEL, (12 INCHES X 12 INCHES) CORROSION AND DELAM. CORROSION AND DELAMINATION; LEVEL 2; TASK J7-270-53100-001, FR 33-36, Y2820, Z240, PANEL NR 242 EF. REPLACED ALUMINUM SKIN IAW TYP REP, SRM. (K) 2L72 4F4 FRTA46NM 20050504000862005050400086CE 2005 5 4 20030822 120050310A53111294400345 FRAME BEECH 1900 1900D 1154162CE FUSELAGE CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03184UX UE184 DURING ROUTINE INSPECTION, FOUND WEB CRACK ON FRAME FS 466.0 STRINGER 10R. REPAIRED CRACK IAW WITH EO. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA24CE 20050504000882005050400088CE 2005 5 4 20030823 120050310A52601294000333 STRUCTURE BEECH 1900 1900D 1154162CE AIRSTAIR DOOR CORRODED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03184UX UE184 DURING ROUTINE INSPECTION, CORROSION DISCOVERED AROUND AIRSTAIR DOOR HANDLE APPROX 2 INCH IN DIA AREA REPAIRED IAW EO. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA24CE 20050504000992005050400099EU 2005 5 4 USAA050186 120050118A5347F53477214202 SEAT TRACK AIRBUS330 A330323 3930335EU PWA 4168 PW4168A NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW 0342 BFM - S1 CK - SEAT TRACK, (1.5 X 1.0 X 0.035 D) CORROSION; LEVEL 2; TASK NR J7-200-2580) Y450, FR 70-72. INSTALLED NEW SECTION OF SEAT TRACK IAW SRM. (K) 2L72 4F4 FRTA46NM 20050504001012005050400101EU 2005 5 4 USAA050187 120050118A5347F53477214202 SEAT TRACK AIRBUS330 A330323 3930335EU PWA 4168 PW4168A NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW 0342 BFM - S1 CK - SEAT TRACK, (.75 X .25 X 0.030 D), CORROSION; LEVEL 2; TASK J7-200-2580, Y450, FR 68-70. INSTALLED NEW SEAT TRACK IAW SRM. (K) 2L72 4F4 FRTA46NM 20050504001052005050400105NM 2005 5 4 USAA050427 120050316A5510 ATTACH ANGLE BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU HORIZONTAL STAB WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19440US39307 24811 CLT - Q4 - ATTACH ANGLE, (.75 INCH X .50 INCH) WORN, LT HORIZONTAL STABILIZER TIP BL249-81. REPLACED WITH FABRICATED ANGLE IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050504001132005050400113NM 2005 5 4 USAA050437 120050331A5313 STRINGER BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19442US40275 24841 CLT - Q6 - STRINGER, (.250 INCH CRACK) STRINGER 4R STA 908.0903. INSTALLED SLICE IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050504001162005050400116NM 2005 5 4 USAA050430 120050328A554265C2584151M SKIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU RUDDER DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19442US 24841 CLT - Q6 - RUDDER SKIN, (.5 INCH X .5 INCH) COMPOSITE DAMAGE, RUDDER T/E STA 151. ACCOMPLISHED COMPOSITE REPAIR IAW EA. (K) 2L72 4F4 FRTA16WE E21EU 20050504001182005050400118NM 2005 5 4 USAA050439 120050331A5340 SUPPORT ANGLE BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19442US 24841 CLT - Q6 - SUPPORT ANGLE, (.075 INCH) CRACK, STRINGER 11R, STATION 354. INSTALLED NEW ANGLE IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050505000062005050500006NM 2005 5 5 P9RA20050074 120050404A2910NAS161212 PACKING BOEING757 757231 1384950NM FLAP MODULE SPLIT A P9RAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO11715TW 30319 CRUISE FLT FL390, EICAS MESSAGE FOR LEFT SYSTEM HYDRAULIC FLUID LOW. FOLLOWED QRH PROCEDURE BUT FLUID LEVEL CONTINUED TO DECREASE. ALTERNATE EXTEND ON GEAR AND FLAPS. EMERGENCY DECLARED ON APPROACH INTO ATL. NORMAL LANDING FOLLOWED BY FULL STOP ON TAXIWAY. AIRCRAFT THEN TOWED TO GATE AREA. FOUND CUT O-RING ON THE DEPRESSURIZATION FLAP SLAT MODULE. REPLACED IAW M/M. FLUID LEVELS SERVICED TO NORMAL. NO FURTHER LEAKS NOTED. 2L72 4F RTA2NM 20050505000072005050500007EA 2005 5 5 A6WA200540134 120050402A3244 TIRE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT MLG DAMAGED A A6WAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL31437AW 7744 REQUEST INSPECTION LT MLG TIRE FOR WEAR. AC PASSENGERS AND CARGO WERE UNLOADED, AIRCRAFT DEFUELED. AIRCRAFT WAS TOWED ONT RAMP AREA. WITHOUT INJURY OR DAMAGE TO AIRCRAFT, GEAR SWING AND MLG BAY ACCOMPLISHED AND REMOVAL/REPLACEMENT LT MLG TIRES AS A PRECAUTIONARY MEASURE. (K) 2L72 4F4 FRTA21EA E15NE 20050505000122005050500012EA 2005 5 5 A6WA200540131 120050404A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FLOOR SUPPORT CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31416AW 7603 FLOOR SUPPORT BEAM CLIP AT FS 280, RBL 9 IB IS CRACKED IN RADIUS APPROX ( 0.50 INCH). (K) 2L72 4F4 FRTA21EA E15NE 20050505000392005050500039NM 2005 5 5 SWAA051073 120050412A53306545765 SKIN BOEING737 7373TO 138447GNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29697SW 23838 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D + 2, STR 12R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050505000442005050500044NM 2005 5 5 72300157 120050412A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 2 INCH AREA OF CORROSION ON STRINGER. 2L73 4F4 FRTA3WE E2EA 20050505000602005050500060SO 2005 5 5 SIMA200509102 120050325A532014525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21702AE11700 145164 THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 24. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED AN EXTERNAL DOUBLER, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (SW21200504814) (K) 2L72 4F4 FRTT00011ATTE6CH 20050505000622005050500062GL 2005 5 5 SIMA200509114 220050328A7200AE3007A CARBON SEAL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL RT ENGINE LEAKING A SIMAO OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21906AE197 14500894 CREW REPORTED SMOKE AND FUMES IN CABIN. FOUND OIL LEAKING FROM NR 2 ENGINE CARBON SEAL. REPLACED NR 2 ENGINE IAW WC. OPS CHECK GOOD, AC RETURNED TO SERVICE. (SW21200504808) (K) 2L72 4T4 FRTT00011ATTE6CH 20050505000642005050500064EA 2005 5 5 COMA0560254 120050409A2750 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01934CA 7042 FLIGHT 5854 FLAPS FAIL CAUTION MESSAGE AFTER LANDING. C/W RIGGING MAINT OF THE FLAP SYSTEM BPSU'S. 2L72 4F RTA21EA 20050505000652005050500065EA 2005 5 5 COMA0560255 120050409A2740 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA STABILIZER MALFUNCTIONED A COMAA UNSCHED LANDING JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 SO01916CA 7014 FLIGHT 5622 STABILIZER CHANNEL 1 INOP. COULD NOT DUPLICATE, SYSTEM OPERATIONAL CHECK IS SATISFACTORY. 2L72 4F RTA21EA 20050505000692005050500069EA 2005 5 5 COMA0570041 120050413A531067053110471 BEAM CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01369CA3711 10079 TRANSVERSE BEAM AT FS 280 FROM LBL 36 TO RBL 36 IS CORRODED ALONG THE UPPER AND LOWER EDGES. REPLACED THE TRANSVERSE BEAM AT FS 280 IAW BOMBARDIER INC REO 670-53-11-047, AND CRJ 700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20050505000702005050500070EA 2005 5 5 COMA0570042 120050410A2782768616C ACTUATOR CNDAIRCL600 CL6002C10 1390015EA NR 2 SLAT MALFUNCTIONED A COMAO OTHER JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 SO01625CA4591 10113 FLT 5165 SLATS FAIL CAUTION. REPLACED THE LEFT NR 2 SLAT ACTUATOR. 2L72 4F RTA21EA 20050505000722005050500072SO 2005 5 5 SIMA200509104 120050317A532014522460007 GUSSET EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21641AE 145191 DURING MBV INSPECTION, FOUND FORWARD CABIN GUSSET BETWEEN FRAMES 20 AND 23 CORRODED ON UPPER SURFACE. REMOVED AND INSTALLED CABIN GUSSET IAW SRM. AC RETURNED TO SERVICE. (SW21200504818) (K) 2L72 4T4 FRTT00011ATTE6CH 20050505000762005050500076SO 2005 5 5 SIMA200509107 120050317A532114522461003 DOUBLER EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL CABIN FLOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21641AE 145191 DURING MBV INSPECTION, FOUND FWD CABIN FLOOR DOUBLER AT FRAME 20 CORRODED AROUND AFT NUTPLATE. INSTALLED NEW DOUBLER AT FRAME 20 IAW SRM 51-40-02. AC RETURNED TO SERVICE. (SW21200504818) (K) 2L72 4T4 FRTT00011ATTE6CH 20050505000792005050500079SO 2005 5 5 SIMA200509110 120050321A5522 SKIN EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL ELEVATOR CRACKED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21641AE 145191 DURING MBV INSPECTION FOUND LT ELEVATOR LWR SKIN SURFACE CRACKED BETWEEN STA 99.9 AND 1280.0. REPLACED LT ELEVATOR IAW AMM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200504818) (K) 2L72 4T4 FRTT00011ATTE6CH 20050505000802005050500080SO 2005 5 5 SIMA200509111 120050322A491012042635001 PROFILE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL APU COWL CRACKED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21641AE 145191 DURING MBV INSPECTION FOUND APU COWL PROFILE CRACKED. REMOVED, MANUFACTURED, AND INSTALLED NEW PROFILE IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200504818) (K) 2L72 4T4 FRTT00011ATTE6CH 20050505000842005050500084WP 2005 5 5 I5HA0524001 120050331A7810 AUGMENTOR TUBE CVAC 240 240* 2422601WP PWA R2800 R2800* 52026NE RT ENGINE FIRE A I5HAFD ACTIVATE FIRE EXT. RETURN TO BLOCK AJ FLAME/FIRE WARNING INDICATION TXTAXI/GRND HDL 1 GL23156PA 324 RT ENG FIRE WARNING BELL SOUNDED AND ASSOC FIRE WARNING LIGHT ILLUMINATED DURING TAXI. RT FIRE BOTTLE WAS DISCHARGED AND ENG SHUTDOWN. FIRE WAS EXTINGUISHED WITH NO FURTHER ACTION. EXAMINATION OF RT ENG REVEALED INSIDE OF AUGMENTOR TUBE HAD CAUGHT FIRE. FIRE WAS CONTAINED INSIDE AUGMENTOR TUBE. AUGMENTOR TUBE WAS REMOVED AND AC WAS INSPECTED FOR DAMAGE. NO DAMAGE TO AC, OTHER THAN AUGMENTOR TUBE WAS FOUND. NO EVIDENCE OF FUEL OR OIL LEAKING IN AREA. RT AUGMENTOR TUBE WAS REPLACED WITH SERVICEABLE UNIT AND AC WAS RETURNED TO SERVICE. COMMON CAUSE, THIS TYPE OF FIRE IS WIND UP THE TAILPIPE COMBINED WITH LOW ENG RPM CREATING ACCUMULATION OF GASOLINE VAPOR IN AUGMENTOR TUBE. (K) 2L72 4R4 R A793 5E8 20050505000852005050500085NM 2005 5 5 SB05046 120050413A335020131A BATTERY PACK BOEING737 737401 1384701NM EMERGENCY LIGHT DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19406US 23876 THE LT EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE AT STATION 304. MAINTENANCE REPLACED THE BATTERY PACK. OPS CHECK OK. 2L72 4F RTA16WE 20050505000862005050500086NM 2005 5 5 SB05047 120050413A3397 WIRE BOEING737 7374B7 1384702NM EMERGENCY LIGHT BROKEN A USAAK NONE O OTHER ININSP/MAINT 1 EA19434US 24556 PIT - MAINTENANCE REPORTED THE EMERGENCY LIGHT AT ROW 10 INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE. SPLICED WIRE AND ACCOMPLISHED OPERATIONAL CHECK OF LIGHTS. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050505000982005050500098CE 2005 5 5 BSYA200500007 120050414A3230583800901 MOTOR BEECH 58 58 1152740CE MLG MALFUNCTIONED E BSYAO OTHER J WARNING INDICATION APAPPROACH 1 GL0733DK TH480 ON APPROACH INTO BNA, PILOT SELECTED GEAR DOWN AND NOTHING HAPPENED. PILOT PULLED GEAR CIRCUIT BREAKER AND HAND CRANKED GEAR DOWN, LANDED NO PROBLEM. MAINTENANCE JACKED A/C RESET CIRCUIT BREAKER GEAR OPERATED NORMALLY. CHANGED GEAR MOTOR AND DYNAMIC BREAK RELAY FOR PRECAUTIONARY MEASURES. 1L72 3O 3A16 20050505001002005050500100EU 2005 5 5 NXT2005F00000 120050325A5302109037017115 SPAR AGUSTAA109 A109E 0260119EU PWC PW206CPW206C NE TAILBOOM CRACKED E NXTAK NONE O OTHER ININSP/MAINT 1 SW19144CF1391 11144 BC032124 A (4) INCH CRACK WAS DISCOVERED IN THE L/E SPAR DOUBLER OF THE VERTICAL FIN. ADDITIONALLY, (2) CRACKS WERE FOUND IN THE VERTICAL STABILIZER ASSY (NOT DETACHABLE). ONE CRACK MEASURED APPROX 5 INCHES AND ONE APPROXIMATELY 7 INCHES. A DETAIL BREAKDOWN OF THIS ASSEMBLY IS NOT PROVIDED AT OPERATOR LEVEL. PN OF INDIVIDUAL CRACKED COMPONENTS ARE NOT AVAILABLE TO THIS OPERATOR. THE APPROXIMATE LOCATION OF DAMAGED AREA IS STATION 9141, LB 1625. TAILBOOM IS BEING RETURNED TO MFG FOR REPAIR EVALUATION. (SW19200509233) (K) 1G72 3U3 URTH7EU E42NE 20050505001032005050500103SO 2005 5 5 SWIA200514847 120050412A3350 SIGN EMB 120 EMB120ER 3260203SO EMERGENCY LIGHTSINOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07563SW 120338 EXIT SIGN AT ROW 9 IS BROKEN. REPLACED SIGN, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050505001062005050500106SO 2005 5 5 SWIA200514850 120050405A275012064207615 SELECTOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07227SW3896 3896 120304 EXTENDING FLAPS FROM 15 DEGREES TO 25 DEGREES GOT A CONTROL FAULT LIGHT. REPLACED FLAP CONTROL HANDLE. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050505001082005050500108EA 2005 5 5 SWIA200514852 120050408A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07907SW 7511 FOUR OF THE 12 EMERGENCY FLOOR LEVEL LIGHTING INOPERATIVE. REPLACED CABLE ADAPTER FOR EMERGENCY FLOOR LEVEL LIGHTING AT SEAT 12CD. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050505001092005050500109EA 2005 5 5 SWIA200514853 120050406A274070609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CLCLIMB 1 NM07912SW2686 2686 7595 STAB TRIM CAUTION AND MACH TRIM CAUTION MSG. REPLACED HSTCU IAW 27-41-01, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050505001112005050500111EA 2005 5 5 SWIA200514855 120050405A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07937SW 7735 RIGHT SPOILERON CAUTION MSG DISPLAYED. REPLACED OUTBOARD SPOILERON PCU, OPERATIONAL CHECK GOOD IAW CRJ MM27-61-05. 2L72 4F RTA21EA 20050505001122005050500112EA 2005 5 5 SWIA200514856 120050409A274070609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07956SW109 109 7825 STAB TRIM CH1 WILL NOT ENGAGE. REPLACED HSTCU. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050505001132005050500113SO 2005 5 5 SWIA200514857 120050409A27203081401003 ACTUATOR EMB 120 EMB120ER 3260203SO RUDDER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CLCLIMB 1 NM07187SW5819 5819 120037 ONCE AIRBORNE, RIGHT RUDDER WOULD ONLY MOVE HALF WAY. REPLACED BLUE SYSTEM RUDDER ACTUATOR IAW EMB MM 27-22-02 , OPERATIONAL CHECK IAW EMB MM 27-24-00 GOOD. 2L72 4T RTA31SO 20050505001142005050500114SO 2005 5 5 SWIA200514858 120050409A275012064207611 SELECTOR EMB 120 EMB120ER 3260203SO TE FLAP BINDING A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07187SW7025 7025 120037 FLAP SELECTOR BINDS IN 45 DEG NOTCH. REPLACED FLAP SELECTOR LEVER ASSY IAW EMB MM 27-50-01, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050505001152005050500115EA 2005 5 5 SWIA200514859 120050406A2150 A/C PACK CNDAIRCL600 CL6002B19 1900309EA RIGHT SMOKE A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM07915SW 7615 SMOKE IN CABIN. SMOKE ORIGINATED WHILE RUNNING PACKS ON FAULTY AIR WISCONSIN GROUND START CART. RAN LEFT AND RIGHT AIR CONDITIONER PACKS FOR TWENTY MINUTES TO CLEAR SMOKE FROM PACKS. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050505001162005050500116EA 2005 5 5 SWIA200514860 120050408A2740 SWITCH CNDAIRCL600 CL6002B19 1900309EA F/O TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07938SW 7741 F/O'S TRIM SWITCH IS STICKY. REPLACED F/O'S TRIM SWITCH IAW MM 27-41-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050505001182005050500118EA 2005 5 5 SWIA200514862 120050330A5315 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07959SW 7840 FLOOR SUPPORT ANGLE CRACKED AT FUSELAGE STA 621.0 LEFT SIDE LBL 38. ITEM FOUND AT C-CHECK INSPECTION. REPAIR ANGLE IAW CRJ REO 601R-53-61-117 REV B. 2L72 4F RTA21EA 20050505001212005050500121EA 2005 5 5 SWIA200514865 120050330A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07959SW 7840 RBL 9 AT FS 280.00 INBOARD ANGLE IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. CLIP REPLACED IAW CRJ SRM 51-42-21 AND 51-42-06. 2L72 4F RTA21EA 20050506000012005050600001NM 2005 5 6 ZN3R2005001 120050414A4920 TURBINE ALIDSG 85129 BOEING737 737100 1384404NM APU SEPARATED B ZN3RO OTHER T ENGINE CASE PENETRATION NRNOT REPORTED 1 WP07 P35204 RECEIVED APU 85-129 PN:380428-1 SN P-35204 FROM LAN CHILE AIRLINES ON 4/11/05. DURING VISUAL INSPECTION OF THE APU IT WAS BROUGHT TO THE ENGINEER'S ATTENTION THAT AN EXDUCER BLADE WAS MISSING FROM THE TURBINE WHEEL AND THERE WAS A HOLE IN THE SIDE OF THE EXHAUST TAILPIPE. IT IS POSSIBLE THAT A PIECE OF THE TURBINE EXITED THE TAILPIPE OUT OF A HOLE PERPINDUCULAR TO THE EXHAUST PATH. NO INFORMATION RELATED TO THIS FINDING WAS SUBMITTED BY THE CUSTOMER. 2L72 4F A16WE 20050506000032005050600003NM 2005 5 6 UIEA200500036 120050323A541265B8094938 BULKHEAD BOEING747 7472D7B 1384803NM NR 3 PYLON CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15527MC 22471 DURING SCHEDULED INSPECTION, NR 3 PYLON, THE BULKHEAD UPPER LEFT AND RIGHT SIDE FORWARD CHORD ANGLES WERE FOUND CRACKED. STOP DRILLED THE CRACK PER 747 SRM 51-10-01. NDT INSPECTED THE REPAIR AREA, INCLUDING HFEC INSPECTION OF ALL TRIMMED FLANGE EDGES AND STOP DRILLED HOLES TO ENSURE CRACK REMOVEAL OR CONTAINMENT. INSTALLED ALUMINUM ANGLES COMMON TO THE UPPER FORWARD AND AFT LT AND RT CHORDS. DETAIL VISUALLY INSPECT THE AFFECTED CHORD AREA FOR CRACKS, CORROSION AND/OR LOOSE FASTENERS EVERY C-CHECK OR 18 MONTHS, WHICHEVER COMES FIRST. ATLAS AIR EO 4754A130 ISSUED TO ACCOMPLISH THE INSPECTION. (M) 2L74 4F RTA20WE 20050506000052005050600005NM 2005 5 6 UIEA200500015 120050308A541465B940512 SKIN BOEING747 7472D7B 1384803NM NR 3 PYLON CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15527MC 22471 DURING INSPECTION, NR 3 PYLON, CRACK DAMAGE WAS FOUND AT PRE-COOLER EXHAUST CUTOUT LOWER AFT CORNER AT NACELLE STATION 248. THE NR 3 STIFFENER WAS REINFORCED WITH A NEW STEEL LOWER REPAIR ANGLE FROM NACELLE STATION 235 TO 254. THE RIB INSTALLATION AT NACELLE STATION 248 WAS MODIFIED TO ACCOMMODATE THE NEW STEEL LOWER REPAIR ANGLE INSTALLATION ON THE NR 3 STIFFENER. (M) 2L74 4F RTA20WE 20050506000092005050600009NM 2005 5 6 UIEA200500031 120050322A3230366103 SEQUENCE VALVE BOEING747 74747UF 1384949NM MLG MALFUNCTIONED A UIEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA15497MC 29258 FLT 862 - AFTER TAKEOFF GEAR LEVER WOULD NOT GO PAST OFF. LOCK OVERRIDE WOULD NOT RELEASE. EICAS MESSAGE GEAR DISAGREE, EICAS MESSAGE GEAR MONITOR, STATUS MESSAGE GEAR DISAGREE, STATUS MESSAGE GEAR MONITOR. NO FUEL DUMPED. LUBRICATED LANDING GEAR LEVER LOCK OVERRIDE MODULE. LANDING GEAR LEVER OPERATED AND LOCK OVER RIDE FUNCTION AND OPERATION FOUND NORMAL AS PER MM 32-33-01. CHECKED CABLE RUN FROM GEAR HANDLE TO SEQ VALVE, ALL FOUND NORMAL PER MM 20-11-03. REPLACED RIGHT GEAR SEQ VALVE PER 32-31-03, LEAK CHECK OK. P/N OFF 36610-3 S/N 2378. REPLACED PSEV PER MM 32-09-03, ALL CHECK OK P/N OFF, 8-569-20 S/N OFF, 5671. (M) 2L74 4F RT1384945 20050506000122005050600012NM 2005 5 6 UIEA200500035 120050323A541265B94111 BULKHEAD BOEING747 7472D7B 1384803NM NR 1 PYLON CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15527MC 22471 DURING SCHEDULED INSPECTION, NR 1 PYLON, THE BULKHEAD UPPER LEFT SIDE FORWARD AND AFT CHORD ANGLES WERE FOUND CRACKED. TRIMMED AND STOP DRILLED THE CRACK PER 747 SRM 51-10-01 NDT INSPECTED THE REPAIRED AREA, INCLUDING HFEC INSPECTION OF ALL TRIMMED FLANGE EDGES AND STOP DRILL HOLES TO ENSURE CRACK REMOVAL OR CONTAINMENT. INSTALLED ALUMINUM, REPAIR ANGLES AND STRAPS COMMON TO THE UPPER AND FORWARD AND AFT CHORDS. DETAIL VISUALLY INSPECT THE AFFECTED CHORD AREA FOR CRACKS, CORROSION AND/OR LOOSE FASTENERS EVERY C CHECK OR 18 MONTHS, WHICHEVER COMES FIRST. ATLAS AIR EO 4754A129 ISSUED TO ACCOMPLISH THE INSPECTION. (M) 2L74 4F RTA20WE 20050506000132005050600013NM 2005 5 6 UIEA200500034 120050323A541465B9040511 SKIN BOEING747 7472D7B 1384803NM NR 2 PYLON DENTED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15527MC 22471 DURING INSPECTION, FOUND DENT (SKIN WRINKLE) NR 2 NACELLE STRUT INBOARD SKIN BETWEEN NACELLE STATION 286 TO 300.1. CONFIRMED THAT THE AFFECTED WAS FREE FROM DISCOLORATION. NDT CONDUCTIVITY MEASURED READING ACCOMPLISHED. HFEC INSPECTED AND WAS FOUND TO BE DAMAGE FREE. AREA IS STRUCTURALLY SATISFACTORY PER BOEING MESSAGE 1-141MMN SERVICE REQUEST ID-67130304. CONDUCT REPEAT DETAILED INSPECTIONS OF THE AFFECTED AREA EVERY C-CHECK, NOT TO EXCEED 18 MONTHS, LOOKING FOR CRACKS AND OR LOOSE/MISSING FASTENERS. ATLAS AIR EO 4754A134 ISSUED TO ACCOMPLISH THE INSPECTION. (M) 2L74 4F RTA20WE 20050506000142005050600014GL 2005 5 6 UIEA200500012 220050303A7261 B-NUT BOEING747 74747UF 1384949NM GE CF6 CF680C2* GL OIL PRESS XMITERLOOSE A UIEAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 EA15409MC 30558 704892A SHORTLY AFTER TAKEOFF OIL QTY DROPPED TO ZERO. DURING CLIMB-OUT, OIL PRESSURE DROPPED EVENTUALLY TO SIX PSI. NR 4 ENGINE WAS SHUT DOWN AS OIL PRESSURE TO 10 PSI. OIL PRESSURE REMAINED AT 6 PSI, N1 AT 25 PERCENT AND N2 BETWEEN 17 AND 21 PERCENT FOR DURATION OF FLIGHT. TIGHTENED B-NUT ON OIL PRESSURE TRANSMITTER PERFORMED 'NO OIL PRESSURE' INSPECTON PER MM 72-00-00. ALSO PERFORMED POST WINDMILLING INSPECTION PER 72-00-00. REPLACED OIL FILTER PER 79-21-04. NO METAL NOTED ON CHIP DETECTORS AND FILTER. NO LEAKS NOTED ON ENGINE RUN UP. ALL INSPECTION SATISFACTORY. (M) 2L74 4F4 FRT1384945 E23EA 20050506000192005050600019NM 2005 5 6 UIEA200500027 120050318A541165B940513 SPAR BOEING747 7472D7B 1384803NM NR 3 PYLON CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15527MC 22471 DURING SCHEDULED MAINTENANCE, NR 3 PYLON INBOARD MIDSPAR CHORD WAS FOUND CRACKED ON THE VERTICAL FLANGE. THE AFFECTED SECTION OF CHORD WAS TRIMMED OUT. NDT INSPECTION WAS PERFORMED AT TRIMMED EDGES AND AT AL AFFECTED FASTENERS LOCATION TO ENDURE A CRACK AND DAMAGE FREE CONDITION. A NEW SECTION OF CHORD REPLACEMENT WAS INSTALLED USING REPAIR SPLICE STRIPS AND FILLERS. THE REPAIR ASSEMBLY CONFORMS TO DESIGN REQUIREMENTS. (M) 2L74 4F RTA20WE 20050506000202005050600020NM 2005 5 6 UIEA200500025 120050318A5754 SKIN BOEING747 7472D7B 1384803NM KRUEGER FLAP CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15527MC 22471 DURING INSPECTION, NR 16 KRUEGER FLAP, FOUND CRACK AT PANEL ATTACH FASTENER HOLE. TRIMMED OUT AFFECTED SPAR SEGMENT. NDT INSPECTED TO ENSURE CRACK AND DEFECT FREE CONDIION. INSTALLED REPAIR FILLER AND ALUMINUM REPAIR ANGLE WITH ADDITIONAL FASTENERS. REFINISHED SPAR TO DESIGN STANDARD. (M) 2L74 4F RTA20WE 20050506000212005050600021NM 2005 5 6 UIEA200500024 120050315A5230 FITTING BOEING747 7472D7B 1384803NM CARGO DOOR ELONGATED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15527MC 22471 DURING INSPECTION, REPORTED ELONGATED HOLES IN THE TEN LATCH FITTING OF THE MAIN DECK SIDE CARGO DOOR. THE TEN LATCH FITTING WERE REWORKED WITHIN ALLOWABLE REWORK LIMITS. (M) 2L74 4F RTA20WE 20050506000222005050600022EU 2005 5 6 USAA050268 120050205A5347F5311198420000 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19671UW22760 0323 BFM - FOUND SEAT FALSE RAIL CORRODED, 1 INCH WIDE BY 1 INCH LONG BY .053 DEEP, FRAME 13A +Y1959 MAIN CABIN FLOOR. REMOVED AND REPLACED FALSE RAIL PER SRM 53-11-14, 51-42-11. CORROSION LEVEL 2, TASK C531172-01. (M) 2L72 4F RTA46NM 20050506000242005050600024NM 2005 5 6 UIEA200500029 120050321A541265B8904938 BULKHEAD BOEING747 7472D7B 1384803NM NR 2 PYLON CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15527MC 22471 DURING SCHEDULE MAINTENANCE, THE BULKHEAD UPPER LEFT AND RIGHT SIDE FORWARD CHORD ANGLES WERE FOUND CRACKED, NR 2 PYLON. STOPPED DRILLED THE CRACK END AND NDT INSPECTED TO ENSURE CRACK CONTAINMENT. INSTALLED ALUMINUM REPAIR ANGLES COMMON TO THE UPPER FORWARD AND AFT LEFT AND RIGHT CHORDS. DETAIL VISUALLY INSPECT THE AFFECTED CHORD AREAS FOR CRACKS, CORROSION AND/OR LOOSE FASTENERS EVERY C-CHECK OR 18 MONTHS, WHICHEVER OCCURS EARLIER. 2L74 4F RTA20WE 20050506000262005050600026CE 2005 5 6 45101041005 120050410A2434 LINE LEAR 45 45LEAR 5170805CE HYD SYS LEAKING E J7SAE ENGINE SHUTDOWN KJAFLUID LOSS WARNING INDICATION FLAME/FIRE APAPPROACH 1 SW05405FX 026 THE PILOT REPORTED THAT ABOUT 3 TO 4 MILES OUT WHEN THE INDICATION APPEARED. DIDN'T DISCHARGE A BOTTLE OR SHUT DOWN THE ENGINE. AFTER CLEARING THE RUNWAY, THE INDICATION EXTINGUISHED ABOUT 1 MINUTE AFTER THE ENGINE WAS SHUT DOWN. AFTER DEPLANING THEY SAW HYD FLUID DRIPPING FROM THE COWLING. DIDN'T GET A HYD PUMP FAILURE INDICATION, BUT HE DID GET A HYD. LOW CAS SHORTLY AFTER LANDING. ENGINE REMOVED DUE TO HEAT GENERATED. EVIDENCE OF MELTING OF CABLE CLAMPS AND WIRING HARNESS AT STARTER/GENERATOR. MAINTENANCE SUSPECTS A PINHOLE IN A HYD LET A FINE MIST SPRAY OF FLUID AGAINST THE AREA. THIS IGNITED AND CAUSED A FIRE WHICH MELTED THE COMPONENTS. INVESTIGATION IS ON-GOING. 2L72 4F RTT00008WI 20050503002032005050300203NM 2005 5 3 05FDEA00771 120050331A5514 SKIN DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE RT HORIZONTAL STABILIZER UPPER BARREL NUT NR 28 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133. 2L73 4F RTA22WE 20050503002282005050300228NE 2005 5 3 GUU2005F00007 220050309A7261311895301 GASKET BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE RT ENGINE LEAKING A GUUAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO17178YV UE178 DURING FLIGHT, RT ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED. SECURED THE RT ENGINE. RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED RT ENGINE OVERSPEED GOVERNOR GASKET. OPS LEAK CHECK NORMAL. (K) 2L72 4T4 TRTA24CE E26NE 20050503002392005050300239SO 2005 5 3 TZR2005F00010 220050222A8530SA52000A00P CYLINDER CESSNA402 402B 207590PCE CONT O520 TSIO520* 17040SO NR 5 CRACKED E TZRAK NONE O OTHER ININSP/MAINT 1 SW05406TE1337 402B1366 502051 CYLINDER HAS A HOLE AT EXHAUST VALVE. (K) 1L72 3O3 O A7CE E8CE 20050503002412005050300241SO 2005 5 3 TZR2005F00012 220050128A8530T1ST712BCA01 CYLINDER CESSNA402 402B 207590PCE CONT O520 TSIO520* 17040SO NR 3 CRACKED E TZRAK NONE O OTHER ININSP/MAINT 1 SW03404TE793 402B0834 1655858E CYLINDER CRACKED FROM EXHAUST VALVE. (K) 1L72 3O3 O A7CE E8CE 20050503002432005050300243EA 2005 5 3 TZR2005F00014 220050317A853005K21118 CYLINDER PIPER PA60 PA60601 7106010NM LYC O540 IO540* 41532EA NR 4 CRACKED E TZRAK NONE O OTHER ININSP/MAINT 1 SW05602TE1217 610583796213L1348048A CYLINDER HAS A CRACK IN THE INTAKE VALVE SEAT. (K) 1M72 3O3 ORTA17WE 1E4 20050503002832005050300283GL 2005 5 3 C2XA05IA053 220050407A7200AE3007A1 ENGINE EMB 145 EMB145ER 3260211SO ALLSN AE300 AE3007A GL LEFT FAILED A C2XAA UNSCHED LANDING Y ENGINE STOPPAGE CRCRUISE 1 SW2714940141454695 145033 CAE310006 OKC - FLIGHT 3453, THE CREW REPORTED AN ENGINE NR 1 INFLIGHT FAILURE, LOUD BANG FOLLOWED BY UNCOMMANDED SHUTDOWN. THE AIRCRAFT RETURNED TO OKC WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE, OPERATIONALLY CHECKED WITHOUT DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20050503002862005050300286CE 2005 5 3 DXTA200500673 120050311A323082182 MANIFOLD CESSNA750 750 2076810CE NLG INOPERATIVE E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07953QS1673 7500153 AFTER TAKEOFF RETRACTED THE GEAR AND THE NOSE STAYED IN THE DOWN AND LOCKED POSITION WITH THE HANDLE IN THE UP POSITION. FOLLOWED THE CHECKLIST AND BLEW THE GEAR DOWN WITH THE BOTTLE AND LANDED BELOW 31,800 LBS. REMOVED AND REPLACED GEAR MANIFOLD ASSY IAW 750 M/M 3230-02. OPERATIONAL CHECK GOOD. 2L72 4J RTT00007WI 20050503002872005050300287CE 2005 5 3 DXTA200500674 120050411A3240 B-NUT CESSNA500 560CESSNA 2076750CE PARK BRAKE VALVELOOSE E DXTAO OTHER K FLUID LOSS LDLANDING 1 GL07374QS 5600475 F/O'S BRAKES (LEFT AND RIGHT) FEELS SPONGY. CAPT'S BRAKES ARE OK. ALSO, IF YOU PUMP THE F/O'S BRAKES, BRAKES COME UP TO HAVING PRESSURE. REMOVED COCKPIT AND DROP AISLE CABIN FLOORBOARDS FOR BRAKE LINE & COMPONENT INSPECTION. FOUND PARKING BRAKE VALVE LEAKING AT B-NUTS. RETORQUED B-NUTS AND LEAK CHECK GOOD. SERVICED BRAKE RESERVOIR. CLOSED FLOORBOARDS AND REINSTALLED SEATS. MAINT C/W IAW 560MM CHP 32-42-03. 2L72 4F RTA22CE 20050503002892005050300289NM 2005 5 3 AWXA200500446 120050315A53116546564506 FRAME BOEING737 737375 13844BNNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 MCN - MAJOR REPAIR - DURING C-05 CHECK CORROSION WAS FOUND ON AFT SIDE OF AFT LOWER FUSELAGE FRAME AT BS 986.5, STR 25 RT. MAINTENANCE CUT OUT CORRODED AREA OF AFT LOWER FUSELAGE FRAME AT BS 986.5, STR 25 RT; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-07 FIG 206. 2L72 4F RTA16WE 20050503002902005050300290NM 2005 5 3 AWXA200500447 120050311A573065C2520418 SKIN BOEING737 737375 13844BNNM LT WING CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 MCN - MAJOR REPAIR - DURING C-05 CHECK EXFOLIATION CORROSION WAS FOUND ON TOP LT WING IN SPAR SKIN AT BS 575, WBL 81.5. MAINTENANCE CUT OUT DAMAGED AREA OF LT WING IN SPAR SKIN AT BS 575, WBL 81.5; FABRICATED A -5 FILLER AND 4 EACH REPAIR PLATES (DOUBLERS); INSTALLED REPAIR PARTS IAW B737-300 SRM 57-20-01 FIG 202. 2L72 4F RTA16WE 20050503002912005050300291NM 2005 5 3 AWXA200500448 120050312A5755654645160A SKIN BOEING737 737375 13844BNNM NR 7 SPOILER DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 MCN - MAJOR REPAIR - DURING C-05 CHECK FOUND THE UPPER SURFACE OF THE NR 7 SPOILER DELAMINATED BETWEEN WS 366 AND WS 368 RT. MAINTENANCE REMOVED DELAMINATED AREA OF NR 7 SPOILER UPPER SURFACE SKIN; FABRICATED A FILLER AND DOUBLER; BONDED REPAIR PARTS TO SPOILER IAW B737-300 SRM 51-70-10 FIG 31. 2L72 4F RTA16WE 20050503002922005050300292NM 2005 5 3 AWXA200500449 120050311A524065C807351 DOOR FRAME BOEING737 737375 13844BNNM R2 DOOR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 MCN - MAJOR REPAIR - DURING C-05 CHECK FOUND CORROSION ON R-2 DOOR INNER CHORD BETWEEN BS 964 AND BS 995, RBL 44 AND RBL 49. MAINTENANCE REMOVED CORRODED R-2 DOOR INNER CHORD FROM BS 964 TO BS 995, RBL 44 TO RBL 49; FABRICATED A NEW REPLACEMENT INNER CHORD; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050504000012005050400001NM 2005 5 4 05FDEA00913 120050409A5230 DOOR BOEING727 727200 138407ENM CARGO OUT OF ADJUST A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25491FE 21529 ON CLIMBOUT AT FL230 AND 310 KTS MAIN CARGO DOOR-B ILLUMINATED. DECLARED EMERGENCY AND RTB. LIGHT WENT OUT DESCENDING THRU FL180 AND 250 KTS, MEL 09APR05. RELEASED FOR SERVICE PER MEL/CDL: 52-15-01 CATEGORY: C EXPIRATION: 19APR05 B-LOOP MEL'D REF MEL 52-15-01: MAIN CARGO DOOR WARNING LIGHT SYS B-INOP. VERIFY DOOR CLOSED AND LOCKED PRIOR TO EACH BLOCKOUT. CYCLED DOOR & VERIFED CLOSED AND LOCKED. ADJUSTED B-SWITCH AFT CABLE ASSY PER NASI MM 52-30-00. OPS CKS NORMAL. 2L73 4F RTA3WE 20050504000082005050400008NM 2005 5 4 2005UALA00286 120050331A5310 CREASE BEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29308UA 23669 AFT CABIN CREASE BEAM RBL 57, WL 208.1 CORRODED IN NUMEROUS LOCATIONS FROM STA 947.5 TO STA 990. REPLACED CREASE BEAM. 2L72 4F4 FRTA16WE E2GL 20050504000092005050400009NM 2005 5 4 2005UALA00287 120050331A5315 FLOORBEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29309UA 23670 STATION 1016 FLOORBEAM UPPER T-CAP HAS CORROSION FROM LBL 25 TO LBL 45. REPLACED T-CAP. 2L72 4F4 FRTA16WE E2GL 20050504000192005050400019NM 2005 5 4 2005UALA00300 120050405A339758781 WIRE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29333UA 24228 EMERGENCY FLOOR PATH LIGHTING INOPERATIVE AFT OF ROW 16. REPLACED POWER CABLE. 2L72 4F4 FRTA16WE E2GL 20050504000212005050400021NM 2005 5 4 2005UALA00302 120050405A3350362624 LAMP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29364UA 24533 EEL FLOOR LIGHT INOP ROW 4 ABC. REPLACED EEL FLOOR LIGHT. 2L72 4F4 FRTA16WE E2GL 20050504000232005050400023NM 2005 5 4 2005UALA00307 120050407A5313 STRINGER BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29584UA 26706 STRINGER 22L CORRODED AT STA 700 TO 720. DAMAGE CAUSED BY CORROSION. MAJOR REPAIR ACCOMPLISHED. STRINGER DAMAGE WAS TRIMMED OUT AND A DOUBLER REPAIR WAS INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050504000362005050400036WP 2005 5 4 GTIA050037 120050223A2700 MOTOR DOUG DC9 DC983 3022083WP PWA JT8 JT8D217A 52053NE TRIM SYS INOPERATIVE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23808NK 49504 PRIMARY LONG TRIM INOPERATIVE, TAIL SWAP WITH AIRCRAFT 829. REMOVED AND REPLACED LONG TRIM MOTOR AND REPAIRED MOTOR GROUNDS, SYSTEM OPS CHECK GOOD. (K) 2L72 4F4 FRTA6WE E9NE 20050504000372005050400037CE 2005 5 4 DJFA2005079 120050407A5510631431025 BOOT CESSNA525 525 2076601CE HORIZONTAL STAB LOOSE E DJFAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 EA23206LX 5250205 MMSD TRIP ID NR 812728 CREW REPORTED FEELING AN UNUSUAL VIBRATION IN THE CONTROL COLUMN MOSTLY DURING PITCH MOVEMENT. AN EMERGENCY WAS DECLARED AND AIRCRAFT RETURNED TO MMSD. CREW DISCOVERED A LOOSE EROSION BOOT ON THE RIGHT HORIZONTAL STABILIZER TIP. MAINTENANCE REPLACED THE EROSION BOOT ON THE RIGHT HORIZONTAL STABILIZER TIP. AIRCRAFT WAS RETURNED TO SERVICE. 1L72 4F RTA1WI 20050504000402005050400040NM 2005 5 4 05FDEA00772 120050331A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE RT HORIZONTAL STABILIZER UPPER BARREL NUT NR 22 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133. 2L73 4F RTA22WE 20050504000422005050400042NM 2005 5 4 05FDEA00915 120050410A5347AEA73256 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 MAIN DECK, RIGHT SEAT TRACK AT STA Y= 1454, X=-29 FOUND WITH CORROSION. MAIN DECK, RIGHT SEAT TRACK CUT FROM STA Y= 1411, X=-29 AND REMOVED AT SPLICE AREA PER SRM 53-70-00 VOLUME I, FIGURE 1. REPAIR SEAT TRACK AND SPLICE FABRICATED PER SRM 53-70-00 VOLUME I, FIGURE 1 AND REPROTECTED PER 51-21-01 VOLUME II. REPAIR TRACK AND SPLICE INSTALLED PER SRM 53-70-00 VOLUME I, FIGURE 1 AND SRM 51-31- 01 VOLUME II. 2L73 4F RTA22WE 20050606000872005060600087SO 2005 6 6 CHQA200500102 120050526A2497 WIRE EMB 145 EMB145LR 3260212SO COCKPIT BURNED A CHQAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 GL11296SK 145514 DURING DECENT, RECEIVED A PITOT 3 INOP MESSAGE. WENT AWAY AFTER A FEW SECONDS. 24 MINS OUT, A HINT OF SMOKE NOTED. AN EMERGENCY DECLARED. AN LG AIR/GND FAIL MESSAGE. SMOKE VISIBLE, DONNED 02 MASKS & SMOKE GOGGLES. SMOKE COMING FROM FO VENT, HEAVY SMOKE SEEN COMING FROM AFT PORTION OF VENT. 4 MILES & 8,000 FT FROM MDW A NO TAKEOFF CONFIG MESSAGE APPEARED. FLT TOUCHED DOWN & CREW COULDN`T GET RT T/R OPEN. MX INSPECTED ACRFT & FOUND BURNED WIRES, RELAYS, & INSULATION. REPAIRED WIRES FOR RT HAND RELAY SUPPORT PANEL IAW EMB 145 WM. R & R DAMAGED RELAYS & RELAY PANEL IN RT RELAY SUPPORT PANEL IAW EMB AMM & EMB WM. MX FOUND PITOT 3 PROBE PITTED & BURNED. R & R PITOT 3 PROBE IAW EMB 145 AMM. TEST FLT GOOD. 2L72 4T RTT00011AT 20050607000022005060700002EA 2005 6 7 QXEA200500867 120050429A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FUSELAGE EXTERIOR, LOWER SKIN HAS TWO CHAFE MARKS FROM FAIRING SCREWS AT STATION 980 AND BL 0.00 TO LBL 1.5. REPAIRED IAW CRJ-700 SRM 51-42-21-001-001-A01, 51-42-21-001-001-A01, 51-25-16-001-001-A01 AND HORIZON AIR EA R-53-319. 2L72 4F RTA21EA 20050504000442005050400044NM 2005 5 4 05FDEA00969 120050412A5711 SPAR DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE RT WING O/B FLAP O/B REAR SPAR MOUNTED HINGE LWR MOUNT EVIDENT OF CORROSION. CORROSION REMOVED & FOUND I/B AND O/B BOLT HOLES EXCEED LIMITS AS PER CMM 57-44-09. 2L73 4F RTA22WE 20050504000752005050400075EU 2005 5 4 USAA050022 120050101A5347F5311170520000 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW22421 0315 BFM - FOUND RAIL CORRODED 1.5 INCH BY 1.5 INCH BY .040 INCH DEEP, FRAME 13-13A, Y1456, MAIN CABIN FLOOR. CORROSION LEVEL 2, TASK NR J7-220-53500. REMOVED AND REPLACED RAIL PER SRM 53-11-14. (M) 2L72 4F RTA46NM 20050504000782005050400078EU 2005 5 4 USAA050150 120050109A5347F53476214200 SEAT TRACK AIRBUS330 A330323 3930335EU PWA 4168 PW4168A NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW21927 0342 BFM, S1 CK, SEAT TRACK, (3 INCHES L X 1 INCH X .040 INCH D) CORROSION; LEVEL 2; TASK NR J7-200-2580C, MAIN CABIN FLOOR Y=450, FR 55-58. REMOVED AND REPLACED SEAT TRACK IAW SRM. (K) 2L72 4F4 FRTA46NM 20050504000802005050400080EU 2005 5 4 USAA050179 120050114A5320F534780017011 FLOOR SUPPORT AIRBUS330 A330323 3930335EU PWA 4168 PW4168 NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW 0342 BFM - S1 - AUX BEAM SUPPORT, (1.0 INCH L X 1.0 INCH W X .050 INCH D) CORROSION; LEVEL 2; TASK NR J7-900-09000-015, FR 71.8, Y2080- Z240. REMOVED AND REPLACED WITH NEW PORT IAW SRM. (K) 2L72 4F4 FRTA46NM E36NE 20050504000822005050400082EU 2005 5 4 USAA050181 120050117A53214E33635 FLOOR PANEL AIRBUS330 A330323 3930335EU PWA 4168 PW4168A NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW21927 0342 BFM - S1 - HEATED FLOOR PANEL, (12 INCHES X 10 INCH) AREA AND DELAMINATED; CORROSION; LEVEL 2; TASK NR J7-270-53100-008, FR 33 TO FR 36, Z240, Y1959 PANEL NR 242 DF FLOORBOARD. REPLACED ALUMINUM SKIN IAW TYP REP, SRM. (K) 2L72 4F4 FRTA46NM 20050504000902005050400090NE 2005 5 4 20054 220050406A7200 ENGINE DHAV DHC8 DHC8103 1386005NM PWA PW121 PW121 52124NE NR 2 MALFUNCTIONED A KPVAO OTHER EO VIBRATION/BUFFET OTHER CRCRUISE 1 WP13829EX 146 120399 DURING FLIGHT AT CRUISE ALT 14,000 FT, A SHARP JOLT/POP WAS FELT WITH AN ASSOCIATED YAW TO THE RT. ALL ENGINE INDICATORS APPEARED NORMAL. DURING DESCENT TO LANDING, AS POWER LEVERS PULLED BACK AN ABNORMAL FAINT "WHINING" WAS HEARD. DURING TAXI TO GATE IN FLIGHT IDLE/START/FEATHER, FUEL FLOW ON NR 2 ENGINE WAS JUMPING BETWEEN 205 AND 290. DURING POST FLIGHT WALK AROUND NOTED FLUID LEAKING DOWN NR 2 ENGINE INTAKE. 2H72 4T4 TRTA13NM E20NE 20050504000922005050400092CE 2005 5 4 GUU2005F00010 120050313A55201016200131 BRACKET BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE RT ELEVATOR CORRODED A GUUAK NONE O OTHER ININSP/MAINT 1 SO298153320161 UE137 AT SCHEDULED ROUTINE MAINTENANCE, RT CENTER ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RT CENTER ELEVATOR HINGE BRACKET. (K) 2L72 4T4 TRTA24CE E26NE 20050505000102005050500010EA 2005 5 5 A6WA200540130 120050404A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FLOOR SUPPORT CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31416AW 7603 FLOOR SUPPORT BEAM CLIP AT FS 280, LBL 9, IB IS CRACKED IN RADIUS APPROX (0.33 INCH). (K) 2L72 4F4 FRTA21EA E15NE 20050505000362005050500036SO 2005 5 5 1392041005 120050410A52101159SCB42013 SEAL GULSTMG1159 GIV 3980115SO PAX DOOR DEFLATED E N93AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO13492QS4849 1392 MAIN ENTRANCE DOOR SEAL DEFLATED ON TAKEOFF. 2L72 4F RTA12EA 20050505000372005050500037SO 2005 5 5 1372040805 120050408A3250KP103 BUSHING GULSTMG1159 GIV 3980115SO NLG STEERING WORN E N93AO OTHER O OTHER TXTAXI/GRND HDL 1 SO13472QS5410 1372 NOISE IN NOSE GEAR AREA WHEN TURNING HAND WHEEL 2L72 4F RTA12EA 20050505000462005050500046NM 2005 5 5 72300159 120050322A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 8 INCH AREA OF CORROSION ON STRINGER BOTTOM. 2L73 4F4 FRTA3WE E2EA 20050505000752005050500075SO 2005 5 5 SIMA200509106 120050317A532014521725015 SILL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21641AE 145191 DURING MBV INSPECTION FOUND FORWARD CABIN FLOOR SILL RT CORRODED AROUND UPPER AFT NUTPLATE BETWEEN FRAMES 19 AND 20. REPAIRED RT FLOOR SILL IAW SRM. AC RETURNED TO SERVICE. (SW21200504818) (K) 2L72 4T4 FRTT00011ATTE6CH 20050505000832005050500083CE 2005 5 5 RU32005F00001 120050324A3260 WARNING LIGHT BEECH 300 300BEECH 1152930CE PWA PT6 PT6A45 52043EA MLG FALSE INDICATIONE RU3AL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 SW1576 FF11 ON FINAL APPROACH, LOWERED GEAR AT FAF - NO LEFT MAIN GEAR LIGHT. CYCLED GEAR ONCE INSIDE FAF - STILL NO LIGHTS, EXECUTED FLY BY RWY 4R. 2 AIRLINE CREWS ADVISED ALL 3 GEARS APPEAR DOWN. FLEW LT TRAFFIC, CYCLED GEAR 3RD TIME, OBSERVED GEAR RETRACT AND EXTEND. (K) 2L72 4T4 T A24CE E4EA 20050505001042005050500104EA 2005 5 5 SWIA200514848 120050402A2750601R590141 DETECTOR CNDAIRCL600 CL6002B19 1900309EA FLAP SKEW MALFUNCTIONED A SWIAD RETURN TO BLOCK JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07442SW 7609 AFTER SELECTING FLAPS AT 20 DEGREES, RECEIVED FLAPS DEGRADED STATUS MESSAGE. INSTALLED FLAP SKEW DETECTION UNIT, OPERATIONAL CHECK GOOD IAW CRJ MM 27-51-15. P/N 601R59014-1, S/N ON A734. 2L72 4F RTA21EA 20050505001052005050500105EA 2005 5 5 SWIA200514849 120050406A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 NM07710BR 7852 SPOILERON FAULT STATUS MESSAGE AFTER TAKEOFF. REPLACED SPOILERON PCU AND REPLACED NR 1 AND NR 2 SECU'S IAW 27-61-00. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050505001102005050500110SO 2005 5 5 SWIA200514854 120050408A3350 LIGHT EMB 120 EMB120ER 3260203SO CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07565SW 120340 WHITE EMERGENCY LIGHT INOPERATIVE BY 4A. REPAIRED WHITE FLOOR STRIP EMERGENCY LIGHT BY SEAT 4A. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050505001172005050500117SO 2005 5 5 SWIA200514861 120050409A5210 BELLCRANK EMB 120 EMB120ER 3260203SO PAX DOOR BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07218SW 120287 MAIN CABIN DOOR WON'T OPEN OR CLOSE. REPLACED BROKEN BELLCRANK. OPERATIONAL CHECKS GOOD IAW 52-11-00. 2L72 4T RTA31SO 20050505001192005050500119EA 2005 5 5 SWIA200514863 120050330A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07959SW 7840 LBL 9 AT FS 280.00 OUTBOARD ANGLE IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIP IAW CRJ SRM 51-42-21, 51-42-06. 2L72 4F RTA21EA 20050506000112005050600011NM 2005 5 6 UIEA200500018 120050314A324126700011 MODULE BOEING747 747228F 1384895NM NLG WW FAILED A UIEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA15809MC 20887 FLT 8452 - AFTER TAKEOFF WITH GEAR RETRACTED, ANTI-SKID HYD LIGHT AND RED PARK LIGHT ILLUMINATED. A/C DIVERTED TO FRA. CLEANED CANNON PLUG AT PARKING BRAKE VALVE. SYSTEM CHECKS NORMAL. ALL INDICATIONS NORMAL PER MM 32-41-00. AS PRECAUTION MCC ISSUED ITEM TO REPLACE PARKING BRAKE VALVE AT ORD. PARKING BRAKE MODULAR REPLACED PER AMM 32-44-04. OPS AND LEAK CHECK GOOD. REF LOG PAGE 554769, S/N OFF DA365. (M) 2L74 4F A20WE 20050506000232005050600023NM 2005 5 6 UIEA200500032 120050322A3230257U000215 MODULE BOEING747 74747UF 1384949NM MLG FAILED A UIEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA15497MC 29258 AFTER TAKEOFF GEAR LEVER WOULD NOT GO PAST OFF POSITION. GEAR MONITOR STATUS MESSAGE. NO FUEL DUMPED. REMOVED AND REPLACED LANDING GEAR MODULE PER AMM 32-31-01 P/N OFF 257U0002-15 S/N OFF D00574. AIRCRAFT IN AIR MODE PER 32-09-02. PERFORMED ALL TESTS PER 32-35-00. CLEANED ALL TARGETS. ALL OPS NORMAL. PERF CMC ALT+PRIM+ CMC PSEU TEST. ALL PASSED. AS PER MCC REQUEST REMOVED AND REPLACED LEFT GEAR SELECTOR VALVE PER MM 32-31-03 LEAK CHECK OK, P/N OFF 60B00216-3 S/N OFF 2379. (M) 2L74 4F RT1384945 20050506000282005050600028NM 2005 5 6 SWAA051090 120050413A53116546525 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, BETWEEN STR 8R & STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050506000292005050600029NM 2005 5 6 SWAA051091 120050413A53116546532 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, BETWEEN STR 8L & STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050506000302005050600030NM 2005 5 6 SWAA051092 120050413A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 500C, STR 9L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050506000322005050600032NM 2005 5 6 SWAA051075 120050412A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29330SW 23694 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 312, STR 18R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050506000332005050600033NM 2005 5 6 SWAA051076 120050412A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29330SW 23694 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500 D, STR 15R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050506000342005050600034NM 2005 5 6 SWAA051077 120050412A53306545775 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29330SW 23694 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STR 19L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050506000372005050600037NM 2005 5 6 SWAA051080 120050413A5343BAC1490 FITTING BOEING737 7373H4 1384600NM RT MLG WW CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND RIGHT MLG W/W FITTING CRACKED AT BS 715, RBL 68, WL 198. REMOVED AND REPLACED MLG FITTING PER SRM. 2L72 4F RTA16WE 20050506000382005050600038NM 2005 5 6 SWAA051081 120050413A53206545410 FLOOR SUPPORT BOEING737 7373H4 1384600NM CABIN FLOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 660, BL 0. REPAIRED BEAM PER PAE ER & SB. 2L72 4F RTA16WE 20050506000412005050600041NM 2005 5 6 SWAA051096 120050413A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29356SW 25251 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 25L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050506000432005050600043NM 2005 5 6 SWAA051098 120050413A3350D71701100 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29736SA 27868 DURING SCHEDULED RON CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20050506000442005050600044NM 2005 5 6 PIDA2005003 120050412A3350 BATTERY PACK BOEING737 7373G7 1384595NM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05370WL 24011 EMERGENCY LIGHT ON SEATS 4ABC THROUGH 11ABC ARE INOP. REPLACED BATTERY PACK. OPS CHECKS GOOD. 2L72 4F RTA16WE 20050506000452005050600045CE 2005 5 6 DXTA200500677 120050313A21101103P0912 LIMIT SWITCH CESSNA750 750 2076810CE CABIN PRESSURE INOPERATIVE E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07903QS390 7500162 AT APPROX 65-70 KIAS ON TAKEOFF ROLL FOR OCF. HP DUCT OVERPRESSURE R EICAS MESSAGE ILLUMINATED .TAKEOFF ABORTED. - REMOVED AND REPLACED SWITCH DUE TO FAILED OPERATION. SYSTEM OPERATIONALLY CHECKS GOOD. ALL WORK DONE IAW CE 750 MM CHP 36-11-00. 2L72 4J RTT00007WI 20050506000472005050600047CE 2005 5 6 DJFA2005081 120050414A32606240999959118 BULB BEECH MU300 400A 1155402CE MLG INDICATOR BURNED OUT E DJFAO OTHER P NO WARNING INDICATION APAPPROACH 1 EA23715TA RK189 KIND - KACY TRIP ID NR 815740 CREW REPORTED THAT WHILE PREPARING FOR LANDING THEY DID NOT RECEIVE THE LEFT MAIN GEAR GREEN INDICATION. FIRE/RESCUE RESPONSE AND PRIORITY HANDLING WAS GIVEN. AIRCRAFT PERFORMED A FLY-BY PAST THE TOWER TO CONFIRM THE GEAR WAS DOWN. THE CREW LANDED THE AIRCRAFT WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE INDICATOR BULBS FOR THE LEFT GEAR INDICATION TO BE BURNED OUT AND THE BULBS WERE REPLACED. A LANDING GEAR RETRACTION AND EXTENSION CHECK WAS PERFORMED WITH NO NOTED DEFECTS. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4F RTA16SW 20050506000482005050600048GL 2005 5 6 CHQA200500082 220050413A7200 ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 2 FAILED A CHQAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL11280SK4900 4900 145381 CAE312346 DURING LATE STAGES OF CLIMB, AT APPROX 24500 FT., NOTICED A SPIKE IN NR 2 ITT OF 911 C. FOR 1 SEC. REDUCED THRUST ON NR 2, ITT RETURNED TO GREEN RANGE. LEVELED OFF AT FL260 & SET TO CRUISE. SET POWER TO SAME N1 TO ALLOW CHK OF ENG PARAMS. BOTH N1 SETTINGS 80.5 BUT NR 1 ITT-642 C, NR 2-792 C. NR 1 N2 90.1 & NR 2, 90.4. NR 1 FUEL FLOW 1230 PPH, NR 2-1480 PPH, FLT CONTINUED. AFTER 30 MINS RECEIVED EICAS MESSAGE "E2 FIRE DETECT FAIL." NO FIRE DETECTED, NR 2 SHUTDOWN & EMERGENCY DECLARED & DIVERTED. AFTER SHUTDOWN, NR 2 ITT REDUCED. FND NO FIRE ON NR 2. ACRFT LANDED UNEVENTFULLY. FOUND CUSTOMER SERVICE VALVE PANEL BLOWN FROM ENG & FIRE LOOP DAMAGED. R & R NR 2 ENG & FIRE LOOP IAW AMM. OPS & LEAK CHK GOOD. 2L72 4T4 FRTT00011ATTE6CH 20050506000492005050600049SO 2005 5 6 CHQA200500080 120050412A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11270SK 145304 UPPER RIGHT EXTERIOR EMERGENCY EXIT LIGHT IS INOP. RELAMPED EXTERIOR EMERGENCY EXIT LIGHT IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050506000502005050600050SO 2005 5 6 CHQA200500079 120050412A335066903 LIGHT EMB 135 EMB135LR 3260305SO CABIN INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11847RP 145608 FORWARD FLOOR EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED FORWARD FLOOR PROXIMITY LIGHT STRIP IAW EMB 135 AMM 33-50-12. OPS CHECK GOOD. 2L72 4F RTT00011AT 20050506000512005050600051SO 2005 5 6 CHQA200500078 120050411A33507287580505 LIGHT EMB 135 EMB135LR 3260305SO CABIN OUT OF ALIGNMENTA CHQAK NONE O OTHER ININSP/MAINT 1 GL11835RP 145702 FLOOR EMERGENCY EXIT LIGHTS DO NOT ALIGN WITH THE EXIT ROW. REARRANGED FLOOR PROXIMITY LIGHTS IAW AMM 33-50-10. OPS CHECK GOOD. 2L72 4F RTT00011AT 20050506000522005050600052SO 2005 5 6 CHQA200500081 120050412A3350RPS1B BATTERY PACK EMB 145 EMB145MP 3260216SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11973RP 145444 EMERGENCY LIGHT ABOVE LEFT HAND WING IS INOP. REMOVED AND REPLACED NR 3 AND NR 4 EMERGENCY BATTERIES IAW EMB 145 AMM 33-50-04. OPS CHECK GOOD. SERIAL NUMBERS REMOVED ARE 18764 AND 17419. 2L72 4F RTT00011AT 20050506000532005050600053EA 2005 5 6 DJFA2005082 120050413A3260327 BULB CNDAIRCL600 CL6002B16 1900305EA MLG INDICATOR BURNED OUT E DJFAL ABORTED APPROACH P NO WARNING INDICATION APAPPROACH 1 EA23653CW 5053 KTYS - KLIT TRIP ID NR 811531 CREW REPORTED THAT AFTER SELECTING GEAR DOWN FOR LANDING THEY NOTED THAT THE LEFT MAIN GEAR GREEN LIGHT WAS NOT ILLUMINATING. CREW FLEW PAST THE TOWER TO VERIFY THAT THE GEAR WAS DOWN. NO OTHER UNSAFE INDICATIONS WERE NOTED. FIRE/RESCUE RESPONSE WAS GIVEN AND AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED (2) NR 327 BULBS. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20050506000542005050600054CE 2005 5 6 20030827 120050330A5311 FRAME BEECH 1900 1900D 1154162CE FUSELAGE CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03122UX UE122 DURING ROUTINE INSPECTION, A .63 INCH CRACK WAS FOUND ON THE INTERCOSTAL FRAME FLANGE AT FS 482.75 BELOW STRINGER 2L. CRACK WAS REPAIRED IAW WITH EO. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA24CE 20050506000582005050600058EU 2005 5 6 05FDEA00989 120050413A3150350B53005313 COMPUTER AIRBUS300 A300F4605R 3930327EU FLT WARNING MALFUNCTIONED A FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25663FE 766 ON TAKEOFF, AFTER TOGA, ENGINES STABLE AT APPROX 98 PERCENT N1 PASSING 60 KTS: ECAM SINGLE CHIMED WITH "ENGINE 1 SHUTDOWN PROCEDURE". RTO COMPLIED WITH. ALL ENGINE ANALOG INDICATIONS WERE NORMAL. REMOVED AND REPLACED NR 1 FWC PER 31-53-34-4. OPS NORMAL. NR 2 FWC PREVIOUSLY CHANGED WRI NR 31-50/8031. PERFORMED AFS/LAND TEST PER 22-00-00-5 AND 22-40-00-5. OPS NORMAL. PERFORMED FWC INPUTS TEST PER 31-51-00-5. OPS NORMAL. PERFORMED ADJ/TEST SYSTEM MONITOR PER 22-40-00-5. OPS NORMAL. A/C REMAINS CAT IIIB AND RVSM CERTIFIED. 2L72 4F RTA35EU 20050506000652005050600065WP 2005 5 6 UPS05844269 120050320A5320 CHANNEL DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 C2 CEILING RIB CORRODED WITH CORROSION UNDER RADIUS FILLER RT W/W ABOVE FLAP BUSS DIRECTION CHANGE PULLEYS STA 930 RBL 58. REMOVED AND REPLACED HAT CHANNEL, STIFFENER, AND U-CHANNEL IAW DWG 5 645332, SRM TR 51-130, AND SRM 51-1-21 AND 51-2-1 FIG 1. 2L74 4F RT4A25 20050506000662005050600066WP 2005 5 6 UPS05844273 120050404A5712 RIB DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 C1 LT WING OB LEADING EDGE UPPER RIB CRACKED 12 INCH OB OF IB END. REPAIRED BY STOP DRILLING AND INSTALLING REPAIR ANGLE IAW SRM 57-2-0. 2L74 4F RT4A25 20050506000682005050600068WP 2005 5 6 UPS05844275 120050401A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 C1 LONGERON .25 INCH LONG CRACKED AT STATION 1726 L15L. REPAIRED LONGERON BY CUTTING OUT DAMAGE. INSTALLING FILLER AND DOUBLER IAW SRM 53-02-02 FIG 11 AND 51-1-20D. 2L74 4F RT4A25 20050506000712005050600071WP 2005 5 6 UPS05844278 120050402A534045976432N FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 C1 FRAME TO CUSP FITTING CRACKED .25 INCH LONG AT STA 260 L21R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-0. 2L74 4F RT4A25 20050506000722005050600072WP 2005 5 6 UPS05844279 120050405A5320 CUSP WEB DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 C1 C PIT STA 1043 RT CUSP RBL 58, VIEW LOOKING UP AT DISHPAN, 2 CRACKS PERPENDICULAR TO EACH OTHER APPROX 2 INCH IN LENGTH EACH. REPAIRED BY STOP DRILLING AND INSTALLING DOUBLER IAW EO DC8 5330-2159B SRM 51-1-15, 51-1-21A. 2L74 4F RT4A25 20050506000732005050600073NM 2005 5 6 DHL2005782569 120050311A5753 STRIP BOEING727 727227 1384078NM TE FLAPS MISSING A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 LEFT I/B FORE FLAP WBL 70 UPPER SURFACE HAS CHAFE STRIP MISSING. REMOVED AND INSTALLED LEFT I/B FORE FLAP AFTER SHEET METAL REPAIR IAW B727 MM 27-51-1, OP CHECK GOOD IAW B727 27-51-0. CUT OUT DAMAGE SKIN, FABBED FILLER 3.5 X 2.5 INCH & DOUBLER 5 X 4 INCH FROM 2024T3 .010 PO 9001660 IAW 727 SRM 57-50-2 FIG 3. BONDED, CLEANED, TREATED, PRIMED, & SEALED REPAIR PARTS IAW 727 SRM 51-40-20 FIG 30. INSTALLED NEW CHAFE STRIPE DIM 13 X 2.25 INCH, P/N 301 1/2 H2 .032 PO 900878 IAW 727 MM 51-51-11. OPS CHECK GOOD 727 MM 27-51-00. 2L73 4F A3WE 20050506000752005050600075EU 2005 5 6 05FDEA00999 120050414A5753 FLAP TRACK AIRBUS310 A310 EU WINGS DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 COMPLY WITH EA 6-5720-86138 REV NO POS P2 WING INSPECTION FLAP TRACK MOVABLE FAIRING. LT NR 2, 4, 5 AND RT NR 3,5. COMPLIED WITH EAN 6-5720-86138 AND REPORTED FINDINGS TO FED EX VIA MAXI MERLIN. 2L72 4F RTA35EU 20050506000762005050600076EA 2005 5 6 SWIA200514866 120050414A274170609 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07460SW 7803 STAB TRIM CH 1 KICKED OFF DURING FLIGHT. REPLACED HSTCU PER CRJ MM 27-41-00. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050506000772005050600077SO 2005 5 6 SWIA200514867 120050413A3350 LAMP EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07227SW 120304 EMERGENCY LIGHT AT PAX ENTRY INOPERATIVE. RELAMPED. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050506000792005050600079NM 2005 5 6 05FDEA00987 120050413A5743 BEAM BOEING727 727227 1384078NM LT MLG CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 CORROSION ON LT MLG BEAM LOWER SURFACE. REPAIRED PER EA 7-5710-86267. 2L73 4F A3WE 20050506000802005050600080WP 2005 5 6 05FDEA01000 120050414A78309105M20G150S2 CHANNEL DOUG DC10 DC1030 3023501WP ZONE 600 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25301FE 46800 COMPLY WITH EA8-7832-55467, EXHAUST-TR-ASSY BLENDING OF CHAFED AREA ON CLOSOUT CHANNEL. CLOSEING ACTION ON 04/15/05. ON N/R S00010. COMPLIED WITH EA 8-7832-55467. 2L73 4F A22WE 20050506000822005050600082 2005 5 6 05FDEA01002 420050414A3418 COMPUTER DOUG DC10 DC1010 3022110WP STALL WARNING MALFUNCTIONED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO2510060 46970 CLIMBING THROUGH 5000 FT, WINGS LVL, THERE WAS A STICK SHAKER ANNUNCIATION WITH ASSOCIATED SLAT RESET LIGHT DUE TO AUTO-SLAT EXTEND. COMPLETED UNSCHEDULED AUTO SLAT EXTENSION &/OR UNSCHEDULED STICK SHAKER RED TAB PROCEDURE. ELECTED TO RETURN TO IND, & LANDED UNEVENTFULLY. PERFORMED ADJ/TEST OF BOTH AT/SC COMPUTERS NR 1 CKS NORMAL. NR 2 COMP TEST WAS INTERMITTENT. R/R,D NR 2 AT/SC AND TESTED PER DC10-10 AMM 22-31-01-2. SYS OPS CHK NORMAL. PERFORMED ADJ/TEST OF BOTH NR 1 & NR 2 LAU,S PER DC10-10 AMM 22-11-01-2. BOTH OPS CHK NORMAL. AUTO SLAT TEST PER DC10-10 AMM 22-30-00-5. SYS OPS CHK OK. STALL WARNING TEST OF NR 1 AND NR 2 SYSTEMS FROM COCKPIT PER DC10-10 AMM 22-33-00-0. BOTH SYSTEMS OPS CHK OK. 2L73 4F A22WE 20050506000832005050600083NM 2005 5 6 FX7A200500004 120050413A5610571762309 WINDOW BOEING727 727214 138407RNM PWA JT8 JT8D17 52049NE COCKPIT CRACKED A FX7AA UNSCHED LANDING O OTHER CRCRUISE 1 SO19211DB 20766 R-2 WINDOW OUTER PANE CRACKED. 2L73 4F4 F A3WE E2EA 20050506000862005050600086EA 2005 5 6 COMA0560258 120050411A2721601R12263 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA RUDDER TRIM MALFUNCTIONED A COMAC ABORTED TAKEOFF FJ FLT CONT AFFECTED WARNING INDICATION TOTAKEOFF 1 SO01796CA 7338 FLIGHT 5220 RUDDER CONFIG MESSAGE DURING T/O. REPLACED THE RUDDER TRIM PANEL. 2L72 4F RTA21EA 20050506000872005050600087NE 2005 5 6 COMA0560257 220050414A72616087T04P05 PUMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT ENGINE FAULTY A COMAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SO01436CA14930 7482 FLIGHT 5440 DURING CRUISE FLT (JFK-JAX) RT ENGINE OIL PRESSURE INDICTION DROPPPED TO 25 PSI ASSOCIATED WITH AN OIL PRESSURE WARNING, CREW DECLARED AN EMERGENCY, SHUT DOWN THE RIGHT ENGINE, DIVERTED TO CHS AND LANDED WITHOUT INCIDENT. REPLACED THE RIGHT ENGINE OIL PUMP. 2L72 4F4 FRTA21EA E15NE 20050506000882005050600088EA 2005 5 6 COMA0570043 120050413A2760 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA SPOILERS MALFUNCTIONED A COMAO OTHER JF WARNING INDICATION FLT CONT AFFECTED DEDESCENT 1 SO01368CA 10075 FLIGHT 5866 SPOILERON AND FLIGHT SPOILER CAUTION. RESET THE SSCU AND SYSTEM OPERATION NORMAL. COULD NOT DUPLICATE. 2L72 4F RTA21EA 20050506000902005050600090NM 2005 5 6 DHL2005770006 120050412A3150 WARNING HORN BOEING727 7272B7 138407LNM COCKPIT ACTIVATED A DHLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01770AT 21953 REJECTED TAKEOFF IN CVG FOR TAKEOFF WARNING HORN. COULD NOT DUPLICATE. SECOND T/O NORMAL. RNW 36L, BELOW 10 KTS IAS, 148000 LBS, TEMP 18 DEGREES CELSIUS. RTO INFO CVG RNWY 36L, LESS THAN 10 KTS IAS, TEMP 18 DEGREES CELSIUS, 148,000 LBS NOTED. PERFORMED T/O WARNING SYS TEST PER B727 MM 31-26-0, OPS CHECK GOOD. 2L73 4F A3WE 20050506000922005050600092EA 2005 5 6 VTZA200500048 120050415A5320601R3117117 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27640BR 7340 INTERCOSTAL CRACKED AT .25 INCH IN LENGTH ON LT SIDE AT FS 484 LEFT BETWEEN BL 36.00. 2L72 4F RTA21EA 20050506000942005050600094EA 2005 5 6 VTZA200500050 120050415A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27640BR 7340 LEFT FS 718 FRAME CRACKED AT 1 INCH IN LENGTH IN RADIUS. 2L72 4F RTA21EA 20050506000962005050600096EA 2005 5 6 VTZA200500052 120050415A5320601R536066 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27640BR 7340 LEFT ENGINE SUPPORT BEAM IS CRACKED IN LOWER WEB AT .75 INCH. 2L72 4F RTA21EA 20050506000992005050600099NM 2005 5 6 DHL2005782570 120050316A5330 SKIN BOEING727 727227 1384078NM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 CRACK ON PREVIOUS REPAIR RADIUS AT STR 21 FUSELAGE STA 950. REMOVED INTERCOSTAL AT STR 21 FUSELAGE STA 950 LT IAW SRM 51-30-2, FABRICATED NEW INTERCOSTAL USING 7075T6 .080 PO 9002012 SIZE 16 X 6 INCH IAW B727 SRM 53-10-2 AND INSTALLED INTERCOSTAL IAW B727 SRM 53-10-2 FIG 5. 2L73 4F A3WE 20050506001012005050600101NM 2005 5 6 DHL2005782572 120050413A5754 ATTACH FITTING BOEING727 727227 1384078NM SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 NR 5 SLAT ACTUATOR ATTACH POINT IS CRACKED INSIDE SLAT. DISCONNECTED NR 5 SLAT ACTUATOR FOR ACCESS IAW 727 MM 27-81-22. OPENED SLAT INNER SKIN IAW 727 SRM 51-30-2. REMOVED DAMAGED PART AND FABBED FROM 2024T3 .071 PO 9001978 DIM 12 X 4.5 INCH IAW 727 SRM 57-50-2 FIG 2. PART TREATED, PRIMED, AND INSTALLED IAW 727 SRM 51-10-2 & 51-30-2. RECONNECTED NR 5 SLAT ACTUATOR IAW 727 MM 27-81-22. ACCOMPLISHED OPS & LEAK CHECK OK IAW 727 MM 27-81-0. 2L73 4F A3WE 20050506001042005050600104NM 2005 5 6 05FDEA01020 120050415A5553651680221 ATTACH FITTING BOEING727 727227 1384078NM VERTICAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 CORROSION VERTICAL STAB TENSION TIE LT FWD FITTING IS CORRODED. REPAIRED PER EA 7-5530-86277. 2L73 4F A3WE 20050506001092005050600109NM 2005 5 6 C8GA20050010 120050415A2752MS9391130ZE MOTOR BOEING727 727227 1384078NM FLAP DRIVE LEAKING A C8GAA UNSCHED LANDING K FLUID LOSS CLCLIMB 1 SO15308AS46800 22002 FLT 712 FROM TOL TO DEN. 10 MINUTES AFTER TAKE OFF AT FL190, CREW NOTICED LOSS OF SYSTEM A-HYDRAULIC FLUID FOLLOWED BY ILLUMINATION OF HYDRAULIC LOW PRESSURE LIGHTS. CREW DUMPED 600 LBS OF FUEL, RETURNED TO TOL, AND LANDED WITHOUT INCIDENT. FOUND RT OUTBOARD FLAP HYDRAULIC DRIVE MOTOR LEAKING. REPLACED FLAP DRIVE MOTOR. OPS AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L73 4F A3WE 20050506001112005050600111WP 2005 5 6 05FDEA01028 120050416A5314AJC7028502 KEELBEAM DOUG MD10 MD1010F 3022112WP ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25362FE 48261 AUXILIARY POWER UNIT KEEL CAP ASSEMBLY HAS 9 INCH CRACK FROM FUSELAGE STATION 2019 TO STATION 2028 AT STRINGER 45 RIGHT. REPAIRED STRINGER IAW EA 8-5310-83868, FUSELAGE - AFT BODY KEEL CAP SPLICE AT STA 2040 - REPAIR, AND MD 10 SRM 51-31-01 VOL 2 AND 51-31-01 VOL 2. 2L73 4F RTA22WE 20050509000032005050900003EU 2005 5 9 WRNA200500010 120050416A5270 CONNECTOR AIRBUS300 A300B4203 3930306EU DOOR SWITCH LOOSE A WRNAJA DUMP FUEL UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO05502TA 075 DURING CLIMB DOORS LIGHT ON MWP CAME ON WITH C1 DOOR OPEN LIGHT AND CARGO SWITCH FAULT LIGHT ON. AIRCRAFT DUMPED FUEL FOR APPROVED LANDING WEIGHT. RETURNED TO AIRFIELD, LANDING NORMAL. MAINTENANCE FOUND CONNECTOR AT SWITCH 14WS NOT SECURED. CLEANED AND SECURED SWITCH, OP'S CHECK GOOD IAW 52-71-11 PAGE 501. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA35EU 20050509000042005050900004NM 2005 5 9 05FDEA01033 120050416A2510 STOP BOEING727 727200 138407ENM ZONE 800 MISSING A FDEAK NONE O OTHER ININSP/MAINT 1 SO25271FE 22036 COMPLY WITH EA 7-2510-55477 REPLACEMENT OF MISSING DOOR STOP. COMPLIED WITH EA 7-2510-55477. 2L73 4F RTA3WE 20050509000072005050900007NM 2005 5 9 P5CA0501337 120050417A3610 CLAMP BOEING747 747230B 1384889NM GE CF6 CF650E2 30018NE NR 2 HIGH STAGE LOOSE A P5CAEC ENGINE SHUTDOWN ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA15508MC 21644 517772 ON TAKEOFF GROUND ROLL & SETTING TAKEOFF THRUST AT 105.4 DEGREES. SET ROLLING APPROXIMATELY 90 KNOTS. NR 2 ENGINE FIRE LIGHT CAME ON, ABORTED TAKEOFF WITH THROTTLES BACK AT IDLE & SHUT DOWN NR 2 ENGINE. BOTH A & B LOOPS READING 8 UNITS. BRAKE TEMPS ALL GREEN. FOUND NR 2 HIGH STAGE VALVE CLAMP LOOSE. RESEATED & RETORQUED CLAMP PER MM 36-11-05. ACCOMPLISHED DUCT LEAK CHECK PER MM 05-51-30, NO LEAKS. ACCOMPLISHED HIGH ENERGY STOP PER 05-51-10. 2L74 4F4 F A20WE E23EA 20050509000092005050900009SO 2005 5 9 CHQA200500085 120050415A2730 YOKE EMB 135 EMB135LR 3260305SO VIBRATION A CHQAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL11835RP 145702 AFTER DEPARTING RUNWAY 35L AT MCO, INSTRUCTED TO TURN TO A WEST HEADING & MAINTAIN 8000 FT. LEVELED OFF & STARTED ACCELERATING TO 250 KNOTS. PASSING THROUGH 230 KNOTS FELT AN UNUSUAL FLUTTER IN YOKE & TAIL. SLOWED A/C DOWN & TOLD TO CLIMB. AGAIN PASSING THROUGH 240 SEEMED WORSE. CONTACTED ATC FOR ABOUT A MINUTE & CONTINUOUSLY BLOCKED BY OTHER AIRCRAFT. EMERGENCY DECLARED. DURING DESCENT, FLUTTER FELT AGAIN & SPEED ABOUT 220 KNOTS & SLOWING. ACRFT LANDED WITHOUT INCIDENT & TAXIED BACK TO GATE. MX PERFORMED INSPECTION OF FLT CONTROLS & FOUND NO DISCREPANCIES. PERFORMED ELEVATOR CABLE TENSION CHK IAW EMB 135 27-31-01. OPS CHK GOOD. TENSION CHK OF ELEVATOR GOOD IAW EMB 135 AMM 27-21-1. NO DEFECTS NOTED. 2L72 4F RTT00011AT 20050509000112005050900011SO 2005 5 9 C2XA05CL020 120050413A3350375911 SIGN EMB 135 EMB135ER 3260203SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715509 145238 DURING ROUTINE MAINTENANCE, THE EXIT ROW EMERGENCY EXIT SIGN DID NOT ILLUMINATE DURING TESTING. MAINTENANCE REPLACED THE EXIT SIGN AND OPERATIONAL TESTS WERE GOOD. 2L72 4F RTT00011AT 20050509000122005050900012SO 2005 5 9 C2XA05SH024 120050410A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713913 145438 SHV-DURING SERVICE/ROUTINE CHECK, THE AFT CABIN OVERHEAD EMERGENCY LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE LAMP IAW EMB 145 AMM33-50-08. THE ENSUING OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050509000142005050900014EU 2005 5 9 DHL2005367501 120050403A5347THS6022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU ZONE 100 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01367DH 265 DURING C-CHECK, N/R 018791 CABIN SEAT TRACK AT FR 18 THRU 21 AT BL 78 L HAS CORROSION (MKD). REMOVED AND REPLACED SECTION OF SEAT TRACK 140 INCH LONG P/N TMS 60-22457 PO 21136224 AS PER A-300 SRM 51-10-40. ALODINE AND PRIMED AS PER A-300 SRM 51-40-12 AND TOP COAT PAINT AS PER A-300 SRM 51-40-2. 2L72 4F RTA35EU 20050509000152005050900015EU 2005 5 9 DJFA2005077 220050408A7200TAY6118 ENGINE GULSTMG1159 GIV 3980115SO RROYCETAY TAY6118 EU RIGHT FAILED E DJFAFA ACTIVATE FIRE EXT. UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 EA23181CW117577402 1001 16012 KMIA TRIP ID NR 812480, CREW REPORTED THAT THE RIGHT ENGINE FAILED WITH A VERY LOUD BANG SHORTLY AFTER THE GEAR WAS RETRACTED. A SEVERE SHUTTER WAS FELT THROUGHOUT THE AIRCRAFT AFTER THE ENGINE FAILURE. THE RIGHT FIRE HANDLE WAS PULLED AND THE NR 1 EXTINGUISHER WAS SHOT DUE TO A VERY HIGH TGT READING. AIRCRAFT MADE AN UNEVENTFUL LANDING IN KMIA. MAINTENANCE REPLACED THE RIGHT ENGINE AND FIRE BOTTLE. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA12EA E25NE 20050509000162005050900016NM 2005 5 9 CALA0500102 120050415A531565C33950 FLOORBEAM BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716617 27330 CABIN FLOOR CORROSION AT STA 986.5, APPROXIMATELY 48 INCHES. REPLACED BEAM PER SRM 53-00-51 FIG 203. 2L72 4F RTA16WE 20050509000172005050900017NM 2005 5 9 CALA0500103 120050416A5320BAC1520377 ANGLE BOEING737 737524 1384721NM FUSLEAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718612 27325 AFT BAG BIN RIGHT PANEL HAS CORROSION AT STA 727-847. INSTALLED PANEL PER SRM 51-40-01. 2L72 4F RTA16WE 20050509000202005050900020NM 2005 5 9 CALA0500106 120050417A3350D71701100 BATTERY PACK BOEING737 737824 13844BZNM EMERGENCY LIGHT INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2727239 28951 LAST SECTION OF AISLE EMERGENCY LIGHTS INOPERATIVE. REPLACED AND TESTED BATTERY PACK. 2L72 4F RTA16WE 20050509000222005050900022NM 2005 5 9 RYNA200500012 120050408A75407898301 TRANSMITTER BOEING757 75728A 1384976NM RROYCERB211 RB211535E4 54555NE NR 1 ENGINE INOPERATIVE A RYNAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE07753NA 24544 30752 DURING CLIMB-OUT ABOVE 14,000, THE CREW NOTICED AN ABNORMAL SPLIT IN ENGINE PARAMETERS WITH THRUST LEVERS MATCHED UP. WHEN TRYING TO MATCH EPR, THERE WAS A HUGE SPLIT IN THRUST LEVER POSITION AND N1, N2, N3, EGT AND FUEL FLOW. AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 EPR TRANSMITTER. OPERATIONAL CHECK NORMAL. 2L72 4F4 FRTA2NM E12EU 20050509000232005050900023WP 2005 5 9 0500529860 120050415A2721258782651 COMPUTER DOUG DC9 DC951 3022051WP RUDDER STAB AUG MALFUNCTIONED A NWAAO OTHER F FLT CONT AFFECTED CLCLIMB 1 GL01769NC17569193 47757 DURING TAKEOFF ROTATION, THE AIRCRAFT YAWED TO THE LT EVENTUALLY REQUIRING FULL RT RUDDER TRIM AND RT WING DOWN. COMPLIED WITH COM PROCEDURES AND FLT WAS ABLE TO CONTINUE TO SCHEDULED DESTINATION. CREW STATED THE LT RUDDER PEDAL WAS ABOUT 5 INCHES FORWARD AND JAMMED AND HAD NO LT RUDDER EFFECT IN MANUAL CONTROL. THE LANDING AT DTW WAS UNEVENTFUL. MAINTENANCE REPLACED THE STABILIZER AUGMENTATION COMPUTER, A JAMMED RUDDER TRIM PEDESTAL KNOB SPIRAL DRIVE TRIM PLATE ASSEMBLY, INDICATOR, AND PEDAL FOLLOWER. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050509000242005050900024NM 2005 5 9 UPS05444294 120050416A3350 LIGHT BOEING747 747123F NM MAIN DECK INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01677UP 20391 MAIN DECK FWD EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY, OPS CHECKED OK. 2L74 4F A20WE 20050509000262005050900026WP 2005 5 9 UPS05844282 120050415A33506012235 BATTERY PACK DOUG DC8 DC873F 302199FWP COCKPIT DISCHARGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 INSPECTION TYPE:N/A EMERGENCY LIGHTS BATTERY DEAD. REMOVED AND REPLACED BATTERY PACK PER DC-8 AMM CH 33-50-01-2. OP CHECKS GOOD. 2L74 4F RT4A25 20050509000322005050900032NE 2005 5 9 COMA0560259 220050415A72616087T04P06 PUMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT ENGINE FAILED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01498CA5726 7792 FLIGHT 5170 DURING CRUISE FLT (BTV/CVG) RECEIVED A RIGHT ENGINE OIL PRESSURE WARNING, CREW DECLARED AN EMERGENCY, PERFORMED RT ENGINE IFSD PROCEDURE, DIVERTED TO BUF AND LANDED WITHOUT INCIDENT. REPLACED THE RT ENGINE LUBRICATION AND SCAVENGE PUMP ASSEMBLY. 2L72 4F4 FRTA21EA E15NE 20050509000342005050900034NM 2005 5 9 RYNA200500014 120050409A3810 POTABLE WATER BOEING737 737201 1384454NM LEAKING A RYNABA EMER. DESCENT UNSCHED LANDING KGJFLUID LOSS MULTIPLE FAILURE WARNING INDICATION CRCRUISE 1 CE07235US 22275 DURING CRUISE AT FL 28.0, EXPERIENCED MULTIPLE MALFUNCTIONS. AUTO-PILOT FAILED, PRESSURIZATION AUTO FAIL LIGHT ILLUMINATED, MACH TRIM FAIL LIGHT ILLUMINATED, ALTITUDE ALERTER FAILED, CAPTAIN'S IVSI FLAG IN VIEW, CAPTAIN'S ALTIMETER FLAG IN VIEW AND LAV SINK WATER WILL NOT SHUT OFF. AN EMERGENCY WAS DECLARED AND AIRCRAFT LANDED AT MEM WITHOUT INCIDENT. PULLED AND DRIED AUTO-PILOT ACCESSORY BOX, PRESSURE CONTROLLER, MACH TRIM COMPUTER, ALT ALERTER CONTROLLER AND AIR DATA COMPUTER. DEACTIVATED POTABLE WATER SYSTEM. OPERATIONAL CHECK NORMAL. 2L72 4F A16WE 20050509000352005050900035EA 2005 5 9 COMA0560261 120050417A2150 ACM CNDAIRCL600 CL6002B19 1900309EA BOTH TRIPPED A COMAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 SO01977CA 7157 FLIGHT 5349 THE LEFT AND RIGHT AIR CONDITIONING PACKS TRIPPED OFF LINE DURING CRUISE FLIGHT (LEX/ATL) AND WOULD NOT RESET, CREW DECLARED AN EMERGENCY AND LANDED AT ATL WITHOUT INCIDENT. RESET CBP1 J1, PERFORMED OPERATIONAL CHECK OF BOTH PACKS. 2L72 4F RTA21EA 20050509000362005050900036EA 2005 5 9 COMA0560262 120050415A3397 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT LOOSE A COMAK NONE L NO TEST ININSP/MAINT 1 SO01807CA 7364 FLIGHT 5426 THE CABIN DOOR EMERGENCY EXIT SIGN FAILED TO ILLUMINATE DURING TEST. REPLACED CONNECTOR ST310 AT EMERGENCY SIGN. 2L72 4F RTA21EA 20050509000372005050900037EA 2005 5 9 COMA0560263 120050416A5270 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR UNSECURE A COMAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 SO01779CA 7306 FLIGHT 5580 DURING CRUISE FLIGHT (MDT/CVG) RECEIVED A CABIN DOOR OUTER HANDLE CAUTION MESSAGE, AIRCRAFT DIVERTED TO MDT. FOUND CABIN DOOR OUTER HANDLE NOT FULLY STOWED, CYCLED CABIN DOOR, ALL INDICATIONS NORMAL. 2L72 4F RTA21EA 20050509000382005050900038EA 2005 5 9 COMA0560264 120050417A32304622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG FAILED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01979CA20236 7159 FLT 5035 RECEIVED A GEAR DISAGREE CAUTION DURING CLIMBOUT OF CVG, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD LANDING WITHOUT INCIDENT. REPLACED THE NLG PRIORITY VALVE. 2L72 4F RTA21EA 20050509000422005050900042EA 2005 5 9 COMA0570044 120050417A2780766359B DRIVE UNIT CNDAIRCL600 CL6002C10 1390015EA SLATS FAULTY A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01371CA6245 10082 FLIGHT 5613 DURING ATL APPROACH RECEIVED A SLAT FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED THE SLAP POWER DRIVE UNIT. 2L72 4F RTA21EA 20050509000432005050900043EA 2005 5 9 COMA0570045 120050417A2780766389L CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA E/E BAY FAULTY A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01371CA6245 10082 FLIGHT 5613 DURING ATL APPROACH RECEIVED A SLAT FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED THE SLAP/FLAPS ELECTRONIC CONTROL UNIT (SFECU). 2L72 4F RTA21EA 20050509000442005050900044NE 2005 5 9 FX7A200500005 220050415A7300 SHAFT BOEING727 727224 1384076NM PWA JT8 JT8D15 52051NE PUMP SHEARED A FX7AA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 SO1979749 1073 22451 ENGINE FLAME OUT NR 1 DURING CRUISE. UPON TROUBLESHOOTING, MAINTENANCE FOUND THE NR 1 ENGINE FUEL PUMP SHAFT SHEARED, REMOVED AND REPLACED THE NR 1 ENGINE FUEL PUMP AS PER MAINTENANCE MANUAL REFERENCE 73-11-1, PERFORMED OPS/LEAK CHECK. 2L73 4F4 F A3WE E2EA 20050509000472005050900047NM 2005 5 9 ASMF200504012 120050412A213046D161 PRESSURE SWITCH DOUG MD88 MD88 3023688NM RT A/C PACK FAILED W ASMFA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW23168PL20595 53174 AIRCRAFT RETURNED FLIGHT AS A CONSEQUENCE OF DURING CLIMB, AIR CONDITIONING SYSTEM WITHOUT FLOW AND ALTITUDE PRESSURE LIGHTS TURNED ON. DURING REVISION AIR CONDITIONING SYSTEM WAS FOUND TURNED ON WITHOUT PRESSURE AND FLOW, THE AUTOMATIC AIR CONDITIONING SHUTOFF BREAKER WAS TURNED TO OVERRIDE REESTABLISHING THE SYSTEM. AIRCRAFT WAS SENT TO THE HANGAR AND WIRING AND SECOND SEGMENT SWITCH WAS DETECTED GROUNDED. THE WIRING WAS REPAIRED AND AT PRESSURIZATION TEST WAS DETECTED SWITCH DAMAGED, THE SWITCH S1-296 WAS REPLACED IAW MM 21-31-09, TESTED CORRECT. TEST FLIGHT WAS PERFORMED AND AIR CONDITIONING SYSTEM OPERATED CORRECTLY. 2L72 4F RTA6WE 20050509000502005050900050EA 2005 5 9 QXEA200500580 120050323A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - CENTER FUSELAGE LEFT SIDE LOWER SKIN AT STATION 565.0 AND UPPER EDGE OF DOOR CUTOUT HAS SKIN NICKED. REPAIRED IAW CRJ700 SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050509000522005050900052EA 2005 5 9 QXEA200500582 120050321A5414 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 400 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - LEFT NACELLE, AFT CORE COWL, UPPER INBOARD SIDE HAS NUMEROUS SCRATCHES. REPAIRED IAW CRJ700 SRM 54-13-00-101-001-A01 AND SRM 51-12-00-001-001-A01. 2L72 4F RTA21EA 20050509000532005050900053EA 2005 5 9 QXEA200500576 120050327A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - CENTER FUSELAGE RIGHT SIDE AT STATION 477 AND STRINGER 21X HAS EVIDENCE OF PRESSURE LEAK AT SKIN BUTT JOINT. REPAIRED IAW CRJ SRM 51-23-00-001-001-A01 AND CRJ700 AMM 21-31-00-910-801. 2L72 4F RTA21EA 20050509000592005050900059EU 2005 5 9 AWXA200500453 120050415A2150757A000010 ACM AIRBUS320 A320232 3930326EU LEFT SEIZED A AWXAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP28653AW26582534 1003 LAS - EMERGENCY LANDING - FLT 0216 - EN ROUTE PHX TO LAS AT APPROXIMATELY FL 280 NOTICED AN ELECTRICAL BURNING SMELL IN COCKPIT FOLLOWED BY REPORT OF WHITE SMOKE IN CABIN BY FLIGHT ATTENDANT, DECLARED EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND LT PACK AIR CYCLE MACHINE SEIZED, REMOVED AND REPLACED AIR CYCLE MACHINE IAW AMM 21-52-21, OPERATIONAL CHECK WAS GOOD. UNABLE TO PERFORM PRETEST DUE TO HIGH BREAKAWAY TORQUE, UNIT SEIZED. VENDOR FAILURE ANALYSIS SHOWS THRUST BEARINGS AND SPRING SUPPORT WORN. UNIT WAS OVERHAULED AND TESTED IAW OEM 21-52-02 REV 7. 2L72 4F RTA28NM 20050509000612005050900061NM 2005 5 9 AWXA200500455 120050415A2560P4010021 BATTERY BOEING737 7373B7 1384580NM FLASHLIGHT DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28332AW 23384 LAS - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY IN THE FORWARD EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050509000622005050900062NM 2005 5 9 AWXA200500456 120050404A5312651758243 VERTICAL BEAM BOEING737 737301 1384611NM BULKHEAD CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - DURING C-19 CHECK 2 EACH .25 INCH CRACKS WERE FOUND IN BS 178 BULKHEAD VERTICAL BEAM WEB AT LBL 17.1, WL 230. MAINTENANCE CUT OUT DAMAGED AREA OF VERTICAL BEAM WEB AT BS 178 BULKHEAD, LBL 17.1, WL 230; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A NEW SECTION OF WEB AND FILLERS; INSTALLED REPAIR PARTS IAW B7B-300 SRM 53-10-08 FIG 212. 2L72 4F RTA16WE 20050509000632005050900063NM 2005 5 9 AWXA200500457 120050405A5312651758243 VERTICAL BEAM BOEING737 737301 1384611NM BULKHEAD CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - DURING C-19 CHECK A .25 INCH CRACK WAS FOUND IN BS 178 BULKHEAD VERTICAL BEAM WEB AT RBL 17.1, WL 230. MAINTENANCE CUT OUT DAMAGED AREA OF VERTICAL BEAM WEB AT BS 178 BULKHEAD, RBL 17.1, WL 230; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A NEW SECTION OF WEB AND A FILLER; INSTALLED REPAIR PARTS IAW B7B-300 SRM 53-10-08 FIG 212. 2L72 4F RTA16WE 20050509000642005050900064NM 2005 5 9 AWXA200500458 120050404A531265163007 BULKHEAD BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - DURING C-19 CHECK A .25 INCH CRACK WAS FOUND EXTENDING PAST STOP DRILL HOLE AND PREVIOUS REPAIR IN BS 178 BULKHEAD WEB AT LBL 5.7, WL 195. MAINTENANCE CUT OUT DAMAGED AREA OF WEB AT BS 178 BULKHEAD, LBL 5.7, WL 195; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A FILLER AND 2 EACH DOUBLERS; INSTALLED REPAIR PARTS IAW B7B-300 SRM 53-10-08 FIG 210. 2L72 4F RTA16WE 20050509000652005050900065NM 2005 5 9 AWXA200500459 120050404A531265163007 BULKHEAD BOEING737 737301 1384611NM FUSLEAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - DURING C-19 CHECK 4 EACH CRACKS WERE FOUND EXTENDING PAST STOP DRILL HOLE AND PREVIOUS REPAIR IN BS 178 BULKHEAD WEB AT RBL 5.7, WL 195. MAINTENANCE CUT OUT DAMAGED AREA OF WEB AT BS 178 BULKHEAD, RBL 5.7, WL 195; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A DOUBLER AND REPAIR FILLERS; INSTALLED REPAIR PARTS IAW B7B-300 SRM 53-10-08 FIG 210. 2L72 4F RTA16WE 20050509000662005050900066NM 2005 5 9 AWXA200500460 120050404A53126516300 FRAME BOEING737 737301 1384611NM BULKHEAD CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - DURING C-19 CHECK A .25 INCH CRACK WAS FOUND IN BS 178 BULKHEAD SIDE CHORD AT LBL 60, WL 207. MAINTENANCE REMOVED CRACKED SIDE CHORD AT BS 178 BULKHEAD, LBL 60, WL 207; FABRICATED A NEW REPLACEMENT CHORD PER DWG 65-16300; INSTALLED REPAIR PART IAW B7B-300 SRM 51-40-02. 2L72 4F RTA16WE 20050505000662005050500066EA 2005 5 5 COMA0560256 120050408A2130 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN PRESSURE FALSE ACTIVATIONA COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01938CA 7046 FLIGHT 5449 CABIN ALTITUDE WARNING. COULD NOT DUPLCIATE. NO DEFECTS FOUND WHEN CABIN PRESSURIZATION SYSTEM WAS TESTED. 2L72 4F RTA21EA 20050505000742005050500074CE 2005 5 5 20030826 120050412A5330 SKIN BEECH 1900 1900D 1154162CE FUSELAGE CORRODED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03240GL UE240 DURING ROUTINE INSPECTION, UNDER BELLY SKIN CORROSION WAS IDENTIFIED AT FS 225.5 TO FS 230.95 APPROX. 5.5 INCH BY 19.5 INCH. CORRODED SKIN WAS REPLACED AND REPAIRED IAW EO. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA24CE 20050505000782005050500078SO 2005 5 5 SIMA200509109 120050317A534714530659011 SEAT TRACK EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21641AE 145191 DURING MBV INSPECTION FOUND FORWARD CABIN LT FWD IB SEAT TRACK CORRODED AROUND FASTENERS. REMOVED AND REPLACED LT FWD IB SEAT TRACK IAW MM. AC RETURNED TO SERVICE. (K) 2L72 4T4 FRTT00011ATTE6CH 20050505000812005050500081NM 2005 5 5 GAIA05018OP 120050330A2611302842 SMOKE DETECTOR BOEING727 727251 138408HNM PWA JT8 JT8D15 52051NE CARGO DECK DIRTY A GAIAO OTHER N FALSE WARNING CRCRUISE 1 SW07278US 21157 DURING CRUISE, MAIN CARGO SMOKE WARNING ILLUMINATED IN FLIGHT. VISUAL INSPECTION REVEALED NO SMOKE IN CARGO AREA. FLIGHT CONTINUED TO DESTINATION, WHERE A LANDING WAS MADE WITHOUT INCIDENT. CLEANED SMOKE DETECTORS FROM NR1 TO NR 6. ON NR 1 REPLACED BOTH LIGHT BULBS, PERFORMED TEST OK. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L73 4F4 F A3WE E2EA 20050505001022005050500102SO 2005 5 5 SWIA200514846 120050412A27523430001005 ACTUATOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CLCLIMB 1 NM07565SW1032310323 120340 AFTER DEPARTURE, RECEIVED DISAGREEMENT FOR FLAPS (INBOARD PAIR). REPLACED LEFT INBOARD FLAP ACTUATOR, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050505001202005050500120EA 2005 5 5 SWIA200514864 120050330A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07959SW 7840 RBL 9 AT FS 280.00 OUTBOARD ANGLE IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. CLIP REPLACED IAW CRJ SRM 51-42-21 AND 51-42-06. 2L72 4F RTA21EA 20050506000062005050600006NM 2005 5 6 UIEA200500016 120050308A541465B940514 SKIN BOEING747 7472D7B 1384803NM NR 4 PYLON CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15527MC 22471 DURING INSPECTION, NR 4 PYLON, CRACK DAMAGE WAS FOUND AT PRE-COOLER EXHAUST CUTOUT LOWER AFT CORNER AT NACELLE STATION 248. THE NR 3 STIFFENER WAS REINFORCED WITH A NEW STEEL LOWER REPAIR ANGLE FROM NACELLE STATION 235 TO STATION 254. THE RIB INSTALLATION AT NACELLE STATION 248 WAS MODIFIED TO ACCOMODATE THE NEW STEEL LOWER REPAIR ANGLE INSTALLATION ON THE NR 3 STIFFENER. (M) 2L74 4F RTA20WE 20050506000082005050600008NM 2005 5 6 UIEA200500030 120050321A575365B1161417 LINK BOEING747 7472D7B 1384803NM NR 4 FLAP TRACK MIGRATED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15527MC 22471 DURING SCHEDULE MAINTENANCE, NR 4 T/E FLAP TRACK FAIL/SAFE LINK TOP END BEARING ON THE 'T' CHORD FOUND MIGRATED. THE LEFT FIXED TRAILING EDGE UPPER CHORD HOLE HAS ELONGATED DAMAGED. OVERSIZED HOUSING BORE TO A MAXIMUM OF .8930 INCH DIAMTER. NDT INSPECTED THE REWORKED AREA TO ENSURE DEFECT FREE CONDITION. INSTALLED CRES SPLIT SLEEVE BUSHING WITH SHRINK FIT METHOD AN CHAMFERS TO MATCH DRAWING REQUIREMENT FOR NEW BEARING INSTALLATION. DETAIL VISUAL INSPECT THE REPAIR AREA AT C-CHECK INTERVALS NOT TO EXCEED 18 MONTHS. ATLAS AIR EO 4757A169 ISSUED TO ACCOMPLISH THE INSPECTION. (M) 2L74 4F RTA20WE 20050506000102005050600010NM 2005 5 6 UIEA200500033 120050323A5397 SEAT TRACK BOEING747 747243B 1384830NM CABIN DAMAGED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15540MC 22508 MAINTENANCE PICK UP DURING DAILY CHECK, FOUND MAIN DECK SEAT TRACK DAMAGED AT STATION 1730. CUT OUT DAMAGED AREA AND REPAIRED PER SRM 53-10-05 FIG 1A. (M) 2L74 4F A20WE 20050506000252005050600025NM 2005 5 6 UIEA200500038 120050324A575365B170688 SPAR BOEING747 7472D7B 1384803NM FLAP TRACK CORRODED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15527MC 22471 DURING SCHEDULE INSPECTION, CORROSION WAS FOUND ON THE REAR SPAR ATTACHMENT HOLES OF NR 5 TRAILING EDGE FLAP TRACK. OVERSIZED THE AFFECTED ATTACHMENT HOLES. MAGNETIC PARTICLE INSPECTED THE REWORKED AREA TO ENSURE CRACK AND DEFECT FREE CONDITION. THE REPAIRED HOLES WERE REPAIRED USING 17-4PH SLEEVE. DETAIL VISUAL INSPECT THE AFFECTED EXPOSED FLANGE EDGES FOR CRACKS FOR CORROSION EVERY C-CHECK INTERVAL NOT TO EXCEED 18 MONTHS. EO 4757A168 ISSUED TO ACCOMPLISH THE INSPECTION. (M) 2L74 4F RTA20WE 20050506000312005050600031NM 2005 5 6 SWAA051093 120050413A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050506000352005050600035NM 2005 5 6 SWAA051078 120050412A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29330SW 23694 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STR 25R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050506000362005050600036NM 2005 5 6 SWAA051079 120050413A335010107451 LIGHT BOEING737 7373H4 1384600NM LT OVERWING EXITLOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 LEFT OVERWING EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT PER MM. 2L72 4F RTA16WE 20050506000462005050600046CE 2005 5 6 DXTA200500679 120050414A2130 PRESSURE SYSTEM CESSNA500 560CESSNA 2076750CE CABIN FLUCTUATES E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL07335QS 5600335 WILD PRESSURIZATION FLUCTUATIONS ON TAKEOFF SHORTLY FOLLOWED BY A PECULIAR ODOR. PRESSURE FLUCTUATIONS APPEARED TO BE ASSOCIATED WITH POWER CHANGES. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20050506000572005050600057WP 2005 5 6 05FDEA00988 120050413A5330 SKIN DOUG MD10 MD1010F 3022112WP ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25372FE 46610 FOUND INDICATIONS OF CORROSION SUCH AS DIMPLED FASTENER HEADS AND SKIN BULGING AT FS 1139 AND STRINGERS 45 LEFT TO 47 LEFT. REPAIRED WITH A SKIN DOUBLER. 2L73 4F RTA22WE 20050506000642005050600064WP 2005 5 6 UPS05844268 120050324A52305754075502 FITTING DOUG DC8 DC873F 302199FWP CARGO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 C2 CRACKED CORNER FITTING IN C-PIT DOOR UPPER AFT CORNER. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-21, 51-1-21A, AND 51-1- 20D. 2L74 4F RT4A25 20050506000672005050600067WP 2005 5 6 UPS05844274 120050328A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 INSPECTION TYPE: C1, FUSELAGE EXTERIOR SKIN CRACKED .25 INCH LONG AT STA 1734 L16L-L17L. REPAIRED BY INTALLING FINGER DOUBLER AND DOUBLER IAW SRM 53-2-01, 53-02-01 FIG 007 SHEET 5, 51-1-8, 51-1-20, 51-1-20D, 51-1-21. 2L74 4F RT4A25 20050506000692005050600069WP 2005 5 6 UPS05844276 120050402A53403779978U1 FITTING DOUG DC8 DC873F 302199FWP L13R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 C1 FITTING CRACKED 2 INCHES LONG AT STA 760 L13R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2L74 4F RT4A25 20050506001002005050600100NM 2005 5 6 DHL2005782571 120050329A5101652427616 FITTING BOEING727 727227 1384078NM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 STRINGER 19 RT ATTACH FITTING CORRODED AT BS 1183. REMOVED & REPLACED FITTING AT STR 19 BS 1183 IAW B727 SRM 51-30-2. 2L73 4F A3WE 20050506001062005050600106NM 2005 5 6 05FDEA01024 120050415A5755 SUPPORT FITTING BOEING727 727200 138407ENM SPOILER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25271FE 22036 LEFT WING, T/E NR 5 SPOILER CENTER HINGE SUPPORT FITTING CRACKED. REMOVED AND INSTALLED THE NR 5 SPOILER PANEL IAW MM 27-61-001-4. REMOVED THE OLD CRACKED SUPPORT FITTING IAW MM 51-30-2. LOCATED, DRILLED AND INSTALLED NEW SUPPORT FITTING IAW MM 51-30-2. COMPLIED WITH MM 27-61-001-4 AND MM 27-61-001-5. ADJUSTMENT AND TEST CHECKED GOOD FOR NR 5 SPOILER PANEL. 2L73 4F RTA3WE 20050506001072005050600107NM 2005 5 6 05FDEA01025 120050415A5330 SKIN PANEL BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25271FE 22036 C/W EA 7-5330-55466 FUSELAGE SKIN - CRACK REPAIR AT BS 1106, NR 3 LWR CARGO DOOR. COMPLIED WITH EA 7-5330-55466 FUSELAGE SKIN - CRACK REPAIR AT BS 1106, NR 3 CARGO DOOR. 2L73 4F RTA3WE 20050506001122005050600112WP 2005 5 6 05FDEA01029 120050416A5314AJC7028502 KEELBEAM DOUG MD10 MD1010F 3022112WP ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25362FE 48261 AUXILIARY POWER UNIT KEEL CAP ASSEMBLY HAS 9 INCH CRACK FROM FUSELAGE STATION 2019 TO STATION 2028 AT STRINGER 45 RIGHT. REPAIRED STRINGER IAW EA 8-5310-83868, FUSELAGE - AFT BODY KEEL CAP SPLICE AT STA 2040 - REPAIR, AND MD 10 SRM 51-31-01 VOL 2 AND 51-31-01 VOL 2. 2L73 4F RTA22WE 20050506001142005050600114NM 2005 5 6 05FDEA01031 120050416A2550 INSULATION BOEING727 727200 138407ENM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25271FE 22036 COMPLY WITH EA 8-7-2580-81688 EQUIPMENT FURNISHINGS INSULATION BLANKETS PARTIAL REPLACEMENT STA 310-1183 MAIN CABIN COMPARTMENT. COMPLIED WITH EA 7-2580-81688. 2L73 4F RTA3WE 20050509000052005050900005NM 2005 5 9 05FDEA01034 120050416A5743 SUPPORT BEAM BOEING727 727200 138407ENM ZONE 700 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25271FE 22036 COMPLY WITH EA 7-5710-55479 WINGS - RT MLG SUPPORT BEAM PANEL ATTACH HOLE OVERSIZED. COMPLIED WITH EA 7-5710-55479. 2L73 4F RTA3WE 20050509000732005050900073EA 2005 5 9 QXEA200500588 120050317A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE INTERIOR, RIGHT OUTBOARD SEAT RAIL AT STATION X522 HAS PITTING CORROSION ON MOST INBOARD SURFACE. REPAIRED IAW CRJ700/900 SRN 51-21-06-001-001-A01. 2L72 4F RTA21EA 20050509000782005050900078EA 2005 5 9 QXEA200500585 120050316A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE INTERIOR, LEFT OUTBOARD SEAT RAIL AT STATION X785 HAS PITTING CORROSION AND TOOL MARKS ON MOST INBOARD SURFACE. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01 AND REO 670-53-00-013. 2L72 4F RTA21EA 20050509000822005050900082EA 2005 5 9 QXEA200500590 120050317A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE INTERIOR, RIGHT OUTBOARD SEAT RAIL AT STATION X584, HAS PITTING CORROSION ON MOST INBOARD SURFACE. REPAIRED IAW CRJ700/90-0 SRM 51-21-06-001-001-A01, PARAGRAPH 3E. 2L72 4F RTA21EA 20050509000832005050900083NM 2005 5 9 UIEA200500044 120050331A3244311792 TIRE BOEING747 74747UF 1384949NM GE CF6 CF680C2* GL NR 11 WHEEL BLOWN A UIEAJA DUMP FUEL UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA15493MC 29254 FLIGHT (90 K FUEL DUMPED). AT ABOUT V1 SPEED, DURING T/O GOT BRAKE LIMITER AND ANTI SKID EICAS FOLLOWED BY GEAR CONFIG AND BODY GEAR STEERING WARNING, AND AFTER LIFT OFF GEAR TILT EICAS. LANDED BACK IN TPE AFTER DUMPING FUEL AND COORDINATING WITH GCC. NR 11 TIRE BURST ON TAKEOFF. ALL 4 TIRES ON RT BODY GEAR REPLACED. FOUND WIRING HARNESS BROKEN AND J-5 BOX DAMAGED ON RT BODY GEAR. REPAIRED AND REPLACED BODY GEAR WIRING IAW CHAPTER 20 AND PERFORMED FULL GEAR SWING AND OPERATION TEST OF BRAKE SYSTEM, ANTI SKID SYSTEM, BODY GEAR. (K) 2L74 4F4 FRT1384945 E23EA 20050509000862005050900086NM 2005 5 9 HNAA0500038 120050411A32305352011 SELECTOR VALVE DHAV DHC8 DHC8102 2809003NM MLG FAILED A HNAAO OTHER J WARNING INDICATION APAPPROACH 1 EA07930HA4318841203 126 WOW CAUTION LIGHT ILLUMINATED UPON LDG EXTENSION CYCLED GEAR AND LIGHT WENT OUT, NO PROBLEMS ON LANDING. INSPECTED AND CLEANED ALL LANDING GEAR WOW SENSORS. PERFORMED PSEU MEMORY TEST, NO FAULTS CODES FOUND. PERFORMED SATISFACTORY EVALUATION FLIGHT. PROBLEM RETURNED LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. MAINTENANCE REPLACED THE PSEU, EVAL FLIGHT WAS UNSATISFACTORY. MAINTENANCE THEN REPLACED THE LANDING GEAR SELECTOR VALVE. OPERATIONAL CHECK WAS GOOD. 2H72 4T RTA13NM 20050509000872005050900087 2005 5 9 XNOA1231 420050414A3100 SELECTOR SWITCH BOEING727 727227 1384078NM FREQ METER BURNED OUT A XN0AD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL2376752 21248 AFTER STARTING NR 3 ENGINE, AC FREQUENCY METER PEGGED OUT AND SMOKE POURED OUT OF FREQ (AC) SELECTOR SWITCH. REMOVED AND REPLACED AC FREQ METER SELECTOR SWITCH AND OPS CHECK OKAY IAW B727 MM 24-20-00. 2L73 4F A3WE 20050509000902005050900090NM 2005 5 9 P5CA0501338 120050329A272032200019 POWERPACK BOEING747 747230B 1384889NM RUDDER FAILED A P5CAK NONE O OTHER ININSP/MAINT 1 EA15509MC 21221 CREW REPORTED ON TAXI OUT UPPER RUDDER SHOWED 5 DEGREES LEFT AND LOWER RUDDER WAS CENTERED. AFTER TAXI IN, RUDDER POSITIONS WERE CONFIRMED BY MAINTENANCE. REPLACED RUDDER POWER PACK (UPPER) PER MM 27-21-16. NO HELP TRANSFERRED TO DMI 34039 MEL 22-3. 2L74 4F A20WE 20050509000932005050900093 2005 5 9 P5CA0501339 420050331A221337572021 YAW DAMPER BOEING747 747230B 1384889NM RUDDER MALFUNCTIONED A P5CAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA15509MC 21221 CREW REPORTED ON TAXI OUT UPPER RUDDER SHOWED 5 DEGREES LEFT AND LOWER RUDDER WAS CENTERED. AFTER TAXI IN, RUDDER POSITIONS WERE CONFIRMED BY MAINTENANCE. REPLACED YAW DAMPER COMPUTER AS PER MM 22-16-02. OPS CHECK PASSED ON GROUND. 2L74 4F A20WE 20050509000942005050900094NM 2005 5 9 UIEA200500049 120050406A5312 PANEL BOEING747 747271C 1384869NM GE CF6 CF650E2 30018NE BULKHEAD CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15537MC 22403 D-CHECK, DURING SCHEDULED INSPECTION, CRACKS WERE FOUND AT THE LOWER CORNERS OF STA 400 BULKHEAD WEB PRESSURE PANEL CUTOUT. ANOTHER CRACK WAS FOUND ON THE LOWER IB SIDE OF THE PRESSURE PANEL ASSY. THE CRACKS ON THE STA 400 WERE TRIMMED OUT. REPAIRED DOUBLERS WERE INSTALLED AT EACH CORNER OF THE CUTOUT, AND A REPAIR STRAP WAS INSTALLED ACROSS THE BOTTOM OF THE CUTOUT. THE CRACKED PRESSURE PANEL ASSY WAS REMOVED AND PREFABRICATED IAW ORIGINAL DWG SPECS. HFEC INSPECTION PERFORMED OF THE TRIM LINE TO COMFIRM NO ADDITIONAL CRACK EXISTS AND OF ALL EXISTING FASTENER HOLES IN THE REPAIR AREA. (K) 2L74 4F4 F A20WE E23EA 20050509000962005050900096EU 2005 5 9 USAA050252 120050205A5347F5332615520002 SEAT TRACK AIRBUS330 A330323 3930335EU FUSLEAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19671UW22760 0323 BFM - FOUND SEAT TRACK CORRODED, FRAME 53.4-53.5 AT -Y1456, MAIN CABIN FLOOR. REPLACED WITH NEW TRACK PER SRM 53-31-15. (M) 2L72 4F RTA46NM 20050509001042005050900104EU 2005 5 9 USAA050279 120050208A5347F5347801400200 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19671UW22760 0323 BFM - FOUND SEAT TRACK CORRODED, 2 INCHES BY 2 INCHES BY .040 INCH AREA, C74 AT Y1117. CORROSION LEVEL 2, TASK C534159-01. REPLACED WITH NEW SEAT TRACK PER SRM 51-44-00, 51-42-11, 52-44-11. (M) 2L72 4F RTA46NM 20050509001082005050900108EU 2005 5 9 USAA050131 120050109A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW21927 0342 BFM - FOUND SEAT TRACK CORRODED .500 INCH BY .375 INCH BY .040 INCH AREA, FRAME 73-74 -Y1147.8 -Z240. REMOVED AND REPLACED WITH NEW SEAT TRACK PER SRM 53-00-15 AND 51-42-11. CORROSION LEVEL 2, TASK NR J7-150-53502-002. (M) 2L72 4F RTA46NM 20050509001092005050900109EU 2005 5 9 USAA050132 120050109A5347F534781720100 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW 0342 BFM - FOUND SEAT TRACK CORRODED 1 INCH BY 1 INCH BY .042 INCH AREA, BETWEEN FRAME 72-75, -Y450 - Z240. REMOVED AND REPLACED WITH NEW SEAT TRACK PER SRM 53-00-15 FIG 101 SH 2 AND 51-42--11. (M) 2L72 4F RTA46NM 20050509001102005050900110EU 2005 5 9 USAA050133 120050109A5347F5711056820400 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW21927 0342 BFM - FOUND SEAT TRACK CORRODED 2 INCH LONG BY 1 INCH WIDE BY .040 INCH DEEP, MAIN CABIN +Y450, FRAME 40-56. REMOVED AND REPLACED SEAT TRACK PER SRM 53-31-15 FIG 101. CORROSION LEVEL 2, TASK NR J7-200-2578C. (M) 2L72 4F RTA46NM 20050509001132005050900113EU 2005 5 9 USAA050128 120050120A5347F5311170420000 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW 0342 BFM - FOUND DUMMY RAIL CORRODED 2.75 INCHES LONG BY 2 INCHES WIDE BY .035 INCHES DEEP, FRAME 13A, -Y953, -Z240. REMOVED AND REPLACED WITH NEW PART PER SRM 53-11-15 FIG 101. (M) 2L72 4F RTA46NM 20050509001152005050900115EU 2005 5 9 USAA050275 120050202A5313F5347823420100 LONGERON AIRBUS330 A330323 3930335EU FS CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19671UW22760 0323 BFM - FOUND LONGERON CORRODED 2 INCHES BY 1.5 INCH BY .042 INCH DEEP, FRAME 75 TO 76, -Y370 MAIN CABIN FLOOR. CORROSION LEVEL 2, TASK C534159-01. REMOVED AND REPLACED BEAM PER SRM 51-72-11. (M) 2L72 4F RTA46NM 20050509001172005050900117EU 2005 5 9 USAA050278 120050208A5347F5311170220000 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19671UW22760 0323 BFM - FOUND RAIL CORRODED 2 INCH IN DIAMETER, .103 INCH DEEP, CABIN FRAME 13A, Y+953. CORROSION LEVEL 2, TASK C531172-01. REMOVED AND REPLACED LONGITUDINAL RAIL PER SRM 53-11-15 FIG 101, SH 1, 51-44-00, 51-42-11. 2L72 4F RTA46NM 20050509001192005050900119EU 2005 5 9 USAA050280 120050203A5320 FLOOR SUPPORT AIRBUS330 A330323 3930335EU FUSLEAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19671UW22760 0323 BFM - FOUND FLOOR SUPPORT BEAM CORRODED, 6.0 INCH LONG BY 2 INCHES WIDE BY .035 INCH DEEP, FRAME 37, Y=450. CORROSION LEVEL 2, TASK C532134-01. SPLICED IN NEW TRACK SECTION PER SRM 53-00-15 FIG 202. (M) 2L72 4F RTA46NM 20050509001212005050900121EU 2005 5 9 USAA050244 120050204A5347F57110568204001 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19671UW22760 0323 BFM - FOUND SEAT TRACK, CORRODED 2 INCHES LONG BY 1.20 INCHES WIDE BY .035 INCHES DEEP AND 4 INCHES LONG BY 1 INCH WIDE BY .037 INCH, FRAME 39.2-47, +Y450 MAIN CABIN FLOOR. REMOVED AND REPLACED SEAT TRACK PER SRM 53-31-15, 51-42-11. (M) 2L72 4F RTA46NM 20050509001222005050900122EU 2005 5 9 USAA050245 120050202A5347F5331140220001 SEAT TRACK AIRBUS330 A330323 3930335EU CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19671UW22760 0323 BFM - FOUND SEAT TRACK CORRODED 5 SQUARE INCHES BY .040 INCH DEEP, FRAME 47-49, Y450 MAIN CABIN FLOOR. REMOVED AND REPLACED SEAT TRACK PER SRM 53-31-15 FIG 101. CORROSION 2 AREAS. (M) 2L72 4F RTA46NM 20050509001232005050900123EU 2005 5 9 USAA050129 120050110A5347F53476211200 SEAT TRACK AIRBUS330 A330323 3930335EU FS CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW21927 0342 BFM - FOUND SEAT TRACK CORRODED 2 INCHES BY 1 INCH BY .35 INCH AND 3.5 INCH BY 1 INCH .036 INCH, Y1959 FRAME 54-58 Z-240. INSTALLED NEW SEAT TRACK PER SRM 53-00-15 FIG 101 SHT 2 AND SRM 51-42-11. CORROSION LEVEL 2, TASK NR J7-200-2580C-030. (M) 2L72 4F RTA46NM 20050509001242005050900124EU 2005 5 9 USAA050130 120050113A5347F53311402202 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW21927 0342 BFM - FOUND SEAT TRACK CORRODED, MAIN CABIN FLOOR -Y953 FRAME 52. REPLACED SECTION OF SEAT TRACK AND ADDED SPLICES PER SRM 53-31-15 FIG 101. CORROSION LEVEL 2, TASK NR J7-200-2578. (M) 2L72 4F RTA46NM 20050509001262005050900126EU 2005 5 9 USAA050120 120050113A5321F5367139200000 FLOORBOARD AIRBUS330 A330323 3930335EU FUSELAGE DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW21927 0342 BFM - FOUND FLOORBOARD WITH HOLE 3.5 INCH BY 3.5 INCH, MAIN CABIN FLOOR PANEL 251JG. FABRICATED NEW FLOORBOARD PER SRM 53-02-00. (M) 2L72 4F RTA46NM 20050509001322005050900132CE 2005 5 9 20030830 120050418A3297 WIRE BEECH 1900 1900D 1154162CE LT MLG UPLOCK CHAFED A GLBAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM03240GL UE240 DURING CLIMB, FLT CREW REPORTED AFX DISABLE AND LEFT AND RIGHT AUTOFEATHER ANNUNCIATORS ILLUMINATED. FLT CREW RETURNED TO AIRPORT WITHOUT INCIDENT. MAINTENANCE REPAIRED CHAFED WIRES AT LT MLG UPLOCK SWITCH. OP CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA24CE 20050509001332005050900133GL 2005 5 9 ALG2005F00019 220050228A7261 CHIP DETECTOR SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL NR 2 ENGINE CONTAMINATED A ALGAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW03518AL 760134 DURING FLIGHT, THE NR 2 ENGINE CHIP LIGHT ILLUMINATED, EMERGENCY CHECK LIST COMPLIED WITH AND RETURNED TO DEPARTURE. MAINTENANCE REMOVED 2 EA CHIP PLUGS FROM THE NR 2 ENGINE, FOUND SMALL CHIP THAT WAS WITHIN LIMITS. REINSTALLED CHIP PLUGS AND COMPLIED WITH THIRTY MINUTE GROUND RUN NO FURTHER DEFECTS NOTED. WORK DONE IAW MM. (K) 1G72 3U3 U H1NE E1GL 20050509001352005050900135NM 2005 5 9 SWAA051103 120050414A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 500A, STR 8L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050509001362005050900136NM 2005 5 9 SWAA051107 120050414A53226546529 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME SHEAR TIE CRACKED AT BS 500B, BETWEEN STR 15R & STR 16R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050509001382005050900138NM 2005 5 9 SWAA051099 120050414A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 727B, BETWEEN STR 13L & STR 14L. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050509001392005050900139NM 2005 5 9 SWAA051109 120050414A53306545777 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29506SW 24183 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 942, STR 23R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050509001402005050900140NM 2005 5 9 SWAA051110 120050414A3350101073 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29627SW 27935 L1 DOOR EMERGENCY EXIT LIGHT LENS FELL OFF. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20050509001432005050900143NM 2005 5 9 SWAA051113 120050414A5313BAC1498156 STRINGER BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON STRINGER AT BS 1010, STR 26R. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20050509001472005050900147NM 2005 5 9 SWAA051117 120050414A52106545776 SKIN BOEING737 7373A4 1384585NM L2 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29678AA 23290 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050509001482005050900148 2005 5 9 SWAA051118 420050414A2565D31354 SLIDE BOEING737 7373A4 1384585NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29678AA 23290 DURING SCHEDULED C1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050509001492005050900149NM 2005 5 9 SWAA051119 120050414A3350311500 LENS BOEING737 7373TO 138447GNM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29697SW 23838 DURING SCHEDULED 1/4D CHECK, FOUND EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 13 ABC. SECURED LENS PER MM. 2L72 4F RTA16WE 20050509001512005050900151NM 2005 5 9 SWAA051121 120050414A53126546568 BULKHEAD BOEING737 7377H4 1384404NM AFT CANNING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29755SA 27871 DURING SCHEDULED HC2 CHECK, FOUND BS 1016 AFT PRESSURE BULKHEAD OIL CANNED AT STR 3L. REPAIRED AFT PRESSURE BULKHEAD PER SRM. 2L72 4F RTA16WE 20050509001542005050900154NM 2005 5 9 SWAA051124 120050414A53306545775 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 807, STR 24L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050509001552005050900155NM 2005 5 9 SWAA051125 120050414A53306545775 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 847, STR 23R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050509001572005050900157NE 2005 5 9 ALG2005F00021 220050322A7261 CHIP DETECTOR SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL1S1 60030NE NR 1 ENGINE CONTAMINATED A ALGAO OTHER J WARNING INDICATION CRCRUISE 1 SW03864AL 760557 DURING FLIGHT THE NR 1 ENGINE ILLUMINATED TEN MINUTES AFTER DEPARTURE. THE NR 1 ENGINE WAS PLACED IN GROUND IDLE IAW EMERGENCY CHECK LIST AND THE FLIGHT CONTINUED. AT ARRIVAL, THE NR 1 ENGINE WAS PLACED IN FLY POSITION IAW CHECK LIST FOR NORMAL LANDING. THERE WERE NO OTHER IRREGULAR CONDITIONS NOTED DURING THE FLIGHT. MAINTENANCE DISCOVERED 1 SMALL DARK PARTICLE ON THE NR 1 ENGINE CHIP DETECTOR. PERFORMED SOA SAMPLE AND CHECKED RUNDOWN TIME OF THE ENGINE. CHIP PLUGS MUST BE PULLED AFTER LAST FLIGHT AND INSPECTED FOR A PERIOD OF 25 HOURS. (K) 1G72 3U3 UNCH1NE E19EU 20050509001582005050900158 2005 5 9 SWAA051133 420050415A25656557463 LATCH BOEING737 7373H4 1384600NM R2 DOOR SLIDE MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR LATCH SPRING MISSING. REMOVED AND REPLACED LATCH ASSY PER MM. 2L72 4F RTA16WE 20050509001612005050900161NM 2005 5 9 SWAA051136 120050417A53206545410 FLOOR SUPPORT BOEING737 7373H4 1384600NM FUSLEAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29333SW 23697 DURING SCHEDULED 1/4D CHECK, FOUND 2 EA CRACKS AT NR 2 LONGITUDINAL FLOOR SUPPORT TEE, BS 664 & BS 668.5. REPAIRED FLOOR SUPPORT PER SWA EA. 2L72 4F RTA16WE 20050509001632005050900163NM 2005 5 9 SWAA051138 120050415A335057771 CAP BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29451WN 32495 FWD END OF EEPLS END CAP MISSING. INSTALLED END CAP PER MM. 2L72 4F RTA16WE 20050509001652005050900165NM 2005 5 9 SWAA051140 120050415A52306558172 FITTING BOEING737 7375H4 138449DNM AFT CARGO DOOR OUT OF ADJUST A SWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW29509SW 24186 AIR TURNBACK. AFTER TAKEOFF, AFT CARGO DOOR LIGHT ILLUMINATED. ACFT WOULD NOT PRESSURIZE. ADJUSTED AFT CARGO DOOR AFT ROLLER LOCK PER MM. 2L72 4F RTA16WE 20050509001692005050900169 2005 5 9 SWAA051144 420050416A2565 BOTTLE BOEING737 7373T5 1384608NM R1 DOOR SLIDE DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 0602A 23062 DURING SCHEDULED SERVICE CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATING LOW. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20050509001712005050900171NM 2005 5 9 SWAA051127 120050416A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 939 TO BS 942, STR 21L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050509001722005050900172NM 2005 5 9 SWAA051128 120050416A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 489, STR 16R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050509001742005050900174NM 2005 5 9 SWAA051130 120050417A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 787, STR 5R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050509001772005050900177SW 2005 5 9 ALG2005F00023 120050407A2913206076030111 PUMP BELL 206 206L1 1182107SW ALLSN 250C 250C30P 03013GL HYD SYSTEM INOPERATIVE A ALGAO OTHER F FLT CONT AFFECTED CRCRUISE 1 SW035759M 45555 DEPARTED, 10 MINUTES INTO FLIGHT AT 1000 FT AGL AND CRUISE POWER, FLIGHT CONTROLS STARTED TO TIGHTEN UP. SLOWED AC AND SUSPECTED HYDRAULIC FAILURE. PULLED HYDRAULIC C/B, POWER DID NOT RESTORE PUSHED THE C/B BACK IN. TURNED OFF THE HYDRAULIC CONTROL SWITCH. AC WAS FLYING GOOD, ELECTED TO FLY THE AC TO DESTINATION. MAINT REMOVE HYDRAULIC PUMP, FOUND WORN SPLINES AND SHAFT WAS LOCKED INTO THE TACH GENERATOR SO REPLACED TACH GENERATOR AND HYDRAULIC PUMP. REMOVED AND REPLACED HYDRAULIC FILTERS, FLUSHED LINES AND RESERVOIR AND RESERVICED HYDRAULIC SYSTEM. COMPLIED WITH GROUND RUN, LEAK CHECK OF HYDRAULICS AND OPS CHECK, FLIGHT ALL SYSTEMS NORMAL. (K) 1G71 3U3 U H2SW E1GL 20050510000042005051000004EA 2005 5 10 DAT2005F00002 220050322A7230PT6A45R GAS GENERATOR STBROSSD3 SD330 8100602EU PWA PT6 PT6A45R 52043EA RT ENGINE LEAKING E DATAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL1358DD 187983245 SH3008 FLT CREW EXPERIENCED PROBLEMS WITH RT ENG. PRIOR TO CRUISING ALTITUDE, IT WAS NOTICED OIL LIGHT WAS FLICKERING ON AND OFF WHILE OIL PRESS GAUGE WAS OSCILLATING BETWEEN 90 PSI, 135 PSI. THOUGHT IT MIGHT HAVE BEEN ERROR WITH GAUGE. GAUGE CONTINUED WITH ITS OSCILLATIONS, BUT RANGE LOWERED TO 80 PSI, 120 PSI. TREND CONTINUED DOWN TO 60 PSI, 90 PSI AT WHICH POINT, REDUCED TORQUE TO 2000 LBS. DECIDED TO SHUT RT ENGINE DOWN WHEN IT DROPPED BELOW 60 PSI. AFTER VITAL ACTIONS WERE COMPLETE, CONTINUED WITH ACTIONS, LANDED PLANE SAFELY. FINAL TRIP OF DAY. MECH DISPATCHED WITH SERVICABLE ENG. OIL WAS ADDED, DISCREPANCY WAS NOT CORRECTED. END REMOVED AND REPLACED. OPS CK GOOD, AC WAS RETURNED TO SERVICE. (K) 2H72 4T4 T A41EU E4EA 20050510000052005051000005NM 2005 5 10 AMTA200500316 120050327A261335008307 OVERHEAT SENSOR BOEING737 73783N 13844HINM GE CFM56 CFM56* 13802NE MLG WW MALFUNCTIONED A AMTAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL11314TZ 30640 AFTER GEAR RETRACTION, WHEEL WELL FIRE LIGHT ILLUMINATED WITH FIRE BELL. COMPLETED WHEEL WELL FIRE PROCEDURES, LIGHT WENT OUT ON SHORT FINAL, BRAKE TEMPS WERE (0) DEG AND HYD NORMAL. REMOVED AND REPLACED OVERHEAT DETECTION CONTROL UNIT IAW MM. OPS CHECK GOOD. (K) 2L72 4F4 FRTA16WE E2GL 20050510000082005051000008NM 2005 5 10 AWXA200500471 120050401A52406545871523 DOOR FRAME BOEING737 73733A 1384673NM R1 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 DURING C-19 CHECK A .3125 INCH CRACK WAS FOUND ON R-1 DOOR AFT FRAME AT 3RD DOOR STOP CUTOUT FROM BOTTOM BS 329, STR 12 RT. MAINTENANCE TRIMMED OUT DAMAGE R-1 DOOR AFT FRAME AT 3RD DOOR STOP CUTOUT FROM BOTTOM BS 329, STR 12 RT; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW ER 03-5200-05103-ES3. 2L72 4F RTA16WE 20050510000102005051000010WP 2005 5 10 WX0500039 120050414A33506011779 POWER SUPPLY DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A WX0AK NONE O OTHER ININSP/MAINT 1 WP19865GA 49998 LAS - MAINTENANCE REPORTED EXTERIOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK. SYSTEM OPERATIONALLY CHECKED GOOD IAW MM 33-53-00. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050510000112005051000011NM 2005 5 10 SB05048 120050416A3397 WIRE BOEING737 7373B7 1384580NM EMERGENCY LIGHT BROKEN A USAAK NONE O OTHER ININSP/MAINT 1 EA19390US 23312 CLT - PILOT REPORTED THE EMERGENCY EXIT LIGHT AT THE R1 DOOR WAS ILLUMINATED. MAINTENANCE FOUND A BROKEN WIRE BETWEEN BATTERY PACKS. RESPLICED WIRE. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050510000122005051000012EA 2005 5 10 QXEA200500612 120050317A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE INTERIOR, LEFTHAND INBOARD SEAT RAIL AT STATION X665 HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW CRJ700/900 SRM 51-21-06-001-001-A01, PARAGRAPH 3E, REO 670-53-00-013 AND CRJ700 SRM 51-21-16, CODE A044. 2L72 4F RTA21EA 20050510000132005051000013EA 2005 5 10 QXEA200500603 120050317A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE INTERIOR, RIGHTHAND INBOARD SEAT RAIL AT STATION X479 HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW CRJ700/900 SRM 51-21-06-001-001-A01, PARAGRAPH 3E, REO 670-53-00-013 AND CRJ700 SRM 51-21-16, CODE A044. 2L72 4F RTA21EA 20050510000152005051000015EA 2005 5 10 QXEA200500594 120050317A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE INTERIOR, RT OUTBOARD SEAT RAIL AT STATION X712 HAS PITTING CORROSION ON INSIDE SURFACE. REPAIRED IAW CRJ700/900 SRM 51-21-06-001-001-A01, PARAGRAGH 3E AND CRJ700 SRM 51-21-16, CODE A044. 2L72 4F RTA21EA 20050510000172005051000017EA 2005 5 10 QXEA200500601 120050319A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE INTERIOR, RIGHTHAND INBOARD SEAT RAIL AT STATION X431 HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW CRJ700/900 SRM 51-21-06-001-001-A01, PARAGRAPH 3E, REO 670-53-00-013 AND CRJ700 SRM 51-21-16, CODE A044. 2L72 4F RTA21EA 20050510000182005051000018NM 2005 5 10 CALA0500107 120050418A574265C2630812 FITTING BOEING737 7373T0 1384582NM RT PYLON CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712319 23370 RIGHT PYLON FRAME CRACKED INBOARD AT AFT ACCESS PANEL. INSTALLED NEW FITTING PER SRM 51-40-02. 2L72 4F RTA16WE 20050510000202005051000020NM 2005 5 10 CALA0500109 120050418A5330147W3351 SKIN BOEING777 777224 1385225NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2778004 27580 ONE INCH SKIN CRACK BELOW 29L, STATION 2000. INSTALLED DOUBLER PER SRM 53-00-01. 2L72 4F RTT00001SE 20050510000212005051000021NM 2005 5 10 CALA0500111 120050417A24000802032501 TRU BOEING737 7373T0 1384582NM NR 2 SMOKE A CALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2714358 23943 DURING CRUISE, ELECTRICAL SMOKE IN COCKPIT AND CABIN. REPLACED NR 2 TRANSFORMER RECTIFIER PER AMM 24. 2L72 4F RTA16WE 20050510000232005051000023NE 2005 5 10 CALA050110 220050418A7200CF680 ENGINE BOEING767 767224 1385170NM GE CF6 CF680 30025NE RIGHT FAILED A CALAC ABORTED TAKEOFF YJ ENGINE STOPPAGE WARNING INDICATION TOTAKEOFF 1 SW2767158 30437 ON TAKEOFF, AT APPROXIMATELY 90 KNOTS, RT ENGINE FAILED. REPLACED ENGINE. 2L72 4F4 FRTA1NM E13NE 20050510000242005051000024EA 2005 5 10 VTZA200500054 120050416A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA ENGINE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27640BR 7340 ENGINE SUPPORT BEAM UPPER ANGLE IS CRACKED AT .250 INCH IN LENGTH AT FS 640.00 AND LBL 8.5. 2L72 4F RTA21EA 20050510000282005051000028EA 2005 5 10 VTZA200500059 120050416A5320601R311719 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27658BR 7500 INTERCOSTAL CRACKED AT .250 INCH IN LENGTH ON RT OUTBOARD SIDE AT FS 484 BETWEEN BL 27.00. 2L72 4F RTA21EA 20050510000292005051000029EA 2005 5 10 VTZA200500062 120050416A5320601R35031239 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27658BR 7500 RIGHT FS 621 FLOOR SUPPORT IS CRACKED AT 1 INCH IN ANGLE. 2L72 4F RTA21EA 20050510000362005051000036EA 2005 5 10 COMA0560266 120050418A3620355924400 ELEMENT CNDAIRCL600 CL6002B19 1900309EA LT ENGIE FAULTY A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01982CA 7168 FLIGHT 5530 DURING CRUISE FLIGHT (ABE-CVG) RECEIVED A LEFT 14 STAGE DUCT MESSAGE, CREW DECLARED AN EMERGENCY, DIVERTED TO PIT AND LANDED WITHOUT INCIDENT. REPLACED THE FORWARD LEFT PYLON 14TH STAGE SENSING ELEMENT. 2L72 4F RTA21EA 20050510000372005051000037SO 2005 5 10 GNB2005F00001 220050403A8520536379 BOLT CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO CRANKSHAFT SHEARED A GNBAK NONE O OTHER ININSP/MAINT 1 SW01402SA 402C0623 RT ENGINE WOULD NOT TURN OVER. REMOVED RT STARTER ADAPTER. FOUND LARGE CRANKSHAFT GEAR NOT ATTACHED. FOUND ALL 6 ATTACH BOLTS SHEARED BUT CONNECTED TOGETHER WITH SAFETY WIRE. (SW01200503998) (K) 1L72 3O3 O A7CE E8CE 20050510000382005051000038CE 2005 5 10 DXTA200500682 120050415A73309850586001 PRESSURE SWITCH RAYTHNDH125 HAWKER800XP 7150012CE GARRTTTFE731TFE7315BR WP FUEL SYSTEM FAILED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07836QS 258436 P107573 NR 1 (LEFT) FUEL LIGHT CAME ON DURING T/O ACCELERATION AT ABOUT 92-95 PERCENT N1, ABORT SPEED WAS BETWEEN 70-80 KTS. TROUBLESHOT SYSTEM. VERIFIED FLIGHT SQK. SWAPPED FUEL BYPASS SWITCHES AND CHANGED BOTH FUEL FILTERS ALL WORK DONE IAW TFE-731 LMM 73-21-02. OPS CHECKED/ LEAK CHECKED GOOD, MX IAW THE H800XP MM CHAPTER 73-34-11. 2L72 4F4 FRTA3EU E6WE 20050510000392005051000039CE 2005 5 10 DXTA200500681 120050415A3240 BRAKE ASSY CESSNA500 560CESSNA 2076750CE MLG MALFUNCTIONED E DXTAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07377QS 5600377 ON TAXI OUT CO-PILOT HAD NO BRAKE PRESSURE, TRIED PILOT SIDE AND STILL NO BRAKE PRESSURE. USED EMERGENCY BRAKE TO STOP THE AIRPLANE, FLUID LEAKING FROM NOSE GEAR BAY ON TO THE GROUND. GROUND RAN A/C AND OPERATED HYDRAULIC SYSTEMS, NO LEAKS NOTED. RESIDUAL FLUID DRIPPING FROM SKID DUE TO T/R CONTROL VALVE REPLACEMENT, HYD SERVICING, AND CLEAN UP AFTER COMPLETION. REMOVED AND REPLACED ANTI SKID CASE FILTER BOWL AND BLEED ANTI-SKID SYSTEM. OPS CHECKED GOOD ALL WORK DONE IAW THE CESSNA CITATION MODEL 560 MAINTENANCE MANUAL 32-42-00. 2L72 4F RTA22CE 20050510000462005051000046 2005 5 10 2005UALA00285 420050104A256564573103 SLIDE BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN LEAKING A UALAK NONE O OTHER ININSP/MAINT 1 WP29560UA 26660 POROSITY THROUGHOUT DOGLEGS AROUND ASPIRATOR FLANGES AND SEAMS. POROSITY LEAKAGE FOUND AT DOGLEGS, ASPIRATOR FLANGES AND SEAMS. REPLACED INFLATABLES. 2L72 4F4 FRTA2NM E17NE 20050510000472005051000047NM 2005 5 10 2005UALA00317 120050411A5330 SKIN BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE FUSELAGE PUNCTURED A UALAK NONE O OTHER ININSP/MAINT 1 WP29665UA 29237 FUSELAGE LEFT SIDE STA 500 PUNCTURED SKIN AT STR 24L. UNDETERMINED CAUSE OF DAMAGE. SKIN REPAIRED PER STANDARD BOEING SRM. 2L72 4F4 FRTA1NM E24NE 20050510000482005051000048NE 2005 5 10 2005UALA00322 220050408A7200 ENGINE BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 2 SHUTDOWN A UALAEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 WP29580UA 26698 RETURNED TO FIELD DUE TO NR 2 ENGINE SHUTDOWN. THE ENGINE EXPERIENCED A SURGE IN THE HPC AND WAS SHUTDOWN. THE ENGINE SURGE WAS CAUSED BY A DISRUPTION IN AIRFLOW THROUGH THE HPC THAT WAS CAUSED BY DAMAGE TO THE COMPRESSOR AIRFOILS. THE AIRFOIL DAMAGE WAS CAUSED BY FOD. THE MATERIAL THAT CAUSED THE FOD WAS NOT RECOVERED NOR IDENTIFIED AT THIS TIME. THE ENGINE WAS REMOVED FROM SERVICE AND OVERHAULED. 2L72 4F4 FRTA2NM E17NE 20050510000522005051000052NM 2005 5 10 2005UALA00328 120050410A5320 CHANNEL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FLOOR SUPPORT CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29308UA 23669 AFT CABIN FLOOR SUPPORT HAT CHANNEL CORRODED AT STA 993 RBL 14 TO 44 WL 208. REPLACED HAT CHANNEL SECTION. 2L72 4F4 FRTA16WE E2GL 20050510000562005051000056NM 2005 5 10 2005UALA00342 120050411A5740 FITTING BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE LT WING SPAR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29665UA 29237 LEFT WING REAR SPAR, OUTBOARD FLAP OUTBOARD DEFLECTION FITTING CRACKED. THE SUBJECT FITTING CRACKED TO CYCLICAL FATIGUE LOAD DURING EXTENSION AND RETRACTION OF THE OUTBOARD FLAP. CORRECTIVE ACTION IS REPLACEMENT OF THE FITTING WITH NEW AND IMPROVED FITTING PER COA 616463. 2L72 4F4 FRTA1NM E24NE 20050510000572005051000057NM 2005 5 10 2005UALA00343 120050414A2752 TRANSMISSION BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE TE FLAPS LEAKING A UALAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP29308UA 23669 NR 8 TRANSMISSION LEAKING, INPUT FROM THE TRANSMISSION HOUSING WHEN TRANSMISSION REMOVED TO BE REPLACED, POSSIBLE CAUSE RETAINER WASHER AND OR NUT FAILED. SUBJECT NR 8 TE FLAP TRANSMISSION (PN 65C27508-3/ PCN 152 9006) EXHIBITED EXCESSIVE LEAKING DO TO IMPROPERLY TORQUED ASSEMBLY NUTS AND BOLTS THAT ALLOWED FLUID LOSS AROUND INPUT SHAFT HOUSING AREA. SUBJECT TRANSMISSION WAS REMOVED AND REPLACED WITH NEW SERVICEABLE UNIT AND OPS CHECKED PER MM 27-51-71. ALL OPS CHECKED GOOD. REPLACED UNIT WAS NEWLY OVERHAULED WITH ZERO HOURS AFTER OVERHAUL. FAILURE OF THIS UNIT WAS NOT OPERATIONAL. FAILURE WAS DUE TO IMPROPER ASSEMBLY DURING OVERHAUL. 2L72 4F4 FRTA16WE E2GL 20050510000622005051000062WP 2005 5 10 ASMF200504014 120050416A32427936907531 LINE DOUG DC9 DC982 3022082WP LEFT BRAKE DAMAGED W ASMFO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW23505MD 49149 CAPTAIN REPORTED THAT DURING FLIGHT LOT HYDRAULIC LIQUID IN THE LEFT SYSTEM WITH HYDRAULIC PRESSURE CORRECT. DURING REVISION WAS DETECTED THE HYDRAULIC TANK LEFT SYSTEM EMPTY, IT WAS RECHARGED. THE LEFT SYSTEM WAS PRESSURIZED AND BRAKE RETURN LINE HAD A LEAK. THE BRAKE RETURN LINE LEFT SYSTEM WAS REPLACED IAW MM 32-42-00, TESTED CORRECT. DURING OVERNIGHT SERVICE, THE RETURN LINE BRAKE LEFT SYSTEM WAS VERIFIED FOR LEAKS IAW MM 32-42-00, TESTED CORRECT. 2L72 4F A6WE 20050510000652005051000065EA 2005 5 10 A6WA200540140 120050406A3234601R5096711 HANDLE CNDAIRCL600 CL6002B19 1900309EA MLG FAILED A A6WAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 GL31424AW 7656 LANDING GEAR DIDN'T RETRACT WHEN SELECTED UP. ANTI-SKID INBOARD AND PBSOV MESSAGE ILLUMINATED WITH GEAR SELECTED UP. REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE IAW 32-30-00 JACKED AIRCRAFT, COMPLIED WITH GEAR SWING. NO DISCREPANCIES NOTED. OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050510000672005051000067EU 2005 5 10 USAA050145 120050112A5347F53275665200 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW 0342 BFM - FOUND SEAT TRACK CORRODED 1.5 INCH LONG BY .312 INCH WIDE BY .040 INCH DEEP, MAIN CABIN, FRAME 32-33.5, Y-1959. REMOVED AND REPLACED SEAT TRACK ASSEMBLY PER SRM 53-00-15, FIG 101, 51-42-11. (M) 2L72 4F RTA46NM 20050510000692005051000069EU 2005 5 10 USAA050147 120050113A5347F53275845200 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW21927 0342 BFM - FOUND SEAT TRACK CORRODED 1.2 INCHES LONG BY .400 INCHES WIDE BY .045 INCH DEEP, FRAME 36-37 -Y450 -Z240. CUT OUT DAMAGED AREA AND REPLACED WITH NEW SEAT TRACK SECTION PER SRM 53-00-15 FIG 202. CORROSION LEVEL 2, TASK NR J7-900-09000-044. (M) 2L72 4F RTA46NM 20050510000712005051000071EU 2005 5 10 USAA050137 120050108A5347F5347820720100 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW21927 0342 BFM - FOUND SEAT TRACK ASSEMBLY CORRODED 1.100 INCH BY .375 INCH BY .025 INCH AND .600 INCH BY .375 INCH BY .040 INCH DEEP, Y-1447 BETWEEN FRAME 73/74 CABIN FLOOR. CORROSION LEVEL 2, TASK J7-150-53502. REMOVED AND REPLACED SEAT TRACK ASSEMBLY PER SRM 51-42-11, 51-44-11, 53-00-15. (M) 2L72 4F RTA46NM 20050510000732005051000073EU 2005 5 10 USAA050149 120050114A5347F5711056820500 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW 0342 BFM - FOUND TRACK CORRODED 2 INCH BY .7 INCH BY .033 INCH DEEP, FRAME 45, -Y450, MAIN CABIN FLOOR. REMOVED AND REPLACED SEAT TRACK PER SRM 53-31-15 FIG 101 SHT 8. CORROSION LEVEL 2, TASK NR J7-200-2578C. (M) 2L72 4F RTA46NM 20050510000742005051000074EA 2005 5 10 A6WA200540136 120050404A5320601R53611172 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31416AW 7603 FLOOR SUPPORT ANGLE AT FS 621 RT IS CRACKED AT RBL 41 APPROX 70 INCHES. REPAIRED BY REMOVING DAMAGE, FABRICATING STRAP, INSTALLING STRAP AND ANGLES P/N 601R-53-61-117-2 AND 601R-53-61-117-4 IAW BOMBARDIER, INC REO 601R-53-61-117 REV C. (M) 2L72 4F RTA21EA 20050510000762005051000076EU 2005 5 10 USAA050135 120050116A5321F5367233700300 FLOORBOARD AIRBUS330 A330323 3930335EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW 0342 FOUND FLOORBOARD CRACKED 2.5 INCHES LONG, MAIN CABIN FLOOR PANEL 272K. REMOVED DAMAGE, FABRICATED REPAIR PATCH PER SRM 53-0002-00. (M) 2L72 4F RTA46NM 20050510000782005051000078EU 2005 5 10 USAA050142 120050111A5315F5347904600500 FLOORBEAM AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW21927 0342 BFM - FOUND BEAM ASSEMBLY CORRODED 1 INCH BY .5 INCH BY .012 INCH, FRAME 75.9, -Y1910 MAIN CABIN FLOOR. REMOVED AND REPLACED BEAM PER SRM 51-72-00. (M) 2L72 4F RTA46NM 20050510000802005051000080EU 2005 5 10 USAA050136 120050107A5347F5347721420300 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW21927 0342 BFM - FOUND SEAT TRACK CORRODED, 1.5 INCHES BY 1 INCH BY .21 INCH, 1.5 INCH BY 1 INCH BY .035 INCH, 2 INCH BY 1 INCH BY .040 INCH, -450 FRAME 67-72 MAIN CABIN FLOOR. INSTALLED NEW SEAT TRACK PER SRM 53-00-15 FIG 101 SH 2 AND SRM 51-42-11. CORROSION 3 AREAS, LEVEL 2, TASK NR J7-200-2580C. (M) 2L72 4F RTA46NM 20050510000812005051000081EU 2005 5 10 USAA050144 120050111A5347F53326711200 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW21927 0342 BFM - FOUND SEAT TRACK CORRODED, FS 53.4-53-5 -Y1959 -Z240. REPLACED SECTION OF SEAT TRACK AND ADDED SPLICES PER SRM 53-31-15 FIG 101 AND 201 SHT 1. CORROSION LEVEL 2, TASK NR J7-260-53500-001. REPLACED SECTION OF SEAT TRACK AND ADDED SPLICES PER SRM 53-31-15 FIG 101 AND 201 SHT 1. (M) 2L72 4F RTA46NM 20050510000832005051000083EA 2005 5 10 A6WA200540135 120050404A5320601R53611171 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31416AW 7603 FLOOR SUPPORT ANGLE AT FS 621 LHS IS CRACKED AT LBL 41.5 APPROX 1 INCH. REPAIRED BY REMOVING DAMAGE, FABRICATING STRAP, INSTALLING STRAP AND ANGLES P/N 601R-53-61-117-1 AND 601R-53-61-117-3 IAW BOMBARDIER, INC REO 601R-53-61-117 REV C. (M) 2L72 4F RTA21EA 20050510000842005051000084NE 2005 5 10 A6WA200540139 220050405A7261 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE MALFUNCTIONED A A6WAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 GL31431AW 7256 LOW OIL ENGINE PRESSURE WARNING. INDICATED LOW ON GAGE LOW PRESSURE. COMPLIED WITH QRH. ENGINE SHUTDOWN INFLIGHT. (M) 2L72 4F4 FRTA21EA E15NE 20050510000912005051000091EA 2005 5 10 QXEA200500636 120050322A5320 FLOOR SUPPORT CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE INTERIOR COCKPIT FLOORBOARD SUPPORT ANGLE AT FUSELAGE STATION 280 IS CORRODED AND CRACKED. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20050510000932005051000093EA 2005 5 10 QXEA200500622 120050320A1430 RIVET CNDAIRCL600 CL6002C10 1390015EA ZONE 200 SMOKE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE EXTERIOR HAS SEVERAL SMOKING RIVETS AT FUSELAGE STATION 677, STRINGER 3L TO STRINGER 6L. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01 AND SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050510000952005051000095EA 2005 5 10 QXEA200500633 120050324A5753 HINGE CNDAIRCL600 CL6002C10 1390015EA ZONE 600 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - RIGHTHAND INBOARD FLAP LOWER SURFACE INBOARD HINGE AREA HAS CHAFED MARKS FROM FAIRING. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01 AND SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050510000972005051000097EA 2005 5 10 QXEA200500615 120050323A1430 RIVET CNDAIRCL600 CL6002C10 1390015EA ZONE 200 SMOKE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE EXTERIOR HAS FOUR SMOKING RIVETS AT STATION 745 AND STRINGER 16R. REPLACED RIVETS IAW CRJ7800 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20050510000982005051000098EA 2005 5 10 QXEA200500617 120050328A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 200 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE EXTERIOR HAS AREAS OF NICKS ABOVE AFT CARGO DOOR BETWEEN FUSELAGE STATION 1015 AND 1031 ON FUSELAGE SKIN. REPAIRED IAW CRJ700 SRM 51-25-01, PAGE 7, PARAGRAPH B AND SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050510001022005051000102NM 2005 5 10 HNAA0500040 120050419A323382910016009 ACTUATOR DHAV DHC8 DHC8102 2809003NM MLG MISRIGGED A HNAAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 EA07848EX2980129801 331 NOSE GEAR DOOR WILL NOT CLOSE AFTER TAKEOFF, CYCLED GEAR OPS NORMAL. ADJUSTED NOSE GEAR DOOR ACTUATOR ROD END AND ADJUSTED SENSOR GAP. OPS CHECK GOOD. 2H72 4T RTA13NM 20050510001042005051000104NM 2005 5 10 HNAA0500035 120050407A3350316 LIGHT DHAV DHC8 DHC8102 2809003NM CABIN INOPERATIVE A HNAAO OTHER O OTHER NRNOT REPORTED 1 EA07826EX2646826468 389 FIRST AND THIRD RED FLOOR EMERGENCY LIGHTS ARE INOP. RELAMPED EMERGENCY LIGHTS, OPS CHECK GOOD. 2H72 4T RTA13NM 20050510001062005051000106NM 2005 5 10 DHL2005786001 120050420A2930B7124 INDICATOR BOEING727 727214 138407RNM HYD SYSTEM MALFUNCTIONED A DHLAB EMER. DESCENT N FALSE WARNING DEDESCENT 1 SO01786AT 21692 NOTED LOSS OF B-HYD SYSTEM QUANTITY AS WELL STANDBY QUANTITY PERFORMED ABNORMAL PROCEDURE AFTER LANDING STANDBY QUANTITY WENT TO FULL. FOUND B SYS QTY INDICATOR DEFECTIVE; FOUND STANDBY QTY FULL REMOVED AND REPLACED B-SYS QTY INDICATOR IAW M/M 29-33-0 SERVICED QTY HYD IAW M/M 29-00. 2L73 4F A3WE 20050510001082005051000108EU 2005 5 10 DHL2005367502 120050410A5347TMS6022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01367DH 265 DURING "C" CHECK, MAIN DECK COURIER AREA SEAT TRACK AT LBL 3 AND FRAME 15A HAS HEAVY CORROSION ON HORIZONTAL FLANGE. REMOVED AND REPLACED MAIN CABIN SEAT TRACK AT FR 15A LBL 3 IAW A-300 SRM 53-10-10 AND 51-30-30 MAT. USED TMS 60-22457 PO NR 2113624 3 FEET. TREATED AND PRIMED IAW A-300 SRM 51-40-12. 2L72 4F RTA35EU 20050510001112005051000111EU 2005 5 10 DHL2005367503 120050403A5347TMS6022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01367DH 265 DURING "C" CHECK IN MIAMI, FLORIDA DISCREPANCY AS FOLLOWS, N/R 018787, CABIN SEAT TRACK AT FS 18 THRU 21A AT BLR 78 HAS CORROSION (MKD). REMOVED AND REPLACED CABIN SEAT TRACK FROM FR 18 TO FR 25 RBL 78 IAW A-300 SRM 53-10-10 AND 51-30-30 MAT. USED TMS 60-22457 PO NR 2113624. TREATED AND PAINTED AS PER A-300 SRM 51-40-12. 2L72 4F RTA35EU 20050510001152005051000115CE 2005 5 10 ACS2005F00000 120050302A5320 STIFFENER BEECH 90 65A901 1152901CE PWA PT6 PT6A20 52043EA NLG WW CRACKED E ACSAK NONE O OTHER ININSP/MAINT 1 AL017165Y LM120 DURING INSPECTION, IT HAS BEEN FOUND THAT 4 OF 4 AIRCRAFT HAVE HAD A CRACK ORIGINATING FROM THE TOP RIVET OF THE AFT STIFFENER, RT SIDE OF NOSE WHEEL WELL. THE CRACK HAS BEEN IN THE SKIN SPREADING IN BOTH FORWARD AND AFT. (K) 1L72 3T3 T 3A20 E4EA 20050510001162005051000116 2005 5 10 PIDA2005006 420050416A22104051600913 COMPUTER BOEING737 737400 138449ANM AUTO FLIGHT FAILED A PIDAO OTHER O OTHER CRCRUISE 1 SO05737DX 24804 AUTO FLIGHT CONTROL SYSTEM A FCC DC CIRCUIT BREAKER TRIPPED IN FLIGHT. WILL NOT RESET. RESULTING FLIGHT DIRECTOR FLAG IN VIEW. REPLACED FLIGHT CONTROL COMPUTER. OPS CHECKS GOOD PER MM 22-11-33. 2L72 4F RTA16WE 20050510001172005051000117NM 2005 5 10 PIDA2005334 120050417A33501010428 LIGHT BOEING737 7373G7 1384595NM CABIN INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05390WL 23219 LEFT EMERGENCY OVERHEAD LIGHT INOP (3RD ONE BACK). REPLACED OVERHEAD EMERGENCY LIGHT ASSY PER MM 33-51-12. OPS CHECKS GOOD. 2L72 4F RTA16WE 20050510001182005051000118NM 2005 5 10 PIDA2005004 120050417A33501010428 LIGHT BOEING737 7373G7 1384595NM CABIN INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05390WL 23219 LEFT EMERGENCY OVERHEAD LIGHT INOP (3RD ONE BACK). REPLACED OVERHEAD EMERGENCY LIGHT ASSY PER MM 33-51-12. OPS CHECKS GOOD. 2L72 4F RTA16WE 20050510001202005051000120SO 2005 5 10 MASA200500279 120050404A3350 SIGN EMB 145 EMB145LR 3260212SO EMERGENCY EXIT MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07853MJ 145464 A RIGHT SIDEWALL EMERGENCY EXIT SIGN INOP. MAINTENANCE CYCLED THE EMERGENCY EXIT SWITCH AND COULD NOT DUPLICATE FAULT. 2L72 4T RTT00011AT 20050510001222005051000122SO 2005 5 10 MASA200500286 120050405A3397 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT UNSECURE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07836MJ 145359 CREW REPORTED EMERGENCY FLOOR PATH LIGHTING BETWEEN ROWS 3 TO 7 INOP. MAINTENANCE RESECURED A LIGHT STRIP CONNECTOR AND OPS CHECKED THE LIGHTS. 2L72 4T RTT00011AT 20050510001232005051000123EA 2005 5 10 MASA200500287 120050406A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0717175 7175 RIGHT WING AFT EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED, OPS CHECKED GOOD. 2L72 4F RTA21EA 20050505000682005050500068SO 2005 5 5 SIMA200509103 120050328A2612360113448022C2 FIRE LOOP EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 2 ENGINE SHORTED A SIMAFBA ACTIVATE FIRE EXT. EMER. DESCENT UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW21907AE 14500895 DURING LEVEL CRUISE AT FLIGHT LEVEL 360, RECEIVED AN ENGINE NR 2 FIRE INDICATION. BOTH FIRE BOTTLES WERE DISCHARGED AND ENGINE WAS SHUTDOWN. DECLARED EMERGENCY AND DIVERTED TO BNA. LANDED OVERWEIGHT BUT THE SINK RATE WAS REPORTED BY THE CREW TO BE 100/MIN OR LESS. THERE WAS NO EVIDENCE OF AN ACTURAL FIRE REVEALED ON POST FLT INSP. REPLACED PYLON FIRE LOOP AND THE NR 1 AND NR 2 FIRE BOTTLES. (SW2120054797) (K) 2L72 4T4 FRTT00011ATTE6CH 20050505000732005050500073SO 2005 5 5 SIMA200509105 120050317A532014522459001 RAMP EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FLOOR SUPPORT CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21641AE 145191 DURING MBV INSPECTION FOUND FORWARD CABIN FLOOR SUPPORT RAMP AT FRAME 19 AND 20 CORRODED ON UPPER AND AFT EDGE. REMOVED AND INSTALLED RAMP IAW SRM. AC RETURNED TO SERVICE. (SW21200504818) (K) 2L72 4T4 FRTT00011ATTE6CH 20050505000772005050500077SO 2005 5 5 SIMA200509108 120050317A532114522461003 DOUBLER EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL CABIN FLOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21641AE 145191 DURING MBV INSPECTION FOUND FORWARD CABIN FLOOR DOUBLER AT FRAME 22 CORRODED AROUND NUTPLATE. INSTALLED NEW DOUBLER AT FRAME 22 IAW SRM. AC RETURNED TO SERVICE. (SW21200504818) (K) 2L72 4T4 FRTT00011ATTE6CH 20050505001072005050500107EA 2005 5 5 SWIA200514851 120050407A2750860D10018 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAP MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07587SW 7062 FLAPS HALF SPEED STATUS DURING PREFLIGHT. REPLACED FECU IAW 27-50-00, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050505001222005050500122EU 2005 5 5 AWXA200500451 120050403A5320D53471124200 WEB AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28638AW 455 SAL - MAJOR REPAIR - DURING C-08 CHECK GALVANIC CORROSION WAS FOUND ON WEB BETWEEN FR 69 AND FR 70, STR 23 RT. MAINTENANCE REMOVED AND REPLACED CORRODED WEB FROM FR 69 TO FR 70, STR 23 RT IAW A320 51-42-11 FIG 5 PG 17. 2L72 4F RTA28NM 20050506000022005050600002NM 2005 5 6 UIEA200500022 120050316A5414 PANEL BOEING747 7472D3B 1384805NM NR 2 PYLON CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15505MC 21251 NR 2 PYLON OUTBOARD SIDE CUTOUT FOR PANEL 463CL HAS A .875 INCH CRACK AT AFT CORNER OF SKIN. CRACK WAS NDT INSPECTED TO VERIFY AREA OF CRACK AS PER B747 NDT MANUAL PART 6 51-00-00 FIG 23. STOP DRILLED CRACK IAW B747 SRM 51-10-01 PAGE 12. HFEC INSPECTED STOP DRILL HOLE AND FOUND NO CRACKS EXTENDING BEYOND STOP DRILL HOLE AS PER B747 NDT MANUAL PART 6-51-00-00 FIG 23. INSTALLED DOUBLER REPAIR IAW SRM 54-31-03 FIG 6. (M) 2L74 4F RTA20WE 20050506000042005050600004NM 2005 5 6 UIEA200500039 120050324A575365B01999204 SKIN BOEING747 7472D7B 1384803NM RT OTBD FLAP DELAMINATED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15527MC 22471 DURING SCHEDULE INSPECTION, DELAMINATION WAS FOUND ON THE OUTBOARD TRAILING EDGE FLAP AFT FLAP LOWER SKIN PANEL. PANELS EXCEEDED 25 PERCENT DAMAGE OF THE TOTAL AREA. TRIMMED OUT THE DELAMINATED SKIN REGIONS. NDT INSPECTED TO ENSURE CRACK AND DEFECT FREE CONDITION. INSTALLED REPAIR FILLERS AT EACH TRIM LOCATION AND A SINGLE DOUBLER TO COVER THE PANEL SURFACE. REFINISHED THE PANEL TO DESIGN STANDARD. DETAIL VISUAL INSPECT THE REPAIR AREA FOR DELAMINATION, CRACKS OR LOOSE FASTENERS AT NEXT AIRPLANE A CHECK, 700 HOURS. THERE AFTER REPEAT INSPECTIONS AT 4 MONTH INTERVALS. REPLACE PANEL AT NEXT C-CHECK OR 18 MONTHS WHICHEVER IS EARLIER. ATLAS AIR EO 4757A166 ISSUED TO ACCOMPLISH THE INSPECTION. (M) 2L74 4F RTA20WE 20050506000072005050600007NM 2005 5 6 2005F00063 120050208A5300 SIGHT GLASS BOEING727 727212 138407GNM RT MLG WW MISSING A PCSAJA DUMP FUEL UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO17598AJ 21947 FLT - 711 - MIA-MEX - CREW REPORTED UNABLE TO PRESSURIZE IN FLIGHT, DUMPED FUEL AND RETURNED TO MIA. FOUND RIGHT MAIN GEAR DOWNLOCK VIEWING WINDOW MISSING, INSTALLED VIEWING WINDOW (P/N 66-16515-1), REPLACED SEAL (P/N 66-16514-1) AND CLIPS (P/N 66-14269-1) PER MM 56-40-0. PRESSURIZED A/C PER MM 5-51-71, PERFORMED DECAY CHECK, GOOD. (M) 2L73 4F A3WE 20050506000152005050600015NM 2005 5 6 UIEA200500037 120050323A541265B941071 MOUNT BOEING747 7472D7B 1384803NM NR 4 PYLON CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15527MC 22471 DURING SCHEDULED INSPECTION, NR 4 PYLON, BULKHEAD UPPER CHORD CRACKED AT STATION 270. STOP DRILLED THE CRACK PER 747 SRM 51-10-01. NDT INSPECTED THE REPAIR AREA, INCLUDING HFEC INSPECTION OF ALL TRIMMED FLANGE EDGES AND STOP DRILLED HOLES TO ENSURE CRACK REMOVAL OR CONTAINMENT. INSTALLED ALUMINUM FILLERS, ANGLES AND STRAPS COMMON TO THE UPPER AND AFT CHORDS. DETAIL VISUALLY INSPECT THE AFFECTED CHORD AREA FOR CRACKS, CORROSION AND/OR LOOSE FASTENERS EVERY C-CHECK OR 18 MONTHS, WHICHEVER OCCURS EARLIER. ATLAS AIR EO 4754A131 ISSUED TO ACCOMPLISH THE INSPECTION. (M) 2L74 4F RTA20WE 20050506000162005050600016NM 2005 5 6 UIEA200500023 120050317A5311 FRAME BOEING747 7472D7B 1384803NM BULKHEAD CHAFED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15527MC 22471 D-CHECK AT SINGAPORE, DURING INSPECTION GOUGES WERE FOUND ON THE STATION 2460 BULKHEAD INNER T-CHORD TOP SURFACE AT LBL 30, AND WL 235. BLENDED OUT THE DAMAGED AREA AND INSTALLED A REPAIR STRAP OF .0710 INCH THICK CLAD 2040-T3 MATERIAL. (M) 2L74 4F RTA20WE 20050506000172005050600017NM 2005 5 6 UIEA200500026 120050318A5312 BULKHEAD BOEING747 7472D7B 1384803NM FUSELAGE CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15527MC 22471 DURING INSPECTION, .5 INCH CRACK FOUND ON RT WHEEL WELL SLOPING PRESSURE DECK AT STATION 1240, RBL 35. THE CRACK ORIGINATED FROM THE WATER LINE CONNECTOR HOLE AND EXTENDS UPWARDS. THE CRACKED SLOPING PRESSURE DECK WEB WAS TRIMMED OUT AND REPAIRED WITH DOUBLERS AND FILLERS. (M) 2L74 4F RTA20WE 20050506000182005050600018NM 2005 5 6 UIEA200500028 120050321A5210 FRAME BOEING747 7472D7B 1384803NM PAX DOOR CRACKED A UIEAO OTHER J WARNING INDICATION DEDESCENT 1 EA15522MC 21783 DURING DESCENT, CABIN STILL CLIMBS APPROX 800 PER MINUTE WITH THROTTLES AT IDLE. REPEAT ITEM, SEE LOG PAGE 548463 ITEM 1. REMOVED AND REPLACED R2 DOOR ASSEMBY DUE TO CRACK IN DOOR FRAME PER MM 52-11-01. PER BOEING TELECOM 1-195VDL CONVERTED DOOR TO CARGO FROM PAX CONFIG. FUNCTIONAL CHECK NORMAL PER MM 52-11-09 AND 52-11-02, LEAK CHECK AND OPS CHECK NORMAL. REMOVED DOOR S/N 000901. (M) 2L74 4F RTA20WE 20050506000272005050600027NM 2005 5 6 SWAA051087 120050413A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 705, STR 7R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050506000392005050600039NM 2005 5 6 SWAA051084 120050413A55516551524 FITTING BOEING737 7373H4 1384600NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND LT & RT HORIZONTAL STAB FITTING LUG FACES CORRODED. REPAIRED LUG FACES PER SRM. 2L72 4F RTA16WE 20050506000402005050600040NM 2005 5 6 SWAA051094 120050413A5313BAC1498150 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 380, STR 5L. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20050506000422005050600042NM 2005 5 6 SWAA051097 120050413A53306545777 SKIN BOEING737 7373TO 138447GNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29697SW 23838 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR CUTOUT, LOWER FWD CORNER. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050506000562005050600056NM 2005 5 6 P5CA0501336 120050414A36009788926 SHUTOFF VALVE BOEING747 747230B 1384889NM GE CF6 CF650E2 30018NE NR 1 ENGINE FAILED A P5CAE ENGINE SHUTDOWN N FALSE WARNING CLCLIMB 1 EA15508MC 21644 517265 DURING CLIMBOUT, NR 1 ENGINE NACELLE LOOPS A & B WENT INTO RED, SET WARNING BELLS OFF. ENGINE SHUTDOWN. OIL PRESSURE 45 PSI. REPLACED NR 1 ENGINE HIGH PRESSURE SHUTOFF VALVE PER MM 36-11-05. LEAK CHECK OIL, OPS CHECK NORMAL ON HIGH POWER RUN UP PER MM 71-00-00 TEST NR 4. ENGINE FIRE WARNING NORMAL DURING ALL PARAMETERS. 2L74 4F4 F A20WE E23EA 20050506000702005050600070WP 2005 5 6 UPS05844277 120050404A5712 RIB DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 C1 LT WING OB LEADING EDGE UPPER RIB CRACKED 6 INCH OB OF IB END. REPAIRED RIB IAW SRM 57-02-00-0. 2L74 4F RT4A25 20050506000742005050600074EU 2005 5 6 05FDEA00998 120050414A5544A55370130008000 ARM AIRBUS310 A310 EU ZONE 300 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 NR 7 RUDDER HINGE ATTACHMENT BRACE ( A-FRAME) HAS GOUGE MARKS AND WEAR MARKS AT ATTACHMENT BOLT. REMOVED AND REPLACED NR 7 HINGE ARM IAW A310-200 AMM 55-36-47-4-01 AND 27-21-21-4-01. 2L72 4F RTA35EU 20050506000812005050600081WP 2005 5 6 05FDEA01001 120050414A2910 LINE DOUG DC10 DC1030 3023501WP HYD SYSTEM LEAKING A FDEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO25304FE 46992 AFTER TAKEOFF, LANDING GEAR HANDLE WOULD NOT GO TO UP POSITION, ACCOMPLISHED QRH PROCEDURE. COULD NOT OVERRIDE. UPON RETURN TO GATE DISCOVERED THE RT MLG TRIM CYLINDER HYDRAULIC LINE HAS PIN HOLE. NO OTHER PROBLEMS NOTED FROM VISUAL INSPECTION. REPLACED HYDRAULIC LINE FOR RT LDG TRIM CYLINDER PER MM 32-37-03-2. BLEED HYDRAULIC SYSTEM AND LEAK CKS GOOD. ALSO, OPS CHECKED CRANK AT MAIN GEAR HYD INTER- LOCK CLYINDER AND OPS CKS GOOD. PERFORMED DUMMY GEAR SWING TO VERIFY GEAR HANDLE RELEASES AND OPS CKS NORMAL. RESAFTIED TRIM CYLINDER BYPASS LEVER TO NORMAL POSITION. A/C OK FOR SERVICE. HYDRAULIC LINE CHANGED IS REFERENCE IPC 32-37-05-01 ITEM 75. 2L73 4F A22WE 20050506000842005050600084NM 2005 5 6 05FDEA01006 120050414A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT NR 14L BARREL NUT BORE FOUND EXCEEDED LIMITS. 2L73 4F RTA22WE 20050506000932005050600093EA 2005 5 6 VTZA200500049 120050415A5320601R311719 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27640BR 7340 INTERCOSTAL CRACKED AT .25 INCH IN LENGTH ON RT OUTBOARD SIDE AT FS 484 LEFT BETWEEN BL 27.00. 2L72 4F RTA21EA 20050506001102005050600110NM 2005 5 6 05FDEA01027 120050416A5753ARC7490501 VANE DOUG MD11 MD11 3023602NM ZONE 600 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 RT WING I/B FLAP VANE I/B T-FITTING FOUND OUT OF LIMIT. REMOVED AND REPLACED AS PER CMM 57-52-03. 2L73 4F RTA22WE 20050506001132005050600113NM 2005 5 6 05FDEA01030 120050416A2550 INSULATION BOEING727 727200 138407ENM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25271FE 22036 COMPLY WITH EA 8-7-2580-81688 EQUIPMENT FURNISHINGS INSULATION BLANKETS PARTIAL REPLACEMENT STA 310-1183 MAIN CABIN COMPARTMENT. 2L73 4F RTA3WE 20050506001152005050600115NM 2005 5 6 05FDEA01032 120050416A2550 INSULATION BOEING727 727200 138407ENM ZONE 200 TORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25271FE 22036 COMPLY WITH EA 7-2580-81688 EQUIPMENT FURNISHINGS INSULATION BLANKETS PARTIAL REPLACEMENT STA 310-1183 MAIN CABIN COMPARTMENT. COMPLIED WITH EA 7-2580-81688. 2L73 4F RTA3WE 20050510001242005051000124EA 2005 5 10 MASA200500289 120050408A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAK NONE O OTHER ININSP/MAINT 1 SW0775993 7372 ON RON AND SCHEDULED FOR A SERVICE CHECK INSPECTION, DURING THE WALK AROUND IT WAS DISCOVERED THAT THE RT FORWARD OVERWING EMERGENCY LIGHT WAS NOT ILLUMINATING. REPLACED THE LIGHT BULB OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050510001262005051000126SO 2005 5 10 MASA200500291 120050408A3397 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT UNSECURE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07835MJ 145353 EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. MAINTENANCE SECURED THE CONNECTION AT THE LIGHTING ASSEMBLY, OPS CHECK GOOD. 2L72 4T RTT00011AT 20050510001272005051000127NM 2005 5 10 MASA200500292 120050409A3350 LAMP DHAV DHC8 DHC8202 2809007NM EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07988HA 426 THE EMERGENCY EXIT FLOOR LIGHT AT ROW 3 WAS DISCOVERED INOPERATIVE. MAINTENANCE REPLACED THE LAMP. 2H72 4T RTA13NM 20050510001282005051000128EA 2005 5 10 MASA200500294 120050410A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0777181 7181 PILOT REPORTED AN OVERWING EMERGENCY EXIT EXTERIOR LIGHT INOP. THE CREW MEL'ED THE LIGHT AND MAINTENANCE RELAMPED IT ON THE NEXT LEG. 2L72 4F RTA21EA 20050510001292005051000129EA 2005 5 10 MASA200500295 120050411A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0797325 7325 CREW REPORTED RIGHT FWD OVERWING EXTERIOR EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT. 2L72 4F RTA21EA 20050510001332005051000133WP 2005 5 10 ABXA050093 120050418A2910 O-RING DOUG DC8 DC863 302198AWP CONTROL VALVE FAILED A ABXAB EMER. DESCENT KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL23817AX 45928 OUT OF MSP ENROUTE TO ILN, THE CREW REPORTED HYDRAULIC QUANTITY LOSS DOWN TO THE STANDPIPE. FOUND O-RING ON SLOT CONTACT VALVE BLOWN. REMOVED AND REPLACED O-RINGS ON SLOT CONTROL VALVE AS REQUIRED. MOVED ALL FLIGHT SURFACES SEVERAL CYCLES. SERVICED HYDRAULICS TO MAXIMUM. NO LEAKS NOTED FROM RIGHT MANIFOLD. 2L74 4F 4A25 20050510001342005051000134SO 2005 5 10 C2XA05RI007 120050420A33501317 LAMP EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT BURNED OUT A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714938 145029 RIC - DURING SCHEDULED MAINTENANCE, THE RIGHT FWD EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BULB. OPS CHECK GOOD. A/C RELEASED TO SERVICE. 2L72 4F RTT00011AT 20050510001382005051000138SO 2005 5 10 C2XA05IA055 120050418A3397MS3476L1412S CONNECTOR EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT DIRTY A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714942 145037 IAH - FLIGHT 2638, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHT ABOVE THE FA SEAT WAS INOPERATIVE. MAINTENANCE CLEANED THE ELECTRICAL CONNECTORS, OPERATIONALLY CHECKED THE EMERGENCY LIGHTS WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050510001472005051000147EU 2005 5 10 MALA050365 120050416A2920 PTU BAC 146 AVRO146RJ85A1500097EU HYD SYSTEM LEAKING A MALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL15520XJ E2345 EN ROUTE TO MSP THE CREW GOT THE GREEN HYD LOOK UP LIGHT WITH GREEN LOW QTY. THE GREEN HYD QTY WAS JUST BELOW 1/4 FULL. REPLACED PTU. 2H74 4F RTA49EU 20050510001482005051000148 2005 5 10 MALA050312 420050405A3440 ANTENNA SAAB SF340 SF340A 7850100EU RADAR ALTIMETER FAILED A MALAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 GL1599XJ 340A099 BANK ANGLE LIGHT SHORTLY AFTER TO AND RA STUCK AT 50 AND TERRAIN WARNING. AC RETURNED TO DTW. REMOVED AND REPLACED BOTH TX AND RX ANTENNAS. REMOVED AND REPLACED RAD ALT ANTENNAS 2L72 4T RTA52EU 20050510001532005051000153NE 2005 5 10 MALA050313 220050405A7200 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LEFT FLUCTUATES A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15433XJ 340B433 AC DID AN AIR RETURN DUE TO LT ENGINE TORQUE FLUX. 2L72 4T4 TRTA52EU E8NE 20050510001552005051000155EU 2005 5 10 MALA050292 120050322A5320 THRESHOLD SAAB SF340 340B 7860101EU PAX DOOR CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15415XJ 340B415 DURING 4K CHECK IN BNA FOUND FLOOR FLANGE NUT PLATE ATTACH POINTS ARE CORRODED OUT OF LIMITS AT PAX DOOR THRESHOLD. BRACKETS HAVE BEEN REMOVED AND REPLACED IAW SRM 51-40-21. 2L72 4T RTA52EU 20050510001572005051000157EU 2005 5 10 MALA050299 120050322A7930 WARNING LIGHT SAAB SF340 340B 7860101EU ENG BYPASS ILLUMINATED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15439XJ 340B439 RIGHT ENGINE BYPASS LIGHT ON AFTER T/O, 15 PSI LOWER. RETURNED AC TO DTW. REPLACED SWITCH. 2L72 4T RTA52EU 20050510001852005051000185WP 2005 5 10 UPS05844301 120050411A5711 SPAR DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE: C2, FOUND POSSIBLE CRACK JUST I/B OF XCW 46 ON LOWER FRONT SPAR CAP VERTICAL ANGLE INSIDE RT CTR FUEL TANK. NDT VERIFIED CRACK APPROX 3 INCH LONG PER NDTSPM 06=10-01.001. CRACK RUNS FROM FASTENER HOLE TO FASTENER HOLE. REPAIRED CRACK IAW DC-8 SRM 57-2 -6 FIG 10. 2L74 4F RT4A25 20050510001872005051000187WP 2005 5 10 UPS05844311 120050402A5313DC853B0093 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 INSPECTION TYPE:C1 LONGERON CRACKED 2 INCH LONG, AT STA 480 L20R, UPPER AND LOWER FLANGE. REMOVED DAMAGED LONGERON AND INSTALLED LONGERON AND SPLICES FROM FROM STA 460 TO 490 IAW SRM 53-02-02 FIG 11, 53-04-0, 53-04-01 AND 51- 1-8. 2L74 4F RT4A25 20050510001892005051000189WP 2005 5 10 UPS05844315 120050406A5330 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 INSPECTION TYPE:C1 B-PIT DOOR AFT TORQUE BOX LWR FRAME AT STA 580 IS CRACKED BETWEEN L33R AND L33R. FABRICATED AND INSTALLED 2 DOUBLERS AND 1 FILLER AND INSTALLED IAW SRM 53-02-00-0 FIG 001B SHT 3, 53-2-0 FIG 1B, 51-1-21A, 51-1-21 AND EO DC-8 5320-6176-B. 2L74 4F RT4A25 20050510001912005051000191NM 2005 5 10 C1HA200595004 120050405A53146015615 KEELBEAM BOEING727 727290 138408WNM FUSELAGE CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 RIGHT WHEEL WELL STA 875 ANGLE CRACKED KEELBEAM APPROX 1 INCH LONG. REMOVED AND REPLACED ANGLE IN RIGHT WHEEL WELL AT STA 875 AT KEEL BEAM IAW B727 SRM 51-30-2. REMOVED AND REINSTALLED APU IAW B727 MM 49-10-00. OPS CHECK & LEAK CHECK GOOD IAW B727 MM 42-20-00 MAT ID WITH ROC. 2L73 4F A3WE 20050510001932005051000193SO 2005 5 10 SIMA200509805 120050331A531314533888001 STRINGER EMB 135 EMB135KL 3260302SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21803AE 145483 FOUND STRINGER 19L WAS FOUND CHAFED. BLENDED THE CHAFED AREA AND PERFORMED NDT. FABRICATED A REINFORCEMENT ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 28 CHAPTER 53-24-02. (M) 2L72 4F RTT00011AT 20050510001952005051000195SO 2005 5 10 SIMA200510113 120050405A532014522459003 SUPPORT EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21701MH 145162 DURING CPCP INSPECTION, FOUND CENTER AISLE RIGHT RAMP SUPPORT AT FRAME 20 IS CORRODED. INSTALLED NEW RAMP IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050510001972005051000197SO 2005 5 10 SIMA200510110 120050404A532014521725013 PLATE EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21701MH 145162 SAW - DURING CPCP INSPECTION, FOUND SERVICE DOOR FORWARD SILL CORRODED. REPLACED SERVICE DOOR FORWARD SILL PLATE IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050510001992005051000199SO 2005 5 10 SIMA200509404 120050403A272015793101 PRESSURE SWITCH EMB 145 EMB145 3260210SO RUDDER DEFECTIVE A SIMAO OTHER J WARNING INDICATION LDLANDING 1 SW21612AE 145079 IN CRUISE FLIGHT RUDDER SYSTEM HALF INOPERATIVE EICAS WARNING ILLUMINATED WENT OUT THEN REILLUMINATED. DECLARED EMERGENCY COMING INTO LGA AND LANDED WITHOUT INCIDENT. REPLACED RUDDER PRESSURE SWITCH IAW AMM 27-2304. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050510002012005051000201NM 2005 5 10 C1HA200595005 120050408A5330 SKIN BOEING727 727290 138408WNM FUSELAGE DENTED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 FUSELAGE SKIN 2.7 INCH AFT OF STA 259 AND JUST BELOW STR 17L HAS OUTWARD DENT, MARKED P4. CUT OUT DENT DAMAGE, FAB FILLER USING .050 2024T3 PO 0440785 AND REPAIR DOUBLER USING .063 2024T3 PO 0442440, DRILLED, ALODINE, PRIMED AND INSTALLED FILLER AND REPAIR DOUBLER IAW 727-200 SRM 53-30. 2L73 4F A3WE 20050510002032005051000203NM 2005 5 10 SWAA051147 120050418A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29325SW 23689 DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 968, STR 21L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050510002082005051000208NM 2005 5 10 SWAA051152 120050418A3350D71701100 BATTERY PACK BOEING737 7377H4 1384404NM CABIN FAILED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29717SA 27851 DURING SCHEDULED HC2 CHECK, LT AFT EMERGENCY LIGHT BATTERY PACK FAILED TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050510002092005051000209NE 2005 5 10 SWAA051153 220050417A7230P333P05 BLADE BOEING737 7377H4 1384404NM GE CFM56 CFM56* 13802NE NR 2 ENGINE DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29786SW 29811 876649 DURING SCHEDULED RON CHECK, C/W BOROSCOPE INSPECTION OF NR 2 ENGINE AND FOUND 1 EA NR 3 HPC BLADE OUT OF LIMITS. REMOVED AND REPLACED NR 2 ENGINE PER MM. 2L72 4F4 FRTA16WE E2GL 20050510002142005051000214NM 2005 5 10 PIDA200500014 120050419A5744 SUPPORT ANGLE BOEING737 73736M 138443BNM NR 5 SPOILER CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05374PA 28333 NUMBER 5 SPOILER I/B ATTACH BRACKET SUPPORT ANGLES CRACKED. REPLACED ANGLES PER SRM 51-10-2. 2L72 4F RTA16WE 20050510002182005051000218NM 2005 5 10 PIDA200500012 120050419A5345 CHANNEL BOEING737 73736M 138443BNM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05374PA 28333 CRACK IN LOWER RADIUS AT AFT END OF THE LEFT MOUNT HAT CHANNEL FOR THE RADAR TR UNIT. REPAIRED HAT CHANNEL PER SRM 51-70-12. 2L72 4F RTA16WE 20050510002212005051000221NM 2005 5 10 PIDA200500008 120050419A5311 FRAME BOEING737 73736M 138443BNM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05374PA 28333 TWO CRACKS IN BS 827 FRAME AT STR 9 LT. REPAIRED PER SRM 53-00-07. 2L72 4F RTA16WE 20050510002222005051000222NM 2005 5 10 PIDA200500013 120050419A532065528948 INTERCOSTAL BOEING737 73736M 138443BNM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05374PA 28333 INTERCOSTAL AT BS 540 CRACKED AT I/B AFT ATTACH FASTENER AT RBL 1. REPLACED INTERCOSTAL PER DWG 65-52894 AND SRM 51-10-2. 2L72 4F RTA16WE 20050510002242005051000224NM 2005 5 10 PIDA200500006 120050419A5311 FRAME BOEING737 73736M 138443BNM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05374PA 28333 TWO CRACKS AT RIVET HOLE IN BS 867 FRAME AT STR 9 RT. REPAIRED PER SRM 53-00-07. 2L72 4F RTA16WE 20050511000022005051100002SO 2005 5 11 SIMA200510106 120050329A532014521707003 SUPPORT EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21701MH 145162 SAW - DURING CPCP INSPECTION, FOUND CENTER AISLE RAMP SUPPORT FRAME 20 CORRODED. MAINTENANCE REPLACED CENTER AISLE RAMP SUPPORT IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050511000062005051100006SO 2005 5 11 SIMA200510109 120050404A532014522461011 DOUBLER EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21701MH 145162 SAW - DURING CPCP INSPECTION, FOUND DOUBLER AT FRAME 20 CORRODED. INSTALLED NEW DOUBLER IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050511000072005051100007SO 2005 5 11 SIMA200510115 120050405A532014522460009 GUSSET EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21701MH 145162 DURING CPCP INSPECTION, FOUND GUSSET IN CENTER HAT TRACK UNDERFLOOR IS CORRODED BETWEEN FRAME 18-23. MAINTENANCE REPLACED GUSSET IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050511000082005051100008SO 2005 5 11 SIMA200510114 120050405A532014522460011 DOUBLER EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21701MH 145162 DURING CPCP INSPECTION, FOUND DOUBLER AT FRAME 18 UNDERFLOOR IS CORRODED. REPLACED DOUBLER IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050511000092005051100009SO 2005 5 11 SIMA200510118 120050407A532013500437001 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21701MH 145162 SAW - DURING CPCP INSPECTION, FOUND RIGHT OMEGA BEAM CORRODED IN FORWARD CABIN AT FRAME 25. REPLACED RIGHT OMEGA BEAM IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050511000132005051100013NM 2005 5 11 2005F00074 120050209A28006000145 GUARD BOEING727 7272D3 138407NNM SWITCH STICKING A PCSAA UNSCHED LANDING O OTHER CLCLIMB 1 SO17804AJ 21021 FLT 725 - MIA-MEX - CREW REPORTED NR 2 CROSSFEED VALVE WOULD NOT OPEN IN FLIGHT. AIRCRAFT RETURNED TO MIA, AIRCRAFT LANDED AT MIA WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND NR 2 FUELING VALVE SWITCH IN THE ON POSITION AT THE WING FUELING STATION. MAINTENANCE RESET THE SWITCH TO THE OFF POSITION, AN OPERATIONAL CHECK WAS ACCOMPLISHED OF THE NR 2 FUELING CROSSFEED VALVE AND WAS FOUND TO BE OPERATING NORMAL IAW BOEING 727 MM CH 28-20-0. AS A PRECAUTIONARY THE NR 2 FUELING VALVE SWITCH GUARD WAS REPLACED IN THE WING FUELING STATION. AIRCRAFT FLEW LATER THAT EVENING MIA-MEX-MID-MIA WITH NO FURTHER FUEL CROSSFEED VALVE PROBLEMS REPORTED. (M) 2L73 4F A3WE 20050511000142005051100014EU 2005 5 11 USAA050465 120050405A5315D5311281820401 FLOORBEAM AIRBUS320 A320214 3930316EU FUSLEAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19106US12932 1044 PIT - FOUND FLOORBEAM CORRODED 1 BY .5 BY .030 INCH, .75 INCH BY .5 INCH BY .030 INCH, .75 BY .3750 BY .05, FLOOR BEAM 10 INCHES LEFT OF CENTER LINE BETWEEN C16 AND C22. DEFECTIVE PART REPLACED WITH IDENT PART. (M) 2L72 4F RTA28NM 20050511000172005051100017NM 2005 5 11 2005F00071 120050210A2781 WARNING LIGHT BOEING727 7272D3 138407NNM NR 5 LE FLAP ILLUMINATED A PCSAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO17804AJ 21021 FLT 847 - SJO-FFR - CREW REPORTED UPON FLAP RETRACTION NR 5 LEADING EDGE FLAPS AMBER LIGHT REMAINED ILLUMINATED. F/E'S ANNUNCIATOR INDICATED NR 5 LEADING EDGE FLAP INTRANSIT. AIRCRAFT RETURNED TO SJO. AIRCRAFT LANDED AT SJO WITHOUT FURTHER INCIDENT. OPERATIONAL CHECK ON GROUND, SYSTEM WORKS OK IAW AMM 27-82-10. AIRCRAFT FLEW LATER THAT EVENING SJO-FFR-MIA WITH NO FURTHER. 2L73 4F A3WE 20050511000192005051100019EU 2005 5 11 AWXA200500472 120050419A2133VFT300A1 OUTFLOW VALVE AIRBUS320 A320232 3930326EU ZONE 126 MALFUNCTIONED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28651AW23208581 866 IAH - AIR TURN BACK - FLT 0103 - ON DEPARTURE OUT OF IAH EN ROUTE FOR LAS RECEIVED UPPER ECAM MESSAGE FOR AVIONICS VENT FAULT, EXTRACT VALVE INDICATED FULL OPEN NOT ALLOWING AIRCRAFT TO PRESSURIZE, TURNED BACK TO IAH AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED SKIN AIR OUTLET VALVE IAW T/C R2A211301, OPERATIONAL CHECK WAS GOOD. FUNCTIONAL TEST OF SKIN AIR VALVE SN 1175 CONFIRMED REASON FOR REMOVAL FINDING THAT ACTUATOR UNIT WAS JAMMING CAUSING TORQUE LIMITER TO SLIP. REPLACED ACTUATOR AND RE-ACCOMPLISHED FUNCTIONAL TEST IAW CMM 21-26-53 REV. 6. 2L72 4F RTA28NM 20050511000222005051100022 2005 5 11 QXEA200500709 420050419A34207003360941 COMPUTER DHAV DHC8 DHC8202 2809007NM AHRS FAILED A QXEAA UNSCHED LANDING O OTHER CLCLIMB 1 NM09357PH26100194 504 SEA - ON FLIGHT 2182 (SEA-YLW) AFTER TAKEOFF, RECEIVED A ADI PITCH MISMATCH AND AHRS FAIL MESSAGES. NO YD FAILURES. FO'S ADI SHOWING 10 DEGREES DOWN WHILE IN A 7 DEGREE CLIMB. RETURNED TO FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE REPLACED THE NR 2 AHRS COMPUTER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050511000232005051100023NM 2005 5 11 QXEA200500707 120050419A5230 LOCK BOMBDRDHC8 DHC8402 1390042NM CARGO DOOR OUT OF RIG A QXEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM09407QX 4049 MFR - ON FLIGHT 2310 (RDD-PDX) DURING CRUISE FLIGHT, THE FORWARD BAGGAGE DOOR WARNING LIGHT CAME ON. AIRCRAFT DIVERTED TO MFR AND ACCOMPLISHED A UNEVENTFUL LANDING. CRF NOT NEEDED. ON THE GROUND NOTICED THE EXTERNAL HANDLE EXTENDED .125 INCH. CYCLED DOOR CHECKS GOOD. MAINTENANCE IN PDX LATER FOUND DOOR LOCKING OVERCENTER OUT OF RIG. RIGGED VENT DOOR MECHANISM IAW 52-00-00-830-801. OPERATIONAL CHECKS GOOD. NO PARTS REPLACED. 2H72 4T RTA13NM 20050511000252005051100025SO 2005 5 11 SWIA200514870 120050413A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT DISCHARGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07308SW 120326 ONE OF THE FLOOR EMERGENCY LIGHTING STRIPS AND THE 2 OVERWING EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED CENTER AND AFT ELBP. OPS CHECKED GOOD, PN D366-04-001 SN/OFF 551 PN D366-04-001 SN/OFF 1219. 2L72 4T RTA31SO 20050511000262005051100026EA 2005 5 11 SWIA200514871 120050415A5610 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAO OTHER O OTHER DEDESCENT 1 NM07927SW 7693 CAPTAIN'S SIDE WINDOW CRACKED. REPLACED CAPTAIN'S SIDE WINDOW IAW CRJ MM 56-12-01. OPERATIONAL CHECK GOOD. PN NP139322-9 SN/OFF 02163H7998. 2L72 4F RTA21EA 20050511000272005051100027EA 2005 5 11 SWIA200514872 120050418A274070623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07956SW 7825 STAB CHANNEL 2 WILL NOT ENGAGE. REPLACED HORIZONTAL STABILIZER MOTOR CONTROL UNIT IAW AMM 27-42-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050511000282005051100028EA 2005 5 11 SWIA200514873 120050415A335020131A BATTERY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSDISCHARGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07956SW7270 7270 EMERGENCY EXIT LIGHTS AT ROW 8 DIM. REPLACED NR 3 POWER SUPPLY IAW MM 33-50. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050511000292005051100029SO 2005 5 11 SWIA200514874 120050413A3350 SIGN EMB 120 EMB120ER 3260203SO EMERGENCY EXIT DISLODGED A SWIAO OTHER D INFLIGHT SEPARATION NRNOT REPORTED 1 NM07580SW 120348 EXIT SIGN NEAR MAIN CABIN DOOR FELL OFF. REPLACED EXIT SIGN BY PAX DOOR IAW MM 33-40-00 . OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050511000302005051100030EA 2005 5 11 SWIA200514875 120050415A2740 SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB TRIM STICKING A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07405SW 7029 FOS TRIM SWITCH IS STICKY. REPLACED FOS TRIM SWITCH, OPERATIONAL CHECK GOOD IAW MM 27-41-00. 2L72 4F RTA21EA 20050511000322005051100032NM 2005 5 11 PIDA200500011 120050419A5320 ATTACH ANGLE BOEING737 73736M 138443BNM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05374PA 28333 UPPER ATTACH ANGLE ON INTERCOSTAL AT BL 0 BETWEEN BS 380 AND BS 400 AT WL 208 IS CRACKED. REPLACED ANGLE PER SRM 51-10-02. 2L72 4F RTA16WE 20050511000342005051100034EA 2005 5 11 SWIA200514878 120050415A2710 BEARING CNDAIRCL600 CL6002B19 1900309EA AILERON TRQ TUBENOISY A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07408SW 7055 NOISES CAN BE HEARD AND FELT WHILE MAKING AILERON INPUTS WITH THE CAPTIAN'S YOKE. REPLACED LEFT AILERON TORQUE TUBE BRACKET BEARING IAW AMM 27-11-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050511000362005051100036EA 2005 5 11 SWIA200514880 120050415A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07440SW 7589 FORWARD AND AFT CEILING EMERGENCY FLOOR LIGHTS INOPERATIVE. REPLACED BULBS OPERATIONAL CHECK OK. 2L72 4F RTA21EA 20050511000372005051100037NM 2005 5 11 P5CA0501341 120050414A36108988061 REGULATOR VALVE BOEING747 747230B 1384889NM GE CF6 CF650E2 30018NE NR 1 ENGINE MALFUNCTIONED A P5CAEA ENGINE SHUTDOWN UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 EA15508MC 21644 517265 DURING CLIMBOUT NR 1 ENGINE NACELLE LOOPS A & B WENT INTO THE RED - SET BELL OFF - ENGINE SHUT DOWN OIL PRESSURE 45 PSI. REPLACED ENGINE PRESSURE REGULATING VALVE, LEAK CHECK OK. OPS CHECKED OK DURING ENGINE HIGH POWER ASSURANCE RUN, MM 36-11-19 & MM 36-11-00 AND TESTED PER MM 71-00-00 TEST NR 4. 2L74 4F4 F A20WE E23EA 20050511000382005051100038EA 2005 5 11 SWIA200514881 120050413A2750860D10018ABCD CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07442SW6815 6815 FLAPS DEGRADED MSG ON EICAS. REPLACED FLAP ELECTRONIC CONTROL UNIT IAW CRJ 200 MM 27-51-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050511000442005051100044EA 2005 5 11 SWIA200514885 120050203A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07589SW 7072 CRACKED ANGLE AT FS 499 LBL 10 UNDER FLOORBOARD. (ITEM FOUND AT C-CHECK INSPECTION.) INSTALLED NEW ANGLE PER SRM 51-23-00 AND 51-42-21. 2L72 4F RTA21EA 20050511000492005051100049EA 2005 5 11 SWIA200514888 120050203A5712 RIB CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07589SW 7072 BATT RIB CRACKED AT UPPER FLANGE, AFT SIDE. LOCATED AT LT MLG BAY, WS 53-600. (ITEM FOUND AT C-CHECK INSPECTION) INSTALLED REPAIR IAW 601R-57-51-046. 2L72 4F RTA21EA 20050511000542005051100054NM 2005 5 11 QXEA200500646 120050412A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - LEFT OUTBOARD SEAT TRACK NR 1 HAS DAMAGE ON TOP OF LUGS AT X278. REPAIRED IAW RD 8-53-1342. 2H72 4T RTA13NM 20050511000562005051100056NM 2005 5 11 QXEA200500657 120050412A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 200 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - GOUGE IN CENTER OF RIGHTHAND OUTBOARD SEAT TRACK AT STATION X282.0. REPAIRED IAW RD 8-53-1342. 2H72 4T RTA13NM 20050511000572005051100057NM 2005 5 11 QXEA200500661 120050412A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - CORROSION IN CENTER OF RIGHT OUTBOARD SEAT TRACK AT STATION X502.0. REPAIRED IAW RD 8-53-1342. 2H72 4T RTA13NM 20050511000582005051100058NM 2005 5 11 QXEA200500658 120050412A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - GOUGE IN RIGHT OUTBOARD SEAT TRACK AT STATION 310.0. REPAIRED IAW RD 8-53-1342. 2H72 4T RTA13NM 20050511000602005051100060NM 2005 5 11 QXEA200500653 120050412A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - LEFT OUTBOARD SEAT TRACK NR 1 HAS CORROSION ON BOTTOM OF CHANNEL AT X345. REPAIRED IAW RD 8-53-1342. 2H72 4T RTA13NM 20050511000632005051100063NM 2005 5 11 QXEA200500652 120050412A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - LEFT OUTBOARD SEAT TRACK NR 1 HAS CORROSION ON TOP OF LUGS AT X345 - 346. REPAIRED IAW RD 8-53-1342. 2H72 4T RTA13NM 20050511000642005051100064NM 2005 5 11 QXEA200500656 120050412A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - LEFT OUTBOARD SEAT TRACK NR 1 HAS CORROSION ON TOP OF LUGS AT X421. REPAIRED IAW RD 8-53-1342. 2H72 4T RTA13NM 20050511000652005051100065EA 2005 5 11 COMA0560267 120050420A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01981CA 7163 CRACK FOUND ON LEFT WING PLANK. REPAIRED IAW CRJ REO 601R-57-21-130. 2L72 4F RTA21EA 20050511000662005051100066NM 2005 5 11 QXEA200500660 120050412A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - GOUGE IN RIGHT OUTBOARD SEAT TRACK AT STATION X468.0. REPAIRED IAW RD 8-53-1342. 2H72 4T RTA13NM 20050511000682005051100068NM 2005 5 11 AALA20050280 120050420A2530 OVEN BOEING767 767323 1385205NM GALLEY MALFUNCTIONED A AALAHA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21349AN 33088 GLA - EN ROUTE FRA - ORD ON FLIGHT 83 CREW REPORTED SMOKE COMING OUT OF OVERHEAD AREA BY 1L DOOR. UTILITY BUSSES TURNED OFF AND SMOKE DISSIPATED. LANDED GLA WITHOUT INCIDENT. REPLACED NUMBER 1 GALLEY OVEN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050511000692005051100069NM 2005 5 11 QXEA200500644 120050412A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - LEFT OUTBOARD SEAT TRACK NR 1 HAS LIGHT CORROSION ON SCRATCH IN BOTTOM OF CHANNEL, FORWARD OF X262. REPAIRED IAW DHC-8 200 NDTM PART 1, 51-00-06 AND RD 8-53-1342. 2H72 4T RTA13NM 20050511000722005051100072NM 2005 5 11 QXEA200500647 120050412A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - LEFT OUTBOARD SEAT TRACK NR 1 HAS LIGHT CORROSION IN BOTTOM OF CHANNEL AT X278 TO X285. REPAIRED IAW RD 8-53-1342. 2H72 4T RTA13NM 20050511000752005051100075NE 2005 5 11 JBGA20050002 220050415A7200 ENGINE LEAR 60 60LEAR 5170707CE PWA 305 PW305 NE FLAMED OUT E JBGAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 GL07529KF 064 CA0273 ENGINE FLAME OUT FOLLOWED BY AMBER ENGINE LIGHT. ENGINE RELIGHT NORMAL. ENGINE CONTINUED OPERATION NORMAL. 2L72 4F4 FRTA10CE E35NE 20050511000762005051100076EA 2005 5 11 COMA0560271 120050420A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA RT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01981CA 7163 CRACK FOUND ON RIGHT WING PLANK. REPAIRED IAW REPAIRED CRJ REO 601R-57-21-130. 2L72 4F RTA21EA 20050511000772005051100077EU 2005 5 11 DHL2005367505 120050403A5347TMS6022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU CABIN CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01367DH 265 DURING "C" CHECK IN MIAMI, FL. AT AVBORNE HEAVY MAINTENANCE DISCREPANCY AS FOLLOWS, N/R 018786 CABIN SEAT TRACK AT FR 18 THRU FR 21A AT BL 58R HAS CORROSION ( MKD. ) REPLACED SEAT TRACK SECTION AT RBL 58" FROM BS 1393 TO 1445 IAW A-300 SRM 51-30-30 AND 53-10-00. MAT USED TMS 60-22457 P/O 2113624 38" LONG = LIFT. 2L72 4F RTA35EU 20050511000782005051100078EA 2005 5 11 COMA0560272 120050420A5320 STRUCTURE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01981CA 7163 RIGHT HAND FUSELAGE 718.00 CRACKED. REPAIRED IAW BOMBARDIER SB 601R-53-055. 2L72 4F RTA21EA 20050511000792005051100079EA 2005 5 11 COMA0560273 120050419A323016600103 UPLOCK CNDAIRCL600 CL6002B19 1900309EA NLG FAULTY A COMAK NONE J WARNING INDICATION APAPPROACH 1 SO01819CA12916 7415 FLIGHT 4947 DURING JFK APPROACH RECEIVED A LANDING GEAR DISAGREE, THE NLG TOOK 1 MINUTE TO INDICATE DOWN AND LOCKED. REPLACED THE NLG UPLOCK ASSEMBLY. 2L72 4F RTA21EA 20050511000832005051100083EU 2005 5 11 MALA050370 120050417A5320 GUSSET BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15503XJ E2310 DURING C2 INSPECTION, FOUND FLOOR GUSSET CORRODED AT FRAME 19 BETWEEN RBL 45 AND 66. 2H74 4F RTA49EU 20050511000872005051100087EU 2005 5 11 MALA050367 120050416A3020 DUCT SAAB SF340 340B 7860101EU LT INTAKE DEFECTIVE A MALAO OTHER O OTHER CLCLIMB 1 GL15445XJ 340B445 JUST AFTER DEPARTING MSP THE LEFT HAND INTAKE HEAT STARTED CYCLING. AIR RETURNED BACK TO MSP. REPLACED LOWER DUCT. 2L72 4T RTA52EU 20050511000882005051100088EU 2005 5 11 MALA050366 120050416A2150 VALVE BAC 146 AVRO146RJ85A1500097EU A/C PACK DEFECTIVE A MALAO OTHER M OVER TEMP NRNOT REPORTED 1 GL15536XJ E2372 FLIGHT DID AIR RETURN AFTER EXPERIENCING A REAR BAY HIGH TEMP IN FLIGHT. REMOVED AND REPLACED NR 2 PACK VALVE. 2H74 4F RTA49EU 20050511000892005051100089 2005 5 11 PIDA200500016 420050421A3422 COMPASS BOEING737 7372K5 138448XNM COCKPIT MALFUNCTIONED A PIDAA UNSCHED LANDING O OTHER CLCLIMB 1 SO05250TR 22597 AFTER TAKEOFF, BOTH COMPASS HEADINGS ROLLED AWAY FROM RUNWAY HEADING. RETURNED TO FIELD. PERFORMED SYSTEM CHECKOUT PER MM 34-21-00. SYSTEM CHECKED NORMAL. PERFORMED VISUAL INSPECTION OF BOTH DIRECTIONAL GYROS, NO PROBLEMS NOTED. 2L72 4F RTA16WE 20050511000902005051100090CE 2005 5 11 DXTA200500686 120050419A324160414201A RELAY CESSNA500 560CESSNA 2076750CE ANTI-SKID SYS MALFUNCTIONED E DXTAO OTHER J WARNING INDICATION APAPPROACH 1 GL07324QS 5600423 WHEN GEAR SELECTED DOWN, BRAKE PRESS LOW AND ANTI SKID INOP ANNUNCIATORS LIT. DIVERTED TO CMH, UPON 2ND GEAR EXTENSION NO ANNUNCIATORS ILLUMINATED. INSTALLED NEW SKID CONTROL RELAY (K74) AND NEW HI-PRESSURE SWITCH (S168) IAW CE-560 WDM 32-40-01. OPS CHECK GOOD. 2L72 4F RTA22CE 20050511000912005051100091CE 2005 5 11 DXTA200500687 120050419A3240MS24166D2 RELAY CESSNA560 560XL 2076702CE BRAKE SYS FAILED E DXTAO OTHER J WARNING INDICATION TOTAKEOFF 1 GL07626QS 5605126 LO BRAKE PRESS & ANTISKID INOP ANNUNCIATOR ILLUMINATED AT START OF T/O ROLL CAUSING WHEEL BRAKE FAILURE, THE EMERGENCY BRAKING SYSTEM WAS USED. TROUBLESHOT TO POWER BRAKE CONTROL RELAY KN003. RELAY WOULD NOT CLOSE. REMOVED AND REPLACED RELAY IAW CC 560XL WIRING DIAGRAMS 32-40-01. BLED ANTISKID BRAKE SYSTEM. LEAK CHECKS AND OPERATIONAL CHECKS GOOD IAW CC 560XL MM CHAPTER 32-42-00. 2L72 4F RTA22CE 20050511000962005051100096NM 2005 5 11 CALA0500115 120050421A3350BR964421 MODULE BOEING737 737824 13844BZNM CABIN LOOSE A CALAK NONE O OTHER ININSP/MAINT 1 SW2726210 28770 AISLE LIGHTING IN THE FIRST CLASS CABIN LOOSE AT G7 GALLEY. REPLACED LIGHT MODULE. 2L72 4F RTA16WE 20050511000972005051100097SO 2005 5 11 C2XA05IA056 120050415A3350BA50933901 CHARGER EMB 145 EMB145XR 3260214SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714125 145690 CRP - DURING MAINTENANCE INSPECTION THE NUMBER TWO EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO EMERGENCY LIGHT BATTERY CHARGER, OPERATIONALLY CHECKED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. NO TIMES ARE AVAILABLE ON THIS PART. 2L72 4F RT 20050511001002005051100100SO 2005 5 11 C2XA05CL022 120050420A33501317 LIGHT EMB 135 EMB135LR 3260305SO EXTERIOR INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2728529 145512 DURING ROUTINE MAINTENANCE THE RIGHT OVERWING EMERGENCY LIGHT DID NOT ILLUMINATE WHEN TESTED. MAINTENANCE INSPECTED AND REPLACED THE LAMPS LOCATED AT THE RIGHT OVERWING EMERGENCY LIGHT FIXTURE AND THE OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20050511001012005051100101SO 2005 5 11 C2XA05CL023 120050418A27403621001009 CONTROL UNIT EMB 145 EMB145LR 3260212SO E/E BAY INOPERATIVE A C2XAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW27185576755 6755 145596 CLE - THE CREW REOPTED PITCH TRIM INOP ON THE EICAS, ALONG WITH NO RESPONSE FROM THE PITCH TRIM SWITCH. MAINTENANCE ACCESSED THE CMC AND FOUND THE HORIZONTAL STAB CONTROL UNIT FAIL MESSAGE. MAINTENANCE REPLACED THE HSCU AND THE AIRCRAFT CONDUCTED A SUCCESSFUL TEST FLIGHT. THE AIRCRAFT THEN CONTINUED WITH NO DIFFICULTIES REPORTED. 2L72 4T RTT00011AT 20050511001032005051100103SO 2005 5 11 C2XA05CL025 120050421A3350 SIGN EMB 145 EMB145ER 3260211SO CABIN MALFUNCTIONED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713935 145022 DURING ROUTINE MAINTENANCE IN CLEVELAND THE EXIT SIGN ON THE RIGHT FORWARD BULKHEAD (FORWARD OF SEAT 3B) DID NOT ILLUMINATE WHEN TESTED. MAINTENANCE CYCLED THE EMERGENCY LIGHT CIRCUIT BREAKER AND THE OPERATIONAL TEST WAS GOOD. 2L72 4F RTT00011AT 20050511001042005051100104SO 2005 5 11 C2XA05CL026 120050421A33501317 LIGHT EMB 145 EMB145ER 3260211SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713935 145022 DURING ROUTINE MAINTENANCE IN CLEVELAND THE EMERGENCY LIGHT ON THE SERVICE DOOR DID NOT ILLUMINATE WHEN TESTED. MAINTENANCE REPLACED THE LAMP AND OPERATIONAL TESTS WERE GOOD. 2L72 4F RTT00011AT 20050511001082005051100108NM 2005 5 11 72300161 120050114A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE GOUGED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 .9375 GOUGE AT SIDE OF FASTENER HOLE ON LOWER FLANGE OF SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050511001142005051100114NM 2005 5 11 72300167 120050413A5315 FLOORBEAM BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 3 INCH BY .75 INCH AREA OF CORROSION ON FLOORBEAM UPPER CHORD. 2L73 4F4 FRTA3WE E2EA 20050511001182005051100118WP 2005 5 11 05FDEA01052 120050419A5753ARC2369503 SKIN DOUG MD10 MD1010F 3022112WP ZONE 500 BULGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25370FE 46608 COMPLY WITH EA 8-5750-55478,WINGS-LT INBD FLAP-UPPER SKIN BULGE REPAIR AT XIFH=183.3 (P/N ARC2369-503). BFM R COMPLIED WITH EA8-5750-55478-WINGS LT INBOARD FLAP, UPPER SKIN BULGE REPAIR AT XIFH 183.3 (P/N ARC2369-503). 2L73 4F RTA22WE 20050511001212005051100121SO 2005 5 11 SIMA200510102 120050401A533014520558003 SKIN EMB 145 EMB145LR 3260212SO FUSELAGE LIGHTNING STRIKEA SIMAK NONE O OTHER ININSP/MAINT 1 SW21689EC 14500853 LIGHTNING STRIKE DAMAGE ON SKIN AT FRAME 32 BETWEEN STRINGER 10L AND 11L. MAINTENANCE REPAIRED DAMAGE IAW SRM 53-22-01 FIG 207, SKIN PATCH AT FRAME REPAIR. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20050511001242005051100124EU 2005 5 11 2005F00066 120050325A612330048000018 AUTOFEATHER SYS AEROSPATR72 ATR72212 8680945EU NR 2 ENGINE MALFUNCTIONED A TRBAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO29434AT 434 DURING TAKEOFF ROLL, A CONFIGURATION WARNING AND ENGINE CAUTION CAME ON. ALSO, CIRCUIT BREAKER D-24 POPPED OUT. TAKEOFF ABORTED. REPLACED AUTOFEATHER UNIT ON NR 2 ENGINE. (M) 2H72 4T RTA53EU 20050511001412005051100141EA 2005 5 11 A6WA200540151 120050409A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA LT WING CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31417AW 7610 LEFT LOWER WING PLANK IS CORRODED UNDER PANEL 550AB, OUTBOARD EDGE 1 INCH LONG BY .100 WIDE BY .002 DEEP. (M) 2L72 4F RTA21EA 20050511001432005051100143EU 2005 5 11 YENA200528 120050416A5210FE240004 ACTUATOR AIRBUS320 A320232 3930326EU L2 DOOR LEAKING A YENAK NONE O OTHER ININSP/MAINT 1 EA15590JB3615 2231 L2 DOOR ASSIST DAMPER CYLINDER LEAKING. REPLACED L2 DOOR ASSIST ACTUATOR PER AMM 52-13-14-04. NO LEAKS NOTED. 2L72 4F RTA28NM 20050511001442005051100144EU 2005 5 11 MALA050375 120050420A3350330151 POWER SUPPLY SAAB SF340 340B 7860101EU CABIN FAILED A MALAK NONE O OTHER ININSP/MAINT 1 GL15456XJ 340B456 EMERGENCY LIGHT POWER SUPPLY FAILED CAPACITY CHECK. P/N 3301-51, S/N 2102. REPLACED BATTERY AND PASSED. 2L72 4T RTA52EU 20050511001452005051100145EU 2005 5 11 MALA050376 120050419A5347 SEAT TRACK BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15503XJ E2310 DURING C2 INSPECTION, FOUND SEAT RAIL BETWEEN FRAMES 18 & 19 AT LBL 39 CORRODED. 2H74 4F RTA49EU 20050511001472005051100147NE 2005 5 11 MALA050378 220050421A7220 PANEL BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE NR 1 & 2 ENGINE WORN A MALAK NONE O OTHER ININSP/MAINT 1 GL15503XJ E2310 DURING A8 INSPECTION, FOUND FASTENER HOLES IN THE NR 1 & NR 2 ENGINE ATTENUATOR PANELS TO BE WORN THROUGH. ONE ON EACH ENGINE PANEL. 2H74 4F4 FRTA49EU E6NE 20050511001492005051100149EA 2005 5 11 VTZA200500065 120050420A78304EN886 POSITION SWITCH CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER FAULTY A VTZAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 EA27665BR 7534 LEFT THRUST REVERSER ICON CAME ON DURING T/O. PERFORMED CHECK OF THROTTLE QUAD AND ARM / OFF SWITCH, THROTTLE QUAD MICRO SWITCH TEST, AND RELAY / WIRE CHECK. REMOVED AND REPLACED STOW MICRO SWITCH REF AMM 78-37-01. COMPLIED WITH RIGGING OF THE THRUST REVERSER STOW MICRO SWITCH IAW TASK 78-37-01-830-801. PERFORMED THRUST REVERSER OPS CHECK IAW 71-00-00, NO DEFECTS NOTED AT THIS TIME. 2L72 4F RTA21EA 20050511001512005051100151SO 2005 5 11 C2XA05IA059 120050420A3350AD20131A BATTERY PACK EMB 145 EMB145XR 3260214SO CABIN DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2717159281 281 145792 IAH - FLIGHT 2039, DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20050511001522005051100152EA 2005 5 11 SWIA200514891 120050406A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07465SW 7845 MAIN FUSELAGE FLOORBEAM AT LBL 9.0 OUTBOARD ATTACH ANGLE AT FS 280 IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-21-11, 51-25-16, 51-23-00. 2L72 4F RTA21EA 20050511001532005051100153EA 2005 5 11 SWIA200514892 120050406A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07465SW MAIN FUSELAGE FLOORBEAM AT RBL 9.0 O/B ATTACH ANGLE AT FS 280 IS CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-21-11, 51-25-16, 51-23-00. 2L72 4F RTA21EA 20050511001552005051100155EA 2005 5 11 SWIA200514893 120050406A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07465SW 7845 FS 621 FLOOR SUPPORT ANGLE RBL 41 IS CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FLOOR SUPPORT ANGLE AS PER IAW CRJ REO 601R-53-61-117 REV. B. 2L72 4F RTA21EA 20050511001582005051100158EA 2005 5 11 SWIA200514894 120050406A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07465SW 7845 FS 621 LBL 41 FLOORBEAM ANGLE IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FLOOR SUPPORT ANGLE AS PER IAW CRJ REO 601R-53-61-117 REV B. 2L72 4F RTA21EA 20050511001592005051100159EA 2005 5 11 SWIA200514895 120050406A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07465SW 7845 CRACKED CLIP AT STA 625.00 STR 14R, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FLOOR SUPPORT ANGLE AS PER IAW CRJ REO 601R-53-61-117 REV B. 2L72 4F RTA21EA 20050511001602005051100160EA 2005 5 11 SWIA200514896 120050414A3350 RETAINER CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07718SK 10184 LOWER RIGHT EMERGENCY LIGHT BY SERVICE DOOR HAS BROKEN LAMP RETAINER. REPLACED LIGHT FIXTURE EMERGENCY LIGHT BY SERVICE DOOR AS NEEDED PER CRJ 700 MM 33-51-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050511001612005051100161SO 2005 5 11 SWIA200514897 120050420A3397 WIRE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07197SW 120186 EMERGENCY LIGHTING STRIP BY GALLEY IS LOOSE AND DOES NOT LIGHT UP. REPAIRED BROKEN WIRE UNDER GALLEY AND REPLACED FORWARD SECTION OF LIGHT TRACK. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050511001622005051100162EA 2005 5 11 SWIA200514898 120050417A274070609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07957SW 7829 MDC REPORTS HSTCU HAS POSITION FAIL AND ADC MACH NUMBER FAIL. REPLACED HSTCU WITH SERVICEABLE UNIT. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050511001632005051100163SO 2005 5 11 SWIA200514899 120050413A3350 LIGHT EMB 120 EMB120ER 3260203SO 9 BC BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07565SW 120340 RED EMERGENCY TRACK LIGHTING OUT AT 9B. RELAMPED RED LIGHT TRACK LIGHTING AT 9BC. 2L72 4T RTA31SO 20050511001762005051100176NM 2005 5 11 SWAA051161 120050419A3350101073 LENS BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29374SW 26582 LEFT OVERWING EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED LENS PER MM. 2L72 4F RTA16WE 20050506000552005050600055CE 2005 5 6 20030828 120050330A5311 FRAME BEECH 1900 1900D 1154162CE FUSELAGE CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03122UX UE122 DURING ROUTINE INSPECTION, A .55 INCH CRACK WAS FOUND ON THE INTERCOSTAL FRAME FLANGE AT FS 498.25 BELOW STRINGER 2L. CRACK WAS REPAIRED IAW WITH EO. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA24CE 20050506000592005050600059WP 2005 5 6 05FDEA00990 120050413A5341ARB7009 TEE FITTING DOUG DC10 DC1030F 3023504WP ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25301FE 46800 COMPLY WITH EA 8-5340-55468, FUSELAGE-CORROSION IN WING-TO-FUSE TEE ATTACH HOLE. CLOSING ACTION ON 04/12/05. ON N/R S00011. COMPLIED WITH EA8-5340-55468 2L73 4F RTA22WE 20050506000602005050600060WP 2005 5 6 05FDEA00991 120050413A5343ACA00071 BRACKET DOUG MD10 MD1010F 3022112WP ZONE 700 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25370FE 46608 COMPLY WITH EA8-5310-55469, FUSELAGE-MAIN FRAME-BRACKET ASSY NOSE RETRACT CHAFE REPAIR (P/NACA0007-1). CLOSING ACTION ON 04/12/05. ON N/R S00011. COMPLIED WITH EA8-5310-55469. 2L73 4F RTA22WE 20050506000612005050600061WP 2005 5 6 05FDEA00992 120050413A5753ARC19842 FITTING DOUG MD10 MD1010F 3022112WP ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25370FE 46608 COMPLY WITH EA8-5750-55470, WINGS-RT OUTBD FLAP INBD HINGE LUG CORROSION REPAIR P/N ARC1984. CLOSING ACTION ON 04/12/05. ON N/RS00012. COMPLIED WITH EA 8-5750-55470. 2L73 4F RTA22WE 20050506000622005050600062WP 2005 5 6 UPS05844266 120050317A5312 BULKHEAD DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE: C2, FWD ACCESSORY COMPT FS 683 BULKHEAD CRACKED .5 INCH LONG AT LOWER END OF VERTICAL STIFFENER LBL 18. REPAIRED FS 683 BULKHEAD IAW DC-8 SRM 53-2-5 FIG 13, 51-1-21, AND 51-1-20D. 2L74 4F RT4A25 20050506000632005050600063WP 2005 5 6 UPS05844267 120050325A5713 STRINGER DOUG DC8 DC873F 302199FWP WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 C2 FOUND STRINGER CRACKED INSIDE FUEL PANEL 506B NR 2 MAIN STRINGER 71. REMOVED CRACKED SECTION OF STRINGER; FABRICATED AND INSTALLED REPLACEMENT SECTION OF STRINGER IAW DC-8 SRM 57-2-2 FIG 3D AND E AND 51-1-20D. 2L74 4F RT4A25 20050506000782005050600078EA 2005 5 6 SWIA200514868 120050412A5610 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAO OTHER O OTHER DEDESCENT 1 NM07460SW 7803 DURING DESCENT, FO'S SIDE WINDOW CRACKED. REPLACED FO'S SIDE WINDOW IAW AMM 56-12-01. OPERATIONAL CHECK GOOD, P/N: NP-139322-10 S/N OFF: 03051H6864 2L72 4F RTA21EA 20050506000912005050600091 2005 5 6 HNA0500039 420050415A3442 ANTENNA DHAV DHC8 DHC8102 2809003NM WX RADAR SYS FAILED A HNAAO OTHER O OTHER NRNOT REPORTED 1 EA07933HA 134 RADAR ANTENNA FAULT. REMOVED AND REPLACED RADAR RT, OPS CHECK GOOD. 2H72 4T RTA13NM 20050506000952005050600095EA 2005 5 6 VTZA200500051 120050415A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27640BR 7340 RIGHT FS 718 FRAME CRACKED AT 1 INCH IN LENGTH IN RADIUS. 2L72 4F RTA21EA 20050506000972005050600097EA 2005 5 6 VTZA200500053 120050415A53116013600129 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27640BR 7340 LEFT FS 640 FRAME DOUBLER IS CRACKED IN RADIUS AT 1 INCH IN LENGTH. 2L72 4F RTA21EA 20050506001022005050600102NM 2005 5 6 05FDEA01018 120050415A2913 PUMP BOEING727 727227 1384078NM HYD SYSTEM MALFUNCTIONED A FDEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO25490FE 21493 TOTALLY LOST SYS A HYDRAULIC FLUID WHEN RAISING GEAR HANDLE ON DEPARTURE. SYSTEM A HYDRAULIC PUMPS RAN W/O FLUID. FLUID SHUTOFF SWITCHES OFF FOR APPROX 40 MIN HYDRAULIC LINE REPAIR AT RIGHT WHEEL WELL FAILED. MPN 65-17840-487 REPLACED NR 1 ENGINE HYDRAULIC PUMP IAW 727 AMM 29-11-033-4, AND REPLACED NR 1 AND NR 2 ENGINE CASE DRAIN FILTERS IAW 727 AMM 29-11-041-2. REMOVED AND REPLACED NR 2 A SYSTEM HYDRAULIC PUMP PER 29-11-033-4. FLUSH SYSTEM PER STEP 7 MM 29-11-000-2. RAN NR 1 AND NR2 ENG PER JRH TO BLEED HYD SYSTEM. SERVICED HYD SYS TO FULL PER 12-12-000-2. SYS OPS AND LEAK CHECKS, NO DEFECTS NOTED. OK FOR SERVICE. 2L73 4F A3WE 20050506001032005050600103NM 2005 5 6 05FDEA01019 120050415A5553651680222 ATTACH FITTING BOEING727 727200 138407ENM VERTICAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 CORROSION VERTICAL STAB TENSION TIE RT FWD FITTING IS CORRODED. REPAIRED PER EA 7-5530-86277. 2L73 4F RTA3WE 20050506001052005050600105NM 2005 5 6 05FDEA01021 120050415A29106517840487 LINE BOEING727 727200 138407ENM HYD SYSTEM LEAKING A FDEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO25490FE 21493 TOTALLY LOST SYS A-HYDRAULIC FLUID WHEN RAISING GEAR HANDLE ON DEPARTURE. SYSTEM A-HYDRAULIC PUMPS RAN W/O FLUID. FLUID SHUTOFF SWITCHES OFF FOR APPROX 40 MIN. HYDRAULIC LINE REPAIR AT RIGHT WHEEL WELL FAILED. 2L73 4F RTA3WE 20050506001082005050600108NM 2005 5 6 05FDEA01026 120050416A5753ARC7490501 VANE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 RT WING I/B FLAP VANE O/B T-FITTING FOUND CORRODED. RT WING I/B FLAP VANE O/B TEE FITTING REMOVED AND REPLACED AS PER CMM 57-52- 03, REFER WORK CARD E1-5750-7-5005 A2 PT 2. 2L73 4F RTA22WE 20050509000182005050900018NM 2005 5 9 CALA0500104 120050416A5315BAC1505100849 FLOORBEAM BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718612 27325 CABIN FLOORBEAM AT STA 986.5, LBL 43 IS CORRODED. REPAIRED BEAM PER ECRA 5310-04470. 2L72 4F RTA16WE 20050509000212005050900021NM 2005 5 9 RYNA200500013 120050408A7540LJ35801 TUBE BOEING757 75728A 1384976NM RROYCERB211 RB211535E4 54555NE NR 2 P1 PROBE CRACKED A RYNAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE07753NA 24544 30752 DURING CLIMB FROM ORD, THE NR 2 ENGINE N1 WAS INDICATING .16 LOWER THAN THE NR 1 ENGINE. THE AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED CRACKED TUBE OFF NR 2 ENGINE P1 PROBE. OPERATIONAL CHECK NORMAL. 2L72 4F4 FRTA2NM E12EU 20050509000272005050900027WP 2005 5 9 UPS05844283 120050401A5310 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 INSPECTION TYPE: C1, LONGERON CRACKED .25 INCH LONG AT STA 1726 L10 RT. REPAIRED LONGERON BY INSTALLING DOUBLER AND FILLER IAW SRM 53-02-02 FIG 11, 51-1-20, 51-3-0. 2L74 4F RT4A25 20050509000292005050900029WP 2005 5 9 UPS05844285 120050412A5321 FLOORBOARD DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 INSPECTION TYPE: C1, LOWER SURFACE OF CABIN FLOORBOARD CORRODED FROM STA 1555 TO 1563 & BL 0 TO RBL 9. BLENDED OUT OF LIMITS AND REPAIRED IAW SRM 53-02-03, 51-1-8, 51-1-21, 51-3-0 AND 51-1-15. 2L74 4F RT4A25 20050509000392005050900039WP 2005 5 9 MWEA050032 120050414A5330591143357 DOUBLER DOUG DC9 DC981 3022081WP FUSLEAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31813ME 48007 SKIN CRACKED APPROXIMATELY 1.5 INCHES, PROGRESSING FROM FORWARD TO AFT SIDE OF RIVET, STATION 1380 ABOUT 1 INCH ABOVE LONGERON 14. REPAIRED DOUBLER. 2L72 4F A6WE 20050509000512005050900051EA 2005 5 9 QXEA200500579 120050323A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - CENTER FUSERLAGE LOWER LEFT SIDE SKIN, STATION 517 TO 533 AND STRINGER 24 TO 26 PORT HAS FOUR NICKS. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01 AND SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050509000542005050900054EA 2005 5 9 QXEA200500577 120050323A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - CENTER FUSELAGE LEFT SIDE SKIN LOWER HAS SKIN NICKS AND STATION 501 BETWEEN STRINGER 22 AND 29 PORT. REPAIRED IAW CRJ700 SRM 51-21-00-001-001-A01 AND SRM 51-25-001-001-A01. 2L72 4F RTA21EA 20050509000552005050900055EA 2005 5 9 QXEA200500573 120050323A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FORWARD FUSELAGE LOWER SKIN FROM 319.7 TO 333.0 AND STRINGER 25 TO 27 PORT HAS THREE SMALL NICKS. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01 AND 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050509000572005050900057EA 2005 5 9 QXEA200500575 120050324A5344 HINGE CNDAIRCL600 CL6002C10 1390015EA ZONE 100 BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FORWARD FUSELAGE RIGHT SIDE SERVICE DOOR AT STATION 379.0 HAS UPPER HINGE BROKEN. REPLACED IAW SRM 51-41-00-001-001-A01. 2L72 4F RTA21EA 20050509000672005050900067NM 2005 5 9 AWXA200500461 120050404A5312651630087 FRAME BOEING737 737301 1384611NM BULKHEAD CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - DURING C-19 CHECK A .25 INCH CRACK WAS FOUND IN BS 178 BULKHEAD SIDE CHORD AT RBL 60, WL 207. MAINTENANCE REMOVED CRACKED SIDE CHORD AT BS 178 BULKHEAD, RBL 60, WL 207; FABRICATED A NEW REPLACEMENT CHORD PER DWG 65-16300; INSTALLED REPAIR PART IAW B7B-300 SRM 51-40-02. 2L72 4F RTA16WE 20050509000722005050900072EA 2005 5 9 QXEA200500686 120050417A284273811812 COMPUTER CNDAIRCL600 CL6002C10 1390015EA FUEL QTY MALFUNCTIONED A QXEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM09613QX5497 10045 BOI FLIGHT NR 4272 RETURNED TO FIELD: FUEL CHANNEL 1/2 FAIL CAUTION MESSAGE. MAINTENANCE REPLACED FQGC. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20050509000792005050900079EA 2005 5 9 QXEA200500586 120050317A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC FUSELAGE INTERIOR LEFT OUTBOARD SEAT RAIL AT STATION X795 HAS PITTING CORROSION ON INSIDE AND MOST INBOARD SURFACES. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01 AND REO 670-53-00-013. 2L72 4F RTA21EA 20050509000892005050900089NE 2005 5 9 UIEA200500046 220050404A7260 DRAIN MAST BOEING747 7472D3B 1384805NM GE CF6 CF650E2 30018NE NR 3 ENGINE DAMAGED A UIEAO OTHER O OTHER LDLANDING 1 EA15506MC 21252 A FIRM LANDING ON TOUCH DOWN, ON WALK AROUND, AFTER PARKING, NOTICED NR 3 ENGINE IAW MM. NO FURTHER DAMAGE NOTED. ALSO ALIGNMENT MARKS ON STRUT DOORS ARE ALIGNED AND NO DAMAGE TO CANOES OR TAIL SECTION OF AIRCRAFT FOUND. REPLACEMENT COWLS OR SLEEVES IS NOT NECESSARY. DAMAGED NR 3 DRAIN MAST TRANSFERRED TO DMI. 2L74 4F4 FRTA20WE E23EA 20050509000912005050900091NM 2005 5 9 UIEA200500047 120050404A2780BACR13CJ2 RELAY BOEING747 747228F 1384895NM GE CF6 CF650E2 30018NE LE FLAPS FAILED A UIEAO OTHER J WARNING INDICATION CLCLIMB 1 EA15809MC 20887 AFTER TAKE OFF, LEADING EDGE FLAPS NR 1 AND NR 3 WOULD NOT RETRACT. PRIMARY LEADING EDGE C/B OPEN. REPLACED R1102 RELAY IAW WDM 27-81-01. INSPECTED PDU`S DAMAGE, NONE FOUND. CLEANED ALL CONNECTORS AND RESEATED C/B. OPS CHECK CARRIED OUT SEVERAL TIMES IAW AMM. OPS CHECK GOOD. (K) 2L74 4F4 F A20WE E23EA 20050509000992005050900099EU 2005 5 9 USAA050241 120050205A5347F53312958201 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19671UW22760 0323 BFM - FOUND SEAT TRACK GOUGED .375 INCH BY .10 INCH BY .043 INCH DEEP, FRAME 47-48.5, -Y2462 MAIN CABIN FLOOR. SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-31-15 FIG 201 SHT 1. (M) 2L72 4F RTA46NM 20050509001032005050900103EU 2005 5 9 USAA050277 120050209A5321F5367112503400 FLOOR PANEL AIRBUS330 A330323 3930335EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19671UW22760 0323 BFM - FOUND FLOOR PANEL CRACKED 1 INCH, MAIN CABIN FLOOR PANEL 231BF, UNREPAIRABLE DAMAGE ON UPPER SURFACE. FABRICATED NEW FLOORBOARD PER SRM 53-02-00. (M) 2L72 4F RTA46NM 20050509001052005050900105EU 2005 5 9 USAA050242 120050204A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19671UW22760 0323 BFM - FOUND SEAT TRACK GOUGED 6 INCHES LONG BY 1.20 INCHES WIDE BY .032 INCH DEEP, FRAME 39.2, Y=-450. SPLICED NEW TRACK SECTION PER SRM 53-31-15 FIG 101 SHEET 8, FIG 201, SHEET 1. (M) 2L72 4F RTA46NM 20050509001112005050900111EU 2005 5 9 USAA050247 120050202A5347F5311351520000 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19671UW22760 0323 BFM - FOUND RAIL CORRODED 4 INCHES BY 2 INCHES BY .27 INCH DEEP, BETWEEN FRAME 13/14, -Y730, MAIN CABIN FLOOR. REMOVED AND REPLACED RAIL PER SRM 53-11-14 FIG 101. CORROSION LEVEL 2, TASK C531172-01. REMOVED AND REPLACED RAIL PER SRM 53-11-14 FIG 101. (M) 2L72 4F RTA46NM 20050509001142005050900114EU 2005 5 9 USAA050250 120050129A5347F5347821720000 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19671UW22760 0323 BFM - FOUND TRACK 1.5 INCH BY 1.2 INCH BY .025 INCH DEEP, FRAME 72, Y450, MAIN CABIN FLOOR SEAT TRACK. REMOVED AND REPLACED SEAT TRACK PER SRM 53-00-15. (M) 2L72 4F RTA46NM 20050509001702005050900170NM 2005 5 9 SWAA051145 120050417A5320146A7503 FLOOR SUPPORT BOEING737 7377H4 1384404NM AFT CARGO BAY CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29765SW 29805 DURING SCHEDULED 5Y CHECK, FOUND 2 EA LONGITUDINAL FLOORBEAM CRACKS AT BS 773, LBL 12 & RBL 3. REPAIRED BEAMS PER SRM. 2L72 4F RTA16WE 20050509001762005050900176SW 2005 5 9 ALG2005F00022 120050323A7603 THROTTLE BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL ENGINE MISUSED A ALGAD RETURN TO BLOCK WXJINADEQUATE Q C ENGINE FLAMEOUT WARNING INDICATION TXTAXI/GRND HDL 1 SO03117AL 2391 1ST START, STARTED ENG, BEGAN HYD CHK, COMPLETED HYDR CHECK, ENG FLAMED OUT. WENT THROUGH ENG SHUTDOWN PROCEDURES, NOTICED THROTTLE WAS NOT QUITE PASSED IDLE DETENT. DUE TO THIS FACT, ATTEMPTED A SECOND START, PRIOR TO ENG IDLE, ENG FLAMED OUT. MAINT DETERMINED PILOT WAS RUNNING AC BELOW FLIGHT IDLE DETENT. PULLED AIRFRAME FUEL FILTER, ENG FUEL PUMP FILTER, FUEL NOZZLE AND INSPECTED FUEL TANK, NO CONTAMINANTS FOUND. INSTALLED FUEL FILTERS AND REINSTALLED FUEL NOZZLE. COMPLIED WITH FUEL FLOW, RAPID DECAL CHK IAW MM. CHKED GOOD, COMPLIED WITH FUEL CONTROL RIG CHK, CHKED GOOD. PERFORMED NORMAL STARTS, AFTER FUEL SYS MAINT CHKS, ALL CHKS GOOD. PILOT PERFORM OPS CHK FLT, RETURNED AC TO SERVICE. (K) 1G71 3U3 U H2SW E4CE 20050509001782005050900178NM 2005 5 9 GAIA05019OP 120050404A33501000679 LIGHT BOEING727 7272J0 138407ENM PWA JT8 JT8D15 52051NE EMERGENCY EXIT ILLUMINATED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07284KH 21108 EMERGENCY EXIT DOOR LIGHT ON ALL THE TIME. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY. AIRCRAFT RETURNED TO SERVICE. (K) 2L73 4F4 FRTA3WE E2EA 20050510000022005051000002SO 2005 5 10 CHQA200500073 120050405A2120 ODOR EMB 135 EMB135KL 3260302SO CABIN DETECTED A CHQAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL11373SK 145543 C-CHECK TEST FLT, DURING ICE TEST, DETECTED A STRONG ODOR. MECH SAID ODOR ASSOCIATED WITH GREASE ON O-RINGS OF 14TH STAGE BLEED AIR VALVE. CREW RECEIVED NO INDS OTHER THAN ODOR, CONTINUED. AFTER T/O, AT 1,000 FT, RECEIVED A "LAV SMOKE" WARNING, ASSOCIATED WITH ODOR. MECH SENT TO LAV TO INVEST, INFORMED APPROACH OF IND OF SMOKE & WOULD RETURN, EMERGENCY NOT DECLARED. FOUND NO SMOKE OR FIRE IN LAV, BUT HAZE COULD BE SEEN. LEVELED OFF AT 3,000 FT & TURNED BACK , ODOR DISSIPATED & LAV SMOKE IND DID NOT RETURN AFTER RESETTING. RAN "LAV SMOKE" QRH, RAN ALL NORMAL CHKLISTS, & LANDED. NR 2 ENG SHUTDOWN. MX PERFORMED OPS TEST OF NR 2 ENG PNEU SYS, NO EVIDENCE OF SMOKE. CONDITION CAN'T BE DUPLICATED IAW MM. 2L72 4F RTT00011AT 20050510000072005051000007NM 2005 5 10 AWXA200500470 120050401A52406545871523 DOOR FRAME BOEING737 73733A 1384673NM R1 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 DURING C-19 CHECK A .375 INCH CRACK WAS FOUND ON R-1 DOOR AFT FRAME AT 4TH DOOR STOP FROM BOTTOM BS 344, STR 13 RT. MAINTENANCE TRIMMED OUT DAMAGE R-1 DOOR AFT FRAME AT 4TH DOOR STOP FROM BOTTOM BS 344, STR 13 RT; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW ER 03-5200-05103-ES3. 2L72 4F RTA16WE 20050510000092005051000009WP 2005 5 10 WX0500038 120050413A33501315 BULB DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A WX0AK NONE O OTHER ININSP/MAINT 1 WP19863GA 49911 DEN - MAINTENANCE REPORTED OVERHEAD EMERGENCY LIGHT AT ROW 17 INOPERATIVE. MAINTENANCE RELAMPED EMERGENCY LIGHT AT ROW 17. SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050510000262005051000026EA 2005 5 10 VTZA200500061 120050416A5210601R317725 DRAG ANGLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27658BR 7500 PASSENGER DOOR AFT DRAG ANGLE IS CRACKED 1.5 INCH. 2L72 4F RTA21EA 20050510000312005051000031EA 2005 5 10 VTZA200500056 120050416A531260034017595 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27640BR 7340 LEFT SIDE PILOTS BULKHEAD AT FS 280 LBL 9.0 IS CRACKED AT 1.0 INCH IN WEB RADIUS. 2L72 4F RTA21EA 20050510000322005051000032EA 2005 5 10 VTZA200500055 120050416A5210 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27640BR 7340 PASSENGER DOOR INTERCOSTAL TOP RADIUS CRACKED AT 1 INCH IN LENGTH AT DATUM 1 FS 338. 2L72 4F RTA21EA 20050510000432005051000043EU 2005 5 10 SA05039 120050412A5610NP1653116 WINDSHIELD AIRBUSA319 A319112 3930323EU COCKPIT CRACKED A USAAH DEACTIVATE SYST/CIRCUITS A FLAME/FIRE CRCRUISE 1 EA19758US12080 1348 PHL FLT 80 ENROUTE SAN - PHL, ABOUT AN HOUR AWAY FROM PHL, THE FIRST OFFICER'S WINDSHIELD BEGAN TO ARC, THEN CRACK. QRH PROCEDURES WERE FOLLOWED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FIRST OFFICER'S WINDSHIELD. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20050510000502005051000050 2005 5 10 2005UALA00326 420050408A256560461101 ASPIRATOR AIRCRUISERS BOEING757 757222 1384956NM PWA 2037 PW2037 NE SLIDE LEAKING A UALAK NONE O OTHER ININSP/MAINT 1 WP29537UA 0786 25157 ASPIRATOR FLAPPER VALVE LEAKS. LEAKAGE OF ASPIRATOR FLAPPER VALVE. ASPIRATOR WAS REPLACED. 2L72 4F4 FRTA2NM E17NE 20050510000512005051000051 2005 5 10 2005UALA00327 420050408A2565B14056015 O-RING AIRCRUISERS BOEING757 757222 1384956NM PWA 2037 PW2037 NE FILLER VALVE LEAKING A UALAK NONE O OTHER ININSP/MAINT 1 WP29587UA 0464 26713 LOW PRESSURE ON CYLINDER. O-RING LEAK AT FILLER VALVE FITTING. REPLACED O-RING. 2L72 4F4 FRTA2NM E17NE 20050510000632005051000063NM 2005 5 10 ASMF200504015 120050417A7931 ENGINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE RIGHT MALFUNCTIONED W ASMFC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW23169PL 53175 718246 AIRCRAFT REJECTED TAKEOFF AS A CONSEQUENCE OF DURING TAKEOFF AT 80 KNOTS, OIL PRESSURE REACHED 60 PSI ON RIGHT ENGINE. THE OIL PRESSURE RIGHT ENGINE WAS ADJUSTED IN 43 PSI IAW MM 79-20-03, TESTED CORRECT. 2L72 4F4 FRTA6WE E9NE 20050510001052005051000105SO 2005 5 10 BSYA200500008 120050420A3260 WARNING SYSTEM PIPER PA31 PA31350 7103110SO MLG MALFUNCTIONED E BSYAL ABORTED APPROACH P NO WARNING INDICATION APAPPROACH 1 GL07106TG 8052002 AIRCRAFT ON APPROACH INTO HFD DID NOT GET RIGHT GEAR DOWN AND LOCK INDICATION, NOTIFIED TOWER AND DID A GO AROUND, LANDED NO PROBLEMS. MAINTENANCE CLEANED AND LUBED DOWN AND LOCK SWITCH, OPS CHECKED GOOD. 1L72 3O A20SO 20050810001302005081000130WP 2005 8 10 IXXA05SMN112S 120050627A5730 SKIN DOUG DC8 DC871F 302199DWP LT WING IMPROPER B IXXAO OTHER O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING C CHECK INSPECTION, LT OTBD FLAP L/E UPPER PART NON STANDARD REPAIR, XF 415.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-1-0 PG 1, DC-8 SRM 57-7-1 FIG 4, TR # 57-94, EO SEMAN NR 2005857 DATE 06-18-05. REMOVED PLATING WITH IMPROPER REPAIR IAW DC-8 SRM 51-1-21 PG 1. FAB`D NEW PLATING (ALCLAD 2024 T3 0.032”) IAW DC-8 SRM 57-7-1 FIG. 4, TR 57-94 ITEM “P”. CLEANED, TREATED AND PRIMED AREA, NEW PLATING INTERNAL PART IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11 PAGE 9. INSTALLED NEW PLATING IAW DC-8 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050510001132005051000113EU 2005 5 10 DHL2005367504 120050413A5347TMS6022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01367DH 265 DURING C-CHECK, CABIN SEAT TRACK AT FS 18 THRU FS 21A AT BL 18L HAS CORROSION ( MKD). REPLACED SECTION OF SEAT TRACK FROM FR 19 TO FR 21A AT BL 18L P/N TMS 60-22457 ABOUT 40 INCH LONG AS PER A-300 51-10-40 PO NR 2113624, SPLICE ANGLES P/N TMS 60-3032 LOT NR 107828-1 PO NR 2981142-1, ALODINE AND PRIMED AS PER A-300 SRM 51-40-12 AND TOP COAT PAINT AS PER A-300 SRM 51-40-12. 2L72 4F RTA35EU 20050510001192005051000119EA 2005 5 10 MASA200500277 120050404A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07650ML 7137 CREW REPORTED OVERHEAD EMERGENCY FLOOD LIGHT AT ROW 5 INOP. PLACED OVERHEAD EMERGENCY FLOOD LIGHT AT ROW 5 ON MEL. MAINTENANCE REMOVED AND REPLACED THE LIGHT. 2L72 4F RTA21EA 20050510001212005051000121SO 2005 5 10 MASA200500282 120050405A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07857MJ 145765 LEFTHAND AFT EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED AND OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050510001252005051000125NM 2005 5 10 MASA200500290 120050408A3350 SIGN DHAV DHC8 DHC8202 2809007NM EMERGENCY EXIT DISLODGED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07987HA 425 THE FORWARD EMERGENCY EXIT LIGHT FELL FROM ITS MOUNT. MAINTENANCE RE-ATTACHED THE SIGN. 2H72 4T RTA13NM 20050510001322005051000132NM 2005 5 10 ABXA050092 120050415A3260 BUSHING BOEING767 767281 1385109NM MLG DIRTY A ABXAO OTHER O OTHER LDLANDING 1 GL23787AX 23020 WHEN LOWERED, THE GEAR HAD 3 GREEN LIGHTS WITH A GEAR DISAGREE LIGHT. LANDED WITH GEAR DISAGREE LIGHT, STAYED ON UNTIL PARKED. SWUNG GEAR AND VERIFIED GEAR DISAGREE LIGHT REMAINED ON WITH GEAR DOWN AND LOCKED. ISOLATED PROBLEM TO DIRTY GEAR LEVER BUSHING. CLEANED GEAR LEVER ROD OF OLD LUBE AND DIRT. BUSHING DID NOT REQUIRE LUBE. SWUNG GEAR AGAIN. PERFORMED SYSTEM TEST IAW B767 AMM 32-32-00. NO FAULTS NOTED. GEAR LEVER WORKED WITHOUT BINDING. 2L72 4F RTA1NM 20050510001362005051000136SO 2005 5 10 C2XA05BT021 120050417A3350 SIGN EMB 145 EMB145ER 3260211SO EMERGENCY EXIT MALFUNCTIONED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712946 145052 BTV - MX DURING CABIN INTERIOR CHECK EMERGENCY EXIT SIGN AT 12A INOP. PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHTING IAW EMB-145 MM 33-50-00. NO FAULT FOUND. 2L72 4F RTT00011AT 20050510001412005051000141SW 2005 5 10 RT62005F00001 120050412A5343206031301121S SUPPORT FITTING BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL MLG CRACKED E RT6AK NONE O OTHER ININSP/MAINT 1 NM03568TD 2976 REAR CROSSTUBE BOX-BEAM ASSEMBLY: LT FORWARD SUPPORT FITTING - 1 INCH VERTICAL CRACK. RT FORWARD SUPPORT FITTING - 1 INCH CRACK IN RADIUS. CRACKS FOUND DURING SCHEDULED INSPECTIONS. (NR2 OF 4) (K) 1G71 3U3 U H2SW E4CE 20050510001432005051000143EU 2005 5 10 MALA050310 120050331A3297 WIRE HARNESS BAC 146 AVRO146RJ85A1500097EU MLG UPLOCK DAMAGED A MALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL15509XJ E2321 LT MLG NOT SHOWING UP AND LOCKED AND THE INTRANSIT LIGHT ILLUMINATED AFTER DEPARTURE. AC AIR RETURNED TO MEM. REPLACED UPLOCK HARNESS FOR GEAR AND DOOR UPLOCKS. REPLACED UPLOCK RELAY GF5. ADJUSTED LT DOOR UPLOCK ROLLER. 2H74 4F RTA49EU 20050510001542005051000154EU 2005 5 10 MALA050323 120050410A7160NH24668165 DUCT SAAB SF340 340B 7860101EU RT INTAKE BURNED A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL15422XJ 340B422 A SMELL OF ELECTRICAL BURNING IN CABIN. CREW THINKS IT WAS COMING FROM HOT JUG. FA PULLED C/B FOR HOT JUG AND SMELL LESSENED. ON POST FLIGHT, CREW FOUND RT INTAKE DUCT WITH 3 BURNED SPOTS IN IT. REPLACED RT ENGINE LOWER DUCT. 2L72 4T RTA52EU 20050510001602005051000160 2005 5 10 MALA050308 420050327A3440 TRANSCEIVER BAC 146 AVRO146RJ85A1500097EU WX RADAR SYS MALFUNCTIONED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15525XJ E2350 WX RADAR FUZZY SCREEN AIR RETURN TO MEM. REMOVED AND REPLACED WX RT. 2H74 4F RTA49EU 20050510001622005051000162EU 2005 5 10 MALA050294 120050322A5320 FLOOR SUPPORT SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15415XJ 340B415 DURING 4K CHECK IN BNA FOUND FLOOR FLANGE IS CORRODED BETWEEN FS 272 AND 288 AT RBL 12. DAMAGE HAS BEEN REPAIRED IAW MESABA EO S53102. 2L72 4T RTA52EU 20050510001642005051000164EU 2005 5 10 MALA050297 120050322A5310 STRUCTURE SAAB SF340 340B 7860101EU LAV SERVICE PORTCORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15415XJ 340B415 DURING 4K CHECK IN BNA FOUND LAV SERVICING PORT P/N 7253680-117 HAS BEEN REPLACED DUE TO HEAVY CORROSION IAW SRM 51-40-22. 2L72 4T RTA52EU 20050510001662005051000166EU 2005 5 10 MALA050316 120050406A2610 WARNING LIGHT SAAB SF340 340B 7860101EU RT TAIL PIPE ILLUMINATED A MALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL15436XJ 340B436 RIGHT HAND TAIL PIPE HOT LIGHT ILLUMINATED ON TAKEOFF. ABORTED TAKEOFF AT 110 KNOTS. RETURNED TO THE GATE WITHOUT INCIDENTS. NO FURTHER INFO AVAILABLE. 2L72 4T RTA52EU 20050510001702005051000170SW 2005 5 10 RT62005F00003 120050412A5343206031301129S SUPPORT FITTING BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL MLG CRACKED E RT6AK NONE O OTHER ININSP/MAINT 1 NM03568TD8146 2976 REAR CROSSTUBE BOX-BEAM ASSEMBLY: LT FORWARD SUPPORT FITTING - 1 INCH VERTICAL CRACK. RT FORWARD SUPPORT FITTING - 1 INCH CRACK IN RADIUS. CRACKS FOUND DURING SCHEDULED INSPECTION. (NR4 OF 4) (K) 1G71 3U3 U H2SW E4CE 20050510001722005051000172NM 2005 5 10 AALA20050278 120050418A3220 LANDING GEAR BOEING757 757223 1384957NM NOSE MALFUNCTIONED A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21190AA 32384 AFTER TAKEOFF FROM TUL, NOSE LANDING GEAR FAILED TO RETRACT. INSPECTED NOSE LANDING GEAR WITH NO DEFECTS NOTED. CYCLED GEAR SEVERAL TIMES. COULD NOT DUPLICATE WRITE UP. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050510001832005051000183WP 2005 5 10 UPS05844299 120050324A53405652580N SUPPORT FITTING DOUG DC8 DC873F 302199FWP FUSLEAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE: C2, 62 COMPARTMENT FITTING FOR "POGO STICK" CRACKED AT FWD RT ATTACH BOLT STA 1875. REMOVED AND REPLACED FITTING FOR "POGO STICK" IAW DC-8 SRM 51-1-21, 51 -3-0, AND 51-3-2. 2L74 4F RT4A25 20050511000042005051100004SO 2005 5 11 SIMA200509402 120050331A532014521721009 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21643AE11958 145200 THE GALLEY FORWARD DIGITAL WAS FOUND CORRODED. REMOVED THE EXISTING FORWARD DIGITAL AND INSTALLED NEW DIGITAL IAW EMB 145 SRM, SRM EMB-145/1142 REV 28, CHAPTER 51-40-02. (M) 2L72 4T RTT00011AT 20050511000122005051100012SO 2005 5 11 SIMA200509802 120050405A27403622009015 ACTUATOR EMB 145 EMB145LR 3260212SO HORIZONTAL STAB INOPERATIVE A SIMAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SW21621AE 145105 FLT 4241 - ORD - RETURN TO FIELD FOR BACK UP PITCH TRIM FAIL. REPLACED HORIZONTAL STABILIZER ACTUATOR IAW EMB 145 AMM 27-40-02. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20050511000162005051100016SO 2005 5 11 SIMA200509804 120050331A531314533888001 STRINGER EMB 135 EMB135KL 3260302SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21803AE8212 145483 ABI - FOUND STRINGER 19R WAS FOUND CHAFED. BLENDED THE CHAFED AREA AND PERFORMED NDT. FABRICATED A REINFORCEMENT ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 28 CHAPTER 53-24-02. (M) 2L72 4F RTT00011AT 20050511000332005051100033 2005 5 11 SWIA200514877 420050417A22166225734002 SERVO EMB 120 EMB120ER 3260203SO RUDDER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07562SW1112311123 120336 RUDDER PEDALS BINDING ON FIRST FLIGHT TEST. REPLACED RUDDER SERVO IAW EMB MM 22-10-05. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050511000352005051100035EA 2005 5 11 SWIA200514879 120050417A274070609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07945SW 7770 NR 2 STAB CHANNEL WONT ENGAGE. REPLACED HSTCU AND MCU IAW 27-41-00 AND 27-41-01, OPERATIONAL CHECK GOOD, PN 7062-3 SN OFF 1027. 2L72 4F RTA21EA 20050511000432005051100043NM 2005 5 11 QXEA200500677 120050401A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09367PH 511 PDX - LEFTHAND INBOARD SEAT TRACK HAS CORROSION PIT AT STATION 312, INSIDE CHANNEL. REPAIRED IAW RD 8-53-4473, RD 8-53-1102 AND DHC-8 200 SRM 51-40-00, 51-40-11. 2H72 4T RTA13NM 20050511000532005051100053NM 2005 5 11 QXEA200500649 120050412A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - LEFT OUTBOARD SEAT TRACK NR 1 HAS CORROSION ON TOP OF LUGS AT X312. REPAIRED IAW RD 8-53-1342. 2H72 4T RTA13NM 20050511000612005051100061NM 2005 5 11 QXEA200500654 120050412A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - LEFT OUTBOARD SEAT TRACK NR 1 HAS CORROSION ON TOP OF LUGS AT X345. REPAIRED IAW RD 8-53-1342. 2H72 4T RTA13NM 20050511000622005051100062NM 2005 5 11 QXEA200500651 120050412A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - LEFT OUTBOARD SEAT TRACK NR 1 HAS CORROSION ON TOP OF LUGS AT X330. REPAIRED IAW RD 8-53-1342. 2H72 4T RTA13NM 20050511000672005051100067NM 2005 5 11 QXEA200500655 120050412A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - LEFT OUTBOARD SEAT TRACK NR 1 HAS DAMAGE ON TOP OF LUGS AT X376. REPAIRED IAW RD 8-53-1342. 2H72 4T RTA13NM 20050511000732005051100073NM 2005 5 11 XEA200500648 120050412A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - LEFT OUTBOARD SEAT TRACK NR 1 HAS CORROSION ON TOP OF LUGS AT X296. REPAIRED IAW RD 8-53-1342. 2H72 4T RTA13NM 20050511000822005051100082EU 2005 5 11 MALA050371 120050417A52607253710871 RAIL SAAB SF340 340B 7860101EU PAX DOOR CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15434XJ 340B434 PAX DOOR RAIL ASSY P/N 7253710871, IS CORRODED AND HAS BEEN REPLACED IAW SRM 51-40-21 AND SRM 51-40-22. 2L72 4T RTA52EU 20050511000992005051100099SO 2005 5 11 C2XA05IA058 120050418A335082321 CONNECTOR EMB 145 EMB145LR 3260212SO CABIN LOOSE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712540 145537 IAH - FLIGHT 2942, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE ROW TWELVE EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE RESECURED THE EMERGENCY LIGHT CONNECTOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050511001742005051100174NM 2005 5 11 SWAA051159 120050419A53126547978 PRESSURE PANEL BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29333SW 23697 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE BEADED WEB CRACKED AT BS 665.5, RBL 39.5. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050511001812005051100181NM 2005 5 11 SWAA051165 120050419A3350101073 LENS BOEING737 7373T5 1384608NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29694SW 23061 DURING SCHEDULED C4 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2L72 4F RTA16WE 20050511001832005051100183 2005 5 11 SWAA051166 420050419A2565D31354 SLIDE BOEING737 737317 138447PNM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050511001852005051100185NM 2005 5 11 SWAA051167 120050419A335090083 BATTERY PACK BOEING737 7377H4 1384404NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29759GS 30544 DURING SCHEDULED MV2 CHECK, FOUND FWD CABIN SECTION OF EMERGENCY EGRESS LIGHTS INOP. REMOVED AND REPLACED BATTERY PACKS PER MM. 2L72 4F RTA16WE 20050511001882005051100188SO 2005 5 11 CHQA200500087 120050425A2120 ODOR EMB 145 EMB145LR 3260212SO CABIN DETECTED A CHQAK NONE BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 GL11579RP 14500871 FLIGHT 6399 CMH-BDL - ON CLIMBOUT LAV SMOKE INDICATION ON EICAS. CREW REPORTED SMELLING SMOKE BUT SAW NO VISUAL SIGNS OF FIRE. THE AIRCRAFT RETURNED TO FIELD AND LANDED UNEVENTFULLY. MAINTENANCE PERFORMED ENGINE RUNS AND COULD NOT DUPLICATE LAV SMOKE. REMOVED AND REPLACED LAV SMOKE DETECTOR IAW EMB 145 AMM. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050511001902005051100190SO 2005 5 11 CHQA200500086 120050422A3350RPS1B BATTERY PACK EMB 135 EMB135KL 3260302SO CABIN DISCHARGED A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11379SK 145606 FORWARD EMERGENCY LIGHTING EGRESS LIGHT STRIPS AND RIGHT WING EGRESS LIGHT ARE INOP. REMOVED AND REPLACED THE NR 2 FORWARD GALLEY EMERGENCY LIGHT BATTERY PACK IAW EMB 140 AMM 33-50-04. OPS CHECK GOOD. 2L72 4F RTT00011AT 20050511001912005051100191NM 2005 5 11 SWAA051168 120050420A53116546594 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND 2 EA CRACKS AT FUSELAGE FRAME, BS 727, BETWEEN STR 14L & STR 16L. REPAIRED FRAME PER PAE ER. 2L72 4F RTA16WE 20050511001922005051100192NM 2005 5 11 SWAA051169 120050420A53306546880 SKIN BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND CORROSION ON FUSELAGE SKIN AT BS 1006, BETWEEN STR 2L & STR 3L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050511001932005051100193NM 2005 5 11 SWAA051170 120050420A33502TC65 CIRCUIT BREAKER BOEING737 7373H4 1384600NM COCKPIT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29324SW 23414 EMERGENCY LIGHT C/B BROKEN. REMOVED AND REPLACED C/B PER MM. 2L72 4F RTA16WE 20050511001952005051100195NM 2005 5 11 SWAA051172 120050420A3350PH22300L COVER BOEING737 7377H4 1384404NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29482WN 29852 DURING SCHEDULED HC1 CHECK, FOUND FWD END OF EEPLS COVER CRACKED. REMOVED AND REPLACED COVER PER MM. 2L72 4F RTA16WE 20050511001962005051100196NM 2005 5 11 SWAA051173 120050420A53116516301 FRAME BOEING737 7373L9 1384470NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT BS 188, LBL 29, WL 208. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050511001972005051100197NM 2005 5 11 SWAA051174 120050420A53126516300 BULKHEAD BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29679AA 23291 DURING SCHEDULED SPECIAL VISIT, FOUND 3 EA CRACKS AT BS 178 BULKHEAD WEB, RBL 9, RBL 10 & RBL 13, WL 234. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050511001982005051100198NM 2005 5 11 SWAA051175 120050420A53126516300 BULKHEAD BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29679AA 23291 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE BS 178 BULKHEAD WEB CRACKED AT LBL 5.5, WL 202. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050511001992005051100199NM 2005 5 11 05FDEA01050 120050419A3220 WARNING LIGHT BOEING727 7272S2F 1384O81NM MLG DOOR ILLUMINATED A FDEAO OTHER J WARNING INDICATION CLCLIMB 1 SO25215FE 22936 DOORS LIGHT ILLUMINATED AFTER RETRACTING LANDING GEAR WITH GEAR DOOR LIGHT ILLUMINATED ON S/O PANEL. 2L73 4F A3WE 20050511002002005051100200NM 2005 5 11 SWAA051176 120050420A53126516300 BULKHEAD BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29679AA 23291 DURING SCHEDULED SPECIAL VISIT, FOUND 2 EA CRACKS AT BS 178 BULKHEAD WEB, BETWEEN LBL 11 & LBL 13, WL 234. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050511002012005051100201NM 2005 5 11 05FDEA01051 120050419A3220 PIN BOEING727 7272S2F 1384O81NM NLG BROKEN A FDEAO OTHER E VIBRATION/BUFFET LDLANDING 1 SO25215FE 22936 UPON LANDING MEM, EXPERIENCED SEVERE VIBRATION IN NOSE GEAR DECELERATING THROUGH NINTY KNOTS. FOUND APEX PIN BROKE WITH LINKS APART. 2L73 4F A3WE 20050511002032005051100203NM 2005 5 11 SWAA051178 120050420A53306545777 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 969.5, STR 21L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050511002042005051100204NM 2005 5 11 05FDEA01058 120050421A5311 STRAP BOEING727 727233 138408ANM FRAME CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25254FE 20936 MAIN DECK CARGO, AT STA 1030 AND 1050 STR 6L, LINER FRAME ASSY HAS CHAFED INTO THE FRAME STRAP'S AND HARDWARE. GOUGE OUT OF LIMITS IAW BOEING SRM 53-10-1. REMOVED AND REPLACED STRAP IAW BOEING SRM 51-30-2. 2L73 4F RTA3WE 20050511002052005051100205NM 2005 5 11 05FDEA01059 120050421A5347FXSRM53102 SEAT TRACK BOEING727 727233 138408ANM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25254FE 20936 SEAT TRACK, STA 344, LBL 24 HAS EXISTING BLEND REPAIRS AND REQUIRES REPLACEMENT PER 7-5340-7-5002. REMOVED SEAT TRACK STA 344 - 480 IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK PER TRAVELER NRT5/510064, BATCH NR 888841, P.O. NR MST0017183. LOCATED AND DRILLED NEW SEAT TRACK IAW SRM 51-10-4. INSTALLED NEW SEAT TRACK IAW SRM 51-30-2. 2L73 4F RTA3WE 20050511002062005051100206NM 2005 5 11 NACA20050012 120050423A7830 LINKAGE BOEING727 72722C 138400FNM PWA JT8 JT8D7B 52053NE THRUST REVERSER LOOSE A NACAE ENGINE SHUTDOWN O OTHER TXTAXI/GRND HDL 1 AL03792A 4294475 19195 654518 NR 2 ENGINE WENT TO FULL POWER UPON TAXI-OUT. SECURED ENGINE AND RETURNED TO RAMP. FOUND THRUST REVERSER LINKAGE LOOSE, (NUT MISSING AT AFT END), AT CROSSOVER TUBE ON RIGHT SIDE OF ENGINE. SECURED LEVER ROD END WITH NEW HARDWARE (NO RIGGING CHANGE). CHECKED THROTTLE FOR PROPER TRAVEL AND MOVEMENT, ALL INDICATIONS NORMAL. 2L73 4F4 F A3WE E2EA 20050511002072005051100207NM 2005 5 11 05FDEA01060 120050421A5347FX5340750020 SEAT TRACK BOEING727 727233 138408ANM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25254FE 20936 SEAT TRACK, STA 344 - 480 HAS EXISTING BLEND REPAIRS AND REQUIRES REPLACEMENT PER 7-5340-7-5002, LBL 45. REMOVED SEAT TRACK STA 344 - 480 LBL 45 IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK PER TRAVELER NR T5/510063, BATCH NR 888841, PO NR MST0017183. LOCATED AND DRILLED SEAT TRACK IAW SRM 51-10-4 AND 51-30-8. INSTALLED NEW SEAT TRACK IAW SRM 51-30-2. 2L73 4F RTA3WE 20050511002092005051100209NM 2005 5 11 EIA2005002 120050106A5720 WEB BOEING747 747212B 1384886NM LT WING CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 LEFT WING AFT SPAR AREA SUPPORT STRUCTURE WEB IS CRACKED AT WBL 285 AT LANDING GEAR BEAM. PERFORMED TYPICAL WEB REPAIR PER B747 SRM 51-40-02 PG 1-5 STEP 1-10. 2L74 4F A20WE 20050511002102005051100210NM 2005 5 11 DHL2005783500 120050405A5520 CLIP BOEING727 727227 1384078NM RT ELEVATOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01783DH 21999 RT ELEVATOR T/E UPPER AND LWR ADJOINING CLIPS CRACKED AT ELEV STA 116. REMOVED CLIP IAW B727 SRM 51-30-2. FABRICATED CLIPS USING 2024T3 032 PO NR 9002034 DIM 3 INCH BY 3/4 INCH IAW B727 SRM 55-20-2 FIG 1. ALODINE AND PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED NEW CLIP IAW B727 SRM 51-30-2 AND 55-20-2 FIG 1. 2L73 4F A3WE 20050511002112005051100211NM 2005 5 11 DHL2005783501 120050405A5542 SKIN BOEING727 727227 1384078NM LT RUDDER DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01783DH 21999 LWR LT RUDDER DENTED MARKED. CUT OUT DAMAGE AREA 3/4 INCH DIA IAW B727 SRM 55-20-3 FIG 1. FAB'D DOUBLER REPAIR FROM MAT 2024-T3 .032 PO NR 9022034 DIM 5 INCH BY 3 INCH IAW B727 SRM 55-20-3 FIG 1. ALODINE AND PRIMED DOUBLER REPAIR IAW B727 SRM 51-10-2 AND INSTALLED DOUBLER REPAIR IAW B727 SRM 55-20-3 FIG 1 AND 51-30-2. 2L73 4F A3WE 20050511002132005051100213 2005 5 11 TSAA0527019 420050420A3418 SENSOR BOEING737 7372X6C 1384552NM AOA SYSTEM FAILED A TSAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP13816AL2795 23122 NON-ETOPS CARGO FLIGHT 913, HNL-LIH: AFTER TAKEOFF, THE STICK-SHAKER ENGAGED AND REMAINED ON UNTIL LANDING. RETURNED TO HNL. REMOVED AND REPLACED AOA SENSOR VANE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA16WE 20050511002142005051100214NM 2005 5 11 EIA2005005 120050218A5314 KEELBEAM BOEING747 747212B 1384886NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 CORROSION FOUND AT KEEL BEAM BS 1250 LBL 10. CORROSION REMOVED PER SRM 51-10-02, FABBED DOUBLER PER 747 SRM 53-10-9 FIG 2 AND INSTALLED. ALODINED, PRIMED AND PAINTED PER 747 SRM 51-10-06. HFEC INSPECTION ON ALL OPEN HOLES PER 747 NDR PART 6 CHAPTER 51-00-11 FIG 16. 2L74 4F A20WE 20050511002152005051100215NM 2005 5 11 EIA2005007 120050221A5313 STRINGER BOEING747 747273C 1384896NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09471EV 20651 STR 22L CRACKED AT STA 303 UNDERNEATH STRINGER. REPAIRED CRACKED STRINGER AT 22L, STA 303 PER ECRA 471-53-248-2. 2L74 4F A20WE 20050511002182005051100218NM 2005 5 11 DHL2005783504 120050405A5542 SKIN BOEING727 727227 1384078NM RUDDER DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01783DH 21999 DENT ON RT UPPER RUDDER FS 1540 MARKED. CUT OUT DAMAGE AREA 0.750 INCH DIA IAW B727 SRM 55-20-3 FIG 1. FAB'D DOUBLER REPAIR FROM MAT 2024-T3 .032 PO NR 9002034 DIM 5 INCH BY 3 1/4 INCH IAW B727 SRM 55-20-3 FIG 1. ALODINED AND PRIMED DOUBLER REPAIR IAW B727 SRM 51-10-2 AND INSTALLED DOUBLER REPAIR IAW B727 SRM 55-20-3 FIG 1 AND 51-30-2. 2L73 4F A3WE 20050511002192005051100219NM 2005 5 11 DHL2005783505 120050403A5744 SUPPORT BOEING727 727227 1384078NM FLAP ACTUATOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01783DH 21999 NR 6 LEADING EDGE FLAP ACTUATOR SUPPORT IS CRACKED AT INBD LWR CORNER WING STA 304. REMOVED NR 6 L/E FLAP ACT I/B SUPPORT IAW 727 SRM 51-30-2. FABBED NEW FROM 7075 T6 .063 PO NR 9001660 DIM 7 1/2 INCH BY 3 !/2 INCH IAW 727 SRM 57-10-25 FIG 3. SUPPORT TREATED AND PRIMED IAW 727 SRM 57-10-2 FIG 3. SUPPORT TREATED AND PRIMED IAW 727 SRM 51-10-2 AND INSTALLED IAW 727 SRM 51-30-2. 2L73 4F A3WE 20050511002202005051100220NM 2005 5 11 EIA2005069 120050330A5340 SHEAR TIE BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 M/D BS 2120 FRAME AT S-21R ATTACH SHEAR TIE FOUND CRACKED. SHEAR TIE REPLACED PER SRM 51-10-01. 2L74 4F A20WE 20050511002222005051100222NM 2005 5 11 L0FR200500004 120050422A3246260356116 WHEEL BOEING747 747200 1384847NM MLG CRACKED B Q2SAK NONE O OTHER ININSP/MAINT 1 AL03 INBOARD WHEEL HALF CRACKED AT TORQUE LUG KEY BOSS. 2L74 4F RTA20WE 20050511002272005051100227NM 2005 5 11 EIA2005073 120050330A5311 FRAME BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 M/D BS 260 S-23R LOWER FRAME CRACKED. FRAME REPAIRED PER SRM 53-10-04 FIG 4. 2L74 4F A20WE 20050511002292005051100229CE 2005 5 11 4510104102005 120050410A2910 LINE LEAR 45 45LEAR 5170805CE ALIDSGTPE331TPE331201A 0517 WP HYD SYS LEAKING E J7SAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SW05410FX 101 P116192 THE PILOT REPORTED HE WAS ABOUT 3 TO 4 MILES OUT WHEN FIRE INDICATION APPEARED. DIDN'T DISCHARGE A BOTTLE OR SHUTDOWN THE ENGINE. AFTER CLEARING THE RUNWAY, THE INDICATION EXTINGUISHED ABOUT 1 MINUTE AFTER THE ENGINE WAS SHUTDOWN. AFTER DEPLANING THEY SAW HYD FLUID DRIPPING FROM THE COWLING. DIDN'T GET A HYD PUMP FAILURE INDICATION, BUT HE DID GET A HYD LOW CAS SHORTLY AFTER LANDING. MAINTENANCE FOUND THE ALTERNATOR WIRING HARNESS HAD CHAFED A PINPOINT HOLE IN THE EDP HYD PRESSURE LINE. THIS CAUSED A HIGH PRESSURE MIST OF 5606 TO SPRAY ON HARNESS. SPRAY IGNITED, MELTING THE HARNESS AND CLAMPS IN THE IMMEDIATE AREA. LOANER ENGINE INSTALLED ON AIRCRAFT. MFG IS DEVELOPING A SERVICE BULLETIN TO ADD CLAMPS 2L72 4F3 TRTT00008WIAEXJ STC 20050511002302005051100230NM 2005 5 11 EIA2005075 120050330A5311 FRAME BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 M/D BS 340 FRAME CRACKED AT STRINGER S15R CUTOUT. FRAME REPAIRED PER SRM 51-40-03 FIG 1 AT M/D BS 340 RT FRAME STRINGER 15R. 2L74 4F A20WE 20050511002312005051100231NM 2005 5 11 EIA2005076 120050331A2520 PANEL BOEING747 747212B 1384886NM CABIN CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 CABIN LT PAX NR 4 DOOR FWD CUTOUT AT STR 18L AREA CUTOUT PANEL FOUND CRACKED. PANEL REPAIRED PER SRM 51-40-02 FIG 1. 2L74 4F A20WE 20050511002342005051100234NM 2005 5 11 EIA2005079 120050331A5311 FRAME BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 M/D BS 320 S15L FRAME CRACKED AT STRINGER CUTOUT. FRAME REPAIRED PER SRM 51-40-03 FIG 1. 2L74 4F A20WE 20050511002392005051100239NM 2005 5 11 EIA2005084 120050401A5320 TIE CLIP BOEING747 747212B 1384886NM FUSELAGE BROKEN A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 COCKPIT LEFT FRAME TIE CLIP BROKEN AT BS 420 S7L. TIE CLIP REPLACED PER SRM 51-30-02 AND 51-10-01. 2L74 4F A20WE 20050511002402005051100240NM 2005 5 11 EIA2005085 120050401A5320 TIE CLIP BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 U/D BS 500 S10R TIE CLIP FOUND CRACKED. TIE CLIP REPLACED PER SRM 51-10-01. 2L74 4F A20WE 20050511002432005051100243WP 2005 5 11 ASMF200504016 120050419A7931 TRANSMITTER DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE OIL PRESSURE DIRTY W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23214AM 49585 725605 AIRCRAFT RETURNED TO PLATFORM. DURING PUSH BACK, LT ENGINE STARTED NORMALLY AND AFTER RT ENGINE STARTED, THE LT ENGINE PRESSURE DECREASE TO 35 PSI’S. DURING REVISION WAS DETECTED OVERFILL OIL. THE EXCESS OIL WAS DRAINED AND PRESS OIL TRANSMITTER CONNECTOR WAS CLEANED. THE LT ENGINE WAS TESTED AND THE PRESSURE WAS STABILIZED AT 40 PSI’S WITH LIGHT TURNED ON AND LT GENERATOR WITH LOW FREQUENCY AND VOLTAGE WITH FLUCTUATIONS IN LT BAR, ACCELERATED TO 1.65 AT EPR AND VOLTAGE AND FREQUENCY STABILIZED WITH OIL PRESSURE ON 42 PSI. DURING OVERNIGHT SERVICE THE LT ENGINE OIL PRESSURE WAS ADJUSTED IAW MM AND OPERATIONAL TEST WAS PERFORMED IAW MM , ALL CORRECT. 2L72 4F4 FRTA6WE E9NE 20050511002442005051100244NE 2005 5 11 ASMF200504017 220050421A7200 ENGINE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE RIGHT DAMAGED W ASMFA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW23838AM3280415433 49397 718220 AIRCRAFT RETURN OF FLIGHT, RT ENGINE FIRE DETECTOR LIGHT TURNED ON AND IT TURNED OFF WHEN ENGINE WAS DECELERATED. DURING CHECK LOOPS WERE DETECTED GROUNDED, BOROSCOPIC INSP WAS PERFORMED TO RT ENGINE DETECTING 13TH STAGE BLEED DUCT DAMAGED. RT ENGINE MANIFOLD WAS REPLACED IAW MM AND A AND B LOOPS WERE ISOLATED AND TESTED IAW MM. AIRCRAFT WAS SENT TO MAIN BASE AND DURING OVERNIGHT DETAILED INSPECTION, IT WAS DETECTED NOISE SUPPRESSOR PANEL WITH DAMAGES. IN ORDER AVOID MORE DAMAGES TO SUCH ENGINE, IT WAS REPLACED IAW MM, TESTED CORRECT IAW MM. 2L72 4F4 FRTA6WE E9NE 20050511002452005051100245NM 2005 5 11 DHL2005783502 120050405A5520 CLIP BOEING727 727227 1384078NM RT ELEVATOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01783DH 21999 RT ELEV T/E UPPER AND LWR ADJOINING CLIPS CRACKED AT ELEV STA 106. REMOVED CLIP IAW B727 SRM 51-30-2. FABRICATED CLIPS USING 2024T3 .032 PO NR 2034 DIM 3 INCH BY 3/4 INCH IAW B727 SRM 55-220-2 FIG 1. ALODINE AND PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED CLIP IAW B727 SRM 51-30-2 AND 55-20-2 FIG 1. 2L73 4F A3WE 20050511002462005051100246NM 2005 5 11 DHL2005783506 120050403A5753 SKIN BOEING727 727227 1384078NM LT TE FLAP DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01783DH 21999 LT OB AFT FLAP LOWER SURFACE, WBL 432 HAS A LARGE SMOOTH DENT. CUT OUT DAMAGED AREA APPROX 3 INCH DIAM L/W O/B FLAP LOWER SKIN IAW B727 SRM 51-40-20 FIG 31. FABRICATED ONE FILLER APPROX 3 INCH ROUND AND ONE DOUBLER APPROX 6 INCH ROUND USING 2024T3 .016 PO NR 9001660 IAW B727 SRM 57-50-2 FIG 4. CLEANED, PREPPED, APPLIED ADHESIVE PRIMER AND ADHESIVE TO ALL SURFACES AND BAGGED IAW B727 SRM 51-40-20 FIG 31. CURED REPAIR, CLEANED AND PERFORMED POST BOND INSPECTION WITH NO DELAM. NOTED IAW B727 SRM 51-40-20 PARA 0. TREATED, PRIMED, AND SEALED REPAIR IAW B727 SRM 51-40-20 PARA P. 2L73 4F A3WE 20050511002472005051100247NM 2005 5 11 DHL2005783507 120050404A5330 SKIN BOEING727 727227 1384078NM FUSELAGE BULGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01783DH 21999 BS 675 STR 28R, FUSELAGE SKIN HAS BULGED SKIN WITH POPPED FASTENERS. CUT OUT CORRODED STRINGER SECTION (DIM. 5") FROM 28R STA 675 TO 680. CUT OFF CORRODED SHEAR TIE (DIM. 6") AT STA 680 BETWEEN S28R AND S27R IAW B727 SRM 53-10-3 FIG 1 AND 53-10-4 FIG 15. FABBED STRINGER REPAIR SPLICE FROM BAC1498-132 EXTRUSION PO NR 4246286 (DIM.19 1/2"). FABBED SHEAR TIE REPAIR FROM .063 7075T6 PO NR 900489 (DIM.6"X 3/4"X 1") IAW B727 SRM 53-10-4 FIG 15. TREATED AND PRIMED REPAIR PARTS IAW B727 SRM 51-10-2. INSTALLED REPAIRS IAW B727 SRM 53-10-3 FIG 1, 53-10-4 FIG 15, AND 51-30-2. 2L73 4F A3WE 20050511002482005051100248NM 2005 5 11 DHL2005783508 120050406A5230 SKIN BOEING727 727227 1384078NM CARGO DOOR DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01783DH 21999 C1 DOOR SKIN LOWER FORWARD CORNER DENTED. REMOVED AND REPLACED C1 DOOR LOWER FORWARD CORNER IAW 727 SRM 51-30-2, P/N 65-57146-4 PO NR 507979. 2L73 4F A3WE 20050511002492005051100249NM 2005 5 11 DHL2005783509 120050406A5230 SKIN BOEING727 727227 1384078NM CARGO DOOR DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01783DH 21999 C1 DOOR SKIN DENTED LOWER AFT CORNER. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 52-00-2 AND 53-30-1 FIG 1. CUT OUT DAMAGED AREA 5 INCH BY 3 1/8 INCH AND FABBED DOUBLER FROM 2024T3 PO NR 9001634 DIM. 10 1/4 INCH BY 8 1/2 INCH IAW SRM 52-00-3 FIG 3 AND 52-30-1 FIG 7. DOUBLER TREATED AND PRIMED IAW 727 SRM 51-10-2 AND INSTALLED IAW 727 SRM 52-00-3 FIG 3. 2L73 4F A3WE 20050511002502005051100250NM 2005 5 11 DHL2005783510 120050415A5754 SKIN BOEING727 727227 1384078NM NR 2 SLAT MISREPAIRED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01783DH 21999 ACCOMPLISH IDENTIFICATION OF EXISTING REPAIR ON NR 2 SLAT AT WS600 PER ASTAR JC FCD500001-018-B. PREVIOUS REPAIR FOUND TO BE NON-COMPLAINT IAW 727 SRM 57-50-3 FIG 1. FABRICATED DOUBLER USING 2024T3 .080 PO NR 9002012 DIM. 9 1/2" BY 7 3/4" IAW B727 SRM 57-50-3 FIG 1. ALODINE AND PRIMED PART IAW B727 SRM 51-10-2 INSTALLED DOUBLER IAW B727 SRM 57-50-3 FIG 1. 2L73 4F A3WE 20050511002512005051100251NM 2005 5 11 DHL2005783511 120050417A5330 SKIN BOEING727 727227 1384078NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01783DH 21999 FUSELAGE SKIN DENTED BS 1070 ABOVE STR 23 RT. DAMAGE FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-30-1 FIG 1. REMOVED FASTENERS AT STA 1070 STR 23R IAW SRM 51-30-2. CUT OUT DAMAGED AREA DIM 1.75 BY 3.75 AND FABRICATED DOUBLER REPAIR FROM MAT USED 2024T3 .071 PO NR 9002139 DIM. 12 X 8.250 AND FILLER FROM MAT. USED 2024T3 .063 PO NR 9001239 DIM. 1 X 1 INCH IAW SRM 53-30-3 FIG 3 AND 53-30-2 FIG 2. PARTS TREATED AND PRIMED IAW 727 SRM 51-10-2, INSTALLED REPAIR WASHER IAW 727 SRM 51-30-8, PARTS INSTALLED IAW 727 SRM 53-30-3 FIG.3. THIS REPAIR IS CAT. "A". 2L73 4F A3WE 20050511002522005051100252EU 2005 5 11 DHL2005367507 120050401A5347TMS6022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01367DH 265 DURING C-CHECK, MAIN DECK COURRIER AREA CORROSION UNDER SEAT TRACK RBL 3 FRAME 15 A -16 MKD. REMOVED AND REPLACED DAMAGED SECTION OF SEAT TRACK IN COURIER AREA FR 15 A - 16 RBL 3 IAW A-300 SRM 53-10-10 AND 51-30-30 MAT USED TMS 60-22457 3 FEET. PO NR 2113624. TREATED AND PAINTED IAW A-300 SRM 51-40-12. 2L72 4F RTA35EU 20050511002532005051100253EU 2005 5 11 SA05041 120050419A335032145410 POWER SUPPLY AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT DEFECTIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19748UW13921 1311 PIT - RECEIVED FAULT MESSAGE EPSU INT LOAD FWD L DURING THE TEST OF THE EMERGENCY LIGHTS SYSTEM. MAINTENANCE REPLACED THE FORWARD CABIN EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20050511002542005051100254EU 2005 5 11 DHL2005367508 120050401A5347TMS6022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01367DH 265 DURING C-CHECK, MAIN DECK COURIER AREA HEAVY CORROSION ON SEAT TRACK RBL 58 FRAME 15A TO 19. REMOVED DAMAGED SEAT TRACK ON RBL 58 FRAME 15A TO 19 AND INSTALL NEW SECTION IAW A-300 SRM 51-30-30. MATERIAL USED TAMS 60-22457 60" LONG P/O 2113624. 2L72 4F RTA35EU 20050511002552005051100255EU 2005 5 11 DHL2005367509 120050404A5720TMS6022457 FLOOR SUPPORT AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01367DH 265 DURING C-CHECK, CABIN FLOOR AT FR 14 BL 78R FLOOR SUPPORT BEAM HAS CORROSION ( MKD.) REMOVED CORROSION AT FR 14 BL 78R FLOOR SUPPORT IAW A-300 SRM 51-40-11. MAT LOSS .018 "OUT OF LIMITS" IAW SRM 53-10-00. INSTALLED NEW SEAT TRACK AT FR 14 RBL 78 IAW A-300 SRM 53-10-00 AND 51-30-30. MAT USED TMS 60-22457 20" LONG PO NR 2113624. TREATED AND PAINTED IAW A-300 SRM 51-40-12. 2L72 4F RTA35EU 20050511002582005051100258EU 2005 5 11 05FDEA01063 120050422A5311A5381171020500 FRAME AIRBUS310 A310 EU ZONE 700 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 CORROSION ON FRAME IN RT WHEEL WELL AFT OF FRAME 47 ON DIAGONAL FRAME. REMOVED CORROSION AND REPROTECTED SURFACE IAW A310-200 SRM 51-74-10 AND 51-23-10. MATERIAL LOSS WITHIN LIMITS PER FEDEX EA 6-5310-87818. 2L72 4F RTA35EU 20050511002592005051100259EU 2005 5 11 05FDEA01064 120050422A5754A57970650000B VANE AIRBUS310 A310 EU LE FLAPS CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 RIGHT FLAP VANE LEADING EDGE HAS 2 CHAFED AREAS. REMOVED RT WING FLAP VANE IAW A310-200 AMM 27-50-15-4. COMPLIED WITH EA 6-5750-87216. INSTALLED RT FLAP VANE IAW A310-200 AMM 27-50-15-4. OPS CHECKED GOOD IAW A310-200 AMM 27-54-00-5. 2L72 4F RTA35EU 20050511002602005051100260EU 2005 5 11 05FDEA01065 120050422A5730 PANEL AIRBUS310 A310 EU RT WING DAMAGED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25402FE 201 RT WING FAIRING 633BB 2 MOUNTED BRACKETS REQUIRES INSTALLATION. NOTE 7 EA HOLES IN WING PLANK ARE COUNTERSUNK. RT WING BRACKETS FOR FAIRING 633BB REAMED HOLES TO 2ND OVERSIZE, SEALED FITTINGS (2EA.). INSTALLED CONICAL WASHERS, AND FITTINGS IAW A310 SRM 51-40-44, SRM 51-71-70, SRM 51-40-21 AND FEDEX EA 6-5720-57820. 2L72 4F RTA35EU 20050815000292005081500029NM 2005 8 15 AWXA200500945 120050726A52306546921531 SKIN BOEING737 7373Y0 1384671NM CARGO DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28334AW 23747 DURING C16 CHECK DISCOVERED FORWARD CARGO DOOR, INNER WEB SKIN CRACKED, .34 INCHES IN LENGTH, AT LIGHTENING HOLE JUST AFT OF THE FORWARD UPPER ACCESS PANEL AT BS 460, STR 22R. MAINTENANCE ROUTED OUT CRACK AT LIGHTENING HOLE JUST AFT OF THE FORWARD UPPER ACCESS PANEL AT BS 460, STR 22R IAW BOEING 737-300 SRM 52-30-01-1 FIG 101. FABRICATED REPAIR DOUBLER IAW BOEING 737-300 SRM 51-70-13-0 FIG 1. INSTALLED FABRICATED REPAIR PARTS ON FORWARD CARGO DOOR, LIGHTENING HOLE JUST AFT OF THE FOWARD UPPER ACCESS PANEL AT BS 460, STR 22R IAW BOEING 737-300 SRM 51-70-13-0 FIG 1. 2L72 4F RTA16WE 20050815000562005081500056 2005 8 15 SWAA052366 420050808A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29327SW 23691 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050815000602005081500060NM 2005 8 15 SWAA052370 120050808A335020121 BATTERY BOEING737 7375H4 138449DNM FWD GALLEY INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29523SW 26565 DURING SCHEDULED SERVICE CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20050815000772005081500077NE 2005 8 15 SWAA052373 220050809A7261CFM567B ENGINE BOEING737 7377H4 1384404NM GE CFM56 CFM56* 13802NE RIGHT FAILED A SWAAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 SW29205WN 34010 892196 INFLIGHT SHUTDOWN/DECLARED EMERGENCY/DIVERSION, LOST NR 2 ENGINE OIL PRESSURE AND QUANTITY. REMOVED AND REPLACED NR 2 ENGINE PER MM. 2L72 4F4 FRTA16WE E2GL 20050815000892005081500089NM 2005 8 15 SWAA052385 120050810A53406551698 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29612SW 27930 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20050815000932005081500093NM 2005 8 15 SWAA052389 120050809A324626066712 WHEEL BOEING737 737317 138447PNM MLG SEPARATED A SWAAO OTHER O OTHER LDLANDING 1 SW29693SW 23174 NR 1 MAIN TIRE RETREAD SEPARATED. FOUND LT INBD T/E FOREFLAP AND GROUND SPOILER DAMAGED. REMOVED AND REPLACED NR 1 MAIN TIRE/WHEEL ASSY, LT INBD T/E FOREFLAP AND GROUND SPOILER PER MM. 2L72 4F RTA16WE 20050815000952005081500095NM 2005 8 15 SWAA052391 120050810A534065C27314 STRINGER CLIP BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29696SW 23064 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 639, STR 4L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050815000982005081500098EU 2005 8 15 05FDEA02420 120050811A5330 SKIN AIRBUS310 A310222 3930315EU FUSELAGE UNKNOWN A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25447FE 251 COMPLY WITH AGING 9-AGING-INSP REV NO. POS PT. INSPECTED IAW CFR 121.368. PREVIOUS REPAIR INSTALLED LEFT SIDE OF FUSELAGE AT FS 70 TO FS 71, STR 27LT TO 31LT. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. NEW REP ACCOMP PER SRM 53-10-12 FIG 225 SHEET 2. REP EVALUATED PER GMM 6-2-100 AND CLASSIFIED MAJOR. 2L72 4F RTA35EU 20050815000992005081500099NM 2005 8 15 05FDEA02427 120050811A5330 SKIN BOEING727 727227 1384078NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 PREVIOUS REPAIR STA 1114 TO 1138 STR 21R TO 22R HAS BEEN FOUND TO BE IAW EA 7-5330-52176 AND IS A MAJOR REPAIR. 2L73 4F A3WE 20050815001022005081500102NM 2005 8 15 05FDEA02432 120050811A5315 FLOORBEAM BOEING727 727227 1384078NM LWR CARGO BAY CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 PREVIOUS REPAIR AT STA 1050 FLOORBEAM AT BL 0 IS IAW SRZ 27-53-034E AND IS A MAJOR REPAIR. 2L73 4F A3WE 20050825000022005082500002 2005 8 25 SWAA052537 420050823A2565D31354 SLIDE BOEING737 7373Q8 1384670NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29317WN 24068 DURING SCHEDULED D-CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050815001212005081500121NM 2005 8 15 05FDEA02446 120050812A5320 VERTICAL BEAM BOEING727 727227 1384078NM UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 REPAIR ON VERTICAL BEAM AT STA 1183, RBL 36.83, WL 230, PREVIOUS REPAIR NEEDS ENG EVALUATION TO DETERMINE IF MAJOR OR MINOR AND IF REPAIR IS IAW FAA APPROVED DATA. NO ENGINEERING ASSISTANCE NEEDED. THIS IS A MODIFICATION COMPLIED WITH PER DRAWING 65C29080. THIS IS A MAJOR REPAIR/ MODIFICATION PER GMM 6-2-100. 2L73 4F A3WE 20050815001222005081500122WP 2005 8 15 05FDEA02447 120050812A5330 SKIN DOUG DC10 DC1010 3022110WP GE CF6 CF66K 30020NE ZONE 100 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25564FE 46984 FOUND REPAIR AT STA 1159 - 1139 LONGERON 41-48 RT. REPAIRED IAW FEDEX 8-5330-84091A. 2L73 4F4 F A22WE E23EA 20050815001252005081500125NM 2005 8 15 UPS05445166 120050726A5311 FRAME BOEING747 747121 1384871NM U/D CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 BS 560 STR 10AL-11L FRAME O/B FOUND CRACK FLANGE. CRACK LENGTH 2" CORROSION BLEND OUT N/A. BS 560 BETWEEN STR 10AL-11L FRAME REPAIRED AS PER HX RS R53-12-35352 AND UPS EO B747-5310-22634-A. 2L74 4F A20WE 20050815001392005081500139WP 2005 8 15 UPS05845145 120050712A534037558241 FITTING DOUG DC8 DC873F 302199FWP FS 360 L34R CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 A-PIT CENTER TORQUE BOX BATHTUB FITTING AT FS 360 BETWEEN TORQUE BOX FRAME AND LONGERON34R HAS CORROSION. REMOVED CORROSION FROM BATH TUB FITTING AT STA 360 LONG 34R AND FOUND OUT OF LIMITS IAW SRM 51-1-8. REPLACED BATHTUB FITTING AT STA 360, 34R IAW 53-02-00-0 FIG 002D. 2L74 4F RT4A25 20050815001552005081500155WP 2005 8 15 UPS05845181 120050709A5311 FRAME DOUG DC8 DC873F 302199FWP FS 55 L24L-L25L CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 CRACK IN FRAME 55 A/C COMPT BETWEEN L24L AND L25L. REMOVED CRACKED FRAME AT STA 55 L24L-L25L IAW SRM 51-3-0. FABRICATED REPAIR FRAME SECTION, REPAIR ANGLES, AND FILLER IAW SRM 53-03-03 FIG3 AND 53-2-0. INSTALLED FRAME SECTION AND REPAIR ANGLES AND FILLER AT STA 55 L24L-L25L IAW SRM 51-1-20D. 2L74 4F RT4A25 20050815001562005081500156WP 2005 8 15 UPS05845182 120050713A5320 PLATE DOUG DC8 DC873F 302199FWP CARGO BAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 MAIN CARGO DOOR LWR AFT CORNER, THE DOOR JAMB CORNER INTERNAL SUPPORT PLATE IS CRACKED. REMOVED FILLET IAW SRM 51-1-21. FABRICATED AND INSTALLED REPLACEMENT FILLET AT THE MAIN CARGO DOOR LWR AFT DOOR JAMB INTERNAL SUPPORT PLATE IAW DWG 5772786 AND SRM 51-3-0. 2L74 4F RT4A25 20050815001572005081500157WP 2005 8 15 UPS05845183 120050714A5330 SKIN DOUG DC8 DC873F 302199FWP FS -21 TO 70 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 REPLACE SKIN PANEL AT STA 70 TO -21.92 LONG 31R-L31L. REMOVED AND REPLACED FWD BELLY SKIN AT STA -21.92 TO STA LONG 31L TO LONG 31R IAW EO DC8-5330-8942-D. 2L74 4F RT4A25 20050815001712005081500171NM 2005 8 15 SWAA052397 120050811A3350101073 LENS BOEING737 7377H4 1384404NM CABIN DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29453WN 29847 CENTER CABIN EMERGENCY EXIT SIGN LENS FELL OFF. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20050815001732005081500173NM 2005 8 15 SWAA052399 120050811A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29612SW 27930 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050815001802005081500180NM 2005 8 15 SWAA052406 120050811A53106547979 CREASE BEAM BOEING737 7373H4 1384600NM CABIN FLOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29612SW 27930 DURING SCHEDULED D CHECK, FOUND FUSELAGE CREASE BEAM WEB CORRODED AT BS 837, LBL 70. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050815001912005081500191 2005 8 15 SWAA052417 420050810A256563551101 SLIDE BOEING737 7377H4 1384404NM L2 DOOR OUT OF LIMITS A SWAAK NONE O OTHER ININSP/MAINT 1 SW29797MX 27890 L2 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATES OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20050815001942005081500194NM 2005 8 15 QXEA200501167 120050811A2120 HAZE BOMBDRDHC8 DHC8402 1390042NM COCKPIT DETECTED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09400QX 4030 FCA FLIGHT NR 2383: AFTER STARTING THE APU AND SELECTING BLEED AIR ON, A HAZE A HAZE WAS NOTICED IN THE COCKPIT AND CABIN. AFTER SHUTTING THE APU OFF, THE HAZE SLOWLY DISSIPATED. MAINTENANCE DEFERRED IAW MEL 49-00-01, RSI #349739. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050815001952005081500195NE 2005 8 15 VTZA200500143 220050808A7261 LINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE SCAVANGE PUMP LEAKING A VTZAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA27655BR 7457 LT ENG OIL PRESSURE WARNING, PRESS FLUXUATION IN FLIGHT DOWN TO 19-22 PSI IN-FLIGHT ENGINE SHUTDOWN. C SUMP SCAVENGE LINES LEAKING - REPLACED LINES,OIL FILTER, INSPECTED CHIP DETECTOR. 2L72 4F4 FRTA21EA E15NE 20050816000082005081600008SO 2005 8 16 SWIA200515406 120050809A3350 LAMP EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07218SW 120287 AFT CEILING EMERGENCY LIGHT INOP. RELAMPED AFT CEILING EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050816000102005081600010EA 2005 8 16 SWIA200515408 120050730A2750766389L CONTROLLER CNDAIRCL600 CL6002C10 1390015EA SLAT/FLAP MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07718SK 10184 FLAPS HALFSPEED STATUS MSG. REPLACED SLAT/FLAP CONTROLLER. OPERATIONAL CHECK GOOD IAW MM 27-52-00. 2L72 4F RTA21EA 20050816000142005081600014SO 2005 8 16 SWIA200515412 120050719A5411 FRAME EMB 120 EMB120ER 3260203SO CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07576SW 120345 RIGHT FRAME 1 OUTBOARD SIDE CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED RIGHT FRAME NR 1 IAW SB 120-54-0036 "REV 02". 2L72 4T RTA31SO 20050816000302005081600030WP 2005 8 16 IXXA05RNG041S 120050723A5720 PLATE DOUG DC8 DC862F 3021972WP RT WING CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW1171CX 670273317 45961 DURING A ROUTINE C CHECK INSPECTION, FOUND CORROSION AT WING OUTER INBD EXTENDED LE PLATING A STA XFS XW 560 TO SPAR RT. CORROSION ON RT WING L/E LOWER SKIN WAS REMOVED AND REPAIR WAS ACCOMPLISHED IAW EWO ATI-57-033 AND SRM 57-2-1 FIGURE 2H. 2L74 4F 4A25 20050816000342005081600034WP 2005 8 16 DHL2005806500 120050809A5543 FRAME DOUG DC8 DC873F 302199FWP RUDDER CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH87034 46002 RUDDER L/E FORMER CRACKED 0.500" STA ZR 115.000. PERFORMED STOP HOLE AND FABRICATED ANGLE DOUBLER (ALCLAD 2024-T3 0.063") IAW SRM 55-2-0 PG 7, 8. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT IAW SRM 51-1-16. INSTALLED ANGLE DOUBLER IAW SRM 55-2-0 PG 7-8, SRM 51-1-20D PG 9 (HILOK), SRM 51-3-1 PG 2A (TORQUE). 2L74 4F RT4A25 20050816000552005081600055NM 2005 8 16 05FDEA02455 120050812A5754 SKIN BOEING727 727200 138407ENM NR 3 SLAT UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 LEFT NR 3 SLAT LOWER SURFACE HAS A PREVIOUS REPAIR THAT IS A MAJOR REPAIR IAW SRM 57-50-3 FIG 1. 2L73 4F RTA3WE 20050816000572005081600057NM 2005 8 16 05FDEA02456 120050812A5754 SKIN BOEING727 727200 138407ENM NR 8 SLAT UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 RIGHT NR 8 SLAT L/E HAS A PREVIOUS REPAIR THAT IS A MAJOR REPAIR IAW SRM 57-50-3. 2L73 4F RTA3WE 20050816000592005081600059NM 2005 8 16 05FDEA02458 120050812A5754 SKIN BOEING727 727200 138407ENM NR 3 SLAT UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 LEFT NR 3 SLAT L/E LOWER SKIN INBOARD OF INBOARD TRACK HAS A PREVIOUS REPAIR THAT IS A MAJOR REPAIR IAW SRM 57-50-3. 2L73 4F RTA3WE 20050816000702005081600070NM 2005 8 16 062005 120050810A2197 WIRE HARNESS BOEING757 757200 1384950NM RROYCERB211 RB211535E4 54555NE RT A/C PACK DAMAGED A ICAAO OTHER O OTHER TXTAXI/GRND HDL 1 SO11TFFID 24567 RT PACK AUTO PWR LT PACK STANDBY PWR C/B OUT, UNABLE TO RESET. ICELANDAIR RECENTLY TOOK DELIVERY OF CONVERTED 757-200 FREIGHTER. REASON FOR C/B POPPING WAS DAMAGE TO APPROX 15 WIRES IN BUNDLE W2356. UPON REMOVING ZIP-TIES FROM WIRE BUNDLE W2356 (2 METER LONG STRETCH) & SHAKING WIRING, AN INCREDIBLE AMOUNT OF METAL CUTTINGS/DEBURS FELL OUT. METAL CUTTINGS HAD TORN THROUGH INSULATION OF WIRES & CAUSED ELECTRICAL ARCING, RESULTING IN 15 WIRES BEING SPLICED/REPAIRED. DAMAGE IS APPROX STA 305, WL 170, RT SIDE. WIRE BUNDLE W2536 RUNS FROM P11 PANEL BEHIND P61 THROUGH FLOOR & AFT UNDER FLOORBOARDS. SEVERAL BREAKERS POPPED IN AIR CONDITIONING, LIGHTS & FUEL. WIRES REPAIRED PER SWPM 20-00 WIRE BUNDLE W2356. 2L72 4F4 FRTA2NM E12EU 20050816000722005081600072NM 2005 8 16 SWAA052429 120050814A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29474WN 33861 DURING SCHEDULED MV3 CHECK, FOUND EEPLS INOP AT ROW 20 TO ROW 24. REPAIRED EEPLS PER MM. 2L72 4F RTA16WE 20050816000902005081600090NM 2005 8 16 SWAA052445 120050812A3350D71701100 BATTERY PACK BOEING737 7377H4 1384404NM MID CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29716SW 27850 DURING SCHEDULED RON CHECK, FOUND LT MID CABIN EMERGENCY BULLNOSE LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050816000932005081600093NM 2005 8 16 SWAA052448 120050813A3350MS155721 BULB BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29794SW 30605 DURING SCHEDULED MV3 CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050816001632005081600163SO 2005 8 16 LR7A05103 120050813A534038848 TEE FITTING LKHEED382 382G 526414USO FS 588-596 CORRODED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 647 4763 DURING SCHEDULED B2 INSPECTION PER JOB CARD HB3200 FOUND LT MLG WHEEL WELL TEE AND WEB CORRODED AT FS 588 TO 596, LBL 65, WL 138. REPLACED TEE AND WEB IAW SRM SMP 583 51-60 AND 70. 2H74 4T A1SO 20050816002032005081600203NM 2005 8 16 DHLA05740013 120050806A5280 DOOR BOEING727 7272Q9 138448MNM NLG DOOR OUT OF ADJUST A DHLAO OTHER J WARNING INDICATION DEDESCENT 1 SO01740DH NOSE GEAR DOOR LIGHT ILLUMINATED IN FLT. LIGHT REMAINED ILLUMINATED EVEN WITH GEAR HANDLE IN UP POSITION. LIGHT ILLUMINATED DURING DESCENT ONLY. LUBED NOSE GEAR DOOR UP WARNING SW 5398 & 5435 . ADJUSTED R&L NLG DOOR PER B727 MM 32-22-1 PG 504 & 505 . JACK A/C NOSE & OPS CK NLG DOOR EXTRET CYCLE OPS CK OK PER B727 MM 32-22-1 PG. 507 #12 2L73 4F RTA3WE 20050816002072005081600207NM 2005 8 16 MZZA0500002 120050325A2560 BATTERY BOEING737 737823 13844BZNM FLASHLIGHT INOPERATIVE A MZZAL ABORTED APPROACH O OTHER NRNOT REPORTED 1 WP1313227 28788 THE FORWARD FLT ATTENDENT FLASHLIGHT WOULD NOT TEST. THE FASHLIGHT BATTERY WAS REPLACED IAW MM 25-64-00. 2L72 4F RTA16WE 20050817000112005081700011WP 2005 8 17 MWEA050077 120050812A5340593056673 SPLICE DOUG DC9 DC981 3022081WP STA 1250-1309 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 MAIN CABIN LEFT OUTBOARD SEAT TRACK FLANGES AROUND NUT PLATE HOLES, STATION 1250 TO 1309 IS CORRODED. FABRICATED AND INSTALLED SPLICE. 2L72 4F A6WE 20050817000172005081700017WP 2005 8 17 MWEA050082 120050815A53465930645105 SUPPORT ANGLE DOUG DC9 DC981 3022081WP ENGINE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 LEFT ENGINE INLET INTERIOR, THREE SUPPORT ANGLES BROKEN ON AFT SIDE OF FORWARD CIRCULAR WEB, LOCATED AT 5,7 AT THE EIGHT O'CLOCK POSITION. FABRICATED AND INSTALLED CLIP. 2L72 4F A6WE 20050817000192005081700019CE 2005 8 17 6018207152005 120050715A2916 CHECK VALVE LEAR 60 60LEAR 5170707CE HYD RESERVOIR LEAKING E J7SAA UNSCHED LANDING KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW05245FX 60182 AFTER TAKEOFF CREW NOTED VISIBLE FUMES AND A HYDRAULIC SMELL IN THE COCKPIT. RETURNED AIRCRAFT TO DEPARTURE AIRPORT FOR MAINTENANCE. MAINTENANCE FOUND HYDRAULIC FLUID IN A PNUEMATIC DUCT AND DEBRIS UNDER THE SEAT OF THE HYDRAULIC RESERVOIR CHECK VALVE. CLEANED VALVE AND ALL ASSOCIATED DUCTS. OPS CHECK PERFORMED WITH NO DEFECTS NOTED. 2L72 4F RTA10CE 20050817000212005081700021EA 2005 8 17 A6WA200540275 120050722A21508084402 VALVE CNDAIRCL600 CL6002B19 1900309EA LT A/C PACK INOPERATIVE A A6WAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL31446AW4983 7806 LT PACK OVERHEATED AND EMITTED BURNING ODOR. SLIGHT SMOKE NOTICED IN COCKPIT. PACK SHUTOFF BEFORE ANY AMBER CAS MESSAGE ILLUMINATED. PLACED ON MEL. VERIFIED DUAL BYPASS VALVE INOPERATIVE. CAUSING LT PACK TO RUN FULL HOT CREATING PACK SMELL. NO SIGNS OF SMOKE. (M) 2L72 4F RTA21EA 20050817000222005081700022EA 2005 8 17 A6WA200540272 120050808A2760 SPOILER CNDAIRCL600 CL6002B19 1900309EA NR 4 OUT OF ADJUST A A6WAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL31420AW 7640 CONFIG SPOILER MESSAGE ON TAKEOFF. ABORTED TAKEOFF AT 120 KNOTS. BRAKE TEMPS 5, 6 AND 7. AIRCRAFT WEIGHT 50,900 LBS. ADJUSTED GAP ON LEFT INBOARD GROUND SPOILER NR 4 TO WITHIN LIMITS IAW AMM 27-60-00-220-801. (M) 2L72 4F RTA21EA 20050817000262005081700026EA 2005 8 17 ASOA05597 120050712A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11860AS 7433 DURING OVERNIGHT MAINTENANCE IN SHV, THE LEFT FORWARD EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE LEFT FORWARD EXTERIOR EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. (M) 2L72 4F RTA21EA 20050817000282005081700028SO 2005 8 17 RAIA00508016 120050812A3010 ODOR EMB 145 EMB145LR 3260212SO COCKPIT DETECTED A RAIAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 CE03850HK 145003 FLT 8002 - ALB - SMELL IN CABIN/FLIGHT DECK WHEN ANTI-ICE SYSTEM WAS ACTIVATED. MAINTENANCE DEFERRED THE ANTI-ICE SYSTEM. 2L72 4T RTT00011AT 20050817000292005081700029SO 2005 8 17 RAIA00508018 120050813A323022270100001 SOLENOID VALVE EMB 145 EMB145LR 3260212SO MLG FAILED A RAIAA UNSCHED LANDING O OTHER CLCLIMB 1 CE03841HK10582 145382 FLT 7984 - IAD - LOUD BANGING NOISE AFTER GEAR RETRACTION. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR SOLENOID VALVE. 2L72 4T RTT00011AT 20050817000302005081700030SO 2005 8 17 RAIA00508017 120050812A4950 WARNING LIGHT EMB 145 EMB145LR 3260212SO BLEED AIR SYS ILLUMINATED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03850HK 145003 FLT 7975 - IAD - APU BLEED VALVE BLINKING OPEN ON APU BLEED SWITCH. MAINTENANCE DEFERRED THE APU BLEED SYSTEM. 2L72 4T RTT00011AT 20050817000312005081700031WP 2005 8 17 ASAA0580385 120050716A3397 WIRE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT LOOSE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM02960AS 53074 SEA LINE CHECK, AFT EXIT, CATWALK, PATH EMERGENCY LIGHT INOPERATIVE. RESECURED LOOSE WIRE CONNECTOR AND REPLACED LIGHT. LIGHT THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20050817000352005081700035WP 2005 8 17 ASAA0580363 120050717A532199579183 FLOOR PANEL DOUG DC9 DC983 3022083WP FS 315-389 BENT A ASAAK NONE O OTHER ININSP/MAINT 1 NM02944AS 53019 OKC - DURING HV CHECK FOUND CABIN FLOOR PANEL BENT AT CORNER. INSTALLED REPAIR FILLER AND DOUBLER. (M) 2L72 4F RTA6WE 20050817000382005081700038WP 2005 8 17 ASAA0580365 120050717A532199365813 FLOOR PANEL DOUG DC9 DC983 3022083WP FS 579-617 DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02944AS 53019 OKC - FOUND DURING HV-CHECK, CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050817000392005081700039NM 2005 8 17 05066 120050812A2432401763 BATTERY BOEING747 747122 1384872NM DISCHARGED A KCSAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 GL23716CK 19753 AFTER T/O, SMELL OF SMOKE IN COCKPIT. LOSS OF BATTERY VOLTAGE - BATTERY OVERHEAT. RETURNED TO HNL. REMOVED AND REPLACED AIRCRAFT BATTERY AND BATTERY CHARGER IAW B747 MM 24-30-00. OPS CHECK GOOD. 2L74 4F A20WE 20050817000432005081700043WP 2005 8 17 ASAA0580369 120050717A532199365813 FLOOR PANEL DOUG DC9 DC983 3022083WP FS 697-769 DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02944AS 53019 OKC - DURING HV-CHECK, FOUND CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050817000452005081700045NM 2005 8 17 ABXA050185 120050813A2120 ODOR BOEING767 767281 1385109NM COCKPIT DETECTED A ABXAO OTHER WB INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 GL23795AX 23145 FORWARD EQUIPMENT COOLING EICAS MESSAGE DISPLAYED AS WELL AS NO COOLING LIGHT. ACRID SMELL IN COCKPIT ABOUT 5 MINUTES BEFORE LIGHTS DISPLAYED. CREW REPORTED THIS HAPPENED JUST BEFORE LANDING. EQUIPMENT COOLING WAS IN OVERRIDE. DUE TO CONFIGURATION, THIS CONDITION MAY OCCUR. INSPECTED FORWARD EQUIPMENT COOLING AREA, UNABLE TO RECREATE DISCREPANCY. 2L72 4F RTA1NM 20050817000462005081700046NM 2005 8 17 UPS05445185 120050722A5330 SKIN BOEING747 747121 1384871NM BS 395 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE:C, RIGHT SIDE AT BS 395 STR 19 UPPER FASTENER ROW FOUND ONE EACH FASTENER HOLE CRACKED AT OUTER SKIN APPROX .125 INCH LONG RUNNING FWD AS MARKED. FX BS 383 TO BS 399 STR 19R AREA OVERLAPPING SKIN REPAIRED WITH ZERO TIMING AT CRITICAL ROW FASTENERS PER SRM 53-30-03 FIG 17. SUBSEQUENT INSPECTION IS NECESSARY FOR CAT B REPAIR REF SRM 53-30-03 FIG 17 SHT 6 TABLE III FOR INSPECTION REQ WITH 15000 FC INSP THRESHOLD. MPI P18050 FOR LFEC INITIAL AT 15000 FC & REPEAT AT 1500 FC THERE AFTER. 2L74 4F A20WE 20050817000472005081700047NM 2005 8 17 UPS05445186 120050722A5330 SKIN BOEING747 747121 1384871NM FX CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE:C RIGHT WING AT BS 395 STR 19 UPPER FASTENER ROW FOUND 1EA FASTENER HOLE CRACK AT OUTER SKIN APPROX .125 INCH LONG RUNNING FWD AS MARKED. FX BS 383 TO BS 399 STR 19R AREA OVERLAPPING SKIN REPAIRED WITH ZERO TIMING AT CRITICAL ROW FASTENERS AS PER SRM 53-30-03 FIG 17. REFER NRC 5902 FOR DETAIL. PER MPI P18050- LFEC INTIAL INSP AT 15000 FC & REPEAT AT 1500 FC THEREAFTER. 2L74 4F A20WE 20050817000482005081700048NM 2005 8 17 UPS05445187 120050728A5330 SKIN BOEING747 747121 1384871NM FX CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE:C FX SKIN S19R AT BS 388 TOP ROW FASTENER ROW 1EA FASTENER HOLE FOUND CRACK AT OUTER SKIN RUNNING FWD & AFT APPROX 0.030 INCH. FX SKIN BS 383 TO BS 399 STR 19R AREA OVERLAPPING SKIN REPAIRED WITH ZERO TIMING AT CRITICAL ROW FASTENERS AS PER SRM 53-30-03 FIG 17 REF NRC 5902 FOR DETAIL. PER MPI P18050 - LFEC INTIAL INSP AT 15000 FC & REPEAT AT 1500 FC THEREAFTER. 2L74 4F A20WE 20050817000512005081700051WP 2005 8 17 UPS05845193 120050802A53403755854502N FITTING DOUG DC8 DC873F 302199FWP FS1180 L27L CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 INSPECTION TYPE:C1 -C- PIT CROSS SLIDE DOOR BANANA FITTING CRACKED AT BUMPER STOPS AT L27L STA 1180. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20050817000532005081700053WP 2005 8 17 UPS05845195 120050802A53403758498U2 FITTING DOUG DC8 DC873F 302199FWP FS 1240 L35R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 INSPECTION TYPE:C1 -C- PIT STA 1240 L35R FITTING CRACKED. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20050817000552005081700055WP 2005 8 17 UPS05845196 120050803A5312 PRESSURE PANEL DOUG DC8 DC873F 302199FWP FS -67 RBL 60 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 INSPECTION TYPE:C1 FOUND EXFOLIATION CORROSION AND CRACKS ON COCK PIT SUBFLOOR AT STA -67 RBL 60 INSIDE RIGHT NOSE TUNNEL. CUT OUT DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR IAW DWG SRO8530 026 AND DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20050817000562005081700056NM 2005 8 17 UPS05M45184 120050720A5340 MOUNT BRACKET DOUG MD11 MD11F 3023600NM CABIN CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01255UP 48404 INSPECTION TYPE:C CHECK CABIN - CORROSION ON SATCOM MOUNT BRACKET AND FRAME AT STA 959 LT. CORROSION REMOVED AND AREA REPROTECTED ON FRAME STA 959 LT AS PER SRM 51-21-01 REV 37 VOL II AND FOUND WITHIN LIMIT AS PER SRM 53-00-01 VOL I REV 37. 2L73 4F RTA22WE 20050817000602005081700060WP 2005 8 17 ASAA0580371 120050717A5321993919511 FLOOR PANEL DOUG DC9 DC983 3022083WP FS 807-826 DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02944AS 53019 OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050817000622005081700062WP 2005 8 17 ASAA0580373 120050717A5321993665169 FLOOR PANEL DOUG DC9 DC983 3022083WP FS 1041-1079 DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02944AS 53019 OKC - FOUND DURING HV-CHECK, CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050817000632005081700063WP 2005 8 17 ASAA0580374 120050717A532199365811 FLOOR PANEL DOUG DC9 DC983 3022083WP FS 1174-1193 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02944AS 53019 OKC - FOUND DURING HV CHECK, CABIN FLOOR PANEL DELAMINATED AND CRACKED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050817000672005081700067NM 2005 8 17 AALA20050525 120050813A3350 BATTERY PACK BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21196AA 32390 DFW - OVERWING EMERGENCY LIGHTS AT RIGHT HAND FORWARD AND LEFT HAND AFT LIGHT INOPERATIVE. REPLACED BATTERY PACKS FOR OVERWING EMERGENCY LIGHTS AT RIGHT HAND FORWARD AND LEFT HAND AFT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050817000682005081700068WP 2005 8 17 AALA20050526 120050814A3350P4010049 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21964TW 53614 ORD - EMERGENCY LIGHTS IN AISLE SEAT ROWS 22 TO 26 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN AISLE SEAT ROWS 22 TO 26. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050817000732005081700073WP 2005 8 17 AALA20050522 120050806A3230 SCHRADER VALVE DOUG DC9 DC982 3022082WP NLG INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21423AA 49335 DFW - NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. FOUND NOSE LANDING GEAR STRUT FLAT. REPLACED SCHRADER VALVE AND SEALS AND RESERVICED STRUT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050817000742005081700074WP 2005 8 17 AALA20050523 120050812A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21969TW 53619 LGA - EMERGENCY LIGHT MID BATTERY CHARGER INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050817000762005081700076NM 2005 8 17 AALA20050518 120050810A3350P4010049 BATTERY PACK DOUG MD80 MD83 3023681NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21951TW 53470 LGA - EMERGENCY SEAT MOUNTED ESCAPE PATH LIGHTING BATTERIES INOPERATIVE. REPLACED BATTERIES AT POSITION AB51 AND AB54 FOR EMERGENCY SEAT MOUNTED ESCAPE PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RT 20050817000772005081700077WP 2005 8 17 AALA20050520 120050810A3350 CHARGER DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21271AA 49293 DFW - COCKPIT AND FORWARD GALLEY CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY FOR COCKPIT AND FORWARD GALLEY CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050817000782005081700078NM 2005 8 17 AALA20050514 120050728A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21909AN 29511 TUL - EMERGENCY LIGHT BATTERY PACK IN CABIN AT STATION 328 INOPERATIVE. REPLACED BATTERY PACK IN CABIN AT STATION 328 FOR EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20050817000822005081700082WP 2005 8 17 IXXA05000940 120050815A7797C65039ATI1 WIRE DOUG DC8 DC871F 302199DWP CFMINTCFM56 CFM562FR 13802EU NR 2 ENGINE DAMAGED A IXXAO OTHER J WARNING INDICATION CLCLIMB 1 SW11828BX83877382 45993 692264 DURING CLIMB & CRUISE NR 2 ENGINE FUEL FLOW & EGT FLUCUATED FROM 811 TO 875, OTHER ENGINES AT 830 TO 835. EGT THEN PEAKED AT 1000 (FLASHING). ALSO WITH STANDARD POWER SET FOR CLIMB, THE EGT & FF FOLLOWED THE THROTTLE & THEN THE FUEL FLOW & EGT WENT HIGH & DID NOT FOLLOW THROTTLE. CREW PERFORMED AN ENGINE SHUTDOWN CHECKLIST IAW QRH AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE LEFT AND RIGHT EGT HARNESS AND THE THERMOCOUPLES. THE PLUG RECEPTACLE WAS CLEANED AT PYLON. THE EGT HARNESS WAS REMOVED & REPLACED AND A RUN-UP WAS PERFORMED OF NR 2 ENGINE IAW ATI ERH 70.01. NR 2 ENGINE EGT OPS CHECK GOOD. NO FLUCTUATION NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F4 FRT4A25 E21EU 20050817000842005081700084GL 2005 8 17 CHQA200500141 220050813A7200AE3007A1P ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 1 UNSERVICEABLE A CHQAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 GL11561RP9609 9609 145447 CAE312008 FLIGHT 6399 CMH-BDL - RECEIVED A LAV SMOKE EICAS WARNING IMMEDIATELY AFTER TAKEOFF. F/A REPORTED MILD FUMES IN THE CABIN WITH NO VISIBLE SMOKE OR FIRE. CONDITIONS CONTINUED FOR 1-2 MINUTES BUT DID NOT WORSEN, AND WARNING EVENTUALLY CLEARED. DECLARED AN EMERGENCY AND RETURNED TO THE AIRPORT AND PERFORMED A VISUAL APPROACH TO RUNWAY 28R. LANDED WITHOUT EVEN AND TAXIED THE AIRCRAFT TO THE GATE AND DEPLANED NORMALLY. MAINTENANCE TROUBLESHOT THE ENGINES. REMOVED AND REPLACED NR 1 ENGINE IAW JOB CARD CE720001. OPS CHECK AND LEAK CHECK GOOD. 2L72 4T4 FRTT00011ATTE6CH 20050817000852005081700085GL 2005 8 17 CHQA200500142 220050813A7200AE3007A1P ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 2 UNSERVICEABLE A CHQAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 GL11260SK9344 9344 145128 CAE312071 APPROX 15 MIN INTO FLT RECEIVED AN E2 IMP BYPASS MESSAGE. RAN QRH AND CONTINUED. MESSAGE WENT OUT VERY SHORTLY AFTER IT APPEARED. APPROX 35 MIN INTO FLT, ITT JUMP FROM GREEN INDICATION TO RED AND BACK TO AMBER AND GREEN. PULLED NR 2 THRUST LEVER BACK. ITT WENT BACK INTO GREEN. ADVANCED THE THRUST LEVER AND ITT SHOT RIGHT BACK INTO RED AND ENGINE SHUT ITSELF DOWN. RAN QRH ENGINE FAILURE CHECKLIST, PRECAUTIONARY ENGINE SHUTDOWN CHECKLIST, EMERGENCY DESCENT CHECKLIST. NOTIFIED ATC AND GOT CLEARANCE FOR EMERGENCY DESCENT. F/A REPORTED SMOKE IN CABIN. DECLARED EMERGENCY. FIRE TRUCKS ROLLED OUT BEHIND & CLEARED AIRCRAFT OF ANY SMOKE COMING FROM NR 2 ENGINE. MX REMOVED AND REPLACED NR 2 ENGINE. 2L72 4T4 FRTT00011ATTE6CH 20050817000882005081700088WP 2005 8 17 IXXA05SMN158S 120050706A5720 VANE DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE XOLDO 67.000 IMPROPER B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, RT WING. OB VANE SLOT HAS INTERIM REPAIR XOLDO 67.000. PERFORMED MAJOR REPAIR, REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-1-21 PAGE 1. REMOVED THE DAMAGED AREA IAW DWG NR ED 4022, PERFORMED NDT INSPECTION. IAW NDT SPM PART 06-10-01-001. NO CRACK, NO CORROSION FOUND. FABRICATED EXTERNAL REPAIR DOUBLER (ALCLAD 7075 T6 0.071) + FILLER (ALCLAD 7075 T6 0.063) + INTERNAL DOUBLER (ALCLAD 7075 T6 0.063) IAW SEMAN DWG ED 4022, SRM 51-1-4 PAGE 1. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PAGE 9. INSTALLED REPAIR PARTS IAW DWG ED 4022, SRM. TORQUED IAW SRM 51-3-1. 2L74 4F4 FRT4A25 E2GL 20050817000892005081700089CE 2005 8 17 DXTA200500895 120050811A3030 WARNING LIGHT CESSNA500 560CESSNA 2076750CE AOA HEATER ILLUMINATED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07306QS 5600266 AOA HEATER ANUNCIATOR ILLUMINATED WITH PITOT/STATIC HEAT ON, ABORTED TAKEOFF. OPS CHECKED AOA HEATER SEVERAL TIMES. COULD NOT DUPLICATE DISCREPANCY. NO DEFECTS FOUND AT THIS TIME. 2L72 4F RTA22CE 20050817000902005081700090WP 2005 8 17 IXXA05SMN129S 120050629A5340 FITTING DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE STA 8.000 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, NOSE SECTION STA. 8.000 RT SIDE FITTING CRACKED 5 INCHES (L-33R) REMOVED CRACKED FITTING IAW SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING IAW DWG DOUGLAS NR 4645453 (ALCLAD 7075 T6 51), EO SEMAN NR 2005938. PERFORMED HEAT TREATMENT IAW SRM 51-1-11 PAGS 1,13,17. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02 TO 07. CLEANED, TREATED AND PRIMED AREA + NEW FITTING IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PAGE 9, SRM 51-3-1. TORQUED IAW SRM 51-3-1. 2L74 4F4 FRT4A25 E2GL 20050817000912005081700091CE 2005 8 17 DXTA200500896 120050811A4930 B-NUT CESSNA560 560XL 2076702CE APU FUEL LINE LEAKING E DXTAO OTHER KBJFLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 GL07605QS 5605321 STRONG ODOR OF FUEL NOTICED IN CABIN, HELL HOLE, AND APU EXHAUST. ODOR NOTICED WITH A APU RUNNING WITH APU OFF. T/S APU FUEL SYSTEM AND APU SMELL. RAN APU. FOUND NO ABNORMAL APU EXHAUST ODOR. REMOVED APU INSPECTION PLATES. FOUND B-NUT LOOSE ON APU MAIN FUEL NOZZLE LINE. TIGHTENED FUEL LINE B-NUT. NO LEAKS NOTED AT THIS TIME IAW CE 560 M/M 20-10-06. 2L72 4F RTA22CE 20050817000932005081700093EU 2005 8 17 DXTA200500893 120050810A3260 WARNING LIGHT BRAERO1000 HAWKER1000 7450005EU MLG MALFUNCTIONED E DXTAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL07546QS 259046 RED LANDING GEAR UNSAFE LIGHT ON THE RIGHT SIDE STAYED LIT AFTER GEAR RETRACTION. EXCESS WIND NOISE AND SLIGHT VIBRATION WAS NOTICED WHILE AIRBORNE. VISUALLY INSPECTED RT MAIN GEAR, INSPECTED MICRO SWITCHES & WIRING HARNESS AT SWITCH & TERMINAL BLOCK, NO DEFECTS NOTED. JACKED AIRCRAFT CYCLED GEAR SEVERAL TIMES. NO DEFECTS NOTED ALL WORK IAW HAWKER 1000 MM 32-30-00. 2L72 4F RTA3EU 20050817000972005081700097EU 2005 8 17 AWXA200500950 120050712A5320D348002069701 SHEAR WEB AIRBUS320 A320231 3930325EU CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28627AW 66 SAL - MAJOR REPAIR - DURING C4 CHECK DISCOVERED CRACK IN SHEAR WEB BETWEEN FR 68 AND FR 68+13", AND BETWEEN -Y1190 AND -Y1432. MAINTENANCE REMOVED CRACKED SHEAR WEB BETWEEN FR 68 AND FR 68+13", AND BETWEEN -Y1190 AND -Y1432 IAW AIRBUS 320 SRM 51-42-11. INSTALLED NEW SHEAR WEB BETWEEN FR 68 AND FR 68+13", AND BETWEEN -Y1190 AND -Y1432 IAW AIRBUS 320 SRM 51-42-11 IAW AIRBUS 320 SRM 51-72-11 PAGE 1. CRACK LENGTH NOT LISTED. 2L72 4F RTA28NM 20050817000982005081700098EU 2005 8 17 AWXA200500951 120050810A3210201160697 PIN MESSIER AIRBUS320 A320231 3930325EU RT MLG WORN A AWXAO OTHER E VIBRATION/BUFFET CLCLIMB 1 WP28629AW507928692 4285791 076 AT ROTATION, CREW NOTICED SEVERE VIBRATION FROM MLG AREA. A/C CONTINUED ONTO MSP, CREW FLEW BY TOWER, UNABLE TO DETERMINE IF TIRE DAMAGE HAD OCCURRED. EMERGENCY LANDING DECLARED. MX INSPECTED TIRES, BRAKES & GEAR, NO DEFECTS NOTED. PERFORMED BSCU BITE TEST, NO FAULTS FOUND. MOC GENERATED FOLLOW UP TO BE PREFORMED IN PHX. MX INSPECTED, FOUND APEX PIN WORN ON UPPER TORQUE LINK AT RT MLG UPPER TORQUE LINK. REPLACED APEX PIN & TORQUE LINK. VIBRATION WRITTEN UP AGAIN RESULTING IN NOSE TIRES & MLG TIRES BEING REPLACED. TORQUE LING APEX PIN WAS SCRAPPED. UPPER TORQUE LING ASSEMBLY WAS REPAIRED, TWO WORN APEX BUSHINGS WERE REPLACED WITH NEW BUSHINGS. WORK WAS ACCOMPLISHED IAW CMM 32-11-33 REV. 29. 2L72 4F RTA28NM 20050817000992005081700099NM 2005 8 17 AWXA200500953 120050813A2120 ODOR AIRBUSA319 A319132 3930340NM CABIN DETECTED A AWXAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP28806AW 1056 PHX - BURNING SMELL - FLT 0880 - DURING FLIGHT, FLIGHT ATTENDANT REPORTED ODOR COMING FROM THE AFT END OF THE AIRCRAFT THAT SMELLED LIKE NAIL POLISH REMOVER, HER EYES WERE BURNING. CREW TURNED OFF RT PACK AND PLACED PACK FLOW TO HIGH POSITION. SMELL DISSIPATED. MAINTENANCE RAN BOTH PACKS FULL HOT THEN FULL COLD, COULD NOT DUPLICATE SMELL. REPORTED FOR PRECAUTIONARY PURPOSES. 2L72 4F RTA28NM 20050817001012005081700101WP 2005 8 17 IXXA05SMN134S 120050629A5730 SKIN PANEL DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE XW84.00-91.00 IMPROPER B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, RT IB FLAP FWD UPPER PLATING NON STANDARD REPAIRS (02 EA ) STA XW 84.00 -XW 91.00. PERFORMED MAJOR REPAIR IAW NR 05258 DATE 06-24-05, DWG ED 4004, EO NR 2005911 DATE 06-24-05. REMOVED FASTENERS IAW SRM. REMOVED PLATING SEGMENT (DAMAGED) IAW DWG NR ED 4004, PERFORMED NDT INSPECTION. IAW NDT SPM PART. NO CRACK, NO CORROSION FOUND. FABRICATED NEW PLATING SEGMENT (ALCLAD 2024 T3 0.040”) + INTERNAL SPLICE (ALCLAD 2024 T3 0.050) + EXTERNAL DOUBLERS (02 EA) (ALCLAD 2024 T3 0.050) IAW DWG ED 4004, SRM. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS INTERNAL PART IAW SRM. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM. INSTALLED REPAIR PARTS AND TORQUED IAW SRM. 2L74 4F4 FRT4A25 E2GL 20050817001022005081700102NM 2005 8 17 AWXA200500955 120050814A2530416000123 THERMISTER BOEING737 7373G7 1384595NM COFFEEMAKER FAILED A AWXAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP28157AW114968936 23779 STRONG ELECTRICAL BURNING ODOR REPORTED BY FLIGHT ATTENDANT. ODOR COMING FROM THE AFT GALLEY. MAINTENANCE FOUND THE AFT NR 3 COFFEEMAKER HOT AND TO HAVE ODOR. REPLACED NR 3 COFFEEMAKER IAW AMERICA WEST AIRLINES TASK CARD R1D25001. OPS CHK GOOD. TEARDOWN CONFIRMS REASON FOR REMOVAL. FOUND THERMISTOR EXTRUDING FROM MAIN BODY OF THERMISTOR, PLASTIC PARTS ON THE LOW WATER SENSOR MELTED AND FOUND 3 MANUAL RE-SETTABLE THERMOSTATS ON TANK ASSY TRIPPED. ROOT CAUSE OF FAILURE WAS EXTRUDING THERMISTOR GIVING A FALSE LOW TEMP. READING WHICH CAUSED PC BOARD TO COMPENSATE FOR LOWER TEMP BY KEEPING HEATERS ON LONGER THAN USUAL, CAUSING AN OVERHEAT CONDITION. OVERHAULED THIS UNIT IAW CMM 25-30-09 REV 5. 2L72 4F RTA16WE 20050817001052005081700105WP 2005 8 17 0501259929 120050814A3397 WIRE DOUG DC9 DC931 3022065WP EMERGENCY LIGHT CHAFED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018923E 45838 EMERGENCY LIGHTS REMAIN ON WHEN SWITCHED OFF AND C/B POPS. FOUND WIRING CHAFED BEHIND OVERHEAD BINS. REPAIRED WIRING AND RECHARGED BATTERY PACKS. CHECKS GOOD. 2L72 4F A6WE 20050817001062005081700106WP 2005 8 17 ASAA0580375 120050717A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP CABIN PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02944AS 53019 OKC - FOUND DURING HV CHECK, CABIN FLOOR PANEL PUNCTURED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050817001072005081700107WP 2005 8 17 ASAA0580376 120050717A532199365859 FLOOR PANEL DOUG DC9 DC983 3022083WP FS 826-864 DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02944AS 53019 OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050817001092005081700109WP 2005 8 17 ASAA0580378 120050717A532199366393 FLOOR PANEL DOUG DC9 DC983 3022083WP FS 946-1003 DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02944AS 53019 OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050817001102005081700110WP 2005 8 17 ASAA0580379 120050717A532199365833 FLOOR PANEL DOUG DC9 DC983 3022083WP FS 826-864 DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02944AS 53019 OKC - FOUND DURING HV CHECK, CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050817001132005081700113WP 2005 8 17 ASAA0580381 120050717A532199365465 FLOOR PANEL DOUG DC9 DC983 3022083WP FS 160-200 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02944AS 53019 OKC - DURING HV CHECK, FOUND FLOOR PANEL HAS MISSING AND CORRODED INSERTS. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050817001142005081700114EA 2005 8 17 DAT2005F00010 220050803A7200 ENGINE STBROSSD3 SD360 8100606EU PWA PT6 PT6A65R 52043EA LEFT SHUTDOWN E DATAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 GL13360RW15194 SH3613 PCE97170 DEPARTING, CAPTAIN NOTICED THE LT ENGINE TORQUE DROPPING AND THE ITT RISE TO APPROX 850 DEGREES. THE CAPTAIN PUSHED THE LT POWER LEVEL UP SLIGHTLY TO VERIFY THAT IT HAD NOT WORKED ITSELF BACK. FLIGHT CREW COMPLETED THE VITAL ACTION ITEMS. FLIGHT CREW DECLARED AN EMERGENCY WITH THE ATC. AC LANDED WITHOUT INCIDENT AND THE AC WAS TAXIED BACK THE RAMP. MECHANIC WAS DISPATCHED WITH A SERVICEABLE ENGINE MODULE, INCLUDING ACCESSORIES. ENGINE MODULE, INCLUDING ACCESSORIES AND PROP WAS REMOVED. SERVICEABLE COMPONENTS WERE INSTALLED IAW MM. ORIGINAL PROP WAS REINSTALLED IAW MM. THE LT ENGINE WAS GROUND RUN AND LEAK AND OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 T A41EU E4EA 20050817001152005081700115WP 2005 8 17 ASAA0580382 120050717A5321993655211 FLOOR PANEL DOUG DC9 DC983 3022083WP FS 200-237 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02944AS 53019 OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL HAS MISSING AND CORRODED INSERTS. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050817001192005081700119WP 2005 8 17 ASAA0580387 120050718A5230 SKIN DOUG DC9 DC983 3022083WP CARGO DOOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02944AS 53019 OKC - DURING HV CHECK, FOUND MID CARGO BAY DOOR SKIN DENTED. REFORMED SKIN AND INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050817001212005081700121WP 2005 8 17 IXXA05SMN135S 120050630A5730 SKIN DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE XF45.000-87.000 IMPROPER B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, RT IB FLAP LOWER UPPER PLATING NON STANDARD REPAIRS (02 EA) STA XF 45.000 - XF 87.000. PERFORMED MAJOR REPAIR IAW SRM 57-2-5 FIG. 1, EO NR 2005947. REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1. REMOVED DAMAGED AREA IAW SRM 57-2-5 FIG. 1 SHEET 1,2. PERFORMED NDT INSPECTION. IAW NDT SPM PART 06-10-01-001. NO CRACK, NO CORROSION FOUND. FABRICATED PLATING SEGMENT (02 EA) (NEW) (ALCLAD 2024 T3 0.050”) + INTERNAL SPLICE (03 EA) (ALCLAD 2024 T3 0.063) IAW SRM 57-2-5 FIG. 1, SRM 57-7-1 FIG. 1 ITEM A,1. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11. INSTALLED REPAIR PARTS IAW SRM. 2L74 4F4 FRT4A25 E2GL 20050817001222005081700122EU 2005 8 17 USAA050887 120050718A5315D5311281520200 FLOORBEAM AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19109UW19030 1065 FOUND FLOOR SUPPORT BEAM 1 INCH DIAMETER .070 DEEP CORROSION, 20 INCH LT OF CENTERLINE AT C16. CORROSION LEVEL 1, TASK JA-220-53500. DEFECTIVE PART REPLACED WITH IDENTICAL PART IAW SRM 51-72-11. (M) 2L72 4F4 FRTA28NM E38NE 20050817001302005081700130WP 2005 8 17 ASAA0580391 120050718A523059101413 DOOR DOUG DC9 DC983 3022083WP FS 1163 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02944AS 53019 OKC - DURING HV CHECK, FOUND AFT CARGO BAY DOOR DENTED. RE-COLD FORMED SKIN AND INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050817001322005081700132WP 2005 8 17 ASAA0580393 120050718A575359304963 VANE DOUG DC9 DC983 3022083WP TE FLAP CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02944AS 53019 OKC - DURING HV CHECK, FOUND LEFT NR 3 OUTBOARD FLAP VANE L/E REPAIR DOUBLER IS CHAFED. REPLACED DOUBLER. (M) 2L72 4F RTA6WE 20050817001332005081700133WP 2005 8 17 ASAA0580395 120050725A5320993061287 CUSP WEB DOUG DC9 DC983 3022083WP FS 1281 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02947AS 53020 OKC - DURING C-CHECK, FOUND RIGHT CUSP WEB CRACKED. STOP DRILLED CRACK. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050817001342005081700134WP 2005 8 17 ASAA0580396 120050725A532099101513 CUSP WEB DOUG DC9 DC983 3022083WP FS 965-984 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02947AS 53020 OKC - DURING C-CHECK, FOUND RIGHT CUSP WEB CORRODED. REMOVED CORRODED SECTION. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050817001362005081700136EA 2005 8 17 A6WA200540279 120050805A2410755469E IDG CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 2 GENERATOR LACK OF LUBE A A6WAC ABORTED TAKEOFF WJ INADEQUATE Q C WARNING INDICATION TOTAKEOFF 1 GL31420AW 7640 DURING TAKEOFF ROLL 70 KNOTS IDG NR FAIL, GEN NR 2 OFF APPEARED MODERATE BREAKING BTMS READOUT 4, 5,6,7 FOUND NR 2 IDG OIL LEVEL LOW SERVICED NR 2 IDG RAN ENGINE NO LEAKS NOTED OPS CHECK GOOD IAW MM. PERFORMED RTO INSPECTION. (K) 2L72 4F4 FRTA21EA E15NE 20050817001372005081700137EA 2005 8 17 A6WA200540277 120050804A2810 FUEL CAP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT WING MISINSTALLED A A6WAA UNSCHED LANDING WK INADEQUATE Q C FLUID LOSS CLCLIMB 1 GL31421ZW 7346 FUEL VENTED OUT L-WING ON TAKEOFF AFTER MANUAL OVERWING FUELING LANDED AT 48000 ORD MLW 47. LT FUEL CAP FOUND TO BE INSTALLED IMPROPERLY. INSTALLED LT WING FUEL CAP PROPERLY COMPLIED WITH OVERWEIGHT INSPECTION . NO DEFECTS NOTED. (K) 2L72 4F4 FRTA21EA E15NE 20050817001382005081700138WP 2005 8 17 ASAA0580398 120050725A5313593271725 LONGERON DOUG DC9 DC983 3022083WP FS 756 DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02947AS 53020 OKC - FOUND DURING C-CHECK, FREEZE PLUG IN LONGERON. REMOVED DAMAGED SECTION AND SPLICED IN NEW SECTION. (M) 2L72 4F RTA6WE 20050817001402005081700140EA 2005 8 17 VNAA0508010 120050810A2710 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE AILERON SYS ILLUMINATED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL05220PS 7887 DURING TAKEOFF ROLL CONFIG AILERON WARNING MESSAGES ILLUMINATED AND SOUNDED. THE CREW PERFORMED A REJECTED TAKEOFF. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE AILERON TRIM SYSTEM IAW CRJ200 AMM 27-11-00-710-801 AND A REJECTED TAKEOFF INSPECTION IAW CRJ200 AMM 05-51-27. NO DISCREPANCIES WERE FOUND. AN OPERATIONAL CHECK FLIGHT WAS PERFORMED WITH NO DEFECTS NOTED. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050817001412005081700141EU 2005 8 17 USAA050940 120050803A5315 FLOORBEAM AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE FR 66 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19110UW 1112 PIT - S2 - FLOORBEAM, 1 INCH DIA AREA CORROSION; LEVEL 1; TASK JA-260-53500, FLOOR SUPPORT BEAM, FR 66 AT RT AFT ENTRY DOOR. INSTALLED DOUBLERS/ REPAIR ANGELS IAW SRM. (K) 2L72 4F4 FRTA28NM E38NE 20050817001432005081700143WP 2005 8 17 ASAA0580399 120050725A53305932717147 SKIN DOUG DC9 DC983 3022083WP FS 756 DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02947AS 53020 OKC - FOUND DURING C-CHECK, FREEZE PLUG IN FUSELAGE SKIN. INSTALLED EXTERNAL REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050817001442005081700144WP 2005 8 17 ASAA0580400 120050725A532098930538U77 CUSP WEB DOUG DC9 DC983 3022083WP FS 598-712 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02947AS 53020 OKC - DURING C-CHECK, FOUND RIGHT FUSELAGE CUSP WEB IS EXFOLIATED CORRODED. REPLACED WEB. (M) 2L72 4F RTA6WE 20050817001452005081700145NM 2005 8 17 USAA050971 120050803A575465C26601168 SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU NR 6 SLAT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19511AU54646 23594 CLT- C4 - SKIN, OB LOWER LE SKIN OF NR 6 SLAT CRACKED MKD 1 INCH CRACK. INSTALLED DOUBLER IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050817001482005081700148WP 2005 8 17 ASAA0580402 120050725A5320993061223 CUSP WEB DOUG DC9 DC983 3022083WP FS 1098-1117 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02947AS 53020 OKC - DURING C-CHECK, FOUND RIGHT CUSP WEB IS CORRODED. REMOVED DAMAGED SECTION OF WEB AND INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050817001532005081700153WP 2005 8 17 ASAA0580405 120050725A53305920323509 SKIN DOUG DC9 DC983 3022083WP FS 471-487 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02947AS 53019 OKC - DURING C-CHECK, FOUND RIGHT FUSELAGE IS DENTED. REMOVED DAMGAED AREA. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050817001582005081700158EU 2005 8 17 KBM2005F00168 120050729A6420350A33214301 PITCH LINK SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE TAIL ROTOR DAMAGED E KBMAO OTHER O OTHER NRNOT REPORTED 1 EA19115SH737 3141 UNIT APPEARS TO BE DAMAGED IN IB BEARING ATTACHMENT. BEARING WORN. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050817001602005081700160NM 2005 8 17 1290503 120050726A275118173810 TRANSMITTER BOEING737 7377BC 1384509NM TE FLAPS INTERMITTENT E BJ6AO OTHER N FALSE WARNING LDLANDING 1 NE03129QS2756 30329 FLAP POSITION DISAGREE WITH FLAP HANDLE. RT FLAP 0 DEGREES, LT FLAP 5 DEGREES. BECAUSE OF SKEW INDICATION THE FLAP SYSTEM WOULD NOT EXTEND. CREW MADE AN UNEVENTFUL -0- FLAP LANDING. PERFORMED FSEU BITE AND OBSERVED CODE 27-52259 LT FLAP TRANSMITTER SWITCH P/N 18-1738-10 IS FAULTY. REPLACED LT & RT FLAP TRANSMITTER SWITCHES WITH NEW SWITCHES THAT COMPLY WITH HONEYWELL SERVICE LETTER SL 18-1738-10. BOEING FLEET TEAM DIGEST 737NG-FTD-27_03004 TITLED TRAILING EDGE FLAP POSITION TRANSMITTERS - INCREASED SYNCHRO BEARING FRICTION ADDRESSES THIS ISSUE. 2L72 4F RTA16WE 20050817001622005081700162NM 2005 8 17 CALA0500266 120050815A5315BAC1518338 FLOORBEAM BOEING757 757224 1384958NM STA 720 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718112 27302 INSPECTION FOUND FLOORBEAM CORRODED AT STA 720, RBL 48.5 TO RBL 60. A REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 201. 2L72 4F RTA2NM 20050817001662005081700166EU 2005 8 17 F3LA200500038 120050815A25303510004405 COFFEEMAKER AIRBUSA319 A319112 3930323EU GALLEY ODOR A F3LAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM03903FR 2012 1560 AIR DIVERSION, SMOKE SMELL IN AFT GALLEY. DECLARED AN EMERGENCY. MX PERFORMED TSM TASK 24-00-00-810-823, FOUND AFT NR 2 COFFEEMAKER C/B'S POPPED ON REAR OF COFFEEMAKER. REMOVED AFT NR 1 COFFEEMAKER & INSTALLED INTO NR 2 POSITION, OPS NORMAL. NO ARCING OR DEFECTS NOTED ON GALLEY WIRING. REINSTALLED COFFEEMAKERS IN ORIGINAL POSITIONS. DETERMINED AFT NR 2 COFFEEMAKER TO BE THE CAUSE OF ODOR SMELL. PERFORMED ENGINE MINIMUM IDLE CHECK TO OPERATE AIR CONDITIONING PACKS, NO ODORS OR SMOKE. PLACED AFT NR 2 COFFEEMAKER ON MEL. REMOVED & INSTALLED AFT NR 2 COFFEEMAKER. REMOVED MEL. 2L72 4F RTA28NM 20050817001692005081700169EU 2005 8 17 USAA050893 120050718A5315 FLOORBEAM AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE FS 66 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19109UW19030 1065 FOUND FLOORBEAM CORRODED .5 INCH BY 1 INCH AREA, FRAME 66 RT SIDE AT DOOR CUTOUT. CORROSION LEVEL 1, TASK JA-260-53500. INSTALLED REPAIR ANGLES AND FILLER IAW SRM 53-41-14. (M) 2L72 4F4 FRTA28NM E38NE 20050817001732005081700173EU 2005 8 17 KBM2005F00171 120050228A2120050085 BLOWER SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1 60030NE EVAPORATOR BROKEN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19215LA700 2143 EVAPORATOR BLOWER ASSY, BROKEN BRUSH HOLDER, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050817001742005081700174WP 2005 8 17 ASAA0580407 120050725A5330 SKIN DOUG DC9 DC983 3022083WP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02947AS 53020 OKC - DURING C-CHECK, FOUND FUSELAGE IS DENTED. COLD-WORKED DAMAGED AREA AND INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20060106000142006010600014WP 2006 1 6 DHL2005803554 120051216A53409755584 FITTING DOUG DC8 DC873 302199CWP GE CFM56 CFM562C 13802NE BS 1080 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 ITEM REF. NR. 039052: AFT CARGO COMPT. FITTING CRACKED 1.500 INCH STA 1080.000 L-21R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PAGE 1. REMOVED CRACKED FITTING IAW SRM 51-3-0 AND SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-3-0, SRM 51-1-20D. FOR FITTING FABRICATION SEE JC EA52400002-001-D (W.O. 600014514) 2L74 4F4 FRT4A25 E2GL 20060106000152006010600015WP 2006 1 6 DHL2005803553 120051209A5730 SKIN DOUG DC8 DC873 302199CWP GE CFM56 CFM562C 13802NE RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 ITEM REF. NR. 038581: RT WING LWR SKIN OB FASTENER HOLE CRACKED 0.250 INCH S-64 (MAJOR REPAIR). PERFORMED MAJOR REPAIR AND REMOVED FASTENERS IAW SRM 51-1-20D. TRIMMED OUT DAMAGED AREA IAW SB 57/100 FIG. 5 SHEET 2 OF 5. FABRICATED DOUBLERS (7075T6 AL 0.125 INCH) (7075T6 AL 0.071 INCH) SHIM (7075T6AL 0.040 INCH) FILLER (7075T6 0.250 INCH) 3 INCH MAXIMUM IAW SB 57/100 PAGE 28 FIG.4-5. CLEANED, TREATED AND PRIMED AREA AND PARTS IAW SRM 51-1-8B. INSTALLED FASTENERS IAW SRM 51-1-20D. FABRICATED CONICAL SPACER IAW SRM 51-1-26. TORQUED IAW SRM 51-3-1. FOR LEAK CHECK (FUEL) SEE NR 039053. COMPLIED AD2001-06-04. 2L74 4F4 FRT4A25 E2GL 20060106000172006010600017WP 2006 1 6 DHL2005803533 120051205A53409755536502N FITTING DOUG DC8 DC873 302199CWP GE CFM56 CFM562C 13802NE BS 1075 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 ITEM REF. NR. 039057: AFT CARGO COMPT. FITTING CRACKED 2 INCHES AT STA 1075.000 L-21R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0. REMOVED CRACKED FITTING IAW SRM 51-3-0, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11. INSTALLED FITTING IAW SRM 51-3-0, SRM 51-3-1 PAGE 2, SRM 51-1-20D. 2L74 4F4 FRT4A25 E2GL 20060106000312006010600031NM 2006 1 6 DHL2005760006 120051208A3260 SWITCH BOEING727 7272B7 138407LNM PWA JT8 JT8D17A 52049NE RT MLG DOOR OUT OF ADJUST A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01760AT 21954 WHEN PUTTING LANDING GEAR LEVER FROM UP TO OFF. IT CAUSED THE RT GEAR DOOR LIGHT TO ILLUMINATE ON S.O. PANEL. PERFORMED ABNORMAL PROCEDURE. LT GEAR HANDLE IN UP POSITION FOR LIGHT TO STAY OUT. CLEANED SWITCH PERFORMED ADJ AND TEST IAW MM REF 32-62-11 GRD OP CK GOOD. 2L73 4F4 F A3WE E2EA 20060106000332006010600033NM 2006 1 6 DHL2005783007 120051207A3297 CONNECTOR BOEING727 727227 1384078NM PWA JT8 JT8D17A 52049NE MLG DOOR DIRTY A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01783DH 21999 AFTER TAKEOFF, GEAR HANDLE TO OFF, DOORS LIGHT ON FWD PANEL AND RT DOOR LIGHT ILLUMINATED. PERFORMED ABNORMAL PROCEDURE, RESTORED NORMAL OPERATIONS. CLEANED AND RESEATED CONNECTOR ON RT MLG DOOR SWITCH AND OPS CHECKED GOOD IAW MM 32-62-11. 2L73 4F4 F A3WE E2EA 20060106000432006010600043WP 2006 1 6 UPS05845871 120051212A33505708458503 BATTERY BEACON DOUG DC8 DC871F 302199DWP CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01730UP 46030 EMERGENCY EXIT LIGHTS FAIL TEST. DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT IAW AMM 35-50-01-2. OPERATIONAL TEST GOOD. PN OFF 60-1223-5 SN OFF 248 PN ON 5708458-503 SN ON FTL31. 2L74 4F RT4A25 20060106000512006010600051WP 2006 1 6 DHL2005801015 120051202A3350 BATTERY PACK DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE EMERGENCY LIGHT INOPERATIVE A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH 46033 EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW MM 33-50-1 CHECKED OPERATION OK. 2L74 4F4 FRT4A25 E2GL 20060106000532006010600053NM 2006 1 6 DHL2005747001 120051108A2497 WIRE BOEING727 727224 1384076NM PWA JT8 JT8D15 52051NE COWLING CHAFED A DHLAC ABORTED TAKEOFF H ELECT. POWER LOSS-50 PC TOTAKEOFF 1 SO01747DH 22253 NR 1 GEN FAILED ON T/O ROLL DISCONECTED CSD RTO INFO OAT 16 C PA 4300 SPEED 45 KNOTS MODERATE BREAKING A/C WEIGHT 131,400 REV. THRUST MODERATE. DEFERRED IAW MEL 24-1CAT B CONTROL NR 23128 MC INATALS KPS. TRANSFERED TO DMI GREEN SHEET. C/W SPECIAL PROCEDURES 24-1. REF DMI NR 23128 NR1 GEN FAILED ON T/O ROLL. DISCONNECTED CSD. FOUND GENERATOR FEEDER WIRE CHAFING ON COWLING REMOVED AND REPLACED GENERATOR FEEDER WIRES IAW MM. THIS CLEARS DMI NR 23128. 2L73 4F4 F A3WE E2EA 20060106000542006010600054NM 2006 1 6 DHL2005753003 120051124A335087067001 BATTERY BOEING727 727223 1384074NM PWA JT8 JT8D15 52051NE EMERGENCY LIGHT DISCHARGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01753DH 22468 EMERGENCY EXIT LIGHTS, BATTERY LOW. REPLACED BATTERIES. EMERGENCY EXIT LITES ILLUMINATED- SERVICEABLE REF. 33-26-00, P/N 87067-001. 2L73 4F4 F A3WE E2EA 20060106000572006010600057NM 2006 1 6 SPAA0500081 120051219A5310 STRUCTURE BOEING737 7372T4 1384492NM PWA JT8 JT8D17 52049NE BS 1156 CRACKED A SPAAK NONE O OTHER ININSP/MAINT 1 WP28703S 22529 CRACK ON BS1156 OUTER CHORD RT SIDE WL270. REPAIRED CRACK IAW SB 737-53-1086. 2L72 4F4 F A16WE E2EA 20060106000692006010600069WP 2006 1 6 ASMF200512021 120051226A29108906K1348 SWITCH DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE HYD SYSTEM DAMAGED W ASMFK NONE J WARNING INDICATION ININSP/MAINT 1 SW23204AM 49404 DURING TRANSIT CHECK, THE AUXILIARY HYDRAULIC PUMP DID NOT SHUT OFF, DELIVERING 29 PSI WITH THE SELECTOR IN OFF POSITION. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT CHECK, THE WIRING WAS CHECKED; THE RULER S3-13 TERMINALS WERE CLEANED IAW WDM 29-21-00 AND THE SWITCH WAS REPLACED IAW MM 29-01-01, TESTED CORRECT. 2L72 4F4 FRTA6WE E9NE 20060106000732006010600073NM 2006 1 6 XN0A1284 120051214A2781 SWITCH BOEING727 727227 1384078NM L/E SLAT INOPERATIVE A XN0AD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL2376752 21248 AMBER LE LIGHT ON WITH FLAPS SET TO 15 DEGREES. NR 6 LE SLAT DOES NOT INDICATE EXTEND. REPLACED NR 6 SLAT POSITION INDICATING SWITCH. OPS CHECKS GOOD IAW MM CHAPTER 27-82-11.(STATUS:SUPP/CLOSED). 2L73 4F A3WE 20060106000752006010600075CE 2006 1 6 DXTA200501164 120051219A2550 LIGHT RAYTHNDH125 HAWKER800XP 7150012CE GARRTTTFE731TFE7315BR WP CARGO BAY HOT E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL07833QS 258433 SHORTLY AFTER TAKEOFF (APPROX 3000 FT MSL) THE BAG RED SMOKE /FIRE LIGHT ON THE FO'S FOWARD PANEL CAME ON AND WENT OUT AND SMELLED SMOKE AT THE SAME TIME. FOUND SUITCASE ON LIGHT AND LIGHT ON IN BAGGAGE COMPARTMENT, MOVED SUITCASE. SYSTEM OPS CHECKS GOOD AT THIS TIME. ALL WORK DONE IAW CHAPTER 33-02-00. 2L72 4F4 FRTA3EU E6WE 20060106000792006010600079EA 2006 1 6 SWIA200515997 120051212A2720 TRANSMITTER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE RUDDER FAULTY A SWIAO OTHER N FALSE WARNING ININSP/MAINT 1 NM07919SW UNABLE TO GET FULL RUDDER TRAVEL INDICATION IN EITHER DIRECTION. REPLACED RUDDER POSITION TRANSMITTER IAW MM 27-24-05. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20060106000872006010600087NM 2006 1 6 P5CA0501421 120051207A3244 TIRE BOEING747 74746NF 13848BTNM PWA JT3D JT3D3B 52039NE LANDING GEAR BLOWN A P5CAK NONE EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 EA15452PA 30810 AT TOP OF CLIMB, CREW REPORTED LOUD BANG FOLLOWED BY EICAS MESSAGE (GEAR DOOR) WITH AC VIBRATION AND AIR NOISE. ACCOMPLISHED MMC 14-7 CHECKLIST DOOR CLOSED, NO VIBRATION OR NOISE, SUSPECT BLOWN TIRE IN LT BODY GEAR WELL, AUTO BRAKE TEMP SENSOR NR 5 FAIL. SOFT LANDING COMPELETED. PERFORMED CONDITIONAL INSP IAW 5-51-34. TIRE BURST. REMOVED AND REPLACED NR 5 AND NR 6 TIRE ASSY IAW MM 32-45-01. BODY GEAR DOOR SYSTEM OPS NORMAL. 2L74 4F4 FRTA20WE 1E8 20060106000882006010600088CE 2006 1 6 DJFA2005174 120051214A3411PH1100RWLT PITOT TUBE BEECH MU300 400A 1155402CE PWA JT15 JT15D5 52112NE PITOT/STATIC SYSFAULTY E DJFAO OTHER S AFFECT SYSTEMS CRCRUISE 1 EA23689TA RK327 CREW REPORTED, WHEN THEY BEGAN DESCENT, NOTICED A LOSS OF AIRSPEED. AIRSPEED CONTINUOUSLY DECREASED ON BOTH PRIMARY FLT DISPLAYS, STANDBY INSTRUMENTS. SPEED DECREASED TO ZERO, WENT BLANK ALONG WITH ALTITUDE ON BOTH PRIMARY FLT DISPLAYS. PFD ARTIFICIAL HORIZONS REMAINED ON, BUT WERE INCORRECT. AC WAS DESCENDED USING STANDBY ARTIFICIAL HORIZON, KNOWN PWR SETTINGS, ANGLE OF ATTACK INSTRUMENTS. ALL PITOT, AOA, AND STATIC HEATS WERE CHECKED AND FOUND TO BE FUNCTIONING. SYS BEGAN FUNCTIONING NORMALLY AT FL 180. NO FAULTS WERE FOUND, MAINTENANCE PERFORMED PITOT / STATIC, AIR DATA AND AIRSPEED CHECKS. BOTH PITOT TUBES WERE REPLACED WITH IMPROVED PROBES IAW SB 34-3628. AC WAS RETURNED TO SERVICE. 2H72 4F4 FRTA16SW E25EA 20060106000942006010600094WP 2006 1 6 ABXA050358 120051030A5312 PRESSURE PANEL DOUG DC8 DC863F 302198FWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 CORROSION FOUND UNDER THREE FASTENERS ON PRESSURE WEB IN RT WHEEL WELL, STA. 857, RT BUTT LINE 27. CORROSION FOUND TO BE OUT OF LIMITS ON PRESSURE WEB IN RT WHEEL WELL, STA. 857, RT BUTT LINE 27 IAW SRM 51-1-8 AND 53-2-0. FABRICATED AND INSTALLED REPAIR IAW REA D853-52533. 2L74 4F 4A25 20060106001052006010600105 2006 1 6 XN0A1285 420051216A3422 GYRO AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE COCKPIT INOPERATIVE A XN0AD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL23472AS 125 NR 3 DG INOPERATIVE. PLACED NR3 DG ON DEFERRAL IAW MEL 34-11-07 CAT C DMI NR 51005 PLACARDS INSTALLED. (ORIG/OPEN) 2L72 4F4 FRTA35EU E23EA 20060109000152006010900015WP 2006 1 9 DHL2005803527 120051204A5311 FRAME DOUG DC8 DC873 302199CWP BS 320 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 MAIN CARGO COMPT FRAME CRACKED 0.500" STA 320.000 L-20L TO L-21L. PERFORMED MAJOR REPAIR IAW SRM. TRIMMED OUT DAMAGED FRAME SEGMENT IAW SRM 53-2-0 FIG 2 SHEET 2. PREPARED NEW FRAME SEGMENT, HEAT TREATED FROM 7075T651 TO 7075-0, FORMED AND HEAT TREATED FROM 7075-0 TO 7075T651 IAW SRM. FABRICATED SPLICE ANGLE IAW SRM 53-2-0 FIG 2 SHEET 7, TR 53-110, SRM 53-2-0 FIG 2 SHEET 2. HEAT TREATED SPLICE AND ANGLE 7075-0 TO 7075T62 IAW SRM 53-2-0 FIG 2 SHEET 6, SRM 51-1-1, DPS 7.00 1 REV "BK". CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW SRM 53-2-0 FIG 2 SHEET 2-6, SRM 51-1-20D, SRM 51-3-1, SRM 51-3-2. 2L74 4F RT4A25 20060109000232006010900023WP 2006 1 9 DHL2005803547 120051211A53403755822501N FITTING DOUG DC8 DC873 302199CWP BS 300 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 FWD CARGO COMPT BILGE FITTING CRACKED STA 300.000 BETWEEN L-35L AND L-36. REMOVED CRACKED FITTING IAW SRM 51-1-20D. FABRICATED ANGLE DOUBLER (2EA) (7075-0 0.125") TO INSTALL FITTING IAW SRM 53-2-0. PERFORMED HEAT TREATMENT TO ANGLE DOUBLER FROM 7075-0 TO 7075T6 IAW SRM 53-2-0 FIG 2D SHEET 1, SRM 51-1-1 DPS 7.00-1 REV "BK". CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED FITTING AND ANGLE DOUBLER IAW SRM 53-2-0 FIG. 2D SHEET 2 SRM 51-1-20D, SRM 51-3-0, SRM 51-3-1. 2L74 4F RT4A25 20060109000252006010900025WP 2006 1 9 DHL2005803537 120051203A5315 FLOORBEAM DOUG DC8 DC873 302199CWP BS 834 MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01803DH82180 46123 WING CTR SECTION FLOORBEAM HOLES (2EA) MISDRILLED, STA 834.500 RBL 32" RBL 37.750 (MAIN CARGO COMPT.) PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 11-28-05, DWG NR AA33-53-R06 REV IR DATE 11-16-05. REMOVED FASTENERS IAW SRM 51-1-21. TRIMMED OUT DAMAGED SECTION, FABRICATED REPAIR ANGLE (7075T6 511 0.140") AND (2EA) FILLERS (7075T6 511 0.140") IAW DWG NR AA33-53-R06. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PAGE 9. INSTALLED REPAIR PARTS IAW DWG AA33-53-R06, SRM 51-1-20D, SRM 51-3-1. 2L74 4F RT4A25 20060109000262006010900026WP 2006 1 9 DHL2005802011 120051123A3350313 BULB DOUG DC8 DC873 302199CWP EMERGENCY LIGHT INOPERATIVE A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH 46076 EMERGENCY LIGHTS DISARM LIGHT INOP. REMOVED AND REPLACED EMER LIGHTS DISARM BULB. OPS CHECK OK IAW MM 33-50-0. P/N 313. 2L74 4F RT4A25 20060109000302006010900030EU 2006 1 9 DHL2005362010 120051213A28407069152 AMPLIFIER AIRBUS300 A300B4203 3930306EU FUEL SYSTEM MALFUNCTIONED A DHLABA EMER. DESCENT UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 SO01362DH 84 FUEL ON GAGES AND TOTALIZER APPEARED TO BE GOING AT AN EXTREME RATE. EMERGENCY DECLARED AND LANDING MADE AT PHL. FUEL QTY WENT DOWN 9000 LBA IN ABOUT 30 MIN. REPLACED F/Q AMP OPS CHECK OK PER MM 28-42-00. RAN ENGS 1/2 PER JRH 16.5. NO DEFECTS NOTED. ADDITIONALLY FOUND FUEL DUMP DOOR TO BE SAFETY WIRED CLOSED NO FUEL LEAKS WERE NOTED BY EMERGENCY CREW ON TAXI WAY. 2L72 4F RTA35EU 20060109000332006010900033WP 2006 1 9 DHL2005803538 120051212A5320 CHANNEL DOUG DC8 DC873 302199CWP BS 970 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 LT MLG INBD DOOR ZEE CHANNEL UPPER AFTER CORNER CRACKED 0.500", STA 970.000. REMOVED FASTENERS IAW SRM 51-1-21. PERFORMED STOP HOLE ON CRACK END AND FABRICATED DOUBLER REPAIR (AL7075T6 0.040") IAW SRM 52-2-0, SRM 52-6-1 PAGE 2. CLEANED, TREATED AND PRIMED AREA AND ANGLE REPAIR IAW SRM 51-1-8B. INSTALLED ANGLE REPAIR WITH FASTENERS IAW SRM 52-2-0, SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20060109000472006010900047NM 2006 1 9 QXEA200501857 120051229A213121178041 CONTROLLER DHAV DHC8 DHC8202 2809007NM CABIN PRESSURE MALFUNCTIONED A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09352PH4287 494 SEA FLIGHT NR 2028 DURING TAXI, PRESSURE RATE INDICATOR WOULD SWING BETWEEN +2000 AND -2000 WITH SMALL POWER LEVER ADJUSTMENTS. MAINTENANCE REPLACED CONTROLLER. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20060109000562006010900056WP 2006 1 9 DHL2005809005 120051223A5230 HANDLE DOUG DC8 DC873F 302199FWP CARGO DOOR UNSECURE A DHLAC ABORTED TAKEOFF WJ INADEQUATE Q C WARNING INDICATION TOTAKEOFF 1 SO01809DH 46047 MASTER WARNING LIGHT CAME ON DURING TAKEOFF ROLL. FOUND "B" PIT HANDLE NOT STOWED, PER M/M 52-31-1, OPS CHECK GOOD. 2L74 4F RT4A25 20060109000582006010900058NM 2006 1 9 DHL2005788019 120051011A3260 DOOR BOEING727 727214 138407RNM NLG DOOR OUT OF ADJUST A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01788AT 21958 FWD GEAR DOOR LIGHT AND NOSE GEAR DOOR LIGHT ILLUMINATED DURING CLIMB-OUT (14,000 + 320K) WITH GEAR HANDLE IN OFF POSITION LIGHT GOES OUT WITH GR LEVER IN UP POSITION. ENTERED ON DMI 22767 IAW MEL 32-1 CAT"C". PLACARD INSTALLED. TRANSFER TO DMICONT 22767, GEAR DOORLIGHT AND NOSE GEAR DOOR LIGHT ILLUMINATED DURING CLIMB TO 14000' AND 320 KNOTS WITH GEAR HANDLE IN OFF POSITION, LIGHT GOES OUT WITH GEAR LEVER IN UP POSITION. ADJUSTED NOSE WHEEL WELL DOORS IAW B-727-MM 32-22-1. OPS CHECK GOOD IAW B-727-MM-32-31-0, THIS CLEAR DMI CONT NR 22767. 2L73 4F A3WE 20060109000602006010900060WP 2006 1 9 DHL2005806004 120051128A261287823902 CONNECTOR DOUG DC8 DC873F 302199FWP FIRE DECTECTION FAULTY A DHLAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01806DH 46002 DURING CLIMB-OUT, NR 3 ENG FIRE LIGHT AND FIRE WARNING BELL ACTIVATED INTERMITTENTLY THEN CAME ON STEADY. ENG FIRE CHECKLIST WAS ACCOMPLISHED. ENGINE FIRE LIGHT REMAINED ILLUMINATED. LOOP SWITCH WAS CHANGED. FOUND LOOP "B" ON NR 3 ENGINE TO BE FAULTY. DEFERRED LOOP "B" IAW MEL 26-2-3. DMI 23361. PLACCARD INSTALLED. REFER TO DMI 23361. DURING CLIMB-OUT NR 3 ENG FIRE LIGHT AND FIRE WARNING BELL ACTIVATED INTERMITTENTLY, THEN CAME ON STEADY. ENG FIRE CHECKLIST WAS ACCOMPLISHED. ENGINE FIRE LIGHT REMAINED ILLUMINATED. LOOP SWITCH WAS CHANGED FROM B TO A AND LIGHT WAS EXTINGUISHED. R & R FAULTY CONNECTOR P1-9007. NR 3 ENG FIRE WARNING TESTED GOOD AS PER MM 26-10-1. BOTH "A" & "B" SYSTEMS. THIS CLEARS D2L74 4F RT4A25 20060109000742006010900074EU 2006 1 9 05FDEA04425 120051230A5270 SWITCH AIRBUSA300 A300F4622R 3930360EU E/E BAY DOOR LOOSE A FDEAC ABORTED TAKEOFF J WARNING INDICATION CLCLIMB 1 SO25719FD 388 AVIONICS LIGHT, CHIME CAME ON PASSING 10000, EXECUTED TURNBACK TO KSMP BURN TO MAX LNDG WEIGHT. FOUND AVIONICS DOOR FLUSH TO FUSELAGE AND DOOR LATCH APPROX 1/8 INCH DOWN. ON INSPECTION FOUND DOOR LOCKED SWITCH WITH BROKEN SAFETY WIRE/ RETIGHTENED. SWITCH OPS NORMAL PER A300 MM REF 52-41-14-5. DOOR VERIFIED CLOSED ON DEPARTURE WITH NO LIGHT. 2L72 4F RTA35EU 20060109000762006010900076 2006 1 9 AWXA200501615 420051223A22134051601935 CONTROL PANEL BOEING737 7373G7 1384595NM NR 1 AFCS MALFUNCTIONED A AWXAA UNSCHED LANDING G MULTIPLE FAILURE CLCLIMB 1 WP28157AW4597011041 23779 PHX - AIR TURN BACK - FLT 478 - CREW REPORTED THAT ON INITIAL TAKEOFF AT HEADING SELECT, THE AIRCRAFT LOST HEADING BUG, AIRSPEED BUG, F/O COURSE INDICATOR, STEERING BARS ON FLT DIRECTOR, AND AUTOPILOT. CREW RETURNED TO PHX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE MCP AND THE FCC, CHANNEL B, OPERATIONAL CHECKS WERE GOOD PER TC R1B22001. COMPUTER, FLIGHT CONTROL, AUTOPILOT; PN 4051600-913; SN 86100696; MFG HONEYWELL; TT 57803; TC 40447; TSR 38511. 2L72 4F RTA16WE 20060109000832006010900083NM 2006 1 9 AWXA200501617 120051229A3397BMS13311122 WIRE BOEING757 7572S7 1384962NM EMERGENCY LIGHTSBROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28905AW 23567 PHX - EEL - DURING OVERNIGHT INSPECTION DISCOVERED ROW 13 LT SEAT EMERGERNCY PATH LIGHT OUT. MAINTENANCE REPAIRED BROKEN WIRE AT ROW 13. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA2NM 20060109000872006010900087WP 2006 1 9 05FDEA04281 120051213A5210 REPAIR DOUG DC10 DC1010 3022110WP L1 DOOR UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25563FE 46948 L-1 DOOR UPPER FWD CORNER HAS AN EXTERNAL DOUBLER REPAIR DIM 12" X 6.5". PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 52-10-00 FIG 12A VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2. 2L73 4F A22WE 20060109001052006010900105EU 2006 1 9 AWXA200600006 120051217A5315D5347217220390 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28649AW 803 MCN - DURING INSPECTION DISCOVERED CORROSION ON CABIN FLOORBEAM AT FS 68-60 MM AND BL Y-1225. CORROSION ON FLOORBEAM WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-14 FIG 102. MAINTENANCE REMOVED AND INSTALLED NEW FLOORBEAM AT FR 68-60 MM AND BL Y-1225 IAW AIRBUS 320 SRM 51-72-11. 2L72 4F RTA28NM 20060109001422006010900142NE 2006 1 9 DHL2005805004 220051205A7200 ENGINE DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C1 13802NE NR 3 FAILED A DHLAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION TXTAXI/GRND HDL 1 SO01805DH 46125 NR 3 ENGINE FAILED DURING TAXI IN. TROUBLESHOT NR 3 ENGINE PER MM 71-00-00. INSPECTED INLET AND EXHAUST PER MM 72-00-00, NO DEFECTS FOUND. 2L74 4F4 FRT4A25 E2GL 20060109001432006010900143NM 2006 1 9 DHL2005763005 120051224A5230 WARNING LIGHT BOEING727 727264 138408MNM CARGO DOOR ILLUMINATED A DHLABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 SO01763AT 22983 MAIN CARGO DOOR WARNING LIGHT ILLUMINATED AT FL 250, NO LOSS OF PRESSURIZATION NOTED. PLACED DMI PER MEL 52-4-1 CAT B DDD 12/27/05 DMI 23781 PLACARDS INSTALLED DOOR IS VERIFIED CLOSED & LOCKED. 2L73 4F A3WE 20060109001572006010900157WP 2006 1 9 AALA20050839 120051221A3213 PISTON DOUG DC9 DC982 3022082WP NLG STRUT INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21457AA 49562 ORD - UNABLE TO RAISE LANDING GEAR AFTER TAKEOFF. NOSE WHEEL STEERING INDEX CENTERED BUT NOSE WHEEL WOULD NOT TURN. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR STRUT PISTON. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20060109001602006010900160NM 2006 1 9 CALA0500457 120051230A5330146N3531 SKIN BOEING757 757224 1384958NM BS 1520 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714115 27557 INSPECTION FOUND AIRPHONE ANTENNA SKIN CORRODED AT STA 1520 BETWEEN S28R AND S29R. THE CORRODED SECTION OF SKIN WAS REMOVED. DOUBLERS AND FILLERS WERE INSTALLED IAW SRM 51-40-02 AND SRM 53-00-01, REPAIR 3. 2L72 4F RTA2NM 20060109001622006010900162NM 2006 1 9 CALA0500459 120051228A5320141T5134146 FLOOR SUPPORT BOEING767 767224 1385170NM BS 303-325 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776153 30432 INSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 303 - 325, LBL 32. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-40-02. 2L72 4F RTA1NM 20060109001642006010900164NM 2006 1 9 CALA0500462 120051229A212165771 COOLING FAN BOEING737 737524 1384721NM E&E BAY INOPERATIVE A CALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2713665 28926 THE NORMAL EXHAUST FAN POWER C/B TRIPPED WHILE IN CRUISE PORTION OF FLIGHT TO SFO AT FL 34,000. PRIOR TO THE C/B TRIP THE FLIGHT ATTENDANT ADVISED OF ELECTRICAL BURNING SMELL IN ROW 5 AREA. THE FLIGHT CONTINUED TO SFO WHERE IT LANDED WITHOUT FURTHER PROBLEM. THE NORMAL EXHAUST FAN (AVIONICS AIR COOLING FAN) WAS REMOVED AND REPLACED IAW MM 21-58-12. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20060109001662006010900166 2006 1 9 CALA0500464 420051231A2330285W00294 CONTROL UNIT BOEING777 777224 1385225NM L-3 DOOR SHORTED A CALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2778009 29479 PASSENGERS AND FLIGHT ATTENDANT'S REPORTED A WHIFF OF ELECTRICAL ODOR IN THE CABIN AT A ZONE, B ZONE, AND IN AFT CABIN NEAR ROW 25 WHILE EN ROUTE TO IAH. THE ODOR RETURNED LATER WITH A VISIBLE HAZE. THE APPROPRIATE CHECKLIST WAS RUN AND THE ODOR AND HAZE CEASED. THE AIRCRAFT LANDED AT IAH WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND THE OEU (OVERHEAD ELECTRONICS UNIT) AT L-3 DOOR SHORTED. THE OEU WAS REMOVED AND REPLACED, OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00001SE 20060109001732006010900173EA 2006 1 9 COMA0560776 120051230A5347601R3831229 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA BS 409 CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA29272 7031 LT SIDE SEAT RAIL CORRODED FROM FS 409+18.02 TO FS 409+111.02. REPAIRED LT SIDE SEAT RAIL FROM FS 409+18.02 TO FS 409+111.02 BY REMOVING AND REPLACING SIDE SEAT RAIL IAW BOMBARDIER EO 601R-53-7965A. 2L72 4F RTA21EA 20060109001742006010900174SO 2006 1 9 C2XA05SD034 120051221A3350110049 POWER SUPPLY EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2724103 145645 SDF - LEFT FWD WING EXTERIOR EMERGENCY LIGHT INOP. A/C RELEASED IAW MEL 33-50-00 CAT C 063546. 12/22/2005 REMOVED AND REPLACED BATTERY POWER SUPPLY. 2L72 4F RT 20060109001772006010900177EA 2006 1 9 COMA0560773 120051230A5347601R3831225 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA BS 535-559 CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA29272 7031 RT SIDE SEAT RAIL TRACK CORRODED FROM FS 535.02 TO 559.79. REPAIRED RT SIDE SEAT RAIL FROM FS 535.02 TO 559.79 BY REMOVING AND REPLACING SEAT RAIL IAW BOMBARDIER EO 601R-53-7965A. 2L72 4F RTA21EA 20060110000042006011000004WP 2006 1 10 UPS06845916 120051229A5712 RIB DOUG DC8 DC871F 302199DWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE:C3 RIGHT O/B LEADING EDGE UPPER RIB IS CRACKED AT XFS 802. STOP DRILLED CRACK, FABRICATED REPAIR ANGLE IAW SRM 57-03--01-0, AND INSTALLED REPAIR ANGLE AT RIGHT OUTBOARD LEADING EDGE WING STA XFS 802 IAW SRM 51-1-20D. 2L74 4F RT4A25 20060110000332006011000033WP 2006 1 10 ABXA060002 120051216A53159923668 FLOORBEAM DOUG DC9 DC933F 302207AWP BS 135 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23932AX 47465 CORROSION ON SUBFLOOR AT FLOORBEAM FS 135, LEFT BUTTLINE 14. REPAIRED CORRODED AREA IAW DC9 SRM 53-01. 2L72 4F A6WE 20060110000472006011000047NM 2006 1 10 WX0500048 120050610A339758791 WIRE DOUG MD80 MD83 3023681NM PWA JT8 JT8D* NE EMERGENCY LIGHT INOPERATIVE A WX0AK NONE O OTHER ININSP/MAINT 1 WP19861GA MAINTENANCE REPORTED EMERGENCY FLOOR ESCAPE LIGHTING ROW 5-8 AC/ RT INOPERATIVE. MAINTENANCE INSTALLED NEW LEAD ASSEMBLY WIRE AT FOR ROWS 5-8 AC RT. SYSTEM OPERATIONALLY CHECKS NORMAL IAW MM 33-53-00. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRT E2EA 20060110000682006011000068EA 2006 1 10 SWIA200516079 120051228A5610 WINDSHIELD CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE COCKPIT CRACKED A SWIAO OTHER O OTHER LDLANDING 1 NM07701SK 10133 CAPTAIN'S WINDSHIELD SHATTERED ON TOUCHDOWN. REPLACED CAPTAIN'S WINDSHIELD IAW CRJ 700 MM 56-11-01. 2L72 4F4 FRTA21EA EOOO63EN 20060110001172006011000117NM 2006 1 10 DL73S060013 120051213A5330 SKIN BOEING737 737232 1384475NM PWA JT8 JT8D* NE BS 727B S-18L CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27330DL 23102 A CRACK WAS FOUND IN THE FUSELAGE SKIN. CRACK IS 3 INCH LONG LOCATED JUST AFT OF BS 727B, JUST BELOW S-18L. INSTALLED A DOUBLER IAW ER/A 452077-14AD. 2L72 4F4 FRTA16WE E2EA 20060110001322006011000132SO 2006 1 10 317051392 120050317A78301159PM4156143 PIN GULSTM GULSTMG1159 GIV 3980115SO THRUST REVERSER INOPERATIVE E N93AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO13492QS4814 0399 1392 RT THRUST REVERSER UNLOCK LIGHT ILLUMINATED CLIMBING THRU 17,000 FEET 2L72 4F RTA12EA 20060111000012006011100001NE 2006 1 11 AWXA200501616 220051226A7200 ENGINE BOEING757 7572S7 1384962NM RROYCERB211 RB211535E4 54555NE NR 2 BIRD INGESTION A AWXAC ABORTED TAKEOFF C F.O.D. TOTAKEOFF 1 WP28905AW 23567 CREW ABORTED TAKE OFF AT 140 KNOTS DUE TO NR 2 ENGINE BIRD INGESTION. CREW RETURNED TO THE GATE WITHOUT ANY FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED DAMAGED FAN BLADE AND ANNULUS FILLER ON THE NR 2 ENGINE. REPORTED FOR PRECAUTIONARY PURPOSES. BORESCOOPE WAS PERFORMED IAW AMERICA WEST AIRLES TASK CARD I5M72609, DAMAGE THAT WAS FOUND WAS BLADE TIP DAMAGE TO THE NR 2 FAN BLADE ON THE NR 2 ENG. THE LEADING EDGE TIP WAS BENT .4 WHICH WAS OUT OF LIMTS. 2L72 4F4 FRTA2NM E12EU 20060111000062006011100006EA 2006 1 11 ASOA051019 120051125A3350OL3071BPEGPL LAMP CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27709EV 10068 DURING A GROUND INSPECTION IN SLC, THE EMERGENCY EXIT LIGHT, AT THE RIGHT SIDE EMERGENCY EXIT DOOR, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT SIDE EMERGENCY EXIT DOOR LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060111000082006011100008EA 2006 1 11 ASOA051016 120051124A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27884AS 7513 DURING A C-CHECK IN MCN, THE LT INBOARD AND OUTBOARD FS 280 CLIPS, AT LBL 9, WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT INBOARD AND OUTBOARD FS 280 CLIPS, AT LBL 9, IAW CRJ SRM 51-42-21. (M) 2L72 4F RTA21EA 20060111000102006011100010EA 2006 1 11 ASOA051010 120051123A3211521153 TORQUE LINK CNDAIRCL600 CL6002C10 1390015EA MLG DAMAGED A ASOAO OTHER J WARNING INDICATION CLCLIMB 1 SO27758EV 10210 DURING CLIMB FROM ABQ-SLC, THE CREW RECEIVED A WOW INPUT CAUTION MESSAGE, AND THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO ABS, AND THE EMERGENCY VEHICLES WERE ROLLED. THE AIRCRAFT LANDED SAFELY IN ABS. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR TORQUE LINKS. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE (M) 2L72 4F RTA21EA 20060111000122006011100012NM 2006 1 11 ASAA0570047 120050801A5330143A32524 SKIN BOEING737 737790 13844CNNM FS 490 BENT A ASAAK NONE O OTHER ININSP/MAINT 1 NM02617AS 30542 PAE - BELT LOADER CONTACTED AIRCRAFT FUSELAGE SKIN AT FORWARD CARGO DOOR CUTOUT AFT EDGE. CUT OUT DAMAGE AND INSTALLED REPAIR IAW SRM 53-00-01 NR 24. (M) 2L72 4F RTA16WE 20060111000172006011100017EA 2006 1 11 ASOA051013 120051124A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA BS 625 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27884AS 7513 DURING A C-CHECK IN MCN, THE LEFT CLIP, AT FRAME FS 625, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT CLIP, AT FRAME FS 625, IAW CRJ200 SRM 50-42-21. (M) 2L72 4F RTA21EA 20060111000192006011100019WP 2006 1 11 ASAA0580527 120051003A5522591041449 SKIN DOUG DC9 DC983 3022083WP ELEVATOR DETERIORATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - DURING HV-CHECK, RIGHT ELEVATOR GEARED TAB INBOARD TRAILING EDGE SKIN IS DETERIORATED. SMOOTHED DETERIORATED AREA AND INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20060111000202006011100020NM 2006 1 11 EIA2005261 120051129A5754 SKIN BOEING747 747SR46 1384816NM KRUEGER FLAP DAMAGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09477EV 20784 LT WING LDG EDGE NR 2 KRUEGER FLAP IB HINGE ARE, IB FRAME WEB LOWER SECTION HAS 4 INCH CRACK AT APPROXIMATELY WS 426. REPAIRED NR 2 KRUEGER FLAP IB FRAME WEB LOWER SECTON AT WS 426 PER ECRA 477-57-107-2P, PART 1. AS APPROVED BY BACFAA FORM 8100-9, DATED NOV 22, 2005. 2L74 4F RTA20WE 20060111000212006011100021NM 2006 1 11 EIA2005262 120051218A2410 CSD BOEING747 747212B 1384886NM PWA JT9 JT9D7J 52054NE NR 1 FAILED A EIAAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 NM09482EV 20713 685607 PERFORMED INFLIGHT ENGINE SHUTDOWN DUE TO FAILURE OF NR 1 CSD TO DISCONNECT. FL 290, TAT -17, SAT -47, 312 KTS, .81 MACH, 11:08Z OIL PRESS 20 PSI, OIL TEMP 78 DEG C, DURATION 2:08. PMG VOLTS 52, N1 30 PERCENT, CSD RPM 520, N2 27 PERCENT. DFRL DMI 572 PER MEL 24-1-M, CAT "C" DUE 12/28/05. CSD AND GENERATOR REMOVED PER MM 24-11-0. (ENGINE TSOH 4656.3 CSOH 1004) PLACARD INSTALLED. REMAINS OPEN UNTIL DMI CLEARED. 2L74 4F4 F A20WE E20EA 20060111000222006011100022NM 2006 1 11 EIA2005263 120051219A2611 SMOKE DETECTOR BOEING747 747132 1384882NM LAVATORY MALFUNCTIONED A EIAAK NONE L NO TEST ININSP/MAINT 1 NM09481EV 19896 LAV SMOKE DETECTOR DOES NOT EMIT AUDIBLE TONE ON TEST. TXFRD TO DMI 747 PER MEL 26-27, CAT "D" DUE 4/17/06, PLACARDED. REMAINS OPEN UNTIL DMI CLEARED. 12/29/05 DMI 747, REMOVED AND REPLACED LAV SMOKE DETECTOR IAW EO 26-747-1762-05, OPS NORMAL, DMI CLEARED, PLACARD REMOVED. 2L74 4F A20WE 20060111000252006011100025NM 2006 1 11 EIA2005266 120051227A3350 LIGHT BOEING747 747212B 1384886NM CABIN INOPERATIVE A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 DURING SERVICE CHECK, FOUND ONE EMERGENCY EXIT LIGHT, UPPER DECK R4 INOPERATIVE. REMOVED AND REPLACED UPPER DECK RT EMERGENCY LIGHT PER MM 33-51-00 PAGE 1, OP'S CK OK. 2L74 4F A20WE 20060111000272006011100027NM 2006 1 11 EIA2005268 120051230A3350 LIGHT BOEING747 747212B 1384886NM CABIN INOPERATIVE A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 NR 11 EMERGENCY EXIT LIGHT, R5 DOOR, FOUND INOP ON INSPECTION. REMOVED AND REPLACED NR 11 EMERGENCY EXIT LIGHT PER MM. 2L74 4F A20WE 20060111000362006011100036EA 2006 1 11 SWIA200516084 120051230A2751601R590141 DETECTOR CNDAIRCL600 CL6002B19 1900309EA SKEW MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07594SW 7285 AT THE GATE IN SFO, RECEIVED A FLAPS DEGRADED STATUS MESSAGE. REPLACED SKEW DETECTION UNIT. OPERATIONAL CHECK GOOD, PN 601R59014-1, SN OFF A560. 2L72 4F RTA21EA 20060111000442006011100044NE 2006 1 11 DL75K050798 220051218A7230736101754 MANIFOLD BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 1 ENGINE CRACKED A DALAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 SO27698DL 29911 716391 LEFT ENGINE SURGE AFTER START. REPLACED P4.9 MANIFOLD AND 14TH STAGE BLEED CONVERTER VALVE 2L72 4F4 FRTA2NM E17NE 20060111000462006011100046NE 2006 1 11 DL76L050801 220051218A7261 CARBON SEAL BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 1 ENGINE DAMAGED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO271200K56899 28457 724655 CREW REPORTED SOMKE/SMELL DURING T/O AND AGAIN ON APPROACH INTO ATL. REPLACED FRONT CARBON SEAL ON NR 1 ENGINE. 2L72 4F4 FRTA1NM E24NE 20060111000482006011100048NM 2006 1 11 DL78K050803 120051218A26124739551 MODULE BOEING737 737832 13844CFNM FIRE DETECTION FAILED A DALAO OTHER N FALSE WARNING CRCRUISE 1 SO27396DA 30378 SEVERAL TIMES DURING FLIGHT AFTER AIRBORNE THE RED FWD CARGO LIGHT AND FIRE BELL FLASHED AND RANG. THIS WAS INTERMITTENT AND LASTED BARELY A SECOND OR TWO THEN WENT AWAY. HAPPENED IN A LOOP, B LOOP, AND BOTH LOOPS. NO DETECTOR FAULT ILLUMINATED. REPLACED CARGO FIRE CONTROL PANEL AND FWD CARGO ELECTRONICS UNIT PER M/M. TESTED PER M/M. TEST OK. SYSTEM CHECKS OK. 2L72 4F RTA16WE 20060111000502006011100050NM 2006 1 11 DL73S050805 120051216A5315 FLOORBEAM BOEING737 737247 138448DNM BS 678 RBL 24.8 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27244WA 23518 THE RBL 24.8 FLOORBEAM HAD A PREVIOUS CHANNEL REPAIR INSTALLED THAT DOES NOT COMPLY WITH A RECENT AD. CHANNEL REPLACED PER ER/A 452157-14AD. 2L72 4F A16WE 20060111000522006011100052NM 2006 1 11 DL73S050807 120051219A3230 SENSOR BOEING737 737247 138448DNM RT MAIN GEAR OUT OF RIG A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27237WA 23185 GEAR HANDLE WOULD NOT COME UP. FOLLOWED QRH PROCEDURE TO GETGEAR UP AND THEN DOWN. ADJUST AIR SENSOR SAFETY GAP. 2L72 4F A16WE 20060111000532006011100053NM 2006 1 11 QXEA200501861 120051215A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM BS 404 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 PDX - LEFT HAND OUTBOARD SEAT TRACK NR 1 HAS PITTING INSIDE TRACK AT APPROXIMATELY STATION 404. REPAIRED IAW DHC-8-200 SRM 51-40-00 AND SRM 51-40-11. 2H72 4T RTA13NM 20060111000542006011100054NM 2006 1 11 QXEA200501862 120051215A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM BS 541 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 PDX - LEFT OUTBOARD SEAT TRACK NR 3 HAS MINOR PITTING INSIDE TRACK AT APPROXIMATELY STATION 541. REPAIRED IAW DHC-8-200 SR, 51-40-00 AND SRM 51-40-11. 2H72 4T RTA13NM 20060111000552006011100055NM 2006 1 11 QXEA200501863 120051215A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM BS 467 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 PDX - LEFT OUTBOARD SEAT TRACK NR 2 HAS PITTING CORROSION AT STATION X467.000. REPAIRED IAW DHC-8-200 SRM 51-40-00 AND SRM 51-40-11. 2H72 4T RTA13NM 20060111000562006011100056NM 2006 1 11 QXEA200501865 120051222A5410 BRACKET DHAV DHC8 DHC8202 2809007NM NACELLE WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 PDX - THE NACELLE FRAME BRACKET AND BUSHING FOR THE OPERATING MECHANISM FORWARD MAIN LANDING GEAR DOOR RIGHT NACELLE IS WORN. REPAIRED IAW DHC-8-200 SRM 51-20-26, PAGE 7, PARAGRAPH 5A-1-4. 2H72 4T RTA13NM 20060111000572006011100057NM 2006 1 11 QXEA200501866 120051218A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM BS 254 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 PDX - RIGHT INBOARD SEAT TRACK NR 7 HAS CORROSION AT ABOUT STATION 254. REPAIRED IAW RD 8-53-4473 AND SRM 51-40-11. 2H72 4T RTA13NM 20060111000582006011100058NM 2006 1 11 QXEA200501867 120051214A5340 CLIP DHAV DHC8 DHC8202 2809007NM BS 291 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 PDX - FRAME TO WEB CLIP CRACKED AT FUSELAGE STATION X291.00, LEFT HAND STRINGER 21. REPAIRED IAW DHC-8 200 SRM 51-40-00 AND SRM 51-40-11. 2H72 4T RTA13NM 20060111000592006011100059NM 2006 1 11 QXEA200501868 120051224A5340 DOME NUT DHAV DHC8 DHC8202 2809007NM FUSELAGE FAILED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 PDX - FOUND PANEL 121AL HAS BAD DOME NUT AT FORWARD UPPER CORNER. REPLACED IAW DHC-8-200 SRM 51-40-00. 2H72 4T RTA13NM 20060111000602006011100060NM 2006 1 11 QXEA200501869 120051219A5320 THRESHOLD DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 PDX - FOUND MAIN CABIN DOOR THRESHOLD BEAM SUSPECT CORROSION AT NUTPLATES (X222 TO X220 Z100). REQUIRED UAW DGC-8-200 SRM 51-40-11, PAGE 6, PARAGRAPH 2C. 2H72 4T RTA13NM 20060111000732006011100073NM 2006 1 11 AALA20050845 120051230A3350BPS73 BATTERY PACK BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21384AA 26996 SFO - GREEN LIGHTS FOR EMERGENCY ESCAPE SLIDES FAILED TEST. REPLACED M961 AND M962 BATTERY PACK FOR GREEN LIGHTS FOR EMERGENCY ESCAPE SLIDES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20060111000782006011100078WP 2006 1 11 AALA20050846 120051230A3230 SCHRADER VALVE DOUG DC9 DC982 3022082WP NLG LEAKING A AALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW2116545 53027 DFW INFLIGHT T2340/30DEC, AFTER TAKEOFF UNABLE TO RETRACT NOSE GEAR. AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEAKING SCHRADER VALVE AND SERVICED NOSE GEAR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20060111000792006011100079NE 2006 1 11 AALA20050849 220051231A7200 COMPRESSOR DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE LT ENGINE STALLED A AALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SW21227AA 49177 717860 DFW INFLIGHT T1027/31DEC, LEFT ENGINE COMPRESSOR STALLED ON CLIMB-OUT AT FL200. ENGINE PARAMETER AST IDLE APPEARED NORMAL. ENGINE SHUTDOWN AS PRECAUTION. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED NUMBER ONE ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 F A6WE E9NE 20060111000882006011100088EA 2006 1 11 COMA0560792 120051231A5712601R10203 RIB CNDAIRCL600 CL6002B19 1900309EA RT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA29272 7031 FOUND RT BATT RIB ASSY CRACKED. INCORPORATED REPAIRS TO RT BATT RIB ASSY AT WS 53.60 IAW BOMBARDIER REO 601R-57-51-046 REV B REPAIR NR 1. 2L72 4F RTA21EA 20060109000402006010900040NM 2006 1 9 DHL2005780004 120051020A7711LG80A6 TRANSMITTER BOEING727 727223 1384074NM NR 2 EPR MALFUNCTIONED A DHLAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01780DH 22006 NUMBER TWO ENGINE EPR GAUGE STUCK AT 1.4 INDICATED EPR WITH THRUST LEVERS ADVANCED FOR TAKEOFF. AC WEIGHT 168.4 IAS 65 KTS. OAT 11 PA 4047. DEFERRED PER MEL 77-1 CAT "A" CONTROL NR 22891 ID NR 30127. REF: DMI 22891, NUMBER ENGINE EPR GAGE STUCK AT 1.4 INDICATED EPR WITH THRUST LEVERS ADVANCED FOR TAKEOFF, A/C WEIGHT 168.4,IAS 65KTS, OAT. REPLACED NR 2 ENG EPR TRANSMITTER IAW B727 MM 77-11-11, OPS TEST GOOD, THIS CLEARS DMI NR 22891, PLACARD REMOVED. 2L73 4F A3WE 20060109000552006010900055WP 2006 1 9 DHL2005806003 120051128A2612 SWITCH DOUG DC8 DC873F 302199FWP FIRE LOOP MALFUNCTIONED A DHLAE ENGINE SHUTDOWN N FALSE WARNING CLCLIMB 1 SO01806DH 46002 DURING CLIMB-OUT, NR 3 ENG FIRE LIGHT AND FIRE WARNING BELL ACTIVATED INTERMITTENTLY THEN CAME ON STEADY. ENG FIRE CHECKLIST WAS ACCOMPLISHED. ENGINE FIRE LIGHT REMAINED ILLUMINATED. LOOP SWITCH WAS CHANGED. FOUND LOOP "B" ON NR 3 ENGINE TO BE FAULTY. DEFERRED LOOP "B" IAW MEL 26-2-3. DMI NR 23361. PLACCARD INSTALLED. 2L74 4F RT4A25 20060109000922006010900092EA 2006 1 9 COMA0560760 120051231A5343601R100312 TRUNNION CNDAIRCL600 CL6002B19 1900309EA RT MLG CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA29272 7031 CORROSION FOUND ON MLG FWD TRUNNION LUG AFT FACE. INCORPORATED REPAIRS IAW BOMBARDIER REO 601R-57-21-673 AND INSTALLED 2ND OVERSIZE BUSHING IAW BOMBARDIER REO 601R-57-21-003 REV B. 2L72 4F RTA21EA 20060109000982006010900098EA 2006 1 9 COMA0560751 120051228A5270 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA PAX DOOR ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01479CA 7675 FLIGHT 4991 - CABIN DOOR OUTER HANDLE CAUTION. DEFERRED MAINTENANCE PER MEL. 2L72 4F RTA21EA 20060109000992006010900099EA 2006 1 9 COMA0560752 120051229A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS WARNING LIGHT A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01937CA 7044 FLIGHT 5643 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2L72 4F RTA21EA 20060109001382006010900138NM 2006 1 9 DHL2005748001 120051117A33501000679 LIGHT BOEING727 727225 1384077NM CABIN MALFUNCTIONED A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01748DH 22440 L1 DOOR EMERGENCY EXIT LIGHTS WILL NOT COME ON DURING TEST. REMOVED AND REPLACED EXIT LIGHT ASSY, OPS CK GOOD PER B727 AMM 33-50-101. 2L73 4F A3WE 20060109001472006010900147NM 2006 1 9 MWEA050138 120051220A32605920493507 LANDING GEAR BOEING717 717200 1383700NM MAIN WARNING LIGHT A MWEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31924ME 55190 UNSAFE & GEAR DOOR OPEN LIGHT CAME ON WITH GEAR HANDLE UP. REMOVED AND REPLACED MAIN LANDING GEAR STRUT PISTON, OPERATIONS CHECKED GOOD. 2L72 4F TRA6WE 20060109001502006010900150EU 2006 1 9 AALA20050842 120051225A3350P4010049 BATTERY PACK AIRBUS300 A300B4605R 3930308EU CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW213075A 606 JFK - EMERGENCY LIGHT AT RIGHT ONE AND TWO DOORS INOPERATIVE. REPLACED BATTERY PACK AT RIGHT ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20060110000072006011000007WP 2006 1 10 UPS06845919 120051230A5712 RIB DOUG DC8 DC871F 302199DWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE:C3, LEFT WING O/B LEADING EDGE HAS CRACKED UPPER RIB AT STA XFS 868. STOP DRILLED CRACK IAW SRM 57-02-00, FABRICATED REPAIR ANGLES AND INSTALLED ANGLES AT LEFT WING LEADING EDGE AT STA XFS 868 IAW SRM 57-02-00, 57-03-00, AND SRM 51-1-20. 2L74 4F RT4A25 20060110000112006011000011EA 2006 1 10 COMA0560778 120051230A5347601R38312115 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA BS 444-495 CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA29272 7031 LEFT SIDE SEAT RAIL CORRODED FROM FS 444.02 TO FS 495.98. REPAIRED THE LEFT SIDE SEAT RAIL FROM FS 444.02 TO FS 495.98 BY REMOVING AND REPLACING SEAT RAIL IAW BOMBARDIER EO 601R-53-7965A. 2L72 4F RTA21EA 20060110000162006011000016EA 2006 1 10 COMA0560772 120051230A5347601R3831225 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA BS 535-559 CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA29272 7031 LT SIDE SEAT RAIL CORRODED FROM FS 535.02 TO 559.79. REPAIRED LT SIDE SEAT RAIL FROM FS 535.02 TO 559.79 BY REMOVING AND REPLACING SEAT RAIL IAW BOMBARDIER EO 601R-53-7965A. 2L72 4F RTA21EA 20060110000182006011000018EA 2006 1 10 COMA0560780 120051230A5347601R38312119 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA BS 409-444 CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA29272 7031 LEFT SIDE SEAT RAIL CORRODED FROM FS 409+111.02 TO FS 444.02. REPAIRED LEFT SIDE SEAT RAIL FROM FS 409+111.02 TO FS 444.02 BY REMOVING AND REPLACING SEAT RAIL IAW BOMBARDIER EO 601R-53-7695A. 2L72 4F RTA21EA 20060110000212006011000021EA 2006 1 10 COMA0560784 120051230A5347601R310327 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA BS 409-559 CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA29272 7031 LEFT FLOOR SEAT RAIL CORRODED FROM FS 409+126 TO FS 559+16. REPAIRED LEFT FLOOR SEAT RAIL FROM FS 409+126 TO FS 559+16 BY REMOVING AND REPLACING SEAT RAIL IAW BOMBARDIER EO 601R-53-796A. 2L72 4F RTA21EA 20060110000232006011000023EA 2006 1 10 COMA0560787 120051230A5347601R310329 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA BS 559 CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA29272 7031 RIGHT FLOOR SEAT RAIL CORRODED FROM FS 559+16 TO 559+96. REPAIRED RIGHT FLOOR SEAT RAIL FROM FS 559+16 TO 559+96 BY REMOVING AND REPLACING SEAT RAIL IAW BOMBARDIER EO 601R-53-7965A. 2L72 4F RTA21EA 20060110000272006011000027CE 2006 1 10 DXTA200501163 120051228A3240 BRAKE ASSY CESSNA500 560CESSNA 2076750CE MLG MALFUNCTIONED E DXTAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL07332QS 5600523 BRAKES FUNCTIONED PROPERLY AT LAX & SMO. TOUCHDOWN BRAKING AT CRQ NORMAL. DURING TAXI, BRAKE PEDALS STIFF AND DO NOT REACT IMMEDIATELY. AFTER A FEW MOMENTS LEFT BRAKE GRABS FIRST, THEN RIGHT CAUSING DIRECTIONAL PROBLEMS. FOUND RESERVOIR AT MINIMUM LEVEL. SERVICED RESERVOIR AND BLED BRAKES. TAXI AIRCRAFT, NO BRAKES DRAGGING. OPS CHECK GOOD. ALL WORK DONE IAW CE560 MM CHAPTER 32-30-00. 2L72 4F RTA22CE 20060110000632006011000063EA 2006 1 10 COMA0560788 120051230A5347601R3831225 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE BS 535-559 CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA29272 7031 RT SIDE SEAT RAIL FROM FS 535.02 TO 559.79. REPAIRED RT SIDE SEAT RAIL FROM FS 535.02 TO 559.79 BY REMOVING AND REPLACING SEAT RAIL IAW MFG EO 601R-53-7965A. 2L72 4F4 FRTA21EA E15NE 20060110000692006011000069EA 2006 1 10 SWIA200516078 120051227A2711 CONTROL PANEL CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE AILERON TRIM MALFUNCTIONED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07701SK 10133 AILERON TRIM WILL NOT TURN LWD. REPLACED AILERON TRIM CONTROL PANEL IAW CRJ AMM CHAP 27-12-00. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA EOOO63EN 20060110001332006011000133SO 2006 1 10 140310262005 120051026A32441150SCL5071 TIRE GULSTMG1159 GIV 3980115SO NLG FAILED E N93AK NONE O OTHER TXTAXI/GRND HDL 1 SO13403QS410 1403 LT NOSE TIRE FAILED ON LANDING. 2L72 4F RTA12EA 20060110001352006011000135SO 2006 1 10 13923172005 120050317A78301159PM4156143 PIN GULSTM GULSTMG1159 GIV 3980115SO THRUST REVERSER FAILED E N93AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO13492QS4814 0399 1392 RT THRUST REVERSER UNLOCK LIGHT ILLUMINATED CLIMBING THRU 17,000 FEET. 2L72 4F RTA12EA 20060111000232006011100023NM 2006 1 11 EIA2005264 120051222A5610 WINDOW BOEING747 747132 1384882NM COCKPIT SMOKE A EIAAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM09481EV 19896 R1 WINDOW BEGAN SMOKING HEAVILY ABOUT 1.5 MINUTES AFTER BEING SWITCHED ON. FURTHER INSPECTION REVEALED CIRCUMFERENTIAL CRACKING IN OUTER PANE. DFRL DMI 754 PER MEL 56-1-1, PLACARDS INSTALLED. REMAINS OPEN UNTIL CLEARED. 2L74 4F A20WE 20060111000452006011100045NM 2006 1 11 DLM90050800 120051218A3246 TIRE DOUG MD900 MD900 3027375NM MLG FAILED A DALAO OTHER O OTHER LDLANDING 1 SO27902DA 53382 REPLACED 2 TIRES AND BOTH DACMS. REPAIRED DAMAGE. 1G72 3U NCH19NM 20060111000472006011100047NM 2006 1 11 DL73S050802 120051218A3233 ROD END BOEING737 737247 138448DNM NLG ACTUATOR BROKEN A DALAL ABORTED APPROACH O OTHER LDLANDING 1 SO27237WA 255 23185 NOSE GEAR UNSAFE ALTERNATE EXTEND, GEAR STILL UNSAFE. NOSE GEAR LOCK ACTUATOR BROKEN ROD END. REPLACED LOCK ACTUATOR. 2L72 4F A16WE 20060111000492006011100049NM 2006 1 11 DL73S050804 120051216A5315 FLOORBEAM BOEING737 737247 138448DNM BS 678 LBL 24.8 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27244WA 23518 THE OVERWING FLOORBEAM AT LBL 24.8 WAS PREVIOUSLY REPAIRED WITH A CHANNEL THAT DID NOT MEET THE REQUIREMENTS OF A RECENT AD. REPLACED THE C-CHANNEL REPAIR WITH A NEW CHANNEL. 2L72 4F A16WE 20060111000512006011100051NM 2006 1 11 DL73S050806 120051217A53306545778556 SKIN BOEING737 737232 1384475NM BS 941 STR 24R CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27306DL 23078 THE FUSELAGE SKIN WAS FOUND WITH A 2.7 INCH CRACK AT BS 941, JUST BELOW STR 23R. INSTALLED DOUBLER PER ER/A 452096-14AD. 2L72 4F RTA16WE 20060112000362006011200036NM 2006 1 12 ASAA0580528 120051003A5347593054787 SEAT TRACK DOUG MD80 MD83 3023681NM FS 200-256 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - DURING HV CHECK, FOUND PAX CABIN SEAT TRACK IS CORRODED. REPLACED DAMAGED SECTION. INSTALLED PLUG AND CHANNEL. (M) 2L72 4F RT 20060112000382006011200038NM 2006 1 12 ASAA0580530 120051010A533059360005 SKIN DOUG MD80 MD83 3023681NM FS 754-755 LIGHTNING STRIKEA ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - DURING HV-CHECK, FOUND FUSELAGE HAS LIGHTNING DAMAGE. REMOVED DAMAGED SECTION. INSTALLED INTERNAL REPAIR DOUBLER. (M) 2L72 4F RT 20060112000392006011200039WP 2006 1 12 ASAA0580531 120051019A53305932344501 SKIN DOUG DC9 DC983 3022083WP FS 845-946 RESTRICTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02949AS 53022 SEA LINE CHECK, FOUND FORWARD LEFT OVERWING EMERGENCY EXIT DOOR `WILL NOT OPEN WITHOUT EXCESSIVE FORCE.` ADJUSTED TRIM AROUND DOOR. DOOR COULD THEN BE OPENED, REMOVED WITHOUT EXCESSIVE FORCE. (M) 2L72 4F RTA6WE 20060112000582006011200058WP 2006 1 12 ASAA0580532 120051017A521049559471 STRUCTURE DOUG DC9 DC983 3022083WP PAX DOOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 SEA - LINE CHECK, L-1 FORWARD PAX DOOR DAMAGED/DENTED. REPAIRED PER SRM 53-04. (M) 2L72 4F RTA6WE 20060112000592006011200059WP 2006 1 12 ASAA0580450 120050808A5330593666751 SKIN DOUG DC9 DC982 3022082WP FS 1234-1244 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02935AS 49236 OKC - DURING C-CHECK, FOUND FUSELAGE SKIN DENTED. COLD WORKED DENT. INSTALLED REPAIR DOUBLER. (M) 2L72 4F A6WE 20060112000612006011200061NM 2006 1 12 ASAA0540551 120051016A531565C3394116 FLOORBEAM BOEING737 7374Q8 138447QNM FS 312 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - FOUND CORROSION ON FLOORBEAM. REMOVED AND REPLACED FLOORBEAM UPPER CHORD AT BS 312 WL 208, LBL 65-23, IAW 737-400 SRM 53-10-51. (M) 2L72 4F RTA16WE 20060112000622006011200062NM 2006 1 12 ASAA0540556 120051018A531565C3394225 FLOORBEAM BOEING737 7374Q8 138447QNM FS 328 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - FOUND CORROSION ON FLOORBEAM. REMOVED CORRODED UPPER CHORD, FABRICATED AND INSTALLED NEW CHORD, REPAIR SPLICES, AND ANGLES IAW 737-400 SRM 53-10-51. (M) 2L72 4F RTA16WE 20060112000632006011200063NM 2006 1 12 ASAA0540553 120051018A5320651630440 WEB BOEING737 7374Q8 138447QNM FS 211.8 GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - FRAME GOUGED ON WEB. REMOVED DAMAGED WEB, FABRICATED AND INSTALLED REPAIR PARTS IAW 737-400 SRM 51-70-03. (M) 2L72 4F RTA16WE 20060112000792006011200079NM 2006 1 12 ASAA0540550 120051015A532065C807351 SILL BOEING737 7374Q8 138447QNM FS 947-996 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - FOUND CORROSION ON MOPSILL. REMOVED AND REPLACED MOPSILL IAW 737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060112000812006011200081WP 2006 1 12 ASAA0580448 120050808A53405956034505 CLIP DOUG DC9 DC982 3022082WP FS 1287 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02935AS 49236 OKC - DURING C-CHECK, FOUND CARGO TRACK-TO-FRAME TIE DOWN CLIP CORRODED. REPLACED CLIP. (M) 2L72 4F A6WE 20060112000952006011200095WP 2006 1 12 ASAA0580446 120050808A53205936597U505 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FS 636 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02935AS 49236 OKC - DURING C-CHECK, FOUND CABIN FLOOR PANEL SUPPORT CORRODED. REPLACED SUPPORT. (M) 2L72 4F A6WE 20060112000982006011200098EA 2006 1 12 COMA0560790 120051231A5730601R100414 SKIN CNDAIRCL600 CL6002B19 1900309EA RT WING DENTED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA29272 7031 RT WING SKIN DENTED 1" DIA BY .033 DEEP AT WS 131.25. REPAIRED RT WING SKIN AT WS 131.25 BY BLENDING DAMAGED AREA, PERFORMED EDDY CURRENT ROTO PEEN AND TOUCHED-UP REWORKED AREA IAW BOMBARDIER REO 601R-57-21-671. 2L72 4F RTA21EA 20060112001002006011200100EA 2006 1 12 COMA0560793 120051231A5730601R100463 SKIN CNDAIRCL600 CL6002B19 1900309EA LT WING CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA29272 7031 LT AFT WING PLANK FUEL BOOST PUMP CUT-OUT LANDING CORRODED. REPAIRED LT AFT WING PLANK FUEL BOOST PUMP CUT-OUT LANDING BY BLENDING DAMAGED AREA, PERFORMED EDDY CURRENT, ROTO PEEN AND APPLIED PROTECTIVE TREATMENT AND FINISH IAW BOMBARDIER EO 601R-57-7968. 2L72 4F RTA21EA 20060113000092006011300009NM 2006 1 13 AWXA200600023 120051221A5347D57130147203 SEAT TRACK AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28814AW 1281 SAL - DURING BC4 CHECK DISCOVERED LEVEL 2 CORROSION ON SEAT TRACK FROM FR 38 TO FR 40 AND Y-1292. RE-WORK AREA WAS FOUND TO BE OUT OF LIMITS IAW 51-31-15 FIG 101. MAINTENANCE REMOVED AND INSTALLED NEW SEAT TRACK FROM FR36 TO FR41 AND Y-1292 IAW AIRBUS 319 SRM 51-72-11. 2L72 4F RTA28NM 20060113000112006011300011NM 2006 1 13 AWXA200600025 120051221A5347D57130147202 SEAT TRACK AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28814AW 1281 SAL - DURING BC4 CHECK DISCOVERED LEVEL 2 CORROSION ON SEAT TRACK FROM FR 37+1 TO FR 40+2 AND Y1292. RE-WORK AREA WAS FOUND TO BE OUT OF LIMITS IAW 53-31-15 FIG 103. MAINTENANCE REMOVED AND INSTALLED NEW SEAT TRACK FROM FR36 TO FR41 AND Y1292 IAW AIRBUS 319 SRM 51-72-11. 2L72 4F RTA28NM 20060113000122006011300012NM 2006 1 13 AWXA200600026 120051223A5347D57130147200 SEAT TRACK AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28814AW 1281 SAL - DURING BC4 CHECK DISCOVERED LEVEL 2 CORROSION ON SEAT TRACK FROM FR36 TO FR 41 AND Y765. RE-WORK AREA WAS FOUND TO BE OUT OF LIMITS IAW 51-31-15 FIG 101. MAINTENANCE REMOVED AND INSTALLED NEW SEAT TRACK FROM FR36 TO FR41 AND Y765 IAW AIRBUS 319 SRM 51-72-11. 2L72 4F RTA28NM 20060113000152006011300015NM 2006 1 13 AWXA200600029 120051223A5315D5311282600101 FLOORBEAM AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28814AW 1281 SAL - DURING BC4 CHECK DISCOVERED CORROSION ON FLOORBEAM LOCATED AT FR 16 AND Y503.2. RE-WORK AREA WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 319 SRM 53-11-14. MAINTENANCE REMOVED AND INSTALLED NEW FLOORBEAM FROM FR 12 TO FR 16 AND Y503.2 IAW AIRBUS 319 SRM 51-72-11. 2L72 4F RTA28NM 20060113000172006011300017NM 2006 1 13 AWXA200600031 120051223A5320534800443204 SILL AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28814AW 1281 DURING BC4 CHECK DISCOVERED CORROSION ON THE LOWER SILL AT FR 68-3 AND Y 1732. MAINTENANCE CUT OUT DAMAGED AREA IAW AIRBUS 319 SRM 53-41-14 FIG 201. FABRICATED REPAIR ANGLE AND REPAIR FILLER IAW AIRBUS 319 SRM 53-41-14 FIG 201. INSTALLED FABRICATED REPAIR PARTS FROM FR 66 TO FR 68 AND Y 1732 IAW AIRBUS 319 SRM 53-41-14 PAGE 201 TO 212, FIG 201, SHEET 3. 2L72 4F RTA28NM 20060113000182006011300018NM 2006 1 13 AWXA200600032 120051227A5320D53112622200 COVER AIRBUSA319 A319132 3930340NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28814AW 1281 SAL - DURING BC4 CHECK DISCOVERED CRACK ON JOINT COVER, FLOOR STRUCTURE SUPPORT, LOCATED AT FR 14 AND Y0.04. MAINTENANCE REMOVED AND INSTALLED NEW JOINT COVER AT FR 14 AND Y-0.040 IAW AIRBUS 319 SRM 51-42-11 AND DRAWING D53112829. 2L72 4F RTA28NM 20060113000272006011300027EU 2006 1 13 05FDEA04095 120051203A5101 REPAIR AIRBUS310 A310203 3930313EU FUSELAGE UNKNOWN A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25424FE 241 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NO. POS PT1. PREVIOUS REPAIR INSTALLED AT FUSELAGE LEFT HAND SIDE, L2 FORWARD DOOR FRAME AT STA 4551, FS 73A, STR 20 LT TO STR 24 LT. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. 2L72 4F RTA35EU 20060113000282006011300028WP 2006 1 13 05FDEA04285 120051213A5101 REPAIR DOUG DC10 DC1010 3022110WP FUSELAGE UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25563FE 46948 MAIN CABIN CTR FUSELAGE L3 DOOR JAMB AFT HAS AN EXTERNAL DOUBLER REPAIR STA 1311 DIM 11" BY 12" BOTTOM PART. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 53-50-00 FIG 19 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO# 8-5100-7-5001 P2. 2L73 4F A22WE 20060113000292006011300029WP 2006 1 13 05FDEA04286 120051213A5700 REPAIR DOUG DC10 DC1010 3022110WP NR 1 SLAT UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25563FE 46948 FOUND LEFT WING NR 1 SLAT HAS AN EXTERNAL DOUBLER REPAIR AT THE LOWER AFT EDGE OF THE OUTER SKIN DIM. 8.5" BY 5". PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 57-10-00 FIG 84 VOL 1 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO# 8-5100-7-5001 P2. 2L73 4F A22WE 20060113000342006011300034WP 2006 1 13 05FDEA04266 120051213A5330 SKIN DOUG DC10 DC1010 3022110WP FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 DURING REMOVAL OF THE SKIN, FOUND 1 CRACK 1.25" LONG ON TEE CAP AT STA 595 Z-63 LT SIDE. ACCOMPLISHED IAW EA NR 8-5310-88854. 2L73 4F A22WE 20060113000352006011300035EU 2006 1 13 05FDEA04267 120051213A7830 THRUST REVERSER AIRBUS310 A310324 3930206EU NR 2 INOPERATIVE A FDEAF ACTIVATE FIRE EXT. J WARNING INDICATION TOTAKEOFF 1 SO25815FD 638 DURING ENGINE RUNUP FOR T/O AT APPROX 40 PERCENT N1 REV NR 2 UNLOCK LT CAME ON. TRIED AGAIN WITH SAME RESULT MEL. ACN RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-C CATEGORY: C EXPIRATION: 19DEC05 "MEL 78-30-01-C: ENGINE (IDENTIFY 1 OR 2) 2 THRUST REVERSER - INOP. THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POSITION." 2L72 4F RTA35EU 20060113000362006011300036WP 2006 1 13 05FDEA04268 120051213A5740 FITTING DOUG DC10 DC1010 3022110WP WING NICKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 DURING ACCOMPLISHED NRC N00197, AFTER REMOVAL FITTING P/N ARC0329-1 FOUND ON ANGLE FITTING (ATTACHED ON WING REAR SPARE) DEEP NICK (LONG 7/16" LARGE 1/4" DEEP 3/32"). FABRICATED AND INSTALLED 1 BUSHING AND 1 ANGLE ON DAMAGED T/E BEAM LOWER CAP IAW EA# 8-5710-88857. 2L73 4F A22WE 20060113000372006011300037WP 2006 1 13 05FDEA04269 120051213A5320 INTERCOSTAL DOUG DC10 DC1030F 3023504WP BS 879 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 FWD CARGO COMPT AT STA 879 RT AT LONG 39 AFTER REMOVAL INTERCOSTAL WITH N/R C40124 FOUND ON STRUT 1 CRACK 2.50" LONG. REMOVED PLATE IAW SRM 51-33-01 PAGE 34/47 VOL 2. TRIMMED OUT CRACKED FLANGE. FABRICATED PART IAW DETAIL PART TRAVELER F161706/3 IAW SRM 53-00-01 FIG 9. INSTALLED REPAIR ANGLE P/N F161706/3 IAW SRM 53-00-01 FIG 9 VOL 1. 2L73 4F RTA22WE 20060113000382006011300038WP 2006 1 13 05FDEA04270 120051213A5101 REPAIR DOUG DC10 DC1030F 3023504WP FUSELAGE UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 PERFORMED INSPECTION IAW EO# 8-5100-7-5001-1D FOUND DOUBLER LENGTH 12" WIDTH 9" ON TOP INTERNAL BULKHEAD NLG AT STA 560 Z-38 X11. NO ACTION TAKEN IAW EO NR 8-5100-7-5001 P1 E3 ATTACHMENT "A" NOTE 3 TREATED AND PRIMED AREA IAW SRM 57-21-01 VOL 1. 2L73 4F RTA22WE 20060113000842006011300084EU 2006 1 13 IXXA0500175S 220050123A7200 SHROUD DOUG DC8 DC871F 302199DWP CFMINTCFM56 CFM563C 13802EU NR 1 ENGINE WORN A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING ROUTINE C-CHECK FOUND NUMBER 1 ENGINE FAN ABRADABLE SHROUD WORN BEYOND LIMITS AT 12:00, AND 1:00 POSITIONS. REMOVED ACCOUSTICAL PANELS, POTTED REPAIR AREAS, APPLIED FIBERGLASS OVERLAYS, CLEANED AND SEALED AREAS. REINSTALLED ACCOUSTICAL PANELS IAW CFM MM 72-23-02. 2L74 4F4 FRT4A25 E21EU 20060113000862006011300086WP 2006 1 13 IXXA0500177S 120050123A5321 FLOOR PANEL DOUG DC8 DC871F 302199DWP ZONE 200 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING ROUTINE C-CHECK FOUND FLOORING IN COURIER AREA CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED FASTENERS, FABRICATED NEW FLOOR PANEL, ALODINED, PRIMED, INSTALLED NEW FLOOR PANEL AND FASTENERS IAW DC8 DRAWING 564827, DC8 SRM 51-1-8, 53-2-0, 51-3-0, 51-1-21, AND 53-7-1. 2L74 4F RT4A25 20060113000882006011300088NM 2006 1 13 2005UALA01399 120051205A3350362624 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29178UA 24385 EEL INOP SEAT 48 LT AND 55 LT. *S/D* REPLACED EEL LIGHT. 2L74 4F4 FRTA20WE E24NE 20060113000892006011300089NM 2006 1 13 2005UALA01242 120051031A2497 WIRE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE BURNED A UALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 WP29540UA 25252 WORKING INOP BLD FOUND CB'S FOR WATER HEATERS & DRAIN MAST POPPED. FOUND BURNED WIRES. *S/D* WIRES BURNED THRU AT STA 1681 , WL 208 DUE TO CHAFE THRU BY HOSE BAND CLAMP FROM IMPROPERLY ROUTED WIRES AND VENT HOSES WHICH LED TO ARCING AND BURN-THRU OF WIRES. BOEING NOTIFIED, AND NO PREVIOUS OCCURRENCES WERE NOTED. STRICTLY DUE TO IMPROPER ROUTING OF VENT HOSES AND WIRING BUNDLE WITH IMPROPER STAND-OFFS, AS VERIFIED IN IPC 38-31-56-004, FIG G. THREE OTHER AIRCRAFT INSPECTED FOR PROPER ROUTING, AND WERE IN ACCORDANCE WITH IPC ABOVE. 2L72 4F4 FRTA2NM E17NE 20060113000902006011300090WP 2006 1 13 IXXA0500159S 120050120A534036410041N ATTACH FITTING DOUG DC8 DC871F 302199DWP STA 870 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING A ROUTINE C-CHECK FOUND LONGERON ATTACH FITTING AT STATION 870 LONGERON 24 LEFT CORRODED. ORIGINAL THICKNESS .125 REMOVED .025 MATERIAL, FITTING OUT OF LIMITS. DURING CORROSION REMOVAL FOUND LONGERON 24 LEFT CRACKED AT STATIION 870. REMOVED FASTENERS, DAMAGED FITTING, AND CRACKED LONGERON SECTION. FABRICATED REPAIR PARTS, RECEIVED NEW FITTING, DRILLED, CLEANED, TREATED, PRIMED AND INSTALLED REPAIR PARTS IAW DAC DRAWING 3641004, DC8 SRM 53-2-0, 51-1-20D, 51-1-24, 51-1-8 MD NDT SPM 06-10-01.001. 2L74 4F RT4A25 20060113000912006011300091WP 2006 1 13 IXXA0500161S 120050120A534036410042N ATTACH FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IXXAO OTHER O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING ROUTINE C-CHECK FOUND ATTACH FITTING CORRODED AT RIGHT WHEEL WELL STATION XCW44.00 LONGERON 24 RIGHT. CLEANED AREA, UPON FURTHER INSPECTION SEVERAL CRACKS NOTED VERIFIED BY INSPECTION. REMOVED FASTENERS AND DAMAGED FITTING. RECEIVED NEW ATTACH FITTING AND REPAIR PARTS, LOCATED DRILLED, TRIMMED, ALODINED, PRIMED AND INSTALLED REPAIR PARTS IAW DC8 MM 53-2-0, 51-1-24, 51-1-8, 51-1-20D, AND 51-3-1. 2L74 4F RT4A25 20060113000932006011300093WP 2006 1 13 IXXA0500164S 120050120A5320 STIFFENER DOUG DC8 DC871F 302199DWP ZONE 100 CRACKED A IXXAO OTHER O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING ROUTINE C-CHECK FOUND THREE CRACKED STIFFENERS IN THE FORWARD PIT RIGHT HAND FORWARD BULKHEAD. REMOVED FASTENERS, AND DAMAGED PARTS. MANUFACTURED REPLACEMENT PARTS. LOCATED, DRILLED, ALODINED, PRIMED, AND INSTALLED REPLACEMENT PARTS IAW DC8 SRM 53-2-0, 51-1-8, AND 51-1-21. 2L74 4F RT4A25 20060113000952006011300095WP 2006 1 13 IXXA050185S 120050127A5240 RIB DOUG DC8 DC871F 302199DWP ZONE 800 CRACKED A IXXAO OTHER O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING ROUTINE C-CHECK FOUND FORWARD RIGHT HAND SERVICE DOOR UPPER INTERNAL RIB CRACKED. STOP DRILLED CRACK. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED AND INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-0, 52-3-0, 51-9-0 AND 51-1-8. 2L74 4F RT4A25 20060113000972006011300097WP 2006 1 13 IXXA0500187S 120050125A5753 SUPPORT ANGLE DOUG DC8 DC871F 302199DWP ZONE 600 CRACKED A IXXAO OTHER O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING ROUTINE C-CHECK FOUND RIGHT WING OUTBOARD FLAP INBOARD EDGE AT STATION XW 129 TRAILING EDGE SUPPORT ANGLE CRACKED. REMOVED FASTENERS, AND DAMAGED SUPPORT ANGLE. FABRICATED NEW SUPPORT ANGLE. LOCATED, DRILLED, TREATED, PRIMED AND INSTALLED NEW SUPPORT ANGLE AND FASTENERS IAW DC8 SRM 51-1-8, 51-7-1, AND 51-1-20D. 2L74 4F RT4A25 20060113000992006011300099WP 2006 1 13 IXXA0500165S 120050131A5720 ANGLE DOUG DC8 DC871F 302199DWP BS 790 CRACKED A IXXAO OTHER O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING ROUTINE C-CHECK FOUND SUPPORT ANGLE CRACKED AT THE RIGHT WHEEL WELL STATION 790 LONGERON 23 RIGHT SWING DOWN PANEL. MANUFACTURED REPAIR ANGLES. LOCATED, DRILLED, TRIMMED, ALODINED, PRIMED, AND INSTALLED REPAIR ANGLES IAW DC8 DRAWING 5643404, DC8 SRM 53-2-0, 51-1-8, AND 51-1-20D. 2L74 4F RT4A25 20060113001012006011300101WP 2006 1 13 IXXA0500167S 120050120A5330 SKIN DOUG DC8 DC871F 302199DWP ZONE 100 GOUGED A IXXAO OTHER O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING ROUTINE C-CHECK FOUND EXTERNAL FUSELAGE GOUGED AT STATION 280 LONGERON 30 RIGHT. REMOVED GOUGE. ORIGINAL MATERIAL THICKNESS IS .071 AFTER DAMAGED REMOVED MATERIAL THICKNESS IS .051 OUT OF LIMITS. FABRICATED DOUBLER, LOCATED, DRILLED, ALODINED, PRIMED, AND INSTALLED DOUBLER IAW DC8 SRM 51-1-8, 53-4-1, 53-2-1, AND 51-1-20D. 2L74 4F RT4A25 20060113001032006011300103WP 2006 1 13 IXXA0500189S 120050125A5753 DOUBLER DOUG DC8 DC871F 302199DWP ZONE 500 TORN A IXXAO OTHER O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING ROUTINE C-CHECK FOUND LEFT WING INBOARD FLAP OUTBOARD FORWARD HINGE FAIRING PANEL DOUBLER TORN. REMOVED FASTENERS AND DAMAGED DOUBLER. FABRICATED NEW DOUBLER, LOCATED, DRILLED, TREATED, PRIMED, INSTALLED NEW DOUBLER WET WITH SEALANT, AND INSTALLED FASTENERS IAW DC8 SRM, 51-1-21, 57-2-0, 51-1-8, 51-1-11, AND 51-1-21. 2L74 4F RT4A25 20060110000292006011000029WP 2006 1 10 ABXA060004 120051218A533059248167 SKIN DOUG DC9 DC933F 302207AWP KEEL BS 600 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23932AX 47465 CRACK IN FUSELAGE KEEL SKIN AT STA 600 BETWEEN LONGERON 30 - 29 LEFT. REPAIRED AREA IAW DC9 SRM 53-04 AND REA D953-52948MR. 2L72 4F A6WE 20060110000662006011000066EA 2006 1 10 QXEA200600013 120050105A3250530133 CONTROLLER CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE NLG STEERING MALFUNCTIONED A QXEAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM09600QX9383 10005 ON FLT 2453, STEERING INOP CAUTION MESSAGE AFTER ARMING THE SYSTEM. ACCOMPLISHED RESET PROCEDURE IAW MX CONTROL. MESSAGE WENT AWAY FOR APPROX 30 SECONDS. ACCOMP RESET PROCEDURE A SECOND TIME IAW MTX CONTROL AND RETURNED TO GATE. MX INTERROGATED MDC FAULT HISTORY. FOUND (NWS ECU NO NWS A BUG TO DCU) (L NWS ACT LVDT OPEN OR SHORT) (R NWS ACT LVDT OPEN OR SHORT). REMOVED AND REPLACED RT STEERING ACTUATOR/LVDT REF TASK 30-52-01-000-801 AND TASK 32-52-01-400-801-A01. LEAK CHECK OF ACTUATOR GOOD, OPS TEST IAW 30-51-00-710-801, OPS CHECK GOOD. REMOVED AND REPLACED PILOTS CONTROL HAND WHEEL, GROUND TAXI AIRCRAFT, TAXI CHECK GOOD. OPERATIONAL CHECK FLIGHT GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20060110000752006011000075EA 2006 1 10 SWIA200516072 120051230A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FLT SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07924SW8296 8296 7681 FOUND SPOILERONS FAULT STATUS MSG. REPLACED RT SPOILERON IB PCU IAW CRJ MM 27-62-01. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20060110000772006011000077EA 2006 1 10 SWIA200516070 120051228A335020131A BATTERY CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT DISCHARGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07954SW1627 1627 7815 FOUND EMERGENCY FLOOR LIGHTING (2 SECTIONS) INOP. REPLACED NR 3 ELBP IAW CRJMM 33-51-04. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20060110000822006011000082EA 2006 1 10 SWIA200516065 120051231A492038004883 APU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE ODOR A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM07963SW252227095 7865 AFTER STARTING THE APU ON TAXI IN CABIN FILLED WITH STRONG SMELL OF FUEL. REPLACED APU ASSY IAW 49-20-01. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20060110000872006011000087EA 2006 1 10 SWIA200516060 120051226A2740 SWITCH CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE YOKE MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07910SW 7566 NR 1 STAB WOULD NOT ENGAGE. REPLACED BOTH PILOT YOKE STAB DISCONNECT SWITCHES. OPERATIONAL CHECK GOOD IAW MM 27-41-00. 2L72 4F4 FRTA21EA E15NE 20060110001342006011000134SO 2006 1 10 0139203172005 120050317A78301159PM4156143 PIN GULSTM GULSTMG1159 GIV 3980115SO THRUST REVERSER INOPERATIVE E N93AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO13492QS4814 0399 1392 RT THRUST REVERSER UNLOCK LIGHT ILLUMINATED CLIMBING THRU 17,000 FEET 2L72 4F RTA12EA 20060111000242006011100024NM 2006 1 11 EIA2005265 120051223A2697 CONNECTOR BOEING747 747273C 1384896NM SMOKE DETECTOR DIRTY A EIAAK NONE L NO TEST ININSP/MAINT 1 NM09470EV 20653 FOUND MAIN DECK CARGO COMPARTMENT SMOKE DETECTOR, ZONE 5, DET A INOPERATIVE. TXFR'D TO DMI NR 869, PLACARD ID NR 060160, PER MEL 26-11 CAT C, AND ADVISED A/C MX CONTROL. DMI CONTINUES UNTIL CLEARED. 12/25/05, AMPLIFIER FOR SMOKE DETECTOR 5A PLUG CLEANED, OPS CK CW PER MM 26-14-02, OP'S CK OK, PLACARD REMOVED. 2L74 4F A20WE 20060111000262006011100026NM 2006 1 11 EIA2005267 120051230A3350 LIGHT BOEING747 747212B 1384886NM CABIN INOPERATIVE A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 NR 10 EMERGENCY LIGHT, L1 DOOR, FWD SILL, FOUND INOP ON INSPECTION. REMOVED AND REPLACED EMERGENCY SILL LIGHT AT L1 DOOR PER MM. 2L74 4F A20WE 20060111000282006011100028NM 2006 1 11 EIA2005269 120051230A3350 LIGHT BOEING747 747212B 1384886NM CABIN INOPERATIVE A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 NR 3 UPPER DECK STAIR EMERGENCY LIGHT FOUND INOP ON INSPECTION. REMOVED AND REPLACED NR 3 UPPER DECK EMERGENCY LIGHT ABOVE STAIRS. 2L74 4F A20WE 20060111000722006011100072WP 2006 1 11 AALA20050844 120051228A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21464AA 49594 LGA - EMERGENCY EXIT LIGHT AT FORWARD AISLE INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHT AT FORWARD AISLE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20060111000742006011100074WP 2006 1 11 AALA20050847 120051230A3397 CONTACT DOUG DC9 DC982 3022082WP BATTERY PACK DIRTY A AALAK NONE L NO TEST ININSP/MAINT 1 SW217521A 49898 RDU - OVERHEAD EMERGENCY LIGHTS AT ROW 29 INOPERATIVE. CLEANED CONTACTS ON EMERGENCY LIGHT BATTERY PACKS FOR OVERHEAD EMERGENY LIGHTS AT ROW 29. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20060111000762006011100076WP 2006 1 11 AALA20050848` 120051230A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21237AA 49253 LGA - EMERGENCY CEILING LIGHT AT ROWS 7 TO 10 INOPERATIVE. REPLACED BATTERY PACK AT B5101 FOR EMERGENCY CEILING LIGHTS AT ROWS 7 TO 10. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20060112000602006011200060WP 2006 1 12 ASAA0580451 120050808A53305936434129 SKIN DOUG DC9 DC982 3022082WP FS 254 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02935AS 49236 OKC - DURING C-CHECK, FOUND FUSELAGE SKIN DENTED. COLD-WORKED DENT. INSTALLED REPAIR DOUBLER. (M) 2L72 4F A6WE 20060112000802006011200080WP 2006 1 12 ASAA0580447 120050808A532059360342 SUPPORT DOUG DC9 DC982 3022082WP FS 1145 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02935AS 49236 OKC - DURING C-CHECK, FOUND SUPPORT STRAP CORRODED. REPLACED STRAP. (M) 2L72 4F A6WE 20060112001012006011200101NE 2006 1 12 545412022005 220051202A72616047T63P04 CARBON SEAL CNDAIRCL604 CL604 1900301EA GE CF34 CF34* NE NR 1 ENGINE LEAKING E J7SAA UNSCHED LANDING KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW05324FX6319 5454 872725 STRONG OIL SMELL NOTICED IN COCKPIT DURING CLIMB-OUT. MAINTENANCE WAS ABLE TO VERIFY DISCREPANCY AND FOUND THE NR 1 CARBON SEAL ON THE LEFT ENGINE FAILED. REPLACED SEAL, OPS CHECK NORMAL. 2L72 4F4 FRTA21EA E15NE 20060112001022006011200102CE 2006 1 12 4513412032005 120051203A323274691 ACTUATOR LEAR 45 45LEAR 5170805CE MLG DOOR MALFUNCTIONED E J7SAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW05423FX4289 134 RIGHT MAIN LANDING GEAR DOOR WILL NOT RETRACT. MX ADVISED THAT THE RT DOOR SWITCH ON THE RT INBOARD GEAR DOOR ACTUATOR IS NOT OPENING WITH POWER ON. THE SWITCH COMES AS PART OF THE ACTUATOR ASSEMBLY. THE ACTUATOR HAS BEEN PLACED ON ORDER AT THIS TIME. 2L72 4F RTT00008WI 20060112001032006011200103EA 2006 1 12 545412132005 120051213A3220 LANDING GEAR CNDAIRCL604 CL604 1900301EA NOSE OBSTRUCTED E J7SAA UNSCHED LANDING CJ F.O.D. WARNING INDICATION CLCLIMB 1 SW05324FX 5454 ON TAKEOFF, NOSE GEAR WOULD NOT RETRACT. RETURNED TO DEPARTURE POINT WITH UNEVENTFUL LANDING. MAINTENANCE FOUND LARGE TRAFFIC CONE STUCK BETWEEN THE TWO NOSE WHEELS WHICH PREVENTED RETRACTION. NO DAMAGE TO AIRCRAFT. OPERATIONAL TEST PERFORMED OF LANDING GEAR SYSTEM WITH NO DEFECTS NOTED. 2L72 4F RTA21EA 20060112001042006011200104CE 2006 1 12 4509512182005 120051218A3232 SWITCH LEAR 45 45LEAR 5170805CE MLG DOOR ACT UNSERVICEABLE E J7SAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW05409FX 095 LANDING GEAR WOULD NOT EXT IN NORMAL OR AUX MODE, REQUIRED FREE FALL TO EXT AND LOCK. PLACED AIRCRAFT ON JACKS, PERFORMED A PRELIMINARY INSPECTION OF BOTH LT AND RT MAIN GEAR WELLS FOUND CONNECTOR S97P1 FOUND LT DOOR SWITCH 1/2 TURN BACKED OFF. RESEATED CONNECTOR. TECHS FOUND THE LT GEAR DOOR ACTUATOR SWITCH BAD. REPLACED LEFT AND RIGHT MAIN GEAR DOOR ACTUATORS. OPS CHECK NORMAL. 2L72 4F RTT00008WI 20060112001052006011200105CE 2006 1 12 4521211282005 120051128A2750 DRIVE ASSY LEAR 45 45LEAR 5170805CE TE FLAP MALFUNCTIONED E J7SAO OTHER SF AFFECT SYSTEMS FLT CONT AFFECTED APAPPROACH 1 SW05434FX 212 ON APPROACH, SELECTED FLAPS 8 DGS, AUX HYDRAULIC PUMP ON. HEARD THUMPING NOISE, THEN AMBER L/R HYDRAULIC PRESSURE LOW CAS. SELECTED HYDRAULIC PAGE, SAW L AND R AMBER MAIN PUMPS WITH MAIN PRESSURE DROPPING THROUGH 1900 PSI. STARTED ABNORMAL CHECKLIST, THUMPING STOPPED, PRESSURE INCREASED TO 3070 PSI, CAS MESSAGE AND AMBER PUMPS CLEARED. AMBER FLAPS FAULT ILLUMINATED. FLAPS STUCK AT 2 DGS DOWN. RAN ABNORMAL CHECKLIST FOR BOTH PROBLEMS. NORMAL GEAR EXTENSION ACQUIRED, NORMAL BRAKE PRESSURE ACHIEVED, BUT COULD NOT CORRECT FLAP FAULT. LANDED WITH 2 DGS FLAPS DOWN. MAINTENANCE REPLACED THE FLAP PDU. OPS CHECK NORMAL 2L72 4F RTT00008WI 20060113000132006011300013NM 2006 1 13 AWXA200600027 120051223A5315D5347218920400 FLOORBEAM AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28814AW 1281 SAL - DURING BC4 CHECK DISCOVERED CORROSION ON FLOORBEAM LOCATED AT FR 68 AND Y-1162. RE-WORK AREA WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 319 SRM 53-00-14. MAINTENANCE REMOVED AND INSTALLED NEW FLOORBEAM FROM FR 68 TO FR 69 AND Y-1162 IAW AIRBUS 319 SRM 51-42-11. 2L72 4F RTA28NM 20060113000162006011300016NM 2006 1 13 AWXA200600030 120051223A5320D53480043205 SILL AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28814AW 1281 SAL - DURING BC4 CHECK DISCOVERED CORROSION ON LOWER SILL OF THE R2 DOOR AT FR 66 AND Y-1732. MAINTENANCE CUT OUT THE DAMAGED AREA IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 25-5341-05365-ES2. FABRICATED REPAIR ANGLES AND FILLER IAW AWA ER NO. 25-5341-05365-ES2 AND AIRBUS 319 SRM 53-41-14 REPAIR 6. INSTALLED FABRICATED REPAIR PARTS AT FS 66 TO FS 68 AND Y-1732 IAW AWA ER NR 25-5341-05365-ES2. 2L72 4F RTA28NM 20060113000192006011300019EA 2006 1 13 COMA0560794 120051231A5730601R100464 SKIN CNDAIRCL600 CL6002B19 1900309EA RT WING CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA29272 7031 FOUND RT AFT WING PLANK, FUEL BOOST PUMP CUT-OUT LANDING CORRODED. REPAIRED RT AFT WING PLANK FUEL BOOST PUMP CUT-OUT LANDING BY BLENDING DAMAGED AREA, PERFORMED EDDY CURRENT, ROTO PEEN AND APPLIED PROTECTIVE TREATMENT AND FINISH IAW BOMBARDIER EO 601R-57-7968. 2L72 4F RTA21EA 20060113000302006011300030WP 2006 1 13 05FDEA04287 120051213A5101 REPAIR DOUG DC10 DC1010 3022110WP FUSELAGE UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25563FE 46948 PYLON NR 1 HAS AN EXTERNAL DOUBLER REPAIR ON THE UPPER SPAR WEB AFT SECTION BETWEEN STA YN 410 AND YN 417 DIM 7" BY 3.5". PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 54-20-00 FIG 34 VOL 1 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO# 8-5100-7-5001 P2. 2L73 4F A22WE 20060113000312006011300031WP 2006 1 13 05FDEA04288 120051213A5700 REPAIR DOUG DC10 DC1010 3022110WP RT WING UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25563FE 46948 RT WING OUTBOARD FLAP LOWER SURFACE HAS A DOUBLER REPAIR ON TWO RIBS AT T/E PANEL BETWEEN STA XOF 580 AND XOF 588 DIM 13" BY 8". PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 57-10-00 FIG 85 VOL 1 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO# 8-5100-7-5001 P2. 2L73 4F A22WE 20060113000332006011300033NM 2006 1 13 05FDEA04265 120051212A3260 ACCESSORY UNIT BOEING727 72722 1384002NM MLG FAILED A FDEAJ DUMP FUEL A FLAME/FIRE CRCRUISE 1 SO25188FE 19081 DURING TEST FLIGHT, HAD NO LEFT MAIN GEAR INDICATION. PERFORMED GOOD RING OUT PER FED EX WDM 32-64-02, 32-64-01. REPLACED LANDING GEAR ACCESSORY UNIT AND PERFORMED GOOD FUNCTIONAL TEST PER FED EX MM 20-10-017-2, 32-09-111-5. 2L73 4F A3WE 20060113000922006011300092WP 2006 1 13 IXXA0500162S 120050126A5330 SKIN DOUG DC8 DC871F 302199DWP STA 680 - 780 CORRODED A IXXAO OTHER O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING ROUTINE C-CHECK, FOUND CORROSION ON EXTERIOR FUSELAGE SKIN FROM STATION 680 TO STATION 780 BETWEEN LONGERON 32 LEFT AND LONGERON 32 RIGHT. REMOVED FASTENERS, AND ANTENNA TO GAIN ACCESS. REMOVED CORROSION. ORIGINAL SKIN THICKNESS .125 AFTER CORROSION REMOVED SKIN THICKNESS WAS .056, OUT OF LIMITS. MANUFACTURED, ALODINED, PRIMED AND INSTALLED REPAIR DOUBLERS IAW DC8 SRM 51-3-8, 51-1-20D, 51-1-8, 53-2-0, AND 53-2-1. 2L74 4F RT4A25 20060113000942006011300094WP 2006 1 13 IXXA0500184S 120050125A53473657503501 SEAT TRACK DOUG DC8 DC871F 302199DWP ZONE 200 WORN A IXXAO OTHER O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING ROUTINE C-CHECK FOUND FLIGHT DECK COURIER SEAT TRACKS FORWARD AND AFT WORN. REMOVED FASTENERS, AND DAMAGED SEAT TRACKS. RECEIVED NEW SEAT TRACKS, LOCATED, DRILLED AND INSTALLED NEW SEAT TRACKS IAW DC8 SRM 51-1-24 AND 51-3-1. 2L74 4F RT4A25 20060113000962006011300096WP 2006 1 13 IXXA0500186S 120050126A5753 ANGLE DOUG DC8 DC871F 302199DWP ZONE 500 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING ROUTINE C-CHECK FOUND LEFT WING OUTBOARD FLAP INBOARD CENTER AFT INSIDE PANEL NUMBER 551 AREA ANGLE CRACKED AND 3 FASTENERS MISSING. REMOVED FASTENERS, AND ANGLE. FABRICATED NEW ANGLE, LOCATED, DRILLED, TREATED, PRIMED AND INSTALLED NEW ANGLE AND INSTALLED MISSING FASTENERS IAW DC8 SRM 51-1-21, 57-7-0, AND 51-1-8. 2L74 4F RT4A25 20060113000982006011300098WP 2006 1 13 IXXA0500188S 120050203A5347 SEAT TRACK DOUG DC8 DC871F 302199DWP ZONE 200 GOUGED A IXXAO OTHER O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING ROUTINE C-CHECK FOUND MAIN CABIN SEAT TRACK GOUGED AT STATION 235 LEFT BUTT LINE 45.5. GOUGE IS OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS AND FASTENERS IAW DC8 SRM 53-2-3, 51-1-21, 51-1-8, 51-3-0, AND 51-3-1. 2L74 4F RT4A25 20060113001002006011300100WP 2006 1 13 IXXA0500166S 120050120A5720 ANGLE DOUG DC8 DC871F 302199DWP 785 LONGERON CRACKED A IXXAO OTHER O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING ROUTINE C-CHECK FOUND SUPPORT ANGLE CRACKED AT THE RIGHT WHEEL WELL STATION 785 LONGERON 23 RIGHT SWING DOWN PANEL. MANUFACTURED REPAIR ANGLES. LOCATED, DRILLED, TRIMMED, ALODINED, PRIMED, AND INSTALLED REPAIR ANGLES IAW DC8 DRAWING 5643404, DC8 SRM 53-2-0, 51-1-8, AND 51-1-20D. 2L74 4F RT4A25 20060113001022006011300102WP 2006 1 13 IXXA0500168S 120050202A7830 BUSHING DOUG DC8 DC871F 302199DWP THRUST REVERSER MIGRATED A IXXAO OTHER O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING A ROUTINE C- CHECK FOUND NUMBER 3 ENGINE OUTBOARD THRUST REVERSER TRANSITION COWL BUSHING MIGRATED AT FRICTION PAD. REPAIRED MIGRATING BUSHING BY REMOVING FASTENERS, REMOVING DAMAGED EDGE ANGLE, FABRICATING NEW ANGLE AND BONDING INTO PLACE. ALODINED, PRIMED, INSTALLED FASTENERS AND SEALED REPAIR AREA IAW TIMCO REO G10300, CFM MM 78-31-20, 78-30-00, 78-31-40 SERVICE BULLETIN CFM56 78-022, DC8 SRM 51-2-21 AND 51-3-1. 2L74 4F RT4A25 20060113001042006011300104WP 2006 1 13 IXXA0500202S 120050126A7110 SHROUD DOUG DC8 DC871F 302199DWP NR 3 INLET WORN A IXXAO OTHER O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING ROUTINE C-CHECK FOUND, NR 3 ENGINE INLET FAN ABRADABLE SHROUD WORN, APPROXIMATELY 40 PERCENT MATERIAL MISSING. REMOVED 2 ACOUSTICAL PANELS, AND DAMAGE. CLEANED AREA AND APPLIED FIBERGLASS REPAIR IAW CFM56 MM 72-33-00. 2L74 4F RT4A25 20060113001052006011300105WP 2006 1 13 IXXA0500190S 120050127A5210 WEB DOUG DC8 DC871F 302199DWP ZONE 800 CRACKED A IXXAO OTHER O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING ROUTINE C-CHECK FOUND LEFT HAND PASSENGER DOOR FORWARD WEB JUST ABOVE OPENING MECHANISM CRACKED. STOP DRILLED CRACK AND FABRICATED DOUBLER. LOCATED, DRILLED, TREATED, PRIMED AND INSTALLED DOUBLER AND FASTENERS IAW DC8 SRM 52-3-2, 52-2-0 51-1-21, AND 51-1-8. 2L74 4F RT4A25 20060113001072006011300107WP 2006 1 13 IXXA0500192S 120050204A57535701446501 VANE DOUG DC8 DC871F 302199DWP ZONE 500 DELAMINATED A IXXAO OTHER O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING ROUTINE C-CHECK FOUND LEFT HAND FLAP STATION 219 FLAP VANE DELAMINATED. REMOVED AND REPLACED FLAP VANE, RIG CHECK GOOD IAW DC8 MM 27-51-14. 2L74 4F RT4A25 20060113001092006011300109WP 2006 1 13 IXXA0500194S 120050125A5753 HINGE DOUG DC8 DC871F 302199DWP ZONE 600 GOUGED A IXXAO OTHER O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING ROUTINE C-CHECK FOUND RIGHT HAND INBOARD FLAP, INBOARD HINGE, OUTBOARD ARM GOUGED AND CHAFED. REMOVED DAMAGE, ORIGINAL THICKNESS WAS .250, REMOVED .081 MATERIAL, REMAINING THICKNESS .169, OUT OF LIMITS. FABRICATED REPAIR PARTS, LOCATED, DRILLED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 57-7-0, 51-1-8, 51-9-0, DC8 DRAWING SR0827008, AND DC8 SERVICE BULLETIN 27-279. 2L74 4F RT4A25 20060113001112006011300111WP 2006 1 13 IXXA050197S 120050126A5753 DOUBLER DOUG DC8 DC871F 302199DWP ZONE 500 GOUGED A IXXAO OTHER O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING ROUTINE C-CHECK FOUND LEFT OUTBOARD TRAILING EDGE FLAP UPPER SKIN REPAIR PATCH GOUGED AT CENTER HINGE. REMOVED FASTENERS AND DAMAGED DOUBLER. FABRICATED NEW DOUBLER, LOCATED, DRILLED, TREATED, PRIMED, INSTALLED NEW DOUBLER, AND FASTENERS IAW DC8 SRM 51-1-21A, 57-2-0, AND 51-1-8. 2L74 4F RT4A25 20060113001132006011300113WP 2006 1 13 IXXA050199S 120050125A2731 TRIM TAB DOUG DC8 DC871F 302199DWP ZONE 300 DENTED A IXXAO OTHER O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING ROUTINE C-CHECK FOUND LEFT ELEVATOR TAB DENTED AT MID SKIN. REMOVED TAB, DISASSEMBLED, CLEANED INSPECTED, AND REPLACED TRAILING EDGE WEDGE. REINSTALLED TAB ON LEFT ELEVATOR IAW DC8 SRM 51-1-21, 51-1-22, 51-1-8B, 51-4-5, 51-3-0, DC8 DRAWING 5702579 AND DC8 OHM 27-16-1. 2L74 4F RT4A25 20060113001152006011300115WP 2006 1 13 IXXA0500201S 120050125A5347 SEAT TRACK DOUG DC8 DC871F 302199DWP ZONE 200 WORN A IXXAO OTHER O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING ROUTINE C-CHECK FOUND MAIN CABIN SEAT TRACK AT STATION 1220 -F- WORN. REMOVED DAMAGE FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-3, AND 51-1-8. 2L74 4F RT4A25 20060113001262006011300126NE 2006 1 13 2006UALA00008 220051231A7261 ENGINE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 1 LEAKING A UALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP29460UA 1248 V10165 FLIGHT DIVERTED DUE TO NR 1 ENGINE OIL LEAK. NUMBER 5 BEARING CARBON SEAL HOUSING WAS FOUND TO BE OUT OF DIMENSION, DEFLECTED, AND SCORED. IT PERMITTED AN OIL PATH TO EXIST AT THE HOUSING/TURBINE EXHAUST CASE(TEC) ATTACHMENT FLANGE. ONCE PAST THE FLANGE OIL MADE ITS WAY INTO THE GASPATH. OIL DID NOT GET BY THE CARBON SEAL BECAUSE NO COKING/STREAKING WAS EVIDENT ON THE ID OF THE T6 INNER ROTATING AIRSEAL. 2L72 4F4 FRTA28NM E40NE 20060113001312006011300131NM 2006 1 13 UPS05645891 120051221A5753 FLAP BOEING767 76734AF 1385212NM GE CF6 CF680C2B7 NE LT WING OB T/E DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01304UP 27242 INSPECTION TYPE: N/A LT WING OB T/E FLAP DELAMINATED. A/C FERRIED TO HEAVY MX FACILITY FOR REPAIR. RMVD LW OB FLAP IAW 27-51-20-4. RMVD LW OB FLAP OB TE DEFLECTION CNTRL CARRIAGE FR DMGD FLAP & INSTLLD RPLCMNT FLAP IAW MM 27-51-24-4. RMVD LW OB FLAP IB/OB AFT FAIRING SCTN FR DMGD FLAP & INSTLLD RPLCMNT FLAP IAW 27-51-16-4. OK TO INSTLL RPLCMNT FLAP. INSTLLD RPLCMNT FLAP IAW MM 27-51-20-4. FUNC TESTED GOOD PER MM 27-51-20-4. 2L72 4F4 FRTA1NM E13NE 20060113001332006011300133NM 2006 1 13 AWXA200501573 120051126A5315143N501413 FLOORBEAM BOEING757 7572S7 1384962NM PWA PT6 PT6A67D NE FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28901AW 23321 MAJOR REPAIR - DURING C-00 CHECK DISCOVERED FLOORBEAM CRACKED, 1.5 INCHES LONG, AT BS 700, WL 206 AND BL 24R. MAINTENANCE CUT OUT DAMAGE ON FLOORBEAM IAW ENGINEERING REPAIR NR 19-5335-05346-RC3. FABRICATED REPAIR ANGLES AND REPAIR SECTION IAW AWA ER NR 19-5335-05346-RC3. INSTALLED FABRICATED REPAIR PARTS IAW AWA ER NR19-5335-05346-RC3. 2L72 4F4 TRTA2NM E26NE 20060113001362006011300136EU 2006 1 13 AWXA200501576 120051204A5320D53480043202 SILL AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE LT SIDE CABIN CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28604AW 1196 DURING BC4 CHECK DISCOVERED CORROSION ON THE LOWER SILL AT FR 68-3 INCHES AND Y1732 ON THE LT SIDE OF CABIN. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14 FIG 101. FABRICATED ANGLE AND FILLERS IAW SRM 53-41-14. INSTALLED FABRICATED REPAIR PARTS AT LOWER SILL FR 68-3 INCHES AND Y1732 IAW SRM 53-41-14 FIG 201. 2L72 4F4 FRTA28NM E40NE 20060113001412006011300141EU 2006 1 13 AWXA200501581 120051204A5320D5347218820400 BEAM AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE LT FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28604AW 1196 DURING BC4 CHECK DISCOVERED LEVEL 2 GALVANIC CORROSION LOCATED ON BEAM ASSEMBLY AT FR 68 AND Y1162. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14 FIG 102. REMOVED AND INSTALLED NEW BEAM ASSEMBLY FROM FR 68 TO FR 69 AND Y1162 SRM 51-42-11. 2L72 4F4 FRTA28NM E40NE 20060113001432006011300143NM 2006 1 13 0501926624 120051018A5320 INTERCOSTAL BOEING747 747251B 1384892NM BS 340 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01624US 21706 DURING M-CHECK FOUND CRACKS IN INTERCOSTAL ATTACHED SUPPORT CLIP AT BS 340 STR 26L. REPAIRED PER EA 66-205519. 2L74 4F A20WE 20060113001452006011300145 2006 1 13 IXXA0500215O 420051227A2310 RADIO DOUG DC8 DC871F 302199DWP HF SYSTEM MALFUNCTIONED A IXXAA UNSCHED LANDING O OTHER CLCLIMB 1 SW11828BX84495999 45993 ON FLIGHT 362 FROM KTOL TO KEWR NR 1 HF CONTINOUSLY ATTEMPTED TO TUNE ON ALL FREQUENCES WITH THE SAME RESULTS. THEN HF RADIO NR 2 WAS KEYED TO TUNE, THE AUTOPILOT KICKED OFF CAUSING THE AIRCRAFT TO YAW AND PITCH. DUE TO INTENDED FLIGHT PLAN, CREW ELECTED TO RETURN TO DEPARTURE STATION KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE CHECKED NR 1 HF, NO DEFECTS WERE NOTED. CALLED AIR INC ON NUMEROUS FREQUENCIES AND CHECKED GOOD. CHECKED NR 2 HF WITH AUTOPILOT ON AND OFF, NO DEFECTS WERE NOTED. CALLED AIR INC ON NUMEROUS FREQUENCIES AND CHECKED GOOD. WORK WAS PERFORMED PER ALL APPLICABLE MANUALS AND AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20060113001492006011300149NM 2006 1 13 QXEA200501815 120051208A5347 SEAT TRACK BOMBDRDHC8 DHC8402 1390042NM PWC 150 PW150A EA FSX94.8 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09403QX 4037 LT OB SEAT TRACK HAS NICKS, SCRATCHES AND CORROSION ON TOP RAIL AND IN CHANNEL BETWEEN STA. X32.4 AND X94.8. MAINTENANCE REPAIRED IAW SRM 51-42-05 AND 51-40-10. 2H72 4T4 TRTA13NM E00062EN 20060113001502006011300150NM 2006 1 13 QXEA200501817 120051206A5347 SEAT TRACK BOMBDRDHC8 DHC8402 1390042NM PWC 150 PW150A EA GALLEY FLOOR CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09403QX 4037 LT OB SEAT TRACK HAS CORROSION ON TOP FLANGE AND IN CHANNEL BETWEEN STA X659.5 AND X664.5. PART OF CORROSION IS UNDER GALLEY HOLD DOWN BRACKET. MAINTENANCE REPAIRED IAW 51-42-05 AND SRM 51-40-10. 2H72 4T4 TRTA13NM E00062EN 20060113001522006011300152NM 2006 1 13 AWXA200501605 120051221A3350 SWITCH AIRBUSA319 A319132 3930340NM IAE V2524 V2524A5 NE OVERHEAD PANEL DEFECTIVE A AWXAK NONE O OTHER CLCLIMB 1 WP28813AW 1223 CREW REPORTED THAT THE EMERGENCY EXIT LIGHT CAME ON SHORTLY AFTER DEPARTURE. CAPTAIN TURNED THE LIGHTS OFF THEN ARMED THEM AGAIN. THE EMERGENCY EXIT LIGHT RE-ILLUMINATED. CREW SWITCHED THE LIGHTS OFF UNTIL LANDING. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT SWITCH ON THE OVERHEAD PANEL, 4WL, IAW AMM 31-14-25-860-002. OPERATIONAL CHECKS WERE NORMAL. **SUPPLEMENTAL** WILL BE SUBITTED ONCE PART INFORMATION BECOMES AVAILABLE. 2L72 4F4 FRTA28NM E40NE 20060113001562006011300156NM 2006 1 13 QXEA200501813 120051208A5347 SEAT TRACK BOMBDRDHC8 DHC8402 1390042NM PWC 150 PW150A EA FSX170 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09403QX 4037 RT OB SEAT TRACK NR 17 HAS PITTING CORROSION INSIDE CHANNEL AT APPROX FS X170. MAINTENANCE REPAIRED IAW RD 8-53-884, SRM 51-42-05 AND SRM 51-40-15. 2H72 4T4 TRTA13NM E00062EN 20060113001572006011300157WP 2006 1 13 ABXA050379 120051221A793041800044 TRANSMITTER DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE NR3 ENGINE DEFECTIVE A ABXAE ENGINE SHUTDOWN Y ENGINE STOPPAGE CRCRUISE 1 GL23816AX22 46093 NR 3 ENGINE OIL PRESSURE WAS 37 TO 39 PSI IN CRUISE. RETARDED THROTTLE TO IDLE TO COMPLY WITH ABNORMAL PROCEDURES, OIL PRESSURE WAS 35 PSI. OIL PRESSURE DROPPED TO 34 PSI, SECURED NR 3 ENGINE AT 0850 HRS - 10 PSI WINDMILLING OIL PRESSURE. 0855 HRS OIL PRESSURE ON WINDMILLING ENGINE ZERO FOR REMAINDER OF FLIGHT (0909 ON TIMER) WINDMILL N1 RPM 16 PERCENT, N2 19 PECENT, OIL QUANTITY 16 QUARTS. REMOVED AND REPLACED NR 3 ENGINE OIL PRESSURE TRANSMITTER IAW MM 79-32-01-2-0003. RAN ENGINE TO TAKEOFF POWER. OPS CHECK NORMAL, OIL PRESSURE WITHIN LIMITS. NO LEAKS NOTED. 2L74 4F4 F 4A25 1E8 20060113001592006011300159SO 2006 1 13 F05012 120051203A33501317 LAMP EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL AFT CABIN BURNED OUT A FDKAK NONE O OTHER NRNOT REPORTED 1 SW07828MJ 145218 THE AIRCRAFT WAS RUN IN CAE LAST NIGHT AND THE CREW FOUND THAT THE AFT CABIN EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP. 2L72 4T4 FRTT00011ATTE6CH 20060113001602006011300160WP 2006 1 13 ABXA050381 120051221A3231 CABLE DOUG DC9 DC941 302207NWP PWA JT8 JT8D15 52051NE NG STOP CABLE BROKEN A ABXAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL23954AX 47612 AFTER TAKEOFF AT GEAR RETRACTION, LOUD NOISE AND SEVERE VIBRATION FROM THE NOSE GEAR AREA WAS FELT. RECYCLED THE LANDING GEAR AND A LOUD BANG WAS HEARD. RETURNED TO THE AIRPORT AND MADE A NORMAL LANDING WITH ALL THE CORRECT INDICATIONS. FOUND THE NOSE GEAR DOOR STOP CABLE BROKEN. REPLACED CABLE AND RIGGED DOORS IAW MM 32-22-01-2-0004. 2L72 4F4 F A6WE E2EA 20060113001612006011300161NM 2006 1 13 MWEA050139 120051220A57305912156343 PANEL BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE RIGHT WING BENT A MWEAK NONE O OTHER ININSP/MAINT 1 GL31918ME 55180 RT WING TRAILING EDGE PANEL FORWARD OF RT IB SPOILER IS BENT UP. REMOVED DAMAGE INSTALLED DOUBLER. 2L72 4F4 FTRA6WE E00061EN 20060113001622006011300162WP 2006 1 13 ASMF200512018 120051221A5270 DOOR DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE FALSE INDICATIONW ASMFC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW23501AM 49188 AIRCRAFT RETURNED TO PLATFORM DURING TAKE OFF, AFTER NOSE LANDING GEAR ROTATION, THE ELECTRICAL/ELECTRONIC COMPARTMENT OPEN DOOR LIGHT TURNED ON. DURING MAINTENANCE REVISION, THE DOOR WAS DETECTED OPEN WITH THE SAFETY PINS ACTIVATED. THE ELECTRICAL/ELECTRONIC COMPARTMENT DOOR OPERATION WAS CHECKED ELECTRICALLY AND MECHANICALLY AND THE OPEN/CLOSE DOOR TEST WAS PERFORMED IAW MM 52-70-07 AND MM 52-43-00 RESPECTIVELY, ALL CORRECT. 2L72 4F4 F A6WE E9NE 20060113001632006011300163NE 2006 1 13 XN0A1286 220051221A7261 RELIEF VALVE BOEING727 727227 1384078NM PWA JT8 JT8D9A 52048NE NR 1 ENG OUT OF ADJUST A XN0AD RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL2373751 21247 NR 1 ENGINE OIL PRESSURE WENT TO REDLINE ON THROTTLE. TO TAKEOFF POWER. ADJUSTED OIL PRESSURE RELIEF VALVE TO 43 PSI AT IDLE IAW MM 72-00. OPS AND LEAK CHECKS GOOD AT IDLE. (ORIG/CLOSED) 2L73 4F4 F A3WE E2EA 20060113001642006011300164NE 2006 1 13 ASMF200501201 220051222A7200JT9D217A ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE LT SIDE VIBRATION W ASMFK NONE JE WARNING INDICATION VIBRATION/BUFFET CRCRUISE 1 SW231003Y5617211837 48068 708437 CAPTAIN REPORTED THAT DURING FLIGHT WITH EPR BETWEEN 1.0 AND 1.2 IN THE LT ENGINE; VIBRATION AMPLITUDE OCCASIONALLY WITH PEAKS FROM 4 TO 0 AND WHEN THE LT ENGINE WAS SHUTDOWN, VIBRATION WAS FELT IN ALL THE AIRCRAFT. THE LT ENGINE CHIP DETECTORS, ACCESSORIES, PNEUMATIC LINES, VIBRATION ABSORBERS WERE INSPECTED, BEING CORRECT. THE LT ENGINE BOROSCOPE INSPECTION WAS PERFORMED AND NO DAMAGES WERE FOUND. DURING THE ENGINE TEST WAS DETECTED THE VIBRATION AT 1.17 OF EPR. THE LT ENGINE WAS REPLACED AND TESTED IAW MM 71-00-02, ALL CORRECT. 2L72 4F4 F A6WE E9NE 20060113001692006011300169EU 2006 1 13 MALA050881 120051215A3210 LIGHT BAC 146 AVRO146RJ85A1500097EU COCKPIT ACTIVATED A MALAA UNSCHED LANDING J WARNING INDICATION ININSP/MAINT 1 GL15518XJ E2337 RT MLG UNSAFE LIGHT REMAINED ON AND RED LIGHT IN HANDLE ILLUMINATED. AIR RETURNED. NO FURTHER INFO AT THIS TIME. 2H74 4F RTA49EU 20060113001722006011300172EA 2006 1 13 A6WA200540351 120051209A2752 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT WING FAILED A A6WAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 GL31418AW 7618 DEPARTING FLAPS FAIL MSG. WHEN FLAPS WENT FROM 8-0 DEGREES PERFORMED QRH RETURNED. WORK ORDER 90809, REMOVED AND REPLACED NR 3 AND NR 4 FLAP ACTUATORS ON RT WING TRIPPED IAW AMM. OPS CHECK GOOD. (K) 2L72 4F4 FRTA21EA E15NE 20060117000032006011700003SO 2006 1 17 F05003 120050919A3350 LIGHT EMB 145 EMB145LR 3260212SO EMERGENCY EXIT INOPERATIVE A FDKAO OTHER O OTHER NRNOT REPORTED 1 SW07825MJ 145179 FRL 9430 CAE-MCO. THE CREW REPORTED A FWD EMERGENCY EXIT LIGHT INOP. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20060117000052006011700005SO 2006 1 17 F05009 120051107A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A FDKAO OTHER O OTHER NRNOT REPORTED 1 SW07829MJ 145228 FRL 6073 MCO - RDU. THE CREW NOTED THAT THE CEILING EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED LIGHT BULB AND OPS CHECKED NORMAL. 2L72 4T RTT00011AT 20060117000062006011700006SO 2006 1 17 F05013 120051202A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A FDKAO OTHER O OTHER NRNOT REPORTED 1 SW07844MJ 145481 FDM 6066 MCO. THE CREW LEFT THE EMERGENCY LIGHT SWITCH IN THE ARMED POSITION WITH THE AIRCRAFT POWERED DOWN. MAINTENANCE RECHARGED THE SYSTEM AND OPS CHECKED NORMAL. 2L72 4T RTT00011AT 20060117000082006011700008EA 2006 1 17 SWIA200516101 120051227A2740 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07906SW 7510 STAB TRIM INOP. REPLACED HORIZONTAL STAB ACTUATOR AND MCU. OPERATIONAL CHECK GOOD. REF CRJ AMM 27-42-01, P/N: 7062-3, S/N OFF: 901, P/N: 8396-3, S/N OFF: 1152. 2L72 4F RTA21EA 20060117000182006011700018NM 2006 1 17 2006UALA00009 120051231A5311 FRAME BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU BS 616 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29337UA 24241 CABIN OVERWING FRAME BS 616L INNER CHORD CRACKED AT LOWER END JUST BELOW CREASE BEAM. REMOVED CRACK ACCOMPLISHED FILLER AND ANGLE REPAIR PER MM 53-11-89. 2L72 4F4 FRTA16WE E21EU 20060117000202006011700020NM 2006 1 17 2006UALA00011 120051230A5311 FRAME BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU BS 616 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29923UA 26643 CABIN FRAME STA 616 LT SIDE IS CRACKED BELOW FLOOR. REMOVED DAMAGE, FABRICATED FILLER AND ANGLE REF MM 53-11-89 AND INSTALLED. 2L72 4F4 FRTA16WE E21EU 20060117000232006011700023NM 2006 1 17 2006UALA00014 120051230A5241 FRAME BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU GALLEY DOOR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29923UA 26643 FWD GALLEY DOOR AFT FRAME CRACKED 3RD FROM TOP STOP FITTING. MAJOR REPAIR ACCOMPLISHED PER SM-90-52-40-14JD, REMOVED DAMAGE, INSTALLED DOUBLER REPAIR. NO FURTHER FINDINGS. O.K. FOR SERVICE. 2L72 4F4 FRTA16WE E21EU 20060117000262006011700026NM 2006 1 17 2006UALA00017 120051229A5311 FRAME BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU BS 787 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29923UA 26643 CABIN STA 787 FRAME IS CRACKED BETWEEN STR 8R AND 9R AT PSU SUPPORT RAIL IS CRACKED. REMOVED THE DAMAGE AND FABRICATED FILER AND ANGLE PER SRM 53-10-84 AND INSTALLED. 2L72 4F4 FRTA16WE E21EU 20060117000282006011700028NM 2006 1 17 2006UALA00019 120051229A5311 FRAME BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU BS 663.75 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29923UA 26643 CABIN STA 663.75 FRAME CRACKED AT NR 3 LT STR CUTOUT. REMOVED DAMAGE AND FABRICATED AND INSTALLED REPAIR ANGLE, SPLICE AND FILLER REF SRM 53-00-07 REPAIR 9, AND 51-40-02 AND 51-40-03. 2L72 4F4 FRTA16WE E21EU 20060117000292006011700029NM 2006 1 17 2006UALA00020 120051229A5311 FRAME BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU BS 663.75 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29923UA 26643 CABIN STA 663.75 FRAME IS CRACKED AT 2 RIGHT STR CUTOUT. REMOVED DAMADE FABRICATED AND INSTALLED REPAIR ANGLE, STRINGER SPLICE, AND FILLER REF SRM 53-00-07 REPAIR 9 AND SRM 51-40-02 AND 51-40-03. 2L72 4F4 FRTA16WE E21EU 20060117000312006011700031WP 2006 1 17 IXXA0500157O 120051209A3260 SCREW DOUG DC8 DC873F 302199FWP PROX SENSOR LOOSE A IXXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW11602AL967572445 45991 ON TAKEOFF FROM KTOL TO KBFI GEAR HANDLE UP GEAR NOT LATCHED LIGHT STAYED ON. LANDING CYCLED DOWN THEN UP LIGHT WENT OUT. MAINTENANCE LUBED GEAR UP LATCHES AND INDICATOR SWITCHES, NO DEFECTS NOTED. MAINTENANCE FOUND A LOOSE SCREW ON RT DOOR UP LATCH PROXIMITY SWITCH. SCREW WAS TIGHTENED AND GEAR SWING WAS PERFORMED PER ALL APPLICABLE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20060117000942006011700094NM 2006 1 17 SCNA05020 120051227A3350 LAMP BOEING737 7378Q8 13844BXNM EMERGENCY LIGHT INOPERATIVE A SCNAK NONE O OTHER ININSP/MAINT 1 GL15801SY 30332 RIGHT FWD OVERWING EMERGENCY EXIT LIGHT IN WINDOW LIGHT ASSY INOP. MAINTENANCE INSTALLED NEW LAMPS & OPERATIONALLY CHECKS GOOD. 2L72 4F RTA16WE 20060112000372006011200037WP 2006 1 12 ASAA0580529 120051003A5347593054790 SEAT TRACK DOUG DC9 DC983 3022083WP FS 200-256 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - DURING HV CHECK, PAX CABIN SEAT TRACK IS CORRODED. REPLACED DAMAGED SECTION. INSTALLED PLUG AND CHANNEL. (M) 2L72 4F RTA6WE 20060112000822006011200082NM 2006 1 12 ASAA0540557 120051021A53206545934259 SUPPORT BOEING737 7374Q8 138447QNM FS 328-340 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - FOUND CORROSION ON FLOOR SUPPORT. REMOVED AND REPLACED FLOOR SUPPORT IAW 737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060113000102006011300010NM 2006 1 13 AWXA200600024 120051221A5347D53371110010 SEAT TRACK AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28814AW 1281 SAL - DURING BC4 CHECK DISCOVERED LEVEL 2 CORROSION ON SEAT TRACK AT FR 42+7" AND Y-765. RE-WORK AREA WAS FOUND TO BE OUT OF LIMITS IAW 53-31-15 FIG 103. MAINTENANCE REMOVED AND INSTALLED NEW SEAT TRACK FROM FR42 TO FR51 AND Y-765 IAW AIRBUS 319 SRM 51-72-11. 2L72 4F RTA28NM 20060113000322006011300032WP 2006 1 13 05FDEA04264 120051212A3243 PEDAL DOUG DC10 DC1010 3022110WP BRAKES BROKEN A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25369FE 46607 CAPTS RT BRAKE PEDAL WILL NOT ACTUATE THE BRAKES. FOUND THE CTR TORQUE TUBE BRACKET FOR THE CAPTS RT PEDAL BROKEN. MPN ABH7271-501 INSTALLED SERVICEABLE BRACKET (SETS PARKING BRAKE) BRAKE PEDALS OPERATE NORMAL AND PARKING BRAKE SETS AND RELEASES NORMAL. INSTALLED BRACKET PER DC-10 SMP. 2L73 4F A22WE 20060113000572006011300057NM 2006 1 13 DL757060028 120050720A5330146N3750 SKIN BOEING757 757232 1384965NM BS 1694 S-14L GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27668DN 25141 THE FUSELAGE SKIN WAS FOUND DENTED AND GOUGED AT STA 1694 BELOW THE S-14L LAP JOINT. DAMAGED SKIN WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED. 2L72 4F RTA2NM 20060113000592006011300059EU 2006 1 13 YENA200588 120051220A2720 WARNING LIGHT AIRBUS320 A320232 3930326EU YAW DAMPER ILLUMINATED A YENAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA15586JB 2160 REJECTED T/O AT APPROX 50 KNOTS DUE TO AUTO FLT YAW DAMPER ECAM. PERFORMED OPS CHECK OF YAW DAMPER IAW AMM 27-26-00. OPS CHECK OK. PERFORMED BRAKE INSPECTION AS PRECAUTIONARY IAW AMM 5-51-16. ALL OK, PER CREW NO HIGH ENERGY STOP PERFORMED. 2L72 4F RTA28NM 20060113000682006011300068WP 2006 1 13 IXXA0500169S 120050121A5310 DOUBLER DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING ROUTINE C-CHECK FOUND AIR START ENCLOSURE GOUGED AND CRACKED. REMOVED FASTENERS, INNER AND OUTER DOUBLER. FABRICATED INNER AND OUTER DOUBLER. LOCATED, DRILLED, TREATED PRIMED, AND INSTALLED NEW INNER AND OUTER DOUBLER IAW DAC DRAWING 5614438, DC8 SRM 53-3-1, AND 51-1-8 2L74 4F RT4A25 20060113000702006011300070WP 2006 1 13 IXXA0500171S 120050122A7110 COWLING DOUG DC8 DC871F 302199DWP NR 1 NACELLE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING ROUTINE C-CHECK FOUND NUMBER 1 ENGINE NOSE COWL EXTERNAL SKIN CRACKED BEYOUND STOP DRILL AT INBOARD ANTI-ICE CUTOUT LOWER FORWARD CORNER. REMOVED FASTENERS. PERFORMED HFEC TO VERIFY CRACK STOPS AT FASTENER HOLE. FABRICATED DOUBLER, LOCATED, DRILLED, TREATED, PRIMED AND INSTALLED DOUBLER IAW DC8 SRM 71-2-0, 51-1-8, AND 51-1-21. 2L74 4F RT4A25 20060113000722006011300072WP 2006 1 13 IXXA0500173S 120050124A78303057759000 STRUCTURE DOUG DC8 DC871F 302199DWP THRUST REVERSER GOUGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING ROUTINE C-CHECK FOUND NUMBER 2 ENGINE THRUST REVERSER INBOARD SHELL HAS GOUGES. REMOVED DAMAGE, RECEIVED REPAIR DOUBLER, LOCATED, DRILLED, TREATED, PRIMED AND INSTALLED DOUBLER IAW CFM MM 78-31-10. 2L74 4F RT4A25 20060113000782006011300078WP 2006 1 13 IXXA0500160S 120050115A53105611002502 CLOSEOUT PANEL DOUG DC8 DC871F 302199DWP ZONE 700 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING ROUTINE C-CHECK FOUND RIGHT HAND GEAR OVERHEAD TRUNNION PANEL CORRODED, DELAMINATED. REMOVED FASTENER AND DAMAGED PANEL. RECEIVED OVERHAULED TRUNNION PANEL. LOCATED, DRILLED AND INSTALLED TRUNNION PANEL IAW DC8 SRM 51-1-24, 51-3-0, AND 51-3-1. 2L74 4F RT4A25 20060113000802006011300080WP 2006 1 13 IXXA0500180S 120050124A5753 CLIP DOUG DC8 DC871F 302199DWP ZONE 500 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING ROUTINE C-CHECK, FOUND LEFT WING OUTBOARD FLAP INBOARD SUPPORT HINGE TRAILING EDGE UPPER WING SUPPORT CLIP CRACKED. REMOVED FASTENERS, FABRICATED NEW CLIP, TREATED, PRIMED, AND INSTALLED NEW CLIP AND FASTENERS IAW DC8 SRM 57-2-0, 51-1-21, AND 51-1-8. 2L74 4F RT4A25 20060113000822006011300082WP 2006 1 13 IXXA0500182S 120050124A5311 FRAME DOUG DC8 DC871F 302199DWP ZONE 200 CHAFED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING ROUTINE C-CHECK FOUND FLIGHT DECK AT STATION 12.00 TO STATION 20.00 LEFT BUTT LINE 10 FRAME CHAFED THROUGH. REMOVED LOWER L-ANGLE WIRE BUNDLE ATTACH ANGLE, STIFFENERS, AND INTERCOSTAL. FABRICATED INTERCOSTAL AND DOUBLER. LOCATED INTERCOSTAL AND DOUBLER, DRILLED, ALODINED AND PRIMED. INSTALLED INTERCOSTAL AND DOUBLER. REINSTALLED L-ANGLE WIRE BUNDLE ATTACH ANGLE AND STIFFENERS IAW DC8 DRAWING 5641543, DC8 SRM 51-1-21, 53-7-0, 51-9-0, 51-1-8, 53-2-0, AND 51-1-20D. 2L74 4F RT4A25 20060113001062006011300106WP 2006 1 13 IXXA0500191S 120050208A57535701446501 VANE DOUG DC8 DC871F 302199DWP ZONE 500 DELAMINATED A IXXAO OTHER O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING ROUTINE C-CHECK FOUND LEFT HAND OUTBOARD FLAP INBOARD FLAP VANE DELAMINATED. REMOVED AND REPLACED FLAP VANE, RIG CHECK GOOD IAW DC8 MM 27-51-14. 2L74 4F RT4A25 20060113001082006011300108WP 2006 1 13 IXXA0500193S 120050125A5753 SKIN DOUG DC8 DC871F 302199DWP ZONE 600 GOUGED A IXXAO OTHER O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING ROUTINE C-CHECK FOUND RIGHT HAND OUTBOARD FLAP UPPER SKIN IS GOUGED AT PREVIOUS REPAIR. REMOVED DAMAGED REPAIR, FABRICATED, NEW REPAIR PART, ALODINED, PRIMED AND INSTALLED NEW REPAIR PART IAW DC8 SRM 57-2-0, 51-1-20D, AND 51-1-8. 2L74 4F RT4A25 20060113001102006011300110WP 2006 1 13 IXXA0500195S 120050125A5330 SKIN DOUG DC8 DC871F 302199DWP ZONE 100 CRACKED A IXXAO OTHER O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING ROUTINE C-CHECK FOUND EXTERNAL FUSELAGE SKIN CRACKED AT STATION 45 LONGERON 28 LEFT IN AREA OF EXISTING REPAIR. PERFORMED HFEC TO VERIFY CRACK. VERIFIED, GAINED ACCESS, REMOVED FASTENERS, EXISTING DOUBLER, AND REMOVED DAMAGE. FABRICATED FILLER AND DOUBLER. TREATED, PRIMED, INSTALLED REPAIR PARTS AND FASTENERS IAW MD NDT SM 06-10-001-001, DC8 SRM 51-3-1, 51-1-21, 53-2-0, 51-1-8, AND 51-1-20D. 2L74 4F RT4A25 20060113001122006011300112WP 2006 1 13 IXXA050198S 120050125A2731 TRIM TAB DOUG DC8 DC871F 302199DWP ZONE 300 DELAMINATED A IXXAO OTHER O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING ROUTINE C-CHECK FOUND LEFT ELEVATOR TAB DELAMINATED. REMOVED TAB, DISASSEMBLED, CLEANED INSPECTED, AND REPLACED TRAILING EDGE WEDGE. REINSTALLED TAB ON LEFT ELEVATOR IAW DC8 SRM 51-1-21, 51-1-22, 51-1-8B, 51-4-5, 51-3-0, DC8 DRAWING 5702579 AND DC8 OHM 27-16-1. 2L74 4F RT4A25 20060113001142006011300114WP 2006 1 13 IXXA0500200S 120050125A2731 BRACKET DOUG DC8 DC871F 302199DWP ZONE 100 CRACKED A IXXAO OTHER O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING ROUTINE C-CHECK FOUND AIRSTART NOZZLE BRACKET CRACKED AT 3 LOCATIONS. STOP DRILLED CRACKS, FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS AND FASTENERS IAW DC8 SRM 53-2-0, 51-9-0, AND 51-1-8. 2L74 4F RT4A25 20060113001162006011300116WP 2006 1 13 IXXA0500203S 120050127A5321 FLOORBOARD DOUG DC8 DC871F 302199DWP ZONE 200 DELAMINATED A IXXAO OTHER O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING ROUTINE C-CHECK FOUND CABIN FLOORBOARD DELAMINATED AT STATION 1120 TO STATION 1260 RIGHT BUTT LINE 54. REMOVED DAMAGED FLOORBOARD, MANUFACTURED NEW FLOORBOARD, LOCATED, DRILLED AND INSTALLED NEW FLOORBOARD IAW DC8 SRM 51-3-0, 51-1-11 AND DOUGLAS SPEC 3932193. 2L74 4F RT4A25 20060113001182006011300118NM 2006 1 13 HNAA0500102 120051207A7931310595601 SHIM DHAV DHC8 DHC8102 2809003NM ENGINE OUT OF ADJUST A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07912HA5146551465 040 AIRCRAFT RETURNED TO FIELD DUE TO OIL PRESSURE RISING TO 70 PSI ON CLIMBOUT. REMOVED TWO SHIMS AT OIL PRESSURE REGULATOR. 2H72 4T RTA13NM 20060113001212006011300121NM 2006 1 13 2006UALA00003 120051230A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29181UA 25278 DOOR 2R BUSTLE EMERGENCY LT INOP. 2L74 4F4 FRTA20WE E24NE 20060113001232006011300123NM 2006 1 13 2006UALA00005 120051230A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29181UA 25278 EMERGENCY LIGHT AT ROW 23 LT CEILING INOP. 2L74 4F4 FRTA20WE E24NE 20060113001472006011300147NE 2006 1 13 NACA20050033 220051224A7421URHB32E SPARK PLUG PWA DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE 4 ENG/16 CYL FOULED A NACAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CRCRUISE 1 AL036174C103 103 197511 44075 P33688 NR 4 ENGINE SHUTDOWN DUE TO EXCESSIVE BACKFIRING, SUSPECT NR 16 CYLINDER. REPLACED NR 4 ENGINE NR 16 CYLINDER FRONT SPARK PLUG AND SHORT LEAD IAW 6-11 AND 6-12 MB PAGES 6-31 AND 6-34. 2L74 4R4 R 6A3 5E8 20060113001712006011300171NM 2006 1 13 ASMF200512016 120051217A2410696233B CSD DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE LEFT SIDE FAILED W ASMFK NONE MJ OVER TEMP WARNING INDICATION CRCRUISE 1 SW23169PL43424553 53175 728194 CAPTAIN REPORTED THAT DURING FLIGHT THE LT CSD REACHED 180 GRADES FOR A MINUTE, OVER TEMPERATURE LIGHT TURNED ON AND THE RT ENGINE EGT WAS OUT OF LIMITS AFTER STARTED. THE OPERATIONAL PROCEDURE WAS PERFORMED, THE LT CSD REPORT WAS DEFERRED IAW MEL 24-14-1, THE OVER TEMPERATURE INDICATION CONNECTOR WAS CLEANED IAW MM 32-42-7 AND THE FCU CHAMBER WAS CHECKED IAW MM 73-20-01. 2L72 4F4 FRTA6WE E9NE 20060117000042006011700004SO 2006 1 17 F05008 120051029A3350SG9632 LIGHT EMB 145 EMB145LR 3260212SO GALLEY INOPERATIVE A FDKAO OTHER O OTHER NRNOT REPORTED 1 SW07850MJ 145568 FRL 6058 CAE-MCO. THE CREW NOTED THAT THE GALLEY EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. 2L72 4T RTT00011AT 20060117001052006011700105WP 2006 1 17 IXXA0500204S 120050204A5347 SEAT TRACK DOUG DC8 DC871F 302199DWP ZONE 200 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING ROUTINE C-CHECK FOUND FLIGHT DECK COUIER SEAT TRACK AFT TRACK CRACKED ON END. REMOVED DAMAGE, MANUFACTURED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-0, 51-1-8, AND 51-1-21. 2L74 4F RT4A25 20060117001132006011700113NM 2006 1 17 TSAA0557058 120051024A5711 SPAR BOEING737 737230 1384401NM RT WING CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13821AL 23155 RIGHT WING FRONT SPAR, LOWER CORD FWD FLANGE CORRODED AT SLAT STA 243.0 AND SLAT STA 254.0. 2L72 4F RTA16WE 20060117001152006011700115NM 2006 1 17 TSAA0553060 120051024A53306551625 SKIN BOEING737 737230 1384401NM BS 998 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13821AL 23155 SECTION 46 FUSELAGE SKIN WITH CORROSION AT BS 998.40, LBL 6.75. 2L72 4F RTA16WE 20060117001192006011700119WP 2006 1 17 IXXA0500222S 120051002A5320 SUPPORT DOUG DC8 DC871F 302199DWP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND SUPPORT CORRODED AT STATION 300 LONGERON 29 LEFT. FABRICATED NEW SUPPORT, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED NEW SUPPORT AND FASTENERS IAW DC8 SRM 53-2-0, 51-1-20 AND 51-1-8. 2L74 4F RT4A25 20060117001212006011700121EU 2006 1 17 YENA200590 120051227A7797 ELECTRICAL BOX AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE LT ENGINE MALFUNCTIONED A YENAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA15536JB 1784 EGT IND FLUCTUATED BETWEEN 190-490 DEGREES AFTER TAKEOFF, WENT AS LOW AS 75 DEGREES DURING RETURN. T/S IAW AMM 77-21-43-05. REPLACED JUNCTION BOX IAW 77-21-43-04. OPERATED LEFT ENG AT VARIOUS POWER SETTINGS, ALL EGT PARAMETERS NORMAL. OK FOR SERVICE. 2L72 4F4 FRTA28NM E40NE 20060117001242006011700124NM 2006 1 17 PIDAS06002 120051231A276165C268642 ACTUATOR BOEING737 7373G7 1384595NM NR 1 SPOILER BROKEN A PIDAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SO05380WL 23218 LOSS OF -A- SYSTEM HYDRAULIC PRESSURE; QUANTITY ZERO; ISOLATED SYSTEM, PERFORMED MANUAL GEAR EXTENSION & FLAPS 25 LANDING, NO FURTHER INCIDENT. FOUND NR 1 SPOILER ACTUATOR CASTING BROKEN. REPLACED NR 1 SPOILER ACTUATOR PER MM 27-62-94. 2L72 4F RTA16WE 20060117001342006011700134NM 2006 1 17 HNAA0500106 120051223A2913 PUMP DHAV DHC8 DHC8102 2809003NM HYD SYSTEM FAILED A HNAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA07907HA 011 NR 1 HYDRAULIC DROPPED TO .5 QTS IN FLIGHT ISO VALVE CAUTION LIGHT ILLUMINATED. REMOVED AND REPLACED NR 1 ENGINE DRIVEN PUMP. 2H72 4T RTA13NM 20060117001362006011700136NM 2006 1 17 HNAA0500107 120051229A2910 HYDRAULIC SYSTEM DHAV DHC8 DHC8102 2809003NM NR 1 LEAKING A HNAAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 EA07931HA 132 NR 1 HYDRAULIC QUANTITY DROPPED TO .5 QTS ON FINAL. REMOVED AND REPLACED HYDRAULIC TUBE AT CASE DRAIN MANIFOLD. 2H72 4T RTA13NM 20060117001462006011700146WP 2006 1 17 IXXA0500131S 120050214A5310 FASTENER DOUG DC8 DC871F 302199DWP BS 1322.00 L35.5MISSING A IXXAK NONE O OTHER ININSP/MAINT 1 SW11821BX858952998 45811 DURING A ROUTINE C-CHECK INSPECTION FOUND RT FUSELAGE AFT CENTER SECTION LOWER PLATING OLD OMEGA ANTENNA DOUBLER MISSING ON ROW FASTENERS AND MAX PITCH EXCEEDS LIMITS AT STA FS 1322.00L, 35.5R. MAJOR REPAIR ACCOMPLISHED REMOVAL OF EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION TO AREA. FABRICATED REPAIR DOUBLER AND INTERNAL FINGER DOUBLERS AND FILLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIRED PARTS IAW DC8 SRM 3-2-1 FIG 7, FIG 1 AND 3, 53-2-0, 53-4-1 FIG 16 SH 1, 51-10-1 FIG 2 SH 5, 51-3-1, 51-3-5, 51-1-4, 51-1-20D, 51-1-21. 2L74 4F RT4A25 20060117001512006011700151EU 2006 1 17 USAA051657 120051229A5315D5348004320401 FLOORBEAM AIRBUSA321 A321211 3930370EU BS 1732 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19162UW 1412 AT 1732L AND FR 66 CORROSION. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 53-41-14; CORROSION LEVEL 1; TASK JA216053500, DEFECT SIZE: .25 X .25 INCH. 2L72 4F RTA28NM 20060117001562006011700156NM 2006 1 17 ASAA0540528 120051012A52306547952358 SKIN BOEING737 737490 1384715NM FS 795-846 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02793AS 28888 PAE - AFT CARGO DOOR HAD 4 SMALL DENTS AND CREASES AT BOTTOM AFT CORNER. REMOVED AND REPLACED AFT CARGO DOOR SKIN IAW B737-400 SRM 52-30-01. (M) 2L72 4F RTA16WE 20060117001582006011700158NM 2006 1 17 ASAA0540584 120051028A53206545833149 INTERCOSTAL BOEING737 7374Q8 138447QNM FS 270 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - FOUND CORROSION ON INTERCOSTAL. REMOVED DAMAGED INTERCOSTAL, FABRICATED NEW AND INSTALLED PER B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060117001602006011700160NM 2006 1 17 ASAA0540570 120051026A53206545834256 FLOOR SUPPORT BOEING737 7374Q8 138447QNM FS 312 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - FOUND CORROSION ON FLOOR SUPPORT. REPLACED FLOOR SUPPORT PER B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060117001622006011700162NM 2006 1 17 ASAA0540585 120051028A53206545833449 ANGLE BOEING737 7374Q8 138447QNM FS 270 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - FOUND CORROSION ON Z-ANGLE. REMOVED CORRODED Z-ANGLE, FABRICATED NEW Z-ANGLE AND INSTALLED PER B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060117001642006011700164NM 2006 1 17 ASAA0540580 120051028A533065458661210 SKIN BOEING737 7374Q8 138447QNM FS 628 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - FOUND CORROSION ON MOUNTING AREA AROUND MARKER BEACON. REMOVED AND REPLACED SKIN PANEL AT MARKER BEACON PER B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060117001662006011700166NM 2006 1 17 ASAA0540577 120051028A5347654681365 SEAT TRACK BOEING737 7374Q8 138447QNM FS 340-360 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - FOUND CORROSION ON SEAT TRACK. REMOVED AND REPLACED SEAT TRACK PER B737-400 SRM 51-40-52. (M) 2L72 4F RTA16WE 20060117001682006011700168NM 2006 1 17 ASAA0540586 120051028A5347654681365 SEAT TRACK BOEING737 7374Q8 138447QNM FS 340-360 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - FOUND CORROSION ON SEAT TRACK. REMOVED AND REPLACED CORRODED SEAT TRACK PER B737-400 SRM 53-00-52. (M) 2L72 4F RTA16WE 20060117001922006011700192NM 2006 1 17 ASAA0540566 120051026A531165465663 FRAME BOEING737 7374Q8 138447QNM FS 992 CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - FOUND FRAME CHAFED. REPAIRED FRAME PER B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060117002002006011700200NM 2006 1 17 ASAA0540541 120051012A531165465292 FRAME BOEING737 737490 1384715NM FS 440 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02793AS 28888 PAE - FRAME CRACKED AT BIN RAIL SUPPORT BETWEEN STRINGER 8 LEFT AND 9 LEFT AT INBOARD FASTENER. REPAIRED DAMAGED FRAME AT BIN RAIL SUPPORT PER B737-200 SRM 53-00-07. (M) 2L72 4F RTA16WE 20060117002022006011700202NM 2006 1 17 ASAA0540518 120051001A5347655384421 CARGO TRACK BOEING737 737490 1384715NM FS 945-915 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02793AS 28888 PAE - CORROSION AT LEFT CARGO TIE DOWN TRACK AN NUT PLATE LOCATIONS. REMOVED CORROSION ON LEFT CARGO TIE DOWN NUT PLATE LOCATIONS. REMOVED CORROSION ON LEFT CARGO TIE DOWN NUT-PLATE LOCATIONS, FABRICATED AND INSTALLED REPAIR PARTS B737-200 SRM 53-60-53. 2L72 4F RTA16WE 20060117002082006011700208NM 2006 1 17 ASAA0540542 120051013A53106552878102 CREASE BEAM BOEING737 737490 1384715NM FS 947-987 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02794AS 26695 OKC - FOUND CORROSION ON CREASE BEAM AT L-2 DOOR, BS 947-987. REMOVED CORRODED PART AND REPLACED WITH NEW PART PER B737-200 SRM 51-40-2. (M) 2L72 4F RTA16WE 20060117002112006011700211NM 2006 1 17 ASAA0540524 120051006A575165C2591130A SKIN BOEING737 737490 1384715NM RT AILERON DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02794AS 28889 OKC - FOUND RIGHT AILERON LOWER SKIN DELAMINATED ON FORWARD INBOARD CORNER. PREPPED AREA, APPLIED BONDED GRAPHITE LAYUP IAW B737-400 SRM 51-70-17. (M) 2L72 4F RTA16WE 20060117002132006011700213NM 2006 1 17 ASAA0540565 120051026A53206517688175 SILL BOEING737 7374Q8 138447QNM FS 320-339 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - FOUND MOPSILL CORRODED. REPLACED MOPSILL PER B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060117002162006011700216NM 2006 1 17 ASAA0540555 120051018A3260 SWITCH BOEING737 737490 1384715NM GROUND SAFETY FAILED A ASAAO OTHER G MULTIPLE FAILURE CRCRUISE 1 NM02706AS 28894 PHX - AT 31,000 FEET AFTER 90 MINUTES IN CRUISE, PRESSURIZATION FAILED. AUTO THROTTLE AND TRANSPONDER FAILED AT SAME TIME. AUTO SPEED BRAKE WARNING LIGHT ILLUMINATED ALSO. REPLACED GROUND SAFETY SWITCH S-105, PER AMM 32-09-01. ALSO REFERENCE EA 3209-01001 FOR GROUND SAFETY SWITCH CLARIFICATION. SYSTEM OPS TEST NORMAL IAW AMM 32-09-01 PAGES 501-505. (M) 2L72 4F RTA16WE 20060117002182006011700218NM 2006 1 17 ASAA0540575 120051028A534065C161216 FITTING BOEING737 7374Q8 138447QNM FS 313 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - FOUND FITTING CORRODED. REPLACED CORRODED FITTING PER B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060117002202006011700220NM 2006 1 17 ASAA0540530 120051012A532065C8073511 SILL BOEING737 737490 1384715NM FS 987 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02793AS 28888 PAE - FOUND CORROSION ON RIGHT MOPSILL. REMOVED AND REPLACED MOPSILL PER B737-200 SRM 53-60-15. (M) 2L72 4F RTA16WE 20060117002222006011700222NM 2006 1 17 ASAA0540594 120051101A53206517688174 SILL BOEING737 7374Q8 138447QNM FS 305-360 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND L-1 DOOR CUTOUT MOPSILL CORRODED. REPLACED L-1 DOOR MOPSILL PER B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060117002242006011700224NM 2006 1 17 ASAA0540535 120051012A531165465501 FRAME BOEING737 737490 1384715NM FS 987 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02793AS 28888 PAE - FOUND FRAME CRACKED AT BIN RAIL SUPPORT. REPAIRED FRAME CRACK PER B737-200 SRM 53-00-07. (M) 2L72 4F RTA16WE 20060117002262006011700226NM 2006 1 17 ASAA0540533 120051012A532065557573 PAN BOEING737 737490 1384715NM FS 950 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02793AS 28888 PAE - FOUND CORROSION, FORWARD LAVATORY DUP SERVICE PAN DOUBLER. REMOVED AND REPLACED DOUBLER PER B737-200 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060117002282006011700228NM 2006 1 17 ASAA0540540 120051012A532069165004 INTERCOSTAL BOEING737 737490 1384715NM FS 767 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02793AS 28888 PAE - WHILE WORKING CARD NR 4953433, FOUND INTERCOSTAL WEB DENTED. REMOVED AND REPLACED INTERCOSTAL WEB IN AFT CARGO BAY PER SRM 53-00-04. (M) 2L72 4F RTA16WE 20060117002382006011700238NM 2006 1 17 ASAA0540590 120051028A53156561777505 FLOORBEAM BOEING737 7374Q8 138447QNM FS 312 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND CORROSION ON TOP CHORD OF FLOORBEAM. REPAIRED FLOORBEAM AT BS 312 LBL 7 - RBL 8 WL 208 PER B737-400 SRM 53-00-51. (M) 2L72 4F RTA16WE 20060117002442006011700244WP 2006 1 17 ASAA0580444 120050808A53203957317501 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FS 696 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02935AS 49236 OKC - DURING C-CHECK, FOUND CABIN FLOOR PANEL SUPPORT FITTING CORRODED AND CRACKED. REPLACED SUPPORT FITTING. (M) 2L72 4F A6WE 20060117002452006011700245WP 2006 1 17 ASAA0580452 120050808A5330593600731 SKIN DOUG DC9 DC982 3022082WP FS 1290 CANNING A ASAAK NONE O OTHER ININSP/MAINT 1 NM02935AS 49236 OKC - DURING C-CHECK, FOUND FUSELAGE SKIN IS `OIL CANNED`. REMOVED DAMAGED AREA. INSTALLED REPAIR DOUBLER. (M) 2L72 4F A6WE 20060117002572006011700257WP 2006 1 17 ASAA0580533 120051019A52105910081405 SKIN DOUG DC9 DC983 3022083WP PAX DOOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 SEA - LINE CHECK, L-1 FWD PAX DOOR DENTED. REPAIRED PER SRM 53-04. (M) 2L72 4F RTA6WE 20060117002592006011700259NM 2006 1 17 ASAA0540552 120051016A53156545808179 FLOORBEAM BOEING737 7374Q8 138447QNM FS 294.5 DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - MECHANICAL DAMAGE TO FLOORBEAM. REMOVED AND REPLACED FLOORBEAM UPPER CHORD AT BS 294.5 IAW 737-400 SRM 53-10-81. (M) 2L72 4F RTA16WE 20060117002622006011700262NM 2006 1 17 ASAA0540558 120051021A53156545818510 FLOORBEAM BOEING737 7374Q8 138447QNM FS 360 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - FOUND CORROSION ON FLOORBEAM. REMOVED DAMAGED UPPER CHORD, FABRICATED NEW UPPER CHORD, REPAIR PARTS AND INSTALLED IAW 737-400 SRM 53-00-51. (M) 2L72 4F RTA16WE 20060117002712006011700271EA 2006 1 17 COMA0560791 120051231A5712601R10203 RIB CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA29272 7031 FOUND LT BATT RIB ASSY CRACKED. INCORPORATED REPAIRS TO LT BATT RIB ASSY AT WS 53.60 IAW BOMBARDIER REO 601R-57-51-046 REV B REPAIR NR 3. 2L72 4F RTA21EA 20060117002732006011700273EU 2006 1 17 USAA051655 120051229A5320GILLFAB4505 BUSHING AIRBUSA321 A321211 3930370EU ZONE 200 LOOSE A USAAK NONE O OTHER ININSP/MAINT 1 EA19162UW 1412 FOUND BUSHING LOOSE, ZONE 200 PANEL 262 EF. MANUFACTURED PER AIRBUS SRM 53-02-00, MCGILL IRM 9701, DEFECT SIZE: BUSHING INSERT LOOSE LOWER SURFACE. 2L72 4F RTA28NM 20060117002752006011700275NM 2006 1 17 DLM88050809 120051220A7711 LINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 ENGINE CONTAMINATED A DALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO27919DE 53422 725452 RIGHT ENG EPR INDICATION STUCK AT 1.06, DRAINED WATER FROM PT7 LINES. 2L72 4F4 FRTA6WE E9NE 20060117002772006011700277NM 2006 1 17 DL76G050811 120051212A5330146T33414 SKIN BOEING767 767332 1382001NM BS 1480 S22L GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO2716065 30199 THE FUSELAGE SKIN WAS FOUND GOUGED NEAR BS 1480 BETWEEN STR 22L AND 23L. DAMAGE WAS APPROX 5.125 IN BY 2.5 IN. INSTALLED A REPAIR DOUBLER PER ER/A 452042-14. 2L72 4F RTA1NM 20060117002782006011700278NM 2006 1 17 DL76L050812 120051220A249700 RECEPTACLE BOEING767 767332 1382001NM ELECTRICAL POWERARCED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27184DN 27111 RAMP REPORTED ELECTRICAL ARCING VISIBLE AT EXTERNAL POWER RECEPTACLE. FOUND EXTERNAL POWER RECEPTACLE PIN DAMAGED. REPLACED RECEPTACLE. 2L72 4F RTA1NM 20060117002792006011700279NM 2006 1 17 DL76S050813 120051220A2910 BOWL BOEING767 767332 1382001NM FILTER STRIPPED A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO27119DL 23278 LOST CENTER SYSTEM HYD. FOUND ADP FILTER MODULE BOWL STRIPPED OFF THE HOUSING. REPLACED MODULE. 2L72 4F RTA1NM 20060117002802006011700280NM 2006 1 17 DL75K050815 120051221A3350 BULB BOEING757 757232 1384965NM EMERGENCY LIGHT BURNED OUT A DALAK NONE L NO TEST ININSP/MAINT 1 SO27644DL 23998 FWD LT OVERWING AND R2 EMERGENCY LIGHTS INOP. RELAMPED, CK OK. 2L72 4F RTA2NM 20060117002822006011700282NM 2006 1 17 DL76G050817 120051222A2720 MODULE BOEING767 767332 1382001NM RUDDER OUT OF POSITION A DALAD RETURN TO BLOCK WJ INADEQUATE Q C WARNING INDICATION TXTAXI/GRND HDL 1 SO271612T 30575 RUDDER RATIO EICAS MSG WITH RUDDER RATIO LIGHT ILLUMINATED ON OVERHEAD PANEL. FOUND RUDDER RATIO MODULE IN TEST. PUT SW TO NORM. MSG AND LIGHT EXT. T/S PER FIM RUDDER RATIO CHECKS GOOD. 2L72 4F RTA1NM 20060117002832006011700283NM 2006 1 17 DL738050818 120051222A2720275201236 MODULE BOEING737 737832 13844CFNM RUDDER TRIM UNSERVICEABLE A DALAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO273744D 29662 RUDDER TRIM INOP IN LT DIR KNOB AND TRIM GOES RT OK. RETURNED TO ATL. OVERWEIGHT LAND AT APPROX 152 K POUNDS TOUCHDOWN WAS MIN SINK AT 148 KTS BRAKES ON AT 100 KTS. NORMAL BRAKING. FLT CONTROLS WERE NORMAL. REMOVED AND REPLACED RUDDER TRIM CTL SWITCH MODULE CYCLED RUDDER TRIM BOTH DIRECTIONS SEVERAL TIMES ALL CKS GOOD ALSO PERFORMED PHASE 1 OVERWEIGHT LANDING INSP PER MM 05-51-35. 2L72 4F RTA16WE 20060117002842006011700284NM 2006 1 17 DL764050819 120051222A2121732591F FAN BOEING767 767432ER 1385134NM FWD CARGO COMPT FAILED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27845MH 29719 AT CRUISE FL340 APPROX 2345Z BEGAN TO SMELL AN ELECTRICAL TYPE BURN SMELL IN COCKPIT. REPLACED EQUIPMENT COOLING FAN. 2L72 4F RTA1NM 20060117002852006011700285NM 2006 1 17 DL738050820 120051223A2751 SHAFT BOEING737 737832 13844CFNM FLAP XMITTER SHEARED A DALAO OTHER F FLT CONT AFFECTED LDLANDING 1 SO2737700 29631 FLAPS WOULD NOT EXTEND PAST 1 FLAPS LOCKED OUT. REPLACED LEFT FLAP POSITION TRANSMITTER. 2L72 4F RTA16WE 20060117002892006011700289EU 2006 1 17 USAA051663 120051229A5320D5311282600101 FLOOR SUPPORT AIRBUSA321 A321211 3930370EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19162UW 1412 FOUND FLOOR SUPPORT CORRODED, Y-503 AT FS 16. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 53-11-14; 51-42-11; CORROSION LEVEL 1; TASK JA-220-53500 DEFECT SIZE: 1" DIA. 2L72 4F RTA28NM 20060117002912006011700291EU 2006 1 17 USAA051665 120051229A5310 BEAM AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19114UW 1148 FOUND BEAM CORRODED, Y1292 AT FS 66. REPLACED BEAM SECTIONS AT Y1292 FROM FRAME 64-70 PER SRM 51-72-11, 51-42-11, DEFECT SIZE: 2" DIA. 2L72 4F RTA28NM 20060113000082006011300008NM 2006 1 13 AWXA200600022 120051223A5347D53472190211 SEAT TRACK AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28814AW 1281 MCN - DURING BC-4 CHECK DISCOVERED CORROSION ON FLOORBEAM SEAT RAIL AT FR 66 AND Y-1292. CORROSION WAS FOUND TO BE OUT OF LIMITS. MAINTENANCE REMOVED AND INSTALLED NEW FLOORBEAM FROM FR 64 TO FR 66 AND Y-1292 IAW AIRBUS 319 SRM 51-72-11. 2L72 4F RTA28NM 20060113000142006011300014NM 2006 1 13 AWXA200600028 120051223A5315D53472172205 FLOORBEAM AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28814AW 1281 SAL - DURING BC4 CHECK DISCOVERED CORROSION ON FLOORBEAM LOCATED AT FR 66+8" AND Y-1292. RE-WORK AREA WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 319 SRM 53-00-14. MAINTENANCE REMOVED AND INSTALLED NEW FLOORBEAM FROM FR 67 TO FS 68 AND Y-1292 IAW AIRBUS 319 SRM 51-42-11 AND DRAWING 53472040. 2L72 4F RTA28NM 20060113000202006011300020NM 2006 1 13 AWXA200600033 120051223A5347D53472190210 SEAT TRACK AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28814AW 1281 SAL - DURING BC4 CHECK DISCOVERED CORROSION ON FLOORBEAM LOCATED AT FR 66 AND Y1292. RE-WORK AREA WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 319 SRM 53-00-14. MAINTENANCE REMOVED AND INSTALLED NEW FLOORBEAM FROM FR 64 TO FR 66 AND Y1292 IAW AIRBUS 319 SRM 51-72-11. 2L72 4F RTA28NM 20060113000672006011300067WP 2006 1 13 IXXA0500163S 120050120A57305769581501 SKIN DOUG DC8 DC871F 302199DWP ZONE 400 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING ROUTINE C-CHECK FOUND LEFT WING JUST ABOVE NUMBER 2 PYLON UPPER SKIN CRACKED. REPLACED UPPER SLOT DOOR WITH NEW, IAW DC8MM 20-12-0, AND 27-81-02. 2L74 4F RT4A25 20060113000692006011300069WP 2006 1 13 IXXA0500170S 120050127A5311 FRAME DOUG DC8 DC871F 302199DWP CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING A ROUTINE C-CHECK FOUND FRAME JUST AFT OF AIRSTART COMPARTMENT CRACKED AT 2 LOCATIONS. REMOVED FASTENERS, AND DAMAGED AREA. FABRICATED REPAIR PARTS. LOCATED, DRILLED, TREATED, PRIMED AND INSTALLED REPAIR PARTS, IAW DC8 SRM 53-2-0, 51-1-20D, 51-3-0, 51-1-8, AND 51-1-21. 2L74 4F RT4A25 20060113000712006011300071WP 2006 1 13 IXXA0500172S 120050123A5311 FRAME DOUG DC8 DC871F 302199DWP STA 1120 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING ROUTINE C-CHECK FOUND FRAME CRACKED IN THE AFT PIT STATION 1120 AT LONGERON 30 RIGHT. REMOVED DAMAGE, FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED AND INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-0, 51-1-8, AND 51-1-20D. 2L74 4F RT4A25 20060113000732006011300073WP 2006 1 13 IXXA0500174S 120050124A78303057759000 HEAT SHIELD DOUG DC8 DC871F 302199DWP THRUST REVERSER DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING ROUTINE C-CHECK FOUND NUMBER 1 ENGINE THRUST REVERSER INBOARD INNER HEAT SHIELD HAS A HOLE WORN THROUGH. RECEIVED NEW HEAT SHIELD, LOCATED, DRILLED AND INSTALLED HEAT SHIELD IAW CFM56 MM 78-31-10. 2L74 4F RT4A25 20060113000752006011300075NM 2006 1 13 CALA0600003 120051230A5411311T245022 FRAME BOEING767 767224 1385170NM LT NACELLE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776153 30432 INSPECTION FOUND A 1 INCH CRACK IN LT PYLON NAC STA 285.4 AREA I/B FRAME CHORD. THE FRAME CHORD WAS REPLACED IAW ECRA 5420-01445. 2L72 4F RTA1NM 20060113000792006011300079WP 2006 1 13 IXXA0500179S 120050104A57534760268U ATTACH FITTING DOUG DC8 DC871F 302199DWP ZONE 500 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING ROUTINE C-CHECK, FOUND LEFT WING INBOARD FLAP OUTBOARD SUPPORT HINGE UPPER TRAILING EDGE ATTACH FITTING CRACKED. REMOVED FASTENERS AND DAMAGED BRACKET. RECEIVED NEW BRACKET, LOCATED, DRILLED, PRIMED AND INSTALLED NEW STEEL BRACKET IAW DC8 SRM 51-3-0, 57-1-24, AND 51-1-8. 2L74 4F RT4A25 20060113000812006011300081WP 2006 1 13 IXXA0500181S 120050125A5347 SEAT TRACK DOUG DC8 DC871F 302199DWP ZONE 200 DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING ROUTINE C-CHECK FOUND FLIGHT DECK FIRST OFFICER SEAT TRACKS AFT SET HOLES ELONGATED. REMOVED SEAT TRACKS. ORIGINAL THICKNESS WAS .125, REMOVED .040 MATERIAL, .080 REMAINING, OUT OF LIMITS. FABRICATED STRAPS FROM .040 THICK 301 STAINLESS STEEL. LOCATED, DRILLED AND INSTALLED REPAIR STRAPS WET WITH SEALANT AND FASTENERS. REINSTALLED SEAT TRACKS AND FUNCTIONAL CHECKED GOOD IAW DC8 SRM 51-1-20-D, 53-2-3, 25-11-1 AND 51-1-11. 2L74 4F RT4A25 20060113000832006011300083WP 2006 1 13 IXXA0500183S 120050125A534736575031 SEAT TRACK DOUG DC8 DC871F 302199DWP ZONE 200 WORN A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING ROUTINE C-CHECK FOUND FLIGHT DECK FLIGHT ENGINEER FORWARD AND AFT SEAT TRACKS WORN. REMOVED FASTENERS AND DAMAGED SEAT TRACKS. RECEIVED NEW SEAT TRACKS, LOCATED, DRILLED AND INSTALLED NEW SEAT TRACKS IAW DC8 SRM 51-3-0, 51-3-1, AND 51-1-21. 2L74 4F RT4A25 20060113000852006011300085WP 2006 1 13 IXXA0500176S 120050124A5753 BRACKET DOUG DC8 DC871F 302199DWP ZONE 500 WORN A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING ROUTINE C-CHECK FOUND LEFT WING OUTBOARD FLAP AT OUTBOARD FLAP TRACK UPPER SURFACE HAS BRACKET WORN / CHAFED THROUGH AND BAD FASTENERS. REMOVED BAD FASTENERS, FABRICATED NEW BRACKET, TREATED, PRIMED, INSTALLED NEW BRACKET AND FASTENERS IAW DC8 DRAWING 5763200, DC8 SRM 51-1-8, AND 51-3-1. 2L74 4F RT4A25 20060113000872006011300087WP 2006 1 13 IXXA0500178S 120050124A5753 SKIN DOUG DC8 DC871F 302199DWP ZONE 500 DENTED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING ROUTINE C-CHECK FOUND LEFT WING INBOARD FLAP LOWER SKIN DENTED SEVERAL PLACES. BLENDED TWO DENTS WITHIN LIMITS ONE DENT OUT OF LIMITS. REPAIRED OUT OF LIMIT DENT IAW DC8 SRM 57-2-0. TREATED AND PRIMED ALL DENTS IAW DC8 SRM 51-1-8. 2L74 4F RT4A25 20060113001172006011300117EU 2006 1 13 YENA200587 120051212A3230D235895201 FITTING AIRBUS320 A320232 3930326EU NOSE GEAR CRACKED A YENAO OTHER J WARNING INDICATION TOTAKEOFF 1 EA15547JB1375213752 1849 DEPARTED LGA, UPON GEAR RETRACTION ECAM GEAR UNSAFE. LANDING GEAR DOOR OPEN, FOLLOWED ECAM ACTIONS & REFERRED FCOM. CYCLED LANDING GEAR. GEAR RETRACTED NORMAL, ALL INDICATIONS NORMAL. PERFORMED INFO NOTICE 2005-TO46RA (LANDING GEAR) EO 3205121. ACCOMPLISHED NLG SHOCK ABSORBER CHARGE PRESSURE CHECK AND NOSE GEAR UPPER SUPPORT (BACK PLATE) INSPECTION. FINDINGS ON NOSE GEAR BORO REF (EO A3205121 REV F REVEALED LUG CRACKED AND SEPARATED ON AFT SIDE OF GEAR. REMOVED AND REPLACED NOSE LANDING GEAR, PERFORMED OPS CHECK OF NOSE RETRACTION, MANUAL GEAR EXTENSION, LEAK CHECK AND STEERING TEST REF AMM 32-21-11-04, 32-31-00-720-003, 32-30-00-720-001, 32-51-00720-003 TEST OK. 2L72 4F RTA28NM 20060113001202006011300120NM 2006 1 13 2006UALA00002 120051231A3350 LIGHT BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU CABIN INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29330UA 24191 AFT CABIN EEL LIGHTS INOP FROM ROW 15 AFT TO AND INCLUDING EEL STRIP IN FRONT OF AFT GALLEY CART STOWAGE COMPARTMENT. 2L72 4F4 FRTA16WE E21EU 20060113001222006011300122NM 2006 1 13 2006UALA00004 120051230A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29181UA 25278 EEL AT SEAT 5E AFT, 3J AFT, 5J AFT INOP. 2L74 4F4 FRTA20WE E24NE 20060113001242006011300124NM 2006 1 13 2006UALA00006 120051230A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29181UA 25278 EMERGENCY LIGHT ASSY AT RT BODY FAIRING INOP, 2ND ROW FROM FWD AND AT RT BODY FAIRING 2ND ASSY FROM AFT. 2L74 4F4 FRTA20WE E24NE 20060113001282006011300128WP 2006 1 13 0501719763 120051211A2170V1211 COALESCER BAG DOUG DC9 DC951 3022051WP PWA JT8 JT8D* NE AC SYSTEM CONTAMINATED A NWAAK NONE B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 GL01763NW 47396 JUST BEFORE LANDING AN ACRID SMELL WAS NOTICED IN THE AIRCRAFT. THE FLIGHT ATTENDANTS REPORTED THE RT AFT LAVATORY SMOKE DETECTOR WAS SOUNDING. NO VISIBLE SMOKE WAS SEEN AND NO FIRE WAS LOCATED. IT WAS NOTED THAT THE APU WAS NOT OPERATING. AIRCRAFT LANDED NORMALLY AND TAXIED TO THE GATE WITHOUT INCIDENT. MAINTENANCE DID NOT FIND A SOURCE FOR THE FUMES BUT REPORTED THE RT SEPARATOR SOCK AS (CONTAMINATED). NO LEAKS OF ANY TYPE (FLUID OR AIR) COULD BE FOUND. COMPLIED WITH BURNOUT PROCEDURES, REPLACED THE RT COALESCER BAG, AND RETURNED THE AIRCRAFT TO SERVICE. 2L72 4F4 FRTA6WE E2EA 20060113001292006011300129EU 2006 1 13 WRNA20050030 120051213A213381001B010300 OUTFLOW VALVE AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE CABIN PR.SYS UNSERVICEABLE A WRNAJA DUMP FUEL UNSCHED LANDING O OTHER CLCLIMB 1 SO05506TA 9 207 AFTER TAKEOFF USING SYSTEM NR1 NOTICED AFT OUTFLOW VALVE STAYED FULL OPEN. OPPOSITE SYSTEM SELECTED, NO HELP, UNABLE TO CLOSE MANUALLY. WITH BOTH PACKS ON COULD MAINTAIN 8500 FT CABIN ALTITUDE AT 14000 FT. DUMPED FUEL TO SAFE LANDING WEIGHT (APPROX 2600 GALS). RETURNED TO AIRFIELD, LANDING NORMAL. REPLACED SYSTEM NR 1 AFT PRESS AND SAFETY VALVE (OUTFLOW VALVE) IAW 21-31-13. SYSTEM FUNCTIONAL CHECK SATISFACTORY IAW 21-31-00 PG 501. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA35EU E23EA 20060113001322006011300132NM 2006 1 13 0501796308 120051220A3350 BULB BOEING747 747451 1384940NM PWA 4056 PW4056 NE TRACK LIGHT BURNED OUT A NWAAK NONE O OTHER ININSP/MAINT 1 GL01668US 24223 EMERGENCY TRACK LIGHTS OUT 72A AND SECTION B LT SIDE SEATS 10A TO 13A. REMOVED AND REPLACED EMERGENCY TRACK LIGHT BULBS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L74 4F4 FRTA20WE E24NE 20060113001342006011300134EU 2006 1 13 AWXA200501574 120051204A5230D53475765200 SILL AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28604AW 1196 SAL - MAJOR REPAIR - DURING BC4 CHECK DISCOVERED CORROSION ON BULK CARGO DOOR SILL, AROUND NUT PLATES, AT FR 61+9.5 AND Y-640. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-44-49 PAGE 403 FIG 101. FABRICATED DOUBLER AND FILLER IAW AIRBUS 320 SRM 53-41-49 FIG 203. INSTALLED FABRICATED REPAIR PARTS ON THE BULK CARGO DOOR SILL, AT FR 61+9.5 AND Y-640 IAW AIRBUS 320 SRM 53-41-49 FIG 203. 2L72 4F4 FRTA28NM E40NE 20060113001402006011300140EU 2006 1 13 AWXA200501580 120051204A5320D53472093000 BEAM AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28604AW 1196 DURING BC4 CHECK DISCOVERED LEVEL 2 GALVANIC CORROSION LOCATED ON BEAM ASSEMBLY AT FR 68 AND Y-765. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14 FIG 102. REMOVED AND INSTALLED NEW BEAM ASSEMBLY FROM FR 66+5 INCHES TO FR 70 AND Y-765 SRM 51-72-11. 2L72 4F4 FRTA28NM E40NE 20060113001462006011300146EU 2006 1 13 AWXA200501582 120051202A5347D5713014720000 SEAT TRACK AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28604AW 1196 DURING BC4 CHECK DISCOVERED CORROSION ON THE RT IB SEAT TRACK AT FR 39+5 INCH AND Y-765. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-31-15 FIG 101, PAGE 102. REMOVED AND INSTALLED NEW SEAT TRACK BETWEEN FR 36 AND FR 41, ALSO AT Y-765 IAW SRM 51-42-11. 2L72 4F4 FRTA28NM E40NE 20060113001482006011300148NM 2006 1 13 QXEA200501814 120051208A5347 SEAT TRACK BOMBDRDHC8 DHC8402 1390042NM PWC 150 PW150A EA FSX278 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09403QX 4037 RT OB SEAT TRACK NR 18 HAS PITTING CORROSION INSIDE CHANNEL AT APPROX FS X278. MAINTENANCE REPAIRED IAW SRM 51-40-15, SRM 51-42-00 AND SRM 51-42-45 2H72 4T4 TRTA13NM E00062EN 20060113001532006011300153EU 2006 1 13 AWXA200501606 120051222A3251C247360011 SERVO AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NLG INOPERATIVE A AWXAA UNSCHED LANDING J WARNING INDICATION DEDESCENT 1 WP28654AW241227 1050 EMERGENCY LANDING, CREW REPORTED NOSE WHEEL FAULT, PERFORMED TWO FLYBYS TO VERIFY NOSE GEAR LOCATION AND AN EMERGENCY WAS DECLARED. AIRCRAFT LANDED AND WAS TOWED TO THE GATE. NO FURTHER EVENTS OCCURRED. MAINTENANCE REMOVED AND REPLACED THE NLG SERVO CONTROL IAW MM 32-51-51. PART WAS INSTALLED IAW EVA 26-3251-05356-RL1. OPERATIONAL CHECK WAS GOOD. **SUPPLEMENTAL** WILL BE SUBMITTED UPON RECEIPT OF VENDOR TEAR DOWN REPORTS. 2L72 4F4 FRTA28NM E40NE 20060113001552006011300155NM 2006 1 13 AWXA200501608 120051221A21317638101 CONTROLLER BOEING737 7373G7 1384595NM GE CFM56 CFM563B1 13802NE CABIN PRESSURE UNKNOWN A AWXAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 WP28157AW32409 23779 CABIN PRESSURE CREW REPORTED DURING CRUISE, AT FL 330, CABIN ALT. HORN SOUNDED. CABIN ALT WAS AT 10,500 FT & DUCT PRESSURE AT 38 PSI. BOTH ENGINE BLEEDS WERE ON AND BOTH PACKS ON. UNABLE TO CONTROL CABIN IN STANDBY MODE. DESCENDED TO FL 240, & ABLE TO CONTROL CABIN IN MANUAL MODE, CABIN DESCENDED TO ALT OF 7500 AT FL 240. LANDED WITHOUT FURTHER EVENT. MX PLACED AUTOMATIC & STANDBY CABIN PRESSURE CONTROL SYSTEM ON MEL. REPLACED CABIN PRESSURE CONTROL IAW BOEING 737-300 MM 21-31-21. OPS CHK GOOD. COULD NOT CONFIRM FAILURE. UNIT WAS INSPECTED AND TESTED IAW MFG SPECIFICATIONS PER ATA 21-31-11 REV 14. 2L72 4F4 FRTA16WE E2GL 20060113001582006011300158WP 2006 1 13 ABXA050380 120051219A3260 LANDING GEAR DOUG DC9 DC931 3022065WP PWA JT8 JT8D7B 52053NE MAIN LDG GEAR OUT OF ADJUST A ABXAO OTHER J WARNING INDICATION CLCLIMB 1 GL23943AX 47528 AFTER TAKE-OFF WITH GEAR HANDLE UP, RT GEAR UNSAFE LIGHT ILLUMINATED ALONG WITH GEAR DOOR OPEN LIGHT. COMPLETED GEAR UPLATCH CHECK AND STILL HAD THE SAME INDICATIONS AS STATED ABOVE. RIGGED LT AND RT UPLATCHES, MAIN LANDING GEAR SEQUENCE PUSH PULL CABLES AND PERFORMED GEAR SWING IAW MM. NO DEFECTS NOTED. WORK ACCOMPLISHED ON WO 2005943. 2L72 4F4 F A6WE E2EA 20060113001672006011300167NM 2006 1 13 QXEA200501793 120051218A30607826895 BRUSH BLOCK DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE NR 2 PROP MALFUNCTIONED A QXEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM09364PH10714287 524 PDX FLIGHT NR 2043 RT TRU CAUTION LIGHT CAME ON IN CRUISE. MAINTENANCE REPLACED NR 2 PROP BRUSH BLOCK AND FUSES. FOUND TRU CIRCUIT BREAKER POPPED. RESET BREAKER IAW GMM 5-18-0. PERFORMED FUNCTION TEST OF TRU'S. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20060113001682006011300168SO 2006 1 13 ENHA2005PA311 120051215A2900 HYDRAULIC SYSTEM PIPER PA31 PA31350 7103110SO LYC O540 TIO540* 41532EA ENGINE LOW E ENHAA UNSCHED LANDING KS FLUID LOSS AFFECT SYSTEMS LDLANDING 1 AL0377HV 318152193 PILOT REPORTS AT FIRST DESTINATION, GEAR HANDLE TO LOWER LANDING GEAR, GEAR DID NOT TRANSIT TO DOWN POSITION, PILOT RETURNED AIRCRAFT TO AIRPORT, MANUALLY LOWERED GEAR TO 3 GREEN, DECLARED EMERGENCY, LANDED WITH OUT FURTHER INCIDENT. DETERMINED HYDRAULIC RESERVOIR REQUIRED SERVICE, SERVICED HYDRAULIC SYSTEM, INSPECTED LANDING GEAR, PERFORMED MULTIPLE EXTENSION AND RETRACTION FUNCTIONAL TESTS. NO FURTHER CORRECTIVE ACTION REQUIRED. 1L72 3O3 O A20SO E14EA 20060117000212006011700021NM 2006 1 17 2006UALA00012 120051230A5311 FRAME BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU BS 616 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29923UA 26643 CABIN FRAME CRACKED STA 616 RT IS CRACKED BELOW FLOOR. REMOVED THE CRACK, FABRICATED FILLER ANGLE REPAIR REF MM 53-11-89 AND INSTALLED. 2L72 4F4 FRTA16WE E21EU 20060117000222006011700022NM 2006 1 17 2006UALA00013 120051230A5241 FRAME BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU GALLEY DOOR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29923UA 26643 FWD GALLEY DOOR LOWER AFT FRAME CORNER IS CRACKED AT FASTENER LOCATION. MAJOR REPAIR ACP'D PER SRM 51-40-02 AND BACO DRAWING 69-69854 SPLICED NEW LOWER FRAME SECTION. NO FURTHER FINDINGS. O.K. FOR SERVICE. 2L72 4F4 FRTA16WE E21EU 20060117000252006011700025NM 2006 1 17 2006UALA00016 120051229A5311 FRAME BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU BS 380 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29923UA 26643 FWD LT CABIN STA 380 FRAME BETWEEN STRINGER 8 AND 9 CRACKED AT RIVET. REMOVED DAMAGE AND FABRICATED AND INSTALLED FILLER AND DOUBLER PER MM 53-10-84. 2L72 4F4 FRTA16WE E21EU 20060117000272006011700027NM 2006 1 17 2006UALA00018 120051229A5311 FRAME BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU BS 360 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29923UA 26643 RIGHT FWD CABIN STA 360 BETWEEN STRINGER 8 AND 9 CLIP AND FRAME CRACKED. REMOVED DAMAGE AND FABRICATED AND INSTALLED ANGLE AND FILLER AND STRINGER CLIP PER MM 53-10-84. 2L72 4F4 FRTA16WE E21EU 20060117000692006011700069WP 2006 1 17 IXXA0500208S 120051020A5300 REPAIR DOUG DC8 DC871F 302199DWP ZONE 100 TEMPORARY A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK, TO COMPLY WITH DTA REQUIREMENTS, REMOVED EXISTING EXTERNAL FUSELAGE DOUBLER AT STATION 1715 LONGERON 26 RIGHT. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED NEW DOUBLER REPAIR AT STATION 1670 TO 1753, LONGERON 24 RIGHT TO LONGERON 30 RIGHT IAW COOPESA EO COO-8-53-413-04. 2L74 4F RT4A25 20060117000812006011700081WP 2006 1 17 IXXA0500229S 120051005A5311 FRAME DOUG DC8 DC871F 302199DWP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND FRAME CORRODED AT STATION 1260 LONGERON 33 RIGHT TO LONGERON 34 RIGHT. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS AND FASTENERS IAW DC8 SRM 51-2-1, 53-4-1, 51-1-4, 51-1-5 AND 51-1-8. 2L74 4F RT4A25 20060117000962006011700096WP 2006 1 17 IXXA0500158S 120050308A5711 SPAR CAP DOUG DC8 DC871F 302199DWP RT WING CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11821BX858952998 45811 DURING A ROUTINE C-CHECK INSPECTION FOUND RT WING UPPER FRONT SPAR CAP STRUCTURE HAS CRACK DAMAGE BETWEEN STA XFS -6 CAP. MAJOR REPAIR ACCOMPLISHED REMOVAL OF FASTENERS. REMOVED CORROSION FROM SLANT PANEL UPPER CAP AND FOUND OUT OF LIMITS. CLEANED, TREATED AND PRIMED AREA. INSTALLED DOUBLER AND REMOVED UPPER SPAR CAP DAMAGE. REMOVED STIFFENER AND PERFORMED NDT INSPECTION. APPLIED SEALING TO ALL FAYING SURFACES AND INSTALLED DOUBLER, ANGLE DOUBLER AND INSTALLED KIT (S/N 0570072-3). TORQUED IAW S/B DC8 57-072 RO3, DWG, DACO 5892075, CN1, DC8 SRM 51-1-8, 51-1-11, 51-1-15, 51-1-20D, 51-1-22, 51-1-26, 51-3-30, 51-3-1, 57-2-0, 57-2-1, 57-3-1, 57-3-2, DPS 1.05-8, 3.67-3, 2.50. 2L74 4F RT4A25 20060117001122006011700112NM 2006 1 17 TSAA0553056 120051214A53306545774 SKIN PANEL BOEING737 737230 1384401NM BS 767 CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13820AL 22138 FOUND TWO FUSELAGE SKIN CRACKS AFT OF LT AFT WING-TO-BODY FAIRING: .5 INCH CRACK AT BS 767, STRINGER 17L AND 3 INCH CRACK AT BS 787, STRINGER 18L. CUT CRACKS OUT .040 INCH INSURANCE CUT. PERFORMED HFEC AROUND CUTOUTS, NO CRACK PROPAGATION NOTED IAW BOEING NDT MANUAL PART 6, 51-00-00. REPAIRED WITH 21 X 53 INCH SKIN PATCH: FABRICATED DOUBLER (0322024T3) AND TRIPLER (0502024T3). REPAIRED CRACKS PER SRM 53-30-3, FIG 48, DETAIL XI. 2L72 4F RTA16WE 20060117001142006011700114NM 2006 1 17 TSAA0553059 120051024A53406546547591 CLIP BOEING737 737230 1384401NM BS 727 CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13821AL 23155 BULKHEAD BS 727, WL 202.6, RBL 10.0", CLIP UPPER CRACKED. 2L72 4F RTA16WE 20060117001162006011700116NM 2006 1 17 TSAA0553057 120051213A53306545778 SKIN PANEL BOEING737 7372T4 1384492NM BS 927 CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13808AL 23445 A 3.5 INCH CRACK FOUND RIGHT SIDE OF FUSELAGE SKIN AFT OF AFT CARGO DOOR AT BS 927 STRINGER 23R. CUT OUT CRACK .040 INCH INSURANCE CUT. PERFORMED HFEC AROUND CUTOUT, NO CRACK PROPAGATION NOTED IAW BOEING NDT MANUAL 51-00-00, PART 6. REPAIRED WITH 10 X 13 INCH SKIN PATCH, FABRICATED DOUBLER (0322024T3) AND TRIPLER (0502024T3). REPAIR COMPLETED IAW SRM 53-30-3, FIG 48, DETAIL XI. 2L72 4F A16WE 20060117001232006011700123NE 2006 1 17 YENA200589 220051223A7532AC69924 BLEED VALVE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 1 ENGINE FAILED A YENAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 EA15546JB1399113991 1827 V11244 AFTER TAKEOFF EN ROUTE TO LGB EXPERIENCED NR 1 ENGINE STALL WITH FULL RECOVERY. A/C AT 11,000 FEET AND 300 KTS. RETURNED TO JFK. PERFORMED TSM TASK 71-00-810-808. CHECKED 7A, 7B, 7C BLEED VALVE AND SOLENOID REF AMM 75-32-52. FOUND 7B VALVE FAILED. REPLACED BLEED VALVE 7B REF AMM 75-32-52. OPS CHECK OK. PERFORMED VSV LUBE REF AMM 75-32-42. CHECKED 2.5 BLEED ACT 4021KS LVDT AND TORQUE MOTOR AND CHAN A & B. REF TSM 75-30-00-810-856 CKS OK. BOROSCOPE PERFORMED NO FINDINGS. PERFORMED HIGH POWER ASSURANCE TEST AS PER AMM 71-00-00. OPS CHECK OK. 2L72 4F4 FRTA28NM E40NE 20060117001252006011700125 2006 1 17 PIDA06003 420050103A221010618165 FORCE LIMITER BOEING737 737306 13844BGNM AUTO PILOT MALFUNCTIONED A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05371PA 23543 A & B AUTO PILOT DISCONNECTS. REPLACED AILERON FORCE LIMITER PER MM 22-11-13. OPS CHECKS GOOD. 2L72 4F RTA16NE 20060117001452006011700145WP 2006 1 17 IXXA0500144S 120050225A5313 LONGERON DOUG DC8 DC871F 302199DWP BS 1770 L17R CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11821BX858952998 45811 DURING A ROUTINE C-CHECK INSPECTION FOUND RT FUSELAGE TAIL SECTION STRUCTURE LONGERON 17 RT HAS CRACK DAMAGE STA 1770.00. MAJOR REPAIR ACCOMPLISHED REMOVAL OF CRACKED LONGERON. FABRICATED NEW LONGERON, CLEANED, TREATED AND PRIMED AREA. APPLIED SEALANT TO FAYING SURFACES. INSTALLED NEW LONGERON IAW DC8 SRM 53-1-0 PG 1, 53-5-1 FIG 7 SH 1, 51-2-0 FIG 50 SH 37, 51-1-20D, 51-1-21, 51-3-1. 2L74 4F RT4A25 20060117001472006011700147WP 2006 1 17 IXXA0500134S 120050224A5730 PANEL DOUG DC8 DC871F 302199DWP WS 74.869 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11821BX858952998 45811 DURING A ROUTINE C-CHECK INSPECTION FOUND RT INNER WING AFT TOP PANEL PLATING CRACK DAMAGE AT STA XRS 74.869, S-2. MAJOR REPAIR ACCOMPLISHED REMOVAL OF FASTENERS AND DAMAGED SECTION. FABRICATED EXTERNAL DOUBLER + FILLER PLUG. CLEANED, TREATED AND PRIMED AREA AND REPAIR DOUBLER + FILLER PLUG. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS IAW SEMAN DRAWING ED-3831 AND FAA FORM 8110-3 05020, DC8 SRM 51-1-11, 51-1-20D, 51-1-22, 51-1-26, 51-3-1, 51-3-2. 2L74 4F RT4A25 20060117001502006011700150EU 2006 1 17 USAA051669 120051229A5315D53472090002 FLOORBEAM AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19114UW 1148 FLOORBEAM Y765 AT FR 66 CORRODED. REMOVED & REPLACED FLOORBEAM PER SRM 51-42-21, DEFECT SIZE: 1 X 1 INCH. 2L72 4F RTA28NM 20060117001712006011700171NM 2006 1 17 AWXA200600036 120051215A5210146N6100488 SKIN BOEING757 757225 1384959NM R4 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28907AW 22691 GYR - MAJOR REPAIR - MAINTENANCE DISCOVERED THE R4 DOOR INNER SKIN CRACKED, .5 INCHES, BELOW WINDOW CUTOUT AT BS 1661 TO BS 1662 AND FROM WL 258 TO WL 260. MAINTENANCE CUT OUT DAMAGED PORTION OF SKIN IAW BOEING 757-200 SRM 51-70-13. FORMED REPAIR DOUBLER AND SHIM IAW BOEING 757-200 SRM 52-10-01-0I 4 FIG 1. INSTALLED FABRICATED REPAIR PARTS AT BS 1661 TO 1662 AND FROM WL 258 TO WL 260 IAW BOEING 757-200 SRM 51-70-13-06 FIG 2. 2L72 4F RTA2NM 20060117001732006011700173NM 2006 1 17 AWXA200600038 120051224A5310 VERTICAL BEAM BOEING737 73733A 1384673NM BS 178 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED VERTICAL BEAM WEB CRACKED, .375 INCHES, AT BS 178, WL 229 AND BL 17.1R. MAINTENANCE REMOVED WEB AT BS 178 IAW BOEING 737-300 SRM 51-40-02-0G. FABRICATED REPLACEMENT WEB IAW BOEING DRAWING 65-17582. INSTALLED FABRICATED REPAIR PARTS AT BS 178, WL 229 AND BL 17.1R IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 8 AND 12. 2L72 4F RTA16WE 20060117001752006011700175NM 2006 1 17 AWXA200600040 120051221A575465C26601174SP WEDGE BOEING737 73733A 1384673NM SLAT DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED DISBOND AREA ON THE TOP OF THE NO. 6 SLAT WEDGE ABOVE THE INBOARD AUX TRACK AT WS 344R TO WS 348.5R. MAINTENANCE REMOVED DAMAGED AREA ON THE NO. 6 SLAT WEDGE IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED FILLER AND DOUBLER IAW BOEING 737-300 SRM 51-70-10-2R4. BONDED AND SEALED FABRICATED REPAIR PARTS TO THE NO. 6 SLAT WEDGE IAW BOEING 737-300 SRM 51-70-10-2R4. 2L72 4F RTA16WE 20060117001852006011700185NM 2006 1 17 ASAA0510339 120051011A53206545401104 STIFFENER BOEING737 737298C 1384490NM FS 540 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02745AS 20794 YXX - VERTICAL STIFFENER AT BS 540, RBL 54 SEVENTH VERTICAL STIFFENER FROM CENTERLINE CORRODED. REPLACED STIFFENER IAW B737-200 SRM 57-30-2. (M) 2L72 4F RTA16WE 20060117001872006011700187NM 2006 1 17 ASAA0510341 120051018A335086210144 BATTERY PACK BOEING737 7372X6C 1384552NM EMERGENCY LIGHTSINOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM02746AS 23123 ANC - FOUND ALL FOUR DOOR EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED L-1, L-2, R-1 AND R-2 EMERGENCY EXIT LIGHT BATTERY PACKS PER AMM 33-50-0. (M) 2L72 4F RTA16WE 20060117001892006011700189NM 2006 1 17 ASAA0540554 120051018A531165C280332 FRAME BOEING737 7374Q8 138447QNM FS 360 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - FOUND FRAME CRACKED. REPAIRED FRAME IAW 737-400 SRM 53-00-07. (M) 2L72 4F RTA16WE 20060117002042006011700204NM 2006 1 17 ASAA0540543 120051013A57536546486150 SKIN BOEING737 737490 1384715NM TE FLAP PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02794AS 28889 OKC - FOUND DURING RIGHT WING INBOARD MID FLAP T/E PANEL LOWER SKIN IS PUNCTURED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PIECES PER B737-200 SRM 51-70-10. (M) 2L72 4F RTA16WE 20060117002062006011700206NM 2006 1 17 ASAA0540549 120051015A575465C26602312A SKIN BOEING737 737490 1384715NM NR 5 SLAT DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02794AS 28889 OKC - NR 5 SLAT INBOARD TRAILING EDGE IS DELAMINATED. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW 737-400 SRM 51-70-10. (M) 2L72 4F RTA16WE 20060117002092006011700209NM 2006 1 17 ASAA0540548 120051015A575465C26601389 SKIN BOEING737 737490 1384715NM NR 1 SLAT CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02794AS 28889 OKC - FOUND NR 1 SLAT LOWER T/E IS CHAFED. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW 737-400 SRM 51-70-10. (M) 2L72 4F RTA16WE 20060117002152006011700215NM 2006 1 17 ASAA0540567 120051026A5320654587514 ANGLE BOEING737 7374Q8 138447QNM FS 317 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - FOUND CORROSION ON Z-ANGLE. REPLACED Z-ANGLE PER B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060117002172006011700217NM 2006 1 17 ASAA0540546 120051012A52106044552 SHAFT BOEING737 7374Q8 138447QNM R1 DOOR HANDLE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 SEA - R-1 DOOR HANDLE WILL NOT STAY IS STOWED POSTION. DOOR HANDLE SHAFT AND SLEEVE ASSY WAS REPLACED AND DOOR RIGGED PER AMM. (M) 2L72 4F RTA16WE 20060117002192006011700219NM 2006 1 17 ASAA0540582 120051028A534065C161215 FITTING BOEING737 7374Q8 138447QNM FS 340 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - FOUND CORROSION ON FITTING. REMOVED AND REPLACED FITTING PER B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060117002212006011700221NM 2006 1 17 ASAA0540572 120051025A552365C2638424A TAB BOEING737 737490 1384715NM RT ELEVATOR BENT A ASAAK NONE O OTHER ININSP/MAINT 1 NM02794AS 28889 OKC - FOUND RIGHT ELEVATOR TAB BENT AT T/E. PREPPED AREA, BONDED REPAIR PER B737-400 SRM 51-70-05 FIGURE 8. (M) 2L72 4F RTA16WE 20060117002232006011700223NM 2006 1 17 ASAA0540588 120051028A533069152242 SKIN BOEING737 7374Q8 138447QNM FS 492.4 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - BS 492.4 RBL 28 FORWARD CARGO DOOR CUTOUT FORWARD SIDE OF CLOSEOUT WEB IS CRACKED .250 INCH. REMOVED DAMAGED SECTION, FABRICATED REPAIR PARTS AND INSTALLED PER B737-400 SRM 51-70-13 FIG 1. (M) 2L72 4F RTA16WE 20060117002252006011700225NM 2006 1 17 ASAA0540538 120051012A532265C323595 SHEAR TIE BOEING737 737490 1384715NM FS 460 BENT A ASAAK NONE O OTHER ININSP/MAINT 1 NM02793AS 28888 PAE - FOUND FRAME SHEAR TIE BENT. REPAIRED FRAME SHEAR TIE AT BS 460, RBL 8 PER EA 5330-02006. (M) 2L72 4F RTA16WE 20060117002272006011700227NM 2006 1 17 ASAA0540536 120051012A5320655384422 FLOOR SUPPORT BOEING737 737490 1384715NM FS 727E CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02793AS 28888 PAE - FLOOR SUPPORT CRACKED AT FRAME FASTENERS. REPAIRED CRACKED FLOOR SUPPORT PER B737-200 SRM 53-00-53. (M) 2L72 4F RTA16WE 20060117002372006011700237NM 2006 1 17 ASAA0540593 120051101A531565468102 FLOORBEAM BOEING737 7374Q8 138447QNM FS 967 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND CORROSION ON FLOORBEAM. REPAIRED FLOORBEAM PER B737-400 SRM 53-60-51. (M) 2L72 4F RTA16WE 20060117002392006011700239NM 2006 1 17 ASAA0540563 120051025A531565C3394311 FLOORBEAM BOEING737 7374Q8 138447QNM FS 344 GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - FOUND CORRODED FLOORBEAM. REMOVED DAMAGED SECTION OF FLOORBEAM, FABRICATED T-CHORD, REPAIR PARTS AND INSTALLED. (M) 2L72 4F RTA16WE 20060117002932006011700293EU 2006 1 17 USAA051667 120051229A5320D53472831 FLOOR SUPPORT AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19114UW 1148 FOUND FLOORBEAM CORRODED Y1292 BETWEEN FR 66 AND 68. REMOVED AND REPLACED THREE PIECE FLOORBEAM PER DWG 53472831; SRM 51-42-11, DEFECT SIZE: 3" X 6'. 2L72 4F RTA28NM 20060117002952006011700295NM 2006 1 17 DL75K050821 120051223A3350 BULB BOEING757 757232 1384965NM EMERGENCY LIGHT BURNED OUT A DALAK NONE L NO TEST ININSP/MAINT 1 SO27608DA 22815 FOUND 1R DOOR EXT EMERGENCY LIGHT INOP. RELAMPED. 2L72 4F RTA2NM 20060117003002006011700300NM 2006 1 17 DLM88050828 120051226A2400 GENERATOR DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 1 ENGINE BURNED A DALAH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CRCRUISE 1 SO27985DL 53312 718235 LEFT GENERATOR OFF LIGHT WITH CROSSTIE LOCKOUT, LEFT ENGINE FIRE INDICATION, REPLACED GENERATOR AND CSD. 2L72 4F4 FRTA6WE E9NE 20060117003022006011700302NM 2006 1 17 DL75K050830 120051226A5330143N33406 SKIN BOEING757 757232 1384965NM BS 445 S22L DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27608DA 22815 FOUND LIGHTNING STRIKE DAMAGE FOUND ON FUSELAGE SKIN AT THE FIFTH FASTENER AFT OF BS 440 BUTT JOINT COMMON TO STR 22L. BURNED AREA OF SKIN WAS CUT OUT AND A DOUBLER WAS INSTALLED. 2L72 4F RTA2NM 20060117003042006011700304NE 2006 1 17 DL76L050832 220051228A7200PW40603 ENGINE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 2 FAILED A DALAE ENGINE SHUTDOWN EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 SO27175DN37219 24803 727649 PASSING THRU 7K FEET ABOUT 4 MINS AFTER T/O, THE RIGHT ENG EXPERIENCED A VIOLENT SURGE WITH VIBRATIONS. THROTTLE PULLEDBACK TO IDLE AND EGT CONTINUED TO CLIMB. ENG SHUTDOWN WITH FUEL CUTOFF SWITCH. EGT REACHED 722 DEGS BEFORE SHUTDOWN AND N1 ROLLED BACK. MX FOUND METAL IN THE TAILPIPE. 4 TIRES BLOWN AFTER PULLING OFF THE RUNWAY. 2L72 4F4 FRTA1NM E24NE 20060117003062006011700306NM 2006 1 17 DL76L050834 120051228A5101 DUCT BOEING767 767332 1382001NM RIGHT UNKNOWN A DALAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO27196DN 28453 RT DUCT LEAK LP 1. RETURN TO BLOCK. TESTED DUCT LEAK. UNABLE TO DUPLICATE OR FIND FAULT. 2L72 4F RTA1NM 20060117003082006011700308NM 2006 1 17 DL733050836 120051228A2910NAS16128 PACKING BOEING737 737347 1384647NM HYD SYSTEM SPLIT A DALAO OTHER KJ FLUID LOSS WARNING INDICATION LDLANDING 1 SO27312WA 23598 DECLARED EMERGENCY HYD QTY A DROPPED TO 1/2. REPLACED LOWER PACKING ON A HYD SYS EMDP ACCOUSTIC FILTER, LEAK CK OK HYD SERVICED. 2L72 4F RTA16WE 20060117003242006011700324NM 2006 1 17 PCSA12020501 120051202A5101 UNKNOWN BOEING727 727225 1384077NM PWA JT8 JT8D NE UNKNOWN NOISY A PCSAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 SO29604AJ 21453 AFTER DEPARTURE FLT 8412 CLIMBED TO CRUISE FL320, REPORTED ACFT EXPERIENCED A LOUD BANG & SUBSEQUENT SIGNIFICANT VIBRATION, RETURNED, VIBRATION FELT BY CREW SEVERAL TIMES PRIOR TO LANDING. MX PREFORMED A VISUAL INSP OF THE NR 1, 2, & 3, ENG INTAKES & EXHAUST IAW MM, NO DAMAGE NOTED. ALL 3 ENG MAIN OIL FILTERS INSP FOR CONTAMINATION IAW PWA MM0. NO DISCREPANCIES NOTED. ALL 3 ENGINES INSP FOR SECURITY & LOOSENESS OF COMPONENTS IAW MM, NO DISCREPENCIES NOTED. ALL 3 ENGINE SADDLE DUCTS INSP FOR SECURITY IAW MM, NO DISCREPENCIES NOTED. ACCOMPLISHED ENGINE RUN. NO DISCREPENCIES NOTED. A DETAILED VISUAL INSP OF AIR CON COMPONANTS & DUCTS PERFORMED IAW 21-20-0, NO DISREPENCIES NOTED, ACFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 20060117003272006011700327NM 2006 1 17 SCNA05014 120051204A2620 NONE BOEING737 7378Q8 13844BXNM CFMINTCFM567CFM567B2US 13802NE UNKNOWN A SCNAK NONE J WARNING INDICATION CLCLIMB 1 GL15801SY 30332 AMBER CARGO FIRE (DISCH) LITE ILLUMINATED ON CLIMBOUT. EXTINGUISHED AFTER ABOUT 10 MINUTES. MAINTENANCE OPERATED TEST SEVERAL TIMES COULD NOT DUPLICATE IAW 26-16-00-710-801. OK FOR SERVICE. 2L72 4F4 FRTA16WE E2GL 20060113001352006011300135EU 2006 1 13 AWXA200501575 120051203A5315D53112818200 FLOORBEAM AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28604AW 1196 DURING BC-4 CHECK DISCOVERED CORROSION ON THE FLOORBEAM LOCATED AT FR 16 AND Y254. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14 PAGE 109, FIG 104. MAINTENANCE CUT OUT DAMAGED AREA IAW SRM 53-11-14. FABRICATED ANGLES AND SUPPORT FLOOR IAW SRM 53-11-14 PAGE 213 AND 214. INSTALLED FABRICATED REPAIR PARTS AT FR 16 AND Y254 IAW SRM 53-11-14. 2L72 4F4 FRTA28NM E40NE 20060113001372006011300137EU 2006 1 13 AWXA200501577 120051204A5320D53480043203 SILL AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE RT SIDE OF CABINCORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28604AW 1196 DURING BC4 CHECK DISCOVERED LEVEL 2 GALVANIC CORROSION ON THE LOWER SILL, RT SIDE OF CABIN, AT FR 66 AND Y-1732. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14. FABRICATED ANGLE AND FILLERS IAW SRM 53-41-14. INSTALLED FABRICATED REPAIR PARTS AT LOWER SILL FR 66 AND Y-1732 IAW SRM 53-41-14 REPAIR NO. 6 FIG 201. 2L72 4F4 FRTA28NM E40NE 20060113001382006011300138EU 2006 1 13 AWXA200501578 120051203A5320D53112600200 RAIL AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28604AW 1196 DURING BC4 CHECK DISCOVERED LEVEL 2 GALVANIC CORROSION LOCATED ON RAIL ASSEMBLY AT FR 16 AND Y503.2. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14 FIG 103. REMOVED AND INSTALLED NEW RAIL ASSEMBLY AT FR 16 AND Y503.2 IAW SRM 51-42-11. 2L72 4F4 FRTA28NM E40NE 20060113001392006011300139EU 2006 1 13 AWXA200501579 120051130A5230D53475765206 SILL AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUS. DOOR SILL CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28603AW 661 DURING C6 CHECK DISCOVERED CORROSION ON BULK FUSELAGE DOOR SILL AROUND 5 NUT PLATE HOLES OVER STR. 38R, Y-670 AND BETWEEN FR 60+1 INCH AND FR 62. MAINTENANCE REWORKED THE DAMAGED ARE AND WAS FOUND OUT OF LIMITS IAW SRM 53-41-49 PAGE 103, FIG 101. CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND FABRICATED REPAIR FILLER IAW SRM 53-41-49 PAGE 221 TO PAGE 222. INSTALLED FABRICATED REPAIR PARTS AT STR 38R, Y-670 AND BETWEEN FR 60+1" AND FR 62 IAW SRM 53-41-49. 2L72 4F4 FRTA28NM E40NE 20060113001512006011300151NM 2006 1 13 QXEA200501818 120051206A5347 SEAT TRACK BOMBDRDHC8 DHC8402 1390042NM PWC 150 PW150A EA RT IB FLOOR FTNGCORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09403QX 4037 RT IB SEAT TRACK NR 10 HAS CORROSION ON TOP OF TRACK AT APPROX FS X3, ALSO UNDER FWD BAG COMPARTMENT FLOOR FITTING AT FS X3. MAINTENANCE REPAIRED IAW NDTM PART 6, 51-00-02 AND RD 8/4-53-884. 2H72 4T4 TRTA13NM E00062EN 20060113001542006011300154EU 2006 1 13 AWXA200501607 120051202A5347D5337111200500 SEAT TRACK AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28604AW 1196 DURING BC4 CHECK DISCOVERED CORROSION ON RT OB SEAT TRACK AT FR42+1 INCH. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-31-15 FIG 101. REMOVED AND INSTALLED NEW SEAT TRACK FROM FR 41 TO FR 47 AND Y-1292 IAW SRM 51-72-11. 2L72 4F4 FRTA28NM E40NE 20060113001652006011300165NM 2006 1 13 HNAA0500103 120051215A304083040015005 WINDSHIELD WIPER DHAV DHC8 DHC8102 2809003NM PWA PW120 PW123 NE RT WINDSHIELD OUT OF ADJUST A HNAAK NONE O OTHER CRCRUISE 1 EA07965HA1554715547 450 F/O'S WINDSHIELD WIPER POPPED UP. ADJUSTED AND SECURED WIPER BLADE. 2H72 4T4 TRTA13NM E20NE 20060113001662006011300166NM 2006 1 13 QXEA200501792 120051218A30607826895 BRUSH BLOCK DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE BURNED A QXEAA UNSCHED LANDING JS WARNING INDICATION AFFECT SYSTEMS CLCLIMB 1 NM09355PH4032 87 500 SEA FLIGHT NR 2285 LT TRU CAUTION LIGHT AND ASSOCIATED CIRCUIT BREAKERS POPPED. LT PROP HEAT LIGHTS NOT ILLUMINATING. MAINTENANCE FOUND NR2 BRUSH BLOCK BURNED, REPLACED BRUSH BLOCK IAW Q200 AMM 61-10-11 AND 61-10-11-820-801. ALSO FOUND AC FUSE POPPED. REPLACED FUSE AS REQUIRED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20060113001702006011300170EU 2006 1 13 MALA050882 120051219A5230 FLANGE BAC 146 AVRO146RJ85A1500097EU AIR DOOR DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15526XJ E2351 GROUND AIR DOOR FLANGE DAMAGED AND REPAIRED IAW EO 5344. 2H74 4F RTA49EU 20060118000162006011800016CE 2006 1 18 DXTA200601194 120050113A2400 UNKNOWN CESSNA750 750 2076810CE BUSS NR 1 UNKNOWN E DXTAO OTHER H ELECT. POWER LOSS-50 PC DEDESCENT 1 GL07948QS 7500149 TEN MILES FROM DESTINATION AIRPORT, BUSS NR 1 WENT TO EMERGENCY POWER. DECLARED EMERGENGY AND LANDED SAFELY. ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20060118001502006011800150NM 2006 1 18 2005UALA01239 120051107A5720313T3380393 ANGLE BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE LT WING CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29668UA 30024 LEFT WING, LEFT PYLON, AFT BULKHEAD, LOWER OUTBOARD ANGLE CRACKED. *S/D* THE LEFT WING LEFT PYLON, AFT BULKHEAD LOWER OUTBOARD ANGLE WAS FOUND CRACKED ON A/C 6768 DURING A C-CHECK VISIT. CRACK IS DUE TO FATIGUE. CRACKED ANGLE WAS REPLACED AND INSTALLED PER SRM 51-40-2. 2L72 4F4 FRTA1NM E24NE 20060118001522006011800152NM 2006 1 18 2005UALA01257 120051110A5330 SKIN BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE BS 1587 LIGHTNING STRIKEA UALAK NONE O OTHER ININSP/MAINT 1 WP29647UA 25284 LIGHTNING STRIKE AT LEFT FUSELAGE STA 1587 JUST AFT OF PRESSURE BULKHEAD. *S/D* LIGHTNING STRIKE DAMAGE CUT OUT AND REPAIRED PER SRM. 2L72 4F4 FRTA1NM E24NE 20060118001542006011800154CE 2006 1 18 DXTA200501162 120051227A2741 WHEEL CESSNA560 560XL 2076702CE TRIM SYSTEM OUT OF ADJUST E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07675QS 5605275 DURING TAKEOFF AS A/C ACCELERATED TO 60 KIAS, A/C WANTED TO OVER-ROTATE. TAKEOFF ABORTED. PITCH TRIM DID NOT MOVE DURING ROLL ON TAKEOFF. TRIM WHEEL FOUND TO BE AT NOSE UP STOP THOUGH INDICATOR IN TAKEOFF POSITION. NO TAKEOFF HORN, NEVER SOUNDED NOR DID LIGHT COME ON. NO TAKEOFF LIGHT COMES ON WHEN TRIM WHEEL MOVED OUT OF MARKED TAKEOFF AREA ON PEDESTAL. ELEVATOR TRIM WHEEL OUT OF ADJUSTMENT, RE-INDEXED ELEVATOR TRIM WHEEL. PERFORMED OPS CHECKS ON ELEVATOR TRIM WHEEL, OPS CHECKS GOOD. RESTORED A/C TO NORMAL. 2L72 4F RTA22CE 20060118001842006011800184EU 2006 1 18 AWXA200600047 120051123A5610NP1653116 WINDOW AIRBUS320 A320232 3930326EU COCKPIT FAILED A AWXAB EMER. DESCENT O OTHER CRCRUISE 1 WP28658AW9543 9543 1110 CREW REPORTED THAT DURING CRUISE, EN ROUTE TO BOS, THE F/O'S WINDOW MIDDLE PANE SHATTERED AND WAS ARCING. PER QRH CREW WAS TO DESCEND. DECLARED EMERGENCY TO EXPEDITE DESCENT. ONCE AT LOWER ALTITUDE CANCELLED EMERGENCY AND CONTINUED TO BOS, LANDING WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED THE F/O'S WINDSHIELD AND THE WHC, RIGHT SIDE. REPORTED FOR PRECAUTIONARY PURPOSES, EMERGENCY WAS DECLARED DUE TO TRAFFIC IN AREA THEN EMERGENCY CANCELLED. COMPUTER, WINDOW HEAT; PN 416-00318-003; SN 4160031800264; MFG PPG; TT 9543; TC 3662; TSR 9543. 2L72 4F RTA28NM 20060118001992006011800199NM 2006 1 18 P5CA0601423 120051220A5230130E10013 ACTUATOR BOEING747 74746NF 13848BTNM GE CF6 CF680C2* GL FAILED A P5CAO OTHER Z SIGNIFICANT FAILURE REPORT TXTAXI/GRND HDL 1 EA15453PA 30811 SIDE CARGO DOOR INOP ELECTRICALLY AND MANUALLY. PWR LIFT ACTUATIOR REPLACED IAW MM 52-32-02. OPS CHECK OK. 2L74 4F4 FRTA20WE E23EA 20060118002082006011800208CE 2006 1 18 Y9A2006F00000 120051125A3230504501019 BELLCRANK CESSNA414 414 2075908CE CONT O520 TSIO520NB 17040SO MCAULY3AF32C3AF32C93 GL LT MLG CRACKED E Y9AAA UNSCHED LANDING O OTHER TOTAKEOFF 1 EA09155SW 4140957 813736R 980388 LT MAIN GEAR BELLCRANK ASSY CRACKED AND FAILED WHEN GEAR SELECTED UP. LT MAIN GEAR RETURNED TO DOWN AND LOCK. BELLCRANK TUBE BROKE AND TWISTED AS IT FAILED. CRACK RADIATED FROM REAR WELDS TO FORK BOLT SOCKETT AND FWD. (EA09200600710) (K) 1L72 3O3 ORTA7CE E8CE 5 CP22EA 20060118002122006011800212 2006 1 18 GTIA050290 420051218A2565 SLIDE DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE DETACHED A GTIAK NONE O OTHER UKUNKNOWN 1 GL23822NK 49392 FWD ENTRY DOOR SLIDE PACK CAME OFF. REINSTALLED SLIDE PACK. (K) 2L72 4F4 FRT E9NE 20060119000052006011900005WP 2006 1 19 ABXA060037 120051207A5320 INTERCOSTAL DOUG DC8 DC863F 302198FWP BS 30 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 UPPER CARGO, STA 30, LEFT BUTT LINE 48, INTERCOSTAL HAD CORROSION JUST AFT OF MAIN CARGO DOOR CONTROL BOX. REMOVED CORROSION ON INTERCOSTAL BEAM AT STA 30, LEFT BUTT LINE 48, AND DETERMINED AREA WAS OUT OF LIMITS. FABRICATED DOUBLER, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 53-2-0, FIG 1F, 53-2-0, FIG 23, 51-1-8, 51-1-21 AND LWR 200302015. 2L74 4F 4A25 20060119000142006011900014NM 2006 1 19 AWXA200600053 120051217A53156546568611 FLOORBEAM BOEING737 7373G7 1384595NM BS 1016 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 MCN - DURING C15 CHECK DISCOVERED CORROSION ON THE BOTTOM OF BS 1016 BEAM, UPPER T-CAP AT BL 33R AND WL 208. CORROSION WAS FOUND OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-51-1A1 FIG 101. MAINTENANCE CUT OUT DAMAGED AREA OF BEAM IAW BOEING 737-300 SRM 53-00-51-2R2. FABRICATED REPAIR ANGLE, SUPPORT ANGLE AND STRAPS IAW BOEING 737-300 SRM 53-00-51-2R2. INSTALLED FABRICATED REPAIR PARTS AT BS 1016, BL 33R AND WL 208 IAW BOEING 737-300 SRM 53-00-51-2R2. 2L72 4F RTA16WE 20060119000152006011900015NM 2006 1 19 AWXA200600054 120051217A531569387776 FLOORBEAM BOEING737 7373G7 1384595NM BS 986 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 MCN - DURING C15 CHECK DISCOVERED CORROSION ON THE BS 986 BEAM, TCAP FROM BL 4.5L TO 33R AND WL 208. CORROSION WAS FOUND OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-51-1A1 FIG 101. MAINTENANCE CUT OUT DAMAGED AREA OF BEAM IAW BOEING 737-300 SRM 53-00-51-2R2. FABRICATED REPAIR BEAM TCAP SECTION IAW BOEING 737-300 SRM 53-00-51-2R2. INSTALLED FABRICATED REPAIR PARTS AT BS 986, FROM BL 4.5L TO 33R AND WL 208 IAW BOEING 737-300 SRM 53-00-51-2R2 2L72 4F RTA16WE 20060119000182006011900018NM 2006 1 19 AWXA200600058 120051217A532065C3267723 SHEAR WEB BOEING737 7373G7 1384595NM BS 986-1006 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 MCN - DURING C15 CHECK DISCOVERED CORROSION ON THE AFT RT WEB FROM BS 986 TO BS 1006 AND FROM BL 35R TO BL 41R AT WL 208. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-51-1A1. MAINTENANCE REMOVED WEB, FABRICATED REPLACEMENT WEB AND INSTALLED FROM BS 986 TO BS 1006, FROM BL 35R TO BL 41R AND WL 208 IAW BOEING 737-300 SRM 51-40-02-0G AND 53-60-51-1A1. 2L72 4F RTA16WE 20060119000192006011900019NM 2006 1 19 AWXA200600059 120051217A532065C327076 SHEAR WEB BOEING737 7373G7 1384595NM BS 1022-1031 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 MCN - DURING C15 CHECK DISCOVERED LEVEL 2 GALVANIC CORROSION ON THE TOP AND BOTTOM SURFACE OF THE RT AFT MAIN DECK SHEAR WEB FROM BS 1022 TO BS 1031, FROM BL 8R TO BL 29R AT WL 208. CORROSION WAS FOUND OUT OF LIMITS IAW BOEING 737-300 SRM 51-60-51-1A1. MAINTENANCE REMOVED CORRODED SHEAR WEB, FABRICATED REPLACEMENT WEB AND INSTALLED MAIN DECK SHEAR WEB FROM BS 1022 TO BS 1031, BL 8R TO BL 29R AND WL 208 IAW BOEING 737-300 SRM 51-40-02-0G FIGS 3, 4, 8, 9 AND BAC DWG 65C32707. 2L72 4F RTA16WE 20060119000202006011900020NM 2006 1 19 AWXA200600060 120051217A532065C334195 SHEAR WEB BOEING737 7373G7 1384595NM BS 1016-1031 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 MCN - DURING C15 CHECK DISCOVERED LEVEL 2 GALVANIC CORROSION ON THE TOP AND BOTTOM SURFACE OF THE LT AFT MAIN DECK SHEAR WEB FROM BS 1016 TO BS 1031, FROM BL 9L TO BL 21L AT WL 208. CORROSION WAS FOUND OUT OF LIMITS IAW BOEING 737-300 SRM 51-60-51-1A1. MAINTENANCE REMOVED CORRODED SHEAR WEB, FABRICATED REPLACEMENT WEB AND INSTALLED MAIN DECK SHEAR WEB FROM BS 1016 TO BS 1031, BL 9L TO BL 21L AND WL 208 IAW BOEING 737-300 SRM 51-40-02-0G FIGS 3, 4, 8, 9 AND BAC DWG 65C33419. 2L72 4F RTA16WE 20060119000252006011900025NM 2006 1 19 AWXA200600065 120051217A531565C3267710 FLOORBEAM BOEING737 7373G7 1384595NM BS 992 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 MCN - DURING C15 CHECK DISCOVERED LEVEL 2 GALVANIC CORROSION ON THE FLOOR SUPPORT AT BS 992, BL 30R AND WL 208. CORROSION WAS FOUND TO BE OUT OF LIMITS. REMOVED FLOOR SUPPORT, FABRICATED REPLACEMENT FLOOR SUPPORT AND INSTALLED AT BS 992, BL 30R AND WL 208 IAW BOEING 737-300 SRM 51-40-02-0G FIG 12 AND BAC DWG 65C32677. 2L72 4F RTA16WE 20060119000272006011900027NM 2006 1 19 AWXA200600067 120051219A532065C320747 INTERCOSTAL BOEING737 7373G7 1384595NM BS 993 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 MCN - DURING C15 CHECK DISCOVERED LEVEL 2 GALVANIC CORROSION ON INTERCOSTAL AT BS 993, BL 21L AND WL 208. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-51-1A1 FIG 101. MAINTENANCE REMOVED AND INSTALLED NEW INTERCOSTAL AT BS 993, BL 21L AND WL 208 IAW BOEING 737-300 SRM 51-40-02-0G FIG 12. 2L72 4F RTA16WE 20060119000302006011900030NM 2006 1 19 AWXA200600070 120051217A575465C26603101 WEDGE BOEING737 7373G7 1384595NM NR 3 SLAT DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 MCN - DURING C15 CHECK DISCOVERED THE UPPER SURFACE OF THE NR 3 SLAT WEDGE DISBONDED FROM SS 12.25L TO SS 16.25. MAINTENANCE REMOVED THE DISBONDED SKIN IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED REPAIR FILLER AND DOUBLER IAW BOEING 737-300 SRM 51-70-10-2R4. BONDED REPAIR PARTS TO THE UPPER SURFACE OF THE NR 3 SLAT WEDGE FROM SS 12.25L TO SS 16.25 IAW BOEING 737-300 SRM 51-70-10-2R4. 2L72 4F RTA16WE 20060119000322006011900032NM 2006 1 19 AWXA200600073 120051217A575465C26603101SP SKIN BOEING737 7373G7 1384595NM NR 3 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 MCN - DURING C15 CHECK DISCOVERED 5 CRACKS, .500 INCHES EACH, ON THE BOTTOM OF THE NR 3 SLAT SKIN FROM SS 102.75L TO SS 107.75L. MAINTENANCE CUT OUT THE DAMAGED SKIN IAW BOEING 737-300 SRM 57-43-01-2R6. FABRICATED FILLER AND SPLICE PLATE IAW BOEING 737-300 SRM 57-43-01-2R6. INSTALLED FABRICATED REPAIR PARTS ON THE BOTTOM OF THE NR 3 SLAT FROM SS 102.75L TO SS 107.75LIAW BOEING 737-300 SRM 57-43-01-2R6. 2L72 4F RTA16WE 20060119000352006011900035NM 2006 1 19 AWXA200600076 120051205A552265C25753 SKIN BOEING737 7373G7 1384595NM LT ELEVATOR DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW55007 24012 PHX - MAINTENANCE DISCOVERED THE LT ELEVATOR UPPER SURFACE HAD SEVERAL PLACES OF COMPOSITE STRANDS DELAMINATE AND TWO SMALL HOLES. MAINTENANCE REMOVED DAMAGE IAW AWA ER 03-5521-05339-RA1. APPLIED REPAIR PLIES TO THE LT ELEVATOR IAW AWA ER 03-5521-05339-RA1. NO WEIGHT CHANGES WERE NOTED. 2L72 4F RTA16WE 20060119000362006011900036NM 2006 1 19 AWXA200600077 120051206A532065528942 CHANNEL BOEING737 7373Y0 1384671NM BS 540 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - DURING C16 CHECK DISCOVERED CHANNEL CRACKED, .7 INCHES, AT BS 540, WL 206 AND BL 1R. MAINTENANCE REMOVED AND INSTALLED NEW CHANNEL ASSY AT BS 540, WL 206 AND BL 1R IAW BOEING 737-300 SRM 51-40-02-0G FIG 12. 2L72 4F RTA16WE 20060119000392006011900039NM 2006 1 19 AWXA200600080 120051209A532065516989 CHANNEL BOEING737 7373Y0 1384671NM BS 907 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - DURING C16 CHECK DISCOVERED CHANNEL CRACKED, 1.1 INCHES, AT BS 907 AND STR 4R. MAINTENANCE REMOVED AND INSTALLED NEW CHANNEL AT BS 907 AND STR 4R IAW BOEING 737-300 SRM 51-40-02-0G FIG 8 AND 12. 2L72 4F RTA16WE 20060119000402006011900040NM 2006 1 19 AWXA200600081 120051214A5313654577817 STRINGER BOEING737 7373Y0 1384671NM BS 907-947 DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - DURING C16 CHECK DISCOVERED STRINGER 9R, BS 907 TO BS 947, HAS 1/4" HOLE IN IT. MAINTENANCE REMOVED AND INSTALLED NEW STRINGER AT STRINGER 9R, BS 907 TO BS 947, IAW BOEING 737-300 SRM 51-40-02-0G FIG 12. 2L72 4F RTA16WE 20060119000422006011900042NM 2006 1 19 AWXA200600083 120051216A534069353521 STRINGER CLIP BOEING737 7373Y0 1384671NM BS 1006 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - DURING C16 CHECK DISCOVERED STRINGER CLIP CRACKED, .25 INCHES, AT STR 8L AND BS 1006. MAINTENANCE REMOVED AND INSTALLED NEW STRINGER CLIP AT STR 8L AND BS 1006 IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 8 AND 12. 2L72 4F RTA16WE 20060119000442006011900044NM 2006 1 19 AWXA200600085 120051230A534065353642 STRINGER CLIP BOEING737 7373Y0 1384671NM BS 1006 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - DURING C16 CHECK DISCOVERED STRINGER TIE CRACKED, .50 INCHES, AT STR 10L. AND BS 1006. MAINTENANCE REMOVED AND INSTALLED NEW STRINGER TIE AT STR 10L AND BS 1006 IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 8 AND 12. 2L72 4F RTA16WE 20060119000482006011900048NM 2006 1 19 AWXA200600071 120051217A575465C26602224 WEDGE BOEING737 7373G7 1384595NM NR 5 SLAT DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 MCN - DURING C15 CHECK DISCOVERED THE UPPER AND LOWER SURFACE OF THE NR 5 SLAT WEDGE DISBONDED FROM SS 124.0R TO SS 129.0R. MAINTENANCE REMOVED THE DISBONDED SKIN IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED REPAIR CORE AND DOUBLER IAW BOEING 737-300 SRM 51-70-10-2R4. BONDED REPAIR PARTS TO THE NR 5 SLAT WEDGE FROM SS 124.0R TO SS 129.0R IAW BOEING 737-300 SRM 51-70-10-2R4. 2L72 4F RTA16WE 20060119000492006011900049NM 2006 1 19 AWXA200600088 120051204A5320654583459 INTERCOSTAL BOEING737 7373Y0 1384671NM BS 347 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - DURING C16 CHECK DISCOVERED INTERCOSTAL CRACKED, 1.5 INCHES, AT BS 347 ABOVE THE E-2 SHELF, BL 11.1 AND WL 207. MAINTENANCE REMOVED AND INSTALLED FABRICATED INTERCOSTAL FROM BS 344 TO BS 360, BL 11.10L AND WL 207 IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NO 03-5310-05355-ES1. 2L72 4F RTA16WE 20060119000512006011900051NM 2006 1 19 AWXA200600090 120051205A57536546435277SP SKIN BOEING737 7373Y0 1384671NM TE FLAP DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - DURING C16 CHECK DISCOVERED LT OUTBOARD AFT FLAP DELAMINATED AT THE INBOARD TRAILING EDGE FROM WS 230.68L TO WS 234.68L. MAINTENANCE REMOVED DISBONDED SKIN AND CORE IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED REPLACEMENT CORE AND DOUBLER IAW BOEING 737-300 SRM 51-70-10-2R4. BONDED REPAIR PARTS TO THE LT OUTBOARD AFT FLAP INBOARD TRAILING EDGE, WS 230.68L TO WS 234.68L, IAW BOEING 737-300 SRM 51-70-10-2R4. 2L72 4F RTA16WE 20060119000542006011900054NM 2006 1 19 AWXA200600093 120051206A5755654645165A SKIN BOEING737 7373Y0 1384671NM ZONE 600 DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - DURING C16 CHECK DISCOVERED TWO SPOTS OF DISBOND ON THE NR 6 SPOILER, LOWER SURFACE, FROM WBL 228.53R TO WBL 330.53R. MAINTENANCE REMOVED DISBONDED SKIN AND CORE IAW BOEING 737-300 SRM 51-70-10-2R4 FIG 203. FABRICATED REPLACEMENT CORE AND DOUBLER IAW BOEING 737-300 SRM 51-70-10-2R4 FIG 203. BONDED REPAIR PARTS TO THE NR 6 SPOILER LOWER SURFACE, WBL 228.53R TO WBL 330.53R, IAW BOEING 737-300 SRM 51-70-10-2R4 FIG 203. 2L72 4F RTA16WE 20060119000562006011900056NM 2006 1 19 AWXA200600095 120051209A53306545871523 SKIN BOEING737 7373Y0 1384671NM BS 294 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - DURING C16 CHECK DISCOVERED, THE R1 DOOR LOWER HINGE CUTOUT, LOWER RADIUS, CRACKED, .25 INCHES AT BS 294 AND STRINGER 13R. MAINTENANCE CUTOUT DAMAGED AREA AT THE R1 DOOR HINGE CUTOUT RADIUS IAW AMERICA WEST AIRLINES ENGINEERING NR 03-5240-05349-RC1. FABRICATED DOUBLER IAW AWA ER NR 03-5240-05349-RC1. INSTALLED FABRICATED REPAIR PARTS AT THE R1 DOOR LOWER HINGE CUTOUT, LOWER RADIUS AT BS 294 AND STRINGER 13R IAW AWA ER 03-5240-05349-RC1. 2L72 4F RTA16WE 20060119000572006011900057NM 2006 1 19 AWXA200600096 120051207A575465C26603100SP SKIN BOEING737 7373Y0 1384671NM NR 4 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - DURING C16 CHECK DISCOVERED 4 CRACKS, .500 INCHES EACH, ON THE BOTTOM OF THE NR 4 SLAT SKIN, FROM SS 57R TO SS 61R. MAINTENANCE CUT OUT DAMAGED SKIN IAW BOEING 737-300 SRM 57-43-01-2R6 FIG 201. FABRICATED FILLER AND SPLICE PLATE IAW BOEING 737-300 SRM 57-43-01-2R6 FIG 201. INSTALLED FABRICATED REPAIR PARTS ON THE NR 4 SLAT SKIN FROM SS 57R TO SS 61R IAW BOEING 737-300 SRM 57-43-01-2R6 FIG 201. 2L72 4F RTA16WE 20060119000602006011900060NM 2006 1 19 AWXA200600099 120051205A575465C2679311 SKIN BOEING737 7373Y0 1384671NM NR 3 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - DURING C16 CHECK DISCOVERED 1 CRACK, .375 INCHES, ON THE BOTTOM OF THE NR 3 SLAT SKIN, AT SS 92L. MAINTENANCE CUT OUT DAMAGED SKIN IAW BOEING 737-300 SRM 57-43-01-2R6 FIG 201. FABRICATED FILLER AND SPLICE PLATE IAW BOEING 737-300 SRM 57-43-01-2R6 FIG 201. INSTALLED FABRICATED REPAIR PARTS ON THE NR 3 SLAT SKIN AT SS 92L IAW BOEING 737-300 SRM 57-43-01-2R6 FIG 201. 2L72 4F RTA16WE 20060119000642006011900064NM 2006 1 19 AWXA200600103 120051220A5340654583347 CLIP BOEING737 7373G7 1384595NM BS 178 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 MCN - DURING C15 CHECK DISCOVERED FLOOR WEB CLIP CRACKED, 1.10 INCHES, AT BS 178, WL 207 AND BL 30L. MAINTENANCE REMOVED CRACKED CLIP AND FABRICATED NEW CLIP IAW BOEING DWG 65-45833. INSTALLED FABRICATED REPAIR PARTS AT BS 178, WL 207 AND BL 30L IAW BOEING 737-300 SRM 51-40-02-0G FIGURE 12. 2L72 4F RTA16WE 20060119000652006011900065NM 2006 1 19 AWXA200600104 120051220A5320654583312 WEB BOEING737 7373G7 1384595NM BS 194 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 MCN - DURING C15 CHECK DISCOVERED FLOOR WEB CRACKED, 1.2 INCHES, AT BS 194, WL 207 AND BL 30R. MAINTENANCE REMOVED CRACKED WEB AND FABRICATED NEW WEB IAW BOEING 737-300 SRM 53-10-51-2R8. INSTALLED FABRICATED REPAIR PARTS AT BS 194, WL 207 AND BL 30R IAW BOEING 737-300 SRM 53-10-51-2R8. 2L72 4F RTA16WE 20050509000062005050900006EU 2005 5 9 05FDEA01035 120050416A2170 COALESCER BAG AIRBUS310 A310203 3930313EU CABIN CONTAMINATED A FDEAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SO25409FE 273 AT 300 FT AGL BOTH CAPT AND F/O SMELLED SMOKE OR BURNING. MIN EQUIP BAY SMOKE ON ECAM ILLUMINATED FOR ONLY 10 SECONDS OR LESS THEN DISAPPEARED. THE SMOKE AND SMELL WENT AWAY. RETURNED TO MEM AND ON LANDING THE SMELL RETURNED, BUT NO SMOKE. CLEARED RUNWAY HAD FIRE TRUCKS INSPECT THEN TAXIED IN. NO REOCCURRANCE OF SMOKE. REMOVED MIN EQUIP BAY PANELS AND DID NOT SMELL ANY SMOKE. REPLACED MIN EQUIPMENT BAY DUCT SMOKE DETECTOR REPLACED DUCT CARTRIDGE FILTER. REMOVED AND REPLACED AIR FLOW DETECTOR. REMOVED AND REPLACED BOTH NR 1 AND NR 2 APU COALESCER FILTERS. RAN ENGS AT HIGH POWER WITH NO FAULTS NOTED. 2L72 4F RTA35EU 20050509000192005050900019NM 2005 5 9 CALA0500105 120050417A3350D71701100 BATTERY PACK BOEING737 737824 13844BZNM EMERGENCY LIGHT INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2727239 28951 FWD EMERGENCY LIGHTS TO COCKPIT INOPERATIVE. REPLACED FWD EMERGENCY LIGHT BATTERY PACK. 2L72 4F RTA16WE 20050509000282005050900028WP 2005 5 9 UPS05844284 120050404A5340 ATTACH FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 INSPECTION TYPE: C1, FRAME TO INTERCOSTAL FITTING CRACKED 3 INCH LONG, AT STA 900 L18L. REMOVED, FABBED AND INSTALLED REPLACEMENT FITTING IAW SRM 53-2-0, 51-1- 8, 51-1-20D, AND DWG 4779496. 2L74 4F RT4A25 20050509000302005050900030WP 2005 5 9 UPS05844288 120050318A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE: C2, LT LWR WING L/E HAS HEAVY CORROSION AT STA XFS 566. REMOVED CORROSION AND FOUND OUT OF LIMITS PER SRM 57-2-0 FIG 7. CUT OUT DAMAGED AREA AND REPAIRED IAW DC-8 SRM 57-2-1, 57-3-0, & 57-2-1. 2L74 4F RT4A25 20050509000332005050900033EA 2005 5 9 COMA0560260 120050416A7830 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ACTIVATED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01963CA 7127 FLIGHT 5134 DURING TAKEOFF DID NOT RECEIVE A T/O CONFIGURATION OK MESSAGE, ABORTED TAKEOFF AND RETURNED TO THE GATE. CYCLED THE RIGHT THRUST REVERSER. 2L72 4F RTA21EA 20050509000402005050900040 2005 5 9 MWEA050033 420050414A2565100503117 SLIDE DOUG DC9 DC981 3022081WP TAILCONE FAILED A MWEAK NONE L NO TEST ININSP/MAINT 1 GL31805ME 48031 TAIL CONE SLIDE DID NOT AUTOMATICALLY DEPLOY WHEN THE TAIL CONE TEST WAS PERFORMED. REPLACED SLIDE COVER ASSEMBLY AND SLIDE. 2L72 4F A6WE 20050509000412005050900041EA 2005 5 9 COMA0560265 120050417A323046193 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA MLG FAULTY A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01979CA20236 7159 FLIGHT 5035 RECEIVED A GEAR DISAGREE CAUTION DURING CLIMBOUT OF CVG, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD LANDING WITHOUT INCIDENT. REPLACED THE MLG PRIORITY VALVE. 2L72 4F RTA21EA 20050509000452005050900045NM 2005 5 9 ASMF200504010 120050411A32227341MT987N SEAL DOUG MD88 MD88 3023688NM NLG STRUT DAMAGED W ASMFD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SW23158PL 49761 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING TAXING NOSE LANDING GEAR STRUT HAS A HYDRAULIC LEAK. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE THE NLG STRUT SEALS WERE REPLACED IAW M/M 32-21-02, TESTED CORRECT. 2L72 4F RTA6WE 20050509000462005050900046NM 2005 5 9 ASMF200504011 120050411A213045D161 PRESSURE SWITCH DOUG MD88 MD88 3023688NM LT A/C PACK FAILED W ASMFA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW23168PL42229 53174 AIRCRAFT RETURNED OF FLIGHT AS A CONSEQUENCE OF AIR CONDITIONING SYSTEM DID NOT PRESSURIZED. IN GROUND, CAPTAIN REPORTED NO AIR FLOW WITH BOTH AIR CONDITIONING PACKAGES OPERATING. DURING REVISION THE FLOW CONTROL VALVE BREAKERS, PRESSURE REGULATOR VALVE AND THE AIR CONDITION SWITCH WERE OPERATING NORMALLY BUT THE AIR CONDITIONING SYSTEM DID NOT PRESSURIZE. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE, THE S1-296 AND S1-297 SWITCHES WERE REPLACED IAW MM 21-31-09, TESTED CORRECT. THE FLIGHT DATA RECORDER WAS REPLACED IAW 31-31-01. 2L72 4F RTA6WE 20050509000482005050900048WP 2005 5 9 ASMF200504013 120050416A2910 PTU DOUG DC9 DC987 3022087WP HYD SYSTEM FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23754RA 49641 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING TAXING, RIGHT HYDRAULIC SYSTEM WAS FAILED. DURING REVISION, RIGHT HYDRAULIC PUMP CONTINUED INDICATING PRESSURE WHEN IT WAS SHUTOFF AND HYDRAULIC POWER TRANSFER UNIT (PTU) WAS DETECTED WITH FAIL. THE PTU WAS REPLACED IAW MM 29-10-08, TESTED CORRECT. 2L72 4F RTA6WE 20050509000562005050900056EA 2005 5 9 QXEA200500574 120050324A5344 HINGE CNDAIRCL600 CL6002C10 1390015EA ZONE 100 BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FORWARD FUSELAGE RIGHT POTABLE WATER SERVICE DOOR HAS UPPER HINGE ASSEMBLY BENT AND BROKEN. REPLACED IAW CRJ700 SRM 51-41-00-001-001-A01. 2L72 4F RTA21EA 20050509000582005050900058EA 2005 5 9 QXEA200500581 120050322A5414 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - LEFT ENGINE TRAILING EDGE TRANSCOWL FORWARD EDGE WORN ON BOTTOM CRACKED ON TOP AT 2 O'CLOCK AND 4 O'CLOCK POSITIONS. REPAIRED IAW REO 670-78-33-347 AND HORIZON AIR EA R-78-26. 2L72 4F RTA21EA 20050509000712005050900071NM 2005 5 9 AWXA200500452 120050414A5270848401 PROXIMITY SENSOR AIRBUSA319 A319132 3930340NM CARGO DOOR MISALIGNED A AWXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP28834AW 2302 LAX - AIR TURNBACK - FLT 0302 - DURING CLIMBOUT OF LAX EN ROUTE FOR JFK ECAM INDICATED THE AFT CARGO DOOR WAS NOT SECURE, TURNED BACK TO LAX, ON TAXI BACK TO GATE THE DOOR OPEN INDICATION DISAPPEARED. ISSUED MEL 52-70-01, COND 8 FOR AFT CARGO DOOR INDICATION INOP. VERIFIED SECURITY OF DOOR AND AIRCRAFT DEPARTED FOR SCHEDULED DESTINATION. *S/D* MAINTENANCE TROUBLESHOT AFT CARGO DOOR AND FOUND THE TARGET GAP ON PROXIMITY SENSOR 32WV OUT OF ADJUSTMENT. ADJUSTED SENSOR IAW AMM TASK 52-71-12-820-051, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050509000742005050900074EA 2005 5 9 QXEA200500592 120050317A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE INTERIOR, RIGHT OUTBOARD SEAT RAIL AT STATION X646 HAS PITTING CORROSION ON MOST INBOARD SURFACE. REPAIRED IAW CRJ700/900 SRM 51-21-06-001-001-A01, PARAGRAPH 3E. 2L72 4F RTA21EA 20050509000772005050900077EA 2005 5 9 QXEA200500584 120050317A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC FUSELAGE INTERIOR, LEFT OUTBOARD SEAT RAIL AT STATION X740 HAS PITTING CORROSION ON ON MOST INBOARD SURFACE. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01 AND REO 670-53-00-013. 2L72 4F RTA21EA 20050509000812005050900081EA 2005 5 9 QXEA200500589 120050317A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE INTERIOR, RIGHT OUTBOARD SEAT RAIL AT STATION X553 HAS PITTING CORROSION ON MOST INBOARD SURFACE. REPAIRED IAW CRJ700/900 SRM 51-21-06-001-001-A01. 2L72 4F RTA21EA 20050509000922005050900092NM 2005 5 9 UIEA200500048 120050405A541465B941004 SKIN BOEING747 747271C 1384869NM GE CF6 CF650E2 30018NE NR 1 NACELLE CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15537MC 22403 D-CHECK, DURING SCHEDULE INSPECTION, CRACK DAMAGE WAS FOUND IN THE SKIN ASSY AND THE ADJACENT NR 3 STIFFENER AT PRE-COOLER EXHAUST CUTOUT LOWER EDGE NEAR THE AFT CORNER AT STA 248 ON THE RT SIDE. THE NR 3 STIFFENER LOWER FLANGE WAS TRIMMED TO REMOVE CRACKS. THE CRACK IN SKIN ASSY WAS CONTAINED WITH 1.0 INCH HOLE AT THE CRACK TIP. THE NR 3 STIFFENER WAS REINFORCED WITH A NEW STEEL LOWER REPAIR ANGLE FROM NAC STA 235 TO 254. THE RIB INSTALLATIONS AT NAC STA 248 WAS MODIFIED TO ACCOMMODATE THE NEW STEEL LOWER REPAIR ANGLE. NDT INSPECTED EACH REPAIR AREA, INCLUDING HFEC INSPECTION OF ALL REPAIR FASTENER LOCATIONS AND TRIMMED EDGES TO ENSURE ABSENCE OF CRACKS, CORROSION AND ANY OTHER DAMAGE. (K) 2L74 4F4 F A20WE E23EA 20050509001012005050900101EU 2005 5 9 USAA050251 120050207A5347F53477214203 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19671UW22760 0323 BFM - FOUND SEAT TRACK CORRODED 3 INCHES LONG BY 1.25 INCHES WIDE BY .032 INCH DEEP/3.5 INCH LONG 1.25 INCHES WIDE .038 INCH, CABIN, FRAME 71, FRAME 72, -Y450. REPLACED SEAT TRACK ASSY PER SRM 53-0015 FIG 101, 53-41-15, 51-21-11. (M) 2L72 4F RTA46NM 20050509001062005050900106EU 2005 5 9 USAA050248 120050202A5347F5311181720000 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19671UW22760 0323 BFM - FOUND RAIL CORRODED 1 INCH BY .25 INCH BY .046 INCH DEEP, FRAME 17, -450, MAIN CABIN FLOOR. REMOVED AND REPLACED RAIL PER SRM 53-11-15 FIG 101. CORROSION LEVEL 2, TASK C531172-01. (M) 2L72 4F RTA46NM 20050509001182005050900118EU 2005 5 9 USAA050249 120050202A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19671UW22760 0323 BFM - FOUND SEAT TRACK CORRODED 4 INCHES BY 1.2 INCHES BY .042 INCH DEEP, FRAME 54, Y450 MAIN CABIN FLOOR. REMOVED DAMAGED SECTION, INSTALLED NEW SECTION OF TRACK AND SPLICES PER SRM 53-31-15 FIG 101. (M) 2L72 4F RTA46NM 20050509001292005050900129EU 2005 5 9 USAA050253 120050205A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19671UW 0323 BFM - FOUND SEAT TRACK CORRODED 7 INCHES BY 1 INCH BY .019 INCH DEEP AND 13 INCHES BY 1 INCH BY .040 INCH DEEP, FRAME 53.7 AND 53.8, -Y450, MAIN CABIN FLOOR. REMOVED CORROSION, FABRICATED SPLICES AND NEW SECTION, INSTALLED REPAIR PARTS PER SRM 53-31-15. (M) 2L72 4F RTA46NM 20050509001372005050900137NM 2005 5 9 SWAA051108 120050414A335065C34691 LIGHT BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29332SW 23696 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY BULLNOSE LIGHT INOP AT ROW 20. RELAMPED PER MM. 2L72 4F RTA16WE 20050509001412005050900141NM 2005 5 9 SWAA051111 120050414A53136551698 SPLICE BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON STRINGER SPLICE AT BS 362, STR 27L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20050509001442005050900144NM 2005 5 9 SWAA051114 120050414A57536546430112 SKIN BOEING737 7373Y0 1384671NM RT WING FOREFLAPDELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED C4 CHECK, FOUND RT WING T/E INBOARD FOREFLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM. 2L72 4F RTA16WE 20050509001592005050900159NM 2005 5 9 SWAA051134 120050417A52106545768 SKIN BOEING737 7373H4 1384600NM L1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29333SW 23697 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050509001602005050900160NM 2005 5 9 SWAA051135 120050417A57206545410 FLOOR SUPPORT BOEING737 7373H4 1384600NM CABIN FLOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29333SW 23697 DURING SCHEDULED 1/4D CHECK, FOUND 3 EA CRACKS AT NR 3 LONGITUDINAL FLOOR SUPPORT TEE, BS 662.5, BS 665.5 & BS 669. REPAIRED FLOOR FLOOR SUPPORT PER SWA EA. 2L72 4F RTA16WE 20050509001642005050900164NM 2005 5 9 SWAA051139 120050416A3350101114 BULB BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29454WN 29851 DURING SCHEDULED MV3 CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. RELAMPED PER MM. 2L72 4F RTA16WE 20050509001662005050900166 2005 5 9 SWAA051141 420050415A25651061323475 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF LIMITS A SWAAK NONE O OTHER ININSP/MAINT 1 SW29624SW 27934 L1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATING OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20050510000062005051000006NM 2005 5 10 AWXA200500469 120050331A52105079454 SKIN BOEING737 737301 1384611NM L1 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 DURING C-19 CHECK A .25 INCH CRACK WAS FOUND ON L-1 DOOR INNER SKIN ABOVE UPPER TORQUE TUBE SLEEVE ON FORWARD RT SIDE BS 312, STR 12 LT. MAINTENANCE CUT OUT DAMAGED L-1 DOOR INNER SKIN AT BS 312, STR 12 LT; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 51-70-13. 2L72 4F RTA16WE 20050510000192005051000019NM 2005 5 10 CALA0500108 120050418A5511655058217 SPAR BOEING737 7373T0 1384582NM HORIZONTAL STAB WORN A CALAK NONE O OTHER ININSP/MAINT 1 SW2712319 23370 HORIZONTAL STABILIZER CENTER SECTION REAR SPAR RIGHT LOWER AFT CLEVIS WORN INTO BY ACCESS PANEL 9224R. BLENDED THE GOUGE PER ECRA 5550-01035. 2L72 4F RTA16WE 20050510000272005051000027EA 2005 5 10 VTZA200500060 120050416A5210 DOUBLER CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27658BR 7500 PASSENGER DOOR DOUBLER IS CRACKED AT 1 INCH IN LENGTH FORWARD OF DATUM 1 AT FS 338.90. 2L72 4F RTA21EA 20050510000302005051000030EA 2005 5 10 VTZA200500063 120050418A5320601R3501163 PLATE CNDAIRCL600 CL6002B19 1900309EA FUSLEAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27658BR 7500 CARGO LANDING PLATE IS CRACKED AT RIVETS ATTACHING IT TO THE INTERCOSTALS .250 INCH. 2L72 4F RTA21EA 20050510000342005051000034EA 2005 5 10 VTZA200500057 120050416A531260034017595 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27640BR 7340 RIGHT SIDE CO-PILOTS BULKHEAD AT FS 280 RBL 9.0 IS CRACKED AT 1.0 INCH IN WEB RADIUS. 2L72 4F RTA21EA 20050510000352005051000035NE 2005 5 10 AT0500014 220050414A7320114E61126120 EEC BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE NR 2 ENGINE INOPERATIVE A ZZDAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO15967AT 55028 ENGINE RIGHT SYSTEM FAIL AND REVERSER RIGHT FAIL IN CLIMB. HAD NO THROTTLE RESPONSE TRIED ALTN FADEC, NO RESPONSE SHUTDOWN ENGINE NECESSARY TO DESCEND AND LAND. REMOVED AND REPLACED NR 2 ENG EEC PER AMM 73-21-01. C/W RTS, RTS GOOD. C/W SPECIAL INSP OF LPC OGV LEADING EDGE, TRAILING EDGE, AND CONCAVED SURFACES PER AMM 72-00-00. CHIP DETECTOR INSPECTION C/W. PERFORMED ENGINE POWER ASSURANCE CK IAW 71-00-13, OPS CHECK OK. 2L72 4F4 FTRA6WE E00061EN 20050510000542005051000054NM 2005 5 10 2005UALA00339 120050414A5313 STRINGER BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29585UA 26709 STRINGER 16L AT BS 758 IS CRACKED. 2L72 4F4 FRTA2NM E17NE 20050510000852005051000085EA 2005 5 10 A6WA200540141 120050406A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31417AW 7600 FOUND CRACK ON CLIP AT FS 280 RIGHT SIDE APPROX .5 INCH IN LENGTH AT TOP CORNER IN. REMOVED AND REPLACED RT FS 280 CLIP IAW CRJ SPM 51-42-06 FOR SOLID RIVETS AND 51-45-21 FOR HILITES. (M) 2L72 4F RTA21EA 20050510000892005051000089EA 2005 5 10 QXEA200500631 120050319A5210 ATTACH BRACKET CNDAIRCL600 CL6002C10 1390015EA ZONE 800 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - PASSENGER DOOR AFT SIDE INTERNAL Z FOR ASSIST MOTOR ATTACH IS CRACKED. REPLACED IAW CRJ700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20050510000922005051000092EA 2005 5 10 QXEA200500637 120050325A5740 ATTACH FITTING CNDAIRCL600 CL6002C10 1390015EA ZONE 600 SCORED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - RIGHTHAND AILERON INBOARD PCU LINK OUTBOARD LUG BORE FOR BUSHINGS SCORED. REPAIRED IAW REO 670-57-01-022 AND HORIZON AIR EA R-57-112. 2L72 4F RTA21EA 20050510000942005051000094EA 2005 5 10 QXEA200500623 120050322A1430 SCREW CNDAIRCL600 CL6002C10 1390015EA ZONE 600 LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - RIGHTHAND WINGLET INBOARD AND OUTBOARD SURFACES HAVE MANY LOOSE SCREWS. RETORQUED IAW CRJ700 MM 57-30-84, PAGE 422/425. 2L72 4F RTA21EA 20050510000962005051000096EA 2005 5 10 QXEA200500616 120050323A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 200 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE EXTERIOR SKIN AT PASSENGER DOOR SURROUND HAS SCRATCHES AT STATION 310 AND 349, STRINGER 15L. REPAIRED IAW CRJ700 SRM 51-25-01, PAGE 7, PARAGRAPH B AND SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050510000992005051000099EA 2005 5 10 QXEA200500618 120050319A5230 HOUSING CNDAIRCL600 CL6002C10 1390015EA ZONE 800 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE, AFT BAGGAGE DOOR HANDLE HOUSING HAS GOUGE ON FORWARD TOP OUTER FACE. REPAIRED IAW CRJ700 SRM 51-12-00-991-802 AND SRM 51-21-01-001-001-A01. 2L72 4F RTA21EA 20050510001002005051000100EA 2005 5 10 QXEA200500626 120050322A5320 PLATE CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FORWARD FUSELAGE, GALLEY SERVICE DOOR FRAME SEAL SKIN SPLICE PLATE CHAFED. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01, SRM 51-12-01-001-001-A01, SRM 51-25-01-001-001-A01 AND SRM 53-21-23-101-001-A01. 2L72 4F RTA21EA 20050510001352005051000135SO 2005 5 10 C2XA05BT022 120050417A3350110049 CHARGER EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT INOPERATIVE A C2XAO OTHER O OTHER NRNOT REPORTED 1 SW2717159 145792 EWR SQUAWK BATT NR 4 EMERGENCY LIGHTS OUT. REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY CHARGER IAW EMB-145XR AMM 33-50-04. OPS CHECK GOOD. 2L72 4F RT 20050510001372005051000137SO 2005 5 10 C2XA05TY033 120050418A3350267005 FUSE EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BLOWN A C2XAK NONE O OTHER ININSP/MAINT 1 SW2726545 145558 TYS- DURING SCHEDULED MAINTENANCE, THE LEFT FWD EXTERNAL EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY RECEPTACLE FUSES. OPS CHECKS GOOD. A/C RELEASED TO SERVICE. 2L72 4T RTT00011AT 20050510001402005051000140SW 2005 5 10 RT62005F00000 120050412A53102060313022695 SUPPORT FITTING BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL FUSELAGE CRACKED E RT6AK NONE O OTHER ININSP/MAINT 1 NM03568TD 2976 REAR CROSSTUBE BOX-BEAM ASSEMBLY: LEFT FORWARD SUPPORT FITTING- 1 INCH VERTICAL CRACK, RT FORWARD SUPPORT FITTING - 1 INCH CRACK IN RADIUS. CRACKS FOUND DURING SCHEDULED INSPECTION. (K) (1 OF 4) 1G71 3U3 U H2SW E4CE 20050510001422005051000142SW 2005 5 10 RT62005F00002 120050412A5343206031301130S SUPPORT FITTING BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL MLG CRACKED E RT6AK NONE O OTHER ININSP/MAINT 1 NM03568TD 2976 REAR CROSSTUBE BOX-BEAM ASSEMBLY: LT FORWARD SUPPORT FITTING - 1 INCH VERTICAL CRACK. RT FORWARD SUPPORT FITTING - 1 INCH CRACK IN RADIUS. CRACKS FOUND DURING SCHEDULED INSPECTION. (NR3 OF 4) (K) 1G71 3U3 U H2SW E4CE 20050510001442005051000144EU 2005 5 10 MALA050326 120050412A4950 BLEED VALVE BAC 146 AVRO146RJ85A1500097EU APU FAILED A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL15521XJ E2346 AFTER DEPARTING CVG CREW SELECTED ENGINE AIRS ON. STRONG OIL SMELL WAS NOTED IN THE CABIN AND THE FLIGHT DECK. CREW ISOLATED TO THE NR 4 ENGINE. FLIGHT CONTINUED ON WITHOUT FURTHER INCIDENT. APU BLEED VALVE. 2H74 4F RTA49EU 20050510001562005051000156EU 2005 5 10 MALA050293 120050322A5320 FLOOR SUPPORT SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15415XJ 340B415 DURING 4K CHECK IN BNA FOUND FLOOR FLANGE AT FS 272 BETWEEN RBL 12 AND RBL 36 IS CORRODED AND HAS BEEN REPAIRED IAW MESABA EOS53102. 2L72 4T RTA52EU 20050510001592005051000159EU 2005 5 10 MALA050307 120050328A7933 INDICATOR SAAB SF340 340B 7860101EU RT ENG OIL TEMP READS HIGH A MALAO OTHER N FALSE WARNING NRNOT REPORTED 1 GL15369PX 340B295 AIR TURNBACK, RT ENGINE OIL TEMP GAUGE READING HIGH IN RED ARCH. VERIFIED GAUGE AT FAULT ON GROUND. REPLACED GAUGE AND RT OIL TEMP DETECTOR. 2L72 4T RTA52EU 20050510001682005051000168NE 2005 5 10 MALA050311 220050402A7200 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LEFT MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15416XJ 340B416 LT ENGINE OIL PRESSURE LIGHT ILLUMINATED AND GAUGE WAS READING LOW (ABOUT 25-30 PSI) ON TAKEOFF. CREW FOLLOWED QRH BUT DID NOT SHUT DOWN ENGINE. AIR RETURNED. REMOVED AND REPLACED LT ENGINE. 2L72 4T4 TRTA52EU E8NE 20050510001742005051000174NE 2005 5 10 AALA20050272 220050415A7230 BLADES DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE COMPRESSOR DAMAGED A AALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SW21462AA 49592 725411 COMPRESSOR STALL ON TAKEOFF AT 50 FEET TO FLEX 50 DEGREES. RIGHT ENGINE EXHAUST GAS TEMPERATURE IN AMBER AREA 590 DEGREES. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND STAGE 7 BLADES DAMAGED. REPLACED RIGHT HAND ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 F A6WE E9NE 20050510001762005051000176NM 2005 5 10 AALA20050275 120050418A3350 LIGHT BOEING757 757223 1384957NM SEAT 2E INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21660AM 25294 DFW- AFT EMERGENCY PATH LIGHT AT SEAT 2E INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY PATH LIGHT AT SEAT 2E. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050510001782005051000178NM 2005 5 10 AALA20050273 120050415A2910BACH8A04EE0557B LINE BOEING757 757223 1384957NM HYDRAULIC SYS LEAKING A AALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW21663AM 25297 RIGHT MAIN GEAR UNDER INDICATION AND LOCKED GEAR DISAGREE EICAS MESSAGE WITH HANDLE UP. RETURNED TO BDA AND LANDED WITHOUT INCIDENT. FOUND RIGHT MAIN GEAR TILT ACTUATOR HYDRAULIC LINE LEAKING. REPLACED HYDRAULIC LINE WITH A FLEX LINE AND NOTIFIED TECH SERVICES FOR FLEX LINE REPLACEMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050510001802005051000180NM 2005 5 10 C1HA200595001 120050405A5754 SKIN BOEING727 727290 138408WNM NR 3 SLAT CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 LEFT WING - L/E NR 3 SLAT AT I/B SLAT TRACK ATTACH POINT SLAT SKIN IS CRACKED APPROX .5 INCH. TRIMMED CRACKED AREA LENGTH OF CRACK APPROX .500 LONG IAW BOEING 727 SRM 57-50-01 FIGURE 2 SHEET 1-5, FOUND TO BE WITHIN LIMITS IAW BOEING EA PO27-57-014 REQUEST NDT AND VERIFIED CRACKED AREA WAS CONTAINED. 2L73 4F A3WE 20050510001822005051000182WP 2005 5 10 UPS05844298 120050321A57445642342U2 FITTING DOUG DC8 DC873F 302199FWP RT FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE:C2 RIGHT FLAP STA 3 SUPPORT FITTING HAS APPROX 6.125 INCH CRACK ON BOTTOM OF FITTING. REMOVED AND REPLACED RIGHT FLAP STA 3 SUPPORT FITTING IAW DC-8 SRM 51-3-0, 51-1-21, AND 51-1-20D. 2L74 4F RT4A25 20050510001842005051000184WP 2005 5 10 UPS05844300 120050318A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE: C2, RT WING UPPER SURFACE CRACKED 2 INCH LONG AROUND FASTENER HEAD AT STA XRS 76 STRINGER 16. REPAIRED RT WING UPPER SURFACE IAW DC-8 SRM 57-2-1 FIG 10. 2L74 4F RT4A25 20050510001862005051000186WP 2005 5 10 UPS05844310 120050412A5321 FLOORBOARD DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 INSPECTION TYPE:C1 REMOVED CORROSION ON FLOORBOARD F86 AND FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-2-0, 53-2-3 FIG 10, AND 51-1-8. 2L74 4F RT4A25 20050510001882005051000188WP 2005 5 10 UPS05844314 120050415A3350 BATTERY PACK DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 330 45967 EMERGENCY LIGHTS BATTERY INOP. REMOVED AND REPLACED BATTERY PACK PER DC-8 AMM CH 33-50-01-2, OPS GOOD. 2L74 4F RT4A25 20050510001902005051000190NM 2005 5 10 C1HA200595003 120050408A5744BAC15141437 ANGLE BOEING727 727290 138408WNM LT WING CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 LEFT WING LOWER ANGLE CRACKED AT STA WS 124 BELOW NR 7 SPOILER SUPPORT FITTING. REMOVED 2 EA AFT ATTACH BOLTS FROM I/B FLAP TRACK, REMOVED TRACKED LOWER ANGLE CHORD AND 2 EA REPAIR ANGLES IAW B727 SRM 51-30-2. CLEANED REPAIR ANGLES IAW B727 M/M 12-90-00, FABRICATED NEW LOWER ANGLE. 2L73 4F A3WE 20050510002022005051000202NM 2005 5 10 SWAA051146 120050418A53306545766 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 DURING WALKAROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 450, STR 15R. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050510002102005051000210NM 2005 5 10 C1HA200595006 120050409A5311 FRAME BOEING727 727290 138408WNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 E & E COMPT STA 320 RBL 17 FRAME LOWER END HAS CORROSION. EGG NEW FLOOR & CLEAR TIE AT FS 320 RBL 17 7075-0 PO 0420685 H/T TO T-6 ON PEMCO TRAVELER 795N000486. LOCATED, TRIMMED, DRILLED, TREATED & INSTALLED IAW 727 SRM 51-10-2 & 51-30-2 SPLICED NEW FRAME. 2L73 4F A3WE 20050510002112005051000211NM 2005 5 10 PIDA200500001 120050419A5330 SKIN BOEING737 73736M 138443BNM FUSELAGE DAMAGED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05374PA 28333 IMPACT DAMAGE TO THE FUSELAGE SKIN, FORWARD ENTRANCE DOORWAY BEARSTRAP AND BS 294.5 BULKHEAD SHEAR TIE AND WEB BETWEEN STR 19LT AND STR 20LT. REPAIRED PER EA 53-074. 2L72 4F RTA16WE 20050510002122005051000212NM 2005 5 10 PIDA200500002 120050419A5330 SKIN PANEL BOEING737 73736M 138443BNM FUSELAGE DAMAGED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05374PA 28333 IMPACT DAMAGE (DENT) AT BS 483 SKIN PANEL BETWEEN STR 21 LT AND STR 22 LT. REPAIRED PER SRM 53-00-01 FIG 229. 2L72 4F RTA16WE 20050510002132005051000213NM 2005 5 10 PIDA200500005 120050419A5311 FRAME BOEING737 73736M 138443BNM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05374PA 28333 TWO CRACKS IN BS 827 FRAME AT STR 9RT. REPAIRED PER SRM 53-00-07. 2L72 4F RTA16WE 20050510002152005051000215NM 2005 5 10 PIDA200500003 120050419A5315 FLOORBEAM BOEING737 73736M 138443BNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05374PA 28333 CORROSION AT CLIP NUT HOLE AT LBL 27 ON FLOORBEAM AT BS 312. REPAIRED PER SRM 53-10-51. 2L72 4F RTA16WE 20050510002202005051000220NM 2005 5 10 PIDA200500007 120050419A5311 FRAME BOEING737 73736M 138443BNM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05374PA 28333 TWO CRACKS IN BS 787 FRAME AT STR 9 LT. REPAIRED PER SRM 53-00-07. 2L72 4F RTA16WE 20050511000012005051100001EU 2005 5 11 MALA050325 120050411A2750 UNKNOWN BAC 146 AVRO146RJ85A1500097EU AIRFRAME OSCILLATES A MALAO OTHER O OTHER CRCRUISE 1 GL15501XJ E2208 PITCH OSCILLATIONS, REPO FLIGHT FROM GLH TO MSP CREW ENCOUNTERED LIGHT TO MODERATE TURBULENCE ON CLIMBOUT. THE AIRCRAFT HAD 2 EVENTS OF SEVERE PITCH OSCILLATIONS ABOUT 15 MINUTES INTO THE FLIGHT BETWEEN 24,000 TO 31,000, LIGHT RIME ICE PROTECTION ON. CREW PERFORMED MEMORY ITEMS AND FOLLOWED THE CHECKLIST. CREW DECLARED AN EMERGENCY AND DIVERTED TO MEM. NO FURTHER INFORMATION AT THIS TIME. 2H74 4F RTA49EU 20050511000102005051100010SO 2005 5 11 SIMA200509806 120050401A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21803AE 145483 THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. PERFORMED A CUTOUT OF THE DAMAGED AREA TO REMOVE THE CORROSION. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB-145/1142 REV 28, CHAPTER 53-21-10 FIG 202. (M) 2L72 4F RTT00011AT 20050511000152005051100015EU 2005 5 11 USAA050466 120050317A5347F57110572202203 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW22938 0337 BFM - FOUND SEAT TRACK CORRODED, 4 INCHES LONG BY 1 INCH WIDE BY .050 INCH DEEP, MAIN CABIN SEAT TRACK Y-2462 FRAME 4-47. FABRICATED SEAT TRACK SPLICE PER SRM 53-31-15. (M) 2L72 4F RTA46NM 20050511000212005051100021NM 2005 5 11 AWXA200500474 120050328A531565C3394016 FLOORBEAM BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - DURING C-19 CHECK CORROSION WAS FOUND ON UPPER CHORD AT BS 294 BETWEEN RBL 7 AND RBL 44, WL 208. MAINTENANCE CUTOUT DAMAGED UPPER CHORD AT BS 294 FROM RBL 7 TO RBL 44; FABRICATED A NEW REPLACEMENT SECTION OF UPPER CHORD AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-51, FIG 205. 2L72 4F RTA16WE 20050511000392005051100039SO 2005 5 11 SWIA200514882 120050418A27523203001007 ACTUATOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07189SW320065657 120048 FLAPS FAILED AT ABOUT 10 DEGREES. REPLACED LEFT OUTBOARD FLAP ACTUATOR IAW MM 27-50-00. 2L72 4T RTA31SO 20050511000402005051100040EA 2005 5 11 SWIA200514883 120050418A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07929SW 7703 SECOND FROM FRONT OVERWING RIGHT SIDE EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050511000482005051100048EA 2005 5 11 SWIA200514887 120050203A5320 THRESHOLD CNDAIRCL600 CL6002B19 1900309EA SERVICE DOOR CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07589SW 7072 CORROSION ON CAP ANGLE FOR SERVICE DOOR THRESHOLD. (ITEM FOUND AT C-CHECK INSPECTION.) INSTALLED NEW CAP ANGLE IAW CRJ 200 SRM 51-42-06. 2L72 4F RTA21EA 20050511000502005051100050EA 2005 5 11 SWIA200514889 120050203A5712 RIB CNDAIRCL600 CL6002B19 1900309EA RT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07589SW 7072 BATT RIB CRACKED AT UPPER FLANGE, AFT SIDE. LOCATED AT RT MLG BAY WS53-600. ITEM FOUND AT C-CHECK INSPECTION, INSTALLED REPAIR PARTS IAW REO 601R-57-51-046. 2L72 4F RTA21EA 20050511000552005051100055NM 2005 5 11 QXEA200500650 120050412A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - LEFT OUTBOARD SEAT TRACK NR 1 HAS CORROSION IN BOTTOM OF CHANNEL AT X312 TO X314. REPAIRED IAW RD 8-53-1342. 2H72 4T RTA13NM 20050511000862005051100086EU 2005 5 11 MALA050369 120050302A5280 BOLT BAC 146 AVRO146RJ85A1500097EU RT MLG DOOR CORRODED A MALAK NONE O OTHER UKUNKNOWN 1 GL15502XJ E2307 RIGHT MLG DOOR UPPER FWD AND AFT ATTACH BOLTS FOUND TO BE CORRODED. BOLTS INSTALLED ON DOOR. 2H74 4F RTA49EU 20050511000932005051100093CE 2005 5 11 DXTA200500688 120050419A3241426691 CONTROL BOX CESSNA650 650 2076802CE ANTI-SKID SYS DEFECTIVE E DXTAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL07713QS4423 6507103 ANTI-SKID LIGHT ILLUMINATED DURING TAXI-OUT. AFTER TEST, LIGHT WENT OUT AFTER 6 SECONDS. AFTER RESET C/B, LIGHT WENT OUT AFTER 6 SEC, LIGHT RE-ILLUMINATED BOTH TIMES AFTER BRAKE APPLICATION, WITH LIGHT ILLUMINATED.; STEP ON RIGHT BRAKE ONLY LT GOES OUT, ON LEFT BRAKE LT STAYS ON. REMOVED AND REPLACED ANTI-SKID CONTROL BOX, OPS CHECK GOOD. 2L72 4F A9NM 20050511000942005051100094NM 2005 5 11 CALA0500114 120050420A361032896265 VALVE BOEING757 757224 1384958NM BLEED AIR SYS MALFUNCTIONED A CALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2713110 27300 CAPTAIN REPORTED BURNING SMELL IN COCKPIT AND CABIN WITH RIGHT ENGINE BLEED OPEN. REPLACED PNEUMATIC AIR CONTROL FAN VALVE PER AMM 36-11-16. 2L72 4F RTA2NM 20050511000952005051100095EU 2005 5 11 DHL2005367506 120050401A5320A5361079723201 FLOOR SUPPORT AIRBUS300 A300B4203 3930306EU CABIN CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01367DH 265 DURING "C" CHECK, CABIN FLOOR AT FR 15 THRU FR 11 AT BL 18L FLOOR SUPPORT BEAM HAS CORROSION ( MKD ). REPLACED CABIN FLOOR AT FR 15 THRU FR 11 AT BL 18L FLOOR SUPPORT AS PER A-300 SRM 53-12-00 P/N A5361079723201. 2L72 4F RTA35EU 20050511001092005051100109NM 2005 5 11 72300162 120050225A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 1.500 INCH BY 3 INCH AREA OF CORROSION ON STRINGER. 2L73 4F4 FRTA3WE E2EA 20050511001112005051100111NM 2005 5 11 72300164 120050317A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 1 INCH BY 5 INCH AREA OF CORROSION ON BOTTOM OF STRINGER. 2L73 4F4 FRTA3WE E2EA 20050511001132005051100113NM 2005 5 11 72300166 120050207A5330 SKIN BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 3 INCH BY 16 INCH AREA OF CORROSION ON SKIN AT LAP SEAM. 2L73 4F4 FRTA3WE E2EA 20050511001172005051100117WP 2005 5 11 ABXA050094 120050418A533057552713 SKIN DOUG DC8 DC863F 302198FWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23812AX 46126 FUSELAGE SKIN COMMON TO THE FACTORY ANTENNA DOUBLER, CORRODED. FABRICATED SKIN AND DOUBLER FOR ANTENNA AND INSTALLED IAW REA D853-51782 ON WO NR 600221026. 2L74 4F 4A25 20050511001192005051100119WP 2005 5 11 05FDEA01053 120050420A5240AKC7011 HINGE DOUG MD10 MD1010F 3022112WP ZONE 800 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25370FE 46608 COMPLY WITH EA8-5240-55472-DOORS-SERVICE-TAILCONE-PATIO DOOR HINGE REPAIR P/N AKC7011 RT. CLOSING ACTION ON 04/15/05. ON N/R S00014. COMPLIED WITH EA 8-5240-55472. 2L73 4F RTA22WE 20050511001222005051100122EU 2005 5 11 2005F00064 120050330A5610NP1588014 WINDSHIELD AEROSPATR72 ATR72212 8680945EU COCKPIT CRACKED A TRBAA UNSCHED LANDING O OTHER CRCRUISE 1 SO29288AM 288 WHILE IN CRUISE, THE RIGHT WINDSHIELD CRACKED. AIRCRAFT DIVERTED TO ST KITTS. ORIGINAL DESTINATION WAS ST LUCIA. REPLACED F/O WINDSHIELD ASSEMBLY. (M) 2H72 4T RTA53EU 20050511001252005051100125CE 2005 5 11 2005F00065 120050328A55201016200131 BRACKET BEECH 1900 1900D 1154162CE RT ELEVATOR CORRODED A GUUAK NONE O OTHER ININSP/MAINT 1 SO2987554 UE227 AT SCHEDULED ROUTINE MAINTENANCE, RIGHT CENTER ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RIGHT CENTER ELEVATOR HINGE BRACKET. (M) 2L72 4T RTA24CE 20050511001272005051100127SO 2005 5 11 SIMA200510116 120050407A532013500437003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21701MH 145162 DURING CPCP INSPECTION, FOUND RIGHT OMEGA BEAM AT CROSS BEAM ATTACHMENT FRAME 29 CORRODED. REMOVED AND INSTALLED NEW OMEGA BEAM IAW EMB SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050511001292005051100129EU 2005 5 11 2005F00068 120050330A3230350A53000100 MFC AEROSPATR72 ATR72212 8680945EU NR 1 FAILED A TRBAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO29369AT 369 WHILE IN CRUISE, ALL THREE GEARS UNSAFE LIGHT ILLUMINATED ON THE LOWER PANEL, ALONG WITH A LOW PRESSURE INDICATION ON THE HYDRAULIC GREEN SYSTEM. UPPER PANEL HAD NO UNSAFE INDICATION. UNABLE TO DUPLICATE DISCREPANCY. AS A PRECAUTIONARY PROCEDURE, THE MULTIFUNCTION COMPUTER NR 1 WAS REPLACED. (M) 2H72 4T RTA53EU 20050511001312005051100131SO 2005 5 11 SIMA200510101 120050401A533014520554001 SKIN EMB 145 EMB145LR 3260212SO FUSELAGE DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21689EC 14500853 SAW - FOUND LIGHTNING STRIKE DAMAGE ON SKIN AT FRAME 22 STRINGER 14L AND 15L. MAINTENANCE INSTALLED SKIN REPAIR DOUBLER IAW SRM 53-21-01. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20050511001322005051100132EA 2005 5 11 A6WA200540138 120050402A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31416AW 7603 LEFT FS 625 OBLIQUE ANGLE CRACKED .5 INCH LONG. S/D - INSTALL NEW ANGLE P/N 601-35012-51 AT LEFT FS 625 IAW CRJ 200 SRM 51-42-06. (M) 2L72 4F RTA21EA 20050511001342005051100134SO 2005 5 11 SIMA200510117 120050407A551014523460003 STRUCTURE EMB 135 EMB135LR 3260305SO HORIZONTAL STAB DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21701MH 145162 SAW - DURING ALTERATION OF GUST LOCK SERVICE BULLETIN 145-55-0086, MISALIGNED HOLES ON RIGHT SIDE OF CARBON BOX OF HORIZONTAL STABILIZER. REPAIRED HOLES IAW ENGINEERING ORDER EB-55MR-094. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050511001352005051100135EA 2005 5 11 A6WA200540153 120050409A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA LT WING CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31417AW 7610 LEFT LOWER WING PLANK IS CORRODED AROUND ENTIRE CIRCUMFERENCE UNDER PANEL 510AB, .100 INCH S BY .002 INCH DEEP. (M) 2L72 4F RTA21EA 20050511001362005051100136EA 2005 5 11 A6WA200540152 120050409A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA LT WING CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31417AW 7610 LEFT LOWER WING PLANK IS CORRODED UNDER PANEL 540BB, FORWARD INBOARD EDGE 4 INCH LONG BY .100 INCH WIDE BY .002 INCH DEEP, AFT EDGE .050 INCH LONG BY .100 INCH WIDE BY .002 INCH DEEP. (M) 2L72 4F RTA21EA 20050511001382005051100138SO 2005 5 11 SIMA200510121 120050404A534713500439007 SEAT TRACK EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21701MH 145162 DURING CPCP INSPECTION, FOUND LEFT FORWARD SEAT TRACK CORRODED AROUND ALL SCREWS. MAINTENANCE REPLACED SEAT TRACK IAW EMB 135 AMM 53-01-06-400-801A. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050511001402005051100140SO 2005 5 11 SIMA200510105 120050411A3150 WARNING LIGHT EMB 135 EMB135KL 3260302SO PITCH TRIM ILLUMINATED A SIMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW21815AE 145545 IN CRUISE RECEIVED F/O BACK UP PITCH TRIM INOPERATIVE MESSAGE. PERFORMED RESET OF THE PITCH TRIM SYSTEM. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050511001422005051100142EA 2005 5 11 A6WA200540137 120050402A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31416AW 7603 RIGHT FS 625.0 OBLIQUE ANGLE CRACKED .5 INCH LONG. S/D - INSTALLED NEW ANGLE AT FS 625 RT P/N 601-35012-52. (M) 2L72 4F RTA21EA 20050511001562005051100156NM 2005 5 11 SWAA051154 120050419A53306545777 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER PAE ER. 2L72 4F RTA16WE 20050511001942005051100194NM 2005 5 11 SWAA051171 120050420A52406545871 DOOR FRAME BOEING737 7373H4 1384600NM R1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29333SW 23697 DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR AFT FRAME CRACKED AT NR 2 & NR 3 STOP FITTING CUTOUTS. REMOVED AND REPLACED DOOR PER MM. 2L72 4F RTA16WE 20050511002162005051100216NM 2005 5 11 EIA2005043 120050329A5311 FRAME BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 M/D BS 1713 STR-13L FRAME CRACKED. CRACKED FRAME REPLACED PER SRM 51-10-01. 2L74 4F A20WE 20050511002282005051100228NM 2005 5 11 EIA2005074 120050330A5320 TIE CLIP BOEING747 747212B 1384886NM FUSELAGE DEFORMED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 M/D BS 1880 S-15R TIE CLIP DEFORMED. TIE CLIP REPLACED PER SRM 51-10-01. 2L74 4F A20WE 20050511002362005051100236NM 2005 5 11 EIA2005081 120050401A5311 FRAME BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 CABIN BS 690 LT BETWEEN STR 23L TO 24L FRAME UPPER FLANGE FOUND CRACKED. CRACKED FRAME REPAIRED PER SRM 53-10-04 FIG 4. 2L74 4F A20WE 20050511002382005051100238NM 2005 5 11 EIA2005083 120050401A5340 SHEAR TIE BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 M/D BS 2160 21R SHEAR TIE CRACKED. SHEAR TIE REPLACED PER SRM 51-10-01. 2L74 4F A20WE 20050511002412005051100241NM 2005 5 11 EIA2005087 120050404A5320 TIE CLIP BOEING747 747212B 1384886NM FUSELAGE CHAFED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 M/D BS 1840 S12R AND S13R TIE CLIP CHAFING. TIE CLIP REPLACED PER SRM 51-10-01 AND 51-30-02. 2L74 4F A20WE 20050511002612005051100261EU 2005 5 11 05FDEA01066 120050422A5730 SKIN AIRBUS310 A310 EU LT WING DAMAGED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25402FE 201 WHILE WORKING EO 6-5710-7-5008PT3, LT WING FOR LANDING ASSY FOR PANEL 575CB 4 EA HOLES NOTED ARE LARGER THAN DRAWING SIZE. THIS IS AN INCOMING CONDITION. HOLE NR 9 .263 INCH, EM PLANK .6 INCH, NR 10 .328 INCH, EM RIB .610 INCH, EM PLANK .760 INCH, NR17 .328 INCH, EM RIB .570 INCH, EM PLANK .840 INCH, NR 21 .263 INCH, EM PLANK .5 INCH. SHOULD BE NR 9 AND 21 AT .187 INCH, NR 10 AND 17 AT .310 INCH. NOTE HOLES NEED COLDWORKING. REPAIRED HOLES IAW EA 6-5730-79121. 2L72 4F RTA35EU 20050511002632005051100263EU 2005 5 11 05FDEA01068 120050422A5313 STRINGER AIRBUS310 A310 EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 AFT CARGO COMPT, BETWEEN FR 54.2 AND FR 54.3 ON STR 56 RT HAS 3 AREAS OF CORROSION. REF FEDEX EA 6-5310-88741, REMOVED SHEAR TIE, REMOVED FASTENERS IAW A310-200 SRM 51-40-21. REMOVED CORROSION, CHECK MATERIAL LOSS IAW A310-200 SRM 53-10-00 PG 123 ITEM 24. FOUND TO BE WITHIN LIMITS. ALODINED, PRIMED, AND TOPCOATED AREA IAW A310-200 SRM 51-23-20. REINSTALLED SHEAR TIE AND FASTENERS IAW A310-200 SRM 51-40-21. 2L72 4F RTA35EU 20050511002652005051100265EU 2005 5 11 05FDEA01069 120050422A5313 STRINGER AIRBUS310 A310203 3930313EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 IN ACM BAY STR 42R HAS AREAS OF CORROSION BETWEEN FRAME 40/41 TO FRAME 44. REMOVED CORROSION PER A310 SRM 51-74-10. C/W EA 6-5310-87784 AND A310 SRM 53-15-12. RESTORED SURFACE PROTECTION PER A310 SRM 51-75-10. 2L72 4F RTA35EU 20050511002672005051100267EU 2005 5 11 05FDEA01071 120050422A5313 STRINGER AIRBUS310 A310 EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 AFT CARGO COMPT JUST AFT OF FR 54.3 ON STR 51 RT HAS 1EA AREA OF CORROSION. REMOVED CORROSION FROM AFT OF FR 54.3 RT STG 51 IAW A310-200 SRM. FOUND MATERIAL TO BE WITHIN LIMITS IAW A310-200 SRM 53-10-00 PG 123 ITEM 24. INSTALLED REMOVED PARTS AND FASTENERS IAW A310-200 SRM 51-40-21. REF FEDEX EA 6-5310-88741 FOR APPROVAL FOR RETURN TO SERVICE. 2L72 4F RTA35EU 20050511002692005051100269NM 2005 5 11 05FDEA00654 120050328A5320AFA7181509 SPLICE DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 CABIN, STA 1641-1661 RT LONGITUDINAL SPLICE AT L11 SUSPECT CRACKED AT FASTENERS HOLES AS MARKED. LONGITUDINAL SPLICE AT STA 1641 TO 1661 RT L-11 REMOVED NEW SPLICE, FABRICATED FROM 1D0755T7150T61511 AS PER DRAWING AFA7181. FPI INSPECTION CARRIED OUT AND FOUND NO EVIDENT OF CRACK. FABRICATED SPLICE REPROTECTED AND PART MARK: AFA 7181-509. FABRICATED SPLICE LOCATED AND INSTALLED BETWEEN STA 1641 TO 1661 RT L-11 AS PER DRAWING NFA6009. 2L73 4F RTA22WE 20050511002782005051100278EU 2005 5 11 05FDEA01080 120050422A5330 SKIN AIRBUS310 A310203 3930313EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 IN A/C BAY, FROM FRAME 46 TO 47, STGR 43R TO 38R HAS SEVERAL AREAS OF CORROSION. REMOVED CORROSION PER A310 SRM 51-74-10. C/W EA 6-5310-87784. FOUND ALL AREAS TO BE WITHIN LIMITS PER EA 6-5310-87784. RESTORED SURFACE PROTECTION PER A310 SRM 51-75-10. 2L72 4F RTA35EU 20050511002802005051100280EU 2005 5 11 05FDEA01082 120050422A5330 SKIN AIRBUS310 A310203 3930313EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 IN AC BAY, FRAME 39 TO 40 AND STGR 47R TO 43R HAS AREAS OF CORROSION. REMOVED CORROSION PER A310 SRM 51-74-10. FOUND ALL AREAS TO BE WITHIN LIMITS IN AREA FR 39 TO 40 AND STR 45R TO 44R AND STR 47R TO 46R. C/W EA 6-5310-87784. INSTALLED FASTENERS PER A310 SRM 51-40-21. RESTORED SURFACE PROTECTION PER A310 SRM 51-75-10. 2L72 4F RTA35EU 20050511002822005051100282EU 2005 5 11 05FDEA01084 120050422A5330 SKIN AIRBUS310 A310203 3930313EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 IN ACM BAY SKIN BETWEEN STR39R AND STR40R AND FR46 TO FR47 HAS AREAS OF CORROSION. REMOVED CORROSION PER A310 SRM 51-74-10. FOUND TO BE WITHIN LIMITS PER A310 SRM 53-15-12 AND EA 6-5310-87784. RESTORED SURFACE PROTECTION PER A310 SRM 51-75-10. C/W EA 6-5310-87784. 2L72 4F RTA35EU 20050511002842005051100284EU 2005 5 11 05FDEA01086 120050422A5330 SKIN AIRBUS310 A310203 3930313EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 IN AC BAY, FROM FRAME 41 TO 42 AND STGR 51R TO 47R, AREA HAS CORROSION ON SKIN. REMOVED FASTENERS IAW A310-200 SRM 51-40-21. REMOVED CORROSION IAW A310-200 SRM 51-74-10. MATERIAL REMOVED WITHIN LIMITS IAW A310-200 SRM 53-10-00. FLAP PEENED AS REQUIRED IAW A310-200 51-29-00, TREATED, PRIMED, AND APPLIED TOP COAT IAW A310-200 SRM 51-75-10. REINSTALLED FASTENERS IAW A310-200 SRM 51-40-21. 2L72 4F RTA35EU 20050511002862005051100286EU 2005 5 11 05FDEA01088 120050422A5330 SKIN AIRBUS310 A310203 3930313EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 IN ACM BAY FR 43 TO FR 44 BETWEEN STR 40L AND STR 41L SKIN HAS AREAS OF CORROSION. REMOVED CORROSION IAW A310 SRM 51-74-10, WITHIN LIMITS, FLAP PEENED IAW A310 SRM 51-29-00 AND RESTORED PROTECTIVE COATING IAW A310 SRM 51-75-10 ON SKIN FR 43 TO FR 44 BETWEEN STR 40L AND 41L. 2L72 4F RTA35EU 20050511002882005051100288EU 2005 5 11 05FDEA01090 120050422A5330 SKIN AIRBUS310 A310203 3930313EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 IN ACM BAY SKIN BETWEEN STR 39R TO STR 40R HAS AREAS OF CORROSION BETWEEN FR 44 TO FR 45. REMOVED CORROSION IAW A310-200 SRM 51-74-10. FOUND TO BE WITHIN LIMITS IAW A310-200 SRM 53-15-12. FLAP PEENED IAW A310-200 SRM 51-29-00. TREATED PRIMED AND TOPCOATED IAW A310-200 SRM 51-23-10. 2L72 4F RTA35EU 20050511002902005051100290EU 2005 5 11 05FDEA01092 120050422A5330 SKIN AIRBUS310 A310203 3930313EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 IN ACM BAY FR 46 TO FR 47 BETWEEN STR 44L AND STR 45L SKIN HAS AREAS OF CORROSION. REMOVED CORROSION IAW A310 SRM 51-74-10 WITHIN LIMITS. FLAP PEENED IAW A310 SRM 51-29-00 AND RESTORED PROTECTIVE COATING IAW A310 SRM 51-75-10. 2L72 4F RTA35EU 20050511002952005051100295EU 2005 5 11 05FDEA01097 120050422A5321 FLOOR PANEL AIRBUS310 A310203 3930313EU ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 FLOOR PANEL 231NH HAS 3 EA CRACKS AND 7 EA MISSING/BROKEN INSERTS. FABBED REPLACEMENT PANEL 231NH IAW FED EX DWG NR SRZ-25-005 REV E. 2L72 4F RTA35EU 20050511002972005051100297EU 2005 5 11 05FDEA01099 120050422A5730 SKIN AIRBUS310 A310203 3930313EU ZONE 500 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 LT WING, 560CB HAS 1 EA ELONGATED HOLE. COMPLIED WITH EA 6-5710-87212. 2L72 4F RTA35EU 20050511002992005051100299EU 2005 5 11 05FDEA01101 120050422A5311A5381122120100 FRAME AIRBUS310 A310203 3930313EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 IN A/C BAY, FRAME 47 AFT SIDE FROM STGR40R TO 47R HAS CORROSION. REMOVED AND REINSTALLED FASTENERS IAW A310 SRM 51-40-21. REMOVED CORROSION IAW A310-200 SRM 51-74-10. ROTOTESTED HOLES AND CLEARED DEFECTS IAW A310 NTM 51-10-01. ALL WORK WAS PERFORMED AND LIMITS ARE GOOD IAW FEDEX EA 6-5310-87236. 2L72 4F RTA35EU 20050511003032005051100303EU 2005 5 11 05FDEA01109 120050424A5330 SKIN AIRBUS310 A310203 3930313EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 CORROSION ON SKIN IN A/C BAY BETWEEN FRAMES 39 TO 40/41 AND STRINGERS 43L TO 47L. REMOVED CORROSION PER A310 SRM 51-74-10. C/W EA 6-5310-87784. FOUND ALL AREAS TO BE WITHIN LIMITS PER EA 6-5310-87784 AND A310 SRM 53-15-12. RESTORED SURFACE PROTECTION PER A310 SRM 51-75-10. 2L72 4F RTA35EU 20050511003052005051100305EU 2005 5 11 05FDEA01110 120050424A7830 WEB AIRBUS310 A310203 3930313EU THRUST REVERSER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 NR 2 ENG O/B REVERSER COWL HAS A CRACKED WEB, ON UPPER ANGLE GEAR BOX ACTUATOR HOLE, REV DEPLOYED). REMOVED NR 2 ENG O/B T/R GEAR BOX ASSY IAW A310-200 MM 78-31-03-2-B, AND FAB FILLER AND REPAIRED DOUBLER IAW EA 6-7830-87417 AND REINSTALLED UPPER GEAR BOX IAW A310-200 MM 78-31-03-2-B. OPS CHECK GOOD. 2L72 4F RTA35EU 20050511003082005051100308NM 2005 5 11 EIA2005045 120050329A5311 FRAME BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 M/D BS 540 FRAME AT STR 25L FOUND CRACKED. FRAME REPAIRED PER SRM 53-10-04 FIG 35. 2L74 4F A20WE 20050511003092005051100309NM 2005 5 11 EIA2005046 120050329A5311 FRAME BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 M/D BS 2235 FRAME AT STR 22R I/B WEB FOUND CRACKED. FRAME WEB REPAIRED PER SRM 53-10-04 FIG 34. 2L74 4F A20WE 20050511003102005051100310NM 2005 5 11 EIA2005047 120050329A5313 STRINGER BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 M/D BS 1238 STR 6R STRINGER END FOUND CRACKED. STRINGER REPAIRED PER SRM 53-10-03 FIG 5. 2L74 4F A20WE 20050511003112005051100311NM 2005 5 11 EIA2005048 120050329A5330 BEAR STRAP BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 CRACK REVEALED AT AFT CARGO DOOR CUTOUT FWD UPPER CORNER BEAR STRAP. CRACK TRIMMED OFF, NDT INSPECTED AND FOUND WITHIN LIMITS SRM 53-20-03 FIG 62 LIMIT. EXISTING DOUBLER REINSTALLED PER SRM 53-30-02 FIG 62. 2L74 4F A20WE 20050511003122005051100312NM 2005 5 11 EIA2005049 120050329A5313 STRINGER BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 CABIN BS 1960 RT STR 25R STRINGER END FOUND CRACKED. THE CRACK PORTION WAS TRIMMED OFF AND NDT CONFIRMED CRACK FREE CONDITION, STRINGER REPAIRED PER SRM 53-10-03 FIG 1. 2L74 4F A20WE 20050511003132005051100313NM 2005 5 11 EIA2005050 120050329A5330 SKIN BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 CRACKED REVEALED AT RT FUSELAGE SKIN BS 980 STR 38R DRAG SPLICE FITTING. BS 980 STR 38R FUSELAGE SKIN REPAIRED PER SRM 53-30-03 FIG 60. 2L74 4F A20WE 20050511003152005051100315NM 2005 5 11 EIA2005052 120050329A5315 FLOORBEAM BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 U/D FLOORBEAM UPPER CHORD ONE FASTENER HOLE FOUND CRACKED AT BS 520 LBL 45 AFT FLANGE. THE CRACK PORTION TRIMMED OFF AND NDT CONFIRMED CRACK FREE CONDITION, THE FLOORBEAM REPAIRED PER SB 747-53-2452 FIG 9. 2L74 4F A20WE 20050511003172005051100317NM 2005 5 11 EIA2005054 120050330A5315 FLOORBEAM BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 UPPER DECK FLOORBEAM UPPER CHORD AT BS 360 FOUND CRACKED AT 4 EA FASTENER HOLES. LOCATION AT LBL 55, RBL 23, RBL 58 REPAIRED PER S/B 53A2431 FIG 9. LBL 33 REPAIRED PER S/B 53A2431 FIG 10. 2L74 4F A20WE 20050511003182005051100318NM 2005 5 11 EIA2005055 120050330A5320 TIE CLIP BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 M/D BS 340 STR 23 TIE CLIP CRACKED. TIE CLIP REPLACED PER SRM 51-10-01. 2L74 4F A20WE 20050511003202005051100320NM 2005 5 11 EIA2005057 120050330A5340 SHEAR TIE BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 M/D BS 1780 AT STR 4R SHEAR TIE FOUND CRACKED. SHEAR TIE REPLACED PER SRM 51-10-01. 2L74 4F A20WE 20050511003212005051100321NM 2005 5 11 EIA2005058 120050330A5320 TIE CLIP BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 M/D BS 980 S-5L STRINGER TIE CLIP FOUND CRACKED. TIE CLIP REPLACED PER SRM 51-10-01. 2L74 4F A20WE 20050511003222005051100322NM 2005 5 11 EIA2005059 120050330A5347 SEAT TRACK BOEING747 747212B 1384886NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 U/D BS 760 RBL 76 SEAT TRACK AND BOTH LIPS FOUND CORROSION. U/D CORRODED SEAT TRACK REPLACED PER SRM 51-10-01 PG 9. DUE TO CORROSION BLEND OUT EXCEEDS SRM LIMIT. 2L74 4F A20WE 20050511003232005051100323NM 2005 5 11 EIA2005060 120050330A5210 SKIN BOEING747 747212B 1384886NM PAX DOOR CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 CABIN PAX DOOR 3L AT DOOR FRAME NR 3 BETWEEN STR 24L & 25L OUTER SKIN CRACKED. CRACK SKIN TRIMMED OFF AND NDT CONFIRMED CRACK FREE SKIN REPAIRED PER SRM 52-00-03 FIG 6. 2L74 4F A20WE 20050511003242005051100324NM 2005 5 11 EIA2005061 120050330A5210 SKIN BOEING747 747212B 1384886NM PAX DOOR CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 CABIN PAX DOOR 1R AT DOOR FRAME NR 4 BETWEEN STR 24R AND 25R OUTER SKIN CRACKED. CRACKED SKIN TRIMMED OFF, NDT CONFIRMS CRACK FREE. SKIN REPAIRED PER SRM 52-00-03 FIG 4. 2L74 4F A20WE 20050509000082005050900008EU 2005 5 9 CHQA200500083 120050415A2810SEEABOVE FLAPPER VALVE EMB ERJ170ERJ170100LR EU FUEL SYSTEM LEAKING A CHQAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL11643RW 17000060 AT CRUISE ALTITUDE FLT ATTENDANT LOOKED OUT THE WINDOW AT ROW 13 TO THE RT AND NOTICED THAT SOMETHING WAS NOT RIGHT. THE OTHER FLT ATTENDANT LOOKED AND SAW SOMETHING WAS GUSHING OUT OF THE RT WING IN LARGE QUANTITIES. THE PILOT REQUESTED FLT ATTENDANT TO COME TO THE FLT DECK SO THE 1ST OFFICER COULD SEE WHAT WAS GOING ON. THE 1ST OFFICER THE LT AND RT SIDE OF THE AIRCRAFT. FLT RETURNED TO MSY. MAINTENANCE FOUND EVIDENCE OF A FUEL LEAK. REMOVED AND REPLACED RIGHT AND LEFT FLAPPER CHECK VALVE P/N 2770088-101 AND RIGHT AND LEFT FLOAT VENT VALVE P/N 2930015-102. OPS AND LEAK CHECK GOOD. NO DEFECTS NOTED. 2L74 4F RTA56NM 20050509000102005050900010SO 2005 5 9 CHQA200500084 120050416A3350375924 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11261SK 145144 FORWARD FACING EMERGENCY LIGHT IN CEILING IS INOP. REMOVED AND REPLACED EMERGENCY EXIT LOCATING SIGN ASSY IAW EMB 145 AMM 33-50-15. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050509000132005050900013WP 2005 5 9 ABXA050091 120050414A32607000010101ABX SWITCH DOUG DC9 DC931 3022065WP NLG POS WARN DEFECTIVE A ABXAO OTHER O OTHER APAPPROACH 1 GL23924AX553 47403 ON APPROACH, NOSE GEAR SAFE FAILED TO ILLUMINATE. RAN ABNORMAL, GEAR RECYCLE, LANDED WITHOUT PROBLEM. VERIFIED WORN PADDLE ON NOSE LANDING GEAR DOWN SWITCH. REMOVED AND REPLACED GEAR DOWN SWITCH IAW DC-9 MM 32-60-01-2-0101. OPS CHECKED GOOD. 2L72 4F A6WE 20050509000252005050900025NM 2005 5 9 UPS05644290 120050415A2560 SMOKE GOGGLES BOEING767 767300 1385204NM COCKPIT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01311UP 27741 INSPECTION TYPE:N/A PILOTS SMOKE GOGGLES CRACKED. REPLACED PILOTS SMOKE GOGGLES. 2L72 4F RTA1NM 20050509000312005050900031WP 2005 5 9 UPS05844289 120050410A5230 SKIN DOUG DC8 DC873F 302199FWP CARGO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE:C2 C-PIT DOOR UPPER AFT CORNER HAS CRACK IN FIRST FASTENER HOLE ABOVE FITTING ATTACH LIP UNDER INTERIOR SKIN. REPAIRED C-PIT DOOR IAW DC-8 SRM 52-2-0 FIG 2. 2L74 4F RT4A25 20050509000492005050900049EA 2005 5 9 QXEA200500578 120050323A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - CENTER FUSELAGE LOWER SKIN LEFT SIDE HAS TWO SKIN NICKS STATION 521 TO 517 AND BETWEEN STRINGERS 24 AND 25 PORT. REPAIRED IAW CRJ700 SRM 51-25-01, PAGE 7, PARAGRAPH B AND SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050509000602005050900060NM 2005 5 9 AWXA200500454 120050415A2560P4010021 BATTERY AIRBUSA319 A319132 3930340NM FLASHLIGHT DISCHARGED A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28832AW 1643 LAX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY IN THE FORWARD EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050509000682005050900068NM 2005 5 9 AWXA200500462 120050404A575465C26603100 SKIN BOEING737 73733A 1384673NM NR 4 SLAT WEDGE DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCN - MAJOR REPAIR - DURING C-19 CHECK THE NR 4 SLAT WEDGE WAS DELAMINATED AT THE BOTTOM OUTBOARD END BETWEEN SLAT STA 120-124 RT. MAINTENANCE REMOVED DAMAGE IN LOWER SURFACE SKIN OF NR 4 SLAT WEDGE; FABRICATED A FILLER AND DOUBLER; BONDED REPAIR PARTS TO SLAT IAW 51-70-10 FIG 16. 2L72 4F RTA16WE 20050509000702005050900070NM 2005 5 9 AWXA200500464 120050404A575465C266021 SKIN BOEING737 73733A 1384673NM NR 2 SLAT WEDGE DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCN - MAJOR REPAIR - DURING C-19 CHECK THE NR 2 SLAT WEDGE WAS FOUND DELAMINATED ON THE UPPER & LOWER SURFACE AT OUTBOARD END BETWEEN SLAT STA 250.9 AND SLAT STA 254.4 LT. MAINTENANCE REMOVED DAMAGE IN UPPER AND LOWER SURFACE SKIN OF NR 2 SLAT WEDGE FROM SS 250.9 TO SS 254.4 LT; FABRICATED A FILLER AND DOUBLER; BONDED REPAIR PARTS TO SLAT IAW 51-70-10 FIG 31. 2L72 4F RTA16WE 20050509000752005050900075EA 2005 5 9 QXEA200500591 120050317A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE INTERIOR, RIGHT OUTBOARD SEAT RAIL AT STATION X613, HAS PITTING CORROSION ON MOST INBOARD SURFACE. REPAIRED IAW CRJ700/900 SRM 51-21-06-001-001-A01, PARAGRAPH 3E. 2L72 4F RTA21EA 20050509001002005050900100EU 2005 5 9 USAA050121 120050112A5321F5367270300000 FLOORBOARD AIRBUS330 A330323 3930335EU FUSELAGE PUNCTURED A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW21927 0342 BFM - FOUND FLOORBOARD PUNCTURED 1 INCH BY 2 INCH PUNCTURE, MAIN CABIN FLOORBOARD 231SF. PUNCTURE IN AREA, NOT REPAIRABLE. FABRICATED NEW FLOORBOARD PER SRM 53-02-00. (M) 2L72 4F RTA46NM 20050509001072005050900107EU 2005 5 9 USAA050134 120050116A5347F5367283800000 FLOORBOARD AIRBUS330 A330323 3930335EU FUSELAGE DENTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW 0342 BFM - FOUND FLOORBOARD WITH 3 DENTS, TWO CRACKS, 12 SQUARE INCHES, MAIN CABIN FLOOR PANEL 242 HF. REMOVED DAMAGED AREAS, FABRICATED REPAIR PATCH PER SRM 53-02-00. (M) 2L72 4F RTA46NM 20050509001122005050900112EU 2005 5 9 USAA050127 120050112A5347F5331140220001 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW21927 0342 BFM - FOUND SEAT TRACK CORRODED 3.70 INCH LONG BY 1.5 INCH WIDE BY .040 INCH DEEP, FRAME 47-53.1 +Y450 -Z240. REMOVED AND REPLACED WITH NEW SEAT TRACK PER SRM 53-31-15, FIG 101 AND 51-74-00. (M) 2L72 4F RTA46NM 20050509001162005050900116EU 2005 5 9 USAA050276 120050209A5321F53671418001 FLOORBOARD AIRBUS330 A330323 3930335EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19671UW22760 0323 BFM - FOUND FLOORBOARDS CRACKED WITH 1 INCH CRACKS ON ALL 3 PANELS, FRAME 53.6 BETWEEN L3 AND R3 DOORS, MAIN CABIN FLOOR. FABRICATED 3 NEW FLOORBOARDS PER SRM 53-02-00. (M) 2L72 4F RTA46NM 20050509001202005050900120EU 2005 5 9 USAA050123 120050111A5320F53113515200 FLOOR SUPPORT AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW21927 0342 BFM - FOUND FLOOR SUPPORT CORRODED, FRAME 134 Y-730 Z-240. REPLACED WITH NEW FLOOR SUPPORT PER SRM 53-11-14 FIG 1 ND 51-74-00. CORROSION LEVEL 2, TASK NR J7-900-09000-042. (M) 2L72 4F RTA46NM 20050509001252005050900125EU 2005 5 9 USAA050243 120050204A5347F5347621420100 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19671UW22760 0323 BFM - FOUND SEAT TRACK, 1 INCH WIDE BY 2 INCHES LONG, BY .032 INCH DEEP AND 1 INCH WIDE BY 2.75 INCH LONG BY .030 INCH, FRAME 55-58, -Y450 MAIN CABIN FLOOR. REMOVED AND REPLACED SEAT TRACK PER SRM 53-00-15, 51-42-11. (M) 2L72 4F RTA46NM 20050509001272005050900127EU 2005 5 9 USAA050124 120050109A5347F5347621420100 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW 0342 BFM - FOUND SEAT TRACK CORRODED, 2.20 INCH LONG BY 1.1 INCH WIDE BY .050 INCH DEEP, MAIN DECK CABIN -450 FRAME 54-59. REMOVED AND REPLACED SEAT TRACK PER SRM 53-00-15, FIG 101. CORROSION LEVEL 2, TASK NR J7-200-25806. REMOVED AND REPLACED SEAT TRACK PER SRM 53-00-15, FIG 101. (M) 2L72 4F RTA46NM 20050509001282005050900128EU 2005 5 9 USAA050125 120050113A5347F5327585200 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19647UW21927 342 BFM - FOUND SEAT TRACK CORRODED, FRAME 37 PLUS Y450 - Z240. CUT OUT DAMAGED AREA AND REPLACED WITH NEW TRACK SECTION PER SRM 53-00-15 FIG 202. (M) 2L72 4F RTA46NM 20050509001452005050900145 2005 5 9 SWAA051115 420050414A25656970843 LATCH BOEING737 7373A4 1384585NM R1 DOOR SLIDE OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29678AA 23290 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE RELEASE MECHANISM OUT OF ADJUST. ADJUSTED RELEASE MECHANISM PER MM. 2L72 4F RTA16WE 20050509001502005050900150NM 2005 5 9 SWAA051120 120050414A53126582671 PRESSURE PANEL BOEING737 7373TO 138447GNM MLG W/W CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29697SW 23838 DURING SCHEDULED 1/4D CHECK, FOUND 2 EA BEADED PRESSURE WEB CRACKS AT BS 664, LBL 31 & LBL 38. REPAIRED WEB PER SWA EA. 2L72 4F RTA16WE 20050509001522005050900152NM 2005 5 9 SWAA051122 120050414A53306545774 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 22L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050509001532005050900153NM 2005 5 9 SWAA051123 120050414A53306545774 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 19R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050509001622005050900162NM 2005 5 9 SWAA051137 120050417A3350101073 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29394SW 27380 L2 DOOR EMERGENCY EXIT SIDE LIGHT LENS MISSING. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20050509001682005050900168NM 2005 5 9 SWAA051143 120050416A53306545766 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29680AA 23505 DURING WALKAROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 450, STR 15R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050509001752005050900175NM 2005 5 9 SWAA051132 120050417A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727A, STR 14R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050510000032005051000003CE 2005 5 10 70332 120050415A5270 SWITCH BEECH 1900 1900D 1154162CE CARGO DOOR OUT OF ADJUST A AMWAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 CE07142ZV UE142 IN CRUISE, CARGO DOOR ANNUNCIATOR ILLUMINATED. RAN APPROPRIATE EMERGENCY CHECKLIST. DECLARED EMERGENCY WITH PHX/ABQ CENTER. LANDED AT PHX WITH NO INJURY TO AIRCRAFT OR PASSENGERS. SYSTEM MEL'D. MAINTENANCE ADJUSTED CARGO DOOR JAM SWITCH. 2L72 4T RTA24CE 20050510000162005051000016EA 2005 5 10 QXEA200500598 120050317A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE INTERIOR RIGHTHAND OUTBOARD SEAT RAIL AT STATION X810 HAS PITTING CORROSION ON MOST INBOARD SURFACE. REPAIRED IAW CRJ700/900 SRM 51-21-06-001-001-A01, PARAGRAPHA 3E, REO 670-53-00-013 AND CRJ700 SRM 51-21-16, CODE A044. 2L72 4F RTA21EA 20050510000402005051000040CE 2005 5 10 DXTA200500683 120050417A3230 ROLLER CESSNA750 750 2076810CE NLG STIFF E DXTAA UNSCHED LANDING O OTHER CRCRUISE 1 GL07967QS 7500067 NOSE GEAR CYCLE - HEARD AND FELT A THUMP, NO LIGHTS. FOUND UPLOCK ROLLERS STIFF TO TURN AND LEFT MLG UPLOCK HOOK WAS STIFF AND WOULD NOT SEAT THE ROLLER EVERY TIME. CLEANED AND LUBED ROLLERS AND UPLOCK HOOK. ADJUSTED BOTH MLG UPLOCK SWITCHES. ALL UPLOCK HOOKS ARE MAKING FULL ENGAGEMENT. OPS CHECKED GOOD ON SEVERAL GEAR SWINGS IAW 750 MM CHAPT 32-30-05. 2L72 4J RTT00007WI 20050510000412005051000041CE 2005 5 10 GNB2005F00002 120050403A32505000008124 CABLE CESSNA402 402C 207590RCE CONT O520 TSIO520* 17040SO NOSE STEERING FRAYED E GNBAK NONE O OTHER ININSP/MAINT 1 SW013292M 402C0304 DURING INSPECTION, FOUND RT NOSE STEERING CABLE BLENDED AND FRAYED AT PULLEY. NEW MFG CABLES (STANLESS STEEL) LAST ONLY FRACTION OF TIME AS OLD STYLE CABLES. HAS BECOME MUCH MORE COMMON OCCURRANCE. (K) 1L72 3O3 O A7CE E8CE 20050510001032005051000103CE 2005 5 10 DJFA2005085 120050419A3244237K232 TIRE RAYTHNDH125 HAWKER800XP 7150012CE MLG FAILED E DJFAO OTHER O OTHER LDLANDING 1 EA23847CW212 258647 KSNA - KCCR CREW REPORTED THAT BOTH LEFT MAIN TIRES BLEW OUT ON LANDING. A/C WAS ABLE TO TAXI CLEAR OF THE RUNWAY. FIRE/RESCUE PERSONNEL WERE ON SCENE. MX REPLACED THE LT MAIN WHEEL ASSEMBLIES. LEFT MAIN GEAR BRAKE ASSEMBLIES WERE INSPECTED WITH NO NOTED DEFECTS. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA3EU 20050510001462005051000146EU 2005 5 10 MALA050291 120050322A5320 FLOOR SUPPORT SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15415XJ 340B415 DURING 4K CHECK IN BNA FOUND FWD AND AFT FLOOR FLANGE AT FS 258, BETWEEN RBL 10 AND LBL 18 IS CORRODED AND HAS BEEN REPAIRED IAW MESABA EO S53102. 2L72 4T RTA52EU 20050510001492005051000149EU 2005 5 10 MALA050327 120050412A2420 TRU BAC 146 AVRO146RJ85A1500097EU NR 1 FAILED A MALAO OTHER SJ AFFECT SYSTEMS WARNING INDICATION CRCRUISE 1 GL15513XJ E2329 INFLIGHT FROM CLE-DTW, THE NR 1 ENGINE DRIVEN GENERATOR FELL OFF LINE. NR 1 TRU FAILED. CAPTAIN LOST ALL OF THE FOLLOWING ITEMS AS A RESULT. FLAP TRIM COMPENSATOR, AUTO PILOT, ELECTRIC TRIM, FTC 1, FGC 1 LIGHT ILLUMINATED, FLIGHT DIRECTOR FAILED AND THE CAPTAIN'S EFFIS FAILED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. REPLACED THE IDG. 2H74 4F RTA49EU 20050510001512005051000151EU 2005 5 10 MALA050344 120050411A2610 WARNING LIGHT SAAB SF340 340B 7860101EU LT TAILPIPE ILLUMINATED A MALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL15410XJ 340B410 LT TAIL PIPE HOT LIGHT. ABORTED TAKEOFF. NO FURTHER INFORMATION AT THIS TIME. 2L72 4T RTA52EU 20050510001582005051000158EU 2005 5 10 MALA050300 120050324A3260 SQUAT SWITCH SAAB SF340 340B 7860101EU MLG CONTAMINATED A MALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL15420XJ 340B420 AIR TURNBACK FOR GEAR TRANSIT LIGHT, DUE TO SNOW AND ICE BUILDUP. CLEANED SNOW FROM SQUAT SWITCH. 2L72 4T RTA52EU 20050510001612005051000161EU 2005 5 10 MALA050309 120050330A7931 CONNECTOR SAAB SF340 340B 7860101EU OIL PRESS XMITERLOOSE A MALAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL15367PX 340B271 RIGHT ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED AFTER START AND THE RT ENGINE OIL PRESSURE GAUGE READ LOW (IN YELLOW RANGE). RETURNED TO GATE. RIGHT ENGINE OIL PRESSURE TRANSMITTER CONNECTOR LOOSE. TIGHTENED PLUG. 2L72 4T RTA52EU 20050510001632005051000163EU 2005 5 10 MALA050295 120050321A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15415XJ 340B415 DURING 4K CHECK IN BNA REMOVED AND REPLACED SEAT TRACK AT BL O IAW MESABA EO S53060 R3, FROM FS 294 TO FS 373. 2L72 4T RTA52EU 20050510001652005051000165EU 2005 5 10 MALA050314 120050405A3610 HOSE SAAB SF340 340B 7860101EU BLEED AIR SYSTEMLEAKING A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15457XJ 340B457 RT BLEED AIR LEAK LIGHT ILLUMINATED INFLIGHT ALONG WITH BLEED CLOSED. THE LIGHT DID NOT EXTINGUISH WITH BLEEDS CLOSED. REMOVED AND REPLACED RT BLEED AIR HOSE. 2L72 4T RTA52EU 20050510001672005051000167EU 2005 5 10 MALA050298 120050323A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15415XJ 340B415 DURING 4K CHECK IN BNA FOUND SEAT TRACK AT BL 0 AND FS 649 IS CORRODED ON THE LOWER LT FLANGE AND HAS BEEN REPAIRED IAW MESABA EO S53076. 2L72 4T RTA52EU 20050510001692005051000169EU 2005 5 10 MALA050296 120050321A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15415XJ 340B415 DURING 4K CHECK IN BNA REMOVED AND REPLACED SEAT TRACK AT LBL 18.3 IAW MESABA EO S53060R3, FROM FS 294 TO 373. 2L72 4T RTA52EU 20050510001712005051000171EU 2005 5 10 AALA20050274 120050416A3260 PROXIMITY SENSOR AIRBUS300 A300B4605R 3930308EU MLG INOPERATIVE A AALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW2170074 517 LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED AIR/GROUND PROXIMITY BOX. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20050510001732005051000173NM 2005 5 10 AALA20050276 120050418A3350 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21798AN 30797 DFW - EMERGENCY PATH LIGHTING IN LEFT ONE AND TWO CLOSET AREA INOPERATIVE. REPLACED BATTERY PACK AT LEFT NR 1 DOOR M33093 FOR EMERGENCY PATH LIGHTING IN LEFT NUMBER ONE AND NUMBER TWO CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20050510001752005051000175WP 2005 5 10 AALA20050277 120050418A2133 GASKET DOUG DC9 DC982 3022082WP LT A/C PACK INOPERATIVE A AALAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SW21210AA 49161 FLIGHT ATTENDANT REPORTED SMOKE IN AFT CABIN AFTER TAKEOFF. RETURNED TO STL AND LANDED WITHOUT INCIDENT. REPLACED GASKETS ON LOOSE LEFT PACK PRESSURE REGULATING AND SHUTOFF VALVE 90 DEGREE ELBOW. REPLACED SOCKS AND ACCOMPLISHED CARDS 21-96-01 AND 21-92-12. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050510001772005051000177NM 2005 5 10 AALA20050271 120050415A3350 LIGHT BOEING767 767323 1385205NM SEAT 28H INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21373AA 25200 DFW - EMERGENCY LIGHT AT SEAT 28H INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 28H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050510001792005051000179NM 2005 5 10 NACA20050011 120050419A291355097 PUMP BOEING727 72722C 138400FNM NR 2 HYD SYS LEAKING A NACAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 AL03792A 37 37 19195 A-SYSTEM QUANTITY DECREASING AT TOP OF CLIMB. REPLACED NR 2 A-SYSTEM PUMP FOR LEAKING AT MATING SURFACE. BLED A-SYSTEM AND SERVICED HYDRAULICS. REPLACED NR 1 & NR 2 CASE DRAIN FILTERS. NO FINDINGS IN REMOVED FILTERS. LEAK & OP CHECKED GOOD. 2L73 4F A3WE 20050510001812005051000181NM 2005 5 10 C1HA200595002 120050405A5754 SKIN BOEING727 727290 138408WNM NR 3 SLAT CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15295AS 22147 LEFT WING - L/E NR 3 SLAT AT O/B SLAT TRACK ATTACH POINT SLAT SKIN IS CRACKED APPROX .5 INCH. TRIMMED CRACKED AREA LENGTH OF CRACK APPROX .500 LONG IAW BOEING 727 SRM 57-50-01 FIGURE 2 SHEET 1-5, FOUND TO BE WITHIN LIMITS IAW BOEING EA PO27-57-014 NDT VERIFIED CRACKED AREA CONTAINED PER 727 DNTM PAR. 2L73 4F A3WE 20050510002052005051000205NM 2005 5 10 SWAA051149 120050418A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29333SW 23697 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 518, STR 15L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050510002062005051000206NM 2005 5 10 SWAA051150 120050418A53156545410 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29333SW 23697 DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOORBEAM T-CHORD CRACKED AT BS 660.5, BL 0. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20050510002232005051000223NM 2005 5 10 PIDA200500004 120050419A5311 FRAME BOEING737 73736M 138443BNM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05374PA 28333 TWO CRACKS IN BS 787 FRAME AT RIVET HOLE AT STR 9RT. REPAIRED PER SRM 53-00-07. 2L72 4F RTA16WE 20050511000052005051100005SO 2005 5 11 SIMA200509401 120050331A532014525381003 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21643AE 145200 ABI - THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. PERFORMED A CUTOUT OF THE OMEGA BEAM TO REMOVED THE CORROSION. FABRICATED A DOUBLER, FILLER, PLATE AND SHIM. REPAIR DONE IAW EMB 145 SRM, SRM EMB-145/1142 REV 28, CHAPTER 53-21-10 FIG 201. (M) 2L72 4T RTT00011AT 20050511000202005051100020EU 2005 5 11 AWXA200500473 120050404A5347D5713014720202 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28638AW 455 SAL - MAJOR REPAIR - DURING C-08 CHECK GALVANIC CORROSION WAS FOUND ON LT OUTBOARD SEAT TRACK AT FR 39+3 INCH. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK AT FR 39+3 INCH; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK PER DWG D53370500; INSTALLED REPAIR PART IAW A320 SRM 51-42-11. 2L72 4F RTA28NM 20050511000412005051100041NM 2005 5 11 QXEA200500685 120050401A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09367PH 511 PDX - LEFTHAND INBOARD SEAT TRACK HAS SURFACE CORROSION ON TOP SURFACE AT STATION 598. REPAIRED IAW RD 8-53-784. 2H72 4T RTA13NM 20050511000462005051100046NM 2005 5 11 AALA20050279 120050419A3230 LANDING GEAR BOEING757 757223 1384957NM NLG MALFUNCTIONED A AALAK NONE O OTHER CLCLIMB 1 SW21190AA 32384 DFW - NOSE LANDING GEAR WOULD NOT RETRACT ON TAKEOFF OUT OF TULSA. LANDED DFW WITHOUT INCIDENT. NOSE LANDING GEAR INSPECTED WITH NO DEFECTS NOTED. SWUNG GEAR SEVERAL TIMES, COULD NOT DUPLICATE WRITE UP. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050511000472005051100047EA 2005 5 11 SWIA200514886 120050203A5315 BRACKET CNDAIRCL600 CL6002B19 1900309EA FLOORBEAM CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07589SW 7072 CRACKED BRACKET FS 461 RBL 10 BELOW FLOOR. (ITEM FOUND AT C-CHECK INSPECTION.) BRACKET INSTALLED IAW SRM 53-41-43, 51-42-06 AND 51-42-21. 2L72 4F RTA21EA 20050511000512005051100051EA 2005 5 11 SWIA200514890 120050203A5347 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07589SW 7072 LT INBOARD SEAT TRACK HAS AN AREA AT APPROX FS 324 THAT HAS CORROSION, (ITEM FOUND AT C-CHECK INSPECTION.) INSTALLED SEAT TRACK IAW CRJ 200 SRM 51-41-02 PG 1 AND 5. 2L72 4F RTA21EA 20050511000522005051100052CE 2005 5 11 20030831 120050419A7930 B-NUT BEECH 1900 1900D 1154162CE TRQ TRANSMITTER LEAKING A GLBAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM03153GL UE153 AFTER DEPARTURE, ON CLIMB-OUT FLT CREW NOTICED LEFT ENGINE OIL PRESSURE FLUCTUATIONS, FOLLOWED BY LOW LEFT OIL PRESSURE GAUGE INDICATION. SHORTLY AFTER LEFT OIL PRESSURE LOW ANNUNCIATION. FLT CREW DECLARED EMERGENCY AND RETURNED TO AIRPORT WITHOUT INCIDENT. MAINTENANCE TIGHTENED LOOSE LEAKING B-NUT ON TORQUE TRANSMITTER, OP/C LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA24CE 20050511000592005051100059NM 2005 5 11 QXEA200500659 120050412A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - CORROISON IN CENTER OF RIGHT OUTBOARD SEAT TRACK AT STATION X489.0. REPAIRED IAW RD 8-53-1342. 2H72 4T RTA13NM 20050511000702005051100070NM 2005 5 11 QXEA200500645 120050412A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - LEFT OUTBOARD NR 1 SEAT TRACK HAS CORROSION ON TOP OF LUGS AT STATION X264 TO X265. REPAIRED IAW RD8-53-1342. 2H72 4T RTA13NM 20050511000712005051100071EA 2005 5 11 COMA0560268 120050420A5712 RIB CNDAIRCL600 CL6002B19 1900309EA WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01981CA 7163 LEFT AND RIGHT HAND BATTERY RIB CRACKED. REPAIRED IAW REO 601R-57-51-046. 2L72 4F RTA21EA 20050511000742005051100074EA 2005 5 11 COMA0560269 120050420A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01981CA 7163 LEFT HAND 621.00 FRAME CRACKED. REPAIRED IAW REO 601R-53-61-117. 2L72 4F RTA21EA 20050511000812005051100081EU 2005 5 11 MALA050373 120050409A6120 PCU SAAB SF340 340B 7860101EU RIGHT MALFUNCTIONED A MALAE ENGINE SHUTDOWN O OTHER CRCRUISE 1 GL15433XJ 340B433 RT PROP OVERSPEED INFLIGHT. SHUT ENGINE DOWN. INSPECTED PCU FOR LEAKS, GENERAL CONDITION OF PCU & ATTACHING HARDWARE. ALL IN PLACE & INTACT. CHECKED OIL LEVEL OF PGB, FOUND GOOD. CHECKED RIGGING WITH PINS IN PCU AND QUADRANT FOR BOTH POWER AND CONDITION LEVER. ALL CHECKS GOOD. TOOK A/C OUT AND PERFORMED ENGINE RUNS AND PROP RUNS IAW SF AMM 71-00-00. ALL RUNS PASS AGAIN. REMOVED AND REPLACED RT PCU DUE TO FDR DOWNLOAD 0368. SWAPPED BETA TUBE SIDE TO SIDE AND BACK TO ORIGINAL POSITION. ALSO PERFORMED ENGINE RUNS ON LT SIDE FOR BETA TUBE. ALL CHECKS GOOD 0368 AND 7112. REMOVED & REINSTALLED AND RIGGED BETA TUBE ON RT ENGINE 13475 AND 7112. PERFORMED ENGINE & PROP RUNS. ALL CHECKS GOOD. 2L72 4T RTA52EU 20050511000842005051100084EU 2005 5 11 MALA050372 120050417A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15434XJ 340B434 GALLEY SEAT TRACK P/N 7253721-459, IS CORRODED AND HAS BEEN REPLACED IAW SRM 51-40-27. 2L72 4T RTA52EU 20050511000852005051100085EU 2005 5 11 MALA050368 120050302A5280 BOLT BAC 146 AVRO146RJ85A1500097EU LT MLG DOOR CORRODED A MALAK NONE O OTHER NRNOT REPORTED 1 GL15502XJ E2307 LT MLG DOOR UPPER FWD ATTACH BOLT FOUND TO BE CORRODED. BOLTS INSTALLED ON DOOR. 2H74 4F RTA49EU 20050511001052005051100105SO 2005 5 11 C2XA05BT023 120050419A2530 ODOR EMB 145 EMB145LR 3260212SO GALLEY DETECTED A C2XAK NONE B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 SW2713970 145146 CLE LOG SQUAWK ELECTRICAL BURNING SMELL EMINATING FROM COFFEE POT AREA. COFFEE POT BREWER OPS CHECK GOOD IAW EMB145 CMM 25-30-39. 2L72 4T RTT00011AT 20050511001062005051100106SO 2005 5 11 C2XA05BT024 120050420A3350110049 POWER SUPPLY EMB 145 EMB145XR 3260214SO CABIN DISCHARGED A C2XAK NONE L NO TEST UKUNKNOWN 1 SW2717159 145792 IAH LOG SQUAWK ON CABIN PREFLIGHT DISCOVERED LIGHT BULB OUT IN EXIT SIGN ABOVE EXIT ROW. REMOVED AND REPLACED NR 4 BATTERY POWER SUPPLY REF EMB145 MM 33-50-04. OPS CHECK GOOD. 2L72 4F RT 20050511001072005051100107WP 2005 5 11 DHL2005801006 120050421A3260 PLUG DOUG DC8 DC873F 302199FWP MLG LOOSE A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01801DH 46033 RT GEAR DOOR UNSAFE LIGHT ILLUMINATED AFTER GEAR RETRACTION WENT OUT AFTER APPROX 2 MINUTES INTERMITTENT AFTER THAT UNTIL UPLATCH CHECK WHEN IT REMAINED OFF. INSPECTED RT GEAR DOOR SWITCH FOUND DEUTCHE PLUG NOT LATCHED, CLEANED AND RESECURED PLUG PERFORMED DOOR SYSTEM OPS CHECK. NO DEFECTS NOTED ON GROUND PER 32-30-0 DC8MM. 2L74 4F RT4A25 20050511001202005051100120WP 2005 5 11 05FDEA01054 120050420A5240AKC7011 HINGE DOUG MD10 MD1010F 3022112WP ZONE 800 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25370FE 46608 COMPLY WITH EA 8-5240-55471, DOORS-SERVICE-TAILCONE-PATIO DOOR HINGE REPAIR P/N AKC7011 LT. CLOSING ACTION ON 04/15/05. ON N/R S00013. COMPLIED WITH EA 8-5240-55471. 2L73 4F RTA22WE 20050511001232005051100123SO 2005 5 11 SIMA200510104 120050409A3350100865 CHARGER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21619AE 145101 THREE FORWARD EMERGENCY EXIT LIGHTS DO NOT ILLUMINATE WHEN TURNED ON. REMOVED AND REPLACED FORWARD EMERGENCY BATTERY CHARGER. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20050511001262005051100126NE 2005 5 11 2005F00067 220050326A73208201541001 EEC AEROSPATR72 ATR72212A 8680902EU PWA PW120 PW127 NE ENGINE MALFUNCTIONED A TRBAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 SO29499AT 499 499 WHILE DESCENDING AT 5,000 FEET, POWER SET AT APPROXIMATELY 20 PERCENT TQ AND THE NP WAS AROUND 15 PERCENT ENGINE QUIT. ENGINE RE-STARTED AND CONTINUE WITHOUT FURTHER INCIDENT. REPLACED NR 1 ELECTRONIC ENGINE CONTROL UNIT. (M) 2H72 4T4 TRTA53EU E20NE 20050511001302005051100130SO 2005 5 11 SIMA200510119 120050407A532013500436001 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21701MH 145162 SAW - DURING CPCP INSPECTION, FOUND LEFT OMEGA BEAM CORRODED AT CROSS BEAM CORRODED AT CROSS BEAM FRAME 25. MAINTENANCE REMOVED AND REPLACED LEFT OMEGA BEAM IAW EMB SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050511001332005051100133SO 2005 5 11 SIMA200510120 120050407A532013500437003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21701MH 145162 SAW - DURING CPCP INSPECTION, FOUND LEFT OMEGA BEAM CORRODED AT CROSSBEAM FRAME 29. MAINTENANCE REMOVED AND REPLACED LEFT OMEGA BEAM IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050511001372005051100137EA 2005 5 11 A6WA200540149 120050409A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA LT WING CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31417AW 7610 LEFT LOWER WING PLANK IS CORRODED UNDER PANEL 660CB, AFT INBOARD EDGE .400 INCH LONG BY .100 INCH WIDE BY .002 INCH DEEP. (M) 2L72 4F RTA21EA 20050511001392005051100139SO 2005 5 11 SIMA200510103 120050401A1430HL10VAZ RIVET EMB 145 EMB145LR 3260212SO LT WING DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21689EC 14500853 SAW - LIGHTNING STRIKE DAMAGE ON SEVERAL RIVETS ON LEFT WING FUEL CELL. MAINTENANCE REPLACED RIVETS IAW SRM 51-40-02 AND 51-20-04. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20050511001482005051100148EU 2005 5 11 MALA050379 120050421A2120 ODOR SAAB SF340 340B 7860101EU CABIN DETECTED A MALAK NONE B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL15412XJ 340B412 THE CREW REPORTED, A SLIGHT CHEMICAL SMELL RIGHT AFTER DEPARTING CRW. THE SMELL QUICKLY WENT AWAY AND MAINTENANCE WAS PERFORMED LAST NIGHT. 2L72 4T RTA52EU 20050511001542005051100154NM 2005 5 11 XN0A1232 120050423A2425 WARNING LIGHT BOEING727 727227 1384078NM COCKPIT ILLUMINATED A XN0AD RETURN TO BLOCK J WARNING INDICATION UKUNKNOWN 1 GL23793A 20774 ALL THREE LIGHTS ILLUMINATED ON NR 1 GENERATOR. TRANSFERRED TO DMI 5350 IAW ENA MEL 24-1. PLACARDS INSTALLED, SP COMPLIED WITH. 2L73 4F A3WE 20050511001572005051100157NM 2005 5 11 SWAA051155 120050419A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727A, STR 6L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050511001642005051100164SO 2005 5 11 SWIA200514900 120050420A2750276003 CONTROL UNIT EMB 120 EMB120ER 3260203SO ELEVATOR MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM0758733 120197 RIGHT ELEVATOR DOES NOT PASS FFOD CHECK WITH 3A OR 3B SYSTEMS. REPLACED RIGHT INBOARD ELEVATOR PCU IAW CRJ MM 27-33-0. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050511001662005051100166EA 2005 5 11 SWIA200514902 120050420A5610 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07429SW 7518 LEFT WINDSHIELD STARTING TO CRACK IN 3 PLACES. FOUND ON GROUND AFTER RIGHT WINDSHIELD CRACKED/SHATTERED INFLIGHT. REPLACED LEFT WINDSHIELD IAW 56-11-01, P/N OFF NP-139321-9 S/N OFF 01199H3456. 2L72 4F RTA21EA 20050511001682005051100168NM 2005 5 11 AWXA200500476 120050328A5315654581094 FLOORBEAM BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - DURING C-19 CHECK CORROSION WAS FOUND ON FLOORBEAM UPPER CHORD AT BS 312 BETWEEN LBL 8 AND RBL 8, WL 208. MAINTENANCE CUTOUT DAMAGED SECTION OF FLOORBEAM UPPER CHORD AT BS 312 FROM LBL 20 TO RBL 21; FABRICATED A NEW REPLACEMENT SECTION OF UPPER CHORD AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-51, FIG 205. 2L72 4F RTA16WE 20050511001702005051100170NM 2005 5 11 AWXA200500478 120050328A575465C266032 SKIN BOEING737 737301 1384611NM NR 4 SLAT WEDGE DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - DURING C-19 CHECK FOUND THE UPPER AND LOWER SURFACE OF NR 4 SLAT WEDGE DELAMINATED AT SS 59 RT. MAINTENANCE CUTOUT DAMAGE IN NR 4 SLAT WEDGE FROM SS 57 TO SS 61 RT; FABRICATED A CORE FILLER AND DOUBLER; BONDED REPAIR PARTS TO SLAT IAW B737-300 SRM 51-70-10, FIG 22. 2L72 4F RTA16WE 20050511001722005051100172NM 2005 5 11 SWAA051158 120050419A5320BAC1489 SHIM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29333SW 23697 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN SHIM CRACKED AT BS 314, STR 17R. REMOVED AND REPLACED SHIM PER SWA EA. 2L72 4F RTA16WE 20050511001732005051100173NM 2005 5 11 AWXA200500480 120050406A3520417N31382 LINE BOEING737 737301 1384611NM ROW 12 RT OXY BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - DURING C-19 CHECK, FOUND THE OXYGEN GENERATOR HOSE ASSEMBLY BROKEN AT SEAT ROW 12 RT. MAINTENANCE REMOVED AND REPLACED OXYGEN GENERATOR HOSE ASSEMBLY AT SEAT ROW 12 RT IAW BMM 35-22-31. 2L72 4F RTA16WE 20050511001752005051100175NM 2005 5 11 SWAA051160 120050419A57126545445 RIB BOEING737 7373H4 1384600NM LT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29333SW 23697 DURING SCHEDULED 1/4D CHECK, FOUND LT WING RIB CHORD CRACKED AT WBL 135.5, FWD OF AFT SPAR. REPAIRED RIB PER SWA EA. 2L72 4F RTA16WE 20050511001792005051100179NM 2005 5 11 SWAA051163 120050419A3350D71701100 BATTERY PACK BOEING737 7377H4 1384404NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29430WN 33659 DURING SCHEDULED HC1 CHECK, FWD & AFT CABIN EMERGENCY EXIT LIGHTS FAILED TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2L72 4F RTA16WE 20050511001802005051100180NM 2005 5 11 SWAA051164 120050419A33509250071 LIGHT BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29456WN 32463 DURING SCHEDULED MV2 CHECK, FOUND EGRESS LIGHT INOP AT ROW 1. RELAMPED PER MM. 2L72 4F RTA16WE 20050511001862005051100186NM 2005 5 11 SB05049 120050422A3350210310005 FUSE BOEING737 737301 1384611NM EMERGENCY LIGHT BLOWN A USAAK NONE O OTHER ININSP/MAINT 1 EA19577US 23742 PIT - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT OVER THE FORWARD SERVICE DOOR INOPERATIVE. MAINTENANCE REPLACED THE FUSES IN THE EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050511002082005051100208NM 2005 5 11 EIA2005001 120050106A5711 SPAR BOEING747 747212B 1384886NM LT WING CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 LEFT WING AUX SPAR UPPER T-CHORD CRACKED ON INBOARD END. FABBED T-CHORD AND INSTALLED PER ECRA 482-57-116-2. 2L74 4F A20WE 20050511002122005051100212NM 2005 5 11 EIA2005003 120050127A2612 CONTROL MODULE BOEING747 747212B 1384886NM FIRE DETECTION FAULTY A EIAAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 NM09482EV 20713 NR 2A FIRE LOOP FLICKERING IN FLIGHT, TESTED ALL AND NR 2A WOULD ONLY RISE TO 3/4 DEFLECTION, NR 3B DID NOT TEST DEFERRED. REPLACED FIRE DETECTION CONTROL ELECTRONIC MODULE PER MM 26-11-03, OPS CHECKED NR 2A FIRE LOOP AND 3B FIRE LOOP, OPS CHECKED OK. FLIGHT DIVERTED TO JFK FOR MAINTENANCE PURPOSES. 2L74 4F A20WE 20050511002172005051100217NM 2005 5 11 EIA2005068 120050330A5320 TIE CLIP BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 M/D BS 1540 STR-15L TIE CLIP CRACKED. TIE CLIP REPLACED PER SRM 51-10-01. 2L74 4F A20WE 20050511002232005051100223NM 2005 5 11 EIA2005070 120050330A5320 STIFFENER BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 U/D SCUFF PLATE I/B SUPPORT I-BEAM WEB STIFFENER 2EA (BS 400 & BS 410) CRACKED. CRACKED STIFFENERS 2EA REPLACED PER SRM 51-10-01. 2L74 4F A20WE 20050511002352005051100235NM 2005 5 11 EIA2005080 120050330A2780 CONNECTOR BOEING747 747212B 1384886NM L/E FLAP DIRTY A EIAAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 NM09486EV 20888 NR 2 LED LEFT SIDE WILL NOT RETRACT BOTH NORMAL OR ALTERNATE. CLEANED AND SECURED C/P ON L/E FLAP LOGIC BOX. CYCLED FLAPS TWICE UP AND DOWN OPS AND INDICATION NORMAL PER MM 27-88-00 AND 27-88-02. 2L74 4F A20WE 20050511002372005051100237NM 2005 5 11 EIA2005082 120050401A5340 SHEAR TIE BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 M/D BS 1280 S11L-12L SHEAR TIE CRACKED. CRACK SHEAR TIE REPLACED PER SRM 51-10-01. 2L74 4F A20WE 20050511002422005051100242NM 2005 5 11 ANCF200400048 120050420A2410 CSD DOUG MD80 MD83 3023681NM RIGHT FAILED W ANCFA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO23632CT 49632 DURING RT ENG START, RT GEN FREQ 396 CPS & GEN CAME ON LINE AT 50 PERCENT N2. REPORTED TO TECH. DURING TAKEOFF ROLL, RT GEN TRIPPED, RESET UNSUCCESFULL. RT CSD OIL TEMP BEGAN RISING UNTIL OFF SCALE, WITH GEN OFF, FOLLOWED CHKLST, CSD DISCONNECTED. THROUGH FL 280, APU OIL TEMP HIGH ANNUNCIATION, APU SHUTDOWN. RT CSD CHIP DETECTOR FOUND NORMAL, FLUSH & REFILL LEVEL IAW AMM. ENG RUN OK IAW AMM. APU OIL LEVEL CHKD & FOUND LOW, OIL ADD IAW AMM & OVERTEMP SWITCH CONNECTORS CLEANED. TESTED OK. AFTER ENG START, RT CSD TEMP ROSE OUT OF RANGE. CSD DISCONNECTED. THOUGH FL 310 APU OIL TEMP HIGH ANNUNCIATION. APU SHUTDOWN. RT CSD REPLACED IAW AMM, RT GEN REPLACED IAW AMM, TEST SATISFACTORY. 2L72 4F RT 20050511002572005051100257EU 2005 5 11 05FDEA01062 120050422A7120 MOUNT AIRBUS310 A310 EU NR 2 ENGINE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 NR 2 ENGINE FWD MOUNT FITTING HAS PITTED CORROSION ON BOLT HOLES, SPIGOT HOLE, LOWER AND UPPER MATING SURFACE. REMOVED CORROSION IN ALL AREAS LISTED. FABBED AND INSTALLED 3 EA BUSHINGS AND REPROTECTED SURFACES IAW A310 SRM 54-51-81 AND FEDEX EA 6-5450-87748. 2L72 4F RTA35EU 20050511002712005051100271EU 2005 5 11 05FDEA01073 120050422A5330 SKIN AIRBUS310 A310 EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 IN A/C BAY, FROM FRAME 45 TO FRAME 46 AND STR 46R TO 41R AREA HAS NUMEROUS SPOTS OF CORROSION ON SKIN. REMOVED CORROSION PER A310 SRM 51-74-10. FOUND TO BE WITHIN LIMITS PER A310 SRM 53- 15-12. INSTALLED FASTENERS PER A310-SRM 51-40-21. RESTORED SURFACE PROTECTION PER A310-SRM 51-75-10. 2L72 4F RTA35EU 20050511002732005051100273EU 2005 5 11 05FDEA01075 120050422A5330 SKIN AIRBUS310 A310 EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 IN AC BAY, FROM FRAME 39 TO 40 AND FROM STR 55-51 RT HAS AREAS OF CORROSION ON SKIN. REMOVED CORROSION PER SRM 51-74-10. FOUND ALL AREAS TO BE WITHIN LIMITS PER EA6-5310-87784. C/W EA 6-5310-87784. INSTALLED FASTENERS PER A310 SRM 51-40-21. RESTORED SURFACE PROTECTION PER A310 SRM 51-75-10. 2L72 4F RTA35EU 20050511002752005051100275EU 2005 5 11 05FDEA01077 120050422A5313 STRINGER AIRBUS310 A310203 3930313EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 IN ACM BAY FR 40/41 BETWEEN STR 44L AND STR 45L, SKIN HAS AREAS OF CORROSION. REMOVED CORROSION PER A310 SRM 51-74-10. C/W EA 6-5310-87784. FOUND ALL AREAS TO BE WITHIN LIMITS PER EA 6-5310-87784 AND A310 SRM 53-15-12. INSTALLED FASTENERS PER A310 SRM 51-40-21. RESTORED SURFACE PROTECTION PER A310 SRM 51-75-10, REF FEDEX EA 6-5310-88751. 2L72 4F RTA35EU 20050511002772005051100277EU 2005 5 11 05FDEA01079 120050422A5730 SKIN AIRBUS310 A310203 3930313EU LT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 L/WING, 550JB HAS ONE EACH ELONGATED HOLE. COMPLIED WITH EA 6-5710-87121. 2L72 4F RTA35EU 20050511002792005051100279EU 2005 5 11 05FDEA01081 120050422A5330 SKIN AIRBUS310 A310203 3930313EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 IN ACM BAY STR 50R BETWEEN FR43 TO FR47 HAS AREAS OF CORROSION. REMOVED CORROSION PER A310 SRM 57-74-10. C/W EA 6-5310-87784. FOUND ALL AREAS TO BE WITHIN LIMITS PER EA 6-5310-87784 AND A310 SRM 53-10-00. INSTALLED FASTENERS PER A310 SRM 51-40-21. RESTORED SURFACE PROTECTION PER A310 SRM 51-75-10. 2L72 4F RTA35EU 20050511002812005051100281EU 2005 5 11 05FDEA01083 120050422A5330 SKIN AIRBUS310 A310 EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 IN A/C BAY, FROM FRAME 46 TO 47, STRINGER 46R TO 43R HAS SEVERAL AREAS OF CORROSION. REMOVED CORROSION PER A310 SRM 51-74-10. FOUND ALL AREAS TO BE WITHIN LIMITS IN AREA STR 44R BETWEEN FR 46 AND 47. C/W EA 6-5310-87784. INSTALLED FASTENERS PER A310 SRM 51-40-21. RESTORED SURFACE PROTECTION PER A310 SRM 51-75-10. 2L72 4F RTA35EU 20050511002832005051100283EU 2005 5 11 05FDEA01085 120050422A5347A5378193620200 SEAT TRACK AIRBUS310 A310203 3930313EU ZONE 200 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 CLS ADAPTER AT FR 37 TRACK L3 IS GOUGED. REMOVED AND REPLACED CLS ADAPTER AT FR 37 TRACK L4, L3 MDC IAW A310-200 SRM 53-10- 16. 2L72 4F RTA35EU 20050511002852005051100285EU 2005 5 11 05FDEA01087 120050422A5330 SKIN AIRBUS310 A310203 3930313EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 IN ACM BAY FR 43 TO FR 44 BETWEEN STR 39L AND 40L SKIN HAS AREAS OF CORROSION. REMOVED CORROSION IAW A310 SRM 51-74-10. WITHIN LIMITS, FLAP PEENED IAW A310 SRM 51-29-00 AND RESTORED PROTECTIVE COATING IAW A310 SRM 51-75-10 ON SKIN FR 43 TO FR 44 BETWEEN STR 39L AND 40L. 2L72 4F RTA35EU 20050511002922005051100292EU 2005 5 11 05FDEA01094 120050422A5330 SKIN AIRBUS310 A310203 3930313EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 AFT CARGO COMPT, ABOUT STGR 57 FWD SIDE OF FR 59 AROUND BASE OF RADIO ALT. TRANSMISSION ANTENNA HAS AREA OF CORROSION. REMOVED FASTENERS AROUND BASE OF ANTENNA IAW A310-200 SRM 51-40-21. REMOVED LIGHT CORROSION IAW A310-200 SRM 51-74-10. INSTALLED FASTENERS IAW A310-200 SRM 51-40-21. TREATED, PRIMED, AND TOPCOATED AREA IAW A310-200 SRM 51-21-10, AND APPLIED SEALING IAW A310-200 AMM 34-42-11-4-01. 2L72 4F RTA35EU 20050511002942005051100294EU 2005 5 11 05FDEA01096 120050422A5313 STRINGER AIRBUS310 A310203 3930313EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 AFT PIT FRAME 67 STR 50L STRINGER HAS 2SQ INCH OF CORROSION. STR 50L FR 67 AFT, SECTION OF STRINGER REMOVED AND REPLACED. 2L72 4F RTA35EU 20050511002962005051100296EU 2005 5 11 05FDEA01098 120050422A5330 SKIN AIRBUS310 A310203 3930313EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 IN ACM BAY SKIN BETWEEN STR 38R TO 39R AND FR44 TO FR45 HAS AREAS OF CORROSION. REMOVED CORROSION IAW A310-200 SRM 51-74-10. FOUND TO BE WITHIN LIMITS IAW A310-200 SRM 53-15-12. FLAP PEENED IAW A310-200 SRM 51-29-00. TREATED AND PRIMED AND TOPCOATED IAW A310-200 SRM 51-23-10. 2L72 4F RTA35EU 20050511002982005051100298EU 2005 5 11 05FDEA01100 120050422A5313A54811373201000 STRINGER AIRBUS310 A310203 3930313EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 IN A/C COMPARTMENT STRINGER 44L FROM FRAME 39 TO 47 HAS AREAS OF CORROSION ON STRINGER AND AROUND FASTENERS. REMOVED FASTENERS IAW A310-200 SRM 51-40-21, REMOVED CORROSION IAW A310-200 SRM 51-74-10, FOUND SECTION OUT OF LIMITS IAW A310-200 SRM 53-10-00, CUTOUT DAMAGED SECTION, FAB REPAIR PARTS, AND INSTALLED REPAIR IAW A310-200 SRM 51-40-21 AND EA 6-5310-87227. REINSTALLED FASTENERS IAW A310-200 SRM 51-40-21. 2L72 4F RTA35EU 20050511003002005051100300NM 2005 5 11 05FDEA01102 120050422A5347FXSRM53102 SEAT TRACK BOEING727 727233 138408ANM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25254FE 20936 SEAT TRACK STA 244 TO 480 RBL 45, HAS EXISTING BLEND REPAIRS AND AN EXISTING SPLICE REPAIR AND REQUIRES REPLACEMENT PER 7-5340-7-5002. REMOVED SEAT TRACK IAW SRM 51-30-2. FAB'D SEAT TRACK ON TRAVELER NR T5/510065. LOCATED AND DRILLED IAW SRM 53-10-5 FIG 3. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED SEAT TRACK IAW SRM 51-30-2. 2L73 4F RTA3WE 20050511003022005051100302EU 2005 5 11 05FDEA01108 120050424A5330 SKIN AIRBUS310 A310203 3930313EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 CORROSION ON SKIN IN A/C BAY BETWEEN FRAMES 45 AND 46, BETWEEN VAPOR BARRIER AND PACK CUTOUT. REMOVED CORROSION PER A310 SRM 51-74-10. C/W EA 6-5310-87784. FOUND ALL AREAS TO BE WITHIN LIMITS PER EA 6-5310-87784 AND A310 SRM 53-15-12. INSTALLED FASTENERS PER A310 SRM 51-40-21. RESTORED SURFACE PROTECTION PER A310 SRM 51-75-10. 2L72 4F RTA35EU 20050511003042005051100304NM 2005 5 11 EIA2005086 120050331A3310 CIRCUIT CARD BOEING747 747212B 1384886NM COCKPIT FAULTY A EIAAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 NM09485EV 20712 ELECTRICAL SMELL COMING FROM AREA OF MASTER DIM AND TEST BOX UNDER F/E PANEL. FOUND DIMMER TYPE II CARD A6 BAD. DIM FUNCTION INOP. REPLACED CARD PER B747 MM 33-11-01, OPS CHECKED OK. 2L74 4F A20WE 20050511003062005051100306NM 2005 5 11 EIA2005044 120050329A5311 FRAME BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 AFT OF BULK CARGO COMPT RT 2200 FRAME IN BETWEEN STR 42 & STR 44 FOUND CRACKED. FRAME REPLACED PER SB 747-53-2302. 2L74 4F A20WE 20050511003162005051100316NM 2005 5 11 EIA2005053 120050329A5313 STRINGER BOEING747 747212B 1384886NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 M/D STA 2020-2021 STR 14 CORROSION FOUND. STRINGER REPAIRED PER SRM 53-10-03 FIG 2. 2L74 4F A20WE 20050511003192005051100319NM 2005 5 11 EIA2005056 120050330A5320 ATTACH BRACKET BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 M/D BS 854 FRAME AT STR 13R ATTACHED BRACKET CRACKED. BRACKET REPLACED PER SRM 51-10-01. 2L74 4F A20WE 20050511003252005051100325NM 2005 5 11 EIA2005062 120050330A5330 SKIN BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 BS 400 NOSE GEAR W/W RIGHT AFT CORNER FOUND CRACK AT SPLICE PLATE AND SKIN AT BS 392 STR 44R CRACKED. SPLICE PLATE AND SKIN REPAIRED PER S/B 747-53-2305. 2L74 4F A20WE 20050511003262005051100326NM 2005 5 11 EIA2005063 120050330A5320 FITTING BOEING747 747212B 1384886NM RT BODY LG WW CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 RIGHT BODY LANDING GEAR W/W INBOARD SIDE WALL STA 1416 VERTICAL POST UPPER END FITTING FOUND CRACKED. END FITTING REPLACED PER SRM 51-10-01 WITH P/N 65B12583-1. 2L74 4F A20WE 20050511003272005051100327NM 2005 5 11 EIA2005064 120050330A5320 TIE CLIP BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 M/D BS 960 STRINGER S12L TIE CLIP FOUND CRACKED. TIE CLIP REPLACED PER SRM 51-10-01. 2L74 4F A20WE 20050511003282005051100328NM 2005 5 11 EIA2005065 120050330A5320 INTERCOSTAL BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 M/D BS 320 AT S-26R INTERCOSTAL WEB CRACKED. INTERCOSTAL WEB TRIMMED OFF AND REPAIRED PER SRM 51-40-03 FIG 1. 2L74 4F A20WE 20050511003292005051100329NM 2005 5 11 EIA2005066 120050330A5340 SHEAR TIE BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 CABIN BS 1120 RT STR 5R TO 6R SHEAR TIE CRACKED. SHEAR TIE REPLACED PER SRM 51-10-01. 2L74 4F A20WE 20050511003302005051100330NM 2005 5 11 EIA2005067 120050330A5320 TIE CLIP BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 CABIN BS 1100 STR 10R TIE CLIP FOUND CRACKED. REPLACED CLIP PER SRM 51-10-01. 2L74 4F A20WE 20050511003322005051100332NM 2005 5 11 SWAA051180 120050421A573065C29255 SKIN BOEING737 7373H4 1384600NM RT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND RIGHT WING UPPER SKIN CRACKED AT RSS 238. REPAIRED SKIN PER PAE ER. 2L72 4F RTA16WE 20050511003362005051100336NM 2005 5 11 SWAA051184 120050421A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29315SW 23337 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 350, STR 15L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050511003372005051100337NM 2005 5 11 SWAA051185 120050421A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29315SW 23337 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 490, STR 17R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050511003382005051100338 2005 5 11 SWAA051186 420050421A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29315SW 23337 DURING SCHEDULED C1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050511003392005051100339NM 2005 5 11 SWAA051187 120050421A32606554791 SENSOR BOEING737 7373H4 1384600NM NLG FAULTY A SWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW29322SW 23343 AIR TURNBACK. NLG WOULD NOT INDICATE RETRACT. RECYCLED GEAR & STILL HAD RED & GREEN LIGHTS INDICATING. REMOVED AND REPLACED S845 SENSOR PER MM. 2L72 4F RTA16WE 20050511003402005051100340NM 2005 5 11 SWAA051188 120050421A5743654610817 FITTING BOEING737 7373H4 1384600NM LT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29333SW 23697 DURING SCHEDULED 1/4D CHECK, FOUND LT WING MLG HYDRAULIC ACTUATOR ATTACH FITTING CRACKED AT WS 134.5. REMOVED AND REPLACED FITTING PER SRM. 2L72 4F RTA16WE 20050511003432005051100343NM 2005 5 11 SWAA051191 120050421A53126517582 BULKHEAD BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29679AA 23291 DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEB CRACKED AT BS 178 BULKHEAD, RBL 17.1, WL 184. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050511003452005051100345NM 2005 5 11 EIA2005010 120050221A5330 DOUBLER BOEING747 747273C 1384896NM FUSELAGE DAMAGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09471EV 20651 REMOVED EXTERNAL DOUBLER REPAIR NR 3 EXTERNAL FUSELAGE BS 2144-2164.5, STR 46R-48R. REMOVED EXTERNAL DOUBLER, FABRICATED REPAIR DOUBLERS AND FILLERS. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER AND FILLER PER B747 SRM 53-30-03 FIG 19. 2L74 4F A20WE 20050511003472005051100347NM 2005 5 11 EIA2005008 120050221A5311 FRAME BOEING747 747273C 1384896NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09471EV 20651 CRACK INDICATION IN LWR TWO FASTENER HOLES IN RT C-3 FRAME UPPER CLOSURE FITTING. REPAIRED RT C-3 FRAME UPPER CLOSURE FITTING PER ECRA 471-53-243-2. 2L74 4F A20WE 20050511003482005051100348NM 2005 5 11 EIA2005012 120050221A5311 STRAP BOEING747 747273C 1384896NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09471EV 20651 CRACK IN FRAME INNER STRAP AT STA 2231 LT FROM STR 25 TO STR 26 AT L-5 DOOR FWD FRAME. REMOVED STRUCTURE AS REQUIRED. FABRICATED REQUIRED PARTS AND INSTALLED FABRICATED STRAPS ALL PER ECRA 471-53-236-2P AND B747 SRM 53-10-04 PG 689-694. 2L74 4F A20WE 20050511003502005051100350NM 2005 5 11 EIA2005014 120050222A5311 FRAME BOEING747 747273C 1384896NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09471EV 20651 MAIN CABIN INTERIOR, RT MAIN FRAME CRACK AT BS 360, BETWEEN STR 14 & 15. REMOVED AND REPLACED MAIN FRAME AT STA 360 RT MAIN CABIN PER ECRA 471-53-240-2 BETWEEN STR 13A TO 23 B747 SRM 51-30-02 PAGES 2, 3, 8 & 9. 2L74 4F A20WE 20050511003512005051100351NM 2005 5 11 EIA2005015 120050222A5311 FRAME BOEING747 747273C 1384896NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09471EV 20651 CRACK INDICATION NOTED IN 4 EA FASTENER HOLES AT STA 800, STR 16L, FWD INNER FRAME CHORD. REMOVED EXISTING REPAIR PARTS, FABRICATED NEW STRAPS AND INSTALLED REQUIRED EXISTING AND FABRICATED STRAPS PER ECRA 471-53-230-2. 2L74 4F A20WE 20050511003522005051100352NM 2005 5 11 EIA2005016 120050222A5313 STRINGER BOEING747 747273C 1384896NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09471EV 20651 BETWEEN STA 300-320 STR 34 RT CRACK AT UPPER SURFACE. REMOVED DAMAGED SECTION BETWEEN STA 280-320 PER B747 SRM 53-10-03 PG 8-10. FABRICATED NEW STRINGER PER B747 SRM 53-10-03 PG 8, 51-30-02, 51-10-02 AND BSOPM 20-41-02 PG 7-9 NDT FOUND NO CRACKS. INSTALLED STRINGER AND FILLER DOUBLER PER B747 SRM 51-40-02 PG 4-5. 2L74 4F A20WE 20050512000022005051200002 2005 5 12 YENA200527 420050409A233050401100001 DISPLAY AIRBUS320 A320232 3930326EU CABIN OVERHEATED A YENAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15550JB 1891 CREW SMELLED BURNING PLASTIC ROWS 18-20 RIGHT SIDE, LIVETV TO STANDBY, SMELL STOPPED. LIVETV ON SMELL RETURNED. TURNED LIVETV MASTER OFF. DEBRIEFED CREW, CREW MENTIONED ELECTRICAL ODOR FROM VDU AT 18E. VERIFIED ODOR AT 18E VDU AND PERFORMED INFO NOTICE 2004-T023TR. REMOVED AND REPLACED VDU AT 18E IAW LTV MM 23-39-00. OPERATIONS CHECK GOOD, NO ODOR NOTED IN CABIN AT THIS TIME. TEARDOWN REPORT INDICATES INDUCTOR AT LOCATION L1 & L2 OVERHEATED. 2L72 4F RTA28NM 20050512000032005051200003NM 2005 5 12 05FDEA01103 120050423A5712ARB292013 RIB DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 LT WING LEADING EDGE CAVITY BETWEEN SLAT TRACK NR 16 AND 17, FOUND RIB FLANGE CRACKED. FABRICATED AS PER DRAWING NR ARB2920. RIB REMOVED AND REPLACED AS PER SRM 51-35-01 VOLUME II. 2L73 4F RTA22WE 20050512000102005051200010CE 2005 5 12 DXTA200500696 120050425A3240 BRAKE CESSNA500 560CESSNA 2076750CE MLG WEAK E DXTAD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07361QS 5600361 BRAKES SOFT ON RIGHT SIDE, NEED TO GO ALMOST TO THE FLOOR BEFORE ANY HINT OF PRESSURE IS FELT. CHECKED BRAKE PEDAL FEEL ON PILOT AND COPILOT SIDE STATICALLY AND WITH POWER, FEELS NORMAL. CHECKED SYSTEM FOR SERVCIE, ALL CHECKS GOOD. INSPECTED THOSE VISUAL BRAKE COMPONENTS FOR LEAKS- NONE FOUND. SERVICED AND BLED BRAKES IAW 560 MM 32-42-00. PRESSURIZED BRAKE SYSTEM FOR 5 MINUTES- NO LEAKS NOTED 2L72 4F RTA22CE 20050512000142005051200014EA 2005 5 12 VTZA200500067 120050501A3244 TIRE CNDAIRCL600 CL6002B19 1900309EA LT MLG SEPARATED A VTZAA UNSCHED LANDING E VIBRATION/BUFFET TOTAKEOFF 1 EA27648BR 7406 BANGING NOISE ON LT SIDE OF AC AFTER ROTATION, NR 2 MAIN TIRE TREAD SEPARATED CAUSING FLAP AND FUSELAGE DAMAGE. REMOVED AND REPLACED NR 2 MLG TIRE REF AMM CH 32-41-01. INSPECTED PRESSURE BEFORE REMOVAL WAS 170PSI. C/W BOROSCOPE OF THE LT ENGINE DUE TO POSSIBLE FOD DAMAGE. NO DEFECTS FOUND. INSPECTED FAN BLADES FOR POSSIBLE DAMAGES NO DEFECTS NOTED. REMOVED AND REPLACED NR 1 MAIN WHEEL ASSY. COMPLIED WITH TIRE BURST INSPECTION. 2L72 4F RTA21EA 20050512000192005051200019SO 2005 5 12 C2XA05TY036 120050425A551014520736004 SUPPORT EMB 145 EMB145LR 3260212SO BEARING WORN A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714959 145091 TYS A/C WAS IN FOR A 5A INSPECTION AND IT WAS OBSERVED THAT THE RIGHT SPHERICAL HOUSING SHOWED SIGNS OF WEAR. MAINTENANCE REAMED THE SPHERICAL HOUSING AND REPLACED THE BEARINGS. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF THE 5A CHECK. 2L72 4T RTT00011AT 20050512000202005051200020EU 2005 5 12 DHL2005363002 120050427A7100 ENGINE AIRBUS300 A300B4203 3930306EU NR 2 FAILED A DHLAJBAEDUMP FUEL EMER. DESCENT UNSCHED LANDING ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SO01363DH 85 AT VR ENGINE NR 2 FAILED. COMPLETED APPROPRIATE ABNORMAL PROCEDURES. DUMP 18,800 LBS OF FUEL. EGT TEMP EXCEEDED 7 SECONDS AT 940. PERFORM BOROSCOPE INSPECTION ON NR 2 ENG FOR EGT OVERTEMP AND COMPRESSOR STALL ON TAKEOFF. PERFORMED BORO INSP PER MM 72-00-00 PG 604 HIGH EGT BORO INSP HPT 1. NO DEFECTS. NORMAL EROSION WEAR. PERFORMED BORO INSP PER MM 72-00-00. 2L72 4F RTA35EU 20050509000692005050900069NM 2005 5 9 AWXA200500463 120050404A575465C26601179 SKIN BOEING737 73733A 1384673NM NR 1 SLAT WEDGE DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCN - MAJOR REPAIR - DURING C-19 CHECK THE NR 1 SLAT WEDGE WAS FOUND DELAMINATED ON THE UPPER & LOWER SURFACE AT SLAT STA 348 LT. MAINTENANCE REMOVED DAMAGE IN UPPER AND LOWER SURFACE SKIN OF NR 1 SLAT WEDGE FROM SS 343 TO SS 350 LT; FABRICATED A CORE FILLER AND DOUBLER; BONDED REPAIR PARTS TO SLAT IAW 51-70-10 FIG 16. 2L72 4F RTA16WE 20050509000762005050900076EA 2005 5 9 QXEA200500583 120050317A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE INTERIOR LEFT OUTBOARD SEAT RAIL AT STATION X615 HAS PITTING CORROSION ON MOST INBOARD SURFACE. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01, PARAGRAPH 3E AND CRM 51-21-16, CODE A044. 2L72 4F RTA21EA 20050509000802005050900080EA 2005 5 9 QXEA200500587 120050317A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE INTERIOR LEFT OUTBOARD SEAT RAIL AT STATION X810 HAS PITTING CORROSION ON MOST INBOARD SURFACE. REPAIRED IAW CRJ 7--/9-- SRM 51-21-06-001-001-A01 AND REO 670-53-00-013. 2L72 4F RTA21EA 20050509000842005050900084NM 2005 5 9 UIEA200500045 120050331A5210 STRUCTURE BOEING747 7472D7B 1384803NM GE CF6 CF650E2 30018NE PAX DOOR CRACKED A UIEAO OTHER O OTHER CRCRUISE 1 EA15522MC 21783 LOUD AIR LEAK FROM AROUND DOOR ON MAIN CARGO DECK. AREA BY PALLET POSITION LR-MR. AFT OBSERVATION WINDOW DOOR. REMOVED AND INSTALLED NR 4 MAIN ENTRY DOOR IAW AMM. LEAK CHECK IAW AMM. NO LEAK NOTED. CABIN PRESSURIZATION LEAKAGE TEST ACCOMPLISHED IAW MM. (K) 2L74 4F4 FRTA20WE E23EA 20050509000852005050900085NM 2005 5 9 HANN0500036 120050407A3232 ACTUATOR DHAV DHC8 DHC8102 2809003NM NLG DOOR OUT OF RIG A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07937HA 148 CREW REPORTED NOSE GEAR DOOR DROPPED OPEN AFTER GEAR RETRACTION. RIGGED NOSE GEAR DOOR ACTUATOR AND ADJUSTED DOOR PROX SWITCH. 2H72 4T RTA13NM 20050509000882005050900088 2005 5 9 HNAA0500039 420050415A3442071131900 ANTENNA DHAV DHC8 DHC8102 2809003NM WX RADAR SYS FAILED A HNAAO OTHER J WARNING INDICATION NRNOT REPORTED 1 EA07933HA4236521953 134 RADAR ANTENNA FAULT. REMOVED AND REPLACED RADAR RT, OPS CHECK GOOD. 2H72 4T RTA13NM 20050509000952005050900095EU 2005 5 9 USAA050126 120050111A5321F5367231300000 FLOOR PANEL AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW 0342 FOUND FLOOR PANEL CORRODED 17.5 INCHES LONG BY .50 INCHES WIDE BY .093 INCH DEEP, BETWEEN FRAME 73-76 PLUS 2820 -Z240. REPLACED WITH NEW PART PER SRM 51-74-00. CORROSION LEVEL 2, TASK NR J7-270-53100-005. (M) 2L72 4F RTA46NM 20050509000972005050900097EU 2005 5 9 USAA050246 120050203A5347F53331132520000 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19671UW22760 0323 BFM - FOUND SEAT TRACK CORRODED .34 INCH DEEP BY 1.75 INCH BY .5 INCH WIDE/.050 INCH DEEP BY 1.5 INCH LONG BY .5 INCH, FRAME 47-53.2, Y-450 MAIN CABIN FLOOR. REMOVED AND REPLACED SEAT TRACK PER SRM 53-31-15 FIG 101, 51-42-11. (M) 2L72 4F RTA46NM 20050509000982005050900098EU 2005 5 9 USAA050240 120050206A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19671UW 0323 BFM - FOUND TRACK GOUGED 1.5 INCH BY 1 INCH BY .25 INCH DEEP, FRAME 53.2, Y1959, MAIN CABIN FLOOR. FABRICATED SPLICES AND NEW SECTION OF SEAT TRACK, INSTALLED PARTS PER SRM 53-31-14 FIG 101 SHT 6. 2L72 4F RTA46NM 20050509001022005050900102EU 2005 5 9 USAA050122 120050112A5321F5367223700100 FLOORBOARD AIRBUS330 A330323 3930335EU FUSELAGE DEBONDED A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW21927 0342 BFM - FOUND FLOORBOARD DISBOND .75 INCH BY 3 INCH AREA, MAIN CABIN FLOORBOARD 262 SG. FABRICATED NEW FLOORBOARD PER SRM 53-02-00. (M) 2L72 4F RTA46NM 20050509001302005050900130NE 2005 5 9 ALG2005F00017 120050408A5246 DOOR SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30P 03013GL OIL FILLER SEPARATED A ALGAA UNSCHED LANDING D INFLIGHT SEPARATION HOHOVERING 1 SW03522AL 760236 PICKED AIRCRAFT UP TO A HOVER ON PAD B1 TO REPOSITION . PAD B3 RADIOED THAT THE OIL FILLER COVER HAD SEPARATED. RADIO OPERATOR THEN CALLED ADVISING RETURN TO PAD B1. RETURNED TO PAD B1 AND SHUTDOWN THE AIRCRAFT. MAINTENANCE INSPECTED MAIN ROTOR BLADES, TAIL ROTOR BLADES AND ENGINE INTAKE AREA FOR DAMAGE AND FOD, NO DEFECTS NOTED. REATTACHED OIL FILLER COVER AS REQUIRED, RETURNED AIRCRAFT TO SERVICE. (K) 1G72 3U3 U H1NE E1GL 20050509001312005050900131SW 2005 5 9 ALG2005F00018 120050330A6320 TRANSMISSION BELL 407 407 1182206SW ALLSN 250C 250C47B GL MAIN ROTOR MAKING METAL A ALGAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW03403AL 53478 ON TAKEOFF, TRANSMISSION CHIP LIGHT ILLUMINATED, PILOT RETURNED TO THE PLATFORM. SHUTDOWN AND NOTIFIED MAINTENANCE. REMOVED UPPER CHIP PLUG AND FOUND 3 SMALL SLIVERS. CLEANED THE PLUG, REINSTALLED CHIP PLUG AND PERFORMED A 30 MINUTE PENALTY RUN AND LEAK CHECKED. APPROPRIATE LOG BOOK ENTRIES WERE MADE. AC WAS RETURNED, IAW MAINTENANCE REQUEST. UPON LANDING, THE MECHANIC REMOVED AND REPLACED THE TRANSMISSION AND THE MAST ASSY AND THE AIRCRAFT WAS RETURNED TO SERVICE. (K) 1G71 3U3 UO H2SW E1GL 20050509001342005050900134SW 2005 5 9 ALG2005F00020 120050310A6340214040806003 PRESSURE SWITCH BELL 407 407 1182206SW ALLSN 250C 250C47B GL XMSN OIL PRESS INOPERATIVE A ALGAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW03436AL 53069 FOLLOWING LIFT OFF, AND AT HOVER TO FLYWAY THE TRANSMISSION PRESSURE LIGHT CAME ON AND STAYED ON. RETURNED TO AIRCRAFT TO PAD AND CALLED MAINTENANCE. MAINTENANCE REPLACED THE TRANSMISSION OIL PRESSURE SWITCH AND COMPLIED WITH GROUND RUN, OPS AND LEAK CHECK, NO OTHER DEFECTS NOTED. (K) 1G71 3U3 UO H2SW E1GL 20050509001422005050900142NM 2005 5 9 SWAA051112 120050414A534065C27314 STRINGER CLIP BOEING737 7373L9 1384470NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050509001462005050900146NM 2005 5 9 SWAA051116 120050414A57536546435273 SKIN BOEING737 7373A4 1384585NM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29678AA 23290 DURING SCHEDULED C1 CHECK, FOUND LT WING T/E OUTBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2L72 4F RTA16WE 20050509001562005050900156NM 2005 5 9 SWAA051126 120050414A53306545775 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 867, STR 25R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050509001672005050900167NM 2005 5 9 SWAA051142 120050417A52306547952 SEAL BOEING737 7373A4 1384585NM AFT CARGO DOOR TORN A SWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW29677AA 23289 DIVERSION AT 37,000 FT, ALTIMETER HORN SOUNDED. NO AUTO-FAIL/STBY LIGHTS INDICATED. WENT TO MANUAL & DIVERTED TO BWI. REMOVED AND REPLACE AFT CARGO DOOR SEAL, APU AFT PNEUMATIC DUCT BOOT & LT A/C PACK FLEX BOOT FWD OF WATER SEPARATOR PER MM. 2L72 4F RTA16WE 20050509001732005050900173NM 2005 5 9 SWAA051129 120050417A53226546529 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME SHEAR TIE CRACKED AT BS 500D, STR 16L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050510000142005051000014EA 2005 5 10 QXEA200500605 120050317A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - FUSELAGE INTERIOR, RIGHTHAND INBOARD SEAT RAIL AT STATION X540 HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW CRJ700/900 SRM 51-21-06-001-001-A01, PARAGRAPH 3E, REO 670-53-00-013 AND SRM 51-21-16, CODE A044. 2L72 4F RTA21EA 20050510000222005051000022NM 2005 5 10 CALA0500112 120050418A7830315A28001 ACTUATOR BOEING737 737724 13844BYNM THRUST REVERSER FAILED A CALAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 SW2723721 28940 UPON LANDING AND APPLYING REVERSE THRUST, THE CABIN FILLED WITH SMOKE. EMERGENCY DECLARED, NO EVACUATION. REPLACED INBOARD THRUST REVERSER LOWER ACTUATOR PER AMM 78-31-03. 2L72 4F RTA16WE 20050510000252005051000025EA 2005 5 10 VTZA200500064 120050418A5320601R3501163 PLATE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27658BR 7500 CARGO LANDING PLATE IS CRACKED AT RIVETS ATTACHING IT TO THE INTERCOSTALS .25 INCH AT FS 589.0. 2L72 4F RTA21EA 20050510000332005051000033EA 2005 5 10 VTZA200500058 120050416A5320601R311719 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27658BR 7500 INTERCOSTAL CRACKED AT .250 INCH IN LENGTH ON RIGHT SIDE AT FS 484 BETWEEN RBL 36.00. 2L72 4F RTA21EA 20050510000492005051000049NM 2005 5 10 2005UALA00325 120050409A5230 DOOR FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CARGO DOOR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29308UA 23669 AFT CARGO DOOR FWD BS 795 FRAME WAS FOUND CRACKED IN LINE WITH 2ND DOOR STOP FROM TOP. INSTALLED U-CHANNEL REPAIR WITH RADIUS BLOCKS AT UPPER AND LOWER FLANGES. 2L72 4F4 FRTA16WE E2GL 20050510000532005051000053NM 2005 5 10 2005UALA00333 120050412A2612 WARNING LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CARGO FIRE ILLUMINATED A UALAO OTHER J WARNING INDICATION DEDESCENT 1 WP29173UA 24380 CREW OBSERVED FWD CARGO FIRE WARNING ACTIVATE. CAUSE OF PROBLEM IS UNDETERMINED. SEVERAL ITEMS WERE ACCOMPLISHED TO FIX PROBLEM INCLUDING CH1924 ADRRESSING THE OUTGASSING OF CERTAIN PRODUCE ITEMS THAT ACCORDING TO THE EXPERTS MAY TRIGGER THE FIRE DETECTION SYSTEM. AS PRECAUTION FORWARD CARGO FIRE DETECTION CARD A31 WAS REPLACED. 2L74 4F4 FRTA20WE E24NE 20050510000552005051000055NM 2005 5 10 2005UALA00341 120050411A5753 ATTACH ANGLE BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE TE FLAP HINGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29665UA 29237 RT WING INBOARD FLAP, INBOARD HINGE SUPPORT ATTACH ANGLE CRACKED OUTBOARD SIDE. THE SUBJECT HINGE SUPPORT FITTING CRACKED DUE TO FATIGUE LOAD. THE CRACKED AREA WAS REPAIRED PER 767-300 SRM 57-53-02. 2L72 4F4 FRTA1NM E24NE 20050510000662005051000066EU 2005 5 10 USAA050141 120050110A5347F3311325200 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW 0342 BFM - FOUND SEAT TRACK CORRODED, 1.5 INCHES LONG BY 1.1 INCH WIDE BY .048 INCH DEEP, MAIN CABIN FLOOR -450, FRAME 47-53. REMOVED AND REPLACED SEAT TRACK PER SRM 53-31-15, FIG 101. (M) 2L72 4F RTA46NM 20050510000682005051000068EU 2005 5 10 USAA050148 120050114A5347F53326287200 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW21927 0342 BFM - FOUND TRACK CORRODED 2.3 INCH BY .4 INCH BY .032 INCH DEEP, FRAME 39.2 - Y450, MAIN CABIN FLOOR. REMOVED AND REPLACED SEAT TRACK PER SRM 53-31-15 FIG 101 SHT 8. (M) 2L72 4F RTA46NM 20050510000702005051000070EU 2005 5 10 USAA050146 120050112A5315F53479046000 FLOORBEAM AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW21927 0342 BFM - FOUND BEAM ASSEMBLY CORRODED, 1 INCH LONG BY .750 INCH WIDE BY .065 INCH DEEP, MAIN CABIN, L-4 DOOR SILL AT Y+1915, Y-1912, 27 CM FORWARD OF FRAME 74. REMOVED AND REPLACED BEAM ASSEMBLY ASSY PER SRM 51-74-00, 51-23-11, 51-42-11, 51-44-11. (M) 2L72 4F RTA46NM 20050510000722005051000072EU 2005 5 10 USAA050138 120050108A5347F53326711204 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW21927 0342 BFM - FOUND SEAT TRACK CORRODED 2.75 INCH BY .350 INCH BY .025 INCH BY 1 INCH BY 1.5 INCH BY .028 INCH, -Y450 FRAME 53.2-54 MAIN CABIN FLOOR. INSTALLED NEW SEAT TRACK PER SRM 51-74-00, 53-31-15 FIG 101 SH 1. (M) 2L72 4F RTA46NM 20050510000752005051000075EU 2005 5 10 USAA050140 120050109A5347F53477214201 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW 0342 BFM - FOUND SEAT TRACK CORRODED, MAIN CABIN FLOOR -450 FRAME 58-68. REMOVED AND REPLACED SEAT TRACK PER SRM 53-00-15, FIG 101 SHT 2. CORROSION LEVEL 2, TASK NR J7-200-2580C. (M) 2L72 4F RTA46NM 20050510000772005051000077EU 2005 5 10 USAA050139 120050109A5347F5327563920000 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW21927 0342 BFM - FOUND TRACK CORRODED TRACK, FRAME 32-33, -Y1552 S, MAIN CABIN FLOOR. REMOVED AND REPLACED TRACK PER SRM 53-00-15 SH 2, FIG 101. CORROSION LEVEL 2, TASK NR J7-230-53500. REMOVED AND REPLACED TRACK PER SRM 53-00-15 SH 2, FIG 101. (M) 2L72 4F RTA46NM 20050510000792005051000079EU 2005 5 10 USAA050143 120050111A5347F53311983200 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW 0342 BFM - FOUND FALSE RAIL CORRODED, MAIN CABIN BETWEEN FRAME 12-13, Y+1456. CORROSION LEVEL 2, TASK NR J7-220-53500. REMOVED AND REPLACED FALSE RAIL PER SRM 53-11-14, 51-42-11, 51-72-00, 51-44-11. (M) 2L72 4F RTA46NM 20050510000822005051000082EA 2005 5 10 A6WA200540142 120050406A5210 DRAG ANGLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31417AW 7600 DOOR AFT DRAG ANGLE CRACKED .7 INCHES LONG AT SUPPORT CABLE PULLEY. (M) 2L72 4F RTA21EA 20050510000882005051000088EA 2005 5 10 QXEA200500630 120050322A5210 BRACKET CNDAIRCL600 CL6002C10 1390015EA ZONE 800 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - PASSENGER DOOR AFT SIDE CRACKED AT BASE OF TOP RISER AND BACK OF TREAD AT HANDRAIL STOWAGE BRACKET. REPAIRED IAW CRJ700 SRM 51-41-02-001-001-A01 REO 670-52-11-104. 2L72 4F RTA21EA 20050510000902005051000090EA 2005 5 10 QXEA200500632 120050323A5210 ANGLE CNDAIRCL600 CL6002C10 1390015EA ZONE 800 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 YYC - PASSENGER DOOR AFT SIDE OF STAIR ANGLE AT DOOR PANEL CRACKED AT ASSIST MOTOR. REPAIRED IAW REO 670-52-11-072. 2L72 4F RTA21EA 20050510001452005051000145EU 2005 5 10 MALA050290 120050322A53477253721495 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15415XJ 340B415 DURING 4K CHECK IN BNA FOUND GALLEY SEAT TRACK PROFILE, P/N 7253721-495 HAS BEEN DAMAGED, REMOVED AND REPLACED IAW SRM 51-40-21. 2L72 4T RTA52EU 20050510001502005051000150EU 2005 5 10 MALA050343 120050411A2613 WEU SAAB SF340 340B 7860101EU RT TAILPIPE MALFUNCTIONED A MALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL15404XJ 340B404 RT TAIL PIPE HOT LIGHT. ABORTED FLIGHT. REMOVED AND REPLACED WEU. 2L72 4T RTA52EU 20050510001522005051000152EU 2005 5 10 MALA050322 120050410A3150 WARNING SYSTEM SAAB SF340 340B 7860101EU CONFIGURATION ACTIVATED A MALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL15425XJ 340B425 CONFIGURATION WARNING ON TAKEOFF ROLLOUT AT 80 UTS. IT WAS NOT A HIGH SPEED ABORT. RAN AC AT VARIOUS POWER SETTINGS WITH FRICTION LOCK ON. 2L72 4T RTA52EU 20050510001922005051000192SO 2005 5 10 SIMA200510111 120050404A532013500469401 PROFILE EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21701MH 145162 SAW - DURING CPCPC INSPECTION, FOUND PROFILE Z-RIGHT SIDE AT FRAME 22 IS CORRODED. MAINTENANCE REPLACED PROFILE Z IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050510001942005051000194SO 2005 5 10 SIMA200509801 120050405A30403801D2 CONTROLLER EMB 135 EMB135KL 3260302SO WINDSHIELD TEMP BURNED A SIMAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW21823AE 145582 COCKPIT AND CABIN HAVE ELECTRIC SMOKE SMELL PERMEATING THROUGHOUT, VERY STRONG AND NOXIOUS. REPLACED NR 2 WINDSHIELD TEMP CONTROLLER AND NR 2 WINDSHIELD HEAT WIRES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050510001962005051000196SO 2005 5 10 SIMA200510112 120050404A531014521713003 BEAM EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21701MH 145162 DURING CPCP INSPECTION, FOUND CENTER HAT SECTION REPAIR DOUBLER AT FRAME 20 IS CORRODED. MAINTENANCE REPLACED HAT BEAM SECTION IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050510001982005051000198SO 2005 5 10 SIMA200510108 120050330A532014521721005 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21701MH 145162 SAW - DURING CPCP INSPECTION, FOUND DIGITAL FORWARD AT FRAME 16 CORRODED. REPAIRED DIGITAL IAW EMB SRM 53-21-10 FIGURE 203. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050510002002005051000200SO 2005 5 10 SIMA200510107 120050329A532014521700007 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21701MH 145162 SAW - DURING CPCP INSPECTION, FOUND LEFT OMEGA BEAM AT FRAME 20 CORRODED. MAINTENANCE REPLACED LEFT OMEGA BEAM AT FRAME 20 IAW SRM 53-21-00. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050510002042005051000204NM 2005 5 10 SWAA051148 120050418A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29333SW 23697 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 297, STR 17R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050510002072005051000207NM 2005 5 10 SWAA051151 120050418A53306545776 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29514SW 25153 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 943, STR 24L. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050510002162005051000216NM 2005 5 10 PIDA200500015 120050419A5744 SUPPORT ANGLE BOEING737 73736M 138443BNM NR 5 SPOILER CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05374PA 28333 NUMBER 5 SPOILER O/B HINGE I/B SUPPORT ANGLE CRACKED. REPLACED SUPPORT ANGLE PER SRM 51-10-2. 2L72 4F RTA16WE 20050510002172005051000217NM 2005 5 10 PIDA200500010 120050419A5320 WEB BOEING737 73736M 138443BNM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05374PA 28333 FOUR CRACKS IN WEB PANEL AT LBL 4 BETWEEN BS 967 AND BS 986. REPAIRED PER DWG 65-46816 AND SRM 51-10-2. 2L72 4F RTA16WE 20050510002192005051000219NM 2005 5 10 PIDA200500009 120050419A5311 FRAME BOEING737 73736M 138443BNM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05374PA 28333 TWO CRACKS IN BS 867 FRAME AT STR 9LT. REPAIRED PER SRM 53-00-07. 2L72 4F RTA16WE 20050511000112005051100011SO 2005 5 11 SIMA200509803 120050406A3397 CONNECTOR EMB 145 EMB145LR 3260212SO BATTERY PACK LOOSE A SIMAK NONE O OTHER ININSP/MAINT 1 SW21659AE 145762 SHV - FLT 3473 - CENTER SECTION OF FLOOR EMERGENCY LIGHTS AND OUTER WING EMERGENCY EXIT LIGHTS INOPERATIVE. FOUND LOOSE CONNECTOR ON BATTERY PACK NR 3 AND RESECURED. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20050511000182005051100018 2005 5 11 P5CA0501340 420050417A2297 WIRE BOEING747 747230B 1384889NM AUTOPILOT MISWIRED A P5CAO OTHER W INADEQUATE Q C CLCLIMB 1 EA15509MC 21221 A-AUTOPILOT TOC F/L 320 SELECTED ALT HOLD A/C WENT 100 FT HIGH THEN DESCENDED TO 31500. DISENGAGED AUTOPILOT HAND FLEW A/C BACK TO F/L 320. SELECTED AUTOPILOT-B ALT HOLD. FOUND ALT HOLD JUMPER WIRES FROM AUTOPILOT-A PITCH COMPUTER AND NR 1 CADC PIN 64,65 SWAPPED. SWAPPED WIRES PER WDM 22-12-13. PERFORMED ALT HOLD SYSTEM PER MM 22-10-00. 2L74 4F A20WE 20050511000242005051100024EA 2005 5 11 SWIA200514869 120050409A27604916406 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07951SW5476 5476 7795 ON TAXI OUT RECEIVED INBOARD GROUND SPOILER, FLIGHT SPOILER, AND SPOILERON CAUTION MESSAGES. REPLACED NR 2 SECU IAW MM 27-61-05. 2L72 4F RTA21EA 20050511000312005051100031EA 2005 5 11 SWIA200514876 120050413A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY FALSE ACTIVATIONA SWIAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 NM07430SW 7523 SMOKE CARGO, WARNING MESSAGE WHILE AIRCRAFT ON GROUND. REPLACED FORWARD SMOKE DETECTOR. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050511000422005051100042EA 2005 5 11 SWIA200514884 120050416A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLIGHT SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07903SW 7425 FLT SPOILERONS FAULT MESSAGE. REMOVED AND REPLACED LT INBOARD SPOILERON PCU IN OF WITH AMM 27-62. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050511000452005051100045NM 2005 5 11 QXEA200500676 120050402A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09367PH 511 PDX - RIGHTHAND INBOARD SEAT TRACK, FLOOR PANEL NUT PLATES DIRTY, POSSIBLY CORRODED ON INSIDE SURFACE BETWEEN STATION X182 AND X235.0. REPAIRED IAW DHC-8 200 SRM 51-40-11. 2H72 4T RTA13NM 20050511000802005051100080EA 2005 5 11 COMA0560270 120050420A5210 STRUCTURE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01981CA 7163 TWO CRACKS FOUND BETWEEN PAX FS 338.90 AND FS 335.70. REPAIRED IAW REO 601R-52-11-402 AND REO 601R-52-11-704. 2L72 4F RTA21EA 20050511000922005051100092CE 2005 5 11 DXTA200500685 120050419A3240 BRAKE CESSNA500 560CESSNA 2076750CE PILOT SIDE MALFUNCTIONED E DXTAO OTHER S AFFECT SYSTEMS LDLANDING 1 GL07307QS 5600307 UPON LANDING PILOT'S (LEFT SIDE) BRAKES VERY SOFT AND SPONGY. TRAVEL ALMOST TO THE STOPS BEFORE FIRM PRESSURE IS FELT. PUMPED UP TO NEAR NORMAL PRESSURE BUT SYSTEM WILL NOT SUSTAIN NORMAL BREAKING PRESSURE. COPILOT'S BRAKES NORMAL. INSPECTED BRAKE RESERVOIR, ACCUMULATOR AND BRAKES ASSY FOR LEAKS, WEAR INDICATORS; PILOT, CO-PILOT BRAKE PEDALS FOR LEAKS, NO DEFECTS NOTED, APPLIED POWER TO AIRCRAFT AND CHECKED BRAKES FOR OPERATION, NO DEFECTS NOTED FROM PILOTS OR CO-PILOTS. CONFERRED WITH TECH SERVICES, RETURN TO SERVICE IS OK. BLED BRAKES IAW 560 M/M 32-42-00, OPS CHECKS NORM. NO DEFECTS NOTED. 2L72 4F RTA22CE 20050511000982005051100098SO 2005 5 11 C2XA05IA057 120050416A335066368 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2719966 145131 BNA - DURING MAINTENANCE INSPECTION, THE NEXT TO LAST EMERGENCY LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED THE AFFECTED EMERGENCY LIGHT STRIP, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050511001022005051100102SO 2005 5 11 C2XA05CL024 120050421A33501317 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST TXTAXI/GRND HDL 1 SW2715572 145636 CLE - THE CREW REPORTED THE EMERGENCY EXIT LIGHT AT THE FLIGHT ATTENDANTS STATION DID NOT ILLUMINATE WHEN TESTED. MAINTENANCE REPLACED THE LAMP AND OPERATIONAL TESTS WERE GOOD. 2L72 4T RTT00011AT 20050511001282005051100128EU 2005 5 11 MALA050377 120050419A5315 FLOORBEAM BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15503XJ E2310 DURING C2 INSPECTION, FOUND FLOORBEAM AT FRAME 20 AND RBL 20 HAS CORROSION ON TOP OF UPPER FLANGE. 2H74 4F RTA49EU 20050511001462005051100146EU 2005 5 11 MALA050374 120050421A3260 INDICATOR BAC 146 AVRO146RJ85A1500097EU COCKPIT MALFUNCTIONED A MALAO OTHER O OTHER CRCRUISE 1 GL15518XJ E2337 CREW RETURNED TO MSP AFTER DEPARTURE DUE TO NOSE WHEEL POSITION INDICATION NOT CENTERED. NO FURTHER INFORMATION AT THIS TIME. 2H74 4F RTA49EU 20050511001652005051100165EA 2005 5 11 SWIA200514901 120050420A5610 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAO OTHER O OTHER DEDESCENT 1 NM07429SW 7518 FO SIDE WINDSHIELD SHATTERED IN FLIGHT. REPLACED RIGHT WINDSHIELD IAW 56-11-01. P/N OFF 601R33033-14 S/N OFF 01046H1005. 2L72 4F RTA21EA 20050511001672005051100167NM 2005 5 11 AWXA200500475 120050420A3397BMS13311122 WIRE BOEING737 7373G7 1384595NM SEAT ROW 21 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 SNA - EEL - DURING A-01 CHECK, FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 21 LT INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRING SPLICE FOR EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 21 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050511001692005051100169NM 2005 5 11 AWXA200500477 120050403A521065C363351 DOOR FRAME BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - DURING C-19 CHECK A .3125 INCH CRACK WAS FOUND ON L-1 DOOR FRAME AT 6TH DOOR STOP FROM TOP BS 344, STR 14 LT. MAINTENANCE CUTOUT DAMAGED SECTION OF L-1 DOOR FRAME AT 6TH DOOR STOP FROM TOP BS 344, STR 14 LT; FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-11. 2L72 4F RTA16WE 20050511001712005051100171NM 2005 5 11 AWXA200500479 120050405A3520417N31382 LINE BOEING737 737301 1384611NM ROW 6 RT OXY BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - DURING C-19 CHECK FOUND THE OXYGEN GENERATOR HOSE ASSEMBLY BROKEN AT SEAT ROW 6 RT. MAINTENANCE REMOVED AND REPLACED OXYGEN GENERATOR HOSE ASSEMBLY AT SEAT ROW 6 R/H IAW BMM 35-22-31. 2L72 4F RTA16WE 20050511001772005051100177NM 2005 5 11 SWAA051162 120050419A3350101073 LENS BOEING737 7373H4 1384600NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29385SW 26600 LEFT LOWER OVERWING EMERGENCY EXIT SIGN LENS MISSING. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20050511001782005051100178NM 2005 5 11 0500546314 120050419A3097 BUSS BAR BOEING747 747451 1384940NM WINDOW FAILED A NWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL01674US 30269 PILOT REPORTED RIGHT WINDOW BUSS BAR GAVE OUT SMOKE. TURNED RIGHT WINDOW HEAT OFF AND SMOKE STOPPED. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. WINDOW WAS MEL'D AND LATER MECHANIC FOUND A LOOSE CONTACT. REPLACED THE TERMINAL CONNECTOR 19JAN05 IN MNL. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20050511001822005051100182EU 2005 5 11 0500533144 120050418A2913887673 PUMP AIRBUS320 A320211 3930320EU HYD SYSTEM FAILED A NWAAC ABORTED TAKEOFF KJ FLUID LOSS WARNING INDICATION TOTAKEOFF 1 GL01344NB381301457 01766 DURING TAKEOFF ACCELERATION, EXPERIENCED LOSS OF YELLOW HYDRAULIC FLUID. ABORTED TAKEOFF AT ABOUT 50 KTS. FOUND FAILURE AT RIGHT ENGINE DRIVEN PUMP. REPLACED RIGHT ENGINE DRIVEN PUMP, CASE DRAIN FILTER, AND RIGHT PRESSURE FILTER. ALL RELATED SYSTEMS LEAK AND OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA28NM 20050511001842005051100184NM 2005 5 11 BB05029 120050422A5210 BEARING BOEING757 757225 1384959NM L2 DOOR BINDING A USAAK NONE O OTHER ININSP/MAINT 1 EA19602AU 22196 LAS - L2 DOOR IS HARD TO OPEN/CLOSE/ARM/DISARM. MAINTENANCE FOUND A BEARING BINDING IN THE DOOR LINKAGE. THE LINKAGE WAS REPOSITIONED AND LUBRICATED. 2L72 4F RTA2NM 20050511001872005051100187EU 2005 5 11 05FDEA01043 120050418A5315A5327536500100 FLOORBEAM AIRBUS300 A300F4605R 3930327EU MAIN DECK CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25683FE 801 FLOORBEAM CRACKED FRAME 58 / -Y953. REMOVED ALL NECESSARY CARGO LOADING SYSTEM AND FLOOR PANELS TO FOM. REMOVED DAMAGED ADAPTER. 2L72 4F RTA35EU 20050511001892005051100189NE 2005 5 11 05FDEA01044 220050417A7297 TERMINAL BLOCK AIRBUS310 A310222 3930315EU PWA JT9 JT9D* NE NR 2 ENGINE LOOSE A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25446FE 224 716116 ON CLIMB-OUT, NOTICED NR 2 EGT NEEDLE/ANALOGUE GAUGE FLUCTATING-RECEIVED ECAM FOR NR 2 ENG OVERLIMITS. PULLED POWER BACK. GAUGE STABILIZED THEN STARTED TO FLUCTUATE AGAIN. RAN QRH, DECIDED TO RETURN. BURNED DOWN FUEL TO MAX LNBW. NORMAL LANDING, TAXI IN. DEBRIEFED CREW NO OTHER INDICATION ON NR 2 ENG FUEL FLOW, N1 AND N2 NORMAL. DURING SECURITY CK OF WIRE HARNESS ON ENG FOUND BOTH NUTS ON ENG TERMINAL BLOCK ON FAN CASE BEFORE CONNECTOR 4951P FINGER TIGHT. TIGHTENED NUTS PER SMP AND PROCEEDED TO CK WIRING FROM T591 JUNCTION BLOCK TO CONNECTOR 4951P. ALSO MEGGED WIRES. ACCOMPLISHED POWER RUN TO 1.3 EPR PER JRH CH 4-35. 2L72 4F4 FRTA35EU E20EA 20050511002022005051100202NM 2005 5 11 SWAA051177 120050420A56105717623121 WINDOW BOEING737 7373Q8 1384670NM COCKPIT ARCED A SWAAK NONE B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 SW29685SW 23401 L2 COCKPIT WINDOW ARCING. REMOVED AND REPLACED WINDOW & HEAT CONTROLLER PER MM. 2L72 4F RTA16WE 20050511002252005051100225NM 2005 5 11 EIA2005071 120050330A5320 FLOOR SUPPORT BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 U/D RIGHT O/B FLOOR SUPPORT BS 400 RBL 79 CRACKED. FLOOR SUPPORT REPAIRED PER SRM 51-40-04 FIG 1. 2L74 4F A20WE 20050511002262005051100226NM 2005 5 11 EIA2005072 120050330A5311 FRAME BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 M/D BS 600 FRAME BETWEEN S24L & 25L FOUND CRACKED. FRAME REPAIRED PER SRM 53-10-04. 2L74 4F A20WE 20050511002322005051100232NM 2005 5 11 EIA2005077 120050331A5320 STIFFENER BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 COCKPIT FRAME BS 340 2AL STIFFENER CRACKED. STIFFENER REPLACED PER SRM 51-10-01 AND 51-30-02. 2L74 4F A20WE 20050511002332005051100233NM 2005 5 11 EIA2005078 120050331A5311 FRAME BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 M/D BS 320 LEFT S14E FRAME CRACKED AT STRINGER CUTOUT. FRAME REPLACED PER SRM 51-40-03 FIG 1. 2L74 4F A20WE 20050512000042005051200004EU 2005 5 12 SA05047 120050428A3213 STRUT AIRBUSA319 A319112 3930323EU NLG LOW A USAAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 EA19714US 1046 PIT FLT 219 ENROUTE PIT - TPA, AFTER TAKEOFF, ECAM MESSAGE 'L/G SHOCK ABSORBER FAULT' DISPLAYED. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE SERVICED THE NOSE LANDING GEAR STRUT. 2L72 4F RTA28NM 20050512000082005051200008EU 2005 5 12 DXTA200500699 120050426A2720AC67141 STRUT BRAERO1000 HAWKER1000 7450005EU RUDDER DAMAGED E DXTAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 GL07544QS 259044 THRU V1, RUDDER BECAME EXTREMELY STIFF AND REMAINED STIFF UNTIL AFTER AIRCRAFT CAME TO A TAXI. YAW DAMPER WAS CYCLED ON THEN OFF TWICE AND APPEARED TO FUNCTION NORMALLY. REMOVED FAULTY LT AND RT RUDDER BIAS STRUTS. INSTALLED LT AND RT UNIT IAW HAWKER 1000 MM 27-20-10. OPERATIONAL CHECK SATISFACTORY. 2L72 4F RTA3EU 20050512000162005051200016WP 2005 5 12 ARWA20050405 120050427A2910 LINE DOUG DC10 DC1010 3022110WP HYD SYSTEM LEAKING A ARWAO OTHER K FLUID LOSS TXTAXI/GRND HDL 1 SO1968041 46900 ON POST FLIGHT, FOUND EVIDENCE OF HYDRAULIC LEAK AT RT WING ROOT AREA AT TOP OF RT MAIN LANDING GEAR AREA. CUT; FABRICATED; AND INSTALLED PERMANENT LINE AT RT WING ROOT AT TOP OF RT MAIN LANDING GEAR IN ACCORDANCE WITH M/M 20-10-01. NO LEAKS NOTED. 2L73 4F A22WE 20050512000182005051200018 2005 5 12 ARWA20050406 420050429A34204520860528 INU DOUG DC10 DC1030 3023501WP ADI FAILED A ARWAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO19524MD 46999 REJECTED TAKEOFF AT 95 KTS. CAPTAIN'S (ADI) ATTITUDE DIRECTOR INDICATOR TUMBLED. REMOVED AND REPLACED INU-3 IAW MM 34-43-04 SYSTEM GROUND TEST OK IAW LTN-72 MM 34-43-04. THIS CLEARS DMI 19174 2L73 4F A22WE 20050512000212005051200021NM 2005 5 12 05FDEA01045 120050418A5530 SHEAR TIE BOEING727 727227 1384078NM VERTICAL STAB TOOL DAMAGE A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25481FE 21463 VERTICLE STAB TENSION TIE FWD SHEAR TIE FITTING HAS PREVIOUS TOOLING MARKS. REPAIRED PER EA 7-5530-86281. 2L73 4F A3WE 20050512000262005051200026NM 2005 5 12 UPS05544287 120050317A2120 ODOR BOEING757 75724APF 1384969NM COCKPIT DETECTED A IPXAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO01454UP 25475 FLEW THRU HEAVY RAIN, LOTS OF STATIC ELECTRICITY. TEMPORARY EICAS MESSAGES RUDDER RATIO & MACH SPEED TRIM & STRONG ELEC FUMES SMELL. ALL CONDITIONS CLEARED W/IN 5 MIN'S REMAINING FLT NORMAL. LT & RT SAM'S TEST NORMAL PER MM 27-09-00-2, NO FAULTS BALLS DISPLAYED. RRCM TEST NORMAL PER MM 27-09-00-2. DRAINED MOISTURE FROM PITOT STATIC SYS PER MM 34-11-00-3. PERFORMED LIGHTNING STRIKE INSP PER MM 5-51-19-2, NO DEFECTS NOTED. 2L72 4F RTA2NM 20050512000272005051200027NM 2005 5 12 05FDEA01003 120050414A5512ALC8107Y2 FITTING DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT HAND UPPER CENTER SKIN PLANK NR 26 RT BARREL NUT BORE FOUND EXCEEDED LIMITS. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. 2L73 4F RTA22WE 20050512000302005051200030NM 2005 5 12 USAA0500AB 120050425A5312 BULKHEAD BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19443US 24842 BS 178, LBL 4.5 WL 199 CRACKED. INSTALLED DOUBLER PER EO 5300V152 AND SRM 53-10-08 DETAIL IV. 2L72 4F RTA16WE 20050512000312005051200031NM 2005 5 12 05FDEA01142 120050427A5713ARB75091 STRINGER DOUG MD11 MD11F 3023600NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 RT WING NR 3 FUEL TANK, INTERIOR, UPPER STRINGER 9, MOST AFT FOUND WITH CRACK APPROXIMATELY 8 INCHES LONG. CARRIED OUT REPAIR PER SRM 57-20-00 VOLUME I, FIGURE 10. 2L73 4F RTA22WE 20050512000322005051200032NM 2005 5 12 05FDEA01143 120050427A293069141061 CYLINDER BOEING727 727227 1384078NM HYD SYSTEM DAMAGED A FDEAO OTHER KJ FLUID LOSS WARNING INDICATION LDLANDING 1 SO25479FE 21461 WITH FLAPS SET AT 15 DEG, WHEN LANDING GEAR PLACED FROM OFF TO DOWN, A SYS HYD PRESSURE WENT TO ZERO, A HYD QUANTITY WENT TO ZERO. RAN QRH PROCEDURES. LEFT AND RIGHT MAINS WERE GREEN, NOSE GEAR INDICATING UP PRIOR TO RUNNING CHECKLIST. MANUALLY EXTENDED GEAR AND LANDED UNEVENTFULLY. SYS A FLUID SHUTOFF. SWITCHES CLOSED W/ENGINES RUNNING FOR 20 MINUTES. INSPECTED A/C AND FOUND NLG HYD TRANSFER CYCLINDER SEPARATED INTO TWO PIECES, NLG W/W AREA COVERED IN HYD FLUID. R & R NOSE GEAR HYD TRANSFER CYCLINDER. PER 727 MM 32-35-01-4, C/W STEPS 1-4C REQ STEPS 4D, E, AND F. 2L73 4F A3WE 20050512000342005051200034EU 2005 5 12 SA05048 120050428A5210 SEAL AIRBUSA319 A319112 3930323EU PAX DOOR CUT A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19721UW 1095 CLT - FLT 1449 ENROUTE CLT - PLS, AFTER TAKEOFF, A LOUD AIR LEAK NOISE GENERATED FROM THE MAIN ENTRANCE DOOR. THE FLIGHT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FORWARD LEFT ENTRANCE DOOR SEAL, AND SEAL RETAINER A THE LOWER AFT CORNER. DOOR SEAL LEAK CHECKED, OK. 2L72 4F RTA28NM 20050512000352005051200035EU 2005 5 12 05FDEA01217 120050506A49503995069010 HOSE AIRBUS300 A300B4622R 3930312EU APU LEAKING A FDEAA UNSCHED LANDING KBJFLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SO25722FD 479 MAIN DECK CARGO SMOKE CAME ON DURING CLIMBOUT. RETURNED, LANDED, F/O SMELLED ODOR JUST PRIOR TO MAIN DECK CARGO SMOKE INDICATION AND THE SCENT DISAPPEARED AFTER NR 2 PACK WAS TURNED OFF. FOUND OIL ON BOTH PACK COALESCER BAGS. OIL LEAK AT APU BEING INJESTED INTO APU INLET. FOUND APU LOW OIL PRESSURE FLEX HOSE LEAKING. MPN 399-506-9010, CPN 4911201, QTY 1 HOSE, MSN 930258. 2L72 4F RTA35EU 20050512000422005051200042NM 2005 5 12 05FDEA00972 120050412A5512ALC8101504 PANEL DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON HORIZ STAB RIGHT HORIZ STAB BORE NR 5R FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-83000. 2L73 4F RTA22WE 20050512000442005051200044NM 2005 5 12 05FDEA00974 120050412A5512ALC8103503 PANEL DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON LEFT HORIZ STAB UPPER AFT SKIN PLANK NR 28L, BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82993. 2L73 4F RTA22WE 20050512000462005051200046NM 2005 5 12 05FDEA00976 120050412A5512ALC8103503 PANEL DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON LEFT HORIZ STAB BORE NR 24L, FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82993. 2L73 4F RTA22WE 20050512000482005051200048NM 2005 5 12 05FDEA00978 120050412A5512ALC8131501 PANEL DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON LT HORIZ STAB UPPER REAR SPAR NR 36L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82995. 2L73 4F RTA22WE 20050512000502005051200050NM 2005 5 12 05FDEA00980 120050412A5512ALC8104502 PANEL DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON HORIZONTAL STABILIZER RT UPPER CENTER SKIN PANEL NR 25R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-83001. 2L73 4F RTA22WE 20050512000522005051200052NM 2005 5 12 05FDEA00982 120050412A5512ALC8121502 PANEL DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON RIGHT HORIZ STAB UPPER FRONT SPAR SKIN PLANK NR 1R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82997. 2L73 4F RTA22WE 20050512000532005051200053NM 2005 5 12 05FDEA00983 120050412A5512ALC8101504 PANEL DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT UPPER FORWARD SKIN PLANK NR 13R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-83000 2L73 4F RTA22WE 20050513000012005051300001NM 2005 5 13 05FDEA00984 120050412A5512ALC8101504 PANEL DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON RIGHT HORIZ STAB UPPER FORWARD SKIN PLANK NR 9R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-83000. 2L73 4F RTA22WE 20050513000022005051300002NM 2005 5 13 05FDEA00985 120050412A5512ALC8104502 PANEL DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT UPPER CENTER SKIN PLANK NR 17R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-83001. 2L73 4F RTA22WE 20050513000042005051300004NM 2005 5 13 05FDEA01004 120050414A5512ALC8103504 PANEL DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT NR 28R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82994. 2L73 4F RTA22WE 20050513000052005051300005NM 2005 5 13 05FDEA01005 120050414A5512ALC8103504 PANEL DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT NR 32R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82994 2L73 4F RTA22WE 20050513000062005051300006NM 2005 5 13 05FDEA01007 120050415A5512ALC8101503 PANEL DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT UPPER FORWARD SKIN PLANK NR 3L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82991. 2L73 4F RTA22WE 20050513000072005051300007NM 2005 5 13 05FDEA01008 120050415A5512ALC8103504 PANEL DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT UPPER AFT SKIN PLANK NR 34R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82994. 2L73 4F RTA22WE 20050513000082005051300008NM 2005 5 13 05FDEA01009 120050415A5512ALC8103503 PANEL DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT UPPER AFT SKIN PLANK NR 34L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82993. 2L73 4F RTA22WE 20050513000092005051300009NM 2005 5 13 05FDEA01010 120050415A5512ALC8104501 PANEL DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT NR 21 LT BARREL NUT BORE, FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82952. 2L73 4F RTA22WE 20050513000102005051300010NM 2005 5 13 05FDEA01011 120050415A5512ALC8104501 PANEL DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT NR 23L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82952. 2L73 4F RTA22WE 20050513000122005051300012NM 2005 5 13 05FDEA01013 120050415A5512ALC8101503 PANEL DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT NR 27L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82993. 2L73 4F RTA22WE 20050513000132005051300013NM 2005 5 13 05FDEA01014 120050415A5512ALC8103503 PANEL DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT BR 29L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82993. 2L73 4F RTA22WE 20050513000142005051300014NM 2005 5 13 05FDEA01015 120050415A5512ALC8103503 PANEL DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT NR 31L, BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82993. 2L73 4F RTA22WE 20050513000152005051300015NM 2005 5 13 05FDEA01016 120050415A5512ALC8103503 PANEL DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT NR 33L. BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82993. 2L73 4F RTA22WE 20050513000162005051300016NM 2005 5 13 0500595657 120050423A5270 WARNING LIGHT BOEING757 757251 1384970NM COCKPIT ILLUMINATED A NWAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL01557NW 33393 ON TAKE OFF ROLL "R AFT ENTRY DOOR" ECAS ILLUMINATED AROUND 110 KNOTS. PILOT ABORTED TAKEOFF AT APPROXIMATELY 120 KNOTS. RETURNED AIRCRAFT TO GATE AND GROUND MAINTENANCE PERFORMED VISUAL AND OPERATIONAL CHECK OF THE RIGHT DOOR WARNING SYSTEM. OPS CHECKED NORMAL WITH NO FAULTS NOTED. COOLED BRAKES FOR 60 MINUTES AND RETURNED AIRCRAFT TO SERVICE. 2L72 4F RTA2NM 20050513000172005051300017NM 2005 5 13 EIA2005017 120050222A5755 SKIN BOEING747 747273C 1384896NM NR 2 SPOILER DELAMINATED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09471EV 20651 NR 2 SPOILER LOWER SURFACE SKIN DOUBLER DELAMINATED. COMPOSITE REPAIR MADE TO DELAMINATION ON PANEL EDGE NR 2 SPOILER PER B747 SRM 51-40-06 PG 13. 2L74 4F A20WE 20050513000182005051300018NM 2005 5 13 EIA2005018 120050222A5311 FRAME BOEING747 747273C 1384896NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09471EV 20651 CRACK INDICATION NOTED IN LWR FASTENER HOLES IN LTC-3 FRAME UPPER CLOSURE FITTING DURING OPEN HOLE HFEC INSPECTION. REAMED HOLE INSTALLED FREEZE PLUG IN LOWER HOLE AND INSTALLED FASTENER PER B747 SRM 51-10-08 PGS 1-11, 51-30-09 PGS 1-16, 20, 29, 30 AND BOEING DRAWING 691U0144 AND EO 53-747-1717-03. 2L74 4F A20WE 20050513000192005051300019NM 2005 5 13 EIA2005019 120050222A5711 SPAR BOEING747 747273C 1384896NM LT WING CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09471EV 20651 LEFT WING, FWD SPAR, LWR CHORD HEAVY CORROSION AND CONFIRMED CRACK AT FSSO 1410. REPAIRED LEFT WING, FWD SPAR LOWER CHORD AND LOWER WING SKIN FROM FSSO 1370-1410 PER ECRA 471-57-247-2. 2L74 4F A20WE 20050513000202005051300020NM 2005 5 13 EIA2005020 120050222A5311 FRAME BOEING747 747273C 1384896NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09471EV 20651 CRACK AT LOWER FRAME STR 25R, R5 DOOR STA 2231. INSTALLED NEW LOWER FRAME STA 2231 AT STR 25R PER B747 SRM 51-30-02 PG 8-9. 2L74 4F A20WE 20050513000212005051300021NM 2005 5 13 EIA2005021 120050222A5711 SPAR BOEING747 747273C 1384896NM RT WING CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09471EV 20651 RT WING FWD T-CHORD CORRODED AT WSS 1336 FSSO 1349.0 LOWER T-CHORD. REPAIRED RIGHT WING FWD SPAR T-CHORD AT WS 1336 (FSSO 1349.0) LOWER CHORD PER ECRA 471-57-242-2. 2L74 4F A20WE 20050513000222005051300022NM 2005 5 13 EIA2005022 120050222A5330 SKIN BOEING747 747273C 1384896NM FUSELAGE DAMAGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09471EV 20651 STA 240 AFT OF NOSE CARGO DOOR BOTTOM FUSELAGE SKIN WRINKLED. LOWER SKIN REPAIRED PER ECRA 471-53-246-2. 2L74 4F A20WE 20050513000232005051300023NM 2005 5 13 EIA2005023 120050222A5315 FLOORBEAM BOEING747 747273C 1384896NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09471EV 20651 BS 420 LBL 43 UPPER DECK FLOORBEAM WEB HAS CRACK AT UPPER T-CHORD AREA. REMOVED DAMAGED SECTION OF WEB AND REPAIRED PER B747 SRM 53-10-07 PG 47-50 FIG II. BONDED WEB AND DOUBLER FOR STA 420 LBL 34-54 PER BAC 5514-5101 BOEING DRAWING 65B10931 SHEET 75 AND B747 SRM 51-40-06 PG 23. ALODINED ALL BARE METAL PER B747 SRM 51-10-02 PGS 7-8 AND PRIMED PER BSOPM 20-41-02 PGS 7-9. 2L74 4F A20WE 20050513000242005051300024NM 2005 5 13 EIA2005024 120050222A5330 SKIN BOEING747 747273C 1384896NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09471EV 20651 FUSELAGE BS 1000 LT BETWEEN STR 37 & 40 HAS CORROSION ON SKIN INSIDE OF FWD PIT. REMOVED CORROSION AT STA 1000 STR 39-41 LT PER B747 SRM 53-30-03 FIG 12. CUT OUT LIMIT SKIN AREA PER B747 SRM 53-10-01 FIG 1, NDT CHECKED NO CRACK NOTED FABRICATED INSTALLED REPAIR PER B747 SRM 53-30-03 FIG 12 PGS 27-30. ALODINED AND PRIMED PER B747 SRM 51-10-02 PG 2-8. 2L74 4F A20WE 20050513000252005051300025NM 2005 5 13 EIA2005025 120050222A5313 STRINGER BOEING747 747273C 1384896NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09471EV 20651 BETWEEN STA 260-280 STRINGER 41 LT CRACKED AT AFT END. REMOVED AND REPLACED STRINGER STA 260-280 NR 41 LT PER B747 SRM 51-30-02 PG 2-9. FABRICATED NEW STRINGER NR 41 LT STA 260-280 PER B747 SRM 51-20-01 PAGE 11-20. 2L74 4F A20WE 20050513000272005051300027NM 2005 5 13 EIA2005089 120050404A5310 CREASE BEAM BOEING747 747212B 1384886NM FUSLEAGE DEFORMED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 M/D BS 980-1000 CREASE BEAM BETWEEN STR 4-STR 5 BEAM WEB FOUND DEFORMED. DEFORMED WEB REPLACED PER SRM 51-30-02 AND 51-10-01. 2L74 4F A20WE 20050513000292005051300029NM 2005 5 13 EIA2005091 120050404A5340 STRINGER CLIP BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 M/D STA 2220 STR 22L ATTACHED TIE CLIP CRACKED. TIE CLIP REPLACED PER SRM 51-10-01 AND 51-30-02. 2L74 4F A20WE 20050513000312005051300031NM 2005 5 13 EIA2005093 120050404A5315 FLOORBEAM BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 U/D FLOORBEAM UPPER CHORD AT BS 340 CRACK FOUND AT 4 EA FASTENERS HOLES AS PER ATTACHED FIGURE. FLOORBEAM UPPER CHORD REPAIRED AT BS 340 RBL 42 TO RT MOST O/B PER HAECO REPAIR SCHEME R53-35268 AND LBL37, LBL 46 REPAIRED PER SB63A2431 FIG 9. 2L74 4F A20WE 20050513000332005051300033NM 2005 5 13 EIA2005095 120050405A5320 FLOOR SUPPORT BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 M/D BS 260 MOST RIGHT RBL 105 FLOOR SUPPORT CRACKED. CRACKED FLOOR SUPPORT REPLACED PER SRM 51-10-01. 2L74 4F A20WE 20050513000352005051300035NM 2005 5 13 EIA2005097 120050405A5330 SKIN BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 LEFT BS 1730 AT STRINGER 34L ONE EACH FASTENER HOLE FOUND CRACKED AT 2ND LAYER 8 O'CLOCK POSITION .0625 INCH APPROX IN LENGTH. THE CRACK TRIMMED OFF AND NDT CONFIRMED CRACK FREE CONDITION. SKIN REPAIRED PER EIA EO 53-747-1701-03. 2L74 4F A20WE 20050513000372005051300037NM 2005 5 13 EIA2005101 120050405A5210 WEB BOEING747 747212B 1384886NM PAX DOOR CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 LEFT BS 488 NR 1 MAIN ENTRY DOOR CRACK FOUND AT BS 488 WEB AND DOUBLER. THE WEB AND DOUBLER REPAIRED PER SRM 53-10-04 FIGURE 92. 2L74 4F A20WE 20050513000392005051300039NM 2005 5 13 EIA2005103 120050405A3350 POWER SUPPLY BOEING747 747212B 1384886NM EMERGENCY LIGHT INOPERATIVE A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 FOUR (4) EXIT DOOR EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLIES AND OPS CHECKED IAW MM 33-51-00. 2L74 4F A20WE 20050513000412005051300041NM 2005 5 13 0500556743 120050323A5312 DOUBLER BOEING747 747249F 1384849NM PRESS PANEL CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01643NW 22245 DURING "L" CHECK, FOUND THREE CRACKED FASTENER HOLES ON DOUBLER AROUND APU PRESSURE PANEL CUTOUT AT BS 2360. REPAIRED PER EA 165204. 2L74 4F A20WE 20050513000432005051300043NM 2005 5 13 0500576743 120050314A5311 FRAME BOEING747 747249F 1384849NM FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01643NW 22245 DURING L-CHECK, FOUND CRACK IN FRAME AT BS 380 S24R. REPAIRED PER EA 67-165195. 2L74 4F A20WE 20050513000442005051300044WP 2005 5 13 DHL2005873001 120050423A291017001 LINE DOUG DC8 DC873F 302199FWP HYD SYSTEM LEAKING A DHLAO OTHER KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SO01873SJ 46091 LOSS HYDRAULICS ON ROLL OUT AFTER LANDING HYDRAULIC LEVEL DROPPED TO AUX LEVEL. FOUND LT HYDRAULIC LINE ON BOGIE TRIM CAL. LEAKING ON LET GEAR. REMOVED AND REPLACED HYDRAULIC LINE IAW 32-33-1. SERVICED RESERVOIR, OPS AND LEAK CK OK LINE PIN 17001. 2L74 4F RT4A25 20050513000462005051300046NM 2005 5 13 DHL2005762002 120050423A3350 LIGHT BOEING727 7272B7 138407LNM EMERGENCY EXIT LOOSE A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01762AT 22162 EMERGENCY EXIT LIGHTS AT FRONT ENTRY DOOR NEEDS TO BE REMOUNTED. INSTALLED EMERGENCY LIGHT AT FWD ENTRY DOOR AND OPS CHECKS SERVICEABLE IAW MM 33-50-01. 2L73 4F A3WE 20050513000482005051300048NM 2005 5 13 UPS05444334 120050414A5312 SPLICE BOEING747 747283B 1384867NM BULKHEAD WEB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 INSPECTION TYPE:C RH BS 1480 B/H #18 HOLE FOUND CRACK AT WEB SPLICE PLATE RUNNING UP APPROX 0.080" LONG ( CRACK LENGTH 0.080" ) NR 18 BOLT HOLE OVERSIZED TO 0.532" AT SPLICE PLATE HFEC INSP C/OUT FOUND CRACK FREE BUSHING REPAIRED AS PER EO B747-5310-10732. 2L74 4F A20WE 20050513000492005051300049NM 2005 5 13 UPS05444335 120050412A534065B105005 STRINGER CLIP BOEING747 747283B 1384867NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 INSPECTION TYPE:C COCKPIT - BS 360 S-8L FRAME/STR TIE CLIP CRACKED. ( CRACK LENGTH 0.5" ). COCKPIT BS 360 STR -8L TIE CLIP REPLACED AS PER SRM 51-10-01 P.9. 2L74 4F A20WE 20050513000502005051300050NM 2005 5 13 UPS05444336 120050410A534065B38600176 STRINGER CLIP BOEING747 747283B 1384867NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 INSPECTION TYPE:C M/D -BS 1940 STR 18R STRINGER TIE CLIP FOUND CRACKED. (CRACK LENGTH 3/8" ) TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9 AT BS 1940 STR 18R AREA. 2L74 4F A20WE 20050513000512005051300051NM 2005 5 13 UPS05444337 120050410A5313 STRINGER BOEING747 747283B 1384867NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 INSPECTION TYPE:C M/D BS 1956 STR 10R FOUND CRACKED. ( CRACK LENGTH .375" ) STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4 AT BS 1930-1960 STR 10R AREA. 2L74 4F A20WE 20050513000532005051300053NM 2005 5 13 UPS05444339 120050409A532065B1471773 STIFFENER BOEING747 747283B 1384867NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 INSPECTION TYPE:C M/D BS 400 STR 14EL STRINGER ATTACH FOUND CRACKED STIFFENER ( CRACK LENGTH .1875" ). M/D BS 400 STR 14EL STRINGER ATTACH STIFFENER REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050513000552005051300055NM 2005 5 13 UPS05444341 120050409A532065B01707529 SPLICE BOEING747 747283B 1384867NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 INSPECTION TYPE: C, BS 280 S-22L TO S-23L FRAME SPLICE FOUND CRACKED. (CRACK LENGTH .250" ) BS 280 S-22L TO S-23L FRAME SPLICE REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050513000562005051300056NM 2005 5 13 UPS05444342 120050409A531365B07654164 STRINGER BOEING747 747283B 1384867NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 INSPECTION TYPE: C, M/D - BS 180 - 200 S-16R STRINGER FWD FOUND CRACKED. (CRACK LENGTH .250"), M/D BS 180-200 S-16R STRINGER REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050513000572005051300057NM 2005 5 13 UPS05444343 120050411A534065B38600160 STRINGER CLIP BOEING747 747283B 1384867NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 INSPECTION TYPE: C, M/D- BS 1640 LT STR -1L TIE-CLIP FOUND CRACKED. (CRACK LENGTH .125" ), M/D BS1640 STR -1L TIE-CLIP REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050513000582005051300058NM 2005 5 13 UPS05444344 120050411A534065B38600170 STRINGER CLIP BOEING747 747283B 1384867NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 INSPECTION TYPE: C, M/D - BS 1640 STR 1R FRAME ATT TIE-CLIP FOUND CRACKED. (CRACK LENGTH .0625"), M/D- BS 1640 STR 1R FRAME ATT TIE-CLIP REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050513000592005051300059WP 2005 5 13 MWEA050034 120050425A5330591140659 DOUBLER DOUG DC9 DC981 3022081WP FUSELAGE DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31806ME 48032 DENT REQUIRES REPAIR AT FRAME STATION 245 BETWEEN 1181 AND 1171. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20050511002622005051100262EU 2005 5 11 05FDEA01067 120050422A5313 STRINGER AIRBUS310 A310203 3930313EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 BULK CARGO COMPT, BETWEEN FR 63 AND FR 64 LT SIDE STR 54 AND STR 55 LT HAS CORROSION AROUND FASTENERS AREA. REMOVED AND REPLACED FASTENERS IAW A310 SRM 51-40-21, REMOVED CORROSION IAW A310-200 SRM 51-74-10, NDT FOR MAT LOSS IAW A310-200 SRM 53-17-12 AND 53-10-00. RETURNED TO SERVICE PER FEDEX EA 6-5310-88741. 2L72 4F RTA35EU 20050511002642005051100264EU 2005 5 11 SA05045 120050421A2120 ODOR AIRBUS320 A320214 3930316EU CABIN DETECTED A USAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA19123UW 1310 DURING FLIGHT, PASSENGERS AND CABIN CREW NOTICED A BURNING ODOR NEAR SEAT ROW 11. CREW ELECTED TO DIVERT TO FLL FOR MAINTENANCE ACTION. MAINTENANCE OPERATIONALLY CHECKED THE AIRCONDITIONING SYSTEM. OPERATIONALLY CHECKED OK. 2L72 4F RTA28NM 20050511002662005051100266EU 2005 5 11 05FDEA01070 120050422A5313 STRINGER AIRBUS310 A310 EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 AFT CARGO COMPT BETWEEN FR 60 AND FR 61 ON STR 50 RT HAS AREA OF CORROSION. REMOVED FASTENERS AND REMOVED CORROSION FROM STG50 BETWEEN FR60 AND FR61 IAW A310-200 SRM 51-40-21 AND SRM 51-74-10; CHECKED LIMITS AND FOUND MATERIAL THICKNESS TO BE WITHIN LIMITS, TREATED, PRIMED, AND TOPCOATED AREA IAW A310-200 SRM 53-10-00 PG 123 ITEM NR4 AND SRM 51-23-10. REF FEDEX EA 6-5310-88741 FOR APPROVAL FOR RETURN TO SERVICE. 2L72 4F RTA35EU 20050511002682005051100268EU 2005 5 11 05FDEA01072 120050422A5313A53970713213 STRINGER AIRBUS310 A310203 3930313EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 AFT CARGO COMPT, BETWEEN FR 54.1 AND FR 54.2 ON STR 56 RT HAS 1 EA AREA OF CORROSION. REMOVED AND REPLACED WITH NEW STRINGER SECTION BETWEEN FRAMES 54.2 AND 54.1 IAW A310 SRM 53-10-14, CUT AND SPLICED FRAME 54.2 IAW A310 SRM 53-10-13 REF EA 6-5320-87234. 2L72 4F RTA35EU 20050511002702005051100270NM 2005 5 11 05FDEA00699 120050329A5347ACA7731504 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 MAIN DECK, BETWEEN STA 495 AND STA 500 RBL 63.5 SEAT TRACK CROWN. FOUND CORRODED. MAIN DECK STATION 495 TO 515 RBL 63.5, CORRODED SEAT TRACK REMOVED AND NEW SEAT TRACK P/N: ACA7731-504 INSTALLED AS PER SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20050511002722005051100272EU 2005 5 11 05FDEA01074 120050422A5313 STRINGER AIRBUS310 A310 EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 IN ACM BAY STR 46 RT BETWEEN FR 43 TO FR 47 HAS AREAS OF CORROSION. REMOVED CORROSION PER A310 SRM 51-74-10. C/W EA 6-5310-87784. FOUND ALL AREAS TO BE WITHIN LIMITS PER A310 SRM 53-10-00 AND EA 6-5310-87784. RESTORED SURFACE PROTECTION PER A310 SRM 51-75-10. 2L72 4F RTA35EU 20050511002742005051100274EU 2005 5 11 05FDEA01076 120050422A5330 SKIN AIRBUS310 A310203 3930313EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 IN A/C BAY, FRAME 44 TO 45, STR 46R TO 43R HAS NUMEROUS AREAS OF CORROSION. REMOVED CORROSION PER A310 SRM 51-74-10. C/W EA 6-5310-87784. FOUND ALL AREAS TO BE WITHIN LIMITS PER EA 6-5310-87784 AND A310 SRM 53-10-00. INSTALLED FASTENERS PER A310 SRM 51-40-21. RESTORED SURFACE PROTECTION PER A310 SRM 51-75-10. 2L72 4F RTA35EU 20050511002762005051100276EU 2005 5 11 05FDEA01078 120050422A5330 SKIN AIRBUS310 A310203 3930313EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 IN ACM BAY FR46 TO FR47 BETWEEN STR 50R AND STR 51R, SKIN HAS AREAS OF CORROSION. REMOVED CORROSION PER A310 SRM 51-74-10. C/W EA 6-5310-87784. FOUND ALL AREAS TO BE WITHIN LIMITS PER EA 6-5310-87784. INSTALLED FASTENERS PER A310 SRM 51-40-21. RESTORED SURFACE PROTECTION PER A310-SRM 51-75-10. 2L72 4F RTA35EU 20050511002872005051100287EU 2005 5 11 05FDEA01089 120050422A5313 STRINGER AIRBUS310 A310203 3930313EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 BULK CARGO COMPT, JUST FWD OF FR68 ON LT STR 50 HAS 1 EA AREA OF CORROSION. REMOVED AND REPLACED STR 50L. 2L72 4F RTA35EU 20050511002892005051100289EU 2005 5 11 05FDEA01091 120050422A5330 SKIN AIRBUS310 A310203 3930313EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 IN ACM BAY FR 44 TO FR45 BETWEEN STR 37L AND 38L SKIN HAS AREAS OF CORROSION. REMOVED CORROSION IAW A310 SRM 51-74-10 WITHIN LIMITS. FLAP PEENED AREA IAW A310 SRM 51-29-00 AND RESTORED PROTECTIVE COATING IAW A310 SRM 51-75-10 ON SKIN FR44 TO FR45 BETWEEN STR 37L TO STR 38L. 2L72 4F RTA35EU 20050511002912005051100291EU 2005 5 11 05FDEA01093 120050422A5313 STRINGER AIRBUS310 A310203 3930313EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 AFT CARGO COMPT, AT FR 54.3 FWD AND AFT SIDE, ON R-STR 48 HAS AREAS OF CORROSION. REMOVED FASTENERS AND STRINGER TIE TO FOM IAW A310 SRM 51-40-21 AND 51-72-10. REMOVED CORROSION IAW A310 SRM 51-74-10. FOUND TO BE WITHIN LIMITS IAW A310 SRM 53-10-00 TABLE 102. REINSTALLED FASTENERS AND STRINGER TIE IAW A310 SRM 51-40-21 AND 51-72-10. 2L72 4F RTA35EU 20050511002932005051100293EU 2005 5 11 05FDEA01095 120050422A5313 STRINGER AIRBUS310 A310203 3930313EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 AFT CARGO COMPT, BETWEEN FR59 AND FR60 ON R STGR 54 HAS AREA OF CORROSION. REMOVED FASTENERS IAW A310-200 SRM 51-40-21. REMOVED CORROSION IAW A310-200 SRM 51-74-10. MEASURED MATERIAL LOSS IAW A310-200 SRM 53-17-12. VERIFIED MATERIAL IS WITHIN LIMITS IAW A310-200 SRM 53-10-00. INSTALLED FASTENERS IAW A310-200 SRM 51-40-21. APPLIED PROTECTIVE FINISH IAW A310-200 SRM 53-21-10. 2L72 4F RTA35EU 20050511003012005051100301NE 2005 5 11 05FDEA01107 220050423A7310 FILTER AIRBUS310 A310203 3930313EU GE CF6 CF680 30025NE FUEL SYSTEM CONTAMINATED A FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25430FE 394 DURING TAKEOFF, APPROACHING 80 KTS, FUEL CLOG LIGHT, ECAM AND SINGLE CHIME FOR 1 ENGINE; REJECTED TAKEOFF AND ACCOMPLISHED RTO CHECKLIST. PULLED FUEL FILTER, FOUND DEBRIS IN FILTER. REPLACED FILTER, RAN ENGINE 15 MINS, REMOVED AND INSPECTED FILTER, NO DEBRIS NOTED. REINSTALLED NEW FILTER, LEAK CHECK GOOD, CLOSED COWL DOORS. OK TO CONTINUE. REF MM 73-12-03-2-B. 2L72 4F4 FRTA35EU E13NE 20050511003072005051100307 2005 5 11 BB05031 420050422A2565 LIFTER BOEING757 757225 1384959NM L2 DOOR SLIDE OUT OF POSITION A USAAK NONE O OTHER ININSP/MAINT 1 EA19602AU 22196 CLT - THE EVACUATION SLIDE ARMING LEVER AT DOOR L2 WAS BINDING. MAINTENANCE FOUND THE GIRT BAR LIFTER PRESSING ON THE GIRT BAR AND ADJUSTED IT. 2L72 4F RTA2NM 20050511003142005051100314NM 2005 5 11 EIA2005051 120050329A5313 STRINGER BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 COCKPIT BS 345 STRINGER 8L FOUND CRACKED. STRINGER 8L REPLACED AT BS 340-360 PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050511003332005051100333NM 2005 5 11 SWAA051181 120050421A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 1006, STR 12R. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2L72 4F RTA16WE 20050511003342005051100334NM 2005 5 11 SWAA051182 120050421A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29315SW 23337 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500B, GROUND A/C RECEPTICLE CUTOUT. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050511003352005051100335NM 2005 5 11 SWAA051183 120050421A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29315SW 23337 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 18R. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050511003412005051100341NM 2005 5 11 SWAA051189 120050421A25606557463 FITTING BOEING737 7375H4 138449DNM L1 DOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29509SW 24186 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON L1 DOOR EMERGENCY EVAC SLIDE FWD & AFT GIRT BAR FLOOR FITTINGS. REMOVED AND REPLACED FITTINGS PER MM. 2L72 4F RTA16WE 20050511003422005051100342 2005 5 11 SWAA051190 420050421A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29653SW 28398 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050511003442005051100344NM 2005 5 11 EIA2005009 120050221A3350 LIGHT BOEING747 747273C 1384896NM CABIN INOPERATIVE A EIAAK NONE L NO TEST ININSP/MAINT 1 NM09471EV 20651 UPPER DECK EMERGENCY LIGHT INOP. REPLACED INOP EMERGENCY LIGHT PER B747 MM 33-51-00. 2L74 4F A20WE 20050511003492005051100349NM 2005 5 11 EIA2005013 120050221A5730 SKIN BOEING747 747273C 1384896NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09471EV 20651 RIGHT WING EXTERIOR, L/E NOSE IS CRACKED AT FASTENER HOLE 10 INCHES LONG AT WS 200.0. HOT BONDED METAL TO METAL REPAIR MADE TO RT WING L/E NOSE AT WS 200.0 PER ECRA 471-57-241-2 AND 747 SRM 51-40-06 PG 23. 2L74 4F A20WE 20050512000052005051200005NM 2005 5 12 SB05053 120050428A2530 COFFEEMAKER BOEING737 737401 1384701NM GALLEY ODOR A USAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA19420US 23987 PIT FL 591 - CREW REPORTED SMOKE IN THE AFT GALLEY THAT WAS ELECTRICAL IN NATURE. FLIGHT DIVERTED TO PIT. ON DESCENT, CREW NOTED THAT THE SMOKE ABATED. MAINTENANCE REPLACED BOTH AFT GALLEY COFFEE MAKERS, WHICH WERE REPORTED TO BE CAKED WITH A BUILD-UP OF DRIED COFFEE. 2L72 4F RTA16WE 20050512000062005051200006 2005 5 12 PIDA20050017 420050501A2230111RAA3 ACTUATOR BOEING737 7373G7 1384595NM AUTOTHROTTLES FAILED A PIDAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO05370WL 24011 AUTO THROTTLE DISENGAGED ON TAKEOFF. WILL RE-ENGAGE AFTER FLAPS ARE UP. DOES NOT MATTER WHAT ENGINE'S ARE SPOOLED TO BEFORE TOGA IS PUSHED. PLACED AUTO THROTTLE ON MEL 22-4. REPLACED NR 2 AUTO THROTTLE SERVO ACTUATOR PER MM 22-31-91. OPS CHECK AND BITE CHECK GOOD PER MM 22-31-00. 2L72 4F RTA16WE 20050512000092005051200009NM 2005 5 12 AWXA200500445 120050412A2133VFT300A1 OUTFLOW VALVE AIRBUSA319 A319132 3930340NM CABIN PRESSURE MALFUNCTIONED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28822AW419002119 1410 ON CLIMB OUT OF PHX EN ROUTE TO ABQ WHILE PASSING THROUGH 800 FT RECEIVED ECAM WARNING FOR AVIONICS VENT SYSTEM FAULT, TURNED BACK TO PHX FOR REPAIR. ISSUED MEL 21-26-04, COND. 1 "SKIN AIR OUTLET VALVE". MAINTENANCE REMOVED AND REPLACED SKIN AIR OUTLET VALVE 22HQ IAW T/C R2A21301, TWO SEPARATE BITE TESTS OF AEVC SYSTEM FOUND NO FAULTS. VENDORS FUNCTIONAL TEST OF SKIN AIR OUTLET VALVE S/N 119 COULD NOT CONFIRM REASON FOR REMOVAL, UNIT TESTED GOOD IN ALL PHASES OF OPERATION PER CMM 21-26-53, REV. 6. 2L72 4F RTA28NM 20050512000112005051200011CE 2005 5 12 DXTA200500697 120050425A291399140751 PUMP CESSNA650 650 2076802CE HYD SYSTEM LEAKING E DXTAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL07792QS4794 6507092 HYD LOW ANNUNCIATOR ILLUMINATED 1 HOUR AFTER TAKEOFF AT FL 390. HYD VOLUME INDICATED =160 CU IN VOLUME CONTINUED TO DECREASE TO 100 CU IN AND HYD PRESS LOW ANNUNCIATORS ILLUMINATED. LANDING GEAR WOULD NOT EXTEND AND HAD TO BE BLOWN DOWN VIA EMERG EXTENSION CHECKLIST. INSPECTION AFTER LANDING REVEALED HYD FLUID OVER THE AFT END OF AIRCRAFT, INCLUDING THE BAGGAGE COMPARTMENT AND HELL HOLE. FOUND LT ENG HYD. PUMP LEAKING. REMOVED AND REPLACED HYD. PUMP. PERFORMED ENG. RUN. OPS/LEAK CHECK GOOD IAW CE 650 MM CHAP. 29-10-04. 2L72 4F A9NM 20050512000122005051200012CE 2005 5 12 DXTA200500698 120050425A215073838433 ACM CESSNA750 750 2076810CE CABIN COOLING UNSERVICEABLE E DXTAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 GL07962QS1642 7500126 STRONG SULFUR ACID ODOR WITH NO SMOKE PRESENT WAS OBSERVED IN COCKPIT ONLY. OCCURRED DURING INITIAL DESCENT FROM CRUISE ALTITUDE AND BECAME STRONGER AGAIN IN LANDING PHASE. FOUND TURBIN ON 'PAC' STIFF TO TURN BY HAND & WILL NOT RUN WITH 'PAC' IN NORM OR HIGH REMOVED FWD AND AFT EXHAUST DUCTS TO GAIN ACCESS. REMOVED AND REPLACED AFT ACM IAW CE 750 M.M. CHAP. 21-50-00. UNIT OPERATIONALLY & LEAK CHECKS GOOD. 2L72 4J RTT00007WI 20050512000232005051200023NM 2005 5 12 05FDEA01160 120050428A5330 SKIN BOEING727 727233 138408ANM FUSLEAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25264FE 21626 BS 720 15 TO 20, CREASED DENT BETWEEN STRINGER 18L-19L. REPAIRED SKIN AT BS 720 PLUS 15 TO PLUS 20, STR 18L - 19L PER SRM 53-30-3. 2L73 4F RTA3WE 20050512000332005051200033EU 2005 5 12 SA05049 120050428A3260 BRACKET AIRBUSA319 A319112 3930323EU PROX TARGET LOOSE A USAAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 EA19714 1046 PIT FLT 709 ENROUTE PIT - TPA, AFTER TAKEOFF, ECAM MESSAGES 'L/G SHOCK ABSORBER FAULT' AND 'L/G NOT UPLOCKED' DISPLAYED. AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TIGHTENED A LOOSE PROXIMITY TARGET BRACKET, AND PERFORMED A GEAR SWING. ALL CHECKS OK. 2L72 4F RTA28NM 20050512000362005051200036NE 2005 5 12 AWXA200500527 220050502A7230 ENGINE AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE NR 1 FAILED A AWXAC ABORTED TAKEOFF XJ ENGINE FLAMEOUT WARNING INDICATION TOTAKEOFF 1 WP28624AW412932585 055 V0101 ON TAKEOFF AT SEA EN ROUTE FOR PHX AFTER APPLYING TAKEOFF THRUST FLIGHT CREW HEARD A LOUD BANG ON LT SIDE OF AIRCRAFT FOLLOWED BY A BURNING ODOR, REJECTED TAKEOFF AT 20 KTS, ANOTHER AIRCRAFT REPORTED SEEING FIRE COMING OUT OF THE NR 1 ENGINE, FIRE FIGHTERS RESPONDED AND FOUND NO EVIDENCE OF FIRE. MAINTENANCE INSPECTED THE NR 1 ENGINE AND FOUND METAL IN THE TAILPIPE, ENGINE WILL BE REPLACED. MX R & R NR 1 ENGINE IAW T/C R5M71302, ENGINE RUN OPERATIONAL CHECK WAS GOOD. TEAR DOWN REPORTS CONFIRMS REASON FOR REMOVAL. MTU ATTRIBUTES THE COMPRESSOR STALL TO A STAGE 4 BLADE TEARING OFF. 2L72 4F4 FRTA28NM E311NE 20050512000382005051200038CE 2005 5 12 DXTA200500678 120050413A324140955 ANTI-SKID SYS CESSNA500 560CESSNA 2076750CE MLG MALFUNCTIONED E DXTAO OTHER J WARNING INDICATION LDLANDING 1 GL07341QS 5600341 UPON LANDING BRAKES HAD " HARD PEDALS " ON PILOT'S AND CO PILOTS SIDE. RELEASED BRAKES AND THEN HAD NORMAL BRAKING. FOUND RIGHT GEAR ANTI SKID TRANSDUCER INDICATOR R/S LATCHED WHITE. PULLED RT GEAR TRANSDUCER AND INSP. LOOKED OK. WENT OUT AND TAXI CHECKED BRAKES FOR CONDITION OF BRAKING, CHECKED OK. R & R RT GEAR ANTI-SKID TRANSDUCER. DID ANTI-SKID RESPONSE CHECK PER CE 560 MM 32-42-30 PAGE 201. OPS CHECK GOOD. 2L72 4F RTA22CE 20050512000472005051200047NM 2005 5 12 05FDEA00977 120050412A5512ALC8104502 PANEL DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT UPPER CENTER SKIN PLANK NR 21R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA1-5510-83001. 2L73 4F RTA22WE 20050512000492005051200049NM 2005 5 12 05FDEA00979 120050412A5512ALC8104502 PANEL DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON HORIZONTAL STABILIZER RT UPPER CENTER SKIN PANEL NR 23R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-83001. 2L73 4F RTA22WE 20050512000512005051200051NM 2005 5 12 05FDEA00981 120050412A5512ALC8103504 PANEL DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON HORIZONTAL STABILIZER RT UPPER AFT SKIN PANEL NR 35R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82994. 2L73 4F RTA22WE 20050513000032005051300003NM 2005 5 13 05FDEA00986 120050412A5512ALC8104502 PANEL DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT UPPER CENTER SKIN PLANK NR 19R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-83001. 2L73 4F RTA22WE 20050513000602005051300060WP 2005 5 13 0500609944 120050422A2780 CONTROL CABLE DOUG DC9 DC931 3022065WP RT WING SLAT OUT OF RIG A NWAAAL UNSCHED LANDING ABORTED APPROACH F FLT CONT AFFECTED APAPPROACH 1 GL011309T 47316 UPON SLAT EXTENSION FOR LANDING AT MBS, THE AIRCRAFT ROLLED SLIGHTLY AND THE "SLAT DISAGREEMENT" LIGHT ILLUMINATED. PER VISUAL CHECK, BOTH WINGS SLATS DID EXTEND BUT THE RIGHT WING WAS NOT AS FAR AS THE LEFT SIDE. COMPLIED WITH COM PROCEDURES, AN EMERGENCY WAS DECLARED, AND THE AIRCRAFT RETURNED TO DTW DUE TO THE LONGER RUNWAY AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE SLAT CABLE TENSION LOW ON THE RIGHT WING AND RE-RIGGED ALL SLAT CABLES ON BOTH WINGS. MAINTENANCE IS STILL IN PROGRESS AS OF 1100 ON 25APR. 2L72 4F A6WE 20050513000612005051300061EU 2005 5 13 AWXA200500483 120050423A2720SC47003 ACTUATOR AIRBUS320 A320232 3930326EU YAW DAMPER LEAKING A AWXAO OTHER J WARNING INDICATION DEDESCENT 1 WP28664AW12842 1621 ON DESCENT, RECEIVED ECAM MESSAGE FOR NR 1 ENGINE HYDRAULIC PUMP POW PRESSURE/ GREEN SYSTEM LOW PRESSURE, DECLARED EMERGENCY AND LANDED WITHOUT FURTHER EVENT. UPON ARRIVAL AT GATE MAINTENANCE FOUND HYDRAULIC FLUID DRIPPING FROM THE TAIL SECTION, APPLIED HYDRAULIC PRESSURE AND FOUND FLUID COMING FROM NR 1 YAW DAMPER ACTUATOR ASSEMBLY. REMOVED AND REPLACED NR 1 YAW DAMPER SERVO ACTUATOR IAW AMM TASK 27-26-51-000-001, OPERATIONAL AND LEAK CHECKS WERE GOOD. UNIT WAS TEST AND REPAIRED IAW CMM 27-26-51 REV. 11. UNIT S/N 3395 WAS VISUALLY AND ELECTRICALLY TESTED, WITH NO FAULT FOUND IAW CMM 27-26-51 REV. 11. UNIT WAS MODIFIED TO SC4700-5. 2L72 4F RTA28NM 20050513000622005051300062EU 2005 5 13 AWXA200500484 120050422A3250C247360012 SERVO AIRBUS320 A320232 3930326EU NLG STEERING FAULTY A AWXAO OTHER SJ AFFECT SYSTEMS WARNING INDICATION APAPPROACH 1 WP28652AW13288 953 NOSE WHEEL STEERING FAILURE - ON SHORT AND FINAL APPROACH INTO CUN EN ROUTE FROM PHX WITH LANDING GEAR DOWN ECAM INDICATED NOSE WHEEL STEERING FAULT (2), GREEN HYDRAULIC PRESSURE WAS NORMAL AND LANDING WAS NORMAL. AFTER CLEARING RUNWAY RECYCLED ANTI-SKID SWITCH AND FAULT CLEARED, DURING TAXI TO GATE NOSE WHEEL COCKED 90 DEGREES LEFT, SET BRAKES. MAINTENANCE REMOVED AND REPLACED NOSE WHEEL STEERING SERVO CONTROL (6GC) IAW AMM 32-51-51-000-001, OPS AND LEAK CHECKS WERE GOOD. TEAR DOWN REVEALED SERVO VALVE FAILED VOTAGE BALANCE TEST. UNIT WAS REPAIRED IAW CMM 32-57-01 REV. 8. 2L72 4F RTA28NM 20050513000632005051300063NM 2005 5 13 AWXA200500485 120050318A574365494427 FITTING BOEING737 737375 13844BNNM MLG BEAM CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 MCN - MAJOR REPAIR - DURING C-05 CHECK CORROSION WAS FOUND ON LT MAIN LANDING GEAR STABILIZER BEAM FORWARD ATTACH FITTING AT LOWER WING AT RS 197. MAINTENANCE REMOVED AND REPLACED LT MAIN LANDING GEAR STABILIZER BEAM FORWARD ATTACH FITTING IAW SOPM 20-50-01. 2L72 4F RTA16WE 20050513000642005051300064NM 2005 5 13 AWXA200500486 120050404A554265C314962 SKIN BOEING737 73733A 1384673NM RUDDER DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCN - MAJOR REPAIR - DURING C-19 CHECK FOUND THE RIGHT TOP AFT SECTION OF RUDDER DELAMINATED AT RUDDER STA 238. MAINTENANCE REMOVED DELAMINATED SECTION OF RT TOP AFT RUDDER CONDUCTIVE FRAME; FABRICATED A NEW REPLACEMENT SECTION OF CONDUCTIVE FRAME PER DWG 65C25841; INSTALLED REPAIR PART IAW B737-300 51-40-04. 2L72 4F RTA16WE 20050513000652005051300065NM 2005 5 13 AWXA200500487 120050404A575465C2660399 SKIN BOEING737 73733A 1384673NM SLAT ASSY DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCN - MAJOR REPAIR - DURING C-19 CHECK FOUND THE UPPER SURFACE OF THE NR 3 SLAT T/E WEDGE ASSEMBLY DELAMINATED AT SLAT STA 84 LT. MAINTENANCE CUT OUT DELAMINATED AREA OF NR 3 SLAT WEDGE UPPER SURFACE SKIN FROM SS 74.5 TO SS 94.4; FABRICATED A CORE FILLER AND EXTERNAL DOUBLER; BONDED REPAIR PARTS TO SLAT IAW ER 03-5700-05110-ES1. 2L72 4F RTA16WE 20050513000662005051300066NM 2005 5 13 AWXA200500488 120050404A575465C2660399 SKIN BOEING737 73733A 1384673NM SLAT ASSY DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCN - MAJOR REPAIR - DURING C-19 CHECK FOUND THE UPPER SURFACE OF THE NR 3 SLAT T/E WEDGE ASSEMBLY DELAMINATED AT SLAT STA 54 LT. MAINTENANCE CUT OUT DELAMINATED AREA OF NR 3 SLAT WEDGE UPPER SURFACE SKIN FROM SS 46.6 TO SS 63.3; FABRICATED A CORE FILLER AND EXTERNAL DOUBLER; BONDED REPAIR PARTS TO SLAT IAW ER 03-5700-05110-ES1. 2L72 4F RTA16WE 20050513000672005051300067NM 2005 5 13 AWXA200500489 120050415A534069424495 CLIP BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCN - MAJOR REPAIR - DURING C-19 CHECK A .5625 INCH CRACK WAS FOUND ON FRAME ATTACH CLIP AT BS 827 BETWEEN STR 25 RT AND STR 26 RT. MAINTENANCE REMOVED CRACKED FRAME ATTACH CLIP AT BS 827 BETWEEN STR 25 RT AND STR 26 RT; FABRICATED A NEW REPLACEMENT CLIP PER DWG 69-42949; INSTALLED REPAIR PART IAW B737-300 51-40-02. 2L72 4F RTA16WE 20050513000682005051300068NM 2005 5 13 AWXA200500490 120050402A5753BOEING SKIN BOEING737 73733A 1384673NM LT WING TE FLAP CHAFED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCN - MAJOR REPAIR - DURING C-19 CHECK THE LEFT INBOARD MID-FLAP LOWER SKIN WAS FOUND CHAFED AT WS 100. MAINTENANCE BLENDED OUT DAMAGE ON LEFT INBOARD MID-FLAP LOWER SKIN AT WS 100; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW ER 03-5753-05112-RC2. 2L72 4F RTA16WE 20050513000722005051300072EU 2005 5 13 SA05046 120050423A3230 LANDING GEAR AIRBUSA321 A321211 3930370EU MALFUNCTIONED A USAAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 EA19109UW 1065 LAX FLT 1 EN-ROUTE PIT TO LAX, DURING APROACH, THE LANDING GEAR DID NOT INDICATE DOWN AND LOCKED. THE FLT PERFORMED A GO-AROUND, AND THEN MANUALLY EXTENDED THE LANDING GEAR. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED TROUBLESHOOTING PROCEDURES AND CYCLED THE LANDING GEAR NUMEROUS TIMES. THE PROBLEM COULD NOT BE DUPLICATED. THE MANUAL EXTENSION HANDLE WAS RESET. AIRCRAFT OK FOR SERVICE. 2L72 4F RTA28NM 20050513000752005051300075SO 2005 5 13 C2XA05TY035 120050419A532014521713005 FLOOR SUPPORT EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712957 145080 TYS, DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE GALLEY CENTER OMEGA BEAM. MAINTENANCE REMOVED AND REPLACED THE GALLEY CENTER OMEGA BEAM IAW EMB-145 SRM-51-40-02. 2L72 4F RTT00011AT 20050516000042005051600004EA 2005 5 16 SWIA200514903 120050421A274070609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07945SW1112 1112 7770 MACH TRIM AND STAB CH 2 DISENGAGED IN FLIGHT AND WOULD NOT RE-ENGAGE. REPLACED HSTCU. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050516000072005051600007 2005 5 16 SWIA200514906 420050423A3418501177003 ACTUATOR CNDAIRCL600 CL6002C10 1390015EA STICK PUSHER MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07713SK1107 1107 10174 CREW REPORTS STALL FAIL CAUTION MSG APPEARS ON EICAS. REPLACED STICK PUSHER ACTUATOR IAW CRJ MM 27-35-15. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050516000082005051600008EA 2005 5 16 SWIA200514907 120050423A2730 TRANSMITTER CNDAIRCL600 CL6002C10 1390015EA LT ELEVATOR MALFUNCTIONED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07740SK 10196 ELEVATOR SPLIT CAUTION MSG ILLUMINATED IN FLIGHT. REPLACED LEFT ELEVATOR POSITION TRANSMITTER IAW 27-34-10, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050516000102005051600010SO 2005 5 16 SWIA200514909 120050415A275012064207611 SELECTOR EMB 120 EMB120ER 3260203SO TE FLAP MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED LDLANDING 1 NM07187SW3803 3803 120037 CREW REPORTED FLAP CONTROL FAULT AND ADVANCED SWS WHEN FLAPS SELECTED. REMOVED AND REPLACED FLAP LEVER IAW MM 27-50-01, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050516000132005051600013EU 2005 5 16 MALA050335 120050413A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15429XJ 340B429 DURING 4Y/2Y CHECK IN BNA FOUND SEAT TRACK AT BL 0 IS CORRODED ON VERTICAL WEB AND FLOOR SUPPORT FLANGE AND HAS BEEN REPAIRED FROM FS 297 TO FS 312 IAW SRM 53-70-60. 2L72 4T RTA52EU 20050516000142005051600014EU 2005 5 16 MALA050351 120050413A5320 SILL BAC 146 AVRO146RJ85A1500097EU PAX DOOR CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15503XJ E2310 DURING C2 INSPECTION FOUND THE AFT PASSENGER DOOR SILL CORRODED BEYOND LIMITS. 2H74 4F RTA49EU 20050516000162005051600016EU 2005 5 16 MALA050306 120050328A5512 SKIN SAAB SF340 SF340A 7850100EU HORIZONTAL STAB DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15110XJ 340A110 DURING 30/12 CYC CHECK IN BNA FOUND RIGHT LOWER HORIZONTAL STAB SKIN IS DENTED AND HAS BEEN REPAIRED IAW MESABA EO S55053. DAMAGE IS 2.1 INCHES AFT OF FRONT SPAR AND 13.3 INCHES FROM I/B EOP. 2L72 4T RTA52EU 20050516000172005051600017EU 2005 5 16 MALA050321 120050406A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15448XJ 340B448 DURING 4K CHECK IN BNA FOUND RAIL ASSEMBLY P/N 7253710-871 BETWEEN FS 258 AND LBL 36 IS CORRODED OUT OF LIMITS AND HAS BEEN REPLACED IAW SRM 51-40-21 AND 51-40-22. 2L72 4T RTA52EU 20050516000182005051600018EU 2005 5 16 MALA050328 120050413A5320 PANEL SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15429XJ 340B429 DURING 4Y/2Y CHECK IN BNA FOUND LEFT AND RIGHT WRAP AROUND PANELS P/N 7253710-243 (RT) AND 7253711-245 (LT) ARE CORRODED AND ARE BEING REPLACED IAW SRM 51-40-21. 2L72 4T RTA52EU 20050516000202005051600020EU 2005 5 16 MALA050381 120050421A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15361PX 340B249 DURING 4Y/2Y CHECK IN BNA FOUND SEAT TRACKS AT LBL 18.3 AND BL 0 ARE CORRODED AND HAVE BEEN REPAIRED IAW MESABA EO S53060 AT LBL 18.3 BETWEEN FS 297 AND 319 AND IAW SRM 53-70-60 AT BL 0 BETWEEN FS 297 AND FS 310. 2L72 4T RTA52EU 20050516000212005051600021EU 2005 5 16 MALA050383 120050425A2120 ODOR SAAB SF340 340B 7860101EU COCKPIT DETECTED A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL15369PX 340B295 AFTER TAKEOFF, BURNED ODOR NOTED IN COCKPIT BLEEDS ON, TEMP IN AUTO AT NR 7. ADJUSTED TEMP TO 5 AND ODOR WENT AWAY. ISOLATED TO THE FLIGHT DECK ONLY, DURATION OF ODOR 1 MINUTE. GROUND RAN AC AT FULL HOT FOR APPROX 15 MIN, NO ODOR NOTED IN COCKPIT. ALL ENGINE IND NORMAL. INSPECTED ACM OIL LEVEL & HEAT EXCHANGERS. NO DEFECTS NOTED. INSPECTED ENG INLET & EXHAUST, NO DEFECTS NOTED. 2L72 4T RTA52EU 20050516000222005051600022EU 2005 5 16 MALA050358 120050414A5230 SKIN BAC 146 AVRO146RJ85A1500097EU CARGO DOOR CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15503XJ E2310 DURING F1.E INSPECTION FOUND AFT CARGO DOOR INNER SKIN CRACKED AT FORWARD HINGE GUIDE PIN ATTACH BRACKET. 2H74 4F RTA49EU 20050516000232005051600023EU 2005 5 16 MALA050359 120050414A5320 GUSSET BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15503XJ E2310 DURING C2 INSPECTION FOUND GUSSET CORRODED AT FRAME 15 LBL 24. 2H74 4F RTA49EU 20050516000242005051600024EU 2005 5 16 MALA050360 120050415A5330 SKIN BAC 146 AVRO146RJ85A1500097EU FUSELAGE CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15503XJ E2310 DURING INCORPORATION OF EO FOUND CHAFING ON FUSELAGE SKIN AND REINFORCING PLATES ALONG SKIN UNDERWING TO FUSELAGE FAIRING ACCESS PANELS ON LEFT AND RIGHT SIDES. 2H74 4F RTA49EU 20050516000262005051600026EU 2005 5 16 MALA050362 120050416A5330 FLOORBEAM BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15503XJ E2310 DURING C2 INSPECTION AND SEAT RAIL REPAIRS, FOUND FLOORBEAM UPPER FLANGE AT FRAME 18 AND RBL 36 CORRODED. 2H74 4F RTA49EU 20050516000282005051600028EU 2005 5 16 MALA050364 120050416A5347 SEAT TRACK BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15503XJ E2310 DURING C2 INSPECTION FOUND AFT RIGHT OUTBOARD SEAT RAIL BETWEEN FRAME 43-44 CORRODED. 2H74 4F RTA49EU 20050516000332005051600033WP 2005 5 16 CALA0500140 120050506A5320 WEB DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714879 49526 INSPECTION FOUND A 2 INCH CRACK IN WEB AFT OF MAIN CABIN DOOR AT STA 210, LONGERON 11L. THE CRACKED AREA OF WEB WAS REMOVED AND A REPAIR WAS INSTALLED IAW ECRA 5314-01010. 2L72 4F RTA6WE 20050516000362005051600036NM 2005 5 16 CALA0500143 120050507A5320143N5015950 FLOOR SUPPORT BOEING757 757224 1384958NM STA CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713113 27555 INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT STA 720, RBL 44 TO RBL 48. REPAIRED IAW SRM 53-00-51, REPAIR 3. 2L72 4F RTA2NM 20050516000372005051600037NM 2005 5 16 CALA0500144 120050509A2597 WIRE BOEING737 737824 13844BZNM COFFEEMAKER BURNED A CALAK NONE O OTHER ININSP/MAINT 1 SW2737253 30584 SMOKE APPEARED IN THE AFT GALLEY WHILE EN ROUTE TO PHX. GALLEY CIRCUIT BREAKERS WERE PULLED AND THE SMOKE CEASED AND DISSIPATED. THE FLIGHT WAS CONTINUED TO PHX WHERE IT LANDED WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND THAT THE AFT GALLEY COFFEE WARMER HAD BURNT WIRES. THE COFFEE WARMER WAS REMOVED AND REPLACED IAW MM 25-30-19. THE COFFEE WARMER WAS TESTED AND ALL OPERATION CHECKED GOOD. 2L72 4F RTA16WE 20050516000402005051600040NM 2005 5 16 CALA0500123 120050425A53306545773 SKIN BOEING737 7373T0 1384582NM FUSELAGE DELAMINATED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712319 23370 DELAMINATION BETWEEN SKIN AND DOUBLER ON LT SIDE OF FUSELAGE AT STA 727D. REPLACED SKIN PER ECRA 5330-03431. 2L72 4F RTA16WE 20050516000412005051600041NM 2005 5 16 CALA0500124 120050425A5313143N3110 STRINGER BOEING757 757224 1384958NM FUSLEAGE DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712125 28967 STRINGER DAMAGED AT S-16L BETWEEN STA 620-640. REPAIRED STRINGER PER SRM 53-00-03. 2L72 4F RTA2NM 20050516000422005051600042NM 2005 5 16 CALA0500125 120050425A5330143N33206 SKIN BOEING757 757224 1384958NM FUSELAGE DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712125 28967 TWO DENTS IN FUSELAGE IN FRONT OF L-2 DOOR. INSTALLED DOUBLER PER ECRA 5330-03433. 2L72 4F RTA2NM 20050516000432005051600043NM 2005 5 16 CALA0500126 120050426A5315BAC1505100246 FLOORBEAM BOEING737 7373T0 1384582NM FUSLEAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770330 23460 CABIN FLOORBEAM CORRODED AT STA 328, LBL 29. INSTALLED NEW ANGLE PER SRM 53-10-51. 2L72 4F RTA16WE 20050516000462005051600046NM 2005 5 16 CALA0500130 120050426A5315 FLOORBEAM BOEING737 737524 1384721NM FUSLEAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717614 27327 FLOORBEAM CORRODED AT STA 986.5, LBL 43. INSTALLED DOUBLER PER ECRA 5321-01210. 2L72 4F RTA16WE 20050516000472005051600047NM 2005 5 16 CALA0500131 120050426A5315 FLOORBEAM BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714609 27322 FLOORBEAM CORRODED AT STA 986.5 AND LBL 43. INSTALLED DOUBLER PER ECRA 5321-01211. 2L72 4F RTA16WE 20050516000502005051600050NM 2005 5 16 CALA0500120 120050425A2120 ODOR BOEING737 737824 13844BZNM COCKPIT DETECTED A CALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SW2714230 28794 JUST PRIOR TO V, F/O AND CAPT DETECTED A STRONG ELECTRICAL BURNING ODOR AND SAW A GRAY HAZE BETWEEN F/O AND F/O CONSOLE AFTER AIRBORNE. PERFORMED INSP PER 05-51-26-200-801C1 WITH NO DEFECTS NOTED. 2L72 4F RTA16WE 20050516000522005051600052NM 2005 5 16 CALA0500134 120050427A53116546563 FRAME BOEING737 737524 1384721NM FUSELAGE DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717627 27531 FRAME 967 DAMAGED AT GROUND STUD ATTACH POINT BETWEEN STRINGERS. INSTALLED FRAME PER SRM 53-00-07, FIG 202 2L72 4F RTA16WE 20050516000532005051600053NM 2005 5 16 CALA0500135 120050428A5311654653949 FRAME BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770330 23460 MAIN CABIN STA 616L FRAME INNER CHORD CRACKED. INSTALLED FRAME PER ECRA 5311-01158. 2L72 4F RTA16WE 20050516000542005051600054NM 2005 5 16 CALA0500136 120050427A5210 HINGE BOEING737 7373T0 1384582NM PAX DOOR LACK OF LUBE A CALAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW2747332 23570 MAIN CABIN DOOR WILL NOT CLOSE. CLEANED AND LUBRICATED TRACKS AND HINGE. 2L72 4F RTA16WE 20050516000562005051600056NM 2005 5 16 CALA0500138 120050425A5330 SKIN BOEING757 757224 1384958NM FUSELAGE DEFORMED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712125 28967 DEFORMED SKIN AT STA 620/640. INSTALLED DOUBLER PER ECRA 5330-03433A. 2L72 4F RTA2NM 20050516000572005051600057WP 2005 5 16 CALA0500145 120050509A5347S00200 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714879 49526 INSPECTION FOUND RT O/B SEAT TRACK CORRODED AT STA 200-256, RBL 40. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05. 2L72 4F RTA6WE 20050516000582005051600058WP 2005 5 16 CALA0500146 120050512A5347S00200 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714879 49526 INSPECTION FOUND LEFT I/B SEAT TRACK CORRODED AT STA 1085, LBL 22. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05 FIGURE 4F. 2L72 4F RTA6WE 20050516000602005051600060NM 2005 5 16 CALA0500117 120050425A5414311A1450 SKIN BOEING737 7373T0 1384582NM LT PYLON CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712319 23370 CRACK IN PYLON SKIN AT 5727L LEFT UPPER PYLON. INSTALLED DOUBLER PER ECRA 5430-01230. 2L72 4F RTA16WE 20050516000632005051600063NM 2005 5 16 CALA0500139 120050405A323126702888 VALVE BOEING757 757324 1384930NM RT MLG DOOR INOPERATIVE A CALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW27748564285 32815 THE GEAR DOOR UNSAFE LIGHT AND GEAR DISAGREE LIGHT ILLUMINATED AFTER TAKEOFF FROM IAH. THE GEAR WAS CYCLED AND THE GEAR LIGHTS TURNED TO GREEN BUT, THE GEAR DOOR UNSAFE LIGHT REMAINED ON. THE AIRCRAFT WAS RETURNED TO IAH AND LANDED WITH THE RT MLG DOOR DOWN. MAINTENANCE REPORTED THAT THE DOOR WAS FULLY CLOSED AFTER THE AIRCRAFT ARRIVED AT THE GATE. THE GEAR WAS SWUNG BUT, THE FAILURE COULD NOT BE DUPLICATED. THE RT MLG DOOR OPERATED SEQUENCE VALVE WAS REMOVED AND REPLACED IAW MM 32-32-05. OPERATIONAL CHECKS WERE GOOD AND NO LEAKS WERE NOTED. 2L72 4F RTA2NM 20050516000652005051600065EU 2005 5 16 MALA050336 120050413A5320 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15429XJ 340B429 DURING 4Y/2Y CHECK IN BNA FOUND SEAT TRACK AT LBL 18.3 IS CORRODED ON VERTICAL WEB AND FLOOR SUPPORT FLANGE. DAMAGE HAS BEEN REPAIRED IAW SRM 53-70-60 BETWEEN FS 297 AND FS 312. 2L72 4T RTA52EU 20050516000692005051600069EU 2005 5 16 MALA050435 120050414A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15435XJ 340B435 DURING 4Y/2Y CHECK IN BNA FOUND SEAT TRACK AT LBL 18.3 IS CORRODED ON VERTICAL WEB AND FLOOR PANEL FLANGE, BETWEEN FS 294 AND 319. DAMAGE HAS BEEN REPAIRED IAW SRM 53-70-60. 2L72 4T RTA52EU 20050516000702005051600070EU 2005 5 16 MALA050347 120050413A5413 STRINGER BAC 146 AVRO146RJ85A1500097EU NR 1 NACELLE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15503XJ E2310 DURING C2 INSPECTION FOUND 18 CRACKED STRINGERS NR 1 ENGINE ON BULKHEAD AFT OF NOSE COWL. 2H74 4F RTA49EU 20050516000712005051600071EU 2005 5 16 MALA050350 120050413A5413 STRINGER BAC 146 AVRO146RJ85A1500097EU NR 3 NACELLE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15503XJ E2310 DURING C2 INSPECTION FOUND A CRACKED STRINGER NR 3 ENGINE AFT OF ANTI-ICE TUBE AT 6 O'CLOCK POSITION. 2H74 4F RTA49EU 20050516000722005051600072EU 2005 5 16 MALA050301 120050316A5320 FLOOR SUPPORT SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15427XJ 340B427 DURING 4Y/2Y CHECK IN BNA FOUND CORROSION IN LT AISLE FLOORBOARD FLANGE AND RISOR AT STA 294 EXTENDING AFT APPROX 10 INCHES. REMOVED CORROSION OUT OF LIMITS. REMOVED DAMAGED SECTION AND INSTALLED NEW SECTION AND SPLICE. REF MESABA EO S53060 REV 3. 2L72 4T RTA52EU 20050516000742005051600074EU 2005 5 16 MALA050339 120050414A5320 PANEL SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15435XJ 340B435 DURING 4Y/2Y CHECK IN BNA FOUND LT WRAP AROUND P/N 7253711-245 IS CORRODED AND HAS BEEN REPLACED IAW SRM 51-40-21. 2L72 4T RTA52EU 20050516000752005051600075EU 2005 5 16 MALA050352 120050414A5315 GUSSET BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15503XJ E2310 DURING C2 INSPECTION FOUND GUSSET CORRODED AT FRAME 18 RBL 37. 2H74 4F RTA49EU 20050516000772005051600077EU 2005 5 16 MALA050320 120050407A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15447XJ 340B447 DURING 4K CHECK IN BNA FOUND GALLEY SEAT TRACK PROFILE P/N 7253721-495 IS CORRODED OUT OF LIMITS AND HAS BEEN REMOVED AND REPLACED IAW SRM 51-40-22. 2L72 4T RTA52EU 20050516000782005051600078EU 2005 5 16 MALA050429 120050413A5311 FRAME SAAB SF340 340B 7860101EU FUSELAGE CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15429XJ 340B429 DURING 4Y/2Y CHECK IN BNA FRAME AT FS 630, RIGHT SIDE AT APPROXIMATE WATER LINE 79.5 IS CHAFED OUT OF LIMITS AND HAS BEEN REPAIRED IAW SAAB DOCUMENT 340SDS008426. 2L72 4T RTA52EU 20050516000792005051600079EU 2005 5 16 MALA050317 120050406A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15447XJ 340B447 DURING 4K CHECK IN BNA FOUND SEAT TRACK FLANGE AT BL 0 BETWEEN FS 363 AND FS 389 IS CORRODED OUT OF LIMITS AND HAS BEEN REPAIRED IAW SRM 53-70-60. 2L72 4T RTA52EU 20050516000802005051600080EU 2005 5 16 MALA050319 120050406A5310 DOOR FRAME SAAB SF340 340B 7860101EU COCKPIT DOOR CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15447XJ 340B447 DURING 4K CHECK IN BNA FOUND COCKPIT DOOR POST AT RBL 10.0 IS CORRODED AND HAS BEEN REPAIRED IAW MESABA EO S53185. 2L72 4T RTA52EU 20050516000822005051600082EU 2005 5 16 MALA050340 120050414A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15435XJ 340B435 DURING 4Y/2Y CHECK IN BNA FOUND GALLEY SEAT TRACK P/N 7253721-459 IS CORRODED AND WILL BE REPLACED IAW SRM 51-40-27. 2L72 4T RTA52EU 20050516000842005051600084EU 2005 5 16 MALA050332 120050413A5320 FLOOR SUPPORT SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15429XJ 340B429 DURING 4Y/2Y CHECK IN BNA FOUND FLOOR SUPPORT AT RBL 15.0 AND FS 278 IS CORRODED AND HAS BEEN REPAIRED IAW SRM 53-70-30 REF. 2L72 4T RTA52EU 20050516000872005051600087EU 2005 5 16 MALA050303 120050324A5260 RAIL SAAB SF340 340B 7860101EU AIRSTAIR CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15415XJ 340B415 DURING 4K CHECK IN BNA FOUND PAX DOOR STEP RAIL ASSEMBLY IS CORRODED AND WILL BE REPLACED WITH A NEW PART, P/N 7253710-871 IAW SRM 51-40-21 AND 51-40-22. 2L72 4T RTA52EU 20050516000882005051600088EU 2005 5 16 MALA050304 120050324A5320 THRESHOLD SAAB SF340 340B 7860101EU FUSLEAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15415XJ 340B415 DURING 4K CHECK IN BNA FOUND RIGHT SERVICE DOOR THRESHOLD IS CORRODED OUT OF LIMITS BETWEEN FS 272 AND FS 294. THIS DAMAGE IS ACCEPTABLE AS IS IAW SAAB DOCUMENT 340S0S008366. 2L72 4T RTA52EU 20050516000892005051600089EU 2005 5 16 MALA050305 120050326A5320 FLOOR SUPPORT SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15415XJ 340B415 DURING 4K CHECK IN BNA FOUND RIGHT O/B FLOOR FLANGE IS CORRODED AND HAS DAMAGE FROM SCREW BETWEEN FS 570-590. DAMAGE HAS BEEN REPAIRED ON EMBRAER WORK ORDER 211921. 2L72 4T RTA52EU 20050516000922005051600092EU 2005 5 16 MALA050355 120050414A5320 SUPPORT BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15503XJ E2310 DURING C2 INSPECTION FOUND SUPPORT PLATE CORRODED AT FRAME 43 LBL 32. 2H74 4F RTA49EU 20050516000932005051600093CE 2005 5 16 DXTA200500691 120050421A3230 LANDING GEAR CESSNA750 750 2076810CE NOSE MALFUNCTIONED E DXTAO OTHER E VIBRATION/BUFFET CRCRUISE 1 GL07967QS 7500067 LOUD BUMP WAS HEARD AND FELT IN THE NOSE COMPARTMENT DURING CRUISE. JACKED AIRCRAFT, INSPECTED NOSE STRUT, UPLOCK & SWITCH. INSPECTED MAIN GEAR UPLOCKS AND SWITCHES, NO DISCREPANCIES NOTED. C/W GEAR SWING, FOUND ALL UPLOCK ROLLERS SEATED CORRECTLY IN HOOKS. FOUND SWITCHES MAKING CORRECTLY AND GEAR RELEASE CABLE RIG GOOD. UNABLE TO DUPLICATE DISCREPANCY, FOUND ORIGINAL LANDING GEAR CONTROL VALVE P/N 991664HO INSTALLED. LANDING GEAR CONTROL SYSTEM OPS CHECK GOOD IAW CE750 MM 32-30-00. 2L72 4J RTT00007WI 20050516000962005051600096CE 2005 5 16 DXTA200500695 120050423A3213 STRUT RAYTHNDH125 HAWKER800XP 7150012CE RT MLG UNDERSERVICED E DXTAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 GL07838QS 258338 RIGHT MAIN LANDING GEAR DID NOT FULLY RETRACT AFTER TAKEOFF, CONFIRMED BY FLY BY OF TOWER CONTROLLER. RE-SERVICED RIGHT MLG STRUT IAW HAWKER 800XP AMM 12-32-00, PERFORMED 25 GEAR RETRACTIONS / EXTENSIONS IAW HAWKER 800XP AMM 32-30-00, OP CHECK GOOD. 2L72 4F RTA3EU 20050516001022005051600102NM 2005 5 16 P5CA0501342 120050420A3150 WARNING SYSTEM BOEING747 74746NF 13848BTNM BRAKES ACTIVATED A P5CAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 EA15453PA 30811 CREW REPORTED REJECTED TAKEOFF - CONFIGURE WARNING BETWEEN 60/70 KTS. CONSULTED BRAKE COOLING. NO ACTION REQUIRED. WALK AROUND VISUAL INSPECTION NORMAL PER MM 05-51-10. NO DEFECTS NOTED. 2L74 4F RTA20WE 20050516001052005051600105 2005 5 16 TXER100210 420050131A2211116SF2C502W1202 POTENTIOMETER UROCOPEC155 EC155B 8681000EU INOPERATIVE B TXERO OTHER O OTHER NRNOT REPORTED 1 SW09588CF 6662 POTENTIOMETER INOPERATIVE. INCORRECT READINGS 1G72 3U H10EU 20050516001072005051600107SW 2005 5 16 YTRR100232 120050414A6510407340339107 BEARING BELL 407 407 1182206SW TAIL ROTOR WORN B YTRAO OTHER O OTHER NRNOT REPORTED 1 SW03595RL846 53595 TAIL ROTOR HANGAR BEARING WORN BEYOND MANUFACTURERS LIMITS. 1G71 3U O H2SW 20050516001202005051600120EU 2005 5 16 AWXA200500496 120050403A5315D5347219420 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28638AW 455 SAL - MAJOR REPAIR - DURING C-08 CHECK GALVANIC CORROSION WAS FOUND ON BEAM Y500 LT AT FR 66. MAINTENANCE REMOVED CORRODED BEAM Y500 LT AT FR 66; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050516001232005051600123NM 2005 5 16 2005UALA00360 120050415A4990 SEAL BOEING757 757222 1384956NM PWA 2037 PW2037 NE APU LEAKING A UALAA UNSCHED LANDING KH FLUID LOSS ELECT. POWER LOSS-50 PC CRCRUISE 1 WP29574UA 26686 DIVERTED TO ORD DUE TO THE LOSS OF APU OIL QUANTITY. OIL LEAK CONFIRMED IN TEST CELL AT 12:00 WHEN GEARBOX PRESSURIZED (SIMULATES APU OPERATION IN ALTITUDE). STAT-O-SEALS AT THE 12:00 POSITION, BETWEEN THE GEARBOX AND DRIVEN COMPRESSOR WERE LEAKING IN THE THE BLEED AIR DUCT. REBUILT COMPRESSOR MODULE AND ALL SHIMMING CORRECTED. THREE WASHERS INDICATE LIMITED SEAL DEFORMATION. TEST CELL LEAK CHECK AND BUILD PROCEDURES ARE BEING CHANGED TO ADD A LEAK CHECK WITH GEARBOX PRESSURIZED AT IDLE CONDITIONS, AND A LEAD CHECK ON THE BOLT TORQUES. 2L72 4F4 FRTA2NM E17NE 20050516001242005051600124NM 2005 5 16 2005UALA00361 120050415A3397 WIRE BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT OPEN A UALAK NONE O OTHER ININSP/MAINT 1 WP29127UA 28813 LEFT OVERWING EEL LIGHT SECOND FROM TOP AFT BULB INOP. RELAMPED, NO HELP. AFT LAMP OF THE UNIT WAS DISBONDED FROM THE CHASSIS GROUND. RECRIMPED THE CONNECTION AND REESTABLISHED GROUND. 2L74 4F4 FRTA20WE E24NE 20050516001282005051600128NM 2005 5 16 2005UALA00372 120050418A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29310UA 23671 DENT AT APPROXIMATELY BS 482 BETWEEN STR 3R AND 4R. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20050516001292005051600129 2005 5 16 2005UALA00373 420050401A2565 SLIDE BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN TORN A UALAK NONE O OTHER ININSP/MAINT 1 WP29199UA 28717 MULTIPLE HOLES AND TEARS IN THE INFLATABLE. CAUSE UNKNOWN, SLIDE REPAIRED PER OEM MAINTENANCE/REPAIR MANUAL. 2L74 4F4 FRTA20WE E24NE 20050516001302005051600130EU 2005 5 16 2005UALA00375 120050419A3350 LIGHT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CABIN MALFUNCTIONED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29433UA 589 EMERGENCY LIGHTS FAILING TEST IN AFT CABIN. AFTER SYSTEM RESET SYSTEM TESTED OK . 2L72 4F4 FRTA28NM E40NE 20050516001322005051600132NM 2005 5 16 2005UALA00377 120050419A5240BACB10FR25 BEARING BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE R1 DOOR WORN A UALAK NONE O OTHER ININSP/MAINT 1 WP29310UA 23671 R1 DOOR BODY TORQUE TUBE LOWER BEARING IS WORN. *S/D* REPLACED LOWER TORQUE TUBE ASSEMBLY AND OPERATIONALLY CHECKED WITH NO DEFECTS NOTED. 2L72 4F4 FRTA16WE E2GL 20050516001332005051600133NM 2005 5 16 2005UALA00378 120050419A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSLEAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29310UA 23671 DENT AFT OF L2 DOOR APPROXIMATELY STA 1004 STR 15L. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND TRIPLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20050516001392005051600139EU 2005 5 16 05FDEA01115 120050425A5712 RIB AIRBUS310 A310203 3930313EU RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 TOP OF RIGHT WING AT RIB 20 SKIN JOINT I/B SIDE OF SPLICE HAS 4 FASTENERS SHOWING CRACK INDICATION USING NDT METHOD. REMOVED CRACKS IAW EA 6-5720--87800. 2L72 4F RTA35EU 20050516001402005051600140EU 2005 5 16 05FDEA01116 120050425A5330 SKIN AIRBUS310 A310203 3930313EU RT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 RIGHT WING BOTTOM SKIN CUTOUT FOR PANEL 650 GB HAS 1 EA ELONGATED SCREW HOLE. COMPLIED EA 6-5710-87212. 2L72 4F RTA35EU 20050516001412005051600141EU 2005 5 16 05FDEA01117 120050425A5712 RIB AIRBUS310 A310203 3930313EU LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 LEFT WING LOWER SURFACE T/E SKIN HAS INDICATION OF CRACK RIB 11 AT PANEL 581 AB. REPAIRED IAW EA 6-5710-87138. 2L72 4F RTA35EU 20050517000022005051700002WP 2005 5 17 05FDEA01118 120050420A2750 CONTROL VALVE DOUG MD10 MD1010F 3022112WP TE FLAPS MALFUNCTIONED A FDEAA UNSCHED LANDING JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 SO25560FE 46938 AFTER TAKEOFF, DURING FLAP RETRACTION LEVEL 2 FLAP DISAGREE ALERT. O/B FLAPS SHOWED 5 AND 6 INBOARD FLAPS WERE AT 0. PER QRH ATTEMPTED TO RETURN FLAPS TO LAST POS THAT ALERT WAS NOT DISPLAYED. AT 12 O/B FLAPS STAYED AT 5 AND 6. DURING RETURN TO KMEM O/B FLAPS STAYED AT 5 AND 6 WHEN 22 FLAPS SELECTED. AT SOME POINT DURING SLOW DOWN O/B FLAPS EXT TO 22. NORMAL LANDING WAS MADE WITH FLAPS 50. REMOVED AND REPLACED THE RIGHT O/B AND THE LEFT O/B FLAP CONTROL VALVES PER MM 27-52-02-2. REMOVED AND REPLACED ALL RESTRICTORS AND CHECK VALVES. CONNECTED AND SAFTIED CONTROL RODS. LEAK CHECKED VALVES AND OPS CHECKED THE FLAP SYSTEM AS WELL AS FLAP IND SYSTEM. OPS CHECKS AND LEAK CHECKS GOOD. 2L73 4F RTA22WE 20050517000032005051700003EU 2005 5 17 05FDEA01119 120050425A3231 UPLOCK AIRBUS300 A300F4605R 3930327EU RT MLG DOOR FAILED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25654FE 738 NOSE GEAR DOORS UNLOCKED LIGHT REMAINED ILLUMINATED WHEN GEAR UP AND LOCKED ON BOTH GEAR INDICATION PANELS. RETRACTED GEAR AND CONFIRMED RIGHT GEAR DOOR UPLOCK WAS BAD. REMOVED AND REPLACED UPLOCK PER A300-600 MM 32-31-14. SWUNG GEAR SEVERAL TIMES, INDICATIONS GOOD ON FRONT AND OVERHEAD PANELS. PREMATURE REMOVAL/INSTALLATION OFF MFG A25431001-2. 2L72 4F RTA35EU 20050517000072005051700007NM 2005 5 17 SB0534 120050303A33503506892 SOCKET BOEING737 7373B7 1384580NM SEAT 12ABC INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19373US 22952 MCO - MAINTENANCE REPORTED THE EMERGENCY LIGHT AT SEAT 12ABC INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT SOCKET AT SEAT 12ABC. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050517000082005051700008NM 2005 5 17 SB05050 120050424A335020131A BATTERY PACK BOEING737 7373B7 1384580NM EMERGENCY LIGHT DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU 23702 PIT - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHTS AT THE LEFT OVERWING EXIT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050517000092005051700009NE 2005 5 17 ASMF200504018 220050422A732176960615 FCU DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE LT ENGINE FAILED W ASMFD RETURN TO BLOCK RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SW23214AM272758743 49585 725605 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING TAXING, THE LEFT ENGINE GENERATOR WENT OUT OF ITS BAR TURNING ON THE MASTER CAUTION LIGHT AND THE LEFT OIL PRESSURE WAS LOW (30 PSI). DURING ENGINE CHECK THE FCU DID NOT MAINTAIN THE RPMS IN IDLE AND DECREASED TO 32 RPM OF N2. LEFT FCU WAS REPLACED IAW MM 73-20-01 AND ENGINE WAS TESTED IAW MM 71-00-00, ALL CORRECT. 2L72 4F4 FRTA6WE E9NE 20050517000112005051700011 2005 5 17 ASMF200504020 420050423A3417HG280D80 CADC DOUG DC9 DC987 3022087WP LEFT SIDE FAILED W ASMFD RETURN TO BLOCK JG WARNING INDICATION MULTIPLE FAILURE TXTAXI/GRND HDL 1 SW23803ML12465 49726 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF ADC NR 1 FAILURE, AUTO SLATS FAIL LIGHT TURNED ON AND RIGHT EFIS LOST INFORMATION. TESTS WERE PERFORMED CONFIRMING THE FAILURES. ADC NR 1, LEFT STALL COMPUTER AND RIGHT AHRU WERE REPLACED IAW MM 34-16-01, 34-19-02 AND 34-21-10, ALL TESTS WERE CORRECT. 2L72 4F RTA6WE 20050517000132005051700013SO 2005 5 17 C2XA05SH025 120050415A531214567137403 RIB EMB 145 EMB145 3260210SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713956 145078 SHV - DURING C-CHECK, THE LT WINGS NR 1 FLAP TORQUE BOX HAS CRACK INDICATION ON FASTENERS O/B FWD AND AFT. MAINTENANCE OVERSIZED LT TORQUE BOX NR 1 O/B HOLE FWD AND AFT TO .277 INCH PER EMB 145 SRM 51-10-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050517000152005051700015NM 2005 5 17 05FDEA01133 120050426A5314 KEELBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25264FE 21626 CORROSION AT BS 950E 3 RT ON KEELBEAM OUTER FLANGE. REPAIRED PER EA 7-5310-86290. 2L73 4F RTA3WE 20050517000162005051700016SO 2005 5 17 C2XA05IA061 120050422A3243429513 CONTROL UNIT EMB 145 EMB145ER 3260211SO BRAKE INOPERATIVE A C2XAO OTHER O OTHER TXTAXI/GRND HDL 1 SW27149403748 3748 145033 DFW - DURING TAXI, THE CREW REPORTED THAT THE BRAKES WERE SPONGY, AND CHATTERING. MAINTENANCE INSPECTED THE AIRCRAFT, AND REMOVED AND REPLACED THE BRAKE CONTROL UNIT, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050517000182005051700018NM 2005 5 17 SB05052 120050426A335020131A BATTERY PACK BOEING737 737401 1384701NM EMERGENCY LIGHT DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19423US 23990 MCO - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT BATTERY WAS WEAK. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050517000192005051700019NM 2005 5 17 SB05051 120050425A335020121 CHARGER BOEING737 7374B7 1384702NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 CLT - MAINTENANCE REPORTED THE EMERGENCY LIGHTS ON SEAT ROWS 24ABC AND 25ABC INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT CHARGER ASSEMBLY AND BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050511003312005051100331NM 2005 5 11 SWAA051179 120050421A33506128251 BATTERY BOEING737 7373H4 1384600NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY AISLE LIGHTS INOP AT BS 720 & BS 850. REMOVED AND REPLACED BATTERY AND CHARGER ASSY PER MM. 2L72 4F RTA16WE 20050511003462005051100346NM 2005 5 11 EIA2005011 120050221A5711 SPAR BOEING747 747273C 1384896NM RT WING CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09471EV 20651 RIGHT WING FWD SPAR AT WS 1485 LOWER T-CHORD CORRODED. REPAIRED THE RIGHT WING FWD SPAR WS 1485 PER ECRA 471-57-238-2P. 2L74 4F A20WE 20050512000072005051200007NM 2005 5 12 05FDEA01114 120050425A5320 ANGLE BOEING727 727227 1384078NM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 WHILE CLOSING AFT CARGO BAY THRESHOLD FOUND LOWER ANGLE AT BS 990 TO BE DAMAGED. REPAIRED DAMAGED AFT CARGO BAY THRESHOLD LOWER ANGLE BS 990 PER FED EX EA 7- 5310-86283. 2L73 4F A3WE 20050512000132005051200013CE 2005 5 12 DXTA200500702 120050429A21201173T0635 SWITCH CESSNA500 560CESSNA 2076750CE CABIN AIR INOPERATIVE E DXTAH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CLCLIMB 1 GL07342QS 5600324 SHORTLY AFTER TAKEOFF, THE EMER PRESS LIGHT ILLUMINATED AND THE EMER PRESSURE ACTIVATED TWICE. TEMP CONTROL KNOB WAS AT THE 11.00 POSITION. WE WERE REQUESTING HEAT NOT COLD AIR. REPLACED 410 SWITCH IAW CE560 MM CH 21-51-00, OPS CHECK GOOD. 2L72 4F RTA22CE 20050512000152005051200015EU 2005 5 12 UPS05144389 120050428A5321 FLOOR PANEL AIRBUSA300 A300F4622R 3930360EU CABIN DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01158UP 0847 FLOOR PANEL IN A/B SECTION HAS DELAM OF FACE PLATE AFT SECTION AS REPORTED BY LOAD CREW. TRIMMED DAMAGE AND COMPLIED WITH EO A300-5320-22110-A. BULK PIT TO BY EMPTY UNTIL PERMANENT REPAIR COMPLETED. REF D301479. 2L72 4F RTA35EU 20050512000172005051200017WP 2005 5 12 ARWA20050404 120050428A2797 CONNECTOR DOUG DC8 DC863F 302198FWP ELEVATOR DIRTY A ARWAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO19441J 45988 DURING TAXI, ELEVATOR POSITION INDICATOR (EPI) FAILED DURING FLIGHT CONTROL CHECK. TRANSFERRED TO DMI NR 19171 AS PER MEL 27-9 CAT "C". CLEANED AND SECURED ELEVATOR EPI INDICATOR IN ACCORDANCE WITH M/M 31-10-30. OPERATIONAL CHECK NORMAL IN ACCORDANCE WITH M/M 27-30-0. THIS CLEARS DMI 19171. 2L74 4F 4A25 20050512000242005051200024NM 2005 5 12 05FDEA01163 120050428A2120 UNKNOWN BOEING727 7272S2F 1384O81NM CABIN/COCKPIT FUMES A FDEABA EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO25216FE 22937 CREW REPORTS THAT AT PASSING THRU 8000 FT, HAD UNKNOWN FUMES IN THE COCKPIT. DECLARED AN EMERGENCY AND C/W WITH CHECKLIST. RETURNED TO RNO. RAMP UNLOADED AND INSPECTED HAZ CONTAINER ALL OK. REMAINDER OF FREIGHT UNLOADED NO SIGNS OF LEAKAGE. RAN ENGINES AND PRESSURIZED A/C TO 4 PSID PER JRH, NO ODORS DETECTED. 2L73 4F A3WE 20050512000252005051200025NE 2005 5 12 DHL2005809003 220050504A7261M832481160 O-RING DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE NR 1 ENGINE LEAKING A DHLAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO01809DH 46047 1+ 12 HR INTO FLT NR 1 ENG LOST OIL QUANTITY WITH RESULT OF LOW OIL PRESS PERFORMED ABNORMAL PROCEDURE AND ENG SHUT DOWN. REPLACED O-RING AT STARTER CASE. PER DC-8 M/M 80-10-02 OPS CHECK NORMAL ON RUNS PER JRH CH 13, P/N M83248-1-160. 2L74 4F4 FRT4A25 E2GL 20050512000392005051200039CE 2005 5 12 DXTA200500680 120050414A215073838432 ACM CESSNA750 750 2076810CE CABIN COOLING UNSERVICEABLE E DXTAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 GL07964QS3428 7500164 CLIMBING THROUGH 36000 FT TO 40000 FT A NOTICEABLE ODOR OF BURNING OR PERHAPS SMOKE DEVELOPED, BUT NO VISIBLE SMOKE. IT WAS IRRITATING TO THE EYES AND WAS CONCENTRATED MOSTLY IN THE COCKPIT, HOWEVER, COULD SMELL IT IN THE CABIN. HAD THE ODOR INTERMITTENTLY AT FIRST, BUT IT INTENSIFIED THE LAST 10 MINS. TROUBLESHOT SMOKE SMELL IN COCKPIT, FOUND COCKPIT ACM FAILED (AFT) R & R WITH OVERHAULED UNIT PER CE 750 M/M CH 21-51-00 OPS/LK CK GOOD 2L72 4J RTT00007WI 20050512000412005051200041NM 2005 5 12 05FDEA00971 120050412A5512ALC8104501 PANEL DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON HORIZONTAL STAB LEFT BORE NR 24L FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82952. 2L73 4F RTA22WE 20050512000432005051200043NM 2005 5 12 05FDEA00973 120050412A5512ALC8101504 PANEL DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON RIGHT HORIZ STAB BORE NR 11R FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-83000. 2L73 4F RTA22WE 20050512000452005051200045NM 2005 5 12 05FDEA00975 120050412A5512ALC8103503 PANEL DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON LEFT HORIZ STAB UPPER AFT SKIN PANEL NR30L, BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82993. 2L73 4F RTA22WE 20050513000112005051300011NM 2005 5 13 05FDEA01012 120050415A5512ALC8104501 PANEL DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT NR25L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82952. 2L73 4F RTA22WE 20050513000692005051300069NM 2005 5 13 AWXA200500491 120050401A57536546431279SP SKIN BOEING737 73733A 1384673NM FORE FLAP DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCN - MAJOR REPAIR - DURING C-19 CHECK THE LT OUTBOARD FORE-FLAP WAS FOUND DELAMINATED AT THE UPPER AFT OUTBOARD CORNER. MAINTENANCE CUT OUT DAMAGE ON LT OUTBOARD FORE-FLAP AT UPPER AFT OUTBOARD CORNER BETWEEN WBL 410.11 AND WBL 413.6; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 51-70-10, REPAIR 22 FIG 31. 2L72 4F RTA16WE 20050513000712005051300071NM 2005 5 13 AWXA200500493 120050401A57536546431279 SKIN BOEING737 73733A 1384673NM FORE FLAP CHAFED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCN - MAJOR REPAIR - DURING C-19 CHECK FOUND THE LOWER CENTER SECTION SKIN OF THE LEFT OUTBOARD FORE-FLAP CHAFED AT WBL 298. MAINTENANCE CUT OUT CHAFED SKIN ON LOWER CENTER LT OUTBOARD FORE-FLAP AT WBL 298; FABRICATED NEW SKIN SECTION AND A DOUBLER; BONDED REPAIR PARTS TO FLAP IAW B737-300 51-70-10. 2L72 4F RTA16WE 20050513000742005051300074SO 2005 5 13 C2XA05BT020 120050415A3260 WARNING LIGHT EMB 145 EMB145LR 3260212SO MLG ILLUMINATED A C2XAO OTHER N FALSE WARNING APAPPROACH 1 SW2712921 145354 EWR - LOG SQUAWK LANDING GEAR AIR/GROUND FAIL CAUTION MESSAGE, OCCURRED ON GEAR DEPLOYMENT, THEN CLEARED A FEW SECONDS LATER. PERFORMED TROUBLESHOOTING, JACKED AIRCRAFT PERFORMED GEAR SWING OPERATIONAL CHECK. SATISFACTORY IAW EMB-145 MM 07-10-00-500-801-A AND EMB-145 FIM 32-63-00-810-801-A. 2L72 4T RTT00011AT 20050513000762005051300076SO 2005 5 13 C2XA05SH026 120050421A5330 SKIN EMB 145 EMB145 3260210SO FUSELAGE DENTED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713956 145078 SHV - DURING C-CHECK, LT SIDE EXTERNAL FUSELAGE HAS A DENT BETWEEN FR 7 & 8 JUST AFT OF GPU CONNECTION. MAINTENANCE REPAIRED LEFT SIDE EXTERNAL FUSELAGE DENT BETWEEN FR 7 & 8 OF GPU IAW EC5330-01342 AND IAW EMB SRM 53-10-01. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20050516000032005051600003NE 2005 5 16 2005000003 220050421A7520 CLAMP DOUG DC10 DC1030 3023501WP GE CF6 CF650C2B 30018NE NR 1 ENGINE LOOSE A CNMAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 SW07810AX 48265 455467 DURING CLIMB AT APPROXIMATELY 240 FT, NR 1 ENGINE A-LOOP LIGHT ILLUMINATED ACCOMPLISHED QRH PROCEDURES ALL OTHER ENGINE INDICATIONS NORMAL. UPON LEVEL OFF AT FL 290 NR 1 ENG INDICATED ENG FIRE, ALL OTHER ENG INDICATIONS NORMAL. FOUND LOOSE PNEUMATIC DUCT CLAMP AT NR 1 ENG L/P RT RECOUP TUBE ASSY RESECURED AND INSPECTED FOR OTHER DAMAGE, NONE FOUND PERFORMED HIGH POWER ENGINE RUNS. NO DEFECTS NOTED. 2L73 4F4 F A22WE E23EA 20050516000092005051600009EA 2005 5 16 SWIA200514908 120050423A2760C13045BA03 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA SPOILERS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07719SK992 992 10188 STAB/SPOILER FAULT WILL NOT CLEAR. REPLACED NR 2 SSCU WITH SERVICEABLE UNIT. OPERATIONAL CHECK GOOD AMM 27-61-05. 2L72 4F RTA21EA 20050516000122005051600012SO 2005 5 16 SWIA200514911 120050417A27503472001001 CONTROL UNIT EMB 120 EMB120ER 3260203SO TE FLAP MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07561SW1147011470 120335 FLAP CONTROL FAULT WHILE DROPPING THE FLAPS. REPLACED FCU AND RIGHT OUTBOARD FLAP ACTUATOR PER MM 27-50-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050516000152005051600015EU 2005 5 16 MALA050361 120050415A5320 STRUCTURE BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15503XJ E2310 DURING C2 INSPECTION FOUND RIGHT AFT Z-MEMBER BETWEEN FRAME 43 & 44 CORRODED. 2H74 4F RTA49EU 20050516000192005051600019EU 2005 5 16 MALA050333 120050413A5320 WEB SAAB SF340 340B 7860101EU CABIN FLOOR CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15429XJ 340B429 DURING 4Y/2Y CHECK IN BNA FOUND FLOOR REINFORCEMENT WEB P/N 7253721-739 IS CORRODED AND HAS BEEN REPLACED IAW SRM 51-40-21. 2L72 4T RTA52EU 20050516000252005051600025EU 2005 5 16 MALA050382 120050421A5320 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15361PX 340B249 DURING 4Y/2Y BNA FOUND AFT RT FUSELAGE IS DENTED AND HAS BEEN REPAIRED IAW SRM 53-90-10 AND MESABA EO S53187. 2L72 4T RTA52EU 20050516000272005051600027EU 2005 5 16 MALA050363 120050415A5320 GUSSET BAC 146 AVRO146RJ85A1500097EU CABIN FLOOR CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15503XJ E2310 DURING C2 INSPECTION FOUND FLOOR GUSSET AT FRAME 19 BETWEEN RBL 18-39 CORRODED. 2H74 4F RTA49EU 20050516000342005051600034WP 2005 5 16 CALA0500141 120050506A5320 WEB DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714879 49526 INSPECTION FOUND A 2 INCH CRACK IN WEB AT AFT SIDE OF MAIN CABIN DOOR JAMB AT STA 210, LONGERON 15L. THE CRACKED AREA OF WEB WAS REMOVED AND A REPAIR WAS INSTALLED IAW ECRA 5314-01010. 2L72 4F RTA6WE 20050516000352005051600035NM 2005 5 16 CALA0500142 120050507A5320143N5015950 FLOOR SUPPORT BOEING757 757224 1384958NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713113 27555 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 720, LBL 45.50 TO 51.50. REPAIRED IAW SRM 53-00-51, REPAIR 3. 2L72 4F RTA2NM 20050516000492005051600049NM 2005 5 16 CALA0500133 120050414A5330 SKIN BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2759302 23353 FUSELAGE SKIN CORRODED AT NR 3 VHF ANTENNA SUPPORT. INSTALLED CHANNEL PER ECRA 5331-01179. 2L72 4F RTA16WE 20050516000512005051600051 2005 5 16 CALA0500121 420050422A2330RDAV300601 CONTROLLER BOEING757 757224 1384958NM VIDEO SYSTEM FAILED A CALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2714102 27292 FIRST CLASS VIDEO SYSTEM HAD BURNING ODOR. REPLACED VIDEO SYSTEM CONTROLLER AND TAPES AND CASES. 2L72 4F RTA2NM 20050516000592005051600059NM 2005 5 16 CALA0500116 120050414A5315143N5013 FLOORBEAM BOEING757 757224 1384958NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714107 27297 FLOORBEAM CORROSION AT BS 680, RBL 53 ON FLOORBOARD FASTENER HOLE. REPAIRED CHORD PER SRM 53-00-51, FIG 201. 2L72 4F RTA2NM 20050516000612005051600061NM 2005 5 16 CALA0500118 120050422A33501000679 LIGHT BOEING767 767* NM CABIN INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW2776054 29449 FLIGHT DECK EMERGENCY EXIT LIGHT WILL NOT TEST. REPLACE EMERGENCY EXIT LIGHT ASSY PER AMM 33-51-01. 2L72 4F RTA1NM 20050516000662005051600066EU 2005 5 16 MALA050338 120050414A5310 DOOR FRAME SAAB SF340 340B 7860101EU 225 CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15435XJ 340B435 DURING 4Y/2Y CHECK IN BNA FOUND COCKPIT ENTRANCE DOOR FRAMES LT AND RT SIDES AT FS 225 ARE CORRODED AND HAVE BEEN REPAIRED IAW MESABA EO S53185. 2L72 4T RTA52EU 20050516000672005051600067EU 2005 5 16 MALA050353 120050414A5347 SEAT TRACK BAC 146 AVRO146RJ85A1500097EU FUSLEAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15503XJ E2310 DURING C2 INSPECTION FOUND SEAT RAILS BETWEEN FRAMES 18-19 AT RBL 18 CORRODED. 2H74 4F RTA49EU 20050516000762005051600076EU 2005 5 16 MALA050318 120050406A5310 DOOR FRAME SAAB SF340 340B 7860101EU COCKPIT DOOR CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15447XJ 340B447 DURING 4K CHECK IN BNA FOUND COCKPIT DOOR POST AT LBL 10.0 IS CORRODED AND HAS BEEN REPAIRED IAW MESABA EO S53185. 2L72 4T RTA52EU 20050516000812005051600081EU 2005 5 16 MALA050331 120050413A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15429XJ 340B429 DURING 4Y/2Y CHECK IN BNA FOUND GALLEY SEAT TRACK P/N 7253721-459 AND PROFILE P/N 7253721-495 ARE CORRODED AND HAVE BEEN REPLACED IAW SRM 51-40-21/22. 2L72 4T RTA52EU 20050516000902005051600090EU 2005 5 16 MALA050330 120050413A5320 THRESHOLD SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15429XJ 340B429 DURING 4Y/2Y CHECK IN BNA FOUND COCKPIT THRESHOLD AT FS 231 BETWEEN LBL 6.0 AND RBL 6.0 IS CORRODED AND HAS BEEN REPAIRED IAW SRM 53-70-30. 2L72 4T RTA52EU 20050516000942005051600094CE 2005 5 16 DXTA200500692 120050422A3240 BRAKE CESSNA500 560CESSNA 2076750CE MLG WEAK E DXTAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07361QS 5600361 BRAKES SOFT, ESPECIALLY ON RIGHT SIDE. CO-PILOTS BRAKES GO ALL THE WAY TO THE FLOOR, MUST PUMP UP PRESSURE. THEN PRESSURE LOST WITHIN SECONDS. PERFORMED BRAKE BLEED PROCEDURE AS REQUIRED. NO OTHER DEFECTS NOTED. WORK PERFORMED IAW CE-560 MM CHAP 32-42-00. 2L72 4F RTA22CE 20050516000972005051600097CE 2005 5 16 DXTA200500690 120050421A3230 HANDLE CESSNA750 750 2076810CE NLG MISLOCATED E DXTAO OTHER E VIBRATION/BUFFET CRCRUISE 1 GL07949QS 7500049 CRUISING AT FL410, A LOUD THUMP CAME FROM UNDER THE NOSE, SOUNDED LIKE THE NOSE GEAR CAME UNLOCKED AND BACK UP. DURING INSPECTION OF THE NOSE GEAR FOUND AN EXCESSIVE AMOUNT OF SLACK IN THE MANUAL UPLOCK HOOK RELEASE CABLE. INSPECTED HANDLE IN THE COCKPIT AND FOUND HANDLE TO BE REMOVED FROM THE STOWED POSITION. THIS HANDLE BEING REMOVED CAUSED GEAR TO UNLOCK IN FLIGHT AND WAS INSTANTLY LOCKED BY THE HYDRAULIC POWER. RESET UPLOCK RELEASE HANDLE TO ITS STOWED POSITION AS REQUIRED. CONTACTED LMCC WITH FINDING. INSPECTED AND RESECURED HANDLE IAW CE-750 MM CHP 32-30-06. REQUIRES GEAR SWINGS FOR FINAL OPS CHECK. JACKED A/C AS REQUIRED. PERFORMED SEVERAL GEAR SWINGS AND OPS CHECKED GOOD. 2L72 4J RTT00007WI 20050516001042005051600104NE 2005 5 16 T48R20050011 220050426A7200 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE DAMAGED B GTIAE ENGINE SHUTDOWN C F.O.D. NRNOT REPORTED 1 GL09803NK227181685 48087 709901 ENGINE WAS REMOVED FROM N803NK FOR INFLIGHT SHUTDOWN. DISASSEMBLY AND INSPECTION REVEALED THE HPC, HPT AND LPT MODULES HAVE HEAVY IMPACT DAMAGE. 2L72 4F4 F A6WE E9NE 20050516001062005051600106EU 2005 5 16 TXER100211 120050207A3300115VM01D002AN6C SWITCH UROCOPEC155 EC155B 8681000EU CABIN INOPERATIVE B TXERO OTHER O OTHER NRNOT REPORTED 1 SW09588CF 6662 LIGHT SWITCH INOPERATIVE 1G72 3U H10EU 20050516001102005051600110EU 2005 5 16 HDN2005F00000 120050418A5210L521M3071801 ARM UROCOPEC135 EC135P1 8680990EU DOOR BROKEN E HDNAK NONE O OTHER ININSP/MAINT 1 SW03312MS3629 0129 ROUND TUBE (ARM) BROKE COMPLETELY IN HALF .1250 INCH ABOVE LOWER MOUNT PLATE. (K) 1G72 3U O H88EU 20050516001152005051600115NM 2005 5 16 USAA200500001 120050419A5330 SKIN BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 FOUND CRACK, STA 767 BELOW S 22 L. INSTALLED DOUBLER AFTER CUT OUT OF CRACKED AREA PER BOEING SRM 53-00-01 FIG 101. 2L72 4F RTA16WE 20050516001192005051600119EU 2005 5 16 AWXA200500495 120050403A5320D53480043202 SILL AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28638AW 455 SAL - MAJOR REPAIR - DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SILL Y1270 LT AT FR 68. MAINTENANCE CUTOUT DAMAGED SECTION OF LOWER SILL Y1270 LT FROM FR 68.3 INCHES TO FR 68 + 7 INCHES; FABRICATED A NEW REPLACEMENT SILL; INSTALLED REPAIR PART IAW A320 SRM 53-41-14 FIG 201. 2L72 4F RTA28NM 20050516001342005051600134NE 2005 5 16 2005UALA00379 220050418A7200 ENGINE BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE RIGHT BIRD INGESTION A UALAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 WP29784UA 26951 RT ENG HAD A SMALL POWER SURGE, ALL INDICATIONS NORMAL SHORTLY THEREAFTER AND REMAINED THAT WAY 5 HRS LATER. APPARENTLY THE MM STATES THAT ATMOSPHERIC CONDS (LIGHTNING) COULD CAUSE THIS. THE ACFT WAS IN VICINITY OF LIGHTNING AT THE TIME (AT FL350.) ENGINE REPLACED. SHOP TEARDOWN REVEALED BIRD REMAINS IN LPC. HPC SUFFERED RESULTANT BLADE/STATOR AIRFOIL DAMAGE. BIRD STRIKE MUST HAVE OCCURRED EARLIER, RESULTING IN A LOSS OF SURGE MARGIN. SUBSEQUENT OPERATION IN CLOSE PROXIMITY TO LIGHTNING RESULTED IN A TRANSIENT OPERATING LINE SHIFT SUFFICIENT TO CAUSE THE SURGE. 2L72 4F4 FRTT0001SE E46NE 20050516001352005051600135 2005 5 16 2005UALA00380 420050420A2565 SLIDE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE 1R DOOR DISLODGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29377UA 24642 EMERGENCY ESCAPE SLIDE AT DOOR 1R CAME UNPACKED AND FELL ON THE FLOOR. WHEN TIGHTLY-PACKED SLIDES ARE OPENED (DURING INSPECTION OR WHILE REMOVING/INSTALLING THE SAFETY PIN) THE SLIDE EXPANDS, CAUSING VALISE LOOP AND HOOK TAPE AND COMPARTMENT/CLAMSHELL LATCH ASSY TO DISENGAGE. COMPRESSED SLIDE AND RE-FASTENED LOOP AND HOOK TAPE AND LATCH. RETURNED SLIDE TO SERVICE. 2L72 4F4 FRTA16WE E2GL 20050516001362005051600136NM 2005 5 16 2005UALA00383 120050422A3350 BATTERY BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29174UA 24381 EMERGENCY EXIT LIGHT ON AT 4L AND 4R. LOW BATTERY. REPLACED BATTERY. 2L74 4F4 FRTA20WE E24NE 20050517000012005051700001CE 2005 5 17 DJFA2005084 120050303A2700 FLT CONTROLS RAYTHNDH125 HAWKER800XP 7150012CE MALFUNCTIONED E DJFAO OTHER FP FLT CONT AFFECTED NO WARNING INDICATION NRNOT REPORTED 1 EA23725TA 258297 DURING STALL TEST AT 120 KIAS, EXPERIENCED AN UNCOMMANDED, UNCONTROLLED RT BANK. NO STALL HORN, STICK SHAKER OR PUSHER IND. APPROX 90 DEG BANK, A/C ROLLED FURTHER RT, & APPROX 140 DEG BANK, A/C ROLLED TO RT AGAIN. CONTINUED ROLL AFTER PASSING INVERT. RECOVERED AT APPROX 180 KIAS, 3000 FT LOWER ALT. STALL VALVE LIGHTS ON DURING PITCH AT 40 DEG BELOW HORIZ. LANDED W/FLAPS 0 DEG. NO FURTHER EVENTS NOTED. MX CHANGED: R&R ALL VORTEX GENS, AILERONS X-RAYED FOR MOISTURE, STALL TRIGGER ADJUST TO NOMINAL, R&R WING VENT TUBE, R&R RT AOA VANE, ELEVATORS RIGGED, R&R LT ELEVATOR CENTER HINGE BEARING. R&R LT AILERON OTBD HINGE BEARING, & R&R RT FLAP OTBD FWD FAIRING. FLT TEST GOOD & A/C RETURNED TO SERVICE. 2L72 4F RTA3EU 20050517000102005051700010NM 2005 5 17 ASMF200504019 120050423A32463910097543 WHEEL DOUG MD80 MD83 3023681NM NLG OUT OF BALANCE W ASMFD RETURN TO BLOCK E VIBRATION/BUFFET TXTAXI/GRND HDL 1 SW23881LF8627 53051 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF AIRCRAFT EXPERIENCED STRONG VIBRATION DURING TAKEOFF. NOSE LANDING GEAR WAS CHECKED BEING ALL CORRECT IAW MM 32-21-01. AIRCRAFT NOSE LANDING GEAR WAS JACKED DETECTING UNBALANCED BETWEEN BOTH WHEELS. REPLACED IAW MM 32-42-00, ALL CORRECT. 2L72 4F RT 20050517000122005051700012 2005 5 17 ASMF200504021 420050425A3416HG280D80 CADC DOUG DC9 DC987 3022087WP LEFT SIDE FAILED W ASMFK NONE J WARNING INDICATION ININSP/MAINT 1 SW23803ML12185 49726 TECHNICAL PERSONNEL INFORMED THAT DURING TRANSIT CHECK AIR SPEED FLAG WAS SHOWN IN LEFT AIR SPEED INDICATOR AND ALTIMETER. TESTS WERE PERFORMED AND FAIL CONTINUED. CADC NR 1 WAS REPLACED IAW MM 34-16-01, TESTED CORRECT. 2L72 4F RTA6WE 20050517000202005051700020WP 2005 5 17 ABXA050097 120050424A53305911415 SKIN DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23983AX 47257 DURING ROUTINE JOB CARD MAINTENANCE, A CRACK WAS FOUND AT FS 737, BETWEEN LONGERON 1 AND LONGERON 2 RIGHT, SKIN EXTERIOR. REPAIRED AREA IAW DC-9 SRM 53-04 FIG 12B. 2L72 4F A6WE 20050517000212005051700021NM 2005 5 17 ABXA050095 120050418A3350 BATTERY BOEING767 767281 1385109NM EMERGENCY LIGHT DISCHARGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23768AX 22786 DURING AM CHECK, FOUND EMERGENCY LIGHT WOULD NOT STAY ON FOR MORE THAN 5 MINUTES. SWAPPED BATTERIES, NO HELP. CHECKED VOLTAGE AT CHARGER IAW AMM 33-51-07-2, CHECKED GOOD. CHARGED BATTERIES FOR MORE THAN 4 HOURS. OPS CHECKED GOOD. 2L72 4F RTA1NM 20050517000222005051700022NM 2005 5 17 ABXA050096 120050420A3397 CONNECTOR BOEING767 767281 1385109NM EMERGENCY LIGHT CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23791AX 23141 EMERGENCY LIGHT AT L1 POSITION (EXTERNAL) INOPERATIVE (GROUND ILLUM) L388. CLEANED CORROSION AT CONNECTOR IAW B767 MM 33-51-06. OPS CHECKED GOOD. 2L72 4F RTA1NM 20050517000232005051700023EU 2005 5 17 F3LA200500017 120050425A2120 SMOKE AIRBUSA319 A319112 3930323EU CABIN DETECTED A F3LAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM03910FR 1781 FLIGHT ATTENDANTS AND PASSENGERS REPORTED ODOR OF SMOKE ON FLIGHT FROM MZT TO DEN. FLIGHT CREW DECLARED AN EMERGENCY AND DIVERTED TO ELP. AIRCRAFT LANDED WITHOUT INCIDENT. TROUBLESHOT SMOKE IN CABIN PER MM 26-17-00-810-804, LAV SMOKE WARNING, NO DEFECTS NOTED; AND PER MM 12-33-21-618-09-02, PRECONDITIONING CHECK OF APU, NO DEFECTS NOTED; AND PER MM 31-50-00-710-01, GROUND SCANNING OF CENTRAL WARNING SYSTEM, NO DEFECTS NOTED. 2L72 4F RTA28NM 20050517000262005051700026SO 2005 5 17 20030836 120050425A3350 CONNECTOR EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT LOOSE A GLBAO OTHER O OTHER TXTAXI/GRND HDL 1 NM03108UX 120108 EMERGENCY LIGHTS OVER ROW 5AQ DIM. MAINTENANCE RESEATED LOOSE CONNECTOR. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA31SO 20050517000272005051700027WP 2005 5 17 AALA20050286 120050423A3350 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21411AA 49322 SFO - EMERGENCY EGRESS LIGHT INOPERATIVE AT ROW 20 AFT. REPLACED BATTERY FOR EMERGENCY EGRESS LIGHT AT ROW 20 AFT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050517000302005051700030NM 2005 5 17 AALA20050283 120050421A3350 LIGHT BOEING737 737823 13844BZNM ROW 12 INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21936AN 29532 DFW - AFT SEAT MOUNTED EMERGENCY LIGHTS AT ROW 12 HAS ONE LAMP INOPERATIVE. REPLACED AFT SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AT ROW 12. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20050517000322005051700032NM 2005 5 17 AALA20050282 120050421A3350 LIGHT BOEING737 737823 13844BZNM ROW 17D INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21936AN 29532 DFW - SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AT 17D HAS ONE LAMP INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20050517000332005051700033WP 2005 5 17 AALA20050285 120050424A3210 LANDING GEAR DOUG DC9 DC982 3022082WP INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW21241AA 49254 BNA - EN ROUTE BNA-DFW LANDING GEAR WOULD NOT RETRACT. RETURNED BNA AND LANDED WITHOUT INCIDENT. PINNED GEAR AND RECYCLED GROUND DOOR RELEASE HANDLE. NO OTHER DEFECTS NOTED. FCF COMPLETED AND GEAR RECYCLED AND OPERATES NORMAL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050517000342005051700034NM 2005 5 17 AWXA200500497 120050423A56105893543140 WINDSHIELD BOEING737 7373Y0 1384671NM COCKPIT CRACKED A AWXAO OTHER O OTHER CRCRUISE 1 WP28334AW4754919292 23747 EN ROUTE FROM LAS TO SEA FLIGHT CREW NOTICED THE FIRST OFFICERS WINDSHIELD ARCING AT THE WINDOW HEAT SENSOR ON LOWER PART OF THE WINDSHIELD, AFTER A FEW MINUTES PASSED THE WINDSHIELD CRACKED. ACFT DESCENDED TO A LOWER ALTITUDE, DID NOT DECLARE AN EMERGENCY. MAINTENANCE REMOVED AND REPLACED FIRST OFFICERS WINDSHIELD IAW T/C R1B56001, INSPECTED WIRING AND PERFORMED WINDOW HEAT CHECK, SYSTEM CHECKED GOOD. DUE TO HIGH TIME ON THE WINDSHIELD A FAILURE ANALYSIS REPORT WILL NOT BE REQUESTED. 2L72 4F RTA16WE 20050517000352005051700035NM 2005 5 17 AWXA200500498 120050329A52105079454 SKIN BOEING737 737301 1384611NM L-1 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 DURING C-19 CHECK A .5 INCH CRACK WAS FOUND IN L-1 DOOR INNER WEB SKIN AT 4TH DOOR STOP FROM THE TOP BS 342, STR 14 LT. MAINTENANCE CUT OUT DAMAGE IN L-1 DOOR INNER WEB SKIN AT BS 342, STR 14 LT; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 51-70-13. 2L72 4F RTA16WE 20050517000362005051700036 2005 5 17 AWXA200500499 420050426A34142083111 INDICATOR BOEING737 7373S3 1384711NM MACH AIRSPEED MALFUNCTIONED A AWXAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 WP28314AW52014820 23733 PHX - ABORTED TAKEOFF - FLT 0583 - ON TAKEOFF ROLL AT PHX EN ROUTE FOR GEG CAPTAINS AIRSPEED INDICATOR AT 200 KTS AND CLIMBING RAPIDLY WITH OFF FLAG, FIRST OFFICERS AIRSPEED INDICATOR AT 80 KTS, REJECTED TAKEOFF AT 90 KTS AND RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED CAPTAINS AIRSPEED INDICATOR, OPERATIONAL CHECK WAS GOOD. REPORTS REVEAL NO FAULT FOUND ON THIS UNIT. UNIT WAS INSPECT AND TESTED IAW CMM 34-12-02 REV 1. 2L72 4F RTA16WE 20050517000372005051700037SO 2005 5 17 PNSA050402 120050422A2434ALY6521 ALTERNATOR PIPER PA32 PA32301 7103207SO ENGINE MALFUNCTIONED E PNSAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 AL0381052 132 328206023 DURING CRUISE, ODOR OF SOMETHING BURNING AND AT SAME TIME NOTICED 0 CHARGE ON AMMETER. MAINTENANCE FOUND ALTERNATOR BAD AND INSPECTED WIRING HARNESS WITH NO DEFECTS FOUND. CHANGE ALTERNATOR AND AIRCRAFT RETURNED TO SERVICE. 1L71 3O A3SO 20050517000392005051700039EA 2005 5 17 ASOA05337 120050414A5330 DOUBLER CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27827AS 7212 DURING AN A-CHECK, THE FS 640 RH DOUBLER, FS 640 RT FRAME AND BONDED SKIN DOUBLER AT RT FS 640, STRINGER 8-13 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FS 640 RT DOUBLER AND THE FS 640 RT FRAME. MAINTENANCE IS ALSO REPAIRING THE BONDED SKIN DOUBLER AT RT FS640, STRINGER 8-13 IAW REO. (K) 2L72 4F RTA21EA 20050517000402005051700040EA 2005 5 17 ASOA05336 120050414A5242H34455 HANDLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE E/E BAY DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27821AS 7194 DURING A C-CHECK, THE MAIN AVIONICS BAY DOOR HANDLE WAS FOUND CRACKED AT THE BASE. MAINTENANCE IS REMOVING AND REPLACING THE MAIN AVIONICS BAY DOOR HANDLE. (K) 2L72 4F4 FRTA21EA E15NE 20050517000422005051700042EA 2005 5 17 ASOA05334 120050414A3350BC10020004 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN DEFECTIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27839AS 7284 DURING HANGAR MAINTENANCE, THE AFT MOST EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT MOST EMERGENCY CEILING LIGHT ASSY. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050517000432005051700043EA 2005 5 17 ASOA05257 120050320A27409960013 SWITCH BOMBDR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TRIM DISCONNECT MALFUNCTIONED A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27821AS 559 7194 DURING CLIMB OUT, BETWEEN 3,000 TO 4,000 FT, CREW RECEIVED A STAB TRIM AND MACH TRIM DISCONNECT CAUTION MESSAGE. CREW LEVELED AC OFF TO 4,000 FT, SLOWED TO 200 KNOTS TO COMPLY WITH QRH, WHICH DID NOT RESOLVE PROBLEM. THE AC RETURNED TO DEPARTURE. UPON APPROACH, WHEN ADVANCING THE FLAPS TO 8 DEGREES AND THEN TO 20 DEGREES, FORWARD PRESSURE WAS REQUIRED AT WHICH TIME THE CREW REQUESTED EMERGENCY VEHICLES BE PLACED ON STANDBY AS A PRECAUTION. AC LANDED SAFELY. MAINT REMOVED AND REPLACED F/O TRIM DISCONNECT SWITCH; AND ALSO PERFORMED FULL HORIZ STAB TRIM CONTROL UNIT OPS CHECK. OPS CHECK GOOD. AC OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050517000442005051700044 2005 5 17 SA05040 420050418A2565D30665105 SLIDE AIRBUSA319 A319112 3930323EU PASSENGER CABIN DEFLATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19713UW18922920 1040 THE AFT LEFT DOOR SLIDE DEPLOYED WITHOUT INFLATING. MAINTENANCE REPLACED THE AFT LEFT EMERGENCY ESCAPE SLIDE. 2L72 4F RTA28NM 20050517000472005051700047EA 2005 5 17 ASOA05333 120050413A5730 SKIN PANEL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT WING CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27821AS 7194 DURING A C-CHECK, THE LOWER WING PLANK AT WS 148.019 LT/RT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LOWER WING PLANK AT WS 148.019 LT/RT IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050517000482005051700048EU 2005 5 17 SA05043 120050419A5610NP1653116 WINDSHIELD AIRBUSA319 A319112 3930323EU COCKPIT CRACKED A USAAHA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING O OTHER CLCLIMB 1 EA19176UW14124 1499 CLT FLT 1086 ENROUTE CLT - BDL, AFTER TAKEOFF, THE FIRST OFFICER'S WINDSHIELD CRACKED. THE CREW PULLED CIRCUIT BREAKER AF3 FOR THE WINDSHIELD HEAT AND RETURNED TO FIELD CLT. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FIRST OFFICER'S WINDSHIELD. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20050517000512005051700051EA 2005 5 17 ASOA05331 120050412A5210601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27860AS 7433 DURING HANGAR MAINTENANCE, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. (K) 2L72 4F4 FRTA21EA E15NE 20050517000522005051700052EU 2005 5 17 ASOA05256 120050318A7921S5411279400000 DOOR AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE OIL COOLER OPEN A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27637AS 383 DURING T/O, FOLLOWING GEAR UP TRANSITION THE CREW FELT A LARGE BUMP FROM THE LT SIDE OF THE AC. AT APPROX 4,000 FT A PASSENGER REPORTED SEEING SOMETHING HANGING FROM JUST BEHIND THE PROP, WHICH WAS CONFIRMED BY THE F/O UPON FURTHER INVESTIGATION. THE CREW ALSO NOTICED A TORQUE INCREASE TO JUST OVER 100 PERCENT ON THE LT ENGINE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED, LANDING SAFELY. MAINT FOUND THE LT AFT ENGINE OIL COOLER DOOR OPEN, REMOVED AND REPLACED IT. MAINT PERFORMED ENGINE GROUND RUNS IAW MM. ALL OPS CHECK GOOD. AC OK FOR SERVICE. (K) 2H72 4T4 TRTA53EU E20NE 20050517000532005051700053EU 2005 5 17 DHL2005367511 120050403A5347TMS6022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU CABIN CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01367DH 265 DURING "C" CHECK, CABIN SEAT TRACK AT FS 21 AT BL 0 HAS CORROSION (MKD.) REPLACED SEAT TRACK SECTION BS 1303-1780 BL0 IAW SRM 51-30-30 AND 53-10-10 162 INCH LONG MAT USED TMS 60-22457 P/O 2113624. 2L72 4F RTA35EU 20050517000562005051700056EA 2005 5 17 ASOA05329 120050410A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE MAIN PAX MALFUNCTIONED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27824AS 7203 DURING A GROUND INSPECTION, THE FLIGHT ATTENDANT REPORTED THE PASSENGER DOOR STIFF TO OPEN AND CLOSE. MAINT OPERATED THE PASSENGER DOOR WITH NO DEFECTS NOTED. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050517000582005051700058EA 2005 5 17 ASOA05328 120050409A3350110049 BATTERY CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE EMERGENCY LIGHT DAMAGED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27722EV3578 10127 DURING A GROUND INSPECTION, THE LEFT AFT EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE FOUND AND RESCURED A RECESSED PIN IN THE NR4 EMERGENCY BATTERY TERMINAL BLOCK. OPERATIONAL CHECKS GOOD. AC OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA EOOO63EN 20050517000592005051700059EA 2005 5 17 A6WA200540111 120050316A5712 RIB CNDAIRCL600 CL6002B19 1900309EA RT WING WW CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31415AW 7593 RIGHT MLG WHEEL WELL AT WS 48.3O FS 523.8 BATTERY RIB IS CRACKED APPROX 1 INCH. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER IAW BOMBARDIER INC REO 601R-57-57-046 REV B. (M) 2L72 4F RTA21EA 20050517000602005051700060EA 2005 5 17 ASOA05271 120050330A3220161271 UPLOCK CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NLG MISALIGNED A ASOAO OTHER J WARNING INDICATION APAPPROACH 1 SO27850AS 7355 DURING APPROACH, CREW RECEIVED A GEAR DISAGREE WARNING MESSAGE ON THE NOSE GEAR. THE QRH WAS COMPLIED WITH AND EMERGENCY WAS DECLARED. AC PERFORMED A FLYBY BUT TOWER WAS UNABLE TO COMFIRM IF NOSE GEAR WAS IN THE DOWN POSITION. UPON FURTHER COMPLETION OF THE QRH, THE GREEN DOWN INDICATOR LIGHT CAME ON. THE AC LANDED SAFELY. MAINT ADJUSTED THE NOSE LANDING GEAR (NLG) UPLOCK PIN IAW EO, CYCLED THE GEAR 50 TIMES AND PERFORMED 5 EMERGENCY GEAR RELEASES. ALL OPS CHECKS WERE GOOD. AC OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050517000612005051700061EA 2005 5 17 ASOA05327 120050409A3260864808 PSEU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE MLG MALFUNCTIONED A ASOAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27860AS9199 6312 7433 DURING CLIMB OUT FROM DEPARTURE, UPON SELECTING GEAR UP, ALL 3 GEARS REMAINED DOWN AND THE CREW RECEIVED AN ANTI-SKID IB MESSAGE ACCOMPANIED BY A PARK BRAKE SOV MESSAGE. THE TOWER DECLARED AN EMERGENCY AS A PRECAUTION AND THE AC RETURNED TO DEPARTURE, LANDING SAFELY. MAINT REMOVED AND REPLACED THE PROXIMITY SENSOR ELECTRONIC UNIT (PSEU); AND ALSO CYCLED THE GEARS SEVERAL TIMES. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050517000642005051700064EA 2005 5 17 ASOA05325 120050408A5210601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27832AS 7243 7243 DURING HANGAR MAINTENANCE, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. (K) 2L72 4F4 FRTA21EA E15NE 20050517000662005051700066EU 2005 5 17 DHL2005367514 120050403A5347TMS6022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01367DH 39174 DURING C-CHECK, CABIN SEAT TRACK AT FR. 18 THRU 21 AT BL 58L HAS CORROSION. REPLACED SEAT TRACK SECTION FROM BS 1393 TO 1446 BLO IAW A-300 SRM 51-30-30 AND 53-10-00 44.0 INCH LONG MAT USED TMS 60-22457 P/O 2113624. 2L72 4F RTA35EU 20050517000672005051700067NE 2005 5 17 ASOA05270 220050329A7200 ENGINE AEROSPATR72 ATR72 EU PWA PW120 PW127 NE LEFT MALFUNCTIONED A ASOAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CRCRUISE 1 SO27641AS 387 DURING CRUISE, THE CREW NOTICED LT ENGINE ITT RISE IN EXCESS OF 800 DEGREES ITT AND REDUCED THE POWER ON THE ENGINE TO BRING IT WITHIN ITT LIMITS AT WHICH TIME THE ENGINE BEGAN TO SURGE. AN EMERGENCY WAS DECLARED AND JUST PRIOR TO THE CREW SHUTTING DOWN THE LT ENGINE, IT RETURNED TO NORMAL AND STOPPED SURGING. THE DECISION WAS MADE TO LEAVE THE LT ENGINE RUNNING AND CONTINUED, AC LANDED SAFELY. MAINT PERFORMED ENGINE RUNS AT ALL POWER SETTINGS IAW MM. NO DEFECTS WERE NOTED. AC OK FOR SERVICE. (K) 2H72 4T4 TRT E20NE 20050517000682005051700068EA 2005 5 17 ASOA05324 120050408A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27913EV 7731 DURING A GROUND INSPECTION, THE LT FORWARD EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINT REMOVED AND REPLACED THE LAMP IN THE LT FORWARD EXTERIOR EMERGENCY LIGHT. OPS CHECK GOOD. AC OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050517000712005051700071NM 2005 5 17 AALA20050288 120050425A3397 WIRE BOEING757 757231 1384950NM EMERGENCY LIGHT DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21727TW 30340 DFW FLOOR LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED FEEDER WIRE AND LENSE SYSTEM FOR FLOOR LIGHTS IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OP. 2L72 4F RTA2NM 20050517000722005051700072EU 2005 5 17 DHL2005367515 120050403A5347TMS6022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01367DH 265 DURING C-CHECK, CABIN SEAT TRACK AT FS 18 THRU 20 AT BL 38L HAS CORROSION. REMOVED CORROSION AT MAIN SEAT TRACK LBL 38 FS 18 TO FS 20 IAW A-300 SRM 51-40-11, MATERIAL LOSS .005 WITHIN LIMITS IAW A-300 SRM 53-10-00. TREATED ALODINED AND PRIMED AND PAINTED THE SEAT TRACK LBL 38 INCH FS 18 TO FS 20 IAW A-300 SRM 51-40-12. 2L72 4F RTA35EU 20050517000752005051700075EA 2005 5 17 ASOA05320 120050408A5210 STRIKER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR SEAL DAMAGED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27876AS 7559 DURING A GROUND INSPECTION, THE PASSENGER DOOR WOULD NOT FULLY LATCH CLOSED AND THE SEAL STRIKER WAS FOUND DAMAGED. MAINT REPAIRED THE PASSENGER DOOR SEAL STRIKER IAW REO. OPS CHECK GOOD. AC OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050517000772005051700077EA 2005 5 17 ASOA05318 120050405A52206003159812 LATCH CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY EXIT MISALIGNED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27862AS11145 7476 DURING A C-CHECK, THE LT OVERWING EMERGENCY EXIT FAILED THE PULL TEST. MAINT ADJUSTED THE LATCH FITTNGS ON THE LT OVERWING EMERGENCY EXIT. OPS CHECK GOOD. (K) 2L72 4F4 FRTA21EA E15NE 20050517000782005051700078EA 2005 5 17 ASOA05317 120050402A3350BR9279106 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27862AS 7476 DURING A C-CHECK, THE EMERGENCY EXIT LIGHT BY THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE AND CRACKED. MAINT REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT BY THE SERVICE DOOR. OPS CHECK GOOD. (K) 2L72 4F4 FRTA21EA E15NE 20050517000792005051700079EA 2005 5 17 ASOA05316 120050407A33501317 LAMP BRUCE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27909EV 7658 DURING A GROUND INSPECTION, THE 2ND OVERHEAD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINT REMOVED AND REPLACED THE LAMP IN THE 2ND OVERHEAD EMERGENCY LIGHT. OPS CHECK GOOD. AC OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050517000802005051700080EA 2005 5 17 ASOA05315 120050406A5712 RIB CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT WING WW CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27820AS 7188 DURING A C-CHECK, THE LT BATT RIB ASSY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LT BATT RIB ASSY AT WS 53.60 IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050517000822005051700082NM 2005 5 17 UPS05444352 120050414A5311 FRAME BOEING747 747200 1384847NM BULKHEAD CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 INSPECTION TYPE: C, RT BS 1480 BULKHEAD NR 11 HOLE FOUND CRACK AT BULKHEAD FRAME RUNNING AFT APPROX 0.040 INCH LONG (CRACK LENGTH .0625 INCH). RIGHT BS 1480 B/H NR 11 HOLE OVERSIZED TO 0.562 INCH & CRACK FREE AS PER EO B747-5310-10732. 2L74 4F RTA20WE 20050517000832005051700083NM 2005 5 17 UPS05444353 120050414A5312 FITTING BOEING747 747200 1384847NM BULKHEAD CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 INSPECTION TYPE:C RIGHT BS 1480 B/H NR 16 HOLE FOUND CRACK AT OUTER CHORD SPLICE FITTING RUNNING OUTBOARD APPROX 0.030 INCH LONG (CRACK LENGTH 0.030 INCH). RIGHT BS 1480 B/H NR 16 HOLE OVERSIZED TO 0.406 INCH & CRACK FREE AS PER EO B747-5310-10732. 2L74 4F RTA20WE 20050517000842005051700084NM 2005 5 17 UPS05444354 120050411A5347 SEAT TRACK BOEING747 747200 1384847NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 INSPECTION TYPE: C, BS 740 RBL 9 SEAT TRACK CORRODED. CORROSION BLEND OUT 0.020 X 2 X 2 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT, SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 4. 2L74 4F RTA20WE 20050517000852005051700085NM 2005 5 17 UPS05444356 120050410A534065B38600Y160 STRINGER CLIP BOEING747 747200 1384847NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 INSPECTION TYPE:C M/D - STA 1980 STR 4R TIE CLIP CORROSION FOUND. CORROSION BLEND OUT 0.016 X 2 X 2 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F RTA20WE 20050517000862005051700086NM 2005 5 17 UPS05444357 120050411A534065B38600170 STRINGER CLIP BOEING747 747200 1384847NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 INSPECTION TYPE:C M/D- BS 1416 STR -1R FRAME TIE CLIP FOUND CORROSION. CORROSION BLEND OUT 0.020 X 0.5 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. TIE CLIP REPLACED AS PER SRM 50-10-01 PG 9. 2L74 4F RTA20WE 20050517000872005051700087NM 2005 5 17 UPS05444358 120050411A534065B38600170 STRINGER CLIP BOEING747 747200 1384847NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 INSPECTION TYPE: C- BS 1460 STR 6R FRAME TIE CLIP FOUND CORROSION. CORROSION BLEND OUT 0.010 X 0.5 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F RTA20WE 20050517000892005051700089NM 2005 5 17 UPS05444360 120050410A534065B38600Y160 STRINGER CLIP BOEING747 747200 1384847NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 INSPECTION TYPE: C, STA 2100 STR 5R TIE CLIP CORROSION FOUND. CORROSION BLEND OUT 0.012 X 0.5 X 0.5 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F RTA20WE 20050517000912005051700091NM 2005 5 17 UPS05544378 120050424A2560 SMOKE GOGGLES BOEING757 75724APF 1384969NM CABIN CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01417UP 23904 AFT PASSENGERS POS, ONE SMOKE GOGGLES FOUND EYESHIELD CRACKED AT NOSE AREA. REMOVED AND REPLACED SMOKE GOGGLES PER EQUIPTMENT FURNISHINGS AMM CHPT 25. 2L72 4F RTA2NM 20050517000922005051700092NM 2005 5 17 UPS05544381 120050427A3350 LIGHT BOEING757 75724APF 1384969NM EMERGENCY EXIT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01448UP 27737 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS ARMED IND LIGHT INOP. RELAMPED EMERGENCY EXIT LIGHTS WITH REF TO MM 33-16-02-2. 2L72 4F RTA2NM 20050517000962005051700096WP 2005 5 17 UPS05844367 120050405A534037540231N FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 INSPECTION TYPE:C1 A PIT AT DOOR CUTOUT APPROX STA 335 HAS 1 EA CRACKED BACK UP FITTING. REMOVED AND INSTALLED BACKUP FITTING AND SPLICES IAW SRM 53-02-00-05, AND 51-1-20D. 2L74 4F RT4A25 20050517000992005051700099WP 2005 5 17 UPS05844370 120050402A5320 INTERCOSTAL DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 INSPECTION TYPE: C1, MAIN CABIN AT STA 1280 L11L INTERCOSTAL HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DC-8 DWG 9756811, 51-1-21 AND 51-1-20D. 2L74 4F RT4A25 20050517001022005051700102WP 2005 5 17 UPS05844375 120050330A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 INSPECTION TYPE: C1, RT WING L/E UPPER RIB CRACKED .25 INCH LONG AT STA XW 754. REPAIRED BY STOP DRILLING AND INSTALLING REPAIR ANGLE IAW SRM 51-1-21, 51-1-20D AND 57-2-0. 2L74 4F RT4A25 20050517001042005051700104EA 2005 5 17 DJFA2005086 120050425A3260327 BULB CNDAIRCL600 CL6002A12 1900304EA NLG INDICATOR BURNED OUT E DJFAO OTHER P NO WARNING INDICATION LDLANDING 1 EA23633CW 3013 CREW REPORTED THAT UPON GEAR EXTENSION THEY DID NOT RECEIVE THE NOSE GEAR DOOR INDICATION. A FLY-BY PAST THE TOWER WAS PERFORMED TO VERIFY NOSE GEAR POSITION. DOOR INDICATION WOULD NOT TEST, AND A MANUAL GEAR EXTENSION WAS PERFORMED. GREEN NOSE GEAR DOOR LIGHT DID NOT ILLUMINATE. A REQUEST WAS MADE TO HAVE FIRE/RESCUE PERSONNEL STANDING BY. AN UNEVENTFUL LANDING WAS PERFORMED IN KSNA. MAINTENANCE REPLACED A 327 BULB FOR THE NOSE LANDING GEAR DOOR INDICATOR. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20050517001092005051700109NM 2005 5 17 72300172 120050426A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 SEVERAL AREAS OF CORROSION ON STRINGER. 2L73 4F4 FRTA3WE E2EA 20050517001132005051700113EA 2005 5 17 ASOA05313 120050402A5320SH670321723 SILL CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27790EV 10066 DURING HANGAR MAINTENANCE, THE RT OB FLOOR SILL PLATE AT FS 280 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINT REPAIRED THE RT OB FLOOR SILL PLATE AT FS 280 IAW EO. (K) 2L72 4F4 FRTA21EA EOOO63EN 20050517001172005051700117NM 2005 5 17 QXEA200500725 120050420A5753 ROLLER DHAV DHC8 DHC8202 2809007NM ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - LEFTHAND NR 4 FLAP TRACK ROLLER SURFACES HAVE CORROSION ON INBOARD AND OUTBOARD FLANGES OF TRACK E. REPAIRED IAW RD 8-57-988. 2H72 4T RTA13NM 20050517001202005051700120NM 2005 5 17 QXEA200500722 120050418A5540 ATTACH FITTING DHAV DHC8 DHC8202 2809007NM ZONE 300 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - RUDDER ATTACH LUG FOR DAMPER HAS GOUGE. REPAIRED IAW HORIZON AIR EA 2-55-107 AND RD 8-55-1544. 2H72 4T RTA13NM 20050517001222005051700122NM 2005 5 17 QXEA200500716 120050418A5340 STOP FITTING DHAV DHC8 DHC8202 2809007NM ZONE 200 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - TOP FORWARD BAG DOOR STOP CHAFED. REPAIRED IAW RD 8-53-3991. 2H72 4T RTA13NM 20050517001232005051700123NM 2005 5 17 QXEA200500720 120050422A5730 PANEL DHAV DHC8 DHC8202 2809007NM ZONE 600 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - RT WING DRY BAY PANEL 622AT FASTENER COUNTER SINK HOLES ARE CORRODED. REPAIRED IAW DHC-8-200 SRM 51-20-51 AND 57-30-00-400-802, PAGE 403-406. 2H72 4T RTA13NM 20050517001242005051700124NM 2005 5 17 QXEA200500723 120050419A5210 SKIN DHAV DHC8 DHC8202 2809007NM ZONE 800 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - MAIN CABIN DOOR SHELL HAS GOUGE AT RED STRIPE. REPAIRED IAW DHC-8-200 SRM 51-20-11 PAGE 3. 2H72 4T RTA13NM 20050517001252005051700125NM 2005 5 17 QXEA200500717 120050418A5340 STOP FITTING DHAV DHC8 DHC8202 2809007NM ZONE 200 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - TOP AFT BAG DOOR STOP CHAFED. REPAIRED IAW RD 8-53-3991. 2H72 4T RTA13NM 20050517001302005051700130NM 2005 5 17 QXEA200500728 120050420A5753 ROLLER DHAV DHC8 DHC8202 2809007NM ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - LEFTHAND NR 4 FLAP TRACK ROLLER SURFACES HAVE CORROSION ON INBOARD AND OUTBOARD FLANGES OF TRACK-C. REPAIRED IAW RD 8-57-988. 2H72 4T RTA13NM 20050517001342005051700134EA 2005 5 17 COMA0560274 120050425A7930 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA RT ENG OIL PRESSILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01976CA 7151 FLIGHT 4946 - RT ENGINE OIL PRESSURE WARNING. ADDED 5.5 QTS OF OIL, C/W OIL CONSUMPTION CHECKS, NO DEFECTS FOUND. 2L72 4F RTA21EA 20050517001362005051700136EA 2005 5 17 COMA0560276 120050426A5330601R3114627 SKIN PANEL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAO OTHER O OTHER NRNOT REPORTED 1 SO01933CA26778 7040 DURING COMPLIANCE OF AN H-6 CHECK, ONE CRACK WAS FOUND IN THE PRESSURE FLOOR SKIN NEAR FS 461 BETWEEN BL 0.0 AND RBL 9.0. THE CRACK WAS 1.5 INCHES LONG. THE PRESSURE FLOOR SKIN WAS REPAIRED IN ACCORDANCE WTIH REO 601R-53-41-102 REV D DATED 9/29/03 AND REO 601R-53-41-162 DATED 6/9/03. OK FOR RETURN TO SERVICE. 2L72 4F RTA21EA 20050517001382005051700138EA 2005 5 17 COMA0560278 120050422A3230601R751461 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA NLG UNRELIABLE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01979CA20282 7159 FLIGHT 5839 - GEAR DISAGREE WARNING. REPLACED THE NLG SELECTOR VALVE. 2L72 4F RTA21EA 20050517001392005051700139WP 2005 5 17 ABXA050098 120050421A5280 BEARING DOUG DC9 DC933F 302207AWP MLG DOORS WORN A ABXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23932AX 47465 DURING GEAR RETRACTION AFTER TAKEOFF, GEAR OPEN LIGHT ILLUMINATED. REMAINED ON FOR INFLIGHT PORTION, EXTINGUISHED DURING GEAR EXTENSION FOR LANDING. REMOVED AND REPLACED WORN BEARINGS AND HINGE PINS ON LEFT AND RIGHT MAIN LANDING GEAR INBOARD DOORS IAW DC-9 OHM 32-13-5. PERFORMED ADJUSTMENT TEST IAW DC-9 AMM 32-30-00-2. PLACARD REMOVED. 2L72 4F A6WE 20050517001402005051700140EA 2005 5 17 COMA0560279 120050423A3010356124310 ELEMENT CNDAIRCL600 CL6002B19 1900309EA ANTI ICE SYSTEM MALFUNCTIONED A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01719CA 7253 FLIGHT 5673- ANTI ICE DUCT WARNING. REPLACED THE LT FUSELAGE SENSING ELEMENT A47WK. 2L72 4F RTA21EA 20050517001412005051700141EA 2005 5 17 COMA0560280 120050423A339759465 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DAMAGED A COMAK NONE O OTHER ININSP/MAINT 1 SO01936CA 7043 FLIGHT 5445 - EMERGENCY FLOOR LIGHTS ARE INOP. REPLACED TRACK LIGHT JUMPER AT ROW 5. 2L72 4F RTA21EA 20050517001432005051700143NM 2005 5 17 AMTA200500335 120050331A5412 SHIM BOEING757 75723N 1384973NM NR 1 NACELLE MIGRATED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11526AT 30735 NR 1 ENGINE STRUT MID BULKHEAD HAS MIGRATING SHIMS AT PP STATION 174 LOWER INBOARD AND LOWER OUTBOARD ATTACH POINTS. REPAIRED PER PART 1 OF ERA 757-54R-5835. (M) 2L72 4F RTA2NM 20050517001462005051700146NM 2005 5 17 AMTA200500336 120050401A5420 BRACKET BOEING757 75723N 1384973NM NR 1 NACELLE CHAFED A AMTAO OTHER O OTHER NRNOT REPORTED 1 GL11526AT 30735 MAIN FRAME, NR 1 ENGINE PYLON WEB UPPER SURFACE CHAFED UNDER BRACKET AT NAC STATION 120. DAMAGE AT PYLON UPPER WEB NAC STATION 120 REPAIRED IAW ER/A NR 757-54R-5846 SEE PARTIAL WORK ABOVE AND M12A NR 747-54R-5846 FOR INDIVIDUAL WORK STEPS. (M) 2L72 4F RTA2NM 20050517001482005051700148EA 2005 5 17 A6WA200540150 120050409A5210G80082 SEAL CNDAIRCL600 CL6002B19 1900309EA PAX DOOR DAMAGED A A6WAO OTHER E VIBRATION/BUFFET CLCLIMB 1 GL31452AW 7835 DOOR SEAL IS LOUD ABOVE 6 DP. VIBRATION NOISE STARTS AT 270 KNOTS IAS. REMOVED AND REPLACED PASSENGER DOOR SEAL. PRESSURE CHECK GOOD. (M) 2L72 4F RTA21EA 20050517001502005051700150NM 2005 5 17 AMTA200500377 120050415A3350D71702001 POWER SUPPLY BOEING757 75733N 1384931NM EMERGENCY LIGHT INOPERATIVE A AMTAK NONE O OTHER ININSP/MAINT 1 GL11550TZ 32584 L4 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED L4 DOOR EMERGENCY LIGHT POWER SUPPLY REF BOEING 757 MM 33-51-07-2. PER FIM 33-51-00 BLOCK 20 REPLACED POWER SUPPLY. OPERATIONAL CHECK NORMAL. (M) 2L72 4F RTA2NM 20050517001522005051700152EA 2005 5 17 A6WA200540144 120050410A331090472 POTENTIOMETER CNDAIRCL600 CL6002B19 1900309EA COCKPIT FAILED A A6WAO OTHER O OTHER CRCRUISE 1 GL31405AW 7362 IN CRUISE FIGHT ED1, ED2, FMS 1 AND 2, RTU 1 AND 2, AND STANDBY RTU DISPLAY ALL WENT BLANK. REMOVED AND REPLACED CENTER PEDESTAL LIGHTING PANEL DISPLAY KNOB POTENTIOMETER. OPS CHECK GOOD IAW AMM 33-12-19. (M) 2L72 4F RTA21EA 20050517001532005051700153EA 2005 5 17 A6WA200540155 120050410A3210601R5721003323 BUSHING CNDAIRCL600 CL6002B19 1900309EA RT MLG TRUNION MIGRATED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31417AW 7610 RIGHT MAIN LANDING GEAR AFT TRUNNION BUSHING MIGRATED .012 INCH. REMOVED MIGRATED BUSHING AND INSTALLED 2ND OVERSIZE BUSHING P/N 601R5721003-2003-23, P/N 601R5721003-23 IAW BOMBARDIER INC REO 601R-57-21-003 REV B. (M) 2L72 4F RTA21EA 20050517001562005051700156NE 2005 5 17 A6WA200540147 220050405A72002810044101 CHECK VALVE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE RT ENGINE STICKING A A6WAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 GL31431AW LOW OIL ENGINE PRESSURE WARNING IN FLIGHT (RED). INDICATED LOW ON GAUGE LOW PRESSURE, COMPLIED WITH QRH. ENGINE SHUTDOWN INFLIGHT. REMOVED AND REPLACED ENGINE NR 2 GEARBOX BB CARBON SEAL AND MATING RING. ALSO, REMOVED AND REPLACED ENGINE NR 2 REPLENISHMENT CHECK VALVE. ALL UNITS LEAK CHECKED GOOD. (M) 2L72 4F4 FRTA21EA E15NE 20050517001572005051700157EA 2005 5 17 A6WA200540125 120050325A49307536893 LINE CNDAIRCL600 CL6002B19 1900309EA APU FUEL SYS CHAFED A A6WAO OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL31443AW 7781 SMELL STRONG FUEL ODOR IN CABIN. REMOVED AND REPLACED CHAFED LINE FROM FUEL SOLENOID TO APU BURNER CAN. REMOVED AND REPLACED AIR PACK COALESCER SOCKS, RAN ENGINES AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050517001582005051700158EA 2005 5 17 A6WA200540129 120050403A5210 DRAG ANGLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A A6WAO OTHER O OTHER NRNOT REPORTED 1 GL31416AW 7603 PASSENGER DOOR AFT DRAG ANGLE IS CRACKED 1 INCH LONG AT THE MOTOR CABLE PULLEY BRACKET. PERFORMED REPAIR TO PASSENGER DOOR AFT DRAG ANGLE IAW BOMBARDIER REO 601R-52-11-513 REV A. (M) 2L72 4F RTA21EA 20050517001592005051700159EA 2005 5 17 A6WA200540148 120050408A2133 OUTFLOW VALVE CNDAIRCL600 CL6002B19 1900309EA CABIN PRESSURE MALFUNCTIONED A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31433AW 7289 AFTER TAKEOFF, AIRCRAFT WOULD NOT PRESSURIZE. RETURNED TO ORD. PER MEL 21-24-06-02 SECURED OVERBOARD VALVE IN THE CLOSED POSITION. PERFORMED OPS TEST, NO DISCREPANCIES NOTED. (M) 2L72 4F RTA21EA 20050517001602005051700160EA 2005 5 17 A6WA200540156 120050412A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FS DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31416AW 7603 LEFT SIDE AFT FUSELAGE SKIN DAMAGED BETWEEN FS 574-621, STRINGERS 17L-19L. MEASURES 2 INCH LONG BY 1 INCH WIDE BY .096 INCH DEEP. INSTALLED EXTERNAL DOUBLER AND TRIPLER TO DAMAGED FUSELAGE SKIN IAW BOMBARDIER, INCH REO 601R-53-61-1039. (M) 2L72 4F RTA21EA 20050517001632005051700163EA 2005 5 17 QXEA200500746 120050419A5210 STRIKER CNDAIRCL600 CL6002C10 1390015EA ZONE 200 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - FUSELAGE AT PASSENGER DOOR OPENING FORWARD BOTTOM SKIN NICKED AND PRESSURE SEAL STRIKER ROUGH IN CONTACT AREA. REPAIRED IAW CRJ700 SRM 51-25-01-001-001-A01 AND HORIZON AIR EA R-53-313. 2L72 4F RTA21EA 20050517001642005051700164EA 2005 5 17 QXEA200500734 120050415A5753 HOUSING CNDAIRCL600 CL6002C10 1390015EA ZONE 500 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - LT WING TRAILING EDGE OUTBOARD FLAP GUIDE ROLLER HOUSING GOUGED AT WING STATION 147.50. REPAIRED IAW CRJ700 SRM 57-51-02-201-001-A01 AND 51-24-11-001-001-A01. 2L72 4F RTA21EA 20050517001652005051700165EA 2005 5 17 QXEA200500735 120050413A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - FORWARD FUSELAGE - BELOW FORWARD BAGGAGE BAY OPENING FUSELAGE STATION 549.00 TO 533.00 BETWEEN STRINGER 25L AND 25R ROCK CHIP PITTING. REPAIRED IAW CRJ700 SRM 51-26-00-001-001-A01, SRM 51-25-01-001-001-A01 AND SRM 53-31-01-101-003-A01. 2L72 4F RTA21EA 20050517001662005051700166EA 2005 5 17 QXEA200500748 120050413A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - LOWER FUSELAGE SKIN AT STATION 981 AND STRINGER 27 HAS TWO GOUGES. REPAIRED IAW CRJ700 SRM 51-42-21-001-001-A01 AND HORIZON AIR EA R-53-307. 2L72 4F RTA21EA 20050517001672005051700167EA 2005 5 17 QXEA200500747 120050412A1430 RIVET CNDAIRCL600 CL6002C10 1390015EA ZONE 100 LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - LOWER FUSELAGE STATION 1098 TO 1108 STRINGER 18 TO 19 RT SKIN HAS FOUR LOOSE RIVETS SMOKING. REPAIRED IAW CRJ700 SRM 51-25-01-001-001-A01, SRM 51-23-00-001-00-A01 AND SRM 51-42-06-001-001-401. 2L72 4F RTA21EA 20050517001702005051700170EA 2005 5 17 QXEA200500739 120050418A7830 STRUCTURE CNDAIRCL600 CL6002C10 1390015EA THRUST REVERSER CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - RT ENGINE UPPER AND LOWER FAN COWLS HAVE CHAFE/WEAR DAMAGE ON THE TORQUE BOX STRUCTURE. REPAIRED IAW REO 670-78-34-364 AND HORIZON AIR EA R-71-104. 2L72 4F RTA21EA 20050512000222005051200022NM 2005 5 12 05FDEA01159 120050428A5340 BRACKET BOEING727 727233 138408ANM LT MLG WW CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25264FE 21626 CORROSION C-53-100-01 AT LEFT MAIN WHEEL WELL, BS 919 WL 189 LBL 65 UPPER SURFACE. WORK TO BE ACCOMPLISHED ON CUSTOMER ID N00428. 2L73 4F RTA3WE 20050512000282005051200028EU 2005 5 12 05FDEA01106 120050423A5330 SKIN AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 IN ACM BAY, ALL SKIN AREAS WHICH HAVE HAD CORROSION REMOVED REQUIRE FLAP PEENING. FLAP PEENED ALL EFFECTED SKIN AREAS IN ACM BAY IAW A310-200 SRM 51-29-00. THIS NR COVERS THE ACM AREA FROM FRAME 39 TO FRAME 47, FROM STRINGER 33L TO 33R, FOR CORROSION REPAIRS THAT WERE WITHIN SRM LIMITS. ALL DOCUMENTS ON FILE AT EADS, W/O 00028159, 0510-0201-0192. 2L72 4F RTA35EU 20050512000292005051200029NM 2005 5 12 05FDEA01141 120050427A5713ARB75102 STRINGER DOUG MD11 MD11F 3023600NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 RIGHT WING NR 3 FUEL TANK, INTERIOR, UPPER STRINGER 8, MOST AFT FOUND WITH CRACK APPROXIMATELY 8 INCHES LONG. CARRIED OUT REPAIR PER SRM 57-20-00 VOLUME I, FIGURE 10. 2L73 4F RTA22WE 20050512000372005051200037 2005 5 12 PIDA20050018 420050501A2297 WIRE BOEING737 737228 13844AGNM YAW DAMPER DAMAGED A PIDAO OTHER J WARNING INDICATION CRCRUISE 1 SO05252TR 23001 YAW DAMPER DISENGAGED DURING FLIGHT AND WILL NOT RE-ENGAGE. PLACED YAW DAMPER ON MEL 22-3-16. REPAIRED BROKEN WIRE PER SWPM 20-30-13. OPS CHECK GOOD PER MM 22-12-01 2L72 4F RTA16WE 20050512000402005051200040CE 2005 5 12 DXTA200500676 120050413A3230H111499 LIMIT SWITCH CESSNA650 650 2076802CE NLG STEERING INOPERATIVE E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07791QS 6507091 MLG WOULD NOT RETRACT. TROUBLESHOT PER 650 WDM AND FOUND FAULTY NLG WHEEL CENTERING SWITCH. R & R NOSE GEAR CENTERING SWITCH PER CESSNA 650 MM CH 32-60-00. DID NOT FIX. AFTER FURTHER TROUBLESHOOTING R & R MLG CONTROL UNIT PER CESSNA 650 MM 32-30-01. OPS CHECK AND GEAR SWING NORMAL. 2L72 4F A9NM 20050513000262005051300026NM 2005 5 13 EIA2005026 120050222A5311 FRAME BOEING747 747273C 1384896NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09471EV 20651 FUSELAGE STA 1000 CHORD IS CRACKED BETWEEN STR 37L-38L NEAR BATHTUB FITTING AT EXTERIOR SIDE UNDER RAM AIR DUCT. REMOVED DAMAGED CHORD FROM STA 1000 BETWEEN STR 37-38 LT AND REPLACED PER B747 SERVICE BULLETIN 747-53A2471 FIG 13 AND EO 53-747-1072-90 REV A PART 2. 2L74 4F A20WE 20050513000282005051300028NM 2005 5 13 EIA2005090 120050404A5310 CREASE BEAM BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 M/D BS 980 S41 CREASE BEAM FOUND CRACKED. CRACKED WEB REPLACED PER SRM 51-30-02 AND 51-10-01. 2L74 4F A20WE 20050513000302005051300030NM 2005 5 13 EIA2005092 120050404A5315 STIFFENER BOEING747 747212B 1384886NM FLOORBEAM CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 U/D B480 FLOORBEAM WEB ATT VERTICAL STIFFENER CRACKED. STIFFENER WAS REPLACED PER SRM 51-10-01. 2L74 4F A20WE 20050513000322005051300032NM 2005 5 13 EIA2005094 120050331A3350 LIGHT BOEING747 747132 1384882NM CABIN INOPERATIVE A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 U/D EMERGENCY LIGHTS RIGHT & LEFT INOP DURING TEST. REPLACED BOTH U/D LEFT & RIGHT EMERGENCY EXIT LIGHTS PER MM 33-51-00 PAGE 1. OPS CHECKED GOOD. 2L74 4F A20WE 20050513000342005051300034NM 2005 5 13 EIA2005096 120050405A5313 STRINGER BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 LEFT BS 1686 AT STRINGER 34L ONE EACH FASTENER HOLE FOUND CRACKED. RUNNING FWD AND AFT 2ND LAYER .0625 INCH APPROX IN LENGTH. THE CRACK TRIMMED OFF AND NDT CONFIRMED CRACK FREE CONDITION. SKIN REPAIRED PER EV EO 53-747-1701-03. 2L74 4F A20WE 20050513000362005051300036NM 2005 5 13 EIA2005098 120050405A5330 SKIN BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 LEFT BS 1708 AT STRINGER 34L ONE EACH FASTENER HOLE FOUND CRACKED AT 9 O'CLOCK POSITION 2ND LAYER .0625 INCH APPROX IN LENGTH. THE CRACK TRIMMED AND NDT CONFIRMED CRACK FREE CONDITION. THE SKIN REPAIRED PER EIA EO 53-474-1701-03. 2L74 4F A20WE 20050513000382005051300038NM 2005 5 13 EIA2005102 120050405A5330 SKIN BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 BS 2230 RT NR 5 DOOR FWD CUTOUT BETWEEN STRINGER 24R AND 25R FOUND CRACKED. BS 2230 RT NR 5 DOOR FWD REVEAL BETWEEN STRINGER 24R AND 25R REPAIRED PER SRM 53-10-04 FIGURE 34. 2L74 4F A20WE 20050513000402005051300040NM 2005 5 13 0500586739 120050307A5311 FRAME BOEING747 747251F 1384898NM FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01639US 23887 DURING LINE CHECK AND IN COMPLIANCE WITH AD 2005-04-51, FOUND CRACK IN FRAME AT BS 460 S12L. REPAIRED PER EA 67-203103. 2L74 4F A20WE 20050513000422005051300042NM 2005 5 13 0500566743 120050316A5312 FITTING BOEING747 747249F 1384849NM BULKHEAD CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01643NW 22245 DURING L-CHECK, FOUND CRACK AND CORROSION AT BS 1480 BULKHEAD CAP FITTING LOWER FLANGE SURFACE BETWEEN S36L AND S40L. REPAIRED PER EA 67-165203. 2L74 4F A20WE 20050513000452005051300045EU 2005 5 13 WRNA200500011 120050423A5280 DOOR AIRBUS300 A300B4203 3930306EU MLG MISSING A WRNAA UNSCHED LANDING DJ INFLIGHT SEPARATION WARNING INDICATION CLCLIMB 1 SO05504TA 216 AFTER TAKEOFF, LEFT MAIN LANDING GEAR SHOWED UNSAFE IN THE RETRACTED POSITION ON BOTH FWD AND F/E INDICATORS. AIRCRAFT LANDED NORMAL. MAINTENANCE PERFORMED A GEAR SWING TEST IAW MM 32-30-00 PAGE BLOCK 501. FOUND LT GEAR DOOR MALFUNCTIONED UPON RETRACTION TEST. REMOVED AND DE-ACTIVATED LT GEAR DOOR IAW 32-00 PAGE 437. ASSIGNED CDL 52-9 LT GEAR DOOR MISSING. 2L72 4F RTA35EU 20050513000472005051300047NM 2005 5 13 UPS05444333 120050414A5312 BULKHEAD BOEING747 747283B 1384867NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 INSPECTION TYPE: C, RT BS 1480 B/H NR 7 HOLE FOUND CRACK AT FX, SKIN RUNNING AFT APPROX .0625 INCH LONG, CRACK LENGTH .0625. HOLE OVERSIZED TO 0.687" AS PER EO B747-5310-10732 AND BUSHING INSTALLED. 2L74 4F A20WE 20050513000522005051300052NM 2005 5 13 UPS05444338 120050409A5311 FRAME BOEING747 747283B 1384867NM FUSLEAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 INSPECTION TYPE: C, M/D BS 240 STR 14L TO STR 14CL FRAME FOUND CRACKED. ( CRACK LENGTH 1.5" ) M/D BS 240 STR 14L TO STR 14CL FRAME REPAIRED AS PER SRM 53-10-04 FIG 11. 2L74 4F A20WE 20050513000542005051300054NM 2005 5 13 UPS05444340 120050409A531365B07618535 STRINGER BOEING747 747283B 1384867NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 INSPECTION TYPE: C, M/D - BS 240-260 STR 11L STRINGER FOUND CRACKED. (CRACK LENGTH .250" ), M/D BS 240-260 STR -11L STRINGER REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050513000702005051300070NM 2005 5 13 AWXA200500492 120050404A523065C2518022 FRAME BOEING737 73733A 1384673NM CARGO DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCN - MAJOR REPAIR - DURING C-19 CHECK A .375 INCH CRACK WAS FOUND IN FORWARD EDGE OF AFT CARGO DOOR AT FASTENER HOLES FOR PULLEY BRACKET BS 801. MAINTENANCE CUT OUT DAMAGED SECTION OF FRAME ON FORWARD EDGE OF AFT CARGO DOOR; FABRICATED A NEW REPLACEMENT FRAME PER DWG 65C25180; INSTALLED REPAIR PART IAW B737-300 51-40-20. 2L72 4F RTA16WE 20050513000732005051300073SO 2005 5 13 C2XA05CL021 120050415A49504952375 BLEED VALVE EMB 145 EMB145LR 3260212SO APU STUCK A C2XAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION APAPPROACH 1 SW2716951 145063 CLE - THE CREW REPORTED A STRONG FUEL ODOR UPON APU START. MAINTENANCE REPLACED THE APU BLEED AIR VALVE AND OPERATIONAL CHECKS WERE GOOD WITH NO FUEL SMELL DURING START. 2L72 4T RTT00011AT 20050516000062005051600006EA 2005 5 16 SWIA200514905 120050424A2740 SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB TRIM INOPERATIVE A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07935SW 7725 CAPTAIN'S STAB TRIM SWITCH INOPERATIVE. REPLACED CAPTAIN'S STAB TRIM SWITCH. OPERATIONAL CHECK GOOD IAW CRJ MM 27-41-00 & 27-41-05. 2L72 4F RTA21EA 20050516000112005051600011EA 2005 5 16 SWIA200514910 120050419A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07430SW 7523 EMERGENCY LIGHT AFT CABIN CEILING FLOODLIGHT INOPERATIVE. REPLACED AFT EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050516000292005051600029EU 2005 5 16 MALA050356 120050414A5753 FLAP TRACK BAC 146 AVRO146RJ85A1500097EU TE FLAP WORN A MALAK NONE O OTHER ININSP/MAINT 1 GL15503XJ E2310 DURING C2 INSPECTION FOUND LEFT AND RIGHT FLAP TRACK SHUTTERS WORN. 2H74 4F RTA49EU 20050516000302005051600030EU 2005 5 16 MALA050357 120050414A5320 BRACKET BAC 146 AVRO146RJ85A1500097EU FUSELAGE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15503XJ E2310 DURING C2 INSPECTION FOUND BRACKET CRACKED AT FRAME 28 LOWER FUSELAGE NEAR MLG FAIRING. 2H74 4F RTA49EU 20050516000322005051600032EU 2005 5 16 MALA050348 120050413A5413 STRINGER BAC 146 AVRO146RJ85A1500097EU NR 4 NACELLE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15503XJ E2310 DURING C2 INSPECTION FOUND A CRACKED STRINGER NR 4 ENGINE ON BULKHEAD AFT OF NOSE COWL. 2H74 4F RTA49EU 20050516000392005051600039NM 2005 5 16 CALA0500122 120050425A53306545773 SKIN BOEING737 7373T0 1384582NM FUSELAGE DELAMINATED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712319 23370 DELAMINATION BETWEEN DOUBLER AND SKIN ON LT SIDE OF FUSELAGE AT STA 727B. REPLACED SKIN PER ECRA 5330-03481. 2L72 4F RTA16WE 20050516000442005051600044NM 2005 5 16 CALA0500127 120050426A5315BAC1505100246 FLOORBEAM BOEING737 7373T0 1384582NM FUSLEAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770330 23460 CABIN FLOORBEAM CORRODED AT STA 328, LBL 29. INSTALLED NEW ANGLE PER SRM 53-10-51. 2L72 4F RTA16WE 20050516000452005051600045NM 2005 5 16 CALA0500129 120050426A5315 FLOORBEAM BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717614 27327 FLOORBEAM CORRODED AT STA 986.5, RBL43. INSTALLED DOUBLER PER ECRA 5321-01209. 2L72 4F RTA16WE 20050516000482005051600048NM 2005 5 16 CALA0500132 120050418A5330654577572 PANEL BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716301 23352 FUSELAGE SKIN CRACKED AT STA 727D, STRINGER 23R. REPLACED PANEL PER ECRA 5331-01178A. 2L72 4F RTA16WE 20050516000622005051600062NM 2005 5 16 CALA0500119 120050423A3350D71701100 BATTERY BOEING737 737824 13844BZNM EMERGENCY LIGHT INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2754241 28953 EMERGENCY EXIT AISLE AND FLOOD LIGHTS ARE INOP IN FIRST CLASS CABIN AND AFT OF ROW 25. REPLACED 2 BATTERIES FOR M1674 AND M1672 AND A FUSE AT M1674 PER AMM 33-51-00-701-801. 2L72 4F RTA16WE 20050516000642005051600064EU 2005 5 16 MALA050349 120050413A5320 ANGLE BAC 146 AVRO146RJ85A1500097EU DOOR SILL DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15503XJ E2310 DURING C2 INSPECTION FOUND THE RIGHT FORWARD SERVICE DOOR SILL ANGLE DENTED BEYOND LIMITS. 2H74 4F RTA49EU 20050516000832005051600083EU 2005 5 16 MALA050345 120050413A5260 RAIL BAC 146 AVRO146RJ85A1500097EU AIRSTAIR CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15503XJ E2310 DURING C2 INSPECTION FOUND INBOARD AIRSTAIR RAIL CORRODED. 2H74 4F RTA49EU 20050516000952005051600095 2005 5 16 DXTA200500693 420050422A3197 CONNECTOR RAYTHNDH125 HAWKER800XP 7150012CE INDICATOR DIRTY E DXTAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL07816QS 258416 WHEN THE APR SYSTEM IS ARMED THE APR GREEN LIGHT COMES ON AND WILL NOT CANCEL. INTEGRATED NR 1 & NR 2 DEEC'S FOR STORED CODES AND NO CODES WERE FOUND. REMOVED CONNECTOR J1 FROM NR 1 & NR 2 DEEC'S, INSPECTED AND CLEANED, NO DISCREPANCIES WERE NOTED, REINSTALLED CONNECTORS. GAINED ACCESS TO APR/SYNC BOX AND REMOVED CONNECTORS J1, J2 & J3. INSPECTED AND CLEANED CONNECTORS, NO DISCREPANCIES WERE NOTED, REINSTALLED CONNECTORS. TAXIED ACRFT TO A HIGH POWER ENGINE RUN AREA. ACCOMPLISHED SEVERAL SATISFACTORY TESTS OF THE AUTOMATIC PERFORMANCE RESERVE SYSTEM AT IDLE AND TAKEOFF POWER, NO DISCREPANCY WAS NOTED AT THIS TIME. ACCOMPLISHED IAW HAWKER 800XP MM 70-00-00 PAGE 530. 2L72 4F RTA3EU 20050516000992005051600099NM 2005 5 16 BB05028 120050409A3397 CONNECTOR BOEING767 7672B7 1385107NM AFT LEFT CABIN DISCONNECTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19655US 25257 CLT - FOUND FLOOR EMERGENCY LIGHTS ON LEFT SIDE, AFT CABIN, INOPERATIVE (LAST THREE LIGHTS). MAINTENANCE RECONNECTED A SOCKET CONNECTOR. 2L72 4F RTA1NM 20050516001032005051600103NM 2005 5 16 P5CA0501343 120050425A361079275515 CONTROLLER BOEING747 74746NF 13848BTNM GE CF6 CF680C2* GL NR 2 ENGINE MALFUNCTIONED A P5CAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA15450PA 30808 706199 AFTER PUSHBACK AND ENGINE START EICAS MESSAGE BLEED 2 OVERHEAT/PRV APPEARED. RETURNED TO GATE. REPLACED NR 2 ENGINE PRV CONTROLLER PER MM 36-11-20. OPS CHECK OK ON RUN UP PER MM 36-11-00. 2L74 4F4 FRTA20WE E23EA 20050516001142005051600114SO 2005 5 16 C2XA05CL027 120050405A3350B6245305 LIGHT EMB 145 EMB145LR 3260212SO MAIN CABIN DOOR INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714993 145289 CLE - CREW REPORTED THAT THE MAIN CABIN DOOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED REMOVED AND REPLACED THE MAIN CABIN DOOR EMERGENCY LIGHT ASSEMBLY. ALL OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20050516001182005051600118EU 2005 5 16 AWXA200500494 120050404A5347D53472133200 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28638AW 455 SAL - MAJOR REPAIR - DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON LT OUTBOARD SEAT TRACK Y1292 AT FR 63 + 18 INCHES. MAINTENANCE CUTOUT DAMAGED SECTION OF SEAT TRACK Y1292 FROM FR 62 + 10 INCHES TO FR 64; FABRICATED A NEW SECTION OF SEAT TRACK, 2 EACH L-PROFILES, AND A DOUBLER; INSTALLED REPAIR PARTS IAW A320 SRM 53-00-15 FIG 202. 2L72 4F RTA28NM 20050516001262005051600126 2005 5 16 2005UALA00368 420050401A2565 BARREL BOEING757 757222 1384956NM PWA 2037 PW2037 NE ASPIRATOR DAMAGED A UALAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP29531UA 25042 DAMAGED ASPIRATOR BARREL. THE EXACT CAUSE OF DAMAGE TO THE ASPIRATOR COULD NOT BE DETERMINED, INVESTIGATION HAS ATTRIBUTED THE CAUSE TO ACCIDENTAL DAMAGE DURING THE LAST PACKING PROCESS. 2L72 4F4 FRTA2NM E17NE 20050517000172005051700017NM 2005 5 17 05FDEA01134 120050426A5314 KEELBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25264FE 21626 CORROSION ON RT KEEL BEAM OUTER FLANGE BS 950D 5 TO 950D 19. REPAIRED RT KEEL BEAM OUTER FLANGE PER FED-EX SR DWG SR27-53-023A. 2L73 4F RTA3WE 20050517000252005051700025SO 2005 5 17 20030835 120050422A3397 WIRE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BROKEN A GLBAO OTHER O OTHER TXTAXI/GRND HDL 1 NM03108UX 120108 EXIT ROW EMERGENCY LIGHTS IN ROW 5A LIGHTS OUT. MAINTENANCE REPAIRED BROKEN WIRES AT OVERHEAD LIGHT AT 5A. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA31SO 20050517000382005051700038SW 2005 5 17 PNSA050303 120050325A7712 INDICATOR SWRNGNSA227 SA227AC 8780603SW NR 1 TORQUE INACCURATE A PNSAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 AL032719H AC713B PILOT REPOTED ON TAKEOFF ROLL THE NR 1 ENGINE POWER LOW, TAKEOFF WAS ABORTED. MX FOUND THAT THE NR 1 TORQUE GAUGE WAS READING WRONG. ALSO FOUND THE NR 1 ENGINE WAS FUEL LIMITED. THE TORQUE GAUGE WAS REPLACED AND THE FUEL FLOW WAS ADJUSTED AS NEEDED. 2L72 4T RTA8SW 20050517000412005051700041EA 2005 5 17 ASOA05335 120050414A2612601R5107083 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CARGO FIRE MALFUNCTIONED A ASOAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27926EV 7843 DURING CLIMB OUT, AT APPROX 5,000 FT THE CREW RECEIVED A CARGO SMOKE WARNING. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. AFTER THE CREW DISCHARGED THE FIRE BOTTLES, THE WARNING WENT OUT. THE AIRCRAFT RETURNED TO DEPARTURE AND LANDED SAFELY. AFTER LANDING THE EMERGENCY SERVICES INSPECTED THE AC AND FOUND NO EVIDENCE OF ANY FIRE OR SMOKE AND THE AC PROCEEDED TO THE GATE. MAINTENANCE REMOVED AND REPLACED THE CARGO FIRE X PANEL AND ALSO THE NR1 AND NR2 FIRE BOTTLES ASSEMBLIES, THE NR1 AND NR2 FIRE BOTTLE SQUIBS AND BOTH CARGO SMOKE DETECTORS. OPS CHECK GOOD. AC OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050517000462005051700046EU 2005 5 17 SA05044 120050419A5610NP1653116 WINDSHIELD AIRBUSA319 A319112 3930323EU COCKPIT CRACKED A USAAH DEACTIVATE SYST/CIRCUITS O OTHER DEDESCENT 1 EA19717UW17683 1069 ON DESCENT INTO BOS, THE FIRST OFFICER'S WINDSHIELD BEGAN TO ARC AND CRACK. CREW FOLLOWED QRH PROCEDURES AND CONTINUED TO BOS. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FIRST OFFICER'S WINDSHIELD. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20050517000882005051700088NM 2005 5 17 UPS05444359 120050411A534065B38600Y160 STRINGER CLIP BOEING747 747200 1384847NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 INSPECTION TYPE: C - BS 1500, STR 3R, FRAME TIE CLIP FOUND CORROSION. CORROSION BLEND OUT 0.029 X 0.5 X 0.5 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS, TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F RTA20WE 20050517000952005051700095WP 2005 5 17 UPS05844366 120050418A523037551721N FITTING DOUG DC8 DC873F 302199FWP CARGO DOOR CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 INSPECTION TYPE: C1, TEE BOLT FITTING FROM A-PIT DOOR STA 285 HAS CORROSION AND MISDRILLED HOLES. REMOVED AND REPLACED TEE BOLT FITTING IAW SRM 51-3-0 & 51-1-20D. 2L74 4F RT4A25 20050517001052005051700105EU 2005 5 17 ASOA05314 120050406A7712311649902 PICKUP AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE LT ENG TORQUE INOPERATIVE A ASOAO OTHER N FALSE WARNING CRCRUISE 1 SO27533AS 460 DURING CRUISE, AT 12,000 FT THE CREW FELT AND HEARD A SUDDEN LOSS OF POWER ON THE LT ENGINE. THE LT TORQUE WAS OBSERVED DOWN BY APPROX 10 PERCENT. JUST PRIOR TO INITIATION OF IMMEDIATE ACTION ITEMS THE TORQUE SLOWLY RETURNED TO NORMAL. SUBSEQUENTLY THE TORQUE EXPERIENCED A SUDDEN INCREASE FROM APPROX 80 PERCENT TO 97 PERCENT. AT THAT POINT THE CREW SHUTDOWN THE LT ENGINE, COMPLIED WITH THE QRH AND DECLARED AN EMERGENCY. THE AIRCRAFT LANDED SAFELY. MAINT REMOVED AND REPLACED THE NR1 IB TORQUE PICK-UP PROBE AND PERFORMED POWER RUNS WITH ALL INDICATIONS BEING NORMAL. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2H72 4T4 TRTA53EU E20NE 20050517001112005051700111NM 2005 5 17 72300174 120050323A5340 STRINGER CLIP BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A .5 X .75 INCH AREA OF CORROSION ON STRINGER CLIP. 2L73 4F4 FRTA3WE E2EA 20050517001312005051700131WP 2005 5 17 MWEA050035 120050426A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT BROKEN A MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 EMERGENCY FLOOR TRACK ALONG GALLEY'S COAT CLOSET HAS BROKEN WIRE AT SPLICE. REPAIRED WIRES BY MEANS OF SLICING. 2L72 4F A6WE 20050517001322005051700132NE 2005 5 17 0500616307 220050424A7230 BLADES BOEING747 747451 1384940NM PWA 4056 PW4056 NE COMPRESSOR BIRD STRIKE A NWAAEJA ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 GL01667US 24222 717561 DURING CLIMB, THE NR 2 ENGINE INGESTED A BIRD. AFTER THE BIRDSTRIKE, THE ENGINE HAD NOTICEABLE VIBRATION. THE ENGINE WAS SHUT DOWN, FUEL WAS DUMPED, AND THE AIRCRAFT RETURNED TO JFK. THE LANDING WAS WITHOUT INCIDENT. MAINTENANCE REPLACED EIGHT PAIRS OF FAN BLADES AND REPAIRED DAMAGE TO THE FAN ACOUSTIC LINER AND A FAN EXIT GUIDE VANE. AN ENGINE RUN WAS THEN ACCOMPLISHED WITH NORMAL INDICATIONS. 2L74 4F4 FRTA20WE E24NE 20050517001372005051700137EA 2005 5 17 COMA0560277 120050422A3097 TERMINAL BLOCK CNDAIRCL600 CL6002B19 1900309EA LT WING DAMAGED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01917CA 7017 FLIGHT 5105- LEFT WING ANTI-ICE OVERHEAT MESSAGE. REPAIRED INSULATION AT TB11WK. SYSTEM TEST SATISFACTORY. 2L72 4F RTA21EA 20050517001422005051700142EA 2005 5 17 COMA0570046 120050424A53126705311052 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01655CA3662 10134 FS 280 BULKHEAD LOWER WEBS ARE CORRODED IN VARIOUS PLACES ALONG THE BOTTOM EDGE FROM LBL36 TO RBL36. REPLACED THE FS 280 BULKHEAD LOWER WEBS I/A/W BOMBARDIER INC REO 670-53-11-052 REV A, REPAIR NR 2. 2L72 4F RTA21EA 20050517001492005051700149NM 2005 5 17 AMTA200500373 120050416A2730 WARNING LIGHT BOEING757 75723N 1384973NM ELEVATOR ILLUMINATED A AMTAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL11520AT 27976 ON CLIMB-OUT AFTER TAKEOFF, STATUS MSG ELEV ASYM WAS NOTICED. UPON LANDING MESSAGE WENT AWAY NO FAULT BALLS ON L/R SAM COMP. PERFORMED BITE PER FIM 27-09-00 FIG 106. COULD NOT DUPLICATE OK FOR SERVICE. (M) 2L72 4F RTA2NM 20050517001622005051700162EA 2005 5 17 QXEA200500736 120050413A5330 STRINGER CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - FORWARD FUSELAGE - FORWARD BAGGAGE BAY OPENING FUSELAGE STATION 565.00 TO 533.0 EDGE OF LOWER DOOR OPENING CUTOUT CHAFED AT STRINGER 25L. REPAIRED IAW REO 670-53-31-036, HORIZON AIR EA R-53-305 AND CRJ700 SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050517001682005051700168EA 2005 5 17 QXEA200500737 120050413A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 TOOL DAMAGE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - FORWARD FUSELAGE LOWER SKIN PANEL TOOLING DAMAGE TO THE LOWER SKIN AT FUSELAGE STATION 549.00 AND 565.00 BETWEEN STRINGER 24R AND 25R. REPAIRED IAW CRJ700 SRM 51-26-00-001-001-A01, SRM 53-31-01-101-003-A01 AND SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050517001692005051700169EA 2005 5 17 QXEA200500730 120050414A5753 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 500 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - LT INBOARD FLAP LOWER SKIN HAS GRAVEL DAMAGE. REPAIRED IAW HORIZON AIR EA R-57-113, REO 670-57-52-024 AND CRJ700 SRM 51-25-101-001-001-A01. 2L72 4F RTA21EA 20050517001722005051700172EA 2005 5 17 QXEA200500742 120050419A5753 ARM CNDAIRCL600 CL6002C10 1390015EA ZONE 600 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - RT WING INBOARD FORWARD FLAP HINGE ARM AFT EDGE IS GOUGED. REPAIRED IAW REO 57-54-005, HORIZON AIR EA R-57-117 AND CRJ700 SRM 51-24-11-001-001-A01. 2L72 4F RTA21EA 20050517001742005051700174EA 2005 5 17 QXEA200500738 120050409A5755 FASTENER CNDAIRCL600 CL6002C10 1390015EA ZONE 600 LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - RIGHTHAND WING MULTI FUNCTION SPOILER LOWER COMPOSITE SHROUD TWO FASTENERS FOUND LOOSE AT CENTER HINGE OF INBOARD SPOILER AND OUTBOARD HINGE OF OUTBOARD SPOILER. REPAIRED IAW CRJ700 SRM 51-42-13-001-001-A01. 2L72 4F RTA21EA 20050517001752005051700175EA 2005 5 17 QXEA200500740 120050420A7830 TORQUE BOX CNDAIRCL600 CL6002C10 1390015EA ZONE 400 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - LT ENGINE UPPER AND LOWER FAN COWLS HAVE CHAFE/WEAR DAMAGE ON THE TORQUE BOX STRUCTURE. REPAIRED IAW REO 670-78-34-304 AND HORIZON AIR EA R-71-103. 2L72 4F RTA21EA 20050517001762005051700176EA 2005 5 17 QXEA200500745 120050405A5755 FASTENER CNDAIRCL600 CL6002C10 1390015EA ZONE 600 LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - RIGHTHAND WING UPPER SKIN, TRAILING EDGE HAS LOOSE FASTENERS BETWEEN TWO MULTI FUNCTION SPOILERS. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20050517001782005051700178EA 2005 5 17 QXEA200500733 120050413A5753 FITTING CNDAIRCL600 CL6002C10 1390015EA ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - RIGHTHAND OUTBOARD FLAP INBOARD ROLLER FITTING HAS FRETTING CORROSION. REPAIRED IAW REO 670-57-53-015 AND CRJ700 SRM 51-25-16-001-001-A01. 2L72 4F RTA21EA 20050517001832005051700183EU 2005 5 17 AWXA200500501 120050425A3350321454 POWER SUPPLY AIRBUS320 A320231 3930325EU EMERGENCY LIGHT DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28620AW4949419126 052 LAS - EEL - FLIGHT CREW REPORTED THE FORWARD EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT FORWARD EMERGENCY POWER SUPPLY UNIT (10WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050517001852005051700185EU 2005 5 17 AWXA200500503 120050403A5310D53480043203 BEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28638AW 455 SAL - MAJOR REPAIR - DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SILL BEAM AT -Y1270 RT, FS 68. MAINTENANCE CUTOUT CORRODED SECTION OF LOWER SILL BEAM AT -Y1270 RT FROM FR 68+3" TO FR 68+7"; FABRICATED A REPAIR ANGLE; INSTALLED REPAIR PART IAW A320 SRM 53-41-14, FIG 201. 2L72 4F RTA28NM 20050517001862005051700186EU 2005 5 17 AWXA200500504 120050403A5320D53480020437 WEB AIRBUS320 A320232 3930326EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28638AW 455 SAL - MAJOR REPAIR - DURING C-08 CHECK, A 1/2 INCH CRACK WAS FOUND ON WEB (TRAY) AT -Y1260 RT, BETWEEN FS 68 AND FS 69. MAINTENANCE REMOVED CRACKED WEB AT -Y1260 RT FROM FS 68 TO FS 69; RECEIVED AND INSTALLED NEW REPLACEMENT WEB IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050517001882005051700188EU 2005 5 17 AWXA200500506 120050403A5347D53472190205 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28638AW 455 SAL - MAJOR REPAIR - DURING C-08 CHECK, EXFOLIATION CORROSION WAS FOUND ON SEAT RAIL BEAM -Y1292 AT FS 66 HARD POINT. MAINTENANCE REMOVED CORRODED SECTION OF BEAM -Y1292 FROM FS 64 TO FS 66; RECEIVED AND INSTALLED NEW REPLACEMENT BEAM IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050517001892005051700189EU 2005 5 17 AWXA200500507 120050403A5315D5347209000300 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28638AW 455 SAL - MAJOR REPAIR - DURING C-08 CHECK, EXFOLIATION CORROSION WAS FOUND ON BEAM -Y765 AT FS 66 HARD POINT. MAINTENANCE REMOVED CORRODED SECTION OF BEAM -Y765 FROM FS 66 TO FS 68+4"; RECEIVED AND INSTALLED NEW REPLACEMENT BEAM IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050517001902005051700190EU 2005 5 17 AWXA200500508 120050403A5315D53472172220290 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28638AW 455 SAL - MAJOR REPAIR - DURING C-08 CHECK, CORROSION WAS FOUND ON BEAM Y1292 AT FR 67. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 FROM FS 66 TO FS 68; FABRICATED A NEW REPLACEMENT BEAM PER DWG D53472172; INSTALLED REPAIR PART IAW A320 SRM 51-42-11. 2L72 4F RTA28NM 20050517001912005051700191EU 2005 5 17 AWXA200500509 120050404A5347D53371110010 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28638AW 455 SAL - MAJOR REPAIR - DURING C-08 CHECK, GALVANIC CORROSION WAS FOUND ON RT INBOARD SEAT TRACK -Y765 AT FR 42+17". MAINTENANCE REMOVED CORRODED SECTION OF RT INBOARD SEAT TRACK -Y765 AT FR 42+17"; RECEIVED AND INSTALLED NEW REPLACEMENT BEAM IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050517001922005051700192NM 2005 5 17 AWXA200500510 120050331A5330654577811 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - DURING C-19 CHECK, A 5/8 INCH CRACK WAS FOUND IN R-2 DOOR CUTOUT AT FASTENER HOLE IN THE FORWARD LOWER CORNER BS 961, STR 17 RT. MAINTENANCE TRIMMED OUT DAMAGE IN SKIN AT R-2 DOOR CUTOUT IN FORWARD LOWER CORNER BS 961, STR 17 RT; FABRICATED A FILLER, 2 EACH DOUBLERS, AND A TRIPLER; INSTALLED REPAIR PARTS IAW ER 03-5300-05111-ES1. 2L72 4F RTA16WE 20050517001932005051700193 2005 5 17 RAIA00504015 420050415A3418C850176 SENSOR JETAIRJETSTMJETSTM4101 1500501EU STALL WARNING INOPERATIVE A RAIAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 CE03574HK111261594 41093 FLT 5544 - STL - LEFT STALL WARNING INDICATION. MAINTENANCE REMOVED AND REPLACED LT STALL SENSOR. 2L72 4T RTA41NM 20050517001962005051700196SO 2005 5 17 C2XA05TY037 120050425A532214525175001 SHEAR TIE EMB 145 EMB145XR 3260214SO FUELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716149 145753 DURING A SCHEDULED 1C INSPECTION CORROSION WAS FOUND ON FRAME TO SKIN SHEAR TIE LOCATED AT FRAME 65, STRINGER 15L. MAINTENANCE FABRICATED AND INSTALLED A NEW SHEAR CLIP AS PER EMBRAER IC. AIRCRAFT TO BE RELEASED TO SERVICE FOLLOWING COMPLETION OF SCHEDULED 1C INSPECTION. 2L72 4F RT 20050517001972005051700197SO 2005 5 17 C2XA05CL028 120050425A2120 ODOR EMB 145 EMB145ER 3260211SO CABIN DETECTED A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2715932 145015 PIT FLT 2864, THE CREW REPORTED AN ELECTRICAL BURNING ODOR. CLEVELAND SENT A MAINTENANCE CREW TO INSPECT AND TROUBLESHOOT THE ODOR, THE MAINTENANCE CREW FOUND A MAGAZINE BLOCKING THE HEATING VENT AND COULD NOT DUPLICATE THE REPORTED CONDITIONS. 2L72 4F RTT00011AT 20050517001982005051700198WP 2005 5 17 0500629866 120050427A5312 STIFFENER DOUG DC9 DC951 3022051WP BULKHEAD CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01775NC 47785 DURING "H" CHECK, FOUND CRACK IN BULKHEAD VERTICAL STIFFENER AT BS 855 LBL 15. REPAIRED PER EA 98-202966. 2L72 4F RTA6WE 20050517001992005051700199WP 2005 5 17 ASMF200504022 120050427A7711LG80E1 COMPUTER DOUG DC9 DC983 3022083WP RIGHT EPR FAILED W ASMFK NONE L NO TEST ININSP/MAINT 1 SW23838AM15749 49397 DURING TRANSIT CHECK, CAPTAIN REPORTED WRONG EPR'S INDICATION IN RIGHT ENGINE, IT JUST INDICATES 1. EPR'S TRANSMITTER WAS REPLACED AN DURING PNEUMATIC LEAK TESTS TO PT2 AND PT7 LINES WAS DETECTED PT7 FLEXIBLE LINE FROM PYLON TO RIGHT ENGINE DISCONNECTED. IT WAS RECONNECTED AND ENGINE RUN INDICATION TEST WAS PERFORMED IAW MM 7711-00 TESTED CORRECT. 2L72 4F RTA6WE 20050517002002005051700200NM 2005 5 17 WRNA200500012 120050428A272060130011 ACTUATOR BOEING747 7472U3B 1384846NM ZONE 300 UNSERVICEABLE A WRNAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO05923FT 22769 RUDDER RATIO LIGHT ILLUMINATED WHILE ACCELERATING TO 230KTS IND. AIRCRAFT RETURNED TO AIRFIELD. LANDING NORMAL. REMOVED AND REPLACED LOWER RUDDER LINEAR ACTUATOR IAW 27-21-12. FUNCTIONAL CHECK SATISFACTORY, AIRCRAFT RETURNED TO SERVICE. 2L74 4F RTA20WE 20050517002012005051700201EA 2005 5 17 QXEA200500750 120050412A5350 CHANNEL CNDAIRCL600 CL6002C10 1390015EA ZONE 100 WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - LOWER FUSELAGE AFT WING TO BODY FAIRING HAS CENTRAL C-CHANNEL WORN. REPAIRED IAW HORIZON AIR EA R-53-307. 2L72 4F RTA21EA 20050517002022005051700202EA 2005 5 17 QXEA200500753 120050413A7110 STRIKER CNDAIRCL600 CL6002C10 1390015EA ZONE 400 WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - LEFT HAND ENGINE, CORE COWL LOWER, BELOW OF DOOR LATCH STRIKER PLATE IS WORN. REPAIRED IAW CRJ700 SRM 51-24-16-001-001-A01, 51-42-06-001-001-A01, AND 51-42-13-001-001-A01. 2L72 4F RTA21EA 20050517002032005051700203EA 2005 5 17 QXEA200500754 120050413A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - FORWARD FUSELAGE, BELOW FORWARD BAGGAGE BAY OPENING FS 565 TO FS 581, BETWEEN STRINGER 26L AND STRINGER 27L ROCK CHIP PITTING IN SKIN PANEL. REPAIRED IAW CRJ700 SRM 53-31-01-101-003-A01, 51-25-16-001-001-A01, AND 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050517002042005051700204EA 2005 5 17 QXEA200500755 120050413A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - FORWARD FUSELAGE, BELOW FORWARD BAGGAGE BAY OPENING FS 581 TO FS 594 BETWEEN STRINGER 27R AND STRINGER 26R ROCK CHIP PITTING IN SKIN PANEL. REPAIRED IAW CRJ700 SRM 53-31-01-101-003-A01, 51-12-00-001-001-A01, 51-25-16-001-001-A01, AND 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050517002052005051700205EA 2005 5 17 QXEA200500749 120050407A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - LOWER FUSELAGE SKIN AT FS 975 AND STRINGER 27 HAS GOUGE CAUSED BY WING/FUSELAGE FAIRING CENTRAL CHANNELS. REPAIRED IAW CRJ700 SRM 51-42-21-001-001-A01 AND SRM 51-25-16-001-001-A01. 2L72 4F RTA21EA 20050517002072005051700207EA 2005 5 17 QXEA200500752 120050413A5310 STRUCTURE CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - LOWER FUSELAGE IN WHEEL WELL HAS LOOSE DIAPHRAGM AT UPPER ATTACH SCREWS AND CHAFING DAMAGE. REPAIRED IAW CRJ700 SRM 51-42-001-001-A01, SRM 51-42-06-001-001-A01, AND SRM 51-42-21-001-001-A01. 2L72 4F RTA21EA 20050517002082005051700208EU 2005 5 17 05FDEA01139 120050426A5315 FLOORBEAM AIRBUS300 A300B4605R 3930308EU FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25662FE 761 AFT CARGO COMPT CEILING M CABIN FLOORBEAM C-59 RT UNDERNEATH SEAT TRACK 3-4 HAS CRACK. REPAIRED AFT CARGO COMPT CEILING MAIN CABIN FLOORBEAM C-59 RT. UNDERNEATH SEAT TRACK IAW EA 6-5310-87788 REF N00016. 2L72 4F RTA35EU 20050517002142005051700214EA 2005 5 17 QXEA200500758 120050411A5754 PANEL CNDAIRCL600 CL6002C10 1390015EA ZONE 500 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - LEFT WING INBOARD FLAP VANE LEADING EDGE PANEL HAS CHAFED MARK. REPAIRED IAW CRJ700 SRM 57-52-02-101-001-A01, 51-21-11-001-001-A01, AND 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050517002192005051700219EU 2005 5 17 05FDEA01154 120050427A5313 STRINGER AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25402FE 201 IN ACM BAY FR 39 - FR 40/41 ON STR 45 L HAS AREAS OF CORROSION. REMOVED CORROSION PER A310 SRM 51-74-10. C/W EA 6-5310-87784, FOUND ALL AREAS TO BE WITH IN LIMITS PER EA 6-5310-87784 AND A310 SRM 53-15-12 INSTALLED FASTENERS PER A310 SRM 51-40-21. RESTORED SURFACE PROTECTION PER A310 SRM 51-75-10. 2L72 4F RTA35EU 20050517002202005051700220EU 2005 5 17 05FDEA01155 120050427A5313 STRINGER AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25402FE 201 IN ACM BAY FR 46 - FR 47 ON STR 46 L HAS AREAS OF CORROSION. REMOVED CORROSION PER A310 SRM 51-74-10 C/W EA 6-5310- 87784, FOUND ALL AREAS TO BE WITH IN LIMITS PER EA 6-5310-87784 AND A310 SRM 53-10-00. INSTALLED FASTENERS PER A310 SRM 51-40-21, RESTORED SURFACE PROTECTION PER A310 SRM 51-75-10. 2L72 4F RTA35EU 20050517002212005051700221NM 2005 5 17 05FDEA01158 120050428A5310 STRUCTURE BOEING727 727233 138408ANM LT MLG WW CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25264FE 21626 CORROSION AT LEFT MAIN WHEEL WELL, BS 928-932 WL 189 LBL 65 UPPER SURFACE. REPLACED STRINGER 18A PER SRM 51-40-3. 2L73 4F RTA3WE 20050517002232005051700223EU 2005 5 17 05FDEA01165 120050428A5347 SEAT TRACK AIRBUS300 A300B4605R 3930308EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25662FE 761 MAIN CABIN SEAT TRACK R3 AT FRAME 51 HAS CORROSIONON O/B FLANGE REF N00632. REMOVED SEAT TRACK IAW SRM 51-72-10, INSTALLED NEW SEAT TRACK IAW SRM 51-72-10. 2L72 4F RTA35EU 20050517002252005051700225NM 2005 5 17 05FDEA01017 120050415A5512ALC8103503 PANEL DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT NR 35L. BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA#1-5510-82993. 2L73 4F RTA22WE 20050517002272005051700227NM 2005 5 17 05FDEA01023 120050415A555365423309 FITTING BOEING727 727200 138407ENM VERTICAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 VERTICAL STAB TENSION TIE LT AFT FITTING CORRODED. REPAIRED IAW EA 7-5530-86279. 2L73 4F RTA3WE 20050517002282005051700228NM 2005 5 17 05FDEA01039 120050418A1430 FASTENER DOUG MD11 MD11 3023602NM LT WING SPAR WRONG PART A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LT WING, DURING ACCOMPLISHMENT OF EO 1-5750-7-5004 PART 1, SEVEN (7) EACH COUNTERSUNK LOCK FASTENERS COMMON TO TENSION STRAP SUPPORT AND LOWER REAR SPAR CAP, FOUND DIFFERENT WITH HEAD SIZE FROM THE SPECIFIED LOCK FASTENER. LOCATION IS BY XORS= 570.00. INSTALLED HLT623 TYPE FASTENERS IN LIEU OF THOSE CALLED OUT IN EO 1-5750-7-5004. COMPLIED WITH FEDEX EA 1-5750-82944, WINGS - LEFT AND RIGHT OUTBOARD FLAP INBOARD HINGE. TENSION STRAP FASTENER HOLES. 2L73 4F RTA22WE 20050517002292005051700229NM 2005 5 17 05FDEA01040 120050418A1430 FASTENER DOUG MD11 MD11 3023602NM RT WING SPAR WRONG PART A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 RT WING, DURING ACCOMPLISHMENT OF EO 1-5750-7-5004 PART 2, SEVEN (7) EACH COUNTERSUNK LOCK FASTENERS COMMON TO TENSION STRAP SUPPORT AND LOWER REAR SPAR CAP, FOUND DIFFERENT WITH HEAD SIZE FROM THE SPECIFIED LOCK FASTENERS. LOCATION IS BY XORS 570.00. INSTALLED HLT623 TYPE FASTENERS IN LIEU OF THOSE CALLED OUT IN EO 1-5750-7-5004. COMPLIED WITH FEDEX EA 1-5750-82944, WINGS - LEFT AND RIGHT OUTBOARD FLAP INBOARD HINGE. TENSION STRAP FASTENER HOLES. 2L73 4F RTA22WE 20050517002302005051700230NM 2005 5 17 05FDEA01041 120050418A5754 SKIN DOUG MD11 MD11 3023602NM NR 6 SLAT PUNCTURED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 LT WING, PUNCTURED LEADING EDGE SLAT NR 6 AFT FACE SKIN. REPAIRED PER SRM 57-10-00 VOLUME I, FIGURE 1. 2L73 4F RTA22WE 20050517002312005051700231CE 2005 5 17 DJFA2005083 120050415A21506411342 SWITCH BEECH MU300 400A 1155402CE ACM FAILED E DJFAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 EA23431CW RK31 CREW REPORTED THAT WHILE IN CRUISE FLIGHT AT FL 360, THE AIR CONDITIONING FAIL LIGHT ILLUMINATED AND THE EMERGENCY PRESSURIZATION SYSTEM ACTIVATED. AN EMERGENCY WAS DECLARED AND CREW DIVERTED TO KSBA. DURING THE EMERGENCY DESCENT, SMOKE WAS NOTICED IN THE AIRCRAFT. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MX FOUND THE 350 DEG TEMP SWITCH), 400 DEG TEMP SWITCH, AND 53 PSI OVERPRESSURE SWITCH TO FAIL BENCH CHECKS. SWITCHES WERE REPLACED AND GROUND CHECKS WERE PREFORMED WITH NO NOTED DEFECTS. TEST FLT SATISFACTORY, AND AIRCRAFT RETURNED TO SERVICE. 2H72 4F RTA16SW 20050517002322005051700232WP 2005 5 17 ARWA20050403 120050412A242150130003 CONTROL PANEL DOUG DC8 DC863F 302198FWP BUSS PROTECTION FAILED A ARWAD RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TXTAXI/GRND HDL 1 SO19906R 46087 ON TAXI OUT, NR 4 GENERATOR TRIPPED OFF. REMOVED AND REPLACED GCU IN ACCORDANCE WITH M/M 24-20-5. REMOVED AND REPLACE BUSS PROTECTION PROTECTION PANEL IN ACCORDANCE WITH 24-20-7. REMOVED AND REPLACED FREQUENCY LOAD CONTROLLER IN ACCORDANCE WITH M/M 24-10-16. OPERATIONAL CHECK GOOD; ALL SYSTEMS NORMAL ON ENGINE RUN IN ACCORDANCE WITH M/M 71-00. 2L74 4F 4A25 20050517002342005051700234CE 2005 5 17 DXTA200500684 120050418A3211 BRACKET CESSNA500 560CESSNA 2076750CE MLG DAMAGED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07330QS 5600329 AFTER DEPARTURE GEAR UNSAFE LIGHT REMAINED LIT AND HYD PRESS LIGHT ALSO REMAINED ILLUMINATED. GEAR RETURNED TO DOWN AND LOCKED AFTER PERFORMING CHECK LIST ITEMS. REPLACED ALL PARTS OF BRACKET ASSY PER CE500 SERIES COMPONENT M/M 32-20-01, PERFORMED LANDING GEAR RETRACTION/EXTENSION WITH NO DEFECTS NOTED. 2L72 4F RTA22CE 20050518000012005051800001NM 2005 5 18 2005UALA00316 120050409A5753 FAIRING AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE FLAP TRACK CONTAMINATED A UALAA UNSCHED LANDING O OTHER CRCRUISE 1 WP29841UA 1545 SMOKE NOTICED EMANATING FROM LEFT WING AREA. INSPECTED LT IB FLAP TRACK FAIRING. FOUND NO SIGNS OF HYD LEAKS. HYD QTY CHECKED OK. RAN NR 1 ENGINE AND OPERATED FLAPS. ALL OPS NORMAL NO SMOKE OR VAPORS FOUND. FLIGHT CREW REPORTED THAT IT HAD RAINED HARD IN GSO PREVIOUS 24 HRS WHILE AIRCRAFT ON GROUND AND SMOKE-VAPOR STOPPED SHORTLY BEFORE LANDING. VAPORS APPEAR TO HAVE BEEN FROM CONDENSING WATER TRAPPED IN FLAP TRACK FAIRING. DRAIN HOLES CONFIRMED CLEARED DURING POST-FLIGHT INSPECTION. 2L72 4F4 FRTA28NM E40NE 20050518000022005051800002NM 2005 5 18 2005UALA00318 120050409A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29584UA 26706 AFT CARGO FRAME STA 1540, NEAR STR 26L, FRAME DENTED. FRAME DENT WAS CUTOUT AND A DOUBLER REPAIR WAS INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050518000032005051800003NM 2005 5 18 2005UALA00319 120050409A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29584UA 26706 AFT CARGO FRAME STA 1520 AT STR 25L, FRAME IS DENTED. FRAME DENT WAS CUTOUT AND A DOUBLER REPAIR WAS INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050518000042005051800004NM 2005 5 18 2005UALA00320 120050409A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29584UA 26706 AFT CARGO FRAME STA 1500 AT STR 25L-27L. FRAME DENT WAS CUTOUT AND A DOUBLER REPAIR WAS INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050518000062005051800006NM 2005 5 18 2005UALA00323 120050409A5230 CROSSBEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CARGO DOOR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29308UA 23669 AFT PIT CARGO DOOR-SECOND FROM BOTTOM CROSS BEAM WEB IS CRACKED. INSTALLED NESTED DOUBLER L-ANGLE AND STRAP REPAIR TO WEB. 2L72 4F4 FRTA16WE E2GL 20050518000082005051800008NM 2005 5 18 2005UALA00330 120050411A5320 STIFFENER BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE E&E BAY CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29665UA 29237 E & E BAY, BS 246 FLOORBEAM, STIFFENER FLANGE CRACKED AT RBL 16.38 INCHES. CRACKS ON STATION 246 FLOORBEAM STIFFENERS ARE A KNOWN PROBLEM. THIS CRACKED STIFFENER WAS REPLACED WITH NEW. 2L72 4F4 FRTA1NM E24NE 20050518000132005051800013NM 2005 5 18 2005UALA00337 120050411A5551 ATTACH FITTING BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE HORIZONTAL STAB CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29308UA 23669 LT HORIZONTAL STAB REAR SPAR UPPER AFT LUG HAS CORROSION AROUND BOLT HOLE ON AFT FACE OF LUG. REMOVED CORROSION AND REPAIRED LUG. 2L72 4F4 FRTA16WE E2GL 20050518000152005051800015NM 2005 5 18 2005UALA00340 120050414A3260848401 PROXIMITY SENSOR AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE MLG FAILED A UALAO OTHER N FALSE WARNING DEDESCENT 1 WP29852UA 1671 GEAR NOT DOWN AND LOCKED ECAM DISPLAYED. MANUAL EXTENSION WAS SUCCESSFUL. FAULTY SENSOR FIN 34GA. GEAR EXTENDED MANUALLY. REPLACED PROX SENSOR 34GA. 2L72 4F4 FRTA28NM E40NE 20050518000162005051800016NM 2005 5 18 05FDEA01047 120050419A5270 SWITCH BOEING727 727227 1384078NM CARGO DOOR OUT OF ADJUST A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25491FE 21529 MAIN CARGO DOOR B LIGHT CAME ON AT 16,000 FT, DURING CLIMB. FLAPS WERE RETRACTED ALREADY. NO LOSS OF PRESSURIZATION. LIGHT WENT OUT AT 7000 FT DID NOT COME BACK ON. FOUND MAIN CARGO DOOR 'B' SWITCH OUT OF ADJUSTMENT ('A' DOOR LIGHT CAME ON BEFORE 'B' LIGHT) ADJUSTED 'B' SWITCH SO THAT BOTH 'A' AND 'B' COME ON AT THE SAME TIME AND ARE WITHIN SPECIFIED LIMITS PER NASI 727-MM14 SUPPLEMENT MANUAL. A/C OK FOR SERVICE. RII 2L73 4F A3WE 20050518000172005051800017NM 2005 5 18 05FDEA01055 120050420A5530 FITTING BOEING727 727227 1384078NM VERTICAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 VERTICAL FIN TENSION TIE RIB LEFT AFT VERT BOLT HOLE CORRODED A/C AND TENSION TIE SIDE. REPAIRED VERT FIN TENSION TIE RIB LT AFT VERT BOLT HOLE PER FED EX EA 7-5530-86280 2L73 4F A3WE 20050518000182005051800018NM 2005 5 18 05FDEA01056 120050420A5530 FITTING BOEING727 727227 1384078NM VERTICAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 CORROSION VERT STAB TENSION TIE AFT SHEER FITTING UPPER SURFACE. REPAIRED VERTICAL FIN TENSION TIE AFT SHEAR FITTING PER FED EX EA. 7-5530-86280. 2L73 4F A3WE 20050518000192005051800019NM 2005 5 18 05FDEA01048 120050419A5413491B1340014006 STRINGER DOUG MD11 MD11 3023602NM ZONE 400 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 NR 2 ENGINE RT THRUST REVERSER INTERIOR NR 3 STRINGER CHAFED. REMOVED AND REPLACED IAW SRM 51-35-02 VOLUME II. 2L73 4F RTA22WE 20050518000202005051800020NM 2005 5 18 05FDEA01049 120050419A5754 SKIN DOUG MD11 MD11F 3023600NM ZONE 500 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 LEFT WING: LEADING EDGE SLAT NR 1 INBOARD AREA LOWER SURFACE FOUND WITH CHAFFING MARK ABOVE SLAT TRACK NR 1. (OPEN) 2L73 4F RTA22WE 20050518000222005051800022NE 2005 5 18 BB05030 220050422A7200 ENGINE BOEING757 7572B7 1384964NM RROYCERB211 RB211535E4 54555NE RIGHT NOISY A USAAEA ENGINE SHUTDOWN UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 EA19622AU 27201 31217 FL 750 AT THE END OF CLIMB (FL350), CREW REPORTED THE RT ENGINE EXHIBITING LOUD NOISE VIBRATION. CREW REDUCED THRUST ON THE ENGINE, BUT THE VIBRATION CONTINUED. THE ENGINE WAS SECURED AND THE FLIGHT RETURNED TO CUN. (SET: 30 MINUTES.) MAINTENANCE ANALYSIS PENDING. 2L72 4F4 FRTA2NM E12EU 20050518000252005051800025NM 2005 5 18 2005UALA00345 120050415A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29585UA 26709 FWD PIT LEFT SIDE STA 640 FRAME HAS A DENT ABOVE STR 25L - 26L, UPPER FLANGE. FRAME DENT WAS ROUTED OUT AND DAMAGE REMOVED. INSTALLED ANGLE DOUBLER. 2L72 4F4 FRTA2NM E17NE 20050518000262005051800026NM 2005 5 18 2005UALA00346 120050415A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29585UA 26709 FRAME DENTED STA 1340, ABOVE STR 25R. DAMAGE TO THE FRAME WAS TRIMMED OUT AND A J-ANGLE DOUBLER REPAIR WAS INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050518000272005051800027NM 2005 5 18 2005UALA00347 120050415A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29585UA 26709 AFT PIT HAS DENTED FRAME, STA 1520, ABOVE STR 25L, DENT IS IN UPPER FWD RADIUS OF UPPER FLANGE. DENT DAMAGE IN FRAME WAS TRIMMED OUT. REPAIR ANGLE WAS INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050518000282005051800028NM 2005 5 18 2005UALA00348 120050415A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29585UA 26709 AFT PIT STA 1480, FRAME HAS DENT ABOVE STR 26L, UPPER FLANGE. DENT DAMAGE WAS TRIMMED OUT AND A DOUBLER ANGLE REPAIR WAS INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050518000292005051800029NM 2005 5 18 2005UALA00349 120050416A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29585UA 26709 AFT PIT STA 1540 RIGHT SIDE FRAME HAS DENT ABOVE STR 26R, UPPER FLANGE. REMOVED DAMAGE AND INSTALLED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20050518000322005051800032NM 2005 5 18 2005UALA00352 120050416A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29585UA 26709 FRAME AT STA 1440 ABOVE STR 25L DENTED. REMOVED DAMAGE AND INSTALLED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20050518000352005051800035NM 2005 5 18 2005UALA00355 120050416A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29585UA 26709 FRAME AT STA 1460 ABOVE STR 25L IS DENTED. REMOVED DAMAGE AND INSTALLED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20050518000362005051800036NM 2005 5 18 2005UALA00356 120050416A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29585UA 26709 FWD PIT FRAME STA 600 ABOVE STR 25L IS DENTED ON UPPER FLANGE. REMOVED DAMAGE AND INSTALLED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20050518000372005051800037NM 2005 5 18 2005UALA00357 120050416A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29585UA 26709 DENT ON FRAME STA 1580, JUST ABOVE STR 23L, AFT PIT. REMOVED DAMAGE AND INSTALLED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20050518000392005051800039NM 2005 5 18 2005UALA00359 120050417A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29585UA 26709 CABIN FLOORBEAM CAP CORRODED AT BS 324, RBL 60-64 UPPER SURFACE. FLOORBEAM WAS REPAIRED USING REPAIR ANGLES AND STRAP. 2L72 4F4 FRTA2NM E17NE 20050518000402005051800040 2005 5 18 2005UALA00362 420050416A23006225272120 TRANSCEIVER BOEING757 757222 1384956NM PWA 2037 PW2037 NE HF SYSTEM MALFUNCTIONED A UALAA UNSCHED LANDING O OTHER NRNOT REPORTED 1 WP29545UA 25323 RETURNED TO LAX DUE TO LOSS OF HF RADIOS. MAINTENANCE OPERATED SYSTEM ON GROUND AND COULD NOT DUPLICATE THE PROBLEM. THE HF SYSTEM FOR LEFT AND RIGHT SIDE OPERATED NORMALLY ON GROUND. AIRCRAFT HAS FLOWN WITHOUT HF PROBLEMS SINCE 4/19/2005. MAINTENANCE DID REPLACE THE RT HF TRANSCEIVER AND COMPONENT SHOP FINDINGS REPORT INDICATE THAT THERE WERE NO PROBLEMS FOUND WITH THE UNIT. 2L72 4F4 FRTA2NM E17NE 20050518000422005051800042NM 2005 5 18 2005UALA00365 120050407A5320 FLOOR SUPPORT BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29585UA 26709 AFT PIT FLOOR THRESHOLD SUPPORT UPPER AND LOWER SURFACE CORRODED AT STA 1380 TO 1440 RBL 20. DAMAGE CAUSED BY CORROSION IN DOOR CUTOUT AREA AT THE AFT PIT THRESHOLD SUPPORT. PART WAS REPLACED. 2L72 4F4 FRTA2NM E17NE 20050518000432005051800043NM 2005 5 18 2005UALA00366 120050418A5270848401 PROXIMITY SENSOR AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE CARGO DOOR DISCONNECTED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29840UA 1522 FWD CARGO DOOR OPEN INDICATED ON ECAM. CONNECTOR CAME OFF OF THE PROXIMITY SENSOR 28WV. REINSTALLED CONNECTOR ON THE DOOR PROXIMITY SENSOR. 2L72 4F4 FRTA28NM E40NE 20050518000462005051800046 2005 5 18 2005UALA00371 420050413A2562P3030029010 ELT AIRCRUISERS 62774413 BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE SLIDE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29792UA 0506 26934 ELT WAS DAMAGED AND CRACKED. SLIDE/RAFT WAS REMOVED FROM AIRCRAFT AT NORMAL MAINTENANCE INTERVAL. DAMAGED ELT WAS OBSERVED DURING SLIDE/RAFT DISASSEMBLY. THE EXACT CAUSE OF DAMAGE TO THE ELT COULD NOT BE DETERMINED. 2L72 4F4 FRTT0001SE E46NE 20050518000492005051800049NM 2005 5 18 2005UALA00384 120050421A3510964312 HOSE BOEING747 747422 1384935NM PWA 4056 PW4056 NE CREW OXYGEN LEAKING A UALAA UNSCHED LANDING O OTHER CRCRUISE 1 WP29176UA 24383 AFTER LEVEL-OFF A/C LEAK RE-DEVELOPED AND SLOW STEADY PRESSURE DROP. LOCATED OXYGEN HOSE LEAK AT PRESSURE REGULATOR. REPLACED HOSE AND SERVICED CREW OXYGEN BOTTLE. 2L74 4F4 FRTA20WE E24NE 20050518000502005051800050WP 2005 5 18 05FDEA01167 120050428A5743 FITTING DOUG MD10 MD1010F 3022112WP ZONE 700 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25370FE 46608 WINGS-MAIN FRAME-DOOR ASSY-MLG STRUT WING FITTING ATTACH HOLE. COMPLIED WITH EA 8-5710-55481. 2L73 4F RTA22WE 20050518000522005051800052EA 2005 5 18 QXEA200500772 120050413A5330 SKIN PANEL CNDAIRCL600 CL6002C10 1390015EA ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - FORWARD FUSELAGE, FORWARD LOWER SKIN PANEL HAS ROCK CHIP PITTING DAMAGE AT STATION 394 TO 409 BETWEEN STRINGER 24R AND STRINGER 25L. REPAIRED IAW REO 670-53-21-096, AND HORIZON AIR EA R-53-309. 2L72 4F RTA21EA 20050518000542005051800054EA 2005 5 18 QXEA200500771 120050413A5330 SKIN PANEL CNDAIRCL600 CL6002C10 1390015EA ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - FORWARD FUSELAGE, FORWARD LOWER SKIN PANEL HAS ROCK CHIP PITTING DAMAGE, STATION 421 TO 437, BETWEEN STRINGER 26R AND STRINGER 27C AND STRINGER 23L AND 22L. REPAIRED IAW CRJ700 SRM 51-26-00-001-001-A01, 53-21-01-101-006-A01, 51-12-00-001-001-A01, AND 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050518000562005051800056EA 2005 5 18 QXEA200500774 120050414A5330 SKIN PANEL CNDAIRCL600 CL6002C10 1390015EA ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - FORWARD FUSELAGE, FORWARD LOWER SKIN PANEL HAS ROCK CHIP PITTING DAMAGE AT STATION 349 TO 379 BETWEEN STRINGER 24R AND STRINGER 23L. REPAIRED IAW HORIZON AIR EA R-53-311 AND REO 670-53-21-097. 2L72 4F RTA21EA 20050518000632005051800063EU 2005 5 18 MALA050390 120050427A7700 SWITCH SAAB SF340 340B 7860101EU COCKPIT BROKEN A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15403XJ 340B403 AIR TURNBACK- CTOT SWITCH BROKE OFF AFTER TAKEOFF. REMOVED AND REPLACED CTOT PANEL P/N BOTH 7239060-503, S/N ON 872621, S/N OFF 0339 NEEDS OPS CHECK LB 9850. OPS CHECKED CTOT SYSTEM IAW AMM CH 71-00-00-5. 2L72 4T RTA52EU 20050518000652005051800065EU 2005 5 18 MALA050385 120050425A53207253710243 STRUCTURE SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15416XJ 340B416 RIGHT WRAP AROUND P/N 7253710243 IS CORRODED AND HAS BEEN REPAIRED IAW SRM 51-40-21. 2L72 4T RTA52EU 20050518000662005051800066EU 2005 5 18 MALA050386 120050425A53207253711245 STRUCTURE SAAB SF340 340B 7860101EU FUSLEAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15416XJ 340B416 LEFT WRAP AROUND P/N 7253711-245 IS CORRODED AND HAS BEEN REPLACED IAW SRM 51-40-21. 2L72 4T RTA52EU 20050518000672005051800067EU 2005 5 18 MALA050387 120050423A53477253721459 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15416XJ 340B416 GALLEY SEAT TRACK HAD PROFILE P/N'S 7253721-459 AND 7253721-495 ARE CORRODED AND HAVE BEEN REPLACED IAW SRM 51-40-21 AND 51-40-22. 2L72 4T RTA52EU 20050518000682005051800068EU 2005 5 18 MALA050388 120050425A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15416XJ 340B416 FUSELAGE SKIN IS DENTED BETWEEN FS 339 AND FS 363 AND BETWEEN STRINGER'S SL1504 AND SL1506. THE DENTS ARE OUT OF LIMITS AND HAVE BEEN REPAIRED IAW MESABA EO S53009. 2L72 4T RTA52EU 20050518000692005051800069EU 2005 5 18 MALA050389 120050427A3350 BATTERY PACK SAAB SF340 SF340A 7850100EU EMERGENCY LIGHT INOPERATIVE A MALAK NONE O OTHER ININSP/MAINT 1 GL15110XJ 340A110 DURING LC1, NOTED LT AND RT AFT EXT EMERGENCY LIGHTS INOP. NOTED SEVERAL OTHER INT LIGHTS INOP ALSO. REMOVED AND REPLACED EMERGENCY SUPPLY AND BATTERY PACK 24LN. OPS CHECK GOOD. DOCUMENTED AND MM 409 237757. 2L72 4T RTA52EU 20050518000702005051800070EU 2005 5 18 MALA050391 120050425A7810 NOZZLE SAAB SF340 340B 7860101EU EXHAUST FAILED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15420XJ 340B420 AIR TURNBACK DUE TO LT ENGINE INTAKE HEAT. REMOVED AND REPLACED LT EXHAUST NOZZLE P/N NF24668-057. OPS CHECK GOOD. REMOVED AND REPLACED LT AIR VALVE, P/N 6068T56P01, S/N ON GRTG0598 OFF GRTB8183. OPS CHECK GOOD. 2L72 4T RTA52EU 20050516000022005051600002WP 2005 5 16 2005000002 120050326A3260806125 PROXIMITY SENSOR DOUG DC10 DC1030 3023501WP MLG INOPERATIVE A CNMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07490821119 1119 47927 LANDING GEAR RED LIGHTS REMAIN ON ALL 4 RECYCLE GEAR NO HELP LIGHTS REMAINED ON FOR 15 MINUTES BEFORE GOING OUT. 2L73 4F A22WE 20050516000052005051600005EA 2005 5 16 SWIA200514904 120050424A2752 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA TE FLAP MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 NM07463SW 7820 RECEIVED FLAPS FAIL CAUTION MSGS ON FINAL APPROACH. FAILED AT 41 DEGREES. REPLACED FLAP ACTUATORS R1, R2, R3, R4, L1, L2, L3, AND L4. OPERATIONAL CHECK GOOD AMM 27-53-01, AMM 27-53-05. P/N 852D100-19, S/N OFF 4982, 5039, 4609, 4941, P/N 853D100-20, S/N OFF 2903, P/N 854D100-20, S/N OFF 2721, P/N 853D100-19, S/N OFF 2898, P/N 854D100-19, S/N OFF 2360. 2L72 4F RTA21EA 20050516000312005051600031EU 2005 5 16 MALA050342 120050414A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15435XJ 340B435 DURING 4Y/2Y CHECK IN BNA FOUND SEAT TRACK AT BL 0 IS CORRODED ON VERTICAL WEB AND FLOOR PANEL FLANGE BETWEEN FS 294 AND FS 319. DAMAGE HAS BEEN REPAIRED IAW SRM 53-70-60. 2L72 4T RTA52EU 20050516000382005051600038NM 2005 5 16 CALA00128 120050425A3260106122615 SENSOR BOEING737 7373T0 1384582NM NLG INTERMITTENT A CALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW2712349 23587 LANDING GEAR UNSAFE LIGHT CAME ON THEN INTERMITTENT AFTER LEVEL AT FL35. REPLACED NLG SENSOR PER AMM 32-61-51. 2L72 4F RTA16WE 20050516000552005051600055NM 2005 5 16 CALA0500137 120050408A5230 SKIN BOEING737 7373T0 1384582NM CARGO DOOR WORN A CALAK NONE O OTHER ININSP/MAINT 1 SW2717326 23456 INNER SKIN WEAR AT THE AFT EDGE OF THE FORWARD MIDDLE ROW LIGHTNING HOLE OF THE AFT CARGO DOOR. INSTALLED DOUBLER PER ECRA 5232-01059. 2L72 4F RTA16WE 20050516000682005051600068EU 2005 5 16 MALA050337 120050414A5320 PANEL SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15435XJ 340B435 DURING 4Y/2Y CHECK IN BNA FOUND RIGHT WRAP AROUND P/N 7253710-243 IS CORRODED AND HAS BEEN REPLACED IAW SRM 51-40-21. 2L72 4T RTA52EU 20050516000732005051600073EU 2005 5 16 MALA050302 120050322A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15415XJ 340B415 DURING 4K CHECK IN BNA FOUND LEFT FUSELAGE IS DENTED BETWEEN FS 345 TO FS 363 AND BETWEEN SL1516 TO SL1518. DAMAGE HAS BEEN REPAIRED BY INSTALLING AN EXTERNAL DOUBLER IAW SRM 53-70-10. 2L72 4T RTA52EU 20050516000852005051600085EU 2005 5 16 MALA050334 120050413A5310 DOOR FRAME SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15429XJ 340B429 DURING 4Y/2Y CHECK IN BAN FOUND LEFT COCKPIT ENTRY DOOR POST IS CORRODED OUT OF LIMITS AND HAS BEEN REPAIRED IAW MESABA EO S53185. 2L72 4T RTA52EU 20050516000862005051600086EU 2005 5 16 MALA050380 120050420A2150 ACM SAAB SF340 340B 7860101EU LEFT ODOR A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL15365PX 340B265 AIR RETURN TO RHI FOR BURNING ODOR, MAINLY IN FLT DECK. REPLACED LEFT ACM. 2L72 4T RTA52EU 20050516000912005051600091EU 2005 5 16 MALA050354 120050414A5347 SEAT TRACK BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15503XJ E2310 DURING C2 INSPECTION FOUND SEAT RAILS BETWEEN FRAMES 18-19 AT RBL 39 CORRODED. 2H74 4F RTA49EU 20050516000982005051600098CE 2005 5 16 DXTA200500694 120050422A323099146371 MODULE CESSNA750 750 2076810CE MLG FAILED E DXTAO OTHER E VIBRATION/BUFFET DEDESCENT 1 GL07903QS3722 7500162 DURING DESCENT THRU FL250 THE NOSE GEAR BUMPED TWICE AND TRIED TO UNLOCK. GAINED ACCESS TO LANDING GEAR CONTROL MODULE AND VERIFIED INSTALLED PART NUMBER OF 9914637-1. REMOVED LGCM AND INSTALLED A MODIFIED LGCM IAW CE750 MM 32-30-02. PERFORMED SATISFACTORY LANDING GEAR RETRACT SYSTEM, OPERATIONAL CHECKS. 2L72 4J RTT00007WI 20050516001082005051600108SW 2005 5 16 ALGA100235 120050309A6510407340339107 DRIVE SHAFT BELL 407 407 1182206SW TAIL ROTOR VIBRATION B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW035NBEO1133 53190 HIGH VIBRATION / REPLACED WITH NEW BY FIELD MAINTENANCE 1G71 3U O H2SW 20050516001272005051600127NM 2005 5 16 2005UALA00370 120050418A2751 WARNING LIGHT BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE TE FLAPS ILLUMINATED A UALAO OTHER J WARNING INDICATION LDLANDING 1 WP29937UA 26668 LANDED UNDER AMBER ALERT IN IAH DUE TO SPLIT FLAPS INDICATION. THE SUBJECT SPLIT FLAP INDICATION AND ASSOCIATED INHIBITED FLAP MOVEMENT WAS DUE TO A FAULTY FLAP POSITION INDICATOR (PN 18-1299-6-2, PCN 421 9632). THE SUBJECT INDICATOR WAS REMOVED AND REPLACED WITH NEW SERVICEABLE UNIT PER MM27-58-41/401. 2L72 4F4 FRTA16WE E2GL 20050516001312005051600131NM 2005 5 16 2005UALA00376 120050419A5321 PRESSURE PANEL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN FLOOR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29374UA 24639 LEFT WHEEL WELL CEILING HAS CRACK AT FWD EDGE APPROXIMATELY SIX INCHES OUTBOARD OF AILERON TOWER SHAFT. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20050517000142005051700014NM 2005 5 17 05FDEA01132 120050426A5310 FLANGE BOEING727 727200 138407ENM ESCAPE HATCH CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25264FE 21626 CORROSION RIGHT FORWARD ESCAPE HATCH LOWER EDGE UNDER THE SEAL. REPLACED RT FWD ESCAPE HATCH PER FED-EX MM 52-20-002-5. 2L73 4F RTA3WE 20050517000242005051700024CE 2005 5 17 20030834 120050423A5270 ANNUNCIATOR BEECH 1900 1900D 1154162CE CARGO DOOR FALSE ACTIVATIONA GLBAB EMER. DESCENT N FALSE WARNING CRCRUISE 1 NM03192GL UE192 CARGO DOOR ANNUCIATOR ILLUMINATED IN FLT, CREW EXECUTED EMEGENCY CHECKLIST, LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED SYSTEM CHECKS AND COULD NOT DUPLICATE DISCREPENCY. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA24CE 20050517000282005051700028WP 2005 5 17 AALA20050287 120050423A3350 MODULE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217525A 49917 ATL - FORWARD SECTION EMERGENCY PATH LIGHTING WILL NOT TEST. REPLACED BATTERY AND MODULE FOR FORWARD SECTION EMERGENCY PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050517000292005051700029NM 2005 5 17 AALA20050281 120050421A3350 BATTERY BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21382AN 25451 DFW - EMERGENCY LIGHTS AT RIGHT HAND SEAT ROW 20 AND 21 INOPERATIVE. REPLACED BATTERY FOR EMERGENCY LIGHTS AT RIGHT HAND SEAT 20 AND 21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050517000312005051700031NM 2005 5 17 AALA20050284 120050422A3350 BATTERY BOEING767 767223 1385123NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21335AA 22333 JFK - EMERGENCY EXIT LIGHTS ILLUMINATED ON RIGHT SIDE OF A/C IN FIRST CLASS THROUGH 9H THEN EXTINGUISHED AFTER APPROXIMATELY 30 SECONDS. OCCURRED SEVERAL TIMES. REPLACED BATTERY AT SEAT 2H-J. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050517000452005051700045EU 2005 5 17 USAA200500002 120050419A5320 FLOOR SUPPORT AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19737US 1245 FWD LAV FLOOR SUPPORT CORRODED AT Y503.2, CORROSION 2 BY 2 INCHES. TRIMMED OUT DAMAGE, INSTALLED FREEZE PLUG AND INSTALLED REPAIR DOUBLER PER EA 96165A. 2L72 4F RTA28NM 20050517000492005051700049EU 2005 5 17 DHL2005367510 120050403A5101TMS6022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAO OTHER O OTHER ININSP/MAINT 1 SO01367DH 265 DURING "C" CHECK, CABIN SEAT TRACK AT FS 18 THRU FS 21A AT BL 28R HAS CORROSION. INSTALLED NEW SECTION OF SEAT TRACK AT MAIN CABIN FROM FS 18 TO FS 21A BL 28R IAW A-300 SRM 53-10-10 MAT. USED TMS 60-22457 PO NR 2113624. TREATED AND PAINTED NEW SEAT TRACK IAW A-300 SRM 51-40-12. 2L72 4F RTA35EU 20050517000542005051700054SO 2005 5 17 CHQA200500088 120050425A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11271SK 145305 THE EMERGENCY LIGHT ON THE SERVICE DOOR IS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BULB ON SERVICE DOOR IAW EMB 145 AMM 33-50-09. OPS CHECK GOOD. MAIN ENTRY DOOR CEILING EMERGENCY EXIT LIGHT IS VERY DIM. REMOVED AND REPLACED LIGHT BULB IAW EMB 145 AMM 33-50-06. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050517000552005051700055EA 2005 5 17 ASOA05330 120050411A3350S72451 SIGN CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE EMERGENCY EXIT DAMAGED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27710EV 10071 DURING A GROUND INSPECTION, THE EMERGENCY EXIT SIGN ON THE PASSENGER DOOR WAS FOUND DAMAGED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT SIGN ON THE PASSENGER DOOR. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA EOOO63EN 20050517000572005051700057EU 2005 5 17 DHL2005367512 120050403A5347TMS6022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01367DH 265 DURING C-CHECK, CABIN SEAT TRACK AT FS 18 THRU FS 38 AT BL 18R HAS CORROSION AT THE TRACK FLOOR SUPPORT AREA. REPLACED MAIN CABIN SEAT TRACK FROM FS 26.5 TO FS 32.5 APPROX AS PER A-300 SRM 51-10-40, MATERIAL USED/TMS 60-22457 SEAT TRACK 120 INCH LONG PO NR 2113624, AND AA-300 SRM 53-10-10. TREAT AND PRIMED AS PER A-300 SRM 51-40-12, TOP COAT PAINT AS PER A-300 SRM 51-40-12. 2L72 4F RTA35EU 20050517000632005051700063EA 2005 5 17 ASOA05326 120050408A5210601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27881AS 7496 DURING A GROUND INSPECTION, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINT REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECK GOOD. AC OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050517000652005051700065NE 2005 5 17 ASOA05270S 220050329A722032448716 HYDROMECH UNIT AEROSPATR72 ATR72 EU PWA PW120 PW127 NE LT ENGINE MALFUNCTIONED A ASOAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27641AS150602484 387 DURING CRUISE, THE CREW NOTICED THE LT ENGINE ITT RISE IN EXCESS OF 800 DEGREES ITT AND REDUCED THE POWER ON THE ENGINE TO BRING IT WITHIN ITT LIMITS AT WHICH TIME THE ENGINE BEGAN TO SURGE. AN EMERGENCY WAS DECLARED AND JUST PRIOR TO THE CREW SHUTTING DOWN THE LT ENGINE, IT RETURNED TO NORMAL AND STOPPED SURGING. THE DECISION WAS MADE TO LEAVE THE LT ENGINE RUNNING AND CONTINUED. THE AIRCRAFT LANDED SAFELY. MAINT REMOVED AND REPLACED THE HYDROMECHANICAL UNIT AND THE FUEL PUMP ON THE LT ENGINE. OPS AND LEAK CHECKS GOOD. AC OK FOR SERVICE. (K) 2H72 4T4 TRT E20NE 20050517000702005051700070EA 2005 5 17 ASOA05322 120050408A33506100976 LAMP CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27713EV 10081 DURING A GROUND INSPECTION, THE EMERGENCY CEILING FLOODLIGHT AT ROW 17 WAS FOUND TO BE INOPERATIVE. MAINT REMOVED AND REPLACED THE LAMP IN THE EMERGENCY CEILING FLOODLIGHT AT ROW 17. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA EOOO63EN 20050517000762005051700076EA 2005 5 17 ASOA05319 120050408A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27820AS 7188 DURING C-CHECK, THE RT INBOARD CLIP AT FS 484 BETWEEN RBL 9 TO RBL 27 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINT REMOVED AND REPLACED THE RT IB CLIP AT FS 484 BETWEEN RBL 9 TO RBL 27 IAW SRM. (K) 2L72 4F4 FRTA21EA E15NE 20050517000812005051700081EU 2005 5 17 UPS05144377 120050424A3350 BULB AIRBUS300 A300B4622R 3930312EU EMERG EXIT SIGN INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01127UP 0811 INSPECTION TYPE:N/A EXIT SIGN ABOVE CREW ENTRY DOOR HAS AN INOP BULB. REMOVED AND REPLACED INOP BULB ON CREW ENTRY DOOR EXIT LIGHT MODULE PER MM 33-51-13-4. 2L72 4F RTA35EU 20050517000902005051700090NM 2005 5 17 UPS05444372 120050411A534065B38600Y160 STRINGER CLIP BOEING747 747200 1384847NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 INSPECTION TYPE: C, BS 1600 LT STR 3L TIE CLIP FOUND CORRODED. CORROSION BLEND OUT 0.021 X 1 X 3 INCH EXCEED SRM LIMITS. TIE CLIP REPLACED AT BS 1600 STR 3L AS PER SRM 51-10-01 PG 9. 2L74 4F RTA20WE 20050517000972005051700097WP 2005 5 17 UPS05844368 120050404A5321 FLOORBOARD DOUG DC8 DC873F 302199FWP STA 70-140 RBL55CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 INSPECTION TYPE:C1 MAIN CABIN FLOORBOARD CORRODED AT STA 70 TO 140 RBL 55. REMOVED CORROSION AND INSTALLED DOUBLER IAW SRM 51-1-8 AND 51-1-21. 2L74 4F RT4A25 20050517000982005051700098WP 2005 5 17 UPS05844369 120050401A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 INSPECTION TYPE: C1, LONGERON CRACKED .5 INCH LONG AT STA 1746 L14L. CUT OUT DAMAGE AND INSTALLED FILLER AND DOUBLER IAW RM 53-02-02, 51-1-20 AND 51-3-0. 2L74 4F RT4A25 20050517001002005051700100WP 2005 5 17 UPS05844371 120050407A5340SAA3750257U1 SPLICE DOUG DC8 DC873F 302199FWP LONGERON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 INSPECTION TYPE: C1, B-PIT LONGERON SPLICE FITTING CRACKED (2) STA 610 L31L. REMOVED, MACHINED AND REPLACED LONGERON SPLICE IAW DWG 3750257, 51-1-20D AND 51-1-21. 2L74 4F RT4A25 20050517001032005051700103WP 2005 5 17 UPS05844379 120050426A3397 WIRE DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT PULLED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01805UP 46117 NO EMERGENCY LIGHTS ON TEST. EMERGENCY BATTERY PACK REPLACED, BUT EMERGENCY LIGHTS WOULD NOT TURN OFF WHEN DISARMED. FOUND WIRE PULLED OUT OF SOCKET NR 8 ON P1-1345. REPLACED SOCKET PER MM 20-50-01-8 AND WDM 33-50-01 PG 5. TEST GOOD PER MM 33-50-01-2. 2L74 4F RT4A25 20050517001122005051700112NM 2005 5 17 PCSA04260501 120050426A21337110033 OUTFLOW VALVE BOEING727 727212 138407GNM ZONE 100 INTERMITTENT A PCSAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO29598AJ 625 21947 FLIGHT 710 MID-MIA, DURING CLIMBOUT CREW REPORTED PRESSURIZATION OUTFLOW VALVE WOULD NOT CLOSE IN ANY MODE IN FLIGHT ON DEPARTURE FROM MID. AIRCRAFT RETURNED BACK TO MID WITH NO FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED A PRESSURIZATION CONTROL SYSTEM TEST IAW BOEING 727 MM CH-21-31-0 & AMERIJET PRESSURIZATION CHECK WORK CARDS 7-29. OUTFLOW VALVE OPERATION CHECKOUT NORMAL. AIRCRAFT RETURNED TO SERVICE. 2L73 4F A3WE 20050517001142005051700114EA 2005 5 17 ASOA05312 120050328A5320CC6703329212 FLOOR SUPPORT CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27790EV 10068 DURING HANGAR MAINTENANCE, THE FS 280 FLOOR SUPPORT ANGLE WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINT REPAIRED THE FS 280 FLOOR SUPPORT ANGLE IAW EO. (K) 2L72 4F4 FRTA21EA EOOO63EN 20050517001182005051700118NM 2005 5 17 QXEA200500724 120050427A5753 BEARING DHAV DHC8 DHC8202 2809007NM ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - PITTING NOTED ON LEFHAND NR 5 FLAP TRACK, OUTBOARD BEARING SURFACE -E-. REPAIRED IAW DHC-8-200 AMM TRASK 27-51-11-830-802 AND RD 8-57-889. 2H72 4T RTA13NM 20050517001192005051700119NM 2005 5 17 QXEA200500721 120050419A5753 FLAP TRACK DHAV DHC8 DHC8202 2809007NM ZONE 600 WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - RIGHTHAND INBOARD FLAP OUTBOARD LOWER FLAP TRACK IS WORN IN THREE PLACES ON THE TOP SURFACE BY THE FLAP ROLLERS. REPAIRED IAW RD 8-57-986 AND DHC-8-200 NDTM PART 6, 51-00-02, PAGES 1-4. 2H72 4T RTA13NM 20050517001282005051700128NM 2005 5 17 QXEA200500713 120050423A5220 STOP FITTING DHAV DHC8 DHC8202 2809007NM ZONE 800 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - ALL RIGHTHAND FORWARD EMERGENCY EXIT DOOR STOPS HAVE LIGHT CHAFING. REPAIRED IAW RD 8-52-349. 2H72 4T RTA13NM 20050517001292005051700129NM 2005 5 17 QXEA200500727 120050420A5753 ROLLER DHAV DHC8 DHC8202 2809007NM ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - LEFTHAND NR 4 FLAP TRACK ROLLER SURFACES HAVE CORROSION ON INBOARD AND OUTBOARD FLANGES OF TRACK-B. REPAIRED IAW RD 8-57-988. 2H72 4T RTA13NM 20050517001332005051700133NM 2005 5 17 PCSA04270501 120050427A2751 PROXIMITY SWITCH BOEING727 727212 138407GNM L E FLAP OUT OF ADJUST A PCSAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO29598AJ 21947 FLIGHT 881 DEPARTED MIA DURING CLIMBOUT CREW REPORTED AMBER LEADING EDGE FLAP INTRANSIT LIGHT REMAINED ILLUMINATED ON CAPTAINS FWD PANEL, CREW VERIFIED INDICATION ON FLIGHT ENGINEERS PANEL NR 3 LEADING EDGE FLAP INTRANSIT LIGHT ON. AIRCRAFT RETURNED BACK TO MIA WITH NO FURTHER INCIDENT. MAINTENANCE FOUND NR 3 LEADING EDGE POSITION SWITCH OUT OF ADJUSTMENT, NR 3 LEADING EDGE POSITION SWITCH ADJUSTED IAW B-727 MM 27-82-1 & OPERATIONALLY CHECKED GOOD PER MM 27-82-1. AIRCRAFT WAS RETURNED TO SERVICE. 2L73 4F A3WE 20050517001352005051700135EA 2005 5 17 COMA0560275 120050425A3350110049 CHARGER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT MALFUNCTIONED A COMAK NONE O OTHER ININSP/MAINT 1 SO01936CA 7043 FLIGHT 5157 FORWARD EMERGENCY FLOOD LIGHT IS INOP. REPLACED THE BATTERY CHARGER ASSY. 2L72 4F RTA21EA 20050517001472005051700147NM 2005 5 17 AMTA200500339 120050331A2497 WIRE BOEING757 75733N 1384931NM CONNECTOR BROKEN A AMTAO OTHER HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 GL11555TZ 32589 EICAS MSG L GEN OFF DISPLAYED. GEN SW RESET DID NOT CORRECT CONDITION. FOUND PIN 5 AT D1396 TO 19 AT D1014P OPEN, FOUND BROKEN WIRE AT PIN 19. REPINNED CONNECTOR D1014 PIN 19. PERFORMED BPCU BITE PROCEDURE PER FIM 24-20-00, NO FAULTS FOUND. NR 1 ENGINE IDG. OPS SATISFACTORY PER 24-11-00-5. (M) 2L72 4F RTA2NM 20050517001512005051700151NM 2005 5 17 AMTA200500374 120050417A3150285N00551 MODULE BOEING757 75723N 1384973NM EICAS MALFUNCTIONED A AMTAO OTHER O OTHER DEDESCENT 1 GL11517AT 27973 LOWR EICAS DISPLAY FLICKERS FOR SEVERAL SECONDS INTERMITTENTLY WITH EIAS DISPLAY MESSAGE DISPLAYED LOWER EICAS INFORMAION ALSO COMPACTED ON UPPER SCREEN DURING FLICKERING. REMOVED AND REPLACED CARD TO LOWER EICAS. OPS CHECK NORMAL. (M) 2L72 4F RTA2NM 20050517001542005051700154EA 2005 5 17 ASOA05292 120050402A5340 STRINGER CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27862AS 7476 DURING A C-CHECK IN MCN, THE RIGHT INBOARD FS 280 CLIP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE RIGHT INBOARD FS 280 CLIP. (M) 2L72 4F RTA21EA 20050517001552005051700155EA 2005 5 17 A6WA200540154 120050411A3230750006000 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A A6WAO OTHER J WARNING INDICATION APAPPROACH 1 GL31433AW4295 7289 GEAR DISAGREE WARNING IN FLIGHT COMPLIED WITH QRH, LANDED NORMAL. REMOVED AND REPLACED GEAR SELECTOR VALVE IAW AMM 32-33-10. PERFORMED GEAR EXTENSION AND RETRACTION TEST IAW AMM 32-30-00. LEAK AND OPS CHECK GOOD. (M) 2L72 4F RTA21EA 20050517001612005051700161EA 2005 5 17 VTZA200500066 120050426A3230750006000 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA NLG FAILED A VTZAO OTHER J WARNING INDICATION DEDESCENT 1 EA27679BR6721 7662 ON FINAL RCV'D GEAR DISAGREE WARNING MSG ALONG WITH NOSE DOOR WARNING MSG WHEN CYCLING GEAR HANDLE, USED MANUAL GEAR EXT. TROUBLESHOT PSEU IN REF TO CRJ FIM 32-60-00 FAULT CODES SHOWED THAT NLG SELECTOR VALVE WAS POSSIBLE FAULT REMOVED IN REF TO CRJ AMM 32-33-10; INSTALLED NLG SELECTOR VALVE REF MM CH 32-33-10. PERFORMED GEAR SWINGS REF MM CH 32-30-00. GEAR SWINGS GOOD AT THIS TIME. 2L72 4F RTA21EA 20050517001712005051700171EA 2005 5 17 QXEA200500741 120050409A5755 FASTENER CNDAIRCL600 CL6002C10 1390015EA ZONE 600 LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - RT WING UPPER SKIN TRAILING EDGE INBOARD OF INBOARD MULTI FUNCTION SPOILER HAS LOOSE FASTENERS. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20050517001802005051700180EA 2005 5 17 QXEA200500729 120050418A3220 CYLINDER CNDAIRCL600 CL6002C10 1390015EA ZONE 700 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - CORROSION FOUND ON NOSE LANDING GEAR OUTER CYLINDER. REPAIRED IAW HORIZON AIR EA R-32-186 AND REO 670-32-21-00-13. 2L72 4F RTA21EA 20050517001812005051700181EA 2005 5 17 QXEA200500731 120050413A5755 FASTENER CNDAIRCL600 CL6002C10 1390015EA ZONE 500 LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - LEFTHAND WING UPPER SKIN TRAILING EDGE, INBOARD OF INBOARD MULTI SPOILER HAS LOOSE FASTENERS. REPAIRED IAW CRJ700 SRM 51-62-06-001-001-A01. 2L72 4F RTA21EA 20050517002122005051700212EA 2005 5 17 QXEA200500769 120050412A5730 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 500 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC-LEFT WING BOTTOM SKIN HAS CHAFE MARK UNDER FAIRING 586AB. REPAIRED IAW CRJ700 SRM 57-00-01-101-001-A01, 51-12-00-04-001-A01, AND 51-25-16-001-001-A01. 2L72 4F RTA21EA 20050517002152005051700215EA 2005 5 17 QXEA200500759 120050414A5753 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 500 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC- LEFT INBOARD FLAP LOWER EXTERNAL SURFACE HAS CHAFE MARKS UNDER INBOARD HINGE ARM FAIRING. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01, 57-52-01-101-001-A01, AND 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050517002172005051700217EU 2005 5 17 05FDEA01152 120050427A2910 PACKING AIRBUS300 A300F4605R 3930327EU HYD TRANSMITTER LEAKING A FDEAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SO25663FE 766 AT FL350 LOST QUANTITY IN THE GREEN HYD SYSTEM. ACCOMPLISHED ECAM ITEMS AND ADDITIONAL QRH ITEMS. MANUAL EXTENSION OF MAIN GEAR. EMERGENCY DECLARED FOUND LEAKAGE AT GREEN SYS PRESS TRANSMITTER ADDED MPN NSA8671-4 CPN 0114019 QTY 2 RING MSN 928916 ADDED MPN NAS1611-010 CPN 0015884 QTY 2 PACKING MSN 928917 ADDED MPN 64250-005-2 CPN 2910415 QTY 1 TRANSMIT. REPLACED PART, SERVICED FLUID, LEAK CHECK SYSTEM RETURNED GEAR TO NORMAL SERVICE CONDITION. 2L72 4F RTA35EU 20050517002182005051700218EU 2005 5 17 05FDEA01153 120050427A5313 STRINGER AIRBUS310 A310203 3930313EU FUSLEAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25402FE 201 IN ACM BAY FR 46- FR 47 ON STG 51L HAS AREA OF CORROSION. REMOVED CORROSION PER A310 SRM 51-74-10 C/W EA 6-5310-87784. FOUND ALL AREAS TO BE WITHIN LIMITS PER EA 6-5310-87784 AND A310 SRM 53-10-00. INSTALLED FASTENERS PER A310 SRM 51-40-21. RESTORED SURFACE PROTECTION PER A310 SRM 51-75-10. 2L72 4F RTA35EU 20050517002242005051700224EU 2005 5 17 05FDEA01166 120050428A5330 SKIN AIRBUS300 A300F4605R 3930327EU FUSELAGE SCRATCHED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25662FE 761 FUSELAGE EXTERNAL SKIN AFT OF FWD CARGO DOOR FR 26 STR 38 RT HAS 1 EA AREA W/ SHARP DEEP SCRATCHED APPROX 1/2 INCH LONG .020 DEEP REFN00086. REMOVED SHARP DEEP SCRATCHES BY BLENDING THE AREA IAW SRM 51-73-10 AREA FOUND TO BE ACCEPTABLE IAW EA 6-5330-87825. 2L72 4F RTA35EU 20050517002332005051700233NE 2005 5 17 MALA050315 220050405A7320 MANIFOLD BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE FUEL SYSTEM MALFUNCTIONED A MALAO OTHER J WARNING INDICATION CLCLIMB 1 GL15515XJ E2333 AFTER LIFT OFF, CREW REPORTED THE NR 1 ENGINE FIRE WARNING LIGHT ILLUMINATED. CREW PULLED POWER LEVER TO IDLE ON THE NR 1 ENGINE AND THE LIGHT EXTINGUISHED. RETURNED TO MLI. REPLACED FUEL MANIFOLD. DATE OF MANUFACTURER 8/18/1998. 2H74 4F4 FRTA49EU E6NE 20050518000102005051800010 2005 5 18 2005UALA00334 420050413A2565140N27669 GIRT BAR BOEING757 757222 1384956NM PWA 2037 PW2037 NE R3 DOOR DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29572UA 26682 GIRT BAR ENGAGEMENT LIGHT EXTINGUISHED WITH EVACUATION SLIDE ARMING LEVER IN ENGAGED POS AT DOOR. DOOR 3R GIRT BAR ENGAGEMENT LIGHT INOP. 2L72 4F4 FRTA2NM E17NE 20050518000232005051800023NM 2005 5 18 05FDEA01104 120050423A5712ARB292014 RIB DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 RT WING LEADING EDGE CAVITY RIB BETWEEN SLAT TRACK NR 16 AND NR 17 FOUND CRACKED AT EDGE. FABRICATED IAW DRAWING NR: ARB2920. RIB REMOVED AND REPLACED AS PER SRM 51-35-01 VOLUME II. 2L73 4F RTA22WE 20050518000302005051800030NM 2005 5 18 2005UALA00350 120050416A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29585UA 26709 FWD PIT STA 540 LEFT SIDE, FRAME HAS DENT ABOVE STR 25L UPPER FLANGE INTO RADIUS. REMOVED DAMAGE AND INSTALLED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20050518000342005051800034NM 2005 5 18 2005UALA00354 120050416A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29585UA 26709 FWD PIT RIGHT SIDE STA 660 FRAME HAS DENT BETWEEN STR 25R AND 26R, UPPER FLANGE. REMOVED DAMAGE AND INSTALLED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20050518000412005051800041NM 2005 5 18 2005UALA00363 120050417A3040 ODOR BOEING747 747422 1384935NM PWA 4056 PW4056 NE COCKPIT DETECTED A UALAO OTHER OJ OTHER WARNING INDICATION NRNOT REPORTED 1 WP29174UA 24381 WINDOW HEAT 2L EICAS MSG DISPLAYED. A WEIRD ODOR WAS APPARENT IN THE COCKPIT THEN C/B TRIPPED FOR 2L. NO RESET ATTEMPTED. INVESTIGATED & FOUND LOOSE WINDOW HEAT CONTROL THERMOSTAT WIRING & "WINDOW HEAT 2L" MESSAGE ON EICAS. LOOSE WIRING MAY HAVE CAUSED ARCING & ODOR. THE LOOSE WIRE WAS REATTACHED TO COCKPIT WINDOW. "WINDOW HEAT 2L" MESSAGE WAS GONE, AND A/C RETURNED TO REVENUE SERVICE WITHOUT FURTHER ODOR OR WINDOW HEAT PROBLEM. 2L74 4F4 FRTA20WE E24NE 20050518000472005051800047EU 2005 5 18 2005UALA00381 120050404A5330 SKIN AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29430UA 568 DENT AFT OF DOOR 1L, APPROX 20 INCHES AFT OF DOOR BOTTOM. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA28NM E40NE 20050518000712005051800071NM 2005 5 18 AALA20050289 120050426A3350 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21782AN 30003 DFW FIRST CLASS GALLEY EMERGENCY LIGHTS INOPERATIVE AT BULKHEAD ISLAND. REPLACED EMERGENCY LIGHT BATTERY PACK M33093 FOR FIRST CLASS GALLEY EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED. 2L72 4F RTT00001SE 20050518000722005051800072EU 2005 5 18 AWXA200500511 120050401A5320D53610183002 SUPPORT ANGLE AIRBUS320 A320232 3930326EU CABIN CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28638AW 455 DURING C-08 CHECK GALVANIC CORROSION WAS FOUND PASSENGER CABIN SUPPORT ANGLE AT FR 12+5 BETWEEN -Y254 AND -Y1292. MAINTENANCE REMOVED CORRODED SUPPORT ANGLE AT FR 12+5" FROM -Y254 TO -Y1292; FABRICATED A NEW ANGLE PER DWG D53610187; INSTALLED REPAIR PART IAW A320 SRM 51-42-11. 2L72 4F RTA28NM 20050518000732005051800073EU 2005 5 18 AWXA200500512 120050404A5347D5713014720000 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28638AW 455 SAL - MAJOR REPAIR - DURING C-08 CHECK INTERGRANULAR CORROSION WAS FOUND LT INBOARD SEAT TRACK Y765 AT FR 39+4". MAINTENANCE REMOVED CORRODED LT INBOARD SEAT TRACK Y765 FROM FS 36 TO FS 41; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK PER DWG D571-30147; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050518000742005051800074EU 2005 5 18 AWXA200500513 120050404A5347D53371112000 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28638AW 455 SAL - MAJOR REPAIR - DURING C-08 CHECK GALVANIC CORROSION WAS FOUND LT OUTBOARD SEAT TRACK Y1292 AT FR 42. MAINTENANCE REMOVED CORRODED LT OUTBOARD SEAT TRACK Y1292 FROM FS 41 TO FS 47 -6"; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK PER DWG D53371112; INSTALLED REPAIR PART IAW A320 SRM 51-42-11. 2L72 4F RTA28NM 20050518000752005051800075EU 2005 5 18 AWXA200500514 120050404A5347D53472178200 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28638AW 455 SAL - MAJOR REPAIR - DURING C-08 CHECK, GALVANIC CORROSION WAS FOUND LT INBOARD SEAT TRACK Y765 AT FS 60+17". MAINTENANCE CUTOUT DAMAGED SECTION OF LT INBOARD SEAT TRACK Y765 AT FS 60+17"; FABRICATED AN "L" PROFILE AND A NEW REPLACEMENT SECTION OF SEAT TRACK; INSTALLED REPAIR PARTS IAW A320 SRM 53-00-15, FIG 201. 2L72 4F RTA28NM 20050518000762005051800076EU 2005 5 18 AWXA200500515 120050404A5347D53371110008 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28638AW 455 SAL - MAJOR REPAIR - DURING C-08 CHECK, GALVANIC CORROSION WAS FOUND LT INBOARD SEAT TRACK Y765 AT FR 42+17". MAINTENANCE CUTOUT DAMAGED SECTION OF LT INBOARD SEAT TRACK Y765 AT FR 42+17"; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK PER DWG D53371110008; INSTALLED REPAIR PART IAW A320 SRM 53-31-15, FIG 103. 2L72 4F RTA28NM 20050518000772005051800077NM 2005 5 18 AWXA200500516 120050331A3397 WIRE HARNESS BOEING737 737301 1384611NM EMERGENCY LIGHT DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - EEL - DURING C-19 CHECK, FOUND NUMEROUS DAMAGED SPLICES AND CONNECTOR ON PASSENGER CABIN EMERGENCY ESCAPE PATH LIGHT HARNESS. MAINTENANCE REMOVED AND REPLACED DAMAGED SPLICES AND CONNECTOR ON EMERGENCY ESCAPE PATH LIGHT HARNESS IAW SWPM 20-42-01, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050518000782005051800078NM 2005 5 18 AWXA200500517 120050424A552365C2635916A TAB BOEING737 737301 1384611NM RT ELEVATOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - FLIGHT CONTROL - DURING C-19 CHECK A 3/8 INCH CRACK WAS FOUND RT ELEVATOR TAB OUTBOARD CONTROL ROD ATTACH POINT AT ELE STA 121.59. MAINTENANCE REMOVED AND REPLACED DAMAGED RT ELEVATOR TAB IAW T/C R6C27007, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050518000792005051800079EA 2005 5 18 QXEA200500787 120050412A5230 RETAINER CNDAIRCL600 CL6002C10 1390015EA ZONE 800 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - FORWARD BAGGAGE DOOR BOTTOM SEAL RETAINER HAS CHAFE MARKS AT FORWARD AND AFT ENDS FROM SEAL STRIKE. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01, AND 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050518000802005051800080EA 2005 5 18 QXEA200500783 120050412A5210 ATTACH ANGLE CNDAIRCL600 CL6002C10 1390015EA PAX DOOR CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - PASSENGER DOOR AFT SIDE STRINGER TO DOOR PANEL ATTACH ANGLE HAS POSSIBLE CRACK AT ASSIST MOTOR. REPAIRED IAW REO 670-52-11-072. 2L72 4F RTA21EA 20050518000812005051800081EA 2005 5 18 QXEA200500788 120050414A5230 ATTACH FITTING CNDAIRCL600 CL6002C10 1390015EA ZONE 800 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - FORWARD BAGGAGE DOOR AFT TOP LUG FOR ROLLER ATTACH TO COUNTER BALANCE HAS NICKS AND SCRATCHES. REPAIRED IAW CRJ700 SRM 52-35-06-101-001-A01, 51-12-00-001-001-A01, AND 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050518000822005051800082EA 2005 5 18 QXEA200500780 120050414A5330 SKIN PANEL CNDAIRCL600 CL6002C10 1390015EA ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - FORWARD FUSELAGE, FORWARD LOWER SKIN PANEL HAS ROCK CHIP PITTING DAMAGE AT STATION 295 TO 310 BETWEEN STRINGER 25R AND STRINGER 26L. REPAIRED IAW CRJ700 SRM 51-26-00-001-001-A01, 53-21-01-101-002-A01, 51-12-00-001-001-A01, AND 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050518000832005051800083EA 2005 5 18 QXEA200500782 120050418A5320 STOP FITTING CNDAIRCL600 CL6002C10 1390015EA ZONE 200 WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - FUSELAGE GALLEY SERVICE DOOR STOP FITTINGS HAVE WEAR MARKS ON END AND AFT INNER FACE. REPAIRED IAW HORIZON AIR EA R-53-310 AND REO 670-53-21-098. 2L72 4F RTA21EA 20050518000842005051800084EA 2005 5 18 QXEA200500784 120050409A5210 BRACKET CNDAIRCL600 CL6002C10 1390015EA ZONE 800 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - PASSENGER DOOR ASSIST MOTOR MOUNT BRACKET HAS SMALL CRACK AT OUTBOARD END. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20050518000852005051800085EA 2005 5 18 QXEA200500785 120050412A5210 STRINGER CNDAIRCL600 CL6002C10 1390015EA ZONE 800 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - PASSENGER DOOR FORWARD STRINGER CRACKED AT RISER AT HANDRAIL STOWING BRACKET. REPAIRED IAW REO 670-52-11-104. 2L72 4F RTA21EA 20050518000862005051800086EA 2005 5 18 QXEA200500781 120050410A5320 SILL CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - FUSELAGE GALLEY SERVICE DOOR SILL PLATE HAS SPOTS OF CORROSION ON UNDER SIDE. REPAIRED IAW CRJ700 SRM 53-21-23-101-002-A01 AND 51-25-00-001-001-A01. 2L72 4F RTA21EA 20050518000872005051800087EA 2005 5 18 QXEA200500786 120050412A5210 STRINGER CNDAIRCL600 CL6002C10 1390015EA ZONE 800 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - PASSENGER DOOR AFT STRINGER CRACKED AT RISER AT HANDRAIL STOWAGE BRACKET. REPAIRED IAW REO 670-52-11-104. 2L72 4F RTA21EA 20050518000882005051800088EA 2005 5 18 SWIA200514912 120050411A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07443SW 7638 FS 484 RIGHT INTERCOSTAL OUTBOARD FLANGE RBL 36 CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED INTERCOSTAL IAW CRJ REO 601R-53-41-059 REV A. 2L72 4F RTA21EA 20050518000892005051800089EA 2005 5 18 SWIA200514913 120050411A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07443SW 7638 FS 460 RIGHT OUTBOARD FLOOR FITTING RBL 9.0 CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ SRM 51-42-06, 51-42-21, 51-23-00, 51-25-16 & 51-21-11. 2L72 4F RTA21EA 20050518000902005051800090EA 2005 5 18 SWIA200514914 120050411A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07443SW 7638 FS 625 LEFT INTERCOSTAL ANGLE STR 14L CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06. 2L72 4F RTA21EA 20050518000912005051800091EA 2005 5 18 SWIA200514915 120050411A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07443SW 7638 FS 625 RIGHT INTERCOSTAL ANGLE STR 14R CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06. 2L72 4F RTA21EA 20050518000922005051800092EA 2005 5 18 SWIA200514916 120050411A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07443SW 7638 FS 621 RIGHT SIDE FLOOR SUPPORT ANGLE RBL 42 CRACKED, ITEM FOUND AT C-CHECK INSPECTION. CRACKED ANGLE REPAIRED IAW CRJ REO 601R-53-61-117 REV "B" . 2L72 4F RTA21EA 20050518000932005051800093EA 2005 5 18 SWIA200514917 120050411A5320 SILL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07443SW 7638 FS 589.0 CARGO BAY FLOOR SILL RBL 44 ANGLE CORRODED, ITEM FOUND AT C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, 51-21-11, 51-41-02. 2L72 4F RTA21EA 20050518000942005051800094EA 2005 5 18 SWIA200514918 120050413A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07960SW 7853 FS 280 LEFT FLOORBEAM LBL 9.0 OUTBOARD ATTACH ANGLE CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-71, 51-42-06, 51-42-21 & 51-23-00. 2L72 4F RTA21EA 20050518000952005051800095EA 2005 5 18 SWIA200514919 120050413A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07960SW 7853 FS 280 RIGHT FLOORBEAM RBL 9.0 INBOARD AND OUTBOARD ATTACH ANGLES CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLES IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21 & 51-23-00 2L72 4F RTA21EA 20050518000962005051800096EA 2005 5 18 SWIA200514920 120050421A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07903SW 7425 CABIN EMERGENCY LIGHTS, CEILING LIGHTS THE ONE MOST FORWARD IS INOPERATIVE. REPLACED FORWARD ELBP CHANGING ASSY. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050519000022005051900002NM 2005 5 19 P5CA0501345 120050426A2820 LINE BOEING747 747341 13848AMNM FUEL CROSSFEED LEAKING A P5CAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA15355MC 23395 FUEL MIGRATING INTO NR 1 MAIN FUEL TANK. FOUND CROSS FEED LINE LEAKING AT FWD BULKHEAD COUPLING. RESEALED AND RETORQUED COUPLING OPS AND LEAK CK OK PER MM 28-22-07 AND 28-11-02. 2L74 4F RTA20WE 20050519000032005051900003EA 2005 5 19 ASOA05311 120050326A5330MM67036511002 PANEL CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27709EV 10068 DURING HANGAR MAINTENANCE, THE RT LUNCH BOX UPPER PANEL ASSY AT THE HYDRAULIC CASE DRAIN LOCATION WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RT LUNCH BOX UPPER PANEL ASSY AT THE HYDRAULIC CASE DRAIN LOCATION IAW. (K) 2L72 4F4 FRTA21EA EOOO63EN 20050519000052005051900005EA 2005 5 19 ASOA05310 120050326A5315 FLOORBEAM CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27709EV 10068 DURING HANGAR MAINTENANCE, THE FS 280 FLOORBEAM WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE FS 280 FLOORBEAM IAW EO. (K) 2L72 4F4 FRTA21EA EOOO63EN 20050519000092005051900009NM 2005 5 19 P5CA0501347 120050427A7810 NOZZLE BOEING747 747230B 1384889NM GE CF6 CF650E2 30018NE EXHAUST DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 EA15509MC 21221 530389 ON WALK AROUND, FOUND A HOLE APPROXIMATELY 1.5 INCH IN DIAMETER ON NR 3 ENGINE LONG FIXED CORE EXHAUST NOZZLE AT 8:00 O’CLOCK POSITION. REPAIRED NR 3 ENGINE LONG FIXED CORE COWL EXHAUST NOZZLE AS PER GE ENGINE MANUAL 78-11-01, REPAIR 010. 2L74 4F4 F A20WE E23EA 20050519000122005051900012NM 2005 5 19 SWAA051247 120050427A33506104789 BATTERY BOEING737 7375H4 138449DNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29523SW 26565 DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY & FUSES PER MM. 2L72 4F RTA16WE 20050519000152005051900015NM 2005 5 19 SWAA051250 120050427A3350101114 BULB BOEING737 7373H4 1384600NM EMERGENCY EXIT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29632SW 27707 DURING SCHEDULED C2 CHECK, FOUND COCKPIT EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY EXIT LIGHT PER MM. 2L72 4F RTA16WE 20050519000162005051900016 2005 5 19 SWAA051251 420050427A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29648SW 27718 DURING SCHEDULED C2 CHECK, FOUND L1 & R1 DOOR EMERGENCY EVAC SLIDES OUT OF ADJUST. ADJUSTED SLIDES PER MM. 2L72 4F RTA16WE 20050519000172005051900017NM 2005 5 19 SWAA051252 120050427A57536546430189 SKIN BOEING737 7373H4 1384600NM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29648SW 27718 DURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD T/E FOREFLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM. 2L72 4F RTA16WE 20050519000182005051900018NM 2005 5 19 SWAA051253 120050427A53306545769 SKIN BOEING737 7373L9 1384470NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT EQUIPMENT COOLING EXHAUST AFT CUTOUT. REPAIRED SKIN PER BFG ER. 2L72 4F RTA16WE 20050519000192005051900019NM 2005 5 19 SWAA051254 120050427A53306545768 SKIN BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON FUSELAGE SKIN LAP JOINT AT BS 259 TO BS 305, STR 19L. REPAIRED SKIN PER BFG ER. 2L72 4F RTA16WE 20050519000222005051900022NM 2005 5 19 SWAA051257 120050427A53306545774 SKIN BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON FUSELAGE SKIN LAP JOINT AT BS 540 TO BS 727, STR 10L. REPAIRED SKIN PER BFG ER. 2L72 4F RTA16WE 20050519000232005051900023NM 2005 5 19 SWAA051258 120050427A53306546881 SKIN BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON FUSELAGE SKIN LAP JOINT AT BS 1016 TO BS 1088, STR 4L. REPAIRED SKIN PER BFG ER. 2L72 4F RTA16WE 20050519000262005051900026NM 2005 5 19 SWAA051261 120050427A53306546881 SKIN BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON FUSELAGE SKIN AT BS 1016 TO BS 1088, FROM STR 26L TO STR 26R. REMOVED AND REPLACED BELLY SKIN SECTION PER BFG ER. 2L72 4F RTA16WE 20050519000272005051900027NM 2005 5 19 SWAA051262 120050427A53306545768 SKIN BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON LOWER FUSELAGE SKIN AT BS 350 TO BS 360, BL 0. REPAIRED SKIN PER BFG ER. 2L72 4F RTA16WE 20050519000282005051900028NM 2005 5 19 SWAA051263 120050427A53306546881 SKIN BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON FUSELAGE SKIN LAP AT BS 1016 TO BS 1088, STR 16R. REPAIRED SKIN PER BFG ER. 2L72 4F RTA16WE 20050519000302005051900030NM 2005 5 19 SWAA051265 120050427A532269353656 SHEAR TIE BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON FUSELAGE LOWER FRAME SHEAR TIE AT BS 360, BL 0. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050519000322005051900032NM 2005 5 19 SWAA051267 120050427A53116546529 FRAME BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON FUSELAGE FRAME ASSY AT BS 500, FROM STR 26L TO STR 27L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050519000332005051900033NM 2005 5 19 SWAA051268 120050427A53306546881 SKIN BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON FUSELAGE SKIN AT BS 907 TO BS 1016, FROM STR 26L TO STR 26R. REMOVED AND REPLACED BELLY SKIN SECTION PER SRM. 2L72 4F RTA16WE 20050519000352005051900035NM 2005 5 19 SWAA051223 120050426A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 402, STR 16R. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050519000402005051900040NM 2005 5 19 SWAA051228 120050426A53306545768 SKIN BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN LAP JOINT CORRODED AT BS 259 TO 360, STR 14L. REPAIRED SKIN PER BFG ER. 2L72 4F RTA16WE 20050519000422005051900042NM 2005 5 19 SWAA051230 120050426A53306545768 SKIN BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN LAP JOINT CORRODED AT BS 350 TO 500C, STR 19L. REPAIRED SKIN PER BFG ER. 2L72 4F RTA16WE 20050519000442005051900044NM 2005 5 19 SWAA051232 120050426A53306545775 SKIN BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN LAP JOINT CORRODED AT BS 727D TO 951, STR 20L. REPAIRED SKIN PER BFG ER. 2L72 4F RTA16WE 20050519000452005051900045NM 2005 5 19 SWAA051233 120050426A53306546881 SKIN BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN LAP JOINT CORRODED AT BS 986 TO BS 1016, STR 14L. REPAIRED SKIN PER BFG ER. 2L72 4F RTA16WE 20050519000462005051900046NM 2005 5 19 SWAA051234 120050426A53306545776 SKIN BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN LAP JOINT CORRODED AT BS 907 TO 1016, STR 14R. REPAIRED SKIN PER BFG ER. 2L72 4F RTA16WE 20050519000472005051900047NM 2005 5 19 SWAA051235 120050426A53306545766 SKIN BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN LAP JOINT CORRODED AT BS 360 TO BS 500C, STR 26R. REPAIRED SKIN PER BFG ER. 2L72 4F RTA16WE 20050519000502005051900050NM 2005 5 19 SWAA051238 120050426A53306545768 SKIN BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN LAP JOINT CORRODED AT BS 259 TO BS 360, STR 19R. REPAIRED SKIN PER BFG ER. 2L72 4F RTA16WE 20050519000512005051900051NM 2005 5 19 SWAA051239 120050426A53306545768 SKIN BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN LAP JOINT CORRODED AT BS 259 TO BS 360, STR 24L. REPAIRED SKIN PER BFG ER. 2L72 4F RTA16WE 20050519000522005051900052NM 2005 5 19 SWAA051240 120050426A53306546881 SKIN BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN LAP JOINT CORRODED AT BS 908 TO BS 1016, STR 4R. REPAIRED SKIN PER BFG ER. 2L72 4F RTA16WE 20050519000542005051900054NM 2005 5 19 SWAA051242 120050426A53306545776 SKIN BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN LAP JOINT CORRODED AT BS 908 TO BS 950, STR 14L. REPAIRED SKIN PER BFG ER. 2L72 4F RTA16WE 20050519000582005051900058NM 2005 5 19 SWAA051208 120050425A53156545410 FLOORBEAM BOEING737 7373H4 1384600NM CABIN FLOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND 2 EA LONGITUDINAL FLOORBEAMS CRACKED AT BS 727A + 18, LBL 45 & RBL 45, WL 208. REPAIRED BEAMS PER PAE ER. 2L72 4F RTA16WE 20050519000592005051900059NM 2005 5 19 SWAA051209 120050425A53206545410 FLOOR SUPPORT BOEING737 7373H4 1384600NM CABIN FLOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL FLOOR SUPPORT CRACKED AT BS 727B - 2, RBL 25, WL 208. REPAIRED BEAM PER PAE ER. 2L72 4F RTA16WE 20050519000602005051900060 2005 5 19 SWAA051210 420050424A25656557463 GIRT BAR BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29363SW 26574 R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR DIFFICULT TO REMOVE FROM FLOOR FITTINGS. ADJUSTED SLIDE & REMOVED DEBRIS FROM GIRT BAR FITTINGS PER MM. 2L72 4F RTA16WE 20050519000642005051900064NM 2005 5 19 SWAA051214 120050424A335007912 COVER BOEING737 7377H4 1384404NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29411WN 29821 FWD END OF EEPLS COVER MISSING. INSTALLED COVER PER MM. 2L72 4F RTA16WE 20050519000662005051900066NM 2005 5 19 SWAA051216 120050424A335010107451 LIGHT BOEING737 7375H4 138449DNM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29513SW 24190 EMERGENCY EXIT LIGHT ASSY LOOSE AT ROW 1. SECURED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20050519000742005051900074EA 2005 5 19 VNAA0504003 120050412A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS ILLUMINATED A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL05254PS 7935 DURING CLIMBOUT (CLT TO CAK) THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED WITH FLAPS AT 20DEGREES. THE CREW OF FLIGHT 2560 FOLLOWED THE QRH, RETURNED TO CLT, AND MADE AN UNEVENTFUL LANDING. PSA MAINTENANCE INTERROGATED AND RESET THE FECU. A FLAP SYSTEM AND FLAP CONTROL LEVER TEST WAS PERFORMED IAW CRJ 200 FIM 27-50-00. THE OPERATIONAL TEST WAS NORMAL AND NO DEFECTS WERE NOTED. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050519000752005051900075EA 2005 5 19 VNAA0504002 120050412A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS ILLUMINATED A VNAAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 GL05209PS 7874 DURING APPROACH TO PHL THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED WITH THE FLAPS AT 20 DEGREES. THE CREW OF FLIGHT 2542 REQUESTED A SECOND APPROACH TO RECONFIGURE THE AIRCRAFT FOR A FLAPS 20 DEGREES LANDING, FOLLOWED THE QRH, AND MADE AN UNEVENTFUL LANDING. PSA MAINTENANCE RESET THE FECU CIRCUIT BREAKERS IAW BOMBARDIER CRJ200 SL: 00-001. OPERATIONAL CHECKS WERE GOOD WITH NO FAULTS FOUND. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050519000782005051900078EA 2005 5 19 VNAA0504007 120050422A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE LIGHTNING STRIKEA VNAAO OTHER O OTHER NRNOT REPORTED 1 GL05256PS 7937 AFTER LANDING CREW REPORTED THAT ACRFT HAD TAKEN A LIGHTNING STRIKE. MX PERFORMED AN ENROUTE LIGHTNING STRIKE INSP IAW CRJ 200 AMM. ENTRY POINT FOUND ON LT AOA TRANSDUCER VANE, & EXIT POINT LOCATED AT RT LOWER WING TIP. NO OTHER DAMAGE NOTED. ACRFT RELEASED FOR SERVICE & SCHEDULED FOR A DETAILED LIGHTNING STRIKE INSP AFTER LAST FLT. PSA MX PERFORMED DETAILED LIGHTNING STRIKE INSP IAW CRJ 200 AMM. 2L72 4F4 FRTA21EA E15NE 20050519000792005051900079EU 2005 5 19 DHL2005364001 120050425A5311 FRAME AIRBUS300 A300B4203 3930306EU FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01364DH 141 FRAME 47 REPAIR RSA FROM AIRBUS IS INTERIM FOR 6 MONTH REF RAS/AS/0114/2004 MSI 05574. REPAIR DESIGN APPROVAL SHEET REF RAS/AS/0114/2004 ISSUE B DATE 12/10/04 INTERIM LIMIT NONE THIS CLEARS MSI 05574. 2L72 4F RTA35EU 20050519000802005051900080EA 2005 5 19 ASOA05305 120050403A5210601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27836AS 7263 DURING A GROUND INSPECTON, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECK GOOD. AC OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050519000812005051900081EA 2005 5 19 ASOA05304 120050403A3397VS643 RELAY CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT DEFECTIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27906EV 7642 DURING A GROUND INSPECTION, THE EMERGENCY LIGHTING REMAINED ILLUMINATED WHEN IN THE ARM POSITION. MAINTENANCE FOUND RELAY K1XD DEVECTIVE, REMOVED AND REPLACED IT IAW AMM. OPS CHECK GOOD. AC OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050519000862005051900086NM 2005 5 19 DHL2005783512 120050413A5712 RIB BOEING727 727227 1384078NM WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01783DH 21999 NR 5 SLAT INTERIOR AT ACTUATOR ATTACHMENT INB RIB CRACK NOTED WS 410. REMOVED NR 5 LE SLAT ACTUATOR ASSY IAW 727 MM 27-81-32 AND 27-81-11. REMOVED CRACKED U-CHANNEL IAW 727 SRM 51-30-2 AND FABBED NEW FROM 2024T3 .071 PONR 9002193 DIM.15 INCH BY 3 1/8 INCH IAW 727 SRM 57-50-2 FIG 2. PART TREATED, PRIMED, AND INSTALLED IAW 727 SRM 51-10-2 AND 51-30-2 DAMAGED RIBS PN 65-17276-9 PO NR 5079118 AND 65-17276-11 PO NR 4246220 IAW 727 SRM 51-30-2. REINSTALLED SLAT ACTUATOR IAW 727 MM 27-81-32 AND 27-81-11. PERFORMED OPS AND LEAK CHECK IAW B727 MM 27-81-0 FOUND OK. 2L73 4F A3WE 20050519000872005051900087NM 2005 5 19 DHL2005783513 120050404A5411 FRAME BOEING727 727227 1384078NM NR 2 NACELLE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01783DH 21999 NR 2 ENGINE STRUT RT COWLING FRAME CRACKED AT 3RD CUTOUT (ENGINE SUPPORT STRUCTURE). ROUTED OUT DAMAGED AREA AND FABBED REPAIR ANGLE FROM 301 1/2HD .050 PO NR 90001233 DIM 7 3/4" BY 3 1/2" IAW 727 SRM 54-10-2 FIG 8 AND 51-40-3 FIG 1. REPAIR ANGLE TREATED, PRIMED, AND INSTALLED IAW 727 SRM 51-10-2 AND 51-40-3 FIG 1. 2L73 4F A3WE 20050519000902005051900090NM 2005 5 19 UPS05444382 120050411A531165B017151029 FRAME BOEING747 747283B 1384867NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 BS 440 FRAME INNER FLANGE AND WEB CRACKED BTN S-14R AND S-14ER (CRACK LENGTH 4" ). BS 440 FRAME INNER FLANGE ANGLE AND WEB REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050519000912005051900091NM 2005 5 19 UPS05444383 120050411A531165B01715U178 FRAME BOEING747 747283B 1384867NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 RT BS 440 FRAME (JUST BELOW U/D FLR BEAM LWR CHORD ) WEB CRACKED. (CRACK LENGTH 2.5" ). BS 440 RT FRAME WEB REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050519000922005051900092NM 2005 5 19 UPS05444384 120050411A531065B01716172 FRAME BOEING747 747283B 1384867NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 RT BS 460 FRAME (JUST BELOW U/D FLOORBEAM LWR CHORD) WEB CRACKED, CRACK LENGTH 1.875. FRAME WEB REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050519000942005051900094NM 2005 5 19 UPS05444386 120050411A533065B09637Y1 SKIN BOEING747 747283B 1384867NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 LOWER FX EXTERNAL SKIN SURFACE RT POTABLE WATER TANK SERVICE CONNECTOR ATT DOUBLER FOUND SURFACE CORROSION AT STA 975 TO STA 980. CORROSION BLEND OUT 0.040 INCH BY 1 INCH BY 3 INCH EXCEED SRM 53-30-01 FIG 1 LIMITS, DOUBLER REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050519000952005051900095NM 2005 5 19 UPS05444387 120050409A5311 FRAME BOEING747 747283B 1384867NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 BS 320 S24 L - S26L, FRAME FOUND CRACKED, CRACK LENGTH 2.5 INCH. FRAME REPAIRED AS PER HX RS R53-12-35287 AND UPS EO NR B747-5310-22087-A. 2L74 4F A20WE 20050519000962005051900096NM 2005 5 19 UPS05444388 120050411A531165B01716171 FRAME BOEING747 747283B 1384867NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 BS 460 LT FRAME, JUST BELOW U/D FLOORBEAM LOWER CHORD. WEB CRACKED, CRACK LENGTH 1 INCH. BS 460 LT FRAME WEB REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050519000982005051900098WP 2005 5 19 05FDEA01173 120050428A3150 CONTROL UNIT DOUG DC10 DC1010 3022110WP AURAL WARNING MALFUNCTIONED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO2540061 46973 PASSING 10000 FT ACCELERATING THROUGH 260 KNOTS. THE AURAL OVERSPEED WARNING SOUNDED (SLATS RETRACTED) CLEAN CONFIGURATION SLOWED AND RECYCLED SLATS AND ACCELERATED AGAIN PASSING 260 KNOTS THE WARNING CAME ON AGAIN. ALSO TRIED CADC BOTH 1 AND BOTH ON 2 AND THE HORN STILL SOUNDED. REMOVED AND REPLACED AURAL WARNING UNIT IAW DC10-10 MM 31-51-00-5. OPS CHECK GOOD IAW DC10-10MM 31-51-00- 5. OK FOR SERVICE. 2L73 4F A22WE 20050517000502005051700050EA 2005 5 17 ASOA05332 120050413A33501317 LAMP BRUCE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27906EV 7642 DURING OVERNIGHT MAINTENANCE, THE EXTERIOR EMERGENCY LIGHT FORWARD OF THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EXTERIOR EMERGENCY LIGHT FORWARD OF THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050517000622005051700062EU 2005 5 17 DHL2005367513 120050403A5347TMS6022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01367DH 39174 DURING C-CHECK, CABIN SEAT TRACK AT FS 18 THRU 21A AT BL 0 HAS CORROSION. REPLACED SEAT TRACK SECTION FROM BS 1393-1780 BL 0 IAW SRM 51-30-30 AND 53-10-10 MAT USED TMS 60-22457 P/O 2113624 162" LONG. 2L72 4F RTA35EU 20050517000692005051700069EA 2005 5 17 ASOA05323 120050408A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27913EV 7731 DURING A GROUND INSPECTION, THE LAST OVERHEAD EMERGENCY FLOODLIGHT WAS FOUND TO INOPERATIVE. MAINT REMOVED AND REPLACED THE LAMP IN THE LAST OVERHEAD EMERGENCY FLOODLIGHT. OPS CHECK GOOD, AC OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050517000732005051700073CE 2005 5 17 BSYA200500009 120050421A3260 LIGHT BEECH 58 58 1152740CE MLG LOOSE E BSYAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL07400RP TH319 ON APPROACH INTO CMH PILOT SAID HE HAD NO GEAR DOWN AND LOCK LIGHT. DID A FLY-BY PAST CONTROL TOWER AND MAINTENANCE PERSONAL ON GROUND CONFIRMED GEAR DOORS WHERE CLOSED AND GEAR LOOK DOWN AND LOCKED. LANDED AIRCRAFT NO PROBLEMS. MAINTENANCE JACKED AIRCRAFT, RAN GEAR, FOUND THAT THE GEAR DOWN AND LOCK LIGHT WAS UNSCREWED FIVE TURNS. RAN LIGHT BACK IN AND OUT 1/2 TURN TO GET IRIS OPEN TO SEE GREEN DOWN AND LOCK INDICATION, RETURNED TO SERVICE. 1L72 3O 3A16 20050517000742005051700074EA 2005 5 17 ASOA05321 120050408A2150 A/C PACK CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LEFT MALFUNCTIONED A ASOABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27849AS 7347 DURING CRUISE, WITH THE LT PACK DEFERRED, AT APPROXIMATELY 25,000 FT THE CREW RECEIVED A MASTER CAUTION (CABIN ALT) MESSAGE. WHILE COMPLYING WITH THE QRH, A MASTER WARNING (CABIN ALT) MESSAGE WAS RECEIVED. THE CREW PERFORMED AN EMERGENCY DESCENT AND DECLARED AN EMERGENCY. THE AIRCRAFT LANDED SAFELY. MAINT DETERMINED THE ABOVE EVENT OCCURRED DUE TO PACK OVERPRESSURE AND IT AUTO SHUTDOWN. MAINT GROUND RAN THE RT ENGINE WITH DUCT PRESSURE AND PACK PRESSURE BEING NORMAL. OPS CHECK GOOD. AC OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050517000932005051700093WP 2005 5 17 UPS05844361 120050402A5340375584741 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 INSPECTION TYPE: C1, BANANA FITTING CRACKED.25 INCH LONG STA 1220 L33R. REMOVED AND REPLACED BANANA FITTING IAW SRM 51-01-20D AND 51-3-0. 2L74 4F RT4A25 20050517000942005051700094WP 2005 5 17 UPS05844364 120050330A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING LE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 INSPECTION TYPE: C1, LT WING LEADING EDGE UPPER SURFACE 10 FT O/B OF NR 1 ENG STUB WING HAS FASTENER BULGING & PULLED THROUGHT SKIN. INSTALLED DOUBLER AND CONICAL WASHERS IAW SRM 51-1-26 & 57-2-1. 2L74 4F RT4A25 20050517001012005051700101WP 2005 5 17 UPS05844373 120050404A57145645332 FINGER DOUBLER DOUG DC8 DC873F 302199FWP WING BOX CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 INSPECTION TYPE:C1 MAIN CABIN CENTER WING BOX SUB FLOOR, FINGER DOUBLER HAS SHEAR HEAD FASTENERS AND CORROSION AT STA 960 TO 980 LBL 65. REMOVED FINGER DOUBLER AND REMOVED CORROSION ON SUB FLOOR. FOUND TO BE WITHIN LIMITS. REPLACED FINGER DOUBLER IAW SRM 51-1-8, DWG 5645332, 53-2-0 FIG 1F AND 51-1-21. 2L74 4F RT4A25 20050517001062005051700106NM 2005 5 17 C8GA20050011 120050422A535065732941 RADOME BOEING727 7272A1 138407FNM FUSELAGE LIGHTNING STRIKEA C8GAA UNSCHED LANDING O OTHER CRCRUISE 1 SO29286SC52737 21601 FLT 716 FROM TOL TO MEM, DURING CRUISE OPERATION, AIRCRAFT FLEW THROUGH HEAVY WEATHER. DIVERTED TO BNA AND LANDED WITHOUT INCIDENT. ON POST FLIGHT FOUND LARGE HOLE IN RADOME APPROXIMATELY ONE FOOT IN DIAMETER. AFTER INSPECTION, DETERMINED TO BE LIGHTNING STRIKE. REPLACED RADOME AND PERFORMED LIGHTNING STRIKE INSPECTION. NO OTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2L73 4F A3WE 20050517001072005051700107NM 2005 5 17 72300170 120050201A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A .75 X 2 INCH AREA OF CORROSION ON BOTTOM OF SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050517001082005051700108NM 2005 5 17 72300171 120050425A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSLEAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A .75 X .75 INCH AREA OF CORROSION ON BOTTOM OF SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050517001152005051700115NM 2005 5 17 QXEA200500714 120050419A5310 STOP FITTING DHAV DHC8 DHC8202 2809007NM ZONE 200 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - BOTTOM FORWARD BAG DOOR STOP CHAFED. REPAIRED IAW RD 8-53-104. 2H72 4T RTA13NM 20050517001162005051700116NM 2005 5 17 QXES200500719 120050423A5310 STOP FITTING DHAV DHC8 DHC8202 2809007NM ZONE 800 WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - RIGHTHAND FORWARD EMERGENCY EXIT DOOR STOPS ON DOOR HAVE STEP WEAR. REPAIRED IAW RD 8-52-349 AND DHC-8-200 TASK 52-20-16-830-802. 2H72 4T RTA13NM 20050517001212005051700121NM 2005 5 17 QXEA200500715 120050419A5310 STOP FITTING DHAV DHC8 DHC8202 2809007NM ZONE 200 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - BOTTOM AFT BAG DOOR STOP CHAFED. REPAIRED IAW RD 8-53-104. 2H72 4T RTA13NM 20050517001262005051700126NM 2005 5 17 QXEA200500726 120050420A5753 ROLLER DHAV DHC8 DHC8202 2809007NM ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - LEFTHAND NR 4 FLAP TRACK ROLLER SURFACE HAVE CORROSION ON INBOARD AND OUTBOARD FLANGES OF TRACK-D. REPAIRED IAW RD 8-57-988. 2H72 4T RTA13NM 20050517001272005051700127NM 2005 5 17 QXEA200500718 120050423A5310 STOP FITTING DHAV DHC8 DHC8202 2809007NM ZONE 800 WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 PDX - RIGHTHAND FORWARD EMERGENCY EXIT DOOR STOPS ON FUSELAGE HAVE STEP WEAR. REPAIRED IAW DHC-8-200 MM 20-21-21 AND RD 8-53-126. 2H72 4T RTA13NM 20050517001442005051700144EA 2005 5 17 ASOA05293 120050402A3350BF10044004 LIGHT CNDAIRCL600 CL6002B19 1900309EA GALLEY CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27862AS 7476 DURING A C-CHECK IN MCN, THE EMERGENCY EXIT LIGHT ABOVE THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY ABOVE THE SERVICE DOOR. OPS CHECKS GOOD. (M) 2L72 4F RTA21EA 20050517001452005051700145NM 2005 5 17 AMTA200500343 120050401A3350 CHARGER BOEING757 75723N 1384973NM EMERGENCY LIGHT INOPERATIVE A AMTAK NONE O OTHER ININSP/MAINT 1 GL11519AT 27975 R4 EXTERIOR EGRESS LIGHT INOPERATIVE. REMOVED AND REPLACED DC CHARGER PER AMM 33-51-07. (M) 2L72 4F RTA2NM 20050517001732005051700173EA 2005 5 17 QXEA200500743 120050419A5753 ARM CNDAIRCL600 CL6002C10 1390015EA ZONE 600 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - RIGHTHAND WING INBOARD FLAP INBOARD HINGE ARM IS GOUGED ON OUTBOARD SIDE OF THE ATTACH LUG RADIUS. REPAIRED IAW REO 67-57-54-005, HORIZON AIR EA R-57-117, CRJ700 SRM 51-24-11-001-001-A01 AND SRM 51-21-16. 2L72 4F RTA21EA 20050517001792005051700179EA 2005 5 17 QXEA200500744 120050409A5755 FASTENER CNDAIRCL600 CL6002C10 1390015EA ZONE 600 BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - RIGHTHAND WING UPPER SKIN TRAILING EDGE, OUTBOARD OF OUTBOARD MULTI FUNCTION SPOILER HAS BROKEN FASTENERS. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20050517001842005051700184EU 2005 5 17 AWXA200500502 120050403A5320D53480048203 SILL AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28638AW 455 SAL - MAJOR REPAIR - DURING C-08 CHECK, EXFOLIATION CORROSION WAS FOUND ON L-2 DOOR LOWER SILL ANGLE AT Y1600 BETWEEN FS 66 AND FS 68. MAINTENANCE REMOVED CORRODED L-2 DOOR LOWER SILL ANGLE AT Y1600 FROM FS 66 TO FS 68; INSTALLED NEW REPLACEMENT SILL ANGLE IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050517001872005051700187EU 2005 5 17 AWXA200500505 120050401A5320D53112818202 FLOOR SUPPORT AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28638AW 455 SAL - MAJOR REPAIR - DURING C-08 CHECK, GALVANIC CORROSION WAS FOUND ON CABIN DUMMY RAIL Y254 BETWEEN FS 16+10" AND FS 20. MAINTENANCE CUTOUT DAMAGED SECTION OF DUMMY RAIL Y254 FROM FR 16+10" TO FR 20; FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED REPAIR PARTS IAW A320 SRM 53-11-14, FIG 201. 2L72 4F RTA28NM 20050517002062005051700206EA 2005 5 17 QXEA200500751 120050412A5350 STRAP CNDAIRCL600 CL6002C10 1390015EA ZONE 100 BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - LOWER FUSELAGE AFT WING TO BODY FAIRING HAS STRAP BROKEN. REPAIRED IAW CRJ700 SRM 53-82-83-400-803-A01 AND HORIZON AIR EA R-53-307. 2L72 4F RTA21EA 20050517002092005051700209NM 2005 5 17 05FDEA01144 120050427A5260 ROLLER BOEING727 727233 138408ANM AIRSTAIR DAMAGED A FDEAO OTHER O OTHER LDLANDING 1 SO25257FE 20939 DURING LANDING ROLLOUT, AFT AIRSTAIR EXTENDED. REMOVED AND REPLACED AFT RT SIDE ROLLER BECAUSE ROLLER DOES NOT TURN. REPLACED MAIN BEARING AS PER 727-200 M/M 52-62-001-1, T/S DOOR OPS CKED OK. OK FOR FLT. 2L73 4F RTA3WE 20050517002102005051700210NM 2005 5 17 L0FR200500005 120050428A324626113555 WHEEL BOEING747 747200 1384847NM MLG CRACKED B Q2SAK NONE O OTHER ININSP/MAINT 1 AL03 CRACKED KEY BOSS IDENTIFIED PER HONEYWELL CMM 32-45-12, APPENDIX A, KEY BOSS INSPECTION AREA. CRACKED IDENTIFIED USING EDDY CURRENT. 2L74 4F RTA20WE 20050517002132005051700213EA 2005 5 17 QXEA200500756 120050413A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - FORWARD FUSELAGE, FORWARD LOWER SKIN PANEL FS 469 TO 477 BETWEEN STRINGER 24L AND 25L ROCK CHIP PITTING DAMAGE. REPAIRED IAW REO 670-53-21-094 AND HORIZON AIR EA R-53-308. 2L72 4F RTA21EA 20050517002162005051700216EA 2005 5 17 QXEA200500757 120050413A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - FORWARD FUSELAGE, FORWARD LOWER SKIN PANEL ROCK CHIP PITTING DAMAGE FS 437 TO 453 BETWEEN STRINGER 25R AND 25L. REPAIRED IAW CRJ700 SRM 51-26-00-001-001-A01, 51-12-00-001-001-A01, AND 53-21-01-101-006-A01. 2L72 4F RTA21EA 20050518000052005051800005NM 2005 5 18 2005UALA00321 120050409A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29584UA 26706 AFT CARGO FRAME IS DENTED AT STA 1420 AT STR 25-26L. FRAME DENT WAS CUTOUT AND A DOUBLER REPAIR WAS INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050518000072005051800007NM 2005 5 18 2005UALA00324 120050409A5230 INTERCOSTAL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CARGO DOOR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29308UA 23669 AFT CARGO DOOR T-CHORD INTERCOSTAL AND WEB CRACKED AT BS 798 IN LINE WITH 2ND DOOR STOP FROM THE LOWER END. ACCOMPLISHED. INSTALLED NESTED DOUBLER L-ANGLE AND STRAP REPAIR. 2L72 4F4 FRTA16WE E2GL 20050518000092005051800009NM 2005 5 18 2005UALA00331 120050411A5320 STIFFENER BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE E&E BAY CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29665UA 29237 E+E COMPT, BS 246 FLOORBEAM VERTICAL STIFFENER FLANGE CRACKED RBL 11.53 INCHES. STIFFENERS ON THIS FLOORBEAM ARE KNOWN TO CRACK. DISCREPANCY FOUND ON ROUTINE INSPECTION. CRACKED PART WAS REPLACED WITH NEW. 2L72 4F4 FRTA1NM E24NE 20050518000122005051800012NM 2005 5 18 2005UALA00336 120050411A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE GOUGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29308UA 23669 FWD CARGO DOOR CUTOUT, FWD SIDE AT APPROXIMATELY MID POSITION WAS FOUND TO HAVE DEEP GOUGE. INSTALLED 25 IN X 27 IN, TRIPLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20050518000142005051800014NM 2005 5 18 2005UALA00338 120050411A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29309UA 23670 FUSELAGE DENT STA 389 BETWEEN STR 17L AND 18L. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20050518000242005051800024NM 2005 5 18 05FDEA01105 120050423A5712ARB2920 RIB DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 LT WING LEADING EDGE CAVITY BETWEEN SLAT TRACK NR 17 AND NR 18 FOUND WITH RIB FLANGE CRACKED. FABRICATED AS PER DRAWING NR: ARB2920. RIBS PN ARB2920-41 AND ARB2920-47. REMOVED AND REPLACED IAW SRM 51-35-01 VOLUME II. 2L73 4F RTA22WE 20050518000382005051800038NM 2005 5 18 2005UALA00358 120050417A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29585UA 26709 EXTERNAL FUSELAGE SKIN AT BS 758, STRINGER 16L IS DENTED. REPAIR DOUBLER AND TRIPLER WERE INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050518000442005051800044 2005 5 18 2005UALA00367 420050331A2565B14056916 O-RING AIRCRUISERS D30654122 BOEING757 757222 1384956NM PWA 2037 PW2037 NE INFLATION VALVE LEAKING A UALAK NONE O OTHER ININSP/MAINT 1 WP29576UA 0457 26690 LOW SLIDE PRESSURE. PRESSURE LOSS WAS DUE TO LEAKAGE AT RESERVOIR TO VALVE O-RING. O-RING WAS REPLACED. 2L72 4F4 FRTA2NM E17NE 20050518000452005051800045 2005 5 18 2005UALA00369 420050408A2565D31354433U1 ASPIRATOR BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE SLIDE LEAKING A UALAK NONE O OTHER ININSP/MAINT 1 WP29303UA 23644 DAMAGED ASPIRATOR, FLAPPER VALVE. SUPPORT ROD LOOSE. FLAPPERS WERE LEAKING. REPLACED OF THE ASPIRATOR. 2L72 4F4 FRTA16WE E2GL 20050518000592005051800059EA 2005 5 18 QXEA200500777 120050413A5414 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 400 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - LEFT NACELLE LIPSKIN HAS GOUGES BETWEEN 6 AND 8 O'CLOCK POSITION. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01, 54-11-08-101-001-A01, AND 51-21-11-001-001-A01. 2L72 4F RTA21EA 20050518000612005051800061NM 2005 5 18 DHL2005752003 120050426A3350 BATTERY PACK BOEING727 727223 1384074NM EMERGENCY LIGHT INOPERATIVE A DHLAK NONE O OTHER ININSP/MAINT 1 SO01752DH2547 22466 ENTRY DOOR EMERGENCY LIGHTS INOP. REPLACED PACK ASSY PER MM 3350, OP NML. 2L73 4F A3WE 20050518000982005051800098SO 2005 5 18 SWIA200514922 120050420A3320 LIGHT EMB 120 EMB120ER 3260203SO CABIN SMOKE A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM07582SW 120350 AISLE LIGHT AT 10A HAD SMOKE COMING OUT OF IT. REPLACED CEILING LIGHT FIXTURE AT 10A. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050518001002005051800100SO 2005 5 18 SWIA200514924 120050424A3350 BATTERY PACK EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT DISCHARGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07229SW 120305 CENTER SECTION OF CABIN EMERGENCY LIGHTS APPEAR INOPERATIVE. REPLACED MIDDLE ELBP IAW MM 24-33-01. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050518001042005051800104SO 2005 5 18 SWIA200514928 120050407A3350 LAMP EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07232SW 120306 ONE FLOOR LEVEL EMERGENCY LIGHT FAILS TO ILLUMINATE. RELAMPED ONE FLOOR LEVEL EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050519000012005051900001NM 2005 5 19 SWAA051207 120050421A53126546568 BULKHEAD BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29509SW 24186 DURING SCHEDULED 1/2D CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT DOME CAP, STR 15R. REPAIRED BULKHEAD PER SWA EA. 2L72 4F RTA16WE 20050519000042005051900004NM 2005 5 19 P5CA0501344 120050425A28202660608M2 CHECK VALVE BOEING747 747341 13848AMNM FUEL SYSTEM MALFUNCTIONED A P5CAO OTHER O OTHER CRCRUISE 1 EA15355MC 23395 DURING CROSS FEED FROM CENTER WING AND NR 2 AND NR 3 MAIN TANKS, ALL CROSS FEED VALVES OPEN AND NR 1 AND NR 4 TANKS BOOST PUMP OFF. NR 1 MAIN TANK QTY INCREASES 1000 KGS PER HOUR. REPLACED CHECK VALVE AT AFT BOOST PUMP NR 1. VERIFIED OPERATION OF DISCHARGE CHECK VALVE OK PER MM 28-22-06. TRANSFERRED FUEL INTO NR 1 MAIN LEAK CHECKED AND SYSTEM OPS OK. 2L74 4F RTA20WE 20050519000132005051900013 2005 5 19 SWAA051248 420050427A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29612SW 27930 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050519000142005051900014NM 2005 5 19 SWAA051249 120050427A3350101073 COVER BOEING737 7373H4 1384600NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29627SW 27935 DURING SCHEDULED SERVICE CHECK, FOUND L1 DOOR LOWER EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED COVER PER MM. 2L72 4F RTA16WE 20050519000202005051900020NM 2005 5 19 SWAA051255 120050427A53306545768 SKIN BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON FUSELAGE SKIN LAP JOINT AT BS 290 TO BS 360, STR 4R. REPAIRED SKIN PER BFG ER. 2L72 4F RTA16WE 20050519000242005051900024NM 2005 5 19 SWAA051259 120050427A53306546881 SKIN BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON FUSELAGE SKIN LAP JOINT AT BS 1016 TO BS 1088, STR 16L. REPAIRED SKIN PER BFG ER. 2L72 4F RTA16WE 20050519000342005051900034EA 2005 5 19 ASOA05306 120050403A5340600310685 FITTING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PRESSURE FLOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27820AS 7188 DURING A (C) CHECK, THE FITTING IN THE RT SIDE PRESSURE FLOOR UNDER 262CRF AT APPROX FS 454.00 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FITTING IN THE RT SIDE PRESSURE FLOOR UNDER 262CRF AT APPROXIMATELY FS 454.00. (K) 2L72 4F4 FRTA21EA E15NE 20050519000362005051900036NM 2005 5 19 SWAA051224 120050426A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500 + 13, STR 16L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050519000382005051900038NM 2005 5 19 SWAA051226 120050426A3350101331 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29443WN 29838 RIGHT OVERWING EMERGENCY EXIT SIGN COVER MISSING. INSTALLED COVER PER MM. 2L72 4F RTA16WE 20050519000482005051900048NM 2005 5 19 SWAA051236 120050426A53306545775 SKIN BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN LAP JOINT CORRODED AT BS 727C TO BS 907, STR 25R. REPAIRED SKIN PER BFG ER. 2L72 4F RTA16WE 20050519000492005051900049NM 2005 5 19 SWAA051237 120050426A53306546881 SKIN BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN LAP JOINT CORRODED AT BS 907 TO BS 1016, STR 20R. REPAIRED SKIN PER BFG ER. 2L72 4F RTA16WE 20050519000562005051900056NM 2005 5 19 SWAA051244 120050426A5313BAC1498 STRINGER BOEING737 7373A4 1384585NM NLG W/W CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29679AA 23291 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER CRACKED AT BS 203, RBL 16. REPAIRED STRINGER PER BFG ER. 2L72 4F RTA16WE 20050519000672005051900067 2005 5 19 SWAA051217 420050425A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29656SW 28401 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050519000692005051900069NM 2005 5 19 SWAA051219 120050425A53306545767 SKIN BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CORRODED BETWEEN BS 360 TO BS 500D, STR 26L. REPAIRED SKIN PER PAE ER. 2L72 4F RTA16WE 20050519000712005051900071NM 2005 5 19 SWAA051221 120050424A3350101114 BULB BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29709SW 27843 DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT R2 DOORWAY. RELAMPED EMERGENCY EXIT LIGHT PER MM. 2L72 4F RTA16WE 20050519000722005051900072 2005 5 19 SWAA051222 420050424A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29739GB 29275 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20050519000832005051900083CE 2005 5 19 20030837 120050425A5511 SPAR BEECH 1900 1900D 1154162CE HORIZONTAL STAB CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03219GL UE219 DURING ROUTINE INSPECTION, FOUR CRACKS APPROX .65 INCH LONG FOUND EXTENDING FROM THE DE-ICE LINE HOLE IN THE HORIZONTAL MAIN SPAR WEB. REPAIRED IAW WITH EO, AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA24CE 20050519000852005051900085WP 2005 5 19 AALA20050291 120050428A2150 SEAL DOUG DC9 DC982 3022082WP RT A/C PACK INOPERATIVE A AALAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SW21413AA 49324 DFW ENROUTE ON FLIGHT 1664 TAIL COMPARTMENT HIGH TEMPERATURE LIGHT CAME ON WHILE CLIMBING THROUGH 12000 FEET. IT WOULD GO OUT AT REDUCED THRUST AND CLIMB POWER AND THEN COME BACK ON. RETURNED DFW AND LANDED WITHOUT INCIDENT. REPLACED PERI-SEALS IN RT A/C PACK SUPPLY COUPLING. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED. 2L72 4F A6WE 20050519000882005051900088NM 2005 5 19 05FDEA01169 120050428A5311 FRAME BOEING727 727233 138408ANM FUSLEAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25264FE 21626 CORROSION ON FRAME BS 700 LBL 13 WL 148. REPAIRED BS 700 FRAME, LBL 13, WL 148 PER SRM 53-10-4. 2L73 4F RTA3WE 20050519001012005051900101EU 2005 5 19 ASOA05302 120050314A5311 FRAME AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27635AS 372 DURING A C-CHECK, THE OUTER CHORD AT FR 17 LT WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE OUTER CHORD AT FR17 LT IAW SRM. (K) 2H72 4T4 TRTA53EU E20NE 20050519001042005051900104SO 2005 5 19 C2XA05IA062 120050422A3350 LIGHT EMB 145 EMB145LR 3260212SO INTERPHONE INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW27149169132 9132 145415 IAH - FLIGHT 2690, DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE CABIN INTERPHONE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CABIN INTERPHONE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050519001062005051900106EU 2005 5 19 ASOA05300 120050310A5710 HOUSING AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUEL PANEL CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27635AS 372 DURING A C-CHECK, THE HOUSING ON FUEL PANEL 622CT BETWEEN RIBS 4 AND 5 ON THE RT WING WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE HOUSING ON FUEL PANEL 622CT BETWEEN RIBS 4 AND 5 ON THE RT WING IAW EO. (K) 2H72 4T4 TRTA53EU E20NE 20050519001072005051900107EU 2005 5 19 ASOA05299 120050310A5720 CHANNEL AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE LT WING CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27635AS 372 DURING C-CHECK, THE OMEGA BRACKET ON THE LT IB WING AT RIB 8 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE OMEGA BRACKET ON THE LT IB WING AT RIB 8 IAW SRM. (K) 2H72 4T4 TRTA53EU E20NE 20050519001082005051900108EU 2005 5 19 SA05042 120050419A27303945128206 COMPUTER AIRBUSA321 A321211 3930370EU ZONE 100 FAILED A USAAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 EA19179UW6857 1094 1521 MCI - FLT 201 - ENROUTE PHL - SFO, DURING CRUISE, ECAM MESSAGE F/CTL ELAC 2 PITCH FAULT GENERATED, FOLLOWED BY AN A/P 2 DISC MESSAGE. AFTERWARDS, CREW FURTHER RECEIVED ECAM MESSAGES F/CTL STABILIZER JAM AND F/CTL ALTN LAW. DURING THIS TIME, STATUS ITEMS THAT BECAME INOPERATIVE WERE: F/CTL ROT, STAB, ELAC PITCH, AND A/P 1 AND 2. AT THIS TIME, THE FLIGHT CREW REPORTED DIFFICULTY IN CONTROLLING PITCH. MANUAL TRIM WAS USED TO CONTROL PITCH. FLIGHT CREW OBSERVED THAT CONTROLLABILTY IMPROVED AS THE AIRCRAFT DESCENDED. MAINTENANCE REPLACED ELAC 2. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20050519001112005051900111EA 2005 5 19 ASOA05296 120050403A5312 FRAME CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27820AS 7188 DURING A C-CHECK, THE FRAME FS 640 BETWEEN STRINGER 9 AND 12 LT WAS FOUND TO BE CRACKED BEYOND LIMITS IN THE RADIUS FORWARD SIDE ABOVE THE BOX BEAM. MAINTENANCE IS REPAIRING THE FRAME FS 640 BETWEEN STRINGER 9 AND 12 LT IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050519001132005051900113NM 2005 5 19 DHL2005783515 120050403A5740 SUPPORT BOEING727 727227 1384078NM LE FLAP ACTUATORCRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01783DH 21999 NR 5 LE FLAP ACTUATOR SUPPORT IS CRACKED AT IB UPPER CORNER WING STA 224.5. REMOVED NR 5 LE FLAP ACT IAW B727 MM 27-81-22. UPON FURTHER EVAL, FOUND O/B SUPPORT CRACKED. REMOVED BOTH I/B AND O/B SUPPORTS IAW B727 SRM 51-30-2, FABRICATED SUPPORTS O/B AND I/B FROM 7075T6 .063 PO NR 9001660 DIM. 9 1/2" BY 6 1/4" AND 9 1/2" BY 6 1/4" IAW B727 SRM 57-10-2 FIG 3. NEW PARTS TREATED AND PRIMED IAW B727 SRM 51-10-2, INSTALLED SUPPORTS O/B AND I/B IAW B727 SRM 51-30-2. INSTALLED NR 5 LE FLAP ACTUATOR IAW B727 MM 27-81-22. OPS AND LEAK CHECK GOOD IAW B727 MM 27-81-0. 2L73 4F A3WE 20050519001152005051900115WP 2005 5 19 0500639611 120050426A216160714622 CONTROLLER DOUG DC9 DC932 3022066WP RT PACK TEMP MALFUNCTIONED A NWAAB EMER. DESCENT GJ MULTIPLE FAILURE WARNING INDICATION DEDESCENT 1 GL01611NA 47435 AT FL290 ON DESCENT, THE AIRCRAFT LOST AUTO PRESSURE CONTROL. CREW ATTEMPTED MANUAL CONTROL BUT RIGHT PACK WENT INTO OVERHEAT CONDITION AND SHUT DOWN. CABIN CLIMBED AT 1500 FPM, CREW DECLARED AN EMERGENCY, PERFORMED COM PROCEDURES, AND QUICKLY DESCENDED. PACK REACTIVATED DURING THE DESCENT, MASK DID NOT DEPLOY, AND THE AIRCRAFT LANDED UNEVENTFULLY AT CLT. BITE SHOED FAILED ALTITUDE ON BOTH AUTO PRESSURE CONTROLLERS. MAINTENANCE REPLACED THE AUTO TEMPERATURE CONTROLLER ON THE RIGHT PACK. MEL'D THE LEFT PACK AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20050519001162005051900116NM 2005 5 19 DHL2005783516 120050403A5720 SUPPORT ANGLE BOEING727 727227 1384078NM SLAT ACTUATOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01783DH 21999 NR 6 SLAT ACTUATOR INBD SUPPORT ANGLE IS CRACKED AT BOTTOM, WING STA 519. REMOVED NR 6 SLAT ACT IAW 727 MM 27-81-32. REMOVED DAMAGED I/B SUPPORT IAW 727 SRM 51-30-2. FABBED NEW SUPPORT ANGLE FROM PN AND 10133-1401 PO NR 501952 DIM.10" BY 3 1/4" IAW 727 SRM 57-10-2 FIG 3. ANGLE TREATED, PRIMED, AND INSTALLED IAW 727 SRM 51-10-2 AND 51-30-2. REINSTALLED NR 6 SLAT ACTUATOR IAW 727 MM 27-81-32. PERFORMED OPS AND LEAK CK. FOUND OK IAW B727 MM 27-81-0. 2L73 4F A3WE 20050519001172005051900117NM 2005 5 19 DHL2005783517 120050404A5753 SKIN BOEING727 727227 1384078NM RT WING FOREFLAPDELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01783DH 21999 RT WING I/B FOREFLAP PREVIOUS REPAIR IS DISBONDED ON LOWER SURFACE WBL 220. REMOVED RT I/B TE FOREFLAP FOR REPAIR IAW B727 MM. REMOVED PREVIOUS REPAIR AND CUTOUT DAMAGE AREA APPROX 4 INCH DIAMETER IAW SRM. FABRICATED ONE FILLER APPROX 4 INCH ROUND AND ONE DOUBLER APPROX 10" BY 6 1/2" USING 2024T3 .016 PO NR 9001660 IAW B727 SRM. CLEANED, PREPPED, AND APPLIED ADHESIVE PRIMER AND ADHESIVE TO ALL REPAIR SURFACES AND BAGGED FOR BONDING IAW B727 SRM. CURED REPAIR AND PERFORMED POST BOND INSP WITH NO DELAMIN NOTED IAW B727 SRM. TREATED, PRIMED, AND SEALED REPAIR IAW B727 SRM. REINSTALLED RT I/B TE FOREFLAP IAW B727 MM. OPS CK GOOD IAW B727 MM 27-51-00. 2L73 4F A3WE 20050519001182005051900118EA 2005 5 19 SWIA200514929 120050426A2741 SWITCH CNDAIRCL600 CL6002B19 1900309EA TRIM STICKING A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07406SW 7030 FO'S TRIM SWITCH STICKING. REPLACED FO'S TRIM SWITCH IAW CRJ MM 27-41-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050519001192005051900119EA 2005 5 19 SWIA200514930 120050424A2741 SWITCH CNDAIRCL600 CL6002B19 1900309EA TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07909SW 7558 STAB TRIM CH 2 MSG. REPLACED CAPTIANS TRIM SWITCH IAW 27-42-00, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050519001202005051900120EA 2005 5 19 SWIA200514931 120050422A274170609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07944SW 7764 STAB TRIM CH 2 WILL NOT ENGAGE. REPLACED HSTCU IAW MM 27-41-01. OPERATIONAL CHECKS GOOD IAW MM 27-41-00. 2L72 4F RTA21EA 20050519001222005051900122CE 2005 5 19 FFS2005F00002 120050331A52101144200341 DOOR FRAME BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA HARTZLHCB4M HCB4MP3 GL PAX DOOR CRACKED A FFSAK NONE O OTHER ININSP/MAINT 1 SO27575Q 28191 UC160 SEVERAL RIVETS HOLDING THE HINGE TO THE AIRSTAIR DOOR ASSY HAD PULLED THROUGH THE LOWER CLOSURE REINFORCEMENT. THE REINFORCEMENT, A COMPONENT OF AN AIRSTAIR DOOR REINFORCEMENT KIN, 114-4023-3, HAD BEEN INSTALLED 1,374 HOURS EARLIER AS PART OF MFG DESIGNED FIELD REPAIR. A NUMBER OF RIVETS SECURING THE AIRSTAIR DOOR HINGE TO THE FUSELAGE WERE FOUND TO BE WORKING. FURTHER INVESTIGATION FOUND CRACKS IN THE DOOR FRAME BETWEEN THE RIVET HOLES IN THE UPPER LINE OF RIVETS TOWARDS THE AFT END OF THE HINGE. (AS01200503513) 2L72 4T4 TRTA24CE E4EA 6 CP56GL 20050519001252005051900125WP 2005 5 19 ABXA050104 120050418A53305911412157 SKIN DOUG DC9 DC932F 3022067WP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23905AX 47147 EVIDENCE OF CORROSION EMITTING FROM FINGER DOUBLER JUST FORWARD OF FS 332 TO 351, LONGERON 26 RT OUTBOARD AND INBOARD SIDES. REPAIRED CORRODED SKIN IAW DC-9 SRM 53-04. 2L72 4F A6WE 20050519001262005051900126WP 2005 5 19 ABXA050103 120050415A532039164112 PANEL DOUG DC9 DC932F 3022067WP RT WHEEL WELL CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23905AX 47147 RIGHT BUTT LINE '0' ANGLE FITTING COMMON TO KEEL WEB AND RIGHT SLANT PANEL CRACKED. REPLACED ANGLE IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20050519001272005051900127WP 2005 5 19 ABXA050101 120050414A53305911423163 SKIN DOUG DC9 DC932F 3022067WP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23905AX 47147 SKIN BULGING AND RIVET HEAD POPPED AT STA 949, LONGERON 24 LEFT. REPLACED LONGERON 24 LEFT, FS 927-996 IAW DC-9 SRM 51-30-2, 51-30-5 AND 53-02. 2L72 4F A6WE 20050519001282005051900128WP 2005 5 19 ABXA050099 120050411A5330 SKIN DOUG DC8 DC863F 302198FWP FUSELAGE DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23819AX 45927 FORWARD CARGO COMPARTMENT, FORWARD DOOR OPENING LOWER AFT SKIN CUTOUT, PREVIOUS SPEED TAPE REPAIR CAME LOOSE. REPAIRED AREA IAW REA D853-51391MR. 2L74 4F 4A25 20050519001292005051900129WP 2005 5 19 ABXA050100 120050420A5730 PANEL DOUG DC8 DC863F 302198FWP LT WING DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23819AX 45927 DURING REMOVAL OF LOWER REAR SPAR FASTENERS SB 57-88, DOUBLER WAS DAMAGED ON EDGE FROM TRAP PANEL ON LEFT WING. REPAIRED AREA IAW REA D857-51393MR. 2L74 4F 4A25 20050519001302005051900130CE 2005 5 19 TIM2005F00003 120050404A5522 SKIN BEECH 1900 1900 1154160CE LT ELEVATOR CORRODED E TIMAK NONE O OTHER ININSP/MAINT 1 NM07127BA22419 UB7 CORROSION FOUND ON LT AND RT ELEVATOR: AFT LOWER SPAR CAP LT SIDE, AFT LOWER SPAR CAP RT SIDE, LT OB HINGE, RT OB HINGE, RT CENTER HINGE, LT ELEVATOR TRIM TAB PUSH ROD, RT ELEVATOR TRIM TAB HORN. (K) 2L72 4T RTA24CE 20050519001312005051900131NE 2005 5 19 ALG2005F00024 120050416A3297 WIRE SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL MLG BROKEN E ALGAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SW03519AL 760058 UPON PERFORMING THE T/O CHECK LIST, BOTH CREW MEMBERS NOTICED THAT THE LANDING GEARS WOULD NOT ACTUATE TO THE UP POSITION. CHECKED THE CIRCUIT BREAKERS AND RECYCLED LANDING GEAR, STILL IN THE LOCKED DOWN POSITION, RETURNED TO BASE WITH LESS THAN 130 KNOTS. MAINT REPAIRED BROKEN WIRE AT X1 OF RELAY K30 IN NR 1 OVERHEAD RELAY PANEL. AC PLACED ON JACKS AND GEAR WAS SWUNG AND WAS CHECKED GOOD. (K) 1G72 3U3 U H1NE E1GL 20050519001392005051900139EU 2005 5 19 AWXA200500518 120050405A5347D4N2001179511 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28638AW 455 SAL - MAJOR REPAIR - DURING C-08 CHECK, GALVANIC CORROSION WAS FOUND ON RT INBOARD SEAT TRACK -Y765 AT FR 64. MAINTENANCE CUTOUT DAMAGE IN RT INBOARD SEAT TRACK -Y765 AT FS 64; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK, A DOUBLER, AND 2 EACH "L" PROFILES; INSTALLED REPAIR PARTS IAW A320 SRM 53-00-15, FIG 202. 2L72 4F RTA28NM 20050519001412005051900141EA 2005 5 19 QXEA200500790 120050412A5730 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 600 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - RIGHT AILERON UPPER SKIN LEADING EDGE HAS CHAFE MARKS. REPAIRED IAW CRJ700 SRM 57-52-32-400-808-A01, 57-52-32-400-809-A01, 57-52-32-400-810-A01 AND SRM 57-52-32-400-811-A01. 2L72 4F RTA21EA 20050519001432005051900143EA 2005 5 19 QXEA200500816 120050408A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - FUSELAGE INTERIOR, RIGHT INBOARD SEAT TRACK AT STATION 665 HAS GOUGES ON TOP AND INSIDE SURFACES. REPAIRED IAW REO 670-53-00-013 AND CRJ700 SRM 51-21-16-001-001-A01. 2L72 4F RTA21EA 20050519001442005051900144EA 2005 5 19 QXEA200500826 120050408A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - FUSELAGE INTERIOR LEFT FLOOR SEAT RAIL AT STATION 539 IS GOUGED. REPAIRED IAW CRJ700 SRM 51-21-16-001-001-A01 AND REO 670-53-00-013. 2L72 4F RTA21EA 20050519001472005051900147EA 2005 5 19 QXEA200500817 120050417A5410 BEAM CNDAIRCL600 CL6002C10 1390015EA ZONE 400 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - LEFT PYLON HINGE BEAM AT PYLON TIE BAR HAS GOUGES ON HINGE, TOP AND LOWER LOCATION FROM TIE BAR BRACKETS RUBBING. REPAIRED IAW CRJ700 MM 78-36-05-000-801-A01, PAGE 402, PARAGRAPH C, STEPS 1-4, REO 670-78-34-360 AND CRJ700 SRM 51-25-06-001-001-A01. 2L72 4F RTA21EA 20050519001482005051900148EA 2005 5 19 QXEA200500809 120050413A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - FORWARD FUSELAGE BELOW FORWARD BAGGAGE BAY OPENING AT STATION 517.00 BETWEEN STRINGER 25L AND 26L ROCK CHIP IN SKIN PANEL. REPAIRED IAW CRJ700 SRM 51-26-00-001-001-A01, SRM 53-31-01-101-003-A01 AND SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050519001492005051900149EA 2005 5 19 QXEA200500820 120050415A7830 RETAINER CNDAIRCL600 CL6002C10 1390015EA ZONE 400 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - RT ENGINE, LOWER TRANSCOWLING HAS THREE RETAINERS THAT ARE CHAFING ON THE TORQUE BOX ASSEMBLY (4:00, 6:00 AND 8:00 O'CLOCK POSITIONS). REPAIRED IAW HORIZON AIR EA R-78-4 AND REO 670-78-34-361. 2L72 4F RTA21EA 20050519001512005051900151EA 2005 5 19 QXEA200500814 120050408A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - FUSELAGE INTERIOR, RIGHT INBOARD SEATRAIL AT STATION 571 HAS GOUGES ON TOP AND INSIDE SURFACES. REPAIRED IAW REO 670-53-00-013 AND CRJ700 SRM 51-21-16-001-001-A01. 2L72 4F RTA21EA 20050519001522005051900152EA 2005 5 19 QXEA200500815 120050408A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - FUSELAGE INTERIOR, RIGHT INBOARD SEAT TRACK AT STATION 632 TO 637 HAS GOUGES ON TOP AND INSIDE SURFACES. REPAIRED IAW REO 70-53-00-013 AND CRJ700 SRM 51-21-16-001-001-A01. 2L72 4F RTA21EA 20050519001532005051900153EA 2005 5 19 QXEA200500811 120050418A5410 COWLING CNDAIRCL600 CL6002C10 1390015EA ZONE 400 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - LEFTHAND ENGINE TRANSLATING COWL IS CHAFING ON FORWARD COWL WHEN STOWED AT UPPER ANDL LOWER COWLS. REPAIRED IAW HORIZON AIR EA R-78-39, EA R-78-40 AND REO 670-78-33-363. 2L72 4F RTA21EA 20050519001552005051900155EA 2005 5 19 QXEA200500810 120050414A7830 COWLING CNDAIRCL600 CL6002C10 1390015EA THRUST REVERSER WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - LEFT ENGINE, THRUST REVERSER, TRANSLATING UPPER COWL, INBOARD "TR CLOSED" RAMPS AND STARTERS ARE WORN. REPAIRED IAW HORIZON AIR EA R-78-41, REO 670-78-34-361. 2L72 4F RTA21EA 20050519001572005051900157EA 2005 5 19 QXEA200500823 120050413A5420 HINGE CNDAIRCL600 CL6002C10 1390015EA ZONE 400 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - RIGHT PYLON HINGE BEAM AT PYLON TIE BAR HAS GOUGES ON HINGE TOP AND LOWER LOCATIONS FROM TIE BAR BRACKETS RUBBING NR 3 HINGE POSITION. REPAIRED IAW REO 670-78-34-360 AND HORIZON AIR EA R-78-36. 2L72 4F RTA21EA 20050519001582005051900158EA 2005 5 19 QXEA200500824 120050418A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - FUSELAGE INTERIOR LEFT FLOOR SEAT RAIL AT STATION 399.0 IS GOUGED. REPAIRED IAW REO 670-53-00-013. 2L72 4F RTA21EA 20050519001602005051900160EA 2005 5 19 QXEA200500797 120050407A5753 FLAP TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 600 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - RIGHT WING OUTBOARD FLAP INBOARD GUIDE ROLLER TRACK GOUGED. REPLACED IAW CRJ700 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. 2L72 4F RTA21EA 20050519001622005051900162EA 2005 5 19 QXEA200500803 120050412A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 200 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - FUSELAGE EXTERIOR HAS NICK AT STATION 823 BELOW STINGER 15R. REPAIRED IAW HORIZON AIR EA R-53-301, REO 670-53-41-013 AND CRJ700 SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050519001642005051900164EA 2005 5 19 QXEA200500822 120050414A5420 BEAM CNDAIRCL600 CL6002C10 1390015EA ZONE 400 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - RIGHT PYLON, HINGE BEAM HAS NICK 6" FORWARD OF PYLON TIE BAR NR 3 HINGE POSITION. REPAIRED IAW HORIZON AIR EA R-78-36 AND REO 670-78-34-260. 2L72 4F RTA21EA 20050519001652005051900165EA 2005 5 19 QXEA200500805 120050411A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 200 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - FUSELAGE EXTERIOR UPPER SKIN HAS NICK AT STATION 364 AND STRINGER 4R. REPAIRED IAW CRJ700 REO 670-53-00-045 AND SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050519001702005051900170EA 2005 5 19 QXEA200500799 120050413A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 200 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - FUSELAGE EXTERIOR HAS SCRATCHES AT STATION 310 AND STRINGER 13L. REPAIRED IAW CRJ700 SRM 53-21-01-101-001-A01, SRM 51-12-00-001-001-A01 AND SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050519001722005051900172EA 2005 5 19 QXEA200500800 120050413A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 200 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - FUSELAGE EXTERIOR HAS AREAS OF NICKS ABOVE AFT CARGO DOOR AT STATION 1031 ON FUSELAGE SKIN. REPAIRED IAW HORIZON AIR EA R-53-315, REO 670-53-61-166, CRJ700 SRM 51-25-01-001-001-A01 AND SRM 51-21-16-001-001-A01. 2L72 4F RTA21EA 20050519001742005051900174EA 2005 5 19 QXEA200500794 120050413A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - FUSELAGE INTERIOR, RIGHT LOWER WEB OF FUSELAGE STATION 280 BULKHEAD IS CORRODED ALONG THE FLOOR LINE. REPAIRED IAW REO 670-53-11-052, REV A. 2L72 4F RTA21EA 20050519001762005051900176EA 2005 5 19 QXEA200500807 120050415A5230 SKIN CNDAIRCL600 CL6002C10 1390015EA CARGO DOOR NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - AFT BAGGAGE BAY DOOR HAS SCRATCHES AND NICKS ON TOP SURFACE OF OUTER SKIN. REPAIRED IAW CRJ700 SRM 52-31-01-101-001-A01, SRM 51-12-00-001-001-A01 AND SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050519001772005051900177EA 2005 5 19 QXEA200500808 120050412A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - AFT FUSELAGE SKIN GOUGED AT STATION 5.00 BETWEEN STRINGER 26R AND 25R. REPAIRED IAW CRJ700/900 SRM 51-12-00-001-001-A01, 53-00-01-101-001-A01 AND CRJ700 SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050519001782005051900178EA 2005 5 19 QXEA200500806 120050411A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 200 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - FUSELAGE EXTERIOR UPPER SKIN HAS THREE NICKS AT FASTENERS BETWEEN STATION 295 TO 322 AND STRINGER 6R. REPAIRED IAW CRJ700 SRM 51-40-00-001-001-A01, REO 670-53-00-045. 2L72 4F RTA21EA 20050519001792005051900179EA 2005 5 19 QXEA200500793 120050413A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - FUSELAGE INTERIOR, LEFT LOWER WEB OF FUSELAGE STATION 280 BULKHEAD IS CORRODED ALONG THE FLOOR LINE. REPAIRED IAW REO 670-53-11-052, REV A. 2L72 4F RTA21EA 20050519001802005051900180EA 2005 5 19 QXEA200500825 120050408A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - FUSELAGE INTERIOR LEFT SIDE SEAT RAIL AT STATION 553.0 IS GOUGED. REPAIRED IAW REO 670-53-00-013. 2L72 4F RTA21EA 20050519001812005051900181EA 2005 5 19 QXEA200500789 120050411A5751 SKIN CNDAIRCL600 CL6002C10 1390015EA AILERON CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - LEFT HAND AILERON UPPER SKIN LEADING EDGE HAS CHAFE MARKS. REPAIRED IAW CRJ700 SRM 51-41-02-001-001-A01, 57-61-01-101-001-A01, 51-25-01-001-001-A01, AND 57-52-32-700-810-A01. 2L72 4F RTA21EA 20050519001822005051900182NM 2005 5 19 05FDEA01168 120050428A5330 SKIN BOEING727 727233 138408ANM DOOR FRAME TORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25264FE 21626 FORWARD ENTRY DOOR LOWER HINGE ARM AND SNUBBER CUTOUT SKIN IS TORN. REPAIRED FORWARD ENTRY DOOR LOWER HINGE ARM CUTOUT PER SRM 51-40-2. 2L73 4F RTA3WE 20050519001832005051900183NM 2005 5 19 05FDEA01170 120050428A5322 SHEAR TIE BOEING727 727233 138408ANM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25264FE 21626 CORROSION ON SHEAR TIE LOWER SURFACE AT SKIN BS 1130 BETWEEN STR 29L AND STR 30. REPLACED SHEAR TIE PER SRM 53-10-1. 2L73 4F RTA3WE 20050519001842005051900184NM 2005 5 19 05FDEA01177 120050429A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 MAIN DECK IN BETWEEN STA 420 & 495 RBL 95.5 SEAT TRACK FOUND CORRODED. SEAT TRACK REMOVED AND NEW SEAT TRACK P/N ABA 7681-503 INSTALLED AS PER SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20050519001862005051900186NM 2005 5 19 05FDEA01179 120050429A5321 FLOOR PANEL BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25254FE 20936 CORROSION ON LEFT TRANS PANEL FWD PIT STA 540-545. REMOVED AND REPLACED TRANSITIONAL PANEL IAW SRM 51-30-2 AT MAE ON N/R N00892. 2L73 4F RTA3WE 20050519001872005051900187EU 2005 5 19 05FDEA01180 120050430A5754 PANEL AIRBUS300 A300F4605R 3930327EU LE SLAT CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25662FE 761 OUTBOARD LANDING LEADING EDGE SLAT INBOARD PANEL 523BB NEXT TO PYLON LANDING IS CRACKED ON CORNER REF N00643. REMOVED AND FABRICATED & INSTALLED NEW LANDING IAW DRW A57248771 AND SRM 51-40-21. 2L72 4F RTA35EU 20050519001892005051900189EU 2005 5 19 05FDEA01182 120050430A5755 SKIN PANEL AIRBUS300 A300B4605R 3930308EU NR 3 SPOILER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25662FE 761 LEFT WING UPPER SURFACE T/E ON THE WING FOUND 6 INCH CRACK ON SKIN PANEL I/B SIDE OF NR 3 SPOILER I/B HINGE REF N00723. CUT OUT DAMAGE & REPAIRED WING T/E IAW SRM 57-51-12. 2L72 4F RTA35EU 20050519001902005051900190EU 2005 5 19 05FDEA01183 120050430A5754 SUPPORT ANGLE AIRBUS300 A300B4605R 3930308EU KRUEGER FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25662FE 761 LEFT WING KRUEGER FLAP SUPPORT ANGLE ON WEB IS CRACKED REF N00164. REMOVED DAMAGE AREA, FABRICATED REPAIR DOUBLER AND FILLER. INSTALLED REPAIR IAW SRM 51-71-40. 2L72 4F RTA35EU 20050519001922005051900192EU 2005 5 19 05FDEA01185 120050430A5730 ACCESS PANEL AIRBUS300 A300B4605R 3930308EU LT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25662FE 761 LEFT WING FUEL CELL ACCESS PANEL CUTOUT 550PB 1 EA SCREW HOLE WITH ELONGATED OUTER FACE REF N00406. COMPLIED WITH EA 6-5710-87830. 2L72 4F RTA35EU 20050519001942005051900194EU 2005 5 19 05FDEA01187 120050430A5730 ACCESS PANEL AIRBUS300 A300B4605R 3930308EU RT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25662FE 761 RIGHT WING FUEL TANK OPENING 650PB AT APPROX 8 O`CLOCK POS HAS 1 EA ELONGATED HOLE REF N00645. COMPLIED WITH EA 6-5710-87830. 2L72 4F RTA35EU 20050519001972005051900197NM 2005 5 19 SB05054 120050429A335020121 CHARGER BOEING737 7374B7 1384702NM EMERGENCY LIGHTSINOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 CLT - FOUND EMERGENCY LIGHTS FROM ROWS 14 THROUGH 20 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER. 2L72 4F RTA16WE 20050519001982005051900198NM 2005 5 19 05FDEA01193 120050501A5322 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25264FE 21626 CORROSION ON SHEAR TIE BS 680 LBL 0 WL 148. REPAIRED SHEAR TIE PER SRM 53-10-1. 2L73 4F RTA3WE 20050517001772005051700177EA 2005 5 17 QXEA200500732 120050413A5755 FASTENER CNDAIRCL600 CL6002C10 1390015EA ZONE 500 BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - LEFTHAND WING UPPER SKIN, TRAILING EDGE, OUTBOARD SIDE OF OUTBOARD MULTI SPOILER HAS TWO BROKEN FASTENERS. REPLACED IAW CRJ700 SRM 51-62-06-001-001-A01. 2L72 4F RTA21EA 20050517001822005051700182EU 2005 5 17 AWXA200500500 120050426A2560P4010021 BATTERY AIRBUS320 A320232 3930326EU FLASHLIGHT DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28661AW 1284 LAS - EMERGENCY EQUIPMENT - DURING 4-DAY CHECK, THE AFT EMERGENCY FLASHLIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050517002112005051700211NM 2005 5 17 MWEA050036 120050426A3350BF50505901 LENS BOEING717 717200 1383700NM SIGN BROKEN A MWEAK NONE O OTHER ININSP/MAINT 1 GL31919ME 55181 THE MAIN CABIN DOOR EMERGENCY LENS EXIT SIGN HAS COME OFF THE CEILING ABOVE THE DOOR. REINSTALLED LENS COVER. 2L72 4F TRA6WE 20050517002222005051700222EU 2005 5 17 05FDEA01164 120050428A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25662FE 761 MAIN CABIN CLS ADAPTOR AT FR 67 BETWEEN SEAT TRACK 3L AND 4L IS CRACKED REF N00622. REMOVED AND REPLACED CLS ADAPTOR IAW SRM 51-72-10. 2L72 4F RTA35EU 20050517002262005051700226NM 2005 5 17 05FDEA01022 120050415A5553654233010 FITTING BOEING727 727200 138407ENM VERTICAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 VERTICAL STAB TENSION TIE RT AFT FITTING CORRODED. REPAIRED IAW EA 7-5530-86279. 2L73 4F RTA3WE 20050518000112005051800011NM 2005 5 18 2005UALA00335 120050411A5241 DOOR FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE GALLEY DOOR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29308UA 23669 FWD GALLEY DOOR, AFT LWR CORNER FRAME IS CRACKED AT FASTENER HOLE 2 EA PLACES. REPLACED FRAME. 2L72 4F4 FRTA16WE E2GL 20050518000212005051800021NM 2005 5 18 HNAA0500041 120050421A3320BR63031023 LIGHT DHAV DHC8 DHC8102 2809003NM CABIN BURNED A HNAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA07810EX3322033220 308 BURNING ODOR AT ROW 4 IN CABIN. FOUND OVERHEAD LIGHT AT 4DF DAMAGED. DEACTIVATED LIGHTS IAW EO 8-33-05-0255. REMOVED AND REPLACED OVERHEAD AFT LIGHT FIXTURE AT 4AC. 2H72 4T RTA13NM 20050518000312005051800031NM 2005 5 18 2005UALA00351 120050416A5310 SHEAR WEB BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29585UA 26709 AFT CABIN SHEAR WEB IS CORRODED AT STA 1681 TO 1720 AROUND DRAIN ATTACH FASTENER HOLES RBL 48. CORROSION WAS REMOVED AND A DOUBLER REPAIR INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050518000332005051800033NM 2005 5 18 2005UALA00353 120050416A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSLAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29585UA 26709 FWD PIT LEFT SIDE STA 660 FRAME HAS DENT ABOVE STR 25L UPPER FLANGE. REMOVED DAMAGE AND INSTALLED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20050518000482005051800048EU 2005 5 18 2005UALA00382 120050421A2931CZ9DM6A600U TRANSDUCER AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE GREEN SYSTEM FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29402UA 439 CREW RECEIVED LOW PRESSURE GREEN HYDRAULIC PUMP INDICATION. GREEN SYSTEM PRESSURE TRANSDUCER FAILED. REPLACED THE TRANSDUCER. 2L72 4F4 FRTA28NM E40NE 20050518000512005051800051EA 2005 5 18 QXEA200500779 120050413A5330 SKIN PANEL CNDAIRCL600 CL6002C10 1390015EA ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - FORWARD FUSELAGE, FORWARD FUSELAGE LOWER SKIN PANEL HAS ROCK CHIP PITTING DAMAGE AT STATION 319.70 TO 333 BETWEEN STRINGER 26R AND STRINGER 25R. REPAIRED IAW CRJ700 SRM 51-26-00-001-001-A01, 53-21-01-101-002-A01, AND 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050518000532005051800053EA 2005 5 18 QXEA200500770 120050411A5240 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 800 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - FUSELAGE GALLEY SERVICE DOOR OUTER SKIN HAS NICK BELOW CLOSE HANDLE. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01, 53-00-01-101-001-A01,AND 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050518000552005051800055EA 2005 5 18 QXEA200500773 120050414A5330 SKIN PANEL CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - FORWARD FUSELAGE, FORWARD LOWER SKIN PANEL CHAFING DAMAGE BY POTABLE WATER SERVICE DOOR STATION 349 TO 364 BETWEEN STRINGER 21R AND STRINGER 24R. REPAIRED IAW HORIZON AIR EA R-53-312 AND REO 670-53-21-095. 2L72 4F RTA21EA 20050518000572005051800057EA 2005 5 18 QXEA200500775 120050413A5330 SKIN PANEL CNDAIRCL600 CL6002C10 1390015EA ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - FORWARD FUSELAGE, FORWARD LOWER SKIN PANEL HAS ROCK CHIP PITTING DAMAGE AT STATION 333 TO 349 BETWEEN STRINGER 25R AND STRINGER 26R. REPAIRED IAW CRJ700 SRM 51-26-00-001-001-A01, 53-21-01-101-006-A01, 51-12-00-001-001-A01, AND 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050518000582005051800058EA 2005 5 18 QXEA200500776 120050414A5414 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 400 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC-RIGHT NACELLE LIP SKIN HAS GOUGES BETWEEN 3 AND 5 O'CLOCK POSITION. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01, 54-11-05-101-001-A01, AND 51-21-11-001-001-A01. 2L72 4F RTA21EA 20050518000602005051800060EA 2005 5 18 QXEA200500778 120050413A5414 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 400 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC-RIGHT PYLON, TOP SIDE, CENTER SECTION MISSING AREA OF PAINT. REPAIRED IAW CRJ700 SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050518000622005051800062NM 2005 5 18 DHL2005752004 120050426A3350 LIGHT BOEING727 727223 1384074NM CABIN INOPERATIVE A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01752DH 22466 DURING SBY PWR CHECK, FWD ENTRY DOOR EXIT LIGHT DID NOT ILLUMINATE. REMOVED AND REPLACED FWD ENTRY DOOR EXIT LIGHT IAW M/M 33-50-00, CKS NORMAL. 2L73 4F A3WE 20050518000642005051800064EU 2005 5 18 MALA050384 120050426A53207253710871 FLOOR SUPPORT SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15416XJ 340B416 AIRSTAIR FLOOR RAIL, P/N 7253710-871 IS CORRODED AND WILL BE REPLACED IAW SRM 51-40-21/22. 2L72 4T RTA52EU 20050518001122005051800112 2005 5 18 SWAA051197 420050422A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29656SW 28401 DURING SCHEDULED C1 CHECK, FOUND L2 DOOR EVACUATION SLIDE PRESS IND OUT OF VIEW. ADJUSTED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20050518001142005051800114 2005 5 18 SWAA051200 420050423A256563551101 SLIDE BOEING737 7377H4 1384404NM R2 DOOR OUT OF LIMITS A SWAAK NONE O OTHER ININSP/MAINT 1 SW29748SW 29800 DURING SCHEDULED MV2, FOUND R2 DOOR EVACUATION SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20050518001162005051800116NM 2005 5 18 SWAA051202 120050423A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29326SW 23690 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 485, STR 16R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050518001182005051800118NM 2005 5 18 SWAA051206 120050421A53116546539 FRAME BOEING737 7375H4 138449DNM MID CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29509SW 24186 DURING SCHEDULED 1/2D CHECK, FOUND 2 EA FUSELAGE BELT FRAME CRACKS AT INBOARD LOWER ATTACH CASTINGS, BS 616, LBL 64 & RBL 64. REPAIRED FRAMES PER SRM AND BOEING SB. 2L72 4F RTA16WE 20050519000082005051900008EA 2005 5 19 ASOA05308 120050405A33979327420513 WIRE BRUCE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE EMERGENCY LIGHT BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27741EV 10155 DURING AN (A) CHECK, THE OVERHEAD EMERGENCY CEILING LIGHT AT ROW 4 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE UNDER THE CEILING PANEL TO THE NR 2 EMERGENCY CEILING LIGHT AT CONNECTOR J357. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA EOOO63EN 20050519000102005051900010EU 2005 5 19 ASOA05307 120050405A33503011210 LIGHT AEROSPATR72 ATR72 EU PWA PW120 PW127 NE CABIN INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27631AS3478 678 362 DURING HANGAR MAINTENANCE, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSY ON THE PASSENGER DOOR. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K) 2H72 4T4 TRT E20NE 20050519000212005051900021NM 2005 5 19 SWAA051256 120050427A53306545774 SKIN BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON FUSELAGE SKIN LAP JOINT AT BS 540 TO BS 727, STR 10R. REPAIRED SKIN PER BFG ER. 2L72 4F RTA16WE 20050519000292005051900029NM 2005 5 19 SWAA051264 120050427A53206558280 STRAP BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON FUSELAGE LOWER FRAME STRAP AT BS 360, FROM RBL 14 TO LBL 14. REPAIRED FRAME PER BFG ER & SRM. 2L72 4F RTA16WE 20050519000532005051900053NM 2005 5 19 SWAA051241 120050426A53306545776 SKIN BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN LAP JOINT CORRODED AT BS 908 TO BS 950, STR 10L. REPAIRED SKIN PER BFG ER. 2L72 4F RTA16WE 20050519000552005051900055 2005 5 19 SWAA051243 420050426A2565D31354 SLIDE BOEING737 7373G7 1384595NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29670SW 23784 DURING SCHEDULED SERVICE CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050519000632005051900063 2005 5 19 SWAA051213 420050425A25656557463 GIRT BAR BOEING737 7373H4 1384600NM R2 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29374SW 26582 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FLOOR FITTING CRACKED. REMOVED AND REPLACED FLOOR FITTING PER MM. 2L72 4F RTA16WE 20050519000652005051900065NM 2005 5 19 SWAA051215 120050425A5753 SKIN BOEING737 7375H4 138449DNM RT WING FOREFLAPDELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29509SW 24186 DURING SCHEDULED 1/2D CHECK, FOUND RT WING OUTBOARD T/E FOREFLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2L72 4F RTA16WE 20050519000702005051900070NM 2005 5 19 SWAA051220 120050425A53306545769 SKIN BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CORRODED BETWEEN BS 178 TO BS 259, STR 19R & STR 24R. REPAIRED SKIN PER PAE ER. 2L72 4F RTA16WE 20050519000732005051900073CE 2005 5 19 DJFA2005087 120050426A7603 LEVER BEECH MU300 400A 1155402CE THROTTLE SPLIT E DJFAH DEACTIVATE SYST/CIRCUITS R PARTIAL RPM/PWR LOSS CRCRUISE 1 EA23795TA RK284 CREW REPORTED THAT WHILE AT CRUISE FLIGHT 380, WITH ENGINE SYNCRONIZATION ON, BOTH ENGINES ROLLED BACK FROM N1 AT 98.0 TO 90.9, OAT WAS -63 DEGREES. THE ENGINE SYNCHRONIZATION WAS TURNED OFF AND ENGINE IGNITERS WERE TURNED ON. THE CREW WAS THEN ABLE TO INCREASE POWER. A LARGE THROTTLE LEVER SPLIT WAS OBSERVED AND THE LEFT ENGINE GAUGES WERE FLUCTUATING. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. 2H72 4F RTA16SW 20050519000762005051900076EA 2005 5 19 VNAA0504004 120050420A3297 CONNECTOR CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE NLG STEERING LOOSE A VNAAO OTHER J WARNING INDICATION LDLANDING 1 GL05720PS 10178 THE CREW OF FLIGHT 2211 REPORTED THAT THE NOSEWHEEL STEERING WAS INOPERATIVE UPON LANDING AND WOULD NOT RESET IN FLIGHT. AFTER AN UNEVENTFUL LANDING AT CLT THE AIRCRAFT WAS TOWED TO THE GATE. PSA MAINTENANCE TROUBLESHOT THE SYSTEM AND FOUND THE J3 CONNECTOR ON THE NWS ECU LOOSE. THE CONNECTOR SECURED IAW CRJ 700 AMM 32-51-10-400-801-A01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050519000772005051900077EA 2005 5 19 VNAA0504005 120050421A32465010598 WHEEL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NLG OUT OF BALANCE A VNAAO OTHER EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 GL05262PS482 7962 THE CREW OF FLIGHT 2411 REPORTED NOSE WHEEL VIBRATION AFTER TAKEOFF FROM PHL. THE FLIGHT CONTINUED TO DAY AND MADE AN UNEVENTFUL LANDING. PSA MAINTENANCE FOUND THE LT NLG WHEEL AND TIRE ASSEMBLY OUT OF BALANCE DUE TO FLAT SPOTS ON THE TIRE. THE LT NLG WHEEL & TIRE ASSEMBLY WAS REMOVED & REPLACED IAW CRJ 200AMM 32-42-01-000-801 AND 32-42-01-400-801. THE NLG WAS LUBRICATED IAW CRJ 200 AMM 12-20-32-640-801. BOTH NOSE WHEEL AXLE NUT TORQUES WERE VERIFIED IAW CRJ 200 SL 32-015. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050519000842005051900084EU 2005 5 19 AALA20050290 120050428A335032141 BATTERY PACK AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217076A 610 JFK EXIT LIGHT AT 2R DOES NOT STAY ILLUMINATED. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHT AT 2R. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED. 2L72 4F RTA35EU 20050519000932005051900093NM 2005 5 19 UPS05444385 120050411A5347 SEAT TRACK BOEING747 747283B 1384867NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 BS 480-485, RBL 47 SEAT TRACK CROWN CORROSION FOUND. CORROSION BLEND OUT 0.030 INCH BY 1 INCH BY 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS, U/D BS 480-530 RBL 47 INCH SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A. 2L74 4F A20WE 20050519001102005051900110EA 2005 5 19 ASOA05297 120050403A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27820AS 7188 DURING A C-CHECK, THE ATTACH CLIP AT FS 625 LT ABOVE THE BOX BEAM WAS FOUND TO BE CRACKED BEYOUND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE ATTACH CLIP AT FS 625 LT. (K) 2L72 4F4 FRTA21EA E15NE 20050519001322005051900132SW 2005 5 19 ALG2005F00025 120050416A2910 HOSE BELL 407 407 1182206SW ALLSN 250C 250C47B GL HYD SYSTEM LEAKING E ALGAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW03587AL 53248 AT CRUISE FLIGHT AT 2750 FT, HEADING NORTH NORTHEAST, HYDRAULIC CAUTION LIGHT ILLUMINATED AND CONTROLS BECAME STIFF. MAINTENANCE FOUND THE CASE DRAIN LINE FLEX HOSE AT HYDRAULIC PUMP WAS TIGHT BUT LEAKING OIL, REMOVED AND REPLACED HYDRAULIC PUMP FOR INTERAL LEAKING. (K) 1G71 3U3 UO H2SW E1GL 20050519001422005051900142EA 2005 5 19 QXEA200500813 120050408A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - FUSELAGE INTERIOR, RIGHT INBOARD SEAT RAIL AT STATION 539 HAS GOUGES ON TOP AND INSIDE SURFACES. REPAIRED IAW REO 670-53-00-013 AND CRJ700 SRM 51-21-16-001-001-A01. 2L72 4F RTA21EA 20050519001452005051900145EA 2005 5 19 QXEA200500828 120050414A5410 DOOR CNDAIRCL600 CL6002C10 1390015EA RT NACELLE DOOR WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - RIGHT ENGINE TRANS COWL LATCH DOOR ASSEMBLY AREA, DOOR LATCH CONTACT POINT WORN. REPLACED IAW CRJ700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20050519001502005051900150EA 2005 5 19 QXEA200500821 120050418A5410 FLANGE CNDAIRCL600 CL6002C10 1390015EA ZONE 400 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - RIGHT ENGINE LOWER TRANSCOWL FORWARD FLANGE IS CHAFING ON THE TORQUE BOX AT APPROXIMATELY 7:00 POSITION. REPAIRED IAW HORIZON AIR EA R-78-38 AND REO 670-78-33-362. 2L72 4F RTA21EA 20050519001542005051900154EA 2005 5 19 QXEA200500812 120050411A1430 RIVET CNDAIRCL600 CL6002C10 1390015EA ZONE 300 LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - VERTICAL STABILIZER, RIGHT SIDE, BOTTOM AFT SKIN HAS NINE SMOKING RIVETS. REPLACED IAW CRJ7000 SRM 51-42-13-001-001-A01. 2L72 4F RTA21EA 20050519001562005051900156EA 2005 5 19 QXEA200500819 120050418A7830 COWLING CNDAIRCL600 CL6002C10 1390015EA THRUST REVERSER CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - RIGHT ENGINE UPPER TRANSCOWLING FORWARD FLANGE IS CHAFING ON TORQUE BOX STRUCTURE IN TWO PLACES AND 11:00 AND 1:00 O'CLOCK POSITIONS. REPAIRED IAW HORIZON AIR EA R-78-37 AND REO 670-78-33-362. 2L72 4F RTA21EA 20050519001592005051900159EA 2005 5 19 QXEA200500827 120050415A7830 DOOR CNDAIRCL600 CL6002C10 1390015EA THRUST REVERSER CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - RIGHT ENGINE, TRANS COWL LATCH DOOR ASSEMBLY, CHAFING ON TRANS COWL STRUCTURE AT AFT EDGE. REPAIRED IAW CRJ700 SRM 54-21-00-101-001-A01 AND SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050519001672005051900167EA 2005 5 19 QXEA200500796 120050413A5753 FITTING CNDAIRCL600 CL6002C10 1390015EA ZONE 600 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - RIGHT OUTBOARD FLAP INBOARD ROLLER FITTING HAS FRETTING CORROSION. REPAIRED IAW REO 670-57-53-015, SRM 51-25-16-001-001-A010 AND SRM 51-24-11. 2L72 4F RTA21EA 20050519001692005051900169EA 2005 5 19 QXEA200500798 120050413A5320 SILL CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - AFT BAGGAGE BAY DOOR STRUCTURE SURROUND HAS FRETTING DAMAGE ON LOWER SILL PLATE AND PAINT/PRIMMER MISSING. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01, SRM 51-21-11-001-001-A01 AND SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050519001712005051900171EA 2005 5 19 QXEA200500802 120050408A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 200 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - FUSELAGE EXTERIOR HAS NICK AT STATION 1060 AND STRINGER 13L. REPAIRED IAW CRJ700/900 SRM 53-61-01-001-002-A01 AND CRJ700 SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050519001852005051900185NM 2005 5 19 05FDEA01178 120050429A5553 ATTACH FITTING DOUG MD11 MD11 3023602NM ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 EMPENNAGE - LT FAIRING PANEL ATTACHMENT IN BETWEEN VERTICAL STABILIZER LOWER UPPER SECTION AND LOWER CENTER SECTION AT APPROX PIN 122 ADJACENT TO ACCESS PANEL 363PL FOUND CRACKED AT AFT EDGE AREA. REPAIR AS PER EA 1-5530-80384 AND SRM 51-33-01 AND 51-35-01 VOL II. MINOR REPAIR PER GMM 6-2-100. EO TITLE STABILIZERS VERTICAL STABILIZER VERTICAL AIR INTAKE PANEL ASSEMBLY REPAIR. 2L73 4F RTA22WE 20050519001882005051900188EU 2005 5 19 05FDEA01181 120050430A5730 PANEL AIRBUS300 A300B4605R 3930308EU RT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25662FE 761 RIGHT WING O/B TANK 660BB HAS 2 EA ELONGATED FASTENER HOLES REF N00383. COMPLIED WITH EA 6-5710-87830. 2L72 4F RTA35EU 20050519001912005051900191EU 2005 5 19 05FDEA01184 120050430A5730 ACCESS PANEL AIRBUS300 A300F4605R 3930327EU RT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25662FE 761 RIGHT WING FUEL OPENING 650PB AT APPROX 830 POSITION 1 EA ELONGATED FASTENER HOLE REF N00646. COMPLIED WITH EA 6-5710-87830. 2L72 4F RTA35EU 20050519001932005051900193EU 2005 5 19 05FDEA01186 120050430A5730 ACCESS PANEL AIRBUS300 A300B4605R 3930308EU RT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25662FE 761 RIGHT WING FUEL PANEL OPENING 650PB AT APPROX 3 O`CLOCK POS 1 EA ELONGATED FASTENER HOLE REF N00641. COMPLIED WITH EA 6-5710-87830. 2L72 4F RTA35EU 20050519001952005051900195NM 2005 5 19 05FDEA01188 120050430A5711 SPAR DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 LT WING REAR SPAR TOPSIDE WING CORROSION FOUND AT XORS 725. SKIN TRIMMED, REPAIR DOUBLER AND FILER FABRICATED AND INSTALLED AS PER EA 1-5720-80383. 2L73 4F RTA22WE 20050519001992005051900199NM 2005 5 19 05FDEA01194 120050501A5322 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25264FE 21626 CORROSION ON SHEAR TIE BS 580 LBL 18 WL 148. 2L73 4F RTA3WE 20050520000152005052000015NM 2005 5 20 05FDEA01121 120050426A5347ADA83891 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 MAIN DECK, FLOOR SEAT TRACK AT STA Y= 904 TO Y= 1059, X= 47 CROWN ELONGATED ADA8389-1. REWORKED AND INSTALLED IAW SRM 53-70-00 VOLUME I, FIGURE 1. 2L73 4F RTA22WE 20050520000172005052000017NM 2005 5 20 05FDEA01122 120050426A5347ADA83901 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 MAIN DECK, FLOOR SEAT TRACK AT STA Y= 804 TO Y= 810, X= -8.5 CROWN ELONGATED ADA8390-1. REWORKED IAW SRM 53-70-00 VOLUME I AND INSTALLED IAW SRM 51-35-01 VOLUME II. 2L73 4F RTA22WE 20050520000182005052000018NM 2005 5 20 05FDEA01123 120050426A5347ADA83901 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 MAIN DECK, FLOOR SEAT TRACK AT STA Y= 794 TO Y= 810, X= -27 CROWN ELONGATED ADA8390-1. REWORKED AND INSTALLED IAW SRM 53-70-00 VOLUME I, FIGURE 1. 2L73 4F RTA22WE 20050520000192005052000019NM 2005 5 20 05FDEA01124 120050426A5347ADA83891 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 MAIN DECK, FLOOR SEAT TRACK AT STA Y= 794, Y=800 AND Y= 908, X= -27 CROWN ELONGATED ADA8389-1. REMOVED IAW SRM 51-33-01 VOLUME II. NEW SEAT TRACK REWORKED AND INSTALLED IAW SRM 53-70-00 VOLUME I, FIGURE 1. 2L73 4F RTA22WE 20050520000202005052000020NM 2005 5 20 05FDEA01125 120050426A5347ADA83891 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 MAIN DECK, FLOOR SEAT TRACK AT STA Y= 970, Y=1027 AND Y= 1099, X= -47 CROWN ELONGATED ADA8389-1. REWORKED AND INSTALLED IAW SRM 53-70-00 VOLUME 1, FIGURE 1. 2L73 4F RTA22WE 20050520000212005052000021NM 2005 5 20 05FDEA01126 120050426A5753ARB0029509N STRAP DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 LEFT HAND WING, OUTBOARD FLAP INBOARD HINGE, TENSION STRAP FOUND CRACKED ARB0029-509N. REMOVED AND REPLACED IAW SRM 51-33-01 VOLUME II. 2L73 4F RTA22WE 20050520000232005052000023NM 2005 5 20 05FDEA01128 120050426A5347AEA75791 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA Y= 1398 TO Y= 1521, X= 47 CROWN ELONGATED AEA7579-1. REMOVED AND REPLACED IAW SRM 53-70-00 VOLUME I, FIGURE 1. 2L73 4F RTA22WE 20050520000242005052000024NM 2005 5 20 05FDEA01129 120050426A5347A5A70821 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA Y= 5-83 TO Y= 5- 113, X= 47 CROWN ELONGATED A5A7082-1. REMOVED, AND REPLACED IAW SRM 53-70-00 VOLUME I, FIGURE 1 2L73 4F RTA22WE 20050520000252005052000025NM 2005 5 20 05FDEA01130 120050426A5347A5A70821 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA Y= 5-83, X= -47 CROWN ELONGATED A5A7082-1. REPAIRED IAW SRM 53-70-00 VOLUME I, FIGURE 1. 2L73 4F RTA22WE 20050520000262005052000026NM 2005 5 20 05FDEA01131 120050426A5347A5A70821 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 SNRM NO.: N0592 - MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA Y= 1139 TO Y= 6- 60, X= 47 CROWN ELONGATED A5A7082-1. REWORKED AND INSTALLED IAW SRM 53-70-01 VOLUME I, FIGURE 1. 2L73 4F RTA22WE 20050520000292005052000029NM 2005 5 20 05FDEA01137 120050426A5314 KEELBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25264FE 21626 CORROSION ON LEFT KEELBEAM OUTER FLANGE BS 950C+2 TO 950C+13. REPAIRED KEELBEAM IAW FED EX SR DRAWING 27-53-023A. 2L73 4F RTA3WE 20050520000312005052000031WP 2005 5 20 UPS05844380 120050426A5330561386261 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 FUSELAGE SKIN DAMAGE RT JUST OUTBOARD OF FWD EQUIPMENT CENTER DOOR MARKED. REMOVED DAMAGED SKIN IN CORRODED AREA DIM APPX 2.9 X 2.5 INCHES. REMOVED ADDITIONAL DAMAGED SKIN APPROX 10 X 9 INCHES TOTAL UNABLE TO CLEAN UP ALL OF UNDERLYING CORROSION AT THIS TIME ACCOMPLISHED INTERIM REPAIR PER EO DC8-5330-22107-A. PERMANENT REPAIR WITHIN 1 NON REV FLT. DEFERRED D301409. 2L74 4F RT4A25 20050520000322005052000032NM 2005 5 20 05FDEA01157 120050428A7830683L213G04 THRUST REVERSER DOUG MD11 MD11F 3023600NM ZONE 400 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 NR 1 ENGINE, LEFT THRUST REVERSER COWL, UPPER TORQUE BOX FORWARD FRAME CHAMPFER FOUND CRACKED P/N 683L213G04 S/N R591-085. REPAIRED PER DRAWING SRZ-78-002. 2L73 4F RTA22WE 20050520000342005052000034 2005 5 20 SWAA051204 420050423A2565416A2200 SLIDE BOEING737 7377H4 1384404NM R2 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29434WN 32454 R2 DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20050520000362005052000036GL 2005 5 20 05FDEA01191 220050501A7261CF66D GEARBOX DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL NR 2 ENGINE CRACKED A FDEAK NONE K FLUID LOSS ININSP/MAINT 1 SO25365FE53304 46601 451280 AT B - 9 CHECK TROUBLESHOOTING OIL LEAK ON NR 2 ENGINE S/N 451280, FOUND ACCESSORY GEARBOX, FUEL PUMP DRIVE PAD, HAD A 4 INCH CRACK, EMANATING FROM DRIVE PAD. DOCUMENTED ON B - 9 CHECK WORK PACKAGE, WORK ORDER 28833, NR 108. ENGINE REPLACED ON SEQ 324 WORK CARD. ENGINE OIL LEAK/CONSUMPT/SERVICE. CLOSED 2L73 4F4 F A22WE E23EA 20050520000382005052000038NM 2005 5 20 2005UALA00387 120050424A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29586UA 26710 AFT CABIN FLOORBEAM UPPER CAP IS CORRODED AT STA 1661 RBL 60. CORROSION WAS REMOVED AND A STRAP REPAIR WAS INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050520000402005052000040NM 2005 5 20 2005UALA00392 120050426A5315141T51482 FLOORBEAM BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE PUNCTURED A UALAK NONE O OTHER ININSP/MAINT 1 WP29658UA54165 27113 E&E COMPARTMENT BS 246 FLOORBEAM WEB PUNCTURED APPROX RBL 45, WL 200. REPAIRED FLOORBEAM WEB. 2L72 4F4 FRTA1NM E24NE 20050520000432005052000043NM 2005 5 20 DHL2005762003 120050503A7921548003 OIL COOLER BOEING727 7272B7 138407LNM PWA JT8 JT8D17 52049NE NR 3 ENGINE LEAKING A DHLAEBA ENGINE SHUTDOWN EMER. DESCENT UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO01762AT 22162 AT 10,000FT, THE CREW OBSERVED THE NR 3 ENGINE PARAMETERS FLUCTUATING,FOLLOWED SPECIAL PROCEDURES SHUT DOWN THE ENGINE,DECLARED AN EMERGENCY AND DIVERTED BACK TO PHOENIX. AFTER TAKE OFF, NR 3 ENGINE PARAMETERS BEGAN FLUCTUATING. PERFORMED ABNORMAL PROCEDURE PER AOM. PERFORMED ENGINE SHUTDOWN PROCEDURE PER AOM. R&R OIL COOLER NR 3 ENG IAW B-727 M/M 79-20-1. ALSO R&R NR 3 ENG OIL TEMP BULB IAW B-727 MM 79-34-21 PN 56B17D (TEMP BULB). CKS GOOD IAW ENG RUN JRH 5.2. 2L73 4F4 F A3WE E2EA 20050520000442005052000044NM 2005 5 20 05FDEA01195 120050503A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25264FE 21626 CREASED DENT - BS 1213 - 1223, JUST ABOVE STR 20L. REPAIRED DENT IAW SRM 53-30-3. 2L73 4F RTA3WE 20050520000452005052000045NM 2005 5 20 05FDEA01205 120050504A5753 FLAP TRACK BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25264FE 21626 LEFT WING NR 3 FLAP TRACK CORRODED AT SPOILER BEAM PAD. REPLACED NR 3 FLAP TRACK ON FED EX CARD 27X5705-03 2L73 4F RTA3WE 20050520000472005052000047NE 2005 5 20 JBGA20050003 220050518A7200 ENGINE LEAR 60 60LEAR 5170707CE PWA 305 PW305 NE FLAMED OUT E JBGAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 GL07529KF 064 CA0273 ENGINE FLAMED OUT FOLLOWED BY AMBER ENGINE LIGHT. 2L72 4F4 FRTA10CE E35NE 20050520000482005052000048WP 2005 5 20 UPS05844415 120050501A5330 STRAP DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01705UP 45949 CORROSION ON SKIN SPLICE STRAP STA 450 LONG 30R. ENGINEERING SUBMITTED PROPOSAL TO BOEING FOR REPAIR. REMOVED ALL FASTENERS IN AREA OF CORROSION WS 05577521. REMOVED CORROSION AS NEEDED FOR REPAIR REF N/R 680150. 2L74 4F RT4A25 20050520000492005052000049NM 2005 5 20 PCSA05040501 120050504A3231 DOOR BOEING727 7272D3 138407NNM MLG MALFUNCTIONED A PCSAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO29804AJ 21021 AFTER TAKEOFF FROM SKBO, GEAR HANDLE WAS PLACED UP. ALL GEARS RETRACTED, BUT RT DOOR DIDN'T CLOSE. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND STOWAWAY IN GEAR DOOR OPERATION. PERFORMED A VISUAL INSPECTION AND OPERATIONAL CHECK GOOD IN ACCORDANCE WITH MM 32-12-00. AIRCRAFT RETURNED BACK TO SERVICE. 2L73 4F A3WE 20050520000502005052000050NM 2005 5 20 USAA050004A 120050501A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19335US 23232 1.250 INCH CRACK FOUND AT STA 328 AND S17R ON SKIN. INSTALLED "TEXAS" PATCH PER SRM 53-10-01 FIG. 202 2L72 4F RTA16WE 20050520000512005052000051CE 2005 5 20 DXTA200500712 120050508A7722 ENGINE CESSNA560 560XL 2076702CE PWA 545 PW545A NE LEFT MALFUNCTIONED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07612QS 5605312 PCEDB0638 ON TAKEOFF , ITT ON LT ENGINE REACHED 725 - 730 INITIALLY DECREASED THROTTLE TO IDLE W/IN 2-3 SECONDS DUPLICATED IN RUN UP PAD ITT ON LT ENGINE REACHED 720 IN CLIMB DETENT DECREASED THROTTLE TO IDLE W/IN 2-3 SECONDS. PERFORMED COMPRESSOR WASH ON LT AND RT ENGINE IAW PWA 545A MM CH 71-00-00 ACCOMPLISHED 5 PT PERFORMANCE CALIBRATION RUN IAW PRATT & WHITNEY 545A MM CH 71-00-04 RUN CHECK GOOD, ALL WITHIN LIMITS. NOTE ENGINE ITT CAN REACH AS HIGH AS 760 DEGREES TRANSIENT FOR 20 SECONDS PER 560XL FLT MANUAL & PWC 545A MM CH 5-10-00. 2L72 4F4 FRTA22CE E00059EN 20050520000522005052000052CE 2005 5 20 DXTA200500714 120050508A3240 FRICTION BRAKE CESSNA500 560CESSNA 2076750CE MLG MALFUNCTIONED E DXTAO OTHER O OTHER LDLANDING 1 GL07800QS 5600598 UPON LANDING BOTH PILOTS AND CO-PILOTS RT BRAKE PEDALS WENT SOFT. BLED AND LEAK CHECKED RT BRAKE, LEAK AND OPS CHECKS GOOD AT THIS TIME. ALL WORK DONE IAW CESSNA 560 MM CHAPTER 32-42-00. 2L72 4F RTA22CE 20050520000542005052000054NM 2005 5 20 2005UALA00407 120050504A5322 FLOORBEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29312UA 23673 AFT CABIN FLOORBEAM CORROSION STA 947 LBL 15 TO 44. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION, FABRICATED REPAIR ANGLE AND INSTALLED. 2L72 4F4 FRTA16WE E2GL 20050520000552005052000055NM 2005 5 20 2005UALA00408 120050504A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29314UA 23675 FUSELAGE FRAME IS CRACKED AT STA 616 BELOW STR 17R. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE AND INSTALLED ANGLE DOUBLER. 2L72 4F4 FRTA16WE E2GL 20050520000562005052000056NM 2005 5 20 2005UALA00410 120050505A5344 HINGE FITTING BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE R1 DOOR MISMANUFACTURED A UALAK NONE O OTHER ININSP/MAINT 1 WP29311UA 23672 UNABLE TO ADJUST GAP ON R1 DOOR. MAJOR REPAIR ACCOMPLISHED. REPLACED UPPER BODY HINGE FITTING HOUSING AND INSTALLED WEB REPAIR. 2L72 4F4 FRTA16WE E2GL 20050520000592005052000059NM 2005 5 20 BB05036 120050511A335020131A BATTERY BOEING757 757225 1384959NM L4 DOOR DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19607AU 22203 PVD - FOUND L4 DOOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. 2L72 4F RTA2NM 20050520000622005052000062NM 2005 5 20 SB05060 120050511A2170V1211 COALESCER BAG BOEING737 7373B7 1384580NM LEFT PACK BAY DIRTY A USAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA19504AU 23379 EN ROUTE FROM GSO TO CLT, CREW REPORTED A BURNING/ELECTRICAL ODOR THROUGHOUT THE CABIN AREA. FLIGHT LANDED AT CLT WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE LEFT PACK COALESCER BAG DIRTY AND HAVING AN OFFENSIVE ODOR. REPLACED SAME. RIGHT PACK COALESCER BAG CHECKED OK. RAN BOTH ENGINES AT 85 PERCENT N2 FOR SEVERAL MINUTES WITH NO BURNING ODOR NOTICED IN CABIN AREA. AIRCRAFT OK FOR SERVICE. 2L72 4F RTA16WE 20050520000632005052000063NM 2005 5 20 PIDA20050021 120050512A3350 LIGHT BOEING737 7373G7 1384595NM CABIN INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05370WL 24011 EMERGENCY EXIT LIGHT LOCATED AT SEAT ROW 7 INOP. RELAMPED EMERGENCY LIGHT AT ROW 7. OPS CHECKS GOOD PER MM 33-50. 2L72 4F RTA16WE 20050520000642005052000064WP 2005 5 20 P9RA20050080 120050513A21206411095 CONTROL VALVE DOUG DC9 DC983 3022083WP TAIL FROZEN A P9RAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO11989PG 49845 DURING TAXI CREW NOTED ELECTRICAL ODOR IN CABIN. RETURNED TO SFB GATE. FOUND WATER DRIPPING FROM RT PACK ONTO HOT DUCTING CAUSING STEAM. INSPECTED ELECTRICAL WIRING IN THE TAIL INTERIOR WITH NO DEFECTS NOTED. ASSIGNED MEL 21-01-01 TO RT PACK. MAINTENANCE ENTRY ON 5/14/05. IAD. REFERENCE ABOVE MEL. FOUND BLEED AIR LINE LOOSE AND CONNECTOR AT TEMPERATURE CONTROL VALVE LOOSE. RECONNECTED BOTH PER MM. GROUND CHECKED GOOD AND CLEARED MEL. 2L72 4F RTA6WE 20050520000652005052000065WP 2005 5 20 05FDEA01256 120050512A3620 MANIFOLD DOUG DC10 DC1030 3023501WP PNUMATIC SYS LEAKING A FDEAAO UNSCHED LANDING OTHER J WARNING INDICATION CLCLIMB 1 SO25321FE 47836 CLIMBING OUT OF SLC THRU 10,000 FT NR 3 MANIFOLD FAIL LIGHT ILLUMINATED, RAN RED TABS AND RETURNED TO SLC DUE TO ICING CONDITIONS. ALSO WING ANTI-ICE WAS NOT ON AND NR 3 TEMP GAUGE WAS RED-LINING. PERFORMED NR 3 SYS DECAY CHECK RAN ENGINES AND DETERMINED NR 3 ENG BLEED SYSTEM RUNNING HIGHER TEMP THAN NR 1 SYSTEM, ACCOMPLISHED DECAY CHECK USING ENG, DETERMINED NO LEAKS IN MANIFOLD. FOUND LEAK IN AC BAY 3 AT THE TRIM AIR PRESSURE REGULATOR VALVE ROTATED CLAMP AND REPLACED FILTER SEAL LEAK CHECKS GOOD NOW, REPLACED SENSE LOOP IN THE AC BAY AS A PRECAUTION ALL WORK DONE IAW SMP. RAN NR 3 ENG AND PERFORMED NR 3 PNEUMATIC SYS TEST IAW JRH 7-3. ALL CHECKS NORMAL. OK FOR SERVICE. 2L73 4F A22WE 20050520000662005052000066NM 2005 5 20 05FDEA01257 120050512A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 FWD CARGO BAY IS CREASED BS 580 STR 24L - 25L. FOUND LEAK IN AC BAY 3 AT THE TRIM AIR PRESSURE REGULATOR VALVE ROTATED CLAMP AND REPLACED FILTER SEAL LEAK CHECKS GOOD NOW, REPLACED SENSE LOOP IN THE AC BAY AS A PRECAUTION ALL WORK DONE IAW SMP. RAN NR 3 ENGINE AND PERFORMED NR 3 PNEUMATIC SYSTEM TEST IAW JRH 7-3. ALL CHECKS NORMAL. OK FOR SERVICE. 2L73 4F RTA3WE 20050520000672005052000067NM 2005 5 20 05FDEA01258 120050512A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 FWD CARGO BAY FRAME IS CREASED AT BS 580 STR 25L. REPAIRED FRAME PER SRM 51-40-3 2L73 4F RTA3WE 20050520000712005052000071WP 2005 5 20 ARWA2005050A 120050517A3230ARG7126501 TARGET DOUG DC10 DC1010 3022110WP MLG DOOR OUT OF ADJUST A ARWAO OTHER J WARNING INDICATION CLCLIMB 1 SO1968041 46900 AFTER GEAR RETRACTION LEFT GEAR; LIGHT REMAINED ILLUMINATED; PERFORMED CHECK LIST, NO HELP, OBSERVED SPEED LIMITS (GEAR). PERFORMED T/S FOUND TARGET SWITCH BROKEN. REMOVED AND REPLACED TARGET BRACKET IN ACCORDANCE WITH M/M 32-14-01. PERFORMED MAIN LANDING GEAR EXTENSION AND RETRACTION, FOUND NORMAL IN ACCORDANCE WITH M/M 32-30-0. 2L73 4F A22WE 20050520000732005052000073NM 2005 5 20 05FDEA00924 120050410A5510 STRUCTURE DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE LT HORIZONTAL STABILIZER UPPER BARREL NUT NR 4 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133. 2L73 4F RTA22WE 20050520000752005052000075NM 2005 5 20 05FDEA00927 120050411A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE LT HORIZONTAL STABILIZER UPPER BARREL NUT NR 18 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133. 2L73 4F RTA22WE 20050520000782005052000078NM 2005 5 20 05FDEA00930 120050411A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE RT HORIZONTAL STABILIZER UPPER BARREL NUT NR 35 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133. 2L73 4F RTA22WE 20050520000802005052000080NM 2005 5 20 05FDEA00933 120050411A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE RT HORIZONTAL STABILIZER UPPER BARREL NUT NR 29 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133. 2L73 4F RTA22WE 20050520000822005052000082NM 2005 5 20 05FDEA00935 120050411A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE LT HORIZONTAL STABILIZER UPPER BARRREL NUT NR 34 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133. 2L73 4F RTA22WE 20050607001502005060700150EA 2005 6 7 QXEA200500934 120050506A7830 TORQUE BOX CNDAIRCL600 CL6002C10 1390015EA ZONE 400 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - RIGHT ENGINE UPPER AND LOWER TORQUE BOX STRUCTURE HAS DAMAGE AT INBOARD FRAMES FROM TRANS COWL CONTACT. REPAIRED IAW REO 670-78-34-375 AND HORIZON AIR EA R-78-48. 2L72 4F RTA21EA 20050520000862005052000086NM 2005 5 20 05FDEA00997 120050413A5753 HINGE DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE LT WING O/B FLAP O/B REAR SPAR MOUNTED HINGE ACTUATOR HOLE EVIDENT OF CORROSION. LT WING O/B FLAP O/B REAR SPAR MOUNTED HINGE ACTUATOR CORROSION REMOVED & FOUND I/B & O/B LUG HOLES EXCEED LIMITS AS PER CMM 57-44-09 .I/B & O/B LUG SPOTFACES THK W/I LIMITS AS PER CMM 57-44-09 . I/B LUG ORG DIA 1.220 FINAL DIA 1.224 O/B LUG ORG DIA 1.192 FINAL DIA 1.193. I/B LUG ORG THK 0.346 REMAIN THK 0.344 MATERIAL REMOVED 0.002. O/B LUG ORG THK 0.360 REMAIN THK 0.358 MATERIAL REMOVED 0.002. FABRICATED BUSHING AND INSTALLED AS PER EA 1-5750-80379. (WINGS-TRAILING EDGE AND TRALING EDGE DEVICES -L/H O/B FLAP O/B HINGE BRACKET REPAIRS). MAJOR REPAIR AS PER 6-2-100. 2L73 4F RTA22WE 20050520000892005052000089NM 2005 5 20 05FDEA01038 120050417A5340 FLOOR SUPPORT DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE MAIN DECK, UPON REMOVAL OF FLOOR SUPPORT STRUCTURE, FLOOR SUPPORT STRUCTURE TO TEE CHORD AT STA 2007 RBL 60 INCH FOUND WITH CORROSION. CORROSION ON TEE CHORD AT STA 2007 RBL 60 REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-40-00 FIG. 7 VOL I. DISCREPANT TEE CHORD REMOVED AS PER SRM 51-31-01 VOL II. NEW TEE CHORD REWORKED FROM S2924410 AS PER DRAWING NJC6040.HOLES PICK-OUT ON NEW TEE CHORDS AS AS PER SRM 51-31-01 VOL II AND REPROTECTED AS PER SRM 51-21-01 VOL II. NEW TEE CHORD PAINTED AS PER SRM 51-21-01 VOL II AND PART MARKED AS PER GMM 7-0-1001 FX NJC6040-175. MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050523000012005052300001NM 2005 5 23 05FDEA01042 120050418A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE RT HORIZONTAL STABILIZER UPPER BARREL NUT NR 34 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133. 2L73 4F RTA22WE 20050523000032005052300003NM 2005 5 23 05FDEA01061 120050422A5340 ATTACH FITTING DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE MAIN DECK, AT STATION 510 LONGERON 27L FRAME TO FLOORBEAM INTERSECTION FOUND WITH 1 INCH CRACK. CARRIED OUT REPAIR AS PER EA 1-5310-80388. 2L73 4F RTA22WE 20050523000042005052300004NM 2005 5 23 05FDEA01145 120050427A5320 FLOOR SUPPORT DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE CABIN, FLOOR SUPPORT AT STA 1911 LBL 22 TO 28 FOUND VARIOUS PLACES OF CORROSION AS MARKED. CORROSION ON FLOOR SUPPORT AT STA 1911 RBL 22 TO LBL 28. REMOVED & FOUND EXCEED LIMIT AS PER SRM 53-00-01 FIG. 4 VOL I. DISCREPANT FLOOR SUPPORT FROM STA 1887 TO 2007 RBL 22 TO LBL 28 REMOVED AS PER SRM 51-31-01 VOL II. NEW FLOOR SUPPORT REWORKED FROM S3932107-7075T6511 AS PER DRAWING AGA 7497 AND HOLES PICK UP AS PER SRM 51-31-01 VOL II. NEW FLOOR SUPPORT REPROTECTED AND PART MARKED FX AGA 7497-503 AS PER GMM 7-0-1001. NEW FLOOR SUPPORT LOCATED AND INSTALLED FROM STA 1887 TO 2007 LBL 22 TO 28 AS PER SRM 51-31-01VOL II. MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050523000052005052300005NM 2005 5 23 05FDEA01146 120050427A5320 FLOOR SUPPORT DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE CABIN, FLOOR SUPPORT FOUND CORROSION AT VARIOUS PLACES FROM STA 1911 TO 2007 RBL19 AS MARKED. CORROSION ON FLOOR SUPPORT AT STA 1911 TO 2007 RBL 19 REMOVED & FOUND EXCEED LIMIT AS PER SRM 53-00-01 FIG. 4 VOL I. DISCREPANT FLOOR SUPPORT REMOVED AT STA 1887 TO 2007 RBL 19 AS PER SRM 51-31-01 VOL II. NEW FLOOR SUPPORT REWORKED FROM S2929169X-7075T6511 AS PER DWG AGA 7498 & HOLES PICK UP AS PER SRM 51-31-01 VOL II. NEW FLOOR SUPPORT REPORTED AS PER SRM 51-21-01 VOL II & PART MARK FX AGA 7498-501 AS PER GMM 7-0-1001. NEW FLOOR SUPPORT LOCATED & INSTALLED FROM STA 1887 TO 2007 RBL 19 AS PER SRM 51-31-01 VOL II. MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050523000062005052300006NM 2005 5 23 05FDEA01147 120050427A5320 FLOOR SUPPORT DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE CABIN, LONGITUDINAL FLOOR SUPPORT FOUND CORROSION AT STA 1888 TO 1913.5 RBL 22 AS MARKED. CORROSION ON FLOOR SUPPORT AT STA 1888 TO 1913.5 RBL 22 REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-00-01 FIG. 4 VOL I. DISCREPANT FLOOR SUPPORT FROM STA 1887 TO 2007 RBL 22 REMOVED AS PER SRM 51-31-01 VOL II. NEW FLOOR SUPPORT REWORKED FROM S3932107-7075T6511 AND HOLES PICK UP AS PER SRM 51-31-01 VOL II. NEW FLOOR SUPPORT REPROTECTED AS PER SRM 51-21-01 VOL II AND PART MARKED FX AGA 7497- 504 AS PER GMM 7-0-1001. NEW FLOOR SUPPORT LOCATED AND INSTALLED AT STA 1887 TO 2007 RBL 21 TO 26 AS PER SRM 51-31-01. MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050523000072005052300007NM 2005 5 23 05FDEA01148 120050427A5315 FLOORBEAM DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE CABIN, FLOOR SUPPORT FOUND CORROSION AT STA 1911 RBL 70 AND 75 AS MARKED. REMOVED AS PER SRM 51-31-01 VOL II. NEW FLOOR SUPPORT FABRICATED FROM S2929348 AS PER DRAWING AGA 7501 AND REPROTECTED AS PER SRM 51-21-01 VOL II. NEW FLOOR SUPPORT LOCATED AND INSTALLED AT STA 1911 RBL 58-84 AS PER SRM 51-31-01 VOL II.CLASSIFIED MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050523000092005052300009NM 2005 5 23 05FDEA01150 120050427A5320 FLOOR SUPPORT DOUG MD11 MD11 3023602NM FUSLEAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE CABIN, FLOOR SUPPORT FOUND VARIOUS PLACES CORROSION AT STA 1959 TO 2007 AND RBL 56 TO 59 AS MARKED. REMOVED & FOUND EXCEED LIMIT AS PER SRM 53-00-01 FIG. 4 VOL I. DISCREPANT FLOOR SUPPORT AT STA 1887 TO 2007 RBL 56 REMOVED AS PER SRM 51-31-01 VOL II. NEW FLOOR SUPPORT REWORKED FROM S3932107-7075T6511 AS PER DRAWING AGA 7496 . HOLES PICK-UP AS PER SRM 51-31-01 VOL II. NEW FLOOR SUPPORT REPROTECTED AS PER SRM 51-21-01 VOL II AND PART MARK FX AGA 7496-502 AS PER GMM 7-0-1001. NEW FLOOR SUPPORT LOCATED AND INSTALLED AS PER SRM 51-31-01 VOL II. MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050523000102005052300010NM 2005 5 23 05FDEA01151 120050427A5320 FLOOR SUPPORT DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE AFT CARGO CEILING AREA HAS CORROSION ON CABIN FLOOR SUPPORTS AT STA 1887 X=58. REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-00-01 FIG. 4 VOL I. DISCREPANT FLOOR SUPPORT AT STA 1887 TO 2007 X=58 REMOVED AS PER SRM 51-31-01 VOL II. NEW FLOOR SUPPORT REWORKED FROM S3932107-7075T6511 AS PER DRAWING AGA 7496 AND HOLES PICK UP AS PER SRM 51-31-01 VOL II. NEW FLOOR REPROTECTED AS PER SRM 51-21-01 VOL II AND PART MARKED FX AGA7496-501 AS PER GMM 7-0-1001. NEW FLOOR SUPPORT LOCATED AND INSTALLED AT STA 1887 TO 2007 X=58 AS PER SRM 51-31-01 VOL II.MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050523000112005052300011NM 2005 5 23 05FDEA01156 120050427A5347 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE CABIN, CURVE SEAT TRACK AT STA 1951 TO 1971 LBL 77 FOUND PREVIOUS REPAIRED AREA NON-STANDARD AS MARKED. SEAT TRACK TRIM OUT AS PER SRM 53-70-00 FIG 1 VOL I . NEW SEAT TRACK REMOVED AS PER SRM 53-70-00 FIG 7 VOL I. SPLICE ANGLE REWORKED AND SPLICE PLATE FABRICATED AS PER SRM 53-70-00 FIG 1 VOL I. 2L73 4F RTA22WE 20050518000972005051800097EA 2005 5 18 SWIA200514921 120050422A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY MALFUNCTIONED A SWIAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NRNOT REPORTED 1 NM07699BR 7801 CARGO SMOKE WARNING MSG FOR 5 SECS THEN EXTINGUISHED. REPLACED AFT CARGO SMOKE DETECTOR. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050518000992005051800099SO 2005 5 18 SWIA200514923 120050422A275012064207615 SELECTOR EMB 120 EMB120ER 3260203SO TE FLAP MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CRCRUISE 1 NM07561SW4105 4105 120335 WHILE ENROUTE AT FL240, RECEIVED SEVERAL CONTROL FAULT WARNINGS ACCOMPANIED BY "AWS" AND FLAP WARNINGS ON MAP. REPLACED FLAP SELECTOR LEVER. CLEARED ALL FAULTS FROM FCU. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050518001012005051800101EA 2005 5 18 SWIA200514925 120050419A3397 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT CONTAMINATED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07463SW 7820 FRONT SECTION OF EMERGENCY LIGHTING SYSTEM INOPERATIVE. CLEANED FORWARD EMERGENCY LIGHT STRIP CONNECTIONS OF WATER. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050518001022005051800102EA 2005 5 18 SWIA200514926 120050418A2751 DETECTOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07442SW 7609 "FLAPS DEGRADED" STATUS MESSAGE. REPLACED SKEW DETECTOR UNIT. OPERATIONAL CHECK GOOD IAW CRJ 200 MM 27-51-15. 2L72 4F RTA21EA 20050518001032005051800103EA 2005 5 18 SWIA200514927 120050420A274170609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07449SW2494 2494 7699 STAB CHANNEL 1 FAILED INFLIGHT. REPLACED HSTCU. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050518001052005051800105 2005 5 18 ANCF200400049 420050426A344220412170415 TRANSCEIVER BOEING757 75728A 1384976NM WX RADAR SYS UNKNOWN W ANCFO OTHER O OTHER CRCRUISE 1 SO23767AN211021374 23767 WXR FAIL DISPLAYED ON HSI AND WXR TEST DISPLAYS WRX FAIL RT. WITH AMM 34-43-01 PAGE 401 WAS REPLACED TRANSCEIVER ALSO WAS CLEANED THE FILTER OF TRANSCEIVER RADAR COOLING. 2L72 4F RTA2NM 20050518001062005051800106SO 2005 5 18 647041805 120050418A27401159SCC5053 DRIVE ASSY GULSTMGV GULFSTREAMGV3980116SO TE FLAP MALFUNCTIONED E N93AO OTHER O OTHER DEDESCENT 1 SO13511QS3593 647 DURING DESCENT FLAP/STAB MESSAGES ILLUMINATED ON THE CAS SYSTEM. 2L72 4F RTA12EA 20050518001072005051800107 2005 5 18 SWAA051192 420050422A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29617SW 27700 L1 DOOR EVACUATION SLIDE FELL OUT OF CONTAINER (DID NOT DEPLOYED). REINSTALLED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20050518001082005051800108NM 2005 5 18 SWAA051193 120050421A3220654623010 DRAG BRACE BOEING737 7373H4 1384600NM NLG WORN A SWAAO OTHER O OTHER NRNOT REPORTED 1 SW29615SW 27698 VIBRATION FELT AT NLG. REMOVED & REPLACED NLG LOWER DRAG BRACE ASSY PER MM DUE TO WORN BEARING. 2L72 4F RTA16WE 20050518001092005051800109 2005 5 18 SWAA051194 420050423A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29612SW 27930 R1 DOOR EVACUATION SLIDE PRESS IND OUT OF VIEW. ADJUSTED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20050518001102005051800110NM 2005 5 18 SWAA051195 120050423A2560P2070001 FLASHLIGHT BOEING737 7373A4 1384585NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29680AA 23505 DURING SCHEDULED RON, FOUND FWD OUTBOARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT ASSY PER MM. 2L72 4F RTA16WE 20050518001112005051800111NM 2005 5 18 SWAA051196 120050423A3350 LAMP BOEING737 7373Y0 1384671NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED A2 CHECK, FOUND R1 DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED PER MM. 2L72 4F RTA16WE 20050518001132005051800113NM 2005 5 18 SWAA051199 120050423A3350D71701100 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29740SW 29276 DURING SCHEDULED RON FOUND BOTH LT & RT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050518001152005051800115NM 2005 5 18 SWAA051201 120050423A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29326SW 23690 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT EXTERNAL A/C RECEPTICLE CUTOUT, BS 520. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050518001172005051800117NM 2005 5 18 SWAA051203 120050423A53306552988 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29326SW 23690 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 913, STR 25L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050519000062005051900006NM 2005 5 19 P5CA0501346 120050427A3150740019 WARNING SYSTEM BOEING747 747123 1384873NM COCKPIT INOPERATIVE A P5CAK NONE P NO WARNING INDICATION ININSP/MAINT 1 EA15858FT 20109 ON PRE-FLIGHT, FOUND NO T/O WARNING ALTITUDE SELECT OR AUTOPILOT DISCONNECT WARNINGS. REPLACED AURAL WARNING DEVICE. OPS CHECK NORMAL IAW 31-26-02. 2L74 4F A20WE 20050519000072005051900007EA 2005 5 19 ASOA05309 120050326A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27709EV 10068 DURING HANGER MAINTENANCE, THE LT AND RT FS 280 LOWER WEB AT THE BULKHEAD WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE LT AND RT FS 280 LOWER WEB AT THE BULKHEAD IAW EO. (K) 2L72 4F4 FRTA21EA EOOO63EN 20050519000112005051900011NM 2005 5 19 SWAA051246 120050427A57126545445 RIB BOEING737 7375H4 138449DNM LT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29509SW 24186 DURING SCHEDULED 1/2D CHECK, FOUND LT WING RIB LOWER CHORD CRACKED AT WBL 135.5, BETWEEN STR 2 & STR 3. REPAIRED RIB PER SWA ACO. 2L72 4F RTA16WE 20050519000252005051900025NM 2005 5 19 SWAA051260 120050427A53306546881 SKIN BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON FUSELAGE SKIN LAP JOINT AT BS 1016 TO BS 1088, STR 24R. REPAIRED SKIN PER BFG ER. 2L72 4F RTA16WE 20050519000312005051900031NM 2005 5 19 SWAA051266 120050427A53116546572 FRAME BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON FUSELAGE LOWER FRAME AT BS 1088, FROM LBL 13 TO RBL 15. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20050519000372005051900037NM 2005 5 19 SWAA051225 120050426A53306545769 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29374SW 26582 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT EQUIPMENT COOLING EXHAUST AFT CUTOUT. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050519000392005051900039NM 2005 5 19 SWAA051227 120050426A57126545445 RIB BOEING737 7375H4 138449DNM RT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29509SW 24186 DURING SCHEDULED 1/2D CHECK, FOUND RT WING RIB LOWER CHORD CRACKED AT WBL 135.5, BETWEEN STR 2 & STR 3. REPAIRED RIB PER SWA ACO. 2L72 4F RTA16WE 20050519000412005051900041NM 2005 5 19 SWAA051229 120050426A53306545767 SKIN BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN LAP JOINT CORRODED AT BS 360 TO 500C, STR 19R. REPAIRED SKIN PER BFG ER. 2L72 4F RTA16WE 20050519000432005051900043NM 2005 5 19 SWAA051231 120050426A53306545768 SKIN BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN LAP JOINT CORRODED AT BS 259 TO BS 360, STR 24R. REPAIRED SKIN PER BFG ER. 2L72 4F RTA16WE 20050519000572005051900057 2005 5 19 SWAA051245 420050426A256565C16820 HOOK BOEING737 7377H4 1384404NM L1 DOOR SLIDE LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29792SW 27887 DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER MM. 2L72 4F RTA16WE 20050519000612005051900061 2005 5 19 SWAA051211 420050425A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29374SW 26582 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050519000622005051900062NM 2005 5 19 SWAA051212 120050425A524065C36231 SKIN BOEING737 7373H4 1384600NM R1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29374SW 26582 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR SKIN CRACKED AT AFT UPPER FASTENER HOLE. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050519000682005051900068NM 2005 5 19 SWAA051218 120050425A53306545775 SKIN BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CORRODED BETWEEN BS 727C TO BS 907, STR 25L. REPAIRED SKIN PER PAE ER. 2L72 4F RTA16WE 20050519000822005051900082EA 2005 5 19 ASOA05303 120050327A3260 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NLG ILLUMINATED A ASOAO OTHER J WARNING INDICATION APAPPROACH 1 SO27856AS 7404 DURING APPROACH, UPON SELECTING THE GEAR DOWN AND FLAPS TO 30 DEGREES, THE CREW RECEIVED A GREEN GEAR DOWN INDICATION FOR THE MLG FOLLOWED BY A NOSE GEAR DISAGREE WARNING MESSAGE ON EICAS. AT APPROX 1,000 FT, THE CREW INITIATED A GO AROUND AND DECLARED AN EMERGENCY. UPON COMPLIANCE WITH THE QRH, 3 GREEN INDICATION FOR THE LANDING GEAR WERE RECEIVED AND THE AIRCRAFT THEN LANDED SAFELY. MAINT TESTED AND INSPECTED THE NLG EXTENSION SYSTEM AND CYCLED NLG NUMEROUS TIMES IAW MM AND COULD NOT DUPLICATE THE DISCREPANCY. NO DEFECTS WERE NOTED. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050519000892005051900089 2005 5 19 05FDEA01171 420050428A2210 COMPUTER DOUG MD11 MD11 3023602NM FCC MALFUNCTIONED A FDEAA UNSCHED LANDING O OTHER CLCLIMB 1 SO25601FE 48401 ON DEPARTURE FROM MEM NEVER GOT AUTOPILOT ON, OR AUTOTHROTLES ON. HAD TO FLY BELOW RVSM DUE TO NO AUTOPILOT. PERFORMED DETAILED AFS SYSTEM CHECK, ALL TESTS PASSED, CHECKED FCC NR 1 AND FCC NR 2 PROFORMED AUTO FLIGHT SYSTEM TEST. REF MD-11 M/M 22-01-10-5. ALL TEST PASSED. A/C OK FOR SERVICE. A/C CAT STATUS DOWN GRADED TO NOT CAT II A/P NR 1 AND NR 2 ARE CHECK CAT II. REMOVED AND REPLACED GLARESHIELD CONTROL PANEL PRECAUTIONARY. REF MD-11 M/M 22-00-04-5. OPS CHECK NORMAL. OK FOR SERVICE. 2L73 4F RTA22WE 20050519000972005051900097NM 2005 5 19 DHL2005783514 120050419A5313 SKIN BOEING727 727227 1384078NM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01783DH 21999 LT FUSELAGE SKIN HAS 2EA CREASES AFT OF BS 1130 ABOVE STR 26L (BELOW PREV REPAIR). REMOVED PREV REPAIR BS 1130 ABOVE STR26L IAW B727 SRM 51-30-2, DAMAGED FOUND TO OUT OF LIMITS IAW B727 SRM. REPAIRED IAW SRM. 2L73 4F A3WE 20050519000992005051900099EU 2005 5 19 05FDEA01174 120050429A5415 ATTACH BRACKET AIRBUSA300 A300F4622R 3930360EU NR 2 PYLON CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25662FE 761 NR 2 PYLON O/B SIDE RIB 9 PRECOOLER COMPT 1 EA ATTACH BRACKET CRACKED REF N00532. REMOVED AND REPLACED FITTING RT IAW SRM 51-72-10. 2L72 4F RTA35EU 20050519001002005051900100EU 2005 5 19 05FDEA01175 120050429A5415 FITTING AIRBUS300 A300B4605R 3930308EU NR 2 NACELLE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25662FE 761 NR 2 ENG FWD MOUNT FITTING HAS 2 EA BOLTS MOUNT HOLES AND 1EA SPIGOT HOLE CORRODED REF N00630. REMOVED AND REPLACED SPIGOT FITTING IAW SRM 51-72-10. 2L72 4F RTA35EU 20050519001032005051900103SO 2005 5 19 C2XA05IA060 120050425A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714993 145289 DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHT AT THE MAIN CABIN DOOR WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050519001052005051900105EU 2005 5 19 ASOA05301 120050310A5311 FRAME AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27635AS 372 DURING A C-CHECK, THE FAIL SAFE FRAME SEGMENT IN THE AFT AVIONICS COMPARTMENT AT FR46, STRINGER 19L AND 19R WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FAIL SAFE FRAME SEGMENT IN THE AFT AVIONICS COMPARTMENT AT FR 46, STRINGER 19L AND L19R IAW SRM. (K) 2H72 4T4 TRTA53EU E20NE 20050519001122005051900112EA 2005 5 19 ASOA05295 120050403A5310 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE ENGINE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27862AS 7476 DURING C-CHECK, THE ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL0 WAS FOUND TO BE CRACKED BEYOND LIMIST. MAINTENANCE IS REPAIRING THE ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL0 IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050519001142005051900114EA 2005 5 19 ASOA05294 120050402A3350BR9279106 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE GALLEY CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27862AS 7476 DURING A C-CHECK, THE EMERGENCY EXIT LIGHT BY THE SERVICE DOOR WAS FOUND TO BE CRACKED AND INOPERATIVE. MAINTENANCE IS REMOVING AND REPLACING THE EMERGENCY EXIT LIGHT ASSY BY THE SERVICE DOOR. (K) 2L72 4F4 FRTA21EA E15NE 20050519001212005051900121CE 2005 5 19 FFS2005F00001 120050412A561010138402521 WINDSHIELD BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA HARTZLHCB4M HCB4MP3 GL COCKPIT DELAMINATED A FFSAK NONE O OTHER ININSP/MAINT 1 AL01575Y UC162 PILOTS WINDSHIELD WAS REPLACED DUE TO ADHESION CHIPS PULLED FROM OB SURFACE OF THE INNER PLY. WINDSHIELD HAD EXPERIENCED SOME PROGRESSIVE DELAMINATION FROM THE RT EDGE. (AL01200503512) (K) 2L72 4T4 TRTA24CE E4EA 6 CP56GL 20050519001232005051900123CE 2005 5 19 TIM2005F00002 120050404A5330 SKIN BEECH 1900 1900 1154160CE CORRODED E TIMAK NONE O OTHER ININSP/MAINT 1 NM07127BA UB7 CORROSION FOUND ON SKIN FS243-FS273 AND STRINGERS 14L-15R. (K) 2L72 4T RTA24CE 20050519001242005051900124WP 2005 5 19 ABXA050102 120050414A5313591141277 LONGERON DOUG DC9 DC932F 3022067WP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23905AX 47147 SKIN BULGING, RIVETS CUPPED AT STA 342, LONGERON 29 RIGHT AND LONGERON 28 RIGHT. REMOVED FASTENERS, EVALUATED. SPLICED LONGERON IAW DC-9 SRM. 2L72 4F A6WE 20050519001402005051900140EU 2005 5 19 AWXA200500519 120050404A5347D57130147200 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28638AW 455 SAL - MAJOR REPAIR - DURING C-08 CHECK, EXFOLIATION CORROSION WAS FOUND ON RT INBOARD SEAT TRACK -Y765 AT FR 36+17". MAINTENANCE REMOVED CORRODED SECTION OF RT INBOARD SEAT TRACK -Y765 AT FR 36+17"; RECEIVED AND INSTALLED A NEW REPLACEMENT SEAT TRACK IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050519001462005051900146EA 2005 5 19 QXEA200500829 120050411A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 200 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - FUSELAGE EXTERIOR AT STATION 310 AND STRINGER 11R HAS TWO NICKS AT FASTENERS. REPAIRED IAW CRJ700 REO 670-53-00-045 AND SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050519001632005051900163EA 2005 5 19 QXEA200500818 120050415A7830 COWLING CNDAIRCL600 CL6002C10 1390015EA THRUST REVERSER CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - RIGHT ENGINE, UPPER COWLING AREA, TRANSCOWL ASSEMBLY, FOUR EACH RETAINERS ARE CHAFING ON THE TORQUE BOX ASSEMBLY. REPAIRED IAW HORIZON AIR EA R-78-42 AND REO 670-78-34-361. 2L72 4F RTA21EA 20050519001662005051900166EA 2005 5 19 QXEA200500791 120050413A5753 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 600 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - RIGHT INBOARD FLAP LOWER SKIN HAS GRAVEL DAMAGE. REPAIRED IAW CRJ700 SRM 51-26-00-001-001-A01 AND SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050519001682005051900168EA 2005 5 19 QXEA200500792 120050413A5315 FLOORBEAM CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - FUSELAGE INTERIOR, FUSELAGE STATION 280 FLOOR SUPPORT CROSSBEAM IS CORRODED ON TOP FLANGE FROM LBL30 TO RBL30. REPAIRED IAW REO 670-53-11-047. 2L72 4F RTA21EA 20050519001752005051900175EA 2005 5 19 QXEA200500795 120050413A5320 FLOOR SUPPORT CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - FUSELAGE INTERIOR, COCKPIT FLOOR PANEL SUPPORT ANGLE IS CORRODED. REPLACED IAW CRJ700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20050607000252005060700025NM 2005 6 7 DHL2005740532 120050327A5347 SEAT TRACK BOEING727 7272Q9 138448MNM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 MAIN CABIN SEAT TRACK BS 760 - BS 870 LBL 45.5 CORROSION AND DAMAGED. REMOVED AND REPLACED SEAT TRACK FROM P/N BAC1520-841 PO NR 9001650 DIM 8 FT IAW B727 SRM 53-10-2 FIG 1 AND 53-10-5 FIG 2. TREATED AND PRIMED SEAT TRACK IAW B727 SRM 51-10-2. 2L73 4F RTA3WE 20050520000142005052000014 2005 5 20 2005UALA00385 420050420A2565D17906111 RESERVOIR AIRCRUISERS D31038201 BOEING757 757222 1384956NM PWA 2037 PW2037 NE SLIDE LOW A UALAK NONE O OTHER ININSP/MAINT 1 WP29568UA 0696 26674 FILL ON LOW SIDE OF GREEN BAND WITHIN MANUAL TOLERANCE. SLIDE WAS REMOVED FROM AIRCRAFT DUE TO LOW INFLATION CYLINDER PRESSURE. WHEN RECEIVED AT COMPONENT SHOP, PRESSURE INDICATOR NEEDLE WAS REPORTED TO STILL BE WITHIN THE GREEN 'GO' BAND. RESERVOIR PRESSURE WAS TOPPED-OFF AND NO LEAKS WERE DETECTED. 2L72 4F4 FRTA2NM E17NE 20050520000332005052000033NM 2005 5 20 SWAA051198 120050422A335065C27093 LIGHT BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29656SW 28401 DURING SCHEDULED C1 CHECK, FOUND COCKPIT DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY EXIT LIGHT PER MM. 2L72 4F RTA16WE 20050520000352005052000035 2005 5 20 SWAA051205 420050424A2565416A2200 SLIDE BOEING737 7377H4 1384404NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29764SW 27878 L1 DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20050520000412005052000041NM 2005 5 20 2005UALA00393 120050423A5312 PRESSURE PANEL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE RT MLG WW CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29311UA 23672 RT WW FWD BULKHEAD STA 663 HAS THE VERTICAL WEB AT LBL 6.15 CRACKED. VERTICAL WEB CRACKS CAUSED BY FATIGUE. REPLACED STIFFENERS AT LBL 6.15 AND RBL 6.15. 2L72 4F4 FRTA16WE E2GL 20050520000572005052000057CE 2005 5 20 DJFA2005091 120050508A2910 B-NUT CESSNA650 650 2076802CE HYD SYSTEM LEAKING E DJFAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA23381CW 6500111 CREW REPORTED THAT WHILE IN CRUISE FLIGHT THE LT AND RT HYDRAULIC LOW PRESSURE LIGHTS HAD ILLUMINATED ALONG WITH THE SPOILER HOLD, AILERON BOOST, AND AUXILLARY HYDRAULIC PUMP LIGHTS. THE HYDRAULIC FLUID VOLUME REMAINED STEADY. CREW DECLARED AN EMERGENCY AND DIVERTED TO KAPA. THE LANDING GEAR WAS MANUALLY EXTENDED, AND THE SPEED BRAKES, SPOILERS, THRUST REVERSERS, AND STEERING WERE INOPERATIVE WHEN AIRCRAFT LANDED IN KAPA. MAINTENANCE RAN THE AIRCRAFT SEVERAL TIMES AND ALL SYSTEMS CHECKED NORMALLY. A LEAK WAS DISCOVERED AT A B-NUT FOR THE OUTBOARD LEFT ROLL SPOILER. B-NUT WAS TIGHTENED AND LEAK CHECK WAS GOOD. NO FURTHER DISCREPANCIES WERE NOTED. AS A PRECAUTIONARY MEASURE, TWO UNLOADING VALVES, PART NUMBE2L72 4F A9NM 20050520000582005052000058NM 2005 5 20 0500676623 120050506A3320 BALLAST BOEING747 747251B 1384892NM CABIN BURNED A NWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL01623US 21705 WHILE INBOUND TO HNL, FLIGHT ATTENDANT REPORTED SPARKS AND BURNING SMELL IN NR 2 MID GALLEY. NR 3 GALLEY POWER TRIP LIGHT WAS ILLUMINATED. DID NOT RESET, BURNING SMELL DISSIPATED. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. HNL MAINTENANCE FOUND WIRES CHAFED BEHIND OVEN. COVERED WIRES AND UNPLUGGED OVEN AND DEFERRED LOG. ALSO FOUND LIGHT AT 13HJK INOPERATIVE AND BALLAST BURNT. REMOVED BALLAST AND DEFERRED LOG. NRT MAINTENANCE REPAIRED WIRES AND REPLACED BALLAST 07MAY05. OPERATIONAL CHECK GOOD. 2L74 4F A20WE 20050520000602005052000060CE 2005 5 20 70786 120050510A326090422912 ANNUNCIATOR BEECH 1900 1900D 1154162CE COCKPIT INOPERATIVE A AMWAO OTHER P NO WARNING INDICATION DEDESCENT 1 CE07144ZV UE144 NLG WILL NOT INDICATE DOWN AND LOCKED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE DETERMINED THE PROBLEM IS IN THE ANNUNCIATOR ASSEMBLY. MAINTENANCE REMOVED AND REPLACED THE ANNUNCIATOR. 2L72 4T RTA24CE 20050520000682005052000068NM 2005 5 20 UPS05244442 120050512A3510358151OV OXYGEN MASK BOEING727 727108C 1384039NM COCKPIT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 CREW PREFLIGHT - F/O O2 MASK WOULD NOT TRANSMIT. REMOVED AND REPLACED F/O'S 02 MASK ASSY. OPS CKS GOOD IAW MM 35-11-00. 2L73 4F A3WE 20050520000692005052000069WP 2005 5 20 05FDEA01341 120050517A5522 SKIN DOUG DC10 DC1010 3022110WP ELEVATOR DENTED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25571FE 47830 HORIZONTAL STABILIZER, RT, UPPER SIDE, THE ELEVATOR HAVE SEVERAL DENTS, IN ADDED, 2EA REPAIRS WITH CHERRYMAX. REMOVED EXISTING REPAIR AT ELEVATOR, STA XE206, AND INSTALLED BIGGER REPAIR COVERING DENT LOCATED AT STA XE200 IAW SRM 55-10-00, FIG 8. 2L73 4F A22WE 20050520000702005052000070NM 2005 5 20 BB05038 120050514A33501010425 LIGHT BOEING757 757225 1384959NM ROW 12 INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19604AU 22199 TPA - FOUND EMERGENCY LIGHT AT ROW 12 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. 2L72 4F RTA2NM 20050520000762005052000076NM 2005 5 20 05FDEA00928 120050411A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE LT HORIZONTAL STABILIZER UPPER BARREL NUT NR 20 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133. 2L73 4F RTA22WE 20050520000832005052000083NM 2005 5 20 05FDEA00936 120050411A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE LT HORIZONTAL STABILIZER UPPER BARREL NUT NR 28 HAS BORE CORROSION EXCEEDING LIMIT. REPAIRED IAW EA 1-5510-78133. 2L73 4F RTA22WE 20050520000852005052000085NM 2005 5 20 05FDEA00938 120050411A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE LT HORIZONTAL STABILIZER UPPER BARREL NUT NR 32 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133. 2L73 4F RTA22WE 20050607000282005060700028NM 2005 6 7 DHL2005740536 120050328A5310 TORQUE BOX BOEING727 7272Q9 138448MNM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 RT LOWER TORQUE BOX CRACKED AT STA 1223. STOP DRILLED CRACK .250 TERMINATED AT END OF CRACK ON RT LOWER TORQUE BOX STA 1223 IAW B727 SRM 51-10-1, HFEC INSP PER NDT PT.6 51-00-00 FIG 23. CRACK ENDS IN STOP HOLE. FABRICATED DOUBLER REPAIR IAW B727 SRM 53-10-2 FIG 6 FROM 7075T6 .032 PO NR 900573 DIM 4 1/2"BY 3" IAW B727 SRM 51-40-2 FIG 1. ALODINED AND PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED DOUBLER REPAIR IAW B727 SRM 51-40-2 FIG 1. 2L73 4F RTA3WE 20050607000332005060700033NM 2005 6 7 DHL2005740542 120050329A5347BAC1520841 SEAT TRACK BOEING737 7372Q9 138448MNM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 MAIN CABIN SEAT TRACK BS 760 - BS 870 RBL 24.75 DAMAGED. REMOVED AND REPLACED SEAT TRACK BS 760 - 870 RBL 24.75 AND FABRICATED NEW SEAT TRACK P/N BAC1520-841 PO NR 9001690 DIM 4 FT AND P/N BAC1520-841 PO NR 9001474 DIM. 4 FT IAW B727 SRM 53-10-2 FIG 1 AND 53-10-5 FIG 2. TREATED AND PRIMED SEAT TRACK IAW B727 SRM 51-10-2. 2L72 4F A16WE 20050523000022005052300002NM 2005 5 23 05FDEA01057 120050421A5347 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE MAIN DECK, UPON REMOVAL OF FLOOR PANEL 291GF FOR SHEETMETAL ACCESS AT STA 1887 LBL 60 INCH SEAT TRACK FOUND CORRODED. CORROSION ON SEAT TRACK REMOVED & FOUND EXCEED LIMIT AS PER SRM 53-70-00 FIG 3 VOL I. SEAT TRACK REWORKED AS PER SRM 53-70-00 FIG.1 VOL I. 2L73 4F RTA22WE 20050519001022005051900102SO 2005 5 19 C2XA05IA054 120050418A3411CS500060D4A RELAY EMB 135 EMB135LR 3260305SO COCKPIT FAILED A C2XAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW2714514 145303 THE CREW REPORTED THAT THE NR 3 PITOT INOPERATIVE WHILE CLIMBING THROUGH CLOUDS, AND THE COCKPIT FILLED WITH SMOKE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE CURRENT SENSING RELAY (K0057) FOR THE NUMBER THREE PITOT PROBE, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. NOTE: THIS PART IS NOT SERIALIZED AND TIMES ARE NOT AVAILABLE. 2L72 4F RTT00011AT 20050519001092005051900109EA 2005 5 19 DJFA2005088 120050427A2751 WARNING LIGHT CNDAIRCL600 CL6002B16 1900305EA TE FLAPS ILLUMINATED E DJFAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA23902TA 5139 DURING TAKEOFF, AS FLAPS WERE BROUGHT UP TO 0 DEGREES AN AMBER FLAPS FAIL LIGHT ILLUMINATED. CREW REQUESTED EMERGENCY EQUIPMENT TO BE POSITIONED WHEN THEY RETURNED TO FIELD. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE POWERED UP ALL HYDRAULIC SYSTEMS, RAN THE ENGINES AND CYCLED ALL HYDRAULIC SYSTEMS. A SIMULATED AIR LOAD WAS APPLIED TO THE FLAPS DURING EXTENSION AND RETRACTION. THE AILERON AND SPOILER SYSTEMS WERE ALSO CYCLED. THE FLAP ROLLERS WERE LUBRICATED. NO FAULTS WERE FOUND. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20050519001612005051900161EA 2005 5 19 QXEA200500804 120050414A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 200 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - FUSELAGE UPPER SKIN AT STATION 300 AND STRINGER 0 HAS SCRATCHES UNDER TCAS ANTENNA. REPAIRED IAW CRJ700 SRM 51-12-00, SRM 51-21-11-001-001-A01, REO 670-53-21-099, HORIZON AIR EA R-53-314 2L72 4F RTA21EA 20050519001732005051900173EA 2005 5 19 QXEA200500801 120050412A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 200 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 YYC - FUSELAGE EXTERIOR SKIN AT STATION 1000, BETWEEN STRINGER 14L AND 15L HAS NICK ON SKIN. REPAIRED IAW HORIZON AIR EA R-53-306, REO 670-53-61-165 AND CRJ700 SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050519001962005051900196NM 2005 5 19 05FDEA01190 120050430A5315 FLOORBEAM DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 CABIN FLOORBEAM FOUND CORRODED AT STA 1873 LBL 10 TO 26 AS MARKED. REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-00-01 FIG. 4 VOL I. DISCREPANT FLOOR SUPPORT AT STA 1873 LBL 33 TO RBL 33 REMOVED AS PER SRM 51-31-01 VOL II. NEW FLOOR SUPPORT REWORKED FROM S2929348-12000 AS PER DWG AGA 7975 AND AND HOLES PICK UP AS PER SRM 51-31-01 VOL II. NEW FLOOR SUPPORT REPROTECTED AS PER SRM 51-21-01 VOL II AND PART MARKED FX AGA 7975-15 AS PER GMM 7-0-1001. NEW FLOOR SUPPORT LOCATED AND INSTALLED AT STA 1873 LBL 33TO RBL 33 AS PER SRM 51-31-01 VOL II. CLASSIFIED MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050520000222005052000022NM 2005 5 20 05FDEA01127 120050426A5347AEA75791 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA Y= 1199 TO Y= 1285, X= -47 CROWN ELONGATED AEA7579-1. REWORKED AND INSTALLED IAW SRM 53-70-00 VOLUME I, FIGURE 1. 2L73 4F RTA22WE 20050520000272005052000027NM 2005 5 20 05FDEA01135 120050426A5314 KEELBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25264FE 21626 CORROSION AT RT KEELBEAM OUTER FLANGE BS 950B+5 TO 950B+15. REPAIRED KEELBEAM IAW FED-EX SR DRAWING 27-53-023A 2L73 4F RTA3WE 20050520000282005052000028NM 2005 5 20 05FDEA01136 120050426A5314 KEELBEAM BOEING727 727200 138407ENM FUSLAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25264FE 21626 CORROSION ON LT KEELBEAM OUTER FLANGE BS 950A+4 TO 950A+12. INSTALLED REPAIR STRAP PER SR DRAWING 27-53-023A 2L73 4F RTA3WE 20050520000392005052000039NM 2005 5 20 2005UALA00390 120050423A5610 WINDOW BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE COCKPIT LEAKING A UALAA UNSCHED LANDING O OTHER CLCLIMB 1 WP29905UA 25005 FLIGHT RETURNED TO IAH DUE TO A FLIGHT DECK WINDOW AIR LEAK. F/O SLIDING WINDOW LEAKED, AFTER TAKEOFF. F/O SLIDING WINDOW HAD AN AIR LEAK. FOUND CLIP LODGED IN WINDOW FRAME. REMOVED AND INSPECTED AREA AND FOUND NO DAMAGES. SEAL INTACT AND AS PRECAUTIONARY, DID PRESSURIZATION TO VERIFY LEAK, NO LEAK FOUND. 2L72 4F4 FRTA16WE E2GL 20050520000422005052000042NM 2005 5 20 2005UALA00394 120050423A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29304UA 23665 FUSELAGE SKIN 4 O'CLOCK POSITION BS 178 IS PULLED AWAY FROM FRAME. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. 2L72 4F4 FRTA16WE E2GL 20050520000532005052000053 2005 5 20 SB05058 420050508A256565C1990115 CABLE BOEING737 737301 1384611NM R2 DOOR SLIDE INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19575US 2289 23740 PIT - THE R2 DOOR SLIDE LANYARD WOULD NOT RELEASE. MAINTENANCE REPLACED THE SLIDE. 2L72 4F RTA16WE 20050520000742005052000074NM 2005 5 20 05FDEA00925 120050410A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE LT HORIZONTAL STABILIZER UPPER BARREL NUT NR 16 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133. 2L73 4F RTA22WE 20050520000772005052000077NM 2005 5 20 05FDEA00929 120050411A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE LT HORIZONTAL STABILIZER UPPER BARREL NUT NR 24 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133. 2L73 4F RTA22WE 20050520000792005052000079NM 2005 5 20 05FDEA00932 120050411A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE RT HORIZONTAL STABILIZER UPPER BARREL NUT NR 31 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133. 2L73 4F RTA22WE 20050520000812005052000081NM 2005 5 20 05FDEA00934 120050411A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE RT HORIZONTAL STABILIZER UPPER BARREL NUT NR 27 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133. 2L73 4F RTA22WE 20050520000842005052000084NM 2005 5 20 05FDEA00937 120050411A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE LT HORIZONTAL STABILIZER UPPER BARREL NUT NR 30 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133. 2L73 4F RTA22WE 20050607000082005060700008EA 2005 6 7 QXEA200500868 120050509A5310 STRUCTURE CNDAIRCL600 CL6002C10 1390015EA ZONE 200 WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FUSELAGE INTERIOR, RIGHT OVERWING EMERGENCY EXIT SURROUND STRUCTURE STOP FITTING PADS ARE WORN. REPAIRED IAW CRJ-700 AMM 52-21-00-220-801-A01, REOI 670-52-21-003 AND HORIZON AIR EA R-52-251. 2L72 4F RTA21EA 20050520000872005052000087NM 2005 5 20 05FDEA01036 120050417A5311 DOOR FRAME DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE CAIN, DOOR 3R ABOVE UPPER DOOR JAMB STA 1263 LONGERON L-12 FOUND CORROSION AS MARKED. REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-00-01 FIG 1A VOL I. MATERIAL THICKNESS: 0.080, REMAIN THICKNESS: 0.049, REMOVED THICKESS: 0.031 FASTENER ON DISCREPANT AREA REMOVED AS PER SRM 51-32-01 VOL II. REPAIR ANGLE REWORKED FROM 1D0964T AS PER SRM 53-10-00 FIG 2A VOL I AND HOLES PICK-UP AS PER SRM 51-31-01 VOL II.REPAIR ANGLE LOCATED AND INSTALLED AS PER SRM 51-33-01 VOL II. CLASSIFIED MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050520000882005052000088NM 2005 5 20 05FDEA01037 120050417A5320 DOOR FRAME DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE SNRM N1749: CABIN, 3R ABOVE UPPER DOOR JAMB STA 1278 FOUND LONGERON L-14 CORROSION AS MARKED. 2L73 4F RTA22WE 20050523000122005052300012NM 2005 5 23 05FDEA01172 120050428A5753 RIB DOUG MD11 MD11 3023602NM RT WING TE FLAP DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE RT WING I/B FLAP ASSY FOUND NEW FLAP SEGMENT ASSY RIB DAMAGED. DAMAGED AREA TRIMMED. REPAIR DOUBLER & FILLER FABRICATED AND INSTALLED AS PER SRM 57-00-01 FIG. 7 VOL I AND 51-35- 01 VOL II. MINOR REPAIR PER GMM 6-2-100. 2L73 4F RTA22WE 20050523001352005052300135CE 2005 5 23 DXTA200500715 120050508A3260602751 PROXIMITY SWITCH CESSNA750 750 2076810CE MLG INOPERATIVE E DXTAO OTHER J WARNING INDICATION APAPPROACH 1 GL07904QS 7500210 LT GEAR UNSAFE ON EXTENSION, FOLLOWING PNEUMATIC AND MANUAL EXTENSION STILL UNSAFE. INTERMITTENT UNLOCK LIGHT. AFTER LANDING DURING TURN OFF OF RUNWAY, STEADY UNLOCK LIGHT AND GEAR HORN CAME ON SHUTDOWN IN PLACE. REMOVED & REPLACED L/H MAIN LANDING GEAR ACTUATOR DOWN LOCK MICRO SWITCH IAW CESSNA 750 MM 32-30-04. OPS CHECKS GOOD IAW CESSNA 750 MM TASK # 32-00-01-720 2L72 4J RTT00007WI 20050523001362005052300136NM 2005 5 23 DXTA200500719 120050512A5270 CONTACT AMD FALC50FALCON2000 2730170NM DOOR DIRTY E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07292QS 93 ON TAKEOFF ROLL, RED MASTER DOOR LIGHT CAME ON. ALL DOORS WERE CLOSED AND LOCKED. MEL'D IAW NETJETS FALCON MEL. ALL DOORS WERE OPEN & CLOSED, AND FOUND CONTACTS ON EMERGENCY EXIT DOOR TO BE DIRTY , CLEANED AND REINSTALLED DOOR AND OPS CHECK SYSTEM AND FOUND SYSTEM TO BE WORKING IAW FALCON 2000 52-700. 2K73 4F RTA50NM 20050523001412005052300141NM 2005 5 23 XNOA1233 120050501A7931 CONNECTOR BOEING727 727173C 1384059NM OIL SYSTEM DIRTY A XN0AD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL23704A 19504 NR 2 LOW OIL PRESSURE LIGHT ILLUMINATED DURING TAXI & WOULD NOT EXTINGUISH. CLEANED CONNECTOR ON NR 2 LOW OIL PRESSURE SWITCH, OPS CHECKED GOOD ON ENGINE RUN-UP IAW B727 MM 72-00. 2L73 4F A3WE 20050523001432005052300143SO 2005 5 23 C2XA05SD019 120050429A2560P2070011100 FLASHLIGHT EMB 145 EMB145XR 3260214SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2718114 145664 SDF - F/O'S EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT. OPS CHECK GOOD, AIRCRAFT RELEASED AND RETURNED TO SERVICE. 2L72 4F RT 20050523001442005052300144CE 2005 5 23 DXTA200500720 120050512A3210 LANDING GEAR CESSNA750 750 2076810CE MAINS DAMAGED E DXTAO OTHER E VIBRATION/BUFFET CLCLIMB 1 GL07936QS 7500036 NOSE GEAR MAKES A LOUD THUMP ON CLIMBOUT AND DESCENT WITH GEAR IN THE UP POSITION. 2L72 4J RTT00007WI 20050523001452005052300145CE 2005 5 23 DXTA200500716 120050511A2750MP50G4 PDU CESSNA750 750 2076810CE TE FLAPS INOPERATIVE E DXTAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 GL07901QS1738 7500102 FLAPS FAIL CAS ILLUMINATED ON APPROACH. SLATS EXTENDED AND FLAPS FAILED AT 5 DEGREES. REMOVED AND REPLACED FLAP PDU IAW 750 MM CHAPTER 27-52-00. OPS CHECK GOOD. 2L72 4J RTT00007WI 20050523001492005052300149SO 2005 5 23 C2XA05BT025 120050502A261147359713 SMOKE DETECTOR EMB 145 EMB145LR 3260212SO CARGO BAY MALFUNCTIONED A C2XAF ACTIVATE FIRE EXT. N FALSE WARNING UKUNKNOWN 1 SW2713997 145298 CREW REPORTED, BAGGAGE SMOKE WARNING, USED EXTINGUISHER BOTTLES. MAINTENANCE TROUBLESHOT SYSTEM REMOVED AND REPLACED FIRE EXTINGUISHER BOTTLES P/N 33700027-1, S/N 3454D1, BOTTLE P/N 34600073-1, S/N 18200F1 FOR BAGGAGE COMPARTMENT IAW EMB145 MM 26-23-01; REMOVED AND REPLACED FORWARD AND AFT SMOKE DETECTOR FOR BAGGAGE COMPARTMENT IAW EMB145 MM 26-15-01 P/N 473597-13, S/N'S 1511 AND 1662]; REMOVED AND REPLACED BAGGAGE COMPARTMENT FIRE DETECTION TEST SWITCH IN MAINTENANCE PANEL IAW EMB145 MM 20-30-00 P/N M83731/10-27. OPS CHECKED SYSTEM GOOD. 2L72 4T RTT00011AT 20050523001502005052300150NM 2005 5 23 2005UALA00388 120050423A2120 ODOR BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN DETECTED A UALAAH UNSCHED LANDING DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP29199UA 28717 CREW ODOR IN CABIN, NOTICED IN AFT CREW REST AREA, SULPHUR LIKE SMELL. CHILLERS SHUT OFF, RECIRCS SHUT OFF & PAX ENT SYSTEM SHUT OFF ODOR STILL EVIDENT. UTILITY BUSSES SHUT OFF AND ODOR STILL EVIDENT. FOUND OUTBOARD OVERHEAD ELECTRONIC UNIT 46HJK BURNED. UNIT WAS REPLACED, DATABASE LOADED AND CHECKED OK. FURTHER DISCUSSION WITH INTERIORS ENGINEERING INDICATES UNIT WAS SCRAPPED. UNIT HAD AN INTERNAL SWITCH THAT FAILED. THE SWITCHES NORMALLY FAIL IN THE CLOSED POSITION BUT THIS ONE HAD A RARE FAILURE IN AN OPEN (CONNECTED) POSITION WHICH ALLOWED IT TO OVERHEAT AND BURN OUT. DRH 2L74 4F4 FRTA20WE E24NE 20050523001512005052300151NM 2005 5 23 2005UALA00389 120050422A5312141T2920184 BULKHEAD BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29648UA56201 25285 NOSE WW BULKHEAD HAS DAMAGE. AUX NOSE JACK ACCIDENTALLY OVERLOADED. BOEING AOG TEAM PERFORMED PERMANENT STRUCTURE REPAIR TO STATION 287 BULKHEAD ASSY AND REPLACED DAMAGED SKIN PANEL. 2L72 4F4 FRTA1NM E24NE 20050523001542005052300154SO 2005 5 23 SWIA200514932 120050426A3350 SIGN EMB 120 EMB120ER 3260203SO CABIN INOPERATIVE A SWIAK NONE L NO TEST NRNOT REPORTED 1 NM07214SW 120280 RED EMERGENCY FLOOR LIGHTS IN GALLEY INOPERATIVE. REPLACED RED EMERGENCY SIGN AT THE GALLEY FLOOR. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050523001552005052300155EA 2005 5 23 SWIA200514933 120050429A2751 SENSOR CNDAIRCL600 CL6002B19 1900309EA RT T/E FLAP MALFUNCTIONED A SWIAO OTHER N FALSE WARNING LDLANDING 1 NM07903SW 7425 FLAPS FAIL CAUTION MESSAGE AFTER LANDING. REPLACED THE RIGHT WING INBOARD AND OUTBOARD FLAP SKEW DETECTION SENSORS IAW CRJ 200 MM 27-51-15. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050523001572005052300157SO 2005 5 23 SWIA200514935 120050429A2611 BATTERY EMB 120 EMB120ER 3260203SO SMOKE DETECTOR DISCHARGED A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07298SW 120328 LAV SMOKE DETECTOR WILL NOT SILENCE. NO VISIBLE SMOKE. REPLACED LAV SMOKE DETECTOR BATTERY. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050523001582005052300158SO 2005 5 23 SWIA200514936 120050428A2611 SMOKE DETECTOR EMB 120 EMB120ER 3260203SO LAVATORY ACTIVATED A SWIAO OTHER J WARNING INDICATION DEDESCENT 1 NM07581SW 120349 ON DESCENT INTO LAX ENCOUNTERED MODERATE CHOP (TURBULANCE) AND RECEIVED A TRIPLE CHIME SMOKE AURAL WARNING. PERFORMED OPERATIONAL CHECK OF LAVATORY SMOKE DETECTOR. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050523001592005052300159SO 2005 5 23 SWIA200514937 120050427A3397 WIRE EMB 120 EMB120ER 3260203SO CABIN CHAFED A SWIAK NONE L NO TEST NRNOT REPORTED 1 NM07585SW 120353 FORWARD PORTION OF FLOOR EMERGENCY LIGHT STRIP INOPERATIVE. REPAIRED CHAFED WIRE IAW MM 33-00-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050523001602005052300160EA 2005 5 23 SWIA200514938 120050427A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA RT SPOILER MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07447SW3413 3413 7677 FLIGHT SPOILER STATUS MESSAGE ILLUMINATED IN FLIGHT. REPLACED RIGHT FLIGHT SPOILER PCU IAW MM CH 27-62-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050523001622005052300162EA 2005 5 23 SWIA200514940 120050429A2760C13045BA03 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA SPOILER MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 NM07719SK164 164 10188 RUDDER LIMIT FAULT STATUS MESSAGE ON CLIMBOUT. REPLACED NR 1 SSCU IAW 27-61-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050523001662005052300166NM 2005 5 23 SWAA051269 120050428A53306545766 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 480, STR 16R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050523001672005052300167NM 2005 5 23 SWAA051270 120050428A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 16L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050523001682005052300168NM 2005 5 23 SWAA051271 120050428A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500B + 11, STR 19L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050523001702005052300170NM 2005 5 23 SWAA051273 120050428A57436552235 ATTACH FITTING BOEING737 7373H4 1384600NM RT WING CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29371SW 26598 DURING SCHEDULED 1/4D CHECK, FOUND RT MLG STABILIZER BEAM FWD & AFT ATTACH FITTINGS CORRODED. REMOVED AND REPLACED STABILIZER BEAM PER MM. 2L72 4F RTA16WE 20050523001722005052300172NM 2005 5 23 SWAA051275 120050428A3350PH22300L STRIP BOEING737 7375H4 138449DNM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29526SW 26568 EEPLS STRIP LOOSE AT FWD LT END. SECURED EEPLS STRIP PER MM. 2L72 4F RTA16WE 20050523001752005052300175NM 2005 5 23 SWAA051278 120050501A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 500A + 6, STR 17L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050523001762005052300176NM 2005 5 23 SWAA051279 120050429A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747 + 6, STR 14R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050523001802005052300180NM 2005 5 23 SWAA051283 120050430A324426078251 TIRE BOEING737 7373H4 1384600NM NLG BLOWN A SWAAD RETURN TO BLOCK O OTHER TOTAKEOFF 1 SW29372SW 26599 DECLARED EMERGENCY. LEFT NLG TIRE BLOWN ON T/O. FOUND NLG W/W FWD BULKHEAD & LOWER TCAS ANTENNA DAMAGED. REPAIRED NLG W/W BULKHEAD PER SWA EA. REMOVED AND REPLACED TCAS ANTENNA PER MM. 2L72 4F RTA16WE 20050523001822005052300182NM 2005 5 23 SWAA051285 120050429A57536546430100 SKIN BOEING737 7373H4 1384600NM RT FOREFLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED C4 CHECK, FOUND RT WING T/E INBOARD FOREFLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM. 2L72 4F RTA16WE 20050523001872005052300187NM 2005 5 23 SWAA051290 120050502A53126546568 BULKHEAD BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29509SW 24186 DURING SCHEDULED 1/2D CHECK, FOUND 3 EA WEB CRACKS AT BS 1016 PRESSURE BULKHEAD DOME CAP 11, 12 & 2 O'CLOCK POSITIONS. REPAIRED WEB PER SWA EA. 2L72 4F RTA16WE 20050523001882005052300188NM 2005 5 23 SWAA051291 120050502A53106546956 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 DURING SCHEDULED D-CHECK, FOUND CORROSION ON RT CREASE BEAM WEB AT BS 370 & BS 406. REPAIRED CREASE BEAM WEB PER SRM. 2L72 4F RTA16WE 20050523001902005052300190NM 2005 5 23 AWXA200500528 120050503A3397ABS0374A24 WIRE AIRBUSA319 A319132 3930340NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28808AW 1088 DEN - EEL - DURING 8-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 10 LT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE LEADING TO EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 10 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050523001942005052300194EU 2005 5 23 AWXA200500532 120050415A5711D57252520006 SPAR AIRBUS320 A320232 3930326EU LT WING CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28638AW 455 SAL - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON LT REAR SPAR HOLES 52, 53, 54, 56, & 60. MAINTENANCE REPAIRED DAMAGE BY REWORKING LT REAR SPAR HOLES PER AIRBUS REPAIR INSTRUCTION R572-58325 ISSUE D AND ER 26-5700-05121-SS1. 2L72 4F RTA28NM 20050523001962005052300196EU 2005 5 23 AWXA200500534 120050415A5711D57252520004 SPAR AIRBUS320 A320232 3930326EU RT WING CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28638AW 455 SAL - MAJOR REPAIR - DURING C-08 CHECK A .5 INCH CRACK WAS FOUND ON RT REAR SPAR HOLE 54 NEXT TO RIB NR 3. MAINTENANCE REPAIRED DAMAGE BY REWORKING RT REAR SPAR HOLE IAW AIRBUS REPAIR INSTRUCTION R572-58325 ISSUE D AND ER 26-5700-05121-SS1. 2L72 4F RTA28NM 20050523001972005052300197WP 2005 5 23 ARWA20050407 120050430A77228DJ175LXP2 INDICATOR DOUG DC10 DC1030 3023501WP COCKPIT FAULTY A ARWAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING TXTAXI/GRND HDL 1 SO19524MD 46999 DURING ENGINE START & FUEL LEVER ON NR 2 ENGINE EGT RISE RAPIDLY; ENGINE SHUTDOWN AT 700 FT AFT ENGINE SHUTDOWN EGT INDICATION CONTINUED TO MAX LIMITS. REMOVED AND REPLACED NR 2 ENGINE EGT INDICATOR; OPERATIONAL CHECK NORMAL IN ACCORDANCE WITH DC-10 M/M 77-10-00. 2L73 4F A22WE 20050523001992005052300199 2005 5 23 05FDEA01196 420050503A2312S6582622A ANTENNA BOEING727 727200 138407ENM LOWER VHF CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25254FE 20936 LOWER AFT VHF ANTENNA HAS CORROSION ON ITS BASE. REMOVED AND REPLACED LWR AFT VHF ANTENNA IAW MM 23-21-031-2, OPS CHECKS GOOD. 2L73 4F RTA3WE 20050523002032005052300203NM 2005 5 23 DHL2005783518 120050404A5330 SKIN BOEING727 727227 1384078NM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01783DH 21999 BS 362 BELOW STR 17L FUSELAGE SKIN IS DENTED. DAMAGE FOUND TO BE OUT OF LIMITS IAW 727 SRM 53-30-1 FIG 1. REMOVED PREVIOUS REPAIR AT LOCATION FOR INCORPORATION IAW SRM 51-30-2. PREVIOUS CUT OUT DIM 2" BY 1 7/16", CUT OUT DAMAGE AREA DIM 4.500 BY 2.500 INCHES AND FABBED REPAIR DOUBLER FROM 2024T3 .071 PO NR 9002193 DIM. 18.3750 BY 13 INCHES AND FILLER FROM 2024T3 .050 PO NR 9001873 DIM 4 BY 2.500 INCHES IAW SRM 53-30-2 FIG 1 AND 53-30-3 FIG 3A AND 1. REPAIR PARTS TREATED, PRIMED, AND INSTALLED IAW 727 SRM 51-10-2 AND 53-30-3 FIG 1 AND 3A. THIS REPAIR IS CAT "B". 2L73 4F A3WE 20050523002042005052300204NM 2005 5 23 DHL2005783519 120050404A5730 SKIN BOEING727 727227 1384078NM RT WING DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01783DH 21999 RT WING INBD AILERON UPPER SKIN IS DENTED, WING STA 436. CUT OUT DAMAGED AREA DIM 3" BY 1 1/4" IAW B727 SRM 57-50-5 FIG 2. FABRICATED DOUBLER FROM 2024T3 .032 PO NR 9002034 DIM. 5 1/8" BY 6 1/4" IAW B727 SRM 57-50-5 FIG 2. TREATED AND PRIMED IAW B727 SRM 51-10-2, INSTALLED DOUBLER REPAIR ON R/WING I/B AILERON SKIN STA 436 IAW B727 SRM 57-50-5 FIG 2 AND 57-50-2 FIG 2. NO REBALANCING REQUIRED FOR INBD AILERON IAW B727 SRM 51-80-1 PARA 1B. 2L73 4F A3WE 20050523002052005052300205NM 2005 5 23 05FDEA01198 120050503A5320652367861 STRAP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25254FE 20936 SUBFLOOR BEAM STRAP STA 312-344 RBL 25 IS CRACKED 3EA PLACES. REMOVED AND REPLACED STRAP IAW SRM 51-30-2. 2L73 4F RTA3WE 20050523002062005052300206NM 2005 5 23 05FDEA01199 120050503A575469179012 MOUNT BRACKET BOEING727 727200 138407ENM NR 1 SLAT CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25254FE 20936 NR 1 SLAT OUTBOARD TRACK MOUNT BRACKET CRACKED. REMOVED AND REPLACED BRACKET IAW SRM 51-30-2. 2L73 4F RTA3WE 20050523002082005052300208NM 2005 5 23 05FDEA01201 120050504A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER UKUNKNOWN 1 SO25254FE 20936 EVALUATE PREVIOUS REPAIR STA 1120 STR 22 FOR REPAIR STATUS (MAJOR/MINOR) AND FAA APPROVAL. REMOVED DAMAGE SECTION OF STRINGER, FABBED FILLER AND SPLICES AND INSTALLED REPAIR IAW SRM 53-10-3 FIG 1 DETAIL I. THIS IS A MAJOR REPAIR ON N/R N00228 AT MAE. 2L73 4F RTA3WE 20050523002112005052300211NM 2005 5 23 05FDEA01204 120050504A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25254FE 20936 CORROSION, STRINGER END TO FWD LWR FUEL TANK CHORD FITTING STA 740 STR 26L. REMOVED DAMAGED AREA IAW SRM 53-10-3 FIG 1 MATERIAL BAC 1498- 147-7075-T6 BATCH 27819 AND SPLICE MAT BMC 1498-131-7075-T6 BATCH 32659. LOCATED AND DRILLED IAW SRM 51-30-5, INSTALLED REPAIR PARTS IAW SRM 53-10-3 FIG 1. 2L73 4F RTA3WE 20050523002122005052300212NM 2005 5 23 WRLA2005085 120050428A5250 LOCK DOUG MD11 MD11 3023602NM COCKPIT DOOR BURNED A WRLAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11277WA 48743 DURING CRUISE (ABOUT 5 HR,S AFTER T/O), THE CREW DETECTED A STRONG ELECTRCAL ODOR WITH LIGHT SMOKE. A DECISION WAS MADE TO DIVERT THE AIRPLANE TO PANC, A NORMAL LANDING WAS MADE, CREW FOLLOWED THE STANDARD EMERGENCY PROCEDURE. MAINTENANCE AT PANC INSPECTED WIRING AND COMPONENTS ABOVE OVERHEAD C/B PANEL AND ELEC CONTROL PANEL WIRING AND FWD ELE BAY, NO DEFECTS NOTED. FOUND MELTED INSULATION AT CKPT DOOR LOCK. PULLED THE CKPT DOOR C/B AND DEFERRED THE COCKPIT AUTOMATIC LOCKING SYSTEM PER MD-11 MEL PROCEDURES. 2L73 4F RTA22WE 20050523002152005052300215CE 2005 5 23 DXTA200500704 120050429A2810MS29513117 O-RING CESSNA750 750 2076810CE FUEL TANK CUT E DXTAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 GL07999QS 7500203 WING TANK OVERFULL R AMBER CAS MESSAGE CAME ON IN FLIGHT. DID NOT STOP OVERVENTING FUEL UNTIL DESCENDING THRU +/- 17000 FEET AND RIGHT FUEL GAUGE 3010 LBS, LEFT GAUGE 3290 LBS. - (M2B) FOUND FUEL COMING FROM RT AILERON BELCRANK DRY BAY. FOUND ONE CROSS OVER TUBE IN THIS DRY BAY TO HAVE A CUT O-RING. REPLACED 4 EA O-RINGS P/N MS29513-117 AND 4 EA O-RINGS P/N MS29415-218 AT THE ENGINES FITTINGS IN THE DRY BAY TUBES. FOUND FLAPPER VALVE AT INBOARD END OF FWD TUBE TO HAVE EXCESSAVE PLAY. REPLACED FLAPPER VALVE WITH NEW VALVE IAW CE750 M/M CH 28-10-0. OPS CHECKED AND LEAK CHECKED GOOD. 2L72 4J RTT00007WI 20050523002162005052300216NM 2005 5 23 UPS05444429 120050410A5320AND101362402 RETAINER BOEING747 747200 1384847NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 INSPECTION TYPE:C FX - KEEL BEAM BOX LWR SUPPORT T-RETAINER FWD UPPER SURFACE FOUND CORROSION AT STA 1297 LBL 6 - RBL 6, CORROSION BLEND OUT 0.032 X .5 X 1.25 INCH, T-RETAINER REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F RTA20WE 20050523002212005052300221NM 2005 5 23 UPS05644419 120050430A2560 SMOKE GOGGLES BOEING767 76734AF 1385212NM COCKPIT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01305UP 27243 INSPECTION TYPE:N/A CAPTAIN'S SMOKE GOGGLES CRACKED. REPLACED CAPTAIN'S SMOKE GOGGLES 2L72 4F RTA1NM 20050523002252005052300225WP 2005 5 23 UPS05844417 120050427A5330561386261 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 INSPECTION TYPE:SP COMPLY WITH D 301309 REGARDING FUSELAGE SKIN CORROSION AT E/E DOOR STA 35. CUT OUT DAMAGED SKIN, FABRICATED AND INSTALLED REPAIR IAW EO DC8-5330- 22128-A AND SAA SK 708-911. 2L74 4F RT4A25 20050523002262005052300226SO 2005 5 23 CHQA200500090 120050426A3397 WIRE EMB 145 EMB145MP 3260216SO EMERGENCY LIGHT BROKEN A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11976RP 145322 LAST FLOOR EMERGENCY PROXIMITY LIGHT STRIP IN CABIN IS INOP. TROUBLE SHOT AND FOUND WIRES W192-8832-22 AND W192-8833-22 BOTH BROKEN AT CONNECTORS SP9Z12PS9213. REPINED CONNECTOR ON AIRFRAME SIDE AND RECONNECTED. OPS CHECK OF EMERGENCY LIGHTS GOOD IAW EMB 145 AMM 33-50-00. WIRE REPAIRS WERE DONE PER EMB 145 WM CHAPTER 20 STANDARD PRACTICES. 2L72 4F RTT00011AT 20050523002292005052300229SO 2005 5 23 CHQA200500093 120050501A335066367 LIGHT EMB 135 EMB135KL 3260302SO CABIN INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11381SK 145619 FLOOR PROXIMITY LIGHT IS INOP. REMOVED AND REPLACED FLOOR PROXIMITY LIGHT IAW EMB 140 AMM 33-50-04. OPS CHECK GOOD AT THIS TIME AND DATE. 2L72 4F RTT00011AT 20050523002302005052300230NM 2005 5 23 UPS05M44418 120050413A5744ARC050311 BRACKET DOUG MD11 MD11F 3023600NM LT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01253UP 48439 INSPECTION TYPE:1C DURING REMOVAL OF LT OUTBOARD FLAP ACTUATOR AIRCRAFT SIDE MOUNT HOLES PITTED & LITE CORROSION. REPAIRED MOUNT HOLES IAW CMM 57-44-09, CMM 57-52-04, MM 27-52-02, SAA SK 253-637 & FAA FORM 8100-9 DATED 25 APR 2005. 2L73 4F RTA22WE 20050523002312005052300231NM 2005 5 23 TSAA0532020 120050428A3244 TIRE BOEING737 73773A 1384606NM NLG WORN A TSAAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 WP13739AL 28500 SNA-OGG: WHEN ADDING FULL POWER, THE AIRCRAFT DEVIATED FROM THE CENTER LINE. TERMINATED TAKEOFF, NOSE WHEEL SCRUBBING OCCURRED. RETURNED TO GATE. INSPECTED THE NLG AND NLG STEERING; FOUND LEFT HAND NOSE SHOULDER WORN BEYOND LIMITS. REMOVED AND REPLACED THE LEFT HAND NOSE TIRE. FUNCTION NOSE WHEEL STEERING, NO DEFECTS NOTED. LEFT HAND NOSE TIRE REMOVED AND REPLACED PER AQ FORM M-711. AS A PRECAUTION, REMOVED AND REPLACED THE RIGHT HAND NOSE TIRE PER AQ FORM M-711. OK FOR SERVICE. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA16WE 20050523002322005052300232GL 2005 5 23 ARWA20050501 220050501A7421595019442352 IGNITER DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL NR 1 ENGINE DEFECTIVE A ARWAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO1968041 46900 451469 DURING ENGINE START NR 1 ENGINE IGNITION -A- INOPERATIVE; TRANSFER TO DMI NR 19182 AS PER MEL 74-1-1 CATEGORY-C. REMOVED AND REPLACED NR 1 ENGINE -A- IGNITOR IN ACCORDANCE WITH M/M 74-20-02; OPERATIONAL CHECK NORMAL. 2L73 4F4 F A22WE E23EA 20050523002332005052300233CE 2005 5 23 ACE050405 120050504A3397 WIRE BEECH 1900 1900C 1154161CE COCKPIT OVERHEATED E YADAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 AL03112AX UC45 PIREP - LEFT LANDING LIGHT CIRCUIT BREAKER POPS OFF APPROXIMATELY 5 MINUTES AFTER LIGHT TURNED ON, ELECTRICAL BURNING SMELL NOTED IN FLIGHT DECK. MAINTENANCE DEFERRED THE DEACTIVATED CIRCUIT. MAINTENANCE WAS UNABLE TO DUPLICATE FAILURE, FOUND EVIDENCE OF HEATED WIRES AT BUSS SIDE OF CIRCUIT BREAKER SWITCH AND SWITCH EXHIBITED EVIDENCE OF HEATING (SUSPECT HIGH RESISTANCE FROM LOOSE TERMINAL). REPLACED CIRCUIT BREAKER SWITCH AND RE-TERMINATED AFFECTED WIRES, CLEARED DEFERRAL. 2L72 4T RTA24CE 20050523002352005052300235EA 2005 5 23 MASA200500083 120050206A7830M8353622025M RELAY CNDAIRCL600 CL6002D24 1390016EA THRUST REVERSER INOPERATIVE A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07924MJ 15024 ASH 6528 PHX - PVR. ABORTED TAKEOFF DUE TO LEFT THRUST REVERSER UNSAFE MESSAGE. MAINTENANCE PLACED THE THRUST REVERSER ON MEL. MAINTENANCE REMOVED AND REPLACED K29 RELAY, OPS CHECK GOOD. 2L72 4F RTA21EA 20050523002362005052300236NM 2005 5 23 MASA200500145 120050222A2910AN81510D UNION DHAV DHC8 DHC8202 2809007NM HYDRAULIC SYS BROKEN A MASAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW07455YV 455 DEN - RAP, CAPT RETURNED TO THE FIELD DUE TO NR 1 ENG HYD LIGHT ILLUMINATED IN FLIGHT. CAPT ALSO REPORTED, THERE WAS NO HYD QUANTITY INDICATION ON NR 1 HYD SYSTEM. MAINTENANCE FOUND A UNION AT NR 1 HYD MANIFOLD BROKE. AOG FOR PARTS AT THIS TIME. MAINTENANCE INSTALLED NEW UNION. 2H72 4T RTA13NM 20050523002372005052300237EA 2005 5 23 MASA200500310 120050422A76032100140007 GEARBOX CNDAIRCL600 CL6002B19 1900309EA THROTTLE WORN A MASAK NONE O OTHER NRNOT REPORTED 1 SW0775993 7372 COMPLIED WITH THE THROTTLE GEARBOX INSPECTION OF THE NR 1 ENGINE AND FOUND WEAR TO BE ACCEPTABLE AND WITHIN LIMITS OF MESA EO CRJ-76-0004. REMOVED AND REPLACED. 2L72 4F RTA21EA 20050523002392005052300239NM 2005 5 23 86 120050505A5320 FLOOR SUPPORT DOUG MD88 MD88 3023688NM FUSELAGE CORRODED B DU4RK NONE O OTHER ININSP/MAINT 1 SO1512FQ 49766 CORRODED CABIN FLOOR SUPPORT STRUCTURE FS 2092.0 RBL-11. 2L72 4F RTA6WE 20050523002412005052300241NM 2005 5 23 88 120050505A5320 WEB DOUG MD88 MD88 3023688NM FUSELAGE CORRODED B DU4RK NONE O OTHER ININSP/MAINT 1 SO1512FQ 49766 CORRODED CABIN FLOOR WEB BS 180.0 RBL-0-36. 2L72 4F RTA6WE 20050523002422005052300242NM 2005 5 23 90 120050505A5320 WEB DOUG MD88 MD88 3023688NM FUSELAGE PUNCTURED B DU4RK NONE O OTHER ININSP/MAINT 1 SO1512FQ 49766 PUNCTURED CABIN FLOOR WEB FS 170.0 LBL-44. 2L72 4F RTA6WE 20050523002432005052300243NM 2005 5 23 91 120050505A5321 FLOOR PANEL DOUG MD88 MD88 3023688NM FUSELAGE DELAMINATED B DU4RK NONE O OTHER ININSP/MAINT 1 SO1512FQ 49766 DELAMINATED LEFT STA 160 - 200 FLOOR PANEL WITH HOLES AND MISSING INSERTS. 2L72 4F RTA6WE 20050523002442005052300244NM 2005 5 23 92 120050505A5330 SKIN DOUG MD88 MD88 3023688NM FUSELAGE DENTED B DU4RK NONE O OTHER ININSP/MAINT 1 SO1512FQ 49766 DENTED FUSELAGE SKIN FS 123 L-26R DEPTH 0.054, 2.30, 3.2. 2L72 4F RTA6WE 20050523002462005052300246NM 2005 5 23 94 120050505A5330 SKIN DOUG MD88 MD88 3023688NM FUSELAGE DENTED B DU4RK NONE O OTHER ININSP/MAINT 1 SO1512FQ 49766 DENTED FUSELAGE SKIN FS 740 BETWEEN L-27L AND L-28L 2.0 X 2.5 INCH DEPTH 0.075 INCH. 2L72 4F RTA6WE 20050523002472005052300247NM 2005 5 23 95 120050505A5330 SKIN DOUG MD88 MD88 3023688NM FUSELAGE DENTED B DU4RK NONE O OTHER ININSP/MAINT 1 SO1512FQ 49766 DENTED FUSELAGE SKIN FS 314 BETWEEN L-23L AND L-24L 2.3 X 1.4 INCH, DEPTH 0.013 INCH. 2L72 4F RTA6WE 20050523002492005052300249EU 2005 5 23 AWXA200500536 120050504A3397ABS0374A24 WIRE AIRBUS320 A320231 3930325EU CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28624AW 055 SEA - EEL - DURING FUNCTIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM-A BROKEN WIRE WAS FOUND AT THE WALL CONNECTOR FOR THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 17 LT. MAINTENANCE REPINNED THE EMERGENCY ESCAPE PATH LIGHT WIRE TO THE WALL CONNECTOR AT SEAT ROW 17 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050523002512005052300251NM 2005 5 23 SWAA051293 120050428A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 395, STR 16L. MX FERRY TO DALLAS. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050523002522005052300252NM 2005 5 23 SWAA051294 120050428A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 416, STR 26L. MX FERRY TO DALLAS. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050523002532005052300253NM 2005 5 23 SWAA051295 120050428A53306545766 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 443, STR 26L. MX FERRY TO DALLAS. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050523002542005052300254NM 2005 5 23 SWAA051296 120050428A53306545766 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 460, STR 17R TO STR 18R. MX FERRY TO DALLAS. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050523002552005052300255NM 2005 5 23 SWAA051297 120050502A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 500C + 17, STR 15R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050523002562005052300256NM 2005 5 23 SWAA051298 120050502A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 500C + 5, STR 15L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050523002572005052300257NM 2005 5 23 SWAA051299 120050502A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 727E + 15, STR 19R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050523002592005052300259NM 2005 5 23 SWAA051301 120050503A335090083 BATTERY BOEING737 7373H4 1384600NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED SERVICE CHECK, FOUND LT AFT CABIN EMERGENCY LIGHTS INOP AT BS 753. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050523002612005052300261NM 2005 5 23 SWAA051303 120050503A3350612825 BATTERY BOEING737 7373H4 1384600NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29331SW 23695 DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN BULLNOSE EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY & POWER SUPPLY PER MM. 2L72 4F RTA16WE 20050523002622005052300262 2005 5 23 SWAA051304 420050503A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29341SW 24091 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050523002632005052300263NM 2005 5 23 SWAA051305 120050503A53116547959 FRAME BOEING737 7375H4 138449DNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29509SW 24186 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON AFT CARGO FWD STUB FRAME AT BS 794.3, STR 24R TO STR 25R. REPAIRED STUB FRAME PER SWA EA. 2L72 4F RTA16WE 20050523002682005052300268NM 2005 5 23 SWAA051306 120050503A53306547955 STRAP BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29509SW 24186 DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO FWD SKIN STRAP CRACKED AT BS 794.3, STR 22R TO STR 23R. REPAIRED SKIN STRAP PER SWA EA. 2L72 4F RTA16WE 20050523002712005052300271NM 2005 5 23 SWAA051307 120050503A53116546539 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 DURING SCHEDULED D-CHECK, FOUND 2 EA FUSELAGE FRAME CHORDS CRACKED AT BS 616, LBL 65 & RBL 65, WL 202. REPAIRED FRAME CHORDS PER BFG ER. 2L72 4F RTA16WE 20050523002722005052300272NM 2005 5 23 SWAA051308 120050503A53156546548 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 727A + 4, RBL 2, WL 155. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20050523002742005052300274NM 2005 5 23 SWAA051310 120050503A53116546549 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 DURING SCHEDULED D-CHECK, FOUND CORROSION ON FUSELAGE FRAME AT BS 767, STR 27L TO STR 25R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050523002772005052300277NM 2005 5 23 SWAA051313 120050503A531165C25229 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050523002782005052300278NM 2005 5 23 SWAA051314 120050503A53116546555 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050523002822005052300282WP 2005 5 23 ABXA050106 120050419A53105910349507 DOOR FRAME DOUG DC9 DC932 3022066WP LT MLG WW CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23985AX 47522 FORWARD DOOR JAMB CRACKED. INBOARD END FORWARD OF DOOR HINGE. REPAIRED AREA IAW DC-9 SRM 53-01. 2L72 4F A6WE 20050523002852005052300285EA 2005 5 23 COMA0560289 120050503A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA WING CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01708CA 7235 FRETTING CORROSION LOWER WING PLANK 193A. REPAIRED IAW REO 601R-57-21-588. 2L72 4F RTA21EA 20050523002892005052300289EA 2005 5 23 COMA0560290 120050503A5320 WEB CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01708CA 7235 FS 280.00 WEB CORRODED ON FACE BETWEEN LBL 9 AND RBL 9. REPAIRED IAW REO 601R-53-11-136, EO 10-5310-00623. 2L72 4F RTA21EA 20050523002952005052300295EA 2005 5 23 COMA0560292 120050503A5210 FRAME CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01708CA 7235 TWO CRACKS FOUND BETWEEN PAX DOOR FS 338 AND FS 320. REPAIRED IAW REO 601R-52-11-402 AND EO 10-5210-00620. 2L72 4F RTA21EA 20050523002982005052300298NM 2005 5 23 UPS05444395 120050409A5311 FRAME BOEING747 747283B 1384867NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 BS 160 S14BL - 14CL FRAME INNER FLANGE FOUND CRACKED, CRACK LENGTH .25 INCH. BS 160 STR 14BL TO STR 14CL FRAME INNER FLANGE REPAIRED AS PER HX RS R-53-12-35288 AND UPS EO NR B747-5310-22088-A. 2L74 4F A20WE 20050523003012005052300301NM 2005 5 23 UPS05444397 120050408A5311141U105717 FRAME BOEING747 747283B 1384867NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 NR 1 LT MED CUTOUT BS 488 FRAME AT STR 25L INNER CHORD TWO FASTENER HOLES FOUND CRACKED AND AS MARKED, CRACK LENGTH 1/8 INCH. NR 1 MED LT BS 488 INNER CHORD REPLACED AS PER SB 747-53-2272 AND DWG 624U0003 SHT 40A. 2L74 4F A20WE 20050523003032005052300303NM 2005 5 23 UPS05444399 120050412A5322 SHEAR TIE BOEING747 747283B 1384867NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 COCKPIT BS 360 STR 1R FRAME SHEAR TIE CRACKED, CRACK LENGTH 1/2 INCH. COCKPIT BS 360 FRAME WEB REPAIRED AT BTN STR 1R AND STR 2R AREA AS PER HX RS R53-12-35290 AND UPS EO NR B747-5310-22086-A. 2L74 4F A20WE 20050523003062005052300306EA 2005 5 23 QXEA200500840 120050426A5753 FLAP CNDAIRCL600 CL6002C10 1390015EA LT WING CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09607QX 10024 PDX - LEFTHAND FLAP HAS CHAFE BACK OF FLAP BY NR 2 FLAP VANE ACCESS PANEL. REPAIRED IAW CRJ700 SRM 51-21-16 AND HORIZON AIR EA R-57-106. 2L72 4F RTA21EA 20050523003132005052300313NM 2005 5 23 QXEA200500838 120050503A2150 SWITCH DHAV DHC8 DHC8202 2809007NM CABIN FAILED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09350PH 488 MFR - DURING CLIMBOUT OBSERVED AIR COND PACK HOT CAUTION LIGHT. INCREASED CABIN TEMP PER ABNORMAL CHECKLIST UNTIL LIGHT EXTINGUISHED. COULD NOT DECREASE TEMP BELOW APPROXIMATELY 30 DEGREES CELSIUS ON DUCT TEMP GAUGE WITHOUT CAUSING LIGHT TO COME BACK ON. MAINTENANCE REPLACED COMPRESSOR DISCHARGE OVER TEMPERATURE SWITCH IAW TASK 21-50-31-000-801 AND 400-801. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050520000132005052000013 2005 5 20 SWAA051430 420050515A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29791SW 27886 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. SLIDE DID NOT DEPLOY. INSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20050520000162005052000016NM 2005 5 20 05FDEA01120 120050426A5347ADA83891 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25608FE 48548 MAIN DECK, FLOOR SEAT TRACK AT STA Y= 1904 TO Y= 1059, X= 47 CROWN ELONGATED ADA8389-1. REMOVED AND REPLACED PER SRM 53-70-00 VOLUME I, FIGURE 1. 2L73 4F RTA22WE 20050520000302005052000030NM 2005 5 20 05FDEA01138 120050426A5330 SKIN BOEING727 727200 138407ENM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25264FE 21626 GOUGE DAMAGE IN SKIN, BS 460, STR - 25R. REPAIRED SKIN AT BS 460, STR 25R IAW SRM 53-30-3. 2L73 4F RTA3WE 20050520000372005052000037EU 2005 5 20 YENA200529 120050429A271031073110 ACTUATOR AIRBUS320 A320232 3930326EU AILERONS MALFUNCTIONED A YENAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 EA15590JB3770 2231 AIRCRAFT EXPERIENCED WING FLUTTER ON CLIMB-OUT PASSING 6000 FT STEADY 250KIAS WHILE TURNING. NO ABNORMAL YAW, NO ABNORMAL INDICATION ON FLIGHT CONTROL ECAM PAGE. NO ABNORMAL INDICATION ON HYD ECAM PAGE. ONSET OF FLUTTER WAS FASTER AT HIGHER SPEED. MAX SPEED WAS 307, MAX ALTITUDE WAS FL 240. FLUTTER IN TURN (ROLL IN / ROLL OUT) CONTINUED THROUGH OUT THE FLIGHT. FLIGHT CREW DECLARED EMERGENCY AND RETURNED TO FIELD. TECHNICIANS DUPLICATED FAULT WITH RT GREEN AILERON SERVO ACTUATOR FLUCTUATING DURING TROUBLESHOOTING PROCEDURE. REMOVED AND REPLACED GREEN SYSTEM RT AILERON SERVO ACTUATOR (FIN 33CE2) IAW AMM 27-14-51. NO LEAKS NOTED, OPERATION TEST NORMAL IAW MM 27-14-00. 2L72 4F RTA28NM 20050520000462005052000046NM 2005 5 20 05FDEA01206 120050504A575365192507 FLAP TRACK BOEING727 727200 138407ENM NR 2 FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25264FE 21626 NR 2 FLAP TRACK REAR SPAR ATTACH AREA IS CORRODED. REPLACED NR 2 FLAP TRACK ON FED EX CARD 27X5706-03. 2L73 4F RTA3WE 20050523000082005052300008NM 2005 5 23 05FDEA01149 120050427A5315 FLOORBEAM DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE CABIN FLOOR SUPPORT AT STA 1913 RBL 42 FOUND PREVIOUS REPAIRED NON- STANDARD AS MARKED. FLOOR SUPPORT REMOVED AS PER SRM 51-31-01 VOL II. NEW FLOOR SUPPORT REWORKED FROM S2929348 AS PER DRAWING AGA 7501 AND REPROTECTED AS PER SRM 51-21-01 VOL II. NEW FLOOR SUPPORT PAINTED AS PER SRM 51-21-01 VOL II AND PART MARKED FX AGA 7501-502 AS PER GMM 7-0-1001. NEW FLOOR SUPPORT LOCATED AND INSTALLED AT STA 1913 RBL 26 TO 53 AS PER SRM 51-31-01 VOL II. CLASSIFIED MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050523001522005052300152 2005 5 23 2005UALA00391 420050426A2565 GAUGE BOEING757 757222 1384956NM PWA 2037 PW2037 NE EVAC SLIDE DEFECTIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29572UA 26682 DOOR 2R LOW SLIDE PRESSURE. PRESSURE GAUGE WAS FALLING APART. NO FAULT FOUND. INSPECTION OF PRESSURE VESSEL/VALVE ASSEMBLY REVEALED NO DISCREPANCIES. UNIT WAS OVERHAULED AND RETURNED TO SERVICE. 2L72 4F4 FRTA2NM E17NE 20050523001562005052300156EA 2005 5 23 SWIA200514934 120050430A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA LT SPOILER MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07437SW9819 9819 7564 UNCOMMANDED SPOILER MOVEMENT LEFT OUTBOARD SPOILERON, SPOILERONS FAULT ON TAXI OUT. REPLACED LEFT SPOILERON PCU NR 2 HYD SYSTEM IAW 27-62-01, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050523001642005052300164SO 2005 5 23 C2XA05IA066 120050502A335078241 INVERTER EMB 145 EMB145LR 3260212SO CABIN MALFUNCTIONED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714993 145289 OKC - FLIGHT 2964, DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHT AT THE FORWARD FLIGHT ATTENDANT SEAT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. NOTE: THIS PART IS NOT SERIALIZED, AND NO TIMES ARE AVAILABLE. 2L72 4T RTT00011AT 20050523001652005052300165SO 2005 5 23 C2XA05IA067 120050503A335066903 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713955 145075 MCI - DURING MAINTENANCE INSPECTION, THE LAST 8 INCHES OF EMERGENCY AISLE PATH LIGHTING WAS FOUND TO BE INOPERATIVE. MAINTENANCE PLACED THE AISLE PATH LIGHTING ON MEL 33-50-12 CAT-C CONTROL NUMBER 056545, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED AT BNA ON FLIGHT 3374 WHERE MAINTENANCE REMOVED AND REPLACED THE AFFECTED AISLE PATH EMERGENCY LIGHT STRIP, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. NOTE: THIS PART IS NOT SERIALIZED, AND NO TIMES ARE AVAILABLE. 2L72 4T RTT00011AT 20050523001792005052300179NM 2005 5 23 SWAA051282 120050430A3350BPS73 BATTERY BOEING737 7373H4 1384600NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29365SW 26576 DURING SCHEDULED SERVICE CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20050523001912005052300191NM 2005 5 23 AWXA200500529 120050503A3397BMS13311122 WIRE BOEING757 7572S7 1384962NM CABIN BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW 23323 BWI - EEL - DURING A-12 CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 14 LT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE LEADING TO EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 14 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20050523001922005052300192EU 2005 5 23 AWXA200500530 120050415A5711D57252520006 SPAR AIRBUS320 A320232 3930326EU LT WING CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28638AW 455 SAL - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON LT ACTUATING CYLINDER HOLES 52, 53, 55, 57, 59, 61, & 66. MAINTENANCE REPAIRED DAMAGE BY REWORKING LT ACTUATING CYLINDER HOLES PER AIRBUS REPAIR INSTRUCTION R572-58325 ISSUE D AND ER 26-5700-05121-SS1. 2L72 4F RTA28NM 20050523001952005052300195EU 2005 5 23 AWXA200500533 120050415A5711D57252520004 SPAR AIRBUS320 A320232 3930326EU RT WING CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28638AW 455 SAL - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON RT ACTUATING CYLINDER HOLES 52, 53, 55, 56, 58, 59, & 79-81. MAINTENANCE REPAIRED DAMAGE BY REWORKING RT ACTUATING CYLINDER HOLES PER AIRBUS REPAIR INSTRUCTION R572-58325 ISSUE D AND ER 26-5700-05121-SS1. 2L72 4F RTA28NM 20050523002072005052300207NM 2005 5 23 05FDEA01200 120050504A52426521634 RETAINER BOEING727 727200 138407ENM E/E BAY DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25212FE 22934 E & E COMPARTMENT DOOR AFT SEAL RETAINER BENT AND CRACKED. REMOVED AND REPLACED SEAL RETAINER IAW SRM 51-30-2. 2L73 4F RTA3WE 20050523002092005052300209NM 2005 5 23 05FDEA01202 120050504A5330 SKIN BOEING727 727200 138407ENM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25254FE 20936 FUSE SKIN AT BS 1228 STR 22L HAS DEEP GOUGED MARK MEASURED 1.5 INCH LONG. FABBED REPAIR PLATE IAW SRM 53-30-3 FIG 1 AND INSTALLED REPAIR PLATE IAW SRM 51-30-2. THIS IS A MAJOR REPAIR AT MAE ON N/R N00818. 2L73 4F RTA3WE 20050523002142005052300214CE 2005 5 23 DXTA200500701 120050426A2730991455810 ACTUATOR CESSNA750 750 2076810CE PITCH FEEL FAULTY E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07961QS1157 7500061 "PITCH FEEL FAIL" CAS CAME ON AT 3000 FT 200 KIAS EVENT MARKER USED, LIGHT EXTINGUISHED AFTER APPROX 3-5 MIN AT 180 KIA, 2500 FT, TROUBLESHOT TO FAULTY RT PITCH FEEL ACTUATOR REMOVED AND REPLACED ACTUATOR IAW 750MM 27-33-00. OPS CHECKED OK IAW 750 MM 27-30-00. 2L72 4J RTT00007WI 20050523002192005052300219CE 2005 5 23 DXTA200500700 120050426A574067305014 ATTACH BRACKET CESSNA750 750 2076810CE ELEVATOR WORN E DXTAK NONE O OTHER ININSP/MAINT 1 GL07924QS 7500124 YOKE HAS 1-2" DEAD SPOT IN PITCH IN BOTH MANUAL AND AUTO PILOT MODES. FOUND PITCH FEEL ELEVATOR CONTROL BRACKETS ATTACHING HOLE WORN AND ELONGATED, REPLACED BRACKET AND ACCOMPLISHED REPAIR IAW REPAIR DEFINITION S-750-0124/04RD FROM CESSNA DATED APRIL 29, 2005. OPS CHECKS GOOD COMPLETED AS REQUIRED REF 750 MM 27-30-00 ADJUSTED COLUMN BALANCE BUNGEE AS REF. 750 MM 27-30-00 PG 527. 2L72 4J RTT00007WI 20050523002232005052300223CE 2005 5 23 DXTA200500707 120050502A3240 BRAKE ASSY CESSNA500 560CESSNA 2076750CE MLG MALFUNCTIONED E DXTAO OTHER O OTHER LDLANDING 1 GL07383QS 5600483 BRAKES SEEMED TO FAIL ON LANDING ROLLOUT AROUND 35KTS FOR ABOUT 2 SECONDS. FAILURE WAS ACCOMPANIED BY CLICKING NOISE UNDER PILOTS FLOORBOARD AREA. BRAKES WORKED WELL DURING TAXI IN. REQUIRES HIGH SPEED TAXI CHECK WITH ANTI SKID AND WITHOUT IT ON. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20050523002272005052300227GL 2005 5 23 CHQA200500092 220050429A7200 ENGINE EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL NR 2 FAILED A CHQAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL11373SK101314036 145543 CAE311855 FLIGHT 5295 CMH-STL, APPROX 700 FT AGL AFTER DEPARTURE ON RUNWAY 28L IN CMH FA REPORTED SMOKE IN CABIN AND A STRONG BURNING SMOKE ODOR WAS IN THE COCKPIT. A MINUTE OR SO LATER LAV SMOKE ON EICAS APPEARED. DECLARED AN EMERGENCY AND RETURNED TO FIELD. WHILE ON BASE LEG THE MESSAGE WENT AWAY, AND FA REPORTED SMOKE WAS CLEARING OUT. LANDED IN CMH ANYWAY AS A PRECAUTION. LANDED APPROX 2000 LBS OVER LANDING WEIGHT, THE VSI WAS APPROX 200 FPM DESCENT WHEN THE WHEELS TOUCHED THE RUNWAY. MAINTENANCE FOUND OIL IN THE NR 2 BLEED SYSTEM. REMOVED AND REPLACED NR 2 ENGINE IAW J/C CE720001. OPS CHECK AND LEAK CHECK GOOD. NO SMELL NOTED. 2L72 4F4 FRTT00011ATTE6CH 20050523002342005052300234NM 2005 5 23 MASA200500041 120050116A291082920010363 HYDRAULIC LINE DHAV DHC8 DHC8202 2809007NM HYDRAULIC SYS LEAKING A MASAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW07987HA 425 ASH 6347 HMO PHX RETURNED TO THE FIELD DUE TO THE NR 2 HYD SYSTEM FAILED ON GEAR RETRACT. MAINTENANCE ARE IN THE PROCESS OF TROUBLESHOOTING. MAINTENANCE INSTALLED A TEMP FLEX LINE ON NR 2 HYD PRESS TRANSDUCER TO FLY THE AIRCRAFT BACK TO PHX. LATER THE FLEX LINE WAS REPLACED WITH THE PERMANENT HYD LINE. TEMP LINE P/N AE2460000E0200 (VARGA ENTERPRISES). 2H72 4T RTA13NM 20050523002452005052300245NM 2005 5 23 93 120050505A5330 SKIN DOUG MD88 MD88 3023688NM FUSELAGE DENTED B DU4RK NONE O OTHER ININSP/MAINT 1 SO1512FQ 49766 DENTED FUSELAGE SKIN FS 585 BETWEEN L-23L AND L-24L 3.25 X 2.25 INCH DEPTH, 0.015 INCH. 2L72 4F RTA6WE 20050523002732005052300273NM 2005 5 23 SWAA051309 120050503A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 DURING SCHEDULED D-CHECK, FOUND 2 EA LONGITUDINAL FLOORBEAMS CORRODED AT BS 727E +2, LBL 2 & RBL 7, WL 155. REPAIRED FLOORBEAMS PER SRM. 2L72 4F RTA16WE 20050523002802005052300280NM 2005 5 23 SWAA051316 120050503A53126517582 BULKHEAD BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEB CRACKED AT BS 178 BULKHEAD, RBL 17.1, WL 225. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050523002812005052300281NM 2005 5 23 SWAA051317 120050503A53306545765 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 12R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050523002932005052300293EA 2005 5 23 COMA0560291 120050503A5320 WEB CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01708CA 7235 FS 280.00 WEB CRACKED AT LOWER 2 RIVETS O/B OF RBL 9. REPAIRED IAW REO 601R-53-11-171. 2L72 4F RTA21EA 20050523003002005052300300NE 2005 5 23 QXEA200500837 220050503A7530 VALVE DHAV DHC8 DHC8202 2809007NM PWA PW120 PW126A NE NR 1 STICKING A QXEAK NONE BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 NM09352PH 494 PCEAG0040 PDX - AFTER TAKEOFF WITH BLEEDS ON AND HEAT IN A WARM SETTING, COULD SMELL ODOR AND SMOKE DETECTOR IN LAVATORY WENT OFF, FLIGHT ATTENDANT RESET ALARM ONCE, SMOKE DETECTOR CAME BACK ON. TURNED HEAT DOWN, ODOR WENT AWAY AND FLIGHT ATTENDANT RESET AGAIN. MAINTENANCE FOUND NR 1 P2.5 SWITCHING VALVE COCKED UP AND STICKING. REPLACED PER MTC 9723001, REPLACED NR 2 P2.5 SWITCHING VALVE IAW MTC 972301. GROUND RAN BOTH ENGINES ONE BLEED ON, TO MAX HEAT, AT A TIME. NO SMOKE OR SMELL IN CABIN, AND RETURN TO FULL COLD AUTO, SYSTEM CHECKS NORMAL. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E2ONE 20050523003162005052300316EA 2005 5 23 COMA0560293 120050501A5270 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01735CA 7267 FLIGHT 4988 CABIN DOOR CAUTION MESSAGE FOLLOWED BY DOOR WARNING. COULD NOT DUPLICATE. INSPECTED DOOR AND WARNING SYSTEM, NO DEFECTS FOUND. 2L72 4F RTA21EA 20050523003172005052300317EA 2005 5 23 COMA0560294 120050501A2751 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA COCKPIT ACTIVATED A COMAK NONE J WARNING INDICATION UKUNKNOWN 1 SO01797CA 7344 FLIGHT 5605 FLAPS FAIL CAUTION. RESET FLAPS SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20050523003182005052300318GL 2005 5 23 UPS05644391 220050429A7230 COMPRESSOR BOEING767 76734AF 1385212NM GE CF6 CF680C2* GL LT ENGINE STALLED A IPXAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SO01308UP 27761 ON T/O LT ENGINE COMPRESSOR STALLED FELT BY CREW. INDICATORS WERE FLUCTUATING AND A/C HAD LOSS OF POWER FROM LT ENGINE. REMOVED AND REPLACED LEFT ENGINE PER TC 6002 AND TC 6001. 2L72 4F4 FRTA1NM E23EA 20050523003202005052300320WP 2005 5 23 UPS05844410 120050406A53403750257U1 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 ALL L31L SPLICE FITTINGS (3 TOTAL) CRACKED BETWEEN STA 440-520. REMOVED AND REPLACED ALL (3 EA.) SPLICE FITTINGS IAW SRM 51-20-00, 53-2-2 AND 51-1-20D. 2L74 4F RT4A25 20050523003232005052300323NM 2005 5 23 DHL2005740004 120050324A5230 SKIN BOEING727 7272Q9 138448MNM CARGO DOOR DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 MAIN CARGO DOOR INNER SKIN DAMAGED (INTERNAL) AFT SECTION. REMOVED INNER SKIN IAW B727 SRM 51-30-2, LOCATED AND DRILLED INNER SKIN P/N AE727-1-032A-17 PO NR 508028 IAW DWG NR AE727-1-032A LTR "A" 4-28-99 AERONAUTICAL ENGINEER INC. TREATED AND PRIMED HOLES AND AREA IAW B727 SRM 51-10-2, INSTALLED INNER SKIN IAW DWG NR AE727-1-032A LTR "A" 4-28-99 AERONAUTICAL ENGINEERS INC AT MAIN CARGO DOOR INNER SKIN BS 670 (INTERNAL AFT SECTION). 2L73 4F RTA3WE 20050523003252005052300325 2005 5 23 BB05034 420050505A2565284T049813 MODULE BOEING767 767201 1385125NM EMERGENCY ESCAPEFAULTY A USAAK NONE O OTHER ININSP/MAINT 1 EA19650US 23902 PHL - DURING SQUIB TEST, THE NR 2 EMERGENCY ESCAPE SPOILER INDICATION REMAINED EXTINGUISHED. MAINTENANCE REPLACED THE M1136 MODULE AND RELAYS K839 AND K838. 2L72 4F RTA1NM 20050523003262005052300326NM 2005 5 23 DHL2005740006 120050325A5730 SKIN PANEL BOEING727 7272Q9 138448MNM RT WING DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 RT WING LOWER TE PANEL AT WING STA 190 WBL 90 IS DELAMINATED ON UPPER SURFACE, BELOW APU EXHAUST DUCT. REMOVED RT WING LOWER TE PANEL AT WING STA 190 RBL 90 IAW B727 SRM 51-30-2. CUT OUT DELAMINATED AREA OF UPPER SURFACE APPROX 6" BY 8". REMOVED INSERTS AND VAC BAGGED FOR MOISTURE REMOVAL IAW B727 SRM 51-40-20 FIG 31. CUT OUT DAMAGED CORE APPROX 8" BY 1 1/2" FROM DUR-5052-44-3/16-N-.500 PO NR 991139. FABBED REPLACED. SKIN APPROX 6" BY 8" AND EXTERNAL DOUBLER APPROX 9" BY 11" FROM 2024T3 .012 PO NR 900534 IAW B727 SRM 51-30-2 FIG 32. BONDED, TREATED, PRIMED, AND SEALED REP IAW B727 SRM 51-40-20 FIG 32. INSTALLED INSERTS IAW SRM 51-40-11. INSTALLED RT WING LOWER TE PNL AT WING STA 190 WBL90 TO FROM IAW 2L73 4F RTA3WE 20050523003282005052300328NM 2005 5 23 AALA20050295 120050430A3350 LIGHT BOEING737 737823 13844BZNM CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21936AN 29532 DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING ASSEMBLY AT SEATS 13D AND 21D INOPERATIVE. REPLACED AFT SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING ASSEMBLY AT SEATS 13D AND 21D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20050523003312005052300331 2005 5 23 RAIA00504016 420050416A3418C850176 SENSOR JETAIRJETSTMJETSTM4101 1500501EU STALL WARNING MALFUNCTIONED A RAIAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 CE03565HK3491 41082 FLT 5561 - IND - RIGHT STALL WARNING INDICATION. MAINTENANCE REMOVED AND REPLACED RT AOA SENSOR. 2L72 4T RTA41NM 20050523003322005052300332 2005 5 23 RAIA00504017 420050416A3418C850176 SENSOR JETAIRJETSTMJETSTM4101 1500501EU STALL WARNING MALFUNCTIONED A RAIAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 CE03562HK7649 5328 41078 FLT 3654 - RIC - LEFT STALL WARNING INDICATION. MAINTENANCE REMOVED AND REPLACED STALL SENSOR. 2L72 4T RTA41NM 20050523003332005052300333 2005 5 23 RAIA00504018 420050418A34177000700967 ADC JETAIRJETSTMJETSTM4101 1500501EU NR 1 FAILED A RAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03566HK177013010 41084 FLT 5711 - STL - LEFT DADC FAIL. MAINTENANCE REMOVED AND REPLACED NR 1 ADC. 2L72 4T RTA41NM 20050523003352005052300335 2005 5 23 RAIA00504020 420050418A3418103650004 STICK SHAKER JETAIRJETSTMJETSTM4101 1500501EU STALL WARNING INOPERATIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03554HK 41067 FLT 5529 - STL - STICK PUSHER WILL NOT TEST. MAINTENANCE REMOVED AND REPLACED STICK PUSHER ASSY. 2L72 4T RTA41NM 20050523003362005052300336SO 2005 5 23 RAIA00504021 120050419A2120 DUCT EMB 145 EMB145 3260210SO A/C BAY LOOSE A RAIAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CE03801HK 145053 FLT 3607 - RIC - SMOKE IN CABIN. MAINTENANCE RE-SECURED HEAT EXCHANGER DUCT. 2L72 4F RTT00011AT 20050523003372005052300337SO 2005 5 23 RAIA00504022 120050421A2120 SMOKE EMB 145 EMB145LR 3260212SO NR 1 PACK DETECTED A RAIAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CE03849HK 145002 FLT 8077 - SYR - SMOKE IN CABIN WHEN USING PACK. MAINTENANCE INSPECTED, VERIFIED SMOKE COMING FROM NR 1 PACK. DEFERRED NR 1 PACK. CLEARED DMI. TROUBLESHOT NR 1 PACK, NO SMOKE OR ABNORMAL SMELL IN AIRCRAFT. 2L72 4T RTT00011AT 20050523003382005052300338EU 2005 5 23 RAIA00504023 120050421A79331173T0651 SWITCH JETAIRJETSTMJETSTM4101 1500501EU OIL SYSTEM FAILED A RAIAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 CE03572HK17965 41091 FLT 3656 - GSO - RIGHT ENGINE HIGH OIL TEMP. MAINTENANCE REMOVED AND REPLACED OIL OVERTEMP WARNING SWITCH LT 3656 - GSO - RIGHT ENGINE HIGH OIL TEMP. MAINTENANCE REMOVED AND REPLACED OIL OVERTEMP WARNING SWITCH. 2L72 4T RTA41NM 20050523003392005052300339EU 2005 5 23 RAIA00504024 120050422A261351228801 OVERHEAT LOOP JETAIRJETSTMJETSTM4101 1500501EU RIGHT FAULTY A RAIAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 CE03556HK 41073 FLT 5502 - CID - RT OVERHEAT WARNING. MAINTENANCE REMOVED AND REPLACED RT OVERHEAT LOOP ASSY. 2L72 4T RTA41NM 20050523003402005052300340SO 2005 5 23 RAIA00504025 120050423A2120 SMOKE EMB 145 EMB145LR 3260212SO COCKPIT DETECTED A RAIAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE03840HK 145341 POSSIBLE LIGHTNING STRIKE. SMOKE IN COCKPIT FOLLOWING POSSIBLE LIGHTNING. MAINTENANCE DID LIGHTNING STRIKE INSPECTION WITH NO DEFECTS NOTED. OPS CHECKED PACKS, NO SMOKE IN AIRCRAFT. 2L72 4T RTT00011AT 20050523003412005052300341EU 2005 5 23 RAIA00504026 120050425A3297AIR135690 WIRE HARNESS JETAIRJETSTMJETSTM4101 1500501EU RT MLG FAULTY A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03566HK 41084 STL - RT LANDING GEAR LIGHT FAILED TO EXTINGUISH AFTER TAKEOFF. MAINTENANCE REMOVED AND REPLACED RT PRIMARY DOWNLOCK HARNESS. 2L72 4T RTA41NM 20050523003422005052300342SO 2005 5 23 RAIA00504027 120050425A27503631001007 CONTROL UNIT EMB 145 EMB145 3260210SO T/E FLAP FAILED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03820HK3694 145064 STL - FLAP FAIL INDICATION. MAINTENANCE REMOVED AND REPLACED FLAP CONTROL UNIT. 2L72 4F RTT00011AT 20050523003432005052300343SO 2005 5 23 RAIA00504028 120050428A361014521182403 DUCT EMB 145 EMB145LR 3260212SO BLEED AIR SYS LEAKING A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03818HK 145059 STL - BLEED 1 LEAK INDICATION. MAINTENANCE REMOVED AND REPLACED DUCT ASSEMBLY, NR 1 ENGINE BLEED LINE. 2L72 4T RTT00011AT 20050523003452005052300345NM 2005 5 23 SWAA051325 120050504A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 663.75, STR 10R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050523003462005052300346NM 2005 5 23 SWAA051326 120050504A53116546525 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050523003482005052300348NM 2005 5 23 SWAA051329 120050504A3350101073 LENS BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2L72 4F RTA16WE 20050523003502005052300350NM 2005 5 23 SWAA051331 120050504A3310695517967 MODULE BOEING737 7373H4 1384600NM COCKPIT FAULTY A SWAAC ABORTED TAKEOFF O OTHER TXTAXI/GRND HDL 1 SW29630WN 27705 ABORTED TAKEOFF. MULTIPLE LIGHTS ILLUMINATED AT COCKPIT FWD INSTRUMENT PANEL. REMOVED AND REPLACED LT SIDE LIGHT DIMMING MODULE PER MM. 2L72 4F RTA16WE 20050523003522005052300352 2005 5 23 SWAA051333 420050504A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29783SW 29809 DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050523003532005052300353NM 2005 5 23 SWAA051319 120050504A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050523003542005052300354NM 2005 5 23 SWAA051320 120050504A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 578, STR 11R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050523003562005052300356NM 2005 5 23 SWAA051322 120050504A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050523003572005052300357NM 2005 5 23 SWAA051323 120050504A53116546526 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R TO STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050523003582005052300358NM 2005 5 23 SWAA051324 120050504A53116558280 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050523003602005052300360 2005 5 23 AWXA200500538 420050505A344146502003030314 IRU AIRBUSA319 A319132 3930340NM NR 2 MALFUNCTIONED A AWXAA UNSCHED LANDING JG WARNING INDICATION MULTIPLE FAILURE CRCRUISE 1 WP28814AW3901 1230 1281 EN ROUTE, AFTER REACHING CRUISE ALTITUDE RECEIVED ECAM MESSAGE ADR 1 FAULT FOLLOWED BY NR 1 IR FAILURE. APPROXIMATELY 2 HRS 45 MINUTES LATER AUTOPILOT, AUTO THROTTLES, AND FLIGHT DIRECTORS DISCONNECTED AND WOULD NOT RE-ENGAGE, NR 2 IR FAULT INDICATED ON ADIRU STATUS AND CENTRALIZED FAULT DISPLAY SYSTEM. DIVERTED INTO PHX FOR REPAIR. MAINTENANCE REMOVED AND REPLACED THE NR 1 AND NR 2 ADIRU'S IAW T/C R2A34304, OPERATIONAL CHECK WAS GOOD. VENDOR CONFIRMED REASON FOR REMOVAL ON THE NO. 1 ADIRU, SN 3138, FAULT WAS ISOLATED TO SENSOR ELECTRONICS ASSEMBLY AS PRIMARY ROOT CAUSE AND WAS A CONFIRMED FAILURE. GYROS WERE A SECONDARY FAULT ON UNIT. UNIT WAS REPAIRED IAW AT261847-01 CMM TP1011 REV 24. 2L72 4F RTA28NM 20050523003622005052300362EA 2005 5 23 SWIA200514951 120050424A5320 STRUCTURE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07418SW 7446 RIGHT ELECTRICAL BAY FLOOR AT FS 193, RBL 30 IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. CRACK REPAIRED IAW CRJ REO 601R-53-11-245 REV "A". 2L72 4F RTA21EA 20050523003632005052300363EA 2005 5 23 SWIA200514952 120050424A2721 CONTROL CABLE CNDAIRCL600 CL6002B19 1900309EA PITCH DISCONNECTTIGHT A SWIAO OTHER F FLT CONT AFFECTED ININSP/MAINT 1 NM07418SW 7446 PITCH DISCONNECT HANDLE CABLE IS TIGHT. ITEM FOUND AT C-CHECK INSPECTION. PITCH, ELEVATOR DISCONNECT SYSTEM RIGGED IAW CRJ MM 27-32-00-830-801. 2L72 4F RTA21EA 20050523003642005052300364EA 2005 5 23 SWIA200514953 120050424A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07418SW 7446 FUSELAGE FS 280.00 RBL 9.0 LOWER FLANGE CRACKED ON TRANSVERSE BEAM. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FS 280, FBL 9, LOWER FLANGE ON TRANSVERSE BEAM IAW CRJ REO 601R-53-11-171 REV B. 2L72 4F RTA21EA 20050523003662005052300366EA 2005 5 23 SWIA200514955 120050424A5320 FLANGE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07418SW 7446 FUSELAGE STA 409.00 PLUS 128, LBL 27.0 INBOARD FLANGE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED CRACKED FLANGE IAW CRJ REO 601R-53-41-056 REV "C". 2L72 4F RTA21EA 20050523003682005052300368EA 2005 5 23 SWIA200514957 120050424A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07418SW 7446 AFT EQUIPMENT COMPARTMENT INTERCOSTAL CLIP IS CRACKED FS 625.00 STR 14R. ITEM FOUND AT C-CHECK INSPECTION. CLIP REPLACED IAW CRJ REO 601R-53-61-100 REV "NC". 2L72 4F RTA21EA 20050523003692005052300369SO 2005 5 23 SWIA200514958 120050503A2611 BATTERY EMB 120 EMB120ER 3260203SO SMOKE DETECTOR DISCHARGED A SWIAK NONE O OTHER NRNOT REPORTED 1 NM07197SW 120186 LAV SMOKE DETECTOR BEEPING INTERMITTENTLY. REPLACED BATTERY. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050523003722005052300372EA 2005 5 23 SWIA200514961 120050503A2721 CONTROL PANEL CNDAIRCL600 CL6002C10 1390015EA RUDDER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07716SK 10180 RUDDER TRIM WILL NOT MOVE LEFT MANUALLY. REPLACED AILERON/RUDDER TRIM CONTROL PANEL IAW CRJ MM 27-12-10. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050523003732005052300373EA 2005 5 23 SWIA200514962 120050501A2711 TRIM SWITCH CNDAIRCL600 CL6002C10 1390015EA COCKPIT STUCK A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07732SK 10194 AILERON TRIM ROLLED UNCOMMANDED TO LEFT DURING PREFLIGHT CHECK. REPLACED AILERON TRIM SWITCH. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050523003792005052300379EU 2005 5 23 ASOA05283 120050311A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27635AS 372 DURING A C-CHECK IN YUL, THE RIGHT OUTBOARD SEAT TRACK BETWEEN FRAME 33/36 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT OUTBOARD SEAT TRACK BETWEEN FRAME 33/36 IAW SRM 51-25-04. (M) 2H72 4T RTA53EU 20050523003812005052300381EA 2005 5 23 ASOA05273 120050330A5210BLC5BC11SFL18C4 CABLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR UNSECURE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27824AS 7203 FLT 4610 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WAS FOUND DIFFICULT TO OPEN. MAINTENANCE FOUND THE PASSENGER DOOR HANDRAIL PIN CABLE UNSECURED CAUSING IT TO STICK BETWEEN THE PASSENGER DOOR AND AIRFRAME. MAINTENANCE RESECURED THE PASSENGER DOOR HANDRAIL PIN CABLE. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050523003822005052300382EU 2005 5 23 ASOA05280 120050311A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27635AS 372 DURING A C-CHECK IN YUL, THE LEFT SEAT TRACK BETWEEN FRAME 39 AND 41 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT SEAT TRACK BETWEEN FRAME 39 AND 41 IAW SRM 51-25-01 AND 51-25-04. (M) 2H72 4T RTA53EU 20050523003832005052300383EU 2005 5 23 ASOA05282 120050311A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27635AS 372 DURING A C-CHECK IN YUL, THE LEFT AND RIGHT SEAT TRACKS BETWEEN FRAME 36 AND 39 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT SEAT TRACKS BETWEEN FRAME 36/39 IAW SRM 51-25-04. (M) 2H72 4T RTA53EU 20050523003872005052300387EA 2005 5 23 ASOA05279 120050401A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27820AS 7188 DURING A C-CHECK IN MCN, THE LOWER WING PLANK AT WS 148.019 LEFT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LOWER WING PLANK AT WS 148.019 LEFT IAW ASA EO 600-57-0134A. (M) 2L72 4F RTA21EA 20050523003882005052300388EA 2005 5 23 ASOA05266 120050325A5260601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27883AS 7504 DURING AN A-CHECK IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20050523003892005052300389NM 2005 5 23 USAA050463 120050405A5320 ANGLE BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19440US39307 24811 CLT - FOUND ANGLE CRACKED 1 INCH, STATION 290-291, STRINGER 11R. REPLACED ANGLE IAW SRM 51-10-02, 51-40-02. (M) 2L72 4F RTA16WE 20050523003902005052300390EA 2005 5 23 ASOA05278 120050401A5260601R319805 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27820AS 7188 DURING A C-CHECK IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE BOTTOM STEP ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20050523003932005052300393NM 2005 5 23 USAA050464 120050402A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US56390 22956 PIT - FOUND SKIN CRACKED 1.5 INCH LONG, BS 747 BETWEEN 19L AND 20L. INSTALLED DOUBLER SKIN REPAIR PER EA 83173, SRM 53-00-01. (M) 2L72 4F RTA16WE 20050523003982005052300398NM 2005 5 23 USAA050458 120050401A5320 ANGLE BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19440US39307 24811 CLT - FOUND Z-ANGLE CORRODED .20 INCH BY 2 INCH, RIGHT AFT SERVICE DOOR Z-ANGLE. INSTALLED NEW Z-ANGLE IAW SRM 51-10-02. (M) 2L72 4F RTA16WE 20050523004002005052300400EU 2005 5 23 ASOA05287 120050311A5320 DOUBLER AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27635AS 372 DURING A C-CHECK IN YUL, THE DOUBLER ON THE FORWARD SIDE OF FRAME 39, STRINGER 14R WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE DOUBLER ON THE FORWARD SIDE OF FRAME 39, STRINGER 14R IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20050523004012005052300401NM 2005 5 23 USAA050453 120050403A5320 TIE CLIP BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19440US39307 24811 CLT - FOUND TIE CLIP CRACKED .3 INCH, STATION 662 STRINGER 10L. REPLACED CLIP IAW SRM 51-40-03. (M) 2L72 4F RTA16WE 20050523004022005052300402NM 2005 5 23 USAA050454 120050402A5320 ANGLE BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19440US 24811 CLT - FOUND ANGLE CORRODED 1.5 INCH BY 4.3 INCH, LEFT AFT SERVICE DOOR Z-ANGLE. INSTALLED FILLER AND DOUBLER IAW SRM 51-70-11. (M) 2L72 4F RTA16WE 20050523004042005052300404NM 2005 5 23 USAA050450 120050401A5315 FLOORBEAM BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19440US39307 24811 CLT - FOUND FLOORBEAM CORRODED .5 INCH, STATION 328 RBL 11. INSTALLED REPAIR DOUBLERS IAW SRM 51-10-51. (M) 2L72 4F RTA16WE 20050523004062005052300406NM 2005 5 23 USAA050455 120050402A5320 STIFFENER BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19440US39307 24811 CLT - FOUND STIFFENER CRACKED 1.3 INCHES, STATION 328, RBL 31. FABRICATED AND INSTALLED NEW STIFFENER IAW SRM 51-10-02 AND DRAWING NR 65-45812. (M) 2L72 4F RTA16WE 20050523004072005052300407NM 2005 5 23 USAA050452 120050402A5311 FRAME BOEING737 7373B7 1384580NM FUSELAGE BROKEN A USAAK NONE O OTHER ININSP/MAINT 1 EA19394US53522 23316 CLT - FOUND FORMER BROKEN, STATION 535 WL 165, LBL 60. REPLACED FORMER. (M) 2L72 4F RTA16WE 20050523004082005052300408EU 2005 5 23 ASOA05290 120050315A5320 FLOOR SUPPORT AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27635AS 372 DURING A C-CHECK IN YUL, THE RIGHT FLOOR SUPPORT BETWEEN FRAME 38 AND 39 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIHT FLOOR SUPPORT BETWEEN FRAME 38 AND 39 IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20050523004092005052300409EA 2005 5 23 ASOA05291 120050402A33506100976 LIGHT CNDAIRCL600 CL6002C10 1390015EA CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27719EV 10099 DURING A GROUND INSPECTION IN SLC, THE EMERGENCY CEILING FLOODLIGHT AT ROW 17 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY CEILING FLOOD LIGHT AT ROW 17. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050523004112005052300411NM 2005 5 23 USAA050456 120050402A5320 GUSSET BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19440US39307 24811 CLT - FOUND GUSSET CRACKED 2.6 INCHES, STATION 312, RBL 31. FABRICATED AND INSTALLED NEW GUSSEIT IAW SRM 53-10-51, 51-20-01. (M) 2L72 4F RTA16WE 20050523004122005052300412NM 2005 5 23 USAA050459 120050401A5320 TIE CLIP BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19440US39307 24811 CLT - FOUND TIE CLIP CRACKED .375 INCH, STATION 663 STRINGER 14R. REPLACED CLIP IAW SRM 51-40-02. (M) 2L72 4F RTA16WE 20050523004142005052300414EA 2005 5 23 ASOA05263 120050323A3350 BATTERY CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN DISCHARGED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27855AS 7395 DURING A GROUND INSPECTION IN ATL, THE EMERGENCY LIGHTS CAME ON WITH THE SWITCH IN THE OFF AND ARMED POSITIONS. MAINTENANCE FOUND CIRCUIT BREAKER P4-C2 POPPED AND THE EMERGENCY LIGHTS BATTERY PACKS LOW RESULTING FROM BOTH MAIN AND AUXILIARY POWER UNIT BATTERIES BEING DISCONNECTED WITH THE SWITCH IN THE ARMED POSITION. MAINTENANCE RESET CIRCUIT BREAKER P4-C2 AND ALSO RECHARGED THE BATTERY PACKS. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F4 FRTA21EA E15NE 20050523004192005052300419EA 2005 5 23 ASOA05339 120050415A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27821AS 7194 DURING A C-CHECK IN MCN, THE FS 280 FRAME AT APPROXIMATELY LBL 11 AND RBL 11 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FS 280 FRAME AT APPROXIMATELY LBL 11 AND RBL 11 IAW ASA EO 600-53-0123. (M) 2L72 4F RTA21EA 20050523004202005052300420EA 2005 5 23 ASOA05338 120050415A5347601R3877913 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27821AS 7194 DURING A C-CHECK IN MCN, THE SEAT TRACK AT FS 559 PLUS 78 TO PLUS 88, RBL 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE SEAT TRACK AT FS 559 PLUS 78 TO PLUS 88, RBL 9. (M) 2L72 4F RTA21EA 20050524000012005052400001WP 2005 5 24 AALA20050293 120050429A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21417AA 49328 BOS - LOW BATTERY IN EXIT EMERGENCY LIGHT AT CENTER AFT DOOR. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHT AT CENTER AFT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050524000022005052400002WP 2005 5 24 AALA20050294 120050429A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21276AA 49273 LAX - CEILING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACKS AT B5104 AND B51-6 FOR CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050524000052005052400005NM 2005 5 24 AALA20050297 120050501A3350D71702001 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21762AN 31479 JFK - SEAT EMERGENCY LIGHTS IN ZONE 3 INOPERATIVE. REPLACED BATTERY PACK AT M33404 BY DOOR 3R FOR SEAT EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20050524000062005052400006SO 2005 5 24 LR7A05042 120050429A5280373554 DOOR LKHEED382 382G 526414USO NLG DAMAGED A LR7AO OTHER O OTHER CLCLIMB 1 AL03401LC 4606 FORWARD NLG DOOR DAMAGED BY BIRD STRIKE ON DEPARTURE FROM PABE. AIRCRAFT CONTINUED TO PANC AND LANDED WITHOUT INCIDENT. REPLACED FWD NLG DOOR AND RIGGED IAW MM SMP 581 32-20. RETRACTION TEST AND EMERGENCY EXTENSION CHECK GOOD, LP 17227, ITEM 1. 2H74 4T A1SO 20050524000122005052400012EU 2005 5 24 ASOA05286 120050311A5315 FLOORBEAM AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27635AS 372 DURING A C-CHECK IN YUL, THE FLOORBEAM AT FRAME 36, STRINGER 14 L/R WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM AT FRAME 36, STRINGER 14 L/R, IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20050524000132005052400013NM 2005 5 24 DHL2005783521 120050404A5753 SKIN BOEING727 727227 1384078NM RT WING FOREFLAPGOUGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01783DH 21999 RT WING INBD FOREFLAP LE IS GOUGED AT OB END WBL 240. REMOVED EXISTING DOUBLER REPAIR IAW B727 SRM 51-30-2 FABRICATED DOUBLER USING 2024T3 .063 PO NR 9002149 DIM. 4 1/2" BY 4 1/2" IAW B727 SRM 57-50-2 AND 57-50-4 FIG 1. ALODINE AND PRIMED DOUBLER AND AREA IAW B727 SRM 51-10-2. INSTALLED DOUBLER IAW B727 SRM 51-30-2 AND 57-50-4 FIG 1. 2L73 4F A3WE 20050524000222005052400022EU 2005 5 24 2005UALA00386 120050422A2133902315703 OUTFLOW VALVE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CABIN PRESSURE FAULTY A UALAGA O2 MASK DEPLOYED UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29434UA31077 592 UNABLE TO CONTROL CABIN PRESSURE IN AUTO OR MANUAL MODE. OXYGEN MASKS MANUALLY DEPLOYED. CABIN PRESSURE SYSTEM 1 AND 2 WARNING WITH ASSOCIATED FAULT OF THE OUTFLOW VALVE. REPLACED THE OUTLFOW VALVE 10HL. 2L72 4F4 FRTA28NM E40NE 20050524000302005052400030SO 2005 5 24 TZR2005F00015 220050427A8530AEC520TI CYLINDER CESSNA402 402B 207590PCE CONT O520 TSIO520E 17040SO MCAULY3AF32C3AF32C* GL ENGINE CRACKED E TZRAK NONE O OTHER ININSP/MAINT 1 SW05404TE1063 402B0834 CRACK RUNS FROM THE SPARK PLUG BASE TO THE EXHAUST VALVE. THIS IS TYPICAL OF MOST CRACKS FOUND IN ECI CYLINDERS. TO DATE, FROM FIRST OF YEAR FOR THIS COMPANY, WE HAVE HAD 10 CRACKED CYLINDERS IN 1800 HOURS OF FLYING. IT IS RECOMMENDED THAT ANY AC OWNER OPERATING WITH ECI CYLINDERS INSTALLED ON THEIR ENGINES, PERFORM A COMPRESSION CHECK EACH 50 HOURS. IT IS FURTHER RECOMMENDED THAT DURING THE COMPRESSION CHECK THAT SOAP SOLUTION BE APPLIED TO THE OUTER PORTION OF CYLINDER IN FIN AREA TO CHECK FOR CRACKS. THIS SHOP HAS FOUND CYLINDER WITH GOOD COMPRESSION AND STILL HAVE CRACK IN CYLINDER FIN AREA. (SW05200507954) (K) 1L72 3O3 O A7CE E8CE 5 CP22EA 20050524000332005052400033SO 2005 5 24 TZR2005F00018 220050405A8530AEC520TI01 CYLINDER CESSNA401 401 207590CCE CONT O520 TSIO520EB 17040SO NR 5 CRACKED E TZRAK NONE O OTHER ININSP/MAINT 1 SW05405TE 4010121 275439R CRACKED FROM INJECTOR TOWARD SPARK PLUG, ECI CYLINDER. (SW05200507951) (K) 1L72 3O3 O A7CE E8CE 20050524000342005052400034SO 2005 5 24 TZR2005F00019 220050415A8530AEC520TI01 CYLINDER CESSNA401 401 207590CCE CONT O520 TSIO520C 17040SO LT ENG, NR 2 CRACKED E TZRAK NONE O OTHER ININSP/MAINT 1 SW05403TE1339 4010008 182946R CYLINDER CRACKED FROM EXHAUST VALVE TO TOP SPARK PLUG PORT. ECI CYLINDER. (SW05200507952) (K) 1L72 3O3 O A7CE E8CE 20050524000352005052400035NM 2005 5 24 P5CA0501348 120050501A29101032003 VALVE BOEING747 747341 13848AMNM GE CF6 CF650E2 30018NE HYD SYSTEM LEAKING A P5CAK NONE K FLUID LOSS ININSP/MAINT 1 EA15355MC 23395 530278 NR 2 ENGINE HYDRAULIC SUPPLY C/B POP’S. REPLACED SUPPLY VALVE, OPS AND LEAK CHECK OK PER MM 29-11-04. 2L74 4F4 FRTA20WE E23EA 20050524000362005052400036EU 2005 5 24 BAQ2005F00001 120050403A7921109045501101 FAN AGUSTAA109 A109E 0260119EU OIL COOLER FAILED E BAQAEA ENGINE SHUTDOWN UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 EA0312UW 2216 11074 DURING TAKEOFF, NR1 ENG OIL HOT LIGHT ILLUMINATED. OIL TEMP WAS 125 DECREES C. PILOT REDUCED POWER AND INITIATED A RETURNE TO HOSPITAL. ENG NR1 OIL TEMP AND PRESSURE CONTINUED TO RISE. PILOT DECLARED AN EMERGENCY WITH TOWER AND DIVERTED FOR A PRECAUTIONARY LANDING. ENROUTE, ENG NR 1, OIL TEMP, AND PRESSURE INCREASED TO MAX LIMITS. PILOT SHUTDOWN NR1 END. AC LANDED WITHOUT FURTHER INCIDENT. AC WAS GROUNDED. POST FLIGHT INSP REVEALED ENG NR 1 OIL COOLER FAN DRIVESHAFT BEARING FAILED. (EA03200503947) (K) 1G72 3U RTH7EU 20050524000432005052400043NM 2005 5 24 PCSA5030501 120050503A2612100012703 CDU BOEING727 727233 138408ANM AFT CARGO SHORTED A PCSAJA DUMP FUEL UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO29495AJ 20937 FLIGHT 711 MIA TO MEX, DURING CRUISE LOWER CARGO FIRE LIGHT AND BELL CAME ON INDICATING A AFT FIRE. FUEL WAS DUMPED, AIRCRAFT DIVERTED TO MID AND LANDED WITH NO FURTHER INCIDENT. UPON INSPECTION OF THE AFT CARGO COMPARTMENT ON THE GROUND NO FIRE WAS OBSERVED IN THE AFT CARGO. MAINTENANCE FOUND A CDU IN THE AFT CARGO SENDING FALSE FIRE INDICATION TO COCKPIT, CDU EXTERNAL WIRE FOUND GROUNDING, WIRE REPAIRED IAW 20-10-13, SYSTEM OP'S CHECK NORMAL IAW HOLLYNDSED AMMS 26-15-00. AIRCRAFT WAS RETURNED TO SERVICE. 2L73 4F RTA3WE 20050524000452005052400045SO 2005 5 24 SIMA200509403 120050402A3350 BATTERY PACK EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A SIMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW21670AE 145790 PIA - FLT 4102 - ON PREFLIGHT CHECK, THREE EMERGENCY FLOOR LIGHT STRIPS COME ON FOR 3 SECONDS THEN GO OUT. REPLACED EMERGENCY LIGHTING BATTERY PACKS NR 2/3/4 IAW EMB 145 AMM 33-50-04. OPS CHECK GOOD. NR 1 P/N 2013BR S/N B1641 NR 2 2012BR S/N 1560, NR 3 2012BR S/N 1614. (M) 2L72 4T RTT00011AT 20050524000462005052400046SO 2005 5 24 SIMA200510807 120050416A2700 CARTRIDGE EMB 135 EMB135KL 3260302SO GUST LOCK OUT OF ADJUST A SIMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW21810AE 145525 CREW NOTED IN CRUISE, THE GUST LOCK LIGHT CAME ON AND LANDED AT THE NEAREST AIRPORT WITH NO PROBLEMS. ADJUSTED GUST LOCK SPRING CARTIRIDGE MECHANISM. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050524000482005052400048EA 2005 5 24 ASOA05259 120050322A5320601R3117121 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27902EV 7620 DURING A C-CHECK IN MCN, THE FS 484 LEFT/RIGHT INTERCOSTALS, BL 27 TO 36 AND THE RIGHT INBOARD CLIP WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FS 484 LT/RT INTERCOSTALS, BL 27 TO 36 AND REMOVING AND REPLACING THE RIGHT INBOARD CLIP IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20050524000492005052400049EA 2005 5 24 ASOA05258 120050321A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27902EV 7620 DURING A C-CHECK IN MCN, THE ENGINE SUPPORT BEAM AT BL 36.20 LT/RT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE ENGINE SUPPORT BEAM UPPER AT BL 36.20 LT/RT IAW ASA EO 600-53-0073. (M) 2L72 4F RTA21EA 20050524000502005052400050EA 2005 5 24 ASOA05341 120050415A5210601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27847AS 7335 DURING A GROUND INSPECTION IN MDT, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050524000522005052400052EA 2005 5 24 2005F00075 120050304A3297601577889 WIRE HARNESS CNDAIRCL600 CL6002B16 1900305EA NLG PROX SWITCH FAILED A IMJAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA25620HF 5021 ON TAKEOFF, NOSE LANDING GEAR WOULD NOT RETRACT. INVESTIGATION REVEALED A FAILED NOSE GEAR WEIGHT-ON-WHEELS PROXIMITY SWITCH HAD FAILED. THIS SWITCH IS PART OF THE NLG WOW AND OLEO HARNESS ASSEMBLY. (M) 2L72 4F RTA21EA 20050524000542005052400054CE 2005 5 24 VNW2005F00000 120050422A323012269 UNIVERSAL JOINT BEECH 100 100BEECH 1152916CE PWA PT6 PT6A27 52043EA RT WING MLG FAILED E VNWAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO15431R B71 UPON DEPARTURE, CREW NOTICED LANDING GEAR INTRANSIT LIGHT ILLUMINATED. THE CREW FOLLOWING EMERGENCY PROCEDURES IT WAS NOTICED THAT THE RT MLG DOWN AND LOCKED DID NOT INDICATE. FLIGHT CREW USED EMERGENCY EXTENSION AND STILL HAD NO RT MLG DOWN AND LOCKED INDICATION. CREW DECLARED EMERGENCY, LANDED. UPON INSP OF LANDING GEAR SYSTEM, IT WAS FOUND THAT RT MLG JOINT, UNIVERSAL HAD INTERNALLY FAILED, CAUSING THE RT MLG NOT TO RESPOND BY LANDING GEAR HANDLE OR EMERGENCY EXTENSION. (K) 1L72 3T4 T A14CE E4EA 20050524000562005052400056CE 2005 5 24 TIM2005F00005 120050419A261230215 FIRE DETECTOR BEECH 99 99 1154002CE PWA PT6 PT6A60A 52043NE LT ENGINE CONTAMINATED E TIMAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 NM0714MV 40311 U59 FIRE DETECTOR GAVE A FALSE FIRE WARNING IN FLIGHT. MOISTURE WAS PROBABLE CAUSE. AFTER TAXI, THE FIRE WARNING LIGHT EXTINGUISHES. NO OTHER PROBLEMS WITH THE SYSTEM. (K) 1L72 3T4 T A14CE E4EA 20050523001332005052300133NM 2005 5 23 SB05062 120050519A335020121 CHARGER BOEING737 737301 1384611NM EMERGENCY LIGHTSINOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19563AU 23551 CLT - MAINTENANCE REPORTED THE EMERGENCY LIGHTS FOR SEAT ROWS 11 THROUGH 16 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050523001472005052300147CE 2005 5 23 DXTA200500717 120050509A3240MS252531 SWITCH CESSNA500 560CESSNA 2076750CE BRAKES MALFUNCTIONED E DXTAO OTHER O OTHER LDLANDING 1 GL07375QS 5600375 POWER BRAKE LOW PRESS AND ANTISKID INOP ANNUNCIATORS ILLUMINATED AND STAYED ILLUMINATED AFTER LANDING GEAR SELECTED DOWN ON APPROACH. INSTALLED NEW GEAR HANDLE SWITCH *112B* PER CESSNA560 ULTRA MAINTENANCE MANUAL CHAPTER 32-31-01. PERFORMED LANDING GEAR FUNCTIONAL TEST PER CESSNA 560 ULTRA MAINTENANCE MANUAL CHAPTER 32-01-00. LANDING GEAR AND ANTI-SKID PUMP OPERATION TEST SATISFACTORY 2L72 4F RTA22CE 20050523001782005052300178NM 2005 5 23 SWAA051281 120050501A2612 FIRE WARNING BOEING737 7373H4 1384600NM COCKPIT MALFUNCTIONED A SWAAFA ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW29361SW 26572 DECLARED EMERGENCY. THE AFT CARGO FIRE LIGHT ILLUMINATED ALONG WITH FIRE WARNING BELL, 1ST FIRE BOTTLE DISCHARGED AND FIRE LIGHT WENT OUT. SECOND BOTTLE THEN DISCHARGED. FIRE LIGHT STAYED OUT, NO VISIBLE SMOKE, FUMES OR FIRE NOTED IN CABIN OR COCKPIT. INSPECTED AFT CARGO COMPARTMENT, NO EVIDENCE OF FIRE. REMOVED AND REPLACED FIRE BOTTLES PER MM. 2L72 4F RTA16WE 20050523001812005052300181NM 2005 5 23 SWAA051284 120050429A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 500D, STR 19L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050523001832005052300183NM 2005 5 23 SWAA051286 120050501A3350101073 COVER BOEING737 7373H4 1384600NM CABIN OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29627SW 27935 DURING SCHEDULED RON CHECK, FWD ENTRY EMERGENCY LIGHT COVER FELL OFF. INSTALLED COVER PER MM. 2L72 4F RTA16WE 20050523001862005052300186NM 2005 5 23 SWAA051289 120050430A53306545765 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29683SW 24008 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 517, STR 12L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050523002172005052300217CE 2005 5 23 DXTA200500703 120050429A33506013211 BATTERY PACK RAYTHNDH125 HAWKER800XP 7150012CE EMERGENCY LIGHT WEAK E DXTAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07816QS 258416 CABIN EMERGENCY LIGHTING SYSTEM INOP. SYSTEM DOES NOT OPERATE WHEN S/W MOVED FROM 'ARM' TO 'MANUAL' AND ONLY OPERATES FOR 3 SEC WHEN S/W IS MOVED TO 'MANUAL' FROM 'OFF' POSITION. TROUBLESHOT SYSTEM, DETERMINED FORWARD AND AFT POWER SUPPLY LOW, DEPLETED AND CHARGED FORE AND AFT POWER SUPPLIES IAW HAWKER 800XP MM 24-30-15 PAGE 201, ACCESSED AND VERIFIED CHARGING CIRCUIT FOR BATTS WITHOUT DEFECT PERFORMED SATISFACTORY GOOD AND CHECK PER H800XPMM33-50-00 PA 501. 2L72 4F RTA3EU 20050523002222005052300222CE 2005 5 23 DXTA200500706 120050501A3240 BRAKE CESSNA500 560CESSNA 2076750CE RIGHT MALFUNCTIONED E DXTAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07810QS 5600625 RIGHT BRAKE CATCHES BEFORE LEFT BRAKE WHEN APPLYING EVEN PRESSURE ON LANDING CAUSING IT TO VERGE TO THE RIGHT. WITH EACH APPLICATION OF BRAKE, CREW HEARD AN "AIR" NOISE THAT IS NOT NORMALLY HEARD. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20050523002242005052300224CE 2005 5 23 DXTA200500705 120050430A2710 AILERON CESSNA750 750 2076810CE STUCK E DXTAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 GL07910QS 7500110 HAD A "CATCH" IN THE ROLL CONTROL TURNING TO THE RIGHT, CONTROLS HEAVIER AFTER OR BEYOND THE CATCH. INSPECTED AILERON ROLL SPOILER SYSTEM BETWEEN CONTROL YOKES AND PCU'S. NO DEFECT NOTED. PERFORMED AILERON AND AILERON/SPOILER DISCONNECT CHECK IAW 750 MM, 27-10-00. ALL CHECKS WERE GOOD. 2L72 4J RTT00007WI 20050523002282005052300228GL 2005 5 23 CHQA200500091 220050428A7200 ENGINE EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL NR 1 FAILED A CHQAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL11373SK103504690 145543 CAE611677 FLIGHT 5319 EWR-STL - ON INITIAL CLIMB-OUT OF EWR, LAV SMOKE ALARM WENT OFF. THE FLIGHT ATTENDANT STATED, HAZE IN THE CABIN AND SMELLED SMOKE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO FIELD IN EWR. MAINTENANCE TROUBLESHOT THE SMELL DOWN TO THE NR 1 BLEED SYSTEM AND THE AIRCRAFT WAS FERRIED TO CMH. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE. OPS CHECK AND LEAK CHECK GOOD. NO SMELL NOTED IN CABIN IAW EMB J/C CE720001. 2L72 4F4 FRTT00011ATTE6CH 20050523002502005052300250NM 2005 5 23 AWXA200500366 120050326A3510 SCREW BOEING737 7373S3 1384711NM OXYGEN MASK FAULTY A AWXAO OTHER O OTHER DEDESCENT 1 WP28316AW 06091 23713 ABQ - EMERGENCY EQUIPMENT FAILURE - FLT 0757 - DURING DESCENT INTO ABQ FOR CAPTAINS WINDSHIELD FAILURE WITH CREW OXYGEN MASKS DONNED, THE CAPTAINS MASK BECAME FOGGED UP. WHEN EMERGENCY POSITION WAS SELECTED ON THE MASK AIRFLOW AND ABILITY TO SPEAK WERE INHIBITED. MAINTENANCE REMOVED AND REPLACED CAPTAINS OXYGEN MASK IAW T/C R1B35001, FUNCTIONAL TEST WAS GOOD. VENDORS TEST OF FULL FACE MASK S/N 06091, CONFIRMED REASON FOR REMOVAL FOR INOPERATIVE HOSE SWIVEL SCREW. REPLACED MASK, HOSE SWIVEL SCREW, AND O-RINGS, FINAL TEST WAS GOOD IAW CMM 35-10-60. 2L72 4F RTA16WE 20050523002582005052300258NM 2005 5 23 SWAA051300 120050428A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 944, STR 24L. MX FERRY TO DALLAS. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050523002602005052300260NM 2005 5 23 SWAA051302 120050503A53306545766 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED C3 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS AT BS 430 TO BS 450, NR 3 & NR 4 RADIO ALTIMETER ANTENNA'S CUT OUTS. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050523002792005052300279NM 2005 5 23 SWAA051315 120050503A25606557463 LATCH BOEING737 7373H4 1384600NM L1 DOOR INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29626SW 27702 L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT FLOOR LATCH SPRING INOP. REMOVED AND REPLACED LATCH ASSY PER MM. 2L72 4F RTA16WE 20050523002832005052300283EA 2005 5 23 COMA0560288 120050503A5712 RIB CNDAIRCL600 CL6002B19 1900309EA RT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01708CA 7235 CRACK FOUND TO BATT RIB ASSEMBLY AT WS 53.60. REPAIRED IAW REO 601R-57-51-046. 2L72 4F RTA21EA 20050523002862005052300286NE 2005 5 23 ASMF200504024 220050430A7200 ENGINE DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE RIGHT MALFUNCTIONED W ASMFD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SW23803ML 49726 716784 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF CAPTAIN REPORTED DID NOT HAVE ACCELERATION IN RIGHT ENGINE. DURING CHECK BOTH ENGINES WERE DETECTED STABILIZED AT 52 PERCENT OF N2, TESTS WERE CORRECT. AIRCRAFT WAS SENT TO THE HANGAR AND TRIM TO BOTH ENGINES WAS PERFORMED IAW MM 71-00-00, TESTED CORRECT. 2L72 4F4 FRTA6WE E9NE 20050523002912005052300291EU 2005 5 23 HE66100341 120050417A5412105623134 FIREWALL BOLKMS105 BO105LSA1 5626021EU ALLSN 250C 250C28 03013GL NACELLE CRACKED B HEERO OTHER O OTHER NRNOT REPORTED 1 SW03202LF 2014 FIREWALL IS CRACKED BY FASTNERS AND HAS BEEN REPAIRED SEVERAL TIMES BEFORE. INTEGRITY IS COMPROMISED AND DO NOT WANT ENGINE TO INGEST FOD. 1G72 3U3 U H3AU E1GL 20050523002942005052300294NM 2005 5 23 UPS05444392 120050411A5311 FRAME BOEING747 747283B 1384867NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 BS 520 FRAME S11L STR CUTOUT CRACKED, CRACK LENGTH ON FRAME CHORD 1.12 INCH, ON FRAME AND DOUBLER 0.43 INCH, DOUBLER 0.56 INCH ). U/DECK BS 520 FRAME REPAIRED AT BETWEEN STR 10L/10AL TO STR 12L AREA AS PER RS R-53-12-35296 AND UPS EO B747-5310-22103-A. 2L74 4F A20WE 20050523002972005052300297NM 2005 5 23 UPS05444394 120050409A5311 FRAME BOEING747 747283B 1384867NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 BS 200 S13AL TO S14L FRAME FOUND CRACKED, CRACK LENGTH .750 INCH. M/DECK BS 200 BETWEEN STR 13AL TO STR 14AL FRAME REPAIRED AS PER HX RS R-53-12-35289 AND UPS EO NR B747-5310-22089-A. 2L74 4F A20WE 20050523002992005052300299NM 2005 5 23 UPS05444396 120050411A5311 FRAME BOEING747 747283B 1384867NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 BS 460 FRAME STR -11L STR CUTOUT CRACKED, CRACK LENGTH 1.38 INCH. FRAME WEB REPAIRED AS PER HX RS NR R53-12-35293 AND UPS EO NR B747-5310-22102-A 2L74 4F A20WE 20050523003022005052300302NM 2005 5 23 UPS05444398 120050412A5311 FRAME BOEING747 747283B 1384867NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 COCKPIT BS 360 FRAME STR 2R WEB CRACKED, CRACK LENGTH 9/16". COCKPIT BS 360 FRAME WEB REPAIRED AT BETWEEN STR 1R AND 2R AREA AS PER HX RS R53-12-35290 AND UPS EO NR B747-5310-22086A, REFER NRC 6590 FOR WORK DETAIL. 2L74 4F A20WE 20050523003052005052300305NM 2005 5 23 UPS05444401 120050411A5313 STRINGER BOEING747 747283B 1384867NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 BS 1478-1480 STR 6R STRINGER END FOUND CRACK. CRACK LENGTH 1.5 INCH. M/DECK BS 1478-1480 STR 6R STRINGER END REPAIRED AS PER RS R-53-41-35294 AND UPS EA ENGINEERING FILE NR 747-53-20244. 2L74 4F A20WE 20050523003192005052300319WP 2005 5 23 UPS05844376 120050412A5321 FLOORBOARD DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 MAIN CABIN , CORROSION ON FLOORBOARD STA 1560,1600 AND 1660, LBL35. REMOVED CORROSION FOUND OUT OF LIMITS, INSTALLED REPAIR DOUBLERS IAW 51-1-8, 53-02-00, 53-02-03 FIG 10 AND 51-1-21. 2L74 4F RT4A25 20050523003222005052300322WP 2005 5 23 UPS05844411 120050405A5340 ATTACH ANGLE DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 HAT CHANNEL ATTACH ANGLE O/B SIDE CORRODED STA 920-940 RBL 58 RT W/W. REPAIRED BY REPLACEMENT OF I/B AND O/B HAT CHANNEL ATTACH ANGLES, WEB AND FINGER DOUBLER, REPAIR SPLICES. REPLACEMENT RETAINER AND REPLACEMENT PRESSURE PANEL ANGLE, IAW 51-1-21, 53-2-0, 51-3-0, 51-3-2 AND 51-1 -20D. 2L74 4F RT4A25 20050523003472005052300347NM 2005 5 23 SWAA051327 120050504A531165C25229 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050523003492005052300349NM 2005 5 23 SWAA051330 120050504A3150FCC4008 RELAY BOEING737 7373H4 1384600NM COCKPIT FAULTY A SWAAA UNSCHED LANDING O OTHER CLCLIMB 1 SW29630WN 27705 AIR TURNBACK. ANNUNCIATOR LIGHTS ILLUMINATED ON FWD INSTRUMENT PANEL & INDICATOR LIGHTS ON FMC STAYED ILLUMINATED. ALL LIGHTS CEASED UPON LANDING. REMOVED AND REPLACED MASTER TEST RELAY-R33 PER MM. 2L72 4F RTA16WE 20050523003552005052300355NM 2005 5 23 SWAA051321 120050504A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 685, STR 11L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050523003592005052300359NM 2005 5 23 AWXA200500537 120050504A27512061141 INDICATOR BOEING737 7373Y0 1384671NM T/E FLAP FAULTY A AWXAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 WP28323AW9356 4016 23684 ON APPROACH, T/E FLAPS WOULD NOT EXTEND PAST 8 DEGREES, L/E FLAP INTRANSIT LIGHT REMAINED ILLUMINATED. MX R & R THE T/E FLAP POSITION INDICATOR IAW 27-58-41. DURING OPS CHECK A LOUD POPPING SOUND OBSERVED COMING FROM NR 3 SLAT AREA. MX FOUND THE NR 3 SLAT OUTBOARD AUX TRACK DETENT ROCKER ARM NOT CENTERED ON THE DETENT ARM AFT TENSION ROD. ADJUSTED FORWARD CLEARANCE IAW AMM 27-81-00, OPS CK OF FLAP SYS GOOD. FUNCTIONAL TEST OF FLAP POSITION INDICATOR SN 3498 CONFIRMED REASON FOR REMOVAL. FINDING UNIT WAS OUT OF CALIBRATION. CLEANED AND LUBRICATED LEFT AND RIGHT SYNCHRO BEARING, RECALIBRATED UNIT AND RE-ACCOMPLISHED FUNCTIONAL TEST IAW CMM 27-50-03. REV. 2. 2L72 4F RTA16WE 20050523003612005052300361SO 2005 5 23 SWIA200514950 120050428A5270 SWITCH EMB 120 EMB120ER 3260203SO PAX DOOR BROKEN A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07301YV 120301 PAX DOOR WILL NOT CLOSE. REPLACED PAX DOOR AFT HINGE FORWARD MICROSWITCH IAW 32-00-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050523003672005052300367EA 2005 5 23 SWIA200514956 120050424A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07418SW 7446 AFT EQUIPMENT COMPARTMENT INTERCOSTAL CLIP IS CRACKED FS 625.00 STR 14L. ITEM FOUND AT C-CHECK INSPECTION. CLIP REPLACED IAW CRJ REO 601R-53-61-100 REV "NC". 2L72 4F RTA21EA 20050523003752005052300375EU 2005 5 23 ASOA05289 120050311A5315 FLOORBEAM AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27635AS 372 DURING A C-CHECK IN YUL, THE LOWER FLOORBEAM AT FRAME 41, STRINGER 18R WAS FOUND TO BE CORRODED BEYOND LIMITS ON TOP OF THE FLANGE AND UNDER THE ANCHOR NUT. MAINTENANCE REMOVED AND REPLACED THE LOWER FLOORBEAM AT FRAME 41, STRINGER 18R IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20050523003802005052300380EA 2005 5 23 ASOA05277 120050401A33501961002 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN DEFECTIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27820AS 7188 DURING A C-CHECK IN MCN, THE EMERGENCY 'EXIT PULL' LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE UNREADABLE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY 'EXIT PULL' BETA LIGHT ON THE PASSENGER DOOR. 2L72 4F RTA21EA 20050523003842005052300384EU 2005 5 23 ASOA05272 120050330A33503011210 LIGHT AEROSPATR72 ATR72212 8680945EU CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27634AS14569 370 DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20050523003952005052300395EU 2005 5 23 ASOA05288 120050311A5315 FLOORBEAM AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27635AS 372 DURING A C-CHECK IN YUL, THE FLOORBEAM AT FRME 40 LT/RT WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM AT FRAME 40 LEFT/RIGHT IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20050523004172005052300417EA 2005 5 23 ASOA05264 120050323A2740 TRIM SYSTEM CNDAIRCL600 CL6002C10 1390015EA NR 1 & 2 MALFUNCTIONED A ASOAK NONE J WARNING INDICATION CRCRUISE 1 SO27708EV 10060 FLT 4182 - DURING CRUISE FROM ATL-OMA, THE MACH TRIM AND STAB TRIM 1 AND 2 FAILED. QRH RESET PROCEDURES WERE SUCCESSFUL. THE CREW REQUESTED EMERGENCY EQUIPMENT BE PLACED ON STANDBY AS A PRECAUTION. THE AIRCRAFT LANDED SAFELY IN OMA. MAINTENANCE PERFORMED A SYSTEM POWER ON SELF TEST AND A SYSTEM RESET WHICH CLEARED THE DISCREPANCY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050524000112005052400011NM 2005 5 24 DHL2005783520 120050404A5751 SKIN BOEING727 727227 1384078NM RT WING AILERONSDENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01783DH 21999 RT WING AILERON UPPER SKIN IS DENTED, WING STA 436. CUT OUT DAMAGED AREA DIM 3 BY 1 1/4 IAW B727 SRM 57-50-5 FIG 2. FABRICATED DOUBLER FROM 2024T3 .032 PO NR 9002034 DIM. 5 1/8" BY 6 1/4" IAW B727 SRM 57-50-5 FIG 2. TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED DOUBLER REPAIR ON R/WING I/B AILERON UPPER SKIN STA 436 IAW B727 SRM 57-50-5 FIG 2 AND 57-50-2 FIG 7. NO REBALANCING REQ FOR IB AILERON IAW B727 SRM 51-80-1 PARA 1B. 2L73 4F A3WE 20050524000182005052400018NM 2005 5 24 AWXA200500525 120050502A33501012721 LIGHT BOEING737 7373G7 1384595NM SEAT ROW 7 LT INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28154AW 23776 DFW - EEL - DURING A-01 CHECK, THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 7 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 7 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050524000192005052400019NM 2005 5 24 AWXA200500526 120050424A2560P4010021 BATTERY BOEING737 737301 1384611NM FLASHLIGHT DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - DURING C-19 CHECK, FOUND THE AFT GALLEY EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT GALLEY EMERGENCY FLASHLIGHT BATTERIES, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050524000472005052400047EA 2005 5 24 ASOA05260 120050322A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27861AS 7445 DURING AN A-CHECK IN BTR, THE EXTERIOR EMERGENCY LIGHT ON THE RIGHT SIDE IN THE FORWARD MOST POSITION WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EXTERIOR EMERGENCY LIGHT ON THE RIGHT SIDE IN THE FORWARD MOST POSITION. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050524000512005052400051EA 2005 5 24 ASOA05340 120050415A5340601R311719 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27821AS 7194 DURING A C-CHECK IN MCN, THE FS 484 RT, RBL 36 CLIP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FS 484 RT, RBL 36 CLIP IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20050524000532005052400053GL 2005 5 24 SIMA200510805 220050413A7200 ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 1 MALFUNCTIONED A SIMAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 SW21676AE 14500807 CAE312582 FLT 4014 - CREW NOTED, SEEING THE OIL PRESSURE STARTING TO DROP AND THEN THE E1 SHUTDOWN. DECLARED AN EMERGENCY AND LANDED SAFELY. REPLACED NR 1 ENGINE IAW WC 72-000-00. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T4 FRTT00011ATTE6CH 20050524000572005052400057WP 2005 5 24 ABXA050105 120050428A21105614845517 COMPRESSOR DOUG DC8 DC863F 302198FWP RT A/C PACK DEFECTIVE A ABXAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL23814AX 46041 NR 2 CTC FAILED, HAD LOUD BEARING SQUEAL ALONG WITH SOME SMOKE IN THE COCKPIT. REMOVED AND REPLACED NR 2 CABIN TURBINE COMPRESSOR IAW DC-8 MM 21-10-01-4-0001. OPS CHECKED GOOD. 2L74 4F 4A25 20050524000582005052400058WP 2005 5 24 WCL2005F00000 220050416A73142070C01 PUMP BRAERODH125 HS125700A 4230170EU GARRTTTFE731TFE731* 01518WP LT FUEL SYS INTERMITTENT E WCLAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA11188KA8355 NA0294 LT FUEL PUMP PRESSURE LIGHT INTERMITTENT. TOOK PRECAUTIONARY ACTIONS AND STARTED TO FEED FUEL AND TURNED. THE INTERMITTENT FUEL PUMP OFF. (EA11200503945) (K) 2L72 4F4 F A3EU E6WE 20050524000592005052400059SO 2005 5 24 1398042505 120050425A5270 WARNING LIGHT GULSTMG1159 GIV 3980115SO PAX DOOR ILLUMINATED E N93AA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO13498QS 1398 MAIN DOOR LIGHT ILLUMINATED IN FLIGHT. 2L72 4F RTA12EA 20050524000672005052400067NM 2005 5 24 BB05032 120050429A3350S417N5091SMI LIGHT BOEING767 7672B7 1385107NM L2 DOOR INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19656US 26847 CLT - FOUND EMERGENCY LIGHT ADJACENT TO L2 DOOR INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. 2L72 4F RTA1NM 20050524000692005052400069 2005 5 24 BA05009 420050426A23309700019001 POWER SUPPLY AIRBUS330 A330323 3930335EU VIDEO CONTROL FAULTY A USAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA19675US 370 LGW FL 94 - YELLOW BULK AVIONICS SMOKE AND IFE OFF ILLUMINATED ON THE F/A IFE CONTROL PANEL. CREW NOTED A 'HAZE' IN THE CABIN NEAR ROW 20. MAINTENANCE REPLACED THE POWER SUPPLY ASSEMBLY. INVESTIGATION IN THE AREA OF ROW 20 SHOW NO EVIDENCE OF ANY PROBLEMS. 2L72 4F RTA46NM 20050524000702005052400070NM 2005 5 24 BB05033 120050430A335020121 CHARGER BOEING767 767201 1385125NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19648US 23900 PHL - FOUND EMERGENCY LIGHTS ON LEFT HAND SIDE OF CABIN INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AND CHARGER AT SEAT ROW 2. 2L72 4F RTA1NM 20050524000742005052400074NM 2005 5 24 DHL2005740008 120050324A2710 SKIN BOEING727 7272Q9 138448MNM LT WING AILERON DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 LT WING OB AILERON UPPER SURFACE HAS DENT WBL 490. REMOVED FASTENER AND CUT OUT DAMAGED AREA IAW B727 SRM 51-30-2 AND 57-50-5. FABBED DOUBLER AND FILLER IAW B727 SRM 57-50-51 AND 57-50-2. TREATED, PRIMED, AND INSTALLED DOUBLER AND FILLER AT L/WING OB AILERON UPPER SURFACE WBL 490 IAW B727 SRM 51-10-2 AND 57-50-5. CALCULATED REPAIR "M" TO BE THE REPAIR WT OF .13436 LB X THE DISTANCE Y=2"+1.2"=3.2" M=1.3436 X 3.2"=.4299 INCH LB "M" IS LESS THAN 2.8 POUND, NO FURTHER ACTION REQUIRED IAW B727 SRM 51-80-4 FIG 1. 2L73 4F RTA3WE 20050524000752005052400075NM 2005 5 24 DHL2005740009 120050324A5755 SKIN BOEING727 7272Q9 138448MNM SPOILER DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 LT WING TE UPPER SURFACE CRACKED AT NR 4 SPOILER HINGE CUT OUT (NR2). REMOVED NR 4 SPOILER TO FACILITATE S/M WORK IAW B727 MM 27-62-1. REMOVED FASTENERS AT LT WING TE UPPER AT NR 4 SPOILER HINGE CUT OUT NR 2 IAW B727 SRM 51-30-2. STOP DRILLED CRACK .250 TERMINATED AT END OF CRACK IAW B727 SRM 51-10-1, NDT AREA IAW B727 MM 51-00-00 PART 6 FIG 23. NO DEFECTS NOTED. FABRICATED DOUBLER REPAIR IAW B727 SRM 57-30-4. ALODINED AND PRIMED IAW B727 SRM 51-10-2, INSTALLED PARTS IAW B727 SRM 57-30-1. INSTALLED NR 4 SPOILER IAW B727 MM 27-62-1. RIG AND OPS CHECK GOOD IAW B727 MM 27-61-0. 2L73 4F RTA3WE 20050524000772005052400077NM 2005 5 24 DHL200574011 120050324A5754 SKIN BOEING727 7272Q9 138448MNM NR 1 SLAT DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 NR 1 SLAT EXTERNAL SKIN DENTED AT WING STA 738. REMOVED PANELS AND WEB FROM SLAT NR 1 FOR ACCESS IAW B727 SRM 51-30-2 CUT OUT DAMAGE AREA FROM SKIN. TRIMMED OUT SKIN TO ACCESS DOUBLER IAW B727 SRM 57-30-3. FABBED FILLER. DOUBLER 3 PIECES IAW B727 SRM 57-50-3 FIG 1 AND 57-50-2 FIG 2. TREATED AND PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B727 SRM 57-50-3 FIG 1. CLOSED PANEL IAW B727 SRM 51-30-2. 2L73 4F RTA3WE 20050524000782005052400078WP 2005 5 24 ASMF200505001 120050502A7910548003 COOLER DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE LT FUEL OIL FAILED W ASMFO OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW23505MD12868 49149 725644 DURING TRANSIT CHECK, IT WAS DETECTED OIL LEAK IN THE LEFT ENGINE FUEL-OIL COOLER AND THE OIL TANK OVERFILLED WITH FUEL SMELT. FUEL-OIL COOLER OF THE LEFT ENGINE WAS REPLACED IAW MM 79-20-01 AND ENGINE LUBRICATING OIL PROCEDURE WAS PERFORMED IAW MM 72-00-00, TESTED CORRECT. 2L72 4F4 F A6WE E9NE 20050524000792005052400079NE 2005 5 24 ASMF200505002 220050503A7200PW2037 ENGINE BOEING757 757200 1384950NM PWA 2037 PW2037 NE RIGHT FAILED W ASMFA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SW23703AM3094615325 27203 AIRCRAFT RETURNED OF FLIGHT AS A CONSEQUENCE OF DURING CLIMB AT 15000 FT THE RIGHT ENGINE OIL TEMPERATURE REACHED 177°C AND INCREASED IN IDLE TO 207°C, SHUTTING DOWN THE ENGINE PER OIL T RED MESSAGE AND RETURNING TO MEX. ENGINE GRAPHICS WERE CHECKED DETERMINING RT ENGINE REPLACEMENT. IT WAS REPLACED IAW MM 71-00-02 AND TESTED IAW MM 71-00-00, ALL CORRECT. 2L72 4F4 FRTA2NM E17NE 20050524000812005052400081WP 2005 5 24 ASMF200505005 120050503A7711LG80E1 COMPUTER DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE LEFT EPR FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23214AM216672245 49585 725605 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF LEFT ENGINE EPR INDICATOR WAS OUT OF SERVICE. EPR TRANSMMITER WAS REPLACED IAW MM 77-11-02, ENGINE WAS TESTED, ALL CORRECT. 2L72 4F4 FRTA6WE E9NE 20050524000822005052400082NE 2005 5 24 ASMF200505006 220050503A7200 LINE DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE PT2 DAMAGED W ASMFO OTHER MJ OVER TEMP WARNING INDICATION NRNOT REPORTED 1 SW23755RA 49727 716734 CAPTAIN REPORTED RIGHT ENGINE REACHED 641°C PER 3 SECONDS. BOROSCOPIC INSPECTION WAS PERFORMED IAW MM 72-00-00, BEING ALL CORRECT. TRIM WAS PERFORMED TO ENGINES, DETECTING A PT2 LINE DAMAGED AND AN INTERNAL LEAK IN TH PT7 LINE. PT2 LINE WAS REPLACED AND PT7 LINE LEAK WAS CORRECTED IAW MM 77-11-00. TRIM WAS CONCLUDED WITH BOTH ACCELERATORS WERE CORRECT. 2L72 4F4 FRTA6WE E9NE 20050524000852005052400085EA 2005 5 24 COMA0560282 120050427A3230750005000 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA MLG MALFUNCTIONED A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01491CA6308 7756 FLIGHT 5547 GEAR DISAGREE WARNING. REPLACED THE MLG SELECTOR VALVE. 2L72 4F RTA21EA 20050524000862005052400086EA 2005 5 24 COMA0570047 120050427A3350 LIGHT CNDAIRCL600 CL6002C10 1390015EA CABIN INOPERATIVE A COMAK NONE L NO TEST ININSP/MAINT 1 SO01379CA 10102 FLIGHT 5490 EMERGENCY LIGHTS ARE INOP. COULD NOT DUPLICATE, OPERATIONAL CHECK OF EMERGENCY LIGHTS SATISFACTORY. 2L72 4F RTA21EA 20050524000872005052400087NM 2005 5 24 DHL2005740014 120050326A2710 SKIN BOEING727 7272Q9 138448MNM RT WING AILERON DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 RT WING OB AILERON TAB IS DELAMINATED AT OB EDGE. CUT OUT DELAMINATED AREA AT RT WING OB AILERON TAB, FABRICATED FILLER AND DOUBLER, BONDED FILLER AND DOUBLER, CURED, CLEANED, PRIMED AND SEALED IAW B727 SRM 57-50-2 AND 51-40-20 FIG 30. 2L73 4F RTA3WE 20050524000882005052400088EA 2005 5 24 COMA0570048 120050429A335020131A BATTERY CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT DISCHARGED A COMAK NONE O OTHER ININSP/MAINT 1 SO01379CA142861355 10102 FLIGHT 5196, 2 EMERGENCY LIGHTS AND OVERHEAD EXIT SIGN ARE INOP. REPLACED EMERGENCY LIGHT BATTERY. 2L72 4F RTA21EA 20050524000892005052400089EA 2005 5 24 COMA0560283 120050430A324061901 FUSE CNDAIRCL600 CL6002B19 1900309EA LT MLG INOPERATIVE A COMAO OTHER O OTHER LDLANDING 1 SO01806CA 7359 FLIGHT 5418, LEFT INBD BRAKE IS INOP. REPLACED THE LT INBD BRAKE FUSE. 2L72 4F RTA21EA 20050524000922005052400092NM 2005 5 24 UPS05444413 120050405A5311 FRAME BOEING747 747283B 1384867NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 BS 1265 STR -26L FRAME BELOW DOOR LOWER SILL FASTENER HOLE FOUND CRACKED AT FRAME WEB RUNNING I/B AND O/B AND FOUND FRAME WEB EDGE CRACKED (CRACK LENGTH 1/16 INCH) BS 1265 LT FRAME WEB INTERIM REPAIRED AS PER DWG 624U0060. 2L74 4F A20WE 20050524000932005052400093NM 2005 5 24 UPS05444414 120050405A5311 FRAME BOEING747 747283B 1384867NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 BS 1265 STR -26R FRAME BELOW DOOR LOWER SILL FASTENER HOLE FOUND CRACKED AT FRAME WEB RUNNING I/B AND O/B (CRACK LENGTH 1/16 INCH), BS 1265 RT FRAME WEB INTERIM REPAIRED AS PER DWG 624U0060. 2L74 4F A20WE 20050524000942005052400094NM 2005 5 24 UPS05444421 120050413A5411 FRAME BOEING747 747283B 1384867NM NR 2 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 NR 2 PYLON AFT BULKHEAD O/B FRAME ADJACENT TO UPPER SPAR FITTING FOUND CRACKED, (CRACK LENGTH .25 INCH AND .9375 INCH ). NR 2 PYLON AFT BULKHEAD O/B FRAME REPAIRED AS PER HX RS NR R54-53-35295 AND UPS ENGINERING FILE NUMBER 747-54-20051. 2L74 4F A20WE 20050524000952005052400095NM 2005 5 24 UPS05444422 120050414A5411 FRAME BOEING747 747283B 1384867NM NR 1 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 NR 1 PYLON AFT BULKHEAD O/B FRAME ADJ TO UPPER SPAR FITTING FOUND CRACKED RUNNING I/B TO EDGE AND RUNNING O/B .9375 INCH LONG, (CRACK LENGTH .9375 ). NR 1 PYLON AFT BULKHEAD O/B FRAME REPAIRED AS PER HX RS NR R54-53-35295 AND UPS ENGINEERING FILE NR 747-54-20051. 2L74 4F A20WE 20050524000962005052400096NM 2005 5 24 UPS05444423 120050407A5315 FLOORBEAM BOEING747 747283B 1384867NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 LH BS 340 U/D FLOORBEAM FOUND 2EA FASTENER HOLES CRACKED AT STR 12L REFER TO ATTACH SKETCH FOR DETAILS. CRACK LENGTH CHORD 0.060", FRAME WEB 1/8" AND THROUGH THICKNESS FLOORBEAM WEB CRK THROUGH THICKNESS. BS 340 LT U/D FLOORBEAM CHORD REPAIRED AT LBL 36 TO LT MOST O/B END AS PER SRM 53-10-07 FIG 23, FLOORBEAM WEB REPAIRED AT LBL 45 INCH TO LH O/B END AS PER SRM 53-10-07 FIG 11 AND FRAME REPAIRED AS PER HX RS R53-12-35291 AND UPS EO B747-5310-22113-A CONTINUE INSP PER BSB 53A2265. 2L74 4F A20WE 20050524000982005052400098NM 2005 5 24 UPS05444425 120050413A5411 FRAME BOEING747 747283B 1384867NM NR 2 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 NR 2 PYLON AFT BULKHEAD I/B FRAME ADJACENT TO UPPER SPAR FITTING FOUND CRACKED, CRACK LENGTH .375 AND .250. NR 2 PYLON AFT BULKHEAD I/B FRAME REPAIRED AS PER HX RS R54-53-35295 AND UPS EA ENGINEERING FILE NR 747-54-20051. 2L74 4F A20WE 20050524000992005052400099NM 2005 5 24 UPS05444426 120050414A5411 FRAME BOEING747 747283B 1384867NM NR 1 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 NR 1 PYLON AFT BULKHEAD I/B FRAME ADJ TO UPPER SPAR FTG CRACKED APPROX .1875 RUNNING I/B AND O/B, CRACK LENGTH .1875. NR 1 PYLON AFT BULKHEAD I/B FRAME REPAIRED AS PER HX RS R54-53-35295 AND UPS EA ENGINEERING FILE NR 747-54-20051. 2L74 4F A20WE 20050524001012005052400101NM 2005 5 24 UPS05444428 120050411A534065B5783913 FITTING BOEING747 747283B 1384867NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 U/D - STA 496 RBL 70 TOILET TANK TIE DOWN FTG CORROSION FOUND. CORROSION BLEND OUT 0.020" BY 1" BY 1". TIE DOWN FTG REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050524001032005052400103NM 2005 5 24 05FDEA01222 120050506A5754 HINGE FITTING BOEING727 727200 138407ENM KRUEGER FLAP GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25264FE 21626 GOUGE IN THE NR 6 K-FLAP CENTER HINGE FITTING COMMON TO L/E FIXED. REPLACED NR 6 K-FLAP CENTER HINGE FITTING PER SRM 51-30-2. 2L73 4F RTA3WE 20050524001052005052400105NM 2005 5 24 SB05059 120050511A335020131A BATTERY BOEING737 7373B7 1384580NM EMERGENCY LIGHT DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19392US 23314 CLT FOUND EXTERIOR EMERGENCY LIGHTS AFT OF THE WINGS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. 2L72 4F RTA16WE 20050524001072005052400107NM 2005 5 24 05FDEA01271 120050513A3020 WARNING LIGHT DOUG MD11 MD11 3023602NM NR 2 ENGINE ILLUMINATED A FDEAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 SO25617FE 48748 FL290 GOT A LEVEL 1 ALERT "ENG 2 ANTI-ICE OFF". A FEW MINUTES LATER GOT A LEVEL 3 "ENG 2 ANTI-ICE DUCT" ALERT WHICH REQUIRED THE NR 2 ENG BE SHUT DOWN. DIVERTED TO RJBB. CHECKED INDIVIDUAL RESISTANCE AND FOUND OVERHEAT SENSOR D1-90 IS 4.8K OHM. REPLACED D1-90 PER MM 30-22-11-4 AND ALSO VISUAL INSPECTED DUCT FROM PANEL NR 364PR AND 364HR, FOUND NORMAL. 2L73 4F RTA22WE 20050524001102005052400110NM 2005 5 24 DHL2005740017 120050327A5315 FLOORBEAM BOEING727 7272Q9 138448MNM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 MAIN CABIN FLOORBEAM TEE CAP DAMAGED AT BS 344 RBL 65.5 TO LBL 65.5. REMOVED AND REPLACED TEE CAP BS 344 RBL 65.5 TO 65.5 FROM P/N BAC1505-29222 PO NR 9001043 DIM 12 FT IAW B727 SRM 53-10-2 FIG 6, 51-30-5 AND DWG NR 2902 VENTURA AEROSPACE. TREATED AND PRIMED TEE CAP AND AREA IAW B727 SRM 51-10-2. 2L73 4F RTA3WE 20050524001112005052400111NM 2005 5 24 0500656718 120050428A5330 SKIN BOEING747 747251F 1384898NM FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01618US 21122 DURING OVERNIGHT LINE CHECK, FOUND CRACK IN FUSELAGE SKIN AT BS 1705 S34L. REFERENCE SB 747-53A2487, AD 2002-23-15 AND AD 2004-07-22. REPAIRED PER EA 67-192649. 2L74 4F A20WE 20050524001122005052400112NM 2005 5 24 DHL2005740018 120050327A5347 SEAT TRACK BOEING727 7272Q9 138448MNM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 MAIN CABIN SEAT TRACK BS 344 TO 480 LBL 24.75 DAMAGED. REMOVED AND REPLACED SEAT TRACK AT BS 344 TO BS 480 LBL 24.75 AND FABRICATED NEW SEAT TRACK P/N BAC1520-792 PO NR 9001465 DIM. 12 FT IAW B727 SRM 53-10-2 FIG1 AND 51-30-5 AND DWG NR 2902 VENTURA AEROSPACE. TREATED AND PRIMED SEAT TRACK IAW B727 SRM 51-10-2. 2L73 4F RTA3WE 20050524001132005052400113NM 2005 5 24 DHL2005740019 120050327A5347 SEAT TRACK BOEING727 7272Q9 138448MNM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 MAIN CABIN SEAT TRACK BS 344 TO 480 LBL 45.5 DAMAGED. REMOVED AND REPLACED NEW SEAT TRACK AT BS 344 TO BS 480 LBL 45.5 AND FABRICATED SEAT TRACK P/N BAC1520-792 PO NR 9001329 DIM. 12 FT IAW B727 SRM 53-10-2 FIG 1 AND 51-30-5 AND DWG NR 2902 VENTURA AEROSPACE. TREATED AND PRIMED SEAT TRACK IAW B727 SRM 51-10-2. 2L73 4F RTA3WE 20050524001172005052400117NM 2005 5 24 QXEA200500834 120050503A2750 CONTROL SYSTEM BOMBDRDHC8 DHC8401 1390041NM TE FLAPS MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION APAPPROACH 1 NM09403QX 4037 GEG - FLIGHT NR 2300 ON APPROACH, WHEN SELECTING FLAPS, THE FLAP POWER CAUTION LIGHT ILLUMINATED. FOLLOWING THE EMERGENCY CHECKLIST, UNABLE TO RESTORE POWER TO THE FLAP SYSTEM. CONDUCTED ZERO FLAP LANDING WITHOUT INCIDENT. MAINTENANCE COMPLIED WITH S/L DH8-400 SL-27-002A CAUTION LIGHT EXTINGUISHED. COMPLIED WITH OPERATIONAL CHECK. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050524001182005052400118NM 2005 5 24 HNAA0500042 120050503A32345352011 SELECTOR PANEL DHAV DHC8 DHC8102 2809003NM MLG INTERMITTENT A HNAAL ABORTED APPROACH O OTHER APAPPROACH 1 EA07943HA42062516 163 ON FINAL APPROACH, GEAR WOULD NOT EXTEND ON GO AROUND GEAR EXTENDED NORMAL. REPLACED LANDING GEAR HANDLE EVALUATION FLIGHT SATISFACTORY. 2H72 4T RTA13NM 20050524001192005052400119EA 2005 5 24 SWIA200514942 120050423A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA LT OVERWING INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07405SW 7029 LEFT OVERWING EMERGENCY LIGHT INOP. REPLACED LEFT OVERWING EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050524001202005052400120EA 2005 5 24 SWIA200514943 120050503A3350 BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07930SW 7713 EMERGENCY EXIT LIGHT FLOOR AND PART OF OVERHEAD SYSTEMS INOPERATIVE. REPLACED NR 2 AND NR 4 EMERGENCY LIGHT BATTERY PACKS. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050524001212005052400121EA 2005 5 24 SWIA200514944 120050503A2740 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA H/S TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07430SW 7523 STAB TRIM CH 2 WILL NOT ENGAGE. REPLACED HSTA AND MCV IAW MM27-42-01, 27-42-05. OPERATIONAL CHECK GOOD, PN 8396-3 SN OFF 899, PN 7062-3 SN OFF 796. 2L72 4F RTA21EA 20050524001222005052400122EA 2005 5 24 SWIA200514945 120050502A5610 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAO OTHER O OTHER APAPPROACH 1 NM07923SW 7664 LEFT WINDOW CRACKED ON FINAL APPROACH. REPLACED LEFT SIDE WINDOW IAW AMM 56-12-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050524001232005052400123SO 2005 5 24 SWIA200514946 120050427A3350 LIGHT EMB 120 EMB120ER 3260203SO CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07582SW 120350 ONE RED EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE AT FORWARD DOOR. REPLACED SECOND FLOOR RED EMERGENCY LIGHT ASSY AT PAX DOOR. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050524001242005052400124SO 2005 5 24 SWIA200514947 120050502A27523431001001 ACTUATOR EMB 120 EMB120ER 3260203SO NACELLE FLAP MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07561SW4361 4361 120335 "FLAP DISAGREEMENT" WHEN PLACING FLAP LEVER FROM 45 DEGREES TO 0 DEGREES. REPLACED RIGHT NACELLE FLAP ACTUATOR IAW EMB MM 27-50-08. REPLACED FLAP SELECTOR HANDLE IAW 27-50-01. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050524001252005052400125EA 2005 5 24 SWIA200514948 120050502A2751 SENSOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07442SW 7609 "FLAPS DEGRADED" STATUS MSG RECEIVED ON START UP. REPLACED LEFT 3 AND 4 ACTUATOR SKEW DETECTION SENSORS AND RIGHT 3 AND 4 ACTUATOR SKEW SECTION SENSORS IAW CRJ MM 27-51-15. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050524001262005052400126SO 2005 5 24 SWIA200514949 120050502A3350 BULB EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07227SW 120304 WHITE EMERGENCY FLOOR LIGHT NEXT TO SEAT 11A INOPERATIVE. REPLACED BULB ASSY FOR AFT WHITE FLOOR EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050524001522005052400152SO 2005 5 24 LAT2005F00000 120050430A2750602509 SWITCH PIPER PA31 PA31350 7103110SO LT WING FLAP FROZEN A LATAA UNSCHED LANDING F FLT CONT AFFECTED DEDESCENT 1 AL0346FA 318152020 (4-30-05-1) UPON DEPARTURE, THE WING FLAPS WOULD NOT RETRACT. AC RETURNED TO BASE. INSPECTION REVEALED A FROZEN UPLOCK LIMIT SWITCH, FLAP OPERTION NORMAL. (AL03200512861) (K) 1L72 3O A20SO 20050524001592005052400159SW 2005 5 24 04210533060 120050421A2913212076011101 PUMP BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE HYDRAULIC SYS NOISY E A1UAA UNSCHED LANDING O OTHER NRNOT REPORTED 1 CE03401MA 33060 6251860169 THE AIRCRAFT WAS DECLARED OUT OF SERVICE AFTER LANDING, BECAUSE OF AN UNUSUAL NOISE DURING SHUTDOWN. ANOTHER COMPANY AIRCRAFT WAS DISPATCHED TO COMPLETE THE TRANSPORT. NR 2 HYDRAULIC PUMP MAKING LOUD NOISE. REPLACED NR 2 HYDRAULIC PUMP. OPS CHECK GOOD, FLIGHT CHECK GOOD. 1G72 4U4 U H4SW E22EA 20050524001622005052400162NM 2005 5 24 05FDEA01207 120050505A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25467FE 21449 RIGHT FUSELAGE SKIN HAS BULGED AREA AT FS 380-400 STR 23R-24R. REWORKED AREA AND NDT FOUND CRACKED. REPAIRED IAW SRM 53-30-3 FIG 13. 2L73 4F RTA3WE 20050524001652005052400165NM 2005 5 24 05FDEA01210 120050505A575365413552 HINGE BOEING727 727200 138407ENM RT T/E FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25254FE 20936 RIGHT WING NR 8 FLAP TRACK FAIRING AFT I/B END IS CRACKED AND FWD FITTING IS GOUGED. REMOVED AND REPLACED FITTING IAW SRM 51-30-2. 2L73 4F RTA3WE 20050524001672005052400167NM 2005 5 24 05FDEA01212 120050505A5720B275700106 SUPPORT ANGLE BOEING727 727200 138407ENM LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25254FE 20936 LEFT WING LOWER FIXED T/E PANEL SUPPORT ANGLE CRACKED AT STA WS 522. REMOVED AND REPLACED SUPPORT ANGLE IAW SRM 51-30-2. 2L73 4F RTA3WE 20050524001682005052400168NM 2005 5 24 05FDEA01213 120050505A3830 TUBE DOUG MD11 MD11 3023602NM WASTE TANK NOT CLOSED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 AFT CARGO - REFERENCE EA 1-2520-7-78127 ITEM 39, AFTER REMOVAL OF WASTE TANK AND PLUMBING FOUND VACUUM PUMPS OUTLETS AND TANK DUMP TUBE OUTLET NOT BLANKED. REMOVED AND DISCARD AS PER AMM 20-50-02 AND SMR 51-33-01 VOL II, NEW PANEL AND COVER PLATE FABRICATED FROM 6061T6-0.160 AND 6061T651-4.5 DIA AS PER DRAWING AWD 8861, AWD 08571 AND AWD 9112. FABRICATED COVER PLATE AND PANEL LOCATED AND INSTALLED AS PER DRAWING AW09112 AND AMM 20-50-02. MAJOR REPAIR AS PER GMM 6-2-100 AND SRM 51-90-01 FIG. 1 VOL II. 2L73 4F RTA22WE 20050524001692005052400169NM 2005 5 24 05FDEA01214 120050505A575566147343 FILLER BOEING727 727200 138407ENM RT SPOILER CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25212FE 22934 RIGHT WING NR 6 TRACK AT SPOILER BEAM ATTACHMENT FITTING HOLES ARE CORRODED. REMOVED AND REPLACED SUPPORT FILLER IAW SRM 51-30-5 & 51-30-2. 2L73 4F RTA3WE 20050524001712005052400171NM 2005 5 24 05FDEA01216 120050506A5350 FAIRING DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 LEFT NR 1 AIR COND BAY BILGE AREA, FAIRING ASSY FOUND WITH CORROSION AS MARKED. CORROSION REMOVED AS PER SRM 51-21-01 VOL II ,MATERIAL ORIGINAL THICKNESS:0.04 REMOVED MATERIAL THICKNESS: 0.006, L:24, W:6, REMAIN THICKNESS: 0.034 AND FOUND WITHIN LIMIT AS PER SRM 53-00-01 FIG 1A VOL I. REPAIR INTERCOSTAL PN ACA3805-11 AND BRACKET ACA3352-5. MINOR REPAIR PER GMM 6-2-100. 2L73 4F RTA22WE 20050524001722005052400172EU 2005 5 24 05FDEA01218 120050506A5753 FLAP AIRBUS310 A310324 3930206EU RT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25802FD 542 DURING C2 CHECK, FOUND AN EXISTING REPAIR ON RIGHT INBOARD FLAP LOWER TRAILING EDGE. NEW REPAIR WAS PERFORMED IAW FEDEX EA 6-5710-84120. 2L72 4F RTA35EU 20050524001732005052400173EU 2005 5 24 05FDEA01219 120050506A5522 SKIN AIRBUS310 A310324 3930206EU LT ELEVATOR DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25802FD 542 DURING C2 CHECK, AN EXISTING REPAIR WAS FOUND ON LEFT ELEVATOR TOP SURFACE OUTBOARD OF RIB 17. NEW REPAIR ACCOMPLISHED PER SRM 55-20-00. 2L72 4F RTA35EU 20050524001742005052400174EU 2005 5 24 05FDEA01220 120050506A5753 SKIN AIRBUS310 A310324 3930206EU T/E FLAP DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25802FD 542 DURING C2 CHECK, 2 EXISTING FLUSH COMPOSITE REPAIRS WHERE FOUND ON LEFT INBOARD FLAP TRAILING EDGE. REPAIRED IAW EA 6-5750-84119. 2L72 4F RTA35EU 20050524001792005052400179EA 2005 5 24 VTZA200500075 120050507A531260034017595 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27625BR 7214 LEFT SIDE PILOTS BULKHEAD AT FS 280 RBL 9.0 IS CRACKED AT 1.0 INCH IN WEB RADIUS. 2L72 4F RTA21EA 20050524001802005052400180EA 2005 5 24 VTZA200500070 120050505A53206013501251 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27625BR 7214 LEFT 624 OBLIQUE ANGLE IS CRACKED AT .750 INCH IN RADIUS. 2L72 4F RTA21EA 20050524001822005052400182NM 2005 5 24 MWEA050039 120050508A57545922533504 SKIN DOUG MD88 MD88 3023688NM L/E SLAT CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 NUMBER THREE SLAT, RIGHT LOWER SURFACE SKIN HAS 3 SMALL CRACKS EMANATING FROM CHERRY MAX RIVETS. FABRICATED AND INSTALLED DOUBLER. 2L72 4F RTA6WE 20050524001842005052400184CE 2005 5 24 ACE050705 120050507A3260444EN496 SAFETY SWITCH BEECH 1900 1900C 1154161CE RT MLG INTERMITTENT E YADAK NONE S AFFECT SYSTEMS CLCLIMB 1 AL03111AX UC81 PIREP - LANDING GEAR WOULD NOT RETRACT. MAINTENANCE REPLACED INTERMITTENT RT LANDING GEAR SAFETY SWITCH. 2L72 4T RTA24CE 20050524001872005052400187SO 2005 5 24 C2XA05CL032 120050505A2611FDS765A2 SMOKE DETECTOR EMB 145 EMB145XR 3260214SO LAVATORY MALFUNCTIONED A C2XAK NONE N FALSE WARNING CRCRUISE 1 SW2714180332 14500900 CLE FLIGHT 3320 THE CREW REPORTED A MOMENTARY LAV SMOKE WARNING AFTER TAKEOFF. MAINTENANCE REPLACED THE LAV SMOKE DETECTOR AND THE OPERATIONAL CHECKS WERE GOOD. 2L72 4F RT 20050523001342005052300134CE 2005 5 23 DXTA200500710 120050506A33501317 BULB RAYTHNDH125 HAWKER800XP 7150012CE EMERGENCY LIGHT BURNED OUT E DXTAK NONE O OTHER ININSP/MAINT 1 GL07867QS 258576 2 EMERGENCY EXIT LIGHTS ABOVE DOOR AND ONE LOCATED AT THE ENTRANCE NOT ILLUMINATED DURING EMERGENCY LIGHT SYSTEM TEST. REPLACED 2 EACH BULBS IAW RAC DWG 149-349514. OP'S CHECKED GOOD. 2L72 4F RTA3EU 20050523001462005052300146CE 2005 5 23 DXTA200500727 120050515A3230S3128C10500G HOSE CESSNA750 750 2076810CE MLG MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07936QS 7500036 UPON RETRACTING GEAR AFTER TAKEOFF THE AMBER HYD LOW A CAS MESSAGE ILLUMINATED QUANTITY SHOWED 1 PERCENT AFTER RUNNING THE CHECKLIST AND BLOWING DOWN THE GEAR THE QUANITY INCREASED TO 33 PERCENT AFTER STOPPING A VISUAL INSPECTION FOUND HYD FLUID LEAKING OUT OF THE RIGHT GEAR. FOUND RT RETRACT HOSE LEAKING, REMOVED & REPLACED RT MLG ACTUATOR RETRACT HOSE IAW CE750 MM 32-30-04. SERVICED A-RESIVOIR & EMER. GEAR BLOW DOWN BOTTLE. IAW CE750 MM 12-10-15 & 12-10-36. 2L72 4J RTT00007WI 20050523001482005052300148NM 2005 5 23 SB05061 120050514A3397 WIRE BOEING737 737301 1384611NM SEAT 5A BROKEN A USAAK NONE O OTHER ININSP/MAINT 1 EA19586US 23931 MAINTENANCE REPORTED THE EMERGENCY LIGHT ON SEAT 5A INOPERATIVE. MAINTENANCE REPAIRED WIRE ON LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050523001532005052300153NM 2005 5 23 05FDEA01192 120050501A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25264FE 21626 BS 1351, STR 17L, CHAFE DAMAGE TO SKIN AND RAIN GUTTER. REPAIRED SKIN AND RAIN GUTTER PER SRM 54-10-3. 2L73 4F RTA3WE 20050523001612005052300161EA 2005 5 23 SWIA200514939 120050501A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY MALFUNCTIONED A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07447SW 7677 SMOKE CARGO WARNING ILLUMINATED. REPLACED NR 2 SMOKE CARGO DETECTOR IAW MM 26-15-01. OPERATIONAL CHECKS GOOD. 2L72 4F RTA21EA 20050523001632005052300163EA 2005 5 23 SWIA200514941 120050424A3350 CONVERTER CNDAIRCL600 CL6002B19 1900309EA CABIN MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07405SW 7029 AFT SECTION OF FLOOR LEVEL EMERGENCY LIGHTING INOPERATIVE. REPLACED NR 4 ELBP CONVERTER IAW CRJ MM 33-51-00. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050523001692005052300169NM 2005 5 23 SWAA051272 120050428A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29371SW 26598 DURING SCHEDULED 1/4D CHECK, FOUND 2 EA AFT CARGO FLOOR SUPPORT BEAMS CORRODED AT BS 770, LBL 3 & RBL 8. REPAIRED BEAMS PER SWA EA. 2L72 4F RTA16WE 20050523001712005052300171NM 2005 5 23 SWAA051274 120050428A3350101114 LIGHT BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29372SW 26599 DURING SCHEDULED A2 CHECK, FOUND EMERGENCY LIGHT INOP AT ROW 21 ABC. RELAMPED EMERGENCY LIGHT PER MM. 2L72 4F RTA16WE 20050523001732005052300173NM 2005 5 23 SWAA051276 120050428A53116545810 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303, STR 16L. REPAIRED FRAME PER BOEING S/B. 2L72 4F RTA16WE 20050523001742005052300174 2005 5 23 SWAA051277 420050501A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29208WN 29856 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050523001772005052300177NM 2005 5 23 SWAA051280 120050429A53126516300 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29354SW 25219 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE BULKHEAD WEB CRACKED AT BS 178, RBL 9, WL 234. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050523001842005052300184NM 2005 5 23 SWAA051287 120050430A53306545774 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29683SW 24008 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D + 13, STR 19R. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050523001852005052300185NM 2005 5 23 SWAA051288 120050430A53306545776 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29683SW 24008 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 943, STR 24L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050523001892005052300189NM 2005 5 23 SWAA051292 120050502A53106546957 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 DURING SCHEDULED D-CHECK, FOUND CORROSION ON LT CREASE BEAM WEB AT BS 500 + 10, BS 500A + 15 & BS 500C + 15. REPAIRED CREASE BEAM WEB PER SRM. 2L72 4F RTA16WE 20050523001932005052300193EU 2005 5 23 AWXA200500531 120050415A5711D57252520004 SPAR AIRBUS320 A320232 3930326EU RT WING CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28638AW 455 SAL - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON RT REAR SPAR HOLES 52, 53, 55-59, & 79-81. MAINTENANCE REPAIRED DAMAGE BY REWORKING RT REAR SPAR HOLES PER AIRBUS REPAIR INSTRUCTION R572-58325 ISSUE D, AND ER 26-5700-05121-SS1. 2L72 4F RTA28NM 20050523002012005052300201NM 2005 5 23 05FDEA01197 120050503A5754692848711 RETAINER BOEING727 727200 138407ENM NR 3 SLAT CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25254FE 20936 NR 3 SLAT INBOARD MOLDED SEAL RETAINER CRACKED ON SEVERAL AREAS. REMOVED AND REPLACED SEAL RETAINER IAW SRM 51-30-2. 2L73 4F RTA3WE 20050523002132005052300213CE 2005 5 23 ACE041905 120050419A32601003810061 DOWNLOCK SWITCH BEECH 1900 1900C 1154161CE NLG FAILED E YADAO OTHER N FALSE WARNING APAPPROACH 1 AL03112AX UC45 PILOT REPORTED NOSE GEAR POSITION INDICATED UNSAFE WITH GEAR SELECTED DOWN. CYCLED GEAR AND PERFORMED GROUND VISUAL CHECK PRIOR TO UNEVENTFUL LANDING. MAINTENANCE CONFIRMED FAILED NOSE GEAR DOWNLOCK SWITCH AND REPLACED SAME. 2L72 4T RTA24CE 20050523002182005052300218 2005 5 23 UPS05544416 420050502A2210154050011 YAW DAMPER BOEING757 75724APF 1384969NM RUDDER LEAKING A IPXAA UNSCHED LANDING KF FLUID LOSS FLT CONT AFFECTED CRCRUISE 1 SO01421UP 25281 INSPECTION TYPE:N/A ATB - EXCESSIVE RUDDER TRIM REQ FOR LEVEL FLIGHT. T/S IN PROGRESS. FOUND BOTH YAW DAMPNERS LEAKING. ORDERED TWO EACH AND TUBE AND LINK ASSY P/N 251N3058-8. AWAITING PARTS. 2L72 4F RTA2NM 20050523002202005052300220NM 2005 5 23 UPS05544420 120050430A2560 SMOKE GOGGLES BOEING757 75724APF 1384969NM COCKPIT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01431UP 25462 INSPECTION TYPE:N/A FIRST OBSERVERS SMOKE GOGGLES CRACKED. REMOVED AND REPLACED SMOKE GOGGLES IAW AMM 25-60-00. 2L72 4F RTA2NM 20050523002382005052300238EA 2005 5 23 MASA200500311 120050422A76032100140007 GEARBOX CNDAIRCL600 CL6002B19 1900309EA THROTTLE WORN A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0775993 7372 COMPLIED WITH THROTTLE GEARBOX INSPECTION OF NR 2 ENGINE AND FOUND WEAR TO BE ACCEPTABLE AND WITHIN LIMITS OF MESA EO CRJ-76-0004. REMOVED AND REPLACED. 2L72 4F RTA21EA 20050523002402005052300240NM 2005 5 23 87 120050505A5320 FLOOR SUPPORT DOUG MD88 MD88 3023688NM FUSELAGE CORRODED B DU4RK NONE O OTHER ININSP/MAINT 1 SO1512FQ 49766 CORRODED CABIN FLOOR SUPPORT STRUCTURE FS 180.0 RBL 0-36. 2L72 4F RTA6WE 20050523002482005052300248NM 2005 5 23 AWXA200500535 120050503A2560P4010021 BATTERY BOEING737 73733A 1384673NM CABIN DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCI - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE AFT CABIN EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT CABIN EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050523002642005052300264SO 2005 5 23 CHQA200500094 120050502A3350RPS1B BATTERY PACK EMB 145 EMB145LR 3260212SO CABIN UNSERVICEABLE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11281SK 145391 REAR EMERGENCY LIGHTS COME ON INTERMITTENTLY. REMOVED AND REPLACED REAR EMERGENCY POWER SUPPLY BATTERY PACKS IAW 145 AMM 33-50-04-00-801-A. OPS CHECK GOOD. SERIAL NUMBERS REMOVED: 14440 AND 18346. 2L72 4T RTT00011AT 20050523002652005052300265EU 2005 5 23 AWXA200500520 120050403A5321D5367200800100 FLOOR PANEL AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28638AW 455 SAL - MAJOR REPAIR - DURING C-08 CHECK, CORROSION WAS FOUND ON FORWARD CARGO COMPARTMENT FLOOR PANEL 132JF. MAINTENANCE REMOVED FORWARD CARGO COMPARTMENT FLOOR PANEL 132JF; FABRICATED A NEW REPLACEMENT FLOOR PANEL AND DOUBLER; INSTALLED REPAIRED PARTS IAW AWA TASK CARD M2M53305. 2L72 4F RTA28NM 20050523002662005052300266EU 2005 5 23 AWXA200500521 120050403A5321D5367200800000 FLOOR PANEL AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28638AW 455 SAL - MAJOR REPAIR - DURING C-08 CHECK, GALVANIC CORROSION WAS FOUND ON FORWARD CARGO COMPARTMENT FLOOR PANEL 131JF. MAINTENANCE REMOVED FORWARD CARGO COMPARTMENT FLOOR PANEL 131JF; FABRICATED A NEW REPLACEMENT FLOOR PANEL AND DOUBLER; INSTALLED REPAIRED PARTS IAW AWA TASK CARD M2M53305. 2L72 4F RTA28NM 20050523002672005052300267EU 2005 5 23 AWXA200500522 120050403A5321D536740100000 FLOOR PANEL AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28638AW 455 SAL - MAJOR REPAIR - DURING C-08 CHECK, GALVANIC CORROSION WAS FOUND ON FORWARD CARGO COMPARTMENT FLOOR PANEL 132FF. MAINTENANCE REMOVED FORWARD CARGO COMPARTMENT FLOOR PANEL 132FF; FABRICATED A NEW REPLACEMENT FLOOR PANEL AND DOUBLER; INSTALLED REPAIRED PARTS IAW AWA TASK CARD M2M53305. 2L72 4F RTA28NM 20050523002692005052300269EU 2005 5 23 AWXA200500523 120050403A5320D53471124200 SHEAR PLATE AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28638AW 455 SAL - MAJOR REPAIR - DURING C-08 CHECK, INTERGRANULAR CORROSION WAS FOUND AT WEB (SHEAR PLATE) Y1162.5 BETWEEN FS 69 AND FS 70 AT FLOOR LEVEL. MAINTENANCE REMOVED AND REPLACED SHEAR PLATE Y1162.5 FROM FR 69 TO FR 70 IAW A320 SRM 51-42-11. 2L72 4F RTA28NM 20050523002702005052300270EU 2005 5 23 AWXA200500524 120050421A5743R57248003002 NUT AIRBUS320 A320232 3930326EU WING CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28638AW 455 SAL - LANDING GEAR - DURING C-08 CHECK, CORROSION WAS FOUND ON THE RETAINING NUT FOR THE FWD PINTLE BEARING ON THE RT MAIN LANDING GEAR. MAINTENANCE REMOVED AND REPLACED RETAINING NUT IAW A320 SRM 57-26-13. 2L72 4F RTA28NM 20050523002752005052300275NM 2005 5 23 SWAA051311 120050503A55516551524 FITTING BOEING737 7373H4 1384600NM HORIZ STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 DURING SCHEDULED D-CHECK, FOUND LT & RT HORIZONTAL STAB FITTING LUG FACES CORRODED. REPAIRED LUG FACES PER SRM. 2L72 4F RTA16WE 20050523002762005052300276NM 2005 5 23 SWAA051312 120050503A55536547450 FITTING BOEING737 7373H4 1384600NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 DURING SCHEDULED D-CHECK, FOUND LT & RT VERTICAL STAB FITTING FWD & AFT PRIMARY CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER. 2L72 4F RTA16WE 20050523002842005052300284 2005 5 23 ASMF200504023 420050428A34142594466906 INDICATOR DOUG MD88 MD88 3023688NM LEFT AIRSPEED FAILED W ASMFC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW23160PL17329 49763 AIRCRAFT REJECTED TAKEOFF AT 80 KTS AS A CONSEQUENCE OF LEFT VELOCIMETER DID NOT HAVE INDICATION AND WHEEL BRAKES WITH 150°C. LEFT CADC WAS CHECKED IAW MM 34-16-00, PITOT STATIC LINES WERE CLEANED AND TESTED IAW MM 34-11-00 AND VELOCIMETER WAS REPLACED IAW MM 34-13-01, TESTED CORRECT. SYSTEM WAS TESTED WITH THE PITOT-STATIC TEST EQUIPMENT IAW MM 34-11-00, ALL CORRECT. DURING OVERNIGHT SERVICE VELOCIMETERS WERE TESTED IAW MM 34-13-01, ALL CORRECT. 2L72 4F RTA6WE 20050523002902005052300290EU 2005 5 23 HE66100337 120050416A324610551522 SKID BOLKMS105 BO105LSA1 5626021EU ALLSN 250C 250C28 03013GL MLG UNSERVICEABLE B HEERO OTHER O OTHER NRNOT REPORTED 1 SW03202LF 2014 RIVETS PULLED AND GOUGES IN BOTTOM OF TUBE. 1G72 3U3 U H3AU E1GL 20050523002922005052300292NM 2005 5 23 DHL2005740003 120050324A5230 SKIN BOEING727 7272Q9 138448MNM CARGO DOOR DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 MAIN CARGO DOOR INNER SKIN DAMAGED (INTERNAL) FWD SECTION. REMOVED INNER SKIN IAW B727 SRM 51-30-2, LOCATED AND DRILLED INNER SKIN P/N AE727-1-032A-17 PO NR 508028 IAW DWG NR AE727-1-032A LTR A 4-28-99 AERONAUTICAL ENGINEERS INC. TREATED AND PRIMED HOLES AND AREA IAW B727 SRM 51-10-2. INSTALLED INNER SKIN AT MAIN CARGO DOOR (INTERNAL FWD SECTION) IAW DWG NR AE727-1-032A. LTR A 4-28-99 AERONAUTICAL ENGINEERS INC. 2L73 4F RTA3WE 20050523002962005052300296NM 2005 5 23 UPS05444393 120050411A5313 STRINGER BOEING747 747283B 1384867NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 BS 1238-1241 STR 7R STRINGER END FOUND CRACK (CRACK LENGTH 1 INCH ). M/DECK BS 1238 STR 7R STR REPAIRED AS PER HX RS R-53-41-35297 AND UPS ENGINEERING FILE NR 747-53-20245. 2L74 4F A20WE 20050523003042005052300304NM 2005 5 23 QXEA200500839 120050504A29136617302 PUMP BOMBDRDHC8 DHC8401 1390041NM HYDRAULIC SYS FAILED A QXEAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 NM09417QX2417 4086 SEA - EXPERIENCED A TOTAL LOSS OF NR 2 MAIN HYDRAULIC SYSTEM PRESSURE. THE GEAR WAS EXTENDED VIA ALTERNATE EXTENSION SYSTEM, AND THE AIRCRAFT LANDED IN SEA WITHOUT INCIDENT. AN INSPECTION OF THE NR 2 HYDRAULIC SYSTEM REVEALED THAT THE NR 2 EDP HAD FAILED, DUE TO A HOLE RUPTURED THROUGHT THE SIDE OF THE PUMP HOUSING. IT IS ESTIMATED THAT THE PUMP OPERATED FOR AT LEAST 10 MINUTES IN A DRY STATE, AND WHEN REMOVED, WAS FOUND TO HAVE A SHEARED SHAFT. MAINTENANCE REPLACED THE NR 2 EDP PUMP. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050523003072005052300307EA 2005 5 23 QXEA200500836 120050502A2120 DUCT CNDAIRCL600 CL6002C10 1390015EA AIR DISTRIBUTIONDIRTY A QXEAK NONE B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 NM09609QX 10031 GEG - UPON INITIATING DESCENT, AIRCRAFT BEGINS TO SMELL OF GYM SOCKS. MAINTENANCE REMOVED AND CLEANED LEFTHAND FLOOR MIXER SUPPLY DUCT IAW 21-23-27. REINSTALLED DUCT, PERFORMED OPS AND LEAK CHECK IAW 21-20-00, NO LEAKS NOTED. RAN AIRCRAFT BLEED AIR FOR SEVERAL MINUTES, NO UNUSUAL ODOR NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20050523003082005052300308NM 2005 5 23 UPS05444402 120050411A5313 STRINGER BOEING747 747283B 1384867NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 BS 1485 LT STR 6L STRINGER END FOUND CRACKED. CRACK LENGTH 0.5 INCH. M/DECK BS 1485 STR 6L REPAIRED AS PER HX RS R-53-41-35294 AND UPS EA ENGINEERING FILE NR 747-53-20244. 2L74 4F A20WE 20050523003092005052300309NM 2005 5 23 UPS05444403 120050406A5311 FRAME BOEING747 747283B 1384867NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 NR 1R MED CUTOUT BS 488 FRAME AT DOOR STOP NR 1 AREA FOUND CRACK AT FRAME FWD DOUBLER 1/2 INCH LONG EXTEND BEYOND DOOR STOP FTG AND CRACK AT WEB 1 EA HOLE APPROX 1/16 INCH LONG. CRACK LENGTH 1/4 INCH AT DOUBLER, 1/16 INCH AT WEB. M/DECK NR 1R MED CUTOUT BS488 FRAME BETWEEN STR 23 TO STR 30. REPAIRED AS PER SRM 53-10-04 FIG 92. 2L74 4F A20WE 20050523003102005052300310NM 2005 5 23 UPS05444404 120050423A5330 SKIN BOEING747 747283B 1384867NM FUSELAGE CHAFED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 EXTERIOR SKIN CHAFING MARK FOUND ABOVE STR 12L BS 2230. CHAFED AREA 0.016 INCH BY 3 INCH BY 1 INCH. SKIN REPAIRED AT BS 2220 TO BS 2240 BETWEEN S11L TO S12L AREA AS PER SRM 53-30-03 FIG 17 WITH ZERO TIMING AT CRITICAL ROW FASTENER CAT B REPAIR REPEAT INSP AT 15000 FLT CYC. 2L74 4F A20WE 20050523003112005052300311NM 2005 5 23 UPS05444405 120050411A531165B01715283 FRAME BOEING747 747283B 1384867NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 BS440 LT FRAME, JUST BELOW U/D FLOORBEAM LWR CHORD, WEB CRACKED WL290, CRACK LENGTH 3/8 INCH. BS 440 LT FRAME WEB REPLACED BETWEEN STR 13L TO 16L AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050523003122005052300312NM 2005 5 23 UPS05444406 120050411A5311 FRAME BOEING747 747283B 1384867NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 STA 440 STR 10R FRAME CRACKED. U/DECK BS440 STR 10R FRAME REPAIRED AS PER SRM 53-10-04 FIG 11. 2L74 4F A20WE 20050523003142005052300314NM 2005 5 23 UPS05444407 120050411A5311 FRAME BOEING747 747283B 1384867NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 U/DECK BS480 STR 12L STR CUTOUT CRACKED. CRACK LENGTH 3/4 INCH. U/DECK BS480 STR 10AL TO STR 12L FRAME REPAIRED AS PER SRM 53-10-04 FIG 22. 2L74 4F A20WE 20050523003152005052300315NM 2005 5 23 UPS05444408 120050411A5311 FRAME BOEING747 747283B 1384867NM FUSLEAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 BS 480 FRAME S10AL STR CUTOUT CRACKED. CRACK LENGTH 3/4 INCH. BS 480 STR 10AL TO STR 12L FRAME REPAIRED AS PER SRM 53-10-04 FIG 22 REFER NRC 6374 FOR WORKING DETAIL. 2L74 4F A20WE 20050523003342005052300334SO 2005 5 23 RAIA00504019 120050418A213122250N030201 CONTROLLER EMB 145 EMB145LR 3260212SO CABIN PRESSURE MALFUNCTIONED A RAIAA UNSCHED LANDING O OTHER CRCRUISE 1 CE03817HK337 145058 FLT 5687 - STL - AUTO AND MANUAL PRESSURIZATION INOP. MAINTENANCE REMOVED AND REPLACED BOTH AUTO AND MANUAL CABIN PRESSURE CONTROLLERS. 2L72 4T RTT00011AT 20050523003442005052300344EU 2005 5 23 RAIA00505001 120050501A2422PC125123B INVERTER JETAIRJETSTMJETSTM4101 1500501EU RIGHT INOPERATIVE A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03572HK1682 41091 FLT 3660 - BWI - RIGHT INVERTER FAIL INDICATION. MAINTENANCE REMOVED AND REPLACED RIGHT STATIC INVERTER. 2L72 4T RTA41NM 20050523003652005052300365EA 2005 5 23 SWIA200514954 120050424A5320 FITTING CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07418SW 7446 FUSELAGE FLOORBEAM FITTING IS CRACKED; FS 460.00 RBL. ITEM FOUND AT C-CHECK INSPECTION. REPLACED FITTING IAW CRJ SRM 51-40-11, 51-23-00, 51-42-21, 51-42-06, 51-25-16, AND 51-21-11. 2L72 4F RTA21EA 20050523003702005052300370EA 2005 5 23 SWIA200514959 120050503A2740 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA COCKPIT INOPERATIVE A SWIAO OTHER F FLT CONT AFFECTED APAPPROACH 1 NM07959SW 7840 CAPTAIN'S TRIM SWITCH INOPERATIVE ON FINAL. REPLACED CAPTAINS TRIM SWITCH IAW CRJ AMM REF CHAP 27-41-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050523003712005052300371EA 2005 5 23 SWIA200514960 120050501A3350 BATTERY CNDAIRCL600 CL6002B19 1900309EA CABIN UNSECURE A SWIAK NONE L NO TEST ININSP/MAINT 1 NM07912SW 7595 EMERGENCY LIGHTS NOT WORKING BEYOND ROW 8 ON PREFLIGHT. RESECURED BATTERY PACK FOR EMERGENCY LIGHT. OPERATIONAL CHECK GOOD IAW CRJ MM 33-51-00. 2L72 4F RTA21EA 20050523003772005052300377EA 2005 5 23 ASOA05267 120050325A5210601R31903309 MECHANISM CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BINDING A ASOAK NONE O OTHER ININSP/MAINT 1 SO27826AS 7210 DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WAS FOUND HARD TO CLOSE. MAINTENANCE ADJUSTED THE LATCH MECHANISM ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050523003782005052300378EA 2005 5 23 ASOA05276 120050331A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27857AS 7411 DURING A GROUND INSPECTION IN CAE, THE SECOND OVERHEAD EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE SECOND OVERHEAD EMERGENCY CEILING LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050523003852005052300385NM 2005 5 23 USAA050460 120050402A5320 INTERCOSTAL BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19442US40275 24841 CLT - FOUND INTERCOSTAL CRACKED .4 INCH, STATION 927 TO 947.5 BL 0. FABRICATED AND INSTALLED NEW INTERCOSTAL IAW SRM 53-60-51. (M) 2L72 4F RTA16WE 20050523004132005052300413EA 2005 5 23 ASOA05265 120050323A499038004883 APU CNDAIRCL600 CL6002B19 1900309EA APU BAY OVERSERVICED A ASOAK NONE WBJINADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION APAPPROACH 1 SO27925EV 7831 FLT 4151 - DURING FINAL APPROACH TO ATL FROM FPO, THE CREW RECEIVED A SMOKE TOILET CAUTION MESSAGE. THE MESSAGE OCCURRED SIMULTANEOUSLY WHEN SHIFTING THE BLEEDS FROM THE ENG TO THE APU. A MILD ACRID ODOR WAS PRESENT BRIEFLY WITH NO HARD INDICATIONS OF SMOKE OR FIRE BEING PRESENT. THE QRH WAS COMPLIED WITH. EMERGENCY EQUIPMENT ASSISTANCE WAS REQUESTED AS A PRECAUTION. THE AIRCRAFT LANDED SAFELY IN ATL. UPON INSPECTION OF THE AFT EQUIPMENT BAY MAINTENANCE FOUND SMOKE IN THE APU ENCLOSURE. AN INSPECTION OF THE APU REVEALED IT TO HAVE BEEN OVERSERVICED. MAINTENANCE REMOVED THE EXCESS OIL AND RAN THE APU. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050523004152005052300415EA 2005 5 23 ASOA05262 120050323A5320601R3501163 SILL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27902EV 7620 DURING A C-CHECK IN MCN, THE CARGO BAY FLOOR SILL AT FS 562.72 - FS 589 UNDER THE FORWARD LATCH ANGLE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO BAY FLOOR SILL AT FS 562.72 - 589 IAW ASA EO 600-53-0095. (M) 2L72 4F RTA21EA 20050523004162005052300416EA 2005 5 23 ASOA05261 120050323A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA T/E FLAP MALFUNCTIONED A ASOAK NONE J WARNING INDICATION DEDESCENT 1 SO27835AS4205 7258 FLT 4381 - DURING CRUISE FROM FWA-ATL, AT APPROXIMATELY 28,000 FEET, THE CREW BELIEVED THE AIRCRAFT WAS STRUCK BY LIGHTNING AND THEN SEVERAL MORE TIMES DURING DESCENT FOR APPROACH INTO ATL. UPON APPROACH, THE CREW SELECTED THE FLAPS TO EIGHT DEGREES AND THEN TO TWENTY DEGREES WHICH WAS FOLLOWED BY AN AMBER FLAPS FAIL MESSAGE ON EICAS WITH AN INDICATION OF ZERO DEGREES FLAPS. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS ALSO DECLARED. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE INSPECTED THE AIRCRAFT FOR LIGHTNING STRIKES WITH NO EVIDENCE FOUND. MAINTENANCE ALSO REMOVED AND REPLACED THE RIGHT BRAKE POSITION SENSOR UNIT (BPSU). OPS AND RIG CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050523004182005052300418EU 2005 5 23 ASOA05342 120050415A33503012001 BALLAST AEROSPATR72 ATR72212 8680945EU CABIN DEFECTIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27641AS 387 DURING A GROUND INSPECTION IN MGM, THE OVERHEAD EMERGENCY LIGHT AT ROWS 7 AND 11 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BALLAST AT STATION 61WL IAW ATR72 AMM 33-51-00. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20050524000092005052400009WP 2005 5 24 DHL2005802007 120050501A242050130003 CONTROL PANEL DOUG DC8 DC873 302199CWP BUSS PANEL MALFUNCTIONED A DHLAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO01802DH 1933 46076 NR 1 BUS FAILED ON ENGINE START. DEFERRED NR 1 GEN AND CSD REF MEL 24-1-1A DMI NR 20731 ASSIGNED PLACARD INSTALLED MPEREZ 8427. REF DMI 20731 NR 1 BUSS FAILED ON ENGINE START. REMOVED AND REPLACED BUSS PROTECTION PANEL IAW 24-20-7. OPS CHECKS OK IAW JRH ENG RUN UP HAND BOOK THIS CLEARS DMI 20731 PLACARD REMOVED. 2L74 4F RT4A25 20050524000312005052400031SO 2005 5 24 TZR2005F00016 220050411A8530AEC520TI01 CYLINDER CESSNA401 401A 207590DCE CONT O520 TSIO520* 17040SO NR 3 ENGINE CRACKED E TZRAK NONE O OTHER ININSP/MAINT 1 SW05409TE 401A0118 519510 CRACKED FROM EXHAUST VALVE TO TOP OF SPARK PLUG. ECI CYLINDER. (SW05200507949) (K) 1L72 3O3 O A7CE E8CE 20050524000412005052400041GL 2005 5 24 0500641225 220050429A7230 COMPRESSOR DOUG DC10 DC1030 3023501WP GE CF6 CF650C 30018GL NR 1 ENGINE STALLED A NWAAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 GL01225NW 46582 528118 DURING TAKEOFF ROLL, THE NR 1 ENGINE EXPERIENCED A COMPRESSOR STALL WITH EGT EXCEEDING RED LINE. TAKEOFF WAS ABORTED AT 110 KTS. THE ENGINE WILL BE REPLACED. 2L73 4F4 F A22WE A23EA 20050524000662005052400066WP 2005 5 24 MWEA050037 120050502A33501315 BULB DOUG DC9 DC981 3022081WP TAILCONE INOPERATIVE A MWEAK NONE O OTHER ININSP/MAINT 1 GL31803ME 48029 FLOURESCENT EMERGENCY LIGHT IN TAILCONE IS NOT ILLUMINATED. SECURED BULB IN LIGHT SOCKET. 2L72 4F A6WE 20050524000712005052400071NM 2005 5 24 C1HA200582001 120050501A561058935578 WINDOW BOEING727 7272S7 138407ZNM COCKPIT CRACKED A C1HAA UNSCHED LANDING O OTHER CRCRUISE 1 GL15682CA10886 22019 ENROUTE WINDOW CRACKED, REPLACED R2 WINDOW REF 56-12-11 AND AJUSTED AND OPS CK GOOD. 2L73 4F A3WE 20050524000722005052400072SW 2005 5 24 M0501 120050103A5610 WINDSHIELD SWRNGNSA227 SA227AC 8780603SW COCKPIT CRACKED A BSAAI CABIN DEPRESSURIZATION O OTHER DEDESCENT 1 NM053114G AC583 NR 1 WINDSHIELD CRACKED AT DESCENT FROM CRUISE, CREW DEPRESSURIZED AIRCRAFT, DESCENDED TO PROPER ALTITUDE, AND DIVERTED TO LAND WITHOUT INCIDENT. OAT WAS -40C, WINDSHIELD HEAT WAS ON "LOW". MAINTENANCE FOUND INNER PANE EXTENSIVELY CRACKED. 2L72 4T RTA8SW 20050524000972005052400097NM 2005 5 24 UPS05444424 120050407A5315 FLOORBEAM BOEING747 747283B 1384867NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 RT BS 340 U/D FLOORBEAM FOUND 2EA FASTENER HOLES CRACKED AT STR 12 RT REFER TO ATTACH SKETCH FOR DETAILS, CRACK LENGTH FS WEB 1/4", 1/8" AND THROUGH THICKNESS FLOORBEAM CHORD 0.060". BS 340 RT U/D FLOORBEAM CHORD REPAIRED AT RBL 48" TO RT MOST O/B END AS PER SRM 53-10-07 FIG 23 AND FRAME REPAIRED AS PER HX RS R53-12-35291 AND UPS EO B747-5310-22113-A CONTINUE INSP PER BSB 53A2265. 2L74 4F A20WE 20050524001632005052400163SO 2005 5 24 TZR2005F00020 220050421A8530 EXHAUST VALVE CESSNA402 402B 207590PCE CONT O520 TSIO520E 17040SO MCAULY3AF32C3AF32C505 GL ENGINE BURNED E TZRAK NONE O OTHER ININSP/MAINT 1 SW05404TE 402B0834 THE EXHAUST VALVE HAD A SMALL PORTION BURNED OFF. THIS IS AN ECI CYLINDER. (K) 1L72 3O3 O A7CE E8CE 5 CP22EA 20050524001772005052400177EA 2005 5 24 VTZA200500073 120050505A5210601R5211680 DOOR FRAME CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27625BR 7214 PAX DOOR FRAME TOP RADIUS CRACKED AT 1 INCH IN LENGTH FORWARD OF DATUM 1 AT FS 320.90. 2L72 4F RTA21EA 20050524001852005052400185WP 2005 5 24 MWEA050041 120050507A2560 LANYARD DOUG DC9 DC982 3022082WP SERVICE DOOR DETACHED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 FORWARD GALLEY SERVICE DOOR SLIDE COVER LANYARD CAME DETACHED. RE-INSTALLED LANYARD. 2L72 4F A6WE 20050524001892005052400189SO 2005 5 24 C2XA05IA070 120050503A261147359713 SMOKE DETECTOR EMB 145 EMB145XR 3260214SO CARGO BAY MALFUNCTIONED A C2XAK NONE N FALSE WARNING CRCRUISE 1 SW27241285796 5796 145700 MKE - FLIGHT 2656, THE CREW REPORTED A FALSE BAGGAGE SMOKE WARNING IN FLIGHT. THE AIRCRAFT LANDED AT MKE WITHOUT INCIDENT WHERE MAINTENANCE PLACED THE BAGGAGE SMOKE DETECTORS ON MEL 26-15-00 CAT C CTL NUMBER 053533, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED AT IAH ON FLIGHT 2743 WHERE MAINTENANCE REMOVED AND REPLACED BOTH BAGGAGE SMOKE DETECTORS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20050524001902005052400190SO 2005 5 24 C2XA05IA069 120050503A261147359713 SMOKE DETECTOR EMB 145 EMB145XR 3260214SO CARGO BAY MALFUNCTIONED A C2XAK NONE N FALSE WARNING CRCRUISE 1 SW27241285796 5796 145700 MKE - FLIGHT 2656, THE CREW REPORTED A FALSE BAGGAGE SMOKE WARNING IN FLIGHT. THE AIRCRAFT LANDED AT MKE WITHOUT INCIDENT WHERE MAINTENANCE PLACED THE BAGGAGE SMOKE DETECTORS ON MEL 26-15-00 CAT C CTL NUMBER 053533, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED AT IAH ON FLIGHT 2743 WHERE MAINTENANCE REMOVED AND REPLACED BOTH BAGGAGE SMOKE DETECTORS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20050524001912005052400191NM 2005 5 24 SWAA051334 120050505A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 14R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050524001932005052400193NM 2005 5 24 SWAA051336 120050505A53306545777 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 976, STR 21L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050524001942005052400194NM 2005 5 24 SWAA051337 120050505A33106937306 PANEL BOEING737 7373H4 1384600NM COCKPIT FOD A SWAAC ABORTED TAKEOFF C F.O.D. TOTAKEOFF 1 SW29630WN 27705 ABORTED TAKEOFF. ALL COCKPIT FWD INSTRUMENT PANEL LIGHTS ILLUMINATED. REMOVED FOD FROM LANDING GEAR INDICATOR LIGHTS PANEL. OPS CHECK GOOD PER MM. 2L72 4F RTA16WE 20050524001952005052400195NM 2005 5 24 SWAA051338 120050505A3350101073 LENS BOEING737 7373H4 1384600NM L1 DOOR MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29637SW 27710 L1 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20050524001972005052400197 2005 5 24 SWAA051340 420050505A2565D31354 SLIDE BOEING737 7373A4 1384585NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29679AA 23291 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050524002032005052400203SO 2005 5 24 LR7A05046 120050428A5320 GUSSET LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK PER JOB CARD HC5311 RIGHT YELLOW STANCHEON TOP GUSSET PLATE AT FS 858 RT FOUND CRACKED AT WL 260, RBL 61. GUSSET PLATE REPLACED IAW SMP583 CHP 51-60 & 51-70, FS 858 RIGHT. 2H74 4T A1SO 20050524002042005052400204SO 2005 5 24 LR7A05047 120050428A5320 CAP LKHEED382 382G 526414USO FUSELAGE DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK PER JOB CARD HC5313 RIGHT CHINE CAP FS 517-597 REMOVAL FOUND WITH EXCESS HOLES QTY 4 EA UPON REMOVAL AT WL 146, RBL 58. RIVETS INSTALLED IAW LAC MEA 382-53-05-040 ED 05-009-5, FS 517-597. 2H74 4T A1SO 20050524002052005052400205SO 2005 5 24 LR7A05048 120050428A5512 SKIN LKHEED382 382G 526414USO HORIZ STAB CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK PER JOB CARD HC5511 LEFT HORIZONTAL STAB LOWER SURFACE SKIN CRACKED AT HSS200, FS 1093, WL 272. REPAIR CARRIED OUT IAW SMP583 FIG 55-20-06. 2H74 4T A1SO 20050524002062005052400206SO 2005 5 24 LR7A05049 120050428A5512 SKIN LKHEED382 382G 526414USO HORIZ STAB CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK PER JOB CARD HC5511 LEFT HORIZONTAL STAB UPPER SURFACE SKIN AND INNER HAT SECTION FLANGE CRACKED AT HSS200, FS 1093, WL 280. REPAIR CARRIED OUT IAW SMP583 FIG 55-20-06. 2H74 4T A1SO 20050524002072005052400207SO 2005 5 24 LR7A05050 120050428A5512 SKIN LKHEED382 382G 526414USO HORIZ STAB CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK PER JOB CARD HC5511 LEFT HORIZONTAL STAB LOWER SURFACE SKIN CRACKED AT HSS220, FS 1093, WL 272. REPAIR CARRIED OUT IAW SMP583 FIG 55-20-06. 2H74 4T A1SO 20050524002092005052400209SO 2005 5 24 LR7A05052 120050428A5310 WINDOW FRAME LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK PER JOB CARD HC5321 RIGHT CLEAR VISION WINDOW FRAME CRACKED AT LOWER FWD CORNER FS 105 WL 230. REPAIR CARRIED OUT IAW DWG R05-009-02 & LAC MEA 382-53-05-038, FS 105 WL 230. 2H74 4T A1SO 20050524002102005052400210SO 2005 5 24 LR7A05053 120050428A5330 SKIN LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK PER JOB CARD HC5321 CRACK FOUND ALONG RIVET HEAD AT RIGHT FS 577 RBL 41 BELLY SKIN EXTERIOR, WL 152. REPAIR CARRIED OUT IAW SMP583 FIG 51-140-12, FS 577 RBL 41. 2H74 4T A1SO 20050524002112005052400211SO 2005 5 24 LR7A05054 120050428A5311LS40107 FRAME LKHEED382 382G 526414USO FUSELAGE CORRODED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK PER JOB CARD HC5313 FOUND CABIN RING SEGMENT CORRODED AT FS 397 WL 140-146 BL 63R. REPAIR CARRIED OUT IAW SMP583 CHP 51-140, RIGHT FS 397. 2H74 4T A1SO 20050524002132005052400213SO 2005 5 24 LR7A05056 120050428A5311LS54087 FRAME LKHEED382 382G 526414USO FUSELAGE CORRODED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK NR 2001 ACCOMPLISHMENT FOUND LT RING SEGMENT CORRODED FS 757E AT WL 140-146, AND NUMEROUS EXCESS HOLES AT WL 160. REPAIR CARRIED OUT IAW SMP583 CHP 51-140-23, FS 757E WL 140-146. 2H74 4T A1SO 20050524002142005052400214SO 2005 5 24 LR7A05057 120050428A5310 WINDOW FRAME LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK PER JOB CARD HC5321 LEFT CLEAR VISION WINDOW FRAME CRACKED AT LOWER FWD CORNER FS 105 WL 230. REPAIR CARRIED OUT IAW DWG R05-009-01 & LAC MEA382-53-05-037, FS 105 WL 230. 2H74 4T A1SO 20050524002182005052400218SO 2005 5 24 LR7A05061 120050428A5311 FRAME LKHEED382 382G 526414USO FUSELAGE DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK INTERIOR FUSELAGE FRAMES FOUND EXCESS & ELONGATED HOLES AT LT & RT FS 637 WL 162 BL 68. FRAME REPAIRED IAW R05-009-03, LAC MEA 382-53-05-045, LEFT & RIGHT FS 637 WL 162 BL 68. 2H74 4T A1SO 20050524002192005052400219SO 2005 5 24 LR7A05062 120050428A5311 FRAME LKHEED382 382G 526414USO FUSELAGE DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK INTERIOR FUSELAGE FRAMES FOUND EXCESS & ELONGATED HOLES AT RIGHT FS 647 WL 162 BL 68. FRAME REPAIRED IAW R05-009-03, LAC MEA 382-53-05-045, RIGHT FS 647 WL 162 BL 68. 2H74 4T A1SO 20050524002202005052400220SO 2005 5 24 LR7A05063 120050428A5311 FRAME LKHEED382 382G 526414USO FUSELAGE DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK INTERIOR FUSELAGE FRAMES FOUND EXCESS & ELONGATED HOLES AT LEFT & RIGHT FS 657 WL 162 BL 68. FRAME REPAIRED IAW R05-009-03, LAC MEA 382-53-05-045, LT & RT FS 657 WL 162 BL 68. 2H74 4T A1SO 20050524002222005052400222SO 2005 5 24 LR7A05065 120050428A5311 FRAME LKHEED382 382G 526414USO FUSELAGE DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK INTERIOR FUSELAGE FRAMES FOUND EXCESS & ELONGATED HOLES AT LT & RT FS 677 WL 162 BL 68. FRAME REPAIRED IAW R05-009-03, LAC MEA 382-53-05-045, LT & RT FS 677 WL 162 BL 68. 2H74 4T A1SO 20050524002232005052400223SO 2005 5 24 LR7A05066 120050428A5311 FRAME LKHEED382 382G 526414USO FUSELAGE DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK INTERIOR FUSELAGE FRAMES FOUND EXCESS & ELONGATED HOLES AT RT FS 687 WL 162 BL 68. FRAME REPAIRED IAW R05-009-03, LAC MEA 382-53-05-045, RT FS 687 WL 162 BL 68. 2H74 4T A1SO 20050524002242005052400224SO 2005 5 24 LR7A05067 120050428A5311 FRAME LKHEED382 382G 526414USO FUSELAGE DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK INTERIOR FUSELAGE FRAMES FOUND EXCESS & ELONGATED HOLES AT LT FS 324E WL 162 BL 68. FRAME REPAIRED IAW R05-009-04, LAC MEA 382-53-05-046, LT FS 324E WL 162 BL 68. 2H74 4T A1SO 20050524002262005052400226SO 2005 5 24 LR7A05069 120050428A5311 FRAME LKHEED382 382G 526414USO FUSELAGE DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK INTERIOR FUSELAGE FRAMES FOUND EXCESS & ELONGATED HOLES AT LT & RT FS 290 WL 162 BL 68. FRAME REPAIRED IAW R05-009-04, LAC MEA 382-53-05-046, LT & RT FS 290 WL 162 BL 68. 2H74 4T A1SO 20050524002272005052400227SO 2005 5 24 LR7A05070 120050428A5311 FRAME LKHEED382 382G 526414USO FUSELAGE DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK INTERIOR FUSELAGE FRAMES FOUND EXCESS & ELONGATED HOLES AT LEFT FS 305 WL 175 BL 77. FRAME REPAIRED IAW R05-009-04, LAC MEA 382-53-05-046, LT FS 305 WL 175 BL 77. 2H74 4T A1SO 20050524002282005052400228SO 2005 5 24 LR7A05071 120050428A5311 FRAME LKHEED382 382G 526414USO FUSELAGE DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK INTERIOR FUSELAGE FRAMES FOUND EXCESS & ELONGATED HOLES AT LT FS 250 WL 162 BL 68. FRAME REPAIRED IAW R05-009-04, LAC MEA 382-53-05-046, LT FS 250 WL 162 BL 68. 2H74 4T A1SO 20050524002302005052400230SO 2005 5 24 LR7A05073 120050428A5311 FRAME LKHEED382 382G 526414USO FUSELAGE DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK INTERIOR FUSELAGE FRAMES FOUND EXCESS & ELONGATED HOLES AT LT & RT FS 284 WL 162 BL 68. FRAME REPAIRED IAW R05-009-04, LAC MEA 382-53-05-046, LT & RT FS 284 WL 162 BL 68. 2H74 4T A1SO 20050524002312005052400231SO 2005 5 24 LR7A05074 120050428A5311 FRAME LKHEED382 382G 526414USO FUSELAGE DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK INTERIOR FUSELAGE FRAMES FOUND EXCESS & ELONGATED HOLES AT LT FS 290 WL 176 BL 77. FRAME REPAIRED IAW R05-009-04, LAC MEA 382-53-05-046, LEFT FS 290 WL 176 BL 77. 2H74 4T A1SO 20050524002342005052400234SO 2005 5 24 LR7A05077 120050428A5311 FRAME LKHEED382 382G 526414USO FUSELAGE DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK INTERIOR FUSELAGE FRAMES FOUND EXCESS & ELONGATED HOLES AT RIGHT FS 324 WL 162 BL 68. FRAME REPAIRED IAW R05-009-04, LAC MEA 382-53-05-046, RIGHT FS 324 WL 162 BL 68. 2H74 4T A1SO 20050524002362005052400236SO 2005 5 24 LR7A05079 120050428A5311 FRAME LKHEED382 382G 526414USO FUSELAGE DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK INTERIOR FUSELAGE FRAMES FOUND EXCESS & ELONGATED HOLES AT LT FS 437 WL 162 BL 68. FRAME REPAIRED IAW R05-009-05, LAC MEA 382-53-05-047, LEFT FS 437 WL 162 BL 68. 2H74 4T A1SO 20050524002422005052400242SO 2005 5 24 LR7A05085 120050428A5311 FRAME LKHEED382 382G 526414USO FUSELAGE DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK INTERIOR FUSELAGE FRAMES FOUND EXCESS & ELONGATED HOLES AT LEFT FS 414 WL 162 BL 68. FRAME REPAIRED IAW R05-009-06, LAC MEA 382-53-05-048, LT FS 414 WL 162 BL 68. 2H74 4T A1SO 20050524002462005052400246SO 2005 5 24 LR7A05089 120050428A5311 FRAME LKHEED382 382G 526414USO FUSELAGE DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK INTERIOR FUSELAGE FRAMES FOUND EXCESS & ELONGATED HOLES AT LEFT FS 457 WL 162 BL 68. FRAME REPAIRED IAW R05-009-06, LAC MEA 382-53-05-048, LEFT FS 457 WL 162 BL 68. 2H74 4T A1SO 20050524002472005052400247SO 2005 5 24 LR7A05090 120050428A5311 FRAME LKHEED382 382G 526414USO FUSELAGE DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK INTERIOR FUSELAGE FRAMES FOUND EXCESS & ELONGATED HOLES AT LEFT FS 470 WL 162 BL 68. FRAME REPAIRED IAW R05-009-06, LAC MEA 382-53-05-048, LEFT FS 470 WL 162 BL 68. 2H74 4T A1SO 20050524002502005052400250NM 2005 5 24 05FDEA01226 120050506A5347 SEAT TRACK BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25254FE 20936 SEAT TRACK BL 0 STA 720F HAS AN EXISTING SPLICE REPAIR AND DOES NOT MEET REQUIREMENTS OF DWG 2902. REMOVED DAMAGED SECTION OF SEAT TRACK AND INSTALLED NEW SECTION OF TRACK WITH REPAIR ANGLES IAW SRM 51-10-5 FIG 1. 2L73 4F RTA3WE 20050524002572005052400257NM 2005 5 24 UIEA200500051 120050413A3231 DOOR BOEING747 74747UF 1384949NM GE CF6 CF680C2* GL MLG MALFUNCTIONED A UIEAO OTHER J WARNING INDICATION CLCLIMB 1 EA15416MC 32838 RT BODY GEAR DOOR OPENED AFTER RETRACTION WHEN GEAR LEVER PLACED IN OFF POSITION. STATUS MSG GEAR DOOR GEAR MONITOR. GEAR PINS INSTALLED. PRESSURIZED HYD SYSTEM. OPS CHECKED DOOR IAW MM. ALL INDICATIONS OK IN ALL HANDLE POSITIONS. RT BODY GEAR DOOR DID NOT DROP AT ALL. OK FOR SERVICE. ALL SYSTEMS OPS NORMAL. GEAR PINS REMOVED. (K) 2L74 4F4 FRT1384945 E23EA 20050524002592005052400259NM 2005 5 24 UIEA200500053 120050421A5330 SKIN BOEING747 74747UF 1384949NM FUSELAGE DENTED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15412MC 30559 STA 2660-2680, 2 DENTS FOUND ON EXT SKIN. REPORTED DENT WAS REPAIRED IAW SRM. PERFORMED HFEC INSP, NO CRACKS WERE FOUND. AFTER SECONDARY INSP FOUND DENT, CREASE, AND CHAFING 2.5 INCH X 1.5 INCH X 0.050 INCH. DOUBLER REPAIR PERFORMED IAW SRM. (K) 2L74 4F RT1384945 20050524002702005052400270NM 2005 5 24 UIEA200500062 120050421A5347 SEAT TRACK BOEING747 74747UF 1384949NM GE CF6 CF680C2* GL FUSELAGE DAMAGED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15493MC 29254 MAIN DECK SEAT TRACK DAMAGED AT SAT 1810 NEXT TO SIDE CARGO DOOR. SEAT TRACK REPAIRED IAW SRM. (K) 2L74 4F4 FRT1384945 E23EA 20050524002752005052400275WP 2005 5 24 05FDEA01223 120050506A3620355823255 LOOP DOUG DC10 DC1030F 3023504WP NR 2 SHORTED A FDEAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO25312FE 48300 LEVEL 2, NR 2 MANIFOLD FAIL ALERT DURING CRUISE, MEL 06MAY05. RELEASED FOR SERVICE PER MEL/CDL: 36-23-01-02. NR 2 MANIFOLD FAIL DETECTION LOOP INOP. MX MUST CLEAR ALERT PRIOR TO EACH DISPATCH. DO NOT PRESSURIZE PNEUMATIC SYS NR 2 EXCEPT FOR ENG START. PERFORMED NR 2 PNEU DECAY CHECK IAW M/M 36-00-01-5 CHECKS NORMAL AT THIS TIME. T/S MANIFOLD FAILURE DETECTION SYSTEM PER MD-10 FIM36-23-09. FOUND SENSING ELEMENT LOOP 2 D1-28 B SHORTED. REMOVED AND REPLACED SENSING ELEMENT (P/N 35582-3-255) PER MD-10 MM 36-23-02, OPS CHECK GOOD PER MD-10 MM 31-43-02. A/C OK FOR SERVICE. 2L73 4F RTA22WE 20050524002802005052400280EA 2005 5 24 VTZA200500077 120050508A5315601R3110114 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27625BR 7214 FLOORBEAM AT FS 310 RBL 9 HAS LEVEL 2 CORROSION. 2L72 4F RTA21EA 20050524002812005052400281EA 2005 5 24 VTZA200500079 120050508A5315601R310113 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27625BR 7214 FLOORBEAM AT FS 310 LBL 9 HAS LEVEL 2 CORROSION. 2L72 4F RTA21EA 20050524002832005052400283EA 2005 5 24 VTZA200500076 120050508A5315601R310112 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27625BR 7214 FLOORBEAM AT FS 310 RBL 27 HAS LEVEL 2 CORROSION. 2L72 4F RTA21EA 20050524002842005052400284NM 2005 5 24 05039 120050507A2697 WIRE BOEING747 7472B4B 138481BNM PWA JT9 JT9D7J 52054NE NR 3 NACELLE DAMAGED A KCSAE ENGINE SHUTDOWN N FALSE WARNING DEDESCENT 1 GL23713CK 21099 685779 DURING DESCENT B-LOOP ON NR 3 NACELLE WENT FIRE INDICATION WITH A-INOP. PRECAUTIONARY SHUTDOWN NR 3 ENG. REPAIRED DAMAGED WIRE ON UPPER LOOP BELOW PYLON CLOSE TO CANNON PLUG AND SECURED LOOSE LOOP ASSY AT UPPER I/B BRACKET IAW B747 MM 26-11-02 AND OPS CHECKED OK. 2L74 4F4 FRTA20WE E20EA 20050524002862005052400286NM 2005 5 24 UIEA200500068 120050426A5311 FRAME BOEING747 747228F 1384895NM GE CF6 CF650E2 30018NE FUSELAGE CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15536MC 21576 NOSE WHEEL WELL STRUCTURE ON INTERIOR OF FUSELAGE CHORD CRACKED AT BS 340, WL 200, LBL 10. REPAIRED IAW MFG MM. (K) 2L74 4F4 F A20WE E23EA 20050524002872005052400287NM 2005 5 24 UIEA200500069 120050426A5330 SKIN BOEING747 747228F 1384895NM GE CF6 CF650E2 30018NE FUSELAGE CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15536MC 21576 NR 1 PYLON LT ACCESS DOOR 452BL CUT OUT LOWER EDGE CRACKED. REPAIRED ACCOMPLISHED IAW MFG MM. (K) 2L74 4F4 F A20WE E23EA 20050524002882005052400288NM 2005 5 24 UIEA200500070 120050426A5320 PAN BOEING747 747228F 1384895NM GE CF6 CF650E2 30018NE FUSELAGE CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15536MC 21576 LT SIDE CANTED BULKHEAD AT BS 1245, LBL 60 CLOSURE PAN FOR AILERON CONTROL CABLE FEED THROUGH TO PRESSURE DECK FOUND WITH (2) CRACKED LINES. CLOSURE PAN REPAIRED IAW MFG MM. (K) 2L74 4F4 F A20WE E23EA 20050524002892005052400289EU 2005 5 24 TRBA2005029 120050421A5610NP1588012 WINDSHIELD AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE COCKPIT CRACKED A TRBAA UNSCHED LANDING O OTHER CLCLIMB 1 SO29348AE9981 349 WHILE IN CLIMB, THE FO WINDSHIELD CRACKED. AIRCRAFT RETURNED TO AIRPORT. REPLACED FO WINDSHIELD ASSY. (K) 2H72 4T4 TRTA53EU E20NE 20050524002902005052400290EU 2005 5 24 TRBA2005028 120050420A2611 WARNING SYSTEM AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE COCKPIT ACTIVATED A TRBAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO29355AT 355 WHILE IN TAXI, ELECTRIC SMOKE WARNING ON THE CAP ALONG WITH SMELL IN THE COCKPIT. AIRCRAFT RETURNED TO THE BLOCKS. PERFORMED OPERATIONS CHECK OF SYSTEM AND UNABLE TO DUPLICATE. (K) 2H72 4T4 TRTA53EU E20NE 20050524002922005052400292SO 2005 5 24 2005F00083 120050321A56101159SCB310214 WINDSHIELD GULSTMG1159 G1159A 3970109SO RROYCESPEY SPEY511* 54523EU COCKPIT BROKEN E A UNSCHED LANDING O OTHER CRCRUISE 1 SO198JL 1553 388 WINDSHIELD SHATTERED AT CRUSE. PILOTS FOLLOWED FLIGHT MANUAL PROCEDURES. COMPONENT WAS REPLACED. REASON FOR COMPONENT FAILED IS UNKNOWN AND IS PRESENTLY BEING INVESTIGATED. 2L72 4F4 F A12EA E2EU 20050524003032005052400303NE 2005 5 24 EGRR100526 120050504A67107640000014055 CONTROL TUBE SKRSKYS76 S76B 8143007NE COLLECTIVE CHAFED B EGRRK NONE O OTHER ININSP/MAINT 1 EA0598AE 3959 760322 DURING A/C INSPECTION FOUND COLLECTIVE CONTROL TUBE IN CABIN VERTICAL TUNNEL CHAFFING ON FWD WALL AND RIVET TAILS SECURING TYE WRAP TIEDOWN STRIP, BEYOND ALLOWABLE LIMITS. (.013 1G72 4U H1NE 20050524003042005052400304GL 2005 5 24 YTRR100737 220050505A732323065121 GOVERNOR BELL 206 206B3 1181506SW ALLSN 250C 250C20 03013GL ENGINE INTERMITTENT B YTRAK NONE O OTHER ININSP/MAINT 1 SW033187D 1369 WHEN A LOAD IS APPLIED TO THE ENGINE THE GOVERNOR DROOPS AND WILL NOT RECOVER. 1G71 3U3 U H2SW E4CE 20050524003052005052400305SW 2005 5 24 ALGA100674 120050505A6220204011179003 DRAG BRACE BELL 212 212 1181420SW M/R HEAD CRACKED E ALGAK NONE O OTHER ININSP/MAINT 1 SW03XATVM442 30934 NDT INSPECTION FOUND CRACK OUTSIDE EDGE, BARREL BORE / REPLACED CLEVIS WITH NEW CLEVIS, BY OVERHAUL SHOP. 1G71 4U H4SW 20050524003062005052400306SW 2005 5 24 ALGA100722 120050420A6220406310405101 PITCH LINK BELL 407 407 1182206SW ALLSN 250C 250C47B GL M/R HEAD BINDING E ALGAK NONE O OTHER ININSP/MAINT 1 SW03937AL268 53383 BINDING, ROUGH AXIAL PLAY BEYOND MAX. REPLACED WITH NEW BY FIELD MAINTENANCE. 1G71 3U3 UO H2SW E1GL 20050524003072005052400307NM 2005 5 24 2005UALA00329 120050412A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29585UA 26709 EXTERNAL FUSELAGE SKIN HAS BLIND FASTENER INSTALLED AT APPROX BS 746 BETWEEN STR 24L AND STR 25L. MAJOR REPAIR ACCOMPLISHED. REMOVED BLIND FASTENERS, CUT OUT SKIN DAMAGE AND INSTALLED DOUBLER AND FILLER. 2L72 4F4 FRTA2NM E17NE 20050524003092005052400309NM 2005 5 24 2005UALA00395 120050426A2997 WIRE BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE RAM AIR TURNIBE BROKEN A UALAK NONE O OTHER ININSP/MAINT 1 WP29658UA54165 27113 RAM AIR TURBINE FAILURE. DURING ROUTINE MAINTENANCE CHECK, A DISCREPANCY WAS NOTICED ON THE RAT SPEED SENSING. UPON FURTHER TROUBLESHOOTING, A WIRE INSIDE THE RAT SPEED SENSOR WAS FOUND BROKEN. AFTER REPAIR, THE RAT TEST WAS COMPLETED SUCCESSFULLY. 2L72 4F4 FRTA1NM E24NE 20050524003102005052400310NM 2005 5 24 2005UALA00396 120050429A2560 PAD BOEING747 747422 1384935NM PWA 4056 PW4056 NE EVAC SLIDE STUCK A UALAK NONE O OTHER ININSP/MAINT 1 WP29118UA 28811 ONE FOAM PAD PACKED UNDERNEATH SLIDE, STUCK TO BOTTLE BAG. 2L74 4F4 FRTA20WE E24NE 20050524003112005052400311NM 2005 5 24 2005UALA00397 120050429A5320 FLOOR SUPPORT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29312UA 23673 AFT PIT RIGHT SIDE FLOOR SUPPORT IS CRACKED UNDER Z-ANGLE INTERCOSTAL IS CRACKED IN RADIUS AT STA 870 STR 26R. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE AND INSTALLED REPAIR ANGLE. 2L72 4F4 FRTA16WE E2GL 20050524003122005052400312NM 2005 5 24 2005UALA00398 120050502A5322 SHEAR TIE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29586UA 26710 CIRCUMFERENTIAL FRAME SHEAR TIE CORRODED AT STA 1460, BETWEEN STR 27L AND 28L. FABRICATED AND INSTALLED A NEW SHEAR TIE. 2L72 4F4 FRTA2NM E17NE 20050524003172005052400317NM 2005 5 24 2005UALA00402 120050501A2497 WIRE BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE CABIN DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29928UA 26651 D3732 HAS MULTIPLE WIRES DAMAGED FROM ARCING. CONNECTOR IS IN CEILING, INBOARD OF FWD LAV. REPLACED DISCONNECT D3732 AND REPAIRED DAMAGED WIRING. SECURED BUNDLE. AN EG CALLOUT WAS ISSUED TO LOOK AT SIX ADDITIONAL AIRPLANES. CHAFING WAS FOUND ON HARNESS INSULATION ON ONE AIRPLANE BUT NO DAMAGE ON WIRE ITSELF. CALLOUT WILL BE EXTENDED TO ENTIRE FLEET TO ENSURE PROBLEM DOES NOT EXIST ON ANY OTHER AIRCRAFT. 2L72 4F4 FRTA16WE E2GL 20050524003232005052400323NE 2005 5 24 2005UALA00411 220050504A7200 COMPRESSOR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE LT & RT ENGINE STALLED A UALAK NONE R PARTIAL RPM/PWR LOSS CRCRUISE 1 WP29414UA 472 CREW HAD MOMENTARY ENGINE STALL ECAM FOR BOTH ENGINES. EVENT LASTED 2 SECONDS AND SUBSEQUENT PARAMETERS WERE NORMAL. CAUSED BY A COMBINATION OF UNIQUE FLIGHT CONTROL INPUT , AND ENVIRONMENTAL FACTORS , AND SPECIFIC ENGINE CONDITIONS . THE FIX FOR THIS PROBLEM WAS AN ENGINE CHANGE. RISK ANALYSIS BY AIRBUS AND IAE SHOW RISK OF RE-OCCURRENCE OF THIS EVENT AS EXCEEDINGLY LOW. HOWEVER, TO FURTHER REDUCE RISK DOWN TO ZERO, ENGINE CONTROL SOFTWARE UPGRADES FROM ENGINE OEM IS DUE IN 2006. 2L72 4F4 FRTA28NM E40NE 20050523003242005052300324NM 2005 5 23 DHL2005740005 120050327A2710 STRUCTURE BOEING727 7272Q9 138448MNM AILERON TAB DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 RT WING INBD AILERON TAB IS DENTED ON LOWER SURFACE WING STA 430 WBL 269. CUT OUT DENT AT RT WING INBD AILERON TAB LOWER SURFACE APPROX 1 INCH DIA. FABRICATED FILLER APPROX 1 INCH DIA AND DOUBLER APPROX 3 INCH DIA FROM .010 2024T3 PO NR 9912184, BONDED, CURED, CLEANED, PRIMED AND SEALED IAW B727 SRM 51-40-20 FIG 30. 2L73 4F RTA3WE 20050523003272005052300327NM 2005 5 23 AALA20050292 120050429A3350 LIGHT BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW2139365 24046 DFW - EMERGENCY LIGHT IN COCKPIT INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY IN COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050523003292005052300329WP 2005 5 23 AALA20050299 120050501A335050030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21271AA 49293 SFO - OVERWING EMERGENCY UPPER DOOR LIGHTS AT ROW 20ABCD INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD OVERWING EMERGENCY LIGHTS AT ROW 20ABCD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050523003302005052300330SO 2005 5 23 RAIA00504014 120050412A2120 SMOKE EMB 145 EMB145 3260210SO CABIN DETECTED A RAIAD RETURN TO BLOCK BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TXTAXI/GRND HDL 1 CE03804HK 145082 FLT 3519 - PIT - LAV SMOKE ALARM SMOKE VISIBLE AND SMELL IN CABIN. MAINTENANCE COULD NOT DUPLICATE MALFUNCTION. DURING GROUND ENGINE RUN AND LAV SMOKE TEST. 2L72 4F RTT00011AT 20050523003512005052300351NM 2005 5 23 SWAA051332 120050504A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 DURING SCHEDULED SERVICE CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS AT BS 730, STR 23L & STR 24L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050523003762005052300376EA 2005 5 23 ASOA05268 120050326A3350362624 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27913EV 7731 DURING HANGAR MAINTENANCE IN BTR, THE EMERGENCY FLOOR TRACK LIGHTING BETWEEN ROWS 2 C/D TO 6 C/D WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR TRACK FLEX LAMP BETWEEN ROWS 2 C/D TO 6 C/D. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050523003862005052300386NM 2005 5 23 USAA050461 120050403A5320 TIE CLIP BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19442US40275 24841 CLT - FOUND TIE CLIP CRACKED .4 INCH, STATION 663 STRINGER 10R. REPLACED TIE CLIP IAW SRM 51-10-02. (M) 2L72 4F RTA16WE 20050523003912005052300391EU 2005 5 23 ASOA05285 120050311A5320 FLOOR SUPPORT AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27635AS 372 DURING A C-CHECK IN YUL THE LEF Z-FLOOR SUPPORT AT FRAME 39-40 AND THE RIGHT Z-FLOOR SUPPORT BETWEEN FRAME 39 AND 41 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT Z-FLOOR SUPPORT AT FRAME 39-40 AND THE RIGHT Z-FLOOR SUPPORT BETWEEN FRAME 39 AND 41 IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20050523003922005052300392NM 2005 5 23 USAA050462 120050403A5320 SPLICE BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19440US39307 24811 CLT - FOUND SPLICE CRACKED .75 INCH, STATION 908M STRINGER S4L. REPLACED SPLICE IAW SRM 51-40-02. (M) 2L72 4F RTA16WE 20050523003942005052300394EU 2005 5 23 ASOA05284 120050311A5320 FLOOR SUPPORT AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27635AS 372 DURING A C-CHECK IN YUL, THE LEFT AND RIGHT FLOOR SUPPORTS BETWEEN FRAME 36/38 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT FLOOR SUPPORTS BETWEEN FRAME 36/38 IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20050523003962005052300396EA 2005 5 23 ASOA05274 120050331A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27870AS 7530 DURING HANGAR MAINTENANCE IN BTR, THE SECOND FROM THE FRONT EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE SECOND FROM THE RONT EMERGENCY CEILING LIGHT. OPERATIONAL CHECKS GOOD. (M) 2L72 4F RTA21EA 20050523003972005052300397EU 2005 5 23 ASOA05281 120050311A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27635AS 372 DURING A C-CHECK IN YUL, THE RIGHT SEAT TRACK BETWEEN FRAME 39 AND 40 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT SEAT TRACK BETWEEN FRAME 39 AND 40 IAW SRM 51-25-04. (M) 2H72 4T RTA53EU 20050523003992005052300399NM 2005 5 23 USAA050457 120050329A5315 FLOORBEAM BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19440US39307 24811 CLT - FOUND FLOORBEAM CORRODED .5 INCH DIAMETER, STATION 312 BL 0 TO BL 10 RT. SPLICED IN NEW T-CAP IAW SRM 53-10-51. (M) 2L72 4F RTA16WE 20050523004032005052300403NM 2005 5 23 USAA050449 120050401A5320 ANGLE BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19442US40275 24841 CLT - FOUND TRANSITON ANGLE 1 INCH BY 9 INCH CORROSION, AFT CARGO TRANSITION ANGLE STATION 727F TO 827. FABRICATED AND INSTALLED Z ANGLE SPLICE IAW SRM 51-10-02. (M) 2L72 4F RTA16WE 20050523004052005052300405NM 2005 5 23 USAA050451 120050401A5320 TIE CLIP BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19440US39307 24811 CLT - FOUND TIE CLIP CRACKED, STATION 706 STRINGER 11R. FABRICATED AND INSTALLED NEW TIE CLIP IAW SRM 51-40-02. (M) 2L72 4F RTA16WE 20050523004102005052300410NM 2005 5 23 USAA050448 120050401A5330 SKIN BOEING737 737401 1384701NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19406US46850 23876 CLT - FOUND SKIN CRACKED 1.3 INCH, STATION 500 STRINGER 17L. INSTALLED DOUBLER IAW EA 87256A. (M) 2L72 4F RTA16WE 20050524000032005052400003WP 2005 5 24 AALA20050296 120050430A3230 CYLINDER DOUG DC9 DC982 3022082WP NLG INOPERATIVE A AALAO OTHER O OTHER APAPPROACH 1 SW2173444 49470 DURING APPROACH INTO BWI, UNABLE TO EXTEND NOSE GEAR. ACCOMPLISHED EMERGENCY GEAR EXTENSION PROCEDURES. LANDED BWI WITHOUT INCIDENT. AIRCRAFT INSPECTED AND FERRIED TO DCA FOR REPAIRS. REPLACED NOSE LANDING GEAR BUNGEE CYLINDER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050524000042005052400004WP 2005 5 24 AALA20050298 120050501A3350 CONNECTOR DOUG DC9 DC983 3022083WP EMERGENCY LIGHT DISCONNECTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21598AA 53288 SFO - AFT GALLEY DOOR SIDEWALL EMERGENCY LIGHT INOPERATIVE. REPINNED CANNON PLUGS FOR AFT GALLEY DOOR SIDEWALL EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050524000322005052400032SO 2005 5 24 TZR2005F00017 220050411A8530AEC520TI01 CYLINDER CESSNA401 401A 207590DCE CONT O520 GTSIO520C 17032SO NR 2 ENGINE CRACKED E TZRAK NONE O OTHER ININSP/MAINT 1 SW05409TE729 401A0118 519510 CRACKED FROM EXHAUST VALVE TO TOP SPARK PLUG. ECI CYLINDER. (SW05200507950) (K) 1L72 3O3 O A7CE E7CE 20050524000442005052400044NM 2005 5 24 BJNA050301 120050316A33506104781 BATTERY PACK BOEING737 737282 13844ATNM EMERGENCY LIGHT DISCHARGED A BJNAK NONE L NO TEST ININSP/MAINT 1 WP11233TM 23043 RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED THE RIGHT OVERWING EXIT LIGHT BATTERY IAW 33-51-21. (M) 2L72 4F RTA16WE 20050524000552005052400055CE 2005 5 24 TIM2005F00004 120050420A261230215 FIRE DETECTOR BEECH 99 99A 1154003CE PWA PT6 PT6A27 52043EA RT ENGINE CONTAMINATED E TIMAO OTHER N FALSE WARNING CRCRUISE 1 NM0799GH 35749 U112 THE FIRE DETECTOR WARNING LIGHT ILLUMINATED IN FLIGHT. MOISTURE WAS THE PROBABLE PROBLEM. AFTER TAXI THE LIGHT EXTINGUISHED. NOT OTHER PROBLEM WITH FIRE DETECTION SYSTEM WAS FOUND. (K) 1L72 3T4 T A14CE E4EA 20050524000602005052400060SW 2005 5 24 MR0510 120050328A2910 LINE FRCHLDSA227 SA227CC 3377522SW HYD SYSTEM CRACKED A BSAAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 NM05159MC AC728B JUST BEFORE LANDING, HYDRAULIC VAPOR/SMOKE NOTED IN CABIN AND COCKPIT. AIRCRAFT LANDED WITHOUT INCIDENT, ENGINES SHUTDOWN AND PAX DEPLANED. MAINTENANCE FOUND FAILED HYDRAULIC LINE IN WING ROOT THAT SPRAYED FLUID INTO AIR CYCLE MACHINE INTAKE WHICH TRANSFERRED VAPOR TO CABIN. 2L72 4T RTA18SW 20050524000732005052400073NM 2005 5 24 DHL2005740007 120050323A5330 SKIN BOEING727 7272Q9 138448MNM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 FWD ENTRY DOOR LOWER CUT OUT SKIN CRACKED. CRACKED CONFIRM BY HFEC NDT. REMOVED FASTENERS PER ACCESS AND CUT OUT DAMAGE AREA (DIM. 2.5 BY 1.5) IAW S/B 727 53A0198. ACCOMPLISHED NDT HFEC AROUND CUT OUT NO CRACKS NOTED IAW B727 NDT MAN. PART 6 51-00-00. FABBED DOUBLER REPAIR AND FILLER IAW SB727-53A0198. TREATED AND PRIMED BARE METAL AND FILLER AND DOUBLER PRIMED. DOUBLER REPAIR IAW B727 SRM 51-10-2, COUNTER SINK WASHER REPAIR INSTALLED IAW B727 SRM 51-30-8 FIG 4. INSTALLED DOUBLER AND FILLER AT FWD ENTRY DOOR LWR CUT OUT IAW SB727-53A0198. 2L73 4F RTA3WE 20050524000762005052400076NM 2005 5 24 DHL2005740010 120050324A5754 RIB BOEING727 7272Q9 138448MNM NR 4 SLAT DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 NR 4 SLAT CRACKED AT ACTUATOR IB RIB. REMOVED NR 4 SLAT TO FOM SHEET METAL REPAIR IAW B727 MM 27-81-11. REMOVED ACCESS PANEL IAW B727 SRM 51-30-2. REMOVED FASTENERS FOR REPAIR AND RIBS IAW B727 SRM 51-30-2. FABRICATED NEW RIBS IB AND OB MAT USED 2024T3 .040 PO NR 9001938 DIM. 15" BY 6" IAW B727 SRM 51-20-1 AND 57-50-2 FIG 2. ALODINED AND PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED NEW RIBS IAW B727 SRM 51-20-1 AND 57-50-2 FIG 2. OK TO CLOSE ACCESS PANEL. INSTALLED ACCESS PANEL IAW B727 SRM 51-30-2. REINSTALLED NR 4 SLAT IAW B727 MM. VOPS/LEAK CHECK GOOD. 2L73 4F RTA3WE 20050524000802005052400080NM 2005 5 24 ASMF200505004 120050503A273090G623 SWITCH DOUG MD80 MD83 3023681NM LT ELEVATOR FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23861LF288 49826 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF LEFT ELEVATOR POWER ON LIGHT DID NOT TURNED ON DURING FLIGHT CONTROL TESTS. ELEVATOR WAS CHECKED PER FREE MOVEMENT, ACCUMULATOR PRESSURE AND HYDRAULIC QUANTITY WERE CORRECT. LIGHT REPORT WAS DEFERRED IAW MEL 27-14. DURING OVERNIGHT SERVICE ELEVATOR PRESSURE SWITCH WAS REPLACED IAW MM 27-30-12, TESTED CORRECT. 2L72 4F RT 20050524000832005052400083NM 2005 5 24 DHL2005740013 120050325A5320 ANGLE BOEING727 7272Q9 138448MNM NLG WW CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 NOSE WW STA 259 LBL 3 L-ANGLE IS CRACKED ABOVE PRESSURE PANELS. REMOVE ANGLE AT NOSE WW STA 259 LBL 3 IAW B727 SRM 51-30-2. FABRICATED NEW ANGLE REPAIR MAT. USED 2024T3 .040 PO NR 9001938 DIM 7" BY 1 1/2" IAW B727 SRM 51-20-1 AND 53-10-2 FIG 1. ALODINED AND PRIMED AREA AND PART IAW B727 SRM 51-10-6. INSTALLED NEW ANGLE IAW B727 SRM 51-20-1 AND 53-10-2 FIG 1. 2L73 4F RTA3WE 20050524000842005052400084EA 2005 5 24 COMA0560281 120050429A3230750005000 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA MLG MALFUNCTIONED A COMAO OTHER J WARNING INDICATION CLCLIMB 1 SO01491CA2501 257 7756 FLIGHT 5863 - LANDING GEAR DISAGREE WARNING. REPLACED THE MLG SELECTOR VALVE. 2L72 4F RTA21EA 20050524000902005052400090NM 2005 5 24 DHL2005740015 120050327A5347 SEAT TRACK BOEING727 7272Q9 138448MNM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 MAIN CABIN SEAT TRACK BS 344 TO BS 480 RBL 45.5 DAMAGED. REMOVED SEAT TRACK FROM BS 344 TO 480 RBL 45.5 IAW B727 SRM 51-30-2. FABRICATED NEW SEAT TRACK P/N BAC1520-792 PO NR 9001329 DIM. 12 FT IAW B727 SRM 53-10-2 FIG 1 AND 51-30-5 AND DWG NR 2902, TREATED AND PRIMED NEW SEAT TRACK IAW B727 SRM 51-10-2. INSTALLED NEW SEAT TRACK AT BS 344 TO 480 RBL 45.5 IAW B727 SRM 51-30-5 AND DWG NR 2902. 2L73 4F RTA3WE 20050524001002005052400100NM 2005 5 24 UPS05444427 120050406A5311 FRAME BOEING747 747283B 1384867NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 NR 1 L MED CUTOUT BS 488 FRAME WEB FOUND CRACK AT DOOR STOP NR 1 AREA APPROX 0.5" LONG EXTEND BEYOND DOOR STOP SUPPORT FTG. CRACK LENGTH 1/2 INCH. M/D NR 1L MED CUTOUT BS 488 FRAME WEB REPAIRED BETWEEN STR 23 TO STR 30 AS PER SRM 53-10-04 FIG 92. 2L74 4F A20WE 20050524001022005052400102NM 2005 5 24 DHL2005740016 120050327A5347 SEAT TRACK BOEING727 7272Q9 138448MNM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 MAIN CABIN SEAT TRACK BS 344 TO 480 RBL 24.75 DAMAGED. REMOVED AND REPLACED NEW SEAT TRACK AT BS 344 TO BS 480 RBL 24.75 AND FABRICATED NEW SEAT TRACK P/N BAC1520-792 PO NR 9001767 DIM 12 FT IAW B727 SRM 53-10-2 FIG 1 AND 51-30-5 AND DWG NR 2902 VENTURA AEROSPACE. TREATED AND PRIMED SEAT TRACK IAW B727 SRM 51-10-2. 2L73 4F RTA3WE 20050524001042005052400104NM 2005 5 24 SB05056 120050507A3397 SOCKET BOEING737 7374B7 1384702NM ROW 25 SHORTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19784AU 25023 FOUND EMERGENCY LIGHTS AT SEATS 24 AND 25, AND THE RIGHT AFT SERVICE DOOR INOPERATIVE. MAINTENANCE FOUND AN OPEN FUSE IN THE BATTERY CHARGER AND THE ROW 25 LIGHT SOCKET SHORTED. THE SOCKET WIRING WAS REPAIRED AND THE FUSE REPLACED. 2L72 4F RTA16WE 20050524001062005052400106EU 2005 5 24 SA05051 120050517A3350 LIGHT AIRBUS320 A320214 3930316EU PASSENGER CABIN FAULTY A USAAK NONE L NO TEST ININSP/MAINT 1 EA19104UW 863 CLT - FLOOR LEVEL EMERGENCY EXIT IDENTIFIER WAS FOUND INOPERATIVE AT THE L-1 DOOR. MAINTENANCE REPLACED THE EXIT IDENTIFIER LIGHT ASSEMBLY, FIN 90WL1. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20050524001082005052400108NM 2005 5 24 05FDEA01356 120050517A5710ARB74023 SKIN DOUG MD11 MD11 3023602NM LT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE LT WING LOWER SKIN, XORS 455, WITH EXISTING BLEND OUT. BLEND OUT AT LT WING LOWER SKIN, XORS 455 EVALUATED AND FOUND REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG 32 VOL I. 2L73 4F RTA22WE 20050524001162005052400116NM 2005 5 24 QXEA200500835 120050503A2840 ELEMENT DHAV DHC8 DHC8202 2809007NM FUEL TEMP MALFUNCTIONED A QXEAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 NM09349PH 486 SEA - FLIGHT NR 2046, NR 2 FUEL TEMP AT 57 DEGREES ON CLIMB AND CRUISE, RAN CHECKLIST, TEMP REMAINED HIGH. ABOUT 25 DEGREES WARMER THAN NR 1. MAINTENANCE REPLACED FUEL TEMP BULB, NR 2 FUEL HEATER THERMAL ELEMENT IAW MTC 9730002. FUEL TEMP INDICATION CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050524001272005052400127NM 2005 5 24 MWEA050038 120050504A30405887275505 ANTI-ICE SYSTEM BOEING717 717200 1383700NM WINDSHIELD FAILED A MWEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL31902ME 55166 CREW REPORTS WINDOW ANTI-ICE FAIL. REMOVED AND REPLACED WINDSHIELD. 2L72 4F TRA6WE 20050524001662005052400166NM 2005 5 24 05FDEA01211 120050505A52406556975502 GATE BOEING727 727200 138407ENM GALLEY DOOR CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25254FE 20936 GALLEY DOOR LWR FLAPPER ASSY INNER STRUCTURE HAS CORROSION (MAG ALLOY ASSY). REMOVED AND REPLACED GALLEY DOOR LWR GATE IAW OHM 52-16-01. 2L73 4F RTA3WE 20050524001752005052400175EU 2005 5 24 05FDEA01221 120050506A5755 SPOILER AIRBUS310 A310324 3930206EU LT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25802FD 542 DURING C2 CHECK, FOUND AN EXISTING REPAIR ON LEFT WING NR 1 SPOILER TRAILING EDGE. REPAIRED PER SRM 57-70-00. 2L72 4F RTA35EU 20050524001762005052400176EA 2005 5 24 VTZA200500072 120050505A5210601R5211680 DOOR FRAME CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27625BR 7214 PAX DOOR FRAME TOP RADIUS CRACKED AT 1 INCH IN LENGTH FORWARD OF DATUM 1 AT FS 338.90. 2L72 4F RTA21EA 20050524001992005052400199SW 2005 5 24 PNSA050502 120050505A7603 DISC SWRNGNSA227 SA227AC 8780603SW COCKPIT FAULTY A PNSABA EMER. DESCENT UNSCHED LANDING R PARTIAL RPM/PWR LOSS CLCLIMB 1 AL03640PA AC759B ON INTIAL CLIMB RT ENGINE ENCOUNTERED POWER SURGES. PILOT DECLARED EMERGENCY AND RETURNED TO ANC. DURING RETURN PILOT DISCOVERED RT SPEED LEVER HAD MOVED AFT FROM TAKEOFF POSITION. MAINTENANCE CHANGED FRICTION LOCK DISCS ON RT SPEED LEVER AND GROUND RUN ENGINE NORMAL. 2L72 4T RTA8SW 20050524002012005052400201SO 2005 5 24 LR7A05044 120050428A5311LS401010 FRAME LKHEED382 382G 526414USO FUSELAGE DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK PER JOB CARD HC5315 CARGO COMPT RING SEGMENT FOUND NUMEROUS EXCESS HOLES AND PATCH REPAIR AT FS 752E LT CABIN; WL 140-200 & WL 200-265. RING SEGMENT REPLACED IAW SMP583 CHP 51-60 & 51-70 FS 752E WL 146-200 & 200-265 LHS. 2H74 4T A1SO 20050524002162005052400216SO 2005 5 24 LR7A05059 120050428A5330 SKIN LKHEED382 382G 526414USO FUSELAGE WRINKLED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK PER JOB CARD HC5321 AFT FUSELAGE EXTERIOR SKIN WRINKLED AT FS 912-918 WL 220-240 RIGHT. REPAIR CARRIED OUT IAW SMP583 FIG 51-140-12, FS 912-918 WL 220-240 RIGHT. 2H74 4T A1SO 20050524002172005052400217SO 2005 5 24 LR7A05060 120050428A5311 FRAME LKHEED382 382G 526414USO FUSELAGE DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK INTERIOR FUSELAGE FRAMES FOUND EXCESS & ELONGATED HOLES AT LEFT & RIGHT FS 627 WL 162 BL 68. FRAME REPAIRED IAW R05-009-03, LAC MEA 382-53-05-045, LT & RT FS 627 WL 162 BL 68. 2H74 4T A1SO 20050524002292005052400229SO 2005 5 24 LR7A05072 120050428A5311 FRAME LKHEED382 382G 526414USO FUSELAGE DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK INTERIOR FUSELAGE FRAMES FOUND EXCESS & ELONGATED HOLES AT LT & RT FS 337E WL 162 BL 68. FRAME REPAIRED IAW R05-009-04, LAC MEA 382-53-05-046, LT & RT FS 337E WL 162 BL 68. 2H74 4T A1SO 20050524002372005052400237SO 2005 5 24 LR7A05080 120050428A5311 FRAME LKHEED382 382G 526414USO FUSELAGE DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK INTERIOR FUSELAGE FRAMES FOUND EXCESS & ELONGATED HOLES AT LEFT FS 357 WL 162 BL 68. FRAME REPAIRED IAW R05-009-06, LAC MEA 382-53-05-048, LEFT FS 357 WL 162 BL 68. 2H74 4T A1SO 20050524002412005052400241SO 2005 5 24 LR7A05084 120050428A5311 FRAME LKHEED382 382G 526414USO FUSELAGE DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK INTERIOR FUSELAGE FRAMES FOUND EXCESS & ELONGATED HOLES AT LT FS 391 WL 162 BL 68. FRAME REPAIRED IAW R05-009-06, LAC MEA 382-53-05-048, LEFT FS 391 WL 162 BL 68. 2H74 4T A1SO 20050524002432005052400243SO 2005 5 24 LR7A05086 120050428A5311 FRAME LKHEED382 382G 526414USO FUSELAGE DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK INTERIOR FUSELAGE FRAMES FOUND EXCESS & ELONGATED HOLES AT LEFT FS 421 WL 162 BL 68. FRAME REPAIRED IAW R05-009-06, LAC MEA 382-53-05-048, LEFT FS 421 WL 162 BL 68. 2H74 4T A1SO 20050524002442005052400244SO 2005 5 24 LR7A05087 120050428A5311 FRAME LKHEED382 382G 526414USO FUSELAGE DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK INTERIOR FUSELAGE FRAMES FOUND EXCESS & ELONGATED HOLES AT RIGHT FS 424 WL 162 BL 68. FRAME REPAIRED IAW R05-009-06, LAC MEA 382-53-05-048, RIGHT FS 424 WL 162 BL 68. 2H74 4T A1SO 20050524002682005052400268NM 2005 5 24 05FDEA01228 120050509A5320 INTERCOSTAL DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 MAIN DECK, STA 513 LONGERON 27L INTERCOSTAL BOTTOM SIDE FOUND CRACKED ABOUT 0.5 INCH. DISCREPANT INTERCOSTAL REMOVED AS PER SRM 51-31-01 VOL II. NEW INTERCOSTAL LOCATED AND INSTALLED AS PER SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20050524002782005052400278EU 2005 5 24 AWXA200500541 120050403A5320D5348002069601 WEB AIRBUS320 A320232 3930326EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28638AW 455 SAL - MAJOR REPAIR - DURING C-08 CHECK A 7.75 INCH CRACK WAS FOUND ON WEB Y1270 BETWEEN FR 68 AND FR 69. MAINTENANCE REMOVED CRACKED WEB Y1270 FROM FR 68 TO FR 69; FABRICATED A NEW REPLACEMENT WEB PER DWG D53480019; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050524002852005052400285NM 2005 5 24 C1HA200595007 120050505A7711 CONNECTOR BOEING727 727290 138408WNM EPR TRANSDUCER LOOSE A C1HAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL15295AS 22147 UPON APPLICATION OF T/O THRUST (FULL), NR 1 ENGINE WOULD NOT MAKE FULL EPR OF 2.14 ONLY 2.05. ALL OTHER PARAMETERS IN YELLOW ARC + POWER LEVER AT FORWARD STOP. ENGINES 2 + 3 POWER LEVERS APPROX 1 1/2 KNOBS BEHIND NR 1 POWER LEVER. (TEMP 31DEG C) ADJUSTED NR 1 ENG THRUST CONTROL SYSTEM. RAN ENGINES AND OBSERVED PARAMETERS. THROTTLES ALIGNED WITH TAKEOFF PWR. BUT EPR READING LOW AT NR 1 ENG. TAKEOFF POWER AVAILABLE BY MEANS OF 99.9% N1 TACH. INDICATION VERIFICATION. WHILE TROUBLESHOOTING NR 1 ENGINE FOUND EPR READING LOW BY .05. NR 1 ENG EPR IND INOP INSP SYSTEM. TIGHTENED CONNECTIONS ON HARD LINE NEAR GANG DRAIN. TIGHTENED LOOSE PLUG ON EPR TRANSDUCER PERFORMED ENG OPS. TARGETS REACHED. 2L73 4F A3WE 20050524002912005052400291EA 2005 5 24 AJC2005F00006 120050414A326084054 PROXIMITY SWITCH CNDAIRCL600 CL6002B16 1900305EA GE CF34 CF34* NE NLG INOPERATIVE E AJCAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA25118MT5481 5077 AFTER TAKEOFF, THE NOSE GEAR DID NOT RETRACT, NOSE GEAR DOORS (OPE) LIGHT DID NOT ILLUMINATE. MLG RETRACTED NORMALLY. CREW CONSULTED THE ABNORMAL PROCEDURES MANUAL AND RECYCLED THE GEAR. CONDITION REMAINED THE SAME. THEN EXTENDED THE GEAR AND GOT 3 GREEN DOWN AND LOCKED LIGHTS. THEY RETURNED TO AIRPORT AND PERFORMED AN UNEVENTFUL OVERWEIGHT LANDING. CREW DID NOT DECLARE EMERG. TROUBLESHOT SYS AND FOUND THE NOSE GEAR RT NR2 GROUND PROXIMITY SWITCH TO BE AT FAULT. REMOVED AND REPLACED NOSE GEAR PROXIMITY SWITCH. PERFORMED SYS OPS CHECK. ALL SYS AND OPS CHECKS WERE GOOD AND AC WAS RETURNED TO SERVICE. (EA25200507764) (K) 2L72 4F4 FRTA21EA E15NE 20050524002932005052400293SO 2005 5 24 2005F00084 120050321A56101159SCB310214 WINDSHIELD GULSTMG1159 G1159A 3970109SO RROYCESPEY SPEY511* 54523EU COCKPIT BROKEN E A UNSCHED LANDING O OTHER CRCRUISE 1 SO198JL 1553 388 WINDSHIELD SHATTERED AT CRUISE. PILOTS FOLLOWED FLIGHT MANUAL PROCEDURES. COMPONENT WAS REPLACED. REASON FOR COMPONENT FAILED IS UNKNOWN AND IS PRESENTLY BEING INVESTIGATED. 2L72 4F4 F A12EA E2EU 20050524003192005052400319 2005 5 24 2005UALA00404 420050503A2565 BOTTLE BOEING747 747422 1384935NM PWA 4056 PW4056 NE EVAC SLIDE LOW A UALAK NONE O OTHER ININSP/MAINT 1 WP29182UA 25279 LOW BOTTLE PRESSURE. 2L74 4F4 FRTA20WE E24NE 20050524003202005052400320EU 2005 5 24 2005UALA00405 120050503A2910 FLUID AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE HYDRAULIC SYS LEAKING A UALAA UNSCHED LANDING K FLUID LOSS CRCRUISE 1 WP29439UA 683 DIVERTED FLIGHT DUE TO LOSS OF GREEN ENGINE HYDRAULIC FLUID. CREW REPORTED IN MSY AFTER NR 1 ENG START GREEN HYD PUMP WOULD NOT COME ONLINE. CYCLED SWITCH SEVERAL TIMES CAME ONLINE. AT FL10 ECAM WARNING GREEN PUMP FAILED CYCLED SWITCH OFF. PTU TOOK OVER OPS NORMAL .CREW REPORTED AT CRUISE WHILE PTU RUNNING GREEN HYD QTY INDICATION STARTED DROPPING BELOW MIN. ON APPROACH TO DENVER INDICATION CAME BACK TO NORMAL AFTER GEAR EXTENSION. FOUND PRESSURE SWITCH FOR PUMP FAILED. REPLACED HYDRAULIC PRESSURE SWITCH. OPS CHECKS NORMAL PER AMM 29-11-17. 2L72 4F4 FRTA28NM E40NE 20050524003252005052400325EU 2005 5 24 2005UALA00413 120050506A2720 LIMITER AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE RUDDER FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29413UA 470 BOTH RUDDER LIMITERS FAILED. MAINTENANCE FOUND FAULT "AFS: FAC2-RTL ACTR 4CC". ELECTRONIC MODULE OF RUDDER TRAVEL LIMITATION UNIT (RTLU) WAS SUBSEQUENTLY REPLACED. OPERATIONAL CHECK WAS NORMAL.NO FURTHER ANOMALY WAS REPORTED. SUBSEQUENT SHOP FINDING FOUND A SIDE BOARD BURNED. MULTIPLE INTERMITTENT FAILURES WERE FOUND ON THE B-SIDE BOARD OF THE ELECTRONIC MODULE. 2L72 4F4 FRTA28NM E40NE 20050524003262005052400326CE 2005 5 24 ACE050805 120050508A5330 SKIN BEECH 1900 1900C 1154161CE FUSELAGE CRACKED E YADAK NONE O OTHER ININSP/MAINT 1 AL03114AX UC36 FOUND CRACKED BELLY SKIN WHILE PERFORMING TURBULENT AIR INSPECTION. CORROSION POSSIBLY ORIGINATING FROM OEM INSTALLATION OF UNPRIMED SHIM STOCK AT STRINGER JOINTS. 2L72 4T RTA24CE 20050524003272005052400327NM 2005 5 24 SWAA051342 120050507A324426066712 TIRE BOEING737 7373H4 1384600NM LT MLG SEPARATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING POST FLIGHT INSPECTION, FOUND LT MLG TIRE TREAD SEPARATED & AFT T/E FLAP DAMAGE. REMOVED AND REPLACED MLG TIRE ASSY & LT INBOARD AFT T/E FLAP PER MM. 2L72 4F RTA16WE 20050524003282005052400328NM 2005 5 24 SWAA051343 120050505A2612894481 FIRE DETECTOR BOEING737 7373H4 1384600NM APU BAY FAULTY A SWAAF ACTIVATE FIRE EXT. O OTHER UKUNKNOWN 1 SW29324SW 23414 APU FIRE WARNING LIGHT ILLUMINATED. DISCHARGED APU FIRE BOTTLE. REMOVED AND REPLACED APU AFT TAILPIPE FIRE DETECTOR PER MM. 2L72 4F RTA16WE 20050524003292005052400329NM 2005 5 24 SWAA051344 120050507A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29327SW 23691 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 11L TO STR 12L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050524003302005052400330NM 2005 5 24 SWAA051345 120050507A53306545775 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29327SW 23691 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 817, STR 18L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050524003312005052400331NM 2005 5 24 SWAA051346 120050507A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29327SW 23691 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510, STR 15R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050524003322005052400332NM 2005 5 24 SWAA051347 120050507A53306545777 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29332SW 23696 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 973, STR 24L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050524003342005052400334NM 2005 5 24 SWAA051349 120050507A3350D71702001 BATTERY PACK BOEING737 7375H4 138449DNM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29505SW 24182 DURING SCHEDULED A1 CHECK, FOUND L2 DOOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050524003352005052400335NM 2005 5 24 SWAA051350 120050506A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 663.75, STR 10L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050524003362005052400336NM 2005 5 24 SWAA051351 120050506A3350612825 BATTERY BOEING737 7373H4 1384600NM CABIN DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 DURING SCHEDULED D-CHECK, L2 DOOR EMERGENCY EXIT LIGHT BATTERY WOULD NOT CHARGE. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20050524003372005052400337 2005 5 24 SWAA051352 420050506A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 & R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29623SW 27933 DURING SCHEDULED C3 CHECK, FOUND R1 & R2 DOOR EMERGENCY EVAC SLIDES OUT OF ADJUST. ADJUSTED SLIDES PER MM. 2L72 4F RTA16WE 20050524003382005052400338NM 2005 5 24 SWAA051353 120050508A53116517684 BELTFRAME BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29669SW 23752 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE BELT FRAME WEB CRACKED AT BS 303, R1 DOOR FWD LOWER CUTOUT. REPAIRED WEB PER SRM AND BAC DRAWING. 2L72 4F RTA16WE 20050524003392005052400339NE 2005 5 24 SWAA051354 220050506A7200CFM563 ENGINE BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE NR 1 MAKING METAL A SWAAK NONE O OTHER ININSP/MAINT 1 SW29684WN 23941 858517 DURING SCHEDULED RON CHECK, NR 1 ENGINE FWD SUMP CHIP DETECTOR HAD EXCESSIVE METAL & PHENOLIC DEBRIS. REMOVED AND REPLACED NR 1 ENGINE PER MM. 2L72 4F4 FRTA16WE E2GL 20050524003402005052400340NM 2005 5 24 SWAA051355 120050507A3350D71702030 BATTERY BOEING737 7377H4 1384404NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29748SW 29800 DURING SCHEDULED RON CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050524003412005052400341NE 2005 5 24 AALA20050311 220050508A7200 ENGINE BOEING757 757223 1384957NM RROYCERB211 RB211535E4B3 NE NR 1 MALFUNCTIONED A AALAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SW21191AN 32385 31799 LAX - IMMEDIATELY AFTER TAKEOFF NUMBER ONE ENGINE VIBRATIONS INTO YELLOW BAND AND WAS VERY LOUD. WHEN POWER PULLED BACK VIBRATIONS REDUCED. REPLACED NUMBER 1 ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA2NM E12EU 20050524003422005052400342NM 2005 5 24 AALA20050312 120050509A3350 LIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21795AN 30257 LHR EMERGENCY ESCAPE PATH LIGHT NEAR FIRST CLASS CLOSET INOPERATIVE. REPLACED EMERGENCY ESCAPE PATH LIGHT ON FIRST CLASS CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATIONS. 2L72 4F RTT00001SE 20050524003432005052400343WP 2005 5 24 AALA20050313 120050508A3350P4010049 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21941AS 49925 LGA - SEAT MOUNTED EMERGENCY LIGHTS AFT OF ROW 20 INOPERATIVE. REPLACED CHARGER AND BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS AFT OF ROW 20. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050524003442005052400344NM 2005 5 24 AALA20050314 120050328A5347FBE12061 SEAT TRACK BOEING757 757223 1384957NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21648AA 24606 TUL - COFFEE BAR TIE DOWN SEAT TRACK NUMBER 3 AT STATION 686 TO 690 CORRODED. REPLACED COFFEE BAR TIE DOWN SEAT TRACK, ALODINED, PRIMED, AND PAINTED. 2L72 4F RTA2NM 20050524003452005052400345NM 2005 5 24 AALA20050316 120050412A5330 SKIN BOEING767 767323 1385205NM FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21360AA 24041 AFW - FUSELAGE SKIN AT STATION 1809 RIGHT HAND UPPER FASTENER HOLE HAD A CRACK INDICATION IN THE FUSELAGE SKIN ONLY AT THE FOUR O`CLOCK POSITION. AREA IS .375 BY .375 AT THE RIGHT HAND FUSELAGE AFT AT STATION 1809. THE HOLE HAD BEEN REAMED TO 0.375 TO REMOVE CRACK INDICATION. OVERSIZED THE HOLE IN THE FUSELAGE OUTER SKIN TO 0.375 INCHES. VERIFIED CRACK WAS COMPLETELY REMOVED. INSTALLED A COUNTERSINK FREEZE PLUG IN SKIN. REINSTALLED EXTERNAL WEAR DOUBLER. 2L72 4F RTA1NM 20050524003462005052400346NM 2005 5 24 AALA320050315 120050328A5320 INTERCOSTAL BOEING757 757223 1384957NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21648AA 24606 TUL - RIGHT NUMBER 4 DOOR DRAIN LINE SUPPORT CORRODED BETWEEN STATION 1640 AND 1661. REPLACED DRAIN LINE SUPPORT INTERCOSTAL WITH A NEW INTERCOSTAL BETWEEN STATIONS 1640 AND 1661 PER SRM 51-10-02. 2L72 4F RTA2NM 20050524003472005052400347SO 2005 5 24 C2XA05IA063 120050426A3230355022002 CONTROL UNIT EMB 145 EMB145ER 3260211SO LANDING GEAR INOPERATIVE A C2XAA UNSCHED LANDING O OTHER CLCLIMB 1 SW27149305928 145 145011 CRP - THE CREW REPORTED THAT DURING TAKEOFF THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO CRP WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT (LGEU), OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050524003482005052400348SO 2005 5 24 C2XA05IA064 120050427A3260M835366022M RELAY EMB 145 EMB145ER 3260211SO COCKPIT FAILED A C2XAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW2714930 145011 IAH - THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL ON TAKEOFF AND A WEIGHT ON WHEEL FAILURE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED RELAYS K0453 & K0352, OPERATIONALLY CHECKED WITH NO DEFECTS, THE AIRCRAFT WAS SATISFACTORILY TEST FLOWN, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. BOTH RELAYS ARE THE SAME PART NUMBER, NOT SERIALIZED, AND NO TIMES ARE AVAILABLE. 2L72 4F RTT00011AT 20050524003492005052400349SO 2005 5 24 C2XA05TY038 120050430A575114569009607 BRACKET EMB 145 EMB145LR 3260212SO LT AILERON DAMAGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716954 145072 TYS, DURING A SCHEDULED INSPECTION THE LEFT AILERON PCA ATTACH FITTING ON THE AILERON WAS FOUND DAMAGED. MAINTENANCE REMOVED AND REPLACED THE AILERON PCA BRACKET IAW EC5750-01177. 2L72 4T RTT00011AT 20050524003502005052400350SO 2005 5 24 C2XA05IA065 120050502A32347455503 CONTROL LEVER EMB 145 EMB145LR 3260212SO COCKPIT DEFECTIVE A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW27139893458 912 145271 IAH - DURING TAKEOFF, THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR SELECTOR LEVER, OPERTAIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050524003512005052400351SO 2005 5 24 C2XA05CL030 120050502A3297 WIRE EMB 145 EMB145XR 3260214SO COCKPIT CHAFED A C2XAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW2712142 145735 CLE - THE CREW REPORTED THE AURAL WARNING SOUNDED CONTINUOUSLY IN FLIGHT AT ALL ALTITUDES UNTIL THE LANDING GEAR WAS LOWERED. MAINTENANCE FOUND AND REPAIRED CHAFED WIRES IN THE CENTER PEDESTAL JUST AFT OF THE FLAP SELECTOR HANDLE. OPERATIONAL TESTS OF THE AURAL WARNING SYSTEM AND THE LANDING GEAR SYSTEM WERE GOOD. 2L72 4F RT 20050524003522005052400352SO 2005 5 24 C2XA05TY039 120050503A531114521805405 FRAME EMB 145 EMB145LR 3260212SO FUSELAGE BENT A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716954 145072 TYS - DURING A SCHEDULED INSPECTION FRAME 72, BETWEEN STRINGERS 15R AND 16R IN THE BAGGAGE COMPARTMENT WAS FOUND BENT. MAINTENANCE REMOVED AND REPLACED THE FRAME IAW EMB-135/145 SRM 51-40-02. 2L72 4T RTT00011AT 20050524003532005052400353SO 2005 5 24 C2XA05TY040 120050505A532014521713003 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO 72 CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716954 145072 TYS - DURING A SCHEDULED INSPECTION THE CENTER OMEGA BEAM FORWARD OF FRAME 25 WAS FOUND CORRODED. MAINTENANCE CUT OUT THE DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER, FILLER AND SHIMS IAW EMB-135/145 SRM 53-22-10. 2L72 4T RTT00011AT 20050524003542005052400354SO 2005 5 24 C2XA05TY041 120050505A532014521700007 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716954 145072 TYS - DURING A SCHEDULED INSPECTION THE LEFT OMEGA BEAM FORWARD OF FRAME 25 WAS FOUND CORRODED. MAINTENANCE CUT OUT THE DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER, FILLER AND SHIMS IAW EMB-135/145 SRM 53-21-10. 2L72 4T RTT00011AT 20050524003552005052400355SO 2005 5 24 C2XA05IA068 120050504A532014524220403 ANGLE EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714974 145161 IAH - DURING MAINTENANCE INSPECTION, THE PAX DOOR THRESHOLD ATTACHMENT ANGLE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050524003562005052400356SO 2005 5 24 C2XA05IA071 120050505A5610163500111 WINDSHIELD EMB 145 EMB145LR 3260212SO COCKPIT CRACKED A C2XAB EMER. DESCENT O OTHER CRCRUISE 1 SW2714558637 637 145598 IAH - THE CREW REPORTED THAT THE CAPTAINS WINDSHIELD SHATTERED IN FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE AFFECTED WINDSHIELD, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050524003572005052400357SO 2005 5 24 C2XA05SH027 120050507A532014522459003 ANGLE EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716987 145261 SHV - DURING C-CHECK CENTER OMEGA BEAM RAMP ANGLE HAS CORROSION AT FRAME 20. MAINTENANCE REMOVED AND REPLACED CENTER OMEGA BEAM RAMP ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050524003582005052400358SO 2005 5 24 C2XA05SH028 120050507A532014521700007 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714522 145383 SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 20. MAINTENANCE REPAIRED LT OMEGA BEAM AT FR 20 IAW EMB 135 SRM 53-21-10, SECTION 2, FIGURE 201, SHEET 2. INSTALLED NUT PLATE IAW EC 5320-01137. PAINTED ON REPAIR AREA IAW EC 5320-01140. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050525000012005052500001EU 2005 5 25 USAA050478 120050410A5315 FLOORBEAM AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19106US 1044 FLOORBEAM CORRODED .5 INCH DIAMETER AREA, FLOORBEAM AT FRAME 20, 9 INCH RIGHT OF CENTER. REMOVED CORROSION, INSTALLED DOUBLER PER SRM 53-11-14. CORROSION LEVEL 1, TASK JA-220-53300. REMOVED CORROSION, INSTALLED DOUBLER PER SRM 53-11-14. (M) 2L72 4F RTA28NM 20050525000042005052500004NM 2005 5 25 USAA050502 120050413A5532 SKIN BOEING737 7374B7 1384702NM VERTICAL STAB CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19440US39307 24811 CLT - FOUND SKIN CHAFED 1 INCH BY 1 INCH, UNDER LE OF DORSAL FIN. INSTALLED DOUBLER IAW EA 96445. (M) 2L72 4F RTA16WE 20050525000072005052500007NM 2005 5 25 USAA050472 120050409A5320 SUPPORT BOEING737 7374B7 1384702NM DOOR FRAME CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19440US39307 24811 CLT - FOUND DOOR STOP SUPPORT CRACKED .5 INCHES, AFT SIDE FORWARD SERVICE DOOR STATION 332, STRINGER 11. REPLACED WITH IDENTICAL PART, NEW FITTING IAW SRM 51-10-02. (M) 2L72 4F RTA16WE 20050525000082005052500008NM 2005 5 25 USAA050471 120050409A5311 FRAME BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19440US39307 24811 CLT - FOUND FRAME CRACKED 3 INCHES, STATION 727B BETWEEN STRINGER 8L-9L. INSTALLED DOUBLER IAW TR 53-10-20B. (M) 2L72 4F RTA16WE 20050525000092005052500009 2005 5 25 QXEA200500830 420050423A3100 DISPLAY BOMBDRDHC8 DHC8401 1390041NM COCKPIT MALFUNCTIONED A QXEAA UNSCHED LANDING O OTHER CRCRUISE 1 NM09402QX 4032 ON DESCENT THROUGH 20,000 FT, THE IAS MIS-MATCH MESSAGE DISPLAYED ON BOTH PFD'S. CAPTAIN'S A/S INDICATED 221 KTS, FO'S INDICATED 206 KTS. AS DESCENT CONTINUED, THE FO'S A/S INDICATION CONTINUED TO DECREASE. ALSO, RECEIVED ELEVATOR FEEL, PITCH TRIM, SPLR OTBD AND RUD CONTROL CAUTION LIGHTS. C/W ABNORMAL CHECKLIST, SWITCHED TO ADC1. DIVERTED TO BOI AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE DRAINED NR 2 PITOT SYSTEM IAW AMM 34-11-06. C/W NR 2 PITOT SYSTEM LEAK IAW MTC 5341001, OPS CHECKS NORMAL. NO PARTS REPLACED. 2H72 4T RTA13NM 20050525000102005052500010 2005 5 25 QXEA200500831 420050422A3414 INDICATION SYS BOMBDRDHC8 DHC8401 1390041NM AIRSPEED MALFUNCTIONED A QXEAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 NM09404QX 4046 SEA - ON FLIGHT 2316 (SEA-YEG). DURING TAKEOFF ROLL, NOTICED SIGNIFICANT AIRSPEED LAG IN FO'S AIRSPEED INDICATOR. AT APPROXIMATELY 60 KTS, IAS MISMATCH MESSAGE DISPLAYED ON BOTH PFD'S. ABORTED TAKEOFF AT APPROXIMATELY 85 KTS IAS ON CAPT'S PFD. AIRSPEED SPLIT WAS BETWEEN 15 AND 20 KTS. CAPTAIN'S WAS HIGHER (85 KTS VS 65 TO 70 KTS ON FO'S). RETURNED TO THE GATE. MAINTENANCE CLEANED NR 1 AND NR 2 PITOT LINES PER Q400 AMM 34-11-00. C/W PITOT/STATIC LEAK CHECK MTC 5341001. LEAK CHECK GOOD. NO AIRSPEED SPLIT OR MISMATCH NOTED. RII C/W. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2H72 4T RTA13NM 20050525000112005052500011NM 2005 5 25 QXEA200500832 120050429A33506104781 BATTERY PACK DHAV DHC8 DHC8202 2809007NM FUSELAGE FAILED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH2753948 480 PDX- LEFT AFT OTBD EMERGENCY LIGHT INOP. MAINTENANCE REPLACED BATTERY PACK PS-3. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050525000122005052500012NM 2005 5 25 QXEA200500833 120050501A33506104781 POWER SUPPLY DHAV DHC8 DHC8202 2809007NM EMERGENCY LIGHT FAILED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09375PH27299262 529 PDX - EMERGENCY LIGHT IN CEILING PANEL INSIDE CABIN HAS 2 LIGHTS INOP. MAINTENANCE REPLACED THE BATTERY PACK PS3. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050525000142005052500014 2005 5 25 PIDA20050019 420050429A22104084042911 COUPLER BOEING737 7373G7 1384595NM YAW DAMPER DAMAGED A PIDAK NONE O OTHER NRNOT REPORTED 1 SO05370WL 24011 PILOT REPORTED YAW DAMPER HARD TO ENGAGE. REPLACED YAW DAMPER COUPLER PER MM 22-12-32. SYSTEM TESTS NORMAL. 2L72 4F RTA16WE 20050525000152005052500015WP 2005 5 25 0500669601 120050430A2134 LINE DOUG DC9 DC932 3022066WP LT AUG VALVE KINKED A NWAAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 GL01601NW 47038 AT FL340, CREW NOTICED THE CABIN ALTITUDE CLIMBING THROUGH 10,000 FEET. A RAPID DESCENT WAS INITIATED AND COMPLIED WITH COM PROCEDURES. CONTROL OF THE CABIN PRESSURE WAS REGAINED ON DESCENT WHEN THE AIRFOIL ANTI-ICE WAS SECURED. AIRCRAFT CLIMBED BACK UP TO FL270 AND CONTINUED TO AN UNEVENTFUL LANDING AT RSW. THE AIRCRAFT WAS FERRIED TO DTW WHERE MAINTENANCE ACCOMPLISHED BITE AND REPLACED THE LEFT HEAT EXCHANGER PERI SEALS, THE LEFT AUGMENTATION VALVE, THE ANTICIPATOR, AND THERMOSTAT. FINALLY, A KINKED HIGH PRESSURE SENSE LINE WAS FOUND AND REPLACED. THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20050525000162005052500016EA 2005 5 25 COMA0560284 120050503A5320 WEB CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01708CA 7235 FS 280.00 WEB CORRODED ON FACE BETWEEN LBL 9 AND RBL 9. REPAIRED IAW EO 10-5310-00621. 2L72 4F RTA21EA 20050525000172005052500017EA 2005 5 25 COMA0560285 120050503A5320 DOUBLER CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01708CA 7235 DOUBLER CRACKED AT LEFT HAND FS 640.00. REMOVED AND REPLACED IAW SRM 51-42-06 AND 51-42-20. 2L72 4F RTA21EA 20050525000182005052500018EA 2005 5 25 COMA0560286 120050503A5320 DOUBLER CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01708CA 7235 DOUBLER CRACKED AT LEFT HAND FS 640.00. REMOVED AND REPLACED IAW SRM 51-42-06 AND 51-42-20. 2L72 4F RTA21EA 20050525000202005052500020CE 2005 5 25 DJFA2005089 120050505A5414258ES16F1A PANEL RAYTHNDH125 HAWKER800XP 7150012CE LT PYLON BENT E DJFAA UNSCHED LANDING O OTHER CLCLIMB 1 EA23722TA 258322 WHILE CLIMBING OUT OF 11,000 FT FOR 23,000 FT, AIRCRAFT MADE AN IMMEDIATE LEFT BANK/YAW OF 35 DEGREES AND THE AUTO-PILOT DISCONNECTED. AIRCRAFT WAS HAND FLOWN TO STRAIGHT AND LEVEL AND CREW DECLARED AN EMERGENCY. THE CREW REPORTED THAT THE AIRCRAFT WAS FISH TAILING WHEN FLAPS AND GEAR WERE SELECTED. AIRCRAFT HAD RETURNED TO KCHA AND MADE AN UNEVENTFUL LANDING. FOLLOWING LANDING, THE CREW DISCOVERED THAT A LEFT ENGINE PYLON LOWER INSPECTION PANEL WAS BENT BACK AND DAMAGED. MAINTENANCE REPLACED THE BENT INSPECTION PANEL. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA3EU 20050525000212005052500021CE 2005 5 25 DXTA200500708 120050504A3240215297 BRAKE CESSNA500 560CESSNA 2076750CE MLG LEAKING E DXTAO OTHER K FLUID LOSS TXTAXI/GRND HDL 1 GL07345QS891 5600445 SPONGY BRAKES ON LANDING. FOUND BRAKE FLUID LEAKING FROM BRAKE ASSEMBLY AIRCRAFT RIGHT SIDE, REMOVED AND INSTALLED BRAKE ASSY, PERFORMED BRAKE BLEED NO DEFECTS NOTED IAW CE560 M/M 32-42-00. 2L72 4F RTA22CE 20050525000232005052500023NM 2005 5 25 DHL2005740500 120050421A5531 STRINGER BOEING727 7272Q9 138448MNM VERTICAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 VERT STAB FIN STA 157 STRINGER 8 LEFT IS CRACKED AT FRAME ATTACH BOLT. REMOVED FASTENERS FOR ACCESS AT VERT STAB FIN STA 157 S-8 LT AND TRIM OUT DAMAGED AREA SIZE 3 1/2" BY 3" IAW B727 SRM 55-30-4 FIG 1. FABRICATED REPAIR PARTS FILLER BAC 1517-1363 7075-T6511 SIZE 3 1/2" BY 3" PO NR 501953, SPLICE 10134-1201 7075-T6511 PO NR 501952 SIZE 18" BY 2" FILLER STRAPS 7075-T6.100 SIZE 19" BY 1/2" PO NR 9001777 SPLICE 10133-1401 7075-T6511 SIZE 18" BY 2" PO NR 501952 IAW B-727 SRM 55-30-1 FIG 1. TREATED AND PRIMED REPAIR PARTS IAW B-727 SRM 51-10-2. INSTALLED STRINGER REPAIR AT VERT STAB FIN STA 157 S-8 LT IAW B727 SRM 55-30-4 FIG 1 AND SRM 51-30-2. 2L73 4F RTA3WE 20050525000242005052500024NM 2005 5 25 72300175 120050502A5340 FITTING BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE STRINGER CRACKED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 .5 INCH CRACK ON STRINGER END FITTING. 2L73 4F4 FRTA3WE E2EA 20050525000252005052500025NM 2005 5 25 P9RA20050078 120050422A3397BACC45FT12A12P CONNECTOR BOEING757 757236 1384971NM LIGHT LOOSE A P9RAK NONE L NO TEST ININSP/MAINT 1 SO11962PG 24119 LAS GATE ITEM 1P, FIRST WHITE TRACK LIGHT INOP ADJACENT TO LAVATORY. SECURED CONNECTOR ON FLOOR EMERGENCY LIGHT. OPS CHECKED GOOD. 2L72 4F RTA2NM 20050525000272005052500027NM 2005 5 25 DHL2005740502 120050412A5322 SHEAR TIE BOEING727 7272Q9 138448MNM FUSLEAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 AFT CARGO COMPT BS 1166 BETWEEN STR 22 RIGHT TO STR 23 RIGHT IS CRACKED AT SHEAR TIE NDT CONFIRMED. CUT OUT FRAME SECTION STR 23R TO STR 24R DIM 22" BY 6 1/2" IAW 727 SRM 53-10-4 FIG 1. FABRICATED FRAME SECTION FROM 7075 T6 .063 DIM 22" BY 6 1/2" FRAME SPLICE 7075T6 .063 DIM 10 3/4" BY 4" SHEAR TIES FROM 7075 T6 .063 4 1/4" BY 3", 6" BY 3" [2EA] 6" BY 2 1/2" 5 1/4" BY 2 1/2" [2EA] AND 5 3/4" BY 2 1/2" PO NR 9002118 IAW B727 SRM 53-10-4 FIG 1 AND 53-10-4 FIG 13. TREATED AND PRIMED FRAME SECTION , FRAME SPLICE AND SHEAR TIES IAW B727 51-10-2. INSTALLED FRAME SECTION AND SPLICE IAW B727 SRM 53-10-4 FIG 1. INSTALLED SHEAR TIES IAW B727 SRM 53-10-4 FIG 13 AND REINSTALLED CLIPS BETWEEN STRINGERS IAW B727 SRM 51-2L73 4F RTA3WE 20050525000302005052500030NE 2005 5 25 ASMF200505008 220050505A7200 ENGINE DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE RIGHT FAILED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23881LF3895015198 53051 725491 DURING OVERNIGHT SERVICE AND IN ORDER TO ATTEND EPR NR 2 WITH DIFFERENCE OF 0.20 DURING CRUISE REPORT, THE RIGHT ENGINE WAS CHECKED BY LEAKS ON PT2 AND PT7 LINES AND EPRS TRANSMITTER AND FCU WERE REPLACED, BEING NOT POSSIBLE TO ADJUST THE ENGINE. IT WAS DETERMINED TO REPLACE THE RIGHT ENGINE IAW MM 71-00-01 AND TESTS WERE PERFORMED IAW MM 71-00-02, ALL CORRECT. 2L72 4F4 FRT E9NE 20050525000312005052500031NM 2005 5 25 DHL2005740503 120050415A5312 BULKHEAD BOEING727 7272Q9 138448MNM FUSLEAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 AFT CARGO COMPT AFT BULKHEAD BS 1183 RBL 18 TO 38 WL167 STIFFENER AND CLIP CORRODED. REMOVED STIFFENER AT AFT CARGO BLKHD BS 1183 RBL 18 TO 38 IAW B727 SRM 51-30-2. FABRICATED STIFFENER FROM BAC 1518-356 7075T6 PO NR 5080179 SIZE 20 INCH AND 2 EA FILLER FROM 2024T3 .090 PO NR 9002149 DIM 19" BY 2" IAW B727 SRM 53-10-2 FIG 5. ALODINED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED STIFFENER UIAW B727 SRM 53-10-2 FIG 5 AND 51-30-2 2L73 4F RTA3WE 20050525000322005052500032NM 2005 5 25 DHL2005740504 120050414A5320 CHANNEL BOEING727 7272Q9 138448MNM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 HORIZ CHANNEL AND ANGLE CORRODED WL 172 RBL 20 STA 1183 AFT CARGO COMPARTMENT. REMOVED ANGLE IAW B727 SRM 51-30-2 FABRICATED NEW ANGLE AT WL 172 RBL 20 STA 1183 AT AFT CARGO MAT USED 2024 T3 .050 PO NR 90020093 DIMENSION 6" BY 3" IAW B727 SRM 51-20-1 AND 53-10-2. INSTALLED NEW ANGLE IAW B727 SRM 51-20-1 AND 53-10-2 FIG 5 51-30-2. 2L73 4F RTA3WE 20050525000332005052500033NM 2005 5 25 SB05055 120050505A335020121 CHARGER BOEING737 7374B7 1384702NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19784AU 25023 ORF - FOUND LAST TWO ROWS OF EMERGENCY LIGHTS AND THE RIGHT EXTERIOR EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER. 2L72 4F RTA16WE 20050525000352005052500035EU 2005 5 25 XNOA1224 120050507A7331 INDICATION SYS AIRBUS300 A300B4203 3930306EU NR 2 FUEL ERRATIC A XN0AO OTHER N FALSE WARNING NRNOT REPORTED 1 GL23373PC 218 NR 2 FUEL FLOW ERRATIC. TRANSFERRED TO DMI NR 5396 IAW A-300 MEL 73-30-01 CAT "B". 2L72 4F RTA35EU 20050525000392005052500039NM 2005 5 25 RYNA200500015 120050429A2612 WARNING LIGHT BOEING757 75728A 1384976NM APU FIRE ILLUMINATED A RYNAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE07753NA 24544 AFTER TAKEOFF FROM NKW, EXPERIENCED AN APU FIRE WARNING INDICATION WITH ALL FIRE WARNING LIGHTS BUT NO HORN DURING CLIMB. APU WAS SHUTDOWN BEFORE TAXI. CREW FOLLOWED EMERGENCY PROCEDURES, DISCHARGED THE FIRE BOTTLE AND RETURNED TO UKW. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED APU COMPARTMENT AND FIRE LOOPS, NO DAMAGE FOUND. CHECKED ECU AND RESET BPCU. BITE CHECKED AND ALL POWER SYSTEMS CHECKED NORMAL. REMOVED AND REPLACED ENGINE FIRE BOTTLE AND SQUIB. RAN APU FOR 2 HOURS WITH NO FAULTS. 2L72 4F RTA2NM 20050525000432005052500043EA 2005 5 25 VTZA200500069 120050505A5712601R107091 RIB CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27625BR 7214 LEFT BATT RIB IS CRACKED 1.5 INCH. 2L72 4F RTA21EA 20050525000462005052500046EA 2005 5 25 REXA2005054 120050419A492038004883 APU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE SMOKE A REXAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO258515F7955 2566 7515 SMOKE IN COCKPIT AND CABIN WHEN THE APU WAS STARTED. INVESTIGATED, FOUND APU TO BE THE SOURCE OF THE SMOKE. APU WAS DEFERRED UNTIL IT CAN BE SCHEDULED OFF. (K) 2L72 4F4 FRTA21EA E15NE 20050525000482005052500048EA 2005 5 25 REXA2005055 120050426A3260 INDICATION SYS CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NLG MALFUNCTIONED A REXAO OTHER N FALSE WARNING APAPPROACH 1 SO258698A 7698 UPON GEAR EXTENSION FOR LANDING, NOSE LANDING GEAR WOULD NOT SHOW DOWN. DECLARED EMERGENCY, FOLLOWED QRH WITH UNEVENTFUL LANDING. PERFORMED GEAR SWING IAW AMM. NO DEFECTS NOTED, OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050525000502005052500050EA 2005 5 25 REXA2005057 120050428A2611PU90421R3 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LAVATORY FALSE ACTIVATIONA REXAO OTHER N FALSE WARNING CLCLIMB 1 SO258444F 7444 SMOKE TOILET MESSAGE AFTER TAKEOFF. REMOVED AND REPLACED LAV SMOKE DETECTOR IAW AMM. OPS CHECK NORMAL. NO SMOKE EVER FOUND. AC READY FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050525000552005052500055EU 2005 5 25 USAA050496 120050410A5315D534721220400 FLOORBEAM AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19106US 1044 FOUND FLOORBEAM CORRODED 1 SQUARE INCH, AROUND NUT PLATE HOLES, FLOORBEAM C66-C69 LEFT OUTBOARD. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-72-11. CORROSION LEVEL 1, TASK JA 260-53500. (M) 2L72 4F RTA28NM 20050525000562005052500056EU 2005 5 25 USAA050477 120050410A5315D53472089004608 FLOORBEAM AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19106US12932 1044 PIT - FOUND FLOORBEAM CORRODED 2.5 INCHES DIAMETER AREAS, FLOORBEAM GALLEY MOUNTING HOLES OUTBOARD FLOORBEAM, BETWEEN RT SIDE C68-69. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M) 2L72 4F RTA28NM 20050525000622005052500062EU 2005 5 25 2005F00078 120050420A3210D232190002 ARM AEROSPATR72 ATR72212 8680945EU MLG CRACKED A TRBAK NONE O OTHER ININSP/MAINT 1 SO29447AM 447 WHILE PERFORMING A NON DESTRUCTIVE TESTING (NDT) INSPECTION OF THE MAIN LANDING GEAR SIDE BRACE, THE LEFT UPPER ARM SHOWED A DEFECT (CRACK). REPLACED LEFT MAIN LANDING GEAR UPPER ARM. (M) 2H72 4T RTA53EU 20050525000632005052500063CE 2005 5 25 2005F00076 120050411A55141016200131 BRACKET BEECH 1900 1900D 1154162CE RT STABILIZER CORRODED A GUUAK NONE O OTHER ININSP/MAINT 1 SO298153519960 UE147 AT SCHEDULED ROUTINE MAINTENANCE, RIGHT CENTER ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RIGHT CENTER ELEVATOR HINGE BRACKET. (M) 2L72 4T RTA24CE 20050525000652005052500065CE 2005 5 25 2005F00081 120050417A3240 BRAKE ASSY BEECH 1900 1900D 1154162CE MLG MALFUNCTIONED A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO2981538 UE199 RT BRAKE VERY SOFT. REQUIRED EXCESSIVE PUMPING TO CREATE PRESSURE AND INCREASE BRAKE EFFECTIVENESS. BLED LEFT AND RIGHT BRAKES. OPERATIONAL CHECK NORMAL. (M) 2L72 4T RTA24CE 20050525000672005052500067CE 2005 5 25 EXO2005F00000 120050326A2701C2006R MASTER SWITCH LEAR 55 55LEAR 5170702CE CONTROL COLUMN SHORTED E EXOAO OTHER O OTHER CRCRUISE 1 SO17556HJ13230 028 PILOT EXPERIENCED LOSS OF YAW DAMPERS NR1, NR2, REENGAGEMENT ATTEMPTS UNSUCCESSFUL. AUTO PILOT DISENGAGED AND COULD NOT BE RESET. IN-OP YAW DAMPER, PILOT WAS ATTEMPTING TO LEVEL AC, NO RESPONSE TO PITCH TRIM CNTRL, SECONDARY PITCH TRIM WAS ACTIVATED W/NEGATIVE RESULTS. CHK LIST PROCEDURES FOR PITCH TRIM FAIL, ATC NOTIFIED, DIFFICULTY IN MAINTAINING PITCH CNTRL. AC LANDED SAFELY. FOUND NO PROBLEMS W/PITCH TRIM SYS. FOUND INTERMITTENT SHORT INTERNALLY VIA LOOSE INTERNAL CONNECTIONS. FOUND BY (TAPPING) CNTRL WHEEL WHICH RECREATED FAILURE. INTERNAL SHORT CREATED PERMANENT NR1 AND NR 2 PITCH TRIM DISCONNECT, AC DIFFICULT TO MANEUVER IN PITCH AXIS. WHEEL MASTER SWITCH WAS REPLACED, AC RETURNED TO SERVICE. 2L72 4F A10CE 20050524000912005052400091NM 2005 5 24 UPS05444412 120050410A534065B38600176 STRINGER CLIP BOEING747 747283B 1384867NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 BS 1940 STR 19R STRINGER TIE CLIP FOUND CRACKED (CRACK LENGTH 1/4 INCH) . BS1940 STR 19R STR TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050524001642005052400164NM 2005 5 24 05FDEA01209 120050505A523065577862 BRACKET BOEING727 727200 138407ENM CARGO DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25254FE 20936 UPPER AFT DOOR BEARING GUIDE BRACKET ON AFT LWR CARGO DOOR FRAME IS CRACKED. REMOVED AND REPLACED DOOR GUIDE BRACKET IAW SRM 51-30-2. 2L73 4F RTA3WE 20050524001702005052400170NM 2005 5 24 05FDEA01215 120050506A5753ARC4125502 FITTING DOUG MD11 MD11 3023602NM T/E FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 RIGHT WING O/B FLAP SECOND FLAP VANE TRACK FROM I/B UP-STOP FITTING FOUND CRACKED. CRACKED STOP FITTING REMOVED. NEW FITTING HOLES TRANSFERED AND INSTALLED AS PER SRM 51-33-01 AND 51-31-01VOL II. CLASSIFIED AS MAJOR REPAIR PER GMM 6-1-100. 2L73 4F RTA22WE 20050524001782005052400178EA 2005 5 24 VTZA200500074 120050505A2710272955 LINK CNDAIRCL600 CL6002B19 1900309EA LT AILERON PCU CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27625BR 7214 LEFT AILERON LINK ON THE OUTBOARD PCU IS CRACKED IN HALF. 2L72 4F RTA21EA 20050524001812005052400181EA 2005 5 24 VTZA200500071 120050505A5311601360021 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27625BR 7214 LEFT FS 640 FRAME IS CRACKED IN RADIUS AT 1 INCH IN LENGTH. 2L72 4F RTA21EA 20050524001832005052400183NM 2005 5 24 MWEA050040 120050508A57545922532506 SKIN DOUG MD88 MD88 3023688NM L/E SLAT CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 NUMBER TWO SLAT, RIGHT LOWER SURFACE SKIN HAS TWO SMALL CRACKS EMANATING FROM CHERRY MAX RIVETS. FABRICATED AND INSTALLED DOUBLER. 2L72 4F RTA6WE 20050524001862005052400186NM 2005 5 24 UPS05M44433 120050508A2560 SMOKE BARRIER DOUG MD11 MD11F 3023600NM CABIN LOOSE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01250UP 48745 INSPECTION TYPE:N/A MCD SMOKE CURTAIN LEFT WALL LOOSE. APPLIED ADHESIVE TO VELCRO OF MCD SMOKE CURTAIN REF AMM 51-33-00. 2L73 4F RTA22WE 20050524001882005052400188SO 2005 5 24 C2XA05CL033 120050506A335074449 SIGN EMB 145 EMB145ER 3260211SO CABIN INOPERATIVE A C2XAK NONE L NO TEST TXTAXI/GRND HDL 1 SW2712946 145052 CLE - THE CREW REPORTED THE EMERGENCY EXIT SIGN DID NOT ILLUMINATE WHEN TESTED. MAINTENANCE REPLACED THE EMERGENCY EXIT SIGN AND THE OPERATIONAL TESTS WERE GOOD. 2L72 4F RTT00011AT 20050524001962005052400196NM 2005 5 24 SWAA051339 120050505A53306545777 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29669SW 23752 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050524002082005052400208SO 2005 5 24 LR7A05051 120050428A5512 SKIN LKHEED382 382G 526414USO HORIZ STAB CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK PER JOB CARD HC5511 LEFT HORIZONTAL STAB UPPER SURFACE SKIN AND INNER HAT SECTION FLANGE CRACKED AT HSS220, FS 1093, WL 280. REPAIR CARRIED OUT IAW SMP583 FIG 55-20-06. 2H74 4T A1SO 20050524002152005052400215SO 2005 5 24 LR7A05058 120050428A5311LS4312 FRAME LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK PER JOB CARD HC2701 CRACK FOUND AT RIGHT AFT FUSELAGE FS 858 UPPER RING SEGMENT EDGE, RBL 61, WL 280. REPAIR CARRIED OUT IAW SMP583 FIG 53-50-05, FS 858. 2H74 4T A1SO 20050524002212005052400221SO 2005 5 24 LR7A05064 120050428A5311 FRAME LKHEED382 382G 526414USO FUSELAGE DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK INTERIOR FUSELAGE FRAMES FOUND EXCESS & ELONGATED HOLES AT LEFT & RIGHT FS 667 WL 162 BL 68. FRAME REPAIRED IAW R05-009-03, LAC MEA 382-53-05-045, LT & RT FS 667 WL 162 BL 68. 2H74 4T A1SO 20050524002322005052400232SO 2005 5 24 LR7A05075 120050428A5311 FRAME LKHEED382 382G 526414USO FUSELAGE DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK INTERIOR FUSELAGE FRAMES FOUND EXCESS & ELONGATED HOLES AT RIGHT FS 310 WL 162 BL 68. FRAME REPAIRED IAW R05-009-04, LAC MEA 382-53-05-046, RIGHT FS 310 WL 162 BL 68. 2H74 4T A1SO 20050524002402005052400240SO 2005 5 24 LR7A05083 120050428A5311 FRAME LKHEED382 382G 526414USO FUSELAGE DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK INTERIOR FUSELAGE FRAMES FOUND EXCESS & ELONGATED HOLES AT LEFT FS 384 WL 162 BL 68. FRAME REPAIRED IAW R05-009-06, LAC MEA 382-53-05-048, LT FS 384 WL 162 BL 68. 2H74 4T A1SO 20050524002452005052400245SO 2005 5 24 LR7A05088 120050428A5311 FRAME LKHEED382 382G 526414USO FUSELAGE DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK INTERIOR FUSELAGE FRAMES FOUND EXCESS & ELONGATED HOLES AT RIGHT FS 431, WL 162 BL 68. FRAME REPAIRED IAW R05-009-06, LAC MEA 382-53-05-048, RIGHT FS 431 WL 162 BL 68. 2H74 4T A1SO 20050524002512005052400251EU 2005 5 24 F3L2005F00000 220050422A7261 ENGINE BOEING737 737300 1384610NM CFMINTCFM56 CFM563B2 13802EU LEAKING A F3LAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 NM03313FL MSN26442 85613 APPROX 11 MIN INTO CLIMB AT FL260, BOTH ENGINES BEGAN TO LOSE OIL QUANTITY. AFTER A SHORT PERIOD OF TIME, OIL QUANTITY ON NR 1 ENG WENT TO ZERO, FOLLOWED BY NR 2 ENG ALSO GOING TO ZERO. NR 1 ENG OIL PRESS THEN DROPPED TO ZERO, NR 2 ENG OIL PRESS DROPPED TO MIDDLE OF AMBER BAND BEFORE DROPPING TO ZERO. AT THIS TIME, BOTH ENGINE AMBER LOW OIL PRESS LIGHTS ILLUMINATED WHILE AN IMMEDIATE RETURN TO THE AIRPORT WAS INITIATED. UPON LANDING AND AFTER ENGINE SHUTDOWN, OBVIOUS OIL LEAKAGE FROM BOTH ENGINES WAS EVIDENT. DETERMINED THAT N2 (PADS) (SP) HAD NOT BEEN REINSTALLED AFTER COMPLETION OF BORESCOPES, BOTH WERE HANGING ALONG SIDE ENGINES BY RESTRAINT LEADS. (K) 2L72 4F4 FRTA16WE E21EU 20050524002562005052400256NM 2005 5 24 UIEA200500050 120050412A3240215152 BRAKE BOEING747 74747UF 1384949NM GE CF6 CF680C2* GL MLG DAMAGED A UIEAD RETURN TO BLOCK A FLAME/FIRE TXTAXI/GRND HDL 1 EA15409MC 30558 EICAS MESSAGE BRAKE TEMP AFTER LANDING ROLLOUT IN MEL, SMALL FIRE NOTICED ON NR 7 BRAKE AFTER AIRCRAFT WAS PARKED. IT WAS QUICKLY EXTINGUISHED WITH A DRY FIRE EXTINGUISHER AGENT. INSPECTION CARRIED OUT. MAX TEMP INDICATION 5, CMC MSG 32127. NO ITEMS NOTED. ALL BRAKE TEMPERATURES AT ZERO FOR DEPARTURE. MCC REQUESTED NR 7 BRAKE AND TIRE REPLACED. (K) 2L74 4F4 FRT1384945 E23EA 20050524002582005052400258NM 2005 5 24 UIEA200500052 120050420A5330 SKIN BOEING747 74747UF 1384949NM GE CF6 CF680 30025NE FUSELAGE DENTED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15412MC 30559 STA 1980-2000, STR 42-44, RT (2 EA) DENT (A) AND (B) WERE FOUND ON THE EXT FUSELAGE. DENT (A) STA 1980-2000, STR 42-43, RT D=0.09, W=1.15 INCH, L=3.8 INCH. DENT (B) STAT 1980-2000, STR 43-44, RT D=0.051, W=1.18, L=1.54. THE DAMAGED AREA TRIMMED OUT. A REPAIR PATCH WAS INSTALLED IAW SRM. THE REPAIR DOUBLER WAS INSTALLED WITH FASTENERS IAW SRM. PERFORMED HFEC INSPECTION AROUND CUTOUT AREA, NO CRACKS WERE FOUND. (K) 2L74 4F4 FRT1384945 E13NE 20050524002612005052400261NE 2005 5 24 UIEA200500055 220050422A7210 GEARBOX BOEING747 7472D3B 1384805NM GE CF6 CF650E2 30018NE NR 2 ENGINE SEIZED A UIEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA15505MC 21251 517824 DURING CRUISE ENGINE NR 2 FUEL FLOW BEGAN FLUCTUATING FOR 30 SECONDS, THEN THE ENGINE SHUTDOWN WITH THE FOLLOWING INDICATIONS. N1=26.1 PERCENT, EGT 0.0, N2 0.0, OIL PRESSURE 0.0, OIL QUANTITY 3.7 GALLONS, AND FUEL FLOW WAS 1.095. ENGINE WAS WINDMILLING 3 HOUR 45 MINUTES. REMOVED AND REPLACED NR 2 ENGINE IAW MM. PERFORMED TEST NR 3 AND 8. FOUND ALL PARAMETERS WITHIN LIMITS. (K) 2L74 4F4 FRTA20WE E23EA 20050524002642005052400264 2005 5 24 UIEA200500057 420050424A221060B00013311 COMPUTER BOEING747 747271C 1384869NM GE CF6 CF650E2 30018NE AUTOPILOT INOPERATIVE A UIEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA15537MC 79091812 22403 AUTOPILOT WILL NOT ENGAGE. AUTOPILOT PUT AIRPLANE IN A 45 DEGREE BANK LT AND RT. DISENGAGED AUTOPILOT, STABILIZED AIRCRAFT AND RE-ENGAGED AUTOPILOT, AIRCRAFT STARTED ROLLING AGAIN. THE AIRCRAFT DIVERTED. RE-RACKED THE AUTOPILOT ROLL COMPUTER IAW MM, AUTOPILOTS CHECK GOOD NOW. SWAPPED AND AUTOPILOT ROLL COMPUTERS FOR TROUBLESHOOTING IAW MM. PN AND SN RECORDED ON LOG PAGE. (K) 2L74 4F4 F A20WE E23EA 20050524002662005052400266NE 2005 5 24 UIEA200500059 220050425A7310AC9227F1740 FUEL FILTER BOEING747 74747UF 1384949NM GE CF6 CF680C2B2 30025NE NR 3 ENGINE UNSERVICEABLE A UIEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA15499MC 29260 AIR TURN BACK. STATUS MESSAGE: ENG 3 FUEL FILTER. THE AIRCRAFT RETURNED TO DEPARTURE. REMOVED AND REPLACED FUEL FILTER IAW MM, LEAK CHECKED SATISFACTORY. (K) 2L74 4F4 FRT1384945 E13NE 20050524002692005052400269NM 2005 5 24 UIEA200500061 120050421A531065B17951 SUPPORT BEAM BOEING747 74747UF 1384949NM FUSELAGE DAMAGED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15493MC 29254 STA 1810 SIDE CARGO DOOR SILL SUPPORT BEAM DAMAGED AT ROLLOUT SAFETY STOPS. FORM 8100-9 SHOWS THAT THE DAMAGED AREA WAS TRIMMED OUT AND A REPAIR ANGLE IS INSTALLED. (K) 2L74 4F RT1384945 20050524002712005052400271NM 2005 5 24 UIEA200500063 120050426A531265B8356321 BULKHEAD BOEING747 747228F 1384895NM GE CF6 CF650E2 30018NE FUSELAGE CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15536MC 21576 BS 400 BULKHEAD WEB CUT OUT FOR NOSE GEAR RETRACT ACTUATOR PAN FOUND BOTH LOWER CORNERS CRACKED. (K) 2L74 4F4 F A20WE E23EA 20050524002732005052400273NM 2005 5 24 UIEA200500065 120050426A5414 PYLON BOEING747 747228F 1384895NM GE CF6 CF650E2 30018NE NR 1 CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15536MC 21576 LT WING NR 1 PYLON STRUT DOOR 453BL UPPER CORNER CRACKED. (K) 2L74 4F4 F A20WE E23EA 20050524002762005052400276NM 2005 5 24 UIEA200500067 120050426A5312 PRESSURE PANEL BOEING747 747228F 1384895NM GE CF6 CF650E2 30018NE FUSELAGE CORRODED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15536MC 21576 BS 1408, LBL 78 WHEEL WELL PRESSURE DECK CORRODED AT FASTENERS LOCATIONS. PRESSURE DECK REPAIRED IAW MM. (K) 2L74 4F4 F A20WE E23EA 20050524002772005052400277NM 2005 5 24 AWXA200500540 120050509A3350321430 BATTERY PACK AIRBUSA319 A319132 3930340NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28802AW 924 JFK - EEL - DURING 8-DAY CHECK THE LT OVERWING EMERGENCY LIGHT POWER SUPPLY BATTERY FAILED DURING EMERGENCY LIGHT TEST. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050524003142005052400314NM 2005 5 24 2005UALA00399 120050502A5322 SHEAR TIE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29586UA 26710 CIRCUMFERENTIAL FRAME SHEAR TIE CORRODED AT STA 1480 + 3 INCHES LEFT OF STR 30. FABRICATED AND INSTALLED NEW SHEAR TIE. 2L72 4F4 FRTA2NM E17NE 20050524003162005052400316NM 2005 5 24 2005UALA00401 120050502A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29586UA 26710 FLOORBEAM AT STA 1640, RBL 60 IS CORRODED. FLOORBEAM WAS BLENDED TO REMOVE CORROSION AND REPAIR STRAP INSTALLED ON THE FLOOR BEAM UPPER CAP. 2L72 4F4 FRTA2NM E17NE 20050524003182005052400318NM 2005 5 24 2005UALA00403 120050502A2824 CONNECTOR BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CROSSFEED VALVE BURNED A UALAK NONE O OTHER ININSP/MAINT 1 WP29383UA 24658 ACCOMPLISHING TEST OF CROSSFEED VALVE, FOUND VALVE INOP AND ELECTRICAL CONNECTOR TO VALVE BURNED. FUEL CROSSFEED VALVE LIGHT ILLUMINATED BRIGHT IN ALL SWITCH POSITIONS. REPLACED FUEL CROSSFEED VALVE MOTOR ACTUATOR ASSEMBLY V39 AND CONNECTOR D792. REMOVED ACTUATOR ASSY WAS DIFFICULT TO OPERATE MANUALLY FROM CLOSE TO OPEN POSITION. CONNECTOR D792, PIN "B" WAS BURNED AND SHOWED EVIDENCE OF CORROSION. 2L72 4F4 FRTA16WE E2GL 20050524003242005052400324EU 2005 5 24 2005UALA00412 120050504A2910 O-RING AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE YELLOW HYD SYS FAILED A UALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 WP29446UA 834 YELLOW RESERVOIR LOW LEVEL FAILURE WITH BLUE SYS LOW AND GREEN FLUCTUATING AS WELL. FLIGHT LANDED WITHOUT INCIDENT. REPLACED B-NUT AND O-RING ON PTU MANIFOLD REF MM 29-13-15-991-001 PTU MANIFOLD ITEM 5 AND 52 LEAK CHECK OK. FOUND BAD O-RING SOURCE OF LEAK. SERVICED YELLOW SYSTEM. 2L72 4F4 FRTA28NM E40NE 20050525000052005052500005EU 2005 5 25 USAA050500 120050410A5311D5311282600101 FRAME AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19714US17533 1046 PIT - FOUND FRAME CORRODED 1 INCH BY 1 INCH BY .072 INCH DEEP AREA, TOP SURFACE OF FRAME FROM C12-16, 12 INCHES LEFT OF C/L. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 53-11-14 FIG 106. CORROSION LEVEL 1, TASK JA-220-53500. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 53-11-14 FIG 108. (M) 2L72 4F RTA28NM 20050525000222005052500022CE 2005 5 25 DXTA200500709 120050505A3241 ANNUNCIATOR CESSNA650 650 2076802CE ANTI SKID SYS ILLUMINATED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07713QS 6507103 DURING OCF TAKEOFF ROLL, AT 70 KIAS, THE ANTI-SKID ANNUNICATOR ILLUMINATED. ABORTED TAKEOFF. LIGHT WENT OUT AFTER WE EXCITED THE RUNWAY. TROUBLESHOT ANTI-SKID LIGHT ILLUMINATED. TROUBLESHOT TRANSDUCER. ALL VOLTAGES AND OHMS READ CORRECTLY. TROUBLESHOT WIRING AND CONNECTED ALL GOOD. TROUBLESHOT CONTROL BOX, BY SLAVING IN KNOWN GOOD CONTROL BOX. ANNUNCIATOR EXTINGUISHED, RECONNECTED OLD CONTROL BOX, LIGHT REMAINED EXTINGUISHED. ALL TEST GOOD, CLEANED ALL CONNECTORS, TAXIED AIRCRAFT AT LOW AND HIGH SPEED. 2L72 4F A9NM 20050525000262005052500026NM 2005 5 25 DHL2005740501 120050413A5754 RIB BOEING727 7272Q9 138448MNM NR 5 SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 NR 5 SLAT INTERIOR AT ACTUATOR ATTACHMENT INBD AND OUTBD RIBS CRACKED NDT CONFIRMED. REMOVED AND REINSTALLED NR 5 SLAT PER 727 MM 27-81-11. OPS CHECKED OK IAW B727 MM 27-81-00. FAB Z NEW RIBS FROM 2024T3 .0140 PO NR 9002012 SIZE 15 1/8" BY 5 1/8" IAW B727 SRM 51-20-1 AND 57-50-2 FIG 2. TREATED AND PRIMED PARTS AND AREA IAW B727 SRM 51-10-2. REMOVED AND REPLACED RIBS AT NR 5 SLAT ACTUATOR ATTACHMENT I/B AND O/B RIBS IAW B727 SRM 51-30-2. 2L73 4F RTA3WE 20050525000362005052500036NM 2005 5 25 05FDEA01208 120050505A5315 FLOORBEAM BOEING727 727200 138407ENM CARGO BAY DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25254FE 20936 EVALUATE PREVIOUS REPAIR STA 1070 MCD FLOORBEAM RBL 12--RBL 62 UPPER CHORD FOR REPAIR STATUS (MAJOR/MINOR) AND FAA APROVAL. EVALUATED PREVIOUS REPAIR, FOUND TO BE IAW SR 27-53-034 REP NR 5 AND A MAJOR REPAIR IAW FED EX GMM 6-2-100. 2L73 4F RTA3WE 20050525000422005052500042EA 2005 5 25 VTZA200500068 120050505A5712601R102328 RIB CNDAIRCL600 CL6002B19 1900309EA WING CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27625BR 7214 RIGHT BATT RIB IS CRACKED .750 INCH BETWEEN THE ATTACHING FASTENERS. 2L72 4F RTA21EA 20050525000452005052500045 2005 5 25 REXA2005049 420050411A2561 G SWITCH CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE ELT FAILED A REXAK NONE L NO TEST ININSP/MAINT 1 SO258775A4867 01439 7775 ELT FAILS G-SWITCH TEST. REMOVED IAW PA 25-048D AND FAR PART 91.207 FOR REPAIR. REMOVED ELT FOR MAINTENANCE IAW FAR 91.207. (K) 2L72 4F4 FRTA21EA E15NE 20050525000512005052500051NM 2005 5 25 USAA050501 120050412A5340 FITTING BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19440US39307 24811 CLT - FOUND BEAM FITTING CRACKED .75 INCH, STATION 601 LEFT LOWER BEAM FITTING. FABRICATED AND INSTALLED REPAIR ANGLE IAW EA 96446 AND TR 53-62-01. (M) 2L72 4F RTA16WE 20050525000522005052500052EU 2005 5 25 USAA050479 120050410A5315D5347209000500 FLOORBEAM AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19106US 1044 PIT - FOUND FLOORBEAM CORRODED 2 INCHES BY 2 INCHES BY .060 INCH DEEP AREA, FLOOR SUPPORT AT Y750 ABOVE C68. CORROSION LEVEL 1, TASK JA-260-53500. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-72-11. (M) 2L72 4F RTA28NM 20050525000542005052500054NM 2005 5 25 USAA050476 120050328A575465C26603102A SKIN BOEING737 737401 1384701NM NR 4 SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19420US44993 23987 PIT - FOUND NR 4 SLAT DELAMINATED 3 INCH BY 6 INCH AREA, NR 4 SLAT UPPER INBOARD CORNER. BOEING SRM REPAIR 17 PER 51-70-10. (M) 2L72 4F RTA16WE 20050525000662005052500066EA 2005 5 25 REXA2005058 120050428A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LAVATORY MALFUNCTIONED A REXAO OTHER N FALSE WARNING APAPPROACH 1 SO258775A 7775 SMOKE TOILET MESSAGE ON FINAL. LANDING UNEVENTFUL. PERFORMED OPERATIONAL TEST OF LAV SMOKE SYSTEM, IAW AMM AND OF THE LAV SMOKE DETECTOR IAW AMM. BOTH OPS CHECK GOOD. (K) 2L72 4F4 FRTA21EA E15NE 20050525000712005052500071SO 2005 5 25 O2G2005F00006 120050415A27501159SOC2135 SHAFT GULSTMG1159 G1159A 3970109SO RROYCESPEY SPEY511* 54523EU FLAP DRIVE FAILED E O2GAO OTHER F FLT CONT AFFECTED DEDESCENT 1 NE03123TL 452 FLAPS STUCK AT 8 DEGREES. REPLACED BROKEN FLAP DRIVE SHAFT. (K) 2L72 4F4 F A12EA E2EU 20050525000752005052500075CE 2005 5 25 DXTA200500711 120050506A4920GTCP15036W APU CESSNA750 750 2076810CE FAILED E DXTAO OTHER B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 GL07977QS6397 7500077 CABIN FILLED WITH OILY SMELLING SMOKE AFTER APU STARTED ON GROUND. SIGNIFICANT DROP NOTED ON APU OIL LEVEL. CHECKED APU OIL LEVEL FOUND TO BE JUST BELOW THE ADD OIL LINE, STARTED APU AND RAN OIL AIRCONDITIONING AT DIFFERENT TEMPERATURE SETTINGS. COULD NOT DUPLICATE OIL SMELLING SMOKE IN THE CABIN. REMOVED COALESSER CLOTHS AND CLEANING THOROUGHLY REINSTALLED COALESSER CLOTHS AND REINSTALLED. OPERATED THE APU AND RAN AIR CONDITIONING PACKS. NO SMOKE OR SMELL NOTED. PERFORMED LEAK CHECK, NO LEAKS NOTED. ALL WORK PERFORMED IAW CE750 MM 12-10-01. 2L72 4J RTT00007WI 20050525000772005052500077NM 2005 5 25 AALA20050308 120050509A3397 CONNECTOR BOEING767 767323 1385205NM EMERGENCY LIGHT LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21399AN 29606 LAX - SEAT MOUNTED ESCAPE PATH LIGHTS AT SEATS 21H TO 23H INOPERATIVE. SECURED LOOSE WIRE CONNECTOR ON SEAT 20H LIGHTS FOR SEAT MOUNTED ESCAPE PATH LIGHTS AT SEATS 21H TO 23H. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA1NM 20050525000782005052500078NM 2005 5 25 AALA20050301 120050504A3350 LIGHT BOEING737 737823 13844BZNM CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21963AN 29543 DFW - FORWARD SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLIES AT 7D AND 27D IS BROKEN. REPLACED SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLIES AT 7D AND 27D. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA16WE 20050525000792005052500079NM 2005 5 25 AALA20050302 120050504A3350 FUSE BOEING777 777223 1385213NM BATTERY PACK INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21762AN 31479 DFW - EMERGENCY PATH LIGHTING IN FIRST CLASS GALLEY FORWARD RIGHT HAND SIDE INOPERATIVE. REPLACED FUSE IN BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTT00001SE 20050525000802005052500080WP 2005 5 25 AALA20050303 120050503A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21417AA 49328 SFO - OVERHEAD EMERGENCY LIGHTS OVER ROWS 9 TO 11 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS OVER ROWS 9 TO 11. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F A6WE 20050525000812005052500081NM 2005 5 25 AALA20050304 120050506A3397 WIRE BOEING767 767323 1385205NM EMERGENCY LIGHT LOOSE A AALAK NONE O OTHER ININSP/MAINT 1 SW21379AA 25448 SFO - EMERGENCY LIGHT ON SEAT 13H IS INOPERATIVE. REINSTALLED LOOSE ELECTRICAL CONNECTION AT SEAT 13H FOR EMERGENCY LIGHT ON SEAT 13H. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA1NM 20050525000822005052500082NM 2005 5 25 AALA20050307 120050508A3350 LIGHT BOEING757 757223 1384957NM CABIN BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21197AN 32391 DFW - EMERGENCY LIGHT ASSEMBLY AT 17D BROKEN. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA2NM 20050525000832005052500083EU 2005 5 25 AALA20050305 120050507A3260 PROXIMITY SENSOR AIRBUS300 A300B4605R 3930308EU MLG INOPERATIVE A AALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW2170074 517 UNABLE TO RETRACT LANDING GEAR ON TAKEOFF. SWITCHED TO SYSTEM TWO BUT WAS STILL UNABLE TO RETRACT GEAR. PITCH TRIM ONE NUMBER 2 CLICKED OFF AND WOULD NOT RESET. AERONAUTICAL TELECOMMUNICATIONS SYSTEM SWITCHED OFF AND WOULD NOT RESET. BOTH FLIGHT DIRECTORS SWITCHED OFF AND WOULD NOT RESET. REPLACED PROXIMITY BOX AND PERFORMED BITE TEST WITH NO FAULTS NOTED. REPLACED NOSE LANDING GEAR PROXIMITY SWITCHES 55GB AND 82GB AND ADJUSTED PER MM 32-00-00-4. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA35EU 20050525000842005052500084WP 2005 5 25 AALA20050306 120050508A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21490AA 49683 SFO - OVERHEAD EMERGENCY EXIT LIGHTS AT SEATS 28D TO 31D INOPERATIVE. RECHARGED THE EMERGENCY LIGHTS SYSTEM IN THE ARM POSITION FOR THE OVERHEAD EMERGENCY EXIT LIGHTS AT SEATS 28D TO 31D. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F A6WE 20050525000882005052500088EA 2005 5 25 SWIA200514964 120050504A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07443SW 7638 AFT CEILING EMERGENCY LIGHT INOPERATIVE. RELAMPED AFT CEILING EMERGENCY LIGHT IAW CRJ MM33-51-00. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050525000892005052500089SO 2005 5 25 SWIA200514965 120050504A3350 BULB EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07585SW 120353 AFT FLOOR EMERGENCY LAMP INOPERATIVE. REPLACED BULB IN AFT FLOOR EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050525000902005052500090EA 2005 5 25 SWIA200514966 120050505A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY MALFUNCTIONED A SWIAO OTHER N FALSE WARNING CRCRUISE 1 NM07441SW 7602 CARGO SMOKE MESSAGE. MESSAGE CLEARED WITHIN 4 SECONDS. REPLACED FORWARD CARGO SMOKE DETECTOR. OPERATIONAL CHECK GOOD, PN: 473597-19 SN OFF: 1942. 2L72 4F RTA21EA 20050525000912005052500091EA 2005 5 25 SWIA200514967 120050507A274070623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07410SW4340 4340 7066 STAB TRIM CH 2 INOPERATIVE. REPLACED STAB TRIM ACTUATOR AND MOTOR CONTROL UNIT IAW 27-42-01. OPERATIONAL CHECK GOOD, PN: 8396-3 SN OFF: 843. 2L72 4F RTA21EA 20050525000922005052500092EA 2005 5 25 SWIA200514968 120050505A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07464SW 7827 EMERGENCY FLOOR LIGHTING HAS ONE SEGMENT INOPERATIVE. REPLACED LIGHT STRIP IAW MM 33-51-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050525000942005052500094 2005 5 25 ASMF200505009 420050506A34149650449002 COMPUTER DOUG DC9 DC982 3022082WP STALL WARNING FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23505MD11258 49149 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING TAXING TO AUTO SLAT FAIL AND AUTO SLAT DISAGREE LIGHTS COME ON. SYSTEM WAS RESET AND TESTED BUT FAILURE CONTINUED. STALL WARNING COMPUTER BITE WAS PERFORMED AND DETECTING FAILURE IN THE NUMBER 1. THE STALL WARNING COMPUTER WAS REPLACED IAW MM 34-14-00, TESTED CORRECT. 2L72 4F A6WE 20050525000952005052500095NM 2005 5 25 ASMF200505010 120050506A2410729825J IDG BOEING757 757200 1384950NM RIGHT FAILED W ASMFK NONE KJ FLUID LOSS WARNING INDICATION ININSP/MAINT 1 SW23703AM234488714 27203 CAPTAIN REPORTED RIGHT IDG WAS DEACTIVATED AND LEFT IDG WITH HIGH TEMPERATURE. THE RIGHT IDG WAS REPLACED IAW MM 24-11-01, TESTED CORRECT. THE LEFT IDG HIGH TEMPERATURE REPORT WAS VERIFIED AND DETECTING LEAK IN DRAIN SEAL. THE LEFT IDG REPORT WAS DEFERRED IAW MEL 24-00-01. DURING OVERNIGHT SERVICE, THE LEFT IDG WAS REPLACED IAW MM 24-11-01, PAGE 401, TESTED CORRECT. DEFERRED REPORT WAS CLOSED. 2L72 4F RTA2NM 20050525000962005052500096 2005 5 25 ASMF200505011 420050508A2210922710127 RELAY DOUG MD88 MD88 3023688NM AUTOPILOT FAILED W ASMFA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW23160PL 49763 AIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT GDL AS CONSEQUENCE OF AUTOPILOT WAS OUT OF SERVICE. LEFT PFD INDICATOR WAS REPLACED IAW MM 34-24-00; TESTS WERE PERFORMED IN STP, SHOWING FAILURE CODE A/P HEART BEAT TEST FAILURE AND AIL/MECH TORQ SWITCH FAILURE. BOTH DFGC WERE REPLACED; TESTS WERE PERFORMED SHOWING FAILURE CODE PITCH TRIM 440 AND A/P FAILURE CODE 440 AND 312. COMPUTERS CONTROL PANEL WAS REPLACED IAW MM 22-01-04; AUTO TEST RTS WAS PERFORMED SHOWING FAILURE CODE PITCH TRIM 440 IN BOTH COMPUTERS. THE R20-14 WAS REPLACED AND TESTS WERE PERFORMED IAW MM 22-01-05, ALL CORRECT. 2L72 4F RTA6WE 20050525000972005052500097NM 2005 5 25 BB05035 120050510A335020131A BATTERY BOEING767 767201 1385125NM RIGHT OUT OF POSITION A USAAK NONE O OTHER ININSP/MAINT 1 EA19650US 23902 FRA - FOUND FORWARD RIGHT FLOOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE FOUND THE BATTERY PACK OUT OF THE CRADLE AND REINSTALLED IT. 2L72 4F RTA1NM 20050525000992005052500099NM 2005 5 25 AMTA200500421 120050505A5312 SHIM BOEING757 75723N 1384973NM RROYCERB211 RB211* 54555NE BULKHEAD MIGRATED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11519AT 27975 ATTACH FITTING, HORIZONTAL STABILIZER RT PIVOT FITTING HAS MIGRATING SHIMS AT ATTACHMENT TO BS 1862.7, BULKHEAD, 1 LOCATION. COMPLIED WITH PART 1: TIME LIMITED REPAIR OF ERA 757-53R-587-3IR FOR THE HORIZONTAL STABILIZER RT PIVOT FITTING. (K) 2L72 4F4 FRTA2NM A12EU 20050525001002005052500100NM 2005 5 25 DHL2005740505 120050327A5753 SKIN BOEING727 7272Q9 138448MNM TE FLAP DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 RT WING OUTBD AFT-FLAP TRAILING EDGE INBD CORNER IS DELAMINATED LOWER SURFACE. CUTOUT DAMAGED LWR SURFACE APPROX 3 INCH BY 5 INCH BAGGED FOR MOISTURE REMOVAL IAW B727 SRM 51-40-20 FIG 32. REMOVAL AND REPLACED HONEYCOMB CORE APPROX 3 INCH BY 4 INCH USING DUR-5052-4.4-3/16-N-.750 PO NR 9911139 IAW B727 SRM 51-40-20 FIG 32. FABRICATED ONE FILLER APPROX 3 INCH BY 5 INCH AND 1 DOUBLER APPROX 4 1/2 INCH BY 6 1/2 INCH USING 2024T3 .016 PO NR 9001660 IAW B727 SRM 57-50-2 FIG 4. CLEANED PREPPED AND APPLIED ADHESIVE PRIMER ADHESIVE TO ALL REPAIR SURFACES AND BAGGED FOR BONDING IAW B727 SRM 51-40-20 FIG 32. CURED REPAIR CLEANED AND PERFORMED POST BOND INSP WITH NO DELAM NOTED IAW B727 SRM 51-40-20 PARA 0. TREATED PR2L73 4F RTA3WE 20050525001032005052500103NM 2005 5 25 AMTA200500422 120050505A5412 SHIM BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE NR 1 STRUT MIGRATED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11519AT 27975 31611 BULKHEAD/ FIREWALL, NR 1 ENGINE STRUT UPPER LINK FITTING HAS MIGRATING SHIM AT OB HORIZONTAL FLANGE PP, STA 174.3. COMPLIED WITH PART 1 OF ERA 757-54R-5870. (K) 2L72 4F4 FRTA2NM E12EU 20050525001042005052500104NM 2005 5 25 C7WA200400082 120050330A278110473 SWITCH BOEING727 7272J7 138400ENM PWA JT8 JT8D17 52049NE LT WING INTERMITTENT A C7WAO OTHER N FALSE WARNING CLCLIMB 1 SO29128NA 20879 NR 2 KRUGER FLAP EXTEND LIGHT REMAINED ON AFTER TAKEOFF. REMOVED AND REPLACED NR 2 KRUGER FLAP SWITCH IAW MM. 2L73 4F4 F A3WE E2EA 20050525001052005052500105NM 2005 5 25 C7WA200500094 120050411A527021EN96 SWITCH BOEING727 727222 1384073NM PWA JT8 JT8D5 52046NE MAIN CARGO DOOR OUT OF ADJUST A C7WAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO297642U 19915 CARGO DOOR LIGHT ILLUMINATED AFTER TAKEOFF. ADJUSTED MAIN CARGO DOOR VENT LIGHT SWITCH IAW MM. OPS CHECK GOOD. (K) 2L73 4F4 F A3WE E2EA 20050525001062005052500106NM 2005 5 25 C7WA200500098 120050411A29135718601 PUMP BOEING727 727222 1384073NM PWA JT8 JT8D5 52046NE B-HYD SYS INOPERATIVE A C7WAK NONE O OTHER ININSP/MAINT 1 SO297642U 19915 AIR RETURN: NR 1 AND NR 2 (B) SYSTEM HYDRAULIC PUMPS FAILED. REMOVED AND REPLACED NR 1 AND NR 2 (B) SYSTEM HYDRAULIC PUMPS. REMOVED AND REPLACED (B) SYSTEM CASE DRAIN FILTERS. (K) 2L73 4F4 F A3WE E2EA 20050525001082005052500108NM 2005 5 25 PCS2005F00001 120050222A21317638101 CONTROLLER BOEING727 727212 138407GNM PWA JT8 JT8D17 52049NE CABIN PRESSURE INTERMITTENT A PCSAA UNSCHED LANDING O OTHER CLCLIMB 1 SO29598AJ 21947 CREW REPORTED AC WILL NOT PRESSURIZE, OUTFLOW VALVE WILL NOT OPERATE IN ANY MODE. AC RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT PRESSURIZATION AND RERACKED THE CABIN PRESSURE CONTROLLER AND ACCOMPLISHED A FUNCTIONAL TEST OF THE CABIN PRESSURIZATION SYSTEM IAW MM, SYSTEM TESTED GOOD. THE AC WAS RETURNED TO SERVICE AND DISPATCHED TO THE INTENDED DESTINATION WITHOUT FURTHER INCIDENT. (K) 2L73 4F4 F A3WE E2EA 20050525001122005052500112CE 2005 5 25 CCJ2005F00000 120050413A321012430192 BRACKET CESSNA210 210M 2073450CE CONT O520 IO520* 17032SO GEAR DOWN BROKEN E CCJAO OTHER O OTHER LDLANDING 1 WP156035N 21062903 THERE WAS NO (GEAR DOWN) INDICATION WHEN THE LANDING GEAR WAS EXTENDED. PILOT DECLARED EMERGENCY AND DIVERTED TO AN AIRPORT WITH A LONGER RUNWAY. LANDING WAS NORMAL AND UNEVENTFUL. UPON EXAMINATION IT WAS FOUND THAT THE BRACKET HOLDING THE NOSE GEAR (DOWN) SQUAT SWITCH HAD BROKEN AND WAS DANGLING. (K) 1H71 3O3 O 3A21 E5CE 20050525001142005052500114SO 2005 5 25 GGS2005F00000 220050426A74146310 MAGNETO CESSNA207 207A 2073604CE CONT O520 IO520F 17032SO ENGINE INTERMITTENT E GGSAO OTHER R PARTIAL RPM/PWR LOSS CRCRUISE 1 NM13207YH 20700637 MAGNETO FAILED DURING FLIGHT. UPON INSPECTION IT WAS DETERMINED THAT THE CONDENSER FAILED TO TAKE A CHARGE. THE SWIVEL TERMINAL ON THE CONTACT POINT SIDE OF THE CONDENSER WAS ROTATED AND THEN THE CONDENSER WAS ABLE TO TAKE A CHARGE. SUSPECT CORROSION AT SWIVEL, RESULTING IN AN OPEN IN THE CONDENSER. REPLACEMENT OF CONDENSER WITH CURRENT PRODUCTION CONDENSER AT NEXT OPPORTUNITY. (NM13200502744) (K) 1H71 3O3 O A16CE E5CE 20050525001152005052500115NM 2005 5 25 JGV2005F00000 120050428A5320CYLB50858 CHECK VALVE ISRAEL1125 1125 NM BULKHEAD BROKEN B JGVRK NONE O OTHER ININSP/MAINT 1 CE091125 6173 021 DURING PRESSURIZATION OF CABIN, COULD NOT ACHIEVE MAX DIFF. INVESTIGATION REVEALED A DEFECTIVE CHECK VALVE INSTALLED IN THE AFT PRESSURE BULKHEAD. THE DEFECTIVE CHECK VALVE HAD A BROKEN SPRING AND THE CHECK VALVE WAS INSTALLED WITH THE HINGE ORIENTED HORIZONTALY WITH THE HINGE HORIZONTAL, WHEN THE SPRING FAILED THE VALUE FAILS IN THE OPEN POSITION. THESE CHECK VALVES ARE NOT CURRENTLY INCLUDED IN THE INSPECTION PROGRAM. RECOMMENDATIONS: INSTALL VALVE WITH HINGE IN THE VERTICAL POSITION. INSPECT VALVE DURING THE (C) INSPECTION. (CE09200503757) (K) 2L72 4F RTA16NM 20050525001172005052500117SO 2005 5 25 XGN2005F00000 220050423A8530TISN712BCA CYLINDER HEAD CESSNA402 402B 207590PCE CONT O520 TSIO520E 17040SO NR 5 CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW053378Q 402B0334 182909R FOUND CRACKED CYLINDER HEAD WHILE DOING A 50 HR INSPECTION. DUE TO THE NR OF CYLINDER HEAD FAILURES, DOING COMPRESSION CHECK AT EACH SCHEDULED INSPECTIONS (50 HOURS). (K) 1L72 3O3 O A7CE E8CE 20050525001202005052500120SO 2005 5 25 XGN2005F00002 220050426A8530TISN712ACA CYLINDER HEAD BEECH 58 58 1152740CE CONT O520 IO520C 17032SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW05577W 1851 TH375 210755 CYLINDER HEAD CRACKED. FOUND DURING 100 HR INSPECTION. THIS IS AN ONGOING PROBLEM THAT WE ARE FINDING IN OUR FLEET OF AIRCRAFT. (K) 1L72 3O3 O 3A16 E5CE 20050525001242005052500124SO 2005 5 25 C2XA05SH029 120050507A532014522459003 ANGLE EMB 135 EMB135LR 3260305SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714522 145383 DURING C-CHECK CENTER RAMP ANGLE HAS CORROSION AT FRAME 20. MAINTENANCE REMOVED AND REPLACED CENTER RAMP ANGLE AT FRAME 20 IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050525001252005052500125SO 2005 5 25 C2XA05CL035 120050508A26123601135 FIRE DETECTOR EMB 135 EMB135ER 3260203SO APU INOPERATIVE A C2XAO OTHER N FALSE WARNING CRCRUISE 1 SW2719503 145176 CLE - THE CREW REPORTED A APU FIRE INDICATION WHILE STARTING THE APU IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE APU FIRE/OVERHEAT DETECTOR. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20050525001262005052500126SO 2005 5 25 C2XA05BT026 120050509A3230355022002 ELECTRICAL BOX EMB 145 EMB145LR 3260212SO FUSELAGE MALFUNCTIONED A C2XAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW27129217075 7075 145354 CREW REPORTED, LANDING GEAR/AIR GROUND FAIL WARNING WHEN EXTENDING LANDING GEAR. MAINTENANCE REMOVED AND REPLACED LGEU IAW EMB145 AMM 32-32-01. GEAR SWING OPS, CHECKED GOOD. 2L72 4T RTT00011AT 20050525001292005052500129NE 2005 5 25 0500683204 220050507A7532121762GH4 DRIVE SHAFT AIRBUS320 A320211 3930320EU GE CFM56 CFM565A 13802NE NR 2 ENGINE BROKEN A NWAAC ABORTED TAKEOFF M OVER TEMP TOTAKEOFF 1 GL01304US 040 731216 DURING TAKEOFF ROLL, THE NR 2 ENGINE EGT EXCEEDED 890C. TAKEOFF ABORTED AT 110 KNOTS. MAINTENANCE FOUND NR 2 ENGINE VBV INTER CONNECTING FLEX DRIVE SHAFT AT 9:00 BROKEN. MAINTENANCE REPOLACED FLEX DRIVE SHAFT. 2L72 4F4 FRTA28NM E29NE 20050525001302005052500130WP 2005 5 25 U2RA2982 120050510A5330 SKIN DOUG DC8 DC863F 302198FWP FUSELAGE CORRODED A U2RAK NONE O OTHER ININSP/MAINT 1 GL23921R 684252039 46145 FS 12 IN NOSE WHEEL WELL CEILING SKIN BULGING WITH 3 POPPED RIVETS, IDENTIFIED AS LEVEL 2 CORROSION. 2L74 4F 4A25 20050525001312005052500131WP 2005 5 25 U2RA3396 120050510A5330 SKIN DOUG DC8 DC863F 302198FWP FUSELAGE CRACKED A U2RAK NONE O OTHER ININSP/MAINT 1 GL23921R 684252039 46145 R2 DOOR HAS CRACK INDICATION AT UPPER AFT CORNER FS 1660, L11R. 2L74 4F 4A25 20050525001332005052500133WP 2005 5 25 U2RA3399 120050510A57135644972502 STRINGER DOUG DC8 DC863F 302198FWP RT WING CRACKED A U2RAK NONE O OTHER ININSP/MAINT 1 GL23921R 684252039 46145 RIGHT WING LOWER INNER STRINGER CRACKED AT WING STATION X624. 2L74 4F 4A25 20050525001342005052500134WP 2005 5 25 U2RA3216 120050510A534037730732 FITTING DOUG DC8 DC863F 302198FWP FUSELAGE CRACKED A U2RAK NONE O OTHER ININSP/MAINT 1 GL23921R 684252039 46145 FITTING CRACKED AFT OF CARGO DOOR AT FS 300 AT CUSP LT SIDE. 2L74 4F 4A25 20050525001362005052500136WP 2005 5 25 U2RA3147 120050510A531156119433N FRAME DOUG DC8 DC863F 302198FWP FUSELAGE CORRODED A U2RAK NONE O OTHER ININSP/MAINT 1 GL23921R 684252039 46145 SEVERAL SMALL AREAS OF CORROSION IN FWD ACCESSORY COMPARTMENT AT AFT BULKHEAD CIRCUMFERENTIAL FS 80 L32L TO L32R. IDENTIFIED AS LEVEL 2 CORROSION. 2L74 4F 4A25 20050525001372005052500137WP 2005 5 25 U2RA3142 120050510A5330 PRESSURE PANEL DOUG DC8 DC863F 302198FWP MLG WW CORRODED A U2RAK NONE O OTHER ININSP/MAINT 1 GL23921R 684252039 46145 FS 980 TO FS 970 TOP SURFACE OF THE RIGHT MAIN LANDING GEAR WELL HAS POPPED RIVETS/BULGING AT ATTACH ANGLE, IDENTIFIED AS LEVEL 2 CORROSION. 2L74 4F 4A25 20050525001412005052500141NM 2005 5 25 96 120050510A5320 FLOOR SUPPORT DOUG MD88 MD88 3023688NM FUSELAGE CORRODED B DU4RK NONE O OTHER ININSP/MAINT 1 SO1512FQ 49766 CABIN FLOOR SUPPORT STRUCTURE FS 160 - 200 RBL 38 CORRODED. 2L72 4F RTA6WE 20050525001432005052500143EU 2005 5 25 USAA050482 120050316A5754F5746357800300 SKIN AIRBUS330 A330323 3930335EU SLAT DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW22938 0337 BFM - FOUND SLAT WITH DAMAGED AREA, 9 INCHES LONG BY 3.75 INCH WIDE BY .380 INCHES DEEP, RT NR 5 SLAT L/E. CUT OUT DAMAGE AND INSTALLED NOSE SKIN REPAIR PER SRM 57-40-00 FIG 204, SHT 3 AND EA 96392. (M) 2L72 4F RTA46NM 20050525001452005052500145NM 2005 5 25 USAA050485 120050406A531511T5010 FLOORBEAM BOEING767 7672B7 1385107NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19651US61980 24764 BFM - FOUND CORROSION 1.6 INCH LONG BY 1.3 INCHES WIDE BY .035 INCH DEEP, BS 870 AND 860 AT RBL 74.8 AT MAIN CABIN FLOOR PANELS. ACCOMPLISHED FLOORBEAM SPLICE REPAIR PER SRM 53-00-51 FIG 203. (M) 2L72 4F RTA1NM 20050525001462005052500146NM 2005 5 25 USAA050490 120050316A5320140T25409 INTERCOSTAL BOEING767 767201 1385125NM CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19648US68950 23900 BFM - FOUND INTERCOSTAL WITH TWO CRACKS, TOTAL LENGTH APPROX .6250 INCH, BS 1395-1417 AT LBL 39. REMOVED AND INSTALLED REPLACEMENT NEWLY FABRICATED PART PER SRM 51-10-02, 51-20-01, 51-40-02, EA 96331. (M) 2L72 4F RTA1NM 20050525001472005052500147NM 2005 5 25 USAA050489 120050316A5320140T25409 INTERCOSTAL BOEING767 767201 1385125NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19648US68950 23900 FOUND INTERCOSTAL CRACKED APPROX .3750, BS 1395-1417 AT RBL 43. REMOVED AND REPLACED WITH NEWLY FABRICATED PART PE SRM 51-10-02, 51-20-01, 51-40-02 AND EA 96331. (M) 2L72 4F RTA1NM 20050525001492005052500149EU 2005 5 25 USAA050486 120050317A5347F5331140220001 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW22938 0337 BFM - FOUND SEAT TRACK CORRODED 2 INCHES LONG BY 1 INCH WIDE BY .040 INCH DEEP, CABIN SEAT TRACK Y450 FRAME 47-50. REPLACED SEAT TRACK PER SRM 53-00-15. (M) 2L72 4F RTA46NM 20050525001522005052500152NM 2005 5 25 USAA050493 120050316A5320141T517614 FLOOR SUPPORT BOEING767 767201 1385125NM FUSLEAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19648US68950 23900 BFM - FOUND FLOOR SUPPORT BRACKET CRACKED .5 INCHES LONG, BS 325 AT L "0". REMOVED AND REPLACED WITH NEW FABRICATED REPLACEMENT PART PER SRM 51-10-02, 51-20-01, 51-40-02, EA 96335. (M) 2L72 4F RTA1NM 20050525001542005052500154EU 2005 5 25 USAA050481 120050315A5320F5331534420200 FLOOR SUPPORT AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW22938 0337 BFM - FOUND PANEL SUPPORT CORRODED 1 INCH LONG BY 1.5 INCHES WIDE BY .040 INCH DEEP, LOWER FUSE AC BAY, AFT END APPROX FRAME 44. REMOVED AND REPLACED SUPPORT PER SRM 51-72-11. (M) 2L72 4F RTA46NM 20050525001562005052500156NM 2005 5 25 USAA050495 120050316A5511 SPAR BOEING767 767201 1385125NM HORIZONTAL STAB CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19648US68950 23900 BFM - FOUND AUX FRONT SPAR CRACKED 2.35 INCHES, LT L/E HORIZ STAB STA 191-240.7 SPAR. REPAIRED SPAR CHORD WITH ANGLES, SHIMS AND FILLERS PER EA 96343. (M) 2L72 4F RTA1NM 20050525001572005052500157EU 2005 5 25 USAA050484 120050320A5320F5347946123200 PROFILE AIRBUS330 A330323 3930335EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW22938 0337 BFM - FOUND PROFILE L CRACKED 3 INCHES, AFT CABIN CUSP ANGLE BETWEEN FRAME 79-80 LEFT SIDE. INSTALLED NEW CUSP ANGLES UPPER AND LOWER PER SRM 53-00-13. (M) 2L72 4F RTA46NM 20050525001592005052500159EU 2005 5 25 USAA050487 120050312A5347F5327591620000 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW22938 0337 BFM - FOUND SEAT TRACK CORRODED 1.95 INCH LONG BY .40 INCH WIDE BY .015 INCH DEEP, Y-1550 AT FRAME 37 PLUS 10 INCHES. FABRICATED SEAT TRACK SPLICE PER SRM 53-00-15. CORROSION LEVEL 2, TASK C532134-01. FABRICATED SEAT TRACK SPLICE PER SRM 53-00-15. (M) 2L72 4F RTA46NM 20050525001622005052500162NM 2005 5 25 USAA050507 120050418A5320 SPLICE BOEING737 7374B7 1384702NM FS CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US39931 24781 CLT - FOUND STRINGER SPLICE WITH TWO CRACKS .250 INCH, EMANATING FROM 2 RIVETS IN S4L SPLICE WEB AT STATION 907. REPAIRED IAW SRM 51-20-02 AND 51-40-02. (M) 2L72 4F RTA16WE 20050525001672005052500167NM 2005 5 25 USAA050509 120050414A5340 STRINGER CLIP BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US39931 24781 CLT - FOUND TIE CLIP WITH TWO CRACKS AT .500 INCH, STATION 663 S10R. REPLACED WITH NEW CLIP IAW SRM 51-10-02. (M) 2L72 4F RTA16WE 20050525001692005052500169NM 2005 5 25 USAA050508 120050415A5340 STRINGER CLIP BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US39931 24781 CLT - FOUND TIE CLIP CRACKED 2.5 INCHES, STATION 500G S8R. REPLACED WITH NEW CLIP IAW 51-10-02. (M) 2L72 4F RTA16WE 20050525001722005052500172NM 2005 5 25 0500695531 120050330A5315 FLOORBEAM BOEING757 757251 1384970NM FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01531US 23846 DURING H-CHECK FOUND CRACK IN FLOORBEAM AT BS 660 LBL 45. REPAIRED PER EA 55-202918. 2L72 4F RTA2NM 20050525001742005052500174SO 2005 5 25 CHQA200500097 120050510A3260 PROXIMITY SWITCH EMB 145 EMB145LR 3260212SO MLG DIRTY A CHQAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL11288SK 145461 FLIGHT 3018 CHS-LGA - THE FLIGHT TOOK OFF FROM RUNWAY 21 AT CHS, AFTER NOSE GEAR RETRACTION, A LG/AIR GND FAIL MESSAGE APPEARED THE EICAS AND THE LANDING GEAR WOULD NOT RETRACT. THE QRH WAS FOLLOWED AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED TO THE FIELD. THE LANDING WAS UNEVENTFUL AND THE MESSAGE CLEARED ITSELF UPON LANDING. MAINTENANCE CLEANED THE PROXIMITY SWITCHES AND RESECURED THE CANNON PLUGS. THE GEAR WAS SWUNG AN NO MESSAGES WERE PRESENT. OPS CHECK GOOD IAW EMB 145 AMM 32-60. 2L72 4T RTT00011AT 20050525001752005052500175NM 2005 5 25 AWXA200500543 120050428A53206552878533 STRUCTURE BOEING737 7373B7 1384580NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28332AW 23384 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON L-2 UPPER INNER CHORD BETWEEN BS 962 AND BS 983 AT LBL 51, WL 209. MAINTENANCE REMOVED CORRODED L-2 UPPER INNER CHORD FROM BS 962 TO BS 983 AT LBL 51; FABRICATED A NEW REPLACEMENT INNER CHORD PER DWG 65-52878; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050525001762005052500176NM 2005 5 25 AWXA200500544 120050429A531565498843 FLOORBEAM BOEING737 7373B7 1384580NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28332AW 23384 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF TRANSVERSE BEAM AT BS 967, LBL 43, WL 208. MAINTENANCE CUT OUT CORRODED SECTION OF TRANSVERSE BEAM AT BS 967, LBL 43; FABRICATED A NEW REPLACEMENT SECTION OF BEAM AND 2 EACH SUPPORT ANGLES & REPAIR STRAPS; INSTALLED REPAIR PARTS IAW ER 03-5310-05125-ES1. 2L72 4F RTA16WE 20050525001832005052500183EU 2005 5 25 SA05050 120050509A3233114122010 ACTUATOR AIRBUSA319 A319112 3930323EU RT MLG FAILED A USAAO OTHER J WARNING INDICATION CLCLIMB 1 EA19707UW17702 949 LGA - FLT 496 EN-ROUTE PIT TO LGA - AFTER GEAR RETRACTION, CREW RECEIVED AN UNSAFE GEAR INDICATION ON ECAM. THE CREW FOLLOWED ECAM INSTRUCTIONS AND RECYCLED THE LANDING GEAR. AT THAT TIME, THE GEAR RETRACTED NORMALLY. THE FLIGHT CONTINUED TO LGA. MAINTENANCE REPLACED THE RIGHT MAIN GEAR DOOR ACTUATOR. OPERATIONALLY CHECKED GEAR WITH A GEAR SWING AND LEAK CHECKED. ALL FOUND OK. 2L72 4F RTA28NM 20050525001852005052500185EU 2005 5 25 UPS05144434 120050508A3350 LIGHT AIRBUS300 A300B4622R 3930312EU EMERGENCY EXIT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01152UP 0835 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT INOP AT EXIT SIGN. RELAMPED EMERGENCY EXIT LIGHT, OPS CHECK OK. 2L72 4F RTA35EU 20050525001862005052500186 2005 5 25 UPS05144435 420050510A2565D31023101 SLIDE AIRBUS300 A300B4622R 3930312EU CABIN MALFUNCTIONED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01128UP 0812 SLIDE HARD TO ARM HAD TO RECYCLE ARMING HANDLE SEVERAL TIMES IN ORDER TO GET A SLIDE ON ECAM. CYCLED EMERGENCY ESCAPE SLIDE RELEASE HANDLE SEVERAL TIMES WITH SLIDE APPEARING ON ECAM HANDLE WAS SMOOTH IN OPERATION IN REF TO MM 52-73-00-0. 2L72 4F RTA35EU 20050525001882005052500188EA 2005 5 25 MASA200500314 120050425A5610 DOOR CNDAIRCL600 CL6002B19 1900309EA PAX LACK OF LUBE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0775987 7405 ASH 7103 IAD TO BNA. THE CREW NOTED THAT THE PASSENGER DOOR WILL NOT OPEN FROM THE OUTSIDE. MAINTENANCE CLEANED AND LUBED THE MAIN PASSENGER DOOR AND OPS CHECKED NORMAL. NO FURTHER DEFECTS NOTED. 2L72 4F RTA21EA 20050525001902005052500190EA 2005 5 25 MASA200500317 120050425A2701 BEARING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CONTROL COLUMN DAMAGED A MASAO OTHER O OTHER APAPPROACH 1 SW0777260 7260 ASH 6146 LAS. ON ARRIVAL TO LAS THE CAPTAIN WROTE UP THE AILERON CONTROL BINDING LEFT TO RIGHT DURING FLIGHT. MAINTENANCE INSPECTED AND PREPARED AIRCRAFT FOR FERRY FLIGHT TO OKC. MAINTENANCE REMOVED AND REPLACED THE PILOT CONTROL WHEEL SHAFT BEARINGS. 2L72 4F4 FRTA21EA E15NE 20050525001912005052500191EA 2005 5 25 MASA200500318 120050426A274070609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW077291Z4125 305 7291 ASH 6383 BIL TO PHX. THE CREW WROTE UP THAT THE STAB TRIM CH NR 1 DISENGAGED AND WOULD NOT RESET IN FLIGHT. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT. 2L72 4F RTA21EA 20050525002062005052500206NM 2005 5 25 XNOA1225 120050511A7400 ENGINE BOEING727 727227 1384078NM NR 2 INOPERATIVE A XN0AO OTHER O OTHER NRNOT REPORTED 1 GL2376752 21248 NR 2 ENGINE WILL NOT START, NO IGNITION. NR 2 ENGINE IGNITION CB'S RESET, OP'S CHECK GOOD. 2L73 4F A3WE 20050525002072005052500207NM 2005 5 25 DL76L050213 120050411A2613 OVERHEAT LOOP BOEING767 767332 1382001NM RIGHT WING FAILED A DALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27198DN 28455 CLIMBING THRU 10,000 FT, 10 MIN AFTER T/O RT DUCT LEAK EICAS AND RT DUCT LEAK ON OVERHEAD. REPLACED RIGHT DUCT OVERHEAT LOOP. 2L72 4F RTA1NM 20050525002122005052500212NM 2005 5 25 DL757050222 120050416A3310233N320215 ANNUNCIATOR BOEING757 757232 1384965NM COCKPIT SHORTED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27632DL 23613 ENTRY DOOR LIGHT ON OVERHEAD INDICATOR PANEL SHORTING OUT AND TRIPPING R IND LIGHT C/B. REMOVED AND REPLACED OVERHEAD IND LIGHT PANEL PER MM, CHECKS OK. 2L72 4F RTA2NM 20050525002142005052500214NE 2005 5 25 DL764050225 220050418A7230 COMPRESSOR BOEING767 767424ER 1385270NM GE CF6 CF680C2B2 30025NE NR 1 ENGINE STALLED A DALAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SO27833MH1069610696 29706 706385 NR 1 ENGINE COMPRESSOR STALL. LOUD BANG HEARD. ABORTED T/O AT 5 KTS. MTC IN WORK REPLACING ENGINE. METAL IN TAILPIPE. 2L72 4F4 FRTA1NM E13NE 20050525002162005052500216 2005 5 25 DL76G050228 420050420A3410066500011001 INDICATOR BOEING767 767332 1382001NM COCKPIT FAILED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO271612T 30575 AFTER TAKEOFF CAPTS VSI WAS INTERMITTENT AND ON THEN OFF. APPROX 15 MIN AFTER T/O CREW SMELLED ELECTRIC SMELL AND PULLED THE P-6-E5 CB FOR CAPT VSI SMELL THEN DISSIPATED. REPLACED CAPT VSI, CHECKS OK. 2L72 4F RTA1NM 20050525002172005052500217NM 2005 5 25 DL777050229 120050421A2560P4010021SM BATTERY BOEING777 777232 1385232NM FLASHLIGHT DISCHARGED A DALAO OTHER O OTHER CRCRUISE 1 SO27860DA 29951 JUMP SEAT 4L FWD FLASHING LIGHT RED LIGHT NOT FLASHING. REPLACED BATTERY. 2L72 4F RTT00001SE 20050525002192005052500219NM 2005 5 25 DLM88050231 120050422A2400 RELAY DOUG MD88 MD88 3023688NM FAILED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27939DL 49812 SMOKE IN COCKPIT. REPLACED DC X-TIE RELAY FOR BURNING. 2L72 4F RTA6WE 20050525002202005052500220NM 2005 5 25 DL76L050232 120050422A77306672M852 SIGNAL COND UNIT BOEING767 767332 1382001NM ENG VIBRATION FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27188DN AD68 27583 NO ENGINE VIBRATION INDICATIONS. REMOVED AND REPLACED DIGITAL VIB SIGNAL CONDITIONING UNIT. OPS CHECKS GOOD. 2L72 4F RTA1NM 20050525002212005052500221NM 2005 5 25 DL73S050233 120050422A3244 TIRE BOEING737 737247 138448DNM LT MLG DAMAGED A DALAO OTHER O OTHER LDLANDING 1 SO27373DL 23520 NR 2 MAIN TIRE LOST CAP ON OUTBOUND HOU /AFTER LOSS OF A-SYSTEM HYDRAULICS, CREW MANUALLY EXTENDED GEAR, LANDED IN ATL WITHOUT INCIDENT. TIRE REMAINED INFLATED /DAMAGE TO LEADING EDGE OF MID FLAP AND HYDRAULIC LEAK PRESENT DUE TO DAMAGED LINES IN WHEEL WELL. REPLACED WHEEL. REPAIRED DAMAGE. 2L72 4F A16WE 20050525002222005052500222NM 2005 5 25 DL764050234 120050423A5230 CONDUIT BOEING767 767432ER 1385134NM CARGO DOOR DAMAGED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27841MH 29714 AFTER T/O OVERHEAD DOOR LIGHT AND EICAS MESSAGE FWD CARGO DOOR. REPLACED CONDUIT ON DOOR FOR DAMAGED WIRING. 2L72 4F RTA1NM 20050524001922005052400192NM 2005 5 24 SWAA051335 120050505A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 920, STR 21L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050524001982005052400198NM 2005 5 24 SWAA051341 120050505A53126516300 BULKHEAD BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29690SW 23783 DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD WEB CRACKED AT RBL 8 TO RBL 9, WL 234. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050524002002005052400200SO 2005 5 24 LR7A05043 120050428A5311LS401010 FRAME LKHEED382 382G 526414USO FUSELAGE DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK PER JOB CARD HC5315 CARGO COMPT RING SEGMENT FOUND NUMEROUS EXCESS HOLES AT CABIN FS 752E; RT WL 140-200 AND WL 200-265. RING SEGMENT REPLACED IAW SMP583 CHP 51-60 & 51-70 FS 752E WL 140-200 & 200-265 RHS. 2H74 4T A1SO 20050524002022005052400202SO 2005 5 24 LR7A05045 120050428A5350 SKIN LKHEED382 382G 526414USO RT MLG FAIRING DELAMINATED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK PER JOB CARD HC3212 RIGHT MWW SKIN (HONEYCOMB PANEL) FOUND DELAMINATED FROM FS 610-617 WL 189-200. RIGHT PANEL REPLACED IAW LAC MEA 382-53-05-024 R1 & DWG I05-005-02 FS 595-617 WL 180-200. 2H74 4T A1SO 20050524002122005052400212SO 2005 5 24 LR7A05055 120050428A5330 SKIN LKHEED382 382G 526414USO FUSELAGE WARPED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK PER JOB CARD HC5321 CTR FUSELAGE EXTERIOR SKIN WARPED AT FS 667-677 WL 156-210 LEFT. SKIN REPAIR CARRIED OUT IAW LAC MEA 382-53-05-049, DWG R05-009-07, FS 667-677 WL 156-210 LEFT. 2H74 4T A1SO 20050524002252005052400225SO 2005 5 24 LR7A05068 120050428A5311 FRAME LKHEED382 382G 526414USO FUSELAGE DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK INTERIOR FUSELAGE FRAMES FOUND EXCESS & ELONGATED HOLES AT RT FS 255E WL 162 BL 68. FRAME REPAIRED IAW R05-009-04, LAC MEA 382-53-05-046, RT FS 255E WL 162 BL 68. 2H74 4T A1SO 20050524002332005052400233SO 2005 5 24 LR7A05076 120050428A5311 FRAME LKHEED382 382G 526414USO FUSELAGE DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK INTERIOR FUSELAGE FRAMES FOUND EXCESS & ELONGATED HOLES AT RT FS 317 WL 162 BL 68. FRAME REPAIRED IAW R05-009-04, LAC MEA 382-53-05-046, RIGHT FS 317 WL 162 BL 68. 2H74 4T A1SO 20050524002352005052400235SO 2005 5 24 LR7A05078 120050428A5311 FRAME LKHEED382 382G 526414USO FUSELAGE DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK INTERIOR FUSELAGE FRAMES FOUND EXCESS & ELONGATED HOLES AT LT & RT FS 377 WL 162 BL 68. FRAME REPAIRED IAW R05-009-05, LAC MEA 382-53-05-047, RIGHT FS 687 WL 162 BL 68. 2H74 4T A1SO 20050524002382005052400238SO 2005 5 24 LR7A05081 120050428A5311 FRAME LKHEED382 382G 526414USO FUSELAGE DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK INTERIOR FUSELAGE FRAMES FOUND EXCESS & ELONGATED HOLES AT LT FS 364 WL 162 BL 68. FRAME REPAIRED IAW R05-009-06, LAC MEA 382-53-05-048, LT FS 364 WL 162 BL 68. 2H74 4T A1SO 20050524002392005052400239SO 2005 5 24 LR7A05082 120050428A5311 FRAME LKHEED382 382G 526414USO FUSELAGE DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2730 4698 DURING SCHEDULED C-6 CHECK INTERIOR FUSELAGE FRAMES FOUND EXCESS & ELONGATED HOLES AT LT FS 371 WL 162 BL 68. FRAME REPAIRED IAW R05-009-06, LAC MEA 382-53-05-048, LEFT FS 371 WL 162 BL 68. 2H74 4T A1SO 20050524002482005052400248WP 2005 5 24 05FDEA01224 120050506A3230 CYLINDER DOUG MD10 MD1010F 3022112WP LANDING GEAR LEAKING A FDEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO25550FE 46521 LANDING GEAR WOULD NOT RETRACT ON T/O COMPLIED WITH QRH PROCEDURES COULD NOT RETRACT RETURNED TO EWR. PLACED FUSE BYPASS LEVER IN BYPASS POSITION, FOUND TRIM CYLINDER RELIEF VALVE LEAKING. REPLACED TRIM CYLINDER RELIEF VALVE IAW M/M 32-37-03-2, LEAK CHECK GOOD. 2L73 4F RTA22WE 20050524002492005052400249NM 2005 5 24 05FDEA01225 120050506A2510 PANEL BOEING727 727200 138407ENM COCKPIT CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25254FE 20936 BELOW CAPTAINS PEDALS RACEWAY (PANEL) HAVE CRACKS. REMOVED AND REPLACED RACEWAYS (PANELS) IAW SRM 51-30-2. 2L73 4F RTA3WE 20050524002602005052400260NM 2005 5 24 UIEA200500054 120050421A5414 NOSE COWL BOEING747 74747UF 1384949NM ENGINE DENTED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15412MC 30559 ENGINE 1 NOSE COWL AT 4 O`CLOCK POSITION DENT AT LIP 5.6 INCHES X 4.2 INCHES X 0.224 INCH. DENTED AREA TRIMMED OUT AND SRM WAS PERFORMED. INSTALLED DOUBLER AND FILLER IAW SRM USING BLIND .1562 FASTENERS. (K) 2L74 4F RT1384945 20050524002622005052400262 2005 5 24 UIEA200500056 420050425A3430 CONTROL SYSTEM BOEING747 7472D7B 1384803NM GE CF6 CF650E2 30018NE ILS INTERMITTENT A UIEAA UNSCHED LANDING G MULTIPLE FAILURE DEDESCENT 1 EA15523MC 21782 AFTER ROLLING OUT 360 DEGREES, VOR COURSE INBOUND, ALL NAV INDICATIONS, OK. AFTER DESCENDING TO FL 10.0 JUST PRIOR TO CROSSING THE VOR SELECTED ILS FREQ ON CAPT AND FO MCP, BOTH HIS SELECTOR SWITCHES WERE SET TO ILS AND NAV MODE ON ILS. CPT HAD COURSE AND G/S INDICATIONS W/NO FLAGS IN VIEW. FO INDICATING TO G/S INDICATIONS WITH LOC TO THE RIGHT. AFTER EXTENDING GEAR CAPTS SIDE BECAME INTERMITTENT AND FLAGS IN VIEW SIMULTANEOUSLY HEARD PULL UP TERRAIN WARNING. FIREWALL THRUST FLAPS 20 EXECUTED. DIVERTED. ILS RECEIVERS 1 AND 2 SELF TEST PERFORMED, SYSTEM CHECKED NORMAL ON THE GROUND. (K) 2L74 4F4 FRTA20WE E23EA 20050524002632005052400263WP 2005 5 24 05FDEA01227 120050507A3620 SWITCH DOUG DC10 DC1030 3023501WP NR 3 MANIFOLD DEFECTIVE A FDEAHA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO25315FE 48313 NR 3 MANIFOLD FAIL ILLUMINATED IN FLT. C/W QRH PROCEDURES, LIGHT EXTINGUISHED. PERFORMED DECAY CHECK OF NR 3 PNEU SYS IAW JRH AND PASSED ITERROGATED FAULT INDICATOR IN CAC AND FOUND RIGHT WING PRESS SWITCH FAULTED WITH APU AIR CHECKED ALL ANTI-ICE TUBING AND LINES ON RT WING FOR LEAKS. CHECKED ALL SLATS FOR EXCESSIVE AIR, ALL NORMAL. REMOVED ALL PERI SEAL CONNECTORS FROM ALL HEATED SLATS AND VISUALLY INSP INSIDE OF PICCOLO TUBES FOR OBVIOUS DAMAGE, ALL NORMAL. FOUND NR 3 MANIFOLD FAIL FAULT BALL REMOVED AND REPLACED NR 3 MANIFOLD FAIL DETECT SWITCH FOUND WORN PERI SEALS ON I/B AND O/B OF NR 6 SLAT. REMOVED AND REPLACED SEALS, OPS CHECKED MAINIFOLD FAIL SYSTEM, OPS CHECK OK. LEAK CHECK OK. 2L73 4F A22WE 20050524002652005052400265NE 2005 5 24 UIEA200500058 220050426A7320441789 HMU BOEING747 74747UF 1384949NM GE CF6 CF680C2B2 30025NE NR 3 ENGINE UNSERVICEABLE A UIEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA15409MC 30558 AFTER ROTATION UP TO 1000 FT, NR3 ENGINE N1 WOULD SURGE (ROLL BACK) BETWEEN 101.5 AND 98.0 N1. AT THRUST REDUCTION ALTITUDE, THE SURGE WOULD STOP. ALL PHASES OF FLIGHT WERE NORMAL. AFTER LANDING, DID A POWER RUN UP AND THE SAME AS ABOVE OCCURRED, NO EICAS OR STATUS MESSAGE DISPLAYED. SERVICEABLE HMU FITTED ENGINE GROUND RUN CARRIED OUT. HMU REPLACED IAW AMM. IAW TAKEOFF POWER, OPS NORMAL. (K) 2L74 4F4 FRT1384945 E13NE 20050524002672005052400267NM 2005 5 24 UIEA200500060 120050422A7931 CONNECTOR BOEING747 74747UF 1384949NM GE CF6 CF680C2B2 30025NE OIL PRESS XMITTRCONTAMINATED A UIEAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 EA15496MC 29254 ON TAXI OUT NR2 ENGINE OIL PRESSURE DROPPED BELOW RED LINE-ENGINE SHUTDOWN. T/S IAW MM. CLEANED OIL PRESSURE TRANSMITTER CONNECTOR. ENGINE GROUND RUN PERFORMED ALL WORKING NORMAL. (K) 2L74 4F4 FRT1384945 E13NE 20050524002722005052400272NM 2005 5 24 UIEA200500064 120050426A5412 PYLON BOEING747 747228F 1384895NM GE CF6 CF650E2 30018NE NR 4 CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15536MC 21576 NR 4 PYLON OB SKIN FOUND (2) CRACKS ON ACCESS DOOR 482AR CUTOUT CRACK 1INCH TO 1.5 INCH ON BOTH SKIN AND DOUBLER. (K) 2L74 4F4 F A20WE E23EA 20050524002742005052400274NM 2005 5 24 UIEA200500066 120050426A3600 PRECOOLER BOEING747 747228F 1384895NM GE CF6 CF650E2 30018NE ENGINE CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15536MC 21576 PYLONS NR1, 2, 3, AND 4, PRECOOLER EXHAUST CUT OUT LOWER EDGE CRACKED. REPAIRS ACCOMPLISHED IAW MM. (K) 2L74 4F4 F A20WE E23EA 20050524002792005052400279NM 2005 5 24 AWXA200500542 120050504A534069414372 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28322AW 25400 MCN - MAJOR REPAIR - DURING C-14 CHECK A .375 INCH CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 663.75, STR 10 RT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 663.75, STR 10 RT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-41437; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050524002822005052400282EA 2005 5 24 VTZA200500078 120050508A5315601R3110111 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27625BR 7214 FLOORBEAM AT FS 310 LBL 27 HAS LEVEL 2 CORROSION. 2L72 4F RTA21EA 20050524003082005052400308NM 2005 5 24 2005UALA00332 120050412A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29585UA 26709 EXTERNAL FUSELAGE AT BS 274 BETWEEN STR 21L AND 22L HAS IMPROPER FASTENER INSTALLED, COUNTERSUNK CHERRY MAX RIVET. MAJOR REPAIR ACCOMPLISHED. REMOVED BLIND RIVET AND CUT OUT SKIN DAMAGE AND INSTALLED DOUBLER AND FILLER. 2L72 4F4 FRTA2NM E17NE 20050524003132005052400313SW 2005 5 24 ALGA100723 120050428A6220406310405101 PITCH LINK BELL 407 407 1182206SW ALLSN 250C 250C47B GL M/R HEAD BINDING E ALGAK NONE O OTHER ININSP/MAINT 1 SW03547AL286 53240 BINDING, ROUGH, AXIAL PLAY BEYOND MAX. REPLACED WITH NEW BY FIELD MAINTENANCE. 1G71 3U3 UO H2SW E1GL 20050524003152005052400315NM 2005 5 24 2005UALA00400 120050502A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29586UA 26710 FLOORBEAM AT STA 324, RBL CORRODED. FLOORBEAM TEE WAS TRIMMED TO REMOVE CORROSION AND REPAIR ANGLES AND STRAPS WERE SPLICED TO REPAIR THE FLOORBEAM UPPER CAP. 2L72 4F4 FRTA2NM E17NE 20050524003222005052400322NM 2005 5 24 2005UALA00409 120050505A2121 FAN AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE COCKPIT FAILED A UALAA UNSCHED LANDING BE SMOKE/FUMES/ODORS/SPARKS VIBRATION/BUFFET CRCRUISE 1 WP29839UA 1507 FUMES IN COCKPIT WITH VIBRATIONS. REPLACED THE AVIONICS BLOWER FAN. TESTED OK. 2L72 4F4 FRTA28NM E40NE 20050525000022005052500002NM 2005 5 25 USAA050469 120050409A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19574US49993 23739 CLT - FOUND FUSELAGE SKIN CRACKED 1.75 INCH, STATION 727D, STRINGER 24L, BELOW ICE LIGHT. INSTALLED DOUBLER AND TRIPLER IAW SRM 53-00-01, FIG 229. (M) 2L72 4F RTA16WE 20050525000032005052500003NM 2005 5 25 USAA050470 120050408A5320 INTERCOSTAL BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19440US39307 24811 CLT - FOUND INTERCOSTAL CRACKED TWO PLACES 1.5 INCH EACH AT S4L, BS 303. REPLACED INTERCOSTAL IAW SRM 51-70-11. (M) 2L72 4F RTA16WE 20050525000292005052500029 2005 5 25 ASMF200505007 420050505A3421 CONNECTOR DOUG DC9 DC983 3022083WP INDICATOR FAILED W ASMFO OTHER HJ ELECT. POWER LOSS-50 PC WARNING INDICATION NRNOT REPORTED 1 SW23583MD 49659 AIRCRAFT ARRIVED WITH CAPTAIN REPORT OF VOR NR 2 WITH OSCILLATIONS OF 30 RADIALS AND RIGHT EHSI WITH OFF FLAG IN LEFT RMI. AIRCRAFT WAS SENT TO THE HANGAR AND RMI INDICATOR WIRING WAS CHECKED DETECTING THE LEFT RMI CONNECTOR FAILED, LINES 36, 37 AND 45. CONNECTOR P10-354 OF THE LEFT COMPASS WAS REPLACED IAW WDM 34-22-02, TESTED CORRECT. ADDITIONALLY, BOTH RX VOR ILS WERE TESTED IAW MM 34-21-00, ALL CORRECT. 2L72 4F RTA6WE 20050525000342005052500034CE 2005 5 25 DJFA2005090 120050505A7830650162 SWITCH BEECH MU300 400A 1155402CE THRUST REVERSER FALSE INDICATIONE DJFAO OTHER J WARNING INDICATION CLCLIMB 1 EA23427CW RK27 DURING CLIMB FROM 28,000 FT TO 33,000 FT, RIGHT THRUST REVERSER DEPLOY LIGHT ILLUMINATED. THE ARM AND UNLOCK LIGHTS REMAINED EXTINGUISHED. CREW PUSHED BOTH THRUST REVERSER EMERGENCY STOW BUTTONS. THE DEPLOY LIGHT EXTINGUISHED AT 9,000 FT AND 190 KTS. AN UNEVENTFUL LANDING WAS MADE IN KORF. AIRCRAFT WAS ISSUED MEL 78-1 FOR THE THRUST REVERSER SYSTEM. ON 06 MAY 2005, MAINTENANCE REPLACED THE RIGHT DEPLOY SWITCH. THE OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4F RTA16SW 20050525000472005052500047NM 2005 5 25 RYNA200500016 120050509A3150 WARNING SYSTEM BOEING757 757200 1384950NM ACTIVATED A RYNAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 CE07151GX 24451 DURING TAKEOFF ROLL, AURAL WARNING BELL SOUNDED. NO LIGHTS OR EICAS INDICATIONS. ABORTED TAKEOFF AND RETURNED TO GATE. RESET AND OPERATIONALLY CHECKED SYSTEM. NO DEFECTS NOTED. 2L72 4F RTA2NM 20050525000492005052500049EA 2005 5 25 REXA2005056 120050428A3260 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NLG OUT OF ADJUST A REXAO OTHER N FALSE WARNING APAPPROACH 1 SO258698A 7698 GEAR DISAGREE LIGHT ON SHORT FINAL. UNEVENTFUL LANDING. ADJUSTED NLG OLEO PROX SENSOR IAW AMM. PERFORMED GEAR SWING, OPS CHECKED GOOD IAW AMM. OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050525000532005052500053NM 2005 5 25 USAA050467 120050407A5320 SPLICE BOEING737 7374B7 1384702NM STRINGER CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19440US39307 24811 CLT - FOUND STRINGER SPLICE CRACKED .5 INCH, BS 908 S-4R. REPLACED STRINGER SPLICE IAW SRM 51-10-02. (M) 2L72 4F RTA16WE 20050525000572005052500057EU 2005 5 25 USAA050499 120050414A53151110108 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19714US17533 1046 PIT - FOUND FLOORBEAM ASSEMBLY .25 INCH BY .5 INCH CORROSION, FRAME 69L Y1440. DEFECTIVE PART REPLACED WITH IDENT PART. (M) 2L72 4F RTA28NM 20050525000582005052500058EU 2005 5 25 USAA050498 120050414A5347 SEAT TRACK AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19714US17533 1046 PIT - FOUND SEAT TRACK CORRODED 1 FT BY 1.5 INCH FRAME 20. DEFECTIVE PART REPLACED WITH IDENT PART. (M) 2L72 4F RTA28NM 20050525000612005052500061EA 2005 5 25 A6WA200540159 120050404A5340601R3111357 CLIP CNDAIRCL600 CL6002B19 1900309EA FLOORBEAM CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31416AW 7603 FLOORBEAM CLIP AT FS 280, LBL 9, INBOARD IS CRACKED IN RADIUS APPROX 33 INCHES. REMOVED AND REPLACED ANGLE P/N 601R31113-57 IAW SRJ SRM 51-42-06, 51-42-21 AND BRAS EO 601R-53-6212. (M) 2L72 4F RTA21EA 20050525000742005052500074CE 2005 5 25 DXTA200500713 120050508A3260 INDICATOR CESSNA650 650 2076802CE MLG INOPERATIVE E DXTAA UNSCHED LANDING P NO WARNING INDICATION APAPPROACH 1 GL07713QS 6507103 LT GEAR ANNUNCIATOR FAILED TO LIGHT DURING GEAR EXTENSION (OR ROTORY TEST) BLEW GEAR DOWN USING CHECK LIST PROCEDURE. DURING ROLL OUT (L) SIDE GEAR BEGAN SMOKING. FOUND LT LANDING GEAR INDICATOR PULLED LOOSE IN ITS SOCKET. RESET INDICATOR AND PERFORMED LANDING GEAR FUNCTIONAL TEST IAW CE-650 M/M 32-00-01. OPS CHECK GOOD. VISUALLY INSPECTED LT GEAR, WHEEL AND BRAKE FOR DAMAGE. NONE NOTED. 2L72 4F A9NM 20050525000932005052500093EA 2005 5 25 SWIA200514969 120050505A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07430SW1653 1653 7523 FFOD THE LEFT SPOILERON WOULD DEPLOY TO THE FULL UP POSITION. REPLACED LEFT SPOILERON INBOARD (PCU) ACTUATOR IAW MM 27-62-01 AND RIGHT SPOILER ELECTRONIC CONTROL UNIT IAW 27-61-05. OPERATIONAL CHECK GOOD, P/N: 49-164-05 S/N OFF: 0283. 2L72 4F RTA21EA 20050525001012005052500101NM 2005 5 25 DHL2005788001 120050507A3260 PROXIMITY SWITCH BOEING727 727214 138407RNM NLG OUT OF ADJUST A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01788AT 21958 INTERMITENT RED DOOR LIGHT WITH 2ND OFFICER AMBER GEAR DOOR LIGHT. ADJUSTED NLG FWD W/W DOOR POSITION SWITCH IAW B727 MM 32-62-0, OPS CHECK GOOD IAW B727 MM 32-61-0. 2L73 4F A3WE 20050525001022005052500102EU 2005 5 25 DHL2005362006 120050510A3260BED00101 PROXIMITY SENSOR AIRBUS300 A300B4203 3930306EU NLG MALFUNCTIONED A DHLAO OTHER P NO WARNING INDICATION APAPPROACH 1 SO01362DH 84 THE RED UNSAFE NOSE GEAR LIGHT ON FWD PANEL DID NOT ILLUMINATE AFTER GEAR HANDLE PUT DOWN. BULB TESTED NORMAL. REPLACED PROX DETECTOR MODULE UNIT IAW M/M 32-61-12. OPS CHECKS GOOD. 2L72 4F RTA35EU 20050525001232005052500123SO 2005 5 25 C2XA05CL031 120050505A33501317 LAMP EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715948 145056 CLE - DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHT LOCATED ON THE PAX DOOR DID NOT ILLUMINATE DURING THE TEST. MAINTENANCE REPLACED THE LIGHT BULB AND THE OPERATIONAL TEST WAS GOOD. 2L72 4F RTT00011AT 20050525001272005052500127SO 2005 5 25 C2XA05BT027 120050509A2120 ODOR EMB 145 EMB145ER 3260211SO CABIN DETECTED A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW2715932 145015 CREW REPORTED, BURNING ODOR COMING FROM RELAY BOX UNDER GEAR PINS. MAINTENANCE PERFORMED VISUAL INSPECTION OF LEFT HAND POWER DISTRIBUTION PANEL, NO ARCING OR BURNED AREAS NOTED. FOUND FORWARD COOLING AIR DUCT DISCONNECTED, RECONNECTED DUCT AND APPLIED POWER TO THE AIRCRAFT FOR FOUR HOURS, NO ODOR NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20050525001322005052500132WP 2005 5 25 U2RA3140 120050510A53404641324U501 FITTING DOUG DC8 DC863F 302198FWP FUSELAGE CRACKED A U2RAK NONE O OTHER ININSP/MAINT 1 GL23921R 684252039 46145 LONGERON 24 LT AFT BATHTUB FITTING CRACKED AT FS 1690. 2L74 4F 4A25 20050525001352005052500135WP 2005 5 25 U2RA2962 120050510A5330 FINGER DOUBLER DOUG DC8 DC863F 302198FWP FUSELAGE CORRODED A U2RAK NONE O OTHER ININSP/MAINT 1 GL23921R 684252039 46145 RIVET HEAD POPPED FS 200, RT SIDE OF THE AIRCRAFT BELOW THE AUX STATIC PORT IDENTIFIED AS LEVEL 2 CORROSION. 2L74 4F 4A25 20050525001442005052500144EU 2005 5 25 2005F00077 120050409A3234F96GA0102 SELECTOR AEROSPATR72 ATR72212 8680945EU MLG STUCK A TRBAA UNSCHED LANDING O OTHER CLCLIMB 1 SO29417AT 417 WHILE IN CLIMB, LANDING GEAR HANDLE STUCK. UNABLE TO SELECT UP POSITION. AIRCRAFT RETURNED. REPLACED LANDING GEAR SELECTOR HANDLE. (M) 2H72 4T RTA53EU 20050525001602005052500160EU 2005 5 25 2005F00079 120050407A3297D23198000 WIRE HARNESS AEROSPATR72 ATR72212 8680945EU RT MLG BROKEN A TRBAA UNSCHED LANDING O OTHER CLCLIMB 1 SO29451AT 451 WHILE IN CLIMB, LANDING GEAR DID NOT RETRACT WHEN SELECTED TO THE UP POSITION. AIRCRAFT RETURNED. REPLACED RT MLG INTERNAL UPPER HARNESS. (M) 2H72 4T RTA53EU 20050525001632005052500163NM 2005 5 25 USAA050513 120050418A5311 FRAME BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US 24781 CLT - FOUND FRAME CRACKED .25 INCH, STATION 787 AND S9R. FABRICATED AND INSTALLED REPAIR ANGLES IAW TR53-10-20B. (M) 2L72 4F RTA16WE 20050525001642005052500164NM 2005 5 25 USAA050511 120050421A5315 FLOORBEAM BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US39931 24781 CLT - FOUND FLOORBEAM CORRODED .250 INCH BY .250 INCH, BL 0 STATION 344. REMOVED CORROSION AND REPAIRED IAW SRM 53-10-51. REPAIR COMPONENTS FABRICATED. (M) 2L72 4F RTA16WE 20050525001652005052500165NM 2005 5 25 USAA050512 120050420A532065617777 SPLICE BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US39931 24781 CLT - FOUND STRINGER SPLICE CRACKED 3 INCHES, S15L SPLICE CRACKED STATION 360 AT TIE CLIP. REMOVED AND REPLACED CRACKED PART WITH NEW SPLICE IAW SRM 51-10-02 AND 51-40-02. (M) 2L72 4F RTA16WE 20050525001872005052500187EA 2005 5 25 MASA200500297 120050411A2701 YOKE CNDAIRCL600 CL6002B19 1900309EA COCKPIT BINDING A MASAO OTHER O OTHER NRNOT REPORTED 1 SW077291Z 7291 ASH 6338 SLC TO PHX. RETURN TO GATE DUE TO YOKE JAMMING/BINDING WHEN TURNED TO THE LEFT. INSPECTED PER SERVICE LETTER 22-045. COULD NOT DUPLICATE. OPS CHECKED NORMAL. 2L72 4F RTA21EA 20050525001962005052500196SO 2005 5 25 FMAA200501 220050107A8500 ENGINE CESSNA185 185D 2072812CE CONT O520 IO520D 17032SO FAILED E FMAAK NONE O OTHER ININSP/MAINT 1 AL011541F 1850896 566996 ENGINE FAILED TO PRODUCE OIL PRESSURE CAUSING INTERNAL BEARING DAMAGE. EXTENT OF DAMAGE AND CAUSE IS PENDING ENGINE TEARDOWN. (K) 1H71 3O3 O 3A24 E5CE 20050525002092005052500209NM 2005 5 25 DL76G050218 120050413A3350 LAMP BOEING767 767332 1382001NM EMERGENCY LIGHT BURNED OUT A DALAK NONE L NO TEST ININSP/MAINT 1 SO271611B 30595 FOUND SEAT 1B E-PATH LIGHT INOP. REPLACED BULB AND LENS OVER AT SEAT 1B E-PATH LIGHT. 2L72 4F RTA1NM 20050525002152005052500215 2005 5 25 DL73S050226 420050420A34100665000110 INDICATOR BOEING737 737232 1384475NM COCKPIT FAILED A DALAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27319DL 23091 DURING PUSHBACK A ELECTRICAL SPARKING ARCING LIKE SOUND A VERY SLIGHT SMELL OF ELECTRICAL FUMES WHICH STOPPED VERY QUICKLY F/O`S VSI WENT INOP. REPLACED VSI. 2L72 4F RTA16WE 20050525002232005052500223 2005 5 25 XN0A1237 420050515A2210 CONNECTOR AIRBUS300 A300B4203 3930306EU YAW DAMPER DIRTY A XN0AD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL23371PC 157 BOTH YAW DAMPERS WOULDN'T DESIGAGE DURING TAXI. CLEANED AND RESEATED YAW RATE CAIRO CONNECTIONS SYSTEM, OPS CHECK GOOD AT THIS TIME IAW A300 MM 22-21-00. (STATUS:ORIG/CLOSED) 2L72 4F RTA35EU 20050525002242005052500224SO 2005 5 25 C2XA05SH032 120050512A532014530644403 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714938 145029 SHV - DURING C-CHECK THE LT OMEGA BEAM HAS CORROSION FROM FRM 39 TO FRM 45. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED REPAIR LT OMEGA BEAM AT FRM 44 IAW SRM 53-21-10, SECTION 2, FIGURE 201 SHEET 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050525002252005052500225NM 2005 5 25 05FDEA01284 120050514A5320AGA717014 STIFFENER DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25621FE 48792 CENTER CARGO, STA 1841 FLOOR AREA BULKHEAD APPROX X= -25 VERTICAL STIFFENER FOUND CRACKED. REMOVED AS PER SRM 51-33-01 VOLUME II. NEW STIFFENER FABRICATED AS PER DRAWING AGA7170 AND INSTALLED AS PER SRM 51-33-01 VOLUME II. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100. 2L73 4F RTA22WE 20050525002262005052500226NM 2005 5 25 05FDEA01294 120050515A5313AFA70751 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25580FE 48471 CENTER CARGO COMPARTMENT FOUND BILGE LEVEL L-49R, STA 1541 WITH STRINGER CORRODED. CARRIED OUT REPAIRED AS PER SRM 53-10-00 FIGURE 2 VOLUME 1. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050525002272005052500227NM 2005 5 25 05FDEA01297 120050516A5347ACA74141 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25580FE 48471 MAIN DECK STATION 839 AND STATION 859 X=-8 SEAT TRACK FOUND CORRODED. TRIMMED OUT AND REPAIRED AS PER SRM 53-70-00 2L73 4F RTA22WE 20050525002282005052500228NM 2005 5 25 05FDEA01299 120050516A5311ACA71281 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25580FE 48471 MAIN DECK LEFT HAND STATION 535 "Z"= 50 FRAME FOUND DENTED AS MARKED. REPAIR CARRIED OUT AS PER DRAWING SRZ-53-503. 2L73 4F RTA22WE 20050525002302005052500230NM 2005 5 25 05FDEA01365 120050518A5311 FRAME BOEING727 727227 1384078NM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 FWD CARGO BAY FRAME IS CREASED AT BS 560 STR 24L TO 25L. REPAIRED FRAME PER SRM 51-40-3. 2L73 4F A3WE 20050525002332005052500233CE 2005 5 25 DXTA200500738 120050522A5610991438012 WINDSHIELD CESSNA560 560XL 2076702CE COCKPIT FAILED E DXTAB EMER. DESCENT O OTHER CRCRUISE 1 GL07618QS608 5605506 RIGHT FRONT WINDSHIELD SHATTERED DURING FLIGHT. REMOVED RT RAIN SHROUD, REMOVED RT HEATED WINDSHIELD, INSTALLED NEW SEAL ON NEW WINDSHILED IAW MM 56-11-00. PERFORMED STEP C1-C8 RETORQUED BOLTS IAW 560XL MM 56-11-00. PERFORMED FUNCTIONAL CABIN PRESSURIZATION LEAK CHECK IAW 560XL M.M. 21-30-00 STEP C1-C16, & C26-C29. LEAK CHECKED GOOD. REMOVED JUMPER & RECONNECTED OUTFLOW VALVE, REMOVED PLUG FROM CABIN ALT. DIFF. PRESS. GUAGE, REMOVED SERVICE AIR CONNECTOR & RE-CAPPED LINE. OK TO CLOSE OUTFLOW VALVE ACCESS. OK TO INSTALL RAIN SHROUD 2L72 4F RTA22CE 20050525002362005052500236 2005 5 25 SA05054 420050519A2565C203740002 SERVO VALVE AIRBUS320 A320214 3930316EU MLG WW FAILED A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19105UW15722 868 DURING TAKE-OFF ROLL, THE BRAKES BEGAN TO SURGE, CAUSING THE AIRCRAFT TO VEER ON THE RUNWAY. AT THE SAME TIME, A BRAKE SYSTEM 1 FAULT ECAM MESSAGE GENERATED. THE TAKE-OFF WAS REJECTED AT 40 KNOTS. THE FLIGHT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NORMAL BRAKE SERVO VALVE, FIN 18GG. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20050525002382005052500238NM 2005 5 25 05FDEA01376 120050519A5230 SKIN BOEING727 727200 138407ENM CARGO DOOR DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25264FE 21626 AFT LOWER CARGO NR 3 HAS DENT 18 INCHES FROM LOWER CORNER 2 INCHES FROM LOWER EDGE. REPLACED SKIN PER SRM 51-30-2 2L73 4F RTA3WE 20050525002392005052500239NM 2005 5 25 05FDEA01377 120050519A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 FWD CARGO BAY FRAME IS CREASED BS 660, STR 24L. REPAIRED FRAME AT BS 660, STR 24L PER SRM 51-40-3 2L73 4F RTA3WE 20050525002412005052500241NM 2005 5 25 05FDEA01379 120050520A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25264FE 21626 EXTERNAL REPAIR BS 1100, STR 26R (8 INCH BY 9 INCH) REQUIRES EVALUATION TO DETERMINE PER SRM OR APPROVED DATA. REMOVED OLD REPAIR AND INSTALLED NEW REPAIR PER FED-EX EA 7-5330-86292. 2L73 4F RTA3WE 20050525002422005052500242NM 2005 5 25 DLM88050235 120050425A2560P2070003001 FLASHLIGHT DOUG MD88 MD88 3023688NM 1L DOOR UNSERVICEABLE A DALAK NONE O OTHER ININSP/MAINT 1 SO27931DL 49718 FLASHLIGHT AT 1L DOOR INOP NOT FLASHING. REPLACED SAME. 2L72 4F RTA6WE 20050525002432005052500243NM 2005 5 25 DL73G050236 120050418A53306546882 SKIN BOEING737 73735B 13844BMNM GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27225DL 25069 AT MID VISIT FOUND FUSELAGE SKIN GOUGED AT STA 1129-1138 WL 265. REPAIRED PER ERA 098117-14. TIME LIMITED REPAIR. ADDITIONAL ER/A IS REQUIRED FOR CONTINUED SERVICE LONGER THAN 12 MONTHS FROM REPAIR ACCOMPLISHMENT ACTL LINE 2050. 2L72 4F RTA16WE 20050526000022005052600002NM 2005 5 26 DL76G050239 120050427A2710 ACTUATOR BOEING767 767332 1382001NM LT AILERON LEAKING A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO271613B 32776 C-HYDRAULIC QUANTITY DECREASED IN FLIGHT. REPLACED O-RING ON NR 4 SPOILER ACTUATOR. 2L72 4F RTA1NM 20050526000032005052600003NE 2005 5 26 DL76G050240 220050427A7230 COMPRESSOR BOEING767 7673P6 1385105NM GE CF6 CF680C2B6 30025NE NR 2 ENGINE STALLED A DALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 SO271501P386482999 24983 695446 AFTER LEVEL OFF AND UPON ADVANCING THRUST LEVERS TO INCREASE SPEED RT ENGINE BEGAN TO HAVE COMPRESSOR STALLS. REPLACED ENGINE FOR INTERNAL DAMAGE. 2L72 4F4 FRTA1NM E13NE 20050526000042005052600004NM 2005 5 26 DL76G050241 120050427A2530 OVEN BOEING767 7673P6 1385105NM MID GALLEY BURNED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27152DL 24984 ON ARRIVAL F/A`S NOTICED A BURNED PLASTIC SMELL COMING FROM MID GALLEY NEAR ROW 5. REMOVED BURNT PLASTIC FROM TRAYS IN NUMBER 2 OVEN MID GALLEY. OVEN CHECKS GOOD. NO PLASTIC SMELL WHILE USING OVEN OR AFTER TURNING OVEN OFF. MCO AND PLACARD REMOVED. 2L72 4F RTA1NM 20050526000062005052600006NM 2005 5 26 DL757050243 120050428A7930 WARNING LIGHT BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 2 ENGINE ILLUMINATED A DALAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 SO27622DL40218 22912 716587 DURING CRUISE RECEIVED RT ENGINE OIL FILTER MESSAGE. REPLACED INTERNAL SCAVENGE PUMP AND ANGLE DRIVE GEARBOX. 2L72 4F4 FRTA2NM E17NE 20050526000072005052600007NM 2005 5 26 DL76G050244 120050428A2420 IDG BOEING767 767332 1382001NM GE CF6 CF680 30025NE APU UNRELIABLE A DALAH DEACTIVATE SYST/CIRCUITS H ELECT. POWER LOSS-50 PC CRCRUISE 1 SO27160658373 30199 P2636 LEFT ENGINE DRIVE LIGHT ON AT CRUISE. FOUND OVERSERVICED, SERVICED SAME, CHECKS GOOD. 2L72 4F4 FRTA1NM E13NE 20050526000122005052600012NM 2005 5 26 DLM90050250 120050502A324050121934 BRAKE DOUG MD90 MD9030 3023690NM LEFT MLG UNSERVICEABLE A DALAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO27914DN 53394 DURING TAXIOUT FOR TAKEOFF, LEFT BRAKE GRABBED DURING TURN, CAUSING FLIGHT ATTENDANT TO STUMBLE. STOPPED A/C TO CHECK ON F/A CONDITION. UPON CONTINUING TAXI WITH TIGHT LEFT TURN ONTO PARALLEL TAXIWAY, NOSE GEAR SLID AT EDGE OF CONCRETE ONTO ASPHALT APRON. A/C STOPPED AND REQUESTED TOW IN. INSPECTED BRAKES, LT SIDE DRAGS, REPLACED BOTH NR 1 & 2 BRAKES PER AMM. INSPECTED NOSE GEAR VISUALLY AND OPERATION CHECKS GOOD. 2L72 4F RTA6WE 20050526000132005052600013NM 2005 5 26 DL76G050251 120050503A2821 FILTER BOEING767 767332 1382001NM GE CF6 CF680C2B6F 30025NE NR 2 ENGINE CONTAMINATED A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO271611B23352 30595 706137 RIGHT ENGINE FUEL FILTER LIGHT ILLUMINATED. REPLACED SAME. 2L72 4F4 FRTA1NM E13NE 20050526000162005052600016NE 2005 5 26 DL75K050254 220050503A7200 ENGINE BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 2 MAKING METAL A DALAC ABORTED TAKEOFF XJ ENGINE FLAMEOUT WARNING INDICATION TOTAKEOFF 1 SO276716C41532 30838 716582 DURING T/O ROLL AS POWER WAS APPLIED RIGHT ENGINE COMPRESSOR STALLED AND SHUTDOWN. REPLACED ENGINE. 2L72 4F4 FRTA2NM E17NE 20050526000172005052600017NM 2005 5 26 DLM88050255 120050504A3320D77311001 BALLAST DOUG MD88 MD88 3023688NM CABIN LIGHTS OVERHEATED A DALAH DEACTIVATE SYST/CIRCUITS M OVER TEMP TXTAXI/GRND HDL 1 SO27910DL 49541 SMOKE IN CABIN JUST PRIOR TO PUSHBACK. FOUND LIGHT BALLAST (B652) AT SEAT ROW 29ABC OVERHEATING. REPLACED BALLAST ASSY LIGHTS AND BALLAST, OPS CHECKS NORM. 2L72 4F RTA6WE 20050526000182005052600018NM 2005 5 26 DLM88050257 120050504A49901945189004 CAP DOUG MD88 MD88 3023688NM APU OIL SYSTEM LEAKING A DALAD RETURN TO BLOCK KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27970DL 43173 HAZE IN CABIN FROM AC PACKS. FOUND OIL IN APU INLET. CLEANED SAME. PERFORMED DUCT BURNOUT. 2L72 4F RTA6WE 20050526000192005052600019NM 2005 5 26 DLM88050258 120050504A4900 ODOR DOUG MD88 MD88 3023688NM A/C PACK DETECTED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27932DL 49719 BURNING SMELL IN CABIN. PERFORMED DUCT BURNOUT. NO SMELLS NOTED. 2L72 4F RTA6WE 20050526000202005052600020 2005 5 26 DL764050259 420050504A2330 ODOR BOEING767 767432ER 1385134NM CABIN DETECTED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27835MH 29708 CREW VERBAL HOT ELECTRONICS SMELL AROUND 23 CDE. OPENED COVERS ON UNDER SEAT ELECTRONIC UNITS AT 21-22-23 CDE. REMOVED DUST AND DERBRIS. CHECKED AUDIO, CHECKS OK. CHECKED FOR ODOR IN E & E COMP, FOUND NONE. 2L72 4F RTA1NM 20050526000212005052600021NM 2005 5 26 DLM88050260 120050506A2612 AMPLIFIER DOUG MD88 MD88 3023688NM FIRE DETECTION MALFUNCTIONED A DALAO OTHER N FALSE WARNING APAPPROACH 1 SO27975DL 53243 6579 ENGINE FIRE DETECTION SYSTEM RIGHT ENGINE LOOP-B LIGHT AND FIRE WARNING ON IN FLIGHT MOMENTARILY, THEN WENT OFF. BOTH INDICATIONS AGAIN ON THE GROUND BOTH WITH ENGINE RUNNING AND AFTER ENGINE SHUT DOWN. TESTED FIRE WARNING. FOUND NR 2 ENGINE B-LOOP STICKING IN TEST WITH FIRE INDICATION. REPLACED A2-6 RIGHT FIRE DETECT AMP (CONTROL). TESTED FIRE WARNING SEVERAL TIMES. OPS TEST NORMAL ON B-LOOP NR 2 ENGINE. A-LOOP NR 2 ENGINE STILL ON MCO AND PLACARD. 2L72 4F RTA6WE 20050526000232005052600023NM 2005 5 26 DL76G050262 120050506A3350 FUSE BOEING767 7673P6 1385105NM POWER SUPPLY FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27155DL 25269 ON EMERGENCY LIGHT TEST, FWD CABIN EMERGENCY LIGHTS INOP ON BUSINESS ELITE SEATS. REPLACED FUSE IN POWER SUPPLY. 2L72 4F RTA1NM 20050526000242005052600024NM 2005 5 26 DL76L050263 120050507A2510251005676 SEAT BOEING767 767332 1382001NM COCKPIT SPARKS A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27183DN 27110 F/O SEAT ADJUST INOP ELEC BURNING SMELL NOTED. REPLACED SEAT ASSY. 2L72 4F RTA1NM 20050526000262005052600026NM 2005 5 26 DLM88050265 120050510A3350 CONNECTOR DOUG MD88 MD88 3023688NM EMERGENC LIGHTS LOOSE A DALAO OTHER O OTHER CRCRUISE 1 SO27970DL 43173 SEAT MOUNTED EMERGENCY LIGHTS INOP AT SEAT 24DE. SECURED LOOSE CONNECTOR, OPERATION NORMAL. 2L72 4F RTA6WE 20050526000272005052600027NM 2005 5 26 DL76L050266 120050510A2597 WIRE BOEING767 767332 1382001NM CABIN DAMAGED A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO27197DN 28454 AFT CARGO PDU INOP. FOUND C/B OUT. RESET SAME AND SPARKS STARTED FLYING IN P-39 PANEL. NUMEROUS WIRES (30-40) BURNED INSIDE PANEL. REPAIRED WIRING. 2L72 4F RTA1NM 20050526000292005052600029SO 2005 5 26 SIMA200511202 120050414A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21850AE4737 145722 THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. PERFORMED A CUTOUT TO REMOVE THE CORROSION ON THE LEFT OMEGA BEAM. FABRICATED AN EXTERNAL ANGLE, FILLER, PLATE AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB145/1142 REV 28, CHAPTERS 53-21-10 FIGURE 201. (M) 2L72 4F RTT00011AT 20050526000302005052600030NM 2005 5 26 HALA0500175 120050206A29108365D8620 FUSE BOEING717 717200 1383700NM HYD SYSTEM FAILED A HALAD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 WP13485HA 55130 FLT 113 - HNL - AT PUSHBACK, WHEN STARTING LEFT ENGINE, GOT LEFT HYD PRESSURE AND QUANTITY TO '0' LINE SERVICE CONFIRMED LEFT HYD FLUID ON RAMP. FOUND LT LOWER FORWARD QTY LIMITER FUSE HOUSING CRACK. REMOVED AND REPLACED QTY LIMITER FUSE PER MM 32-44-10-4. OPS AND LEAK CHECK OK. BEFORE REMOVING FUSE FORWARD LT SYSTEM QTY AT 2.0 PERFORMED FIM TASK 29-30-00-810-802 AND 29-30-00-801. OK FOR SERVICE. (M) 2L72 4F TRA6WE 20050526000312005052600031NM 2005 5 26 USAA050525 120050405A53226558280 SHEAR TIE BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19374US56183 22953 FOUND FRAME BOTTOM SHEAR TIE CORRODED, 2 INCHES LONG BY .80 INCH WIDE BY .032 INCH DEEP, BS 360 WL 148.5 RBL 4. REPLACED SHEAR TIE PER SRM 51-40-02. (M) 2L72 4F RTA16WE 20050526000322005052600032EA 2005 5 26 A6WA200540145 120050409A5730 SKIN PANEL CNDAIRCL600 CL6002B19 1900309EA LT WING CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31417AW 7610 LEFT LOWER WING PLANK IS CORRODED UNDER PANEL 550HB AT FORWARD CENTER EDGE .600 INCH LONG BY .100 INCH WIDE BY .002 INCH DEEP, INBOARD EDGE 4 INCHES LONG BY .050 INCH WIDE BY .003 INCH DEEP, OUTBOARD SIDE 4.5 INCH LONG BY .025 INCH WIDE BY .003 INCH DEEP. S/D - REPAIRED LT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT FOR PANEL S SCH B IAW BOMBARDIER, INC REO 601R-57-21-030. (M) 2L72 4F RTA21EA 20050526000332005052600033EA 2005 5 26 A6WA200540146 120050409A5730 SKIN PANEL CNDAIRCL600 CL6002B19 1900309EA LT WING CORRODED A A6WAO OTHER O OTHER NRNOT REPORTED 1 GL31417AW 7600 LT LOWER WING PLANK IS CORRODED UNDER PANEL 550FB, INBOARD SIDE 3 INCH LONG BY .100 WIDE BY .002 INCH DEEP, FORWARD SIDE .200 INCH LONG BY .100 INCH WIDE BY .002 INCH DEEP. S/D - REPAIRED LEFT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT FOR PANEL 550 FB IAW BOMBARDIER, INC REO 601R-57-21-030 REV D.(M) 2L72 4F RTA21EA 20050526000342005052600034NM 2005 5 26 USAA050518 120050421A5320 STRAP BOEING737 737401 1384701NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19422US45217 23989 CLT - FOUND STRAP CRACKED 3.750 INCH, STATION 312 RBL 20. REPAIRED IAW SRM 51-70-11. (M) 2L72 4F RTA16WE 20050526000352005052600035SO 2005 5 26 SIMA200510806 120050414A335066367 LIGHT EMB 145 EMB145LR 3260212SO CABIN WRONG PART A SIMAD RETURN TO BLOCK W INADEQUATE Q C TXTAXI/GRND HDL 1 SW21659AE 145762 FLT 3640 - GSP - CREW NOTED ON PREFLIGHT THAT THE EMERGENCY LIGHTS AT THE OVERWING EXITS ARE GREEN AND NOT AMBER. REPLACED EMERGENCY FLOOR LIGHT STRIP AT OVERWING EXIT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20050526000462005052600046NM 2005 5 26 USAA050515 120050422A5320 ATTACH ANGLE BOEING737 7374B7 1384702NM CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US39931 24781 CLT - FOUND ATTACH ANGLE CRACKED .750 INCH, FRAME 360 S14L. REPLACED WITH FABRICATED ANGLE IAW SRM 51-10-02, 51-40-00. (M) 2L72 4F RTA16WE 20050526000482005052600048NM 2005 5 26 USAA050533 120050330A5320USTR5310064LF FLOOR SUPPORT BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19374US56183 22953 BFM - FOUND FLOOR SUPPORT CORRODED 1 INCH WIDE BY 2 INCHES LONG BY .053 INCH DEEP, AFT CARGO FLOOR SUPPORT BS 825 LBL 8.10 INCH AND RBL 3. INSTALLED REPAIR ANGLE PER TYP REPAIR 53-10-06B, 53-60-53, 51-10-02. (M) 2L72 4F RTA16WE 20050526000492005052600049NM 2005 5 26 USAA050535 120050328A5320USTR531006LF FLOOR SUPPORT BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19374US56183 22953 BFM - FOUND FLOOR SUPPORT ANGLE CORRODED 1.6 INCH BY .90 INCH BY .043 INCH, AFT CARGO COMPARTMENT 3 INCHES AFT OF BS 727B. CORROSION LEVEL 1, TASK C53-202-01. INSTALLED REPAIR IAW TR 53-10-06B, SRM 53-60-53. (M) 2L72 4F RTA16WE 20050526000502005052600050NM 2005 5 26 USAA050537 120050407A5315 FLOORBEAM BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19374US 22953 BFM - FOUND SUPPORT, T-ANGLE, WEB CORRODED AND CRACKED 4 INCHES LONG, 1 INCH WIDE AND 1 INCH, BS 994 WL 208 AFT CABIN FLOOR. BLENDED SUPPORT, REMOVED AND REPLACED T-ANGLE AND WEB WITH NEW FABRICATED PARTS PER SRM 51-40-02, 53-60-51. (M) 2L72 4F RTA16WE 20050526000522005052600052NM 2005 5 26 USAA050529 120050330A5315115TR5310061F FLOORBEAM BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19374US56183 22953 BFM - FOUND FLOOR SUPPORT CORRODED 4 INCHES LONG BY 2.5 INCHES WIDE BY .05 INCHES DEEP, AFT CARGO COMPARTMENT FLOOR SUPPORT BS 727D PLUS LBL 12.5- RBL 8.10 INCH. CORROSION LEVEL 1, TASK C53-202-01. INSTALLED REPAIR ANGLE IAW TYPICAL REPAIR 53-10-06B AND 53-60-53. (M) 2L72 4F RTA16WE 20050526000552005052600055NM 2005 5 26 USAA050538 120050407A5744 SUPPORT ANGLE BOEING737 7373B7 1384580NM LT WING CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19374US56183 22953 BFM - FOUND SUPPORT ANGLE CRACKED 4 INCHES, LT WING TE NR 3 (INBOARD TO OUTBOARD) HINGE WS 573.872 WBL, 415.93. REMOVED, FABRICATED NEW, INSTALLED NEW SUPPORT ANGLE PER SRM 57-51-02, 51-40-05, 51-40-02. (M) 2L72 4F RTA16WE 20050526000592005052600059EU 2005 5 26 USAA050519 120050416A53471161201 SEAT TRACK AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19714US 1046 PIT - FOUND SEAT TRACK CORRODED .25 INCH DIAMETER SPOT, RT OUTBOARD SEAT TRACK, FRAME 66. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-72-11. CORROSION LEVEL 1, TASK NR JA-260-53500. (M) 2L72 4F RTA28NM 20050526000602005052600060WP 2005 5 26 AMTA200500415 120050502A339758791 LEAD LKHEED1011 10113853 5265020WP EMERGENCY LIGHT DAMAGED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11161AT 1219 EGRESS LIGHT OUT ON RIGHT SIDE FORWARD HALF OF 'B' SECTION. REMOVED AND REPLACED POWER STRIP IAW AMM 33-50-01. AIRCRAFT EMERGENCY LIGHTS OPERATE NORMALLY. AIRCRAFT OK FOR SERVICE. (M) 2L73 4F A23WE 20050526000632005052600063EU 2005 5 26 USAA050522 120050405A5315D6347209200000 FLOORBEAM AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19106US 1044 PIT - FOUND FLOORBEAM CORRODED 2 INCH BY 2 INCH AREA, LEFT INBOARD AFT FLOORBEAM Y765 FRAME C64-C70. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 53-41-14. CORROSION LEVEL 1, TASK JA-260-53500. (M) 2L72 4F RTA28NM 20050526000662005052600066NM 2005 5 26 AMTA200500407 120050502A33501317 BULB BOEING757 75733N 1384931NM EMERGENCY LIGHT FAILED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11551TZ 32585 EGRESS AISLE LIGHT AT ROW 17ABC IS INOPERATIVE. REPLACED LAMP AS REQUIRED. OPS CHECK NORMAL. (M) 2L72 4F RTA2NM 20050526000672005052600067NM 2005 5 26 USAA050534 120050401A5315 FLOORBEAM BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19374US56183 22953 BFM - FOUND FLOOR SUPPORT CORRODED 2.5 INCHES LONG BY 1 INCH WIDE BY .045 INCH DEEP, AFT CARGO FLOOR SUPPORT BS 773 LBL 12.5 - RBL 8.10. FABRICATED DOUBLERS AND INSTALLED PER TYPICAL REPAIR 53-10-06B. (M) 2L72 4F RTA16WE 20050526000702005052600070CE 2005 5 26 DJFA2005092 120050511A2820 TRANSFER TUBE BEECH MU300 400A 1155402CE FUEL SYS MALFUNCTIONED E DJFAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA23799TA RK209 CREW FOUND FUEL CROSSFEED NOT MAINTAINING A BALANCED CONDITION AS RT WING TANK CONTINUED TO DEPLETE. CROSSFEED SWITCHES CYCLED & CIRCUIT BREAKERS CHKD. REPORTED FUSELAGE FUEL NOT TRANSFERRING TO WING TANKS. ACFT PREVIOUSLY ISSUED MEL 28-2-2 FOR DISCREPANCY OF RT FUEL XFER PRESS LOW LIGHT. DECLARED AN EMERGENCY & DIVERTED. MADE AN UNEVENTFUL LANDING WITH 600 LBS OF FUEL IN RT WING TANK. MX OPERATED FUEL CROSSFEED SYS IN BOTH POSITIONS OF LT & RT TANK. CROSSFEED SYS OPS NORMAL. OPS CHECK OF LT FUSELAGE FUEL TRANSFER PROVED SATISFACTORY. NOTED BY MX THAT RT FUSELAGE FUEL TRANSFER SYS CURRENTLY UNDER MEL & LT TANK TO BE SELECTED ON FUEL CROSSFEED TO MAINTAIN FUEL BALLANCE. ACFT RETURNED TO SERVICE. 2H72 4F RTA16SW 20050526000732005052600073NM 2005 5 26 AWXA200500545 120050428A533065458001129 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28332AW 23384 MCN - MAJOR REPAIR - DURING C-18 CHECK 2 EACH .75 INCH CRACKS WERE FOUND IN EXTERNAL FUSELAGE SKIN AT LOWER AFT CORNER OF R-1 DOOR CUTOUT BS 329, STR 17 RT. MAINTENANCE CUT OUT CRACKED SKIN AT LOWER AFT CORNER OF R-1 DOOR CUTOUT BS 329, STR 17 RT; FABRICATED A INNER PLATE, MIDDLE PLATE, OUTER PLATE, AND 2 EACH FILLERS & TAPERED FILLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-01 FIG 202. 2L72 4F RTA16WE 20050526000742005052600074NM 2005 5 26 AWXA200500547 120050506A5322654583312 SHEAR TIE BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28322AW 25400 MCN - MAJOR REPAIR - DURING C-14 CHECK A .75 INCH CRACK WAS FOUND IN SHEAR TIE ON FORWARD SIDE OF FRAME AT BS 196.5, LBL 29, WL 207. MAINTENANCE REMOVED CRACKED SHEAR TIE AT BS 196.5, LBL 29; FABRICATED A NEW REPLACEMENT SHEAR TIE PER DWG 65-45833; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050526000752005052600075NM 2005 5 26 AWXA200500548 120050503A532065673129 REVEAL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28322AW 25400 MCN - MAJOR REPAIR - DURING C-14 CHECK A .375 INCH CRACK WAS FOUND IN REVEAL AT INTERNAL LOWER FORWARD CORNER OF R-2 DOOR CUTOUT BS 959, STR 17 RT. MAINTENANCE REMOVED CRACKED REVEAL AT LOWER FORWARD CORNER OF R-2 DOOR CUTOUT BS 959, STR 17 RT; FABRICATED A NEW REPLACEMENT REVEAL PER DWG 65-67312; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050526000772005052600077NM 2005 5 26 AWXA200500546 120050504A534069414372 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28322AW 25400 MCN - MAJOR REPAIR - DURING C-14 CHECK A .375 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT BS 663.75, STR 10 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 663.75, STR 10 LT; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER DWG 69-41437; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050526000782005052600078WP 2005 5 26 0500709989 120050507A217017946081 WATER SEPARATOR DOUG DC9 DC931 3022065WP CABIN AIR DAMAGED A NWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL018945E 47181 DURING CLIMBOUT AT ABOUT 600 FEET THE FLIGHT ATTENDANT NOTIFIED THE COCKPIT THAT THE CABIN HAD SMOKE COMING OUT OF ALL VENTS AND ITS ACCOMPANIED BY AN ACRID SMELL. THE FLIGHT RETURNED TO AN UNEVENTFULL LANDING BACK AT MSP. NO MENTION OF COM PROCEDURE COMPLIANCE. MAINTENANCE COULD NOT FIND A SOURCE FOR THE SMOKE, NO EVIDENCE OF ANY FIRE WAS FOUND. ALL ENGINE AND COMPONENT OIL LEVELS WERE NORMAL. THE WATER SEPARATOR BAGS WERE REPLACED, SYSTEM WAS PURGED AND THE AIRCRAFT HAS RETURNED TO SERVICE. 2L72 4F A6WE 20050526000812005052600081CE 2005 5 26 20030842 120050510A261224409015 FIRE LOOP BEECH 1900 1900D 1154162CE FALSE INDICATIONA GLBAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 NM03219GL UE219 DURING THE TAKEOFF ROLL, THE RT RED T-HANDLE ANNUNCIATOR AND YELLOW FIRE LOOP ANNUNCIATOR ILLUMINATED. MAINTENANCE REPLACED THE DEFECTIVE REAR (AFT) FIRE LOOP. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA24CE 20050526000822005052600082CE 2005 5 26 K5L2005F00001 120050103A2750AGX10 FUSE BEECH 200 A200 1152921CE PWA PT6 PT6* 52043EA TE FLAPS FAILED E K5LAO OTHER J WARNING INDICATION APAPPROACH 1 EA05636B 400 BC61 SELECTED APPROACH FLAPS DESCENDING, FLAPS FAILED TO EXTEND. RESET CIRCUIT BREAKER AND CYCLED FLAP SELECTOR BUT STILL NO FLAP MOVEMENT. MADE UNEVENTFUL NO FLAP LANDING. AFTER LANDING, FLAPS WORKED FINE A COUPLE OF TIMES, UP AND DOWN. TROUBLESHOT AND FOUND LT SPLIT FLAP FUSE WAS FAILED. REPLACED FUSE AND FUSE HOLDER AND FLAPS WORKED NORMAL ON GROUND AND AFTER MAINTENANCE FLIGHT. HAVE HAD PREVIOUS PROBLEM WITH FUSES. GOING TO ADD THIS AS A CHANGE TO INSTALL A NEW FUSE, LT AND RT FLAPS EACH PHASE INSPECTION. (K) 1L72 4T3 T A24CE E2NE 20050526000912005052600091EA 2005 5 26 COMA0560296 120050504A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION DEDESCENT 1 SO01969CA 7141 FLIGHT 5727 FLAPS FAIL CAUTION. RESET FLAP SYSTEM, FOUND NO DEFECTS, DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20050526000922005052600092EA 2005 5 26 COMA0560297 120050508A2750860D10018ABCD CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ACTIVE A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01809CA146966302 7366 FLIGHT 5366 FLAPS FAIL CAUTION. REPLACED THE FECU. 2L72 4F RTA21EA 20050526000932005052600093EA 2005 5 26 COMA0560298 120050507A2750860D10018ABCD CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ACTIVE A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01969CA2729 7141 FLIGHT 5142 FLAPS FAIL CAUTION. REPLACED THE FECU. 2L72 4F RTA21EA 20050526000942005052600094EA 2005 5 26 COMA0560299 120050505A3010 ANTI-ICE SYSTEM CNDAIRCL600 CL6002B19 1900309EA WINGS MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01479CA 7675 FLIGHT 5345 ANTI ICE DUCT WARNING. INSPECTION OF WING ANTI ICE SYSTEM, FOUND NO DEFECTS. 2L72 4F RTA21EA 20050526001002005052600100NE 2005 5 26 RNV2005F00001 220050120A72613008786 SHAFT CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE MCAULY3AF34C3GFR34C703 GL SCAVANGE PUMP SHEARED E RNVAO OTHER FHJFLT CONT AFFECTED ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 WP13305PW1040 208B0828 WHILE ENROUTE, THE PILOT EXPERIENCED A FAILURE OF THE STANDARD ELECTRICAL POWER SYSTEM FOLLOWED BY FLUCTUATING AND DECREASING OIL PRESSURE. THE PILOT LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL FOUND THAT THE AFT END OF THE ACCESSORY DRIVE OF THE ACCESSORY DRIVE FOR THE EXTERNAL SCAVANGE PUMP HAD SHEARED OFF. THIS FAILURE ALLOWED ENGINE OIL IN THE SCAVANGE PUMP HOUSING TO EXIT BY THE PLAIN SEAL AND VENT OVERBOARD THROUGH THE ALTERNATOR DRIVE PULLEY ASSY DRAIN TUBE. THE LOSS OF OIL PRESSURE. POSSIBLE CAUSE OF FAILURE OF THE SCAVANGE PUMP DRIVE SHAFT IS A TWIST LOAD INDUCED BY EITHER THE ALTERNATOR DRIVE PULLEY BEARINGS OR THE ALTERNATOR BEARINGS. (K) 1H71 3T3 T A37CE E4EA 5 CP60GL 20050526001012005052600101NM 2005 5 26 SWAA051364 120050510A324626066712 WHEEL BOEING737 7373H4 1384600NM RT MLG DEPARTED A SWAAO OTHER O OTHER LDLANDING 1 SW29309SW 22948 NR 3 MLG TIRE/WHEEL ASSY DEPARTED THE AIRCRAFT ON LANDING ROLL. INSPECTED RT MLG FOR WHEEL BEARING FAILURE. NO DAMAGE NOTED. REMOVED AND REPLACED NR 3 MLG TIRE/WHEEL ASSY, BRAKE ASSY & TRANSDUCER PER MM. 2L72 4F RTA16WE 20050526001022005052600102 2005 5 26 SWAA051365 420050510A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29339SW 24090 DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050526001052005052600105NM 2005 5 26 SWAA051368 120050510A534065C27314 STRINGER CLIP BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29669SW 23752 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 616, STR 4L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050526001062005052600106NM 2005 5 26 SWAA051369 120050510A53306545777 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29669SW 23752 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR CUTOUT, FWD LOWER CORNER AT FASTENER HOLE. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050526001072005052600107 2005 5 26 SWAA051370 420050510A2565D31354 SLIDE BOEING737 7373Q8 1384670NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29685SW 23401 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDES OUT OF ADJUST. ADJUSTED SLIDES PER MM. 2L72 4F RTA16WE 20050526001082005052600108NM 2005 5 26 SWAA051371 120050510A53306545776 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29685SW 23401 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 904, STR 25R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050526001122005052600112NM 2005 5 26 SWAA051358 120050509A5210MS166241037 LOCK RING BOEING737 7373H4 1384600NM L1 DOOR MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29339SW 24090 L1 DOOR WOULD NOT OPEN. INSTALLED UPPER GUIDE ARM LOCK RING PER MM. 2L72 4F RTA16WE 20050526001152005052600115NM 2005 5 26 SWAA051362 120050509A52406545871 DOOR FRAME BOEING737 7373A4 1384585NM R1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29669SW 23752 DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR AFT FRAME CRACKED AT NR 4 STOP FITTING. REMOVED AND REPLACED DOOR PER MM. 2L72 4F RTA16WE 20050526001162005052600116NM 2005 5 26 SWAA051363 120050509A53116545808 FRAME BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29669SW 23752 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 291.5, STR 16R. REPAIRED FRAME PER SWA EA. 2L72 4F RTA16WE 20050526001222005052600122EA 2005 5 26 COMA0560302 120050509A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01982CA 7168 FLIGHT 5144 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20050526001232005052600123EA 2005 5 26 COMA0560303 120050509A3230864808 PSEU CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01986CA142386353 7174 FLIGHT 5371 - GEAR DISAGREE WARNING, NLG FAILED TO RETRACT. REPLACED THE PSEU. 2L72 4F RTA21EA 20050526001242005052600124EA 2005 5 26 COMA0570049 120050509A531267053110521 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01376CA5331 10092 FS 280 LT BULKHEAD LOWER WEB IS CORRODED IN VARIOUS PLACES ALONG THE BOTTOM EDGE FROM LBL36 TO LBL9. REPLACED THE FS 280 LT BULKHEAD LOWER WEB IAW BOMBARDIER INC REO 670-53-11-052, REV A REPAIR NR 2 AND CRJ 700 SRM 51-42-13-001-001-A01 AND CRJ 700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20050524003332005052400333NE 2005 5 24 SWAA051348 220050508A7310MS29513258 PACKING BOEING737 7373H4 1384600NM GE CFM56 CFM563B1 13802NE LT PYLON WORN A SWAAK NONE K FLUID LOSS UKUNKNOWN 1 SW29384SW 26590 PAX REPORTED VAPOR SPEWING FROM LT WING, UPON ARRIVAL, FOUND SIGNIFICANT FUEL LEAK FROM NR 1 ENGINE PYLON AFT VENT. REMOVED AND REPLACED PACKINGS & SECURED FLEX FUEL FEED LINE PER MM. 2L72 4F4 FRTA16WE E2GL 20050525000062005052500006NM 2005 5 25 USAA050468 120050406A5315 FLOORBEAM BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19440US39307 24811 CLT - FOUND FLOORBEAM CORRODED 1 INCH BY 7 INCHES, FS 271 LBL 8 TO RBL 8. SPLICED A NEW Z ANGLE. (M) 2L72 4F RTA16WE 20050525000132005052500013EU 2005 5 25 DHL2005367516 120050317A5347F0511310 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAO OTHER O OTHER ININSP/MAINT 1 SO01367DH 265 DURING "C" CHECK IN MIAMI, FL AT AVBORNE HEAVY MAINTENANCE DISCREPANCY AS FOLLOWS, N/R FIRST OBSERVER SEAT TRACK HAS WEAR MARKS. REMOVED AND REPLACED SEAT TRACK "FWD" OF 1ST OBSERVER AT COCKPIT IAW A-300 MM 53-41-11. 2L72 4F RTA35EU 20050525000192005052500019EA 2005 5 25 COMA0560287 120050503A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01708CA 7235 LEFT 621.00 FLOOR SUPPORT ANGLE CRACKED. REPAIRED IAW REO 601R-53-61-117. 2L72 4F RTA21EA 20050525000282005052500028WP 2005 5 25 4511104292005 220050429A7200 MONOPOLE LEAR 45 45LEAR 5170805CE ALIDSGTPE331TPE331201A 0517 WP NR 2 ENGINE MALFUNCTIONED E J7SAEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 SW05414FX 111 P116214 DURING CRUISE, NR 2 ENGINE ROLLED BACK TO FLIGHT IDLE. MAINTENANCE REPLACED THE N-2 MONOPOLE. NO DEFECTS NOTED ON SUBSEQUENT POWER RUNS. 2L72 4F3 TRTT00008WIAEXJ STC 20050525000372005052500037NM 2005 5 25 SB05057 120050506A2797BACC63BP16C24S7 CONNECTOR BOEING737 7373B7 1384580NM LT WING INTERMITTENT A USAAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 EA19519AU 23705 MHT - FL 725 - ON APPROACH, THE FLAPS LOCKED OUT WHEN SELECTED TO 25. THE CREW NOTED A 3 DEGREE SPLIT BETWEEN THE LEFT AND RIGHT FLAPS. CREW PERFORMED A GO-AROUND DURING WHICH THE FLAPS BEGAN OPERATING NORMALLY. FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND A BENT PIN IN THE LEFT FLAP POSITION TRANSMITTER WHICH WAS MAKING INTERMITTENT CONTACT. MAINTENANCE STRAIGHTENED THE PIN. SUBSEQUENTLY, THE CONNECTOR (D275) AND TRANSMITTER WERE REPLACED. 2L72 4F RTA16WE 20050525000592005052500059EU 2005 5 25 USAA050497 120050413A5315D5397209000200 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19714US17533 1046 PIT - FOUND FLOORBEAM CORRODED 1 INCH IN DIAMETER, LT INBOARD SEAT TRACK BEAM AT FRAME 66. DEFECTIVE PART REPLACED WITH IDENT PART. CORROSION LEVEL 1, TASK JA 260-53500. (M) 2L72 4F RTA28NM 20050525000602005052500060NM 2005 5 25 USAA050473 120050410A5320 WEB BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19440US39307 24811 CLT - FOUND WEB CRACKED 3.25 INCH, LEFT SIDE OF KEEL BEAM AT STATION 620. INSTALLED DOUBLER IWA EA 96411. (M) 2L72 4F RTA16WE 20050525000642005052500064NM 2005 5 25 AMTA200500386 120050415A5300 SKIN BOEING757 75723N 1384973NM FUSELAGE DAMAGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11519AT 27975 FOUND SKIN SCRATCHED, SCRIBE MARKS, FS 440-660, S4L-S4R. COMPLIED WITH ERA 757-53R-5866. (M) 2L72 4F RTA2NM 20050525000862005052500086NE 2005 5 25 AALA20050309 220050507A7200 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE LEFT INOPERATIVE A AALAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CRCRUISE 1 SW217547A 53029 717310 ABOUT 20 MINUTES INTO FLIGHT LEFT OIL PRESSURE LOW LIGHT ON. PRESSURE AND OIL QUANTITY DROPPED TO ZERO. SHUTDOWN LEFT ENGINE PER QRH. OIL TEMPERATURE 80, QUANTITY ZERO NUMBER TWO. 55 PERCENT ENGINE SHUTDOWN. AFTER OIL QUANTITY ZERO THREE MINUTES ENGINE WINDMILLED 23 MINUTES. REPLACED LEFT HAND ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F4 F A6WE E9NE 20050525000872005052500087SO 2005 5 25 SWIA200514963 120050505A3350 BULB EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07236SW 120312 ROW 9 EMERGENCY LIGHT BULB IS INOPERATIVE. REPLACED BULB AT ROW 9, FORWARD RED, EMERGENCY LIGHT AT FLOOR TRACK. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050525001072005052500107NM 2005 5 25 C7WA200500095 120050411A2612 WARNING SYSTEM BOEING727 727222 1384073NM PWA JT8 JT8D5 52046NE APU FIRE MALFUNCTIONED A C7WAK NONE N FALSE WARNING ININSP/MAINT 1 SO297642U 19915 APU FIRE BELL SOUNDS OFF AND CANNOT BE SILENCED. NO WARNING LIGHTS OR OTHER INDICATIONS THAT A PROBLEM EXISTS. REMOVED, CLEANED AND REINSTALLED APU FIRE DETECTOR POWER UNIT. SYSTEM OPS. CHECK NORMAL IAW MM. (K) 2L73 4F4 F A3WE E2EA 20050525001422005052500142NM 2005 5 25 97 120050510A5320 FLOOR SUPPORT DOUG MD88 MD88 3023688NM FUSELAGE CORRODED B DU4RK NONE O OTHER ININSP/MAINT 1 SO1512FQ 49766 CABIN FLOOR SUPPORT STRUCTURE FS 200.0 - 256.0 LBL 15 CORRODED. 2L72 4F RTA6WE 20050525001502005052500150EU 2005 5 25 USAA050488 120050321A5320F5347946123200 ANGLE AIRBUS330 A330323 3930335EU FUSLEAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW22938 0337 BFM - CUSP ANGLE CRACKED .75 INCH AREA, FRAME 79-80. CUT OUT CRACKED ANGLE AND REPLACED WITH NEW PART PER SRM 53-00-13 FIG 209. (M) 2L72 4F RTA46NM 20050525001512005052500151NM 2005 5 25 USAA050492 120050315A5312148T2610 BULKHEAD BOEING767 767201 1385125NM FUSELAGE DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19648US68950 23900 BFM - FOUND WEB WITH .490 INCH HOLE, AFT PRESSURE BULKHEAD LBL 10 INCH WL 258. INSTALLED DOUBLER PER EA 95971. (M) 2L72 4F RTA1NM 20050525001532005052500153NM 2005 5 25 USAA050494 120050316A5320453T15388 ANGLE BOEING767 767201 1385125NM FUSLAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19648US68950 23900 BFM - FOUND FLOOR SUPPORT ANGLE WITH 2 CRACKS TOTAL LENGTH APPROX .75 INCH, BS 1263-1285 AT RBL 58. INSTALLED NEWLY FABRICATED REPLACEMENT PART PER SRM 51-10-02, 51-20-01, 51-40-02, EA 96331. (M) 2L72 4F RTA1NM 20050525001552005052500155NM 2005 5 25 USAA050506 120050417A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19390US 23312 CLT - FOUND SKIN CRACKED 2.25 INCH, 727E STRINGER 24L. INSTALLED DOUBLER IAW SRM 53-00-01 FIG 229. (M) 2L72 4F RTA16WE 20050525001582005052500158EU 2005 5 25 USAA050483 120050316A5347F5711056820300 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW 0337 BFM - FOUND SEAT TRACK CORRODED 1 INCH LONG BY 1.5 INCH WIDE BY .27 INCH DEEP, MAIN CABIN Y-450 FRAME 40-42. REMOVED AND REPLACED SEAT TRACK PER SRM 53-00-15. (M) 2L72 4F RTA46NM 20050525001612005052500161NE 2005 5 25 2005F00080 220050409A7200 ENGINE AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE RIGHT FAILED A TRBAD RETURN TO BLOCK MB OVER TEMP SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO29399AT 399 127160 WHILE TAXIING, THE RIGHT ENGINE NACELLE OVERHEAT LIGHT ILLUMINATED. ALSO, SMOKE CAME OUT OF THE ENGINE. AIRCRAFT RETURNED TO BLOCKS. REPLACED RIGHT ENGINE ASSY. ENGINE SENT FOR INSPECTION AND EVALUATION. (M) 2H72 4T4 TRTA53EU E20NE 20050525001662005052500166EA 2005 5 25 2005F00082 220050311A7261 SCREEN BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA SCAVANGE PUMP CONTAMINATED A GUUAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO2981556 UE239 FLT - 9141 - FLL/FPO - DURING FLIGHT, DETECTED SMOKE AND FUMES IN THE CABIN. RETURNED TO FLL. LANDED WITHOUT INCIDENT. CLEANED CARBON FROM RIGHT ENGINE INTERNAL SCAVENGE PUMP INLET SCREEN. RAN ENGINE. NO SMOKE OR FUMES DETECTED. (M) 2L72 4T3 TRTA24CE E2NE 20050525001712005052500171CE 2005 5 25 GNB2005F00003 120050111A291058171029 LINE CESSNA404 404 2075901CE CONT O520 GTSIO520F 17032SO HYD SYSTEM CORRODED E GNBAK NONE O OTHER ININSP/MAINT 1 SW0154ZP 4040694 FAILED HYDRAULIC PRESSURE CHECK. LINE LAYING ON DUCTING FOR HEATING CAUSING CORROSION TO FORM. (SW01200502894) (K) 1L72 3O3 ORTA25CE E7CE 20050525001822005052500182NM 2005 5 25 DHL2005740506 120050329A5533 STRINGER BOEING727 7272Q9 138448MNM VERTICAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 VERT STAB FIN STA 180 STR IS CRACKED AT FRAME ATTACH BOLT. REMOVED FASTENERS FOR ACCESS AT VERT STAB FIN STA 180 S-8 RT AND TRIMMED OUT DAMAGED AREA SIZE 4 1/2 INCH BY 3 INCH IAW B727 SRM 55-30-4 FIG 1 AND 51-30-2. FABRICATED REPAIR FILLER P/N BAC 1517-1367 7075T6511 SIZE 4 1/2 INCH BY 3 INCH PO NR 501953 SPLICE P/N 10134-1201 7075- T6511 PO NR 501952 SIZE 17 1/2 INCH BY 2 INCH FILLERS P/N 7075-T6 .100 SIZE 19 1/2 BY 1/2 PO NR 9001777 SPLICE P/N AND 10133-1401 7075-T6511 SIZE PO NR 501952 IAW B727 SRM 55-30-4 FIG 1. TREATED AND PRIMED PARTS AND AREA IAW B727 SRM 51-10-2. INSTALLED REPAIRS AT VERT STAB FIN STA 180 S-8 RT IAW B727 SRM 55-30-4 FIG 1 AND SRM 51-30-2. 2L73 4F RTA3WE 20050525002132005052500213NM 2005 5 25 DL76S050223 120050416A2597 WIRE BOEING767 767332 1382001NM PDU BROKEN A DALAO OTHER O OTHER TXTAXI/GRND HDL 1 SO27138DL 25409 UPON ARRIVAL NOTIFIED BY RAMP, WHILE UNLOADING CARGO FROM FWD CARGO COMPARTMENT, NOTICED LARGE SPARKS AND SMOKE FROM AREA AROUND NR 8 PDU ON THE LEFT SIDE. C/B FOR PDUS 2, 6, 8 LEFT POPPED. REMOVED PDU, SPLICED 7 WIRES ON P1242, ALL EXCEPT W 704-318, BRY-20 SPLICED W 704-318 BRY -20 WIRES AND ROUTED CORRECTLY. PDU CHECKS NORMAL. 2L72 4F RTA1NM 20050525002182005052500218NM 2005 5 25 DL764050230 120050421A21508252092 ACM BOEING767 767432ER 1385134NM RIGHT SEIZED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO27835MH 29708 FLIGHT ATTENDANT REPORT A VISIBLE HAZE WITH A STRING ODOR IN MID CABIN. REPLACED RIGHT AIR CYCLE MACHINE. 2L72 4F RTA1NM 20050525002322005052500232CE 2005 5 25 DXTA200500731 120050520A27102648 ROD END CESSNA750 750 2076810CE RT AILERON OUT OF ADJUST E DXTAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 GL07909QS 7500009 DURING FLIGHT, REQUIRED LARGE AMOUNT OF RIGHT AILERON TRIM FOR LEVEL FLIGHT AMOUNT INCREASED TO AT LEAST ONE QUARTER TRIM DEFLECTION (RIGHT WING DOWN TRIM) AT 250 KIAS. DID NOT INCREASE SPEED ABOVE 250 KIAS AS TRIM REQUIRED INCREASED WITH SPEED. REMOVED R/H AIRLERON ROD END INSTALLED NEW ROD END. ADJUSTED ROD END RT AILERON AND LT AILERON TO 2.0 DEGREES IAW 750 MM 57-60-00. INSTALLED NEW BOLTS. TRAVEL CHECK GOOD. IAW CE750 M.M. 27-10-00. 2L72 4J RTT00007WI 20050525002372005052500237NM 2005 5 25 05FDEA01374 120050519A5230 DEPRESSOR BOEING727 727200 138407ENM CARGO DOOR DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25264FE 21626 FWD LOWER CARGO DOOR FWD CORNER IS DAMAGED AT AFT END. REPLACED FWD LOWER CARGO DOOR FWD CORNER PER SRM 51-30-2 2L73 4F RTA3WE 20050525002402005052500240NM 2005 5 25 05FDEA01378 120050519A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 FWD CARGO BAY FRAME IS CREASED BS 680, STR 24L TO 25L. REPAIRED FRAME AT BS 680 STR 24L-25L PER SRM 51-40-3. 2L73 4F RTA3WE 20050526000082005052600008NM 2005 5 26 DL75K050245 120050429A3244B757M WHEEL BOEING757 757232 1384965NM MLG SEPARATED A DALAO OTHER O OTHER NRNOT REPORTED 1 SO2767171 30839 NR 6 TIRE SEPARATED CAUSING DAMAGE TO LEFT INBOARD T/E FLAP. TIRE REMAINED INFLATED. REPLACED WHEEL ASSY AND REPAIRED DAMAGE. 2L72 4F RTA2NM 20050526000092005052600009NM 2005 5 26 DLM88050246 120050430A291631914916 O-RING DOUG MD88 MD88 3023688NM RT HYD RES BROKEN A DALAO OTHER KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO27910DL 49541 ON CLIMBOUT NOTED RT HYD QTY AT 2 WITH CAUTION LIGHT ON, HYD PRESS WAS GOOD. TURNED RT ENGINE HYD PUMP AND HYD QTY SLOWLY ROSE UP TO 10 LEFT PUMP, UNTIL APPROACH RT HYD WOULDN'T COME UP WITH ENGINE PUMP SWITCH ON AND AUX PUMP. PERFORMED FLAP 15 LANDING AFTER EMERGENCY EXT OF LANDING GEAR. REPLACED LEAKING O-RING ON BOTTOM OF RT RESERVOIR. SERVICED FLUID. 2L72 4F RTA6WE 20050526000102005052600010 2005 5 26 DL76L050247 420050501A2565251004926 SLIDE BOEING767 767332 1382001NM R1 DOOR UNSERVICEABLE A DALAO OTHER W INADEQUATE Q C TXTAXI/GRND HDL 1 SO27181DN 25986 INADVERTENT SLIDE DEPLOYMENT AT R1 DOOR BY MTC PERSONNEL. DEPLOYMENT SUCCESSFUL. 2L72 4F RTA1NM 20050526000112005052600011NM 2005 5 26 DL764050249 120050502A2450 RELAY BOEING767 767432ER 1385134NM E/E BAY BURNED A DALAO OTHER H ELECT. POWER LOSS-50 PC TXTAXI/GRND HDL 1 SO27827MH 29698 MULTIPLE STATUS MESSAGES DURING TAXI IN. (I.E., MAIN BAT CHG FWD AND AFT DET FAN 1A AND AB, FWD AND AFT CARGO DET AIR) HYD QTY WENT TO 0.03RF ALL THREE RESERVOIRS. WHILE AT THE GATE, MTC FOUND GRD SERVICE BUSS C/B POPPED. RESET SAME AND NOTICED ARCING COMING FROM K105 AND K120 RELAYS IN THE P32 R GEN PWR PANEL IN LOWER E/E COMPT. REPLACED RELAYS AND BPCU. 2L72 4F RTA1NM 20050526000142005052600014NM 2005 5 26 DLM88050252 120050502A2550 DRIVE BELT DOUG MD88 MD88 3023688NM CARGO LOADING WORN A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27998DL 53370 AFTER LIFTOFF, F/A`S REPORTED AN ODOR IN CABIN. ODOR DISSIPATED QUICKLY, HAD A BURNED RUBBER SMELL AND WAS STRONGEST IN THE FWD CABIN. BOROSCOPED NR 1 AND 2 ENGINE NR 3 BEARING AREA. NO WETTING FOUND. BOROSCOPED NR 1 AND 2 ENGINES AREA AROUND BURNER CAN. NO WETTING NOTED. INSPECTED APU INLET FOR CONTAMINATION, NONE NOTED. FOUND MID CARGO LOADING SYSTEM SOURCE OF RUBBER SMELL. BELTS ON DRIVE WORN AND BROKEN. REPLACED SAME. 2L72 4F RTA6WE 20050526000152005052600015NM 2005 5 26 DL757050253 120050503A3244 TIRE BOEING757 757232 1384965NM MLG FAILED A DALAO OTHER O OTHER LDLANDING 1 SO27671DN 25332 TOWER REPORTED BLOWN TIRE ON LANDING NR 5 POSITION. REPLACED NR 5 AND NR 6 MAIN TIRES. WHEEL ASSYS IAW M/M. 2L72 4F RTA2NM 20050526000382005052600038NM 2005 5 26 USAA050514 120050418A5340 CLIP BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US39931 24781 CLT - FOUND CLIP ANGLE BRACKET CRACKED .25 INCH, STATION 360 AT S4L. FABRICATED ANGLE FROM BOEING DRAWING AND INSTALLED IAW DWG 69-48747. (M) 2L72 4F RTA16WE 20050526000412005052600041SO 2005 5 26 SIMA200510804 120050414A3350110049 CHARGER EMB 135 EMB135KL 3260302SO EMERGENCY LIGHT INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21803AE 145483 LGA - LEFT SIDE FORWARD EXTERIOR EMERGENCY LIGHT, EMERGENCY LIGHT AT ROW 3 AND COCKPIT CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY POWER SUPPLY CHARGER NR 1 IAW MM 33-50-04. OPS CHECK GOOD. (M) 2L72 4F RTT00011AT 20050526000542005052600054NM 2005 5 26 USAA050528 120050401A532011565558431LF CHANNEL BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19374US56183 22953 BFM - FOUND CHANNEL CORRODED 2 INCHES WIDE BY .056 INCHES DEEP BY 4.0 INCHES LONG, BETWEEN BS 986-1006, S-24L AND S-25L. INSTALLED REPAIR SUPPORT PLATE, CHANNEL, PER BOEING DWG 65-55843 AND SRM 51-40-02. (M) 2L72 4F RTA16WE 20050526000562005052600056NM 2005 5 26 USAA050541 120050412A5315USTR5310063 FLOORBEAM BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19374US56183 22953 BFM - FOUND FLOOR SUPPORT/ANGLE CORRODED 1 INCH LONG BY 1 INCH WIDE BY .028 INCH DEEP, AFT CARGO FLOOR SUPPORT BS 867 LBL 8.10 INCH. INSTALLED REPAIR ANGLE PER TYPICAL REPAIR 53-10-06B AND SRM 53-60-53. (M) 2L72 4F RTA16WE 20050526000642005052600064EU 2005 5 26 USAA050523 120050415A53471161274 SEAT TRACK AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19714US17533 1046 PIT - FOUND SEAT TRACK BEAM CORRODED .25 INCH BY 1.5 INCH AREA, FRAME 66-68. DEFECTIVE PART REPLACED WITH IDENT PART NUMBER. (M) 2L72 4F RTA28NM 20050526000652005052600065EU 2005 5 26 USAA050520 120050416A5315D53472075001 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19714US17533 1046 PIT - FOUND BEAM CORRODED .25 INCH DIAMETER, RT OUTER SILL BEAM, FRAME 66. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-43-00 DWG IED 53474180. (M) 2L72 4F RTA28NM 20050526000682005052600068NM 2005 5 26 USAA050531 120050323A5320US652072634LF WEB BOEING737 7373B7 1384580NM FUSLEAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19374US56183 22953 BFM - FOUND DOOR SILL WEB CORRODED 1 INCH BY 1 INCH BY .063 INCH AREA, FORWARD CARGO DOOR SILL BS 440-485. CORROSION LEVEL 1, TASK C53-208-01. FABRICATED SILL WEB TR 501886, SRM 53-30-15, 51-40-02. (M) 2L72 4F RTA16WE 20050526000952005052600095EA 2005 5 26 COMA0560300 120050507A77326233M30A ACCELEROMETER CNDAIRCL600 CL6002B19 1900309EA LT ENGINE VIBRATION A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01491CA6362 7756 FLIGHT 5091 LEFT ENGINE 3.5 VIBE CAUTION. REPLACED THE ACCELEROMETER. 2L72 4F RTA21EA 20050526001042005052600104NM 2005 5 26 SWAA051367 120050510A53306545777 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 960, STR 26R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050526001262005052600126EA 2005 5 26 COMA0570051 120050507A531267053110521 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA FS280 CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01376CA5330 10092 LOWER WEB AT LT FS 280 (BACK OF PILOTS CB BULKHEAD) IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE LOWER LT WEB P/N 670-53-11-052-1 IAW CRJ 700 SRM 51-42-06-001-A01. 2L72 4F RTA21EA 20050526001282005052600128EA 2005 5 26 SWIA200514970 120050505A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07466SW 7856 FS 280 RBL 9.0 INBOARD AND OUTBOARD ANGLES ARE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED OB ANGLE IAW CRJ SRM 51-42-06, 51-42-21. 2L72 4F RTA21EA 20050526001292005052600129EA 2005 5 26 SWIA200514971 120050505A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07466SW 7856 FS 280 LBL 9.0 OUTBOARD ANGLE IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED OB ANGLE IAW CRJ SRM 51-42-06, 51-42-21. 2L72 4F RTA21EA 20050526001312005052600131EA 2005 5 26 SWIA200514973 120050511A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07410SW4353 4353 7066 STAB TRIM CHANNEL TWO WOULD NOT ENGAGE. REPLACED HSTCA IAW 27-42-01 AND MCU IAW 27-42-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050526001322005052600132EA 2005 5 26 SWIA200514974 120050511A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07944SW3823 3823 7764 STAB TRIM NR 2 INOP. REPLACED HSTA IAW MM 27-42-01 & MCU IAW MM 27-42-05. OPERATIONAL CHECK GOOD. MCU P/N: 7062-3, S/N OFF: 1095. 2L72 4F RTA21EA 20050526001362005052600136EA 2005 5 26 SWIA200514978 120050508A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY MALFUNCTIONED A SWIAO OTHER N FALSE WARNING CRCRUISE 1 NM07441SW 7602 EN ROUTE RECEIVED SMOKE AURAL, SMOKE WARNING AND ON CARGO FIREX PANEL, LASTED FOR ABOUT 5 SEC, THEN WENT OUT. REPLACED AFT CARGO SMOKE DETECTOR. OPERATIONALCHECK GOOD. P/N: 473597-19, S/N OFF: 1945. 2L72 4F RTA21EA 20050526001392005052600139EA 2005 5 26 SWIA200514981 120050506A2760 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TOTAKEOFF 1 NM07447SW 7677 AFTER TAKEOFF, SPOILERONS FAULT STATUS MSG APPEARED. REPLACED RIGHT OUTBOARD FLIGHT SPOILER PCU IAW 27-60-00. OPERATIONAL CHECK GOOD. P/N 77000-7, S/N OFF MAL3287. 2L72 4F RTA21EA 20050526001402005052600140EA 2005 5 26 SWIA200514982 120050508A2740 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA COCKPIT INOPERATIVE A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07928SW 7701 CAPTAIN'S TRIM SWITCH (STAB TRIM) IS INOPERATIVE. REPLACED CAPTAIN'S TRIM SWITCH. OPERATIONAL CHECK GOOD IAW CRJ MM27-41-05. 2L72 4F RTA21EA 20050526001442005052600144NM 2005 5 26 QXEA200500842 120050508A5330 SKIN DHAV DHC8 DHC8202 2809007NM ZONE 100 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09350PH 488 PDX - EIGHT DENTS IN FUSELAGE SKIN AT RIGHT SIDE, STATION X331-S342 BETWEEN STRINGER 23R-21R. REPAIRED IAW RD 8-53-8523 AND HORIZON AIR EA 2-53-622. 2H72 4T RTA13NM 20050526001452005052600145WP 2005 5 26 ARWA20050502 120050505A3231H61004 SWITCH DOUG DC8 DC863F 302198FWP MLG DOOR MALFUNCTIONED A ARWAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO19661AV 45969 DOORS NOT LATCHED LIGHT REMAINS ON AFTER GEAR RETRACTED AND UPLATCH CHECK. PERFORMED T/S FOUND RT DOOR LATCHED SW INOP. REMOVED AND REPLACE RT DOOR LATCHED SW IN ACCORDANCE WITH M/M DC8 32-60-0. PERFORMED LANDING GEAR DOOR SWITCH TEST SYSTEM OPERATIONAL CHECK NORMAL IN ACCORDANCE WITH DC8 M/M 32-60-0 PAR 3B. 2L74 4F 4A25 20050526001462005052600146NM 2005 5 26 72300176 120050201A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CRACKED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 .5 INCH CRACK IN SHEAR TIE RADIUS. 2L73 4F4 FRTA3WE E2EA 20050526001472005052600147NM 2005 5 26 72300177 120050504A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CRACKED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 .5 INCH CRACK BETWEEN FASTENER HOLES IN STRINGER. 2L73 4F4 FRTA3WE E2EA 20050526001492005052600149NM 2005 5 26 72300179 120050416A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 1 INCH BY 4 INCH AREA OF CORROSION ON BOTTOM OF STRINGER. 2L73 4F4 FRTA3WE E2EA 20050526001532005052600153SO 2005 5 26 C2XA05SH031 120050512A532014530644405 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714938 145029 SHV - DURING C-CHECK THE LT OMEGA BEAM HAS CORROSION FROM FRM 46 TO FRM 52. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED REPAIR LT OMEGA BEAM FRM 46 TO FRM 52 IAW EC 5320-01231. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050526001542005052600154SO 2005 5 26 C2XA05SH033 120050513A532014521713005 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714938 145029 SHV - DURING C-CHECK THE CENTER OMEGA BEAM HAS CORROSION AT FRAME 20. MAINTENANCE REMOVED AND REPLACED CENTER OMEGA BEAM FROM FR 17-24 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050526001582005052600158WP 2005 5 26 ARWA20050504 120050507A242131229000 GENERATOR DOUG DC8 DC863F 302198FWP AC SYSTEM FAILED A ARWAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 SO19441J 45988 DURING CLIMB-OUT, NR 2 GEN SYSTEM DEVELOPED A ZNS. AFTER PERFORMING ABNORMAL CHECK-LIST ONLY LT EMERGENCY BUSS WAS RESTORED. REMOVED AND REPLACED CSD AND AC GENERATOR IN ACCORDANCE WITH DC-8 M/M 24-10-1 AND 24-20-1. LEAKS CHECKED; NO LEAKS NOTED; GENERATOR (GND) TEST NORMAL IN ACCORDANCE WITH M/M 24-00 AND M/M 71-00. 2L74 4F 4A25 20050526001612005052600161NM 2005 5 26 SWAA051372 120050511A2611100064901 SMOKE DETECTOR BOEING737 7373H4 1384600NM AFT CARGO FAULTY A SWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW29326SW 23690 AIR TURNBACK/DECLARED EMERGENCY. CLIMBING THRU 11,000 FT AFT CARGO FIRE WARNING LIGHT CAME ON. DISCHARGED FIRE BOTTLE & LANDED. NO FIRE INDICATIONS NOTED. REMOVED AND REPLACED 3 EA SMOKE DETECTORS IN AFT CARGO BAY & FIRE WARNING CONTROL UNIT PER MM. 2L72 4F RTA16WE 20050526001632005052600163NM 2005 5 26 SWAA051374 120050511A53226545805 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29352SW 24888 DURING SCHEDULED 1/2D CHECK, FOUND BELT FRAME SHEAR TIE CRACKED AT BS 276, STR 9L TO STR 10L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050526001652005052600165NM 2005 5 26 SWAA051376 120050511A53306545775 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 882, STR 26R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050526001662005052600166 2005 5 26 SWAA051377 420050510A2565D31354 SLIDE BOEING737 7373T5 1384608NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29696SW 23064 DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050526001682005052600168 2005 5 26 SWAA051379 420050511A256565C16820 HOOK BOEING737 7377H4 1384404NM R2 DOOR SLIDE OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29795SW 30606 R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR STOW HOOKS OUT OF ADJUST. ADJUSTED HOOKS PER MM. 2L72 4F RTA16WE 20050526001712005052600171NM 2005 5 26 SWAA051382 120050511A53306545766 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 440 TO BS 446, STR 16R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050526001752005052600175EA 2005 5 26 MASA200500319 120050428A3350 SIGN CNDAIRCL600 CL6002B19 1900309EA EMERGENCY EXIT MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0737208 7208 ASH 2934. THE CREW REPORTED A CABIN EMERGENCY EXIT LIGHTED SIGN AT THE SERVICE DOOR THAT WAS 50 PERCENT LIT. MAINTENANCE RESET AND OPS CHECKED GOOD. 2L72 4F RTA21EA 20050526001772005052600177EA 2005 5 26 MASA200500329 120050502A3350 LIGHT CNDAIRCL600 CL6002C10 1390015EA CABIN INTERMITTENT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07504MJ 10066 ASH 7038 ATL - THE CAPTAIN REPORTED THE AISLE CEILING EMERGENCY LIGHT AND A I/H AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE COULD NOT DUPLICATE THE DISCREPANCY. 2L72 4F RTA21EA 20050526001792005052600179SO 2005 5 26 MASA200500336 120050506A3350 SIGN EMB 145 EMB145LR 3260212SO EMERGENCY EXIT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07826MJ 145214 ASH 2857 CLT TO BNA, THE CREW REPORTED A EMERGENCY EXIT SIGN AT THE LEFT EXIT ROW INOP. MAINTENANCE REPLACED LIGHT ASSEMBLY. 2L72 4T RTT00011AT 20050526001802005052600180EA 2005 5 26 MASA200500338 120050506A3350 SIGN CNDAIRCL600 CL6002B19 1900309EA EMERGENCY EXIT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0777331 7331 ASH 7216 ORD - THE CREW HAD AN EMERGENCY EXIT SIGN AT THE LEFT OVERWING EXIT INOP. MAINTENANCE SECURED WIRING AT THE LIGHT ASSEMBLY. 2L72 4F RTA21EA 20050526001822005052600182SO 2005 5 26 MASA200500345 120050510A3350 SIGN EMB 145 EMB145LR 3260212SO EMERGENCY EXIT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07836MJ 145359 ASH 2663 CLT TO STL - THE CREW HAD THE LT OVERWING EMERGENCY EXIT SIGN INOP. MAINTENANCE REPLACED THE EXIT SIGN POWER INVERTER AND THE SIGN OPERATED NORMALLY. THE AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. 2L72 4T RTT00011AT 20050526001862005052600186EA 2005 5 26 MASA200500308 120050421A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA EMERGENCY EXIT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0777278 7314 ASH 6150 COS TO PHX - THE CREW REPORTED AN EMERGENCY LIGHT AFT OF THE RIGHT HAND WING EMERGENCY EXIT INOP. MAINTENANCE RELAMPED THE LIGHT. 2L72 4F RTA21EA 20050526001872005052600187NE 2005 5 26 XN0A1234 220050507A7320 FUEL CONTROL AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE NR 2 FLOW ERRATIC A XN0AO OTHER O OTHER NRNOT REPORTED 1 GL23373PC 218 NR 2 FUEL FLOW ERRATIC. TRANSFERRED TO DMI NR 5396 IAW A-300 MEL 73-30-01 CAT "B". (STATUS:ORIG/OPEN) 2L72 4F4 FRTA35EU E23EA 20050526001882005052600188NM 2005 5 26 XN0A1235 120050511A7400 IGNITION UNIT BOEING727 727227 1384078NM NR 2 ENGINE MALFUNCTIONED A XN0AO OTHER O OTHER NRNOT REPORTED 1 GL2376752 21248 NR 2 ENGINE WILL NOT START, NO IGNITION. NR 2 ENGINE IGNITION CB'S RESET, OP'S CHECK GOOD. 2L73 4F A3WE 20050526001892005052600189NM 2005 5 26 DL757050238 120050427A2120 ODOR BOEING757 757232 1384965NM CABIN DETECTED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27683DA 27103 A/C DIVERTED TO DEN DUE TO ACRID ODOR IN CABIN. AFTER INTENSIVE TROUBLESHOOTING, COULD NOT DUPLICATE ODOR. ALL A/C SYSTEMS FUNCTIONING AND OPERATING NORMALLY. 2L72 4F RTA2NM 20050526001902005052600190NM 2005 5 26 XN0A1236 120050513A3600 WARNING LIGHT BOEING727 727227 1384078NM LT DUCT ILLUMINATED A XN0AO OTHER J WARNING INDICATION DEDESCENT 1 GL2376752 21248 DURING EMERGENCY DESCENT, LT DUCT OVERHEAT LIGHT TRIP, PERFORMED ALL CHECKLIST. 2L73 4F A3WE 20050526001912005052600191NM 2005 5 26 AWXA200500550 120050505A57536546430129 SKIN BOEING737 7373G7 1384595NM LT FORE FLAP DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28322AW 25400 MCN - MAJOR REPAIR - DURING C-14 CHECK THE UPPER SURFACE SKIN OF THE LT INBOARD FORE FLAP WAS FOUND DELAMINATED 12 INCHES FROM THE INBOARD END BETWEEN WBL 84 AND WBL 86. MAINTENANCE CUT OUT DAMAGE IN UPPER SURFACE SKIN OF THE LT INBOARD FORE FLAP; FABRICATED A FILLER AND DOUBLER; BONDED REPAIR PARTS TO FLAP IAW B737-300 SRM 51-70-10. 2L72 4F RTA16WE 20050526001932005052600193NM 2005 5 26 AWXA200500552 120050509A5320655287854 ANGLE BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28322AW 25400 MCN - MAJOR REPAIR - DURING C-14 CHECK A .375 INCH CRACK WAS FOUND IN L-2 INNER CHORD LOWER STIFFENER AT BS 967, LBL 44, WL 207.5. MAINTENANCE REMOVED CRACKED STIFFENER AT BS 967, LBL 44; RECEIVED NEW REPLACEMENT STIFFENER AND DRILLED IT TO SPECIFICATION OF DWG 65-52878; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050526001942005052600194NM 2005 5 26 AWXA200500553 120050429A532065617777 CHANNEL BOEING737 7373B7 1384580NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28332AW 23384 MCN - MAJOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK WAS FOUND IN LOWER SURFACE OF STRINGER SPLICE CHANNEL AT BS 360, STR 15 LT. MAINTENANCE REMOVED CRACKED STRINGER SPLICE CHANNEL AT BS 360, STR 15 LT; FABRICATED A NEW REPLACEMENT SPLICE CHANNEL PER DWG 65-61777; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050526001952005052600195EU 2005 5 26 AWXA200500554 120050505A5347D5347209000200 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28639AW 471 SAL - MAJOR REPAIR - DURING C08 CHECK GALVANIC CORROSION WAS FOUND ON SEAT TRACK BEAM Y765 AT FR 66. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK BEAM Y765 AT FR 66; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050526001972005052600197NM 2005 5 26 AWXA200500556 120050504A53206545875520 STRAP BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28322AW 25400 MCN - MAJOR REPAIR - DURING C-14 CHECK GALVANIC CORROSION WAS FOUND ON R-1 LOWER INNER CHORD UPPER STRAP AT BS 294, RBL 60, WL 208.5. MAINTENANCE REMOVED CORRODED UPPER STRAP AT BS 294, RBL 60; RECEIVED NEW REPLACEMENT STRAP AND DRILLED IT TO SPECIFICATION OF DWG 65-45875; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050526001982005052600198NM 2005 5 26 AWXA200500557 120050429A53206553594501 REVEAL BOEING737 7373B7 1384580NM FUSLEAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28332AW 23384 DURING C-18 CHECK A .25 INCH CRACK WAS FOUND IN REVEAL AT UPPER AFT CORNER OF R-1 DOOR CUTOUT BS 323, STR 16 RT. MAINTENANCE REMOVED CRACKED REVEAL AT UPPER AFT CORNER OF R-1 DOOR CUTOUT BS 323, STR 16 RT; FABRICATED A NEW REPLACEMENT REVEAL PER DWG 65-53594; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050526001992005052600199WP 2005 5 26 UPS05844436 120050419A5712 RIB DOUG DC8 DC873F 302199FWP RH XFS CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE: C1, RT WING L/E UPPER RIB CRACKED 1 INCH LONG AT XFS 841.25. REPAIRED IAW DC-8 SRM 57-3-3 AND SRM 51-1-21. 2L74 4F RT4A25 20050526002002005052600200WP 2005 5 26 UPS05844437 120050421A53404750419U501 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE:C1 MAIN CABIN STA 1180 L20R FRAME ATTACH FITTING CRACKED .5 INCH LONG. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20050526002012005052600201WP 2005 5 26 UPS05844438 120050422A53403755827U2 FITTING DOUG DC8 DC873F 302199FWP CARGO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE:C1 A CARGO DOOR CUTOUT LOWER FWD BANANA FITTING CRACKED. REMOVED AND REPLACED BANANA FITTING IAW DC-8 SRM 51-1-20D AND 51-3-2. 2L74 4F RT4A25 20050526002032005052600203WP 2005 5 26 UPS05844440 120050422A534037558271N FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE:C1 A CARGO DOOR CUTOUT LOWER AFT BANANA FITTING HAS .5 INCH CRACK. REMOVED AND REPLACED BANANA FITTING IAW DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20050526002052005052600205EU 2005 5 26 DXTA200500718 120050509A32301EM15N111 PROXIMITY SWITCH BRAERO1000 BAE1251000 1500287EU MLG MALFUNCTIONED E DXTAO OTHER J WARNING INDICATION APAPPROACH 1 GL07514QS NA1005 NOSE GEAR GREEN LIGHT WILL NOT ILLUMINATE WITH GEAR DOWN. REPLACED NOSE LANDING GEAR CHANGE OVER SWITCH. OPS CHECK GOOD IAW THE HAWKER 1000 MM 32-60-05. REPLACED NOSE LANDING GEAR CHANGE OVER MICRO SWITCH P/N WITH NEW P/N 1EN1-14N119. PERFORMED SATISFACTORY, OPS CHECKS IAW THE HAWKER 1000 MM 32-60-05. 2L72 4F RTA3EU 20050526002082005052600208WP 2005 5 26 0500729854 120050510A2900 HYDRAULIC SYSTEM DOUG DC9 DC951 3022051WP RIGHT MALFUNCTIONED A NWAAO OTHER GS MULTIPLE FAILURE AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL01763NC 47716 FLT CREW HAD REPORTED THE FAILURE OF THE RIGHT HYDRAULIC SYSTEM DURING CLIMBOUT FROM CMH. COMPLIED WITH COM PROCEDURES AND THE SYSTEM RETURNED TO NORMAL. FLIGHT CONTINUED TO DESTINATION, REPORTED ALL SYSTEMS NORMAL BUT REQUESTED CFR AS A PRECAUTION, AND DECLARED AN EMERGENCY WITH ATC. FLIGHT LANDED WITHOUT INCIDENT BUT DURING TAXI TO GATE, THE AIRCRAFT MADE CONTACT WITH A PARKED A-319 TYPE AIRCRAFT. THIS INCIDENT IS CURRENTLY UNDER INVESTIGATION AND MECHANICAL DETAILS ARE NOT AVAILABLE AT THIS TIME. POSSIBLE BRAKE SYS FAILURE AND/OR NOSE STEERING FAILURE. 2L72 4F RTA6WE 20050526002092005052600209EA 2005 5 26 SWIA200514986 120050504A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07423SW 7456 FUSELAGE TRANSVERSE BEAM LOWER FLANGE IS CRACKED; FS 280.00 LBL 12.0. ITEM FOUND AT C-CHECK INSPECTION. REPAIR PARTS INSTALLED IAW CRJ REO 601R-53-11-171 REV "B". 2L72 4F RTA21EA 20050526002102005052600210EA 2005 5 26 SWIA200514987 120050504A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07423SW 7456 FUSELAGE TRANSVERSE BEAM LOWER FLANGE IS CRACKED; FS 280.00 RBL 12.0. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R 53-11-171 REV "B". 2L72 4F RTA21EA 20050526002122005052600212EA 2005 5 26 SWIA200514989 120050504A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07423SW 7456 FS 529.00 RIGHT FLOORBEAM RBL 9.0 STANDOFF SUPPORT ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED ANGLE IAW CRJ SRM 51-31-00, 51-24-21, 51-24-36, 51-21-11, 51-25-06, 51-42-06, 51-42-13. 2L72 4F RTA21EA 20050526002162005052600216EA 2005 5 26 SWIA200514993 120050510A3350 LIGHT CNDAIRCL600 CL6002C10 1390015EA CABIN BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07707SK 10003 EMERGENCY LIGHT BURNED OUT, BULKHEAD AFT OF FIRST CLASS SECTION. REWIRED REF RIL FROM BOMBARDIER 0375 AND C & D AEROSPACE ENGINEERING CHANGE NOTICE CAGE 56135 DRAWING A407008. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050526002172005052600217WP 2005 5 26 AALA20050317 120050510A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21262AA 49290 HDQ - COCKPIT AND FORWARD CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR COCKPIT AND FORWARD CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050526002182005052600218WP 2005 5 26 AALA20050320 120050511A3350P4010051111 MODULE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21570AA 49352 BOS - DURING CHECK FOUND EMERGENCY LIGHTS FROM FIRST CLASS BACK TO ROW 24 INOPERATIVE. REPLACED FIRST CLASS CHARGER AND THREE BATTERY PACKS FOR EMERGENCY LIGHTS FROM FIRST CLASS BACK TO ROW 24. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050526002192005052600219NM 2005 5 26 AALA20050321 120050511A3350 LIGHT BOEING737 737823 13844BZNM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21919AN 29520 DFW - FORWARD EMERGENCY PATH LIGHT ON SEAT 7D INOPERATIVE. REPLACED FORWARD EMERGENCY PATH LIGHT ON SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20050526002202005052600220WP 2005 5 26 AALA20050322 120050511A49905940405503 APU DOUG DC9 DC982 3022082WP APU BAY LEAKING A AALAA UNSCHED LANDING KBJFLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SW21410AA 49321 ORD - AFTER TAKEOFF FLIGHT ATTENDANT REPORTED SMOKE FILLING BACK OF CABIN FROM LIGHTS IN OVERHEAD AND SIDEWALLS. FOUND APU OIL LEAK. APU WAS REPLACED PER CARD 49 96 82. ACCOMPLISHED BURN OUT OF PNEUMATIC DUCTING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050526002212005052600221WP 2005 5 26 AALA20050318 120050510A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21262AA 49290 DFW - AFT OVERWING EMERGENCY LIGHT EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK FOR AFT OVERWING EMERGENCY LIGHT EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050526002232005052600223NM 2005 5 26 AALA20050324 120050512A3350P4010049 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21188AN 32382 LAX - EMERGENCY LIGHTS ON RIGHT HAND SIDE FROM ROW 25 TO 36 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS ON RIGHT HAND SIDE FROM ROW 25 TO 36. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050526002242005052600224NM 2005 5 26 AALA20050319 120050510A3350 LIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21757AN 32636 MIA - EMERGENCY LIGHT AT COMAT 371 FIRST CLASS GALLEY MODULES INOPERATIVE. FOUND LIGHT ASSEMBLY BY COMAT 371 SHORTING EMERGENCY LIGHT POWER SUPPLY. REPLACED EMERGENCY LIGHT AND BATTERY PACK FOR EMERGENCY LIGHT AT COMAT 371 FIRST CLASS CALLEY MODULES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20050526002252005052600225 2005 5 26 AALA20050325 420050419A2565 SPRING BOEING767 767323 1385205NM PAX DOOR SLIDE INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21361AA 24042 AFW - SPRING ON RIGHT NR 1 DOOR PER AD 2001 26 19 WILL NOT STAY IN COTTER PIN. FORWARD SPRING RIGHT NUMBER ONE DOOR ON GIRT BAR. REPLACED GIRT BAR ON RIGHT NUMBER ONE DOOR. 2L72 4F RTA1NM 20050526002272005052600227EU 2005 5 26 200505122 120050512A6123 WARNING LIGHT SAAB SF340 SF340A 7850100EU AUTOCOARSEN ILLUMINATED A UHLAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL1719XS 340A019 AUTOCOARSEN LIGHT ON CWP ILLUMINATED WITH AUTOCOARSEN ON. AIRCRAFT SAFELY ARRIVED TO IAD. 2L72 4T RTA52EU 20050526002282005052600228EU 2005 5 26 200505121 120050512A6123 COMPUTER SAAB SF340 SF340A 7850100EU AUTOCOARSEN MALFUNCTIONED A UHLAO OTHER J WARNING INDICATION CRCRUISE 1 GL1719XS 340A019 AUTOCOARSEN LIGHT ILLUMINATED. THE AIRCRAFT SAFELY ARRIVED IN IAD. REMOVED AND REPLACED AUTOCOARSEN COMPUTER, OPS CHECK GOOD IAW 61-20-00. 2L72 4T RTA52EU 20050526002292005052600229NM 2005 5 26 QXEA200500843 120050509A5320 SILL BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09412QX 4059 PDX - FORWARD PASSENGER DOOR SILL HAS CORROSION IN NUMEROUS LOCATIONS BETWEEN STATION X1 AND X32. REPAIRED IAW DHC-8-400 SRM 51-21-10 AND SRM 51-42-05. 2H72 4T RTA13NM 20050526002302005052600230NM 2005 5 26 QXEA200500845 120050509A5420 DIAPHRAGM BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09412QX 4059 PDX - LEFTHAND NACELLE TO WING DIAPHRAGM IS CRACKED, OUTBOARD AFT TRAILING EDGE. REPAIRED IAW DHC-8 400 SRM 51-42-05. 2H72 4T RTA13NM 20050526002322005052600232CE 2005 5 26 CIEA200500002 120050512A3397 CONNECTOR BEECH 200 B200 1152922CE INSTRUMENT PANELBENT E CIEAA UNSCHED LANDING O OTHER CLCLIMB 1 NM035ST 7435 BB926 SHORTLY AFTER TAKEOFF, THE ENGINE INSTRUMENT AND AUDIO PANEL CIRCUIT BREAKER POPPED. THE AIRCRAFT WAS FLYING AT NIGHT. THE AIRCRAFT RETURNED TO THE AIRPORT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A STUD FOR THE LIGHT PANEL ON THE AVIONICS OVERLAY TO BE BENT AND CONTACTING THE FRAME. THE PIN WAS STRAIGHTENED AND POSITIONED AND PROTECTED TO ELIMINATE THE SHORTING CONDITION. THE PI WAS MOST LIKELY BENT WHILE MOVING THE AVIONICS PANEL IN AND OUT OF THE AIRCRAFT AND DUE TO VIBRATION FINALLY CAME INTO CONTACT WITH THE FRAME. 1L72 4T A24CE 20050526002342005052600234CE 2005 5 26 CIEA200500004 120050514A1420PT06SE106S CONNECTOR LEAR 35 35A 5170602CE BROKEN E CIEAK NONE O OTHER ININSP/MAINT 1 NM03222BE10033179 35A489 THE STALL WARNING ACCELEROMETER WAS BEING USED TO TROUBLESHOOT A PROBLEM ON ANOTHER AIRCRAFT. DURING THE REMOVAL OF THE ACCELEROMETER, THE WIRE BROKE ON PIN B OF THE CANNON PLUG. AS PART OF THE TROUBLESHOOTING IT WAS DETERMINED THE PROBLEM ON THE OTHER AIRCRAFT WAS ALSO A BROKEN WIRE ON THE CANNON PLUG FOR THE ACCELEROMETER AS WELL. THE WIRES TO THE CANNON PLUG ARE VERY SMALL. DURING COMPLIANCE OF AD 82-01-05 R2, THE WIRES ARE FLEXED AS PART OF THE CHECK. THIS AD HAS A RECURRING INTERVAL OF 220 HOURS. THE CONTINUED TESTING OF THE ACCELEROMETER IS GOING TO RESULT IN MORE WIRE FAILURES. 2L72 4F A10CE 20050526002362005052600236NM 2005 5 26 P5CA0501349 120050512A273065B818751 ACTUATOR BOEING747 747249F 1384849NM ELEVATOR MALFUNCTIONED A P5CAK NONE O OTHER ININSP/MAINT 1 EA15920FT 22237 CREW RETURNED AIRCRAFT TO BLOCKS ADVISING ELEVATORS WERE STIFF DURING FLIGHT CONTROL CHECK. REPLACED ELEVATOR FEEL ACTUATOR PER MM 27-31-17. OPS CHECK PER MM 27-31-14, NO DISCREPANCIES NOTED. 2L74 4F A20WE 20050526002372005052600237NE 2005 5 26 C8GA20050013 220050512A7230 COMPRESSOR BOEING727 727223 1384074NM PWA JT8 JT8D15 52051NE NR 1 ENGINE STALLED A C8GAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SO29899AA506136904 22015 700754 FLT 711 FROM DEN TO TOL, ON CLIMB FROM DEN, NR 1 ENGINE COMPRESSOR STALLED. AIRCRAFT RETURNED TO DEN AND LANDED WITHOUT INCIDENT. AFTER RETURN TO BLOCKS, WITH ENGINE OPERATING AT 1.40 EPR, ENGINE COMPRESSOR STALLED AGAIN. PERFORMED BORESCOPE INSPECTION AND FOUND 6TH STAGE BLADE FAILURE. REPLACED ENGINE. AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 20050526002382005052600238 2005 5 26 P9RA20050079 420050513A2565D198391 GIRT BAR DOUG DC9 DC982 3022082WP CABIN DIRTY A P9RAO OTHER O OTHER NRNOT REPORTED 1 SO1114816 49370 SFB GATE ITEM P1, L2 DOOR WILL NOT DISARM. CLEANED AND LUBRICATED GIRT BAR IAW MM. OPERATIONAL CHECKED NORMAL. 2L72 4F A6WE 20050526002402005052600240NM 2005 5 26 DHL2005740509 120050329A5311 FRAME BOEING727 7272Q9 138448MNM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 CABIN INTERIOR FRAME AT BS 360 IS DENTED BETWEEN ST4R AND 5R PREVIOUS FRAME REPAIR. REMOVED ANGLE SUPPORT DUE TO DENT IAW B727 SRM 51-30-2. LOCATED AND DRIILED NEW ANGLE P/N AE 727-2-360-11 PO507998 AND DOUBLER AE 727-2-360-12 PO5080133. TREATED AND PRIMED HOLES AND AREA IAW B727 51-10-2, INSTALLED ANGLE AND DOUBLER SUPPORT AT BS 360 BETWEEN STR 4R IAW DWS AE 727-2-360 REV-G AEI. 2L73 4F RTA3WE 20050526002432005052600243EA 2005 5 26 VTZA200500080 120050513A7830 LOCK TAB CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER BROKEN A VTZAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA27630BR 7255 RIGHT THRUST REVERSER UNLOCK MESSAGE ON TAKEOFF. REMOVED AND REPLACED BROKEN ANTI-ROTATION TANGS AT 5 & 7 O`CLOCK POSITIONS. 2L72 4F RTA21EA 20050526002442005052600244NM 2005 5 26 05FDEA01230 120050510A5720652165835 SUPPORT ANGLE BOEING727 727200 138407ENM LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25212FE 22934 LEFT WING LOWER T/E SUPPORT ANGLES CRACKED BELOW INBOARD END OF NR 4 SPOILER. REMOVED AND REPLACED INBOARD AND OUTBOARD SUPPORT ANGLES IAW SRM 51-30-2. 2L73 4F RTA3WE 20050526002462005052600246NM 2005 5 26 05FDEA01232 120050510A53206517592248 FLOOR SUPPORT BOEING727 727200 138407ENM COCKPIT FLOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25212FE 22934 COCKPIT FLOOR DENTED AND 3 EACH SUPPORT ANGLES CRACKED AT APPROX FS 259 LBL 5 AND 9 AS SEEN THRU NWW UPPER CEILING PANEL. REWORKED DENT IAW SRM 51-40-1. REMOVED AND REPLACED IAW SRM 51-30-2. 2L73 4F RTA3WE 20050526002472005052600247NM 2005 5 26 05FDEA01233 120050511A5311 FRAME BOEING727 727200 138407ENM FUSLEAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25264FE 21626 BS 740 LOWER CHORD CORRODED AT RBL 6. *S/D* REPAIRED PER EA 7-5310-86287. 2L73 4F RTA3WE 20050526002482005052600248NM 2005 5 26 05FDEA01234 120050511A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25480FE 21462 LOWER FUSELAGE BETWEEN STRINGER 27R AND 28R, STA 1065 TO 1074. EVALUATED REPAIR, FOUND TO END ON A STRINGER AND THEREFORE A CAT-B REPAIR. REMOVED DOUBLER IAW SRM 51-30-2. FABRICATED NEW DOUBLER IAW SRM 53-30-3. LOCATED & DRILLED DOUBLER REPAIR IAW 51-30-5. TREATED, ALODINED & PRIMED IAW SRM 51-10-2. INSTALLED NEW DOUBLER REPAIR IAW SRM 51-30-2. 2L73 4F RTA3WE 20050526002492005052600249NM 2005 5 26 05FDEA01235 120050511A5315 FLOORBEAM BOEING727 727200 138407ENM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25212FE 22934 REMOVED NUT PLATES IAW SRM 51-30-2, REMOVED CORROSION IAW SRM 51-10-6, FOUND TO BE OUT OF LIMIT IAW SRM 53-10-1 FIG 1. FABRICATED NEW SUPPORT ON TRAVELER T5/516572 IAW SRM 53-10-2 FIG 8, INSTALLED 2 ANGLE REPAIR IAW SRM 51-40-4 FIG 1, INSTALLED NUT PLATE IAW SRM 51-30-2. 2L73 4F RTA3WE 20050526002502005052600250NM 2005 5 26 05FDEA01236 120050511A5313651842043 STRINGER BOEING727 727200 138407ENM MAIN CARGO CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25212FE 22934 MAIN CARGO COMPT FS 344-360 STR 5L HAS CORROSION JUST AFT OF L-1 DOOR CUTOUT. REMOVED AND REPLACED STRINGER IAW SRM 51-30-2. 2L73 4F RTA3WE 20050526002582005052600258EU 2005 5 26 05FDEA01244 120050512A5754 SLAT TRACK AIRBUS310 A310203 3930313EU LT WING WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25403FE 230 LEFT SLAT TRACK NR 8 WEAR IS BEYOND ALLOWABLE LIMITS PER A310-200 SRM 57-40-00 TABLE 101 AND FIGURE 108 AND REQUIRES REPLACEMENT PER NOTE ON EA 6-5740-49974A. REMOVED AND REPLACED SLAT TRACK AND BUSHINGS IAW A310-200 AMM 27-80-14-4 AND COMPLIED WITH EA 6-5750-88829, OPS CHECK GOOD IAW A310-200 AMM 27-80-00-05. 2L72 4F RTA35EU 20050526002602005052600260EU 2005 5 26 05FDEA01246 120050512A5320A2577105300400 WATER TRAP AIRBUS310 A310203 3930313EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25403FE 230 BAY BEHIND FWD CARGO COMPARTMENT DRAIN FOR FLOOR HAS EXFOLIATION CORROSION EXTENDING AROUND AND UNDER FASTENERS. REMOVED AND REPLACED 1 EA WATER TRAP FOR FORWARD CARGO COMPARTMENT DRAIN IAW A310-200 SRM 51-40-21. 2L72 4F RTA35EU 20050526002612005052600261EU 2005 5 26 05FDEA01247 120050512A5320A36170327200 BRACKET AIRBUS310 A310203 3930313EU ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25403FE 230 APU BLEED AIR DUCT ATTACH BRACKET AT FR 58 ON FLOORBEAM IN AFT PIT LT SIDE HAS A CRACK IN THE RADIUS. REMOVED EXISTING BRACKET AND REPLACED WITH NEW BRACKET IAW A310-200 SRM 51-72-10. 2L72 4F RTA35EU 20050526002632005052600263EU 2005 5 26 05FDEA01249 120050512A5420A5451526850300 GUSSET AIRBUS310 A310203 3930313EU ZONE 400 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25403FE 230 NR 2 PYLON OUTBOARD SIDE RIBS 15A, 16A, AND 17A UPPER AREA OF PYLON HAVE CORROSION AROUND, IN FASTENER HOLES AND EXTENDING UNDER NUT PLATES AS MARKED. REMOVED AND REPLACED GUSSETS IAW A310-200 SRM 51-40-21 AND 51-72-10. 2L72 4F RTA35EU 20050526002652005052600265EU 2005 5 26 05FDEA01251 120050512A53509228M64G21 FAIRING AIRBUS310 A310203 3930313EU ZONE 400 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25403FE 230 UPON INSPECTION OF REMOVED PARTS ON TC 44C0204 FOUND STATOR VANE SPACER IS CRACKED AT TIP (OFF AIRCRAFT PART). REPLACED STATOR VANE SPACER TO BE INSTALLED ON N00682 IAW A310-200 AMM 72-23-00. 2L72 4F RTA35EU 20050526002682005052600268EU 2005 5 26 05FDEA01254 120050512A5340A572419142000 BRACKET AIRBUS310 A310203 3930313EU ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25403FE 230 LANYARD BRACKET ON L/E PANEL 612BB IS CRACKED. REMOVED AND REPLACED ANGLE BRACKET IAW A310-200 SRM 51-40-23. 2L72 4F RTA35EU 20050526002692005052600269EU 2005 5 26 05FDEA01255 120050512A5420 SHROUD AIRBUS300 A300B4605R 3930308EU ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25653FE 736 PYLON NR 1 SHROUD/PAN, UNDER THE ENGINE BLEED AIR DUCT, IS CRACKED. VIEWED THRU ACCESS PANEL 413EL. REMOVED CRACKED SHROUD, FAB NEW SHROUD ON TR T5/517007 301-25 .025SS BATCH 0000887337, INSTALLED SHROUD IAW SRM 51-4-21. 2L72 4F RTA35EU 20050526002702005052600270WP 2005 5 26 0500739881 120050513A7830 O-RING DOUG DC9 DC951 3022051WP THRUST REVERSER WORN A NWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 GL01676MC 47652 DURING APPROACH FOR LANDING AT DTW, THE CREW NOTICED THAT THE LEFT HYDRAULIC SYSTEM FLUID DROPPED TO ZERO QUANTITY INDICATION. COMPLIED WITH COM PROCEDURES AND THE AIRCRAFT LANDED WITHOUT INCIDENT. DTW MAINTENANCE FOUND THE LEFT HYDRAULIC SYSTEM WAS COMPLETELY DRAINED BY A LEAKING SEAL ON THE CHECK VALVE AT THE BOTTOM OF THE THRUST REVERSER. THE O-RING WAS REPLACED, THE SYSTEM WAS RESERVICED, AND THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050526002712005052600271WP 2005 5 26 0500749856 120050512A2170 COALESCER BAG DOUG DC9 DC951 3022051WP CABIN AIR ODOR A NWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL01765NC 47718 SOON AFTER TAKEOFF, BOTH THE LEFT AND RIGHT AIR CONDITION SUPPLY TEMP HIGH LIGHTS ILLUMINATED. AT ABOUT THE SAME TIME THE FLIGHT ATTENDANT REPORTED VISIBLE SMOKE IN THE CABIN. THE CREW COMPLIED WITH COM PROCEDURES, RETURNED TO MSP, AND MADE AN UNEVENTFUL BUT OVERWEIGHT LANDING. SMOKE SLOWLY DISSIPATED AFTER THE AIRFOIL ANTI-ICE SYSTEM WAS TURNED OFF. MAINTENANCE AT MSP COULD NOT FIND ANY SOURCE OF SMOKE. RAN ENGINES AT TAKEOFF POWER WITH AIRFOIL ANTI-ICE ON. NO SMOKE OR SMELLS WERE NOTED. THE WATER SEPARATOR BAGS WERE REPLACED, STRINGER CHECK PERFORMED, AND THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050526002742005052600274CE 2005 5 26 DJFA2005094 120050509A2760 SPEED BRAKE BEECH MU300 400A 1155402CE MALFUNCTIONED E DJFAO OTHER F FLT CONT AFFECTED APAPPROACH 1 EA23741TA RK201 CREW REPORTED; ON APPROACH ABOVE 10,000 FT SPEEDBRAKES WERE EXTENDED & A YAWING / ROLLING MOVEMENT OF ACFT OCCURRED WITH NOSE MOVING 15-20 DEG. SPEEDBRAKES RETRACTED & CREW DISCONNECTED AUTOPILOT & PERFORMED A CONTROL CHK OF ACFT. ACFT THEN BEHAVED NORMAL. AT APPROX 4,000 FT THE SPEEDBRAKES EXTENDED, & SAME OSCILLATION OBSERVED. SPEEDBRAKES AGAIN RETRACTED & OSCILLATION CEASED. FLT CONTINUED & ACFT LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED SPEEDBRAKES, & PERFORMED AN OPS CHK. OPS CHK NORMAL. A CHK FLT COMPLETED & SPEED BRAKES EXTENDED AT 200-KTS, WITH AUTOPILOT ON & IN TURNS WITH AUTOPILOT ON & OFF. NO UNUSUAL TURNS OR ROLLS NOTED. ACFT RETURNED TO SERVICE. 2H72 4F RTA16SW 20050526002752005052600275NM 2005 5 26 05FDEA01281 120050514A5340A5A7114511 FITTING DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25580FE 48471 CENTER CARGO COMPARTMENT, FOUND BILGE LOCATION L-49R STA 1531 SPLICE FITTING CRACKED. REMOVED AS PER SRM 51-33-01 VOLUME II AND NEW SPLICE FITTING FABRICATED AS PER DRAWING NR A5A7114 AND INSTALLED AS PER SRM 51-33-01 VOLUME II. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050526002762005052600276WP 2005 5 26 05FDEA01395 120050521A5330 SKIN DOUG DC10 DC1010 3022110WP FUSELAGE DAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25571FE 47830 EXISTING REPAIR ON FUSELAGE LOWER SKIN AT STA 695/715, LONG 51/52. REMOVED AND RETAINED EXTERNAL DOUBLER IAW SRM 51-35-01 AND SRM 51-33-01. REPAIRED FUSELAGE SKIN PER SRM 53-20-00, FIG 6, SHT 3. REINSTALLED REMOVED DOUBLER PER DWG SR10530038-11 AND GN 17-18. 2L73 4F A22WE 20050526002772005052600277WP 2005 5 26 05FDEA01396 120050521A5512ALC7227501 PANEL DOUG DC10 DC1010 3022110WP ZONE 300 DAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25571FE 47830 HORIZONTAL STABILIZER, UPPER CONSTANT SECTION, WITH PLANK NR 15 WITH CRACK (0,51" LENGTH), P/N ALC7227-1. REMOVED OLD PANEL ALC7228-1 PER SB 55-16. REMOVED PANEL ALC7227-1 PER SB 55-16. REWORKED ALC7227-1 NEW PANEL PER SB 55-16. INSTALLED NEW PANEL ALC7227-1 PER SB 55-16. 2L73 4F A22WE 20050526002782005052600278WP 2005 5 26 05FDEA01397 120050521A5512ALC7228501 PANEL DOUG DC10 DC1010 3022110WP FUSELAGE DAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25571FE 47830 HORIZONTAL STABILIZER, UPPER CONSTANT SECTION, WITH PLANK NR 11 WITH CRACK ( 0,75" LENGTH), P/N ALC7228-. REMOVED ALC7228-1 OLD PANEL PER SB 55-16 FIG 4 GR 2. REWORKED NEW PANEL PER SB 55-16 FIG 4 GR 2. INSTALLED NEW PANEL PER SB 55-16 FIG 4 GR 2. 2L73 4F A22WE 20050531000012005053100001NM 2005 5 31 05FDEA01260 120050512A532069648411 ANGLE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25254FE 20936 STA 740 STR 27R CORROSION FOUND ON LOWER LEG OF ANGLE. REMOVED AND REPLACED ANGLE IAW EA 7-5310-55482 ON N/R CARD S00011. 2L73 4F RTA3WE 20050606000932005060600093EU 2005 6 6 BA05010 120050518A3350321431 BATTERY AIRBUS330 A330323 3930335EU EMERGENCY LIGHT DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19677UW 388 BATTERY PACKS AT DOORS 2R, 2L AND 3R FAILED THE CAPACITY CHECK. MAINTENANCE REPLACED THE BATTERIES. 2L72 4F RTA46NM 20050531000022005053100002NM 2005 5 31 05FDEA01262 120050512A5754 SKIN DOUG MD11 MD11 3023602NM L/E SLAT DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE RIGHT WIN , DROOP LEADING EDGE, TOP SURFACE, FOUND WITH A EXISTING REPAIR DOUBLER AND EXISTING FASTENERS HEAD EMITTING RUST. REPAIRED IAW SRM 57-10-00 FIG. 26 VOL I. 2L73 4F RTA22WE 20050525000732005052500073NM 2005 5 25 QXEA200500841 120050508A2720 PRESSURE SWITCH DHAV DHC8 DHC8202 2809007NM RUDDER MALFUNCTIONED A QXEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM09361PH 516 SEA FLIGHT NR 2269, UPON APPLICATION OF TAKEOFF POWER, RUDDER FULL PRESSURE CAUITON LIGHT ILLUMIANTED. ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE REPLACED NR 1 AND NR 2 RUDDER FULL PRESSURE SWITCHES IAW MCN 22788-001. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050525000762005052500076NM 2005 5 25 AALA20050300 120050503A3350A3060698101 CONNECTOR BOEING757 757231 1384950NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21717TW 28485 MCO EGRESS LIGHT AT ROW 31 AFT INOPERATIVE. SPLICED WIRING FOR CONNECTOR FOR EGRESS LIGHT AT ROW 31 AFT. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA2NM 20050525000852005052500085NM 2005 5 25 AALA20050310 120050503A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21966AN 30094 TUL - TWO EMERGENCY EXIT LIGHT BATTERY PACKS AT CABIN SIDEWALL DOES NOT HOLD CHARGE. REPLACED BATTERY PACKS AT CABIN SIDEWALL FOR EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA16WE 20050525000982005052500098NM 2005 5 25 AMTA200500420 120050505A5312 SHIM BOEING757 75723N 1384973NM RROYCERB211 RB211* 54555NE BULKHEAD MIGRATED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11519AT 27975 ATTACH FITTING, HORIZONTAL STABILIZER LT PIVOT FITTING HAS MIGRATING SHIMS AT ATTACHMENT TO BS 1862.7 BULKHEAD - 3 LOCATIONS. COMPLIED WITH PART 1: TIME LIMITED REPAIR OF ERA NR 757-53R-58-73IR. (K) 2L72 4F4 FRTA2NM A12EU 20050606000082005060600008WP 2005 6 6 UPS05844484 120050503A5712 RIB DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE: C3, LT WING L/E UPPER RIB CRACKED .25 INCH LONG AT XFS 809. STOP DRILLED CRACK AND FABRICATED INSTALLED REPAIR ANGLE IAW SRM 57-2-0, 51-1-21 AND 51-1-20D. 2L74 4F RT4A25 20050525001092005052500109SO 2005 5 25 CHQA200500095 120050506A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11270SK 145304 EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED EMERGENCY EXTERIOR EXIT LIGHT BULB IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050525001102005052500110NE 2005 5 25 PCS2005F00002 220050219A7261P79518 O-RING PWA BOEING727 7272F9 138407DNM PWA JT8 JT8D17 52049NE FUEL PUMP SHAFT LEAKING A PCSAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO29199AJ GT4640 21426 CREW REPORTED NR2 ENG OIL QUANTITY DROPPED IN FLIGHT, THEN ENGINE OIL PRESSURE DROPPED, THEN OIL TEMP ROSE. CREW SHUTDOWN NR2 ENGINE AND AC RETURNED TO DEPARTURE, AC LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND NR2 ENGINE GEARBOX LEAKING OIL FROM THE FUEL PUMP SHAFT. MAINTENANCE REMOVED AND REPLACED THE O-RING ON THE FUEL PUMP TO THE GEARBOX AND REPLACED THE CARBON SEAL ON THE NR2 ENGINE GEARBOX IAW MM. MAINTENANCE INSP NR 2 ENGINE OIL FILTER FOR CONTAMINANTS, NONE FOUND, OIL SAMPLE TAKEN, SAMPLE SENT OUT FOR SOAP TEST. NR2 ENG LEAK CHECK WAS PERFORMED IAW MM. NO OIL LEAKS NOTED LEAK CK GOOD. AC FLEW NEXT FLIGHT WITH NO FURTHER ENGINE OIL QUANTITY PROBLEMS REPORTED. (K) 2L73 4F4 FRTA3WE E2EA 20050525001112005052500111CE 2005 5 25 FFS2005F00003 120050502A53471144300743 SEAT TRACK BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA CORRODED A FFSAK NONE O OTHER ININSP/MAINT 1 AL01575F UC99 THE LT FORWARD SEAT TRACK WAS CORRODED THROUGH THE SIDE OF THE TRACK AND THE TRACK AND THE FLANGE THAT SUPPORTS THE FLOORBOARD. CORROSION WAS PARTICULARLY EVIDENT AT FUSELAGE STA 158.5 - 170.5. THE LOCATION OF THE CORROSION, JUST INSIDE THE AIRSTAIR DOOR, SUGGESTS THAT IT MAY BE THE RESULT OF MOISTURE AND ICE-MELT PRODUCTS (SALT) CARRIED INTO THE CABIN ON PASSENGERS FOOTWEAR. (K) 2L72 4T4 TRTA24CE E4EA 20050525001182005052500118CE 2005 5 25 SFO2005F00000 120050414A57110024300185 SPAR BEECH 58 58 1152740CE CONT O520 IO520* 17032SO CARRY-THRU CRACKED E SFOAK NONE O OTHER ININSP/MAINT 1 EA2337SF 12474 TH627 DURING ANNUAL INSP, CRACKS WERE NOTED IN FWD CARRY-THRU SPAR WEB. LOCATED AT LT UPPER OB MOST HUCK BOLTS (2 EA) ON FWD SIDE OF CARRY-THRU ASSY. HEAD SIDE OF UPPER HUCK BOLT IS INACCESSIBLE FOR VIEWING WITHOUT WING REMOVAL. LWR HUCK BOLT IS ACCESSIBLE, NO MOVEMENT OR CRACKING WAS NOTED. WEB SKIN AROUND HUCK BOLTS WAS REMOVED DOWN TO WEB TIE PLATE. PLATE WAS EDDY CURRENT INSPECTED FOR CRACKS, NONE WERE DETECTED. THIS AREA WILL BE REINSPECTED BY DYE PENETRANT EVER ANNUAL INSP, AND BY EDDY CURRENT METHOD EVERY 500 HRS. THIS AC HAS 2 BOLT AREAS CRACKED ON ONE SIDE, REQUIRED REPAIR DOES NOT EXTEND INTO THIS AREA. THE HIGH AC TIME AND DAMAGE HISTORY WERE CONTRIBUTING FACTORS TO THE CRACKING IN THIS AREA. 1L72 3O3 O 3A16 E5CE 20050525001192005052500119SO 2005 5 25 XGN2005F00001 220050504A8530TISN712BCA CYLINDER HEAD CESSNA402 402B 207590PCE CONT O520 TSIO520E 17040SO NR 2 CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW054165G 402B1212 502537 THIS CYLINDER WAS INSTALLED AS A SERVICEABLE CYLINDER 135.5 HOURS AGO. THE CRACK WAS FOUND DURING A 100 HR INSPECTION COMPRESSION CHECK. (K) 1L72 3O3 O A7CE E8CE 20050525001482005052500148NM 2005 5 25 USAA050491 120050317A5320140T25409 INTERCOSTAL BOEING767 767201 1385125NM FUSLEAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19648US68950 23900 BFM - FOUND INTERCOSTAL WITH 3 CRACKS TOTAL LENGTH APPROX 1 INCH, BS 1241-1263 AT LBL 39. INSTALLED NEWLY FABRICATED REPLACEMENT PART PER SRM 51-10-02, 51-20-01, 51-40-02 AND EA 96331. (M) 2L72 4F RTA1NM 20050525001682005052500168NM 2005 5 25 USAA050510 120050416A5740 SUPPORT FITTING BOEING737 7374B7 1384702NM RT WING CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19440US39307 24811 CLT - FOUND SUPPORT FITTING CRACKED .3750 INCH, RT AFT SPAR WBL 142. REPLACED FITTING IAW EO 5702V054. (M) 2L72 4F RTA16WE 20050525001732005052500173SO 2005 5 25 CHQA200500096 120050510A33501317 BULB EMB 145 EMB145MP 3260216SO EMERGENCY LIGHT BURNED OUT A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11973RP 145444 LEFT HAND EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED LEFT AFT EMERGENCY EXIT LAMP IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD. LEFT OVERWING EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED LEFT OVERWING EMERGENCY EXIT LIGHT BULB. OPS CHECK GOOD IAW EMB 145 AMM 33-44-02. 2L72 4F RTT00011AT 20050525001842005052500184NM 2005 5 25 DHL2005740507 120050329A5531 STRINGER BOEING727 7272Q9 138448MNM VERTICAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 VERT STAB FIN STA 180 STRINGER S-8 LT IS CRACKED AT FRAME ATTACH SCREW. REMOVED FASTENERS FOR ACCESS AT VERT STAB FIN STA 180 S-8 LT AND TRIMMED OUT DAMAGED AREA SIZE 3 1/2 INCH BY 3 INCH IAW B727 SRM 55-30-4 FIG1. FABRICATED REPAIR PARTS P/N BAC 1517-1367 7075-T6511 SIZE 3 1/2" BY 3" PO NR 501953 SPLICE P/N AND10134 -1201 7075-T6511 PO NR501952 SIZE 17 1/2" BY 2" FILLER P/N 7075-T6 .100 SIZE 19 1/2" BY 1/2" PO#9001777 SPLICE P/N AND 10133 -1401 7075-T6511 SIZE 17 1/2" BY 2" PO#501952 IAW B727 SRM 55-30-4 FIG 1. TREATED AND PRIMED PARTS AND AREA IAW B727 SRM 51-10-2. INSTALLED STRINGER REPAIR AT VERT STAB STA 180 S-8 LT IAW B727 SRM 55-30-4 FIG 1 SRM 51-30-2. 2L73 4F RTA3WE 20050525001892005052500189EA 2005 5 25 MASA200500316 120050425A3030 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA PITOT HEAT ILLUMINATED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07650ML 7137 ASH 2940 PHL. THE AIRCRAFT RETURNED TO THE FIELD DUE TO PITOT BASE HEAT CAUTION MESSAGE. MAINTENANCE REMOVED AND REPLACED THE P/B HEAT SPLICE. 2L72 4F RTA21EA 20050525001922005052500192EA 2005 5 25 MASA200500321 120050428A5320 BRACKET CNDAIRCL600 CL6002B19 1900309EA DOOR FRAME BROKEN A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0775998 7336 ASH 7100 ATL TO IAD. THE CREW WROTE UP THE DOOR FRAME BRACKET BEING BROKEN ON MAIN PAX DOOR. THE AIRCRAFT WAS FERRIED TO IAD WHERE MAINTENANCE REMOVED AND REPLACED THE SWIVEL ARM BRACKET. 2L72 4F RTA21EA 20050525002082005052500208NM 2005 5 25 DLM88050217 120050411A291659369865501 RESERVOIR DOUG MD88 MD88 3023688NM HYD SYSTEM FAILED A DALAA UNSCHED LANDING KG FLUID LOSS MULTIPLE FAILURE DEDESCENT 1 SO27921DL 49645 EN ROUTE TO SAT FROM CVG AIRCRAFT SUFFERED COMPLETE HYDRAULIC PRESSURE LOSS ON BOTH SYSTEMS. FLIGHT DIVERTED TO AUS AND LANDED UNEVENTFULLY. REPLACED RT ENGINE DRIVEN PUMP AND BOTH RESERVOIRS. 2L72 4F RTA6WE 20050525002102005052500210NM 2005 5 25 DL75K050219 120050413A2121216001013 FAN BOEING757 757232 1384965NM E&E BAY FAILED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO276710E 30482 COCKPIT EXPERIENCED SMELL OF SMOKE ON FINAL. ON ROLLOUT EQUIPMENT OVERHEAT LIGHT AND EICAS MSG ILLUMINATED. REPLACED FWD EQUIPMENT COOLING FAN. 2L72 4F RTA2NM 20050525002112005052500211NM 2005 5 25 DL757050220 120050414A563065457914AR WINDOW BOEING757 757232 1384965NM ROW 25 SEAT F FAILED A DALAO OTHER D INFLIGHT SEPARATION CRCRUISE 1 SO27681DA 26957 CABIN WINDOW AT ROW 25F OUTER PANE BROKE AWAY IN FLIGHT. REPLACED SAME. 2L72 4F RTA2NM 20050525002342005052500234 2005 5 25 DXTA200500734 420050521A2210 WIRE BRAERO1000 HAWKER1000 7450005EU ANNUNCIATOR BROKEN E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07549QS 259049 AFTER TAKEOFF, THE MACH TRIM YAW DAMPER AND AUTO-PILOT WOULD NOT ENGAGE ON THE FGC PANEL. REPAIRED BROKEN WIRES AT LAFGS ANNUNCIATOR TRANSFER BUTTON. CLEANED BUTTON CONTACTS IAW ARKANSAS AERO DWG A1-44-001 REV B AND A1-44-003 REV B. OPERATIONAL CHECK SATISFACTORY. 2L72 4F RTA3EU 20050525002352005052500235 2005 5 25 SA05053 420050519A2565 LINE AIRBUS320 A320214 3930316EU ESCAPE SLIDE MISROUTED A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19105UW 868 PIT - MAINTENANCE FOUND THE FORWARD, RIGHT SIDE, DOOR EMERGENCY ESCAPE SLIDE ASSEMBLY MOORING LINE INCORRECTLY ROUTED. MAINTENANCE CORRECTLY ROUTED THE MOORING LINE. OK FOR SERVICE. 2L72 4F RTA28NM 20050526000052005052600005NM 2005 5 26 DL76S050242 120050328A3397 WIRE HARNESS BOEING767 767332 1382001NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27134DL 25123 SEAT 30FG EMERGENCY LIGHT INOP AND LENS MISSING. REPLACED WIRE HARNESS AT SEAT 30FG AND INSTALLED NEW LENS COVER. CHECKS GOOD. 2L72 4F RTA1NM 20050526000362005052600036SO 2005 5 26 SIMA200510802 120050406A532014525480003 SILL EMB 135 EMB135KL 3260302SO CARGO BAY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21803AE 145483 ABI - THE CARGO DOOR OPENING LOWER SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED LOWER DOOR SILL. INSTALLED NEW SILL IAW EMB SRM, SRM 145.1142 REV 28, CHAPTER 51-40-02 AND 51-20-03. (M) 2L72 4F RTT00011AT 20050526000392005052600039NM 2005 5 26 USAA050527 120050331A531220240040 ACCESS PANEL BOEING737 7373B7 1384580NM RT MLG WW CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19374US56183 22953 BFM - FOUND ACCESS PANEL CRACKED AND CORRODED 1.5 INCH CRACK, 3 INCH CORROSION .050 DEEP, RIGHT W/W LOWER PANEL. FABRICATED NEW PART PER 51-40-02. (M) 2L72 4F RTA16WE 20050526000422005052600042SO 2005 5 26 SIMA200511201 120050413A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21850AE 145722 THE RIGHT OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND TO BE CORRODED. BLENDED THE DAMAGED AREA TO REMOVE THE CORROSION. FABRICATED A DOUBLER FROM REPAIR. REPAIR DONE IAW EMB REPAIR STATEMENT IC2005-145/1917 PARA 2 DATED APRIL 13, 2005. (M) 2L72 4F RTT00011AT 20050526000432005052600043NM 2005 5 26 USAA050516 120050421A5315 FLOORBEAM BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US39931 24781 CLT - FOUND FLOORBEAM UP CHORD 1 INCH BY 1 INCH, STATION 986 RBL 8 TO RBL 38. REPLACED UPPER CHORD IAW TR 53-60-01. (M) 2L72 4F RTA16WE 20050526000442005052600044NM 2005 5 26 USAA050517 120050421A5414 DOUBLER BOEING737 737401 1384701NM LT PYLON CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19422US45217 23989 CLT - FOUND SKIN DOUBLER CRACKED .250 INCH, LEFT PYLON AT PANEL 5738L. STOP DRILLED AND ROUTED OUT DAMAGE PER TR 54-30-07 AND EA 96511. (M) 2L72 4F RTA16WE 20050526000452005052600045NM 2005 5 26 USAA050524 120050407A5320BAC1509100146 CHANNEL BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19374US56183 22953 BFM - FOUND FLOOR SUPPORT CHANNEL CORRODED 2 INCHES LONG BY .90 INCHES WIDE BY .030 INCHES DEEP, AFT CARGO BS 704 RBL 8.10. INSTALLED REPAIR ANGLE PER TYPICAL REPAIR 53-10-06B. (M) 2L72 4F RTA16WE 20050526000512005052600051NM 2005 5 26 USAA050536 120050408A5320 STIFFENER BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19374US56183 22953 BFM - FOUND STIFFENER EXFOLIATED AND CORRODED CHORD, BS 290-303, LBL 11.10 FLOOR SUPPORTS WL 208. INSTALLED FABRICATED PARTS PER SRM 53-10-51, 51-40-02. (M) 2L72 4F RTA16WE 20050526000532005052600053NM 2005 5 26 USAA050530 120050330A5420313A1380108 PLATE BOEING737 7373B7 1384580NM FAIRING CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19374US56183 22953 BFM - FOUND PANEL FLANGE PLATE CORRODED 4 INCHES LONG BY 2.5 INCHES WIDE BY .05 INCH DEEP, NR 1 PYLON MID FAIRING PANEL FLANGE PLATE. INSTALLED REPAIR SPLICE PLATE PER SRM 54-50-70 AND BOEING DWG 313A1380. (M) 2L72 4F RTA16WE 20050526000572005052600057EU 2005 5 26 USAA050521 120050416A5347D53111461202 SEAT TRACK AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19714US17533 1046 PIT - FOUND SEAT TRACK CORRODED, RT INBOARD SEAT TRACK AT FRAME 20. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-72-11. CORROSION LEVEL 1, TASK JA-220-53500. (M) 2L72 4F RTA28NM 20050526000582005052600058NM 2005 5 26 USAA050542 120050412A5315 FLOORBEAM BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19374US56183 22953 BFM - FOUND FLOORBEAM CORRODED 3 INCHES LONG BY 1 INCH WIDE BY .055 INCH DEEP AND 3 INCHES LONG BY 1 INCH WIDE BY .043 INCH DEEP, AFT CARGO FLOOR LBL 12.5 AND RBL 3. FABRICATED REPAIR ANGLES AND INSTALLED PER TYP REPAIR 53-10-06B. CORROSION LEVEL 1, TASK C53-202-01. (M) 2L72 4F RTA16WE 20050526000612005052600061NM 2005 5 26 USAA050539 120050415A5343 SLEEVE BOEING737 7373B7 1384580NM RT MLG CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19374US56184 22953 BFM - FOUND SUPPORT SLEEVE CHAFED MARK .086 WEAR, RT MLG FORWARD TRUNNION BEARING SUPPORT FITTING. REMOVED AND REPLACED FORWARD TRUNNION SUPPORT SLEEVE PER TYPICAL REPAIR 57-20-04. (M) 2L72 4F RTA16WE 20050526000762005052600076EU 2005 5 26 AWXA200500549 120050404A5347D53371110010 SEAT TRACK AIRBUS320 A320232 3930326EU FSUELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28638AW 455 SAL - MAJOR REPAIR - DURING C-08 CHECK GALVANIC CORROSION WAS FOUND ON RT INBOARD SEAT TRACK -Y765 AT FR 42+17 INCH. MAINTENANCE REMOVED CORRODED SEAT TRACK -Y765 AT FR 42+17 INCH; ORDERED, RECEIVED, AND INSTALLED A NEW REPLACEMENT SECTION OF SEAT TRACK IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050526001032005052600103NM 2005 5 26 SWAA051366 120050510A335065C27093 LIGHT BOEING737 7377H4 1384404NM R2 DOOR BROKEN A SWAAO OTHER O OTHER NRNOT REPORTED 1 SW29482WN 29852 R2 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20050526001102005052600110NM 2005 5 26 SWAA051356 120050508A26972615000103 WIRE HARNESS BOEING737 7373H4 1384600NM APU BAY FAULTY A SWAAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 SW29324SW 23414 DIVERSION, APU FIRE WARNING LIGHT ILLUMINATED IN FLT. APU FIRE BOTTLE DISCHARGED. APU FIRE WARNING LIGHT STILL ILLUMINATED MULTIPLE TIMES AFTER BOTTLE DISCHARGED. FOUND APU AFT TAILPIPE HARNESS CONNECTORS GROUNDING OUT THRU CERAMIC. REMOVED AND REPLACED APU AFT TAILPIPE HARNESS PER MM. 2L72 4F RTA16WE 20050526001142005052600114NM 2005 5 26 SWAA051360 120050509A335010107451 SIGN BOEING737 7377H4 1384404NM MID CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29731SA 27863 RIGHT OVERWING EMERGENCY EXIT SIGN MISSING. INSTALLED SIGN PER MM. 2L72 4F RTA16WE 20050526001332005052600133EA 2005 5 26 SWIA200514975 120050509A27604916420 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07986SW 7967 FLT SPLRS FAULT, I/B AND O/B GND SPLR FAULT MESSAGES. REPLACED NR 1 SECU. OPERATIONAL CHECK GOOD IAW MM 27-61-00. 2L72 4F RTA21EA 20050526001342005052600134EA 2005 5 26 SWIA200514976 120050429A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07961SW 7857 FS 280 LBL 9.0 OUTBOARD FLOORBEAM ATTACH ANGLE IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-21-11, 51-25-16, 51-23-00. 2L72 4F RTA21EA 20050526001412005052600141EA 2005 5 26 SWIA200514983 120050508A27604916406 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07946SW 7776 BOTH SPOILERONS AND BOTH INBOARD AND OUTBOARD GROUND SPOILERS SHOW STATUS. REPLACED NR 1 SECU IAW MM 27-61-65. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050526001432005052600143SO 2005 5 26 SWIA200514985 120050502A27503472001001 CONTROL UNIT EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07215SW9582 9582 120281 FLAP CONTROL FAULT ON OUTBOARD FLAPS. REPLACED FLAP CONTROL LEVER & FCU IAW MM 27-50-06 & 27-50-01. OPERATIONAL CHECKS GOOD. P/N 120-64207-615; S/N OFF 120278. 2L72 4T RTA31SO 20050526001522005052600152SO 2005 5 26 C2XA05SH030 120050512A532014530644403 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2748901 145501 SHV - DURING C-CHECK THE LT OMEGA BEAM HAS CORROSION ALONG THE SIDE FR 36 TO 52. MAINTENANCE REMOVED THE DAMAGE AREA AND PERFORMED REPAIR LT OMEGA BEAM AT FR 44 IAW EC 5320-01238. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050526001622005052600162NM 2005 5 26 SWAA051373 120050511A5340BAC1503100046 SUPPORT ANGLE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29352SW 24888 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE WEB SUPPORT ANGLE CRACKED AT R1 DOOR CUTOUT, BS 287, STR 9R. REMOVED AND REPLACED ANGLE PER SRM. 2L72 4F RTA16WE 20050526001642005052600164NM 2005 5 26 SWAA051375 120050511A27406549568 PULLEY BOEING737 7377H4 1384404NM HORIZONTAL STAB WORN A SWAAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SW29483WN 32472 AIR TURNBACK. POPPING NOISE/METALIC SOUND HEARD IN FLOOR NEAR L1 DOOR. INSPECTED FWD E & E COMPARTMENT & FOUND BOTH HORIZONTAL STAB TRIM CABLE PULLEYS WORN. REMOVED AND REPLACED BOTH PULLEYS PER MM. 2L72 4F RTA16WE 20050526001672005052600167NM 2005 5 26 SWAA051378 120050511A57536573731 SKIN BOEING737 7373T5 1384608NM LT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29696SW 23064 DURING SCHEDULED C4 CHECK, FOUND LT WING INBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2L72 4F RTA16WE 20050526001692005052600169NM 2005 5 26 SWAA051380 120050511A53126545819 ACCESS PANEL BOEING737 7373H4 1384600NM NLG WW CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED SERVICE CHECK, FOUND 4 EA CRACKS BELOW NLG W/W FWD ACCESS PANELS, LT & RT SIDE, BS 236 TO BS 243 + 1. REPAIRED WEB PER SWA EA. 2L72 4F RTA16WE 20050526001722005052600172NM 2005 5 26 SWAA051383 120050511A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 26R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050526001742005052600174SO 2005 5 26 MASA200500312 120050423A3350 SIGN EMB 145 EMB145LR 3260212SO EMERGENCY EXIT LOOSE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07847MJ 145517 ASH 2686 CLT TO GSO - THE CREW NOTED THAT THE OVERWING CEILING EMERGENCY EXIT SIGN WAS INTERMITTENT DURING TEST. MAINTENANCE RE-SECURED THE SIGN ASSEMBLY AND IT OPERATED NORMALLY. THE AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. 2L72 4T RTT00011AT 20050526001762005052600176SO 2005 5 26 MASA200500323 120050429A3350B6245 LIGHT EMB 145 EMB145LR 3260212SO PAX DOOR INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07838MJ 145384 THE PASSENGER DOOR EMERGENCY LIGHT WAS INOP. MAINTENANCE RELAMPED. 2L72 4T RTT00011AT 20050526001842005052600184SO 2005 5 26 MASA200500302 120050418A3350 SIGN EMB 145 EMB145LR 3260212SO EMERGENCY EXIT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07840MJ 145429 ASH 2824 FROM XNA TO CLT, THE CREW NOTED THE PASSENGER DOOR EMERGENCY EXIT SIGN INOP. THE AIRCRAFT WAS FERRIED TO CLT AND MAINTENANCE REPLACED THE INVERTER AND THE SIGN OPERATED NORMALLY. THE AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. 2L72 4T RTT00011AT 20050526001922005052600192NM 2005 5 26 AWXA200500551 120050501A57536546430129 SKIN BOEING737 7373G7 1384595NM LT FORE FLAP DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28322AW 25400 MCN - MAJOR REPAIR - DURING C-14 CHECK THE UPPER SURFACE SKIN OF THE LT INBOARD FORE FLAP WAS FOUND DELAMINATED BETWEEN WBL 136 AND WBL 154. MAINTENANCE CUTOUT DAMAGE IN UPPER SURFACE SKIN OF THE LT INBOARD FORE FLAP FROM WBL 141.274 TO 154.275; FABRICATED A CORE FILLER AND DOUBLER; BONDED REPAIR PARTS TO FLAP IAW B737-300 SRM 51-70-10. 2L72 4F RTA16WE 20050526001962005052600196NM 2005 5 26 AWXA200500555 120050504A5320655287855 ANGLE BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28322AW 25400 MCN - MAJOR REPAIR - DURING C-14 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF L-2 INNER CHORD LOWER STIFFENER AT BS 980, LBL 44, WL 207.5. MAINTENANCE REMOVED CORRODED STIFFENER AT BS 980, LBL 44; RECEIVED NEW REPLACEMENT STIFFENER AND DRILLED IT TO SPECIFICATION OF DWG 65-52878; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050526002022005052600202WP 2005 5 26 UPS05844439 120050425A53403779762U501 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE:C1 LONGERON END FITTING CRACKED AT STA 673 L8L. REMOVED AND REPLACED LONGERON END FITTING IAW DC-8 SRM 51-1-20D AND 51 -1-21. 2L74 4F RT4A25 20050526002262005052600226NE 2005 5 26 MWEA050042 220050512A73218061965 FMU BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE ENGINE INOPERATIVE A MWEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL31920ME 55182 LEFT ENGINE PARAMETER N1 AND N2 ENGINE PRESSURE RATIO BEGAN FLUCUATING. PERFORMED FAULT REVIEW. FAULTS 732132. INSPECTED AND CHANGED LEFT ENGINE LOW AND HIGH PRESSURE FUEL FILTERS, NO CONTAMINATION. REMOVED AND REPLACED LEFT ENGINE FUEL METERING UNIT. 2L72 4F4 FTRA6WE E00061EN 20050526002312005052600231CE 2005 5 26 CIEA200500001 120050512A3397 CONNECTOR BEECH 200 B200 1152922CE INSTRUMENT PANELBENT E CIEAA UNSCHED LANDING O OTHER CLCLIMB 1 NM035ST 7435 BB926 SHORTLY AFTER TAKEOFF, THE ENGINE INSTRUMENT AND AUDIO PANEL CIRCUIT BREAKER POPPED. THE AIRCRAFT WAS FLYING AT NIGHT. THE AIRCRAFT RETURNED TO THE AIRPORT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A STUD FOR THE LIGHT PANEL ON THE AVIONICS OVERLAY TO BE BENT AND CONTACTING THE FRAME. THE PIN WAS STRAIGHTENED AND POSITIONED AND PROTECTED TO ELIMINATE THE SHORTING CONDITION. THE PI WAS MOST LIKELY BENT WHILE MOVING THE AVIONICS PANEL IN AND OUT OF THE AIRCRAFT AND DUE TO VIBRATION FINALLY CAME INTO CONTACT WITH THE FRAME. 1L72 4T A24CE 20050526002412005052600241NM 2005 5 26 MWEA050043 120050512A5350 SKIN BOEING717 717200 1383700NM TAILCONE LIGHTNING STRIKEA MWEAA UNSCHED LANDING O OTHER CLCLIMB 1 GL31910ME 55174 LIGHTNING STRIKE DAMAGE TO TAILCONE BOTTOM RIGHT EDGE. NO OTHER INFORMATION AT THIS TIME WAITING FOR FIX. 2L72 4F TRA6WE 20050526002422005052600242WP 2005 5 26 05FDEA01229 120050510A7110 DOOR DOUG MD10 MD1010F 3022112WP NR 2 NACELLE MISSING A FDEAO OTHER D INFLIGHT SEPARATION CLCLIMB 1 SO25372FE 46610 PORTION OF NR 2 ENG FAN COWLING MISSING. CENTER ADVISED METAL WAS FOUND ON DEPARTURE PATH FROM OAK. PASSING 15,000 FEET THE A/C WAS JOLTED BUT NO OTHER INDICATIONS WERE NOTED. INSTALLED LEFT HAND FAN COWL FWD, CTR AND AFT HINGE BRACKETS. INSTALLED LEFT HAND FAN COWL. REFERENCE DWG AVB7050 AND EA 8-5410-89203. SECURED AND CLOSED FAN COWL AND PATIO. RETURNED TO SERVICE. 2L73 4F RTA22WE 20050526002452005052600245NM 2005 5 26 05FDEA01231 120050510A532069656452 CLIP BOEING727 727200 138407ENM RT MLG WW CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25254FE 20936 RT MLG WHEEL WELL ABOVE UPLOCK MECHANISM WEB UPPER SURFACE BETWEEN STA 930 - 940 SURFACE CORROSION. REMOVED AND REPLACED CLIP IAW SRM 51-30-2. 2L73 4F RTA3WE 20050526002542005052600254EU 2005 5 26 05FDEA01240 120050512A5322 SHEAR TIE AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25403FE 230 UNDER FLOOR AREA BAY BEHIND FWD PIT FR 38.2 SHEAR TIE BETWEEN STG 49R AND 50R HAS CORROSION ON ALL OF SURFACE EXTENDING AROUND AND UNDER FASTENERS FOUND WHILE CLEANING FOR CIC APPLICATION. REMOVED CORROSION ON SHEAR TIE, AFTER BLENDING PART WENT OUT OF LIMITS IAW A310-200 SRM 53-10-00 AND CORROSION REMOVAL IAW A310-200 SRM 51-74-10. REPLACED WITH NEW SHEAR TIE IAW A310-200 SRM 51-72-10 AND 51-40-21. RESTORED PROTECTIVE COATING IAW A310-200 SRM 51-75-10 AND 51-23-10. INSTALLED SOLID RIVETS 5 EA IAW A310-200 SRM 51-40-21. 2L72 4F RTA35EU 20050526002622005052600262EU 2005 5 26 05FDEA01248 120050512A5753 FLAP TRACK AIRBUS310 A310203 3930313EU RT WING GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25403FE 230 RIGHT WING NR 5 FLAP TRACK OUTBOARD ROLLER TRACK HAS GOUGES IN BEND RADIUS OF TRACK. COMPLIED WITH EA 6-5720-88814 PT 1 AND RAS/DABRE/7005151/2005. 2L72 4F RTA35EU 20050526002642005052600264EU 2005 5 26 05FDEA01250 120050512A5320A255738070000 ANGLE AIRBUS310 A310203 3930313EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25403FE 230 AFT CARGO FORWARD LWR SLANT PANEL HAS CORROSION AROUND NUT PLATES ON LANDING AT STA 3196, BETWEEN FRAMES 59-60, JUST FWD BY DOOR FRAME. REMOVED CORROSION IAW A310-200 SRM 51-74-10. ANGLE OUT OF LIMITS IAW A310-200 SRM 53-10-12. REPLACED ANGLE IAW A310-200 SRM 51-72-10. TREATED AND PRIMED BARE METAL IAW A310-200 SRM 51-74-10. 2L72 4F RTA35EU 20050526002732005052600273NM 2005 5 26 05FDEA01269 120050513A5347ACA73995017 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25621FE 48792 MAIN DECK, SEAT TRACK LBL 47 CRACKED AT STA 755. CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I FIGURE 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050608000672005060800067EU 2005 6 8 MALA050432 120050521A2612 FIRE LOOP SAAB SF340 340B 7860101EU ENGINE MALFUNCTIONED A MALAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 GL15435XJ 340B435 CREW SHUT DOWN AN ENGINE FOLLOWING ANNUNCIATION OF ENGINE FIRE WARNING SYSTEM DURING FLIGHT. ENGINE FIRE BOTTLE WAS DISCHARGED FOLLOWED BY UNEVENTFUL LANDING. AIRCRAFT TOWED TO GATE. MAINT FOUND THERE WAS NO INDICATION OF UNCONTAINED FIRE OR NON-NORMAL COMBUSTION WITHIN THE ENGINE. FOUND A BROKEN WELD ON THE JET PIPE, ALSO KNOWN AS THE INDUCTOR SHROUD, THAT CHANNELS EXHAUST GASES OUT OF ENGINE. THE ENGINE FIRE SENSOR (ONE OF WHICH IS NEAR THE BROKEN WELD) PICKED UP THE HOT (700+C) EXHAUST AIR TEMPS & INDICATED A FIRE. THE ONLY REMNANTS OF SOOT THAT WERE FIRST DISCOVERED INSIDE ENGINE COWLING CAME FROM INDUCTOR BREAK THAT ALLOWED THAT EXHAUST AIR TO CIRCULATE IN AREAS IT NORMALLY CAN NOT GO. 2L72 4T RTA52EU 20050531000042005053100004NM 2005 5 31 05FDEA01270 120050513A3297 WIRE BOEING727 72722 1384002NM LANDING GEAR BROKEN A FDEAK NONE J WARNING INDICATION APAPPROACH 1 SO25185FE 18871 EXTENDING GEAR, DID NOT GET RIGHT MAIN GEAR GREEN LIGHT. TAIL SKID LIGHT ON S/O PANEL WAS ALSO ILLUMINATED. CHECKLIST LEAD US TO TEST GREEN LIGHT, LIGHT WAS WORKING. CB PRESS TO TEST AND LIGHTS WERE RESET PER CHECKLIST. VERIFIED RIGHT MAIN DOWN WITH MANUAL GEAR EXTENSION GREEN MARKER. LANDED UNEVENTFULLY. REPLACED SW S98 RT MAIN DOWNLOCK PER MM 32-61-021-4 AND FOUND BROKEN WIRE IN PIN 3 OF BULKHEAD PLUG D302. OPS CHECKS OK PER MM 32-61-021-5. 2L73 4F A3WE 20050531000052005053100005SO 2005 5 31 C2XA05TY042 120050513A553414520735003 HOUSING EMB 145 EMB145LR 3260212SO VERTICAL STAB WORN A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714902 145496 TYS - DURING A SCHEDULED INSPECTION THE LEFT VERTICAL STAB SPHERICAL BEARING HAS PLAY. MAINTENANCE REPAIRED THE SPHERICAL BEARING HOUSING IAW EMB-145 AMM 55-10-00 AND EC5510-01116. 2L72 4T RTT00011AT 20050531000092005053100009SO 2005 5 31 C2XA05SH036 120050516A532014521713003 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714938 145029 SHV - DURING C-CHECK THE RT OMEGA BEAM HAS CORROSION AROUND NUT PLATE AT FRAME 23. REPAIRED CORROSION ON RT OMEGA BEAM AROUND NUT PLATE AT FRAME 23 WITH INSTALLATION OF NEW OMEGA BEAM AT FRAME 23 IAW EMB 145 SRM 51-40-02 WITH NUT PLATE INSTALLATION PER EC 5320-01137. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050531000112005053100011NM 2005 5 31 DHL2005740510 120050320A5752 STRUCTURE BOEING727 7272Q9 138448MNM AILERON TAB DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 CUT OUT DELAMINATED AREA AT RT WING OUTBOARD AILERON TAB APPROX 1 X 1 INCH, FABRICATED FILLER APPROX 1 X 1 X 1 INCH AND DOUBLER APPROX 2.5 X 3 INCH FROM .010 INCH 2024T3 PO9912184 BONDED FILLER AND DOUBLER, CURED, CLEANED, PRIMED AND SEALED IAW B727 SRM 57-50-2 AND 51-40-20 FIG 30. 2L73 4F RTA3WE 20050531000132005053100013CE 2005 5 31 ACE051405 120050514A261224412886 FIRE LOOP BEECH 1900 1900C 1154161CE RT ENGINE SHORTED E YADAK NONE N FALSE WARNING UKUNKNOWN 1 AL03112AX UC45 PIREP - RIGHT T-HANDLE LIGHT COMES ON INTERMITTENTLY. MAINTENANCE VERIFIED "OPEN" RIGHT ENGINE FORWARD FIRE LOOP. 2L72 4T RTA24CE 20050531000162005053100016EU 2005 5 31 AWXA200500559 120050514A2560P2070001214 FLASHLIGHT AIRBUS320 A320231 3930325EU CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28646AW 271 LAS - EMERGENCY EQUIPMENT DURING 8-DAY CHECK, THE AFT FLIGHT ATTENDANT FOLD OUT JUMP SEAT EMERGENCY FLASHLIGHT WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050531000172005053100017EU 2005 5 31 AWXA200500560 120050513A3397ABS0374A24 WIRE AIRBUS320 A320231 3930325EU CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28626AW 65 PHX - EEL - DURING E-03 CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 13 LT INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT THE CONNECTOR OF EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 13 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050531000182005053100018 2005 5 31 AWXA200500561 420050514A2565D31516113 SLIDE AIRBUS320 A320232 3930326EU L1 DOOR FAULTY A AWXAK NONE O OTHER ININSP/MAINT 1 WP28659AW164171662 1166 LAS - EEL - DURING 8-DAY CHECK THE EMERGENCY LIGHT SYSTEM TEST FAILED FOR EPSU EXT LOAD FWD L. MAINTENANCE ISOLATED PROBLEM TO THE L-1 DOOR SLIDE, REMOVED AND REPLACED L-1 DOOR SLIDE ASSEMBLY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050531000202005053100020NM 2005 5 31 AWXA200500563 120050429A53206545834551 INTERCOSTAL BOEING737 7373B7 1384580NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28332AW 23384 MCN - MAJOR REPAIR - DURING C-18 CHECK A .625 INCH CRACK WAS FOUND IN INTERCOSTAL AT BS 329, LBL 46, WL 208. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT BS 329, LBL 46; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER DWG 65-45834; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050531000212005053100021NM 2005 5 31 AWXA200500564 120050427A52106545871523A DOOR FRAME BOEING737 7373B7 1384580NM R1 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28332AW 23384 MCN - MAJOR REPAIR - DURING C-18 CHECK A .375 INCH CRACK WAS FOUND IN R-1 DOOR FRAME AT 3RD DOOR STOP CUTOUT FROM BOTTOM ON AFT SIDE BS 328, STR 14 RT. MAINTENANCE TRIMMED OUT CRACK AT R-1 DOOR STOP CUTOUT BS 328, STR 14 RT; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW ER 03-5200-05124-ES1. 2L72 4F RTA16WE 20050531000262005053100026WP 2005 5 31 UPS05844444 120050425A53205652580N FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE:C1 INSIDE DOOR 62 POGO STICK FITTING CRACKED .5 INCH LONG AT STA 1875 L36. REMOVED AND REPLACED POGO STICK FITTING IAW DC-8 SRM 51-1-20D AND 51-3 -0. 2L74 4F RT4A25 20050531000282005053100028WP 2005 5 31 UPS05844446 120050425A53203755847U2 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE:C1 C-PIT DOOR CUTOUT BANANA FITTING CRACKED AT STA 1160 L32R. REMOVED AND REPLACED BANANA FITTING IAW DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20050531000332005053100033WP 2005 5 31 UPS05844451 120050421A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE:C1 LONGERON CRACKED 1 INCH LONG AT STA 1746 L15L AND STA 1726 L15L. REMOVED AND REPLACED LONGERON SECTION AND INSTALLED SPLICE FITTINGS IAW DC-8 SRM 53-2-2 FIG 10 AND 51-3-2. 2L74 4F RT4A25 20050531000352005053100035WP 2005 5 31 UPS05844453 120050421A532047504192 ATTACH FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE:C1 MAIN CABIN STA 1230 L18R FRAME ATTACH FITTING .5 INCH CRACK. REMOVED CRACKED FITTING, FABRICATED REPLACMENT FITTING IAW DWG 4750419, AND INSTALLED IAW DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20050531000362005053100036WP 2005 5 31 UPS05844455 120050424A532097540222 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE:C1 CRACKED FLOORBEAM FITTING AT A-PIT DOOR JAMB AT FS 340. REMOVED CRACKED FLOORBEAM FITTING, FABRICATED REPLACEMENT IAW DWG 975 4022, AND INSTALLED IAW DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20050531000372005053100037WP 2005 5 31 UPS05844456 120050425A532037502571 SPLICE DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE:C1 B-PIT BETWEEN STA 480-460 L31L SPLICE FITTING CRACKED. REMOVED CRACKED SPLICE FITTING, FABRICATED REPLACEMENT FITTING IAW DWG 3750257, AND INSTALLED IAW DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20050531000392005053100039WP 2005 5 31 UPS05844458 120050421A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE:C1 LONGERON CRACKED .5 INCH LONG AT STA 1746 L16L. REMOVED AND REPLACED LONGERON SECTION AND INSTALLED SPLICE FITTING IAW DC-8 SRM 53-2-2 FIG 10. 2L74 4F RT4A25 20050531000402005053100040WP 2005 5 31 UPS05844459 120050421A523047732951 ANGLE DOUG DC8 DC873F 302199FWP MAIN CARGO DOOR CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE:C1 MAIN CARGO DOOR UNDER THRESHOLD 17 INCHES FWD OF AFT CUTOUT LWR ANGLE ATTACH JUST FWD OF AFT LATCH SPOOL HAS EXFOLIATION CORROSION. REMOVED AND REPLACED ANGLE IAW DC-8 SRM 51-1-21 AND 51-3-0. 2L74 4F RT4A25 20050531000412005053100041WP 2005 5 31 UPS05844460 120050421A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE:C1 MAIN CABIN FLOORBEAM HEAVY CORRODED AT STA 1700 RBL 34. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW DC-8 SRM 53-2-0 FIG 1F. FABRICATED AND INSTALLED FLOORBEAM REPAIR IAW DC-8 SRM 53-2-0 FIG 1G, 51-1-20D, AND 51-3-0. 2L74 4F RT4A25 20050531000432005053100043WP 2005 5 31 UPS05844462 120050422A5320 FINGER DOUBLER DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE:C1 MAIN CABIN CENTER WING BOX SUBFLOOR FINGER DOUBLER HAS SHEAR HEAD FASTENERS AND POSSIBLE CORROSION UNDER THE DOUBLER AT STA 915 BL 0. REMOVED FINGER DOUBLER AND FOUND OUT OF LIMITS. CENTER WING BOX PRESSURE WEB FOUND WITHIN LIMITS AFTER CORROSION REMOVAL. FABRICATED REPLACEMENT FINGER DOUBLER IAW DWG 5645332 AND INSTALLED IAW DC-8 SRM 51-1-21. 2L74 4F RT4A25 20050531000442005053100044WP 2005 5 31 UPS05844463 120050422A5320 FINGER DOUBLER DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE:C1 MAIN CABIN CENTER WING BOX FINGER DOUBLER HAS SEVERAL SHEAR HEAD FASTENERS AND POSSIBLE CORROSION UNDER THE DOUBLER AT STA 865 BL 0. REMOVED FINGER DOUBLER AND FOUND OUT OF LIMITS, CENTER WING BOX PRESSURE WEB FOUND IN LIMITS AFTER CORROSION REMOVAL. FABRICATED REPLACEMENT FINGER DOUBLER IAW DWG 5645332, AND INSTALLED IAW DC-8 SRM 51-1-20D, 51-1-21, AND DWG 5645332. 2L74 4F RT4A25 20050531000462005053100046WP 2005 5 31 UPS05844467 120050515A3510 OXYGEN MASK DOUG DC8 DC871F 302199DWP COCKPIT LEAKING A IPXAK NONE O OTHER ININSP/MAINT 1 SO01755UP 46055 INSPECTION TYPE:N/A F/O'S OXYGEN MASK LEAKS. REMOVED AND REPLACED F/O'S REGULATOR AND MASK PER MM CHAPT 35-10-08-2 AND CHAPT 35-10-07-4. OPS LEAK CHECK GOOD. 2L74 4F RT4A25 20050531000512005053100051NM 2005 5 31 RYNA200500017 120050509A521080530035 BOTTLE BOEING757 757200 1384950NM R4 DOOR DISCHARGED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07929RD5402 5402 23929 R-4 DOOR EMERGENCY ASSIST POWER RESERVOIR BOTTLE FOUND DEPLETED, GAUGE READS ZERO. REMOVED AND REPLACED POWER RESERVOIR BOTTLE. 2L72 4F RTA2NM 20050531000522005053100052WP 2005 5 31 ABXA050109 120050502A5320991556135 FLOOR SUPPORT DOUG DC9 DC941 302207NWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23951AX 47616 FLOOR SUPPORT AT STA 1072 WAS CORRODED TOP AND BOTTOM SIDE LONGERON 28 LEFT - LONGERON 28 RIGHT. REMOVED AND REPLACED FLOOR SUPPORT SECTIONS IAW DC-9 SRM 51-30-2, 51-30-5, AND SSRM DRAWING K05159. 2L72 4F A6WE 20050531000532005053100053WP 2005 5 31 ABXA050110 120050503A53203917624511 STIFFENER DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23951AX 47616 AFT PRESSURE BULKHEAD RIGHT SIDE DOOR JAMB STIFFENER CRACKED. REMOVED AND REPLACED STIFFENER IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 20050531000542005053100054WP 2005 5 31 ABXA050111 120050503A52304920233503 STOP FITTING DOUG DC9 DC941 302207NWP CARGO DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23951AX 47616 FORWARD UPPER STOP TEE FITTING CRACKED FORWARD LOWER CARGO DOOR. REMOVED AND REPLACED FITTING IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20050531000552005053100055WP 2005 5 31 ABXA050112 120050504A5320991050313 CUSP WEB DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23951AX 47616 RIGHT CUSP WEB CRACKED AT EXISTING REPAIR, STA 1021 - 1041, RIGHT BUTT LINE 50. REMOVED AND REPLACED CUSP AT STA 1021 - 1041 IAW DC-9 SRM 53-03 AND 51-30-4. 2L72 4F A6WE 20050531000562005053100056WP 2005 5 31 ABXA050108 120050503A5415591326227 ATTACH ANGLE DOUG DC9 DC941 302207NWP RT PYLON CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23951AX 47616 UPPER PYLON ATTACH ANGLE CRACKED AT FORWARD END. REPAIRED AREA IAW DC-9 SRM 54-04. 2L72 4F A6WE 20050531000602005053100060NM 2005 5 31 AWXA200500567 120050515A3830 DUMP VALVE BOEING737 7373G7 1384595NM FWD LAVATORY OBSTRUCTED A AWXAA UNSCHED LANDING K FLUID LOSS CLCLIMB 1 WP28160AW 23782 LAS - AIR TURNBACK - FLT 113 - ON CLIMB-OUT OF LAS EN ROUTE TO LAX, VISUAL INDICATION OF LAVATORY BLUE JUICE WAS OBSERVED COMING FROM THE FRONT LAVATORY. MX COMPLIED WITH LAVATORY CLEAN UP PER AWA TASKCARD I1D38001. MX REMOVED PLASTIC BAG FROM DUMP VALVE. OPERATIONAL CHECKS OF THE LAVATORY WERE GOOD. 2L72 4F RTA16WE 20050531000622005053100062WP 2005 5 31 CALA0500148 120050513A5347593054765N SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714879 49526 INSPECTION FOUND LEFT O/B SEAT TRACK CORRODED AT STA 1183-1227, LBL 35. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05-00. 2L72 4F RTA6WE 20050531000662005053100066NM 2005 5 31 CALA0500152 120050515A53155149A02045 FLOORBEAM BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2726210 28770 INSPECTION FOUND FLOORBEAM CORRODED ON UPPER SURFACE NEAR R-1 DOOR, STA 320, BL 0 TO RBL 24. REPAIRED FLOORBEAM IAW ECRA 5321-01216. 2L72 4F RTA16WE 20050531000722005053100072SO 2005 5 31 RAIA00505002 120050504A28102770138101 VALVE EMB 145 EMB145LR 3260212SO RT TANK DEFECTIVE A RAIAA UNSCHED LANDING K FLUID LOSS CLCLIMB 1 CE03824HK 145498 FLT-5697 - STL - TOWER REPORTED SMOKE OR VAPOR COMING FROM RIGHT WING TIP. MAINTENANCE REMOVED AND REPLACED RT TANK FLAP VALVE. 2L72 4T RTT00011AT 20050531000762005053100076SO 2005 5 31 RAIA00505007 120050512A301010006492 CONTROL VALVE EMB 145 EMB145LR 3260212SO ANTI-ICE SYSTEM MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03813HK3107 145044 FLT 5773 - STL - STAB ANTI-ICE FAIL MESSAGE. MAINTENANCE REMOVED AND REPLACED STAB ANTI-ICE CONTROL VALVE. 2L72 4T RTT00011AT 20050531000772005053100077EU 2005 5 31 RAIA00505008 120050512A3260 UPLOCK SWITCH JETAIRJETSTMJETSTM4101 1500501EU LT MLG DIRTY A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03556HK 41073 FLT 5459 - STL - RED LIGHT IN GEAR HANDLE ILLUMINATED. MAINTENANCE CLEANED LT MLG UPLOCK SWITCH. 2L72 4T RTA41NM 20050531000792005053100079SO 2005 5 31 RAIA00505004 120050507A324039807 CONTROL VALVE EMB 145 EMB145LR 3260212SO LEFT MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03816HK15752 145055 FLT 5745 - STL - OUTBOARD BRAKE TEMP INDICATION IN YELLOW. MAINTENANCE REMOVED AND REPLACED LT BRAKE CONTROL VALVE. 2L72 4T RTT00011AT 20050531000822005053100082NM 2005 5 31 AMTA200500402 120050430A335020131A BATTERY PACK BOEING757 75723N 1384973NM CABIN DISCHARGED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11519AT 27975 DOOR R4 ESCAPE SLIDE LIGHT INOPERATIVE. FOUND RIGHT BATTERY PACK DEAD, REPLACED BATTERY. OPS OK. (M) 2L72 4F RTA2NM 20050531000852005053100085NM 2005 5 31 USAA050551 120050420A5347 SEAT TRACK BOEING767 7672B7 1385107NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19656US51362 26847 BFM - FOUND SEAT TRACK CORRODED 10 INCHES BY 3 INCHES, STATION 871 RBL 54.81. INSTALLED REPAIR AND SPLICES PER SRM 53-00-51 FIG 203 AND 51-40-02. (M) 2L72 4F RTA1NM 20050531000862005053100086NM 2005 5 31 USAA050550 120050501A5720 ANGLE BOEING767 7672B7 1385107NM LT WING CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19656US 26847 BFM - FOUND LE WEB, LOWER ANGLE CRACKED .75 INCH LONG, LEFT WING INBOARD OF FUELING PANEL. DAMAGE AREA REMOVED, INSTALLED REPAIR STRAP, FILLERS AND DOUBLER PER SRM 57-41-13 FIG 202 AND 51-40-02. (M) 2L72 4F RTA1NM 20050531000872005053100087EU 2005 5 31 USAA050555 120050428A53151160852 FLOORBEAM AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19105UW13610 0868 PIT - FOUND BEAM CORRODED 1 INCH DIAMETER, FLOORBEAM AT Y525L AFT HOLE ABOVE CROSSBEAM C-16. REPLACED BEAM PER DWG 53110900. CORROSION LEVEL 2, TASK JA-220-53500. (M) 2L72 4F RTA28NM 20050531000882005053100088EU 2005 5 31 USAA050556 120050429A5315D5347218820400 FLOORBEAM AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19105UW13610 0868 PIT - FOUND FLOORBEAM CORRODED 4 INCHES BY 5 INCHES, Y1292 LT FLOORBEAM ON TOP SURFACE AT SEVERAL LOCATIONS FORWARD OF FRAME 66-68. CORROSION LEVEL 1, TASK JA-360-53500. REMOVED AND REPLACED ORIGINAL PART PER AIRBUS DWG D53472815. (M) 2L72 4F RTA28NM 20050531000892005053100089NM 2005 5 31 USAA050544 120050423A5312 BULKHEAD BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19443US39447 24842 CLT - FOUND BULKHEAD CRACKED .250 INCH, BS 178, LBL 4, 5 WL 199. INSTALLED DOUBLER IAW EO 5300V152 AND SRM 53-10-08 DETAIL IV. (M) 2L72 4F RTA16WE 20050531000902005053100090NM 2005 5 31 USAA050546 120050427A5320 INTERCOSTAL BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US39931 24781 CLT - FOUND ANGLE INTERCOSTAL CRACKED .25 INCH, STATION 291.5 BELOW STRINGER 11R. REPLACED ANGLE INTERCOSTAL IAW SRM 51-10-02. (M) 2L72 4F RTA16WE 20050531000922005053100092NM 2005 5 31 USAA050543 120050425A5754 SKIN BOEING737 7374B7 1384702NM L/E SLAT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US39931 24781 CLT - FOUND SKIN CRACKED .125 INCH, NR 6 SLAT AFT ROW OF RIVETS AT NR 6 SLAT INBOARD AUX TRACK. INSTALLED DOUBLER, SDA UPDATED IAW SRM 57-43-01 FIG 206. (M) 2L72 4F RTA16WE 20050531000932005053100093NM 2005 5 31 USAA050554 120050419A5320US65516987 STRINGER SPLICE BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19374US56183 22953 BFM - FOUND STRINGER SPLICE CRACKED .750 INCH, FASTENERS MOUNTING HOLE, AFT CABIN LEFT CEILING, STRINGER 4L AT BS 908. FABRICATED PARTS, INSTALLED FABRICATED CHANNEL ON STRINGER SPLICE PER SRM 51-40-02. (M) 2L72 4F RTA16WE 20050531000942005053100094NM 2005 5 31 USAA050549 120050427A5320 INTERCOSTAL BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US39931 24781 CLT - FOUND INTERCOSTAL CORRODED 1 INCH BY 5 INCH, STATION 294-312 AT LBL 10.5 INCH. REMOVED AND REPLACED WITH NEW INTERCOSTAL IAW ARM 51-40-02. (M) 2L72 4F RTA16WE 20050531000962005053100096NM 2005 5 31 USAA050545 120050427A5320 STRAP BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US39931 24781 CLT - FOUND STRAP .5 INCH, STATION 328, RBL 32, WL 200. REPLACED STRAP IAW SRM 51-40-02. (M) 2L72 4F RTA16WE 20050531000972005053100097NM 2005 5 31 USAA050547 120050427A5320 ANGLE BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US39931 24781 CLT - FOUND Z-ANGLE CORRODED 1 INCH BY 2 INCH, FROM STATION 979 TO 933 RBL 46. REPAIRED REMOVED LIGHT SURFACE CORROSION FOUND WITHIN LIMITS IAW SRM 53-60-15. (M) 2L72 4F RTA16WE 20050531000992005053100099NM 2005 5 31 USAA050548 120050427A5320 INTERCOSTAL BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US39931 24781 CLT - FOUND INTERCOSTAL CORRODED 3 INCHES BY 1.5 INCHES, STATION 946 TO 986 RBL 16. INSTALLED NEW INTERCOSTAL (1123578) IAW SRM 51-10-02. (M) 2L72 4F RTA16WE 20050531001052005053100105 2005 5 31 KBM2005F00048 420050430A34205050017901 GYRO SNIAS 350 AS350B2 8680813EU COCKPIT FAULTY A KBMAO OTHER O OTHER NRNOT REPORTED 1 SW29751H 3403 ALTITUDE GYRO SHOWS 10 DEGREES RIGHT TURN DURING STRAIGHT AND LEVEL FLIGHT. REMOVED AND REPLACED. (M) 1G71 3U H9EU 20050531001072005053100107SO 2005 5 31 SIMA200511709 120050414A532014000418401 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21847AE 145707 DURING CPCP INSPECTION FOUND; CENTER OMEGA BEAM CORRODED AT FRAME 25. MAINTENANCE INSTALLED REPAIR DOUBLER AT FRAME 25 IAW SRM. AIRCRAFT RETURNED TO SERVICE. (SW21200505715) (K) 2L72 4F4 FRTT00011ATTE6CH 20050531001092005053100109WP 2005 5 31 GTIA050150 120050416A5320 BRACKET DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23829NK 49931 FTW - AFT PIT, UPPER LATCH BRACKET SUPPORT IS CRACKED. REMOVED AND FABRICATE NEW BRACKET. TREAT, PRIMED AND INSTALLED BRACKET. (M) 2L72 4F A6WE 20050531001132005053100113SO 2005 5 31 SIMA200511707 120050414A532014521700007 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21847AE 145707 DURING CPCP INSPECTION FOUND; LT OMEGA BEAM IS CORRODED AT FRAME 20. MAINTENANCE REPAIRED LT OMEGA BEAM AT FRAME 20 IAW SRM BY INSTALLING REPAIR DOUBLER. AIRCRAFT RETURNED TO SERVICE. (SW21200505715) (K) 2L72 4F4 FRTT00011ATTE6CH 20050531001142005053100114NM 2005 5 31 GTIA050145 120050425A2810 VALVE AIRBUSA319 A319132 3930340NM FUELING PANEL OPEN A GTIAO OTHER J WARNING INDICATION CLCLIMB 1 GL23502NK 2433 CAE - CENTER TANK PUMP NR 1 FAULTED DURING CLIMB-OUT. FOUND CENTER TANK REFUEL VALVE LEFT MANUALLY OPEN AT FUELING PANEL, PUT VALVE SWITCH TO NORMAL AND IT CLOSED, OPS CHECK NORMAL. (M) 2L72 4F RTA28NM 20050531001152005053100115SO 2005 5 31 SIMA200511708 120050414A532014000421001 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21847AE 145707 DURING CPCP INSPECTION; FOUND LT OMEGA BEAM CORRODED AT FRAME 25 CROSSBEAM. INSTALLED REPAIR DOUBLER AT FRAME 25 IAW SRM. AIRCRAFT RETURNED TO SERVICE. (SW21200505715) (K) 2L72 4F4 FRTT00011ATTE6CH 20050531001162005053100116WP 2005 5 31 GTIA050146 120050426A2910 HYDRAULIC SYSTEM DOUG DC9 DC982 3022082WP RIGHT CONTAMINATED A GTIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL23830NK 49932 FLL - RIGHT HYDRAULIC TEMP HIGH LIGHT CAME ON DURING FLIGHT, AIRCRAFT TAIL SWAP WITH 819NK. BLED RIGHT HYDRAULIC SYSTEM RESERVOIR OF EXCESS AIR AND SERVICED TO PROPER LEVEL, OPS CHECK NORMAL. (M) 2L72 4F A6WE 20050531001192005053100119SO 2005 5 31 SIMA200511703 120050420A532014525480003 SILL EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21807AE8257 145506 THE CARGO DOOR CUT OUT LOWER SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED LOWER DOOR SILL. INSTALLED SERVICEABLE SILL IAW SRM. (SW21200505714) (K) 2L72 4F4 FRTT00011ATTE6CH 20050531001202005053100120SO 2005 5 31 SIMA200512203 120050425A532014000492401 PROFILE EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21806AE 145503 DURING AN MBV INSPECTION, MAINTENANCE FOUND THE (Z) PROFILE HAS CORROSION IN SEVERAL AREAS BETWEEN FRAMES 22 AND 23, RT SIDE BY AFT GALLEY AREA. MAINTENANCE REPLACED (Z) PROFILE IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200505710) (K) 2L72 4F4 FRTT00011ATTE6CH 20050531001232005053100123NE 2005 5 31 GTIA050143 220050424A7200 ENGINE DOUG DC9 DC981 3022081WP PWA JT8 JT8D219 52053NE NR 2 MALFUNCTIONED A GTIAO OTHER O OTHER TXTAXI/GRND HDL 1 GL23818NK 48018 718231 NR 2 ENGINE VERY SLOW TO SPOOL UP, 20 SECONDS FROM IDLE TO 1.4 EPR, AIRCRAFT TAIL SWAP WITH N800NK. REMOVED AND REPLACED NR 2 ENGINE, OPS CHECK NORMAL. (M) 2L72 4F4 F A6WE E9NE 20050531001252005053100125WP 2005 5 31 GTIA050141 120050413A5320 BRACKET DOUG DC9 DC982 3022082WP A/C BAY BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23829NK 49931 FTW - AFT ACCY COMP LEFT SIDE CANT 1463 WIRE HARNESS BRACKET IS BROKEN. REMOVED AND FABRICATE NEW BRACKET. TREAT, PRIMED AND REPAIRED BRACKET INSTALLED. (M) 2L72 4F A6WE 20050531001262005053100126SO 2005 5 31 SIMA200512205 120050425A531313500400019 STRINGER EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21806AE 145503 DURING AN MBV INSPECTION, MAINTENANCE FOUND STRINGER 19R WITH CHAFE DAMAGE BETWEEN FRAMES 52 AND 53. MAINTENANCE REPAIRED STRINGER 19R BETWEEN FRAMES 52 AND 53 IAW SRM DOUBLER REPAIR. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200505710) (K) 2L72 4F4 FRTT00011ATTE6CH 20050531001282005053100128SO 2005 5 31 SIMA200512206 120050425A531313500400005 STRINGER EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21806AE 145503 DURING AN MBV INSPECTION, MAINTENANCE FOUND STRINGER 19L WITH CHAFE DAMAGE BETWEEN FRAMES 52 AND 53. MAINTENANCE REPAIRED STRINGER 19L BETWEEN FRAMES 52 AND 53 IAW SRM DOUBLER REPAIR. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200505710) (K) 2L72 4F4 FRTT00011ATTE6CH 20050525002292005052500229NM 2005 5 25 05FDEA01304 120050516A5311ACA71281 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25580FE 48471 MAIN DECK LEFT STATION 535 "Z"= 24 FRAME FOUND DENTED AS MARKED. REPAIR CARRIED OUT AS PER DRAWING SRZ-53-503. 2L73 4F RTA22WE 20050525002312005052500231CE 2005 5 25 DXTA200500730 120050520A215073838433 ACM CESSNA750 750 2076810CE UNSERVICEABLE E DXTAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07902QS745 7500002 WHEN CABIN PACK IS IN OPERATION SMOKE ENTERS THE CABIN TEMPERATURE IS UNCONTROLLABLE IN BOTH AUTOMATIC AND MANUAL MODES (SUPPLY TEMP WAS 247 DEG) DISCOVERED AFTER LANDING. FOUND FWD PAC TURBINE SEIZED. REPLACED FWD AIR CYCLE MACHINE IAW CE750 MM 21-51-00. OPERATIONAL AND LEAK CHECK GOOD 2L72 4J RTT00007WI 20050526000012005052600001NM 2005 5 26 DLM88050237 120050427A4990499701338 PRESSURE SWITCH DOUG MD88 MD88 3023688NM APU FAILED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27998DL 53370 SMOKE IN COCKPIT AND CABIN IMMEDIATELY AFTER TAKEOFF. REPLACED APU OIL PRESSURE SWITCH. 2L72 4F RTA6WE 20050526000222005052600022NM 2005 5 26 DLM88050261 120050506A2612269001001 AMPLIFIER DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE FIRE DETECTION FAILED A DALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO27975DL 53243 718217 NR 2 ENGINE FIRE WARNING CAME ON INTERMITTENTLY, ON AND OFF INCLUDING FIRE BELL/ B-LOOP LIGHT / VOICE / HANDLE LIGHT. A-LOOP WAS ON MCO. REPLACED A2-6 FIRE DETECTOR AMP. OPS GOOD ON B-LOOP. 2L72 4F4 FRTA6WE E9NE 20050526000252005052600025NE 2005 5 26 DLM88050264 220050509A7200719001589 ENGINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 FLAMED OUT A DALAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SO27933DL40080 49720 725416 RIGHT ENGINE FLAME OUT DURING CLIMBOUT FROM ATL. REPLACED FUEL PUMP FOR SHEARED SHAFT AND GEARBOX. 2L72 4F4 FRTA6WE E9NE 20050526000282005052600028SO 2005 5 26 SIMA200510801 120050409A532014521713005 BEAM EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21849AE 145716 THE LAV FLOOR CENTER HAT BEAM WAS FOUND TO BE CORRODED. BLENDED OUT THE AREA AND REMOVED THE CORROSION. PERFORMED EDDY CURRENT INSPECTION WITH NO DISCREPANCIES. FABRICATED A DOUBLER FOR REPAIR. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 28, CHAPTER 53-21-10, FIG 207 AND EMB IC2005-145/1805 DATED APRIL 7, 2005. (M) 2L72 4F RTT00011AT 20050526000372005052600037NM 2005 5 26 HALA0500169 120050202A2923861555 PUMP BOEING717 717200 1383700NM AUX HYD SYS FAILED A HALAK NONE O OTHER ININSP/MAINT 1 WP13480HA 55125 DURING EO 29-02-02-11 REV A, FOUND AUX PUMP ELECTRICAL CONNECTOR ON PUMP MELTED, NEED TO REPLACE PUMP. AIRCRAFT SIDE PLUG DISCONNECTED FROM PUMP. REMOVED AND REPLACED AUX HYD PUMP IAW AMM 29-21-01, OPS AND LEAK CHECK GOOD. (M) 2L72 4F TRA6WE 20050526000402005052600040SO 2005 5 26 SIMA200510803 120050408A532014525381003 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21644AE 145204 ABI - PREVIOUS REPAIR ON THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. REMOVED THE PREVIOUS REPAIR. FABRICATED AN EXTERNAL ANGLE, FILLER, PLATE AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 28 CHAPTER 53-21-10. (M) 2L72 4T RTT00011AT 20050526000472005052600047NM 2005 5 26 USAA050526 120050405A532065C334191LF SHEAR WEB BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19374US56183 22953 FOUND SHEAR WEB CORRODED 10 INCHES BY 27 INCHES, BS 1016 FLOOR BL 0 - LBL 27. CORROSION LEVEL 1, TASK C53-202-01. FABRICATED NEW SHEAR WEB AND INSTALLED NEW PARTS PER SRM 53-60-51, 51-30-01, 51-24-00, 51-40-02. (M) 2L72 4F RTA16WE 20050526000622005052600062NM 2005 5 26 USAA050540 120050420A5347BAC1520792 SEAT TRACK BOEING737 7373B7 1384580NM FUSELAGE GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19374US56183 22953 BFM - FOUND SEAT TRACK WITH NICKS AND GOUGES, .90 INCH BY .2 INCH BY .022 INCH AND .40 INCH BY .10 INCH BY .025 INCH, MCD FROM STATION 480-520. FABRICATED NEW SEAT TRACK, REMOVED AND REPLACED PER SRM 53-00-52, SRM 51-40-02. (M) 2L72 4F RTA16WE 20050526000692005052600069NM 2005 5 26 USAA050532 120050330A5313 STRINGER BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19374US56183 22953 BFM - FOUND STRINGER CORRODED 8 INCHES LONG BY 1 INCH WIDE BY .035 INCH DEEP AREA, BS 967, STRINGER 25L. INSTALLED NEW STRINGER SECTION AND REPAIR SPLICE PER SRM 53-00-03. (M) 2L72 4F RTA16WE 20050526000722005052600072NM 2005 5 26 C8GA20050012 120050510A801297907821 START VALVE BOEING727 727200 138407ENM NR 3 ENGINE INOPERATIVE A C8GAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 SO29815AA51877 22552 FLT 718 FROM STL TO ELP, ON CLIMB FROM STL, NR 3 ENGINE START VALVE LIGHT ILLUMINATED AT 15000 FT. SHUTDOWN NR 3 ENGINE AS A PRECAUTION. DUMPED 6000 LBS OF FUEL, RETURNED TO STL, AND LANDED WITHOUT INCIDENT. FOUND NR 3 ENGINE START VALVE INOPERATIVE. REPLACED START VALVE. AIRCRAFT RETURNED TO SERVICE. 2L73 4F RTA3WE 20050526000902005052600090EA 2005 5 26 COMA0560295 120050507A5330601R3114627 SKIN PANEL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01929CA27335 7035 DURING COMPLIANCE OF TASK 002-53-160-610 (COMAIR TASK CRJ-2-162011), 1 CRACK WAS FOUND IN THE PRESSURE FLOOR SKIN AT FS 460.0, BETWEEN BL 0.0 AND RBL 9.0 THE CRACK WAS 2.0 INCH IN LENGTH. REPAIRED IN ACCORDANCE WITH BOMBARDIER REO 601R-53-41-102, REV D, DATED 9-29-2003. 2L72 4F RTA21EA 20050526000962005052600096EA 2005 5 26 COMA0560301 120050507A2750 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS OUT OF RIG A COMAO OTHER J WARNING INDICATION CRCRUISE 1 SO01809CA 7366 FLIGHT 5349 FLAPS FAIL CAUTION. RERIGGED THE LT AND RT BPSU. 2L72 4F RTA21EA 20050526001112005052600111NM 2005 5 26 SWAA051357 120050509A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29324SW 23414 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D + 12, STR 15L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050526001132005052600113 2005 5 26 SWAA051359 420050509A2565D31354 SLIDE BOEING737 7375H4 138449DNM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050526001202005052600120SO 2005 5 26 20030843 120050509A3397 WIRE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT DAMAGED A GLBAO OTHER O OTHER TXTAXI/GRND HDL 1 NM03108UX 120108 EXIT ROW EMERGENCY LIGHTS IN ROW 5A LIGHTS DIM. MAINTENANCE RESOLDERED WIRE. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA31SO 20050526001252005052600125EA 2005 5 26 COMA0570050 120050509A5315CC670341757 FLOORBEAM CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01376CA5331 10092 TRANSVERSE BEAM AT FS 280 FROM LBL36 TO RBL 36 IS CORRODED ALONG THE UPPER AN LOWER EDGES. REPLACED THE TRANSVERSE BEAM AT FS 280 IAW BOMBARDIER AEROSPACE REO 670-53-11-047, REV A., CRJ 700 SRM 51-25-16-001-001-A01, CRJ 700 SRM 51-40-11-001-001-A01 AND CRJ 700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20050526001302005052600130SO 2005 5 26 SWIA200514972 120050508A5210 LATCH EMB 120 EMB120ER 3260203SO PAX DOOR BACKED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07569SW 120344 MAIN CABIN DOOR WON'T OPEN. DOOR CAPTURE LATCH HAD BACKED OUT. REMOVED LATCH, CLEANED AND REINSTALLED. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050526001372005052600137EA 2005 5 26 SWIA200514979 120050508A2740 SWITCH CNDAIRCL600 CL6002B19 1900309EA COCKPIT INOPERATIVE A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07410SW 7066 STAB TRIM CH 2 INOP. REPLACED CAPT'S STAB DISCONNECT SWITCH IAW CRJ MM 27-41-30, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050526001422005052600142 2005 5 26 SWIA200514984 420050503A31708221310102 DCU CNDAIRCL600 CL6002C10 1390015EA NR 1 MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07732SK 10194 AILERON TRIM ROLLED UNCOMMANDED TO LEFT. REPLACED NR 1 AND NR 2 DCU IAW CRJ AMM 31-70-00. OPERATIONAL CHECK GOOD. P/N 822-1310-102, S/N OFF 1L5JD, P/N 822-1310-102, S/N OFF 1MB3L. 2L72 4F RTA21EA 20050526001572005052600157WP 2005 5 26 ASMF200505012 120050509A32503920208507 LINK ASSY DOUG DC9 DC987 3022087WP NLG STEERING DAMAGED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23753RA5150027366 49587 CAPTAIN REPORTED STRONG NOISE WHEN TURN THE STEERING AND IT WAS NOT POSSIBLE TO CONTROL THE TEMPERATURE IN BOTH AIR CONDITIONING PACKS IN AUTO AND MANUAL. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE, THE LINK ASSY WAS REPLACED AND SHOCK STRUT SERVICE WAS PERFORMED IAW MM 32-21-04, TEMPERATURE CONTROL VALVES AND AIR CONDITIONING WATER SEPARATORS WERE REPLACED IAW MM 21-20-03 AND MM 21-20-02 RESPECTIVELY, TESTED CORRECT. 2L72 4F RTA6WE 20050526001782005052600178SO 2005 5 26 MASA200500333 120050504A3350 LIGHT EMB 145 EMB145LR 3260212SO EMERGENCY EXIT MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07836MJ 145359 ASH 2726 CLT TO MGM - THE CREW NOTED THAT THE LT OVERWING EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE. MAINTENANCE RESET POWER TO EMERGENCY LIGHTS AND PERFORMED OPERATIONAL TEST. NO FURTHER DEFECTS NOTED. 2L72 4T RTT00011AT 20050526001812005052600181EA 2005 5 26 MASA200500343 120050509A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA EMERGENCY EXIT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0727172 7172 ASH 2903 MCI TO PHL - THE CREW REPORTED ONE OVERWING EMERGENCY EXIT LIGHT INOP. MAINTENANCE RELAMPED AND OPS CHECKED GOOD. 2L72 4F RTA21EA 20050526001832005052600183NM 2005 5 26 MASA200500300 120050415A3350 LAMP DHAV DHC8 DHC8202 2809007NM EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07988HA 426 ASH 6370 YUM TO PHX - TWO OF FIVE LAMPS INOPERATIVE ON WALL MOUNTED EMERGENCY EXIT IDENTIFIER AT ROW 4A. RELAMPED ASSEMBLY AND SYSTEM OPERATED NORMALLY. 2H72 4T RTA13NM 20050526001852005052600185SO 2005 5 26 MASA200500303 120050418A3350 LIGHT EMB 145 EMB145LR 3260212SO EMERGENCY EXIT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07828MJ 145218 ASH 2735 FROM CLT TO JAX - THE CREW NOTED ALL OF THE PASSENGER EMERGENCY EXIT LIGHTS INOP. MAINTENANCE REPLACED A BATTERY PACK AND THE LIGHTS OPERATED NORMALLY. THE AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. 2L72 4T RTT00011AT 20050526002132005052600213EA 2005 5 26 SWIA200514990 120050504A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07423SW 7456 AFT EQUIPMENT COMPARTMENT INTERCOSTAL CLIP IS CRACKED; FS 625.00 STR 14L. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED INSTERCOSTAL CLIP AT FS 625 STR 14L IAW CRJ REO 601R-53-61-100 AND 601R-53-61-422. 2L72 4F RTA21EA 20050526002152005052600215SO 2005 5 26 SWIA200514992 120050215A5320 BUTTSTRAP EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07214SW 120280 THERE IS CORROSION ON BUTT STRAP JUST AFT OF PAX DOOR ENTRANCE. ITEM FOUND AT C-CHECK INSPECTION. REPLACED AFFECTED BUTT STRAP AND SECURED SAME IAW EMB 120 MM 51-10-02 PG 3 SEC 3A. 2L72 4T RTA31SO 20050526002222005052600222NM 2005 5 26 AALA20050323 120050512A3350 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21915AN 29516 DFW - EMERGENCY LIGHT BATTERY PACK AT M1675 INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK M1675. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20050526002352005052600235NM 2005 5 26 BB05037 120050516A335020131A BATTERY BOEING767 767201 1385125NM EMERGENCY LIGHT DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19648US 23900 FOUND EXTERIOR RIGHT OVERWING AND R1 DOOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE M731 BATTERY. 2L72 4F RTA1NM 20050526002512005052600251NM 2005 5 26 05FDEA01237 120050511A5330 SKIN BOEING727 727200 138407ENM FUSELAGE PUNCTURED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25212FE 22934 FUSELAGE SKIN AT STA 1110 BELOW STR 20R IS PUNTURED. REPAIRED AREA IAW SRM 53-30-3 FIG 5. THIS IS A CLASS B-REPAIR PER SRM 53-30-3 FIG 5 SHT 6. 2L73 4F RTA3WE 20050526002552005052600255EU 2005 5 26 05FDEA01241 120050512A5720 PLATE AIRBUS310 A310203 3930313EU LT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25403FE 230 LEFT WING LANDING PLATE AREA BETWEEN STA WAIX-7.35 AND STA WAIX-14.7 JUST FWD OF AILERON HAS 2 EACH HOLE OVERSIZED AT 0.328, AND CARD E6-5710-7-5008 A PT 3 MOD REQUIRES TO REAM THESE HOLES TO 0.313 DIAMETER. COMPLIED WITH EA 6-5730-88784 PART 1 AND RAS/BAE/100692/2005 ISSUE A. 2L72 4F RTA35EU 20050526002592005052600259EU 2005 5 26 05FDEA01245 120050512A5534 FITTING AIRBUS310 A310203 3930313EU VERTICAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25403FE 230 VERTICAL LEADING EDGE PANEL 322CL HAS CORROSION ON LOWER SPLICE FITTING. REMOVED NUT PLATES IAW A310-200 SRM 51-40-21, REMOVED CORROSION IAW A310-200 SRM 51-74-10. CHECKED MATERIAL LOSS OUT OF LIMITS IAW A310-200 SRM 55-30-00. REMOVED AND REPLACED SPLICE FITTING IAW A310-200 SRM 51-40-21. 2L72 4F RTA35EU 20050526002662005052600266EU 2005 5 26 05FDEA01252 120050512A5320A2557382720600 STRAP AIRBUS310 A310203 3930313EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25403FE 230 AFT CARGO COMPT STRAP FOR PANEL 151EC HAS EXFOLIATION CORROSION ON STRAP. REPLACED STRAP IAW A310-200 SRM 51-72-10. 2L72 4F RTA35EU 20050526002672005052600267EU 2005 5 26 05FDEA01253 120050512A5320A5517869020100 STRAP AIRBUS310 A310203 3930313EU ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25403FE 230 THS PANEL 341BB HAS AREAS OF CORROSION AROUND ANCHOR NUTS ON PANEL ATTACH POINT. REMOVED CORROSION IAW A310-200 SRM 51-74-10. MATERIAL IS OUT OF LIMITS IAW A310-200 SRM 55-10-00. FABRICATED PART IAW A55178690 DWG INSTALLED PART IAW A310-200 SRM 51-40-21. 2L72 4F RTA35EU 20050526002792005052600279NM 2005 5 26 05FDEA01403 120050523A5311 FRAME DOUG MD11 MD11 3023602NM FUSLEAGE CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25628FE 48447 DURING AIRPLANE'S CONVERSION FROM P TO F, FOUND CRACK 2.5 INCHES LONG ON FRAME LUG AT STA 1256 B/T L11 AND L12, RT SIDE. CUT OUT DAMAGED AREA AND REPAIR FRAME IAW SRM 53-30-00 FIG 2. CUT OUT DAMAGED AREA AND REPAIR FRAME IAW SRM 53-30-00 FIG 2. 2L73 4F RTA22WE 20050531000062005053100006SO 2005 5 31 C2XA05TY043 120050513A553414520736004 HOUSING EMB 145 EMB145LR 3260212SO VERTICAL STAB WORN A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714902 145496 TYS - DURING A SCHEDULED INSPECTION THE RIGHT VERTICAL STAB SPHERICAL BEARING HAS PLAY. MAINTENANCE REPAIRED THE SPHERICAL BEARING HOUSING IAW EMB-145 AMM 55-10-00 AND EC5510-01116. 2L72 4T RTT00011AT 20050531000072005053100007SO 2005 5 31 C2XA05IA073 120050512A3340D649015 LIGHT EMB 145 EMB145ER 3260211SO LANDING GEAR DETACHED A C2XAO OTHER O OTHER DEDESCENT 1 SW2712934 145019 IAH - FLIGHT 3205, DURING DESCENT THE CREW REPORTED LOUD NOISES WHILE EXTENDING THE GEAR. THE CREW HAD THREE GREEN GEAR INDICATIONS, PERFORMED AN EMERGENCY DESCENT AND A FLY-BY WHICH VERIFIED THE GEAR TO BE DOWN AND LOCKED, AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE LEFT HAND UPPER TAXI LIGHT TO BE DETACHED FROM THE GEAR. MAINTENANCE REMOVED AND REPLACED THE TAXI LIGHT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050531000232005053100023EU 2005 5 31 AWXA200500566 120050506A5320D5311282600101 DUMMY RAIL AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28639AW 471 SAL - MAJOR REPAIR - DURING C-08 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM DUMMY RAIL Y503.2 AT FR 16. MAINTENANCE REMOVED DAMAGED DUMMY RAIL Y503.2 AT FR 16; FABRICATED A NEW REPLACEMENT DUMMY RAIL PER DWG D53112826; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050531000242005053100024NM 2005 5 31 UPS05544466 120050515A5610 SEAL BOEING757 75724APF 1384969NM L2 WINDOW LEAKING A IPXAK NONE O OTHER ININSP/MAINT 1 SO01451UP 27739 INSPECTION TYPE:N/A CAPT SIDE NR 2 WINDOW LEAKS WATER DURING RAIN. DEFERRED PER GMM 36-11. NO REPORTS OF PRESS PROBLEMS 2 FLT CYCLE LIMIT. REMOVED AND REPLACED CAPT'S L2 WINDOW SEAL PER MM 56-11-53-4. THIS CLEARS D302375. 2L72 4F RTA2NM 20050531000252005053100025WP 2005 5 31 UPS05844443 120050330A533057552713 SKIN DOUG DC8 DC873F 302199FWP STA 262-269 L32RDAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 INSPECTION TYPE:C1 REMOVE C-1 DOOR JAMB LWR CORNER THAT DOES NOT COMPLY WITH SRM 53-2-0, FIG 22 AND REPAIR PER SRM. REPLACED C-1 DOOR JAMB, LOWER FORWARD CORNER IAW DC8 5330-22155, SAA SK 810-265, 8100-9. 2L74 4F RT4A25 20050531000302005053100030WP 2005 5 31 UPS05844448 120050421A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE:C1 RIGHT LONGERON 16R CRACKED 2 INCHES LONG AT STA 1756. REMOVED AND REPLACED LONGERON SECTION AND INSTALLED SPLICE FITTING IAW DC-8 SRM 53-2-2 FIG 10 AND 51-1-20D. 2L74 4F RT4A25 20050531000422005053100042WP 2005 5 31 UPS05844461 120050425A5320559799213 BRACE DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE:C1 FLOORBEAM & BRACE APPEAR HEAVILY CORRODED IN COCKPIT SUBFLOOR AT FWD PRESSURE WEB STA -129 LBL 33. REMOVED FLOORBEAM BRACE, FABRICATED REPLACEMENT FLOORBEAM BRACE IAW DWG 5597992, AND INSTALLED IAW DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20050531000452005053100045WP 2005 5 31 UPS05844464 120050422A53205643483501N FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE:C1 MAIN CABIN CENTER WING BOX AT STA 879.375 L20L SIDE FRAME FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED STA 879 FUSELAGE FRAME FITTING IAW DC-8 SRM 51-1-20D AND 51-1-21. 2L74 4F RT4A25 20050531000652005053100065NM 2005 5 31 CALA0500151 120050515A5310147A812634 DOOR FRAME BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2726210 28770 INSPECTION FOUND R-2 DOOR FRAME CORRODED AT Z-CHANNEL SILL, STA 990, RBL 64 TO LBL 24. THE FRAME WAS REPAIRED IAW ECRA 5311-01225. 2L72 4F RTA16WE 20050531001012005053100101NM 2005 5 31 AMTA200500306 120050325A2612BACC63BP14D7S7 CONNECTOR BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE FIRE DETECTION DEFECTIVE A AMTAK NONE N FALSE WARNING ININSP/MAINT 1 GL11557TZ 32591 EICAS MSG LT ENGINE OH LP2 DISPLAYED. REMOVED AND REPLACED CONNECTOR D41162P CCN NR 2623422 REF: AWM 20-61-00. FIRE DETECTOR SYSTEM, OPS CHECKED OK. (K) 2L72 4F4 FRTA2NM E12EU 20050531001062005053100106EU 2005 5 31 KBM2005F00049 120050424A7931 INDICATOR SNIAS 350 AS350BA 8680817EU COCKPIT INOPERATIVE E FDEAO OTHER O OTHER NRNOT REPORTED 1 WP19375H 2300 CUSTER GAUGE OIL PRESSURE INDICATOR INOPERATIVE. REMOVED AND REPLACED. (M) 1G71 3U NCH9EU 20050531001102005053100110WP 2005 5 31 GTIA050149 120050416A5230 HINGE DOUG DC9 DC982 3022082WP CARGO BAY CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23829NK 49931 FTW - AFT PIT, BARRIER DOOR SUPPORT CRACKED AT HINGE HALF. REMOVED AND REPLACED HINGE HALF, TREATED AND PRIMED. (M) 2L72 4F A6WE 20050531001112005053100111WP 2005 5 31 GTIA050147 120050415A5720 SUPPORT BRACKET DOUG DC9 DC982 3022082WP LT WING BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23829NK 49931 LEFT WING LEADING EDGE PANEL NR 1160C HAS BROKEN SHIELD SUPPORT BRACKET. REMOVED AND FABRICATE NEW SHIELD SUPPORT BRACKET. TREAT, PRIMED AND INSTALLED SHIELD SUPPORT BRACKET. (M) 2L72 4F A6WE 20050531001292005053100129WP 2005 5 31 GTIA050139 120050413A5230 RETAINER DOUG DC9 DC982 3022082WP CARGO DOOR GOUGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23829NK 49931 FTW - FORWARD CARGO COMPARTMENT DOOR UPLOCK GUIDE BRACKETS FORWARD AND AFT AT SEAL RETAINER HAVE DEEP GOUGES. BLENDED FORWARD AND AFT BRACKETS, FOUND TO BE OUT OF LIMITS. FABRICATED BRACKET, TREATED AND PRIMED. REPAIRED PART INSTALLED. (M) 2L72 4F A6WE 20050531001302005053100130WP 2005 5 31 GTIA050138 120050421A4990 B-NUT DOUG DC9 DC981 3022081WP APU LOOSE A GTIAK NONE KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 GL23819NK 48016 DTW - STARTED APU, LEFT PACK. CABIN FILLED WITH SMOKE SHUT DONE APU. FOUND RESIDUE OIL ON APU ACCESS DOOR AND SUPPLY LINE TO APU, B-NUT. SECURED SUPPLY LINE B-NUT. CLEANED AREA, RAN APU. OPS CHECK GOOD. NO LEAKS NOTED. (M) 2L72 4F A6WE 20050531001322005053100132SO 2005 5 31 SIMA200512202 120050424A2130200001015 VALVE EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL CABIN PRESSURE FAILED A SIMAB EMER. DESCENT O OTHER CLCLIMB 1 SW21719AE 145276 CREW REPORTED A LOSS OF CABIN PRESSURIZATION WHEN CLIMBING THROUGH FL210. CABIN ALT WENT ABOVE 10000 FT DURING DESCENT. MAINTENANCE REMOVED AND REPLACED THE E1 HIGH STAGE AND PRESS OUTFLOW VALVE IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT DID A FUNCTIONAL CHECK FLIGHT. AIRCRAFT WAS THEN RETURNED TO SERVICE. (SW21200505705) (K) 2L72 4F4 FRTT00011ATTE6CH 20050531001332005053100133NE 2005 5 31 2005UALA00096 220050125A723058H305 BLADE BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE NR 1 ENGINE FRACTURED A UALAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 WP29662UA 27159 727577 NR 1 ENGINE SURGED, FLAMED OUT AND SEIZED. ENGINE WAS REMOVED FROM SERVICE AND DISASSEMBLED. ROOT CAUSE OF THE FAILURE WAS DETERMINED TO BE A FRACTURE OF THE 5TH STAGE HPC BLADE IN THE ROOT. 2L72 4F4 FRTA1NM E24NE 20050531001362005053100136NM 2005 5 31 2005UALA00415 120050506A5313 STRINGER BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29586UA 26710 AFT PIT LWR BILDGE, BETWEEN STA 1440-1460, STRINGER 29L IS CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED SECTION OF CORRODED STRINGER AND SPLICED IN NEW STRINGER SECTION. 2L72 4F4 FRTA2NM E17NE 20050531001372005053100137NM 2005 5 31 2005UALA00416 120050506A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29586UA 26710 FWD PIT FRAME DENTED STA 600, STR 24L. FRAME DENT WAS TRIMMED OUT AND J ANGLE REPAIR INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050531001382005053100138NM 2005 5 31 2005UALA00417 120050506A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29586UA 26710 AFT PIT FRAME DENTED STA 1440, STR 26L. FRAME DENT WAS TRIMMED OUT AND J ANGLE REPAIR INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050531001422005053100142NM 2005 5 31 2005UALA00421 120050506A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29586UA 26710 AFT PIT FRAME DENTED STA 1480, STR 25L. FRAME DENT WAS TRIMMED OUT AND J ANGLE REPAIR INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050531001452005053100145NM 2005 5 31 2005UALA00424 120050507A5320 THRESHOLD BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29586UA 26710 AFT PIT STA 1420 RBL 26, CARGO DOOR THRESHOLD T-CAP REPAIR FILLER CORRODED AT THRESHOLD FORMING HORN. INSTALLED NEW T CAP AND REPLACED FILLER. 2L72 4F4 FRTA2NM E17NE 20050531001472005053100147NM 2005 5 31 2005UALA00426 120050506A5711 SPAR BOEING737 737322 1384676NM RT WING CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29311UA 23672 LT & RT MLG SUPPORT BEAMS OUTBOARD FITTINGS AND RT WING SPAR UPPER CHORD ARE CRACKED AT HOLE C. INTERIM REPAIR. ACP. PER EVA IMC-10243. ACP HFEC INSP. OF THE LOWER VERTICAL CHORD FOR CRACK INDICATIONS AT EVERY "C" CHECK. IF A CRACK IS FOUND AT HOLE "C", CONTACT FLEET EG. PERM REPAIR. TO BE ACP. AT NEXT HMV. REPLACED FITTING AT HMV ON SNR JIC'S. 2L72 4F RTA16WE 20050531001482005053100148NM 2005 5 31 2005UALA00427 120050506A5312 BULKHEAD BOEING737 737322 1384676NM FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29311UA 23672 STA 178 BULKHEAD WEB CRACKED AT UPPER LT RADAR MOUNT, UPPER OUTBOARD SIDE. MAJOR REPAIR ACCOMPLISHED. REPAIRED WEB, INSTALLED DOUBLER. 2L72 4F RTA16WE 20050531001492005053100149NM 2005 5 31 2005UALA00428 120050506A339764641 WIRE BOEING737 737322 1384676NM CABIN CUT A UALAK NONE L NO TEST ININSP/MAINT 1 WP29336UA 24240 FLOOR EMERGENCY LIGHTING ROW 11 THROUGH 15 INOP. EEL WIRING WAS CUT AT SEAT TRACK NEAR MAIN GEAR DOWNLOCK VIEWPORT AND WAS REPAIRED WITH SPLICE. 2L72 4F RTA16WE 20050531001502005053100150 2005 5 31 2005UALA00429 420050507A3418 MOTOR BOEING737 737522 138449FNM STICK SHAKER INOPERATIVE A UALAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 WP29927UA 26649 RETURNED TO BLOCKS DUE TO A CAPTAIN'S STICK SHAKER PROBLEM. CAPTAIN'S STICK SHAKER INOPERATIVE WHEN PERFORMING NR 1 STALL WARNING TEST. CLEANED AND INSPECTED PINS TO EIS DISPLAY AND STALL MANAGEMENT COMPUTER. THE EIS PRIMARY DISPLAY WAS REPLACED TO GET STICK SHAKER MOTOR TO OPERATE FOR STALL WARNING CHECK. SYSTEM CHECKED NORMAL. 2L72 4F RTA16WE 20050531001512005053100151NM 2005 5 31 2005UALA00430 120050507A5310 CREASE BEAM BOEING737 737322 1384676NM FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29314UA 23675 AFT GALLEY AREA STA 947.5 AND 986 HAS CORROSION, 50 PERCENT MATERIAL LOSS, CREASE BEAM. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW CREASE BEAM & DRAIN PAN. 2L72 4F RTA16WE 20050531001522005053100152NM 2005 5 31 2005UALA00431 120050508A2410 O-RING BOEING737 737322 1384676NM GENERATOR DRIVE MISSING A UALAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 WP29333UA 24228 RETURNED TO FIELD WITH GENERATOR DRIVE LOW OIL PRESSURE. FOUND THE NR 1 CSD CHARGE FILTER HOUSING O-RING MISSING. REPLACED THE O-RING, LEAK AND OPERATIONALLY CHECKED GOOD. 2L72 4F RTA16WE 20050531001532005053100153NM 2005 5 31 2005UALA00432 120050507A2781 WARNING LIGHT BOEING737 737322 1384676NM COCKPIT ACTIVATED A UALAK NONE J WARNING INDICATION CRCRUISE 1 WP29307UA 23668 WITH FLAPS UP (CRUISE CONFIG), THE L/E FLAPS TRANSIT LIGHT IS ON AND ANNUNCIATOR FLAP NR 2 TRANSIT LIGHT IS ON INTERMITTENTLY. THE L.E. FLAPS TRANSIT LIGHT AND FLAP NR 2 ANNOUNCIATOR LIGHT WERE ILLUMINATED BECAUSE OF A FAULTY NR 2 SLAT SENSOR (PN 10-6222-1, PCN 420-2108). THE SUBJECT SENSOR WAS REMOVED AND REPLACED PER MM 27-88-11/401. CURRENT MAINTENANCE PROGRAM: ON CONDITION CURRENTLY THE ARE NO UNUSUAL MAINTENANCE TRENDS ATTRIBUTED TO THIS SENSOR OR EVENT. NO MAINTENANCE PROGRAM CORRECTIVE ACTION WILL BE GENERATED IN RESPONSE TO THIS EVENT. 2L72 4F RTA16WE 20050531001542005053100154 2005 5 31 2005UALA00433 420050509A256563667103 FITTING AIRBUS320 A320232 3930326EU ASPIRATOR DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29456UA 1128 INFLATION HOSE WAS SNAPPED AT THE ASPIRATOR. HOSE ASSEMBLY FITTING BROKEN DURING PREVIOUS PACKING OF THE SLIDE ASSEMBLY. REMOVED BROKEN HOSE AND REPLACED WITH ONE FROM UAL INVENTORY. 2L72 4F RTA28NM 20050531001552005053100155NM 2005 5 31 2005UALA00434 120050509A2120 ODOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE COCKPIT DETECTED A UALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP29529UA 25019 DIVERTED TO ORD UNDER AMBER ALERT DUE TO AN ELECTRICAL SMELL IN THE FLIGHT DECK. REPLACED FAN. 2L72 4F4 FRTA2NM E17NE 20050531001572005053100157NM 2005 5 31 2005UALA00436 120050509A2824 UNKNOWN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUEL TRANSFER MALFUNCTIONED A UALAB EMER. DESCENT J WARNING INDICATION APAPPROACH 1 WP29587UA 26713 LANDED UNDER AMBER ALERT DUE TO A FUEL TRANSFER PROBLEM. UNEXPLAINABLE FUEL TRANSFER FROM RIGHT MAIN TANK TO CENTER TANK. MAINTENANCE ACCOMPLISHED INTERNAL LEAK CHECK OF SYSTEM BY PRESSURIZING FUEL FEED AND FUELING MANIFOLDS USING AIRCRAFT BOOST PUMPS. AFTER SEVERAL HOURS NO LEAKS (UNCOMMANDED TRANSFER) OCCURED. 2L72 4F4 FRTA2NM E17NE 20050531001582005053100158NM 2005 5 31 2005UALA00437 120050508A2701 UNKNOWN BOEING757 757222 1384956NM PWA 2037 PW2037 NE CONTROL COLUMN UNKNOWN A UALAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 WP29548UA 25396 RETURNED TO FIELD DUE TO A LOUD BANG IN THE CAPTAIN'S CONTROL COLUMN. THE SUBJECT DISCREPANCY WAS DUE TO A BROKEN SPRING RETAINER ON THE ELEVATOR TENSION REGULAR WHICH ALLOWED THE SUBJECT TENSION STRING TO BECOME DETACHED. THE SUBJECT TENSION REGULATOR WAS REMOVED AND REPLACED AND OPS CHECKED PER MM 27-31-12 AND 27-31-00. ALL OPS CHECKS WERE GOOD. 2L72 4F4 FRTA2NM E17NE 20050531001602005053100160NM 2005 5 31 2005UALA00439 120050512A5315 FLOORBEAM BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29672UA 30027 AFT BULK PIT STA 1439 CABIN FLOORBEAM LOWER CHORD FLANGE CRACKED. THIS REPAIR REQUIRED DUE TO KNOWN PROBLEM OF BULK CARGO DOOR IMPACTING LOWER CHORD OF MAIN CABIN FLOORBEAM UPON OPENING OF DOOR. DAMAGE REPAIRED PER FAA APPROVED REPAIR. 2L72 4F4 FRTA1NM E24NE 20050531001642005053100164SO 2005 5 31 CHQA200500098 120050513A335074441 LIGHT EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL CABIN INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11843RP 145599 EMERGENCY EXIT SIGN NEXT TO THE SERVICE DOOR IS INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT SIGN IAW EMB 135 AMM 33-50-13. OPS CHECK GOOD. 2L72 4F4 FRTT00011ATTE6CH 20050531001652005053100165SO 2005 5 31 CHQA200500099 120050516A2611 SMOKE WARNING EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL COCKPIT FALSE INDICATIONA CHQAA UNSCHED LANDING N FALSE WARNING UKUNKNOWN 1 GL11579RP 14500871 (A LAV SMOKE EICAS) MSG APPEARED JUST AFTER LANDING GEAR UP ON TAKEOFF. EMERG WAS DECLARED, RETURNED FOR LANDING. AFTER TURNING ONTO DOWNWIND LEG IN TRAFFIC PATTERN, EICAS MESSAGE DISAPPEARED. FA CHECKED LAVATORY, CABIN FOR ANY SIGNS OF SMOKE OR FIRE. REPORTED NO SIGNS OF SMOKE OR FIRE. THERE WERE NO SIGNS OF SMOKE IN THE COCKPIT. FLIGHT PROCEEDED TO LAND UNDER MAX LANDING WEIGHT WITH FIRE TRUCKS FOLLOWING TO GATE AS A PRECAUTION. MAINT PERFORMED ENG RUNS WITH PACKS ON AND OFF, IN VARIOUS CONFIGURATIONS, COULD NOT DUPLICATE PROBLEM. MAINT INSP DUCTING FROM ENG AND APU BLEEDS TO VERIFY NO OIL OR CARBON BUILDUP PRESENT. NO EVIDENCE WAS NOTED. OPS CHECK GOOD WITH NO LAV SMOKE INDICATIONS PRESENT. 2L72 4T4 FRTT00011ATTE6CH 20050531001662005053100166SO 2005 5 31 CHQA200500089 120050426A3350RPS1B BATTERY PACK EMB 135 EMB135LR 3260305SO CABIN DISCHARGED A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11837RP 145715 UPON ARRIVING AT THE AIRCRAFT, FOUND THE EMERGENCY LIGHTS ON WITH THE SWITCH IN THE OFF POSITION. CYCLED THE ON/OFF SWITCH AND LIGHTS RESET TO OFF. REMOVED AND REPLACED ALL FOUR EMERGENCY LIGHT BATTERIES IAW ERJ 135 AMM 33-50-04. 2L72 4F RTT00011AT 20050531001672005053100167WP 2005 5 31 GTIA050098 120050310A5514 DOUBLER DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE HORIZ STAB CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 HORIZONTAL STABILIZER, RT SIDE IB UPPER BRACKET SUPPORT HAS CRACK ON DOUBLER. REMOVED CRACKED DOUBLER. FABRICATED NEW DOUBLER. TREATED AND PRIMED, INSTALLED DOUBLER IAW SRM. (K) 2L72 4F4 F A6WE E9NE 20050531001692005053100169NM 2005 5 31 DHL2005740511 120050331A5230 SKIN BOEING727 7272Q9 138448MNM CARGO DOOR DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 C1 CARGO DOOR HAS NUMEROUS DENTS ON SKIN BETWEEN STA 560 TO 620. REMOVED FASTENERS AT C1 DOOR STA 560 TO 620 IAW B727 SRM 51-30-2. CUT OUT DAMAGED AREA 59 X 14.5 INCHES IAW B727 SRM 52-00-03 FIG 3. FAB NEW SKIN WITH 2024T3 .080 PO 9002012 SIZE 59 X 14.5 INCH ONE STRAP MAT 2024 T3 .080 PO 9002012 SIZE 59 X 6.5 INCH IAW B727 SRM 52-00-03 FIG 3. ALODINED AND PRIMED AREAS AND PARTS IAW B727 SRM 51-10-2, INSTALLED PARTS REPAIR IAW B727 52-00-03 FIG 3. 2L73 4F RTA3WE 20050531001722005053100172WP 2005 5 31 GTIA050136 120050414A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23829NK 49931 FOUND CORROSION ON TOP OF FLOORBOARD SUPPORT AT STATION 180 RBL 7 TO RBL 30. REMOVED CORROSION, FOUND OUT OF LIMITS. FABRICATED AND DRILLED SUPPORT. TREATED, PRIMED AND INSTALLED FLOOR SUPPORT. (M) 2L72 4F A6WE 20050531001742005053100174NM 2005 5 31 DHL2005740513 120050327A5753 SKIN BOEING727 7272Q9 138448MNM T/E FLAP DEBONDED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740 21930 RT WING TE OB AFT FLAP LOWER SKIN DISBONDED AT TE CENTER. CUT OUT DAMAGED AREA LWR SKIN APPROX 5 INCHES BY 1 1/2 INCHES IAW B727 SRM 54-40-20 FIG 31. FABRICATED ONE FILLER APPROX 5 INCHES BY 1 1/2 INCHES AND ONE DOUBLER APPROX 8 INCHES BY 3 INCHES USING .016 2024T3 PO NR 9001660 IAW B727 SRM 57-50-2 FIG 4. CLEANED PREPPED APPLIED ADHESIVE PRIMER AND ADHESIVE TO ALL REPAIR SUFACES AND BAGGED FOR BONDING IAW B727 SRM 51-40-20 FIG31. CURED REPAIR CLEANED AND PERFORMED POST BOND INSP WITH NO DELAM NOTED IAW B727 SRM 51-40-20 PARA 0 TREATED PRIMED AND SEALED REPAIR IAW B727 SRM 51-40-2 PARA P. 2L73 4F RTA3WE 20050531001752005053100175NM 2005 5 31 DHL2005740517 120050404A53471520792 SEAT TRACK BOEING727 7272Q9 138448MNM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 MAIN CABIN SEAT TRACK BS 480 T0 BS 560 LBL 24.75 DAMAGED. REMOVED AND REPLACED SEAT TRACK AT BS 480 TO BS 690 LBL 24 .75 AND FABRICATED SEAT TRACK FROM BAC 1520-792, PO NR 900146 AND 900146 DIM 18 FT. FABRICATED SPLICE FROM P/N BAC 1503-100122 PO NR 900943,DIM 13 INCHES (2 EA) SPLICE AND 7075T6 .250 DIM 2 INCHES BY 7.5 INCHES PO NR 9001189 IAW B727 SRM 53-10-5 FIG 1,TREATED AND PRIMED SEAT TRACK IAW B727 SRM 51-10-2. 2L73 4F RTA3WE 20050531001772005053100177WP 2005 5 31 GTIA050134 120050413A5320 SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23829NK 49931 FTW - MID PIT, STATION 712 RIGHT SIDE CHANNEL WALL SUPPORT IS CRACKED. FABRICATED REPAIR DOUBLER. TREATED AND PRIMED DOUBLER. OK TO INSTALL. (M) 2L72 4F A6WE 20050531001822005053100182WP 2005 5 31 GTIA050132 120050414A5320 CUSP WEB DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23829NK 49931 FTW - CABIN LEFT CUSP CORRODED FS 237-256. REMOVED CORROSION AT CUSP WEB FS 237-256. FOUND OUT OF LIMITS. REMOVED DAMAGED CUSP WEB. FABRICATED DOUBLER AND FILLER IAW SRM 51-70-4. TREATED AND PRIMED, INSTALLED REPAIRED PARTS IAW SRM 51-70-4. (M) 2L72 4F A6WE 20050531001852005053100185WP 2005 5 31 GTIA050084 120050315A5320 WEB DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 CABIN STA 180-200, RBL 54, RBL59, SUB FLOOR CORRODED. REMOVED CORROSION AT WEB. MATERIAL LOSS OUT OF LIMITS. REMOVED FWD AIRSTAIR. REMOVED FLOOR SUPPORT RT STA 160 TO 200. CUT OUT DAMAGED AREA AND FABED DOUBLER. PRIMED AND TREATED, INSTALLED FLOOR SUPPORT AND DOUBLER IAW SRM. INSTALLED FWD AIRSTAIR IAW MM. (K) 2L72 4F4 F A6WE E9NE 20050531001872005053100187CE 2005 5 31 DXTA200500723 120050513A33501317 LIGHT RAYTHNDH125 HAWKER800XP 7150012CE CABIN INOPERATIVE E DXTAK NONE L NO TEST ININSP/MAINT 1 GL07838QS 258338 FLOOR LEVEL EMERGENCY LIGHT ACROSS FROM EMERGENCY EXIT INOP. REMOVED AND REPLACED FLOOR LEVEL EMERGENCY LIGHT IAW HAWKER 800XP AMMA 33-20-00, OPS CHECK GOOD. 2L72 4F RTA3EU 20050531001882005053100188CE 2005 5 31 DXTA200500725 120050513A3230 CONTROL CABLE CESSNA750 750 2076810CE NLG OUT OF RIG E DXTAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 GL07938QS 7500183 IN FLIGHT, WITH THE NOSE GEAR IN THE UP POSITION, THERE IS A BUMPING NOISE UNDER THE FLIGHT DECK. FOUND EMERGENCY NOSE GEAR CABLE OUT OF RIG. RE-RIGGED NOSE GEAR EMERGENCY RELEASE CABLE. PREFORMED OPERATIONAL CHECK. CHECKED GOOD. WORK DONE IAW CHAP 32-30-00 OF THE CE 750 MM. 2L72 4J RTT00007WI 20050601000052005060100005CE 2005 6 1 DXTA200500724 120050513A284299144272 FLOAT SWITCH CESSNA750 750 2076810CE FUEL TANK FAULTY E DXTAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL07935QS4261 7500135 NO TAKEOFF AND MASTER WARNING CAME ON DURING TAKEOFF ROLL. DU NR 2 SHOWS FUEL QUALITY LOW, ABORTED TAKEOFF. FOUND FUEL QTY LOW LEVEL LT ILLUMINATED UP TO 630 LBS, SHOULD EXTINGUISH AT 500. DEFUELED ACFT AND GAINED ACCESS TO LOW LEVEL SWITCH OHMED OUT SWITCH AT PIN X. FOUND RESISTANCE READING WHEN SIMULATING FUEL LEVEL, 3352, SHOULD BE OPEN. REMOVED AND REPLACED LT LOW LEVEL FUEL SWITCH WITH NEW PER 750 M/M, CH 28-20-07. FUEL ACFT TO DUPLICATE SQK. SEALED SWITCH & BUILT UP WIRES W/ PINS. REMOVED LT BATTERY TO RESTORE CONNECTION PY011. RESTORED BATTERY. SWITCH OPS CHECKS GOOD BY MANUALLY OPERATING FLOAT SWITCH. MAINT PERFORMED IAW 750 M/M CH 28-20-07. 2L72 4J RTT00007WI 20050601000062005060100006CE 2005 6 1 DXTA200500722 120050512A3222CPD750322 SEAL CESSNA750 750 2076810CE NLG STRUT LEAKING E DXTAK NONE KE FLUID LOSS VIBRATION/BUFFET CRCRUISE 1 GL07944QS 7500144 THE BUMP IN THE NIGHT OCCURRED AT FL280 LEVEL FLIGHT FOLLOWED BY A NOSE RED UNLOCK LIGHT ON. STAYED ON FOR 20 MIN UNTIL LOWERING THE LANDING GEAR, 3 GREEN, NO RED, NO LIMITATIONS EXCEEDED. DISASSEMBLED NOSE GEAR STRUT, REPLACED SEALS, RETORQUED ORFICE ASSY. REASSEMBLED NOSE STRUT IAW CESSNA 750 MM CH 32-20-02, SERVICED IAW 12-10-38. PERFORMED GEAR FUNCTIONAL CHECK IAW CH 32-41-02, OPERATIONAL CHECK GOOD. 2L72 4J RTT00007WI 20050601000082005060100008 2005 6 1 GTIA050130 420050416A2230 AUTOTHROTTLE SYS DOUG DC9 DC983 3022083WP COCKPIT MALFUNCTIONED A GTIAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NRNOT REPORTED 1 GL23814NK 49619 FLL - F/O AND F/A SMELLED A POSSIBLE ODOR OF SOMETHING BURNING, AIRCRAFT ALSO HAD WINDSHEAR WARNING ON INBOARD AND AUTO THROTTLES DID NOT KEEP UP WITH SELECTED SPEED, AIRCRAFT TAIL SWAP WITH 825. RAN ENGINES AT VARIOUS POWER SETTINGS WITH ALL ELECTRICAL SYSTEMS, OPERATED BOTH PACKS AND APU NO ABNORMALITIES OR ODORS. PERFORMED FAULT REVIEW ON STP FOR WINDSHEAR COMP. NO FAULTS FOUND, COULD NOT DUPLICATE. RAN RTS ON BOTH DFGC, BOTH PASS, NO FAULTS NOTED. (M) 2L72 4F RTA6WE 20050601000102005060100010WP 2005 6 1 GTIA050129 120050419A2150 ACM DOUG DC9 DC982 3022082WP A/C BAY FAILED A GTIAO OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL23800NK 49144 RIGHT PACK CAUSING SMOKE IN CABIN, GATE RETURN. FOUND OIL AT OUTLET OF RIGHT ACM TURBINE. REMOVED AND REPLACED RT ACM AND COALESCER BAG. OPS CHECK GOOD. (M) 2L72 4F A6WE 20050601000132005060100013WP 2005 6 1 GTIA050079 120050311A2530 DOUBLER DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE G2 GALLEY CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 G-2 GALLEY, CART ENCLOSURE, AFT LOWER LIP AND (2 EA) DOUBLERS ARE CORRODED. REMOVED LOWER LIP AND DOUBLERS, FOUND LIP AND DOUBLERS OUT OF LIMITS. FABRICATED LIP CHANNEL AND DOUBLERS OUT OF LIMITS. FABRICATED LIP CHANNEL AND DOUBLERS. TREAT AND PRIMED. INSTALLED LIP CHANNEL AND DOUBLERS IAW SRM. (K) 2L72 4F4 F A6WE E9NE 20050601000142005060100014WP 2005 6 1 GTIA050078 120050311A2530 SUPPORT ANGLE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE G2 GALLEY CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 G-2 GALLEY, UPPER SECTION, LOWER EDGE AND SUPPORT ANGLE ARE CORRODED. REMOVED CORROSION ON LOWER EDGE AND SUPPORT ANGLE. FOUND SUPPORT ANGLE OUT OF LIMITS FABRICATED SUPPORT ANGLE IAW SRM. PRIMED AND INSTALLED SUPPORT ANGLE. (K) 2L72 4F4 F A6WE E9NE 20050601000152005060100015NE 2005 6 1 GTIA050127 220050412A7260 STUD DOUG MD80 MD83 3023681NM PWA JT8 JT8D* NE NR 2 GEARBOX STRIPPED A GTIAO OTHER K FLUID LOSS NRNOT REPORTED 1 GL23822NK 49392 NR 2 ENGINE USED 4 QUARTS OF OIL DURING FLT NR 931, AIRCRAFT TAIL SWAP WITH 830. FOUND ENGINE OIL FILTER COVER LEAKING. REPLACED 3 HELI-COILS FOR THE PULLED OUT STUDS ON THE GEARBOX, NO LEAKS NOTED ON ENGINE RUN. (M) 2L72 4F4 FRT E2EA 20050601000192005060100019WP 2005 6 1 GTIA050125 120050407A2840 O-RING DOUG DC9 DC982 3022082WP RT WING WORN A GTIAK NONE K FLUID LOSS ININSP/MAINT 1 GL23804NK 49104 FUEL SEEPAGE FROM RIGHT WING OVER RIGHT MAIN LANDING GEAR, TAIL SWAP WITH AIRCRAFT 829. REPLACED O-RING ON JUNCTION PROBE. LEAK CHECK GOOD. (M) 2L72 4F A6WE 20050601000222005060100022NM 2005 6 1 DHL2005740518 120050330A5210 WEB BOEING727 7272Q9 138448MNM PAX DOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH21930 21930 REMOVED FASTENERS AT FWD CORNER ENTRY DOOR WEB (INTERIOR) IAW B727 SRM 51-30-2,STOP DRILLED CRACK IAW B727 SRM 51-30-2. .250 TERMINATED OF END OF CRACK,NDT HFEC INSP PER 727 NDT PT6 51-00-00 FIG 23 CRACK END IN STOP HOLE, FABRICATED DOUBLER REPAIR MATL USED 7075T6 .050 PO 9002126 SIZE 5 X 6 INCH IAW B727 SRM 51-40-2 FIG 1 AND 52-40-1 FIG 1. ALODINED AND PRIMED PART AND AREA IAW B727 SRM 51-10-2 AND INSTALLED DOUBLER REPAIR IAW B727 SRM 51-40-2 FIG 1 AND 51-30-2. 2L73 4F RTA3WE 20050601000242005060100024WP 2005 6 1 DHL2005807501 120050411A5347S2772660 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH86990 45990 MAIN CARGO COMPT NR 5 TRACK LUGS WORN STA 1680.000. CUT OUT TRACK DAMAGED SEGMENT AND FABRICATED SPLICES (AL7075T6 0.160) (AL7075T6 0.125) (AL7075T6 0.100) IAW SRM 53-2-3 PG 49-50 FIG 14. CLEANED, TREATED AND PRIMED AREA AND SPLICES IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT AND SPLICES IAW SRM 53-2-3 PG 49-50 FIG 14, SRM 51-3-0 PG 1. TORQUED IAW SRM 51-3-1 PG 2A. 2L74 4F RT4A25 20050601000252005060100025WP 2005 6 1 DHL2005807507 120050427A5751 SKIN DOUG DC8 DC873F 302199FWP RT AILERON CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH86990 45990 RT INBOARD AILERON FWD UPPER SKIN 0.500 CRACK, STA XA 502.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-8-1 FIG 1. REMOVED DAMAGED PLATING IAW SRM 51-1-21 PG 1. FABRICATED NEW PLATING (AL7075T6 0.040) IAW SRM 57-8-1 FIG 1. CLEANED, TREATED AND PRIMED AREA AND NEW PLATING INTERIOR IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW PLATING IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. TORQUED IAW SRM 51-3-1. PERFORMED BALANCING OF RT INBOARD AIL IAW SRM 51-4-1 PG 1-3. REMOVED (2EA) WEIGHTS P/N 5706734-43 AT STA XA 523.000. FOUND WITHIN TOLERANCE (MOMENT: 3326.64 IN-LBS). 2L74 4F RT4A25 20050601000262005060100026WP 2005 6 1 DHL2005807509 120050424A5313S1616757 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH86990 45990 AFT FUSELAGE SECTION L-17L CRACK 2.000 AT STA 1766.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 53-5-3 FIG 5. REMOVED CRACKED LONGERON IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21, SRM 51-3-0 PG 1. FABRICATED NEW LONGERON (EXTRUSION 7075 P/N S1616757) IAW SRM 53-5-3 FIG 5. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW LONGERON IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9, SRM 51-3-0 PG 1, SRM 51-1-11 PG 9, SRM 51-3-2. TORQUED IAW SRM 51-3-1 PG 2A. 2L74 4F RT4A25 20050601000272005060100027WP 2005 6 1 DHL2005807510 120050503A5753 SKIN DOUG DC8 DC873F 302199FWP T/E FLAP DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH86990 45990 RT OUTBOARD FLAP INTERIM REPAIR ON FWD UPPER PLATING, STA XF 227.000. PERFORMED MAJOR REPAIR. REMOVED ALL FASTENERS WITHIN REPAIR AREA IAW SRM 51-1-21 PG 1. TRIMMED OUT DAMAGED SECTION IAW EO AST-050405. PERFORMED DETAIL VISUAL INSP OF AREA, FABRICATED NEW PLATING SEGMENT (AL2024T3 0.071) SPLICE STRAP (AL2024T3 0.080) AND INNER DOUBLER (AL2024T3 0.080) IAW EO AST 050405. CLEANED, TREATED AND PRIMED AREA, INNER DOUBLER, SPLICE STRAP AND NEW PLATING SEGMENT INNER SURFACE IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW EO AST-050405, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. TORQUED NUTS IAW SRM 51-3-1. 2L74 4F RT4A25 20050601000282005060100028WP 2005 6 1 DHL2005807511 120050503A5753 SKIN DOUG DC8 DC873F 302199FWP T/E FLAP DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH86990 45990 RT INBOARD FLAP FWD LWR PLATING HAS TWO DENTS OF 6 AND 5 STA XW 43.000 - 50.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 04-18-05, EO AST 050403 DATED 04-12-05. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. CUT OUT DAMAGED SECTION IAW EO AST 050403. PERFORMED DETAIL VISUAL INSP, NO CORROSION OR CRACK FOUND. FABRICATED NEW SKIN SEGMENT (AL2024T3 0.032), BONDED DOUBLER (AL2024-T3 0.020) 2EA SPLICE STRAPS (AL2024T3 0.063) AND 2EA FILLERS (AL2024T3 0.020) IAW EO AST 050403 DATED 04-12-05. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. BONDED DOUBLER ON NEW PLATING SEGMENT IAW SRM 51-1-9 PG 1, SRM 51-1-9A PG 1. INSTALLED REPAIR PARTS IAW EO AST 050403, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050601000332005060100033WP 2005 6 1 DHL2005807504 120050414A57203645612U BRACKET DOUG DC8 DC873F 302199FWP WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH86990 45990 NR 1 ALT TANK BOOSTER PUMP FWD BRACKET CRACKED. REMOVED CRACKED BRACKET AND INSTALLED A NEW ONE IAW SRM 51-1-20D PG 21-9. TORQUED NUT IAW SRM 51-3-1 PG 2A. 2L74 4F RT4A25 20050601000342005060100034WP 2005 6 1 DHL2005807500 120050419A5712 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH86990 45990 NR 1 LT STUB WING FORMER CRACK 0.500, STA XW 540.000. REMOVED FASTENERS IAW SRM 51-1-20D PG 21. PERFORMED STOP HOLE AND FABRICATED REINFORCING ANGLE (ALCLAD 7075-T6 0.063) IAW SRM 57-2-0. CLEANED, TREATED AND PRIMED REINFORCING ANGLE AND AREA IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE WITH NEW FASTENERS IAW SRM 51-1-20D PG 9, SRM 57-2-0, SRM 51-3-1 PG 2A. 2L74 4F RT4A25 20050601000382005060100038WP 2005 6 1 DHL2005807516 120050424A5320 SPLICE DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH86990 45990 AFT CARGO COMPT SPLICE FITTING CRACKED 2.000 (STA 1040.000 - 1060.000, L-31L) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9. TORQUED IAW SRM 51-3-1 PG 2A. 2L74 4F RT4A25 20050601000392005060100039WP 2005 6 1 DHL2005807505 120050427A5753 SKIN DOUG DC8 DC873F 302199FWP T/E FLAP DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH86990 45990 RIGHT INBOARD FLAP AFT LWR PLATING HAS SEVERAL DENTS (STA XW 4.000 - 91.000) (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-7-1 FIG 1. REMOVED DAMAGED PLATING AND FASTENERS WITHIN REPAIR AREA IAW SRM 51-3-0 PG 1, SRM 51-1-21 PG 1. FABRICATED NEW PLATING (AL2024T3 0.032) AND INNER BONDED FINGER DOUBLER (AL2024T3 0.020) IAW SRM 57-7-1 FIG 1. BONDED INNER FINGER DOUBLER ON NEW PLATING IAW SRM 51-1-9, SRM 51-1-9A. CLEANED, TREATED AND PRIMED AREA AND NEW PLATING INTERIOR IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW SRM 51-3-0 PG 1, SRM 51-1-21 PG 1. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050601000402005060100040WP 2005 6 1 DHL2005807506 120050420A5542 SKIN DOUG DC8 DC873F 302199FWP RUDDER DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH86990 45990 RIGHT RUDDER EXTERNAL SKIN INTERIM REPAIR (STA ZR 253.000 - 265.218). PERFORMED MAJOR REPAIR IAW SRM 55-1-0 PG 1, SRM 55-6-1 PG 2. REMOVED PLATING SEGMENT WITH INTERIM REPAIR ON IT IAW SRM 51-1-21 PG 1. FABRICATED NEW PLATING SEGMENT AND FINGER DOUBLER (AL2024T3 0.016) IAW SRM 55-6-1 PG 2. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. BONDED FINGER DOUBLER ON NEW PLATING SEGMENT WITH HYSOL IAW SRM 51-1-9 PG 1, SRM 51-1-9A PG 1. INSTALLED NEW PLATING SEGMENT IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. TORQUED IAW SRM 51-3-1. PERFORMED RUDDER BALANCING IAW SRM 51-4-6 PG 1-4. FOUND WITHIN ALLOWABLE LIMITS. 2L74 4F RT4A25 20050601000412005060100041WP 2005 6 1 DHL2005807519 120050503A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH86990 45990 LEFT WING CTR L/E EXTERNAL SKIN HOLES ELONGATED STA XFS 526.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 04-16-05, EO AST050404 DATED 04-13-05. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. CUT OUT DAMAGED SECTION IAW EOAST 050404. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER (AL7075T60.071) AND 2EA FILLERS (AL7075T6 0.063) IAW EO AST050404. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW EO AST050404, SRM 51-1-21 PG 1, SRM 51-3-0 PG 1, SRM 51-1-20D PG 9. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050601000422005060100042WP 2005 6 1 DHL2005807520 120050505A5315LS3983 FLOORBEAM DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH86990 45990 AFT ACCY COMPT FLOORBEAM UPPER FLANGE CORRODED, STA 1680.000 RBL 26. PERFORMED MAJOR REPAIR. REMOVED FASTENERS FROM REPAIR AREA. REMOVED CORROSION, FOUND OUT OF LIMITS. CUT OUT DAMAGED SECTION IAW SRM 51-2-1 FIG 1 SHEET 7. PERFORMED NDT INSPECTION IAW NDT SPM PART 06-10-01-001. FABRICATED REPAIR ANGLE (EXTRUSION 7075-0-0.125), FILLER (AL7075T6 0.125) IAW SRM 51-2-1 FIG 1 SHEET 7-12. HEAT TREATED IAW SRM 51-1-1 PG 1-13-17, DPS 7.00-1 REV BX. CLEANED, TREATED AND PRIMED REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW SRM 51-2-1 FIG 1 SHEET 7-12, TR 51-130, SRM 51-1-20D PG 9. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050601000432005060100043WP 2005 6 1 DHL2005807521 120050512A5754 BRACKET DOUG DC8 DC873F 302199FWP L/E SLOT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH86990 45990 RIGHT OUTBOARD SLOT MECHANISM BRACKET CRACKED. REMOVED AND REPLACED (1EA) RIGHT OUTBOARD SLOT MECHANISM BRACKET IAW MM 20-16-0 PG 201-202. REFER TO NR 036397 FOR OPS CHECK. 2L74 4F RT4A25 20050601000442005060100044WP 2005 6 1 DHL2005807518 120050505A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01807DH86990 45990 MAIN CARGO COMPT FLOORBEAM MISDRILLED HOLE AT STA 920.000 LBL 32 ON REPAIR DOUBLER. PERFORMED MAJOR REPAIR. REMOVED EXISTING REPAIR AND FASTENERS FROM AREA. FABRICATED REPAIR DOUBLER (AL7075T6 0.1000) REPAIR ANGLE EXTRUSION 7075T6 0.100 HORZ FLANGE 0.070 (VERTICAL FLANGE), REPAIR ANGLE EXTRUSION 7075T6 0.100 HORZ FLANGE 0.083 (VERT FLANGE)) AND STRAP (AL 7075T6 0.050) IAW EO-AST050406. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. PLUGGED MISDRILLED HOLES WITH RIVETS (NAS1097AD8-X, NAS 1097AD5-X) IAW SRM 51-1-21. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW EO AST-050406, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050601000482005060100048WP 2005 6 1 DHL2005807523 120050505A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01807DH86990 45990 MAIN CARGO COMPT FLOORBEAM MISDRILLED HOLE AT STA 960.000 LBL 38 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 04-28-05, EO AST050408 DATED 04-22-05. REMOVED FASTENERS FROM REPAIR AREA IAW SRM 51-1-21 PG 1. PERFORMED VISUAL DETAIL INSP, FABRICATED (1EA) REPAIR STRAP (AL7075T6 0.200) IAW EO AST050408. CLEANED, TREATED AND PRIMED AREA AND NEW STRAP IAW SRM 51-1-8B. REPAIRED AREA PLUGGING MISDRILLED HOLE WITH RIVET (NAS 1097 AD) IAW EO AST050408, SRM 51-1-21 PG 1. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED STRAP IAW EO AST050408, SRM 51-1-20D PG 9. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050601000522005060100052NM 2005 6 1 DHL2005740519 120050329A5311BAC1505100246 FRAME BOEING727 7272Q9 138448MNM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH46106 21930 FRAME BS 720C STR 28 LT AND STR 28 RT FOUND AFTER REMOVING SEALANT (CORROSION) TO BE OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 1. REMOVED LOWER SECTION OF FRAME BS 720C BETWEEN STR 28L TO 28R IAW B727 SRM 51-40-3 FIG 1. EVALUATED LOWER SKIN SECTION OK, NO DAMAGE. NOTED IAW B727 SRM 53-30-1 FIG 1 OF DETAIL 2. FABRICATED FRAME REPAIR FROM P/N BAC 1505-100246, PO 449326 DIM 9.75 X 2 X 1.125 INCH AND FORMED. SECTION P/N 7075 T6 .063 PO 900489, DIM 5.875 X 1 X 1 INCH IAW B727 SRM 51-40-3 FIG 1 AND 53-1-2 FIG 3, TREATED AND PRIMED FRAME, FORMED SECTION AND AREA IAW B727 SRM 51-10-2, INSTALLED FRAME AND FORMED SECTION IAW B727 SRM 51-40-3 FIG 1. 2L73 4F RTA3WE 20050601000532005060100053CE 2005 6 1 DJFA2005093 120050510A3246AHA1814 WHEEL RAYTHNDH125 HAWKER800XP 7150012CE MLG DAMAGED E DJFAD RETURN TO BLOCK Z SIGNIFICANT FAILURE REPORT TXTAXI/GRND HDL 1 EA23808TA 3 258548 THE FOLLOWING IS BEING REPORTED IAW ROC/FAA REQUEST. CREW REPORTED THAT WHILE TAXIING OUT FOR TAKEOFF, THE NR3 MAIN WHEEL CAME APART. THE LT AFT BELLY DRAIN MAST WAS DAMAGED FROM THE WHEEL ASSEMBLY. MAINTENANCE REPLACED THE NR3 MAIN WHEEL ASSEMBLY. THE LT AFT BELLY DRAIN MAST WAS ALSO REPLACED AND A HIDDEN DAMAGE VISUAL INSPECTION WAS CARRIED OUT FOR THE AREA OF THE LT WHEEL WELL AND AIRCRAFT VENTRAL AREA. NO DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA3EU 20050601000542005060100054CE 2005 6 1 DJFA2005095 120050513A3246 WHEEL RAYTHNDH125 HAWKER800XP 7150012CE GARRTTTFE731TFE7315BR WP LEFT SEPARATED E DJFAO OTHER Z SIGNIFICANT FAILURE REPORT TXTAXI/GRND HDL 1 EA23817TA 258552 THE FOLLOWING IS BEING REPORTED IAW REQUEST OF ROC/FAA. WHILE TAXIING AIRCRAFT FOR A STEERING OPERATIONAL CHECK A LOUD BANGING NOISE WAS HEARD IN THE AIRCRAFT CABIN AREA. UPON FURTHER INVESTIGATION IT WAS DISCOVERED THAT A LT IB WHEEL HALF WAS MISSING AND THERE WAS DAMAGE TO THE CENTER FUSELAGE AREA. 2L72 4F4 FRTA3EU E6WE 20050601000572005060100057NM 2005 6 1 AALA20050327 120050513A3260 SWITCH BOEING737 737823 13844BZNM LANDING GEAR MALFUNCTIONED A AALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW21941AN 29534 MIA - AIR/GROUND SWITCH DID NOT CYCLE ON TAKEOFF. LANDING GEAR OVERRIDE USED TO RAISE GEAR. WARNING HORN ON WITH FLAPS UP. RECONFIGURED AND LANDED. PSEU LIGHT LIT ON TAXI OUT BUT EXTINGUISHED ON RESET. LANDED MIA WITHOUT INCIDENT. PSEU LIGHT LIT ON TAXI BACK AND WOULD NOT RESET. ACCOMPLISHED ALL REQUIRED TESTS ON GROUND INSPECTED CONNECTORS (SPECIAL ITEMS CARD 7900). FUNCTIONAL CHECK FLIGHT LANDING GEAR AND TAKEOFF WARNING SYSTEM WORKED NORMALLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20050601000582005060100058NM 2005 6 1 AALA20050332 120050516A7920 FILTER BOEING737 737823 13844BZNM CFMINTCFM567CFM567B22 13802NE NR 2 ENGINE DIRTY A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21931AN 30079 874589 RDU - NUMBER 2 ENGINE OIL BYPASS WARNING CAME ON DURING CLIMBOUT WITH CLIMB POWER. RETURNED TO RDU AND LANDED WITHOUT INCIDENT. REPLACED OIL SUPPLY AND SCAVENGE FILTER. RAN ENGINE AT TAKEOFF SPEED FOR THREE MINUTES. ALL INDICATIONS NORMAL. ENGINEERING REQUESTED DOWNLOAD OF FLIGHT DATA RECORDER FOR EVALUATION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA16WE E00055EN 20050601000602005060100060NM 2005 6 1 AALA20050333 120050505A5312 PRESSURE PANEL BOEING757 757223 1384957NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21694AN 26974 TUL - CORROSION FOUND IN RIGHT HAND WHEEL WELL ON LOWER SIDE OF PRESSURE DECK ABOVE SLIDE BOX. SIX SEPARATE CUTOUTS AT STATIONS 1140 TO 1180, RIGHT BUTTLINE 40 TO RIGHT BUTTLINE 70 AND 50. LARGEST IS 2 INCHES BY 2.5 INCHES. 2L72 4F RTA2NM 20050601000612005060100061NM 2005 6 1 AALA20050334 120050425A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21934AN 29531 TUL - CEILING EMERGENCY LIGHTS AT FORWARD ENTRY INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT FORWAD ENTRY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20050601000622005060100062NM 2005 6 1 AALA20050336 120050505A5320 SILL BOEING767 767323 1385205NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21371AA 25198 AFW - LOWER MAIN SILL OUTER CHORD HAS CORROSION REMOVAL ON VERTICAL LEG INBOARD SURFACE. AREA IS 1.6 INCH BY 3.2 INCH WITH A DEPTH OF 0.039 INCH. BLENDED OUT CORROSION. NO CRACKS FOUND ON HIGH FREQUENCY EDDY CURRENT. REFINISHED THE BLENDED AREA PER SRM. ENSURED SURFACE WAS FLAT FOR PROPER FASTENER INSTALLATION. RETURNED TO SERVICE WITH NOTED CONDITION. 2L72 4F RTA1NM 20050601000632005060100063WP 2005 6 1 AALA20050330 120050516A3350P4010049 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21560AA 53090 LGA - FORWARD EMERGENCY ESCAPE PATH LIGHTING AND FORWARD EXIT SIGN AT LEFT ONE DOOR AND FORWARD GALLEY DOOR INOPERATIVE. REPLACED BATTERY PACK ON AB51 CONTROL MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050601000642005060100064NM 2005 6 1 AALA20050326 120050512A3350 LIGHT BOEING767 767323 1385205NM EXTERIOR INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21363AA 24044 DFW - LOWER AFT EMERGENCY LIGHT ON FUSELAGE INOPERATIVE. REPLACED LIGHT FOR LOWER AFT EMERGENCY LIGHT ON LEFT FUSELAGE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050601000662005060100066EU 2005 6 1 AALA20050331 120050516A3350321441 BATTERY PACK AIRBUS300 A300B4605R 3930308EU CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW217083A 645 JFK - RIGHT NUMBER 3 DOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT RIGHT NUMBER 3 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20050601000672005060100067 2005 6 1 AALA20050335 420050421A25655A33073 SLIDE BOEING737 737823 13844BZNM EMERGENCY ESCAPEFAILED A AALAK NONE O OTHER ININSP/MAINT 1 SW21933AN 30080 TUL - EMERGENCY ESCAPE SLIDE AT STATION 326 HAD TO BE INFLATED MANUALLY. REPLACED EMERGENCY ESCAPE SLIDE AT STATION 326. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20050601000682005060100068EU 2005 6 1 MALA050396 120050503A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15449XJ 340B449 SEAT TRACK AT LBL 18.3, FROM FS 297 TO FS 319 IS CORRODED. DAMAGE HAS BEEN REPAIRED AS REQUIRED IAW SRM 53-70-60. REF: EAMS WORK ORDER 212113 TASK 1505. 2L72 4T RTA52EU 20050601000692005060100069EU 2005 6 1 MALA050404 120050501A7931 WARNING SYSTEM SAAB SF340 340B 7860101EU COCKPIT ACTIVATED A MALAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL15422XJ 340B422 CREW RETURNED TO DTW AFTER DEPARTURE DUE TO ENGINE 1 LOW OIL PRESSURE INDICATION. EMERGENCY WAS NOT DECLARED AND EMERGENCY TRUCKS WERE CALLED OUT AS A PRECAUTION. NO FURTHER INFORMATION AT THIS TIME. 2L72 4T RTA52EU 20050601000722005060100072EU 2005 6 1 MALA050414 120050516A5320 FLOOR SUPPORT BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15519XJ E2344 DURING C3 CHECK IN YYC, FOUND FRAME 37 FLOOR SUPPORT ANGLE IN CARGO PIT IS CORRODED BEYOND LIMITS BETWEEN STR 27L ABD 27R. 2H74 4F RTA49EU 20050601000732005060100073EU 2005 6 1 MALA050415 120050516A5320 FLOOR SUPPORT BAC 146 AVRO146RJ85A1500097EU FUSELAGE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15519XJ E2344 DURING C3 CHECK IN YYC, FOUND FRAME 35 FLOOR SUPPORT ANGLE IS CRACKED IN 3 PLACES IN THE AFT CARGO PIT. 2H74 4F RTA49EU 20050601000742005060100074EU 2005 6 1 MALA050405 120050509A3350 POWER SUPPLY SAAB SF340 340B 7860101EU CABIN FAILED A MALAK NONE O OTHER ININSP/MAINT 1 GL15422XJ 340B422 EMERGENCY POWER SUPPLY FAILED BATTERY CAPACITY CHECK TEST. REMOVED AND REPLACED EMERGENCY POWER SUPPLY IAW SAAB MM 33-50-10-4. 2L72 4T RTA52EU 20050526001352005052600135EA 2005 5 26 SWIA200514977 120050429A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07961SW 7857 FS 280 AT RBL 9.0 INBOARD AND OUTBOARD FLOORBEAM ATTACH ANGLES CRACKED. ITEM FOUND AT C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-21-11, 51-25-16, 51-23-00. 2L72 4F RTA21EA 20050526001382005052600138EA 2005 5 26 SWIA200514980 120050507A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07935SW 7725 LAST EMERGENCY LIGHT PAD ON CEILING INOPERATIVE. RELAMPED LAST CEILING EMERGENCY LIGHT IAW MM CHAPTER 33-50-00, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050526001482005052600148NM 2005 5 26 72300178 120050416A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 8 INCH BY 3 INCH AREA OF CORROSION ON STRINGER. 2L73 4F4 FRTA3WE E2EA 20050526001552005052600155SO 2005 5 26 C2XA05SH034 120050513A532014521700007 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2748901 145501 SHV - DURING C-CHECK THE LT OMEGA BEAM HAS CORROSION AT VARIOUS AREAS BETWEEN FRM 29-36. MAINTENANCE REPAIRED LT OMEGA BEAM AT FRM 29 IAW EC5320-01237 AND EC5320-01137. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050526001562005052600156WP 2005 5 26 ARWA20050505 120050511A2612 CONNECTOR DOUG DC8 DC863F 302198FWP FIRE DETECTOR DIRTY A ARWAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SO19784AL 46135 DURING MAINTENANCE INSPECTION, NR 2 FIRE WARNING DOES NOT TEST; NO LIGHT; NO BELL. CLEANED NR 2 FIRE CONNECTOR WARNING; OPERATIONAL CHECK TEST NORMAL IN ACCORDANCE WITH M/M 26-10-0. 2L74 4F 4A25 20050526001592005052600159NE 2005 5 26 ASMF200505014 220050509A72614958982501 BOLT DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE OIL SYSTEM FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23169PL 53175 718246 AIRCRAFT RETURNED TO PLATFORM, DURING RT ENGINE START, THE LOW PRESSURE LIGHT DID NOT TURN OFF AND THE INDICATION WAS ZERO, N2 REACHED 35 PERCENT AND IT DID NOT INCREASE. THE OIL LEVEL AND RT ENGINE WERE VERIFIED, BEING CORRECT, MAIN OIL FILTER WAS REMOVED AND IT WAS CLEAN. THE PRESSURE TX LINE WAS BLOWN IAW MM 79-33-01. THE RT ENGINE WAS STARTED IAW MM 71-00-01, TESTED CORRECT. DURING OVERNIGHT SERVICE, LV3 AND LP2 RESTRICTOR WERE REPLACED AND THE PRESSURE TX LINE AND OIL RESTRICTOR WAS BLOWN IAW MM 79-33-01, OIL PRESSURE TRANSMITTER WAS REPLACED IAW MM 79-33-01. RT ENGINE WAS TESTED IAW MM 71-00-01, ALL CORRECT. 2L72 4F4 FRTA6WE E9NE 20050526001602005052600160NE 2005 5 26 ASMF200505015 220050512A7261 O-RING DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE RT ENGINE LEAKING W ASMFD RETURN TO BLOCK KMJFLUID LOSS OVER TEMP WARNING INDICATION TXTAXI/GRND HDL 1 SW23831LF 53050 716778 AIRCRAFT RETURNED TO PLATFORM, LOW ACCELERATION (1.4 OF EPR) AND HIGH TEMPERATURE (600°C). DURING CHECK, THE RT ENGINE ACCELERATION CHAMBER WAS SERVICED, TESTS WERE PERFORMED TO BOTH ENGINES IAW MM 71-00-00, BEING CORRECT. DUE TO ART WAS INOPERATIVE, IT WAS DEFERRED IAW MEL 73-8. DURING OVERNIGHT SERVICE, RT ENGINE WAS CHECKED BY LEAKS ON PT2 AND PT7 LINES, BEING CORRECT. EPR TRANSMITTER AND RT ENGINE BULLET O-RING WERE CHECKED, ALL CORRECT. TRIM TO BOTH ENGINES WAS PERFORMED IAW MM 76-11-00, TESTED CORRECT. 2L72 4F4 FRT E9NE 20050526001702005052600170NM 2005 5 26 SWAA051381 120050511A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 16R. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050526001732005052600173WP 2005 5 26 ASMF200505013 120050511A322039567851 LINK ASSY DOUG DC9 DC9* WP NLG DAMAGED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23501AM112822917 49188 DURING TRANSIT CHECK AT PLATFORM, A RIGHT NOSE GEAR FORWARD DOOR WAS DETECTED OPEN. SAFETY MECHANISM WAS VERY HARD. AIRCRAFT WAS SENT TO THE HANGAR AND NOSE LANDING GEAR DOOR ACTUATORS WERE REPLACED IAW MM 32-22-01, TESTED CORRECT. 2L72 4F A6WE 20050526002042005052600204WP 2005 5 26 UPS05844441 120050421A53404750419U501 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE:C1 MAIN CABIN AT STA 1160 L18R FRAME ATTACH FITTING CRACKED 1 INCH LONG. REMOVED AND REPLACED FRAME ATTACH FITTING IAW DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20050526002072005052600207WP 2005 5 26 0500719983 120050320A5347 SEAT TRACK DOUG DC9 DC932 3022066WP FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01983US 47282 DURING H-CHECK FOUND CORROSION ON SEAT TRACK AT BS 239 LBL 25. REPAIRED PER EA 99-202920. 2L72 4F A6WE 20050526002112005052600211EA 2005 5 26 SWIA200514988 120050504A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07423SW 7456 FS 460 RIGHT FLOORBEAM RBL 9.0 OUTBOARD FITTING CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED FITTING IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21. 2L72 4F RTA21EA 20050526002142005052600214EA 2005 5 26 SWIA200514991 120050504A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07423SW 7456 AFT EQUIPMENT COMPARTMENT INTERCOSTAL CLIP IS CRACKED; FS 625.00 STR 14R. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED INTERCOSTAL CLIP AT FS 625, STR 14R IAW CRJ REO 601R-53-61-100 AND 601R-53-61-422. 2L72 4F RTA21EA 20050526002332005052600233CE 2005 5 26 CIEA200500003 120050514A1420 WIRE LEAR 35 35A 5170602CE ELECTRIAL CONNECBROKEN E CIEAK NONE O OTHER ININSP/MAINT 1 NM03553V 11340212 35A141 DURING COMPLIANCE OF AD 82-01-05 R2, THE TEST OF THE STALL WARNING ACCELEROMETER FAILED TO FUNCTION PROPERLY. WHEN THE ACCELEROMETER WAS ROTATED PAST THE 45 DEGREE POSITION THE PULLER WOULD NOT WORK AT ALL. IN THE PROCESS OF TROUBLESHOOTING THE SYSTEM, TWO WIRES ATTACHED TO THE CONNECTOR OF THE ACCELEROMETER WERE FOUND BROKEN LOOSE. THE WIRES WERE RESOLDERED ONTO THE CANNON PLUG AND THE SYSTEM WORKED NORMAL. PROBABLE CAUSE. THE WIRES ARE VERY SMALL, AND DUE TO THE CONTINUED TESTING OF THE SYSTEM, HAD BEEN FLEXED SO MANY TIMES THAT THE FINALLY BROKE. ADDITIONAL NOTE: IN THE PROCESS OF TROUBLE SHOOTING THIS AIRCRAFT, THE ACCELEROMETER WAS REMOVED FROM ANOTHER AIRCRAFT. DURING THAT PROCESS, A WIRE WAS BROKE2L72 4F A10CE 20050526002392005052600239NM 2005 5 26 DHL2005740508 120050407A5330 SKIN BOEING727 7272Q9 138448MNM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 ACCOMPLISHED IDENTIFICATION OF EXISTING REPAIR ON FUSELAGE SKIN AT STA 1148 AND STRINGER 29L PER ASTAR J/C FCD 500001-001B. REMOVED EXISTING REPAIR AT STA 1148 AND STR 29L IAW B727 SRM 51-30-2, DRAIN MAST REMOVED IN EA 38100001-001B. CUT OUT DAMAGE AT SKIN DIMENSION 10 X 8.5 INCH IAW B727 SRM 53-30-3 FIG 3, FABRICATED REPAIR DOUBLER FROM 2024T3 .125 PO9001873 DIMENSIONS 19 X 18 INCH AND 2EA FILLERS FROM 2024T3 .100 PO9001576 DIMENSION 10.25 X 1 INCH IAW B727 SRM 53-30-3 FIG 3. TREATED AND PRIMED IAW B727 51-10-2. INSTALLED REPAIR DOUBLER AND FILLERS IAW B727 SRM 53-30-3 FIG 3. THIS IS CATEGORY B. 2L73 4F RTA3WE 20050526002522005052600252EU 2005 5 26 05FDEA01238 120050512A5313 STRINGER AIRBUS310 A310203 3930313EU FUSLEAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25403FE 230 UNDER FLOOR AREA BEHIND FWD PIT FR 38.2 TO FR 39 STR 54L HAS CORROSION ON STRINGER EXTENDING AROUND AND UNDER FASTENERS, FOUND WHILE CLEANING FOR CIC APPLICATION. REMOVED CORROSION IAW A310-200 SRM 51-74-10. UPON CORROSION REMOVAL 17 AREAS ON ANGLE REINFORCEMENT WENT OUT OF LIMITS IAW A310-200 SRM 53-10-00. REMOVED AND REPLACED ANGLE AND SPLICE REPAIR IAW SRM 51-72-10 AND 51-71-40. RESTORED PROTECTIVE COATING AND PART MARKING IAW A310-200 SRM 51-75-10, 51-23-10, AND GMM CHAPTER 9. 2L72 4F RTA35EU 20050526002532005052600253EU 2005 5 26 05FDEA01239 120050512A5720 PLATE AIRBUS310 A310203 3930313EU RT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25403FE 230 RIGHT WING AILERON LANDING PLATE AREA BETWEEN STA WAIX-7.35 AND WAIX-14.7 JUST FWD OF AILERON HAS 2 EACH HOLES OVERSIZED AT 0.328 AND 0.371 DIAMETER, WORK CARD E6-5710- 7-5008A PT 4 REQUIRES THESE HOLES TO BE REAMED UP TO 0.313 DIAMETER. COMPLIED WITH EA 6-5730-88784, RAS/BAE/1000692/2005 ISSUE A. 2L72 4F RTA35EU 20050526002562005052600256EU 2005 5 26 05FDEA01242 120050512A5320 BRACKET AIRBUS310 A310203 3930313EU FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25403FE 230 COCKPIT STA 904/FR 7, NUT PLATE BRACKET IS CRACKED 0.5 INCH. REMOVED BRACKET IAW A310-200 SRM 51-40-21. FABRICATED NEW BRACKET IAW EA 6-5610- 89174. INSTALLED NEW BRACKET IAW A310-200 SRM 51-72-10. REMOVED AND REINSTALLED STRIP PANEL IAW A310-200 SRM 51-40-10. REPAIR IS CLASSIFIED AS A MINOR REPAIR. 2L72 4F RTA35EU 20050526002572005052600257EU 2005 5 26 05FDEA01243 120050512A5320 ANGLE AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25403FE 230 AFT CARGO PIT FORWARD AREA L-ANGLE IS CORRODED, AFT OF FR 54. REMOVED CORROSION IAW A310-200 SRM 51-74-10. MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW A310-200 SRM 53-10-00. REMOVED, FABRICATED AND INSTALLED L-ANGLE RT IAW A310-200 SRM 51-40-10. ALSO FOUND CENTER L-ANGLE CORRODED OUT OF LIMITS. REMOVED, FABRICATED AND INSTALLED CENTER L-ANGLE IAW A310-200 SRM 51-40-21. SURFACE TREATED IAW A310-200 SRM 51-21-10. 2L72 4F RTA35EU 20050526002722005052600272NM 2005 5 26 05FDEA01268 120050513A5320A5A7114519 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25621FE 48792 CENTER CARGO - RIGHT HAND UTILITY TUNNEL AT STA 1531 L-37 RIGHT HAND LONGERON SPLICE FOUND CRACK. REMOVED AS PER SRM 51-33-01 VOLUME II. NEW SPLICE FABRICATED AS PER DRAWING A5A7114 AND INSTALLED AS PER SRM 51-33-01 VOLUME II. REPAIR IS CLASSIFIED MAJOR PER GMM 6-2-100. 2L73 4F RTA22WE 20050526002802005052600280NM 2005 5 26 05FDEA01259 120050512A531269648411 DOUBLER BOEING727 727233 138408ANM BULKHEAD CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25254FE 20936 FUSELAGE STA 740 BULKHEAD SUPPORT DOUBLER CORROSION. COMPLIED WITH EA 7-5310-55482 FUSELAGE STA 740 BULKHEAD SUPPORT DOUBLER CORROSION AT MAE. THIS IS A MAJOR REPAIR. 2L73 4F RTA3WE 20050607000092005060700009EA 2005 6 7 QXEA200500882 120050503A5751 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 500 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - LEFT WING AILERON UPPER SKIN FORWARD AREA HAS CHAFE MARKS. REPAIRED IAW CRJ-700 SRM 51-41-00-001-A01, 51-12-00-001-001-A01, 51-25-00-001-001-A01 AND 51-41-02-001-001-A01. 2L72 4F RTA21EA 20050606000722005060600072NM 2005 6 6 05FDEA01296 120050515A5511ALC8131502 SPAR CAP DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25621FE 48792 HORIZONTAL STABILIZER RIGHT HAND AFT SPAR CAP NR 36R BARREL NUT BORE CORROSION REMOVAL FOUND EXCEEDED LIMITATIONS. REWORKED AS PER FEDEX EA 1-5510-83007. 2L73 4F RTA22WE 20050531000142005053100014WP 2005 5 31 ABXA050107 120050512A2810 FUEL CAP DOUG DC9 DC931 3022065WP LT WING DEFECTIVE A ABXAA UNSCHED LANDING K FLUID LOSS CLCLIMB 1 GL23946AX 47003 AFTER TAKEOFF, TOWER ADVISED FUEL VENTING FROM LEFT WING. AIR TURNBACK, MADE RETURN TO ILN. LOST 1000 LBS OF FUEL IN FLIGHT. EMERGENCY DECLARED BY TOWER. FOUND LEFT OVER THE WING FILL CAP POPPED. CAP FOUND TO BE NOT LOCKING. REMOVED AND REPLACED LEFT OVERWING FILL CAP IAW DC9 AMM 28-10-04-20. 2L72 4F A6WE 20050531000192005053100019NM 2005 5 31 AWXA200500562 120050513A2410735511A CSD BOEING737 7373Y0 1384671NM NR 1 ENGINE FAILED A AWXAA UNSCHED LANDING JH WARNING INDICATION ELECT. POWER LOSS-50 PC CRCRUISE 1 WP28323AW4927511555 23684 EN ROUTE NR 1 CONSTANT SPEED DRIVE (CSD) LOW OIL PRESSURE LIGHT ILLUMINATED & NR 1 GENERATOR DROPPED OFF LINE, APU ALREADY ON MEL, DIVERTED INTO RNO FOR REPAIR. MX R & R NR 1 CSD / GENERATOR IAW T/C R5M24007, AND CSD OIL COOLER AND IN-LINE FILTER IAW T/C R5M24008, OPERATIONAL CHECK OF NR 1 CSD / GENERATOR GOOD. TEAR DOWN REPORT OF CSD CONFIRMS FAILURE. WHEN CSD OPENED, FOUND UNIT FULL OF METAL & SEVERAL COMPONENTS SEIZED/DAMAGED. TEAR DOWN OF CSD SHOWS CARRIER SHAFT BORES CLOGGED WITH DEBRIS CAUSING A LACK OF LUBE TO GEARS WITH ASSOCIATED LOW OIL PRESSURE LIGHT ILLUMINATING. THIS CAUSED PLANET GEAR & SHOULDER SHAFT TO SEIZE TOGETHER, DROPPING GENERATOR OFF LINE. UNIT WAS OVERHAULED AND RE-TESTED IAW CMM. 2L72 4F RTA16WE 20050531000272005053100027WP 2005 5 31 UPS05844445 120050421A53204750419U501 ATTACH FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE:C1 MAIN CABIN AT STA 1160 L19R FRAME ATTACH FITTING CRACKED .5 INCH LONG. REMOVED AND REPLACED FRAME ATTACH FITTING IAW DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20050531000312005053100031WP 2005 5 31 UPS05844449 120050421A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE:C1 LONGERON 15R CRACKED 1 INCH LONG AT STA 1757. REMOVED AND REPLACED LONGERON SECTION AND INSTALLED SPLICE FITTING IAW DC-8 SRM 53-2-2 FIG 10 AND 51-1-20D. 2L74 4F RT4A25 20050531000342005053100034WP 2005 5 31 UPS05844452 120050422A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE:C1 LONGERON CRACKED .5 INCH LONG AT STA 1746 L5R. REMOVED AND REPLACED LONGERON SECTION AND INSTALLED SPLICE FITTING IAW DC-8 SRM 53-2-2 FIG 10 AND 51-1-20D. 2L74 4F RT4A25 20050531000642005053100064NM 2005 5 31 CALA0500150 120050515A5315141A5505 FLOORBEAM BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2726210 28770 INSPECTION FOUND FLOORBEAM CORRODED AT STA 344, RBL 8 TO LBL 12. REPAIRED IAW ECRA 5321-01219. 2L72 4F RTA16WE 20050531000672005053100067NM 2005 5 31 CALA0500153 120050515A5315147A55067 FLOORBEAM BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2726210 28770 INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, BL 0 TO RBL 12. THE FLOORBEAM WAS REPAIRED IAW ECRA 5321-01220. 2L72 4F RTA16WE 20050531000732005053100073SO 2005 5 31 RAIA00505003 120050507A21208151136 DUCT EMB 145 EMB145LR 3260212SO NR 2 PACK BLOWN A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03814HK 145046 FLT - 5498 - STL - PACK 2 OVERLOAD INDICATION. MAINTENANCE REMOVED AND REPLACED BLOWN DUCT AT NR 2 PACK. 2L72 4T RTT00011AT 20050531000742005053100074 2005 5 31 RAIA00505005 420050509A34257011672112 SYMBOL GENERATOR JETAIRJETSTMJETSTM4101 1500501EU COCKPIT FAILED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03572HK11537 41091 FLT - 3672 - EADI AND EAHSI WENT BLANK FO SIDE. MAINTENANCE REMOVED AND REPLACED FO'S SYMBOL GENERATOR. 2L72 4T RTA41NM 20050531000752005053100075 2005 5 31 RAIA00505006 420050509A612231057165 GOVERNOR JETAIRJETSTMJETSTM4101 1500501EU NR 2 MALFUNCTIONED A RAIAC ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 CE03568HK2543 372 41086 FLT 3680 - RIC - LEFT ENGINE LOW TORQUE. MAINTENANCE REMOVED AND REPLACED NR 2 PROP GOVERNOR. 2L72 4T RTA41NM 20050531000782005053100078EU 2005 5 31 RAIA00505009 120050512A3260 UPLOCK SWITCH JETAIRJETSTMJETSTM4101 1500501EU RT MLG DIRTY A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03561HK 41077 FLT 5469 - STL - RED LIGHT IN GEAR HANDLE STAYED ON AFTER RETRACTION. MAINTENANCE CLEANED RT UPLOCK SWITCH. 2L72 4T RTA41NM 20050531000802005053100080NM 2005 5 31 TSAA0521021 120050511A213171211997101AC CONTROLLER BOEING737 73776N 13844CHNM NR 2 MALFUNCTIONED A TSAAK NONE S AFFECT SYSTEMS CLCLIMB 1 WP13741AL 28641 OAK - HNL: AFTER T/O CLIMB, CABIN ALTITUDE STUCK AT 0. SWITCHED TO ALTERNATE, BUT NO CHANGE. CONTINUED TO CLIMB IN MANUAL MODE. SWITCH BACK TO AUTO AT CRUISE, OKAY. FURTHER STEP CLIMB HAD TO BE DONE IN MANUAL. ALL QRH PROCEDURES ACCOMPLISHED. REMOVED AND REPLACED THE NR 2 PRESSURE CONTROLLER PER MM 21-31-01-000-801 AND 21-31-01-400-801. BITE TEST FOR NR 1 AND NR 2 CONTROLLER SHOWED NO FAULT. AIRCRAFT RETURNED TO SERVICE. VERIFICATION FLIGHT GOOD (5/12/05). 2L72 4F RTA16WE 20050531000832005053100083NM 2005 5 31 AMTA200500423 120050505A5420 SHIM BOEING757 75723N 1384973NM NR 1 STRUT MIGRATED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11519AT 27975 BULKHEAD/FIREWALL, NR 1 ENGINE STRUT MID BULKHEAD HAS MIGRATING SHIMS AT FORWARD OUTBOARD LOWER MID SPAR BOLT ATTACH POINT PP STATION 174. COMPLIED WITH PART 2 OF ERA 757-54R-5870. (M) 2L72 4F RTA2NM 20050531000842005053100084NM 2005 5 31 AMTA200500410 120050503A335020131A BATTERY PACK BOEING757 75723N 1384973NM CABIN DISCHARGED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11519AT 27975 BULLNOSE EMERGENCY LIGHT AT ROW 31DEF INOPERATIVE. REPLACED BATTERY PACK FOR EGRESS LIGHTS PER AMM 33-51-07-2, OPS NORMAL. (M) 2L72 4F RTA2NM 20050531000912005053100091EU 2005 5 31 USAA050558 120050428A53151160824 FLOORBEAM AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19105UW 0868 PIT - FOUND BEAM CORRODED .125 INCH TO .25 INCH, AROUND NUTPLATE HOLES ON FLOORBEAM Y425L FROM C21-C23. REPLACED BEAM PER DWG 53110900. (M) 2L72 4F RTA28NM 20050531000952005053100095EU 2005 5 31 USAA050557 120050429A5347D534720900200 SEAT TRACK AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19105UW13610 0868 PIT - FOUND SEAT RAIL CORRODED 2 INCHES BY 2 INCHES, Y765 LET FLOORBEAM, TOP SURFACE AT BARREL NUT HOLE AT FRAME 66. REMOVED AND REPLACED ORIGINAL PART PER AIRBUS DWG D53472780 AND SRM 53-31-15. (M) 2L72 4F RTA28NM 20050531000982005053100098NM 2005 5 31 USAA050553 120050428A574365C3649223 SUPPORT BEAM BOEING737 7373B7 1384580NM LT WING CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19374US56183 22953 BFM - FOUND AFT SUPPORT BEAM CRACKED, LT MLG BEAM AFT SUPPORT FITTING ON AFT SPAR, APPROX WBL 157.0 S1 WING. REMOVED FASTENERS, PERFORMED NDT INSPECTION, REINSTALLED FASTENERS PER TYPICAL REPAIR 57-40-13 REV A. (M) 2L72 4F RTA16WE 20050531001002005053100100NM 2005 5 31 AMTA200500424 120050505A5420 SHIM BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE NR 2 STRUT MIGRATED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11519AT 27975 BULKHEAD/FIREWALL, NR 2 ENGINE STRUT MID BULKHEAD HAS MIGRATING SHIMS AT FWD IB AND OB LOWER MID SPAR BOLT ATTACH POINTS PP STA 174. COMPLIED WITH PART 1 OF ERA. (K) 2L72 4F4 FRTA2NM E12EU 20050531001022005053100102 2005 5 31 KBM2005F00047 420050428A34205040017907 GYRO SNIAS 350 AS350B2 8680813EU COCKPIT FAULTY E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19751H 3403 ALTITUDE GYRO 10 DEGREES OFF DURING TURNS. REMOVED AND REPLACED. (M) 1G71 3U H9EU 20050531001032005053100103EA 2005 5 31 A6WA200540162 120050430A5753 CHANNEL CNDAIRCL600 CL6002B19 1900309EA T/E FLAP CRACKED A A6WAK NONE O OTHER NRNOT REPORTED 1 GL31451AW 7832 LEFT OUTBOARD FLAP T/E PUSHED FORWARD, .375 INCH WIDE BY .0625 INCH DEEP. REPAIRED LEFT OUTBOARD FLAP TRAILING EDGE. REMOVED CRACKED CHANNEL P/N 601R14538-3 AND INSTALLED SERVICEABLE CHANNEL P[/N 601R14538-3, IAW CRJ 200 SRM 51-25-01, 51-42-06, 51-42-10 AND BOMBARDIER DRAWING 601R14501. (M) 2L72 4F RTA21EA 20050531001082005053100108WP 2005 5 31 GTIA050151 120050429A5320 CHANNEL DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23829NK 49931 FTW - FOUND MAIN CABIN, LEFT SIDE WEB PANEL STATION 826 TO 927 CRACKED/DAMAGED AT HAT SECTION. REMOVED DAMAGED CRACK AREA FROM HAT CHANNEL. FABRICATE FILLER AND DOUBLER. TREAT, PRIMED AND INSTALLED REPAIRED FILLER AND DOUBLER. (M) 2L72 4F A6WE 20050531001172005053100117SO 2005 5 31 SIMA200511701 120050420A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21807AE8257 145506 THE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. PERFORMED A CUT OUT TO REMOVE THE CORROSION. FABRICATED A DOUBLER, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (SW21200505714) (K) 2L72 4F4 FRTT00011ATTE6CH 20050531001222005053100122SO 2005 5 31 SIMA200511704 120050420A531514521721009 FLOORBEAM EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21645AE11610 145212 THE GALLEY FORWARD DIGITAL WAS FOUND TO BE CORRODED. BLENDED THE CORRODED AREA. FABRICATED A DOUBLER AND INSTALLED. REPAIR DONE IAW SRM. (SW21200505716) (K) 2L72 4T4 FRTT00011ATTE6CH 20050531001272005053100127WP 2005 5 31 GTIA050140 120050413A5320 BRACKET DOUG DC9 DC982 3022082WP A/C BAY CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23829NK 49931 AFT ACCY COMPT, OVERHEAD CANT 1463, HAND RAIL SUPPORT ROD MOUNT BRACKET IS CRACKED. REMOVED AND FABRICATE NEW BRACKET. TREATED AND PRIMED. REPAIRED BRACKET INSTALLED. (M) 2L72 4F A6WE 20050531001312005053100131SO 2005 5 31 SIMA200512201 120050427A533014000194003 SKIN PANEL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE GOUGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21693AE 14500868 DURING REPAIR OF TDMI 53003E, FOUND 2 SCRATCHES ON RT SIDE OF AIRCRAFT BELOW PASSENGER WINDOW BETWEEN FRAMES 24 AND 25 AND STRINGERS 13R AND 12R. MAINTENANCE APPLIED PATCH IAW SRM. AIRCRAFT RETURNED TO SERVICE. (SW21200505707) (K) 2L72 4T4 FRTT00011ATTE6CH 20050531001342005053100134NM 2005 5 31 2005UALA00374 120050419A21636240162SER1 SENSOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE MIX MANIFOLD FAILED A UALAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 WP29526UA 24994 COCKPIT TEMPERATURE RISING & UNCONTROLLABLE. CAUSE ATTRIBUTED TO A MIX MANIFOLD SENSOR. REPLACED SENSOR. 2L72 4F4 FRTA2NM E17NE 20050531001352005053100135NM 2005 5 31 2005UALA00414 120050506A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29586UA 26710 AFT PIT FRAME DENTED STA 1420 BETWEEN STR 25 & 26 LEFT. DAMAGE WAS CUTOUT OF FRAME AND REPAIR ANGLES INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050531001442005053100144NM 2005 5 31 2005UALA00423 120050506A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29586UA 26710 AFT PIT FRAME DENTED STA 1560, STR 26R. FRAME DENT WAS TRIMMED OUT AND J ANGLE REPAIR INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050531001762005053100176WP 2005 5 31 GTIA050096 120050310A5230 SKIN DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE CARGO DOOR DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 DENT ON AFT CARGO DOOR SKIN 21 INCHES FROM AFT EDGE AND 11 INCHES FROM BOTTOM EDGE OF DOOR (X=0.035 INCH, D=1.75 INCH, D/X=50). STRIPPED AREA OF DENT ON AFT CARGO DOOR FS 1185 IS UNDER CONDITION IAW SRM. DYE PENETRANT INSP, NO CRACK FOUND. REMOVED LATCH HANDLE MECHANISM PAN GOUGED BEYOND 50 PERCENT IN CUP. CUT OUT DENT AREA (1.5 INCH DIAMETER) IAW SRM. FAB FILLER AND REPAIR DOUBLER IAW SRM. TREATED AND PRIMED, INSTALLED DOUBLER AND FILLER. INSTALLED DOOR PAN HANDLE AND MECHANISM IAW SRM. (K) 2L72 4F4 F A6WE E9NE 20050531001782005053100178 2005 5 31 ASMF200505016 420050514A2340 INTERPHONE DOUG MD80 MD83 3023681NM CABIN MALFUNCTIONED W ASMFD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SW23831LF 53050 DURING TRANSIT CHECK INTERCOMMUNICATION SYSTEM WAS DETECTED OUT SERVICE. MAINTENANCE TEST WAS PERFORMED IAW MM 23-40-00, ALL CORRECT. AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF INTERCOMMUNICATION SYSTEM FAIL. MAINTENANCE PROCEDURE TEST WAS PERFORMED IAW MM 23-40-00, TESTED CORRECT. 2L72 4F RT 20050531001792005053100179NM 2005 5 31 P9RA20050081 120050516A3350767 LIGHT BOEING757 757231 1384950NM EXTERIOR INOPERATIVE A P9RAK NONE L NO TEST ININSP/MAINT 1 SO11720TW 30319 AIRCRAFT IN MAINTENANCE, DURING LINE CHECK FOUND DOOR 4R SLIDE LIGHT INOPERATIVE. RELAMPED DOOR 4R SLIDE LIGHT IN ACCORDANCE WITH THE M/M. CHECKED GOOD. 2L72 4F RTA2NM 20050531001832005053100183WP 2005 5 31 GTIA050094 120050307A5712 FRAME DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE RT WING CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FROM C/O 0155770 RT WING L/E 2 EA FORMERS ST APPROX STA 351 CRACKED. FABRICATED DOUBLER IAW SRM. HEAT TREATED 2 EA DOUBLER IAW SRM. TREATED AND PRIMED INSTALLED REPAIR DOUBLER IAW SRM. LP NR 01476783. (K) 2L72 4F4 F A6WE E9NE 20050531001862005053100186WP 2005 5 31 GTIA050083 120050304A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 AFT CARGO COMPARTMENT, STA 1174, LBL 12, MAIN CABIN FLOORBEAM UPPER FLOOR SUPPORT ANGLE IS CORRODED (EXFOLIATION). REMOVED DAMAGED FLOORBEAM AND FOUND OUT OF LIMITS. FABRICATED NEW SUPPORT ANGLE, PRIMED AND TREATED. INSTALLED FLOOR SUPPORT ANGLE IAW SRM. (K) 2L72 4F4 F A6WE E9NE 20050601000022005060100002 2005 6 1 GTIA050131 420050421A3418 COMPUTER DOUG DC9 DC983 3022083WP STALL WARNING MALFUNCTIONED A GTIAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL23802NK 53168 LGA - ON TAXI OUT, AUTOSLAT FAIL LIGHT ILLUMINATED WITH FLAPS EXTENDED TO 11 DEGREES, AIRCRAFT TAIL SWAP TO 827. TROUBLESHOT SYSTEM VERIFIED FLAP SLAT HANDLE READING. OPS CHECK GOOD. REMOVED AND REPLACED NR 1 AND NR 2 AUTOSLAT ACTUATORS. NO HELP. PERFORMED CONTINUITY CHECKS OF SLAT ACTUATORS. NO FAULTS NOTED. REMOVED AND REPLACED NR 2 STALL WARNING COMPUTERS. SYSTEM CHECKS GOOD. (M) 2L72 4F RTA6WE 20050601000162005060100016SO 2005 6 1 SIMA200512202A 120050424A21332099L011100 OUTFLOW VALVE EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL CABIN PRESSURE FAILED A SIMAK NONE O OTHER CLCLIMB 1 SW21719AE 145276 CREW REPORTED A LOSS OF CABIN PRESSURIZATION WHEN CLIMBING THROUGH FL210. CABIN ALT WENT ABOVE 10,000 FT DURING DESCENT. MAINTENANCE REMOVED AND REPLACED THE E1 HIGH STAGE AND PRESSURE OUTFLOW VALVE IAW MM. OPS CHECK WAS GOOD AND AIRCRAFT DID A FUNCIONAL CHECK FLIGHT. AIRCRAFT WAS THEN RETURNED TO SERVICE. (K) 2L72 4F4 FRTT00011ATTE6CH 20050601000302005060100030WP 2005 6 1 DHL2005807512 120050420A5347 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH86990 45990 MAIN CARGO COMPT NR 2 TRACK LUG WORN, STA 689.000. CUT OUT NR 2 TRACK DAMAGED SECTION, STA 689.000 IAW SRM 53-2-3 PG 17 FIG 6D. CLEANED AND TREATED AREA IAW SRM 51-1-8B. INSTALLED NEW CHANNEL AND PLUG IAW SRM 53-2-3 SRM 51-3-0 PG 1. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050601000352005060100035WP 2005 6 1 DHL2005807514 120050420A5347 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE DETERIORATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH86990 45990 MAIN CARGO COMPT NR 2 TRACK LUGS DETERIORATED, STA 1210.000. CUT OUT NR 2 TRACK DAMAGED SECTION IAW SRM 53-2-3 PG 17 FIG 6D. CLEANED AND TREATED AREA IAW SRM 51-1-8B. INSTALLED NEW CHANNEL AND PLUG IAW SRM 53-2-3, SRM 51-3-0 PG 1. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050601000492005060100049WP 2005 6 1 DHL2005807508 120050427A5751 SKIN DOUG DC8 DC873F 302199FWP RT AILERON CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH86990 45990 RIGHT OUTBOARD AILERON UPPER SKIN 0.500 CRACK, STA XW 698.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-8-1 FIG 4, DACO DWG 5763133. REMOVED DAMAGED PLATING IAW SRM 51-1-21 PG 1. FABRICATED NEW PLATING (AL2024T3 0.020) AND FINGER DOUBLER (AL2024T3 0.016) IAW SRM 57-8-1 FIG 4 ITEM F, G, DACO DWG 5763133. BONDED FINGER DOUBLER ON NEW PLATING IAW SRM 51-1-9 PG 1, SRM 51-1-9A PG 1. CLEANED, TREATED AND PRIMED NEW PLATING INTERIOR IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW DACO DWG 5763133, SRM 51-1-21 PG 1. PERFORMED RIGHT OUTBOARD AIL BALANCING IAW SRM 51-4-3 PG 1-3. FOUND WITHIN TOLERANCE (MOMENT 3354.93 IN-LBS). 2L74 4F RT4A25 20050601000652005060100065WP 2005 6 1 AALA20050328 120050513A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21467AA 49597 SFO - EMERGENCY LIGHTS AT AFT GALLEY DOOR AND ALL LIGHTS FROM SEAT 21D AFT INOPERATIVE. REPLACED BATTERY PACK ABOVE AFT SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050601000752005060100075EU 2005 6 1 MALA050416 120050512A3230D49412001 CONTROL UNIT SAAB SF340 340B 7860101EU LANDING GEAR MALFUNCTIONED A MALAO OTHER J WARNING INDICATION UKUNKNOWN 1 GL15366PX 340B267 LANDING GEAR TRANSIT LIGHT ON AND OFF AFTER TAKEOFF. DIVERTED TO RHI. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED LANDING GEAR CONTROL UNIT IAW SAAB AMM 31-31-05. OPS CHECK GOOD PN ON/OFF D494-12-001, SN ON 113/1-85, SN OFF 116/11-8. 2L72 4T RTA52EU 20050601000762005060100076EU 2005 6 1 MALA050419 120050515A3020 DEICE SYSTEM SAAB SF340 340B 7860101EU RT ENGINE MALFUNCTIONED A MALAO OTHER N FALSE WARNING UKUNKNOWN 1 GL15434XJ 340B434 RIGHT ENGINE INTAKE CAUTION LIGHT ILLUMINATED. CREW RETURNED TO DTW. PERFORMED OHMS CHECK ON INTAKE SYSTEM. CHECKS GOOD. PERFORMED DIAGNOSTIC ON DE-ICE MODULE. CHECKS GOOD. CLEANED CANNON PLUGS AS REQUIRED. GROUND RUN A/C FOR 30 MIN. ALL CHECKS GOOD. 2L72 4T RTA52EU 20050601000772005060100077EU 2005 6 1 MALA050409 120050415A5330 SKIN BAC 146 AVRO146RJ85A1500097EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15503XJ E2310 DURING C1, C2 INSPECTION IN YYC, FOUND FUSELAGE SKIN DENT REPAIR AFT OF FRAME 19 BETWEEN STR 19L AND 20L. 2H74 4F RTA49EU 20050601000792005060100079EU 2005 6 1 MALA050412 120050430A5753 FLAP BAC 146 AVRO146RJ85A1500097EU RT WING DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15503XJ E2310 DURING C1, C2 INSPECTION IN YYC FOUND RT OB LEADING EDGE OB OF NR 4 FLAP TRACK THERE IS A TEMP REPAIR IAW EOA57099. 2H74 4F RTA49EU 20050601000802005060100080EU 2005 6 1 MALA050413 120050513A33506122751 BATTERY BAC 146 AVRO146RJ85A1500097EU CABIN FAILED A MALAK NONE O OTHER ININSP/MAINT 1 GL15517XJ E2335 BATTERY FAILED CAPACITY CHECK. 2H74 4F RTA49EU 20050601000822005060100082EU 2005 6 1 MALA050397 120050503A532072553711245 STRUCTURE SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15449XJ 340B449 DURING 4K INSPECTION IN BNA, FOUND LT WRAP AROUND PN 72553711-245, IS CORRODED AND HAS BEEN REMOVED AND REPLACED IAW SRM 51-40-21. REF: EAMS WORK ORDER 212113 TASK 1506. 2L72 4T RTA52EU 20050601000842005060100084EU 2005 6 1 MALA050400 120050504A52607253710871 RAIL SAAB SF340 340B 7860101EU AIRSTAIR CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15412XJ 340B412 DURING 4K INSPECTION IN BNA FOUND AIRSTAIR RAIL ASSEMBLY PN 7253710-871 IS CORRODED AND WILL BE REMOVED AND REPLACED IAW SRM 51-40-21/22. REF EAMS WORK ORDER 212166 TASK 1521. 2L72 4T RTA52EU 20050601000862005060100086EU 2005 6 1 MALA050392 120050422A3260ATG130902 DOWNLOCK SWITCH SAAB SF340 340B 7860101EU LT MLG FAULTY A MALAA UNSCHED LANDING N FALSE WARNING APAPPROACH 1 GL15450XJ 340B450 ON FINAL APPROACH INTO BGM, LT MAIN GEAR LIGHT WAS FLICKERING. PERFORMED QRH. RECYCLED GEAR, LT MAIN GEAR LIGHT FLICKERED 2X AFTER BEING ON STEADY FOR 2 MINUTES. LIGHT REMAINED ON STEADY THEREAFTER. FERRIED A/C FROM BGM TO DTW FOR REPAIRS. MAINTENANCE REPLACED LT MLG DOWNLOCK SWITCH PN ATG130902, IAW MM 32-61. REPLACED LT MLG C/P 5GA-J1, (FEMALE SIDE) PN MS347W1419SX, PERFORMED OPS CHK OF LT MLG EXTENTION/RETRACTION. ALL CHECKS GOOD. 2L72 4T RTA52EU 20050601000912005060100091EU 2005 6 1 MALA050411 120050428A5311 FRAME BAC 146 AVRO146RJ85A1500097EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15503XJ E2310 DURING C1, C2 INSPECTION IN YYC FOUND DENT AND GOUGE LT SIDE FUSELAGE FRAME 25 (ABOUT 5 INCHES AFT OF FRAME 25) BELOW CABIN WINDOW. 2H74 4F RTA49EU 20050601000932005060100093 2005 6 1 GTIA050123 420050405A3454 CONNECTOR DOUG DC9 DC982 3022082WP E/E BAY FAULTY A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23800NK 49144 NR 1 VOR NEEDLES WON’T POINT TO STATION AND DOESN’T PULL BARBER POLE, FLAGS INDICATOR. AIRCRAFT TAIL SWAP WITH 817. REMOVED R50-318 NR 1 NAV RECEIVER RACK CONNECTOR. REPLACED ALL PINS, RETERMINATED BOTH VOR/ILS COAX AND SHIELD CONNECTORS. REINSTALLED CONNECTOR IN RACK. ALL CHECKS GOOD. (M) 2L72 4F A6WE 20050601000952005060100095WP 2005 6 1 GTIA050121 120050402A3260 INDICATOR DOUG DC9 DC982 3022082WP COCKPIT FAULTY A GTIAK NONE N FALSE WARNING APAPPROACH 1 GL23821NK 49508 ON APPROACH, RECEIVED NO DOWN AND LOCKED INDICATION (GREEN LIGHT) ON FORWARD PANEL, MECHANICAL PIN ON PEDESTAL WAS EXTENDED, AIRCRAFT TAIL SWAP WITH 818. REMOVED AND REPLACED LANDING GEAR POSITION INDICATORS. OPS HEK NORMAL. (M) 2L72 4F A6WE 20050601000972005060100097 2005 6 1 GTIA050119 420050404A2565D29985107 SLIDE DOUG DC9 DC982 3022082WP SERVICE DOOR FAILED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK5056 49508 AFT SERVICE DOOR EVAC SLIDE DID NOT DEPLOY DURING OPS CHECK, FIRING LANYARD FAILED TO PULL OUT OF FIRING MECHANISM. AFT SERVICE DOOR EVAC SLIDE TO BE REPLACED ON WORK CARD 7809-1-01086/05. (M) 2L72 4F A6WE 20050601000992005060100099WP 2005 6 1 GTIA050118 120050310A5532 FAIRING DOUG DC9 DC982 3022082WP VERTICAL STAB GOUGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 VERT STAB TIP FAIRING HAVE SCRATCHED/GOUGED ON BOTH SIDE. BLENDED DAMAGED AREA AT VERT STAB MATERIAL LOSS OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED FILLER AND DOUBLER IAW SRM 55-01 FIG 4. TREATED AND PRIMED, INSTALLED FILLER AND DOUBLER IAW SRM 51-30-2. (M) 2L72 4F A6WE 20050601001042005060100104WP 2005 6 1 GTIA050115 120050310A5522 FAIRING DOUG DC9 DC982 3022082WP LT ELEVATOR CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 LEFT ELEVATOR FAIRING EDGE CRACKED STATION XE 171. TRIMMED LEFT ELEV FAIRING EDGE AT STATION XE 171. MATERIAL LOSS WITHIN LIMITS. TREAT AND PRIMED IAW SRM 51-10-3. (M) 2L72 4F A6WE 20050601001052005060100105WP 2005 6 1 GTIA050114 120050307A5320 STRIP DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - MID PIT LEFT SIDE STATION 541, UPPER SIDEWALL SUPPORT STRIP CRACKED. REPAIRED DAMAGED AREA IAW SRM 53-05 PG 137. FABRICATED DOUBLER, TREATED AND PRIMED. INSTALLED DOUBLER IAW SRM 51-30-2. (M) 2L72 4F A6WE 20050601001082005060100108NM 2005 6 1 SWAA051406 120050513A53116516301 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STUB FRAME CRACKED AT BS 188, RT SIDE, WL 208. REMOVED AND REPLACED STUB FRAME PER SRM. 2L72 4F RTA16WE 20050601001092005060100109NM 2005 6 1 SWAA051407 120050515A5315146A7503 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29352SW 24888 DURING SCHEDULED 1/2D CHECK, FOUND 2 EA LONGITUDINAL FLOORBEAMS CORRODED AT BS 772, RBL 8 & LBL 12. REPAIRED FLOORBEAMS PER SWA EA. 2L72 4F RTA16WE 20050601001102005060100110NM 2005 6 1 SWAA051408 120050515A53226546540 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29352SW 24888 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 639, JUST BELOW WL 208, LT SIDE. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050601001112005060100111NM 2005 6 1 SWAA051409 120050515A53126517583 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29352SW 24888 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE BS 178 BULKHEAD VERTICAL BEAM WEB CRACKED AT LBL 5.7, WL 178. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050601001132005060100113 2005 6 1 SWAA051412 420050513A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29391SW 27378 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050601001162005060100116NM 2005 6 1 SWAA051415 120050515A57536546486156 WEDGE BOEING737 7375H4 138449DNM T/E FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 DURING SCHEDULED RON CHECK, FOUND RT WING INBOARD MIDFLAP T/E WEDGE DELAMINATED. REMOVED AND REPLACED MIDFLAP T/E WEDGE PER MM. 2L72 4F RTA16WE 20050601001172005060100117NM 2005 6 1 SWAA051416 120050515A335010107451 LENS BOEING737 7375H4 138449DNM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29526SW 26568 RIGHT OVERWING EXIT SIGN LENS MISSING. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20050601001182005060100118 2005 6 1 SWAA051417 420050515A2565D31354 SLIDE BOEING737 7373T5 1384608NM L2 & R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 L2 & R2 EMERGENCY EVAC SLIDES OUT OF ADJUST. ADJUSTED SLIDES PER MM. 2L72 4F RTA16WE 20050601001212005060100121NM 2005 6 1 SWAA051384 120050512A53306545777 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050601001222005060100122NM 2005 6 1 SWAA051385 120050512A5320BAC1518 STIFFENER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND LT & RT MLG W/W VERTICAL STIFFENERS CRACKED AT BS 663 BULKHEAD, LBL 6 & RBL 6, WL 166. REPAIRED STIFFENERS PER SRM. 2L72 4F RTA16WE 20050601001232005060100123NM 2005 6 1 SWAA051386 120050512A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 294, STR 12L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050601001242005060100124NE 2005 6 1 SWAA051387 220050512A7200CFM563 ENGINE BOEING737 7373H4 1384600NM GE CFM56 CFM56* 13802NE NR 1 MAKING METAL A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 856818 DURING SCHEDULED C4 CHECK, NR 1 ENGINE FWD SUMP CHIP DETECTOR HAD EXCESSIVE METAL DEBRIS. REMOVED AND REPLACED NR 1 ENGINE PER MM. 2L72 4F4 FRTA16WE E2GL 20050601001262005060100126NM 2005 6 1 SWAA051389 120050512A53306545777 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 972, STR 21L. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050601001272005060100127 2005 6 1 SWAA051390 420050512A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050601001322005060100132NM 2005 6 1 SWAA051395 120050512A53156545410 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29352SW 24888 DURING SCHEDULED 1/2D CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 666 & BS 670, RBL 25. REPAIRED BEAM PER SWA EA. 2L72 4F RTA16WE 20050601001332005060100133NM 2005 6 1 SWAA051396 120050512A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN DISCONNECTED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29475WN 32474 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT MID CABIN. RECONNECTED EEPLS PER MM. 2L72 4F RTA16WE 20050601001342005060100134NM 2005 6 1 SWAA051397 120050512A551265C25727 SKIN BOEING737 7373A4 1384585NM HORIZ STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29669SW 23752 DURING SCHEDULED 1/4D CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED AT REAR SPAR, STAB STA 157.10. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050601001372005060100137WP 2005 6 1 GTIA050113 120050307A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 DENT AT FS 1304 BETWEEN LONGERONS 18R AND 19R, D=1 INCH BY .020 INCH D/X=50, CONDITION 1B. INSPECTED FOUND FURTHER DAMAGE IN DENT (GOUGE) REQUIRING REPAIR. CUT OUT DAMAGE SKIN SECTION (2.10 DIAMETER). FABRICATED SKIN FILLER AND INTERNAL DOUBLER IAW SRM 53-04 FIG 38 SHT 23. TREATED AND PRIMED, INSTALLED SKIN FILLER AND INTERNAL DOUBLER IAW SRM 53-04 FIG 38. (M) 2L72 4F A6WE 20050601001382005060100138WP 2005 6 1 GTIA050112 120050307A5230 SKIN DOUG DC9 DC982 3022082WP CARGO DOOR DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 DENT AT FS 1174 BETWEEN LONGERON 21R AND 22R ON AFT CARGO DOOR, D=1.5, X=0.035, D/X=42.85, CONDITION 1B. REMOVED 2 INCH ROUND CUT OUT DAMAGED AREA OF DOOR. FABRICATED FILLER AND DOUBLER FOR AFT CARGO DOOR STATION 1174 BETWEEN L21R AND 22R IAW SRM 51-10-4 AND 52-05. TREATED AND PRIMED DOUBLER. INSTALLED DOUBLER AND FILLER ON AFT CARGO DOOR STATION 1174 BETWEEN 21R=22R IAW SRM 52-05 AND 51-30-2. (M) 2L72 4F A6WE 20050601001402005060100140NM 2005 6 1 SWAA051400 120050513A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND CORROSION ON FUSELAGE FLOORBEAM AT BS 344, LBL 9, WL 208. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20050601001422005060100142NM 2005 6 1 SWAA051402 120050513A53116546526 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND 2 EA FUSELAGE FRAME CRACKS AT BS 400, STR 8L TO STR 9L & STR 15R TO STR 16R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050601001442005060100144NM 2005 6 1 SWAA051404 120050513A55516551524 FITTING BOEING737 7373H4 1384600NM HORIZ STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND LT & RT HORIZONTAL STAB ATTACH FITTING LUG FACES CORRODED. REPAIRED LUG FACES PER SRM. 2L72 4F RTA16WE 20050601001452005060100145NM 2005 6 1 SWAA051420 120050516A57546573714 WEDGE BOEING737 7373H4 1384600NM L/E SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND NR 2 L/E SLAT INBOARD T/E WEDGE DELAMINATED. REPAIRED SLAT PER SRM. 2L72 4F RTA16WE 20050601001462005060100146NM 2005 6 1 SWAA051421 120050516A53116546540 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, STR 16R TO STR 17R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050601001482005060100148NM 2005 6 1 SWAA051424 120050516A3350101073 LENS BOEING737 7373H4 1384600NM EXTERIOR DEFECTIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29352SW 24888 DURING SCHEDULED 1/2D CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT LENS CLOUDY. REMOVED AND REPLACED LENS PER MM. 2L72 4F RTA16WE 20050601001502005060100150NM 2005 6 1 SWAA051426 120050516A5344BAC1507 HINGE BOEING737 7373H4 1384600NM L1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29647SW 27717 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR UPPER HINGE BOX LOWER RADIUS CRACKED. REMOVED AND REPLACED UPPER HINGE BOX PER SRM. 2L72 4F RTA16WE 20050601001522005060100152NM 2005 6 1 SWAA051429 120050514A3350311500 LENS BOEING737 7373G7 1384595NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29671SW 23785 EMERGENCY BULLNOSE LIGHT LENS MISSING AT ROW 12DEF. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20050601001542005060100154WP 2005 6 1 GTIA050110 120050308A5323 STRUCTURE DOUG DC9 DC982 3022082WP CATWALK CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 CATWALK SIDE FILLER STATION 1510 IS CRACKED ON RIGHT SIDE. STOP DRILLED CRACK, FABRICATED REPAIR DOUBLER. TREATED AND PRIMED, INSTALLED DOUBLER IAW SRM 51-30-2. (M) 2L72 4F A6WE 20050601001552005060100155WP 2005 6 1 GTIA050108 120050307A5260 ATTACH ANGLE DOUG DC9 DC982 3022082WP FWD AIRSTAIRS CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FORWARD AIRSTAIR UPPER ATTACH ANGLE ON SHROUD IS CRACKED AND DAMAGED. REMOVED ANGLE FROM FORWARD AIRSTAIR SHROUD. FABRICATE NEW ANGLE. TREATED AND PRIMED, INSTALLED ANGLE IAW SRM 51-30-1. (M) 2L72 4F A6WE 20050601001622005060100162WP 2005 6 1 GTIA050107 120050310A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE GOUGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - GOUGE ON FUSELAGE SKIN FS 497 BETWEEN LONGERONS 20R AND 21R. BLEND OUT GOUGE FUSELAGE SKIN FS 497. AFTER BLENDED OUT LIFT .036 FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGED AREA. FABRICATED SKIN PLUG AND FINGER DOUBLER. TREATED AND PRIMED SKIN PLUG AND FINGER DOUBLER. INSTALLED INTERNAL DOUBLER AND FILLER IAW SRM 53-04. (M) 2L72 4F A6WE 20050601001682005060100168NM 2005 6 1 05FDEA01276 120050514A5330 SKIN BOEING727 727227 1384078NM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 DENT IN SKIN AT BS 1348, STR 14L. REPLACED SKIN PANEL PER SRM 51-30-2. 2L73 4F A3WE 20050601001692005060100169WP 2005 6 1 GTIA050103 120050310A5230 SUPPORT BRACKET DOUG DC9 DC982 3022082WP BARRIER DOOR CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - MID PIT BARRIER DOOR AFT SKIN SUPPORT BRACKET CRACKED TWO PLACES. REMOVED AND REPLACED MID PIT BARRIER DOOR IAW SRM 51-30-1 AND 51-30-2. (M) 2L72 4F A6WE 20050601001702005060100170NM 2005 6 1 05FDEA01277 120050514A5330 SKIN BOEING727 727227 1384078NM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 DENT IN SKIN BS 1347, STR 7L. REPLACED SKIN PANEL PER SRM 51-30-2. 2L73 4F A3WE 20050601001732005060100173WP 2005 6 1 GTIA050102 120050310A5323 STRUCTURE DOUG DC9 DC982 3022082WP CATWALK WORN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 AFT AIRSTAIRS STATION 1370 AT FLOOR LINE HAS A HOLE WORN IN IT FROM THE CATWALK ON LEFT SIDE. TRIMMED OUT DAMAGED SECTION AT FLOOR LINE LEFT SIDE AT STATION 1370. FABRICATED REPAIR DOUBLER AND HEAT TREATED. TREATED AND PRIMED. INSTALLED DOUBLER IAW 51-70-4. (M) 2L72 4F A6WE 20050601001742005060100174NM 2005 6 1 05FDEA01283 120050514A5312 DOUBLER DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25580FE 48471 LANDING GEAR, CENTER LANDING GEAR LEFT HAND FORWARD BULKHEAD SIDE DOUBLER CRACKED. DOUBLER REMOVED AND NEW DOUBLER INSTALLED AS PER SRM 51-33-01 VOLUME II. THIS REPAIR CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050601001762005060100176NM 2005 6 1 05FDEA01288 120050515A25706560958 INSULATION BOEING727 727233 138408ANM ACCCESSORY BAY DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25254FE 20936 COMPLY WITH EA 7-2580-81691 "EQUIPMENT AND FURNISHINGS. INSULATION BLANKETS, PARTIAL REPLACEMENT, STA 178-294, LOWER SECTION 41 INCH. 2L73 4F RTA3WE 20050601001772005060100177NM 2005 6 1 05FDEA01289 120050515A5280651841585 RETAINER BOEING727 727233 138408ANM NLG DOOR CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25254FE 20936 LT NOSE GEAR AFT DOOR SEAL RETAINER CORRODED. REMOVED AND REPLACED SEAL RETAINER IAW SRM 51-30-2. 2L73 4F RTA3WE 20050601001782005060100178NM 2005 6 1 05FDEA01290 120050515A5320 CLIP DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25580FE 48471 AFT FUSELAGE COMPARTMENT DOGHOUSE NR 2 AFT TOP FRAME TO CROWN ATTACHMENT CLIP SUSPECT CRACK. REMOVED AND REPLACED AS PER SRM 51-35-01 AND SRM 51-33-01 VOLUME II. 2L73 4F RTA22WE 20050601001792005060100179NM 2005 6 1 05FDEA01300 120050516A5311 FRAME DOUG MD11 MD11 3023602NM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25580FE 48471 MAIN DECK CABIN RIGHT HAND STATION 1681 LONGERON 12R FRAME FOUND DENTED AS MARKED. REPAIRED AS PER SRM 53-30-00 FIGURE I VOLUME I. 2L73 4F RTA22WE 20050601001802005060100180NM 2005 6 1 05FDEA01301 120050516A5311 FRAME DOUG MD11 MD11 3023602NM FUSELAGE CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25580FE 48471 MAIN DECK CABIN RIGHT STATION 1701 LONGERON 12R FRAME, FOUND CHAFED AS MARKED. REPAIR CARRIED OUT AS PER SRM 53-30-00 FIGURE I VOLUME I. 2L73 4F RTA22WE 20050601001832005060100183WP 2005 6 1 GTIA050101 120050310A5320 STIFFENER DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FS 190 RBL 34 FLOOR WEB STIFFENER IS CRACKED. REMOVED DAMAGE STIFFENER, FOUND OUT OF LIMITS. FABRICATE NEW STIFFENER IAW SRM 51-10-2 AND 51-10-4. TREAT AND PRIMED, INSTALLED STIFFENER IAW 51-30-2. (M) 2L72 4F A6WE 20050601001852005060100185EU 2005 6 1 05FDEA01310 120050516A5320 ADAPTER AIRBUS300 A300F4605R 3930327EU FUSELAGE UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25679FE 793 ADAPTER BETWEEN TRACK R-1 AND R-2 AT FR 29 REF N00318. REMOVED AND REPLACED ADAPTER IAW SRM 51-72-10 AND 51-40-21. 2L72 4F RTA35EU 20050601001882005060100188NM 2005 6 1 SWAA051439 120050516A53306545775 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29322SW 23343 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 797, STR 17L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050601001892005060100189NM 2005 6 1 SWAA051440 120050517A53126517582 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29352SW 24888 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE VERTICAL BEAM WEB CRACKED AT BS 178 BULKHEAD, RBL 17.1, WL 230. REMOVED AND REPLACED VERTICAL BEAM WEB PER SRM. 2L72 4F RTA16WE 20050601001902005060100190NM 2005 6 1 SWAA051441 120050517A53206551698 STRINGER SPLICE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29352SW 24888 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER SPLICE CRACKED AT BS 908, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20050601001932005060100193 2005 6 1 SWAA051444 420050517A2565D31354 SLIDE BOEING737 7373A4 1384585NM L1 DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29679AA 23291 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. SLIDE DID NOT DEPLOY. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20050601001952005060100195NM 2005 6 1 SWAA051432 120050517A55536546874 FITTING BOEING737 7373H4 1384600NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND LT & RT VERTICAL STAB FAILSAFE FITTING FWD & AFT PRIMARY CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER. 2L72 4F RTA16WE 20050601002002005060100200WP 2005 6 1 DHL2005807526 120050505A5315LS3983 FLOORBEAM DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH86990 45990 MAIN CARGO COMPT FLOORBEAM CORRODED, STA 660.000 RBL 10. PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. CUT OUT DAMAGED SECTION IAW SRM 51-2-1 FIG 1 SHEET 7. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED REPAIR ANGLE (EXTRUSION LS3983 7075 "0" 0.125) AND FILLER (7075T6 0.125) IAW SRM 51-2-1 FIG 1 SHEET 7-12. HEAT TREATED REPAIR ANGLE IAW SRM 51-1-1 PG 1, 13, 17 DPS 7.00-1 REV BK. CLEANED, TREATED AND PRIMED REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SRM 51-2-1 FIG 1 SHEET 7-12, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050601002012005060100201NM 2005 6 1 DHL2005740520 120050505A5313BAC1498142 STRINGER BOEING727 7272Q9 138448MNM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH46106 21930 FWD CARGO COMPT BS 550 AT STRINGER 27L CORROSION AT FLANGE. CUT OUT STRINGER SECTION DIM 4 INCH IAW B727 SRM 53-10-3 FIG 1. FABRICATED STRINGER SECTION P/N BAC 1498-142 PO NR 9001678 DIM 4 INCH SPLICE REPAIR P/N 7075T6 .050 PO NR 9001777 DIMENSIONS 14 1/2 INCH BY 1 INCH BY 1 1/8 INCH BY 1 INCH BY 1 1/8 INCH BY 1 AN (3 EA.) SHIMS 12 1/2 INCHES BY 3/4 INCH (2EA) AN 14 1/2 INCHES BY 1 INCHES IAW B727 53-10-2 FIG 9 AND 53-10-3 FIG 1. TREATED AN PRIMED STR , SPLICE AN SHIMS AND AREA IAW B727 SRM 51-10-2. INSTALLED STRINGER AN SPLICE REPAIR AN SHIMS IAW B727 SRM 53-10-3 FIG 1. 2L73 4F RTA3WE 20050531000032005053100003NM 2005 5 31 05FDEA01266 120050513A5753 SKIN DOUG MD11 MD11 3023602NM T/E FLAP DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE RT WING, INBD FLAP, EXTERIOR UPPER SURFACE MOST UPPER ABOUT 20 INCHES FROM INBD TO OUTBD, FOUND 1 EACH EXISTING REPAIR DOUBLER. 2L73 4F RTA22WE 20050531000082005053100008SO 2005 5 31 C2XA05SH035 120050516A532014530643401 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714938 145029 SHV - DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION BETWEEN FRAMES 23 & 24. REPAIRED CENTER OMEGA BEAM AT FRAME 24 IAW EMB 145 SRM 53-22-10 PARAGRAPH 2 FIGURE 201. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050531000122005053100012NM 2005 5 31 DHL2005788002 120050514A3397 WIRE BOEING727 727214 138407RNM CABIN DAMAGED A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01788AT 21958 EXIT LIGHT DOES NOT ILLUMINATE DURING THE STANDBY POWER CHECK. RELAYS NR 10-60450-3 AND BACR13CG-2A. (NO HELP) RE-TERMINATED WIRE W508-075-10 TO ESSENTIAL BREAKER IAW WDM 24-52-01. LYS. CHECK SERV IAW M/M 33-50-01. 2L73 4F A3WE 20050531000152005053100015EU 2005 5 31 AWXA200500558 120050513A3397ABS0374A24 WIRE AIRBUS320 A320232 3930326EU CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28655AW 1075 ORD - EEL - DURING 4-DAY CHECK, FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 11 RT INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE LEADING TO THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 11 RT; OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050531000222005053100022EU 2005 5 31 AWXA200500565 120050506A5320D53480043205 SILL AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28639AW 471 SAL - MAJOR REPAIR - DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SILL BEAM -Y1292 AT CUTOUT FOR R-2 DOOR AROUND GIRT BAR FITTING RIVET HEADS & NUT PLATES BETWEEN FR 67 AND FR 68. MAINTENANCE CUT OUT DAMAGE ON LOWER SILL BEAM -Y1292; FABRICATED A NEW REPLACEMENT SECTION OF SILL BEAM, A REPAIR PLATE, AND 4 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW A320 SRM 53-41-14 FIG 201. 2L72 4F RTA28NM 20050531000292005053100029WP 2005 5 31 UPS05844447 120050425A53203755854502N FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE:C1 C-PIT DOOR STOP FWD SIDE BANANA FITTING CRACKED AT STA 1180 L26L. REMOVED AND REPLACED BANANA FITTING IAW DC-8 SRM 51-1-20D, 51-1-21, AND 51-1-20A. 2L74 4F RT4A25 20050531000322005053100032WP 2005 5 31 UPS05844450 120050421A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE:C1 LONGERON 14R CRACKED .25 INCH LONG AT STA 1757. REMOVED AND REPLACED LONGERON SECTION AND INSTALLED SPLICE FITTING IAW DC-8 SRM 53-2-2 FIG 10 AND 51-1-20D. 2L74 4F RT4A25 20050531000382005053100038WP 2005 5 31 UPS05844457 120050421A532047504192 ATTACH FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 INSPECTION TYPE:C1 MAIN CABIN AT STA 1280 L18R FRAME ATTACH FITTING CRACKED .5 INCH LONG. REMOVED CRACKED FITTING, FABRICATED REPLACEMENT FITTING IAW DWG 475041 9, AND INSTALLED IAW DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20050531000502005053100050NM 2005 5 31 MWEA050044 120050513A2560P4010021 BATTERY BOEING717 717200 1383700NM FLASHLIGHT DISCHARGED A MWEAK NONE L NO TEST ININSP/MAINT 1 GL31903ME 55167 COCKPIT FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED BATTERIES. 2L72 4F TRA6WE 20050531000612005053100061NM 2005 5 31 CALA0500147 120050513A531565C3394824 FLOORBEAM BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2752616 27329 INSPECTION FOUND FLOORBEAM CORRODED AROUND FASTENER HOLES AT STA 947.5, LBL 15 TO RBL 15. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-00-51, PAGE 212-215. 2L72 4F RTA16WE 20050531000632005053100063NM 2005 5 31 CALA0500149 120050514A5315147A5506 FLOORBEAM BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2726210 28770 INSPECTION FOUND THE L-2 DOOR AREA FLOORBEAM NUT CLIP HOLES CORRODED AT STA 986.5, LBL 22.5 TO LBL 43. REPAIRED IAW ECRA 5321-01215. 2L72 4F RTA16WE 20050531001042005053100104SO 2005 5 31 SIMA200511702 120050416A532014522178005 SILL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21645AE11610 145212 THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. BLENDED THE DAMAGED AREA TO REMOVE THE CORROSION. ALODIZED AND APPLIED EPOXY TO THE REWORKED AREA. FILL THE BLENDED AREA WITH HYSOL EA AND APPLIED PRIMER AFTER CURING. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SRM. (SW212005716) (K) 2L72 4T4 FRTT00011ATTE6CH 20050531001122005053100112SO 2005 5 31 SIMA200511710 120050414A5320145242280003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21847AE 145707 DURING CPCP INSPECTION; FOUND ANGLE SUPPORT AT RT FUSELAGE FLOORBOARD SUPPORT AT FRAME 23 IS CORRODED. REPLACED ANGLE IAW SRM. AIRCRAFT RETURNED TO SERVICE. (SW21200505715) (K) 2L72 4F4 FRTT00011ATTE6CH 20050531001182005053100118 2005 5 31 GTIA050144 420050423A3425 AHRS DOUG DC9 DC983 3022083WP NR 2 FAILED A GTIAO OTHER J WARNING INDICATION CLCLIMB 1 GL23827NK 49793 EFIS FAILURE, CAPTAINS FMA FAIL CORRESPONDING COMPARATOR LIGHTS, AIRCRAFT TAIL SWAP WITH 817NK. REMOVED AND REPLACED NR 2 AHRS, OPS CHECK GOOD. (M) 2L72 4F RTA6WE 20050531001212005053100121SO 2005 5 31 SIMA200512204 120050425A531313500400019 STRINGER EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21806AE 145503 DURING AN MBV INSPECTION, MAINTENANCE FOUND STRINGER 19R WITH CHAFE DAMAGE BETWEEN FRAMES 52 AND 53. MAINTENANCE REPAIRED STRINGER 19R BETWEEN FRAMES 52 AND 53 IAW SRM DOUBLER REPAIR. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200505710) (K) 2L72 4F4 FRTT00011ATTE6CH 20050531001242005053100124WP 2005 5 31 GTIA050142 120050415A5320 SUPPORT BRACKET DOUG DC9 DC982 3022082WP FUSELAGE BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23829NK 49931 FTW - FORWARD PIT RIGHT UPPER SIDEWALL, WATER LINE SUPPORT BRACKET IS BROKEN AT STATION 465. REMOVED AND FABRICATED NEW SUPPORT BRACKET. TREATED, PRIMED AND INSTALLED NEW SUPPORT BRACKET. (M) 2L72 4F A6WE 20050531001412005053100141NM 2005 5 31 2005UALA00420 120050506A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29586UA 26710 AFT PIT FRAME DENTED STA 1540, STR 26L. FRAME DENT WAS TRIMMED OUT AND J ANGLE REPAIR INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050531001592005053100159EU 2005 5 31 2005UALA00438 120050510A3610 BLEED AIR SYS AIRBUS320 A320232 3930326EU NR 1 TRIPPED A UALAB EMER. DESCENT JG WARNING INDICATION MULTIPLE FAILURE CRCRUISE 1 WP29496UA 1845 NUMBER 1 BLEED TRIPPED OFF. CABIN DEPRESSURIZED. NUMBER 2 BLEED AND APU PREVIOUSLY DEFERRED. NR 1 BLEED TRIPPED 45 MINUTES AFTER TAKEOFF. NR 2 AND APU WERE PREVIOUSLY DEFERRED INOP. AT 9000 FEET, NR 1 BLEED WAS TURNED BACK ON AND APPEARED TO HOLDING STEADY. REPLACED NR 1 ENGINE FAN AIR SENSOR/THERMOSTAT CONTROL (7170HM) PER IPC-36-11-06-06B. ALSO REPLACED RIGHT PACK RAM AIR INLET ACTUATOR (28HH) PER MM-21-61-51 DUE TO FAILURE DURING TEMPERATURE CONTROL TEST. OP CHECKS NORMAL. MR21603, PCN 565-9202 2L72 4F RTA28NM 20050531001682005053100168WP 2005 5 31 GTIA050097 120050325A5320 SUPPORT ANGLE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE CARGO BAY CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 AFT CARGO DOOR FWD UPLOCK SUPPORT ANGLE CRACKED. REMOVED AND FABRICATED NEW ANGLE IAW SRM. TREATED AND PRIMED, INSTALLED SUPPORT ANGLE IAW SRM. (K) 2L72 4F4 F A6WE E9NE 20050601000012005060100001NE 2005 6 1 ASMF200505018 220050515A7200 ENGINE DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE LEFT MALFUNCTIONED W ASMFD RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TXTAXI/GRND HDL 1 SW23831LF 53050 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF LEFT GENERATOR FREQUENCY WITH OSCILLATION. MEL 24-1 PROCEDURE WAS APPLIED. AGAIN AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF LEFT ENGINE WAS NOT ACCELERATED. ACCELERATION CHAMBER WERE DRAINED AND LUBRICATED IAW MM 73-20-03, TESTED CORRECT. DURING OVERNIGHT SERVICE LEVEL OIL AND CHIP DETECTOR WERE VERIFIED, LEFT ENGINE SLOW ACCELERATION PROCEDURE WAS PERFORMED IAW 71-00-00 AND LEFT GENERATOR WAS TESTED IAW MM 24-10-00, ALL CORRECT. DEFERRED REPORT WAS CLOSED. 2L72 4F4 FRT E9NE 20050601000032005060100003CE 2005 6 1 DXTA200500726 120050515A3240CPD5601 SEAL CESSNA500 560CESSNA 2076750CE BRAKE SYSTEM LEAKING E DXTAD RETURN TO BLOCK K FLUID LOSS TXTAXI/GRND HDL 1 GL07339QS 5600339 BRAKES PULSATE WHEN MEDIUM PRESSURE IS APPLIED. TAXIED A/C. FOUND EXCESSIVE VIBRATION IN PEDAL AND NOSE. BLED BRAKES AND SERVICED RESERVOIR IAW CE560 M/M CH 12-12-02. FOUND SHIMMY DAMPER NEEDS SERVICE. SERVICED SHIMMY DAMPER IAW CE560 M/M CH 12-14-01. CHECKED NOSE STRUT AND FOUND EXCESSIVE AMOUNT OF FLUID ON AIR SIDE. REPACKED NOSE STRUT IAW CE560 COMPONENT M/M CHAP 32-20-01, ALL OPERATIONAL AND LEAK CHECKS GOOD. 2L72 4F RTA22CE 20050601000092005060100009WP 2005 6 1 GTIA050081 120050310A5347 SEAT TRACK DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 RT OB SEAT TRACK HAS AREA OF CORROSION AT FS 229. REMOVED CORROSION, FOUND OUT OF LIMITS. FABRICATED NEW SEAT TRACK. FOUND WEB OB OF SEAT TRACK FS 218 CRACKED, FABED DOUBLER AND FILLER IAW SRM. PRIMED AND TREATED. INSTALLED DOUBLER, FILLER AND SEAT TRACK IAW SRM. (K) 2L72 4F4 F A6WE E9NE 20050601000112005060100011WP 2005 6 1 GTIA050128 120050415A7711 TRANSMITTER DOUG DC9 DC983 3022083WP RIGHT FAULTY A GTIAO OTHER O OTHER DEDESCENT 1 GL23835NK 53044 ON DESCENT, RIGHT ENGINE N1 LOW AT FH IDLE AT 15,000 (38 PERCENT), DIFFERENCE DROPPED AT LOWER ALTITUDE, NOTE ENGINE PARAMETERS WITH THROTTLE AT IDLE STOPS, AIRCRAFT TAIL SWAP WITH 819. FOUND RIGHT ENGINE EPR READING LOW, REMOVED AND REPLACED RIGHT EPR TRANSMITTER. CHECKED LEFT AND RIGHT ENGINE THROTTLE RIGGING, PART POWER STOPS DROPPED, ADJUSTED BOTH ENGINE FUEL CONTROL TRIMS, STOWED PART POWER STOPS. GROUND CHECKS GOOD. (M) 2L72 4F RTA6WE 20050601000122005060100012WP 2005 6 1 GTIA050080 120050304A5315 FLOORBEAM DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 AFT CARGO COMPARTMENT, STA 1309. CABIN FLOORBEAM IS CORRODED (EXFOLIATION) AT RBL 20. FOUND LWR AFT ANGLE SUPPORT CRACKED. CORROSION FOUND TO BE ALL THE WAY THROUGH FLOORBEAM AND IS OUT OF LIMITS. DETENTIONED CABLE RUNS, DISCONNECTED 2 HYD LINES AND POT. WATER AND HEATING ELEMENT. FABED SUPPORT ANGLE, PRIMED AND TREATED IAW SRM.. FABED FLOORBEAM CUT OUT SECTION, PRIMED AND TREATED IAW SRM. FABED REPAIR DOUBLERS AND FILLERS, PRIMED AND TREATED. REINSTALLED POT. WATER, HYD LINES, PULLEY BRACKETS AND RE-TENSIONED CABLE RUNS IAW MM. (K) 2L72 4F4 F A6WE E9NE 20050601000172005060100017NE 2005 6 1 GTIA050126 220050410A7320 FUEL CONTROL DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE NR 1 & 2 ENGINE OUT OF TRIM A GTIAO OTHER O OTHER ININSP/MAINT 1 GL23820NK 49126 NR 1 ENGINE IDLE IS TO LOW WITH BLEED 45-47 PERCENT N2 ENGINE EXTREMELY SLOW TO ACCELERATE, EGT IS 490 AT IDLE, MUST MOVE THROTTLE 1 KNOB FORWARD TO MAINTAIN 50 PERCENT N2, NR 2 ENGINE IDLE IS TO LOW WITH BLEED ON 48 PERCENT N2 ENGINE IS VERY SLOW TO ACCELERATE, EGT IS 450 AT IDLE, MUST MOVE THROTTLE 1/2 KNOW TO MAINTAIN 50 PERCENT N2, AIRCRAFT TAIL SWAP TO 815. PERFORMED ENGINE TRIM ON BOTH NR 1 AND NR 2 ENGINES AND ACCELERATION CHECK, BOTH OPS CHECK NORMAL. (M) 2L72 4F4 F A6WE E9NE 20050601000312005060100031WP 2005 6 1 DHL2005807513 120050420A5347 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE DETERIORATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH86990 45990 MAIN CARGO COMPT NR 3 TRACK LUGS DETERIORATED, STA 863.000. CUT OUT NR 3 TRACK DAMAGED SECTION IAW SRM 53-2-3 PG 17 FIG 6D. CLEANED AND TREATED AREA IAW SRM 51-1-8B. INSTALLED NEW CHANNEL AND PLUG IAW SRM 53-2-3, SRM 51-3-0 PG 1. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050601000322005060100032WP 2005 6 1 DHL2005807503 120050414A5712 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH86990 45990 RIGHT WING INBOARD L/E UPPER FORMER 0.250 CRACK, STA XFS 207.500. REMOVED FASTENERS IAW SRM 51-1-20D PG 21. PERFORMED STOP HOLE AND FABRICATED REINFORCING ANGLE (AL7075T6 0.050) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND REINFORCING ANGLE IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 PG 9-10, SRM 51-1-20D PG 9. TORQUED IAW SRM 51-3-1 TABLE II. 2L74 4F RT4A25 20050601000362005060100036WP 2005 6 1 DHL2005807515 120050503A5330 DOUBLER DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH86990 45990 MODIFICATION DOUBLER AT AFT LWR CORNER OF RT PRIMARY HEAT EXCHANGER WITH 0.75 CRACK IN IT, STA 12.000 L-27R FUSELAGE EXTERIOR. PERFORMED MAJOR REPAIR. REMOVED ALL FASTENERS WITHIN THE REPAIR AREA IAW SRM 51-1-20D PG 21, SRM 51-3-0 PG 1. PERFORMED STOP HOLE AT END OF CRACK IAW EO AST050402. PERFORMED NDT INSP IAW NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER (AL2024T3 0.050), REPAIR TRIPLER (AL2024T3 0.050) IAW EO AST 050402. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW EO AST050402, SRM 51-1-20D PG 9, SRM 51-3-0 PG 1. TORQUED NUTS IAW SRM 51-3-1. 2L74 4F RT4A25 20050601000452005060100045WP 2005 6 1 DHL2005807524 120050505A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH86990 45990 MAIN CARGO COMPT FLOORBEAM UPPER FLANGE WORN, STA 798.000 LBL 38 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 04-27-05, EO AST050409 DATED 04-22-05. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. CUT OUT DAMAGED SECTION IAW EO AST050409. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED REPAIR ANGLE (EXTRUSION 7075T6 0.225) AND FILLER (AL7075T6 0.180) IAW EO AST 050409. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW EO AST 050409, SRM 51-1-20D PG 21-9, TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050601000462005060100046WP 2005 6 1 DHL2005807522 120050505A5330 DOUBLER DOUG DC8 DC873F 302199FWP FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH86990 45990 EXTERIOR FUSELAGE NR 2 ACCESS DOOR INTERNAL DOUBLER DAMAGED. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 04-20-05, EO AST050407 DATED 04-16-05. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. CUT OUT DAMAGED SECTION IAW EO AST050407. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED NEW INTERNAL DOUBLER SEGMENT (AL7075 -O- 0.050) AND 4EA INNER STRAPS (AL7075T6 0.050) IAW EO AST050407. HEAT TREATED NEW INTERNAL DOUBLER SEGMENT IAW SRM 51-1-1 PG 1, 13, 17 DPS 7.00 REV BK. CLEANED, TREATED AND PRIMED REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW EO AST050407, SRM 51-1-21 PG 1, SRM 51-3-0 PG 1, SRM 51-3-1 (TORQUE). 2L74 4F RT4A25 20050601000552005060100055EA 2005 6 1 VTZA200500081 120050515A2421 GENERATOR CNDAIRCL600 CL6002B19 1900309EA ELECTRICAL SYS DEPLOYED A VTZAA UNSCHED LANDING O OTHER CLCLIMB 1 EA27660BR 7519 AIR DRIVEN GENERATOR DEPLOYED IMMEDIATELY AFTER TAKEOFF. 2L72 4F RTA21EA 20050601000592005060100059NM 2005 6 1 AALA20050329 120050515A3350 CONNECTOR BOEING737 737823 13844BZNM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21912AN 29513 DFW - EMERGENCY PATH LIGHTING AT SEAT 7D INOPERATIVE. FOUND BAD CONNECTOR AT HARNESS IN SIDEWALL OF 7D. REPLACED EMERGENCY PATH LIGHT AT SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20050601000712005060100071EU 2005 6 1 MALA050403 120050429A2613 SENSOR SAAB SF340 340B 7860101EU TAIL PIPE DIRTY A MALAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL15403XJ 340B403 IN MEM, THE CREW ABORTED THE TAKEOFF DUE TO HIGH TAIL PIPE TEMPERATURE INDICATION. CLEANED SENSOR. 2L72 4T RTA52EU 20050601000782005060100078EU 2005 6 1 MALA050410 120050418A5753 FLAP BAC 146 AVRO146RJ85A1500097EU RT WING WORN A MALAK NONE O OTHER ININSP/MAINT 1 GL15503XJ E2310 DURING C1, C2 INSPECTION IN YYC FOUND RT IB FLAP TAB BOTTOM HAS WEAR MARKS FROM TAB FAIRINGS. 2H74 4F RTA49EU 20050601000812005060100081 2005 6 1 MALA050418 420050515A3460 COMPUTER BAC 146 AVRO146RJ85A1500097EU COCKPIT FAILED A MALAO OTHER O OTHER UKUNKNOWN 1 GL15506XJ E2314 FLIGHT GUIDANCE COMPUTER FAILED INFLIGHT. CREW DIVERTED TO DTW FOLLOWING FAILURE OF THE FLIGHT GUIDANCE COMPUTER. LANDING WAS UNEVENTFUL. REMOVED AND REPLACED DEGC. ALL CHECKS GOOD IAW RJ-85 MM CH 34 PN ON/OFF 4068300-904. SN ON 98080330 SN OFF 96110262. 2H74 4F RTA49EU 20050601000852005060100085EU 2005 6 1 MALA050401 120050505A243651539007B GCU SAAB SF340 340B 7860101EU E/E BAY FAILED A MALAO OTHER O OTHER UKUNKNOWN 1 GL15444XJ 340B444 AFTER DEPARTING FROM DTW, THE RIGHT HAND DC GENERATOR FELL OFF LINE. CREW FOLLOWED QRH TO TRY AND RESET IT, AND IT WOULD NOT COME BACK ONLINE. RETURNED TO DTW. REMOVED AND REPLACED DC GCU PN 51539-007B. SN ON 96944. SN OFF 97730 IAW SAAB AMM. ALL CHECKS GOOD. FOUND, RAN DC POWER FOR 20 MIN. 2L72 4T RTA52EU 20050601000962005060100096WP 2005 6 1 GTIA050120 120050404A3220 BOLT DOUG DC9 DC981 3022081WP NLG UNKNOWN A GTIAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL23818NK 48018 UPON RETRACTION LOUD RUMBLE AND VIBRATION NOTED. REPEATED PROCESS WITH SAME RESULT LOWERED GEAR AND RETURNED TO ACY LANDED BELOW LDG WT OF 128,000. FOUND SHEAR BOLT AT DRIVE RELEASE MECHANISM LEVER OF LEFT NLG. REMOVED AND REPLACED BOLT IAW MD80 MM 20-30-01. OPS CHECK OF DRIVE RELEASE MECHANISM OK IAW 32-22-02. NO OVERWEIGHT INSPECTION REQUIRED. (M) 2L72 4F A6WE 20050601001252005060100125NM 2005 6 1 SWAA051388 120050512A53306545766 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 468, STR 16R. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050601001292005060100129NM 2005 6 1 SWAA051392 120050512A2560PH22300L GLOWSTRIP BOEING737 7373H4 1384600NM CABIN DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29341SW 24091 DURING SCHEDULED C3 CHECK, FOUND PHOTOLUMINESCENT STRIPS DISCOLORED AT ROWS 1D, 7D & 9D. REMOVED AND REPLACED STRIPS PER MM. 2L72 4F RTA16WE 20050601001302005060100130NM 2005 6 1 SWAA051393 120050512A53116547959 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29352SW 24888 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 787, STR 22L TO STR 25L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050601001312005060100131NM 2005 6 1 SWAA051394 120050512A53146545866 KEELBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29352SW 24888 DURING SCHEDULED 1/2D CHECK, FOUND KEEL BEAM CORRODED AT BS 788, STR 27R. REPAIRED KEEL BEAM PER SWA EA. 2L72 4F RTA16WE 20050601001352005060100135NM 2005 6 1 SWAA051398 120050512A5610141A481018 WINDOW BOEING737 7377H4 1384404NM COCKPIT CRACKED A SWAAK NONE O OTHER UKUNKNOWN 1 SW29770SA 30589 R2 COCKPIT WINDOW STARTED ARCING, THEN SHATTERED. REMOVED AND REPLACED R2 WINDOW & HEAT CONTROLLER PER MM. 2L72 4F RTA16WE 20050601001432005060100143NM 2005 6 1 SWAA051403 120050513A53126546568 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND 2 EA CRACKS AT BS 1016 PRESS BULKHEAD WEB, STR 15L & STR 23R. REPAIRED BS 1016 PRESS BULKHEAD PER BFG ER. 2L72 4F RTA16WE 20050601001652005060100165WP 2005 6 1 GTIA050104 120050310A5240 STRUCTURE DOUG DC9 DC982 3022082WP R1 DOOR DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 DENT ON R1 DOOR FS 199 ONE INCH FROM AFT EDGE AND 13 INCHES FROM BOTTOM EDGE, D=.3, X=0.018 INCH, D/X=16/6. REMEASURED DENT AT R1 DOOR (D=0.3, X=.026 D/X 11.5). CUTOUT DAMAGED (DENTED) AREA. FABRICATED REPAIR DOUBLER AND FILLER. TREATED AND PRIMED, INSTALLED DOUBLER AND FILLER ON AFT R1 DOOR IAW SRM 51--30-2. (M) 2L72 4F A6WE 20050601001662005060100166NM 2005 6 1 05FDEA01272 120050514A2750MFGMS9391130Z POWER UNIT BOEING727 727227 1384078NM T/E FLAP LEAKING A FDEAA UNSCHED LANDING K FLUID LOSS CLCLIMB 1 SO25241FE 20979 DURING FLAP RETRACTION INDICATORS SHOWED SPLIT FLAP W/INBOARDS REMAINING AT 2 DEG W/FLAP UP. AFTER RUNNING QRH AND INBOARDS GOING TO FULL UP, HYD A SYSTEM INDICATED 0 QTY. RAN QRH AGAIN W/ALTERNATE FLAPS SYSTEM AND MANUAL GEAR EXTENSION PROCEDURES. WHEN ARRIVING AT A/C NOTICED HYD FLUID COMING FROM LT WHEEL-WELL AREA, OPENED GEAR DOORS AND FLAP DRIVE MOTOR WAS DUMPING FLUID. REMOVED AND REPLACED FLAP POWER UNIT HYDRAULIC MOTOR IN ACCORDANCE WITH 727-200 MM REF NR 27-51-062-4. SERVICED HYDRO, CYCLED FLAPS SEVERAL TIMES AND INDICATIONS FOLLOWED CORRECTLY. OPS CHK GOOD. NO LEAKS NOTED. 2L73 4F A3WE 20050601001922005060100192NM 2005 6 1 SWAA051443 120050517A53306545765 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D + 6, STR 15R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050601002032005060100203NM 2005 6 1 05FDEA01338 120050517A5730 PANEL DOUG MD11 MD11 3023602NM RT WING BULGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25580FE 48471 RIGHT WING TRAILING EDGE UPPER PANEL LEADING EDGE FOUND BULGING AT XORS 1042. REMOVED AND REPAIR CARRIED OUT AS PER FEDEX EA NR 1-5710-86607. 2L73 4F RTA22WE 20050601002042005060100204EU 2005 6 1 05FDEA01344 120050517A7160 ACOUSTIC PANEL AIRBUS300 A300F4605R 3930327EU NR 1 INTAKE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25653FE 736 COMPLY WITH EA 6-7110-55485 POWER PLANT-INLET COWL NR 1 ENGINE ACOUSTIC PANEL DENT REPAIR. REPAIRED AREA PER EA 6-7110-55485. 2L72 4F RTA35EU 20050601002062005060100206NM 2005 6 1 05FDEA01358 120050517A25506560958 INSULATION BOEING727 727233 138408ANM CABIN DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25254FE 20936 EQUIPMENT AND FURNISHINGS INSULATION BLANKETS. PARTIAL REPLACEMENT STA 360-1183, MAIN CABIN COMPARTMENT. COMPLIED WITH EA 7-2580-81692. 2L73 4F RTA3WE 20050601002112005060100211EU 2005 6 1 05FDEA01364 120050518A3350321430 BATTERY AIRBUS300 A300F4605R 3930327EU CABIN FAILED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25653FE 736 EMERGENCY LIGHT POWER SUPPLY FAILED TEST PER 33-51-14 (NR#N0060, W/O NR 28630). REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY IAW MM 33-51-14 TEST OF EMERGENCY LIGHTS GOOD IAW MM 33-51-14 (NR#N0060, W/O#28630) 2L72 4F RTA35EU 20050601002172005060100217WP 2005 6 1 ABXA050116 120050503A532029560321 BRACKET DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23946AX 47003 FRAME BRACKET CRACKED AND CORRODED AT STA 389, LONGERON 29 - 28 LEFT. REMOVED AND REPLACED BRACKET IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20050602000022005060200002WP 2005 6 2 ABXA050118 120050504A523059101419 PAN DOUG DC9 DC931 3022065WP CARGO DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23946AX 47003 FORWARD LOWER CARGO DOOR PAN FLANGE CRACKED AFT LATCH POSITION. REPAIRED AREA IAW DC-9 SRM 52-05. 2L72 4F A6WE 20050602000042005060200004WP 2005 6 2 ABXA050115 120050503A55325912166225 SKIN DOUG DC9 DC931 3022065WP VERTICAL STAB CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23946AX 47003 VERTICAL STAB JUST ABOVE AFT TIP OF RUDDER, LEFT SIDE, CRACKED AND MISSING FASTENERS. REPAIRED AREA IAW DC-9 SRM 55-01. 2L72 4F A6WE 20050602000052005060200005WP 2005 6 2 ABXA050119 120050510A531049122791 STOP FITTING DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23946AX 47003 STOP FITTING CRACKED FOR FORWARD LOWER CARGO DOOR JAMB TOP FORWARD FITTING. REPLACED FORWARD LOWER CARGO DOOR JAMB STOP FITTING IAW DC-9 SRM 51-30-5 AND 51-30-1. 2L72 4F A6WE 20050602000072005060200007 2005 6 2 DHL2005763003 420050518A3414 INDICATOR BOEING727 727264 138408MNM COCKPIT MALFUNCTIONED A DHLAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO01763AT 22983 REJECTED TAKEOFF AT APPROX 115 KTS ON CAPT AIRSPEED AND 90-95 ON F/O AIRSPEED INDICATOR WEIGHT 139.2 BRAKE ENERGY CHART SAYS MAINTENANCE INSP REQUIRED. ACCOMPLISHED HIGH ENERGY STOP CONDITIONAL INSPECTION IAW B727 MM 05-51-121, NO HEAT DAMAGE NOTED. 2L73 4F A3WE 20050602000102005060200010 2005 6 2 DHL2005763004 420050518A3414 INDICATOR BOEING727 727264 138408MNM COCKPIT FAULTY A DHLAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO01763AT 22983 RTO DUE TO 25 TO 30 KNOT DIFFERENCE BETWEEN CAPT AND F/O AIRSPEED INDICATOR. REPLACED F/O AIRSPEED INDICATOR, OPS CHECK NORMAL IAW B727 MM 34-12-21. 2L73 4F A3WE 20050602000112005060200011NM 2005 6 2 DHL2005783001 120050518A3260 CONNECTOR BOEING727 727227 1384078NM RT MLG DIRTY A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01783DH 21999 AFTER PLACING LANDING GEAR LEVER FROM UP TO OFF LANDING GEAR DOOR WARNING LIGHT ON FWD PANEL AND RIGHT GEAR DOOR LIGHT ON S OFFICIERS PANEL ILLUMINATED PERFORMED ABNORMAL PROCEDURE. REMOVED CONNECTOR TO RMLG DR SWITCH INSPECTED AND CLEANED CONNECTOR REINSTALLED SYS, OPS CHECKED OK ON GRD IAW B727 MM 32-31-00. 2L73 4F A3WE 20050602000122005060200012NM 2005 6 2 DHL2005741501 120050414A5320 TORQUE BOX BOEING727 7272Q9 138448MNM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21930 RT LOWER TORQUE BOX CRACKED IN AFT AIR STAIR WELL AT BS 1238. STOP DRILLED CRACK .250 IAW B727 SRM 51-10-1. FABRICATED REPAIR PART 7075-T6 .032 PO NR 9002090 (5 INCHES BY 3 INCHES) IAW B727 SRM 51-40-2 FIG 1 AND 53-10-2 FIG 6. TREATED AND PRIMED PART IAW B727 SRM 51-10-2. INSTALLED REPAIR PART IAW B727 SRM 51-40-2 FIG 1 AND 51-30-2 FIG 7. 2L73 4F RTA3WE 20050602000132005060200013NE 2005 6 2 AWXA200500568 220050517A73203957985205 INTERFACE UNIT AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE NR 2 ENGINE FAULTY A AWXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP28636AW1956 42 098 EN ROUTE TO EWR PILOTS REPORTED A NR 2 ENGINE EIU FAULT. ACFT RETURNED TO PHX WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE ENGINE INTERFACE UNIT IAW AMM 73-25-3-04 AND PERFORMED A POWER ASSURANCE TEST IAW AWA TASKCARD NR F5M71302. OPERATIONAL CHECK WAS GOOD. TEAR DOWN REPORT SHOWS THE EIU SN 4076 PASSING FUNCTIONAL TESTS AND ENVIRONMENTAL TESTS IAW CMM 73-25-35 REV. 4. MINOR DENTS WERE NOTED ON THE UNIT BUT ARE CONSIDERED COSMETIC IN NATURE. UNIT DID NOT NEED ANY CALIBRATION ADJUSTMENTS. 2L72 4F4 FRTA28NM E311NE 20050602000162005060200016NM 2005 6 2 DHL2005740515 120050331A5320 TORQUE BOX BOEING727 7272Q9 138448MNM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH46106 21930 CRACK ON TORQUE BOX UPPER WEB STA 1231. REMOVED FASTENERS FOR ACCESS CUT OUT DAMAGED AREA DIM 5 X 1.75 INCH AT WEB LOWER TORQUE BOX BS 1231 IAW B727 SRM 51-30-2 AND 51-40-2 FIG 1. HFEC INSP CUTOUT WITH NO CRACKS NOTED IAW B727 NDT MAN PT6 51-00-00 FIG 23. FABRICATED DOUBLER FROM 7075 T6 .040 PO 9001777 DIM 7 X 5 FILLER FROM 7075 T6 .032 DIM 5 X 1.75 INCH PO 9813 IAW B727 SRM 51-40-2 FIG 1. TREATED AND PRIMED FILLER AND DOUBLER IAW B727 SRM 51-10-2 AND INSTALLED FILLER AND DOUBLER REPAIR AT L/ LWR TORQUE BOX WEB BS 1231 IAW B727 SRM 51-40-2 FIG 1. 2L73 4F RTA3WE 20050602000182005060200018NM 2005 6 2 DHL2005740516 120050324A5720 SUPPORT ANGLE BOEING727 7272Q9 138448MNM LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 LEFT WING ROOT FIXED LEADING EDGE HAS LOWER ANGLE SUPPORT CRACKED L/E STA 130. REMOVED FASTENERS FOR ACCESS AT LEFT WING ROOT FIXED EDGE L/E STA 130 STOP DRILLED CRACK .250 TERMINATED AT END OF CRACKED IAW B727 SRM 51-10-1 NDT HFEC INSP PER B727 NDT MAN PT6 51-00-00 FIG 23. CRACK ENDS IN STOP DRILL HOLE. FABRICATED ANGLE REPAIR MAT USED 2024 T3 .063 PO 9002118 DIM 9.5 X 2 INCHES IAW B727 SRM 51-40-3 FIG 1 AND 57-20-2. ALODINED AND PRIMED AREA AND PART IAW B727 SRM 51-10-2. INSTALLED ANGLE REPAIR IAW B727 SRM 51-40-3 FIG 1 AND 57-20-2 FIG 1. 2L73 4F RTA3WE 20050602000222005060200022WP 2005 6 2 UPS05844472 120050506A5313DC853B00939 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE:C3 LONGERON CRACKED 1/4 INCH LONG AT STA 1726 L15L. REMOVED AND REPLACED LONGERON SECTION AND INSTALLED STRAPS 2 EA IAW DC-8 SRM 53-02-02, 51-1-8, 53-2-2 FIG 10 AND 51-1-20D. 2L74 4F RT4A25 20050602000232005060200023WP 2005 6 2 UPS05844474 120050429A53203755827U2 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE:C3 C-1 CARGO FITTING CRACKED AT FS 280 L32R. FOUND ON X-RAY OF DOOR CORNER EO DC8-5330-20206-B. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-2. 2L74 4F RT4A25 20050602000242005060200024WP 2005 6 2 UPS05844475 120050430A5320SAA565122116 WEB DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 RT MLG AFT WEB CRACKED AT GEAR CUTOUT LWR CORNER OLD REPAIR CRACKED IN RADIUS. REMOVED WEB, FAB REPLACEMENT WEB AND INSTALLED IAW SRM51-1-21, 51-1-21D, SAA FAB TRAVLER NR 0001 AND 21-1-21A. 2L74 4F RT4A25 20050602000262005060200026WP 2005 6 2 UPS05844477 120050427A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE:C3 FUSELAGE SKIN AT APROX STA 1723 L16L HAS CRACK APROX 3/4 INCH LONG. REMOVED EXISTING DOUBLER AND FINGER DOUBLER AND FABRICATED EXTERNAL DOUBLER AND INSTALLED EXISTING FINGER DOUBLER, EXTERNAL DOUBLER AND FILLER IAW DC-8 SRM 51-1-21, 51-1-20D, 53-2-1 FIG 7, 51-1-20D AND 51-1-11. 2L74 4F RT4A25 20050602000272005060200027NM 2005 6 2 DHL2005740522 120050324A5754 SKIN BOEING727 7272Q9 138448MNM PWA JT8 JT8D17 52049NE L/E SLAT DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 NR 1 SLAT EXTERNAL SKIN DENTED AT W STA 738. REMOVED PANELS AND WEB FROM SLAT NR 1 FOR ACCESS. CUTOUT DAMAGED AREA FROM EXT SKIN 3.25 INCH BY 3.125 INCH, TRIMMED OUT SKIN AND ACCESS TO DOUBLER IAW SRM. FAB PARTS FILLER 3 .125 INCH BY 3.0625 MAT 2024 2024 T3 .04 PO NR 9001938 DOUBLER 3EA 6.5 INCH BY 1.75 INCH WITH 2024T3 .04 PO NR 9001938 AND FILLERS 4.75 INCH BY .75 INCH, 5.125 INCH BY .75 INCH, 3.375 INCH BY .75 INCH , 2.375 INCH BY 3.25 INCH AND 6EA 1.375 INCH BY .75 INCH WITH 2024T3 .125 PO 9001666 AND COVERS .025 2024T3 8.75 INCH BY 3.75 INCH, 1.75 INCHES BY 8.375 PO NR 9001873 IAW SRM. TREATED AND PRIMED PARTS IAW SRM. INSTALLED REPAIR PARTS, CLOSED PANEL IAW SRM. 2L73 4F4 FRTA3WE E2EA 20050602000322005060200032NM 2005 6 2 QXEA200500851 120050512A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09412QX 4059 PDX - RIGHT INBOARD SEAT TRACK HAS LIGHT CORROSION ON TOP OF SEAT LUG RAILS AT X 0.0 TO X 1.0. REPAIRED IAW DHC-8 400 SRM 51-42-05, 51-40-10 AND SRM 42-42-45. 2H72 4T RTA13NM 20050602000332005060200033NM 2005 6 2 QXEA200500852 120050512A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09412QX 4059 PDX - RIGHT INBOARD SEAT TRACK HAS PITTING CORROSION ON EXPOSED SURFACES AT X19-X27, X37-X41 AND X67-X71. REPAIRED IAW DHC-8-400 SRM 51-42-05, 51-40-11 AND SRM 51-42-45. 2H72 4T RTA13NM 20050602000342005060200034NM 2005 6 2 QXEA200500849 120050513A5720 BRACKET BOMBDRDHC8 DHC8401 1390041NM RT WING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09412QX 4059 PDX - RIGHT WING INBOARD LOWER TRAILING EDGE SHROUD SECOND BRACKET FROM INBOARD END AFT BRACKET CRACKED. REPAIRED IAW RD 8/4-57-261. 2H72 4T RTA13NM 20050602000352005060200035EU 2005 6 2 MALA050420 120050426A2913521449 PUMP BAC 146 AVRO146RJ85A1500097EU NR 2 MALFUNCTIONED A MALAO OTHER J WARNING INDICATION UKUNKNOWN 1 GL15505XJ E2313 CREW RETURNED TO MSP AFTER DEPARTURE FOLLOWING YELLOW HYDRAULIC SYSTEM HIGH TEMPERATURE. EMERGENCY TRUCKS WERE CALLED AND FLIGHT LANDED WITHOUT FURTHER INCIDENT. FOUND AC PUMP COMING ON LINE CAUSING YELLOW HYD HIGH TEMP NOTED DURING YELLOW SYS FLT CONT OPERATION NR 2 HYD EDP PRESS DROP BELOW 1500 PSI CAUSING A/C PUMP TO AUTO ARM. REPLACED NR 2 HYD EDP P/N 521449, S/N ON F911285, S/N OFF F9911343. REF AMM 29-10-17. OPS AND LEAKS CHECKS GOOD. RAN NR 2 AND NR 3 ENGINE WITH EDP'S ON DURING HYD SERVICE. 2H74 4F RTA49EU 20050602000392005060200039 2005 6 2 MALA050424 420050517A344220412170414 TRANSCEIVER BAC 146 AVRO146RJ85A1500097EU WEATHER RADAR MALFUNCTIONED A MALAO OTHER J WARNING INDICATION UKUNKNOWN 1 GL15533XJ E2367 THE WEATHER RADAR DISPLAY IS SHOWING RT FAULT. REPLACED WX RADAR RT, P/N 204-1217-0414, S/N ON 7576, S/N OFF 7213. 2H74 4F RTA49EU 20050602000422005060200042SO 2005 6 2 LR7A05092 120050506A5312 BULKHEAD LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03405LC 731 5025 DURING SCHEDULED B-3 CHECK FOUND CABIN BULKHEAD CRACKED AT RT FS477 WL210 BL55R. WEB REPAIRED IAW SMP583 FIG 53-40-09. RT FS477 WL210 BL55R. NR 2056. 2H74 4T4 T A1SO E282 20050602000432005060200043NM 2005 6 2 CALA0500154 120050517A5730 SKIN BOEING757 757224 1384958NM RT WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714107 27297 INSPECTION FOUND A 10 INCH CRACK IN RT WING FIXED LEADING EDGE SKIN AT FSS 416. REPAIRED IAW EA 5731-01010, REV D AND SRM 51-40-02 AND IAW MM 27-81-02. 2L72 4F RTA2NM 20050602000442005060200044WP 2005 6 2 CALA0500155 120050517A5313S27779226 LONGERON DOUG DC9 DC983 3022083WP FUSLEAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714879 49526 INSPECTION FOUND LONGERON 30 CORRODED WITH POPPED RIVETS AT STA 484. A NEW SECTION OF LONGERON WAS INSTALLED IAW SRM 53-02, FIGURE 18. 2L72 4F RTA6WE 20050602000452005060200045NM 2005 6 2 HNAA0500043 120050517A291082970009125 HYDRAULIC LINE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE HYDRAULIC SYS LEAKING A HNAAD RETURN TO BLOCK K FLUID LOSS CLCLIMB 1 EA07807EX3395333953 292 LOST NR2 HYDRAULIC CONTENTS AFTER TAKEOFF, INDICATOR SHOWS .5 QTS. REMOVED AND REPLACED DOOR SEQUENCE VALVE PRESSURE LINE. 2H72 4T4 TRTA13NM E20NE 20050602000482005060200048NM 2005 6 2 05FDEA01280 120050514A5315 FLOORBEAM BOEING727 727227 1384078NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 UPPER LOBE INTERIOR, STR 950A, LBL 10-22 TOP OF FLOORBEAM CORRODED. REPAIRED FLOORBEAM PER SRM 53-10-8. 2L73 4F A3WE 20050602000492005060200049NM 2005 6 2 05FDEA01285 120050514A5312AGA717041 BULKHEAD DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25621FE 48792 CENTER CARGO, STA 1841 FLOOR AREA BULKHEAD APPROX X= 3 WEB FOUND CRACKED. CRACKED AREA OF WEB AT CENTER CARGO STA 1841 FLOOR AREA BULKHEAD X= 3 TRIMMED OUT AS PER SRM 53-00-01 FIGURE 5 VOLUME I. REPAIR FILLER AND DOUBLER FABRICATED AND INSTALLED AS PER SRM 53-00-01 FIGURE 5 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2L73 4F RTA22WE 20050602000502005060200050NM 2005 6 2 05FDEA01366 120050518A5330 SKIN BOEING727 727227 1384078NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 CRACK IN SKIN AT BODY STATION 1053 STR 28L. 2L73 4F A3WE 20050602000512005060200051EU 2005 6 2 05FDEA01368 120050518A5330 SKIN AIRBUS300 A300B4605R 3930308EU FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25679FE 793 A/C FUSELAGE RT SIDE FR 55 STR 39 HAS GOUGES REF N00057. BLENDED AREAS AND CHECKED LIMITS IAW SRM 53-10-00 AND 53-16-12 WITHIN LIMITS IAW SRM 53-10-12 FIG 102. FOLLOW UP INSP REQ AT OR BEFORE 1500FC AS STATED ON EA 6-5330-89211 AND SRM 53-10-12 FIG 102. 2L72 4F RTA35EU 20050602000522005060200052WP 2005 6 2 05FDEA01369 120050518A5330 DOUBLER DOUG MD10 MD1010F 3022112WP FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568049 47803 REPAIR DOUBLER STA 808-824 L47L-L46L REQUIRES EVALUATION. INSTALLED NEW REPAIR IAW DC-10 SRM 53-20-00, FIG 13 DETAIL VOL 1 SHT 5. 2L73 4F RTA22WE 20050602000532005060200053WP 2005 6 2 05FDEA01370 120050518A5755ARC0391503 BRACKET DOUG DC10 DC1030F 3023504WP NR 1 SPOILER CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25303FE 46802 COMPLY WITH EA 8-5740-55486, WINGS, NR 1 SPOILER ACTUATOR MOUNT HOLD-DOWN BRACKET CORROSION. COMPLIED WITH EA 8-5740-55486, WINGS NR 1 SPOILER ACTUATOR MOUNT/HOLD-DOWN BRACKET CORROSION. 2L73 4F RTA22WE 20050602000552005060200055NM 2005 6 2 HNAA0500045 120050516A3260864202 PROXIMITY SENSOR DHAV DHC8 DHC8102 2809003NM LANDING GEAR BROKEN A HNAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA07912HA5009150091 040 LEFT AMBER GEAR DOOR LIGHT ON DURING GEAR RETRACTION. REPLACED PROXIMITY SENSOR. (M) 2H72 4T RTA13NM 20050602000572005060200057NM 2005 6 2 HNAA0500044 120050516A5330 SKIN DHAV DHC8 DHC8102 2809003NM FUSELAGE DAMAGED A HNAAK NONE O OTHER TXTAXI/GRND HDL 1 EA07331 279 TUG STRUCK AIRCRAFT LEAVING A GASH APPROX 3 FEET LONG AFT OF BAG BAY DOOR. 2H72 4T RTA13NM 20050602000592005060200059 2005 6 2 70891 420050518A6122 CONNECTOR BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA PROP GOVERNOR DIRTY A AMWAD RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TXTAXI/GRND HDL 1 CE07163YV UE163 RT PROP WILL ONLY MAKE 1550 UNDER POWER. MAINTENANCE CLEANED OVERSPEED GOVERNOR CONNECTOR PLUG. THEREFORE NO PARTS WERE USED. 2L72 4T3 TRTA24CE E2NE 20050602000612005060200061NM 2005 6 2 98 120050519A5320 FITTING BOEING737 737522 138449FNM FUSELAGE DAMAGED B K NONE O OTHER ININSP/MAINT 1 SO15953UA 26700 STRINGER 13L END FITTING REQUIRES PERMANENT REPAIR. 2L72 4F RTA16WE 20050602000622005060200062NM 2005 6 2 99 120050519A5230 SKIN BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE CARGO DOOR DENTED B K NONE O OTHER ININSP/MAINT 1 SO15953UA 26700 NUMEROUS DENTS ON AFT CARGO DOOR SKIN AND CREASES ON THE REPAIR DOUBLER. S/O 269010, NR 22292 2L72 4F4 FRTA16WE E2GL 20050602000632005060200063SO 2005 6 2 XGN2005F00004 220050504A8530TISN712ACA CYLINDER CONT IO520C BEECH 58 58 1152740CE CONT O520 IO520C 17032SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW05577W 400 561711 TH375 561711 CYLINDERS WERE FOUND DURING COMPRESSION CHECK AT THE 100 HOUR INSPECTION. WE ARE USING A SOAP SOLUTION TO DETECT CRACKS IN THE EXHAUST SIDE OF THE CYLINDER WHILE DOING A COMPRESSION CHECK. WE ARE DOING COMPRESSION CHECKS EACH 50 HOURS. 3 CRACKED CYLINDERS WERE FOUND ON THE SAME ENGINE AT THIS INSPECTION. (K) 1L72 3O3 O 3A16 E5CE 20050602000662005060200066NM 2005 6 2 DHL2005741503 120050414A5320 TORQUE BOX BOEING737 7372Q9 138448MNM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 RT LOWER TORQUE BOX CRACKED IN AFT AIR STAIR WELL AT BS 1225. STOP DRILLED CRACK (.250) IAW B727 SRM 51-10-1. FABRICATED DOUBLER 7075-T6, .032 PO NR 209041(5 INCH BY 3 INCH) IAW B727 SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1. TREATED AN PRIMED AREA AND PART IAW B727 SRM 51-10-2. INSTALLED DOUBLER IAW B727 SRM 51-40-2 FIG 1 AND 51-30-2. 2L72 4F A16WE 20050602000682005060200068NM 2005 6 2 DHL2005741504 120050414A5320 TORQUE BOX BOEING737 7372Q9 138448MNM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 LT LOWER TORQUE BOX CRACKED AT BS 1213 IN AFT STAIR WELL. REMOVED EXISTING FASTENERS IN AREA AND CUT OUT DAMAGED SECTION (1 IN BY 1 IN) IAW B727 SRM 51-40-2 FIG 1. FABRICATED DOUBLER 7075-T6 .032 PO NR 900878 (5 1/2 INCH BY 2 1/2 INCH), FILLER 7075-T6 .025 7075-T6 PO NR 900878 IAW B727 SRM 53-10-2 FIG 6 AN 51-40-2 FIG 1. TREATED AN PRIMED REPAIR PARTS IAW B727 SRM 51-10-2. INSTALLED REPAIR AT AFT AIRSTAIR TORQUE BOX IAW B727 SRM 51-40-2 FIG 2, FIG 1 AN 51-30-2. 2L72 4F A16WE 20050602000702005060200070NM 2005 6 2 DHL2005741505 120050414A5320 TORQUE BOX BOEING727 7272Q9 138448MNM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 LT LOWER TORQUE BOX CRACKED AT BS 1233 IN AFT AIR STAIR WELL. STOP DRILLED CRACK .250 IAW B727 SRM 51-10-1 FABBED PART 7075-T6 .032, PO NR 209041 (5 INCH BY 3 INCH) IAW B727 SRM 53-10-2 FIG 6, 51-40-2. TREATED AN PRIMED AREA AND PART IAW B727 SRM 51-10-2. INSTALLED REPAIR IAW B727 SRM 51-40-2 AN 51-30-2. 2L73 4F RTA3WE 20050602000712005060200071EA 2005 6 2 VTZA200500082 120050517A2910 HYDRAULIC LINE CNDAIRCL600 CL6002B19 1900309EA HYDRAULIC SYS CHAFED A VTZAA UNSCHED LANDING K FLUID LOSS CRCRUISE 1 EA27658BR 7500 NR 1 HYDRAULIC SYSTEM LOST ALL FLUID DUE TO CHAFFED LINES FROM A FAILED FAIRLEAD BLOCK NEAR THE NR 1 HYDRAULIC RESERVOIR. 2L72 4F RTA21EA 20050602000732005060200073WP 2005 6 2 MWEA050045 120050518A5240 SERVICE DOOR DOUG DC9 DC982 3022082WP AFT NOT CLOSED A MWEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31809ME 48071 CABIN FLOW LIGHT ON, AFT FLIGHT ATTENDANT REPORTED GALLEY SERVICE DOOR LEAKING. FOUND SERVICE DOOR BAYONET IMPROPERLY POSITIONED IN BAYONET ROLLER, OPENED AND CLOSED DOOR INSPECTED DOOR AND BAYONET. NO DEFECTS NOTED, PRESSURIZED AIRCRAFT AND CHECKED DOOR AND AFT ACCESSORY FOR LEAKING. NO LEAKING NOTED. 2L72 4F A6WE 20050602000762005060200076EA 2005 6 2 A6WA200540163 120050503A5610 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A A6WAA UNSCHED LANDING O OTHER CRCRUISE 1 GL31432AW 7257 CAPTAINS WINDSCREEN CRACKED AT 32 FL FOLLOWED QUICK REFERENCE HANDBOOK AND DECLARED EMERGENCY. DIVERTED TO BUFFALO, NO SIGNS OF CRACKING ON INSIDE OR OUTSIDE OF WINDSCREEN. REMOVED AND REPLACED CAPTAINS WINDSCREEN. OPS AND LEAK CHECK GOOD REFERENCE CHAPTER 56-11-01. (M) 2L72 4F RTA21EA 20050602000802005060200080SO 2005 6 2 C2XA05CL034 120050507A3350110049 CHARGER EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714558 145598 CLE FLIGHT NR 2634 , THE CREW REPORTED BOTH AFT OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 4 BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20050602000822005060200082WP 2005 6 2 0500759866 120050504A5312 BULKHEAD DOUG DC9 DC951 3022051WP FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01775NC 47785 DURING "H" CHECK, FOUND CRACK IN BULKHEAD SKIN AT BS 37. REPAIRED PER EA 98-203212. 2L72 4F RTA6WE 20050602000852005060200085SO 2005 6 2 C2XA05BT030 120050509A335074441 SIGN EMB 145 EMB145XR 3260214SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713118 145672 EWR - CO2641, DURING ROUTINE CHECK MAINTENANCE FOUND EMERGENCY EXIT LIGHT SIGN ABOVE FLIGHT ATTENDANTS FORWARD JUMPSEAT INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT MARKING SIGN ASSEMBLY ABOVE FLIGHT ATTENDANTS FORWARD JUMPSEAT IAW EMB AMM NR 33-50-14, OPS CHECKED GOOD. 2L72 4F RT 20050602000862005060200086SO 2005 6 2 C2XA05IA072 120050512A3350744412 SIGN EMB 135 EMB135LR 3260305SO CABIN UNSECURE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2727523 145389 IAH - DURING 3A INSPECTION, THE FORWARD RIGHT EMERGENCY EXIT SIGN WAS FOUND TO BE INOPERATIVE. MAINTENANCE RE-SECURED THE CONNECTOR ON THE SIGN, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050602000872005060200087NE 2005 6 2 KBM2005F00052 220050427A72100235237600 CHIP DETECTOR SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE ENGINE DEFECTIVE E KBMAO OTHER J WARNING INDICATION NRNOT REPORTED 1 WP19351WM 2167 ENGINE CHIP LIGHT ON. REMOVED AND REPLACED ENGINE HORIZONTAL CHIP DETECTOR. (M) 1G71 3U3 U H9EU E19EU 20050602000892005060200089SO 2005 6 2 C2XA05CL036 120050516A2560P2070005120 HOLDER EMB 145 EMB145LR 3260212SO FLASHLIGHT CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713949 145057 DURING ROUTINE MAINTENANCE, THE F/A`S FLASHLIGHT HOLDER/CHARGER WAS FOUND CRACKED AND THE FLASHLIGHT WOULD NOT STAY LOCKED ONTO THE HOLDER. MAINTENANCE REPLACED THE FLASHLIGHT HOLDER. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20050602000932005060200093EU 2005 6 2 KBM2005F00055 120050421A7160350A54108421 SEAL SNIAS 350 AS350B2 8680813EU AIR INTAKE DAMAGED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19751H 3403 AIR INTAKE SEAL REQUIRED REPLACEMENT. REMOVED AND REPLACED. (M) 1G71 3U H9EU 20050602000952005060200095WP 2005 6 2 BMAC050006 220050513A7200 ENGINE JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE331* 01514WP RIGHT BIRD STRIKE A B16AE ENGINE SHUTDOWN C F.O.D. DEDESCENT 1 NE05536PA 681 P63075 AIRCRAFT EXPERIENCED "BIRD STRIKE" DURING DESCENT AT 3500 FEET. MAINTENANCE REPLACED PROPELLER, SPINNER, AND TO REPLACE RT ENGINE FOR TEARDOWN INSPECTION. 2L72 4T3 TRTA41NM E2WE 20050602000962005060200096EU 2005 6 2 KBM2005F00057 120050411A2435150SG10095 BRUSHES SNIAS 350 AS350B2 8680813EU STARTER/GEN WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19345SH 3345 BRUSH WORN BEYOND LIMITS. (M) 1G71 3U H9EU 20050602000972005060200097EU 2005 6 2 DHL2005365003 120050518A4930 FUEL LINE AIRBUS300 A300B4203 3930306EU APU RUPTURED A DHLABF EMER. DESCENT ACTIVATE FIRE EXT. KA FLUID LOSS FLAME/FIRE APAPPROACH 1 SO01365DH 149 APU FIRE ON APU START DURING APPROACH. PERFORMED VISUAL INSP AND FOUND A RUPTURED FUEL LINE. FOUND NO STRUCTURAL DAMAGE. VERIFIED FUEL SHUT OFF VALVE IN CLOSED POS AND DEACTIVATED. EVACUATED REMAINING FUEL IN APU. PERFORMED HEAT DAMAGE EVALUATION IAW 2L72 4F RTA35EU 20050602000982005060200098CE 2005 6 2 20030846 120050517A5511 SPAR BEECH 1900 1900D 1154162CE HORIZ STAB CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03202UX UE202 DURING ROUTINE INSPECTION, FOUR CRACKS APPROX .5 INCH LONG FOUND EXTENDING FROM THE DE-ICE LINE HOLE IN THE HORIZONTAL MAIN SPAR WEB. REPAIRED IAW WITH COMPANY EO. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA24CE 20050602000992005060200099EU 2005 6 2 KBM2005F00058 120050324A6230350A37116200 RETAINER SNIAS 350 AS350BA 8680817EU MAIN ROTOR BROKEN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19115SH 3141 DROP RING RETAINER CRACKED AND BROKEN BETWEEN BLUE AND YELLOW BLADES. REMOVED AND REPLACED. (M) 1G71 3U NCH9EU 20050602001002005060200100EU 2005 6 2 AWXA200500570 120050517A3397ABS0374A24 WIRE AIRBUS320 A320231 3930325EU CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28625AW 064 PHX - EEL - DURING ROUTINE MX ROW 17 ABC EMERGENCY EXIT ESCAPE PATH LIGHTING WAS INOPERATIVE. TERMINALS CONNECTING WIRES TO SEAT ASSEMBLY INOPERATIVE. MAINTENANCE RETERMINATED TERMINALS AT ROW 17 A,B,C IAW AMM 20-48-14. OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050602001012005060200101NM 2005 6 2 AWXA200500571 120050429A53156546811 FLOORBEAM BOEING737 7373B7 1384580NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28332AW 23384 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON THE TOP OF THE BS 986.5 T-CAP AT LBL 18, WL 208 ON PREVIOUS REPAIR CAP. MAINTENANCE REMOVED AND REPLACED TEE CAP REPAIR ON TOP OF BS 986.5 BEAM AT WL208 FROM LBL50 TO RBL50 IAW AWA ER 03-5310-05125-ES2. 2L72 4F RTA16WE 20050602001032005060200103NM 2005 6 2 AWXA200500576 120050429A5320654583473 INTERCOSTAL BOEING737 7373B7 1384580NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28332AW 23384 MCN - MAJOR REPAIR - DURING C-18 CHECK A CRACK WAS FOUND AT A INTERCOSTAL TOP CHORD ANGLE BETWEEN BS 294, RBL 30, WL 208. MAINTENANCE REMOVED, FABRICATED, AND REPLACED INTERCOSTAL TOP CHORD ANGLE IAW B737-300 SRM 51-40-02-0 (FIGURES 3,4,8, AND 12), B737-300 SRM 51-30-01-0 (FIGURE 7) AND BOEING DRAWING 65-45834. 2L72 4F RTA16WE 20050602001042005060200104NM 2005 6 2 AWXA200500578 120050429A53156545808179 FLOORBEAM BOEING737 7373B7 1384580NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28332AW 23384 MCN - MAJOR REPAIR - DURING C-18 CHECK, EXFOLIATION CORROSION WAS FOUND ON TOP AND BOTTOM SECTIONS OF T-CAP LOCATED AT BS 294, RBL 38, WL 208. MAINTENANCE REMOVED, REPAIRED AND REINSTALLED T-CAP IAW B737-300 SRM 53-10-51-2 (FIGURE 205). 2L72 4F RTA16WE 20050602001072005060200107NM 2005 6 2 AWXA200500581 120050428A575465C266031585P WEDGE BOEING737 7373B7 1384580NM L/E SLAT DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28332AW 23384 MCN - FLIGHT CONTROL - DURING C-18 CHECK, DELAMINATION WAS FOUND AT THE NR 4 SLAT WEDGE. DELAMINATION WAS FOUND ON TOP AND BOTTOM SURFACES. MAINTENANCE FOUND THAT THE DELAMINATION WAS BEYOND REPAIRABLE LIMITS. MAINTENANCE REMOVED AND REPLACED THE NR 4 SLAT ASSEMBLY IAW B737-300 AMM 27-81-21-4. 2L72 4F RTA16WE 20050602001102005060200110NM 2005 6 2 AWXA200500584 120050502A532069156096 ATTACH ANGLE BOEING737 7373B7 1384580NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28332AW 23384 MCN- MAJOR REPAIR- DURING C-18 CHECK, A CRACK WAS FOUND AT A UPPER DOOR STOP FITTING ATTACH ANGLE CLIP, THAT WAS LOCATED AT BS 349, STRINGER 16L. MAINTENANCE REMOVED, FABRICATED AND REPLACED UPPER DOOR STOP FITTING ATTACH ANGLE CLIP IAW AMERICA WEST AIRLINES ENGINEERING REPAIR 03-5300-05135-SS1. 2L72 4F RTA16WE 20050602001112005060200111NM 2005 6 2 AWXA200500585 120050429A33503404302 CONNECTOR BOEING737 7373B7 1384580NM CABIN DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28332AW 23384 MCN- EEL- DURING C-18 CHECK, EPLS HARNESS WAS FOUND TO HAVE SEVERAL DAMAGED CONNECTORS AND HOOK UPS THAT WERE LOCATED ON HARNESS AND AIRCRAFT SIDE. MAINTENANCE REMOVED AND REPLACED CONNECTORS AND HOOK UPS FOR EPLS HARNESS AND AIRCRAFT CONNECTION SIDE IAW BSWPM 20-90-14 (PAGE 1-7), BSWPM 20-42-01 (PAGE 1-4). OPERATIONAL CHECK WAS COMPLIED WITH PER AMERICA WEST AIRLINES TASK CARD NR A1C33006 2L72 4F RTA16WE 20050602001132005060200113EA 2005 6 2 QXEA200500854 120050428A5755 FASTENER CNDAIRCL600 CL6002C10 1390015EA SPOILER LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - LEFT WING BOTTOM TRAILING EDGE, MULTI FUNCTION SPOILER SHROUD HAS SMOKY FASTENERS. REPLACED FASTENERS IAW CRJ-700 SRM 51-42-06-001-A01. 2L72 4F RTA21EA 20050602001152005060200115EA 2005 6 2 QXEA200500856 120050502A5730 PANEL CNDAIRCL600 CL6002C10 1390015EA LT WING DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - LEFT WING LEADING EDGE PANEL HAS RUBBING MARKS AT TWO LOCATION. REPAIRED IAW CRJ-700 SRM 51-12-00-001-001-A01 AND SRM 51-25-00-001-001-A01. 2L72 4F RTA21EA 20050602001172005060200117EA 2005 6 2 QXEA200500858 120050502A5414 SKIN CNDAIRCL600 CL6002C10 1390015EA LT NACELLE GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - LEFT NACELLE LIP SKIN HAS GOUGES AND SCRATCHES AT 6 O'CLOCK POSITION. REPAIRED IAW CRJ-700 SRM 54-11-01-201-001-A01 AND SRM 51-21-11-001-001-A01. 2L72 4F RTA21EA 20050602001192005060200119EA 2005 6 2 QXEA200500862 120050508A5320 FITTING CNDAIRCL600 CL6002C10 1390015EA FUSELAGE GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FORWARD BAGGAGE BAY DOOR SURROUND STRUCTURE FORWARD UPPER GUIDE FITTING GOUGED AT STATION 536.00 AND STRINGER 21L. REPAIRED IAW REO 670-53-31-037, HORIZON AIR EA R-53-330, CRJ-700 SRM 51-21-16-001-001 AND CRJ-700 AMM TASK 52-35-00-710-801-A01. 2L72 4F RTA21EA 20050602001222005060200122EA 2005 6 2 QXEA200500861 120050503A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA FUSELAGE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FORWARD FUSELAGE - LOWER PANEL ROCK CHIP DAMAGE AT STATION 285.00 AND 310.00, BETWEEN STRINGER 25R AND 25L. REPAIRED IAW CRJ-700 SRM 51-26-00-001-001-A01, 51-123-00-001-001-A01 AND 51-25-16-001-001-A01. 2L72 4F RTA21EA 20050602001292005060200129NM 2005 6 2 EIA2005105 120050513A5330 SKIN BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 NDT - LT FUSELAGE SKIN UNDER DRAG SPLICE FITTING AT BS980, STRINGER 38L. FOUND ONE EACH FASTENER HOLE CRACKED. SKIN REPAIRED AT SA 950-990, BTN STRINGER 36L AND STRINGER 39L, PER SRM 53-3-03 FIGURE 60, AND HAECO REPAIR SCHEME, R53-21-35304. 2L74 4F A20WE 20050602001302005060200130NM 2005 6 2 EIA2005106 120050513A5313 STRINGER BOEING747 747212B 1384886NM FUSELAGE DAMAGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 FX - DURING BS 980 LT SKIN REPAIR, FOUND STRINGER 37L AND SKIN HAD A METALLIC PLUG INSTALLED PREVIOUSLY. REPAIRED STRINGER 37L AT BS 970- BS 983, AND REPAIRED SKIN AT BS 950 TO BS 990, BETWEEN STRINGER 36L AND 39L PER HAECO REPAIR SCHEME R-53-21-35304. 2L74 4F A20WE 20050602001322005060200132NM 2005 6 2 EIA2005108 120050513A5322 SHEAR TIE BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 M/D BS 1940 RT STRINGER 4 TO 5 SHEAR TIE FOUND CRACKED. CRACKED SHEAR TIE REPLACED PER SRM 51-10-01, P9. 2L74 4F A20WE 20050602001332005060200133NM 2005 6 2 EIA2005109 120050513A5322 SHEAR TIE BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 M/D STA 1880 RT STRINGER 4 TO 5, SHEAR TIE FOUND CRACKED. CRACKED SHEAR TIE REPLACED PER SRM 51-10-01, P 9. 2L74 4F A20WE 20050602001362005060200136NM 2005 6 2 EIA2005112 120050513A5322 SHEAR TIE BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 M/D BS 1920 STRINGER 4R TO 5R, SHEAR TIE FOUND CRACKED. CRACKED SHEAR TIE REPLACED PER SRM 51-10-01 2L74 4F A20WE 20050602001382005060200138NM 2005 6 2 EIA2005114 120050513A5322 SHEAR TIE BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 M/D BS 1820 STRINGER 4R TO 5R SHEAR TIE FOUND CRACKED. CRACKED SHEAR TIE REPLACED PER SRM 21-10-01. 2L74 4F A20WE 20050602001392005060200139NM 2005 6 2 EIA2005115 120050513A5322 SHEAR TIE BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 M/D BS 1800 STRINGER 4R TO 5R SHEAR TIE FOUND CRACKED. CRACKED SHEAR TIE REPLACED PER SRM 51-10-01. 2L74 4F A20WE 20050602001402005060200140NM 2005 6 2 EIA2005116 120050513A5322 SHEAR TIE BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 M/D BS 1780 STRINGER 4R TO 5R, SHEAR TIE FOUND CRACKED. CRACKED SHEAR TIE REPLACED PER SRM 51-10-01. 2L74 4F A20WE 20050602001422005060200142NM 2005 6 2 EIA2005118 120050513A5347 SEAT TRACK BOEING747 747212B 1384886NM FUSELAGE UNKNOWN A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 M/D BS 610 TO BS 620 LBL 33, SEAT TRACK RT-05, FIG 1A. 2L74 4F A20WE 20050602001432005060200143NM 2005 6 2 EIA2005119 120050513A5347 SEAT TRACK BOEING747 747212B 1384886NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 M/D BS 1535 TO BS 1545, LBL 33, SEAT TRACK CROWN FOUND CORROSION. M/D BS 1480 TO BS 1550, SEAT TRACK SECTIONAL REPLACED PER SRM 53-10-05, FIG 1A. 2L74 4F A20WE 20050602001442005060200144NM 2005 6 2 EIA2005120 120050513A5347 SEAT TRACK BOEING747 747212B 1384886NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 M/D BS 1000, LBL 33, SEAT TRACK OUTBOARD FLANGE FOUND CORROSION. M/D BS 990 TO BS 1000, LBL 33, SEAT TRACK SECTIONAL REPLACED PER SRM 53-10-05 FIG 1A. 2L74 4F A20WE 20050602001452005060200145NM 2005 6 2 EIA2005121 120050513A5347 SEAT TRACK BOEING747 747212B 1384886NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 M/D BS 996 RBL 33, SEAT TRACK, RT FLANGE FOUND CORROSION. SEAT TRACK AT BS 990 TO BS 1000, RBL 33, SECTIONAL REPLACED PER SRM 53-10-05, FIG 1A. 2L74 4F A20WE 20050602001472005060200147NM 2005 6 2 EIA2005123 120050513A5347 SEAT TRACK BOEING747 747212B 1384886NM FUSELAGE BROKEN A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 M/D BS 1883 RBL 11, SEAT TRACK FLANGE FOUND BROKEN. M/D BS 1870 TO BS 1950 RBL 11, SEAT TRACK REPAIRED PER SRM 53-10-05, FIG 14. 2L74 4F A20WE 20050602001482005060200148NM 2005 6 2 EIA2005124 120050513A3350 LIGHT BOEING747 747273C 1384896NM CABIN INOPERATIVE A EIAAK NONE L NO TEST ININSP/MAINT 1 NM09471EV 20651 DURING INSPECTION, FOUND EMERGENCY LIGHT AT STATION 600 L/S INOPERATIVE. RELAMPED LIGHT ASSEMBLY 600 L/S, OP'S CHECK GOOD IAW MM 33-51-07. 2L74 4F A20WE 20050602001502005060200150NM 2005 6 2 EIA2005127 120050518A3350 LIGHT BOEING747 747212B 1384886NM CABIN INOPERATIVE A EIAAK NONE L NO TEST ININSP/MAINT 1 NM09486EV 20888 L5 DOOR AFT EMERGENCY EXIT LIGHT FOUND INOP. REMOVED AND REPLACED LIGHT ASSY IAW MM 33-51-05. 2L74 4F A20WE 20050602001522005060200152NM 2005 6 2 ANCF200400050 120050514A2810 TANK DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE LT WING LEAKING W ANCFK NONE K FLUID LOSS DEDESCENT 1 SO23593AN 53093 DURING FLIGHT A FUEL LEAK WAS DETECTED ON LEFT MAIN FUEL TANK. ALL FUEL FLOW NORMAL AND ENGINE CONSUMPTION WAS NORMAL. PER AMM 72-00-04 P 197 ACCOM T/S FOUND FUEL PUMP DUCT CORK. ADJ IAW 73-34-01PG 201. RUN UP TEST NORMALLY IAW 72-44-0 PAG 532 , NO LEAKS FOUND. AFTER REACH TOP OF CLIMB NOTICED LACK OF FUEL BUT DUE TO FLIGHT LEVEL PLAN CHANGED 320 TO 340, DIDN'T NOTICE ABNORMAL SITUATION. 5 MINUTES BEFORE TOP OF DESCENT WE HAD A LACK OF 3000 POUNDS, MADE APPROX AND AFTER SECOND ATTEMPT LANDED. ATC WAS INFORMED BEFORE LANDING AND THEY KEPT THE PLANE IN A PARALLEL WAY TO AVOID FUEL CONTAMINATION OF THE PLATFORM. AVIANCA'S MAINTENANCE TEAM NEEDS TO WAIT FOR CIVIL INSPECTOR TO CHECK THE AIRPLANE. 2L72 4F4 FRT E9NE 20050602001532005060200153NM 2005 6 2 DHL2005765002 120050519A242150086003 CIRCUIT BREAKER BOEING727 727264 138408MNM COCKPIT FAULTY A DHLAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO01765AT 23014 AFTER CARGO DOOR WAS CLOSED, CREW SMELLED ACRID ODOR IN COCKPIT. REMOVED AND REPLACED APU GEN CIRCUIT BREAKER IAW 727 MM CHI 24-20-41. REPAIRED WIRES TO TERMINAL L2 IAW 727 SWIM CHI 20-30-13. 2L73 4F A3WE 20050602001542005060200154EU 2005 6 2 SA05052 120050519A3350 LIGHT AIRBUSA319 A319112 3930323EU CABIN MALFUNCTIONED A USAAK NONE O OTHER ININSP/MAINT 1 EA19724UW 1122 BOS - EMERGENCY LIGHT TEST AT PTP SHOWS 'TEST OK" BUT THE GREEN LIGHT DOES NOT ILLUMINATE. MAINTENANCE ACTION PENDING. 2L72 4F RTA28NM 20050531001392005053100139NM 2005 5 31 2005UALA00418 120050506A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29586UA 26710 AFT PIT FRAME DENTED STA 1560, STR 26L. FRAME DENT WAS TRIMMED OUT AND J ANGLE REPAIR INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050531001402005053100140NM 2005 5 31 2005UALA00419 120050506A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29586UA 26710 AFT PIT FRAME DENTED STA 1460, STR 26L. FRAME DENT WAS TRIMMED OUT AND J ANGLE REPAIR INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050531001432005053100143NM 2005 5 31 2005UALA00422 120050506A5240 DOOR FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE R4 DOOR CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29586UA 26710 DOOR R4 FWD FRAME AT STA 1645 IS CORRODED. REPAIR CONSISTED OF REMOVING CORROSION AND INSTALLING 0.032 REPAIR DOUBLER AS OUTLINED IN REPAIR DOCUMENT. 2L72 4F4 FRTA2NM E17NE 20050531001462005053100146NM 2005 5 31 2005UALA00425 120050506A5311 FRAME BOEING737 737322 1384676NM FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29312UA 23673 LT AND RT BS 616 FRAME CHORD WEB CRACKED JUST BELOW CREASE BEAM. MAJOR REPAIR ACCOMPLISHED. REMOVED THE CRACK. ACCOMPLISHED HFEC NO CRACKS FOUND, FABRICATED FILLER AND ANGLE AND INSTALLED THE REPAIR. 2L72 4F RTA16WE 20050531001562005053100156NM 2005 5 31 2005UALA00435 120050509A5230 DOOR FRAME BOEING737 737322 1384676NM CARGO DOOR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29312UA 23673 AFT CARGO DOOR FWD FRAME BS 795 WAS FOUND CRACKED AT EXISTING JOINT WITH LOWER FRAME SECTION. CUTOUT DAMAGE ON UPPER FRAME AND REPLACED LOWER FRAME AND INSTALLED WITH NESTED 'U' CHANNEL. 2L72 4F RTA16WE 20050531001612005053100161NM 2005 5 31 2005UALA00440 120050512A5313 STRINGER BOEING737 737322 1384676NM FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29314UA 23675 STR 25L HAS CORROSION FROM STA 767 TO 787. 2L72 4F RTA16WE 20050531001622005053100162NM 2005 5 31 2005UALA00441 120050512A5230 STOP FITTING BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE CARGO DOOR DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29672UA 30027 AFT CARGO DOOR STOP FITTING WAS BLENDED BEYOND LIMITS. 2L72 4F4 FRTA1NM E24NE 20050531001632005053100163WP 2005 5 31 GTIA050099 120050404A5320 WEB DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE FUSELAGE PUNCTURED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 AT STA 200, NR 1 SEAT TRACK LT FLOOR WEB HAS A PUNCTURE. CUT OUT PUNCTURE FROM FLOOR WEB STA 200, NR 1 SEAT TRACK. FABRICATE DOUBLERS AND FILLERS. TREATED AND PRIMED, INSTALLED DOUBLER AND FILLER IAW SRM. (K) 2L72 4F4 F A6WE E9NE 20050531001702005053100170NM 2005 5 31 DHL2005740012 120050324A5754 RIB BOEING727 7272Q9 138448MNM L/E SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 NR 4 SLAT CRACKED AT ACTUATOR I/B RIB. REMOVED NR 4 SLAT TO FOM SHEET METAL REPAIR IAW B727MM 27-81-11, REMOVED ACCESS PANEL IAW B727 SRM 51-30-2, REMOVED FASTENERS FOR REPAIR AND RIBS IAW B727 SRM 51-30-2, FABRICATED NEW RIBS I/B AND O/B MAT USED 2024T3 .040 PO 9001938 DIM 15 X 6 INCH IAW B727 SRM 51-20-1 AND 57-50-2 FIG 2. ALODINED AND PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED NEW RIBS IAW B727 SRM 51-20-1 AND 57-50-2 FIG 2. OK TO CLOSE ACCESS PANEL, INSTALLED ACCESS PANELS IAW B727 SRM 51-30-2, REINSTALLED NR 4 SLAT IAW B727 MM 2781-11, OPS AND LEAK CHECK GOOD. 2L73 4F RTA3WE 20050531001712005053100171WP 2005 5 31 GTIA050137 120050415A5260 DOOR DOUG DC9 DC982 3022082WP AFT AIRSTAIRS DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23829NK 49931 FTW - FOUND DENT ON LOWER AFT CORNER OF AFT AIRSTAIR DOOR STATION 1510, D=.5, X=.040. CUT OUT DENTED AREA. FABRICATED DOUBLER AND FILLER. TREATED, PRIMED AND INSTALLED REPAIRED DOUBLER AND FILLER. (M) 2L72 4F A6WE 20050531001732005053100173WP 2005 5 31 GTIA050135 120050413A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23829NK 49931 FTW - WEB CRACKED AT STATION 210 LEFT CABIN JUST AFT OF L1 DOOR BAYONET CATCH. TRIMMED OUT CRACKED AREA. FABRICATED DOUBLER AND FILLER. TREATED, PRIMED AND INSTALLED REPAIRED PARTS. (M) 2L72 4F A6WE 20050531001802005053100180WP 2005 5 31 GTIA050133 120050416A5230 HINGE DOUG DC9 DC982 3022082WP BARRIER DOOR CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23829NK 49931 FORWARD PIT, BARRIER DOOR SUPPORT HINGE HALF CRACKED, 3 HOLES MOUNTING CRACKED. REMOVED HINGE AND BLENDED OUT CRACK IN HINGE. STOP DRILLED CRACK IN HAT CHANNEL. PERFORMED DYE PEN, SHOWS CRACK CONTAINED. FABRICATED DOUBLER ON BARRIER DOOR SUPPORT HINGE. (M) 2L72 4F A6WE 20050531001812005053100181WP 2005 5 31 GTIA050095 120050310A5330 SKIN DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE FUSELAGE DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 DENT ON FUSELAGE SKIN FS421 BETWEEN LONGERONS 19R AND 20R (D=0.5 INCH, X=0.008 INCH, D/X - 62.5 INCHES). REMOVED CARGO DOOR TO FOM IAW SRM. FOUND DENT HAS GOUGED IN CENTER, REMOVED DAMAGED AREA OF SKIN (1.5 INCH X 0.8 INCH) IAW SRM. FABRICATED DOUBLER AND FILLER IAW SRM. TREATED AND PRIMED, INSTALLED REPAIRED PARTS IAW SRM. INSTALLED FWD CARGO DOOR IAW SRM. INSTALLED FWD PIT BARRIER DOOR IAW SRM. LEAK AND FAIR CHECK IAW MM. (K) 2L72 4F4 F A6WE E9NE 20050531001842005053100184WP 2005 5 31 GTIA050093 120050311A5320 STRAP DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 ALUMINUM STRAP ON LOWER SIDE OF L2 DOOR THRESHOLD HAS CORROSION. STRAP CORROSION IS OUT OF LIMITS. FABRICATED NEW STRAP IAW SRM. TREATED AND PRIMED, INSTALLED STRAP ON L2 DOOR THRESHOLD IAW SRM. (K) 2L72 4F4 F A6WE E9NE 20050601000042005060100004NE 2005 6 1 DXTA200500721 220050504A73204106T48P19 FADEC AMD FALC50FALCON2000 2730170NM CFE CFE73811B NE NR 2 MALFUNCTIONED E DXTAE ENGINE SHUTDOWN E VIBRATION/BUFFET ININSP/MAINT 1 GL07210QS4074 211 P105340 DURING NR 2 ENGINE START - INITIALLY EXPERIENCED SURGING NOISE WHICH EVOLVED INTO EXTREMELY VIOLENT VIBRATION RESULTING IN SHAKING ENTIRE A/C AND THEN IT IMMEDIATELY BEGAN RAPID RISE TO YELLOW ARC PRIOR TO MANUAL SHUTDOWN. REPLACED NR 2 B FADEC IAW FALCON 2000 MM CH 76-00. GROUND CHECKED GOOD. 2K73 4F4 FRTA50NM E44NE 20050601000072005060100007WP 2005 6 1 GTIA050082 120050310A5320 CUSP WEB DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 MID PIT STA 522-636, A LONG 18, RBL 52, FLOOR PANEL UNDER FEDDER CABLES CORRODED. REMOVED CORROSION FROM 522-636, FOUND OUT OF LIMITS. REMOVED WEB STA 503-598, FABED NEW WEB, PRIMED AND TREATED. INSTALLED WEB AT STA 503-598, RBL 52, IAW SRM. (K) 2L72 4F4 F A6WE E9NE 20050601000232005060100023WP 2005 6 1 DHL2005807517 120050503A2150 DOUBLER DOUG DC8 DC873F 302199FWP HEAT EXCHANGER CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH86990 45990 LT PRIMARY HEAT EXCHANGER; AFT LWR CORNER MODIFICATION DOUBLER WITH 0.75 CRACK IN IT, STA 12.000 L-27L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 04-16-05, EO AST050401 DATED 04-12-05. REMOVED ALL FASTENERS WITHIN THE REPAIR AREA. PERFORMED STOP HOLE AT END OF CRACK IAW EO AST050401. NDT INSPECTED AREA IAW NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER (AL2024T3 0.050) AND REPAIR TRIPLER (AL2024T3 0.050) IAW EO AST050401. CLEANED, TREATED AND PRIMED REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW EO AST 050401, SRM 51-3-0 PG 1, SRM 51-1-20D PG 9. TORQUED NUTS IAW SRM 51-3-1. 2L74 4F RT4A25 20050601000292005060100029NM 2005 6 1 DHL2005783503 120050405A5524 CLIP BOEING727 727227 1384078NM RT ELEVATOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01783DH 21999 RIGHT ELEV T/E UPPER & LWR ADJOINING CLIPS CRACKED AT ELEV STA 60 MARKED. REMOVED CLIP IAW B727 SRM 51-30-2, FAB'D CLIPS USING 2024T3 .032 PO 9002034 DIM 3 X .75 INCH IAW B727 SRM 55-20-2 FIG 1. ALODINED AND PRIMED PARTS IAW B727 SRM 51-10-2. REINSTALLED RIGHT ELEVATOR T/E UPPER AND LWR CLIPS IAW B727 SRM 51-30-2 AND 55-20-2 FIG 1. 2L73 4F A3WE 20050601000372005060100037WP 2005 6 1 DHL2005807502 120050408A5347S2772660 CARGO TRACK DOUG DC8 DC873F 302199FWP DHL2005807517 DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH86990 45990 MAIN CARGO COMPT NR 4 TRACK LUGS DETERIORATED STA 1700.000. CUT OUT DAMAGED SECTION AND FABRICATED SPLICES (AL7075T6 0.160) (AL7075T6 0.125) (AL7075T6 0.100) IAW SRM 53-2-3 PG 49-50 FIG 14. CLEANED, TREATED AND PRIMED AREA AND SPLICES IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT AND SPLICES IAW SRM 53-2-3 PG 49-50 FIG 14, SRM 51-3-0 PG 1. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050601000472005060100047WP 2005 6 1 DHL2005807525 120050503A5730 CAP DOUG DC8 DC873F 302199FWP LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH86990 45990 LT WING INBOARD L/E SLANT PANEL UPPER CAP CORRODED STA XFS 138.750 - 151.250. PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW SRM 51-3-0 PG 1. PERFORMED BLENDEOUT (7.125*1.875*0.092) FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG 37. PERFORMED VISUAL DETAIL INSPECTION, NO CORROSION NOR CRACK FOUND. FABRICATED FILLER (AL7075T6 0.080) AND EXTERNAL REPAIR DOUBLER (AL7075T6 0.125) IAW BOEING SKETCH 05-04-18-001, SRM 57-2-1 FIG 37. CLEANED, TREATED AND PRIMED REPAIR PARTS IAW SRM 51-1-8B. INSTALLED FILLER ON SLANT PANEL UPPER CAP WITH PRC SEALANT IAW SRM 51-1-15 PG 1, BOEING SKETCH 03-04-18-001, SRM 57-2-1 FIG 31 AND EXTERNAL REPAIR DOUBLER. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050601000702005060100070EU 2005 6 1 MALA050417 120050514A2434 GENERATOR SAAB SF340 340B 7860101EU LEFT OVERTEMP A MALAO OTHER M OVER TEMP UKUNKNOWN 1 GL15439XJ 340B439 LT DC GENERATOR OVER TEMP CAUTION LIGHT ILLUMINATED. CREW TURNED BACK TO LBE FOLLOWING OVER TEMPERATURE INDICATION OF THE DC GENERATOR. LANDING WAS UNEVENTFUL. REPLACED GENERATOR. 2L72 4T RTA52EU 20050601000872005060100087EU 2005 6 1 MALA050393 120050425A2120 ODOR SAAB SF340 340B 7860101EU COCKPIT DETECTED A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL15369PX 340B295 AFTER TAKEOFF A "BURNT TOAST" SMELL IN COCKPIT, DURING TAKEOFF, BLEEDS ON AUTO, TEMP SEL ON 7, ADJUSTED TO 5. SMELL WENT AWAY AFTER 30 SECONDS. SMELL LASTED APPROXIMATELY 1 MINUTE. MAINTENANCE GROUND RAN A/C AT FULL "HOT" FOR APPROXIMATELY 15 MINUTES. NO SMELL NOTED IN COCKPIT. ALL ENGINE INDICATIONS NORMAL. INSPECTED ACM OIL LEVEL, AND HEAT EXCHANGER. NO DEFECTS NOTED. INSPECTED ENGINE INLET AND EXHAUST. NO DEFECTS NOTED. 2L72 4T RTA52EU 20050601000882005060100088EU 2005 6 1 MALA050402 120050429A2613 SENSOR SAAB SF340 340B 7860101EU RT TAIL PIPE DIRTY A MALAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL15403XJ 340B403 ON TAKEOFF ROLL, THE RIGHT TAIL PIPE HOT LIGHT ILLUMINATED. CREW ABORTED TAKEOFF AT 70 KNTS WITH MINIMUM BRAKING. CLEANED SENSOR. 2L72 4T RTA52EU 20050601000922005060100092WP 2005 6 1 GTIA050124 120050426A2780 CONTROL CABLE DOUG DC9 DC983 3022083WP L/E SLAT OUT OF ADJUST A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 ON WALKAROUND, FOUND LEFT WING SLATS NOT FULLY RETRACTED, AIRCRAFT TAIL SWAP WITH 832. REMOVED CABLE 212B LEFT WING NR 1 L/E SLAT AND INSTALLED NEW CABLE RUN, OPS CHECK GOOD. (M) 2L72 4F RTA6WE 20050601001362005060100136NM 2005 6 1 SWAA051399 120050512A335007912 COVER BOEING737 7377H4 1384404NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29793SA 27888 DURING SCHEDULED MV2 CHECK, FOUND SEVERAL EEPLS COVERS CRACKED AT ROWS 1 TO ROW 17. REMOVED AND REPLACED EEPLS COVERS PER MM. 2L72 4F RTA16WE 20050601001392005060100139NM 2005 6 1 SWAA051419 120050516A552365C26485 TRIM TAB BOEING737 7373H4 1384600NM LT ELEVATOR DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 LT ELEVATOR TRIM TAB LOWER T/E DELAMINATED. REPAIRED TAB PER SWA EA. 2L72 4F RTA16WE 20050601001492005060100149NM 2005 6 1 SWAA051425 120050516A3350101114 LIGHT BOEING737 7377H4 1384404NM EXTERIOR INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29499WN 32481 DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT LIGHT, AFT OF L1 DOOR INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050601001532005060100153WP 2005 6 1 GTIA050111 120050308A5323 STRUCTURE DOUG DC9 DC982 3022082WP CATWALK CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 CATWALK SIDE FILLER STTION 1361 LEFT AND RIGHT IS CRACKED IN RADIUS. STOP DRILLED CRACKS ON CAT WALK STATION 1361 LEFT AND RIGHT. FABRICATED TWO REPAIR DOUBLER LEFT AND RIGHT WEB REPAIR. TREATED AND PRIMED, INSTALLED TWO REPAIR ON CATWALK STATION 1361 LEFT AND RIGHT IAW SRM 51-70-4 AND 51-30-2. (M) 2L72 4F A6WE 20050601001642005060100164WP 2005 6 1 GTIA050105 120050310A5230 SKIN DOUG DC9 DC982 3022082WP CARGO DOOR DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 DENT ON AFT CARGO DOOR FS 1183 22.5 INCH FROM TOP EDGE AND 26 INCHES FROM AFT EDGE OF DOOR, D=1 INCH, X=.016 INCH, D/X=62. DENT ON AFT CARGO DOOR FS 1183 UNDER CONDITION 1B IS ACCEPTABLE. DYE PENETRANT INSPECTION AFT CARGO DOOR FS 1183. CUTOUT DAMAGED SECTION. FABRICATE REPAIR DOUBLER AND FILLER. TREATED AND PRIMED, INSTALLED DOUBLER AND FILLER IAW SRM 52-05 FIG 1 AND 51-30-2. (M) 2L72 4F A6WE 20050601001712005060100171NM 2005 6 1 05FDEA01278 120050514A5330 SKIN BOEING727 727227 1384078NM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 DENT IN SKIN BS 1348, STR 22L. REPLACED SKIN PANEL PER SRM 51-30-2. 2L73 4F A3WE 20050601001722005060100172NM 2005 6 1 05FDEA01282 120050514A5312 DOUBLER DOUG MD11 MD11F 3023600NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25580FE 48471 LANDING GEAR, CENTER LANDING GEAR RIGHT HAND FORWARD BULKHEAD SIDE DOUBLER CRACKED. DOUBLER REMOVED AND NEW DOUBLER INSTALLED AS PER SRM 51-33-01 VOLUME II. 2L73 4F RTA22WE 20050601001842005060100184WP 2005 6 1 GTIA050100 120050309A5320 SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FORWARD PIT CEILING, STATION 484 RBL 34, BUSTED NUT PLATE AND DAMAGED STRUCTURE SUPPORT. REMOVED AND REPAIRED DAMAGED SUPPORT IAW SRM 53-01. TREATED AND PRIMED, INSTALLED DOUBLER AND SUPPORT IAW 51-30-2. (M) 2L72 4F A6WE 20050601001942005060100194NM 2005 6 1 SWAA051431 120050517A55536547450 FITTING BOEING737 7373H4 1384600NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND LT & RT VERTICAL STAB ATTACH FITTING FWD & AFT PRIMARY CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER. 2L72 4F RTA16WE 20050601002072005060100207NM 2005 6 1 05FDEA01359 120050517A5315 FLOORBEAM BOEING727 727233 138408ANM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25254FE 20936 FLOORBEAM LBL 7-RBL 40 UPPER CHORD REQUIRES MAJOR REPAIR. REMOVED AND REPLACED UPPER T-CHORD IAW SRZ 53-034E REPAIR NR 7. 2L73 4F RTA3WE 20050601002082005060100208NM 2005 6 1 05FDEA01360 120050517A5753 FAIRING BOEING727 727233 138408ANM T/E FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25254FE 20936 LT WING LOWER T/E FLAP TRACK SKATE FAIRING BEHIND MLG STRUT IS CRACKED. REMOVED AND REPLACED SKATE FAIRING IAW SRM 51-30-2. 2L73 4F RTA3WE 20050601002092005060100209NM 2005 6 1 05FDEA01361 120050518A5313 LONGERON DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25580FE 48471 FUSELAGE-CORROSION OBSERVED IN CENTER ACCESSORY COMPARTMENT ON LONGERON 49R BETWEEN STATION 6-70 TO 6-90. REMOVED AND REPAIR CARRIED OUT AS PER FEDEX EA NR 1-5310-86604. 2L73 4F RTA22WE 20050601002102005060100210NM 2005 6 1 05FDEA01363 120050518A5330 SKIN DOUG MD11 MD11 3023602NM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25580FE 48471 FUSELAGE GOUGE MARK FOUND ON RIGHT HAND FUSELAGE STATION 1959 BETWEEN LONGERON 31 AND 32. TRIMMED OUT AND CARRIED OUT REPAIR AS PER SRM 53-20-00 VOLUME I FIGURE 6. REPAIR ACCOMPLISHED UNDER CATEGORY 'B' AND REQUIRE REPETITIVE INSPECTION AS PER FEDEX EA NR 1-5330-86627. 2L73 4F RTA22WE 20050602000032005060200003WP 2005 6 2 ABXA050114 120050502A57539957579 STRUCTURE DOUG DC9 DC931 3022065WP T/E FLAP CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23946AX 47003 RIGHT FLAP NR 2 TRAILING EDGE SECTION HAD BULGING RIVETS ON THE LOWER SURFACE AT THE OUTBOARD AFT CORNER. REPAIRED AREA IAW DC-9 SRM. 2L72 4F A6WE 20050602000062005060200006NM 2005 6 2 DHL2005740514 120050327A5753 SKIN BOEING727 7272Q9 138448MNM T/E FLAP DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH46106 21930 CUT OUT DAMAGED AREA LWR SKIN APPROX 5 X 1.5 INCH IAW B727 SRM 51-40-20 FIG 31. FABRICATED ONE FILLER APPROX 5 X 1.5 INCH AND ONE DOUBLER APPROX 8 X 3 INCHES USING .016 2024-T3 PO 9001660 IAW B727 SRM 57-50-2 FIG 4. CLEANED, PREPPED, APPLIED ADHESIVE PRIMER AND ADHESIVE TO ALL REPAIR SURACES AND BAGGED FOR BONDING IAW B727 SRM 51-40-20 FIG 31. CURED REPAIR CLEANED AND PERFORMED POST BOND INSP WITH NO DELAM NOTED IAW B727 SRM 51-40-20. TREATED, PRIMED AND SEALED REPAIR IAW B727 SRM 51-40-2. 2L73 4F RTA3WE 20050602000092005060200009NM 2005 6 2 DHL2005741500 120050418A5730 SKIN BOEING727 7272Q9 138448MNM RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21930 RT WING T/E SKIN CRACKED AT NR 11 SPOILER 32 HINGE CUTOUT. STOP DRILLED CRACK RT WING T/E SKIN AT NR 11 SPOILER IAW B727 SRM 51-10-1. FABRICATED REPAIR DOUBLER FROM MATERIAL USE 7075T6 .071 PO NR 900573 IAW B727 SRM 57-30-4 FIG 11. DIMENSIONS 6 INCHES BY 4 INCHES, TREATED AN PRIMED IAW B727 SRM 51-10-2 PARTS INSTALLED IAW B727 SRM 57-30-4 FIG 11. 2L73 4F RTA3WE 20050602000152005060200015NM 2005 6 2 DHL2005741502 120050414A5320 TORQUE BOX BOEING727 7272Q9 138448MNM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01 21930 RT LOWER TORQUE BOX CRACKED IN AFT AIR STAIR WELL AT BS 1225. STOP DRILLED CRACK (.250) IAW B727 SRM 51-10-1. FABRICATED DOUBLER 7075T6,.032 PO NR 209041, (5 INCHES BY 3 INCHES) IAW B727 SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1. TREATED AN PRIMED AREA AND PART IAW B727 SRM 51-10-2, INSTALLED DOUBLER IAW B727 SRM 51-40-2 FIG 1 AND 51-30-2. 2L73 4F RTA3WE 20050602000172005060200017EA 2005 6 2 A6WA200540161 120050501A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31417AW 7600 RIGHT FS 621 FLOOR SUPPORT ANGLE IS CRACKED. PERFORMED A MAJOR REPAIR BY REMOVING DAMAGED ANGLE AND INSTALLING A REPAIR ANGLE IAE BOMBARDIER, INC REO 601R-53-61-117 REV C. (M) 2L72 4F RTA21EA 20050602000202005060200020WP 2005 6 2 UPS05844470 120050504A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE:C3 LT WING L/E AT XFS 454, LWR SURFACE FASTENER HOLES ARE ELONGATED. REMOVE DAMAGE AND INSTALLED DOUBLER AND FILLER IAW EO DC-8 5720- 7767-A AND SRM 51-1-21. 2L74 4F RT4A25 20050602000212005060200021WP 2005 6 2 UPS05844471 120050503A5712 RIB DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE:C3 LT WING L/E UPPER RIB CRACKED 1/4 INCH LONG AT XFS779. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE DOUBLER IAW SRM 57-2-0 FIG 2, DWG 5769470-29 AND SRM 51-1-20D,51-1-21 AND 51-1-15. 2L74 4F RT4A25 20050602000312005060200031NM 2005 6 2 QXEA200500850 120050513A5720 DIAPHRAGM BOMBDRDHC8 DHC8401 1390041NM WING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09412QX 4059 PDX - YW 191.20 AND TRAILING WING SHROUD NACELLE DIAPHRAGM CRACKED. REPAIRED IAW DHC8/400 SRM 51-42-05-330-801. 2H72 4T RTA13NM 20050602000382005060200038EU 2005 6 2 MALA050423 120050515A5230 DOOR SAAB SF340 340B 7860101EU CARGO DOOR DAMAGED A MALAK NONE O OTHER TXTAXI/GRND HDL 1 GL15413XJ 340B413 CREW NOTED A SMALL DENT/CREASE UNDER THE CARGO DOOR. PERFORMED EDDY CURRENT WITH NO DEFECTS NOTED. NO FURTHER ACTION NEEDED. 2L72 4T RTA52EU 20050602000402005060200040CE 2005 6 2 ACE051805 120050518A561010138402523 WINDSHIELD BEECH 1900 1900C 1154161CE PWA PT6 PT6A60A 52043NE COCKPIT CRACKED E YADAK NONE O OTHER NRNOT REPORTED 1 AL03111AX 2553 UC81 PILOT REPORTED LT WINDSHIELD CRACKED OUTER PLY VERIFIED CRACKED - REPLACED WINDSHIELD (WITHIN MFG. WARRANTY PERIOD). 2L72 4T4 TRTA24CE E4EA 20050602000412005060200041SO 2005 6 2 LR7A05091 120050506A5312 BULKHEAD LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03405LC 731 5025 DURING SCHEDULED B-3 CHECK FOUND AFT FUSELAGE INTERIOR BULKHEAD CRACKED 4 INCHES VERTICALLY AT FS880 LHS LOWER POSITION WL200 BL68R. WEB REPAIRED IAW SMP583 FIG 51-140-17. LT FS880 WL200 BL68L. NR 2019 2H74 4T4 T A1SO E282 20050602000472005060200047NM 2005 6 2 05FDEA01279 120050514A5313 STRINGER BOEING727 727227 1384078NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 FOUND CRACK IN STR 24L BS 560. REPAIRED STRINGER PER SRM 53-10-3. 2L73 4F A3WE 20050602000602005060200060SO 2005 6 2 XGN2005F00003 220050504A8530TISN712ACA CYLINDER CONT IO520C BEECH 58 58 1152740CE CONT O520 IO520C 17032SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW05577W 400 561711 TH375 561711 CYLINDERS WERE FOUND DURING COMPRESSION CHECK AT THE 100 HOUR INSPECTION. ARE USING A SOAP SOLUTION TO DETECT CRACKS IN THE EXHAUST SIDE OF THE CYLINDER WHILE DOING A COMPRESSION CHECK. WE ARE DOING COMPRESSION CHECKS EACH 50 HOURS. 3 CRACKED CYLINDERS WERE FOUND ON THE SAME ENGINE AT THIS INSPECTION. (K) 1L72 3O3 O 3A16 E5CE 20050602000722005060200072EA 2005 6 2 A6WA200540164 120050503A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31451AW 7832 LHS FS 621 FLOOR SUPPORT ANGLE IS CRACKED. INSTALLED REPAIR ANGLE IAW BOMBARDIER, INC REO 601R-53-61-117 REV C. (M) 2L72 4F RTA21EA 20050602000782005060200078CE 2005 6 2 GUU2005F00011 120050225A32404500SA1 VALVE BEECH 1900 1900D 1154162CE PARK BRAKE FAILED A GUUAO OTHER O OTHER TXTAXI/GRND HDL 1 SO2981538 UE199 FLT 9132 - EYW/TPA - DURING TAXI, RIGHT BRAKE LOCKED UP. REMOVED AND REPLACED RIGHT PARKING BRAKE VALVE. (M) 2L72 4T RTA24CE 20050602000912005060200091EU 2005 6 2 KBM2005F00053 120050413A2910 HYDRAULIC LINE SNIAS 350 AS350B2 8680813EU HYDRAULIC SYS LEAKING E KBMAO OTHER K FLUID LOSS CRCRUISE 1 WP193455H 3345 HYDRAULIC HOSE FAILED DURING CRUISE FLIGHT, 10 MINUTES IN TO FLIGHT. FOUND PIN HOLE IN LINE. REMOVED AND REPLACED HYDRAULIC LINE. (M) 1G71 3U H9EU 20050602001022005060200102NM 2005 6 2 AWXA200500572 120050429A5315654581094 FLOORBEAM BOEING737 7373B7 1384580NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28332AW 23384 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION ON THE BOTTOM SURFACE OF THE BS 312 T-CAP LWR AFT REPAIR SPLICE ANGLE AT RBL 21 WL 208. MAINTENANCE REMOVED, FABRICATED, INSTALLED, REPLACEMENT SPLICE ANGLE ON BOTTOM SURFACE OF BS312 TEE CAP AT RBL21 WL208 IAW B737-300 SRM 53-10-51-2 FIG 205. 2L72 4F RTA16WE 20050602001212005060200121EA 2005 6 2 QXEA200500864 120050503A5751 SKIN CNDAIRCL600 CL6002C10 1390015EA RT AILERON CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - RIGHT WING, RIGHT AILERON UPPER LEADING EDGE SKIN HAS CHAFE AREA AT PANEL 698AT AND 698CT. REPAIRED IAW CRJ-700 SRM 51-12-00-001-001-A01, 51-21-11-001-001-A01, 51-25-01-001-001-A01 AND 51-41-02-001-001-A00. 2L72 4F RTA21EA 20050602001242005060200124NM 2005 6 2 EIA2005088 120050404A5313 STRINGER BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 AFTER REMOVAL OF SKIN STRINGER BS380 STR38R, FOUND CRACK AT 1EA FASTENER HOLE APPROX 1/8 INCH RUNNING UP AND 3/16 RUNNING DOWN. STRINGER REPAIRED PER SRM 53-10-03 FIG 1. 2L74 4F A20WE 20050602001272005060200127NM 2005 6 2 EIA2005100 120050405A5313 STRINGER BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 FUSELAGE BS 393 STRINGER 44L ONE EACH FASTENER HOLE FOUND CRACKED RUNNING FOWARD LOWER 1/8 INCH APPROX AND 3/16 INCH AFT. STRINGER PLATE REPAIRED PER SB 747-53-2305. 2L74 4F A20WE 20050602001282005060200128NM 2005 6 2 EIA2005104 120050504A3340 SWITCH BOEING747 747132 1384882NM COCKPIT FAULTY A EIAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 NM09479EV 19898 SMOKE IN COCKPIT DURING DESCENT, MADE EMERGENCY LANDING AT OTBD (DOHA INTL A/P QATAR) AFTER LANDING, FOUND LT INBOARD LANDING LIGHT SWITCH SMOLDERING. OPENED ALL LANDING LIGHT C/B'S. DMI 424, MEL 33-8, INSTALLED PLACARD NR 034516 5/5/2005 AT JFK. REMOVED AND REPLACED LT INBOARD LANDING LIGHT SWITCH IAW MM 33-42-05. OPS CHECK OK. REMOVED PLACARD. 2L74 4F A20WE 20050602001312005060200131NM 2005 6 2 EIA2005107 120050513A5347 CARGO TRACK BOEING747 747212B 1384886NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 M/D BS 1680-1700 LBL 11 TIE DOWN TRACK FLANGE FOUND CORROSION AS MARKED. M/D BS 1680-1730 LBL 11 TIE DOWN TRACK REPAIRED PER SRM 53-10-05, FIG 14. 2L74 4F A20WE 20050602001352005060200135NM 2005 6 2 EIA2005111 120050513A5312 BULKHEAD BOEING747 747212B 1384886NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 FX BS 1480 KEEL BEAM BOX BULKHEAD, FWD FACE BETWEEN RBL2 AND LBL2, FOUND CORROSION. REPAIRED PER HAECO REPAIR SCHEME R-53-49-35300. 2L74 4F A20WE 20050602001412005060200141NM 2005 6 2 EIA2005117 120050513A5315 FLOORBEAM BOEING747 747212B 1384886NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 CORROSION REVEALED ON UPPER DECK FLOORBEAM, UPPER CHORD AT BS 420 RBL 68, PER ATTACH FIG. UPPER DECK BEAM, UPPER CHORD REPAIRED PER SB 747-53A2452. 2L74 4F A20WE 20050602001562005060200156NM 2005 6 2 DHL2005740524 120050325A5230 HINGE BOEING727 7272Q9 138448MNM CARGO DOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH46106 21930 FWD AND AFT SECTIONS OF MCD HINGE CRACKED. REMOVED AND REPLACED FWD AND AFT SECTIONS OF MAIN CARGO DOOR HINGE IAW S/B AEI01-01 REVB 10-26-01 P/N MS 2001-16-7200 PO NR 900733 DIM 6FT FWD AND AFT P/N MS 2001-16-7200 PO NR 90002150 DIM 6FT. 2L73 4F RTA3WE 20050602001582005060200158 2005 6 2 DLM88050268 420050512A3417HG280D80 ADC DOUG MD88 MD88 3023688NM NR 2 FAULTY A DALAA UNSCHED LANDING O OTHER CLCLIMB 1 SO27903DL 49534 A/S INDICATOR ON CO-PILOTS CONTINUED TO GO UP WHILE CAPTS AIRSPEED WENT DOWN. REPLACED CADC NR 2. 2L72 4F RTA6WE 20050602001592005060200159 2005 6 2 DL777050269 420050512A2310235040037 TRANSCEIVER BOEING777 777232 1385232NM E/E BAY FAILED A DALAA UNSCHED LANDING G MULTIPLE FAILURE CRCRUISE 1 SO27861DA 29952 CREW REPORTS LOST ABILITY TO USE RIGHT HF SYSTEM, APPROX 40 MINUTES LATER LOST ABILTIY TO USE THE LEFT HF SYSTEM. A/C DIVERSION. REPLACED BOTH HF TRANSCEIVERS. 2L72 4F RTT00001SE 20050602001622005060200162NM 2005 6 2 DL764050272 120050515A2120 ODOR BOEING767 767432ER 1385134NM COCKPIT DETECTED A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SO27841MH 29714 AT DEPARTURE AND DESCENT HAD RUBBER SMELL IN COCKPIT. UNABLE TO DUPLICATE. 2L72 4F RTA1NM 20050602001632005060200163NM 2005 6 2 DL757050273 120050516A2560 GIRT BAR BOEING757 757232 1384965NM 4L DOOR LOOSE A DALAO OTHER J WARNING INDICATION CLCLIMB 1 SO27660DL 24422 INBOUND REPORT 4L DOOR EICAS MSG. RE-ATTACHED GIRT BAR FEET TO BAR. 2L72 4F RTA2NM 20050602001642005060200164NM 2005 6 2 DLM88050275 120050516A3234 CONTROL HANDLE DOUG MD88 MD88 3023688NM COCKPIT DIRTY A DALAO OTHER N FALSE WARNING LDLANDING 1 SO27979DL 53266 THREE RED GEAR UNSAFE LIGHTS AFTER GEAR EXTENSION. CLEANED LANDING GEAR HANDLE AND SWITCH ASSEMBLY. 2L72 4F RTA6WE 20050602001662005060200166NM 2005 6 2 DL76S050277 120050517A2421 IDG BOEING767 767332 1382001NM GE CF6 CF680 30025NE LT ENGINE MALFUNCTIONED A DALAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 SO27118DL35562 23277 P345 DURING CLIMB-OUT AT 8000 FT, THE LEFT GENERATOR WENT OFF LINE, TRIED TO RESET ONCE BUT DID NOT COME BACK. DIVERT INTO JFK DUE TO SINGLE GENERATOR OPERATION. REPLACED LEFT IDG AND APU EXCITER. 2L72 4F4 FRTA1NM E13NE 20050602001672005060200167NM 2005 6 2 DL75K050278 120050517A2910000AE906D0522 HYDRAULIC LINE BOEING757 757232 1384965NM RT MLG LEAKING A DALAO OTHER K FLUID LOSS LDLANDING 1 SO27650DL 24390 LEFT HYDRAULIC SYSTEM WENT TO ZERO IN FLIGHT. FOUND RIGHT MAIN TRUCK POSITION HYDRAULIC LINE LEAKING. REPLACED LINE. 2L72 4F RTA2NM 20050602001682005060200168NM 2005 6 2 DL75K050279 120050517A256061020 BATTERY BOEING757 757232 1384965NM FLASHLIGHT DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27639DL 23993 F/C EMERGENCY FLASHLIGHT INOP. REPLACED EMERGENCY FLASHLIGHT BATTERY, CKS GOOD. 2L72 4F RTA2NM 20050602001692005060200169NE 2005 6 2 DLM88050280 220050518A7200JT8D219 ENGINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 MALFUNCTIONED A DALAC ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 SO27956DL43237 49887 718026 ADVANCED POWER FOR TAKEOFF, INITIATED T/O ROLL. NO RESPONSE FROM NR 2 ENGINE, DISCONTINUED T/O. RAN BOTH ENGINES PER PFHB. 2L72 4F4 FRTA6WE E9NE 20050602001702005060200170NM 2005 6 2 DLM88050281 120050518A3251 ACTUATOR DOUG MD88 MD88 3023688NM NGL STEERING BYPASSING A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27919DL 49584 AFTER TAKEOFF, NOSE GEAR DID NOT RAISE. LOUD VIBRATION FELT IN NOSE GEAR, BUT IT DID NOT RAISE. NOSE LANDING GEAR INDICATOR ON CENTER CONSOLE REMAINED EXTENDED. FOUND STEERING ACTUATOR BYPASSING FLUID. REPLACED SAME. 2L72 4F RTA6WE 20050602001712005060200171NM 2005 6 2 DL76L050282 120050518A3242 BRAKE BOEING767 767332 1382001NM LT MLG FAILED A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 SO271201P 28458 UPON LANDING, FELT SLT GRABBING OF BRAKES, NR 8 TEMP RISE. TOWER REPORTED SMOKE FROM RT MAIN GEAR. UPON FURTHER INSPECTION FOUND NR 8 BRAKE SHOWS METAL SHAVINGS. REPLACED BRAKE. 2L72 4F RTA1NM 20050602001722005060200172NM 2005 6 2 DHL2005740525 120050329A5313 STRINGER BOEING727 7272Q9 138448MNM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 DURING A "C" CHECK, 2 EACH RIVET HEADS POPPED RT FUSELAGE SKIN STA 1177 STR 22R. REMOVED RIVETS RT FUSELAGE SKIN AT BS 1177 ON STR 22R EVALUATED STRINGER OUT OF LIMITS IAW B727 SRM 51-30-2 AND 53-10-1 FIG 1. CUT OUT STRINGER AND REMOVED SPLICE AND COVER, 3 EACH STRAPS IAW B727 SRM 51-30-2 AND 53-10-3 FIG 1. FABRICATE STRINGER REPAIR FROM BAC 1498-142 IAW B727 SRM 53-10-3 FIG 1 DETAIL 1. TREATED AND PRIMED STRINGER AND SPLICE IAW B727 SRM 51-10-2. INSTALLED STRINGER, SPLICE AND STRAP, REINSTALLED "T" FITTING SUPPORT CLIP IAW B727 SRM 51-10-3 FIG 1 DETAIL 1. REINSTALLED OUTFLOW VALVE IAW B727 MM.21-31-11 REINSTALLED GILL LINER ON RT SIDE IAW B727 MM.25-52-1. OPS CHECK GOOD IAW B727 MM. 21-31-0 2L73 4F RTA3WE 20050602001742005060200174NM 2005 6 2 DHL2005741506 120050419A5753 SKIN BOEING727 7272Q9 138448MNM MID FLAP DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 IMPROPER REPAIR ON RT IB MID FLAP UPPER SURFACE WBL 100. REMOVED PREVIOUS REPAIR R/W I/B MID FLAP T/E WEDGE SURFACE AN CUTOUT DAMAGE AREA APPROX 4 1/4 INCH BY 9 1/4 INCH IAW B727 SRM 51-40-20 FIG 30. FABRICATED ONE SKIN REPLACEMENT APPROX 4 1/4" BY 9 1/4" AND TWO DOUBLERS APPROX 4 1/4" BY 3" EACH USING 2024-T3 .016 PO NR 9001660 IAW B727 SRM 57-50-2 FIG 3. CLEANED, PREPPED, AN APPLIED ADHESIVE PRIMER AN ADHESIVE TO ALL SURFACES AN BAGGED FOR BONDING IAW B727 SRM 51-40-20 FIG 30. CURED REPAIR CLEANED AN PERFORMED POST INSP WITH NO DEFECTS NOTED IAW B727 SRM 51-40-20 PARA O TREATED AN PRIMED AN SEALED REPAIR IAW B727 SRM 51-40-20 PARA O. 2L73 4F RTA3WE 20050602001752005060200175NM 2005 6 2 DHL2005740526 120050401A5330 SKIN BOEING727 7272Q9 138448MNM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 DURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; SKIN REPAIR DOUBLER STA 318-339 AND STR 1-4L AT LOCATION OF VENTURA AEROSPACE 9G BULKHEAD INST OF EXTERNAL SUPPORT PLATE,( STC;ST00848LA). REMOVED EXISTING FUSELAGE SKIN REPAIR DOUBLER/FILLER AT STA 318-339 AND STR 4L PER ASTAR EVA NR 5310-044 REV IR. FABRICATED NEW FILLER FROM 2024-T3 .063 PO 9002149, 39 BY 16 INCHES. TREATED AND PRIMED PER EVA 5310-044 REV IR AND INSTALLED NEW DOUBLER FILLER AND EXTERNAL SUPPORT PLATE P/N 2942 ON FUSELAGE SKIN BETWEEN STR 4L-5L PER ASTAR EVA NR 5310-044 REV IR WITH 8110-3 DATED 04-03-2005. 2L73 4F RTA3WE 20050602001782005060200178NM 2005 6 2 PCSA0519051 120050519A2781H1010262 CONNECTOR BOEING727 727233 138408ANM L/E SLAT LOOSE A PCSAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO29495AJ 20937 FLIGHT 846 DURING CLIMB FROM KIN CREW REPORTED LEADING EDGE AMBER LIGHT CAME ON, CYCLED FLAPS TO 5 DEGREES AND BACK TO 0 DEGREES. LIGHT REMAINED ON, CONFIRMED WITH FLT ENGINEER FLAP SLAT ANNUNCIATOR PANEL. FOLLOWED INOPERATIVE L/E FLAP/SLATS ALTERNATE PROCEDURE. CREW DIVERTED TO SDQ LANDED WITH NO FURTHER INCIDENT. CREW REPORTED AFTER LANDING FLAPS WERE RETRACTED, AMBER LIGHT WENT OUT. MAINTENANCE INSPECTED L/E FLAP/SLAT SYSTEM IN SDQ, FOUND NR 4 L/E SLAT PROXIMITY SWITCH CONNECTOR LOOSE. SECURED TWO LOOSE NUTS, & CLEANED ELECTRICAL CONNECTOR, IAW B-727 MM CH 27-82-11. ACCOMPLISHED 3 RECYCLES FOR L/E FLAP/SLATS IAW B-727 MM CH 27-82-0, OPERATIONAL CHECKED OK. A/C WAS RETURNED TO SERVICE. 2L73 4F RTA3WE 20050602001822005060200182NM 2005 6 2 DHL2005741507 120050414A5720 STIFFENER BOEING727 7272Q9 138448MNM LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 L/WING FRONT SPAR VERTICAL STIFFENER CORRODED BETWEEN TANK 2 FWD AN AFT FUEL PRESSURE SWITCHES WS 260. CORROSION FOUND TO BE OUT OF LIMITS IAW B727 SRM 57-10-1 FIG 1. REMOVED DAMAGED VERT STIFFENER ON L/WING FRONT SPAR AN FABBED NEW FROM BAC 1517-1372 PO NR 509695, DIM 20 IN LENGTH AND FILLER FROM 7075-T6 .160 PO NR 9002012 DIM 16 IN BY 1 IN IAW B727 SRM 57-10-2 FIG 3. NEW PARTS TREATED AN PRIMED AN INSTALLED IAW B727 SRM 51-10-2 AN 51-30-2. LEAK CHECK ACCOMPLISHED ON N/R 98132. 2L73 4F RTA3WE 20050602001832005060200183WP 2005 6 2 DHL2005807534 120050516A572037048412 FITTING DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH86990 45990 NR 2 MAIN TANK FWD FITTING CRACK 1.000, STA XRS 74.000 OUTBD SIDE, S-51 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED AND APPLIED COATING MATERIAL AREA IAW SRM 51-1-12. INSTALLED NEW FITTING (PN 3704841-2) IAW SRM 51-1-20D PG 9, SRM 51-3-0 PG.1, SRM 51-1-23, SRM 51-1-15. TORQUED IAW SRM 51-3-1. REFER TO NR 036403 FOR LEAK CHECK. 2L74 4F RT4A25 20050602001842005060200184WP 2005 6 2 DHL2005807531 120050516A57203704841502 FITTING DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH86990 45990 NR 2 MAIN TANK AFT FITTING CRACK 2.000 STA XRS 74.000 INBD SIDE S-51 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED AND APPLIED COATING MATERIAL IAW SRM 51-1-12. INSTALLED NEW FITTING (PN 3704841-502) IAW SRM 51-1-20D PG. 9, SRM 51-3-0 PG 1, SRM 51-1-23, SRM 51-1-11. TORQUED IAW SRM 51-3-1. REFER TO NR 036403 FOR LEAK CHECK. 2L74 4F RT4A25 20050602001872005060200187WP 2005 6 2 DHL2005807536 120050516A57203704841501 FITTING DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH86990 45990 NR 3 MAIN TANK INTERNAL SKIN AFT FITTING CRACKED 3.000 AT STA 74.000 S-51 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED AND APPLIED COATING MATERIAL AREA IAW SRM 51-1-12. INSTALLED NEW FITTING (PN 3704841-501) IAW SRM 51-1-20D PG 9, SRM 51-3-0 PG 1, SRM 51-1-23, SRM 51-1-11. TORQUED IAW SRM 51-3-1. REFER TO NR 036405 FOR LEAK CHECK. 2L74 4F RT4A25 20050602001882005060200188NM 2005 6 2 DHL2005741508 120050414A5754 SKIN BOEING727 7272Q9 138448MNM L/E SLAT DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 NR 3 SLAT EXTERIOR SKIN DENTED WS 500-519. CUTOUT DAMAGED SKIN (20" BY 19") AN DAMAGED HEAT SHIELD (16" BY 9"). FABRICATED REPAIR PARTS, SKIN 2024-T3, PO NR 9002235(20: X 19") HEAT SHIELD- 2024-T3 .025, PO NR 9001660 (16' BY 9"). SPLICES (2 EA) 2024-T3,.090 (16" BY 3") (1 EA) 2024-T3,.090 (12" BY 3"), (1 EA) 2024-T3,.090 (3' BY 4") PO NR 9002144, FILLERS 2024-T3, PO NR 9001203, .032 (16" BY 1 1/2"), (11' BY 3"0,(6" BY 3"),(4" BY 1 1/2") AN RIB 7075-T6 .032, PO NR 900573,(17" BY 8") IAW B727 SRM 57-50-2, FIG 2 AN 57-50-3 FIG 1. TREATED AN PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED PARTS IAW B727 SRM 57-50-3 FIG 1. 2L73 4F RTA3WE 20050606000022005060600002NM 2005 6 6 DHL2005741509 120050504A5520 SUPPORT FITTING BOEING727 7272Q9 138448MNM LT ELEVATOR WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 LT ELEVATOR HINGE SUPPORT FITTINGS (2 EA) BEARINGS HAVE PLAY. REMOVED AND REPLACED HINGES ON LT HORIZONTAL REAR SPAR 2 EA PN 69-30221-3, PO NR 5096174 AN 2 EA PN 69-30222U5 PO NR 4496610 IAW B727 SRM 27-30-05. LT ELEVATOR REMOVED FOR ACCESS AN REINSTALLED ON N/R 97391. 2L73 4F RTA3WE 20050606000072005060600007WP 2005 6 6 UPS05844483 120050501A53402649943U2 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE: C3, LWR CUSP AT STA 153 RT CUSP TO FRAME FITTING AT TORQUE BOX IS CRACKED BOTH UPPER AND LWR OF CUSP, LENGTH OF FITTING. REMOVED AND REPLACED FRAME FITTING IAW SRM 51-1-21 AND 51-1-20D. 2L74 4F RT4A25 20050606000102005060600010WP 2005 6 6 UPS05844486 120050504A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE: C3, LT WING L/E UPPER SKIN FASTENER HOLES CRACKED .125 INCH LONG AT XFS 450. CUT OUT DAMAGE, FABRICATED AND INSTALLED FILLER AND REPAIR DOUBLER IAW SRM 57-2-1-0 AND 51-3-2. 2L74 4F RT4A25 20050606000152005060600015WP 2005 6 6 UPS05844491 120050504A5712 RIB DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE: C3, LT WING L/E UPPER RIB CRACKED AT XFS 385.250. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLERS 2 EA IAW SRM 57-2-0 FIG 018, 51-1-20D, 51-1-15 AND DWG 5770087. 2L74 4F RT4A25 20050606000172005060600017WP 2005 6 6 UPS05844495 120050519A3510 OXYGEN MASK DOUG DC8 DC873F 302199FWP COCKPIT WILL NOT TEST A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01810UP 46001 F/O'S 02 MASK DOESN'T SEAL DURING TEST. REPLACED 02 MASK AT F/O'S POS. OPS & LEAK CHECK GOOD PER MM 35-10-00. 2L74 4F RT4A25 20050606000182005060600018WP 2005 6 6 UPS05844496 120050504A5713 RIB DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE: C3, LEFT WING L/E UPPER RIB CRACKED AT XFS 391. STOP DRILLED CRACK, FABBED AND INSTALLED 2 EA DOUBLERS IAW SRM 57-2-0 FIG 2, 57-2-0, 51-1-20D, 51-1-8 AND DWG 5770087. 2L74 4F RT4A25 20050606000202005060600020WP 2005 6 6 UPS05844498 120050504A5712 RIB DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE:C3 LEFT WING L/E UPPER RIB CRACKED AT STA XFS 438. STOP DRILLED CRACK, FABRICATED AND INSTALLED 2 EA REPAIR ANGLE DOUBLERS IAW SRM 53-02-00 FIG 001B, 51-1-21. 2L74 4F RT4A25 20050606000212005060600021EA 2005 6 6 QXEA200500939 120050514A7120 MOUNT CNDAIRCL600 CL6002C10 1390015EA ZONE 400 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09602QX 10010 PDX - AFT THRUST MOUNT HAS NUMEROUS GOUGES ON THE BALL END AND BEARING. REPAIRED IAW CRJ-700 SRM 71-22-01-000-801-A01, HORIZON AIR EA R-71-109 AND CRJ-700 AMM TASK 71-22-01-400-801-A01. 2L72 4F RTA21EA 20050606000232005060600023NM 2005 6 6 ABXA050121 120050515A3230161T000044 DRAG BRACE BOEING767 767281 1385109NM RT MLG CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23795AX 23145 RIGHT MAIN LANDING GEAR DRAG BRACE LUG HAD CRACK INDICATION REF: EA 32110006-001. REPLACED RIGHT MAIN LANDING GEAR IAW DC-9 MM. 2L72 4F RTA1NM 20050606000272005060600027EA 2005 6 6 COMA0560307 120050514A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS UNRELIABLE A COMAO OTHER J WARNING INDICATION DEDESCENT 1 SO01917CA5367 4 7017 FLIGHT 5076 - FLAPS FAIL CAUTION. COULD NOT DUPLICATE. REPLACED THE LT BPSU. 2L72 4F RTA21EA 20050606000292005060600029NM 2005 6 6 DHL2005741512 120050421A5330 SKIN BOEING727 7272Q9 138448MNM FUSELAGE CANNING A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 FUSELAGE NOSE BS 185, 7 O’CLOCK POS HAS SKIN OIL-CANNING. CUT OUT DAMAGED AREA 2 BY 2 INCHES. FABRICATED DOUBLER 2024-T3 .050 PO NR 9001873, (11 BY 7.5 INCHES) IAW B727 SRM 53-30-2 FIG 1, AN 53-30-3 FIG 1. TREATED AN PRIMED PARTS AN AREA IAW B727 SRM 51-10-2, INSTALLED DOUBLER REPAIR IAW B727 SRM 53-30-3 FIG 1. 2L73 4F RTA3WE 20050606000302005060600030EA 2005 6 6 COMA0560308 120050515A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS UNRELIABLE A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01917CA7638 4 7017 FLIGHT 5851 - FLAPS FAIL CAUTION. COULD NOT DUPLICATE, REPLACED THE LT BPSU AND WIRING HARNESS. 2L72 4F RTA21EA 20050606000312005060600031EA 2005 6 6 COMA0560309 120050514A215032156222 SHUTOFF VALVE CNDAIRCL600 CL6002B19 1900309EA A/C PACKS MALFUNCTIONED A COMAO OTHER O OTHER CRCRUISE 1 SO01709CA4267 2227 7238 FLIGHT 4987 - LT AND RT AIR CONDITIONING PACKS FAILED. REPLACED THE LEFT AND RIGHT 10TH STAGE PRSOV. 2L72 4F RTA21EA 20050606000322005060600032NM 2005 6 6 DHL2005741513 120050425A5311 FRAME BOEING727 7272Q9 138448MNM FUSELAGE BENT A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 FRAME BENT AT FUSELAGE STA 700 STR 24R. CUT OUT DAMAGED AREA DIM 2.250 IAW B727 SRM 51-10-1 FIG 1. FABBED ANGLE REPAIR FROM 7075-T6 .063 PO NR 900489 DIM 11 X 3 INCHES. FABBED SHIM FROM 7075-T6 .100 PO NR 9911586 DIM 11 X 1 INCHES. FABBED FILLER FROM 7075-T6 .050 PO 9001417 DIM 2.5 X 1 INCHES, IAW B727 SRM 53-10-2 AN 51-40-3 FIG 3. ALODINED AN PRIMED PART REPAIR IAW B727 SRM 51-10-2 AND INSTALLED FRAME REPAIR IAW B727 SRM 51-40-3 FIG 3 AND 51-30-2. 2L73 4F RTA3WE 20050606000332005060600033WP 2005 6 6 DHL2005807537 120050517A27503651809U2 FITTING DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH86990 45990 RT WING T/E RT INBD FLAP WELL FITTING HAS TWO 2.000 CRACKS, STA XRS 59.000 RT WING. REMOVED CRACKED FITTING IAW SRM 51-3-0 PG 1, SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-3-0 PG.1, SRM 51-1-21 PG 1. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050606000342005060600034NM 2005 6 6 DHL2005741514 120050428A5313 STRINGER BOEING727 7272Q9 138448MNM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 STR 28R BS 624 CORRODED. CUT OUT STRINGER INNER RADIUS STRAP (8 X 1 INCHES) CLEANED INNER AREA OF STRINGER, NO CORROSION NOTED ON STRINGER IAW B727 SRM 53-10-3. REPLACED CUT OUT DAMAGED RADIUS STRAP WITH FILLER 7075-T6 .200, (8 X 1 INCHES) PO NR 314676 AN SPLICE STRAP 7075-T6.200, (15.50 X 1 INCHES) PO NR 314676 IAW B727 SRM 53-10-3 FIG 1. TREATED AN PRIMED AREA AN REPAIR PARTS IAW B727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 53-10-3 FIG 1 AN 51-30-2. 2L73 4F RTA3WE 20050606000352005060600035NM 2005 6 6 DHL2005741515 120050425A5313 STRINGER BOEING727 7272Q9 138448MNM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01 21931 STR 28L CORRODED AT FS STA 1013. REMOVED CORROSION FOUND TO BE OUT OF LIMITS ON STR 28L AT FUSE 1013 IAW B727 SRM 51-10-6 AN 53-10-1. CUT OUT DAMAGED AREA SIZE 12 INCHES ON STR 28L AT STA 1013 IAW B727 SRM 53-10-3 FIG 1. FABRICATED STRINGER FROM BAC 1498-132 SIZE 12 INCHES PO NR 424628 AN 2 EA SPLICES FROM BAC 1498-144 SIZE 12 INCHES PO NR 335792 IAW B727 SRM 53-10-3 FIG 1. TREATED AN PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED STRINGER REPAIR IAW B727 SRM 53-10-3 FIG 1. 2L73 4F RTA3WE 20050606000362005060600036NM 2005 6 6 DHL2005741516 120050425A5313 STRINGER BOEING727 7272Q9 138448MNM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01 21931 STR 28L CORRODED AT FS STA 1013. REMOVED CORROSION FOUND TO BE OUT OF LIMITS ON STR 28L AT FUSE 1013 IAW B727 SRM 51-10-6 AN 53-10-1. CUT OUT DAMAGED AREA SIZE 12" ON STR 28L AT STA 1013 IAW B727 SRM 53-10-3 FIG 1. FABRICATED STRINGER FROM BAC 1498-132 SIZE 12" PO 424628 AN 2 EA SPLICES FROM BAC 1498-144 SIZE 12" PO NR 335792 IAW B727 SRM 53-10-3 FIG 1. TREATED AND PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED STRINGER REPAIR IAW B727 SRM 53-10-3 FIG 1. 2L73 4F RTA3WE 20050606000382005060600038NM 2005 6 6 DHL2005741517 120050421A5313 STRINGER BOEING727 7272Q9 138448MNM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 STRINGER AND FRAME CORRODED AT FUSE STA 720,STR 26R. REMOVED FASTENERS AN STRINGER 19.50 INCH AT STA 720 STR 26R IAW B727 SRM 51-30-2 AN 53-10-3 FIG 1. FABRICATED STRINGER REPLACEMENT PN BAC 1498-144, PO NR 335792 SIZE 19.50 INCH AN 2 SPLICES PN BAC 1498-132 SIZE 14 IAW B727 SRM 53-10-3 FIG 1. ALODINED AN PRIMED REPAIR PARTS AN AREAS IAW B727 SRM 51-10-2. REMOVED CORROSION LIGHT CORROSION FRAME AT STA 720 STR 26R IAW B727 51-10-6 MAT. LOSE .002 FOUND TO BE WITHIN LIMITS IAW B727 SRM 53-10-1 FIG 1 AND INSTALLED STRINGER AN 2 SPLICES IAW B727 SRM 53-10-3 FIG 1, 51-30-2. 2L73 4F RTA3WE 20050606000392005060600039NM 2005 6 6 DHL2005741518 120050420A5330 SKIN BOEING727 7272Q9 138448MNM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DENT ON RT FUSELAGE STA 1346 AT STR 13 MARED NR 51. CUT OUT DAMAGE AREA SIZE 2.50 X .250 IAW B 727 SRM 54-30-1 FIG 1. FABRICATED DOUBLER USING 2024T3 .050 PO NR 9002219 DIM 11.50 BY 10 AND FILLER USING 2024T3 .040 PO NR 9001030 DIM 2.50 X .250 IAW B 727 SRM 54-30-2 FIG 4. ALODINED AN PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED DOUBLER IAW B727 SRM 54-30-3 FIG 7. 2L73 4F RTA3WE 20050606000432005060600043NM 2005 6 6 AALA20050339 120050518A3397 WIRE HARNESS BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21940AN 30598 DFW - SEAT MOUNTED EMERGENCY PATH LIGHTS AT ROWS 18 AND 19 INOPERATIVE. REPAIRED DAMAGED WIRES FOR SEAT MOUNTED EMERGENCY PATH LIGHT ON SEAT HARNESS AT SEAT 18DEF AND REPINNED WIRES AND SECURED IN CONNECTOR FOR SEAT MOUNTED EMERGENCY PATH LIGHT AT SEAT 19. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20050606000472005060600047NM 2005 6 6 AWXA200500574 120050429A53206517684629 INTERCOSTAL BOEING737 7373B7 1384580NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28332AW 23384 MCN - MAJOR REPAIR - DURING C-18 CHECK A CRACK WAS FOUND AT S8L BS 294.5 INTERCOSTAL WEB. MAINTENANCE REMOVED, FABRICATED, AND REPLACED INTERCOSTAL WEB AT S8L BS 294.5 IAW AWA ER 03-5300-05135-SS1. 2L72 4F RTA16WE 20050606000482005060600048NM 2005 6 6 AWXA200500575 120050429A534065163312 ANGLE BOEING737 7373B7 1384580NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28332AW 23384 MCN - MAJOR REPAIR - DURING C-18 CHECK A STRINGER ATTACH ANGLE CRACK AT BS 294.5 S13L - FORWARD SIDE OF 294.5 FRAME WAS FOUND. MAINTENANCE REMOVED, FABRICATED, AND REPLACED STRINGER ATTACH ANGLE AT BS 294.5 S13L FWD SIDE OF 294.5 FRAME IAW AWA ER 03-5300-05135-SS1. 2L72 4F RTA16WE 20050606000532005060600053EU 2005 6 6 MALA050428 120050518A1420 BOLT SAAB SF340 SF340A 7850100EU VIBRAT ISOLATOR ELONGATED A MALAK NONE O OTHER ININSP/MAINT 1 GL1599XJ 340A099 RT NACELLE, FWD LOWER VIBRATION ISOLATOR MOUNT BOLTS ARE ELONGATED AND HAVE BEEN REPAIRED IAW MESABA EOS5416. 2L72 4T RTA52EU 20050606000572005060600057EU 2005 6 6 MAC5301 120050312A2910S291805621300 LINE AEROSPATR42 ATR42320 8680930EU HYDRAULIC SYS CRACKED A MTNAD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SO33907FX 286 DURING TAXI, NORMAL BRAKING ACTION WAS LOST. AFTER TROUBLESHOOTING A TUBE TO THE BRAKE METERING VALVE WAS FOUND TO BE BROKEN. THE TUBE WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA53EU 20050606000582005060600058EU 2005 6 6 MAC5302 120050322A2910 HYDRAULIC SYSTEM AEROSPATR42 ATR42320 8680930EU BLUE MALFUNCTIONED A MTNAA UNSCHED LANDING SJ AFFECT SYSTEMS WARNING INDICATION CLCLIMB 1 SO33905FX 271 DURING CLIMB, THE A/C EXPERIENCED LIGHTNING AND A MOMENTARY LOSS OF BLUE SYSTEM HYDRAULICS. AN EMERGENCY WAS DECLARED AND THE A/C LANDED WITHOUT FURTHER INCIDENT. AN INSPECTION IAW ATR JIC 05-51-13OUI 1000 WAS PERFORMED AND AN OPERATIONAL TEST OF THE HYDRAULIC SYSTEM IAW ATR JIC 29-52-53 OPT 1000. NO DEFECTS WERE FOUND. 2H72 4T RTA53EU 20050606000592005060600059WP 2005 6 6 UPS05844515 120050526A56105887276501 WINDOW DOUG DC8 DC873F 302199FWP COCKPIT FAILED A IPXAO OTHER O OTHER NRNOT REPORTED 1 SO01802UP 46100 CREW REPORTED WINDOW WAS ARCING AND TURNED OFF WINDOW HEAT. 30 SECONDS LATER, WINDOW SHATTERED (CAPTAIN'S SIDE WINDOW). REMOVED AND REPLACED LEFT SIDE WINDOW PER MM 56-10-02-2. OPERATIONAL A ND LEAK CHECK NORMAL. 2L74 4F RT4A25 20050606000602005060600060NM 2005 6 6 05FDEA01309 120050516A5330ACA38227 SKIN DOUG MD11 MD11 3023602NM A/C BAY DOOR DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 AIR COND BAY AT STA 496-615 WITH EXISTING BLEND OUT. EXISTING BLENDOUT AT NR 2 AIR COND BAY DOOR STA 496-615 EVALUATED FOUND CARRIED OUT AS PER ATTACHED FAA FORM 8110-3. REPAIR CLASSIFIFED AS MAJOR PER GMM 6-2-100. EO-1-5100-7-5001 ACCOMLISHED. 2L73 4F RTA22WE 20050606000612005060600061NM 2005 6 6 05FDEA01339 120050517A5711ARB74132 SPAR CAP DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25580FE 48471 RT WING REAR SPAR UPPER CAP FOUND CORROSION AT XORS 470. REPAIRED AS PER FEDEX EA NR 1-5710-83099 THIS REPAIR CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050606000622005060600062NM 2005 6 6 05FDEA01340 120050517A5711ARB74132 SPAR CAP DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25580FE 48471 RT WING REAR SPAR UPPER CAP FOUND CORROSION AT XORS 450. REPAIRED AS PER FEDEX EA NR 1-5710-86608. THIS REPAIR CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050606000632005060600063NM 2005 6 6 05FDEA01342 120050517A5730ARB71882 ACCESS PANEL DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25580FE 48471 RT WING LEADING EDGE ACCESS PANEL 626FB INSIDE LOWER SURFACE FOUND CORROSION. REMOVED AND REPAIRED AS PER FEDEX EA NR 1-5710-86606. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050606000652005060600065NE 2005 6 6 USAABB05041 220050525A7320ETPU10003C SENSOR BOEING757 7572B7 1384964NM RROYCERB211 RB211535E4 54555NE RT ENGINE FAULTY A USAAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION DEDESCENT 1 EA19611AU3104631046 31297 27123 31297 DURING DESCENT, THE RT ENGINE FLAMED OUT WHEN POWER WAS APPLIED (12.00 FEET AT LEVEL OFF). THE CREW RESTARTED THAT ENGINE, AND LANDED WITH BOTH ENGINES POWERED. MAINTENANCE REPLACED THE TRANSIENT PRESSURE SENSOR. 2L72 4F4 FRTA2NM E12EU 20050606000672005060600067NM 2005 6 6 05FDEA01275 120050514A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 DENT IN SKIN, BS 1348, STR 23L. REMOVED DAMAGED SKIN & REPLACED DAMAGE SKIN BS 1342-1352 WL 190.3 - 259.5. ALL WORK DONE IAW SRM 51-10-1, 51-30-2, 51-30-5, 51-30-8, 51-10-2 & M/M 51-20-013-7 2L73 4F RTA3WE 20050606000692005060600069NM 2005 6 6 05FDEA01291 120050515A5730ARB74063 SKIN DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25580FE 48471 LT WING UPPER SURFACE FOUND CORROSION AT XORS 77 STRINGER 21. CORRODED AREA REPAIRED AS PER FEDEX EA NR 1-5710-86605. THIS REPAIR CLASSIFIED AS MINOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050606000702005060600070NM 2005 6 6 05FDEA01292 120050515A5340AGA74381 FITTING DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25580FE 48471 AFT CARGO COMPARTMENT FOUND BILGE LOCATION LONGERON-48R STA 1851 SPLICE FITTING WITH CORROSION. NEW SPLICE END FITTING MACHINED AS PER DRAWING NR AGA7438. AFT CARGO COMPARTMENT STA 1851, LONGERON-48R SPLICE END FITTING REMOVED AND NEW SPLICE END FITTING INSTALLED AS PER SRM 51-31-01 VOLUME II. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050606000712005060600071NM 2005 6 6 05FDEA01295 120050515A5512 PANEL DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25621FE 48792 HORIZONTAL STABILIZER RT FORWARD PLANK NR 14R BARREL NUT BORE CORROSION REMOVAL FOUND EXCEEDED LIMITATIONS. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. 2L73 4F RTA22WE 20050606000762005060600076NM 2005 6 6 05FDEA01362 120050518A5514C8106Y2 FITTING DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 RT HORIZONTAL STABILIZER UPPER BARREL NUT NR 14 HAS BORE CORROSION EXCEEDING LIMITS. SPLICE FITTING REMOVED AND REPLACED IAW EO-1-5510-7-5000 REV D -PT1. MAJOR REPAIR PER GMM 6-2-100. 2L73 4F RTA22WE 20050606000792005060600079 2005 6 6 USAASA05056 420050527A2565 CONDUIT AIRBUSA319 A319112 3930323EU PAX DOOR SLIDE MISROUTED A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19729US6924 4682 1170 DURING A MAINTENANCE VISIT, FOUND THE EMERGENCY LIGHT CONDUIT FOR THE EMERGENCY ESCAPE SLIDE MISROUTED. MAINTENANCE REPLACED THE SLIDE ASSEMBLY. OK FOR SERVICE. 2L72 4F RTA28NM 20050606000802005060600080NM 2005 6 6 05FDEA01293 120050515A5340AFA71021 FITTING DOUG MD11 MD11F 3023600NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25580FE 48471 CENTER CARGO COMPARTMENT FOUND SUMP LOCATION WITH SPLICE CRACKED AT STA 1710, L-51L. CARRIED OUT REMOVAL AS PER SRM 51-33-01 VOL II AND NEW SPLICE FITTING FABRICATED BY MACHINING AS PER DRAWING NR AFA7102 AND INSTALLED AS SRM 51-33-01 VOL II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050606000812005060600081NM 2005 6 6 05FDEA01305 120050516A5313ADA7020509 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25580FE 48471 FUSELAGE-CORROSION OBSERVED IN CENTER ACCESSORY COMPARTMENT ON LONGERON 47R STATION 6-90. REPAIRED AS PER SRM 53-10-00 FIGURE 2 VOLUME I. 2L73 4F RTA22WE 20050606000852005060600085NM 2005 6 6 AALA20050352 120050523A3350BPS73 BATTERY PACK BOEING767 767323 1385205NM EMERGENCY LIGHTSINOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21379AA 25448 CDG ALL EMERGENCY LIGHTS AT RT AFT CABIN INOPERATIVE. FOUND FUSE ON POWER SUPPLY BLOWN AND CONNECTORS ON RIGHT HAND SEATS 35HJ AND 39HJ DAMAGED. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS WITH FUSE ON POWER SUPPLY BLOWN. SYSTEM GROUND CHECKED NORMAL OPERATION. PLACARDED EMERGENCY LIGHTS ON SEAT 35HJ AND 39HJ INOP PER MEL 33 16A. CONNECTORS NOT IN STOCK IN CDG. REPAIRED SHORTED CONNECTOR AT 39H EMERGENCY PATH LIGHT AND CLEARED MEL AT LAX. SYSTEM GROUND CHECKED NORMAL OPERATION. (SUPP CLOSED) 2L72 4F RTA1NM 20050606000952005060600095CE 2005 6 6 DXTA200500737 120050522A323015231007 RETRACT CYLINDER CESSNA500 560CESSNA 2076750CE MLG DAMAGED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07318QS7623 5600418 LEFT MAIN WOULD NOT RETRACT. - PERFORMED GEAR SWINGS AND TROUBLESHOOTING IAW CE560 MM CHAPTER 32-30-00 WITH NO DISCREPANCIES NOTED. SUSPECTED MLG RETRACT ACTUATOR, REMOVED LEFT MAIN GEAR ACTUATOR AND INSTALLED AN INSPECTED ACTUATOR IAW CE 560 MM 32-31-04. PERFORMED SATISFACTORY GEAR SWINGS AND LEAK CHECKS. 2L72 4F RTA22CE 20050606000962005060600096CE 2005 6 6 DXTA200500728 120050518A2720 CONTROL CABLE CESSNA750 750 2076810CE RUDDER OUT OF ADJUST E DXTAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 GL07913QS 7500113 AIRCRAFT ROLLS RIGHT DURING CRUISE. AILERON TRIM IS ROLLED OVER HALFWAY TO HOLD LEVEL FLIGHT. RUDDER TRIM IS ALSO TO LEFT OF CENTER. CONTROL RIGGING NEEDS TO BE CHECKED. - TROUBLESHOT BOTH AILERON AND RUDDER SYS. FOUND AILERONS TO BE RIGGED CORRECTLY. RUDDERS MADE TRAVELS BUT NEUTRAL WAS NOT IN SPECS. ACCESSED BOTH RUDDER COMPONENTS AND RIGHT TO NEUTRAL. BOTH RUDDER COMPONENTS AND RESET TO NEUTRAL. BOTH RUDDERS NOW TRAVEL AND OP CHECKS GOOD IAW 750 MM CH 27-20-00. 2L72 4J RTT00007WI 20050606000972005060600097NE 2005 6 6 DXTA200500740 220050522A7297 WIRE HARNESS CESSNA560 560XL 2076702CE PWA 545 PW545A NE LT ENGINE FAULTY E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07617QS482 5605509 DURING TAKEOFF ROLL LEFT ENGINE PRODUCED 80% N1. SCHEDULED TAKEOFF POWER WAS 90.1% - REMOVED AND REPLACED ENGINE WIRING HARNESS PER P&WC M/M CH 76-20-02 OPERATIONAL CHECKS SATISFACTORY. BOTH AUTO AND MANUAL MODES. 2L72 4F4 FRTA22CE E00059EN 20050606000982005060600098NM 2005 6 6 DXTA200500746 120050530A2597 CONNECTOR GULSTM200 200 4500308NM VIDEO MONITOR SHORTED E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07720QS1029 085 VIP SEAT VIDEO MONITOR PORT SHORTED OUT. SMOKE AND ACID SMELL WAS OBSERVED COMING FROM THE MONITOR PORT. - VERIFIED DISCREPANCY, FOUND VIP VIDEO MONITOR CONNECTOR TO BE BAD. DISABLED AND STOWED VIP VIDEO MONITOR CONNECTOR CANNON PLUG. ALL OTHER VIDEO MONITOR OPS CHECK GOOD. NO SMOKE OR ACID SMELL OBSERVED. OP CHECK GOOD IAW G200 COMPLETION MANUAL 23-50-00. 2L72 4F RTA53NM 20050606001002005060600100NM 2005 6 6 BB05039 120050517A33508100022601 LIGHT BOEING767 767201 1385125NM ROW 6R INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19649US 23901 PHL - FOUND FLOOR MOUNTED EMERGENCY LIGHT AT ROW 6R INOPERATIVE. MAINTENANCE REPLACED THE SOCKET. 2L72 4F RTA1NM 20050606001012005060600101NM 2005 6 6 05FDEA00656 120050328A5512ALC8100XXX PANEL DOUG MD11 MD11 3023602NM HORIZONTAL STABICORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 RIGHT HORIZONTAL STABILIZER UPPER BARREL NUT NR 36 HAS BORE CORROSION EXCEEDING LIMITS. BARREL NUT BORE NR 36 RIGHT REPAIRED IAW EA 1-5510-78133 ATTACHMENT 18, HORIZONTAL STABILIZER BARREL NUT BORE REWORK/ REPAIR AD 2003-22-08. MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050607000012005060700001EA 2005 6 7 QXEA200500880 120050502A5751 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 500 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - LT WING AILERON BOTTOM FORWARD SKIN HAS CHAFE MARKS. REPAIRED IAW CRJ-700 SRM 51-12-00-001-001-A01, 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050607000032005060700003EA 2005 6 7 QXEA200500870 120050506A5530 TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 300 LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - HORIZONTAL STABILIZER STEADY BLOCK FOR STAB TRIM TRACK IS LOOSE. REPAIRED IAW REO 670-55-11-024, HORIZON AIR EA R-55-34 AND CRJ-700 MM TASK 27-40-00-710-801-A01. 2L72 4F RTA21EA 20050607000112005060700011EA 2005 6 7 QXEA200500884 120050503A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FORWARD FUSELAGE LOWER SKIN PANEL ROCK CHIP DAMAGE STATION 333.00 TO 349.00 BETWEEN STRINGER 25R AND 25L. REPAIRED IAW CRJ-700 SRM 51-26-00-001-001-A01, 51-12-00-001-001-A01 AND SRM 51-25-16-001-001-A01. 2L72 4F RTA21EA 20050607000122005060700012EA 2005 6 7 QXEA200500872 120050503A5210 BRACKET CNDAIRCL600 CL6002C10 1390015EA ZONE 800 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - PASSENGER DOOR AFT HANDRAIL STOWAGE BRACKET HAS BENT AND CRACKED HOLE. REPAIRED IAW CRJ-700 SRM 51-42-21-001-001-A01. 2L72 4F RTA21EA 20050607000152005060700015EA 2005 6 7 QXEA200500869 120050509A5310 STRUCTURE CNDAIRCL600 CL6002C10 1390015EA ZONE 200 WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FUSELAGE INTERIOR, LEFT OVERWING EMERGENCY EXIT SURROUND STRUCTURE STOP FITTING PADS ARE WORN. REPAIRED IAW REO 670-52-21-003, HORIZON AIR EA R-52-251 AND CRJ-700 AMM TASK 52-21-00-220-801-A01. 2L72 4F RTA21EA 20050607000162005060700016EA 2005 6 7 QXEA200500871 120050509A5230 RETAINER CNDAIRCL600 CL6002C10 1390015EA ZONE 800 CRUSHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - AFT BAGGAGE BAY DOOR BOTTOM SEAL RETAINER HAS CRUSHED AREA AT BOTTOM AFT PRESSURE STOP AND LIGHT DENT AT AFT CORNER. REPAIRED IAW CRJ-700 SRM 51-42-06-001-001-A01 AND MM TASK 52-00-00-780-801. 2L72 4F RTA21EA 20050601000832005060100083EU 2005 6 1 MALA050398 120050503A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15449XJ 340B449 DURING 4K INSPECTION IN BNA, FOUND SEAT TRACK AT BL 0 FROM FS297 TO FS319 IS CORRODED. DAMAGE HAS BEEN REPAIRED AS REQUIRED IAS SRM 53-70-60. REF EAMS WORK ORDER 212113 TASK 1507. 2L72 4T RTA52EU 20050601000892005060100089EU 2005 6 1 MALA050407 120050507A5510 STRUCTURE BAC 146 AVRO146RJ85A1500097EU HORIZ STAB LIGHTNING STRIKEA MALAK NONE O OTHER UKUNKNOWN 1 GL15524XJ E2349 REPAIR LIGHTNING STRIKE DAMAGE ON RT HORIZ STAB IAW EOA55023. 2H74 4F RTA49EU 20050601000902005060100090EU 2005 6 1 MALA050408 120050507A2612703045 FIRE LOOP SAAB SF340 340B 7860101EU RT ENGINE FAULTY A MALAO OTHER N FALSE WARNING UKUNKNOWN 1 GL15452XJ 340B452 RT ENGINE FIRE INDICATION ILLUMINATED WHEN PULLED IN TO PARK. THE CAPT PULLED THE FIRE HANDLE AND SHUT DOWN THE ENGINE. FIRE INDICATION EXTINGUISHED. THE CREW DIDN'T BLOW THE BOTTLES. REMOVED AND REPLACED RT FIRE LOOP, PN 703045. ALL CHECKS GOOD. 2L72 4T RTA52EU 20050601000942005060100094WP 2005 6 1 GTIA050122 120050403A7830 FAIRING DOUG DC9 DC981 3022081WP THRUST REVERSER MISSING A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 NR 1 T/R FILLER FAIRING MISSING, AIRCRAFT TAIL SWAP WITH 830. DTW, SHEET METAL REPAIRED FILLET PANEL AND INSTALLED. (M) 2L72 4F A6WE 20050601001002005060100100WP 2005 6 1 GTIA050116 120050310A5312 ANGLE DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FTW - MID PIT FORWARD BULKHEAD STATION 522 LEFT LOWER CORNER HAS CRACKED ANGLE. REMOVED CRACKED ANGLE STATION 522. FABRICATED NEW ANGLE IAW SRM 51-10-2. TREATED AND PRIMED, INSTALLED ANGLE AT STATION 522 IAW SRM 51-30-2. (M) 2L72 4F A6WE 20050601001072005060100107NM 2005 6 1 SWAA051405 120050513A53156545410 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND CABIN FLOORBEAM UPPER CHORD CRACKED AT BS 639, LBL 59, WL 206. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20050601001122005060100112NM 2005 6 1 SWAA051410 120050515A53306545766 SKIN BOEING737 7373H4 1384600NM FUSELAGE ACTIVATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29352SW 24888 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN OIL CANNED AT BS 460 + 10, STR 14L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050601001142005060100114NM 2005 6 1 SWAA051413 120050513A33976042221 WIRE BOEING737 7377H4 1384404NM CABIN DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29475WN 32474 FWD FLOOR EMERGENCY EXIT LIGHT BROKEN. REPAIRED WIRING, REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20050601001152005060100115NM 2005 6 1 SWAA051414 120050514A53306545775 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29502SW 24179 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 790, STR 17L. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050601001192005060100119NM 2005 6 1 SWAA051418 120050514A3350101114 LIGHT BOEING737 7373TO 138447GNM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29697SW 23838 DURING SCHEDULED SERVICE CHECK, FOUND FWD LT EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050601001282005060100128NM 2005 6 1 SWAA051391 120050512A53306545775 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 794, STR 19L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050601001412005060100141NM 2005 6 1 SWAA051401 120050513A53116546532 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND 2 EA FUSELAGE FRAME CRACKS AT BS 480, STR 8L TO STR 9L & STR 8R TO STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050601001472005060100147NM 2005 6 1 SWAA051423 120050516A53206546833 WEB BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FLOOR WEB CRACKED AT BS 188 TO BS 196, RBL 30, WL 208. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050601001512005060100151NM 2005 6 1 SWAA051428 120050516A534065C27314 STRINGER CLIP BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050601001632005060100163WP 2005 6 1 GTIA050106 120050310A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FOUND DENT ON FUSELAGE SKIN FS 421 BETWEEN LONGERONS 19R AND 20R, D=.5, X=.008, D/X=62.5. REMOVED FORWARD CARGO DOOR TO FOM. REMOVED DAMAGED AREA OF SKIN 1.5 INCH BY .8 INCH. FABRICATED DOUBLER AND FILLER IAW 53-04. TREATED AND PRIMED, INSTALLED REPAIR DOUBLERS AND FILLERS IAW SRM 53-05. INSTALLED FORWARD CARGO DOOR PER MM 52-31-00. DOOR WARNING CHECK GOOD IAW MM 53-70-00. (M) 2L72 4F A6WE 20050609000012005060900001NM 2005 6 9 05FDEA01273 120050514A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 DAMAGED AIRCRAFT ON RIGHT SIDE WHILE REMOVING BALLAST BARREL'S AT B.S. 420-426 STR 18. REPAIRED SKIN PER FED EX EA 7-5330-86306. 2L73 4F RTA3WE 20050607000142005060700014EA 2005 6 7 QXEA200500865 120050502A5751 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 500 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - LEFT WING, LEFT AILERON LOWER LEADING EDGE HAS CHAFED AREA ON OUTBOARD END. REPAIRED IAW CRJ-700 SRM 51-12-00-001-001-A01 AND SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050601001812005060100181NM 2005 6 1 05FDEA01302 120050516A5311 FRAME DOUG MD11 MD11 3023602NM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25580FE 48471 MAIN DECK CABIN LEFT STATION 1661 LONGERON 12L FRAME FOUND DENTED AS MARKED. REPAIRED IAW SRM 53-30-00 FIGURE I VOLUME I. 2L73 4F RTA22WE 20050601001822005060100182NM 2005 6 1 05FDEA01303 120050516A5311 FRAME DOUG MD11 MD11 3023602NM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25580FE 48471 MAIN DECK CABIN LEFT STATION 1641 LONGERON 12L FRAME FOUND DENTED AS MARKED. REPAIRED IAW SRM 53-30-00 FIGURE I VOLUME I. 2L73 4F RTA22WE 20050601001862005060100186EU 2005 6 1 05FDEA01311 120050516A5330 SKIN AIRBUS300 A300F4605R 3930327EU FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25679FE 793 A/C FUSELAGE RT SIDE FR 57.1STR 43 APPROX HAS GOUGES REF N00066. BLENDED AREA IAW SRM 51-73-10, AREAS OUT OF LIMITS PER SRM 53-10-00. REMOVED DAMAGED SKIN SECTIONS AND REPAIRED PER A300-600 SRM 53-10-12. 2L72 4F RTA35EU 20050601001872005060100187EU 2005 6 1 05FDEA01312 120050516A5730 PANEL AIRBUS310 A310 EU LT WING WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25403FE 230 OFF A/C PART LEFT WING PNL 512AT HAS WEAR MARKS ON BOTTOM SIDE OF PNL. COMPLIED WITH EA6-5740-89200. 2L72 4F RTA35EU 20050601001912005060100191NM 2005 6 1 SWAA051442 120050517A3350101073 LENS BOEING737 7373H4 1384600NM EXTERIOR DEFECTIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29352SW 24888 DURING SCHEDULED 1/2D CHECK, FOUND EXTERNAL EMERGENCY EXIT LIGHT LENS CLOUDY AFT OF LT EMERGENCY EXIT CUTOUT. REMOVED AND REPLACED LENS PER MM. 2L72 4F RTA16WE 20050601001962005060100196NM 2005 6 1 SWAA051435 120050517A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727D, STR 6L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050601001972005060100197NM 2005 6 1 SWAA051436 120050517A53226545948 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 967, STR 6L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050601001992005060100199EA 2005 6 1 A6WA200540160 120050418A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA RT WING CHAFED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31417AW 7610 RIGHT LOWER WING PLANK UNDER PANEL 650HB IS CHAFED IN TWO AREAS. INBOARD AREA CHAFED .050 INCH WIDE 6 INCHES LONG APPROX .002 INCH DEEP. OUTBOARD AREA CHAFED .050 INCH WIDE 4 INCHES LONG APPROX .001 INCH DEEP. FORWARD CENTER IS AT STARTING STAGES OF CORROSION .5 INCH LONG .1 INCH WIDE. REPAIRED BY BLENDING OUT DAMAGE, PERFORMING NDT, ROTO-PEENED RE-WORKED AREA IAW BOMBARDIER INC REO 601R-57-21-030 REVD. (M) 2L72 4F RTA21EA 20050602000012005060200001WP 2005 6 2 ABXA050117 120050504A53474925848M36000 SEAT TRACK DOUG DC9 DC931 3022065WP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23946AX 47003 HEAVILY CORRODED CENTER SEAT TRACK STA 214. CENTER SEAT TRACK REMOVED AND REPLACED ON JC 0281 IAW DC-9 SRM. 2L72 4F A6WE 20050602000292005060200029NE 2005 6 2 QXEA200500847 220050513A72003038400 ENGINE DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE NR 1 LEAKING A QXEAK NONE B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM09362PH152614682 518 PCEAG0090 SEA FLIGHT NR 2267 - DURING TAXI OUT, A BLUISH TINT SMOKE FILLED FLIGHT DECK AND CABIN AFTER APPROXIMATELY 20 MINUTES OF TAXI TIME. MAINTENANCE FOUND SMOKE CAME FROM NR 1 BLEED SYSTEM. REPLACED NR 1 ENGINE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20050602000302005060200030NM 2005 6 2 QXEA200500848 120050516A2612 FIRE WARNING DHAV DHC8 DHC8202 2809007NM COCKPIT ACTIVATED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09359PH 514 SEA FLIGHT NR 2017 - NR 1 ENGINE CHECK FIRE DET MASTER WARNING, ACCOMPLISHED CHECKLIST NR 1 ENGINE LOOP (FAULT B) COMPLETED FLIGHT WITH LOOP A SELECTED, NO OTHER INDICATIONS NOTED. MAINTENANCE DEFERRED AND AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050602000462005060200046NM 2005 6 2 05FDEA01274 120050514A5315 FLOORBEAM BOEING727 727227 1384078NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 CORROSION AT FLOORBEAM FASTENER HOLES BS 720 RBL 50 LBL 50, WL 200. REPAIRED FLOORBEAM PER SRM 53-10-8. 2L73 4F A3WE 20050602000542005060200054NM 2005 6 2 05FDEA01371 120050518A5330 SKIN PANEL BOEING727 727233 138408ANM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25254FE 20936 COMPLY WITH EA 7-5330-55484 FUSELAGE, PLATES AND SKIN GOUGE REPAIR AT BS 950E, STR 19R. COMPLIED WITH EA 7-5330-55484 FUSELAGE, PLATES AND SKIN GOUGE REPAIR AT BS 950E, STR 19R. THIS IS A MAJOR REPAIR. 2L73 4F RTA3WE 20050602000642005060200064SO 2005 6 2 XGN2005F00005 220050504A8530TISN711ACA CYLINDER CONT IO520C BEECH 58 58 1152740CE CONT O520 IO520C 17032SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW05577W 400 561711 TH375 561711 CYLINDERS WERE FOUND DURING COMPRESSION CHECK AT THE 100 HOUR INSPECTION. WE ARE USING A SOAP SOLUTION TO DETECT CRACKS IN THE EXHAUST SIDE OF THE CYLINDER WHILE DOING A COMPRESSION CHECK. WE ARE DOING COMPRESSION CHECKS EACH 50 HOURS. 3 CRACKED CYLINDERS WERE FOUND ON THE SAME ENGINE AT THIS INSPECTION. (K) 1L72 3O3 O 3A16 E5CE 20050602000692005060200069EA 2005 6 2 A6WA200540165 120050503A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA RT WING FRETTED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31451AW 7832 RIGHT LOWER WING PLANK HAS FRETTING DAMAGE AT FUEL TANK ACCESS DOOR CUT OUTS AT WS 116.366 AND WS 136-676. MEASURES .001 TO .002 WIDTH DEEP AROUND ENTIRE CUT OUT. REPAIRED FRETTING DAMAGE BY BLENDING IAW BOMBARDIER INC REO 601R-57-21-030 REV C. (M) 2L72 4F RTA21EA 20050602000772005060200077SW 2005 6 2 KBM2005F00050 120050504A772212444412 INDICATOR BELL 206 206B 1181511SW COCKPIT STICKING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19188TV 2704 UNIT STICKING. (M) 1G71 3U H2SW 20050602000812005060200081WP 2005 6 2 0500769968 120050414A5320 CUSP WEB DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019332 47264 DURING "M" CHECK, FOUND CRACK IN RT CUSP WEB AT BS 834. REPAIRED PER EA 99-203527. 2L72 4F A6WE 20050602000842005060200084SO 2005 6 2 C2XA05BT029 120050509A335074449 SIGN EMB 145 EMB145ER 3260211SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714943 145040 EWR - CO2338, DURING SERVICE AND ROUTINE CHECK MAINTENANCE FOUND THE LEFT EMERGENCY EXIT SIGN WINDOW EXIT DOES NOT ILLUMINATE. REMOVED AND REPLACED LEFT EMERGENCY EXIT SIGN WINDOW EXIT IAW EMB AMM NR 33-50-13, OPS CHECKED GOOD. 2L72 4F RTT00011AT 20050602000882005060200088SO 2005 6 2 C2XA05SD020 120050513A3350 LIGHT EMB 145 EMB145XR 3260214SO CABIN MALFUNCTIONED A C2XAK NONE O OTHER UKUNKNOWN 1 SW2714153 145761 FLT NR 2124 - LEFT EMERGENCY EXIT DOOR LIGHT INOP. PERFORMED OPS CHECK OF EMERGENCY LIGHTS AND LEFT EXIT DOOR LIGHT OPS CHECK GOOD. NO DISCREPANCY FOUND. AIRCRAFT RELEASED AND RETURNED TO SERVICE. 2L72 4F RT 20050602000902005060200090SO 2005 6 2 C2XA05CL037 120050517A3350AD20131A BATTERY EMB 145 EMB145XR 3260214SO CABIN DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2741104 145646 DURING ROUTINE MAINTENANCE, THE EMERGENCY EXIT LIGHT ABOVE THE FORWARD FLIGHT ATTENDANT SEAT WAS INTERMITTENT. MAINTENANCE REPLACED THE NR 1 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RT 20050602001052005060200105NM 2005 6 2 AWXA200500579 120050428A575465C26601180 WEDGE BOEING737 7373B7 1384580NM L/E SLAT DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28332AW 23384 MCN - FLIGHT CONTROL - DURING C-18 CHECK, DELAMINATION WAS FOUND AT THE NR 6 SLAT WEDGE. DELAMINATION WAS FOUND ON TOP AND BOTTOM SURFACES. MAINTENANCE FOUND THAT THE DELAMINATION WAS BEYOND REPAIRABLE LIMITS. MAINTENANCE REMOVED AND REPLACED THE NR 6 SLAT ASSEMBLY IAW B737-300 AMM 27-81-21-4. 2L72 4F RTA16WE 20050602001062005060200106NM 2005 6 2 AWXA200500580 120050518A2120 ODOR BOEING737 7373S3 1384711NM COCKPIT DETECTED A AWXAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP28312AW 24060 BUR - BURNING SMELL - IMMEDIATELY AFTER TAKEOFF PILOTS REPORTED NOTICEABLE SMELL OR ODOR OF SMOKE. SMELL APPEARED TO DISSIPATE RAPIDLY THEREAFTER. NOTHING REPORTED EN ROUTE. MAINTENANCE REMOVED AND REPLACED THE RECIRCULATION FILTER IAW AWA TASKCARD S2B21003. MAINTENANCE RAN BOTH ENGINES AT HIGH POWER SETTINGS WITH BLEEDS ON, BLEEDS OFF, PACKS ON PACKS OFF, APU BLEEDS AND PACKS. COULD NOT DUPLICATE SUSPECTED ODOR/SMELL AIRCRAFT RELEASED TO SERVICE. 2L72 4F RTA16WE 20050602001082005060200108NM 2005 6 2 AWXA200500582 120050428A575465C26602218 WEDGE BOEING737 7373B7 1384580NM L/E SLAT DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28332AW 23384 MCN- FLIGHT CONTROL - DURING C-18 CHECK, DELAMINATION WAS FOUND AT THE NR 5 SLAT WEDGE. DELAMINATION WAS FOUND ON TOP AND BOTTOM SURFACES. MAINTENANCE FOUND THAT THE DELAMINATION WAS BEYOND REPAIRABLE LIMITS. MAINTENANCE REMOVED AND REPLACED THE NR 5 SLAT ASSEMBLY IAW B737-300 AMM 27-81-21-4. 2L72 4F RTA16WE 20050602001122005060200112EA 2005 6 2 QXEA200500860 120050502A5753 VANE CNDAIRCL600 CL6002C10 1390015EA T/E FLAP CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - LEFT INBOARD FLAP VANE INBOARD LEADING EDGE ACCESS PANEL 584ET HAS CHAFE MARK. REPAIRED IAW CRJ-700 SRM 51-12-00-001-001-A01, 57-52-02-001-A01, 51-25-16-001-001-A01 AND SRM 51-21-11-001-001-A01. 2L72 4F RTA21EA 20050602001142005060200114EA 2005 6 2 QXEA200500855 120050502A5753 SKIN CNDAIRCL600 CL6002C10 1390015EA T/E FLAP DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - LEFT WING OUTBAORD FLAP UPPER SURFACE HAS RUBBED MARK AT MID SECTION. REPAIRED IAW CRJ-700 SRM 51-12-00-001-001-A01 AND 51-25-00-001-001-A01. 2L72 4F RTA21EA 20050602001162005060200116EA 2005 6 2 QXEA200500857 120050502A5414 SKIN CNDAIRCL600 CL6002C10 1390015EA RT NACELLE GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - RIGHT NACELLE LIPSKIN HAS GOUGES BETWEEN 3 AND 6 O'CLOCK POSITION. REPAIRED IAW CRJ-700 SRM 54-11-01-201-001-A01 AND SRM 51-21-11-001-001-A01. 2L72 4F RTA21EA 20050602001182005060200118EA 2005 6 2 QXEA200500859 120050505A5753 SKIN CNDAIRCL600 CL6002C10 1390015EA T/E FLAP DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - LEFT WING INBOARD FLAP LOWER SKIN HAS GRAVEL DAMAGE. REPAIRED IAW CRJ-700 SRM 51-26-00-001-001-A01, 57-52-01-101-001-A01 AND SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050602001202005060200120EA 2005 6 2 QXEA200500863 120050502A5220 STOP FITTING CNDAIRCL600 CL6002C10 1390015EA EMERGENCY EXIT NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FUSELAGE RIGHT OVERWING EMERGENCY EXIT DOOR HAS NICKS ON STOP FITTING, SECOND AND THIRD FROM TOP AFT. REPAIRED IAW HORIZON AIR EA R-52-24*-, REO 670-52-21-002, CRJ-700 SRM 51-25-16-001-001-A01 AND CRJ-700 AMM TASK 20-51-00-400-802-A01. 2L72 4F RTA21EA 20050602001232005060200123EA 2005 6 2 QXEA200500853 120050502A5753 FITTING CNDAIRCL600 CL6002C10 1390015EA T/E FLAP DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - LEFT OUTBOARD FLAP INBOARD GUIDE ROLLER FITTING DAMAGE AT TRAILING EDGE WING STATION 138.98. REPAIRED IAW CRJ-700 SRM 57-51-02-201-001-A01, 51-42-06-001-001-A01 AND 51-41-21-001-001-A01. 2L72 4F RTA21EA 20050602001262005060200126NM 2005 6 2 EIA2005006 120050405A5320 SPLICE BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 BS 400 NLG W/W AFT CORNER FOUND CRACKED AT SPLICE PLATE. SPLICE PLATE REPAIRED PER SB 747-53-2305. 2L74 4F A20WE 20050602001372005060200137NM 2005 6 2 EIA2005113 120050513A5322 SHEAR TIE BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 M/D BS 1860 STRINGER 4R TO 5R SHEAR TIE FOUND CRACKED. CRACKED SHEAR TIE REPLACED PER SRM 51-10-01. 2L74 4F A20WE 20050602001492005060200149NM 2005 6 2 EIA2005126 120050517A5730 SKIN BOEING747 747132 1384882NM LT WING CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 CORROSION ON LOWER SKIN IN SPAR CAVITY IN LEFT END OF LT WING AT WS 1275. CUT OUT DAMAGED SKIN, FABRICATED AND INSTALLED REPAIR IAW B747 SRM 57-30-03, FIG 9 AND BOEING MESSAGE 1-1JWDXE. 2L74 4F A20WE 20050602001552005060200155NM 2005 6 2 DHL2005740523 120050324A5320 TORQUE BOX BOEING727 7272Q9 138448MNM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH46106 21930 RT AFT AIRSTAIR TORQUE BOX AT VENTRAL STAIR ACTUATOR SUPPORT REPAIR IS CRACKED AND DAMAGED AND WEB IS IMPROPERLY INSTALLED BS 1253 TO 1273. REPAIRED RT AFT AIRSTAIR TORQUE BOX AT VENTRAL STAIR ACTUATOR SUPPORT AND WEB BS 1253 TO 1283 IAW S/B 727-53-0129 REV 5 AND DWG 65C27136. 2L73 4F RTA3WE 20050602001612005060200161NM 2005 6 2 DL738050271 120050515A3610 PNEUMATIC SYSTEM BOEING737 737832 13844CFNM GE CFM56 CFM56* 13802NE A/C BAY CONTAMINATED A DALAC ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO273742C13322 30835 875403 ABORTED T/O FOR SMOKE IN COCKPIT AND CABIN. PERFORMED OIL CONTAMINATION REMOVAL FROM AIR COND AND PNUEM SYS. NO SMELL OF CONTAMINATION NOTED. RAN PACKS AND ENGS TO T/O. NO SMOKE NOTED. 2L72 4F4 FRTA16WE E2GL 20050602001812005060200181WP 2005 6 2 DHL2005807530 120050516A572037048412 FITTING DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH86990 45990 NR 3 MAIN TANK FWD FITTING CRACK 1.000 STA XRS 74.000 S-51 (INBD SIDE) (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED AND APPLIED COATING MATERIAL IAW SRM 51-1-12. INSTALLED NEW FITTING (PN 3704841-2) IAW SRM 51-1-20D PG 9, SRM 51-3-0 PG1, SRM 51-1-23, SR 51-1-11. TORQUED IAW SRM 51-3-1. REFER TO NR 036405 FOR LEAK CHECK. 2L74 4F RT4A25 20050602001852005060200185WP 2005 6 2 DHL2005807533 120050516A572037048411 FITTING DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH86990 45990 NR 2 MAIN TANK AFT FITTING CRACK 1.500, STA XRS 74.000 OUTBD SIDE, S-51. PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED AND APPLIED COATING MATERIAL AREA IAW SRM 51-1-12. INSTALLED NEW FITTING (PN 3704841-1) IAW SRM 51-1-20D PG 9, SRM 51-3-0 PG 1, SRM 51-1-23, SRM 51-1-11. TORQUED IAW SRM 51-3-1. REFER TO NR 036403 FOR LEAK CHECK. 2L74 4F RT4A25 20050606000012005060600001EU 2005 6 6 YENA200530 120050516A2720 YAW DAMPER AIRBUS320 A320232 3930326EU CONTAMINATED A YENAH DEACTIVATE SYST/CIRCUITS WB INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 EA15543JB 1823 HEAVY ELECTRICAL SMELL THROUGHOUT CABIN ON DESCENT. (TURNED LIVE TV OFF). PERFORMED JB INFO NOTICE 2004-T023TR. NO EVIDENCE OF LTV SYSTEM BEING COMPROMISED. NO FAULTS FOUND. SMELL IN THE CABIN DUE TO RESIDUAL FLUID FROM YAW DAMPER CHANGE, REMOVED AND REPLACED. INSPECTED HYDRAULICS AND ACTUATOR, NO LEAKS NOTED AT THIS TIME. CLEANED HYDRAULIC FLUID FROM FUSELAGE IAW AMM 12-21-00. OPS CHECK OF YAW DAMPER IAW AMM 29-00-00 CLEAN AIRCRAFT. 2L72 4F RTA28NM 20050606000062005060600006WP 2005 6 6 UPS05844479 120050505A5712 RIB DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE: C3, LT WING L/E UPPER RIB CRACKED XFS 316.000. REPAIRED BY FABRICATING AND INSTALLING REPAIR DOUBLERS IAW SRM 57-2-0 FIG 2, 51-1-21, 51-1-20D AND 51-1-15. 2L74 4F RT4A25 20050606000262005060600026EA 2005 6 6 COMA0560306 120050510A2750860D10018ABCD CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01926CA187558280 7027 FLIGHT 5146 - FLAPS FAIL CAUTION. COULD NOT DUPLICATE REPLACED THE FECU. 2L72 4F RTA21EA 20050606000402005060600040NM 2005 6 6 DHL2005741519 120050421A5313 STRINGER BOEING727 7272Q9 138448MNM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 STR 27L CORRODED AT FUSELAGE STA 680. REMOVED EXISTING STR SPLICE AN REMOVED CORROSION MORE THAN 509. OF MAT LOSS AN IS OUT OF LIMITS IAW B727 SRM 51-30-2 FIG 7 AN 53-10-1 FIG 1. LOCATED AN DRILLED FASTENER HOLES IN REPLACEMENT PART BAC 1498-132, PO NR 4496180, (14) IAW B727 SRM 51-30-51-30-2 FIG 1 AN 53-10-3 FIG 1. TREATED AN PRIMED PART IAW B727 51-10-2. INSTALLED STR SPLICE IAW B727 SRM 51-30-2 AN 53-10-3 FIG 1. 2L73 4F RTA3WE 20050606000502005060600050NM 2005 6 6 AWXA200500588 120050429A5210 STRUCTURE BOEING BOEING737 7373B7 1384580NM PAX DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28332AW 1030 23384 MCN - MAJOR REPAIR - DURING C-18 CHECK A CRACK WAS FOUND ON THE L2 DOOR LOWER CORNER OF UPPER HINGE CUTOUT BS 967, STR 10 LT. MAINTENANCE ROUTED OUT CRACK AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS PRESENT; FABRICATED A REPAIR DOUBLER AND INSTALLED REPAIR IAW AMERICA WEST AIRLINES ENGINEERING REPAIR 03-5200-05138-SS6. 2L72 4F RTA16WE 20050606000662005060600066NM 2005 6 6 05FDEA01400 120050521A2840 WARNING SYSTEM DOUG MD11 MD11 3023602NM FUEL QTY SYS ACTIVATED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25583FE 48421 5 MINUTES AFTER TAKE OFF LAT FUEL IMB.C/W QRH HAD YELLOW NR 3 FUEL QTY LAT FUEL IMBALANCE ALERT EXT LATER FUEL QTY FAULT. C/W QRH. TIP TANK LOW ALERT. C/W QRH AND ALERT EXT TIP TANK LOW ALERT AGAIN, BEGAN QRH THEN GOT TIP TNK TRAPPED ALERT WITH 5700 BELOW ON SD. TURNED ON ALL CROSSFEED VALVES ACCORDING TO QRH. LAT FUEL FUEL IMB ALERT WITH 18000 TANK 1, 8000 TANK 3. BALANCED TANKS BEFORE LANDING. LANDING UNEVENTFUL AT KDEN. T/S NR 3 FUEL QTY SYS AND REPLACED BOTH INNER AND OUTER MJP'S. REPLACED MJP'S PER MD-11 MM 28-41-40-4. LEAKED CHECKED MJP'S. ALL PROBES AND COMPUTERS READ NORMAL FUEL QTY TEST NORMAL. NO TIP TANK TRAPPED WARNINGS OCCURED. SYSTEM OPERATES NORMALLY. 2L73 4F RTA22WE 20050606000682005060600068NM 2005 6 6 05FDEA01286 120050514A5312AGA717042 BULKHEAD DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25621FE 48792 CENTER CARGO STA 1841 FLOOR AREA BULKHEAD APPROX X= -23 WEB FOUND CRACKED. CRACKED WEB AT CENTER CARGO STA 1841 FLOOR AREA BULKHEAD X= -23 CUT AT STA 1841 X= -23 AND REMOVED AS PER SRM 53-00-01 FIGURE 10 VOLUME I. REPAIR WEB AND DOUBLER FABRICATED AND INSTALLED AS PER SRM 53-00-01 FIGURE 10 VOLUME I. REPAIR IS CLASSIFIED MAJOR PER GMM 6-2-100. 2L73 4F RTA22WE 20050606000752005060600075NM 2005 6 6 05FDEA01308 120050516A5712ARB2850506 RIB DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25580FE 48471 RT WING LEADING EDGE SLAT TRACK NR 16 INBOARD RIB FOUND CRACKED. CRACKED RIB REMOVED AND REPLACED AS PER SRM 51-33-01 AND SRM 51-35-01 VOLUME II. THIS REPAIR CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050606000782005060600078NM 2005 6 6 05FDEA01464 120050525A5230 SKIN BOEING727 727200 138407ENM CARGO DOOR DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 FWD LOWER CARGO DOOR, EXTERIOR SKIN HAS A DENT, 16 INCHES DOWN FROM TOP, 35 INCHES AFT FROM FWD EDGE. REPAIRED DOOR PER SRM 52-00-3 2L73 4F RTA3WE 20050606000882005060600088NE 2005 6 6 VTZA200500090 220050525A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RIGHT SHUTDOWN A VTZAC ABORTED TAKEOFF XJ ENGINE FLAMEOUT WARNING INDICATION TOTAKEOFF 1 EA27625BR 7214 RT ENG SHUTDOWN ON TAKEOFF ROLL AT ROTATION. 2L72 4F4 FRTA21EA E15NE 20050606000892005060600089NM 2005 6 6 USAA20050006 120050517A5512 SKIN BOEING737 7373B7 1384580NM HORIZONTAL STAB CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19387US 22959 A 2.1875 INCH CRACK IN LOWER SKIN, AFT SPAR OF HORIZ STAB, STA 123. INSTALLED REPAIR DOUBLER WITH BLIND FASTENERS PER TRR 55-10-07 REV B. 2L72 4F RTA16WE 20050606000902005060600090NM 2005 6 6 SB05063 120050521A3350210310005 FUSE BOEING737 737301 1384611NM EMERGENCY LIGHT BLOWN A USAAK NONE O OTHER ININSP/MAINT 1 EA19577US 23742 MAINTENANCE REPORTED MULTIPLE EMERGENCY LIGHTS IN THE FORWARD CABIN AND GALLEY AREA INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND THE FUSE IN THE FORWARD RIGHT EMERGENCY LIGHT BATTERY CHARGER. ALL EMERGENCY LIGHTS CHECK GOOD. 2L72 4F RTA16WE 20050606000912005060600091 2005 6 6 SA05057 420050527A2565D30664105 SLIDE AIRBUSA319 A319112 3930323EU PASSENGER CABIN MISROUTED A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19716UW169601399 1055 DURING HEAVY INSPECTION, MAINTENANCE FOUND THAT THE RIGHT FORWARD ESCAPE SLIDE ASSEMBLY HAD AN INCORRECTLY INSTALLED MOORING LINE, AND AN INCORRECTLY ROUTED LIGHT HARNESS ASSEMBLY. MAINTENANCE CORRECTLY ROUTED THE LIGHT HARNESS ASSEMBLY AND INSTALLED THE MOORING LINE TO THE LEFT END OF THE GIRT ASSEMBLY. SLIDE OK FOR SERVICE. 2L72 4F RTA28NM 20050606000922005060600092NM 2005 6 6 UPS05444468 120050515A5315 FLOORBEAM BOEING747 747123 1384873NM FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 FLOORBEAM AT STA 1800 HAS ELONGATED HOLES. A/C OOS AND WILL REQUIRE MX FERRY (9127) TO SAT. INSTALLED FREEZE PLUG AT STA 1800 LBL 99 IN FLOORBEAM IAW SA SK 675-800542. 2L74 4F RTA20WE 20050607000182005060700018EU 2005 6 7 F3LA200500020 120050518A27103945128102 COMPUTER AIRBUSA319 A319112 3930323EU NR 2 ELAC INOPERATIVE A F3LAK NONE F FLT CONT AFFECTED DEDESCENT 1 NM03915FR 3000 1851 FLIGHT CREW REPORTED ELAC 2 FAULT. ON SHORT FINAL LOST BOTH AILERONS WENT TO DIRECT LAW. REPLACED NR 2 ELAC. OPERATIONAL CHECK GOOD PER MM 27-93-34, PAGE 401. PERFORMED LAND CAT 3 TEST, OPS CHECK GOOD PER MM 22-97-00-710-001. UMP STATUS REMAINED CAT 3B. REPLACED RUDDER PEDAL TRANSDUCER UNIT AS PRECAUTIONARY. 2L72 4F RTA28NM 20050607000202005060700020NM 2005 6 7 DHL2005740527 120050327A5330 SKIN BOEING727 7272Q9 138448MNM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH21930 21930 PREVIOUS FLUSH REPAIR RT FUSELAGE SKIN IS DENTED FWD OF STA 1243 ABOVE STR 22R. REMOVED PREVIOUS REPAIR TO BE OUT OF LIMITS AT R/SIDE FUSELAGE SKIN STA 1243 STR 22R IAW B727 SRM 51-30-2. CUTOUT DAMAGED AREA DIM 4.5 BY 4 INCHES IAW B727 SRM 53-30-3 FIG 24. FABRICATED DOUBLER REPAIR MAT USED 2024T3 .063 PO NR 9002118 DIMENSION 40 BY 22 INCHES AND 1EA FILLER MAT USED 2024T3 .063 PO NR 9002118 DEMENSION 42 BY 17 INCHES IAW B727 SRM 53-30-2 FIG 48 AND 53-30-3 FIG 24. ALODINED AND PRIMED IAW B727 SRM 51-10-2. REMOVED PNEUMATIC DUCTING AT STA 1223 TO 1263 ON RIGHT SIDE. INSTALLED DOUBLER REPAIR IAW B727 SRM 53-30-3 FIG 24. INSTALLED PNEUMATIC DUCTING AT STA 1223 IAW B727 36-00-01, LEAK CK GOOD. 2L73 4F RTA3WE 20050607000242005060700024NM 2005 6 7 DHL2005740531 120050327A5711 SPAR BOEING727 7272Q9 138448MNM FLAP TRACK CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH21930 21930 RT WING TRAILING EDGE FALSE SPAR HAS A TWO INCH CRACK JUST INBD OF NR 6 FLAP TRACK WBL 202 WING STA 330.5. REMOVED AND DISPLACED R/WING LOWER T/EDGE PANELS AS REQUIRED FOR ACCESS IAW B727 SRM 51-30-2. CUT OUT AND REMOVED 52" SECTION OF CRACKED AUX SPAR LWR CHORD FROM WBL 192.5 TO OUTBD END IAW B727 S/B 57-158 REV 1 FIG 6. FABRICATED NEW SECTION OF LOWER SPAR CHORD 52" L FROM P/N BAC 1514-1437 MATPO NR 5080207 RADIUSED STRAP 15 1/2".090 7075T6 MAT PO NR 9001777 AND 2EA REPAIR ANGLE 2" BY 1" BY 15 1/2"L FROM 7075T6 .071 PO NR 5080213 IAW B727 S/B 57-158 REV 1 FIG 6. TREATED AND PRIMED NEW CHORD SECTION RADIUS STRAPS REPAIR ANGLE IAW B727 SRM 51-10-2. INSTALLED NEW SPAR AND SPLICE REPAIR IAW B727 S/B 57-158 R2L73 4F RTA3WE 20050607000262005060700026NM 2005 6 7 DHL2005740533 120050405A5330 SKIN BOEING727 7272Q9 138448MNM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 REMOVED EXTERNAL SKIN DOUBLER AT STA 1157-1183, STR 19L-22L DUE TO PILLOWING AT UPPER END IAW B727 SRM 51-30-2, CLEANED UP INTERNAL STRUCTURE AND FUSELAGE SKIN AREA FOR RE-EVALUATION IAW B727 MM 12-40-0 WITH NO CORROSION NOTED, CUT OUT 1 BY 1 1/2 IN SECTION OF FUSELAGE SKIN DUE TO DENT BEYOND ALLOWABLE LIMITS AT STA 1171 AND STR 19L IAW B727 SRM 53-30-3 FIG 3. TREATED AND PRIMED FUSLAGE INTERNAL STRUCTURE, SKIN FILLER AND REPAIR DOUBLER AND INSTALLED ON FUSELAGE IAW B727 SRM 53-30-3 FIG 3 AND AEI DWG NR AE5093 REV B. THIS REPAIR IS CATEGORY "B". 2L73 4F RTA3WE 20050607000272005060700027NM 2005 6 7 DHL2005740534 120050328A5347BAC1520841 SEAT TRACK BOEING727 7272Q9 138448MNM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 MAIN CABIN SEAT TRACK BS 760 - 870 RBL 45.5 DAMAGED. REMOVED AND REPLACED SEAT TRACK BS760 - 870 RBL 45.5 IAW SRM 53-10-5 FIG 2. FABRICATED FROM P/N BAC1520-841 PO NR 9001690 DIM 8 FT IAW B727 SRM 53-10-2 FIG 1 AND 53-10-5 FIG 2. TREATED AND PRIMED SEAT TRACK IAW B727 SRM 51-10-2. 2L73 4F RTA3WE 20050607000312005060700031NM 2005 6 7 DHL2005740540 120050329A5311AE727236013 FRAME BOEING727 7272Q9 138448MNM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 CABIN INTERIOR FRAME AT BS348 IS BENT AND ELONGATED HOLES BETWEEN STR 4L - 6L. PREVIOUS FRAME REPAIR. REMOVED ANGLE SUPPORT IAW B727 SRM 51-30-2, DUE TO ELONGATED HOLES, CUT OUT DAMAGED AREA DIM .50 INCH EDGE UPPER AND LOWER FRAME IAW B727 SRM 51-10-1 AND DWG NR AE727-2-360 REV G AEI. LOCATED AND DRILLED NEW ANGLE P/N AE727-2-360-13 PO NR 508068 IAW B727 SRM 51-30-5 AND DWG NR AE727-2-360 REVG AEI. TREATED AND PRIMED HOLES AND AREA FRAME IAW B727 SRM 51-10-2. INSTALLED ANGLE SUPPORT AT BS348 BETWEEN STR 4L - 6L IAW DWG NR AE727-2-360 AEI. 2L73 4F RTA3WE 20050607000322005060700032NM 2005 6 7 DHL2005740541 120050428A5330 SKIN BOEING727 7272Q9 138448MNM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH46106 21930 REMOVED MAST AT BS 720C ON EA 38100001-001-B, FABRICATED REPAIR DOUBLER FROM 2024T3 .050 P.O 9002093 DIM 14 1/2" BY 6" IAW B727 SRM 53-30-3 FIG 3 AND 53-50-1 FIG 1. TREATED AND PRIMED DOUBLER AND AREA IAW B727 SRM 51-10-2, INSTALLED DOUBLER REPAIR AT BS 720C IAW B727 SRM 53-30-3 FIG 3. 2L73 4F RTA3WE 20050607000342005060700034NM 2005 6 7 DHL2005740544 120050329A5347BAC1520841 SEAT TRACK BOEING727 7272Q9 138448MNM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 MAIN CABIN SEAT TRACK BS 760 - BS 870 LBL 24.75 DAMAGED. REMOVED SEAT TRACK BS 760 - BS 870 LBL 24.75 IAW B727 SRM 51-30-2. FABRICATED NEW SEAT TRACK FROM P/N BAC1520-841 PO NR 9001474 DIM 4 FT AND P/N BAC1520-841 PO NR 9001690 DIM 4 FT IAW B727 SRM 53-10-2 FIG 1 AND 53-10-5 FIG 2. TREATED AND PRIMED NEW SEAT TRACK IAW B727 SRM 51-10-2. INSTALLED NEW SEAT TRACK BS 760 - BS 870 LBL 24.75 IAW B727 SRM 53-10-5 FIG 2. 2L73 4F RTA3WE 20050607000372005060700037NM 2005 6 7 DHL2005740547 120050329A5311 FRAME BOEING727 7272Q9 138448MNM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 FRAME BS 640 SHOW DENT BETWEEN STR 16R AND 17R PREVIOUS FRAME REPAIR. REMOVED PREVIOUS REPAIR AT FUSELAGE FRAME BS 640 BETWEEN STR 16R AND 17R IAW B727 SRM 51-30-2. FABRICATED NEW FRAME REPAIR MAT. USED 7075T6 .071 PO NR 9001737 DIM 7" BY 5" IAW B727 SRM 53-10-2 FIG 3 AND 51-40-3 FIG 1. ALODINED AND PRIMED AREA IAW B727 SRM 51-10-2. INSTALLED FRAME REPAIR IAW B727 SRM 51-40-3 FIG 1. 2L73 4F RTA3WE 20050607000382005060700038NM 2005 6 7 DHL2005740545 120050329A5311 FRAME BOEING727 7272Q9 138448MNM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 FUSELAGE FRAME AT STA 520 SHOW DENT BTW STR 16R AND 17R PREVIOUS REPAIR. REMOVED PREVIOUS REPAIR AT BS 520 BTW STR16R AND 17R IAW B727 SRM 51-30-2. FABRICATED NEW FRAME REPAIR MAT USED 7075T6 .071 PO NR 9001737 DIMENSION 8" BY 5" IAW B727 SRM 53- SRM 10-2 FIG3 AND 51-40-3 FIG 1. ALODINED AND PRIMED PART AND AREA IAW B727 SRM 51-10-2. INSTALLED FRAME REPAIR IAW B727 SRM 51-40-3 FIG 1. 2L73 4F RTA3WE 20050607000392005060700039NM 2005 6 7 DHL2005740548 120050320A5311 FRAME BOEING727 7272Q9 138448MNM FUSLEAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 REMOVED PREVIOUS REPAIR FUSELAGE FRAME BS 580 STR 16R AND 17R IAW B727 SRM 51-30-2. FABRICATED NEW FRAME REPAIR MAT USED 7075T6 .071 PO 9001737 DEM 6" BY 5" IAW B727 SRM 53-10-2 FIG 3 AND 51-40-3 FIG 1. ALODINED AND PRIMED AREA AND PART IAW B727 SRM 51-40-2. INSTALLED NEW FRAME REPAIR IAW B727 SRM 51-40-2 FIG 1. 2L73 4F RTA3WE 20050607000402005060700040NM 2005 6 7 DHL2005740549 120050329A5313 STRINGER BOEING727 7272Q9 138448MNM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 STR 26L AT BS 480 IS CORRODED. REMOVED STRINGER SLICE FOUND TO BE OUT IF LIMITS AT STR 26L AT BS 480 IAW B727 SRM 51-30-2. FABRICATED NEW STRINGER REPAIR MAT USED 7075T6 .040 PO NR 9001068 DIM. 13" BY 4" IAW B727 SRM 51-20-1 AND 53-10-2 FIG 9. ALODINED AND PRIMED PART AND AREA IAW B727 SRM 51-10-2. INSTALLED STRINGER SPLICE IAW B727 SRM 51-30-2 AND 53-10-2 FIG 9. 2L73 4F RTA3WE 20050607000432005060700043NM 2005 6 7 DHL2005740550 120050329A5347 SEAT TRACK BOEING727 7272Q9 138448MNM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH46106 21930 MAIN CABIN SEAT TRACK 0 BS 344 TO BS 580 RBL .5. REMOVED AND REPLACED 0 SEAT TRACK BS 344 TO BS 580 RBL .5 IAW DWG NR AE 727-2-063 REVP. FABRICATED NEW SEAT TRACK P/N S139966 PO NR 438032 DIA 12FT P/N S139966 PO NR 991600 DIM 8FT IAW B727 SRM 51-30-5 AND DWG AE 727-2-063 REV P AERONAUTICAL ENGINEERS INC. 2L73 4F RTA3WE 20050607000442005060700044NM 2005 6 7 DHL2005740556 120050331A5320 STRAP BOEING727 7272Q9 138448MNM FUSLEAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 REPAIRED STRAP AT FWD E/E BS STA 328-344 LBL 24 IAW B727 SRM 53-10-8 FIG 6. TREATED AND PRIMED STRAP IAW B727 SRM 51-10-2, DIM 24"X2 5/8" PO 900505. 2L73 4F RTA3WE 20050607000452005060700045NM 2005 6 7 DHL2005740554 120050331A5310 TORQUE BOX BOEING727 7272Q9 138448MNM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 CRACK AT INBD WED RT LOWER TORQUE BOX, LOWER LIGHTENING HOLE STA 1240. STOP DRILLED CRACK .250 TERMINATED AT END OF CRACK ON RT LOWER TORQUE BOX WEB STA 1240 IAW B727 SRM 51-10-1 NDT INSP AREA USING HFEC IAW B727 NDTM PAR 6 51-00-00 FIG 23. CRACK TERMINATED IN STOP HOLE. FABRICATED DOUBLER REPAIR MAT USED 7075T6 .032 PO NR 900513 DIM. 3 3/4" BY 3 1/2" IAW B727 SRM 53-1-2 FIG 6 AND 51-40-2 FIG1. ALODINED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED DOUBLER IAW B727 SRM 51-40-2 FIG 1. 2L73 4F RTA3WE 20050607000472005060700047NM 2005 6 7 DHL2005740551 120050329A5311 FRAME BOEING727 7272Q9 138448MNM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 REMOVED PREVIOUS REPAIR AT FUSELAGE FRAME BS 600 BTW 16R AND 17R IAW B727 SRM 51-30-2. FABRICATED NEW FRAME REPAIR MAT USED 7075T6 .071 PO 9001737 DIM 6" BY 5" IAW B727 SRM 53-10-2 FIG 3 AND 51-40-3 FIG 1. ALODINED AND PRIMED PART AND AREA IAW B727 SRM 51-10-2. INSTALLED FRAME REPAIR IAW B727 SRM 51-40-3 FIG 1. 2L73 4F RTA3WE 20050607000482005060700048NM 2005 6 7 DHL2005740558 120050404A5347 SEAT TRACK BOEING727 7272Q9 138448MNM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 MAIN CABIN SEAT TRACK BS 480 TO 690 LBL 45.5 DAMAGED. REMOVED SEAT TRACK FROM BS 480- 740 LBL 45.5 IAW B727 SRM 51-30-2. FAB NEW SEAT TRACK FROM PN BAC 1520-792 PO NR 9001707 DIM 29' IAW B727 SRM 53-10-5 (1) AN DWN NR 2902 VENTURA AEROSPACE. FAB NEW ANGLES (SPLICES) 2 EA FROM PN BAC 1503-100122. PO NR 900943 DIM 13" EACH AND SPLICE PLATE FROM 7075T6 .0.250 DIM 2" BY 7 1/2 " IAW B727 SRM 53-10-5, PO NR 9001189. ALODINED AN PRIMED PARTS AN BARE METAL IAW B727 SRM 51-10-2. INSTALLED SEAT TRACK, SPLICE PLATE AN SPLICES (ANGLES) AT BS 480-740 LBL 45.5 IAW B727 SRM 53-10-5 FIG 1. 2L73 4F RTA3WE 20050607000492005060700049NM 2005 6 7 DHL2005740555 120050331A5310 WEB BOEING727 7272Q9 138448MNM TORQUE BOX CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH21930 21930 CRACK AT INBD WEB R/LOWER TORQUE BOX LWR LIGHTENING HOLES STA 1248. STOP DRILLED CRACK .250 TERMINATED AT END OF CRACK AT INBD R/LOWER TORQUE BOX LWR LIGHTENING HOLE STA 1248 IAW B727 SRM 51-10-1 NDT INSPECTED USING HFEC IAW B727 NDT MAN PART 651-00-00 FIG 23 CRACKS TERMINATED IN STOP DRILL HOLE FABRICATED DOUBLER REPAIR MAT USED 7075T6 .032 PO NR 900573 DIMENSION 3 3/4" BY 3 1/2" IAW B727 SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1. ALODINED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED IAW B727 SRM 51-40-2 FIG 1. 2L73 4F RTA3WE 20050607000512005060700051NM 2005 6 7 DHL2005740559 120050331A5330 SKIN BOEING727 7272Q9 138448MNM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH46106 21930 DENT LT FUSELAGE SKIN AT STA 1355 NR 2 ENGINE SUPPORT STRUCTURE. REMOVED FASTENERS AT L/SIDE FUSELAGE SKIN AT STA 1355 NR 2 ENG SUPPORT IAW B727 SRM 51-30-2. CUT-OUT DAMAGE AREA DIMENSION 1" BY 1 1/4" IAW B727 SRM 51-40-2 FIG 1. FABRICATED DOUBLER MAT USED 2024T3 .050 PO NR 9002093 SIZE 12 1/2" BY 11 1/2" IAW B727 SRM 51-40-2 FIG1 AND 54-30-2 FIG 4. ALODINED AND PRIMED PART AND AREA IAW B727 51-10-2 AND INSTALLED DOUBLER IAW B727 SRM 54-30-2 FIG 4 AND 51-30-2. 2L73 4F RTA3WE 20050607000522005060700052SO 2005 6 7 RAIA00505010 120050513A243430086011 GENERATOR EMB 145 EMB145EP 3260221SO RIGHT INOPERATIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03827HK7381 1691 145021 FLT 5657 - STL - RIGHT GENERATOR INOP. MAINTENANCE REMOVED AND REPLACED NR 2 GENERATOR. 2L72 4F RTT00011AT 20050607000562005060700056EU 2005 6 7 RAIA00505014 120050517A7710 SENSE LINE JETAIRJETSTMJETSTM4101 1500501EU LT ENGINE LOOSE A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03568HK 41086 FLT 5436 - SPI - LEFT ENGINE WOULD NOT MAKE TARGET TORQUE. MAINTENANCE SECURED NR 1 ENGINE P-3 SENSING LINE, AND OPS CK OK. 2L72 4T RTA41NM 20050607000572005060700057EU 2005 6 7 RAIA00505015 120050517A3260AIR135668 UPLOCK SWITCH JETAIRJETSTMJETSTM4101 1500501EU LT MLG MALFUNCTIONED A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03556HK 41073 FLT 5447 - STL - LIGHT REMAINED ON IN GEAR HANDLE AFTER RETRACTION. MAINTENANCE REMOVED AND REPLACED LT MLG UPLOCK SWITCH. 2L72 4T RTA41NM 20050607000582005060700058EU 2005 6 7 RAIA00505016 120050517A3260877701 CONTROL HANDLE JETAIRJETSTMJETSTM4101 1500501EU MLG MALFUNCTIONED A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03561HK1203 447 41077 FLT 5711 - STL - LIGHT IN GEAR HANDLE REMAINED ON AFTER GEAR RETRACTION. MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE. 2L72 4T RTA41NM 20050607000602005060700060EU 2005 6 7 MAC5402 120050405A2436153912B VOLT REGULATOR FOKKERF27 F27MK500 4990629EU NR 2 GENERATOR FAILED A MTNAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO33716FE 10471 NR 2 GENERATOR DROPPED OFFLINE DURING CLIMBOUT. 2H72 4T A817 20050607000642005060700064SO 2005 6 7 CHQA200500100 120050517A3350RPS1B BATTERY PACK EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSUNSERVICEABLE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11272SK 145306 ON INITIAL WALK OUT TO THE AIRCRAFT THE EMERGENCY LIGHTS WERE ALL ON. FOUND THE SWITCH IN THE COCKPIT TO BE IN THE OFF POSITION. INSPECTED AIRCRAFT AND FOUND IT TO BE SAFE FOR FERRY FLIGHT FROM TPA TP CMH. REMOVED AND REPLACED ALL FOUR EMERGENCY BATTERY PACKS. OPS CHECK GOOD IAW EMB 145 AMM 33-50-4. 2L72 4T RTT00011AT 20050607000652005060700065NM 2005 6 7 DHL2005782002 120050517A3230 ACCESSORY UNIT BOEING727 727227 1384078NM MLG MALFUNCTIONED A DHLAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TXTAXI/GRND HDL 1 SO01782DH 21998 WHILE TAXI IN TO STL HEARD ELECTRICAL RELAYS CYCLING OFF AND ON AND THEN SMELLED SMOKE AND A LIGHT HAZE WAS IN THE COCKPIT. AS THE RELAYS WERE CLICKING STALL WARNING AMBER LIGHT FLICKERED OFF AND ON. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT REF MM 32-00. PERFORMED VISUAL CHECK OF WIRING IN COCKPIT AND FOUND NO IRREGULARITIES. PERFORMED GROUND OPERATIONAL CHECKS PER MM 31-26-0. 2L73 4F A3WE 20050607000662005060700066NM 2005 6 7 DHL2005751001 120050521A2612 CONNECTOR BOEING727 727264 138408MNM FIRE LOOP BROKEN A DHLAFEB ACTIVATE FIRE EXT. ENGINE SHUTDOWN EMER. DESCENT N FALSE WARNING APAPPROACH 1 SO01751DH 22982 AT 5000 FT ON FINAL NR 1 FIRE HANDLE ILLUMINATED AND BELL SOUNDED PERFORMED PHASE 1'S AND ENERGENCY CHECKLIST BLEW BOTH FIRE BOTTLES LIGHT REMAINED ILLUMINATED UNTIL AFTER LANDING. REPLACED BROKEN AFT, "A" LOOP CONNECTOR PER BOEING STD WRG PCTS MAN 20-62-16 AND AND WP DIAG 26-11-01. CHECKS SERV PER B-727 M/M 26-11-01, P/N 878238-02. 2L73 4F A3WE 20050607000702005060700070SW 2005 6 7 EGRR100766 120050505A243523046020 STARTER GEN BELL 412 412EP 1182205SW PWA PT6 PT6* 52043EA NR 2 INOPERATIVE B EGRRO OTHER J WARNING INDICATION CRCRUISE 1 EA17412PP 33207 THE NR 2 STARTER GENERATOR FAILED AFTER 317.8 HOURS (TSO). FOUND BRUSHES BADLY WORN, MISSING AND SMALL PIECES OF BRUSH MATERIAL WERE FOUND UNDER THE STARTER GENERATOR ON AIRCRAFT. REPLACED STARTER GENERATOR WITH OVERHAULED UNIT, ADJUSTED AND OPS CHECKED OK. 1G72 4U3 T H4SW E2NE 20050607000752005060700075EU 2005 6 7 TXER100821 120050422A7100365A54802001 BAFFLE UROCOPEC155 EC155B 8681000EU ENGINE WORN B TXERO OTHER O OTHER NRNOT REPORTED 1 SW09155EW 6660 WORN BAFFLE. 1G72 3U H10EU 20050607000802005060700080SW 2005 6 7 AC2A100893 120050503A6220 PIN BELL 430 430 1182150SW RESTRAINT DEBONDED B AC2AK NONE O OTHER ININSP/MAINT 1 SO07430CM3477 LP0468 49090 PIN DEBONDED/ REPLACED RESTRAINT. 1G72 3U RTH9SW 20050607000812005060700081SW 2005 6 7 AC2A100892 120050503A6220 PIN BELL 430 430 1182150SW RESTRAINT DEBONDED B AC2AK NONE O OTHER ININSP/MAINT 1 SO07430CM3477 LP0473 49090 PIN DEBONDED/ REPLACED RESTRAINT. 1G72 3U RTH9SW 20050607000832005060700083CE 2005 6 7 DXTA200500739 120050522A499038007221 APU CESSNA560 560XL 2076702CE APU BAY OVERSERVICED E DXTAA UNSCHED LANDING WB INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL07651QS 5605251 AFTER TAKEOFF, HAD A SMOKE SELL FROM AN UNIDENTIFIABLE SOURCE. NO SMOKE WAS VISIBLE. NO UNUSUAL INDICATIONS, NO C/B OPENED, SMELL DISSIPATED WITH APU SHUT DOWN) - FOUND APU OIL TANK OVERSERVICED, OPERATED APU FOR AN EXTENSIVE PERIOD WAS ABLE TO DUPLICATE SMELL FOR A SHORT TIME THROUGH AIR OUTLETS, CONTINUED OPERATING APU TO PURGE EXCESS OIL. SCENT OF OIL NO LONGER PRESENT. WORK PERFORMED AS PER 560 MMCH 49-00-00 AND 12-11-03. 2L72 4F RTA22CE 20050607000842005060700084CE 2005 6 7 DXTA200500732 120050518A3240215671 BRAKE CESSNA750 750 2076810CE NR 3 WORN E DXTAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07964QS1628 7500164 BRAKES FEEL SOFTER THAN NORMAL CE750 APPLICATION WHEN AIRCRAFT IS STOPPED GRADUALLY HIGH FREQUENCY VIBRATION OCCURS. FOUND NR 3 BRAKE ASSEMBLY WORN TO LIMITS. REMOVED OLD BRAKE. INSTALLED EXCHANGE BRAKE. BLED BRAKE. PERFORMED ANTI-SKID FUNCTIONAL TEST. TEST GOOD. TAXI CHECK GOOD. WORK DONE IAW CITATION 750 MM, CHAPTER 32-42-01, AND BF GOODRICH COMPONENT MM CHAPTER 32-46-47. 2L72 4J RTT00007WI 20050607000862005060700086NM 2005 6 7 CALA0500156 120050522A5315BAC15181210 FLOORBEAM BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2724212 28772 INSPECTION FOUND FLOORBEAM CORRODED AT STA 312, LBL 12. A CAP WAS INSTALLED ON FLOORBEAM IAW ECRA 5321-01224. 2L72 4F RTA16WE 20050607000872005060700087NM 2005 6 7 CALA0500157 120050522A5315BAC15181208 FLOORBEAM BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2724212 28772 INSPECTION FOUND FLOORBEAM CORRODED AT STA 344, LBL 10. A REPAIR WAS INSTALLED IAW ECRA 5321-01223. 2L72 4F RTA16WE 20050607000882005060700088NM 2005 6 7 CALA0500158 120050522A5315BAC1505100246 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714325 23455 INSPECTION FOUND FLOORBEAM CORRODED AT STA 344, LBL 48 TO RBL 48. THE FLOORBEAM SECTION WAS REMOVED AND REPLACED IAW SRM 53-10-51. 2L72 4F RTA16WE 20050607000892005060700089NE 2005 6 7 CALA0500159 220050520A7200 BLADES BOEING757 757224 1384958NM RROYCERB211 RB211535E4B3 NE NR 2 ENGINE DAMAGED A CALAEA ENGINE SHUTDOWN UNSCHED LANDING CJ F.O.D. WARNING INDICATION CLCLIMB 1 SW273413138571 28971 31224 THE NR 2 ENGINE WAS SHUTDOWN AFTER TAKEOFF DUE TO HIGH VIBRATION AND HIGH EGT. THE AIRCRAFT WAS RETURNED TO SNN WHERE IT LANDED WITHOUT INCIDENT. INSPECTION FOUND EVIDENCE OF BIRD INGESTION WITH NOSE COWL DAMAGE AND SEVERAL FAN BLADES HAD MISSING TIPS. THE NR 2 ENGINE WAS REMOVED AND REPLACED. 2L72 4F4 FRTA2NM E12EU 20050607000912005060700091NM 2005 6 7 ASMF200505020 120050519A7931 TRANSMITTER DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE RT ENGINE OIL LOOSE W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23169PL 53175 718246 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE, DURING PUSH BACK AND RIGHT ENGINE STARTING, IT WAS NO OIL PRESSURE INDICATIONS. THE LP2 RESTRICTOR AND THE RESPECTIVE CONNECTOR WERE CLEANED. THE ENGINES WERE STARTED AND OIL PRESSURE INDICATION WAS CORRECT IAW MM 71-00-00, TESTED CORRECT. DURING OVERNIGHT SERVICE LV3 LINE CONNECTION TO OIL PRESSURE TRANSMITTER WAS FOUND LOOSE. THE LINE WAS INSTALLED IAW MM 20-10-11, TESTS WERE PERFORMED IAW MM 71-00-00, ALL CORRECT. 2L72 4F4 FRTA6WE E9NE 20050607000932005060700093EA 2005 6 7 QXEA200500892 120050502A5320 FLOOR SUPPORT CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FUSELAGE INTERIOR COCKPIT FLOOR BOARD SUPPORT ANGLE AT STATION 280 IS CORRODED. REPAIRED IAW CRJ-700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20050607000942005060700094EA 2005 6 7 QXEA200500891 120050503A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FUSELAGE INTERIOR LEFT LOWER WEB OF STATION 280 BULKHEAD IS CORRODED ALONG THE FLOOR LINE. REPAIRED IAW REO 670-73-11-052. 2L72 4F RTA21EA 20050607000952005060700095EA 2005 6 7 QXEA200500893 120050502A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FORWARD FUSELAGE LOWER SKIN PANEL ROCK CHIP DAMAGE AT STATION 564.5 BETWEEN STRINGER 26R AND 25R. REPAIRED IAW CRJ 700 SRM 51-12-00-001-001-A01, 51-21-11-001-001-A01, 51-25-01-001-001-A01 AND 53-31-01-101-003-A01. 2L72 4F RTA21EA 20050607000962005060700096EA 2005 6 7 QXEA200500894 120050505A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FORWARD FUSELAGE FORWARD BAGGAGE BAY SKIN PANEL DAMAGED AT STATION 542.5 AND 571.3, STRINGER 26L. REPAIRED IAW REO 670-53-31-040, HORIZON AIR EA R-53-325, CRJ 700 SRM 51-25-00-001-001-A01 AND 51-21-11-001-001-A01. 2L72 4F RTA21EA 20050607000972005060700097EA 2005 6 7 QXEA200500885 120050505A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FORWARD FUSELAGE LOWER SKIN PANEL DAMAGED AROUND POTABLE WATER SERVICE AND DRAIN DOOR, STATION 349.00 TO 364.00 BETWEEN STRINGER 24R AND 22R. REPAIRED IAW CRJ-700 SRM 51-12-00 AND REO 670-53-21-104 ABD HORIZON AIR EA R-53-330. 2L72 4F RTA21EA 20050607000992005060700099EA 2005 6 7 QXEA200500887 120050505A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FORWARD FUSELAGE LOWER SKIN PANEL GOUGED AT STATION 364.00 AND BETWEEN STRINGER 22L AND 23L. REPAIRED IAW CRJ700 SRM 51-21-01-101-006-A01 AND 51-12-00-001-001-A01. 2L72 4F RTA21EA 20050607001012005060700101EA 2005 6 7 QXEA200500889 120050503A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FORWARD FUSELAGE LOWER SKIN PANEL ROCK CHIP DAMAGE STATION 409.00 TO 421.00 BETWEEN STRINGER 27L AND 25L. REPAIRED IAW CRJ700 SRM 51-12-00, 51-25-16-001-001-A01, 51-21-11-001-001-A01, HORIZON AIR EO R-53-331 AND REO 670-53-21-103. 2L72 4F RTA21EA 20050607001052005060700105WP 2005 6 7 UPS05844499 120050519A3510 OXYGEN MASK DOUG DC8 DC873F 302199FWP COCKPIT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 02 MASK INOPERATIVE. DEFERRED M302656. REMOVED AND REPLACED 1ST OBSERVER'S 02 MASK PER MM 35-10-08. OPS CHECK NORMAL. THIS CLEARS M302656. 2L74 4F RT4A25 20050607001072005060700107EA 2005 6 7 QXEA200500898 120050429A1430 RIVET CNDAIRCL600 CL6002C10 1390015EA ZONE 200 LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FUSELAGE EXTERIOR HAS SMOKING RIVETS AT STATION 693 AND STRINGER 7R. REPAIRED IAW CRJ-700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20050607001082005060700108EA 2005 6 7 QXEA200500899 120050429A1430 RIVET CNDAIRCL600 CL6002C10 1390015EA ZONE 200 LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FUSELAGE EXTERIOR HAS SMOKING RIVET AT STATION 830 AND STRINGER 7R. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20050607001092005060700109EA 2005 6 7 QXEA200500900 120050428A1430 RIVET CNDAIRCL600 CL6002C10 1390015EA ZONE 200 LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FUSELAGE EXTERIOR HAS SMOKING RIVET AT STATION 850 AND STRINGER 10L. REPLACED IAW CRJ700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20050607001102005060700110EA 2005 6 7 QXEA200500901 120050509A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 200 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FUSELAGE EXTERIOR HAS SCRATCHES AT STATION 310, STRINGER 15L, FORWARD OF PASSENGER DOOR. REPAIRED IAW CRJ700 SRM 51-12-00, REO 67-53-21-102 AND HORIZON AIR EA R-53-329. 2L72 4F RTA21EA 20050607001122005060700112EA 2005 6 7 QXEA200500897 120050506A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 200 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FUSELAGE EXTERIOR HAS SCRATCH ON FUSELAGE SKIN AT STATION 1047, SFT OF BAGGAGE DOOR CUTOUT. REPAIRED IAW REO 670-53-61-169 AND HORIZON AIR EA R-53-327, CRJ700 SRM 51-21-16-001-001-A01. 2L72 4F RTA21EA 20050607001182005060700118EA 2005 6 7 QXEA200500914 120050428A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FUSELAGE INTERIOR LEFT SIDE SEAT RAIL HAS SURFACE CORROSION ON INNER MOST SURFACE AT STATION 582. REPAIRED IAW REO 670-53-00-013. 2L72 4F RTA21EA 20050607001212005060700121EA 2005 6 7 QXEA200500908 120050428A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FUSELAGE INTERIOR RIGHT INBOARD FLOOR SEAT RAIL HAS PITTING AND SURFACE CORROSION ON TOP AND INNER SURFACES AT FOLLOW LOCATION, STATION 601- 664. REPAIRED IAW REO 670-53-00-013. 2L72 4F RTA21EA 20050607001272005060700127EA 2005 6 7 QXEA200500922 120050506A5410 LATCH CNDAIRCL600 CL6002C10 1390015EA ZONE 400 WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - LEFT ENGINE UPPER AND LOWER BLOW OFF DOOR LATCH REBATE WORN. REPAIRED IAW CRJ700 SRM 51-23-00-001-001-A01, 51-42-06-001-001-A01 AND SRM 51-42-13-001-001-A01. 2L72 4F RTA21EA 20050607001282005060700128EA 2005 6 7 QXEA200500923 120050505A5410 RETAINER CNDAIRCL600 CL6002C10 1390015EA ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - LEFT ENGINE PYLON ACCESS PANEL 432BB SEAL RETAINER IS CRACKED. REPAIRED IAW CRJ700 SRM 51-42-13-001-001-A01, 51-24-21-001-001-A01. 2L72 4F RTA21EA 20050607001302005060700130EA 2005 6 7 QXEA200500925 120050502A5310 DOOR FRAME CNDAIRCL600 CL6002C10 1390015EA ZONE 200 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - AFT BAGGAGE DOOR SURROUND STRUCTURE HAS GOUGE ON FORWARD FRAME, LOWER INBOARD CORNER. REPAIRED IAW CRJ700 SRM 51-25-16-001-001-A01 AND 51-21-11-001-001-A01. 2L72 4F RTA21EA 20050607001322005060700132EA 2005 6 7 QXEA200500920 120050505A5411 RIB CNDAIRCL600 CL6002C10 1390015EA ZONE 400 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - LEFT PYLON AFT ENGINE MOUNT SUPPORT RIB HAS SCRATCHES ON LOWER SIDE OF MOUNT. REPAIRED IAW HORIZON AIR EA R-54-93 AND REO 670-54-51-006. 2L72 4F RTA21EA 20050607001332005060700133EA 2005 6 7 QXEA200500916 120050428A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FUSELAGE INTERIOR LEFT SIDE SEAT RAIL HAS GOUGES, STATION 919-950. REPAIRED IAW REO 670-53-00-013. 2L72 4F RTA21EA 20050607001342005060700134EA 2005 6 7 QXEA200500917 120050428A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FUSELAGE INTERIOR RIGHT SIDE SEAT RAIL HAS CORROSION ON INSIDE SURFACE AT STATION 785. REPAIRED IAW REO 670-53-00-013. 2L72 4F RTA21EA 20050607001352005060700135EA 2005 6 7 QXEA200500918 120050503A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FUSELAGE BELLY SKIN HAS IMPACT MARKS BETWEEN STATION 202.75 AND 235.00, LEFT STRINGER 26 AND 25. REPAIRED IAW CRJ700 SRM 53-11-01-101-008-A01, 51-26-00-001-001-001-A01 AND 51-25-16-001-001-A01. 2L72 4F RTA21EA 20050607001362005060700136EA 2005 6 7 QXEA200500921 120050505A5730 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 500 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - LEFT WING LEADING EDGE PANEL FORWARD OPENING HAS RUB MARKS ON THE EDGE. REPAIRED IAW REO 670-57-41-074 AND HORIZON AIR EA R-51-118. 2L72 4F RTA21EA 20050607001392005060700139NE 2005 6 7 DL75K050284 220050520A7200 ENGINE BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 2 FAILED A DALAE ENGINE SHUTDOWN J WARNING INDICATION DEDESCENT 1 SO276714Q14947 30485 716457 CREW REPORTS RT ENG OIL FILTER STATUS MSG APPEARED DURING FLIGHT. CREW FOLLOWED QRH PROCEDURES AND MSG DID NOT CLEAR. ENGINE SHUTDOWN PER QRH. REPLACED ENGINE. 2L72 4F4 FRTA2NM E17NE 20050607001412005060700141NM 2005 6 7 DLM88050286 120050522A3260387 LAMP DOUG MD88 MD88 3023688NM MLG INDICATOR INOPERATIVE A DALAO OTHER P NO WARNING INDICATION DEDESCENT 1 SO27998DL 53370 UPON GEAR EXTENSION, RT MAIN GEAR GREEN LIGHT DID NOT ILLUMINATE. C/W LANDING GEAR UNSAFE, GEAR HANDLE DOWN QRH. VISUAL CONFIRMED. RELAMPED INDICATOR LIGHTS. 2L72 4F RTA6WE 20050607001432005060700143 2005 6 7 DL777050288 420050522A23301301273110 VIDEO UNIT BOEING777 777232 1385232NM SEAT 48 GHJ BURNED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27863DA 29735 VIDEO SYSTEM IN CNTR SECTION 45-49 DID NOT WORK PROPERLY. FLICKERING ON AND OFF RESET NO HELP. UNFAMILIAR ODOR ASSOCIATED WITH THE FLICKERING. INSPECTED FOUND AVU UNDER SEAT 48 GHJ OVERHEATING CAUSING BURNING ODOR. REPLACED AVU LOADED SOFTWARE, CHECKS OK, ODOR GONE. 2L72 4F RTT00001SE 20050607001442005060700144EA 2005 6 7 QXEA200500938 120050502A5753 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 600 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - RIGHT WING INBOARD FLAP HAS ROCK CHIPS ON LOWER FLAP INNER AREA. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01 AND 57-52-01-101-001-A01. 2L72 4F RTA21EA 20050607001462005060700146EA 2005 6 7 QXEA200500930 120050428A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - FUSELAGE INTERIOR LEFT FLOOR SEAT RAIL HAS GOUGES AT THE FOLLOWING LOCATIONS, STATION 860.5, 890-891 AND 921-722. REPAIRED IAW REO 670-53-00-013. 2L72 4F RTA21EA 20050607001472005060700147EA 2005 6 7 QXEA200500931 120050429A1430 RIVET CNDAIRCL600 CL6002C10 1390015EA ZONE 600 LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 YYC - RIGHT WING INBOARD MFS AREA, TWO LOOSE RIVETS INBOARD NEAR PIE SHAPE AREA. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01 AND SRM 51-25-16-001-001-A01. 2L72 4F RTA21EA 20050613001302005061300130 2005 6 13 0500786310 420050523A23971167840413 WIRE BOEING747 747451 1384940NM SEAT FAILED A NWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL01670US 24225 DURING FLIGHT, MAIN CABIN AUDIO AND READING LIGHTS WENT INOP. SPARKS AND SMOKE IN FIRST ROW OF COACH CLASS. HKG MAINTENANCE FOUND SEAT CABLE FROM 24HJK TO SIDEWALL BURNED AND ZONE C/D SERVICE TO C/B POPPED. JFK MAINTENANCE REMOVED AND REPLACED SEAT CABLE AND WALL CABLE. OPERATIONAL CHECKS GOOD. 2L74 4F RTA20WE 20050613001322005061300132NM 2005 6 13 CALA0500176 120050529A3234D72403001 SWITCH BOEING767 767424ER 1385270NM MLG LEVER INOPERATIVE A CALAO OTHER J WARNING INDICATION APAPPROACH 1 SW276605120005 29446 WHEN MLG WAS SELECTED TO DOWN ON APPROACH TO FCO CREW REPORTED THAT ALL WAS QUIET & NOTHING HAPPENED. ALT GEAR EXTENSION USED & CREW GOT EICAS MSG GEAR DISAGREE AND NO GREEN NLG LIGHT. ALT GEAR EXTENSION USED AGAIN DURING A GO AROUND AND 3 GREEN MLG LIGHTS WERE ILLUMINATED. A/C LANDED W/O PROBLEM. GEAR SWUNG 3 TIMES & ALL OPS CHECKED GOOD. GEAR AREA INSPECTED INCLUDING GEAR, DOORS, ALL THE STOPS, AND CONTROL MECHANISMS & NO FAULTS WERE FOUND. GEAR FULLY LUBRICATED & MLG LEVER CONTROL MODULE (SWITCH) R & R IAW MM 32-31-01 AS A PRECAUTIONARY MEASURE. MLG CONTROL SYS, ALT EXTEND SYS, & POSITION INDICATION WARNING SYS TESTED IAW MM 32-31-00, 32-35-00, AND 32-61-00 AND ALL TESTS PASSED WITH NO DEFECTS NOTED. 2L72 4F RTA1NM 20050613001342005061300134NM 2005 6 13 CALA0500178 120050531A335020131A BATTERY BOEING737 737524 1384721NM EMERGENCY LIGHT INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2752616 27329 INSPECTION FOUND THE LAST FOUR ROWS OF EMERGENCY LIGHTS INOPERATIVE. THE BATTERY PACK IN THE AFT GALLEY OVERHEAD WAS REMOVED AND REPLACED. 2L72 4F RTA16WE 20050613001352005061300135NM 2005 6 13 DHL2005741522 120050423A5315BAC1505100246 FLOORBEAM BOEING727 7272Q9 138448MNM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 BS 324 T CAP UPPER CORROSIONS. FOUND CORROSION TO BE OUT OF LIMITS AT STA 324 "T" CAP UPPER AT BLR 48 AND BLR 20 AND BLL 32 IAW B727 SRM 53-10-1 FIG 5. REMOVE STA 324 "T" CAP IAW B727 SRM 51-30-2. FABRICATED OF NEW "T" CAP DIM 128" FROM BAC1505-100242 PO NR 5096102 IAW SRM 53-10-2 FIG 7. MAT. ID TREATED AND PRIMED PART AND AREA IAW B727 SRM 51-10-2. INSTALLED NEW "T" CAP AT STA 324 IAW B727 SRM 51-30-2. 2L73 4F RTA3WE 20050613001372005061300137NM 2005 6 13 DHL2005741523 120050421A5313BAC1498143 STRINGER BOEING727 7272Q9 138448MNM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 STR 27R CORRODED AT FUSELAGE STA 686. REMOVED CORROSION FOUND TO BE OUT OF LIMITS ON STR 27R AT STA 686 IAW B727 SRM 51-10-6 AND SRM 53-10-1. CUT OUT SECTION OF STR SIZE 10 INCH IAW B727 SRM 53-10-3 FIG 1. FABRICATED STR FROM BAC1498-143 SIZE 10 INCH PO NR 5096198 AND SPLICE FROM BAC1498-132 SIZE 10 INCH PO NR 4246286 IAW B727 SRM 53-10-3 FIG 1. TREATED AND PRIMED PARTS AND AREA IAW B727 SRM 51-10-2 AND INSTALLED STR AND SPLICE IAW B727 SRM 53-10-3 FIG 1 AND 51-30-2. 2L73 4F RTA3WE 20050613001392005061300139NM 2005 6 13 MASA200500349 120050512A3350 BULB DHAV DHC8 DHC8202 2809007NM EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07989HA 427 ASH 6346 - PHX TO HMO - THE CREW REPORTED EMERGENCY LIGHTS SWITCH LIGHT INOP. MAINTENANCE REPLACED LIGHT BULBS IN SWITCHLIGHT AND OPS CHECK NORMAL. 2H72 4T RTA13NM 20050613001402005061300140SO 2005 6 13 MASA200500353 120050514A3350 CONNECTOR EMB 145 EMB145LR 3260212SO SIGN LOOSE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07831MJ 145273 ASH 2698 CLT - THE CREW HAD AN EMERGENCY EXIT SIGN ROW 12 THAT WOULD NOT ILLUMINATE. MAINTENANCE SECURED THE CONNECTOR. 2L72 4T RTT00011AT 20050613001422005061300142EA 2005 6 13 MASA200500356 120050514A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0737228 7228 ASH 6717 - LAS TO OKC - THE CREW NOTED THAT THE PASSENGER DOOR EMERGENCY EXIT LIGHT 2 OF 5 LIGHTS INOP. MAINTENANCE COMPLIED WITH THE MEL PROCEDURES AND RELAMPED THE BULB. 2L72 4F RTA21EA 20050613001432005061300143EA 2005 6 13 MASA200500359 120050515A3350CM1317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BLOWN A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0775987 7405 THE CREW NOTED THAT THE RT AFT EXTERIOR EMERGENCY LIGHT WAS INOP. MAINTENANCE RELAMPED. 2L72 4F RTA21EA 20050613001452005061300145CE 2005 6 13 DXTA200500744 120050529A3240 BRAKE CESSNA500 560CESSNA 2076750CE MLG MALFUNCTIONED E DXTAD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07312QS 5600312 BRAKE PEDALS ON THE RIGHT SIDE FEEL MUSHY GO ALL THE WAY TO THE STOPS AND GRAB. LEFT SIDE IS NORMAL. BLED BRAKES PER CE560 M/M 32-42-00. OPS CHECKED GOOD. 2L72 4F RTA22CE 20050613001472005061300147NM 2005 6 13 BB05043 120050529A3350S417N5091SMI LIGHT BOEING767 767201 1385125NM ROW 6 RIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19648US 23900 SNN - FOUND EMERGENCY LIGHT AT ROW 6 RIGHT INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. 2L72 4F RTA1NM 20050613001482005061300148EU 2005 6 13 UPS05144551 120050507A3350 LIGHT AIRBUS300 A300B4622R 3930312EU L1 DOOR INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01120UP 0805 INSPECTION TYPE:N/A SEVERAL LAMPS INOP IN EMERGENCY LIGHT ABOVE L1 DOOR. RELAMPED, CHECKS OK. 2L72 4F RTA35EU 20050613001502005061300150NM 2005 6 13 UPS05444518 120050519A5320 STIFFENER BOEING747 747123F NM NLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C RT SIDE NWW SIDE PANEL AT BS 280-300 NR 2 STIFFENER (COUNT FROM TOP) FOUND RADIUS CRACKED APPROX 1.25 INCH LONG RUNNING FROM FWD EDGE (CRACK LENGTH 1.25 INCH). STIFFENER REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050613001522005061300152NM 2005 6 13 UPS05444520 120050518A5311 FRAME BOEING747 747123F NM CARGO BAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C FWD CARGO COMPT BS 660 S37L - 38L FRAME CRACKED (CRACK LENGTH 8.25 INCH). FWD CARGO COMPT - BS 660 BETWEEN S37L AND S38L FRAME REPAIRED AS PER SRM 53-10-04 FIG 52. 2L74 4F A20WE 20050613001542005061300154NM 2005 6 13 UPS05444522 120050520A5315 FLOORBEAM BOEING747 747123F NM FUSELAGE MISDRILLED A IPXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C CABIN - U/D BS 380 FWD FLANGE OF FLOORBEAM FLOOR PANEL ATT HOLES SHORT EDGE MARGIN FOUND AT RBL 55 & 65 AREA. CABIN - U/D BS 380 FLOORBEAM FWD FLANGE RBL 55 & 65 REPAIRED AS PER UPS EO B747-5320-12407 APPENDIX D PLAN -C-. 2L74 4F A20WE 20050613001562005061300156NM 2005 6 13 UPS05444524 120050520A5315 FLOORBEAM BOEING747 747123F NM PWA JT9 JT9D7A 52054NE FUSELAGE MISDRILLED A IPXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C CABIN - U/D FLR BEAM BS 340 FWD FLANGE RBL 40 INCHES SHORT EDGE MARGIN FOUND AT CLIP NUT HOLES AREA. CABIN - U/D BS 340 FLR BEAM FWD FLANGE RBL 40 INCH AREA REPAIRED IAW EO B747-5320-12407-D PLAN C. 2L74 4F4 F A20WE E20EA 20050613001582005061300158NM 2005 6 13 UPS05444527 120050516A5315 FLOORBEAM BOEING747 747123F NM PWA JT9 JT9D3 52050NE FUSLEAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C M/D BS 1220 RBL 105 FLOORBEAM WEB FOUND CRACKED. ( 0.5 INCH) M/D - BS 1220 RBL 105 INCHES FLR BEAM WEB REPAIRED IAW SRM 51-40-02 FIG 1. 2L74 4F4 F A20WE E20EA 20050613001602005061300160NM 2005 6 13 UPS05444529 120050520A5313 STRINGER BOEING747 747123F NM PWA JT9 JT9D3 52050NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C U/D STA 640 STRINGER S-9R END CRACKED. (CRACK LENGTH .4375 INCH). U/D - BS 640 STRINGER 9R REPAIRED IAW SRM 53-10-03 FIG 2. 2L74 4F4 F A20WE E20EA 20050613001622005061300162NM 2005 6 13 UPS05444531 120050520A5313 STRINGER BOEING747 747123F NM PWA JT9 JT9D3 52050NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C U/D - LT SIDE BS 620 STR END S-9L CRACKED. ( CRACK LENGTH .4375 INCH ) U/D - LT SIDE BS 620 STR - 9L REPAIRED IAW SRM 53-10-03 FIG 2. 2L74 4F4 F A20WE E20EA 20050613001642005061300164NM 2005 6 13 UPS05444533 120050518A534065B38600346 STRINGER CLIP BOEING747 747123F NM PWA JT9 JT9D3 52050NE CARGO BAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C AFT CARGO COMPT BS 1920 S40L TIE CLIP CRACKED. (CRACK LENGTH .3750 INCH) AFT CARGO COMPT BS 1920 STR 40L TIE CLIP REPLACED AND INSTALLED IAW SRM 51-10-01 PG 9. 2L74 4F4 F A20WE E20EA 20050613001662005061300166NM 2005 6 13 UPS05444535 120050515A5330 SKIN BOEING747 747123F NM PWA JT9 JT9D7A 52054NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE: C EMP - STA 2638 BETWEEN S-7L AND S-8L EXT. SKIN CRACKED APPROX 10 INCHES ( CRACK LENGTH 10 INCHES ) EMP - BS 2638 BETWEEN S-7L & S-8L SKIN REPAIRED IAW SRM 53-30-03 FIG 1A. 2L74 4F4 F A20WE E20EA 20050613001742005061300174NM 2005 6 13 UPS05444543 120050519A5313 STRINGER BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C M/D BS 742 S-9L STRINGER END FOUND CRACKED. CRACK LENGTH 2.875 INCH. M/D BS 742 STR -9L TO BS 770 STR 9L AREA STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4. 2L74 4F A20WE 20050613001762005061300176NM 2005 6 13 UPS05444545 120050518A532065B07936297 STIFFENER BOEING747 747123F NM FWD CARGO CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C FWD CARGO COMPT BS 400 RBL 1 INCH BULKHEAD STIFFENER CRACKED BELOW MEC FLR (CRACK LENGTH .375 INCH). FWD CARGO COMPT BS 400 RBL 1 INCH BULKHEAD STIFFENER REPLACED AS PER SRM 51-10-01 PG 9, (JUST BELOW MEC FLOOR). 2L74 4F A20WE 20050613001772005061300177NM 2005 6 13 UPS05444546 120050519A5347 SEAT TRACK BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C M/D- BS 640 - 660 RBL 75 SEAT TRACK I/B FLANGE CORROSION CRACKED (CRACK LENGTH 1 INCH CORROSION CRACK). M/D BS 640-670 RBL 75 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A. 2L74 4F A20WE 20050613001792005061300179WP 2005 6 13 UPS05844549 120050524A5730576960040 DOUBLER DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE:C3 RIGHT OUTBOARD L/E INNER DOUBLER HAS 2 EA CRACKS AROUND DRAIN HOLE AT XFS 579. REMOVED CRACKED INNER DOUBLER, FABRICATED REPLACEMENT DOUBLER IAW DWG 5769600-40, AND INSTALLED IAW DC-8 SRM 51-1-20D AND 51-1-21. 2L74 4F RT4A25 20050613001812005061300181WP 2005 6 13 UPS05844559 120050528A2910 CASE DOUG DC8 DC873F 302199FWP HYD SYSTEM LEAKING A IPXAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 SO01880UP 46080 INSPECTION TYPE:N/A EMERGENCY DECLARED, NR 3 ENGINE HYDRAULIC CASE DRAIN FILTER DUE INSPECTION DUE TO LOSS OF HYDRAULIC PRESSURE. LANDED UNEVENTFUL AND TOWED TO RAMP TWO. REMOVED AND REPLACED NR 3 ENGINE HYDRAULIC CASE DRAIN FILTER IAW MM 29-1 0-15-2, FILTER WAS CLEAN, LEAK CHECK DUE. LEAK CHECK OF NR 3 ENG HYDRAULIC CASE DRAIN FILTER OK IAW MM 29-10-00. 2L74 4F RT4A25 20050613001832005061300183NM 2005 6 13 P5CA0501351 120050518A5414 SKIN BOEING747 747230B 1384889NM NR 2 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 EA15508MC 21644 NR 2, 3 AND 4 PYLON PRECOOLER CUTOUT CRACKED AT AFT LOWER CORNER. ACCOMPLISHED REPAIR PER BOEING INSTRUCTIONS 1-1I08HV AND FAA FORM 8100-3. 2L74 4F A20WE 20050613001852005061300185NM 2005 6 13 P5CA0501353 120050518A5512 SKIN BOEING747 747230B 1384889NM DORSAL FIN DEFORMED A P5CAK NONE O OTHER ININSP/MAINT 1 EA15508MC 000336 21644 DORSAL FIN FOUND WITH DEFECTS DEFORMED AT TOP EDGE. ACCOMPLISHED REPAIR PER BOEING INSTRUCTIONS 1-1I9VRK AND FAA FORM 8100-3. 2L74 4F A20WE 20050613001872005061300187NM 2005 6 13 P5CA0501355 120050518A5414 SKIN BOEING747 747230B 1384889NM NR 4 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 EA15508MC 21644 NR 4 PYLON INBOARD ACCESS PANEL CUTOUT AT NAC STATION 275-295 CRACKED AT EDGE. ACCOMPLISHED REPAIR PER BOEING INSTRUCTIONS 1-1HGUJB AND FAA FORM 8100-3. 2L74 4F A20WE 20050613001892005061300189NM 2005 6 13 AWXA200500617 120050504A143069736971 BOLT BOEING737 7373G7 1384595NM HORIZONTAL STAB CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28322AW 25400 MCN - FLIGHT CONTROL - DURING C-14 CHECK, CORROSION WAS FOUND ON RT HORIZONTAL STABILIZER, FWD UPPER SPAR TO CENTER ATTACH BOLT. NO CORROSION REMOVAL LIMITS WERE AVAILABLE FOR THE BOLT. MAINTENANCE REMOVED AND REPLACED THE RT HORIZONTAL STABILIZER, FWD UPPER SPAR TO CENTER ATTACH BOLT IAW AMERICA WEST AIRLINES TASK CARD NR I6C55038. 2L72 4F RTA16WE 20050614000082005061400008EU 2005 6 14 AWXA200500636 120050506A5340D53112198201 FITTING AIRBUS320 A320232 3930326EU SILL CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28639AW 471 SAL - MAJOR REPAIR - DURING C08 CHECK, GALVANIC CORROSION WAS FOUND AT LOWER SILL R1 DOOR -Y1732 BETWEEN FS 16 AND FS 20. MAINTENANCE REMOVED AND REPLACED THE CORRODED FITTING AT LOWER SILL R1 DOOR -Y1732 BETWEEN FS 16 AND FS 20 IAW A320 SRM 51-72-11AND DRAWING D53112198. 2L72 4F RTA28NM 20050614000092005061400009EU 2005 6 14 AWXA200500637 120050506A5310D534711242000 SHEAR PLATE AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28639AW 471 DURING C08 CHECK, GALVANIC CORROSION WAS FOUND AT SHEAR PLATE -Y1300 BETWEEN FS 69 TO FS 70. MAINTENANCE REMOVED AND REPLACED SHEAR PLATE -Y1300 BETWEEN FS 69 TO FS 70 IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050614000232005061400023EA 2005 6 14 VTZA200500093 120050529A5320301R311719 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27660BR 7519 INTERCOSTAL CRACKED AT .250 INCH IN LENGTH ON RT INBOARD SIDE AT FS 484 AT BL 27.00. 2L72 4F RTA21EA 20050614000272005061400027EU 2005 6 14 YENA200533 120050524A2510TAAI303CE0001 SEAT AIRBUS320 A320232 3930326EU CO PILOT UNSERVICEABLE A YENAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15563JB8556 2006 APPROXIMATELY ONE HOUR INTO FLIGHT, AN ELECTRICAL OR METAL SMELL BECAME INCREASINGLY NOTICEABLE IN COCKPIT, ESPECIALLY ON F/O SIDE. THEN SEEMED TO COME AND GO. PERFORMED TSM TASK 24-00-00-810-823. FOUND F/O'S SEAT ASSY IS CAUSE OF SMELL. REPLACED F/O SEAT REF AMM 25-11-51. 2L72 4F RTA28NM 20050614000302005061400030SO 2005 6 14 C2XA05CL042 120050527A32608005701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212SO MLG LOOSE A C2XAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW2715910 145455 CLE FLIGHT 2722 CREW REPORTED, RECEIVED AN AIR/GROUND FAIL MESSAGE ON EICAS AFTER TAKEOFF. RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND RESECURED THE CONNECTORS ON THE AIR/GROUND PROXIMITY SWITCHES. ALL OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20050614000332005061400033NM 2005 6 14 05FDEA00693 120050329A5347AEA732515 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 MAIN DECK, ALONG STA 1341 TO STA 1365 RBL 75.25 SEAT TRACK FOUND CORRODED. MAIN DECK STA 1341 TO 1365 RBL 75.25 CORROSION SEAT TRACK REPAIRED AS PER SRM 53-70-00 FIG 1 VOL I. REPAIR SEAT TRACK PART FABRICATED AS PER SRM 53-70-00 FIG 1 VOL I. CLASSIFIED MAJOR REPAIR GMM 6-2-100. 2L73 4F RTA22WE 20050614000422005061400042NM 2005 6 14 AALA20050365 120050529A3350D71702001 BATTERY PACK BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21374AA 25201 DFW - SEAT MOUNTED EMERGENCY LIGHTS FROM ROW 23 RIGHT SIDE TO ROW 34 RIGHT SIDE INOPERATIVE. REPLACED BATTERY PACK M1209 FOR EMERGENCY LIGHTS AT ROW 23 RIGHT HAND TO ROW 34 RIGHT HAND. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050614000442005061400044WP 2005 6 14 AALA20050369 120050530A33506011779 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21589AA 53252 SFO - LEFT AND RIGHT HAND OVERWING EMERGENCY DOOR EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR LEFT AND RIGHT OVERWING EMERGENCY DOOR EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050614000632005061400063EA 2005 6 14 SWIA200515070 120050519A2797 WIRE CNDAIRCL600 CL6002B19 1900309EA TE FLAPS DAMAGED A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07442SW 7609 FLAP DEGRADED STATUS MESSAGE. REPLACED R4 SKEW SENSOR IAW 27-51-15. REPAIRED WIRE CONNECTOR AT R4 SKEW SENSOR IAW 27-51-10. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050614000692005061400069SO 2005 6 14 SWIA200515076 120050527A3350 SIGN EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07561SW 120335 LOWER LEFT EXIT EMERGENCY LIGHT 6C BROKEN. REPLACED EMERGENCY EXIT SIGN ASSY AT 6C. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050614000712005061400071SO 2005 6 14 SWIA200515078 120050529A2121EVAC523C2 GASPER FAN EMB 120 EMB120ER 3260203SO CABIN INOPERATIVE A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 NM07299SW101967487 120329 SMELLED SMOKE IN THE CABIN RIGHT BEFORE LANDING. REPLACED GASPER FAN. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050614000742005061400074EA 2005 6 14 SWIA200515081 120050525A27604916405 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07431SW9990 9990 7536 ON TAXI OUT THE LEFT SPOILERON RAN AWAY TO THE FULL UP POSITION. REPLACED NR 1 AND NR 2 SECU'S IAW MM 27-61-04. OPERATIONAL CHECK GOOD. P/N 49-164-06, S/N OFF 1052. 2L72 4F RTA21EA 20050614000782005061400078 2005 6 14 QXEA200500958 420050528A3400 UNKNOWN DHAV DHC8 DHC8202 2809007NM INSTRUMENT PANELMULTIPLE FAIL A QXEAA UNSCHED LANDING G MULTIPLE FAILURE CLCLIMB 1 NM09354PH 498 PDX - ON FLIGHT 2139 CAPTAIN'S ADI FAILED, AHRS INVALID MESSAGE, WEATHER RADAR INOP, AND COMM RADIOS P-STATIC. AIRCRAFT RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE PERFORMED OPERATIONAL AND FUNCTIONAL CHECKS OF THE COMM SYSTEM, THE AHRS SYSTEM, AND THE WEATHER RADAR SYSTEMS. ALL CHECKS GOOD. ALSO A LIGHTNING STRIKE INSPECTION WAS PERFORMED WITH NO DEFECTS NOTED AND NO EVIDENCE OF LIGHTNING STRIKE. NO PARTS REPLACED AND AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050614000792005061400079NM 2005 6 14 QXEA200500957 120050531A5230 HANDLE BOMBDRDHC8 DHC8402 1390042NM CARGO DOOR UNSECURE A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09414QX 4061 YEG - ON FLIGHT 2315 THE AFT BAGGAGE DOOR CAUTION ILLUMINATED. PRESSURIZATION LOST AT 6,000 FEET. AIRCRAFT RETURNED TO FIELD AND ACCOMPLISHED AN UNEVENTFUL LANDING. MAINTENANCE FOUND THE HANDLE NOT STOWED. INSPECTED DOOR AND OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2H72 4T RTA13NM 20050614001552005061400155NM 2005 6 14 SWAA051621 120050601A53116516301 FRAME BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 188, RIGHT SIDE, WL 208. REPAIRED STUB FRAME PER SRM. 2L72 4F RTA16WE 20050614001602005061400160NM 2005 6 14 SWAA051614 120050601A53306545777 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29360SW 26571 DURING SCHEDULED C3 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS AT L2 DOOR UPPER HINGE CUTOUT & 1 EA AT L2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050614001622005061400162NM 2005 6 14 SWAA051616 120050601A53306545775 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29506SW 24183 DURING SCHEDULED SERVICE CHECK, FOUND 4 EA FUSELAGE SKIN CRACKS AT BS 749, STR 18L, BS 772, STR 18L, BS 780, STR 17L & BS 784, STR 18L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050615001382005061500138SO 2005 6 15 SIMA200515201 120050529A533012301825005 SKIN EMB 145 EMB145LR 3260212SO FUSELAGE BIRD STRIKE A SIMAK NONE O OTHER ININSP/MAINT 1 SW21673AE 145797 SAW - DURING A BIRDSTRIKE, MAINTENANCE FOUND DAMAGE/DENT TO FUSELAGE SKIN BETWEEN STRINGERS 01L AND 04L AND FRAMES 11 AND 13 OVER COCKPIT LEFT SIDE FROM BIRDSTRIKE. REMOVED AND INSTALLED NEW UPPER SKIN IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20050615001402005061500140NE 2005 6 15 AT0500017 220050522A7320 ENGINE BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE NR 1 FAILED A ZZDAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 SO15969AT 55030 13143 AT FL 290, ENGINE LT SURGE APPEARED ON EAD. LOST OIL PRESSURE ON LEFT ENGINE; LOUD BANG PRECEEDED THESE TWO ALERTS FOLLOWED QRH PROCEDURES AND SHUT DOWN ENGINE. REMOVED AND REPLACED NR 11 ENGINE REF TASK CARD 603, OPS CHECK GOOD OK FOR SERVICE. 2L72 4F4 FTRA6WE E00061EN 20050615001422005061500142SO 2005 6 15 SIMA200515103 120050519A531014521713005 BEAM EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21709GB 145211 ABI - DURING AN MBV INSPECTION, THE GALLEY CENTER BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. REMOVED THE CORRODED CENTER BEAM. INSTALLED NEW BEAM IAW EMB SRM (SRM-145/1142 REV 29) CHAPTER 51-40-02. (M) 2L72 4F RTT00011AT 20050615001452005061500145NM 2005 6 15 USAA050563 120050429A5330 SKIN BOEING737 7374B7 1384702NM FUSELAGE DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US 24781 CLT - 18.5 INCH BY 10.375 INCH EXTERNAL DOUBLER INSTALLED, BETWEEN RBS 739 RBS 760 AND BETWEEN S24R AND S25R. REPAIR PCW IAW SRM 53-00-01. REPAIR PCW IAW SRM 53-00-01. (M) 2L72 4F RTA16WE 20050615001472005061500147NM 2005 6 15 SWAA051665 120050605A53306545768 SKIN BOEING737 7373H4 1384600NM R1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29357SW 26594 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050615001492005061500149NM 2005 6 15 SWAA051667 120050605A53306545767 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 443, STR 16R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050615001512005061500151NM 2005 6 15 SWAA051591 120050530A55536547450 LUG BOEING737 737301 1384611NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND LT & RT VERTICAL STAB FITTING FWD & AFT PRIMARY CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER. 2L72 4F RTA16WE 20050615001532005061500153NM 2005 6 15 SWAA051593 120050530A53126546568 BULKHEAD BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND FUSELAGE BS 1016 PRESS BULKHEAD DOME WEB CRACKED AT BL 0, WL 249. REPAIRED WEB PER BFG ER. 2L72 4F RTA16WE 20050615001552005061500155NM 2005 6 15 SWAA051596 120050529A53306545765 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 DURING SCHEDULED SERVICE CHECK, FOUND 3 EA FUSELAGE SKIN CRACKS AT BS 500C + 5, STR 15R, BS 500D + 3, STR 16R & BS 520, STR 16R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050615001572005061500157NM 2005 6 15 SWAA051598 120050529A53306545775 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 DURING SCHEDULED SERVICE CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS AT BS 750 TO BS 752, STR 21L & STR 24L. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050615001592005061500159 2005 6 15 SWAA051600 420050527A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29723SW 27855 DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050615001612005061500161NM 2005 6 15 SWAA051595 120050529A27100327119001 ACTUATOR BOEING737 7377H4 1384404NM MLG WW FAULTY A SWAAD RETURN TO BLOCK O OTHER UKUNKNOWN 1 SW29742SW 29278 AIR TURNBACK/DECLARED EMERGENCY. AILERONS FEEL UNRESPONSIVE WITH A NOTICEABLE DEAD BAND. REMOVED AND REPLACED AILERON TRIM ACTUATOR PER MM. 2L72 4F RTA16WE 20050616000102005061600010CE 2005 6 16 ENHA0507 120050127A242010300BR ALTERNATOR CESSNA207 T207A 2073614CE ENGINE FAILED E ENHAO OTHER O OTHER NRNOT REPORTED 1 AL038NZ 491 20700421 REMOVED DUE TO CB POPPING FREQUENTLY. 1H71 3O A16CE 20050616000112005061600011CE 2005 6 16 ENHA0508 120050120A242010300BR ALTERNATOR CESSNA207 207A 2073604CE FUSELAGE INOPERATIVE E ENHAO OTHER O OTHER NRNOT REPORTED 1 AL039973M 520 20700771 ALTERNATOR INOPERATIVE. 1H71 3O A16CE 20050616000152005061600015CE 2005 6 16 ENHA0512 120050427A242010300JR ALTERNATOR CESSNA207 207 2073602CE ENGINE DAMAGED E ENHAO OTHER O OTHER NRNOT REPORTED 1 AL03207VA 368 20700291 ALTERNATOR FAILED, LOOSE CONNECTION AT OUTPUT TERMINAL CAUSED BY HEAVY ARCING. 1H71 3O A16CE 20050616000172005061600017CE 2005 6 16 ENHA0514 120050423A242010300BR ALTERNATOR CESSNA207 207A 2073604CE ENGIEN INOPERATIVE E ENHAO OTHER O OTHER NRNOT REPORTED 1 AL039874M 83 20700745 ALTERNATOR INOPERATIVE. 1H71 3O A16CE 20050616000292005061600029NM 2005 6 16 SWAA051655 120050603A5753 SKIN BOEING737 7373H4 1384600NM LT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29395SW 2312 27689 DURING SCHEDULED C4 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM. 2L72 4F RTA16WE 20050616000372005061600037NM 2005 6 16 SWAA051676 120050607A3260654482517 ACTUATOR BOEING737 7373H4 1384600NM RT MLG WW FAULTY A SWAAO OTHER J WARNING INDICATION DEDESCENT 1 SW29348SW 24375 UPON NORMAL GEAR EXTENSION, RT MAIN GEAR DID NOT INDICATE EXTENDED, RED LIGHT ILLUMINATED. MANUALLY EXTENDED RT MAIN GEAR, NORMAL INDICATIONS, GREEN LIGHT ILLUMINATED. REMOVED AND REPLACED UPLOCK ACTUATOR PER MM. 2L72 4F RTA16WE 20050616000512005061600051NM 2005 6 16 SWAA051695 120050608A3350D71702001 BATTERY PACK BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29703SW 27837 DURING SCHEDULED MV2 CHECK, FOUND CABIN EMERGENCY EXIT LIGHTS INOPERATIVE AT ROWS 10 ABC TO ROWS 23 ABC. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050616000532005061600053NM 2005 6 16 SWAA051687 120050608A5310BAC15171489 FLOOR SUPPORT BOEING737 7373H4 1384600NM COCKPIT FLOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND COCKPIT FLOOR ZEE FITTING CORRODED AT BS 270, RBL 11 TO LBL 11, WL 208. REPAIRED ZEE FITTING PER SRM. 2L72 4F RTA16WE 20050616000542005061600054NM 2005 6 16 SWAA051688 120050608A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER BFG ER. 2L72 4F RTA16WE 20050616000552005061600055NM 2005 6 16 SWAA051689 120050608A335090083 BATTERY PACK BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29349SW 24408 DURING SCHEDULED RON CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050616000572005061600057EU 2005 6 16 AWXA200500642 120050506A5320D53113322200 WEB AIRBUS320 A320232 3930326EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28639AW 471 SAL - MAJOR REPAIR - DURING C-8 CHECK, A 5/8 INCH CRACK WAS FOUND IN WEB AT FR 11 AND FLOOR STR Y770. MAINTENANCE REMOVED CRACKED WEB FROM FS 8 TO FS 11. FABRICATED A NEW REPLACEMENT WEB PER DRAWING D53113322, INSTALLED REPAIR PART IAW A320 SRM 51-42-11. 2L72 4F RTA28NM 20050616000582005061600058NM 2005 6 16 SWAA051691 120050608A5753 SKIN BOEING737 7373H4 1384600NM RT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29370SW BN603 26597 DURING SCHEDULED C2 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM. 2L72 4F RTA16WE 20050616000592005061600059EU 2005 6 16 AWXA200500643 120050504A5315D53230465201 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28639AW 471 SAL - MAJOR REPAIR - DURING C-8 CHECK A 3/8 INCH CRACK WAS FOUND IN FLOORBEAM UPPER FLANGE -Y254 AT FR 27 + 19". MAINTENANCE CUTOUT CRACK IN FLOORBEAM -Y254 BETWEEN FS 27 AND FS 28. FABRICATED A FILLER AND REPAIR ANGLE AND INSTALLED REPAIR PART IAW 53-21-11 FIG 201. 2L72 4F RTA28NM 20050616000602005061600060NM 2005 6 16 SWAA051692 120050608A5753 SKIN BOEING737 7373H4 1384600NM LT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29370SW 999 26597 DURING SCHEDULED C2 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM. 2L72 4F RTA16WE 20050616000612005061600061 2005 6 16 SWAA051579 420050527A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29202WN 33999 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050616000622005061600062NM 2005 6 16 SWAA051580 120050527A531169353656 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE BELT FRAME CRACKED AT BS 400, STR 18R. REPAIRED BELT FRAME PER SWA EA & SRM. 2L72 4F RTA16WE 20050616000632005061600063NM 2005 6 16 SWAA051581 120050527A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING WALK AROUND INSP, FOUND FUSELAGE SKIN CRACKED AT BS 480 TO BS 500, STR 16L. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050616000642005061600064NM 2005 6 16 AWXA200500644 120050601A3260 WARNING SYSTEM BOEING737 7373S3 1384711NM COCKPIT MALFUNCTIONED A AWXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP28312AW 24060 AFTER T/O & EN ROUTE, RECEIVED RT MLG RED & GREEN LIGHT INDICATION. ON APPROACH, AFTER LOWERING GEAR ALL THREE LIGHTS INDICATED GREEN. AFTER LANDING MX PINNED GEAR FOR TAXI TO GATE. MX CYCLED GEAR 5 TIMES COULD NOT DUPLICATE PROBLEM. AS A PRECAUTION REPLACED RT MLG HYD MODULE IAW BMM 32-32-61. ALSO REPLACED TRANSFER CYLINDER IAW BMM 32-32-71. OPERATIONAL CHECK GOOD. RECEIVED TEAR DOWN REPORTS FOR HYDRAULIC MODULE & TRANSFER CYLINDER. THE MLG HYDRAULIC MODULE WAS INSPECTED, TEST & OVERHAULED IAW CMM NO FAULTS WERE FOUND. HYDRAULIC TRANSFER CYLINDER INSPECTED, TESTED, AND OVERHAULED IAW CMM 32-40-01 REV. 20, NO FAULTS WERE FOUND ON THIS UNIT EITHER. 2L72 4F RTA16WE 20050616000672005061600067NM 2005 6 16 SWAA051583 120050527A53226546529 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 500A, STR 15L TO STR 16L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050616000712005061600071NM 2005 6 16 AWXA200500648 120050601A3610 CONTROLLER AIRBUSA319 A319132 3930340NM BLEED AIR SYS MALFUNCTIONED A AWXAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 WP28826AW 1534 ON CLIMB-OUT, BOTH NR 1 AND NR 2 ENGINE BLEED AIR FAULTS OCCURRED. TURNED BACK AND LANDED WITHOUT FURTHER DIFFICULTY. MX R & R NR 1 BMC IAW AIRBUS MM 36-11-34. ALSO REPLACED FAN AIR VALVE CONTROL THERMOSTATS ON BOTH NR 1 AND NR 2 ENGINES IAW AIRBUS MM 36-11-43. OPS CHECKS WERE GOOD. TEMP CONTROL THERMOSTAT, FAULT CONFIRMED REASON FOR RETURN JUSTIFIED. UNIT HAD SEVERAL COMPONENTS REPLACED. UNIT REPAIRED & RECERTIFIED IAW CMM. THERMOSTAT, CONFIRMED FAILURE. PRESSURE REDUCER OUT OF SEATING AND STICK S/A WORN. REPLACED STICK & SEAT S/A. ALL WORK PERFORMED IAW CMM. COMPUTER, BLEED MON, UNIT PRE-TESTED & PASSED ALL FUNCITIONAL TESTS. NO FAULTS FOUND, UNIT TESTED IAW CMM. 2L72 4F RTA28NM 20050616000732005061600073NM 2005 6 16 05FDEA01499 120050531A54101538M8G21 CASE DOUG MD11 MD11 3023602NM ZONE 400 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 NR 2 ENGINE, LT FAN CASE APPROXIMATELY 7 - 8 O' CLOCK POSITION, FOUND CRACKED PROPAGATED THRU STOP DRILL HOLE AT AFT CRADLE MOUNT FLANGE. REPAIRED PER AMM 72-33-00-300-801. 2L73 4F RTA22WE 20050616000742005061600074NM 2005 6 16 AWXA200500650 120050522A575465C2660297SP WEDGE BOEING737 737301 1384611NM NR 2 SLAT DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 DURING C-19 CHECK, NR 2 SLAT WEDGE WAS FOUND TO BE DISBONDED ON TOP AND BOTTOM AT SLAT STATION 168. MAINTENANCE REMOVED DISBONDED SKIN AND CORE FROM TOP AND BOTTOM OF SLAT WEDGE. FABRICATED REPAIR CORE AND DOUBLER. BONDED REPAIR PIECES TO NR 2 SLAT WEDGE IAW BOEING 737-300 SRM 51-70-10-0 REPAIR 7 FIGURE 16. 2L72 4F RTA16WE 20050616000762005061600076NM 2005 6 16 AWXA200500652 120050522A575465C26602107SN SKIN BOEING737 737301 1384611NM L/E SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-19 CHECK, 4 CRACKS EACH .3 INCH IN LENGTH FOUND ON BOTTOM OF NR 2 SLAT SKIN BELOW OUTBOARD MAIN TRACK AT SLAT STATION 228 TO SLAT STATION 232. MAINTENANCE CUT OUT AND REMOVED CRACKED SECTION OF NR 2 SLAT SKIN. FABRICATED FILLER AND SPLICE PLATE. INSTALLED FABRICATED REPAIR PARTS IAW BOEING 737-300 SRM 51-40-02-0 FIG 8. 2L72 4F RTA16WE 20050616000772005061600077EU 2005 6 16 AWXA200500653 120050604A2932501310000 PRESSURE SWITCH AIRBUS320 A320231 3930325EU NR 2 ENGINE FAULTY A AWXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP28620AW 052 ATL - AIR TURN BACK - FLT 617 - ON CLIMB-OUT FROM ATL EN ROUTE TO PHX RECEIVED YELLOW ENGINE DRIVEN HYDRAULIC PUMP LOW PRESSURE INDICATION, TURNED BACK TO ATL FOR REPAIR. MAINTENANCE FOUND YELLOW HYDRAULIC RESERVOIR OVER SERVICED, SERVICED CORRECTLY IAW TASK CARD S2C29311. CHECKED CASE DRAIN FILTER, FOUND CLEAN. REMOVED AND REPLACED NR 2 ENG HYDRAULIC PRESSURE SWITCH IAW AMM 29-13-17-000-10, ENGINE RUN OPERATIONAL CHECKS GOOD. 2L72 4F RTA28NM 20050616000792005061600079 2005 6 16 05FDEA01509 420050602A3418 SENSOR BOEING727 727200 138407ENM AOA MALFUNCTIONED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25213FE 22935 ON DEPARTURE AT APPROX 1000 FT AGL CALLED FOR QUIET EPP, FLAPS 5 DEGREES, STICK SHAKER INITIATED AT FLAPS 15 DEGREES, SPEED 160 KIAS, APPEARED TO ACTIVATE 15 KTS ABOVE MMS DURING CLIMBOUT. VIBRATED ONCE AT 8 - 10 KTS ABOVE BUG SPEED AT FLAPS 30 DEGREES, GEAR DOWN THEN WORKED WELL AT BUG 5 - 10 KTS. REMOVED & REPLACED AOA SENSOR IAW MM 34-18-051. OP'S CHECK GOOD IAW MM 34-18-001. 2L73 4F RTA3WE 20050616000812005061600081NM 2005 6 16 AWXA200500656 120050605A335015AT48 SWITCH BOEING737 7373G7 1384595NM CABIN FAULTY A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 PHX - EEL - FLT 763 - FLIGHT CREW FOUND EMERGENCY EXIT LIGHTS ON, UNABLE TO TURN OFF. MAINTENANCE RAN WIRES AND FOUND COCKPIT SWITCH TO BE BAD. REMOVED AND REPLACED SWITCH S7 IAW BOEING SWPM 20-00-10. ALSO, USED WDM FIGURES 33-51-21 AND WDM 33-51-11. LIGHTS OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050616000832005061600083EU 2005 6 16 AWXA200500658 120050604A2560P4010021 BATTERY AIRBUS320 A320232 3930326EU FLASHLIGHT DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28655AW 1075 PHX - EMERGENCY EQUIPMENT - FLT 98 - DURING TURN TO SEA, FOUND 2 AFT FLASHLIGHTS BATTERIES LOW. REMOVED AND REPLACED BATTERIES IN EACH AFT CABIN FLASHLIGHTS. OPERATIONAL CHECK GOOD. 2L72 4F RTA28NM 20050616000852005061600085NM 2005 6 16 AWXA200500660 120050521A53206545834551 CHANNEL BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 DURING C-19 CHECK, FOUND ONE CRACK 1.1 INCH LONG ON CHANNEL LOCATED AT BS 328, LEFT BL 54, WL 208. MAINTENANCE REMOVED CRACKED CHANNEL AT BS 328, LEFT BL 54, WL 208. FABRICATED AND INSTALLED NEW CHANNEL AT BS 328, LEFT BL 54, WL 208 IAW BOEING DWG 65-45834 AND B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050616000882005061600088NM 2005 6 16 AWXA200500662 120050606A5330654577467 SKIN BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 AFT FUSELAGE FROM BS 727E TO BS 747 JUST ABOVE STRINGER 22L A 1.0 INCH SKIN CRACK WAS FOUND. MAINTENANCE REMOVED DAMAGE AREA AND OLD DOUBLER. FABRICATED REPAIR DOUBLER TRIPLER AND NEW INTERNAL LIGHT RING DOUBLER. INSTALLED FABRICATED REPAIR PARTS IAW AMERICA WEST AIRLINES ENGINEERING REQUEST 03-5330-05157-SS1. REPAIR WAS PLACED ON MONITOR, CONTROL NR 250650, AND WILL BE INSPECT AT 60,000 FLT CYCLES AFTER REPAIR INSTALLATION. 2L72 4F RTA16WE 20050616000902005061600090NM 2005 6 16 05FDEA01514 120050602A5753ARC1984502 SUPPORT BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) OUTBOARD CENTER AND AFT BOLT HOLES FOUND CORRODED DURING ACCOMPLISHMENT OF EA 1-5750-83126. REMOVED AND REPAIRED PER FEDEX EA 1-5750-86625. 2L73 4F RTA22WE 20050616000912005061600091NM 2005 6 16 AWXA200500664 120050606A3350321454 EPSU AIRBUSA319 A319132 3930340NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28823AW460999555 1463 PHX - EEL - DURING 8 DAY CHECK, FOUND CABIN EMERGENCY EXIT LIGHTS INOP IN THE FWD CABIN AREA. MAINTENANCE REMOVED AND REPLACED THE FORWARD LEFT EMERGENCY SUPPLY POWER UNIT IAW AIRBUS MAINTENANCE MANUAL 33-51-38. OPERATION CHECK WAS GOOD. 2L72 4F RTA28NM 20050616000922005061600092NM 2005 6 16 05FDEA01510 120050602A3230 ACTUATOR BOEING727 727200 138407ENM NLG UPLOCK MALFUNCTIONED A FDEAO OTHER J WARNING INDICATION LDLANDING 1 SO25265FE 21671 ON GEAR EXTENSION FROM OFF POSITION TO DOWN, NLG DID NOT UNLOCK (OR GO GREEN), RECYCLED GEAR HANDLE TO UP, LIGHTS OUT, GEAR HANDLE DOWN, 3 GREEN LIGHTS. REPLACED NOSE GEAR LOCK ACTUATOR IN REFERENCE TO 727-200 AMM 32-33-011-4, OPERATION AND LEAK CHECKED GOOD AT THIS TIME. 2L73 4F RTA3WE 20050616000932005061600093NM 2005 6 16 AWXA200500665 120050529A57536546435277 SKIN BOEING737 73733A 1384673NM T/E FLAP DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW669 669 23632 DURING C-21 CHECK, FOUND DISBONDED AREA ON LOWER SURFACE OF LT OUTBOARD AFT FLAP, 94 INCHES FROM INBOARD END. MAINTENANCE REMOVED AND CLEANED OUT DAMAGED AREA ON LOWER SURFACE OF LT OUTBOARD AFT FLAP. FABRICATED DOUBLER AND INSTALLED FABRICATED REPAIR PARTS IAW BOEING 737-300 SRM 51-70-10 FIGURE 30. 2L72 4F RTA16WE 20050616000942005061600094NM 2005 6 16 AWXA200500668 120050607A33501012621 SIGN BOEING737 737301 1384611NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28324AW 23261 PHX - EEL - DURING 4 DAY CHECK, FOUND EMERGENCY EXIT SIGN AT FOWARD LOWER CORNER OF L1 DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LIGHT ASSEMBLY, OPS CK GOOD . 2L72 4F RTA16WE 20050616000982005061600098NM 2005 6 16 2005UALA00486 120050527A5311 FRAME BOEING737 737322 1384676NM CFMINTCFM56 CFM562AFR 13802EU FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29313UA 23674 CABIN OVERWING BS 616 LT SIDE FRAME WEB INNER CHORD IS CRACKED THROUGH FIRST FASTENER APPROX 7 INCHES BELOW FLOOR. REPAIRED WEB AT BS 616 LT PER MM 53-11-81 AND REPAIRED FRAME INNER CHORD PER MM 53-11-89. MANUFACTURED ANGLE AND WEB AND INSTALLED. 2L72 4F4 FRTA16WE E21EU 20050616001042005061600104NM 2005 6 16 2005UALA00489 120050527A2530 COFFEEMAKER BOEING777 777222 1385219NM PWA PW4077PW4077 NE GALLEY SPARKS A UALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP29212UA 30218 COFFEEMAKER ELECTRICAL SPARKING. REPEATED ARCING NEAR MID GALLEY COFFEEMAKER PWRD OFF GALLEY & LTS. CONVERSATION WITH PURSER DESCRIBES 2 INSTANCES OF FLASH FROM BELOW COUNTERTOP AFTER POWERING OFF GALLEY. EXAMINATION OF AIRCRAFT GALLEY WIRING & COFFEEMAKERS REVEALS NO SIGNS OF ARCING. ALL DEVICES WERE OPERATED IN EXCESS OF 30 MINUTES WITH NO ANOMALIES NOTED. 2L72 4F4 FRTT0001SE E46NE 20050616001092005061600109 2005 6 16 2005UALA00491 420050526A2565B14056904 O-RING AIRCRUISERS BOEING757 757222 1384956NM PWA 2037 PW2037 NE ESCAPE SLIDE LEAKING A UALAK NONE O OTHER ININSP/MAINT 1 WP29578UA 0856 26694 NEEDLE IN RED (LOW). PRESSURE GAGE FITTING LEAKING. REPLACED O-RING. 2L72 4F4 FRTA2NM E17NE 20050616001112005061600111NM 2005 6 16 2005UALA00493 120050601A5330 SKIN BOEING737 737522 138449FNM GE CFM56 CFM563US 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29914UA 25381 SKIN DAMAGE AT FS 482, APPROX 2.5 FT AFT OF FORWARD CARGO DOOR, IN LINE WITH LOWER CUTOUT OF DOOR. UPPER DENT IS A=1.5 IN AND Y=0.093 IN. LOWER DENT IS A=1.0 IN AND Y=0.062 IN. DAMAGE AREAS ARE 2.5 INCHES APART. MAJOR REPAIR ACP'D PER SRM 53-00-01 FIGURE 229, DETAIL XIX, DOUBLER TRIPLER REPAIR 18 X 27 INCHES USED. 2L72 4F4 FRTA16WE E2GL 20050616001122005061600112NM 2005 6 16 2005UALA00494 120050601A5310 CREASE BEAM BOEING737 737522 138449FNM GE CFM56 CFM563B1 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29910UA 25254 CREASE BEAM AT DOOR 2R HAS CORROSION. REPLACED CREASE BEAM PER SRM 53-60-15 AND BOEING DRAWING 65-45855. 2L72 4F4 FRTA16WE E2GL 20050616001132005061600113NM 2005 6 16 05FDEA01518 120050606A5510 BEAM BOEING727 727227 1384078NM HORZIONTAL STAB DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 RT HORIZ STAB, LOWER TRAILING EDGE BEAM DAMAGED WITH LOOSE FASTENERS AT I/B RUB PLATE. REPAIRED IAW FED EX EA 7-5510-86315. 2L73 4F A3WE 20050616001142005061600114NM 2005 6 16 05FDEA00655 120050328A5320AFA7181511 SPLICE DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 CABIN STA 1661 TO 1681 LONGITUDINAL SPLICE AT L26 RIGHT FOUND 7 INCHES CRACKED AS MARKED. LONGITUDINAL SPLICE AT STA 1661 TO 1681 RIGHT L-26 REMOVED. NEW SPLICE FABRICATED FROM 1D0755T7150T6511 AS PER DRAWING AFA7181 AND CARRIED OUT FPI INSPECTION AS PER DPS 4.707 AND FOUND NO CRACK EVIDENT. FABRICATED SPLICE REPROTECTED AND PART MARK AFA7181-511 AS PER GMM 7-0-1001. FABRICATED SPLICE LOCATED AND INSTALLED BETWEEN STA 1661 TO 1681 RIGHT L-26 AS PER DRAWING NFA6310. CLASSIFIED MAJOR REPAIR AS PER GMM 6-2-100 AND SRM 51-90-01 FIG 1 VOL II. 2L73 4F RTA22WE 20050616001162005061600116NM 2005 6 16 05FDEA00675 120050328A5347AFA7795509 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 MAIN DECK, ALONG STA 1817 TO STA 1887 LBL 27.5 SEAT TRACK FOUND CORRODED. CORROSION ALONG STA 1817 TO 1887 LBL 27.5 REMOVED & FOUND EXCEED LIMIT AS PER SRM 53-70-00 FIG 3 VOL I. DISCREPANT SEAT TRACK TRIM OUT AT STA 1791 LBL 27.5 AS PER SRM 53-70-00 FIG 1 VOL I. NEW SEAT TRACK AND SPLICE ANGLE REWORKED FROM S4929147-7075T6511 AND S4932154-7075T6511 AS PER SRM 53-70-00 FIG 1 VOL I. SPLICE PLATE FABRICATED FROM 7075T6-0.050 AS PER SRM 53-70-00 FIG 1 VOL I. NEW SEAT TRACK AND REPAIR PARTS LOCATED AND INSTALLED AS PER SRM 53-70-00 FIG 1 VOL I. CLASSIFIED MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050616001182005061600118NM 2005 6 16 HNAA0500052 120050607A61233014403 CONTROL UNIT DHAV DHC8 DHC8201 2809001NM AUTO FEATHER SYSFAULTY A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07969HA1454514545 468 AT 400 FEET, NR 2 PROPELLER AUTO FEATHERED THE ENGINE TORQUE WAS AT 95 PERCENT. CREW ALSO REPORTED THE TORQUE WENT TO THE RED LINE AND REMAINED. REPLACED THE NR 2 TSCU. 2H72 4T RTA13NM 20050616001192005061600119NM 2005 6 16 05FDEA00677 120050328A5347AFA7795510 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 MAIN DECK, AT STA 1831 RBL 27.5 SEAT TRACK CROWN AND BASE FOUND CORRODED. CORROSION ON SEAT TRACK AT STA 1831 RBL 27.5 REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-70-00 FIG 3 VOL I. DISCREPANT SEAT TRACK TRIM OUT AT STA 1811 RBL 27.5 AS PER SRM 53-70-00 FIG 1 VOL I. HFEC CARRIED AS PER DAC NDT SPM REV 11 PART 06-10-01- 001 ON TRIM-OUT AREA AND FOUND NO CRACK EVIDENT. NEW SEAT TRACK REWORKED FROM S4929147-7075T6511 AS PER SRM 53-70-00 FIG I VOL I. NEW SEAT TRACK AND REPAIR PARTS LOCATED AND INSTALLED AS PER AS PER SRM 53-70-00 FIG 1 VOL I. MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050616001212005061600121NM 2005 6 16 05FDEA00694 120050329A5347 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 MAIN DECK, AT STA 889 RBL 75.25 SEAT TRACK CROWN FOUND CORRODED. MAIN DECK STA 869 TO 909 RBL 75.25 CORROSION SEAT TRACK REPAIRED AS PER EA 1-3620-80387. PNEUMATIC SYSTEMS - FUSELAGE PNEUMATIC OVERHEAT DETECTOR - MOUNTING BRACKET INSTALLED. CLASSIFIED MINOR ALTERNATION AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050616001232005061600123NM 2005 6 16 05FDEA00698 120050329A5347ACA7104509 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 MAIN DECK, ALONG STA 812 TO STA 855 LBL 8.5 SEAT TRACK CROWN FOUND CORRODED. CORROSION ON SEAT TRACK CROWN AT STA 812 TO 855 LBL 8.5 REMOVED & FOUND EXCEED LIMIT AS PER SRM 53-70-00 FIG 3 VOL I. DISCREPANT SEAT TRACK TRIM-OUT FROM STA 800 TO 869 LBL 8.5 AS PER SRM 53-70-00 FIG 1 VOL I. REPAIR PARTS REWORKED FROM S4929147- 7075T6511, S4932154-7075T6511 & FABRICATE SPLICE PLATE FROM 7075T6-0.050 AS PER SRM 53-70-00 FIG 1 VOL I. HFEC CARRIED OUT ON TRIM-OUT AREA & FOUND NO CRACK EVIDENT. REPAIR PARTS REPROTECTED AS PER SRM 51-21-01 VOL II & INSTALLED AS PER SRM 53-70-00 FIG 1 VOL I. MAJOR REPAIR AS PER GMM 6-2-100 AND SRM 51-90-01 FIG 1 VOL II. 2L73 4F RTA22WE 20050616001252005061600125NM 2005 6 16 05FDEA01474 120050527A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 EVALUATE 15 INCH BY 20 INCH EXTERNAL DOUBLER AT BS 656-672 STR 28L-28R, WL 148. REMOVED AND REPLACED DOUBLER PER SRM 53-30-3. 2L73 4F RTA3WE 20050616001272005061600127NM 2005 6 16 05FDEA01476 120050527A5320 INTERCOSTAL BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 CORROSION ON INTERCOSTAL, BS 259 - 277, LBL 7.5, WL 208. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-30-2. 2L73 4F RTA3WE 20050616001292005061600129EU 2005 6 16 ALGA101072 120050519A6220C62242006601 PIN UROCOPEC120 EC120B 8680987EU MAIN ROTOR CORRODED B ALGAK NONE O OTHER NRNOT REPORTED 1 SW03524AL883 1263 EXCESSIVE CORROSION ON INSIDE AND OUTSIDE OF PINS. SCRAPPED PINS. 1G72 3U NCR0001RD 20050616001302005061600130EU 2005 6 16 ALGA101073 120050519A6220C62242006601 PIN UROCOPEC120 EC120B 8680987EU MAIN ROTOR CORRODED B ALGAK NONE O OTHER NRNOT REPORTED 1 SW03524AL883 1263 EXCESSIVE CORROSION ON INSIDE AND OUTSIDE OF PINS. SCRAPPED PINS. 1G72 3U NCR0001RD 20050616001312005061600131NM 2005 6 16 DHL2005741531 120050516A5313 STRINGER BOEING727 7272Q9 138448MNM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH46665 21931 STRINGER 15L AT BS 720B CRACKED FWD OF EMERGENCY LIGHT LT SIDE. REMOVED FASTENERS CUT OUT AREA DIM .75 INCH ON STRINGER 15 AND BS 720B IAW B727 SRM 53-10-3 FIG 5. FABRICATED CHANNEL FROM BAC 1498-140 SIZE 4 INCH PO 4246397 AND RADIUS FILLER FROM 7075-T6 .100 SIZE .875 X 4 INCH PO 9911586 AND TAPER FILLER FROM 7075 T6 .100 SIZE 2.625 X .875 INCH PO 9911586 AND FILLER FROM 7075 T6 .050 SIZE .75 X .875 INCH PO 9002126 IAW B727 SRM 53-10-3 FIG 5. TREATED AND PRIMED PARTS AND AREA IAW B727 SRM 51-10-2. INSTALLED PARTS REPAIR IAW B727 SRM 53-10-3 FIG 5. 2L73 4F RTA3WE 20050616001322005061600132NM 2005 6 16 DHL2005745009 120050602A3260 WARNING SWITCH BOEING727 727224 1384076NM RT MLG OUT OF ADJUST A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01745DH 20665 AFTER GEAR RETRACTION RED DOOR LIGHT ILLUMINATED. S/O PANEL INDICATED RT GEAR DOOR. ACCOMPLISHED ABNORMAL PROCEDURE PLACE HANDLE UP POSITION DOOR LIGHTS OUT. ADJUSTED RT MAIN GEAR DOOR WARNING SWITCH IAW MM 32-62-11. OPS CHECK GOOD. 2L73 4F A3WE 20050616001332005061600133NM 2005 6 16 CALA0500179 120050601A5330146A3230 SKIN BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2726215 28775 INSPECTION FOUND CORROSION ON SKIN AROUND CENTER DRAIN PLUG BETWEEN STA 727E AND 727F. REPAIRED IAW ECRA 5330-03444 AND PLACED ON DIP TO PERFORM PERMANENT REPAIR PER PART 3 WITHIN 12 MONTHS. 2L72 4F RTA16WE 20050616001352005061600135NM 2005 6 16 CALA0500181 120050601A3350D71701100 BATTERY PACK BOEING737 737824 13844BZNM CABIN DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW2724211 28771 THE EMERGENCY AISLE LIGHTS ON BAGGAGE BINS AT SEATS 14, 16, 19, 21, AND 26 RIGHT WERE FOUND INOPERATIVE DURING TESTING. THE BATTERY PACK AT SEAT 19DEF WAS REMOVED AND REPLACED IAW MM 33-51-06-960-805. 2L72 4F RTA16WE 20050616001372005061600137CE 2005 6 16 DXTA200500748 120050601A3240NAS161204 O-RING CESSNA500 560CESSNA 2076750CE BRAKE LINE LEAKING E DXTAD RETURN TO BLOCK K FLUID LOSS TXTAXI/GRND HDL 1 GL07371QS 5600471 LOST BRAKE PRESSURE ON TAXI. BRAKE FLUID LEAKING OUT OF RIGHT BRAKE ASSEMBLY. REMOVED AND REPLACED LEAKING O-RING ON BRAKE LINE FITTING. OPS AND LEAK CHECK GOOD IAW BF GOODRICH CMM 32-46-13. 2L72 4F RTA22CE 20050616001392005061600139NE 2005 6 16 AT050016 220050527A7321114E6112G1 EEC BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE RT ENGINE MALFUNCTIONED A ZZDAK NONE R PARTIAL RPM/PWR LOSS CLCLIMB 1 SO15603AT 55127 DURING CLIMBOUT AT CLIMB THRUST AT APPROX 14,000 FEET THE RIGHT ENGINE ROLLED BACK (THROTTLES DID NOT MOVE) EPR & TGT FELL, AUTO-IGNITION CAME ON & ENGINE RECOVERED. NO AUDIBLE INDICATIONS, NO ALERTS, NO FAULTS. THIS REOCCURRED APPROXIMATELY 2 MINUTES LATER. AGAIN NO INDICATIONS AND ENGINE RECOVERED WHEN AUTO-IGNITION CAME ON. ACTED LIKE A FLAMEOUT THAT RESTARTED WHEN THE IGNITION CAME ON. CLEAR AIR. REMOVED AND REPLACED NR 2 EEC PER B717 AMM 73-21 PERFORMED RTS ON NR 2 EEC PER B717 AMM 73-21 RTS PASSED NO FAULTS NOTED. 2L72 4F4 FTRA6WE E00061EN 20050616001402005061600140NM 2005 6 16 05FDEA00651 120050328A5512ALC8101501 SKIN PANEL DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576F 48501 LEFT HORIZONTAL STABILIZER UPPER BARREL NUT NR 11 HAS BORE CORROSION EXCEEDING LIMIT. HOLE AT BARREL NUT BORE NR 11 LT FURTHER REAMED TO 1.002 INCH DIA, SMOOTHED AND FOUND CLEAN HOLE CONDITION AND IS WITHIN LIMITS AS PER EO E1-5510-7-5000D. STABILIZER HORIZONTAL INSPECT / REPAIR HORIZONTAL STABILIZER BARREL NUT HOLE AND SB/MD11 55-023. 2L73 4F RTA22WE 20050616001422005061600142 2005 6 16 05FDEA01500 420050601A3418 STICK SHAKER BOEING727 727200 138407ENM STALL WARNING ACTIVATED A FDEAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 SO25213FE 22935 DURING TAKEOFF, AIRSPEED BUGS SET CORRECTLY GOT STICK SHAKER AT MMS 15 ADVANCED TO FIREWALL POWER APPROX 16 SEC. CLEANED UP, ACCELERATED STICK STOPPED AT 0 MMS 30 (230 KTS) STICK SHAKER RETURNED AND REMAINED ON THROUGH OUT APPROACH. 2L73 4F RTA3WE 20050614000852005061400085NM 2005 6 14 USAA050585 120050502A5330 SKIN BOEING737 7374B7 1384702NM FUSELAGE DAMAGED A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19439US 24781 CLT - EXTERNAL DOUBLER INSTALLED 8.5 BY 10.375 INCH, STATION 500 PLUS 12 INCHES BETWEEN STRINGER 22L AND 23L. INSTALLED DOUBLER IAW SRM 53-00-01 FIG 202. (M) 2L72 4F RTA16WE 20050614000892005061400089NM 2005 6 14 USAA050589 120050503A5420 STIFFENER BOEING737 737301 1384611NM PYLON CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19560AU54874 23514 CLT - FOUND STIFFENER CRACKED .4 INCH IN VERTICAL STIFFENER AT AFT SIDE OF PYLON LOWER SIDE OF WING. FABRICATED REPAIR PART AND INSTALLED SRM 51-10-02. (M) 2L72 4F RTA16WE 20050614000912005061400091NM 2005 6 14 USAA050591 120050505A575465C26602223 WEDGE BOEING737 7374B7 1384702NM NR 3 SLAT DEBONDED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US39931 24781 CLT - FOUND WEDGE HAS AREA OF DISBOND 3 INCHES BY 5 INCHES, OUTBOARD TE WEDGE OF NR 3 SLAT. REMOVED DAMAGED CORE, INSTALLED NEW CORE FILLER AND DOUBLER IAW TR 57-42-02. (M) 2L72 4F RTA16WE 20050614000932005061400093NM 2005 6 14 USAA050593 120050505A575465C26603101 WEDGE BOEING737 7374B7 1384702NM NR 3 SLAT DEBONDED A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19439US39931 24781 CLT - FOUND NR 3 SLAT WEDGE DISBOND 2 INCHES, UNDERSIDE SKIN AT INBOARD END. SDA COMPLETED ACCOMPLISHED COMPOSITE REPAIR IAW SRM 57-43-02. (M) 2L72 4F RTA16WE 20050614000952005061400095NM 2005 6 14 USAA050598 120050425A5320 WEB BOEING737 7374B7 1384702NM FUSELAGE DEBONDED A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19439US39931 24781 CLT - FOUND WEB DISBONDED 1 INCH BY 1 INCH, STATION 14912. DEFECTIVE PART REPLACED WITH IDENTICAL PART IAW 51-40-02. (M) 2L72 4F RTA16WE 20050614000982005061400098NM 2005 6 14 USAA050583 120050430A5320 ANGLE BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US39931 24781 CLT - FOUND ANGLE CRACKED .125 ICH, 1 INCH FORWARD OF STATION 520 RBL 45.5. MAJOR REPAIR INSTALLED ANGLE IAW SRM 51-10-02. (M) 2L72 4F RTA16WE 20050614001002005061400100NM 2005 6 14 USAA050559 120050428A532065516989 SPLICE BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US39931 24781 CLT - FOUND STRINGER SPLICE WITH TWO CRACKS .250 INCH EACH, EMANATING FROM 2 RIVETS IN S4L SPLICE WEB AT STATION 907. SDA COMPLETE IAW SRM 51-20-02 AND 51-40-02. (M) 2L72 4F RTA16WE 20050614001022005061400102NM 2005 6 14 USAA050561 120050428A5320 CLIP BOEING737 7374B7 1384702NM FUSLEAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US 24781 CLT - FOUND CLIP ANGLE BRACKET CRACKED .25 INCH, STATION 360 AT S4L. FABRICATED ANGLE FROM BOEING DRAWING AND INSTALLED IAW DWG 6948747. (M) 2L72 4F RTA16WE 20050614001492005061400149NM 2005 6 14 SWAA051636 120050602A53306545769 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT EQUIPMENT COOLING EXHAUST CUTOUT, BS 378, BL 0. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050615000372005061500037NM 2005 6 15 SWAA051604 120050531A335065C34691 LIGHT BOEING737 7377H4 1384404NM MID CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29403WN 29815 DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY BULLNOSE LIGHT INOP AT ROW 21 DEF. REMOVED AND REPLACED LIGHT PER MM. 2L72 4F RTA16WE 20050615000382005061500038NM 2005 6 15 SWAA051603 120050531A551265C25727 SKIN BOEING737 7373H4 1384600NM HORIZONTAL STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29353SW 24889 DURING SCHEDULED 1/2D CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED 36 INCHES FROM INBOARD AFT SPAR. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050615000402005061500040NM 2005 6 15 SWAA051606 120050531A57116959886 SPAR BOEING737 737301 1384611NM WINGS CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND LT & RT WING REAR SPAR UPPER CHORDS CRACKED AT MLG BEAM 2ND INBOARD CUTOUT HOLE. REMOVED AND REPLACED REAR SPAR UPPER CHORDS PER BFG ER. 2L72 4F RTA16WE 20050615000422005061500042NM 2005 6 15 SWAA051608 120050531A53306545774 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D + 7, STR 24L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050615000442005061500044NM 2005 6 15 SWAA051610 120050531A57546573714 WEDGE BOEING737 737301 1384611NM NR 5 SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND NR 5 L/E SLAT UPPER INBOARD T/E WEDGE DELAMINATED. REPAIRED NR 5 SLAT PER SRM. 2L72 4F RTA16WE 20050615000462005061500046NM 2005 6 15 SWAA051669 120050606A3234273A33016 LEVER BOEING737 7377H4 1384404NM MLG FAULTY A SWAAO OTHER O OTHER DEDESCENT 1 SW29778SW 27883 DECLARED EMERGENCY, LANDING GEAR LEVER STUCK IN THE OFF POSITION, WOULD NOT MOVE UP OR DOWN. REMOVED AND REPLACED LANDING GEAR CONTROL LEVER ASSY PER MM. 2L72 4F RTA16WE 20050615000482005061500048NM 2005 6 15 SWAA051671 120050606A533065458197 PRESSURE PANEL BOEING737 737317 138447PNM NLG WW CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED SERVICE CHECK, FOUND NLG W/W PRESSURE WEB CRACKED AT RT FWD PANEL CUTOUT, BS 246, WL 168.5. REPAIRED WEB PER SWA EA. 2L72 4F RTA16WE 20050615000502005061500050NM 2005 6 15 SWAA051663 120050606A335010107451 SIGN BOEING737 7377H4 1384404NM EMERGENCY EXIT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29208WN 29856 R2 DOOR EMERGENCY EXIT SIGN LENS MISSING. REMOVED AND REPLACED EXIT SIGN PER MM. 2L72 4F RTA16WE 20050615000512005061500051NM 2005 6 15 SWAA051664 120050606A53146545866 KEELBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND KEELBEAM CORRODED BETWEEN BS 500D + 2 TO BS 727 + 8. REMOVED AND REPLACED KEELBEAM PER SRM. 2L72 4F RTA16WE 20050615001412005061500141NM 2005 6 15 DHL2005784515 120050519A5754 RIB BOEING727 727227 1384078NM NR 5 SLAT CRACKED A DHLAO OTHER O OTHER ININSP/MAINT 1 SO01784DH 22001 NR 5 SLAT L/E INTERIOR AT ACTUATOR ATTACH POINT INBD AND OUTBD RIBS CRACKED, PREVIOUSLY REPAIRED. REMOVED AND REPLACED DAMAGED RIBS AT NR 5 SLAT L/E SLAT ATTACH ON SLAT P/N 65-17276U11 AND 65-17276-9,BOTH PO NR 518347 IAW B727 SRM 51-30-2. 2L73 4F A3WE 20050615001432005061500143 2005 6 15 AWXA200500666 420050604A34426225135002 DRIVE ASSY BOEING737 7373G7 1384595NM WEATHER RADAR FAILED A AWXAA UNSCHED LANDING O OTHER CRCRUISE 1 WP28158AW473292860 23780 DFW - FLT 152 - DURING FLT TO STL, LOST WEATHER RADAR. RECEIVED "ANT FAIL" MSG OCCURRED DURING CLOUDY WEATHER CONDITIONS. DIVERTED TO DFW WHERE MAINTENANCE REMOVED AND REPLACED WEATHER RADAR PEDESTAL DRIVE UNIT IAW AMERICA WEST AIRLINES TASK CARD R1A34003. OPERATIONAL CHECK WAS GOOD IAW AMERICA WEST AIRLINES TASK CARD A1B34036. TEAR DOWN REPORT CONFIMS FAILURE OF THE PEDISTAL DRIVE UNIT. UNIT FAILED BENCH TEST, THE AZIMUTH GEAR NEEDED TO BE REPLACED. REPLACED DEFECTIVE PARTS AND OVERHAULED UNIT IAW CMM 34-45-22 REV. 17. 2L72 4F RTA16WE 20050615001442005061500144NM 2005 6 15 QXEA200501004 120050601A33506138001 BATTERY PACK BOMBDRDHC8 DHC8402 1390042NM EMERGENCY LIGHT INOPERATIVE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX3342 1360 4061 SEA- FORWARD EMERGENCY LIGHTS ARE INOP. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050616000072005061600007NM 2005 6 16 DU4R107 120050527A5320 ANGLE BOEING737 7373L9 1384470NM FUSELAGE CORRODED B DU4RK NONE O OTHER ININSP/MAINT 1 SO15312FL 24569 FWD ENTRY DOOR THRESHOLD HAS CORRODED ANGLE (OB OF INNER CHORD). S/O 109001, N/R 23118. 2L72 4F RTA16WE 20050616000142005061600014SO 2005 6 16 ENHA0511 120050325A2420ALU8521RS ALTERNATOR PIPER PA31 PA31350 7103110SO ENGINE INOPERATIVE E ENHAO OTHER O OTHER NRNOT REPORTED 1 AL03417PM 54 318052051 HIGH FIELD RESISTANCE, ALTERNATOR INOPERATIVE. 1L72 3O A20SO 20050616000242005061600024NM 2005 6 16 SWAA051650 120050603A53306545775 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29331SW 23695 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STR 19L TO STR 20L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050616000262005061600026NM 2005 6 16 SWAA051652 120050603A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29331SW 23695 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 28R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050616000442005061600044NM 2005 6 16 SWAA051683 120050607A33507003661 BALLAST BOEING737 7375H4 138449DNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29524SW 26566 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BALLAST PER MM. 2L72 4F RTA16WE 20050616000502005061600050NM 2005 6 16 SWAA051694 120050608A52306547952 SKIN BOEING737 7373L9 1384470NM AFT CARGO DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29658SW 23332 DURING SCHEDULED C1 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS AT AFT CARGO DOOR HANDLE CUTOUT. REMOVED AND REPLACED AFT CARGO DOOR PER MM. 2L72 4F RTA16WE 20050616000722005061600072NM 2005 6 16 AWXA200500649 120050523A5752654645521C TAB BOEING737 737301 1384611NM LT AILERON DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-19 CHECK, LT AILERON TAB WAS FOUND TO BE SEPARATED ALONG THE AFT EDGE NEAR THE OUTBOARD END. MAINTENANCE REMOVED ALL CONTAMINANTS AND WATER FROM DAMAGED AREA AND REPAIRED LT AILERON TAB IAW BOEING 737-300 SRM 51-70-06-0 FIG 13. 2L72 4F RTA16WE 20050616000752005061600075NM 2005 6 16 AWXA200500651 120050522A575465C26601167SP SKIN BOEING737 737301 1384611NM L/E SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-19 CHECK, 3 CRACKS, .3' IN LENGTH EACH, FOUND ON BOTTOM NR 1 SLAT SKIN. MAINTENANCE REMOVED PREVIOUS REPAIR AND CRACKED SECTION ON NR 1 SLAT. FABRICATED FILLER AND SPLICE PLATE. INSTALLED FABRICATED REPAIR PARTS IAW BOEING 737-300 SRM 57-43-01-2 FIG 206. 2L72 4F RTA16WE 20050616000952005061600095NM 2005 6 16 05FDEA01517 120050603A5330 PAN BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25477FE 21394 CORROSION ON ANTENNA PAN IN AFT CARGO BILGE AT BS 1033, BETWEEN STR 30 AND STR 29R. REMOVED AND REPLACED IAW SRM 51-30-2, 51-20-1. 2L73 4F RTA3WE 20050616000992005061600099EU 2005 6 16 AWXA200500671 120050603A3350 LIGHT AIRBUS320 A320232 3930326EU CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28639AW 471 PERFORMING OPERATIONAL TEST OF EMERGENCY LIGHTING, TEST DON'T PASS. 2L72 4F RTA28NM 20050616001012005061600101NM 2005 6 16 2005UALA00488 120050530A5330 SKIN BOEING737 737522 138449FNM CFMINTCFM56 CFM562AFR 13802EU FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29910UA 25254 CRACKS FOUND AT BS 1006-1016 STR S6L. REPLACED TEMPORARY REPAIR AND INSTALLED PERMANENT DOUBLER REPAIR PER SRM 53-60-01 FIG 205. 2L72 4F4 FRTA16WE E21EU 20050616001022005061600102NM 2005 6 16 AWXA200500673 120050608A3150 WARNING SYSTEM BOEING737 7373S3 1384711NM COCKPIT MALFUNCTIONED A AWXAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 WP28316AW 23713 LAS - ABORTED TAKEOFF - FLT 879 - DURING TAKEOFF, WHEN THROTTLES WERE ADVANCED FOWARDED RECIEVED TAKEOFF WARNING ALERT FOR STABILIZER TRIM OUT OF GREEN BAND. ABORTED TAKEOFF AND PUT STAB TRIM BACK IN GREEN BAND. TOOK OFF FROM LAS WITHOUT FURTHER INCIDENT. 2L72 4F RTA16WE 20050616001342005061600134NM 2005 6 16 CALA0500180 120050602A52306546921528 SKIN BOEING737 7373T0 1384582NM CARGO DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714325 23455 INSPECTION FOUND A 1.75 INCH CRACK IN C-1 DOOR INNER SKIN AT CENTER LIGHTENING HOLES. A DOUBLER WAS INSTALLED IAW ECRA 5232-01063. 2L72 4F RTA16WE 20050616001362005061600136NM 2005 6 16 DHL2005741532 120050516A5313 STRINGER BOEING727 7272Q9 138448MNM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH46665 21931 STRINGER 15L AT BS 720C CRACKED AFT OF EMERGENCY LIGHT. REMOVED FASTENERS CUT OUT AREA DIM .75 X STR 15 AND BS 720C IAW B727 SRM 53-10-3 FIG 5. FABRICATED CHANNEL FROM BAC 1498-140 SIZE 4 INCH PO 4246397 AND RADIUS FILLER FROM 7075-T6 .100 SIZE .875 X 4 INCH PO 9911586 AND TAPPER FILLER FROM 7075- T6 .100 SIZE 2.75 X .875 INCH PO 9911586 AND FILLER FROM 7075- T6 .050 SIZE .75 X .875 INCH PO 9002126 IAW B727 SRM 53-10-3 FIG 5. TREATED AND PRIMED PARTS AND AREA IAW B727 SRM 51-10-2. INSTALLED PARTS REPAIR IAW B727 SRM 53-10-3 FIG 5. 2L73 4F RTA3WE 20050616001412005061600141NM 2005 6 16 05FDEA00841 120050405A5512ALC8100XXX SKIN PANEL DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 RIGHT HORIZONTAL STABILIZER UPPER BARREL NUT NR 12 HAS BORE CORROSION EXCEEDING LIMITS. BARREL NUT BORE NR 12 RIGHT, REPAIRED IAW EA 1-5510-78133 ATTACHMENT 13. HORIZONTAL STABILIZER BARREL NUT BORE REWORK/ REPAIR AD 2003-22-08. MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050616001432005061600143EU 2005 6 16 05FDEA01502 120050601A3260 WARNING SYSTEM AIRBUS300 A300B4605R 3930308EU COCKPIT MALFUNCTIONED A FDEAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 SO25686FE 804 DURING APPROACH WHEN LANDING GEAR LOWERED, LANDING GEAR INDICATIONS ON FORWARD PANEL INDICATED 3 DOWN GREEN WITH 3 RED UNLOCKED INDICATION, POSITION DETECTION SYSTEM WAS SELECTED TO SYS 1. ECAM DIRECTED SWITCH TO POSITION DETECTOR SYS 2. SWITCHED TO SYSTEM 2 FORWARD INDICATION SYSTEM REMAINED THE SAME 3 GREEN, 3 RED OVERHEAD LANDING GEAR INDICATORS INDICATED 3 GREEN, RECYCLED LANDING GEAR USING SYS 1 DETECTOR AND RECEIVED NORMAL INDICATIONS 3 GREEN, NO RED UNLOCKED. INSPECTED AND PERFORMED PROX BOX UNIT TEST IAW AMM 32-00-00-501 PROX UNIT TESTED GOOD NO FAULTS LOGGED OR SHOWING. ALL COCKPIT LANDING GEAR INDICATION SYS TEST GOOD. COULD NOT DUPLICATE, OK TO CONTINUE. 2L72 4F RTA35EU 20050616001462005061600146NM 2005 6 16 CALA0500182 120050527A523065C36231 SKIN BOEING737 7373T0 1384582NM CARGO DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714325 23455 INSPECTION FOUND A .5 INCH CRACK IN C-2 DOOR OUTER SKIN. THE CRACK WAS LOCATED AT THE AFT UPPER CORNER OF C-2 DOOR HANDLE CUTOUT. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-30-01. 2L72 4F RTA16WE 20050616001472005061600147NM 2005 6 16 CALA0500183 120050602A53106545829505 DOOR FRAME BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714325 23455 INSPECTION FOUND SKIN BULGED AND RIVET HEADS STRESSED AT STA 360 AND S28L. THE E&E DOOR CUTOUT BEAM LOWER T-CHORD WAS FOUND CORRODED. THE T-CHORD WAS REPAIRED IAW ECRA 5311-01229. 2L72 4F RTA16WE 20050616001492005061600149NM 2005 6 16 72300188 120050521A5320 STRUCTURE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 1 INCH AREA OF CORROSION. 2L73 4F4 FRTA3WE E2EA 20050616001532005061600153NM 2005 6 16 72300192 120050524A5320 ANGLE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 3 X 2 INCH AREA OF CORROSION. 2L73 4F4 FRTA3WE E2EA 20050616001552005061600155NM 2005 6 16 05FDEA01479 120050530A5753 SKIN DOUG MD11 MD11 3023602NM T/E FLAP NICKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25631FE 48454 RIGHT INBOARD FLAP TOP SKIN XIRH 207.30/215.30 RIVETS INSTALLED ON EXISTING NICKS IN SKIN. SKIN TRIMMED REPAIR DOUBLER FABRICATED AND INSTALLED AS PER SRM 57-10-00 FIG 34 VOL I AND 51-35-01 VOL II. MATERIAL USED AS PER DWG ARC 2369. MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050616001572005061600157NM 2005 6 16 05FDEA01515 120050603A5320 FLOOR SUPPORT DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25631FE 48454 FWD CABIN, FLOOR SUPPORT FWD EDGE FOUND CORROSION AS MARKED AS STA 421 TO 459 BL-0. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20050616001582005061600158WP 2005 6 16 AALA20050377 120050602A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21412AA 49323 DFW - CEILING EMERGENCY LIGHTS ABOVE SEAT ROWS 28 THROUGH 31 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS ABOVE SEAT ROWS 28 THROUGH 31. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050616001592005061600159NM 2005 6 16 AALA20050375 120050601A3241 VALVE BOEING737 737823 13844BZNM ANTI-SKID SYS FAULTY A AALAK NONE J WARNING INDICATION DEDESCENT 1 SW21933AN 30080 JFK - AFTER AUTOBRAKES WERE SELECTED FOR LANDING, ANTI SKID INOPERATIVE LIGHT CAME ON AND STAYED ON UNTIL AFTER LANDING. LIGHT WENT OFF WHEN ENGINES WERE SHUT DOWN. FOUND ANTI SKID VALVES 3/4 FAULTED. REPLACED 3/4 ANTI SKID VALVES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20050616001602005061600160EU 2005 6 16 AALA20050376 120050602A3350 PIN AIRBUS300 A300B4605R 3930308EU CONNECTOR DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW2114056 463 MIA - EMERGENCY LIGHT AT SEAT 24G INOPERATIVE. REPLACED PINS IN CONNECTION FOR EMERGENCY LIGHT AT SEAT 24G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20050616001612005061600161NM 2005 6 16 AALA20050371 120050526A5311 FAILSAFE BOEING767 767323 1385205NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21385AM 27059 AFW - FOUND CORROSION ON THE LOWER SURFACE OF THE LOWER MAIN SILL FAIL SAFE STRAP IN THE FORWARD CARGO AREA AT STATION 566. CORROSION WAS 2 INCHES BY 4 INCHES. BLENDED CORROSION AND PERFORMED HIGH FREQUENCY EDDY CURRENT INSPECTION OF THE BLENDED AREA TO ENSURE IT WAS CRACK-FREE. PERFORMED OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION OF ALL FASTENER HOLES IN BLENDED AREA AND REFINISHED BLENDED AREA. REINSTALL NON-ALUMINUM FASTENERS WITH BMS595 SEALANT. RETURNED TO SERVICE WITH NOTED CONDITION. 2L72 4F RTA1NM 20050616001622005061600162WP 2005 6 16 AALA20050373 120050531A3397 WIRE HARNESS DOUG DC9 DC983 3022083WP CABIN DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21594AA 53284 SFO - RED AND WHITE EMERGENCY LIGHTS AT 23D INOPERATIVE. REPAIRED EMERGENCY LIGHT WIRE HARNESS BEHIND SEAT 27D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050616001632005061600163WP 2005 6 16 AALA20050374 120050601A3350 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21463AA 49593 DTW - EMERGENCY LIGHTS IN FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050616001642005061600164NM 2005 6 16 AALA20050378 120050503A3350 CONNECTOR BOEING767 767323 1385205NM CABIN DISCONNECTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21394AN 29431 AFW - EMERGENCY LIGHTS FORWARD OF SEAT 2DC INOPERATIVE. CONNECTED EMERGENCY LIGHTS FORWARD OF SEAT 2DC. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050616001652005061600165NM 2005 6 16 AALA20050372 120050526A5310 DOOR FRAME BOEING767 767323 1385205NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21385AM 27059 AFW - FORWARD CARGO DOOR CUTOUT LOWER OUTER CHORD HAD CORROSION BLENDED FROM VERTICAL LEG AT STATION 569. BLEND IS IN AREA OF 2.3 INCHES BY 1.1 INCH AND 0.021 INCH DEEP. BLEND OUT CORROSION AND PERFORMED HIGH FREQUENCY EDDY CURRENT INSPECTION TO ENSURE BLENDED AREA AND FASTENER HOLES ARE CRACK-FREE. INSTALLED FREEZE PLUG DIAMETER 0.0437 INCH IN FORWARD HOLE. REFINISH THE BLENDED AREA AND ENSURE SURFACE IS FLAT FOR PROPER FASTENER INSTALLATION. REINSTALL NON-ALUMINUM FASTENERS WET WITH BMS595 SEALANT. RETURNED TO SERVICE WITH THE NOTED CONDITION. 2L72 4F RTA1NM 20050616001662005061600166WP 2005 6 16 AALA20050370 120050519A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN OUT OF POSITION A AALAK NONE L NO TEST ININSP/MAINT 1 SW21593AA 53256 TUL - VARIOUS CEILING EMERGENCY LIGHTS AND TAIL COMPARTMENT LIGHTS INOPERATIVE. REPOSITIONED BATTERY FOR INOPERATIVE CEILING EMERGENCY LIGHTS AND TAIL COMPARTMENT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050616001672005061600167WP 2005 6 16 AALA20050379 120050603A3350 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW217537A 49991 DFW - EMERGENCY LIGHTS IN CEILING ABOVE SEATS 18-21 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN CEILING ABOVE SEATS 18-21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050616001682005061600168NM 2005 6 16 CALA0500184 120050603A531565C33948 FLOORBEAM BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716618 27331 INSPECTION FOUND CORROSION AROUND NUT PLATE HOLE ON FLOORBEAM AT STA 947.5, RBL 6 AND RBL 18. REPAIRED IAW SRM 53-00-51, FIGURE 203. 2L72 4F RTA16WE 20050616001692005061600169NM 2005 6 16 CALA0500185 120050604A5320147A576213 INTERCOSTAL BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2727213 28773 INSPECTION FOUND FLOOR INTERCOSTAL CORRODED AT STA 957, RBL 48. THE FLOOR INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20050616001702005061600170NM 2005 6 16 CALA0500186 120050605A5347143A5310 SEAT TRACK BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2727213 28773 INSPECTION FOUND LEFT I/B SEAT TRACK CORRODED AT STA 380, LBL 18. A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-40-02. 2L72 4F RTA16WE 20050616001722005061600172NM 2005 6 16 05FDEA01504 120050601A5534 TIE BOEING727 727200 138407ENM VERTICAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 VERTICAL FIN TENSION TIE RT FWD VERTICAL BOLT HOLE IN TENSION TIE & SHEAR FITTING HAS CORROSION. REPAIRED TENSION TIE PER FED EX EA 7-5530-86296. 2L73 4F RTA3WE 20050616001732005061600173WP 2005 6 16 MWEA050046 120050605A2530 DRAIN DOUG DC9 DC982 3022082WP FWD GALLEY OBSTRUCTED A MWEAA UNSCHED LANDING O OTHER CLCLIMB 1 GL31810ME 48072 LOUD SQUEAL WAS AUDIBLE THROUGHOUT CABIN AND COCKPIT SEEMED TO BE IN FORWARD GALLEY. FOUND GALLEY DRAIN PLUGGED POSSIBLE CAUSE OF SQUEAL. CLEANED DRAIN, CLEANED GALLEY PASSENGER DOOR SEALS, PRESSURIZED CABIN TO 7.5 PSI, LEAK DOORS AND SEALS NO AUDIBLE SQEALS IN CABIN. 2L72 4F A6WE 20050616001742005061600174EU 2005 6 16 U30A200500004 120050602A25308203110000 OVEN AIRBUS320 A320214 3930316EU NR 1 UNKNOWN A U30AH DEACTIVATE SYST/CIRCUITS A FLAME/FIRE CRCRUISE 1 EA17269AV3805 3805 2187 DURING CRUISE, AFT F/A SMELLED SMOKE IN AFT GALLEY (G5). OPENED NR 1 OVEN, FOUND MEALS CONTAINED IN BOXES BURNED ON END. SMALL FIRE EXISTED & EXTINGUISHED. POWER REMOVED FROM OVEN, PULLED C/B. NR 1 OVEN INSERT (CARRIER FOR MEALS) DID NOT HAVE A METAL BACK AS THE OTHER OVENS. CAPT & CABIN CREW CERTAIN MEAL BOXES TOO CLOSE, OR TOUCHING HEATING ELEMENT. BANNED USE OF OVEN INSERTS WITH OPEN BACKS. ACFT LANDED WITHOUT INCIDENT. MX INSPECTED GALLEY AREA, OVEN MOUNTING AREA, ADJACENT OVENS FOR DAMAGE, NO FAULTS FOUND. INSPECTED EXTERNAL & INTERNAL SURFACES OF OVEN, ELEMENTS & TEMP SENSORS, NO DAMAGE FOUND. OVEN C/B COLLARED & OVEN DEFERRED. ACFT RETURNED TO SERVICE. OVEN SENT FOR BENCH CHECK & EVALUATION. 2L72 4F RTA28NM 20050616001752005061600175NM 2005 6 16 SWAA051624 120050524A3350311500 LENS BOEING737 7373H4 1384600NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 EMERGENCY BULLNOSE LIGHT LENS MISSING AT ROW 1 DEF. INSTALLED LENS ASSY PER MM. 2L72 4F RTA16WE 20050616001762005061600176NM 2005 6 16 SWAA051625 120050602A3350612825 BATTERY BOEING737 7373H4 1384600NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED C1 CHECK, FOUND L1 & R1 DOOR LOWER EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY & CHARGER PER MM. 2L72 4F RTA16WE 20050616001772005061600177NM 2005 6 16 SWAA051626 120050602A3350612825 BATTERY PACK BOEING737 7373H4 1384600NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29331SW 23695 DURING SCHEDULED C4 CHECK, FOUND LEFT SIDE CABIN EMERGENCY EXIT BULLNOSE LIGHTS INOP. RECHARGED BATTERY PACKS PER MM. 2L72 4F RTA16WE 20050616001782005061600178NM 2005 6 16 SWAA051627 120050602A3350101073 LENS BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29331SW 23695 DURING SCHEDULED C4 CHECK, FOUND FWD GALLEY OVERHEAD EMERGENCY LIGHT LENS LOOSE. SECURED LENS PER MM. 2L72 4F RTA16WE 20050616001792005061600179NM 2005 6 16 SWAA051628 120050602A3350BR2013 LIGHT BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29331SW 23695 DURING SCHEDULED C4 CHECK, FOUND EEPLS FLOOR STRIPS INOP AT ROWS 1 TO ROWS 4, LT SIDE & ROWS 10 TO ROWS 14, RT SIDE. REMOVED AND REPLACED EEPLS PER MM. 2L72 4F RTA16WE 20050616001802005061600180NM 2005 6 16 SWAA051629 120050602A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29332SW 23696 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 312, STR 19R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050616001812005061600181NM 2005 6 16 SWAA051630 120050602A53306545769 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29358SW 26595 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT EQUIPMENT COOLING EXHAUST CUTOUT, BS 378, LBL 2. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050616001822005061600182NM 2005 6 16 SWAA051631 120050602A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29360SW 26571 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR CUTOUT, LOWER AFT CORNER. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050616001832005061600183NM 2005 6 16 SWAA051632 120050602A3350612825 BATTERY BOEING737 7373H4 1384600NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29365SW 26576 DURING SCHEDULED RON CHECK, FOUND EMERGENCY BULLNOSE LIGHT INOP AT ROW 15 DEF. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20050616001842005061600184NM 2005 6 16 SWAA051633 120050602A53126546568 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29370SW 26597 DURING SCHEDULED 1/4D CHECK, FOUND BS 1016 AFT PRESS BULKHEAD WEB CRACKED AT STR 7R. REPAIRED BS 1016 AFT PRESS BULKHEAD WEB PER SWA EA. 2L72 4F RTA16WE 20050616001852005061600185NM 2005 6 16 SWAA051634 120050602A57536546435365A FLAP BOEING737 7375H4 138449DNM LT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED A2 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM. 2L72 4F RTA16WE 20050616001862005061600186 2005 6 16 SWAA051635 420050602A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29612SW 27930 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050616001872005061600187EU 2005 6 16 WRNA200500014 120050604A2780 SLAT AIRBUS300 A300B4203 3930306EU WING MALFUNCTIONED A WRNAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO05505TA 271 AFTER TAKEOFF SLATS WOULD NOT RETRACT. AIRCRAFT RETURNED TO AIRFIELD. LANDING NORMAL. MAINTENANCE OPS CHECKED SLAT SYSTEM ON GROUND, COULD NOT DUPLICATE, OP'S CHECKED SATISFACTORY IAW MM 27-81-00. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA35EU 20050616001892005061600189NM 2005 6 16 SWAA051584 120050527A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29353SW 24889 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 380, STR 15L. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20050616001912005061600191NM 2005 6 16 SWAA051586 120050527A53306545857 BEAR STRAP BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29353SW 24889 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FUSELAGE SKIN BEAR STRAP AT BS 848, STR 25R TO STR 26R. REPAIRED BEAR STRAP PER SWA EA & SRM. 2L72 4F RTA16WE 20050616001932005061600193NM 2005 6 16 SWAA051588 120050528A3350D71702030 BATTERY BOEING737 7377H4 1384404NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29442WN 32459 DURING SCHEDULED MV3 CHECK, FOUND RIGHT AFT EXTERNAL EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050616001942005061600194NM 2005 6 16 SWAA051589 120050529A335020121 POWER SUPPLY BOEING737 7375H4 138449DNM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29525SW 26567 DURING SCHEDULED A2 CHECK, AFT CABIN EMERGENCY LIGHTS INOP WHEN POWER REMOVED. REMOVED AND REPLACED AFT POWER SUPPLY PER MM. 2L72 4F RTA16WE 20050616001952005061600195NM 2005 6 16 SWAA051590 120050530A53116545854 FRAME BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 986, ABOVE L2 DOOR UPPER AFT CUTOUT. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050616001972005061600197CE 2005 6 16 DJFA2005106 120050602A2731 TRIM SYSTEM RAYTHNDH125 HAWKER800XP 7150012CE ELEVATOR OUT OF ADJUST E DJFAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 EA23829LX 258466 DURING CLIMB, REACHED THE FORWARD LIMITS OF THE PITCH TRIM AT 190 KTS. AIRCRAFT DIVERTED TO CYYZ, AN EMERGENCY DECLARED. DURING THE FINAL APPROACH, THE RUDDER PEDALS WERE VIBRATING AND FELT AS THOUGH THEY WERE BINDING. THE CREW PERFORMED A NORMAL LANDING AND ROLL OUT. MAINTENANCE FOUND THE ELEVATOR TRIM TO BE OUT OF ADJUSTMENT. THE ELEVATOR TRIM SYSTEM WAS RIGGED. THE RUDDER SPRING STRUT WAS SERVICED AND THE SYSTEM WAS EXERCISED THROUGH FULL TRAVEL SEVERAL TIMES. NO DEFECTS WERE NOTED. THE SYSTEM CABLES AND BELLCRANKS WERE INSPECTED IN THE TAIL COMPARTMENT. A SATISFACTORY FLIGHT TEST WAS COMPLETED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA3EU 20050616001982005061600198WP 2005 6 16 ARWA20050602 120050607A7931396100S1D2 INDICATOR DOUG DC8 DC863F 302198FWP COCKPIT DEFECTIVE A ARWAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO19661AV 45969 PRIOR TO TAKEOFF SPOOLED ALL FOUR ENGINES; NR 1 ENGINE -0- OIL PRESSURE FOLLOWED BY ABNORMAL CHECKLIST. REMOVED AND REPLACED NR 1 OIL PRESSURE INDICATOR IN ACCORDANCE WITH M/M 79-32-0; OPERATIONAL CHECK IN ACCORDANCE WITH M/M 7100 FOUND NORMAL. 2L74 4F 4A25 20050616001992005061600199NM 2005 6 16 MWEA050047 120050607A1430591140213 RIVET BOEING717 717200 1383700NM FUSELAGE LIGHTNING STRIKEA MWEAK NONE O OTHER ININSP/MAINT 1 GL31903ME 55167 ONE EACH RIVET AT STATION 64-83 ABOVE LONGERON 18 LEFT HAS EVIDENCE OF A LIGHTNING STRIKE. HEAT DAMAGE HAS BEEN REMOVED AND INSTALLED RIVETS. 2L72 4F TRA6WE 20050616002012005061600201NM 2005 6 16 MWEA050049 120050607A5330591140885 SKIN BOEING717 717200 1383700NM FUSELAGE LIGHTNING STRIKEA MWEAK NONE O OTHER ININSP/MAINT 1 GL31903ME 55167 LIGHTNING STRIKE AT RIVET ATTACHMENT 3, 6 AND 10 FORWARD OF FRAME STATION 408 LONGERON 8 LEFT, FRAME STATION 541 LONGERON 7 LEFT AND FRAME STATION 560 BELOW LONGERON 5 LEFT. FABRICATED AND INSTALLED DOUBLER. 2L72 4F TRA6WE 20050616002042005061600204NM 2005 6 16 2005UALA00485 120050528A3350582233 BATTERY BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29121UA 29167 DOOR 3 LT, ZONE C EEL BATTERY INOP. BATTERY NOT HOLDING CHARGE. EEL LIGHT BATTERY REPLACED. 2L74 4F4 FRTA20WE E24NE 20050616002052005061600205NM 2005 6 16 2005UALA00487 120050529A5230 SKIN BOEING737 737322 1384676NM CFMINTCFM56 CFM562AFR 13802EU CARGO DOOR DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29313UA 23674 FWD CARGO DOOR HAS SEVERAL DENTS ON EXTERIOR SKIN. REPAIRED PER SRM52-30-01, LARGE 20 X 40 INCH DOUBLER INSTALLED ON OUTER EXT SKIN AT HMV-4. 2L72 4F4 FRTA16WE E21EU 20050616002062005061600206 2005 6 16 2005UALA00490 420050527A256560070102 TAPE AIRCRUISERS AIRBUS320 A320232 3930326EU EVAC SLIDE SEPARATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29430UA A7026 568 AFTER ONE (1) HOUR INTO AIR RETENTION TEST HINGE TAPE SEPARATED IN RAMP AREA. ADHESIVE FAILURE, RESULTED IN TAPE SEPARATION DURING THE PRESSURIZATION OF THE ASSEMBLY. UNIT WAS SENT TO OEM FOR REPAIR/DISPOSITION. 2L72 4F RTA28NM 20050616002072005061600207NM 2005 6 16 2005UALA00492 120050531A5313 STRINGER BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29503UA 24624 LT FUSELAGE STRINGER 16L IS CRACKED AT STA 610. REMOVED DAMAGE AND FABRICATED NEW STRINGER SECTION PER SRM 53-30-03. 2L72 4F4 FRTA2NM E17NE 20050719001802005071900180NM 2005 7 19 AALA20050434 120050710A3350 CONNECTOR BOEING757 757223 1384957NM EMERGENCY LIGHTSNOT SEATED A AALAK NONE O OTHER ININSP/MAINT 1 SW21691AA 25697 SEAT MOUNTED EMERGENCY LIGHT AT SEAT 24D INOPERATIVE. SECURED CONNECTOR AT SEAT 24F FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 24D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050616002102005061600210NM 2005 6 16 2005UALA00498 120050603A3350321454 EPSU AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29813UA 858 EEL LIGHTS INOPERABLE AT ROWS 15,16,19, 20, 23 & 24. THE EMERGENCY POWER SUPPLY UNIT (EPSU) WAS REPLACED AT DOOR 2R. 2L72 4F4 FRTA28NM E40NE 20050616002122005061600212SO 2005 6 16 LR7A05094 120050603A5320342590R FITTING LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 654 4763 DURING SCHEDULED B-1 CHECK INSPECTION PER JOB CARD HB5303 FOUND FS 792 RT SUPPORT BEAM TO SLOPING LONGERON LOWER ATTACHMENT T FITTING CRACKED. FITTING REPLACED IAW DRW 342590 AND SMP583 51-60 & 51-70. FS 792, RBL 62.5, WL 160.5-162. 2H74 4T A1SO 20050616002152005061600215 2005 6 16 VNAA0505003 420050519A2230 AUTOTHROTTLE SYS CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE COCKPIT MALFUNCTIONED A VNAAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 GL05725PS 10186 GEE965621 DURING TAKEOFF ROLL THE FLEX SETTING ON THE NR 1 ENGINE WAS LOST. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. THE FLEX SYSTEM WAS OPERATIONALLY CHECKED IAW CRJ 700 AMM 71-00-00-710-803-A01. THE SYSTEM OPS CHECKED GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050616002172005061600217EA 2005 6 16 VNAA0505006 120050522A2720 WARNING SYSTEM CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE COCKPIT MALFUNCTIONED A VNAAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 GL05706PS 10150 AFTER DEPARTING CLT THE CREW REPORTED A RUDDER LIMITER FAULT STATUS MESSAGE FOLLOWED BY A RUDDER LIMITER CAUTION MESSAGE. THE CREW RETURNED TO CLT. MAINTENANCE COMPLIED WITH INSTRUCTIONS FOUND IN BOMBARDIER CRJ700/900-SL-27-028REV A. THE SYSTEM OPS CHECKED GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050616002182005061600218EA 2005 6 16 VNAA0505005 120050520A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE LIGHTNING STRIKEA VNAAK NONE O OTHER UKUNKNOWN 1 GL05223JS 7892 DURING POST FLIGHT INSPECTION THE CREW REPORTED EVIDENCE OF A LIGHTNING STRIKE ON THE FRONT LEFT NOSE SECTION OF THE FUSELAGE. THE AIRCRAFT WAS FERRIED TO DAY WHERE LIGHTNING STRIKE INSPECTIONS WERE COMPLIED WITH IAW CRJ 200 AMM 05-51-05-210-801 AND 05-51-05-220-801. ALL DISCREPANCIES WERE REPAIRED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050616002192005061600219NM 2005 6 16 DL76L050295 120050527A2120 ODOR BOEING767 767332 1382001NM CABIN DETECTED A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO27185DN 27961 F/A REPORTED STRONG ODOR FROM 1L AREA DURING DESCENT. BOTH AIR CONDITIONING PACKS CYCLED. NIL FAULTS FOUND. FWD CABIN AREA CHECKED. NIL FAULTS FOUND. BOTH CARGO HOLDS CHECKED. ALSO NIL FAULTS FOUND. 2L72 4F RTA1NM 20050616002202005061600220NM 2005 6 16 DL76L050296 120050528A3242 DISC BOEING767 767332 1382001NM NR 2 BRAKE DAMAGED A DALAK NONE Z SIGNIFICANT FAILURE REPORT ININSP/MAINT 1 SO27198DN DL1894 28455 ON ARRIVAL IN MADRID WALKAROUND PDC 2 INSPECTION, FOUND NR 2 BRAKE INNER ROTOR DISC DAMAGED. KEYS SHEARED OFF. REPLACED BRAKE. 2L72 4F RTA1NM 20050616002232005061600223NM 2005 6 16 DLM88050298 120050530A2120 DUCT DOUG MD88 MD88 3023688NM A/C BAY BIRD INGESTION A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27913DL 49544 ATB DUE TO OVER POWERING STENCH OF ROASTED BIRD AFTER TAKEOFF, OUT OF LGA. PERFORMED DUCT BURNOUT. 2L72 4F RTA6WE 20050616002252005061600225NM 2005 6 16 DL764050299 120050531A3350 LIGHT BOEING767 767432ER 1385134NM EXTERIOR INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27830MH 29701 THE 2L EMERGENCY LIGHT EXTERIOR INOP. 2L72 4F RTA1NM 20050616002282005061600228NM 2005 6 16 DL764050300 120050601A2121732591F FAN BOEING767 767432ER 1385134NM CARGO BAY FAILED A DALAK NONE BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 SO27833MH 29706 FAINT ELECTRICAL SMELL NOTICED INFLIGHT. FWD EQ EXHAUST FAN STATUS MESSAGE APPEARED. SMELL DISSIPATED. REPLACED FWD EQ EXHAUST FAN. 2L72 4F RTA1NM 20050616002292005061600229NM 2005 6 16 DL76L050301 120050601A324226124121A BRAKE BOEING767 767332 1382001NM NR 4 FIRE A DALAO OTHER A FLAME/FIRE ININSP/MAINT 1 SO27190DN 28447 ARRIVAL WITH A/C PARKED AT GATE NUMBER 4 BRAKE FIRE. REPLACED BRAKE. 2L72 4F RTA1NM 20050616002302005061600230NM 2005 6 16 DLM88050302 120050602A2910 O-RING DOUG MD88 MD88 3023688NM RT MLG WW LEAKING A DALAK NONE K FLUID LOSS APAPPROACH 1 SO27940DL 49813 RIGHT HYD SYSTEM ENG DRIVEN PUMP INOP W/AUX PUMP OFF QTY 6. WHEN AUX PUMP ON QTY 3. WHEN ATTEMPTING TO PRESSURIZE SYS FOR GEAR EXTENSION PRESS WAS AT ZERO AND QTY WAS AT 3. REPLACED O-RING ON RIGHT SPOILER PRESSURE REDUCING VALVE. ALSO REPLACED AUX PUMP AND RIGHT EDP. 2L72 4F RTA6WE 20050616002312005061600231NM 2005 6 16 DLM88050303 120050602A38108256M4 COMPRESSOR DOUG MD88 MD88 3023688NM POTABLE WATER FAILED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27950DL 49881 AT FL 340 CRUISE FLIGHT COCKPIT DETECTED ELECTRICAL SMELL. REPLACED FAILED POTABLE WATER SYSTEM COMPRESSOR. 2L72 4F RTA6WE 20050616002322005061600232NM 2005 6 16 DL76S050304 120050603A2820 SWITCH BOEING767 767332 1382001NM COCKPIT BURNED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27132DN 24981 RIGHT FWD FUEL BOOST PUMP SWITCH REMOVED AND EVIDENCE OF BURNING NOTED AND PLASTIC MELTED. REPLACED SWITCH AND REPAIRED WIRING. 2L72 4F RTA1NM 20050616002362005061600236NE 2005 6 16 DL76P050307 220050604A73106355132A COUPLING BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE RT ENGINE CRACKED A DALAA UNSCHED LANDING K FLUID LOSS CRCRUISE 1 SO27140LL 25988 FUEL LEAK COMING FROM RT ENGINE AREA. FOUND RT ENGINE FUEL FEED TUBE COUPLING BROKEN. REPLACED SAME. 2L72 4F4 FRTA1NM E24NE 20050616002372005061600237NM 2005 6 16 DL738050308 120050605A2750113A39102 BELLCRANK BOEING737 737832 13844CFNM T/E FLAP BROKEN A DALAO OTHER F FLT CONT AFFECTED LDLANDING 1 SO273753 29671 CREW VERBAL A/C TOOK 2 DEGREES TRIM WITH FLAPS DOWN ON LANDING. FOUND WITH FLAPS DOWN RIGHT O/B FLAP I/B ATTACH POINT BELLCRANK BROKEN. REPLACED SAME. 2L72 4F RTA16WE 20050616002382005061600238NM 2005 6 16 DL764050310 120050606A2730271040020 COMPUTER BOEING767 767432ER 1385134NM E/E BAY FAULTY A DALAA UNSCHED LANDING O OTHER TOTAKEOFF 1 SO27841MH 8 29714 CREW REPORTED SHORLTY AFTER T/O STATUS MSG ELEV FEEL. REPLACED ELEVATOR FEEL COMPUTER. 2L72 4F RTA1NM 20050616002402005061600240NM 2005 6 16 UPS05444621 120050519A5320BAC1509100312 FLOOR SUPPORT BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C M/D - BS 550 LBL 11 - RBL 11 FLOOR SUPPORT HAT SECTION FOUND CORROSION BLEND OUT: 0.016 X 1 X 1.5 INCH. HAT SECTION REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050616002422005061600242NM 2005 6 16 UPS05444623 120050519A5320BAC1509100312 FLOOR SUPPORT BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C M/D BS 550 LBL 11 - 33 FLOOR SUPPORT HAT SECTION FOUND CORROSION. CORROSION BLEND OUT 0.012 X .875 X 1.75 INCH HAT SECTION REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050616002442005061600244NM 2005 6 16 UPS05444625 120050519A5320BAC1509100312 FLOOR SUPPORT BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C M/D BS 570 RBL 11-33 FLOOR SUPPORT HAT SECTION FOUND CORRODED. CORROSION BLEND OUT: 0.026 X .875 X 1.25 INCH. HAT SECTION REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050616002462005061600246NM 2005 6 16 UPS05444627 120050519A5347 SEAT TRACK BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C M/D - BS 860-980 RBL 97 SEAT TRACK I/B FLANGE CORRODED. CORROSION BLEND OUT: 0.028 X 1 X 2 INCH. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A FROM BS 850-990 RBL 97 INCH. 2L74 4F A20WE 20050616002482005061600248NM 2005 6 16 UPS05444629 120050601A532065B0794233 STIFFENER BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C NWW LT SIDE WALL PANEL BS 280 TO 300 NR 4 HORIZONTAL STIFFENER (COUNT FROM TOP) 1 EA FASTENER HOLE FOUND CRACKED (CRACK LENGTH .0625 INCH). NWW LT SIDE WALL PANEL BS 280 TO 300 NR 4 HORIZONTAL STIFFENER REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050616002502005061600250NM 2005 6 16 UPS05444631 120050601A532065B0794234 STIFFENER BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C NWW RT SIDE WALL PNL BS 300 TO BS 320 NR 4 HORIZONTAL STIFFENER (COUNT FROM TOP) 1 EA FASTENER HOLE FOUND CRACKED AS MARKED (CRACK LENGTH .0625 INCH). NWW RT SIDE WALL PNL BS 300 TO BS 320 NR 4 HORIZONTAL STIFFENER REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050616002522005061600252NM 2005 6 16 UPS05444633 120050601A532065B0792434 STIFFENER BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C NWW RT SIDE WALL PNL BS 280 TO BS 300 NR 3 HORIZONTAL STIFFENER (COUNT FROM TOP) 2 EA FASTENER HOLES FOUND CRACKED AS MARKED (CRACK LENGTH .0625 INCH). NWW RT SIDE WALL PNL BS 280 TO BS 300 NR 3 HORIZONTAL STIFFENER REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050616002542005061600254NM 2005 6 16 UPS05444635 120050601A532065B0794233 STIFFENER BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C NWW LT SIDE WALL PANEL BS 300 TO 320 NR 3 HORIZONTAL STIFFENER (COUNT FROM TOP) 1 EA FASTENER HOLE FOUND CRACKED (CRACK LENGTH .0625 INCH). NWW LT SIDE WALL PANEL BS 300 TO 320 NR 3 HORIZONTAL STIFFENER REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050615001372005061500137EA 2005 6 15 ASOA05418 120050508A5320601R3501153 PLATE CNDAIRCL600 CL600* EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27867AS 7463 DURING A C-CHECK IN MCN, THE CARGO DOOR FLOOR LANDING PLATE WAS FOUND TO BE CRACKED AT RIVET FS 605. MAINTENANCE IS REPAIRING THE CARGO DOOR FLOOR LANDING PLATE AT FS 605 IAW ASA EO 600-53-0117. (M) 2L72 4F RTA21EA 20050616000012005061600001NM 2005 6 16 DU4R104 120050527A5320 FLOOR SUPPORT BOEING737 7373L9 1384470NM FUSELAGE CORRODED B DU4RK NONE O OTHER ININSP/MAINT 1 SO15312FL 24569 CORROSION AT FLOORBOARD SUPPORT ANGLE FROM BS 949 TO 1000 RBL 68.0. S/O 109001, N/R 22787 2L72 4F RTA16WE 20050616000032005061600003NM 2005 6 16 DU4R05105 120050527A5511 BUSHING BOEING737 7373L9 1384470NM HORIZONTAL STAB CORRODED B DU4RK NONE O OTHER ININSP/MAINT 1 SO15312FL 24569 LT HORIZONTAL STAB FRONT SPAR, UPPER ATTACH BOLT BORE, BUSHINGS HAVE PITTING CORROSION. S/O 109001, N/R 22971. 2L72 4F RTA16WE 20050616000182005061600018CE 2005 6 16 ENHA0515 120050501A2420DOFF10300BR ALTERNATOR CESSNA207 207A 2073604CE ENGINE MALFUNCTIONED E ENHAO OTHER O OTHER NRNOT REPORTED 1 AL039651M 2 20700715 ALTERNATOR LOW VOLTAGE. 1H71 3O A16CE 20050616000302005061600030NM 2005 6 16 SWAA051656 120050604A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29401WN 29813 EEPLS COVER DAMAGED AT ROW 1. REMOVED AND REPLACED COVER PER MM. 2L72 4F RTA16WE 20050616000382005061600038NM 2005 6 16 SWAA051677 120050607A53306545777 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 971, STR 21L. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050616000412005061600041 2005 6 16 SWAA051680 420050607A256565C16820 GIRT BAR BOEING737 7373H4 1384600NM R1 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29352SW 24888 DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED GIRT BAR HOOK PER MM. 2L72 4F RTA16WE 20050616000562005061600056NM 2005 6 16 SWAA051690 120050608A3350BR9442 LAMP BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29370SW 26597 DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EXTERNAL EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050616000652005061600065NM 2005 6 16 AWXA200500645 120050521A5753654643512 STRUCTURE BOEING737 737301 1384611NM T/E FLAP DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 DURING C-19 CHECK, THE RT OUTBOARD FLAP INBOARD LOWER CORNER WAS FOUND DELAMINATED. MAINTENANCE REMOVED DAMAGE ON RT OUTBOARD FLAP INBOARD LOWER CORNER, FABRICATED REPAIR CORE AND EXTERNAL DOUBLER, BONDED REPAIR PARTS TO FLAP IAW BOEING SRM 51-70-10 FIG 16. 2L72 4F RTA16WE 20050616000662005061600066NM 2005 6 16 SWAA051582 120050527A53206545410 FLOOR SUPPORT BOEING737 7373H4 1384600NM CABIN FLOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND CABIN LONGITUDINAL FLOOR SUPPORT UPPER TEE CRACKED AT BS 663, BL 0, WL 208. REPAIRED FLOOR SUPPORT PER BFG ER. 2L72 4F RTA16WE 20050616000782005061600078NM 2005 6 16 AWXA200500654 120050413A5320141N516078 CHANNEL BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28902AW 23322 DURING C-10 CHECK, EXFOLIATION CORROSION WAS FOUND INBOARD OF R1 DOOR THRESHOLD ON SUPPORT CHANNEL BETWEEN BS 324 AND BS 345. MAINTENANCE REMOVED CORRODED R1 DOOR THRESHOLD SUPPORT CHANNEL FROM BS 324 TO BS 345; FABRICATED A NEW REPLACEMENT SUPPORT CHANNEL; AND INSTALLED REPAIR PART IAW BOEING 757 SRM 51-40-02. 2L72 4F RTA2NM 20050616000962005061600096NM 2005 6 16 AWXA200500669 120050607A3350BR944411 LIGHT BOEING737 7373G7 1384595NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28156AW 23778 DEN - EEL - DURING 4 DAY DISCOVERED ROW 8 SEAT MOUNTED EMERGENCY ESCAPE LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20050616000972005061600097NM 2005 6 16 AWXA200500670 120050601A3350 LIGHT AIRBUSA319 A319132 3930340NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28831AW 1576 PHX - EEL - DURING PHASE 8 CHECK, AFT EMERGENCY LIGHTS FAILED TO ILLUMINATE DURING STEP 11 OF PHASE GENERAL TASK CARD. 2L72 4F RTA28NM 20050616001002005061600100EU 2005 6 16 AWXA200500672 120050605A3350 LIGHT AIRBUS320 A320232 3930326EU CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28604AW 1196 SEAT 24 ABC, SEAT MOUNTED EMERGENCY LIGHT INOP, BULBS GOOD. 2L72 4F RTA28NM 20050616001032005061600103EU 2005 6 16 AWXA200500674 120050520A5321D5367302900000 FLOOR PANEL AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28639AW 471 DURING C-8 CHECK, FOUND CORROSION ON LOWER SURFACE OF SIDE WALL PANEL 152 MF FROM FS 56 TO FS 58. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS. REMOVED CORRODED PANEL AND FABRICATED REPLACEMENT FLOOR PANEL. INSTALLED FABRICATED REPAIR PARTS WITH ORIGINAL DOUBLER PROTECTIVE COVER IAW IRM 9701 REV F. 2L72 4F RTA28NM 20050616001062005061600106EU 2005 6 16 AWXA200500676 120050506A5321D5361033200900 FLOOR PANEL AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28639AW 471 SAL - MAJOR REPAIR - DURING C-8 CHECK FOUND CORROSION ON FLOOR PANEL 222FF LOCATED IN FORWARD GALLEY FROM FR 16 TO FR 20. MAINTENANCE BLENDED OUT DAMAGED AREA ON FLOOR PANEL 222FF LOCATED IN FORWARD GALLEY FROM FR 16 TO FR 20 AND FABRICATED REPAIR DOUBLER IAW AMERICA WEST ENGINEERING REPAIR NO. 26-5312-000151-BA1A. FABRICATED REPAIR PARTS WERE INSTALLED IAW AMERICA WEST ENGINEERING REPAIR NO. 26-5312-000151-BA1A. 2L72 4F RTA28NM 20050616001082005061600108NM 2005 6 16 AWXA200500678 120050602A5320654583311 WEB BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 DURING C-21 CHECK, FOUND FLOOR WEB CRACKED AT BS 196.5, WL 207, RIGHT BL 28. MAINTENANCE REMOVED CRACKED FLOOR WEB AT BS 196.5, WL 207, RIGHT BL 28 AND FABRICATED NEW WEB IAW BOEING 737-300 SRM 51-40-02 FIGURE 2 AND DWG 65-45833. INSTALLED FABRICATED REPAIR PARTS AT BS 196.5, WL 207, RIGHT BL 28 IAW BOEING 737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050616001152005061600115NM 2005 6 16 05FDEA00658 120050328A5347AFA7789542 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 CABIN, STA 1961 RIGHT SEAT TRACK FOUND CORROSION AS MARKED AS RBL 77. CORROSION ON SEAT TRACK AT STA 1961 RBL 77 REMOVED & FOUND EXCEED LIMIT AS PER SRM 53-70-00 FIG 3 VOL I. DISCREPANT SEAT TRACK TRIM-OUT AT STA 1831 RBL 107 AS PER SRM 53-10-00 FIG 1 VOL I. NEW SEAT TRACK REWORKED FROM AFA 7789-542 AS PER SRM 53-70-00 FIG 7 VOL I. SPLICE ANGLE REWORKED FROM S4932154-7075T6511. FABRICATED SPLICE PLATE AS PER SRM 53-70-00 FIG 1 VOL I. HOLES PICK UP ON NEW SEAT TRACK & REPAIR PARTS AS PER SRM 51-31-01 VOL II. NEW SEAT TRACK & REPAIR PARTS LOCATED & INSTALL AS PER SRM 53-20-00 FIG 1 VOL I. MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050616001172005061600117NM 2005 6 16 05FDEA00676 120050328A5347AFA7795507 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 MAIN DECK, ALONG STA 1821 TO STA 1887 RBL 8.5 SEAT TRACK FOUND CORRODED. CORROSION ON SEAT TRACK AT STA 1821 TO 1887 REMOVED & FOUND EXCEED LIMIT AS PER SRM 53-70-00 FIG 3 VOL I. DISCREPANT SEAT TRACK FROM STA 1811 TO 1887 RBL 8.5 TRIM OUT AS PER SRM 53-70-00 FIG 1 VOL I. HFEC CARRIED OUT ON TRIM-CUT AREA AS PER DAC NDT SPM REV 11 06-10-01-001 AND FOUND NO CRACK EVIDENT. NEW SEAT TRACK AND SPLICE ANGLE REWORKED FROM S4929147 AND S4932154 AS PER SRM 53-70-00 FIG I. NEW SEAT TRACK AND SPLICE ANGLE PAINTED AS PER SRM 51-21-01 VOL II. REPAIR PARTS LOCATED AND INSTALLED AS PER SRM 53-70-00 FIG 1 VOL I. MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050616001202005061600120NM 2005 6 16 05FDEA00678 120050328A5347AFA7T95507 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 MAIN DECK, ALONG STA 1821 TO STA 1887 LBL 8.5 SEAT TRACK FOUND CORRODED. CORROSION ON SEAT TRACK ALONG STA 1821 TO 1887 LBL 8.5 REMOVED & FOUND EXCEED LIMITED AS PER SRM 53-70-00 FIG 3 VOL I. DISCREPANT SEAT TRACK TRIM-OUT AT STA 1811 LBL 8.5 AS PER SRM 53-70-00 FIG 1 VOL I. NEW SEAT TRACK REWORKED FROM S4929147-7075T6511 AS PER SRM 53-70-00 FIG 1 VOL I. SPLICE PLATE FABRICATED FROM 7075T6-0.050 AS PER SRM 53-70-00 FIG I. HOLES PICK-UP ON NEW SEAT TRACK & REPAIR PARTS AS PER SRM 51-31-01 VOL II. NEW SEAT TRACK AND REPAIR PARTS LOCATED AND INSTALL AS PER SRM 53-70-00 FIG 1 VOL I. MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050616001222005061600122NM 2005 6 16 05FDEA00695 120050329A5347ACA7101509 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 MAIN DECK, BETWEEN STA 804 AND STA 841 LBL 107.25 SEAT TRACK CROWN AND BASE FOUND CORRODED. CORROSION ON SEAT TRACK BETWEEN STA 804 TO 841 LBL 107 REMOVED & FOUND EXCEED LIMIT AS PER SRM 53-70-00 FIG 3 VOL I. DISCREPANT SEAT TRACK TRIM-OUT FROM STA 765 TO 889 LBL 107 AS PER SRM 53-70-00 FIG 3 VOL I. NEW SEAT TRACK AND SPLICE ANGLE REWORKED FROM S4929148-7075T6511 AND S4932154-7075T6511 AS PER SRM 53-70-00 FIG 1 VOL I. SPLICE PLATE FABRICATED FROM 7075T6-0.05 AS PER SRM 53-70-00 FIG 1 VOL I. NEW SEAT TRACK AND REPAIR PARTS LOCATED AND INSTALLED AS PER SRM 53-70-00 FIG 1 VOL I. MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050616001242005061600124NM 2005 6 16 05FDEA00700 120050329A5347ADA83891 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25576FE 48501 MAIN DECK, AT STA 822 RBL 44.5 SEAT TRACK CROWN FOUND CORRODED. CORROSION ON SEAT TRACK CROWN STA 822 RBL 44.5 REMOVED & FOUND EXCEED LIMIT AS PER SRM 53-70-00 FIG 3 VOL I. DISCREPANT SEAT TRACK TRIM-OUT FROM STA 815 TO 832 RBL 44.5 AS PER SRM 53-70-00 FIG 1 VOL I. REPAIR PARTS REWORKED FROM S4929147-7075T6511 AND S4932154-7075T6511 AND FABRICATED SPLICE PLATE FROM 7075T6-0.050 AS PER SRM 53-70-00 FIG 1 VOL I. REPAIR PARTS REPROTECTED AS PER SRM 51-21-01 VOL II AND INSTALLED AS PER SRM 53-70-00 FIG 1 VOL I. FLOOR PANEL INSTALLED ALONG STA 822 RBL 44.5 AS PER AMM 53-21-04. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 AND SRM 51-90-01 FIG 1 VOL II. 2L73 4F RTA22WE 20050616001262005061600126NM 2005 6 16 05FDEA01475 120050527A5310 BEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 A 9G FITTING CORRODED, BS 266, LBL 5, WL 208. REMOVED AND REPLACED G-BEAM PER SRM 51-30-2. 2L73 4F RTA3WE 20050616001282005061600128NM 2005 6 16 05FDEA01498 120050531A5753 VANE DOUG MD11 MD11 3023602NM T/E FLAP DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 RIGHT HAND WING INBOARD FLAP VANE FOUND DELAMINATED OF ABOUT 57 INCHES LONG BY 28 INCHES WIDE AT LOWER OUTBOARD SURFACE. 2L73 4F RTA22WE 20050616001562005061600156NM 2005 6 16 05FDEA01501 120050601A7711 UNKNOWN BOEING727 727200 138407ENM NR 3 ENGINE MALFUNCTIONED A FDEAC ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 SO25220FE 20934 ENGINE NR 3 EPR SETTING WOULD NOT GO TO 2.13 WHEN SET TO MAX POWER FOR T/O. REJECTED T/O BELOW 60 KTS. MAX EPR ONLY REACHED 2.05 AT MECHANICAL STOPS. EXECUTED THE RTO PROCEDURES FROM THE QRH IN ACCORDANCE WITH PROCEDURES. PERFORMED WET MOTORED DRY MOTORED, AND IDLE LEAK CHECK, PERFORMED RICK CHECKED FOUND OK. AS PER M/M 73-21-000-4; PERFORMED HIGH POWER RUN ON NR 3 ENGINE, ALL PARAMETERS NORMAL AS PER JRH 6-39. ALL TEST NORMAL. 2L73 4F RTA3WE 20050616001712005061600171NM 2005 6 16 05FDEA01503 120050601A5534 TIE BOEING727 727200 138407ENM VERTICAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 CORROSION, VERTICAL FIN TENSION TIE RIGHT FWD BOLT HOLE HAS CORROSION ON FACE OF TENSION TIE LUGS UNDER NUT & BOLT HEAD SIDE. REPAIRED TENSION TIE PER FED EX EA 7-5530-86296. 2L73 4F RTA3WE 20050616002032005061600203CE 2005 6 16 71141 120050603A27101295240051 SPRING RAYTHN BEECH 1900 1900D 1154162CE AILERON/RUDDER BROKEN A AMWAK NONE F FLT CONT AFFECTED CLCLIMB 1 CE07138YV19041 UE138 CREW REPORTED DURING INTERMEDIATE CLIMB, IT TOOK FULL RIGHT AILERON TRIM TO KEEP THE AIRCRAFT WINGS LEVEL. CREW NOTED NO CONTROLLABILITY PROBLEMS. CRUISE TRIM SETTING APPEARED MORE NORMAL AT 3 RIGHT. AIRCRAFT REQUIRED NO AILERON RETRIMMING DURING DESCENT. MAINTENANCE FOUND THE FORWARD AILERON/RUDDER INTERCONNECT SPRING BROKEN. THE BREAK OCCURRED BETWEEN THE HOOK OF THE SPRING AND THE COILS OF THE SPRING. REPLACED FORWARD SPRING IN ACCORDANCE WITH THE BEECH CRAFT MAINTENANCE MANUAL. A TEST FLIGHT WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA24CE 20050616002142005061600214EA 2005 6 16 VNAA0504008 120050430A3244299K631 TIRE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT MLG SEPARATED A VNAAO OTHER O OTHER LDLANDING 1 GL05241PS249 7909 DURING POSTFLIGHT INSPECTION AFTER LANDING AT PHL, THE CREW OF FLIGHT 2437 (PWM TO PHL) REPORTED THAT TREAD WAS MISSING FROM THE RT INBOARD MLG TIRE AND THE RT INBOARD FLAP WAS DENTED. PSA MAINTENANCE REMOVED AND REPLACED THE RT INBOARD MLG WHEEL & TIRE ASSEMBLY IAW CRJ200 AMM 32-41-01-400-801. THE AIRCRAFT WAS THEN FERRIED TO CAK WHERE PSA MAINTENANCE REMOVED AND REPLACED THE RT INBOARD FLAP IAW CRJ200 AMM 27-54-01-400-801. THE OPERATIONAL CHECK WAS GOOD IAW CRJ200 AMM 27-54-00-710-801. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050616002212005061600221NM 2005 6 16 DL75K050297 120050528A2910271N61192 HYDRAULIC LINE BOEING757 757232 1384965NM LT MLG LEAKING A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO27685DA 27588 ON CLIMBOUT AT 15,000 HAD L HYD QTY STATUS MSG THE LEFT RESEVOIR STEADILY DECLINED TO .10. THEN RECEIVED L HYD SYS PRESS LIGHT. EXECUTED ALL QRM PROCEDURES INCLUDING ALT FLAP AND GEAR EXTENSION. FOUND LEFT MLG DOWN LOCK ACTUATOR LINE LEAKING. REPLACED HYD LINE, LEAK CHECKS OK. P/N 321204329 2L72 4F RTA2NM 20050616002342005061600234NM 2005 6 16 DLM88050306 120050604A2916 RESERVOIR DOUG MD88 MD88 3023688NM HYDRAULIC SYS CONTAMINATED A DALAO OTHER O OTHER LDLANDING 1 SO27954DL 49885 LEFT HYD PSI WENT TO ZERO AT SLAT EXTENSION. FOUND LARGE AMOUNT OF AIR IN LEFT HYD RESERVIOR. BLED LEFT HYD SYSTEM AND OPS CHECK OK. 2L72 4F RTA6WE 20050616002682005061600268NM 2005 6 16 UPS05444654 120050519A5711 SPLICE BOEING747 747123F NM LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C LEFT BS 1241 WING REAR SPAR UPPER SPLICE BOLT HOLE NR 8 CRACKED AT CHORD (CRACK LENGTH 0.08 INCH). HOLE REWORKED AS PER EO B747-5740-17032-C. 2L74 4F A20WE 20050616002722005061600272NM 2005 6 16 USAA050647 120050502A534765B578392 GALLEY TRACK BOEING757 757225 1384959NM RROYCERB211 RB211535E4 54555NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19608AU64222 22204 BFM - C4 - GALLEY MOUNT PAD, 1.5 INCH L X .5 INCH W X .035 INCH D. CORROSION; NO LEVEL OR TASK, STA 330, LBL 21. REMOVED AND REPLACED IAW SRM. (K) 2L72 4F4 FRTA2NM E12EU 20050616002732005061600273NM 2005 6 16 UPS05444662 120050516A5330 LAP JOINT BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C FX SKIN LAP JOINT FOUND CORROSION AT BS 398 - 400 STR 19L AROUND 2 EA FASTENERS AS MARKED (APPROX 15 PERCENT MATERIAL LOSS). CORROSION BLEND OUT 0.016 X 1.125 X 2.25 INCH EXCEED EO B747-5330-20503-D LIMITS. FX BS 388 TO BS 400 STR 19L SKIN REPAIRED AS PER HX RS R53-11-35313 & UPS EO B747-5330-22315-A. 2L74 4F A20WE 20050617000022005061700002NM 2005 6 17 USAA05686 120050522A5315 FLOORBEAM BOEING757 7572B7 1384964NM RROYCERB211 RB211535E4 54555NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19614AU 27145 BFM - C4 - FLOORBEAM UPPER CHORD, 1.5 L X 2.0 W X .020, 1.5: X 2 W X .029, 2L, CORROSION (3 AREAS); LEVEL 1; TASK C53-251-03, STA 1640 FROM BL0 - RBL 60. REPLACED UPPER CHORD SECTION IAW TYP REP. (K) 2L72 4F4 FRTA2NM E12EU 20050617000042005061700004NM 2005 6 17 USAA050735 120050525A5320415N40026 SUPPORT FITTING BOEING757 7572B7 1384964NM RROYCERB211 RB211535E4 54555NE GALLEY CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19614AU 27145 BFM - C4 - GALLEY SUPPORT FITTINGS, .6 INCH L X .2 INCH W X .032 INCH D, .2 INCH L X .2W X .032, CORROSION; NO LEVEL OR TASK, STA 1686, RBL 6.5 AND LBL6.5. REPLACED GALLEY SUPPORT FITTINGS IAW SRM. (K) 2L72 4F4 FRTA2NM E12EU 20050617000062005061700006NM 2005 6 17 QXEA200501054 120050601A5330 SKIN BOMBDRDHC8 DHC8402 1390042NM ZONE 200 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09415QX 4081 DENT IN FUSELAGE APPROXIMATELY 8 INCHES BELOW PASSENGER WINDOW (LAST WINDOW ON LEFT SIDE OF FUSELAGE, JUST PRIOR TO AFT PASSENGER DOOR). REPAIRED IAW Q400 SRM 51-25-05-370-801 AND HORIZON AIR EA 6-53-554, RD 8/4-53-1255. 2H72 4T RTA13NM 20050617000082005061700008CE 2005 6 17 DXTA200500755 120050605A3230 LANDING GEAR RAYTHNDH125 HAWKER800XP 7150012CE LEFT MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07873QS 258573 LT MAIN GEAR WOULD NOT RETRACT FULLY. AFTER 6 MINUTES THE RED LIGHT WENT OUT BUT BASED ON POWER AND FUEL FLOW SETTINGS AND SPEEDS REFLECTED EXTRA DRAG. ON PUTTING THE GEAR DOWN THE FIRST ONE TO LOCK WAS THE LEFT. JACKED ACFT & SWUNG GEAR APPROX 15 TIMES GEAR CHECKED GOOD. CHECK RIGGING ON GEAR DOOR SEQUENCE VALVE & REVERSING VALVE, CHECKED GOOD. CHECKED SIDESTAY CLEARANCES GOOD. RIGGED UPLOCK SPRING LATCH AS REQUIRED. ALL WORK DONE REFERENCING THE 800XP MM CHAP 29-10-00, 32-10-65, 32-30-31, 32-30-41 AND 32-10-41. COULD NOT DUPLICATE SQUAWK DOWN JACKED AIRCRAFT. 2L72 4F RTA3EU 20050617000092005061700009NM 2005 6 17 CALA0500187 120050607A5320BAC1505100849 FLOOR SUPPORT BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2727213 28773 INSPECTION FOUND FLOOR SUPPORT CORRODED AROUND NUT PLATE AT STA 986, LBL 43. REPAIRED IAW ECRA 5321-01230. 2L72 4F RTA16WE 20050617000392005061700039NM 2005 6 17 CALA0500188 120050607A5320BAC1509 SUPPORT ANGLE BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2727213 28773 INSPECTION FOUND SUPPORT ANGLE CORRODED AT STA 1000, RBL 32. A NEW ANGLE WAS INSTALLED IAW DRAWING 147A5710, SRM 51-20-01, AND 51-40-02. 2L72 4F RTA16WE 20050617000422005061700042NM 2005 6 17 CALA0500191 120050608A5310141A81121 FRAME BOEING737 737824 13844BZNM THRESHOLD CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2727213 28773 INSPECTION FOUND R-1 DOOR FLOOR CUTOUT THRESHOLD FRAME CORRODED AT STA 290-300, RBL 48. THE THRESHOLD FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20050617000432005061700043CE 2005 6 17 DXTA200500756 120050606A2910AE366323E0113 LINE CESSNA560 560XL 2076702CE HYDRAULIC SYS LEAKING E DXTAD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 GL07676QS 5605176 LEFT BRAKE PEDAL (PILOTS SIDE) DEPRESSED TO FLOOR WITH NO RESISTANCE AND NO BRAKING UPON LANDING. DURING TAXI, PEDAL WAS DEPRESSED TO FLOOR WITH NO RESISTANCE OR BRAKING. RIGHT SIDE PEDAL OK, RIGHT SEAT L/R PEDAL OK. FOUND COPILOT, LEFT BRAKE PEDAL, UPPER BRAKE FLEX LINE FAILED AND LEAKING SKYDROL. REMOVED AND REPLACED BRAKE FLEX LINE USING NEW LINE ASSY. BLED BRAKES AND ANTISKID SYSTEM USING CESSNA BRAKE BLEEDING FIXTURE. BRAKE OPERATIONAL CHECKS GOOD. TAXI CHECK GOOD. ALL WORK PERFORMED IAW CESSNA 560XL MM CH 32-42-00 AND 32-44-20. 2L72 4F RTA22CE 20050617000492005061700049NM 2005 6 17 PCSA06080501 120050606A2797 CONNECTOR BOEING727 727233 138408ANM FLAP INDICATOR DIRTY A PCSAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO29495AJ 20937 FLIGHT 8113 TTPP/SVMC - AFTER DEPARTURE FROM TTPP, CREW REPORTED UNABLE TO RETRACT OUTBOARD FLAPS FROM 5 DEGREES. RETURNED AIRCRAFT TO TTPP USING THE SPLIT FLAP ALTERNATE PROCEDURE IAW AMERIJET 727 AIRCRAFT OPS MANUAL CHAPTER 5 PAGE 53 AND 54. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED INDICATOR CONNECTOR , CLEANED AND RESEATED. PERFORMED OPERATIONAL CHECK NORMAL IAW MM CHAPTER 27-51-00. AIRCRAFT RETURNED TO SERVICE. 2L73 4F RTA3WE 20050617000502005061700050EA 2005 6 17 VTZA200500107 120050607A2613355924400 ELEMENT CNDAIRCL600 CL6002B19 1900309EA LT PYLON FAILED A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27622BR 7187 LT 14TH STAGE DUCT FAILURE MESSAGE. EMERGENCY DECLARED. REMOVED AND REPLACED LT PYLON 14TH STAGE BLEED AIR LOOP. 2L72 4F RTA21EA 20050617000512005061700051 2005 6 17 VTZA200500108 420050608A3418 COMPUTER CNDAIRCL600 CL6002B19 1900309EA STALL WARNING MALFUNCTIONED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27701BR 7448 STALL FAIL MSG POSTED AFTER T/O. FOUND NO FAULTS LOGGED ON STALL SYSTEM. RESET STALL COMPUTER AND NO FURTHER DEFECTS NOTED AT THIS TIME. 2L72 4F RTA21EA 20050617000532005061700053EA 2005 6 17 VNAA0505007 120050522A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE UNKNOWN A VNAAA UNSCHED LANDING F FLT CONT AFFECTED NRNOT REPORTED 1 GL05206PS 7860 INBOUND TO DCA THE FLAPS FAILED AT 20 DEGREES. THE CREW ELECTED TO DIVERT TO IAD. MAINTENANCE TROUBLESHOT THE SYSTEM IAW CRJ 200 FIM 27-50-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050617000562005061700056EA 2005 6 17 VNAA0505012 120050525A2741 TRIM SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE STAB UNKNOWN A VNAAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 GL05242JS 7911 STABILIZER TRIM FAILED IN FLIGHT AND THE MACH TRIM DISENGAGED. MAINTENANCE OPERATIONALLY CHECKED THE STAB TRIM SYSTEM IAW BOMBARDIER RJ-SL-00-001. THE SYSTEM CHECKED GOOD AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050617000572005061700057NM 2005 6 17 05FDEA01554 120050608A5310 DOOR FRAME DOUG MD11 MD11 3023602NM CARGO BAY DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25631FE 48454 AT DOOR JAMB AFT CARGO DOOR STA 1959 LOWER EXISTING DENT/SCRATCH, BLEND OUT. REPAIRED AS PER SRM 53-00-00 VOL I FIG 16 (SHT 9). MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050617000612005061700061EU 2005 6 17 05FDEA01568 120050609A7931 INDICATION SYS AIRBUS310 A310222 3930315EU NR 2 ENGINE OIL MALFUNCTIONED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25421FE 342 WHILE CLIMBING THROUGH FL 130 NR 2 ENG OIL QTY WENT TO ZERO (BOTH GAUGE AND ECAM) ENG OIL PRESSURE AND TEMP INDICATED NORMAL. ENGINE 2, OIL QTY INDICATIONS INOP. (1 OR 2) VERIFY AND RECORD IN EAML THAT OIL TANK QTY HAS BEEN VERIFIED PRIOR TO EACH DEPARTURE. VERIFIED NR 2 ENG OIL TANK QTY FULL. 2L72 4F RTA35EU 20050617000632005061700063NM 2005 6 17 ANCF200400051 120050605A3040 HEATER BOEING767 767200 1385120NM PWA 4060 PW4060 52119NE WINDOW DEFECTIVE W ANCFA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO23421AV 04076R8154 25421 ELECTRICAL SMOKE OF UNKNOW ORIGIN FROM THE CAPTAIN'S SIDE, BETWEEN THE LIGHT CONTROL PANEL AND THE GLARESHIELD PANEL, ACCORDING TO THE ABNORMAL CHECKLIST THE RECIRCULATION FANS AND THE UTILITY BUSES WERE SWITCHED OFF AND THE EQUIPMENT COOLING SELECTOR WAS SELECTED TO STANDBY POSITION, NO HELP THE SMOKE CONTINUES. SMOKE AND OXYGEN MASKS WERE USED. INSPECTION WAS PERFORMED, AND IT WAS FOUND A WINDOW NEAR CONNECTOR BURN AND BROKEN (IT WAS THE SMOKE SOURCE). THE CONNECTOR WAS ISOLATED ACCORDING TO MEL 30-41-1 CAT C. THE L FWD WINDOW WAS REPLACED, AND THE J5 PLUG WAS REPLACED TOO. 2L72 4F4 FRTA1NM E24NE 20050617000642005061700064NM 2005 6 17 C8GA20050015 120050608A341165189462 PITOT TUBE BOEING727 727227 1384078NM RIGHT LEAKING A C8GAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO298942759340 21365 FLT 842 FROM TOL TO PHL. ON TAKEOFF ROLL, CREW NOTED NO AIRSPEED INDICATION ON THE F/O SIDE. CREW ABORTED TAKEOFF WITHOUT INCIDENT AND RETURNED TO BLOCKS. FOUND OBSTRUCTION IN THE RT PITOT TUBE. REMOVED OBSTRUCTION AND PERFORMED PITOT/STATIC LEAK CHECK. OPS AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L73 4F A3WE 20050617000662005061700066NM 2005 6 17 05FDEA01573 120050609A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 MAIN DECK, SEAT TRACK LBL 27 CRACKED AT STA 635. CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2L73 4F RTA22WE 20050617000682005061700068NM 2005 6 17 05FDEA01575 120050609A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 MAIN DECK, SEAT TRACK LBL 47 CRACKED AT STA 635. CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2L73 4F RTA22WE 20050617000702005061700070NM 2005 6 17 05FDEA01577 120050610A5343AEA7051501 FITTING DOUG MD11 MD11 3023602NM ZONE 700 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 CENTER LANDING GEAR WHEEL WELL, LEFT HAND TRUNNION SUPPORT FITTING GUIDE PIN HOLE BUSHING CORRODED. CENTER LANDING GEAR WHEEL WELL, LEFT HAND TRUNNION SUPPORT FITTING GUIDE PIN HOLE CORROSION REMOVED PER SRM 53-40-00 VOLUME I, FIGURE 15. FINAL HOLE DIAMETER 1.680 INCHES FOUND WITHIN LIMITS PER SRM 53-40-00 VOLUME I, FIGURE 15. CORRODED BUSHING REMOVED AND REPLACED WITH NEW FABRICATED BUSHING PER CMM 20-20-07. REPAIR CLASSIFIED AS MAJOR REPAIR PER GMM 6-2-100. 2L73 4F RTA22WE 20050617000722005061700072NM 2005 6 17 05FDEA01579 120050602A534794041 SEAT TRACK BOEING727 727200 138407ENM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25495FE 21669 SEAT TRACK, RBL 45, FS 500 - 540 HAS CORROSION AND FROM STATIONS 580 TO 690 HAS EXISTING BLEND REPAIRS AND REQUIRES REPLACEMENT PER EO 7-5340-7-5002. REMOVED AND REPLACED SEAT TRACK, STA 480-690 IAW SRM 51-30-2. SEAT TRACK FABBED ON TRAVELER T5-524064. 2L73 4F RTA3WE 20050617000732005061700073SO 2005 6 17 RAIA00506007 120050607A3260 WARNING LIGHT EMB 145 EMB145ER 3260211SO MLG ILLUMINATED A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03808HK 145157 SPS ADVANCED MESSAGE ON EICAS FOLLOWED BY LG AIR/GRD FAILURE MESSAGE. LANDING GEAR HANDLE WOULD NOT RELEASE TO THE UP POSITION. MAINTENANCE INSPECTED ALL LANDING GEAR PROXIMITY SWITCHES AND SERVICED ALL THREE LANDING GEAR STRUTS. OPS CHECKED GOOD. 2L72 4F RTT00011AT 20050617000752005061700075NE 2005 6 17 RAIA00506008 220050608A7310 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114HR 01514NE FUEL CONTROL LOOSE A RAIAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 CE03568HK 41086 FLT 3656 - BWI - ABORTED TAKEOFF DUE TO NR 1 ENGINE NOT PRODUCING TAKEOFF POWER. MAINTENANCE TIGHTENED A LOOSE CONNECTOR ON THE FUEL CONTROL AND OPS CHECKED GOOD. 2L72 4T4 TRTA41NM E18NE 20050617000762005061700076EU 2005 6 17 RAIA00506009 120050608A2450A2105F PDU JETAIRJETSTMJETSTM4101 1500501EU NR 2 ENGINE FAILED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03568HK2305 41086 FLT 3656 - BWI - NR 2 ENGINE WOULD NOT START. MAINTENANCE REMOVED AND REPLACED THE RIGHT PDU. OPS CHECKED GOOD. 2L72 4T RTA41NM 20050617000772005061700077WP 2005 6 17 P9RA20050089 120050613A3260833703 PROXIMITY SENSOR DOUG DC9 DC982 3022082WP NLG INTERMITTENT A P9RAO OTHER N FALSE WARNING CLCLIMB 1 SO1110801 49127 ON GEAR RETRACTION FROM SJU, NOSE GEAR RED LIGHT REMAINED ON. RECYCLED GEAR PER QRH AND LIGHT EXTINGUISHED. REMOVED AND REPLACED NOSE GEAR PROXIMITY SWITCH PER M/M. 2L72 4F A6WE 20050617000782005061700078NM 2005 6 17 05FDEA01519 120050606A5743 SKATE ANGLE BOEING727 727200 138407ENM LT MLG TRUNNION CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 LEFT MLG FWD TRUNNION SKATE ANGLE CHAFED ON LWR WING SURFACE (I/B). REPAIRED PER FED EX EA 7-5710-86301. 2L73 4F RTA3WE 20050617000792005061700079NM 2005 6 17 05FDEA01520 120050606A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25477FE 21394 CORROSION ON FLOORBEAM UPPER AFT FLANGE, BS 344, RBL 10, TO LBL 20, WL 208. *S/D* REPAIRED FLOORBEAM AT BS 344 PER FED-EX DWG SR27-53-017A. 2L73 4F RTA3WE 20050617000802005061700080NM 2005 6 17 TSAA0532022 120050528A3244 TIRE BOEING737 737230 1384401NM MLG FAILED A TSAAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 WP13821AL 23155 NON-ETOPS FLT 68, HNL-ITO: ON TAKEOFF ROLL, FELT LIKE BOTH RIGHT MAIN LANDING GEAR TIRES BLEW. FOLLOWED BY AN EXTREME STRUCTURAL POUNDING COMING FROM THE RIGHT SIDE UNTIL SLOWED TO ABOUT 60KTS. DECLARED AN EMERGENCY. NO SMOKE OR FIRE. MAINTENANCE REMOVED AND REPLACED NR 3 AND NR 4 BRAKES AND MAIN LANDING GEAR TIRES. ALSO REMOVED AND REPLACED THE NR 1 & NR 2 BRAKES AND TIRES AS A PRECAUTION. COLLATERAL DAMAGE TO RIGHT FLAP, MAIN LANDING GEAR DOOR AND WING-TO-BODY FAIRING. AIRCRAFT NOT IN SERVICE AT THIS TIME. NUMEROUS PART REPLACEMENT AND CHECKS WERE ACCOMPLISHED. AIRCRAFT RETURNED TO SERVICE ON 6/7/05. 2L72 4F RTA16WE 20050617000812005061700081NM 2005 6 17 TSAA0549024 120050603A4920 ENGINE BOEING737 73776N 13844CHNM APU FAILED A TSAAO OTHER J WARNING INDICATION CRCRUISE 1 WP13748AL 30050 NON-ETOPS FLT 441, LAS-OAK: APU FAILED IN FLIGHT WITH FAULT LIGHT AND SHUT DOWN AUTOMATICALLY. TROUBLESHOT PER FIM 49-31-00-810-808, BITE CHECK SHOWS NO CURRENT FAULTS. FAULT WAS INTERMITTENT. OPS CHECK GOOD. COULD NOT DUPLICATE ON GROUND. FLIGHT VERIFICATION REQUIRED. FLIGHT VERIFICATION OKAY (6/3/05). AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA16WE 20050617000822005061700082EA 2005 6 17 VNAA0505008 120050523A5753 FAIRING CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE TE FLAP LIGHTNING STRIKEA VNAAK NONE O OTHER ININSP/MAINT 1 GL05720PS 10178 DURING THE INTERMEDIATE EXTERNAL INSP INBOARD FLAP INBOARD FAIRING AND ON THE LT STABILIZER TIP. MAINTENANCE COMPLIED WITH A DETAILED LIGHTNING STRIKE INSPECTION IAW CRJ 700 AMM 05-51-07-220-801-A01. NO OTHER DISCREPANCIES WERE FOUND. THE FLAP FAIRING WAS REPAIRED IAW CRJ 700 SRM 57-54-84-101-001-A01 AND THE STAB TIP IAW BOMBARDIER REO 670-55-12-030. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050617000842005061700084NE 2005 6 17 MWEA050052 220050607A7320114E6112G120 EEC BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE ZONE 400 FAULTY A MWEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31906ME 55170 INFLIGHT CREW HAD THE LEFT ENGINE SYSTEM FAIL ALERT AND THE NR 1 EPR WENT INOPERATIVE. MAINTENANCE FOUND FAULT CODE 732160 AND REMOVED AND REPLACED THE LEFT ENGINE EEC. 2L72 4F4 FTRA6WE E00061EN 20050617000862005061700086EA 2005 6 17 COMA0570063 120050612A5240 ACCESS PANEL CNDAIRCL600 CL6002C10 1390015EA FUSELAGE UNSECURE A COMAA UNSCHED LANDING WE INADEQUATE Q C VIBRATION/BUFFET CLCLIMB 1 SO01659CA 10153 FLIGHT 5296 - DURING CLIMBOUT OF BUF AN ABNORMAL AIR NOISE EMINATING FROM THE NOSE AREA. AIRCRAFT RETURNED TO THE FIELD. CLOSED THE EXTERNAL POWER ACCESS PANEL. 2L72 4F RTA21EA 20050617000872005061700087NM 2005 6 17 05FDEA01583 120050610A5340 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 UPPER FUSELAGE, STA 440, STR 0, STR TO FRAME CLIP DAMAGED. *S/D* REPLACED CLIP PER SRM 51-30-2. 2L73 4F RTA3WE 20050617000882005061700088EA 2005 6 17 COMA0560345 120050610A2150 DUCT CNDAIRCL600 CL6002B19 1900309EA COMPRESS DISCHARDISLODGED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01915CA 7013 FLIGHT 5326 - DURING CLIMBOUT OF CVG THE LEFT ACM TRIPPED OFF LINE. AIRCRAFT RETURNED TO THE FIELD. FOUND LEFT COMPRESSOR DISCHARGE DUCT BLOWN OFF OF BELL HOUSING CAUSING AN OVER TEMPERATURE CONDITION. RESECURED DUCT ON BELL HOUSING. 2L72 4F RTA21EA 20050617000892005061700089NM 2005 6 17 05FDEA01584 120050610A5340 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 UPPER FUSELAGE, STA 440, STR 6L, STRINGER TO FRAME CLIP CRACKED. *S/D* REPLACED CLIP PER SRM 51-30-2. 2L73 4F RTA3WE 20050617000902005061700090NM 2005 6 17 05FDEA01585 120050610A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 UPPER FUSELAGE STA 360, MULTIPLE OPEN HOLES IN CIRCUM FRAME, FROM BL 0 TO STR 5L. *S/D* REPAIRED MULTIPLE OPEN HOLES IAW SRM 51-40-3 AND 51-30-02. 2L73 4F RTA3WE 20050617000912005061700091NM 2005 6 17 05FDEA01586 120050608A3260189915 SENSOR BOEING727 727200 138407ENM ZONE 700 MALFUNCTIONED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25204FE 22926 AFTER DEPARTURE L/G LEVER WOULD NOT MOVE PAST OFF DURING GEAR RETRACTION. L/G LEVER LATCH FAILED TO RELEASE. LEVER LATCH LIGHTES C/B LEFT OUT PER QRH. QRH PROCEDURES COMPLIED WITH, LANDED AT KABE. REMOVED AND REPLACED LANDING GEAR AIR SAFTEY SENSOR PER M/M REF 32-09-221-4. TESTED OK PER EA 7-3210-90155. AIRCRAFT OK FOR FURTHER SERVICE. PREMATURE REMOVAL/INSTALLATION OFF MFG 1-899-15. 2L73 4F RTA3WE 20050617000922005061700092NM 2005 6 17 05FDEA01587 120050607A5270 CONNECTOR BOEING727 727200 138407ENM CARGO DOOR DIRTY A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25254FE 20936 ON T/O MCD A LIGHTS ON FWD ILLUM. FOLLOWED QRH RED TABS AND RETURNED TO AFW. A LIGHT WENT OUT ON FINAL. MAIN CARGO DOOR WARNING LIGHT SYSTEM (A OR B) INOP. VERIFY DOOR CLOSED AND LOCKED PRIOR TO EACH BLOCK OUT. CLEANED CONNECTOR ON SYS-A MICROSWITCH PER SMP AND RAN DOOR THROUGH SEVERAL CYCLES. OPS CHECK SATISFACTORY IAW NASI SYSTEM DOOR MANUAL FXV-727-MM14. OK FOR SERVICE. 2L73 4F RTA3WE 20050617000942005061700094NM 2005 6 17 05FDEA01593 120050613A2782651781820 ACTUATOR BOEING727 727200 138407ENM KRUEGER FLAP LEAKING A FDEAB EMER. DESCENT KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SO25213FE 22935 LOSS SYSTEM-A HYDRALICS IN FLIGHT. COMPLETED QRH/RED TAB PROCEDURES. SYSTEM-A FLUID SHUTOFF SWITCHED CLOSED AT 1032, LANDED AT 1048. *S/D* REMOVED AND REPLACED A-HYD SYS PRESS FILTERS PER M/M 29-11-062-3, NO CONTAMINATION FOUND. REMOVED AND REPLACED A-HYD SYS CASE DRAIN FILTERS PER M/M 29-11-041-2, NO CONTAMINATION FOUND. REMOVED AND REPLACED NR 4 KRUEGER FLAP ACT PER M/M 27-81-022-4. SERVICED HYD SYS-A PER M/M 12-12-000-2. 2L73 4F RTA3WE 20050617000952005061700095EA 2005 6 17 COMA0560348 120050612A3260864202 DOWNLOCK SENSOR CNDAIRCL600 CL6002B19 1900309EA NLG FAULTY A COMAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 SO01978CA 7158 FLIGHT 5179 - DURING CVG APPROACH, RECEIVED A NLG RED BAR INDICATION WITH NO DISAGREE MESSAGE. CREW DECLARED AN EMERGENCY, ABORTED FIRST APPROACH, THEN LANDED WITHOUT INCIDENT ON SECOND ATTEMPT. REPLACED THE NR 2 NLG DOWNLOCK SENSOR. 2L72 4F RTA21EA 20050617000962005061700096EA 2005 6 17 COMA0560349 120050612A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A COMAK NONE L NO TEST ININSP/MAINT 1 SO01818CA 7408 FLIGHT 5034 - DURING A MAINTENANCE INSPECTION NOTED THE EMERGENCY FLOOD LIGHT AT ROW 10 INOPERATIVE. DEFERRED ROW 10 EMERGENCY FLOOD LIGHTING PER MEL 33-51-01-1. 2L72 4F RTA21EA 20050617000972005061700097 2005 6 17 C2XA05RI009 420050528A3420 COMPUTER EMB 145 EMB145LR 3260212SO NAVIGATION INACCURATE A C2XAA UNSCHED LANDING O OTHER CLCLIMB 1 SW2713949 145057 FLT 2609 - RIC - AFTER TAKEOFF, THE CREW REPORTED THAT HEADING WAS NOT MATCHING COMPASS IN DG AND SLVD MODE. CREW RETURNED TO RIC AND LANDED WITHOUT INCIDENT. RIC MAINTENANCE UPDATED NAV DATA BASE. OPERATIONAL CHECK WAS PERFORMED SUCCESFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20050617001052005061700105SO 2005 6 17 C2XA05RI010 120050611A335020131A BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DEFECTIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW27185568786 2095 145595 RIC - DURING ROUTINE INSPECTION, MAINTENANCE FOUND EMERGENCY LIGHTS ON THE FLOOR AT EMERGENCY EXIT AND REAR INOP. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY POSITION 4. OPERATIONAL TEST WAS PERFORMED SUCCESFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20050617001072005061700107SO 2005 6 17 C2XA05SH046 120050611A532014530646401 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714942 145037 SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT VARIOUS AREAS BETWEEN FRAMES 52 & 59. MAINTENANCE REPAIRED LT OMEGA BEAM AT FRAME 54 AND AT FRAME 59 PER EC 5320-01247, NO FURTHER ACTION REQUIRED. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050617001092005061700109SO 2005 6 17 C2XA05SH048 120050611A532014530627003 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714942 145037 SHV - DURING C-CHECK LT OMEGA BEAM HAS VARIOUS AREAS OF CORROSION BETWEEN FRAMES 29-36. MAINTENANCE REPAIRED LT OMEGA BEAM AT FRAME 33 - FRAME 34 PER EC 5320-01247, NO FURTHER ACTION REQUIRED. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20050617001112005061700111SO 2005 6 17 C2XA05SH051 120050611A491012010732001 FIREWALL EMB 145 EMB145ER 3260211SO APU CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714942 145037 SHV - DURING C-CHECK RIVET HEAD WEAR MARKS ON BOTTOM RT SIDE OF APU FIREWALL. MAINTENANCE REPAIRED THE APU FIREWALL AT FRAME 81 IAW EC 5310-01337. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050617001132005061700113SO 2005 6 17 C2XA05IA079 120050612A27403622009015 ACTUATOR EMB 145 EMB145LR 3260212SO VERTICAL STAB INOPERATIVE A C2XAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 SW27145587644 1091 145598 CLT - FLIGHT 3268, THE CREW REPORTED THE PITCH TRIM ONE INOP AND ASSOCIATED AUTO TRIM FAIL MESSAGES IN CRUISE FLIGHT, AND THE INABILITY TO USE PITCH TRIM WITH PRIMARY OR BACKUP TRIM. THE AIRCRAFT LANDED AT CLT WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STAB ACTUATOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050617001252005061700125NE 2005 6 17 RAIA00506014 220050609A732131059008 FUEL CONTROL JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114 01514NE NR 1 ENGINE MALFUNCTIONED A RAIAC ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 CE03568HK10057659 41086 FLT 3646 - RIC - ABORTED TAKEOFF DUE TO NR 1 ENGINE NOT PRODUCING POWER. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE FUEL CONTROL. OPS CHECKED GOOD. 2L72 4T4 TRTA41NM E18NE 20050617001262005061700126SO 2005 6 17 RAIA00506018 120050614A3231 SOLENOID VALVE EMB 145 EMB145LR 3260212SO NLG DOOR MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03849HK 145002 FLT 8063 - STL - NOSE GEAR DOOR OPENED IN FLIGHT. MAINTENANCE REMOVED AND REPLACED THE GEAR DOOR SOLENOID VALVE. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050617001272005061700127EU 2005 6 17 RAIA00506015 120050610A3060D45081B TIMER JETAIRJETSTMJETSTM4101 1500501EU DE ICE SYS MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03561HK 41077 FLT 5469 - STL - LEFT PROP REMOTE CAPTION ILLUMINATED DURING TAXI. MAINTENANCE REMOVED AND REPLACED THE LEFT PROP DE-ICE TIMER. OPS CHECKED GOOD. 2L72 4T RTA41NM 20050617001282005061700128SO 2005 6 17 RAIA00506016 120050613A2923100FU01080 FUSE EMB 145 EMB145LR 3260212SO HYD PUMP INOPERATIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03822HK 145069 FLT 5761 - STL - NR 1 ELECTRIC HYDRAULIC PUMP INOP. MAINTENANCE REMOVED AND REPLACED THE FUSE FOR THE NR 1 HYDRAULIC PUMP. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050617001292005061700129SO 2005 6 17 RAIA00506019 120050614A325012302328403 TILLER EMB 145 EMB145LR 3260212SO NLG STEERING BROKEN A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03841HK7889 5045 145382 FLT 8077 - ROA - NOSEWHEEL STEERING WILL NOT ENGAGE WITH THE TILLER. MAINTENANCE REMOVED AND REPLACED THE HANDWHEEL. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050617001302005061700130SO 2005 6 17 FFKR102 120050531A71106878004 COWLING PIPER PA32 PA32R300 7103213SO ZONE 400 DEPARTED B FFKRBA EMER. DESCENT UNSCHED LANDING D INFLIGHT SEPARATION CLCLIMB 1 SO05333TG13000 32R7680320 TOP RIGHT SIDE OF THE COWLING SEPERATED FROM THE BOTTOM COWLING ON TAKE OFF, STRIKING THE ELEVATOR. 1L71 3O A3SO 20050617001312005061700131NM 2005 6 17 05FDEA01603 120050614A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 N01425 BS 360, STR 2R BS 360 S2R FRAME IS DAMAGED AT TOOLING HOLE. REPAIRED FRAME PER SRM 51-40-3 2L73 4F RTA3WE 20050617001322005061700132NM 2005 6 17 05FDEA01609 120050615A575365192492 FLAP TRACK BOEING727 727200 138407ENM NR 3 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 NR 3 FLAP TRACK HAS CORROSION EMINATING FROM AFT ATTACH AREA. REPLACED NR 3 FLAP TRACK PER MM 27-51-031-4 2L73 4F RTA3WE 20050617001332005061700133NM 2005 6 17 DL764050311 120050606A5754114T41455 BOLT BOEING767 767432ER 1385134NM RT WING BROKEN A DALAO OTHER J WARNING INDICATION APAPPROACH 1 SO27830MH 29701 EMERGENCY DECLARED INTO LAX DUE L/E SLAT ASYM MESSAGE PSEU FAULTING NR 12 OUTBOARD SLAT SENSOR. FOUND BOLT BROKEN. REPLACED BOLT. 2L72 4F RTA1NM 20050617001342005061700134EA 2005 6 17 VNAA0505009 120050524A5753 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAP DENTED A VNAAK NONE O OTHER ININSP/MAINT 1 GL05257PS 7939 DURING THE INTERMEDIATE EXTERNAL INSPECTION THE CREW DISCOVERED A DENT ON THE BOTTOM OF THE LEFT INBOARD FLAP. MAINTENANCE REMOVED & REPLACED THE FLAP IAW CRJ 200 AMM 27-54-01-000-801 AND 27-54-01-400-801. THE SYSTEM WAS RIGGED AND OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050617001352005061700135SO 2005 6 17 CHQA200500108 120050607A2120 ODOR EMB 145 EMB145LR 3260212SO COCKPIT DETECTED A CHQAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL11282SK 145409 FLIGHT 3049 DCA-GSO - AFTER TAKEOFF, CAPTAIN AND FIRST OFFICER DETECTED A BURNING ODOR IN THE COCKPIT AND CABIN. CYCLED BOTH BLEED SYSTEMS AND ODOR WENT AWAY. MAINTENANCE RAN BOTH ENGINES AND CYCLED BOTH BLEED VALVES. NO ODORS NOTED AT THIS TIME. OPS CHECK GOOD IAW AMM 36-11-05. 2L72 4T RTT00011AT 20050617001362005061700136SO 2005 6 17 CHQA200500109 120050608A3397 WIRE EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DAMAGED A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11269SK 145293 MAIN ENTRY DOOR EMERGENCY LIGHT IS INOP. REPAIRED WIRE W737-0038-20 IAW EMB 145 WM CHAPTER 20 STANDARD PRACTICES. OPS CHECK OF EMERGENCY LIGHTS GOOD IAW CHQ J/C E33-50-00-710-001. 2L72 4T RTT00011AT 20050617001382005061700138NM 2005 6 17 UPS05444652 120050513A5312 PRESSURE PANEL BOEING747 747123F NM NLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C NLG W/W RIGHT SIDEWALL NR 2 STRIP BLUGED AT BS 280 AS MARK (COUNT FROM TOP, CRACK LENGTH 1.5 INCH). NLG W/W RIGHT SIDEWALL BS 270 TO BS 290 WL 170 WEB REPAIRED AS PER SRM 53-10-04 FIG 116. 2L74 4F A20WE 20050617001392005061700139NM 2005 6 17 UPS05444656 120050519A5712 RIB BOEING747 747123F NM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C RIGHT WING BS 1241 UPPER REAR SPAR SPLICE BOLT HOLE NR 9 FOUND CRACKED AT RIB CHORD (CRACK LENGTH 0.040 INCH). HOLE REWORKED AS PER EO B747-5740-17032-C. 2L74 4F A20WE 20050617001402005061700140NM 2005 6 17 UPS05444658 120050514A571265B078315 RIB BOEING747 747123F NM LOT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C LT WING NR 5 VC FLAP O/B ARM O/B SUPPORT RIB I/B FACE D-HOLE CRACKED. (CRACK LENGTH .5 INCH). LT WING NR 5 VC FLAP O/B ARM O/B SUPPORT RIB I/B AREA REPAIRED AS PER HX RS R57-41-35308 DETAIL VISUAL INSPECT AT EALIER OF C-CHECK OR 18 MONTH INTERNALS REQUIRE REF UPS EO B747-5740-22314-A. 2L74 4F A20WE 20050617001412005061700141NM 2005 6 17 UPS05444659 120050514A571265B101405 RIB BOEING747 747123F NM LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C LT WING NR 7 VC FLAP O/B ARM I/B SUPPORT RIB FWD VERTICAL FLANGE FASTENER HOLE CRACKED (CRACK LENGTH 1 INCH). LT WING NR 7 VC FLAP O/B ARM I/B SUPPORT RIB FWD VERTICAL FLANGE REPAIRED AS PER HX RS R57-41-35307 DETAIL VISUAL INSPECT AT 6 MONTH INTERNAL FOR CRACKING, ELONGATED HOLES MISSING OR LOSE FASTENERS CORROSION OR OTHER SIGN OF DAMAGE. 2L74 4F A20WE 20050617001422005061700142NM 2005 6 17 UPS05444660 120050514A571265B101456 RIB BOEING747 747123F NM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C RT WING NR 19 VC FLAP I/B ARM O/B SUPPORT RIB FWD VERTICAL FLANGE FASTENER HOLES FOUND CRACKED (CRACK LENGTH 1 INCH). RT WING NR 19 VC FLAP I/B ARM O/B SUPPORT RIB FWD VERTICAL FLANGE REPAIRED AS PER HX RS R57-41-35307. DETAIL VISUAL INSPECT AT 6 MONTH INTERVALS FOR CRACKING, ELONGATED HOLES MISSING OR LOSE FASTENERS CORROSION OR OTHER OF DAMAGE. 2L74 4F A20WE 20050617001432005061700143NM 2005 6 17 UPS05444665 120050516A531165B04282403 FRAME BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C AFT CARGO COMPT BS 1500 STR 33L FRAME INNER FLANGE CRACKED (CRACK LENGTH 9 INCH APPROX). AFT CARGO COMPT BS 1500 STR 32L TO 38L INNER FLANGE REPAIRED AS PER HX RS R53-62-35311 CONTINUED INSPECTION REQUIRE TO THE REPAIR AREA PER SB 747-53A2349 REV 2 & UPS EO B747-5310-22294-A. 2L74 4F A20WE 20050620000022005062000002NM 2005 6 20 UPS05444668 120050520A534769B621371 CARGO TRACK BOEING747 747123F NM FUSELAEG CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE: C, M/D BS 800 LBL 55 TIE DOWN FITTING FLANGE CORRODED. CORROSION BLEND OUT 0.026 X .875 X 1.125 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. M/D BS 800 LBL 55 TIE DOWN FITTING REPLACED AS PER MM 20-50-01. 2L74 4F A20WE 20050620000052005062000005NM 2005 6 20 UPS05544676 120050607A2560 SMOKE GOGGLES BOEING757 75724APF 1384969NM COCKPIT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01422UP 25324 INSPECTION TYPE:N/A FIRST OBSERVERS SMOKE GOGGLES LENS CRACKED. REMOVED AND REPLACED SMOKE GOGGLES IAW MM 25-60-00. 2L72 4F RTA2NM 20050620000062005062000006WP 2005 6 20 UPS05844671 120050517A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE:C3 FUSELAGE SKIN CRACKED .25 INCH LONG AT STA 1746 L15L. CUT OUT DAMAGED SECTION OF SKIN, FABRICATED AND INSTALLED REPAIR DOUBL ER, FINGER DOUBLER, AND FILLER IAW DC-8 SRM 53-2-1 FIG 7, 51-1-20D, 51-1-21. 2L74 4F RT4A25 20050620000072005062000007WP 2005 6 20 UPS05844672 120050517A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE: C3, FUSELAGE SKIN CRACKED AT STA 1746 L15R. CUT OUT DAMAGED SECTION OF SKIN, FABRICATED AND INSTALLED REPAIR DOUBLER, FINGER DOUBLER, AND FILLER IAW DC-8 SRM 53-2-1 FIG 7. 2L74 4F RT4A25 20050620000082005062000008 2005 6 20 UPS05M44657 420050606A2562 ELT DOUG MD11 MD11F 3023600NM R-1 DOOR SLIDE ACTIVATED A IPXAO OTHER W INADEQUATE Q C CRCRUISE 1 SO01271UP 48572 SUSPECT AIRCRAFT IS TRANSMITTING AN ELT SIGNAL. CONTINUOUS RECEPTION ON 121.5 FROM SDF TO ANC. FOUND R-1 DOOR SLIDE ELT ACTIVATED. REMOVED AND REPLACED R-1 DOOR SLIDE PER AMM 25-61-01. OPS CHECK GOOD. 2L73 4F RTA22WE 20050616000482005061600048NM 2005 6 16 SWAA051675 120050607A3350101073 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29347SW 24374 DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2L72 4F RTA16WE 20050616000492005061600049NM 2005 6 16 SWAA051693 120050608A53126582671 PRESSURE PANEL BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29508SW 24185 DURING SCHEDULED 1/2D CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 663, LBL 30. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050616000522005061600052NM 2005 6 16 SWAA051696 120050608A3350BR9442 LAMP BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29733SA 27865 DURING SCHEDULED HC1 CHECK, FOUND CABIN EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 5 DEF. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050616000682005061600068NM 2005 6 16 AWXA200500647 120050521A57536546486129 SKIN BOEING737 737301 1384611NM T/E FLAP DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-19, LT INBOARD MID FLAP TRAILING EDGE PANEL 7220 WAS FOUND DELAMINATED AT UPPER AND LOWER SURFACES, APPROX 39 INCHES FROM OUTBOARD EDGE. MAINTENANCE CUT OUT DELAMINATED SKIN AND CORE ON LT INBD MIDFLAP TRL EDGE PANEL UPPER AND LOWER SURFACES. FABRICATED REPAIR CORE AND EXTERNAL DOUBLER, BONDED REPAIR PARTS TO FLAP IAW BOEING SRM 51-70-10 FIG 16. 2L72 4F RTA16WE 20050616000692005061600069NM 2005 6 16 AWXA200500646 120050525A532065353654 INTERCOSTAL BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-19 CHEC, INTERCOSTAL FOUND CRACKED AT BODY STATION (BS) 500D THROUGH BS 520. MAINTENANCE REMOVED TOP OF INTERCOSTAL AT BS 500D-520 AND FABRICATED ATTACH ANGLE FOR TOP OF INTERCOSTAL IAW BOEING SRM 51-40-02. INSTALLED FABRICATED PART IAW BOEING 737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050616000802005061600080NM 2005 6 16 AWXA200500655 120050407A5320146N539124 FLOOR SUPPORT BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28902AW 23322 DURING C-10 CHECK CORROSION WAS FOUND AT NUT PLATE HOLES ON UPPER SURFACE OF AFT CARGO DOOR SILL FLOOR SUPPORT FRAME BETWEEN BS 1380 AND BS 1410. MAINTENANCE REMOVED CORRODED AFT CARGO DOOR SILL FLOOR SUPPORT FRAME FROM BS 1380 TO BS 1410; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT; AND INSTALLED REPAIR PART IAW BOEING 757 SRM 51-40-02. 2L72 4F RTA2NM 20050616000822005061600082EU 2005 6 16 AWXA200500657 120050603A3397ABS0374A24 WIRE AIRBUS320 A320231 3930325EU CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28629AW 076 PHX - EEL - DURING 8-DAY CHECK, FOUND EMERGENCY EXIT ROW LIGHT INOP AT SEAT 26. MAINTENANCE REPAIRED BROKEN WIRE UNDER SEAT. OPERATIONAL CHECKS GOOD. 2L72 4F RTA28NM 20050616000842005061600084EU 2005 6 16 AWXA200500659 120050605A3350AD321430 BATTERY AIRBUS320 A320231 3930325EU CABIN DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 DURING 4-DAY CHECK, FOUND RIGHT EMERGENCY SUPPLY POWER UNIT HAD LOW BATTERY. MAINTENANCE REMOVED AND REPLACED RIGHT ESPU BATTERY IAW AIRBUS MM 33-51-38-04 STEP 7. OPERATIONAL CHECK GOOD. 2L72 4F RTA28NM 20050616000862005061600086NM 2005 6 16 AWXA200500661 120050526A3350D43637 CONNECTOR BOEING737 737301 1384611NM CABIN DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 DURING C-19 CHECK, FOUND ESCAPE PATH LIGHTING HARNESS DAMAGED AT CONNECTORS AND SPLICES FROM BS 360 TO BS 947 AT LBL 26. MAINTENANCE REMOVED DAMAGED CONNECTORS AND SPLICES FROM BS 360 TO BS 947 AT LBL 26. REPLACED CONNECTORS AND SPLICES FROM BS 360 TO BS 947 AT LBL 26 IAW BOEING 737-300 SWPM 20-42-01, 20-90-14, AND 20-30-12. OPERATIONALLY CHECKED GOOD IAW AMERICA WEST TASK CARD A1C33006. 2L72 4F RTA16WE 20050616000872005061600087CE 2005 6 16 DJFA2005105 120050601A2170 COALESCER BAG BEECH MU300 400A 1155402CE ACM CONTAMINATED E DJFAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA23798TA RK198 DURING CRUISE WITH ANTI-ICE SYS ON, NOTICED A STRANGE ODOR IN CABIN. WHILE LOOKING INTO CABIN THERE WAS A HAZY SMOKE EMANATING FROM REAR CABIN AROUND LAV AREA. CREW SELECTED RT ENG AS BLEED AIR SOURCE SMOKE APPEARED TO DECREASE. ACFT DIVERTED TO KAGS & MADE AN UNEVENTFUL LANDING. A STRONG ODOR REMAINED AROUND AFT BAGGAGE AREA. MX PERFORMED HIGH POWER ENGINE RUNS WHILE CYCLING THROUGH BLEED AIR SOURCES USING VARIOUS TEMP SETTINGS. COALESCER SOCK IN ACM REPLACED AND ENGS RUN AGAIN USING DIFFERENT BLEED AIR SOURCES & TEMP SETTINGS. LINES AT ACM & WING ANTI-ICE DUCTS IN LAV WERE INSPECTED WITH NO NOTED DEFECTS. A CHECK FLT OF THE AIRCRAFT WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4F RTA16SW 20050616000892005061600089NM 2005 6 16 AWXA200500663 120050606A5330654577467 SKIN BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 FUSELAGE SKIN CRACKED AT APPROXIMATELY BS 870 AND STRINGER 24R. MAINTENANCE ROUTED OUT CRACK AT BS 870 AND STRINGER 24R THEN FABRICATED DOUBLER IAW AIRBUS SRM 53-00-01 FIGURE 229. INSTALLED DOUBLER, FILLET WAS SEALED AND DOUBLER PAINTED IN REFERENCE TO AIRBUS SRM 53-00-01 FIGURE 229. DAMAGE AREA WAS PLACED ON MONITOR, CONTROL NR 250645, AND WILL BE RE-INSPECTED AT 60,000 CYCLES WITH REPLACEMENT OF SKIN TERMINATING THE MONITOR. 2L72 4F RTA16WE 20050616001052005061600105EU 2005 6 16 AWXA200500675 120050524A2550D5367302100000 PANEL AIRBUS320 A320232 3930326EU AFT CARGO BAY CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28639AW 471 DURING C-8 CHECK FOUND CORROSION ON LOWER SURFACE OF SIDEWALL PANEL 151EF IN THE AFT CARGO COMPARTMENT FROM FS 49 TO FS 53. MAINTENANCE FOUND THE CORROSION ON LOWER SURFACE OF SIDEWALL PANEL 151EF IN THE AFT CARGO COMPARTMENT TO BE OUT OF LIMITS. FABRICATED REPLACEMENT PANEL IAW IRM 9701 REV F. INSTALLED REPAIR PARTS IAW AIRBUS SRM 53-02-00. 2L72 4F RTA28NM 20050616001072005061600107NM 2005 6 16 AWXA200500677 120050602A5320654583311 WEB BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 DURING C-21 CHECK, FOUND FLOOR WEB CRACKED AT BS 196.5, WL 207, LEFT BL 28. MAINTENANCE REMOVED CRACKED FLOOR WEB AT BS 196.5, WL 207, LEFT BL 28 AND FABRICATED NEW WEB IAW BOEING 737-300 SRM 51-40-02 FIGURE 2 AND DWG 65-45833. INSTALLED FABRICATED REPAIR PARTS AT BS 196.5, WL 207, LEFT BL 28 IAW BOEING 737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050616001102005061600110NM 2005 6 16 AWXA200500679 120050531A531065535953 REVEAL BOEING737 73733A 1384673NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 DURING C-21 CHECK, CORROSION FOUND AT R1 DOOR CUTOUT ON FORWARD UPPER CORNER AT BS 300. CORROSION WAS FOUND TO BE OUT OF LIMITS AT R1 DOOR CUTOUT ON FORWARD UPPER CORNER AT BS 300 IAW BOEING 737-300 SRM 53-10-15 FIG 101. MAINTENANCE REMOVED AND INSTALLED NEW REVEAL AT R1 DOOR CUTOUT ON FORWARD UPPER CORNER AT BS 300 IAW BOEING 7373-300 51-40-02, FIGURE 4 AND FIGURE 8. 2L72 4F RTA16WE 20050616001382005061600138NE 2005 6 16 HNAA0500053 220050509A729782455044201 WIRE HARNESS DHAV DHC8 DHC8201 2809001NM PWA PW120 PW123 NE NR 2 ENGINE INTERMITTENT A HNAAE ENGINE SHUTDOWN N FALSE WARNING CLCLIMB 1 EA07969HA1454614546 468 BETWEEN 500 AND 1000 FEET AGL, CREW HEARD A LOUD NOISE FROM NR 2 ENGINE FOLLOWED BY A HIGH PITCH SOUND. CREW NOTICED THE NR 2 TORQUE AT 111 PERCENT (DIGITAL) AND RISING, THE ANALOG WAS OFF SCALE. FLIGHT ATTENDANT REPORTED SMOKE COMING FROM UNDER THE NR 2 PROP. REMOVED AND REPLACED THE NR 2 ENGINE STRUT WIRE HARNESS. 2H72 4T4 TRTA13NM E20NE 20050616001882005061600188WP 2005 6 16 TCA004 220050605A7261 ENGINE SWRNGNSA226 SA226TC 8780404SW GARRTTTPE331TPE33110UA 01514WP NR 1 OVERSERVICED E E18AO OTHER WB INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 GL23629EK TC396 THE PILOT REPORTED THAT INBOUND FLIGHT TO LRD THERE WAS A SMELL OF OIL IN THE COCKPIT. SHUT DOWN THE BLEED AIR AND THE SMELL DISAPPEARED. DID NOT DECLARE AN EMERGENCY AND LANDED WITHOUT INCIDENT. AFTER LANDING, WAS INSTRUCTED BY BASE MX IN TOL TO CHECK ALL CB'S AND PERFORM AN ENGINE RUN WITH BLEED AIR ON. REPORTED ALL NORMAL AND WAS CONFIDENT IN THE AIRCRAFT SYSTEMS. UPON RETURN TO TOL THE AIRCRAFT WAS RUN WITH BLEED AIR ON AND NO DEFECTS OR SMELLS WERE NOTED. NR 1 ENGINE OIL LEVEL FOUND TO BE OVERSERVICED AND MX CORRECTED OIL LEVEL. 2L72 4T4 TRTA8SW E4WE 20050616001902005061600190NM 2005 6 16 SWAA051585 120050527A532265C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29353SW 24889 DURING SCHEDULED 1/2D CHECK, FOUND 2 EA FUSELAGE STRINGER CLIPS CRACKED AT BS 887, STR 2L & 2R. REMOVED AND REPLACED CLIPS PER SRM. 2L72 4F RTA16WE 20050616001922005061600192NM 2005 6 16 SWAA051587 120050528A326027976006 LIGHT BOEING737 7373H4 1384600NM COCKPIT FAULTY A SWAAK NONE O OTHER DEDESCENT 1 SW29357SW 26594 RIGHT MLG GREEN LIGHT INDICATOR INOP DURING GEAR EXTENSION. RECYCLED MLG HANDLE-LIGHT ILLUMINATED. REMOVED AND REPLACED KORRY LIGHT PER MM. 2L72 4F RTA16WE 20050616002002005061600200NM 2005 6 16 MWEA050048 120050607A533059114063 SKIN BOEING717 717200 1383700NM FUSELAGE LIGHTNING STRIKEA MWEAK NONE O OTHER ININSP/MAINT 1 GL31903ME 55167 FUSELAGE SKIN AT STATION 148 BETWEEN LONGERON 14 AND 15 LEFT HAS EVIDENCE OF A LIGHTNING STRIKE. BLENDED DAMAGE. 2L72 4F TRA6WE 20050616002022005061600202NM 2005 6 16 MWEA050050 120050607A5330592480569 SKIN BOEING717 717200 1383700NM FUSELAGE LIGHTNING STRIKEA MWEAK NONE O OTHER ININSP/MAINT 1 GL31903ME 55167 LIGHTNING STRIKE AT RIVET ATTACHMENT JUST ABOVE LONGERON 6 LEFT. FABRICATED AND INSTALLED DOUBLER. 2L72 4F TRA6WE 20050616002392005061600239NM 2005 6 16 UPS05444620 120050518A531569B044821 SPLICE PLATE BOEING747 747123F NM FLOORBEAM CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C M/D- BS 860 LBL 95 - 113 FLOORBEAM UPPER SURFACE SPLICE PLATE CORRODED. CORROSION BLEND OUT 0.015 X 1.5 X 1.5 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS, SPLICE PLATE REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050616002412005061600241NM 2005 6 16 UPS05444622 120050519A5320BAC1509100312 CHANNEL BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C M/D BS 909 LBL 11 - 33 HAT SECTION SUPPORT CORRODED. CORROSION BLEND OUT: 0.015 X .875 X 1.25 INCH. HAT SECTION SUPPORT REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050616002432005061600243NM 2005 6 16 UPS05444624 120050519A5320BAC1509100312 FLOOR SUPPORT BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C M/D BS 570 LBL 11 - 33 FLOOR SUPPORT HAT SECTION FOUND CORRODED. CORROSION BLEND OUT: 0.011 X 1 X 1.5 INCH HAT SECTION REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050616002452005061600245NM 2005 6 16 UPS05444626 120050519A5347 SEAT TRACK BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C M/D - BS 860 LBL 75 SEAT TRACK O/B FLANGE CORRODED. CORROSION BLEND OUT: 0.021 X 1 X 1.75 INCH. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A FROM BS 850 - 870 LBL 75 INCH. 2L74 4F A20WE 20050616002472005061600247NM 2005 6 16 UPS05444628 120050518A532065B079535 STIFFENER BOEING747 747123F NM FUSLEAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C FWD CARGO COMPT - BS 295 WL 130 LT NWW VERTICAL WALL STIFFENER CORRODED. CORROSION BLEND OUT 0.058 X 0.5 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS, STIFFENER REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050616002492005061600249NM 2005 6 16 UPS05444630 120050601A532065B0794234 STIFFENER BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C NWW RT SIDE WALL PNL BS 300 TO BS 320 NR 3 HORIZONTAL STIFFENER (COUNT FROM TOP) 1EA FASTENER HOLE FOUND CRACKED AS MARKED (CRACK LENGTH .0625 INCH). NWW RT SIDE WALL PNL BS 300 TO BS 320 NR 3 HORIZONTAL STIFFENER REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050616002512005061600251NM 2005 6 16 UPS05444632 120050601A532065B0794233 STIFFENER BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C NWW LT SIDE WALL PANEL BS 280 TO 300 NR 3 HORIZONTAL STIFFENER (COUNT FROM TOP) 1 EA FASTENER HOLE FOUND CRACKED (CRACK LENGTH .0625 INCH). NWW LT SIDE WALL PANEL BS 280 TO 300 NR 3 HORIZONTAL STIFFENER REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050616002532005061600253NM 2005 6 16 UPS05444634 120050519A532065B07942180 STIFFENER BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C, RT SIDE NWW SIDE PANEL AT BS 320 - 340 NR 6 STIFFENER (COUNTED FROM TOP) FOUND RADIUS CRACKED (CRACKED LENGTH .375 INCH). RT SIDE NWW SIDE PANEL AT BS 320 - 340 NR 6 STIFFENER REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050616002552005061600255NM 2005 6 16 UPS05444638 120050601A5311 FRAME BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C NWW RT SIDE WALL PNL BS 300 WL 140-160 FOUND 3 EA FASTENER HOLES CRACKED AT VENT. BEAM INNER CHORD ALL APPROX .0625 INCH IN LENGTH. NWW RT SIDE WALL PNL BS 300 WL 140 TO 160 VERTICAL BEAM INNER CHORD REPAIRED AS PER SRM 51-40-04 FIG 2. 2L74 4F A20WE 20050616002562005061600256NM 2005 6 16 UPS05444639 120050601A5311 FRAME BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C NWW LT SIDE WALL PNL BS 300 WL 140-160 4 EA FASTENER HOLES FOUND CRACKED AT VERTICAL BEAM INNER CHORD ALL CRACKS APPROX .0625 INCH IN LENGTH. NWW LT SIDE PANEL BS 300 WL 140-160 VERTICAL BEAM INNER CHORD REPAIRED AS PER SRM 51-40-04 FIG 2. 2L74 4F A20WE 20050617000072005061700007EU 2005 6 17 AWXA200500341 120050315A2780903A000001 SOLENOID AIRBUS320 A320231 3930325EU ZONE 500 RATCHETING A AWXAO OTHER JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 WP28633AW 082 APPROACH, SELECTING FLAPS POSITION 1 RECEIVED ECAM SLAT LOCKED WING TIP BRAKE, DECLARED EMERGENCY & LANDED. R&R NR 1 SLAT/FLAP CONTROL COMPUTER. PERF SFCC 1&2 GRD SCAN, SLATS NO FAULTS. T/E FLAPS FAULTED LT PROXIMITY SENSOR 37CV. BITE TEST LGCIU NR 1, FAULT. REPLACED SENSOR, FAULT REMAINS. RANG OUT WIRES CONNECTOR 7514VC PIN A&B, TO LGCIU CONNECTOR 5GA1-AA, CONTAMINATION CONNECTOR 4035VC. CLEANED CONNECTOR. OPS TEST FLAPS, RATCHETING SOUND, ISOLATED TO LT T/E FLAP WING TIP BRAKE. R & R LT T/E FLAP WING TIP BRAKE ASSY. VENDORS TEARDOWN, SFCC SN 03234, NO FAULTS. UNIT INSP & TESTED. WING TIP BRAKE SN 458 CONFIRMED FAILURE. PISTON P/N 831-0001 OUT OF LIMITS, SOLENOID SYS 1 & 2 DEFECT. UNIT OVERHAULED2L72 4F RTA28NM 20050617000402005061700040NM 2005 6 17 CALA0500189 120050607A5320BAC1509 ANGLE BOEING737 737824 13844BZNM STA CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2727213 28773 INSPECTION FOUND L-ANGLE CORRODED AT STA 1002, LBL 32. A NEW ANGLE WAS INSTALLED IAW DRAWING 147A5710, SRM 51-20-01, AND 51-40-02. 2L72 4F RTA16WE 20050617000412005061700041NM 2005 6 17 CALA0500190 120050607A5315141A5502 FLOORBEAM BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2727213 28773 INSPECTION FOUND FLOORBEAM TEE CAP CORRODED AT STA 294.5, RBL 0 TO RBL 24. A REPAIR WAS INSTALLED IAW ECRA 5321-01231. 2L72 4F RTA16WE 20050617000622005061700062NM 2005 6 17 05FDEA01571 120050609A53476615731 SEAT TRACK BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25495FE 21669 SEAT TRACK STA 682 TO 686 HAS CORROSION BL 0. REMOVED & REPLACED SECTION OF SEAT TRACK STA 600 - 720 BL 0 IAW SRM 51-30-2. 2L73 4F RTA3WE 20050620000042005062000004NM 2005 6 20 UPS05444670 120050513A5330 SKIN BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE: C, AT BS 1681 STR 46R LAP JOINT MID ROW FASTENER (ONE EACH) FOUND SKIN BULGE UP (CORROSION BLEND OUT 0.019 X 0.5 X 1.5 INCH). FUSELAGE BS 1676 TO BS 1688 STR 46R AREA SKIN REPAIRED WITH ZERO-TIME FASTENER HOLES OVERSIZED AT CRITICAL ROW AREA AS PER SRM 53-30-03 FIG 17. SUBSEQUENT INSPECTION ARE NECESSARY FOR CATEGORY-B REPAIR REF TO SRM 53-30-03 FIG 17. 2L74 4F A20WE 20050620000092005062000009NM 2005 6 20 UPS05M44674 120050508A5711ARB01747 SPAR CAP DOUG MD11 MD11F 3023600NM LT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01254UP 48406 INSPECTION TYPE: 2C, LT WING, UPPER SURFACE, AFT WING SPAR JUST FWD OF NR 3 SPOILER, STRAP HAS BULGE & CRACKED SEALANT, NEED TO EVALUATE FOR CORROSION (2 SPOTS). PERFORMED CORROSION REPAIR ON LT WING UPPER SURFACE AFT WING SPAR IAW SAA SK 254-796823 & UPS REPAIR/ALTERATION AUTHORIZATION ENGRG FILE MD11-57-20021. 2L73 4F RTA22WE 20050620000102005062000010NM 2005 6 20 UPS05M44677 120050607A5245 STRUCTURE DOUG MD11 MD11F 3023600NM A/C PACK DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01272UP 48571 LT SIDE FUSELAGE FWD AIR CONDITION PACK ACCESS DOOR APPEARS CRACKED AT TOP OF DOOR. C/W HFEC AREA VERIFIED DOOR IS CRACKED APPROX 2.75 IN LENGTH MKD (QC0558905). REMOVED DOOR TO SM SHOP FOR REPAIR (0996300). REPLACED DOOR ASSY PER MM 52-42-01. 2L73 4F RTA22WE 20050620000122005062000012WP 2005 6 20 WRLA2005086 120050608A360034H40600 COUPLER DOUG DC10 DC1030F 3023504WP GE CF6 CF650C2 30018NE NR 2 ENGINE DAMAGED A WRLAEA ENGINE SHUTDOWN UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO11303 46917 455871 AIR TURNBACK INITIAL CLIMB OBSERVED MASTER WARNING & ENG FIRE WARNING LIGHT & BELL CAME ON & THEN OFF. NR 2 ENG NACELLE TEMP 260 DEG, NR 1 & 3 160 DEG. REDUCED ENG THRUST LEVER TOWARD IDLE TEMP FOLLOWED, PUSHED LEVER FORWARD & TEMP INCREASED, TESTED FIRE WARNING, NORMAL ON NR 1 & 3 BUT NO INDICATION ON 2. ACCOMPLISHED ENG FIRE CHECKLIST AND ALL OTHER APPLICABLE CHECKLISTS. FOUND DUCT APART ABOVE HIGH STAGE VALVE, REPOSITIONED SAME, REPLACED COUPLER. RAN ENG OPS CHECK, LEAK DOWN DECAY CHECK FOUND GOOD. PRESSURE WENT FROM 40 PSI TO 30 PSI WITH SYSTEM OFF IN 38 SEC ENG TEMP READ 200DEG PNEUMATIC TEMP AFTER 10 MIN AT 80 PERCCENT N2 55 PERCENT N1 NACELLE TEMP READS 80 DEG CELCIUS. OPS CHECK NORMAL. 2L73 4F4 FRTA22WE E23EA 20050620000152005062000015EU 2005 6 20 MALA050462 120050601A5330 SKIN SAAB SF340 340B 7860101EU FUSLAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15417XJ 340B417 DURING 4K INSPECTION FOUND RT FUSELAGE IS DENTED AND HAS BEEN REPAIRED IAW MESABA EO S53005 BETWEEN FS 319 TO 307 AND BETWEEN SL1616 TO SL1617. 2L72 4T RTA52EU 20050620000182005062000018EU 2005 6 20 MALA050459 120050601A53207253710243 PANEL SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15417XJ 340B417 DURING 4K INSPECTION FOUND LT AND RT WRAP AROUND PANELS P/N 7253710-243 (RT) AND 7253711-245 (LT) HAVE BEEN REMOVED AND REPLACED DUE TO CORROSION DAMAGE. 2L72 4T RTA52EU 20050620000192005062000019EU 2005 6 20 MALA050460 120050601A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15417XJ 340B417 DURING 4K INSPECTION LT FUSELAGE IS DENTED AND HAS BEEN REPAIRED IAW MESABA EOS53009, BETWEEN FS 351 AND 364 AND BETWEEN SL1505 TO SL1507. 2L72 4T RTA52EU 20050620000202005062000020EU 2005 6 20 MALA050461 120050601A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15417XJ 340B417 DURING 4K INSPECTION FOUND LT FUSELAGE IS DENTED AND HAS BEEN REPAIRED IAW MESABA EOS53009 BETWEEN FS 351 AND 364 AND BETWEEN SL1515 TO SL1517. 2L72 4T RTA52EU 20050620000212005062000021NM 2005 6 20 AWXA200500667 120050606A75007061M31G05 VALVE BOEING737 7373U3 13844CCNM CFMINTCFM56 CFM563B1US GL NR 1 ENGINE FAILED A AWXAC ABORTED TAKEOFF MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 WP28335AW 28740 ON TAKEOFF NR 1 ENG EGT ACCELERATED RAPIDLY TO 940 DEGREES CELSIUS FOR 2 SECONDS. EGT INCREASED RAPIDLY FROM STEADY TAKEOFF SETTING. ABORTED TAKEOFF AT 90-100 KNOTS & TAXIED CLEAR OF RUNWAY THEN TOWED TO GATE WITH NR 1 ENG EGT DIGITAL GAUGE FLASHED OVERTEMP. MX R & R NR 1 ENG TURBINE CLEARANCE VALVE, NR 1 ENG TIMER SOLENOID IAW MM 75-24-02, & NR 1 ENG TIMER IAW MM 75-24-00. COMPLIED WITH HPTCC TIMER & VALVE CHECK IAW MM 75-24-00. OPERATIONAL TEST WERE GOOD. TEAR DOWN REPORT FOR TC VALVE, SN GAT5C673. UNIT FAILED INCOMING OPERATIONAL TEST FOR OVERBOARD LEAKAGE. UNIT WAS OVERHAULED AND ALL PARTS WERE REPLACED IAW CMM 75-21-30 REV 2. 2L72 4F4 FRTA16WE E2GL 20050620000232005062000023EU 2005 6 20 AWXA200500682 120050608A335032145410 POWER SUPPLY AIRBUS320 A320232 3930326EU EMERGENCY LIGHT INOPERATIVE A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28662AW 1274 DURING TURN FLIGHT CREW DISCOVERED EMERGENCY EXIT LIGHTS ON THE RIGHT SIDE OF THE AIRCRAFT WERE INOP. MAINTENANCE REMOVED AND REPLACED THE RIGHT OVERWING CABIN EMERGENCY POWER SUPPLY. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA28NM 20050620000242005062000024EU 2005 6 20 AWXA200500683 120050609A3350321454 POWER SUPPLY AIRBUS320 A320232 3930326EU EMERGENCY LIGHT INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28602AW 565 DURING 4 DAY CHECK BOTH EMERGENCY EXIT LIGHTS IN THE FORWARD GALLEY WERE NOT ILLUMINATING. MAINTENANCE REMOVED AND REPLACED THE FORWARD POWER SUPPLY IAW TC R1433303 AND TC A1C33302. OPERATIONAL CHECK NORMAL. 2L72 4F RTA28NM 20050620000252005062000025 2005 6 20 BMAC050007 420050604A2565146110018 SLIDE BOEING727 727222 1384073NM L1 DOOR DEPLOYED A B16AO OTHER O OTHER TXTAXI/GRND HDL 1 SO29342PA 21893 L1 EMERGENCY DOOR SLIDE ACTIVATED WHEN DOOR WAS OPENED, GIRT BAR WAS NOT ATTACHED. HOLDING CONTAINER MALFUNCTIONED. REMOVED AND REPLACED SLIDE ASSEMBLY. 2L73 4F A3WE 20050620000262005062000026WP 2005 6 20 0500879871 120050409A5315 FLOORBEAM DOUG DC9 DC951 3022051WP FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01780NC 48102 DURING H-CHECK FOUND CRACK IN FLOORBEAM AT BS 237 LBL 5. REPAIRED PER EA 98-203186. 2L72 4F RTA6WE 20050620000272005062000027WP 2005 6 20 P9RA20050088 120050610A3260833703 PROXIMITY SENSOR DOUG DC9 DC982 3022082WP NLG OUT OF ADJUST A P9RAO OTHER J WARNING INDICATION CLCLIMB 1 SO1110801 49127 ON GEAR RETRACTION FROM SYR, NOSE GEAR LIGHT INITIALLY EXTINGUISHED THEN ILLUMINATED. RECYCLING GEAR CAUSED LIGHT TO EXTINGUISH. FLIGHT CONTINUED. SFB MAINTENANCE ADJUSTED PROXIMITY SWITCH PER M/M. LOCAL ACCEPTANCE FLIGHT CHECKED SATISFACTORY. 2L72 4F A6WE 20050620000282005062000028SO 2005 6 20 MASA200500183 120050305A335082324 SIGN EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07826MJ 145214 ASH 2824 CLT. ROW 12 OVERHEAD EMERGENCY EXIT SIGN LIGHTS INOP. MAINTENANCE REPLACED THE SIGN. 2L72 4T RTT00011AT 20050620000302005062000030EA 2005 6 20 MASA200500394 120050525A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0737208 7208 ASH 2740 AVP TO PHL. THE CREW HAD THE CENTER EMERGENCY FLOOD LIGHT INOPERATIVE. MAINTENANCE RELAMPED. 2L72 4F RTA21EA 20050620000312005062000031SO 2005 6 20 MASA200500397 120050526A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07836MJ 145359 ASH 2857 CLT TO CAE. THE FLOOR EMERGENCY PROXIMITY LIGHT STRIPS FROM ROW 3 TO 7 INOP. MAINTENANCE PERFORMED THE OPS CHECK OF THE LIGHT STRIPS AND LIGHTS OPERATED NORMALLY. THE AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. 2L72 4T RTT00011AT 20050620000332005062000033 2005 6 20 SB05069 420050612A3421H321AKM1 INDICATOR BOEING737 737301 1384611NM COCKPIT FAILED A USAAA UNSCHED LANDING P NO WARNING INDICATION CRCRUISE 1 EA19340US4341425324 23237 EN ROUTE FROM PHL TO CUN, CREW REPORTED THE STANDBY ATTITUDE INDICATOR FAILED. DECISION WAS MADE TO DIVERT TO CLT FOR REPAIRS. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE STANDBY ATTITUDE INDICATOR. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050620000352005062000035CE 2005 6 20 56000972 120050610A3297 WIRE CESSNA500 560CESSNA 2076750CE MLG BROKEN E ERYAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 CE07898CB5397 5600097 UPON APPROACH FOR LANDING, LT MAIN LANDING GEAR INDICATED UNSAFE AFTER GEAR EXTENSION. PERFORMED EMERGENCY PROCEDURES AND BLEW GEAR DOWN. LANDED WITHOUT INCIDENT. FOUND BROKEN WIRE AT LT MAIN DOWN AND LOCKED SWITCH. REPAIRED BROKEN WIRE, PURGED SYSTEMS AND SERVICED BLOW DOWN BOTTLE WITH NITROGEN. OPS CHECK NORMAL. 2L72 4F RTA22CE 20050620000362005062000036SO 2005 6 20 1408060605 120050606A2760 CONTROL SYSTEM GULSTMG1159 GIV 3980115SO SPOILERS MALFUNCTIONED E N93AA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 SO13401QS 1408 DURING FLIGHT AT 250-290 KIAS, MOVING THE FLIGHT SPOILER HANDLE .5 - 1 INCH FROM CLOSED RESULTED IN AN ABRUPT ROLL TO THE LEFT. 2L72 4F RTA12EA 20050620000382005062000038GL 2005 6 20 CHQA200500110 220050609A7200 ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL MALFUNCTIONED A CHQAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL11262SK5482 5482 145168 CAE312376 FLIGHT 3201 BUF-LGA - ON INITIAL CLIMB AT APPROXIMATELY 8000 FT, E2 ITT BEGAN TO RISE ABOVE 900 DEGREES. RAN QRH AND THE PROBLEM STILL PERSISTED. THERE WERE NO OTHER ABNORMAL INDICATIONS. THE OIL TEMP AND PRESSURES WERE NORMAL. THE TEMP CONTINUED TO RISE ABOVE 903-905. AT THAT POINT THE CREW DECIDED TO SHUTDOWN ENGINE AND RETURN TO BUF. AN EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT EVENT IN BUF. MAINTENANCE FOUND DAMAGE TO THE CUSTOMER SERVICE MANIFOLD. REMOVED AND REPLACED NR 2 ENGINE IAW JOB CARD CE720001. OPS CHECK GOOD. 2L72 4T4 FRTT00011ATTE6CH 20050620000402005062000040NM 2005 6 20 CALA0500192 120050610A531565C339503 FLOORBEAM BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716618 27331 INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, LBL 14.5. THE CORRODED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-60-51. 2L72 4F RTA16WE 20050620000412005062000041NM 2005 6 20 CALA0500193 120050610A5322149A721410 SUPPORT BRACKET BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2727213 28773 INSPECTION FOUND SUPPORT BRACKET FOR BELLY PANEL RT SIDE OF A/C EXHAUST DUCT CORRODED AT STA 649.96. REPAIRED IAW ECRA 5336-01002 AND SRM 53-40-01. 2L72 4F RTA16WE 20050620000472005062000047EU 2005 6 20 03082005 120050308A2613 WARNING LIGHT SAAB SF340 340B 7860101EU RT TAILPIPE ILLUMINATED A NSVAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA27294CJ 294 RT TAILPIPE HOT LIGHT ILLUMINATED. 2L72 4T RTA52EU 20050620000482005062000048EU 2005 6 20 04022005 120050402A2613 WARNING LIGHT SAAB SF340 340B 7860101EU RT TAILPIPE ILLUMINATED A NSVAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA27233CJ 233 RT ENGINE TAILPIPE HOT LIGHT ILLUMINATED. 2L72 4T RTA52EU 20050620000492005062000049EU 2005 6 20 04242005 120050424A2613 WARNING LIGHT SAAB SF340 340B 7860101EU RT TAILPIPE ILLUMINATED A NSVAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA27294CJ 294 RT TAILPIPE HOT LIGHT ILLUMINATED. 2L72 4T RTA52EU 20050620000512005062000051NM 2005 6 20 AT0500018 120050610A33508039251 BATTERY PACK BOEING717 717200 1383700NM EMERGENCY LIGHT INOPERATIVE A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15910AT 55086 ROW 1 TO 10 EMERGENCY LIGHTS ARE INOP. REMOVED AND REPLACED SEAT MOUNTED EMERGENCY FLOOR AISLE LIGHT ASSY AT ROW 5. OPS CK GOOD. REMOVED AND REPLACED B5-118 BATTERY PACK. 2L72 4F TRA6WE 20050620000532005062000053EU 2005 6 20 06062005 120050606A2910 PRESSURE SWITCH SAAB SF340 340B 7860101EU HYD SYSTEM MALFUNCTIONED A NSVAO OTHER J WARNING INDICATION APAPPROACH 1 EA27338CJ 338 HYDRAULIC LIGHT ON. BOTH MAIN AND EMERGENCY PRESSURE LOW IN FLIGHT THEN MAIN READ 0 PSI. PERFORMED EMERGENCY GEAR EXTENSION. 2L72 4T RTA52EU 20050620000542005062000054NM 2005 6 20 AWXA200500690 120050601A531265163007 BULKHEAD BOEING737 73733A 1384673NM FUSLAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 DURING C-21 CHECK FOUND A CRACK .275 INCHES IN LENGTH AT BULKHEAD WEB BS 178, WL 234, AND LBL 14. MAINTENANCE REMOVED CRACKED AREA AT BULKHEAD WEB BS 178, WL 234, LBL 14 AND FABRICATED DOUBLER AND FILLER IAW BOEING 737-300 SRM 53-10-08-2 FIG 209. INSTALLED FABRICATED REPAIR PARTS AT BS 178, WL 234, LBL 14 IAW BOEING 737-300 SRM 53-10-08-2 FIG 209. 2L72 4F RTA16WE 20050620000552005062000055NM 2005 6 20 AWXA200500691 120050602A575465C2660318 SKIN BOEING737 73733A 1384673NM NR 6 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 MCN - MAJOR REPAIR - DURING C-21 CHECK DISCOVERED 2 CRACKS .275 INCHES LONG LOCATED AT THE BOTTOM OF THE NR 6 SLAT SKIN, SLAT STATION 307 TO SLAT STATION 309. MAINTENANCE REMOVED DAMAGED AREA FROM THE BOTTOM OF NR 6 SLAT SKIN FROM SLAT STATION 307 TO SLAT STATION 309. FABRICATED REPAIR FILLER AND SPLICE PLATE IAW BOEING 737-300 SRM 57-43-01-2 FIG 206. INSTALLED FABRICATED REPAIR PARTS AT BOTTOM OF NR 6 SLAT SKIN FROM SLAT STA 307 TO SLAT STA 309 IAW BOEING 737-300 SRM 57-43-01-2 FIG 206. 2L72 4F RTA16WE 20050620000562005062000056NM 2005 6 20 AWXA200500692 120050602A531296368207 BULKHEAD BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 MCN - MAJOR REPAIR - DURING C-21 CHECK FOUND 3 CRACKS .271 INCHES LONG AT FRAME WEB STA 178 WL 230 RBL 17.1. MAINTENANCE REMOVED DAMAGED AREA FROM FRAME WEB STA 178 WL 230 RBL 17.1 AND FABRICATED WEB AND TAPERED SHIMS IAW BOEING 737-300 SRM 53-10-08-2 FIG 212. INSTALLED FABRICATED PARTS AT FRAME WEB STA 178 WL 230 RBL 17.1 IAW BOEING 737-300 SRM 53-10-08-2 FIG 212. 2L72 4F RTA16WE 20050620000572005062000057NM 2005 6 20 AWXA200500693 120050607A5312651758261 STIFFENER BOEING737 73733A 1384673NM BULKHEAD CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 MCN - MAJOR REPAIR - DURING C-21 CHECK FOUND SUPPORT ANGLE CRACKED AT BS 178 WL 230 RBL 17.1. MAINTENANCE REMOVED CRACKED SUPPORT ANGLE AND FABRICATED SUPPORT ANGLE IAW BOEING DWG 65-17582. INSTALLED FABRICATED REPAIR PARTS AT BS 178 WL 230 RBL 17.1 IAW BOEING 737-300 51-40-02-0 FIG 12. 2L72 4F RTA16WE 20050620000592005062000059NE 2005 6 20 03102005 220050310A7200 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LEFT FAILED A NSVAA UNSCHED LANDING Y ENGINE STOPPAGE CLCLIMB 1 EA27356CJ 356 785208 DURING CLIMB THE LEFT ENGINE FAILED. 2L72 4T4 TRTA52EU E8NE 20050620000602005062000060NE 2005 6 20 05202005 220050520A7200 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RIGHT FAILED A NSVAC ABORTED TAKEOFF Y ENGINE STOPPAGE TOTAKEOFF 1 EA27277MJ 277 785426 RT ENGINE FAILURE ON TAKEOFF ROLL. 2L72 4T4 TRTA52EU E8NE 20050620000612005062000061NM 2005 6 20 DHL2005741550 120050414A5730 SKIN BOEING727 7272Q9 138448MNM LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 LT WING L/E CRACKED AT NR 4 SLAT O/B TRACK CUTOUT. STOP DRILLED CRACK AT CUTOUT. FABRICATED REPAIR PARTS PLATE 301 1/2 HARD, 0.020 (6.8 X 5.2 INCH) PO 509613, BACKING STRAPS 2 EA 2024-T3, 0.063 (.80 X 3.0 INCH) PO 9001978, FILLER 301 1/2 HARD, .032 (2.2 X 6.85 INCH) PO 9001777 IAW B727 SRM 57-30-04 FIG 9. TREATED & PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B727 SRM 57-30-4, FIG 9. 2L73 4F RTA3WE 20050620000622005062000062 2005 6 20 DXTA200500765 420050611A3414 INDICATOR CESSNA500 560CESSNA 2076750CE AIRSPEED FAILED E DXTAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 GL07336QS 5600336 DURING TAKEOFF ROLL, STANDBY AIRSPEED INDICATOR STAYED AT 0 KTS. BOTH PFD AIRSPEED INDICATIONS WERE ACCELERATING THROUGH 60 KTS. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20050620000642005062000064CE 2005 6 20 DXTA200500763 120050610A2910S3128B0166000G HOSE CESSNA750 750 2076810CE HYD SYSTEM RUPTURED E DXTAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 GL07902QS 7500002 LOST A-SYSTEM HYDRAULICS IN FLIGHT. HYD VOL LOW (A), HYD PUMP FAIL (A). BLEW GEAR DOWN AND USED EMERGENCY BRAKE SYSTEM. FOUND NOSE CENTER HYDRAULIC LINE RUPTURED. REMOVED AND REPLACED NOSE CENTER HYDRAULIC LINE AND BLEED MAIN SYSTEM IAW CESSNA 750 M/M 32-30-00. 2L72 4J RTT00007WI 20050620000682005062000068CE 2005 6 20 DXTA200500760 120050609A3230 WARNING LIGHT CESSNA750 750 2076810CE MLG ILLUMINATED E DXTAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 GL07924QS 7500124 DURING CLIMB THROUGH FL370 AT MACH .80, GEAR UNLOCK LIGHT ILLUMINATED ACCOMPANIED BY AUDIBLE CLUNK. AIRCRAFT WAS SLOWED AND A DESCENT WAS BEGUN. LIGHT WENT OFF AT FL260 AND 250 KNOTS WITH ANOTHER CLUNK. ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20050620000692005062000069CE 2005 6 20 DXTA200500761 120050610A3240 LINE CESSNA560 560XL 2076702CE BRAKE ASSY LEAKING E DXTAD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 GL07651QS 5605251 BRAKE SYSTEM FAILURE ON GROUND. AIRCRAFT PUMPED BRAKE LINE FLUID OUT OF NOSE COMPARTMENT ON TO GROUND AROUND NOSE WHEEL. ASSOCIATED AMBER ANNUNCIATORS + M/C (LOW BRAKE PRESS, ANTI-SKID FAIL). ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20050620000712005062000071CE 2005 6 20 DXTA200500768 120050612A3150 WARNING LIGHT BEECH MU300 400A 1155402CE COCKPIT INTERMITTENT E DXTAC ABORTED TAKEOFF J WARNING INDICATION TXTAXI/GRND HDL 1 GL07116QS RK385 DURING T/O ROLL & TAXI BACK TO FBO THE RIGHT WINDSHIELD OVERHEAT & MASTER WARNING LIGHTS ILLUMINATED ON & OFF INTERMITTENTLY. ITEM IS UNDER INVESTIGATION. 2H72 4F RTA16SW 20050620000722005062000072CE 2005 6 20 DXTA200500769 120050612A3397 WIRE CESSNA500 560CESSNA 2076750CE ANTI COLL LIGHT BURNED E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07342QS 5600324 ANTI COLLISION CIRCUIT BREAKER POPPED. THERE WAS A LIGHT ELECTRICAL BURNING SMELL ASSOCIATED WITH IT. TROUBLESHOT AND FOUND A CHAFED WIRE ON RIGHT WING WIRE BUNDLE FOR ANTI COLLISION LIGHTS. REPAIRED WIRE IAW CESSNA CITATION 560 ULTRA MM 33-41-00. ANTI COLLISION LIGHTS OP CHECKED GOOD. INSPECTED CIRCUIT BREAKER AREA FOR ARCHING DUE TO ELECTRICAL BURNING SMELL AND NO EVIDENCE OF ARCHING FOUND. 2L72 4F RTA22CE 20050620000732005062000073CE 2005 6 20 DXTA200500770 120050612A3240 BRAKE CESSNA500 560CESSNA 2076750CE MLG DAMAGED E DXTAD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07366QS 5600466 CO-PILOTS LEFT PEDAL GOES TO THE FLOOR BEFORE ANY PRESSURE CAN BE BUILT UP. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20050620000742005062000074NE 2005 6 20 UIA0505 220050612A7200 ENGINE DOUG MD90 MD9030 3023690NM IAE V2525 V2525D5 NE RIGHT FAILED Z A UNSCHED LANDING XH ENGINE FLAMEOUT ELECT. POWER LOSS-50 PC DEDESCENT 1 TW0017918129932855 53571 V20083 RT ENGINE IN FLIGHT SHUTDOWN (IFSD) CAUSED BY SURGE MESSAGE SHOW ON EOAP, THEN FOLLOW EGT RAPID INCREASE. AFTER LANDING CHECK FOUND SEVERAL STAGE 4 BLADES MATERIAL MISSING AND BEND WITH DENTS. STAGE 5-12 BLADES BURN. THIS CASE COULD BE IOD IAW AMM 71-00-10. REPLACED NR 2 ENG ASSY AND IAW AMM 71-00-00 PFM ENG RUNUP FUNCTION CHECK CONDITION NORMAL. 2L72 4F4 FRTA6WE A40NE 20050620000762005062000076NE 2005 6 20 BA05011 220050612A720055T24801 LINE AIRBUS330 A330323 3930335EU PWA 4168 PW4168A NE RT ENGINE BROKEN A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19671UW 323 733514 CREW RECEIVED THE ECAM WARNING ENG 2 EPR MOD FAULT. THE CREW ALSO NOTED THE LOSS OF AUTOTHROUTTLES. DUE TO LACK OF PARTS IN FRA, THE FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED A BROKEN P4.95 SENSE LINE. 2L72 4F4 FRTA46NM 20050620000782005062000078EU 2005 6 20 SA05068 120050611A335032145410 EPSU AIRBUS320 A320214 3930316EU EMERGENCY LIGHT FAULTY A USAAK NONE L NO TEST ININSP/MAINT 1 EA19122US146334723 1298 PIT - THE EMERGENCY LIGHTS SYSTEM TESTED INOPERATIVE. MAINTENANCE REPLACED THE AFT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20050620000792005062000079EU 2005 6 20 SA05069 120050613A3350079123 LIGHT AIRBUSA319 A319112 3930323EU CABIN MISSING A USAAK NONE O OTHER ININSP/MAINT 1 EA19750UW 1315 CLT - THE EMERGENCY EXIT LIGHT ASSEMBLY WAS FOUND NOT INSTALLED ON THE AISLE SIDE OF THE LEFT AFT LAV WALL. MAINTENANCE REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY ON THE WALL OF THE AFT LEFT LAV. OK FOR SERVICE. 2L72 4F RTA28NM 20050620000822005062000082SO 2005 6 20 C2XA05BT039 120050614A335020131A BATTERY PACK EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT FAULTY A C2XAO OTHER O OTHER NRNOT REPORTED 1 SW2718556157383199 145595 AFT EMERGENCY LIGHT STRIP NOT WORKING. MAINTENANCE REMOVED AND REPLACED NR 4 BATTERY PACK IAW EMB145 AMM 33-50-04, OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050620000852005062000085NM 2005 6 20 SWAA051686 120050607A3350BR9442 BULB BOEING737 7377Q8 1384418NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29799SW 28209 DURING SCHEDULED RON CHECK, FOUND R2 DOOR EXTERNAL EMERGENCY LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050620000892005062000089NM 2005 6 20 SWAA051703 120050609A534065C27314 STRINGER CLIP BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29508SW 24185 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050620000902005062000090NM 2005 6 20 SWAA051704 120050609A33502121A BATTERY PACK BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED RON CHECK, FOUND 2 EA CABIN EMERGENCY BULLNOSE LIGHTS INOP AT FWD CABIN, LT SIDE. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050620000912005062000091NM 2005 6 20 SWAA051705 120050609A3350D71701100 BATTERY PACK BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29763SW 27877 DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EXTERNAL EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050620000922005062000092NM 2005 6 20 SWAA051706 120050608A32307453993 PUSH-PULL CABLE BOEING737 7377H4 1384404NM MLG FAULTY A SWAAO OTHER O OTHER DEDESCENT 1 SW29778SW 27883 DECLARED EMERGENCY, LANDING GEAR LEVER STUCK IN THE OFF POSITION, WOULD NOT MOVE UP OR DOWN. REMOVED AND REPLACED LANDING GEAR PUSH/PULL CABLE & LEVER GEARBOX PER MM. 2L72 4F RTA16WE 20050620000942005062000094NM 2005 6 20 SWAA051698 120050609A5753 SKIN BOEING737 7373H4 1384600NM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED C1 CHECK, FOUND LT WING INBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM. 2L72 4F RTA16WE 20050620000952005062000095NM 2005 6 20 SWAA051699 120050609A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29335SW 23939 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 766, STR 18R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050620000962005062000096SO 2005 6 20 C2XA05TY034 120050419A7700M83536 RELAY EMB 145 EMB145LR 3260212SO COCKPIT FAILED A C2XAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 SW2711548 145565 TYS, AIRCRAFT DECLARED AN EMERGENCY LANDING FOR ENGINE 1 THRUST REVERSER, DISAGREE IN FLIGHT (MESSAGE WENT AWAY WHEN THE LANDING GEAR WAS LOWERED) AND LANDING GEAR AIR/GRD FAIL ON EICAS IN FLIGHT (MESSAGE WENT AWAY AT TOUCH DOWN). MAINTENANCE REMOVED AND REPLACED RELAYS KO453, KO352 AND KO353 IAW 20-13-03, OPS CHECKED GOOD. AIRCRAFT RELEASED TO SERVICE. 2L72 4T RTT00011AT 20050620001032005062000103NM 2005 6 20 SWAA051713 120050611A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29447WN 33720 EEPLS COVER MISSING AT ROW 1. INSTALLED COVER PER MM. 2L72 4F RTA16WE 20050620001072005062000107NM 2005 6 20 SWAA051717 120050612A53206545410 FLOOR SUPPORT BOEING737 7375H4 138449DNM CABIN FLOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29508SW 24185 DURING SCHEDULED 1/2D CHECK, FOUND 5 EA NR 3 LONGITUDINAL FLOORBEAM CRACKS BETWEEN BS 658 TO BS 673.5, RBL 24.75. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20050620001102005062000110NM 2005 6 20 SWAA051720 120050611A335065C34691 LIGHT BOEING737 7375H4 138449DNM BULLNOSE LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29514SW 25153 DURING SCHEDULED A2 CHECK, FOUND EMERGENCY BULLNOSE LIGHT LOOSE AT ROW 15 ABC. SECURED LIGHT PER MM. 2L72 4F RTA16WE 20050620001112005062000111 2005 6 20 SWAA051721 420050610A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050620001132005062000113 2005 6 20 SWAA051723 420050610A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29640SW 27713 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050620001182005062000118NM 2005 6 20 05FDEA01608 120050614A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 MAIN DECK, SEAT TRACK RBL 47 CRACKED AT STA 6-70. CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2L73 4F RTA22WE 20050620001192005062000119 2005 6 20 SWAA051726 420050613A256565659723 PLATE BOEING737 7373H4 1384600NM GIRT BAR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR ATTACH AFT PLATE CORRODED AT BS 344, LBL 58. REMOVED AND REPLACED GIRT BAR ATTACH AFT PLATE PER MM. 2L72 4F RTA16WE 20050620001202005062000120NM 2005 6 20 SWAA051727 120050613A3350101331 LENS BOEING737 7373Q8 1384670NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29317WN 24068 LT OVERWING EMERGENCY EXIT DOOR LIGHT LENS MISSING. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20050620001242005062000124NM 2005 6 20 SWAA051731 120050613A53306545777 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29526SW 26568 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050620001252005062000125NM 2005 6 20 SWAA051732 120050613A3350D71701100 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT WILL NOT TEST A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29712SW 27846 DURING SCHEDULED HC1 CHECK, R1 DOOR, L1 DOOR, L2 DOOR & LT OVERWING HATCH EMERGENCY LIGHTS BATTERIES FAILED TEST. REMOVED AND REPLACED BATTERIES PER MM. 2L72 4F RTA16WE 20050620001262005062000126EU 2005 6 20 SA05070 120050612A4930 FUEL CONTROL AIRBUS320 A320214 3930316EU APU FAILED A USAAO OTHER H ELECT. POWER LOSS-50 PC CRCRUISE 1 EA19118US 1264 EN ROUTE, PHL TO SFO - DURING FLIGHT, THE APU AUTO-SHUTDOWN WITH THE NR 1 ENGINE IDG ON MEL. FLIGHT CONTINUED TO DESTINATION AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE SERVICED THE APU WITH 2.5 QUARTS OF OIL AND TIGHTENED A LINE TO THE APU FUEL CONTROL UNIT. ALSO, REPLACED THE FILLER COUPLING ON THE NR 1 ENGINE IDG. OPERATIONALLY AND LEAK CHECKS OK. 2L72 4F RTA28NM 20050620001272005062000127 2005 6 20 SA05071 420050613A2565 WIRE HARNESS AIRBUS320 A320214 3930316EU ESCAPE SLIDE MISROUTED A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19102UW 844 PHL - THE AFT, LEFT HAND SLIDE HAD A LIGHT HARNESS ROUTED INCORRECTLY AND A COVER RELEASE CABLE DISCONNECTED. MAINTENANCE CORRECTLY ROUTED THE LIGHT HARNESS ASSEMBLY AND CONNECTED THE COVER RELEASE CABLE. 2L72 4F RTA28NM 20050620001282005062000128NM 2005 6 20 AWXA200500700 120050613A53436576717217 FITTING BOEING737 73733A 1384673NM ZONE 500 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 MCN - MAJOR REPAIR - DURING C-21 CHECK FOUND CORROSION ON LEFT MAIN LANDING GEAR STABILIZER BEAM ATTACH FITTING ON WING AT RSS 197.56. MAINTENANCE BLENDED CORROSION ON LEFT MAIN LANDING GEAR STABILIZER BEAM ATTACH FITTING AND DETERMINED TO BE OUT OF LIMITS. REMOVED AND REPLACED ATTACH FITTING IAW BOEING 737-300 AMM 57-15-00-4. 2L72 4F RTA16WE 20050620001292005062000129 2005 6 20 AWXA200500701 420050614A3414 INDICATOR BOEING737 7373Q8 1384670NM LT AIRSPEED FAILED A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28327AW 23507 PHX - ABORTED TAKEOFF - FLT 792 - DURING TAKEOFF CAPTAINS AIRSPEED INDICATOR WAS FLAGGED AND NO AIRSPEED INDICATION. ABORTED TAKEOFF AT 90 KNOTS, RETURNED TO THE GATE IN PHOENIX WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 1 MACH AIRSPEED INDICATOR IAW BOEING 737-300 MM 34-12-21-424-05. OPERATIONAL TESTS WERE GOOD. TEAR DOWN REPORTS THEY COULD NOT CONFIRM FAULT HOWEVER DID REVEAL INTERMITTENT FLAGS THE 'N' POINTERS. UNIT WAS OVERHAULED WITH THE A/S MOTOR, DRIVER BOARD AND NEW 'N' POINTERS INSTALLED IAW CMM 34-12-02 REV. 1 2L72 4F RTA16WE 20050620001312005062000131NM 2005 6 20 AWXA200500703 120050530A521065512769 STOP FITTING BOEING737 73733A 1384673NM L1 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 MCN - MAJOR REPAIR - DURING C-21 CHECK FOUND L1 DOOR AFT UPPER CORNER STOP FITTING CRACKED .550 INCHES IN LENGTH AT STRINGER 8L AND BS 344. MAINTENANCE REMOVED THE DAMAGED L1 DOOR AFT UPPER STOP FITTING AND REPLACED IT IAW BOEING 737-300 SRM 51-40-02-0 FIGURE S 3, 6, 7, 8, 12 AND 14. 2L72 4F RTA16WE 20050620001322005062000132SO 2005 6 20 RAIA00506013 120050609A3242 SENSOR EMB 145 EMB145LR 3260212SO BRAKE TEMP MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03810HK 145231 FLT 3592 - RIC - BRAKE OVERHEAT MESSAGE ON EICAS JUST BEFORE TAKEOFF. NR 2 BRAKE TEMP INDICATION SPIKES MOMENTARILY. MAINTENANCE DEFERRED LT INBOARD BRAKE TEMP SENSOR. 2L72 4T RTT00011AT 20050620001352005062000135EU 2005 6 20 SA05073 120050614A30301663214301 COMPUTER AIRBUSA319 A319112 3930323EU PROBE HEAT FAILED A USAAO OTHER O OTHER APAPPROACH 1 EA19738US8963 3184 1254 ON FINAL APPROACH, AT 500 FEET AGL, THE CAPTAIN'S AIRSPEED INDICATOR READ 25 KNOTS SLOWER THAN THE FIRST OFFICER'S INDICATION. JUST BEFORE LANDING, THE POWER SURGED TO TOGO WITHOUT PILOT INPUT. THE PILOT FLYING PULLED THE POWER BACK TO IDLE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 PROBE HEAT COMPUTER. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20050620001372005062000137EU 2005 6 20 AWXA200500705 120050613A5347D5337111001000 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28642AW 584 SAL - MAJOR REPAIR - DURING C-7 CHECK FOUND CORROSION ON PASSENGER SEAT TRACK AT FR 46, -Y765. CORROSION ON SEAT TRACK AT FR 46, -Y765 WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS SRM 53-31-15 FIG 101. MAINTENANCE REMOVED SEAT TRACK AT FR 46, -Y765 AND REPLACED SEAT TRACK AT FR 46, -Y765 IAW AIRBUS SRM 51-42-11. 2L72 4F RTA28NM 20050620001382005062000138EU 2005 6 20 AWXA200500706 120050613A5347D5713014920202 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28642AW 584 SAL - MAJOR REPAIR - DURING C-7 CHECK FOUND CORROSION AT PASSENGER SEAT TRACK BETWEEN FR 39 AND FR 40, Y1292. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS SRM 53-31-15. MAINTENANCE REMOVED SEAT TRACK IAW AIRBUS SRM 51-42-11 AND REPLACED WITH NEW SEAT TRACK BETWEEN FR 39 AND FR 49, Y1292 AIRBUS SRM 51-42-11. 2L72 4F RTA28NM 20050620001402005062000140NM 2005 6 20 AWXA200500708 120050615A33501012721 LIGHT BOEING737 7373G7 1384595NM CABIN INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 PHX - EEL - DISCOVERED EMERGENCY EXIT LIGHT ON SEAT 16 ON THE LT SIDE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AT ROW 16 ON THE LEFT SIDE. OPERATIONAL CHECKS GOOD. 2L72 4F RTA16WE 20050620001442005062000144CE 2005 6 20 DJFA2005109 120050613A7500257SF7299 DUCT RAYTHNDH125 HAWKER800XP 7150012CE BLEED AIR BROKEN E DJFAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA23791TA 258291 DURING CLIMB, THE CREW RECEIVED A REAR BAY OVERHEAT ANNUNCIATOR. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT WAS RETURNED TO KIAD. A NORMAL LANDING WAS MADE AND ENGINES WERE SHUT DOWN ON THE TAXIWAY. MAINTENANCE REPLACED THE RIGHT ENGINE BLEED AIR DUCT. ENGINE GROUND RUNS WERE PERFORMED AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA3EU 20050620001462005062000146NM 2005 6 20 HNAA0500056 120050613A6120 PROPELLER DHAV DHC8 DHC8102 2809003NM NR 1 ENGINE MALFUNCTIONED A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07933HA 132 AFTER TAKEOFF AT APPROX 100 AGL THE NR 1 ENGINE CYCLED 10 PERCENT TQ ALONG WITH POWER UPTRIM LIGHT CYCLING ON AND OFF WITH BOTH PROP RPM'S AT 1200. 2H72 4T RTA13NM 20050620001472005062000147NM 2005 6 20 DHL2005741567 120050421A5313 STRINGER BOEING727 7272Q9 138448MNM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 STR 27L AT FUSELAGE STA 490 CORRODED C1 CARGO AREA. REMOVED FASTENER & CUT OUT DAMAGED AREA AT STR 27L BS 490 DIM: 16 INCH IAW B727 SRM 53-10-3. REPAIR PARTS FILLER: BAC 1498-113 PO5096102 (16 INCH) & SLICES P/N BAC 1498-132 PO 4496180 10 INCH. LOCATED DRILLED FASTENERS HOLES IAW B727 SRM 53-10-2 FIG 1. TREATED & PRIMED PARTS & AREA IAW B727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B727 SRM 53-10-3 FIG 1. 2L73 4F RTA3WE 20050620001482005062000148NM 2005 6 20 DHL2005784546 120050515A5740 BRACKET BOEING727 727227 1384078NM NR 2 LE ACTUATORCRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01784DH 22001 NR 2 LEADING EDGE ACTUATOR UPPER MOUNT IS CRACKED AT LWR INBOARD CORNER, WING STA 224. REMOVED DAMAGED MOUNT ANGLE IAW B727 SRM 51-30-2 AND FABBED NEW FROM 2024T3.063 PO 9002199 DIM 7.375 X 6.5 IAW B727 SRM 57-20-2 FIG 1. TREATED & PRIMED ANGLE IAW B727 SRM 51-10-2. INSTALLED NEW ANGLE ON NR 2 LEADING EDGE FLAP ACUATOR IAW B727 SRM 57-20-2 FIG 1. 2L73 4F A3WE 20050620001502005062000150NM 2005 6 20 DHL2005741554 120050418A5542 SKIN BOEING727 7272Q9 138448MNM RUDDER DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 UPPER RUDDER RT SIDE PANEL 9801 DENTED IN SEVERAL PLACES. CUT OUT DAMAGED AREAS DIM .25 INCH AND .375 INCH ON UPPER RUDDER RT SIDE PANEL 9801 IAW B727 SRM 51-10-1. FABRICATED 2 EA DOUBLER FROM 2024-T3 .032 SIZE 2.5 X 2.5 AND 2.5 X 2.5 PO 9001634 IAW B727 SRM 55-30-3 FIG 3. TREATED AND PRIMED PARTS AND AREA IAW B727 SRM 51-10-2. INSTALLED 2EA REPAIR DOUBLERS IAW B727 SRM 55-30-3 FIG 3. 2L73 4F RTA3WE 20050620001542005062000154NM 2005 6 20 DHL2005741571 120050425A5230 HINGE BOEING727 7272Q9 138448MNM CARGO DOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 FWD MCD HINGE CRACKED AT FUSELAGE STA 500. REMOVED FWD HALF HINGE IAW B727 SRM 51-30-2 FIG 7. FABBED TEMPLATE & DRILLED NEW HINGE IAW B727 SRM 51-30-2 FIG 1. CUT NEW HINGE SECTION IAW AEI STC DRAWING NO AE5291, REV C SHEET 3, 4 & 5 P/N:MS20001-16-17200 PO 7002150. TREATED AND PRIMED NEW HINGE SECTION IAW B727 SRM 51-10-2 & AEI STC DRAWING NO AE 5291 REV C. INSTALLED FWD HINGE SECTION IAW AEI STC DRAWING NO AE 5291 REV C, OPS CHECK GOOD IAW B727 AEI MM PAGE 190. 2L73 4F RTA3WE 20050620001552005062000155NM 2005 6 20 DHL2005764002 120050617A3260 LANDING GEAR BOEING727 727264 138408MNM MAIN MALFUNCTIONED A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01764AT 22984 LEFT GEAR DOOR LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. PERFORMED GEAR DOOR WARNING LIGHT ILLUMINATED WITH GEAR HANDLE UP OR OFF. ABNORMAL PROC RECYCLED GEAR AND LIGHT WENT OUT. CYCLED DOOR SEVERAL TIMES. INSP DOOR, NO DEFECTS NOTED. COULD NOT DUPLICATE, OPS NORMAL IAW MM 32-62-0. 2L73 4F A3WE 20050620001562005062000156NM 2005 6 20 DHL2005741572 120050425A5230 HINGE BOEING727 7272Q9 138448MNM CARGO DOOR BROKEN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 AFT MCD HINGE PIN BROKEN AT FUSE 580. REMOVED AFT HINGE SECTION IAW B727 SRM 51-30-2 FIG 7. CLEANED HINGE SECTION AND FUSE SKIN, EVAL NO CRACKS NOTED. CUT HINGE SECTION IAW AEI STC DRAWING NR AE5291, REV, C SHEETS 3, 4 & 5. TREATED & PRIMED HINGE SECTION & SKIN IAW B727 SRM 51-10-2 & AEI STC DRAWING NR AE5291 REV C. REPLACED HINGE PIN P/N:MS20233 P4-7200 IAW S/B AEI01-01-B. INSTALLED AFT HINGE SECTION IAW STC DRAWING NR AE5291 REV C. 2L73 4F RTA3WE 20050620001572005062000157EU 2005 6 20 DHL2005363003 120050617A3260 SWITCH AIRBUS300 A300B4203 3930306EU NLG STICKING A DHLAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 SO01363DH 85 NOSE GEAR INDICATED UNSAFE ON FWD PANEL DURING CVG APPROACH. THREE GREEN AND SAFE ON S/O PANEL. COMPLETED ABNORMAL PROCEDURE. FOUND 40GB SWITCH PLUNGER STICKING. LUBED PLUNGER GEAR INDICATION CKS GOOD IAW MM 32-61-00. 2L72 4F RTA35EU 20050620001582005062000158NM 2005 6 20 DHL2005784547 120050515A5320 WEB BOEING727 727227 1384078NM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01784DH 22001 VERTICAL STAB SLANT WEB AT 1303 LOWER LEFT CORNER IS CRACKED STA 1303 FRAME SECTION ABOVE CENTER INLET DUCT. COMPLIED WITH COTNEY AEROSPACE EA: EAZ04-1 REV A 8110-3. DATED 6/805 STOP DRILLED CRACK ON VERTICAL STAB WEB BS 1303 LBL 22 IAW 727 SRM 51-10-01 & S/B 727-53-0094. 2L73 4F A3WE 20050621000032005062100003NM 2005 6 21 SWAA051742 120050614A3350311500 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29315SW 23337 EMERGENCY EXIT BULLNOSE LIGHT LENS OUT OF POSITION AT ROW 8 DEF. REINSTALLED LENS PER MM. 2L72 4F RTA16WE 20050621000042005062100004NM 2005 6 21 SWAA051743 120050614A33506556633 LIGHT BOEING737 7373H4 1384600NM EMERGENCY EXIT ERRATIC A SWAAK NONE O OTHER ININSP/MAINT 1 SW29368SW 26579 OVERWING EMERGENCY EXIT LIGHTS REMAINED ILLUMINATED WITH EMERGENCY EXIT LIGHT SWITCH ARMED. POWERED DOWN AIRCRAFT & PERFORMED OPERATION CHECKS. ALL LIGHTS WORKING NORMAL PER MM. 2L72 4F RTA16WE 20050621000052005062100005NM 2005 6 21 SWAA051744 120050614A21214101054 FAN BOEING737 7377H4 1384404NM E & E BAY FAULTY A SWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW29473WN 33832 DIVERSION, ACRID ELECTRICAL ODOR IN CABIN. GASPER FAN & RECIRCULATION FAN SWITCHES TURNED OFF, ODOR DISSIPATED. REMOVED AND REPLACED EQUIPMENT COOLING FAN PER MM. 2L72 4F RTA16WE 20050621000062005062100006NM 2005 6 21 SWAA051745 120050614A3350BR2013 LIGHT BOEING737 7377H4 1384404NM AFT CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29481WN 29853 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT AFT CABIN. REINSTALLED EEPLS WIRING PER MM. 2L72 4F RTA16WE 20050621000072005062100007NM 2005 6 21 SWAA051746 120050614A534065C27314 STRINGER CLIP BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29508SW 24185 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 344, STR 11R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050621000082005062100008 2005 6 21 SWAA051747 420050614A2565D31354 SLIDE BOEING737 7373G7 1384595NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29683SW 24008 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050621000092005062100009NM 2005 6 21 SWAA051748 120050613A53306545765 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 16R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050621000132005062100013NM 2005 6 21 SWAA051736 120050614A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM CABIN FLOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FLOORBEAM UPPER CHORD CORRODED AT BS 328, BETWEEN LBL 28 & RBL 49. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20050621000162005062100016 2005 6 21 SWAA051750 420050615A256565659723 PLATE BOEING737 7373H4 1384600NM GIRT BAR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR ATTACH AFT PLATE CORRODED AT BS 344, LBL 58. REMOVED AND REPLACED AFT PLATE PER SRM. 2L72 4F RTA16WE 20050621000172005062100017NM 2005 6 21 SWAA051751 120050615A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050621000182005062100018NM 2005 6 21 SWAA051752 120050615A531065C26402 CREASE BEAM BOEING737 7373H4 1384600NM CABIN FLOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND FUSELAGE CREASE BEAM WEB CORRODED BETWEEN BS 727B TO BS 727C & BETWEEN BS 807 TO BS 827, RBL 70. REMOVED AND REPLACED CREASE BEAM WEB SECTIONS PER SRM. 2L72 4F RTA16WE 20050621000192005062100019NM 2005 6 21 SWAA051753 120050615A531065C26402 CREASE BEAM BOEING737 7373H4 1384600NM CABIN FLOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND FUSELAGE CREASE BEAM WEB CORRODED BETWEEN BS 767 TO BS 787, RBL 65. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM. 2L72 4F RTA16WE 20050621000202005062100020NM 2005 6 21 SWAA051754 120050615A53206545410 FLOOR SUPPORT BOEING737 7373H4 1384600NM CABIN FLOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727A + 18, RBL 45, WL 208. REPAIRED FLOORBEAM PER BFG ER. 2L72 4F RTA16WE 20050621000242005062100024NM 2005 6 21 SWAA051759 120050615A52406969854 GUSSET BOEING737 7375H4 138449DNM R1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29508SW 24185 DURING SCHEDULED 1/2D CHECK, FOUND R1 DOOR AFT LOWER GUSSET CRACKED. REMOVED AND REPLACED GUSSET PER SRM & BAC DRAWING. 2L72 4F RTA16WE 20050621000302005062100030NM 2005 6 21 SWAA051763 120050615A3350D71702001 BATTERY PACK BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29773SA 27881 DURING SCHEDULED RON CHECK, FOUND BATTERY PACK INOP FOR FWD RT SIDE BULLNOSE LIGHTS & R1 DOOR EVAC SLIDE LIGHTS. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050621000312005062100031WP 2005 6 21 ARWA20050603 120050607A793131800040 TRANSMITTER DOUG DC8 DC863F 302198FWP OIL PRESSURE MALFUNCTIONED A ARWAEA ENGINE SHUTDOWN UNSCHED LANDING RN PARTIAL RPM/PWR LOSS FALSE WARNING CRCRUISE 1 SO19661AV 45969 AT 1845Z NR 1 ENGINE OIL PRESSURE WENT -0- PSI, PERFORMED ABNORMAL CHECKLIST AND ENGINE INFLIGHT SHUTDOWN AT 1848Z. REMOVED AND REPLACED NR 1 ENGINE OIL PRESSURE TRANSMITTER IN ACCORDANCE WITH M/M 79-32-1; OPERATIONAL CHECK GOOD IN ACCORDANCE WITH M/M 79-32-0 AND 71-00 AND INSPECTED ENGINE INLET AND EXHAUST AREA FOR EVIDENCE OF FOD DAMAGE IN ACCORDANCE WITH PRATT & WHITNEY M/M 72-00; NO DAMAGE FOUND OR OIL LEAKS; VISUALLY VERIFIED OIL QUANTITY AND FOUND FULL. 2L74 4F 4A25 20050616001452005061600145NE 2005 6 16 C8GA20050014 220050602A7321 FCU BOEING727 727227 1384078NM PWA JT8 JT8D17 52049NE NR 2 ENGINE CONTAMINATED A C8GAEA ENGINE SHUTDOWN UNSCHED LANDING RE PARTIAL RPM/PWR LOSS VIBRATION/BUFFET CRCRUISE 1 SO29308AS535083505 22002 687407 FLT 722 FROM TOL TO RDU. IN CRUISE AT FL310, CREW NOTED POWER LOSS OF NR 2 ENGINE ACCOMPANIED BY EPR FLUXUATION, COMPRESSOR STALL, AND VIBRATION. CREW REDUCED POWER SETTING TO IDLE AND PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN. THE AIRCRAFT RETURNED TO TOL AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND AND DRAINED MOISTURE IN THE NR 2 ENGINE FCU, VERSALUBED FCU BELLOWS, LUBED ANTI-SURGEBLEED VALVES, CHECKED PS3 STRAINER AND FOUND NO DEFECTS, REPLACED OIL FILTER AS A PRECAUTION AND FOUND NO CONTAMINATION, INSPECTED INLET AND EXHAUST AND FOUND NO DAMAGE, AND PERFORMED GROUND HIGH POWER RUN WITH NO DEFECTS NOTED. CONDUCTED ACCEPTANCE FLIGHT TO FL 310 WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 20050616001482005061600148NM 2005 6 16 72300187 120050521A5320 STRUCTURE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 10 X 1 INCH AREA OF CORROSION. 2L73 4F4 FRTA3WE E2EA 20050616001502005061600150NM 2005 6 16 72300189 120050521A5320 STRUCTURE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 1 INCH AREA OF CORROSION. 2L73 4F4 FRTA3WE E2EA 20050616001522005061600152NM 2005 6 16 72300191 120050513A5320 ANGLE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 2 INCH AREA OF CORROSION. 2L73 4F4 FRTA3WE E2EA 20050616001542005061600154NM 2005 6 16 72300193 120050524A5340 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AO OTHER K FLUID LOSS ININSP/MAINT 1 GL23723CK 20545 A 6 X 1 INCH AREA OF CORROSION. 2L73 4F4 FRTA3WE E2EA 20050616001962005061600196CE 2005 6 16 DJFA2005107 120050605A3246AHA1814 NUT RAYTHNDH125 HAWKER800XP 7150012CE LT WHEEL MISSING E DJFAK NONE O OTHER ININSP/MAINT 1 EA23781TA 55 258281 KBED - THE FOLLOWING IS BEING REPORTED PER ROC/FAA REQUEST. DURING A ROUTINE MAINTENANCE VISIT IT WAS DISCOVERED THAT THE NR 2 MAIN WHEEL ASSEMBLY WAS MISSING SEVERAL LOCK NUTS. MAINTENANCE REPLACED THE NR 2 MAIN WHEEL ASSEMBLY. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA3EU 20050616002082005061600208NM 2005 6 16 2005UALA00496 120050602A5330 SKIN BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE GOUGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29128UA 30023 SKIN DENTED AND GOUGED 9 INCHES FWD OF BS 1961, 2 INCHES BELOW STRINGER 41R. DAMAGE REPAIRED PER SRM 53-00-01, FIGURE 201. 2L74 4F4 FRTA20WE E24NE 20050616002092005061600209NM 2005 6 16 2005UALA00497 120050602A5311 FRAME BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29128UA 30023 AFT CARGO LWR FRAME AT BS 1760, BL 0 IS DENTED ON UPPER TEE CHORD. DAMAGE REPAIRED PER FAA-APPROVED ENGINEERING DOCUMENT 747-5360-13-1295. 2L74 4F4 FRTA20WE E24NE 20050616002112005061600211EU 2005 6 16 2005UALA00499 120050530A5610 WINDOW AIRBUS320 A320232 3930326EU COCKPIT CRACKED A UALAA UNSCHED LANDING O OTHER CRCRUISE 1 WP2949UA 851 CAPTAIN'S INNER WINDOW PANE SHATTERED. ENGINEERING EVALUATED WINDOW AND CANNOT DETERMINE THE EXACT CAUSE OF THE FAILURE DUE TO A LACK OF OBVIOUS DAMAGE (INITIATION/CAUSE). THE WINDOW HAS BEEN FORWARDED TO THE MANUFACTURER SULLY (SAINT-GOBAIN) IN FRANCE FOR FURTHER EVALUATION (CONFIRMED IN FRANCE ON JUNE 21). 2L72 4F RTA28NM 20050616002132005061600213SO 2005 6 16 LR7A05095 120050603A5320342593R FITTING LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 654 4763 DURING SCHEDULED B-1 CHECK INSPECTION PER JOB CARD HB5303 FOUND FS 858 RT SUPPORT BEAM TO SLOPING LONGERON LOWER ATTACHMENT T FITTING CRACKED. FITTING REPLACED IAW DRW 342593 AND SMP583 51-60 & 51-70, FS 858, RBL 62.5, WL 190-192. 2H74 4T A1SO 20050616002332005061600233 2005 6 16 DL777050305 420050603A2330 HEADSET BOEING777 777232 1385232NM CABIN ARCED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27860DA 29951 LOG BOOK WRITE UP STATED THAT THERE WAS ARCING AT SEAT 38E. CREW CONFIRMED TO MTC HEADSET WAS PROBLEM NOT A/C EQUIPMENT. DISCARDED HEADSET. 2L72 4F RTT00001SE 20050616002712005061600271NM 2005 6 16 UPS05444661 120050513A5312 BULKHEAD BOEING747 747123F NM RT MLG WW CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C, RT WLG W/W FWD BULKHEAD LOWER AREA CORROSION REVEALED AT STA 1241 RBL 75-99. CORROSION BLEND OUT 0.063 X .875 X 1.25 INCH EXCEED SRM 57-10-01 FIG 1 LIMITS. RT WLG W/W FWD BULKHEAD LOWER AREA RBL 75-99 AREA CORROSION REMOVED & REPAIRED AS PER HX RS R57-12-35310 & UPS EO B747-5710-22305-A. 2L74 4F A20WE 20050616002742005061600274NM 2005 6 16 UPS05444663 120050518A531165B04315403 FRAME BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C AFT CARGO COMPT BS 1560 STR 34L FRAME INNER CHORD CRACKED (CRACK LENGTH 10.5 APPROX). AFT CARGO COMPT BS 1560 STR 32L TO STR 38L FRAME REPAIRED AS PER HX RS R53-62-35312 CONTINUED INSPECTION REQUIRE TO THE REPAIR AREA PER SB 747-53A2349 REV 2 & UPS EO B747-5310-22293-A. 2L74 4F A20WE 20050616002762005061600276NM 2005 6 16 USAA050638 120050509A5311 FRAME BOEING757 757225 1384959NM RROYCERB211 RB211535E4 54555NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19608AU 22204 BFM - C4 - FRAME, 1 INCH LONG CRACK AT STA 1743 AT STR 29 AR. INSTALLED TYPICAL FORMED SECTION REPAIR IAW SRM. (K) 2L72 4F4 FRTA2NM E12EU 20050617000012005061700001NM 2005 6 17 USAA050644 120050508A531553150213646LF FLOORBEAM BOEING757 757225 1384959NM RROYCERB211 RB211535E4 54555NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19608AU 22204 BFM - C4 - ANGLE, 0.9 INCH WIDE X 1.3 INCHES LONG X .025 INCH DEEP, CORROSION; LEVEL 2; TASK C53-242-02, FLOORBEAM AT RBL 60 APROX, STA 1320, FABED PARTS ON TR 513602 AND TR 513603 IAW TYP REP AND SRM. (K) 2L72 4F4 FRTA2NM E12EU 20050617000052005061700005NM 2005 6 17 USAA050728 120050526A5320146N87226312375 WEB BOEING757 7572B7 1384964NM RROYCERB211 RB211535E4 54555NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19614AU41219 27145 BFM - C4 - WEB, 3.0 INCH L X 2.0 W X .04 D, CORROSION; LEVEL 1; TASK C53-251-03 BETWEEN STA 1620, LBL 60. REMOVED WEB, FAB NEW IAW DWG AND SRM. (K) 2L72 4F4 FRTA2NM E12EU 20050617000452005061700045CE 2005 6 17 DXTA200500758 120050608A3260 UPLOCK SWITCH CESSNA750 750 2076810CE MLG OUT OF ADJUST E DXTAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL07962QS 7500126 CLIMBING THRU FL400 HEARD A THUMP, THEN THE RED GEAR UNSAFE LIGHT CAME ON. DESCENDING THRU FL300, HEARD ANOTHER THUMP THEN THE GEAR (RED) UNSAFE LIGHT WENT OUT. RED UNSAFE IS RED UNLOCK LIGHT. ADJUSTED AND SECURED LT MAIN AND NOSE GEAR UPLOCK SWITCHES. VERIFIED NOSE GEAR EXTENSION AT 9.75 INCHES. PERFORMED SEVERAL FAULT FREE GEAR SWINGS, NO DEFECTS NOTED. ALL WORK PERFORMED IAW CESSNA CE-750 MM CHAP 32-30-00. 2L72 4J RTT00007WI 20050617000462005061700046SO 2005 6 17 C2XA05TY046 120050605A3350110049 POWER SUPPLY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DEFECTIVE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2718556 145595 TYS MAINTENANCE FOUND THE LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED THE NR 4 EMERGENCY BATTERY POWER SUPPLY AND OPS CHECKS WERE GOOD. 2L72 4T RTT00011AT 20050617000472005061700047EA 2005 6 17 VNAA0505015 120050529A325016735109 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NLG STEERING FAILED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL05245PS2408 7919 THE AIRCRAFT VEERED HARD LEFT AND THE CREW ABORTED THE TAKEOFF. MAINTENANCE REMOVED & REPLACED THE RT & LT NLG STEERING FEEDBACK RVDTS IAW CRJ 200 AMM 32-51-20-400-801. OPERATIONAL CHECKS AND HIGH SPEED TAXI CHECK CONFIRMED THE SYSTEM SERVICEABLE. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050617000482005061700048EU 2005 6 17 SF20050608 120050608A3260 WARNING LIGHT SAAB SF340 SF340A 7850100EU MLG ILLUMINATED A UHLAO OTHER J WARNING INDICATION LDLANDING 1 GL1740SZ 40 PILOT REPORTED GEAR TRANSIT LIGHT REMAINED ON, WITH NO RIGHT MAIN GEAR DOWN AND LOCKED INDICATION. PILOT PERFORMED THE QRH, CYCLED LANDING GEAR, PERFORMED EXTENSION WITH EMERGENCY HYDRAULIC HAND PUMP, AND PULLED EMERGENCY LANDING GEAR HANDLE (EXPLOSIVE BOLTS). VERIFIED THE GEAR WAS DOWN BY THE CREW AND TOWER. GEAR COLLAPSED ON LANDING. ALL PASSENGERS AND CREW WERE SAFE AND UNHARMED UPON LANDING IN IAD. AIRCRAFT IS IN IAD AWAITING MAINTENANCE. 2L72 4T RTA52EU 20050617000542005061700054WP 2005 6 17 P9RA20050087 120050606A3260833703 PROXIMITY SENSOR DOUG DC9 DC982 3022082WP NLG DIRTY A P9RAO OTHER N FALSE WARNING CLCLIMB 1 SO1110801 49127 AFTER TAKEOFF FROM SYR, NOSE GEAR LIGHT REMAINED RED. PERFORMED GEAR RECYCLE IAW QRH AND LIGHT WENT OUT. CONTINUED FLIGHT. SFB MAINTENANCE INSPECTED AND FOUND OCCLUDED TARGET ON NOSE LANDING GEAR. CLEANED TARGET AND BITE CHECKED SYSTEM IAW M/M. NO FURTHER FAULTS NOTED. NO PART REPLACEMENT. 2L72 4F A6WE 20050617000602005061700060NM 2005 6 17 05FDEA01567 120050602A5347TXMACH84039 SEAT TRACK BOEING727 727200 138407ENM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25495FE 21669 SEAT TRACK, RBL 24, FS 480 - 690 HAS CORROSION AND EXISTING BLEND REPAIRS AND REQUIRES REPLACEMENT PER 7-5340-7-5002. REMOVED AND REPLACED TRACK, FABBED ON TRAVERLER T5-524062 AND INSTALLED IAW SRM 51-30-2. 2L73 4F RTA3WE 20050617000652005061700065NM 2005 6 17 05FDEA01572 120050609A53476615731 SEAT TRACK BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25495FE 21669 SEAT TRACK LBL 24.5 HAS CORROSION FROM STA 480 TO 540. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2. 2L73 4F RTA3WE 20050617000672005061700067NM 2005 6 17 05FDEA01574 120050609A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 MAIN DECK, SEAT TRACK LBL 47 CRACKED AT STA 755. CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2L73 4F RTA22WE 20050617000692005061700069 2005 6 17 05FDEA01576 420050610A3410ACP803047 STATIC PORT DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 FUSELAGE, LEFT HAND PRIMARY STATIC PORT (PRESSURE COMPENSATING PLATE ASSEMBLY) EXTERIOR SURFACE FOUND WITH SEVERAL PIT MARKS. FUSELAGE, LEFT HAND PRIMARY STATIC PORT REMOVED AND REPLACED PER AMM 34-11-03-4. CRITICAL WAVINESS CHECK COMPLIED WITH PER WORK CARD 34T1201, PRIMARY / ALTERNATE STATIC PORT WAVINESS. INSPECTION HEATER TEST CARRIED OUT PER AMM 30-30-00-700-801, LEAK TEST CARRIED OUT PER AMM 34-11-00-700-801 AND AMM 34-11-00-700-802. 2L73 4F RTA22WE 20050617000712005061700071NM 2005 6 17 05FDEA01578 120050610A5343AEA7051502 FITTING DOUG MD11 MD11 3023602NM ZONE 700 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 CENTER LANDING GEAR WHEEL WELL, RIGHT HAND TRUNNION SUPPORT FITTING GUIDE PIN HOLE BUSHING CORRODED. CENTER LANDING GEAR WHEEL WELL, RIGHT HAND TRUNNION SUPPORT FITTING GUIDE PIN HOLE CORROSION REMOVED PER SRM 53-40-00 VOLUME I, FIGURE 15. FINAL HOLE DIAMETER 1.680 INCHES FOUND WITHIN LIMITS PER SRM 53-40-00 VOLUME I, FIGURE 15. CORRODED BUSHING REMOVED AND REPLACED WITH NEW FABRICATED BUSHING PER CMM 20-20-07. REPAIR CLASSIFIED AS MAJOR REPAIR PER GMM 6-2-100. 2L73 4F RTA22WE 20050617000742005061700074SO 2005 6 17 RAIA00506010 120050608A2497 CONTACTOR EMB 145 EMB145 3260210SO NR 2 MFD DAMAGED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03805HK 145096 FLT 3542 - STL- NO PFD - MFD DISPLAY AND COMM NR 2 FAILURE. SHED BUSS FAILURE. MAINTENANCE REMOVED AND REPLACED THE SHED BUSS CONTACTOR. OPS CHECKED GOOD. 2L72 4F RTT00011AT 20050617000832005061700083 2005 6 17 MWEA050051 420050606A34604083700903 COMPUTER BOEING717 717200 1383700NM FAULTY A MWEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31907ME 55171 IN CLIMBOUT OF MKE OVER BRR NR 2 FCC FAIL WITH ENGINE LEFT AND RIGHT SYSTEMS FAULT AND A STALL WARNING FAULT. REMOVED AND REPLACED BOTH FCC. 2L72 4F TRA6WE 20050617000852005061700085NM 2005 6 17 05FDEA01582 120050610A5340 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 UPPER FUSELAGE, STA 440, STR 1R, STR TO FRAME CLIP DAMAGED. *S/D* REPLACED CLIP PER SRM 51-30-2. 2L73 4F RTA3WE 20050617000932005061700093EU 2005 6 17 05FDEA01592 120050613A5754 SKIN AIRBUS310 A310203 3930313EU KRUEGER FLAP BENT A FDEAK NONE O OTHER ININSP/MAINT 1 SO25404FE 233 WHILE INSPECTING AREA ON SNRM N00815, FOUND LEFT L/E TOP OUTBOARD AREA OF LT KRUEGER FLAP OUTBOARD HINGE CUTOUT HAS A 2 X 1 INCH AREA BENT OUT WITH A 0.4 INCH CRACK AND TWO GOUGES. COMPLIED WITH EA 6-5740-90157. OPS AND LEAK CHECK GOOD IAW A310-200 AMM 27-88-11-4. THIS IS A MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L72 4F RTA35EU 20050617000982005061700098EA 2005 6 17 VTZA200500114 120050613A5712601R102328 RIB CNDAIRCL600 CL6002B19 1900309EA WING CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27628BR 7240 RIGHT BATT RIB IS CRACKED .750 INCH BETWEEN THE ATTACHING FASTENERS. 2L72 4F RTA21EA 20050617001002005061700100EA 2005 6 17 VTZA200500112 120050613A5712601R107091 RIB CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27628BR 7240 LEFT BATT RIB IS CRACKED 1.5 INCH. 2L72 4F RTA21EA 20050617001022005061700102EA 2005 6 17 VTZA200500111 120050613A5320601R3111359 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27628BR 7240 LEFT 280 VERTICAL ANGLE IS CRACKED AT .5 INCH BETWEEN FASTENERS. 2L72 4F RTA21EA 20050617001042005061700104EA 2005 6 17 COMA0560342 120050609A326016600101 UPLOCK CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01936CA245262115 7043 FLIGHT 5736 - GEAR DISAGREE WARNING. REPLACED THE NLG UPLOCK ASSEMBLY. 2L72 4F RTA21EA 20050617001062005061700106SO 2005 6 17 C2XA05SH045 120050611A532014530644403 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714942 145037 SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION FR 39-45. MAINTENANCE REPAIRED LT OMEGA BEAM AT FR 44 PER EC 5320-01247, NO FURTHER ACTION REQUIRED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050617001082005061700108SO 2005 6 17 C2XA05SH047 120050611A532014530627001 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714942 145037 SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT VARIOUS AREAS BETWEEN FRAMES 22 & 29. MAINTENANCE REPAIRED LT OMEGA BEAM AT FRAME 29 PER EC 5320-01247, NO FURTHER ACTION REQUIRED. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050617001102005061700110SO 2005 6 17 C2XA05SH050 120050611A532014530644401 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714942 145037 SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT VARIOUS AREAS BETWEEN FRAMES 35-39. MAINTENANCE REPAIRED LT OMEGA BEAM BETWEEN FRAME 38 - FRAME 39 PER EC 5320-01247, NO FURTHER ACTION REQUIRED. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050617001122005061700112SO 2005 6 17 C2XA05CL045 120050610A323022270100001 SOLENOID VALVE EMB 145 EMB145LR 3260212SO NLG FAULTY A C2XAO OTHER O OTHER DEDESCENT 1 SW27159109090 9090 145455 CLE FLIGHT 2682 THE CREW REPORTED A VERY STRONG AND LOUD THUMPING FELT FROM THE NOSE WHEEL AREA WHEN THE GEAR WAS DOWN AND LOCKED. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR SOLENOID VALVE AND THE LANDING GEAR ELECTRONIC UNIT. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4T RTT00011AT 20050617001152005061700115EA 2005 6 17 VNAA0505010 120050523A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE PUNCTURED A VNAAO OTHER O OTHER NRNOT REPORTED 1 GL05206PS 7860 DURING THE INTERMEDIATE EXTERNAL INSPECTION THE CREW DISCOVERED TWO HOLES PUNCTURED IN THE FUSELAGE SKIN BELOW AND AFT OF THE CARGO DOOR. THE HOLES WERE TEMP REPAIRED AND THE AIRCRAFT WAS FERRIED TO DAY. MAINTENANCE REPAIRED DAMAGED STRINGERS 22L & 23L IAW CRJ 200 SRM 53-00-03 AND REPAIRED THE FUSELAGE SKIN AT FS 605-654.50 STR 20L-24L IAW BOMBARDIER REPAIR ENGINEERING ORDER 601R-53-61-1391. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050617001172005061700117EA 2005 6 17 VNAA0505016 120050529A5755CC670171135 HINGE FITTING CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE SPOILER CRACKED A VNAAK NONE O OTHER ININSP/MAINT 1 GL05702PS2573 10135 DURING A SCHEDULED INSPECTION THE RT OUTBOARD MULTI FUNCTION SPOILER CENTER HINGE FITTING ASSEMBLY WAS FOUND CRACKED. MAINTENANCE REMOVED & REPLACED THE HINGE FITTING ASSEMBLY IAW CRJ 700 AMM 57-73-27-000-801-A01 AND 57-73-27-400-801-A01. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050617001182005061700118EA 2005 6 17 VNAA0505017 120050531A2700 UNKNOWN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE UNKNOWN A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL05251PS 7931 THE CREW ABORTED THE TAKEOFF AFTER RECEIVING A CONFIG TRIM VOICE WARNING AT 80 KTS. AFTER CONFERRING WITH MAINTENANCE CONTROL, THE CREW PUT THE AIRCRAFT INTO PROPER TAKEOFF CONFIGURATION. THE CONFIGURATION WARNING SYSTEM OPS CHECKED GOOD. THE AIRCRAFT THEN DEPARTED WITH NO INCIDENT. 2L72 4F4 FRTA21EA E15NE 20050617001192005061700119EU 2005 6 17 05FDEA01545 120050608A5313 STRINGER AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25404FE 233 CORROSION ON INSIDE OF FWD CARGO DOOR CUTOUT ON STRINGER 42R AT FRAME 20A AROUND RIVET BUCKTAIL. REMOVED CORROSION IAW A310/200 SRM 51-74-10 CHECKED BEFORE AND AFTER THICKNESS IAW A310/200 SRM 51-10-04. REPAIR IAW EA6-5313-89485, TREATED AREA IAW A310/200 SRM 51-21-10 AND 5123-10. 2L72 4F RTA35EU 20050617001202005061700120NM 2005 6 17 05FDEA01552 120050608A5315AEA03901 FLOORBEAM DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 UPPER CARGO COMPARTMENT, FLOOR PANEL SUPPORT AT STA 1321, X= -33 TO -75 FOUND CORRODED. (PANEL 262EF AND 262LF). UPPER CARGO COMPARTMENT, FLOOR PANEL SUPPORT AT STA 1321, X= -33 TO -75 REMOVED AS PER SRM 51-35-01 VOLUME II. NEW REWORKED FLOOR PANEL SUPPORT INSTALLED AS PER DWG AEA0390 AND SRM 51-35-01 VOLUME II. CLASSIFIED MINOR REPAIR PER GMM 6-2-100. 2L73 4F RTA22WE 20050617001212005061700121EU 2005 6 17 AALA20050382 120050606A3350BR964814 LIGHT AIRBUS300 A300B4605R 3930308EU CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW2170079 619 JFK - SEAT MOUNTED EMERGENCY LIGHT COVER AT SEAT 33G BROKEN. REMOVED AND REPLACED SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AT SEAT 33G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20050617001222005061700122 2005 6 17 RAIA00506012 420050608A3418 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU STALL WARNING SYLOOSE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03567HK 41085 FLT 5446 - JLN - RIGHT HAND STALL SYSTEM WILL NOT TEST. MAINTENANCE RESECURED LOOSE CONNECTION. OPS CHECKED GOOD. 2L72 4T RTA41NM 20050617001232005061700123EU 2005 6 17 RAIA00506011 120050608A5270 WARNING LIGHT JETAIRJETSTMJETSTM4101 1500501EU CARGO DOOR ILLUMINATED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03574HK 41093 FLT 5711 - STL - ON T/O ROLL, BAG DOOR LIGHT ON CAPTION PANEL ILLUMINATED. MAINTENANCE DEFERRED THE BAG DOOR LIGHT PER THE MEL. 2L72 4T RTA41NM 20050617001242005061700124SO 2005 6 17 RAIA00506017 120050613A2720 WARNING LIGHT EMB 145 EMB145 3260210SO RUDDER ILLUMINATED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03803HK 145077 FLT 3580- RIC - RUDDER HARDOVER PROTECTION FAIL MESSAGE ON EICAS. MAINTENANCE PERFORMED OPS CHECK OF RUDDER CONTROL SYSTEM. OPS CHECKED GOOD. 2L72 4F RTT00011AT 20050620000012005062000001NM 2005 6 20 UPS05444667 120050519A534069B620501 SUPPORT FITTING BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C, BS 860 RBL 60 CARGO HANDLING FITTING SUPPORT PLATE FOUND CORROSION. CORROSION BLEND OUT 0.023 X .875 X 1.5 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. M/D BS 860 RBL 60 TIE DOWN FITTING REPLACED AS PER MM 20-51-01. 2L74 4F A20WE 20050620000032005062000003NM 2005 6 20 UPS05444669 120050520A534769B620491 CARGO TRACK BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE: C, M/D BS 700 LBL 78 TIE DOWN FITTING FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.020 X 1 X 1.25 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. M/D BS 700 LBL 78 TIE DOWN FITTING REPLACED AS PER MM 20-51-01. 2L74 4F A20WE 20050620000342005062000034CE 2005 6 20 DJFA2005108 120050613A3297 CONNECTOR CESSNA525 525 2076601CE CONTROL HANDLE DISCONNECTED E DJFAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 EA23253CW 5250253 ON VISUAL APPROACH, LANDING GEAR WAS SELECTED DOWN, DID NOT RECEIVE A GREEN GEAR POSITION INDICATION OR A GEAR UNSAFE INDICATION. DECLARED AN EMERGENCY. CHECKED LANDING GEAR ANNUNCIATORS USING ROTARY SWITCH, STILL DID NOT RECEIVE INDICATION. A LOW PASS WAS MADE PAST THE TOWER AND CONFIRMATION WAS GIVEN FROM THE TOWER THAT THE GEAR WAS DOWN. AIRCRAFT WAS LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND CONNECTOR P1013 ON LANDING GEAR CONTROL HANDLE TO BE PARTIALLY DISCONNECTED. THE CONNECTOR WAS RECONNECTED AND NEW BULBS WERE INSTALLED FOR DOWN LOCK INDICATORS. A LANDING GEAR EXTENSION AND RETRACTION FUNCTIONAL TEST WAS PERFORMED WITH NO NOTED DEFECTS. THE EMERGENCY GEAR EXTENSION LEVER WAS RESET. 1L72 4F RTA1WI 20050620000392005062000039SO 2005 6 20 CHQA200500111 120050609A5730 PANEL EMB 145 EMB145LR 3260212SO RT WING LEAKING A CHQAA UNSCHED LANDING K FLUID LOSS CRCRUISE 1 GL11286SK 145443 IN CRUISE AT FL310, A PASSENGER NOTIFIED F/A THAT A FLUID BUBBLE WAS COMING DOWN FLAPS ON RT WING. CAPT OBSERVED RT WING FROM FORWARD FLAP SECTION TO REAR FLAP WAS DARK GRAY COLOR & APPEARED WET. DIVERTED FOR FURTHER INSPECTION, AN EMERGENCY DECLARED. ON RUNWAY, RT ENGINE WAS SHUT DOWN, FUEL PUMP WAS TURNED OFF, FLAPS WERE LEFT DOWN. NO FIRE, AIRCRAFT TAXIED TO GATE. MX INSPECTED ACFT & FOUND TO BE SAFE FOR FERRY FLIGHT FROM RIC TO CMH FOR REPAIR OF THE RIGHT WING FUEL LEAK. REMOVED FUEL PANELS 631DB AND 641AB AND APPLIED SEALANT IN BAY UNDER 641AB IAW EMB 145 SRM 51-2000. REINSTALLED PANELS 631DB AND 641AB IAW EMB 145 AMM 28-11-01. PERFORMED TANK LEAK CHECK IAW EMB 145 MM 28-11-00. NO LEAKS NOTED. 2L72 4T RTT00011AT 20050620000432005062000043NM 2005 6 20 CALA0500195 120050611A3350D71702030 CHARGER BOEING737 737924 13848A1NM SEATS 19 & 22 INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2771411 30128 THE EMERGENCY LIGHTS WERE FOUND INOPERATIVE AT SEATS 19DEF AND 22DEF. THE BATTERY CHARGER WAS REMOVED AND REPLACED IAW MM 33-51-06. 2L74 4F RTA16WE 20050620000462005062000046EU 2005 6 20 01262005 120050126A2611 WARNING LIGHT SAAB SF340 340B 7860101EU E/E BAY ILLUMINATED A NSVAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA27277MJ 277 AVIONICS SMOKE LIGHT ILLUMINATED ON THE GROUND. 2L72 4T RTA52EU 20050620000502005062000050EU 2005 6 20 05062005 120050506A26131734362450 WARNING LIGHT SAAB SF340 340B 7860101EU RT TAILPIPE ILLUMINATED A NSVAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA27233CJ 233 RT TAILPIPE HOT LIGHT ILLUMINATED DURING TAKEOFF ROLL. 2L72 4T RTA52EU 20050620000632005062000063CE 2005 6 20 DXTA200500767 120050611A332046380191 LIGHT CESSNA750 750 2076810CE CABIN SMOKE E DXTAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07982QS 7500182 AT 41,000 FT WHITE PUFF OF SMOKE APPEARED FROM F/O CHART HOLDER LIGHT. THE LIGHT WAS OFF. THE MAP CB WAS PULLED AND THE SMOKE STOPPED. ITEM DEFERRED PER NJA CARRY OVER PROCEDURE AND MAINTENANCE CONTROLLER COLLARED AND INOP STICKER INSTALLED, CAT 99-9, CAT A, DUE 3 FLIGHT CYCLES. REMOVED SHORTED CHART HOLDER P/N 4638019-1, INSTALLED NEW CHART HOLDER OF SAME P/N . OPS CHECK GOOD, NO DEFECTS NOTED. WORK PERFORMED IAW CE-750 MM CHAP 27-13-00. 2L72 4J RTT00007WI 20050620000652005062000065CE 2005 6 20 DXTA200500764 120050610A3220 LANDING GEAR CESSNA750 750 2076810CE NOSE NOISY E DXTAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL07984QS 7500084 ON CLIMB A LOUD BANG CAME FROM NOSE GEAR AREA. ON DESCENT TWO LOUD BANGS CAME FROM SAME AREA. THE LAST ONE WAS VERY LOUD. ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20050620000802005062000080NM 2005 6 20 USAA200506002 120050613A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19522AU 23857 A 2.625 INCH CRACK IN FUSELAGE SKIN AT STR 3L, STA 727D. INSTALLED DOUBLER PER EA 81022. 2L72 4F RTA16WE 20050620000842005062000084NM 2005 6 20 SWAA051685 120050607A3350D71701100 BATTERY PACK BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29703SW 27837 DURING SCHEDULED RON CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050620000932005062000093NM 2005 6 20 SWAA051697 120050609A33506104789 BATTERY PACK BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED A1 CHECK, FOUND L1 & R1 DOOR LOWER EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050620000972005062000097NM 2005 6 20 SWAA051707 120050610A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29338SW 23960 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D + 17, STR 12R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050620000982005062000098NM 2005 6 20 SWAA051708 120050612A57436937877 FITTING BOEING737 7373H4 1384600NM LT WING CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29353SW 24889 DURING SCHEDULED SERVICE CHECK, FOUND LT WING WALKING BEAM AFT HANGER FITTING CORRODED. REMOVED AND REPLACED AFT HANGER FITTING PER MM. 2L72 4F RTA16WE 20050620001042005062000104NM 2005 6 20 SWAA051714 120050612A53306545769 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29508SW 24185 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT EQUIPMENT COOLING EXHAUST AFT CUTOUT, BS 378.13, LBL 2.80. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050620001052005062000105NM 2005 6 20 SWAA051715 120050612A53116545805 FRAME BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29508SW 24185 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16R. REPAIRED FRAME PER SWA EA. 2L72 4F RTA16WE 20050620001122005062000112NM 2005 6 20 SWAA051722 120050611A3350PH22300L STRIP BOEING737 7373H4 1384600NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29639SW 27712 DURING SCHEDULED C1 CHECK, FOUND PHOTOLUMINESCENT LIGHT STRIP LENS MISSING AT ROWS 6 ABC TO ROWS 8 ABC. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER MM. 2L72 4F RTA16WE 20050620001152005062000115NM 2005 6 20 SWAA051725 120050611A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29685SW 23401 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 737, STR 25R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050620001172005062000117NM 2005 6 20 P9RA20050090 120050613A3350767 BULB BOEING757 757231 1384950NM EMERGENCY LIGHT INOPERATIVE A P9RAK NONE L NO TEST ININSP/MAINT 1 SO11708TW 28480 LT NR 2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. ITEM DEFERRED PER 33-51-2; CANCUN MAINTENANCE. SAT MAINTENANCE 6/13/05 REMOVED AND REPLACED BULB. CLEARED MEL. 2L72 4F RTA2NM 20050620001392005062000139EU 2005 6 20 AWXA200500707 120050613A5347D5337111000800 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28642AW 584 SAL - MAJOR REPAIR - DURING C-7 CHECK FOUND CORROSION AT PASSENGER SEAT TRACK AT FR 43 AND Y765. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS SRM 53-31-15. MAINTENANCE REMOVED SEAT TRACK IAW AIRBUS SRM 51-42-11 AND REPLACED WITH NEW SEAT TRACK BETWEEN FR 41 AND FR 47, Y765 IAW AIRBUS SRM 51-42-11. 2L72 4F RTA28NM 20050620001422005062000142NM 2005 6 20 AWXA200500710 120050602A575465C26601156 SKIN BOEING737 73733A 1384673NM NR 4 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 MCN - DURING C-21 CHECK FOUND 2 CRACKS .275 INCHES IN LENGTH. BOTH CRACKS LOCATED ON THE BOTTOM OF THE NR 4 SLAT SKIN, AT SS 72 TO SS 74. MAINTENANCE CUT OUT DAMAGED AREA AT NR 4 SLAT SKIN AND FABRICATED REPAIR DOUBLER AND FILLER IAW BOEING 737-300 SRM 57-43-01. INSTALLED REPAIR PARTS IAW BOEING 737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050620001452005062000145NM 2005 6 20 DHL2005741552 120050418A5720 STIFFENER BOEING727 7272Q9 138448MNM RT WING BULGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 VERTICAL STIFFENER AT R/W WBL 92 BULGED AT LWR END. REMOVED DAMAGED EXISTING DOUBLER ON VERTICAL STIFFENER AT R/W WBL 92 IAW B727 SRM 51-30-2 FABRICATED REPAIRED DOUBLER FOR VERTICAL STIFFENER AT R/W WBL 92 DIM 8.375 X 2.125 INCH P/N 7075 T6 .071 PO 900573 IAW B727 SRM 57-10-2 FIG 3 AND 51-40-3 FIG 1. TREATED & PRIMED AREA AND DOULBER IAW B727 SRM 51-10-2. INSTALLED DOUBLER ON VERTICAL STIFFENER AT R/W WBL 92 IAW B727 SRM 51-30-2 & 51-40-3 FIG 1. 2L73 4F RTA3WE 20050621000102005062100010 2005 6 21 SWAA051733 420050612A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29755SA 27871 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050621000142005062100014NM 2005 6 21 SWAA051737 120050614A53106546956 CREASE BEAM BOEING737 7373H4 1384600NM CABIN FLOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND FUSELAGE CREASE BEAM WEB CORRODED AT BS 332 TO BS 344, RBL 63. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050621000212005062100021NM 2005 6 21 SWAA051755 120050615A53116546539 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME INNER CHORD CRACKED AT BS 616, LBL 64, WL 201. REPAIRED FRAME INNER CHORD PER BOEING SB. 2L72 4F RTA16WE 20050621000282005062100028NM 2005 6 21 ASMF200506009 120050606A3030 HEATER BOEING737 73776N 13844CHNM PITOT FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23997AM 30283 AIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCE OF AUXILIARY PITOT DID NOT GET HOT FRM 303 060 00. THE REPORT WAS DEFERRED BY MEL 30-5. MAINTENANCE PROCEDURE WAS PERFORMED IAW FIM 30-31 TASK PAGE 801. DEFERRED REPORT WAS CLOSED. 2L72 4F RTA16WE 20050621000292005062100029EA 2005 6 21 X6PA200500005 220050610A8500 CRANKCASE PIPER PA32 PA32R300 7103213SO LYC O540 AEIO540* EA RT ENGINE CRACKED E X6PAK NONE K FLUID LOSS ININSP/MAINT 1 SO336934J 32R7680389 1799548A ENGINE INSPECTED DUE TO AN OIL LEAK. DURING THE INSPECTION THE RIGHT CRANK CASE WAS FOUND CRACKED SIX INCHES IN LENGTH AROUND THE BOTTOM PERIMETER OF THE NR 3 CYLINDER. ENGINE TTSMOH 1028.22 1L71 3O3 O A3SO 1E4 20050621000332005062100033WP 2005 6 21 ASMF200506011 120050606A325039346895001 CYLINDER DOUG DC9 DC987 3022087WP NLG STEERING LEAKING W ASMFK NONE K FLUID LOSS ININSP/MAINT 1 SW23205AM13023 49405 DURING TRANSIT CHECK WAS DETECTED HYDRAULIC LEAK IN RIGHT NOSE WHEEL STEERING CYLINDER. AIRCRAFT WAS SENT TO THE HANGAR AND RIGHT NOSE WHEEL STEERING CYLINDER WAS REPLACED IAW MM 32-5202, TESTED CORRECT. 2L72 4F RTA6WE 20050621000342005062100034EU 2005 6 21 F3LA200500024 120050601A2121 BLOWER AIRBUSA319 A319112 3930323EU CABIN PRESSURE SMOKE A F3LAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM03901FR 1488 AIR TURNBACK, FLIGHT CREW REPORTED AVIONICS SMOKE INDICATION ON DEPARTURE. AIRCRAFT RETURNED TO CUN AND LANDED WITHOUT INCIDENT. PERFORMED OPERATIONAL CHECK OF EXTRACTION AND BLOWER FAN BY MCDU PER MM 21-26-00-710-001. NO FAULTS DETECTED. 2L72 4F RTA28NM 20050621000352005062100035EA 2005 6 21 DJFA2005103 120050530A28102780491117 RELIEF VALVE CNDAIRCL600 CL6002A12 1900304EA FUEL STORAGE LEAKING E DJFAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 EA23633CW 3013 SHORTLY AFTER T/O, TOWER REPORTED FUEL SPRAYING FROM RT WING. CREW VISUALLY VERIFIED, RETURNED AND LANDED WITHOUT INCIDENT. INSP FOUND FUEL LEAKING FROM RT WING VENT. WING FUEL PRESSURE RELIEF VALVE FOUND TO BE OPEN. EXTENDED REFUELING TEST WAS PERFORMED AND VALVE WENT TO CLOSED POSITION. STUCK VALVE WAS SUSPECTED. LT AND RT WINGS WERE REFUELED TO MAX LEVEL AND A/C STOPPED LEAKING FUEL. NO FURTHER DISCREPANCIES WERE NOTED. WHEN A/C ATTEMPTED T/O, FUEL WAS NOTICED STREAMING FROM RT WING. T/O WAS ABORTED PRIOR TO REACHING V1 SPEED. REPLACED RT WING LEVEL CONTROL VALVE AND FUEL VENT VALVE. BOTH ENGINES RUN TO T/O POWER WITH NO NOTED DEFECTS. A/C RETURNED TO SERVICE. 2L72 4F RTA21EA 20050621000392005062100039NM 2005 6 21 USAA050567 120050429A5330 SKIN BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US 24781 CLT - FOUND SKIN CRACKED, BS 727D PLUS 19 INCHES AND BS 727E AND BETWEEN S20R AND S23R. REPAIR PCW IAW SRM 53-00-01. (M) 2L72 4F RTA16WE 20050621000412005062100041EU 2005 6 21 ALGA101075 120050519A6220C62242006601 PIN UROCOPEC120 EC120B 8680987EU MAIN ROTOR CORRODED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03524AL883 1263 EXCESSIVE CORROSION ON INSIDE AND OUTSIDE OF PINS, SCRAPPED PINS. 1G72 3U NCR0001RD 20050621000432005062100043EU 2005 6 21 ALGA101077 120050519A6220C62242006601 PIN UROCOPEC120 EC120B 8680987EU MAIN ROTOR CORRODED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03524AL883 1263 EXCESSIVE CORROSION ON INSIDE AND OUTSIDE OF PINS, SCRAPPED PINS. 1G72 3U NCR0001RD 20050621000452005062100045EU 2005 6 21 B65A101081 120050425A7130105623134 FIREWALL BOLKMS105 BO105LSA1 5626021EU ENGINE BAY DAMAGED E B65AO OTHER O OTHER NRNOT REPORTED 1 GL13202LF 2014 FIREWALL REPAIRED TOO MANY TIMES AND NOW IS UNSAFE. 1G72 3U H3AU 20050621000462005062100046NM 2005 6 21 USAA050565 120050429A5311 FRAME BOEING737 737400 138449ANM FUSELAGE CRACKED A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19439US 24781 CLT - FOUND FRAME CRACKED, BS 727E BETWEEN S24R AND S25R. REPAIR PCW IAW SRM 53-00-07. (M) 2L72 4F RTA16WE 20050621000482005062100048WP 2005 6 21 ABXA050137 120050516A57535914872503 ATTACH BRACKET DOUG DC9 DC932F 3022067WP LT FLAP HINGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23909AX 47148 LEFT INBOARD FLAP HINGE ATTACH BRACKET CRACKED IN TWO PLACES INSIDE FLAP. MOVED AND REPLACED LEFT INBOARD FLAP HINGE ATTACH BRACKET IAW DC-9 DWG 5914872. 2L72 4F A6WE 20050621000492005062100049WP 2005 6 21 ABXA050138 120050516A2133565373501 OUTFLOW VALVE DOUG DC9 DC932F 3022067WP CABIN PRESSURE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23909AX 47148 CORROSION AROUND FASTENERS ON SUGAR SCOOP BETWEEN STA 945 - 965. REMOVED AND REPLACED OUTFLOW VALVE NOZZLE VALVE IAW DC-9 MM 21-32-05-4-0002. 2L72 4F A6WE 20050621000512005062100051WP 2005 6 21 ABXA050140 120050517A5347DWG53AA18STC055 SEAT TRACK DOUG DC9 DC932F 3022067WP FUSELAGE BROKEN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23909AX 47148 OUTBOARD SEAT TRACK AT FS 579 LEFT BLOWN AT SPLICE. REMOVED AND REPLACED LEFT OUTBOARD SEAT TRACK FS 579 - 560. 2L72 4F A6WE 20050621000532005062100053NM 2005 6 21 ABXA050142 120050531A5610141T483517 WINDOW BOEING767 767205 1385121NM COCKPIT DEFECTIVE A ABXAK NONE O OTHER ININSP/MAINT 1 GL23713AX 23058 L2 WINDOW WOULD NOT LOCK SHUT. REMOVED AND REPLACED L2 WINDOW IAW BOEING MM. 2L72 4F RTA1NM 20050621000542005062100054WP 2005 6 21 ABXA050136 120050513A53135914258501N LONGERON DOUG DC9 DC932F 3022067WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23909AX 47148 LONGERON 20 LT AFT OF TRAP PANEL FITTING CRACKED. REMOVED AND REPLACED LONGERON 20 LT IAW DC-9 SRM 51-30-1 AND 51-30-5. 2L72 4F A6WE 20050621000552005062100055NM 2005 6 21 USAA050645 120050506A5320 SUPPORT ANGLE BOEING757 757225 1384959NM RROYCERB211 RB211535E4 54555NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19608AU64222 22204 BFM - C4 - SUPPORT ANGLE, 26 INCHES L X 1 INCH W X .015 INCH DEEP, CORROSION; LEVEL 2; TASK C53-353-02, MAIN CABIN BETWEEN STA 1688-1715, RBL 6, FABRICATED NEW SUPPORT ANGLE IAW DWG AND SRM. (K) 2L72 4F4 FRTA2NM E12EU 20050621000572005062100057EA 2005 6 21 COMA0560320 120050529A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ACTIVATED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01819CA 7415 RIGHT ENGINE THRUST REVERSER CAUTION DURING TAKEOFF. DEFERRED MAINTENANCE ON THRUST REVERSER I/A/W MEL. 2L72 4F RTA21EA 20050621000582005062100058NM 2005 6 21 USAA050577 120050430A5320 ANGLE BOEING737 7374B7 1384702NM FWD CARGO BAY CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US 24781 CLT - FOUND TRANSITION ANGLE CRACKED .6 INCHES, FORWARD CARGO COMPARTMENT AT STRINGER 26R JUST FWD OF THE DOOR. INSTALLED A NEW TRANSITION ANGLE IAW SRM 51-10-02. (M) 2L72 4F RTA16WE 20050621000592005062100059NM 2005 6 21 USAA050575 120050430A5320 SUPPORT ANGLE BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US 24781 CLT - FOUND SUPPORT ANGLE CRACKED 1 INCH, INSIDE AIRSTAIR CONTROL BOX STRUCTURE AT STATION 348 STRINGER 15L. FABRICATED AND INSTALLED A NEW SUPPORT ANGLE IAW BOEING DRAWING NR 69-16970. (M) 2L72 4F RTA16WE 20050621000612005062100061EA 2005 6 21 A6WA200540191 120050605A3210601R572100323 BUSHING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT MLG TRUNNION MIGRATED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31418AW 7618 LT MLG AFT TRUNNION BUSHING MIGRATED .025 INCH. REMOVED BUSHING AND INSTALLED 2ND OVERSIZE BUSHING IAW REO. (K) 2L72 4F4 FRTA21EA E15NE 20050621000672005062100067NM 2005 6 21 C1HA200593003 120050529A7603 ROD BOEING727 727212 138407GNM PWA JT8 JT8D* NE POWER LEVER OUT OF ADJUST A C1HAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 GL15293AS 21348 696741 UPON APPLICATION OF FULL T/O THRUST NR 3 ENGINE POWER LEVER WENT TO FORWARD STOP AND EPR ONLY 2.00 (T/O EPR 2.09) T/O ABORTED IAW CHAMPION PROCEDURES. SOC, MX CONTROL NOTIFIED. ALL OTHER PARAMETERS IN YELLOW BAND FOR NR 3, NR 3 ENGINE INTAKE AND EXHAUST INSPECTED NO DAMAGE FOUND. PS4 & EPR (PT2/PT7) SENSITIVE LINES INSPECTED FOUND NORMAL. T/S PERFORMED IAW PWA JT8D MM 72-00-00 PAGE 151. LOWER THRUST ROD ADJUSTED IAW MM 76-12-00 PAGE 506. ENGINE POWER TEST PERFORMED ALL PARAMETERS NORMAL, REQUIRED T/O POWER MET. 2L73 4F4 F A3WE E2EA 20050621000682005062100068NM 2005 6 21 C1HA200593004 120050529A7603 POWER LEVER BOEING727 727212 138407GNM PWA JT8 JT8D* NE NR 3 ENGINE OUT OF RIG A C1HAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 GL15293AS 21348 696741 UPON APPLICATION OF T/O THRUST, NR 3 ENGINE POWER LEVER TO FORWARD STOP AND EPR ONLY 2.05 FULL T/O EPR = 2.13 T/O ABORTED IAW CHAMPION PROCEDURES. SOC, MX CONTROL NOTIFIED. ALL OTHER ENGINE PARAMETERS IN YELLOW BAND FOR NR 3, PERFORMED STATIC RIG CHECK IAW MM 71-00-00, ALSO PERFORMED TRIM OF NR 3 ENGINE IAW MM 71-00-00, OK FOR CONTINUED SERVICE. 2L73 4F4 F A3WE E2EA 20050621000702005062100070NM 2005 6 21 USAA050685 120050524A5320 SUPPORT BOEING757 7572B7 1384964NM RROYCERB211 RB211535E4 54555NE R4 THRESHOLD CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19614AU41219 27145 BFM - C4 - THRESHOLD SUPPORT, .028 INCH D X 1.5 INCH WIDE X 1.5 INCH L, CORROSION; LEVEL 1; TASK C53-252-03, BS 1658, RBL 60 R4 DOOR. R & R THRESHOLD SUPPORT IAW SRM. (K) 2L72 4F4 FRTA2NM E12EU 20050621000712005062100071SW 2005 6 21 KBM2005F00095 120050523A242415891F VOLT REGULATOR BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL ALTERNATOR FAILED E KBMAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 WP19188TV 2704 VOLTAGE REGULATOR ELECTRICAL FAILURE IN FLIGHT, REMOVED AND REPLACED. (K) 1G71 3U3 U H2SW E4CE 20050621000722005062100072NM 2005 6 21 USAA050564 120050429A5311 FRAME BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19439US 24781 CLT - FOUND FRAME CRACKED, BS 727B BETWEEN S22L AND S24L. REPAIR PCW IAW SRM 53-00-07. (M) 2L72 4F RTA16WE 20050621000732005062100073NM 2005 6 21 USAA050572 120050430A5754 SKIN BOEING737 7374B7 1384702NM RT WING SLAT DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US39931 24781 CLT - PREVIOUS REPAIR OF NR 5 SLAT, RT WING NR 5 SLAT 7 INCH BY 8 INCH AT OUTBOARD END. REPAIR PCW IAW SRM 57-43-01. (M) 2L72 4F RTA16WE 20050621000742005062100074NM 2005 6 21 USAA050573 120050430A5330 SKIN BOEING737 7374B7 1384702NM FUSELAGE DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US 24781 CLT - DOUBLER PREVIOUSLY INSTALLED, BETWEEN S12L AND S14L, BS 312 AT LOVER HINGE, CUTOUT FOR MED. REPAIR PCW IAW TR-52-10-12. (M) 2L72 4F RTA16WE 20050621000772005062100077NE 2005 6 21 KBM2005F00091 220050524A75329550158260 BLEED VALVE SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE ENGINE STICKING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P 2347 4126 BLEED VALVE STICKING, REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20050621000782005062100078 2005 6 21 KBM2005F00092 420050530A3452 TRANSPONDER SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE ATC MALFUNCTIONED A KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P 2347 TRANSPONDER, SHOWING 2 CODE AS TOWER CONTROL RECEIVES 1, REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20050621000792005062100079SW 2005 6 21 KBM2005F00093 120050507A772212444412 INDICATOR BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL TOT STICKING E KBMAO OTHER O OTHER TXTAXI/GRND HDL 1 WP19188TV6 2704 TOT GAUGE STICKING ON START UP. REMOVED AND REPLACED. (K) 1G71 3U3 U H2SW E4CE 20050621000802005062100080NM 2005 6 21 USAA050566 120050429A5330 SKIN BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19439US39931 24781 CLT - FOUND SKIN CRACKED, BETWEEN BS 907 AND BS 946 AND BETWEEN S20L AND S23L. REPAIR PCW IAW SRM 53-00-01. (M) 2L72 4F RTA16WE 20050621000812005062100081NM 2005 6 21 USAA050569 120050430A52306546921225 DOOR BOEING737 7374B7 1384702NM CARGO DAMAGED A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19439US 24781 CLT - PREVIOUS DOUBLER INSTALLED, 11.5 INCH FORWARD OF AFT EDGE OF DOOR, 8.5 INCH DOWN FROM UPPER EDGE OF DOOR, 10 INCH BY 11.5 INCH. REPAIR PCW IAW SRM 52-30-01. (M) 2L72 4F RTA16WE 20050621000842005062100084EA 2005 6 21 A6WA200540187 120050528A53206013501252 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31418AW 7618 RT SIDE FS 621- 625.3 INTERCOSTAL AT STR 14R IS CRACKED IN RADIUS APPROXIMATELY 1.2 INCH LONG. REMOVED AND REPLACED RT SIDE FS 621- FS625.3 INTERCOSTAL AT STR 14R IAW SRM. (K) 2L72 4F4 FRTA21EA E15NE 20050621000862005062100086EA 2005 6 21 A6WA200540188 120050530A5340 ATTACH FITTING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31418AW 7618 UNDERFLOOR INTERCOSTALS HAVE CRACKED ATTACH FLANGES AT FS 484, LBL 36, AND RBL 36. REPAIRED INTERCOSTAL IAW REO. (K) 2L72 4F4 FRTA21EA E15NE 20050621000872005062100087NM 2005 6 21 USAA050731 120050525A5320146N52467 FLOOR SUPPORT BOEING757 7572B7 1384964NM RROYCERB211 RB211535E4 54555NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19614AU41219 27145 PIT - C4 - FLOOR SUPPORT, 6 INCHES L X 1.5 INCHES W X .050 INCH D, 8 INCH L X 2 INCH WIDE X .060 INCH D, CORROSION; LEVEL 1; TASK C53-251-03, BS 1640, LBL 56. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM. (K) 2L72 4F4 FRTA2NM E12EU 20050621000882005062100088NM 2005 6 21 USAA050729 120050521A5320 INTERCOSTAL BOEING767 767222 1385122NM RROYCERB211 RB211535E4 54555NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19614UA41219 21875 BFM - C4- INTERCOSTAL UPPER CHORD, 20 INCHES L X 1 INCH W X .008 INCH D, CORROSION; LEVEL 1; TASK C53-252-03; CABIN FLOOR BS 1661-1680, RBL 10. FAB NEW INTERCOSTAL UPPER CHORD IAW SRM. (K) 2L72 4F4 FRTA1NM E12EU 20050621000892005062100089NM 2005 6 21 USAA050734 120050525A5320 SILL BOEING757 7572B7 1384964NM RROYCERB211 RB211535E4 54555NE DOOR FRAME CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19614AU41219 27145 BFM - C4 - UPPER CAP, 3.1 INCH L X .5 INCH W X .2 INCH D; CORROSION, NO LEVEL OR TASK AFT CARGO DOOR LOWER SILL FROM AFT TO FWD DOOR CUTOUT. REMOVED AND REPLACED UPPER CAP. (K) 2L72 4F4 FRTA2NM E12EU 20050621000902005062100090EA 2005 6 21 A6WA200540192 120050605A5542CC6702200103 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RUDDER DENTED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31418AW 7618 RUDDER RT SKIN DENTED 2.0 INCHES ABOVE RIB STATION 72.75 AND 14.3750 FORWARD OF TRAILING EDGE. DENT IS 2 INCHES LONG X 1.5 INCHES WIDE AND .020 INCH DEEP. REPAIRED RUDDER RT SKIN IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050621000922005062100092WP 2005 6 21 DHL2005801011 120050527A323257155835501 ACTUATOR DOUG DC8 DC873F 302199FWP MLG DOOR FAULTY A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01801DH 46033 "DOORS NOT LATCHED" LIGHT (UPPER LEFT) REMAINED ON FOR EXTENDED PERIOD AFTER TAKEOFF/GEAR RETRACTION (ABOUT 1 MIN) THEN FLASHED INTERMITTENTLY FOR 2-3 MINS BEFORE STAY ON,GO OUT, ALSO HAD RT. R & R RT MLG DOOR ACTUATING CYLINDER AND CONTROL VALVE IAW MM 32-32-7. CHECKED DOOR LIGHTS OPERATING INDICATION IAW WDM 32-1-0, TESTED OPERATION OF MLG DOORS AND OPERATING LIGHTS. OK. 2L74 4F RT4A25 20050621000932005062100093NM 2005 6 21 USAA050649 120050512A53405360511013630LF MOUNT BOEING757 757225 1384959NM RROYCERB211 RB211535E4 54555NE AFT GALLEY CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19608AU64222 22204 BFM - C4 - MOUNTPAD - .050 INCH L X .100 INCH W X .020 INCH D, CORROSION; NO LEVEL OR TASK, AFT GALLEY CTR RT MOUNT PAD. REMOVED, FABRICATED NEW PART AND INSTALLED IAW SRM. (K) 2L72 4F4 FRTA2NM E12EU 20050621000942005062100094NM 2005 6 21 USAA050727 120050524A5320 FLOOR SUPPORT BOEING757 7572B7 1384964NM RROYCERB211 RB211535E4 54555NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19614AU 27145 BFM - C4 - FLOOR SUPPORT, 1.0 INCH X 1.3 INCH X .020 INCH. CORROSION; LEVEL 2; TASK C53-221-03, S17L BET STA 365 AND 377 FL. FABRICATED ON TRAVELER NR T5/520007 21R FLOOR SUPPORT IAW SRM. (K) 2L72 4F4 FRTA2NM E12EU 20050621000952005062100095EU 2005 6 21 KBM2005F00099 120050530A77149580113720 TRANSMITTER SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE ENG TORQUE MALFUNCTIONED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH 2337 TORQUE TRANSMITTER UNIT CAUSES TORQUE GAUGE TO SPIN CLOCKWISE. REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20050621000962005062100096NM 2005 6 21 USAA050653 120050508A5313 STRINGER BOEING757 757225 1384959NM RROYCERB211 RB211535E4 54555NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19608AU64222 22204 BFM - C4 - STRINGER AND SPLICE, 2.5 INCH L X 1 INCH W X .045 INCH D, CORROSION; NO LEVEL OR TASK, STA 1720, STR 27R IB VERTICAL LEG. FAB PARTS AND INSTALLED IAW SRM. (K) 2L72 4F4 FRTA2NM E12EU 20050621000972005062100097NM 2005 6 21 USAA050578 120050430A5311 FRAME BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US 24781 CLT - FOUND A FRAME CORRODED, FS 294.5-S16L. INSTALLED REPAIR DOUBLER IAW SRM 57-70-11. (M) 2L72 4F RTA16WE 20050621000982005062100098WP 2005 6 21 ARWA20050601 120050602A2770 CABLE DOUG DC8 DC863F 302198FWP GUST LOCK BROKEN A ARWAK NONE O OTHER ININSP/MAINT 1 SO19661AV 45969 GUST LOCK HARD TO ENGAGE SUSPECT CABLE BROKEN. R & R GUST LOCK CABLE RUNNING NR 79A IN ACCORDANCE WITH DC8 M/M 27-70-0. RIGGED AND OPERATIONAL CHECK FOUND NORMAL IN ACCORDANCE WITH DC8 M/M 27-70-0. 2L74 4F 4A25 20050621001002005062100100NM 2005 6 21 USAA050733 120050525A5315 FLOORBEAM BOEING757 7572B7 1384964NM RROYCERB211 RB211535E4 54555NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19614AU41219 27145 BFM - C4 - FLOORBEAM, 2.5 IN L X 2 IN W X .027 IN D, 2 IN L X 2 IN W X .016 IN D; CORROSION; LEVEL 1; TASK C53-252-03, STA1640, BL 0-LBL 60. REPAIRED AS OUTLINED. (K) 2L72 4F4 FRTA2NM E12EU 20050621001012005062100101 2005 6 21 KBM2005F00108 420050606A3452066106200 TRANSPONDER SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE NAVIGATION INACCURATE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19351WM 2167 TRANSPONDER, FREQ OFF +3 MHZ, SENSITIVITY -68 DB. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050621001022005062100102NM 2005 6 21 USAA050646 120050502A5347BAC1520792 SEAT TRACK BOEING757 757225 1384959NM RROYCERB211 RB211535E4 54555NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19608AU 22204 BFM - C4 - SEAT TRACK, 3 INCHES LONG X .750 INCH WIDE X .058 INCHES DEEP, CORROSION; LEVEL 2; TASK C53-221-02. CABIN SEAT TRACK STA 365.25 TO 440, LBL 45.50. REMOVED AND REPLACED SEAT TRACK IAW SRM. (K) 2L72 4F4 FRTA2NM E12EU 20050621001072005062100107EU 2005 6 21 KBM2005F00115 120050524A6510350A33215300 BEARING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE T/R DRIVE SHAFT DELAMINATED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19966SH496 3787 TAIL ROTOR LAMINATED BEARINGS, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050621001082005062100108NM 2005 6 21 USAA050732 120050525A5320 FLOOR SUPPORT BOEING757 7572B7 1384964NM RROYCERB211 RB211535E4 54555NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19614AU41219 27145 BFM - C4 - FLOOR SUPPORT, 1.5 INCH L X 1.5 INCH W X .06 INCH D, 1.5 INCH L X 2 INCH X .050. CORROSION; LEVEL 1; TASK C53-252-03, BS 1640-1680 RBL 56. (K) 2L72 4F4 FRTA2NM E12EU 20050621001122005062100112NE 2005 6 21 ASMF200506012 220050608A7200109382351 ENGINE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE LEFT FOD W ASMFK NONE C F.O.D. ININSP/MAINT 1 SW23838AM3294 49397 725520 DURING TRANSIT TO PLATFORM WITH APU OUT OF SERVICE AND THE LEFT ENGINE DID OPERATE, IT HAD AN FOD DUE TO INGESTION OF WOOD CHOCK. DURING REVISION WERE DETECTED FOUR BLADES AND NOISE SUPPRESSOR WITH LEAST DAMAGES AND THERE WERE REWORKED IAW 72-33-22. BOROSCOPE INSPECTION WAS PERFORMED TO THE SIX, SEVEN AND THIRTEEN STAGES, BEING ALL CORRECT. THE LEFT ENGINE RUNNING TEST WAS PERFORMED IAW MM 71-00-00, ALL CORRECT. THE FCU AND PNEUMATIC SHUT OFF VALVE APU WERE REPLACED IAW 49-30-01, CONTINUED PNEUMATIC APU OUT OF SERVICE. 2L72 4F4 FRTA6WE E9NE 20050621001132005062100113NM 2005 6 21 DHL2005741553 120050418A5730 SKIN BOEING727 7272Q9 138448MNM RT WING DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DENT ON RT WING L/E AT WING STA 131-198. DENT FOUND TO BE OUT OF LIMITS IAW 727 SRM 57-20-1 FIG 1. REMOVED AND REPLACED RT WING FIXED L/E ASSY AT L/E STA 130 TO L/E STA 349 P/N 65-16209-6 PO 5096106 IAW 727 SRM 51-30-2 PER CUSTOMER REQUEST. 2L73 4F RTA3WE 20050621001142005062100114NM 2005 6 21 HNAA0500054 120050611A533085300022 SKIN PANEL DHAV DHC8 DHC8102 2809003NM FUSELAGE CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07943HA4181241812 167 A 6 INCH CRACK, 1.5 INCH CRACK DOUBLER SEPARATION AND NUMEROUS AREAS OF SURFACE CORROSION ON BELLY SKIN. REMOVED AND REPLACED SKIN PANEL. 2H72 4T RTA13NM 20050621001152005062100115 2005 6 21 MWEA050053 420050612A3421TSG420102 INVERTER DOUG DC9 DC981 3022081WP HORIZON INDICATOINOPERATIVE A MWEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31805ME 48031 THE STANDBY HORIZON INDICATOR FLAGGED OFF. REMOVED AND REPLACED STANDBY HORIZON INVERTER. 2L72 4F A6WE 20050621001162005062100116EU 2005 6 21 WRNA200500015 120050607A2497 WIRE AIRBUS300 A300B4203 3930306EU CONTROL PANEL BURNED A WRNAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO05504TA 216 AFTER ENG START CHECK LIST COMPLETED THERE WAS A STRONG ELECTRICAL SMOKE ODOR, FOLLOWED BY SMOKE COMING FROM BEHIND THE F/E PANEL (LEFT SIDE). AFTER PUTTING LINE AND TRANSFER SWITCH'S TO OFF, SMOKE STOPPED. BY PUTTING LINE AND TANSFER SWITCHES BACK TO NORMAL SMOKE NEVER STARTED AGAIN. MX PERFORMED A VISUAL INSPECTION OF AIRCRAFT ELECTRICAL COMPONENTS. NO DEFECTS NOTED, REMOVED F/E PANEL (51VU) FOR FURTHER INSPECTION. FOUND WIRE INSULATION CHAFED ON TRANSFER SWITCH NR 1. REPAIRED INSULATION ON WIRE AND REPOSITIONED IAW ESPM 20-53-29 VISUAL INSPECTION IAW ESPM 20-52-11 PERFORMED, AIRCRAFT ELECTRICAL SYSTEM TEST AND FUNTIONAL CHECK IAW 24-00-06, OP'S CHECKED SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA35EU 20050621001182005062100118EU 2005 6 21 AWXA200500694 120050609A5347D53472176200 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28642AW 584 SAL - MAJOR REPAIR - DURING C-7 CHECK FOUND CORROSION ON PASSENGER SEAT TRACK FROM FR59 TO FR60 AND BL Y 1292. MAINTENANCE MECHANICALLY REMOVED CORROSION IAW AIRBUS 320 SRM 51-74-00 AND FOUND REWORKED AREA TO BE OUT OF LIMITS. CUT OUT DAMAGED AREA IAW AIRBUS 320 SRM 53-00-11 FIG 201. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW 53-00-15 FIG 201. 2L72 4F RTA28NM 20050621001202005062100120NM 2005 6 21 AWXA200500696 120050607A53209630896 STIFFENER BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 MCN - MAJOR REPAIR - DURING C-21 CHECK DISCOVERED CRACK .322 INCHES LONG AT FORMED CHANNEL LOCATED AT BS 178 WL 230 RBL 17.1. MAINTENANCE REMOVED AND FABRICATED NEW CHANNEL IAW BOEING DWG 9-63089. INSTALLED FABRICATED REPAIR PARTS AT BS 178 WL 230 RBL 17.1 IAW BOEING 737-300 SRM 51-40-02-0 FIG 212. 2L72 4F RTA16WE 20050621001252005062100125NM 2005 6 21 ASMF200506013 120050610A2410729825L IDG BOEING757 7572Q8 1384972NM LEFT FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23805AM13985 26272 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING THE LEFT ENGINE STARTED, THE N2 REACHED 30 PERCENT AND IT DID NOT INCREASE. THE LEFT ENGINE WAS STARTED AGAIN OPENING THE STARTER VALVE MANUALLY AND IT STARTED TO SLOW, APPEARING THE L DRIVE AND L GEN OFF IN SUPERIOR PANEL MESSAGES AND L GEN OFF AND L DRIVE OFF EICAS MESSAGES COME ON. DURING REVISION WAS DETECTED OIL LEAK IN LEFT IDG; THE DPI WAS REVISED, BUT FAIL CONTINUED. AIRCRAFT WAS SENT TO THE HANGAR AND LEFT IDG WAS REPLACED IAW MM 24-11-01, TESTED CORRECT. 2L72 4F RTA2NM 20050616002572005061600257NM 2005 6 16 UPS05444640 120050517A532065B07953551 ANGLE BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C FWD CARGO COMPT - LT TUNNEL BS 295 WL 130 NWW VERTICAL WALL ANGLE FWD SURFACE CORROSION. CORROSION BLEND OUT 0.015 X 1 X 4 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT, FWD CARGO COMPT - LT TUNNEL BS 295 WL 130 VERTICAL WALL ANGLE REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050616002582005061600258NM 2005 6 16 UPS05444641 120050519A532065B0794233 STIFFENER BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C LT SIDE NWW SIDE PANEL AT BS 300-320 NR 4 STIFFENER (COUNT FROM TOP) FOUND RADIUS CRACKED APPROX .5625 INCH LONG RUNNING FROM FWD EDGE AS MARKED. LT SIDE NWW SIDE PANEL AT BS 300-320 NR 4 STIFFENER REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050616002592005061600259NM 2005 6 16 UPS05444642 120050519A5347 SEAT TRACK BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C M/D - BS 630-670 RBL 11 TIE DOWN TRACK CROWN & FLANGE FOUND CORROSION. CORROSION BLEND OUT 0.025 X .5 X 2 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. M/D BS 630-770 RBL 11 TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 14. 2L74 4F A20WE 20050616002602005061600260NM 2005 6 16 UPS05444643 120050519A5347 SEAT TRACK BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C M/D - BS 728, RBL 11 SEAT TRACK O/B FLANGE CORRODED. CORROSION BLEND OUT 0.025 X .75 X 3 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. M/D - BS 630 - BS 770 RBL 11 TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 14. 2L74 4F A20WE 20050616002612005061600261NM 2005 6 16 UPS05444644 120050519A5347 SEAT TRACK BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C M/D - BS 680-700 RBL 11 SEAT TRACK O/B FLANGE CORRODED. CORROSION BLEND OUT 0.024 X .5 X 5 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. M/D BS 630-770 RBL 11 TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 14. 2L74 4F A20WE 20050616002622005061600262NM 2005 6 16 UPS05444645 120050518A5347 SEAT TRACK BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C M/D- BS 1000-1100 LBL 11 SEAT TRACK SURFACE CORRODED AS MARKED. CORROSION BLEND OUT 0.036 X .875 X 2.25 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. M/D- BS 1000-1110 AND BS 1110-1150 LBL 11 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 34. 2L74 4F A20WE 20050616002632005061600263NM 2005 6 16 UPS05444646 120050518A5347 SEAT TRACK BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C M/D- BS 1040-1090 LBL 10 SEAT TRACK FLANGE CORROSION. CORROSION BLEND OUT 0.040 X 1 X 1.75 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. M/D BS 1000-1110 LBL 10 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 34. 2L74 4F A20WE 20050616002642005061600264NM 2005 6 16 UPS05444647 120050519A5347 SEAT TRACK BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C M/D- BS 760-780 RBL 75 TIE DOWN TRACK FLANGE FOUND CORROSION. CORROSION BLEND OUT 0.029 X .5 X 4 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. M/D BS 750-870 RBL 75 TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A. 2L74 4F A20WE 20050616002652005061600265NM 2005 6 16 UPS05444648 120050518A5347 SEAT TRACK BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C M/D- BS 862 RBL 74 SEAT TRACK FLANGE CORROSION. CORROSION BLEND OUT 0.035 X 1.5 X 1.5 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. M/D BS 750-870 RBL 75 TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A. 2L74 4F A20WE 20050616002662005061600266NM 2005 6 16 UPS05444650 120050519A5347 SEAT TRACK BOEING747 747123F NM FUSELAGE CORRUPTED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C M/D- BS 520-540 LBL 86 SEAT TRACK O/B FLANGE CORRODED. CORROSION BLEND OUT 0.018 X .5 X 10 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A FROM BS 480-570 LBL 86. 2L74 4F A20WE 20050616002672005061600267NM 2005 6 16 UPS05444653 120050519A5730 SKIN BOEING747 747123F NM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C RIGHT WING BS 1241 UPPER REAR SPAR BOLT HOLE NR 5 UPPER SKIN AND CHORD FOUND CRACKED (CRACK LENGTH 0.030 / 0.060 INCH). HOLE REWORKED AS PER EO B747-5740-17032-C. 2L74 4F A20WE 20050616002692005061600269NM 2005 6 16 UPS05444655 120050518A5711 SPAR BOEING747 747123F NM RT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C RIGHT BS 1241 WING UPPER REAR SPAR NR 3 BOLT HOLE FOUND CORROSION. HOLE REWORKED AS PER EO B747-5740-17032-C. HOLE OVERSIZED TO 1 INCH. 2L74 4F A20WE 20050617000032005061700003NM 2005 6 17 USAA050730 120050525A5320 SUPPORT BOEING757 7572B7 1384964NM RROYCERB211 RB211535E4 54555NE THRESHOLD CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19614AU41219 27145 BFM - C4- THRESHOLD SUPPORT, 4.0 INCH X 3.4 INCH W X .040 INCH D - 3 AREAS - CORROSION; LEVEL 1; TASK C53-251-03, BS 1640-1680, LBL 60 INCH. REMOVED AND REPLACED THRESHOLD SUPPORTS IAW SRM. (K) 2L72 4F4 FRTA2NM E12EU 20050617000442005061700044CE 2005 6 17 DXTA200500757 120050607A3260 LIGHT CESSNA750 750 2076810CE LT MLG INOPERATIVE E DXTAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL07970QS 7500070 LT LANDING MAIN GEAR LIGHT OUT. BEFORE LANDING GEAR WAS BLOWN DOWN AND MAIN GEAR UPLOCK TEE HANDLE WAS PULLED ACCORDING TO CHECK LIST. ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20050617000522005061700052EA 2005 6 17 VTZA200500109 120050609A2910AE4096G0060000 TUBE CNDAIRCL600 CL6002B19 1900309EA NR 3 HYD SYS LEAKING A VTZAO OTHER J WARNING INDICATION DEDESCENT 1 EA27657BR 7491 NR 3 HYD SYS QTY DROPPED TO 0 DURING DESCENT. REMOVED AND REPLACED NR 3 A PUMP TUBE ASSY. 2L72 4F RTA21EA 20050617000552005061700055NE 2005 6 17 TSAA0572023 220050512A7320442317 HMU BOEING737 73776N 13844CHNM CFMINTCFM567CFM567B22 13802NE NR 2 ENGINE DEFECTIVE A TSAAD RETURN TO BLOCK XL ENGINE FLAMEOUT NO TEST TXTAXI/GRND HDL 1 WP13742AL 30830 888375 ETOPS, MAINTENANCE RUN: NR 2 ENGINE FLAMED OUT DURING ENGINE RUN. THE ENGINE RUN WAS PERFORMED AFTER A HEAVY PHASE CHECK. REMOVED AND REPLACED NR 2 ENGINE FUEL PUMP AND HMU PER MM 73-21-10-4 AND 73-11-01-4. LEAK AND OPS CHECK GOOD PER MM 71-00-00. NO FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE 5/14/05. 2L72 4F4 FRTA16WE E00055EN 20050617000582005061700058NM 2005 6 17 05FDEA01555 120050609A5414 SKIN DOUG MD11 MD11 3023602NM NOSE COWL DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 0965 48436 NR 1 ENGINE, NOSE COWL AT APPROXIMATELY SEVEN O' CLOCK POSITION EXTERIOR SURFACE FOUND WAVINESS. NR 1 ENGINE, NOSE COWL REMOVED AND REPLACED PER AMM 71-11-01-4. 2L73 4F RTA22WE 20050617000592005061700059NM 2005 6 17 05FDEA01566 120050602A5347FXSRM53102 SEAT TRACK BOEING727 727200 138407ENM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25495FE 21669 SEAT TRACK, RBL 24 FS 690, SPLICE FOUND CORRODED UPON REMOVAL OF SPLICE PARTS. SPLICED IN SECTION OF SEAT TRACK STA 690 - 710 RBL 24 IAW SRM 53-10-5 FIG 1. SEAT TRACK FABBED ON TRAVELER T5/524451. SPLICES FABBED FROM P/N 60-3338/24, BATCH 913828, SPLICE PLATE FABBED FROM 7075-T6 .250. 2L73 4F RTA3WE 20050617000992005061700099EA 2005 6 17 VTZA200500110 120050614A5310601R5211680 DOOR FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27628BR 7240 PASSENGER DOOR FRAME TOP RADIUS CRACKED AT 1 INCH IN LENGTH FORWARD OF DATUM 1 AT FS 338.90. 2L72 4F RTA21EA 20050617001012005061700101EA 2005 6 17 VTZA200500113 120050613A531260034017595 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27628BR 7240 RIGHT SIDE COPILOTS BULKHEAD AT FS 280 RBL 9.0 IS CRACKED AT 1.0 INCH IN WEB RADIUS. 2L72 4F RTA21EA 20050617001032005061700103EA 2005 6 17 VTZA200500115 120050613A5320601R3111358 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27628BR 7240 RIGHT 280 VERTICAL ANGLE IS CRACKED AT .5 INCH BETWEEN FASTENERS. 2L72 4F RTA21EA 20050617001142005061700114EA 2005 6 17 COMA0570065 120050614A5315CC670341757 FLOORBEAM CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01340CA7435 10062 TRANSVERSE BEAM AT FS 280 FROM LBL 36 TO RBL 36 CORRODED ALONG UPPER AND LOWER EDGES. REPLACED THE TRANSVERSE BEAM AT FS 280 IAW BOMBARDIER REO 670-53-11-047 REV C. 2L72 4F RTA21EA 20050617001162005061700116EA 2005 6 17 VNAA0505011 120050524A3244184F234 TIRE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT MLG DAMAGED A VNAAK NONE O OTHER ININSP/MAINT 1 GL05251PS74 7931 EN ROUTE TO DAY THE CREW WAS NOTIFIED OF POSSIBLE NOSE WHEEL DAMAGE DUE TO A MISSING TOW BAR SHEAR PIN IN PHL. THE CREW CONTINUED TO DAY AND MADE AN UNEVENTFUL LANDING. MAINTENANCE FOUND THE RT NLG TIRE CHINE DAMAGED. THE WHEEL & TIRE ASSEMBLY WAS REMOVED & REPLACED IAW CRJ 200 AMM 32-42-01-000-801 AND 32-42-01-400-801. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050620000112005062000011NM 2005 6 20 UPS05M44678 120050607A3220 LANDING GEAR DOUG MD11 MD11F 3023600NM NOSE DAMAGED A IPXAO OTHER O OTHER LDLANDING 1 SO01272UP 48571 NOSE GEAR DAMAGED ON LANDING (FIRE). 2L73 4F RTA22WE 20050620000322005062000032NM 2005 6 20 SB05068 120050612A3260806007 CIRCUIT CARD BOEING737 737301 1384611NM E11 LOGIC SHELF UNKNOWN A USAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19558AU 23512 ON CLIMBOUT FROM CLT, CREW RAISED THE LANDING GEAR AND RECEIVED A RIGHT MAIN LANDING GEAR UNSAFE INDICATION OF BOTH RED AND GREEN LIGHTS. FLIGHT RETURNED TO FIELD AT CLT WITHOUT INCIDENT AND TAXIED TO THE GATE NORMALLY. NO EMERGENCY WAS DECLARED. CREW NOTED A NORMAL GEAR INDICATION OF THREE GREEN LIGHTS ON GEAR EXTENSION. MAINTENANCE CHECKED THE RIGHT MAIN LANDING GEAR SENSORS PER MM, JACKED AIRCRAFT AND SWUNG GEAR SEVERAL TIMES. COULD NOT DUPLICATE FAULT. REMOVED AND REPLACED CIRCUIT CARDS M981 AND M986, AS PRECAUTIONARY. GEAR INDICATION CHECKS GOOD PER MM. 2L72 4F RTA16WE 20050620000372005062000037EU 2005 6 20 0500883212 120050611A3350321454 POWER SUPPLY AIRBUS320 A320211 3930320EU EMERGENCY LIGHT BURNED A NWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL01312US453866048 152 AFTER TAKEOFF, ALL CREW MEMBERS OBSERVED A BURNING ODOR. CABIN EMERGENCY LIGHTING CIRCUIT BREAKER TRIPPED. RETURNED TO DTW AND LANDED UNEVENTFULLY. REPLACED EMERGENCY LIGHT POWER SUPPLY AND TESTED OK. CHECKED WIRING FOR DAMAGE AND FOUND OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA28NM 20050620000422005062000042NM 2005 6 20 CALA0500194 120050610A5711112A2101 SPAR BOEING737 737824 13844BZNM LT WING CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2727213 28773 INSPECTION FOUND LT WING FRONT SPAR CORRODED AT LT NR 1 BOOST PUMP UPPER BONDING JUMPER STRAP CONTACT, WS 120-121. REPAIRED IAW ECRA 5711-01140. 2L72 4F RTA16WE 20050620000582005062000058EU 2005 6 20 06102005 120050610A7722 INDICATOR SAAB SF340 340B 7860101EU ENGINE ITT WARNING LIGHT A NSVAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA27350CJ 350 LEFT ITT WENT TO 955 DURING TAKEOFF. 2L72 4T RTA52EU 20050620000662005062000066CE 2005 6 20 DXTA200500766 120050611A2120 ODOR CESSNA500 560CESSNA 2076750CE CABIN DETECTED E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07339QS 5600339 IN FLIGHT THERE WAS A SLIGHT BURNING SMELL, THOUGHT IT WAS BLEED AIR FOR HEAT. DURING SHUTDOWN, CAPTAIN SMELLED ELECTRICAL BURNING/MELTING SMELL AND 20 MINUTES LATER F/O TURNED ON MASTER & AVIONICS, AND SMELLED SAME SMELL A LITTLE STRONGER. COULDN'T TELL WHERE THE SMELL WAS COMING FROM. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20050620000772005062000077EU 2005 6 20 SA05067 120050611A335032145410 EPSU AIRBUS320 A320214 3930316EU EMERGENCY LIGHT FAULTY A USAAK NONE L NO TEST ININSP/MAINT 1 EA19122US15363 1298 PIT - THE EMERGENCY LIGHTS SYSTEM TESTED INOPERATIVE. MAINTENANCE REPLACED THE FORWARD EMERGENCY POWER SUPPLY UNIT AND BATTERIES. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20050620000862005062000086NM 2005 6 20 SWAA051700 120050609A55236959227 BUSHING BOEING737 7373H4 1384600NM ELEVATOR TAB WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29335SW 23939 DURING SCHEDULED C4 CHECK, LT & RT ELEVATOR TABS FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED LT & RT ELEVATOR TABS NR 1 HINGE BUSHINGS & HARDWARE. 2L72 4F RTA16WE 20050620000882005062000088NM 2005 6 20 SWAA051702 120050608A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29376SW 26584 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727B, STR 16R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050620000992005062000099NM 2005 6 20 SWAA051709 120050612A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29375SW 26583 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D + 17, STR 12R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050620001002005062000100NM 2005 6 20 SWAA051710 120050610A55236959227 BUSHING BOEING737 7373H4 1384600NM RT ELEV TAB WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29383SW 26589 DURING SCHEDULED C3 CHECK, RT ELEVATOR TAB FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB NR 1 HINGE BUSHING & HARDWARE PER MM. 2L72 4F RTA16WE 20050620001092005062000109NM 2005 6 20 SWAA051719 120050612A57126545445 RIB BOEING737 7375H4 138449DNM RT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29508SW 24185 DURING SCHEDULED 1/2D CHECK, FOUND RT WING RIB LOWER CHORD CRACKED AT WBL 135.5, BETWEEN STR 2 & STR 3. REPAIRED RIB PER SRM & SWA TASKCARD. 2L72 4F RTA16WE 20050620001142005062000114NM 2005 6 20 SWAA051724 120050611A3697W176005 WIRE BOEING737 737301 1384611NM BLEED SYSTEM CHAFED A SWAAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW29660SW 23230 DIVERSION/DECLARED EMERGENCY. CABIN ALTITUDE HORN SOUNDED, PERFORMRED EMERGENCY PROCEDURE AND INITIATED EMERGENCY DESCENT. REPAIRED WIRING HARNESS ON BLEED VALVE PER WDM. 2L72 4F RTA16WE 20050620001222005062000122NM 2005 6 20 SWAA051729 120050613A534065C27314 STRINGER CLIP BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29508SW 24185 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 947, STR 25R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050620001232005062000123NM 2005 6 20 SWAA051730 120050613A531265C35740 PRESSURE PANEL BOEING737 7375H4 138449DNM NLG W/W CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29508SW 24185 DURING SCHEDULED 1/2D CHECK, FOUND NLG W/W CEILING PANEL CRACKED AROUND LT & RT BRAKE MOUNT PADS. REPAIRED PANEL PER SWA EA & SRM. 2L72 4F RTA16WE 20050620001332005062000133 2005 6 20 DJFA2005110 420050614A2397 WIRE BEECH MU300 400A 1155402CE RADIO BURNED E DJFAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA23735TA 1860 RK274 THE CREW REPORTED A SMELL OF BURNING WIRES AND NOTICED SMOKE COMING FROM THE GLARESHIELD AND FROM THE FRONT OF THE WINDSHIELD. THE CREW ALSO NOTICED THAT THE NR 1 RADIO TRANSFER UNIT WAS INOPERATIVE. PULLED THE RTU CIRCUIT BREAKER TO STOP THE SMOKE. THE AIRCRAFT WAS DIVERTED TO KMEM AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RADIO TRANSFER UNIT. AN OPERATIONAL CHECK WAS PERFORMED WITH NO NOTED DEFECTS. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4F RTA16SW 20050620001342005062000134 2005 6 20 SA05072 420050614A2565 STRAP AIRBUS320 A320214 3930316EU ESCAPE SLIDE MISROUTED A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19109UW 1065 PIT - THE AFT RIGHT SLIDE YELLOW RELEASE STRAP WAS FOUND NOT ROUTED THROUGH THE RELEASE TRIGGER OF THE GIRT BAR. MAINTENANCE CORRECTLY ROUTED THE RELEASE STRAP. OK FOR SERVICE. 2L72 4F RTA28NM 20050620001362005062000136EU 2005 6 20 AWXA200500704 120050613A5347D5337111200400 SEAT TRACK AIRBUS320 A320232 3930326EU CORRODED CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28642AW 584 SAL - MAJOR REPAIR - DURING C-7 CHECK FOUND CORROSION ON PASSENGER SEAT TRACK FROM FR 41 TO FR 47, BL Y1292. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW SRM 51-72-11. MAINTENANCE REMOVED AND REPLACED SEAT TRACK FROM FR 41 TO FR 47, BL Y1292 IAW AIRBUS SRM 51-72-11. 2L72 4F RTA28NM 20050620001412005062000141EU 2005 6 20 AWXA200500709 120050613A5347D5337111200500 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28642AW 584 SAL - MAJOR REPAIR - DURING C-7 CHECK FOUND CORROSION AT PASSENGER SEAT TRACK AT FR 44 AND -Y1292. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS SRM 53-31-15. MAINTENANCE REMOVED SEAT TRACK IAW AIRBUS SRM 51-42-11 AND REPLACED WITH NEW SEAT TRACK BETWEEN FR 41 AND FR 47, -Y1292 AIRBUS SRM 51-42-11. 2L72 4F RTA28NM 20050620001432005062000143NM 2005 6 20 SB05070 120050614A2133322684004 OUTFLOW VALVE BOEING737 737301 1384611NM CABIN AIR INOPERATIVE A USAAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 EA19575US5278052780 23740 EN ROUTE WITH THE AUTO PRESSURIZATION ON MEL, LOST CONTROL OF STANDBY PRESSURIZATION MODE. CABIN ALTITUDE BEGAN TO CLIMB, PILOT REQUESTED AN EMERGENCY DESCENT. REGAINED PRESSURIZATION CONTROL AT APPROX FL280. LANDED WITHOUT INCIDENT. MX CLEARED MEL WITH REPLACEMENT OF CABIN PRESSURE CONTROLLER & OVERHEAD PANEL. OPS TEST GOOD. DURING PRESSURE CONTROL SYS OPS CHECK, FOUND FORWARD OUTFLOW VALVE INOP. REPLACED FORWARD OUTFLOW VALVE. OPS CHECK & LEAK CHECK GOOD. DURING LEAK DOWN RATE CHECK, FOUND EQUIP COOLING VALVE LEAKING IN CLOSED POSITION. REPLACED VALVE, APU BLEED VALVE FOR NOT FULLY CLOSING, RIGHT AIR CYCLE MACHINE AND OVERHEAT SWITCH FOR NOT COOLING. ALL OPS & LEAK CHECKS GOOD. 2L72 4F RTA16WE 20050620001492005062000149NM 2005 6 20 DHL2005741568 120050421A5313 STRINGER BOEING727 7272Q9 138448MNM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 STR 28L AT FUSELAGE STA 545 CORRODED C1 CARGO AREA. REMOVED CORROSION ON STR 28L FUSE STA 545 FOUND TO OUT OF LIMITS IAW B727 SRM 51-10-6 AND 53-10-1 CUT OUT DAMAGED SECTION OF STR 28L DIM 18 INCHES IAW B727 SRM 53-10-3 FIG 1. FABRICATED STRINGER FROM BAC 1493-412 SIZE 18 INCHES PO 4246397 AND CHANNEL FROM 7075-T6 .050 2 EA SIZE 11.75 INCH AND HAT SECTION FROM 7075-T6 .050 4 EA SIZE 9 INCH AND FILLERS FROM 7075-T6.050 SIZE 9 INCH PO 9002126 IAW B727 SRM 53-10-3 FIG 1 DETAIL II. TREATED AND PRIMED PARTS AND AREA IAW B727 SRM 51-10-2. INSTALLED STR REPAIR PARTS IAW B727 SRM 53-10-3 FIG 1 DETAIL II. 2L73 4F RTA3WE 20050620001512005062000151NM 2005 6 20 DHL2005741555 120050418A5311 FRAME BOEING727 7272Q9 138448MNM FUSELAGE BENT A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 AFT CARGO STA 1010 AT STR 24 FRAME BENT RIGHT. FRAME OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 1. CUT OUT DAMAGE AREA DIMS 1.5 X 1.5 INCH AND FABRICATED REPAIR DOUBLER FROM MAT USED 7075-T6 .071 PO 9002118 AND DIMS 14 X 14 INCH IAW B727 SRM 51-40-3 FIG 1 & MAT ID 53-10-2. TREATED AND PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED REPAIR DOUBLER IAW B727 SRM 51-20-2 & 51-10-3 FIG 1. 2L73 4F RTA3WE 20050620001532005062000153NM 2005 6 20 DHL2005741574 120050425A5347 SEAT TRACK BOEING727 7272Q9 138448MNM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 SEAT TRACK 24R AT BS 760 TO 848 CORRODED. REMOVED SEAT TRACK AT BS 76 - 848 RBL 24 IAW B727 SRM 51-30-2. REPLACED, LOCATED & DRILLED FASTENER HOLES IN P/N BAC1520-841 PO 9002155 (8FT) IAW B727 SRM 51-30-2 FIG 1. TREATED AND PRIMED AREA & PART IAW B727 SRM 51-10-2. INSTALLED SEAT TRACK IAW B727 SRM 51-30-2 FIG 15 & 53-10-5 FIG 1. 2L73 4F RTA3WE 20050621000112005062100011NM 2005 6 21 SWAA051734 120050614A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FLOORBEAM UPPER CHORD CORRODED AT BS 294.5, BETWEEN LBL 7.5 & RBL 7.5. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20050621000122005062100012NM 2005 6 21 SWAA051735 120050614A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM CABIN FLOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FLOORBEAM UPPER CHORD CORRODED AT BS 312, BETWEEN RBL 8 & RBL 35. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20050621000232005062100023NM 2005 6 21 SWAA051758 120050615A335065C34691 LIGHT BOEING737 7373H4 1384600NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29355SW 25250 BULLNOSE EMERGENCY EXIT LIGHT MISSING AT ROW 2. INSTALLED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20050621000262005062100026NM 2005 6 21 SWAA051761 120050615A53306545776 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 942, STR 25R. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050621000272005062100027 2005 6 21 SWAA051762 420050615A2565D31354 SLIDE BOEING737 7373T5 1384608NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050621000362005062100036CE 2005 6 21 71138 120050602A3350 DIODE BEECH 1900 1900D 1154162CE EMERGENCY LIGHTSFAULTY A AMWAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 CE07126YV UE126 EMERGENCY COCKPIT LIGHTING ON, OFF HOT BATTERY BUSS, MAIN BATTERY SWITCH OFF AND SWITCH FOR FLIGHT INSTRUMENT INDIRECT LIGHTS ON. ELECTRICAL ODOR IN COCKPIT AREA. MAINTENANCE REMOVED AND REPLACED DIODE. 2L72 4T RTA24CE 20050621000372005062100037CE 2005 6 21 71124 120050601A3320 RHEOSTAT BEECH 1900 1900D 1154162CE CABIN LIGHTS BURNED A AMWAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 CE07126YV UE126 CREW CALLED IN AND REPORTED THAT WITH COCKPIT EMERGENCY LIGHTS ON, BATTERY OFF, INDIRECT LIGHTING ON, THERE WAS AN ELECTRICAL BURNING ODOR. MAINTENANCE REMOVED AND REPLACED INDIRECT LIGHT RHEOSTAT SWITCH. 2L72 4T RTA24CE 20050621000402005062100040EU 2005 6 21 ALGA101074 120050519A6220C62242006601 PIN UROCOPEC120 EC120B 8680987EU MAIN ROTOR CORRODED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03524AL883 1263 EXCESSIVE CORROSION ON INSIDE AND OUTSIDE OF PINS, SCRAPPED PINS. 1G72 3U NCR0001RD 20050621000422005062100042EU 2005 6 21 ALGA101076 120050519A6220C62242006601 PIN UROCOPEC120 EC120B 8680987EU MAIN ROTOR CORRODED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03524AL883 1263 EXCESSIVE CORROSION ON INSIDE AND OUTSIDE OF PINS, SCRAPPED PINS. 1G72 3U NCR0001RD 20050621000442005062100044EU 2005 6 21 B65A101079 120050425A63104639202011 CLUTCH BOLKMS105 BO105LSA1 5626021EU M/R XMSN UNSERVICEABLE E B65AK NONE O OTHER ININSP/MAINT 1 GL13202LF4719 2014 CLUTCH WORN BEYOND LIMITS. 1G72 3U H3AU 20050621000472005062100047WP 2005 6 21 ABXA050141 120050516A5230SB0952008945 PAN DOUG DC9 DC932F 3022067WP FWD CARGO DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23909AX 47148 CRACK IN OUTER PAN AT FASTENER AFT EDGE STOP NR 3. REPAIRED CRACK IAW DC-9 SRM 52-03. 2L72 4F A6WE 20050621000502005062100050WP 2005 6 21 ABXA050139 120050516A5320591141237 INTERCOSTAL DOUG DC9 DC932F 3022067WP FWD CARGO CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23909AX 47148 INTERCOSTAL CRACKED BETWEEN STA 484 AND 503 AT LONGERON 30 FORWARD LOWER CARGO. REPAIRED AREA IAW DWG K05159 AND DC-9 SRM 51-30-5. 2L72 4F A6WE 20050621000602005062100060SW 2005 6 21 KBM2005F00094 120050504A772212444412 INDICATOR BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL TOT STICKING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19188TV41 2704 TOT INDICATOR STICKING, REMOVED AND REPLACED. (K) 1G71 3U3 U H2SW E4CE 20050621000642005062100064 2005 6 21 SA05061 420050601A2565 CABLE AIRBUS320 A320214 3930316EU ESCAPE SLIDE DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19120US12685 1286 PHL - DURING INSP FOUND FORWARD RIGHT SIDE DOOR SLIDE RELEASE COVER CABLE CONNECTION BAD. REPLACED FORWARD RIGHT SIDE DOOR SLIDE/RAFT ASSEMBLY. 2L72 4F RTA28NM 20050621000652005062100065NM 2005 6 21 USAA050576 120050430A575465026602 SKIN BOEING737 7374B7 1384702NM NR 6 SLAT DEBONDED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US39931 24781 CLT - NR 6 SLAT SKIN DISBOND 6 INCHES, INBOARD EDGE OF THE WEDGE. R & R DAMAGED SKIN AND CORE IAW TR 57-42-04 AND 51-30-03. (M) 2L72 4F RTA16WE 20050621000752005062100075NM 2005 6 21 USAA050648 120050512A5347 GALLEY TRACK BOEING757 757225 1384959NM RROYCERB211 RB211535E4 54555NE AFT GALLEY CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19608AU 22204 BFM - C4 - PLATE ASSY, 1 INCH X .5 INCH X .050 INCH, CORROSION; NO LEVEL OR TASK, CABIN FLOOR AFT GALLEY, LT MOUNT PAD AND SUPPORT PLATE ASSY. REMOVED AND REPLACED MOUNT PAD AND SUPPORT PLATE ASSY WITH FAB PART IAW SRM. (K) 2L72 4F4 FRTA2NM E12EU 20050621000912005062100091 2005 6 21 KBM2005F00101 420050512A34215040017901 GYRO SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE ATTITUDE INACCURATE A KBMAO OTHER O OTHER CRCRUISE 1 WP1937SH 2300 ATTITUDE GYRO INDICATES 5 DEGREES RT TURN DURING STRAIGHT AND LEVEL FLIGHT. AIRCRAFT MEL`D. (K) 1G71 3U3 UNCH9EU E19EU 20050621000992005062100099EU 2005 6 21 KBM2005F00102 120050606A255052801000 CARGO HOOK SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1D NE CARGO BAY FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1953SH 731 2009 CARGO HOOK WILL NOT HOLD LOAD. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050621001052005062100105 2005 6 21 KBM2005F00113 420050531A2310 SWITCH SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE TRANSCEIVER DEFECTIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH1 1395 2884 FM TRANSCEIVER, CHANNEL SELECTION SWITCH DEFECTIVE, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050621001242005062100124NM 2005 6 21 HNAA0500055 120050610A793345E041 VALVE DHAV DHC8 DHC8102 2809003NM NR 2 ENGINE STICKING A HNAAA UNSCHED LANDING M OVER TEMP CLCLIMB 1 EA07942HA4230542305 163 NR 2 ENGINE OIL TEMP WENT TO REDLINE, DECREASED POWER TO FLIGHT IDLE AND OIL TEMP DROPPED TO TOP OF GREEN ARC. REMOVED AND REPLACED NR 2 DIVERTER VALVE. 2H72 4T RTA13NM 20050621001312005062100131NM 2005 6 21 AWXA200500713 120050602A531069719478 DOUBLER BOEING737 73733A 1384673NM WINDOW FRAME CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 MCN - MAJOR REPAIR - DURING C-21 CHECK FOUND TOP 3 OUTBOARD SCREW HOLES ON FIRST OFFICERS NR 1 WINDOW FRAME TO HAVE EVIDENCE OF CRACKING INSIDE HOLES. MAINTENANCE REMOVED CRACKED DOUBLER IAW BOEING 737-300 SRM 53-10-01-2 FIG 210. INSTALLED REPLACEMENT DOUBLER IAW BOEING 737-300 SRM 51-40-02-0 FIG 4. 2L72 4F RTA16WE 20050621001322005062100132NM 2005 6 21 AWXA200500714 120050606A57536546434301 SKIN BOEING737 7373B7 1384580NM ZONE 500 DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28328AW 23377 MCN - MAJOR REPAIR - DURING C-13 CHECK FOUND DISBONDED AREA ON UPPER SURFACE OF THE LT INBOARD AFT FLAP 3.0 INCH FROM INBOARD END AT WBL 73 TO WBL 79. MAINTENANCE REMOVED DAMAGED AREA FROM UPPER SURFACE OF THE LT INBOARD AFT FLAP 3.0 INCH FROM INBOARD END AT WBL 73 TO WBL 79 AND CLEANED REPAIR AREA IAW BOEING 737-300 SRM 51-70-10-0 FIG 31. FABRICATED FILLER AND DOUBLER IAW BOEING 737-300 SRM 57-53-02 FIG 1. INSTALLED FABRICATED REPAIR PARTS IAW BOEING 737-300 SRM 51-70-10-0. 2L72 4F RTA16WE 20050621001332005062100133NM 2005 6 21 SWAA051764 120050616A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 935, STR 25L. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050621001392005062100139NM 2005 6 21 SWAA051770 120050616A53226558280 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 360, STR 13L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050621001402005062100140NM 2005 6 21 SWAA051771 120050616A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 500D, STR 10L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050621001422005062100142NM 2005 6 21 SWAA051773 120050616A534065C27314 STRINGER CLIP BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29508SW 24185 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050621001452005062100145NM 2005 6 21 SWAA051776 120050616A53116520723 FRAME BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 DURING SCHEDULED C3 CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME CRACKED AT NR 2 STOP FITTING CUTOUT. REPAIRED FRAME PER SWA EA. 2L72 4F RTA16WE 20050621001482005062100148NM 2005 6 21 DHL2005741556 120050418A5311 FRAME BOEING727 7272Q9 138448MNM FUSELAGE BENT A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 AFT CARGO STA 1030 AT STR 24 RIGHT BENT FRAME. FRAME OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 1. CUT OUT DAMAGE AREA DIMS 1.125 X 1.5 INCH AND FABRICATED REPAIR DOUBLER FROM MAT USED 7075-T6 .080 PO 90002012 AND DIMS 9.25 X 4 INCH IAW B727 SRM 51-40-3 FIG 1 & MAT ID 53-10-2 FIG 5. TREATED AND PRIMED PARTS IAW B727 SRM 51-10-2 AND INSTALLED REPAIR DOUBLER IAW B727 SRM 51-30-2. 2L73 4F RTA3WE 20050621001492005062100149NM 2005 6 21 HNAA0500057 120050607A61203014403 CONTROL UNIT DHAV DHC8 DHC8201 2809001NM NR 2 PROPELLER MALFUNCTIONED A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07969HA1454514545 468 AT 400 FEET NR 2 PROPELLER AUTO FEATHERED THE ENGINE TORQUE WAS AT 95 PERCENT. CREW ALSO REPORTED THE TORQUE WENT TO THE RED LINE AND REMAINED. REPLACED THE NR 2 TSCU. 2H72 4T RTA13NM 20050621001502005062100150EA 2005 6 21 COMA0560350 120050613A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ILLUMINATED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01819CA 7415 FLIGHT 5021 - RECEIVED A RIGHT THRUST REVERSER UNLOCK MESSAGE DURING TAKEOFF ROLL. ABORTED TAKEOFF AND RETURNED TO THE GATE. DEFERRED THE RIGHT THRUST REVERSER PER MEL 78-30-01. 2L72 4F RTA21EA 20050621001512005062100151NM 2005 6 21 2005UALA00518 120050606A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY EXIT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29128UA 30023 L3 MED AFT EMERGENCY EXIT LIGHT IS INOP. DOOR 3 EXIT LIGHT INOP (BURNED OUT), REPLACED LIGHT. OK 2L74 4F4 FRTA20WE E24NE 20050621001532005062100153 2005 6 21 2005UALA00500 420050604A3400 PROBE AIRBUS320 A320232 3930326EU TAT NR 1 FAILED A UALAA UNSCHED LANDING G MULTIPLE FAILURE CRCRUISE 1 WP29414UA 472 LOST BOTH FAC'S, WENT INTO ALTERNATE LAW. INDICATION DUE TO PROBE TAT 1 FAILURE, TAT 2 REPLACED PRECAUTIONARY. TAT 1 AND TAT 2 PROBES REPLACED. 2L72 4F RTA28NM 20050621001542005062100154NM 2005 6 21 2005UALA00501 120050604A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29592UA 28143 FUSELAGE SKIN DENTED STA 600-640, STR 27L TO 16L. TRIMMED OUT DAMAGE AND INSTALLED SKIN SPLICE REPAIR PER SRM53-30-12, AND EVA-50352 AND REO -G10623A. 2L72 4F4 FRTA2NM E17NE 20050621001552005062100155NM 2005 6 21 2005UALA00502 120050605A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29503UA 24624 AFT PIT LT SIDE AT STA 1460, FRAME HAS DENT ON INBOARD FLANGE BETWEEN STR 25L-26L. REPAIRED FRAME WITH FABRICATED PRODUCTION SPLICE ANGLE-DOUBLER PER TIMCO REO(EVA) G10547, REV. B. 2L72 4F4 FRTA2NM E17NE 20050621001562005062100156NM 2005 6 21 2005UALA00503 120050605A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP2903UA 24624 AFT PIT STA 1520 FRAME HAS DENT BETWEEN STR 25L AND 26L ON INBOARD FLANGE. REPAIRED FRAME WITH FABRICATED PRODUCTION SPLICE ANGLE DOUBLER PER TIMCO REO(EVA) G10549, REV B. 2L72 4F4 FRTA2NM E17NE 20050621001572005062100157NM 2005 6 21 2005UALA00504 120050605A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29503UA 24624 AFT PIT STA 1480 FRAME HAS DENT ABOVE STR 26L ON INBOARD FLANGE. REPAIRED FRAME WITH FABRICATED NESTED J-ANGLE PER TIMCO REO(EVA) G-10556, REV. C. 2L72 4F4 FRTA2NM E17NE 20050621001582005062100158EA 2005 6 21 COMA0560351 120050614A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ILLUMINATED A COMAO OTHER J WARNING INDICATION DEDESCENT 1 SO01526CA 7824 FLIGHT 4993 - DURING PWM APPROACH RECEIVED A RIGHT THRUST REVERSER UNLOCK MESSAGE. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. DEFERRED THE RIGHT THRUST REVERSER PER MEL 78-30-01. 2L72 4F RTA21EA 20050621001602005062100160EA 2005 6 21 COMA0570064 120050614A531267053110521 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA FUSLEAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01340CA7435 10062 FS 280 BULKHEAD LOWER WEBS ARE CORRODED BEYOND LIMITS FROM LBL 36 TO RBL 36. REPLACED THE FS 280 BULKHEAD LOWER WEBS IAW BOMBARDIER REO 670-53-11-052 REV A REPAIR 2. 2L72 4F RTA21EA 20050621001622005062100162EA 2005 6 21 COMA056343 120050609A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION LDLANDING 1 SO01938CA 7046 FLIGHT 5217- FLAPS FAIL CAUTION. INSPECTED FLAP SYSTEM PER AS 98-20-01, NO DEFECTS FOUND. RESET SYSTEM, CND. 2L72 4F RTA21EA 20050621001632005062100163EA 2005 6 21 COMA0560344 120050609A2730276003 PCU CNDAIRCL600 CL6002B19 1900309EA NR 3 FAILED A COMAO OTHER O OTHER NRNOT REPORTED 1 SO01814CA13764 7387 FLIGHT 5580 - ELEVATOR CONTROLS STIFF USING SYSTEM NR 3. NR 3 SYSTEM PCU FAILED. REPLACED THE LEFT ELEVATOR NR 3 PCU. 2L72 4F RTA21EA 20050621001652005062100165 2005 6 21 RAIA00506006 420050606A3418 DAU EMB 145 EMB145 3260210SO NR 2 INOPERATIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03809HK 145187 FLT 3535 - PIT - SPS NR 2 INOP AND DAU NR 2 WARNING MESSAGE DISPLAYED ON EICAS. MAINTENANCE REMOVED AND REPLACED THE NR 2 DAU AND OPS CHECKED GOOD. 2L72 4F RTT00011AT 20050621001662005062100166SO 2005 6 21 RAIA00506004 120050606A2720M83536 RELAY EMB 145 EMB145 3260210SO RUDDER CONTROL FAILED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03803HK 145077 FLT 3580 - RIC- RUDDER HARDOVER PROTECTION FAILURE MESSAGE ON THE EICAS. MAINTENANCE REMOVED AND REPLACED THE K0326 RELAY. OPS CHECKED GOOD. 2L72 4F RTT00011AT 20050621001672005062100167EA 2005 6 21 COMA0570066 120050614A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01340CA7435 10062 CORROSION ON INNER SIDE OF SKIN ON FWD SIDE BL 10R TO 10L AND AFT SIDE BL 0 TO 10R OF AVIONICS BAY CUTOUT. REMOVED CORROSION AT AVIONICS BAY DOOR CUTOUT IAW BOMBARDIER EO 601R-53-6614. 2L72 4F RTA21EA 20050621001682005062100168NM 2005 6 21 HNAA0500058 120050614A612078249050 CONTROL UNIT DHAV DHC8 DHC8102 2809003NM NR 1 ENGINE LEAKING A HNAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 EA07807EX337059718 292 NR 1 OIL PRESSURE GAGE FLUCTUATING TO JUST BELOW 55. NO OIL PRESSURE WARNING LIGHT. ACCOMPLISHED ABNORMAL CHECK LIST OIL PRESSURE STABILIZED AT 55. FOUND OIL LEAK BELOW NR 1 PCU. OIL LEVEL DOWN. REMOVED AND REPLACED NR 1 PCU. 2H72 4T RTA13NM 20050621001712005062100171EA 2005 6 21 COMA0560347 120050611A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ILLUMINATED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01518CA 7816 FLIGHT 5364 - DURING GSP APPROACH RECEIVED A LEFT THRUST REVERSER UNLOCK MESSAGE, CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. PERFORMED OPERATIONAL TEST OF THE LEFT THRUST REVERSER, NO DEFECTS NOTED, DISCREPANCY COULD NOT BE DUPLICATED. 2L72 4F RTA21EA 20050621001732005062100173EU 2005 6 21 USAAEM05008 120050619A3244 TIRE EMB ERJ170ERJ170100 EU MLG VIBRATION A USAAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 EA19823MD 17000044 DURING TAKEOFF, CREW FELT A VIBRATION IN THE AIRCRAFT. ONCE AIRBORNE, THE VIBRATION CEASED AND THE LANDING GEAR WAS RETRACTED. AT THAT TIME, A LANDING GEAR DISAGREE MESSAGE, ALONG WITH A GROUND SPOILER MESSAGE WAS GENERATED. THE LANDING GEAR MESSAGE WENT AWAY, BUT THE GROUND SPOILER MESSAGE DID NOT. FLIGHT RETURNED TO THE FIELD, AND UPON GEAR EXTENSION, DID NOT RECEIVE A GEAR DOWN AND LOCKED INDICATION. THE FLIGHT PERFORMED A FLY-BY OF THE TOWER, AND RECEIVED CONFIRMATION THAT THE GEAR WAS DOWN. SINCE THE GEAR COULD NOT BE VERIFIED -LOCKED- THE CREW INITIATED PROCEDURES FOR A PARTIAL GEAR UP LANDING. AFTER BURNING 45 MINUTES OF FUEL WHILE HOLDING, THE FLIGHT LANDED IN IAH. VIBRATION OCCURRED AGAIN DURIN2L74 4F RTA56NM 20050621001742005062100174EU 2005 6 21 200506012 120050601A3350 BATTERY PACK SAAB SF340 SF340A 7850100EU EMERGENCY LIGHT INOPERATIVE A UHLAO OTHER O OTHER NRNOT REPORTED 1 GL17148SD 340A148 EXIT SIGN OVER SEAT 1F INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK, OPS CHECK NORMAL. 2L72 4T RTA52EU 20050621001752005062100175EU 2005 6 21 SF20050606 120050606A3320 BATTERY PACK SAAB SF340 SF340A 7850100EU EMERGENCY LIGHT INOPERATIVE A UHLAO OTHER O OTHER CRCRUISE 1 GL17121CQ 121CQ EMERGENCY LIGHTS OVER MAIN CABIN DOOR INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK, OPS CHECKED GOOD. 2L72 4T RTA52EU 20050621001772005062100177NM 2005 6 21 2005UALA00506 120050603A33503004083 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE LT OVERWING INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29104UA 26902 TWO AFT, LT OVERWING EMERGENCY LIGHTS INOP. REPLACED PWR SUPPLY FIRST WITH NO HELP (PRECAUTIONARY), THEN REPLACED 2 EA LIGHT ASSY, LIKELY ONE OF WHICH WAS SHORTED. LIGHTS WORKED FINE AFTER REPLACEMENT. 2L74 4F4 FRTA20WE E24NE 20050621001782005062100178NM 2005 6 21 2005UALA00507 120050605A3350 BATTERY BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29174UA 24381 EMERGENCY EXIT LIGHTS ON IN BUSINESS CLASS RIGHT SIDE ROW 6-8 AND DOOR 2R. REPLACED EMERGENCY LIGHT BATTERY AT DOOR 2R, OPS CHECKED OK. 2L74 4F4 FRTA20WE E24NE 20050621001802005062100180NE 2005 6 21 2005UALA00509 220050606A7200 ENGINE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 1 FAILED A UALAA UNSCHED LANDING XMJENGINE FLAMEOUT OVER TEMP WARNING INDICATION CLCLIMB 1 WP29411UA 464 V10345 LOUD BANG ON CLIMBOUT FROM NR 1 ENGINE. OIL QUANTITY AND PRESSURE WENT TO ZERO, EGT RED LINED. ENGINE WAS REPLACED AND AIRCRAFT CONTINUED FUTHER FLYING WITHOUT INCIDENT. THE ENGINE FAILURE WAS CONFIRMED AS A HIGH PRESSURE COMPRESSOR 3RD STAGE BLADE (R3 BLADE) FAILURE. THIS IS AN INDUSTRY-WIDE AND KNOWN ISSUE, WITH BOTH A SHORT-TERM AND LONG-TERM FLEET MANAGEMENT PLAN: SHORT TERM IS BORESCOPE MONITORING OF FLEET FOR C3 MID-SPAN CONDITION. LONGER TERM IS UPGRADING OF C3 BLADE TO MORE ROBUST DESIGN.. 2L72 4F4 FRTA28NM E40NE 20050621001832005062100183NM 2005 6 21 2005UALA00512 120050531A5230 SKIN BOEING747 747422 1384935NM PWA 4056 PW4056 NE CARGO DOOR DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP2993UA 26890 DENT FOUND ON BULK CARGO DOOR OUTER SURFACE. DENT'S DIMENSION APPROX 0.5 X 0.2 INCH WITH LESS THAN 0.04 INCH IN DEPTH. DENT ON BULK CARGO DOOR EXTERNAL SURFACE. DAMAGE DUE TO IMPACT WITH GROUND EQUIPMENT. REPAIRED PER 747 SRM 52-00-01. 2L74 4F4 FRTA20WE E24NE 20050621001842005062100184NM 2005 6 21 2005UALA00513 120050530A5330 SKIN BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29193UA 26890 SMALL SCRAPE ON FUSELAGE BETWEEN DOOR 5 LEFT AND STATIC PORT. SMALL SCRAPE AND DENT ON FUSELASE MEASURES-MINOR AXIS 5.0", DEPTH 0.15" A OVER Y EQUALS 50.0 - ACCOMPLISHED SKIN CUTOUT AND FABBED DOUBLER PER SRM 53-00-01 FIG.201. AREA AFFECTED IS STA 2350 APPROX 4 FT AFT OF DR 5L. TOP COAT NOT DAM AGED. NO DAMAGE OVER STATIC PORT AREA. INSTALLED INSULATION BLANKET AT STA. 2320-2340 STRGR 21L-22L AS WELL AS CIC APPLY. 2L74 4F4 FRTA20WE E24NE 20050621001852005062100185NM 2005 6 21 2005UALA00514 120050606A2612 FIRE LOOP BOEING737 737322 1384676NM NR 1 ENGINE DAMAGED A UALAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29330UA 24191 FLIGHT DIVERTED TO DTW WITH A NR 1 ENGINE FIRE WARNING INDICATION. CREW REPORTED AT ROTATION OVERHEAT DETECTION LIGHT AND MASTER CAUTION LIGHT ILLUMINATED. CREW SHUTDOWN NR 1 ENGINE AFTER OVERHEAT LIGHT ILLUMINATED AGAIN AND DIVERTED THE AIRCRAFT TO DTW. FOUND WIRE W1508-006-16R (LOOP B) SHORTED AND BROKEN THRU AT CLAMP LOCATED AT 12 O'CLOCK POSITION ABOVE CORE ENGINE. ALSO FOUND WIRE W1506-044-16R (LOOP A) CHAFED THRU AT 10 O'CLOCK FAN POSITION. BOTH CORE LOOP A AND B FAILED MEGGER TEST. REPAIRED WIRE HARNESS, REPLACED BOTH A AND B CORE LOOP M1122. ACCOMPLISHED HIGH POWER RUN. BOTH A & B LOOP FIRE DETECTION SYS CHECKED NORMAL. 2L72 4F RTA16WE 20050621001862005062100186NM 2005 6 21 2005UALA00515 120050606A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29128UA 30023 UPPER DECK CEILING EEL LIGHTS ARE OUT BETWEEN 14AB & 14GH AND 16AB & 16GH. EMER EXIT LIGHTS OUT UPPER DECK DUE TO BATTERY NOT HOLDING CHARGE. REPLACED EMERGENCY LIGHT BATTERY. OK 2L74 4F4 FRTA20WE E24NE 20050621001872005062100187NM 2005 6 21 2005UALA00517 120050606A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29128UA 30023 B-CLASS SEAT 21 THRU 26 (RT) EEL LIGHTS ARE INOP. UPDATE B-ZONE SEAT 21 THRU 26 (RH) EEL LIGHTS ARE INOP DUE TO BATTERY NOT HOLDING CHARGE. REPLACED EEL BATTERY. OK 2L74 4F4 FRTA20WE E24NE 20050621001892005062100189NM 2005 6 21 2005UALA00520 120050607A335078941 LAMP BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29796UA 26931 EEL INOP AT SEAT 3F. LIGHT ASSEMBLY WAS REPLACED. 2L72 4F4 FRTT0001SE E46NE 20050621001912005062100191NM 2005 6 21 2005UALA00523 120050608A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29503UA 24624 FLOORBEAM CORRODED AT STA 367, RBL 56 UPPER SURFACE. REPLACED SUPPORT 141N5161- 52 PER SRM 51-40-02. 2L72 4F4 FRTA2NM E17NE 20050621001922005062100192NM 2005 6 21 2005UALA00524 120050608A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29503UA 24624 RIGHT SIDE BS 1640 FLOORBEAM, RBL 0 - RBL 60, TOP CAP IS CORRODED. DAMAGE DUE TO CORROSION IN TYPICAL WET AREA. REMOVED CORRODED REPAIR STRAP AND INSTALLED NEW REPAIR STRAP. 2L72 4F4 FRTA2NM E17NE 20050621001952005062100195NM 2005 6 21 2005UALA00527 120050608A5340 ATTACH ANGLE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSLEAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29503UA 24624 FWD NOSE AREA STA 202 BULKHEAD, RT SIDE HAS ATTACH ANGLE CRACKED OUTBOARD OF FRAME ON LOWER REAR SIDE OF BULKHEAD, RBL 30-36. REPLACED BULKHEAD ATTACH ANGLE PER BAC DWG 141N5811-U2 AND INSTALLED PER SRM 51-40-2. 2L72 4F4 FRTA2NM E17NE 20050621001992005062100199NM 2005 6 21 2005UALA00531 120050607A3350 LIGHT BOEING737 737322 1384676NM CABIN INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29334UA 24229 FLOOR MOUNTED EEL LIGHTS INOP FROM ROW 14 TO AFT GALLEY. POWER STRIP IN FLOOR TRACK WAS REPLACED.OK 2L72 4F RTA16WE 20050621002022005062100202NM 2005 6 21 2005UALA00534 120050514A5311 FRAME BOEING737 737322 1384676NM FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29312UA 23673 STA 188 STR 17L FRAME CRACKED. FABRICATED AND INSTALLED REPAIR ANGLE PER MM 53-11-83. 2L72 4F RTA16WE 20050621002032005062100203NM 2005 6 21 2005UALA00535 120050514A5311 FRAME BOEING737 737322 1384676NM FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29312UA 23673 STA 188 STR 17R FRAME CRACKED. REMOVED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE PER MM 53-11-83. 2L72 4F RTA16WE 20050621002042005062100204NE 2005 6 21 2005UALA00536 220050607A7200 ENGINE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 1 STALLED A UALAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 WP29405UA 452 V10311 NR 1 ENGINE EXPERIENCED TWO COMPRESSOR STALLS, ONE IN CRUISE AND ONE AT TOP OF DESCENT. ENGINE WAS CHANGED AND AIRCRAFT CONTINUED FLYING AFTERWARDS WITHOUT FURTHER INCIDENT. COMPRESSOR STALL WAS CAUSED BY HIGH-PRESSURE COMPRESSOR (HPC) BLADE DAMAGE PRIMARILY IN THE 6TH STAGE (R6), WHICH WAS CAUSED BY F.O.D. INGESTION. 2L72 4F4 FRTA28NM E40NE 20050708000932005070800093NM 2005 7 8 ASAA0540289 120050613A575465C26602311 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU NR 2 SLAT DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 NR 2 SLAT IB T/E DELAMINATED AT CORNER. REMOVED DAMAGE, FABRICATED SKIN AND DOUBLER AND INSTALLED REPAIR PIECES IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050621002062005062100206NM 2005 6 21 AWXA200500681 120050610A2780655280739 MODULE BOEING737 7373G7 1384595NM FLAP/SLATS MALFUNCTIONED A AWXAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 WP28155AW 23777 ON CLIMBOUT FROM MKE EN ROUTE TO PHX THE NR 3 SLAT WOULD NOT RETRACT. AIRCRAFT RETURNED TO MKE WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT IAW BOEING 737-300 MM 27-88-00, REMOVED AND REPLACED M229, FLAP/SLAT POSITION MODULE P/N;65-52807-76 SN; D00880. ALSO REMOVED AND REPLACED L00351, LEADING EDGE FLAP TRANSIT LIGHT. TEAR DOWN REPORT OF THE LEADING EDGE FLAP/SLAT MODULE, SN D00880, CONFIRMS FAULT. THE UNIT FAILED THE ANNUNCIATOR TEST AND UPON TEARDOWN FOUND COLD SOLDER JOINT IN THE A22 BOARD. RE-SOLDERED BOARD AND RE-TESTED IAW BOEING OHM 27-56-40 REV 39. 2L72 4F RTA16WE 20050621002072005062100207NM 2005 6 21 AWXA200500685 120050530A532069434961 INTERCOSTAL BOEING737 73733A 1384673NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 DURING C-21 CHECK FOUND CORROSION AROUND SCREW HOLE AND UNDER 2 NUT PLATES AT AFT CARGO COMPARTMENT INTERCOSTAL PANEL BS 858, WL 150, RBL 23. MAINTENANCE BLENDED OUT CORROSION AND DETERMINED CORROSION TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-15. FABRICATED NEW INTERCOSTAL PANEL IAW BOEING 737-300 SRM 51-40-02. INSTALLED FABRICATED REPAIR PARTS IAW BOEING 737-300 SRM 53-60-15-1 FIGURE 101. 2L72 4F RTA16WE 20050621002082005062100208NM 2005 6 21 AWXA200500686 120050531A531265163007 BULKHEAD BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 MCN - MAJOR REPAIR - DURING C-21 CHECK FOUND A CRACK .375 INCH AT 178 BULKHEAD WEB, WL 207, RBL 10. MAINTENANCE REMOVED DAMAGED AREA FROM 178 BULKHEAD WEB, WL 207, RBL 10 IAW BOEING 737-300 SRM 53-10-08 FIG 209. FABRICATED DOULBER AND INSTALLED REPAIR PARTS AT 178 BULKHEAD WEB, WL 207, RBL 10 IAW BOEING 737-300 SRM 53-10-08 FIG 209. 2L72 4F RTA16WE 20050621002092005062100209NM 2005 6 21 AWXA200500687 120050531A532065458076 ANGLE BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 MCN - MAJOR REPAIR - DURING C-21 CHECK FOUND CRACK .5 INCH IN LENGTH AT R1 DOOR CUTOUT ANGLE ON BS 294.5 AND BS 294.6, BETWEEN STRINGER 7R AND STRINGER 8R. MAINTENANCE REMOVED DAMAGED AREA IAW BOEING 737-300 SRM 51-70-11 AND FABRICATED NEW ANGLE IAW BOEING 737-300 SRM 51-70-11. INSTALLED FABRICATED REPAIR PARTS IAW BOEING 737-300 SRM 51-70-11. 2L72 4F RTA16WE 20050621002102005062100210NM 2005 6 21 AWXA200500688 120050601A53106546812188 SUPPORT BEAM BOEING737 73733A 1384673NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 MCN - MAJOR REPAIR - DURING C-21 CHECK FOUND CORROSION ON DIAGONAL SUPPORT BEAM BOTTOM SIDE AROUND FASTENER HOLES FROM BS 1006 TO BS 1016, RBL 6. MAINTENANCE BLENDED OUT CORROSION AT BS 1006 TO BS 1016, RBL 6 AND FOUND REMAINING MATERIAL TO BE OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORT BEAM AT BS 1006 TO BS 1016, RBL 6 IAW BOEING 737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050621002112005062100211NM 2005 6 21 AWXA200500689 120050601A53119638203 FRAME BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 MCN - MAJOR REPAIR - DURING C-21 CHECK FOUND CRACK .211 INCHES LONG AT 178 BULKHEAD FRAME WEB, RBL 17, WL 182. MAINTENANCE REMOVED DAMAGED AREA AT BULKHEAD FRAME WEB 178, RBL 17, WL 182 AND FABRICATED NEW WEB IAW BOEING 737-300 SRM 53-10-08-2 FIGURE 212. INSTALLED FABRICATED REPAIR PARTS IAW BOEING 737-300 SRM 53-10-08-2 FIG 212. 2L72 4F RTA16WE 20050621002122005062100212NM 2005 6 21 05FDEA01596 120050613A53216519575 FLOOR PANEL BOEING727 727200 138407ENM COCKPIT CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25203FE 22925 COCKPIT F/O OUTBOARD RUDDER PEDAL FLOOR PANEL CRACKED. REMOVED AND REPLACED PANEL IAW SRM 51-30-2. 2L73 4F RTA3WE 20050621002142005062100214NM 2005 6 21 ASMF200506015 120050615A27826010N000104 ACTUATOR DOUG MD80 MD83 3023681NM SLATS FAILED W ASMFO OTHER J WARNING INDICATION CRCRUISE 1 SW23861LF5369838685 49826 CAPTAIN REPORTED THAT DURING FLIGHT LIGHT AUTO SLAT FAIL CAME ON. DURING CHECK, APPLICABLE CIRCUIT BREAKERS WERE RESET AND FLAPS/SLATS WERE OPERATIONALLY TESTED TURNING ON THE OVERHEAD LIGHT IN THE SLATS PANEL LIGHTS. BITE TO BOTH STALL COMPUTERS WERE PERFORMED SHOWING AUTO SLATS FAIL RED LIGHTS. TECHNICAL PERSONNEL WAS SENT FROM MEX AND SLATS ACTUATORS WERE REPLACED IAW MM 27-80-08, TESTED CORRECT. DURING OVERNIGHT SERVICE, TESTS TO AUTO-SLAT SYSTEM, PERFORMED IAW MM 27-80-08, ALL CORRECT. 2L72 4F RT 20050621002152005062100215NM 2005 6 21 05FDEA01599 120050613A54106519686387 FRAME BOEING727 727200 138407ENM NR 1 ENG COWL CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25262FE 21624 NR 1 ENG FIXED COWL AFT LWR END SKIN AND FRAME IS CRACKED. TRIMMED DAMAGE SKIN IAW SRM 54-30-1 FIG 1 DETAIL 6. REMOVED AND REPLACED FRAME IAW SRM 51-10-1 AND SRM 51-30-2. 2L73 4F RTA3WE 20050621002162005062100216 2005 6 21 05FDEA01601 420050613A34535221837000 ANTENNA BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25262FE 21624 AFT LOWER FUSE ADF LOOP ANT BASE CORRODED. REMOVED AND REPLACED ADF ANTENNA IAW MM 34-37-012-4, OPS CHECKS GOOD. 2L73 4F RTA3WE 20050621002172005062100217NM 2005 6 21 05FDEA01606 120050614A57306521655 SKIN BOEING727 727200 138407ENM RT WING DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25262FE 21624 RIGHT WING UPPER SURFACE PANEL AT APU EXHAUST HAS DELAMINATION, CORROSION AND OLD REPAIR TORN OFF JUST AFT OF EXHAUST PORT. FABRICATED NEW PANEL AND INSTALLED NEW PANEL IAW SRM 51-30-5 & 51-30-2. 2L73 4F RTA3WE 20050621002192005062100219 2005 6 21 05FDEA01602 420050613A34535221837000 ANTENNA BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25262FE 21624 FWD LOWER FUSE ADF ANT BASE CORRODED. REMOVED AND REPLACED ADF ANTENNA IAW MM 34-37-012-4, OPS CHECKS GOOD. 2L73 4F RTA3WE 20050621002202005062100220NM 2005 6 21 05FDEA01604 120050614A533053FX130111 DOUBLER BOEING727 727200 138407ENM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25262FE 21624 COMPLY WITH EA 7-5330-87786, FUSELAGE -PLATING -GOUGE IN MAIN CARGO DOOR CUTOUT REINFORCEMENT DOUBLER AND TRIPLER. COMPLIED WITH EA 7-5330-87786 - FUSELAGE PLATING GOUGED IN MAIN CARGO DOOR CUTOUT REINFORCEMENT DOUBLER & TRIPLER (MINOR REPAIR). 2L73 4F RTA3WE 20050621002212005062100221NE 2005 6 21 EGRR101110 120050531A3097 WIRE SKRSKYS76 S76C 8143008NE ANTI-ICE SYSTEM BURNED B EGRRK NONE O OTHER ININSP/MAINT 1 EA1722CP 760530 ANTI-ICE SYSTEM FAILED 12 MOS TEST - NR 1 HEATER INOPERATIVE DURING TROUBLESHOOTING FOUND BROKEN WIRE AT CONNECTOR J703 PIN A (BLACKENED AS IF BURNED). STRIPPED WIRE TO INSTALL NEW CONNECTOR PIN AND WIRE STRANDS APPEARED COPPER IN COLOR. STRIPPED WIRE BACK TO FIND CLEAN LOOKING SECTION FOUND DISCOLORED ALL THE WAY TO SPLICE. NOTIFIED MFG AIRCRAFT. 1G72 3U NCH1NE 20050621002222005062100222WP 2005 6 21 ASMF200505030 120050530A27605910055526 SKIN DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE RT SPOILER CRACKED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23501AM4278 49188 CAPTAIN REPORTED THAT HE PERFORMED THE FINAL APPROACH AND LANDING WITH 3450 POUNDS OUT OF BALANCE BETWEEN TANKS. OUT OF BALANCE INSPECTION WAS PERFORMED IAW MM, DETECTING A CRACK IN THE RT WING IB FLIGHT SPOILER OF 9 INCHES LONG. SPOILER WAS REPLACED IAW MM 27-61-01 AND 27-61-02, TESTED CORRECT. 2L72 4F4 F A6WE E9NE 20050622000012005062200001CE 2005 6 22 DXTA200500794 120050620A3230327 BULB BEECH MU300 400A 1155402CE MLG INDICATOR BURNED OUT E DXTAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL07117QS304 RK391 LEFT GEAR GREEN DOWN LOCK INDICATOR INOPERATIVE (LIGHT BULB INOPERATIVE). REMOVED AND REPLACED ALL DOWN AND LOCKED INDICATOR BULBS, OPS CHECK GOOD. 2H72 4F RTA16SW 20050622000052005062200005NM 2005 6 22 SWAA051783 120050619A53226546569 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 967, STR 7L. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050622000062005062200006NM 2005 6 22 SWAA051784 120050619A55516551524 FITTING BOEING737 7373H4 1384600NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND LT & RT HORIZONTAL STAB ATTACH FITTING LUG FACES CORRODED. REPAIRED LUG FACES PER SRM. 2L72 4F RTA16WE 20050622000072005062200007NM 2005 6 22 SWAA051785 120050619A55536547450 FITTING BOEING737 7373H4 1384600NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND LT & RT VERTICAL STAB ATTACH FITTING FWD & AFT PRIMARY CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER SRM & BFG ER. 2L72 4F RTA16WE 20050622000082005062200008NM 2005 6 22 SWAA051786 120050619A53116546548 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050622000092005062200009NM 2005 6 22 SWAA051787 120050619A53116545853 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 947, STR 18L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050622000102005062200010NM 2005 6 22 SWAA051788 120050619A5754 WEDGE BOEING737 7373H4 1384600NM RT WING SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND RT WING NR 5 L/E SLAT T/E WEDGE CRACKED. REMOVED AND REPLACED SLAT ASSY PER MM. 2L72 4F RTA16WE 20050620000132005062000013WP 2005 6 20 AALA20050380 120050608A3260 SENSOR DOUG DC9 DC982 3022082WP NLG DIRTY A AALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW2133502 49739 SLC - LANDING GEAR WOULD NOT RETRACT. RETURNED SLC AND LANDED WITHOUT INCIDENT. CHECKED NOSE GEAR PER MM 32-52-07-2 AND CLEANED SENSORS AND COMPLETED SWING TEST. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050620000142005062000014EU 2005 6 20 AALA20050381 120050607A3350P4010049 BATTERY PACK AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2159081 639 ACCESS LIGHTS INOPERATIVE FROM ROW 29 BACK ON LEFT SIDE OF AIRCRAFT. REPLACED BATTERY PACK FOR ACCESS LIGHTS FROM ROW 29 BACK ON LEFT SIDE OF AIRCRAFT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20050620000162005062000016EU 2005 6 20 MALA050463 120050602A2910 SWITCH BAC 146 AVRO146RJ85A1500097EU HYDRAULIC SYSTEMLEAKING A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15512XJ E2326 THE CREW REPORTED THAT THE GREEN HYD FLUID GOING TO EMPTY. LOST GREEN HYDS. CREW FOLLOWED QRH AND LANDED IN DTW. MAINTENANCE FOUND HYD BAY FULL OF FLUID. FOUND GREEN SYSTEM PRESSURE SWITCH LEAKING INTERNALLY. REPLACED PRESSURE SWITCH P/N HE15258-1, S/N ON 3948TW. ALL CHECKS GOOD. SERVICED GREEN SYS HYD AS REQUIRED. ALL IAW ARJ85 AMM. 2H74 4F RTA49EU 20050620000172005062000017EU 2005 6 20 MALA050458 120050531A5315 FLOORBEAM BAC 146 AVRO146RJ85A1500097EU FUSELAGE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15506XJ E2314 DURING C1 & C2 CHECKS IN YYC FOUND FRAME 20 FLOORBEAM CRACKED AND CORRODED THROUGH THE TOP FLANGE AT RBL 22. 2H74 4F RTA49EU 20050620000222005062000022 2005 6 20 AWXA200500680 420050607A2565D31517317 SLIDE AIRBUSA319 A319132 3930340NM L2 DOOR MALFUNCTIONED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28807AW 1064 DURING 4 DAY CHECK DISCOVERED L2 DOOR EMERGENCY EXIT SLIDE PRESSURE BELOW LIMITS. MAINTENANCE REMOVED AND REPLACED L2 DOOR EMERGENCY EXIT SLID IAW TC R1C25305. 2L72 4F RTA28NM 20050620000292005062000029SO 2005 6 20 MASA200500265 120050401A3320 ELEC CONNECTOR EMB 145 EMB145LR 3260212SO LIGHT ASSY BURNED A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW07833MJ 145327 ASH 2780 TYS TO CLT. DURING FLIGHT CREW REPORTED SMOKE IN CABIN AT ROW 15. MX IN CLT FOUND BURNED ELECTRICAL CONNECTOR ON SIDEWALL LIGHT 14A. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSY. 2L72 4T RTT00011AT 20050620000442005062000044NM 2005 6 20 CALA0500196 120050611A3260 SWITCH BOEING757 757324 1384930NM MLG INOPERATIVE A CALAO OTHER N FALSE WARNING LDLANDING 1 SW2774856 32815 THE GEAR DISAGREE LIGHT AND GEAR DOOR MESSAGE LIGHT ILLUMINATED ALONG WITH A GEAR AND DOOR AMBER LIGHT AFTER GEAR RETRACTION. THE GEAR LIGHT AND GEAR DOOR LIGHT EXTINGUISHED DURING CLIMBOUT. ALL THREE GEAR DOORS WERE OPEN ON LANDING IN EWR. MAINTENANCE WAS UNABLE TO DUPLICATE THE FAILURE DURING SEVERAL GEAR SWINGS. THE K10370 LATCH RELAY AND S10260 ALTERNATE GEAR EXTENSION SWITCH WERE REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE IAW MM 20-00-00. NORMAL AND ALTERNATE GEAR SWINGS WERE PERFORMED AND NO FAULTS WERE NOTED. 2L72 4F RTA2NM 20050620000452005062000045EU 2005 6 20 019105 120050114A2612 WARNING LIGHT SAAB SF340 340B 7860101EU LT TAIL PIPE ILLUMINATED A NSVAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27237MJ 340B237 LEFT TAIL PIPE HOT LIGHT ILLUMINATED AFTER TAKEOFF. 2L72 4T RTA52EU 20050620000522005062000052EU 2005 6 20 06022005 120050602A7712 INDICATOR SAAB SF340 340B 7860101EU LT ENGINE TORQUEILLUMINATED A NSVAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA27341CJ 341 NO TORQUE INDICATION ON LEFT ENGINE DURING TAKEOFF ROLL. 2L72 4T RTA52EU 20050620000672005062000067CE 2005 6 20 DXTA200500759 120050531A3220 LANDING GEAR CESSNA500 560CESSNA 2076750CE NOSE MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07837QS 5600685 NOSE GEAR WILL NOT RETRACT. PERFORMED LANDING GEAR HYDRO SYSTEMS ADJUSTMENT TEST IAW 560 MM 32-01-00. OPS CHECK GOOD. INSPECTED NOSE GEAR, NO DEFECTS FOUND. 2L72 4F RTA22CE 20050620000702005062000070CE 2005 6 20 DXTA200500771 120050612A2432 BATTERY CESSNA750 750 2076810CE MASTER OVERHEATED E DXTAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL07923QS 7500023 DURING PRESTART PROCEDURE OF APU WITH BATTERIES AND EICAS ON MULTIPLE EICAS MESSAGES STARTED APPEARING (PRI-STAB, SECONDARY STAB FAIL, DAU, FADEC FAILS) ANY MESSAGE ASSOCIATED WITH ELECTRICAL, RED CHECK RED ON TOP. A STRONG BURNING SMELL WAS ALSO NOTICED, BATTERIES WHERE DISCONNECTED. ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20050620000752005062000075SO 2005 6 20 C2XA05RI011 120050612A33502013BR BATTERY EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT DEFECTIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716183193 14500914 RIC - DURING ROUTINE INSPECTION, ROW 12 CEILING EMERGENCY LIGHT AND OVERWING EMERGENCY LIGHT DIM/WADE OUT. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY. OPERATIONAL TEST WAS PERFORMED SUCCESFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RT 20050620000812005062000081SO 2005 6 20 C2XA05BT038 120050614A335020131A BATTERY EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT FAULTY A C2XAO OTHER O OTHER NRNOT REPORTED 1 SW2713935109891155 145022 CREW REPORTED, CABIN AFT EMERGENCY LIGHTS NOT WORKING. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY LIGHT BATTERY IAW EMB145ER AMM 33-50-04, OPS CHECKED GOOD. 2L72 4F RTT00011AT 20050620000832005062000083SO 2005 6 20 C2XA05SH049 120050611A532014530644405 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714942 145037 SHV - DURING C-CHECK LT OMEGA BEAM HAS AREAS OF CORROSION BETWEEN FRAMES 45 & 53. MAINTENANCE REPAIRED LT OMEGA BEAM AT FRAME 49 PER EC 5320-01247, NO FURTHER ACTION REQUIRED. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050620000872005062000087 2005 6 20 SWAA051701 420050609A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29351SW 24572 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050620001012005062000101 2005 6 20 SWAA051711 420050610A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29383SW 26589 DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050620001022005062000102 2005 6 20 SWAA051712 420050610A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29383SW 26589 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050620001062005062000106NM 2005 6 20 SWAA051716 120050612A53116546569 BELTFRAME BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29508SW 24185 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE BELTFRAME CRACKED AT BS 1006, STR 17R. REPAIRED BELTFRAME PER SRM. 2L72 4F RTA16WE 20050620001082005062000108NM 2005 6 20 SWAA051718 120050612A53206545410 FLOOR SUPPORT BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29508SW 24185 DURING SCHEDULED 1/2D CHECK, FOUND 4 EA NR 2 LONGITUDINAL FLOORBEAM CRACKS BETWEEN BS 658 TO BS 673.5, LBL 24.75. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20050620001162005062000116WP 2005 6 20 05FDEA01594 120050613A5744NRC6068510 SUPPORT FITTING DOUG MD10 MD1010F 3022112WP ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25391FE 46625 COMPLY WITH EA 8-5750-55487, WINGS - FLAP VANE SUPPORT CORROSION REWORK (RIGHT OUTBOARD FLAP). COMPLIED WITH EA 8-5750-55487. 2L73 4F RTA22WE 20050620001212005062000121NM 2005 6 20 SWAA051728 120050613A53306545768 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29508SW 24185 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR CUTOUT, AFT LOWER CORNER. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050620001302005062000130NM 2005 6 20 AWXA200500702 120050529A5753 SKIN BOEING737 73733A 1384673NM ZONE 500 DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 MCN - MAJOR REPAIR - DURING C-21 CHECK FOUND DISBONDED AREA ON LOWER SURFACE OF LT OUTBOARD FORE FLAP 18 INCHES FROM INBOARD END FROM WBL 206.5 TO WBL 225.2. MAINTENANCE CUT OUT DISBONDED AREA ON LOWER SURFACE OF LT OUTBOARD FORE FLAP. FABRICATED REPLACEMENT LOWER SKIN, DOUBLERS AND FILLERS IAW AMERICA WEST AIRLINES ENGINEERING REPAIR 03-5754-05161-ES2. INSTALLED FABRICATED REPAIR PARTS IAW REPAIRED IAW AWA ER NR 03-5754-05161-ES2. A MONITOR WAS ISSUED TO RE-INSPECT THE REPAIR AREA EVER 3500 FLIGHTS OR 24 MONTHS, MONITOR NR 250672. 2L72 4F RTA16WE 20050620001522005062000152NM 2005 6 20 DHL2005741569 120050421A5312 BULKHEAD BOEING727 7272Q9 138448MNM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 VERTICAL STAB BS 1303 RT BULKHEAD WEB CRACK AT STR CUTOUTS 2 PL- MARKED STR 8. COMPLIED WITH COTNEY AEROSPACE EA:EAZ04-2 REV:IR WITH 8710-3 DATED JUNE 8, 2005. STOP DRILLED 2EA CRACKS ON BS 1303 WEB RBL 22 IAW S/B 727-53-0094. 2L73 4F RTA3WE 20050621000022005062100002NM 2005 6 21 ASMF200506016 120050613A783041000740104 CONTROL VALVE DOUG MD88 MD88 3023688NM THRUST REVERSER FAILED W ASMFO OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 SW23158PL11329 49761 CAPTAIN REPORTED THAT DURING LANDING HYDRAULIC LIQUID QUANTITY OF LT SYSTEM DROPPED TO ZERO AND DENSE SMOKE AT PASSENGER CABIN. DURING REVERSE SYSTEM AND TAIL CONE CHECK, IT WAS DETECTED THAT THE LT HYDRAULIC CONTROL VALVE LEAKED DUE TO ITS TEST PORT CAP WAS BROKEN. THE LT HYDRAULIC CONTROL VALVE WAS REPLACED AND REVERSES OPERATION TESTS WERE PERFORMED IAW MM 78-31-04, ALL CORRECT. DUE TO APU INGESTED HYDRAULIC LIQUID IT DID NOT START. APU WAS DEFERRED IAW MEL 49-10. DURING OVERNIGHT SERVICE, THE APU WAS REPLACED IAW MM 49-10-00 AND A/C WATER SEPARATORS AT BOTH A/C PACKS WERE REPLACED TOO IAW MM 21-20-02, TESTED CORRECT. DEFERRED REPORT WAS CLOSED. 2L72 4F RTA6WE 20050621000152005062100015NM 2005 6 21 SWAA051749 120050615A53126546568 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND BS 1016 PRESSURE BULKHEAD WEB CRACKED AT STR 15R. REPAIRED BS 1016 BULKHEAD WEB PER BFG ER. 2L72 4F RTA16WE 20050621000222005062100022NM 2005 6 21 SWAA051757 120050615A53116558280 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050621000252005062100025NM 2005 6 21 SWAA051760 120050615A2560PH22300L GLOWSTRIP BOEING737 7373H4 1384600NM CABIN FLOOR DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 DURING SCHEDULED SERVICE CHECK, FOUND PHOTOLUMINESCENT STRIP DELAMINATED AT FWD END OF CABIN. REMOVED AND REPLACED STRIP PER MM. 2L72 4F RTA16WE 20050621000562005062100056NM 2005 6 21 USAA050571 120050330A575465C26601197 STRUCTURE BOEING737 7374B7 1384702NM NR 1 SLAT DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US39931 24781 CLT - FOUND NR 1 SLAT, NR 1 SLAT LOWER NOSE SURFACE T/E AT AFT ROW OF FASTENERS. REPAIR PCW IAW SRM 57-43-01. (M) 2L72 4F RTA16WE 20050621000622005062100062 2005 6 21 SA05059 420050601A2565 LANYARD AIRBUS320 A320214 3930316EU ESCAPE SLIDE MISSING A USAAK NONE O OTHER ININSP/MAINT 1 EA19118US 1264 DCA - AFT RIGHT DOOR SLIDE/RAFT ASSEMBLY SURVIVAL LANYARD AND RELEASE SNAP FOUND MISSING. REPLACED AFT RIGHT DOOR SLIDE/RAFT ASSEMBLY. OK FOR SERVICE. 2L72 4F RTA28NM 20050621000692005062100069 2005 6 21 KBM2005F00096 420050505A2330DMP100 ENTERTAIN SYS SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE COMMUNICATIONS FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19250SH 3874 DIGITAL MEDIA PLAYER SHOWS FAILURE, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050621000762005062100076EU 2005 6 21 KBM2005F00097 120050529A7332642792002 TRANSMITTER SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE FUEL PRESS SYS INOPERATIVE E KBMAO OTHER P NO WARNING INDICATION NRNOT REPORTED 1 WP19250SH113 3874 FUEL PRESSURE TRANSMITTER, NO GAUGE INDICATION, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050621000822005062100082EU 2005 6 21 KBM2005F00098 120050529A6510350A33215300 BEARING SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE TAIL ROTOR TORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH476 2337 TAIL ROTOR LAMINATE BEARING, TORN, REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20050621000832005062100083EU 2005 6 21 KBM2005F00100 120050517A771456337078012 INDICATOR SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE NG FLUCTUATES E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH459 2337 NG GAUGE, FLUCTUATES IN FLIGHT, REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20050621001032005062100103EU 2005 6 21 KBM2005F00109 120050524A7931704A47270102 INDICATOR SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE ENG OIL PRESSUREFAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19351WM 2167 CLUSTER GAUGE, NO OIL PRESSURE INDICATION, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050621001062005062100106EU 2005 6 21 KBM2005F00112 120050526A2130090004 PRESSURE SWITCH SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE AIR CONDITIONINGDEFECTIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH 2884 AIR CONDITIONING, HI PSI SWITCH DEFECTIVE, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050621001262005062100126NM 2005 6 21 AWXA200500697 120050613A26126937307145 CONTROL MODULE BOEING737 7373G7 1384595NM FIRE CONTROL INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28154AW188493303 23776 DEN - EES - DURING 8 DAY RIGHT SQUIB, ON FIRE CONTROL PANEL, WOULD NOT TEST IN EITHER POSITION 1 OR 2. MAINTENANCE REMOVED AND REPLACED ENGINE AND FIRE CONTROL MODULE, P/N 69-37307-145, S/N D01215, IAW BOEING 737-300 MM 26-21-51. OPERATIONAL TESTS GOOD. UNIT WAS FOUND TO HAVE WORN LAMPS AND INDICATORS L1, L3 AND L11 DAMAGED BY EXTERNAL CONTAMINATION. UNIT WAS REPAIRED AND TESTED IAW BOEING OHM 26-10-48 REV 38. NOT AN SDR REPORTABLE EVENT. 2L72 4F RTA16WE 20050621001282005062100128NM 2005 6 21 AWXA200500699 120050613A531265C376077 STIFFENER BOEING737 73733A 1384673NM BULKHEAD CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 MCN - MAJOR REPAIR - DURING C-21 CHECK DISCOVERED 2 CRACKS .113 INCHES IN LENGTH ON ANGLE LOCATED AT BULKHEAD STA 178 LBL 5.7 WL 184. MAINTENANCE CUT OUT AND REMOVED DAMAGED AREA FROM BULKHEAD LOCATED AT STA 178. FABRICATED REPAIR ANGLES, STRAPS, FILLERS IAW BOEING 737-300 SRM 53-10-08-2 FIG 205 AND INSTALLED REPAIR PARTS AT BULKHEAD STA 178 IAW BOEING 737-300 SRM 53-10-08-2 FIG 205. 2L72 4F RTA16WE 20050621001382005062100138NM 2005 6 21 SWAA051769 120050616A53116546525 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050621001432005062100143NM 2005 6 21 SWAA051774 120050616A53306545768 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29508SW 24185 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050621001522005062100152NE 2005 6 21 2005UALA00522 220050603A7261 OIL COOLER BOEING747 747422 1384935NM PWA 4056 PW4056 NE NR 4 ENGINE LEAKING A UALAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 WP29174UA 24381 717593 FUEL LEAK NR 4 ENGINE. DIVERTED TO NARITA. CP07 AIR/OIL COOLER TUBE CRACKED. TUBE & CLAMPS WERE REPLACED. AGB REMOVED. SUSPECT AGB VIBRATION CAUSED TUBE CRACK. AGB TEARDOWN REVEALED NO DISCREPANCIES. ENGINE SUBSEQUENTLY REMOVED AS PRECAUTIONARY. SHOP INPUT POSTPONED INDEFINITELY. 2L74 4F4 FRTA20WE E24NE 20050621001692005062100169NM 2005 6 21 05FDEA01521 120050606A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25477FE 21394 EVIDENCE OF CRACK IN VERTICAL CHORD COMMON TO BS 870 BULKHEAD AND RIGHT KEELBEAM 6 INCHES UP FROM BOTTOM END OF CHORD. *S/D* REPLACED BS 870 CHORD PER SRM 51-30-2. 2L73 4F RTA3WE 20050621001702005062100170EA 2005 6 21 COMA0560346 120050611A76032100140007 GEARBOX CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE RT ENG THROTTLE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01785CA8157 7326 807651 WHEN PERFORMING EO 76-011 AD, THE RIGHT ENGINE THROTTLE GEARBOX HOUSING WAS FOUND CRACKED AT THE ATR ATTACH POINT. REMOVED AND INSTALLED A SERVICABLE GEARBOX. 2L72 4F4 FRTA21EA E15NE 20050621001932005062100193NM 2005 6 21 2005UALA00525 120050608A2497BACT12AC36 TERMINAL BLOCK BOEING757 757222 1384956NM PWA 2037 PW2037 NE LT GENERATOR CRACKED A UALAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP29568UA 26674 RETURNED TO FIELD DUE TO MULTIPLE CB'S TRIPPED PRIOR TO ROTATION, MULTIPLE EICAS MSG'S. LEFT GENERATOR CONTACTOR, C901, PHASE -B- TERMINAL LUG WAS FOUND CRACKED / BROKEN, PROMOTING ELECTRICAL PROBLEMS AND CAUSING SOME CIRCUIT BREAKERS TO POP. THE TERMINAL LUG WAS REPLACED, THE AFFECTED C/BS WERE RESET AND CORRESPONDING SYSTEM OPS CHECKS WERE DONE AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA2NM E17NE 20050621002012005062100201NM 2005 6 21 2005UALA00533 120050609A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSLEAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP2903UA 24624 AFT PIT LT SIDE STA 1540 HAS 3 EACH DENTS BETWEEN STR 25L AND 26L, ON INBOARD FLANGE. REPAIRED FRAME WITH FABRICATED NEW PRODUCTION SPLICE ANGLE PER TIMCO REO (EVA) G10550, REV. B. 2L72 4F4 FRTA2NM E17NE 20050621002182005062100218NM 2005 6 21 05FDEA01607 120050614A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25266FE 21672 AFT FUSELAGE LOWER SKIN EXTERNAL SURFACE APPROX FS 1010 BETWEEN STRINGERS 27L AND 28L AREA IS EXFOLIATED CORROSION. REPAIRED DAMAGED AREA IAW SRM 53-30-3 FIG 3, MAJOR REPAIR. 2L73 4F RTA3WE 20050622000112005062200011NM 2005 6 22 SWAA051789 120050619A53116545812 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 328, STR 20R TO STR 21R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050622000132005062200013NM 2005 6 22 SWAA051800 120050619A5313BAC1498 STRINGER BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29508SW 24185 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 344, STR 8R. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2L72 4F RTA16WE 20050622000142005062200014NM 2005 6 22 SWAA051801 120050619A534065C27314 STRINGER CLIP BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29508SW 24185 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 294.5, STR 11L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050622000152005062200015NM 2005 6 22 SWAA051802 120050619A5330 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29508SW 24185 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE BOX CUTOUT, BEAR STRAP UPPER CORNER. REMOVED AND REPLACED STRAP PER SRM. 2L72 4F RTA16WE 20050622000182005062200018NE 2005 6 22 SWAA051805 220050616A7200CFM563 ENGINE BOEING737 7373H4 1384600NM GE CFM56 CFM563B1 13802NE RIGHT VIBRATION A SWAAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 SW29617SW 27700 858325 NR 2 ENGINE HAD NOTICABLE SHUDDER. VIBRATION GAUGE INDICATED 4.5. IDLE DESCENT OK. INCREASE POWER AT 12,000FT & ENGINE VIBRATION INDICATED OFF THE SCALE. REMOVED AND REPLACED NR 2 ENGINE ASSY PER MM. 2L72 4F4 FRTA16WE E2GL 20050622000202005062200020NM 2005 6 22 SWAA051807 120050619A56105893543130 WINDOW BOEING737 7373H4 1384600NM COCKPIT CRACKED A SWAAA UNSCHED LANDING O OTHER CLCLIMB 1 SW29637SW 27710 AIR TURNBACK/DECLARED EMERGENCY. CLIMBING THROUGH 20,000FT NOTICED LARGE CRACK DEVELOPING ON R1 COCKPIT WINDSHIELD. REMOVED AND REPLACED R1 WINDOW & HEAT CONTROLLER PER MM. 2L72 4F RTA16WE 20050622000212005062200021NM 2005 6 22 SWAA051777 120050619A53116546554 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050622000222005062200022NM 2005 6 22 SWAA051778 120050619A53116546555 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050622000232005062200023NM 2005 6 22 SWAA051780 120050619A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727D, STR 6R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050622000242005062200024 2005 6 22 SWAA051790 420050619A2565D31354 SLIDE BOEING737 7373K2 13844BANM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29345SA 23786 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050622000262005062200026NM 2005 6 22 SWAA051792 120050619A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29402WN 29814 EEPLS COVER LOOSE AT FWD END. SECURED COVER PER MM. 2L72 4F RTA16WE 20050622000272005062200027NM 2005 6 22 SWAA051793 120050618A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29458WN 33857 EEPLS COVER DAMAGED AT ROW 1. REMOVED AND REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20050622000282005062200028 2005 6 22 SWAA051794 420050618A256565C16820 HOOK BOEING737 7377H4 1384404NM L1 DOOR GIRT BARLOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29493WN 32477 L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER MM. 2L72 4F RTA16WE 20050622000292005062200029NM 2005 6 22 SWAA051795 120050617A53306545767 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29501SW 24178 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 400, STR 16R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050622000302005062200030NM 2005 6 22 SWAA051796 120050617A53306545776 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29501SW 24178 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 870, STR 23R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050622000312005062200031NM 2005 6 22 SWAA051797 120050617A53306545765 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29501SW 24178 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520 + 6, STR 10R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050622000332005062200033NM 2005 6 22 SWAA051808 120050619A3350101073 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29638SW 27711 L1 DOOR EMERGENCY EXIT SIGN LENS COVER MISSING. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20050622000342005062200034NM 2005 6 22 SWAA051809 120050617A3234A42006028305 SOLENOID BOEING737 7373Q8 1384670NM MLG HANDLE FAULTY A SWAAA UNSCHED LANDING O OTHER CLCLIMB 1 SW29687SW 23388 AIR TURNBACK. LANDING GEAR LEVER WOULD NOT MOVE UP AFTER TAKEOFF. LEVER LOCK SOLENOID FAILURE INDICATED. REMOVED AND REPLACED MLG HANDLE SOLENOID PER MM. 2L72 4F RTA16WE 20050622000362005062200036NM 2005 6 22 SWAA051811 120050617A3350D71702001 BATTERY PACK BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29705SW 27839 DURING SCHEDULED MV2 CHECK, FOUND SEVERAL CABIN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050622000372005062200037NE 2005 6 22 SWAA051812 220050616A7230P333P05 BLADE BOEING737 7377H4 1384404NM GE CFM56 CFM567B24 NE NR 2 ENGINE TORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29708SW 27842 874194 DURING SCHEDULED HC2 CHECK, C/W BOROSCOPE INSPECTION OF NR 2 ENGINE AND FOUND 1 EA NR 3 HPC BLADE OUT OF LIMITS. REMOVED AND REPLACED NR 2 ENGINE PER MM. 2L72 4F4 FRTA16WE E00055EN 20050622000402005062200040CE 2005 6 22 DXTA200500762 120050610A490038007221 APU CESSNA560 560XL 2076702CE SMOKE E DXTAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL07665QS3398 5605165 TAXIING FOR T/O ENGINES RUNNING, APU & BLEED AIR ON, ALL AVIONICS ON, THE CABIN & COCKPIT FILLED WITH SMOKE. SMOKE STOPPED WHEN I SHUT EVERYTHING DOWN AND TURNED ELECTRICAL POWER OFF. A LARGE AMOUNT OF WATER DRIPPING FROM BOTTOM OF APU. INSPECTED ENGINE INTAKES, APU INTAKE & EXHAUST, NO DISCREPANCIES NOTED. REMOVED WATER SEPARATOR & INSPECTED, NO DISCREPANCIES. OPERATED LT &RT ENGINES FOR 45 MINUTES WITH ALL AVIONICS OPERATING, NO DISCREPANCIES. OPERATED APU & WITHIN 30 SECONDS OF TURNING APU BLEED ON COCKPIT FILLED WITH SMOKE. SMOKE WAS WHITE WITH A DISTINCT OIL SMELL. TURNED APU BLEED OFF AND SMOKE DISSIPATED. SHUT LT & RT ENGINES DOWN. TURNED APU BLEED ON AGAIN & SMOKE RETURNED. APU CAUSE OF SMOKE2L72 4F RTA22CE 20050622000432005062200043CE 2005 6 22 DXTA200500773 120050613A275067183201 CONTROLLER CESSNA750 750 2076810CE TE FLAPS MALFUNCTIONED E DXTAO OTHER J WARNING INDICATION APAPPROACH 1 GL07958QS4066 7500158 FLAPS FAIL CAS ILLUMINATED AT ALTITUDE TRIED ONE RESET PER CHECK LIST BUT FAILED AGAIN CONDUCTED NO FLAP LANDING AND MESSAGE STILL ILLUMINATED ON GROUND. TROUBLESHOT DISCREPANCY TO FLAP CONTROLLER DUE TO MULTIPLE BIT FAULTS 1, 2, 7 & 8 TRIPPED. REMOVED AND REPLACED FLAP CONTROLLER AND PERFORMED ELECTRICAL RIG AND CONTROLLER FUNCTIONAL TEST. OP CHECKED GOOD IAW 750-27-50-00 MM. 2L72 4J RTT00007WI 20050622000452005062200045NE 2005 6 22 DXTA200500774 220050614A7200 ENGINE CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE RIGHT MALFUNCTIONED E DXTAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 GL07302QS7733 5600402 PCEJCO277 ABORTED TAKEOFF, RIGHT ENGINE WOULD NOT MAKE TAKEOFF POWER (97.2) ONLY ACHIEVED 95.3 PERCENT. RAN RIGHT ENGINE TO TAKEOFF POWER [97.2], ALL PARAMETERS WERE WITHIN ACCEPTABLE LIMITS IAW CE 560 MM 71-01-02. 2L72 4F4 FRTA22CE E25EA 20050622000462005062200046CE 2005 6 22 DXTA200500775 120050614A291399121662 PUMP CESSNA500 560CESSNA 2076750CE HYD SYSTEM LEAKING E DXTAO OTHER KJ FLUID LOSS WARNING INDICATION LDLANDING 1 GL07314QS 5600441 ON SHORT FINAL, ANTI-SKID INOP AND POWER BRAKE LOW PRESS LIGHTS ILLUMINATED. NO BRAKES ON LANDING. LARGE HYD FLUID LEAK NOTICED ON POST FLIGHT. FLUID ON NOSE GEAR & INSIDE NOSE COMPARTMENT. REMOVED AND REPLACED PUMP ASSY, REPLACED FILTER ELEMENT & FILTER CASE BOWL. PERFORMED ANTI SKID BRAKE BLEED IN ACCORDANCE WITH MM 32-42-00. OPS AND LEAK CHECKED GOOD. 2L72 4F RTA22CE 20050622000502005062200050CE 2005 6 22 DXTA200500777 120050615A2740 TRIM SYSTEM CESSNA750 750 2076810CE STABILIZER FROZEN E DXTAA UNSCHED LANDING P NO WARNING INDICATION CRCRUISE 1 GL07910QS 7500110 STABILIZER TRIM JAMMED DURING FLIGHT AT -2.3 POSITION ON EICAS TRIM CLACKER WAS HEARD AT FIRST INTERMITTENTLY THEN ALMOST CONTINUOUSLY WHILE STAB REMAINED AT -2.3 POSITION. ONCE DESCENT WAS INITIATED STABILIZER UNFROZE AND SUDDEN PITCH CHANGE OCCURRED SOME SCUFFING APPARENT ON VERTICAL STABILIZER ON LEFT SIDE AT THE LEADING EDGE OF THE STAB. ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20050622000522005062200052NM 2005 6 22 SB05073 120050619A21337110033 OUTFLOW VALVE BOEING737 737301 1384611NM CABIN PRESSURE FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19575US5963859638 23740 EN ROUTE FROM CLT TO BUF, 100 MILES SOUTH OF PIT, AIRCRAFT LOST AUTO AND STANDBY PRESSURIZATION MODES. HOWEVER, CREW WAS ABLE TO REGAIN CONTROL IN MANUAL PRESSURIZATION MODE AT FL230. DUE TO OPERATIONAL CONCERNS, FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE AFT OUTFLOW VALVE PER MM 21-31-11-4. ALSO, REPLACED THE CABIN PRESSURE CONTROLLER. LEAK AND OPERATIONAL CHECK GOOD. ACCOMPLISHED SUCCESSFUL PRESSURIZATION CONFIDENCE CHECK PER JOB CARD J321-00-01. 2L72 4F RTA16WE 20050622000532005062200053SO 2005 6 22 SIMA200512507 120050503A335020131A BATTERY EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT INOPERATIVE A SIMAO OTHER L NO TEST NRNOT REPORTED 1 SW21717AE 145272 EMERGENCY EXIT SIGN AT ROW 2 NOT ILLUMINATED. REPLACED NR 2 EMERGENCY LIGHT BATTERY ASSEMBLY IAW EMB 135 AMM 33-50-04. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050622000552005062200055SO 2005 6 22 SIMA200515706 120050526A531112010732001 FRAME EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21646AE 145213 ABI - DURING AN MBV INSPECTION, THE LOWER FRAME 81 WAS FOUND GOUGED. REMOVED THE GOUGED FRAME. INSTALLED NEW FRAME IAW EMB 145 SRM, SRM EMB145/1142 REV 29, CHAPTERS 51-20-01, 51-20-03, 51-40-02 AND 51-40-04. (M) 2L72 4T RTT00011AT 20050622000562005062200056SO 2005 6 22 SIMA200515707 120050525A534014522460013 GUSSET EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A SIMAO OTHER O OTHER NRNOT REPORTED 1 SW21648AT 145225 SAW - DURING AN MBV, FORWARD CABIN FLOOR GUSSET HAS CORROSION IN NUMEROUS AREAS FROM FRAME 20 TO 23. INSTALLED NEW FORWARD CABIN FLOOR GUSSET IAW EMB SRM 51-40-02 PAGE 1. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20050622000572005062200057SO 2005 6 22 SIMA200515705 120050527A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21812AE 145531 ABI - DURING AN IMBV INSPECTION, THE CENTER BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND TO BE CORRODED. BLENDED THE DAMAGED AREA ON THE CENTER OMEGA BEAM TO REMOVED THE CORROSION. APPLIED ALODINED AND EPOXY PRIMER TO THE REWORK AREA. FILLED THE BLENDED AREA WITH EA934NA EPOXY RESIN AND CURED. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW EMB REPAIR STATEMENT IC2005-145/2667 PARA 2 DATED MAY 23, 2005. (M) 2L72 4F RTT00011AT 20050622000592005062200059EA 2005 6 22 ASOA05407 120050505A21707536893 COALESCER BAG CNDAIRCL600 CL6002B19 1900309EA RT A/C PACK ODOR A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27836AS 7263 FLT 4518 - DURING CLIMB-OUT FROM SHV-ATL, THE CREW NOTICED AN OILY ODOR POSSIBLY FROM THE AIR CONDITIONING PACKS. THE FLIGHT CONTINUED AND THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT COALESCER BAGS. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050622000612005062200061EA 2005 6 22 QXEA200500987 120050410A3150 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA ILLUMINATED A QXEAO OTHER J WARNING INDICATION APAPPROACH 1 NM09605QX2430 10022 RECEIVED LT AND RT WING ANTI-ICE CAUTION MESSAGE ON 5 MILE FINAL. RAN CHECKLIST FOR WING ANTI-ICE CAUTION. CAUTION REMOVED. CAUTION RETURNED ON SHORT FINAL WITH BLEED AIR CROSS BLEED SET TO FROM RT. MX INTERROGATED MDC. REPORTS AFLC INTERNAL FAULT. LOSS OF A AND B CHANNELS TO DCU'S. REPLACED AILC IAW CRJ AMM 30-12-400-801-A01. OPS CHECK GOOD. ACFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20050622000632005062200063NM 2005 6 22 QXEA200501046 120050526A5330 SKIN BOMBDRDHC8 DHC8402 1390042NM ZONE 100 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09415QX 4081 PDX - RT LOWER FUSELAGE SKIN HAS TWO NICKS ALONG STRINGER 30R, FORWARD OF X49.75. REPAIRED IAW RD 8/4-53-505, PAGE 5. 2H72 4T RTA13NM 20050622000652005062200065NM 2005 6 22 QXEA200501045 120050531A5330 SKIN BOMBDRDHC8 DHC8402 1390042NM ZONE 100 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09415QX 4081 PDX - LEFT LOWER FUSELAGE SKIN HAS A NICK AT STRINGER 31L, AT X59. REPAIRED IAW Q400 RD 8/4-53-505, PAGE 5. 2H72 4T RTA13NM 20050622000662005062200066NM 2005 6 22 QXEA200501047 120050526A5330 SKIN BOMBDRDHC8 DHC8402 1390042NM ZONE 100 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09415QX 4081 PDX - THREE NICKS IN LEFT LOWER FUSELAGE SKIN BETWEEN X1.0 AND X19.4 ALONG STRINGER 32L. REPAIRED IAW RD 8/4-53-666, PAGE 5. 2H72 4T RTA13NM 20050622000672005062200067NM 2005 6 22 QXEA200501048 120050604A5347 SEAT TRACK BOMBDRDHC8 DHC8402 1390042NM ZONE 200 WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09415QX 4081 PDX - CO-PILOTS OUTBOARD SEAT TRACK HAS WEAR ON TOP SURFACE. REPAIRED IAW Q400 SRM 51-25-10 AND SRM 51-42-45. 2H72 4T RTA13NM 20050622000682005062200068NM 2005 6 22 QXEA200501049 120050527A5420 DIAPHRAGM BOMBDRDHC8 DHC8402 1390042NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09415QX 4081 PDX - LEFT NACELLE, OUTBOARD SIDE, DIAPHRAGM CRACKED AT STATION 197.00. REPAIRED IAW RD 8/4-54-155 AND DHC-8-400 SRM 51-40-10 AND 51-42-05. 2H72 4T RTA13NM 20050622000702005062200070NM 2005 6 22 QXEA200501040 120050531A5753 SKIN BOMBDRDHC8 DHC8402 1390042NM ZONE 500 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09415QX 4081 PDX - LEFT WING OUTBOARD FLAP UPPER SURFACE IS CHAFFED AT APPROX YW 271.00 TO YW 265.00, 14" FROM TRAILING EDGE. BLENDED CHAFED AREA IAW DHC-8-400 SRM 57-52-30-320-801 AND REPAIRED IAW HORIZON AIR EA 6-57-437. 2H72 4T RTA13NM 20050622000712005062200071NM 2005 6 22 QXEA200501041 120050612A26214739512 FIRE BOTTLE BOMBDRDHC8 DHC8402 1390042NM APU BAY MALFUNCTIONED A QXEAK NONE J WARNING INDICATION CRCRUISE 1 NM09402QX6953 4032 "CHECK FIRE DETECT" WARNING LIGHT ILLUMINATED, ASSOCIATED WITH THE APU "BTL LOW" ADVISORY LIGHT. REPLACED APU FIRE BOTTLE PER MTC 6262301, 6262302 AND HORIZON AIR EA 6-26-17, PERFORMED OPERATION TEST OF APU FIRE DETECTION SYSTEM PER Q400 AMM TASK 26-13-00-710-801, APU CHECKED GOOD. ACRFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050622000772005062200077NM 2005 6 22 QXEA200500978 120050606A2140 LINE BOMBDRDHC8 DHC8402 1390042NM HEATING SYS BROKEN A QXEAA UNSCHED LANDING O OTHER CLCLIMB 1 NM09415QX 4081 UNABLE TO WARM ACFT CABIN AND FLIGHT COMPARTMENT. DUCT TEMP INDICATED 0 AND REMAINED THERE IN BOTH AUTO AND MANUAL. INSP AND FOUND AIR CONDITIONING PACK FLOW CONTROL VALVE SENSING LINE BROKEN. REPLACED VALVE SENSING LINE AND PACK FLOW CONTROL VALVE FILTER IAW MM TASK 21-52-00-618-801. PERFORMED OPS CHECK OF BOTH CABIN AND FLIGHT COMPARTMENT TEMPERATURE CONTROL. OPS CHECK GOOD IN BOTH AUTO AND MANUAL CONTROL. SENSING LINE LEAKS CHECK GOOD. ACFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050622000782005062200078NM 2005 6 22 QXEA200500979 120050531A5330 SKIN BOMBDRDHC8 DHC8402 1390042NM ZONE 100 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09415QX 4081 LT LOWER FUSELAGE SKIN HAS NICK AT STRINGER 31L AND STATION X59. REPAIRED IAW RD 8/4-53-505. 2H72 4T RTA13NM 20050622000792005062200079NM 2005 6 22 FX7A200500006 120050602A2612 WARNING LIGHT BOEING737 73733A 1384673NM GE CFM56 CFM56* 13802NE APU FIRE ILLUMINATED A FX7AF ACTIVATE FIRE EXT. J WARNING INDICATION CLCLIMB 1 SO19371FA 23631 APU FIRE WARNING SWITCH LIGHT ILLUMINATED AND FIRE WARNING. INDICATION AFTER TAKEOFF, SHUT DOWN APU AND PERFORMED FALCON AIR EMERGENCY PROCEDURES. 2L72 4F4 FRTA16WE E2GL 20050622000802005062200080NM 2005 6 22 QXEA200500989 120050423A3060 WARNING LIGHT BOMBDRDHC8 DHC8402 1390042NM PROP DE-ICE ILLUMINATED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09407QX2006 1237 4049 PROP DE-ICE CAUTION LIGHT ILLUMINATED. RAN CHECKLIST. RESET. PROP HEAT DE-ICE CAUTION LIGHT ILLUMINATED AND CYCLED. CAUTION LIGHT WOULD COME ON WHEN RT PROP GREEN LIGHT CAME ON. REPLACED NR 2 BRUSH BLOCK, NR 2 TMCU, NR 2 BLADE/NR 2 HEATER LEAD AND CALIBRATED. OPS CHECK GOOD. ACFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050622000822005062200082NM 2005 6 22 QXEA200500988 120050420A3030 ODOR DHAV DHC8 DHC8202 2809007NM COCKPIT DETECTED A QXEAO OTHER BW SMOKE/FUMES/ODORS/SPARKS INADEQUATE Q C CRCRUISE 1 NM09349PH 486 ACRID ELECTRICAL ODOR IN ACFT STRONGEST IN COCKPIT. FOUND ICE PROTECTION LEFT IN "ON" POSITION. ODOR DIMINISHED THROUGHOUT FLIGHT. MX INVESTIGATED ACFT INTERIOR FOR ANY ODOR. NONE NOTED. ATTRIBUTE ODOR TO SEVERAL ICE PROTECTION SWITCHES IE VALVE HEAT AND PITOT HEAT IN "ON" POSITION WITH ACFT ON GROUND IN RDM. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050622000832005062200083NM 2005 6 22 QXEA200500985 120050409A2750C1486561 POWER UNIT BOMBDRDHC8 DHC8402 1390042NM TE FLAP CONTROL MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM09403QX6316 10 4037 AFTER PUSHBACK FROM GATE AND SELECTED FLAPS -15 DEGREES, FLAP POWER CAUTION ILLUMINATED. PERFORMED ABNORMAL FLAP POWER CAUTION CHECK LIST. RESET FLAP CONTROL CIRCUIT BREAKER. SET FLAPS TO 15 DEGREES AND FLAP POWER CAUTION CAME ON AGAIN. MX REPLACED FLAP POWER UNIT IAW AMM TASK 27-52-01-000-801, ALL CHECKS GOOD. LEAK CHECK GOOD. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050622000862005062200086NM 2005 6 22 QXEA200500984 120050407A2750C1486742003 CONTROL UNIT BOMBDRDHC8 DHC8402 1390042NM FLAP CONTROL SYSMALFUNCTIONED A QXEAO OTHER J WARNING INDICATION APAPPROACH 1 NM09403QX11118 4037 UPON SELECTION OF FLAPS FROM 0 TO 5 DEGREES, FLAP POWER CAUTION LIGHT ILLUMINATED. FLAP CONTROL CIRCUIT BREAKER RESET VIA EMERGENCY PROCEDURE. FLAPS OPERATED NORMALLY FOR LANDING. MX REPLACED FLAP CONTROL UNIT AS A PRECAUTIONARY MEASURE IAW AMM 27-51-01, PAGE 401-409. FUNCTIONAL TEST GOOD. ACFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050622000872005062200087NM 2005 6 22 QXEA200500982 120050403A2750 WARNING LIGHT BOMBDRDHC8 DHC8402 1390042NM FLAP CONTROL SYSFALSE INDICATIONA QXEAO OTHER J WARNING INDICATION APAPPROACH 1 NM09403QX 4037 FLAP POWER CAUTION LIGHT ON APPROACH WHEN FLAPS WERE SELECTED TO 5 DEGREES. FOLLOWED EMERGENCY CHECKLIST. CIRCUIT BREAKER L7-L ESSENTIAL PULLED AND FLAPS OPERATED NORMALLY. MX CONTACTED VIA SELCAL. NO FURTHER MX ACTION REQUIRED. NO PARTS REPLACED. ACFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050622000892005062200089NM 2005 6 22 F3LA200500025 120050603A3411 PITOT TUBE AIRBUSA319 A319111 3930336NM PITOT/STATIC SYSCONTAMINATED A F3LAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 NM03929FR 2240 ABORTED TAKEOFF AT APPROX 100 KTS, FLIGHT CREW REPORTED DISCREPANCY BETWEEN NR 1 AND NR 2 AIRSPEED INDICATORS. TROUBLESHOT PER TSM 34-13-00-810-998 AND FOUND WATER IN CAPT AND F/O LINES TO PITOT TUBES. REMOVED WATER AND PERFORMED LEAK CHECK PER AMM 34-13-00-790-002. PERFORMED FUNCTIONAL TEST PER AMM 34-11-00-720-001 AND CHECKED OKAY. PERFORMED BRAKE OVERHEAT INSP PER AMM 05-51-16/601. SYSTEMS OPERATED NORMAL. 2L72 4F RTA28NM 20050622000922005062200092NM 2005 6 22 QXEA200501044 120050526A5330 SKIN BOMBDRDHC8 DHC8402 1390042NM ZONE 100 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09415QX 4081 LT LOWER FUSELAGE SKIN HAS AREA OF THREE LIGHT NICKS, OUTBOARD OF STRINGER 31L, FORWARD OF X49.75. REPAIRED IAW Q400 RD 8/4-53-666, PAGE 5, STEPS 4 THROUGH 6. 2H72 4T RTA13NM 20050622000932005062200093NM 2005 6 22 QXEA200501051 120050604A5347 SEAT TRACK BOMBDRDHC8 DHC8402 1390042NM ZONE 200 WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09415QX 4081 PILOTS OUTBOARD SEAT TRACK WORN ON TOP SURFACE. REPAIRED IAW Q400 AMM 25-11-01 TASK 25-11-01-00-801 AND Q400 SRM 51-25-10 AND 25-11-01. 2H72 4T RTA13NM 20050622000992005062200099NE 2005 6 22 SIMA200513603 220050513A7200CT79B ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RIGHT FAILED A SIMAC ABORTED TAKEOFF MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 SW21400BR 340B400 GEE785244 DURING TAKEOFF RT ENGINE FAILED. ITT WAS NOTED AT 1148 DEGREES. ACFT DID NOT GET OFF GROUND. MX REMOVED AND REPLACED RT ENGINE IAW SAAB MM. OPS AND LEAK CHECKS WERE SATISFACTORY. ACFT RETURNED TO SERVICE. (M) 2L72 4T4 TRTA52EU E8NE 20050622001002005062200100NM 2005 6 22 QXEA200501022 120050520A2430 WARNING LIGHT BOMBDRDHC8 DHC8402 1390042NM ZONE 100 FALSE INDICATIONA QXEAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM09415QX6464 5271 4081 NR 2 DC GENERATOR CAUTION LIGHT ON. CHECKLIST PROCEDURE DOES NOT CLEAR. C/W FIM TASK 24-31-00-810-813. FOUND NO EPCU FAULT CODES. C/W NR 2 DC GENERATOR OPERATIONAL CHECK. NO DEFECTS NOTED. NO PARTS REPLACED. ACFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050622001012005062200101EA 2005 6 22 COMA0560336 120050605A5244 ACCESS PANEL CNDAIRCL600 CL6002B19 1900309EA GROUND COMM OPEN A COMAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 SO01982CA 7168 LOUD SQUEAL DURING ROTATION AND CLIMB. GROUND COMMUNICATION PANEL LEFT OPEN. INSP FOR DAMAGE AND CLOSED DOOR. 2L72 4F RTA21EA 20050622001022005062200102NM 2005 6 22 QXEA200501023 120050525A33506138001 BATTERY PACK BOMBDRDHC8 DHC8402 1390042NM ZONE 200 INOPERATIVE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09405QX3527 1592 4047 FORWARD ESCAPE DOOR EMERGENCY LIGHTS INOP. R & R BATTERY PACKS 2LH, OPS CHECK GOOD. RETURNED TO SERVICE. 2H72 4T RTA13NM 20050622001052005062200105NM 2005 6 22 QXEA20051024 120050519A5210 DOOR BOMBDRDHC8 DHC8402 1390042NM AFT CABIN LACK OF LUBE A QXEAO OTHER O OTHER TXTAXI/GRND HDL 1 NM09413QX 4060 FLIGHT ATTENDANT REPORTS AFT PAX DOOR DIFFICULT TO OPEN. STICKS. CLEANED AND LUBED TRACK. OPS CHECK GOOD. NO PARTS REPLACED. ACFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050622001062005062200106NE 2005 6 22 ASOA05436 220050514A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RIGHT FAILED A ASOAEA ENGINE SHUTDOWN UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CRCRUISE 1 SO27876AS 7559 FLT 4109 - DURING CRUISE FROM ATL-DCA, AT APPROXIMATELY 27,000 FEET, THE CREW NOTICED THE RIGHT ENGINE OIL TEMPERATURE TURNED RED AND INDICATED ABOVE ONE HUNDRED AND SEVENTY DEGREES CENTIGRADE. THE QRH WAS COMPLIED WITH AND THE CREW SHUT DOWN THE RIGHT ENGINE SINCE THE OIL TEMPERATURE WAS UNCONTROLLABLE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO GSO WITH A SINGLE ENGINE LANDING PERFORMED SAFELY. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE ASSEMBLY. OPERATIONAL AND LEAKS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F4 FRTA21EA E15NE 20050622001072005062200107EA 2005 6 22 ASOA05445 120050517A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN DISCONNECTED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27845AS 7324 FLT 4620 - DURING A GROUND INSPECTION IN ATL, THE MIDDLE TO REAR SECTION OF EMERGENCY FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND AN EMERGENCY FLOOR TRACK LIGHT FILAMENT KNOCKED OUT OF THE TRACK CONNECTOR AND RECONNECTED IT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050622001082005062200108EA 2005 6 22 ASOA05444 120050507A3350BR9279106 LIGHT CNDAIRCL600 CL6002B19 1900309EA GALLEY CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27867AS 7463 DURING A C-CHECK IN MCN, THE BASE AND LENS ON THE EMERGENCY EXIT LIGHT BY THE SERVICE DOOR WERE FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY BY THE SERVICE DOOR. OPERATIONAL CHECKS GOOD. (M) 2L72 4F RTA21EA 20050622001122005062200112EA 2005 6 22 ASOA05451 120050519A2530 COFFEEMAKER CNDAIRCL600 CL6002C10 1390015EA GALLEY ODOR A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27752EV 10166 FLT 4914 - DURING CRUISE FROM SLC-LAX, THE CREW NOTICED WHAT APPEARED TO BE AN ELECTRICAL ODOR AT THE COFFEE POTS WITH NO VISIBLE SIGNS OF SMOKE AND TURNED OFF THE COFFEE POTS. THE AIRCRAFT LANDED SAFELY IN LAX. MAINTENANCE INSPECTED THE FORWARD GALLEY LIGHTING, FORWARD LAV LIGHTING, AVIONICS COMPARTMENT, COFFEE MAKERS, FORWARD POTABLE WATER SYSTEM, PACKS WITH AUXILIARY POWER UNIT AND ENGINE OPERATING AND FOUND THE RIGHT COFFEE MAKER WITH AN ELECTRICAL ODOR. MAINTENANCE DEFERRED THE LT AND RT COFFEEMAKERS UNDER MEL NR 25-70-01, CAT D, EXPIRING 9-16-05. THIS MRR WILL REMAIN OPEN PENDING THE APPROPRIATE CORRECTIVE ACTION TO THE COFFEEMAKERS. (M) 2L72 4F RTA21EA 20050622001132005062200113EA 2005 6 22 ASOA05448 120050519A3350OL307BPEGPL LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27931EV 8015 FLT 4906 - DURING A GROUND INSPECTION IN CAE, THE LEFT INBOARD FORWARD EMERGENCY EXIT SIGN WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE LEFT INBOARD FORWARD EMERGENCY EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050622001142005062200114EA 2005 6 22 ASOA05447 120050518A3230 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA MLG MALFUNCTIONED A ASOAO OTHER J WARNING INDICATION CLCLIMB 1 SO27844AS 7317 DURING CLIMB-OUT FROM TYS-ATL, UPON GEAR RETRACTION, THE CREW RECEIVED A RED GEAR DISAGREE WARNING MESSAGE FOR BOTH MAIN LANDING GEAR, MLG. CONCURRENTLY, THE NOSE GEAR FAILED TO EXTEND AND SUBSEQUENTLY EXTENDED AFTER THE CREW PERFORMED THE GEAR DOWN DISAGREE CHECKLIST. UPON COMPLETION OF THE REMAINING QRH ITEMS, THE DECISION WAS MADE TO CONTINUE THE FLIGHT TO ATL AND AN EMERGENCY WAS DECLARED. THE APPROACH AND LANDING IN ATL WERE MADE SAFELY. MAINTENANCE REMOVED AND REPLACED THE MLG SELECTOR VALVE AND BYPASS RUN AROUND VALVE. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050622001152005062200115SO 2005 6 22 SIMA200513606 120050513A335081502 LIGHT EMB 135 EMB135KL 3260302SO CABIN INOPERATIVE A SIMAK NONE O OTHER ININSP/MAINT 1 SW21833AE 145629 ORD - MAINTENANCE REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHT STRIP AT ROW 16 TO BE INOPERATIVE. MAINTENANCE REPLACED THE LIGHT STRIP AT ROW 16 IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050622001162005062200116EU 2005 6 22 USAA050725 120050524A5320 SILL AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19717UW17895 1069 PIT - FOUND FLOOR SILL PLATE CORRODED, C-66, FORWARD END OF RIGHT SILL PLATE. MACHINED REPAIR ANGLES AND FILLER PER SRM 53-41-14 REP NR 6. MACHINED REPAIR ANGLES AND FILLER PER SRM 53-41-14 REP NR 6. CORROSION LEVEL 2, TASK JA-260-53500. (M) 2L72 4F RTA28NM 20050622001172005062200117EU 2005 6 22 USAA050726 120050524A5320D5348004320501 SILL AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19716UW18358 1055 PIT - FOUND DOOR SILL CORRODED 1.25 INCH BY .200 INCHES DEEP, 2 INCHES FORWARD OF FORWARD GIRT BAR LATCH ON AFT SERVICE DOOR. CORROSION LEVEL 1, TASK JA-260-53500. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-72-11. (M) 2L72 4F RTA28NM 20050622001182005062200118NM 2005 6 22 USAA050715 120050601A5347 CARGO TRACK BOEING737 7374B7 138449CNM CARGO BAY CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19445US 24863 CLT - FOUND FLOOR TRACK ANGLE CORRODED 104 INCHES, CARGO FLOOR TRACK ANGLE, AFT CARGO STATION 787-847 STRINGER 27R. FABRICATED AND INSTALLED A NEW CARGO TRACK IAW SRM 53-00-53 FIG 202. (M) 2L72 4F RTA16WE 20050622001202005062200120SO 2005 6 22 SIMA200514502 120050520A532014521713005 CHANNEL EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21812AE 145531 ABI - THE GALLEY CENTER HAT BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED AND INSTALLED A DOUBLER. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 29 CHAPTER 53-21-10. (M) 2L72 4F RTT00011AT 20050622001212005062200121SO 2005 6 22 SIMA200515704 120050526A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO FUSLEAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21812AE 145531 ABI - DURING AN IMBV INSPECTION, THE CENTER OMEGA BEAM BETWEEN FRAMES 26 AND 27 WAS FOUND CORRODED. PERFORMED A CUTOUT OF THE CENTER OMEGA TO REMOVE CORROSION. FABRICATED A EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2005-145/2723 PARA 1 DATED MAY 25, 2005. (M) 2L72 4F RTT00011AT 20050622001222005062200122SO 2005 6 22 SIMA200515702 120050527A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21812AE 145531 ABI - DURING AN IMBV INSPECTION, THE LEFT OMEGA BEAM BETWEEN FRAMES 26 AND 27 WAS FOUND CORRODED. BLENDED THE DAMAGE AREA ON THE OMEGA BEAM TO REMOVED THE CORROSION. APPLIED ALODINE AND EPOXY PRIMER TO THE REWORKED AREA. FILLED THE BLENDED AREA WITH EA934NA EPOXY RESIN AND CURED. FABRICATED A REPAIR DOUBLER FOR REPAIR. REPAIR DONE IAW EMB REPAIR STATEMENT IC2005-145/2667 PARA 3 DATED MAY 23, 2005. 2L72 4F RTT00011AT 20050622001232005062200123SO 2005 6 22 SIMA200514301 120050514A532014521713006 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21852AE 145736 SAW - DURING AN MBV INSPECTION, MAINTENANCE FOUND THE LEFT OMEGA BEAM AT FRAME 20 CORRODED. REPAIRED DAMAGED OMEGA BEAM IAW SRM 53-21-10 FIGURE 201. INSTALLATION OF EXTERNAL ANGLE. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050622001242005062200124SO 2005 6 22 SIMA200512207 120050501A335037592 SIGN EMB 145 EMB145LR 3260212SO EMERGENCY EXIT INOPERATIVE A SIMAO OTHER O OTHER TXTAXI/GRND HDL 1 SW21649PP 145234 PIT - FLT 4297 - DURING PREFLIGHT, CREW REPORTED THE FORWARD CENTER OVERWING EXIT SIGN TO BE INOPERATIVE. MAINTENANCE REPLACED SIGN ASSEMBLY IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20050622001252005062200125EA 2005 6 22 ASOA05390 120050429A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27907EV 7648 DURING A C-CHECK IN HOT, THE FLOOR SUPPORT ANGLE AT FS 621 RIGHT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FLOOR SUPPORT ANGLE AT FS 621 RIGHT IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20050622001262005062200126SO 2005 6 22 SIMA200514304 120050519A2740KSC357620V BEARING EMB 135 EMB135KL 3260302SO HORIZONTAL STAB WORN A SIMAK NONE O OTHER ININSP/MAINT 1 SW21852AE 145736 SAW - DURING AN MBV INSPECTION, MAINTENANCE FOUND THE HORIZONTAL STABILIZER LEFT LINK BEARING BACKLASH FAILED. REPAIRED NR 1 AND NR 4 BUSHINGS IAW ENGINEERING ORDER EB-55MR-037. PERFORMED FUNCTIONAL CHECK OF HORIZONTAL STABILIZER BACKLASH OF LEFT AND RIGHT LINKS IAW WORK CARD 27-700-23. CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050622001272005062200127SO 2005 6 22 SIMA200509112 120050329A3350110049 CHARGER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A SIMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW21649PP 145234 DFW - FLT 3762 - FORWARD OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20050622001302005062200130SO 2005 6 22 SIMA200514501 120050513A532014525480003 SILL EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21814AE 145541 THE CARGO DOOR OPENING LOWER SILL WAS FOUND CORRODED. REMOVED EXISTING LOWER SILL AND INSTALLED NEW SILL IAW EMB 145 SRM, SRM EMB-145/1142 REV 29) CHAPTERS 51-40-02 AND 51-20-03. (M) 2L72 4F RTT00011AT 20050622001342005062200134SO 2005 6 22 SIMA200515106 120050526A2510 SEAT EMB 145 EMB145LR 3260212SO COCKPIT OUT OF TRACK A SIMAO OTHER O OTHER NRNOT REPORTED 1 SW21670AE 145790 ORD - FLT 4395 - CREW REPORTED THE FIRST OFFICERS SEAT WAS INOPERATIVE AND WAS OUT OF ITS TRACK. MAINTENANCE INSPECTED THE SEAT AND FOUND NO DEFECTS. SEAT WAS REINSTALLED IN ITS SEAT TRACKS IAW EMB MM. (M) 2L72 4T RTT00011AT 20050622001372005062200137SO 2005 6 22 SIMA200515107 120050528A21408125464 CONTROL MODULE EMB 135 EMB135KL 3260302SO TEMP CONTROL INOPERATIVE A SIMAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW21817AE 145554 AMA - FLT 3545 - CREW REPORTED SMOKE AND AN ELECTRICAL ODOR FROM THE FIRST OFFICERS SIDE INSTRUMENT PANEL. SHUTOFF ALL POWER AND SMOKE AND ODOR STARTED TO DISSIPATE. MAINTENANCE REPLACED TEMPERATURE CONTROL MODULE IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050622001382005062200138SO 2005 6 22 SIMA200515102 120050505A531112010732001 FRAME EMB 135 EMB135LR 3260305SO FUSELAGE CRACKED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21 145211 ABI - DURING AN INSPECTION, FOUND FRAME 81 TO BE CRACKED. REMOVED THE CRACKED FRAME AND INSTALLED NEW FRAME IAW EMB SRM, SRM 145/1142 REV 29, CHAPTER 51-40-02. (M) 2L72 4F RTT00011AT 20050622001402005062200140EA 2005 6 22 ASOA05443 120050508A5210601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27867AS 7463 DURING A C-CHECK IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND BROKEN LOOSE FROM THE ACTUATOR ROD. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP IAW CRJ-200 SRM 51-42. (M) 2L72 4F RTA21EA 20050622001412005062200141EU 2005 6 22 ASOA05442 120050516A3397 WIRE AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT LOOSE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27632AS 338 DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY FLOOR LIGHT AT ROW 17 A/B WAS FOUND TO BE INOPERATIVE. MAINTENANCE RESECURED THE WIRING TO THE EMERGENCY FLOOR LIGHT AT ROW 17 A/B. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20050622001432005062200143NM 2005 6 22 USAA050718 120050602A5753 WEDGE BOEING737 7374B7 1384702NM TE FLAPS CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19445US 24863 CLT - FOUND SKIN CRACKED, RT INBOARD MID FLAP WEDGE. INSTALLED DOUBLR IAW RM 51-70-10. (M) 2L72 4F RTA16WE 20050622001442005062200144SO 2005 6 22 SIMA200515202 120050530A2120 SMOKE EMB 145 EMB145LR 3260212SO CABIN DETECTED A SIMAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW21646AE 145213 DFW - PASSENGER REPORTED SMOKE IN CABIN WHILE SITTING AT THE GATE WITH APU RUNNING AND ENGINES SHUT DOWN. MAINTENANCE GROUND RAN ENGINES AND REPORTED NO SMOKE OR FUMES. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20050622001452005062200145SO 2005 6 22 SIMA200514503 120050523A32347455501 LEVER EMB 145 EMB145LR 3260212SO MLG INOPERATIVE A SIMAO OTHER J WARNING INDICATION LDLANDING 1 SW21636AE 145160 ORD - FLT 4204 - ON APPROACH TO ORD LANDING GEAR RECEIVED AIR/GND FAIL MESSAGE. CREW USED EMERGENCY EXTENSION PROCEDURES TO LOWER LANDING GEAR. REPLACED LANDING GEAR SELECTOR LEVER. OP CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20050622001472005062200147SO 2005 6 22 SIMA200513605 120050513A335078241 INVERTER EMB 135 EMB135KL 3260302SO EMERGENCY LIGHT INOPERATIVE A SIMAK NONE O OTHER ININSP/MAINT 1 SW21833AE 145629 ORD - FLT 1484 - CREW REPORTED THE EMERGENCY LIGHT AT ROW 3 BC TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT INVERTER IAW EMB EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050622001482005062200148SO 2005 6 22 SIMA200513104 120050511A335020131A BATTERY EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT INOPERATIVE A SIMAO OTHER O OTHER TXTAXI/GRND HDL 1 SW21738NR 145401 CLT - FLT 4892 - CREW REPORTED THE EMERGENCY LIGHTING SYSTEM FLOOR PROXIMITY STRIPS BY ROW 3, 4, 5 AND 6 TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 BATTERY AND CHARGER IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050622001502005062200150SO 2005 6 22 SIMA200513604 120050510A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21814AE 145541 ABI - DURING AN INSPECTION, THE LEFT OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND CORRODED. PERFORMED CUT OUT OF THE OMEGA BEAM TO REMOVE THE CORROSION. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 29, CHAPTER 53-22-10 FIG 202. (M) 2L72 4F RTT00011AT 20050622001532005062200153EA 2005 6 22 ASOA05431 120050512A4930MS59882904 O-RING CNDAIRCL600 CL6002B19 1900309EA APU FUEL LEAKING A ASOAA UNSCHED LANDING KBJFLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 SO27821AS 7194 FLT 4358 - DURING CRUISE FROM DHN-ATL, THE CREW NOTICED A BURNING OIL TYPE ODOR COMING THROUGH THE AIR CONDITIONING SYSTEM INTERMITTENTLY, OCCURRING ON BOTH THE ENIGNE AND AUXILLARY POWER UNIT BLEEDS. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE FOUND A EXCESSIVE FUEL LEAK ON THE AUXILLARY POWER UNIT AND REMOVED AND REPLACED AN O-RING ON THE FUEL SOLENOID. MAINTENANCE ALSO REMOVED AND REPLACED A COALESCER BAG FOR PREVENTATIVE MAINTENANCE AND CLEANED ALL AREAS AROUND THE APU. MAINTENANCE RAN THE PACKS WITH THE APU AND ENGINE FOR ONE HOUR. NO SMELLS WERE NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050622001542005062200154EA 2005 6 22 ASOA05430 120050511A21707536893 COALESCER BAG CNDAIRCL600 CL6002B19 1900309EA RT AND LT ODOR A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27821AS 7194 FLT - 4393 - DURING CRUISE, DESCENT AND LANDING FROM MGM-CVG, THE CREW NOTICED AN OILY TYPE SMELL IN THE COCKPIT AND CABIN. THE AIRCRAFT LANDED SAFELY IN CVG. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT COALESCER BAGS IAW CRJ AMM 21-00. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050622001552005062200155EA 2005 6 22 ASOA05428 120050511A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27880AS 7606 FLT 4786 - DURING A GROUND INSPECTION IN ATL, A FORWARD OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN A FORWARD OVERWING EMERGENCY LIGHT. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050622001562005062200156EA 2005 6 22 ASOA05446 120050518A5210 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAO OTHER O OTHER NRNOT REPORTED 1 SO27861AS 7445 DURING AN A-CHECK IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND BROKEN AT THE ATTACH POINT. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. (M) 2L72 4F RTA21EA 20050622001582005062200158EU 2005 6 22 USAA050724 120050520A5315D5311282600101 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19717UW17895 1069 PIT - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH AREA, FRAME 17 BLL 18 INCHES. CORROSION LEVEL 2, TASK JA-220-53500. REPLACED FLOORBEAM PER SRM 53-11-14, DWG B2D53112826. (M) 2L72 4F RTA28NM 20050621000322005062100032WP 2005 6 21 ASMF200506010 120050606A2910 LINE DOUG DC9 DC987 3022087WP HYD SYSTEM LEAKING W ASMFK NONE K FLUID LOSS ININSP/MAINT 1 SW23754RA 49641 DURING TRANSIT CHECK WAS DETECTED HYDRAULIC LEAK IN RIGHT WING. DURING REVISION IN RIGHT INBOARD SPOILER ACTUATOR LINE WAS DETECTED LEAKED, HYDRAULIC TUBE WAS REMOVED AND HYDRAULIC HOSE WAS INSTALLED IAW MM 20-12-04, TESTED CORRECT. DURING OVERNIGHT SERVICE, THE HYDRAULIC HOSE WAS REPLACED PER RIGHT PIPING ASSY HYDRAULIC GROUND SPOILER DOWN RIGHT SIDE IAW MM 27-61-07, TESTED CORRECT. 2L72 4F RTA6WE 20050621000382005062100038EU 2005 6 21 DHL2005367517 120050525A5540A554700100451 HINGE FITTING AIRBUS300 A300B4203 3930306EU ZONE 300 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01367DH 265 DURING "C" CHECK FOUND N/R 018535, RUDDER HINGE AND HYDRAULIC ACTUATOR FITTING ATTACHMENT TO RUDDER AT RIB 19 (UPPER ACTUATOR) AREA CRACKED. R & R SERVICEABLE RUDDER IAW A-300 MM 27-21-21. OP CHECK FOUND GOOD IAW A-300 MM 27-21-21. REMOVE RUDDER FOR REPAIR IAW A-300 MM 27-21-21. OK TO INSTALL SERV RUDDER. TORQUE NR 1 AND NR 7 HINGE IAW A-300 MM 27-21-21. TORQUE 3 SERVO ACTUATOR IAW A-300 MM 27-21-21. TORQUE NR 5 AND NR 6 HINGE IAW A-300 MM 27-21-21. TORQUE NR 2 AND NR 3 HINGE IAW A-300 A-300 MM 27-21-21. TORQUE NR 4 HINGE IAW A-300 MM 27-21-21. 2L72 4F RTA35EU 20050621000522005062100052WP 2005 6 21 ABXA050135 120050513A57519957570504 SKIN DOUG DC9 DC932F 3022067WP RT AILERON CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23909AX 47148 SEVERAL AREAS OF CORROSION (BULGING SKIN) EVIDENT ON BOTTOM SKIN OF RIGHT AILERON. REPAIRED AREA IAW DC-9 SRM. 2L72 4F A6WE 20050621000632005062100063 2005 6 21 SA05060 420050601A2565 STRAP AIRBUSA319 A319112 3930323EU ESCAPE SLIDE MISROUTED A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19711UW 1033 PIT - DURING INSP, FOUND AFT RIGHT SLIDE/RAFT ASSEMBLY RELEASE STRAP ROUTED INCORRECTLY. CORRECTLY ROUTED RELEASE STRAP TO AFT RIGHT SLIDE/RAFT ASSEMBLY. OK FOR SERVICE. 2L72 4F RTA28NM 20050621000662005062100066WP 2005 6 21 DXTA200500747 220050531A7261S9413117 O-RING RAYTHNDH125 HAWKER800XP 7150012CE GARRTTTFE731TFE731* 01518WP ENG OIL CAP TORN E DXTAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 GL07886QS 258486 LT OIL PRESSURE GAUGE READ BETWEEN 25 PSI AND 40 PSI AT 38,000 FEET. TEN MINUTES LATER OIL PRESSURE LOW LIGHT ILLUMINATED AND GAUGE READ 23 PSI. PERFORMED PRECAUTIONARY SHUTDOWN VIA CHECKLIST. FOUND OIL TO BE ORIGINATING FROM OIL SERVICING CAP AREA. REMOVED OIL CAP AND FOUND 1/2 INCH SECTION O-RING REMAINING IN STAND PIPE. REMOVED 1/2 INCH SECTION OF O-RING. INSTALLED NEW O-RING, SERVICED ENG OIL 5 1/2 QTS OIL. WASHED AREA. LEAK AND OPS CHECKED GOOD MM 79-10-02. 2L72 4F4 FRTA3EU E6WE 20050621000852005062100085EA 2005 6 21 A6WA200540190 120050530A5210 DRAG ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31418AW 7618 PASSENGER DOOR AFT DRAG ANGLE IS CRACKED AT POWER ASSIST PULLEY BRACKET. REPAIRED AFT DRAG ANGLE IAW REO. (K) 2L72 4F4 FRTA21EA E15NE 20050621001042005062100104SW 2005 6 21 KBM2005F00111 120050523A6510327211 DISC BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL T/R DRIVESHAFT CRACKED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19667JM 3444 DISC ASSEMBLY, TAIL ROTOR DRIVESHAFT DISC ASSY CRACKING, REMOVED AND REPLACED. (K) 1G71 3U3 U H2SW E4CE 20050621001172005062100117WP 2005 6 21 ASMF200506014 120050611A2130 UNKNOWN DOUG DC9 DC982 3022082WP CABIN PRESSURE UNKNOWN W ASMFO OTHER J WARNING INDICATION DEDESCENT 1 SW231003Y15947 48068 CAPTAIN REPORTED BOTH AIR CONDITION PACKS WITH LOW FLOW AND DURING DESCENT IT WAS NECESSARY TO MAINTAIN THRUST. BOTH A/A PILOT AND PNEUMATIC REGULATORS WERE REPLACED IAW MM 21-20-00, TESTS WERE PERFORMED BUT PRESSURIZATION PROBLEMS CONTINUED. DURING TESTS, LEAKS WERE DETECTED AND CORRECTED, FLOW CONTROL VALVES AND LEFT WATER SEPARATOR TEMPERATURE CONTROL VALVE WERE REPLACED IAW MM 21-31-1, 21-31-11, 21-20-03 AND 36-10-02 AND FORWARD CARGO COMPARTMENT DOOR SEAL WAS REPLACED. CABIN PRESSURE CONTROL AND FUNCTIONAL TESTS TO BOTH AIR-CONDITIONING AND FUSELAGE LEAKAGE TEST WERE PERFORMED IAW MM 21-32-00 AND 36-10-00, ALL CORRECT. 2L72 4F A6WE 20050621001192005062100119EU 2005 6 21 AWXA200500695 120050610A5347D5311278220 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28642AW 584 SAL - MAJOR REPAIR - DURING C-7 CHECK FOUND SEVERE EXFOLIATION CORROSION ON PASSENGER SEAT TRACK FROM FR 20 TO FR 24 AT BL -Y765. REMOVED SEAT TRACK FROM FR 20 TO FR 24 AT BL -Y765 AND MACHINED SEAT TRACK IAW AIRBUS DWG D53112782. FABRICATED REPAIR PARTS WERE INSTALLED AT FR 20 TO FR 24 IAW AIRBUS 320 SRM 51-24-00 FIG 1 AND AIRBUS 320 SRM 51-72-11. 2L72 4F RTA28NM 20050621001212005062100121NM 2005 6 21 DHL2005741549 120050414A5751 SKIN BOEING727 7272Q9 138448MNM LT WING AILERON GOUGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 LEFT WING I/B AILERON I/B LOWER SKIN & FITTING GOUGED. REMOVED UPPER SKIN (DAMAGED) IAW B727 SRM 51-30-2 FIG 7. REMOVED FASTENERS FOR I/B AILERON FITTING REMOVAL IAW B727 SRM 51-30-2 FIG 7. FABRICATED NEW UPPER SKIN 2024-T3, 0.040 PO 9001938 (51 X 21.5 INCH) IAW SRM 57-50-2 FIG 7. LOCATED AND DRILLED UPPER & LOWER I/B AILERON SKINS & FITTING P/N 65-21737-7, PO 509669 IAW B727 SRM 57-50-2 FIG 7, 51-30-2, FIG 7. TREATED & PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED UPPER & LOWER SKINS & FITTING IAW B727 SRM 51-30-2 FIG 8. 2L73 4F RTA3WE 20050621001222005062100122NM 2005 6 21 DHL2005741551 120050414A5320 TORQUE BOX BOEING727 7272Q9 138448MNM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 LT LOWER TORQUE BOX DENTED AT BS 1235 IN AFT STAIR WELL. FABRICATED DOUBLER 7075-T6, .032, PO 209041 (5 X 3 INCH) IAW B727 SRM 51-40-2 AND 53-10-2, FIG 6. TREATED AND PRIMED AREA & PART IAW B727 SRM 51-10-2. INSTALLED DOUBLER IAW B727 SRM 51-40-2 FIG 1 AND 51-30-2 FIG 7. 2L73 4F RTA3WE 20050621001232005062100123NM 2005 6 21 DHL2005741548 120050414A5751 SKIN BOEING727 7272Q9 138448MNM LT WING AILERON BENT A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 LEFT WING O/B AILERON TAB UPPER L/E SKIN BENT & CRACKED AT NR 2 & NR 4 HINGE AREA. REMOVED LT O/B AILERON TRIM TAB IAW B727 MM 27-10-44. REMOVED UPPER L/E PANELS FROM LT WING, O/B AILERON TRIM TAB 3 EA, IAW B727 SRM 51-30-2. FABRICATED NEW L/E PANELS FROM 2024-T3, 0.016 PO 9001394 (15.5 X 2.5; 13.625 X 2.5; 13 X 2.5 INCH) IAW B727 SRM 57-50-2 FIG 8 & SRM 51-20-1 FIG 2. TREATED & PRIMED PARTS & WORK AREA IAW B727 SRM 51-10-2. INSTALLED NEW L/E PANELS ON LT WING O/B AILERON TRIM TAB IAW B727 SRM 51-30-2 & 51-20-4. 2L73 4F RTA3WE 20050621001292005062100129EU 2005 6 21 AWXA200500711 120050616A3397ABS0374A24 TERMINAL AIRBUS320 A320232 3930326EU EMERGENCY LIGHT DISCONNECTED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28661AW 1284 DTW - EEL - DURING 4 DAY CHECK FOUND EMERGENCY PATH LIGHTING AT ROW 9 INOPERATIVE. MAINTENANCE FOUND A DISCONNECT WIRE. RECONNECTED WIRE OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA28NM 20050621001302005062100130EU 2005 6 21 AWXA200500712 120050606A5347D531112782200 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28642AW 584 SAL - MAJOR REPAIR - DURING C-7 CHECK FOUND SEVERE EXFOLIATION CORROSION ON PASSENGER SEAT TRACK AT RT OUTBOARD FR 20 TO F4 24 AT -Y1292. MAINTENANCE REMOVED SEAT TRACK RT OUTBOARD FR 20 TO F4 24, -Y1292. SEAT TRACK WAS MACHINED IAW DRAWING NR B2D53112782. SEAT TRACK WAS INSTALLED IAW AIRBUS SRM 53-21-11 FIG 201. 2L72 4F RTA28NM 20050621001362005062100136NM 2005 6 21 SWAA051767 120050616A53116546526 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND 2 EA FUSELAGE FRAME CRACKS AT BS 400, STR 9L & STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050621001412005062100141NM 2005 6 21 SWAA051772 120050616A53106545806 SHEAR WEB BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR WEB CRACKED AT BS 304, STR 4L. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050621001442005062100144NM 2005 6 21 SWAA051775 120050616A53116545808 FRAME BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29508SW 24185 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 303, L1 DOOR LOWER STOP FITTING CUTOUT. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050621001722005062100172EU 2005 6 21 TXER104274 120050422A6730SC50911 SERVO UROCOPEC120 EC120B 8680987EU CYCLIC LEAKING B TXERO OTHER K FLUID LOSS NRNOT REPORTED 1 SW09588SC 1130 SERVO LEAKING. 1G72 3U NCR0001RD 20050621001792005062100179NM 2005 6 21 2005UALA00508 120050603A5330 SKIN BOEING737 737522 138449FNM FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29910UA 25254 FUSELAGE SKIN AT AFT CARGO DOOR CUTOUT AFT SIDE HAS HOLE IN FUSELAGE SKIN BUT NOT IN BEAR STRAP, MID WAY UP CUTOUT. DAMAGED REMOVED, INSTALLED DOUBLER AND TRIPLER WITH FILLER PER SRM 53-00-01. 2L72 4F RTA16WE 20050621001812005062100181NM 2005 6 21 2005UALA00510 120050606A5280 SKIN BOEING747 747422 1384935NM PWA 4056 PW4056 NE LT MLG DOOR DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP2918UA 28811 LEFT MAIN GEAR DOOR SUSTAINED DAMAGE DUE TO TIRE BLOW OUT. DAMAGE IS LOCATED ON INBOARD SIDE AT LOWER EDGE. HOLE IS APPROX 4 X 6 INCHES IN SIZE. DAMAGE DUE TO IMPACT WITH TIRE DEBRIS. SKIN DAMAGE LIMITED TO EXTERNAL SKIN ONLY, REPAIRED WITH EXTERNAL DOUBLER PATCH. 2L74 4F4 FRTA20WE E24NE 20050621001902005062100190NE 2005 6 21 2005UALA00521 220050602A7297 WIRE HARNESS BOEING747 747422 1384935NM PWA 4056 PW4056 NE ENGINE BURNED A UALAO OTHER O OTHER NRNOT REPORTED 1 WP29197UA 26901 724642 WIRE BUNDLE APPEARS BURNED UNDER CLAMP, AFT OF LEFT 2.9 BLEED VALVE AT BRACKET. CLOSER RE-EXAMINATION DISCLOSED THAT HARNESS WAS NOT BURNED. IT HAD BEEN OVERSPRAYED BY SOME UNKNOWN SUBSTANCE. NO CORRECTIVE ACTION REQUIRED. 2L74 4F4 FRTA20WE E24NE 20050621001942005062100194NM 2005 6 21 2005UALA00526 120050608A5340 ATTACH ANGLE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29503UA 24624 FWD NOSE AREA, STA 202 BULKHEAD, LT SIDE HAS ATTACH ANGLE CRACKED OUTBOARD OF FRAME ON LOWER SIDE LBL 36 AREA, REAR SIDE OF BULKHEAD. REPLACED BULKHEAD ATTACH ANGLE PER BAC DWG 141N5811-U1 AND INSTALLED PER SRM 51-40-2 2L72 4F4 FRTA2NM E17NE 20050621001982005062100198NM 2005 6 21 2005UALA00530 120050607A5311 FRAME BOEING737 737522 138449FNM BS AT STRING CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29910UA 25254 BODY STATION 663 FRAME IS CRACKED AT STRINGER CUTOUTS 1R, 2R AND 3R. CRACKS ARE ON LT SIDE OF STRINGERS IN RADIUS NEAR FUSELAGE SIDE OF FRAME. INSTALLED DOUBLER REPAIR PER SRM 53-00-07 FIG 209. 2L72 4F RTA16WE 20050621002052005062100205NM 2005 6 21 2005UALA00537 120050609A5320 INTERCOSTAL BOEING737 737322 1384676NM FUSELAGE WORN A UALAK NONE O OTHER ININSP/MAINT 1 WP29315UA 23947 DOOR 1L CUTOUT FWD FRAME HORIZONTAL INTERCOSTAL WORN AREA UPPER SURFACE JUST FWD OF LWR HINGE COVER. FABRICATED & REPLACE INTERCOSTAL PER SRM 53-10-15. 2L72 4F RTA16WE 20050621002132005062100213NM 2005 6 21 05FDEA01597 120050613A53206273179 FLOOR SUPPORT BOEING727 727200 138407ENM AFT CARGO PIT CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25262FE 21624 AFT CARGO COMPT FLOOR SUPPORT IS CRACKED AT FS 1030-1050 RBL 11. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 27-53-039. 2L73 4F RTA3WE 20050622000032005062200003NM 2005 6 22 SWAA051781 120050619A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 827, STR 10L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050622000042005062200004NM 2005 6 22 SWAA051782 120050619A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 967, STR 7L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050622000162005062200016NM 2005 6 22 SWAA051803 120050619A53106547978 CREASE BEAM BOEING737 7375H4 138449DNM CABIN FLOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29508SW 24185 DURING SCHEDULED 1/2D CHECK, FOUND LT CREASE BEAM WEB CRACKED AT BS 616 TO BS 639, STR 17L. REPAIRED WEB PER SWA EA. 2L72 4F RTA16WE 20050622000172005062200017NM 2005 6 22 SWAA051804 120050617A335020131A BATTERY BOEING737 7375H4 138449DNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29526SW 26568 DURING SCHEDULED SERVICE CHECK, FOUND LT EMERGENCY OVERWING EXIT LIGHT & CENTER AISLE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050622000192005062200019 2005 6 22 SWAA051806 420050618A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29635SW 27708 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050622000252005062200025 2005 6 22 SWAA051791 420050617A2565D31354418 SLIDE BOEING737 7373H4 1384600NM R2 DOOR DEPLOYED A SWAAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW29357SW 26594 R2 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY DEPLOYED. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20050622000352005062200035 2005 6 22 SWAA051810 420050617A256561620466 SLIDE BOEING737 7373G7 1384595NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29690SW 23783 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REMOVED AND REPLACED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20050622000492005062200049CE 2005 6 22 DXTA200500779 120050615A275099145104 RESOLVER CESSNA750 750 2076810CE TE FLAPS FAULTY E DXTAO OTHER J WARNING INDICATION CRCRUISE 1 GL07958QS 7500158 FLAP FAIL AMBER CAS MSG CAME ON DURING CRUISE ATTEMPTED ONE RESET PER CHECKLIST LIGHT DID NOT GO OUT PERFORMED NO FLAP LDG PER CHECKLIST SLATS DID EXTEND NORMALLY. PLACED FLAP BREAK OUT BOX ON FLAP SYSTEM & RAN FLAPS FOUND FAULT CODES 1, 6 & 8 POINTING TO FLAP RESOLVERS. FOUND BOTH RESOLVERS BAD. REMOVED AND REPLACED LT & RT FLAP RESOLVERS. LT P/N OFF CA2-C LH, P/N ON 9914510-4, LT S/N OFF UNKNOWN, LT S/N ON A0272, RT P/N OFF CA2-C, RT P/N ON 9914510-4, RT S/N OFF UNKNOWN, RT S/N ON A0290, OP'S CHECK GOOD IAW CE750 MM 27-50-00. 2L72 4J RTT00007WI 20050622000542005062200054EU 2005 6 22 USAA050723 120050521A5340 CLIP AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19717UW17895 1069 PIT - FOUND CLIP CORRODED 2 INCH BY 2 INCH AREA, FRAME 19, Y 66 INCH. FABRICATED NEW CLIP PER SRM 53-11-14. FABRICATED NEW CLIP PER SRM 53-11-14, ITEM 190. (M) 2L72 4F RTA28NM 20050622000582005062200058EA 2005 6 22 ASOA05412 120050508A5712 RIB CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27867AS 7643 DURING A C-CHECK IN MCN, THE LEFT BATTERY RIB AT THE UPPER CORNER WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT BATTRY RIB ASSEMBLY AT WS 53.60 IAW ASA EO 600-57-039A. (M) 2L72 4F RTA21EA 20050622000602005062200060SO 2005 6 22 SIMA200515105 120050524A532014522178005 SILL EMB 145 EMB145LR 3260212SO SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21646AE 145213 ABI - DURING AN MBV INSPECTION, THE SERVICE DOOR SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED SILL. INSTALLED NEW SILL IAW EMB SRM, SRM 145/1142 REV 29, CHAPTER 51-20-01, 03, 51-40-02, 04, 06 AND EMB CPM, CPM 145/1132 REV 12 CHAPTER 51-21-04. (M) 2L72 4T RTT00011AT 20050622000642005062200064NM 2005 6 22 QXEA200501043 120050526A5330 SKIN BOMBDRDHC8 DHC8402 1390042NM ZONE 100 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09415QX 4081 PDX - LEFT LOWER FUSELAGE SKIN HAS A LIGHT NICK OUTBOARD OF STRINGER 31L, AFT OF X19.4. REPAIRED IAW Q400 RD 8/4-53-505, PAGE 5, STEP 4. 2H72 4T RTA13NM 20050622000692005062200069NM 2005 6 22 QXEA200501050 120050527A5420 DIAPHRAGM BOMBDRDHC8 DHC8402 1390042NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09415QX 4081 PDX - RIGHT NACELLE OUTBOARD SIDE, DIAPHRAGM CRACKED AT STATION 197.00 ABOVE NR 3 FLAP TRACK. REPAIRED IAW Q400 SRM 51-40-07. 2H72 4T RTA13NM 20050622000722005062200072NM 2005 6 22 DHL2005784524 120050606A5320 WEB BOEING727 727227 1384078NM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01784DH 22001 LT AFT AIRSTAIR BET BS 1223 AND 1243 WEB CRACKED (MARKED RED). STOP DRILLED CRACK, SIZE 249 IAW B727 SRM 51-10-1. FABRICATED DOUBLER REPAIR, MAT USED 7075T6 .032 PO NR 9813, DIMENSIONS 6.125 X 4.5625 IAW B727 SRM 53-10-2 FIG 6, ALODINE AND PRIMED IAW SRM 51-10-2. INSTALLED DOUBLER REPAIR IAW B727 SRM 51-30-2. 2L73 4F A3WE 20050622000752005062200075EA 2005 6 22 QXEA200501028 120050606A2612 FIRE LOOP CNDAIRCL600 CL6002C10 1390015EA RT ENGINE SHORTED A QXEAO OTHER J WARNING INDICATION APAPPROACH 1 NM09612QX 10042 FIRE SYSTEM FAULT STATUS MESSAGE OCCURRED INTERMITTENTLY DURING DESCENT. MAINTENANCE INTERROGATED MDC SHOWS RT ENGINE LOOP INTERMITTENT SHORT. DEFERRED. ACFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20050622000762005062200076 2005 6 22 QXEA200500977 420050604A3418C12851AA03 COMPUTER CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE STALL WARNING MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09609QX6394 10031 GEE965314 RT AND LT FADEC FAULT STATUS MESSAGES. REMOVED STALL PROTECTION COMPUTER. RT AND LT FADEC FAULT STATUS MESSAGES EXTINGUISHED. OPERATIONAL CHECK GOOD. ACFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050622000962005062200096SO 2005 6 22 SIMA200512504 120050428A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21808AE 145519 CENTER OMEGA BEAM BETWEEN FRAMES 24 AND 25 FOUND CORRODED. BLENDED DAMAGED AREA TO REMOVE CORROSION. APPLIED ALODINE AND EPOXY PRIMER TO EXPOSED SURFACE. FABRICATED DOUBLER FOR REPAIR. REPAIR DONE IAW EMB REPAIR STATEMENT IC2005-145/2057 PARA 5 DATED APRIL 25, 2005. (M) 2L72 4F RTT00011AT 20050622000972005062200097NM 2005 6 22 DHL2005784506 120050515A5754 SPAR BOEING727 727227 1384078NM NR 7 SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01784DH 22001 RT WING NR 7 SLAT SPAR WEB CRACKED AT TAI DUCT CUT OUT AT WS 610.5. STOP DRILL CRACK IAW B727 SRM 51-10-1. NDT IAW B727 NDT MAN 51-00-0. FABRICATED ANGLE USING 2024-T3 .040 PO 9002219. DIM.5 3/4"X 4 1/4" IAW B727 SRM 57-50-3 FIG.4 ALODINE AND PRIME IAW B727 SRM 51-10-2, INSTALLED ANGLE IAW B727 SRM 51-40-3 FIG 1. 2L73 4F A3WE 20050622001032005062200103NM 2005 6 22 QXEA200500980 120050410A3411 ODOR DHAV DHC8 DHC8202 2809007NM COCKPIT DETECTED A QXEAO OTHER BW SMOKE/FUMES/ODORS/SPARKS INADEQUATE Q C TXTAXI/GRND HDL 1 NM09352PH 494 STRONG ODOR DETECTED IN COCKPIT. MX FOUND PITOT HEAT 1 AND 2 AND STALL WITH HEAT ON FOR OVER 1 HOUR. SHUT OFF ALL HEAT. INSP PITOT TUBES AND STATIC PORTS. NO DAMAGE NOTED. AIRED OUT FLIGHT COMPARTMENT. NO OTHER PROBLEMS NOTED. ACFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050622001102005062200110SO 2005 6 22 SIMA200515701 120050529A2700 PITCH CONTROL EMB 135 EMB135KL 3260302SO MALFUNCTIONED A SIMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW21811AE 145529 ALB - FLT 4230 - TAKEOFF PITCH TRIM RECEIVED BY CREW DURING TAKEOFF. MAINTENANCE COMPLIED WITH OPERATIONAL CHECK IAW EMB MM AND COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050622001292005062200129SO 2005 6 22 SIMA200514305 120050521A3220 STRUT EMB 135 EMB135LR 3260305SO NLG DISCHARGED A SIMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21730KW 145346 BGR - FLT 4505 - DURING TAKEOFF, CREW REPORTED, THE LANDING GEAR WOULD NOT RETRACT ALSO RECEIVED LANDING GEAR AIR GROUND FAIL ON EICAS. MAINTENANCE SERVICED THE NOSE LANDING GEAR SHOCK STRUT IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050622001312005062200131SO 2005 6 22 SIMA200514303 120050517A491014526850401 FIREWALL EMB 135 EMB135KL 3260302SO APU BAY CRACKED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21852AE 145736 SAW - DURING AN MBV INSPECTION, MAINTENANCE FOUND THE APU FIREWALL TO BE CRACKED AROUND UPPER RIGHT APU MOUNT PAD. REPAIRED CRACK AROUND APU MOUNT PAD BY INSTALLATION OF A DOUBLER IAW EMB SRM 53-32-13 FIG 202. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050622001322005062200132SO 2005 6 22 SIMA200514302 120050516A521014540853407 SKIN EMB 135 EMB135KL 3260302SO PAX DOOR DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21852AE 145736 TIME DELAY MAINTENANCE ITEM NR 852520147 DENT ON PASSENGER DOOR. REPAIRED DOOR BY INSTALLING DOUBLER IAW EMB SRM 52-10-01 FIGURE 201. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050622001332005062200133SO 2005 6 22 SIMA200509113 120050329A3350110049 BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A SIMAO OTHER O OTHER NRNOT REPORTED 1 SW21655AE 145452 FOUND THE RIGHT OVERWING AND INSIDE CABIN EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED NR 2 AND 4 EMERGENCY BATTERY SUPPLIES IAW EMB 145MM 33-50-04. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20050622001362005062200136SO 2005 6 22 SIMA200513607 120050513A3097 TERMINAL EMB 135 EMB135KL 3260302SO HEAT CONTROLLER BURNED A SIMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21842AE 636 145673 LAX - FLT 3121 - DURING CLIMB, THE FLIGHT ATTENDANT REPORTED A SMOKE ODOR IN THE CABIN. NO VISIBLE SMOKE NOTED. CREW ELECTED TO RETURN TO LAX AND DECLARED EMERGENCY. MAINTENANCE FOUND THE CAUSE TO BE THE NR 1 WINDSHIELD HEAT CONTROLLER TERMINALS WERE BURNED. THE CONTROLLER AND THE TERMINALS WERE REPLACED IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050622001572005062200157EA 2005 6 22 ASOA05427 120050510A5220600313942 BRACKET CNDAIRCL600 CL6002B19 1900309EA EMERGENCY EXIT MISALIGNED A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27867AS 7463 DURING A C-CHECK IN MCN, THE RIGHT EMERGENCY EXIT DOOR FAILED THE FUNCTIONAL TEST. MAINTENANCE ADJUSTED THE DOOR MOUNTING BRACKETS ON THE RIGHT EMERGENCY EXIT. OPERATIONAL CHECKS GOOD. (M) 2L72 4F RTA21EA 20050622001612005062200161EU 2005 6 22 USAA050722 120050522A5320D5347209000200 FLOOR SUPPORT AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19717UW 1069 PIT - FOUND FLOOR SUPPORT CORRODED 1 INCH DIAMETER AREA, FLOOR SUPPORT AT Y765 AND C-66. CORROSION LEVEL 2, TASK JA-260-53500. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-72-11. (M) 2L72 4F RTA28NM 20050622001632005062200163EA 2005 6 22 ASOA05429 120050511A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27915EV 7754 DURING AN OVERNIGHT SERVICE CHECK IN CAE, THE EMERGENCY EXIT LIGHT BY THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMPS IN THE EMERGENCY EXIT LIGHT BY THE SERVICE DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050622001642005062200164EA 2005 6 22 ASOA05426 120050503A5220600313942 BRACKET CNDAIRCL600 CL6002B19 1900309EA EMERGENCY EXIT MISALIGNED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27867AS 7463 DURING A C-CHECK IN MCN, THE LEFT EMERGENCY EXIT DOOR FAILED THE FUNCTIONAL TEST. MAINTENANCE ADJUSTED THE DOOR MOUNTING BRACKETS ON THE LEFT EMERGENCY EXIT. OPS CHECKS GOOD. (M) 2L72 4F RTA21EA 20050622001652005062200165EA 2005 6 22 ASOA05449 120050519A5210 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27854AS 7382 DURING A GROUND INSPECTION IN ATL, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050622001672005062200167SO 2005 6 22 SIMA200515101 120050525A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21812AE 145531 ABI - DURING AN INSPECTION, THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. PERFORMED A CUTOUT AND REMOVED THE CORROSION. FABRICATED A DOUBLER, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB-145/1142 REV 29 CHAPTER 53-21-10 FIGURE 201. (M) 2L72 4F RTT00011AT 20050622001682005062200168EA 2005 6 22 ASOA05425 120050510A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27859AS 7421 DURING A ROUTINE SERVICE CHECK IN CAE, THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE LEFT OVERWING EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050622001712005062200171EA 2005 6 22 ASOA05393 120050502A3350BF10044004 LIGHT CNDAIRCL600 CL6002B19 1900309EA EMERGENCY EXIT CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27839AS 7284 DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY EXIT LIGHT AT THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT AT THE SERVICE DOOR. (M) 2L72 4F RTA21EA 20050622001732005062200173EA 2005 6 22 ASOA05391 120050502A3350 BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27871AS 7537 FLT 4430 - FOLLOWING SHUTDOWN OF THE AIRCRAFT IN ATL, THE CREW RECEIVED AN EMERGENCY LIGHTS ON STATUS MESSAGE WITH THE EMERGENCY LIGHTS N THE ARMED POSITION AND THE FLIGHT ATTENDANTS PANEL IN THE OFF POSITION. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTS BATTERY PACKS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050622001742005062200174EA 2005 6 22 ASOA05432 120050512A291673031 RESERVOIR CNDAIRCL600 CL6002B19 1900309EA NR 3 HYD SYS MALFUNCTIONED A ASOAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO27844AS 7317 DURING TAKEOFF FROM ALT-GPT, UPON RAISING THE GEAR A GEAR UP DISAGREE MESSAGE WAS RECEIVED. THE QRH WAS COMPLIED WITH AND THE AIRCRAFT RETURNED TO ATL, LANDING SAFELY. EMERGENCY EQUIPMENT WAS ON STANDBY AS A PRECAUTION. MAINTENANCE REMOVED AND REPLACED THE NR 3 HYDRAULIC RESERVOIR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050622001752005062200175NM 2005 6 22 USAA050717 120050602A5320 ANGLE BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19445US40360 24863 CLT - FOUND TRANSITION ANGLE CORRODED 1 INCH, RT TRANSITION ANGLE IN AFT CARGO COMPARTMENT STATION 727B-947. FABRICATED AND INSTALLED REPAIR PIECES IAW 737-400 SRM 56-60-53 AND 51-10-02. (M) 2L72 4F RTA16WE 20050622001772005062200177EA 2005 6 22 ASOA05424 120050505A5321 FLOOR PANEL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27849AS 7347 DURING A C-CHECK IN MCN, TH LEFT/RIGHT FLOOR PLANKS AT FS 409 PLUS 128 TO FS 559.00, LBL 36 AND RBL 36 IAW ASA EO 600-53-0257. (M) 2L72 4F RTA21EA 20050622001782005062200178EU 2005 6 22 ASOA05423 120050509A33503011162 COVER AEROSPATR72 ATR72 EU EMERGENCY LIGHT WORN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27630AS 336 FLT 4094 - DURING A GROUND INSPECTION IN ATL, THE EXIT SIGN BY THE RIGHT FRONT EMERGENCY DOOR COULD NOT BE READ. MAINTENANCE REMOVED AND REPLACED THE COVER ON THE EXIT SIGN BY THE RIGHT FRONT EMERGENCY DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20050622001812005062200181EA 2005 6 22 ASOA05440 120050515A3350 LIGHT CNDAIRCL600 CL6002C10 1390015EA PAX DOOR HANDLE INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27701EV 10020 FLT - 4832 - DURING A GROUND INSPECTION IN SLC, THE EMERGENCY EXIT PLACARD ON THE PASSENGER DOOR HANDLE WAS FOUND NOT TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT BETA LIGHT ON THE PASSENGER DOOR HANDLE. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050622001822005062200182EA 2005 6 22 ASOA05439 120050514A3350 BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27871AS 7537 FLT 4201 - DURING A GROUND INSPECTION IN ATL, THE EMERGENCY LIGHTS REMAINED ON WHEN IN THE ARMED OR OFF POSITIONS. MAINTENANCE REMOVED AND REPLACED ALL FOUR OF THE EMERGENCY LIGHT BATTERY PACKS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050622001842005062200184EA 2005 6 22 ASOA05454 120050521A3260864808 PSEU CNDAIRCL600 CL6002B19 1900309EA MLG MALFUNCTIONED A ASOAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27830AS 7236 DURING TAKEOFF FROM CVG-MSG, THE NOSE GEAR FAILED TO RETRACT AND A GEAR DISAGREE WARNING MESSAGE WAS RECEIVED. THE CREW LEVELED THE AIRCRAFT OFF AT 4,000 FEET TO COMPLY WITH THE QRH AND DECLARED AN EMERGENCY. THE AIRCRAFT RETURNED TO CVG AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE PROXIMITY SENSOR ELECTRONIC UNIT (PSEU). OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050622001862005062200186EA 2005 6 22 ASOA0544 120050517A3350 LENS CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27867AS 7463 DURING A C-CHECK IN MCN, THE BASE AND LENS ON THE EMERGENCY EXIT LIGHT BY THE SERVICE DOOR WERE FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY BY THE SERVICE DOOR. OPS CHECKS GOOD. (M) 2L72 4F RTA21EA 20050622001872005062200187EA 2005 6 22 ASOA05421 120050508A5310 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27867AS 7463 DURING A C-CHECK IN MCN, THE ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW ASA EO 600-53-0072B. (M) 2L72 4F RTA21EA 20050622001892005062200189EA 2005 6 22 ASOA05434 120050514A5210601R319085 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27876AS 7576 DURING A GROUND INSPECTION IN ATL, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050622001922005062200192EA 2005 6 22 ASOA05420 120050508A5340601R950159 BRACKET CNDAIRCL600 CL6002B19 1900309EA RAM AIR DUCT CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27867AS 7463 DURING A C-CHECK IN MCN, THE RAM AIR SPIDER DUCT UPPER BRACKET IN THE AFT EQUIPMENT BAY WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RAM AIR SPIDER DUCT UPPER BRACKET IN THE AFT EQUIPMENT BAY. (M) 2L72 4F RTA21EA 20050622001932005062200193EA 2005 6 22 ASOA05417 120050506A1430 FASTENER CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27849AS 7347 DURING A C-CHECK IN MCN, THE FASTENERS UNDER THE CABIN FLOORBOARD AT FS 333 APPROXMATELY RBL 7-9 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FASTENERS UNDER THE CABIN FLOORBOARD AT FS 333, APPROXIMATELY RBL 7-9 IAW CRJ SRM 51-42-00. (M) 2L72 4F RTA21EA 20050622001952005062200195EA 2005 6 22 ASOA05413 120050508A335020131ASI BATTERY PACK CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT DISCHARGED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27703EV 10038 DURING HANGAR MAINTENANCE IN BTR, THE RIGHT EXTERIOR OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHTS BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050622001972005062200197EA 2005 6 22 ASOA05409 120050507A52101170715 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR DAMAGED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27820AS 7188 FLT 4475 - DURING A GROUND INSPECTION IN MLU, THE FLIGHT ATTENDANT HAD DIFFICULTY CLOSING THE PASSENGER DOOR AND DURING TAKEOFF FROM MLU-ATL A PASSENGER DOOR HANDLE EICAS MESSAGE WAS RECEIVED. THE FLIGHT CONTINUED AND AFTER LANDING SAFELY IN ATL, THE FLIGHT ATTENDANT HEARD A LOUD BANG WHEN THE PASSENGER DOOR WAS UNLOCKED. MAINTENANCE REPAIRED THE PASSENGER DOOR HANDLE, LOCK MECHANISM AND ADJUSTED THE DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050622001982005062200198EA 2005 6 22 ASOA05415 120050508A34110856KV10 PITOT TUBE CNDAIRCL600 CL6002B19 1900309EA AIRSPEED CLOGGED A ASOAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 SO27848AS 7339 DURING TAKEOFF FROM ATL-HOU, THE FIRST OFFICERS AIRSPEED INDICATOR FAILED AND DURING CLIMB-OUT THE CREW RECEIVED STALL FAIL AND MACH TRIM MESSAGES FOLLOWED BY A YAW DAMP 1 INOPERATIVE MESSAGE. THE QRH WAS COMPLIED WITH WITHOUT THE MESSAGES CLEARING. AIRCRAFT HANDLING DEGRADED WITH NO FLIGHT CONTROL FAILURES. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO ATL, LANDING SAFELY. MAINTENANCE FOUND THE RIGHT PITOT TUBE HEAD CLOGGED WITH REMAINS FROM A BIRD STRIKE. NO DAMAGE WAS NOTED TO THE PITOT TUBE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050622001992005062200199EA 2005 6 22 ASOA05414 120050508A335058728 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27873AS 7549 DURING HANGAR MAINTENANCE IN MCN, AN EMERGENCY FLOOR LIGHT STRIP WAS FOUND CRACKED IN SEVERAL LOCATIONS. MAINTENANCE REMOVED AND REPLACED AN EMERGENCY FLOOR LIGHT STRIP IAW CRJ AMM 25-80. (M) 2L72 4F RTA21EA 20050622002022005062200202EA 2005 6 22 MASA200500226 120050317A2150 A/C PACK CNDAIRCL600 CL6002B19 1900309EA ODOR A MASAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW0717217 7217 ASH 7106 CAE TO IAD RETURNED TO FIELD DUE TO AN ODOR OF SMOKE IN CABIN ASSOCIATED WITH A PACK TEMP OVERHEAT. MAINTENANCE CONFIRMED THE DISCREPANCY IN THE PACK AND COMPLIED WITH MEL. 3/17/05 MAINTENANCE COULD NOT DUPLICATE, NO FURTHER DEFECTS NOTED. 2L72 4F RTA21EA 20050622002052005062200205EA 2005 6 22 MASA200500231 120050318A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS OUT OF RIG A MASAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW0727314 7314 ASH 6930 FROM OKC TO PHX. CREW RETURNED TO THE FIELD AS INSTRUCTED FOR AILERON TRIM NEEDS 1/2 SCALE DELECTION RT WING DOWN TO MAINTAIN LEVEL FLIGHT. AAR MAINTENANCE RERIGGED FLAP AND CREW PERFORMING TEST FLIGHT. 2L72 4F RTA21EA 20050622002062005062200206CE 2005 6 22 71323 120050616A3242 BRAKE ASSY BEECH 1900 1900D 1154162CE LEFT MALFUNCTIONED A AMWAO OTHER O OTHER LDLANDING 1 CE07161YV UE161 ON LANDING IN LWB LEFT BRAKE WAS WEAK. MAINTENANCE BLED THE BRAKES. THEREFORE NO PARTS WERE USED. 2L72 4T RTA24CE 20050622002072005062200207 2005 6 22 71331 420050616A3100 WARNING LIGHT BEECH 1900 1900D 1154162CE COCKPIT FALSE ACTIVATIONA AMWAD RETURN TO BLOCK GJ MULTIPLE FAILURE WARNING INDICATION TXTAXI/GRND HDL 1 CE07167YV UE167 TAXIED INTO GATE WHEN MASTER WARNING FLASHER ILLUMINATED INDICATING FIRE IN RT ENG. FIREWALL FUEL VALVE WAS ILLUMINATED. DECLARED AN EMERGENCY, ACCOMPLISHED APPROPRIATE CHECKLISTS & CONDUCTED AN ORDERLY DEBARKATION WHILE DIRECTING PASSENGERS AWAY FROM PLANE. DFW GROUND OPS THEN COORDINATED THE TRANSPORTATION OF PASSENGERS AND FLIGHT CREW TO THE GATE AREA. THERE WERE NO INJURIES TO ANY PASSENGERS OR CREW AND THE PLANE WAS TOWED TO THE GATE AREA FOR MAINTENANCE INSPECTION. MAINTENANCE RINSED THE ENGINE, INSPECTED AND FOUND NO DEFECTS THAT WERE NOTED. UNABLE TO DUPLICATE THE WRITE UP, BUT REMOVED AND REPLACED THE FIRE BOTTLE. 2L72 4T RTA24CE 20050622002082005062200208EA 2005 6 22 MASA200500101 120050211A3230750005000 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA MLG MALFUNCTIONED A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07571ML2221 7209 ASH 2725 FROM PHL TO BGM RETURNED TO THE FIELD DUE TO A GEAR DISAGREE. MAINTENANCE IS IN THE PROCESS OF TROUBLESHOOTING. MAINTENANCE REMOVED AND REPLACED THE SELECTOR VALVE, OPS CHECKED GOOD. 2L72 4F RTA21EA 20050622002102005062200210EA 2005 6 22 MASA200500126 120050217A3260 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA MLG ICED A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0777181 7181 ASH 2839 YUL RETURNED TO THE FIELD IN YUL FOR A NOSE GEAR THAT WOULD NOT RETRACT. MAINTENANCE FOUND THE NOSE GEAR COVERED WITH ICE. MAINTENANCE IS NOW IN THE PROCESS OF REMOVING THE ICE AND PERFORMING A GEAR SWING. 2/17/05 MAINTENANCE ADJUSTED THE PROX SENSOR AND OPS CHECK GOOD. 2L72 4F RTA21EA 20050622002112005062200211EA 2005 6 22 MASA200500127 120050217A32304622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG FAILED A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07771819918 7181 ASH 9430 YUL - PHL, CAPT RETURNED TO THE FIELD DUE TO NOSE GEAR WOULD NOT RETRACT. MAINTENANCE IS TROUBLESHOOTING. MAINTENANCE REMOVED AND REPLACED PRIORITY VALVE AND SERVICED THE STRUT. 2L72 4F RTA21EA 20050622002162005062200216NM 2005 6 22 0500896316 120050610A2530 CONTROL PANEL BOEING747 747451 1384940NM GALLEY SPARKS A NWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL01676NW 33002 WHILE INBOUND TO JFK, FLIGHT ATTENDANT REPORTED U/D OVEN 1-29 RUNS TOO HOT, SPARKS AND SMOKE WERE SEEN COMING FROM CONTROL PANEL. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. JFK MAINTENANCE REPLACED OVEN AND RESEATED RELAY. OPERATIONAL CHECKS NORMAL. 2L74 4F RTA20WE 20050622002182005062200218WP 2005 6 22 ABXA050152 120050615A2133 OUTFLOW VALVE DOUG DC9 DC932 3022066WP CABIN PRESSURE FROZEN A ABXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL23900AX 47380 AT 35,000 FEET, RED CABIN PRESS LIGHT ILLUMINATED AND OUTFLOW VALVE WAS FROZEN IN PLACE. ONCE DESCENDED TO FL 190, PRESSURIZATION WORKED OKAY IN MANUAL AND AUTO. OPS CHECKED CABIN PRESS SWITCH IAW DC-9 MM 21-30-00-0-0202. OPS NORMAL, NO DEFECTS NOTED. THIS PROBLEM OCCURRED OUT OF LAS EN ROUTE TO ILN. FOLLOWING THE PROBLEM, THE CREW DID NOT HAVE THE REQUIRED FUEL TO MAKE IT TO ILN. FLIGHT CONTROL AIR DIVERTED FLIGHT 115 TO SGF FOR FUEL. 2L72 4F A6WE 20050622002222005062200222NM 2005 6 22 DHL2005741534 120050421A5311 FRAME BOEING727 7272Q9 138448MNM FUSELAGE BENT A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH46665 21931 FRAME BENT AT FS 660 STR 24R. FOUND DENT TO BE OUT OF LIMITS ON STA 660 STR 24R IAW B727 SRM 53-10-1 FIG1. CUT OUT AREA OF FRAME DIM 1 X 8 IAW B727 SRM 51-40-3 FIG 1. FABRICATED ANGLE REPAIR FROM 7075 T6 .071 SIZE 16 X 3 PO NR 900573 AND FILLER FROM 7075 T6 .063 SIZE 1 X 8 PO 9001660 IAW B727 SRM 51-40-3 FIG1. TREATED AND PRIMED PARTS AND AREA IAW B727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B727 SRM 51-40-3 FIG 1. 2L73 4F RTA3WE 20050622002232005062200223NM 2005 6 22 DHL2005741535 120050418A5720 STIFFENER BOEING727 7272Q9 138448MNM RT WING BULGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH46665 21931 VERTICAL STIFFENER AT RT WING WBL 92 BULGED AT LOWER END. REMOVED DAMAGED EXISTING DOUBLER ON VERTICAL STIFFENER AT R/W WBL 92 IAW B727 SRM 51-10-2. FABRICATED REPAIR DOUBLER FOR VERTICAL STIFFENER AT RT WING WBL 92 DIM 8.750 BY 2.125 MAT ID 7075T-6 .071 PO NR 900573 IAW 727 SRM 57-10-2 FIG 3 AND 51-40-3 FIG 1. TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-10-2. INSTALLED DOUBLER ON VERTICAL STIFFENER AT R/W WBL 92 IAW B727 SRM 51-30-2 AND 51-40-3 FIG 1. 2L73 4F RTA3WE 20050622002252005062200225NM 2005 6 22 DHL2005741539 120050519A5542 SKIN BOEING727 7272Q9 138448MNM RUDDER CHAFED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH46665 21931 LWR RUDDER UPPER WEB FASTENERS AND SKIN CHAFED RUDDER STA 152. DAMAGED TO LWR RUDDER UPPER WEB FOUND TO BE OUT OF LIMITS IAW B727 SRM 55-40-1 FIG 1. REMOVED WEB ON LWR RUDDER UPPER WEB IAW B727 SRM 51-30-2. FABRICATED WEB FROM 2024 T3 .040 SIZE 14.500 X 14.750 PO 9002297 IAW B727 SRM 55-40-2 FIG 2. TREATED AND PRIMED PART AND AREA IAW B727 SRM 51-10-2. INSTALLED WEB IAW B727 51-30-2. 2L73 4F RTA3WE 20050622002262005062200226NM 2005 6 22 DHL2005741540 120050421A5531 STRINGER BOEING727 7272Q9 138448MNM VERTICAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH46665 21931 VERT STAB FIN STA 180 STRGR 8LT IS CRACKED AT FRAME ATTACH BOLT. REMOVED FASTENERS IN VERTICAL STAB FIN STA 180 STR 8LT IAW B727 SRM 51-30-2. CUT OUT DAMAGED AREA 2.0625 X 1.0625 IAW B727 55-30-5 FIG 1. FABRICATED REPAIR PARTS AS FOLLOWS FILLER FROM FROM 7075T6 .063 PO NR 501952 DIM 2.6875 X 1.0625 AND ANGLE REPAIR FROM 7075T6 .071 PO NR 9002118 DIM 11.125 X 1.375 X 1.125 IAW B727 SRM 55-30-5 FIG 1. TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B727 SRM 53-30-5 FIG 1 AND 51-30-2. 2L73 4F RTA3WE 20050622002302005062200230WP 2005 6 22 DHL2005807544 120050525A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH86990 45990 RT EXTERNAL SKIN CORRODED STA 1395.000 L-34R - 35R. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS. CUT OUT DAMAGED SECTION, PERFORMED DETAIL VISUAL INSP NO CRACK FOUND. FABRICATED EXTERNAL REPAIR DOUBLER, 16 EA INTERNAL REPAIR FINGER DOUBLER, 12EA INTERNAL REPAIR STRAPS (AL7075T6 0.125) AND NEW SKIN SECTION IAW BOEING ROD SKETCH 05-05-02-002, CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED PRC TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW ROD SKETCH BOEING 05-05-02-002, ED SEMAN 3945-2, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050622002312005062200231WP 2005 6 22 DHL2005807539 120050516A532037517372SP STRAP DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH86990 45990 STRAP AT RT UPPER CORNER OF RT MLG WW CORRODED, STA 857.000 RBL 69.500. REMOVED CORROSION FROM STRAP AT RT UPPER CORNER OF RT MLG WW STA 857.000 RBL 69.500 IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED STRAP IAW SRM 51-1-20D PG 21. FABRICATED NEW STRAP (AL7075T-6 51) IAW JC EA53100128-001-D, EA05917 AND DWG 3751737. PERFORMED NDT INSP IAW NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED AREA AND NEW STRAP IAW SRM 51-1-8B. INSTALLED NEW STRAP IAW SRM 51-1-20D PG 21. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050622002322005062200232WP 2005 6 22 DHL2005807540 120050517A534037504971 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH86990 45990 AFT ACCY COMPT FRAME FITTING 1.000 CRACK APRROX STA 660.000-670.000, L-35 TO L-36L. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 JC EA53100129-001-D, EA05918, DWG 3750497. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. FABRICATED NEW FITTING IAW EA05918, DWG 3750497. PERFORMED NDT INSP IAW NDT SPM PART 08-00-02 TO 07. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 21, SRM 51-1-21 PG.1, SRM 51-3-0 PG 1. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050622002332005062200233WP 2005 6 22 DHL2005807543 120050525A53205616674 INTERCOSTAL DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH86990 45990 INTERCOSTAL CHANNEL CORRODED STA 1400.000-1420.000, L-34R AFT ACCY COMPT. REMOVED CORROSION FROM INTERCOSTAL CHANNEL IN AFT CARGO COMPT. (STA 1400.000-1420.000,L-34R) IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CHANNEL IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. FABRICATED NEW CHANNEL IAW DWG 5616674. HEAT TREATED IAW SRM 51-1-1 PG 13-17. CLEANED, TREATED AND PRIMED AREA AND NEW CHANNEL IAW SRM 51-1-8B. INSTALLED NEW CHANNEL IAW SRM 51-1-21 PG. 1, SRM 51-1-20D PG 9, SRM 51-1-11. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050622002352005062200235NM 2005 6 22 DHL2005741536 120050414A57116516201185 SPAR BOEING727 7272Q9 138448MNM FUSLEAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH46665 21931 LEFT WING REAR SPAR WBL124 CORROSION AT ATTACH CLIP TO LOWER SPAR (FWD OF APU BOTTLE DISCHARGE LINE). REMOVED AND RERPLACED T FITTING P/N 65-16201-185 PO NR 3348293 IAW B727 SRM 51-30-2 AND 57-10-2 FIG 3. 2L73 4F RTA3WE 20050622002392005062200239NM 2005 6 22 DHL2005741542 120050428A5315150529222 FLOORBEAM BOEING727 7272Q9 138448MNM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH46665 21931 COCKPIT FLOORBEAM HAS LIGHT SURFACE CORROSION AT BS 290 BL0. REMOVED CORROSION AT BS294 BL0 DAMAGED SPREAD FROM LBL24 AND RBL24 MAT, LOSS IS MORE THAN 40 PERCENT AND IS OUT IS OUT OF THE ALLOWABLE LIMITS OF 10 PERCENT CROSS SECTION IAW B727 SRM 53-10-1 FIG 1. REMOVED T ANGLE CUT OUT DAMAGED SECTION AT BS 294 FROM LBL 15 - RBL15 IAW 727 SRM 53-10-8 FIG 1 LOCATED AND DRILLED NEW PART FROM LBL15-RBL15 IAW B727 SRM 53-10-8 FIG 1. TREATED AND PRIMED T ANGLE AND AREA IAW B727 SRM 53-10-2. INSTALLED T SECTION IAW B727 SRM 53-10-8 FIG 1. 2L73 4F RTA3WE 20050622002412005062200241NM 2005 6 22 DHL2005784505 120050515A5754 SKIN BOEING727 727227 1384078NM NR 6 SLAT DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01784DH 22001 RT WING, DENT IN NR 6 L/E SLAT AT WS 491 ON L/E. FOUND DENT OUT OF LIMITS IAW B727 SRM 57-50-1 FIG 2. CUT OUT DAMAGED SKIN IAW B727 SRM 57-50-3 AND INNER SKIN FOR ACCESS. CUT OUT SKIN DIM 10" BY 5" IAW B727 SRM 57-50-3 FIG 1. FAB PART FOR OUTER SKIN REPAIR, FILLER, FAB OUTER SKIN, FILLER STRIP IAW B727 SRM 57-50-3 FIG 1. ALODINE AND PRIMED IAW B727 SRM 51-10-2. INSTALLED PARTS IAW B727 SRM 57-50-3. 2L73 4F A3WE 20050622002432005062200243NM 2005 6 22 DHL2005784507 120050516A5753 SKIN BOEING727 727227 1384078NM LT WING FLAP GOUGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01784DH 22001 LT WING INBD FORE FLAP OUTBD END IS GOUGED BY LONG SCREW, WBL 240. FOUND AREA OUT OF LIMITS. REPAIRED IAW SRM. 2L73 4F A3WE 20050622002442005062200244NM 2005 6 22 DHL2005741544 120050418A5754 SKIN BOEING727 7272Q9 138448MNM LE SLAT DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH46665 21931 DENT WAS EVALUATED AND FOUND BEYOND ALLOWABLE LIMITS IAW B727 SRM 57-50-1 FIG 2. REPAIRED IAW SRM. 2L73 4F RTA3WE 20050622002502005062200250NM 2005 6 22 DHL2005784513 120050518A5311 FRAME BOEING727 727227 1384078NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01784DH 22001 STA 700 FRAME IS DENTED ABOVE STR 4R. FOUND DENT TO BE OUT OF LIMITS. REPAIRED IAW SRM. 2L73 4F A3WE 20050623000032005062300003WP 2005 6 23 AALA20050383 120050611A3242 BRAKE DOUG DC9 DC982 3022082WP MLG FIRE A AALAO OTHER A FLAME/FIRE TXTAXI/GRND HDL 1 SW217536A 49990 YYZ - TAXI T564 AFTER TURNING OFF RUNWAY NR 2 MAIN LANDING GEAR BRAKE TEMPERATURE LIGHT ILLUMINATED. CAPTAIN REQUESTED MAINTENANCE AND FIRE RESCUE. ON ARRIVAL FOUND SMALL BRAKE FIRE. FIRE WAS EXTINGUISHED. AIRCRAFT WAS EVACUATED THROUGH TAIL SLIDE. ONE MINOR INJURY REPORTED. AIRCRAFT WAS MOVED TO GATE. REPLACED NR 2 MAIN LANDING GEAR BRAKE, NR 1 AND 2 MAIN LANDING GEAR WHEEL ASSEMBLY AND ACCOMPLISHED INTERIM REPAIR TO TAILCONE PER SRM. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050623000052005062300005EA 2005 6 23 SWIA200515143 120050616A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07445SW 7651 CEILING LEVEL EMERGENCY FLOODLIGHT A BEAM ROW 10 IS INOPERATIVE. RELAMPED IAW CRJ 200 AMM 33-51-16. 2L72 4F RTA21EA 20050623000082005062300008EA 2005 6 23 MASA200500386 120050523A3230750006000 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07271854123 7185 ASH 2912 BTV TO PHL. THE CAPTAIN RETURNED TO THE FIELD FOR A GEAR DISAGREE MESSAGE WITH NO GEAR RETRACTION. ON CALL MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND IT OK TO FERRY. THE AIRCRAFT FERRIED TO PHL WHERE MAINTENANCE REPLACED THE NWS SELECTOR VALVE. 2L72 4F RTA21EA 20050623000102005062300010EA 2005 6 23 MASA200500396 120050525A5210 LANYARD CNDAIRCL600 CL6002B19 1900309EA PAX DOOR TANGLED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0737178 7178 ASH 6041 PHX. THE CREW REPORTED THAT THE PASSENGER DOOR WAS DIFFICULT TO OPEN. MAINTENANCE FOUND A LANYARD IN THE HANDLE ROLLER. REMOVED LANYARD AND OPERATIONS WERE NORMAL. 2L72 4F RTA21EA 20050623000122005062300012EA 2005 6 23 MASA200500404 120050505A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0777195 7195 ASH 2658 PHL TO CLE. THE CREW NOTED THAT THE AFT EMERGENCY EXIT FLOOD LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED AFT EMERGENCY EXIT FLOOD LIGHT BULB AND OPS CHECKED NORMAL. 2L72 4F RTA21EA 20050623000132005062300013NM 2005 6 23 05FDEA01441 120050524A5753 DOUBLER DOUG MD11 MD11 3023602NM LT TE FLAP MISINSTALLED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25631FE 48454 LT INBOARD FLAP LOWER SIDE INBOARD SEGMENT XIFH 183.30/201.30 RIVETS INSTALLED ON EXISTING SHARP NICKS. LT INBOARD FLAP INBOARD SEGMENT LOWER SIDE DAMAGE AREA FASTENERS. REMOVED AND SKIN TRIMMED. REPAIR SKIN AND 02 EACH SPLICE DOUBLER FABRICATED AND INSTALLED AS PER SRM 57-10-00 FIG 2 VOL I AND 51-35-01 VOL II. MATERIAL USED AS PER DWG ARC 2736. MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050623000152005062300015NM 2005 6 23 05FDEA01611 120050615A5512 SKIN BOEING727 727200 138407ENM HORIZONTAL STAB DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25477FE 21394 LEFT HORIZONTAL STAB UPPER SURFACE HAS DENT WITH GOUGE 17.5 INCHES FROM I/B END AND 16.5 INCHES FROM AFT END. REPAIRED PER FED EX EA 7-5510-86317. 2L73 4F RTA3WE 20050623000162005062300016NM 2005 6 23 05FDEA01612 120050616A5531 STRINGER BOEING727 727200 138407ENM VERTICAL STAB CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25477FE 21394 CRACKED STRINGER INSIDE VERTICAL STAB AT STRINGER 7 FIN STATION 157.2 LT. REPAIRED STRINGER PER SRM 55-30-4 FIG 1. 2L73 4F RTA3WE 20050623000182005062300018NM 2005 6 23 05FDEA01615 120050617A5753 TEE FITTING DOUG MD11 MD11 3023602NM LT WING TE FLAP WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25631FE 48454 LT WING I/B FLAP ASSY I/B SEGMENT APPROX ALONG STA XIFH 207.30 FOUND TEE FITTING WORN. REMOVED AND REPLACED AS PER SRM 51-35-01 VOL II & DRAWING ARC 2482 FABRICATE NEW TEE SUPPORT. 2L73 4F RTA22WE 20050623000192005062300019EA 2005 6 23 MASA200500412 120050528A5270 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA PAX DOOR MALFUNCTIONED A MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW0737178 7178 PAX DOOR WARNING MSG. R2 PS1B & PS2MB HANDLE PROX SENSORS. 2L72 4F RTA21EA 20050623000212005062300021EA 2005 6 23 MASA200500440 120050604A5210 LOCK CNDAIRCL600 CL6002B19 1900309EA PAX DOOR OBSTRUCTED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0737178 7178 ASH 6022 FAT. MAIN CABIN DOOR THAT WAS DIFFICULT TO OPEN. MX REMOVED DEBRIS FROM DOOR LOCKING MECHANISM AND LUBED DOOR. 2L72 4F RTA21EA 20050623000232005062300023EA 2005 6 23 MASA200500457 120050610A2750 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07652ML 7036 ASH FLT 2787 CLT RETURNED TO FIELD DUE TO THE FLAPS FAILED AT 8 DEGREES. MAINTENANCE REMOVED AND REPLACED THE RT BPSU AND FECU. 2L72 4F RTA21EA 20050623000252005062300025EA 2005 6 23 MASA200500408 120050524A3230 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA MLG MALFUNCTIONED A MASAO OTHER J WARNING INDICATION CLCLIMB 1 SW0727185 7185 ASH 2742 DTW TO PHL. THE CREW REPORTED GEAR DISAGREE AFTER TAKEOFF. THE AIRCRAFT LANDED UNEVENTFULLY IN PHL WHERE MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL. 2L72 4F RTA21EA 20050623000272005062300027EA 2005 6 23 MASA200500428 120050601A5270 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA PAX DOOR ILLUMINATED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW0737178 7178 ASH 6491 BFL. THE CREW HAD A PAX DOOR WARNING MESSAGE IN FLIGHT. MX SHIMMED THE DOOR LATCH TORQUE TUBE AND ADJUSTED THE PROX SENSOR STRIKER TORQUE TUBE. THE AIRCRAFT WAS TEST FLOWN AFTER THE REPAIR. THE TEST FLIGHT WAS SATISFACTORY. 2L72 4F RTA21EA 20050623000292005062300029NM 2005 6 23 72300206 120050418A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 20 X 3 INCH AREA OF CORROSION ON STRINGER. 2L73 4F4 FRTA3WE E2EA 20050623000302005062300030NM 2005 6 23 72300207 120050426A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 8 X 2 INCH AREA OF CORROSION ON STRINGER. 2L73 4F4 FRTA3WE E2EA 20050623000312005062300031NM 2005 6 23 72300208 120050426A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 6 INCH AREA OF CORROSION ON STRINGER. 2L73 4F4 FRTA3WE E2EA 20050623000322005062300032NM 2005 6 23 72300209 120050504A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 8 X 3 INCH AREA OF CORROSION ON STRINGER. 2L73 4F4 FRTA3WE E2EA 20050623000332005062300033NM 2005 6 23 72300210 120050517A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CRACKED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 INCH CRACK ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050623000342005062300034NM 2005 6 23 72300211 120050517A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CRACKED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 2.5 INCH CRACK ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050623000392005062300039SO 2005 6 23 CHQA200500116 120050618A335078812 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11570RP 14500821 EMERGENCY FLOOR PROXIMITY LIGHT STRIP IS INOP. REMOVED AND REPLACED NR 4 EMERGENCY FLOOR PROXIMITY LIGHT STRIP IAW EMB 145 AMM 33-50-12. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050623000402005062300040SO 2005 6 23 CHQA200500117 120050620A335066368 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11260SK 145128 FLOOR PROXIMITY LIGHT AT POSITION NR 8 WILL NOT ILLUMINATE. REMOVED AND REPLACED FLOOR PROXIMITY LIGHT IAW EMB AMM 33-50-00. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050623000412005062300041SO 2005 6 23 CHQA200500114 120050616A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11257JQ 14500812 RIGHT HAND OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB IAW EMB 145 AMM 33-50-09. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050623000422005062300042SO 2005 6 23 CHQA200500115 120050617A33503025103 LIGHT EMB 145 EMB145LR 3260212SO LT OVERWING INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11276SK 145348 LEFT HAND OVERWING EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED LIGHT ASSEMBLY IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050623000432005062300043SO 2005 6 23 CHQA200500118 120050620A2611FDS765A2 SMOKE DETECTOR EMB 145 EMB145MP 3260216SO LAVATORY DIRTY A CHQAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL11975RP 145337 FLIGHT 3409 LGA-ILM - AFTER LEVELING OFF AT FL 340, THE FLIGHT ATTENDANT REPORTED THE LAV SMOKE DETECTOR HAD ACTIVATED. THE LAV APPEARED TO BE NORMAL WITH NO SMOKE NOTED. THERE WAS NO WARNING MESSAGE IN THE COCKPIT. THE ALARM STOPPED AFTER A FEW MINUTES AND THEN STARTED BACK UP AGAIN. THE FLIGHT DIVERTED INTO ORF AND LANDED WITHOUT EVENT. MAINTENANCE INSPECTED THE LAV SMOKE DETECTOR AND REMOVED A LARGE AMOUNT OF DUST FROM THE DETECTOR. THE LAV SMOKE DETECTOR WAS TESTED AND OPS CHECKED GOOD. THE FLIGHT CONTINUED TO ILM WITHOUT PROBLEMS. 2L72 4F RTT00011AT 20050623000442005062300044EA 2005 6 23 5336003 120050615A2697 WIRE CNDAIRCL600 CL6002B16 1900305EA OVERHEAT DETECT CHAFED E ERYAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE07212RR7102 5336 DURING CLIMBOUT THRU 34,000 FT, OBSERVED AN INTERMITTENT JET PIPE OVERHEAT WARNING ILLUMINATION. MADE DECISION TO RETURN TO DEPARTURE AIRPORT FOR FURTHER TROUBLESHOOTING. MECHANIC TROUBLESHOT SYSTEM WITH NO APPARENT FAULTS NOTED AND COULD NOT DUPLICATE ERRONEOUS INDICATION OF JET PIPE OVERHEAT. DECISION WAS MADE TO RE-LOCATE A/C TO HIGHER MX FACILITY FOR THOROUGH TROUBLESHOOTING. MX FOUND CHAFING WIRE BUNDLE CAUSING INTERMITTENT SHORTING OF SYSTEM. RE-INSULATED WIRE AND REPLACED CLAMP. OPS CHECK SYSTEM SATISFACTORY AND FOUND NO SUBSEQUENT PROBLEMS ON NEXT FLIGHT. THIS SDR IS SUBMITTED AS A FOLLOW-UP TO ORIGINAL SQUAWK WHERE FIRE LOOP WAS REPLACED ON 6/14/05 AND INTERMITTENT WARNING INDICATION FOLLOWED. 2L72 4F RTA21EA 20050623000452005062300045 2005 6 23 SWAA051826 420050621A2565NAS60222P SCREW BOEING737 7373H4 1384600NM R2 DOOR SLIDE WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE CABLE HARDWARE WORN. REMOVED AND REPLACED HARDWARE PER MM. 2L72 4F RTA16WE 20050623000482005062300048WP 2005 6 23 ASMF200505031 120050530A3230392491 SERVO VALVE DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE LT SIDE FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23204AM108112200 49404 AIRCRAFT RETURNED TO PLATFORM DURING TAXING, AFTER AUTO BRAKES WERE ARMED TO TAKEOFF, ALL THE ANTISKID LIGHTS TURNED ON AND THE CIRCUIT BREAKERS POPPED OUT. TECH REMOVED AND INSTALLED THE AUTO BRAKE BOX AND DURING BRAKE VALVES CHECK WAS DETECTED THAT WHEN THE LT EXTERNAL VALVE WAS DISCONNECTED THE EXTERNAL THE LIGHT TURNED ON. LT DUAL SERVO VALVE WAS REPLACED IAW MM 32-43-03, TESTED CORRECT. AIRCRAFT WAS SENT FERRY IAW MGM 4-14-1 WITH ANTI-SKID SYSTEM INOPERATIVE. WIRING WAS CHECKED FROM ANTI-SKID CONTROL TO CONTROL VALVE IAW WDM 32-41-00 AND TESTS WERE PERFORMED IAW MM 32-43-00, ALL CORRECT. 2L72 4F4 FRTA6WE E9NE 20050623000492005062300049WP 2005 6 23 ASMF200506001 120050602A2750 SWITCH DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE TE FLAPS OUT OF ADJUST W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23751RA 49779 AIRCRAFT RETURNED TO PLATFORM, DEPLOYED SPOILER LIGHT DID NOT COME ON DURING FLIGHT CONTROLS TESTS. AIRCRAFT WAS DISPATCHED AND RETURNED TO PLATFORM, TAKE OFF FAILED. AIRCRAFT SENT TO THE HANGAR AND THE SWITCH S1-492 CAM IN FLAPS ADJUSTED IAW MM 27-53-01, TESTED CORRECT. 2L72 4F4 FRTA6WE E9NE 20050623000512005062300051NM 2005 6 23 ASMF200506003 120050602A4960729825J IDG BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE LT SIDE FAILED W ASMFA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW23805AM5401 26272 AIRCRAFT RETURNED, LT GENERATOR FAILURE, APU DID NOT START AT 35 000 FT, 24 22 25 EICAS MESSAGES, 01 GEN OFF DISPLAYED AND 01 AS BUSS OFF REMAINED ILLUMINATED. QRH ABNORMAL PROCEDURE WAS PERFORMED, PAGE 09-03, RETURNING. DURING TEST WAS DETECTED LOW QUANTITY OF OIL AND LEAK IN THE IDG, IT WAS REPLACED. LATER, AIRCRAFT RETURNED, AGAIN 24 11 03 EICAS MESSAGES, 01 GEN DRIVE DISPLAYED AND GEN DRIVE LIGHT ILLUMINATED. QRH ABNORMAL PROCEDURE WAS PERFORMED PAGE 09-04, RETURNING. THE APU WAS TIRED TO START SEVERAL TIMES AND IT STARTED AT 20 000 FT. DURING OVERNIGHT SERVICE, THE LT IDG WAS REPLACED IAW MM 24-11-01 AND SENSORS MODULE WAS REPLACED IAW MM 49-53-08, TESTED CORRECT. 2L72 4F4 FRTA2NM E17NE 20050623000522005062300052NM 2005 6 23 UIA0504 120050605A3222 STRUT DOUG MD90 MD9030 3023690NM NLG UNDERSERVICED Z A UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 TW0017913 53537 NOSE GEAR RED LIGHT ON AFTER TAKEOFF, A/C AIR TURN BACK. GROUND CHECK FOUND NOSE LANDING GEAR SHOCK STRUT DIMENSION ABOUT 1 INCH , IAW AMM 32-21-01 RE-SERVICE NLG STOCK STRUT TO 4 INCH, CHECK AIR NO LEAKING ,CONDITION BACK NORMAL. 2L72 4F RTA6WE 20050623000552005062300055NM 2005 6 23 QXEA200500963 120050603A3620 PRESSURE SENSOR BOMBDRDHC8 DHC8402 1390042NM BLEED AIR MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09412QX 4059 NR 1 BLEED HOT CAUTION LIGHT ILLUMINATED. COMPLIED WITH CHECKLIST. NR 1 BLEED SELECTED OFF, LIGHT REMAINED ILLUMINATED. MX INTERROGATED CDS, FOUND FAULT CODE 7002 AND 7006. R & R WING PRESSURE SWITCH NR 1 IAW 36-11-36, PAGES 401-406. R & R WING DIFFERENTIAL PRESSURE SENSOR NR 1 IAW 36-11-41, PAGES 401-406. COMPLIED WITH OPERATIONAL TEST OF BLEED AIR SYSTEM. NO DEFECTS NOTED. ACFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050623000562005062300056NM 2005 6 23 QXEA200500964 120050604A3620 SWITCH BOMBDRDHC8 DHC8402 1390042NM BLEED AIR SYS MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09412QX 4059 NR 1 BLEED HOT CAUTION LIGHT ILLUMINATED. RAN CHECKLIST AND LIGHT REMAINED ON. MX INTERROGATED CDS, FOUND FAULT CODE 1801 "LEFT WING LEAK SWITCH. COMPLIED WITH FIM TASK 36-20-00-810-801. R & R LT DUCT LEAK SWITCH IAW AMM TASK 36-11-21-00-801. NR 1 BLEED CAUTION LIGHT EXTINGUISHED. OPS CHECK GOOD. ACFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050623000572005062300057NM 2005 6 23 QXEA200500965 120050515A5230 SEAL BOMBDRDHC8 DHC8402 1390042NM AFT CARGO DOOR DEFECTIVE A QXEAO OTHER O OTHER DEDESCENT 1 NM09417QX 4086 ON DESCENT AT APPROX 2.0 PSI, CABIN RATE OF DESCENT WENT FROM 500 FPM, SPIKED TO CLIMB OF 3000 FPM, THEN SPIKED TO DESCENT OF 3000 FPM, THEN RETURNED TO NORMAL. ACFT DEPRESSURIZED APPROX 10 MILES FROM AIRPORT. R & R AFT CARGO DOOR SEAL. PRESSURIZED AIRCRAFT. OPS CHECK GOOD. ACFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050622000742005062200074EA 2005 6 22 QXEA200501027 120050606A2612 DETECTION SYS CNDAIRCL600 CL6002C10 1390015EA FIRE PROTECTION MALFUNCTIONED A QXEAO OTHER O OTHER CRCRUISE 1 NM09604QX 10019 FIRE SYSTEM FAULT MESSAGE. FIRE DETECT "A" CIRCUIT BREAKER POPPED. RESET BREAKER IAW GMM 5-18-0. CIRCUIT BREAKER REMAINED IN// PERFORMED FIRE SYSTEM TEST. TEST GOOD. NO PARTS REPLACED. ACFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20050622000812005062200081EA 2005 6 22 QXEA200500981 120050423A2120 ODOR CNDAIRCL600 CL6002C10 1390015EA COCKPIT DETECTED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM09604QX 10019 COCKPIT/CABIN HAS FOUL ODOR WHICH IS CAUSING CREW TO SNEEZE. HEAVY ODOR OF GYM SOCKS. CHECKED SYSTEMS. NO ODOR NOTED IN FLIGHT DECK UPON COMPLETION OF OPS AND LEAK CHECKS. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20050622000842005062200084NM 2005 6 22 QXEA200500986 120050411A2930 CONNECTOR DHAV DHC8 DHC8202 2809007NM HYD PUMP DIRTY A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09349PH 486 AFTER TAKEOFF, NR 2 STANDBY PUMP HOT LIGHT BEGAN CYCLING AND THEN CAME ON STEADY. PERFORMED NR 2 STANDBY PUMP HOT CHECKLIST AND LIGHT EXTINGUISHED APPROX A MINUTE. OPERATED NORMALLY FOR REMAINDER OF FLIGHT. MX CLEANED CONNECTOR ON NR 2 STANDBY PUMP. GROUND RAN ACFT AND CYCLED APPLICABLE HYDRAULIC SYSTEM USING NR 2 STANDBY PUMP. LIGHT REMAINED EXTINGUISHED. NO FURTHER DEFECTS NOTED. NO PARTS REPLACED. ACFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050622000902005062200090NM 2005 6 22 QXEA200501053 120050604A5347 SEAT TRACK BOMBDRDHC8 DHC8402 1390042NM ZONE 200 WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09415QX 4081 CO-PILOT INBOARD SEAT TRACK WORN ON TOP SURFACE. REPAIRED IAW Q400 SRM 51-42-45 AND 51-25-10. 2H72 4T RTA13NM 20050622000912005062200091NM 2005 6 22 QXEA200501042 120050526A5330 SKIN BOMBDRDHC8 DHC8402 1390042NM ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09415QX 4081 RT LOWER FUSELAGE SKIN GOUGED 6 INCHES FORWARD OF LAV SERVICE DOOR APERATURE. REPAIRED IAW RD 8/4-53-505, PAGE 3, STEPS 1 AND 2 AND Q400 SRM 51-21-11, PAGE 202, STEP 4-A AND Q400 AMM 51-25-30-370-801. 2H72 4T RTA13NM 20050622000942005062200094NM 2005 6 22 QXEA200501056 120050601A5330 SKIN BOMBDRDHC8 DHC8402 1390042NM ZONE 200 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09415QX 4081 FOUR DENTS IN FUSELAGE SKIN ON LT HAND SIDE AFT OF ICE SHIELD ABOVE WINDOW STATION X295 TO X330. REPAIRED IAW HORIZON AIR EA 6-53-541, Q400 RD 8-53-1231 AND SRM 51-25-05-370-801. 2H72 4T RTA13NM 20050622001192005062200119SO 2005 6 22 SIMA200515709 120050601A5330AL2024T3 SKIN EMB 135 EMB135KL 3260302SO FUSELAGE DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21851AE 145734 DURING AN MBV INSPECTION AND REPAIR OF DENT ON LEFT CENTER FUSELAGE 1 TDMI 851530243. PERFORMED CUT OUT OF THE SKIN PANEL BETWEEN FRAMES 22 AND 23 AND STRINGERS 13L AND 14. FABRICATED A FILLER AND REPAIR DOUBLER. REPAIR DONE IAW EMB 145 SRM, SRM EMB-145/1142 REV 29, CHAPTERS 53-21-01 FIG 201. (M) 2L72 4F RTT00011AT 20050622001282005062200128SO 2005 6 22 SIMA200511706 120050424A2130 CONTROL SYSTEM EMB 135 EMB135LR 3260305SO CABIN PRESSURE MALFUNCTIONED A SIMAB EMER. DESCENT J WARNING INDICATION CLCLIMB 1 SW21719AE 145276 BNA - LOSS OF CABIN PRESSURIZATION WHEN CLIMBING THROUGH FL210. CABIN ALT WENT ABOVE 10,000 DURING DESCENT. OXYGEN MASKS DEPLOYED. (M) 2L72 4F RTT00011AT 20050622001392005062200139EA 2005 6 22 ASOA05450 120050519A5210601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27845AS 7324 DURING A GROUND INSPECTION IN ATL, THE ATTACH ROD CONNECTED TO THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN OFF. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050622001422005062200142SO 2005 6 22 SIMA200515708 120050525A532014521700007 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A SIMAO OTHER O OTHER NRNOT REPORTED 1 SW21648AT 145225 SAW - DURING AN MBV, THE FORWARD CABIN FLOOR OMEGA SHAPE IS CORRODED AT FRAME 20 BY BEAM CROSS. COMPLETED DOUBLER REPAIR OF FORWARD CABIN FLOOR OMEGA BEAM AT FRAME 20 IAW EMB SRM 53-21-10 FIGURE 201. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20050622001592005062200159NM 2005 6 22 USAA050713 120050602A5310 BEAM BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19445US40360 24863 CLT - FOUND STUB BEAM CRACKED .375 INCH, UPPER CHORD LT 578 ATTACH POINT TO CREASE BEAM, INNER CHORD LBL 64 FROM RIVET. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-20=05 AND EA 96603. (M) 2L72 4F RTA16WE 20050622001702005062200170EA 2005 6 22 ASOA05422 120050509A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27867AS 7463 DURING A C-CHECK IN MCN, THE ATTACH CLIP AT FS 484, LBL 30 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE ATTACH CLIP AT FS 484, LBL 30 IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20050622001722005062200172EA 2005 6 22 ASOA05392 120050502A3350BR9279232 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN DAMAGED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27839AS 7284 DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY FLOODLIGHT BY THE PASSENGER DOOR WAS FOUND TO BE DAMAGED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOODLIGHT BY THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050622001762005062200176EA 2005 6 22 ASOA05433 120050513A5210 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAO OTHER O OTHER NRNOT REPORTED 1 SO27850AS 7355 FLT 4336 - DURING A GROUND INSPECTION IN CVG, THE PASSENGER DOOR BOTTOM STEP WAS FOUND BROKEN LOOSE FROM THE TIE ROD WHICH WAS ALSO FOUND BENT. MAINTENANCE REATTACHED THE BOTTOM STEP TO THE TIE ROD AND ADJUSTED THE ACTUATING ARM. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050622001802005062200180SO 2005 6 22 SIMA200512501 120050501A3350 SIGN EMB 145 EMB145LR 3260212SO OVERWING INOPERATIVE A SIMAO OTHER O OTHER TXTAXI/GRND HDL 1 SW21649PP 145234 CREW NOTED WHEN DOING CABIN PREFLIGHT THE FORWARD CENTER OVERWING EXIT SIGN INOPERATIVE. REPLACED SIGN ASSEMBLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20050622002042005062200204EA 2005 6 22 MASA200500230 120050318A2760601R751245 MANIFOLD CNDAIRCL600 CL6002B19 1900309EA SPOILERS FAILED A MASAO OTHER J WARNING INDICATION APAPPROACH 1 SW072718510302 7185 ASH 2883 FROM SYR TO PHL ON APPROACH HAD THE OUTBOARD GROUND SPOILERS DEPLOY. PHL MAINTENANCE IS IN THE PROCESS OF TROUBLESHOOTING. MAINTENANCE REPLACED GROUND SPOILER MANIFOLD, OPS CHECK GOOD. 2L72 4F RTA21EA 20050622002142005062200214NM 2005 6 22 CALA0500197 120050612A5315143N501555 FLOORBEAM BOEING757 757224 1384958NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712109 27299 INSPECTION FOUND UPPER CHORD OF FLOORBEAM CORRODED AT BS 720 FROM RBL 24-52. REPAIRED IAW SRM 53-00-51, FIGURE 201. 2L72 4F RTA2NM 20050622002212005062200221NM 2005 6 22 P5CA0501362 120050610A3610NH100241010 CLAMP BOEING747 747283B 1384867NM PWA JT9 JT9D70A 52054NE NR 1 ENGINE FAILED A P5CAE ENGINE SHUTDOWN J WARNING INDICATION DEDESCENT 1 EA15921FT 21575 689167 NR 1 ENGINE FIRE WARNING SOUNDED ON DESCENT. CLOSED THRUST AND START LEVER, LIGHT WENT OUT. FIRE HANDLE WAS NOT PULLED. REPLACED CLAMP TO HIGH STAGE VALVE. OPS AND LEAK CHECK OK PER MM 36-13-00 AND 71-00-00. 2L74 4F4 F A20WE E3NE 20050622002242005062200224NM 2005 6 22 DHL2005741537 120050428A5330 SKIN BOEING727 7272Q9 138448MNM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH46665 21931 FUSELAGE SKIN UPPER AT GPS ANTENNA LOCATION BS 430 BTN STR1 AND 2L CRACK INDICATION NDT CONFIRMED. CUT OUT DAMAGED AREA DIM [3.500 X 2.250. FABRICATED DOUBLER 2024T3 .050, 11.500 X 7.500 IAW B727 SRM 53-30-2 FIG 1 AND 53-30-3 FIG 1. TREATED AND PRIMED REPAIR DOUBLER IAW B727 SRM 51-10-2. INSTALLED DOUBLER IAW B727 SRM 53-30-3 FIG 1. 2L73 4F RTA3WE 20050622002272005062200227NM 2005 6 22 DHL2005741541 120050517A57119516201188 SPAR BOEING727 7272Q9 138448MNM RT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH46665 21931 RT WING AT LOWER REAR SPAR WBL 124.2 HAS A CORRRODED TEE ANGLE FITTING. REMOVED AND REPLACED TEE FITTING P/N 65-16201- 188 PO NR 5096248 IAW B727 SRM 51-30-2. 2L73 4F RTA3WE 20050622002342005062200234WP 2005 6 22 DHL2005807542 120050520A57305755231509 ACCESS PANEL DOUG DC8 DC873F 302199FWP RT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH86990 45990 RT WING ACCESS PANEL NR 505B LT UPPER EDGE CORRODED STA XRS 460.000. REMOVED CORROSION LEVEL II FROM RT ACCESS DOOR NR 505B IAW SRM 51-1-8 PG 17-18. MEASURED BLENDOUT, FOUND OUT OF ALLOWABLE LIMITS IAW SRM 57-2-0 PAGE 76. REMOVED CORRODED ACCESS DOOR IAW SRM 51-3-0 PG 1. INSTALLED NEW ACCESS DOOR, REFUELED AND LEAK CHECKED (NR 4 ALT TANK). NO LEAK FOUND IAW MM 20-16-0 PG 201-210, MM 12-11-1 PG 301-306. 2L74 4F RT4A25 20050622002362005062200236NM 2005 6 22 DHL2005784501 120050515A5740 MOUNT BOEING727 727227 1384078NM TE FLAP ACTUATORCRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01784DH 22001 NR 1 LEADING EDGE FLAP ACTUATOR UPPER MOUNT IS CRACKED AT LWR OUTBOARD CORNER, WING STA 304. REMOVED UPPER ACTUATOR MOUNT AND FABRICATED NEW ANGLE IAW B727 SRM 57-20-2 FIG 1,TREATED AND PRIMED IAW B727 SRM 51-10-2 AND INSTALLED NEW ANGLE ON NR 1 LEADING EDGE FLAP ACTUATOR MOUNT, IAW B727 SRM 51-30-2 AND 57-20-2 FIG 1. 2L73 4F A3WE 20050622002382005062200238NM 2005 6 22 DHL2005784503 120050515A5752 TAB BOEING727 727227 1384078NM AILERON DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01784DH 22001 LT OUTBD AILERON TAB UPPER SURFACE IS DENTED AND LOWER SURFACE IS DELAMINATED AT PREVIOUS REPAIR, WING STA 716. REMOVED DELAMINATED EXISTING REPAIR ON LT, O/B,AILERON TAB LOWER SURFACE CUT OUT APPROX 3 1/4" BY 7 1/2", FABRICATE FILLER APPROX 3 1/4" BY 7 1/2" AND DOUBLER APPROX 4 1/2"X 10 1/2" FROM .010 2024-T3 P.O. 9912184, BONDED FILLER AND DOUBLER, CLEANED, PRIMED AND SEALED IAW B727 SRM 57-50-2 FIG 8 AND 51-40-20 FIG 30 MEASURED DENTS 2 EA ON UPPER SURFACE AND FOUND TO BE WITHIN LIMITS IAW B727 SRM 57-50-1 FIG 4 DETAIL 4. 2L73 4F A3WE 20050623000062005062300006EA 2005 6 23 SWIA200515144 120050615A3397 CONTACT CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DIRTY A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07445SW 7651 EMERGENCY FLOOR LIGHTING STRIP AFT SECTIONS WILL NOT ILLUMINATE. CLEANED CONTACTS AT SEGMENTS. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050623000072005062300007EA 2005 6 23 SWIA200515145 120050615A274070609 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CRCRUISE 1 NM07978SW5453 5453 7953 AP PITCH TRIM CAUTION MSG IN FLIGHT. REPLACED HSTCU WITH AS SERVICEABLE UNIT. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050623000172005062300017NM 2005 6 23 05FDEA01613 120050616A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25477FE 21394 FOUND STRINGER 27R TO BE CORRODED BS 1178. 2L73 4F RTA3WE 20050623000262005062300026EA 2005 6 23 MASA200500419 120050531A2613 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA MLG WW OVERHT ILLUMINATED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07653ML 7039 ASH 2991 PHL. ABORTED T/O DUE TO MLG BAY OVERHEAT MSG, R2 LOOP. 2L72 4F RTA21EA 20050623000282005062300028EA 2005 6 23 MASA200500441 120050605A2560 FLASHLIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A MASAO OTHER L NO TEST NRNOT REPORTED 1 SW0777195 7195 ASH 2657. INOPERATIVE EMERGENCY FLASHLIGHT AT THE AFT FLIGHT ATTENDANT'S POSITION, R2 FLASHLIGHT. 2L72 4F RTA21EA 20050623000352005062300035NM 2005 6 23 72300212 120050520A5311 FRAME BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE BULKHEAD CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 2 INCH AREA OF CORROSION ON BULKHEAD FRAME. 2L73 4F4 FRTA3WE E2EA 20050623000502005062300050NM 2005 6 23 ASMF200506002 120050602A3020320115 ANTI-ICE VALVE DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE LT SIDE FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23945AS1937412818 49643 AIRCRAFT RETURNED TO PLATFORM, LT STARTER VALVE DID NOT OPEN AND ANTI-ICE BREAKER OF NOSE COWLING POPPED OUT. THE REPORT WAS DEFERRED BY MEL 80-2 AND THE ANTI ICE VALVE WAS REPLACED IAW MM 30-20-01, TESTED CORRECT. DEFERRED REPORT WAS CLOSED. 2L72 4F4 FRT E9NE 20050623000582005062300058NM 2005 6 23 QXEA200500966 120050515A213192146A010401 CONTROLLER BOMBDRDHC8 DHC8402 1390042NM CABIN PRESSURE MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION DEDESCENT 1 NM09417QX2470 4086 DURING CONSTANT 1500 FPM DESCENT, NO CHANGE TO POWER LEVERS OR INPUT TO PRESSURIZATION CONTROLLER, CABIN WENT FROM CONSTANT 500 FPM DESCENT TO A CLIMB RATE OF 3000 FPM, THEN A DESCENT RATE OF 3000 FPM, THEN STABILIZED. CABIN DIFFERENTIAL APPROX 1.5 PSI AT THE TIME. ACFT ALTITUDE APPROX 9000 FEET. MX R & R CABIN PRESSURE CONTROLLER IAW Q400 AMM TASK 21-31-06-000-801. COMPLIED WITH FUNCTIONAL CHECK OF PRESSURE CONTROL. OPS CHECK GOOD. ACFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050623000802005062300080EA 2005 6 23 SWIA200515131 120050531A3350 CHARGER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSINOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07905SW 7437 EXIT EMERGENCY LIGHT BY STAIRS AND CABIN OVERHEAD EXIT LIGHT IS INOPERATIVE. REPLACED NR 2 BATTERY CHARGER ASSEMBLY. OPS CHECK GOOD. 2L72 4F RTA21EA 20050623000812005062300081SO 2005 6 23 SWIA200515132 120050614A27523430001005 ACTUATOR EMB 120 EMB120ER 3260203SO TE FLAP MALFUNCTIONED A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07293SW1179311793 120320 RT INBOARD FLAP HANGS DOWN APPROX 2 INCHES ON THE GROUND. R & R RT INBOARD FLAP ACTUATOR IAW EMB 120 MM 27-50-00. OPS CHECK GOOD. 2L72 4T RTA31SO 20050623000982005062300098 2005 6 23 QXEA200501026 420050528A2310CDU3933AE04 CDU BOMBDRDHC8 DHC8402 1390042NM ZONE 200 FAILED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09412QX3150 238 4059 F/O ARCDU SCREEN FLICKERED, THEN WENT BLANK WITH NO FAIL MESSAGE. CHECKLIST RAN AND SCREEN RETURNED, BUT WENT BLANK AGAIN SOON AFTER. CHECKLIST RAN AGAIN AND IT CAME BACK ON AND DID NOT REPEAT. MX REPLACED ARCDU. OPS CHECKS GOOD. ACFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050623001092005062300109NM 2005 6 23 QXEA200501015 120050406A33506104781 BATTERY PACK DHAV DHC8 DHC8202 2809007NM EMERGENCY LIGHTSDISCHARGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09345PH26452657 476 ACCESS EMERGENCY LIGHT INOP. MX REPLACED BATTERY PACK FOR LOW VOLTAGE. OPS CHECKS GOOD. ACFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050623001142005062300114NM 2005 6 23 QXEA200500968 120050509A2740 CONTROL UNIT BOMBDRDHC8 DHC8402 1390042NM STAB CONTROL MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09414QX 4061 AT 230 KIAS AT 8000 MSL, (AUTOPILOT WAS NOT ENGAGED) PITCH TRIM AND AUTO TRIM FAIL CAUTION ADVISORY MESSAGE AND LIGHTS ILLUMINATED SIMULTANEOUSLY. ACCOMPLIESHED EMERGENCY CHECKLIST AND RETURNED TO LAX. FCECU FAILURE 63, 67, E3, E7, CLEARED IAW 400 FIM TASK 27-00-00-810-805, 27-32-06-810-808 AND 27-32-06-810-803. OPS CHECK OF PITCH TRIM GOOD. NO MESSAGES, CAUTION LIGHTS OR FAULT CODES SHOWN. NO PARTS REPLACED. ACFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050623001172005062300117EA 2005 6 23 QXEA200500975 220050518A7200 ENGINE BOMBDRDHC8 DHC8402 1390042NM PWC 150 PW150A EA NR 1 MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION APAPPROACH 1 NM09413QX 4060 PCEFA0093 APPROACH, NR 1 ENGINE FADEC CAUTION ILLUMINATED AND POWERPLANT MESSAGE ON ENGINE DISPLAY. PERFORMED ABNORMAL CHECKLIST. NO OTHER MALFUNCTIONS NOTED. REPLACED NR 1 ENGINE P2. 2 BLEED OFF VALVE SCREEN PER AMM TASKS 75-31-33-000-801 AND 75-31-33-400-801. CLEARED FAULT CODES PER AMM TASK 73-21-00-070-801. GROUND RAN NR 1 ENGINE NO FAULTS NOTED. ACFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E00062EN 20050623001452005062300145NM 2005 6 23 72300204 120050413A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 2 X 2 INCH AREA OF CORROSION ON STRINGER. 2L73 4F4 FRTA3WE E2EA 20050623001472005062300147NM 2005 6 23 DHL2005741570 120050425A5313 STRINGER BOEING727 7272Q9 138448MNM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 STR 28L CORRODED AT FS 1013. REMOVED CORROSION FOUND TO BE OUT OF LIMITS ON STR 28L AT FS 1013 IAW B727 SRM 51-10-6 AND SRM 53-10-1. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM. 2L73 4F RTA3WE 20050623001522005062300152NM 2005 6 23 WRLA200587 120050614A5512 PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST LT BARREL NUT HOLE NR 1. (OPEN) 2L73 4F4 FRTA22WE E24NE 20050623001552005062300155NM 2005 6 23 DL76P050314 120050608A2150 A/C PACK BOEING767 767332 1382001NM LEFT ODIFEROUS A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27143DA 25991 SMOKE/FUMES IN CABIN CAUSING LAV SMOKE DETS TO GO OFF. DIVERTED TO RIC. L PACK TURNED OFF SMELL DISSIPATED. RAN ENGS AND PACKS. RAN PACKS TOGETHER AND ISOLATED UNABLE TO DUPLICATE. DUE TO HIST L PACK FWD TO MCO. ATL MTC WILL REPLACE NO.1 ENGINE. 2L72 4F RTA1NM 20050623001562005062300156NM 2005 6 23 DL767050317 120050603A5330 SKIN BOEING767 767232 1385132NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27101DA 22213 REPAIR OF CORROSION WAS FOUND AT SEVERAL LOCATIONS ALONG STRINGER 38R AND 39R AF FS 434. THE DAMAGE TO THE BUTT SPLICE STRIP WAS BLENDED AND HFEC INSPECTED. SKIN DAMAGE WAS REPAIRED PER THE SRM 53-00-01 FIG 201. INFORMATION WAS PROVIDED TO BOEING AND BOEING APPROVED THE REPAIR VIA 8100-9 FORM. 2L72 4F RTA1NM 20050623001572005062300157NE 2005 6 23 DLM88050318 220050610A7200JT8D219 ENGINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 1 FAILED A DALAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 SO27988DL41642 53339 718128 LT ENGINE FAILED AT 15K FT AND 300 KNOTS - REPLACED ENGINE FOR INTERNAL FAILURE 2L72 4F4 FRTA6WE E9NE 20050623001622005062300162NM 2005 6 23 DL733050323 120050613A213328410 OUTFLOW VALVE BOEING737 737347 1384647NM CABIN PRESSUR UNSERVICEABLE A DALAO OTHER J WARNING INDICATION CLCLIMB 1 SO27308WA 23441 AIRCRAFT WOULD NOT PRESSURIZE. FOUND AUTO FLOW CONTROL VALVE NOT CLOSING PER CABIN PRESS LEAK TEST 05-51-91-702. REPLACED VALVE PER MM 21-58-31. OP CK OK. AIRCRAFT PRESSURIZED ON GROUND PER MM. 2L72 4F RTA16WE 20050623001642005062300164NM 2005 6 23 DL777050325 120050615A21214100945A FAN BOEING777 777232 1385232NM CABIN FAILED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27865DA 29737 RECIRC FAN STAUS MSG STRONG ELECTRICAL ODOR. REPLACED FAN. 2L72 4F RTT00001SE 20050624000012005062400001NM 2005 6 24 WRLA2005100 120050614A5512 PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098, FOUND CORROSION IN HST LT BARREL NUT HOLE NR 31. 2L73 4F4 FRTA22WE E24NE 20050624000022005062400002NM 2005 6 24 WRLA2005101 120050614A5512 PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098, FOUND CORROSION IN HST LT BARREL NUT HOLE NR 32. 2L73 4F4 FRTA22WE E24NE 20050624000142005062400014WP 2005 6 24 AALA20050387 120050615A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW219624T 53594 SFO - EMERGENCY LIGHTS AT ROWS 18, 20, AND 21 CEILING INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROWS 18, 20, AND 21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050624000152005062400015WP 2005 6 24 AALA20050388 120050615A33506011779 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW219624T 53594 SFO - LEFT AND RIGHT HAND FORWARD OVERWING EXIT DOOR EXIT SIGNS INOPERATIVE. REPLACED BATTERY PACK FOR LEFT AND RIGHT HAND FORWARD OVERWING EXIT DOOR EXIT SIGNS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050624000162005062400016WP 2005 6 24 AALA20050386 120050612A323139567851 LINK DOUG DC9 DC982 3022082WP NLG DOOR INOPERATIVE A AALAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 SW21258AA 49288 LGA - UPON GEAR RETRACTION SEVERE VIBRATION FELT IN NOSE OF AIRCRAFT. CONTINUED THROUGH FLIGHT. EMERGENCY DECLARED AND AIRCRAFT LANDED WITHOUT INCIDENT. NOSE GEAR DOOR FOUND OPEN ON ARRIVAL. REPLACED FAULTY LINK ON LEFT HAND NOSE GEAR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050624000172005062400017NM 2005 6 24 AALA20050389 120050616A3350D71702001 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21786AN 30250 LAX - EMERGENCY SEAT LIGHTING AT ROWS 20 THROUGH 26 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY SEAT LIGHTING AT ROWS 20 THROUGH 26. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20050624000182005062400018EU 2005 6 24 RAIA00506023 120050616A2611 WARNING LIGHT JETAIRJETSTMJETSTM4101 1500501EU CARGO SMOKE FALSE ACTIVATIONA RAIAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 CE03557HK 41074 FLT 3660 BWI - RED SMOKE WARNING ILLUMINATED ON CAP DURING TAXI. NO INDICATION AFTER 30 SECONDS ON PRIMARY SYSTEM. PANEL LIGHT EXTINGUISHED AFTER 2 MINUTES. MAINTENANCE INSPECTED THE MAIN BAGGAGE COMPARTMENT SMOKE DETECTORS. NO DEFECTS NOTED. 2L72 4T RTA41NM 20050624000252005062400025NM 2005 6 24 05FDEA01620 120050620A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25619FE 48770 MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 1230 - 1239, LBL 47 FOUND CROWN ELONGATED. CARRIED OUT REPAIR AS PER SRM 53-70-00 VOL I FIG 1. 2L73 4F RTA22WE 20050624000272005062400027SO 2005 6 24 C2XA05IA078 120050611A2121524864 INVERTER EMB 145 EMB145LR 3260212SO E/E BAY FAN INOPERATIVE A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW27169511602616026 145063 BHM - FLIGHT 3240, THE CREW REPORTED AN ELECTRICAL ODOR IN THE COCKPIT DURING CRUISE. THE AIRCRAFT LANDED AT BHM WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE FORWARD AVIONICS RECIRC FAN ON MEL. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED AT IAH ON FLIGHT 2026 ON 06/13/05 WHERE MAINTENANCE REMOVED AND REPLACED THE INVERTER FOR THE AVIONICS FAN, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, REMOVED THE MEL AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050624000292005062400029GL 2005 6 24 C2XA05CL048 220050616A720023070401 ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 1 FAILED A C2XAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SW27265497639 145571 CAE312086 CLE FLIGHT 2668 THE CREW REPORTED A LOUD BANG FOLLOWED BY NR 1 ENGINE SHUTDOWN. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE. OPERATIONAL CHECKS WERE GOOD. 2L72 4T4 FRTT00011ATTE6CH 20050624000302005062400030WP 2005 6 24 ARWA20050605 120050615A2720 CONTROL CABLE DOUG DC8 DC863F 302198FWP HYD SHUTOFF BROKEN A ARWAK NONE O OTHER ININSP/MAINT 1 SO19906R 46087 ON PRE-FLIGHT RUDDER CONTROL LIGHT OFF WITH AUXILIARY HYDRAULIC PUMP ON AND RUDDER POWER LEVER OFF POSITION. FOUND RUDDER HYDRAULIC SHUT-OFF CABLE BROKEN. REMOVED AND REPLACED CONTROL CABLE IN ACCORDANCE WITH M/M 20-17-0 AND 91-10-0; OPERATIONAL CHECK NORMAL IN ACCORDANCE WITH M/M 27-20-0. 2L74 4F 4A25 20050624000312005062400031NE 2005 6 24 06202005 220050620A7261 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE MALFUNCTIONED A NSVAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA27346CJ 346 785564 AT 5 TO 6 MINUTES IN FLIGHT OIL PRESSURE FLUCUATED. STARTED SMALL AND INCREASED, OIL PRESSURE DROPPED. SHUTDOWN ENGINE WHEN CLOSE TO 0, OIL TEMP STILL IN GREEN. 2L72 4T4 TRTA52EU E8NE 20050624000322005062400032EU 2005 6 24 06192005 120050620A32465006227 WHEEL SAAB SF340 340B 7860101EU NLG VIBRATION A NSVAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 EA27308CE 210 VERY STRONG SHIMMY / VIBRATION AT ABOUT 60 KIAS ON TAKEOFF ROLL. 2L72 4T RTA52EU 20050624000332005062400033EA 2005 6 24 VTZA200500099 120050601A27409960013 TRIM SYSTEM CNDAIRCL600 CL6002B19 1900309EA COCKPIT FAULTY A VTZAO OTHER J WARNING INDICATION DEDESCENT 1 EA27639 7313 BOTH STABILIZER CHANNELS AND MACH TRIM FAILED. 2L72 4F RTA21EA 20050624000342005062400034NM 2005 6 24 UPS05444582 120050514A571265B08150103 RIB BOEING747 747123F NM LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSP TYPE: C, LT WING UPPER T/E PANEL SUPPORT RIB UPPER CHORD CRACKED REVEALED AT WBL 445.8 INCHES FWD OF I/B AILERON I/B EDGE (CRACK LENGTH 0.5 INCH). LT WING UPPER T/E PANEL SUPPORT RIB UPPER CHORD REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050624000362005062400036NM 2005 6 24 UPS05444584 120050520A5313 STRINGER BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSP TYPE: C M/D BS 742 STR 8L STRINGER END FOUND CRACK AS MARKED. ( CRACK LENGTH 3 INCHES). M/D BS 741 TO BS 770 STR 8L AREA STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4. 2L74 4F A20WE 20050624000402005062400040NM 2005 6 24 UPS05444588 120050518A5313 STRINGER BOEING747 747123F NM FWD CARGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSP TYPE: C FWD CARGO COMPT STR 47L CORRODED AT BS 745. CORROSION BLEND OUT 0.021 INCH BY 0.875 INCH BY 2.0 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT, FWD CARGO COMPT - BS 740 - BS 760 STR 47L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. 2L74 4F A20WE 20050624000432005062400043NM 2005 6 24 UPS05444591 120050516A5330 SKIN BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSP TYPE: C FX- SKIN LAP JOINT FOUND CORRODED AT BS 379-381 STR 23L AROUND 2EA FASTENERS AS MARKED (APPROX 15 PERCENT MATERIAL LOSS). CORROSION BLEND OUT 0.011 BY 0.875 BY 1.75 INCHES. EXCEED EO NR B747-5330-20503-D LIMIT. FX SKIN LAP JOINT REPAIRED AS PER SRM 53-30-03 FIG 26 FROM BS 375-38L BTN STR 22L - STR 23L. 2L74 4F A20WE 20050624000442005062400044NM 2005 6 24 UPS05444592 120050517A5311 FRAME BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSP TYPE: C, M/D BS 660 STR 24L CUTOUT CRACKED, (CRACK LENGTH 0.5 IN). M/D BS 660 STRINGER 24L, CUTOUT FRAME REPAIRED AS PER SRM 53-10-04 FIG 35. 2L74 4F A20WE 20050624000462005062400046WP 2005 6 24 UPS05844577 120050502A53305649028 DOUBLER DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSP TYPE: C3, A/C BAY L30R AT APPROX STA 38 TO STA 58 DOME NUTS UNDER LONGERON HAVE CORROSION OUT OF LIMITS AT ATTACH INTERNAL DOUBLER. R & R INTERNAL DOUBLER AT STA 38-58 L31R AND 2 EA LONGERONS AT STA 8 TO 70 L27R AND L30R IAW SRM 51-1-21 AND 51-1-20D. 2L74 4F RT4A25 20050624000472005062400047WP 2005 6 24 UPS05844578 120050512A53133646937U1 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 INSP TYPE: C3, D PIT INTERGRANULAR CORROSION ON L34R STA 1412. REMOVED AND REPLACED LONGERON 34R STA 1390-1460 IAW SRM 51-1-21D. 2L74 4F RT4A25 20050624000482005062400048WP 2005 6 24 UPS05844594 120050602A3350 BATTERY PACK DOUG DC8 DC871F 302199DWP EMERGENCY LIGHTSINOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER 33-50-01. 2L74 4F RT4A25 20050624000522005062400052NM 2005 6 24 MASA200500360 120050514A3350063071BPEGPL LIGHT DHAV DHC8 DHC8202 2809007NM CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07987HA 425 CREW REPORTED FWD WHITE LIGHT ESCAPE PATH INOP. MX REMOVED AND REPLACED ESCAPE PATH LIGHT. 2H72 4T RTA13NM 20050624000552005062400055SO 2005 6 24 MASA200500368 120050519A3350 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSINOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07846MJ 145507 RT AFT EXTERNAL OVERWING EMERGENCY LIGHT NOT ILLUMINATING. MX REPLACED BULB AND OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050624000592005062400059SO 2005 6 24 MASA200500376 120050521A3350 LIGHT EMB 145 EMB145LR 3260212SO ROW 12 MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07825MJ 145179 ROW 12 EMERGENCY EXIT LIGHT INOPERATIVE. MX REPLACED LIGHT ASSEMBLY. 2L72 4T RTT00011AT 20050624000602005062400060SO 2005 6 24 MASA200500377 120050521A3350 LIGHT EMB 145 EMB145LR 3260212SO EMERGENCY EXIT MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07843MJ 145478 FWD BULKHEAD EMERGENCY EXIT LIGHT INOPERATIVE. MX FOUND LIGHT TO OPERATE NORMALLY. 2L72 4T RTT00011AT 20050624000662005062400066WP 2005 6 24 05FDEA01614 120050617A5230AFA38735 RETAINER DOUG DC10 DC1010 3022110WP CARGO DOOR BROKEN A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25571FE 47830 ON CTR CARGO DOOR VANE STA 1781, BETWEEN STR 39/42, RETAINER FOR SEAL BROKEN, LENGTH 1,830 INCH, MISSING MATERIAL ON SKIN CUT OUT VANE. REMOVED SCUFF PLATE WEBS INTERNAL JAMB CARGO DOOR TO GAIN ACCESS PER MM 20-50-02 SRM 51-35-01; CUT RIB FAIRING AND 7280 AND ANGLE AFA7173. REMOVED DAMAGED SECTION OF SEAL RETAINER PER SRM 51-35-02, PAGE 3/9; CUT DAMAGED SECTION OF EXTERNAL SKIN IAW SRM 53-50-00; REPAIRED SKIN PER SRM 53-50-00, FIG 26. SPLICING RIB AND ANGLE PER SRM 53-00-01, FIG 8. SPLICING WEB INTERNAL JAMB DOOR PER SRM 53-00-01, FIG 10, SHT 1. REPLACED DAMAGED SEAL RETAINER PER SRM 51-35-01 PG 1/13; REINSTALLED REMOVED PARTS PER SRM 51-33-01, PG 36/47. 2L73 4F A22WE 20050624000672005062400067NM 2005 6 24 05FDEA01616 120050617A5314 KEELBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25263FE 21625 AFT CARGO CORROSION ON KEELBEAM STA 950D TO 950E, STR 29L. BLENDED CORROSION AT KEELBEAM STA 950D TO 950E OUT OF LIMITS. INSTALLED REPAIR IAW SR27-53-023A. FOUND TO BE A MINOR REPAIR. 2L73 4F RTA3WE 20050624000682005062400068NM 2005 6 24 05FDEA01617 120050617A5311 FRAME BOEING727 727200 138407ENM FUSEAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 WHILE WORKING N01404 FOUND HOLES IN FRAME AT BS 520 RBL 65 WL 201 DAMAGE. *S/D* REMOVED AND REPLACED BS 520 FRAME SEGMENT STR 13R TO 25R, FOUND TO BE A MAJOR REPAIR PER SRM 51-30-5 AND 51-30-2. 2L73 4F RTA3WE 20050624000692005062400069NM 2005 6 24 05FDEA01619 120050619A5755 ATTACH ANGLE BOEING727 727200 138407ENM NR 2 SPOILER DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 NR 2 SPOILER ACTUATOR LWR ATTACH ANGLE HOLES ARE ELONGATED. *S/D* REPLACED NR 2 SPOILER ACTUATOR SUPPORT FITTING PER SRM 51-30-2. 2L73 4F RTA3WE 20050624000702005062400070NM 2005 6 24 05FDEA01621 120050620A5710 STRUCTURE DOUG MD11 MD11 3023602NM LT WING TANK CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25631FE 48454 LT WING NR 1 TANK STRUCTURE APPROX ALONG STA XORS 504 SUSPECTED CRACK. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20050624000752005062400075EA 2005 6 24 COMA0560352 120050615A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01810CA 7370 FLIGHT 5265 - EN ROUTE CVG - RIC RECEIVED A LEFT THRUST REVERSER CAUTION MESSAGE. CREW DECLARED AN EMERGENCY AND DIVERTED TO CHO, LANDING WITHOUT INCIDENT. DEFERRED THE LEFT THRUST REVERSER PER MEL 78-30-01. 2L72 4F RTA21EA 20050624000762005062400076EA 2005 6 24 COMA0560353 120050616A2913848847 PUMP CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM FAULTY A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01929CA27419 7035 FLIGHT 5851 - DURING CLIMBOUT OF DSM RECEIVED A GEAR DISAGREE CAUTION. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD, LANDING WITHOUT INCIDENT. 2L72 4F RTA21EA 20050624000802005062400080EU 2005 6 24 AWXA200500724 120050619A2730 ACTUATOR AIRBUS320 A320232 3930326EU ZONE 300 VIBRATION A AWXAO OTHER E VIBRATION/BUFFET CLCLIMB 1 WP28605AW 543 VIBRATION FELT IN REAR ACFT APPROX 260 ALTITUDE & 310 SPEED. MX FOUND AFT LAV/POTABLE WATER SERVICING DOORS LOOSE. LATCHES ADJUSTED. ACFT FAILED FUNCTIONAL TEST FLT. RETURNED, FOUND RT BLUE & RT YELLOW ELEVATOR SERVOS OUT OF LIMITS. R&R RT BLUE & RT YELLOW ELEVATOR SERVOS. PASSED OPS CHECKS. ACFT FAILED FUNCTIONAL TEST FLT. ACFT RETURNED. FOUND ACTUATOR S/N 0587, OUT OF RIG. R&I NEW THS ACTUATOR S/N 0075. OPS TEST FAILED, OUT OF RIG. REMOVED THS ACTUATOR S/N 0075 & INSTALLED NEW THS ACTUATOR, OPS TEST PASSED. FOUND BEARINGS & ROD ENDS WORN, INCLUDING LT BLUE ELEV SERVO, LT GREEN ELEV SERVO. ROD ENDS & BEARINGS REPLACED. ACFT PASSED FUNCTIONAL TEST FLT. ACTUATOR P/N 47145-121, S/N 0587. 2L72 4F RTA28NM 20050624000862005062400086NM 2005 6 24 BB05044 120050621A3397 WIRE BOEING767 767201 1385125NM EMERGENCY LIGHT STRETCHED A USAAK NONE O OTHER ININSP/MAINT 1 EA19648US 23900 VCE FOUND FIRST FOUR EMERGENCY FLOOR LIGHTS, RIGHT SIDE, INOPERATIVE. MAINTENANCE FOUND THE CABLE STRETCHED CAUSING A FALSE CONTACT. THE CABLE WAS REPOSITIONED. 2L72 4F RTA1NM 20050624000882005062400088EU 2005 6 24 XN0A1239 120050622A2611 CONTROL BOX AIRBUS300 A300B4203 3930306EU SMOKE DETECTOR LOOSE A XN0AC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL23373PC 218 ON TAXI OUT, FLT DECK SMOKE LIGHT ILLUMINATED. RESEATED SMOKE DETECTION BOX IN 96VU. REMOVED & RESEATED C/P ON FLT DECK SMOKE DETECTION LIGHTS OUT. SYSTEM TESTS NORMALLY IAW MAINT MANUAL CHAPT 26-11-00. 2L72 4F RTA35EU 20050624000892005062400089NM 2005 6 24 SWAA051821 120050620A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM AFT CARGO BAY CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 807, RBL 5 TO BL 0, WL 149. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050624000912005062400091NE 2005 6 24 SWAA051823 220050619A7200 ENGINE BOEING737 7373Y0 1384671NM GE CFM56 CFM563B1 13802NE NR 2 FAILED A SWAAEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 SW29665WN 23497 724321 INFLIGHT SHUTDOWN/DECLARED EMERGENCY/DIVERSION. NR 2 ENGINE FAILED AT 34,000 FT, LOUD BANG TWICE & LOSS OF THRUST. REMOVED AND REPLACED NR 2 ENGINE PER MM. 2L72 4F4 FRTA16WE E2GL 20050624000942005062400094NM 2005 6 24 SWAA051814 120050620A53406551698 SPLICE BOEING737 7373H4 1384600NM AFT CARGO BAY CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 907 + 3, STR 25R. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20050624000952005062400095NM 2005 6 24 SWAA051815 120050620A53116546554 FRAME BOEING737 7373H4 1384600NM AFT CARGO BAY CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 847, STR 27L TO STR 27R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050624000962005062400096NM 2005 6 24 SWAA051816 120050620A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM AFT CARGO BAY CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 747, LBL 5 TO RBL 5, WL 148. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050624000982005062400098NM 2005 6 24 SWAA051818 120050620A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM AFT CARGO BAY CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 767, BL 0 TO RBL 5, WL 148. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050624000992005062400099NM 2005 6 24 SWAA051819 120050620A53226546569 SHEAR TIE BOEING737 7373H4 1384600NM AFT CARGO BAY CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 967, LBL 8, WL 148. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050624001002005062400100NM 2005 6 24 SWAA051820 120050620A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM AFT CARGO BAY CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 767, LBL 17, WL 148. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050624001042005062400104NM 2005 6 24 SWAA051830 120050621A53226546529 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 400, STR 14R. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050624001052005062400105NM 2005 6 24 SWAA051831 120050621A53116516301 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND 2 EA FUSELAGE STUB FRAMES CRACKED AT BS 188, LT & RT SIDE, WL 208. REMOVED AND REPLACED STUB FRAMES PER SRM. 2L72 4F RTA16WE 20050624001072005062400107NM 2005 6 24 SWAA051833 120050621A3350MS155721 BULB BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29324SW 23414 DURING SCHEDULED SERVICE CHECK, FOUND RT AFT EXTERNAL EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050624001092005062400109 2005 6 24 SWAA051835 420050621A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29444WN 29839 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050624001112005062400111NM 2005 6 24 SWAA051837 120050621A55236959227 BUSHING BOEING737 7373Q8 1384670NM LT ELEVATOR TAB WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 DURING SCHEDULED C1 CHECK, LT ELEVATOR TAB FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR TAB NR 1 & 2 HINGE BUSHINGS & HARDWARE PER MM. 2L72 4F RTA16WE 20050624001142005062400114NM 2005 6 24 PIDA20050056 120050614A5751 SKIN BOEING737 737291 138448WNM AILERON DELAMINATED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05583CC 21069 LEFT AILERON DELAMINATED. REMOVED AILERON, REPAIRED PER SRM, BALANCED AND REINSTALLED. 2L72 4F A16WE 20050624001162005062400116NM 2005 6 24 PIDA200050052 120050610A5320 INTERCOSTAL BOEING737 737400 138449ANM FUSELAGE DAMAGED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05801DM 26240 SCRATCHES ON INTERCOSTALS FROM BS1640 TO BS1681 AT BL0. REPLACED INTERCOSTALS PER BOEING DRAWING 146N5230 AND SRM 51-10-2. 2L72 4F RTA16WE 20050624001182005062400118NM 2005 6 24 PIDA20050055 120050610A335020131A BATTERY PACK BOEING737 737400 138449ANM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05801DM 26240 INTERIOR OVERWING DOOR EMERGENCY EXIT LIGHT IS INOP. REPLACED BATTERY PACK AND OPS CHECKED PER MM 33-51-00. 2L72 4F RTA16WE 20050624001192005062400119NM 2005 6 24 PIDA20050053 120050610A5320 INTERCOSTAL BOEING737 737400 138449ANM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05801DM 26240 CORROSION ON INTERCOSTALS AT L4 DOOR FROM BS1640 TO BS1681 UNDER THE THRESHOLD DRAIN. REPLACED INTERCOSTALS PER BOEING DRAWING 146N5230 AND SRM 51-10-2. 2L72 4F RTA16WE 20050624001212005062400121NE 2005 6 24 PIDA20050050 220050606A7200 ENGINE BOEING737 7373G7 1384595NM GE CFM56 CFM56* 13802NE RIGHT BIRD INGESTION A PIDAC ABORTED TAKEOFF C F.O.D. TOTAKEOFF 1 SO05380WL 23218 726177 INGESTED BIRD IN RIGHT ENGINE AT ROTATION. VIBRATION INDICATION 4.0 UNITS AT POWER REDUCTION. INSPECTED ENGINE PER MM 71-00-47. UNSHINGLED BLADES NR 20, 21, 22, 23, AND 24. ALL ENGINE PARAMETERS AND VIBRATION CHECKS NORMAL ON ENGINE RUN. 2L72 4F4 FRTA16WE E2GL 20050624001232005062400123NM 2005 6 24 PIDA20050038 120050603A5347 MOUNT BOEING757 757200 1384950NM GALLEY CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05750WL 23928 CORROSION ON AFT GALLEY MOUNTS AT BS 1681 AND BS 1720 AT LBL54. REPLACED MOUNT FITTINGS PER SRM 51-10-00. 2L72 4F RTA2NM 20050624001242005062400124NM 2005 6 24 PIDA20050037 120050603A5320 CHANNEL BOEING757 757200 1384950NM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05750WL 23928 CORROSION ON HAT CHANNEL AT BS 1720 AT LBL 9. REPLACED HAT CHANNEL PER SRM 51-10-00. 2L72 4F RTA2NM 20050624001262005062400126NM 2005 6 24 PIDA20050036 120050603A5320 INTERCOSTAL BOEING757 757200 1384950NM THRESHOLD CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05750WL 23928 CORROSION ON R-4 DOOR THRESHOLD INTERCOSTALS FROM BS 1640 TO BS 1681 AT RBL60. REPAIRED INTERCOSTALS PER SRM 51-70-11. 2L72 4F RTA2NM 20050624001282005062400128NM 2005 6 24 PIDA20050047 120050603A5320 INTERCOSTAL BOEING757 757200 1384950NM THRESHOLD CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05750WL 23928 R-2 DOOR THRESHOLD INTERCOSTAL AT BS 730 CORRODED. REPLACED INTERCOSTAL PER SRM 51-40-00. 2L72 4F RTA2NM 20050624001302005062400130NM 2005 6 24 PIDA20050048 120050603A5320 INTERCOSTAL BOEING757 757200 1384950NM THRESHOLD CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05750WL 23928 L-2 DOOR THRESHOLD INTERCOSTALS FROM BS 680 TO BS 740 CORRODED. REPLACED INTERCOSTALS PER SRM 51-10-00. 2L72 4F RTA2NM 20050624001332005062400133NM 2005 6 24 PIDA20050027 120050603A5320 STRAP BOEING757 757200 1384950NM FLOORBEAM BROKEN A PIDAK NONE O OTHER ININSP/MAINT 1 SO05750WL 23928 RIGHT O/B SONIC VIBRATION STRAP BROKEN AT BS 1380. REPAIRED PER SRM 51-70-13 (FIG 1). 2L72 4F RTA2NM 20050624001352005062400135NM 2005 6 24 PIDA20050025 120050603A5315 FLOORBEAM BOEING757 757200 1384950NM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05750WL 23928 CORROSION ON BS 1320 FLOORBEAM FROM LBL 16 TO LBL 58. REPAIRED PER SRM 53-00-51. 2L72 4F RTA2NM 20050624001392005062400139NM 2005 6 24 PIDA20050031 120050603A5320 ANGLE BOEING757 757200 1384950NM CARGO BIN CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05750WL 23928 CORROSION ON TRANSITION ANGLE IN AFT CARGO BIN FROM BS 1460 TO BS 1480 AT STR 26 RT. REPLACED RIGHT TRANSITION ANGLE FROM BS 1440 TO BS 1530 PER SRM 51-10-00 AND SRM 51-40-02. 2L72 4F RTA2NM 20050624001412005062400141NM 2005 6 24 PIDA20050029 120050603A5340 ATTACH ANGLE BOEING757 757200 1384950NM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05750WL 23928 CORROSION AT BS 1560 FRAME TO SIDEWALL ATTACH ANGLE AT STR 26 RT. REPLACED ATTACH ANGLE PER SRM 51-10-02. 2L72 4F RTA2NM 20050624001432005062400143NM 2005 6 24 PIDA20050044 120050603A5320 ANGLE BOEING757 757200 1384950NM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05750WL 23928 L-ANGLE CORRODED BS 1260 TO BS 1280 AT RBL 64. REPAIRED PER SRM 51-70-12. 2L72 4F RTA2NM 20050624001452005062400145NM 2005 6 24 PIDA20050042 120050603A5347 MOUNT BOEING757 757200 1384950NM LAVATORY CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05750WL 23928 LAVATORY MOUNTS CORRODED AT BS 1280 AT LBL 25. REPLACED MOUNT FITTINGS PER SRM 51-10-00. 2L72 4F RTA2NM 20050624001482005062400148NM 2005 6 24 PIDA20050034 120050603A5340 ATTACH ANGLE BOEING757 757200 1384950NM CARGO BIN BROKEN A PIDAK NONE O OTHER ININSP/MAINT 1 SO05750WL 23928 ATTACH ANGLE BROKEN AT BS1300 +3 AT LBL3 IN AFT CARGO BIN. REPLACED ATTACH ANGLE PER SRM 51-10-02. 2L72 4F RTA2NM 20050627000032005062700003EA 2005 6 27 SWIA200515089 120050602A274170609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CRCRUISE 1 NM07916SW1023 1023 7634 "STAB CH 1 INOP" STATUS MSG IN FLIGHT. REPLACED HSTCU IAW CRJ 200 MM CHAPTER 27-41-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050627000082005062700008SO 2005 6 27 SWIA200515095 120050531A27203081401003 ACTUATOR EMB 120 EMB120ER 3260203SO RT RUDDER INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07560SW1195811958 120334 UNABLE TO PRESS RIGHT RUDDER FAST 2" OF CENTER. REPLACED BLUE RUDDER ACTUATOR IAW 27-22-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050627000102005062700010EA 2005 6 27 SWIA200515097 120050601A27604916406 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07407SW994 994 7034 SPOILERON FAULT STATUS MSG. REPLACED NR 1 SECU IAW 27-60-00, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050627000112005062700011EA 2005 6 27 SWIA200515098 120050602A276052C52610 MANIFOLD CNDAIRCL600 CL6002B19 1900309EA GROUND SPOILER MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07455SW 7760 INBOARD GROUND SPOILER FAULT ON TAXI IN. INSTALLED SERVICEABLE MANIFOLD ASSY FOR INBOARD GROUND SPOILERS. REPLACED SECU NR 1 AND NR 2 IAW MM 27-61-04. OPS CK GOOD. P/N OFF 49-164-06 S/N OFF 01786, 01787. 2L72 4F RTA21EA 20050627000122005062700012SO 2005 6 27 SWIA200515099 120050524A3330 BALLAST EMB 120 EMB120ER 3260203SO CARGO LIGHTS SMOKE A SWIAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM07569SW 120344 ON TAXI OUT, SMELLED SMOKE IN CABIN/COCKPIT THEN RECEIVED BAGGAGE COMPARTMENT FIRE/SMOKE INDICATION. REPLACED LIGHT BALLASTS AS NEEDED. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050627000192005062700019EA 2005 6 27 SWIA200515106 120050531A2741 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA COCKPIT STICKING A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07433SW 7550 CAPTAINS TRIM SWITCH STICKY. REPLACED CAPTAINS TRIM SWITCH IAW MM 27-41-05. OPERATIONAL CHECK GOOD IAW MM 27-40-00. 2L72 4F RTA21EA 20050627000202005062700020SO 2005 6 27 SWIA200515107 120050604A275012064207615 HANDLE EMB 120 EMB120ER 3260203SO TE FLAP MALFUNCTIONED A SWIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM07290SW4026 4026 120317 ON TAXI OUT, WHEN FLAP SELECTOR PUT AT 15 DEGREE POSITION, GOT FLAP AND ADV SWS ON MAP, CONTROL FAULT AND ALL FLAP BARS FLASHING. REPLACED FLAP SELECTOR HANDLE ASSY. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050627000212005062700021EA 2005 6 27 SWIA200515108 120050515A5321 FLOOR PANEL CNDAIRCL600 CL6002B19 1900309EA E/E BAY CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07592SW 7279 FS 193 - LEFT SIDE ELECTRICAL BAY FLOOR CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED CRACK IAW CRJ REO 601R-53-11-001 REV NC. 2L72 4F RTA21EA 20050627000222005062700022EA 2005 6 27 SWIA200515109 120050515A5210 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07592SW 7279 PAX DOOR TOP STEP HAS CORROSION ON HINGE, ITEM FOUND AT C-CHECK INSPECTION. HINGE REPLACED IAW CRJ SRM 51-41-02. 2L72 4F RTA21EA 20050627000232005062700023EA 2005 6 27 SWIA200515110 120050515A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSLEAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07592SW 7279 FLOOR ANGLE CORRODED IN NUMEROUS LOCATIONS FROM FS 409 +128 TO FS 559 AND RBL 36 TO 47, ITEM FOUND AT C-CHECK INSPECTION. BLENDED OUT DAMAGE IAW CRJ SRM 53-41-45 PAGE 101-108, FOUND TO BE WITHIN LIMITS IAW SRM 53-41-45. 2L72 4F RTA21EA 20050627000242005062700024EA 2005 6 27 SWIA200515111 120050515A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07592SW 7279 FLOOR ANGLE CORRODED IN NUMEROUS LOCATIONS FROM FS 409 +128 TO FS 559 AND LBL 36 TO 47, ITEM FOUND AT C-CHECK INSPECTION. BLENDED OUT DAMAGE IAW CRJ SRM 53-41-45 PAGE 101-108. FOUND TO BE WITHIN LIMITS IAW SRM 53-41-45. 2L72 4F RTA21EA 20050627000262005062700026EA 2005 6 27 SWIA200515113 120050520A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07964SW 7868 FS 280 AT RBL 9.0 OUTBOARD FLOORBEAM ATTACH ANGLE IS CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-21, 51-23-00, 51-21-11, 51-42-06. 2L72 4F RTA21EA 20050627000272005062700027EA 2005 6 27 SWIA200515114 120050520A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07964SW 7868 FS 621 AT LBL 41 FLOORBEAM ANGLE IS CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FLOOR SUPPORT ANGLE AS PER IAW REO 6014-53-61-117 REV "B" . 2L72 4F RTA21EA 20050622001602005062200160NM 2005 6 22 USAA050716 120050601A5320 SPLICE BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19445US 24863 CLT - FOUND SPLICE PLATE CORRODED 3.75 INCH, AFT CARGO COMPARTMENT AT STATION 771 FLOORBOARD. FABRICATED AND INSTALLED A NEW SPLICE PLATE IAW BOEING DRAWING 65C26459 AND SRM 51-10-02. (M) 2L72 4F RTA16WE 20050622001622005062200162NM 2005 6 22 USAA050712 120050602A5320 ANGLE BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19445US 24864 CLT - FOUND TRANSITIONAL ANGLE CORRODED .3125 INCH, FS 727B-847. FABRICATED AND INSTALLED TRANSITION ANGLE AND COVE PANEL IAW 737 SRM 57-43-01, 53-60-53. (M) 2L72 4F RTA16WE 20050622001662005062200166EA 2005 6 22 ASOA05395 120050502A5730 SKIN PANEL CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27849AS 7347 DURING A C-CHECK IN MCN, THE LOWER WING PLANK AT WS 148.019 LEFT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LOWER WING PLANK AT WS 148.019 LEFT IAW ASA EO 600-57-0134A. (M) 2L72 4F RTA21EA 20050622001832005062200183EA 2005 6 22 ASOA05441 120050515A33501951001 LIGHT CNDAIRCL600 CL6002C10 1390015EA EMERGENCY EXIT WEAK A ASOAK NONE O OTHER ININSP/MAINT 1 SO27701EV 10020 DURING A GROUND INSPECTION IN SLC, THE EMERGENCY EXIT PLACARD ON THE FORWARD SERVICE DOOR HANDLE WAS FOUND NOT TO FULLY ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT BETA LIGHT ON THE FORWARD SERVICE DOOR HANDLE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050622001852005062200185EA 2005 6 22 ASOA05453 120050521A5210601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27870AS 7530 DURING A GROUND INSPECTION IN ATL, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050622001882005062200188EA 2005 6 22 ASOA05419 120050508A5210601R3807413 ANCHOR FITTING CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27867AS 7483 DURING A C-CHECK IN MCN, THE AFT CABLE ANCHOR MOUNT FITTING ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFT CABLE ANCHOR MOUNT FITTING ON THE PASSENGER DOOR IAW CRJ AMM 52-00-00. (M) 2L72 4F RTA21EA 20050622001942005062200194EA 2005 6 22 ASOA05416 120050508A3250 STEERING SYS CNDAIRCL600 CL6002B19 1900309EA NLG UNKNOWN A ASOAO OTHER O OTHER NRNOT REPORTED 1 SO27828AS 7213 DURING TAKEOFF FROM MSP-CVG, UPON GEAR RETRACTION THE CREW RECEIVED GEAR DISAGREE WARNING, NOSE DOOR OPEN WARNING, STEERING INOPERATIVE CAUTION, AND WEIGHT ON WHEELS INPUT CAUTION MESSAGES. THE QRH WAS COMPLIED WITH. AN EMERGENCY WAS DECLARED DUE TO THE LOSS OF NOSE WHEEL STEERING. THE AIRCRAFT RETURNED TO MSP AND LANDED SAFELY WITH EXCEPTION TO THE NOSE WHEEL STEERING BEING INOPERATIVE. THE AIRCRAFT WAS SAFELY TOWED TO THE GATE. MAINTENANCE FOUND THE NOSE LANDING GEAR SCISSOR LINKS DISCONNECTED AND RECONNECTED THEM. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE NOSE WHEEL STEERING, INSPECTED THE NLG AND NG AREA WITH NO DEFECTS NOTED AND RESTOWED THE MLG RELEASE HANDLE. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050622002012005062200201EA 2005 6 22 MASA205500076 120050131A2910601R752863 LINE CNDAIRCL600 CL6002B19 1900309EA HYDRAULIC SYS CRACKED A MASAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0737228 7228 ASH 6318 SBA - LAX, PILOT DIVERTED INTO LAX EN ROUTE TO PHX DUE TO NR 1 HYD QUANTITY AND PRESSURE LOW. MAINTENANCE FOUND A CRACKED LINE AT THE NR 1 CASE DRAIN FILTER. 1/31/05 MAINTENANCE INSTALLED A TEMP HYD LINE, SERVICED HYD SYSTEM OPS CHECKED GOOD. LATER THE PERM HYD LINE WAS INSTALLED. OPS CHECKED GOOD. 2L72 4F RTA21EA 20050622002122005062200212EA 2005 6 22 MASA200500136 120050220A3213 STRUT CNDAIRCL600 CL6002B19 1900309EA NLG DAMAGED A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07652ML 7036 ASH 2762 FROM PHL TO ALB RETURNED TO THE FIELD DUE TO A GEAR DISAGREE. MAINTENANCE IS IN THE PROCESS OF TROUBLESHOOTING. MAINTENANCE REPLACED THE NOSE LANDING GEAR STRUT ASSY, OPS CHECKED GOOD ON THE GROUND. 2L72 4F RTA21EA 20050622002172005062200217NE 2005 6 22 PNSA050601 220050607A7200 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT7TP* 30030NE LEFT MALFUNCTIONED A PNSAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 AL03665PA 340B181 LT ENGINE HAD AUTO IGNITION EVENT DURING CRUISE IN CLOUDS WITH ANTI-ICE SYSTEM ON. NO VISIBLE ICE NOTED BY CREW HOWEVER THERE WAS ICE FORCAST. CREW REPORTED 1 IGNITION RELIT AND CONFIRMED IGNITION LIGHTS ON. ALL OTHER PARAMETERS NORMAL. CREW ELECTED TO RETURN TO ANC WHERE MAINTENANCE BORESCOPED COMPRESSOR AND CHECKED ENGINE ANTI-ICE SYSTEM. EVERYTHING WAS FOUND NORMAL AND AIRCRAFT RELEASED FOR SERVICE. NO OTHER PROBLEMS NOTED ON LATER FLIGHTS. 2L72 4T4 TRTA52EU E8NE 20050622002422005062200242NM 2005 6 22 DHL2005741543 120050418A5754 SKIN BOEING727 7272Q9 138448MNM NR 5 SLAT DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH46665 21931 FOUND DENT TO BE OUT OF LIMITS ON NR 5 SLAT L/E SKIN WS 330- 357 IAW B727 SRM 57-50-1 FIG 2. REPAIRED IAW SRM. 2L73 4F RTA3WE 20050622002472005062200247NM 2005 6 22 DHL2005784510 120050517A5531 RIB BOEING727 727227 1384078NM VERTICAL STAB WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01784DH 22001 VERT STAB L/E PNL NR 9501 UPPER FORMER RIB IS WORN FIN STA 87. DAMAGED AREA FOUND TO BE OUT OF LIMITS IAW B727 SRM 55-30-1. REPAIRED IAW B727 SRM. 2L73 4F A3WE 20050622002492005062200249NM 2005 6 22 DHL2005784512 120050517A5524 ANGLE BOEING727 727227 1384078NM ELEVATOR SKIN CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01784DH 22001 RT ELEVATOR LOWER SKIN INBD ANGLE SUPPORT AFT OF L/E IS CRACKED AT OUTBD END, ELEV STA 17.2. REPAIRED IAW SRM. 2L73 4F A3WE 20050623000042005062300004SO 2005 6 23 SWIA200515142 120050613A2797 CONNECTOR EMB 120 EMB120ER 3260203SO TE FLAPS DIRTY A SWIAO OTHER J WARNING INDICATION CRCRUISE 1 NM07296SW 120325 IN CRUISE FLIGHT, RECEIVED CONTROL FAULT ON FLAPS. REPLACED STALL WARNING TEST PANEL ON CENTER PEDESTAL. CLEANED LEFT WING OUTBOARD FLAP CONNECTOR. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050623000112005062300011EA 2005 6 23 MASA200500400 120050505A3220 INDICATOR CNDAIRCL600 CL6002B19 1900309EA MLG MALFUNCTIONED A MASAO OTHER N FALSE WARNING DEDESCENT 1 SW07154SF 7154 ASH 6087 MFR TO PHX. DURING FINAL DESCENT, THE NOSE GEAR INDICATION WAS RED DASHES WITH NO WARNINGS OR AURALS. MAINTENANCE CYCLED THE GEAR AND OPS WERE NORMAL. 2L72 4F RTA21EA 20050623000142005062300014NM 2005 6 23 05FDEA01610 120050615A5710 STRINGER BOEING727 727200 138407ENM RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25477FE 21394 WHILE WORKING N00525, FOUND RT WING UPPER STRINGER NR 10 CRACKED AT WS 686.5 RIB BOLT. REPAIRED STRINGER PER FED EX EA 7-5710-86308. 2L73 4F RTA3WE 20050623000242005062300024EA 2005 6 23 MASA200500275 120050403A5270 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR UNSECURE A MASAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW0747239 7239 ASH 7024 ORD. RETURNED TO GATE FOR A PAX DOOR HANDLE CAUTION MESSAGE ON TAXI OUT. MAINTENANCE FOUND THE DOOR HANDLE POPPED UPON RETURN TO GATE. MAINTENANCE PERFORMED OPS CHECKS OF DOOR LATCH AND INDICATION SYSTEM AND COULD NOT DUPLICATE FAULT. 2L72 4F RTA21EA 20050623000362005062300036NM 2005 6 23 72300213 120050528A5315 FLOORBEAM BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 8 INCH AREA OF CORROSION ON FLOORBEAM. 2L73 4F4 FRTA3WE E2EA 20050623000372005062300037NM 2005 6 23 72300214 120050603A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 14 INCH AREA OF CORROSION ON STRINGER. 2L73 4F4 FRTA3WE E2EA 20050623000382005062300038NM 2005 6 23 72300215 120050604A5311 FRAME BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 2 X 2 INCH AREA OF CORROSION ON FRAME. 2L73 4F4 FRTA3WE E2EA 20050623000462005062300046NE 2005 6 23 AC2A101188 120050606A63107636104008103 DISC PACK SKRSKYS76 S76A 8143006NE MAIN ROTOR CRACKED B AC2AK NONE O OTHER ININSP/MAINT 1 SO175402T 760140 NR 1 ENGINE, MAIN ROTOR DRIVE SHAFT HAD 10 CRACKED DISCS ON FORWARD DISC PACK. DISC PACKS WERE REPLACED ON BOTH ENDS OF DRIVESHAFT. THE ENGINE TO TRANSMISSION DRIVESHAFT ALIGNMENT WAS CHECKED AND FOUND TO BE WITHIN LIMITS. A VIBRATION CHECK WAS RUN ON THE TRANSMISSION INPUT SECTIONS AND FOUND TO BE OK. 1G72 3U H1NE 20050623000542005062300054NM 2005 6 23 QXEA200500962 120050604A2611 SMOKE DETECTOR BOMBDRDHC8 DHC8402 1390042NM LAVATORY ACTIVATED A QXEAO OTHER J WARNING INDICATION APAPPROACH 1 NM09405QX 4047 LAVATORY SMOKE DETECTOR WENT OFF. FLT ATTENDANTS REPORT SMOKE IN CABIN. SMOKE CONCENTRATED IN MIDDLE OF CABIN. MX INTERROGATED CDS, FOUND 3B01 FAULT ON DISTRIBUTION DAMPER. REMOVED FLOOR PANEL 143BZ TO ACCESS DISTRIBUTION DAMPER. DISTRIBUTION DAMPER OPS CHECK GOOD. REINSTALLED FLOOR PANEL 143BZ. GROUND RAN ACFT. OPERATED ECS SYSTEM. DID NOT GET LAVATORY SMOKE DETECTOR TO GO OFF AND DID NOT RECEIVE ANY SMOKE IN CABIN. NO FAULTS RECORDED IN CDS. NO PARTS REPLACED. ACFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050623000692005062300069EU 2005 6 23 KBM2005F00104 120050511A6410355A09103601 BEARING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE TAIL ROTOR TORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19345SH496 3345 HALF SHELL BEARING KIT, TORN LAMIFICATIONS, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050623000702005062300070EU 2005 6 23 KBM2005F00105 120050511A6310350A35110500 GIMBAL RING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE MAIN ROTOR DEBONDED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19345SH 3345 GIMBAL RING DEBONDED, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050623000712005062300071EU 2005 6 23 KBM2005F00106 120050527A2110590008 COMPRESSOR SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE AIR CONDITIONER BURNED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH 2957 AIR CONDITIONING COMPRESSOR LEAKING OIL AND CLUTCH BURNED. NEEDS NEW CLUTCH/COIL ASSEMBLY. (K) 1G71 3U3 UNCH9EU E19EU 20050623001042005062300104NM 2005 6 23 QXEA200501007 120050604A3230 SEQUENCE VALVE DHAV DHC8 DHC8202 2809007NM ZONE 200 MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION DEDESCENT 1 NM09366PH11584517 510 LANDING GEAR INOP CAUTION ILLUMINATED. FLIGHT CREW PERFORMED ALTERNATE EXTENSION OF GEAR AND LANDED WITHOUT INCIDENT. MX REPLACED PSEU FOR FAULT CODE 63 (SEQUENCE VALVE). OPS CHECKS GOOD. ACFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050623001162005062300116NM 2005 6 23 QXEA200500971 120050503A2760 WARNING LIGHT BOMBDRDHC8 DHC8402 1390042NM DRAG CONTROL SYSILLUMINATED A QXEAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM09417QX 4086 ROLL SPOILER INBOARD GROUND AND ROLL SPOILER OUTBOARD GROUND CAUTION LIGHTS CAME ON DURING TAXI TO GATE. COMPLIED WITH CHECKLIST AND PROBLEM DID NOT REOCCUR. OCCURRENCE NOTED BY MX CONTROL. NO FAULT FOUND. ACFT OK FOR CONTINUED SERVICE. 2H72 4T RTA13NM 20050623001242005062300124NM 2005 6 23 QXEA200501018 120050404A5210 DOOR DHAV DHC8 DHC8202 2809007NM ZONE 800 STIFF A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09366PH 510 FLIGHT ATTENDANT REPORTS MAIN CABIN DOOR STIFF TO OPEN. CHECK OPERATION OF DOOR IAW D-8 MM 52-10-00. FOUND TO BE WITHIN LIMITS. NO PARTS REPLACED. ACFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050623001282005062300128NM 2005 6 23 USAA050580 120050426A5320 ANGLE BOEING757 757225 1384959NM RROYCERB211 RB211535E4 54555NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19608AU64222 22204 BFM - C4 CHECK- ANGLE AREA EXCEEDS 30 PERCENT OF ANGLE, CRACKED AND BROKEN, BS 780-800 AT BL0. REMOVED (FAB ANGLE IAW SAMPLE) AND INSTALLED NEW IAW SRM. (K) 2L72 4F4 FRTA2NM E12EU 20050623001422005062300142NM 2005 6 23 72300201 120050323A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 1 AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050623001462005062300146NM 2005 6 23 72300205 120050418A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A .75 X .5 INCH AREA OF CORROSION ON STRINGER. 2L73 4F4 FRTA3WE E2EA 20050623001542005062300154WP 2005 6 23 P9RA20050093 120050617A5260 MECHANISM DOUG DC9 DC982 3022082WP AIRSTAIR LACK OF LUBE A P9RAO OTHER J WARNING INDICATION DEDESCENT 1 SO1110801 49127 ON DESCENT INTO SJU, AFT AIRSTAIR DOOR LIGHT ILLUMINATED. DECALRED EMERGENCY. PRIOR TO LANDING, THE LIGHT EXTINGUISHED. PERFORMED ADJUSTMENT TEST PER M/M INSTRUCTIONS. LUBRICATED CONTROL CABLE PULLEY MECHANISM OF AFT AIRSTAIRS. CLEANED AND VERIFIED UP LATCH SWITCH OPERATION. NO DEFECTS NOTED. AIRCRAFT RELEASED FOR CONTINUED SERVICE. NO PART REPLACEMENT AT THIS TIME. 2L72 4F A6WE 20050623001652005062300165NM 2005 6 23 WRLA200588 120050614A5512 PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 ITEM: DURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST LT BARREL NUT HOLE NR 7.(OPEN) 2L73 4F4 FRTA22WE E24NE 20050623001692005062300169NM 2005 6 23 WRLA200592 120050614A5511 PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST LT BARREL NUT HOLE NR 15.(OPEN) 2L73 4F4 FRTA22WE E24NE 20050624000042005062400004NM 2005 6 24 WRLA2005105 120050614A5512 PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE NR 15. 2L73 4F4 FRTA22WE E24NE 20050624000052005062400005NM 2005 6 24 WRLA2005106 120050614A5512 PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE NR 17. 2L73 4F4 FRTA22WE E24NE 20050624000082005062400008NM 2005 6 24 WRLA2005108 120050616A5512 PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE NR 20. 2L73 4F4 FRTA22WE E24NE 20050624000092005062400009EA 2005 6 24 COMA0570068 120050614A3220 CYLINDER CNDAIRCL600 CL6002C10 1390015EA NLG DAMAGED A COMAK NONE O OTHER ININSP/MAINT 1 SO01340CA7435 10062 NLG OUTER CYLINDER P/N 52101-1, S/N BA0025 HAS HOLE IN THE CHROME BAND. REPAIR NLG OUTER CYLINDER IAW BOMBARDIER REO 670-32-21-0059 AND GOODRICH SCR 0024-05. 2L72 4F RTA21EA 20050624000102005062400010EA 2005 6 24 COMA0570069 120050614A3220 CYLINDER CNDAIRCL600 CL6002C10 1390015EA NLG CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01340CA7435 10062 NLG OUTER CYLINDER P/N 52101-1, S/N BA0025 CORRODED. CORROSION REPAIRED IAW BOMBARDIER REO 670-32-21-058, GOODRICH SCR 0008-04 REV C, BOMBARDIER REO 670-32-21-0030 AND GOODRICH SCR 0001-005. 2L72 4F RTA21EA 20050624000202005062400020NE 2005 6 24 RAIA00506022 220050615A7320940919 ACTUATOR JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114HR 01514NE RT ENG FUEL UNKNOWN A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03556HK11136 41073 FLT 5394 IND - NO HP FUEL PRESSURE ON THE RIGHT ENGINE. MAINTENANCE REMOVED AND REPLACED THE RT MOTIVE FLOW ACTUATOR AND PERFORMED AN ENGINE RUN. OPS CHECKED GOOD. 2L72 4T4 TRTA41NM E18NE 20050624000222005062400022CE 2005 6 24 71342 120050617A3242 BRAKE BEECH 1900 1900D 1154162CE MLG MALFUNCTIONED A AMWAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE07143YV UE143 AFTER LANDING IN DUJ AND TAXIING TO GATE WITH NO INCIDENT, CREW CALLED MAINTENANCE TO WRITE UP THE RIGHT BRAKE AS WEAK. MAINTENANCE BLED BRAKE. THEREFORE NO PARTS WERE USED. 2L72 4T RTA24CE 20050624000242005062400024EU 2005 6 24 05FDEA01618 120050616A2150 VALVE AIRBUS300 A300B4605R 3930308EU AVI COOLING STUCK A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25672FE 779 AFTER PUSHBACK AND BOTH ENGINES STARTED EQUIPMENT COOLING OVERBOARD VALVE FAULTED. FOLLOWED ECAM WHICH WAS TO TURN IT OFF. CHECK MEL-NOT FLAGGED ITEM. OVERBOARD VALVE WAS NOT USED BOTH PACKS OPERATING NORMALLY, CONTINUED FLIGHT. AFTER T/O, AIRCRAFT WOULD NOT HOLD PRESSERIZATION. TRIED MANUAL PRESSURIZATION, NO HELP. TRIED TO SLOW CLIMB, NO HELP. RETURNED TO IND, GOC TO MEM, NO PROBLEMS. AVI COOLING EXTRACTION VALVE IS STUCK FULL OPEN. REMOVED AND REPLACED OVERBOARD EXTRACT VALVE PER AMM 21-23-13-4, OPS CHECK GOOD. 2L72 4F RTA35EU 20050624000262005062400026NM 2005 6 24 QXEA200501066 120050618A2760 WARNING LIGHT BOMBDRDHC8 DHC8402 1390042NM SPOILERS FALSE ACTIVATIONA QXEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM09413QX 4060 BOI FLIGHT 2385, OUTBOARD SPOILER CAUTION ON CLIMBOUT. MAINTENANCE COMPLIED WITH FIM TASK NO FURTHER FAULTS NOTED. NO PARTS REPLACED AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050624000372005062400037NM 2005 6 24 UPS05444585 120050519A5313 STRINGER BOEING747 747123F NM AFT CARGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSP TYPE: C AFT CARGO COMPT BS 1645 STR 35R STRINGER CORRODED. CORROSION BLENDED OUT 0.039 INCHES BY 0.25 INCHES BY 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. AFT CARGO COMPT BS 1645 STR 35R REPAIRED AS PER SRM 53-10-03 FIG 2. 2L74 4F A20WE 20050624000542005062400054NM 2005 6 24 MASA200500364 120050517A3350 LIGHT DHAV DHC8 DHC8202 2809007NM CABIN LOOSE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07989HA 427 CREW NOTED THAT EMERGENCY FLOOR PATH LIGHTING STRIP COVER LOOSE. MX RESECURED THE COVER. 2H72 4T RTA13NM 20050624000562005062400056EA 2005 6 24 MASA200500369 120050519A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSINOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0737208 7208 CREW FOUND EMERGENCY LIGHT AT PAX DOOR ON OUTSIDE OF ACFT INOPERATIVE. MX REPLACED LIGHT BULB, OPS CHECKED GOOD AND ACFT CONTINUED OPERATIONS. 2L72 4F RTA21EA 20050624000582005062400058SO 2005 6 24 MASA200500375 120050520A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07835MJ 145353 2 EACH FLOOR EMERGENCY PROXIMITY LIGHT STRIPS INOP AT ROW 12. MX PERFORMED OPS CHECK AND FLOOR LIGHT STRIPS OPERATED NORMALLY. ACFT DEPARTED WITHOUT FURTHER INCIDENT. 2L72 4T RTT00011AT 20050624000712005062400071EU 2005 6 24 06172005 120050617A3234 HANDLE SAAB SF340 340B 7860101EU LANDING GEAR MALFUNCTIONED A NSVAO OTHER J WARNING INDICATION APAPPROACH 1 EA27339CJ 339 LANDING GEAR WOULD NOT COME DOWN OR PUMP DOWN. BLEW EMERGENCY BOLTS TO EXTEND. 2L72 4T RTA52EU 20050624000772005062400077EA 2005 6 24 COMA0560354 120050616A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION CRCRUISE 1 SO01981CA 7163 FLIGHT 5611- EN ROUTE LAN - CVG RECEIVED A FLAP FAIL CAUTION AT ZERO DEGREE FLAP POSITION. AIRCRAFT LANDED WITHOUT INCIDENT. FLAP SYSTEM WAS RESET. 2L72 4F RTA21EA 20050624000872005062400087NM 2005 6 24 BB05045 120050622A3397 WIRE BOEING767 7672B7 1385107NM EMERGENCY LIGHT DISCONNECTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19656US 26847 CLT - FOUND FLOOR EMERGENCY LIGHT AT ROWS 1 THROUGH 3, LEFT, INOPERATIVE. MAINTENANCE RESECURED A DISCONNECTED WIRE. 2L72 4F RTA1NM 20050624000902005062400090NM 2005 6 24 SWAA051822 120050620A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM AFT CARGO BAY CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND 2 EA FUSELAGE SHEAR TIES CORRODED AT BS 827 & BS 847, RBL 5 TO BL 0, WL 149. REMOVED AND REPLACED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20050624000972005062400097NM 2005 6 24 SWAA051817 120050620A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM AFT CARGO BAY CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 747, RBL 16 TO RBL 20, WL 148. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050624001032005062400103NM 2005 6 24 SWAA051829 120050621A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 727A, STR 14R. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050624001062005062400106NM 2005 6 24 SWAA051832 120050621A53216517590 FLOOR PANEL BOEING737 7373H4 1384600NM COCKPIT FLOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND 2 EA FUSELAGE FLOOR WEB CRACKS BETWEEN BS 188 TO BS 197, LT & RT SIDE, WL 208. REPAIRED FLOOR WEB PER SRM. 2L72 4F RTA16WE 20050624001102005062400110NM 2005 6 24 SWAA051836 120050621A53116546569 BELTFRAME BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29508SW 24185 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE BELT FRAME WEB CRACKED AT BS 1040, LT SIDE BLEED AIR DUCT. REPAIRED BELT FRAME WEB PER SRM. 2L72 4F RTA16WE 20050624001122005062400112NM 2005 6 24 SWAA051838 120050621A3040 CONTROLLER BOEING737 7377H4 1384404NM WINDSHIELD HEAT FAILED A SWAAA UNSCHED LANDING O OTHER CLCLIMB 1 SW29719SW 27853 DIVERSION, CLIMBING THROUGH 31,000 FT - R1 COCKPIT WINDSHIELD SHATTERED. REMOVED AND REPLACED R1 WINDSHIELD & HEAT CONTROLLER. 2L72 4F RTA16WE 20050624001152005062400115NM 2005 6 24 PIDA20050057 120050614A5314 KEELBEAM BOEING737 737291 138448WNM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05583CC 21069 CORROSION AND CRACK IN THE LOWER CHORD OF THE KEEL BEAM AT BS540. CUT OUT DAMAGE. FABRICATED AND INSTALLED REPAIR ANGLES AND SPLICES PER RRG2377 REV. A DATED 6/13/05 WITH DER APPROVED 8110-3 DATED JUNE 13, 05. 2L72 4F A16WE 20050624001172005062400117NM 2005 6 24 PIDA200050051 120050610A5320 INTERCOSTAL BOEING737 737400 138449ANM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05801DM 26240 CORROSION ON INTERCOSTAL AT R4 DOOR FROM BS1640 TO BS1681 AT RBL56. REPAIRED INTERCOSTAL PER SRM 51-70-11. 2L72 4F RTA16WE 20050624001292005062400129NM 2005 6 24 PIDA20050049 120050603A5320 WEB BOEING757 757200 1384950NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05750WL 23928 WEB PANEL CRACKED IN THREE PLACES BETWEEN BS 660 AND BS 680 AT BBL0. REPAIRED SUPPORT ANGLE PER SRM 53-00-51. 2L72 4F RTA2NM 20050624001402005062400140NM 2005 6 24 PIDA20050030 120050603A5340 ATTACH ANGLE BOEING757 757200 1384950NM CARGO BIN CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05750WL 23928 CORROSION ON SHEAR WEB UPPER ATTACH ANGLE IN AFT CARGO BIN FROM BS 1480 TO BS 1500 AT STR 26LT. REPLACED ATTACH ANGLE PER SRM 51-40-02. 2L72 4F RTA2NM 20050624001442005062400144NM 2005 6 24 PIDA20050043 120050603A5347 MOUNT BOEING757 757200 1384950NM LAVATORY CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05750WL 23928 LAVATORY MOUNTS CORRODED AT BS 1280 AND BS 1315. REPLACED MOUNT FITTINGS PER SRM 51-10-00. 2L72 4F RTA2NM 20050627000172005062700017EA 2005 6 27 SWIA200515104 120050604A276052C52610A1 MANIFOLD CNDAIRCL600 CL6002B19 1900309EA GROUND SPOILER MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07455SW942 942 7760 INBOARD GROUND SPOILER FAULT STATUS MSG. REMOVED AND REPLACED INBOARD GROUND SPOILER MANIFOLD IAW AMM 27-63-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050627000282005062700028EA 2005 6 27 SWIA200515115 120050520A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07964SW 7868 FS 621 AT RBL 41 FLOORBEAM ANGLE IS CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FLOOR SUPPORT ANGLE IAW CRJ REO 601R-53-61-117 REV "B". 2L72 4F RTA21EA 20050627000312005062700031EA 2005 6 27 SWIA200515118 120050612A2741 TRIM SWITCH CNDAIRCL600 CL6002C10 1390015EA COCKPIT STICKING A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07713SK 10174 CA'S TRIM SWITCH IS STICKING. REPLACED CAPTIANS TRIM SWITCH IAW MM 27-41-00. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050627000322005062700032EA 2005 6 27 SWIA200515119 120050612A274170744 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA STAB TRIM MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07703SK 10139 STAB CHANNEL/2 STATUS MESSAGE ON EICAS. REPLACED STAB TRIM MOTOR CONTROL UNIT IAW CRJ 700 MM 27-42-07. OPERATIONAL CHECK GOOD IAW CRJ MM 27-61-05. 2L72 4F RTA21EA 20050627000332005062700033SO 2005 6 27 SWIA200515120 120050607A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT DISCHARGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07189SW9768 9768 120048 AFT EMERGENCY FLOOR LIGHTING INOPERATIVE. REPLACED AFT EMERGENCY LIGHT BATTERY PACK IAW 33-50-00. OPERATIONAL CHECK GOOD, PN D366-04-001; SN ON 984; SN OFF 1058. 2L72 4T RTA31SO 20050627000352005062700035EA 2005 6 27 SWIA200515122 120050606A2740 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA STABILIZER INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07595SW 7292 STAB CH 1WILL NOT MOVE STAB TRIM. REPLACED CAPTIANS STAB TRIM SWITCH ON YOKE, OPERATIONAL CHECK GOOD IAW 27-41-00. 2L72 4F RTA21EA 20050627000382005062700038EA 2005 6 27 SWIA200515125 120050323A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAO OTHER O OTHER ININSP/MAINT 1 NM07958SW 7833 FS 621 LT FLOORBEAM ANGLE CRACKED AT LBL 41.0, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-61-117 REV B. 2L72 4F RTA21EA 20050627000392005062700039EA 2005 6 27 SWIA200515126 120050323A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07958SW 7833 PULLEY INTERCOSTAL CRACKED OB FLANGE; FS 484.00 LBL 36.0, ITEM FOUND AT C-CHECK INSPECTION. DAMAGE REPAIRED IAW CRJ REO 601R-53-41-059 REV A. 2L72 4F RTA21EA 20050627000462005062700046NM 2005 6 27 C1HA200594001 120050601A5753 ROLLER BOEING727 727290 138408WNM TE FLAP OUT OF ADJUST A C1HAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL15294AS 22146 ON CLIMBOUT APPROX 200, CREW BEGAN TO FEEL VIBRATION. ALL ENGINE INDICATIONS NORMAL. BEGAN TROUBLESHOOTING AND UPON VISUAL INSP FOUND LT INBOARD T/E FLAPS FLUTTERING APPROX 4 TO 5 INCHES AT SPEEDS ABOVE APPROX 290 KIAS. DECISION MADE TO AIR RETURN TO MMUN MADE AND PHONE PATCH ACQUIRED. APPROX 4000 LBS OF FUEL DUMPED IN ORDER TO LAND BELOW MAX LANDING WT SOC, MX CONTROL, DISPATCH, CHIEF PILOT NOTIFIED. INSP AIRFRAME VIBRATION CONDITION PER AMM 0551-181. FOUND AFT ROLLERS OUT OF ADJUSTMENT. ADJUSTED PER AMM 27-51-02/27-51-01 TO .012 INCH. ALL OTHER ITEMS FOUND WITHIN LIMITS. NO DEFECTS FOUND. OK FOR SVC. 2L73 4F A3WE 20050627000482005062700048SO 2005 6 27 C2XA05SH041 120050523A532014521700007 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717984 145246 DURING C CHECK, PREVIOUS REPAIR TO LT OMEGA BEAM AT FS 20 WAS FOUND TO BE CORRODED. MX REMOVED DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EMB 145 SRM 51-40-02 AND EMB 145 SRM 51-40-02, EC5320-01140 AND EC 5320-01137. ACFT APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050627000492005062700049SO 2005 6 27 C2XA05CL040 120050525A521014523092403 BELLCRANK EMB 135 EMB135ER 3260203SO MAIN CABIN DOOR WORN A C2XAO OTHER O OTHER TXTAXI/GRND HDL 1 SW2715509 145238 CREW REPORTED MAIN CABIN DOOR HARD TO OPEN. MX INSP AND REPLACED ACTUATING CAM BELLCRANK AND BUSHING. OPS CHECK GOOD. 2L72 4F RTT00011AT 20050627000502005062700050SO 2005 6 27 C2XA05BT033 120050527A2120 ODOR EMB 145 EMB145XR 3260214SO CABIN/COCKPIT DETECTED A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW2721129 145703 CREW REPORTED, "STRONG ODOR OF SMOKE IN CABIN AND COCKPIT". MX PERFORMED GENERAL VISUAL INSP OF BLEED SYSTEM DUCTS NR 1 AND NR 2 IAW EMB145XR AMM NR 36-11-09, NO DEFECTS NOTED. RAN BOTH ENGINES ON 2 DIFFERENT OCCASIONS IAW EMB145XR AMM NR 71-00-01 AT LOW AND HIGH POWER SETTINGS, CHECKED BOTH AIRBLEED SYSTEMS IAW EMB145XR AMM NR 36-00-00-700-803-A. NO SMOKE ODOR FOUND IN CABIN OR COCKPIT, SYSTEMS OPS CHECKED GOOD. 2L72 4F RT 20050627000512005062700051GL 2005 6 27 ALGA101180 220050602A7240E23008614 SHROUD BELL 206 206L1 1182107SW ALLSN 250C 250C28B 03013GL COMBUSTION LINERDEFECTIVE E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW031081K 45407 FUEL NOZZLE REMOVED FOR STARTING PROBLEM. HOUSING UNSCREWED FROM SHROUD. SHROUD STAYED IN LINER FERRULE. DIMENSIONALLY CHECKED LINER FOUND TOO SMALL AND TAPERED CAUSING INTERFERENCE FIT. REPLACED WITH SERVICEABLE LINER. 1G71 3U3 U H2SW E1GL 20050627000532005062700053SO 2005 6 27 MASA200500383 120050523A3350 LIGHT EMB 145 EMB145LR 3260212SO ROW 12 INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07843MJ 145478 CAPTAIN REPORTED OVERHEAD EMERGENCY LIGHT AT ROW 12 INOP. MX FOUND LIGHTS OPERATIONAL AFTER RESET. 2L72 4T RTT00011AT 20050627000552005062700055SO 2005 6 27 MASA200500390 120050524A3350 LIGHT EMB 145 EMB145LR 3260212SO RT OVERWING INOPERATIVE A MASAO OTHER L NO TEST NRNOT REPORTED 1 SW07837MJ 145367 CAPTAIN REPORTED RT OVERWING EMERGENCY ESCAPE LIGHT INOPERATIVE DURING TEST. MX RESET ELECTRICAL POWER TO ACFT AND LIGHT CHECKED OK. 2L72 4T RTT00011AT 20050627000572005062700057NM 2005 6 27 SB05067 120050606A33503114981 REFLECTOR BOEING737 7373B7 1384580NM EMERGENCY LIGHT CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU 23702 FORWARD ENTRY DOOR EXTERIOR EMERGENCY EVACUATION LIGHT INOPERATIVE. R & R REFLECTOR ASSEMBLY DUE TO CORROSION. ALSO, R & R LAMP. OPS CHECK GOOD. 2L72 4F RTA16WE 20050627000592005062700059WP 2005 6 27 NACA20050015 120050524A5713 STRINGER DOUG DC6 DC6A 3021706WP RT WING CRACKED A NACAK NONE O OTHER ININSP/MAINT 1 AL0399330 43576 STRINGER 19 CAP CRACKED AT STA 196 AND 233. REPAIRED RIGHT WING LOWER STR 19 AND 21 CAP SPLICE WING STA 222 PER DWG NAC 2005-02 DATED 24 MAY 2005. 2L74 4R 6A3 20050627000612005062700061EA 2005 6 27 COMA0560331 120050601A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA ENG ATTACH FIT CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01710CA 7241 CENTER ENGINE SUPPORT BEAM (LOWER WEB) CRACKED. REPAIRED IAW REO 601R-53-61-1353. 2L72 4F RTA21EA 20050627000622005062700062EA 2005 6 27 COMA0560332 120050601A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01710CA 7241 LT AND RT FS 718 FRAME CRACKED. REPAIRED IAW EO 53-027. 2L72 4F RTA21EA 20050627000632005062700063EA 2005 6 27 COMA0560333 120050601A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01498CA 7792 OUTBOARD INTERCOSTALS CRACKED AT FS 484. REPAIRED IAW REO 601R-53-41-059. 2L72 4F RTA21EA 20050627000642005062700064SO 2005 6 27 C2XA05CL043 120050531A335020131A BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSDISCHARGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2726545 145558 LT AND RT OVERWING EMERGENCY LIGHTS FOUND INOPERATIVE. MX INSP AND REPLACED NR 2 EMERGENCY LIGHT BATTERY. OPS CHECKS WERE GOOD. 2L72 4T RTT00011AT 20050627000662005062700066SO 2005 6 27 C2XA05BT035 120050601A335078241 INVERTER EMB 145 EMB145XR 3260214SO EMERGENCY LIGHTSFAULTY A C2XAK NONE O OTHER ININSP/MAINT 1 SW2734110 145658 MID-CEILING EMERGENCY EXIT SIGN NOT WORKING. REMOVED AND REPLACED NR 6 EMERGENCY EXIT SIGN INVERTER IAW EMB145XR AMM NR 33-50-11. OPS CHECKED GOOD. 2L72 4F RT 20050627000682005062700068SO 2005 6 27 C2XA05IA076 120050603A3350110049 CHARGER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSINOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716951 145063 DURING PRE-FLIGHT INSP, CREW REPORTED FORWARD BULKHEAD EMERGENCY EXIT LIGHT INOPERATIVE. MX R & R NR 2 EMERGENCY LIGHT BATTERY CHARGER, OPS CHECKED WITH NO DEFECTS. ACFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20050627000702005062700070EA 2005 6 27 COMA0560334 120050601A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA CARGO BAY CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01498CA 7792 LT AND RT CARGO FLOOR ANGLE FS 621.00 CRACKED. REPAIRED IAW REO 601R-53-61-117. 2L72 4F RTA21EA 20050627000712005062700071NM 2005 6 27 UPS05444595 120050512A5312 PRESSURE PANEL BOEING747 747123F NM LT MLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 LT MLG WW APU BLEED AIR DUCT CUTOUT CRACKED AT 2 AND 7 O'CLOCK POSITION AT STA 1480 (CRACK LENGTH 2.5 IN). LT MLG WW AREA BLEED AIR DUCT CUTOUT REPAIRED AS PER UPS EO B747-5310-3100-C AND DWG 144U2602. 2L74 4F A20WE 20050627000722005062700072NM 2005 6 27 UPS05444596 120050518A531365B0689513 STRINGER BOEING747 747123F NM AFT CARGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 AFT CARGO COMPT, BS 1737 S-35R STRINGER END CORRODED. CORROSION BLEND OUT 0.020 BY 1.0 BY 1.75 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS. STRINGER SPLICE REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050627000752005062700075NM 2005 6 27 UPS05444599 120050519A5347 CARGO TRACK BOEING747 747123F NM CARGO BAY CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 BS 550- 570 LBL 32 TIE DOWN TRACK FLANGE FOUND CORROSION. CORROSION BLEND OUT 0.048 BY 0.4375 BY 1.0 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A. 2L74 4F A20WE 20050627000762005062700076NM 2005 6 27 UPS05444600 120050519A5347 SEAT TRACK BOEING747 747123F NM MAIN DECK CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 BS 778 LBL 33 SEAT TRACK I/B FLANGE CORRODED. CORROSION BLEND OUT 0.026 BY 0.5 BY 0.5 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A FROM BS 770-810 LBL 33. 2L74 4F A20WE 20050627000782005062700078NM 2005 6 27 UPS05444602 120050516A5347 SEAT TRACK BOEING747 747123F NM MAIN DECK CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 M/D BS 1130-1140 RBL 11 SEAT TRACK FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.063 BY 1.5 BY 2.0 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS. M/D BS 1130 TO 1265 RBL 11 TRACK REPAIRED AS PER SRM 53-10-05 FIG 34. 2L74 4F A20WE 20050627000802005062700080NM 2005 6 27 UPS05444604 120050518A5315 FLOORBEAM BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 BS 980 LBL 75-98 BELOW FLOOR VERT WEB BASE FOUND CORRODED AS MARKED. CORROSION BLEND OUT 0.019 BY 0.5 BY 1.75 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, BS 980 FLOORBEAM LOWER CAP ATTACH ANGLE REPLACED AT LBL 75 - LBL 117. AREA AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050627000822005062700082NM 2005 6 27 UPS05444606 120050519A5315 FLOORBEAM BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSP TYPE: C, M/D BS 640 RBL 40-60 FLOORBEAM CORROSION. CORROSION BLEND OUT 0.063 BY 1.0 BY 2.0. EXCEED SRM 53-10-01 FIG 1 LIMIT. M/D BS 640 RBL 43 TO RBL 66 FLOORBEAM REPAIRED AS PER SRM 51-40-04 FIG 1. 2L74 4F A20WE 20050627000832005062700083NM 2005 6 27 UPS05444607 120050518A5347 SEAT TRACK BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 BS 980-1000 RBL 11 INCH SEAT TRACK FLANGE CORROSION. CORROSION BLEND OUT 0.060 BY 0.875 BY 2.0 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, M/D BS 890 - BS 1000 RBL 11 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 14. 2L74 4F A20WE 20050627000852005062700085NM 2005 6 27 UPS05444609 120050518A5347 SEAT TRACK BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 BS 900-920 RBL 12 SEAT TRACK FLANGE CORROSION. CORROSION BLEND OUT 0.020 BY 1.0 BY 3.0 IN. EXCEED SRM 53-10-01 FIG 1 LIMIT, M/D BS 890- BS 1000 RBL 11 SEAT TRACK. REPAIRED AS PER SRM 53-10-05 FIG 14 WORK DETAIL REF NRC 6392. 2L74 4F A20WE 20050627000862005062700086NM 2005 6 27 UPS05444610 120050518A5347 SEAT TRACK BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 BS 910-940 RBL 11 SEAT TRACK FLANGE CORROSION. CORROSION BLEND OUT 0.022 BY 1.0 BY 4.0 IN. EXCEED SRM 53-10-01 FIG 1 LIMIT. M/D BS 890 - BS 1000 RBL 11 SEAT TRACK. REPAIRED AS PER SRM 53-10-05 FIG 14 WORK DETAIL REF NRC 6392. 2L74 4F A20WE 20050627000872005062700087NM 2005 6 27 UPS05444611 120050519A5315 FLOORBEAM BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 BS 860 LBL 84 FLOORBEAM CORROSION. CORROSION BLENDED OUT, EXCEED SRM 53-10-01 FIG 1 LIMITS, REPAIRED AS PER SRM 51-40-04 FIG 1. 2L74 4F A20WE 20050627000892005062700089NM 2005 6 27 UPS05444613 120050519A5347 SEAT TRACK BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 BS 770- 800 RBL 11 SEAT TRACK I/B FLANGE CORROSION. CORROSION BLENDED OUT. EXCEEDED SRM 53-10-01 FIG 1 LIMITS, SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 14. 2L74 4F A20WE 20050627000902005062700090NM 2005 6 27 UPS05444614 120050519A5347 SEAT TRACK BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 BS 830 RBL 11 SEAT TRACK FLANGE CORRODED. CORROSION BLENDED OUT. EXCEEDED SRM 53-10-01 FIG 1 LIMITS, SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 14. 2L74 4F A20WE 20050627000922005062700092NM 2005 6 27 UPS05444616 120050514A5330 SKIN BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 SKIN AT BS 396-397 S23R FOUND 1 TOP ROW FASTENER AREA FOUND CORRODED. CORROSION BLENDED OUT. EXCEEDED EO B747-5330-20503-D LIMITS. FX SKIN BS 388 TO BS 400 STR 23R SKIN REPAIRED AS PER SRM 53-30-03 FIG 26. 2L74 4F A20WE 20050627000932005062700093NM 2005 6 27 UPS05444617 120050519A5347 SEAT TRACK BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 BS 720-740 LBL 75 SEAT TRACK O/B FLANGE CORRODED. CORROSION BLENDED OUT. EXCEEDED SRM 53-10-01 FIG 1 LIMITS, SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A FROM BS 670-770 LBL 75. 2L74 4F A20WE 20050627000942005062700094NM 2005 6 27 UPS05544618 120050603A2560MXP21000 SMOKE GOGGLES BOEING757 75724APF 1384969NM COCKPIT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01468UP 25484 ON PS CHECK, FOUND F/O SMOKE GOGGLES CRACKED. REMOVED AND REPLACED F/O SMOKE GOGGLES PER AMM 25-60-00. 2L72 4F RTA2NM 20050627000972005062700097SO 2005 6 27 MASA200500426 120050601A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07836MJ 145359 TWO ADJACENT FLOOR PROXIMITY LIGHT STRIPS INOPERATIVE IN CABIN. MAINTENANCE R2 LIGHT STRIP. 2L72 4T RTT00011AT 20050627000992005062700099EA 2005 6 27 SWIA200515086 120050531A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSDIRTY A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07448SW 7678 FRONT SECTION EMERGENCY LIGHTS INOP. CLEANED CONNECTIONS AT FLOOR STRIPS. OPS CHECK GOOD. 2L72 4F RTA21EA 20050627001012005062700101NM 2005 6 27 05FDEA01623 120050621A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25619FE 48770 MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT LBL 47, STATION 635 FOUND CRACKED APPROXIMATELY 2 INCHES LONG. CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I FIGURE I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050627001082005062700108WP 2005 6 27 VGC2005F00001 120050516A5100 UNKNOWN CVAC 440 440 2422902WP ALLSN 501D 501D13 03004GL UNKNOWN A VGCAHA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING BHGSMOKE/FUMES/ODORS/SPARKS ELECT. POWER LOSS-50 PC MULTIPLE FAILURE CRCRUISE 1 GL23171FL 318 NR 2 FUEL PUMP FAILED. RT DC GENERATOR OFF LINE, FOLLOWED BY LT DC GENERATOR OFF LINE. (ELECTRIC ODOR NOTED). TRU TO EMERGENCY SELECTED FOR DC BUSS POWER. PRECAUTIONARY LANDING MADE. (K) 2L72 4R4 T 6A6 E282 20050627001152005062700115CE 2005 6 27 A3L2005F00000 120050513A3246FN22A524 NUT DUNLOP RAYTHNDH125 HAWKER800XP 7150012CE GARRTTTFE731TFE7315BR WP WHEEL ASSY FAILED B A3LDO OTHER O OTHER NRNOT REPORTED 1 EA05817TA HK015 258552 AC WAS TAXING ON A MAINTENANCE CHECK AT THE AIRPORT WHEN THE LT IB (NR 2) WHEELS OUTER HALF SEPARATED FROM THE IB HALF. THE 12 TIE BOLTS REMAINED ON THE IB WHEEL HALF AND THEREFORE RECOVERED. ONLY 4 TIE NUTS AND 2 WASHERS WERE RECOVERED BY PORT AUTHORITY. AN INTERVAL INVESTIGATION IS STILL ON GOING BUT IT IS SUSPECTED THAT THE TIE BOLT NUTS FAILED. (K) 2L72 4F4 FRTA3EU E6WE 20050627001182005062700118NM 2005 6 27 05FDEA01638 120050621A5347ADA83891 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 MAIN DECK, SEAT TRACK CROWN FROM STA 1059 TO STA 1119 , X= -47 FOUND WORN. SEAT TRACK CUT AND REMOVED PER SRM 51-33-01 VOLUME II. REPAIR PARTS INSTALLED PER SRM 53-70-00 VOLUME I, FIGURE 1. 2L73 4F RTA22WE 20050627001202005062700120NM 2005 6 27 05FDEA01636 120050621A5347ADA83891 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 MAIN DECK, SEAT TRACK CROWN AT STA 799, X= -47 FOUND WORN. 2L73 4F RTA22WE 20050627001222005062700122NM 2005 6 27 05FDEA01523 120050607A5347ADA83891 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 MAIN DECK, SEAT TRACK LBL 47 CRACKED AT STA 999. CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2L73 4F RTA22WE 20050627001242005062700124NM 2005 6 27 05FDEA01530 120050607A5320A5A7114531 FITTING DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 CENTER CARGO COMPARTMENT, FOUND RIGHT SIDE LOWER SIDEWALL LOCATION BETWEEN STA 5-113 AND STA 1541 L38R WITH SPLICE FITTING CRACKED. REMOVED AS PER SRM 51-33- 01 VOLUME II. NEW SPLICE FITTING FABRICATED AS PER DRAWING NR A5A7114 AND NEW SPLICE FITTING INSTALLED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2L73 4F RTA22WE 20050627001292005062700129NM 2005 6 27 05FDEA01629 120050621A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25264FE 21626 CORROSION ON FLOORBEAM LBL 12 BS 480. FABRICATED AND INSTALLED FLOORBEAM REPAIR LBL 12, BS 480 PER SRM 53-10-08 FIG 3 2L73 4F RTA3WE 20050627001332005062700133NM 2005 6 27 QXEA200501072 120050621A2197 CONNECTOR BOMBDRDHC8 DHC8402 1390042NM ZONE 100 DIRTY A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09410QX 4053 PDX - ON FLIGHT 2290, RETURNED TO GATE, UNABLE TO GET ANY AIR FLOW FROM BLEEDS 1 OR 2 (APU BLEED DID NOT SEEM TO WORK EITHER). CLEANED AND RESEATED CONNECTOR TO PACK FLOW CONTROL VALVE. BLEED AIR SYSTEM OPERATIONAL CHECKS GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050627001352005062700135 2005 6 27 QXEA200501073 420050621A3440MI585066 PEDESTAL DHAV DHC8 DHC8202 2809007NM ZONE 100 MALFUNCTIONED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09361PH 516 SEA - ON FLIGHT 2244, RETURNED TO FIELD, WEATHER RADAR SHOWS WX AND NOTHING ELSE WHEN TURNED ON. REPLACED WEATHER RADAR ANTENNA PEDESTAL. ALL TESTED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050627001382005062700138NM 2005 6 27 QXEA200501075 120050621A33506038443 BATTERY DHAV DHC8 DHC8202 2809007NM ZONE 200 INOPERATIVE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09364PH7848 7848 524 SEA - EMERGENCY EXIT LIGHTS INOP, TWO IN CEILING AND ONE LT AFT EGRESS LIGHT. REMOVED AND REPLACED BATTERY AND POWER SUPPLY AT 3351 PS-3. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050627001392005062700139SO 2005 6 27 01062005 120050621A323012038594001 CONTROL BOX EMB 120 EMB120ER 3260203SO MLG MALFUNCTIONED G HSYAO OTHER J WARNING INDICATION DEDESCENT 1 NM05125AM 120017 DURING ARRIVAL OF FLIGHT 7788 JAC-CPR, CAPTAIN SELECTED GEAR DOWN AND OBSERVED GEAR UNSAFE LIGHT ILLUMINATED. CAPTAIN TRIED TO CYCLE GEAR UNSUCCESSFULLY. LANDING GEAR WAS THEN EXTENDED AS PER THE QRH SUCCESSFULLY. LANDING IN CPR WITHOUT INCIDENT. APPARENT CAUSE OF PROBLEM: LANDING GEAR CONTROL BOX. TROUBLESHOT AND FOUND LANDING GEAR CONTROL BOX BAD. REMOVED AND REPLACED LANDING GEAR CONTROL BOX WITH A REPAIRED SERVICEABLE CONTROL BOX IAW EMB-120 MM 32-31-01, PG 401-403. OPS CHECKED GOOD. 2L72 4T RTA31SO 20050627001402005062700140WP 2005 6 27 U2RAM83088 120050621A53404611067501N FITTING DOUG DC8 DC871F 302199DWP FUSLEAGE CORRODED A U2RAK NONE O OTHER ININSP/MAINT 1 GL23872SJ813323486 46040 LONGERON END FITTING LOCATED AT FRAME 80 AFT, L27R FOUND CORRODED BEYOND LIMITS. CLASSIFIED AS LEVEL 2 CORROSION. 2L74 4F RT4A25 20050627001412005062700141NM 2005 6 27 05FDEA01642 120050622A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 MAIN DECK, SEAT TRACK CROWN AT STA 625, X= 47 FOUND WORN ACA7399-501. REMOVED AND REPLACED PER SRM 53-70-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2L73 4F RTA22WE 20050627001422005062700142WP 2005 6 27 MWEA050054 120050618A2560 BATTERY DOUG DC9 DC981 3022081WP FLASHLIGHT INOPERATIVE A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 RIGHT COCKPIT FLASHLIGHT BATTERIES ARE INOPERATIVE. INSTALLED NEW BATTERIES. 2L72 4F A6WE 20050627001432005062700143WP 2005 6 27 MWEA050055 120050622A57535930496503 VANE DOUG DC9 DC982 3022082WP LEFT WING FLAP GOUGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 LEFT WING FIXED VANE HAS A 2 INCH GOUGE ON UPPER VANE SURFACE, AFT OF INBOARD FLIGHT SPOILER ACTUATOR, WING STATION 214. FABRICATED AND INSTALLED WING VANE. 2L72 4F A6WE 20050627001442005062700144NM 2005 6 27 05FDEA01639 120050621A7830 SLEEVE DOUG MD11 MD11 3023602NM THRUST REVERSER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 NR 1 ENGINE, LT THRUST REVERSER TRANSLATING SLEEVE, UPPER SLIDER TRACK END SUSPECTED CRACKED. LT THRUST REVERSER COWL REMOVED AND REPLACED. 2L73 4F RTA22WE 20050627001452005062700145 2005 6 27 05FDEA01640 420050622A3414 INDICATOR AIRBUS310 A310222 3930315EU AIRSPEED INOPERATIVE A FDEAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 SO25447FE 251 ON T/O ROLL RW 36R AT TUL NOTED NO AIRSPEED INDICATION ON CAPTS PFD REJECTED TO BELOW 80 KTS. BLEW OUT CAPTS PITOT TUBE CHECKED GOOD WITH PITOT STATIC TESTER. 2L72 4F RTA35EU 20050627001462005062700146NM 2005 6 27 05FDEA01641 120050622A5347ACA7104511 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 MAIN DECK, SEAT TRACK CROWN AT STA 635 , X= 8 FOUND WORN. REMOVED AND REPLACED PER SRM 53-70-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2L73 4F RTA22WE 20050627001472005062700147NM 2005 6 27 05FDEA01643 120050622A5347AEA75791 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 MAIN DECK, SEAT TRACK CROWN AT STA 1491, X= 47 FOUND WORN. REMOVED AND REPLACED AT EXISTING SPLICES PER SRM 53-70-00 VOLUME I, FIGURE 1. 2L73 4F RTA22WE 20050627001482005062700148EA 2005 6 27 QXEA200501063 120050616A2760 INDICATOR CNDAIRCL600 CL6002C10 1390015EA SPOILERS MALFUNCTIONED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09607QX17128894 10024 PDX - FLIGHT 2505 RETURN TO GATE, INTERMITTANT SPOILER/STAB FAULT, RUDDER LIMIT FAULT STATUS MESSAGES. MAINTENANCE REPLACED ISI. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20050627001492005062700149NM 2005 6 27 QXEA200501062 120050616A21507827906 ACM DHAV DHC8 DHC8102 2809003NM MALFUNCTIONED A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09366PH2889820850 510 SEA FLIGHT 2025 RETURNED TO GATE CABIN TEMPERATURE FULL HOT. MAINTENANCE REPLACED THE AIR CYCLE MACHINE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050627001502005062700150NM 2005 6 27 HNAA0500060 120050621A3244 TIRE DHAV DHC8 DHC8102 2809003NM NR 1 MLG FAILED A HNAAO OTHER O OTHER LDLANDING 1 EA07810EX 308 UPON LANDING THE AIRCRAFT VEERED OFF RUNWAY. POST FLIGHT INSPECTION REVEALED THE NR 1 MAIN WHEEL TIRE ASSY HAD BLOWN OUT (SHREADED) AND QLV LEAKING IN NR 1 NACELLE. REPLACED O-RING ON QLV AND REPLACED WHEEL ASSYS AND PERFORMED ANTI SKID FUNCTION CHECK. REPLACED ANTISKID COMPUTER, ANTISKID CONTROL VALVE, AND ANTISKID TRANSDUCER FOR TROUBLESHOOTING. MORE TO FOLLOW UPON RECEIPT OF TEARDOWN REPORTS. 2H72 4T RTA13NM 20050627001512005062700151NM 2005 6 27 QXEA200501067 120050619A3244 TIRE DHAV DHC8 DHC8202 2809007NM ZONE 700 FAILED A QXEAO OTHER O OTHER TXTAXI/GRND HDL 1 NM09357PH 504 RDM - ON FLIGHT 2122, RETURNED TO GATE (RDM-PDX), ON TAXI OUT NR 1 TIRE BLEW AND NR 2 TIRE WENT FLAT. PASSENGERS WERE BUSED FROM TAXIWAY TO TERMINAL. A/C WAS TOWED TO GATE. REMOVED AND REPLACED NR 1 AND 2 MAIN LANDING GEAR WHEEL ASSEMBLIES. C/W BLOWN TIRE INSPECTION WITH GEAR EXTENDED, CHECKS GOOD. NO OTHER DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050627001522005062700152NM 2005 6 27 2005UALA00539 120050610A2150 A/C PACK AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE BOTH FAILED A UALABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29813UA 858 V10324 ECAM NR 1 ENG EIU DISPLAYED DURING CRUISE. LOST BOTH AIR CONDITIONING PACKS. EIU REMOVED TO SFO HOME SHOP. UNIT TESTED NO FAULTS FOUND. CCOA 0-4499 ACCOMPLISHED 1/29/2004 PER SB 395798-73-004 AS RECOMMENDED BY AIRBUS TFU 73.25.00.019. FLEET ENGINEERING SETTING UP A PROJECT TO ACCOMPLISH AIRBUS SB A320-21-1121. 2L72 4F4 FRTA28NM E40NE 20050627001532005062700153NM 2005 6 27 2005UALA00540 120050611A2121EVT3454 FAN AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE E/E BAY FAILED A UALAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 WP2939UA 1507 CREW REPORTED SMOKE IN FLIGHT DECK. REPLACED THE AVIONICS BLOWER FAN. TESTED OK. REPLACED THE AVIONICS BLOWER FAN. TESTED OK. 2L72 4F4 FRTA28NM E40NE 20050627001542005062700154NM 2005 6 27 QXEA200501065 120050618A33506138001 BATTERY BOMBDRDHC8 DHC8402 1390042NM ZONE 200 INOPERATIVE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX1421 1421 4051 PDX - ALL FOUR EMERGENCY EXIT SIGNS IN AFT GALLEY AND LEFT AND RIGHT AFT EXTERIOR EGRESS LIGHTS FAIL TO ILLUMINATE WHEN SELECTED ON. REPLACED BATTERIES IN AFT EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050623000792005062300079SO 2005 6 23 SWIA200515130 120050527A3350 LIGHT EMB 120 EMB120ER 3260203SO CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07308SW 120326 FIRST 4 FLOOR LEVEL EMERGENCY LIGHTS NOT WORKING. REPLACED LIGHT ASSY WITH SERVICEABLE UNIT. OPS CHECK GOOD. 2L72 4T RTA31SO 20050623000872005062300087SO 2005 6 23 CHQA200500112 120050612A329714544841401 WIRE HARNESS EMB 145 EMB145LR 3260212SO LG BRAKE SYS UNSERVICEABLE A CHQAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL11278SK 145370 ON DEPARTURE "BRAKE OVERTEMP" MESSAGE ON EICAS. HYD PAGE SHOWED LT OUTBOARD BRAKE TEMP WAS AT YELLOW/GREEN MERGE ON GAUGE. BRAKE TEMPS LOW PRIOR TO T/O. NO FEELING OF DRAGGING BRAKE ON DEPARTURE ROLL. COMPLIED WITH QRH AND LOWERED LG. BRAKE TEMP IND WENT FULL HOT ON GAUGE, THEN FLUCTUATED UP AND DOWN. EMERGENCY DECLARED AND RETURNED. ON STOP OF ACFT, NO SMOKE OBSERVED. TEMPS NORMAL. BRAKE TEMP IND RETURNED TO NORMAL. R & R LT OB BRAKE TEMP SENSOR. PERFORMED TAXI CHECK. ALL BRAKE TEMPS EQUAL DURING TAXI. OPS CHECK GOOD. ACFT DEPARTED. SAME THING HAPPENED AGAIN. TEMP GAUGE STAYED IN FULL HOT. RETURNED. BRAKE TEMP ON LT OB BRAKE FULL HOT. R & R BRAKE TEMP SENSOR HARNESS ON LT MLG. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050623000892005062300089EA 2005 6 23 QXEA20051025 120050521A5210 DOOR CNDAIRCL600 CL6002C10 1390015EA ZONE 200 STIFF A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09615QX 10065 MAIN CABIN DOOR DIFFICULT TO LATCH AND OPEN. OPERATED MAIN CABIN DOOR SERVERAL TIMES. OPS CHECK NORMAL. NO DEFECTS NOTED. NO PARTS REPLACED. ACFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20050623000932005062300093EU 2005 6 23 RAIA00505025 120050531A2750 CONTROL UNIT JETAIRJETSTMJETSTM4101 1500501EU FLAP CONTROL SYSBYPASSING A RAIAA UNSCHED LANDING O OTHER CLCLIMB 1 CE03557HK 41074 FLAPS WOULD NOT RETRACT TO 0 DEGREES ON DEPARTURE. MX INSP AND FOUND FLAP CONTROL UNIT BYPASS PIN POPPED. RESET AND OPS CHECKED GOOD. 2L72 4T RTA41NM 20050623001022005062300102NM 2005 6 23 QXEA200501031 120050606A2120 ODOR BOMBDRDHC8 DHC8402 1390042NM PWC 150 PW150A EA CABIN DETECTED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM09405QX 4047 PCEFA0097 ODOR IN ACFT WITH BLEEDS ON. MX REPLACED NR 2 ENGINE IAW MTC 6710003 AND 6710004. OPS CHECK AND LEAK CHECK GOOD. ACFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E00062EN 20050623001082005062300108NM 2005 6 23 QXEA200501014 120050418A3320BR6306104101 LAMP DHAV DHC8 DHC8202 2809007NM CABIN INOPERATIVE A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM09352PH 494 STRONG ELECTRICAL ODOR FOUND IN AFT CABIN AND CARGO AREA. INSP OVERHEAD LIGHTS AT ROWS 6-9. RELAMPED INTERMITTENT LAMPS. OPS CHECKS GOOD. ACFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050623001182005062300118EA 2005 6 23 QXEA200500972 120050510A2760 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA DRAG CONTROL SYSFALSE ACTIVATIONA QXEAO OTHER N FALSE WARNING APAPPROACH 1 NM09615QX 10065 ON FINAL APPROACH DEPLOYED FLIGHT SPOILERS AND RECEIVED MASTER CAUTION "FLIGHT SPOILER DEPLOY", CAUTION WENT AWAY WHEN RETRACTED FLIGHT SPOILERS. MX INTERROGATED MDC. NO CURRENT FAULTS NOTED. COMPLIED WITH CRJ700 FIM TASK 27-61-00-810-A01. NO DEFECTS NOTED. NO PARTS REPLACED. ACFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20050623001232005062300123NM 2005 6 23 QXEA200501019 120050517A242131708001A GENERATOR DHAV DHC8 DHC8202 2809007NM ZONE 100 MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09367PH9844 1887 511 RT STALL WARNING AND RT TRU CAUTION LIGHTS ILLUMINATED AFTER TAKEOFF. WERE ON FOR ABOUT 2 SECONDS AND THEN WENT OUT WHEN THE NR 2 AC GENERATOR CAUTION LIGHT CAME ON. RAN APPROPRIATE CHECKLIST AND IT DIDN'T RESET THE LIGHT. REPLACED NR 2 AC GENERATOR. OPS AND LEAK CHECK GOOD. ACFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050623001262005062300126NM 2005 6 23 QXEA200501005 120050603A5210 DOOR BOMBDRDHC8 DHC8402 1390042NM CABIN LACK OF LUBE A QXEAO OTHER O OTHER TXTAXI/GRND HDL 1 NM09403QX 4037 FLIGHT ATTENDANT REPORTED MAIN CABIN DOOR HARD TO OPEN. MX CLEANED AND LUBRICATED DOOR. OPS CHECKS GOOD. ACFT RETURNED TO SERVICE. NO PARTS REPLACED. 2H72 4T RTA13NM 20050623001352005062300135NM 2005 6 23 72300194 120050525A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 4 X 1 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050623001532005062300153NM 2005 6 23 P9RA20050091 120050615A3350SG9442 LIGHT BOEING727 727231 1384079NM CABIN FLOOR DETERIORATED A P9RAK NONE O OTHER ININSP/MAINT 1 SO1154344 21631 FLOOR TRACK LIGHTING IN FORWARD CABIN AREA DETERIORATED AND LOSING LIGHTING EFFECT. REMOVED AND REPLACED 12 LINEAR FEET OF FLOOR TRACK LIGHTING IAW SAFTGLO M/M. 2L73 4F A3WE 20050624000122005062400012NM 2005 6 24 WRLA2005110 120050614A5512 PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE NR 25. 2L73 4F4 FRTA22WE E24NE 20050624000192005062400019SO 2005 6 24 RAIA00506021 120050615A28242930003102 VALVE EMB 145 EMB145LR 3260212SO FUEL CROSSFEED NOT CLOSED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03836HK3486 145695 FLT 7997 IAD - FUEL CROSSFEED WILL NOT CLOSE. STUCK IN THE OPEN POSITION. MAINTENANCE REMOVED AND REPLACED THE CROSSFEED VALVE. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050624000422005062400042NM 2005 6 24 UPS05444590 120050517A5320 WEB BOEING747 747123F NM BLEED AIR DUCT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSP TYPE: C LT BS 1480 APU BLEED AIR DUCT CUTOUT CRACK FOUND 1EA FASTENER HOLE APPROX 0.0625 INCH IN LENGTH . LT BS 1480 APU BLEED AIR DUCT CUTOUT REPAIRED AS PER UPS EO NR B747-5310-3100-C AND DWG 144U2602. 2L74 4F A20WE 20050624000812005062400081EU 2005 6 24 AWXA200500725 120050619A253067262001003 OVEN AIRBUS320 A320232 3930326EU FWD GALLEY DIRTY A AWXAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP28648AW 770 LT FWD GALLEY OVEN SMOKES DURING OPERATION. MAINTENANCE REMOVED AND REPLACED THE LT FWD GALLEY OVEN IAW AMERICA WEST AIRLINES TASK CARD F1D25303. OPERATIONAL TESTS WERE GOOD. UNIT WAS RECEIVED DIRTY. UNIT'S THERMOSTAT WAS ADJUSTED AND THE DOOR SEAL WAS REPLACED IAW OHM 25-35-53. 2L72 4F RTA28NM 20050624001082005062400108NM 2005 6 24 SWAA051834 120050621A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29422WN 29826 DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER CRACKED AT ROW 1. REMOVED AND REPLACED COVER PER MM. 2L72 4F RTA16WE 20050624001202005062400120NM 2005 6 24 PIDA20050054 120050610A5320 STRAP BOEING737 737400 138449ANM FLOORBEAM CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05801DM 26240 SONIC VIBRATION STRAP ON LOWER SURFACE OF FLOORBEAM AT BS367 AT LBL24 IS CRACKED. REPAIRED STRAP PER SRM 53-10-51. 2L72 4F RTA16WE 20050624001252005062400125NM 2005 6 24 PIDA20050023 120050603A5315 FLOORBEAM BOEING757 757200 1384950NM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05750WL 23928 CORROSION ON BS 1641 FLOORBEAM AT RBL 59. REPAIRED PER SRM 53-00-51. 2L72 4F RTA2NM 20050624001322005062400132NM 2005 6 24 PIDA20050035 120050603A5320 ANGLE BOEING757 757200 1384950NM CARGO BIN CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05750WL 23928 RIGHT TRANSITION ANGLE CORRODED IN AFT CARGO BIN FROM BS 1506 TO BS 1528. REPLACED TRANSITION ANGLE FROM BS 1460 +8 TO BS 1520 +10 PER SRM 51-10-00 AND SRM 51-40-02. 2L72 4F RTA2NM 20050624001342005062400134NM 2005 6 24 PIDA20050028 120050603A5340 ATTACH ANGLE BOEING757 757200 1384950NM CARGO BIN CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05750WL 23928 CORROSION ON SHEAR WEB UPPER ATTACH ANGLE IN AFT CARGO BIN AT STR 26 LT FROM BS 1360 TO BS 1380. REPAIRED PER SRM 51-40-00 AND SRM 51-10-00. 2L72 4F RTA2NM 20050624001362005062400136NM 2005 6 24 PIDA20050032 120050603A5340 ATTACH ANGLE BOEING757 757200 1384950NM CARGO BIN CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05750WL 23928 CORROSION ON UPPER SHEAR WEB ATTACH ANGLE IN AFT CARGO BIN FROM BS 1360 TO BS 1380 AT STR 26 RT. REPLACED UPPER SHEAR WEB ATTACH ANGLE PER SRM 51-10-02. 2L72 4F RTA2NM 20050624001382005062400138NM 2005 6 24 PIDA20050033 120050603A5340 ATTACH ANGLE BOEING757 757200 1384950NM CARGO BIN CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05750WL 23928 CORROSION ON UPPER SHEAR WEB ATTACH ANGLE IN AFT CARGO BIN FROM BS 1280 TO BS 1300 AT STR 26RT. REPLACED UPPER SHEAR WEB ATTACH ANGLE PER SRM 51-10-02. 2L72 4F RTA2NM 20050624001422005062400142NM 2005 6 24 PIDA20050024 120050603A5315 FLOORBEAM BOEING757 757200 1384950NM FUSLEAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05750WL 23928 CORROSION AROUND NUT PLATE HOLES ON BS 1661 FLOORBEAM FROM RBL 15 TO RBL 8. REPAIRED PER SRM 53-00-51. 2L72 4F RTA2NM 20050624001472005062400147NM 2005 6 24 PIDA20050040 120050603A5347 MOUNT BOEING757 757200 1384950NM LAVATORY CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05750WL 23928 LAVATORY MOUNT AT BS 1315 AT LBL 25 HAS CORROSION. REPLACED MOUNT FITTING PER SRM 51-10-00. 2L72 4F RTA2NM 20050627000022005062700002SO 2005 6 27 SWIA200515088 120050316A5315 BUTTSTRAP EMB 120 EMB120ER 3260203SO FLOORBEAM CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07299SW 120329 CENTER BUTT STRAP BELOW CABIN FLOOR AFT OF ROW 10 CORRODED, ITEM FOUND AT C-CHECK INSPECTION. NEW BUTT STRAP INSTALLED IAW SRM 120 51-10-02 PG 3 SEC 3.A. 2L72 4T RTA31SO 20050627000062005062700006EA 2005 6 27 SWIA200515093 120050601A2741 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA COCKPIT STICKING A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07963SW 7865 FO'S TRIM SWITCH IS STICKING. REPLACED FO'S STAB TRIM SWITCH IAW MM 27-41-05, OPERATIONAL CHECK GOOD IAW MM 27-41-00. 2L72 4F RTA21EA 20050627000072005062700007EA 2005 6 27 SWIA200515094 120050531A2741 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA COCKPIT INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07939SW 7742 CAPT'S SIDE STAB TRIM SWITCH ON YOKE IS INOPERATIVE. REPLACED CAPTIANS STAB TRIM SWITCH, OPERATIONAL CHECK GOOD IAW 27-41-05. 2L72 4F RTA21EA 20050627000252005062700025EA 2005 6 27 SWIA200515112 120050515A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07592SW 7279 FS 280 BELOW FLOOR RBL 9.0 OUTBOARD ANGLE CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-13, 51-42-21, 51-23-00, 51-25-00. 2L72 4F RTA21EA 20050627000372005062700037EA 2005 6 27 SWIA200515124 120050323A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07958SW 7833 FS 621 RT FLOOR SUPPORT ANGLE CRACKED AT LBL 41.0, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FLOOR SUPPORT ANGLE IAW CRJ REO 601R-53-61-117 REV B. 2L72 4F RTA21EA 20050627000562005062700056SO 2005 6 27 MASA200500393 120050525A3350 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSBURNED OUT A MASAK NONE O OTHER ININSP/MAINT 1 SW07842MJ 145457 DURING WALK AROUND DISCOVERED LT AFT EXTERNAL EMERGENCY LIGHT NOT ILLUMINATING. MX REPLACED LIGHT BULB AND OPS CHECK GOOD. 2L72 4T RTT00011AT 20050627000582005062700058WP 2005 6 27 NACA20050014 120050524A5713 STRINGER DOUG DC6 DC6A 3021706WP RT WING CRACKED A NACAK NONE O OTHER ININSP/MAINT 1 AL0399330 43576 X-RAY REVEALED CRACK, STR 19, STA 182. REPAIRED LOWER RIGHT WING STRINGER NR 19, STA 181 RT PER DWG NAC2005-01. 2L74 4R 6A3 20050627000692005062700069SO 2005 6 27 C2XA05IA077 120050602A33501317 BULB EMB 145 EMB145XR 3260214SO EMERGENCY LIGHTSBURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2711127 145697 DURING "A" CHECK INSP, GALLEY OVERHEAD EMERGENCY EXIT LIGHT FOUND TO BE INOPERATIVE. MX R & R AFFECTED LIGHT BULB. OPS CHECKED WITH NO DEFECTS NOTED. ACFT APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20050627000732005062700073NM 2005 6 27 UPS05444597 120050518A5315 FLOORBEAM BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 BS 1170 LBL 11- RBL 11 FLOOR SUPPORT CORROSION. CORROSION BLEND OUT 0.036 BY 1.215 BY 1.5 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS. M/D - BS 1170 LBL 11 - RBL 11 FLOOR SUPPORT REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050627000842005062700084NM 2005 6 27 UPS05444608 120050519A5347 SEAT TRACK BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 BS 890-910 RBL 11 SEAT TRACK O/B FLANGE CORRODED. CORROSION BLEND OUT 0.025 BY 0.5 BY 3.0 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, M/D BS 890 - BS 1000 RBL 11 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 14 WORK DETAIL REF NRC NR 6392. 2L74 4F A20WE 20050627000912005062700091NM 2005 6 27 UPS05444615 120050519A5315 FLOORBEAM BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 BS 800 RBL 75-80 FLOORBEAM UPPER TEE FOUND CORRODED. CORROSION BLENDED OUT. EXCEEDED SRM 53-10-01 FIG 1 LIMITS, M/D BS 800 RBL 75-80 FLOORBEAM UPPER TEE REPAIRED AS PER SRM 51-40-04 FIG 1. 2L74 4F A20WE 20050627001172005062700117NM 2005 6 27 05FDEA01637 120050621A5347AGA7082505 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 MAIN DECK, SEAT TRACK BASE AT STA 6 - 10, X= -8 FOUND WITH CORROSION. REMOVED AND TREATED AS PER SRM 51-21-01 VOLUME II. 2L73 4F RTA22WE 20050627001192005062700119NM 2005 6 27 05FDEA01635 120050621A5347ADA83891 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 MAIN DECK, SEAT TRACK CROWN FROM STA 899 TO STA 923, X= 47 FOUND WORN. 2L73 4F RTA22WE 20050627001212005062700121NM 2005 6 27 05FDEA01522 120050607A5347A6A7082505 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 MAIN DECK, SEAT TRACK RBL 47 CRACKED AT STA 999 TO STA 929 CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2L73 4F RTA22WE 20050627001232005062700123NM 2005 6 27 05FDEA01529 120050607A5340A5A71151 FITTING DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 CENTER CARGO COMPARTMENT, FOUND RIGHT SIDE LOWER SIDEWALL LOCATION BETWEEN STA 5-113 AND STA 1541 L41R WITH SPLICE FITTING CRACKED. REMOVED AS PER SRM 51-33- 01 VOLUME II. NEW SPLICE FITTING FABRICATED AS PER DRAWING NR A5A7115 AND NEW SPLICE FITTING INSTALLED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2L73 4F RTA22WE 20050627001252005062700125SO 2005 6 27 RAIA00506005 120050606A7830 SWITCH EMB 145 EMB145 3260210SO THRUST REVERSER MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03821HK 145068 ENGINE NR 2 REV FAIL INDICATION ON EICAS DURING START. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENG T/R STOW SWITCH. OPS CHECKED GOOD. 2L72 4F RTT00011AT 20050627001262005062700126NM 2005 6 27 05FDEA01531 120050608A5320A6A70821 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 MAIN DECK, SEAT TRACK RBL 27 CRACKED AT STA 6-80. CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2L73 4F RTA22WE 20050627001302005062700130SO 2005 6 27 CHQA200500120 120050621A21214611028900 GASPER FAN EMB 135 EMB135LR 3260305SO COCKPIT INOPERATIVE A CHQAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 GL11836RP 145713 FLIGHT 6260 FLL-TLH - DURING DESCENT INTO TLH, THE SMELL OF HOT PLASTIC WAS NOTED IN THE COCKPIT. FA REPORTED SAME NOTED IN THE FORWARD CABIN AND GALLEY. RAN "SMOKE" PROCEDURE MEMORY ITEMS AND DECLARED EMERGENCY. NEAREST AIRPORT AT THIS POINT WAS DESTINATION (TLH). AFTER NORMAL LANDING, SMELL WAS GONE. TAXIED TO GATE WITHOUT INCIDENT AND DEPLANED PASSENGERS AT GATE. MAINTENANCE INSPECTED THE WINDSHIELD HEAT TERMINALS, LEFT AND RIGHT RELAY SUPPORT PANELS WITH NO DEFECTS NOTED. THE GASPER FAN WAS FOUND TO BE INOP WITH RELAY K0337 POWERED. THE GASPER FAN WAS PLACED ON MED 21-23-03-1 CAT C TICKET NR 18507. NO SMELL NOTED. 2L72 4F RTT00011AT 20050627001362005062700136NM 2005 6 27 QXEA200501076 120050621A33506519020BG LIGHT DHAV DHC8 DHC8202 2809007NM ZONE 200 INOPERATIVE A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09353PH 496 SEA - ON FLT 2258, FLOOR PROXIMITY LIGHTING NEAR ROW 1 LOOSE. REMOVED AND REPLACED FORWARD FLOOR PROXIMITY LIGHT ASSY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050627001562005062700156NM 2005 6 27 2005UALA00541 120050612A3610NSA860114 CLAMP AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE NR 2 PYLON FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP2909UA 825 V10376 NR 2 ENGINE BLEED FAULT. RIGHT WING BLEED LEAK DISPLAYED AFTER TAKEOFF. FOUND LEAK ABOVE NR 2 ENG PYLON AT DUCT CLAMP (REF IPC 36-11-05 FIG 02 ITEM 20). REPLACED CLAMP. LEAK WAS 2 INCHES IN FRONT OF RT WING LOOP -A- ELEMENTS 43HF AND 44HF. 2L72 4F4 FRTA28NM E40NE 20050627001572005062700157NM 2005 6 27 2005UALA00544 120050512A5340 STRINGER CLIP BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU FUSLEAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29313UA 23674 AFT PIT STA 727D STR 23 LEFT STRINGER CLIP DAMAGED. *S/D* REMOVED AND REPLACED STRINGER CLIP REF SRM 51-40-02. 2L72 4F4 FRTA16WE E21EU 20050627001582005062700158NM 2005 6 27 2005UALA00545 120050512A5340 STRINGER CLIP BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29313UA 23674 AFT PIT STRINGER CLIP DAMAGED, STR 20L STA 727A. *S/D* REPLACED STRINGER CLIP PER SRM 51-40-02. 2L72 4F4 FRTA16WE E21EU 20050627001592005062700159NM 2005 6 27 2005UALA00546 120050527A5310 DOOR FRAME BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29313UA 23674 AFT CARGO DOOR FWD BS 795 FRAME WAS FOUND CRACKED AT JOINT WITH LOWER FRAME SECTION. *S/D* REPAIR ACP' D PER AAR EA I050096. FRAME SECTION WAS REPLACED USING A NESTED U-CHANNEL REPAIR SCHEME, AT AAR HMV-4. 2L72 4F4 FRTA16WE E21EU 20050627001602005062700160NM 2005 6 27 2005UALA00547 120050527A5311 FRAME BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29313UA 23674 EXTERNAL FUSELAGE HAS A DENT AT FRAME STA 807 STR 28L & STR 28R. *S/D* REMOVED DAMAGE, FABRICATED AND INSTALLED NEW SHEAR TIE CLIP SUPPORT ANGLE PER SRM 51-40-02 AND SRM 53-00-07. 2L72 4F4 FRTA16WE E21EU 20050627001612005062700161NM 2005 6 27 2005UALA00548 120050528A5310 DOOR FRAME BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29313UA 23674 FWD GALLEY DOOR 2 EACH CRACKS FOUND AFT FRAME, FIRST CRACK AFT FRAME CUTOUT OF THE 3RD STOP, SECOND CRACK AROUND THE FASTENER HOLE ADJACENT TO THE LWR STOP. *S/D* FABRICATED AND INSTALLED DOUBLER PER CMM SM90-52-40-14JD AND BOEING REPAIR KIT 69-69854 INSTALLED PER CMM. 2L72 4F4 FRTA16WE E21EU 20050627001622005062700162NM 2005 6 27 2005UALA00549 120050529A5330 SKIN BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29313UA 23674 EXTERNAL FUSELAGE SKIN CRACKED AT AFT EDGE OF EQ COOLING EXHAUST OUTLET BS 378 LBL 02. *S/D* DURING REPAIR DETAILED IN MM53-30-99 (DOUBLER INSTALLATION), THE EXISITNG INTERNAL DOUBLER AROUND PERIMETER OF THE CUTOUT WAS TORN ADJACENT TO THE SKIN CRACK. THIS MAJOR REPAIR IS TIME LIMITED AND MUST BE REPLACED BY 6000 CYCLES. 2L72 4F4 FRTA16WE E21EU 20050627001632005062700163NM 2005 6 27 2005UALA00550 120050529A5511 RIB BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU HORIZONTAL STAB CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29313UA 23674 LT HORIZONTAL STAB L/E RIB LOWER FLANGE AT STA 151.8 WAS FOUND CRACKED. *S/D* REPAIR ACP' D PER EVA-50305, FABRICATED REPAIR ANGLE REPAIR SCHEME AT HMV-4. 2L72 4F4 FRTA16WE E21EU 20050627001892005062700189NM 2005 6 27 SWAA051841 120050622A3350101073 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29353SW 24889 DURING SCHEDULED C1 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE AT FWD GALLEY. SECURED LENS PER MM. 2L72 4F RTA16WE 20050627001912005062700191 2005 6 27 SWAA051843 420050622A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29444WN 29839 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050627001932005062700193 2005 6 27 SWAA051845 420050622A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29499WN 32481 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050627002082005062700208EU 2005 6 27 06212005 120050621A2612 FIRE LOOP SAAB SF340 340B 7860101EU RT NACELLE SHORTED A NSVAE ENGINE SHUTDOWN N FALSE WARNING TXTAXI/GRND HDL 1 EA27356CJ 356 WHILE AT GROUND IDLE RECEIVED A RT ENGINE FIRE INDICATION (INTERNITTENT). SHUT DOWN ENGINE. FOUND FILE LOOP TOUCHING CASE, REPOSITIONED, NO FURTHER DISCREPANCY. 2L72 4T RTA52EU 20050627002102005062700210NM 2005 6 27 EVAS094002 120050616A2710 ACTUATOR DOUG MD11 MD11F 3023600NM AILERON DEFLECT MALFUNCTIONED W QOCFB EMER. DESCENT J WARNING INDICATION CLCLIMB 1 WP0316110 48786 DURING CLIMB, AIRCRAFT RECEIVED AILERON DEFLECTION DISAGREE WARNING MESSAGE, CAPTAIN DECIDED TO AIR RETURN. ON GROUND CHECK, FOUND LEFT AILERON DEFLECTION ACTUATOR FUNCTION NO GOOD. REPLACED ACTUATOR AND OPERATION CHECK NORMAL. 2L73 4F RTA22WE 20050627002122005062700212NM 2005 6 27 05FDEA01644 120050622A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 MAIN DECK, SEAT TRACK CROWN AT STA 1199, X= 47 FOUND WORN AEA7579-1. REMOVED AND REPLACED AT EXISTING SPLICES PER SRM 53-70-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2L73 4F RTA22WE 20050627002142005062700214NM 2005 6 27 05FDEA01646 120050622A5711 SPAR BOEING727 727200 138407ENM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 CORROSION ON RT WING FUEL CELL FWD SPAR WEB FWD FACE AROUND CUTOUT 7540R. *S/D* REPAIRED RIGHT WING FUEL CELL FWD SPAR WEB FACE AROUND PANEL 7540 PER FED EX EA 7-5710-86300. 2L73 4F RTA3WE 20050628000022005062800002WP 2005 6 28 I5HA0524003 120050528A7714R2800 LINE CVAC 240 240* 2422601WP PWA R2800 R2800* 52026NE LT ENGINE LOOSE A I5HAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL23156PA 324 WHILE ENROUTE, MAINTENANCE, THE PILOT OBSERVED A LOSS OF TORQUE PRESSURE ON THE LT ENGINE WITH NO SECONDARY INDICATIONS. AS A PRECAUTION, THE PILOT ELECTED TO SHUT-DOWN THE ENGINE AND MADE AN UNEVENTFUL LANDING. DURING INSPECTION OF ENGINE, LOOSE TORQUE TRANSMITTER LINE WAS DISCOVERED. LINE WAS TIGHTENED AND AFTER A SUCCESSFUL POST MAINTENANCE ENGINE RUN, THE AC WAS RETURNED TO SERVICE. IN ADDITION TO ENGINE INSPECTION, THE OIL SCREEN WAS INSPECTED FOR METAL. NONE WAS FOUND. A NEGLIGIBLE AMOUNT OF WATER WAS FOUND IN THE LT FUEL TANK SUMP. (K) 2L72 4R4 R A793 5E8 20050628000062005062800006WP 2005 6 28 ASMF200506019 120050617A3251S4916688AS04210 CONTROL CABLE DOUG DC9 DC982 3022082WP NLG STEERING BROKEN W ASMFO OTHER O OTHER TXTAXI/GRND HDL 1 SW231003Y 48068 AFTER LANDING WHILE TAXING, THE STEERING WENT LOOSE. DURING CHECK, THE STEERING CABLE WAS DETECTED BROKEN. AIRCRAFT WAS SENT TO THE HANGAR AND STEERING CABLE WAS REPLACED IAW MM 32-51-02, NOSE WHEEL STEERING ADJUSTMENT WAS PERFORMED IAW MM 32-51-00, TESTED CORRECT. 2L72 4F A6WE 20050628000082005062800008EA 2005 6 28 A6WA200540184 120050525A5743601R572100321 BUSHING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT MLG TRUNNION MIGRATED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31456ZW 7849 LT MLG AFT TRUNNION FITTING BUSHING IS MIGRATED .055 INCH OUT OF BORE. REMOVED MIGRATED BUSHING AND INSTALLED 1ST OVERSIZE BUSHING, IAW MFG REO. (K) 2L72 4F4 FRTA21EA E15NE 20050628000092005062800009WP 2005 6 28 ASAA0580156 120050228A57535930493 VANE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE RT WING TE FLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02975AS 53451 C-CHECK - RT WING IB FLAP VANE DENTED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER AND FILLER. (K) 2L72 4F4 FRTA6WE E9NE 20050628000102005062800010WP 2005 6 28 ASAA0580171 120050307A5523591041449 TAB DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE LT ELEVATOR DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 HV-CHECK - LT ELEVATOR GEAR TAB IS DELAMINATED. BONDED CORE AND INSTALLED REPAIR DOUBLER. (K) 2L72 4F4 FRTA6WE E9NE 20050628000122005062800012EU 2005 6 28 UPS05144680 120050607A2597 CONNECTOR AIRBUSA300 A300F4622R 3930360EU DOOR SLIDE DIRTY A IPXAK NONE O OTHER ININSP/MAINT 1 SO01121UP 0806 MAIN ENTRY DOOR SLIDE LT INOP. CLEANED CONNECTOR TO ASPSU OPS GOOD PER MM 52-73-18-04. 2L72 4F RTA35EU 20050628000132005062800013NM 2005 6 28 UPS05444651 120050519A5313 STRINGER BOEING747 747123F NM CARGO BAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 BS 2185 S35R STRINGER CORROSION CRACK. STRINGER 35R REPAIRED AS PER SRM 53-10-03 FIG 1 AND SPLICE REINSTALLED AS PER SRM 51-30-02. 2L74 4F A20WE 20050628000152005062800015NM 2005 6 28 UPS05544679 120050608A2560 SMOKE GOGGLES BOEING757 75724APF 1384969NM COCKPIT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01442UP 27387 OBS SMOKE GOGGLES CRACKED. REMOVED AND REPLACED OBS SMOKE GOGGLES. 2L72 4F RTA2NM 20050628000182005062800018WP 2005 6 28 UPS05844685 120050501A5311SK8087855212 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 STA 1160 SEVERE CORROSION ON BASE OF FRAME AT L33L. REMOVED, FABRICATED AND INSTALLED IAW SRM 51-1-20D, 51-1-20 D, DWG 3755842 AND SK808-785521. 2L74 4F RT4A25 20050628000202005062800020WP 2005 6 28 UPS05844687 120050429A5312 PRESSURE PANEL DOUG DC8 DC873F 302199FWP RT MLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 RT MLG WW FWD BULKHEAD LOWER SECTION FASTENERS HAVE MILD CORROSION IN SEVERAL PLACES RUNNING INBD TO OTBD AT SPLICE. REMOVED CORROSION FOUND TO BE WITHIN LIMITS IAW SRM 53-2-0. HFEC INSP DETECTED 3 CRACKS. FABRICATED AND INSTALLED 3 EA. REPAIR ANGLES AND 1 SPACER IAW SRO 08570009, 51-3-2, 51-1-20D, 51-1-21 AND 51-3-0. 2L74 4F RT4A25 20050628000272005062800027NM 2005 6 28 P5CA0501361 120050604A5753 SKIN BOEING747 74746NF 13848BTNM RT FLAP DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 EA15451PA 000569 30809 DELAMINATION OF LEADING EDGE OF RT OUTBD FORE FLAP FOUND NOT TO BE WITHIN SRM LIMITS FOR CONTINUED SERVICE. RT OUTBD FORE FLAP REPLACED PER MM 27-51-05. 2L74 4F RTA20WE 20050628000282005062800028EA 2005 6 28 COMA0560340 120050607A7830 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ACTIVATED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01721CA 7259 RT THRUST REVERSER UNLOCK CAUTION. DEFERRED MAINTENANCE ON RIGHT THRUST REVERSER PER MEL. 2L72 4F RTA21EA 20050628000322005062800032WP 2005 6 28 WX0500042 120050508A33501001191 LIGHT DOUG DC9 DC987 3022087WP EMERGENCY EXIT INOPERATIVE A WX0AK NONE O OTHER ININSP/MAINT 1 WP19948MA 49778 FORWARD EMERGENCY EXIT LIGHT ASSEMBLY INOPERATIVE. MAINTENANCE REPLACED EMERGENCY EXIT LIGHT ASSEMBLY IAW MM 25-60-00. SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050628000332005062800033WP 2005 6 28 WX0500043 120050518A2120 CLAMP DOUG DC9 DC983 3022083WP FLOW CTRL VALVE LOOSE A WX0AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP19862GA 49556 TAIL COMPARTMENT TEMP HIGH WARNING LIGHT ILLUMINATED TEN MINUTES AFTER TAKEOFF WITH HP BLEED OFF PER CHECKLIST WITH NO EFFECT. TURNED OFF RIGHT PACK AND LIGHT WENT OUT AFTER TWO MINUTES. AIRCRAFT RETURNED TO LAS AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND LOOSE CLAMP ON RIGHT FLOW CONTROL VALVE, MAINTENANCE SECURED CLAMP IAW MM 21-31-02. SYSTEM OPERATIONALLY CHECKED GOOD WITH NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050628000342005062800034WP 2005 6 28 WX0500045 120050519A5350 SKIN DOUG DC9 DC983 3022083WP TAILCONE LIGHTNING STRIKEA WX0AK NONE O OTHER ININSP/MAINT 1 WP19891GA 49423 EVIDENCE OF 3 LIGHTNING EXIT POINTS ON TAILCONE AT DRAIN PORT AFT OF FUSELAGE, DRAIN PORT IN TAIL ACCESS PANEL AND AT 8 O’CLOCK POSITION ABOVE ACCESS. MAINTENANCE PERFORMED LIGHTNING STRIKE INSPECTION IAW MM 05-53-00. AIRCRAFT INSPECTED AND RELEASED FOR FERRY FLIGHT TO LAS. LAS - MAINTENANCE COMPLIED WITH TEMPORARY REPAIR AS OUTLINED BY BOEING LETTER NR 1-1LD5Z6 WITH CONTINUED INSPECTIONS EVERY 2 FLIGHTS UNTIL PERMANENT REPAIR AT NEXT A CHECK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050628000352005062800035WP 2005 6 28 WX0500046 120050528A3350 LAMP DOUG DC9 DC983 3022083WP EMERGENCY LIGHTSINOPERATIVE A WX0AK NONE O OTHER ININSP/MAINT 1 WP19866GA 49910 OVERHEAD EMERGENCY LIGHT INOPERATIVE AT ROW 21. MAINTENANCE RELAMPED THE OVERHEAD EMERGENCY LIGHT AT ROW 21. SYSTEM OPERATIONALLY CHECKED GOOD IAW MM 33-53-00. AIRCRAFT RETURNED TO SERVICE 2L72 4F RTA6WE 20050628000362005062800036WP 2005 6 28 WX0500047 120050530A5330 SKIN DOUG DC9 DC983 3022083WP FWD FUSELAGE BIRD STRIKE A WX0AO OTHER O OTHER DEDESCENT 1 WP19868GA 49554 BIRD STRIKE ABOVE CENTER COCKPIT WINDSHIELD. AIRCRAFT LANDED LAS WITHOUT INCIDENT. MAINTENANCE CLEANED AND INSPECTED AREA ABOVE CENTER WINDSHIELD IAW MM 05-51-02 WITH NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050628000372005062800037 2005 6 28 WX0500040 420050501A341810000165101 TRANSDUCER DOUG DC9 DC987 3022087WP STALL WARNING FAULTY A WX0AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP19948MA 49778 STALL INDICATOR ANNUNCIATOR ILLUMINATED PAST APPROXIMATELY 11,000 FEET MSL. QRH PROCEDURE ACCOMPLISHED. CIRCUIT BREAKER X-23 PULLED PER THE QRH. CAPTAIN’S STALL INDICATION SYSTEM INOPERATIVE. AIRCRAFT RETURNED TO LAS AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED AOA TRANSDUCER IAW MM 34-19-01. COMPLETED BITE CHECK IAW MM 34-19-00 WITH NO FAULTS REPORTED. AIRCRAFT AIRBORNE SYSTEM TEST SUCCESSFUL. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050628000382005062800038 2005 6 28 WX0500044 420050521A22104034241973 CONTROLLER DOUG DC9 DC987 3022087WP NR 2 AUTOPILOT FAILED A WX0AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP19948MA 49778 NR 2 AUTOPILOT INOPERATIVE, NR 2 DFGC FAILED. AIRCRAFT RETURNED TO LAS AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 DFGC AND PERFORMED RETURN TO SERVICE TEST. SYSTEM OPERATIONALLY CHECKED GOOD IAW AMM 22-01-01. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050628000392005062800039EU 2005 6 28 05FDEA01524 120050607A5753 SKIN AIRBUS310 A310 EU RT FLAP GROOVED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25404FE 233 RT WING I/B FORE FLAP, CENTER LWR L/E HAS A 1.5 INCH GROOVE WORN INTO SKIN. REMOVED AND REINSTALLED , OPS TEST FLAP IAW A310-200 AMM 27-50-15-4 OPS TEST GOOD. REPAIRED FORE FLAP PER EA 6-5750-89216 AND A310-200 SRM 51-25-00. MAJOR REPAIR IAW FED-EX GMM 6-2-100. 2L72 4F RTA35EU 20050628000402005062800040EU 2005 6 28 05FDEA01525 120050607A5330 BUTTSTRAP AIRBUS310 A310 EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25404FE 233 CORROSION AT TWO NUT PLATE HOLES ON PANEL SPLICE FOR 326JL. REMOVED CORROSION ON PANEL 326JL BUTTSTRAP. MATERIAL LOSS FOUND TO BE OUT OF LIMITS PER A310 SRM 55-40-00. REMOVED AND REPLACED BUTTSTRAP PER A310 SRM 51-40-21. 2L72 4F RTA35EU 20050628000412005062800041EU 2005 6 28 05FDEA01526 120050607A5330 BUTTSTRAP AIRBUS310 A310 EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25404FE 233 CORROSION AROUND NUTPLATE RIVETS ON PANEL SPLICE FOR 326GL, 1 AREA ON ONE END AND 4 AREAS ON OTHER END OF PANEL. REMOVED CORROSION ON PANEL 326GL BUTTSTRAP. MATERIAL LOSS FOUND TO BE OUT OF LIMITS PER A310 SRM 55-40-00. REMOVED AND REPLACED BUTTSTRAPS PER A310 SRM 51-40-21. MINOR REPAIR. 2L72 4F RTA35EU 20050628000422005062800042EU 2005 6 28 05FDEA01527 120050607A5420 SUPPORT BRACKET AIRBUS310 A310 EU NR 2 PYLON CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25404FE 233 FOUND ANGLE SUPPORT BRACKET FOR MAIN HYDRAULIC LINE CRACKED INBD SIDE OF PYLON AT RIB 20. REMOVED AND REPLACED ANGLE ON NR 2 PYLON IAW A310 SRM 51-40-21 AND 51-72-10. 2L72 4F RTA35EU 20050628000442005062800044NM 2005 6 28 DHL2005784551 120050525A5754 DOUBLER BOEING727 727227 1384078NM NR 6 SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01784DH 22001 FOUND NR 6 SLAT PREVIOUS REPAIR AT T/E I/B HOOK IS CRACKED. REMOVED PREVIOUS REPAIR. FABBED NEW REPAIR IAW 727 SRM 51-30-2 AND 57-50-3 FIG 10. DOUBLER TREATED, PRIMED, AND INSTALLED IAW 727 SRM 51-10-2 AND 57-50-3 FIG 10. 2L73 4F A3WE 20050628000452005062800045WP 2005 6 28 0500869952 120050605A2750 FLAP SYSTEM DOUG DC9 DC931 3022065WP WINGS OUT OF RIG A NWAAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL01916RW 47144 ACFT BEING CONFIGURED FOR LANDING AND ONCE FLAPS EXTENDED PAST 25 DEGREES ACFT ROLLED TO RIGHT. CREW DID NOT NOTICE ANY UNCOMMANDED AIRCRAFT MOVEMENTS WHEN FLAPS WERE INITIALLY LOWERED, ONLY AFTER THE 25 DEGREE DOWN SETTING. FLIGHT CREW STABILIZED ACFT FOR REMAINDER OF APPROACH PATH AND FLIGHT LANDED WITHOUT INCIDENT. MX COULD NOT FIND ANY DISCREPANCIES BUT RIGGED TRAILING EDGE FLAP SYSTEM. ACFT RETURNED TO SERVICE. 2L72 4F A6WE 20050628000482005062800048WP 2005 6 28 ABXA050145 120050608A3260 BULB DOUG DC9 DC931 3022065WP MLG DOOR IND FAILED A ABXAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL23946AX 47003 GEAR DOOR OPEN LIGHT DID NOT ILLUMINATE BEFORE EXTENSION OF LANDING GEAR. NORMAL OPERATION OF LANDING GEAR SYSTEM OCCURRED (3 GREEN, GOOD HYDRAULICS). EMERGENCY CALLED, CREW DID FLY BY TOWER TO VERIFY GEAR DOWN AND DOORS UP. INSPECTED GEAR DOOR SWITCHES AND LAMP ASSEMBLIES. FOUND LAMP FILAMENT BROKEN POST INSIDE BULB. REPLACED BULB ON GEAR DOOR OPEN INDICATOR. SYSTEM OPS CHECKED GOOD IAW DC-9 MM 32-60. 2L72 4F A6WE 20050628000492005062800049WP 2005 6 28 ABXA050146 120050527A5210SB095201385 DOOR DOUG DC9 DC931 3022065WP LT MAIN CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23947AX 47004 LT MAIN ENTRY DOOR FORWARD UPPER CORNER APPEARED TO BE CRACKED. DOOR REPLACED ON NON ROUTINE 0311, IAW DC-9 MM. 2L72 4F A6WE 20050628000522005062800052WP 2005 6 28 ABXA050149 120050601A5312991224617 BULKHEAD DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23947AX 47004 LEFT BULKHEAD SPAR STUB (HORIZONTAL WEB) AT FS 1039 APPROX LONGERON 15 LEFT CRACKED ON BOTTOM COMING FROM INBOARD FORWARD BOLT HOLE. STOP DRILLED/REPAIRED IAW DC-9 SRM 53-01. 2L72 4F A6WE 20050628000542005062800054EA 2005 6 28 VTZA200500100 120050603A5320601R3117117 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27627BR 7233 INTERCOSTAL CRACKED AT .250 IN LENGTH ON LT INBOARD SIDE AT FS 484 LEFT BETWEEN BL 27.00. 2L72 4F RTA21EA 20050628000562005062800056EA 2005 6 28 VTZA200500102 120050603A5320601R35031239 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27627BR 7233 LT FS 621 FLOOR SUPPORT CRACKED 1 IN. 2L72 4F RTA21EA 20050628000592005062800059NM 2005 6 28 DHL2005784517 120050519A5754 RIB BOEING727 727227 1384078NM NR 5 LE SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01784DH 22001 FOUND NR 5 SLAT LE INT AT ACTUATOR ATTACH POINT INBD AND OUT RIBS CRACKED. PREVIOUSLY REPAIRED. REMOVED AND REPLACED DAMAGED RIBS AT NR 5 L/E SLAT ACT ATTACH ON SLAT PN 65-17276U1 AND 65-17276-9 BOTH PO NR 516347 IAW 727 SRM 51-30-2. 2L73 4F A3WE 20050628000612005062800061 2005 6 28 2005UALA00483 420050527A3417 ADC BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE RIGHT FAILED A UALAA UNSCHED LANDING O OTHER CRCRUISE 1 WP29663UA 27160 FAILURE OF F/O AIR DRIVEN COMPUTER AND ALTIMETER. RT AIR DATA COMPUTER RPL, MR41190, NO DASH, BUT S/N=88041280. A/C HAD PREVIOUS HISTORY ON 18 MAY. NO UNIT HISTORY AVAILABLE IN CIDER FOR THIS S/N, SUSPECT THIS IS 1ST REMOVAL. 2L72 4F4 FRTA1NM E24NE 20050628000622005062800062NM 2005 6 28 2005UALA00484 120050530A3350582233 BATTERY BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHTSDISCHARGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29104UA 26902 LT SIDE EMERGENCY STRIP LIGHTING IN ZONE C GOES ON AND OFF. BATTERY NOT HOLDING CHARGE. EEL LIGHT BATTERY REPLACED. 2L74 4F4 FRTA20WE E24NE 20050628000662005062800066EU 2005 6 28 05FDEA01542 120050608A5320A5377265020202 FITTING AIRBUS310 A310 EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25404FE 233 FS 20A STR 41R TO STR 45R HAS 1EA FITTING WITH CORROSION (OFF ACFT PART) PART NR A5377265020202. PART WAS REMOVED ON N00500 ITEM NR 22 ON JPF LOCATED AND DRILLED FITTING P/N A5377265020202 IAW A310/200 SRM 51-40-21. RESTORED PROTECTIVE COATING IAW A310/200 SRM 51-75-10. PART REMOVED AND WILL BE RE-INSTALLED ON NR N00500. 2L72 4F RTA35EU 20050628000672005062800067NM 2005 6 28 05FDEA01533 120050608A5754 RIB DOUG MD11 MD11 3023602NM NR 8 SLAT CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 RIGHT WING, NR 8 SLAT MOST OUTBOARD RIB FOUND CRACKED. SLAT REMOVED AND REPLACED AS PER AMM 27-80-30-4. ADJUSTMENT AND OPERATION CHECK CARRIED OUT FOUND SATIS AS PER AMM 27-80-00-5. 2L73 4F RTA22WE 20050628000682005062800068NM 2005 6 28 DL764050294 120050527A3350D71702030 CHARGER BOEING767 767432ER 1385134NM EMERGENCY LIGHTSINOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27829MH 29700 EMERGENCY TRACK LIGHTS INOP FROM 25FG TO 32 FG. FOUND BATT CHARGER BAD AT 29 FG SIDEWALL AND REPAIRED SHORTED WIRE AT ROW 25 FG SIDEWALL. OPS CK NORMAL . ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS. 2L72 4F RTA1NM 20050628000692005062800069EA 2005 6 28 COMA0560339 120050606A3230750006000 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A COMAO OTHER J WARNING INDICATION CLCLIMB 1 SO01912CA142935016 7011 GEAR DISAGREE AND NOSE DOOR OPEN MESSAGE. REPLACED NLG SELECTOR VALVE. 2L72 4F RTA21EA 20050628000702005062800070EA 2005 6 28 COMA0560338 120050606A3233 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA NLG BAY NOISY A COMAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO01912CA 7011 ACTUATOR NOISE IN NLG BAY. CLEANED AND LUBRICATED NLG DOOR ACTUATING MECHANISM. 2L72 4F RTA21EA 20050628000712005062800071 2005 6 28 RAIA005040029 420050411A34207003360948 AHRS JETAIRJETSTMJETSTM4101 1500501EU NR 1 INTERMITTENT A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03565HK 41082 NR 1 AHRS ADI CAP FAIL INTERMITTENTLY. MAINTENANCE REMOVED AND REPLACED NR 1 AHRU. OPS CHECKED GOOD. 2L72 4T RTA41NM 20050628000722005062800072SO 2005 6 28 RAIA00506001 120050603A7603MS252531 SWITCH EMB 145 EMB145 3260210SO POWER LEVER MALFUNCTIONED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03807HK 145119 LT ENGINE IDLE STOP FAILED. MAINTENANCE REMOVED AND REPLACED NR 1 IDLE STOP SWITCH. OPS CHECKED GOOD. 2L72 4F RTT00011AT 20050628000762005062800076SO 2005 6 28 RAIA00504030 120050413A2913971533 PUMP EMB 145 EMB145LR 3260212SO NR 2 INOPERATIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03834HK 145269 ELECTRIC HYDRAULIC PUMP INOPERATIVE. MX REMOVED AND REPLACED NR 2 ELECTRIC DRIVEN PUMP. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050628000782005062800078EA 2005 6 28 VTZA200500106 120050604A5712601R102328 RIB CNDAIRCL600 CL6002B19 1900309EA RT WING CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27627BR 7233 RT BATTERY RIB CRACKED .750 IN. BETWEEN ATTACHING FASTENERS. 2L72 4F RTA21EA 20050628000792005062800079NM 2005 6 28 HNAA0500050 120050606A291082910009143 LINE DHAV DHC8 DHC8102 2809003NM HYD SYS LEAKING A HNAAL ABORTED APPROACH KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 EA07940HA4283742837 156 ON APPROACH, CREW NOTICED NR 2 HYDRAULIC QTY AT 0 PSI. AFTER NORMAL SELECTION OF GEAR DOWN NR 2 ENGINE HYDRAULIC PUMP CAUTION LIGHT ILLUMINATED. ENGINE HYDRAULIC PUMP RAN FOR 10 MINS AT 0 QTY FOUND DOWN LINE FOR NOSE LANDING GEAR DOORS LEAKING. INSTALLED TEMP FLEX LINE. PEFORMED LEAK CHECKS. 2H72 4T RTA13NM 20050628000802005062800080NM 2005 6 28 DHL2005784514 120050518A5311 FRAME BOEING727 727227 1384078NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01784DH 22001 STA 720A FRAME IS DENTED ABOVE STR 23R. FOUND DENT TO BE OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 1, CUT OUT DAMAGED AREA . FABRICATED ANGLE REPAIR IAW B727 SRM 53-10-2 FIG 3. ALODINE AND PRIMED PART AND AREA IAW B727 SRM 51-10-2. INSTALLED PART IAW B727 SRM 51-40-3 FIG 1. 2L73 4F A3WE 20050628000812005062800081SO 2005 6 28 C2XA05BT036 120050606A33502013BR BATTERY PACK EMB 145 EMB145XR 3260214SO EMERGENCY LIGHTSFAULTY A C2XAK NONE O OTHER ININSP/MAINT 1 SW27311313597 3597 145705 DURING ROUTINE INSP FOUND EMERGENCY LIGHTS SYSTEM NR 1 TO BE FAULTY. REMOVED AND REPLACED NR 1 EMERGENCY LIGHT BATTERY PACK IAW EMB145XR AMM NR 33-50-04. OPS CHECKED GOOD. 2L72 4F RT 20050628000822005062800082SO 2005 6 28 C2XA05BT037 120050606A3350 LIGHT EMB 145 EMB145XR 3260214SO LT OVERWING BROKEN A C2XAK NONE O OTHER ININSP/MAINT 1 SW2726545 145558 DURING ROUTINE INSP FOUND NR 1 (LT SIDE) EMERGENCY OVERWING EMERGENCY LIGHT ASSEMBLY AND NUT PLATES BROKEN. REMOVED AND REPLACED NR 1 LT EMERGENCY OVERWING LIGHT ASSEMBLY IAW EMB145 MM NR 33-50-07, REMOVED AND REPLACED NR 1 EMERGENCY LIGHT BATTERY CHARGER AND BATTERY [PART NUMBERS 11-0049 AND AD-2013-1A] IAW EMB145 AMM NR 33-50-04. OPS CHECKED GOOD. 2L72 4F RT 20050628000842005062800084WP 2005 6 28 ABXA050144 120050606A3150R6259ABX7 ANNUNCIATOR DOUG DC9 DC931 3022065WP COCKPIT MALFUNCTIONED A ABXAK NONE NGLFALSE WARNING MULTIPLE FAILURE NO TEST ININSP/MAINT 1 GL23907AX1072 47203 AFTER EMERGENCY POWER CHECK, LOWER CARGO FIRE, TAIL COMP TEMP HIGH, APU FIRE, AND DC EMERGENCY BUSS OFF LIGHTS ILLUMINATED. REMOVED AND REPLACED ANNUNCIATOR PANEL. OPS CHECKED GOOD IAW DC-9 AMM 31-03-00-2-0002. 2L72 4F A6WE 20050628000852005062800085NM 2005 6 28 DHL2005784516 120050521A5752 TAB BOEING727 727227 1384078NM LT O/B AILERON DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01784DH 22001 LT O/B AILERON TAB INB END DELAMINATED (AREA MARKED). REMOVED DELAMINATED EXISTING REPAIR FROM LT O/B AILERON TAB LWR SURFACE, FABRICATED FILLER AND DOUBLER. CLEANED, PREPPED, APPLIED ADHESIVE PRIMER, BONDED, CLEANED, TREATED, PRIMED AND SEALED EDGES, IAW B727 SRM 57-50-2 FIG 8 AND 51-40-20 FIG 31 TAB WEIGHT 3.65 LBS WITHIN LIMITS IAW B727 SRM 51-40-20- FIG 31 2L73 4F A3WE 20050628000872005062800087NE 2005 6 28 NACA20050013 220050602A85303556993 CYLINDER DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE NR 2 ENGINE FAILED A NACAO OTHER RY PARTIAL RPM/PWR LOSS ENGINE STOPPAGE CRCRUISE 1 AL0399330607 607 43576 P34218 NR 2 ENGINE SHUTDOWN DUE TO RUNNING ROUGH AND WOULDN'T STAY RUNNING. NR 18 CYLINDER FAILURE. REPLACED NR 18 CYLINDER. OPS CHECKED GOOD. 2L74 4R4 R 6A3 5E8 20050628000882005062800088WP 2005 6 28 ASAA0580153 120050228A5322993644817 SHEAR TIE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02975AS 53451 C-CHECK - SHEAR TIE CORRODED ON AFT SIDE OF LONGER. REMOVED DAMAGED SECTION AND INSTALLED REPAIR DOUBLERS. (K) 2L72 4F4 FRTA6WE E9NE 20050628000892005062800089EA 2005 6 28 ASOA05363 120050421A33501317 LAMP BRUCE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27902EV 7620 DURING A GROUND INSPECTION, THE THIRD EXTERIOR EMERGENCY LIGHT ON THE LT SIDE WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE THIRD EXTERIOR EMERGENCY LIGHT ON THE LT SIDE. OPS CHECK GOOD. AIRCRAFT OF FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050628000952005062800095WP 2005 6 28 JRAA587060705 120050607A571334033101027 LONGERON CVAC 440 440 2422902WP RROYCEDART DART54210 54522EU LT WING CORRODED A JRAAK NONE O OTHER ININSP/MAINT 1 GL11587CA43490 463 INTERGRANULAR CORROSION WAS FOUND ON THE LONGERON CHANNEL AT FUSELAGE BUTTOCK LINE 0, WING STATION 403.0. THIS CORROSION NOTED ON THE LT SIDE, 10 INCHES FORWARD OF THE REAR LOWER WING SPAR. ACCESS THROUGH THE LT WING IB DRY BAY PANEL. (K) 2L72 4R4 T 6A6 E5EU 20050628000972005062800097EA 2005 6 28 ASOA05460 120050525A25101C30941AJF STEP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE COPILOT SEAT MISSING A ASOAK NONE O OTHER ININSP/MAINT 1 SO27874AS 10341405 7551 DURING A GROUND INSPECTION, THE EMERGENCY EGRESS STEP LOCATED ON TOP OF THE COPILOTS SEAT ASSEMBLY WAS FOUND MISSING. MAINTENANCE INSTALLED THE EMERGENCY EGRESS STEP ON TOP OF THE COPILOTS SEAT ASSY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050628000982005062800098EA 2005 6 28 ASOA05467 120050527A5210 HANDLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR BINDING A ASOAK NONE O OTHER ININSP/MAINT 1 SO27820AS 7188 DURING A GROUND INSPECTION, THE PASSENGER DOOR WAS FOUND DIFFICULT TO OPEN AND THE SLOW HANDLE PUSHING OUT. MAINTENANCE LUBRICATED THE PASSENGER DOOR HANDLE AND INTERNAL MECHANISM. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050628001012005062800101EA 2005 6 28 ASOA05456 120050510A5242H34455 HANDLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE E/E BAY DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27867AS11377 7464 7463 DURING A C-CHECK, THE AVIONICS BAY DOOR OUTER HANDLE CUP WAS FOUND CRACKED AROUND THE HANDLE BOSS. MAINTENANCE REMOVED AND REPLACED THE AVIONICS BAY DOOR HANDLE ASSEMBLY IAW AMM AND SRM. OPS CHECK GOOD. (K) 2L72 4F4 FRTA21EA E15NE 20050628001022005062800102EA 2005 6 28 ASOA05459 120050524A2120 ODOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE COCKPIT DETECTED A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27833AS 7246 DURING TAKEOFF AND LANDING, THE CREW NOTICED A HOT BRAKE ODOR. THE AC LANDED SAFELY. MAINTENANCE JACKED THE MAIN LANDING GEARS WITH BRAKES RELEASED. BOTH IB AND OB BRAKES OPERATED FREELY AND ALL GEAR INDICATIONS WERE GOOD. MAINTENANCE ALSO TESTED THE ANTI-SKID SYSTEM. NO DEFECTS WERE NOTED. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050628001032005062800103EA 2005 6 28 ASOA05462 120050525A33506100928 LAMP CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE EMERGENCY LGIHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27707EV 10057 DURING AN A-CHECK, THE EMERGENCY LIGHT AFT OF THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMPS IN THE EMERGENCY LIGHT AFT OF THE SERVICE DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA EOOO63EN 20050628001042005062800104EA 2005 6 28 ASOA05466 120050527A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27851AS 7360 DURING HANGAR MAINTENANCE, THE LT FRAME STA 640 WAS FOUND TO BE CRACKED AFT OF LBL 10 BEYOND LIMITS. THE AIRCRAFT WAS INSPECTED AND FOUND TO BE SAFE FOR A FERRY FLIGHT FOR PERFORMANCE OF THE APPROPRIATE CORRECTIVE ACTION. THE AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE LT 640 FRAME AND DOUBLER IAW SRM. (K) 2L72 4F4 FRTA21EA E15NE 20050628001142005062800114EA 2005 6 28 ASOA05397 120050503A5210601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27845AS 7324 7324 DURING A-CHECK, THE PASSENGER DOOR BOTTOM STEP WAS FOUND CRACKED AT THE HANDRAIL HINGE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP IAW MM. OPERATIONAL CHECKS GOOD. (K) 2L72 4F4 FRTA21EA E15NE 20050628001192005062800119WP 2005 6 28 ASAA0580165 120050307A532199365811 FLOORBOARD DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE CABIN DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 HV - CHECK - PAX CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (K) 2L72 4F4 FRTA6WE E9NE 20050628001202005062800120WP 2005 6 28 ASAA0580044 120050129A3397 WIRE HARNESS DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE LIGHT BALLAST SHORTED A ASAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM02931AS 49232 (SMOKE/FLAMES/FUMES OVERHEAD AT 21 ABC) REPORTED BY PASSENGER AND AS A PIREP, THIS WAS PRECEEDED BY AN EARLIER REPORT PRIOR TO FLIGHT OF (WATER LEAKING AT ROW 21 ABC/DEF O/H). INSP REVEALED (FRIED) BALLAST CONNECTOR. REPLACED BALLASTS AND BALLAST HARNESS ADAPTERS AT 21-22 ABC AND 23-24 ABC LOCATIONS PRIOR TO FLIGHT THE UPPER STROBE LIGHT ASSY HAD BEEN RESEALED IN RESPONSE TO THE WATER LEAK SQUAWK. 2L72 4F4 F A6WE E9NE 20050628001242005062800124WP 2005 6 28 ASAA0580166 120050307A53219936640501 FLOORBOARD DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE CABIN DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 HV - CHECK - PAX CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (K) 2L72 4F4 FRTA6WE E9NE 20050628001262005062800126EA 2005 6 28 ASOA05496 120050603A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27850AS 7355 DURING A C-CHECK, THE FORWARD AND AFT FLOOR SUPPORT ANGLES FS 280 BETWEEN LBL 9 AND RBL 9 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FORWARD AND AFT FLOOR SUPPORT ANGLES FS 280 BETWEEN LBL 9 AND RBL 9 IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050628001282005062800128CE 2005 6 28 GUU2005F00022 120050605A3240MS28775112 PACKING BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA LT BRAKE LEAKING A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO2982539 UE168 LT BRAKE INOPERATIVE. PEDAL GOES TO FLOOR. REPLACED LT BRAKE INTERCONNECT PACKINGS. BLED BRAKE SYS. (K) 2L72 4T3 TRTA24CE E2NE 20050624000212005062400021SO 2005 6 24 RAIA00506020 120050614A2130 UNKNOWN EMB 145 EMB145LR 3260212SO UNKNOWN A RAIAD RETURN TO BLOCK GJ MULTIPLE FAILURE WARNING INDICATION TXTAXI/GRND HDL 1 CE03812HK 145373 FLT 3511 LGA - ON TAXI OUT WITH NR 2 ENGINE ONLY, AIRPLANE SUDDENLY STARTED TO PRESSURIZE AND BOTH PFD'S AND MFD'S SHUT OFF, CHANNEL 1 WARNING CAME ON, PUSHER AND SHAKER WENT ON, ALL LIGHTS WENT OFF AND APU SHUT ITSELF OFF. MAINTENANCE INSPECTED THE BATTERY COMPARTMENT, BOTH LT AND RT POWER CONTROL BITES, REVIEWED CMC DATA AND PERFORMED OPS CHECKS OF THE AIRCRAFT ELECTRICAL SYSTEM, APU, SINGLE AND DUAL ENGINE RUNS AT LOW POWER SETTINGS. UNABLE TO DUPLICATE THE PROBLEM. 2L72 4T RTT00011AT 20050624000232005062400023NM 2005 6 24 AT0500019 120050610A2612473465MOD01 CONTROL UNIT BOEING717 717200 1383700NM FIRE DETECTION INOPERATIVE A ZZDAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO15969AT 55030 IN CLIMB RT ENG FIRE IND CAME ON WITH NO LIGHT IN RT FIRE HANDLE. LANDED IN BWI AT 108000 LBS. PERFORMED FIM TASK 26-11, TASK 807-808 ALERT ENGINE RT FIRE. REMOVED AND REPLACED RIGHT ENGINE FDCU IAW B717 AMM 26-11 FAULT TEST OK. (REF 44EB02) NOTED BY MX OVERWEIGHT LANDING INSP REQUIRED AT 110,000 LBS. 2L72 4F TRA6WE 20050624000282005062400028SO 2005 6 24 C2XA05CL046 120050615A2611 WARNING LIGHT EMB 145 EMB145LR 3260212SO CARGO SMOKE FALSE ACTIVATIONA C2XAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW2712996 145296 MHT FLIGHT 3054, THE CREW REPORTED A BAGGAGE COMPARTMENT SMOKE INDICATION ON THE EICAS THAT WOULD NOT CLEAR. MAINTENANCE INSPECTED AND RESET AIRCRAFT POWER. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20050624000352005062400035NM 2005 6 24 UPS05444583 120050520A5313 STRINGER BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSP TYPE: C M/D BS 742 STR 10L STR END FOUND CRACK AS MARKED, (CRACK LENGTH 2.75 INCHES). M/D BS 741 TO BS 770 STR 10L AREA STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4. 2L74 4F A20WE 20050624000382005062400038NM 2005 6 24 UPS05444586 120050518A5347 SEAT TRACK BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSP TYPE: C U/D BS 660-710 RBL 48, SEAT TRACK CROWN HI-LOCK AREA FOUND CORROSION. CORROSION BLENDED OUT 0.045 INCH BY 0.5 INCH BY 2 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. U/D BS 650 TO 720 RBL 48 INCH TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A. 2L74 4F A20WE 20050624000392005062400039NM 2005 6 24 UPS05444587 120050518A5322 SHEAR TIE BOEING747 747123F NM FWD CARGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSP TYPE: C FWD CARGO BS 900 STR 46R- 47R FWD SHEAR TIE FOUND CORRODED. CORROSION BLEND OUT 0.036 INCH BY 0.75 INCH BY 2.0 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. FWD CARGO BS 900 STR 46R - 47R SHEAR TIE REPAIRED AS PER SRM 53-10-04 FIG 3A. 2L74 4F A20WE 20050624000412005062400041NM 2005 6 24 UPS05444589 120050518A5320 WEB BOEING747 747123F NM AFT CARGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSP TYPE: C AFT CARGO COMPT BS 1794 S34R CLOSURE WEB CORRODED. CORROSION BLEND OUT 0.019 INCH BY 0.75 INCH BY 1.5 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT, WEB REPAIRED AS PER SRM 51-40-02 FIG 1. 2L74 4F A20WE 20050624000452005062400045NM 2005 6 24 UPS05444593 120050515A5315 FLOORBEAM BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSP TYPE: C, M/D - BS 460 RT FLOORBEAM WEB FOUND CRACKED AT STR 13R RBL 98 AREA, (CRACK LENGTH 0.3750 IN). FLOORBEAM WEB REPAIRED AS PER SRM 53-10-07 FIG 11. 2L74 4F A20WE 20050624000532005062400053EA 2005 6 24 MASA200500361 120050516A3350 BATTERY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSDISCHARGED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0777275 7275 EMERGENCY FLOOR TRACK SECTIONS AT ROW 2, 3, 4 AND 5 INOP. MX CHARGED BATTERIES FOR 1 HR AND LIGHT OPERATED NORMALLY. 2L72 4F RTA21EA 20050624000722005062400072EA 2005 6 24 QXEA200501068 120050620A3240 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA ZONE 200 ILLUMINATED A QXEAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM09616QX4241 4241 10128 BOI - ON FLIGHT 4276, RETURNED TO GATE, ANTI SKID INBOARD CAUTION MESSAGE. REMOVED AND REPLACED PARKING BRAKE SHUTOFF VALVE. OPERATIONAL CHECK GOOD, MESSAGE CLEARED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20050624000822005062400082EU 2005 6 24 AWXA200500727 120050620A3260C24730100 UPLOCK AIRBUS320 A320231 3930325EU NLG MALFUNCTIONED A AWXAO OTHER J WARNING INDICATION CLCLIMB 1 WP28644AW 317 DURING GEAR RETRACTION AFTER TAKEOFF, NOSE GEAR STAYED DOWN & ALL GEAR DOORS STAYED DOWN. MX R & R THE NLG DOOR UPLOCK ASSY IAW AWXA TASK CARD F4N32301. OPS CHECKS GOOD. TEAR DOWN REPORT CONFIRMS REASON FOR REMOVAL OF NLG DOOR UPLOCK ASSEMBLY. FOUND BINDING BETWEEN STOPS ON UNIT. BOTH STOPS WERE FOUND WORN. STOPS WERE REPLACED AND UNIT WAS TESTED IAW CMM 32-37-09 REV. 7 2L72 4F RTA28NM 20050624000922005062400092 2005 6 24 SWAA051824 420050620A25651061323478 SLIDE BOEING737 7373A4 1384585NM L1 DOOR DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29677AA 23289 DURING SCHEDULED RON CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATING LOW. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20050624000932005062400093NM 2005 6 24 SWAA051825 120050620A5753 SKIN BOEING737 7377H4 1384404NM LT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29742SW 000176 29278 LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2L72 4F RTA16WE 20050624001012005062400101NM 2005 6 24 SWAA051827 120050621A55536546874 FITTING BOEING737 7373H4 1384600NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND LT & RT VERTICAL STAB FWD & AFT FAILSAFE CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER. 2L72 4F RTA16WE 20050624001022005062400102NM 2005 6 24 SWAA051828 120050621A532269353656 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 360, STR 14L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050624001132005062400113NM 2005 6 24 SWAA051839 120050621A3350MS155721 BULB BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29750SA 29802 DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050624001222005062400122NM 2005 6 24 PIDA20050039 120050603A5320 INTERCOSTAL BOEING757 757200 1384950NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05750WL 23928 INTERCOSTAL FROM BS 1661 TO 1681 AT RBL 10 CRACKED. REPLACED UPPER CHORD OF INTERCOSTAL PER SRM 53-60-51. 2L72 4F RTA2NM 20050624001272005062400127NM 2005 6 24 PIDA20050045 120050603A5320 CHANNEL BOEING757 757200 1384950NM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05750WL 23928 HAT CHANNEL CRACKED AND CORRODED AT BS 374 FROM RBL 12 TO RBL 23. REPLACED CHANNEL PER SRM 51-10-00. 2L72 4F RTA2NM 20050624001312005062400131NM 2005 6 24 PIDA20050046 120050603A5320 ANGLE BOEING757 757200 1384950NM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05750WL 23928 ZEE ANGLE AT L-2 DOOR CORRODED. REPLACED ZEE ANGLE PER SRM 51-10-00. 2L72 4F RTA2NM 20050624001372005062400137NM 2005 6 24 PIDA20050026 120050603A5340 SUPPORT BOEING757 757200 1384950NM LIFE RAFT CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05750WL 23928 AFT CABIN, AT BS 1620, AFT LIFE RAFT, RIGHT HAND SUPPORT FRAME CRACKED. REPAIRED PER SRM 51-70-11. 2L72 4F RTA2NM 20050624001462005062400146NM 2005 6 24 PIDA20050041 120050603A5347 SEAT TRACK BOEING757 757200 1384950NM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05750WL 23928 SEAT TRACK AT LBL25 CORRODED AT BS1320. REPLACED SECTION OF SEAT TRACK FROM BS 1320 TO BS 1370 PER SRM 53-00-52. 2L72 4F RTA2NM 20050624001492005062400149EA 2005 6 24 SWIA200515085 120050601A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07951SW4838 865 7795 ON START AT THE GATE,STAB CH 1 INOP STATUS MSG ILLUMINATED. REPLACED HORIZONTAL STAB TRIM ACTUATOR IAW CRJ 200 M/M 27-42-01 AND REPLACED MOTOR CONTROL UNIT IAW CRJ 200 M/M 27-42-05. OPERATIONAL CHECK GOOD, PN 7062-3; SN OFF 2001. 2L72 4F RTA21EA 20050627000052005062700005EA 2005 6 27 SWIA200515091 120050601A2741 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA COCKPIT STICKING A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07980SW 7955 FO TRIM SWITCH STICKS. REPLACED FO'S STAB TRIM SWITCH, OPERATION CHECK GOOD IAW CRJ 200 MM 27-41-05. 2L72 4F RTA21EA 20050627000092005062700009EA 2005 6 27 SWIA200515096 120050602A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07465SW7842 7842 7845 STAB CHANNEL 2 FAILED. REPLACED HST ACTUATOR AND MCU IAW CRJ MM 27-42-01, 27-42-05. OPERATIONAL CHECK GOOD, P/N 7062-3 S/N OFF 1077. 2L72 4F RTA21EA 20050627000132005062700013EA 2005 6 27 SWIA200515100 120050604A3397 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT LOOSE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07592SW 7279 OVERHEAD EMERGENCY EXIT SIGN AT OVERWING EXITS INOP. RESECURED LOOSE CONNECTOR. OPERATIONAL CHECK GOOD IAW AMM SUBTASK 33-51-00-720-801. 2L72 4F RTA21EA 20050627000142005062700014EA 2005 6 27 SWIA200515101 120050607A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07439SW 7578 FLOOR EMERGENCY FLOODLIGHT ON BACKWARD OF WARDROBE UNIT BROKEN. REPLACED FLOODLIGHT ASSY WITH NEW UNIT. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050627000152005062700015EA 2005 6 27 SWIA200515102 120050604A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA LAVATORY MALFUNCTIONED A SWIAO OTHER N FALSE WARNING APAPPROACH 1 NM07916SW 7634 PRIOR TO FINAL APPROACH RECEIVED SMOKE TOILET CAUTION. FOUND NO EVIDENCE OF BURNING OR COMPONENT OVERHEATING IN LAV. PERFORMED LAV SMOKE DETECTOR SELF TEST. SELF TEST GOOD. 2L72 4F RTA21EA 20050627000162005062700016EA 2005 6 27 SWIA200515103 120050601A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07934SW 7722 OVERHEAD AISLE LIGHT INOP, LOCATION FORWARD. RELAMPED OVERHEAD EMERGENCY LIGHT "FWD". OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050627000182005062700018EA 2005 6 27 SWIA200515105 120050603A2741 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA COCKPIT STICKING A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07589SW 7072 BOTH STAB TRIM SWITCHES STICKY. REPLACED CA AND FO'S STAB TRIM SWITCHES PER MM 27-41-05. OPERATIONAL CHECK GOOD IAW MM 27-40-00. 2L72 4F RTA21EA 20050627000302005062700030EA 2005 6 27 SWIA200515117 120050606A5610 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07437SW 7564 FO'S WINDSHIELD UPPER AFT SHOWS SMALL CRACK FORMING IN WINDSHIELD. REPLACED FO'S WINDSHIELD IAW 56-11-01, PN NP-139321-12; SN OFF 0115148972. 2L72 4F RTA21EA 20050627000342005062700034EA 2005 6 27 SWIA200515121 120050609A271010231007 DAMPER CNDAIRCL600 CL6002B19 1900309EA AILERON FLUTTER LEAKING A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION DEDESCENT 1 NM07943SW8996 7762 FLUTTER DAMPER STATUS MSG ILLUMINATED ON DESCENT. REPLACED RT AILERON FLUTTER DAMPER IAW CRJ MM 27-15-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050627000362005062700036EA 2005 6 27 SWIA200515123 120050606A2760C13045BA03 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA SPOILER MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07732SK 10194 CREW REPORTS RUDDER LIMIT FAULT STATUS MESSAGE. REPLACED SSCU 1 IAW CRJ MM 27-61-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050627000742005062700074NM 2005 6 27 UPS05444598 120050518A5315 FLOORBEAM BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 BS 1090 LBL 11 - RBL 11 FLOOR SUPPORT CORROSION. CORROSION BLEND OUT 0.052 BY 1.125 BY 1.75 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, M/D BS 1090 LBL 11 - RBL 11 FLOOR SUPPORT REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050627000772005062700077NM 2005 6 27 UPS05444601 120050518A5347 SEAT TRACK BOEING747 747123F NM MAIN DECK CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 BS 1000-1060 RBL 10 SEAT TRACK FLANGE CORROSION. CORROSION BLEND OUT 0.028 BY 1.0 BY 1.0. EXCEED SRM 53-10-01 FIG 1 LIMIT, M/D BS 1000-1130 RBL 11 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 34. 2L74 4F A20WE 20050627000792005062700079NM 2005 6 27 UPS05444603 120050516A5347 SEAT TRACK BOEING747 747123F NM MAIN DECK CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 BS 1140 - 1265 RBL 11 SEAT TRACK FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.052 BY 1.5 BY 1.5 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, M/D -BS 1130-1265 RBL 11 SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 34. 2L74 4F A20WE 20050627000952005062700095EA 2005 6 27 MASA200500418 120050530A3350 LENS CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHTSMISSING A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07506MJ 10073 EMERGENCY EXIT SIGN LENS COVER MISSING AT ROW 12. MAINTENANCE FOUND LENS AND REINSTALLED IT. 2L72 4F RTA21EA 20050627001002005062700100NM 2005 6 27 05FDEA01622 120050621A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25619FE 48770 MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT LBL 27, STATION 635 FOUND CRACKED APPROXIMATELY 2 INCHES LONG. CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I FIGURE I. 2L73 4F RTA22WE 20050627001282005062700128NM 2005 6 27 05FDEA01628 120050621A5315BAC1518338 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25264FE 21626 CORROSION ON FLOORBEAM LBL 25 - RBL 25 BS 620. CORROSION FOUND TO BE OUT OF LIMITS REPAIRED FLOORBEAM IAW SRM 53-10-8 FIG 3 2L73 4F RTA3WE 20050627001372005062700137 2005 6 27 QXEA200501074 420050621A23506229852108 RADIO CNDAIRCL600 CL6002C10 1390015EA ZONE 200 MALFUNCTIONED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09608QX5043 5043 519K DEN - ON FLT 4333, RETURNED TO FIELD, RADIO TUNING UNIT 1 STUCK ON TX AND THEN CLEARED, THEN UNABLE TO TX. REMOVED AND REPLACED NR 1 RADIO TUNING UNIT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20050627001652005062700165NM 2005 6 27 2005UALA00553 120050609A5311 FRAME BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29315UA 23947 RIGHT OVERWING FRAME INNER CHORD CRACKED THROUGH LOWER FASTENER HOLE AT BS 616 MID CABIN AREA. *S/D* REMOVED CRACK, FABRICATED STIFFENER ANGLE & FILLER AND INSTALLED REPAIR PER AMM 53-11-89. 2L72 4F4 FRTA16WE E21EU 20050627001692005062700169NM 2005 6 27 2005UALA00555 120050612A5410 STRUCTURE BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU NR 2 INLET COWL DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29910UA 25254 NR 2 ENGINE INLET COWL DENTED AT APPROXIMATELY 4 O`CLOCK. DENT IS OUT OF LIMITS. INSTALLED REPAIR PER SRM 54-10-01 FIG 203 DET II. 2L72 4F4 FRTA16WE E21EU 20050627001722005062700172NM 2005 6 27 2005UALA00558 120050506A5321 PRESSURE PANEL BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU CABIN FLOOR WORN A UALAK NONE O OTHER ININSP/MAINT 1 WP29313UA 23674 LOWER SURFACE OF THE MID CABIN FLOOR PRESSURE WEB AT BS 670 RBL 20 WAS FOUND WORN. REPAIR DOUBLER FABRICATED, FORMED TO FIT AROUND EXISTING BEAD-UP AREA AND INSTALLED. 2L72 4F4 FRTA16WE E21EU 20050627001752005062700175NM 2005 6 27 2005UALA00561 120050613A3397MB12P1 CONNECTOR BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU ROW 15 INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29904UA 25004 EEL LIGHTS OUT FROM ROW 15 BACK. *S/D* EEL LIGHT CONNECTORS WERE REMOVED, CLEANED AND REINSTALLED. 2L72 4F4 FRTA16WE E21EU 20050627001772005062700177NM 2005 6 27 2005UALA00563 120050613A5241 DOOR FRAME BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU FWD GALLEY DOOR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29315UA 23947 FWD GALLEY DOOR AFT LWR FRAME CRACKED AT FASTENER HOLE. REPAIR ACP'D AT HMV4 AAR - REPLACED AFT FRAME PER SRM 51-40-02 & 51-10-02, GNMM 5-0-4-11 & 5-0-7-1. 2L72 4F4 FRTA16WE E21EU 20050627001792005062700179 2005 6 27 2005UALA00565 420050613A256563667 HOSE AIRCRUISERS AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE SLIDE BROKEN A UALAK NONE O OTHER ININSP/MAINT 1 WP29441UA A6400 751 THE HOSE WAS FOUND BROKEN BY ASPIRATOR DURING THE UNPACKING PROCESS. DURING UNPACKING OF THE SLIDE IN THE SHOP, THE HOSE WAS FOUND BROKEN FROM PLATE. THE PROBABLE CAUSE IS KINKED ROUTING OF THE HOSE DURING THE PREVIOUS PACKING OF THE ASSEMBLY. THE CONTINUES STRESS ON THE HOSE RESULTED IN ITS BREAKAGE. HOSE WAS REPLACED. 2L72 4F4 FRTA28NM E40NE 20050627001822005062700182 2005 6 27 2005UALA00568 420050615A2565 STRAP AIRCRUISERS BOEING777 777222 1385219NM PWA PW4077PW4077 NE SLIDE MISROUTED A UALAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP29213UA 0275 30219 THE MIDDLE STRAP UNDER THE SLIDE WAS WRAPPED AROUND THE OUTER TUBES WHICH WOULD HAVE CAUSED THE SLIDE TO NOT DEPLOY AND FUNCTION LIKE IT SHOULD. DURING SLIDE/RAFT DISASSEMBLY, CENTER TENSION WEB WAS FOUND MISROUTED AROUND INFLATION TUBES. IT IS SUSPECTED MISROUTE OCCURRED DURING PACKING PROCESS AT LAST COMPONENT SHOP VISIT. OEM PACKING PROCEDURE P-12061 REVISION /F/ TEXT AND ILLUSTRATIONS PROVIDE CLEAR ROUTING INSTRUCTIONS. COMPONENT SHOP THAT PERFORMED THIS DISCREPANT PACKING NO LONGER EXISTS. SLIDE IS NOW MAINTAINED BY AN OSV SHOP. PACKING DISCREPANCY IS CONSIDERED AN ISOLATED INCIDENT. 2L72 4F4 FRTT0001SE E46NE 20050627001852005062700185NM 2005 6 27 2005UALA00571 120050616A5297 CONNECTOR AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE PROXIMITY SENSORLOOSE A UALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP29805UA 783 AFT CARGO DOOR OPEN DISPLAYED ON UPPER ECAM SCREEN. CONNECTOR TO 32WV PROXIMITY SENSOR CAME LOOSE. COA 404692 WAS PERFORMED INCORRECTLY. FIRST INCIDENT SINCE INCORPORATION IN MAY 2004. EG4352. 2L72 4F4 FRTA28NM E40NE 20050628000072005062800007EU 2005 6 28 COE2005F00001 120050606A33509750W03505 BATTERY AEROSPATR42 ATR42300 8680920EU PWA 120 PW120 NE HAMSTD14SF 14SF5 NE EMERGENCY LIGHT MALFUNCTIONED A COEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM13917FX 354 121012 921114 EMERGENCY BATTERY CHARGE FAULT LIGHT CAME ON DURING CLIMB OUT. AC RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY. MAINTENANCE CONTROL STATES BATTERY WAS NOT HOT WHEN REMOVED. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2H72 4T4 TRTA53EU E20NE 6 CP7NE 20050628000142005062800014NM 2005 6 28 UPS05444681 120050608A3350 BATTERY PACK BOEING747 747212B 1384886NM EMERGENCY LIGHTSINOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 EMERGENCY BATTERY PACK INOP FOR AFT 2 CEILING LIGHTS IN UPPER DECK. REPLACED EMERGENCY BATTERY PACK M335. OPS CHECK GOOD PER 33-51-00 PG 501. 2L74 4F A20WE 20050628000162005062800016WP 2005 6 28 UPS05844682 120050609A5330 DOUBLER DOUG DC8 DC871F 302199DWP FUSELAGE DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 UNDER BELLY PANELS (4EA) DELAMINATED ON PREVIOUS REPAIR. LT WING TO BODY LOWER FILLET PANEL DELAMINATED. D303878 LT WING TO BODY FAIRING FILLET PANEL DELAMINATED D303879 LT WING TO BODY FAIRING FILLET PANEL DELAMINATED. 2L74 4F RT4A25 20050628000212005062800021WP 2005 6 28 0500839875 120050416A5312 STIFFENER DOUG DC9 DC951 3022051WP FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01784NC 48109 DURING H-CHECK, FOUND CRACKED BULKHEAD STIFFENER AT BS 1168 RBL 60. REPAIRED PER EA 98-203198. 2L72 4F RTA6WE 20050628000252005062800025WP 2005 6 28 ABXA050150 120050531A5210591412157 PAN DOUG DC9 DC931 3022065WP PAX DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23947AX 47004 PASSENGER ENTRY DOOR PAN CRACKED IN 3 LOCATIONS ON FORWARD SIDE. REMOVED AND REPLACED MAIN ENTRY DOOR IAW DC-9 MM 52-11-00-5-001. WORK ACCOMPLISHED ON NON ROUTINE 0311. (2 EACH - 5 INCH CRACKS, 1 EACH - 2 INCH CRACKS). 2L72 4F A6WE 20050628000502005062800050WP 2005 6 28 ABXA050147 120050527A532059560805 FLOOR SUPPORT DOUG DC9 DC931 3022065WP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23947AX 47004 STA 218 FLOOR SUPPORT HAD INTERGRANULAR CORROSION ON LOWER SIDE. REMOVED AND REPLACED FLOOR SUPPORT IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20050628000552005062800055EA 2005 6 28 VTZA200500101 120050603A5320601R311719 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27627BR 7233 INTERCOSTAL CRACKED AT .250 IN LENGTH ON RT OUTBOARD SIDE AT FS 484 RIGHT BETWEEN BL 36.00. 2L72 4F RTA21EA 20050628000572005062800057EA 2005 6 28 VTZA200500103 120050603A5320601R35031239 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27627BR 7233 RT FS 621 FLOOR SUPPORT IS CRACKED 1 IN. 2L72 4F RTA21EA 20050628000582005062800058EA 2005 6 28 VTZA200500104 120050603A5310601R5211680 DOOR FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27627BR 7233 PAX DOOR FRAME TOP RADIUS CRACKED 1 INCH IN LENGTH FORWARD OF DATUM 1 AT FS 338.9. 2L72 4F RTA21EA 20050628000602005062800060EA 2005 6 28 COMA0570061 120050605A5610NP1393229 WINDOW CNDAIRCL600 CL6002C10 1390015EA COCKPIT FAILED A COMAO OTHER O OTHER CRCRUISE 1 SO01369CA3995 10079 PILOT SIDE WINDOW SHATTERED. REPLACED WINDOW. 2L72 4F RTA21EA 20050628000732005062800073SO 2005 6 28 RAIA00506003 120050602A2197 CONNECTOR EMB 145 EMB145LR 3260212SO PRESS CONTROLLERUNSECURE A RAIAA UNSCHED LANDING O OTHER CLCLIMB 1 CE03811HK 145256 AFTER DEPARTURE, ACFT FAILED TO PRESSURIZE. MX RESECURED CONNECTOR ON DIGITAL PRESSURIZATION CONTROLLER. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050628000832005062800083NM 2005 6 28 05FDEA01357 120050517A5511ALC8131502 SPAR CAP DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25580FE 48471 NR 36R BORE FOUND EXCEEDED LIMIT AFTER CORROSION REMOVAL. EMPENNAGE NR 36R BORE REWORKED AS PER FEDEX EA NR 1-5510-83129. HORIZONTAL STABILIZER, BARREL NUT BORE 36R. REWORKED BEYOND S/B MD11-55-023 REV 2 LIMITS. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050628000902005062800090 2005 6 28 SA05075 420050618A2565D31517113 SLIDE AIRBUSA319 A319112 3930323EU PAX CABIN READS LOW A USAAK NONE O OTHER ININSP/MAINT 1 EA19764US9773 5701 1369 THE AFT LT SLIDE INDICATED LOW PRESSURE DURING INSPECTION. MAINTENANCE REPLACED THE AFT LT SLIDE. OK FOR SERVICE. 2L72 4F RTA28NM 20050628000942005062800094EA 2005 6 28 ASOA05475 120050524A3350BC50393106 COVER BRUCE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE EXIT LIGHT CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27701EV 10020 DURING A C-CHECK, THE EMERGENCY EXIT LIGHT COVER JUST FORWARD OF THE RT EMERGENCY EXIT WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT COVER JUST FORWARD OF THE RT EMERGENCY EXIT. OPERATIONAL CHECKS GOOD. (K) 2L72 4F4 FRTA21EA EOOO63EN 20050628001052005062800105EU 2005 6 28 ASOA05455 120050522A1430 FASTENER AEROSPATR72 ATR72 EU PWA PW120 PW127 NE PASSENGER DOOR MISSING A ASOAK NONE O OTHER ININSP/MAINT 1 SO27643AS 1378 413 DURING A GROUND INSPECTION, THE PASSENGER DOOR WAS FOUND DIFFICULT TO OPEN. MAINTENANCE REINSTALLED 2 FASTENERS (SCREWS) FOUND MISSING FROM THE PASSENGER DOOR COVER IN THE UPPER AFT CORNER. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K) 2H72 4T4 TRT E20NE 20050628001062005062800106EA 2005 6 28 ASOA05461 120050525A5210601R31980 STEP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27889AS 7538 DURING A GROUND INSPECTION, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050628001072005062800107EA 2005 6 28 ASOA05463 120050525A1100S72451 PLACARD CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE PAX DOOR DAMAGED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27752EV 10166 DURING A GROUND INSPECTION, THE EXIT PLACARD ON THE EXIT PLACARD ON THE PASSENGER DOOR WAS FOUND DAMAGED. MAINTENANCE REMOVED AND REPLACED THE EXIT PLACARD ON THE PASSENGER DOOR. AIRCARFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA EOOO63EN 20050628001092005062800109EA 2005 6 28 ASOA05469 120050528A5210601R319805 STEP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27824AS 7203 DURNG A GROUND INSPECTION, THE PASSENGER DOOR BOTTOM STEP RETRACTING HINGE LINKAGE WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050628001122005062800112EA 2005 6 28 ASOA05476 120050526A5220H341937 HANDLE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE ESCAPE HATCH CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27701EV 10026 10020 DURING A C-CHECK, THE CREW ESCAPE HATCH OUTER HANDLE WAS FOUND TO BE CORRODED ON THE INSIDE BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CREW ESCAPE HATCH OUTER HANDLE IAW AMM. OPERATIONAL CHECKS GOOD. (K) 2L72 4F4 FRTA21EA EOOO63EN 20050628001222005062800122WP 2005 6 28 ASAA0580161 120050301A57309919459509 SKIN PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE LT WING ELONGATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 HV- CHECK - LT WING ACCESS PANEL 1392C HAD ELONGATED FASTENER HOLES. REPLACED PANEL. (K) 2L72 4F4 FRTA6WE E9NE 20050628001342005062800134WP 2005 6 28 ASAA0580158 120050301A575359100414 VANE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE TE FLAP CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 HV-CHECK - LT OB FLAP NR 1 VANE IB END L/E SKIN IS CHAFED. INSTALLED REPAIR DOUBLER. (K) 2L72 4F4 FRTA6WE E9NE 20050628001402005062800140EA 2005 6 28 ASOA05495 120050603A5312 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27850AS 7355 DURING C-CHECK, THE PILOTS BULKHEAD WEB FS 280 BETWEEN LBL 9 AND RBL 9 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE PILOTS BULKHEAD WEB FS 280 BETWEEN LBL 9 AND RBL 9 IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050628001442005062800144EA 2005 6 28 ASOA05478 120050601A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE ENGINE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27850AS 7355 DURING A C-CHECK, THE ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL0 IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050628001452005062800145CE 2005 6 28 GUU2005F00020 120050530A3240 BRAKE BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA MLG FAILED A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO2982539 UE168 CAPTAIN`S SIDE LT BRAKE PEDAL WOULD NOT BRAKE. SERVICED BRAKE SYSTEM. NO LEAK NOTED. (K) 2L72 4T3 TRTA24CE E2NE 20050628001472005062800147EA 2005 6 28 A6WA200540194 120050610A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE DENTED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31459AW 7863 REPAIR DENT IN FUSELAGE SKIN AT FS 409 TO FS 409+16 BETWEEN STR 13L AND STR 15L. PERFORMED EXTERNAL FLUSH PERMANENT REPAIR IN FUSELAGE SKIN AT FS 409 TO FS 409+16 BETWEEN STR 13L AND STR 15L IAW SRM. (K) 2L72 4F4 FRTA21EA E15NE 20050628001482005062800148EA 2005 6 28 A6WA200540193 120050609A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE GOUGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31418AW 7618 THE RT SIDE FUSELAGE SKIN AT FS 225.20 ON THE SURROUND STRUCTURE FOR THE ACCESS PANEL WAS GOUGED APPROXIMATELY .5 INCH W X .4 INCH L X .012 DEEP. BLENDED DAMAGED AREA, PERFORMED EDDY CURRENT INSPECTION, ADDED PROTECTIVE TREATMENT AND EXTERIOR FINISH IAW SRM. (K) 2L72 4F4 FRTA21EA E15NE 20050628001492005062800149WP 2005 6 28 ASAA0580154 120050228A5320991555416 INTERCOSTAL DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02975AS 53451 C-CHECK - INTERCOSTAL CORRODED ON TOP AND BOTTOM FLANGES. REPLACED INTERCOSTAL. (K) 2L72 4F4 FRTA6WE E9NE 20050628001522005062800152WP 2005 6 28 ASAA0580169 120050309A5321993655811 FLOORBOARD DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 HV-CHECK - PAX CABIN FLOOR PANEL IS WATER DAMAGED AND HAS CORRODED FASTENERS. REPLACED FLOOR PANEL. (K) 2L72 4F4 FRTA6WE E9NE 20050628001542005062800154WP 2005 6 28 ASAA0580162 120050301A53305920323547 SKIN DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 HV - CHECK - RT SIDE OF THE FUSELAGE IS DENTED. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLERS, DOUBLERS, AND FINGER DOUBLERS. (K) 2L72 4F4 FRTA6WE E9NE 20050628001562005062800156WP 2005 6 28 ASAA0580170 120050307A5523591041449 GEAR DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE ELEV TAB DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 HV - CHECK - LT ELEVATOR GEAR TAB IS DENTED. INSTALLED REPAIR DOUBLER. (K) 2L72 4F4 FRTA6WE E9NE 20050628001612005062800161WP 2005 6 28 ASAA0580155 120050228A575359304963 VANE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE TE FLAP CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02975AS 53451 C-CHECK, RT WING OB FLAP VANE CHAFED BEHIND IB HINGE FAIRING. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER AND FILLER. (K) 2L72 4F4 FRTA6WE E9NE 20050628001622005062800162WP 2005 6 28 ASAA0580151 120050228A5320 INTERCOSTAL DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02975AS 53451 C-CHECK, INTERCOSTAL CORRODED. REPLACED INTERCOSTAL. (K) 2L72 4F4 FRTA6WE E9NE 20050628001662005062800166 2005 6 28 CLC2005F00000 420050527A25655WD230100101 SLIDE DOUG DC10 DC1030 3023501WP GE CF6 CF650* 30018NE R1 DOOR DEPLOYED A CLCAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO29279AX 47816 DURING LINE MAINTENANCE THE R1 DOOR ESCAPE SLIDE WAS ACCIDENTALLY DEPLOYED BY MAINTENANCE. REPLACED ESCAPE SLIDE. AIRCRAFT WAS RETURNED TO REVENUE SERVICE. (K) 2L73 4F4 F A22WE E23EA 20050628001682005062800168WP 2005 6 28 ASAA0580164 120050307A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE PAX CABIN DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 HV - CHECK - PAX CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (K) 2L72 4F4 FRTA6WE E9NE 20050628001692005062800169SO 2005 6 28 GUU2005F00024 120050601A3350D3660401 BATTERY PACK EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE EMERGENCY LIGHT INOPERATIVE A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO29261AS 120141 AT SCHEDULED ROUTINE MAINTENANCE, LT AND RT AFT EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED NR 3 EMERGENCY BATTERY PACK. OPS CHECK NORMAL. (K) 2L72 4T4 TRTA31SO E20NE 20050628001732005062800173WP 2005 6 28 ASAA0580152 120050228A5320993053653 CUSP WEB DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE CANNING A ASAAK NONE O OTHER ININSP/MAINT 1 NM02975AS 53451 C-CHECK - CUSP WEB IS (OIL CANNING). REMOVED DAMAGED SECTION AND INSTALLED REPAIR DOUBLER. (K) 2L72 4F4 FRTA6WE E9NE 20050628001752005062800175EA 2005 6 28 ASOA05473 120050511A5712 RIB CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT WING CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27829AS 7232 DURING A C-CHECK, THE RT MAIN LANDING GEAR WHEEL WELL BATT RIB ASSEMBLY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RT MAIN LANDING GEAR WHEEL WELL BATT RIB ASSEMBLY AT WS 53.60 IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050628001772005062800177EA 2005 6 28 A6WA200540182 120050525A29106017523843 TUBE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE HYD SYSTEM LEAKING A A6WAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL31427ZW 7685 HYDRAULIC NR2 SYSTEM PRESSURE LOSS FOLLOWED BY LOSS OF QTY. NR2 SYSTEM, COMPLIED WITH QRH. INSPECTED AND FOUND HYD PRESSURE LINE NR2 IN APU BAY LEAKING, ALSO ENG DRIVEN HYD PUMP NR 2 FAILED. REMOVED/REPLACED ENGINE DRIVE HYD PUMP NR 2. REMOVED AND REPLACED ENG DRIVE PUMP CASE DRAIN FILTER. (REMOVED AND REPACED TUBE ASSY AND FAIRLEADS). (K) 2L72 4F4 FRTA21EA E15NE 20050628001782005062800178EA 2005 6 28 ASOA05343 120050412A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27820AS 7188 DURING C-CHECK, THE TRANSVERSE BEAM AT FS 280 BETWEEN LBL9 AND LBL 27 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE TRANVERSE BEAM AT FS 280 BETWEEN LBL 9 AND LBL 27 IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050628001792005062800179EA 2005 6 28 ASOA05493 120050605A5312 PRESSURE PANEL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27850AS 7355 DURING A C-CHECK, THE PRESSURE FLOOR AT FS 424-449.85 LT WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE PRESSURE FLOOR AT FS 424-449.85 LT IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050628001822005062800182EA 2005 6 28 ASOA05489 120050605A5270 FITTING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR BINDING A ASOAK NONE O OTHER ININSP/MAINT 1 SO27829AS 7232 DURING A GROUND INSPECTION, UPON CLOSING THE PASSENGER DOOR AN OVERBOARD COOL MESSAGE WAS RECEIVED AND THE FLIGHT ATTENDANT REPORTED THE PASSENGER DOOR DIFFICULT TO OPEN. THE AIRCRAFT WAS INSPECTED AND FOUND SAFE FOR A FERRY FLIGHT FOR THE PURPOSE OF MAINTENANCE REPAIR TO THE PASSENGER DOOR. THE AIRCRAFT WAS FERRIED AND LANDED SAFELY. MAINTENANCE ADJUSTED THE DOOR FRAME SPIGOT FITTING IAW MM. OPS CHECK GOOD, AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050628001832005062800183EA 2005 6 28 ASOA05458 120050523A5310601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27902EV 7614 7620 DURING HANGAR MAINTENANCE, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR IAW AMM. (K) 2L72 4F4 FRTA21EA E15NE 20050629000012005062900001EA 2005 6 29 ASOA05350 120050417A326016600103 UPLOCK CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NLG INOPERATIVE A ASOAO OTHER J WARNING INDICATION APAPPROACH 1 SO27884AS 7513 DURING FINAL APPROACH, UPON SELECTING GEAR DOWN, A GEAR DISAGREE MASTER WARNING WAS RECEIVED. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR (NLG) UPLOCK ASSY. OPERATIONAL CHECKS GOOD. AC OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050629000052005062900005EA 2005 6 29 ASOA05354 120050407A5312CC67034170 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27703EV 10038 DURING HANGAR MAINTENANCE, THE FS 280 LT AND RT LOWER BULKHEAD WEB WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE FS 280 LT AND RT LOWER BULKHEAD WEB IAW EO. (K) 2L72 4F4 FRTA21EA EOOO63EN 20050629000102005062900010 2005 6 29 AMTA200500492 420050531A2565 LIGHT BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE ESCAPE SLIDE INOPERATIVE A AMTAO OTHER O OTHER TXTAXI/GRND HDL 1 GL11555TZ 32589 ESCAPE SLIDE ENGAGEMENT LIGHT INOPERATIVE AT R2. REMOVED AND REPLACED R2 DOOR RT GRIT BAR PROXIMITY SWITCH IAW MM. OPS CK NORMAL. (K) 2L72 4F4 FRTA2NM E12EU 20050629000112005062900011EA 2005 6 29 A6WA200540185 120050525A5753 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT IB FLAP DENTED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31456ZW 7849 RT IB FLAP LOWER SKIN 4.5 INCH FROM T/E ND 17. INCH FROM IB EDGE. DENT IS 2 INCHES X 2 INCHES X 0.45 INCHES. PERFORMED MAJOR REPAIR BY INSTALLING NON-FLUSH REPAIR IAW SRM. (K) 2L72 4F4 FRTA21EA E15NE 20050629000132005062900013EA 2005 6 29 ASOA05361 120050419A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE MAIN PAX MALFUNCTIONED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27846AS 7328 DURING A GROUND INSPECTION, THE PASSENGER DOOR COULD NOT BE OPENED FROM THE INSIDE. MAINTENANCE INSPECTED THE PASSENGER DOOR AND NO DEFECTS WERE NOTED. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050629000142005062900014EA 2005 6 29 ASOA05347 120050414A3350 COVER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY EXIT CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27821AS 7194 DURING C-CHECK, THE EMERGENCY EXIT LIGHT COVER ABOVE THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT COVER ABOVE THE SERVICE DOOR. (K) 2L72 4F4 FRTA21EA E15NE 20050629000152005062900015EA 2005 6 29 A6WA200540183 120050509A53303775 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE DENTED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31454AW 7842 2 DENTS RT SIDE AF FS409 + 32 BETWEEN STR 21R AND 22R. 3.5 INCHES LONG X 1.65 INCHES WIDE X 0.39 INCHES DEEP. 2.5 INCHES LONG X 1.5 INCHES WIDE X .022 INCHES DEEP. REPAIRED DAMAGE AT FS 409 +32 BETWEEN STR 21R AND 22R IAW SRM. (K) 2L72 4F4 FRTA21EA E15NE 20050629000172005062900017EA 2005 6 29 ASOA05369 120050418A52106003145021 PIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR BINDING A ASOAK NONE O OTHER ININSP/MAINT 1 SO27846AS 7330 7328 DURING A GROUND INSPECTION, THE PASSENGER DOOR COULD NOT BE OPENED FROM THE INSIDE OR OUTSIDE. MAINTENANCE INSPECTED THE PASSENGER DOOR LINKAGES AND LUBRICATED THE (LATCH) PINS. MAINTENANCE ALSO PRESSURIZED THE AIRCRAFT AND CYCLED THE DOOR SEVERAL TIMES. OPERATIONAL CHECKS GOOD. AC OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050629000212005062900021EA 2005 6 29 ASOA05351 120050417A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE ENGINE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27821AS 7194 DURING A C-CHECK, THE ENGINE SUPPORT BEAM AT BOTH RIVET HOLES UNDER THE FIRE LOOP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL0 IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050629000262005062900026CE 2005 6 29 181EF061205JC 120050612A7830451255445601 LATCH LEAR 35 35A 5170602CE GARRTTTFE731TFE731* 01518WP THRUST REVERSER MISSING A AOQAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 EA11181EF 190 AFTER TAKEOFF, CREW FELT A VIBRATION. CREW RETURNED FOR INSPECTION AND EVALUATION. AC LANDED UNEVENTFULLY. AIRCRAFT WAS INSPECTED. FOUND T/R LOCK ACCESS PANEL MISSING FROM LT IB ENGINE. AC WAS INSPECTED FOR DAMAGE OR DEFECT- NONE NOTED. NEW PANEL INSTALLED. AC WAS RETURNED TO SERVICE. (K) 2L72 4F4 F A10CE E6WE 20050629000302005062900030SO 2005 6 29 GUU2005F00026 120050607A2120 SMOKE EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE COCKPIT DETECTED A GUUAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO29266AS 120188 AFTER TAKEOFF, DETECTED CONDENSATION AND POSSIBLE SMOKE IN THE COCKPIT AND CABIN WITH PASSENGER SMOKE ALARM GOING OFF. RETURNED TO DEPARTURE, LANDED WITHIN INCIDENT. INSPECTED AIRCRAFT AIR CONDITIONING PACKS AND ENGINE FOR LEAKS. NO LEAKS DETECTED. GROUND RUN OPERATIONAL CHECK NORMAL. (K) 2L72 4T4 TRTA31SO E20NE 20050629000312005062900031EA 2005 6 29 ASOA05481 120050601A3350 HOUSING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27850AS 7355 DURING A C-CHECK, THE EMERGENCY EXIT LIGHT HOUSING BY THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY BY THE SERVICE DOOR. OPERATIONAL CHECKS GOOD. (K) 2L72 4F4 FRTA21EA E15NE 20050629000322005062900032EA 2005 6 29 ASOA05483 120050601A5210600319469 PUSH-PULL ROD CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR BINDING A ASOAK NONE J WARNING INDICATION ININSP/MAINT 1 SO27820AS 7188 7188 DURING A GROUND INSPECTION, THE PASSENGER DOOR WAS FOUND HARD TO CLOSE WHICH WAS ACCOMPANIED BY AN OUTER HANDLE CAUTION MESSAGE. THE AC WAS INSPECTED AND FOUND SAFE FOR A FERRY FLIGHT FOR MAINTENANCE REPAIRS TO THE PASSENGER DOOR. THE AC WAS FERRIED AND LANDED SAFELY. MAINTENANCE ADJUSTED THE PASSENGER DOOR PUSH-PULL ROD ASSEMBLY IAW MM. OPERATIONAL AND PRESSURIZATION LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050629000332005062900033EA 2005 6 29 ASOA05464 120050525A2612 FIRE WARNING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE APU BAY FALSE ACTIVATIONA ASOAF ACTIVATE FIRE EXT. N FALSE WARNING DEDESCENT 1 SO27833AS 7246 DURING DESCENT, THE CREW RECEIVED AN APU FIRE WARNING. THE QRH WAS COMPLIED WITH AND THE MESSAGE EXTINGUISHED PRIOR TO DISCHARGING THE APU FIRE BOTTLE. THE TOWER DECLARED AN EMERGENCY AND THE AIRCARFT LANDED SAFELY. EMERGENCY VEHICLES MET AND FOLLOWED THE AIRCRAFT TO THE GATE AS A PRECAUTION. MAINTENANCE INSPECTED THE AFT EQUIPMENT BAY, AUXILIARY POWER UNIT (APU) ENCLOSURE AND PERFORMED A SYSTEM TEST. NO DEFECTS WERE NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050629000352005062900035EA 2005 6 29 ASOA05389 120050427A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE ENGINE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27907EV 7648 DURING A C-CHECK, THE ENGINE SUPPORT BEAM LOWER BEW AT BL 36.20 LT AND RT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE ENGINE SUPPORT BEAM LOWER WEB AT BL 36.20 LT AND RT IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050629000382005062900038EA 2005 6 29 ASOA05497 120050607A3350BF50390901 COVER BRUCE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27830AS 7236 DURING A C-CHECK, THE EMERGENCY EXIT LIGHT LENS COVER ABOVE THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE LENS COVER ON THE EMERGENCY EXIT LIGHT ABOVE THE SERVICE DOOR. (K) 2L72 4F4 FRTA21EA E15NE 20050629000392005062900039NM 2005 6 29 UIEA200500078 120050520A291087014 SERVO VALVE BOEING747 7472F6B 1384807NM GE CF6 CF650E2 30018NE NR 2 HYD SYSTEM LEAKING A UIEAH DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA15534MC 21832 DURING CRUISE, NR 2 HYD QUANTITY WENT FROM 6.1 TO 2.2, 5 HOURS INTO FLIGHT. SUSPECT HYD LEAK. RAN PROCEDURES TO SHUTDOWN HYD SYSTEM NR 2 IAW FLIGHT HAND BOOK. REPLACED LOWER RUDDER POWER PACKAGE SERVO VALVE IAW MM. PRESSURIZED HYD SYSTEM IAW MM. LEAD CHECK OK, SN OFF 1895 (K) 2L74 4F4 F A20WE E23EA 20050629000412005062900041EA 2005 6 29 ASOA05358 120050418A3220521173 TORQUE LINK CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE NLG DAMAGED A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27752EV 10166 DURING TAKEOFF, WHEN THE CREW ATTEMPTED TO MOVE THE GEAR HANDLE, IT WOULD NOT MOVE FROM THE DOWN LOCKED POSITION. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE LOWER TORQUE LINK ON THE NOSE LANDING GEAR (NLG). OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA EOOO63EN 20050629000432005062900043NE 2005 6 29 AMTA200500514 220050612A7230 COMPRESSOR LKHEED1011 10113853 5265020WP RROYCERB211 RB211524B4 54555NE NR 3 ENGINE STALLED E AMTAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 GL11162AT 1220 14855 NR 3 ENGINE COMPRESSOR STALLED ON CLIMB AT FL 27.0 TGT SPIKED AT 860 DEGREES FOR LESS THAN 2 SECONDS. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN WINDMILLED FOR 40 MINUTES WITH POSITIVE OIL PRESSURE INDICATION. PERFORMED CLAPPER LUBE, REPLACED SPINNER, BORESCOPED ENGINE AND INSPECTED INLET AND EXHAUST. PERFORMED ENGINE TAKEOFF POWER TEST NR 13 REF MM. NO DEFECTS NOTED. (K) 2L73 4F4 F A23WE E12EU 20050629000452005062900045EA 2005 6 29 ASOA05484 120050602A5320601R3117117 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27850AS 7355 DURING A C-CHECK, THE CLIP AT FS 484, LBL 27 FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIP AT FS 484, LBL 27 FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIP AT FS 484, LBL 27 IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050629000472005062900047EU 2005 6 29 ASOA05498 120050607A33503011162 COVER AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE EMERGENCY LGIHT DAMAGED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27632AS 3011160 338 DURING A GROUND INSPECTION, THE EMERGENCY EXIT LIGHT COVER AT ROW 1 ON THE LT SIDE FLOOR LEVEL WAS FOUND TO BE UNREADABLE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT COVER AT ROW 1 ON THE LT SIDE FLOOR LEVEL. OPS CHECK GOOD. AC OK FOR SERVICE. (K) 2H72 4T4 TRTA53EU E20NE 20050629000492005062900049EA 2005 6 29 ASOA05479 120050601A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27850AS 7355 DURING A C-CHECK, THE CLIP AT FS 625 LT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CLIP AT FS 625 LT. (K) 2L72 4F4 FRTA21EA E15NE 20050629000502005062900050SO 2005 6 29 GUU2005F00018 120050511A3397 CONNECTOR EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE EMERGENCY LIGHT LOOSE A GUUAK NONE L NO TEST ININSP/MAINT 1 SO29268AS 120202 AT SCHEDULED ROUTINE MAINTENANCE, FOUND EMERGENCY PATH LIGHTING INOPERATIVE BETWEEN SEATS 3A AND 5A. RESECURED LOOSE CONNECTOR AT ONE LIGHT. OPERATIONAL CHECK NORMAL. (K) 2L72 4T4 TRTA31SO E20NE 20050629000522005062900052CE 2005 6 29 U8DA011105 120050611A3230AN62776 SHUTTLE VALVE CESSNA414 414A 2075907CE CONT O520 TSIO520* 17040SO MLG BOTTLE STUCK E U8DAA UNSCHED LANDING J WARNING INDICATION DEDESCENT 1 NM11415ST 414A0467 NOSE LANDING GEAR DID NOT SHOW DOWN AND LOCKED. GEAR LAMP WOULD INTERMITTENTLY LIGHT AND HYDRAULIC PRESSURE LIT WOULD INTERMITTNETLY ILLUMINATE. DISASSEMBLY AND T/S SHOWED SHUTTLE VALVE STUCK. CLEANED, REASSEMBLED AND TESTED. N2 BOTTLE REMOVE, CLEANED, INSPECTED AND REFILLED, LEAK CHECKED, REINSTALLED. MONITOR FOR PRESSURE DROP, NONE NOTED. ACTIVATED EMERGENCY NITROGEN BLOW-DOWN BOTTLE. GEAR DOWN AND LOCKED WITH BOTTLE PRESSURE. SUSPECT POSSIBLE N2 BOTTLE LEAK, DIRTY SHULLTE VALVE, HOWER, PREFLIGHT INSPECTION OF PRESSURE BOTTLE WAS WITHIN LIMITS. (K) 1L72 3O3 O A7CE E8CE 20050629000572005062900057NE 2005 6 29 HALA0500597 220050528A7320114E6112G120 EEC BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE RT ENGINE MALFUNCTIONED A HALAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP13476HA5411 55118 13301 RT ENGINE AUTO SHUTDOWN DURING THE START SEQUENCE, AFTER IGNITION AND STARTER CUTOUT. NO EXCEEDENCES NOTED. REMOVED AND REPLACED NR 2 ENGINE EEC IAW AMM. RTS TEST PASSED. GROUND RUN OPS CHECK GOOD. (K) 2L72 4F4 FTRA6WE E00061EN 20050629000592005062900059EA 2005 6 29 ASOA05357 120050416A5320 SILL CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27703EV 10038 DURING HANGAR MAINTENANCE, THE FS 280 FLOOR SILL AT RBL 42 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE THE FS 280 FLOOR SILL AT RBL 42 IAW EO. (K) 2L72 4F4 FRTA21EA EOOO63EN 20050629000612005062900061EA 2005 6 29 ASOA05362 120050420A5312 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE BULKHEAD CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27821AS 7194 DURING A C-CHECK, THE JAY ANGLE ON THE PILOTS BULKHEAD AT FS 280, LBL 9 AND RBL 9 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE JAY ANGLE ON THE PILOTS BULKHEAD AT FS 280, LBL 9, AND RBL 9 IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050629000632005062900063EA 2005 6 29 ASOA05492 120050605A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27850AS 7355 DURING A C-CHECK, THE MAINFRAME AT FS 473.15 AT THE FLOOR LEVEL UNDER THE LT AND RT OVERWING EXITS WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE MAINFRAME AT FS 473.15 AT THE FLOOR LEVEL UNDER THE LT AND RT OVERWING EXITS IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050629000642005062900064EA 2005 6 29 ASOA05487S 120050604A2612 FIRE WARNING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE APU BAY FALSE ACTIVATIONA ASOAF ACTIVATE FIRE EXT. N FALSE WARNING DEDESCENT 1 SO27833AS1023778 7246 DURING DESCENT, THE CREW RECEIVED AN AUXILIARY POWER UNIT (APU) OVERTEMP MESSAGE. DURING COMPLIANCE WITH THE QRH, AND APU FIRE WARNING WAS RECEIVED AT WHICH TIME THE CREW DISCHARGED THE APU FIRE BOTTLE FOLLOWED BY ALL INDICATIONS GOING AWAY. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY. UPON LANDING THE AIRCRAFT WAS INSPECTED BY THE FIRE CREW WITH NO EVIDENCE OF A FIRE FOUND. THEN PROCEEDED TO THE GATE SAFELY. UPON INSPECTION OF AC BY MAINTENANCE, NO EVIDENCE OF A FIRE, FUEL OR OIL LEAKS WERE FOUND. MAINTENANCE REMOVED AND REPLACED THE APU FIRE AND OVERHEAT CONTROL CARD NR3 AND THE APU FIRE BOTTLE. OPERATIONAL CHECKS GOOD. AC OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050627000292005062700029EA 2005 6 27 SWIA200515116 120050606A5610 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07437SW 7564 CAPTAIN'S WINDSHIELD SHOWING STAR CRACKS IN ALL FOUR CORNERS. REPLACED CAPTIANS WINDSHIELD IAW AMM 56-11-01. 2L72 4F RTA21EA 20050627000402005062700040 2005 6 27 SA05062 420050603A2565 LANYARD AIRBUSA319 A319112 3930323EU ESCAPE SLIDE DAMAGED A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19750UW 1315 PLS - THE MAIN ENTRY DOOR SLIDE WOULD NOT ARM. MAINTENANCE REMOVED A LANYARD FROM THE GIRT BAR MECHANISM. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20050627000472005062700047NM 2005 6 27 C1HA200594002 120050601A5753 CARRIAGE BOEING727 727290 138408WNM LT TE FLAP VIBRATION A C1HAJA DUMP FUEL UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL15294AS 22146 DURING CLIMB-OUT AT APPROX FL 190, VIBRATION FELT THROUGHOUT A/C. VISUAL INSP FOUND LT TE FLAP VIBRATING AS BEFORE (LOG PAGE 3059). VIBRATION PERSISTED FROM 310 KIAS TO 250 KIAS. FUEL DUMPED (APPROX 4000 LBS) AND AIR RETURN TO MMUN. REF LP C03060 ITEM 3. LT I/B AFT FLAP VIBRATION IN FLIGHT. R & R LT I/B AFT FLAP CARRIAGE ASSY POSITION 3 AND 4. OPS CHECKS NORMAL. REF MM 27-51-01. 2L73 4F A3WE 20050627000522005062700052SO 2005 6 27 MASA200500381 120050523A33503025103 LIGHT EMB 145 EMB145LR 3260212SO LT OVERWING INOPERATIVE A MASAK NONE O OTHER ININSP/MAINT 1 SW07841MJ 145448 DURING WALK AROUND DISCOVERED LT EXTERNAL OVERWING EMERGENCY LIGHT NOT ILLUMINATING. MX REPLACED LIGHT ASSEMBLY. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050627000542005062700054SO 2005 6 27 MASA200500389 120050524A3397 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSLOOSE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07836MJ 145359 CAPTAIN REPORTED SEVERAL ROWS OF FLOOR EMERGENCY PROXIMITY LIGHTING INOPERATIVE. MX FOUND AND SECURED A LOOSE CONNECTOR. 2L72 4T RTT00011AT 20050627000602005062700060EA 2005 6 27 COMA0560330 120050601A5343 DRAG ANGLE CNDAIRCL600 CL6002B19 1900309EA LT MLG CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01710CA 7241 LT MLG DRAG ANGLE INBOARD OF BATTERY RIB CRACKED. REPAIRED IAW CRJ SRM 51-42-21. 2L72 4F RTA21EA 20050627000672005062700067SO 2005 6 27 C2XA05IA075 120050603A335020131A BATTERY PACK EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW27169512801 2801 145063 DURING PREFLIGHT INSP, CREW REPORTED THAT FWD BULKHEAD EMERGENCY EXIT LIGHT INOPERATIVE. MX R & R NR 2 EMERGENCY LIGHT BATTERY PACK. OPS CHECKED WITH NO DEFECTS. ACFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20050627000812005062700081NM 2005 6 27 UPS05444605 120050519A5347 CARGO TRACK BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 BS 525-610 RBL 11 TIE DOWN TRACK FLANGE ANCHOR NUTS AREA FOUND CORROSION. CORROSION BLEND OUT 0.025 BY 1.0 BY 9.0 IN. EXCEED SRM 53-10-01 FIG 1 LIMIT. M/D BS 510- BS 630 RBL 11 TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 14. 2L74 4F A20WE 20050627000882005062700088NM 2005 6 27 UPS05444612 120050513A531465B100983 STIFFENER BOEING747 747123F NM KEELBEAM CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 FX AIR CONDITIONING BAY LT KEELBEAM BOX EXTERNAL SURFACE VERTICAL WEB ATTACH STIFFENER FOUND CRACKED AT STA 983 LBL 9 WL 95 INCH (CRACK LENGTH .500) FX AIR CONDITIONING BAY LT KEELBEAM BOX EXTERNAL SURFACE VERTICAL WEB ATTACH STIFFENER REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02. 2L74 4F A20WE 20050627000962005062700096EA 2005 6 27 MASA200500422 120050531A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSINOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0727318 7318 FIRST EMERGENCY CEILING LIGHT IN THE CABIN INOPERATIVE. MX RELAMPED THE LIGHT. 2L72 4F RTA21EA 20050627000982005062700098SO 2005 6 27 MASA200500427 120050601A3397 WIRE EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSLOOSE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07853MJ 145464 OVERWING EXIT SIGN INOPERATIVE. MX FOUND CONNECTIONS LOOSE AND DIRTY. AFTER CLEANING AND RESECURING SIGN ILLUMINATED AS REQUIRED. 2L72 4T RTT00011AT 20050627001272005062700127NM 2005 6 27 AWXA200500684 120050612A2910 HYDRAULIC SYSTEM BOEING737 7373G7 1384595NM A-RESERVOIR OVERSERVICED A AWXAA UNSCHED LANDING WGJINADEQUATE Q C MULTIPLE FAILURE WARNING INDICATION CLCLIMB 1 WP28158AW 23780 AIR TURNBACK, AFTER TAKEOFF DURING FLAP AND GEAR RETRACTION YAW DAMPER, FEEL DIFFERENTIAL AND FLIGHT CONTROL BELOW PRESSURE LIGHTS ILLUMINATED. WENT TO STANDBY RUDDER -B- AND LIGHTS EXTINGUISHED. AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND SYSTEM -A- RESERVOIR OVERSERVICED. SERVICED TO CORRECT LEVEL. PERFORMED OPERATIONAL CHECK ON LOW PSI WARNING PER BOEING 737-300 AMM 27-31-00, PERFORMED ELEVATOR AND TAB CONTROL SYSTEM TEST IAW BOEING 737-300 AMM 27-31-00, PERFORMED HYDRAULIC MODULAR TEST IAW BOEING 737-300 AMM 27-09-21 PERFORMED LANDING GEAR TRANSFER VALVE OPERATIONAL TEST IAW BOEING 737-300 AMM 32-31-71, PERFORMED POWER-ON HYD LEAK CHECK, ALL SYS CHECKED NORMAL. 2L72 4F RTA16WE 20050627001312005062700131EA 2005 6 27 QXEA200501069 120050620A2760C13045BA03 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA SPOILERS MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION APAPPROACH 1 NM09605QX320 7 10022 PITCH FEEL FAULT STATUS MESSAGE. MESSAGE DISAPPEARED WHEN TERMINATING CHECKLIST WAS COMPLETED. REPLACED NR 2 SSCU IAW CRJ-700 AMM 27-61-05-000-801-A01 AND 400-801-A01. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20050627001322005062700132EU 2005 6 27 F3LA200500026 120050621A27303945128206 COMPUTER AIRBUSA318 A318111 3940019EU ELAC 1 UNSERVICEABLE A F3LAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM03802FR 3537 1991 AIR TURNBACK DUE TO FAULT: FLT/CTL ALTN LAW PROT LOST ECAM. PERFORMED EFCS GROUND SCAN PER AMM 27-96-00-740-001. FOUND ELAC NR 1 FAULT. REPLACED ELAC NR 1 PER AMM 27-93-34, PB401. PERFORMED OPS TEST OF ELAC NR 1 PER AMM 27-93-00-710-001 AND TESTED OKAY. NO FAULTS NOTED. PERFORMED LAND CAT III OPERATIONAL TEST PER AMM 22-97-00-710-001 AND TESTED OKAY. AIRCRAFT CAT IIIB STATUS RETAINED. 2L72 4F RT 20050627001342005062700134NM 2005 6 27 QXEA200501071 120050621A6120954215B653323 SELECTOR SWITCH BOMBDRDHC8 DHC8402 1390042NM ZONE 200 INOPERATIVE A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09401QX 4031 RETURNED TO GATE, WHEN AUTO FEATHER WAS INITIALLY SELECTED, ALL INDICATIONS WERE NORMAL. 24 HOUR SYSTEM TEST WAS NORMAL PRIOR TO TAXI AS WELL. DURING TAXI, AFTER CHECKLIST WAS DONE, INDICATIONS FOR AUTO FEATHER ON BOTH SWITCH LIGHT AND ED DISAPPEARED, THERE MAY HAVE BEEN A POP ASSOCIATED WITH INDICATING FAILURE. FOUND CDS FAULT CODES 64, 494. FOUND AUTO FEATHER SELECT SWITCH WOULD NOT STAY ENGAGED IF SELECTED ON POSITION. REPLACED AUTO FEATHER SELECT SWITCH. OPERATIONAL TEST GOOD WITH NO RECURRENCE OF FAULT CODES OR DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050627001662005062700166NM 2005 6 27 HNAA0500059 120050619A3260 PSEU DHAV DHC8 DHC8102 2809003NM MLG INDICATOR FAULTY A HNAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA07934HA335892166 139 NOSE GEAR LIGHT WILL NOT EXTINGUISH AFTER TAKEOFF. CYCLED GEAR AND LIGHT REMAINED ON. REMOVED AND REPLACED THE PSEU. 2H72 4T RTA13NM 20050627001682005062700168WP 2005 6 27 ARWA20050606 120050616A5210 SEAL DOUG DC8 DC863F 302198FWP PAX DOOR OPEN A ARWAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO19906R 46087 UNABLE TO CONTROL PRESSURIZATION DURING CLIMB. PERFORMED AIR TURNBACK - OVERWEIGHT LANDING INTO KMIA WITHOUT ANY FURTHER INCIDENTS. PRESSURIZED AIRCRAFT AND FOUND CABIN ENTRANCE DOOR ANGLE-SEAL UPPER AND LOWER RETAINER PARTIALLY OPEN, LUBE CABIN SEAL IN ACCORDANCE WITH M/M 12-83-1; OPERATIONAL CHECK NORMAL IN ACCORDANCE WITH M/M 21-30-0; PRESSURALIZATION NORMAL. 2L74 4F 4A25 20050627001712005062700171NM 2005 6 27 2005UALA00557 120050506A5313 STRINGER BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE GOUGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29313UA 23674 GOUGE FOUND ON THE INSIDE FLANGE OF S20R AT BS 943. REPAIR CHANNEL FABRICATED AND INSTALLED IN CENTER OF THE STRINGER. 2L72 4F4 FRTA16WE E21EU 20050627001732005062700173NM 2005 6 27 2005UALA00559 120050506A5322 SHEAR TIE BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29313UA 23674 OVERSIZE HOLES WERE FOUND COMMON TO SHEAR TIE AT STA 727D BETWEEN S23R, S24R AND THE SKIN. FUSELAGE FRAME SHEAR TIE WAS REPLACED AND REINFORCED PER SRM 51-00-04. 2L72 4F4 FRTA16WE E21EU 20050627001782005062700178NM 2005 6 27 2005UALA00564 120050611A5512 SKIN BOEING777 777222 1385219NM PWA PW4077PW4077 NE HORIZONTALS TAB LIGHTNING STRIKEA UALAK NONE O OTHER ININSP/MAINT 1 WP29213UA 30219 LIGHTNING STRIKES LT HORIZONTAL STAB UPPER SURFACE, INBOARD END. LIGHTNING STRIKES LT HORIZ STAB UPPER SURFACE, INBD END. A MAJOR REPAIR WAS INSTALLED PER REO-G1067A & EVA-50377. THIS COMPOSITE REPAIR IS INTERIM (FOR 24 MONTHS - 10JUN07) OR NEXT SCHEDULED 'C' CHECK (09OCT06), WHICHEVER COMES FIRST. THIS REPAIR MUST BE REINSPECTED EVERY 500 FLIGHT-CYCLES WITH MAXIMUM LIMIT AT 3,000 FLIGHT-CYCLES. N-R U1634H. MF 4982 WAS CREATED TO MONITOR THIS TEMPORARY REPAIR. 2L72 4F4 FRTT0001SE E46NE 20050627001812005062700181 2005 6 27 2005UALA00567 420050615A256563667103 HOSE AIRCRUISERS AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE SLIDE BROKEN A UALAK NONE O OTHER ININSP/MAINT 1 WP29426UA A7207 510 BROKEN HOSE AT ASPIRATOR. THE HOSE WAS FOUND BROKEN AT ASPIRATOR CONNECTION DURING MAINTENANCE OF THE SLIDE IN THE SHOP. A PROBABLE CAUSE IS KINKED ROUTING OF THE HOSE DURING THE PREVIOUS PACKING OF THE ASSEMBLY. THE STRESS ON THE HOSE RESULTED IN ITS BREAKAGE. HOSE WAS REPLACED AND CMM PROCEDURE WAS FOLLOWED. 2L72 4F4 FRTA28NM E40NE 20050627001842005062700184NM 2005 6 27 2005UALA00570 120050615A5330 SKIN BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE GOUGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29383UA 24658 EXTERNAL FUSELAGE SKIN BELOW AFT PIT DOOR THRESHOLD SKIN HAS DEEP GOUGES. REMOVED DAMAGE, INSTALLED DOUBLER, TRIPLER AND QUADRUPLER PER EAI050117 AND BOEING 8100-9. 2L72 4F4 FRTA16WE E21EU 20050627001872005062700187EU 2005 6 27 2005UALA00573 120050527A2197 ELEC CONNECTOR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE OUTFLOW VALVE DISCONNECTED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29427UA 512 SKIN VALVE FAULT DISPLAYED ON UPPER ECAM. FOUND CONNECTOR ON SKIN EXCHANGER ISOLATION VALVE 24HQ NOT CONNECTED. RECONNECTED CONNECTOR AND REACTIVATED SKIN VALVE. ALL TEST PASSED. 2L72 4F4 FRTA28NM E40NE 20050627001882005062700188 2005 6 27 SWAA051840 420050622A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29215WN 32487 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050627001902005062700190NM 2005 6 27 SWAA051842 120050622A2797MS21260L6RH TERMINAL BOEING737 7373H4 1384600NM TE FLAPS FAULTY A SWAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SW29373SW 26581 AIR TURNBACK, AFTER DEPARTURE, L/E FLAPS TRANSIT LIGHT AND NR 1 FLAP OVERHEAD LIGHT STAYED ILLUMINATED. RECYCLED FLAPS, NO CHANGE. REMOVED AND REPLACED NR 1 FLAP GROUND TERMINAL PER MM. 2L72 4F RTA16WE 20050627001922005062700192NM 2005 6 27 SWAA051844 120050622A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29458WN 33857 EEPLS COVER LOOSE AT ROW 1. REMOVED AND REPLACED COVER PER MM. 2L72 4F RTA16WE 20050627001942005062700194 2005 6 27 SWAA051846 420050622A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29631SW 27706 DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050627001962005062700196NM 2005 6 27 SWAA051848 120050623A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 505, STR 16R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050627001982005062700198 2005 6 27 SWAA051850 420050623A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29333SW 23697 DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050627002002005062700200NM 2005 6 27 SWAA051852 120050623A3350BR2013 LIGHT BOEING737 7373H4 1384600NM MID CABIN WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29366SW 26577 DURING SCHEDULED C3 CHECK, FOUND EEPLS STRIP WORN AT ROW 20 DEF. REMOVED AND REPLACED EEPLS STRIP PER MM. 2L72 4F RTA16WE 20050627002022005062700202NM 2005 6 27 SWAA051854 120050623A2913849589 PUMP BOEING737 7377H4 1384404NM HYD SYSTEM FAILED A SWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW29440LV 29835 DECLARED EMERGENCY. ENGINE DRIVEN HYDRAULIC A-PUMP LOW PRESSURE LIGHT ILLUMINATED. AFTER 10 MINUTES A-SYSTEM HYDRAULIC QUANTITY DROPPED TO 20 PERCENT. A ELECTRIC TURNED OFF UNTIL LANDING. REMOVED AND REPLACED NR 1 ENGINE DRIVEN HYDRAULIC PUMP PER MM. 2L72 4F RTA16WE 20050627002042005062700204NM 2005 6 27 SWAA051856 120050623A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29685SW 23401 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 23R. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050627002062005062700206NM 2005 6 27 SWAA051858 120050623A3350 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29701GS 27836 DURING SCHEDULED MV2 CHECK, FOUND LOWER EMERGENCY EXIT LIGHT LENS BROKEN AT R1 DOOR. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20050628000192005062800019WP 2005 6 28 UPS05844686 120050428A5320 WEB DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 LT FWD UPPER AC BAY AT APPROX STA 8 WEB IS CRACKED APPROX 4 INCH LONG IN 2 PLACES. FABRICATED AND INSTALLED 2 DOUBLERS AND REPAIR WEB IAW SRM 53-03-03-0, 53-02-00-0 FIG 001D, 53-2-0 FIG 1D 51-1-21,51-1-20D AND 51-1-21A. 2L74 4F RT4A25 20050628000232005062800023WP 2005 6 28 0500829606 120050329A5312 VERTICAL SUPPORT DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01606NW 47225 DURING H-CHECK, FOUND CRACK IN BULKHEAD VERTICAL SUPPORT AT BS 756 L26L AND L26R. REPAIRED PER EA 96-202532. 2L72 4F A6WE 20050628000242005062800024WP 2005 6 28 0500859859 120050603A5347 SEAT TRACK DOUG DC9 DC951 3022051WP FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01768NC 47729 DURING H-CHECK, FOUND CORROSION ON SEAT TRACK AT BS 198-200 RBL 44. REPAIRED PER EA 98-204363. 2L72 4F RTA6WE 20050628000292005062800029NM 2005 6 28 HNAA0500051 120050608A5280 HINGE DHAV DHC8 DHC8102 2809003NM LT MLG DOOR MISSING A HNAAD RETURN TO BLOCK O OTHER CLCLIMB 1 EA07931HA4344343443 132 LT MAIN FORWARD GEAR DOOR REMAINED DOWN AFTER GEAR RETRACTION. REPLACED LT MAIN FORWARD GEAR DOOR AND MISSING HARDWARE ON AFT HINGE. REPLACED DAMAGED FRAME ASSY. ADJUSTED DOOR AND SWUNG GEAR. 2H72 4T RTA13NM 20050628000302005062800030SO 2005 6 28 C2XA05SH044 120050607A3230355022002 CONTROL UNIT EMB 145 EMB145ER 3260211SO MLG FAILED A C2XAO OTHER J WARNING INDICATION DEDESCENT 1 SW2714940 145033 LANDING GEAR AIR GROUND FAILED ON EXTENSION DURING DESCENT. MAINTENANCE REMOVED AND REPLACED LANDING GEAR ELECTRONIC UNIT IAW EMB 145 AMM 32-32-01, OPS CHECK GOOD. ACFT APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050628000312005062800031WP 2005 6 28 WX0500041 120050503A3350 LIGHT DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A WX0AK NONE O OTHER ININSP/MAINT 1 WP19860GA 49786 RED EMERGENCY PATH LIGHTS AT LAST ROW OF SEATS INOPERATIVE. MAINTENANCE REPLACED RED EMERGENCY FLOOR LIGHTS (EXIT IDENTIFIER) AT LAST ROW OF SEATS IAW MM 33-53-01. SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050628000632005062800063EA 2005 6 28 COMA0560337 120050607A5210601R3199831 DOOR FRAME CNDAIRCL600 CL6002B19 1900309EA PAX DOOR DAMAGED A COMAK NONE O OTHER ININSP/MAINT 1 SO01914CA28458 7012 DURING HEAVY MX CHECK PAX DOOR DETAILED INSP, PAX DOOR FORWARD AND AFT BOTTOM CORNERS FOUND SEVERELY DAMAGED. BOTH PARTS REPLACED IAW CRJ SRM STANDARD PRACTICES. 2L72 4F RTA21EA 20050628000642005062800064EA 2005 6 28 COMA0570060 120050603A3350YAD4F RELAY CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHTSMALFUNCTIONED A COMAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01655CA 10134 EMERGENCY LIGHTS TURN ON AND OFF WHILE IN THE ARM POSITION. REPLACED RELAY K135. 2L72 4F RTA21EA 20050628000652005062800065NM 2005 6 28 DHL2005784523 120050606A5260 WEB BOEING727 727227 1384078NM AIRSTAIR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01784DH 22001 RT AFT AIRSTAIR AT BS 1243 WEB CRACKED (MARKED RED). 2 STOP DRILL CRACK SIZE 249 IAW B727 SRM 51-10-1. FABRICATED DOUBLER REPAIR. ALODINED AND PRIMED SRM 51-10-2. INSTALLED DOUBLER REPAIR IAW B727 SRM 51-30-2 2L73 4F A3WE 20050628000742005062800074SO 2005 6 28 RAIA00504031 120050413A2611 WARNING LIGHT EMB 145 EMB145LR 3260212SO LAVATORY FALSE INDICATIONA RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03824HK 145498 LAVATORY SMOKE INDICATION IN FLIGHT. MAINTENANCE PERFORMED OPS CHECK OF LAV SMOKE SYSTEM. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050628000962005062800096EA 2005 6 28 ASOA05457 120050522A26218978892 FIRE BOTTLE CNDAIRCL600 CL6002B19 1900309EA APU BAY BLOWN A ASOAO OTHER N FALSE WARNING DEDESCENT 1 SO27833AS9398 165 DURING DESCENT, APPROXIMATELY 30 TO 40 SECONDS AFTER THE CREW STARTED THE CREW STARTED THE AUXILIARY POWER UNIT (APU), APU FIRE WARNING AND APU FAULT CAUTION MESSAGES WERE RECEIVED. THE QRH WAS COMPLIED WITH AND THE FIRE WARNING MESSAGE EXTINGUISHED BEFORE THE FO PUSHED THE APU FIRE SWITCH. THE AIRCRAFT LANDED SAFELY. MAINTENANCE CLEARED THE DEFERRAL (DML NR 66488) BY REMOVING AND REPLACING THE APU FIRE BOTTLE AND FIRE BOTTLE CARTRIDGE. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F RTA21EA 20050628001082005062800108SW 2005 6 28 LNX2005F00000 120050513A215020475546 COOLING TURBINE SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP LT AIR CON SEIZED A LNXAO OTHER O OTHER NRNOT REPORTED 1 SO2961NE AC761B AC HAD DEPARTED THE GATE AND WAS TAXIING TO RUNWAY FOR DEPARTURE. SEVERAL MINUTES AFTER ACTIVATION OF THE LT AND RT AIR CONDITIONING SYS. SMOKE WAS NOTED IN THE CABIN AND COCKPIT. THE SMOKE WAS ISOLATED BY TROUBLESHOOTING TO THE LT AIR CONDITIONER. THE AC RETURNED TO THE GATE AND MAINTENANCE VERIFIED THE LT AIR CONDITIONING COOLING TURBINE WAS SEIZED. THE AFFECTED COOLING TURBINE WAS REMOVED AND REPLACED. (K) 2L72 4T4 TRTA8SW E4WE 20050628001132005062800113EA 2005 6 28 ASOA05474 120050513A5730 SKIN PANEL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT WING CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27829AS 7232 DURING A C-CHECK, THE LOWER WING PLANK AT WS 148.019 LT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LOWER WING PLANK AT WS 148.019 LT SIDE IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050628001232005062800123NM 2005 6 28 UIEA200500079 120050524A5322 SHEAR TIE BOEING747 747271C 1384869NM GE CF6 CF650E2 30018NE FUSELAGE CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15536MC 22403 FRAME 440, RT SIDE BETWEEN STRINGERS 10A AND 11 TOP HOLE OF FRAME TO FUSELAGE SKIN ATTACHMENT ANGLE HAS .2500 INCH CRACK GOING UPWARD AND .0625 INCH CRACK GOING DOWNWARD. CUTOUT CRACKED SECTION OF ATTACHMENT ANGLE IAW SRM. ACCOMPLISHED HFEC INSP OF CUTOUT OF DAMAGE IAW NDT. NO DEFECTS NOTED. INSTALLED REPAIR ANGLE IAW SRM. EO ISSUED TO DOCUMENT MAJOR REPAIR. (K) 2L74 4F4 F A20WE E23EA 20050628001292005062800129CE 2005 6 28 GUU2005F00023 120050605A55101016200111 HINGE BRACKET BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA RT ELEVATOR CORRODED A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO298755018637 UE205 AT SCHEDULED ROUTINE MAINTENANCE, RT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RT OB ELEVATOR HINGE BRACKET. (K) 2L72 4T3 TRTA24CE E2NE 20050628001322005062800132NM 2005 6 28 AMTA200500501 120050601A3350 WIRE BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE EMERGENCY LIGHT DISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11561TZ 33526 EGRESS LIGHTS OUT RT OVERWING EXIT DOORS. FOUND BAD SOLDER JOINT ON M10614. CORRECTED SOLDER CONNECTION IAW MFG W/S/P CHP 20 OPS CHECK EGRESS IAW MM. (K) 2L72 4F4 FRTA2NM E12EU 20050628001412005062800141SW 2005 6 28 JJWA0061549 120050428A6210206010200133 BLADE BELL 206 206B 1181511SW ALLSN 250C 250C40B 03032NE MAIN ROTOR FOD E JJWAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 SO1725PM 831 1839 GROUND CREW CLOTH SAFARI HAD BLEW OFF IN HIGH WIND AND WENT THROUGH MAIN ROTOR. NO VIBRATIONS OR APPARENT DAMAGE FELT IN AIRCRAFT, WAS SMOOTH RETURNING TO AIRPORT. FOUND DENT TOP AND BOTTOM AT STA 141 TO 145, IB OF OB TRIM TABS. OTHER AIRCRAFT SENT TO MOVE GROUND CREW, BLADE REMOVED AND SENT FOR EVALUATION FOR PATCH. FACTORY ENGINEERING CONDEMED BLADE FOR TOP DENT TOO DEEP FOR REPAIR. (K) 1G71 3U3 U H2SW E1GL 20050628001422005062800142EA 2005 6 28 ASOA05499 120050607A3350HA4A039 RELAY CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHTSSHORTED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27838AS 7276 DURING A GROUND INSPECTION, AN AC ESS BUSS FAULT MESSAGE WAS RECEIVED AND THE EMERGENCY LIGHTS REMAINED ON. MAINTENANCE REMOVED AND REPLACED THE AC ESS TRANSFER RELAY. OPERATIONAL CHECKS GOOD AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050628001582005062800158 2005 6 28 CLC2005F00001 420050527A25655WD230100101 SLIDE DOUG DC10 DC1030 3023501WP GE CF6 CF650* 30018NE R1 DOOR DEPLOYED A CLCAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO29279AX 47816 DURING LINE MAINTENANCE THE R1 DOOR ESCAPE SLIDE WAS ACCIDENTLY DEPLOYED BY MAINTENANCE. REPLACED ESCAPE SLIDE. AIRCRAFT WAS RETURNED TO REVENUE SERVICE. (K) 2L73 4F4 F A22WE E23EA 20050628001742005062800174EA 2005 6 28 ASOA05472 120050510A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A AOSAK NONE O OTHER ININSP/MAINT 1 SO27829AS 7232 DURING C-CHECK, THE RT OB FS 484 ANGLE AT BL 27 TO 36 IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050628001802005062800180CE 2005 6 28 GNB2005F00004 120050608A8120470908 VALVE CESSNA402 402C 207590RCE CONT O360 TSIO360* 17025SO WASTEGATE WARPED E GNBAO OTHER O OTHER NRNOT REPORTED 1 SW01494BC2339 402C0308 823664 WARPED VALUE. (K) 1L72 3O3 O A7CE E9CE 20050629000032005062900003EA 2005 6 29 ASOA05348 120050415A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27821AS 7194 DURING C-CHECK, THE FLOOR ATTACH ANGLE AT FS 621 TO FS 559+112, LBL27 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING HE FLOOR ATTACH ANGLE AT FS 621 TO FS 559+112, LBL 27 IAW REO. (K) 2L72 4F4 FRTA21EA E15NE 20050629000082005062900008EA 2005 6 29 ASOA05344 120050412A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27820AS 7188 DURING C-CHECK, THE ANGLE AT FS 280 BETWEEN LBL 9 AND RBL 9 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE ANGLE AT FS 280 BETWEEN LBL 9 AND RBL 9 IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050629000122005062900012EA 2005 6 29 A6WA200540186 120050528A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31418AW 7618 LT SIDE FS 621-625.3 INTERCOSTAL AT STR 14L IS CRACKED IN RADIUS APPROXIMATELY 0.9 INCH LONG. REMOVED AND REPLACED LT SIDE FS621-625.3 INTERCOSTAL AT STR 14L IAW SRM. (K) 2L72 4F4 FRTA21EA E15NE 20050629000162005062900016NM 2005 6 29 AMTA200500506 120050606A5330 SKIN BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE FUSELAGE GOUGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11557TZ 32591 SEVERAL GOUGES FOUND UNDER PANEL AREA 321AL. REPAIRED DAMAGE IAW ERA. (K) 2L72 4F4 FRTA2NM E12EU 20050629000552005062900055EA 2005 6 29 ASOA05356 120050407A5310 POST CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE BULKHEAD DOOR CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27703EV 10038 DURING HANGAR MAINTENANCE, THE FS 280 BULKHEAD, DOOR POST AT LBL 11.128 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE FS 280 BULKHEAD, DOOR POST AT LBL 11.128 IAW EO. (K) 2L72 4F4 FRTA21EA EOOO63EN 20050629000582005062900058EA 2005 6 29 ASOA05345 120050412A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27820AS 7188 DURING C-CHECK, THE FLOOR MEMBER WEBBING AT FS 280 BETWEEN LBL9 AND RBL 9 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FLOOR MEMBER WEBBING AT FS 280 BETWEEN LBL 9 AND RBL 9 IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050629000652005062900065EA 2005 6 29 ASOA05488 120050605A33508GH00247308 LAMP CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27705EV 302778 10051 DURING A GROUND INSPECTION, THE RT AFT EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE RT AFT EXTERIOR EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA EOOO63EN 20050629000672005062900067CE 2005 6 29 K2Z2005F00000 120050531A531207126161 BULKHEAD CESSNA182 182J 2072722CE CONT O470 O470* 17026SO FUSLAGE CRACKED E K2ZAO OTHER O OTHER NRNOT REPORTED 1 NM113474F 18257474 CRACKS FOUND IN BOTH SIDES, UPPER CORNER OF RUDDER CABLE CUTOUT BETWEEN COUTOUT AND FLANGE. DYE PENETRANT INSPECTION OF FRONT FLANGE REVEALED NO DEFECTS. INSPECTION OF THIS BULKHEAD PREVIOUSLY ACCOMPLISHED AT 3607. NOT REQUIRED FOR INSPECTION IAW AD. RECOMMEND SHORTEN INSPECTION INTREVALS. BULKHEAD REPLACED. (K) 1H71 3O3 ONT3A13 E273 20050629000702005062900070EA 2005 6 29 ASOA05396 120050503A3350362624 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN SHORTED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27843AS 7310 DURING A GROUND INSPECTION, THE FORWARD SECTION OF EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AN EMERGENCY FLOOR LIGHT STRIP IN THE FORWARD SECTION. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050629000762005062900076NE 2005 6 29 QXEA200501070 220050621A72304114T15P02 FAN BLADE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE LT ENGINE VIBRATION A QXEAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 NM09605QX701 10022 GEE965274 ON CLIMBOUT, LEFT ENGINE VIB OF 1.9 INDICATION, REDUCED N1 TO CLIMB THRUST IN ORDER TO MAINTAIN A GREEN VIB INDICATION WITHIN .05. IT WAS NECESSARY TO REDUCE N1 TO 67.5 TO MAINTAIN A GREEN INDICATION (A 3 THRUST LEVER KNOB WIDTH SPLIT) RETURNED TO DEN. DESCENT, REDUCED THRUST SETTINGS. LEFT ENGINE REMAINED OUT OF YELLLOW ON TOUCHDOWN, WITH REVERSE THRUST DEPLOYED, ENGINE VIB INDICATION WAS A YELLOW 2.6. MX REPLACED NR 1 ENGINE FAN BLADES. OPS CHECK GOOD. 2L72 4F4 FRTA21EA EOOO63EN 20050629000782005062900078EA 2005 6 29 PNSA060502 220050622A7321252427312 FUEL CONTROL PIPER PA32 PA32301 7103207SO LYC O540 IO540K1G5 41532EA ENGINE FUEL UNKNOWN E PNSAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS CLCLIMB 1 AL034327P 328406002 PILOT WAS TAKING OFF AND JUST AS HE ROTATED THE ENGINE BEGAN TO RUN ROUGH, THE PILOT HAVING RUNAWAY LEFT LANDED AND SHUT DOWN ENGINE. MX STARTED THE ENGINE AFTER SOME DIFFICULTY THEN REPLACED FUEL SERVO, CLEANED FUEL NOZZLES, SUMPED A VERY SMALL AMOUNT OFF WATER OUT OFF FUEL TANKS, PURGED ENTIRE FUEL SYSTEM. THE ENGINE WAS STARTED AND A PERFORMANCE GROUND RUN DONE, OPS CHECKED NORMAL. 1L71 3O3 O A3SO 1E4 20050629000792005062900079WP 2005 6 29 P9RA20050092 120050616A3260833703 PROXIMITY SENSOR DOUG DC9 DC982 3022082WP NLG INTERMITTENT A P9RAO OTHER N FALSE WARNING CLCLIMB 1 SO1110801 49127 AFTER GEAR RETRACTION FROM SJU, NOSE GEAR LIGHT REMAINED ON. RECYCLED GEAR AND LIGHT EXTINGUISHED. REMOVED PROXIMITY BOX AND CLEANED THE CONTACTS. PERFORMED A-SYSTEM TEST IAW M/M. SYSTEM CHECKS NORMAL. NO PART REPLACEMENT. 6/22/05 ADDITIONAL MAINTENANCE ACTIONS PERFORMED. EVALUATION OF REPEAT WRITE UPS CONCERNING NOSE GEAR INDICATION. REMOVED AND REPLACED NOSE GEAR UP/DOWN LOCK SENSOR IAW M/M. REPAIRED CHAFED WIRE AT NOSE GEAR PROXIMITY SENSOR IAW SWPM. CYCLED GEAR NUMEROUS TIMES WITH NO FAULT INDICATION. RETRACT CYLINDER LEAK TESTED PER M/M. NO DEFECTS NOTED. 2L72 4F A6WE 20050629000812005062900081NM 2005 6 29 SWAA051876 120050627A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050629000842005062900084NM 2005 6 29 SWAA051880 120050627A2560PH22300L GLOWSTRIP BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29370SW 26597 DURING SCHEDULED A1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP LOOSE AT FWD END. REMOVED AND REPLACED STRIP PER MM. 2L72 4F RTA16WE 20050629000862005062900086NM 2005 6 29 SWAA051882 120050627A3350101114 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29403WN 29815 EMERGENCY EXIT LIGHT LENS COVER MISSING AT ROW 17. INSTALLED COVER PER MM. 2L72 4F RTA16WE 20050629000882005062900088EA 2005 6 29 VNAA0506005 120050611A2750 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A VNAAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL05241PS 7909 THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED AFTER FLAPS REACHED 45 DEGREES ON APPROACH. MAINTENANCE RESET THE FLAP ELECTRONIC CONTROL UNIT IAW RJ-SL-00-001. OPERATIONAL CHECKS WERE NORMAL. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050629000902005062900090CE 2005 6 29 DJFA2005112 120050619A2613 WARNING LIGHT RAYTHNDH125 HAWKER800XP 7150012CE OVERHEAT SYS ILLUMINATED E DJFAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA23791TA 258291 THE CREW REPORTED THAT 7 MINUTES AFTER TAKEOFF WHILE PASSING THROUGH 11,000 FEET, RECEIVED A REAR BAY OVERHEAT LIGHT. WHEN POWER WAS REDUCED BELOW 90 PERCENT, THE LIGHT WOULD EXTINGUISH. PRIORITY WAS REQUESTED FOR RETURN TO KPBI. 2L72 4F RTA3EU 20050629000912005062900091EA 2005 6 29 DJFA2005111 120050619A3230555405 SELECTOR VALVE CNDAIRCL601 CL6012A12 1900303EA NLG INOPERATIVE E DJFAO OTHER J WARNING INDICATION LDLANDING 1 EA23664CW 3064 THE CREW REPORTED THAT DURING A NORMAL GEAR EXTENSION, THE NOSE WHEEL WOULD NOT EXTEND. THE LANDING GEAR WAS CYCLED TWICE, AND THE NOSE GEAR REMAINED RETRACTED. A MANUAL EXTENSION WAS PERFORMED, AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR SELECTOR VALVE. OPERATIONAL AND LEAK CHECKS WERE GOOD. EXTENSION AND RETRACTION CHECKS WERE PERFORMED WITH NO NOTED DEFECTS. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21AE 20050629000942005062900094EA 2005 6 29 VNAA0506006 120050611A3220 UNKNOWN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NLG UNKNOWN A VNAAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 GL05260JS 7957 UPON POWER APPLICATION FOR TAKEOFF THE AIRCRAFT VEERED LEFT WITH NO RESPONSE TO RUDDER INPUT. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE INSPECTED THE NOSE LANDING GEAR AND FOUND NO DEFECTS. A HIGH SPEED TAXI WAS PERFORMED WITH THE CREW AND THE PROBLEM COULD NOT BE DUPLICATED. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050629001042005062900104NM 2005 6 29 SWAA051860 120050624A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500A + 17, STR 8R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050629001062005062900106 2005 6 29 SWAA051862 420050624A2565D31591474 SLIDE BOEING737 7373H4 1384600NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29341SW 24091 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20050629001082005062900108NM 2005 6 29 SWAA051864 120050623A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29355SW 25250 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR CUTOUT, LOWER AFT CORNER. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050629001102005062900110NM 2005 6 29 SWAA051866 120050625A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29362SW 26573 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 23L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050629001122005062900112 2005 6 29 SWAA051868 420050625A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29469WN 33859 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050629001142005062900114NM 2005 6 29 SWAA051870 120050625A532269353656 SHEAR TIE BOEING737 7377H4 1384404NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29495WN 33869 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 380, STR 17L. REPAIRED SHEAR TIE PER SWA EA. 2L72 4F RTA16WE 20050629001162005062900116NM 2005 6 29 SWAA051872 120050626A33506104781 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29774SW 27882 DURING SCHEDULED 5Y CHECK, FOUND RT OVERWING EXIT EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20050629001182005062900118SO 2005 6 29 C2XA05SH057 120050623A491014547494403 FIREWALL EMB 145 EMB145LR 3260212SO APU BAY CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714904 145477 SHV - DURING C-CHECK THE APU FIREWALL IS CRACKED AT RT O/B EDGE. MAINTENANCE REPAIRED THE DAMAGE ON THE APU FIREWALL RT O/B IAW EC5330-01473. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050629001202005062900120WP 2005 6 29 ABXA050157 120050613A53403920324501 FITTING DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47492 END FITTING LONGERON 30, CRACKED FS 644, LEFT SIDE. REMOVED AND REPLACED END FITTING AT LONGERON 30, FS 644 IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20050629001212005062900121WP 2005 6 29 ABXA050153 120050531A5320591412157 PAN DOUG DC9 DC931 3022065WP DOOR SEGMENT CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23947AX 47004 PASSENGER ENTRY DOOR PAN CRACKED IN 3 LOCATIONS ON FORWARD SIDE, 2 EACH 5 INCH CRACKS, 1 EACH 2 INCH CRACK. REMOVED AND REPLACED MAIN ENTRY DOOR IAW DC-9 MM 52-11-00-5-001. 2L72 4F A6WE 20050629001222005062900122WP 2005 6 29 ABXA050154 120050614A53135750198 LONGERON DOUG DC8 DC863F 302198FWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 CORROSION DISCOVERED ALONG LONGERON 24 RIGHT, BEHIND THE INBOARD SPLICE FITTING AT STA 980 IN THE RIGHT WHEEL WELL. REMOVED CORROSION FROM THE LONGERON AND FITTING BY BLENDING. ALL REWORKED AREAS ARE WITHIN SRM LIMITS. 2L74 4F 4A25 20050629001232005062900123WP 2005 6 29 ABXA050155 120050612A523059101575 PAN DOUG DC9 DC941 302207NWP AFT CARGO DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47492 AFT LOWER CARGO DOOR CRACK INDICATION IN RADIUS OF OUTER, ADJACENT TO TOP MOST STOP. REPAIRED DOOR IAW DC-9 SRM 52-03, 51-30-7, 51-30-1, 51-20-0 AND 51-30-5. 2L72 4F A6WE 20050629001242005062900124WP 2005 6 29 ABXA050156 120050613A532299234549 SHEAR TIE DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47492 SHEAR TIE CRACKED AT LONGERON 27 LEFT, FS 695. REPAIRED IAW DC-9 SSRM DWG K05159 AND DC-9 SRM 51-30-5. 2L72 4F A6WE 20050629001252005062900125EA 2005 6 29 VNAA0506009 120050616A3244299K631 TIRE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT MLG FAILED A VNAAO OTHER O OTHER LDLANDING 1 GL05250PS183 7929 INSPECTION AFTER LANDING REVEALED THE NR 2 TIRE TREAD HAD SEPARATED DURING LANDING, CAUSING DAMAGE TO THE LT INBD FLAP AND TO THE NR 1 ENGINE FAN BLADES. A BURST TIRE DAMAGE INSPECTION WAS PERFORMED IAW CRJ200 AMM 05-51-29-210-801. ALL DAMAGED COMPONENTS WERE REPLACED OR REPAIRED. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050629001262005062900126WP 2005 6 29 MWEA050056 120050514A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 SECTION OF EMERGENCY TRACK LIGHTS ARE INOPERATIVE FROM SEAT 9 THROUGH 18. REPAIRED WIRE. 2L72 4F A6WE 20050629001272005062900127WP 2005 6 29 MWEA050057 120050623A5330591140659 DOUBLER DOUG DC9 DC981 3022081WP FUSELAGE DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31807ME 48033 DENT REQUIRES REPAIR BETWEEN FRAME STATION 237 AND 256 BETWEEN LONGERON 17 AND 18 LEFT. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20050629001282005062900128CE 2005 6 29 FFKR103 120050603A32306046H39B RELAY BEECH 58 58 1152740CE CONT O520 IO520* 17032SO HARTZLHCJ3Y PHCJ3YF1 GL ZONE 100 BURNED OUT B FFKRA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO0511HW 12419 TH271 238964R ED4714A PILOT REPORTED THAT THE LANDING GEAR STOPPED RETRACTING DURING NORMAL OPERATION. MAINTENANCE INSPECTED LANDING GEAR SYSTEM AND FOUND THE L/G RELAY TO BE INOP CAUSING THE LANDING GEAR MOTOR TO CONTINUE TO OPERATE CAUSING IT TO FAIL AS WELL. REPLACED BOTH PARTS SWUNG LANDING GEAR, FOUND TO BE OPERATING NORMALLY. 1L72 3O3 O 3A16 E5CE 5 CP36EA 20050629001292005062900129EA 2005 6 29 VNAA0506002 120050606A3244299K631 TIRE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT MLG FAILED A VNAAO OTHER O OTHER LDLANDING 1 GL05248PS203 7925 AFTER LANDING INSPECTION REVEALED NR 3 TIRE THREAD HAD SEPARATED DURING LANDING CAUSING DAMAGE TO RT INBD FLAP AND TO NR 2 ENGINE FAN BLADES. NR 3 WHEEL & TIRE ASSEMBLY WAS REMOVED & REPLACED IAW CRJ200 AMM 32-41-01-000-801 & 32-41-01-400-801. SIX FAN BLADE ASSEMBLIES WERE REMOVED & REPLACED ON THE NR 2 ENGINE IAW CRJ200 AMM 72-20-00-000-801 & 72-20-00-400-801. THE AIRCRAFT WAS INSPECTED, FOUND SAFE FOR FLIGHT, AND FERRIED TO DAY. THE RT INBOARD FLAP ASSEMBLY WAS REMOVED AND REPLACED IAW CRJ200 AMM 27-54-01-000-801 & 27-54-01-400-801. THE RT MLG INBOARD BRAKE LINE ASSEMBLY WAS REMOVED AND REPLACED IAW CRJ200 AMM 32-11-25-000-801 AND 32-11-25-400-801. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050629001302005062900130EA 2005 6 29 VNAA0506004 120050611A2750 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A VNAAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 GL05241PS 7909 THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED ON SHORT FINAL WITH FLAPS AT 45 DEGREES. MAINTENANCE CHECKED THE FLAP ELECTRONIC CONTROL UNIT AND SKEW DETECTION SYSTEM FOR CODES IAW RJ-SL-27-84. SYSTEM FAULTS CLEARED. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050629001312005062900131EA 2005 6 29 VNAA0506007 120050612A3260895304 PROXIMITY SENSOR CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE MLG FAILED A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL05703PS2834 10137 THE GEAR DISAGREE MASTER WARNING MESSAGE ILLUMINATED ON CLIMBOUT. THE CREW RETURNED TO CLT. THE AIRCRAFT WAS FERRIED TO DAY WITH THE GEAR DOWN. MAINTENANCE OPERATIONALLY TESTED THE LANDING GEAR SYSTEM, THE PROXIMITY SENSING ELECTRONIC CONTROL, AND THE 3A & 3B AC HYDRAULIC PUMPS. ALL OPERATIONAL TESTS WERE GOOD. DUE TO MULTIPLE MAINTENANCE DATA COMPUTER FAULT INDICATIONS THE PSEU WAS REMOVED & REPLACED IAW CRJ700 AMM 32-61-01-000-801-A01 & 32-61-01-400-801-A01. OPERATIONAL TESTS WERE GOOD. A SATISFACTORY OPERATIONAL CHECK FLIGHT WAS PERFORMED. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050629001322005062900132EA 2005 6 29 VNAA0506010 120050618A5200 ACCESS DOOR CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE FUSLAGE OPEN A VNAAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 GL05723PS 10181 AFTER TAKEOFF THE CREW HEARD SOUNDS FROM THE RT SIDE OF THE FWD FUSELAGE THAT INDICATED AN ACCESS PANEL WAS OPEN. THE FLIGHT RETURNED TO CLT. MAINTENANCE FOUND THE GROUND SERVICE PANEL (HEADSET) ACCESS DOOR OPEN. THE DOOR WAS VISUALLY INSPECTED. NO DAMAGE WAS FOUND. THE DOOR WAS SECURED CLOSED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050629001332005062900133NE 2005 6 29 PCSA6210501 220050621A7261 OIL SYSTEM BOEING727 727233 138408ANM PWA JT8 JT8D17 52049NE NR 3 ENGINE LEAKING A PCSAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO17395AJ 21100 688721 DURING CRUISE NR 3 ENGINE OIL TEMP WAS BETWEEN 125 & 130 DEG FOR 15 MINUTES. PERFORMED ALT PROCEDURES, RETARDED THROTTLE, DIDN'T HELP. SHUTDOWN NR 3 ENGINE, ENGINE WINDMILLED FOR 45 MIN. OIL PRESSURE STAYED ABOVE 25 PSI. DIVERTED & LANDED AT SJU. MX INSPECTED NR 3 ENGINE & FOUND AN OIL LEAK COMING FROM MAIN OIL FILTER PACKING. ENGINE MAIN OIL FILTER & PACKINGS WERE REMOVED INSPECTED & REPLACED. OIL FILTER INSPECTION REVEALED NO CONTAMINATION NOTED. NR 3 ENGINE WAS RUN AT TAKEOFF POWER FOR 5 MIN, ENGINE OIL TEMP STAYED BELOW 125 DEG. ALL PERAMETERS NORMAL. NO LEAKS NOTED, ALL WORK ACCOMPLISHED IAW BOEING MM CH-71-00 PG 609 & 71-00 PG 212A & AMERIJET ENGINE RUN FORM B-41. AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 FRTA3WE E2EA 20050629001342005062900134EA 2005 6 29 VNAA0506001 120050605A29136619002 PUMP CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE HYDRAULIC SYS FAILED A VNAAO OTHER J WARNING INDICATION CLCLIMB 1 GL05710PS924 10167 ON CLIMBOUT FROM CLE THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP FAILED. THE CREW CONTINUED TO DESTINATION CLT. MAINTENANCE REMOVED & REPLACED THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP IAW CRJ 700 AMM 29-11-01-400-801-A01. OPERATIONAL AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050629001352005062900135EA 2005 6 29 VNAA0506003 120050607A5270 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE CARGO DOOR FALSE ACTIVATIONA VNAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL05703PS 10137 DURING CLIMBOUT THE AFT CARGO DOOR CAUTION MESSAGE AND A PROX SYS FAULT STATUS MESSAGE ILLUMINATED. THE CREW ELECTED TO RETURN TO CLT. MAINTENANCE INSPECTED AND OPERATIONALLY CHECKED THE CARGO DOOR IAW CRJ 700 AMM 52-31-00-710-801-A02. THE CARGO DOOR WAS FOUND TO BE IN SERVICEABLE CONDITION. THE DOOR AND HANDLE WERE PROPERLY CLOSED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050629001362005062900136EA 2005 6 29 VNAA0505014 120050527A5200 ACCESS DOOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE OXYGEN SYSTEM OPEN A VNAAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 GL05245PS 7919 DURING CLIMB THE STALL FAIL WARNING MESSAGE ILLUMINATED. THE CREW RETURNED TO CLT. MAINTENANCE INTERROGATED THE MDC AND FOUND NO FAULT CODES. THE STALL WARNING SYSTEM OPERATIONALLY CHECKED GOOD. THE OXYGEN SERVICING DOOR WAS FOUND OPEN ON THE RIGHT SIDE OF THE FUSELAGE FORWARD OF THE NR 2 STALL VANE. THE DOOR AND FUSELAGE WERE INSPECTED AND NO DAMAGE WAS FOUND. THE DOOR WAS SECURED. AN OVERWEIGHT LANDING INSPECTION WAS PERFORMED WITH NO DISCREPANCIES FOUND. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050629001372005062900137NM 2005 6 29 2005UALA00574 120050617A339758783 WIRE BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU EMERGENCY LIGHT DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29331UA 24192 EEL FLOOR LIGHTS INOP ROW 1-2AB. EEL CABLE REPLACED, OK. 2L72 4F4 FRTA16WE E21EU 20050629001382005062900138NM 2005 6 29 2005UALA00575 120050618A3350362624 LAMP BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU ROW 15 DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29351UA 24319 EEL LIGHTS INOP FROM ROW 15 AFT TO AND INCLUDING EEL STRIP IN FRONT OF AFT GALLEY CONTAINER STOWAGE. *S/D* REPLACED EEL LAMP, OK. 2L72 4F4 FRTA16WE E21EU 20050629001392005062900139 2005 6 29 2005UALA00576 420050617A2565 HOSE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE ESCAPE SLIDE BROKEN A UALAK NONE O OTHER ININSP/MAINT 1 WP29434UA 592 THE HOSE WAS FOUND BROKEN AT SWIVEL AND BY ASPIRATOR DURING UNPACKING PROCEDURE. HOSE WAS FOUND BROKEN AT SWIVEL AND AT ASPIRATOR CONNECTION DURING MAINTENANCE OF THE SLIDE IN THE SHOP. PROBABLE CAUSES COULD BE MISHANDLING DURING TRANSPORTATION OR THAT THE ROUTING OF THE HOSE DURING THE PREVIOUS SLIDE PACKING WAS INCORRECT AND THAT RESULTED IN ITS BREAKAGE. HOSE WAS REPLACED. 2L72 4F4 FRTA28NM E40NE 20050629001402005062900140EU 2005 6 29 2005UALA00577 120050620A3610 LINE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE BLEED AIR LEAKING A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29429UA 539 LEFT WING BLEED LEAK. LEFT WING BLEED LEAK IN CRUISE. FLIGHT RETURNING TO DEN DUE TO ICING AND WX. FOUND VERY LARGE LEAK ON THE RT PACK OZONE CONVERTER AFT CLAMP, REMOVED CLAMP RE-ADJUSTED SEAL AND SECURED CLAMP, LEAK WAS BLOWING AT OVERHEAT LOOP ON KEELBEAM AREA, RAN PACKS AND WAI TEST MANY TIMES COULD NOT GET TO FAIL. 2L72 4F4 FRTA28NM E40NE 20050629001412005062900141NM 2005 6 29 2005UALA00578 120050621A5230135W1112 SKIN BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE FWD CARGO DOOR DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29794UA34386 26953 FWD CARGO DOOR AFT CORNER DAMAGED. DAMAGE DUE TO IMPACT WITH GROUND EQUIPMENT. REPAIRED PER 777 SRM 52-30-01. 2L72 4F4 FRTT0001SE E46NE 20050629001422005062900142NM 2005 6 29 2005UALA00579 120050620A3350362624 LAMP BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU ROW 12 DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29364UA 24533 EEL LIGHTS AFT OF ROW 12 DO NOT LIGHT. REPLACED EEL LAMP, OK. 2L72 4F4 FRTA16WE E21EU 20050629001432005062900143NM 2005 6 29 2005UALA00580 120050620A5330 SKIN BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU BS800 RBL25 STR2DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29315UA 23947 DURING FUSELAGE SKIN REPLACEMENT IN AFT PIT RT AFT LOWER FUSELAGE BS 800 RBL 25 STRINGER 25, SKIN HAS MISDRILLED HOLE. TRIPLER - FREEZE PLUG REPAIR ACP'D ON FWD LOWER CUTOUT PER SRM 53-00-01. 2L72 4F4 FRTA16WE E21EU 20050629001442005062900144NM 2005 6 29 2005UALA00581 120050621A339758781 WIRE BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU ROW 16 DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29304UA 23665 EEL FLOOR LIGHTS ARE INOP FROM SEAT 16ABC TO AFT GALLEY. REPLACED EEL CABLE, OK. 2L72 4F4 FRTA16WE E21EU 20050629001452005062900145NM 2005 6 29 2005UALA00582 120050621A4920 APU BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE APU BAY SHUTDOWN A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29641UA 25091 DIVERTED DUE TO AUXILIARY POWER UNIT AUTO-SHUTDOWN WITH LEFT GENERATOR DEFERRED INOPERATIVE. UPON LANDING APU FOUND 4.0 QUARTS LOW. MM ADDED OIL. ENGINEERING MONITORING OIL CONSUMPTION. TO DATE CONSUMPTION IS .014 QT/HOUR. LIMIT IS .20 QT/HR. SAMC REQUESTED ALITUDE START AND RAN APU ONE HOUR AT ALTITUDE WITH NO OIL CONSUMPTION. CAUSE OF LOW OIL QTY UNKNOWN. 0.3 OF QT USED SINCE EVENT WITH .001 QT/HR. 2L72 4F4 FRTA1NM E24NE 20050629001472005062900147 2005 6 29 2005UALA00584 420050620A256519C181918E RELIEF VALVE AIRCRUISERS BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE ESCAPE SLIDE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29792UA 0641 26934 THE PRV WAS DAMAGED INSIDE OF THE PACK. SLIDE/RAFT WAS REMOVED FROM AIRCRAFT AT NORMAL MAINTENANCE INTERVAL. DAMAGED PRESSURE RELIEF VALVE WAS OBSERVED DURING SLIDE/RAFT MAINTENANCE. THE EXACT CAUSE OF THE DAMAGE TO THE PRESSURE RELIEF VALVE COULD NOT BE DETERMINED, BUT IT IS SPECULATED IT WAS DAMAGED DURING THE LAST PACKING PROCESS. PRESSURE RELIEF VALVE ASSEMBLY WAS REPLACED. 2L72 4F4 FRTT0001SE E46NE 20050629001482005062900148EU 2005 6 29 2005UALA00585 120050622A2121EVT3454H BLOWER AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE E/E BAY SMOKE A UALAA UNSCHED LANDING BE SMOKE/FUMES/ODORS/SPARKS VIBRATION/BUFFET CRCRUISE 1 WP29481UA11695 1559 VIBRATIONS & RUMBLING NOISE UNDER FLT DECK ACCOMPANIED BY SMOKE. FOUND AVIONICS BLOWER FAN 20HQ FAILED. REPLACED FAN. 2L72 4F4 FRTA28NM E40NE 20050629001502005062900150EU 2005 6 29 2005UALA00587 120050623A3230848401 SENSOR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE MLG MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29407UA 456 V10365 NR 2 ENGINE REVERSER FAULT EMAC MESSAGE. ENG 2 REV ECAM MESSAGE AIRCRAFT RETURNED TO FIELD. REVERSER FAULT DUE TO LGCIU DUE TO CHRONIC ECAM ENG 2 REV FAULT IN FLIGHT THAT OCCURS AT THE SAME TIME AS A LGCIU2 FAULT. LANDING GEAR SENSOR 23GA REPLACED PER AMM 32-31-73 PG 401. 2L72 4F4 FRTA28NM E40NE 20050629001512005062900151NM 2005 6 29 2005UALA00588 120050624A335020131A BATTERY PACK BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU EMERGENCY LIGHT DISCHARGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29921UA 25388 EMERGENCY LIGHTS INOP AT DOOR 1L EXTERIOR SLIDE LIGHT, FIRST CLASS EEL LIGHTS, BULLNOSE LIGHT AT SEATS 2B & 6C, EXIT SIGN OVER DOOR 1R & FLIGHT DECK DOOR, AND FLIGHT DECK EMERGENCY DOME LIGHT. BATTERY PACK WAS REPLACED, OK. 2L72 4F4 FRTA16WE E21EU 20050629001532005062900153 2005 6 29 2005UALA00590 420050624A2565 TAPE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE ESCAPE SLIDE SEPARATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29451UA A6922 865 HINGE TAPE ON FLOOR RAMP IS SEPARATED. ADHESIVE FAILURE, RESULTED IN TAPE SEPARATION DURING THE PRESSURIZATION OF THE ASSEMBLY. UNIT WAS SENT TO OEM FOR REPAIR/DISPOSITION. 2L72 4F4 FRTA28NM E40NE 20050629001552005062900155NM 2005 6 29 CALA0500205 120050622A5315 FLOORBEAM BOEING757 757224 1384958NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712109 27299 INSPECTION FOUND FLOORBEAM CORRODED ON UNDERSIDE OF UNDER ANCHOR NUT ATTACH PLATE AT BS 1681, LBL 52. REPAIRED IAW ECRA 5320-01781. 2L72 4F RTA2NM 20050629001572005062900157CE 2005 6 29 DXTA200500807 120050626A3240 WARNING LIGHT CESSNA560 560XL 2076702CE BRAKES ILLUMINATED E DXTAO OTHER J WARNING INDICATION APAPPROACH 1 GL07676QS 5605176 UPON GEAR EXTENSION, LO BRAKE PRESS AND ANTI-SKID INOP LIGHT ILLUMINATED, FLUID IS LEAKING ON TO NOSE GEAR. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20050629001582005062900158CE 2005 6 29 DXTA200500808 120050626A3240 BRAKE ASSY CESSNA560 560XL 2076702CE MLG LEAKING E DXTAO OTHER KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 GL07692QS 5605092 LOW BRAKE PRESSURE AND ANTI-SKID INOP LIGHTS CAME ON JUST AFTER TAXI OFF RUNWAY THE BRAKE FLUID IS COMING OUT OF THE OVERFLOW NEAR THE NOSE WHEEL. WOULD NOT CANCEL. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20050629001602005062900160CE 2005 6 29 DXTA200500806 120050626A3220 LANDING GEAR CESSNA750 750 2076810CE NOSE MALFUNCTIONED E DXTAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL07989QS 7500089 WHILE CLIMBING THRU 35,400 FT NOSE GEAR UNLOCK AND BUMP WAS FELT. ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20050629001612005062900161CE 2005 6 29 DXTA200500804 120050624A326041EN496 POSITION SWITCH CESSNA500 560CESSNA 2076750CE MLG INOPERATIVE E DXTAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL07375QS 5600375 AFTER T/O OUT OF KHTO GEAR WOULD NOT RETRACT, HANDLE DID NOT MOVE. BEFORE LANDING AT HPN COMPLETED EMERGENCY GEAR EXTENSION PROCEDURE. REPLACED LEFT MAIN GEAR SQUAT SWITCH AND RIGGED PER CE560MM 32-61-00. PERFORMED GEAR RETRACTION AND EXTENSIONS PER CE560 MM 32-30-00 OPERATION NORMAL. SQUAT SWITCH FUNCTION NORMAL. ALL WORK IAW CE560MM. 2L72 4F RTA22CE 20050629001622005062900162CE 2005 6 29 DXTA200500803 120050624A3260 WARNING LIGHT CESSNA500 560CESSNA 2076750CE MLG FALSE ACTIVATIONE DXTAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL07313QS 5600325 AFTER TAKEOFF WHEN GEAR WAS RETRACTED RIGHT MAIN LIGHT AND RED GEAR UNSAFE REMAINED ILLUMINATED. RECYCLED GEAR DOWN NORMAL INDICATION AND LANDED A/C. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20050629001642005062900164EU 2005 6 29 MALA050510 120050621A5315 FLOORBEAM SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15421XJ 340B421 DURING 4K INSPECTION IN BNA FOUND FLOORBEAM AT FS 258 IS CORRODED AND HAS BEEN REPAIRED IAW SRM 53-70-30. 2L72 4T RTA52EU 20050629001652005062900165EU 2005 6 29 MALA050511 120050621A53207253721439 FLOOR SUPPORT SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15421XJ 340B421 DURING 4K INSPECTION IN BNA FOUND FLOOR REINFORCEMENT P/N 7253721-439 IS CORRODED AND HAS BEEN REPAIRED IAW SRM 53-70-30 AND 51-40-21. 2L72 4T RTA52EU 20050629001662005062900166EU 2005 6 29 MALA050509 120050626A3350 POWER SUPPLY SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15417XJ 340B417 ONE OUTPUT OF EMERGENCY POWER SUPPLY INOP. 2L72 4T RTA52EU 20050629001682005062900168EA 2005 6 29 MASA200500204 120050311A2400055046B SQUIB CNDAIRCL600 CL6002B19 1900309EA ADG BLOWN A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07271732567 7173 ASH 2912 BTV-PHL, THE PILOT RETURNED TO THE FIELD WHEN THE ADG AUTO DEPLOYED. ON CALL MAINTENANCE PLACED THE AUTO DE[PLOY FUNCTION ON DEFERRAL AND THE AIRCRAFT CONTINUED SERVICE. 3/14/05 MAINTENANCE REPLACED THE ADG SQUIB. 2L72 4F RTA21EA 20050630000012005063000001WP 2005 6 30 ABXA050158 120050623A3260 RELAY DOUG DC9 DC931 3022065WP MLG INDICATOR MALFUNCTIONED A ABXAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL23929AX 45874 NOSE LANDING GEAR LIGHTS DID NOT ILLUMINATE. UNSAFE LIGHT WAS OUT. CYCLED GEAR WITH THE SAME RESULT. WIGGLED GEAR HANDLE AND NOSE LIGHT ILLUMINATED NORMAL. REMOVED AND REPLACED RELAY R2-28. SWUNG GEAR IAW DC-9 ADJ/TEST 32-60-00-2-0201. OPS CHECKED GOOD. 2L72 4F A6WE 20050627001642005062700164 2005 6 27 2005UALA00551 420050608A2565196181914E RELIEF VALVE BOEING757 757222 1384956NM PWA 2037 PW2037 NE ESCAPE SLIDE LEAKING A UALAK NONE O OTHER ININSP/MAINT 1 WP29547UA 25368 EES WAS TEST FIRED AND PRESSURE RECORDED GOOD. HOWEVER, THE BOTTOM TUBE WENT FLAT WITHIN 5 MINUTES OF INFLATION PRESSURE RELIFE VALVE FOUND LEAKING. PRESSURE RELIEF VALVE ASSEMBLY WAS REPLACED. 2L72 4F4 FRTA2NM E17NE 20050627001672005062700167NM 2005 6 27 2005UALA00554 120050612A5230 SKIN BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU CARGO DOOR DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29315UA 23947 AFT CARGO DOOR EXTERNAL SKIN HAS SEVERAL DENTS BEYOND LIMITS. *S/D* REPAIR ACP'D AT HMV4 AT AAR-IND. ALL DAMAGES CUTOUT AND INSTALLED 43 X 48 INCH REPAIR DOUBLER PER SRM 52-30-01 FIG 202. 2L72 4F4 FRTA16WE E21EU 20050627001702005062700170EU 2005 6 27 2005UALA00556 120050613A2121 FAN AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE E/E BAY FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29419UA 487 BOTH AVIONICS BLOWER AND EXTRACT FANS BECAME INOPERATIVE. PFR SHOWS ECAM VENT AVIONICS SYS FAULT WITH ASSOCIATED FAILURE MSG NO AEVC DATA. TSM SHOWS POSSIBLE COMPUTER FAULT 10HQ. REPLACED AEVC AND BITE TEST CHECKS GOOD. NO FAILURES OR FAULTS NOTED. 2L72 4F4 FRTA28NM E40NE 20050627001742005062700174NM 2005 6 27 2005UALA00560 120050613A5230135W1112 SKIN BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE AFT CARGO DOOR DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29798UA31815 26928 AFT CARGO DOOR HAS LOWER AFT CORNER DAMAGED. AIRCRAFT REPAIRED PER 777 SRM 52-30-01, REPAIR 17. 2L72 4F4 FRTT0001SE E46NE 20050627001762005062700176NM 2005 6 27 2005UALA00562 120050613A5241 FRAME BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU GALLEY DOOR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29315UA 23947 FWD GALLEY DOOR FWD LOWER FRAME CRACKED AT FASTENER HOLE. *S/D* REPAIR ACP'D AT HMV4 AAR WITH FWD FRAME REPLACEMENTT PER SRM 051-40-02 & 51-10-02, GNMM 5-0-4- -11 & 5-0-7-001. 2L72 4F4 FRTA16WE E21EU 20050627001802005062700180 2005 6 27 2005UALA00566 420050614A2565D17961103 PIN BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU CYLINDER HEAD BROKEN A UALAK NONE O OTHER ININSP/MAINT 1 WP29347UA 2208 24251 THE SAFETY PIN WAS BROKEN OFF IN THE CYLINDER HEAD. CAUSE COULD NOT BE DETERMINED. REMOVED THE BROKEN PIN FROM CYLINDER AND REPLACE WITH A NEW SAFETY PIN. 2L72 4F4 FRTA16WE E21EU 20050627001832005062700183NE 2005 6 27 2005UALA00569 220050616A7200 ENGINE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 2 STALLED A UALAEC ENGINE SHUTDOWN ABORTED TAKEOFF MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 WP29446UA 834 V10374 NR 2 ENGINE OVERTEMPTED & STALLED ON TAKEOFF. ENGINE WAS REPLACED AND AIRCRAFT CONTINUED FUTHER FLYING WITHOUT INCIDENT. THE ENGINE FAILURE WAS CONFIRMED AS A HIGH PRESSURE COMPRESSOR 3RD STAGE BLADE (R3 BLADE) FAILURE. THIS IS AN INDUSTRY-WIDE AND KNOWN ISSUE, WITH BOTH A SHORT-TERM AND LONG-TERM FLEET MANAGEMENT PLAN: SHORT TERM IS BORESCOPE MONITORING OF FLEET FOR R3 MID-SPAN CONDITION. LONGER TERM IS UPGRADING OF R3 BLADE TO MORE ROBUST DESIGN. 2L72 4F4 FRTA28NM E40NE 20050627001862005062700186 2005 6 27 2005UALA00572 420050617A2562SRB10 ELT AIRCRUISERS BOEING777 777222 1385219NM PWA PW4077PW4077 NE SLIDE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29214UA 0224 30220 ELT WAS BROKEN. SLIDE/RAFT WAS REMOVED FROM AIRCRAFT AT NORMAL MAINTENANCE INTERVAL. DAMAGED ELT WAS OBSERVED DURING SLIDE/RAFT DISASSEMBLY. THE EXACT CAUSE OF DAMAGE TO THE ELT COULD NOT BE DETERMINED. IT IS SUSPECTED, HOWEVER, THAT THE ELT WAS ACCIDENTALLY DAMAGED DURING THE LAST PACKING PROCESS AND HAD REMAINED UNDETECTED. DAMAGED ELT IS CONSIDERED AN ISOLATED INCIDENT. 2L72 4F4 FRTT0001SE E46NE 20050627001952005062700195NM 2005 6 27 SWAA051847 120050622A3040141A48108 WINDOW BOEING737 7377H4 1384404NM COCKPIT ARCED A SWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW29793SA 27888 R2 COCKPIT WINDOW ARCING WITH WINDOW HEAT SWITCH TURNED ON. REMOVED AND REPLACED R2 WINDOW & HEAT CONTROLLER PER MM. 2L72 4F RTA16WE 20050627001972005062700197NM 2005 6 27 SWAA051849 120050623A575465C26686 SKIN BOEING737 7373H4 1384600NM RT WING SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29333SW 23697 DURING SCHEDULED C4 CHECK, FOUND RT WING NR 5 L/E SLAT T/E LOWER SKIN CRACKED. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050627001992005062700199NM 2005 6 27 SWAA051851 120050623A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 18L. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050627002012005062700201NM 2005 6 27 SWAA051853 120050623A55236959227 BUSHING BOEING737 7373H4 1384600NM ELEVATOR TAB WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29380SW 26587 DURING SCHEDULED C3 CHECK, RT ELEVATOR TAB FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB NR 1 HINGE BUSHING & HARDWARE PER MM. 2L72 4F RTA16WE 20050627002032005062700203 2005 6 27 SWAA051855 420050623A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29629SW 27704 DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050627002052005062700205NM 2005 6 27 SWAA051857 120050623A53306545774 SKIN BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E + 14, STR 18L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050627002092005062700209 2005 6 27 EVASN105EV01 420050621A3417 ADC DOUG MD11 MD11 3023602NM NR 2 INOPERATIVE W QOCFBA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP03105EV 48544 AFTER TAKEOFF FROM TAIPEI, DURING AIRCRAFT CLIMBING, CAPTAIN REPORT FIRST OBSERVOIR'S AIRSPEED INDICATION AND ALTITUDE INDICATION BLANK, CAPTAIN REQUEST AIR RETURN. ON GROUND CHECK FOUND NR 2 AIR DATA COMPUTER INOPERATIVE, AFTER REPLACED COMPUTER AND PERFORM PITOT-STATIC TEST, SYSTEM BACK TO NORMAL. 2L73 4F RTA22WE 20050627002132005062700213NM 2005 6 27 05FDEA01645 120050622A2750 CONTROL VALVE BOEING727 727200 138407ENM TE FLAP CONTROL LACK OF LUBE A FDEAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION NRNOT REPORTED 1 SO25211FE 22933 L/E DEVICES WOULD NOT RETRACT AT FLAPS 2 DEGREES. PERFORMED ADJUSTMENT AND TEST OF FLAP 2 DEG SWITCH AS PER M/M 27-82-021-2, OPS CK GOOD. INSPECTED PULLEYS ROD END GOING TO FLAP CONTROL VALVE AND LUBED AS NEEDED. FLAPS AND LEADING EDGE DEVICES GROUND CKS NORMAL. A/C OK TO CONTINUE. 2L73 4F RTA3WE 20050627002152005062700215CE 2005 6 27 71405 120050621A2750 CONTROL SYSTEM BEECH 1900 1900D 1154162CE TE FLAPS MALFUNCTIONED A AMWAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE07138YV UE138 AFTER TAKEOFF, CREW OBSERVED FLAPS WILL NOT RETRACT TO ZERO. AIRCRAFT RETURNED TO FIELD WITH NO FURTHER INCIDENT. MAINTENANCE CHECKED RIGGING AND CLEAND FLAP SPLIT FLAP SAFETY SWITCHES. THEREFORE NO PARTS WERE USED. 2L72 4T RTA24CE 20050628000112005062800011EU 2005 6 28 UPS05144675 120050524A5315A538133790000 FLOORBEAM AIRBUSA300 A300F4622R 3930360EU FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01120UP 0805 MAIN CABIN RT FLOORBOARD SUPPORT BRACE CRACKED STA 51 RBL 24. REMOVED AND REPLACED FLOORBOARD SUPPORT BRACE (CROSSBEAM) IAW A300 SRM 51-40-00, AIRBUS STANDARDS MANUAL ANSA 2814 AND DWG 15-A53813309. 2L72 4F RTA35EU 20050628000172005062800017WP 2005 6 28 UPS05844684 120050608A33505708458503 BATTERY PACK DOUG DC8 DC873F 302199FWP EMERGENCY LIGHTSINOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK IAW DC8 MM 33-50-01-2. TEST OK. 2L74 4F RT4A25 20050628000222005062800022WP 2005 6 28 0500849754 120050405A5320 FLOOR SUPPORT DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01754NW 47178 DURING H-CHECK, FOUND CRACKED VERTICAL FLOOR SUPPORT AT BS 794 LBL 22. REPAIRED PER EA 97-203199. 2L72 4F A6WE 20050628000262005062800026WP 2005 6 28 ABXA050151 120050610A3297 WIRE DOUG DC9 DC931 3022065WP MLG INDICATOR BROKEN A ABXAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 GL23908AX 47008 RT MAIN GEAR DOWN INDICATION "GREEN LIGHT" INTERMITTENT. CHECKED WITH ALT MAIN GEAR INDICATION. SHOWED GEAR DOWN. DID A MISSED APPROACH AND DECLARED AN EMERGENCY. VERIFIED NO RIGHT GEAR INDICATION, ALT SYS GOOD, FOUND CORROSION ON SWITCH S1-184 AND CONNECTOR P1-129. CONNECTOR P1-129 HAD THREE BROKEN WIRES AT PINS. REMOVED AND REPLACED CONNECTOR P1-129 AND SWITCH S1-184 IAW DC-9 MM 32-61-00 AND 32-60-01-2. COMPLIED WITH GEAR SWING IAW DC-9 MM 32-60-00-22A1-23. OPS CHECKED GOOD. 2L72 4F A6WE 20050628000432005062800043NM 2005 6 28 DHL2005784518 120050521A5754 RIB BOEING727 727227 1384078NM NR 6 SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01784DH 22001 FOUND NR 6 SLAT LE INTERIOR AT WS 491 INBOARD AND OUTBOARD RIBS CRACKED. REMOVED AND REPLACED RIBS AT NR 6 SLAT LE WS 491 INBD AND OUTBOARD IAW B727 SRM 51-30-2 PN 65-17289-20 AND 65-17289-22 BOTH PO NR 5080320. 2L73 4F A3WE 20050628000462005062800046NM 2005 6 28 DHL2005784519 120050525A5754 SKIN BOEING727 727227 1384078NM NR 6 SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01784DH 22001 FOUND NR 6 SLAT PREVIOUS REPAIR AT T/E I/B HOOK IS CRACKED. REMOVED PREVIOUS REPAIR AND FABBED NEW IAW 727 SRM 51-30-2 AND 57-50-3 FIG 10 DOUBLER TREATED, PRIMED, AND INSTALLED IAW 727 SRM 51-10-2 AND 57-50-3 FIG 10. 2L73 4F A3WE 20050628000472005062800047EU 2005 6 28 05FDEA01528 120050607A5414 PANEL AIRBUS310 A310 EU NR 2 PYLON CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25404FE 233 NR 2 PYLON PNL 423EL HAS SEVERAL AREAS OF CORROSION AND WEAR MARKS ALONG FASTENER HOLES IN EDGE OF PANELS. REMOVED CORROSION AND WEAR MARKS FROM NR 2 PYLON PNL NR 423EL IAW A310-200 SRM 51-74-10. MATERIAL LOSS IS OUT OF LIMITS IAW A310-200 SRM 54-50-00. REPLACED DAMAGED PNL 423EL WITH NEW PNL IAW A310 SRM 51-72-10. 2L72 4F RTA35EU 20050628000512005062800051WP 2005 6 28 ABXA050148 120050531A5320SB095201389 PAN DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23947AX 47004 PASSENGER ENTRY DOOR PAN CRACKED ABOVE UPPER DOOR HINGE MOUNT APPROX 3 INCHES EMANATING FROM PREVIOUS REPAIR. REPLACED DOOR ON NON ROUTINE 0311 AND IAW DC-9 MM. 2L72 4F A6WE 20050628000532005062800053EA 2005 6 28 COMA0560335 120050603A3230601R751461 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA NLG FAULTY A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01966CA20962 7132 AFTER DEPARTURE, RECEIVED NOSE GEAR DISAGREE WARNING MESSAGE. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD LANDING WITHOUT INCIDENT. REPLACED NLG SELECTOR VALVE. 2L72 4F RTA21EA 20050628000752005062800075EU 2005 6 28 RAIA00506002 120050602A3234877701 SELECTOR JETAIRJETSTMJETSTM4101 1500501EU MLG MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03556HK 41073 RED LIGHT IN GEAR HANDLE ILLUMINATED. MAINTENANCE REMOVED AND REPLACED GEAR CONTROL UNIT. OPS CHECKED GOOD. 2L72 4T RTA41NM 20050628000772005062800077EA 2005 6 28 VTZA200500105 120050604A5712601R107091 RIB CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27627BR 7233 LT BATTERY RIB CRACKED. 2L72 4F RTA21EA 20050628000862005062800086WP 2005 6 28 ABXA050143 120050603A213121011403 CONTROLLER DOUG DC9 DC931 3022065WP CABIN PRESSURE DEFECTIVE A ABXAO OTHER J WARNING INDICATION CRCRUISE 1 GL23943AX1 47528 AT 5000 FT. LOST CABIN PRESSURE. BOTH BLUE LIGHTS ON PRESSURE CONTROLLER ON. DID ABNORMAL, COULD NOT REGAIN CABIN CONTROL. REMOVED AND REPLACED NR 2 CABIN PRESSURE CONTROLLER AND PERFORMED OPS CHECK IAW DC-9 AMM 21-32-00. OPS CHECKED GOOD. 2L72 4F A6WE 20050628000932005062800093CE 2005 6 28 AOQ2005F00001 120050608A21333203353 OUTFLOW VALVE LEAR 60 60LEAR 5170707CE PWA 305 PW305 NE CABIN PRESSURE DEFECTIVE A AOQAO OTHER O OTHER NRNOT REPORTED 1 EA111940 002 (REF: 1940060805JC) CLIMBING THROUGH 12,000 FEET, CABIN PRESSURE PANEL DISPLAYED A FAULT LIGHT. SIMULTANEOUSLY AN EMERGENCY PRESS LIGHT ILLUMINATED FOLLOWED BY EMERGENCY PRESSURIZATION SYS ACTIVATION. CABIN ALT ONLY REACHED APPROX 6000 FT INDICATED. CREW THEN PROCEEDED TO FOLLOW CHECKLIST PROCEDURES. AC WAS INSPECTED AND PERFORMED PRESSURIZATION GROUND CHECKS. FOUND AUTO PRESS SYS FAILED. AUTO SYS PLACED ON MEL. UPON FURTHER TESTING AT MFG, FOUND DEFECTIVE FLOW CONTROL VALVE. REPLACED VALVE. ALL OPS CHECKS PERFORMED SATISFACTORY. AC RETURNED TO SERVICE. AC DIVERTED AND LANDED UNEVENTFULLY. (K) 2L72 4F4 FRTA10CE E35NE 20050628000992005062800099EA 2005 6 28 ASOA05468 120050528A5297 WIRE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE DOOR HANDLE BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27820AS 7188 DURING A GROUND INSPECTION, THE PASSENGER DOOR WOULD NOT OPEN FROM THE INSIDE AND THE GREEN ALIGNMENT MARKS WERE NOT ALIGNED. MAINTENANCE INSPECTED THE AC AND FOUND IT SAFE FOR A FERRY FLIGHT FOR PERFORMANCE OF THE APPROPRIATE C/A. MAINT FOUND THE INNER HANDLE PROXIMITY SWITCH PREVENTING THE HANDLE FROM STOWING PROPERLY AND ADJUSTED THE SWITCH. MAINT ALSO REPAIRED A BROKEN WIRE ON THE OUTER HANDLE STOW SWITCH AND INNER HANDLE SWITCH; ALSO ADJUSTED THE CAM ROLLER TO THE TORQUE TUBE. OPS CHECK GOOD. AC OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050628001102005062800110EA 2005 6 28 ASOA05470 120050528A3230533407 SELECTOR VALVE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE MLG MALFUNCTIONED A ASOAO OTHER J WARNING INDICATION APAPPROACH 1 SO27708EV2932 10060 DURING APPROACH, UPON SELECTING THE GEAR DOWN A GER DISAGREE MESSAGE WAS RECEIVED WITHOUT THE GEARS EXTENDING. THE QRH WAS COMPLIED WITH AND THE CREW MANUALLY EXTENDED THE GEARS SUCCESSFULLY. AN EMERGENCY WAS DECLARED AND AS A PRECAUTION IN CASE THE NOSE WHEEL STEERING DID NOT OPERATE PROPERLY. THE AIRCRAFT LANDED SAFELY AND WAS TOWED SAFELY TO THE GATE DUE TO THE NOSE WHEEL STEERING NOT OPERATING PROPERLY. MAINTENANCE REMOVED AND REPLACED THE MAIN LANDING GEAR (MLG) SELECTOR VALVE. OPERATIONAL AND LEAK CHECKS GOOD. AC OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA EOOO63EN 20050628001152005062800115WP 2005 6 28 ASAA0580168 120050307A532199336582503 FLOORBOARD DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE CAIBN DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 HV - CHECK - PAX CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (K) 2L72 4F4 FRTA6WE E9NE 20050628001252005062800125EU 2005 6 28 ASOA05387 120050501A33503012000 POWER SUPPLY AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHTSINOPERATIVE A ASOAO OTHER O OTHER NRNOT REPORTED 1 SO27634AS 370 DURING A GROUND INSPECTION, HALF OF THE EMERGENCY LIGHTS IN THE CABIN WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTS POWER SUPPLY 61WL. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2H72 4T RTA53EU 20050628001332005062800133EA 2005 6 28 ASOA05399 120050503A273170744 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE HORIZ STAB TRIM MALFUNCTIONED A ASOAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 SO27748EV2245 10158 DURING CRUISE, JUST PRIOR TO INITIAL DESCENT AT APPROX 37,000 FT, CREW RECEIVED MACH TRIM CAUTION MSG AND A STAB TRIM CAUTION. QRH WAS COMPLIED WITH FOR BOTH MESSAGES WITH NO CORRECTION. SHORTLY THEREAFTER, CREW RECEIVED AUTOPILOT TRIM CAUTION MSG AND COMPLIED WITH QRH WITH NO CORRECTION. CREW DECLARED EMERGENCY AND ELECTED TO PERFORM NO FLAP LANDING DUE TO HEAVY CONTROL FORCES WITH NOSE DOWN. AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED HORIZONTAL STAB TRIM MOTOR CONTROL UNIT (MCU). OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA EOOO63EN 20050628001552005062800155EA 2005 6 28 ASOA05491 120050605A5312 PRESSURE PANEL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27850AS 7355 DURING A C-CHECK, THE PRESSURE FLOOR BETWEEN FS 449.85-473.15, BL45 TO THE FLOOR UNDER THE LT AND RT OVERWING EXITS WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE PRESSURE FLOOR BETWEEN FS 449.85-473.15, BL45 TO THE FLOOR UNDER THE LT AND RT OVERWING EXITS IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050628001602005062800160EA 2005 6 28 ASOA05490 120050603A1100S1859 PLACARD CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE ESCAPE HATCH WORN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27850AS 7356 7355 DURING A C-CHECK, THE EXTERIOR EXIT PLACARD ON THE PILOTS ESCAPE HATCH WAS FOUND WORN. MAINTENANCE REMOVED AND REPLACED THE EXTERIOR EXIT PLACARD ON THE PILOTS ESCAPE HATCH. (K) 2L72 4F4 FRTA21EA E15NE 20050628001642005062800164WP 2005 6 28 ASAA0580173 120050228A575359114471 VANE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE TE FLAP DAMAGED A ASAAK NONE W INADEQUATE Q C ININSP/MAINT 1 NM02965AS 53079 HV - CHECK - FRAME HAS RIVET SET MARKS. REMOVED DAMAGED SECTION. INSTALED REPAIR FILLER, ANGLE, AND PLATE. (K) 2L72 4F4 FRTA6WE E9NE 20050628001652005062800165WP 2005 6 28 ASAA0580144 120050228A5315993658087 INTERCOSTAL DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FLOORBEAM CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 HV - CHECK - FLOORBEAM INTERCOSTAL IS CRACKED. REPLACED INTERCOSTAL. (K) 2L72 4F4 FRTA6WE E9NE 20050629000022005062900002EA 2005 6 29 ASOA05349 120050417A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27821AS 7194 DURING A C-CHECK, THE FS 625 LT/RT CLIPS IN THE AFT EQUIPMENT BAY WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FS 625 LT/RT CLIPS IN THE AFT EQUIPMENT BAY. (K) 2L72 4F4 FRTA21EA E15NE 20050629000092005062900009NE 2005 6 29 HALA0500610 220050601A7320 EEC BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE LT ENGINE FAULTY A HALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP13478HA 55123 SELECT L FADEC ON EAD (FOLLOWED SOP). AFTER 2 MIN EPR RETURNED TO NORMAL OPS. A/C RETURNED WHERE AN UNEVENTFUL LANDING WAS MADE. REMOVED AND REPLACED LT ENGINE EEC IAW AMM. OPS CHECK OK. NO FAULTS NOTED. (K) 2L72 4F4 FTRA6WE E00061EN 20050629000292005062900029EA 2005 6 29 ASOA05485 120050602A5320601R3117121 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27850AS 7355 DURING A C-CHECK, THE FS 484 INTERCOSTAL AT LBL 36 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FS 484 INTERCOSTAL AT LBL 36 IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050629000342005062900034EU 2005 6 29 ASOA05465 120050526A33507012210 LAMP AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27633AS 1432 344 DURING HANGAR MAINTENANCE, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY LIGHT ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. (K) 2H72 4T4 TRTA53EU E20NE 20050629000372005062900037WP 2005 6 29 ASAA0580160 120050301A5753 SKIN DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE RT IB FLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 HV - CHECK - RT IB FLAP BOTTOM SKIN DENTED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER. (K) 2L72 4F4 FRTA6WE E9NE 20050629000402005062900040NE 2005 6 29 KNK2005F00001 220050512A73200292208230 MANIFOLD SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE FUEL INJECTION COKED E KNKAO OTHER O OTHER NRNOT REPORTED 1 WP13111AK7561 3092 AC WOULD NOT START FOR MID-DAY FLIGHT. UPON INSPECTION, FOUND THAT ENGINE COMPRESSOR WOULD NOT ROTATE. ASSUMED FROM PROBLEMS WITH OTHER ENGINES THAT THIS WAS BEING CAUSED BY FUEL COKING ON THE INJECTION MANIFOLD. THIS WAS CONFIRMED DURING ENGINE DISASSEMBLY BY MFG TECH. (K) 1G71 3U3 UNCH9EU E19EU 20050629000422005062900042EA 2005 6 29 ASOA05346 120050413A5210601R3198055 STEP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27821AS 7194 DURING C-CHECK, THE PASSENGER DOOR TOP STEP WAS FOUND CRACKED. MAINTENANCE REPAIRED THE PASSENGER DOOR TOP STEP IAW CMM. (K) 2L72 4F4 FRTA21EA E15NE 20050629000442005062900044NM 2005 6 29 AMTA200500507 120050606A5420 SHIM BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE NR 1 ENGINE MIGRATED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11557TZ 32591 SHIMS MIGRATING IN NR 1 ENGINE MID-SPAR BULKHEAD AT OB AFT LOWER ATTACH BOLT UPPER SURFACE. REPAIRED DAMAGE IAW ERA. (K) 2L72 4F4 FRTA2NM E12EU 20050629000462005062900046EA 2005 6 29 ASOA05486 120050602A5712 RIB CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT WING CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27850AS 7355 DURING A C-CHECK, THE RT BATT RIB ASSEMBLY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE RT BATT RIB ASSEMBLY AT WS 53.60 IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050629000482005062900048WP 2005 6 29 ASAA0580163 120050307A532199365851 FLOORBOARD DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE CABIN DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 HV - CHECK - PAX CABIN FLOOR PANEL IS DELAMINATED AND CRACKED. REPLACED FLOOR PANEL. (K) 2L72 4F4 FRTA6WE E9NE 20050629000512005062900051WP 2005 6 29 ASAA0580167 120050307A532199365851 FLOORBOARD DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE CABIN DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 HV- CHECK - PAX CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (K) 2L72 4F4 FRTA6WE E9NE 20050629000602005062900060EA 2005 6 29 ASOA05355 120050407A5315 FLOORBEAM CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE FUSELAGE CORRODED A ASOAO OTHER O OTHER NRNOT REPORTED 1 SO27703EV 10038 DURING HANGAR MAINTENANCE, THE FS 280 TRANSVERSE BEAM WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE FS 280 TRANSVERSE BEAM IAW EO. (K) 2L72 4F4 FRTA21EA EOOO63EN 20050629000692005062900069EA 2005 6 29 ASOA05480 120050601A5330 DOUBLER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27850AS 7355 DURING C-CHECK, THE DOUBLERS AT FS 718, STRINGER 10-12 LT AND RT SIDES WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE DOUBLERS AT FS 718, STRINGER 10-12 LT AND RT SIDES. (K) 2L72 4F4 FRTA21EA E15NE 20050629000722005062900072EU 2005 6 29 ASOA05352 120050418A33503012000 POWER SUPPLY AEROSPATR72 ATR72 EU PWA PW120 PW127 NE EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27631AS229731009 362 DURING TAXI OUT, THE AFT FIVE ROWS OF EMERGENCY FLOOR LIGHTS AND EXIT SIGNS CAME ON ERRONEOUSLY. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY AT 73WL. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K) 2H72 4T4 TRT E20NE 20050629000752005062900075CE 2005 6 29 BSYA200500011 120050623A245025680756 GROUNDING STRAP LEAR 35 35A 5170602CE GENERATORS BURNED E BSYAA UNSCHED LANDING GHJMULTIPLE FAILURE ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 GL0756JA 342 ON TAKEOFF OUT OF BDL BOTH GENERATORS FELL OFF LINE, LEFT GENERATOR RESET BUT THE RIGHT GENERATOR WOULD NOT. FOUND GENERATOR GROUNDING STRAP HAD BEEN HOT AND BURNT, REMOVED AND REPLACED STRAP, OPS CHECKS GOOD. 2L72 4F A10CE 20050629000772005062900077NM 2005 6 29 20058 120050624A291082910010207 LINE DHAV DHC8 DHC8103 1386005NM NR 2 HYD SYSTEM LEAKING A KPVAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP13805WP 353 NR 2 HYD SYSTEM LEAK. NR 2 HYD AND NR 2 ENG HYD PUMP LIGHTS ILLUMINATED. FOUND A LEAK IN NLG WHEEL WELL BEHIND THE DEBRIS GUARD ON LINE (P/N 82910010-207) WHICH EMPTIED NR 2 HYD RES. INSTALLED A TEMP LINE IAW DHC -8 MM CH 20-06-03 PG 6 & SERVICED NR 2 HYD RES. OPS & LEAK CHECK GOOD. 2H72 4T RTA13NM 20050629001032005062900103NM 2005 6 29 SWAA051859 120050624A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727C + 8, STR 14R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050629001052005062900105NM 2005 6 29 SWAA051861 120050624A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED SERVICE CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS AT BS 500D + 18, STR 7R & STR 8R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050629001072005062900107NM 2005 6 29 SWAA051863 120050623A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29355SW 25250 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT A/C GROUND SERVICE DOOR CUTOUT, LT FWD CORNER, BS 520, STR 28L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050629001092005062900109NM 2005 6 29 SWAA051865 120050623A5753 SKIN BOEING737 7373H4 1384600NM LT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29355SW BN659 25250 DURING SCHEDULED C2 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM. 2L72 4F RTA16WE 20050629001112005062900111NM 2005 6 29 SWAA051867 120050625A33501330122 BATTERY BOEING737 7373H4 1384600NM EMERGENCY LIGHT FAULTY A SWAAK NONE O OTHER ININSP/MAINT 1 SW29370SW 26597 DURING SCHEDULED RON CHECK, LT & RT AFT CABIN EMERGENCY LIGHTS STAY CONSTANTLY ON. REMOVED AND REPLACED BATTERY & CHARGER ASSY PER MM. 2L72 4F RTA16WE 20050629001132005062900113NM 2005 6 29 SWAA051869 120050626A3350207377 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29483WN 32472 EEPLS LENS LOOSE AT R1 DOOR. SECURED LENS PER MM. 2L72 4F RTA16WE 20050629001152005062900115NM 2005 6 29 SWAA051871 120050615A55236959227 BUSHING BOEING737 7375H4 138449DNM ELEVATOR TAB WORN A SWAAO OTHER EF VIBRATION/BUFFET FLT CONT AFFECTED NRNOT REPORTED 1 SW29505SW 24182 IN ALL PHASE OF FLIGHT - VIBRATION FELT & TAIL OSCILLATION. REMOVED AND REPLACED LT ELEVATOR TAB INBOARD HINGE HARDWARE PER MM. 2L72 4F RTA16WE 20050629001462005062900146NM 2005 6 29 2005UALA00583 120050621A5512 SKIN BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU HORIZTONAL STAB DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29315UA 23947 LT LEADING EDGE OF HORIZONTAL STABILIZER HAS DENT MIDWAY ON THE LEADING EDGE. CUTOUT DAMAGE & EVALUATED PER SRM 55-10-01. ACP NDT PER B737 NDT MANUAL NO DEFECTS NOTED. FABRICATED & INSTALLED INTERNAL DOUBLER REPAIR, FILLER & NEW RIB PER AAR EA I050118. 2L72 4F4 FRTA16WE E21EU 20050629001492005062900149NM 2005 6 29 2005UALA00586 120050622A5330 BEAR STRAP BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29318UA 23950 AFT CARGO DOOR CUTOUT AFT SIDE HAS BEAR STRAP REPAIR THAT WAS REMOVED WHEN ACCOMPLISHED SKIN REPLACEMENT. INSTALLED DOUBLER-TRIPLER REPAIR PER SRM 53-00-01 FIG 230. 2L72 4F4 FRTA16WE E21EU 20050629001522005062900152 2005 6 29 2005UALA00589 420050602A2565D37085101 HOSE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE ESCAPE SLIDE BROKEN A UALAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP29433UA A7412 589 HOSE FOUND BROKEN DURING THE PACKING PROCEDURE. HOSE WAS FOUND BROKEN AT END NEAR ASPIRATOR CONNECTION DURING MAINTENANCE OF THE SLIDE IN THE SHOP. PROBABLE CAUSES COULD BE MISHANDLING DURING TRANSPORTATION OR THAT THE ROUTING OF THE HOSE DURING THE PREVIOUS SLIDE PACKING WAS INCORRECT AND THAT RESULTED IN ITS BREAKAGE. HOSE WAS REPLACED. 2L72 4F4 FRTA28NM E40NE 20050629001542005062900154 2005 6 29 2005UALA00591 420050624A2565D37085101 HOSE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE ESCAPE SLIDE BROKEN A UALAK NONE O OTHER ININSP/MAINT 1 WP29433UA A7412 589 HOSE FOUND BROKEN BY ASPIRATOR. HOSE WAS FOUND BROKEN AT END NEAR ASPIRATOR CONNECTION DURING MAINTENANCE OF THE SLIDE IN THE SHOP. PROBABLE CAUSES COULD BE MISHANDLING DURING TRANSPORTATION OR THAT THE ROUTING OF THE HOSE DURING THE PREVIOUS SLIDE PACKING WAS INCORRECT AND THAT RESULTED IN ITS BREAKAGE. HOSE WAS REPLACED. 2L72 4F4 FRTA28NM E40NE 20050629001562005062900156NM 2005 6 29 CALA0500206 120050615A5315143N5013 FLOORBEAM BOEING757 757224 1384958NM FUSEAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712109 27299 INSPECTION FOUND FLOORBEAM UPPER STRUCTURE CORRODED AT BS 680, RBL 53. REPAIRED IAW SRM 53-00-51, FIGURE 201, REPAIR 3. 2L72 4F RTA2NM 20050629001592005062900159CE 2005 6 29 DXTA200500805 120050624A2740 CONNECTOR CESSNA750 750 2076810CE HORIZONTAL STAB CONTAMINATED E DXTAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL07939QS 7500193 PRI STAB TRIM FAIL CAS MESSAGES IN FLT AT FL380, PRI STAB TRIM FAIL, A/P FAIL AND MACH TRIM OFF. CHECKED SYSTEM FOR PROPER OPERATION. COULD NOT DUPLICATE SQUAWK. REMOVED LT & RT HORIZONTAL STAB ACTUATOR ACCESS PANELS. FOUND WATER ON ALL CONNECTORS. CLEANED ALL CONNECTORS. CHECKED POWER AND GROUND; BRAKE AND CLUTCH CIRCUITS, ALL CHECKED GOOD. APPLIED DC4 TO ALL CONNECTORS AND RECONNECTED. OPS CHECKED GOOD, IAW 750 M/M CH 27-40-00. CLOSED UP REMOVED PANELS. 2L72 4J RTT00007WI 20050629001632005062900163CE 2005 6 29 DXTA200500782 120050616A323099146372 MANIFOLD CESSNA750 750 2076810CE NLG FAILED E DXTAO OTHER E VIBRATION/BUFFET DEDESCENT 1 GL07984QS2332 7500084 ON DESCENT TWO LOUD BANGS CAME FROM THE SAME AREA IN THE NOSE GEAR. - REMOVED LANDING GEAR CONTROL MANIFOLD DUE TO INTERNAL FAILURE. INSTALLED SERVICEABLE MANIFOLD IAW CE750 M/M CH 32-30-02. OPS CHECKED AND LEAK CHECKED GOOD. MANIFOLD WAS MODIFIED AND RETURNED TO SERVICE BY PNEUDRAULICS INC CRS PD6R469J 2L72 4J RTT00007WI 20050630000032005063000003EU 2005 6 30 MALA050507 120050624A3830 LAVATORY BAC 146 AVRO146RJ85A1500097EU FWD CABIN LEAKING A MALAA UNSCHED LANDING K FLUID LOSS CRCRUISE 1 GL15518XJ E2337 THE FWD F/A REPORTED THAT BLUE JUICE IS COMING OUT OF THE FWD LAVATORY. F/A NOTED THAT THE FLUID LOOKED LIKE IT WAS COMING OUT OF THE FLOORBOARDS. RETURNED TO MSP. DRAINED FWD LAVATORY. 2H74 4F RTA49EU 20050630000042005063000004EU 2005 6 30 05FDEA01544 120050608A5320 STRAP AIRBUS310 A310 EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25404FE 233 CORROSION AROUND NUT PLATE HOLES ON PANEL SPLICE FOR 326EL. REMOVAL OF CORROSION OUT OF LIMIT PER SRM 55-40-00. REMOVED AND REPLACED STRAP IAW A310/200 SRM 51-72-10. 2L72 4F RTA35EU 20050630000062005063000006EA 2005 6 30 QXEA200500992 120050518A5753 FITTING CNDAIRCL600 CL6002C10 1390015EA RT WING FLAP WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09616QX 10128 RT WING TRAILING EDGE OUTBOARD FLAP ROLLER GUIDE FITTING HAS WEAR DAMAGE. REPAIRED IAW CRJ 700 SRM 57-51-02-201-001-A01 AND SRM 51-41-02-001-001-A01. 2L72 4F RTA21EA 20050630000082005063000008EA 2005 6 30 QXEA200501003 120050517A1430 FASTENER CNDAIRCL600 CL6002C10 1390015EA LT WING SPOILERSLOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09616QX 10128 LT WING OUTBOARD FLIGHT SPOILERS HAVE LOOSE FASTENERS, OUTBOARD AND INBOARD SIDES. REPAIRED IAW CRJ 700 SRM 51-42-07-001-001-A01 AND SRM 51-25-01-00-001-A01. 2L72 4F RTA21EA 20050630000092005063000009EA 2005 6 30 QXEA200500994 120050517A1430 FASTENER CNDAIRCL600 CL6002C10 1390015EA RT WING SKIN LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09616QX 10128 RT WING UPPER SKIN TRAILING EDGE HAS LOOSE FASTENERS AT INBOARD OF MULTI-FUNCTION SPOILERS. REPAIRED IAW CRJ 700 SRM 51-42-07-001-001-A01 AND 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050630000102005063000010EA 2005 6 30 QXEA200501000 120050519A5330 SKIN PANEL CNDAIRCL600 CL6002C10 1390015EA FUSELAGE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09616QX 10128 FUSELAGE SKIN PANEL, SKIN DAMAGED AT STATION 421.00 TO 437.00, BETWEEN STRINGER 26L AND 24L. REPAIRED IAW CRJ 700 SRM 53-21-03-101-006-A01 AND SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050630000112005063000011EA 2005 6 30 QXEA200501001 120050517A5315 FLOORBEAM CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09616QX 10128 FORWARD FUSELAGE INTERIOR, FLOORBEAM AT STATION 280 IS CORRODED ALONG TOP FLANGE FROM LBL 30 TO RBL 30. REPAIRED IAW REO 670-53-11-047. 2L72 4F RTA21EA 20050630000122005063000012EA 2005 6 30 QXEA200501002 120050517A5315 FLOORBEAM CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09616QX 10128 FUSELAGE INTERIOR COCKPIT FLOORBEAM ANGLE HAS SPOTS OF CORROSION AT STATION 280, LBL 11 TO RBL 11. REPAIRED IAW CRJ 700 SRM 51-21-06-001-001-A01 AND SRM 51-21-11-001-001-A01. 2L72 4F RTA21EA 20050630000132005063000013EA 2005 6 30 QXEA200500995 120050520A5751 SKIN CNDAIRCL600 CL6002C10 1390015EA RT WING AILERON WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09616QX 10128 RT WING AILERON UPPER AND LOWER SKIN LEADING EDGE HAS WEAR MARKS. REPAIRED IAW CRJ 700 SRM 57-61-10-101-001-A01 AND SRM 57-52-32-400-811-A01. 2L72 4F RTA21EA 20050630000142005063000014EA 2005 6 30 QXEA200500996 120050516A5350 CHANNEL CNDAIRCL600 CL6002C10 1390015EA FUSELAGE BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09616QX 10128 AFT BELLY FAIRING 195DL JOINT STRAP, AFT CHANNEL HAS A BROKEN FLANGE AT AFT END OF CHANNEL. REPAIRED IAW HORIZON AIR EA R-53-333. 2L72 4F RTA21EA 20050630000152005063000015EA 2005 6 30 QXEA200500997 120050516A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA FUSELAGE GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09616QX 10128 EXTERNAL FUSELAGE SKIN, STATION 975.0, STRINGER 27 HAS A GOUGES IN SKIN. REPAIRED IAW HORIZON AIR EA R-53-333 AND CRJ SRM 51-42-21-001-001-A01. 2L72 4F RTA21EA 20050630000162005063000016EA 2005 6 30 QXEA200500998 120050517A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09616QX 10128 EXTERNAL FUSELAGE SKIN, STATION 981.0, STRINGER 26L TO 27 HAS GOUGES IN SKIN. REPAIRED IAW HORIZON AIR EA R-53-333 AND CRJ 700 SRM 51-21-16. 2L72 4F RTA21EA 20050630000172005063000017EA 2005 6 30 QXEA200500999 120050517A5753 VANE CNDAIRCL600 CL6002C10 1390015EA RT WING FLAP CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09616QX 10128 RT INBOARD FLAP VANE LEADING EDGE HAS CHAFED MARK. REPAIRED IAW CRJ 700 SRM 51-12-00-001-001-A01 AND SRM 51-25-01-00-001-A01. 2L72 4F RTA21EA 20050630000182005063000018NM 2005 6 30 QXEA200501032 120050610A33506104781 BATTERY PACK DHAV DHC8 DHC8202 2809007NM EMERGENCY LIGHTSINOPERATIVE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09352PH19054494 494 FORWARD EMERGENCY LIGHT STRIP LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK PS6. OPS CHECK GOOD. ACFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050630000192005063000019NM 2005 6 30 QXEA200501034 120050611A3260301450301 PSEU BOMBDRDHC8 DHC8402 1390042NM RT MLG DOOR MALFUNCTIONED A QXEAA UNSCHED LANDING O OTHER CLCLIMB 1 NM09407QX2823 2823 4049 DURING CLIMB-OUT, GEAR PARTIALLY CYCLED THREE TIMES OVER A FIVE MINUTE PERIOD. PASSENGER REPORTED SEEING GEAR DOORS COME OPEN DURING CLIMB-OUT. RETURNED TO FIELD WITHOUT FURTHER INCIDENT. ALL PASSENGERS WERE OK. NO CFR. INSPECTED PSEU, FOUND RT MLG DOOR RCLG GAP TOO LARGE. FOUND RGD RCL GAP TO FLUCTUATE WILDLY. INSTALLED NEW SENSOR. PERFORMED EXTENSION AND RETRACTION OPERATION IAW DHC-8-402 MM 32-31-00-710-801. OPS CHECK GOOD. NO DEFECTS NOTED. ACFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050630000212005063000021NM 2005 6 30 QXEA200501036 120050611A2160BYLF51514 SENSOR DHAV DHC8 DHC8202 2809007NM CABIN TEMP SYS MALFUNCTIONED A QXEAO OTHER O OTHER CRCRUISE 1 NM09346PH14152611 477 UNABLE TO CONTROL CABIN TEMP IN AUTO MODE. AUTO MODE STILL DID NOT WORK AFTER RESETTING CABIN TEMP AUTO, L MAIN E4 CIRCUIT BREAKER AS PER E/A CHECKLIST. MANUAL MODE WORKS FINE. MX REPLACED CABIN ZONE TEMP SENSOR. OPS CHECK GOOD. ACFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050630000222005063000022EA 2005 6 30 QXEA200501037 120050610A3411 STATIC SYSTEM CNDAIRCL600 CL6002C10 1390015EA CONTAMINATED A QXEAD RETURN TO BLOCK JG WARNING INDICATION MULTIPLE FAILURE TXTAXI/GRND HDL 1 NM09607QX 10024 RETURN TO GATE, SPOILER STAB FAULT, RUDDER LIMIT FAULT. MX PURGED MOISTURE FROM STANDBY STATIC SYSTEM. OPS CHECK GOOD. NO PARTS REPLACED. ACFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20050630000232005063000023NM 2005 6 30 QXEA200501038 120050611A33506104781 BATTERY PACK DHAV DHC8 DHC8202 2809007NM EMERGENCY LIGHTSINOPERATIVE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09362PH677 177 518 FORWARD STRIP OF EMERGENCY FLOOR STRIP LIGHTING, AFT 2 RED LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK AT PS6. OPS CHECK GOOD. ACFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050630000242005063000024EU 2005 6 30 UPS05144691 120050612A3350 BULB AIRBUSA300 A300F4622R 3930360EU EMERGENCY LIGHTSINOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01130UP 0814 2 EMERGENCY EXIT SIGN BULBS ARE INOP INSIDE AND UNDER AND AFT. RELAMPED, OPS CHECK NORMAL. 2L72 4F RTA35EU 20050630000262005063000026NM 2005 6 30 DHL2005741545 120050413A5542 PANEL BOEING727 7272Q9 138448MNM RUDDER DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 RUDDER STA 0.00 RT TRAPEZOIDAL PANEL HAS 10 DENTS. MEASURED 10 EA DENTS ON RT TRAPEZOIDAL PANEL. A/Y RATIO OF 9 DENTS WITH-IN LIMITS. A/Y RATIO OF 1 DENT OUT-OF-LIMITS. CLEANED, PREPPED, APPLIED POTTING COMPOUND TO DENT, CURED AND SANDED SMOOTH. FABRICATED DOUBLER APPROX 3 INCHES DIA FROM 2024-T3 .020 PO NR 9912281. CLEANED, PREPPED, APPLIED ADHESIVE PRIMER, BONDED, CLEANED, TREATED, SEALED EDGES AND PRIMED IAW B727 SRM 55-30-1 FIG 2 AND 51-40-22 FIG 1. 2L73 4F RTA3WE 20050630000272005063000027NM 2005 6 30 DHL2005741546 120050414A575465173273 RIB BOEING727 727227 1384078NM NR 1 SLAT CHAFED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01784DH 21931 NR 1 SLAT ACTUATOR ROD END BOLT CHAFING AGAINST I/B SLAT RIB. REMOVED DAMAGED I/B RIB IAW B727 SRM 51-30-2. DRILLED, TREATED, PRIMED RIB AND AREA IAW B727 SRM 51-30-2 AND 51-10-2. INSTALLED I/B RIB IAW B727 SRM 51-30-2 PO 5096329 P/N 65-17327-3. 2L73 4F A3WE 20050630000282005063000028EA 2005 6 30 ASOA05386 120050429A2612601R5790011 FIRE LOOP CNDAIRCL600 CL6002B19 1900309EA RT ENGINE DEFECTIVE A ASOAK NONE N FALSE WARNING CRCRUISE 1 SO27836AS 7263 DURING CRUISE, CREW RECEIVED RT ENGINE FIRE FAIL CAUTION MESSAGE WARNING. WHEN COMPLYING WITH THE QRH, FIRE LOOP-A WAS SELECTED AND FIRE WARNING RECEIVED. QRH COMPLIED WITH AND LOOP-B SELECTED. ACFT LANDED SAFELY. MX CLEARED DEFERRED FIRE LOOP BY REMOVING AND REPLACING RT ENGINE FIRE LOOP-A. OPS CHECKS GOOD. ACFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050630000292005063000029SO 2005 6 30 SIMA200512502 120050426A532014522178005 SILL EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21808AE 145519 SERVICE DOOR CENTER SILL FOUND CORRODED. BLENDED CORROSION OUT. FABRICATED 2 DOUBLERS. REPAIR DONE IAW EMB IC2005-145/2057, DATED APRIL 25, 2005. (M) 2L72 4F RTT00011AT 20050630000312005063000031SO 2005 6 30 SIMA200512503 120050424A532014521713005 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21808AE 145519 CENTER HAT BEAM AT FRAME 20 FOUND TO BE CORRODED. REMOVED CORRODED CENTER HAT BEAM AND INSTALLED SERVICEABLE BEAM. REPAIR DONE IAW EMB SRM 145/1142 REV 28, CHAPTER 51-40-02. (M) 2L72 4F RTT00011AT 20050630000332005063000033SO 2005 6 30 SIMA200513601 120050510A21502152403 ACM EMB 135 EMB135LR 3260305SO NR 1 SMOKE A SIMAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW21705AE 145184 CREW REPORTED BURNING ODOR IN BOTH COCKPIT AND CABIN. REAR OF ACFT HAD SMALL AMOUNT OF SMOKE VISIBLE. MEL WAS ISSUED AND ACFT RETURNED TO SERVICE. MX REMOVED AND REPLACED NR 1 ACM IAW EMB MM. OPS CHECK GOOD. ACFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050630000342005063000034NM 2005 6 30 QXEA200501033 120050610A5270301450301 PROXIMITY SENSOR BOMBDRDHC8 DHC8402 1390042NM CARGO DOOR MALFUNCTIONED A QXEAO OTHER N FALSE WARNING CLCLIMB 1 NM09407QX3073 4049 REAR BAGGAGE DOOR WARNING LIGHT ILLUMINATED DURING CLIMB-OUT. LIGHT CYCLED ON AND OFF SEVERAL TIMES DURING DESCENT. REMOVED AND REPLACED PROX SENSOR UNIT. OPS CHECK GOOD. ACFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050630000372005063000037NM 2005 6 30 DHL2005741557 120050415A5311 FRAME BOEING727 7272Q9 138448MNM FUSELAGE BENT A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 AFT CARGO STA 1050 AT STR 24 RT FRAME BENT. FRAME OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 1 CUT OUT DAMAGED AREA AND FABRICATED REPAIR DOUBLER IAW B727 SRM 51-40-3 FIG 1 AND MAT ID 53-10-2. PARTS TREATED AND PRIMED IAW B727 51-10-2. INSTALLED REPAIR DOUBLER IAW B727 SRM 51-30-2 AND 51-40-3 FIG 1. 2L73 4F RTA3WE 20050630000382005063000038NM 2005 6 30 DHL2005741558 120050419A5753 SKIN BOEING727 7272Q9 138448MNM RT INBOARD FLAP CHAFED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 RT I/B FORFLAP CHAFED AT UPPER I/B END. REMOVED CHAFFED EXISTING DOUBLER FROM RT I/B FORE FLAP UPPER I/B END, CLEANED, PREPPED, APPLIED ADHESIVE PRIMER, BONDED, CLEANED, TREATED, PRIMED AND SEALED EDGE IAW B727 SRM 57-50-1 FIG 3 57-50-2 FIG3 AND 51-40-20 FIG 30. 2L73 4F RTA3WE 20050630000392005063000039NM 2005 6 30 DHL2005741559 120050420A5330 SKIN BOEING727 7272Q9 138448MNM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 FOUND DENT ON RT FUSELAGE STA 1193 BELOW STR 18 MARKED NR 5. EVALUATED DENTS AT B/S 1185, 1188, 1190, 1193 FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-30-1 (1). CUT OUT DAMAGED AREA (4EA) IAW B727 SRM 53-30-3 FIG (3A). FAB DOUBLER IAW B727 SRM 53-30-3 FIG (3A) AND 53-30-2 FIG (3). TREATED AND PRIMED AREA AND DOUBLER REPAIR IAW B727 SRM 51-10-2. INSTALLED DOUBLER REPAIR AT RT FS 1183 BELOW STR 18 IAW B727 SRM SRM 53-30-3 FIG (3A). 2L73 4F RTA3WE 20050630000402005063000040NM 2005 6 30 DHL2005741560 120050420A5330 SKIN BOEING727 7272Q9 138448MNM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 FOUND DENT ON RT FUSELAGE STA 1335 BELOW STR 23 MARKED NR 45. DENT EVAL AT BS 1335 AND A/Y RATIO IA OUT OF LIMITS IAW B727 SRM 53-30-1 FIG 1 DENT AT 1329 IS OUT OF LIMITS PER 97566. CUT OUT DAMAGE AT BS 1329 AND AT BS 1335 IAW B727 SRM 53-30-3 FIG 1. FABRICATED DOUBLER 2024-T3 063. PO NR 9002268 IAW B727 SRM 53-30-3 FIG 1. TREATED AND PRIMED AREA AND DOUBLER IAW B727 SRM 51-10-2. INSTALLED DOUBLER 1335 IAW B727 SRM 53-30-3 FIG 1. 2L73 4F RTA3WE 20050630000412005063000041NM 2005 6 30 DHL2005741561 120050420A5330 SKIN BOEING727 7272Q9 138448MNM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 FUSELAGE SKIN CRACKED AT STA 1210 AFT OF TAILSKID AT CUT OUT. TRIMMED OUT CRACKED AREA OF SKIN AND FABRICATED DOUBLER IAW B727 SRM 53-30-2 FIG 1 AND 51-40-2 FIG 1. TREATED AND PRIMED DOUBLER AND AREA IAW B727 SRM 51-10-2. INSTALLED DOUBLER IAW B727 SRM 51-40-2 FIG 1. 2L73 4F RTA3WE 20050630000422005063000042NM 2005 6 30 DHL2005741562 120050421A555465624353 HINGE FITTING BOEING727 7272Q9 138448MNM RUDDER TAB LOOSE A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 LOWER RUDDER TAB UPPER HINGE ATTACH HAS PLAY AT BEARING. REMOVED AND REPLACED FITTING ASSY PN 65-62435-3 PO NR 5096142, 3EA HINGE ASSY PN 69-49678-1 PO NR 5096115, AND HINGE ASSY PN65-16792-1 PO NR 5096116 5EA IAW 727 SRM 51-30-2 LWR RUDDER TAB REMOVED FOR ACCESS AND REINSTALLED IAW 727 MM 27-20-11. 2L73 4F RTA3WE 20050630000442005063000044NM 2005 6 30 DHL2005741564 120050421A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 FOUND RT FUSELAGE BS 180 BELOW STR 26 IS DENTED. REMOVED FASTENERS IN AREA FOR DAMAGE ACCESS. CUT OUT DAMAGED AREA IAW B727 SRM 51-30-2 FIG 7 AND 53-30-3 FIG 24. FABBED FILLER IAW B727 SRM 53-30-3 (FIG 24). TREATED AND PRIMED AREA AND PARTS IAW B7272 SRM 51-10-2. INSTALLED DOUBLER REPAIR IAW B727 SRM 53-30-3 FIG 24. 2L73 4F RTA3WE 20050630000452005063000045NM 2005 6 30 DHL2005741566 120050421A5330 DOUBLER BOEING727 7272Q9 138448MNM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 FOUND FUSELAGE BS 1110 AND 1130 AT STR 18 RT HAS DOUBLER WITH 2 EA DENTS. REMOVED EXISTING DOUBLER AT BS 1110 AND 1130 STR 18R IAW B727 SRM 51-30-2. FABRICATED DOUBLER IAW B727 SRM 53-30-3 FIG 3 AND 53-30-2 FIG 1. TREATED AND PRIMED DOUBLER AND AREA IAW B727 SRM 51-10-2. INSTALLED DOUBLER IAW B727 SRM 53-30-3 FIG 3. 2L73 4F RTA3WE 20050630000472005063000047NE 2005 6 30 UPS05544695 220050614A7200 ENGINE BOEING757 75724APF 1384969NM RROYCERB211 RB211535E4 54555NE LEFT POWER LOSS A IPXAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SO01438UP 25469 113398 LOSS OF POWER LT ENGINE. LT ENG HIGH EGT AND EPR INDICATION. 2L72 4F4 FRTA2NM E12EU 20050630000492005063000049WP 2005 6 30 UPS05844697 120050525A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CHAFED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 RT CENTER WING L/E RIB CHAFED THROUGH AROUND PNEUMATIC DUCT SUPPORT ROD CONNECTION AT XFS 513. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57 -2-0 FIG 2 AND 51-1-20D. 2L74 4F RT4A25 20050630000512005063000051WP 2005 6 30 UPS05844700 120050601A5712 RIB DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 LT WING CENTER L/E AT XFS 335 RIB CRACKED ON L/E LOWER SURFACE. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2 -0 FIG 2, 51-1-20D, AND 51-1-21. 2L74 4F RT4A25 20050630000542005063000054WP 2005 6 30 UPS05844704 120050522A5312 BULKHEAD DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 FWD ACCESSORY COMPARTMENT 680 BULKHEAD HAS CRACKS IN 4 PLACES. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53 -2-5 FIG 13, 51-1-20D, AND 51-1-21. 2L74 4F RT4A25 20050630000552005063000055WP 2005 6 30 UPS05844705 120050527A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 CRACK APPROX 3 INCHES LONG ON LONGERON 35R AT FS 1270. REMOVED DAMAGED SECTION OF LONGERON. FABRICATED AND INSTALLED REPLACEMENT SECTION OF LONGERON IAW DC-8 SRM 51-1-20D AND DWG'S 3758593 AND 575 0322. 2L74 4F RT4A25 20050630000562005063000056SO 2005 6 30 SIMA200515104 120050525A532014525480003 SILL EMB 135 EMB135KL 3260302SO CARGO BAY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21812AE 145531 CARGO DOOR LOWER CUT OUT FLOOR SILL WAS FOUND TO BE CORRODED. REMOVED CORRODED SILL AND INSTALLED NEW SILL. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 29 CHAPTER 51-40-02. (M) 2L72 4F RTT00011AT 20050630000572005063000057NM 2005 6 30 P5CA0501364 120050531A575465B151782 PANEL BOEING747 747230B 1384889NM WING BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 EA15508MC 21644 NR 22 LEADING EDGE PANEL BROKEN. REPLACED NR 22 LEADING EDGE PANEL, 2 ROTARY ACTUATORS AND TORQUE TUBE. RIGGED AND OPS CHECK PER MM 27-81-00. 2L74 4F A20WE 20050630000582005063000058NM 2005 6 30 P5CA0501365 120050531A278065B803908 TORQUE TUBE BOEING747 747230B 1384889NM WING LE DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 EA15508MC 21644 NR 22 LEADING EDGE PANEL BROKEN. REPLACED NR 22 LEADING EDGE PANEL, 2 ROTARY ACTUATORS AND TORQUE TUBE. RIGGED AND OPS CHECK PER MM 27-81-00. 2L74 4F A20WE 20050630000602005063000060SO 2005 6 30 SWIA200515137 120050610A27503472001001 CONTROL UNIT EMB 120 EMB120ER 3260203SO TE FLAP MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07251YV1168011680 120251 FLAP DISAGREEMENT FROM FLAP 25 DEGREES TO 45 DEGREES. REPLACED FLAP CONTROL UNIT IAW MM 27-50-06. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050630000612005063000061EA 2005 6 30 SWIA200515138 120050608A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSDISCONNECTED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07426SW 7468 EMERGENCY LIGHTS NOT WORKING. RECONNECTED AFT SECTION OF LIGHTING. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050630000642005063000064SO 2005 6 30 SWIA200515141 120050610A2121AE1711AA0 COOLING FAN EMB 120 EMB120ER 3260203SO LT A/C PACK FAILED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM07251YV1169311693 120251 LT PACK BLOWS SMOKE INTO CABIN AND GENERATES A PACK FAIL LIGHT ON GROUND. REPLACED LT GROUND COOLING FAN IAW 21-51-03. OPS CHECK GOOD. 2L72 4T RTA31SO 20050630000652005063000065EA 2005 6 30 MASA200500069 120050129A5270 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR UNKNOWN A MASAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW0777195 7195 RETURNED TO FIELD DUE TO PASSENGER DOOR OUTER HANDLE CAUTION MESSAGE ILLUMINATED. MAINTENANCE COMPLIED WITH MEL PROCEDURES. 1/29 - MAINTENANCE PERFORMED NUMEROUS OPS CHECKS AND NO DEFECTS NOTED. 2L72 4F RTA21EA 20050630000662005063000066EA 2005 6 30 MASA200500075 120050131A3260 SQUAT SWITCH CNDAIRCL600 CL6002B19 1900309EA NLG DOOR BENT A MASAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW0775993 7372 RETURNED TO FIELD DUE TO NLG DOOR DISAGREE ON RETRACTION. FERRIED AIRCRAFT FOR REPAIR. 1/31/05 MAINTENANCE FOUND WOW SENSOR BENT. FIXED AND READJUSTED. OPS CHECK GOOD. 2L72 4F RTA21EA 20050630000672005063000067EA 2005 6 30 MASA200500087 120050209A2741 TRIM SYSTEM CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A MASAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SW07154SF 7154 RETURNED TO FIELD DUE TO STAB TRIM FAILURE. MX PERFORMED HSTCU FUNCTIONAL CHECK AND STAB TRIM OPS CHECK. NO FAULTS FOUND. ACFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20050630000682005063000068EA 2005 6 30 MASA200500110 120050213A3620 SHUTOFF VALVE CNDAIRCL600 CL6002B19 1900309EA PNEUMATIC SYS INOPERATIVE A MASAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW0777278 7278 RETURNED TO GATE WITH OVERBOARD COOL STATUS MESSAGE. MX INFORMED TO REMOVE AND REPLACE SHUTOFF VALVE. VALVE FOUND TO BE INOPERATIVE. WAITING PART INFO. 2/13/05 PCW WITH MEL PROCEDURE 21-24-602. 2L72 4F RTA21EA 20050630000702005063000070NM 2005 6 30 0500906638 120050604A33201TP121 SWITCH BOEING747 747251B 1384892NM GALLEY LIGHTS FAILED A NWAAO OTHER A FLAME/FIRE CRCRUISE 1 GL01638US 23549 DURING FLIGHT, TWO FLIGHT ATTENDANTS IN FORWARD GALLEY NR 1 HEARD POPPING SOUND THEN SAW A FLAME OUT OF PANEL ABOVE AUX GALLEY COUNTER. TURNED OFF COUNTER LIGHT SWITCH AND PULLED CB. ACFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. NRT MX DEACTIVATED CB. NRT MX REMOVED AND REPLACED SWITCH AND RESISTOR 15JUNE05. OPS CHECKS GOOD. 2L74 4F A20WE 20050630000712005063000071EA 2005 6 30 MASA200500134 120050219A2120 SMOKE CNDAIRCL600 CL6002B19 1900309EA CABIN DETECTED A MASAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION APAPPROACH 1 SW0775996 7357 ON APPROACH, LAVATORY SMOKE CAUTION APPEARED ON EICAS AFTER TRANSFERING BLEEDS FROM ENGINE TO APU. FLIGHT ATTENDENT ALSO REPORTED SMOKE IN CABIN AFT OF ROW 10. INSP LAVATORY FIRE DETECTOR AND FOUND IT HAD NOT DISCHARGED. PERFORMED OPERATIONAL TEST OF APU AND ACM. NO OTHER DEFECTS NOTED, ACFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20050630000722005063000072EA 2005 6 30 MASA200500151 120050223A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A MASAA UNSCHED LANDING JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 SW0737218 7218 ON APPROACH FLAPS FAIL AT 8 DEGREES. A/C DIVERTED TO LAX AND LANDED UNEVENTFULLY. MAINTENANCE C/W PART A IN LAX AND REPOSITIONED TO PHX FOR PART B. 2L72 4F RTA21EA 20050630000732005063000073NE 2005 6 30 MASA200500167 220050301A7261 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 2 LEAKING A MASAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW07591ML 7388 872692 EMERGENCY DECLARED. SHUTDOWN NR 2 ENGINE AND DIVERTED TO IAD DUE TO LOSS OF OIL PRESSURE. MX IS IN THE PROCESS OF TROUBLESHOOTING. 2L72 4F4 FRTA21EA E15NE 20050630000742005063000074EA 2005 6 30 MASA200500171 120050303A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A MASAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW0797325 7325 RTG FOR FLAP FAIL CAUTION MESSAGE. MAINTENANCE COMPLIED WITH PART A INSP. 2L72 4F RTA21EA 20050630000762005063000076EA 2005 6 30 MASA200500194 120050308A27603995100208 ECU CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07592ML4765 7410 ABORTED TAKEOFF DUE TO STALL FAIL AND SPOILER CONFIG WARNING. MAINTENANCE REPLACED SPS COMPUTER AND SPOILER ELECTRONIC CONTROL UNIT. SPOILER ECU P/N 49-164-05 S/N OFF 0371 NR 2 POSITION. 2L72 4F RTA21EA 20050630000772005063000077EA 2005 6 30 MASA200500205 120050311A5280 DOOR CNDAIRCL600 CL6002B19 1900309EA NLG OBSTRUCTED A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0727185 7185 PILOT RETURNED TO FIELD WHEN NLG DOOR LIGHT ILLUMINATED AFTER RETRACTION. GEAR WAS EXTENDED NORMALLY AND PERFORMED A SAFE LANDING. MX REMOVED EXCESSIVE AMOUNT OF SLUSH AND ICE FROM NLG DOOR. DOORS WERE CYCLED AND ALL COMPONENTS INSP WITH NO DEFECTS FOUND. ACFT SUCESSFULLY TEST FLOWN AND PLACED BACK INTO SERVICE. 2L72 4F RTA21EA 20050630000782005063000078EA 2005 6 30 MASA200500213 120050313A2611PU90421R3 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA LAVATORY MALFUNCTIONED A MASAO OTHER N FALSE WARNING CRCRUISE 1 SW0775996 7357 CAPT GOT SMOKE TOILET MSG APPROX 5 MIN PRIOR TO DESCENT. F/O WENT TO LAVATORY AND VERIFIED NO SMOKE OR FIRE. CREW COMPLIED WITH FIM PROCEDURES. REPLACED SMOKE DETECTOR. 2L72 4F RTA21EA 20050630000832005063000083EA 2005 6 30 MASA200500270 120050403A3260 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA MLG ILLUMINATED A MASAO OTHER J WARNING INDICATION CRCRUISE 1 SW0737208 7208 CREW REPORTED GEAR DISAGREE IN FLIGHT. CREW DECLARED EMERGENCY LANDING. LANDED UNEVENTFULLY. MX IN PROCESS OF TROUBLESHOOTING PROBLEM. 2L72 4F RTA21EA 20050630000842005063000084EA 2005 6 30 MASA200500271 120050403A2760 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07591ML 7388 REJECTED TAKEOFF FOR SPOILER CONFIG MESSAGE ON EICAS AT 70 KTS. MESSAGE CLEARED AT 80 KTS. MX INSP MDC FOR FAULTS. NONE NOTED. MX RESET SPOILER CONTROL SYSTEM AND PERFORMED OPS CHECK. SYSTEM OPERATED NORMALLY. 2L72 4F RTA21EA 20050630000852005063000085EA 2005 6 30 MASA200500283 120050405A2760 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA SPOILERS ILLUMINATED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07154SF 7154 CAPTAIN REJECTED TAKEOFF DUE TO CONFIG SPOILER MESSAGE AND RETURNED TO GATE. MX PERFORMED HIGH ENERGY STOP/REJECTED TAKEOFF INSP. NO DEFECTS NOTED. CREW AND MX PERFORMED HIGH SPEED TAXI OF A/C. NO DEFECTS NOTED. 2L72 4F RTA21EA 20050630000872005063000087EA 2005 6 30 MASA200500313 120050424A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA MAIN PAX INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0727172 7172 CREW NOTED THAT PASSENGER DOOR WOULD NOT OPEN FROM INSIDE OF ACFT. MX COMPLIED WITH PERMANENT REPAIR. 2L72 4F RTA21EA 20050628001302005062800130EA 2005 6 28 ASOA05477 120050526A3350BA670406071 LIGHT CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE CABIN DAMAGED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27701EV 10020 DURING A C-CHECK, THE EMERGENCY FLOOR LIGHT TRACKS WERE FOUND TO BE DAMAGED IN SEVERAL PLACES THROUGH OUT THE CABIN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT ASSEMBLIES THROUGH OUT THE CABIN. (K) 2L72 4F4 FRTA21EA EOOO63EN 20050628001432005062800143EA 2005 6 28 ASOA05471 120050510A5310 FRAME CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27829AS 7232 DURING A C-CHECK, THE PASSENGER DOOR AFT FRAME AT FS 338.90 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE PASSENGER DOOR AFT FRAME AT FS 338.90 IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050628001532005062800153EA 2005 6 28 ASOA05360 120050413A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27821AS 7194 DURING A C-CHECK, THE NOSE LANDING GEAR WHEEL WELL AFT CUT OUT ON THE LT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTNANCE IS REPAIRING THE NOSE LANDING GEAR WHEEL WELL FUSELAGE SKIN RADIUS LT AT FS 235 IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050628001572005062800157EA 2005 6 28 ASOA05388 120050501A5210601R3807423 ANCHOR FITTING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27882AS 7503 DURING HANGAR MAINTENANCE, THE FORWARD ANCHOR FITTING ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVE AND REPLACED THE FORWARD ANCHOR FITTING ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050628001632005062800163WP 2005 6 28 ASAA0580159 120050301A575459359525 SKIN DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE RT LE FLAP CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 HV - CHECK - RT IB FLAP L/E PANEL IS CHAFED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER. (K) 2L72 4F4 FRTA6WE E9NE 20050628001702005062800170SO 2005 6 28 GUU2005F00025 120050604A2120 ODOR EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE CABIN DETECTED A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO29280AS 120231 DURING FLIGHT, OIL SMELL ODOR WITH A FOG APPEARANCE IN COCKPIT WITH ENGINE BLEEDS ON. RETURNED TO DEPARTURE. INSPECTED AIRCRAFT, DO DISCREPANCIES FOUND. RAN ENGINE. OPERATIONAL CHECKS NORMAL. (K) 2L72 4T4 TRTA31SO E20NE 20050628001722005062800172WP 2005 6 28 ASAA0580172 120050307A575359100413 VANE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE TE FLAP WORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 HV-CHECK - LT IB FLAP IB VANE IS WORN AT LEADING EDGE. INSTALLED REPAIR DOUBLER. (K) 2L72 4F4 FRTA6WE E9NE 20050628001762005062800176CE 2005 6 28 GUU2005F00021 120050604A3240 RESERVOIR BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA LT BRAKE LOW A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO2982539 UE168 LT BRAKE INOPERATIVE. FOUND BRAKE RESERVOIR LOW. SERVICED RESERVOIR. BLED LT BRAKE ASSEMBLY. (K) 2L72 4T3 TRTA24CE E2NE 20050628001812005062800181EA 2005 6 28 ASOA05487 120050604A2613472698 CIRCUIT CARD CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE OVERHEAT LOOP MALFUNCTIONED A ASOAF ACTIVATE FIRE EXT. N FALSE WARNING DEDESCENT 1 SO27833AS 7246 DURING DESCENT, THE CREW RECEIVED AN AUXILIARY POWER UNIT (APU) OVERTEMP MESSAGE. DURING COMPLIANCE WITH THE QRH, AN APU FIRE WARNING WAS RECEIVED AT WHICH TIME THE CREW DISCHARGED THE APU FIRE BOTTLE FOLLOWED BY ALL INDICATIONS GOING AWAY. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY. UPON LANDING, THE AC WAS INSPECTED BY THE FIRE CREW WITH NO EVIDENCE OF A FIRE, FOUND; THEN PROCEEDED TO THE GATE SAFELY. UPON INSPECTION OF THE AIRCRAFT BY MAINTENANCE, NO EVIDENCE OF A FIRE, FUEL OR OIL LEAKS WERE FOUND. MAINTENANCE REMOVED AND REPLACED THE APU FIRE AND OVERHEAT CONTROL CARD NR 3 AND THE APU FIRE BOTTLE. OPS CHECK GOOD. AC OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050629000062005062900006NE 2005 6 29 ILD2005F00000 220050510A7310 MANIFOLD SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE FUEL INJECTION DAMAGED E ILDAO OTHER O OTHER NRNOT REPORTED 1 WP13451H 3231 ON THE FIRST FLIGHT, ENGINE COULDN`T START DUE TO FUEL COKING AT GENERATOR INJECTION MAINIFOLD (MODULE 3 COMBINATION) INJECTION MANIFOLD WAS REMOVED AND REPLACED WITH SERVICEABLE INJECTION MAINIFOLD. AC RETURNED TO SERVICE AFTER RUN UP LEAK CHECK AND OPERATION. CHECK FLIGHT. (K) 1G71 3U3 U H9EU E19EU 20050629000202005062900020EA 2005 6 29 ASOA05494 120050602A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27850AS 7355 DURING C-CHECK, THE ANGLE IB OF LBL 9 AT FS 280 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE ANGLE IB OF LBL 9 AT FS 280 IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050629000222005062900022CE 2005 6 29 GUU2005F00019 120050528A3240 BRAKE BEECH 1900 1900D 1154162CE LEFT UNRESPONSIVE A GUUAK NONE O OTHER ININSP/MAINT 1 SO1787552 UE216 LT TOE BRAKE DOES NOT WORK. HAVE TO PUMP UP PRESSURE. BLED LT BRAKE SYSTEM. OPS CHECK NORMAL. (K) 2L72 4T RTA24CE 20050629000562005062900056EA 2005 6 29 ASOA05398 120050503A5210 MECHANISM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR CONTAMINATED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27860AS 7433 DURING A GROUND INSPECTION, THE PASSENGER DOOR WOULD NOT CLOSE AND A PASSENGER DOOR LATCH CAUTION MESSAGE WAS RECEIVED. MAINTENANCE REMOVED SAND AND GRIT FROM ALL THE ROLLING COMPONENTS ON THE PASSENGER DOOR AND CHECKED THE ADJUSTMENT ON THE LINKAGES. MAINTENANCE ALSO CLEANED ALL THE MOVING PARTS WITH NO DEFECTS NOTED. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050629000662005062900066EA 2005 6 29 ASOA05482 120050601A5320 THRESHOLD CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27850AS 7355 DURING A C-CHECK, THE CARGO COMPARTMENT THRESHOLD PLATE WAS FOUND TO BE CRACKED AT THE THRESHOLD COVER FORWARD LATCH BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO COMPARTMENT THRESHOLD PLATE AT FS 562.72 TO FS589.00 IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050629000802005062900080NM 2005 6 29 SWAA051875 120050627A53116546539 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CHORD CRACKED AT BS 639, STR 17L, WL 210. REPAIRED FRAME CHORD PER SRM. 2L72 4F RTA16WE 20050629000822005062900082NM 2005 6 29 SWAA051877 120050627A53116546539 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME UPPER STRUCTURE IS CRACKED AT BS 663, STR 1L TO STR 3L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050629000832005062900083NM 2005 6 29 SWAA051879 120050627A335010107451 SIGN BOEING737 7373H4 1384600NM EMERGENCY EXIT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29326SW 23690 FWD ENTRY EMERGENCY EXIT SIGN BROKEN. REPAIRED SIGN PER MM. 2L72 4F RTA16WE 20050629000852005062900085NM 2005 6 29 SWAA051881 120050627A5753 SKIN BOEING737 7373H4 1384600NM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29397SW 27691 DURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REPAIRED FLAP PER SRM. 2L72 4F RTA16WE 20050629000872005062900087NM 2005 6 29 SWAA051883 120050627A575369763032 BOLT BOEING737 7373H4 1384600NM FLAP TRACK BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29639SW 27712 BROKEN BOLT AND MISSING FLAP TRACK ROLLER FOUND AT LT WING OUTBOARD T/E FLAP, OUTBOARD ROLLER. INSTALLED BOLT & ROLLER PER MM. 2L72 4F RTA16WE 20050629000952005062900095EA 2005 6 29 VNAA0506008 120050613A2750860D10018 FCU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS FAILED A VNAAO OTHER J WARNING INDICATION APAPPROACH 1 GL05241PS2551 7909 THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED WITH BOTH FLAPS AT 45 DEGRESS ON FINAL APPROACH. MAINTENANCE CYCLED THE CIRCUIT BREAKERS AND OPERATIONALLY TESTED THE FLAP SYSTEM IAW CRJ 200 AMM 27-54-00-710-801. ALL OPS CHECKS WERE GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. THE AIRCRAFT WAS REMOVED FROM SERVICE 06/13/05 DUE TO REPEAT FLAP FAIL CAUTION MESSAGES WITH FLAPS AT 45 DEGREES. THE FLAP SYSTEM WAS TROUBLESHOT IAW THE CRJ 200 FAULT ISOLATION MANUAL. RECURRENT FLAP ELECTRONIC CONTROL UNIT FAULT CODES WERE FOUND. THE FECU WAS REMOVED & REPLACED IAW CRJ200 AMM 27-51-05-000-(400)-801. RIG, FUNCTIONAL TEST, AND OPERATIONAL TESTS WERE GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050630000072005063000007EA 2005 6 30 QXEA200500993 120050511A5230 RETAINER CNDAIRCL600 CL6002C10 1390015EA CARGO DOOR SEAL BENT A QXEAK NONE O OTHER ININSP/MAINT 1 NM09616QX 10128 FORWARD BAGGAGE BAY DOOR OUTER SEAL RETAINER BENT AT 2 LOCATIONS AND GOUGED AT 2 ALONG LOWER EDGE OF DOOR. REPAIRED IAW CRJ 700 SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050630000302005063000030NM 2005 6 30 DHL2005784548 120050518A5534 WEB BOEING727 727227 1384078NM VERTICAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01784DH 22001 FOUND VERTICAL STAB SLANT WEB AT 1303 LOWER RIGHT CORNER CRACKED STA 1303, FRAME SECTION ABOVE CENTER INLET DUCT. COMPLIED WITH COTNEY AEROSPACE EA: EAZ04-1 REV : A, 8110-3 DATED 6/8/05. STOP DRILLED CRACK ON VERT STAB WEB BS 1303 RBL 22 IAW 727 SRM 51-10-1 AND S/B 727-53-0094. 2L73 4F A3WE 20050630000322005063000032SO 2005 6 30 SIMA200512505 120050425A5320 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO FUSELAGE DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21808AE 145519 CENTER OMEGA BEAM AT FRAME 27 WAS FOUND TO HAVE ELONGATED HOLE IN AN EXISTING REPAIR. REMOVED EXISTING REPAIR AND FABRICATED NEW REPAIR DOUBLER. REPAIR DONE IAW EMB IC2005-145/2057 DATED APRIL 22, 2005. (M) 2L72 4F RTT00011AT 20050630000362005063000036EA 2005 6 30 SWIA200515128 120050612A3220 LANDING GEAR CNDAIRCL600 CL6002B19 1900309EA NOSE MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION LDLANDING 1 NM07960SW 7853 NLG DISAGREE ON APPROACH. RETURNED. NLG WOULD NOT COME DOWN WITH EMERGENCY EXTEND. ACFT LANDED WITH NOSE GEAR UP. 2L72 4F RTA21EA 20050630000532005063000053WP 2005 6 30 UPS05844703 120050527A53103755847U501 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 CRACKED FITTING ON TORQUE BOX AT CARGO DOOR AT FS 1160 BETWEEN L31 AND L32 R. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20050630000622005063000062EA 2005 6 30 SWIA200515139 120050612A2740 COMPUTER CNDAIRCL600 CL6002B19 1900309EA STAB CONTROL MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07948SW 7789 STAB CH 1 INOPERATIVE. REPLACED HSTCU COMPUTER IAW CRJ MM 27-41-01. REPLACED MCU AND HSTA IAW 27-42-01 AND 27-42-05. OPS CHECK GOOD, PN: 7060-9, SN OFF: 1117 PN: 8396-3, SN OFF: 382, PN: 7062-3, SN OFF: 942. 2L72 4F RTA21EA 20050630000632005063000063EA 2005 6 30 SWIA200515140 120050607A274070609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB CONTROL MALFUNCTIONED A SWIAO OTHER OJ OTHER WARNING INDICATION NRNOT REPORTED 1 NM07925SW 7682 STAB CH NR 1 STATUS MESSAGE. REPLACED HSTCU IAW MM 27-40-00. OPS CHECK GOOD. 2L72 4F RTA21EA 20050630000692005063000069EA 2005 6 30 MASA200500112 120050214A284173664310 COMPUTER CNDAIRCL600 CL6002B19 1900309EA FUEL QTY SYS MALFUNCTIONED A MASAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW07472029691 7202 RETURNED TO FIELD DUE TO THE LT WING FUEL TANK QUANTITY INDICATION ERRATIC. MAINTENANCE WILL EITHER CHANGE THE FUEL COMPUTER OR COMPLY WITH MEL PROCEDURES. MAINTENANCE REMOVED AND REPLACED FUEL COMPUTER. 2L72 4F RTA21EA 20050630000752005063000075 2005 6 30 MASA200500192 420050307A3418 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA STALL WARNING ACTIVATED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07592ML 7410 ABORTED TAKEOFF BECAUSE OF STALL FAIL ON TAKEOFF ROLL. MSG CLEARED AS ACFT SLOWED. ALSO RECEIVED GROUND SPOILER FAIL EICAS MESSAGE. PERFORMED FUNCTIONAL CHECK OF STALL PROTECTION AND SPOILER CONTROL SYSTEMS. NO FURTHER DEFECTS WERE NOTED. 2L72 4F RTA21EA 20050630000792005063000079EA 2005 6 30 MASA200500249 120050323A2611 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA LAVATORY ILLUMINATED A MASAO OTHER J WARNING INDICATION CRCRUISE 1 SW0775996 7357 LAVATORY SMOKE WARNING IN FLIGHT. ACFT LANDED AND MAINTENANCE WORKED DISCREPANCY. OPS CHECK. NO DEFECTS NOTED. 2L72 4F RTA21EA 20050630000812005063000081EA 2005 6 30 MASA200500258 120050326A5210 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A MASAO OTHER O OTHER TXTAXI/GRND HDL 1 SW0775992 7401 MAIN PAX DOOR HANDLE BROKE. ACFT FERRIED WHERE MX REPAIRED DOOR HANDLE AND ACFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20050630000892005063000089EA 2005 6 30 MASA200500344 120050509A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA MAIN PAX UNKNOWN A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0777195 7195 CREW REPORTED DIFFICULTY OPENING PAX DOOR. MX COULD NOT DUPLICATE DISCREPANCY. 2L72 4F RTA21EA 20050630000902005063000090EA 2005 6 30 MASA200500346 120050510A5210 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR LACK OF LUBE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0747239 7239 CREW REPORTED PASSENGER DOOR STOW HANDLE HARD TO PULL OUT AND STOW. MX LUBED HANDLE. 2L72 4F RTA21EA 20050630000932005063000093NE 2005 6 30 MASA200500371 220050519A7310 FILTER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUEL SYS LEAKING A MASAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 SW0777195 7195 DUE TO LOSS OF FUEL QTY AND PRESSURE, CREW SHUTDOWN NR 2 ENG AND DIVERTED TO ORF. MX CALLED OUT TO TROUBLESHOOT AND REPLACED FORWARD FILTER ASSEMBLY. 2L72 4F4 FRTA21EA E15NE 20050630000962005063000096EA 2005 6 30 MASA200500384 120050523A5210 FITTING CNDAIRCL600 CL6002B19 1900309EA PAX DOOR OUT OF ADJUST A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0737178 7178 CREW EXPERIENCED PASSENGER DOOR HARD TO OPEN. MX ADJUSTED UPPER AFT ROLLER LATCH LUG FITTING. 2L72 4F RTA21EA 20050630000972005063000097NM 2005 6 30 WRLA200597 120050614A5512 PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C04 CHECK WHILE PERFORMING INSP PER EO 02-5510-098, FOUND CORROSION IN HST LT BARREL NUT HOLE NR 28. 2L73 4F4 FRTA22WE E24NE 20050630000992005063000099WP 2005 6 30 ABXA050160 120050614A53105912285513 RETAINER DOUG DC9 DC932 3022066WP CABIN WINDOW CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 STA 598, LONGERON 10 RT, HAD CRACK AT WINDOW RETAINER. REPAIRED WINDOW RETAINER AT FS 598, LONGERON 10 RIGHT IAW DC-9 SSRM DWG K07226. 2L72 4F A6WE 20050630001002005063000100WP 2005 6 30 ABXA050159 120050614A53103914137502 RETAINER DOUG DC9 DC932 3022066WP CABIN WINDOW CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 STA 756, LONGERON 15 RIGHT, HAD CRACK AT WINDOW RETAINER. REMOVED AND REPLACED DAMAGED CLIP. FABRICATED AND INSTALLED NEW CLIP IAW DACO DWG 3914137 AND DC-9 SRM 51-30-5. 2L72 4F A6WE 20050630001012005063000101WP 2005 6 30 ABXA050161 120050614A531599581811 FLOORBEAM DOUG DC9 DC932 3022066WP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 LOWER LEG OF FLOORBEAM WAS CORRODED ON UPPER AND LOWER SURFACE AT STA 313, BUTTLINE 38 RIGHT. REPAIRED FLOORBEAM IAW DC-9 SRM 53. 2L72 4F A6WE 20050630001022005063000102WP 2005 6 30 ABXA050162 120050615A5311991125241 FRAME DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 SHEAR TIE CRACKED IN RADIUS FRAME STA 813 BETWEEN LONGERON 29 LEFT AND 30. REPAIRED SHEAR TIE IAW DC-9 SRM 53-03 AND DWG SR09530212. 2L72 4F A6WE 20050630001042005063000104WP 2005 6 30 ABXA050164 120050617A53105912995503 DOOR FRAME DOUG DC9 DC932 3022066WP CABIN CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 LEFT AFT UPPER DOOR JAMB CRACKED, EMERGENCY EXIT, IN 2 PLACES. REPAIRED LEFT AFT UPPER DOOR JAMB IAW DC-9 SRM 53-05. 2L72 4F A6WE 20050630001052005063000105SO 2005 6 30 C2XA05BT044 120050623A2150 DUCT EMB 145 EMB145ER 3260211SO NR 2 A/C PACK FAILED A C2XAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW2714933 145018 BNA/EWR---CO2882, DURING PREFLIGHT INSPECTION CREW REPORTED, SMOKE FROM VENTS, ELECTRICAL IN NATURE FROM PACK NR 2. NASHVILLE MAINTENANCE INSPECTED AIRCRAFT AND RELEASED IAW MEL NR 21-51-00/1 CATEGORY-C CONTROL NUMBER 059962. AIRCRACT ARRIVED IN EWR AND NEWARK MAINTENANCE PERFORMED OPERATIONAL CHECK OF PACK NR 2. FOUND BLOWN DUCT ON PACK NR 2 REPLACED DUCT ON NR 2 PACK IAW EMB AMM 21-51-03. RAN FOR 30 MINUTES. NO FAULTS [OR SMOKE] NOTED IAW EMB145 AMM 21-51-00. OPS CHECKED GOOD. REMOVED AIRCRAFT FROM MEL. 2L72 4F RTT00011AT 20050630001082005063000108NM 2005 6 30 MWEA050058 120050625A5297 WIRE BOEING717 717200 1383700NM EMERGENCY EXIT UNSECURE A MWEAK NONE O OTHER ININSP/MAINT 1 GL31910ME 55174 SEAT 13D EMERGENCY EXIT ROW DOOR HAS A WIRE HANGING OUT OF LOWER PANEL. RESECURED WIRE. 2L72 4F TRA6WE 20050630001102005063000110EU 2005 6 30 XN0A1240 120050625A3260 PROXIMITY SENSOR AIRBUS300 A300B4203 3930306EU MLG DIRTY A XN0AC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL23474AS 219 ON GEAR RETRACTION, LT GEAR DOOR AMBER INDICATION ON OR BOTH INDICATORS. GEAR EXTENSION NORMAL AND AMBER LIGHT EXTINGUISHED ON BOTH POSITION. INSPECTS & CHECK MAIN LAND AND GEAR DOORS & WASHING SYSTEM PER MM CH 32-12-11. CLEANED SENSORS & ELECT CONNECTION ALL TEST OK AT PROX BOX PER MM CH 32-00-00 PG 505. 2L72 4F RTA35EU 20050630001112005063000111NM 2005 6 30 C1HA200592002 120050624A2782 ACTUATOR BOEING727 727212 138407GNM NR 6 SLAT FAILED A C1HAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15292AS 21458 ON DEPARTURE THE NR 6 L/E FAILED TO RETRACT, COMPLIED WITH COM PROCEDURE 2.27.12 SLAT WAS STILL EXTENDED. CONFERRED WITH DISPATCH/MDC, DECLARED AN EMERGENCY. COMPLIED WITH COM PROCEDURE 2.28.4 AND DUMPED APPROXIMATELY 23K LBS FUEL BEFORE RETURN TO STL. REMOVED AND REPLACED NR 6 L/E SLAT ACTUATOR IAW 27-81-32, ALL OPS NORMAL IAW 27-81-00. SERVICED HYDRAULICS TO FULL IAW 12-12-00. 2L73 4F A3WE 20050701000022005070100002EU 2005 7 1 BMAC050008 120050619A2121SZ670031 BLOWER BAG JETSTMJETSTM3101 1500215EU CABIN BURNED A B16AO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 NE05525PA 666 SMOKE IN COCKPIT. DURING TROUBLESHOOTING MAINTENANCE FOUND AC BLOWER BURNED OUT. 2L72 4T RTA21EU 20050701000042005070100004NM 2005 7 1 P5CA0501367 120050624A3610 VALVE BOEING747 747341 13848AMNM GE CF6 CF650E2 30018NE NR 1 ENGINE STUCK A P5CAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA15355MC 23395 528105 ON TAKEOFF NR 1 ENGINE A-FIRE LOOP WENT TO 4.0. B-FIRE LOOP WENT TO 5.0 AND STAYED THERE UNTIL THROTTLES WERE RETARDED FOR DESCENT. FOUND NR 1 ENGINE HIGH STAGE VALVE STUCK OPEN, LOCKED CLOSED, OPENED MEL 36-01-3B. 2L74 4F4 FRTA20WE E23EA 20050701000072005070100007CE 2005 7 1 RTE2005F00001 120050404A8011CC150A CLUTCH CESSNA150 150M 2071830CE CONT O200 O200A 17020SO STARTER CRACKED E RTEAO OTHER O OTHER NRNOT REPORTED 1 NM019198U1556 15078149 254381SO DURING 100 HOUR INSPECTION ROUTINE MAINTENANCE OF THE STARTER DRIVE CLUTCH, INSTALLED UNDER STC NR SE995GL DATED 08 SEPT 86, FOUND BEARING RACE CRACKED AND SEVERAL ROLLERS LOOSE ENOUGH TO FALL OUT OF THE RACE. THIS ITEM REQUIRES DISASSEMBLY, CLEANING AND LUBRICATION AT 100 HOUR INTERVALS, WHICH IT HAS HAD. CAUSE AND PREVENTATIVE ACTIONS UNKNOWN. POSSIBLY MFG DEFECT? (K) 1H71 3O3 O 3A19 E252 20050701000132005070100013NM 2005 7 1 P5CA0501368 120050622A5312 PRESSURE PANEL BOEING747 747230B 1384889NM NLG WW CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 EA15509MC 21221 NOSE WHEEL WELL WEB AT STATION BS 400 STR 47R FOUND CRACKED AT RETRACT ACTUATOR CUTOUT. NOSE WHEEL WELL WEB REPAIRED AS PER BOEING MESSAGE 1-1MCB8E AND FAA FORM 8100-9. 2L74 4F A20WE 20050701000152005070100015GL 2005 7 1 C2XA05IA080 220050614A723023073717 COMPRESSOR EMB 145 EMB145XR 3260214SO ALLSN AE300 AE3007A GL NR 1 ENGINE FRACTURED A C2XAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 SW27211445230 5230 145741 CAE312433 TUL - FLIGHT 2723, DURING CRUISE AT FLIGHT LEVEL 350, THE CREW REPORTED A NUMBER ONE ENGINE FAILURE. THE AIRCRAFT DIVERTED TO TUL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRT TE6CH 20050701000162005070100016NM 2005 7 1 UPS05244735 120050607A5330 LAP JOINT BOEING727 72731C 1384011NM FUSLEAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 INSPECTION TYPE:C SUSPECT CORROSION AT LAP JOINT S19R BETWEEN BS 390 AND 441 AREA BETWEEN BS 390 AND 441 PAINT STRIPPED IAW MM 51-20-01. AREA REINSPECTED, COROSION FOUND EVIDENT CONTINUE OPEN UP AND REPAIR IAW APPX C OF EO B727-5330-0509. REMOVED CORROSION IAW SRM 51-10-06 AND FOUND OUT OF LIMITS IAW SRM 53-30-01. UPPER LAP SKIN CUT AT BS 390-441 IAW SRM 53-30-03. LOWER SKIN CORROSION REMOVED IAW SRM 51-10-06, REINSPECTED. 2L73 4F A3WE 20050701000172005070100017NM 2005 7 1 UPS05244736 120050607A5523 SKIN BOEING727 72731C 1384011NM LT ELEVATOR TAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 INSPECTION TYPE:C LT ELEVATOR TAB UPPER SKIN CORRODED 5 INCHES FROM O/B END. REMOVED CORROSION IAW SRM 51-10-01, BLENDOUT FOUND TO BE OUT OF LIMITS IAW SRM 55-20-01. REMOVED TAB IAW MM 27-30-11. TAB UPPER SKIN REPAIRED IAW SRM 51-40-20. TAB REPAINTED IAW MM 51-20-00. TAB REBALANCED IAW SRM 51-20-09. TAB REINSTALLED IAW MM 27-30-11. ADJUSTMENT/TEST CARRIED OUT IAW MM 27-30-11 AND FOUND OK. 2L73 4F A3WE 20050701000182005070100018NM 2005 7 1 UPS05244737 120050607A552357025792 SKIN BOEING727 72731C 1384011NM ELEVATOR TAB DEBONDED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 INSPECTION TYPE:C RT ELEVATOR TAB DISBONDED AT LOWER SURFACE 24 INCHES O/B OF INNER EDGE, AT LOWER SURFACE 3 INCHES FROM O/B EDGE 2 SUSPECT AREA RT UPPER OUTER CORNER AND RT UPPER INNER CORNER. REMOVED ELEVATOR TAB IAW MM 27-30-11. REPAIRED TAB IAW SRM 51-40-20. TAB REPAINTED IAW MM 51-21-00. DURING REBALANCING TAB MOVEMENT FOUND TO BE EXCESSIVELY OUT OF LIMITS. REPLACED TAB IAW MM 27-30-11. ADJUSTMENT/TESTED IAW MM 27-30-11 AND FOUND OK. 2L73 4F A3WE 20050701000192005070100019NM 2005 7 1 UPS05244738 120050607A5751AUB7719505 HINGE BOEING727 72731C 1384011NM AILERON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 INSPECTION TYPE:C SUSPECT CRACK ON LEFT O/B AILERON I/B TAB HINGE ASSY LWR HALF. HFEC CARRIED OUT ON SUSPECT AREA IAW B727 NDTM 51-00-00 PT6 FIG 4, CRACK CONFIRMED. FWD HINGE HALF REPLACED IAW SRM 51-30-02. APPLIED CIC TO EXPOSED AREA IAW SRM 51-10-02. 2L73 4F A3WE 20050701000202005070100020NM 2005 7 1 UPS05544739 120050628A2560 SMOKE GOGGLES BOEING757 75724APF 1384969NM COCKPIT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01418UP 23905 INSPECTION TYPE:N/A CAPTS SMOKE GOGGLES LENS CRACKED. REPLACED CAPTS SMOKE GOGGLES. 2L72 4F RTA2NM 20050701000232005070100023SO 2005 7 1 C2XA05CL054 120050625A5210 DOOR EMB 145 EMB145LR 3260212SO MAIN PAX OUT OF ADJUST A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713566 145622 CLE FLIGHT 2441 THE CREW REPORTED THE MAIN CABIN DOOR WAS HARD TO CLOSE. MAINTENANCE INSPECTED AND ADJUSTED THE MAIN CABIN DOOR IAW 52-18-05. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20050701000272005070100027EA 2005 7 1 SWIA200515186 120050627A2760C13045BA03 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07706SK 10149 SSCU 2 INOP MESSAGE. REPLACED NR 1 SSCU PER CRJ MM 27-61-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050701000282005070100028EA 2005 7 1 SWIA200515187 120050623A2720 PULLEY CNDAIRCL600 CL6002B19 1900309EA LT RUDDER OBSTRUCTED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07925SW 7682 LEFT RUDDER BINDS. REMOVED DEBRIS FROM AFT LEFT RUDDER PULLEY, OPERATIONAL CHECK GOOD IAW 27-21-00. 2L72 4F RTA21EA 20050701000302005070100030EA 2005 7 1 SWIA200515189 120050627A5210 PIN CNDAIRCL600 CL6002B19 1900309EA PAX DOOR LACK OF LUBE A SWIAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 NM07946SW 7776 MAIN CABIN DOOR WOULD NOT CLOSE. LUBED MAIN CABIN DOOR PINS & MOVING MECHANISMS. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050701000332005070100033SO 2005 7 1 SWIA200515192 120050618A3350 BULB EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07217SW 120286 EMERGENCY LIGHT UNDER F/A'S SEAT INOP. INSTALLED NEW BULB IN EMERGENCY LIGHT UNDER F/A'S SEAT, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050701000342005070100034EA 2005 7 1 SWIA200515193 120050620A274170609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07975SW 7951 STAB TRIM CH1 FAILS TO ENGAGE. REPLACED HSTCU IAW 27-41-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050701000402005070100040EA 2005 7 1 A6WA200540209 120050617A5610 WINDOW CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE COCKPIT CRACKED A A6WAO OTHER O OTHER APAPPROACH 1 GL31450AW 7823 LT SIDE WINDOW CRACKED IN COCKPIT (ON APPROACH). REMOVED AND REPLACED LT SIDE WINDOW IAW MM. (K) 2L72 4F4 FRTA21EA E15NE 20050701000442005070100044EA 2005 7 1 A6WA200540216 120050621A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31423AW 7636 RT FS 460.00 ANGLE AT RBL 9 HAS A .5 INCH CRACK. REMOVED CRACK ANGLE AND INSTALL NEW ANGLE AT RBL 9. (K) 2L72 4F4 FRTA21EA E15NE 20050701000472005070100047EA 2005 7 1 A6WA200540213 120050605A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSLEAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31418AW 7618 THE UNDER FLOOR INTERCOSTAL AT FS 484, RBL 36 IS CRACKED 1 INCH LONG. REPAIRED INTERCOSTAL IAW REO. (K) 2L72 4F4 FRTA21EA E15NE 20050701000482005070100048EA 2005 7 1 A6WA200540214 120050621A5320453310300 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSLEAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31419AW 7633 LT OBLIQUE ANGLE AT FS 625, CRACKED ON AFT SIDE .5 INCHES LONG. REMOVED OBLIQUE ANGLE LT FS 625, INSTALLED NEW SERVICEABLE ANGLE IAW SRM. (K) 2L72 4F4 FRTA21EA E15NE 20050701000582005070100058CE 2005 7 1 FFS2005F00005 120050613A324613600LA92A3 BEARING BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA HARTZLHCB4M HCB4MP3 GL WHEEL ASSEMBLY DISINTEGRATED A FFSAO OTHER O OTHER NRNOT REPORTED 1 AL01575G SEP88441 UC155 LT OB WHEEL AND TIRE ASSEMBLY SEPARATED FROM AIRCRAFT ON TAKEOFF ROLL. PILOT LANDED UNEVENTFULLY AT NEXT SCHEDULED DESTINATION UNAWARE OF THE LOSS OF THE WHEEL. OUTER WHEEL BEARING FAILED ALLOWING WHEEL TO SEPARATE OVER THE AXLE NUT. WHEEL AND TIRE ASSEMBY HAD 386 HOURS AND 364 LANDINGS SINCE BUILD-UP, BEARING LUBRIATION AND INSTALLATION. (K) 2L72 4T4 TRTA24CE E4EA 6 CP56GL 20050701000622005070100062SO 2005 7 1 F2P2005F00001 120050621A2121587815 SWITCH PIPER PA31 PA31350 7103110SO LYC O540 TIO540* 41532EA AIR CON FAN BURNED E F2PAO OTHER O OTHER NRNOT REPORTED 1 SO17684JJ2000 317952194 PILOT REPORTED SMELL OF SMOKE IN COCKPIT, WHEN PILOT TURNED AIR CONDITION OFF AND CABIN FAN ON PRIOR TO TAKEOFF. TAXIED BACK TO MAIN, REMOVED OVERHEAD PANEL, FOUND WIRING TO AIR CONDITION/FAN SWITCH BURNED. REMOVED SWITCH, FOUND TERMINAL FOR FAN CIRCUIT LOOSE ON SWITCH. FOUND LOOSE TERMINAL, HAD MOVED AND CONTACTED OTHER TERMINAL CAUSING SHORT. (K) 1L72 3O3 O A20SO E14EA 20050701000642005070100064SO 2005 7 1 FXT2005F00000 220050621A8530AEC631397RB CYLINDER HEAD CESSNA207 207A 2073604CE CONT O520 IO520F 17032SO MCAULYD3A34 D3A34C404 GL ENGINE CRACKED E FXTAO OTHER O OTHER NRNOT REPORTED 1 AL019964M 489 20700766 818792R 830103 AFTER TAKEOFF, PILOT HEARD A POP FROM THE ENGINE AND THE ENGINE STARTED RUNNING RUFF. BROUGHT PLANE BACK TO AIRPORT RUNNING WITH NO OTHER PROBLEMS. AN INSPECTION OF THE ENGINE WAS DONE AND THE NR 3 CYLINDER WAS FOUND TO BE CRACKED. THE HEAD WAS SEPARATED FROM THE BARREL. THE ENGINE IS 30 HOURS FROM TBO AND IS BEING REMOVED FROM SERVICE. THE NR 3 CYLINDER WAS SERVICED. (K) 1H71 3O3 O A16CE E5CE 5 CP47GL 20050701000662005070100066NE 2005 7 1 ALG2005F00032 120050525A2432407612 BATTERY SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL MASTER INOPERATIVE E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03519AL 100 760058 DURING FLIGHT, BATTERY HOT AND BATTERY OFF LIGHT ILLUMINATED. EMERGENCY CHECKLIST CONSULTED, TURNED BATTERY SWITCH OFF AS A PRECAUTION. PROCEEDED FOR MAINTENANCE. MAINTENANCE REMOVED BATTERY AND INSTALLED SERVIEABLE BATTERY. THE OPS CHECK WAS GOOD AND SET VOLTAGE REGULATOR. (K) 1G72 3U3 U H1NE E1GL 20050701000672005070100067NM 2005 7 1 SB05077 120050630A335020121 CHARGER BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19519AU 23705 MAINTENANCE REPORTED THE EMERGENCY EXIT SIGN BETWEEN THE AFT LAVATORIES, OVER THE R2 DOOR AND OUTSIDE OF THE L2 DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY ALONG WITH THE BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA16WE E21EU 20050701000682005070100068CE 2005 7 1 DJFA2005114 120050622A2760 BONDING JUMPER BEECH MU300 400A 1155402CE SPOILERS OUT OF POSITION E DJFAO OTHER F FLT CONT AFFECTED DEDESCENT 1 EA23402CW RK2 ON DESCENT, THE SPEED BRAKES WERE USED TO INCREASE THE DESCENT RATE FOR APPROACH. LT YOKE WAS APPLIED TO COUNTER ACT A TURBULENCE INDUCED ROLL. THE CREW DISCOVERED THEY ONLY HAD ABOUT .2500 LT OR RT ROLL CONTROL MOVEMENT OF THE YOKE. WHEN THE SPOILERS WERE RETRACTED FULL ROLL CONTROL WAS RETURNED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPOSITIONED THE SPOILER BONDING STRAPS ON THE RT WING. A CONTROL WHEEL OPERATING FORCE CHECK, AND SPOILER CONTROL FUNCTION TEST WERE COMPLETED WITH NO NOTED BINDING. A SATISFACTORY FLIGHT TEST WAS COMPLETED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4F RTA16SW 20050701000702005070100070CE 2005 7 1 20030856 120050625A261224409015 FIRE LOOP BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA RT ENGINE BAY DEFECTIVE A GLBAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 NM03211GL UE211 DURING FLIGHT, FLIGHT CREW NOTICED RT ENGINE T-HANDLE ANNUNCIATOR AND YELLOW (LOOP) ANNUCIATOR FLICKERING ON AND OFF AND WAS DETERMINED BY CREW THAT IT WAS A FALSE INDICATION. MAINTENANCE TROUBLESHOT PROBLEM TO DEFECTIVE RT AFT FIRE LOOP IN ENGINE COMPARTMENT. FIRE LOOP WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE. 2L72 4T3 TRTA24CE E2NE 20050701000762005070100076WP 2005 7 1 05FDEA01713 120050628A54202170004172 SEAL DOUG MD10 MD1010F 3022112WP PYLON FAIRING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25391FE 46625 COMPLY WITH EA 8-5410-82094. NACELLES/PYLON-REPLACEMENT OF DAMAGED PYLON FAIRING SEAL. CLOSING ACTION ON 06/27/05, ON N/R S00083.COMPLIED WITH EA8-5410-82094. 2L73 4F RTA22WE 20050701000772005070100077EA 2005 7 1 QXEA200501084 220050629A7532 BLEED VALVE BOMBDRDHC8 DHC8402 1390042NM PWC 150 PW150A EA ZONE 200 MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION APAPPROACH 1 NM09401QX 4031 NR 1 BLEED HOT CAUTION LIGHT ILLUMINATED IN FLARE FOR LANDING. NR 1 BLEED VALVE WAS TURNED OFF UPON EXITING RUNWAY IAW CHECKLIST. NR 1 BLEED HOT CAUTION LIGHT WENT OUT APPROX 10 SECONDS AFTER TURNING BLEED VALVE OFF. COMPLIED WITH FIM TASK 36-20-00-810-801 AND AMM TASK 36-11-00-710-802. NO FAULTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E00062EN 20050701000812005070100081NE 2005 7 1 EGRR104348 120050623A33977655006001011 WIRE HARNESS SKRSKYS76 S76C 8143008NE STROBE LIGHT CHAFED B EGRRK NONE O OTHER ININSP/MAINT 1 EA1722CP 859 760530 DISCOVERED WIRING HARNESS FOR HORIZONTAL STABILIZER MOUNTED POSITION/STROBE LIGHT ASSEMBLIES CHAFFED THROUGH INSULATION TO CONDUCTOR INSIDE THE STABILIZER. THE CHAFE DAMAGE WAS DISCOVERED WHILE REMOVING THE HARNESS. REPLACED ALL INTERNAL WIRING WITH NEW AND APPLIED CHAFE PROTECTION. 1G72 3U NCH1NE 20050701000832005070100083SW 2005 7 1 ALGA104358 120050524A6410206310105101 BEARING BELL 206 206L4 1182110SW ALLSN 250C 250C30 03013GL TAIL ROTOR WORN E ALGAK NONE O OTHER ININSP/MAINT 1 SW03176AL385 52146 BEARING AXIAL PLAY BEYOND MAX. INSTALLED NEW BEARINGS AND SLEEVES BY O/H SHOP. 1G71 3U3 UNCH2SW E1GL 20050701000842005070100084SW 2005 7 1 ALGA104359 120050524A6410206010733003 SLEEVE BELL 206 206L4 1182110SW ALLSN 250C 250C30 03013GL TAIL ROTOR WORN E ALGAK NONE O OTHER ININSP/MAINT 1 SW03176AL385 52146 BEARING AXIAL PLAY BEYOND MAX. INSTALLED NEW BEARINGS AND SLEEVES BY O/H SHOP 1G71 3U3 UNCH2SW E1GL 20050701000852005070100085SW 2005 7 1 ALGA104360 120050501A6410206310105101 BEARING BELL 206 206L4 1182110SW ALLSN 250C 250C30 03013GL TAIL ROTOR WORN E ALGAK NONE O OTHER ININSP/MAINT 1 SW03176AL385 52146 BEARING AXIAL PLAY BEYOND MAX. INSTALLED NEW BEARINGS AND SLEEVES BY O/H SHOP. 1G71 3U3 UNCH2SW E1GL 20050705000052005070500005CE 2005 7 5 2005FA0605 120050703A8011655566F24V STARTER CESSNA207 207A 2073604CE CONT O520 IO520F 17032SO MCAULYD3A34 D3A34C404 GL ENGINE FAILED E H DEACTIVATE SYST/CIRCUITS JHSWARNING INDICATION ELECT. POWER LOSS-50 PC AFFECT SYSTEMS CLCLIMB 1 GL259946M98 20700588 830423R 807151 "LIGHT WEIGHT" STARTER SUPPLIED ON A TCM REMANUFACTURED ENGINE INSTALLED IN JUNE,2004. ID TAG SAYS "MADE IN SLOVENIA" BY "ISKRA". WAS INSTALLED FOR 98.0 HOURS, NOTICED HIGH CURRENT DRAW ON AMMETER, AFTER TAKEOFF. STARTER RELAY "STUCK" & WOULD NOT DE-ENERGIZE STARTER. TURNED OFF MASTER SWITCH, & MADE A "NO FLAP LANDING" AT A NEARBY AIRPORT. INSTALLED A NEW MAGNET STARTER. 1H71 3O3 O A16CE E5CE 5 CP47GL 20050705000102005070500010EU 2005 7 5 USAA050692 120050518A5315D5347209000300 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19716UW18358 1055 PIT - FOUND FLOORBEAM CORRODED 3 FT BY 3 INCHES, AT -Y31 BETWEEN FRAME 64-66. REPLACED FLOORBEAM PER AIRBUS DWG D53472815 AND TR 51-40-01. (M) 2L72 4F RTA28NM 20050705000112005070500011EU 2005 7 5 USAA050693 120050523A5315D5347217220400 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19716UW18358 1055 PIT - FOUND FLOORBEAM CORRODED 20 INCH BY 3 INCH WIDESPREAD AT Y48 FRAME 66. REPLACED FLOORBEAM PER AIRBUS DWG D53472780 AND SRM 51-72-11. (M) 2L72 4F RTA28NM 20050705000122005070500012EU 2005 7 5 USAA050694 120050517A5320D534720300200 FLOOR SUPPORT AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19716UW 1055 PIT - FOUND FLOOR SUPPORT CORRODED 1 INCH BY 3 INCH AREA, AT Y 28 AND FRAME 66. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR. (M) 2L72 4F RTA28NM 20050705000132005070500013EU 2005 7 5 USAA050695 120050517A5320 FLOOR SUPPORT AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19716UW 1055 PIT - FOUND FLOOR SUPPORT CORRODED 3 INCHES BY 3 INCHES, AT FRAME 67 AND Y - 28 INCHES. CORROSION LEVEL 1, TASK JA-260-53500. DEFECTIVE PART REPLACED WITH IDENT PART. (M) 2L72 4F RTA28NM 20050705000142005070500014EU 2005 7 5 USAA050696 120050516A5347D5311282600101 SEAT TRACK AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19716UW18358 1055 PIT - FOUND DUMMY RAIL CORRODED, 3 INCHES BY 10 INCHES AT Y254 BETWEEN C-14 AND C-16. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M) 2L72 4F RTA28NM 20050705000162005070500016EU 2005 7 5 USAA050698 120050525A5320D5348004320401 SILL AIRBUSA319 A319112 3930323EU L2 DOOR CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19717UW17895 1069 PIT - FOUND SILL CORRODED 3 SQUARE INCHES, L2 DOOR SILL. CORROSION LEVEL 1, TASK JA-260-53500. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-72-11 PAGE 1 AND 2. (M) 2L72 4F RTA28NM 20050705000172005070500017NM 2005 7 5 USAA050711 120050601A5310 BEAM BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19445US 24863 CLT - FOUND STUB BEAM CRACKED .375 INCH, STATION 578 LBL 64. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-20-05. (M) 2L72 4F RTA16WE 20050705000182005070500018NM 2005 7 5 USAA050710 120050601A5320 CLIP BOEING737 7374B7 1384702NM FUSLEAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19445US40360 24863 CLT - FOUND SUPPORT CLIP CRACKED, AFT CARGO COMPARTMENT SUPPORT CLIP AT STATION 771 STRINGER 26R. FABRICATED AND INSTALLED A NEW CLIP IAW BOEING DRAWING 69-43445. (M) 2L72 4F RTA16WE 20050705000202005070500020NM 2005 7 5 USAA050707 120050526A5320 SILL BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19445US 24863 CLT - FOUND SILL PLATE CORRODED 15 - 1 INCH SQUARE AREAS AROUND SCREW HOLES, NUMEROUS CORRODED AREAS AROUND SCREW HOLES IN AFT, CARGO DOOR SILL. REMOVED AND REPLACED SILL STRAP AND SILL COVER IAW DRAWING 65-47957 AND SRM 51-10-02. (M) 2L72 4F RTA16WE 20050705000212005070500021NM 2005 7 5 USAA050706 120050601A5420 STIFFENER BOEING737 737401 1384701NM NACELLE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19406US47279 23876 CLT - FOUND STIFFENER AND CHANNEL CRACKED .5 INCHES, NR 2 ENGINE AFT STRUT STRUCTURE. FABRICATED AND INSTALLED NEW CHANNEL REMOVED AND REPLACED STIFFENER IAW SRM 51-10-01 AND DRAWING 313H1355. (M) 2L72 4F RTA16WE 20050705000222005070500022NM 2005 7 5 USAA050705 120050529A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19531AU50089 24478 CLT - FOUND SKIN CRACKED 2.25 INCH, STATION 727D BELOW S-23R. INSTALLED REPAIR DOUBLER IAW SRM 53-00-01. (M) 2L72 4F RTA16WE 20050705000232005070500023NM 2005 7 5 USAA050704 120050531A5320 WEB BOEING737 7374B7 1384702NM DOOR SILL CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19445US40360 24863 CLT - FOUND WEB CORRODED 3 INCHES, AFT CARGO DOOR SILL WEB. FABRICATED AND INSTALLED REPAIR DOUBLER IAW 51-70-11 FIG 1. (M) 2L72 4F RTA16WE 20050705000252005070500025EU 2005 7 5 UPS05144708 120050615A3350 LIGHT AIRBUSA300 A300F4622R 3930360EU CABIN INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01120UP 0805 EMERGENCY EXIT LIGHT JUST OUTSIDE CABIN ENTRY INOPERATIVE. RESET SOCKET AND OPS CHECKED PER AMM 33-51-00-0. OPS CHECK. THIS CLEARS M304232. PLACARD REMOVED. 2L72 4F RTA35EU 20050705000262005070500026 2005 7 5 UPS05144716 420050617A2565 WARNING SYSTEM AIRBUSA300 A300F4622R 3930360EU ESCAPE SLIDE INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01126UP 0810 FWD ENTRY DOOR EVACUATION SLIDE WARNING SYSTEM BUZZER INOPERATIVE. LIGHTS INOPERATIVE. CYCLED POWER. TESTED WARNING SYSTEM. CHECKS GOOD IAW 52-20-00. 2L72 4F RTA35EU 20050705000282005070500028NM 2005 7 5 UPS05444715 120050617A5312 PRESSURE PANEL BOEING747 747123 1384873NM NLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 AD LT NLG WW SIDE PANEL WEB FOUND 2 LOCATIONS CRACKED BETWEEN STA 265 AND 280, WL 160 AND 170. CRACK LENGTH APPROX 1 INCH. LT NLG WW SIDE PANEL WEB REPAIRED AT BETWEEN BS 265 AND 280 WL 160 AND 170 AREA AS PER SRM 53-10-04 FIG 116. SUBSEQUENT INSP NECESSARY FOR CAT B REPAIR. REFER TO SRM 53-10-04 FIG 116 TABLE II FOR REPEAT INSP REQUIREMENT. 2L74 4F A20WE 20050705000312005070500031WP 2005 7 5 ASMF200506022 120050619A2932ST107Q TRANSMITTER DOUG DC9 DC983 3022083WP HYD PRESS SENSORINOPERATIVE W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23583MD5912 1728 49659 CAPTAIN REPORTED RT HYDRAULIC BRAKE PRESS INDICATION SYSTEM INOPERATIVE. WIRING SYSTEM CHECK DETECTED ELECTRICAL LINE DAMAGED ON RT BRAKE PRESS TRANSMITTER CONNECTOR. ELECTRICAL LINE, RT BRAKE TRANSMITTER AND PRESS INDICATOR REPLACED IAW MM 32-42-00, OPS CHECK PERFORMED, ALL CORRECT. 2L72 4F RTA6WE 20050705000322005070500032SO 2005 7 5 C2XA05CL051 120050619A32221170C000004 STRUT EMB 145 EMB145LR 3260212SO NLG FAILED A C2XAO OTHER J WARNING INDICATION CLCLIMB 1 SW27299179757 9757 145414 CREW REPORTED LANDING GEAR AIR/GROUND FAIL MESSAGE AND ENG 1-2 REVERSER DISAGREE MESSAGE ON EICAS IN FLIGHT. MX INSP AND REPLACED NLG ASSEMBLY. OPS CHECKS GOOD. 2L72 4T RTT00011AT 20050705000332005070500033SO 2005 7 5 C2XA05CL049 120050616A2611FDS765A2 SMOKE DETECTOR EMB 145 EMB145ER 3260211SO LAVATORY INTERMITTENT A C2XAO OTHER J WARNING INDICATION CRCRUISE 1 SW2714933 145018 CREW REPORTED INTERMITTENT LAVATORY SMOKE WARNING ON GROUND AND INFLIGHT. MX INSP AND REPLACED LAVATORY SMOKE DETECTOR. OPS CHECKS GOOD. 2L72 4F RTT00011AT 20050705000342005070500034SO 2005 7 5 C2XA05SH052 120050618A532014521700007 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713903 145479 DURING C-CHECK, LT OMEGA BEAM HAS VARIOUS AREAS OF CORROSION BETWEEN FS 24 AND FS 32. MX REPAIRED LT OMEGA BEAM AT FRM 29 IAW EC 5320-01249. ACFT APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050705000362005070500036SO 2005 7 5 C2XA05SH054 120050619A532014521700007 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714904 145477 DURING C-CHECK, LT OMEGA BEAM HAS CORROSION FS 23-FS 29. MX REPAIRED LT OMEGA BEAM FS 23-FS 29 I/A/W EC 5320-01249. ACFT APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20050705000422005070500042NM 2005 7 5 CALA0500204 120050618A531565C33950 FLOORBEAM BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717619 27332 INSP FOUND MAIN CABIN FLOORBEAM CORRODED AT STA 986.5, LBL 14 TO LBL 43. FLOORBEAM UPPER CAP REPAIR WAS INSTALLED IAW ECRA 5310-04471. 2L72 4F RTA16WE 20050705000432005070500043NE 2005 7 5 ASMF200506020 220050618A7200 ENGINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE RIGHT VIBRATION W ASMFO OTHER E VIBRATION/BUFFET CRCRUISE 1 SW23169PL 53175 718246 CAPTAIN REPORTED VIBRATION IN RT ENGINE DURING CRUISE. ACFT SENT TO HANGAR AND WAS CHECKED BY CONDITION AND TESTS PERFORMED IAW MM 72-00-00. ALL CORRECT. RT ENGINE WAS ACCELERATED UNTIL TAKEOFF POWER AND MAXIMUM VIBRATION REGISTERED 0.5, MAXIMUM VIBRATION ALLOWED 3.0. DURING OVERNIGHT SERVICE, OPS TESTS PERFORMED IAW MM 72-00-00, ALL CORRECT AND WITHOUT VIBRATION. 2L72 4F4 FRTA6WE E9NE 20050705000442005070500044NM 2005 7 5 AWXA200500715 120050607A575465C2660399 SKIN BOEING737 7373B7 1384580NM NR 3 SLAT DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28328AW 23377 DURING C-13 CHECK DISCOVERED DISBONDED AREA LOCATED AT TOP OF NR 3 SLAT WEDGE INBOARD END FROM SS 12.25 TO SS 16.25. MX REMOVED DISBONDED AREA AT TOP OF NR 3 SLAT WEDGE INBOARD END FROM SS 12.25 TO SS 16.25 IAW BOEING 737-300 SRM 51-70-10 FIG 16. FABRICATED REPAIR CORE AND REPAIR DOUBLER IAW BOEING 737-300 SRM 51-70-10-0 FIG 16. BONDED FABRICATED REPAIR CORE AND DOUBLER IAW BOEING 737-300 SRM 51-70-10-0 FIG 16. 2L72 4F RTA16WE 20050705000472005070500047NM 2005 7 5 AWXA200500718 120050614A3350110049 CHARGER BOEING737 73733A 1384673NM EMERGENCY LIGHTSINOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 DURING C-21 CHECK EMERGENCY EXIT LIGHTS AT SEATS 1-4 INOPERATIVE AND SEAT 17 LAMP OUT. MX REMOVED AND REPLACED EMERGENCY LIGHT BATTERY CHARGER IAW BOEING 737-300 AMM 31-51-51-962-016. OPS CHECK GOOD IAW AMERICA WEST AIRLINES TASK CARD A1C33006. 2L72 4F RTA16WE 20050705000482005070500048NM 2005 7 5 AWXA200500719 120050531A531065C80735183 DOOR FRAME BOEING737 73733A 1384673NM FWD CARGO DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 DURING C-21 CHECK, FOUND CRACK .750 INCHES IN LENGTH AT FORWARD CARGO DOOR LOCATED ON FORWARD EDGE BELOW HOLD OPEN HOOK. MX REMOVED CRACKED CARGO DOOR FRAME IAW BOEING 737-300 SRM 51-40-02-0 FIG 8. INSTALLED NEW FRAME ASSEMBLY IAW BOEING 737-300 SRM 51-40-02-0 FIG 3, 4, 6, 7, 8, 12, 13, 14 AND BAC DWG 65-46921. 2L72 4F RTA16WE 20050705000532005070500053EU 2005 7 5 SA05063 120050604A2120 ODOR AIRBUSA319 A319112 3930323EU CABIN DETECTED A USAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 EA19742UW 1275 DURING DESCENT, CABIN CREW REPORTED HOT, ELECTRICAL, AND OILY ODOR IN AFT CABIN. CREW TURNED OFF RT PACK AND GALLEY/CABIN SWITCHES ON OVERHEAD PANEL. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MX RAN AIR CONDITIONING PACKS FOR AN HOUR, AND COULD NOT DUPLICATE ODOR IN CABIN DURING DESCENT. OK FOR SERVICE. 2L72 4F RTA28NM 20050705000542005070500054 2005 7 5 SA05064 420050606A2565 LINE AIRBUSA319 A319112 3930323EU PAX DOOR SLIDE MISROUTED A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19750UW 1315 MAIN ENTRY DOOR SLIDE MOORING LINE FOUND IMPROPERLY ROUTED. MX CORRECTLY ROUTED MAIN ENTRY DOOR SLIDE MOORING LINE. OK FOR SERVICE. 2L72 4F RTA28NM 20050705000552005070500055EU 2005 7 5 SA05065 120050606A2597 WIRE HARNESS AIRBUSA319 A319112 3930323EU ESCAPE SLIDE MISROUTED A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19750UW 1315 LT AFT ENTRANCE DOOR SLIDE LIGHT HARNESS FOUND ROUTED INCORRECTLY. MX CORRECTLY ROUTED LT AFT ENTRANCE DOOR SLIDE LIGHT HARNESS. 2L72 4F RTA28NM 20050705000562005070500056EU 2005 7 5 SA05066 120050606A5610NP1653116 WINDSHIELD AIRBUSA319 A319112 3930323EU COCKPIT CRACKED A USAAH DEACTIVATE SYST/CIRCUITS O OTHER CRCRUISE 1 EA19770UW12955 1393 AT FL 380, F/O WINDSHIELD STARTED CRACKING FROM SEVEN O'CLOCK POSITION TO TWO O'CLOCK POSITION. FLIGHT CREW COMPLIED WITH QRH PROCEDURES AND PULLED WINDOW HEAT CIRCUIT BREAKER. FLIGHT DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MX REMOVED AND REPLACED F/O WINDSHIELD. OPS CHECKS OK. 2L72 4F RTA28NM 20050705000572005070500057EU 2005 7 5 MALA050483 120050619A3020 WARNING LIGHT SAAB SF340 340B 7860101EU ANTI/DEICE SYS ILLUMINATED A MALAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL15416XJ 340B416 CREW RETURNED TO MSP FOLLOWING INDICATION OF DUCT OVER TEMPERATURE INDICATION. NO EMERGENCY DECLARED AND FLIGHT RETURNED TO GATE WITHOUT FURTHER INCIDENT. NO FURTHER INFORMATION AT THIS TIME. 2L72 4T RTA52EU 20050705000592005070500059EU 2005 7 5 MALA050489 120050616A3213 STRUT BAC 146 AVRO146RJ85A1500097EU MLG UNDERSERVICED A MALAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 GL15524XJ E2349 AFTER GEAR RETRACTION SELECTED, GEAR TOOK 8 SECONDS TO COME UP. SERVICED MLG STRUT. 2H74 4F RTA49EU 20050705000672005070500067SO 2005 7 5 C2XA05CL047 120050614A3297 WIRE HARNESS EMB 145 EMB145ER 3260211SO NLG UPLOCK SHORTED A C2XAO OTHER O OTHER NRNOT REPORTED 1 SW2712934 145019 CREW REPORTED LANDING GEAR INDICATOR NR 2 C/B POPPED. MX INSP AND REPLACED NOSE GEAR UPLOCK BOX 2 HARNESS. OPS CHECKS GOOD. 2L72 4F RTT00011AT 20050705000752005070500075 2005 7 5 IXXA0500078O 420050609A34251783993485 HSI DOUG DC8 DC871F 302199DWP COCKPIT MALFUNCTIONED A IXXAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 SW11820BX86455461 46065 ON TAKEOFF, NR 1 COMPASS FAILED WITH OFF FLAG IN CAPTAIN HSI. CREW RETURNED AND LANDED WITHOUT INCIDENT. MX REMOVED AND REPLACED CAPTAIN HSI PER ALL APPLICABLE MAINTENANCE MANUALS. OPS CHECK GOOD. ACFT RETURNED TO SERVICE. 2L74 4F RT4A25 20050705000762005070500076EU 2005 7 5 MALA050464 120050610A2910 LINE BAC 146 AVRO146RJ85A1500097EU HYDRAULIC SYS LEAKING A MALAO OTHER K FLUID LOSS TXTAXI/GRND HDL 1 GL15530XJ E2364 AFTER LANDING, THERE WAS HYDRAULIC MIST IN CABIN FOLLOWED BY LOUD BANG. PASSENGERS EVACUATED. REPLACED HYD PIPE. 2H74 4F RTA49EU 20050705000792005070500079NM 2005 7 5 WRLA2005117 120050616A5511 RIB DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C04 CHECK, WHILE PERFORMING INSP PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE NR 36. 2L73 4F4 FRTA22WE E24NE 20050705000812005070500081NM 2005 7 5 WRLA2005119 120050616A5511 RIB DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C04 CHECK, WHILE PERFORMING INSP PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE NR 13. 2L73 4F4 FRTA22WE E24NE 20050705000832005070500083EU 2005 7 5 RAIA00506024 120050616A2611 WARNING LIGHT JETAIRJETSTMJETSTM4101 1500501EU CARGO BAY ILLUMINATED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03557HK 41074 CARGO BAY SMOKE DETECTION CAPTION ILLUMINATED. MX REMOVED AND REPLACED SMOKE DETECTOR. OPS CHECKED GOOD. 2L72 4T RTA41NM 20050705000842005070500084 2005 7 5 1290502 420050620A23301F220100101 AMPLIFIER BOEING737 7377BC 1384509NM CABIN FAILED E BJ6AA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NE03129QS 30329 ELECTRICAL ODOR IN DINING/CONFERENCE AREA. SHUT OFF CABIN ENTERTAINMENT & GALLEY POWER. ODOR DID NOT FULLY GO AWAY. ACFT DIVERTED & LANDED. MX DISPATCHED. FOUND SOURCE OF ELECTRICAL ODOR FROM DINING ROOM/CONFERENCE AUDIO AMPLIFIER FOR ENTERTAIN SYS. NO CIRCUIT BREAKERS OR FUSES FOUND BLOWN OR TRIPPED. AUDIO AMPLIFIER ELECTRICALLY ISOLATED UNTIL FURTHER TESTS CAN BE PERFORMED. AUDIO AMPLIFIER REMOVED AND SENT TO SHOP FOR REPAIR. RECEIVED TEARDOWN REPORT. SHOP FOUND AMP MODULE BLOWN AND MODULE TRANSFORMENR LEAKING FLUID WHICH HAS COATED WIRING AND OTHER COMPONENTS. AUDIO AMPLIFIER IS DAMAGED BEYOND ECONOMICAL REPAIR AND HAS BEEN SCRAPPED AND DESTROYED. [CLOSED] 2L72 4F RTA16WE 20050705000862005070500086NM 2005 7 5 WRLA2005113 120050616A5511 RIB DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C04 CHECK, WHILE PERFORMING INSP PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE NR 30. 2L73 4F4 FRTA22WE E24NE 20050705000872005070500087NM 2005 7 5 WRLA2005114 120050616A5511 RIB DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C04 CHECK, WHILE PERFORMING INSP PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE NR 31. 2L73 4F4 FRTA22WE E24NE 20050629000712005062900071WP 2005 6 29 ASAA0580150 120050228A5311991224619 FRAME DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02975AS 53451 C-CHECK, UPPER LT ACCY COMPARTMENT FWD EDGE OF FRAME WEB IS CHAFED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLERS AND FILLER. (K) 2L72 4F4 FRTA6WE E9NE 20050629001672005062900167 2005 6 29 MALA050508 420050624A3440 TRANSMITTER SAAB SF340 340B 7860101EU WX RADAR SYS FAILED A MALAO OTHER O OTHER CRCRUISE 1 GL15418XJ 4654 340B418 AIR RETURN TO CWA DUE TO WEATHER RADAR FAILING. REMOVED AND REPLACED WX-RADAR TRANSMITTER. PN ON/OFF 622-7337-001, S/N ON 4690, S/N OFF 4654. 2L72 4T RTA52EU 20050630000052005063000005EU 2005 6 30 05FDEA01546 120050608A5311 FRAME AIRBUS310 A310 EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25404FE 233 CORROSION ON FRAME 20A AFT SIDE AT STRINGER 44R FORWARD CARGO. FR20A LOWER SECTION AT STR 44R CORROSION WAS FOUND TO BE OUT OF LIMITS IAW A310/200N SRM 53-10-00 FIG 102. REPAIRED BY CUTTING AND REMOVING FRAME SECTION 20A FROM STR 38R TO STR 45R. INSTALLED NEW FRAME SECTION AND SPLICE REPAIR ANGLES IAW FED EX DRAWING SR30-53-001. 2L72 4F RTA35EU 20050630000252005063000025NM 2005 6 30 UPS05444693 120050601A2612 CONNECTOR BOEING747 747212B 1384886NM FIRE DETECT SYS DIRTY A IPXAE ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 SO01526UP 21937 NR 4 ENG A- LOOP DISPLAYED INTERMITTENT FAULT LIGHTS AND BELL TEMPERATURE WAS IN RED BANK BUT FLUCTUATED SOMEWHAT. PERFORMED PRECAUTIONARY ENGINE SHUT DOWN PROCEDURE. TEMP STAYED IN HIGH ORANGE TO RED BAND. FOUND LOWER RIGHT A- LOOP CONNECTORS SOAKED WITH OIL. CLEANED CONNECTORS AND TEMP BANK RETURNED TO NORMAL. TESTED PER MM 26-11-00 TEST GOOD. 2L74 4F A20WE 20050630000462005063000046EA 2005 6 30 QXEA200501058 220050613A7261 ENGINE BOMBDRDHC8 DHC8402 1390042NM PWC 150 PW150A EA NR 1 LEAKING A QXEAO OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM09414QX 4061 PCEFA0062 WHILE ON THE GROUND WITH ENGINES RUNNING, F/A ADVISED CABIN GETTING HAZY OR SMOKY WITH ODOR DETECTED. REPLACED NR 1 ENGINE. OPS CHECK GOOD. NO LEAKS NOTED. ACFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E00062EN 20050630000522005063000052WP 2005 6 30 UPS05844701 120050525A2810 FUEL TANK DOUG DC8 DC873F 302199FWP RT WING DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 RT AUX TANK UPPER SURFACE FASTENER HOLE ELONGATED AT XW 208. FABRICATED REPAIR DOUBLER, INSTALLED CONICAL WASHERS AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 57-2-1 FIG 37, 51-1-26, 51-1-20D, AND 51-1-21. 2L74 4F RT4A25 20050630000592005063000059SO 2005 6 30 SWIA200515136 120050612A2121AE1711AA0 COOLING FAN EMB 120 EMB120ER 3260203SO COCKPIT FAILED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM07567SW5140 5140 120342 BURNING ODOR FROM COCKPIT VENTS. REPLACED LT GROUND COOLING FAN. OPS CHECK GOOD MM 21-51-03. 2L72 4T RTA31SO 20050630000802005063000080EA 2005 6 30 MASA200500252 120050325A4990 VENT LINE CNDAIRCL600 CL6002B19 1900309EA APU GEARBOX DIRTY A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 SW0775996 7357 DECLARED EMERGENCY DUE TO SMOKE IN CABIN AFTER SWITCHING TO APU BLEED WHEN LANDING. LT ACM PREVIOUSLY MEL FOR SIMILAR SMOKE IN CABIN SITUATION. MX PERFORMED COMPREHENSIVE TEST OF RT ACM RUNNING IT OFF ENGINE BLEED AND COULD NOT DUPLICATE PROBLEM, MEL APU. MX CLEANED APU GEARBOX VENT LINE. OPS CHECKED GOOD. 2L72 4F RTA21EA 20050630000822005063000082 2005 6 30 MASA200500269 420050403A3414WL102AMS5 INDICATOR CNDAIRCL600 CL6002B19 1900309EA AUX AIRSPEED FAILED A MASAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 SW0775993882 7372 ABORTED TAKEOFF AND RETURNED TO GATE FOR STANDBY AIRSPEED INDICATOR HAVING NO INDICATIONS. MX IN PROCESS OF REPLACING STANDBY AIRSPEED INDICATOR. WAITING PART INFO. REPLACED STANDBY AIRSPEED INDICATOR. 2L72 4F RTA21EA 20050630000862005063000086EA 2005 6 30 MASA200500299 120050415A5210 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR OUT OF ADJUST A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0727172 7172 MAIN PAX DOOR WILL NOT OPEN. FERRIED ACFT FOR TROUBLESHOOTING. MX ADJUSTED PASSENGER DOOR OUTER HANDLE. OPS CHECKED GOOD. 2L72 4F RTA21EA 20050630000922005063000092EA 2005 6 30 MASA200500363 120050516A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA CABIN STIFF A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0737178 7178 CREW REPORTED MAIN PASSENGER DOOR HARD TO OPEN AND CLOSE. MX CYCLED DOOR MULTIPLE TIMES AND OPS CHECKED NORMAL. 2L72 4F RTA21EA 20050630000942005063000094EA 2005 6 30 MASA200500378 120050522A3260 PROXIMITY SWITCH CNDAIRCL600 CL6002B19 1900309EA LT MLG MALFUNCTIONED A MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW07570ML 7206 CREW RETURNED TO FIELD DUE TO GEAR DISAGREE. MX ADJUSTED LT GEAR UPLOCK TARGET AND PROX SWITCH. 2L72 4F RTA21EA 20050630000952005063000095EA 2005 6 30 MASA200500382 120050523A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA CABIN MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0737178 7178 UPON ARRIVAL IN PHX, F/A COULD NOT OPEN DOOR. MX OPERATED DOOR NORMALLY MANY TIMES AND OUTBOUND F/A OPERATED DOOR NORMALLY. 2L72 4F RTA21EA 20050630001072005063000107SO 2005 6 30 C2XA05SH058 120050624A533014535010001 SKIN EMB 145 EMB145LR 3260212SO FUSELAGE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715985 145248 SHV - DURING C-CHECK 2 RIVET HOLE CRACKED ON FUSELAGE SKIN UNDER AFT RAR 2 SUPPORT. MAINTENANCE PERFORMED REPAIR OF FUSELAGE SKIN UNDER RAR 2 ANTENNA SUPPORT IAW EC5330-01475. THE AIRCRAFT WAS APPROVED TO RETURNED FOR SERVICE. 2L72 4T RTT00011AT 20050701000062005070100006EU 2005 7 1 DJFA2005117 120050626A2120 DUCT BRAERODH125 BAE125800A 1500285EU COALESCER SOCK LOOSE E DJFAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA23851CW 258051 THE CREW REPORTED THAT WHILE CLIMBING THROUGH FL200, THE CABIN ALTITUDE WENT ABOVE 12,000 FEET. AN EMERGENCY WAS DECLARED AND A DESCENT WAS INITIATED TO 11,000 FEET. THE CABIN ALTITUDE ANNUNCIATOR ILLUMINATED ALONG WITH THE WARNING HORN AND OXYGEN MASK DEPLOYMENT. THE AIRCRAFT RETURNED TO KPHX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REATTACHED THE DUCTING FROM THE COALESCER TO THE COOLING TURBINE. THE AIRCRAFT WAS PRESSURIZED TO 8.5 DIFFERENTIAL PRESSURE WITH NO NOTED LEAKS. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA3EU 20050701000212005070100021WP 2005 7 1 UPS05844740 120050626A5330 SKIN DOUG DC8 DC871F 302199DWP FUSLEAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 SKIN BULGING AT SEAM APPROX 6 FT AFT OF NOSE GEAR LEFT SIDE OF FX MARKED. DAMAGED FINGER 5 INOP FOUND CORRODED. REMOVED DAMAGE, INSPECTED AREA TO INSTALL REPAIR. FABRICATED NEW FINGER DOUBLER SECTION IAW PRELIM EO DC8-5330-22410-A. INSTALLED 80 PERCENT OF FASTENERS. COMPLETED PER EO 5330-22410-A. 2L74 4F RT4A25 20050701000252005070100025NE 2005 7 1 P5CA0501373 220050614A7200CF650E2 ENGINE BOEING747 747230B 1384889NM GE CF6 CF650E2 30018NE NR 1 FAILED A P5CAEJA ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 EA15508MC 21644 530167 AFTER TAKEOFF NR 1 ENGINE FAILED. SHUT DOWN ENGINE AND JETTISON FUEL IAW CHECK LIST. AFTER SHUT DOWN OIL PRESSURE ZERO. NR 1 ENGINE REPLACED PER ENGINE CHANGE FORM 00-AA-45. RUN UP OK PER MM 71-00-00 TEST NR 3, 8 AND 9. 2L74 4F4 F A20WE E23EA 20050701000312005070100031EA 2005 7 1 SWIA200515190 120050625A2720 ACTUATOR CNDAIRCL600 CL6002C10 1390015EA RUDDER MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07728SK 10192 RUDDER LIMIT FAULT MESSAGE. REPLACED NR 1 RUDDER LIMITER ACTUATOR IAW CRJ MM 27-25-03. OPERATIONAL CHECK GOOD. P/N OFF BA620-93490-3, S/N OFF 0535. 2L72 4F RTA21EA 20050701000382005070100038EA 2005 7 1 SWIA200515197 120050626A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLIGHT SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07441SW5190 5190 7602 RIGHT SPOILERON CAUTION MESSAGE. REPLACED RIGHT SIDE INBOARD SPOILERON PCU IAW 27-62-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050701000432005070100043EA 2005 7 1 A6WA200540218 120050622A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31423AW 7636 RT FS 621.00 ANGLE IS CRACKED .5 INCH LONG ON OB RADIUS. REPAIRED BY REMOVING DAMAGED SECTION OF ANGLE, FABRICATING ANGLES AND STRAP, INSTALLING REPAIR PART IAW MFG REO. (K) 2L72 4F4 FRTA21EA E15NE 20050701000452005070100045EA 2005 7 1 A6WA200540217 120050622A5320 THRESHOLD CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CARGO BAY CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31423AW 7636 CARGO DOOR THRESHOLD PLATE HAS A .2500 INCH CRACK AT FS 589.00, LBL 41.5. REPAIRED BY REMOVING DAMAGED SECTION OF FLOOR LANDING PERFORMING EDDY CURRENT INSP, PAINTING REPAIR AREA AND FILLED REDUNDANT HOLE IAW MFG REO. (K) 2L72 4F4 FRTA21EA E15NE 20050701000612005070100061CE 2005 7 1 JGV2005F00001 120050610A321116577 BEARING LEAR 35 35A 5170602CE MLG TRUNNION WORN B JGVRO OTHER O OTHER NRNOT REPORTED 1 CE09365N 300 FOUND WHILE TRYING TO SEE IF MLG STRUT COULD BE RE-SHIMMED TO GET RID OF THE PLAY IN THE BEARING. UPON STRUT REMOVED FOUND BEARINGS ON LT AND RT MLG FWD TRUNNIONS CRACKED WITH WISE THROUGH BEARING RACE. (K) 2L72 4F A10CE 20050705000012005070500001NE 2005 7 5 05FDEA01677 220050624A7200 TORQUE RING DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE ZONE 400 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25619FE 48770 NR 3 ENG, RIGHT FORWARD FRAME UPPER TORQUE RING CRACKED APPROXIMATELY 5 INCHES IN LENGTH. THRUST REVERSER REMOVED AND INSTALLED AS PER WORK CARD 78T3003-R AND WORK CARD 78T3903-R FOR WORK DETAILS. THRUST REVERSER ADJUSTMENT AND OPERATION CHECK CARRIED OUT AS PER WORK CARD 78T3903-R, GE NR 3 RT THRUST REVERSER DOOR - INSTALL FOR WORK DETAIL. 2L73 4F4 FRTA22WE E13NE 20050705000022005070500002NM 2005 7 5 05FDEA01654 120050622A5347 CARGO TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25619FE 48770 MAIN DECK CARGO COMPARTMENT FLOOR CARGO TRACK AT STA 1119, LBL 8.5, FOUND WITH CORROSION. CARRIED OUT REPAIR AS PER SRM 53-70-00 VOL I FIG 1. 2L73 4F RTA22WE 20050705000032005070500003NM 2005 7 5 05FDEA01665 120050623A5330 SKIN BOEING727 727233 138408ANM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25263FE 21625 AFT CARGO CORROSION ON FUSELAGE SKIN STA 1010, STR 29L. OUT OF LIMITS AREA CUT OUT, INSTALLED SRM REPAIR TO THE SKIN AT STA. 1010, STR 29L, REF SRM 53-30-3 PAGE 14E-14O FIG 3A 2L73 4F RTA3WE 20050705000042005070500004NM 2005 7 5 05FDEA01670 120050623A5320AFA7181509 SPLICE DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 MAIN DECK, LT LONGERON L-11 SPLICE BETWEEN STA 1641 TO STA 1661, FOUND CRACKED. REMOVED AND REPLACED PER SRM 51-33-01- VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2L73 4F RTA22WE 20050705000272005070500027NM 2005 7 5 UPS05444712 120050618A3350S135610A BATTERY PACK BOEING747 747121 1384871NM EMERGENCY LIGHTSINOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 PS EMERGENCY EXIT LIGHT IN OVERHEAD FWD OF LAVATORY COMES ON ONLY MOMENTARILY THEN GOES OUT. REPLACED EMERGENCY LIGHT BATTERY PACK PER M/M 33-51-07. OPS CHECK GOOD. 2L74 4F A20WE 20050705000302005070500030SO 2005 7 5 C2XA05SH055 120050602A531112010732001 FRAME EMB 145 EMB145LR 3260212SO FUSELAGE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713903 145479 FRAME 81 FOUND CHAFED AT 6 O'CLOCK POSITION. MX REMOVED DAMAGED AREA AND INSTALLED NESTED DOUBLER REPAIR IAW EC5330-01472 AND EMB 145 SRM 51-40-03. ACFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20050705000382005070500038NE 2005 7 5 ASMF200506018 220050617A73201853M33P06 EEC BOEING737 737* NM CFMINTCFM567CFM567B22 13802NE RT ENGINE FAILED W ASMFED ENGINE SHUTDOWN RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23851AM342 29363 891646 ACFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING RT ENGINE STARTING, ENGINE SHUT OFF BY ITSELF AT 20 PERCENT, STAR VALVE INDICATION FLASHING AND LOW OIL PRESS INDICATED ON 7 PSI (RED ZONE). EEC TEST PERFORMED AND 72-30102 INTERNAL EEC FAULT MESSAGE SHOWN IAW TASK 73-21-00700-804-F00. EEC CHANNEL CHANGED AND ENGINE WAS STARTED SHOWING UNSTABLE PARAMETERS. EEC REPLACED AND SOFTWARE LOADED IAW TASK 73-21-60-000-801-F00, 73-21-60-400-8001-F00 AND 75-21-00-700-804-F00 RESPECTIVELY, TESTED CORRECT. RT ENGINE STARTED IAW MM 73-21-12 / -60, ALL CORRECT. 2L72 4F4 FRTA16WE E00055EN 20050705000462005070500046NM 2005 7 5 AWXA200500717 120050612A55116552907501 SPAR BOEING737 73733A 1384673NM RT HORIZTL STAB CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 DURING C-21 CHECK, DISCOVERED RT HORIZONTAL STAB CHANNEL CRACKED ON AFT SPAR WEB AT STAB STATION 170. MX CUT OUT CRACKED SECTION ON AFT SPAR WEB AT STAB STATION 170 AND FABRICATED REPLACEMENT PARTS IAW BOEING 737-300 SRM 51-70-11-0 FIG 1. BONDED AND INSTALLED FABRICATED REPAIR PARTS IAW BOEING 737-300 SRM 51-70-11-0 FIG 1. 2L72 4F RTA16WE 20050705000492005070500049NM 2005 7 5 AWXA200500720 120050529A57536546430100 SKIN BOEING737 73733A 1384673NM RT INBD FLAP DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 DURING C-21 FOUND DISBONDED AREA ON LOWER SURFACE OF RT INBOARD FORE FLAP 11.25 INCHES FROM INBOARD END AND 10 INCHES FROM AFT EDGE. DIMENSIONS OF THE DISBONDED AREA MEASURED 10 BY 8 INCHES MAKING IT OUT OF LIMITS IAW BOEING 737-300 SRM 57-53-021-1 FIG 101. REMOVED AND REPLACED INBOARD FLAP IAW AMERICA WEST AIRLINES TASK CARD R3M27008. WORK FOR REMOVAL AND REPLACEMENT OF FLAP WAS DOCUMENTED ON NON-ROUTINE 5857780. 2L72 4F RTA16WE 20050705000512005070500051NE 2005 7 5 AWXA200500722 220050617A7200 ENGINE AIRBUSA319 A319132 3930340NM IAE V2524 V2524A5 NE NR 1 MALFUNCTIONED A AWXAC ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 WP28822AW 1410 DURING TAKEOFF AT T/O POWER SETTING, APPROX 1.04 EPR, ACFT VEERED LEFT. REJECTED TAKEOFF BEFORE FURTHER POWER. NO ABNORMAL INDICATIONS NOTED BUT SUSPECTED NR 1 ENG LAGGED NR 2 ENG IN SPOOLING UP. RAN ENGINES UP TO 70 PERCENT N1 PER MAINTENANCE CONTROL. ALL INDICATIONS NORMAL AND STATUS PAGE NORMAL. ATTEMPTED ANOTHER TAKEOFF WITH MAINTENANCE CONTROL CONCURRENCE. TAKEOFF WAS UNEVENTFUL. 2L72 4F4 FRTA28NM E40NE 20050705000642005070500064NM 2005 7 5 WRLA2005104 120050614A5511 RIB DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C04 CHECK, WHILE PERFORMING INSP PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE NR 14. 2L73 4F4 FRTA22WE E24NE 20050705000652005070500065EA 2005 7 5 SWIA200515159 120050604A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07919SW 7657 AFT EQUIPMENT BAY INTERCOSTAL CLIP CRACKED FS 625.00 STR 14R. FOUND AT C-CHECK INSPECTION. REPLACED CLIP IAW CRJ REO 601R-53-61-100 REV NC. 2L72 4F RTA21EA 20050705000742005070500074EA 2005 7 5 SWIA200515166 120050528A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07965SW 7871 RT FUSELAGE FLOOR SUPPORT ANGLE FS 621 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-61-117 REV "B" . 2L72 4F RTA21EA 20050705000852005070500085NM 2005 7 5 WRLA2005112 120050616A5511 RIB DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C04 CHECK, WHILE PERFORMING INSP PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE NR 29. 2L73 4F4 FRTA22WE E24NE 20050705000882005070500088NM 2005 7 5 WRLA2005115 120050616A5511 RIB DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C04 CHECK, WHILE PERFORMING INSP PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE NR 32. 2L73 4F4 FRTA22WE E24NE 20050705000902005070500090NM 2005 7 5 1290501 120050620A2913NAS16124 O-RING ABEX BOEING737 7377BC 1384509NM HYDRAULIC PUMP CUT E BJ6AA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 NE03129QS 259 K2129 30329 COMPLETE A-SYSTEM HYDRAULIC FLUID LOSS IN FLIGHT. REPLACED O-RING P/N NAS 1612-4 ON "A" SYSTEM ELECTRIC MOTOR DRIVEN HYDRAULIC PUMP BLANKING PLUG. RESERVOIR "A" RESERVICED AND LEAK CHECKED SATISFACTORY. A RECORDS REVIEW REVEALED THAT THIS PUMP WAS INSTALLED ON 1/31/05 AFTER REPAIR AT DELTA AIRLINES. THERE ALSO WAS AN ENTRY IN THE FLIGHT LOGBOOK ON 2/5/05 WHICH STATED THE "A" SYSTEM WAS LEAKING HOWEVER GROUND MAINTENANCE DID NOT FIND A LEAK AT THAT TIME AND THE AIRCRAFT WAS RETURNED TO SERVICE. THIS PUMP ACCUMULATED 259 HRS SINCE INSTALLATION BEFORE FAILURE. IT IS SUSPECTED THAT THE O-RING WAS DAMAGED AT DELTA AIRLINES DEPT 360 DURING BUILD UP. THIS SDR CONTROL NUMBER 1290501 IS CLOSED. 2L72 4F RTA16WE 20050705000912005070500091SW 2005 7 5 AC2A100978 120050520A2435427362425103 INTAKE DUCT BELL 427 427 1182207SW PWC PW207 PW207D NE STARTER/GEN TORN B AC2AK NONE O OTHER ININSP/MAINT 1 SO07427GT143 56044 NR 2 ENGINE STARTER/GENERATOR INTAKE DUCT FOUND TORN AT SCAT TUBE. DURING A 300 HR INSPECTION/REPLACED DUCT. 1G71 3U3 U R00001RCE42NE 20050705000932005070500093EA 2005 7 5 SWIA200515146 120050617A27604916406 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07435SW5409 5409 7555 AFTER FLIGHT SPOILER RETRACTION, RECEIVED FLIGHT SPOILER FAULT STATUS. REPLACED NR 1 SECU IAW 27-61-00. OPS CHECK GOOD. 2L72 4F RTA21EA 20050705000942005070500094EA 2005 7 5 SWIA200515147 120050618A274283963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07978SW2528 2528 7953 AP PITCH TRIM MESSAGE DISPLAYED NUMEROUS TIMES DURING FLIGHT. REPLACED HSTA AND MCU IAW CRJ MM 27-42-01 AND 27-42-05. OPS CHECK GOOD, PN: 7062-3 SN OFF: 1296. 2L72 4F RTA21EA 20050705000962005070500096SO 2005 7 5 SWIA200515149 120050614A3350 SOCKET EMB 120 EMB120ER 3260203SO EMERGENCY LIGHTSINOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07580SW 120348 EMERGENCY FLOOR LEVEL LIGHT INOPERATIVE ABEAM 2A. REPLACED ONE LIGHT FIXTURE EMERGENCY FLOOR LIGHTS. REPLACED FUSE IN RIGHT OVERHEAD PANEL. OPS CHECK GOOD. 2L72 4T RTA31SO 20050705000982005070500098SO 2005 7 5 SWIA200515151 120050611A3110 CIRCUIT BOARD EMB 120 EMB120ER 3260203SO INSTR LIGHTING MALFUNCTIONED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM07224SW 120294 SMOKE AND BURNING ODOR COMING FROM BACKUP BATTERY BACKLIGHTING PANEL. REPLACED BACK-UP BATTERY CIRCUIT BOARD AND PANEL. OPS CHECK GOOD. 2L72 4T RTA31SO 20050705000992005070500099EA 2005 7 5 SWIA200515152 120050614A3350 CHARGER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSMALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07969SW 7876 PAX DOOR/SERVICE DOOR FUSELAGE EMERGENCY LIGHTS INOPERATIVE (EXTERIOR). REPLACED FWD EMERGENCY LIGHT BATTERY CHARGER. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050705001002005070500100EA 2005 7 5 SWIA200515153 120050604A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07919SW 7657 FS 280 RT FLOORBEAM RBL 9.0 INBOARD AND OUTBOARD ATTACH CLIPS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLES IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13 & 51-23-00. 2L72 4F RTA21EA 20050705001012005070500101EA 2005 7 5 SWIA200515154 120050604A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07919SW 7657 FS 280 LEFT FLOORBEAM LBL 9.0 INBOARD AND OUTBOARD ATTACH CLIPS CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLES IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13, 51-23-00. 2L72 4F RTA21EA 20050705001042005070500104EA 2005 7 5 SWIA200515157 120050604A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07919SW 7657 CARGO PIT FLOOR SUPPORT ANGLE CRACKED AT FS 621.0 RBL 42.0, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-61-117 REV "B". 2L72 4F RTA21EA 20050705001052005070500105EA 2005 7 5 SWIA200515158 120050604A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07919SW 7657 AFT EQUIPMENT BAY INTERCOSTAL CLIP CRACKED FS 625.00 STR 14L. ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIP IAW CRJ REO 601R-53-61-100 REV NC. 2L72 4F RTA21EA 20050705001082005070500108NM 2005 7 5 USAA050701 120050517A532065728942 FLOOR SUPPORT BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19574US50136 23739 FOUND FLOOR SUPPORT CRACKED .75 INCH, FORWARD CARGO AIR DIST BAY BS 540 BL 0 O/B ANGLE FLOOR SUPPORT. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-40-02. (M) 2L72 4F RTA16WE 20050705001092005070500109NM 2005 7 5 USAA050700 120050517A532065525941 FLOOR SUPPORT BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19574US50136 23739 BFM - FOUND FLOOR SUPPORT CRACKED .5 INCH, FORWARD CARGO AIR DIST BAY BS 540 LBL "0", OUTBOARD ANGLE FLOOR SUPPORT. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-40-02. (M) 2L72 4F RTA16WE 20050705001102005070500110NM 2005 7 5 USAA050689 120050526A5315 FLOORBEAM BOEING737 7374B7 1384702NM FUSLEAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19445US40360 24863 CLT - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH, LBL 36 STATION 967. (M) 2L72 4F RTA16WE 20050705001142005070500114NM 2005 7 5 USAA050474 120050407A5420 LINK BOEING757 7572B7 1384964NM RT PYLON OUT OF ROUND A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19611AU40721 27123 CLT - FOUND UPPER LINK FITTING OUT OF ROUND, RT PYLON. REPAIRED OVERSIZED HOLE IN LINK, FABRICATED REPAIR BUSHING IAW EA 96400. (M) 2L72 4F RTA2NM 20050705001162005070500116NM 2005 7 5 USAA050505 120050414A5412 SHIM BOEING757 7572B7 1384964NM NR 1 PYLON MIGRATED A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19611AU 27123 BFM - FOUND PYLON MID BULKHEAD SHIM MIGRATION, NR 1 PYLON MID BULKHEAD SHIMS, UPPER, REPLACEMENT AND REAMNG AFT UPPER HOLE. ACCOMPLISHED PER EO 5402R022A PARTS 2/6. (M) 2L72 4F RTA2NM 20050705001212005070500121NM 2005 7 5 USAA050595 120050502A5313 STRINGER BOEING757 757225 1384959NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19608AU 22204 BFM - FOUND STRINGER CORRODED .750 INCH LONG BY .500 INCH WIDE BY .045 INCH DEEP, STRINGER 28R AT FS 1720. CUT OUT DAMAGED STRINGER PORTION, REPLACED WITH NEW SECTION AND SPLICE REPAIR PER SRM 53-00-3 FIG 201. (M) 2L72 4F RTA2NM 20050705001242005070500124EU 2005 7 5 USAA050635 120050427A5321F5367235800000 FLOOR PANEL AIRBUS330 A330323 3930335EU FUSELAGE DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW24199 0333 FOUND FLOOR PANEL DELAMINATED GREATER THAN 10 PERCENT, MAIN CABIN FLOOR PANEL 271PF. FABRICATED AND INSTALLED NEW FLOOR PANEL PER SRM 53-02-00. (M) 2L72 4F RTA46NM 20050705001252005070500125EU 2005 7 5 USAA050634 120050502A5321 FLOOR PANEL AIRBUS330 A330323 3930335EU FUSELAGE DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW 0333 BFM - FOUND FLOOR PANEL WITH DAMAGED AREA, MAIN CABIN FLOOR PANEL 252JG. FABRICATED AND INSTALLED FLOOR PANEL PER SRM 53-02-00. (M) 2L72 4F RTA46NM 20050705001272005070500127EU 2005 7 5 USAA050632 120050420A5320F5347823420100 FLOOR SUPPORT AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW24199 0333 BFM - FLOOR SUPPORT CORRODED 2 INCHES LONG BY .4 INCHES WIDE BY .045 INCHES DEEP, BETWEEN FRAME 75-78 Y=-450. INSTALLED NEW FLOORBOARD SUPPORT PER SRM 53-00-15, 51-42-00. LEVEL 2, TASK C534159-01. (M) 2L72 4F RTA46NM 20050705001302005070500130EU 2005 7 5 USAA050629 120050421A5315F5347821320100 FLOORBEAM AIRBUS330 A330323 3930335EU FUSLEAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW24199 0333 BFM - FOUND FLOORBEAM CORRODED 5 INCHES LONG BY 1 INCH WIDE BY .020 INCH DEEP, FRAME 73, Y-794.3 -Z240. REMOVED AND REPLACED WITH NEW PART PER SRM 53-00-15, 51-42-11. (M) 2L72 4F RTA46NM 20050705001312005070500131EU 2005 7 5 USAA050628 120050423A5310F5347801100500 BEAM AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA01672UW24199 0333 BFM - FOUND LONGITUDE BEAM ASSY CORRODED FIVE AREAS, 1.20 INCHES LONG, .300 INCHES WIDE, .050 INCHES DEEP, 3 INCHES LONG, 1.20 INCHES WIDE, .080, MAIN CABIN, B/T FRAME 79-80, Y-450. REMOVED AND REPLACED BEAM ASSEMBLY PER SRM 51-72-11, 51-43-11, 51-42-00. (M) 2L72 4F RTA46NM 20050705001342005070500134EU 2005 7 5 USAA050625 120050426A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW 0333 BFM - FOUND SEAT TRACK CORRODED 1 INCH BY 18 INCHES BY .032 INCHES, Y-1959 FRAME 53.4-53.5. FABRICATED AND INSTALLED SEAT TRACK SPLICE PER SRM 53-31-15, 51-22-00, 51-74-00. (M) 2L72 4F RTA46NM 20050705001362005070500136EU 2005 7 5 USAA050623 120050429A5320 FLOOR SUPPORT AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW24199 0333 BFM - FOUND FLOOR SUPPORT CORRODED 4 INCHES BY 1 INCH BY .048 INCH, Y 1456 AT FRAME 13B. FABRICATED AND INSTALLED FLOOR SUPPORT SPLICE PER SRM 51-74-00, 53-11-14, 51-42-11, 53-11-14. (M) 2L72 4F RTA46NM 20050705001422005070500142EU 2005 7 5 USAA050617 120050505A5340 TEE FITTING AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW24199 0333 BFM - FOUND TEE FITTING ANGLE CORRODED 2.5 INCHES LONG BY 1.8 INCHES WIDE BY .033 INCH DEEP, FRAME 39.1 FORWARD AC BAY. FABRICATED AND INSTALLED REPAIR PER EA 96525, SRM 51-74-00, 51-10-08. (M) 2L72 4F RTA46NM 20050705001432005070500143EU 2005 7 5 USAA050616 120050428A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW 0333 BFM - FOUND SEAT TRACK CORRODED 3.8 INCHES LONG BY .040 INCH WIDE BY .040 INCH DEEP, SEAT TRACK Y1959 FRAME 53.2-54. FABRICATED SEAT TRACK SPLICE PER SRM 51-74-00, 53-31-15, 51-23-00, 51-35-00. (M) 2L72 4F RTA46NM 20050705001442005070500144EU 2005 7 5 USAA050615 120050429A5347F5327584520000 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW24199 0333 BFM - FOUND SEAT TRACK CORRODED 1.3 INCHES LONG BY .305 INCH WIDE BY .030 INCH, .800 INCH LONG BY .400 INCH WIDE, AT FRAME 32-37 Y-450. REMOVED AND REPLACED SEAT TRACK PER SRM 51-74-00, 53-00-15, 51-44-11. (M) 2L72 4F RTA46NM 20050705001462005070500146EU 2005 7 5 USAA050613 120050426A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW24199 0333 BFM - FOUND SEAT TRACK CORRODED, Y-1959 AT FRAME 37. FABRICATED AND INSTALLED SEAT TRACK PER SRM 51-74-00, 53-00-15, 51-44-11, 51-21-11, 51-23-11. (M) 2L72 4F RTA46NM 20050705001472005070500147EU 2005 7 5 USAA050612 120050423A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW24199 0333 BFM - FOUND SEAT TRACK ASSEMBLY, FRAME 53.2 - 54, Y450. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER SRM 53-31-15, 51-23-11, 51-42-11. (M) 2L72 4F RTA46NM 20050705001482005070500148EU 2005 7 5 USAA050611 120050422A5347F5311181720000 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW 0333 BFM - FOUND SEAT TRACK CORRODED 1.60 INCH LONG BY 1.15 INCH WIDE BY .038 INCH DEEP, Y-450 FRAME 18. REMOVED AND REPLACED SEAT TRACK PER SRM 51-74-00, 53-11-15. (M) 2L72 4F RTA46NM 20050705001492005070500149EU 2005 7 5 USAA050610 120050429A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19672UW 0333 BFM - FOUND SEAT TRACK CORRODED 3.8 INCHES LONG BY .400 INCHES WIDE BY .0290, SEAT TRACK Y953 AT FRAME 34.5. FABRICATED AND INSTALLED SEAT TRACK SPLICE PER SRM 51-74-00, 53-00-15, 51-21-11, 51-40-11. (M) 2L72 4F RTA46NM 20050705001512005070500151EU 2005 7 5 USAA050608 120050405A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW 0333 BFM - FOUND SEAT TRACK CORRODED 2 INCHES BY .025 INCH, Y1456 AT FRAME 33. FABRICATED AND INSTALLED SEAT TRACK PER SRM 51-74-00, 53-00-15, 53-21-15, 51-42-11, 51-44-11, 53-21. (M) 2L72 4F RTA46NM 20050705001532005070500153EU 2005 7 5 USAA050606 120050423A5320BAC14963777075T6FLOOR SUPPORT AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW24199 0333 BFM - FOUND FLOOR SUPPORT CORRODED 6 INCHES LONG BY 2.5 INCHES WIDE BY .012 INCHES DEEP, AFT CARGO BETWEEN BS 727D AND BS 727E. REMOVED AND REPLACED PER SRM 53-60-53. (M) 2L72 4F RTA46NM 20050705001562005070500156EU 2005 7 5 USAA050603 120050510A5320F5332561620201 RAIL AIRBUS330 A330323 3930335EU FUSELAGE CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW24199 0333 BFM - FOUND HINGED RAIL CHAFED 1 INCH WIDE BY 1.5 INCHES LONG BY .040 INCH DEEP, MAIN CABIN SEAT TRACK, FRAME 39.8; Y-953. REMOVED AND REPLACED HINGED RAIL PER SRM 53-31-15, 51-42-11. (M) 2L72 4F RTA46NM 20050705001572005070500157EU 2005 7 5 USAA050602 120050423A5320F5347721420200 RAIL AIRBUS330 A330323 3930335EU FUSELAGE CHAFED A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19672UW24199 0333 BFM - FOUND RAIL CHAFED 4 INCHES LONG BY 1 INCH WIDE BY .034 IN DEEP AND 4 INCHES LONG BY 1 INCH WIDE BY .037 INCH DEEP, MAIN CABIN, FRAME 69; Y 450/ FRAME 70-71; Y450. REMOVED AND REPLACED RAIL PER SRM 53-00-15; 51-73-00; 51-44-00. (M) 2L72 4F RTA46NM 20050705001592005070500159EU 2005 7 5 USAA050656 120050503A5347 SEAT TRACK AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19105UW 0868 PIT - FOUND OUTBOARD SEAT TRACK FLOORBEAM CORRODED 1 INCH DIAMETER IN 5 AREAS, OUTBOARD SEAT TRACK, FLOORBEAM AT Y1292L. CORROSION LEVEL 2; TASK JA-220-53500. FOUR AREAS BLENDED, 1 AREA HAD CORROSION CUT OUT AND REPAIR INSTALLED PER SRM 53-11-15. (M) 2L72 4F RTA28NM 20050706000022005070600002EU 2005 7 6 USAA050659 120050501A5315 FLOORBEAM AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19105UW13610 0868 PIT - FOUND FLOORBEAM CORRODED TWO .5 INCH AREAS, AROUND SCREW HOLES, FLOORBEAM Y1292 RT AT C68. CORROSION LEVEL 2, TASK JA-260-53500. DEFECTIVE PART REPLACED WITH IDENT PART PR D5347218920400. (M) 2L72 4F RTA28NM 20050706000042005070600004EU 2005 7 6 USAA050655 120050502A53151160826 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA01715UW17968 1051 BFM - FOUND FLOORBEAM CORRODED 3 INCH BY 3 INCH AREA, TOP OF FLOORBEAM AT FRAME 66 AND 50 INCHES LEFT OF CENTER. PART REPLACED PER D53472780. (M) 2L72 4F RTA28NM 20050706000052005070600005EU 2005 7 6 USAA050661 120050502A5315 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19715UW 1051 FOUND FLOORBEAM CORRODED 1 INCH BY 2 INCHES AND 1 INCH BY 3 INCHES, LEFT FLOORBEAM BETWEEN FRAME 66-69 APPROX 50 INCHES FROM CENTER. DEFECTIVE PART REPLACED WITH IDENT PART. (M) 2L72 4F RTA28NM 20050706000062005070600006EU 2005 7 6 USAA050677 120050519A5320D5347112420100 WEB AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19716UW18358 1055 PIT - FOUND WEB CORRODED 3 INCH BY 5 INCH, Y 48 INCHES BETWEEN FRAME 69-70 FLOOR LEVEL 23.5. REMOVED AND REPLACED WEB WITH IDENTICAL PART NUMBER. (M) 2L72 4F RTA28NM 20050706000082005070600008EU 2005 7 6 USAA050679 120050523A5310D5347208900400 BEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19716UW 1055 PIT - FOUND BEAM CORRODED 2 FT AND 20 INCHES, Y 52 INCHES BETWEEN FRAME 68-69. REMOVED AND REPLACED PER SRM 51-72-11. (M) 2L72 4F RTA28NM 20050706000092005070600009EU 2005 7 6 USAA050680 120050523A5310D5347209001000 BEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19716UW18358 1055 PIT - FOUND BEAM CORRODED 1 INCH BY 2 INCHES, Y-49 AT FRAME 66 TOP OF FLANGE. REMOVED AND REPLACED PER SRM 51-72-11. (M) 2L72 4F RTA28NM 20050706000112005070600011EU 2005 7 6 USAA050682 120050524A5320D5347228400800 FLOOR SUPPORT AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19716UW18358 1055 PIT - FOUND FLOOR SUPPORT CORRODED 1 INCH AREA .030 INCH DEEP, TOP FLANGE OF FLOOR SUPPORT AT -Y20, FRAME 66, AFT CABIN AREA. REMOVED AND REPLACED FLOOR SUPPORT, BOLTED INSTALLATION PER SRM 53-11-14. (M) 2L72 4F RTA28NM 20050706000142005070600014NM 2005 7 6 USAA050639 120050510A575465C2660223 WEDGE BOEING737 7374B7 1384702NM SLAT DEBONDED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US 24781 CLT - FOUND SLAT WEDGE DEBONDED 4 INCHES BY 3 INCHES, SLAT WEDGE INBOARD TRAILING EDGE. REMOVED DAMAGED CORE, INSTALLED NEW CORE, NEW FILLER AND DOUBLER IAW TR 57-42-02. (M) 2L72 4F RTA16WE 20050706000162005070600016NM 2005 7 6 USAA050641 120050510A5514 BEAM BOEING737 7374B7 1384702NM HORIZONTAL STAB DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19433US 24555 CLT - FOUND BEAM STRUCTURE WITH HOLE .25 INCH, HORIZ STAB LOBE T/E BEAM. DAMAGE TRIMMED AND REPAIR DOUBLER, INSTALLED IAW EA 96571 BOEING 737 SRM 55-10-13. (M) 2L72 4F RTA16WE 20050706000172005070600017NM 2005 7 6 USAA050642 120050512A5320 CLIP BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19445US40364 24863 CLT - FOUND TIE CLIP CRACKED .5 INCH, STATION 344, 45 INCHES ABOVE FLOOR. REPLACED WITH FABRICATED PART PER DRAWING NR 69-38939-6. (M) 2L72 4F RTA16WE 20050706000182005070600018NM 2005 7 6 USAA050643 120050513A5754 SKIN BOEING737 7374B7 1384702NM NR 6 SLAT DEBONDED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US 24781 CLT - FOUND NR 6 SLAT SURFACE DISBOND 2 INCHES BY 5 INCHES, NR 6 SLAT OUTBOARD T/E. ACCOMPLISHED COMPOSITE REPAIR IAW EA 96487. (M) 2L72 4F RTA16WE 20050706000192005070600019NM 2005 7 6 USAA050650 120050515A5340 STRINGER CLIP BOEING737 7374B7 1384702NM FUSELAGE WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19445US40360 24863 CLT - FOUND TIE CLIP WITH WORKING FASTENER, STRINGER TIE CLIP STRINGER 11R STATION 867. REMOVED WORKING RIVETS AND ENLARGED HOLES IAW SRM 51-40-05 AND INSTALLED HI LOCKS IAW 51-40-03. (M) 2L72 4F RTA16WE 20050706000222005070600022NM 2005 7 6 USAA050662 120050515A5320US655169821F SPLICE BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19574US 23739 BFM - FOUND STRINGER SPLICE CRACKED .5 INCH, RT CEILING AT STATION 987 STRINGER 4. FABRICATED PARTS AND INSTALLED FABRICATED SPLICE AND SHEAR TIE IAW SRM 51-40-02. (M) 2L72 4F RTA16WE 20050706000242005070600024NM 2005 7 6 USAA050664 120050515A5320US6551698OIF SPLICE BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19574US50136 23739 PIT - FOUND STRINGER SPLICE CRACKED 1 INCH, LEFT AFT CABIN AT STATION 907 STRINGER 4. FABRICATED PARTS, INSTALLED SPLICE AND SHEAR TIE PER SRM 51-40-02. (M) 2L72 4F RTA16WE 20050706000252005070600025NM 2005 7 6 USAA050665 120050513A575465026601169 SKIN BOEING737 737301 1384611NM SLAT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19574US50136 23739 BFM - FOUND NR 1 LE FLAP CRACKED .125 INCH, WS 505, NR 1 LE FLAP LOWER SKIN. CUT OUT DAMAGED AREA, INSTALLED NEW DOUBLER AND FILLER PER SRM 57-43-01, 51-40-02, 51-21-00, 51-20-05. (M) 2L72 4F RTA16WE 20050706000262005070600026NM 2005 7 6 USAA050666 120050520A5320 SPLICE BOEING737 7374B7 1384702NM FUSELAGE DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19445US 24863 CLT - FOUND STRINGER SPLICE MISSING RIVETS, STRINGER 4R STATION 360. REMOVED AND REPLACED STRINGER SPLICE IAW SRM 51-10-02 AND 51-40-02. (M) 2L72 4F RTA16WE 20050706000282005070600028NM 2005 7 6 USAA050668 120050520A552265C25746131A SKIN BOEING737 7373B7 1384580NM LT ELEVATOR DEBONDED A USAAK NONE O OTHER ININSP/MAINT 1 EA19373US56099 22952 CLT - FOUND ELEVATOR SKIN DISBOND 1 INCH, LEFT ELEVATOR LOWER SURFACE 6.2 INCHES FROM THE OUTBOARD EDGE. COMPOSITE REPAIR IAW SRM 51-70-17. (M) 2L72 4F RTA16WE 20050706000302005070600030NM 2005 7 6 USAA050670 120050520A5340 STRINGER CLIP BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19445US40360 24863 CLT - FOUND TIE CLIP CRACKED .250 INCH, STATION 500E STRINGER 4R. REPLACED TIE CLIP IAW SRM 51-10-02. (M) 2L72 4F RTA16WE 20050706000322005070600032NM 2005 7 6 USAA050672 120050523A5315 FLOORBEAM BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US 24781 CLT - FOUND FLOORBEAM STRAP CRACKED .5 INCH, BS 312, RBL 48 WL 200, BELOW CABIN FLOORBEAM. REMOVED DAMAGED PART, DRILLED AND INSTALLED NEW STRAP IAW SRM 51-10-02. (M) 2L72 4F RTA16WE 20050706000332005070600033NM 2005 7 6 USAA050673 120050523A53306545871523 SKIN BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19446US39187 24873 CLT - FOUND SKIN CRACKED .5 INCH, FORWARD GALLEY SERVICE DOOR UPPER AFT CORNER. INSTALLED DOUBLER AND FILLER IAW SRM 52-00-01. (M) 2L72 4F RTA16WE 20050706000342005070600034NM 2005 7 6 USAA050674 120050522A5753 SKIN BOEING737 7374B7 1384702NM LT WING TE FLAP DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19446US39206 24873 CLT - FOUND FLAP DELAMINATED, .5 INCH BY .5 INCH, LOWER SURFACE OF LT WING INBOARD AFT FLAP. COMPOSITE REPAIR IAW 737 SRM 57-53-02 AND 51-70-10. (M) 2L72 4F RTA16WE 20050706000352005070600035NM 2005 7 6 USAA050675 120050522A57536546431286A SKIN BOEING737 7373B7 1384580NM TE FLAP GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19373US56099 22952 CLT - FOUND FLAP SKIN GOUGED 1 INCH BY .5 INCH, TOP SKIN OF RIGHT OUTBOARD FOREFLAP. COMPOSITE REPAIR IAW 737-3 SRM 57-53-02 DETAIL XV, TABLE VI. (M) 2L72 4F RTA16WE 20050706000372005070600037NM 2005 7 6 DHL2005741601 120050512A5330 SKIN BOEING727 7272Q9 138448MNM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 CORROSION ON INNER FUSELAGE SKIN, FWD PIT, BETWEEN BS 550 - 565, STR 28R. BLENDED OUT CORR MAT LOSS .055 AT BS 550 AND .050 BS 570 AND BOTH FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-30-1 FIG 1. CUT OUT DAMAGED 2 LOCATIONS BS 552 DIM 3.625 X 1.25 INCH & BS 568 SIZE 5.125 X 1.5 INCH IAW B727 SRM 53-30-3 FIG 1. REMOVED EXISTING DOUBLER SIZE 33.5 X 24 INCH IAW B727 SRM 53-30-2 FIG 1. FABRICATED DOUBLER FROM 2024-T3 .0.125 SIZE 69 X 33.5 INCH PO 9002329 IAW COTNEY AEROSPACE EA ED 700-1 REV:IR. TREATED AND PRIMED PARTS & AREA IAW COTNEY AEROSPACE EA, ED 700-1 REV IR. INSTALLED REPAIR PART IAW B727 SRM 51-30-2. 2L73 4F RTA3WE 20050706000382005070600038NM 2005 7 6 DHL2005741608 120050603A5410 DUCT BOEING727 7272Q9 138448MNM NR 2 INTAKE DEFECTIVE A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 REPAIR OF NR 2 ENG S-DUCT INNER SKIN AREA. CUT OUT 5 EA HAT CHANNEL SECTION ON OUTER RING OF THE S-DUCT FOR ACCESS TO THE 5 REPAIRS WITH BLIND FASTENERS FROM BS 1223-1275 AND REPLACED WITH SOLID FASTENERS IAW B727 SRM 51-30-2 FIG 7. FABRICATED HAT CHANNEL REPAIRS MAT'L 7075-T6 .050 PO 9002126 FOR BS 1275 2 EA 9.5 X 4.5 INCH BS 1265 2 EA 8.5 X 4.5 INCH BS 1255 2 EA 8.5 X 4.375 INCH BS 1243 2 EA 9.5 X 4.5 INCH AND 1223 2 EA 8.5 X 4.5 INCH BL 0.0 IAW B727 SRM 54-10-3 FIG 10. TREATED AND PRIMED ALL REPAIR ZEE ANGLES IAW B727 SRM 51-10-2. INSTALLED ALL REPAIR ZEE ANGLES IAW B727 SRM 54-10-3 FIG 10. 2L73 4F RTA3WE 20050706000402005070600040NM 2005 7 6 DHL2005741597 120050626A2730401602728A COMPUTER BOEING727 7272Q9 138448MNM ELEVATOR FEEL LEAKING A DHLAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO01741DH 21931 DURING A HEAVY MAINTENANCE EXCEPTANCE FLIGHT, THE AIRCRAFT LOST A-SYSTEM HYDRAULICS, ALL QUANTITY LOST, ABNORMAL PROCEDURE COMPLETED, HYD FLUID SHUTOFF VALVE CLOSED FOR 1.5 MINUTES APPROX. REMOVED AND REPLACED ELEVATOR FEEL COMPUTER IAW B727 MM 27-30-101, LEAK CHECK GOOD IAW B727 MM 27-30-0, OP'S CHECK GOOD IAW B727 MM 27-30-101. 2L73 4F RTA3WE 20050706000422005070600042NM 2005 7 6 DHL2005741604 120050513A5311 FRAME BOEING727 7272Q9 138448MNM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 STRUCTURE SUPPORT FRAMES AT JACK POINT FROM BS 350 TO 360 IS CORRODED. REMOVED FWD & AFT FRAME AT BS 351 STR 22 RT IAW B727 SRM 51-30-2. FWD & AFT FRAME FOUND TO BE CORRODED BEYOND ALLOWABLE LIMITS. FAB FWD FRAME FROM 7075T6 .071 29 X 4.5 INCH PO9002118 & AFT FRAME FROM 7075T6 .063 40 X 13 INCH PO 50962574 IAW B727 SRM 53-10-1 FIG 1 & 53-10-2. TREATED & PRIMED 2 EA FRAMES IAW B727 SRM 51-10-2. INSTALLED FWD & AFT FRAMES AT BS 351 IAW B727 SRM 51-30-2. 2L73 4F RTA3WE 20050706000432005070600043EU 2005 7 6 06242005 120050624A32465006227 WHEEL SAAB SF340 340B 7860101EU NLG VIBRATION A NSVAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 EA27306CE 203 NOSE WHEEL SHIMMY ON TAKEOFF. 2L72 4T RTA52EU 20050706000452005070600045NM 2005 7 6 DHL2005741598 120050512A5330 SKIN BOEING727 7272Q9 138448MNM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DENT ON RT FUSELAGE STA 1140 BELOW STR 25R. EVALUATED DENT AT BS 1140 STR 25R IS BEYOND ALLOWABLE LIMITS IAW B727 SRM 53-30-1 FIG 1, CUT OUT DAMAGED SECTION, DIM 4 X 2 INCH IAW B727 SRM 53-30-3 FIG 1. FABRICATED REPAIR DOUBLER 2024-T3 .071 DIM 13 X 8 INCH IAW B727 SRM 53-30-2 FIG 4 AND 53-30-3 FIG 1, TREATED AND PRIMED, PART AND AREA IAW B727 SRM 51-10-2, INSTALLED REPAIR DOUBLER IAW B727 SRM 53-30-3 FIG 1. 2L73 4F RTA3WE 20050706000472005070600047 2005 7 6 ASMF200506029 420050628A23406861000001 HANDSET DOUG MD80 MD83 3023681NM COCKPIT FAILED W ASMFD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SW23881LF2432 53051 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF FLIGHT INTERPHONE FROM CABIN TO FLIGHT DECK OF 3RD STATION INOPERATIVE. INTERPHONE WAS DISCONNECTED AND DEFERRED IAW MEL 23-8. DURING OVERNIGHT SERVICE, HANDSET NR 4 WAS REPLACED IAW MM 23-50-00, TESTED CORRECT. DEFERRED REPORT WAS CLOSED. 2L72 4F RT 20050706000542005070600054NM 2005 7 6 P5CA0501369 120050622A5520 STRUCTURE BOEING747 747230B 1384889NM RT ELEVATOR CRACKED A P5CAO OTHER O OTHER ININSP/MAINT 1 EA15509MC 21221 RIGHT O/B ELEVATOR FOUND CRACKED AT LEADING EDGE AREA I/B OF ELEVATOR STATION 256.811 AND BRACKET CRACKED AT ELEVATOR STATION 256.811. RIGHT O/B ELEVATOR REPAIRED PER BOEING INSTRUCTIONS 1-1N575W AND FAA FORM 8100-9. 2L74 4F A20WE 20050706000552005070600055NM 2005 7 6 P5CA0501370 120050622A5320 VERTICAL BEAM BOEING747 747230B 1384889NM FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 EA15509MC 21221 FOUND 2 CRACKS AT VERTICAL WEB BEAM BS 280 AND ONE CRACK AT BS 320. VERTICAL WEB BEAM REPAIR ACCOMPLISHED PER BOEING MESSAGE 1-1MEI6G AND FAA FORM 8100-9. 2L74 4F A20WE 20050706000582005070600058NM 2005 7 6 DHL2005741605 120050516A5754 RIB BOEING727 7272Q9 138448MNM NR 7 SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 NR 7 SLAT O/B RIB AT ACTUATOR ROD END IS CRACKED. REMOVED NR 7 SLAT RIB O/B OF ROD END IAW B727 SRM 51-30-2 FIG 7 LATE ENTRY, REMOVED ACCESS PANELS IAW B727 SRM 51-30-2 FIG 7. LOCATED, DRILLED AND INSTALLED NEW RIB PN 65-17310-4 PO 5096251 IAW B727 SRM 51-30-2 FIG 1 AND 57-50-2 FIG 2. RE-INSTALLED ACCESS PANELS IAW B727 SRM 51-30-2. 2L73 4F RTA3WE 20050706000592005070600059NE 2005 7 6 ALG2005F00035 120050520A7334955017200 PRESSURE SWITCH SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL2B NE FUEL CONTROL INOPERATIVE E ALGAA UNSCHED LANDING J WARNING INDICATION HOHOVERING 1 SW03866AL653 760562 20662TEC AT A HOVER, THE NR 2 ENGINE FUEL FILTER LIGHT CAME ON DURING LIFT OFF, RETURNED TO PAD. MAINTENANCE REMOVED NR 2 ENGINE FUEL FILTER PRESSURE SWITCH AND REPLACED WITH A NEW SWITCH, WORK DONE IAW MM AND GROUND RUN LEAK CHECK WAS GOOD. (K) 1G72 3U3 UNCH1NE E00054EN 20050706000692005070600069SO 2005 7 6 TZR2005F00024 220050610A8530ACE520T101 CYLINDER CESSNA402 402B 207590PCE CONT O520 GTSIO520C 17032SO RT ENGINE CRACKED E TZRAO OTHER O OTHER NRNOT REPORTED 1 SW05406TE317 402B1366 CRACK IS TYPICAL FOR THESE CYLINDERS. RT ENGINE, NR 3. (SW05200509364) (K) 1L72 3O3 O A7CE E7CE 20050706000782005070600078SW 2005 7 6 ALG2005F00033 120050527A6520 CHIP DETECTOR BELL 407 407 1182206SW ALLSN 250C 250C47B GL TRANSMISSION CONTAMINATED E ALGAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW03527AL 53211 DURING TAKE OFF, TRANSMISSION CHIP LIGHT CAME ON DURING TAKEOFF, RETURNED TO DEPARTURE. MAINTENANCE REMOVED ALL CHIP PLUGS, FOUND NORMAL WEAR LINT LIKE PARTICLE ON LOWER PLUG. CLEANED PLUGS AND A 30 MINUTE PENALTY RUN WAS PERFORMED ALL CHECKS WERE GOOD. WORK WAS DONE IAW MM. (K) 1G71 3U3 UO H2SW E1GL 20050706000792005070600079NE 2005 7 6 ALG2005F00034 120050604A261230326E7 AMPLIFIER SKRSKYS76 S76A 8143006NE TMECA ARRIELARRIEL1S1 60030NE FIRE CONTROL UNSERVICEABLE A ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03521AL 760132 BEFORE ENGINE START CHECK OF THE FIRE DETECTION SYSTEM, TEST HAD NO TONE. MAINTENANCE REMOVED FIRE CONTROL AMPLIFIER SN 11595 AND INSTALLED SERVICEABLE CONTROL AMPLIFIER 2329. ALL WORK WAS DONE IAW MM. OPS CHECK WAS GOOD. (K) 1G72 3U3 U H1NE E19EU 20050706000852005070600085EU 2005 7 6 DJFA2005115 120050623A2750 SPRING BRAERODH125 BAE125800A 1500285EU GARRTTTFE731TFE731* 01518WP TE FLAPS CONTAMINATED E DJFAL ABORTED APPROACH F FLT CONT AFFECTED APAPPROACH 1 EA23801CW 258012 ON APPROACH, FLAPS WERE SELECTED TO 15 DEGREES WHILE AC WAS SLOWED. NO FLAP EXTENSION WAS INDICATED. CREW DECLARED EMERGENCY DUE TO FAILURE OF FLAPS. AC WAS DIVERTED, WHILE ON APPROACH, FLAPS WERE SUCESSFULLY EXTENDED. AC, MADE AN UNEVENTFUL LANDING. MAINT CHECKED FLUID LEVEL IN GEARBOXES, FLAP CONTROL UNIT. ALL LEVELS WERE FOUND TO BE FULL. SYS CABLE TENSION WAS CHECKED FOUND TO BE WITHIN LIMITS. LT AND RT SYNCHRONIZER, POSITION INDICATION TRANSMITTER, OPS CHECKED NORMAL. SPRING DRUM BEARINGS WERE CHECKED FOR LOOSENESS, OPS CHECKED NORMAL. BLUE WATER WAS FOUND IN SPRING DRUM AREA. AREA WAS CLEANED AND A FUNCTIONAL TEST OF FLAP CNTRL SYS WAS PERFORMED. SYS OPS WERE NORMAL. AC WAS RETURNED TO SERVICE. 2L72 4F4 FRTA3EU E6WE 20050706000862005070600086CE 2005 7 6 CIEA200500007 120050628A3520C3512000 OXYGEN MASK BEECH 200 B200 1152922CE CABIN MISMANUFACTURED E CIEAO OTHER W INADEQUATE Q C CLCLIMB 1 NM03203LG7502 BB926 DURING THE CLIMB THE CABIN LOST PRESSURIZATION. (NOTE: SEE SEPARATE SDR ON THE PRESSURIZATION ISSUE). AS A RESULT OF THE PRESSURIZATION LOSS THE OXYGEN MASKS DROPPED. ONE OF THE PASSENGERS HAD AN ALLERGIC REACTION SIMILAR TO A LATEX ALLERGIC REACTION. IF THE OXYGEN MASKS ARE OF A LATEX MATERIAL, THIS COULD HAVE VERY SERIOUS EFFECTS ON SOME PASSENGERS. THIS PASSENGER WAS FAMILIAR WITH THE REACTION TO LATEX AND NO FURTHER PROBLEM RESULTED, AS THE AIRCRAFT WAS WELL BELOW 12,000 FEET WHEN THE REACTION STARTED. 1L72 4T A24CE 20050706000872005070600087EU 2005 7 6 06232005 120050623A2611 SMOKE WARNING SAAB SF340 340B 7860101EU E/E BAY FALSE INDICATIONA NSVAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 EA27239CJ 239 AVIONICS SMOKE LIGHT ILLUMINATED IN FLIGHT. 2L72 4T RTA52EU 20050706000882005070600088NM 2005 7 6 USAA050690 120050526A5315 FLOORBEAM BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19445US40360 24863 CLT - FOUND FLOORBEAM CORRODED 2 INCH BY 3 INCH, LBL 5 STATION 967 FLOORBEAM. INSTALLED NEW T-CAP IAW SRM 53-00-51. (M) 2L72 4F RTA16WE 20050706000902005070600090NM 2005 7 6 DL757050332 120050623A2432246001095 BATTERY BOEING757 757232 1384965NM E/E BAY OVERHEATED A DALAO OTHER MB OVER TEMP SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27620DL 22910 UNUSUAL ODOR IN COCKPIT NOTICED JUST PRIOR TO PUSH BACK . FOUND APU BATTERY AT ZERO VOLTS AND OVERHEATED. REPLACED APU BATTERY AND APU BATTERY CHARGER. 2L72 4F RTA2NM 20050706000912005070600091NM 2005 7 6 DL73S050330 120050620A5330654577518 SKIN BOEING737 737247 138448DNM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27245WA 23519 FUSELAGE, SKIN, STA 727B, STRINGER 18R AND 19R SKIN CRACK. FATIGUE CRACK AT CHEM-MIL LINE. SKIN CRACK WAS FOUND DURING INSPECTION FOR CHEM-MIL LINE CRACKS NEAR AN EXISTING REPAIR. ADJACENT REPAIR WAS REMOVED AND A SINGLE REPAIR ENCOMPASSING BOTH DAMAGE LOCATIONS WAS INSTALLED. THE ERA INSTALLS A SINGLE REPAIR DOUBLER OVER BOTH LOCATIONS PER 737 SRM 53-30-3 FIGURE 48 DETAIL IX. ERA 089987-14AD REV B. 2L72 4F A16WE 20050706000922005070600092NM 2005 7 6 DLM88050329 120050618A3320D77311001 BALLAST DOUG MD88 MD88 3023688NM SEAT 37DE BURNED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27944DL 49817 ARRIVED IN ATL WITH AN INBOUND WRITE UP THAT READ, ON TAKEOFF RECEIVED BURNING SMELL THROUGHOUT CABIN AND COCKPIT. DISSIPATED WITHIN A FEW MINUTES. IT RETURNED 2 HRS LATER AT CRUISE FOR A FEW MINUTES (SECURED GALLEY POWER). UNABLE TO LOCATE SOURCE. RETURNED 3RD TIME BRIEFLY ON APPROACH, AFTER TROUBLE SHOOTING PER OPN 5088, FOUND THE ODOR COMING FROM INOP BALLAST AT SEAT 37DE. AFTER OPN OF PACKS, APU AND ENGS NO FURTHER ODORS NOTED. BALLAST P/N D773-11-001 AND S/N 4666 WAS CHANGED. 2L72 4F RTA6WE 20050706000932005070600093NM 2005 7 6 DL76S050328 120050617A5330 SKIN BOEING767 767332 1382001NM FUSELAGE LIGHTNING STRIKEA DALAK NONE O OTHER ININSP/MAINT 1 SO27136DL19852 23146 0 LIGHTENING STRIKE BLEND OUT AT STA 390 STR 12L BEYOND LIMITS REF SRM 53-00-01 FIG 101. SKIN REPAIRED PER SRM 53-00-01 FIG 201 CAT B REPAIR REPEAT INSPECTIONS PER SRM 53-00-01 FIG 201. AIRCRAFT LOG ITEM F744553. 2L72 4F RTA1NM 20050706000952005070600095NM 2005 7 6 05FDEA01715 120050628A3210 SUPPORT ANGLE BOEING727 727200 138407ENM LT MLG CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25263FE 21625 LT MLG FWD TRUNNION I/B SUPPORT ANGLE IS CHAFED ON LWR EDGE. REPAIR (BLENDED), STRESS RELIEVED AND REFINISHED LT MLG FWD TRUNNION SUPPORT ANGLE ON LWR EDGE IAW SRM 51-10-1, SOPM 20-10-03 AND FED EX EA 7-5710-86323 REPAIR WITHIN LIMITS IAW EA - 7-5710-86323. 2L73 4F RTA3WE 20050706000982005070600098NM 2005 7 6 05FDEA01740 120050629A5347 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 CABIN, ALONG STA 1821 TO STA 1887 LBL 27.75 SEAT TRACK CROWN AND BASE FOUND CORRODED. CARRIED OUT REPAIR AS PER SRM 53-70-00. [CLOSED] 2L73 4F RTA22WE 20050706001042005070600104NM 2005 7 6 05FDEA01724 120050628A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25619FE 48770 RT BARREL NUT HOLE NR 17R. FOUND OUT OF LIMIT AFTER CORROSION REMOVAL. REPAIRED AS PER FEDEX EA 1-5510-83024. 2L73 4F RTA22WE 20050706001052005070600105NM 2005 7 6 05FDEA01725 120050628A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25619FE 48770 RT BARREL NUT HOLE NR 29R FOUND OUT OF LIMIT AFTER CORROSION REMOVAL. REPAIRED AS PER FEDEX EA 1-5510-83026. 2L73 4F RTA22WE 20050706001072005070600107NM 2005 7 6 05FDEA01727 120050628A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25619FE 48770 LT BARREL NUT HOLE NR 16L FOUND OUT OF LIMIT AFTER CORROSION REMOVAL. REPAIRED AS PER FEDEX EA 1-5510-83025. 2L73 4F RTA22WE 20050706001082005070600108NM 2005 7 6 05FDEA01728 120050628A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25619FE 48770 LT BARREL NUT HOLE NR 22L FOUND OUT OF LIMIT AFTER CORROSION REMOVAL. REPAIRED AS PER FEDEX EA 1-5510-83025. 2L73 4F RTA22WE 20050706001112005070600111NM 2005 7 6 05FDEA01719 120050628A5753 HINGE FITTING BOEING727 727200 138407ENM RT WING TE FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25203FE 22925 AFT FLAP RT INBD AT HINGE FITTING 111.0 FROM INBD, LE LWR SKIN CRACKED (.450 LONG) REPLACED FLAP ON W/C 76C071-00 2L73 4F RTA3WE 20050706001132005070600113NM 2005 7 6 05FDEA01742 120050629A5347 SEAT TRACK DOUG MD11 MD11 3023602NM FUSLEAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 CABIN, AT STA 1837 RBL 98.5 SEAT TRACK BASE FOUND CORRODED. CARRIED OUT REPAIR AS PER SRM 53-70-00 AND INSTALLED AS PER SRM 51-31-01. [CLOSED] 2L73 4F RTA22WE 20050706001162005070600116NM 2005 7 6 05FDEA01745 120050629A2910 HYDRAULIC SYSTEM BOEING727 727100 1384036NM A-SYSTEM LEAKING A FDEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO25180FE 18867 AT ROTATION A-SYS HYD FLUID WENT TO ZERO, RAN QRH, KEPT GEAR DOWN AND FLAPS 15, HAD A-SYS FLUID SHUT OFF SWITCHED OFF 23 MIN. DECLARED EMERGENCY. R & R INBOARD FLAP FLOW LIMITING VALVE PER MM. R & R NR 1 & 2 ENGINE PUMP CASE DRAIN FILTERS PER MM. R & R BOTH SYS A-PRESS FILTERS PER MM. SERVICED HYD SYS TO FULL AND LEAK CHECKED ALL FILTERS AND VALVE. 2L73 4F RTA3WE 20050630000982005063000098NM 2005 6 30 WRLA200598 120050614A5512 PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C04 CHECK, WHILE PERFORMING INSP PER EO 02-5510-098, FOUND CORROSION IN HST LT BARREL NUT HOLE NR 29. 2L73 4F4 FRTA22WE E24NE 20050630001032005063000103WP 2005 6 30 ABXA050163 120050616A5320591140753 THRESHOLD DOUG DC9 DC932 3022066WP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 SERVICE DOOR THRESHOLD SKIN BULGING AT STA 176, RIGHT BUTT LINE 58. REPAIRED AREA IAW DC-9 SRM 51-10-2. 2L72 4F A6WE 20050630001062005063000106SO 2005 6 30 C2XA05TY047 120050623A531114523182403 FRAME EMB 145 EMB145ER 3260211SO FUSELAGE DAMAGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714947 145054 TYS, DURING A SCHEDULED INSPECTION ELONGATED HOLES WAS FOUND ON FRAME 19A AT STRINGER 16R. MAINTENANCE REPAIRED FR-19A BY CUTTING OUT THE DAMAGED AREA, FABRICATING A FILLER AND DOUBLER AND INSTALLING IAW-EC5310-01340. 2L72 4F RTT00011AT 20050630001092005063000109NM 2005 6 30 USAA200506003 120050624A5330 SKIN BOEING737 737301 1384611NM FUSLAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19334US 23231 A 1.5 INCH CRACK IN SKIN AND HOLE IN STRINGER 22R AT STA 727E, STR 22R. INSTALLED DOUBLER ON SKIN AND STRINGER PER SRM 53-00-01 FIG 229, DET 19 AND 53-00-03 FIG 201. 2L72 4F RTA16WE 20050630001122005063000112NM 2005 6 30 C1HA200581001 120050624A2150 REGULATOR BOEING727 7272S7 138407ZNM RT A/C PACK MALFUNCTIONED A C1HAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 GL15681CA 22020 AFTER DEPARTURE, RIGHT PACK TRIPPED FOLLOWED BY NR 3 BLEED TRIP. TRIPPED AGAIN COM 21.15 AND 2.36.2 AFTER COM PROCEDURE. REMOVED AND REPLACED RT HIGH PRESSURE REGULATOR PER M/M 36-12-51, OPS CHECK NORMAL PER M/M 36-12-01. 2L73 4F A3WE 20050701000012005070100001CE 2005 7 1 DJFA2005113 120050622A2910 O-RING RAYTHNDH125 HAWKER800XP 7150012CE NR 2 HYD SYS LEAKING E DJFAA UNSCHED LANDING K FLUID LOSS DEDESCENT 1 EA23840LX 258666 AT FL290 THE NR 2 HYDRAULIC LOW PRESSURE ANNUNCIATOR ILLUMINATED AND THEN EXTINGUISHED. A FEW SECONDS LATER THE ANNUNCIATOR ILLUMINATED AGAIN AND THE HYDRAULIC PRESSURE GAUGE WAS FLUCTUATING BETWEEN 2,000 TO 3,000 PSI FOR THE REMAINDER OF THE FLIGHT. SHORTLY THEREAFTER, BOTH HYDRAULIC LOW PRESSURE ANNUNCIATORS WERE ILLUMINATED. THE CREW THEN DECLARED AN EMERGENCY AND HAD TO MANUALLY LOWER THE LANDING GEAR. THE AIRCRAFT WAS DIVERTED TO KPHX AND A UNEVENTFUL LANDING WAS MADE. MAINTENANCE REPLACED AN O-RING ON THE NR 1 SYSTEM LOW PRESSURE SWITCH SNUBBER. THE HYDRAULIC SYSTEM WAS SERVICED AND ENGINES WERE RAN. A SATISFACTORY LEAK CHECK OF THE SYSTEM WAS PERFORMED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA3EU 20050701000032005070100003 2005 7 1 P5CA0501366 420050616A3197 WIRE BOEING747 747341 13848AMNM WARNING HORN BROKEN A P5CAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 EA15355MC 23395 CREW REPORTED STAB TRIM GREEN BAND AMBER LIGHT ON PILOT’S CENTER PANEL AND GREEN BAND LIGHT ON CONTROL STAND. CAME ON AFTER APL NOSE UP SELECTED. ACCORDING TO WEIGHT AND BALANCE CALCULATION. NO TAKEOFF WARNING HORN WITH FLAPS 20 DEGREES. FOUND BROKEN WIRE ADJACENT TO CONNECTOR D8113. REPAIRED BROKEN WIRE PER MM 20-10-13, INDICATION NORMAL. 2L74 4F RTA20WE 20050701000052005070100005CE 2005 7 1 DJFA2005116 120050624A215073838415 ACM CESSNA650 650 2076802CE AFT SMOKE E DJFAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA23384CW 1964 6500144 WHILE PERFORMING A TEST FLIGHT FOR A STABILIZER REPLACEMENT, CREW REPORTED A GREY BLUISH SMOKE BEGAN FILLING CABIN & COCKPIT. RETURNED TO KTUL. REPLACED FORWARD AIR CYCLE MACHNE AND FORWARD AND AFT WATER SEPARATOR SOCKS. FORWARD AND AFT ACM OIL WAS SERVICED. AN OPERATONAL CHECK OF AIR CONDITIONING SYSTEM WAS PERFORMED. THE OPERATIONAL CHECKS WERE GOOD & NO LEAKS WERE NOTED FOLLOWING A 30 MINUTE GROUND RUN. AIRCRAFT RETURNED TO SERVICE. CREW REPORTED THAT SMOKE WAS FILLING THE CABIN & COCKPIT. SMOKE HAD DISSIPATED AFTER AIRCRAFT RETURNED TO KTUL. CREW PERFORMED A GROUND RUN OF AIRPLANE & THERE WERE NO FURTHER INDICATIONS OF SMOKE. 2L72 4F A9NM 20050701000292005070100029EA 2005 7 1 SWIA200515188 120050622A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07908SW 7540 EXIT LIGHT BY MCD INOP. REPLACED FORWARD LOWER EMERGENCY LIGHT ASSY BY MAIN CABIN DOOR. OPERATIONAL CHECK GOOD IAW CRJ MM 33-51-21. 2L72 4F RTA21EA 20050701000372005070100037EA 2005 7 1 SWIA200515196 120050624A2741 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07457SW 7773 F/O RIGHT SIDE OF TRIM SWITCH IS STICKY. REPLACED F/O'S TRIM SWITCH IAW MM 27-41-05. OPERATIONAL CHECK GOOD IAW MM 27-40-00. 2L72 4F RTA21EA 20050701000392005070100039EA 2005 7 1 SWIA200515198 120050623A274170609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07924SW2408 2408 7681 MACH TRIM WILL NOT ENGAGE. REPLACED HSTCU IAW CRJ MM 27-41-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050701000422005070100042EA 2005 7 1 A6WA200540215 120050621A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31423AW 7636 RT FS 484.00 INTRCOSTAL AT LBL 36.0 HAS A .5 INCH LONG CRACK. FABRICATED ANGLE IAW EO. REMOVED FLANGE AND INSTALLED ANGLE IAW MFG REO. (K) 2L72 4F4 FRTA21EA E15NE 20050701000462005070100046EA 2005 7 1 A6WA200540219 120050622A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSLEAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31423AW 7636 LT FS 621.00 ANGLE IS CRACKED .5 INCH LONG ON OB RADIUS. REPAIRED BY REMOVING DAMAGED SECTION OF ANGLE, FABRICATING REPAIR ANGLES AND STRAP, INSTALLING REPAIR PARTS IAW MFG REO. (K) 2L72 4F4 FRTA21EA E15NE 20050701000492005070100049EA 2005 7 1 A6WA200540197 120050613A5220600352171001 HINGE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE ESCAPE HATCH CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31419AW 7633 CREW ESCAPE HATCH HINGES ARE CRACKED AROUND BASE. REPLACED BOTH HINGE ARMS WITH NEW HINGE ARMS IAW REO SRM. (K) 2L72 4F4 FRTA21EA E15NE 20050701000652005070100065EU 2005 7 1 ALG2005F00031 120050616A561012N544102 WINDOW UROCOPEC120 EC120B 8680987EU TMECA ARRIUSARRIU2F NE PILOTS DOOR SEPARATED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03524AL 1263 34281 WHILE IN FLIGHT, TRAVELING APPROX 105 KNOTS AT 800 FEET THE TOP AFT CORNER OF THE PILOTS WINDOW DELAMINATED AND POPPED OUT APPROX 1 INCH. IMMEDIATELY FOLLOWING (2-3 SECONDS) THE ENTIRE WINDOW DELAMINATED AND SEPARATED FROM THE AIRCRAFT. I SLOWED THE AIRCRAFT AND VISUALLY AND PHYSICALLY CHECKED THE FLIGHT CONTROLS AND DIVERTED. MAINTENANCE INSPECTED THE AIRCRAFT AND NO DAMAGE WAS FOUND. INSTALLED SERVICEABLE WINDOW IAW MM. (K) 1G72 3U3 UNCR0001RD E34NE 20050701000692005070100069CE 2005 7 1 CIEA200500006 120050628A52105043006127 DOOR SEAL BEECH 200 B200 1152922CE MAIN PAX DOOR INOPERATIVE E CIEAGA O2 MASK DEPLOYED UNSCHED LANDING SJ AFFECT SYSTEMS WARNING INDICATION CLCLIMB 1 NM03203LG BB926 DURING CLIMB, PAX HEARD WIND NOISE FROM AFT CABIN. BROUGHT TO ATTENTION OF PILOT, NOTICED CABIN PRESSURIZATION WAS DROPPING, RESULTING IN CABIN ALTITUDE CLIMBING. PILOT ATTEMPTED TO ADJUST PRESSURIZATION CONTROLLER, CABIN LOST PRESSURIZATION. OXYGEN MASKS DROPPED, AC RETURNED TO AIRPORT. CABIN ENTRY DOOR SEAL CORNER CUSHION INSIDE OF DOOR SEAL HAD MIGRATED APPROX 6 INCHES. CUSHION WAS REPOSITIONED. INFLATION TUBE MAY HAVE TWISTED AND KINKED, RESULTING IN DOOR SEAL NOT BEING FULLY PRESSURIZED. CORNER SEAL CUSHION WAS REPOSITIONED, DOOR WAS CLOSED PRESSURIZATION WAS CHECKED ON GROUND. AC WAS TEST FLOWN, SYST WORKED NORMAL. NOTE: OXYGEN MASK RESULTED IN GIVING PASSENGER AN ALLERGIC REACTION. 1L72 4T A24CE 20050701000862005070100086EU 2005 7 1 01142005 120050114A2612 FIRE WARNING SAAB SF340 340B 7860101EU GE CT7TS CT71 30030NE LT TAILPIPE ILLUMINATED A NSVAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA27237MJ 340B237 LT TAIL PIPE HOT LIGHT ILLUMINATED AFTER TAKE OFF. 2L72 4T4 URTA52EU E8NE 20050705000072005070500007NE 2005 7 5 05FDEA01707 220050627A7200 ENGINE DOUG MD10 MD1010F 3022112WP GE CF6 CF680 30025NE NR 1 FAILED A FDEAFA ACTIVATE FIRE EXT. UNSCHED LANDING ERJVIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SO25565FE 46996 AFTER TAKEOFF AT SMF NR 1 ENG RPM ROLLED BACK TO 42 PERCENT EGT TO 992 AN HAD SEVERE VIBRATION. SHUTDOWN NR 1 IAW QRH. NOTE HAD NO FIRE WARNING IND. 1 FIRE BOTTLE USED- GND WITNESS OBS FLAMES FROM CENTER OF ENG. EXHAUST REMOVED AND REPLACED #1 ENG NR 1 FIRE EXTINGUISHER BOTTLE, PERFORMED STALL INSPECTIONS, OVERTEMP INSPECTIONS, FAIL TO RESPOND TO THROTTLE MOVEMENT TROUBLESHOOTING FOUND VSV OUT OF RIG ,CORRECTED, ALSO UPON ENGINE RUN FOUND BAD CIT SENSOR, REPLACED. OK FOR SERVICE. 2L73 4F4 FRTA22WE E13NE 20050705000082005070500008EA 2005 7 5 ASOA05410 120050508A5320601R3117117 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 SO27867AS 7463 DURING A C-CHECK IN MCN, THE CLIP AT FS 484, LBL 36 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CLIP AT FS 484, LBL 36 IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20050705000242005070500024NM 2005 7 5 USAA050703 120050531A5320 INTERCOSTAL BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19445US 24893 CLT - FOUND INTERCOSTAL CORRODED 2 INCHES, LBL 24.75 BETWEEN STATIONS 947 AND 967. REPLACED INTERCOSTAL IAW BOEING DRAWING 65C34059. (M) 2L72 4F RTA16WE 20050705000292005070500029NM 2005 7 5 UPS05544713 120050618A2611 SMOKE DETECTOR BOEING757 75724APF 1384969NM CARGO BAY CONTAMINATED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01474UP 28844 FWD CARGO BAY SMOKE DETECTOR 10459 FAILED (TC 26-016-05). REMOVED COVER ON SMOKE DETECTOR. FOUND LARGE CONCENTRATION OF BUGS INSIDE SMOKE DETECTOR. CLEANED SENSE TUBES IN FWD PIT AND INSTALLED NEW SMOKE DETECTOR. OPS CHECK GOOD. ALL WORK IAW MM 26-16-01-2. 2L72 4F RTA2NM 20050705000372005070500037NM 2005 7 5 193 120050612A793356B94 BULB BOEING737 737201 1384454NM PWA JT8 JT8D9A 52048NE ENG OIL TEMP MALFUNCTIONED A RYNAEA ENGINE SHUTDOWN UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 CE07240AU 22355 655811 DURING CLIMB, ENGINE NR 1 HAD HIGH OIL PRESSURE AND SHORTLY THEREAFTER NR 1 OIL TEMPERATURE STARTED CLIMBING TOWARDS REDLINE. ON RETURN, NR 1 ENGINE SHUTDOWN. 2L72 4F4 F A16WE E2EA 20050705000522005070500052EU 2005 7 5 AWXA200500723 120050617A335032145410 POWER SUPPLY AIRBUS320 A320232 3930326EU EMERGENCY LIGHTSMALFUNCTIONED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28639AW 471 DURING 4 DAY CHECK, FOUND LT MID CABIN SLIDE ARM LIGHT ALWAYS ON. MX REMOVED AND REPLACED MID CABIN LT EMERGENCY POWER SUPPLY IAW AMERICA WEST AIRLINES TASK CARD R1C33303. OPS CHECKS GOOD. 2L72 4F RTA28NM 20050705000582005070500058NE 2005 7 5 MALA050484 220050619A7323 CONTROLLER BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE NR 3 ENGINE MALFUNCTIONED A MALAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15519XJ E2344 CREW RETURNED FOLLOWING ENGINE NR 3 OVERSPEED CONDITION. EMERGENCY DECLARED AND ENGINE SHUT DOWN. REPLACED OVERSPEED CONTROLLER, HMA AND DOWNLOADED FADAMS. 2H74 4F4 FRTA49EU E6NE 20050705000612005070500061NM 2005 7 5 WRLA2005103 120050614A5511 RIB DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C-04 CHECK, WHILE PERFORMING INSP PER EO 02-5510-098, FOUND CORROSION IN HST LT BARREL NUT HOLE NR 35. 2L73 4F4 FRTA22WE E24NE 20050705000632005070500063SO 2005 7 5 20030855 120050616A2120 SMOKE EMB 120 EMB120ER 3260203SO COCKPIT DETECTED A GLBAK NONE B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM03297UX 120297 DURING TAXI, SMOKE WAS DETECTED IN COCKPIT BUT CEASED AFTER CREW SHUT OFF PACKS. ACFT RETURNED TO GATE. MX PERFORMED INSP AND OPERATIONALLY CHECKED LT/RT PACKS AND BLEED SYSTEMS WITH NO DEFECTS NOTED. ACFT RETURNED TO SERVICE. 2L72 4T RTA31SO 20050705000662005070500066SO 2005 7 5 C2XA05CL044 120050606A21508152402 ACM EMB 145 EMB145LR 3260212SO NR 1 SEIZED A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW27139491625416254 145057 CREW REPORTED STRONG ODOR OF MELTING RUBBER PREVALENT WITHIN A/C CABIN DURING PACK USAGE. MX INSP AND RELEASED A/C IAW MEL 21-51-00/1. SUPPLEMENT TO FOLLOW. MX REPLACED NR 1 ACM. OPS CHECKS GOOD. 2L72 4T RTT00011AT 20050705000702005070500070EA 2005 7 5 SWIA200515162 120050603A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07710BR 7852 FLOOR SUPPORT ANGLE AT FS 621, LT SIDE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FLOOR SUPPORT ANGLE AT FS 621 LT SIDE IAW CRJ REO 601R-53-61-114 REV B. 2L72 4F RTA21EA 20050705000722005070500072EA 2005 7 5 SWIA200515164 120050528A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07965SW 7871 FS 280 AT LBL 9.0 OUTBOARD FLOORBEAM ATTACH ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-21-11, 51-25-16, 51-23-00. 2L72 4F RTA21EA 20050705000782005070500078NM 2005 7 5 WRLA2005116 120050616A5511 RIB DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C04 CHECK, WHILE PERFORMING INSP PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE NR 33. 2L73 4F4 FRTA22WE E24NE 20050705000802005070500080NM 2005 7 5 WRLA2005118 120050616A5511 RIB DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C04 CHECK, WHILE PERFORMING INSP PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE NR 11. 2L73 4F4 FRTA22WE E24NE 20050705000822005070500082SO 2005 7 5 RAIA00506025 120050619A7830 WARNING LIGHT EMB 145 EMB145ER 3260211SO THRUST REVERSER ILLUMINATED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03808HK 145157 ENGINE 1 REVERSE DISAGREE CAME ON DURING T/O ROLL AT 40 KNOTS. MX DEFERRED NR 1 T/R. 2L72 4F RTT00011AT 20050705000892005070500089NM 2005 7 5 WRLA200599 120050614A5511 RIB DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C-04CHECK, WHILE PERFORMING INSP PER EO 02-5510-098, FOUND CORROSION IN HST LT BARREL NUT HOLE NR 30. 2L73 4F4 FRTA22WE E24NE 20050705000952005070500095EA 2005 7 5 SWIA200515148 120050617A2750855D10011 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07445SW4667 4667 7651 CLIMBING THRU FLT LEVEL 280, RECEIVED AMBER FLAPS FAIL CAUTION MSG. REPLACED RT BPSU IAW MM 27-51-10 AND FECU IAW MM 27-51-05. OPS CHECK GOOD, PN: 860D100-18 SN OFF: 1104. 2L72 4F RTA21EA 20050705001022005070500102EA 2005 7 5 SWIA200515155 120050604A5340 FITTING CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07919SW 7657 FS 460 RT FLOOR RBL 9.0 OUTBOARD FITTING CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED IAW CRJ SRM 51-40-11, 51-42-06 & 51-42-21. 2L72 4F RTA21EA 20050705001132005070500113NM 2005 7 5 USAA050504 120050414A5412300N05019 BULKHEAD BOEING757 7572B7 1384964NM PYLON DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19611AU40729 27123 FOUND PYLON MID BULKHEAD DAMAGED 1.25 INCH DIAMETER BY .030 INCH DEEP, NR 1 PYLON, MID BULKHEAD, UPPER AFT SLEEVER BOLT ATTACH AREA. ACCOMPLISHED SPOTFACING TO REMOVE DAMAGE PER EA 96386. (M) 2L72 4F RTA2NM 20050705001202005070500120NM 2005 7 5 USAA050596 120050506A5311 FRAME BOEING757 757225 1384959NM BULKHEAD BUCKLED A USAAK NONE O OTHER ININSP/MAINT 1 EA19608AU 22204 BFM - FOUND FORWARD BULKHEAD CHORD BUCKLED, AFT PRESS BULKHEAD STATION 1720, LOWER CHORD B/T S28R-29L. CUT OUT DAMAGED CHORD AND SPLICED IN NEW SECTION PER SRM 53-80-08 FIG 201. (M) 2L72 4F RTA2NM 20050705001322005070500132EU 2005 7 5 USAA050627 120050423A5347F5711056820401 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW24199 0333 BFM - FOUND SEAT TRACK CORRODED 6 INCHES LONG BY 1 INCH WIDE BY .020 INCH DEEP, MAIN CABIN, FRAME 41, Y450, INBOARD AND OUTBOARD LOBES. REMOVED AND REPLACED SEAT TRACK ASSEMBLY PER SRM 53-31-15, 51-44-11, 51-41-11. (M) 2L72 4F RTA46NM 20050705001352005070500135EU 2005 7 5 USAA050624 120050428A53201161459 FLOOR SUPPORT AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW24199 0333 BFM - FOUND FLOOR SUPPORT CORRODED 3 INCHES LONG AREA, FRAME 13B FLOOR SUPPORT Y-450 TO Y-953. REMOVED AND REPLACED SUPPORT PER SRM 53-11-14. (M) 2L72 4F RTA46NM 20050705001372005070500137EU 2005 7 5 USAA050622 120050426A5320 FLOOR SUPPORT AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW 0333 BFM - FOUND FLOOR SUPPORT CORRODED 1 INCH BY .56 INCH DEEP, Y0 AT FRAME 73. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 53-00-15, 51-74-00, 51-44-11, 51-42-11. (M) 2L72 4F RTA46NM 20050705001382005070500138EU 2005 7 5 USAA050621 120050428A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW24199 0333 BFM - FOUND SEAT TRACK CORRODED 4 INCHES LON BY .600 INCH WIDE BY .049 INCH DEEP, Y1552.5 AT FRAME 35. FABRICATED SEAT TRACK PER SRM 51-74-00, - 53-00-15, 51-42-11, 51-44-11, 51-23-11. (M) 2L72 4F RTA46NM 20050705001542005070500154EU 2005 7 5 USAA050605 120050424A5315F5347821220300 FLOORBEAM AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW24199 0333 BFM - FOUND FLOORBOARD SUPPORT CORRODED .5 INCH LONG BY .2 INCH WIDE BY .050 INCH DEEP, MAIN CABIN FRAME 80; 2 INCHES INBOARD OF Y-450. CORROSION LEVEL 2, TASK C534159-01. REMOVED AND REPLACED FLOORBOARD SUPPORT PER SRM 53-41-14; 51-44-11; 51-42-11. (M) 2L72 4F RTA46NM 20050706000122005070600012EU 2005 7 6 USAA050683 120050522A5315D5348004320401 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSLEAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19716UW18358 1055 PIT - FOUND FLOORBEAM CORRODED 1 INCH DIAMETER, AT FRAME 66 Y1500 LEFT. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-45-00, 51-72-11, DWG D534-74350. 2L72 4F RTA28NM 20050706000212005070600021NM 2005 7 6 USAA050652 120050516A5330 SKIN BOEING737 7374B7 1384702NM FS CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US 24781 CLT - FOUND SKIN CRACKED .5 INCH, FUSELAGE BL 0 STATION 863. REMOVED DAMAGE AND INCORPORATE FABRICATED REPAIR FILLERS AND DOUBLERS IAW EA 96545. (M) 2L72 4F RTA16WE 20050706000462005070600046 2005 7 6 06272005 420050624A34256229681001 EADI BEECH 1900 1900D 1154162CE COCKPIT FAILED A NSVAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA2760MJ UE60 BURNING ODOR PRESENT AND NR 1 EADI FLASHING ON AND OFF. 2L72 4T RTA24CE 20050706000482005070600048NM 2005 7 6 DHL2005741599 120050517A5340 TEE FITTING BOEING727 7272Q9 138448MNM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 VERTICAL BEAM AT BS 1183, LBL 8, HAS A CRACK AT LWR AFT T-SECTION. TERMINATED CRACK BY STOP DRILLING .250 DRILL HOLE AT END OF CRACK IAW B727 SRM 53-01-75 FIG 3 AND SRM 51-10-1, ACCOMPLISHED 727 HFEC INSPECTION AT END OF CRACK FOUND TRIMMED AND DRILLED ANGLES AND RADIUS FILLERS IAW B727 S/B 727-53-0175 REV 3 FIG 3. TREATED AND PRIMED PARTS AND AREA IAW B727 SRM 51-10-2, INSTALLED REPAIR PARTS IAW B727 S/B 727-53-0175 FIG 3. 2L73 4F RTA3WE 20050706000492005070600049NE 2005 7 6 06262005 220050626A7200 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RIGHT OVERTEMP A NSVAC ABORTED TAKEOFF MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 EA27251CJ 251 785341 ON TAKEOFF, RT ENGINE HAD AN ITT OF 907 WITH TAKEOFF POWER ON BOTH ENGINES AT 88 PERCENT WHILE CLIMBING TO POWER. 2L72 4T4 TRTA52EU E8NE 20050706000502005070600050NM 2005 7 6 DHL2005741565 120050421A5230 SKIN BOEING727 7272Q9 138448MNM CARGO DOOR BULGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 C-1 DOOR EXT LOWER SKIN AT SPLICE HAS 6 BILGED AREAS. REMOVED PREVIOUS REPAIR DOUBLER C1 DOOR STA 560 TO 620 IAW B727 SRM 51-30-2. FABRICATED EXTERNAL DOUBLER 204T3 .071 PO 9002193 DIM 59 X 6.5 INCH IAW B727 SRM 52-00-3 FIG 3. TREATED AND PRIMED DOUBLER IAW B727 SRM 51-10-2. INSTALLED DOUBLER IAW B727 SRM 52-00-3 AND 51-30-2. 2L73 4F RTA3WE 20050706000512005070600051NM 2005 7 6 DHL2005741602 120050513A5340 FITTING BOEING727 7272Q9 138448MNM FUSLEAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 FUSELAGE JACK POINT AT BS 350 ABOVE STR 22R HAS FITTINGS EXFOLIATING AT LWR END. REMOVED FWD & AFT FITTING AT BS 351 JACKPOINT EVALUATED FITTINGS CORRODED ON 2 EA & FOUND TO BE BEYOND ALLOWABLE LIMITS IAW B727 SRM 51-30-2 & 51-10-1 FIG 1. LOCATED & DRILLED FASTENERS HOLES IN 2 EA FITTINGS P/N 65-17617-2 PO 5096289 & P/N 65-18693-2 PO 5096289 IAW B727 SRM 51-30-5 FIG 1. TREATED & PRIMED FITTINGS IAW B727 51-10-2. INSTALLED 2 EA FITTINGS IAW B727 SRM 51-30-2 FIG 14. 2L73 4F RTA3WE 20050706000522005070600052NM 2005 7 6 DHL2005741611 120050616A5512 SKIN BOEING727 7272Q9 138448MNM HORIZONTAL STAB DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 RIGHT HORIZONTAL STABILIZER LOWER INTERSPAR SKIN AT STAB STA 109.97 IS DENTED. CUT OUT DAMAGED AREA TWO PLACES DIM 3.5 X 1.25 & 8.5 X 2 INCH IAW B727 SRM 55-10-3 FIG 3. FAB DOUBLER FROM 2024T3 .080 PO 9002555 DIM 15 X 101.5 INCH IAW B727 SRM 55-10-3 FIG 3. TREATED & PRIMED DOUBLER & BARE METAL IAW B727 SRM 51-10-2. INSTALLED DOUBLER IAW B727 SRM 51-30-2 AND 55-10-3 FIG 3. 2L73 4F RTA3WE 20050706000532005070600053NM 2005 7 6 DHL2005741610 120050615A5330 SKIN BOEING727 7272Q9 138448MNM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DENT AT RIGHT FUSELAGE STA 1330 ABOVE STR 19R. CUT OUT DAMAGE AREA SIZE 1.75 X 2.75 INCH ON RIGHT FUSELAGE STA 1330 ABOVE STR 19R IAW B727 SRM 53-30-3 FIG 1. FAB'D DOUBLER FROM 2024-T3 0.63 SIZE 7.5 X 10.75 INCH PO 9001978. TREATED & PRIMED PART AND AREA IAW B727 SRM 51-10-2. INSTALLED REPAIR DOUBLER IAW B727 SRM 53-30-3 FIG 1 & 51-30-2. 2L73 4F RTA3WE 20050706000622005070600062SO 2005 7 6 TZR2005F00023 220050610A8530ACE520T101 CYLINDER CESSNA401 401A 207590DCE CONT O520 GTSIO520C 17032SO NR 3 CRACKED E TZRAO OTHER O OTHER NRNOT REPORTED 1 SW05409TE455 401A0118 CRACK IS TYPICAL FOR THESE CYLINDERS, RT ENGINE NR 3. (K) 1L72 3O3 O A7CE E7CE 20050706000672005070600067SO 2005 7 6 TZR2005F00025 220050610A8530ACE5207101 CYLINDER CESSNA401 401 207590CCE CONT O520 GTSIO520C 17032SO RT ENGINE CRACKED E TZRAO OTHER O OTHER NRNOT REPORTED 1 SW05405TE 143 4010121 CRACK IS TYPICAL FOR THESE CYLINDERS. RT ENGINE, NR 3 CYL. (SW05200509364) (K) 1L72 3O3 O A7CE E7CE 20050706000832005070600083 2005 7 6 DXTA200500812 420050630A3497MS3456L10SL4S WIRE CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE STICK SHAKER BROKEN E DXTAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 GL07344QS 5600344 STICK SHAKER INOP DURING ROTARY TEST. A LIGHT TAP ON THE YOKE CAUSED A SPARK AND A SMALL PUFF OF SMOKE. AOA CIRCUIT BREAKER POPPED. FOUND WIRE BROKEN ON CONNECTOR. REMOVED AND REPLACED CONNECTOR WITH A NEW CONNECTOR . STICK SHAKER OPS CHECKS GOOD IAW M/M AND WIRE DIAGRAM MANUAL. 2L72 4F4 FRTA22CE E25EA 20050706000972005070600097EU 2005 7 6 05FDEA01716 120050628A5330 SKIN AIRBUS300 A300B4605R 3930308EU FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25657FE 748 FWD CARGO DOOR AT FUSELAGE CUT-OUT FWD LOWER SKIN EDGE AND WEB SKIN HAS CHAFED MARK. ITEM WAS BLENDED AND RESULTING CONDITION WAS OUT OF LIMITS. REPAIR PARTS FABRICATED, REF. TRAVELER T5/527985. REPAIRS AFFECTED USING STANDARD WORK DRAWING SR30-53-001. MAJOR REPAIR/RDR/SDR REPAIRS INCLUDED A SPLICE TO FRAME 20A AND THE ADJACENT SKIN DOUBLERS, ALL REFERENCE SR30-53-001. 2L72 4F RTA35EU 20050706000992005070600099NM 2005 7 6 05FDEA01741 120050629A5347 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 CABIN, ALONG STA 1821 TO STA 1887 RBL 27.75 SEAT TRACK CROWN AND BASE FOUND CORRODED. CARRIED OUT REPAIR AS PER SRM 53-70-00. [CLOSED] 2L73 4F RTA22WE 20050706001122005070600112NM 2005 7 6 05FDEA01720 120050628A5311 FRAME BOEING727 727200 138407ENM COCKPIT CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25203FE 22925 COCKPIT LT FRAME STA 277 BTWN STR S-14 TO S-16 FRAME WEB ANGLES CRACKED AT FWD & AFT SIDE OF FRAME AT 6 EA PLACES AS MARKED. REPAIRED FRAME WEB ANGLE IAW SRM 53-10-4 MAJOR REPAIR 2L73 4F RTA3WE 20050706001152005070600115NE 2005 7 6 05FDEA01744 220050629A7200 ENGINE AIRBUS310 A310 EU PWA JT9 JT9D7R4E1 52054NE RIGHT BIRD INGESTION A FDEAC ABORTED TAKEOFF CEJF.O.D. VIBRATION/BUFFET WARNING INDICATION TOTAKEOFF 1 SO25422FE 346 707728 RTO AT 120 KIAS DUE TO LOUD BANG,VIBRATION,AND PULL TO THE RIGHT. F/O SAW AT LEAST TWO BIRDS MOMENTARILY BEFORE EVENT. MAX POWER DUE WET RUNWAY WINDS CALM. VIBRATION CEASED WHEN NR 2 ENGINE SHUTDOWN ON RUNWAY. REMOVED AND INSTALLED NR 2 ENG, NOSE COWL, RT THRUST REVERSER AND LT FAN COWL. 2L72 4F4 FRTA35EU E3NE 20050706001172005070600117NM 2005 7 6 05FDEA01746 120050629A2840 INDICATOR BOEING727 727100 1384036NM NR 3 FUEL FALSE INDICATIONA FDEAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO25151FE 19147 NR 3 FUEL GAGE ERRONEOUS INDICATION, AT T/O SHOWED 11.1, SHORTLY INTO FLIGHT GAGE DROPPED 5K LBS. AT CRUISE FLT BOOST PUMPS ILLUMINATED. UPON LANDING AT KFSD, NR 3 FUEL QTY SHOWED EMPTY. ACFT RELEASED FOR SERVICE PER MEL/CDL: 28-11-02. FOUND NR 3 INDICATOR VERY ERATIC. REMOVED AND REPLACED NR 3 FUEL QTY IND. (CLOSED) 2L73 4F RTA3WE 20050706001212005070600121EU 2005 7 6 05FDEA01750 120050630A3610 WARNING LIGHT AIRBUS310 A310 EU NR 1 BLEED ILLUMINATED A FDEAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO25456FE 318 BLEED AIR NR 1 FAULT WITH ANTI-ICE SELECTED AFTER SELECTING WITH ANTI ICE THEN BOTH PACKS WOULD FAULT AND NOT RESET COULD NOT MAINTAIN CABIN PRESSURE WITH APU BLEED NR 2 BLEED WAS DEFERRED NR 1 ENGINE BLEED WOULD NOT RESET. UNSCHEDULED LANDING T/S PER A310 TSM BITE NR 1 & 2 PSC PRIOR TO AND AFTER NR 1 ENG GROUND RUN, OPENED NR 1 ENG COWLING TO INSPECT BLEED AIR DUCTING FOR LEAK AND SECURITY NO DEFECT NOTED. GEAR PINS INSTALLED AND REMOVED AFTER ENGINE RUN. (OPEN) 2L72 4F RTA35EU 20050706001242005070600124NM 2005 7 6 05FDEA01755 120050630A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25619FE 48770 LT NR 4L BARREL NUT BORE CORROSION EXCEEDED TO LIMIT. REPAIRED AS PER FEDEX EA 1-5510-83028. 2L73 4F RTA22WE 20050706001322005070600132NM 2005 7 6 05FDEA01734 120050629A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) FORWARD HINGE FITTING INBOARD MID BOLT HOLE FOUND CORRODED. REMOVED AND REPLACED PER AMM 27-50-30-4. 2L73 4F RTA22WE 20050706001352005070600135NM 2005 7 6 05FDEA01738 120050629A5347 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 ALONG STA 1821 TO STA 1887 LBL 8.75 SEAT TRACK CROWN AND BASE FOUND CORRODED. CARRIED OUT REPAIR AS PER SRM 53-70-00. [CLOSED] 2L73 4F RTA22WE 20050706001372005070600137NM 2005 7 6 05FDEA01709 120050627A5510 FITTING DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25619FE 48770 LT NR 26L FITTING BARREL NUT BORE FOUND CORROSION EXCEEDED TO LIMIT. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. (CLOSED) 2L73 4F RTA22WE 20050706001402005070600140NM 2005 7 6 05FDEA01712 120050628A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LT WING, OUTBOARD FLAP INBOARD HINGE AFT HINGE FITTING AFT HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-87551. 2L73 4F RTA22WE 20050706001422005070600142NM 2005 7 6 BB05046 120050622A33501000679 LIGHT BOEING767 7672B7 1385107NM COCKPIT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19656US 26847 CLT - FOUND COCKPIT INTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. 2L72 4F RTA1NM 20050706001442005070600144 2005 7 6 UPS05144721 420050622A2565 SLIDE AIRBUS300 A300B4622R 3930312EU PAX DOOR WILL NOT TEST A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01126UP 0810 FWD ENTRY DOOR EMERGENCY ESCAPE SLIDE EVACUATION SLIDE WARNING HORN SYS WILL NOT TEST; LIGHTS OK. EMERGENCY ESCAPE SLIDE WARNING HORN INOP; DEFERRED PER MEL 52-73-01-2-4. EMERGENCY DOOR TEST BUTTON SEEMS TO HAVE STICKY SUBSTANCE IN BUTTON CLEANED BUTTON WITH CONTACT CLEANER. BUZZER AND LIGHT WORKS OK. THIS CLEARS M304686. 2L72 4F RTA35EU 20050706001482005070600148CE 2005 7 6 DXTA200500789 120050619A32606583543 PCB CESSNA500 560CESSNA 2076750CE MLG INOPERATIVE E DXTAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL07313QS 5600325 AFTER TAKEOFF WHEN GEAR WAS RETRACTED, ALL 3 GREEN LIGHTS EXTINGUISHED THE RED GEAR UNSAFE STAYED ILLUMINATED THEN THE RIGHT MAIN LIGHT REAPPEARED. RECYCLED GEAR AND ALL LIGHTS EXTINGUISHED. REMOVED PRINTED CIRCUIT BOARD PLB2-4 BOARD FROM ZONE 245 AND INSTALLED NEW PLB IAW CITATION ULTRA MM CH 25-41-02. PERFORMED GEAR FUNCTIONAL CHECK WITH NO DEFECTS NOTED IAW CITATION ULTRA MM CH 32-01-00. 2L72 4F RTA22CE 20050706001502005070600150CE 2005 7 6 DXTA200500787 120050619A213121198623 CONTROLLER CESSNA750 750 2076810CE CABIN PRESSURE INOPERATIVE E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07930QS2333 7500130 CABIN ALTITUDE AMBER EICAS MSG CAME ON AS WE CLIMBED THRU 12,000 FT CABIN ALTITUDE SHOWED 9000 FEET 1.4 DIFFERENTIAL AND RATE OF CLIMB OF 1000 FEET. LEVELED AT 14000 FEET AND SELECTED FULL HOT ON PAC TEMP SEL RATE OF CLIMB WENT TO ZERO AND CABIN STAYED AT 9000 UNTIL WE DESCENED THRU 9000 AT GEAR DOWN THERE WAS A PRESSURE SPIKE AND THE CABIN FOLLOWED THE PLANE ALTITUDE AND RATE OF DESCENT. REMOVED & REPLACED CABIN PRESSURIZATION CONTROLLER IAW CITATION 750 AMM 21-31-00. SELF TEST SATISFACTORY. 2L72 4J RTT00007WI 20050706001572005070600157EU 2005 7 6 MALA050500 120050623A2432 BATTERY BAC 146 AVRO146RJ85A1500097EU DC GEN SYS FAILED A MALAK NONE O OTHER ININSP/MAINT 1 GL15509XJ E2321 BATTERY FAILED CAPACITY CHECK. 2H74 4F RTA49EU 20050706001592005070600159EU 2005 7 6 MALA050502 120050622A2432 BATTERY SAAB SF340 340B 7860101EU DC GEN SYS FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15424XJ 340B424 BATTERY FAILED CAPACITY CHECK. 2L72 4T RTA52EU 20050706001612005070600161WP 2005 7 6 IXXA05SMN05S 120050427A5320 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX834963359 45993 DURING ROUTINE C-CHECK INSPECTION, FWD CARGO COMPARTMENT INTERIOR SPLICE FITTING CRACKED 8 IN., STA 440.000 - STA 460.000 , L-31L. REMOVED CRACKED FITTING IAW DC-8 SRM 53-1-0 PAGE 1, DC-8 SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING IAW DWG 3750257. PERFORMED NDT INSPECTION TO FITTING IAW NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED AREA + NEW FITTING IAW DC-8 SRM 51-1-8B. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D PAGE 9. TORQUED IAW DC-8 RM 51-3-1. 2L74 4F RT4A25 20050706001622005070600162WP 2005 7 6 IXXA05SMN07S 120050427A5320 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX834963359 45993 DURING ROUTINE C-CHECK INSPECTION, FWD CARGO COMPT INTERIOR SPLICE FITTING CRACKED 3 IN., STA 440.000 - STA 460.000, L-31R. REMOVED CRACKED FITTING IAW DC-8 SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING IAW DWG 3750257. PERFORMED NDT INSPECTION TO FITTING IAW NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED AREA AND NEW FITTING IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO IAW DC-8 SRM 51-1-11 PAGE 9. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D PAGE 9. TORQUED IAW DC-8 RM 51-3-1. 2L74 4F RT4A25 20050706001762005070600176SO 2005 7 6 CHQA200500119 120050621A32608005701 PROXIMITY SENSOR EMB 145 EMB145LR 3260212SO MLG DAMAGED A CHQAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL11283SK 145424 AFTER TAKEOFF WHEN GEAR UP WAS SELECTED, NLG AIR/GND FAIL CAUTION MESSAGE APPEARED ON EICAS. AFTER DISCUSSIONS WITH BOTH DISPATCH AND MAINTENANCE CONTROL DECISION MADE TO DIVERT. PRECAUTIONARY EMERGENCY DECLARED. FULL STOP LANDING MADE AND SYSTEMS ALL NORMAL. DECISION WAS MADE TO TAXI BACK TO THE GATE. REMOVED AND REPLACED DAMAGED PROXIMITY SENSOR IAW EMB 145 AMM 32-10-02-3. PERFORMED OPS CHECK OF AIR GROUND SYSTEM IAW J/C E 32-63-00-710-001. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050706001862005070600186SO 2005 7 6 C2XA05BT043 120050615A261147359713 SMOKE DETECTOR EMB 135 EMB135LR 3260305SO CARGO BAY FALSE INDICATIONA C2XAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW2717521999 999 145378 CREW REPORTED EN ROUTE, THAT BAGGAGE SMOKE WARNING CAME ON INFLIGHT. DEPLOYED EXTINGUISHING BOTTLES, THEN DIVERTED ACFT. MX FOUND NO SIGNS OF FIRE OR SMOKE IN BAGGAGE COMPARTMENT. SUSPECT FAULTY SMOKE DETECTOR. REMOVED AND REPLACED BAGGAGE COMPARTMENT SMOKE DETECTORS NR 1 AND NR 2 IAW EMB135 AMM NR 26-15-01. OPS CHECKED GOOD, DUE TO BAGGAGE COMPARTMENT FIRE BOTTLES BEING EXTINGUISHED, REMOVED AND REPLACED HIGH RATE AND METERED BAGGAGE COMPARTMENT FIRE BOTTLES IAW EMB135 AMM NR 26-23-01. TESTED GOOD. ACFT RETURNED TO SERVICE, 2L72 4F RTT00011AT 20050706001902005070600190EA 2005 7 6 COMA0560360 120050620A3260172825 UPLOCK TARGET CNDAIRCL600 CL6002B19 1900309EA MLG PROX SWITCH UNRELIABLE A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01966CA 7132 GEAR DISAGREE WARNING. TIGHTENED LOOSE PROX SWITCH TARGET ON RT MLG UPLOCK. 2L72 4F RTA21EA 20050706001922005070600192EA 2005 7 6 COMA0570071 120050617A5753601R145022 VANE CNDAIRCL600 CL6002C10 1390015EA RT OB FLAP CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01340CA7435 10062 RT OUTBOARD FLAP VANE HAS 0.5 INCH CRACK ON UPPER SKIN APPROX 24 INCHES FROM INBOARD EDGE. CUT OFF INBOARD END OF SKIN PANEL TO REMOVE DAMAGE. FABRICATED AND INSTALLED REPAIR SKIN AND INTERNAL SPLICE DOUBLER (2024-13-040) IAW BRAS EO 601R-52-6696. 2L72 4F RTA21EA 20050706002192005070600219EU 2005 7 6 UPS05144719 120050621A3350 CONNECTOR AIRBUSA300 A300F4622R 3930360EU EMERGENCY LIGHTSDIRTY A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01130UP 0814 EMERGENCY EXIT LIGHTS DO NOT TEST. CLEANED CONNECTOR AT POWER SUPPLY UNIT. CKS GOOD AMM 33-51-14-4. 2L72 4F RTA35EU 20050706002212005070600221EA 2005 7 6 COMA0560359 120050619A5270 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN DOOR ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01779CA 7306 CABIN DOOR OUTER HANDLE CAUTION. DEFERRED MAINTENANCE PER MEL. 2L72 4F RTA21EA 20050706002232005070600223NM 2005 7 6 AWXA200500728 120050621A56105717623075 WINDOW BOEING737 7373G7 1384595NM COCKPIT MALFUNCTIONED A AWXAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 WP28305AW 24012 ABORTED TAKEOFF. DURING TAKEOFF, CAPT SLIDING WINDOW CAME OPEN, TAKEOFF ABORTED AT 138 KNOTS. FUSE PLUGS BLOWN ON MLG TIRES. PASSENGERS BUSED BACK TO TERMINAL AND ACFT TOWED BACK TO HANGER WITHOUT FURTHER INCIDENT. MX FOUND CAPTAINS NR 2 WINDOW REAR ROLLERS WERE NOT GOING OVER CENTER TO LATCH CLOSED. MX REMOVED AND REPLACED CAPTAINS NR 2 WINDOW IAW AMERICA WEST AIRLINES TASK CARD R1B56003. OPERATIONAL CHECKS WERE GOOD. ALL 4 TIRES AND BRAKES REPLACED DUE TO HIGH ENERGY STOP/INSPECTION. 2L72 4F RTA16WE 20050706002252005070600225NM 2005 7 6 AWXA200500730 120050617A5320652072629 THRESHOLD BOEING737 7373B7 1384580NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28328AW 23377 DURING C-13 CHECK, FOUND CORROSION IN FORWARD CARGO PIT ON 20 NUT PLATES LOCATED ON THRESHOLD WEB FROM STA 450 TO STA 490. MX FOUND CORROSION TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-30-15-1 FIG 101. REMOVED THRESHOLD WEB FROM STA 450 TO STA 490 AND FABRICATED NEW FORWARD PIT THRESHOLD WEB IAW BOEING 737-300 SRM 51-40-05-0 FIG 2 AND BOEING DWG 65-20726. INSTALLED FABRICATED REPAIR PARTS IAW BOEING 737-300 SRM 51-40-05 FIG 2. 2L72 4F RTA16WE 20050706002432005070600243WP 2005 7 6 IXXA05SMN41S 120050429A5330 SKIN DOUG DC8 DC871F 302199DWP OVERWING CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX834963359 45993 FUSELAGE SKIN CORRODED, STA 722.000 781.000, L-35L TO L-35R. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05163 DATE 04-28-05; SEMAN DWG ED-3961 DATED 04-20-05. REMOVED DAMAGED PLATING SEGMENT IAW SEMAN DWG ED-3961. PERFORMED NDT INSPECTION IAW DC-8 NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER STRAP (ALCLAD 7075 T6 0.090”), REPAIR TRIPLER STRAP (ALCLAD 7075 T6 0.100”), PLATING SEGMENT (ALCLAD 7075 T6 0.125”) IAW SEMAN DWG ED-3961. CLEANED, TREATED AND PRIMED REPAIR PARTS IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11 PAGE 9. INSTALLED REPAIR PARTS IAW SEMAN DWG ED-3961, DC-8 SRM 51-1-20D PAGE 9, DC-8 SRM 51-3-1 PAGE 1, DC-8 SRM 51-3-0 PAGE 1. 2L74 4F RT4A25 20050706002442005070600244WP 2005 7 6 IXXA05SMN42S 120050429A5313 LONGERON DOUG DC8 DC871F 302199DWP AFT CARGO BAY CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX834963359 45993 DURING ROUTINE C-CHECK INSPECTION, AFT CARGO COMPARTMENT CORROSION ON LONGERON 36 BETWEEN STA FS 1380.000 AND 1420.000. PERFORMED BLEND OUT 0.015, MATERIAL THICKNESS 0.150, REMAINING MATERIAL 0.135 ON LWR RADIO AREA AND BLEND OUT 0.011, MATERIAL THICKNESS 0.135, REMAINING MATERIAL 0.124 ON LONGITUDINAL HORIZONTAL LWR AREA FOUND WITHIN ALLOWABLE LIMITS IAW DC-8 SRM 53-2-0 FIG IF SHEET 3 PAGE 2P. APPLIED ALODINE AND REPAINTED AREA IAW DC-8 SRM 51-1-8B. 2L74 4F RT4A25 20050706002452005070600245WP 2005 7 6 IXXA05SMN43S 120050429A5230 SKIN DOUG DC8 DC871F 302199DWP CARGO DOOR CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX834963359 45993 DURING ROUTINE C-CHECK INSPECTION, CARGO DOOR EXTERNAL SKIN HAS 0.25 IN. CRACKS ON EDGES STA 1160.000 TO STA 1220.000, L-31R TO L-31L. PERFORMED MAJOR REPAIR IAW DC-8 SRM 52-1-0 PAGE 1, DC-8 SRM 52-4-1 FIG 1. REMOVED EXISTING DAMAGED SKIN IAW DC-8 SRM 51-1-21 PAGE 1. FABRICATED NEW SKIN (ALCLAD 2024 T6 0.050”) IAW DC-8 SRM 52-4-1 FIG. 1 ITEM Q CLEANED, TREATED AND PRIMED NEW SKIN AND AREA IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11 PAGE 9. INSTALLED NEW SKIN IAW DC-8 SRM 51-1-21 PAGE 1, DC-8 SRM 51-3-0 PAGE 1. TORQUED IAW DC-8 SRM 51-3-1. 2L74 4F RT4A25 20050706002462005070600246NM 2005 7 6 DHL2005741579 120050429A5543 SKIN BOEING727 7272Q9 138448MNM RUDDER TAB DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 LOWER RUDDER TAB DELAMINATED ON UPPER 4H SIDE STA 1523. CUT OUT DELAMINATED AREA ON LWR RUDDER TAB APPROX 1 INCH DIA. CLEANED, PREPPED AND APPLIED FIBERGLASS OVERLAYS. CURED, SANDED SMOOTH AND PRIMED AREA IAW B727 SRM 55-40-2 FIG 1 AND 51-40-9 PART 3 AND 4. 2L73 4F RTA3WE 20050706002472005070600247WP 2005 7 6 0500919623 120050609A5310 DOOR FRAME DOUG DC9 DC932 3022066WP FWD SERVICE DOORCRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01623NW 47591 DURING L-CHECK, FOUND CRACK IN FORWARD UPPER CORNER OF FORWARD SERVICE DOOR FRAME. REPAIRED PER EA 96-203593. 2L72 4F A6WE 20050707000022005070700002CE 2005 7 7 DXTA200500795 120050617A3241 ANTI-SKID SYS CESSNA500 560CESSNA 2076750CE MLG BRAKES MALFUNCTIONED E DXTAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL07334QS 5600434 PILOTS LEFT BRAKE IS MUSHY AND HAS TO BE PUMPED UP TO OPERATE. CO-PILOTS RIGHT BRAKE DOES THE SAME THING. DRAINED AND FLUSHED RESERVIOR AND BRAKE LINES. BLED ANTI-SKID BRAKE SYSTEM WITH SKYDROL 500-B-4. 2L72 4F RTA22CE 20050707000032005070700003NE 2005 7 7 DXTA200500792 220050620A7200 ENGINE CESSNA560 560XL 2076702CE PWA 545 PW545A NE LEFT MALFUNCTIONED E DXTAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 GL07624QS 5605302 PCEDB0335 ON TAKEOFF WITH THROTTLE IN THE T/O DETENT, THE LT ENGINE ITT EXCEEDED 720 DEG CELSIUS WITHIN 10 SECS. THE LT ITT INDICTED 724 DEG CELSIUS AND WAS STILL SLOWLY INCREASING. LT THROTTLE REDUCED TO CLIMB. DETENT AND ITT INDICATION IMMEDIATLY DECREASED BELOW 720DEG CELSIUS. NO OTHER PROBLEMS OBSERVED. PERFORMED 5 POINT PERFORMANCE RUN AND CHECK BOV POSITION. CHECKED RESISTANCE ON ITT HARNESS IAW PWA 545A MM 71-00-00. NO DEFECTS NOTED. OCF REQUESTED PER TECH REP. 2L72 4F4 FRTA22CE E00059EN 20050707000052005070700005NM 2005 7 7 DXTA200500800 120050623A2121 FAN AMD FALC50FALCON2000 2730170NM NR 4 PDU ODOR E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL07290QS 190 MODERATE TO STRONG BURNING ODOR WAS NOTICED IN COCKPIT AFTER DEPARTURE, ODOR BECAME FAINT AND THEN STRONGER SEVERAL TIMES. REMOVED AND REPLACED NR 4 PDU COOLING FAN ASSY. WITH A NEW FAN ASSEMBLY. OPS CHECK GOOD NO ODOR NOTED IN CABIN. WORK PERFORMED IAW FALCON 2000 MM 34-001. 2K73 4F RTA50NM 20050707000062005070700006NM 2005 7 7 05FDEA01653 120050622A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LEFT WING, FUEL TANK UPPER STRINGER END S-10 BETWEEN XORS 799 TO XORS 827. FOUND WITH APPROXIMATELY 10 INCH CRACKED. TRIMMED OUT PER SRM 57-20-00 VOLUME I, FIGURE 10. FABRICATED REPAIR DOUBLER INSTALLED PER SRM 51-33-01 VOLUME II. 2L73 4F RTA22WE 20050707000072005070700007NM 2005 7 7 05FDEA01669 120050623A5753ARC4009 SUPPORT FITTING DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 RT WING, WHILE ACCOMPLISHING EA NR 1-5750-87541, OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING FOUND CRACKED. REMOVED AND REPLACED PER AMM 27-50-30-4. FLAP RIGGING CARRIED OUT PER AMM 27-50-30-5. 2L73 4F RTA22WE 20050707000122005070700012NM 2005 7 7 TSAA0526026 120050625A2613899929 ELEMENT BOEING737 7372T4 1384492NM PWA JT8 JT8D9A 52048NE NR 2 ENG OVRHT FAILED A TSAAF ACTIVATE FIRE EXT. N FALSE WARNING TXTAXI/GRND HDL 1 WP13807AL 23443 P707403 DURING PUSHBACK AND PRIOR TO ENGINE START, THE CREW NOTED NR 2 ENGINE OVERHEAT INDICATION ILLUMINATED. THE CREW COMPLETED THE ENGINE OVERHEAT AND ENGINE FIRE CHECK LISTS AND DISCHARGED BOTH ENGINE FIRE EXTINGUISHER BOTTLES. AFTER DISCHARGING THE BOTTLES, THE INDICATION REMAINED ILLUMINATED. RETURNED TO GATE. MAINTENANCE R & R NR 2 ENGINE LOWER FIRE AND OVERHEAT ELEMENT. ENGINE RUN OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A16WE E2EA 20050707000182005070700018NE 2005 7 7 SF200506271 220050627A7230 COMPRESSOR SAAB SF340 SF340A 7850100EU GE CT7TS CT71 30030NE LT ENGINE FOD A UHLAA UNSCHED LANDING CRJF.O.D. PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 GL17121CQ 121 LT ENGINE NOTICEABLE HOTTER IN FLIGHT. ITT INCREASED 40 DEGREES FROM PREVIOUS FLIGHT. UNABLE TO HOLD CHARTED TQ BY AT LEAST 15 PERCENT AT ANY ALTITUDE OR OAT. ITT CHANGED FROM 7 DEGREES SPLIT TO 50 DEGREES SPLIT FROM PREVIOUS TREND. AIRCRAFT RETURNED AND WAS DETERMINED TO HAVE COMPRESSOR FOD DAMAGE. 2L72 4T4 URTA52EU E8NE 20050707000242005070700024NM 2005 7 7 DU4R0507131 120050630A5330 SKIN BOEING737 737 UTILSYSNM GE CFM56 CFM56* 13802NE FUSELAGE MISREPAIRED B DU4RK NONE W INADEQUATE Q C ININSP/MAINT 1 SO15387UA 24662 FUSELAGE RT SIDE BS 927-945.5 S-21R-22R HAS PREVIOUS REPAIR THAT ENDS ON A STRINGER. 2L72 4F4 FRTA16WE E2GL 20050707000292005070700029NE 2005 7 7 WRNA200500016 220050621A7200 ENGINE BOEING747 7472U3B 1384846NM PWA JT9 JT9D7Q 52054NE NR 2 DAMAGED A WRNAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO05922FT 22768 702340 VERY LOUD RUMBLE ON TAKE OFF. UPON LANDING, NR 2 ENGINE WAS FOUND TO HAVE COILS MISSING FROM LT SIDE. RT SIDE DAMAGED, ALONG WITH VARIOUS OTHER AREAS OF DAMAGE TO DUCT WORK, FIRE SEAL, AND HYD RACEWAY. ALL ITEMS WERE REPAIRED/REPLACED IAW MM 72-11-02,75-24-00,71-11-06, AND SRM 51-01-10. BOTH LT AND RT UPPER COWL LATCHES (COWL MOUNTS) INSPECTED. PERFORMED OVERALL VISUAL INSP OF ENTIRE ENGINE AND RELATED SYSTEMS TO INCLUDE FIRE PROTECTION. REPOSITIONED CLAMPS, BRACKETS, AND HOSES AS REQUIRED IAW 71-00-00. NO FURTHER DEFECTS NOTED, AIRCRAFT RETURNED TO SERVICE. 2L74 4F4 FRTA20WE E3NE 20050707000302005070700030NM 2005 7 7 TSAA0526025 120050619A2697 CONNECTOR BOEING737 7372T4 1384492NM PWA JT8 JT8D9A 52048NE OVERHEAT LOOP DIRTY A TSAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP13807AL 23443 P707403 ON CLIMB BETWEEN 11,000 FT AND 13,00 FT, PILOTS REPORTED NR 2 ENGINE OVERHEAT LIGHT FLICKERING AND THEN BECOMING STEADY. THE ENGINE OVERHEAT CHECKLIST WAS COMPLETED AND LIGHT WAS EXTINGUISHED. ENGINE WAS NOT SHUTDOWN, EMERGENCY DECLARED, AND THE AIRCRAFT RETURNED UNEVENTFULLY. CLEANED NR 2 ENGINE LOWER LOOP OVERHEAT DETECTION CONNECTORS. NO FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A16WE E2EA 20050707000312005070700031EA 2005 7 7 JBGA20050004 120050623A56106003303026 WINDSHIELD CNDAIRCL600 CL6002B16 1900305EA GE CF34 CF34* NE COCKPIT CRACKED E JBGAO OTHER O OTHER CRCRUISE 1 GL07881TW3781 5348 COPILOT WINDSHIELD CRACKED OUTER PLY. 2L72 4F4 FRTA21EA E15NE 20050707000342005070700034CE 2005 7 7 DXTA200500815 120050702A2130 PRESSURE SYSTEM CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE CABIN PRESSURE FAILED E DXTAO OTHER G MULTIPLE FAILURE CLCLIMB 1 GL07339QS 5600339 AIRCRAFT LOST ALL PRESSURIZATION AT 23,000 FT AS THE THROTTLES WERE PULLED BACK PAST 90 PERCENT. THE EMERGENCY CABIN ALT LIGHT AND MASTER WARNING CAME ON. EMERGENCY PRESSURE FAILED TO PRESSURIZE THE PLANE. THE MASKS DID NOT DROP. ITEM IS UNDER INVESTIGATION. 2L72 4F4 FRTA22CE E25EA 20050707000382005070700038EA 2005 7 7 COMA0560363 120050621A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE EMERGENCY LIGHT DAMAGED A COMAO OTHER O OTHER TXTAXI/GRND HDL 1 SO27427CA 7460 FWD SECTION OF EMERGENCY FLOOR LIGHTING INOPERABLE. WARDROBE EMERGENCY LIGHT WIRING DAMAGED. REPAIRED WIRING AND EMERGENCY LIGHTS. OPERATION SATISFACTORY. 2L72 4F4 FRTA21EA E15NE 20050707000402005070700040EA 2005 7 7 COMA0560364 120050626A335060206 SIGN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE EMERGENCY EXIT INOPERATIVE A COMAO OTHER O OTHER TXTAXI/GRND HDL 1 SO27455CA 7592 FWD EMERGENCY EXIT SIGN INOPERATIVE. REPLACED EXIT SIGN. 2L72 4F4 FRTA21EA E15NE 20050707000412005070700041NM 2005 7 7 ASMF200506025 120050624A2741 TRIM SYSTEM BOEING737 737500* NM STABILIZER MALFUNCTIONED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23852AM 33787 AIRCRAFT RETURNED TO PLATFORM, PSEU AND OVERHEAD LIGHTS TURNED ON IN UPPER PANEL. BITE TO PROXIMITY UNIT SWITCH WAS PERFORMED SHOWING STAB TRIM DISAGREE FAILURE CODE. STABILIZER WAS COMPLETELY DEPLOYED AND CONFIGURED AGAIN IN TAKEOFF MODE TURNING OFF THE LIGHT AND TESTED CORRECT IAW FIM 32-09 TASK 816. DURING OVERNIGHT SERVICE, TEST WAS PERFORMED IAW FIM 32-09 TASK 801, ALL CORRECT. 2L72 4F RTA16WE 20050707000422005070700042NM 2005 7 7 ASMF200506026 120050626A30106712125180 THERMOSWITCH DOUG MD88 MD88 3023688NM PWA JT8 JT8D* NE ANTI ICE SYSTEM FAILED W ASMFO OTHER J WARNING INDICATION CRCRUISE 1 SW23168PL 53174 AIRCRAFT ARRIVED WITH CAPTAIN REPORT WHEN AIRFOIL ANTI-ICE IS IN USE, THE AIRFOIL PRESS ABNORMAL LIGHTS TURNED ON, THE TIME PRESS INDICATION SHOWS 60 PSI, THE LAND R ICE PROTECT TEMP LOW LIGHTS TURNED ON AND LT AND RT AIR COND TEMP HIGH LIGHTS TURNED ON. ANTI-ICE REGULATOR VALVE WAS REPLACED NOT CORRECTING THE FAILURE, SO THE ELECTRICAL CIRCUIT WAS CHECKED IAW WDM 30-11-01, DETECTING THE SWITCH S1-293 FAILED. IT WAS REPLACED IAW MM 30-10-11, TESTED CORRECT. DURING OVERNIGHT SERVICE WERE PERFORMED TESTS IN MODE 2 IAW MM 36-10-00, BEING ALL CORRECT. 2L72 4F4 FRTA6WE E2EA 20050707000432005070700043CE 2005 7 7 DJFA2005118 120050628A2120 SMOKE BEECH MU300 400A 1155402CE PWA JT15 JT15D5 52112NE COCKPIT DETECTED E DJFAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA23689TA RK327 CREW REPORTED A WHITE HAZY SMOKE LIKE VAPOR EMITTING INTO THE COCKPIT. SOON AFTER COMPLETING THE REQUIRED CHECKLISTS THE SMOKE HAD DISSIPATED AND DID NOT RETURN. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT WAS DIVERTED. 2H72 4F4 FRTA16SW E25EA 20050707000442005070700044EU 2005 7 7 DHL2005363005 120050630A2420 GCU AIRBUS300 A300B4203 3930306EU GE CF6 CF650* 30018NE NR 1 GENERATOR FAILED A DHLAC ABORTED TAKEOFF H ELECT. POWER LOSS-50 PC TOTAKEOFF 1 SO01363DH 85 POWER INTERUPTION B4 GEN 1 RESULTING IN RTO. DEFERRED NR 1 GEN IAW MEL 24-11-01 CONTROL NR 21499 ID NR 8742. PERFORMED AC GEN ADJ/TEST IAW MM 24-11-00 SYS OPS OK FOR SERVICE THIS CLEARS DMI NR 21499 REPLACED NR 1 GCU IAW MM 24-21-00. RAN ENG. IAW JRH 16.5. 2L72 4F4 FRTA35EU E23EA 20050707000452005070700045SO 2005 7 7 RAIA00506029 120050622A3260 PROXIMITY SENSOR EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL MLG DIRTY A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03822HK 145069 LANDING GEAR AIR GROUND MESSAGE ON EICAS. MAINTENANCE CLEANED ALL AIR/GRD PROXIMITY SWITCHES AND PERFORMED RESET OF LGEU AIR/GRD LOGIC. OPS CHECKED GOOD. 2L72 4T4 FRTT00011ATTE6CH 20050707000462005070700046SO 2005 7 7 RAIA00506030 120050623A32608005701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL MLG FAILED A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03822HK 145069 LANDING GEAR AIR/GROUND FAIL MESSAGE. MAINTENANCE REMOVED AND REPLACED THE RT NR 2 AND THE LT NR 2 PROXIMITY SWITCHES. EXTENSION AND RETRACTION CHECKED GOOD. 2L72 4T4 FRTT00011ATTE6CH 20050707000472005070700047 2005 7 7 RAIA00506031 420050627A31407013348949 DAU EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 1 FAILED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03810HK878 145231 DATA ACQUISITION UNIT FAILED. MAINTENANCE REMOVED AND REPLACED THE NR 1 DAU. OPS CHECKED GOOD. 2L72 4T4 FRTT00011ATTE6CH 20050707000482005070700048SO 2005 7 7 RAIA00506032 120050627A3230355022002 CONTROL UNIT EMB 145 EMB145ER 3260211SO ALLSN AE300 AE3007A GL MLG FAILED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03808HK 145157 LANGING GEAR AIR/GROUND FAILURE MESSAGE. MAINTENANCE REMOVED AND REPLACED THE LGEU. OPS CHECKED GOOD. 2L72 4F4 FRTT00011ATTE6CH 20050707000492005070700049SO 2005 7 7 RAIA00506034 120050628A3260852701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL MLG FAILED A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03822HK139498886 145069 LANDING GEAR AIR/GROUND FAIL MESSAGE ON EICAS. MAINTENANCE REMOVED AND REPLACED THE AFT PROX SWITCH ON THE RT MLG. OPS CHECKED GOOD. 2L72 4T4 FRTT00011ATTE6CH 20050707000502005070700050SO 2005 7 7 RAIA00506033 120050628A3620 RELAY EMB 145 EMB145LR 3260212SO ALLSN AE3007AE3007C GL BLEED AIR FAILED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03819HK 145062 NR 2 BLEED VALVE CLOSED ADVISORY MESSAGE CYCLING ON AND OFF. MAINTENANCE REMOVED AND REPLACED THE C7 RELAY IN THE RT RELAY SUPPORT. OPS CHECKED GOOD. 2L72 4T4 FRTT00011ATTE6CH 20050707000522005070700052SO 2005 7 7 647062705 120050627A523032156481 REGULATOR GULSTMGV GULFSTREAMGV3980116SO RROYCEBR700 BR700710A110 NE CARGO DOOR SEAL FAILED E N93AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO13511QS3798 647 CLIMBING OUT CARGO BAY LOW PRESSURE INDICATION ILLUMINATED. 2L72 4F4 FRTA12EA E00057EN 20050707000532005070700053SO 2005 7 7 XGN2005F00006 220050614A8530784819 CYLINDER CESSNA402 402B 207590PCE CONT O520 TSIO520E 17040SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW055421M1094 402B0021 THIS CYLINDER WAS IN THE NR 6 POSITION AND IS A TYPE (X) HEAD. THIS CRACKED VYLINDER HEAD WAS FOUND AT THE 100 HOUR INSPECTION. WE ARE FINDING SIGNS OF AIR LEAKAGE ON THE EXHAUST SIDE OF THE CYLINDER HEAD WHEN DOING A COMPRESSION CHECK. WE ARE SPRAYING SOAPY WATER ON THE CYLINDER HEAD. (K) 1L72 3O3 O A7CE E8CE 20050707000552005070700055EA 2005 7 7 MASA200500493 120050626A3350 LAMP CNDAIRCL600 CL6002D24 1390016EA GE CF34 CF34* NE EMERGENCY LIGHT INOPERATIVE A MASAK NONE O OTHER ININSP/MAINT 1 SW07908FJ 15008 EMERGENCY LIGHT OVER ROW 17F WAS INOPERATIVE. MAINTENANCE RELAMPED THE LIGHT. 2L72 4F4 FRTA21EA E15NE 20050707000562005070700056SO 2005 7 7 MASA200500496 120050627A3397 CONNECTOR EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT UNSECURE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07853MJ 145464 RT EMERGENCY EXIT SIGN LIGHT INOPERATIVE. MAINTENANCE SECURED CONNECTOR TO LIGHT ASSY. NO FURTHER DEFECTS NOTED. 2L72 4T4 FRTT00011ATTE6CH 20050707000582005070700058SO 2005 7 7 MASA200500514 120050703A3350 LIGHT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL CABIN INTERMITTENT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07853MJ 145464 THE CAPTAIN REPORTED THE FIRST 2 EMERGENCY EXIT FLOOR LIGHTING STRIPS WERE INOPERATIVE. MAINTENANCE RESPONDED TO THE AIRCRAFT AND FOUND THEM TO CHECK NORMALLY. 2L72 4T4 FRTT00011ATTE6CH 20050707000592005070700059 2005 7 7 YENA200535 420050628A23303042865102 ELECTRICAL BOX AIRBUS320 A320232 3930326EU IAE V2524 V2524A5 NE LIVE TV SYS FAILED A YENAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15523JB7637 1506 DURING CRUSE, DETECTED ELECTRICAL BURNING ODOR ROW 23-25. AFTER TURNING THE TV MASTER OFF THE ODOR WENT AWAY. INSPECTED ROW 23-25 ABC DEF AND NO FAULT FOUND. REMOVED AND REPLACED LIVE TV SEB AT 24E AS PRECAUTIONARY IAW INFO NOTICE 2004-T023TR. OPS CHECK NORMAL. 2L72 4F4 FRTA28NM E40NE 20050707000632005070700063NM 2005 7 7 05FDEA01776 120050701A5310601023418 TEE FITTING BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25272FE 22037 TEE CHORD 760 -787 RBL 45 IS CORRODED. REMOVED AND REPLACED TEE CHORD IAW SRM 51-30- 2 2L73 4F RTA3WE 20050707000652005070700065NM 2005 7 7 05FDEA01778 120050702A5347 SEAT TRACK BOEING727 727200 138407ENM FUSLEAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25272FE 22037 SEAT TRACK LBL 24 HAS CORROSION AT 500 TO 520 AND STA 620. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-10-5 FIG 1 PG 4 2L73 4F RTA3WE 20050707000662005070700066NM 2005 7 7 05FDEA01779 120050703A5313 LONGERON DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 CENTER CARGO BAY. RT STA 1641 LONGERON 44 , FOUND CORRODED AS MARKED. CENTER CARGO COMPT. R/H STA 1641 LONGERON 44 ,NEW LONGERON 44 FABRICATED AS PER DRAWING AFA 7779 AND NEW SPLICE REPAIRED AS PER SRM 53-10-00 VOL I AND AS PER SRM 51-32-01 VOL II. MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050707000682005070700068NM 2005 7 7 05FDEA01786 120050703A5311 FRAME DOUG MD11 MD11 3023602NM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 CENTER CARGO BAY AT STA 1841 RT LOWER FRAME PATCH REPAIR FOUND DENTED AS MARKED. CENTER CARGO COMPARTMENT,LOWER FRAME AT STA 1841 RH WEB REMOVED AS PER SRM 51-53-01 VOL II. NEW WEB FABRICATED AS PER DRAWING AGA 7170, NEW WEB INSTALLED AS PER SRM 51-53-01 VOL II. MINOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050705000922005070500092NM 2005 7 5 ASMF200506021 120050619A8011784750A3 STARTER BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE RT ENGINE FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23804AM276041255 26271 716340 ACFT RETURNED TO PLATFORM. DURING RT ENGINE STARTING, N2 INDICATION REACHED 23 PERCENT AND WENT TO ZERO. PNEUMATIC STARTER AND PNEUMATIC STARTER VALVE REPLACED IAW MM 80-11-01 / -02, TESTED CORRECT. 2L72 4F4 FRTA2NM E17NE 20050705000972005070500097SO 2005 7 5 SWIA200515150 120050614A3397 WIRE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHTSDAMAGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07218SW 120287 EXIT ROW LIGHT ROW 9 DOES NOT ILLUMINATE. REPAIRED WIRING INSIDE OVERHEAD BIN AT ROW 9. OPS CHECK GOOD. 2L72 4T RTA31SO 20050705001032005070500103EA 2005 7 5 SWIA200515156 120050604A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07919SW 7657 CARGO PIT FLOOR SUPPORT ANGLE CRACKED AT FS 621.0 LBL 38.0. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-61-117 REV "B". 2L72 4F RTA21EA 20050705001072005070500107NM 2005 7 5 USAA050702 120050517A532269730578LF SHEAR TIE BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19574US50136 23739 FOUND SHEAR TIE CRACKED 1 INCH, FS 520 BETWEEN S13R AND S14R. REMOVED, FABRICATED AND REPLACED SHEAR TIE PER SRM 51-40-02 AND DWG 69-73057. (M) 2L72 4F RTA16WE 20050705001112005070500111NM 2005 7 5 USAA050688 120050526A5315 FLOORBEAM BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19445US 24863 FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH, RBL 24 STATION 965. REPLACED TEE CAP IAW SRM 53-00-51. (M) 2L72 4F RTA16WE 20050705001182005070500118NM 2005 7 5 USAA050552 120050423A5330148N3211 SKIN BOEING757 757225 1384959NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19608AU 22204 BFM - FOUND SKIN CRACKED 3 INCHES, FRAME 1735 BETWEEN S11 R AND S13 R, . ACCOMPLISHED TYPICAL WEB REPAIR DOUBLER PER SRM 51-70-13, 53-80-01. (M) 2L72 4F RTA2NM 20050705001192005070500119NM 2005 7 5 USAA050597 120050506A5313 STRINGER BOEING757 757225 1384959NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19608AU 22204 FOUND STRINGER CORRODED 2 INCHES BY .6 INCHES BY .045 INCH DEEP, STRINGER 29L, STATION 1720. REMOVED DAMAGED SECTION. INSTALLED NEW STRINGER WITH SPLICES PER SRM 53-00-03 PAGE 101 AND FIG 201. (M) 2L72 4F RTA2NM 20050705001282005070500128EU 2005 7 5 USAA050631 120050419A5320F5347823420000 FLOOR SUPPORT AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW24199 0333 BFM - FOUND FLOOR SUPPORT CORRODED 1 INCH BY 1 INCH BY .060 INCH DEEP, Y450 AT FRAME 75. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-74-00, 53-00-15, 51-42-11. (M) 2L72 4F RTA46NM 20050705001452005070500145EU 2005 7 5 USAA050614 120050503A5320F53315329200 FLANGE AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW24199 0333 BFM - FOUND FLANGE CORRODED 2.3 INCHES LONG BY 2 INCHES WIDE BY .035 INCHES DEEP, 2.7 INCHES LONG BY 2 INCHES WIDE BY.036 INCH, A/C BAY 1, FRAME 40. REMOVED AND REPLACE FLANGE PER SRM 51-72-11, 51-42-00, 51-42-11. (M) 2L72 4F RTA46NM 20050705001522005070500152EU 2005 7 5 USAA050607 120050427A5315F5311171120000 FLOORBEAM AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW24199 0333 BFM - FOUND FLOORBEAM CORRODED 1.300 INCHES LONG BY 1 INCHES WIDE BY .035 INCH DEEP, FRAME 13B Y-450 TO -953. CORROSION LEVEL 2, TASK C531172-01. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 53-11-14, 51-74-00. (M) 2L72 4F RTA46NM 20050705001582005070500158EU 2005 7 5 USAA050601 120050428A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW24199 0333 BFM - FOUND SEAT TRACK CHAFED 4 INCHES LONG BY 1 INCH WIDE BY .019 INCH DEEP, SEAT TRACK Y2462 AT FRAME 51.1. FABRICATED SEAT TRACK PER SRM 53-31-15, 51-42-11, 51-23-11. (M) 2L72 4F RTA46NM 20050706000072005070600007EU 2005 7 6 USAA050678 120050523A5310D5347217220500 BEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19716UW 1055 PIT - FOUND BEAM CORRODED 2 INCHES BY 20 INCHES, AT -Y 52 INCHES BETWEEN FRAME 67-68. REMOVED AND REPLACED BEAM PER SRM 51-72-11. (M) 2L72 4F RTA28NM 20050706000132005070600013EU 2005 7 6 USAA050684 120050518A5315 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19716UW 1055 PIT - FOUND FLOORBEAM CORRODED 20 INCHES BY 3 INCHES, AT Y 48 INCHES BETWEEN FRAME 66-68. REPLACED FLOORBEAM PER SRM 51-72-11 AND D53472780 A/D DWG. (M) 2L72 4F RTA28NM 20050706000152005070600015NM 2005 7 6 USAA050640 120050510A5514 WEB BOEING737 7374B7 1384702NM HORIZONTAL STAB DEBONDED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US 24781 CLT - FOUND WEB DISBOND 1 INCH BY 1 INCH, LEFT HORIZ STAB RIB DISBONDED OUTBOARD OF OUTBOARD BALANCE, PANEL STATION 149.12. DEFECTIVE PART REPLACED WITH IDENTICAL PART, IAW SRM 51-40-02. (M) 2L72 4F RTA16WE 20050706000292005070600029NM 2005 7 6 USAA050669 120050520A5315 FLOORBEAM BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19445US40360 24863 CLT - FOUND FLOORBEAM CAP CORRODED .250 INCH BY .250 INCH, STATION 312 FLOORBEAM AROUND SCREW HOLE RBL 38. FABRICATING NEW SECTION OF FLOORBEAM P/N BAC 1505-100246 FLOOR IAW SRM 53-10-51. (M) 2L72 4F RTA16WE 20050706000362005070600036NM 2005 7 6 USAA050676 120050521A5512657378352 SKIN BOEING737 7374B7 1384702NM HORIZONTAL STAB CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19445US40364 24863 CLT - FOUND HORIZ STAB LOWER SKIN CRACKED .25 INCH, STATION 125. 3 INCHES FORWARD OF AFT SPAR. REPLACED DOUBLER AND INSTALLED SOLID FASTENERS IAW T/R 55-10-07 REV B, BOEING SRM 55-10-01 FIG 204. (M) 2L72 4F RTA16WE 20050706000392005070600039NM 2005 7 6 DHL2005741600 120050525A5754 RIB BOEING727 7272Q9 138448MNM NR 7 SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 NR 7 SLAT O/B OF ACTUATOR ROD HAS CRACKED RIB AT WS 650. REMOVED CRACK RIB, FABRICATED NEW RIB, MATL 2024-T3 .040 PO 9002248, 16 X 5 INCH IAW B727 SRM 51-30-2 AND 57-50-2 FIG 2. TREATED AND PRIMED RIB IAW B727 SRM 51-10-2, INSTALLED RIB IAW B727 SRM 51-30-2. 2L73 4F RTA3WE 20050706000572005070600057NM 2005 7 6 P5CA0501372 120050622A5414 SKIN BOEING747 747230B 1384889NM NR 4 NACELLE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 EA15509MC 21221 CRACK AT NR 4 NACELLE STRUT TOP FORWARD CORNER OF PRECOOLER EXHAUST CUTOUT. PRECOOLER EXHAUST CUTOUT REPAIRED PER BOEING INSTRUCTIONS 1-1MNS9D AND FAA FORM 8100-9. 2L74 4F A20WE 20050706000632005070600063SO 2005 7 6 TZR2005F00026 220050610A8530ACE520T101 CYLINDER CESSNA401 401A 207590DCE CONT O520 GTSIO520C 17032SO RT ENGINE CRACKED E TZRAO OTHER O OTHER NRNOT REPORTED 1 SW05409TE455 401A0118 CRACK IS TYPICAL FOR THESE CYLINDERS, RT ENGINE NR 6 CYLINDER. (SW05200509365) (K) 1L72 3O3 O A7CE E7CE 20050706000652005070600065SO 2005 7 6 TZR2005F00021 220050610A8530ACE5207101 CYLINDER CESSNA401 401A 207590DCE CONT O520 GTSIO520* 17032SO LT ENGINE CRACKED E TZRAO OTHER O OTHER NRNOT REPORTED 1 SW05409TE 89 401A0118 CRACK IS TYPICAL FOR THESE CYLINDERS, LT NR 3, (SW05200509362). (K) 1L72 3O3 O A7CE E7CE 20050706000842005070600084CE 2005 7 6 DXTA200500811 120050629A323397125373 ACTUATOR CESSNA560 560XL 2076702CE PWA 545 PW545A NE MLG OUT OF ADJUST E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07645QS4585 5605145 AFTER TAKEOFF AND RETRACTING GEAR AND FLAPS-GEAR UNLOCK (RED) LIGHT REMAINED LIT AND STAB MISCOMPARE LIGHT CAME ON. ADJUSTED LT MAIN LANDING GEAR ACTUATOR IAW MM. OPS TESTED LANDING GEAR TEN TIMES WITH NO FAULTS. 2L72 4F4 FRTA22CE E00059EN 20050706000942005070600094NM 2005 7 6 DL76L050327 120050618A256061020 BATTERY BOEING767 767332 1382001NM 2L DOOR DISCHARGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27175DN 24803 FLIGHT ATTENDANT 2L DOOR FLASHLIGHT INOP. BATTERY LOW, REPLACED SAME. 2L72 4F RTA1NM 20050706000962005070600096 2005 7 6 05FDEA01714 420050628A3416 INDICATOR AIRBUS310 A310 EU AIRSPEED MALFUNCTIONED A FDEAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 SO25432FE 326 REJECTED TAKE OFF, CAPT'S AIRSPEED READ 100 KTS, FO STILL BELOW 80. REJECT NORMAL. PUMPED UP BOTH FO AND CAPT AIRSPEED WITH TEST BOX. FO LAGGED BEHIND CAPT. REMOVED AND REPLACED ADC 2 PER AMM 34-11-34-4. TESTED FO AIRSPEED INDICATOR WITH TEST BOX PER AMM 34-13-00-0. OPS CHECKS NORMAL. BLEW OUT FO PITOT SYSTEM WITH DRY NITROGEN PER AMM 34-10-00-3. NO DEBRIS FOUND. AIRCRAFT OK FOR SERVICE. PREMATURE REMOVAL/INSTALLATION . 2L72 4F RTA35EU 20050706001012005070600101NM 2005 7 6 05FDEA01721 120050628A5320602757019 FLOOR SUPPORT BOEING727 727200 138407ENM CARGO BAY CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25203FE 22925 AFT PIT BS 950A BL 0 FLOOR SUPPORT ANGLE HAS CORROSION UNDER NUT PLATES. REPLACED FLOOR SUPPORT ANGLE IAW SRM 51-30-2 2L73 4F RTA3WE 20050706001092005070600109NM 2005 7 6 05FDEA01729 120050628A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25619FE 48770 LT BARREL NUT HOLE NR 28L FOUND OUT OF LIMIT AFTER CORROSION REMOVAL. REPAIRED AS PER FEDEX EA 1-5510-83022. 2L73 4F RTA22WE 20050706001102005070600110NM 2005 7 6 05FDEA01718 120050628A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25272FE 22037 344 FRAME CHAFED AT STR'S 4R,6R & 8R. FABRICATED AND INSTALLED REPAIR CHANNEL IAW SRM 51-40-3 2L73 4F RTA3WE 20050706001262005070600126NM 2005 7 6 05FDEA01757 120050701A5330 SKIN DOUG MD11 MD11 3023602NM ZONE 300 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25619FE 48770 DURING AFT EXTENDED TAILCONE REMOVAL, FOUND INTERIOR SKIN DETACHED AT SEVERAL LOCATIONS. EXTENDED TAILCONE REPLACED AS PER AMM 53-52-01-4. (CLOSED) 2L73 4F RTA22WE 20050706001312005070600131NM 2005 7 6 05FDEA01733 120050629A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) AFT HINGE FITTING AFT BOLT HOLE FOUND CORRODED. REMOVED AND REPLACED PER AMM 27-50-30-4. 2L73 4F RTA22WE 20050706001362005070600136NM 2005 7 6 05FDEA01739 120050629A5347 SEAT TRACK DOUG MD11 MD11 3023602NM FUSLEAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 ALONG STA 1821 TO STA 1887 RBL 8.75 SEAT TRACK CROWN AND BASE FOUND CORRODED. CARRIED OUT REPAIR AS PER SRM 53-70-00. [CLOSED] 2L73 4F RTA22WE 20050706001392005070600139NM 2005 7 6 05FDEA01711 120050628A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 RT WING, OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) FORWARD HINGE. COMPLIED WITH FEDEX EA 1-5750-87546. 2L73 4F RTA22WE 20050706001412005070600141NM 2005 7 6 05FDEA01595 120050613A5320ABA72027 WEB DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 RT OBSERVER SEAT CUT OUT FOUND CRACKED. CRACKED WEB AT COCKPIT FAC CARRIED OUT REPAIR AS PER SRM 53-00-01 VOLUME I, FIGURE 5 AT STA 366. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050706001432005070600143NM 2005 7 6 RYAN200500019 120050525A5315 FLOORBEAM BOEING757 757236 1384971NM FUSELAGE CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07526NA 24794 FLOORBEAM HAS CORROSION AT UPPER CAP BS 1640 RBL48. 2L72 4F RTA2NM 20050706001452005070600145CE 2005 7 6 DXTA200500796 120050621A321367940624 STRUT CESSNA750 750 2076810CE MLG FAILED E DXTAO OTHER J WARNING INDICATION LDLANDING 1 GL07990QS3296 7500190 AFTER TO GEAR RETRACTION NORMAL, A FEW MINUTES LATER GEAR MOVEMENT TYPE NOISE HEARD WITH NO LIGHTS OR PARTIAL EXTENSION. NOISES FOLLOWED A FEW SECONDS LATER BY RED 'UNLOCK' LIGHT NO EXTENSION AND HYD PRESSURES AND QTY'S NORMAL THROUGHOUT FLIGHT. GEAR EXTENDED NORMALLY WHEN SELECTED DOWN. REMOVED AND REPLACED UPPER & LOWER BARREL ASSY. ON THE NOSE LANDING GEAR DUE TO INTERNAL FAILURE. OPS AND LEAK CHECK NORMAL. WORK IAW CESSNA 750 M/M CHPT 32-20-04. 2L72 4J RTT00007WI 20050706001512005070600151EU 2005 7 6 DXTA200500788 120050619A3260 POSITION SWITCH BRAERO1000 HAWKER1000 7450005EU MLG MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07551QS 259051 DEPARTING LIT GEAR SELECTED UP L MAIN GEAR UNSAFE LIGHT ILLUMINATED. 400FT AGL SELECTED FLAPS UP AND GEAR LIGHT EXTINGUISHED. CYCLED LANDING GEAR OPS GOOD. AT 15000 MSL, L MAIN GEAR LIGHT ILLUMINATED AND WOULD NOT EXTINGUISH. ADJUSTED LT MLG DOOR UPLOCK SWITCH IAW HAWKER 100 AAM 32-60-05 OPS GOOD. 2L72 4F RTA3EU 20050706001632005070600163WP 2005 7 6 IXXA05SMN08S 120050429A5320 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX834963359 45993 DURING ROUTINE C-CHECK INSPECTION, AFT CARGO COMPT SPLICE FITTING CRACKED 9 IN., L-31L , STA 1040.00 - STA 1060.000. REMOVED CRACKED FITTING IAW DC-8 SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING IAW DWG 3750257. PERFORMED NDT INSPECTION TO FITTING IAW NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED AREA AND NEW FITTING IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO IAW DC-8 SRM 51-1-11 PAGE 9. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D PAGE 9. TORQUED IAW DC-8 RM 51-3-1. 2L74 4F RT4A25 20050706001642005070600164WP 2005 7 6 IXXA05SMN09S 120050429A5320 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX834963359 45993 DURING ROUTINE C-CHECK INSPECTION, AFT CARGO COMPARTMENT SPLICE FITTING CRACKED 3 IN., STA 1040.000, STA 1060.00, L-31R. REMOVED CRACKED FITTING IAW DC-8 SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING IAW DWG 3750330. PERFORMED NDT INSPECTION TO FITTING IAW NDT SPM PART 08-00-02/07. CLEANED, TREATED, PRIMED AREA AND NEW FITTING IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO IAW DC-8 SRM 51-1-11 PAGE 9. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D PAGE 9. TORQUED IAW DC-8 RM 51-3-1. 2L74 4F RT4A25 20050706001662005070600166WP 2005 7 6 IXXA05SMN11S 120050429A5342 FITTING DOUG DC8 DC871F 302199DWP HORIZONTAL STAB CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX834963359 45993 DURING ROUTINE C-CHECK INSPECTION, RT HORIZONTAL STABILIZER FITTING CRACKED 1 IN., XFS 47.000 - XFS 60.000 (LWR PART). REMOVED CRACKED FITTING IAW DC-8 SRM 51-1-20D PAGE 21. CLEANED, TREATED AND PRIMED IAW DC-8 SRM 51-1-8B. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D PAGE 9, DC-8 SRM 51-1-21 PAGE 1. TORQUED IAW DC-8 RM 51-3-1. 2L74 4F RT4A25 20050706001692005070600169WP 2005 7 6 IXXA05SMN14S 120050429A5730 SKIN DOUG DC8 DC871F 302199DWP RT WING CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX834963359 45993 RT WING, LE LWR SKIN WITH 03 CRACKS , XW 422.750. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3. REMOVED EXISTING REPAIR DOUBLER IAW SEMAN DWG ED-3950, DC-8 SRM. REMOVED DAMAGED AREA IAW SEMAN DWG ED-3950. PERFORMED NDT INSPECTION IAW DC-8 NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER, FILLERS IAW SEMAN DWG ED-3950. CLEANED, TREATED AND PRIMED REPAIR PARTS IAW DC-8 SRM. APPLIED SEALANT TO FAYING SURFACES IAW DC-8 SRM. 2L74 4F RT4A25 20050706001852005070600185EU 2005 7 6 MALA050493 120050620A5347 SEAT TRACK SAAB SF340 340B 7860101EU CABIN CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15421XJ 340B421 DURING 4K INSPECTION, FOUND SEAT TRACK AT LBL18.3 CORRODED AND HAS BEEN REPAIRED IAW SRM 53-70-60 BETWEEN FS 297 AND 304. 2L72 4T RTA52EU 20050706002072005070600207NM 2005 7 6 AALA20050392 120050618A3350P4010049 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHTSINOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21620AA 24578 FIRST CLASS EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FIRST CLASS EMERGENCY LIGHTS. SYSTEM GROUND CHECKED. NORMAL OPERATION. 2L72 4F RTA2NM 20050706002092005070600209WP 2005 7 6 AALA20050394 120050620A3350 SOCKET DOUG DC9 DC983 3022083WP EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21984TW 53634 EMERGENCY LIGHT AT 11D INOPERATIVE. REPLACED EMERGENCY LIGHT SOCKET AT SEAT 11D. SYSTEM GROUND CHECKED. NORMAL OPERATION. 2L72 4F RTA6WE 20050706002112005070600211WP 2005 7 6 AALA20050396 120050619A339760030451 WIRE DOUG DC9 DC983 3022083WP EMERGENCY LIGHTSSHORTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW219620D 53591 EMERGENCY LIGHTS CAME ON WHEN SELECTED OFF. CIRCUIT BREAKER Z37 POPPED. FOUND SHORTED WIRE ON BATTERY PACK B5105. REPOSITIONED AND SECURED WIRE ON BATTERY PACK B5105 FOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED. NORMAL OPERATION. 2L72 4F RTA6WE 20050706002132005070600213WP 2005 7 6 AALA20050395 120050620A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21492AA 49730 CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK B5 107 AT STATION 1190 FOR CEILING EMERGENCY LIGHT. SYSTEM GROUND CHECKED. NORMAL OPERATION. 2L72 4F A6WE 20050706002152005070600215NM 2005 7 6 AALA20050398 120050620A3350P4010049 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21172AJ 32400 EMERGENCY EXIT DOOR LIGHTS ON SEATS 16D THROUGH 25D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT DOOR LIGHTS ON SEATS 16D THROUGH 25D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050707000042005070700004CE 2005 7 7 DXTA200500793 120050620A2797 GROUND WIRE CESSNA750 750 2076810CE RESOLVER CONVERTFAULTY E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07962QS 7500126 DURING CLIMB AROUND FL270, OBSERVED AN AMBER "FLAPS FAIL" CAS MESSAGE. IT RESET/WENT OUT WHEN PRESSED THE FLAP RESET BUTTON. THIS HAPPENED 4 TIMES. ON APPROACH AND LANDING THE FLAPS OPERATED NORMALLY. FOUND FAULTY GROUND AT G7048-COMMON GROUND FOR RESOLVER CONVERTER, REWORKED GROUND STUD, FLAP SYSTEM OPS CHECK GOOD. IAW CE750 MM CHAP. 27-50-00 2L72 4J RTT00007WI 20050707000082005070700008NM 2005 7 7 QXEA200501083 120050627A3320404930 LIGHT DHAV DHC8 DHC8202 2809007NM ZONE 200 BURNED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM09352PH 494 ELECTRICAL SMOKE ODOR DETECTED IN AFT CABIN. FOUND SIDEWALL LIGHT ROW 9A BURNED. REMOVED BULB AND DISABLED SYSTEM BY PULLING C/B'S. CLEANED LIGHT ASSEMBLY. NO ELECTRICAL ODOR NOTED WITH POWER ON. PLACED ON MEL. REPLACED DAMAGED LAMP SOCKET FOR SIDEWALL LIGHT AT ROW 9A. INSTALLED NEW FLOURESCENT TUBES FOR SIDEWALL LIGHT AT ROW 8 & 9A. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050707000262005070700026NM 2005 7 7 DHL2005741609 120050611A5330 DOUBLER BOEING727 7272Q9 138448MNM PWA JT8 JT8D17 52049NE FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 MAIN CARGO DOOR CUTOUT SURROUNDING EXTERNAL DOUBLER HAS 3EA CRACKS AT STA: 561 (MATING SURFACE FOR MCD HINGE) TRIMMED-OUT 3.45 INCH X .440 INCH SECTION OF AEI-38 EXTERNAL SURROUND DOUBLER AT STA 561 TO REMOVE ALL 3 CRACKS IAW AEI EO 1448 FABRICATED FILLER FOR EXTERNAL DOUBLER SIZE 3.34 INCH X .440 INCH X .100 INCH THICK 2024-T3 MATERIAL PO9002219, TREATED/PRIMED FILLER AND TRIMMED EDGE IAW AEI EO NR 1448, SRM 51-10-2 INSTALLED NEW FILLER SECTION AND SEALED EDGES GAP IAW EAI RO 1448 AND B727 SRM 51-20-4 W/8110-3 DATED 6-10-05 ASTAR INSP NOTE: A RFES WAS REQUIRED AND WRITTEN TO A/F ENGINEERING TO CREATE AN MSI FOR NDT INSP NO LATER THAN NEXT C-CHECK. 2L73 4F4 FRTA3WE E2EA 20050707000512005070700051EA 2005 7 7 COMA0560365 120050628A3397 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE EMERGENCY LIGHT DIRTY A COMAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01495CA 7774 AFT EMERGENCY FLOOR LIGHTS ARE INOPERATIVE. CLEANED WIRE CONNECTION. 2L72 4F4 FRTA21EA E15NE 20050707000542005070700054SO 2005 7 7 XGN2005F00008 220050614A85301119419 CYLINDER BEECH 36 36BEECH 1151602CE CONT O520 IO520BA 17032SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW051194A497 E159 THIS CYLINDER WAS IN THE NR2 POSITION AND IS A TYPE (A) HEAD. THIS CRACKED CYLINDER HEAD WAS FOUND AT THE 100 HOUR INSPECTION. WE ARE FINDING SIGNS OF AIR LEAKAGE ON THE EXHAUST SIDE OF THE CYLINDER HEAD WHEN DOING A COMPRESSION CHECK. WE ARE SPRAYING SOAPY WATER ON THE CYLINDER HEAD. 1L71 3O3 O 3A15 E5CE 20050707000572005070700057NM 2005 7 7 MASA200500498 120050628A3350 LIGHT DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE CABIN UNSECURE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07989HA 427 EMERGENCY FLOOR TRACK LIGHTING STRIP UNSECURED. MAINTENANCE RESECURED STRIP. 2H72 4T4 TRTA13NM E20NE 20050707000622005070700062NM 2005 7 7 05FDEA01775 120050701A5310601023418 TEE FITTING BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25272FE 22037 TEE FITTING APPROX STA 760-787 RBL 45 IS CORRODED. REMOVED AND REPLACED TEE FITTING IAW SRM 51-30-2 2L73 4F RTA3WE 20050707000642005070700064EU 2005 7 7 05FDEA01777 120050702A29133508806 PUMP AIRBUS300 A300B4605R 3930308EU NR 1 GREEN HYD FAILED A FDEAO OTHER J WARNING INDICATION DEDESCENT 1 SO25678FE1182 792 NR 1 GREEN HYD PUMP FAILED. LOST ALL GREEN HYDRAULIC FLUID. R & R NR 1 ENGINE GREEN SYSTEM EDP PER MM 29-11-32-4-02, ALSO REPLACED NR 1 ENGINE CASE DRAIN FILTER PER MM 29-11-36-4-02, ACP DRY MOTOR AND LEAK CHECKED REF JRH 5-37. CHECKED GOOD. ALSO CHECKED NR 2 ENGINE EDP GREEN SYSTEM CASE DRAIN FILER INDICATOR CHECKED NORMAL. RAN BOTH ENGINES REF JRH 5-9, CYCLED ALL FLT CONTROLS AND CYCLED FLAPS AND GEAR HANDLE, SERVICED GREEN HYD SYSTEM TO TOP OF TOP HAT PER MM 12-12-29-0. 2L72 4F RTA35EU 20050707000672005070700067NM 2005 7 7 05FDEA01780 120050703A5313 LONGERON DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 CENTER CARGO BAY RT STA 1641 LONGERON SPLICE FITTING 44 , FOUND CORRODED AS MARKED. CENTER CARGO COMPARTMENT R/H STA 1641 LONGERON 44 SPLICE FITTING REMOVED AND REPLACED NEW SPLICE FITTING AS PER DRAWING AFA 7105 AND SRM 51-33-01 VOL II. MINOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050707000692005070700069NE 2005 7 7 05FDEA01767 220050630A7230 COMPRESSOR BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE NR 2 ENGINE STALLED A FDEAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SO25488FE 21491 ON TAKEOFF ROLL THROTTLES SMOOTHLY ADVANCED TO T/O PWR NR 2 ENGINE HAD AVERY PRONOUNCED COMPRESSOR STALL APPROX. 5-8 SEC. INTO TAKEOFF ROLL REJECTED T/O AND CLEARED RUNWAY. INSPECTED INLET AND EXHAUST NO DAMAGE NOTED. PERFORMED TAKEOFF POWER EPR TEST REF TO 727 JRH CHAP 4. ALL NR 2 ENGINE PARAMETERS NORMAL NO STALLS NOTED ON 2 RUN UPS. 2L73 4F4 FRTA3WE E2EA 20050707000702005070700070NM 2005 7 7 05FDEA01816 120050705A5320 STIFFENER DOUG MD11 MD11 3023602NM OVERWING EXIT CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 CABIN OVERWING EXTERIOR STIFFENER FOR UPPER AUX TANK FOUND CORRODED AT STA 1339 RBL 98 AS MARKED. REMOVED AS PER SRM 51-31-01 VOL.II AND NEW STIFFENER INSTALLED AS PER DRAWING APB 7242.NEW STIFFENER REWORKED PER DWG 7242. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. [CLOSED] 2L73 4F RTA22WE 20050707000742005070700074NM 2005 7 7 05FDEA01793 120050703A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25619FE 48770 REFERENCE EO 1-5510-7-5000 D1 PART 1, LT NR 36L BARREL NUT BORE CORROSION EXCEEDED TO LIMIT. REPAIRED AS PER FEDEX EA 1-5510-83027. 2L73 4F RTA22WE 20050707000762005070700076NM 2005 7 7 05FDEA01795 120050704A5753ARC40041 HINGE FITTING DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 DURING ACCOMPLISHEMENT OF EA 1-5750-87541, LT WING OUTBOARD FLAP INBOARD HINGE FITTING (FLAP SIDE) INBOARD FORWARD BOLT HOLE FOUND CORRODED. LT WING OUTBOARD FLAP ASSY R & R PER AMM 27-50-30-4. 2L73 4F RTA22WE 20050707000772005070700077NM 2005 7 7 05FDEA01796 120050704A5280ARC28271 DOOR DOUG MD11 MD11 3023602NM ZONE 700 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 REFER TO EA 1-5280-57095, LT MLG FLIPPER DOOR ASSY, EXISTING CRACK HAS PROPAGATED PAST STOP-DRILL HOLE. LT MLG FLIPPER DOOR ASSY R & R PER AMM 32-14-10-4. ADJUSTMENT AND TEST OF THE LT FLIPPER DOOR CARRIED OUT PER AMM 32-31-700-803. 2L73 4F RTA22WE 20050707000782005070700078NM 2005 7 7 05FDEA01797 120050704A5753 SUPPORT DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LT WING OUTBOARD FLAP INBOARD HINGE SUPPORT FOUND COROSSION EXCEEDED LIMITS. LT WING OUTBOARD FLAP ASSY R & R PER AMM 27-50-30-4. REMOVED AND REPLACED PER AMM 27-50-30-4. (CLOSED) 2L73 4F RTA22WE 20050707000792005070700079EU 2005 7 7 05FDEA01802 120050705A5753 FITTING AIRBUS330 A300* EU LT WING TE FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25718FD 365 LT WING INBOARD FLAP OUTBOARD LEADING EDGE MOUNT FITTING CRACKED. (OPEN) 2L72 4F RTA26NM 20050707000802005070700080NM 2005 7 7 05FDEA01808 120050705A5532 SKIN DOUG MD11 MD11 3023602NM VERTICAL STAB CANNING A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 VERTICAL STABILIZER HAS OIL CANNING ON SKIN JUST ABOVE 373BL. REPAIR DOUBLER INSTALLED IAW SRM 51-35-01. [CLOSED] 2L73 4F RTA22WE 20050707000812005070700081NM 2005 7 7 05FDEA01809 120050705A5532 SKIN DOUG MD11 MD11 3023602NM VERTICAL STAB CANNING A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 VERTICAL STABILIZER HAS OIL CANNING ON SKIN JUST ABOVE 373BR. RIGHT I/B FLAP UPPER SKIN BETWEEN 140.6 TO 147.3, 03 EACH EXISTING DENTS SMOOTHENED OUT AND REPROTECTED AS PER SRM 51-21-01 VOL II, DEEPEST DENT IS 0.025", DIAMETER: 1/2" FOUND WITHIN LIMIT AS PER SRM 51-80-01 PAGE 1 ITEM 2E VOL II. MINOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050707000822005070700082NM 2005 7 7 05FDEA01810 120050705A5313 LONGERON DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 CENTER CARGO BAY, RT STA 1641 AFT LONGERON 44 FOUND WITH CORROSION AS MARKED. FABRICATED AS PER DWG AFA7127 AND SPICED REPAIR AS PER SRM 53-10-00 VOL1 FIG1. [CLOSED] 2L73 4F RTA22WE 20050707000832005070700083NM 2005 7 7 05FDEA01811 120050705A5340 SUPPORT DOUG MD11 MD11 3023602NM LAVATORY MOUNT CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 CABIN AT STA 1834 LBL 36.25 LAVATORY MOUNTING SUPPORT STRUCTURE AT TOP FOUND CORRODED. (OPEN) 2L73 4F RTA22WE 20050707000842005070700084NM 2005 7 7 05FDEA01812 120050705A5340 SEAT TRACK DOUG MD11 MD11 3023602NM FUSLEAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 STA 912 RBL 8.5 SEAT TRACK BASE FOUND CORRODED. (OPEN) 2L73 4F RTA22WE 20050707000862005070700086NM 2005 7 7 05FDEA01814 120050705A5320 STIFFENER DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 OVERWING STIFFENER FOR UPPER AUX TANK FOUND CORRODED AT STA 1352 RBL 98 AS MARKED. REMOVED AS PER SRM 51-31-01 VOL.II AND NEW STIFFENER REPLACED PER DWG APB7242. NEW STIFFENER REWORKED PER DWG APB7242. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. [CLOSED] 2L73 4F RTA22WE 20050707000872005070700087NM 2005 7 7 05FDEA01815 120050705A5320 STIFFENER DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 OVERWING EXTERIOR STIFFENER FOR UPPER AUX TANK FOUND CORRODED AT STA 1332 RBL 98 AS MARKED. CORRODED STIFFENER REMOVED AND REPLACED AS PER SRM 51-31-01 VOL.II. 2L73 4F RTA22WE 20050707000882005070700088NM 2005 7 7 05FDEA01774 120050701A5347602351124 SEAT TRACK BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25272FE 22037 SEAT TRACK STA 740-760 LBL 24 IS CORRODED. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-1. 2L73 4F RTA3WE 20050707000902005070700090NM 2005 7 7 05FDEA01790 120050703A2520 FLOOR SUPPORT DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 STA 1909 TO STA 2007 LBL 60 ALONG FLOOR SUPPORT STRUCTURE FOUND CORRODED. FLOOR SUPPORT REWORKED IAW DWG AGA7496 AND INSTALLED IAW SRM 51-31-01. 2L73 4F RTA22WE 20050707000912005070700091NM 2005 7 7 05FDEA01787 120050703A5320 FLOOR SUPPORT DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 BELOW FLOOR PANEL 271CF AT STA 1381 LBL 36.5 FLOOR SUPPORT STRUCTURE FOUND CRACKED. REMOVED AS PER SRM 51-31-01 VOL II. NEW FLOOR SUPPORT REWORKED FROM S2932222T12000 AS PER DRAWING ACA 3762 AND INSTALLED AS PER SRM 51-31-01 VOL II. CLASSIFIED MINOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050707000932005070700093NM 2005 7 7 05FDEA01784 120050703A5320 SPLICE DOUG MD11 MD11 3023602NM LONGERON CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 CENTER CARGO BAY RT STA 1531 LONGERON SPLICE 44 FOUND WITH A HAIR LINE CRACK AS MARKED. REMOVED AND REPLACED LONGERON SPLICE FITTING AS PER SRM 51-33-01. [CLOSED] 2L73 4F RTA22WE 20050707000942005070700094NM 2005 7 7 05FDEA01785 120050703A5320 SPLICE DOUG MD11 MD11 3023602NM LONGERON CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 STA 6-90 TO 1139 LONGERON SPLICE FOUND CRACKED AT L-12 RT AS MARKED. SPLICE FABRICATED AS PER DWG AFA7112 AND INSTALLED AS PER SRM 51-33-01 VOL2. [CLOSED] 2L73 4F RTA22WE 20050707000962005070700096NM 2005 7 7 05FDEA01782 120050703A5313 LONGERON DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 CENTER CARGO BAY, RT STA 1531 LONGERON 44 FOUND WITH HAIR LINE CRACK AS MARKED. LONGERON REMOVED IAW SRM 51-33-01. NEW LONGERON FABRICATED IAW DWG AGA 7028 & NEW LONGERON & SPLICE REPAIR INSTALLED IAW SRM 52-10-00. [CLOSED] 2L73 4F RTA22WE 20050707000972005070700097NM 2005 7 7 05FDEA01783 120050703A5313 LONGERON DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 CENTER CARGO BAY, RT STA 1531 LONGERON 45 FOUND WITH HAIR LINE CRACK AS MARKED. LONGERON REMOVED IAW SRM 51-32-01. NEW LONGERON AND SPLICE REPAIR INSTALLED IAW SRM 53-10-01. [CLOSED] 2L73 4F RTA22WE 20050707001042005070700104NM 2005 7 7 AWXA200500779 120050606A5711113N22523 SPAR BOEING757 7572S7 1384962NM ZONE 500 DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28905AW 23567 DURING C-10 CHECK FOUND TWO ELONGATED HOLES ON BRACKET, FORWARD FLAP SPAR AND FLAP SKIN LOCATED ON THE LT WING INBOARD MAIN FLAP, FORWARD OF LOWER SPAR AND SKIN. MAINTENANCE REMOVED DAMAGE FROM ELONGATED HOLES ON BRACKET, FORWARD FLAP SPAR AND FLAP SKIN LOCATED ON THE LT WING INBOARD MAIN FLAP, FORWARD OF LOWER SPAR AND SKIN IAW AWA ER 19-5753-05175-ES1. FABRICATED FREEZE PLUGS AND REPAIR DOUBLERS IAW AWA ER 19-5753-05175-ES1. INSTALLED FABRICATED REPAIR PARTS IAW BOEING 757 SRM 51-20-07, SOPM 20-10-03 AND AWA ER 19-5753-05175-ES1. 2L72 4F RTA2NM 20050707001052005070700105EU 2005 7 7 AWXA200500780 120050704A3230 MODULE AIRBUS320 A320231 3930325EU LANDING GEAR FAILED A AWXAO OTHER J WARNING INDICATION CLCLIMB 1 WP28644AW 317 AFTER TAKEOFF, TRIED TO RAISE MLG, GEAR UNLOCKED ILLUMINATED FOR NLG. CYCLED GEAR PER ECAM, GEAR CAME UP & LOCKED. LANDED IN SEA WITHOUT FURTHER INCIDENT. A/C FERRIED BACK TO PHX. MX R & R MLG CONTROL MODULE IAW AIRBUS MM 32-30-00. TEAR DOWN REPORT CONFIRMS FAILURE. DURING PRE-TEST "DOWN-UP SWITCHING BY S1" TEST FAILED. SEVERAL CONTACTS OVER VOLTAGE DROPS STATED IN CMM. UNIT REPAIRED & RETESTED IAW CMM 32-31-13. OPS TESTS GOOD. 2L72 4F RTA28NM 20050707001062005070700106EU 2005 7 7 WRNA200500017 120050625A3213C23005303 DAMPENER AIRBUS300 A300B4203 3930306EU MLG LEAKING A WRNAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO05821SC 6261 211 AIRCRAFT TOOK OFF, MLG WOULD NOT RETRACT. RETURNED TO BASE. LANDING NORMAL. FOUND LT PITCH DAMPNER LEAKING FLUID. REMOVED AND REPLACED PITCH DAMPNER IAW 32-11-05. FUNCTIONAL CHECK SATISFACTORY, AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA35EU 20050707001072005070700107WP 2005 7 7 0500979759 120050705A2170V1211 COALESCER BAG DOUG DC9 DC941 302207NWP CABIN AIR CONTAMINATED A NWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL01759NW 47287 SMOKE WAS REPORTED COMING OUT OF UPPER CABIN SIDEWALL DURING CLIMBOUT. THE AIRCRAFT RETURNED TO AN UNEVENTFUL LANDING BACK AT OMA. NO FIRE EXTINGUISHER ACTIVATED BUT ONE FLIGHT ATTENDANT DONNED PROTECTIVE BREATHING EQUIPMENT. CONTRACT MAINTENANCE AT OMA DISCOVERED THE RIGHT COALESCER BAG OUT OF POSITION BUT NO OTHER DISCREPANCIES FOUND. INSPECTED THE AIRCRAFT FOR SIGNS OF FLUID/OIL LEAKS, WIRE PROBLEMS, LIGHT FAULTS, HEAT OR SMOKE SOURCE; BUT NO TROUBLE WAS FOUND. SUSPECT VISIBLE CONDENSATION DUE TO COALESCER BAG BEING OUT OF POSITION. THE AIRCRAFT HAS RETURNED TO SERVICE. 2L72 4F A6WE 20050707001082005070700108WP 2005 7 7 AALA20050617 120050629A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2170524 49916 DTW - AFT CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR AFT CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050707001112005070700111WP 2005 7 7 AALA20050410 120050624A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHTSSTRIPPED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21561AA 53091 BOS - EMERGENCY SEAT MOUNTED PATH LIGHT AT 4EF INOPERATIVE. FOUND WIRE PLUG STRIPPED. SPLICED AND REPAIRED EMERGENCY SEAT MOUNTED PATH LIGHT AT 4EF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050707001212005070700121GL 2005 7 7 CHQA200500125 220050627A7200 ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 2 SMOKE A CHQAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL11568RP101384042 145800 CAE311855 ONE MINUTE AFTER TAKEOFF, F/A REPORTED LAV SMOKE ALARM ACTIVATED, SMOKE PRESENT IN REAR OF CABIN. EMERGENCY DECLARED & VECTORED BACK FOR VISUAL INTO CMH. RAN QRH FOR LAV SMOKE AND FOLLOWED PROCEDURE. THE AIRCRAFT WAS CONFIGURED FOR AN OVERWEIGHT LANDING AND STARTED VISUAL APPROACH TO RUNWAY 28R. THE LAV SMOKE EICAS MESSAGE EXTINGUISHED AFTER POWER REDUCTION FOR LANDING. A NORMAL LANDING ACCOMPLISHED. TAXIED BACK TO THE GATE TO DEPLANE PASSENGERS. AFTER DEPLANING PASSENGERS, FIRE RESCUE BOARDED AIRCRAFT AND DID NOT DETECT ANY SIGN OF HEAT OR FIRE ON THE AIRCRAFT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE IAW CHQ J/C CE72-00-01. OPS CHECK AND LEAK CHECK GOOD. NO SMELL OR EICAS MESSAGES PRESENT. 2L72 4T4 FRTT00011ATTE6CH 20050708000022005070800002NM 2005 7 8 SWAA051884 120050628A5310573149 WINDOW POST BOEING737 7373H4 1384600NM L1 COCKPIT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29332SW 23696 DURING SCHEDULED 1/4D CHECK, FOUND L1 COCKPIT WINDOW POST CRACKED AT UPPER OUTBOARD CORNER. REPAIRED POST PER SRM. 2L72 4F RTA16WE 20050708000042005070800004NM 2005 7 8 SWAA051886 120050628A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN FLOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29458WN 33857 EEPLS LOOSE AT ROW 1 ABC. REMOVED AND REPLACED EEPLS PER MM. 2L72 4F RTA16WE 20050708000062005070800006NM 2005 7 8 SWAA051897 120050629A534465557807 HINGE BOEING737 7373H4 1384600NM R2 DOOR BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 R2 DOOR UPPER HINGE LINK ASSY BROKEN. REMOVED AND REPLACED HINGE LINK ASSY PER MM. 2L72 4F RTA16WE 20050708000082005070800008NM 2005 7 8 SWAA051899 120050629A552365C2638425A TAB BOEING737 7373H4 1384600NM LT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29368SW 26579 DURING SCHEDULED C3 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB PER MM. 2L72 4F RTA16WE 20050708000092005070800009 2005 7 8 SWAA051900 420050629A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29368SW 26579 DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050708000112005070800011NM 2005 7 8 SWAA051902 120050629A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29443WN 29838 EEPLS COVER MISSING AT FWD END OF CABIN. INSTALLED EEPLS COVER PER MM. 2L72 4F RTA16WE 20050708000132005070800013NM 2005 7 8 WRNA200500018 120050703A291065B8324843 LINE BOEING747 7472U3B 1384846NM HYD SYSTEM UNSERVICEABLE A WRNAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO05922FT 22768 T/O FROM TPE, LANDING GEAR HANDLE WOULD NOT MOVE TO UP POSITION. AIRCRAFT RETURNED TO BASE, LANDING NORMAL. FOUND HYDRAULIC LINE TO TRUCK POSITION ACTUATOR LEAKING (BLOWN). REMOVED AND REPLACED LINE IAW 32-13-05, OP'S CHECK SATISFACTORY, NO LEAKS NOTED. A/C RETURNED TO SERVICE. 2L74 4F RTA20WE 20050708000152005070800015NM 2005 7 8 SWAA051888 120050627A53306518420 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29513SW 24190 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 259.5, STR 19L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050708000172005070800017NM 2005 7 8 SWAA051890 120050628A3350101114 COVER BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29639SW 27712 FWD ENTRY DOOR LOWER EMERGENCY LIGHT LENS COVER LOOSE. SECURED COVER PER MM. 2L72 4F RTA16WE 20050708000182005070800018NM 2005 7 8 SWAA051891 120050628A3350311500 LENS BOEING737 7373A4 1384585NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY BULLNOSE LIGHT LENS LOOSE. SECURED LENS PER MM. 2L72 4F RTA16WE 20050708000202005070800020NM 2005 7 8 SWAA051893 120050627A52306547952 SKIN BOEING737 7373T0 1384582NM AFT CARGO DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29684WN 23941 DURING SCHEDULED C4 CHECK, FOUND 2 EA AFT CARGO DOOR SKIN CRACKS AT SECOND ROW LIGHTENING HOLES. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050708000212005070800021NM 2005 7 8 SWAA051894 120050627A5240 GATE BOEING737 7373T0 1384582NM R2 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29684WN 1530 23941 DURING SCHEDULED C4 CHECK, FOUND R2 DOOR UPPER & LOWER GATES CRACKED AT FASTENER HOLES. REMOVED AND REPLACED R2 DOOR PER MM. 2L72 4F RTA16WE 20050708000252005070800025NM 2005 7 8 SWAA051919 120050702A53116546532 FRAME BOEING737 7373H4 1384600NM FWD CARGO BAY CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 460, LBL 18. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050708000262005070800026NM 2005 7 8 SWAA051920 120050702A53306545766 SKIN BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CORRODED BETWEEN BS 466 TO BS 470, LBL 1 TO RBL 1. REPAIRED SKIN PER SRM & BFG ER. 2L72 4F RTA16WE 20050708000272005070800027NM 2005 7 8 SWAA051921 120050704A53156545410 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29332SW 23696 DURING SCHEDULED 1/4D CHECK, FOUND CABIN LONGITUDINAL FLOORBEAM CRACKED AT BS 663, BL 0. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20050708000282005070800028NM 2005 7 8 SWAA051922 120050704A53226546529 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29332SW 23696 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500, BL 0. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050708000302005070800030NM 2005 7 8 SWAA051925 120050704A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29332SW 23696 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 25L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050708000312005070800031NE 2005 7 8 SWAA051909 220050702A7250305392503 GUIDE VANE BOEING737 7373H4 1384600NM GE CFM56 CFM563B1 13802NE NR 2 ENGINE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 722405 DURING SCHEDULED BOROSCOPE INSP, FOUND NR 2 ENGINE LPT NOZZLE GUIDE VANES CRACKED. REMOVED AND REPLACED NR 2 ENGINE PER MM. 2L72 4F4 FRTA16WE E2GL 20050708000332005070800033NM 2005 7 8 SWAA051911 120050702A53116552271 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED D-CHECK, FOUND LT CREASE BEAM WEB CRACKED AT BS 500C + 14. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM. 2L72 4F RTA16WE 20050708000352005070800035NM 2005 7 8 SWAA051905 120050630A53216545833 FLOOR SKIN BOEING737 7373H4 1384600NM COCKPIT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED D-CHECK, FOUND COCKPIT FLOOR SKIN CRACKED AT BS 244, RBL 15. REPAIRED FLOOR SKIN PER SRM. 2L72 4F RTA16WE 20050708000392005070800039NM 2005 7 8 SWAA051912 120050702A53116546525 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED D-CHECK, FOUND 2 CRACKS IN FRAME AT BS 380, STR 15R & STR 16R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050708000402005070800040NM 2005 7 8 SWAA051914 120050702A57126545445 RIB BOEING737 7373H4 1384600NM LT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED D-CHECK, FOUND LT WING LOWER RIB CRACKED AT WBL 135.5, BETWEEN STR 2 & STR 3. REPAIRED RIB PER BFG ER. 2L72 4F RTA16WE 20050708000412005070800041NM 2005 7 8 SWAA051916 120050702A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 344, STR 11R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050708000422005070800042NM 2005 7 8 SWAA051926 120050704A53106545409 WEB BOEING737 7373H4 1384600NM LT MLG WW CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29332SW 23696 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE BEADED WEB CRACKED AT BS 664, LBL 33. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050708000442005070800044 2005 7 8 SWAA051928 420050702A3417C17001BA01 ADC BOEING737 7377H4 1384404NM E/E BAY FAULTY A SWAAA UNSCHED LANDING G MULTIPLE FAILURE CRCRUISE 1 SW29428WN 29844 AIR TURNBACK. DUAL EEC LIGHTS ILLUMINATED FOLLOWED BY LOSS OF F/O MAP MODE, BOTH FMC'S, BOTH FLIGHT DIRECTORS & BOTH AUTO PILOTS. REMOVED AND REPLACED LT PITOT AIR DATA MODULE PER MM. 2L72 4F RTA16WE 20050708000462005070800046NM 2005 7 8 SWAA051930 120050701A53306545765 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29506SW 24183 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 10L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050708000472005070800047NM 2005 7 8 SWAA051931 120050701A53306545775 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29506SW 24183 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 770, STR 18L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050708000502005070800050NE 2005 7 8 SWAA051934 220050703A73209368M57P21 MEC BOEING737 7373H4 1384600NM GE CFM56 CFM563B1 13802NE NR 1 ENGINE FAULTY A SWAAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SW29605SW 27956 727291 INFLIGHT SHUTDOWN/DIVERSION. NR 1 ENGINE FAILED FOR 5 SECONDS, THEN SURGED & RE-STARTED ITSELF. REMOVED AND REPLACED NR 1 ENGINE FUEL SHUT-OFF VALVE, NR 1 ENGINE FUEL PUMP & NR 1 ENGINE MEC PER MM. 2L72 4F4 FRTA16WE E2GL 20050708000512005070800051NE 2005 7 8 SWAA051935 220050702A7200 ENGINE BOEING737 7373H4 1384600NM GE CFM56 CFM563B1 13802NE NR 2 OVERTEMP A SWAAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SW29646SW 28331 857927 DIVERSION, NR 2 ENGINE OVERTEMP AT 500 FT AGL, 970 DEGREES INDICATED WITH RED LIGHT ILLUMINATED. REMOVED AND REPLACED NR 2 ENGINE PER MM. 2L72 4F4 FRTA16WE E2GL 20050708000532005070800053NM 2005 7 8 SWAA051937 120050701A3397 WIRE BOEING737 737317 138447PNM EXIT SIGN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29686SW 23175 DURING SCHEDULED SPECIAL VISIT, FOUND AFT CABIN CENTER EMERGENCY EXIT SIGN WIRES BROKEN. REPAIRED WIRES PER SWPM & SOPM. 2L72 4F RTA16WE 20050708000562005070800056NM 2005 7 8 SWAA051940 120050630A2720BACC63 CONNECTOR BOEING737 7377H4 1384404NM E/E BAY FAULTY A SWAAA UNSCHED LANDING F FLT CONT AFFECTED NRNOT REPORTED 1 SW29700GS 27835 DIVERSION/DECLARED EMERGENCY. RUDDER TRIM FAILED. REMOVED AND REPLACED RUDDER TRIM ACTUATOR CONNECTOR PER MM. 2L72 4F RTA16WE 20050708000592005070800059NM 2005 7 8 ASAA0540256 120050519A5210507945178 GUIDE ARM BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU L1 DOOR OUT OF ADJUST A ASAAK NONE O OTHER TXTAXI/GRND HDL 1 NM02709AS 28896 L1 DOOR WAS REPORTED DIFFICULT TO CLOSE THROUGH LAST 4 INCHES OF TRAVEL. ADJUSTED GUIDE ARM. (K) 2L72 4F4 FRTA16WE E21EU 20050708000602005070800060NM 2005 7 8 ASAA0540276 120050528A5754 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU NR 4 SLAT CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02776AS 25109 NR 4 SLAT IB T/E CHAFED. REMOVED DAMAGE, FABRICATED FILLER SKIN AND DOUBLER AND INSTALLED REPAIR IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050708000612005070800061NM 2005 7 8 ASAA0540278 120050606A57536546430129 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU LTWING TE FLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02776AS 25109 DENT FOUND AT LT WING IB T/E FORE FLAP. REPAIRED LT WING IB T/E FORE FLAP IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050708000622005070800062NM 2005 7 8 ASAA0540279 120050610A5347655384422 CARGO TRACK BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02703AS 28893 CORROSION ON CARGO TRACK TIE DOWN AT STA 947, RBL 13, WL 179. REMOVED AND REPLACED. (K) 2L72 4F4 FRTA16WE E21EU 20050708000632005070800063NM 2005 7 8 ASAA0540282 120050613A532265465542 SHEAR TIE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSLEAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 B-STA 847 FRAME SHEAR TIE IS CORRODED BETWEEN STRINGER 27L AND 27R. REMOVED CORROSION, FABRICATED REPAIR SHEAR TIE AND FLOOR SUPPORT CLIP, AND INSTALLED REPAIR PARTS IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050708000642005070800064NM 2005 7 8 ASAA0540283 120050613A533065566552 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 AFT CARGO DOOR FWD INNER SURROUND SKIN IS CORRODED BETWEEN STRINGER 23R AND 26R, FS 793. REMOVED CORRODED SKIN, FABRICATED AND INSTALLED IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050708000652005070800065NM 2005 7 8 ASAA0540292 120050614A53206552878122 SILL BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02792AS 28887 CORROSION AT R-2 DOOR MOP SILL. REMOVED AND REPLACED MOP SILL. (K) 2L72 4F4 FRTA16WE E21EU 20050708000662005070800066NM 2005 7 8 ASAA0540253 120050518A5311654655514 FRAME BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02792AS 28887 FRAME CRACKED AT HAT RACK ATTACH POINT. REPAIRED CRACKED FRAME AT HAT RACK ATTACH POINT. (K) 2L72 4F4 FRTA16WE E21EU 20050708000672005070800067NM 2005 7 8 ASAA0540262 120050525A532269730577 SHEAR TIE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSLEAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02776AS 25109 SHEAR TIE CRACKED AND CORRODED AT STR 28L B-STA 500G. FABRICATED SHEAR TIE, REMOVED AND REPLACED SHEAR TIE IAW SRM AND MFG DWG. (K) 2L72 4F4 FRTA16WE E21EU 20050708000682005070800068NM 2005 7 8 ASAA0540263 120050525A531069771851 SHEAR WEB BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU SEAT ROW 8 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02776AS 25109 LT SHEAR WEB IS CORRODED AT SEAT ROW 8. REMOVED DAMAGED AREA AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050708000692005070800069NM 2005 7 8 ASAA0540257 120050519A521069203214 GUIDE ARM BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU R1 DOOR OUT OF ADJUST A ASAAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM02709AS 28896 R1 DOOR WAS REPORTED DIFFICULT TO CLOSE THROUGH LAST 4 INCHES OF TRAVEL. ADJUSTED GUIDE ARM. (K) 2L72 4F4 FRTA16WE E21EU 20050708000712005070800071NM 2005 7 8 ASAA0540255 120050518A531165C323949 FRAME BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02792AS 28887 VERTICAL ANGLE CRACKED AT B-STA 601, RBL 64, WI 204, AND B-STA 601 FRAME. CUT OUT DAMAGED SECTION OF 601 FRAME AND FABRICATED REPAIR ANGLE IAW EA 5330-01934, ER 05-2867. (K) 2L72 4F4 FRTA16WE E21EU 20050708000722005070800072NM 2005 7 8 ASAA0540258 120050523A5347BAC152792 SEAT TRACK BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FUSLEAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02705AS 29318 LT OB SEAT TRACK HAS MULTIPLE GOUGES AT BS 500C. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-00-52. (K) 2L72 4F4 FRTA16WE E21EU 20050708000732005070800073NM 2005 7 8 ASAA0540259 120050523A5347BAC152792 SEAT TRACK BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02705AS 29318 PREVIOUS BLEND-OUT AT PAX CABIN SEAT TRACK, BS 500+12 INCHES, LBL 25, WL 208 OUT OF LIMITS. CUTOUT DAMAGE AND REPAIRED IAW SRM 53-00-52. (K) 2L72 4F4 FRTA16WE E21EU 20050708000752005070800075NM 2005 7 8 ASAA0540268 120050526A5753 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FORE FLAP DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02776AS 2342 25109 LT WING OB FORE FLAP DELAMINATED AT IB END. REMOVED DAMAGED AREA OF LT OB FORE FLAP IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050708000812005070800081NM 2005 7 8 ASAA0540260 120050521A521065495831 STOP FITTING BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU R1 DOOR CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02799AS 29270 R-1 DOOR STOP FITTING CRACKED. REMOVED AND REPLACED DOOR. (K) 2L72 4F4 FRTA16WE E21EU 20050708000822005070800082NM 2005 7 8 ASAA0540269 120050525A532269730577 SHEAR TIE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSLAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02776AS 25109 SHEAR TIE CRACKED AND CORRODED AT STR 28L B-STA 500G. FABRICATED SHEAR TIE, REMOVED AND REPLACED SHEAR TIE IAW SRM AND MFG DWG. (K) 2L72 4F4 FRTA16WE E21EU 20050708000842005070800084NM 2005 7 8 ASAA0540251 120050518A55406552490118 BEAM BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU RUDDER CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02792AS 28887 RT VERTICL T/E BEAM AT RUDDER STA 13.33 CRACKED. REMOVED, FABRICATED AND INSTALLED VERTICAL RT T/E BEAM. (K) 2L72 4F4 FRTA16WE E21EU 20050708000862005070800086NM 2005 7 8 ASAA0540290 120050613A575465C26602311 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU NR 2 SLAT DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 NR 2 SLAT OB T/E DELAMINATED AT CORNER. REMOVED DAMAGE, FABRICATED SKIN AND DOUBLER AND INSTALLED REPAIR PIECES IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050708000902005070800090NM 2005 7 8 ASAA0540272 120050529A534069773081 ATTACH FITTING BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02792AS 28887 CORRODION LAV ATTACH FITTING. REMOVED AND REPLACED. (K) 2L72 4F4 FRTA16WE E21EU 20050708000912005070800091NM 2005 7 8 ASAA0540274 120050529A534065B5783930 SUPPORT FITTING BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02792AS 28887 CORROSION ON FWD LAV SUPPORT FITTING. REMOVED AND REPLACED FWD LAV SUPPORT FITTING. (K) 2L72 4F4 FRTA16WE E21EU 20050708000922005070800092NM 2005 7 8 ASAA0540284 120050613A57536546435282 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU TE FLAP DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 RT OB AFT FLAP DELAMINATED AT IB AFT CORNER. REPAIRED IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050706001272005070600127WP 2005 7 6 05FDEA01760 120050701A5730 SKIN DOUG DC10 DC1010 3022110WP RT WING DELAMINATED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25571FE 47830 DURING CONVERSION FOUND ON RT WING, LE UPPER SIDE, STA XW 346, WITH DELAMINATION. REPAIRED IAW SRM 57-00-01 FIG 4, SH 2. (OPEN) 2L73 4F A22WE 20050706001472005070600147CE 2005 7 6 DXTA200500786 120050619A3210 LANDING GEAR CESSNA750 750 2076810CE MALFUNCTIONED E DXTAO OTHER O OTHER DEDESCENT 1 GL07933QS 7500133 LANDING GEAR BUMP THROUGH 15,000 FT, NO UNLOCK LIGHT INDICATED. COULD NOT DUPLICATE PROBLEM ON GROUND. CARRIED OUT T/S. MADE ADJUSTMENTS TO R/S CLEAR UPLOCK SWITCH. MLG SYSTEM OPS CHECK GOOD. COMPLIED WITH GEAR BUMP TROUBLESHOOTING IAW CE 750 MM. INSTRUCTED TO DO A COMPLETE CHECK FROM TOP OF T/S LIST. CARRIED OUT VISUAL CHECKS TO CABLES, HOOKS FOR THE EMER SYS COMPARED TENSIONS TO THAT OF OTHER CE-750 ON SITE. RANG UPLOCK SWITCHES FOR OPS & GROUND TO A/C GOOD. CHECK ADJUSTMENTS TO UPLOCK SWITCHES VIA O-RING CHECK HAD TO ASDJUST RT SWITCH. CARRIED OUT MANIFOLD BLEED RATE CHECK & BLED TO LESS THAN 1500 PSI IN LESS THAN 1/2 MIN. DURING T/S SWUNG GEAR SEVERAL TIMES & COULD NOT DUPLICATE BUMP. MLG OPS CHECK GOOD. 2L72 4J RTT00007WI 20050706001492005070600149CE 2005 7 6 DXTA200500784 120050618A27107011702929 CONTROLLER CESSNA750 750 2076810CE AILERONS MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL07949QS303 7500049 FLIGHT CONTROL FAULT CAS AND AILERON CONTROL LIGHT FLASHING. INSTALLED DMU . FOUND FORCE FIGHT BETWEEN PCU'S. ALL 4 TRANSDUCERS FUNCTION NORMALLY, ADJUSTED PCU'S. OPS CHECK NORMAL. WORK IAW CESSNA 750 MM CHAPT 27-10-01 2L72 4J RTT00007WI 20050706001532005070600153NM 2005 7 6 DHL2005741580 120050429A5542 SKIN BOEING727 7272Q9 138448MNM RUDDER DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 UPPER RUDDER T/E DENTED 2 IN. ABOVE NR 1 HINGE TAB 4H SIDE MARKED. CUT-OUT DAMAGED AREA 2EA PLACES DIM .75 BY .75 AND .5 BY .5 AT UPPER RUDDER LT L/E IAW B727 SRM 51-40-2 FIG 1. FABRICATED REPAIR FROM 2024T3 .032 PO9001634 DIM 10 BY 5.5 IN IAW B727 SRM 55-40-2 FIG 2 AND SRM 51-40-2 FIG 1. TREATED AND PRIMED REPAIR PART AND AREA IAW B727 SRM 51-10-2. INSTALLED REPAIR IAW B727 SRM 51-40-2 FIG 1. 2L73 4F RTA3WE 20050706001702005070600170WP 2005 7 6 IXXA05SMN16S 120050429A5340 FITTING DOUG DC8 DC871F 302199DWP FWD CARGO BAY CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX834963359 45993 DURING ROUTINE C-CHECK INSPECTION, FWD CARGO BAY FITTING CRACKED 1 IN., STA 240.000. L-31R. REMOVED CRACKED FITTING IAW DC-8 SRM 53-1-0 PAGE 1. CLEANED, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8B. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D PAGE 9. TORQUED IAW DC-8 RM 51-3-1. 2L74 4F RT4A25 20050706001722005070600172WP 2005 7 6 IXXA05SMN36S 120050429A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX834963359 45993 EXT FS RT FUSELAGE FWD CTR SECTION PLATING CORRODED AND HOLES ELONGATED, STA 260.000 L-3. MAJOR REPAIR IAW FAA 8110-3 NR 05168 AND SEMAN DWG ED-3951. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FOUND OUT OF LIMITS IAW DC-8 SRM 53-2-0. REMOVED EXISTING DOUBLER DC-8 SRM 51-1-21 AND DC-8 SRM 51-1-20D. REMOVED DAMAGED AREA IAW SEMAN DWG ED-3951. PERFORMED NDT INSP IAW DC-8 NDT SPM PART 06-10-01-001. FAB NEW SEGMENT OF SKIN, EXTERNAL SPLICE DOUBLER , INTERNAL FINGER DOUBLERS , FINGER DOUBLER , FILLER , INTERNAL DOUBLER S, AND STRAPS IAW SEMAN DWG ED-3951. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11 PAGE 9. 2L74 4F RT4A25 20050706001742005070600174NM 2005 7 6 DHL2005741582 120050429A5542 SKIN BOEING727 7272Q9 138448MNM RUDDER DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 UPPER RUDDER T/E DENTED AT NR 6 TAB HINGE LT SIDE MARKED. CUT OUT DAMAGED AREA IAW B727 SRM 51-40-2 FIG 1. FABRICATED DOUBLER REPAIR IAW B727 SRM 55-40-2 FIG 2 AND SRM 51-40-2 FIG 1. TREATED AND PRIMED PART AND AREA IAW B727 SRM 51-10-2. INSTALLED REPAIR IAW B727 SRM 51-40-2 FIG 1. 2L73 4F RTA3WE 20050706001792005070600179EU 2005 7 6 MALA050497 120050622A2913521449 PUMP BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE NR 2 MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15524XJ E2349 DURING CLIMB-OUT, YELLOW HYDRAULIC SYSTEM HIGH TEMP LIGHT ILLUMINATED. FOLLOWED QRH AND LIGHT EXTINGUISHED. RETURNED TO MEM. REMOVED AND REPLACED NR 2 EDP. 2H74 4F4 FRTA49EU E6NE 20050706001822005070600182EU 2005 7 6 MALA050491 120050620A53207253711245 PLATE SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15421XJ 340B421 DURING 4K INSPECTION, FOUND LT WRAP AROUND CORRODED AND HAS BEEN REMOVED AND REPLACED IAW SRM 51-40-21. 2L72 4T RTA52EU 20050706001832005070600183EU 2005 7 6 MALA050492 120050620A52607253710871 RAIL SAAB SF340 340B 7860101EU PAX STAIR CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15421XJ 340B421 DURING 4K INSPECTION, FOUND PAX STAIR SLIDE RAIL ASSY CORRODED AND HAS BEEN REPLACED IAW SRM 51-40-21/22. 2L72 4T RTA52EU 20050706002272005070600227NM 2005 7 6 AWXA200500732 120050609A53206545834300 SUPPORT BOEING737 7373B7 1384580NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28328AW 23377 DURING C-13 CHECK, FOUND CORROSION ON INTERCOSTAL SUPPORT AT STATION 297, WL 208, BL 31R. CORROSION OUT OF LIMITS IAW BOEING 737-300 SRM 53-10-51-1 FIG 101. REMOVED CORRODED INTERCOSTAL SUPPORT AT STATION 297, WL 208, BL 31R AND FABRICATED NEW INTERCOSTAL SUPPORT IAW BOEING 737-300 SRM 51-40-05 FIG 2-4, BOEING 737-300 SRM 51-40-02 FIG 8 AND BOEING DWG 65-45834. INSTALLED FABRICATED REPAIR PARTS AT STATION 297, WL 208, BL 31R IAW BOEING 737-300 SRM 51-40-02-0 FIG 4. 2L72 4F RTA16WE 20050706002292005070600229WP 2005 7 6 IXXA0500079O 120050621A2910 CONNECTOR DOUG DC8 DC862F 3021972WP HYD SYS LOOSE A IXXAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW1171CX 668433400 45961 DURING CRUISE, ACFT STARTING LOSING HYDRAULIC FLUID. CREW ACCOMPLISHED EMERGENCY PROCEDURES AND RETURNED ACFT. LANDED WITHOUT INCIDENT. MX FOUND LOOSE HYDRAULIC CONNECTOR RT SIDE OF NR 2 ENGINE. SECURED LINE. OPS CHECK GOOD PER ALL APPLICABLE MANUALS. ACFT RETURNED TO SERVICE. 2L74 4F 4A25 20050706002312005070600231NM 2005 7 6 DHL2005741590 120050504A5320 INTERCOSTAL BOEING727 7272Q9 138448MNM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 MAIN CABIN BS 344 BELOW STR 7R HAS CRACKED INTERCOSTAL. REMOVED INTERCOSTAL. FABBED NEW 7075T6 .040 PO9002219 18" BY 5" IAW B727 SRM 53-10-2 FIG 1. TREATED AND PRIMED PART IAW B727 SRM 51-10-2. INSTALLED PART IAW B727 SRM 51-30-2. 2L73 4F RTA3WE 20050706002342005070600234EA 2005 7 6 COMA0560356 120050616A2913887055 PUMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE NR 2 HYD SYS FAULTY A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01797CA15403 7344 RECEIVED HYDRAULIC NR 2 LOW PRESSURE CAUTION MESSAGE. CREW DECLARED AN EMERGENCY AND DIVERTED TO IAD. ACFT LANDED WITHOUT INCIDENT. REPLACED RT ENGINE HYDRAULIC. 2L72 4F4 FRTA21EA E15NE 20050707000112005070700011NE 2005 7 7 AWXA200500772 220050703A7320FMU550MK1 FMU AIRBUS320 A320232 3930326EU IAE V2524 V2524A5 NE NR 1 ENG FAILED A AWXAC ABORTED TAKEOFF GJ MULTIPLE FAILURE WARNING INDICATION TOTAKEOFF 1 WP28650AW258855204 856 DURING TAKE OFF AFTER APPLYING POWER, RECEIVED MULTIPLE WARNINGS ALONG WITH NR 1 ENGINE OVERSPEED. ACFT ABORTED TAKEOFF AT APPROX 80 KNOTS. TAXIED BACK TO GATE WITHOUT FURTHER INCIDENT. MX TROUBLESHOT IAW MFG MANUAL. R & R NR 1 FMU IAW TASK CARD R5M73308. OPS CHKS GOOD. (OPEN) 2L72 4F4 FRTA28NM E40NE 20050707000152005070700015EU 2005 7 7 XN0A050629001 120050629A5610 WINDOW AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE COCKPIT LACK OF LUBE A XN0AK NONE W INADEQUATE Q C ININSP/MAINT 1 GL23474AS 219 CAPTAIN`S WINDOW LOCK PIN WILL NOT ENGAGE. LUBED AND CYCLED CAPTAIN`S WINDOW. OPS CK GOOD 56-12-00. (ORIG/CLOSED) 2L72 4F4 FRTA35EU E23EA 20050707000232005070700023NM 2005 7 7 DU4R0507130 120050630A5330 SKIN BOEING737 737 UTILSYSNM GE CFM56 CFM56* 13802NE FUSELAGE MISREPAIRED B DU4RK NONE W INADEQUATE Q C ININSP/MAINT 1 SO15387UA 24662 FUSELAGE LT SIDE BS 927-945.5 S-19L- 20L HAS PREVIOUS REPAIR THAT ENDS ON A LAP SEAM. 2L72 4F4 FRTA16WE E2GL 20050707000272005070700027 2005 7 7 MWEA050059 420050627A2312 TRANSCEIVER BOEING717 717200 1383700NM RROYCEBR700 BR700710A110 NE VHF COMMS INOPERATIVE A MWEAA UNSCHED LANDING G MULTIPLE FAILURE CLCLIMB 1 GL31908ME 55172 AFTER DEPARTURE LOST COMUNICATION ON NR 1 AND NR 2 COMM. REMOVED AND REPLACED NR 1 VHF TRANCEIVER. 2L72 4F4 FTRA6WE E00057EN 20050707000602005070700060NM 2005 7 7 05FDEA01759 120050701A7710LG80A6 TRANSMITTER BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE EPR MALFUNCTIONED A FDEAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO25465FE 21289 ON TAKEOFF WITH STANDARD EPR SET NR3 N1,N2 AND FUEL FLOW WERE LOW. AC RELEASED FOR SERVICE IAW MEL/CDL: 77-01-01 01JUL05 14:55 ORF REMOVED PT2 SENSOR FROM ENG, BLEW AIR THROUGH LINE TO INSURE NO OBSTRUCTIONS PRESENT. RE-INSTALLED SAME. DISCONNECTED NR3 ENG EPR PT2 LINE AT PRESSURE TRANSMITTER AND DID SAME. REMOVED AND REPLACED TRANSMITTER AND EPR IND FOR NR 3 ENG. RAN NR 1 AND NR 3 ENGS AT TAKEOFF EPR IAW JRH, ENGS OP CHECK GOOD IAW JRH CHAP 4,PG 4-8. ENT BY: 127651 2L73 4F4 FRTA3WE E2EA 20050707000982005070700098EU 2005 7 7 05FDEA01772 120050701A5270 WARNING LIGHT AIRBUS310 A310 EU CARGO DOOR FALSE INDICATIONA FDEAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO25433FE 335 FWD CARGO DOOR LIGHT CAME ON DURING TAKEOFF. RTO (LIGHT CAME ON & OFF.) AC RELEASED FOR SERVICE PER MEL/CDL: 52-71-01 11JUL05 DOOR CLOSED & LOCKED INDICATION ON ECAM DOOR PAGE - INOPERATIVE. DOOR VISUALLY CHECKED CLOSED & LOCKED. DOOR VISUALLY VERIFIED CLOSED AND LOCKED PRIOR TO DEPARTURE. (OPEN) 2L72 4F RTA35EU 20050707001102005070700110WP 2005 7 7 AALA20050408 120050625A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21565AA 49347 OVERHEAD LT AND RT OVERWING EMERGENCY EXIT SIGNS INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD LEFT AND RIGHT HAND OVERWING EMERGENCY EXIT SIGNS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050707001132005070700113WP 2005 7 7 AALA20050618 120050629A335060030451 LIGHT DOUG DC9 DC982 3022082WP SEAT 28 INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217521A 49898 SFO - CEILING EMERGENCY LIGHTS AFT OF SEAT 28 INOPERATIVE. CHARGED CEILING EMERGENCY LIGHTS AFT OF SEAT 28. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050707001152005070700115WP 2005 7 7 AALA20050411 120050623A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21402A 49313 BOS - EMERGENCY LIGHTS OVER FIRST CLASS CEILING INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS OVER FIRST CLASS CEILING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050707001172005070700117NM 2005 7 7 AALA20050412 120050623A3350 CONNECTOR BOEING757 757223 1384957NM EMERGENCY LIGHT LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21604AA 27055 MIA - EMERGENCY LIGHTS AT SEAT 16D INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHTS AT SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050707001192005070700119WP 2005 7 7 0500949859 120050517A5312 BULKHEAD DOUG DC9 DC951 3022051WP FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01768NC 47729 DURING M-CHECK FOUND CRACK IN FORWARD PRESSURE BULKHEAD AT RIVET BELOW UPPER LT AND RT RADOME ALIGNMENT PIN AT BS 37. REPAIRED PER EA 98-203219. 2L72 4F RTA6WE 20050708000032005070800003NM 2005 7 8 SWAA051885 120050628A53306545766 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 446, STR 16L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050708000052005070800005NM 2005 7 8 SWAA051896 120050629A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 706, STR 10L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050708000072005070800007NM 2005 7 8 SWAA051898 120050627A5755 HINGE BOEING737 7373H4 1384600NM LT WING SPOILER BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW MA3095 24153 DURING SCHEDULED RON CHECK, FOUND LT WING INBOARD T/E GROUND SPOILER BROKEN AT HINGE CASTING. REMOVED AND REPLACED SPOILER PER MM. 2L72 4F RTA16WE 20050708000122005070800012 2005 7 8 SWAA051903 420050629A256563550 SLIDE BOEING737 7377H4 1384404NM L1 & R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29743SW 29279 DURING SCHEDULED HC1 CHECK, FOUND L1 & R2 DOOR EMERGENCY EVAC SLIDES OUT OF ADJUST. ADJUSTED SLIDES PER MM. 2L72 4F RTA16WE 20050708000162005070800016NE 2005 7 8 SWAA051889 220050628A73208063207 MEC BOEING737 7373H4 1384600NM GE CFM56 CFM563B1 13802NE NR 2 ENGINE FAULTY A SWAAE ENGINE SHUTDOWN XJ ENGINE FLAMEOUT WARNING INDICATION DEDESCENT 1 SW29627SW 27935 856622 INFLIGHT SHUTDOWN & DECLARED EMERGENCY. AT 31,000 FT NR 2 ENGINE FLAMEOUT WHEN THRUST LEVER PLACED IN IDLE. RESTARTED NR 2 ENGINE, ALL SYSTEMS NORMAL, EXCEPT NR 2 ENGINE EGT 100 DEGREES HIGHER THAN NR 1 ENGINE EGT AFTER RESTART. REMOVED AND REPLACED NR 2 ENGINE FUEL PUMP & MEC, FUEL FILTER & SPAR VALVE ACTUATOR PER MM. 2L72 4F4 FRTA16WE E2GL 20050708000192005070800019NM 2005 7 8 SWAA051892 120050628A53306545774 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E + 16, STR 24L. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050708000232005070800023NM 2005 7 8 SWAA051917 120050702A53226546529 SHEAR TIE BOEING737 7373H4 1384600NM FWD CARGO BAY CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500, LBL 4. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050708000322005070800032NM 2005 7 8 SWAA051910 120050702A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 480, STR 12L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050708000362005070800036NM 2005 7 8 SWAA051906 120050630A3350 LAMP BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29370SW 26597 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM. 2L72 4F RTA16WE 20050708000742005070800074NM 2005 7 8 ASAA0540266 120050526A5754 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU NR 2 SLAT DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02776AS PA669 25109 NR 2 SLAT HAS DELAMINATED AT IB TRAILING EDGE. REPAIRED DAMAGED AREA OF NR 2 SLAT IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050708000782005070800078NM 2005 7 8 ASAA0540261 120050519A53306546881 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02776AS 25109 DENT AT FUSELAGE STATION 1019, 1 INCH ABOVE STR 13L. REPAIRED FUSELAGE SKIN IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050708000962005070800096NM 2005 7 8 ASAA0540280 120050614A532265737439 SHEAR TIE BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02703AS 28893 CORROSION ON FRAME SHEAR TIE B-STA 500C BETWEEN BETWEEN 28L-29R. REPAIRED IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050708000972005070800097NM 2005 7 8 ASAA0540281 120050613A57536546431244 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU RT TE FLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 RT OB FORE FLAP HAS 4 EACH DENTS ON UPPER AFT SURFACE. REPAIRED RT OB FORE FLAP UPPER SURFACE IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050708000982005070800098NM 2005 7 8 ASAA0540286 120050613A575465C26603202 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU NR 4 SLAT CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 NR 4 SLAT LOWER SURFACE OUTER SKIN CRACKED AT OB END. CUT OUT DAMAGE, INSTALLED FILLER AND DOUBLER IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050708000992005070800099NM 2005 7 8 ASAA0540273 120050529A5311654655080 FRAME BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU AFT CARGO BAY DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02792AS 28887 FRAME UPPER CHORD DENTED AFT CARGO BAY S-STA 787 BETWEEN STR 24R AND 25R. REPAIRED FRAME. (K) 2L72 4F4 FRTA16WE E21EU 20050708001002005070800100NM 2005 7 8 ASAA0540285 120050613A57536546430150 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU TE FLAP CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 RT IB FORE UPPER SURFACE CHAFED. REPAIRED IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050711000012005071100001NE 2005 7 11 ASMF200506031 220050630A7200 ENGINE DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE RIGHT MALFUNCTIONED W ASMFD RETURN TO BLOCK RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SW23204AM 49404 725566 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF RIGHT ENGINE WITH N2 OUT OF LIMITS AFTER STARTED AT 46 PERCENT. THE ENGINE WAS ADJUSTED IN LOW RPM'S IAW MM 71-00-00, PARAMETERS WERE BETWEEN LIMITS (N2 :54 PERCENT AND EGT: 440), TESTED CORRECT. 2L72 4F4 FRTA6WE E9NE 20050711000022005071100002CE 2005 7 11 2005F00089 120050615A2150 CASE LEAR 35 35LEAR 5170600CE CONDENSER SPLIT G O OTHER O OTHER CLCLIMB 1 SW01882SC 590 AIRCRAFT DEPARTED LBB AND AIR CONDITIONING SYSTEM WAS BLOWING HOT AIR. THE CREW REPORTED PROBLEM TO DISPATCH UPON ARRIVING AT ELP AND AIRCRAFT WAS REMOVED FROM SERVICE. INSPECTION FROM MAINTENANCE REVEALED THAT CONDENSER CASE HAD SPLIT AND ALL THE FREON HAD DISPERSED THE SYSTEM. RECORDS SHOW THE UNIT HAD BEEN OVERHAULED BY DRAKE AIR ON 6/18/2001. 2L72 4F A10CE 20050711000032005071100003WP 2005 7 11 MWEA050061 120050629A3620 B-NUT DOUG DC9 DC981 3022081WP SENSOR LINE LEAKING A MWEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31814ME 48010 TAIL CONE COMPARTMENT TEMPERATURE HIGH LIGHT CAME ON. FOUND AUGMENTATION VALVE SENSOR LINE LEAKING, TIGHTENED B-NUT. LEAK CHECKED GOOD. 2L72 4F A6WE 20050711000042005071100004WP 2005 7 11 MWEA050062 120050628A362039271012 AUGMENT VALVE DOUG DC9 DC981 3022081WP PNEUMATIC SYS OVERTEMP A MWEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31814ME 48010 TAIL CONE TEMPERATURE LIGHT CAME ON. RETORQUED LEFT AUGMETATION VALVE AND PRESSURE REGULATOR, TIGHTENED V-BAND ON LEFT AUGMENTATION VALVE. 2L72 4F A6WE 20050711000052005071100005CE 2005 7 11 71535 120050630A5210 RELEASE MECH BEECH 1900 1900D 1154162CE PAX DOOR FAILED A AMWAK NONE O OTHER ININSP/MAINT 1 CE0710675 10675YV AIRCRAFT PASSENGER DOOR WILL NOT RELEASE THE RELEASE LOCK. FOUND BEFORE CHECK FLIGHT. MAINTENANCE REMOVED AND REPLACED THE RELEASE MECHANISM BUTTON ASSY. MORE INFORMATION WILL BE AVAILABLE AT A LATER DATE. 2L72 4T RTA24CE 20050711000062005071100006EU 2005 7 11 F3LA200500027 120050622A2740321000M03 TRANSMITTER AIRBUSA318 A318111 3940019EU ELEVATORS UNSERVICEABLE A F3LAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM03802FR 3537 1991 AIR TURNBACK DUE TO FAULT, FLT/CTL ALTN LAW L&R AIL FAULT. REPLACED CAPTAIN'S SSTU 4CE1 PER AMM 27-92-41, PB 401. PERFORMED OPERATIONAL TEST PER AMM 27-92-41-710-001. REPLACED ELEV SERVO 34CE3 PER AMM 27-34-56-400-001. PERFORMED OPERATIONAL TEST, OPS CHECK GOOD. REPLACED NR 1 & NR 2 FCDC, PERFORMED OPS CHECK. PERFORMED FLIGHT CONTROL CHECKS PER GMM 50-13 FUNCTIONAL CARDS C271001-1 THRU C271001-6. PERFORMED AFS TEST PER AMM 22-96-00-710-001. NR 2 ELAC NOT REPLACED. PERFORMED LAND CAT III TEST, TEST OKAY. ACFT RETAINS CAT III STATUS. PERFORMED OPERATIONAL TEST FLIGHT. TEST FLIGHT SATISFACTORY. PERFORMED POST FLIGHT WALKAROUND AND FOUND AIRCRAFT SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. 2L72 4F RT 20050711000072005071100007EA 2005 7 11 SWIA200515211 120050321A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07915SW 7615 FS 625 LT INTERCOSTAL ANGLE STR 14L CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11 AND 51-42-06. 2L72 4F RTA21EA 20050711000082005071100008SO 2005 7 11 PNSA050603 120050624A3240 LINE PIPER PA32 PA32301 7103207SO RT BRAKE FAILED E PNSAO OTHER K FLUID LOSS APAPPROACH 1 AL038259V 328006097 BEFORE LANDING PILOT CHECHED BRAKES AND FOUND THAT RT BRAKE WENT TO THE FLOOR WITH NO BRAKE PRESSURE. TRIED PARKING BRAKE AND STILL HAD NO BRAKE PRESSURE. NO EMERGENCY WAS DECLARED BUT LOCAL FSS INFORMED AND A FIRE TRUCK WAS DISPATCHED AS A PRECAUTION, AN UNEVENTFUL LANDING WAS MADE. MX FOUND THAT THE RT BRAKE LINE FAILED, A NEW LINE WAS INSTALLED AND OPERATIONAL CKECK WAS NORMAL. 1L71 3O A3SO 20050711000092005071100009EU 2005 7 11 SA05080 120050627A212087292325V04 COMPUTER AIRBUSA319 A319112 3930323EU ZONE 100 OVERHEATED A USAAGA O2 MASK DEPLOYED UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 EA19720US1218 1089 DURING CLIMB OUT, FLT CREW NOTED AN AVIONICS SMOKE ECAM MESSAGE. THE CREW DONNED OXYGEN MASKS AND CONTINUED TO FOLLOW THE APPROPRIATE PROCEDURES. THE FLIGHT DIVERTED TO IAD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE AVIONICS EQUIPMENT VENTILATION COMPUTER. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20050711000122005071100012CE 2005 7 11 DXTA200500816 120050703A3240 BRAKE CESSNA500 560CESSNA 2076750CE RIGHT MALFUNCTIONED E DXTAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07312QS 5600312 RIGHT SIDE FOOT BRAKES HAVE TO BE PUSHED TO THE FLOOR TO EFFECT BRAKING. FEELS LIKE AIR IN BRAKE LINE. BLED BRAKES IAW CESSNA 560 MM 32-42-00, OPS CHECK GOOD. 2L72 4F RTA22CE 20050711000132005071100013CE 2005 7 11 DXTA200500814 120050701A3297 CONNECTOR CESSNA500 560CESSNA 2076750CE MLG LOOSE E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07399QS 5600510 LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF, COULDN'T GET HANDLE TO GO UP. TROUBLESHOT LANDING GEAR SYSTEM, LANDING GEAR LEVER PLUG (P160 ) WAS LOOSE. RE-SECURED LOOSE PLUG AND PERFORMED OPERATIONAL CHECK. OPS CHECK NORMAL IAW CE 560 MM 32-30-00. 2L72 4F RTA22CE 20050711000142005071100014CE 2005 7 11 DXTA200500817 120050703A3240 BRAKE CESSNA750 750 2076810CE MLG MALFUNCTIONED E DXTAO OTHER O OTHER LDLANDING 1 GL07908QS 7500108 DURING LANDING ROLLOUT BRAKES WERE SOFT AND FELT UNRESPONSIVE WHEN HARD BRAKING WAS APPLIED. ON TAXI IN BRAKES WERE CHECKED BY BOTH PILOTS AND BOTH PILOTS HAD THE SAME PROBLEM AT SLOW SPEEDS AS WELL. ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20050711000162005071100016NM 2005 7 11 SB05078 120050702A531210327431 SEAL BOEING737 7373B7 1384580NM AFT BULKHEAD LEAKING A USAABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19397US 23319 CREW REPORTED A LOSS OF CABIN PRESSURIZATION. CREW ACCOMPLISHED AN EMERGENCY DESCENT, DECLARED AN EMERGENCY AND DIVERTED TO RIC WHERE THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO OXYGEN MASKS WERE DEPLOYED. MAINTENANCE FOUND AND RESECURED LOOSE POTABLE WATER TANK INSULATION BLANKETS FROM THE AFT OUTFLOW VALVE AREA AND REPLACED THE AFT OUTFLOW VALVE AS PRECAUTION. PERFORMED FUNCTIONAL CHECK OF PRESSURIZATION SYSTEM PER JOB CARD J321-00-01 WITH STEP 7 FAILING. AIRCRAFT WAS THEN MAINTENANCE FERRIED TO CLT WHERE A LEAKING PRESSURE SEAL FOR THE APU DUCT PASSING THROUGH THE AFT PRESSURE BULKHEAD WAS REPLACED. PRESSURIZATION CHECK PER JOB CARD J321-00-01 WITHIN LIMITS NOW. 2L72 4F RTA16WE 20050711000202005071100020WP 2005 7 11 MWEA050066 120050705A53479957871515 SEAT TRACK DOUG DC9 DC982 3022082WP COCKPIT WORN A MWEAK NONE O OTHER ININSP/MAINT 1 GL31810ME 48072 CAPTAIN'S UPPER AND LOWER SEAT TRACK IS WORN AND ADJUSTMENT HOLES ELONGATED. FABRICATED AND INSTALLED UPPER AND LOWER SEAT TRACK. 2L72 4F A6WE 20050711000222005071100022 2005 7 11 SA05082 420050702A2565D31516113 SLIDE AIRBUSA319 A319112 3930323EU PAX DOOR DEFECTIVE A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19746UW137406553 1297 PHL - THE MAIN ENTRY DOOR WAS OPENED WHILE THE ESCAPE SLIDE WAS ARMED. THE SLIDE DID NOT INFLATE. MAINTENANCE REPLACED THE SLIDE ASSEMBLY. OK FOR SERVICE. 2L72 4F RTA28NM 20050711000242005071100024EU 2005 7 11 YENA200538 120050705A25304110001137 COFFEEMAKER AIRBUS320 A320232 3930326EU GALLEY SMOKE A YENAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15534JB171624856 1705 FORWARD GALLEY - DURING BREW PROCESS, F/A SAW WHAT APPEARED TO BE SMOKE COMING FROM THE COFFEEMAKER. TURNED OFF POWER TO COFFEEMAKER THAT STOPPED THE SMOKE. INITIALLY THE ITEM WAS DEFERRED PER MEL 25-22-03, C/B WAS PULLED AND COLLARED. THE COFFEEMAKER WAS REPLACED AT JFK. 2L72 4F RTA28NM 20050711000262005071100026WP 2005 7 11 MWEA050063 120050630A2120 DUCT DOUG DC9 DC982 3022082WP A/C PACK DETACHED A MWEAA UNSCHED LANDING S AFFECT SYSTEMS CRCRUISE 1 GL31809ME 48071 NO AIR FLOW FROM RIGHT AIR CONDITIONING PACK, PRESSURE INDICATION WAS NORMAL, BUT WHEN LEFT PACK WAS SELECTED OFF THE CABIN PRESSURE WAS LOST. FOUND DUCT OFF FROM HEAT EXCHANGER, INSTALLED NEW DUCT AND LEAK CHECKED GOOD. 2L72 4F A6WE 20050711000282005071100028NM 2005 7 11 WRLA2005120 120050622A5510 STRUCTURE DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C-04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE NR 35. 2L73 4F4 FRTA22WE E24NE 20050711000342005071100034NM 2005 7 11 WRLA2005130 120050622A5510 STRUCTURE DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C-04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098, FOUND CORROSION IN HST LT BARREL NUT HOLE NR 21. 2L73 4F4 FRTA22WE E24NE 20050711000352005071100035NM 2005 7 11 WRLA2005133 120050622A5510 STRUCTURE DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C-04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098, FOUND CORROSION IN HST LT BARREL NUT HOLE NR 17. 2L73 4F4 FRTA22WE E24NE 20050711000402005071100040NM 2005 7 11 WRLA2005128 120050622A5510 STRUCTURE DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C-04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098, FOUND CORROSION IN HST LT BARREL NUT HOLE NR 24. 2L73 4F4 FRTA22WE E24NE 20050711000442005071100044NM 2005 7 11 WRLA2005124 120050622A5510 STRUCTURE DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C-04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE NR 1. 2L73 4F4 FRTA22WE E24NE 20050711000472005071100047NM 2005 7 11 BB05047 120050624A3397 WIRE BOEING767 767201 1385125NM EMERGENCY LIGHTSLOOSE A USAAK NONE O OTHER ININSP/MAINT 1 EA19649US 23901 FOUND EMERGENCY LIGHT FLOOR STRIP NEAR MID LEFT LAV INOPERATIVE. MAINTENANCE REINSERTED A LOOSE WIRE TO A LAMP SOCKET. 2L72 4F RTA1NM 20050711000482005071100048WP 2005 7 11 IXXA05SMN24S 120050429A5320 FITTING DOUG DC8 DC871F 302199DWP CARGO BAY CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX834963359 45993 DURING ROUTINE C-CHECK INSPECTION, MAIN CARGO BAY STA 781.000 L-14R AFT FITTING CRACKED 1 IN STA 781.000. REMOVED CRACKED FITTING IAW DC-8 SRM 53-1-0 PAGE 1, DC-8 SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING IAW DWG NR 3779970. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02 TO 07. CLEANED, TREATED AND PRIMED AREA AND NEW FITTING IAW DC-8 SRM 51-1-8B. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D PAGE 9. TORQUED IAW DC-8 RM 51-3-1. 2L74 4F RT4A25 20050711000492005071100049WP 2005 7 11 IXXA05SMN52S 120050429A5512 SKIN DOUG DC8 DC871F 302199DWP HORIZONTAL STAB DENTED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX834963359 45993 DURING ROUTINE C-CHECK INSPECTION, EVALUATE FOR REPAIR DENT OF RT HORIZ STAB. PERFORMED MAJOR REPAIR IAW DC-8 SRM 55-2-1 FIG 4. FABRICATED REPAIR DOUBLER IAW DC-8 SRM 55-2-1 FIG 4. CLEANED, TREATED AND PRIMED REPAIR DOUBLE INTERNAL PART IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11 PAGE 9. INSTALLED REPAIR DOUBLER IAW DC-8 SRM 51-2-1 FIG 1, DC-8 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050711000522005071100052WP 2005 7 11 IXXA05SMN26S 120050429A5730 SKIN DOUG DC8 DC871F 302199DWP ZONE 600 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX834963359 45993 RT WING CTR L/E OUTER PLATING UPPER SURFACE CRACKED STA. XFS 430.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, SEMAN DWG ED-3937. REMOVED FASTENERS IAW DC-8 SRM. REMOVED DAMAGED AREA IAW SEMAN ED-3937. PERFORMED NDT INSPECTION IAW NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER, FILLER IAW SEMAN DWG ED-3937. CLEANED, TREATED AND PRIMED AREA+ REPAIR PARTS INTERNAL PART IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11 PAGE 9. INSTALLED REPAIR PART IAW SEMAN DWG ED-3937, DC-8 SRM 51-1-21 PAGE 1, DC-8 SRM 51-3-0 PAGE 1, DC-8 SRM 51-1-20D APGE9. TORQUED IAW DC-8 RM 51-3-1. 2L74 4F RT4A25 20050711000532005071100053WP 2005 7 11 IXXA05SMN27S 120050429A5730 SKIN DOUG DC8 DC871F 302199DWP ZONE 600 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX834963359 45993 RT WING CTR L/E LOWER OUTER PLATING CRACKED. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, SEMAN DWG ED-3944. REMOVED FASTENERS FROM REPAIR AREA IAW DC-8 SRM. REMOVED DAMAGED AREA IAW SEMAN DWG ED-3944. PERFORMED NDT INSPECTION IAW DC-8 NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER, FILLER IAW SEMAN DWG ED-3944. CLEANED, TREATED AND PRIMED AREA, FILLER AND REPAIR DOUBLER INTERIOR IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11 PAGE 9. INSTALLED REPAIR PARTS IAW SEMAN DWG ED-3944, DC-8 SRM 51-1-20D PAGE 9, DC-8 SRM 51-1-21 PAGE 1. TORQUED IAW DC-8 SRM 51-3-1. 2L74 4F RT4A25 20050711000552005071100055WP 2005 7 11 IXXA05SMN29S 120050429A5551 ATTACH FITTING DOUG DC8 DC871F 302199DWP HORIZONTAL STAB CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX834963359 45993 LT HORIZ STAB FAIRING SUPPORT AFT FITTING CRACKED STA 1870.000. REMOVED CRACKED FITTING IAW DC-8 SRM 51-3-0 PAGE 1. FABRICATED NEW FITTING IAW DWG NR 3702408. PERFORMED HEAT TREATMENT IAW DC-8 SRM 51-1-1 PAGES 1, 13, 17. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02 TO 07. CLEANED, TREATED AND PRIMED AREA AND NEW FITTING IAW DC-8 SRM 51-1-8B. INSTALLED NEW FITTING IAW DC-8 SRM 51-3-0 PAGE 1. TORQUED IAW DC-8 RM 51-3-0 PAGE 1, DC-8 SRM 51-3-1 PAGE 2A. 2L74 4F RT4A25 20050711000572005071100057WP 2005 7 11 IXXA05SMN31S 120050429A5322 FITTING DOUG DC8 DC871F 302199DWP CARGO BAY CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX834963359 45993 MAIN CARGO BAY FITTING INTERNAL SKIN CRACKED, STA 700.000 L-21 - L-22R. REMOVED CRACKED FITTING IAW DC-8 SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING IAW DWG NR 3616948. PERFORMED HEAT TREATMENT IAW DC-8 SRM 51-1-1 PAGES 1, 13, 17. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02 TO 07. CLEANED, TREATED AND PRIMED AREA AND NEW FITTING IAW DC-8 SRM 51-1-8B. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D PAGE 9. TORQUED DC-8 SRM 51-3-1. 2L74 4F RT4A25 20050711000602005071100060WP 2005 7 11 IXXA05SMN34S 120050429A5340 ATTACH FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX834963359 45993 MAIN CARGO BAY INTERNAL FUSELAGE FITTING CORRODED, STA 41520.000 L-21L. REMOVED CORROSION IAW DC-8 SRM 51-1-8 PAGE 17-18. FOUND OUT OF LIMITS IAW DC-8 SRM 53-2-0 PAGE 2P. REMOVED CORRODED FITTING IAW DC-8 SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING IAW DWG NR 4640162. PERFORMED NDT INSPECTION IAW NDT DC-8 NDT SPM PART 08-00-02 TO 07. CLEANED, TREATED AND PRIMED AREA AND NEW FITTING IAW DC-8 SRM 51-1-8B. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D PAGE 9. TORQUED DC-8 SRM 51-3-1. 2L74 4F RT4A25 20050711000622005071100062WP 2005 7 11 IXXA05SMN18S 120050429A5320 TEE FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX834963359 45993 MAIN CARGO BAY FWD TYPE I DOOR INNER JAMB FITTING CRACKED, STA 384.000 L-11 AND L-12R. REMOVED DAMAGED TEE IAW DC-8 SRM 53-1-0, DC-89 SRM 51-1-20D PAGE 21. FABRICATED NEW TEE IAW DGW 9755815. PERFORMED NDT INSPECTION TO TEE IAW NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED AREA AND NEW TEE IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11 PAGE 9. INSTALLAED NEW TEE IAW DC-8 SRM 51-1-20D PAGE 9. TORQUED IAW DC-8 SRM 51-3-1. 2L74 4F RT4A25 20050711000642005071100064WP 2005 7 11 IXXA05SMN20S 120050429A5340 ATTACH FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX834963359 45993 MAIN CARGO BAY STA 680.000 L-11L AFT FITTING CRACKED. REMOVED CRACKED FITTING IAW DC-8 SRM 53-1-0 PAGE 1, DC-8 SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING IAW DWG NR 4751625. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02 TO 07. CLEANED, TREATED AND PRIMED AREA AND NEW FITTING IAW DC-8 SRM 51-1-8B. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D PAGE 9. TORQUED IAW DC-8 RM 51-3-1. 2L74 4F RT4A25 20050711000652005071100065WP 2005 7 11 IXXA05SMN21S 120050429A5340 ATTACH FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX834963359 45993 MAIN CARGO BAY RT WING CTR SECTION FITTING CRACKED, STA 759.000 RBL 23. REMOVED CRACKED FITTING IAW DC-8 SRM 53-1-0 PAGE 1, DC-8 SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING IAW DWG NR 4646547. PERFORMED HEAT TREATMENT IAW DC-8 SRM 51-1-1 PAGES 1, 13, 17. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02 TO 07. CLEANED, TREATED AND PRIMED AREA AND NEW FITTING IAW DC-8 SRM 51-1-8B. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D PAGE 9. TORQUED IAW DC-8 RM 51-3-1. 2L74 4F RT4A25 20050711000662005071100066WP 2005 7 11 IXXA05SMN22S 120050429A5340 ATTACH FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX834963359 45993 MAIN CARGO BAY RT WING SECTION INTERIOR FITTING CRACKED, STA 781.000 - RBL 23. REMOVED CRACKED FITTING IAW DC-8 SRM 53-1-0 PAGE 1, DC-8 SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING IAW DWG NR 4646547. PERFORMED HEAT TREATMENT IAW DC-8 SRM 51-1-1 PAGES 1, 13, 17. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02 TO 07. CLEANED, TREATED AND PRIMED AREA AND NEW FITTING IAW DC-8 SRM 51-1-8B. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D PAGE 9. TORQUED IAW DC-8 SRM 51-3-1. 2L74 4F RT4A25 20050711000692005071100069NM 2005 7 11 QXEA200501077 120050621A243023088002B GENERATOR DHAV DHC8 DHC8202 2809007NM NR 1 MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09356PH1171 883 502 NR 1 DC GENERATOR CAUTION ILLUMINATED. CHECKLIST EXTINGUISHED LIGHT THEN NR 1 DC GENERATOR CAUTION ILLUMINATED AND FAILED TO RESET. REMOVED AND REPLACED NR 1 DC GENERATOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050711000702005071100070NE 2005 7 11 AWXA200500368 220050325A72202607MK2 ACTUATOR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE VSV MALFUNCTIONED A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28670AW168511871 2029 ON TAKEOFF ROLL RECEIVED ECAM MESSAGE FOR NR 2 ENGINE COMPRESSOR VANE, REJECTED TAKEOFF BELOW 70 KTS AND RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED VARIABLE STATOR VANE (VSV) ACTUATOR IAW T/C R5M75303, OPERATIONAL CHECK WAS GOOD. VENDORS TEAR DOWN REPORT SHOWS UNIT FAILED TESTING, CONFIRMING THE FAULT. INVESTIGATIONS REVEALED FUEL LACQUER PARTIALLY BLOCKING SERVO VALVE SUPPLY PORT FILTER SCREEN. ROOT CAUSE OF FAILURE. VENDORS SUGGESTS THAT DUE TO LOW TIME ON VSV THAT AMERICA WEST AIRLINES REVIEW QUALITY OF FUEL USED. UNIT OVERHAULED AND TESTED IAW CMM 75-32-61 REV 1. 2L72 4F4 FRTA28NM E40NE 20050711000722005071100072NM 2005 7 11 05FDEA01678 120050624A7160 SKIN DOUG MD11 MD11 3023602NM NR 2 NACELLE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25619FE 48770 NR 2 ENGINE, NOSE INLET LIP FOUND CRACKED AT 8 O'CLOCK POSITION AND EXISTING REPAIR DOUBLER HAS LOOSE FASTENERS. REMOVED AND REPLACED AS PER AMM 54-22-01-4 AND APPLIED SEALANT AS PER AMM 54-22-01-4. 2L73 4F RTA22WE 20050711000732005071100073NM 2005 7 11 05FDEA01679 120050624A7830 TORQUE RING DOUG MD11 MD11 3023602NM THRUST REVERSER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25619FE 48770 NR 1 ENGINE, RT THRUST REVERSER FORWARD FRAME, UPPER TORQUE RING CRACKED APPROXIMATELY 1.5 IN LENGTH. THRUST REVERSER REMOVED AND INSTALLED NEW REVERSER AS PER WORK CARD 78T3001-R AND WORK CARD 78T3901-R, GE NR 1 RIGHT REVERSER DOOR - INSTALL. REVERSER ADJUSTMENT AND OPERATION CHECK CARRIED OUT AS PER WORK CARD 78T3901-R, GE NR 1 RT REVERSER DOOR - INSTALL. 2L73 4F RTA22WE 20050711000742005071100074WP 2005 7 11 05FDEA01680 120050624A77008062127 ENGINE DOUG MD10 MD1010F 3022112WP GE CF6 CF66K 30020NE NR 1 MALFUNCTIONED A FDEAO OTHER RGYPARTIAL RPM/PWR LOSS MULTIPLE FAILURE ENGINE STOPPAGE DEDESCENT 1 SO25565FE 46996 NR 1 ENGINE REMAINED AT FLIGHT IDLE DURING DESCENT AND WOULD NOT FOLLOW THROTTLE. N1 AND N2 SLOWLY STARTED DECAYING UNTIL GEN, AIR, HYDRAULIC ALERTS STARTED COMING ON. EGT WAS BELOW OTHER ENGINES 150-200 DEG FF WAS APPROX 500 PPH. FIRST NOTED PROBLEM FL220, RPM LOW AT FL180. MOTORIZED NR 1 ENG AS PER FEC MD-10 JRH AND NO FOG FROM TAILPIPE. TRIED STARTING ENG AND ENG WOULD FLAME OUT AT APPROX 41 PERCENT. FF WOULD DECREASE AND ENG WOULD SPIN DOWN. 2L73 4F4 FRTA22WE E23EA 20050711000752005071100075GL 2005 7 11 05FDEA01681 220050624A7310 FUEL LINE DOUG MD10 MD1010F 3022112WP GE CF6 CF66D 30020GL NR 3 ENGINE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25391FE 46625 NR 3 ENGINE FUEL LINE CRACKED ABOVE PYLON AT CONNECTING BRACKET UNDER PANEL 617CT. REMOVED AND REINSTALLED AFTER REPAIR PER TRAVLER T5/527309, NR 3 ENGINE PYLON. MAIN FUEL LINE AT PANEL 617CT IAW MM 20-50-01-2. LEAK CHECK GOOD IAW MM 28-00-02-2. 2L73 4F4 FRTA22WE E23EA 20050711000762005071100076WP 2005 7 11 05FDEA01682 120050624A5414 ACCESS PANEL DOUG MD10 MD1010F 3022112WP GE CF6 CF6* 30020GL NR 1 PYLON CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25391FE 46625 NR 1 PYLON FUEL LINE INSIDE ACCESS PANEL 517CT HAS IMPROPER STOP DRILL INSIDE RADIUS OF WELD. CRACK APPEARS TO HAVE PROPAGATED ONTO THE WELD. REMOVED AND REINSTALLED AFTER REPAIR PER TRAVELER T5/522336 NR 1 PYLON FUEL LINE INSIDE ACCESS 517CT IAW MM 20-50-01-2. LEAK CHECK GOOD IAW MM 28-00-02-2. 2L73 4F4 FRTA22WE E23EA 20050711000772005071100077EU 2005 7 11 05FDEA01683 120050624A5311 FRAME AIRBUS300 A300B4622R 3930312EU FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25719FD 388 FRAME 45 RT SIDE JUST ABOVE STRINGER 27 FRAME FITTING HOLE NR H2 MEASURE AT .372 DIA UPON REMOVAL OF FASTENER FOR NDT ON EO NR E6-5310-7-5006 PT 4. REF N CARD N00061. COMPLIED WITH EA 6-5310-90201 PT2. 2L72 4F RTA35EU 20050711000782005071100078EU 2005 7 11 05FDEA01684 120050624A5311 FRAME AIRBUS300 A300B4622R 3930312EU FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25719FD 388 FRAME 46 RT SIDE AT STRINGER 27 FRAME FITTING HOLE NR H1 HAS A BUSHING IN THE FITTING MEASURING AT .436 DIA WITH A 2ND OVERSIZE HOLE AT .278 DIA FOUND UPON REMOVAL OF FASTENER ON EO 6-5310-7-5006 PT4 REF N CARD N00062. COMPLIED WITH EA 6-5310-90201 PT1. 2L72 4F RTA35EU 20050711000792005071100079EU 2005 7 11 05FDEA01685 120050624A5311 FRAME AIRBUS300 A300B4622R 3930312EU FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25719FD 388 FRAME 41 LT SIDE BETWEEN STRINGERS 25 AND 26 FRAME FITTING HOLE H1 HAS A BUSHING INSTALLED WITH A FASTENER HOLE AT 2ND OVERSIZE AT .278 DIA FOUND UPON REMOVAL OF FASTENER FOR NDT ON EO 6-5310-7-5006 PT3 REF N CARD N00059. COMPLIED WITH EA 6-5310-90201 PT1. 2L72 4F RTA35EU 20050711000802005071100080CE 2005 7 11 DXTA200500799 120050617A2720972260 DMU CESSNA750 750 2076810CE RUDDER MALFUNCTIONED E DXTAO OTHER E VIBRATION/BUFFET CRCRUISE 1 GL07909QS 7500009 AT CRUISE ALTITUDE, HEARD CLICK OR SNAP AND FELT ABRUPT JERK OF NOSE TO LT . RUDDER TRIM RAN AWAY WITH 50 PERCENT DEFLECTION AND STOPPED RETRIMMED RUDDER WITH NO FURTHER INCIDENT. CHECKED RUDDER CABLE TENSIONS AND DMU FOR A PCU FORCE FLIGHT. CONNECTED DMU AND FOUND NO INDICATIONS OF A FORCE FIGHT ON ANY PCU. REMOVED DMU AND RESTORED ACFT TO ORIGINAL POSITION CONFIGURATION. NEED TO LOCATE RUDDER CONTOUR BOARDS TO PERFORM RUDDER CONTROL SYSTEM CHECK. 2L72 4J RTT00007WI 20050711000812005071100081CE 2005 7 11 DXTA200500801 120050623A7930 ENGINE CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE RIGHT MALFUNCTIONED E DXTAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 GL07367QS 5600367 PCEJCO410 T/O N1 REQUIRED 96.1; AS POWER WAS ADVANCED FOR T/O AND GOING THRU APPROX 84-85 PERCENT RT ENGINE OIL PRESS EXCEEDED 95 PSI AND TEMP WAS APPROACHING 120 DEGREES. T/O WAS ABORTED. GROUND RAN ENG AT VARIOUS POWER SETTINGS INCLUDING T/O N1 OF THE DAY. ALL ENGINE PARAMETERS FOUND TO BE WITHIN LIMITS. OPS CHECK GOOD IAW CE560 M/M 71-10-03. 2L72 4F4 FRTA22CE E25EA 20050711000822005071100082CE 2005 7 11 DXTA200500802 120050623A29106311301 HYDRAULIC SYSTEM CESSNA650 650 2076802CE RIGHT MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07797QS3115 6507097 AUX HYD PRESS, SPOILER HOLDDOWN, HYD PRESS LOW LT AND RT. AILERON BOOST OFF. ANNUNCIATORS ALL ILLUMINATED. UPON GEAR RETRACTION GREEN LIGHTS WENT OUT BUT RED UNLOCKED LIGHT STAYED ON. AUDIBLE DRAG NOISE AND CLUNK NOISE HEARD. DRAG NOISE DISSIPATED AND RED UNLOCKED LIGHT WENT OUT. WHEN AUX HYDRAULIC PUMP WAS TURNED ON, ALL OF ABOVE ANNUNCIATORS WENT OUT. HYDRAULIC VOLUME GAUGE PEGGED TO MAX FULL. FOUND AIR IN HYDRAULIC SYSTEM. BLED SYSTEM AS NEEDED. REMOVED LT HYDRAULIC PUMP AND INSTALLED ON RT SIDE FOR CONVENIENCE. REMOVED RT HYDRAULIC PUMP AND INSTALLED ON LT SIDE FOR CONVENIENCE. PERFORMED SATISFACTORY ENGINE GROUND RUN AND LEAK CHECK. WORK DONE IAW CESSNA 750 MM 29-10-04 AND 12-10-15. 2L72 4F A9NM 20050711000842005071100084NM 2005 7 11 AWXA200500737 120050622A3397BMS13311122 WIRE BOEING737 737300 1384610NM EMERGENCY LIGHTSBROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 FOUND EMERGENCY EXIT LIGHTS AT ROWS 11 THROUGH ROW 15 ESCAPE PATH LIGHTING INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE. SEATS OPERATIONAL CHECKS GOOD. 2L72 4F RTA16WE 20050711000852005071100085NM 2005 7 11 AWXA200500738 120050622A521080330035 BOTTLE BOEING757 7572S7 1384962NM L1 DOOR EMPTY A AWXAK NONE O OTHER ININSP/MAINT 1 WP28904AW 23566 FOUND L-1 DOOR ASSIST BOTTLE EMPTY. MAINTENANCE REMOVED AND REPLACED THE L-1 DOOR ASSIST BOTTLE IAW BOEING 757 MM 52-11-30-4. 2L72 4F RTA2NM 20050711000862005071100086EU 2005 7 11 AWXA200500739 120050622A3350321431 BATTERY AIRBUS320 A320232 3930326EU EMERGENCY LIGHTSDISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28602AW 565 FOUND EMERGENCY LIGHTS AT PASSENGER SEATS 9L AND 11L ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED RT MID CABIN EMERGENCY LIGHT BATTERY IAW AMERICA WEST AIRLINES T/C A1C33302. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA28NM 20050711000872005071100087NM 2005 7 11 AWXA200500740 120050606A57536546434362 SKIN BOEING737 7373B7 1384580NM TE FLAPS DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28328AW 23377 FOUND DISBOND AREA AT OUTBOARD END OF RT INBOARD AFT FLAP UPPER AND LOWER SURFACE. MAINTENANCE REMOVED DAMAGED AREA ON OUTBOARD END OF RT INBOARD AFT FLAP AND FABRICATED REPAIR DOUBLER AND REPAIR CORE IAW BOEING 737-300 SRM 51-70-10-0 FIG 16. BONDED FABRICATED REPAIR PARTS TO THE OUTBOARD END OF THE RT INBOARD AFT FLAP IAW BOEING 737-300 SRM 51-70-10-0, REPAIR 7, FIG 16. 2L72 4F RTA16WE 20050711000892005071100089NM 2005 7 11 AWXA200500742 120050608A5414311A14509 SKIN BOEING737 7373B7 1384580NM LT PYLON CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28328AW 23377 FOUND TOP LT PYLON CRACKED AT ACCESS PANEL 5727L. MAINTENANCE STOP DRILLED CRACK AT LT PYLON PANEL 5727L AND INSTALLED DOUBLER AT LT PYLON ACCESS PANEL 5727L IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5430-05166-SS1. 2L72 4F RTA16WE 20050711000902005071100090 2005 7 11 05FDEA01652 420050622A3451 ANTENNA BOEING727 7272S2F 1384O81NM NR 2 DME CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25203FE 22925 NR 2 DME ANTENNA CORRODED. REMOVED AND REPLACED NR 2 DME ANTENNA IAW MM34-45-011-4. PERFORMED OPS CHK IAW MM 34-45-000-0. OPS CHECKS GOOD. 2L73 4F A3WE 20050711000912005071100091NM 2005 7 11 05FDEA01655 120050622A54116519686765 FRAME BOEING727 7272S2F 1384O81NM NR 1 ENG COWL CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25203FE 22925 NR 1 ENG FIXED COWL UPPER FRAME CRACKED BETWEEN NR 2 AND NR 3 LATCHES. REMOVED AND REPLACED COWL PANEL IAW SRM 51-30-2. 2L73 4F A3WE 20050711000962005071100096NM 2005 7 11 05FDEA01661 120050623A522065372913A HANDLE BOEING727 7272S2F 1384O81NM EMERGENCY EXIT CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25203FE 22925 LT FWD EMERGENCY EXIT LOWER HANDLE ESCATION IS CRACKED. REMOVED AND REPLACED HANDLE ASSY IAW SRM 51-30-2. (M) 2L73 4F A3WE 20050711000982005071100098 2005 7 11 05FDEA01663 420050623A34553400137 ANTENNA BOEING727 7272S2F 1384O81NM NR 2 ADF CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25203FE 22925 NR 2 ADF ANTENNA DISBONDED AND CORRODED. REMOVED AND REPLACED NR 2 ADF LOOP ANTENNA IAW 34-37-012-4. PERFORMED OP CHECK IAW MM 34-37-001-5. OPS CHECKS GOOD. 2L73 4F A3WE 20050711000992005071100099WP 2005 7 11 05FDEA01647 120050622A3260 UPLOCK SENSOR DOUG DC10 DC1010 3022110WP RT MLG OUT OF ADJUST A FDEAO OTHER N FALSE WARNING CLCLIMB 1 SO2568054 47808 RETRACTED GEAR AFTER T/O, RT MLG INDICATED UNSAFE UP BOTH PANELS. COMPLIED WITH QRH. FOLLOWING SECOND RETRACT, RED LIGHT EXTINGUISHED AFTER SEVERAL MINUTES, A/S 205KTS. BITE CHECKED PROX SENSOR BOX, CHECK GOOD. INSP RT MLG UPLOCK SENSOR, SENSOR WIRING, AND TARGET. WIRING LOOKED OK AND TERMINAL ENDS CLEAN. FOUND TARGET AND SENSOR AIR GAP NOT PARALLEL. ADJUSTED SENSOR SHIMS SO THAT AIR GAP WAS PARALLEL TO TARGET AND TO OBTAIN PROPER CLEARANCE PER AMM 32-34-03-2 1. 2L73 4F A22WE 20050711001022005071100102EU 2005 7 11 MALA050503 120050623A2432 BATTERY SAAB SF340 340B 7860101EU DC GEN SYS FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15426XJ 340B426 BATTERY FAILED CAPACITY CHECK. 2L72 4T RTA52EU 20050711001032005071100103NM 2005 7 11 DHL2005741593 120050511A5754 RIB BOEING727 7272Q9 138448MNM NR 1 SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 NR 1 SLAT AT ACT ROD END HAS O/B SLAT RIB CRACKED. REMOVED DAMAGED O/B RIB IAW B727 SRM 51-30-2. DRILLED, TREATED AND PRIMED RIB IAW B727 SRM 51-30-2. DRILLED, TREATED AND PRIMED RIB AND AREA IAW B727 SRM 51-30-2 AND SRM 51-10-2. INSTALLED O/B RIB IAW B727 SRM 51-30-2 OI 410674 PN65-17327-4. 2L73 4F RTA3WE 20050711001072005071100107GL 2005 7 11 CHQA200500122 220050624A7200AE3007A1P ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 2 SMOKE A CHQAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 GL11568RP3659 3659 145800 CAE312588 DURING CLIMB-OUT, LAV SMOKE MESSAGE APPEARED ON EICAS AND BURNING ODOR NOTED IN COCKPIT. F/A REPORTED DETECTING BURNING OIL ODOR IN CABIN AS WELL. EMERGENCY DECLARED AND AIRCRAFT RETURNED TO FIELD WITHOUT EVENT. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE IAW J/C CE72-00-01. ENGINE WOULD LATER FAIL IT'S TEST RUN DUE TO LAV SMOKE ON EICAS. 2L72 4T4 FRTT00011ATTE6CH 20050711001082005071100108SO 2005 7 11 RAIA00506026 120050619A2120 UNKNOWN EMB 145 EMB145LR 3260212SO CABIN FUMES A RAIAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE03822HK 145069 F/A REPORTED ACRID FUMES, POSSIBLY ELECTRICAL, AT ROW 7. ALSO, INDICATED AIR OUTLET AT FLOOR HOT TO AN EXTREME AT SAME LOCATION. MAINTENANCE INSPECTED AND PERFORMED OPS CHECK OF CABIN COOLING SYSTEM AND COULD NOT DUPLICATE PROBLEM. 2L72 4T RTT00011AT 20050711001092005071100109SO 2005 7 11 RAIA00506027 120050621A326023092900001 UPLOCK SENSOR EMB 145 EMB145 3260210SO MLG BROKEN A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03804HK14997 145082 LANDING GEAR/LEVER DISAGREE MESSAGE ON EICAS. MAINTNENACE REMOVED AND REPLACED NR 1 GEAR UPLOCK BOX. OPS CHECKED GOOD. 2L72 4F RTT00011AT 20050711001102005071100110NM 2005 7 11 - 120050622A3350 CONNECTOR BOEING757 757223 1384957NM EMERGENCY LIGHTSLOOSE A AALAK NONE O OTHER ININSP/MAINT 1 SW21619AA 24577 FOUND 2 ADJACENT ESCAPE PATH EMERGENCY LIGHTS INOPERATIVE AT SEAT 16D. FOUND LOOSE CONNECTOR AT SEAT 16F. SECURED CONNECTOR FOR EMERGENCY ESCAPE PATH LIGHTS AT SEAT 16F. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050711001142005071100114 2005 7 11 AALA20050404 420050621A2565D30656126 SLIDE BOEING757 757223 1384957NM NR 4 DOOR DEPLOYED A AALAK NONE O OTHER ININSP/MAINT 1 SW21676AN 29426 CABIN SERVICES PERSONNEL OPENED LT NR 4 DOOR AND PARTIALLY DEPLOYED SLIDE FROM INSIDE AIRCRAFT. DOOR ASSIST BOTTLE DISCHARGED. SLIDE DEPLOYED BUT DID NOT INFLATE. REPLACED SLIDE AND DOOR ASSIST BOTTLE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050711001172005071100117WP 2005 7 11 AALA20050405 120050622A3350P4010051111 MODULE DOUG DC9 DC982 3022082WP AFT GALLEY INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21286AA 49298 EMERGENCY LIGHTS IN AFT GALLEY AREA AT SEAT 21DEF TO 32DEF INOPERATIVE. REPLACED MODULE AND BATTERY FOR EMERGENCY LIGHTS IN AFT GALLEY AREA AT SEAT 21 DEF TO 32 DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050711001182005071100118NE 2005 7 11 BB05049 220050703A7310 O-RING BOEING757 7572B7 1384964NM RROYCERB211 RB211535E4 54555NE FUEL SYSTEM LEAKING A USAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA19632AU 27810 31371 IND FLT 634 EN ROUTE, LAS TO PHL. THE FLIGHT CREW NOTICED A 2400 LB PER HOUR FUEL LOSS. THE FIRST OFFICER CONFIRMED THAT THERE WAS A VAPOR COMING FROM THE RIGHT ENGINE PYLON AREA. THE CREW DIVERTED TO IND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED O-RINGS GOING ON THE FUEL TUBE FROM THE FUEL FLOW REGULATOR TO THE HIGH PRESSURE PUMP INLET. AIRCRAFT LEAK CHECKS OK. 2L72 4F4 FRTA2NM E12EU 20050711001192005071100119NM 2005 7 11 SB05075 120050628A291065449913 SHUTOFF VALVE BOEING737 7373B7 1384580NM HYD SYSTEM LEAKING A USAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 EA19393US 23315 PHL FLT 1085 AFTER TAKEOFF AND GEAR RETRACTION, CREW REPORTED A SUBSTANTIAL DROP IN THE A-HYDRAULIC SYSTEM QUANTITY. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE FLIGHT CONTROL SHUTOFF VALVE MANIFOLD LEAKING NEAR THE A-SYSTEM INLET LINE. REPLACED FLIGHT CONTROL SHUTOFF VALVE ASSEMBLY. LEAK CHECK GOOD. ALSO, REPLACED A-HYDRAULIC SYSTEM QUANTITY INDICATOR. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050711001202005071100120NM 2005 7 11 DHL2005741004 120050707A3260 WARNING LIGHT BOEING727 7272Q9 138448MNM MLG ILLUMINATED A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01741DH 21931 AFTER TAKEOFF WHEN SELECTING GEAR HANDLE OFF, RIGHT GEAR DOOR LIGHT ILLUMINATED. COMPLIED WITH ABNORMAL PROCEDURE. LIGHT EXTINGUISHED. INSPECTED & CLEANED RT GEAR DOOR POSITION SWITCH. CYCLED GEAR DOOR SEVERAL TIMES, NO DEFECTS NOTED IAW MM 32-62-11 & 32-62-00. 2L73 4F RTA3WE 20050711001212005071100121NM 2005 7 11 DHL2005741607 120050601A5315 FLOORBEAM BOEING727 7272Q9 138448MNM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 FLOORBEAM AT BS 1110, BL-0, LWR CHORD IS EXFOLIATED. REMOVED WEB FOR ACCESS FROM STA 1110 BL 0 TO STA 1130 BL 0 IAW B727 SRM 51-30-2. CUT OUT DAMAGED AREA FLOORBEAM LOWER CHORD STA 1110 BL 0 SIZE 4.5 X 2 INCH IAW B727 SRM 53-10-8. FABRICATED REPAIR ANGLES FILLER AND STRAP MAT USED ANGLES 7075-T6 .071 SIZE 16.5 X 2.25 INCH PO 5096275 FILLER 7075-T6 .0125 SIZE 4.5 X 2 INCH PO 9912445 STRAP 7075-T6 .100 PO 9911586 SIZE 18.5 X 2 INCH IAW B727 SRM 53-10-8. TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED REPAIR AT FLOORBEAM CHORD STA 1110 BL 0 IAW B727 SRM 53-102. INSTALLED WEB WHICH WAS REMOVED TO GET ACCESS TO THE DAMAGED AREA FROM STA 1110 TO 1130 BL 0 IAW B727 SRM 51-30-2. 2L73 4F RTA3WE 20050711001222005071100122NM 2005 7 11 SB05076 120050630A335020131A BATTERY PACK BOEING737 737401 1384701NM AFT CABIN DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19405US 23885 PIT - MAINTENANCE REPORTED THE EMERGENCY LIGHT BATTERY PACK M1137 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE M1137 BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050711001232005071100123NM 2005 7 11 DHL2005741003 120050626A2910 FEEL UNIT BOEING727 7272Q9 138448MNM ELEVATOR MALFUNCTIONED A DHLABA EMER. DESCENT UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SO01741DH 21931 ON TEST FLIGHT LOST A-SYSTEM HYDRAULICS ON APPROACH BACK INTO JAX, DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. LOST A-SYSTEM HYDRAULICS, ALL QUANTITY LOST ABNORMAL PROCEDURE COMPLETED HYD FLUID SHUT OFF VALVES CLOSE FOR ONLY 1.5 MINUTES (APPROX). REMOVED AND REPLACED ELEV FEEL COMPUTER IAW B727 MM 27-30-101. LEAK CHECK GOOD IAW B727 MM 27-30-0, OPS CK GOOD IAW B727 MM 27-30-101. 2L73 4F RTA3WE 20050711001242005071100124CE 2005 7 11 PNSA050701 120050706A5730262001423 FAIRING CESSNA208 208 2073702CE LT WING FAILED E PNSABA EMER. DESCENT UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 AL039481F13761 20800070 DEPARTED AKN EN ROUTE FOR DLG ON V453, JUST AFTER LEVELING OFF AT 4000 FEET THE AIRCRAFT STARTED SHAKING. CREW DECLARED AN EMERGENCY AND RETURNED TO AKN WITHOUT INCIDENT. MAINTENANCE FOUND LT WING FAIRING P/N 2620014-23 HAD FAILED. 1H71 3T NTA37CE 20050711001252005071100125NE 2005 7 11 PNSA050602 220050607A7200 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LEFT MALFUNCTIONED A PNSAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 AL03665PA 340B181 LT ENGINE HAD AUTO IGNITION EVENT DURING CRUISE IN CLOUDS ANTI-ICE SYSTEM WAS ON. NO VISIBLE ICE NOTED BY CREW HOWEVER THERE WAS ICE FORECAST. CREW REPORTED ONE IGNITION RELIT AND CONFIRMED IGNITION LIGHTS ON. ALL OTHER PARAMETERS NORMAL. CREW ELECTED TO RETURN TO ANC WHERE MAINTENANCE BORESCOPED COMPRESSOR AND CHECKED ENGINE ANTI-ICE SYSTEM. EVERYTHING WAS FOUND NORMAL AND AIRCRAFT RELEASED FOR SERVICE. NO OTHER PROBLEMS NOTED ON LATER FLIGHTS. 2L72 4T4 TRTA52EU E8NE 20050711001272005071100127NE 2005 7 11 AALA20050401 220050622A7310 FUEL FILTER AIRBUS300 A300B4605R 3930308EU GE CF6 CF680C2A5 NE NR 1 ENGINE CONTAMINATED A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2170072 515 690268 NR 1 ENGINE FUEL CLOG LIGHT CAME ON MOMENTARILY WITH CLIMB-OUT. INSPECTED ENGINE. REPLACED MAIN ENGINE FUEL FILTER ASSEMBLY AND DIFFERENTIAL PRESSURE SWITCH. OPERATIONAL CHECK NORMAL AND NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA35EU E13NE 20050711001312005071100131EA 2005 7 11 VTZA200500119 120050623A5343601R536066 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA RT ENGINE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27642BR 7356 RT ENGINE SUPPORT BEAM CRACKED IN LOWER WEB. 2L72 4F RTA21EA 20050711001322005071100132NM 2005 7 11 05FDEA01668 120050623A7830 TRACK GE ESCF62G13 DOUG MD11 MD11 3023602NM THRUST REVERSER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE R592103 48460 NR 2 ENGINE, RT THRUST REVERSER COWL, UPPER SLIDER TRACK END SUSPECTED CRACKED. THRUST REVERSER COWL REMOVED AND REPLACED. 2L73 4F RTA22WE 20050711001332005071100133NM 2005 7 11 05FDEA01672 120050623A7830 FRAME GE DOUG MD11 MD11 3023602NM THRUST REVERSER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE R592054 48460 NR 3 ENGINE, LT THRUST REVERSER COWL, FORWARD FRAME UPPER RADIUS SUSPECTED CRACKED. THRUST REVERSER COWL REMOVED AND REPLACED. 2L73 4F RTA22WE 20050711001342005071100134NM 2005 7 11 05FDEA01673 120050624A5514ALC8106Y2 FITTING DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25619FE 48770 EMPENNAGE WITH REFERENCE TO EO 1-5510-7-5000-01 PART 1, FOUND NR 14R FITTING BORE CORRODED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. 2L73 4F RTA22WE 20050711001352005071100135NM 2005 7 11 05FDEA01674 120050624A5514ALC8107Y2 FITTING DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25619FE 48770 EMPENNAGE WITH REFERENCE TO EO 1-5510-7-5000-01 PART 1, FOUND NR 26R FITTING BORE CORRODED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. 2L73 4F RTA22WE 20050711001362005071100136NM 2005 7 11 05FDEA01671 120050623A5730 SKIN DOUG MD11 MD11 3023602NM RT WING BULGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 RT WING TRAILING EDGE UPPER SURFACE AT XORS 826.50, OUTBOARD OF NR 5 SPOILER, FOUND BULGING. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. 2L73 4F RTA22WE 20050711001382005071100138EA 2005 7 11 VTZA200500121 120050623A5320601R35031239 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27642BR 7356 RT FS 621 FLOOR SUPPORT CRACKED IN ANGLE. 2L72 4F RTA21EA 20050711001392005071100139EA 2005 7 11 VTZA200500122 120050623A53116013600130 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27642BR 7356 RT FS 640 FRAME DOUBLER CRACKED IN RADIUS. 2L72 4F RTA21EA 20050711001412005071100141EA 2005 7 11 VTZA200500123 120050623A5712601R107091 RIB CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27642BR 7356 LT BATTERY RIB CRACKED. 2L72 4F RTA21EA 20050711001422005071100142EU 2005 7 11 AWXA200500781 120050706A3397A9299304600600 WIRE HARNESS AIRBUS320 A320232 3930326EU IAE V2524 V2524A5 NE EMERGENCY LIGHT INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28638AW 455 DURING 4 DAY, FOUND THE EMERGENCY EXIT SEAT LIGHTS AT ROW 19ABC WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED WIRING HARNESS AT SEAT 19ABE IAW MFG MM 33-51-00. OPERATIONAL CHECKS WERE GOOD. (OPEN) 2L72 4F4 FRTA28NM E40NE 20050711001432005071100143NE 2005 7 11 AWXA200500782 220050706A7321UL26051 LINE BOEING757 757225 1384959NM RROYCERB211 RB211535E4 54555NE NR 2 ENGINE CRACKED A AWXAO OTHER J WARNING INDICATION CRCRUISE 1 WP28913AW 22207 DURING CRUISE, EN ROUTE, ENGINE NR 2 EPR INDICATION WAS HIGH COMPARED TO THE LT ENGINE WITH OTHER INDICATIONS BEING PAIRED. ALSO HAD THRUST LEVER SPLIT. REDUCED THRUST TO IDLE ON NR 2 ENG FOR REMAINDER OF FLIGHT. LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE P1 LINE ON THE NR 2 ENG SPLIT IN HALF. REMOVED AND REPLACED THE P1 LINE IAW MFG MM 20-11-00-912-009 AND 73-21-04-4. OPERATIONAL CHECKS WERE NORMAL. 2L72 4F4 FRTA2NM E12EU 20050711001442005071100144NM 2005 7 11 AWXA200500783 120050627A335020121 CHARGER BOEING757 7572S7 1384962NM RROYCERB211 RB211535E4 54555NE EMERGENCY LIGHT INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28905AW 23567 DURING C-10 CHECK FOUND SEVERAL EMERGENCY BULL NOSE LIGHTS INOPERATIVE AT L3 AND R3 DOORS. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY AT M735. OPERATIONAL CHECKS WERE GOOD. 2L72 4F4 FRTA2NM E12EU 20050711001452005071100145NM 2005 7 11 AWXA200500784 120050630A5321654583311 WEB BOEING737 7373G7 1384595NM GE CFM56 CFM563B1 13802NE COCKPIT FLOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 DURING C-16 CHECK, DISCOVERED FLOOR WEB CRACKED FROM FRAME CUT OUT AT BS 197, WL 207, BL 28R. MAINTENANCE REMOVED THE CRACKED WEB AT BS 197, WL 207, BL 28R IAW MFG 737-300 SRM 51-40-02-0 FIG 8. FABRICATED REPLACEMENT SHEAR TIE WEB IAW MFG DWG 65-45833, SRM 51-40-05-0 FIG 3. INSTALLED FABRICATED REPAIR PARTS IAW SRM 51-40-02-0 FIG 8, 51-40-05-0 FIG 3, AND 51-40-04-0 FIG 1. 2L72 4F4 FRTA16WE E2GL 20050711001462005071100146NM 2005 7 11 AWXA200500785 120050628A53126516300511 BULKHEAD BOEING737 7373G7 1384595NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 DURING C16 CHECK DISCOVERED 178 BULKHEAD WEB CRACKED AT WL 234, BL 12R. MAINTENANCE REPAIRED CRACK AT 178 BULKHEAD BY CUTTING OUT THE DAMAGED AREA IAW MFG SRM 53-10-08-2 FIG 209. FABRICATED DOUBLER AND FILLER IAW MFG SRM 53-10-08-2 FIG 209. INSTALLED FABRICATED REPAIR PARTS IAW SRM 53-10-08-02. 2L72 4F4 FRTA16WE E2GL 20050711001472005071100147NM 2005 7 11 AWXA200500786 120050628A53126516300512 BULKHEAD BOEING737 7373G7 1384595NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 DURING C16 CHECK FOUND BULKHEAD 178 CRACKED 1.5 INCHES IN LENGTH LOCATED AT WL 234, BL 12L. MAINTENANCE REMOVED THE DAMAGED AREA AT BULKHEAD 178, WL 234, BL 12L IAW 53-10-08-1. FABRICATED FILLER AND DOUBLER REPAIR PARTS IAW SRM 53-10-08-1 FIG 209. INSTALLED FABRICATED REPAIR PARTS AT BULKHEAD 178, WL 234, BL 12L IAW SRM 53-10-08-1 FIG. 209. 2L72 4F4 FRTA16WE E2GL 20050711001492005071100149NE 2005 7 11 XNA01244 220050706A7314 TUBE BOEING727 727227 1384078NM PWA JT8 JT8D7B 52053NE FUEL DE-ICING CRACKED A XN0AC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL23793A 20774 654663 ENGINE FIRE WARNING NR 2 ENGINE PERFORMED ALL REQUESTED CHECKLIST RETURN TO AIRPORT AS REQUEST. REMOVED AND REPLACED FUEL DE-ICING CRACKED TUBE ASSY IAW MM 73-14-00. OPS CK OK IAW MM 73-10-00. (ORIG/CLOSED) 2L73 4F4 F A3WE E2EA 20050711001512005071100151EA 2005 7 11 VTZA200500125 120050623A5310601R5211680 DOOR FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27642BR 7356 PASSENGER DOOR FRAME, TOP RADIUS CRACKED AT FORWARD OF DATUM 1 AT FS 338.90. 2L72 4F RTA21EA 20050711001532005071100153CE 2005 7 11 CIEA200500005 120050621A32225082020441 STRUT BEECH 200 B200 1152922CE NLG CORRODED E CIEAK NONE O OTHER ININSP/MAINT 1 NM03203LG7488 2125 BB926 DURING SCHEDULED LG INSP, NLG UPPER STRUT HSG WAS FOUND TO BE CORRODED. CORROSION WAS IN 2 AREAS OF STRUT, NEAR TOP CROSS BRACE. CORROSION IN EXCESS OF 70 PERCENT AROUND STRUT. IT WAS IN SHAPE OF VALLEY, MORE THAN 50 PERCENT OF CORROSION WAS MORE THAN 50 PERCENT OF WAY THROUGH HSG MATERIAL. 20 PERCENT WAS ABOUT 80 PERCENT THROUGH HSG MATERIAL. CORROSION COMPLETELY THROUGH HSG MATERIAL IN 2 PLACES RESULTING IN 2 HOLES APPROX .3750 INCH IN DIA. UPPER HSG DOES NOT RETAIN FLUID. OUTSIDE PAINT ON HSG WAS HOLDING MATERIAL IN PLACE. LWR AREA OF STRUT HSG WAS CORRODED, APPROX 4.5 INCHES ABOVE LWR STRUT BRG AREA. CORROSION COVERED STRUT. DEPTH OF CORROSION WAS 10-30 PERCENT OF DEPTH OF HSG MATERIAL. 1L72 4T A24CE 20050707000012005070700001CE 2005 7 7 DXTA200500798 120050622A2170 COALESCER BAG CESSNA750 750 2076810CE A/C PACK ODOR E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL07916QS 7500116 AFTER DEPARTING KBED AND RAISING THE LANDING GEAR, A STRONG SMELL OF SMOKE WAS SMELLED IN THE COCKPIT. NO SMOKE WAS PRESENT, BUT THE SMELL OF SMOKE CONTINUED UNTIL LANDING BACK AT KBED. RAN BOTH PACKS WITH APU, NR 1 AND 2 ENGINE. NO OIL SMELL NOTED. COCKPIT PACK CONTROLLED AND OPS CHECKED GOOD. CHECKED PACK OIL NO EVIDENCE OF BURNED OIL NOTED. NO LEAKS NOTED. REF CE 750 M/M 21-51. REMOVED AND INSPECTED BOTH COCKPIT AND CABIN WATER SEPERATOR SOCKS AND FOUND THERE TO BE STRONG OIL SMELL COMMING FROM THE COCKPIT WATER SEPERATOR. CLEANED BOTH WATER SEPERATOR SOCKS AND REINSTALLED IAW CE750 MM 21-51-00. 2L72 4J RTT00007WI 20050707000092005070700009NM 2005 7 7 AWXA200500763 120050610A5710112N700912 FITTING BOEING757 7572S7 1384962NM ZONE 600 DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28905AW 23567 DURING C-10 CHECK, FOUND ELONGATED HOLE ON THE RT WING SIDE LOAD DRAG FITTING. MAINTENANCE OVERSIZED THE HOLE IAW AMERICA WEST AIRLINES (AWA) ENGINEERING REPAIR (ER) 19-5704-05175-ES3. FABRICATED BUSHING WITH AN INTERNAL HOLE DIAMETER OF .375 IAW SERVICE BULLETIN 757-54-0035 R2, STEP 14. INSTALLED SIDE LINK AND TENSION CLIP WITH SB 757-54-0035 R2 BOLTS IAW AWA ER 19-5704-05175-ES3. 2L72 4F RTA2NM 20050707000102005070700010NE 2005 7 7 YENA200536 220050702A73208249722010 EEC AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 1 ENGINE UNSERVICEABLE A YENAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION APAPPROACH 1 EA15548JB13258 1868 DURING VISUAL APPROACH EXPERIENCED FAILURE OF ENGINE NR 1. DECLARED EMERGENCY AND LANDED. PFR SHOWING FMU CH A AND B FAULTS. PERFORMED TSM TASKS 73-00-00-810-904 AND 906. ALL WIRING CHECKS GOOD IAW 76-12-00. FOUND EEC AT FAULT. REMOVED AND REPLACED EEC IAW AMM 73-22-34. OPS AND HIGH POWER ASSURANCE R TESTS, GOOD. 2L72 4F4 FRTA28NM E40NE 20050707000132005070700013NM 2005 7 7 DU4R0507001 120050701A5753 SKIN BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE TE FLAP DENTED B DU4RK NONE O OTHER ININSP/MAINT 1 SO15954UA 26739 LT WING IB FWD FLAP LWR SIDE HAS 8 DENTS AT STA. WBL 85 TO 95 AT VARIOUS LOCATIONS. 2L72 4F4 FRTA16WE E2GL 20050707000192005070700019GL 2005 7 7 C2XA05CL056 220050630A7261 CARBON SEAL EMB 145 EMB145XR 3260214SO ALLSN AE300 AE3007A GL NR 1 ENGINE LEAKING A C2XAB EMER. DESCENT BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DEDESCENT 1 SW2711113 145662 CAE312289 THE CREW REPORTED SMOKE IN THE CABIN AT FL 200 FOLLOWED BY A LAV SMOKE WARNING. THEY ALSO REPORTED SMOKE IN THE COCKPIT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE. OPERATIONAL CHECKS WERE GOOD. THE NR 4 CARBON SEAL WAS FOUND DETERIORATED CAUSING OIL TO LEAK BY. 2L72 4F4 FRT TE6CH 20050707000212005070700021NM 2005 7 7 USAA200506004 120050629A5330 SKIN BOEING737 7373B7 1384580NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19511AU 23594 2.25 INCH CRACK FOUND AT 727E, S25R ON SKIN. INSTALLED DOUBLER IAW SRM 53-00-01 FIG. 229. 2L72 4F4 FRTA16WE E2GL 20050707000252005070700025NM 2005 7 7 DU4R0507132 120050630A5330 SKIN BOEING737 737 UTILSYSNM GE CFM56 CFM56* 13802NE FUSELAGE DENTED B DU4RK NONE O OTHER ININSP/MAINT 1 SO15387UA 24662 BS 1024, S-6L-S-7L HAS A DENT WIDTH 1.5 INCH X .070 DEPTH. 2L72 4F4 FRTA16WE E2GL 20050707000282005070700028WP 2005 7 7 MWEA050060 120050627A5310 STRUCTURE DOUG DC9 DC981 3022081WP PWA JT8 JT8D* NE FUSELAGE VIBRATION A MWEAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 GL31804ME 48030 DURING CRUISE PILOT REPORTED A LOUD HUMMING SOUND AND VIBRATION. VISUALLY INSPECTED ALL LANDING GEARS AND WHEEL WELLS, INSPECTED AIRCRAFT FUSELAGE, DOORS,WINGS AND PANELS. PERFORMED ENGINE VIBRATION TEST. NO DEFECTS FOUND. 2L72 4F4 F A6WE E2EA 20050707000372005070700037EA 2005 7 7 VTZA200500128 120050628A3220 LANDING GEAR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE NOSE COLLAPSED A VTZAO OTHER O OTHER TXTAXI/GRND HDL 1 EA27623BR 7192 NOSE LANDING GEAR COLLAPSED AT THE GATE UPON SWITCHING TO GROUND POWER. SPANNER END CAP BACKED OUT, VERY HIGH LEAKAGE IN NEUTRAL WITH PRESSURE TO C.2.- DIODE IN NR 2 SOLENOID SHORTED. 2L72 4F4 FRTA21EA E15NE 20050707000392005070700039NE 2005 7 7 COMA0570074 220050625A72614119TO4PO1 OIL FILTER CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF34* NE RT ENGINE DIRTY A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27668CA2271 10162 RT ENGINE OIL PRESSURE IN AMBER DASHES. REPLACED THE OIL FILTER. 2L72 4F4 FRTA21EA E15NE 20050707000712005070700071 2005 7 7 05FDEA01818 420050706A2562 ANTENNA DOUG MD11 MD11 3023602NM ELT DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25631FE 48454 LT FX EXTERIOR AT STA 1996 ABOVE MED NR 4, FOUND DEACTIVATED ELT TRANSMITTER ANTENNA DELAMINATED. REPAIRED AS PER EA 1-5330-87580. 2L73 4F RTA22WE 20050707000722005070700072NM 2005 7 7 05FDEA01791 120050703A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25619FE 48770 REFERENCE TO EO 1-5510-7-5000 D1 PART 1, LT HAND NR 3L BARREL NUT BORE CORROSION EXCEEDED TO LIMIT. REPAIRED AS PER FEDEX EA 1-5510-83028. 2L73 4F RTA22WE 20050707000732005070700073NM 2005 7 7 05FDEA01792 120050703A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25619FE 48770 REFERENCE EO 1-5510-7-5000 D1 PART 1, RT NR 34R BARREL NUT BORE CORROSION EXCEEDED TO LIMIT. REPAIRED AS PER FEDEX EA 1-5510-83026. 2L73 4F RTA22WE 20050707000752005070700075NM 2005 7 7 05FDEA01794 120050703A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25619FE 48770 REFERENCE EO 1-5510-7-5000 D1 PART 1, RT NR 1R BARREL NUT BORE CORROSION EXCEEDED TO LIMIT. REPAIRED AS PER FEDEX EA 1-5510-83029. 2L73 4F RTA22WE 20050707000992005070700099 2005 7 7 AWXA200500774 420050703A2565D31516313 SLIDE AIRBUS320 A320232 3930326EU L1 DOOR DEFECTIVE A AWXAO OTHER W INADEQUATE Q C TXTAXI/GRND HDL 1 WP28650AW 856 CAPTAIN OPENED THE L1 DOOR WITH THE DOOR ARMED. SLIDE DID NOT DEPLOY. MAINTENANCE REMOVED AND REPLACED THE L1 DOOR SLIDE IAW AMERICA WEST AIRLINES IAW R1C25305. VENDOR OVERHAULED SLIDE IAW CMM 25-60-56. 2L72 4F RTA28NM 20050707001002005070700100NM 2005 7 7 AWXA200500775 120050624A5210140N28254 CABLE BOEING757 7572S7 1384962NM L1 DOOR LOOSE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28905AW 23567 DURING C-10 CHECK THE L1 DOOR EMERGENCY POWER ASSIST CABLE FAILED TRAVEL CHECK. MAINTENANCE ADJUSTED TRAVEL OF L1 EMERGENCY POWER ASSIST CABLE IAW BOEING 757 MM 52-11-32-4. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA2NM 20050707001012005070700101 2005 7 7 AWXA200500776 420050615A2565 GIRT BAR BOEING757 7572S7 1384962NM R1 DOOR OUT OF ADJUST A AWXAK NONE O OTHER ININSP/MAINT 1 WP28905AW 23567 DURING C-10 CHECK THE R1 DOOR GIRT BAR WAS NOT FULLY ENGAGING IN LATCHES ON FLOOR.. MAINTENANCE ADJUSTED R1 GIRT BAR AND LATCHES IAW BOEING 757 MM 52-11-25-5 PAGE 2, STEP F2. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA2NM 20050707001022005070700102 2005 7 7 AWXA200500777 420050615A2565 GIRT BAR BOEING757 7572S7 1384962NM R4 DOOR OUT OF ADJUST A AWXAK NONE O OTHER ININSP/MAINT 1 WP28905AW 23567 DURING C-10 CHECK THE R4 DOOR GIRT BAR WAS NOT FULLY ENGAGING IN LATCHES ON FLOOR. MAINTENANCE ADJUSTED R4 GIRT BAR AND LATCHES IAW BOEING 757 MM 52-11-25-5 PAGE 2, STEP F2. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA2NM 20050707001032005070700103 2005 7 7 AWXA200500778 420050615A2565 GIRT BAR BOEING757 7572S7 1384962NM L4 DOOR OUT OF ADJUST A AWXAK NONE O OTHER ININSP/MAINT 1 WP28905AW 23567 DURING C-10 CHECK THE L4 DOOR GIRT BAR WAS NOT PROPERLY ENGAGING LATCHES ON FLOOR. MAINTENANCE ADJUSTED L4 GIRT BAR AND LATCHES IAW BOEING 757 MM 52-11-25-5 PAGE 2, STEP F2. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA2NM 20050707001092005070700109NM 2005 7 7 AALA20050409 120050625A3350D71702001 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21798AN 30797 NRT - EMERGENCY ESCAPE PATH LIGHTS IN FIRST CLASS GALLEY AND PARTITION INOPERATIVE. REPLACED BATTERY PACK M33093 AT DOOR 1L CEILING FOR EMERGENCY ESCAPE PATH LIGHTS IN FIRST CLASS GALLEY AND PARTITION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20050707001222005070700122WP 2005 7 7 0500959996 120050623A7711611425 TUBE DOUG DC9 DC931 3022065WP LEFT ENGINE FAILED A NWAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL018932E 47141 DURING THE TAKEOFF ROLL, THE NR 1 ENGINE EPR INDICATION ROLLED BACK. THE TAKEOFF WAS ABORTED AT 120KTS. MAINTENANCE FOUND A FAILED TUBE IN THE PT7 MANIFOLD. THE TUBE WAS REPLACED AND THE LEAK CHECK WAS GOOD. 2L72 4F A6WE 20050707001232005070700123WP 2005 7 7 0500969918 120050627A5311 FRAME DOUG DC9 DC932 3022066WP FUSLEAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01940N 45772 DURING M-CHECK FOUND CRACKED FRAME AT VENTRAL STAIR CUTOUT BS 1087. REPAIRED PER EA 99-203533. 2L72 4F A6WE 20050708000292005070800029NM 2005 7 8 SWAA051924 120050704A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29332SW 23696 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 24R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050708000432005070800043 2005 7 8 SWAA051927 420050702A25651061323468 SLIDE BOEING737 7373H4 1384600NM L1 DOOR DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29378SW 26585 L1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATING LOW. REMOVED AND REPLACED SLIDES PER MM. 2L72 4F RTA16WE 20050708000482005070800048NM 2005 7 8 SWAA051932 120050704A53306545774 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29509SW 24186 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 23L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050708000542005070800054NM 2005 7 8 SWAA051938 120050704A53306545775 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 781, STR 18L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050708000552005070800055NM 2005 7 8 SWAA051939 120050704A53306545775 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 810, STR 25L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050708000572005070800057NM 2005 7 8 ASAA0540249 120050513A53106552490118 BEAM BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02792AS 28887 RT VERT T/E BEAM CRACKED AT STA 13.33. REMOVED AND REPLACED. (K) 2L72 4F4 FRTA16WE E21EU 20050708000582005070800058NM 2005 7 8 ASAA0540252 120050518A531165465811 FRAME BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02792AS 28887 FRAME CRACKED AT HAT RACK ATTACH POINT. REPAIRED CRACKED FRAME AT HAT RACK ATTACH POINT. (K) 2L72 4F4 FRTA16WE E21EU 20050708000702005070800070NM 2005 7 8 ASAA0540254 120050518A5347654659222 CARGO TRACK BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02792AS 28887 CORROSION AFT CARGO BAY, TIE DOWN ON FLOOR TRACK. REMOVED DAMAGE AND INSTALLED NEW TRACK IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050708000802005070800080NM 2005 7 8 ASAA0540267 120050526A5730 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU RT WING TE FLAP DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02776AS 25109 RT WING OB AFT FLAP DELAMINATED AT IB TRAILING EDGE. REMOVED DAMAGED MATERIAL, INSTALLED CORE, SKIN, AND DOUBLER IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050708000832005070800083NM 2005 7 8 ASAA0540250 120050513A5330654576921 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02783AS 25114 TWO DENTS AND GOUGES AT STA 480-500 +12 STRINGER 26R. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW AS EA 533001932 AND AAR EA 10944. (K) 2L72 4F4 FRTA16WE E21EU 20050708000852005070800085NM 2005 7 8 ASAA0540264 120050525A5754 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU NR 5 SLAT CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02776AS 25109 NR 5 SLAT IB TRAILING EDGE CHAFED. REMOVED DAMAGE, BONDED FILLER SKIN AND DOUBLER IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050708000882005070800088NM 2005 7 8 ASAA0540275 120050529A53106552870504 FITTING BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU CARGO DOOR FRAMECORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02792AS 28887 CORROSION ON LT AFT ENTRY DOOR CUTOUT IB FWD SIDE OF CUTOUT JUST AFT OF UPPER FWD LATCH FITTING. REMOVED AND REPLACED FITTING. (K) 2L72 4F4 FRTA16WE E21EU 20050708000892005070800089NM 2005 7 8 ASAA0540277 120050530A573065C2520415 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU LT WING GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02776AS 25109 LT WING UPPER SKIN GOUGED AT WING STA 223 BETWEEN STA 12 AND 13. BLENDED AREA, TREATED AND PRIMED IAW EA. (K) 2L72 4F4 FRTA16WE E21EU 20050711001592005071100159EU 2005 7 11 AALA20050423 120050703A2910A2793161500400 LINE AIRBUS300 A300B4605R 3930308EU GE CF6 CF680C2A5 NE HYD SYSTEM LEAKING A AALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW2111060 470 YELLOW SYSTEM HYDRAULIC QUANTITY LOST ON CLIMB-OUT. FOUND HYDRAULIC LINE IN LT WHEEL WELL LEAKING. REPLACED HYDRAULIC LINE IN LT WHEEL WELL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA35EU E13NE 20050711001612005071100161NM 2005 7 11 AALA20050419 120050627A521060B1000316 BOTTLE BOEING757 757223 1384957NM RROYCERB211 RB211535E4B3 NE L1 DOOR DISCHARGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21687AA 25695 LT NR 1 DOOR BOTTLE HAS ZERO PRESSURE. CHANGED THE BOTTLE AND CHECKED FOR LEAKS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA2NM E12EU 20050711001632005071100163WP 2005 7 11 AALA20050421 120050704A3350 SOCKET DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21973TW 53623 EMERGENCY LIGHT AT SEAT 18D INOPERATIVE. REPLACED EMERGENCY LIGHT SOCKET FOR EMERGENCY LIGHT AT SEAT 18D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA6WE E9NE 20050711001652005071100165WP 2005 7 11 AALA20050420 120050702A3320 BALLAST DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE SIGN BURNED A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW217536A 49990 APPROXIMATELY 20 MINUTES AIRBORNE, DEVELOPED SMOKE AND FUMES IN CABIN. SMOKE COULD BE SMELLED IN COCKPIT. FLIGHT ATTENDANTS REPORTED SEAT 22 DEF FASTEN SEAT BELTS SIGNS FLICKER WHEN PAUSED FROM COCKPIT OR CABIN. FUMES AND SMOKE SEEMED TO BE FROM AREA OF SEAT 22DEF. FOUND CEILING LIGHT BALLAST BURNED AT MID CABIN AREA. REPLACED OVERHEAD LIGHT BALLAST AND COALESCER BAGS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 F A6WE E9NE 20050711001732005071100173SO 2005 7 11 C2XA05SH063 120050705A532014521700007 FLOOR SUPPORT EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716961 145103 DURING C-CHECK MAINTENANCE FOUND LT OMEGA BEAM REPAIR WITH CORROSION AT FRAME 20. MAINTENANCE REPAIRED LT OMEGA BEAM AT FRAME 20 IAW SRM 53-21-10 AND EC 5320-01137. AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20050711001762005071100176 2005 7 11 SA05081 420050628A2565 SLIDE AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE L1 DOOR UNSECURE A USAAK NONE O OTHER ININSP/MAINT 1 EA19122US 1298 THE L1 DOOR SLIDE BECAME PARTIALLY UNSTOWED DURING THE CLOSING OF THE DOOR. MAINTENANCE REMOVED AND THEN INSTALLED THE SAME GIRT BAR. OPERATIONAL CHECKS NORMAL. 2L72 4F4 FRTA28NM E38NE 20050711001782005071100178NM 2005 7 11 BB05048 120050628A5350141N782012P RADOME BOEING757 757225 1384959NM NOSE COLLAPSED A USAAO OTHER O OTHER DEDESCENT 1 EA19603AU132742957 22198 DURING DESCENT, THE CREW HEARD A POP SOUND. AT THE SAME TIME, THE WEATHER RADAR WENT OUT OF SERVICE. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RADOME WHICH HAD COLLAPSED AND OPERATIONALLY CHECKED THE WEATHER RADAR SYSTEM. OPERATIONALLY CHECKS OK. 2L72 4F RTA2NM 20050711001792005071100179 2005 7 11 AT0500020 420050703A2565D29982225 SLIDE BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE R1 DOOR DEPLOYED A ZZDAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO15942AT 55005 R1 DOOR SLIDE DEPLOYED BY GROUND PERSONNEL. REMOVED AND REPLACED R-1 DOOR SLIDE. 2L72 4F4 FTRA6WE E00061EN 20050711001802005071100180WP 2005 7 11 05FDEA01687 120050625A2750 WARNING LIGHT DOUG MD10 MD1010F 3022112WP TE FLAPS FALSE INDICATIONA FDEAL ABORTED APPROACH JN WARNING INDICATION FALSE WARNING APAPPROACH 1 SO2568057 48264 ON APPROACH, GOING FROM FLAPS 22 TO FLAPS 35, GOT LEVEL 2 ALERT SLATS DISAGREE. AFTER GO AROUND, FOUND SLAT HANDLE SCREW LOOSE. EXTENDED FLAPS AND SLATS. VISUAL INSPECTION OF FLAPS AND SLATS BOTH SIDES. NO DEFECTS FOUND. RAN FLAPS AND SLATS SEVERAL TIMES AND COULD NOT DUPLICATE FAULT. TEST FLAP POSITION IND PER MM NR 27-50-00-5 PAR F. C/W RETURN TO SERVICE ON THE FCC NR 1 AND NR 2. ALL TEST PASSED. NO FAULTS FOUND ON BOTH FCC FAULT REVIEW. 2L73 4F RTA22WE 20050711001822005071100182EA 2005 7 11 SWIA200515167 120050616A2740 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB CONTROL SYSMALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CLCLIMB 1 NM07925SW 7682 DURING CLIMB, RECEIVED STAB TRIM AND MACH TRIM CAUTION MESSAGES. REPLACED F/O'S TRIM SWITCH IAW MM 27-41-07. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050711001842005071100184SO 2005 7 11 SWIA200515169 120050615A5210 DOOR EMB 120 EMB120ER 3260203SO MAIN CABIN LACK OF LUBE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07217SW 120286 MAIN CABIN DOOR HARD TO OPEN AND CLOSE. LUBRICATED CABIN DOOR LINKAGE. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050711001872005071100187EA 2005 7 11 SWIA200515172 120050620A2751855D10011 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CLCLIMB 1 NM07448SW 7678 AFTER TAKEOFF, FLAPS FAILED AT 8 DEGREES WITH FLAP FAIL MSG. REPLACED RT BPSU IAW CRJ MM 27-51-10. 2L72 4F RTA21EA 20050711001882005071100188SO 2005 7 11 SWIA200515173 120050620A3350 BULB EMB 120 EMB120ER 3260203SO EMERGENCY LIGHTSBURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07235SW 120310 EMERGENCY EXIT LIGHT ROW 6 INOPERATIVE. REPLACED BULB ON EMERGENCY LIGHT AT 6A. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050711001892005071100189EA 2005 7 11 SWIA200515174 120050617A27507455001 CONTROL HANDLE CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION APAPPROACH 1 NM07595SW7010 7010 7292 ON APPROACH, FLAPS FAILED AT 20 DEGREES. REPLACED FLAP CONTROL HANDLE IAW CL 600 MM 27-51-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050711001912005071100191NM 2005 7 11 ASAA0590024 120050328A5320146A750348 ANGLE BOEING737 737990 NM GE CFM56 CFM567B24 NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02307AS 30015 DURING C-CHECK, FOUND CORROSION ON FLOOR SUPPORT SPLICE ANGLE AT BS7271+6 AND LBL12. REPAIRED IAW SRM. (K) 2L74 4F4 FRTA16WE E00055EN 20050711001942005071100194NM 2005 7 11 ASAA0590025 120050328A5320146A750352 FLOOR SUPPORT BOEING737 737990 NM GE CFM56 CFM567B24 NE FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02307AS 30015 DURING C-CHECK, FOUND BENT ON FLOOR SUPPORT AT BS 767 AND RBL 7.5. REPAIRED IAW SRM. (K) 2L74 4F4 FRTA16WE E00055EN 20050711001982005071100198NM 2005 7 11 ASAA0590021 120050328A5320143A751012 INTERCOSTAL BOEING737 737990 NM GE CFM56 CFM567B24 NE FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02307AS 30015 DURING C-CHECK, FOUND DAMAGE INTERCOSTAL AT BS 500A-500B. REPAIRED IAW SRM. (K) 2L74 4F4 FRTA16WE E00055EN 20050711002002005071100200EA 2005 7 11 SWIA200515176 120050614A5320 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07709BR 7850 FS 280 RT FLOOR BEAM RBL 9.0 OUTBOARD ATTACH ANGLE CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13, 51-23-00. 2L72 4F RTA21EA 20050711002022005071100202NM 2005 7 11 05FDEA01649 120050622A5320 INTERCOSTAL BOEING727 727233 138408ANM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25264FE 21626 INTERCOSTAL CRACKED STA 358, STR 16 LT. REPAIRED INTERCOSTAL PER SRM 51-40-2. 2L73 4F RTA3WE 20050711002042005071100204SW 2005 7 11 AC2A100887 120050512A3246FT245172 COVER BELL 427 427 1182207SW LANDING GEAR CRACKED B AC2AK NONE O OTHER ININSP/MAINT 1 SO07427CK428 56043 CRACKED, FITTING ON R/H AFT FLOAT WAS AT AN INCORRECT ANGLE FROM THE FACTORY CAUSING THE LINE TO PUSH AGAINST THE COVER./ REPLACED THE COVER AND REPOSITIONED THE FITTING. 1G71 3U R00001RC 20050711002082005071100208NM 2005 7 11 05FDEA01664 120050623A5315 FLOORBEAM BOEING727 727233 138408ANM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25264FE 21626 CORROSION ON FLOORBEAM LBL 10, BS 560. REPAIRED PER SRM 53-10-8. 2L73 4F RTA3WE 20050711002092005071100209NM 2005 7 11 05FDEA01666 120050623A534760654724 SEAT TRACK BOEING727 727233 138408ANM MAIN CABIN CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25272FE 22037 SEAT TRACK LBL 24 HAS CORROSION FROM STA 344-480. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2. 2L73 4F RTA3WE 20050711002102005071100210NM 2005 7 11 05FDEA01667 120050623A334066172074 STRAP BOEING727 7272S2F 1384O81NM RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25203FE 22925 RT WING LANDING LIGHT RETENSION STRAP CRACKED ON BACK OF NR 6 K-FLAP. REMOVED AND REPLACED RETENSION STRAP IAW SRM 51-30-2. 2L73 4F A3WE 20050711002112005071100211NM 2005 7 11 05FDEA01692 120050626A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25619FE 48770 WITH REFERENCE TO WORK CARD E1-5510-7-5000, LT BARREL NUT HOLE NR 33L FOUND OUT OF LIMIT AFTER CORROSION REMOVAL. REPAIR CARRIED OUT AS PER FEDEX EA 1-5510-83022 2L73 4F RTA22WE 20050711002122005071100212NM 2005 7 11 05FDEA01693 120050626A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25619FE 48770 WITH REFERENCE TO WORK CARD E1-5510-7-5000, LT BARREL NUT HOLE NR 35L FOUND OUT OF LIMIT AFTER CORROSION REMOVAL. REPAIR CARRIED OUT AS PER FEDEX EA 1-5510-83022 2L73 4F RTA22WE 20050711002132005071100213NM 2005 7 11 05FDEA01650 120050622A53206519606350 SHEAR WEB BOEING727 7272S2F 1384O81NM MAIN DECK CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25203FE 22925 MAIN DECK SHEAR WEB BTWN 1164 TO 1183, RBL 18 TO 65 IS CORRODED. REMOVED AND REPLACED L-CHANNEL IAW SRM 51-30-2. 2L73 4F A3WE 20050711002152005071100215EU 2005 7 11 MALA050505 120050623A2432 BATTERY SAAB SF340 340B 7860101EU DC GEN SYS DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15426XJ 340B426 BATTERY FAILED CAP CHECK, 2L72 4T RTA52EU 20050711002162005071100216EU 2005 7 11 MALA050504 120050623A2432 BATTERY SAAB SF340 340B 7860101EU DC GEN SYS DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15426XJ 340B426 BATTERY FAILED CAP CHECK, 2L72 4T RTA52EU 20050711002172005071100217NM 2005 7 11 05FDEA01694 120050626A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25619FE 48770 WITH REFERENCE TO WORK CARD E1-5510-7-5000, LT BARREL NUT HOLE NR 1L FOUND OUT OF LIMIT AFTER CORROSION REMOVAL. REPAIR CARRIED OUT ON LT HORIZONTAL STABILIZER, LT BARREL NUT HOLE NR 1 AS PER FEDEX EA 1-5510-83020. 2L73 4F RTA22WE 20050711002192005071100219NM 2005 7 11 05FDEA01696 120050626A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25619FE 48770 WITH REFERENCE TO WORK CARD E1-5510-7-5000, REQUIRE TO TRIM LT OPERATING BULKHEAD FOR NR 35L BARREL NUT REWORK ACCESS. TRIMMED OUT AS PER SRM 51-31-01 VOL. II AND FOUND EXCEEDED LIMIT AS PER FEDEX EO 1-5510-7-5000. REPAIR CARRIED OUT ON TRIMMED AREA AT LT OPERATING BULKHEAD AS PER FEDEX EA 1-5510-87552 2L73 4F RTA22WE 20050711002222005071100222 2005 7 11 DXTA200500783 420050617A2211701730031444 COMPUTER CESSNA750 750 2076810CE AUTOPILOT MALFUNCTIONED E DXTAO OTHER G MULTIPLE FAILURE CRCRUISE 1 GL07971QS 1670 7500071 NR 1 IAC FAILED IN FLIGHT, DU 1, 2, 3, RED X THROUGH SCREENS, NR 1 FMS INOP, NR 1 RMU STILL WORKS, NO HEADING BUG OR ALTITUDE SETTING CAPABILITY EITHER. REMOVED AND REPLACED HONEYWELL PRIMUS 2000 IC800 WITH A REPAIRED UNIT FROM HONEYWELL NR LV2R992K S/N ON : 96070577 IAW CESSNA 750 M/M 34-25-01. FUNCTION CHECKED SYSTEM IAW CESSNA 750 M/M 23-80-01. CHECKS GOOD. 2L72 4J RTT00007WI 20050711002232005071100223NM 2005 7 11 UPS05544723 120050621A3350 LIGHT BOEING757 75724APF 1384969NM EMERGENCY LIGHTSINTERMITTENT A IPXAK NONE O OTHER ININSP/MAINT 1 SO01437UP 25468 EMERGENCY EXIT LIGHT OVER DOOR BLINKS ON AND OFF WITH SWITCH IN ARMED POSITION. OPERATED EMERGENCY LIGHT SWITCH SEVERAL TIMES. COULD NOT DUPLICATE. 2L72 4F RTA2NM 20050711002242005071100224NM 2005 7 11 UPS05M44720 120050622A3350 LIGHT DOUG MD11 MD11F 3023600NM R1 DOOR SLIDE INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01271UP 48572 R1 DOOR EVAC SLIDE PRESS TO RESET LT INOPERATIVE. RELAMPED AND TESTED SYSTEM PER MM 25-61-04-1. SYS CHECK NORMAL. PLACARD REMOVED. 2L73 4F RTA22WE 20050711002272005071100227NM 2005 7 11 05FDEA01648 120050622A5330 SKIN BOEING727 727233 138408ANM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25263FE 21625 FUSELAGE EXTERNAL SKIN GOUGED AT AFT AIRSTAIR CUTOUT, BS 1230, LBL 20. REPAIRED SKIN AT AFT AIR STAIR CUTOUT BS 1230, LBL 20 PER SRM 53-30-3. 2L73 4F RTA3WE 20050711002302005071100230WP 2005 7 11 0500929915 120050620A2130 PRESSURE SYSTEM DOUG DC9 DC931 3022065WP CABIN MALFUNCTIONED A NWAAIA CABIN DEPRESSURIZATION UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL01965N 47417 LEVEL AT FL 340, FLIGHT WAS DIVERTED DUE TO WEATHER. RED MASTER WARNING AND CABIN PRESS LIGHTS ILLUMINATED AS CABIN ALTITUDE CLIMBING THROUGH 10,000 FT. COM PROCEDURES COMPLIED WITH BUT DID NOT HELP. CREW INITIATED RAPID DESCENT AND DECLARED EMERGENCY. CABIN NEVER WENT ABOVE 11,000 FT AND O2 MASKS DID NOT DEPLOY. FLIGHT LANDED UN-PRESSURIZED BUT WITHOUT INCIDENT. CONTRACT MAINTENANCE COULD NOT DUPLICATE PROBLEM, APPLIED MEL 21-24B, AND RENDER PRESSURIZATION INOPERATIVE. AIRCRAFT RETURNED TO REVENUE SERVICE AND FLEW BACK UN-PRESSURISED AT 9000 FT. 2L72 4F A6WE 20050711002312005071100231NM 2005 7 11 05FDEA01700 120050627A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25619FE 48770 WITH REFERENCE TO EO1-5510-7-5000 PART 1, RT NR 5R BORE CORROSION FOUND EXCEEDED LIMIT. REPAIRED AS PER FEDEX EA 1-5510-83023. 2L73 4F RTA22WE 20050711002342005071100234NM 2005 7 11 05FDEA01675 120050624A7830 TRACK DOUG MD11 MD11 3023602NM THRUST REVERSER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25619FE 48770 NR 2 ENGINE, RT THRUST REVERSER UPPER SLIDE TRACK CRACKED. REMOVED AND REPLACED AS PER WORK CARD 78T3002-R AND WORK CARD 78T3902-R. ADJUSTMENT AND OPERATIONAL CHECK CARRIED OUT AS PER WORK CARD 78T3902-R, GE NR 2 RIGHT THRUST REVERSER DOOR - INSTALL. 2L73 4F RTA22WE 20050711002352005071100235NM 2005 7 11 05FDEA01460 120050525A5315 FLOORBEAM BOEING727 727227 1384078NM FUSELAGE MISDRILLED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 UPPER LOBE INTERIOR, STA 520, RBL 43, TOP OF FLOORBEAM HAS DOUBLE DRILLED HOLES. REPAIRED BS 520 UPPER CHORD PER FED-EX EA 7-5310-86321. 2L73 4F A3WE 20050711002442005071100244SO 2005 7 11 CHQA200500124 120050626A2611 SMOKE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL CABIN DETECTED A CHQAA UNSCHED LANDING JB WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL11574RP 14500845 ON INITIAL CLIMB AT APPROX 500 AGL, RECEIVED LAV SMOKE WARNING EICAS. SMOKE ODOR IN COCKPIT, SMOKE NOT VISIBLE. SMOKE MASKS DONNED AND EMERGENCY RETURN TO FIELD INITIATED. F/A REPORTED CLOUD OF SMOKE MOVING THROUGH CABIN. CABIN BRIEFED FOR PRECAUTIONARY EVACUATION AFTER LANDING. NO VISIBLE FIRE OR SMOKE AFTER INITIAL CLOUD. MX RAN ENGINES WITH NO PROBLEMS NOTED. BLEED DUCTS WERE INSPECTED FOR EVIDENCE OF OIL. NO EVIDENCE NOTED IN INLET OR TAILPIPE. UNABLE TO FIND ANY DEFECTS. A/C WAS TEST FLOWN WITH NO LAV SMOKE MESSAGES OR SMOKE ODOR NOTED. OPS CHECK GOOD. ENGINE SERIAL NUMBERS CAE312670 AND CAE312675. 2L72 4T4 FRTT00011ATTE6CH 20050711002462005071100246NM 2005 7 11 UPS05244726 120050611A783006453010059 SUPPORT BRACKET BOEING727 72731C 1384011NM THRUST REVERSER CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 ENG NR 1 THRUST REVERSER O/B FAIRING MID SUPPORT BRACKET CRACKED. BRACKET REPLACED IAW SRM 51-30-2. 2L73 4F A3WE 20050711002482005071100248NM 2005 7 11 UPS05244728 120050614A5420 STRUCTURE BOEING727 72731C 1384011NM NR 1 NACELLE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 ENG NR 1 FWD MOUNT BOTH O/B HOLES HAVE PITTING CORROSION ON REPAIR BUSHINGS. BUSHINGS REPLACED IAW UPS EO B727-5440-11592-A. 2L73 4F A3WE 20050711002492005071100249NM 2005 7 11 UPS05244729 120050614A5420 BUSHING BOEING727 72731C 1384011NM NR 3 NACELLE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 ENGINE NR 3 FWD MOUNT AFT O/B HOLE REPAIR BUSHING DAMAGED. BUSHING REPLACED IAW UPS EO B727-5440-11592-A. 2L73 4F A3WE 20050711002532005071100253NM 2005 7 11 UPS05544734 120050625A2560 SMOKE GOGGLES BOEING757 75724APF 1384969NM COCKPIT BROKEN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01437UP 25468 1ST SUPERNUMERARY SMOKE GOGGLES LENS BROKEN. REMOVED AND REPLACED 1ST SUPERNUMERARY SMOKE GOGGLES. 2L72 4F RTA2NM 20050711002542005071100254SO 2005 7 11 RAIA00506028 120050625A32608005701 PROXIMITY SWITCH EMB 145 EMB145ER 3260211SO LG INOPERATIVE A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03808HK 145157 AIR/GND FAIL MESSAGE ON EICAS. MAINTENANCE REMOVED AND REPLACED THE NR 1 AFT WOW SWITCH. OPS CHECKED GOOD. 2L72 4F RTT00011AT 20050711002552005071100255SO 2005 7 11 SWIA200515177 120050404A5320 INTERCOSTAL EMB 120 EMB120ER 3260203SO FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07393SW 120330 CLIP CRACKED AT FRAME 12A JUST AFT LT DV WINDOW, ITEM FOUND AT C-CHECK INSPECTION. REPLACED INTERCOSTAL AT FRAME 12A AFT OF PILOT'S DV WINDOW PER EMB120 SRM 51-40-02. 2L72 4T RTA31SO 20050711002602005071100260EA 2005 7 11 SWIA200515182 120050622A2760C13045BA03 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07706SK1955 1955 10149 SPOILER/STAB FAULT STATUS MSG. REPLACED NR 2 SSCU IAW CRJ MM 27-61-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050711002622005071100262EA 2005 7 11 SWIA200515184 120050625A3350 BULB CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHTSBURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07710SK 10170 EMERGENCY LIGHT NEXT TO SERVICE DOOR HAS SOME BULBS BURNED OUT. RELAMPED EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050711002632005071100263EA 2005 7 11 SWIA200515185 120050623A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSINOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07588SW 7069 2ND OVERHEAD EMERGENCY LIGHT IS INOPERATIVE. REPLACED LAMP. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050712000472005071200047 2005 7 12 SWAA051965 420050707A25656557463 FITTING BOEING737 7373H4 1384600NM L1 DOOR SLIDE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED D-CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD & AFT GIRT BAR FLOOR FITTINGS CORRODED. REMOVED AND REPLACED FITTINGS PER MM. 2L72 4F RTA16WE 20050712000482005071200048NM 2005 7 12 SWAA051966 120050707A53106545834 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED D-CHECK, FOUND CORROSION ON CREASE BEAM WEB AT BS 312, RBL 60. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM. 2L72 4F RTA16WE 20050712000512005071200051NM 2005 7 12 SWAA051969 120050707A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 767, STR 25L TO STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050712000542005071200054NM 2005 7 12 SWAA051972 120050707A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 870, STR 26R. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20050712000552005071200055NM 2005 7 12 SWAA051973 120050707A53116546558 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 907, STR 27L TO STR 27R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050712000572005071200057NM 2005 7 12 SWAA051975 120050707A52306545871 FRAME BOEING737 7373H4 1384600NM AFT CARGO DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29324SW 23414 DURING SCHEDULED C1 CHECK, FOUND AFT CARGO DOOR LOWER STOP FITTING CUTOUT CRACKED. REMOVED AND REPLACED AFT CARGO DOOR PER MM. 2L72 4F RTA16WE 20050712000592005071200059NM 2005 7 12 SWAA051977 120050707A3350207377 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29442WN 32459 EEPLS TRACK LENS LOOSE AT ROW 14. SECURED LENS PER MM. 2L72 4F RTA16WE 20050712000732005071200073 2005 7 12 SWAA051961 420050706A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29442WN 32459 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050712000762005071200076 2005 7 12 SWAA051964 420050706A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29749SW 29801 L1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATING LOW. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20050712000772005071200077NM 2005 7 12 SWAA051946 120050705A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 1010, STR 7L. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2L72 4F RTA16WE 20050712000782005071200078NM 2005 7 12 SWAA051947 120050705A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727D, STR 6L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050712000812005071200081 2005 7 12 AWXA200500736 420050616A2565D31041146 SLIDE BOEING757 7572S7 1384962NM L3 DOOR BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28905AW200941428 23567 DURING C-10 CHECK, FOUND MAIN CABIN L-3 DOOR SLIDE UPPER END TANGS BROKEN. MAINTENANCE REMOVED AND REPLACED L-3 DOOR SLIDE IAW BOEING 757 MM 25-66-03-4. 2L72 4F RTA2NM 20050712000822005071200082NM 2005 7 12 ASMF200506024 120050624A3241426071 CONTROL BOX DOUG MD88 MD88 3023688NM ANTI SKID SYS FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23169PL6951 53175 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF RIGHT INBOARD ANTISKID LIGHT TURNED ON. AT PLATFORM, BITE TO ANTISKID CONTROL BOX WAS PERFORMED DETECTING FAILURE IN THE RIGHT INTERIOR DOUBLE SERVO VALVE. VALVE WAS REPLACED IAW MM 32-43-04, TESTED CORRECT. 2L72 4F RTA6WE 20050712000832005071200083NM 2005 7 12 SWAA051979 120050707A53306545777 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 957, STR 21L. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050712000882005071200088NE 2005 7 12 AWXA200500745 220050625A7321FFG022AC FUEL CONTROL BOEING757 757225 1384959NM RROYCERB211 RB211535E4 54555NE NR 1 ENGINE MALFUNCTIONED A AWXAO OTHER O OTHER TXTAXI/GRND HDL 1 WP28914AW381032009 22208 DURING ENGINE SHUTDOWN, AT GATE, NR 1 ENGINE CONTINUED TO OPERATE FOR 20 SECONDS AFTER PLACING FUEL CONTROL TO SHUTOFF POSITION. MAINTENANCE REMOVED AND REPLACED NR 1 FUEL FLOW GOVERNOR IAW AMERICA WEST AIRLINES (AWA) TASK CARD R5M73603 AND AWA TASK CARD F5M73601. OPERATIONAL CHECKS WERE GOOD. VENDOR REPORT REVEALS THE PRECISION SWITCH TO BE INOPERATIVE AND BEARING INOPERATIVE. UNIT WAS OVERHAULED IAW CMM 73-21-02 REV. 5 2L72 4F4 FRTA2NM E12EU 20050712000892005071200089EU 2005 7 12 YENA200534 120050622A2120 ODOR AIRBUS320 A320232 3930326EU CABIN DETECTED A YENAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15593JB 2280 IN CRUISE, F/A'S REPORTED AN ELECTRICAL ODOR IN ROW 26 O/H COMPT LEVEL. SHUT OFF AFT AVIONICS COMPT RACK POWER AND ODOR WENT AWAY. LATER F/A'S REPORTED ODOR AGAIN, CORRELATED ODOR WITH FLUSHING OF LAV-E. CONTINUED WITH LAV-E BLOCKED & RACK POWER OFF, NO FURTHER ODORS REPORTED. SPOKE TO C/P & INFLIGHT CREW VERIFIED ODOR AROUND ROW 26, TURNED L/TV OFF AND ODOR CAME BACK WHEN LAV-E FLUSHED. CONFIRMED THAT NO ODOR NOTICED BY PASSENGER INSIDE OR OUTSIDE LAV. INSPECTED LTV, ACCOMPLISHED INFO NOTICE 2004-T023TR, NO FAULTS FOUND, LTV OPS CHECK NORMAL. INSPECTED O/H LIGHTS AND CEILING AREA, LAV E FLUSH MOTOR/ VALVE, GALLEY EQUIPMENT, NO DEFECT OR SMELL NOTED PER TSM AND INFO NOTICE A/C OK FOR SERVICE. 2L72 4F RTA28NM 20050712000902005071200090NM 2005 7 12 SWAA051980 120050707A323365448105 ACTUATOR BOEING737 7373A4 1384585NM RT MLG WW FAULTY A SWAAO OTHER J WARNING INDICATION CLCLIMB 1 SW29680AA 23505 RIGHT MLG EXTENDED AFTER SUCCESSFUL RETRACTION. GEAR HANDLE RECYCLED & RIGHT GEAR REMAINED IN RETRACT POSITION. REMOVED AND REPLACED RIGHT MLG UPLOCK ACTUATOR PER MM. 2L72 4F RTA16WE 20050712000912005071200091NM 2005 7 12 SWAA051981 120050707A3350101114 COVER BOEING737 7377H4 1384404NM EMERGENCY EXIT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29771SA 27879 MID CABIN EMERGENCY EXIT SIGN COVER MISSING. INSTALLED COVER PER MM. 2L72 4F RTA16WE 20050712000922005071200092NM 2005 7 12 SWAA051982 120050707A53156546804 FLOORBEAM BOEING737 7377H4 1384404NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29779SW 27884 DURING SCHEDULED 5Y CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 767, BETWEEN LBL 12.0 TO RBL 7.5. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20050712000932005071200093NM 2005 7 12 SWAA051989 120050710A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29404WN 27892 CABIN EEPLS TRACK COVER LOOSE. SECURED COVER PER MM. 2L72 4F RTA16WE 20050712000962005071200096NM 2005 7 12 SWAA051992 120050710A53306545776 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29501SW 24178 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 944, STR 25R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050712000992005071200099NM 2005 7 12 SWAA051998 120050708A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29608SW 27928 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 559, STR 11R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050712001012005071200101NM 2005 7 12 SWAA052001 120050708A53116546524 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29608SW 27928 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050712001022005071200102NM 2005 7 12 SWAA052002 120050708A53156546811 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29608SW 27928 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, RBL 35 TO RBL 39, WL 208. REPAIRED FLOORBEAM PER BFG ER. 2L72 4F RTA16WE 20050707000852005070700085NM 2005 7 7 05FDEA01813 120050705A5320 STIFFENER DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 OVERWING EXTERIOR STIFFENER FOR UPPER AUX TANK FOUND CORRODED AT STA 1345 RBL 98 AS MARKED. REMOVED AND INSTALLED AS PER SRM 52-57-12. 2L73 4F RTA22WE 20050707000892005070700089NM 2005 7 7 05FDEA01789 120050703A5320 FLOOR SUPPORT DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 FLOOR SUPPORT FOUND CRACKED AT STA 5-11 AT RBL 69 AS MARKED. CORRECTIVE ACTION: SNRM N1342: DISPREPANT FLOOR SUPPORT REMOVED AS PER SRM 51-31-01 VOL II. NEW FLOOR SUPPORT REWORKED FROM S2932222T12000 AS PER DRAWING ACA 3762 AND INSTALLLED AS PER SRM 51-31-01 VOL II. CLASSIFIED MINOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050707000922005070700092NM 2005 7 7 05FDEA01788 120050703A5320 FLOOR SUPPORT DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 BELOW FLOOR PANEL 271CF AT STA 1401 LBL 36.5 FLOOR SUPPORT STRUCTURE FOUND CRACKED. REMOVED AS PER SRM 51-31-01 VOL II. NEW FLOOR SUPPORT REWORKED FROM S2932222T12000 AS DRAWING ACA 3762 AND INSTALLED AS PER SRM 51-31- 01 VOL II. CLASSIFIED MINOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050707000952005070700095NM 2005 7 7 05FDEA01781 120050703A5313 LONGERON DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 CENTER CARGO BAY RT STA 1531 LONGERON 47 FOUND WITH HAIR LINE CRACK AS MARKED. 47 REMOVED IAW SRM 51-33-01 VOL.II. NEW LONGERON FABRICATED AS PER DWG AFA 0618 AND NEW SPLICE REPAIR FABRICATED IAW SRM 53-10-00 FIG.2 VOL I. NEW LONGERON AND NEW SPLICE REPAIR INSTALLED IAW SRM 51-33-01 VOL II. MAJOR REPAIR PER GMM 6-2-100. 2L73 4F RTA22WE 20050707001122005070700112EU 2005 7 7 AALA20050413 120050626A3350P4010049 BATTERY PACK AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2114065 508 JFK - EMERGENCY LIGHT AT SECTION 4 LEFT HAND SIDE INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SECTION 4 LEFT HAND SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20050707001142005070700114NM 2005 7 7 AALA20050416 120050627A3397 CONNECTOR BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21374AA 25201 SFO - EMERGENCY LIGHT AT SEAT 35H INOPERATIVE. REPLACED CONNECTOR AND RELAMPED FOR EMERGENCY LIGHT AT SEAT 35H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050707001162005070700116WP 2005 7 7 AALA20050414 120050627A3397 CONNECTOR DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21290AA 49302 SJC - EMERGENCY LIGHTS AT FLIGHT ATTENDANT STATION INOPERATIVE. REPLACED PIN ON CONNECTOR P11161 FOR EMERGENCY LIGHTS AT FLIGHT ATTENDANT STATION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050707001182005070700118WP 2005 7 7 AALA20050415 120050627A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217508 49802 SJC - COCKPIT OVERHEAD EMERGENCY PEANUT LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND CHARGER FOR COCKPIT OVERHEAD EMERGENCY PEANUT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050707001202005070700120 2005 7 7 ARWA20050607 420050624A3442 CONNECTOR DOUG DC10 DC1030F 3023504WP WX RADAR SYS UNSECURE A ARWAA UNSCHED LANDING O OTHER CLCLIMB 1 SO19478CT 47819 WEATHER RADAR SYSTEM FAILED DURING FLIGHT (CLIMBOUT); UNABLE TO FIX; RETURNED TO KMIA. CLEANED AND RE-SECURED CONNECTORS AT ANTENNA RADOME; PERFORMED TEST RADAR SYSTEM IN ACCORDANCE WITH M/M 34-41-00; NO DUPLICATE FAIL AT THIS TIME. 2L73 4F RTA22WE 20050708000102005070800010NM 2005 7 8 SWAA051901 120050629A3350MS155721 BULB BOEING737 7373H4 1384600NM EMERGENCY LIGHTSINOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29397SW 27691 DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050708000142005070800014NM 2005 7 8 SWAA051887 120050627A53306545776 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29512SW 24189 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 25R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050708000222005070800022NE 2005 7 8 SWAA051895 220050627A7261CFM563 ENGINE BOEING737 7373T0 1384582NM GE CFM56 CFM563B1 13802NE LEFT MAKING METAL A SWAAK NONE O OTHER ININSP/MAINT 1 SW29684WN 23941 721287 DURING SCHEDULED C4 CHECK, FOUND SEVERAL METAL PARTICLES AT THE NR 1 ENGINE FWD SCAVENGE SCREEN. REMOVED AND REPLACED NR 1 ENGINE PER MM. 2L72 4F4 FRTA16WE E2GL 20050708000242005070800024NM 2005 7 8 SWAA051918 120050702A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 489, RBL 7. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050708000342005070800034NM 2005 7 8 SWAA051904 120050630A3350101114 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29432WN 33715 EMERGENCY EXIT LIGHT LENS MISSING AT ROW 1. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20050708000372005070800037 2005 7 8 SWAA051907 420050630A2565D31354 SLIDE BOEING737 7373A4 1384585NM FWD DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29677AA 23289 DURING SCHEDULED C3 CHECK, FOUND L1 & R1 DOOR EVACUATION SLIDES OUT OF ADJUST. READJUSTED SLIDES PER MM. 2L72 4F RTA16WE 20050708000382005070800038 2005 7 8 SWAA051908 420050630A2565416A2200 SLIDE BOEING737 7377H4 1384404NM R2 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29781WN 30601 R2 DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20050708000452005070800045NM 2005 7 8 SWAA051929 120050701A3350D71701100 BATTERY PACK BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29429WN 33658 DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050708000492005070800049NM 2005 7 8 SWAA051933 120050701A335020131A BATTERY BOEING737 7375H4 138449DNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29521SW 25320 DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20050708000522005070800052NM 2005 7 8 SWAA051936 120050701A3350101331 LENS BOEING737 737317 138447PNM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29661SW 23173 OVERHEAD BIN EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 15 DEF. SECURED LENS PER MM. 2L72 4F RTA16WE 20050708000762005070800076NM 2005 7 8 ASAA0540270 120050529A5320654659234 SUPPORT BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02792AS 28887 CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT LWR SURFACE. REMOVED AND REPLACED. (K) 2L72 4F4 FRTA16WE E21EU 20050708000772005070800077SO 2005 7 8 XGN2005F00007 220050614A8530920644 CYLINDER CESSNA401 401 207590CCE CONT O520 TSIO520E 17040SO ENGINE CRACKED E XGNAO OTHER O OTHER NRNOT REPORTED 1 SW0531DB 1102 4010202 275320R THIS CYLINDER WAS IN THE NR 6 POSITION AND IS A TYPE (A) HEAD. THIS CRACKED CYLINDER HEAD WAS FOUND AT THE 50 HOUR INSPECTION. WE ARE FINDING SIGNS OF AIR LEAKAGE ON THE EXHAUST SIDE OF THE CYLINDER HEAD WHEN DOING A COMPRESSION CHECK. WE ARE SPRAYING SOAPY WATER ON THE CYLINDER HEAD. (K) 1L72 3O3 O A7CE E8CE 20050708000792005070800079NM 2005 7 8 ASAA0540265 120050525A532269407124 SHEAR TIE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02776AS 25109 SHEAR TIE BETWEEN STR 26L AND 25R, B-STA 947 HAS SURFACE CORROSION. REMOVED FABRICATED AND INSTALLED SHEAR TIE AND CLIP IAW SRM . (K) 2L72 4F4 FRTA16WE E21EU 20050708000872005070800087NM 2005 7 8 ASAA0540271 120050529A5320692471 THRESHOLD BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM02792AS 28887 CORROSION ON FWD ENTRY DOOR THRESHOLD ZEE CHANNEL. REMOVED AND REPLACED. (K) 2L72 4F4 FRTA16WE E21EU 20050708000942005070800094NM 2005 7 8 ASAA0540291 120050614A5311654655080 FRAME BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU AFT CARGO BAY DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02792AS 28887 FRAME UPPER CHORD DENTED AFT CARGO BAY B-STA 787 BETWEEN STR 24R AND 25R. REPAIRED FRAME. (K) 2L72 4F4 FRTA16WE E21EU 20050708000952005070800095NM 2005 7 8 ASAA0540288 120050613A57536546435282 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU TE FLAP PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 RT OB AFT FLAP IB END HAS A PUNCTURE IN THE LWR SURFACE. REMOVED DAMAGED AREA FABRICATED AND INSTALLED FILLER AND DOUBLER AND INSTALLED REPAIR PIECES IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050708001012005070800101NM 2005 7 8 ASAA0540287 120050613A531165C25229081 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 FRAME AT STA 727D BETWEEN STR 26 AND 25L IS CORRODED. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050711000102005071100010CE 2005 7 11 DXTA200500813 120050701A323041EN496 LIMIT SWITCH CESSNA500 560CESSNA 2076750CE MLG FAILED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07383QS 5600483 LANDING GEAR WOULD NOT RETRACT AFTER T/O. FMS PLAN PAGE 5 FLIGHT TIMES DID NOT ACTIVATE AND FLIGHT TIME CLOCK DID NOT START AFTER T/O. REPLACED LEFT HAND MAIN SQUAT SWITCH WITH A NEW ONE IAW CE560 MM CH 32-61-00, OPS CHECK GOOD. 2L72 4F RTA22CE 20050711000152005071100015CE 2005 7 11 71599 120050705A3210 WARNING LIGHT BEECH 1900 1900D 1154162CE MLG ILLUMINATED A AMWAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 CE07159YV UE159 UPON FINAL, CREW EXTENDED MAIN LANDING GEAR AND OBSERVED RIGHT MAIN LANDING GEAR GREEN. DOWN AND LOCKED INDICATOR WILL NOT ILLUMINATE. CREW ACCOMPLISHED TOWER FLY-BY FOR DOWN AND LOCK VERIFICATION AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED ACTUATOR. 2L72 4T RTA24CE 20050711000182005071100018NE 2005 7 11 XN0A1243 220050705A7200 ENGINE AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE NR 1 MALFUNCTIONED A XN0AC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL23371PC 157 ON TAKEOFF NR 1 ENGINE EGT EXCEED LIMITS, ABORTED TAKEOFF AT APPROXIMATELY 120KTS. 2L72 4F4 FRTA35EU E23EA 20050711000192005071100019NM 2005 7 11 DHL2005754003 120050702A33501000679 LIGHT BOEING727 727223 1384074NM EMERGENCY EXIT WILL NOT TEST A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01754DH 22008 ENTRY DOOR EMERGENCY EXIT LIGHT WILL NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHT ASSY IAW MM 33-50-01, OPS CHECK GOOD. 2L73 4F A3WE 20050711000212005071100021WP 2005 7 11 MWEA050067 120050705A53479957871519 SEAT TRACK DOUG DC9 DC982 3022082WP COCKPIT WORN A MWEAK NONE O OTHER ININSP/MAINT 1 GL31810ME 48072 FIRST OFFICERS UPPER AND LOWER SEAT TRACK IS WORN AND ADJUSTMENT HOLES ELONGATED. REMOVED AND REPLACED SEAT TRACK. 2L72 4F A6WE 20050711000252005071100025NM 2005 7 11 DHL2005741606 120050516A5754 RIB BOEING727 7272Q9 138448MNM NR 7 SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 NR 7 SLAT I/B RIB AT ACTUATOR ROD END IS CRACKED. REMOVED CRACKED RIB AT I/B OF ROD END IAW B727 SRM 51-30-2 FIG 7. LOCATED, DRILLED AND INSTALLED NEW RIB, P/N 65-17310-3, PO 5096251 IAW B727 SRM 51-30-2 FIG 1 AND 57-50-2 FIG 2. 2L73 4F RTA3WE 20050711000272005071100027EU 2005 7 11 AWXA200500735 120050615A3397ABS0374A24 WIRE AIRBUS320 A320232 3930326EU EMERGENCY LIGHTSDAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28642AW 584 DURING C-7 CHECK, FOUND DAMAGED WIRE AT PASSENGER SEAT 17L EMERGENCY EXIT LIGHT. MAINTENANCE REPLACED CONNECTOR AT PASSENGER SEAT 17L EMERGENCY EXIT LIGHT IAW AIRBUS MM 20-44-11, OPERATIONAL CHECKS GOOD. 2L72 4F RTA28NM 20050711000322005071100032NM 2005 7 11 WRLA2005126 120050622A5510 STRUCTURE DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C-04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098, FOUND CORROSION IN HST LT BARREL NUT HOLE NR 34. 2L73 4F4 FRTA22WE E24NE 20050711000432005071100043NM 2005 7 11 WRLA2005132 120050622A5510 STRUCTURE DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C-04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098, FOUND CORROSION IN HST LT BARREL NUT HOLE NR 19. 2L73 4F4 FRTA22WE E24NE 20050711000462005071100046NM 2005 7 11 WRLA2005134 120050622A5510 STRUCTURE DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C-04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098, FOUND CORROSION IN HST LT BARREL NUT HOLE NR 12. 2L73 4F4 FRTA22WE E24NE 20050711000512005071100051WP 2005 7 11 IXXA05SMN25S 120050429A5730 DOUBLER DOUG DC8 DC871F 302199DWP RT WING CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX834963359 45993 RT WING CTR L/E INTERNAL DOUBLER CRACKED. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 AND SEMAN DWG ED-3953. REMOVED FASTENERS FROM REPAIR AREA IAW DC-8 SRM. REMOVED DAMAGED AREA IAW SEMAN ED-3953. PERFORMED NDT INSPECTION TO AREA IAW NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER , SHIM, FILLER, INTERNAL REPAIR DOUBLER IAW SEMAN DWG ED-3953. CLEANED, TREATED AND PRIMED AREA, SHIM, FILLER REPAIR DOUBLER, REPAIR DOUBLER INTERNAL PART IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11 PAGE 9. INSTALLED REPAIR PART IAW SEMAN DWG ED-3953, DC-8 SRM 51-1-21 PAGE 1, DC-8 SRM 51-3-0 PAGE 1. TORQUED IAW DC-8 RM 51-3-1. 2L74 4F RT4A25 20050711000582005071100058WP 2005 7 11 IXXA05SMN32S 120050429A5340 ATTACH FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX834963359 45993 MAIN CARGO BAY INTERNAL FUSELAGE FITTING CORRODED, STA 1614.000 L-21L. REMOVED CORROSION IAW DC-8 SRM 51-1-8 PAGE 17-18. FOUND OUT OF LIMITS IAW DC-8 SRM 53-2-0 PAGE 2P. REMOVED CORRODED FITTING IAW DC-8 SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING IAW DWG NR 9750448. PERFORMED NDT INSPECTION IAW NDT DC-8 NDT SPM PART 08-00-02 TO 07. CLEANED, TREATED AND PRIMED AREA AND NEW FITTING IAW DC-8 SRM 51-1-8B. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D PAGE 9. TORQUED DC-8 SRM 51-3-1. 2L74 4F RT4A25 20050711000832005071100083NM 2005 7 11 AWXA200500743 120050610A52106517684642 INTERCOSTAL BOEING737 7373B7 1384580NM L1 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28328AW 23377 FOUND ON FORWARD SIDE OF L1 DOOR CUTOUT INTERCOSTAL WEB CRACKED AT STR 7L AND BS 294. MAINTENANCE REMOVED INTERCOSTAL WEB AND CLIP ON L1 DOOR IAW BOEING 737-300 SRM 51-40-01. FABRICATED INTERCOSTAL WEB, AUXILIARY INTERCOSTAL AND SHEAR TIE CLIP IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5300-05172-RC1. FABRICATED REPAIR PARTS WERE INSTALLED IAW AWA ER NR 03-5300-05172-RC1. 2L72 4F RTA16WE 20050711001042005071100104EA 2005 7 11 VTZA200500116 120050623A5320601R311719 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27642BR 7356 INTERCOSTAL CRACKED RT INBOARD SIDE AT FS 484 LT BETWEEN BL 27.00. 2L72 4F RTA21EA 20050711001052005071100105NM 2005 7 11 DHL2005741594 120050511A5754 ATTACH BRACKET BOEING727 7272Q9 138448MNM NR 1 SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 NR 1 SLAT ROD END ATTACH BRACKET IS CRACKED. REMOVED NR 1 SLAT ATTACH BRACKET. FABRICATED BRACKET IAW B727 SRM 57-20-2 FIG 3. TREATED AND PRIMED BRACKET IAW B727 SRM 51-10-2. INSTALLED ATTACH BRACKET IAW B727 SRM 51-30-2. 2L73 4F RTA3WE 20050711001152005071100115WP 2005 7 11 MWEA050064 120050630A3397 WIRE DOUG DC9 DC982 3022082WP FORWARD CABIN MISROUTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31810ME 48072 FLOOR TRACK LIGHTING IN FORWARD CABIN G2 AISLE AREA, WIRES ARE MISROUTED AND IS MISSING PROTECTIVE TRACK PIECE FROM CENTER TO RIGHT WALL. SECURED EMERGENCY FLOOR TRACK LIGHTING WIRES AT FORWARD CABIN INTO THE NEW WIRE PROTECTION TRACKS, OPERATIONS CHECKED GOOD. 2L72 4F A6WE 20050711001162005071100116WP 2005 7 11 MWEA050065 120050703A5220 DOOR DOUG DC9 DC982 3022082WP OVERWING EXIT INOPERATIVE A MWEAK NONE O OTHER ININSP/MAINT 1 GL31810ME 48072 DURING INVESTIGATION OF LOOSE EXIT SIGN, COULD NOT REMOVE LEFT AFT OVERWING EXIT DOOR. REMOVED LEFT AFT DOOR BY DISPLACING FORWARD AND AFT ADJACENT SIDE WALL TRIM STRIPES, ADJUSTED SAME SIDE WALL PANELS AND REINSTALLED DOOR, OPERATIONAL CHECKED NORMAL. 2L72 4F A6WE 20050711001282005071100128EA 2005 7 11 VTZA200500117 120050623A5320601R3117117 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27642BR 7356 INTERCOSTAL CRACKED ON LT OUTBOARD SIDE AT FS 484 BETWEEN BL 36.00. 2L72 4F RTA21EA 20050711001292005071100129NM 2005 7 11 RYAN20050018 120050612A7930 WARNING SYSTEM BOEING737 737201 1384454NM PWA JT8 JT8D9A 52048NE NR 1 ENGINE ACTIVATED A RYNAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 CE07240AU 22355 655811 DURING CLIMB, ENGINE NR 1 HAD HIGH OIL PRESSURE AND SHORTLY THEREAFTER NR 1 OIL TEMPERATURE STARTED CLIMBING TOWARDS REDLINE. ON RETURN NR 1 ENGINE WAS SHUTDOWN. 2L72 4F4 F A16WE E2EA 20050711002012005071100201 2005 7 11 AWXA200500734 420050615A2565D30664105 SLIDE AIRBUS320 A320232 3930326EU R1 DOOR INTERFERENCE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28642AW466453712 584 DURING C-7 CHECK, R1 DOOR CAN'T BE LOCKED IN FULLY OPEN POSITION DUE TO SLIDE RAFT TOUCHES FUSELAGE. MAINTENANCE REMOVED AND REPLACED SLIDE IAW AMERICA WEST AIRLINES TASK CARD R1C25304. SLIDE WAS OVERHAULED IAW CMM 25-61-20 REV 9. 2L72 4F RTA28NM 20050711002202005071100220NM 2005 7 11 05FDEA01697 120050626A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25619FE 48770 WITH REFERENCE TO WORK CARD E1-5510-7-5000 D1 PART 1, NR 14L FITTING BARREL NUT BORE FOUND BADLY CORRODED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. 2L73 4F RTA22WE 20050711002332005071100233WP 2005 7 11 0500939754 120050606A2150 DUCT DOUG DC9 DC941 302207NWP LT ACM BLOWN A NWAAI CABIN DEPRESSURIZATION J WARNING INDICATION CRCRUISE 1 GL01754NW 47178 LEVEL AT FL 290 WITH ENGINE AND AIRFOIL ANTI-ICE ON, CREW FELT A PRESSURE BUMP AND NOTICED CABIN ALTITUDE CLIMBING AT 1500 FPM. CYCLED PRESSURE CONTROLLERS FROM AUTO TO MANUAL AND BACK, ANTI-ICE SWITCHED OFF, BUT CABIN STILL CLIMBED. INITIATED RAPID DESCENT TO FL 140; CLEARED WITH ATC. FLIGHT CREW DONNED O2 MASKS AND PERFORMED COM PROCEDURES. CLEARED TO 10,000 FT FOR REST OF FLIGHT. CABIN MAXED OUT AT 10,500 FT MSL. MASKS DID NOT DEPLOY AND LANDING WAS UNEVENTFUL. MAINTENANCE RECONNECTED A BLOWN BOOT ON LT ACM AND RETURNED AIRCRAFT TO SERVICE. 2L72 4F A6WE 20050711002362005071100236NM 2005 7 11 05FDEA01708 120050627A5330 SKIN BOEING727 727233 138408ANM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25263FE 21625 FUSELAGE EXTERNAL SKIN OF AFT AIRSTAIR, SECTION 48, AREA FROM LE TO 27 INCH AFT OF LE, LBL 21 TO RBL 21, HAS GRAVEL DAMAGE. 2L73 4F RTA3WE 20050711002582005071100258EA 2005 7 11 SWIA200515180 120050623A5210 FITTING CNDAIRCL600 CL6002B19 1900309EA MAIN CABIN DOOR LACK OF LUBE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07916SW 7634 MAIN CABIN DOOR WILL NOT CLOSE. LUBRICATED ALL PAX DOOR FITTINGS AND PINS PER CRJ 200 MM 12-20-52. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050711002592005071100259EA 2005 7 11 SWIA200515181 120050620A2750 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07919SW 7657 ON FLAP RETRACTION, FLAPS FAILED AT 8 DEGREES. RIGGED RT BPSU IAW CRJ MM 27-51-10. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050712000562005071200056NM 2005 7 12 SWAA051974 120050707A3350MS155721 BULB BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29324SW 23414 DURING SCHEDULED C1 CHECK, FOUND FWD GALLEY EMERGENCY LIGHTS INOP. RELAMPED LIGHTS PER MM. 2L72 4F RTA16WE 20050712000582005071200058NM 2005 7 12 SWAA051976 120050707A335010107451 SIGN BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29326SW 23690 FWD CABIN EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM. 2L72 4F RTA16WE 20050712000742005071200074NE 2005 7 12 SWAA051962 220050706A7261 ENGINE BOEING737 7377H4 1384404NM CFMINTCFM567CFM567B22 13802NE NR 1 LEAKING A SWAAO OTHER KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SW29467WN 33830 874912 NR 1 ENGINE SMOKED AFTER START DUE TO OIL LEAK. REMOVED AND REPLACED NR 1 ENGINE PER MM. 2L72 4F4 FRTA16WE E00055EN 20050712000942005071200094NM 2005 7 12 SWAA051990 120050709A3350101073 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29439WN 29834 RIGHT AFT LOWER EMERGENCY EXIT SIGN COVER BROKEN. REMOVED AND REPLACED COVER PER MM. 2L72 4F RTA16WE 20050712000982005071200098NM 2005 7 12 SWAA051996 120050708A53226546569 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29608SW 27928 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 1006, BL 0, WL 185. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050712001032005071200103NM 2005 7 12 SWAA052003 120050708A57126545445 RIB BOEING737 7373H4 1384600NM RT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29608SW 27928 DURING SCHEDULED D-CHECK, FOUND RT WING LOWER RIB CHORD CRACKED AT WBL 135.5, BETWEEN STR 2 & STR 3. REPAIRED RIB PER SWA ACO. 2L72 4F RTA16WE 20050712001042005071200104NM 2005 7 12 SWAA052004 120050708A55536546874 FITTING BOEING737 7373H4 1384600NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29608SW 27928 DURING SCHEDULED D-CHECK, FOUND LT & RT VERTICAL STAB ATTACH FITTING FWD & AFT PRIMARY CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER. 2L72 4F RTA16WE 20050712001072005071200107NM 2005 7 12 SWAA052007 120050708A5320BAC1506714 WEB BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29608SW 27928 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 294 TO BS 341, RBL 55, WL 208. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050712001082005071200108EU 2005 7 12 AWXA200500746 120050623A7500 BLEED AIR SYS AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE ENGINES MALFUNCTIONED A AWXAAD UNSCHED LANDING RETURN TO BLOCK JG WARNING INDICATION MULTIPLE FAILURE CLCLIMB 1 WP28651AW 866 AIR TURN BACK. DURING CLIMB RECEIVED ECAM MESSAGE FOR ENG BLEED 1 FAULT FOLLOWED BY PACK FAULT THEN NR 2 ENG BLEED FAULT FOLLOWED BY PACK FAULT. RETURNED WITHOUT FURTHER INCIDENT. MX REMOVED AND REPLACED NR 1 AND NR 2 BMC. REMOVED AND REPLACED NR 1 ENGINE HP VALVE. REMOVED AND REPLACED NR 1 ENGINE PRESSURE REGULATING VALVE. PERFORMED POWER ASSURANCE RUNS. POWER ASSURANCE RUNS WERE GOOD. REMOVED AND REPLACED NR 1 AND NR 2 ENGINE FAN AIR VALVE CONTROL THERMOSTAT. REMOVED AND REPLACED NR 2 BLEED PRESSURE REGULATOR VALVE CONTROL SOLENOID. COMPLIED WITH FUNCTIONAL TEST OF OVERPRESSURE VALVE. ALL MX ACCOMPLISHED IAW AIRBUS MM. OPERATIONAL CHECKS GOOD. 2L72 4F4 FRTA28NM E40NE 20050712001092005071200109NM 2005 7 12 SWAA052008 120050708A53116545874 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29608SW 27928 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 294, RBL 55, WL 209. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20050712001102005071200110NM 2005 7 12 SWAA052009 120050708A53106547978 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29608SW 27928 DURING SCHEDULED D-CHECK, FOUND FUSELAGE CREASE BEAM WEB CORRODED AT BS 500 TO BS 500D, LBL 68, WL 208. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050712001132005071200113NM 2005 7 12 SWAA052012 120050708A3350MS155721 BULB BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29734SA 27866 DURING SCHEDULED MV2 CHECK, FOUND RT AFT CABIN EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050712001142005071200114NM 2005 7 12 SWAA051983 120050708A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 311, STR 20R. MX FERRY TO PHX, REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050712001152005071200115NM 2005 7 12 SWAA051984 120050708A53206551698 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CORRODED AT BS 907, STR 22R. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20050712001162005071200116NM 2005 7 12 SWAA051985 120050708A53116546524 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 360, STR 28R TO STR 28L, WL 149. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050712001202005071200120EU 2005 7 12 AWXA200500750 120050624A3350321431 BATTERY PACK AIRBUS320 A320231 3930325EU EMERGENCY LIGHTSDISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28646AW 271 DURING 8-DAY CHECK, FOUND BOTH LT AND RT OVERWING SEAT MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LT (11WL) AND RT (12WL) BATTERY PACKS IAW AIRBUS MM 33-51-38-04. OPERATIONAL TESTS WERE GOOD. 2L72 4F RTA28NM 20050712001212005071200121 2005 7 12 AWXA200500751 420050624A2565 CABLE AIRBUS320 A320231 3930325EU R2 DOOR SLIDE LOOSE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28627AW 66 DURING 8-DAY CHECK, FOUND R2 DOOR SLIDE CABLE LOOSE. MAINTENANCE REMOVED AND REPLACED R2 DOOR SLIDE IAW AMERICA WEST AIRLINES TASK CARD R1C25304. 2L72 4F RTA28NM 20050712001232005071200123 2005 7 12 SWAA051988 420050710A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29333SW 23697 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050712001252005071200125EU 2005 7 12 06152005 120050615A21507769106 ACM SAAB SF340 340B 7860101EU SMOKE A NSVAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA27277MJ 277 AFTER TURNING PACK ON, SMOKE INVADED FLIGHT DECK AND SMALL PARTICLES OF SOOT CAME OUT OF THE EYEBALL VENTS. 2L72 4T RTA52EU 20050712001272005071200127NM 2005 7 12 EIA2005129 120050614A5330 SKIN BOEING747 747212B 1384886NM FUSELAGE BULGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 BULGED BELLY SKIN AT TWO (2) LOCATIONS, STA 2160 BL 0 AND RBL 12. ACCOMPLISHED SKIN REPAIR PER B 747-SRM 53-03-03 AND STRINGER REPAIR PER B 747 SRM 53-10-03. 2L74 4F A20WE 20050712001282005071200128NM 2005 7 12 EIA2005130 120050618A3350 LIGHT BOEING747 747132 1384882NM EMERGENCY LIGHTSINOPERATIVE A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 UPPER DECK LT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSY IAW MM 33-51-07, PAGE 201. OPS CK OK IAW MM 33-51-00. 2L74 4F A20WE 20050712001322005071200132NM 2005 7 12 AWXA200500754 120050616A532069418611 INTERCOSTAL BOEING737 7373B7 1384580NM FWD CARGO CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28328AW 23377 DURING C-13 CHECK FOUND INTERCOSTAL CRACKED, .25 INCHES IN LENGTH INSIDE FORWARD CARGO DOOR AT CENTER OF DOOR, 20 IN FROM LOWER EDGE OF DOOR AT BS 470, WL 176, STRINGER 23R. MAINTENANCE REMOVED INTERCOSTAL AT FORWARD CARGO DOOR AT CENTER OF DOOR, 20 IN FROM LOWER EDGE OF DOOR AT BS 470, WL 176, STRINGER 23R AND FABRICATED NEW INTERCOSTAL IAW BOEING DWG 69-41861. INSTALLED FABRICATED REPAIR PARTS AT FORWARD CARGO DOOR AT CENTER OF DOOR, 20 IN FROM LOWER EDGE OF DOOR AT BS 470, WL 176, STRINGER 23R IAW BOEING 737-300 SRM 51-40-02-0 FIG 3, 4, 6 AND BOEING 737-300 SRM 51-40-04 FIG 2. 2L72 4F RTA16WE 20050712001332005071200133NM 2005 7 12 AWXA200500755 120050609A5315654581292 FLOORBEAM BOEING737 7373B7 138447FNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28328AW 23377 DURING C-13 CHECK, FOUND CORROSION ON FLOORBEAM STA 328, FROM BL 10R TO BL 30R. MAINTENANCE REMOVED CORROSION. FOUND CORROSION TO BE OUT OF LIMITS. REMOVED DAMAGED AREA FROM FLOORBEAM AT STA 328 IAW BOEING 7637-300 SRM 53-10-51-2 FIG 205. RECEIVED NEW UPPER CHORD AND PREPPED FOR INSTALL IAW BOEING 737-300 SRM 53-10-51. FABRICATED REPAIR ANGLE, ANGLE SPLICES, STIFFENERS, AND SHIMS IAW BOEING 737-300 SRM 53-10-51. INSTALLED FABRICATED REPAIR PARTS IAW BOEING 737-300 SRM 35-10-51-2 FIG 205. 2L72 4F RTA16WE 20050712001362005071200136EU 2005 7 12 06222005 120050622A6120 GEARBOX SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE HAMSTD14RF 14RF19 NE PROPELLER MALFUNCTIONED A NSVAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 EA27341CJ 341 785407 718 LT PROPELLER FEATHERED DURING TAKEOFF ROLL. 2L72 4T4 TRTA52EU E8NE 6 CP11NE 20050712001372005071200137EA 2005 7 12 VTZA200500130 120050706A5320601R311719 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27662BR 7526 INTERCOSTAL CRACKED AT .250 INCH IN LENGTH ON RT OUTBOARD SIDE AT FS 484 RIGHT BETWEEN BL 36.00. 2L72 4F RTA21EA 20050712001382005071200138EA 2005 7 12 VTZA200500131 120050706A5320601R3117117 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSLEAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27662BR 7526 INTERCOSTAL CRACKED AT .250 INCH IN LENGTH ON LT OUTBOARD SIDE AT FS 484 BETWEEN BL 36.00. 2L72 4F RTA21EA 20050712001392005071200139EA 2005 7 12 VTZA200500132 120050706A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27662BR 7526 INTERCOSTAL ON AFT SIDE OF FS 621 LT SIDE AT STR 15 CRACKED .726 INCH. 2L72 4F RTA21EA 20050712001412005071200141EA 2005 7 12 VTZA200500134 120050706A5712601R107091 RIB CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27662BR 7526 LEFT BATT RIB IS CRACKED 1.5 INCH. 2L72 4F RTA21EA 20050712001432005071200143NM 2005 7 12 ASMF200506028 120050628A4900 APU DOUG MD88 MD88 3023688NM APU BAY MALFUNCTIONED W ASMFD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SW23169PL 53175 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF APU DID NOT SUPPORT PNEUMATIC CHARGES FOR ENGINE STARTING. GPU WAS CONNECTED TO ENGINES STARTING AND APU WAS DEFERRED IAW MEL 49-1. DURING OVERNIGHT SERVICE APU WAS TESTED IAW MPCM 49-00-01 SETTING BOTH ENGINES IN 23 PERCENT OF N2 IAW MM 71-00-00, OPERATING CORRECTLY THE APU. DEFERRED REPORT WAS CLOSED. 2L72 4F RTA6WE 20050712001462005071200146NM 2005 7 12 SWAA051950 120050705A53146545866 KEELBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29332SW 23696 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE KEELBEAM CORRODED AT BS 520, RBL 7. REPAIRED KEEL BEAM PER SRM. 2L72 4F RTA16WE 20050712001522005071200152NM 2005 7 12 AWXA200500760 120050608A5414311A14504 SKIN BOEING737 7373B7 1384580NM NR 2 PYLON CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28328AW 23377 DURING C-13 CHECK, FOUND CRACK, .650 INCHES IN LENGTH, LOCATED ON KEEL SKIN AT EDGE OF ACCESS PANEL 5823R, ON THE NR 2 PYLON. MAINTENANCE STOP DRILLED CRACK ON KEEL SKIN AT EDGE OF ACCESS PANEL 5823R IAW AMERICA WEST AIRLINES ENGINEERING REQUEST (ER) NR 03-5400-05175-RC1. FABRICATED REPAIR DOUBLER IAW ER 03-5400-05175-RC1. INSTALLED FABRICATED REPAIR PARTS ON KEEL SKIN AT EDGE OF ACCESS PANEL 5823R ON THE NR 2 PYLON IAW ER 03-5400-05175-RC1. 2L72 4F RTA16WE 20050712001532005071200153NM 2005 7 12 AWXA200500761 120050603A5753113N280062 SKIN BOEING757 7572S7 1384962NM TE FLAPS DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28905AW 23567 DURING C-10 CHECK A PYLON STAND HIT RT INBOARD AFT FLAP TRAILING EDGE, DELAMINATING AFT EDGE APPROX 8 INCHES BY 2 INCHES. ALSO, CRACKING LOWER SKIN MEASURING .76 INCHES IN LENGTH EXTENDING FROM AFT EDGE FORWARD LOCATED AT STA 205, BL 21.5L. MAINTENANCE REMOVED DAMAGED AREA FROM RT INBOARD AFT FLAP TRAILING EDGE AND PREPPED REPAIR AREA FOR BONDING OF UPPER AND LOWER SKIN PLYS IAW BOEING 57 SRM 51-70-17, PARAGRAPH 4M. BONDED UPPER AND LOWER SKIN IAW BOEING 757 SRM 51-70-17, PARAGRAPH 4M AND AMERICA WEST AIRLINES ENGINEERING REQUEST 19-5733-05173-ES1. 2L72 4F RTA2NM 20050712001542005071200154NM 2005 7 12 AWXA200500762 120050608A5414 SKIN BOEING757 7572S7 1384962NM RT WING PYLON DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28905AW 23567 DURING C-10 CHECK, DRILL DAMAGE OCCURRED TO FASTENER HOLE ON RT WING PYLON SIDE LOAD FITTING AT BL 9R, 3RD HOLE FROM AFT END ON OUTBOARD SIDE OF FITTING. MAINTENANCE SPOT FACED AND REMOVED DAMAGE FROM DISCREPANT HOLE IAW AMERICA WEST AIRLINES (AWA) ENGINEERING REQUEST (ER) 19-5704-05174-ES3. FLAP PEENED, TREATED AND PRIMED AREA IAW BOEING 757 SRM 51-20-06, SOPM 20-10-03, AND ER 19-5704-05174-ES3. 2L72 4F RTA2NM 20050712001552005071200155NM 2005 7 12 AWXA200500764 120050609A53126546568524 PRESSURE BLKHD BOEING737 7373B7 1384580NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28328AW 23377 DURING C-13 CHECK DISCOVERED CORROSION ON AFT PRESSURE BULKHEAD STA 1016, WL 150 TO WL 155, STR 27R, ON FORWARD SIDE AND RUNNING UNDER LEVELING COMPOUND. MAINTENANCE REMOVED CORROSION ON AFT PRESSURE BULKHEAD STA 1016, WL 150 TO WL 155, STR 27R, ON FORWARD SIDE AND FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-80-01-1 FIG 101. MAINTENANCE CUT OUT DAMAGE AREA ON AFT PRESSURE BULKHEAD AT STATION 1016, WL 150, STR 27R AND FABRICATED REPAIR DOUBLER, STIFFENER, SPLICES AND FILLER IAW BOEING 737-300 SRM 53-80-08-2 FIG 201. INSTALLED AND SEALED FABRICATED REPAIR PARTS IAW BOEING 737-300 SRM 53-80-08-2 FIG 201. 2L72 4F RTA16WE 20050712001562005071200156NM 2005 7 12 AWXA200500765 120050628A53126546568520 STIFFENER BOEING737 7373B7 1384580NM PRESSURE BLKHD CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28328AW 23377 DURING C-13 CHECK FOUND CORROSION PRESENT ON STIFFENER CHANNEL LOCATED AT AFT PRESSURE BULKHEAD FORWARD SIDE AT BS 1016, WL 155, BL 0. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW BOEING 737-300 SRM 53-80-08-1 FIG 101. MAINTENANCE REMOVED CORROSION ON STIFFENER CHANNEL LOCATED AT AFT PRESSURE BULKHEAD BS 1016, WL 155, AND BL 0. MAINTENANCE REMOVED DAMAGE STIFFENER ON THE AFT PRESSURE BULKHEAD AT STATION 1016, WL 150, BL 0 AND FABRICATED REPAIR STIFFENER IAW BOEING 737-300 SRM 53-80-08-2 FIG 201. INSTALLED FABRICATED REPAIR PARTS IAW BOEING 737-300 SRM 53-80-08-2 FIG 201. 2L72 4F RTA16WE 20050712001572005071200157WP 2005 7 12 ASAA0580157 120050301A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHTSDISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM02944AS 53019 PREFLIGHT CHECK, FOUND OVERHEAD EMERGENCY LIGHTS DID NOT ILLUMINATE WHEN TURNED ON. RESEATED ASSOCIATED BATTERY PACK POWER SUPPLY. CONNECTION WAS LOOSE. (M) 2L72 4F RTA6WE 20050712001582005071200158WP 2005 7 12 ASAA0580207 120050404A5330 SKIN DOUG DC9 DC983 3022083WP FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02976AS 53452 FOUND DURING HV CHECK, FUSELAGE SKIN GOUGED ON LT SIDE. REMOVED DAMAGED SECTION. INSTALLED 2 FINGER DOUBLERS AND 1 REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050712001602005071200160WP 2005 7 12 ASAA0580212 120050420A5321993061223 CUSP WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02958AS 53024 DURING C-CHECK, FOUND CABIN FLOOR PANEL CUSP WEB CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLER AND DOUBLER. (M) 2L72 4F RTA6WE 20050712001612005071200161WP 2005 7 12 ASAA0580213 120050420A55225910411 SKIN DOUG DC9 DC983 3022083WP ELEVATOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02958AS 53024 FOUND DURING C-CHECK, LT ELEVATOR ANTI-FLOAT TAB UPPER SURFACE DENTED. INSTALLED REPAIR DOUBLERS. (M) 2L72 4F RTA6WE 20050712001632005071200163WP 2005 7 12 ASAA0580217 120050425A575359304943 SKIN DOUG DC9 DC983 3022083WP FLAP VANE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02958AS 53024 FOUND DURING C-CHECK, LT WING INBOARD FLAP VANE OUTBOARD SEGMENT DELAMINATED. REMOVED DAMAGE. INSTALLED REPAIR FILLERS AND DOUBLERS. (M) 2L72 4F RTA6WE 20050712001652005071200165WP 2005 7 12 ASAA0580219 120050425A575359304953 SKIN DOUG DC9 DC983 3022083WP FLAP VANE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02958AS 53024 DURING C-CHECK, FOUND RT WING INBOARD FLAP OUTBOARD FLAP VANE UPPER SURFACE DENTED. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050712001662005071200166WP 2005 7 12 ASAA0580220 120050425A5753 SKIN DOUG DC9 DC983 3022083WP FLAP VANE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02958AS 53024 DURING C-CHECK FOUND, LT WING OUTBOARD FLAP INBOARD FLAP VANE LEADING EDGE GOUGED. REMOVED DAMAGE. INSTALLED REPAIR FILLER AND DOUBLER. (M) 2L72 4F RTA6WE 20050712001672005071200167WP 2005 7 12 ASAA0580209 120050418A53105936038501 DOOR FRAME DOUG DC9 DC983 3022083WP AFT CARGO BAY CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02972AS 53448 FOUND HV CHECK, AFT CARGO BAY DOOR JAMB BEAM CORRODED. REPLACED BEAM. (M) 2L72 4F RTA6WE 20050712001682005071200168WP 2005 7 12 ASAA0580210 120050418A575359100404 SKIN DOUG DC9 DC983 3022083WP FLAP VANE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02972AS 53448 FOUND RT OUTBOARD FLAP VANE CHAFED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050712001742005071200174SO 2005 7 12 MASA200500402 120050505A3350 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSDIRTY A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07836MJ 145359 CREW NOTED THAT 3RD AND 4TH STRIP OF EMERGENCY ESCAPE PATH LIGHTING STRIPS INOPERATIVE. MAINTENANCE CLEANED CONNECTIONS TO LIGHTING STRIPS AND NO FURTHER DEFECTS NOTED. 2L72 4T RTT00011AT 20050712001752005071200175EA 2005 7 12 MASA200500403 120050505A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSINOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0777302 7302 CREW NOTED THAT LT FWD EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED LAMP. 2L72 4F RTA21EA 20050712001762005071200176EA 2005 7 12 MASA200500415 120050529A3397 WIRE CNDAIRCL600 CL6002D24 1390016EA EMERGENCY LIGHTSBROKEN A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07909FJ 15009 EMERGENCY LIGHT INOPERATIVE AT ROW 20. REPAIRED BROKEN WIRE AND R2 BATTERY CHARGER AND BATTERY. 2L72 4F RTA21EA 20050712001772005071200177SO 2005 7 12 MASA200500432 120050603A3350 LIGHT EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSINOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07846MJ 145507 NR 2 AISLE CEILING EMERGENCY LIGHT INOPERATIVE. RELAMPED. 2L72 4T RTT00011AT 20050712001782005071200178EA 2005 7 12 COMA570076 120050627A2150 SMOKE CNDAIRCL600 CL6002C10 1390015EA CABIN DETECTED A COMAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO01371CA 10082 SMOKE IN CABIN DURING TAXI. DEFERRED MAINTENANCE ON RT A/C SYSTEM PER MEL. 2L72 4F RTA21EA 20050712001822005071200182NM 2005 7 12 SWAA051953 120050705A21206937319148 CONTROL PANEL BOEING737 7373H4 1384600NM GASPER FAN FAULTY A SWAAK NONE O OTHER ININSP/MAINT 1 SW29347SW 24374 SMOKE/ELECTRICAL ODOR BEHIND GASPER FAN SWITCH & A/C PANEL. REMOVED AND REPLACED P5-10 PANEL PER MM. 2L72 4F RTA16WE 20050712001832005071200183NM 2005 7 12 SWAA051954 120050705A335020131 BATTERY PACK BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29359SW 26596 DURING SCHEDULED RON CHECK, AFT CABIN EMERGENCY LIGHTS WOULD NOT TURN OFF. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050712001842005071200184EA 2005 7 12 MASA200500448 120050607A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSINOPERATIVE A MASAO OTHER L NO TEST NRNOT REPORTED 1 SW0775993 7372 AFT EMERGENCY EXIT LIGHT INOPERATIVE UPON TEST. MAINTENANCE RELAMPED. 2L72 4F RTA21EA 20050712001862005071200186NM 2005 7 12 SWAA051958 120050705A33509250071 LAMP BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29744SW 29490 DURING SCHEDULED MV3 CHECK, FOUND CABIN EMERGENCY LIGHT INOP AT ROW 18 DEF. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050712001872005071200187SO 2005 7 12 MASA200500452 120050609A3350 CHARGER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSINOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07838MJ 145384 EMERGENCY EXIT LIGHTS AT PASSENGER DOOR INOPERATIVE. MAINTENANCE REPLACED BATTERY CHARGER. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050712001882005071200188SO 2005 7 12 MASA200500453 120050609A3350 LIGHT EMB 145 EMB145LR 3260212SO OVER WING DOOR INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07845MJ 145502 EMERGENCY EXIT LIGHTS AT OVER WING DOOR INOPERATIVE. MAINTENANCE CHECKED CONNECTIONS, OPS CHECK WAS GOOD. 2L72 4T RTT00011AT 20050712001892005071200189EA 2005 7 12 MASA200500454 120050609A3350 SIGN CNDAIRCL600 CL6002C10 1390015EA EMERGENCY EXIT MISSING A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07510MJ 10101 CREW REPORTED AN AFT EMERGENCY EXIT SIGN MISSING. MAINTENANCE REPLACED EMERGENCY EXIT SIGN, OPS CHECKED NORMAL. 2L72 4F RTA21EA 20050712001902005071200190NM 2005 7 12 SWAA051941 120050705A53156546811 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORRODED AT BS 986, LBL 17 TO RBL 50, WL 208. REPAIRED FLOORBEAM PER BFG ER. 2L72 4F RTA16WE 20050712001932005071200193NM 2005 7 12 05FDEA01822 120050707A5330 SKIN BOEING727 727200 138407ENM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25263FE 21625 FUSELAGE EXTERNAL SKIN, SECTION 48, BS 1329 LBL 22 3 INCHES O/B OF AFT AIRSTAIR CUTOUT GOUGED. *S/D* GOUGED IN EXTERNAL SKIN OF THE AFT AIRSTAIR CUTOUT AT BS 1329 LBL 22 WAS OUT OF LIMITS IAW SRM 53-30-1. CUT OUT DAMAGE AND FABRICATED REPAIR IAW SRM 51-10-2, ALODINE & PAINTED IAW FED EX 51-20-031-7. INSTALLED FASTENERS IAW SRM 53-30-2. 2L73 4F RTA3WE 20050712001952005071200195EA 2005 7 12 COMA0560366 120050628A2510R1340300 VISOR CNDAIRCL600 CL6002B19 1900309EA COCKPIT BROKEN A COMAA UNSCHED LANDING O OTHER CRCRUISE 1 SO01468CA 7649 PILOT SUN VISOR BROKEN. REPLACED SUN VISOR. 2L72 4F RTA21EA 20050712001972005071200197NM 2005 7 12 05FDEA01830 120050707A5310 PLATE BOEING727 727200 138407ENM DOOR FRAME GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25263FE 21625 MAIN CARGO DOOR BS 460 TO 480 LBL 24 WL 287 DOOR CUTOUT INNER PLATE HAS NUMEROUS GOUGES. *S/D* BLENDED NUMEROUS GOUGES IN DOOR CUTOUT INNER PLATE IAW EA 7-5330-89309. 2L73 4F RTA3WE 20050712001992005071200199WP 2005 7 12 05FDEA01852 120050707A5230 SEAL DOUG DC10 DC1030 3023501WP CARGO DOOR UNSECURE A FDEAAB UNSCHED LANDING EMER. DESCENT J WARNING INDICATION CRCRUISE 1 SO25321FE 47836 IN CRUISE AT FL330 FOR FL340 HAD A RAPID DECOMPRESSION. THE CABIN RAPIDLY CLIMBED TO THE A/C ATTITUDE & A EMERGENCY DESCENT WAS IN PROGRESS. PERFORMED QRH PHASE ONE'S AND LOSS OF PRESSURIZATION CHECKLIST. FOUND MAIN A SECTION OF MAIN CARGO DOOR SEAL PROTRUDING FROM THE DOOR. FOUND TWO FWD LATCH SPOOL BRACKETS AND SURROUNDING AREAS DAMAGED. REPLACED UPPER & LOWER DOOR SUPPORT BEAMS (STA 622-767). REPLACED ATTACH FITTINGS (632-634) REPLACED DOOR SPOOLS. REPLACED DOOR STRIKER & LATCH TRIGGER. PERFORMED EDDY CURRENT INSPECTIONS. INSTALLED DOOR SEAL. CHECKED DOOR JAM FIT/FAIR AND RIG. PERFORMED PRESSURIZATION LEAK CHECK 2L73 4F A22WE 20050712002002005071200200EU 2005 7 12 05FDEA01850 120050707A7603 WIRE AIRBUS310 A310222 3930315EU PWA JT9 JT9D* NE THROTTLE BROKEN A FDEAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 SO25446FE 224 716116 ABORTED TAKEOFF DUE TO ENG NR 2 FAILED TO STABILIZE AT 40 PERCENT POWER, WITH NR 1 ENG THROTTLE SET NORMALLY TO PRODUCE 40 PERCENT N1 THE NR 2 THROTTLE WAS THREE KNOB WIDTHS AHEAD AND STILL ONLY PRODUCING 25 PERCENT N1. FOUND WIRE BROKEN INSIDE RING TERMINAL. RE-TERMINATED WIRE 072007-18 PER STD WIRING PRACTICES. IDLE CHECK AND UP TO 40 PERCENT N1 WAS NORMAL ACCELERATION. 2L72 4F4 FRTA35EU E20EA 20050712002012005071200201EU 2005 7 12 05FDEA01851 120050707A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25656FE16517 745 MCD - SEAT TRACK HAS CORROSION FR 38 PLUS 11.0, RBL 37.5. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-02 AND 53-10-16 FIG 201. SEAT TRACK SPLICE ASSY FABRICATED ON TRAVELER T5/529101 W/O 29203. 2L72 4F RTA35EU 20050712002042005071200204NM 2005 7 12 AWXA200500789 120050616A532069455787 FITTING BOEING757 7572G7 1384963NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28909AW 24522 SAL - MAJOR REPAIR - DURING C1 CHECK FOUND CORROSION ON LOWER SILL FITTING CUTOUT FROM STA 1380 TO STA 1440. NO ALLOWABLE DAMAGE LIMITS LISTED. MAINTENANCE REMOVED AND REPLACED THE LOWER SILL FITTING CUT OUT FROM STA 1380 TO STA 1440 IAW BOEING 757 SRM 51-10-02. 2L72 4F RTA2NM 20050712002062005071200206NM 2005 7 12 AWXA200500790 120050619A5320BAC1510335 FLOOR SUPPORT BOEING757 7572G7 1384963NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28909AW 24522 SAL - MAJOR REPAIR - DURING C1 CHECK DISCOVERED GALVANIC CORROSION LOCATED ON THE FLOOR SUPPORT EXTRUSION AT STA 1718, BL 0, WL 208.1. NO ALLOWABLE DAMAGE LIMITS FOUND. MAINTENANCE REMOVED CORRODED FLOOR EXTRUSION LOCATED AT STA 1718, BL 0, WL 208.1 IAW BOEING 757 SRM 51-40-02 PG 1. INSTALLED REPLACEMENT FLOOR EXTRUSION AT STA 1718, BL 0, WL 208.1 IAW BOEING 757 SRM 51-40-02. 2L72 4F RTA2NM 20050712002072005071200207NM 2005 7 12 AWXA200500791 120050619A5347146N5130 SEAT TRACK BOEING757 7572G7 1384963NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28909AW 24522 SAL - MAJOR REPAIR - DURING C1 CHECK FOUND CORROSION ON SEAT TRACK LOCATED AT STA 1560, BL 24.5R, WL 208.1. MAINTENANCE REMOVED CORROSION AT SEAT TRACK LOCATED AT STA 1560, BL 24.5R, WL 208.1 IAW BOEING 757 SRM 53-00-52 AND FOUND OUT OF LIMITS IAW BOEING 757 SRM 53-00-52 FIG 101. REMOVED SEAT TRACK AT STA 1560, BL 24.5R, WL 208 AND INSTALLED REPLACEMENT SEAT TRACK IAW BOEING 757 SRM 51-40-02. 2L72 4F RTA2NM 20050712002102005071200210EU 2005 7 12 AWXA200500802 120050706A3230 LANDING GEAR AIRBUS320 A320231 3930325EU MAINS MALFUNCTIONED A AWXAO OTHER J WARNING INDICATION CLCLIMB 1 WP28644AW 317 AFTER TAKEOFF MLG HANDLE UP, ECAM CAUTION: L/G GEAR NOT UPLOCKED. CYCLED MLG PER ECAM ALL GEAR UP & LOCKED OK. MX CYCLED MLG, OPS CHK GOOD. ACFT RETURNED TO SERVICE. WITHIN 8 CYCLES DISCREPANCY RETURNED. ACFT MX FERRIED BACK TO PHX. SEVERAL SENSORS INSPECTED, ADJUSTED & REPLACED IAW AIRBUS MM. NLG RESTRICTORS 2535GM, 2536GM & 2691GM REPLACED. MLG SELECTOR VALVE 40GA CHANGED, NLG DOOR BYPASS VALVE REPLACED. R & R RELAYS 48GA AND 53GA. TEAR DOWN REPORT CONFIRMS REPLACEMENT OF MLGCU. FOUND S1 SWITCH FAULTY. SWITCH REPLACED & UNIT TESTED OK. ALL WORK PERFORMED IAW CMM 32-31-13 REV 9. 2L72 4F RTA28NM 20050712002112005071200211EU 2005 7 12 AWXA200500792 120050709A3397ABS0374A24 WIRE HARNESS AIRBUS320 A320232 3930326EU EMERGENCY LIGHT DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 ORD - EEL - DURING 8 DAY CHECK THE EMERGENCY EXIT LIGHT, AT ROW 26L, FAILED OPERATIONAL CHECK. MAINTENANCE REMOVED AND REPLACED THE WIRING HARNESS UNDER THE SEAT AT ROW 26L. 2L72 4F RTA28NM 20050712002122005071200212EA 2005 7 12 MASA200500456 120050610A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSBROKEN A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0777331 7331 EMERGENCY EXIT SIGN ON SERVICE DOOR INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE. 2L72 4F RTA21EA 20050712002132005071200213NM 2005 7 12 AWXA200500793 120050710A3350321454 POWER SUPPLY AIRBUSA319 A319132 3930340NM RT OVERWING FAILED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28829AW 1563 PHX - EEL - DURING 8 DAY CHECK THE OPERATIONAL TEST OF EMERGENCY LIGHTS FAILED. MAINTENANCE REMOVED AND REPLACED THE RT ESPU IAW TASK CARD A133302. OPERATIONAL TESTS WERE GOOD. 2L72 4F RTA28NM 20050712002152005071200215EA 2005 7 12 MASA200500458 120050611A3350 LIGHT CNDAIRCL600 CL6002D24 1390016EA EMERGENCY LIGHTSINOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07906FJ 15006 AFT CEILING EMERGENCY FLOODLIGHT 1 BULB INOPERATIVE. RESET. OPS CHECKED GOOD. 2L72 4F RTA21EA 20050712002172005071200217NM 2005 7 12 AWXA200500796 120050625A552365C2638416A SKIN BOEING737 7373G7 1384595NM RT ELEVATOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 MCN - MAJOR REPAIR - DURING C16 CHECK FOUND RT ELEVATOR TAB CRACKED IN 2 PLACED AT THIRD UPPER HINGE CUTOUT, INBOARD CORNER, FROM ELEVATOR STA 55.075 TO ELEVATOR STA 56.075. MAINTENANCE REPAIRED RT ELEVATOR TAB CUTOUT BY REMOVING DAMAGED AREA LOCATED AT THIRD UPPER HINGE CUTOUT, INBOARD CORNER OF THE RT ELEVATOR TAB. OBTAINED MATERIAL FOR REPAIR THEN BONDED REPAIR IAW BOEING 737-300 SRM 51-70-05-0 FIG 17. 2L72 4F RTA16WE 20050712002182005071200218NM 2005 7 12 AWXA200500797 120050630A5320654583311 WEB BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 MCN - MAJOR REPAIR - DURING C-16 CHECK FOUND FLOOR WEB SHEAR TIE CRACKED 1.5 INCHES IN LENGTH. CRACK LOCATED AT FRAME CUTOUT, BS 197, WL 207, LBL 28. MAINTENANCE REMOVED CRACKED FLOOR WEB AT FRAME CUT OUT, BS 197, WL 207, LBL 28 IAW BOEING 737-300 SRM 51-40-02-0 FIG 8. FABRICATED NEW FLOOR WEB SHEAR TIE IAW BOEING DWG 65-45833. INSTALLED FABRICATED REPAIR PARTS AT FRAME CUTOUT, BS 197, WL 207, LBL 28 IAW BOEING 737-300 SRM 51-40-02-0 FIGS 8 AND 12. 2L72 4F RTA16WE 20050712002202005071200220NM 2005 7 12 AWXA200500798 120050629A5753BACB30NR6K BOLT BOEING737 7373G7 1384595NM FLAP CARRIAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED GALVANIC CORROSION ON 4 BOLTS LOCATED AT THE LT INBOARD MID FLAP OUTBOARD CARRIAGE. THERE ARE NO LIMITS ON CORRODED BOLTS. MAINTENANCE REMOVED AND REPLACED THE 4 BOLTS FOR THE LT INBOARD MID FLAP, OUTBOARD CARRIAGE IAW BOEING SOPM 20-50-01. 2L72 4F RTA16WE 20060217000522006021700052NM 2006 2 17 UPS06M46162 120051216A5510 BEARING DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01282UP 48452 INSPECTION TYPE:C EMPENNAGE-BARREL NUT HOLE NR 36 LT FOUND BEARING WITH SURFACE CORROSION ON SIDE AND BOTTOM AREA. CORROSION REMOVAL C/OUT ON AFFECTED AREA PER SRM 51-21-01.V2.R38, FOUND BLEND OUT EXCEEDED LIMIT PER MD11-5510-19409-K FIG5. REPAIR SLEEVE BUSHING FAB PER MD11-5510-19409-K, APPLIED SEALANT PR1422B 1/2 ON SLEEVE AND AFFECTED BORE AREA. INSTALLED REPAIR SLEEVE BUSHING ON B/N HOLE NR 36 LT BORE, REPAIR ACCOMPLISHED AT B/N HOLE NR 36LH PER EN 1617-05, FOUND SATIS. 2L73 4F RTA22WE 20060221001572006022100157SW 2006 2 21 ALGA106433 120050922A6321 BEARING BELL 412 412 1182202SW QUILL ASSY FAILED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03XASYL MB4718 36101 TRANSMISSION ASSY MAKING METAL, DISSEMBLED FOUND ROTOR BRAKE QUILL DUPLEX BEARING BEARING BREAKING DOWN. / REMOVEN AND REPLACED DUPLEX BEARING P/N 222-342-420-101 1G72 4U H4SW 20060221002372006022100237NM 2006 2 21 UPS06M46177 120051208A5754 SKIN DOUG MD11 MD11F 3023600NM L/E SLAT CHAFED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01282UP 48452 INSPECTION TYPE:C RHW DROOP L/E SLAT LWR I/B EDGE FOUND CHAFING MARK. CHAFING MARK BLENDED AND PROTECTED PER SRM51-21-01.V2.R.38.ORI THK 0.069 MAT REMOVED 0.055", REMAIN MAT THK 0.014", FOUND EXCEEDED LIMIT. REWORKED AREA EDGE TRIMMING FOUND REMAIN MAT THK 0.035". FASTENER EDGE DISTANCE IS 0.312" AND FASTENER HOLE SIZE IS 0.157" WITHIN LIMIT PER EN1005-06. RE WORK ACCOMPLISHED PER EN1005-06, FOUND SATIS. 2L73 4F RTA22WE 20060221002432006022100243NM 2006 2 21 UPS06M46168 120051206A2810 FUEL TANK DOUG MD11 MD11F 3023600NM CENTER CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01282UP 48452 INSPECTION TYPE:C CABIN, CORROSION ON UPPER SURFACE OF UPPER CTR FUEL TANK AROUND FASTENER HEAD AT STA1209-1239 X=+.97 TO+107. FASTENERS REMOVED FOR ACCESS AT STA1209-1239, CORROSION REMOVAL C/OUT PER SRM 51-21-01.V2.R38, FOUND EXCEEDED LIMIT. C/OUT MAGNIFIED V/INSP AND FPI FOUND SATIS. FLAP PEENING C/OUT ON REWORKED AREAS PER CMM20-11-01R.51, IAW EN1009-06. INSTALL FASTENERS AND REPAIR ACCOMPLISHED PER EN1009-06, FOUND SATIS. 2L73 4F RTA22WE 20060221002842006022100284WP 2006 2 21 DHL2005803504 120051117A5713 FRAME DOUG DC8 DC873 302199CWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 ITEM REF NR 033451: RT WING CTR LE LWR FORMER CRACKED 1 INCH XFS 347.750. PERFORMED STOP HOLE ON CRACK END AND FABRICATED ANGLE DOUBLER (AL7075T6 0.040") IAW SRM 57-2-0 PG. 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH FASTENERS (HILOKS) IAW SRM 57-2-0 PG. 9-10, SRM 561-1-20D. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20060221002852006022100285WP 2006 2 21 DHL2005803505 120051116A5753 SKIN DOUG DC8 DC873 302199CWP T/E FLAP WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 ITEM REF NR 032704: RT OUTBD FLAP UPPER SURFACE WORN (STA XF 203.000-210.000) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG. 4, TR 57-94. REMOVED DAMAGED PLATING IAW SRM 57-1-0 PG. 1, SRM 51-1-21. FABRICATED NEW PLATING (AL 2024T3 0.040") IAW SRM 57-7-1 FIG. 4, TR 57-94 ITEM "C". CLEANED, TREATED AND PRIMED AREA AND PLATING INNER SIDE IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG. 9. INSTALLED NEW PLATING IAW SRM 51-1-21, SRM 51-3-0, SRM 51-3-1 (TORQUE). 2L74 4F RT4A25 20060221002872006022100287WP 2006 2 21 DHL2005803507 120051116A5753 SKIN DOUG DC8 DC873 302199CWP T/E FLAP WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 ITEM REF NR 038897: LT WING INBD FLAP PLATING UPPER PART WORN 1" XW 104.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG. 1. REMOVED DAMAGED PLATING IAW SRM 51-1-21. FABRICATED NEW PLATING (AL 2024T3 0.040") IAW SRM 57-7-1 FIG. 1 ITEM D. CLEANED, TREATED AND PRIMED AREA AND NEW PLATING INTERNAL PART IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG. 9. INSTALLED NEW PLATING IAW SRM 51-1-21 2L74 4F RT4A25 20060221002892006022100289WP 2006 2 21 DHL2005803509 120051117A5542 SKIN DOUG DC8 DC873 302199CWP RUDDER CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 ITEM REF NR 033464: RUDDER SKIN DELAMINATED AT STA ZR 166.656 AND LEVEL 2 CORROSION (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 55-6-1 FIG. 1. REMOVED DAMAGED PANEL PLATING IAW SRM 55-1-0, SRM 51-1-21. REMOVED CORROSION FROM RUDDER SKIN AT ZR 166.656 IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 55-2-0 PG. 12. FABRICATED NEW PLATING AND BONDED FINGER DOUBLER (AL 2024T3 0.016") IAW SRM 55-6-1 FIG. 1 ITEM "A". STUCK BOTH PARTS IAW SRM 51-1-9. CLEANED, TREATED AND PRIMED AREA AND INNER SIDE OF NEW PANEL PLATING IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACE IAW SRM 51-1-11 PG. 9. INSTALLED NEW PANEL PLATING IAW SRM 51-1-21. FOR WEIGHT SEE NR 039066. 2L74 4F RT4A25 20060221002902006022100290WP 2006 2 21 DHL2005803510 120051116A53204751625U1 FITTING DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 ITEM REF NR 033357: MAIN CARGO COMPT FITTING CRACKED 3.500 INCHES STA 680.000 L-11R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG.1. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D (HI LOK) SRM 51-1-23 (PLI WASHER), SRM 51-3-0 (NUT) SRM 51-3-1 PG. 2A (TORQUE). 2L74 4F RT4A25 20060221003412006022100341EA 2006 2 21 SWIA200516261 120050917A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07405SW 7029 CRACKED ANGLE FS 625 RBL33 WL90.0 AFT SIDE PRESSURE BULKHEAD AFT EQUIPMENT BAY, ITEM FOUND AT C CHECK INSPECTION. INSTALLED NEW ANGLE TO AFT SIDE OF PRESSURE BULKHEAD AT FS625 RBL33 WL90.0 IAW CRJ200 SRM 51-42-06 PG 11-12. 2L72 4F RTA21EA 20060221003422006022100342EA 2006 2 21 SWIA200516262 120050917A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07405SW 7029 RT FS 280 CRACKED AT TOP SIDE, ITEM FOUND AT C CHECK INSPECTION. INSTALLED ANGLE IAW DWG 601R-11436 AT FS 280. 2L72 4F RTA21EA 20060221003432006022100343EA 2006 2 21 SWIA200516263 120050917A5720 ANGLE CNDAIRCL600 CL6002B19 1900309EA RT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07405SW 7029 RT BATT ANGLE CRACKED, ITEM FOUND AT C CHECK INSPECTION. INSTALLED ANGLE DOUBLER PER REO 601R-57-51-046 REV 'B STEPS 5-10 OF RT BAT ANGLE. 2L72 4F RTA21EA 20060221003442006022100344EA 2006 2 21 SWIA200516264 120051002A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07925SW 7682 INBD AND OTBD ANGLES CRACKED AT FS 280 LBL 9, ITEM FOUND AT C CHECK INSPECTION. INSTALLED NEW CLIPS AT FS 280 LBL 9 IAW REO 601R-53-11-136 CRJ200 SRM 51-42-06; PG 1-21; 51-42-21 PG 1-21; CW REO 601R-53-11-136. 2L72 4F RTA21EA 20060221003452006022100345EA 2006 2 21 SWIA200516265 120051002A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07925SW 7682 INBD AND OTBD ANGLES CRACKED AT FS 280 RBL 9.0, ITEM FOUND AT C CHECK INSPECTION. INSTALLED IB BRACKET IAW CRJ200 SRM 51-40-11 AND REO 601R-53-11-136. 2L72 4F RTA21EA 20060221003462006022100346EA 2006 2 21 SWIA200516266 120051002A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07925SW 7682 OTBD ANGLE CRACKED AT FS 280 LBL9 ITEM FOUND AT C CHECK INSPECTION. INSTALLED NEW OB CLIP AT FS 280 LBL 9 IAW REO 601R-53-11-136 CRJ200 SRM 51-42-06 PG 1-21; 51-42-21 PG 1-21; CW REO 601R-53-11-136. 2L72 4F RTA21EA 20060221003472006022100347EA 2006 2 21 SWIA200516267 120051002A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07925SW 7682 OTBD ANGLE CRACKED AT FS 280 RBL9, ITEM FOUND AT C CHECK INSPECTION. INSTALLED OB BRACKET IAW CRJ200 SRM 51-40-11 AND REO 601R-53-11-136. 2L72 4F RTA21EA 20060221003562006022100356EA 2006 2 21 SWIA200516250 120050912A5347 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07408SW 7055 CORROSION FOUND ON SEAT TRACK RBL 9 + STA 559 + 80 - STA 559 + 112, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW SEAT TRACK IAW CRJ SRM 51-41-02 AND 51-23-00. 2L72 4F RTA21EA 20060221003572006022100357EA 2006 2 21 SWIA200516251 120050912A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07408SW 7055 FUSELAGE, FRAME STATION 265 STR 16 LT, FRAME FLANGE DAMAGED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW REO 601R-53-11-927. 2L72 4F RTA21EA 20060221002442006022100244NM 2006 2 21 UPS06M46169 120051214A2810 FUEL TANK DOUG MD11 MD11F 3023600NM CENTER CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01282UP 48452 INSPECTION TYPE:C, CABIN-UPPER SURFACE OF UPPER CTR FUEL TANK AROUND FASTENERS HEAD AT STA 1159-1209X=97.70 TO 107.00 FOUND CORROSION. FASTENERS AT UPPER SURFACE CTR F/TANK AT STA1159-1209 REMOVAL FOR ACCESS. CORROSION REMOVAL C/OUT PER SRM51-21-01.V2.R38, FOUND EXCEEDED LIMIT. C/OUT MAGNIFIED V/INSP AND FPI FOUND SATIS. FLAP PEENING C/OUT ON REWORKED AREA PER CMM20-11-01.R51, IAW EN1009-06. INSTALL FASTENERS AND REPAIR ACCOMPLISHED PER EN1009-06, FOUND SATIS. 2L73 4F RTA22WE 20060221002502006022100250WP 2006 2 21 DHL2005803502 120051116A5321 FLOOR PANEL DOUG DC8 DC873 302199CWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 ITEM REF. NR. 033228: MAIN CARGO COMPT INTERIOR FLOOR PANEL SUPPORT CORRODED, STA 1726.000 RBL 30. REMOVED CORROSION IAW SRM 51-1-8 PG. 17-18. MEASURED THICKNESS 0.090". BLEND OUT 0.024", REMAINING MATERIAL 0.066". FOUND OUT OF ALLOWABLE LIMITS IAW SRM 53-2-0 FIG. 1 SHEET 3. FABRICATED DOUBLER (EXTRUSION PN 52537716 0.090") IAW SRM 53-2-0 FIG. 1G. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 53-2-0 FIG. 1G, SRM 51-1-20D. TORQUED IAW SRM 51-3-1 PG. 2A. 2L74 4F RT4A25 20060221002932006022100293WP 2006 2 21 DHL2005803540 120051128A5720 FITTING DOUG DC8 DC873 302199CWP NR 4 ALT TANK CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 ITEM REF NR 039051: NR 4 ALT TANK S-64 END CRACKED 1 INCH STA XRS 445.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-2 FIG. 3D TR# 57-86. REMOVED FASTENERS IAW SRM 51-1-20D. FABRICATED REPAIR ANGLE (EXTRUSION AND 101342003 0.090") IAW SRM 57-2-2 FIG. 3D SHEET 2, TR# 57-86, SRM 57-4-3 FIG. 6 ITEM "D". TAPERED REPAIR ANGLE FROM 0.090" TO 0.063" IAW SRM 57-2-2 FIG. 3D SHEET 1, TR 57-86. CLEANED, TREATED AND APPLIED YELLOW TOP COATING IAW SRM 51-1-12 PG. 7,25. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-12. INSTALLED REPAIR ANGLE IAW SRM 51-1-20D. TORQUED IAW SRM 51-3-1. FOR LEAK CHECK REFER TO NR. 039053 2L74 4F RT4A25 20060221002942006022100294WP 2006 2 21 DHL2005805003 120051104A361032143262 REGULATOR VALVE DOUG DC8 DC873F 302199FWP NR 2 ENGINE MALFUNCTIONED A DHLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01805DH 46125 ON TAKEOFF NR 2 ENGINE OVERPRESS LIGHT ILLUMINATED. REJECTED T/O A/C WEIGHT 252000 IAS 20KTS OAT 13C PA 1000FT. DEFFERRED NR 2 HIGH PRESS 9TH STAGE REG & SO VALVE IAW MEL 36-1-5 SPEC PROC C/W NR 2 HS PRESS 9TH STAGE REG & SO CLOSED. DMI NR 23103 PLACARDS INSTALLED. REF DMI NR 23103/ ON TAKE OFF THRU 20 KTS THE NR 2 ENGINE OVERPRESSURE LIGHT ILLUMINATED. R/R NR 2 ENG PRESS REG VALVE IAW DC8MM 36-12-1 PERFORMED ENG RUN IAW JRH MANUAL AND PNEUMATIC TEST SYST OPS CK'D GOOD THIS ACTION CLEARS DMI NR 23103 PLACARDS REMOVED. 2L74 4F RT4A25 20060222000292006022200029CE 2006 2 22 S2YA05066 120051013A2750100384040 MOTOR BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE FLAP SYS DAMAGED A S2YAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 GL13901SK UE90 SHORTLY AFTER TAKEOFF, THE CREW REPORTED THE FLAPS WERE AT 17 DEGREES AND WILL NOT RETRACT. THE AC CONTINUED WITH THE FLAPS AT 17. THE FLAPS WERE RAISED USING THE OVERRIDE SWITCH AND THE SYSTEM WAS PUT ON MEL. DISCOVERED THE FLAP MOTOR/GEAR BOX STRUGGLING TO MOVE AND THE RT FLEX DRIVE CABLES NEAR THE GEARBOX TWISTED AT THE SPLINE. MX REPLACED THE FLAP MOTOR, GEAR BOX AND BOTH RT FLEX DRIVE CABLES. WITH ALL OPS CHECKS WERE GOOD AND NO FURTHER DEFECTS RETURNED THE AC TO SERVICE. (K) 2L72 4T4 TRTA24CE E26NE 20060222000792006022200079WP 2006 2 22 05FDEA04142 120051205A5520 REPAIR DOUG DC10 DC1030F 3023504WP GE CF6 CF6* 30020GL ELEVATOR DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 DISCREPANCY IN THE UPPER SURFACE OF RT DETACHABLE ELEVATOR AT STA XE 80 FOUND 1EA REPAIR DOUBLER 3.5 INCH DIA. PERFORMED A GVI OF REPAIR IAW SRM 55-00-01 FIG 3 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001-2P, RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 PAR 33 VOL 2. 2L73 4F4 FRTA22WE E23EA 20060222001052006022200105NM 2006 2 22 05FDEA04340 120051215A5700 REPAIR BOEING727 727200 138407ENM RT WING UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25274FE 22039 FOUND PREVIOUS REPAIR ON RIGHT WING NR 7 L/E SLAT WAS ACCOMPLISHED IAW SRM 57-50-3 FIG 1 BASED ON AN EXTERNAL EVALUATION CONSISTED OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL THICKNESS AND GENERAL WORKMANSHIP, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2L73 4F RTA3WE 20060222001072006022200107NM 2006 2 22 05FDEA04344 120051215A5700 REPAIR BOEING727 727200 138407ENM UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25274FE 22039 FOUND PREVIOUS REPAIR ON UPPER LEADING EDGE OF LEFT WING AT NR 3 LEADING EDGE SLAT WAS ACCOMPLISHED IAW SRM 57-30-4, FIG 1. BASED ON AN EXTERNAL EVALUATION CONSISTED OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS, GENERAL WORKMANSHIP, REPAIR CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100. 2L73 4F RTA3WE 20060222001402006022200140CE 2006 2 22 DJFA2005172 120051208A7897 WIRE CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE THRUST REVERSER DAMAGED E DJFAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA23593CW 5600223 PCE108407 DURING TAKEOFF WHILE PASSING THROUGH 800 FT AGL THE CREW RECEIVED A MASTER WARNING ANNUNCIATOR WITH THE ASSOCIATED LT THRUST REVERSER ARM AND UNLOCK LIGHTS. THE EMERGENCY STOW SWITCH WAS PLACED IN THE EMERGENCY POSITION AND THE THRUST REVERSER LEVER WAS CONFIRMED AS BEING DOWN. PRIORITY HANDLING WAS REQUESTED AND THE AIRCRAFT WAS DIVERTED AND WHERE A LANDING WAS MADE WITHOUT FURTHER INCIDENCE. MAINTENANCE ISSUED MEL 78-1 FOR BOTH LT AND RT THRUST REVERSER SYSTEMS. ON 10 DECEMBER, 2005 A WIRE WAS REPAIRED LEADING TO THE STOW LIMIT SWITCH. THE THRUST REVERSER LOCK OUTS WERE REMOVED AND OPERATIONAL CHECKS OF THE THRUST REVERSER SYSTEMS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA22CE E25EA 20060222001412006022200141EU 2006 2 22 05FDEA04241 120051209A2420 GENERATOR AIRBUS330 A300* EU GE CF6 CF680 30025NE NR 1 FAILED A FDEAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 SO25662FE 761 REMOVED AND REPLACED NR1 GCU I/A/W M.M 24-22-12-4, PERFORMED ENG RUN NR 1 GEN. OPS CHECKS GOOD. R/I 10DEC05 07:13 PHL R R/I FROM FACT PREMATURE REMOVAL/INSTALLATION OFF MFG 764067A SRL A115 ON MFG 764067A SRL 0359. 2L72 4F4 FRTA26NM E13NE 20060222001432006022200143NM 2006 2 22 A0512001 120051122A2700 JACKSCREW BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE FAILED A K11AO OTHER FEJFLT CONT AFFECTED VIBRATION/BUFFET WARNING INDICATION APAPPROACH 1 EA23720CK 21298 ON APPROACH, WITH FLAPS SELECTED TO 5 DEG, STAB TRIM WHEEL RAN AWAY FROM APPROX 5 UNITS NOSE UP TO 0 DEG AND BUFFETING WAS FELT IN FLT CONTROLS. AC STARTED A 2000 TO 4000 RPM RATE OF DESCENT, PILOTS TRIED TO INPUT UP ELEVATOR TO ARREST SINK RATE, THERE WAS NO EFFECT ON FLIGHT PATH. ELEVATORS HAD LOST THEIR AUTHORITY EVEN THOUGH SPEED WAS WELL ABOVE FLAPS 5 MANEUVERING SPEED. AC WAS ONLY 3000 FT. AGL AT THIS POINT. FULL POWER WAS ADDED ON ALL 3 ENGINES, WHICH WERE FUNCTIONING NORMALLY, EVEN THOUGH PITCH WAS AT APPROX ZERO DEG, IT TOOK A LONG TIME TO ARREST SINK RATE AND ELEVATORS FINALLY BEGAN RESPONDING AT APPROX. 1000 FT.AGL FROM WHICH AC WAS LANDED SAFELY. MAIN REPLACED HORIZ STAB JACKSCREW AND GEARBOX. 2L73 4F4 FRTA3WE E2EA 20060222001442006022200144NM 2006 2 22 20018 120051211A2700H188L INDICATOR DHAV DHC8 DHC8103 1386005NM PWA PW121 PW121 52124NE PFCS FALSE INDICATIONA KPVAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 WP13809WP 146 ON TAKE OFF ROLL, PFCS INDICATOR SHOWED RT SIDE SPOILERS DEPLOYED AFTER ADVANCING TAKEOFF POWER WITH CONTROLS IN NEUTRAL POSITION. REMOVED AND REPLACED PFCS INDICATOR IAW PSM 1-8-2, 27-05-00 PG. 201-203. OPS CHECK PASS IAW PSM 1-8-2, 27-00-05 PG. 204-206. 2H72 4T4 TRTA13NM E20NE 20060222001462006022200146NM 2006 2 22 200517 120051211A2611475054 SMOKE DETECTOR DHAV DHC8 DHC8103 1386005NM PWA PW121 PW121 52124NE FALSE INDICATIONA KPVAO OTHER N FALSE WARNING CLCLIMB 1 WP13811WP 366 SMOKE WARNING ILLUMINATED NUMEROUS TIMES IN FLIGHT. PREFORMED SMOKE WARNING ADJ/TEST IAW MM 26-12-00 PG. 201. ADJ/TEST GOOD. REMOVE AND REPLACED NR 2 SMOKE DETECTOR. PREFORMED ADJ/TEST GOOD. IAW MM 26-12-00 PG. 207. 2H72 4T4 TRTA13NM E20NE 20060222001472006022200147EA 2006 2 22 REXA200500153 120051210A2750865D1007 PDU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE TE FLAPS INOPERATIVE A REXAO OTHER J WARNING INDICATION APAPPROACH 1 SO258721B 7721 FLAPS FAILED AT 20 ON APPROACH, QRH FOLLOWED WITH UNEVENTFUL LANDING. REMOVED AND REPLACED POWER DRIVE UNIT IAW AMM SYSTEM OPERATIONALLY CHECKED GOOD. 2L72 4F4 FRTA21EA E15NE 20060222001482006022200148CE 2006 2 22 BSYA200500029 120051108A3260 SQUAT SWITCH BEECH 58 58 1152740CE CONT O520 IO520* 17032SO MLG INOPERATIVE E BSYAA UNSCHED LANDING O OTHER CLCLIMB 1 GL0778RE TH371 ON TAKEOFF, PILOT SELECTED GEAR UP NOTHING HAPPENED, THEN ELECTED TO RETURN. MAINTENANCE JACKED AIRCRAFT CLEANED AND LUBED SQUAT SWITCH. OPS CHECKED GOOD. 1L72 3O3 O 3A16 E5CE 20060222000722006022200072CE 2006 2 22 DJFA2005165 120051122A5280 DOOR BEECH MU300 400A 1155402CE PWA JT15 JT15D5 52112NE MLG LOOSE E DJFAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA23442CW RK42 WITH LANDING GEAR IN UP POSITION GEAR DOOR LIGHT WOULD REMAIN ILLUMINATED. WHILE AC WAS BEING RETURNED. A LOW-PASS WAS FLOWN PAST TOWER AND CONFIRMED SOMETHING WAS HANGING DOWN FROM AC. TOWER DECLARED AN EMERGENCY, CREW PERFORMED A MANUAL LANDING GEAR EXTENSION IN AN UNSUCESSFUL ATTEMPT TO GET GEAR DOOR TO CLOSE. A SOFT LANDING WAS MADE. IB LT MAIN GEAR DOOR WAS CONFIRMED TO BE HANGING DOWN. HEAVY ACCUMULATION OF ICE ON IB LT MAIN GEAR DOOR AND LT GEAR DOOR UPLOCK ROLLER. UPLOCK HOOK AND SWITCH WERE FOUND TO BE OUT OF ADJUSTMENT. UPLOCK HOOK AND SWITCH WERE ADJUSTED, AND LT MLG DOOR WAS REPLACED. OPS AND LEAK CHECKS WERE GOOD. AC RETURNED TO SERVICE. 2H72 4F4 FRTA16SW E25EA 20060222000772006022200077NM 2006 2 22 05FDEA04109 120051203A2910BACU24X8 UNION BOEING727 727200 138407ENM PWA JT8 JT8D* NE HYD SYSTEM LEAKING A FDEAA UNSCHED LANDING K FLUID LOSS CLCLIMB 1 SO25240FE 20978 AFTER T/O WHEN GEAR LVR WAS RAISED TO THE UP POS THE HYD SYS (A) RESERVOIR WENT TO ZERO. THE GEAR REMAINED DOWN AND FLAPS STAYED AT 15 DEG. REMOVED AND REPLACED PACKING AND UNION FOR THE OB TE FLAP CONTROL VALVE IAW IPC REF 27-50-00-30AZZ ITEM 145. LEAK AND OP CK, GOOD ON ENG RUN. DEBRIEF INDICATED THAT (A) PUMPS OPERATED FOR 15 MIN AT ZERO QTY. REMOVED AND REPLACED NR 1 AND NR 2 ENG DRIVEN HYD PUMPS IAW MM 29-11-033-4. REMOVED AND REPLACED BOTH NR 1 AND NR 2 ENG HYD CASE DRAIN FILTERS. SERVICED AND CYCLED ALL FLT CONTROLS NUMEROUS TIMES AND RESERVICED HYD AFTER SHUTDOWN. 2L73 4F4 FRTA3WE E2EA 20060222000782006022200078NM 2006 2 22 05FDEA04143 120051205A56105893543109 WINDOW BOEING727 727200 138407ENM COCKPIT BROKEN A FDEAA UNSCHED LANDING O OTHER CLCLIMB 1 SO25237FE 5971 21331 PDIS 237 56-10 0007743 04DEC05 FSD CLOSE R AT FL200, CAPT'S NR1 WINDSCREEN OUTER PANE CRACKED. TURNED CAPT'S WINDOW HEAT OFF AND COMPLIED WITH QRH PROCEDURE. FACT 04DEC05 23:58 FSD U REMOVED AND REPLACED L-1 WINDOW IAW AMM 56-11-011-4. ALSO REMOVED AND REPLACED L-1 WINDOW HEAT CONTROLLER IAW AMM 30-41-013-5. OPS CHECKS GOOD. OK FOR SERVICE. 2L73 4F RTA3WE 20060222000822006022200082CE 2006 2 22 DJFA2005170 120051204A3230MS243311 SWITCH BEECH MU300 400A 1155402CE PWA JT15 JT15D5 52112NE RT MLG INTERMITTENT E DJFAO OTHER O OTHER APAPPROACH 1 EA23478LX RK387 AFTER LANDING GEAR WAS SELECTED DOWN DURING APPROACH THEY ONLY RECEIVED A GREEN NOSE AND LT GEAR INDICATION. NO RT GEAR INDICATION WAS RECEIVED, RED IN-TRANSIT LIGHT DID NOT ILLUMINATE AND GEAR HORN DID NOT SOUND. RT GEAR INDICATION WAS NOT RECEIVED AFTER AN EMERGENCY GEAR EXTENSION WAS PERFORMED. AN EMERGENCY WAS DECLARED, AC LANDED WITHOUT FURTHER INCIDENT. FOLLOWING LANDING, RT LANDING GEAR INDICATION WAS RECEIVED. REPLACED RT GEAR DOWN LOCK SWITCH AND RE-ROUTED WIRING TO DOWN LOCK POSITION SWITCH AT RT MLG TO AVOID JAMMING. RT MLG BULB WAS FOUND TO HAVE MINOR DEFECT, WAS REPLACED. LANDING GEAR OPS WERE FOUND TO BE GOOD AFTER SEVERAL GEAR CYCLES. CK FLT WAS COMPLETED AND AC RETURNED TO SERVICE. 2H72 4F4 FRTA16SW E25EA 20060223000032006022300003WP 2006 2 23 05FDEA04299 120051214A5101 REPAIR DOUG DC10 DC1010 3022110WP BS 1159 NONE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25563FE 46948 DISCREPANCY FOUND SPLICE REPAIR INSTALLED AT FRAME STATION 1159 LT SIDE CORRECTIVE ACTION PERFORMED INSPECTION ON SPLICE REPAIR IAW ESO NR 7346-1275302JP FOUND IAW CRITERIA REQUEST BY EO 8-5100-7-5001 P2. 2L73 4F A22WE 20060223000042006022300004WP 2006 2 23 05FDEA04300 120051214A5101 REPAIR DOUG MD10 MD1010F 3022112WP GE CF6 CF6* 30020GL CARGO DOOR NONE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25563FE 46948 DISCREPANCY CENTER CARGO DOOR FWD LWR CORNER HAS AN EXTERNAL REPAIR DOUBLER INSTALLED CORRECTIVE ACTION PERFORMED INSPECTION ON EXTERNAL REPAIR DOUBLER IAW 1255201JP ESO 7349 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2. 2L73 4F4 FRTA22WE E23EA 20060223000052006022300005CE 2006 2 23 DJFA2005173 120051212A329765183543 PCB CESSNA525 525 2076601CE WILINTFJ44 FJ44 66000GL CABIN DEFECTIVE E DJFAO OTHER O OTHER LDLANDING 1 EA23254CW 5250154 LANDING GEAR WAS SELECT DOWN, CREW RECEIVED LT AND RT MAIN GEAR GREEN DOWN, LOCKED IND WITH NO NOSE GEAR IND. RED GEAR UNLOCK LIGHT WAS NOT ILLUMINATED. FLAPS EXTENDED TO LANDING POSITION, THROTTLES RETARDED TO IDLE, NML GEAR DOWN, LOCKED IND WAS GIVEN BY ABSENCE OF GEAR UNSAFE WARNING HORN. EMER GEAR EXT WAS PERFORMED, 3 GREEN GEAR IND LIGHTS WERE NOT RECEIVED. AN EMER WAS DECLARED. TOWER INFORMED CREW LANDING GEAR APPEARED TO BE DOWN AND LOCKED. AC LANDED W/O INCIDENT. REPAIRED BROKEN WIRE AT PIN J OF FWD PRESS BLKHD, SEVERAL WIRES, BLKHD CONNECT JN007. PRINTED CB PC044 FOR GEAR LOGIC WAS REPLACED AFTER FOUND DEFECTIVE. LANDING GEAR WAS CYCLED, ALL OP CHECKS WERE NML. AC WAS RETURNED TO SERVICE. 1L72 4F4 FRTA1WI E3GL 20060223000082006022300008WP 2006 2 23 05FDEA04272 120051213A5330 REPAIR DOUG DC10 DC1030F 3023504WP BS 655-675 MISINSTALLED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25302FE 46801 DISCREPANCY PERFORMED INSPECTION IAW EO 8-5100-7-5001-1P FOUND 1 DOUBLER DIMENS 13" BY 10" RT EXT FUSELAGE STA 665 LONG 41. REMOVED DOUBLER IAW SRM 51-30-00 AND SRM 51-35-02 STRIPPED PAINT IAW SRM 51-21-01 VOL 2. REMOVED FINGER DOUBLER EXTERNAL IAW SRM 51-35-01 VOL 1. REMOVED CHANNEL AND BUMPER FOR ACCESS IAW DC10-30 MM 20-50-02. ACCOMPLISHED REPAIR IAW BOEING ROD SKETCH 05-10-18-004R1 AND FEDEX EA NR 8-5330-93228. INSTALLED CHANNEL AND BUMPER IAW DC10-30 MM 20-50-02. REPROTECTED AREA AND SEAL REPAIR IAW SRM 51-21-01 VOL 2. 2L73 4F RTA22WE 20060223000112006022300011NM 2006 2 23 05FDEA04342 120051215A5700 REPAIR BOEING727 727233 138408ANM FOREFLAP UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25274FE 22039 FOUND PREVIOUS REPAIR ON LT OUTBOARD FOREFLAP LEADING EDGE WAS ACCOMPLISHED IAW SRM 57-50-4, FIG 1, BASED ON AN EXTERNAL EVALUATION CONSISTED OF LOCATION, SHAPE, SIZE, MATERIAL THICKNESS AND TYPE, FASTENERS NUMBER AND SPACING AND GENERAL WORKMANSHIP, REPAIR IS CLASSIFIED AS MAJOR REPAIR PER FEDEX GMM 6-2-100. 2L73 4F RTA3WE 20060223000122006022300012NM 2006 2 23 05FDEA04343 120051215A5700 REPAIR BOEING727 727233 138408ANM FOREFLAP UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25274FE 22039 FOUND PREVIOUSLY REPAIR ON LT INBOARD FORE FLAP LEADING EDGE WAS ACCOMPLISHED IAS SRM 57-50-4, FIG 1, BASED ON AN EXTERNAL EVALUATION CONSISTED OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS, GENERAL WORKMANSHIP, REPAIR IS CLASSIFIED AS MAJOR REPAIR PER FEDEX GMM 6-2-100. 2L73 4F RTA3WE 20060223000132006022300013NM 2006 2 23 FX7A200500011 120051210A27821U110322 ACTUATOR BOEING727 727224 1384076NM NR 4 SLAT INOPERATIVE A FX7AA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO1979749 22451 FLIGHT CREW REPORTED THAT DURING FLAP RETRACTION, THE NR 4 SLAT DID NOT RETRACT FROM 5 TO 2 FLAP SETTINGS, FUEL DUMPING WAS ACCOMPLISHED. LOG PAGE # 36436. REMOVED AND REPLACED THE NR 4 SLAT ACTUATOR ASSEMBLY AND THE SLAT SWITCH, IAW 727 MM REF 27-81-22 AND 27-82-11, OP CHECKED NORMAL. 2L73 4F A3WE 20060223000172006022300017WP 2006 2 23 05FDEA04301 120051214A5500 REPAIR DOUG DC10 DC1010 3022110WP VERTICAL STAB NONE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25563FE 46948 VERTICAL STABILIZER LT SIDE FOUND A FITTING AND DOUBLER REPAIR ON NR 4 BANJO FITTING. PERFORMED INSPECTION FITTING AND DOUBLER REPAIR IAW ESO7349-ACF1275501. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2. 2L73 4F A22WE 20060223000192006022300019WP 2006 2 23 05FDEA04302 120051214A5400 REPAIR DOUG DC10 DC1010 3022110WP FUSELAGE NONE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25563FE 46948 NR 1 PYLON FOUND TWO BLEND OUTS ON THE OUTBOARD SKIN AREA BELOW THE TRUST REVERSER HINGE STA YN250. PERFORMED INSPECTION ON PREVIOUS REPAIR IAW 1275402-ESO7349 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2. 2L73 4F A22WE 20060223000202006022300020NM 2006 2 23 05FDEA04161 120051206A5343AEA7051502 SUPPORT DOUG MD11 MD11 3023602NM ZONE 700 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 UPON REMOVAL OF CLG SHOCK STRUT ASSEMBLY, FOUND WHEEL WELL SIDE RIGHT TRUNNION FITTING LOWER MATING SURFACE WITH CORROSION. RIGHT HAND TRUNNION FITTING LOWER MATING SURFACE CORROSION. REMOVED AND REPAIR CARRIED OUT AS PER FEDEX EA#1-5340-90704, TITLE:"FUSELAGE-CENTER LANDING GEAR RIGHT HAND SUPPORT FITTING CORROSION REPAIR". 2L73 4F RTA22WE 20060223000222006022300022WP 2006 2 23 05FDEA04355 120051216A5710ARC105979 BALANCE WEIGHT DOUG DC10 DC1010 3022110WP RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25359FE 46635 RIGHT WING OUTBOARD AILERON BALANCE WEIGHT CORRODED. REMOVED AND REPLACED BALANCE WEIGHT IAW DAC DC10 CMM 57-51-02. CALCULATED NEW BALANCE WEIGHT IAW DC10 SRM 57-50-00 VOL I, SEE FEDEX NONROUTINE NR N00245 OF WORK ORDER NR 00031297. 2L73 4F A22WE 20060223000232006022300023NM 2006 2 23 05FDEA04356 120051216A5315 FLOORBEAM BOEING727 727227 1384078NM BS 1010 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 CORROSION ON FLOORBEAM LOWER FLANGE BS 1010 BBL0-LBL44 WL 201. CORROSION WAS OUT OF LIMITS REF SRM 53-10-1. REMOVED DAMAGE FROM RBL 5 TO LBL 44. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-10-8. 2L73 4F A3WE 20060223000252006022300025NM 2006 2 23 05FDEA04346 120051215A5510 CHANNEL BOEING727 727227 1384078NM HORIZONTAL STAB DEFORMED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 RT HORIZONTAL STABILIZER T/E, NR 5 ELEVATOR BALANCE PANEL SUPPORT 'U' CHANNEL IS DEFORMED ON O/B SIDE. REPLACED RT HORIZONTAL STAB TE NR 5 BALANCE PANEL SUPPORT CHANNEL PER SRM 51-30-2. 2L73 4F A3WE 20060223000262006022300026WP 2006 2 23 05FDEA04358 120051216A5753 SKIN DOUG DC10 DC1010 3022110WP ZONE 600 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25359FE 46635 RIGHT WING FLAP LOWER SKIN, DENT AT XFS 535, 12" FROM TRAILING EDGE IS OUT OF LIMITS. REPAIRED SKIN IAW DC-10 SRM 57-10-00 FIG 85 VOL I. SEE FEDEX NONROUTINE NR N00597 OF WORK ORDER NR 00031297. 2L73 4F A22WE 20060223000272006022300027WP 2006 2 23 05FDEA04303 120051214A5101 REPAIR DOUG DC10 DC1010 3022110WP FUSELAGE NONE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25563FE 46948 CENTER CARGO DOOR LOWER AFT CORNER HAS AN EXTERNAL DOUBLER REPAIR DIM 7 INCHES BY 4 INCHES. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 52-10-00 FIG 17 VOL 1 . FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2. 2L73 4F A22WE 20060223000292006022300029WP 2006 2 23 05FDEA04305 120051214A5101 REPAIR DOUG DC10 DC1010 3022110WP GE CF6 CF6* 30020GL FUSLEAGE NONE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25563FE 46948 LT HORIZONTAL STABILIZER LOWER SURFACE TRAILING EDGE PANEL FOUND AN EXTERNAL DOUBLER REPAIR AT STA XE 169.333 DIM. 8.5 INCHES BY 5.5 INCHES. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 55-00-01 FIG 3 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2. 2L73 4F4 F A22WE E23EA 20060223000302006022300030WP 2006 2 23 05FDEA04306 120051214A5101 REPAIR DOUG DC10 DC1010 3022110WP GE CF6 CF6* 30020GL FUSLEAGE NONE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25563FE 46948 FOUND RT SIDE HORIZONTAL STABILIZER IB ELEVATOR UPPER SURFACE ON SKIN HAS AN EXTERNAL DOUBLER REPAIR AT STA XE 216.885 DIM. 8 INCHES BY 8.5 INCHES. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 55-10-00 FIG 8 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2. 2L73 4F4 F A22WE E23EA 20060223000312006022300031WP 2006 2 23 05FDEA04307 120051214A5101 REPAIR DOUG DC10 DC1010 3022110WP GE CF6 CF6* 30020GL FUSELAGE NONE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25563FE 46948 RT HORIZONTAL STABILIZER UPPER SURFACE ON SKIN FOUND AN EXTERNAL DOUBLER. REPAIR BETWEEN STA XE 67.333 AND XE 87.167 DIM. 15 INCHES X 11 INCHES. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SB 55-16 FIG 19 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2. 2L73 4F4 F A22WE E23EA 20060223000332006022300033WP 2006 2 23 05FDEA04309 120051214A5100 NONE DOUG DC10 DC1030 3023501WP GE CF6 CF650C2 30018NE NONE NONE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 LT WING L/E EXT SKIN FOUND FLUSH DOUBLER DIM 2.25 INCHES BY 1.75 INCHES AT STA XORS 532. PERFORMED A GVI OF REPAIR IAW SRM 57-10-00 FIG 39 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 E3. 2L73 4F4 F A22WE E23EA 20060223000342006022300034NM 2006 2 23 05FDEA04351 120051216A5230 DOOR BOEING727 72722 1384002NM CARGO BAY OBSTRUCTED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25189FE 19082 ON DEPARTURE, FORWARD CARGO DOOR LIGHT ILLUMINATED, COULD NOT PRESSURIZE AIRCRAFT, RETURNED TO MEM. FOUND DOOR LATCH HANDLE STOWED, DOOR CL0SED BUT NOT LOCKED OVER CENTER. ALSO, FOUND BUNGEE STUCK IN DOOR LATCH MECHANISM ON FWD SIDE OF DOOR. OPENED DOOR, PULLED HANDLE OUT, ROTATED LOCKED. OK FOR SVC DOOR OPERATES NORMALLY. 2L73 4F A3WE 20060223000352006022300035WP 2006 2 23 05FDEA04352 120051216A5100 REPAIR DOUG DC10 DC1010 3022110WP FUSELAGE UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 RT HORIZONTAL STAB CENTER SECTION ON SKIN PANEL UPPER AFT SIDE FOUND 1 REPAIR DOUBLER DIM 16" BY 11" BEWTEEN STA XE 72 AND STA XE 83. STRIPPED PAINT IAW SRM 51-21-01 PAR 32C VOL 2. PERFORMED NDT INSPECTION IAW NDT SPM 06-10-01.006 AND 04-00-06 REPAIR PREVIOUSLY ACCOMPLISHED BY DWG SR10550004. RESTORED PAINT IAW SRM 51-21-01 VOL 2. 2L73 4F A22WE 20060223000362006022300036WP 2006 2 23 05FDEA04353 120051216A5101 REPAIR DOUG DC10 DC1030 3023501WP FUSELAGE NONE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 FOUND MAIN CARGO COMPT STA 1921 Z 31 BY 92 FOUND 1 NEW SECTION OF FRAME 33" LONG WITH 2 SPLICE. PERFORMED INSPECTION ON FRAME IAW SRM 53-30-00 FIG 5 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2, RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 PAR 33/24 VOL 2. 2L73 4F A22WE 20060223000392006022300039WP 2006 2 23 05FDEA04360 120051216A3260 MECHANISM DOUG DC10 DC1030 3023501WP MLG DIRTY A FDEAO OTHER N FALSE WARNING CLCLIMB 1 SO25313FE 48311 AFTER TAKEOFF FROM SBKP ALL 4 RED GEAR LIGHTS REMAINED ILLUMINATED AT BOTH PILOTS AND FLT ENG POSITIONS. RAN RED TABS, CYCLED GEAR PER CHECKLIST. ALL 4 RED LIGHTS REMAINED ON. SLOWED A/C TO 210 KNOTS (15DEG./EXT) RECYCLED GEAR AGAIN ALL 4 RED LIGHTS EXTINGUISHED. CONTINUED TO MEM. PERFORMED OPS CHECK OF POSITION AND WARNING SYSTEM. GEAR CONTROL HANDLE "STICKY" AND CONTAMINATED WITH DEBRIS. WHEN HANDLE WAS PULLED STRAIGHT OUT INDICATION WOULD NOT CHANGE FROM GREEN TO RED. PERFORMED CLEANING AND LUBE OF LANDING CONTROL MECHANISM DC-10-30 MM 32-31-02-7. PERFORMED OPS CHECK AGAIN. CHECKS GOOD. 2L73 4F A22WE 20060223000402006022300040WP 2006 2 23 05FDEA04311 120051214A5700 REPAIR DOUG DC10 DC1030 3023501WP GE CF6 CF650C2 30018NE RT WING UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 RT WING SLAT NR 2 FOUND DOUBLER REPAIR ON UPPER SKIN T/E OB SIDE DIM 3 INCHES BY 3 INCHES. REMOVED REPAIR IAW SRM 51-35-01 PAGE 13 AND SRM 51-33-01 PAGE 34/47. CLEANED AREAS AND REMOVED PART IAW SRM 51-41-01 VOL 2. PERFORMED INSPECTION IAW NDI SPM08. FOUND CRACK 2 INCHES LONG SIGNED STOP CRACK, REPAIRED SKIN IAW SRM 57-10-00 FIG 30 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F161048-2 SKIN F161048-4 FILLER AND F161048-6 STRAP IAW SRM 57-10-00 FIG 30 VOL 1. 2L73 4F4 F A22WE E23EA 20060223000422006022300042EU 2006 2 23 05FDEA04363 120051216A5755 SKIN AIRBUS310 A310222 3930315EU NR 1 SPOILER DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25450FE 162 RT WING 1 SPOILER HAS PENETRATION DAMAGE 3" BY 1". REPAIRED NR 1 SPOILER IAW A310-200 SRM 57-70-00 REPAIR. 2L72 4F RTA35EU 20060223000472006022300047EA 2006 2 23 DJFA2005179 120051221A5312 BULKHEAD CNDAIRCL601 CL6012A12 1900303EA BS 409 CRACKED E DJFAK NONE O OTHER ININSP/MAINT 1 EA23664CW 3064 DURING A SCHEDULED MAINTENANCE VISIT, A CRACK WAS DISCOVERED IN THE PRESSURE BULKHEAD WEB AT FUSELAGE STATION 409.00 WHILE PERFORMING AIRWORTHINESS DIRECTIVE 97-24-02, SERVICE BULLETIN 601-0501. THE CRACK IS LOCATED AT THE CORNER OF THE KEEL BEAM LINK CUTOUT ANGLE, EXTENDING UP TO THE LEFT SIDE CORNER OF THE CUTOUT. 2L72 4F RTA21AE 20060223000492006022300049WP 2006 2 23 05FDEA04379 120051220A5310 STRUCTURE DOUG DC10 DC1010 3022110WP FUSELAGE GROUND DAMAGE A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25556FE 46710 DURING GROUND OPERATIONS OAN ACCIDENTALLY DAMAGE EXT FUSELAGE BETWEEN 1059/1039 LONG 32/33 LT SIDE. THE DIMENSION OF DAMAGE IS L= 4.17" W=3" D=0.114". BLENDED DAMAGE IAW SRM 53-00-01 VOL1 FIG 1A SHEET 3. PERFORMED US INSP FOUND MATERIAL THK 0.53". REPAIRED AND CUT OUT THE DAMAGE IAE SRM 53-20-00 SHEET 2 THRU 5 FIG VOL 1. 2L73 4F A22WE 20060223000512006022300051CE 2006 2 23 74798 120051218A3243 MASTER CYLINDER BEECH 1900 1900D 1154162CE MLG FAILED P AMWAO OTHER O OTHER TXTAXI/GRND HDL 1 CE07176YV UE176 DURING TAXI IN, THE CREW REPORTED THE BRAKES FEELING SPONGY. THEN FERRIED TO ICT WHERE MAINTENANCE REMOVED AND REPLACED THE MASTER CYLINDER. 2L72 4T RTA24CE 20060223000522006022300052SW 2006 2 23 2006F00006 120051222A3250 STEERING SYS SWRNGNSA227 SA227AC 8780603SW NLG MALFUNCTIONED G XEIAO OTHER O OTHER LDLANDING 1 GL27 AC532 NOSE WHEEL STEERING INOPERATIVE WITH SPEEDS LOW RESULTING IN AN UNCOMMANDED RIGHT TURN ON LANDING. DEPRESSING NWS POWER LEVER SWITCH HAD NO RESULT ON CONDITION. GROUND TESTED IAW SA227 MM. COULD NOT DUPLICATE PROBLEM. 2L72 4T RTA8SW 20060223000552006022300055CE 2006 2 23 121405N332CS1 120051214A3230 DOWNLOCK SWITCH CESSNA500 550 2076604CE MLG SHORTED E Z5FALA ABORTED APPROACH UNSCHED LANDING GJ MULTIPLE FAILURE WARNING INDICATION LDLANDING 1 NE03332CS1850 5501081 ON FINAL, MLG WOULDN`T EXTEND NORMAL. ONLY NLG EXTENDED AND C/B WOULD POP. NLG RETRACTED & A/C DIVERTED. ON APPROACH, MLG LEVER SELECTED DOWN & NLG EXTENDED AND C/B AGAIN POPPED. PULLED EMERG EXTEND HANDLE, DISCOVERED HANDLE WOULD NOT COME OUT & MLG STILL FAILED TO EXTEND. ATTEMPTED IN FLT MANEUVER TO TAKE WEIGHT OFF MLG & UPLOCKS, MANEUVER EXECUTED AND PULLED EMERGENCY HANDLE. ALL 3 GEAR FREE FELL & LOCKED DOWN. DID AN EMERG BLOW DOWN AS A PRECAUTION. DECLARED EMERG. UNEVENTFUL LANDING, RT MLG DOWNLOCK SWITCH FOUND TO HAVE BENT PIN CAUSING SHORT SO ACTUATOR REPLACED. INABILITY TO ACTIVATE EMERG RELEASE MECHANISM ATTRIBUTED TO FRICTION IN SYS DUE TO MLG DOOR ADJUSTMENT & STIFF UPLOCK ROLLER BEARINGS. 1L72 4F A22CE 20060223000562006022300056NM 2006 2 23 05FDEA04347 120051215A5101 REPAIR BOEING727 727227 1384078NM FSUELAGE NONE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 RT FUSELAGE SKIN REPAIR DOUBLER, 14" BY 7" LOCATED AT BS 1223-1243 REQUIRES EVALUATION TO DETERMINE IF THE REPAIR IS MAJOR OR MINOR AND IF REPAIR IS IN ACCORDANCE WITH FAA APPROVED DATA. REPAIRED SKIN DOUBLER PER SRM 53-30-3 FIG 1. 2L73 4F A3WE 20060223000572006022300057NM 2006 2 23 05FDEA04349 120051215A5311 FRAME BOEING727 727227 1384078NM BS 560 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 FRAME IS CREASED AT BS 560, LBL 10, WL 148.5. REPAIRED FRAME PER SRM 54-40-3 FIG 1. 2L73 4F A3WE 20060223000582006022300058NM 2006 2 23 05FDEA04365 120051216A5320 STRUCTURE BOEING727 727227 1384078NM PWA JT8 JT8D15 52051NE FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 CHORD DAMAGED AND RUB STRIP MISSING ON LWR EDGE BELOW NR 2 ENGINE BS 1352. 2L73 4F4 F A3WE E2EA 20060223000602006022300060NM 2006 2 23 05FDEA04362 120051216A5311 FRAME BOEING727 727227 1384078NM BS 680 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 FWD CARGO BAY FRAME IB FLANGE DENTED AT BS 680, BETWEEN STR 21RT AND 24RT. REPAIRED FRAME AT BS 680 BETWEEN STR 21R-24R PER SRM 51-40-3. 2L73 4F A3WE 20060223000622006022300062NM 2006 2 23 05FDEA04396 120051221A531565196051 FLOORBEAM BOEING727 727223 1384074NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25220FE 20934 FOUND STA BS1179, 3 EACH ELONGATED NUTPLATE FASTENER HOLES; LBL 2 IS ELONGATED AND CRACKED, AND RBL 3.5 AND RBL 10.5 ARE ELONGATED. COMPLIED WITH FEDEX EA# 7-5321-92600 "FUSELAGE FLOOR CHORD AT STA BS 1179 HAS DAMAGED FLANGE - REPAIR ". 2L73 4F A3WE 20060223000662006022300066WP 2006 2 23 05FDEA04400 120051222A5315 FLOORBEAM DOUG DC10 DC1030 3023501WP BS 1902 MISREPAIRED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 AFT CARGO COMPT AT STA 1902 FOUND 1 FLOORBEAM REPAIRED FROM X 55 LT TO X -55 RT AT Z-83 WITH 1 SPLICE AND 1 WEB. STRIPPED AREA IAW SRM 51-21-01 PAR 33 VOL 2. PERFORMED INSPECTION AND REPORTED VALUE ON ATTACHED SHEET. PERFORMED CONDUCTIVITY INSPECTION REPORTED VALUES ON ATTACHED SHEET. REMOVED AND REPLACED PARTS IAW FEDEX EA# 8-5310-93235. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F160289-3 SPLICE CHANNEL, F160289-5 SPLICE CHANNEL, AND F160289-7 SPLICE PLATE IAW FEDEX EA# 8-5310-93235. 2L73 4F A22WE 20060223000672006022300067WP 2006 2 23 05FDEA04401 120051222A5730 SKIN DOUG DC10 DC1030 3023501WP LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 LT WING L/E FOUND 1 CRACK 3.50" LONG ON SKIN AT STA XORS 505 AND 1 CRACK ON INT STRUCTURE LOWER CHORD FIXED PANEL. CLEANED AREA IAW M/M 12-22-01. REMOVED REFUELING DOOR IAW SRM 51-31-01 PAGE 36/41 VOL 2. REMOVED FASTENERS, WEB AND SKIN AS REQUIRED, REMOVED AND REPLACED TEE IAW DWG ARB1137. REMOVED AND REPLACED DOUBLER IAW SRM 51-35-01 PAGE 1/13 AND SRM 51-33-01. REINSTALLED FASTENERS ON WEB AND SKIN IAW SRM 51-35-01 PAGE 1/13 AND SRM 51-33-01 PAGE 34/47 VOL 2 AND DWG ARB1137. REPAIRED CRACK ON L/E SKIN IAW SRM 57-10-00 FIG 68 SHT 2/3 VOL 1. REINSTALLED REFUELING DOOR IAW SRM 51-31-01 PAGE 36/41 VOL 2. FABRICATED PART IAW DETAIL PART TRAVELER #F160730/N00730. 2L73 4F A22WE 20060223000702006022300070NM 2006 2 23 05FDEA04390 120051221A5315 FLOORBEAM BOEING727 727227 1384078NM BS 560 MISREPAIRED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25490FE 21493 EVALUATED FLOORBEAM REPAIR AT BS 560 RBL 10 FOUND NOT TO BE DONE IAW SRM 53-10-8. REPAIRED FLOORBEAM IAW SRM 53-10-8 FIG 3. 2L73 4F A3WE 20060223000712006022300071NM 2006 2 23 05FDEA04391 120051221A5101 REPAIR BOEING727 727227 1384078NM FUSELAGE MISINSTALLED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 EVALUATED REPAIR AT BS 1050 STR 23R-24R FOUND NOT TO BE IAW SRM 53-30-3. REPLACED DOUBLER PER SRM 53-30-03 FIG 1. 2L73 4F A3WE 20060223000722006022300072NM 2006 2 23 05FDEA04392 120051221A5311 FRAME BOEING727 727227 1384078NM BS 560 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 FWD CARGO BAY FRAME IB FLANGE DENTED AT BS 560 BETWEEN STR 24 LT AND STR 25 LT. REPAIRED FRAME PER SRM 51-40-3. 2L73 4F A3WE 20060223000732006022300073NM 2006 2 23 05FDEA04393 120051221A5330 REPAIR BOEING727 727227 1384078NM BS 720A MISINSTALLED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25490FE 21493 EXTERNAL DOUBLER AT BS 720A, STR 19L - 21L REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED. REPAIRED DOUBLER PER SRM 53-30-3. 2L73 4F A3WE 20060223000742006022300074NE 2006 2 23 Z1RA107272 120051206A62107610208004101 BOLT SKRSKYS76 S76C 8143008NE M/R BLADE DAMAGED B Z1RAK NONE O OTHER ININSP/MAINT 1 SW11760AF3233 760523 1 M/R BLADE RETENTION BOLT HAS 1 PULLED THREAD. 1G72 3U NCH1NE 20060223000762006022300076NE 2006 2 23 Z1RA107276 120051206A3030 HEATER SKRSKYS76 S76C 8143008NE STATIC PORT INOPERATIVE B Z1RAK NONE S AFFECT SYSTEMS ININSP/MAINT 1 SW11760AF3233 760523 LT UPPER HEATED STATIC PORT WILL NOT HEATUP. 1G72 3U NCH1NE 20060223000772006022300077 2006 2 23 Z1RA107279 420051206A3100M3901614008M RELAY SKRSKYS76 S76C 8143008NE ATTITUDE NO TEST B Z1RAK NONE L NO TEST ININSP/MAINT 1 SW11760AF3233 760523 STANDBY ATTITUDE IND WILL NOT TEST. 1G72 3U NCH1NE 20060223000872006022300087NE 2006 2 23 Z1RA107281 120051206A30202820 PRESSURE SWITCH SKRSKYS76 S76C 8143008NE INLET ANTI ICE STICKING B Z1RAK NONE O OTHER ININSP/MAINT 1 SW11760AF3233 760523 NR 1 ENGINE INLET ANTI-ICE LIGHTS INTERMITTENTLY. 1G72 3U NCH1NE 20060223000942006022300094NM 2006 2 23 DL757060110 120050322A5330146N37505 SKIN BOEING757 757232 1384965NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27676DL 25981 A DENT WAS FOUND IN THE FUSELAGE SKIN JUST FORWARD OF THE FUSELAGE FRAME AT BS 1701 AND JUST BELOW THE S-14L LAP SPLICE. THE DENT IS 1 INCH IN DIA AND 0.029 INCH DEEP. INSPECTED DAMAGE, INSTALLED DOUBLER AT HMV IN YVR. 2L72 4F RTA2NM 20060223000992006022300099NE 2006 2 23 Z1RA107285 120051204A30977630407900112 HEATER SKRSKYS76 S76C 8143008NE RT NACELLE BURNED OUT B Z1RAK NONE J WARNING INDICATION ININSP/MAINT 1 SW11761AF3019 760524 RT FWD HEATED SNOW BLANKET WILL NOT HEAT. TEMP SENSOR OUT OF RANGE. 1G72 3U NCH1NE 20060223001092006022300109NE 2006 2 23 HEEA107315 120051108A29317645001078121 TRANSMITTER SKRSKYS76 S76C 8143008NE NR 1 HYD SYSTEM FAILED B HEEAO OTHER O OTHER CLCLIMB 1 SW03505PH 760505 DURING CLIMB-OUT FROM LAFAYETTE, NR 1 HYDRAULIC PRESSURE WENT FROM THE GREEN TO THE RED LINE. RETURNED TO LAFAYETTE. MAINTENANCE REPLACED THE NR 1 HYDRAULIC PRESSURE TRANSMITTER. 1G72 3U NCH1NE 20050711000172005071100017NE 2005 7 11 XN0A1242 220050704A7200 ENGINE AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE NR 1 OVERTEMP A XN0AC ABORTED TAKEOFF MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 GL23371PC 157 DURING TAKEOFF NR 1 ENGINE EGT EXCEED LIMIT. RED EGT LIGHT ON, LESS THAN 100KTS. PER A300 MM 72-00-00 INSPECTED ENG INLET & EXHAUST, PERFORMED BOROSCOPE INSPECTION ON STAGE. 1 & 2 HPT BLADES, INSPECTED EGT INDICATION SYSTEM AS PER A300 MM 77-21-00. NO DEFECT NOTED. EGT TREND SHIFT HAS A SERVICEABLE EGT HARGIN. 2L72 4F4 FRTA35EU E23EA 20050711000232005071100023NM 2005 7 11 SB05079 120050703A27512061141 INDICATOR BOEING737 7373B7 1384580NM COCKPIT FAILED A USAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19374US4374843748 22953 CLT FLT 1417 AFTER TAKEOFF FROM CLT ENROUTE TO PBI, CREW REPORTED THE FLAPS LOCKED DURING RETRACTION DUE TO AN ASYMMETRY CONDITON. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD AT CLT WHERE THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED FLAPS AND FLAP DRIVE. NO FAULTS NOTED. REMOVED AND REPLACED THE FLAP POSITION INDICATOR. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050711000292005071100029EU 2005 7 11 MALA050506 120050623A2120 ODOR SAAB SF340 340B 7860101EU CARGO BAY DETECTED A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL15410XJ 340B410 ELECTRICAL ODOR IN CARGO AREA. INSPECTED WIRING TO CARGO SMOKE DETECTORS. INSPECTED WIRING IN AFT CARGO BAY, LT AND RT BATTERY AND PDU COMPARTMENTS. ALL SMOKE DETECTORS TESTED GOOD. ODOR BELIEVED TO BE FROM A/C SITTING IN HEAT CLOSED UP ALL DAY. 2L72 4T RTA52EU 20050711000302005071100030NM 2005 7 11 WRLA2005122 120050622A5510 STRUCTURE DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C-04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE NR 22. 2L73 4F4 FRTA22WE E24NE 20050711000332005071100033NM 2005 7 11 WRLA2005129 120050622A5510 STRUCTURE DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C-04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098, FOUND CORROSION IN HST LT BARREL NUT HOLE NR 22. 2L73 4F4 FRTA22WE E24NE 20050711000362005071100036NM 2005 7 11 WRLA2005123 120050622A5510 STRUCTURE DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C-04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE NR 16. 2L73 4F4 FRTA22WE E24NE 20050711000372005071100037NM 2005 7 11 WRLA2005127 120050622A5510 STRUCTURE DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C-04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098, FOUND CORROSION IN HST LT BARREL NUT HOLE NR 27. 2L73 4F4 FRTA22WE E24NE 20050711000382005071100038NM 2005 7 11 WRLA2005136 120050622A5510 STRUCTURE DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C-04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098, FOUND CORROSION IN HST LT BARREL NUT HOLE NR 2. 2L73 4F4 FRTA22WE E24NE 20050711000392005071100039NM 2005 7 11 WRLA2005137 120050622A5510 STRUCTURE DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C-04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE NR 2. 2L73 4F4 FRTA22WE E24NE 20050711000412005071100041NM 2005 7 11 WRLA2005121 120050622A5510 STRUCTURE DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C-04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE NR 34. 2L73 4F4 FRTA22WE E24NE 20050711000422005071100042NM 2005 7 11 WRLA2005131 120050622A5510 STRUCTURE DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C-04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098, FOUND CORROSION IN HST LT BARREL NUT HOLE NR 20. 2L73 4F4 FRTA22WE E24NE 20050711000452005071100045NM 2005 7 11 WRLA2005135 120050622A5510 STRUCTURE DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C-04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098, FOUND CORROSION IN HST LT BARREL NUT HOLE NR 3. 2L73 4F4 FRTA22WE E24NE 20050711000502005071100050WP 2005 7 11 IXXA05SMN53S 120050429A5347 CARGO TRACK DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX834963359 45993 DURING ROUTINE C-CHECK INSPECTION, AFT CARGO BAY LT TRACK STA 980.000 - 1160.000 CORRODED. REMOVED CRACKED FITTING IAW DC-8 SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW DC-8 SRM 53-2-3 FIG 12. REMOVED CORRODED TRACK IAW DC-8 SRM 51-3-0 PAGE 1. CLEANED, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8B. INSTALLED NEW TRACK IAW DC-8 SRM 51-3-0 PAGE 1. TORQUED IAW DC-8 SRM 51-3-1. 2L74 4F RT4A25 20050711000542005071100054WP 2005 7 11 IXXA05SMN28S 120050429A5551 ATTACH FITTING DOUG DC8 DC871F 302199DWP HORIZONTAL STAB CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX834963359 45993 LT HORIZONTAL STABILIZER FAIRING SUPPORT AFT FITTING CRACKED STA 1880.000 LT. REMOVED CRACKED FITTING IAW DC-8 SRM. FABRICATED NEW FITTING IAW DWG NR 3702464. PERFORMED HEAT TREATMENT IAW DC-8 SRM. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02 TO 07. CLEANED, TREATED AND PRIMED AREA AND NEW FITTING IAW DC-8 SRM. INSTALLED NEW FITTING IAW DC-8 SRM. TORQUED IAW DC-8 RM 51-3-1. 2L74 4F RT4A25 20050711000562005071100056WP 2005 7 11 IXXA05SMN30S 120050429A5343 FITTING DOUG DC8 DC871F 302199DWP NLG CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX834963359 45993 NOSE SECTION RT TUNNEL FITTING CRACKED STA 8.000. REMOVED CRACKED FITTING IAW DC-8 SRM 53-1-0 PAGE 1, DC-8 SRM 51-3-0 PAGE 1. FABRICATED NEW FITTING IAW DWG NR 4640117. PERFORMED HEAT TREATMENT IAW DC-8 SRM 51-1-1 PAGES 1, 13, 17. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02 TO 07. ENCLOSED SMN FORM 242-4. CLEANED, TREATED AND PRIMED AREA AND FITTING IAW DC-8 SRM 51-1-8B. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D PAGE 9. TORQUED IAW DC-8 RM 51-3-1 PAGE 2A. 2L74 4F RT4A25 20050711000592005071100059WP 2005 7 11 IXXA05SMN33S 120050429A5340 ATTACH FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX834963359 45993 MAIN CARGO BAY END FITTING CRACKED, STA 680.000, L-4R. REMOVED CRACKED FITTING IAW DC-8 SRM 53-1-0 PAGE 1, DC-8 SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING IAW DWG NR 3779762. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02 TO 07. CLEANED, TREATED AND PRIMED AREA AND NEW FITTING IAW DC-8 SRM 51-1-8B. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D PAGE 9. TORQUED DC-8 SRM 51-3-1. 2L74 4F RT4A25 20050711000612005071100061WP 2005 7 11 IXXA05SMN17S 120050429A5712 RIB DOUG DC8 DC871F 302199DWP LT WING CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX834963359 45993 LT NR 1 STUB WING FORMER CRACKED, STA XFS 526.000. PERFORMED MAJOR REPAIR IAW DWG 9753247. REMOVED CRACKED RIB IAW DC-8 SRM 54-1-0 PAGE 1, DC-8 SRM 51-1-21 PAGE 1, DC-8 SRM 51-1-20D PAGE 21. FABRICATED NEW RIB IAW DWG 9753297, DC-8 SRM. DPS 369-4 REV AM. PERFORMED HEAT TREATMENT IAW DC-8 SRM. CLEANED, TREATED AND PRIMED AREA AND RIB IAW DC-8 SRM 51-1-8B. INSTALLED NEW RIB IAW DC-8 SRM 51-1-20D PAGE 9. TORQUED IAW DC-8 SRM 51-3-1. 2L74 4F RT4A25 20050711000632005071100063WP 2005 7 11 IXXA05SMN19S 120050429A5340 ATTACH FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX834963359 45993 MAIN CARGO BAY, STA 857.000 L-19L AFT FITTING CRACKED. REMOVED CRACKED FITTING IAW DC-8 SRM 53-1-0 PAGE 1, DC-8 SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING IAW DWG NR 4750423. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02 TO 07. CLEANED, TREATED AND PRIMED AREA AND NEW FITTING IAW DC-8 SRM 51-1-8B. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D PAGE 9. TORQUED IAW DC-8 RM 51-3-1. 2L74 4F RT4A25 20050711000672005071100067WP 2005 7 11 IXXA05SMN23S 120050429A5340 ATTACH FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX834963359 45993 MAIN CARGO BAY FWD SERVICE DOOR INTERNAL JAMB FITTING CRACKED, STA 474.000 L-11R. REMOVED CRACKED FITTING IAW DC-8 SRM 53-1-0 PAGE 1, DC-8 SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING IAW DWG NR 9755586. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02 TO 07. CLEANED, TREATED AND PRIMED AREA AND NEW FITTING IAW DC-8 SRM 51-1-8B. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D PAGE 9. TORQUED IAW DC-8 RM 51-3-1. 2L74 4F RT4A25 20050711000712005071100071NM 2005 7 11 05FDEA01676 120050624A7830 TRACK DOUG MD11 MD11 3023602NM THRUST REVERSER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25619FE 48770 NR 2 ENGINE, LT THRUST REVERSER UPPER SLIDER TRACK CRACKED. REMOVED AND INSTALLED NEW REVERSER AS PER WORK CARD 78T3002-L AND WORK CARD 78T3902-L. ADJUSTMENT AND OPERATION CHECK CARRIED OUT AS PER WORK CARD 78T3902-L, GE NR 2 LEFT THRUST REVERSER DOOR - INSTALL. 2L73 4F RTA22WE 20050711000882005071100088NM 2005 7 11 AWXA200500741 120050601A575465C26602218SP SKIN BOEING737 73733A 1384673NM NR 5 SLAT DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 FOUND DISBOND AREA ON UPPER SURFACE OF NR 5 SLAT, 1.75 IN FROM OUTBOARD END, FROM RT SS 252 TO RT SS 253. MAINTENANCE CUTOUT SKIN AND DISBOND CORE FROM UPPER SURFACE OF NR 5 SLAT, 1.75 IN FROM OUTBOARD END, IAW BOEING 737-300 SRM 51-70-10-0 REPAIR 7, FIG 16. FABRICATED REPAIR DOUBLER AND REPAIR CORE IAW BOEING 737-300 SRM 51-70-10-0, REPAIR 7, FIG 16. BONDED REPAIR CORE AND REPAIR DOUBLER TO THE UPPER SURFACE OF NR 5 SLAT, 1.75 IN FROM OUTBOARD END, IAW BOEING 737-300 SRM 51-70-10-0 REPAIR 7, FIG 16. 2L72 4F RTA16WE 20050711000922005071100092WP 2005 7 11 05FDEA01657 120050622A5754ARB1121Y502 DOOR DOUG MD10 MD1010F 3022112WP NR 8 SLAT TRACK CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25391FE 46625 RT WING NR 8 SLAT TRACK DOOR HAS CRACK AND WORN. REMOVED AND REPLACED NR 8 SLAT TRACK DOOR IAW MM 57-21-01--2 AND OPS CHECKED GOOD IAW MM 27-80-01-4. 2L73 4F RTA22WE 20050711000932005071100093NM 2005 7 11 05FDEA01658 120050622A574365222212 SUPPORT BOEING727 7272S2F 1384O81NM RT MLG CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25203FE 22925 RT SHAFT ASSY HOUSING SUPPORT AT WING STA 315 NEXT TO RT MLG SUPPORT BEAM BUSHING CRACKED. REMOVED AND REPLACED TORQUE TUBE BEARING SUPPORT FITTING IAW MM 27-51-131-2. 2L73 4F A3WE 20050711000942005071100094 2005 7 11 05FDEA01659 420050623A3452 ANTENNA BOEING727 7272S2F 1384O81NM NR 2 ATC CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25203FE 22925 LOWER NR 2 ATC ANTENNA CORRODED. REMOVED AND REPLACED NR 2 ATC ANTENNA IAW MM 34-54-001-2. 2L73 4F A3WE 20050711000952005071100095NM 2005 7 11 05FDEA01660 120050623A522065372913A HANDLE BOEING727 7272S2F 1384O81NM EMERGENCY EXIT CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25203FE 22925 LT AFT EMERGENCY EXIT LOWER HANDLE ESCATION IS CRACKED. REMOVED AND REPLACED HANDLE ASSY IAW SRM 51-30-2. 2L73 4F A3WE 20050711000972005071100097NM 2005 7 11 05FDEA01662 120050623A5755 ANGLE BOEING727 7272S2F 1384O81NM NR 2 SPOILER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25203FE 22925 NR 2 SPOILER UPPER SURFACE CRACKED AT 2 CENTER ATTACHMENTS. REMOVED AND REPLACED LT NR 2 SPOILER HINGE CUTOUT ANGLE IAW SRM 51-30-2. 2L73 4F A3WE 20050711001002005071100100NM 2005 7 11 QXEA200501080 120050625A5210 DOOR BOMBDRDHC8 DHC8402 1390042NM AFT PAX OUT OF ADJUST A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09415QX 4081 AFT PASSENGER DOOR WILL NOT OPEN. INSPECTED AND FOUND DOOR COCKED. STRAIGHTENED DOOR. DOOR OPENED. OPENED AND CLOSED DOOR. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050711001012005071100101NM 2005 7 11 DHL2005741596 120050512A5313 STRINGER BOEING727 7272Q9 138448MNM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 FWD CARGO BS 560 STR 28R IS CORRODED. CORRODED BEYOND LIMITS. CUT OUT SECTION OF STR 28R FROM BS 550 TO 570 20 IN IAW B727 SRM 53-10-3 FIG 1. FABRICATED STRINGER SECTION FROM BAC 1498-147 SIZE 20 IN PO 4112 AND SPLICE FROM BAC 1498-131 SIZE 13.875 PO22374 IAW B727 SRM 53-10-3 FIG 1 STR 4 DETAIL 1. TREATED AND PRIMED PARTS AND AREA IAW B727 SRM 51-10-2. INSTALLED STRINGER REPAIR AT BS 550 STR 28R IAW B727 SRM 53-10-3 FIG 1.FD 2L73 4F RTA3WE 20050711001062005071100106NM 2005 7 11 DHL2005741595 120050511A5313 STRINGER BOEING727 7272Q9 138448MNM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 AFT CARGO BAY AT BS 1166 STR 29R IS CORRODED. STRINGER 29 RT CORRODED BEYOND ALLOW LIMITS. REMOVED FASTENERS. CUT OUT SECTIONS OF STRINGER IAW B727 SRM. TREATED AND PRIMED PARTS IAW B727 SRM. INSTALLED NEW STR 29 RT IAW B727 SRM. FABRICATED STRINGER SPLICE IAW B727 SRM 53-10-3 FIG 1. 2L73 4F RTA3WE 20050711001112005071100111NM 2005 7 11 AALA20050406 120050620A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21931AN 30079 EMERGENCY LIGHT BATTERY PACK AT RT OVERWING AT STATION 578 FAILED TEN MINUTE CAPACITY TEST. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT RT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20050711001122005071100112NM 2005 7 11 AALA20050407 120050620A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21931AN 30079 EMERGENCY LIGHT BATTERY PACK AT LT OVERWING STATION 578 INOPERATIVE. REPLACED BATTERY PACK FOR EMERENCY LIGHTS AT LT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20050711001132005071100113 2005 7 11 AALA20050403 420050619A3417 ADC BOEING757 757223 1384957NM COCKPIT INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW21685AA 25342 AT FLIGHT LEVEL 330, IN ICING CONDITIONS WITH ENGINE AIR INDICATION ON SELECTED WING ANTI-ICE. 45 SECONDS LATER SPEED RIM MESSAGE FOLLOWED BY LOSS OF BOTH AIR SPEED INDICATORS. DESCENDED TO WARMER TEMPERATURES OUT OF ICING CONDITIONS. INSTRUMENT INDICATION RETURNED TO NORMAL. WING AND ENGINE AIR INDICATION DESELECTED ACCOMPANIED BY POSSIBLE ELECTRIC ODOR DURING EMERGENCY DESCENT. ENCOUNTERED MODERATE TO SEVERE TURBULENCE. CEILING PANEL OVER 22A VENT BY 21A BENT AND DISLODGED. LANDED WITHOUT INCIDENT. REPLACED F/O AIR DATA COMPUTER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050711001262005071100126NM 2005 7 11 DHL2005741603 120050513A5313 STRINGER BOEING727 7272Q9 138448MNM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 STRINGER 20R AT BS 360 IN DOGHOUSE IS CORRODED. REMOVED FASTENERS AND CORROSION FOUND TO BE OUT OF LIMITS ON STR 20R BS 360 IAW B727 SRM 51-30-2 & 51-10-6. CUT OUT SECTION OF STR 20R DIM 17 INCH IAW B727 SRM 53-10-3 FIG 1. FABRICATED STR SECTION FROM BAC 1493-412 SIZE 17 INCH PO 4246397 AND CHANNEL FROM 7075-T6 .050 SIZE 14.5 X 3 INCH PO 9002126 AND ANGLES 2EA FROM 7075-T6 .050 SIZE 13 X 1.375 INCH PO 9002126 AND FILLERS 2EA FROM 7075-T6 .050 SIZE 12 X 12 INCH PO 9002126 IAW B727 SRM 53-10-3 FIG 1. TREATED AND PRIMED PARTS AND AREA IAW B727 SRM 51-10-2. INSTALLED STR REPAIR PARTS IAW B727 SRM 53-10-3 FIG 1. 2L73 4F RTA3WE 20050711001302005071100130EA 2005 7 11 VTZA200500118 120050623A5320601R3117117 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27642BR 7356 INTERCOSTAL CRACKED ON LT INBOARD SIDE AT FS 484 LT BETWEEN BL 27.OO. 2L72 4F RTA21EA 20050711001372005071100137EA 2005 7 11 VTZA200500120 120050623A5712601R102328 RIB CNDAIRCL600 CL6002B19 1900309EA RT WING CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27642BR 7356 RT BATTERY RIB CRACKED BETWEEN ATTACHING FASTENERS. 2L72 4F RTA21EA 20050711001502005071100150EA 2005 7 11 VTZA200500124 120050623A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27642BR 7356 LT FS 621 SUPPORT CRACKED IN ANGLE. 2L72 4F RTA21EA 20050711001522005071100152EA 2005 7 11 VTZA200500126 120050623A5320601R311719 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27642BR 7356 INTERCOSTAL CRACKED AT .250 IN LENGTH ON RT OUTBD SIDE AT FS 484 RT BETWEEN BL 36.00. 2L72 4F RTA21EA 20050711001562005071100156NE 2005 7 11 XN0A1245 220050708A7200 ENGINE BOEING727 727227 1384078NM PWA JT8 JT8D9A 52048NE NR 2 FAILED A XN0AD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL2379754 21363 665909 ENGINE NR 2 WOULD NOT START. REMOVED AND REPLACED NR 2 ENGINE, OPS CK GOOD REF MM 74-11. (ORIG/CLOSED) 2L73 4F4 F A3WE E2EA 20050711001582005071100158NM 2005 7 11 QXEA200501095 120050705A2110 CONDENSER DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE ZONE 100 PLUGGED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 NM09346PH 477 WHEN THE BLEEDS ARE TURNED ON AFTER TAKEOFF, AN ODOR (LIKE DIRTY GYM SOCKS) COMES OUT AND LAST FOR 6-10 MINUTES, THEN CLEARS UP. MAINTENANCE FOUND WATER DRAIN FILTER COMING OUT OF THE CONDENSER/MIXER PLUGGED. CLEANED FILTER AND REINSTALLED DRAIN LINE. PERFORMED FUNCTIONAL TEST OF THE BLEED AIR SYSTEM, ALL CHECKS GOOD. NO SMELL NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20050711001602005071100160NM 2005 7 11 AALA20050417 120050702A2530 OVEN BOEING777 777223 1385213NM RROYCERB211 RB211TRENT89 NE GALLEY CONTAMINATED A AALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21760AN 31477 BUSINESS CLASS GALLEY OVEN 4B SMOKES. RAN OVEN DURING GROUND TIME. FOOD AND DEBRIS CLEANED UP BY CABIN SERVICES. NO OTHER FAULTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTT00001SEE00050EN 20050711001622005071100162WP 2005 7 11 AALA20050418 120050703A3350 LIGHT DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21441AA 49460 ALL OVERHEAD EMERGENCY LIGHT IN AFT TAIL CONE ARE INOPERATIVE. 2L72 4F4 F A6WE E9NE 20050711001642005071100164WP 2005 7 11 AALA20050422 120050705A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21288AA 49300 EMERGENCY LIGHTS IN FORWARD ENTRY AREA INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN FORWARD ENTRY AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 F A6WE E9NE 20050711001692005071100169NM 2005 7 11 05FDEA01433 120050524A5347S4929147 SEAT TRACK DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25631FE 48454 FWD FUSELAGE STA 765-1129 X = 8.5 LT GALLEY 7 EXISTING REPAIR ON CORRODED SEAT TRACK. SEAT TRACK REPAIR AT FWD FUSELAGE STA 765-1129 X = 8.5 LT EVALUATED FOUND CARRIED OUT IAW SRM 53-70-00 FIG 3 VOL I. EO 1-5100-7-5001 ACCOMPLISHED. 2L73 4F4 FRTA22WE E24NE 20050711001702005071100170SO 2005 7 11 C2XA05SH060 120050705A532014530628003 FLOOR SUPPORT EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716961 145103 DURING C-CHECK MAINTENANCE FOUND THE CENTER OMEGA BEAM HAS CORROSION FROM FRAME 29- JUST AFT OF FRAME 35. MAINTENANCE REPAIRED THE CENTER OMEGA BEAM AT CROSSBEAM LOCATED AT FRAME 33 IAW EC 5320-01251, NO FURTHER ACTION REQUIRED. AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20050711001712005071100171SO 2005 7 11 C2XA05SH061 120050705A531112010732001 FRAME EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL AFT FUSELAGE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716961 145103 SHV-DURING C-CHECK MAINTENANCE FOUND APU FIREWALL ATTACHMENT FRAME CRACKED AT THE SIX O'CLOCK POSITION AT FRAME 81 (INTERNAL). MAINTENANCE REPAIRED THE APU FIREWALL IAW EC 5310-01342. AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20050711001722005071100172SO 2005 7 11 C2XA05SH062 120050705A532014521700007 FLOOR SUPPORT EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716961 145103 DURING C-CHECK MAINTENANCE FOUND THE LT OMEGA BEAM HAS CORROSION IB SIDE AT FRAME 23. MAINTENANCE REPAIRED CORROSION ON LT OMEGA BEAM IB SIDE AT FRAME 23 IAW 145 SRM 53-22-10 AND EC 5320-01140. AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20050711001742005071100174SO 2005 7 11 C2XA05SH064 120050705A532014530628001 FLOOR SUPPORT EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716961 145103 SHV-DURING C-CHECK MAINTENANCE FOUND CENTER OMEGA BEAM HAS CORROSION FROM FRAME 23-JUST AFT OF FRAME 29. MAINTENANCE REPAIRED CENTER OMEGA BEAM FROM FRAME 23 TO FRAME 29 IAW SRM 53-22-10. AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20050711001752005071100175NE 2005 7 11 05052 220050703A7200 ENGINE BOEING747 747209B 138489BNM PWA JT9 JT9D7Q 52054NE NR 3 FIRE A KCSAFA ACTIVATE FIRE EXT. UNSCHED LANDING AJ FLAME/FIRE WARNING INDICATION CLCLIMB 1 GL23714CK 22446 702272 AFTER INITIATING CLIMB THRUST AT 1,000 FT, NR 3 ENGINE FIRE LIGHT ILLUMINATED WITH ACCOMPANYING FIRE WARNING BELL AND BOTH MASTER WARNING LIGHTS. ENGINE FIRE CHECKLILST, FUEL JETTISON CHECKLIST AND NR 2 GENERATOR INOPERATIVE CHECKLIST ACCOMPLISHED IAW WITH QRH RETURNED TO LAND. 2L74 4F4 FRTA20WE E3NE 20050711001812005071100181NM 2005 7 11 05FDEA01688 120050626A5320 FLOOR SUPPORT BOEING727 7272S2F 1384O81NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25203FE 22925 MAIN DECK BELOW FLOOR FS 1183 L-ANGLE CRACKED RBL 55, REMOVED L-ANGLE DITCHING SEAL, SEAL SUPPORT AND LT AND RT ANGLES IAW SRM 51-30-2. FABRICATED SEALS SUPPORT IAW DWG 65-29548. LOCATED, DRILLED AND INSTALLED PARTS IAW SRM 51-30-5 AND 51-30-2 MINOR REPAIR. 2L73 4F A3WE 20050711001862005071100186SO 2005 7 11 SWIA200515171 120050619A3350 LIGHT EMB 120 EMB120ER 3260203SO EMERGENCY LIGHTSINOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07295UX 120295 ONE RED EMERGENCY LIGHT ON FLOOR INOPERATIVE. REPLACED RED EMERGENCY LIGHT ON FLOOR. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050711001902005071100190NM 2005 7 11 ASAA0590022 120050328A5320143A948535 SUPPORT BOEING737 737990 NM GE CFM56 CFM567B24 NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02307AS 30015 DURING C-CHECK, FOUND CORROSION ON BULKHEAD TO FILLER PANEL SUPPORT AT BS500L. REPAIRED IAW SRM. (K) 2L74 4F4 FRTA16WE E00055EN 20050711001922005071100192NM 2005 7 11 ASAA0590023 120050328A5320146A750347 FLOOR SUPPORT BOEING737 737990 NM GE CFM56 CFM567B24 NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02307AS 30015 DURING C-CHECK, FOUND CORROSION ON FLOOR SUPPORT SPLICE ANGLE AT BS 7271+6. REPAIRED IAW SRM. (K) 2L74 4F4 FRTA16WE E00055EN 20050711001932005071100193EA 2005 7 11 SWIA200515175 120050615A3350 SOCKET CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSDAMAGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07454SW 7749 AFT EMERGENCY LIGHT DAMAGED. INSTALLED NEW EMERGENCY LIGHT SOCKET IAW CRJ MM 20-00-00. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050711001952005071100195NM 2005 7 11 ASAA0590026 120050328A5320146A7502 FLOOR SUPPORT BOEING737 737990 NM GE CFM56 CFM567B24 NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02307AS 30015 DURING C-CHECK, FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT AT BS 7271+21 AND RBL 20. REPAIRED IAW SRM. (K) 2L74 4F4 FRTA16WE E00055EN 20050711001972005071100197NM 2005 7 11 ASAA0540295 120050615A5320654659247 FLOOR SUPPORT BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02703AS 28893 OPEN HOLES IN FLOOR SUPPORT. REMOVED DAMAGED AREA AND REPAIRED. (K) 2L72 4F4 FRTA16WE E21EU 20050711002032005071100203SW 2005 7 11 ALGA104278 120050515A7120406040506101 HOUSING BELL 407 407 1182206SW ENGINE MOUNT CRACKED B ALGAK NONE O OTHER NRNOT REPORTED 1 SW035NBFI2491 53550 DURING FIRST 2500 HR OVERHAUL, CRACKED HOUSING FOUND DURING NDT. 1G71 3U O H2SW 20050711002262005071100226 2005 7 11 UPS05M44722 420050620A2565 LIGHT DOUG MD11 MD11F 3023600NM R1 EVAC SLIDE INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP 48774 R1 EVAC SLIDE REMOTE PRESSURE INDICATOR INOPERATIVE. RELAMPED R1 EVAC PRESSURE LIGHT. OPS CHECK NORMAL. PLACARD REMOVED. 2L73 4F RTA22WE 20050711002282005071100228NM 2005 7 11 05FDEA01691 120050626A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25619FE 48770 WITH REFERENCE TO WORK CARD E1-5510-7-5000, LT BARREL NUT HOLE NR 29L, FOUND OUT OF LIMIT AFTER CORROSION REMOVAL. REPAIR CARRIED OUT AS PER FEDEX EA 1-5510-83022. 2L73 4F RTA22WE 20050711002452005071100245NM 2005 7 11 UPS05244725 120050613A5330 SKIN BOEING727 72731C 1384011NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 CRACK IN FUSELAGE SKIN BS 355 BETWEEN S26L AND 27L. REPAIR CARRIED OUT IAW SRM 53-30-3 AND 51-10-2. 2L73 4F A3WE 20050711002472005071100247NM 2005 7 11 UPS05244727 120050611A783006453010059 SUPPORT BRACKET BOEING727 72731C 1384011NM THRUST REVERSER CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 ENG NR 3 THRUST REVERSER O/B FAIRING MID SUPPORT BRACKET CRACKED. BRACKET REPLACED IAW SRM 51-30-2. 2L73 4F A3WE 20050711002502005071100250NM 2005 7 11 UPS05244730 120050610A2752 SUPPORT BRACKET BOEING727 72731C 1384011NM FLAP ACTUATOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 NR 2 LE FLAP ACTUATOR O/B SUPPORT BRACKET CRACKED AT UPPER FWD CORNER. BRACKET FABRICATED AND REPLACED IAW SRM 51-20-1, 51-30-02 AND DRAWING 65 -16269. 2L73 4F A3WE 20050711002512005071100251NM 2005 7 11 UPS05244731 120050615A5330 SKIN BOEING727 72731C 1384011NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 C NDI HAS MATERIAL LOSS INDICATION AT S19 RT BS 441, SKIN CUT OUT AND REPAIR IN CONJUNCTION WITH NRC 792106 LAP REPAIR. 2L73 4F A3WE 20050711002522005071100252NM 2005 7 11 UPS05244733 120050610A5330 SKIN BOEING727 72731C 1384011NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 CRACK ON SKIN AT FWD ENTRY DOOR UPPER FWD AREA (BETWEEN S6 AND S 7L) OF CUT OUT. REPAIR CARRIED OUT IAW EO B727-5330-1460 OPTION 1. 2L73 4F A3WE 20050711002572005071100257EA 2005 7 11 SWIA200515179 120050622A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07408SW8715 8715 7055 FLIGHT SPOILER FAULT MSG DURING TAXI. REPLACED LT INBOARD FLIGHT SPOILER PCU IAW 27-62-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050711002612005071100261EA 2005 7 11 SWIA200515183 120050623A2780 SENSOR CNDAIRCL600 CL6002C10 1390015EA LE SLAT MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07712SK 10172 SLAT FAULT STATUS MSG. REPLACED RT INBOARD SLAT DISCONNECT SENSOR IAW MM 27-81-39. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050712000422005071200042EA 2005 7 12 QXEA200501081 120050623A4950 APU CNDAIRCL600 CL6002C10 1390015EA ZONE 100 ODOR A QXEAK NONE B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 NM09601QX 10009 STRONG ODOR IN AIRCRAFT. MOST NOTICEABLE ON GROUND. RAN BOTH ENGINES WITH APU AIR OFF AND BOTH PACKS OPERATING. ODOR SEEMED TO DISSIPATE. STARTED APU AND RAN BOTH PACKS WITH APU AIR. ODOR SEEMED TO REAPPEAR. APU PLACED ON MEL. 2L72 4F RTA21EA 20050712000432005071200043EA 2005 7 12 QXEA200501079 120050624A7714829599 SENSOR CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE NR 1 ENGINE FAILED A QXEAD RETURN TO BLOCK O OTHER UKUNKNOWN 1 NM09604QX 10019 RETURNED TO GATE, LEFT START ABORT (N2 BETWEEN 57 AND 58.5%). REMOVED AND REPLACED NR 1 ENGINE N2 SPEED SENSOR. OPERATIONAL AND LEAK CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050712000492005071200049NM 2005 7 12 SWAA051967 120050707A55536547450 FITTING BOEING737 7373H4 1384600NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED D-CHECK, FOUND LT & RT VERTICAL STAB ATTACH FITTING FWD & AFT PRIMARY CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER. 2L72 4F RTA16WE 20050712000502005071200050NM 2005 7 12 SWAA051968 120050707A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED D-CHECK, FOUND 2 EA FUSELAGE SHEAR TIES CORRODED AT BS 727E & BS 747, STR 27L TO STR 26R. REMOVED AND REPLACED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20050712000522005071200052NM 2005 7 12 SWAA051970 120050707A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED D-CHECK, FOUND 2 EA FUSELAGE SHEAR TIES CORRODED AT BS 787 & BS 807, STR 26L TO STR 26R. REMOVED AND REPLACED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20050712000532005071200053NM 2005 7 12 SWAA051971 120050707A53226546554 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 847, STR 25L TO STR 27L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050712000612005071200061NM 2005 7 12 CALA0500213 120050706A256061020 BATTERY BOEING737 737824 13844BZNM FLASHLIGHT DISCHARGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718223 28932 THE LEFT HAND AFT FLASHLIGHT LED WAS NOT BLINKING. THE FLASHLIGHT BATTERY WAS REMOVED AND REPLACED IAW MM 25-64-00. 2L72 4F RTA16WE 20050712000712005071200071 2005 7 12 SWAA051959 420050706A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050712000722005071200072NM 2005 7 12 SWAA051960 120050706A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29332SW 23696 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C + 18, STR 13L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050712000752005071200075NE 2005 7 12 SWAA051963 220050706A7200 ENGINE BOEING737 7373H4 1384600NM GE CFM56 CFM563B1 13802NE NR 1 POWER LOSS A SWAAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SW29605SW 27956 727291 NR 1 ENGINE WOULD NOT DEVELOP FULL POWER ON TAKEOFF. REMOVED AND REPLACED NR 1 ENGINE PER MM. 2L72 4F4 FRTA16WE E2GL 20050712000792005071200079NM 2005 7 12 SWAA051948 120050705A53126546568 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED D-CHECK, FOUND 2 EA CRACKS AT BS 1016 PRESSURE BULKHEAD DOME CAP WEB, 6 & 7 O'CLOCK POSITIONS. REPAIRED WEB PER BFG ER. 2L72 4F RTA16WE 20050712000842005071200084NE 2005 7 12 AWXA200500744 220050626A7320FFG021BH FUEL CONTROL BOEING757 7572S7 1384962NM RROYCERB211 RB211535E4 54555NE NR 1 ENGINE INOPERATIVE A AWXAO OTHER O OTHER TXTAXI/GRND HDL 1 WP28901AW498991369 23321 DURING ENGINE SHUTDOWN, AT GATE, LT ENGINE WOULD NOT SHUT DOWN WITH FUEL CONTROL SWITCH AT CUT OFF POSITION. PULLED LT ENGINE FIRE HANDLE. ENGINE SHUT DOWN. MAINTENANCE REMOVED AND REPLACED NR 1 FUEL FLOW GOVERNOR IAW AMERICA WEST AIRLINES (AWA) TASK CARD R5M73603 AND AWA TASK CARD F5M73601. OPERATIONAL CHECKS GOOD. VENDOR REPORTS THAT THEY COULD NOT CONFIRM FAULT. FFG WAS RECEIVED AND FOUND TO BE FUNCTIONING PROPERLY. UNIT WAS TESTED AND RE-CALIBRATED IAW CMM 73-21-02 REV 5. 2L72 4F4 FRTA2NM E12EU 20050712000952005071200095NM 2005 7 12 SWAA051991 120050710A53306545774 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29501SW 24178 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 764, STR 23L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050712000972005071200097NM 2005 7 12 SWAA051993 120050708A53116546550 FRAME BOEING737 7373H4 1384600NM FUSLEAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29608SW 27928 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 787, STR 24R TO STR 25R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050712001002005071200100NM 2005 7 12 SWAA051999 120050708A53106546956 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29608SW 27928 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FUSELAGE CREASE BEAM WEB CORRODED AT BS 400 TO BS 420, RBL 68, WL 208. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050712001062005071200106NM 2005 7 12 SWAA052006 120050708A53206935367 WEB BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29608SW 27928 DURING SCHEDULED D-CHECK, FOUND 2 EA CREASE BEAM WEBS CORRODED AT BS 360 TO BS 400, LBL 68 & RBL 70, WL 208. REPAIRED CREASE BEAM WEBS PER SRM. 2L72 4F RTA16WE 20050712001112005071200111NM 2005 7 12 SWAA052010 120050709A3397 WIRE BOEING737 737301 1384611NM EMERGENCY LIGHT DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED SERVICE CHECK, FOUND AFT GALLEY LOWER EMERGENCY EXIT LIGHT INOP. REPAIRED WIRES TO LIGHT PER WDM. 2L72 4F RTA16WE 20050712001122005071200112NM 2005 7 12 SWAA052011 120050709A3297806002 CIRCUIT CARD BOEING737 7373Q8 1384670NM E/E BAY ARCED A SWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW29689SW 23387 AIR TURNBACK/DECLARED EMERGENCY. RED NOSE GEAR LIGHT ILLUMINATED, ACFT DID NOT PRESSURIZE ABOVE 10,000 FT, LOW IDLE LIGHT ILLUMINATED DURING DESCENT. FOUND ARCING ON M1112, M990 & M991 CIRCUIT CARDS. REMOVED AND REPLACED CIRCUIT CARDS PER MM. 2L72 4F RTA16WE 20050712001172005071200117EU 2005 7 12 AWXA200500748 120050624A2497 WIRE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 1 GENERATOR BROKEN A AWXAAD UNSCHED LANDING RETURN TO BLOCK O OTHER CRCRUISE 1 WP28657AW286056643 1083 AIR TURN BACK. DURING FLIGHT LOST APU WITH NR 1 GENERATOR ALREADY ON MEL. AIRCRAFT RETURNED WITHOUT FURTHER INCIDENT. MX REMOVED AND REPLACED NR 1 IDG IAW AMERICA WEST AIRLINES TASK CARD R5M24301. OPERATIONAL CHECKS WERE GOOD. PLACED THE APU ON MEL. TEAR DOWN REPORT CONFIRMS REASON FOR REMOVAL. UPON TEAR DOWN, FOUND TWO LEAD WIRES BROKEN ON THE EXCITER ROTOR. THIS STOPPED RESISTANCE FLOW AND OUTPUT TO THE CORRESPONDING PHASES, TRIGGERING THE IDG OFFLINE. UNIT WAS REPAIRED IAW CMM 24-11-79 REV. 18. 2L72 4F4 FRTA28NM E40NE 20050712001182005071200118NM 2005 7 12 SWAA051986 120050708A53156545410 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 712, LBL 25, WL 203. REPAIRED FLOORBEAM PER BFG ER. 2L72 4F RTA16WE 20050712001192005071200119NM 2005 7 12 AWXA200500749 120050624A2910271N63111099 LINE BOEING757 7572S7 1384962NM HYD SYS CRACKED A AWXAAD UNSCHED LANDING RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP28902AW 23322 DURING FLIGHT, LT HYDRAULIC QUANTITY SHOWED ZERO. RETURNED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND HYDRAULIC LINE TO PTU PRESSURE SWITCH CRACKED. REMOVED AND REPLACED LINE IAW BOEING 757 MM 29-31-00 AND BOEING 757 MM 20-11-00. NO LEAKS WERE NOTED. 2L72 4F RTA2NM 20050712001222005071200122NM 2005 7 12 SWAA051987 120050708A3350100031 LIGHT BOEING737 7373H4 1384600NM EMERGENCY EXIT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29329SW 23693 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING LOWER EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT PER MM. 2L72 4F RTA16WE 20050712001262005071200126NM 2005 7 12 EIA2005128 120050614A5330 SKIN BOEING747 747212B 1384886NM FUSELAGE BULGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 SKIN BULGED ON FUSELAGE BELLY STA 2180 BL 0. SKIN REPLACEMENT COMPLIED WITH PER B 747 SRM 53-30-03 IN CONJUNCTION WITH NON-ROUTINE CARD 1095. 2L74 4F A20WE 20050712001302005071200130NM 2005 7 12 QXEA200501082 120050627A33506104781 BATTERY PACK DHAV DHC8 DHC8202 2809007NM EMERGENCY LIGHTSDISCHARGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH337 337 477 MAIN CABIN DOOR EMERGENCY EXIT LIGHT INTERMITTENTLY FLICKERS AND NOISE IS HEARD THROUGH PASSENGER ADDRESS SYSTEM. CYCLING EMERGENCY LIGHTS CANCELS IT OUT. REMOVED AND REPLACED EMERGENCY EXIT POWER SUPPLY PS1. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050712001312005071200131NM 2005 7 12 AWXA200500752 120050607A5313654687711 STRINGER BOEING737 7373B7 1384580NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28328AW 23377 MAJOR REPAIR. DURING C-13 CHECK, FOUND CRACK ON STRINGER 18A AT STATION 727 ON THE RT SIDE. MAINTENANCE REMOVED CRACK ON STRINGER 18A AT STATION 727 ON THE RT SIDE IAW AMERICA WEST AIRLINES (AWA) ENGINEERING REPAIR (E.R.) NR 03-5361-05175-ES2. FORMED FILLER AND RADIUS FILLER IAW AWA ER 03-5361-057175. INSTALLED FABRICATED REPAIR PARTS IN ADDITION TO REPAIR GUSSET AND ORIGINAL ANGLE IAW AWA ER NO 03-5361-05175-ES2. 2L72 4F RTA16WE 20050712001342005071200134NM 2005 7 12 AWXA200500756 120050624A2797 CONNECTOR BOEING737 73733A 1384673NM TE FLAPS DIRTY A AWXAO OTHER F FLT CONT AFFECTED LDLANDING 1 WP28174AW50837859 23633 ON LANDING, FLAPS AT ZERO, HOT LANDING. LANDED WITHOUT FURTHER INCIDENT. CREW REPORTED FLAP PROBLEM TO TOWER PRIOR TO LANDING. CREW REQUESTED PRIORITY LANDING DUE TO FLAP PROBLEM. UPON LANDING, CREW WROTE UP FLAP INDICATOR SHOWS SPILT FLAPS AT FLAPS UP POSITION. USED ALTERNATE FLAP SWITCH TO EXTEND LEADING EDGES. MX ORIGINALLY R & R FLAP INDICATOR ON 06/22/05. INDICATOR WAS NOT THE FIX, R & R IAW AMWEST PART TASK CARD ALONG WITH LT TRANSMITTER IAW AWA TASK CARD. OPS TESTS GOOD. TEAR DOWN REPORT OF THE TRANSMITTER SHOWS THAT THE CONNECTOR WAS DIRTY CAUSING THE UNIT TO BE INTERMITTENT. UNIT WAS CLEANED, EO COMPLIED WITH AND RE-TESTED IAW CMM 27-50-18 REV4. OPS TESTS GOOD. 2L72 4F RTA16WE 20050712001402005071200140EA 2005 7 12 VTZA200500133 120050706A53206013501223 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27662BR 7526 INTERCOSTAL ON AFT SIDE OF FS 621 LT SIDE AT STRINGER 16 CRACKED 1.214 INCH. 2L72 4F RTA21EA 20050712001482005071200148NM 2005 7 12 SWAA051952 120050705A335020131 BATTERY BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 DURING SCHEDULED RON CHECK, FOUND AFT GALLEY OVERHEAD EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20050712001492005071200149NE 2005 7 12 AWXA200500757 220050626A7230 COMPRESSOR AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE NR 1 ENGINE DIRTY A AWXAO OTHER B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 WP28644AW 317 219 ODOR DETECTED. DURING FLIGHT, PACKS CREATING GYM SOCK ODOR WITH PASSENGERS COMPLAINING. MAINTENANCE OPERATED PACKS WITH APU BLEED AIR AND ENGINE BLEED AIR. DISCOVERED ODOR COMING FROM NR 1 ENGINE BLEED AIR SOURCE, ABOVE IDLE. INSPECTED NR 1 ENG AND UNABLE TO FIND OIL LEAK. FOUND BLACK SUBSTANCE PRESENT AT STAGE 3 HPC. SUSPECT VSV LUBRICANT. PERFORMED COMPRESSOR WASH OF NR 1 ENG IAW AMERICA WEST AIRLINES (AWA) TASK CARD S5M72303. ALSO, REPLACED NR 1 AND NR 2 OZONE FILTERS DUE TO CONTAMINATION FROM NR 1 ENG BLEED AIR, IAW AWA TASK CARD S2C21301. OPERATIONAL CHECKS GOOD, NO ODOR PRESENT WHEN PACKS RUNNING OFF OF NR 1 ENG BLEED AIR SOURCE. 2L72 4F4 FRTA28NM E311NE 20050712001502005071200150NM 2005 7 12 AWXA200500758 120050609A5315654581094 FLOORBEAM BOEING737 7373B7 138447FNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28328AW 23377 DURING C-13 CHECK FOUND CORROSION ON FLOORBEAM AT BS 312, WL 208, BL 12R. MAINTENANCE REMOVED CORROSION ON FLOORBEAM AT BS 312, WL 208, BL 12R AND FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-10-51-2 FIG 205. FABRICATED REPAIR ANGLES IAW BOEING 737-300 SRM 53-10-51-2 FIG 205. CUT AND DRILLED EXTRUSION FOR UPPER CHORD IAW BOEING 737-300 SRM 53-10-51-2 FIG 205. INSTALLED FABRICATED REPAIR PARTS AT BS 312, WL 208, BL 12R IAW BOEING 737-300 SRM 53-10-51-2 FIG 205. 2L72 4F RTA16WE 20050712001512005071200151NM 2005 7 12 AWXA200500759 120050610A52106545871523 SKIN BOEING737 7373B7 1384580NM R1 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28328AW 23377 MAJOR REPAIR. DURING C-13 CHECK FOUND R1 DOOR OUTER SKIN CRACKED AT UPPER HINGE CUTOUT. CRACK .125 INCHES IN LENGTH. MAINTENANCE CUT OUT CRACKED AREA AT R1 DOOR OUTER SKIN. CRACKED AT UPPER HINGE. CUTOUT IAW AMERICA WEST AIRLINES ENGINEERING REQUEST (E.R.) NO. 03-5241-05166-SS2. FABRICATED REPAIR DOUBLER IAW E.R. NO. 03-5241-05166-SS2. INSTALLED FABRICATED REPAIR PARTS AT R1 DOOR OUTER SKIN CRACKED AT UPPER HINGE CUTOUT IAW E.R. NO. 03-5241-05166-SS2. 2L72 4F RTA16WE 20050712001592005071200159WP 2005 7 12 ASAA0580211 120050420A5330 SKIN DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02958AS 53024 DURING C-CHECK, FOUND FUSELAGE SKIN CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050712001622005071200162WP 2005 7 12 ASAA0580216 120050425A575499375903 RIB DOUG DC9 DC983 3022083WP NR 4 SLAT CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02958AS 53024 DURING C-CHECK, FOUND LT WING NR 4 SLAT ACCESS CUTOUT RIB CRACKED. INSTALLED REPAIR DOUBLER PER EA 5740-01447. (M) 2L72 4F RTA6WE 20050712001692005071200169WP 2005 7 12 ASAA0580214 120050421A523059101417 SKIN DOUG DC9 DC983 3022083WP CARGO BAY DOOR CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02972AS 53448 DURING HV-CHECK, FOUND AFT CARGO BAY DOOR FORWARD EDGE CHAFED AT UPLATCH HOOK. REMOVED DAMAGED AREA. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050712001702005071200170WP 2005 7 12 ASAA0580215 120050427A521059100817 SKIN DOUG DC9 DC983 3022083WP L1 DOOR GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02972AS 53448 FOUND DURING HV CHECK, FORWARD PAX (L-1) DOOR SKIN GOUGED AND BENT AT BOTTOM FORWARD EDGE. REMOVED DAMAGE. INSTALLED REPAIR DOUBLER AND FILLER. (M) 2L72 4F RTA6WE 20050712001712005071200171EA 2005 7 12 COMA0570075 120050626A3350YAD4F RELAY CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHTSMALFUNCTIONED A COMAK NONE O OTHER TXTAXI/GRND HDL 1 SO01340CA 10062 CABIN EMERGENCY LIGHTS FLICKER ON AND OFF. REPLACED RELAY K135. 2L72 4F RTA21EA 20050712001722005071200172SO 2005 7 12 MASA200500281 120050404A335020131A BATTERY PACK EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSDISCHARGED A MASAO OTHER O OTHER TXTAXI/GRND HDL 1 SW07842MJ 145457 EMERGENCY LIGHTS INOPERATIVE. APU AUTO SHUTDOWN WHILE AIRCRAFT UNATTENDED. MAINTENANCE CURRENTLY TROUBLESHOOTING SYSTEM AS WELL AS OTHER BATTERY BUS SYSTEMS. MAINTENENCE REMOVED AND REPLACED 1-4 BATTERY PACKS. 2L72 4T RTT00011AT 20050712001802005071200180EA 2005 7 12 MASA200500445 120050606A3350 POWER SUPPLY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSDISCONNECTED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0717275 7275 EMERGENCY EXIT STRIP LIGHTS THAT WOULD NOT ILLUMINATE. MX SECURED CONNECTION TO NR 2 POWER SUPPLY TO CLEAR FAULT. 2L72 4F RTA21EA 20050712001852005071200185EA 2005 7 12 MASA200500450 120050608A3350 LIGHT CNDAIRCL600 CL6002D24 1390016EA EMERGENCY LIGHTSMISSING A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07908FJ 15008 SEATS 16A AND C EMERGENCY FLOOR LIGHTING MISSING. MAINTENANCE INSTALLED NEW LIGHTING STRIP. 2L72 4F RTA21EA 20050712001912005071200191NM 2005 7 12 SWAA051942 120050705A53156546811 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 1016, LBL 15 TO LBL 35, WL 208. REPAIRED FLOORBEAM PER BFG ER. 2L72 4F RTA16WE 20050712001942005071200194NM 2005 7 12 05FDEA01824 120050707A5330 SKIN BOEING727 727200 138407ENM FUSELAGE LIGHTNING STRIKEA FDEAK NONE O OTHER ININSP/MAINT 1 SO25263FE 21625 LIGHTNING STRIKE IN SKIN AT BS 441 1.5 X 1.5 INCH AT STR 23. *S/D* REPAIRED LIGHTNING STRIKES IAW SRM 53-30-3. 2L73 4F RTA3WE 20050712002022005071200202NM 2005 7 12 AWXA200500787 120050707A25602013A BATTERY BOEING737 73733A 1384673NM FLASHLIGHT DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW 23634 LAS - EES - WHILE ON GROUND CREW REPORTED THE FORWARD EMERGENCY FLASHLIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY FLASHLIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20050712002082005071200208NM 2005 7 12 AWXA200500800 120050706A53206545834525 INTERCOSTAL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 MCN - MAJOR REPAIR - DURING C16 CHECK FOUND INTERCOSTAL CRACKED 1.12 INCHES IN LENGTH AT FORWARD SIDE OF FLOORBEAM AT BL 0, WL 208, AND BS 360. MAINTENANCE REMOVED INTERCOSTAL AT FORWARD SIDE OF FLOORBEAM AT BL 0, WL 208, BS 360 IAW BOEING 737-300 SRM 51-40-02-0 FIG 8 AND FIG 12. RECEIVED NEW INTERCOSTAL AND PREPARED FOR INSTALLATION IAW BOEING 737-300 SRM 51-40-05-0 FIG 2, 3 AND 4. INSTALLED REPAIR PARTS AT FORWARD SIDE OF FLOORBEAM AT BL 0, WL 208, BS 360 IAW BOEING 737-300 SRM 51-40-02 FIGURES 3, 4, 6, 7 AND 12. 2L72 4F RTA16WE 20050712002092005071200209EU 2005 7 12 AWXA200500801 120050709A3250C247360001 CONTROL SERVO AIRBUS320 A320232 3930326EU NLG STEERING INOPERATIVE A AWXAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 WP28619AW4694211606 527 PHX - LANDING GEAR - DURING TAXI OUT AND START UP OF NUMBER TWO ENGINE, NOSE WHEEL STEERING FAILED. MAINTENANCE REMOVED AND REPLACED THE NOSE WHEEL STEERING SERVO CONTROL, 6GC, IAW AIRBUS MM 32-51-51-04. OPERATIONAL CHECKS WERE GOOD. VENDOR CONFIRMED FAILURE. EXCESSIVE CURRENT WAS REQUIRED TO MAINTAIN HYDRAULIC BALANCE. ALSO FOUND THE SERVO VALVE, SENSOR OUTPUT VOLTAGE EXCEEDING THE MANUFACTURE SPECIFICATIONS. UNIT WAS REPAIRED AND TESTED IAW OHM 32-57-01 REV.8. ALSO COMPLIED WITH SERVICE BULLETINS C24736-32-3173, C24736-32-3174 AND C24736-32-3193. UNIT WAS ALSO MODIFIED PER AMERICA WEST EO 3251-01001. 2L72 4F RTA28NM 20050712002192005071200219EA 2005 7 12 MASA200500459 120050611A3350 LIGHT CNDAIRCL600 CL6002D24 1390016EA EMERGENCY LIGHTSINOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07906FJ 15006 FWD CEILING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE RESET SYSTEM. 2L72 4F RTA21EA 20050712002272005071200227SO 2005 7 12 SWIA200515200 120050629A3350 SIGN EMB 120 EMB120ER 3260203SO EMERGENCY LIGHTSLOOSE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07564SW 120339 LT OVERWING EXIT (6A) SIGN FELL OFF. REINSTALLED EXIT SIGN AS REQUIRED. 2L72 4T RTA31SO 20050712002282005071200228SO 2005 7 12 SWIA200515201 120050624A27523430001005 ACTUATOR EMB 120 EMB120ER 3260203SO TE FLAPS LEAKING A SWIAO OTHER K FLUID LOSS APAPPROACH 1 NM07291SW1166011660 120318 LT INBOARD FLAP COVERED WITH HYDRAULIC FLUID. REPLACED LT INBOARD FLAP ACTUATOR IAW EMB 120 AMM 27-50-00. 2L72 4T RTA31SO 20050712002292005071200229EA 2005 7 12 SWIA200515202 120050626A2750 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS OUT OF RIG A SWIAAD UNSCHED LANDING RETURN TO BLOCK F FLT CONT AFFECTED CLCLIMB 1 NM07919SW 7657 AFTER DEPARTURE FLAPS WOULD NOT RETRACT PAST FLAPS 8. RIGGED BPSU'S IAW CRJ MM 27-51-10. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050712002312005071200231EA 2005 7 12 SWIA200515204 120050629A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07407SW3347 3347 7034 FLAPS FAIL CAUTION MESSAGE AFTER FLAPS RETRACTED. REPLACED LT BPSU AND RE-RIGGED FLAP SYSTEM IAW MM 27-51-10. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050711001832005071100183EA 2005 7 11 SWIA200515168 120050618A274170623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07925SW 7682 STAB TRIM CHANNEL NR 1 WILL NOT ENGAGE. INSTALLED SERVICEABLE MOTOR CONTROL UNIT REF AMM 27-42-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050711001852005071100185EA 2005 7 11 SWIA200515170 120050613A2741 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA COCKPIT STICKS A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07410SW 7066 CAPT YOKE STAB TRIM SWITCH STICKS. REPLACE TRIM SWITCH IAW MM 27-44-03. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050711001962005071100196 2005 7 11 ASAA0540294 420050613A256561620468 SLIDE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU R1 DOOR FAILED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM02773AS343814566 25106 OKC - DURING HEAVY MX, R1 DOOR ESCAPE SLIDE OP-CHECK WAS ACCOMPLISHED ON 737-400. OPS CHECK OF THIS EES INCLUDED ARMING THE DOOR SLIDE AND OPENING THE DOOR. THE SLIDE COMPART OPENED AND THE SLIDE FELL, ACTIVATING THE INFLATION PROCESS PROPERLY. TE INFLATABLE BEGAN TO FILL, REACHING, BUT NO BREAKING THE FRANGIBLE LINKS. THE COMPRESSED GAS FLOWED UNTIL THE BOTTLE WAS EMPTY HOWEVER THE FRANGIBLE LINKS NEVER PARTED. THE SLIDE WAS NOT USEABLE AS AN EXIT ROUTE AND FAILED THE CHECK. DUE TO THE SIMILARITY OF THESE FAILURES, FEEL THE ROOT CAUSE OF THIS FAILURE WAS INGESTIONS OF BUBBLE WRAP INTO THE ASPIRATOR, STALLING INFLATION, PREVENTING THE FRANGIBLE LINKS FROM BREAKING AND RENDERING THE INFLATABLE UNUSABLE. 2L72 4F4 FRTA16WE E21EU 20050711001992005071100199NM 2005 7 11 ASAA0540293 120050605A57536546430129 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU T/E FORE FLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02785AS 27628 DENT FOUND AT LT WING IB T/E FORE FLAP. REPAIRED LT WING IB T/E FORE FLAP IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050711002142005071100214 2005 7 11 05FDEA01651 420050622A3451 ANTENNA BOEING727 7272S2F 1384O81NM NR 1 DME CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25203FE 22925 NR 1 DME ANTENNA CORRODED. REMOVED AND REPLACED NR 1 DME ANTENNA IAW 34-45-011-4. 2L73 4F A3WE 20050711002182005071100218NM 2005 7 11 05FDEA01695 120050626A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25619FE 48770 WITH REFERENCE TO WORK CARD E1-5510-7-5000, RT BARREL NUT HOLE NR 36R FOUND OUT OF LIMIT AFTER CORROSION REMOVAL. REPAIR CARRIED OUT AS PER FEDEX EA 1-5510-83021 2L73 4F RTA22WE 20050711002212005071100221CE 2005 7 11 DXTA200500797 120050621A2611 CONNECTOR RAYTHNDH125 HAWKER800XP 7150012CE CARGO BAY LOOSE E DXTAA UNSCHED LANDING JN WARNING INDICATION FALSE WARNING CRCRUISE 1 GL07893QS 258393 CARGO BAY FIRE LIGHT ANNUNICATOR ILLUMINATED STEADY IN FLIGHT (APPROX 5 SECONDS). REMOVED ACCESS PANELS TO FOM ON FWD AFT SMOKE DETECTORS. VISUALLY INSPECTED SMOKE DETECTORS (3EA). FOUND FWD CONNECTOR LOOSE. TIGHTENED PLUG. CLEANED SCREEN. RE-INSTALLED ACCESS PANELS. INSPECTED AREA AROUND SMOKE DETECTORS. NO DEFECTS AT THIS TIME. OPS CHECK GOOD IAW HAWKER 800XP AMM. REMOVED ACCESS PANELS TO FOM ON FWD AFT SMOKE DETECTORS. VISUALLY INSPECTED SMOKE DETECTERS (3EA). FOUND FWD CONNECTOR LOOSE. TIGHTENED PLUG. CLEANED SCREENS. PERFORMED OPS CHECK, GOOD. TIGHTENED CONNECTORS. RE-INSTALLED ACCESS PANEL. INSPECTED AREA AROUND SMOKE DETECTOR. NO DEFECTS AT THIS TIME IAW HAWKER 800XP AMM. 2L72 4F RTA3EU 20050711002292005071100229NM 2005 7 11 05FDEA01690 120050626A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25619FE 48770 WITH REFERENCE TO WORK CARD E1-5510-7-5000, LT BARREL NUT HOLE NR 27L FOUND OUT OF LIMIT AFTER CORROSION REMOVAL. REPAIRED AS PER FEDEX EA 1-5510-83022. 2L73 4F RTA22WE 20050711002432005071100243SO 2005 7 11 CHQA200500121 120050626A335066368 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11267SK 145268 LAST EMERGENCY LIGHT STRIP ON FLOOR IS INOPERATIVE. REMOVED AND REPLACED LIGHT STRIP IN ACCORDANCE WITH AMM 33-50-12. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050711002562005071100256EA 2005 7 11 SWIA200515178 120050620A2720 RUDDER PEDAL CNDAIRCL600 CL6002B19 1900309EA COCKPIT BINDING A SWIAK NONE L NO TEST ININSP/MAINT 1 NM07969SW 7876 CAPT RUDDER PEDALS BIND WHEN DOING FLIGHT CONTROL CHECK. REPLACED UPPER AND LOWER BEARING HOUSING WITH NEW BEARINGS FOR THE LT FORWARD RUDDER PIVOT ASSY, AMM 27-21-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050712000602005071200060NM 2005 7 12 SWAA051978 120050707A5320BAC15171489 CHANNEL BOEING737 7373H4 1384600NM COCKPIT FLOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29608SW 27928 DURING SCHEDULED D-CHECK, FOUND COCKPIT FLOOR ZEE CHANNEL CORRODED AT BS 270, RBL 10 TO LBL 10, WL 207.5. REMOVED AND REPLACED ZEE CHANNEL PER SRM. 2L72 4F RTA16WE 20050712000802005071200080NM 2005 7 12 QXEA200501078 120050623A6123YD4N RELAY DHAV DHC8 DHC8202 2809007NM HAMSTD14SF 14SF7 NE PROP FEATHER INOPERATIVE A QXEAD RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 NM09355PH 500 RETURNED TO GATE, FAILURE OF AUTOFEATHER TO ARM ON TAKEOFF. AIRSPEED 60 KTS. TRQ APPROX 85 PERCENT. REMOVED AND REPLACED 6121 K-5 RELAY. ALL CHECKS GOOD. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 6 CP7NE 20050712001052005071200105NM 2005 7 12 SWAA052005 120050708A53206936656 WEB BOEING737 7373H4 1384600NM FUSLEAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29608SW 27928 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FLOOR WEB CORRODED AT BS 1030, RBL 2, WL 208. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050712001292005071200129NM 2005 7 12 EIA2005125 120050516A3350 CONNECTOR BOEING747 747273C 1384896NM EMERGENCY LIGHTSLOOSE A EIAAK NONE O OTHER ININSP/MAINT 1 NM09471EV 20651 FOUND NR 5 EMERGENCY EXIT SIGN AT R5 DOOR INOPERATIVE, DMI 962 ISSUED. RECONNECTED CONNECTORS TO WIRING FROM SIGN. R5 DOOR EMERGENCY EXIT SIGN OPS CKS OK IAW MM 33-51-00 PG 501. DMI CLEARED. PLACARD REMOVED. 2L74 4F A20WE 20050712001422005071200142 2005 7 12 ASMF200506027 420050627A3422 GYRO DOUG MD80 MD83 3023681NM COCKPIT FAILED W ASMFED ENGINE SHUTDOWN RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23861LF 49826 DURING LEFT ENGINE STARTING, CAPTAIN REPORTED DFGC NR 1 OUT OF SERVICE AND FLIGHT DIRECTOR SHOWED FD AND SPD MESSAGES. ENGINES WERE SHUTDOWN. DFGCS WERE INTERCHANGED AND BREAKERS WERE RESET, DISAPPEARING TRI FLIGHT DIRECTOR FLAGS. TESTS WERE PERFORMED IAW MM 34-22-00. DURING OVERNIGHT SERVICE, RETURN TO SERVICE TEST TO BOTH DFGCS WERE PERFORMED IAW MM 22-01-05, TESTED CORRECT. 2L72 4F RT 20050712001452005071200145NM 2005 7 12 SWAA051949 120050705A53306545777 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29332SW 23696 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050712001472005071200147NM 2005 7 12 SWAA051951 120050705A53206545409 WEB BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29332SW 23696 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE BEADED WEB CRACKED AT BS 664, RBL 40. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050712001642005071200164WP 2005 7 12 ASAA0580218 120050425A533099055601 SKIN DOUG DC9 DC983 3022083WP FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02958AS 53024 FOUND DURING C-CHECK, FUSELAGE SKIN GOUGED. REMOVED DAMAGE. REPAINTED. (M) 2L72 4F RTA6WE 20050712001732005071200173EA 2005 7 12 MASA200500399 120050527A3350 LIGHT CNDAIRCL600 CL6002D24 1390016EA EMERGENCY LIGHTSINOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07909FJ 15009 ALL EMERGENCY EXTERIOR LIGHTS INOPERATIVE. CREW CAME OUT TO AIRCRAFT AND NOTICED EMERGENCY SWITCH WAS LEFT ON OVERNIGHT. LIGHTS OPERATED NORMALLY. 2L72 4F RTA21EA 20050712001792005071200179SO 2005 7 12 MASA200500433 120050603A3350 LIGHT EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSINOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07846MJ 145507 RT OVERWING EMERGENCY LIGHT INOPERATIVE. RELAMPED. 2L72 4T RTT00011AT 20050712001812005071200181SO 2005 7 12 MASA200500447 120050606A3350 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSNOT SEATED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07855MJ 145614 ROW 12F EMERGENCY EXIT SIGN INOPERATIVE. MX SECURED CONNECTOR TO LIGHT ASSY. NO FURTHER DEFECTS NOTED. 2L72 4T RTT00011AT 20050712001922005071200192 2005 7 12 CALA0500214 420050707A2330RDAA707601 MONITOR BOEING767 767424ER 1385270NM SEAT 27L INOPERATIVE A CALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2778060 29455 THE VIDEO LCD MONITOR AT THE SEAT BACK OF SEAT 27L BECAME HOT TO THE TOUCH AND BEGAN TO SMOKE WHILE EN ROUTE FROM EWR TO HNL. THE SEATS IN THE ZONE FROM ROW 23 TO ROW 27 WERE POWERED OFF AND THE SMOKE CEASED. THE FLIGHT WAS CONTINUED TO HNL WHERE IT LANDED WITHOUT FURTHER INCIDENT. THE AREA AND HARNESS WERE INSPECTED FOR DAMAGE AND NONE WAS FOUND. THE FAULT WAS ISOLATED TO THE MONITOR AND THE MONITOR WAS REPLACED IAW MM 23-32-83. OPERATIONAL CHECKS WERE NORMAL. 2L72 4F RTA1NM 20050712001962005071200196NM 2005 7 12 05FDEA01828 120050707A5330 SKIN BOEING727 727200 138407ENM FUSLEAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25263FE 21625 MAIN CARGO DOOR BS 620 TO 640 LBL 24 WL 287 DOOR CUTOUT INNER PLATE HAS NUMEROUS GOUGES. *S/D* BLENDED NUMEROUS GOUGES AT MAIN CARGO DOOR CUTOUT INNER PLATE PER EA 7-5330-89309. 2L73 4F RTA3WE 20050712001982005071200198NM 2005 7 12 05FDEA01832 120050707A5310 PLATE BOEING727 727200 138407ENM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25263FE 21625 MAIN CARGO DOOR BS 460 TO 640 LBL 45 WL 295 DOOR CUTOUT INNER PLATE HAS NUMEROUS GOUGES. *S/D* BLENDED AND REPAIRED GOUGES IN MAIN CARGO DOOR INNER PLATE IAW EA 7-5330-89309. 2L73 4F RTA3WE 20050712002032005071200203NM 2005 7 12 AWXA200500788 120050630A521080330035 RESERVOIR BOEING757 7572G7 1384963NM DOOR R2 LOW A AWXAK NONE O OTHER ININSP/MAINT 1 WP28909AW 24522 SAL - EES - DURING C1 CHECK FOUND THE L2 EMERGENCY RESERVOIR PRESSURE LOW. MAINTENANCE REMOVED AND REPLACED THE RESERVOIR IAW BOEING 757 MM 52-11-30. 2L72 4F RTA2NM 20050712002052005071200205EA 2005 7 12 COMA0560368 120050629A2751 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA FLAPS ACTIVATED A COMAO OTHER JN WARNING INDICATION FALSE WARNING APAPPROACH 1 SO01796CA 7338 FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2L72 4F RTA21EA 20050712002142005071200214NM 2005 7 12 AWXA200500794 120050625A5754 SKIN BOEING737 7373G7 1384595NM ZONE 500 DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 296 23777 MCN - MAJOR REPAIR - DURING C16 CHECK FOUND DISBOND AREA ON BOTTOM OF NR 2 SLAT WEDGE. MAINTENANCE REMOVED SKIN AND DISBONDED CORE SECTION FROM BOTTOM OF NR 2 SLAT WEDGE IAW BOEING 737-300 SRM 51-70-10-0 REPAIR 7, FIG 16. MAINTENANCE FABRICATED REPAIR DOUBLER AND OBTAINED REPAIR HONEYCOMB CORE IAW BOEING 737-300 SRM 51-70-10-0 REPAIR 7. BONDED REPAIR PARTS TO BOTTOM OF THE NR 2 SLAT WEDGE IAW BOEING 737-300 SRM 51-70-10-0. 2L72 4F RTA16WE 20050712002162005071200216NM 2005 7 12 AWXA200500795 120050627A5754 SKIN BOEING737 7373G7 1384595NM ZONE 600 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 273R 23777 MCN - MAJOR REPAIR - DURING C-16 CHECK DISCOVER 4 CRACKS IN BOTTOM OF THE NR 5 SLAT SKIN AT SS 163 TO SS 174. MAINTENANCE REMOVED DAMAGED AREA IAW BOEING 737-300 SRM 57-43-01-2. FABRICATED REPAIR FILLER AND SPLICE PLATE IAW BOEING 737-300 SRM 57-43-01. INSTALLED FABRICATED REPAIR PARTS IAW BOEING 737-30051-40-02-0 FIG 14. 2L72 4F RTA16WE 20050712002222005071200222NM 2005 7 12 MASA200500462 120050613A3350 CONNECTOR DHAV DHC8 DHC8202 2809007NM EMERGENCY LIGHTSDISCONNECTED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07991HA 431 SEAT 8 AND 9 C, D PASSENGER KICKED FLOOR EMERGENCY STRIP LIGHT. MX RE-SECURED LIGHT STRIP. 2H72 4T RTA13NM 20050712002232005071200223NM 2005 7 12 AWXA200500766 120050608A532065C1988316 CHANNEL BOEING737 7373B7 1384580NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28328AW 23377 DURING C-13 CHECK DISCOVERED CORROSION ON HAT CHANNEL LOCATED AT BS 956.5 + 7 AND FROM BL 14R TO BL 44R, WL 204. MAINTENANCE REMOVED CORROSION AT BS 956.5 + 7, FROM BL 14R TO BL 44R, WL 204 AND FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-51-1 FIG 101. ALSO, DISCOVERED TO BE A PREVIOUS BLEND OUT OF SECTION. REMOVED HAT CHANEL AT BS 956.5 + 7, FROM BL 14R TO BL 44R, WL 204 FOR REPLACEMENT AND FABRICATED HAT SECTION IAW BOEING 737-300 SRM 51-40-02-0 FIG 13, BOEING 737-300 SRM 51-40-05-0 PAR 4A AND BOEING DWG 65C19883. INSTALLED FABRICATED REPAIR PARTS AT BS 956.5 + 7, FROM BL 14R TO BL 44R, WL 204 IAW BOEING 737-300 51-40-02-0 FIG 12. 2L72 4F RTA16WE 20050713000322005071300032EA 2005 7 13 SWIA200515199 120050629A2740 TRIM PANEL CNDAIRCL600 CL6002B19 1900309EA STAB MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07975SW 7951 IN FLIGHT STAB TRIM CH 1 INOP MSG. REPLACED STAB TRIM ENGAGE PANEL. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050713000342005071300034EA 2005 7 13 SWIA200515205 120050628A2760C13045BA03 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07726SK 10190 CREW REPORTS SPLR/STAB FAULT MESSAGE IN FLIGHT. REPLACED NR 2 SSCU. OPERATIONAL CHECK GOOD. REF CRJ MM27-61-05. 2L72 4F RTA21EA 20050713000352005071300035EA 2005 7 13 SWIA200515206 120050321A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07915SW 7615 FS 280 L FLOORBEAM LBL 9.0 OB ATTACH ANGLE CRACKED (ITEM FOUND AT C-CHECK INSPECTION.) ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00 AND 51-21-11. 2L72 4F RTA21EA 20050713000482005071300048EA 2005 7 13 SWIA200515209 120050321A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07915SW 7615 ENGINE SUPPORT BEAM LHS LWR WEB LBL 38 CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-61-366 REV E. 2L72 4F RTA21EA 20050713000512005071300051EA 2005 7 13 SWIA200515212 120050321A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07915SW 7615 FS 621 FLOOR SUPPORT ANGLE LBL 42 CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED ANGLE IAW CRJ REO 601R-53-61-117 REV B. 2L72 4F RTA21EA 20050713000532005071300053 2005 7 13 AWXA200500768 420050629A256561620468 GIRT BAR BOEING737 7373Y0 1384671NM L1 DOOR SLIDE LOOSE A AWXAO OTHER O OTHER TXTAXI/GRND HDL 1 WP28323AW 23684 DURING GROUND HANDLING CREW REPORTED DOOR L1 SLIDE/GIRT BAR LOOSE. MAINTENANCE REPACKED L1 DOOR SLIDE GIRT BAR AND SLIDE IAW AMERICA WEST AIRLINES TASKCARD R1C25001. 2L72 4F RTA16WE 20050713000542005071300054EU 2005 7 13 AWXA200500769 120050628A2560P4010021000 BATTERY AIRBUS320 A320232 3930326EU FLASHLIGHT DISCHARGED A AWXAO OTHER O OTHER TXTAXI/GRND HDL 1 WP28662AW 1274 DURING GROUND HANDLING, FLIGHT ATTENDANT REPORTED FORWARD INBOARD CABIN EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED FORWARD INBOARD EMERGENCY EXIT FLASHLIGHT BATTERY. 2L72 4F RTA28NM 20050713000562005071300056NM 2005 7 13 AWXA200500771 120050630A5330 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 DURING CHECK, FOUND 2 INCH LONG CRACK ON FUSELAGE SKIN AT STATION 767, STRINGER 24R. MAINTENANCE REMOVED DAMAGED SKIN AT STATION 767, STRINGER 24R AND FABRICATED REPAIR DOUBLER IAW BOEING 737-300 SRM 53-00-01 FIG 229. INSTALLED FABRICATED REPAIR PARTS AT STATION 767, STRINGER 24R AND ISSUED MONITOR TO RE-INSPECT REPAIR IN 60,000 FLT CYCLES IAW BOEING 737-300 SRM 53-00-01 FIG 229. MONITOR CONTROL NR 250772. 2L72 4F RTA16WE 20050713000582005071300058EU 2005 7 13 UPS05144745 120050615A5411A5451506320400 ANGLE AIRBUSA300 A300F4622R 3930360EU NR 2 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01122UP 0807 NR 2 AFT LOWER PYLON AT RIB 18 HAS CRACK APPROX .75 L AT RIB SECTION MEMBER INBD. MEMBER 2 PLACES ABOVE AND BELOW NUTPLATE. REMOVED AND REPLACED L-ANGLE ON THE NR 2 PYLON IAW A300 SRM 51-40-00. 2L72 4F RTA35EU 20050713000592005071300059EU 2005 7 13 UPS05144746 120050615A5420A5451506320300 ANGLE AIRBUSA300 A300F4622R 3930360EU NR 1 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01122UP 0807 NR 1 AFT LOWER PYLON AT RIB 18 BOTH INBD AND OTBD SECTION MEMBERS ARE CRACKED ABOVE AND BELOW CNTR NUTPLATE. REMOVED AND REPLACED L-ANGLE MEMBERS IAW A300 SRM 51-40-00 AND 51-40-21. 2L72 4F RTA35EU 20050713000622005071300062WP 2005 7 13 UPS05844743 120050529A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 DEEP CORROSION AROUND SHEAR TIE FASTENER HEADS AFT SIDE OF FRAME, STA 1300 LONGERON 36. REMOVED CORROSION AND FOUND FRAME OUT OF LIMITS. REMOVED DAMAGED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0 FIG 2. 2L74 4F RT4A25 20050713000652005071300065WP 2005 7 13 UPS05844760 120050630A3350 BATTERY PACK DOUG DC8 DC873F 302199FWP EMERGENCY LIGHTSDISCHARGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 EMERGENCY LIGHT BATTERY INOP. REMOVED & REPLACED EMERGENCY LIGHTING BATTERY & RELAY ASSY & OPS CK GOOD IAW MM 33-50-01-2. 2L74 4F RT4A25 20050713000702005071300070NM 2005 7 13 MASA200500479 120050622A3350 BULB DHAV DHC8 DHC8202 2809007NM EMERGENCY LIGHTSBURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07444YV 444 CREW REPORTED AN AFT EMERGENCY EXIT LIGHT INOP. MX REPLACED LIGHT BULB AND OPS CHECK NORMAL. 2H72 4T RTA13NM 20050713000712005071300071 2005 7 13 2005UALA00597 420050622A256562772213 SLIDE BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE 2L DOOR LEAKING A UALAK NONE L NO TEST ININSP/MAINT 1 WP29794UA 26953 HOLE FOUND ON LOWER SIDE OF UPPER TUBE. SLIDE WOULD NOT HOLD PRESSURE. SLIDE WAS REMOVED FROM AIRCRAFT AT NORMAL MAINTENANCE INTERVAL. SLIDE FAILED AIR RETENTION TEST DUE TO WEAR DAMAGE ON INFLATABLE LOWER TUBE. IT WAS OBSERVED THAT THE SLIDE HAD BEEN PACKED CORRECTLY. THE EXACT CAUSE OF THE WEAR DAMAGE COULD NOT BE DETERMINED. DAMAGE WAS REPAIRED BY PATCHING PER AIR CRUISERS CMM 25-61-32. 2L72 4F4 FRTT0001SE E46NE 20050713000732005071300073NM 2005 7 13 CALA0500209 120050701A53206545812 FLOOR SUPPORT BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714334 23572 INSPECTION FOUND 4 INCH CRACK IN FLOOR SUPPORT AT STA 328, LBL 11. CRACKED AREA CUT OUT AND REPAIRED IAW SRM 51-70-12, FIGURE 1, SHEET 6. 2L72 4F RTA16WE 20050713000752005071300075NM 2005 7 13 CALA0500211 120050703A53306545775594 SKIN BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776355 23593 INSPECTION FOUND 1.625 INCH CRACK IN FUSELAGE SKIN AT STA 727E, S22R TO S23R. SKIN REPAIRED IAW ECRA 5330-03459. 2L72 4F RTA16WE 20050713000762005071300076NE 2005 7 13 CALA0500212 220050701A7200 ENGINE BOEING737 737824 13844BZNM GE CFM56 CFM56* 13802NE NR 2 MALFUNCTIONED A CALAAFD UNSCHED LANDING ACTIVATE FIRE EXT. RETURN TO BLOCK O OTHER CLCLIMB 1 SW2716234 28946 874822 LOUD THUMP HEARD AFTER T/O. ALL ENG IND`S NORMAL THROUGH CLIMB-OUT TO 10,000 FT. PASSING 10,000 FT SEVERAL SUCCESSIVE THUMPS WITH NO ABNORMAL ENG IND`S. A/C RETURNED WITH NORMAL LANDING. ENG SHUTDOWN AFTER LANDING. L-1 AND L-2 DOOR SLIDES DEPLOYED & PAX`S EVACUATED AS PRECAUTION DUE TO REPORTS OF POSSIBLE SMOKE ON NR 2 ENG. BOTH FIRE BOTTLES BLOWN. INITIAL EXAM OF NR 2 ENG FOUND NO EVIDENCE OF FIRE DAMAGE OR UNCONTAINED FAILURE. NR 2 ENG R & R. OPS CHKS GOOD. IN ADDITION, L-1 AND L-2 DOOR SLIDES AND FIRE BOTTLES REPLACED. VSV STAGE ONE ROTATED OUT OF TIMING(NUT BACKED OFF) RESULTING IN VSV FRACTURE. OUT OF TIME VSV INDUCED HPC FAILURE. 2L72 4F4 FRTA16WE E2GL 20050713000772005071300077NM 2005 7 13 2005UALA00592 120050626A5330141W23136 SKIN BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29216UA18546 30549 DENT IN FUSELAGE RT SIDE OF ACFT FWD OF STATION 382 HALFWAY BETWEEN E/E DOOR AND ELECTRICAL PANEL P30. DAMAGE RESULTING FROM GROUND EQUIPMENT IMPACT. INITIAL INTERIM REPAIR ACCOMPLISHED AT 2,641 PTC, 18,546 PTT. PERMANENT REPAIR ACCOMPLISHED PER 777SRM 53-00-01, REPAIR 3 AT 2,749 PTC AND 19,696 PTT. 2L72 4F4 FRTT0001SE E46NE 20050713000782005071300078NM 2005 7 13 2005UALA00593 120050626A5230 SKIN BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE CARGO DOOR DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29657UA 27112 DENT IN BULK CARGO DOOR, .5 INCHES BELOW EXISTING EXTERNAL REPAIR DOUBLER. INTERIM REPAIR PER EVA MOC1-8779A. ACCOMPLISH A DETAILED, EXTERNAL VISUAL INSPECTION EVERY 'A' CHECK UNTIL NEXT 'C10' CHECK. INTERIM REPAIR PER EVA MOC1-8779A. ACCOMPLISH A DETAILED, EXTERNAL VISUAL INSPECTION EVERY 'A' CHECK UNTIL NEXT 'C10' CHECK. MF4762 CREATED TO MONITOR. 2L72 4F4 FRTA1NM E24NE 20050713000792005071300079NM 2005 7 13 2005UALA00594 120050626A5220 DOOR AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE EMERGENCY EXIT OPEN A UALAA UNSCHED LANDING JN WARNING INDICATION FALSE WARNING CLCLIMB 1 WP29844UA 1581 PILOTS REPORTED LT OVERWING DOOR OPEN ECAM MESSAGE. LATCH COVER (PLASTIC PART) FELL OFF IN FLIGHT (REMOVED?). PART SHOULD HAVE BEEN REINSTALLED AND WARNING WOULD HAVE GONE OUT. COVER HAS PROXIMITY SWITCH TO ENSURE CLOSED. THIS PROXIMITY SWITCH, IN ADDITION TO PROXIMITY SWITCH ON THE PLUG DOOR ARE WHAT WILL SEND MESSAGES TO ECAM. 2L72 4F4 FRTA28NM E40NE 20050713000802005071300080NM 2005 7 13 2005UALA00598 120050625A5514 ATTACH ANGLE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE HORIZONTAL STAB CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29340UA 24244 HORIZONTAL STAB CENTER SECTION CENTER LT SIDE 3 EACH BEAM ATTACHED ANGLES CRACKED, NR 1 UPPER FWD, NR 2 LOWER FWD AND NR3 LOWER AFT. REPLACED 3 EACH CRACKED FITTINGS REF SRM 51-40-02. 2L72 4F4 FRTA16WE E2GL 20050713000812005071300081NM 2005 7 13 2005UALA00602 120050627A335058807 STRIP BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE EMERGENCY LIGHTSMISSING A UALAK NONE O OTHER ININSP/MAINT 1 WP29937UA 26668 AFT GALLEY EMERGENCY EEL STRIP IN FRONT OF CART STOWAGE COMPARTMENT MISSING. SUPPLEMENTAL DATA UPDATE EEL STRIP WAS MISSING AND WAS REPLACED. 2L72 4F4 FRTA16WE E2GL 20050713000842005071300084NM 2005 7 13 2005UALA00605 120050627A3350 LIGHT BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE EMERGENCY LIGHTSINOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29664UA 29236 EEL INOP AT SEAT ROW 26 TO 36 RT SIDE. FOUND SEAT EEL HARNESS AT 35HJ RIPPED OUT OF ITS MOLEX CONNECTORS UNDER THE SEAT AND FROM THE SIDEWALL CONNECTOR. WIRING WAS REPAIRED. OK 2L72 4F4 FRTA1NM E24NE 20050713000882005071300088 2005 7 13 2005UALA00608 420050629A2565D30664105 TUBE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE ESCAPE SLIDE DAMAGED A UALAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP29403UA 442 3 IN LONG SLICE ON LOWER TUBE. SLICE OR LACERATION ON THE INFLATABLE TUBE COULD BE DUE TO MISHANDLING DURING UNIT TRANSPORTATION. THE DAMAGE WAS REPAIRED AND RETESTED OK. 2L72 4F4 FRTA28NM E40NE 20050713000902005071300090NM 2005 7 13 UPS05444775 120050627A533065B0766151 SKIN BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INTERIM REPAIR AFT OF ELECTRICAL ACCESS DOOR. CORROSION BLEND OUT 2 BY 5 IN , SKIN INTERNAL BONDED DOUBLER CORRODED. REMOVED PER HX RS NR R53-30-35332 AND UPS EA NR 747-53-20252 AND STRAP REPLACED PER SRM 51-10-01. 2L74 4F A20WE 20050713000922005071300092NM 2005 7 13 UPS05444777 120050629A5312 PRESSURE PANEL BOEING747 747121 1384871NM NLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 RT NWW SIDE PANEL FOUND 2 EA CRACK BOTH APPROX 1 INCH AT BTN BS 260 AND 280, WL 150, CRACK LENGTH 1 IN. RT NWW SIDE PANEL REPAIRED AS PER SRM 53-10-04 FIG 116. 2L74 4F A20WE 20050713000932005071300093NM 2005 7 13 UPS05444778 120050629A5312 PRESSURE PANEL BOEING747 747121 1384871NM NLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 LT NWW SIDE PANEL FOUND CRACK AT BTWN BS 280 AND 300, WL 170 APPROX 1 IN, CRACK LENGTH 1 IN. LT NWW SIDE PANEL REPAIRED AS PER SRM 53-10-04 FIG 11. 2L74 4F A20WE 20050713000942005071300094NM 2005 7 13 UPS05444779 120050629A5312 PRESSURE PANEL BOEING747 747121 1384871NM NLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 LT NWW SIDE PANEL FOUND CRACKED AT BTN BS 280 AND 300 WL 160 APPROX 2 INCH. REPAIRED AS PER SRM 53-10-04 FIG 116. 2L74 4F A20WE 20050713000972005071300097NM 2005 7 13 UPS05444782 120050617A5347 SEAT TRACK BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 BS 540-660 LBL 28 INCH SEAT TRACK CORRODED. CORROSION BLEND OUT 0.050 BY 2 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A. 2L74 4F A20WE 20050713001042005071300104NM 2005 7 13 UPS05444789 120050618A5315 FLOORBEAM BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 BS 980 LBL 11 TO 33 FLOORBEAM CORRODED. CORROSION BLEND OUT 0.043 BY 1.0 BY 1.5 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS. FLOORBEAM REPAIRED AS PER SRM 51-40-04 FIG 1. 2L74 4F A20WE 20050713001072005071300107NM 2005 7 13 UPS05444792 120050621A5347 SEAT TRACK BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 BS 640 RBL 47 SEAT TRACK CROWN FOUND CORRODED. CORROSION BLEND OUT 0.040 BY 0.5 BY 1.0 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A. 2L74 4F A20WE 20050713001082005071300108NM 2005 7 13 UPS05444793 120050621A5311 FRAME BOEING747 747123F NM AFT CARGO CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 AFT CARGO, STA 1560 RT FRAME UPR FLANGE FOUND CRACK JUST BELOW SLOPE PANEL SUPPORT, CRACK LENGTH 2.0 IN. AFT CARGO BAY BS 1560 BTN STRINGER 36R - 38R FRAME REPAIRED AS PER SRM 53-10-04 FIG 66 DETAIL 1. 2L74 4F A20WE 20050713001092005071300109NM 2005 7 13 UPS05444794 120050617A5320 WEB BOEING747 747123F NM CARGO BAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 BULK CARGO, BS 1960 STR 36L TO STR 37L FRAME WEB AND INNER CHORD FOUND CRACKED, CRACK LENGTH WEB 5 IN, CHORD 1.5 IN. BULK CARGO, BS 1960 STR 36L TO STR 37L FRAME WEB REPAIRED AS PER SRM 53-10-04 FIG 66 AND INNER CHORD REPAIRED AS PER SRM 51-40-03 FIG 2. 2L74 4F A20WE 20050713001102005071300110NM 2005 7 13 UPS05444795 120050618A5315 FLOORBEAM BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 BS 760 LBL 65 FLOORBEAM FOUND CORRODED. CORROSION BLEND OUT 0.055 BY 0.5 BY 2.5 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS. FLOORBEAM REPAIRED AS PER SRM 51-40-04 FIG 1. 2L74 4F A20WE 20050713001122005071300112WP 2005 7 13 UPS05844754 120050524A5320 FLOOR SUPPORT DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE:C-3. MAIN CABIN SUB FLOOR STA 960 RBL 60 UNDER FLOORBEAM AREA CORRODED. CUT OUT DAMAGE ON SUBFLOOR STA 960 RBL60. REMOVED CORROSION ON FLOORBEAM. FABRICATED AND INSTALLED FILLER, 2 FINGER DOUBLERS, 2 DOUBLERS AND 1 SPLICE DOUBLER IAW EO DC8-5310-22416-A AND SAA SK 840-8 07643. 2L74 4F RT4A25 20050713001132005071300113WP 2005 7 13 UPS05844755 120050525A5330 SKIN DOUG DC8 DC873F 302199FWP L1 DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE:C-3. EXTERNAL FUSELAGE L1 DOOR CUTOUT UPPER AFT CORNER, SKIN VISUALLY CRACKED. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER, TRIPLER AND FILLER IAW EO DC8 5330-22342-A AND SAA SK 840-807798. 2L74 4F RT4A25 20050713001162005071300116WP 2005 7 13 UPS05844761 120050608A5347 SEAT TRACK DOUG DC8 DC871F 302199DWP CABIN CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01705UP 45949 MAIN CABIN SEAT TRACK HAS HEAVY CORROSION, STA 1480 RBL 50. REMOVED AND REPLACED SEAT TRACK SECTION FROM STA 1460-1580 RBL 50 IAW SRM 51-3-0. 2L74 4F RT4A25 20050713001192005071300119WP 2005 7 13 UPS05844765 120050605A55225644440501 SKIN DOUG DC8 DC871F 302199DWP LT ELEVATOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01705UP 45949 INSPECTION TYPE:C-2. LT ELEVATOR CONTROL TAB SKIN AND DOUBLER CRACKED AT INBD EYEBOLT ACCESS HOLE LWR SKIN. REMOVED AND REPLACED LT ELEVATOR CONTROL TAB ASSY PER TASK CARD 3016 STEP 13. 2L74 4F RT4A25 20050713001212005071300121SW 2005 7 13 YTRR104408 120050630A6321407340302101 CALIPER BELL 407 407 1182206SW ROTOR BRAKE CRACKED B YTRAO OTHER O OTHER NRNOT REPORTED 1 SW03595RL1156 53595 ON ROUTINE INSPECTION FOUND CALIPER HOUSING CRACKED AT MOUNTING FLANGE ON ROTOR BRAKE. 1G71 3U O H2SW 20050713001222005071300122WP 2005 7 13 UPS05844766 120050608A534037540231N FITTING DOUG DC8 DC871F 302199DWP CARGO BAY CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01705UP 45949 INSPECTION TYPE:C-2. A-PIT AT STA 320 L33R, BATH TUB FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED BATH TUB FITTING AT A-PIT STA 320 L33R IAW SRM 53-2-0 FIG 1F, 51-1-20D, AND 51-1-21. 2L74 4F RT4A25 20050713001232005071300123WP 2005 7 13 UPS05844767 120050608A5347DC853B003501 SEAT TRACK DOUG DC8 DC871F 302199DWP STA375 RBL59 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01705UP 45949 INSPECTION TYPE:C-2. HEAVY CORROSION IN SEAT TRACK ALONG RBL 59 STA 375-420. REMOVED AND FABRICATED SEAT TRACK PER DWG S2400463. INSTALLED FABBED SEAT TRACK AT STA 375-420 PER SRM 53-2-3. 2L74 4F RT4A25 20050713001242005071300124WP 2005 7 13 UPS05844768 120050607A532037552222 FLOOR SUPPORT DOUG DC8 DC871F 302199DWP MAIN CABIN CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01705UP 45949 INSPECTION TYPE:C-2. MAIN CABIN STA 759 LBL24 UNDER SEAT TRACK. SEAT TRACK FLOOR SUPPORT FITTING CRACKED. REMOVED AND REPLACED SUPPORT FITTING AT STA 759 LBL24 IAW 51-1-20D, AND 51-3-0. 2L74 4F RT4A25 20050713001262005071300126WP 2005 7 13 UPS05844771 120050608A534037558271N FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01705UP 45949 INSPECTION TYPE:C-2. BANANA FITTING CRACKED AT STA 340 L33R. REMOVED AND REPLACED BANANA FITTING AT STA 340 L33R IAW SRM 51-1-20D. 2L74 4F RT4A25 20050713001272005071300127WP 2005 7 13 UPS05844772 120050607A5542 SKIN DOUG DC8 DC871F 302199DWP RUDDER DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01705UP 45949 INSPECTION TYPE:C-2. UPPER PORTION OF RUDDER ON RT SIDE JUST ABOVE LOGO, OIL CANNING OF SKIN. REMOVED AND REPLACED SKIN ON RT SIDE OF RUDDER JUST ABOVE LOGO IAW DC8 DWG 5655077 AND SRM 51-1-8, AND 51-1-21A. NO WEIGHT AND BALANCE DUE TO 1FOR 1 SKIN CHANGE. 2L74 4F RT4A25 20050713001332005071300133EA 2005 7 13 MASA200500490 120050625A3350 POWER SUPPLY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSDISCHARGED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0787353 7353 RT EMERGENCY LIGHT OVER WING INOP. MAINTENANCE REMOVED AND REPLACED EMERGENCY NR 2 BATTERY POWER SUPPLY. 2L72 4F RTA21EA 20050714000012005071400001EU 2005 7 14 ALGA104413 120050606A6510C651A200H01 COUPLING UROCOPEC120 EC120B 8680987EU TAIL ROTOR CRACKED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03510AL 1251 ONE LAMINATE CRACKED. REPLACED WITH NEW BY FIELD MAINTENANCE. 1G72 3U NCR0001RD 20050714000022005071400002SW 2005 7 14 ALGA104382 120050622A6220406310405101 PITCH LINK BELL 407 407 1182206SW MAIN ROTOR BINDING B ALGAK NONE O OTHER ININSP/MAINT 1 SW03436AL200 53069 BINDING AND RATCHETY / REPLACED WITH NEW BY FIELD MAINTENANCE. 1G71 3U O H2SW 20050714000032005071400003SW 2005 7 14 ALGA104430 120050624A6220406310405101 PITCH LINK BELL 407 407 1182206SW MAIN ROTOR BINDING B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03409AL183 53494 PITCH LINK HAS EXCESSIVE AXIAL PLAY; BINDING AND RATCHETY / REPLACED WITH NEW BY FIELD MAINTENANCE. 1G71 3U O H2SW 20050714000042005071400004EU 2005 7 14 ALGA104383 120050622A6220C622A1003103 SCISSORS UROCOPEC120 EC120B 8680987EU MAIN ROTOR DEBONDED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03514AL263 1266 WEAR PLATE DEBONDED / REPLACED WITH NEW OR SERVICEABLE BY FIELD MAINTENANCE. 1G72 3U NCR0001RD 20050714000062005071400006EU 2005 7 14 109070705DG 120050707A3210NAS624H8 BOLT AGUSTAA109 A109A 0260109EU MLG SHEARED B JBZRK NONE O OTHER ININSP/MAINT 1 WP2722RX 7155 DURING A ROUTINE PREFLIGHT INSPECTION, OUR BASE MECHANIC VISUALLY IDENTIFIED A LOOSE BOLT (P/N NAS624H8) ATTACHING THE MAIN LANDING GEAR INBOARD ACTUATOR SUPPORT TO THE AIRFRAME. UPON CLOSER INSPECTION, THE BOLT WAS FOUND TO BE SHEARED ABOUT 2 THREADS AWAY FROM THE SHANK OF THE BOLT. THE AIRCRAFT WAS HOISTED TO EXPAND THE INSPECTION TO INCLUDE REMOVING THE AIRFRAME CROSS BRACE (P/N 109-0320-19-3). NO ADDITIONAL DEFECTS WERE NOTED AND THE AIRCRAFT LANDING GEAR ASSEMBLIES WERE REINSTALLED IN THE AIRCRAFT USING NEW HARDWARE PER AGUSTA MM CHAPT 32-10-00. 1G72 3U H7EU 20050714000082005071400008EA 2005 7 14 COMA0550382 120050706A5210 VENT CNDAIRCL600 CL6002B19 1900309EA PAX DOOR OBSTRUCTED A COMAEA ENGINE SHUTDOWN UNSCHED LANDING O OTHER DEDESCENT 1 SO01785CA 7326 FLIGHT 5811- CABIN ALTITUDE CAUTION. F/A REPORTS LOUD SQUEAL FROM CABIN DOOR. FOUND DOOR TRIM OBSTRUCTING THE DOOR VENT VALVE, SECURED TRIM. PRESSURE CHECKS SATISFACTORY. 2L72 4F RTA21EA 20050714000132005071400013NM 2005 7 14 05FDEA01837 120050707A5753 HINGE DOUG MD11 MD11 3023602NM LT WING TE FLAPSCORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 LT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. REPAIR CARRIED OUT AS PER EA 1-5750-87588. 2L73 4F RTA22WE 20050714000142005071400014NM 2005 7 14 05FDEA01838 120050707A5753 HINGE DOUG MD11 MD11 3023602NM LT WING TE FLAPSCORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 LT WING - O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. CORROSION REPAIRED AS PER CMM 20-11-02 AND EA 1-5750- 87588. 2L73 4F RTA22WE 20050714000162005071400016NM 2005 7 14 05FDEA01840 120050707A5753 HINGE DOUG MD11 MD11 3023602NM LT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 LT WING - O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. REPAIR CARRIED OUT AS PER EA 1-5750-87588. 2L73 4F RTA22WE 20050714000182005071400018EA 2005 7 14 VNAA0506011 120050624A3234 HANDLE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE MLG UNSECURE A VNAAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 GL05705PS 10144 WHEN GEAR UP WAS SELECTED THE GEAR DISAGREE WARNING MESSAGE ILLUMINATED AND THE LANDING GEAR DID NOT RETRACT. THE CREW FOLLOWED THE QRH AND RETURNED TO DAY. MAINTENANCE FOUND THE LANDING GEAR EMERGENCY EXTENSION HANDLE NOT FULLY STOWED. THE HANDLE WAS PROPERLY STOWED AND THE LANDING GEAR WAS OPERATIONALLY CHECKED IAW CRJ700 AMM 32-30-00-710-801-A01. ALL OPS CHECKS WERE GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050714000192005071400019EA 2005 7 14 VNAA0506012 120050624A2520 SWITCH CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE SEAT 11 D-F STUCK A VNAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL05244PS 7912 DURING CLIMB THE FLIGHT ATTENDANT CALL SWITCH AT SEATS 11D/F BECAME STUCK IN THE ON POSITION CAUSING THE AURAL CHIME TO SOUND CONTINUOUSLY IN THE CABIN. WHEN THE FLIGHT ATTENDANT TRIED TO UNSTICK THE SWITCH THE OXYGEN MASKS ABOVE 11D/F DEPLOYED. THE CREW RETURNED TO CLT. MAINTENANCE STOWED THE OXYGEN MASKS AND DEFERRED THE PSU AT SEAT 11D/F PER MEL 25-70-01-4 CAT D. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050714000202005071400020EA 2005 7 14 VNAA0507003 120050703A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE FUSELAGE BIRD STRIKE A VNAAO OTHER O OTHER NRNOT REPORTED 1 GL05719PS 10177 THE CREW REPORTED A LIGHTNING STRIKE ON THE NOSE OF THE AIRCRAFT. MAINTENANCE COMPLIED WITH LIGHTNING STRIKE INSPECTIONS IAW CRJ700 AMM 05-51-07-210-801 & 05-51-07-220-801. THE DAMAGE WAS REPAIRED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050714000212005071400021EA 2005 7 14 VNAA0506015 120050629A5330 ACCESS PANEL CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE EXTERIOR OPEN A VNAAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 GL05703PS 10137 THE CREW OF FLIGHT 2258 RETURNED TO MEM AFTER HEARING A LOUD SQUEAL AND WIND NOISE FROM THE NOSE OF THE AIRCRAFT DURING CLIMBOUT. MAINTENANCE FOUND THE EXTERNAL SERVICE PANEL DOOR OPEN. THE DOOR WAS INSPECTED AND OPERATIONALLY CHECKED IAW CRJ700 AMM 52-45-36-400-801-A01. NO DAMAGE WAS FOUND. THE DOOR WAS SECURED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050714000222005071400022EA 2005 7 14 VNAA0506014 120050628A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT WING TIP LIGHTNING STRIKEA VNAAO OTHER O OTHER NRNOT REPORTED 1 GL05241PS 7909 AFTER LANDING THE CREW REPORTED A LIGHTNING STRIKE. MAINTENANCE COMPLIED WITH LIGHTNING STRIKE INSPECTIONS IAW CRJ200 AMM 05-51-05-210-801 AND 05-51-05-220-801. LIGHTNING DAMAGE FOUND ON THE LEFT WING TIP WAS REPAIRED IAW BOMBARDIER REO 601R-57-30-001. NO ADDITIONAL DEFECTS WERE FOUND. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050714000242005071400024EA 2005 7 14 VNAA0507002 120050703A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE LIGHTNING STRIKEA VNAAO OTHER O OTHER DEDESCENT 1 GL05202PS 7858 THE CREW REPORTED A LIGHTNING STRIKE DURING DESCENT. MAINTENANCE COMPLIED WITH A DETAILED LIGHTNING STRIKE INSPECTION IAW CRJ200 AMM 05-51-05-220-801. THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE REPAIRED THE LIGHTNING DAMAGE AND RELEASED THE AIRCRAFT FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050714000252005071400025 2005 7 14 2005UALA00552 420050609A256569B522155 BEARING BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE GIRT BAR BROKEN A UALAK NONE O OTHER ININSP/MAINT 1 WP29661UA 27158 DURING PACKING PROCEDURES, 6 BEARINGS BROKE WHEN TENSION PUT ON BAR. AIRFRAME MANUFACTURER IS AWARE OF THIS ISSUE AND IS EVALUATING CHANGE TO MORE DURABLE BEARING MATERIAL. IN THIS CASE, ALL OF THE BROKEN BEARINGS WERE REPLACED. 2L72 4F4 FRTA1NM E24NE 20050714000262005071400026NM 2005 7 14 2005UALA00611 120050703A5311 FRAME BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CHAFED A UALAK NONE O OTHER ININSP/MAINT 1 WP29318UA 23950 STA 211 FRAME WEB WAS CHAFED BEYOND LIMITS BETWEEN STR 15R AND 16R, FRAME WAS ALSO GOUGED BEYOND LIMITS. SPLICED IN NEW SECTION OF WEB REF SRM 51-70-13 FIG 1 AND SPLICED IN NEW FRAME FROM STR 15R TO 17R REF SRM 51-70-12. 2L72 4F4 FRTA16WE E21EU 20050714000282005071400028NM 2005 7 14 2005UALA00613 120050701A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29562UA 26664 EXTERNAL FUSELAGE SKIN DENTED 1 INCH BELOW FLOOR LEVEL AND 10 INCHES FORWARD OF 2 LT MED. MAJOR REPAIR WAS ACCOMPLISHED PER UA-EVA-50430. 2L72 4F4 FRTA2NM E17NE 20050714000292005071400029NM 2005 7 14 2005UALA00615 120050705A335020131A BATTERY PACK BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU RT OVERWING DISCHARGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29343UA 24247 RIGHT OVERWING EMERGENCY EXIT SIGN AND SIDEWALL EXIT LIGHT INOP. LOW BATTERY REPLACED, OK. 2L72 4F4 FRTA16WE E21EU 20050714000312005071400031NM 2005 7 14 2005UALA00617 120050701A5312 BULKHEAD AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE FUSLEAGE CUT A UALAK NONE O OTHER ININSP/MAINT 1 WP29855UA 1737 DAMAGE CUT THROUGH SKIN FWD OF PRESSURE BULKHEAD APPROX 6 INCHES LONG AND 8-9 INCHES WIDE. INSTALLED DOUBLER REPAIR AND SPLICED STRINGER SECTION REF UA EVA-50432 AND SRM53-00-11 FI G 227. 2L72 4F4 FRTA28NM E40NE 20050714000332005071400033NM 2005 7 14 2005UALA00619 120050705A3350362624 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT BURNED OUT A UALAK NONE L NO TEST ININSP/MAINT 1 WP29187UA 26877 EEL AT ROW 56 SEATS DEF INOPERATIVE. EEL LIGHT BURNED OUT. REPLACED, OK. 2L74 4F4 FRTA20WE E24NE 20050714000352005071400035NM 2005 7 14 2005UALA00621 120050702A3350362624 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE RH ROWS 32,33,34BURNED OUT A UALAK NONE L NO TEST ININSP/MAINT 1 WP29194UA 26892 EEL INOPERATIVE RT ROWS 32, 33, 34. EEL LIGHTS BURNED OUT. REPLACED, OK. 2L74 4F4 FRTA20WE E24NE 20050714000362005071400036NM 2005 7 14 2005UALA00622 120050703A3350582240 POWER SUPPLY BOEING747 747422 1384935NM PWA 4056 PW4056 NE DOOR 1R & 1ST CLMALFUNCTIONED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29193UA 26890 1R DOOR EMERGENCY LIGHT AND 1ST CLASS RIGHT SIDE FLOOR EMERGENCY LIGHTS ON WITH SWITCH ARM INFLIGHT. SIDE & FLOOR EMERGENCY LIGHTS ON WITH SWITCH ARMED. REPLACED POWER SUPPLY. 2L74 4F4 FRTA20WE E24NE 20050714000372005071400037NM 2005 7 14 2005UALA00623 120050703A339760243 WIRE BOEING757 757222 1384956NM PWA 2037 PW2037 NE DOOR 2L TORN A UALAK NONE L NO TEST ININSP/MAINT 1 WP29506UA 24627 EEL FEEDER MID CABIN BY L2 DOOR IS TORN. REPLACED EEL STRIP. 2L72 4F4 FRTA2NM E17NE 20050714000382005071400038NM 2005 7 14 2005UALA00624 120050701A3350362624 LAMP BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE DOOR 2R INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29660UA 27115 EEL LIGHT ADJACENT DR 2R INOPERATIVE. EEL LAMP WAS DAMAGED. REPLACED EEL LAMP, OK. 2L72 4F4 FRTA1NM E24NE 20050714000402005071400040 2005 7 14 2005UALA00626 420050703A2565 SLIDE AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE DOOR 1L LOW A UALAK NONE L NO TEST ININSP/MAINT 1 WP29829UA 1211 DOOR 1L SLIDE PRESS JUST OUTSIDE GREEN ARC. SLIDES BEING REMOVED DUE TO LOW BOTTLE PRESSURE IS NOT TOTALLY AN UNCOMMON EVENT. THE OPERATING ENVIRONMENT OF SLIDES (VIBRATION, DOOR OPENING/CLOSING, CARTS IMPACTING DOORS, TEMPERATURE & PRESSURE CHANGES) ARE AMONG THE FACTORS THAT COULD RESULT IN BOTTLE LEAKS. SEALS HOWEVER SHOULD AS MUCH AS POSSIBLE KEEP THE PRESSURE DURING THE 36-MONTH SERVICE LIFE OF THE SLIDE ASSEMBLY. ANY BOTTLE THAT IS FOUND LEAKING IS REQUALIFIED IN THE SHOP AS REQUIRED BY THE 49CFR. DURING BOTTLE REQUALIFICATION, ALL SEALS ARE REPLACED WITH NEW ONES. SINCE SLIDE BOTTLES ARE NOT 100% RELIABLE, THEY ARE CHECKED BEFORE EACH FLIGHT TO ENSURE THAT THE PRESSURE IS NORMAL. 2L72 4F4 FRTA28NM E40NE 20050714000412005071400041 2005 7 14 2005UALA00627 420050707A2565 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE DOOR 1R SLIDE INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29104UA 26902 SLIDE LIGHT AT DOOR 1R INOPERATIVE. RELAMPED. 2L74 4F4 FRTA20WE E24NE 20050714000432005071400043NM 2005 7 14 2005UALA00596 120050625A2150 SMOKE BOEING757 757222 1384956NM PWA 2037 PW2037 NE COCKPIT DETECTED A UALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP29553UA 25277 RETURNED TO THE FIELD DUE TO SMOKE IN THE COCKPIT. CAUSE OF INCIDENT WAS A FAILED THRUST DISK & BEARING IN LT ACM. COMPONENT FINDINGS WERE A FAILED THRUST DISK & A FAILED BEARING WHICH ALSO DAMAGED TURBINE & COMPRESSOR SECTIONS. THRUST DISK, BEARING TURBINE ASSY & COMPRESSOR WERE ALL REPLACED & UNIT MADE SERVICEABLE. THIS UNIT INSTALLED ON 06 JUN 2000 & ACCUMULATED A TOTAL OF 15,397 HRS & 5,718 CYCLES PRIOR TO FAILURE. CURRENT MX PROGRAM IS ON CONDITION FOR ACM. A HEALTH CHECK IS PERFORMED ON SYS & TEMP SENSORS CHECKED & CALIBRATED AT 1C. NO CORRECTIVE ACTIONS OR MX PROGRAM CHANGES REQUIRED AT THIS TIME. 2L72 4F4 FRTA2NM E17NE 20050714000482005071400048NM 2005 7 14 2005UALA00633 120050705A33500105924001 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE ROW 13 INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29187UA 26877 EMERGENCY LIGHT INOPERATIVE, CEILING ROW 13. REPLACED BURNED OUT LIGHT. 2L74 4F4 FRTA20WE E24NE 20050714000502005071400050NM 2005 7 14 2005UALA00635 120050705A3350582233 BATTERY BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29187UA 26877 EEL INOPERATIVE, UPPER DECK AFT SIDEWALL. REPLACED LOW BATTERY. 2L74 4F4 FRTA20WE E24NE 20050714000512005071400051NM 2005 7 14 2005UALA00636 120050705A33977956323 WIRE BOEING747 747422 1384935NM PWA 4056 PW4056 NE ROWS 55 - 59 LOOSE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29187UA 26877 EEL INOPERATIVE, SEAT ROWS 55-59 RT. RESECURED LOOSE CABLE. 2L74 4F4 FRTA20WE E24NE 20050712002212005071200221NM 2005 7 12 AWXA200500799 120050630A531165163005 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 MCN - MAJOR REPAIR - DURING C16 CHECK FOUND FRAME WEB CRACKED AT FASTENER HOLE AT BS 178, WL 230, AND LBL 17.1. MAINTENANCE REMOVED DAMAGED AREA OF FRAME WEB AT BS 178, WL 230, LBL 17.1 IAW BOEING 7370399 SRM 53-10-08-2 FIG 212. OBTAINED AND PREPARED NEW WEB AND SHIMS FOR INSTALLATION IAW BOEING 737-300 SRM 53-10-08-2 FIG 212. INSTALLED REPAIR PARTS AT BS 178, WL 230, LBL 17.1 IAW BOEING 737-300 SRM 53-10-08-2 FIG 212. 2L72 4F RTA16WE 20050712002252005071200225NM 2005 7 12 CALA0500207 120050701A323065C310991 LOCK ACTUATOR BOEING737 7373T0 1384582NM NLG MALFUNCTIONED A CALAO OTHER J WARNING INDICATION APAPPROACH 1 SW2714324 23375 MLG EXTENDED INSTANTLY WHEN GEAR HANDLE WAS PLACED DOWN ON APPROACH. NLG EXTENDED AFTER MLG EXTENDED DOWN AND LOCKED. MAINTENANCE UNABLE TO DUPLICATE FAULT. NLG LOCK ACTUATOR REMOVED AND REPLACED AS PRECAUTIONARY MEASURE IAW MM 32-33-31. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20050713000432005071300043EA 2005 7 13 SWIA200515207 120050321A5340 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07915SW 7615 FS 280 RT FLOORBEAM RBL 9.0 IB AND OB ANGLES CRACKED ITEM FOUND AT C-CHECK INSPECTION. ANGLES REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00 AND 51-21-11. 2L72 4F RTA21EA 20050713000472005071300047EA 2005 7 13 SWIA200515208 120050321A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07915SW 7615 INTERCOSTAL CRACKED, FS 484, LBL 36, ITEM FOUND AT C-CHECK INSPECTION. REPAIR CARRIED OUT IAW REO 601R-53-41-059 REV A. 2L72 4F RTA21EA 20050713000572005071300057EA 2005 7 13 QXEA200501086 120050630A2840 CIRCUIT BREAKER CNDAIRCL600 CL6002C10 1390015EA FUEL INDICATING POPPED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09613QX 10045 RETURNED TO GATE. CROSSFLOW PUMP CAUTION MESSAGE. RESET FUEL CONTROL SYSTEM CIRCUIT BREAKERS. FAULTS CLEARED. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20050713000612005071300061NM 2005 7 13 UPS05444742 120050622A5311 FRAME BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 CARGO BAY, STA 2180 RBL 58 FRAME UPPER CHORD LWR SURFACE FOUND CRACKED. CRACK LENGTH 1.25 IN . CORROSION BLEND OUT N/A. CARGO BAY STA 2180 RBL 58 IN FRAME REPAIRED AS PER SRM 53-10-04 FIG 66. 2L74 4F A20WE 20050713000642005071300064WP 2005 7 13 UPS05844751 120050630A3350 BATTERY PACK DOUG DC8 DC873F 302199FWP EMERGENCY LIGHTSDISCHARGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 EMERGENCY LIGHTING SYS INOP. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACK PER MM 33-50-01. OPS CKS GOOD. 2L74 4F RT4A25 20050713000672005071300067NM 2005 7 13 ASMF200507001 120050701A274295901 MOTOR DOUG MD80 MD83 3023681NM STAB FAILED W ASMFK NONE L NO TEST ININSP/MAINT 1 SW23831LF2742418 53050 CAPTAIN REPORTED PRIMARY STAB TRIM STICKS OCCASIONALLY. COMPENSATION MECHANISM OF HORIZONTAL STABILIZER CHECKED IAW MM 27-40-0, BEING CORRECT. DURING TESTS, PRIMARY MOTOR OF STABILIZER FAILED. REPLACED IAW MM 27-40-01. TESTED CORRECT. 2L72 4F RT 20050713000742005071300074NM 2005 7 13 CALA0500210 120050701A53306545774 SKIN BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2777303 23354 INSPECTION FOUND 2.5 IN CRACK FORWARD OF STA 787 ABOVE S24L. DOUBLER REPAIR INSTALLED IAW SRM 53-00-01. 2L72 4F RTA16WE 20050713000872005071300087 2005 7 13 2005UALA00607 420050628A256519C181918E PRESSURE VALVE BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE ESCAPE SLIDE MALFUNCTIONED A UALAK NONE O OTHER ININSP/MAINT 1 WP29793UA 26946 BROKEN PRV FOUND IN SLIDE WHEN OPENED FOR OVERHAUL. SLIDE WOULD NOT HOLD AIR PRESSURE. DAMAGED PRESSURE RELIEF VALVE WAS OBSERVED DURING SLIDE/RAFT COMPONENT SHOP MAINTENANCE. THE EXACT CAUSE OF THE DAMAGE TO THE PRESSURE RELIEF VALVE COULD NOT BE DETERMINED, BUT IT IS SPECULATED IT WAS DAMAGED DURING THE LAST PACKING PROCESS. PRESSURE RELIEF VALVE ASSEMBLY WAS REPLACED. 2L72 4F4 FRTT0001SE E46NE 20050713000912005071300091NM 2005 7 13 UPS05444776 120050629A5320 WEB BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 RT NWW SIDE PANEL FOUND CRACKED AT BTN BS 260 AND 280 WL 170, CRACK LENGTH 2.5 IN. REPAIRED AS PER SRM 53-10-04 FIG 116. 2L74 4F A20WE 20050713000962005071300096NM 2005 7 13 UPS05444781 120050629A5312 PRESSURE PANEL BOEING747 747121 1384871NM NLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 LT NWW SIDE PANEL FOUND CRACKED AT BTN BS 280 AND 300 WL 150 APPROX 1 INCH CRACK LENGTH 1 INCH. REPAIRED AS PER SRM 53-10-04 FIG 116. 2L74 4F A20WE 20050713001032005071300103NM 2005 7 13 UPS05444788 120050618A5347 SEAT TRACK BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 STA 550-590 LBL 47 IN SEAT TRACK CORROSION. CORROSION BLEND OUT 0.030 BY 0.25 BY 3.5 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A. 2L74 4F A20WE 20050713001052005071300105NM 2005 7 13 UPS05444790 120050617A5347 SEAT TRACK BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 U/D BS 600 TO 660 LBL 47 SEAT TRACK CORRODED. CORROSION BLEND OUT 0.040 BY 1.0 BY 3.0 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A. 2L74 4F A20WE 20050713001152005071300115WP 2005 7 13 UPS05844759 120050525A5312 PANEL DOUG DC8 DC873F 302199FWP LT WW CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 HEAVY CORROSION ON LT WW CEILING STA 860 LBL 61. CUT OUT DAMAGE AND INSTALLED REPAIR PARTS IAW EO DC8-5310-22401-A AND SAA SK 840-807868. 2L74 4F RT4A25 20050713001182005071300118WP 2005 7 13 UPS05844763 120050608A5347 SEAT TRACK DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01705UP 45949 C2 SEAT TRACK HEAVILY CORRODED AT STA 420 LBL 25. REMOVED AND REPLACED SEAT TRACK AT STA 360-560 LBL 25 IAW SRM 51-3-0, 51-3-2, 53B-003-501. 2L74 4F RT4A25 20050713001202005071300120EU 2005 7 13 B65A104368 120050626A6340L771M40C1004 INDICATOR UROCOPEC135 EC135T1 5620026EU TRIPLE TACH INOPERATIVE B B65AO OTHER P NO WARNING INDICATION CRCRUISE 1 GL13135CR2168 0164 BOTH ENGINE N2 INDICATIONS FAILED IN FLIGHT. 1G72 3U H88EU 20050713001292005071300129SO 2005 7 13 MASA200500469 120050615A3350 LIGHT EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSINOPERATIVE A MASAO OTHER L NO TEST NRNOT REPORTED 1 SW07831MJ 145273 OVER WING EMERGENCY EXIT LIGHT WOULD NOT TEST WHEN TESTED BY FLIGHT ATTENDANT. MX PERFORMED OPERATIONAL CHECK OF LIGHTS. CHECKED OK. 2L72 4T RTT00011AT 20050713001312005071300131EA 2005 7 13 MASA200500483 120050623A3350 CIRCUIT BOARD CNDAIRCL600 CL6002D24 1390016EA EMERGENCY LIGHTSMALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07915FJ 15015 EMERGENCY LIGHTS ILLUMINATE IN ARMED POSITION. MAINTENANCE REMOVED AND REPLACED CIRCUIT BOARD. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050713001322005071300132EA 2005 7 13 MASA200500489 120050625A3350BR9279232 LIGHT CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHTSINOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07510MJ 10101 DURING WALK AROUND DISCOVERED ROW 12 EMERGENCY FLOOR LIGHT NOT ILLUMINATING. REPLACED LIGHT ASSEMBLY AFTER TROUBLESHOOTING. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050714000072005071400007EA 2005 7 14 COMA0570082 120050705A5610NP1393226 WINDOW CNDAIRCL600 CL6002C10 1390015EA COCKPIT CRACKED A COMAO OTHER O OTHER NRNOT REPORTED 1 SO01641CA4920 10122 FLIGHT 5296- COPILOT SIDE WINDOW CRACKED. REPLACED WINDOW. 2L72 4F RTA21EA 20050714000442005071400044NM 2005 7 14 2005UALA00629 120050704A3350362624 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE ROW 36 INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29116UA 26908 EEL INOPERATIVE ROW 36 RT. EEL LAMP INOP. REPLACED EEL LAMP, OK. 2L74 4F4 FRTA20WE E24NE 20050714000472005071400047NM 2005 7 14 2005UALA00632 120050703A3350582233 BATTERY BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29182UA 25279 AT RANDOM TIMES AFTER TAKEOFF & IN CRUISE THE EMERGENCY LIGHTS COME ON, U-D & STAIRS. REPLACED LOW BATTERY. 2L74 4F4 FRTA20WE E24NE 20050714000492005071400049NM 2005 7 14 2005UALA00634 120050705A3350582233 BATTERY BOEING747 747422 1384935NM PWA 4056 PW4056 NE SEAT 17AB DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29187UA 26877 EEL INOPERATIVE, SEAT 17AB. REPLACED LOW BATTERY. 2L74 4F4 FRTA20WE E24NE 20050714000522005071400052NM 2005 7 14 2005UALA00637 120050702A3350362624 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT BURNED OUT A UALAK NONE L NO TEST ININSP/MAINT 1 WP29194UA 26892 EEL INOP CROSS AISLE BETWEEN MID LAVS. REPLACED BURNED OUT EEL LIGHT, OK. 2L74 4F4 FRTA20WE E24NE 20050714000532005071400053NM 2005 7 14 2005UALA00638 120050702A3350209 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE DOOR 3 RT BURNED OUT A UALAK NONE L NO TEST ININSP/MAINT 1 WP29194UA 26892 EMERGENCY EXIT SIGN INOPERATIVE DOOR 3 RT AFT EXIT SIGN. REPLACED BURNED OUT LAMP. 2L74 4F4 FRTA20WE E24NE 20050714000542005071400054NM 2005 7 14 2005UALA00639 120050702A33501317 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE COCKPIT CEILING BURNED OUT A UALAK NONE L NO TEST ININSP/MAINT 1 WP29194UA 26892 EMERGENCY LIGHT INOPERATIVE COCKPIT CEILING. REPLACED BURNED OUT LAMP. 2L74 4F4 FRTA20WE E24NE 20050714000552005071400055NM 2005 7 14 2005UALA00640 120050706A2120 ODOR BOEING777 777222 1385219NM PWA PW4077PW4077 NE CABIN DETECTED A UALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP29213UA 30219 ELECTRICAL ODOR IN CABIN. THE FWD LAV FLUORESCENT LIGHT WAS ARCING CAUSING ELECTRICAL ODOR. THE CB WAS PULLED AND THE LAV INOP'D FOR REMAINDER OF FLIGHT UNTIL MECHANIC COULD EXAMINE LIGHT ON GROUND. MECHANIC RESET CIRCUIT BREAKER AND DETERMINED LIGHT TO BE OK FOR SERVICE. IF FLOURESCENT LIGHT TUBES ARE NOT INSTALLED PROPERLY IN LIGHT SOCKETS, ARCING CAN OCCUR. BOEING 777 MT 33-002 GIVES INSTRUCTIONS TO ENSURE THAT FLOURESCENT LIGHT TUBES ARE INSTALLED FIRMLY INTO RECEPTACLES TO PREVENT ARCING. 2L72 4F4 FRTT0001SE E46NE 20050714000702005071400070EA 2005 7 14 SWIA200515215 120050701A5610 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07405SW 7029 PILOT SIDE WINDOW CRACKED. REPLACED PILOT SIDE WINDOW IAW MM56-12-01, P/N NP-139322-5, S/N OFF 03105R1941. 2L72 4F RTA21EA 20050714000712005071400071SO 2005 7 14 SWIA200515218 120050619A3350 BULB EMB 120 EMB120ER 3260203SO EMERGENCY LIGHTSBURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07288SW 120316 ROW 10 FLOOR LEVEL EXIT ROW WHITE LIGHT OUT. REPLACED BULBS AT ROW 10 EMERGENCY LIGHTS. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050714000742005071400074SO 2005 7 14 MASA200500492 120050626A3350 CONNECTOR EMB 145 EMB145LR 3260212SO EXIT SIGN LIGHT LOOSE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07840MJ 145429 OVERHEAD EMERGENCY EXIT SIGN LIGHT AT CENTER AISLE INOP. MX RESECURED CONNECTOR. 2L72 4T RTT00011AT 20050714000762005071400076SO 2005 7 14 20030857 120050705A2121EVA2322C2 COOLING FAN EMB 120 EMB120ER 3260203SO AIR DISTRIBUTIONSMOKE A GLBAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM03108UX7377 120108 DURING TAXI, CREW DISCOVERED RT GROUND COOLING FAN CAUSING SMOKE. FAN PLACED ON MEL AND SCHEDULED FOR REPLACEMENT. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA31SO 20050714000772005071400077CE 2005 7 14 20030858 120050702A6120 PRESSURE SWITCH BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE RT PROP MALFUNCTIONED A GLBAO OTHER O OTHER APAPPROACH 1 NM03254GL UE254 ON APPROACH, CREW REPORTED RT ENGINE AUTOFEATHERED. MAINTENANCE CHECKED AND CLEANED PRESSURE SWITCHES AND PERFORMED OPERATIONAL CHECK OF AUTOFEATHER SYSTEM WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4T4 TRTA24CE E26NE 20050714000792005071400079NM 2005 7 14 QXEA200501085 120050701A7712312306401 TSCU DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE NR 2 ENGINE MALFUNCTIONED A QXEAA UNSCHED LANDING O OTHER CLCLIMB 1 NM09353PH8692 9 496 RETURNED TO FIELD. ON INITIAL CLIMB-OUT, NR 2 ENGINE TORQUE SURGED TO 101 PERCENT, THEN TO 126 PERCENT. NO NOTICEABLE YAW OF AIRCRAFT, ALL OTHER INDICATIONS NORMAL. REMOVED AND REPLACED FLIGHT DATA RECORDER (980-4700-001) FOR DATA INFORMATION AND TORQUE SIGNAL CONTROL UNIT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20050714000852005071400085NM 2005 7 14 UPS05444801 120050615A5315 FLOORBEAM BOEING747 747123 1384873NM AFT CARGO CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 AFT CARGO BAY BS 1800 BL 0 AND FLOORBEAM UPPER FLANGE CRACKED. CRACK LENGTH 2.5 IN. AFT CARGO BAY BS 1800 LBL 22 TO RBL 40 FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 2. 2L74 4F A20WE 20050714000862005071400086NM 2005 7 14 UPS05444802 120050617A531365B0765833 STRINGER BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 FX LT TUNNEL STR 41 AFT END CRACKED BETWEEN STA 260-280, CRACK LENGTH 0.75 IN. FX BS 260-280 STR 41L STRINGER REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050714000972005071400097NM 2005 7 14 QXEA200501090 120050705A2150 FILTER DHAV DHC8 DHC8202 2809007NM CABIN COOLING DIRTY A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 NM09346PH 477 WHEN BLEEDS TURNED ON AFTER TAKEOFF, ODOR LIKE DIRTY GYM SOCKS COMES OUT AND LASTS FOR 6 TO 10 MINUTES. THEN CLEARS UP. UPON INSPECTION, FOUND WATER DRAIN FILTER COMING OUT OF CONDENSER/MIXER PLUGGED. CLEANED FILTER AND REINSTALLED DRAIN LINE IAW DHC-8 -200 AMM 21-50-21, PAGE 404, STEP 3.A(7). PERFORMED FUNCTIONAL TEST OF BLEED AIR SYSTEM. ALL CHECKS GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050714000982005071400098NM 2005 7 14 QXEA200501092 120050701A243423088008 GENERATOR DHAV DHC8 DHC8202 2809007NM NR 2 INOPERATIVE A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09351PH993 993 490 NR 2 DC GENERATOR CAUTION ILLUMINATED. CYCLED ON AND OFF TWICE BEFORE RETURNING TO GATE. MAINTENANCE REMOVED AND REPLACED NR 2 DC GENERATOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050714001012005071400101NM 2005 7 14 QXEA200501091 120050702A33506038443 BATTERY DHAV DHC8 DHC8202 2809007NM ZONE 200 DISCHARGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09360PH1657216572 515 RT FORWARD EMERGENCY EXIT SIGN AND EXIT EGRESS LIGHTS OUT. REMOVED AND REPLACED POWER SUPPLY UNIT 3351 PS2 AND BATTERY PACK. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050714001022005071400102 2005 7 14 QXEA200501088 420050705A34257003110901 DISPLAY DHAV DHC8 DHC8202 2809007NM COCKPIT INOPERATIVE A QXEAO OTHER O OTHER UKUNKNOWN 1 NM09366PH150778846 510 RT SIDE ATTITUDE INDICTOR INOPERATIVE (WENT BLANK). ALL DATA TRANSFERRED TO LOWER CRT AS PER CHECKLIST. MAINTENANCE FOUND F/O ADI INOPERATIVE. REMOVED AND REPLACED ADI. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050714001042005071400104EA 2005 7 14 COMA0560372 120050630A3230750005000 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA MLG MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01999CA18499 7230 GEAR DISAGREE WARNING. REPLACED MLG SELECTOR VALVE. 2L72 4F RTA21EA 20050714001132005071400113EA 2005 7 14 COMA0560371 120050630A3222 STRUT CNDAIRCL600 CL6002B19 1900309EA NLG UNDERSERVICED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01712CA 7244 GEAR DISAGREE. SERVICED NLG SHOCK STRUT, GEAR SWINGS SATISFACTORY. 2L72 4F RTA21EA 20050714001142005071400114 2005 7 14 SWAA052025 420050711A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29715SW 27849 DURING SCHEDULED RON CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050714001152005071400115NM 2005 7 14 SWAA052038 120050711A53306545765 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29664WN 23495 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 28R. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050714001162005071400116NM 2005 7 14 SWAA052026 120050712A53206551698 SPLICE BOEING737 7373H4 1384600NM E / E BAY CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER SPLICE CORRODED AT BS 360, STR 27L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20050714001182005071400118 2005 7 14 YENA200537 420050702A31603907130402 DISPLAY AIRBUS320 A320232 3930326EU CABIN FAILED A YENAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 EA15554JB6570 6497 1898 BEFORE LANDING PILOTS SMELLED A BURNING ODOR IN FLT DECK. UPON LANDING TURNED OFF LIVE TV. ON GROUND PERFORMED TSM TASK 24-00-00-810-823, NO FAULT CONFIRMED. NO C/B TRIPPED OR OTHER EVIDENCE. AFTER RELEASED FOR FLT AIRCRAFT RETURNED TO GATE WITH ODOR IN COCKPIT. T/S PER TSM 24-00-00-810-823. REMOVED EACH DU, INSPECTED AND REINSTALLED DU'S, NO ABNORMALITIES NOTED. REMOVED BOTH MCDU'S, INSPECTED & REINSTALLED. NO ABNORMALITIES NOTED. OPERATED WEATHER RADAR, RAN BOTH ENGINES & PACKS AT FULL HOT THEN FULL COLD FOR 10 MINUTES, NO ABNORMALITIES. INSPECTED AVIONICS BAYS, TAXI AIRCRAFT FOR 25 MINUTES, COULD NOT DUPLICATE ANY ABNORMALITIES. REPLACED F/O'S DU'S AS PRECAUTIONARY. REMOVED DU P/N 3907130402. 2L72 4F RTA28NM 20050714001192005071400119CE 2005 7 14 CIEA200500009 120050705A2612302158 FIRE DETECTOR BEECH 200 200BEECH 1152920CE RT ENGINE FALSE ACTIVATIONE CIEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM035ST 10819 BB289 DURING THE AFTER CLIMBING THROUGH ABOUT 18,000 FEET, THE PILOT NOTICED A RED WARNING FLASHED BUT WENT BACK OFF BEFORE CAUSE WAS DETERMINED. A SHORT TIME LATER THE RIGHT ENGINE FIRE WARNING LIGHT CAME ON AND STAYED ON. THE PILOT COMPLIED WITH THE FIRE WARNING CHECKLIST AND DECIDED TO RETURN TO THE AIRPORT. THERE WAS NO EVIDENCE OF AN ACTUAL ENGINE FIRE. ALL ENGINE INDICATIONS WERE NORMAL. THE AIRCRAFT RETURNED TO THE AIRPORT WITHOUT INCIDENT AND LANDED. THE AIRCRAFT WAS BROUGHT INTO THE HANGAR FOR TROUBLESHOOTING AND REPAIR. IT WAS VERIFIED THAT THERE WAS NO FIRE IN THE ENGINE AREA. THE RIGHT ENGINE TOP DETECTOR WAS DETERMINED TO BE BAD. BY JUST TAPPING ON IT, IT WOULD GO BACK OFF. 1L72 4T A24CE 20050714001202005071400120CE 2005 7 14 DJFA2005119 120050701A3260 DOWNLOCK SWITCH BEECH MU300 400A 1155402CE MLG OUT OF ADJUST E DJFAO OTHER N FALSE WARNING APAPPROACH 1 EA23476LX RK376 KSMO - KCOS THE CREW REPORTED WHEN EXTENDING THE LANDING GEAR THE RIGHT MAIN GEAR GREEN INDICATION WAS NOT RECEIVED. THE GEAR WAS CYCLED AND THE CREW RECEIVED THE SAME INDICATION. A LIGHT TEST CONFIRMED THE LAMP WAS WORKING. THE CHECKLIST PROCEDURES WERE FOLLOWED AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ADJUSTED THE RIGHT DOWN AND LOCKED SWITCH. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4F RTA16SW 20050714001222005071400122EA 2005 7 14 COMA0560369 120050630A2150GG670950091 ACM CNDAIRCL600 CL6002C10 1390015EA CABIN COOLING MALFUNCTIONED A COMAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO01369CA 10079 SMOKE IN AFT LAV. REPLACED RT ACM. 2L72 4F RTA21EA 20050714001242005071400124EA 2005 7 14 COMA0560373 120050701A7931601509197 TRANSDUCER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT ENGINE MALFUNCTIONED A COMAO OTHER J WARNING INDICATION CRCRUISE 1 SO01498CA 7792 RT ENGINE OIL PRESSURE WARNING. REPLACED OIL PRESSURE TRANSDUCER. 2L72 4F4 FRTA21EA E15NE 20050714001252005071400125EA 2005 7 14 COMA0560374 120050702A2752854D10012 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01932CA 7038 FLAPS FAIL CAUTION. REPLACED RT FLAP OUTBD ACTUATOR. 2L72 4F RTA21EA 20050714001262005071400126EA 2005 7 14 COMA0560375 120050702A2130 CABIN PRESSURE CNDAIRCL600 CL6002B19 1900309EA CABIN MALFUNCTIONED A COMAA UNSCHED LANDING O OTHER CLCLIMB 1 SO01958CA 7111 AIRCRAFT CABIN NOT CLIMBING, DELTA P 4.2. CABIN PRESSURE SYSTEM OPS CHECK NORMAL. NO DEFECTS FOUND. 2L72 4F RTA21EA 20050714001272005071400127NM 2005 7 14 SWAA052013 120050711A3350MS155721 BULB BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED A1 CHECK, FOUND RT FWD CABIN EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050714001292005071400129NM 2005 7 14 SWAA052015 120050711A55536546874 FITTING BOEING737 7373H4 1384600NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED D-CHECK, FOUND LT & RT VERTICAL STAB FWD & AFT FAILSAFE CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER. 2L72 4F RTA16WE 20050714001312005071400131NM 2005 7 14 SWAA052017 120050711A53216546833 WEB BOEING737 7373H4 1384600NM COCKPIT FLOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED D-CHECK, FOUND 2 EA FUSELAGE FLOOR WEB CRACKS BETWEEN BS 188 TO BS 196, LT & RT SIDE, WL 208. REPAIRED FLOOR WEB PER SRM. 2L72 4F RTA16WE 20050714001332005071400133NM 2005 7 14 SWAA052019 120050706A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29408WN 27895 DURING SCHEDULED MV2 CHECK, FOUND EEPLS TRACK COVER BROKEN. REMOVED AND REPLACED COVER PER MM. 2L72 4F RTA16WE 20050714001342005071400134EU 2005 7 14 SWAA052020 220050711A73208063209 MEC BOEING737 7373H4 1384600NM CFMINTCFM56 CFM563C 13802EU NR 1 ENGINE FAULTY A SWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW29605SW 27956 AIR TURNBACK, NR 1 ENGINE HAD UNCOMMANDED ACCELERATION. REMOVED AND REPLACED NR 1 ENGINE MEC & PMC PER MM. 2L72 4F4 FRTA16WE E21EU 20050714001362005071400136NM 2005 7 14 SWAA052021 120050711A55516551524 FITTING BOEING737 7373H4 1384600NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29608SW 27928 DURING SCHEDULED D-CHECK, FOUND LT & RT HORIZONTAL STAB ATTACH FITTING LUG FACES CORRODED. REPAIRED LUG FACES PER SRM. 2L72 4F RTA16WE 20050714001372005071400137NM 2005 7 14 SWAA052022 120050711A53206545855 WEB BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29608SW 27928 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FLOOR WEB CORRODED AT BS 993 TO BS 1006, RBL 47, WL 208. REMOVED AND REPLACED WEB SECTION PER SRM. 2L72 4F RTA16WE 20050714001392005071400139NM 2005 7 14 ASAA0510096 120050518A53206545895 SPLICE BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE FUSLEAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 AFT CARGO PIT BS 907 BUTT SPLICE HAS CORROSION AT STR 27R. REMOVED AND REPLACED STRINGER SPLICE. (K) 2L72 4F4 F A16WE E2EA 20050714001402005071400140EA 2005 7 14 COMA0560367 120050629A2750 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ACTIVATED A COMAO OTHER JN WARNING INDICATION FALSE WARNING TXTAXI/GRND HDL 1 SO01917CA 7017 FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2L72 4F RTA21EA 20050714001412005071400141NM 2005 7 14 ASAA0510114 120050531A5314 KEELBEAM BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 KEELBEAM CORRODED AT B-STA 535, STR 28 RT. REPLACED KEELBEAM . (K) 2L72 4F4 F A16WE E2EA 20050714001432005071400143NM 2005 7 14 ASAA0510155 120050613A53306545866114 SKIN BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE FUSELAGE MISMANUFACTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 SKIN PANEL BETWEEN KEELBEAMS BSTA 727 TO S-STA 663 HAS LOW EDGE MARGIN AT FASTENER HOLES. REMOVED AND REPLACED PANEL IAW SRM. (K) 2L72 4F4 F A16WE E2EA 20050714001452005071400145NM 2005 7 14 ASAA05101109 120050530A53226546595139 SHEAR TIE BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 AFT CARGO PIT AND AFT SHEAR TIE HAS CORROSION AT B-STA 727A BETWEEN STR 27L AND 26L. SHEAR TIE REPLACED. (K) 2L72 4F4 F A16WE E2EA 20050714001462005071400146NM 2005 7 14 ASAA0510095 120050511A534065353524 STRINGER CLIP BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 AFT CARGO B-STA 907 CORRODED TIE CLIP AT STR 21L. REMOVED AND REPLACED TIE CLIP. (K) 2L72 4F4 F A16WE E2EA 20050714001472005071400147NM 2005 7 14 ASAA0510097 120050518A532269414551 SHEAR TIE BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 SKIN TO FRAME ATTACHMENT AT B-STA 614 BETWEEN LT AND RT BEAM DAMAGED. REMOVED AND REPLACED SKIN TO FRAME ATTACHMENT. (K) 2L72 4F4 F A16WE E2EA 20050714001482005071400148NM 2005 7 14 ASAA0510098 120050518A532269366935 SHEAR TIE BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 SKIN TO FRAME ATTACHMENT AT B-STA 572 BETWEEN LT AND RT BEAM DAMAGED. REMOVED AND REPLACED SKIN TO FRAME ATTACHMENT. (K) 2L72 4F4 F A16WE E2EA 20050714001522005071400152NM 2005 7 14 ASAA0590028 120050328A5320146A9403113 REVEAL BOEING737 737990 NM GE CFM56 CFM567B24 NE DOOR FRAME DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02307AS 30015 DURING C-CHECK, FOUND AFT CARGO DOOR FWD FRAME CUTOUT REVEAL DAMAGED. REPAIRED IAW SRM. (K) 2L74 4F4 FRTA16WE E00055EN 20050714001542005071400154NM 2005 7 14 ASAA0590027 120050328A5320143A7501165 FLOOR SUPPORT BOEING737 737990 NM GE CFM56 CFM567B24 NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02307AS 30015 DURING C-CHECK FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT AT BS 500. REPAIRED IAW SRM. (K) 2L74 4F4 FRTA16WE E00055EN 20050714001552005071400155NM 2005 7 14 ASAA0510105 120050530A53146545886502 KEELBEAM BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 KEELBEAM WEB B-STA 702 LT ONE HOLE BELOW MINIMUM EDGE MARGIN. REPLACED STRUCTURE, LOW EDGE MARGIN AREA CUTOUT AND REPAIR ANGLE INSTALLED. (K) 2L72 4F4 F A16WE E2EA 20050714001562005071400156NM 2005 7 14 ASAA0510106 120050527A532069412608 STIFFENER BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 CORROSION FOUND ON VERTICAL STIFFENER. VERTICAL STIFFENER REPLACED. (K) 2L72 4F4 F A16WE E2EA 20050714001582005071400158NM 2005 7 14 ASAA0510113 120050531A5340654868957 SUPPORT BRACKET BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 BS 670 AT LT KEELBEAM SUPPORT BRACKET CRACKED. REPLACED SUPPORT BRACKET. (K) 2L72 4F4 F A16WE E2EA 20050714001602005071400160EA 2005 7 14 COMA0560377 120050703A2421 IDG CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 1 UNDERSERVICED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01957CA 7109 NR 1 IDG CAUTION. SERVICED IDG OIL. OPERATION CHECKS SATISFACTORY. 2L72 4F4 FRTA21EA E15NE 20050714001632005071400163EA 2005 7 14 COMA0570079 120050705A5315CC670341757 FLOORBEAM CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01317CA7613 10055 TRANSVERSE BEAM AT FS 280 FROM LBL 36 TO RBL 36. CORRODED ALONG UPPER AND LOWER EDGES. REPLACED TRANSVERSE BEAM AT FS 280 IAW BOMBARDIER REO 670-53-11-047 REV C. 2L72 4F RTA21EA 20050714001642005071400164EA 2005 7 14 COMA0570080 120050705A3222521011 CYLINDER CNDAIRCL600 CL6002C10 1390015EA NLG CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01317CA7613 10055 NLG OUTER CYLINDER P/N 52101-1 S/N BA0025 CORRODED. CORROSION REPAIRED IAW BOMBARDIER REO 670-32-21-0060 AND GOODRICH SCR 0028-05. 2L72 4F RTA21EA 20050714001652005071400165NM 2005 7 14 ASAA0510107 120050530A5314654589611 KEELBEAM BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 KEELBEAM CORRODED B-STA 516 TO 535 STR 28L. REPAIRED WITH MADE REPAIR PART. (K) 2L72 4F4 F A16WE E2EA 20050714001662005071400166NM 2005 7 14 ASAA0510111 120050531A534069414551 SUPPORT ANGLE BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE FUSLEAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 CORROSION FOUND ON SUPPORT ANGLE AT BAST 622 BETWEEN LT AND RT KEELBEAMS. REPLACED SHEAR TIE. (K) 2L72 4F4 F A16WE E2EA 20050714001672005071400167EA 2005 7 14 COMA0570081 120050705A5522 SKIN CNDAIRCL600 CL6002C10 1390015EA ELEVATOR LIGHTNING STRIKEA COMAK NONE O OTHER ININSP/MAINT 1 SO01317CA7613 10055 LIGHTNING STRIKE EXIT DAMAGE ON LT ELEVATOR TRAILING EDGE. REPAIRED ELEVATOR UPPER SKIN TRAILING EDGE IAW BOMBARDIER EO 601R-55-6779. 2L72 4F RTA21EA 20050714001682005071400168EA 2005 7 14 COMA0560379 120050704A2700 FLT CONTROLS CNDAIRCL600 CL6002B19 1900309EA COCKPIT VIBRATION A COMAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 SO01716CA 7250 MODERATE VIBRATION IN CONTROLS AT SPEED GREATER THAN 260. INSPECTED FUSELAGE, VERTICAL STAB FAIRINGS AND FLIGHT CONTROLS. NO DEFECTS NOTED. 2L72 4F RTA21EA 20050714001722005071400172NM 2005 7 14 ASAA0510128 120050607A534066232546 ATTACH ANGLE BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE FUSLEAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 AFT CARGO PIT B-STA 727B FRAME TO KEELBEAM (STA 27L) ATTACH ANGLE HAS CORROSION. REPLACED ATTACH ANGLE. (K) 2L72 4F4 F A16WE E2EA 20050714001752005071400175NM 2005 7 14 ASAA0510179 120050614A5322654655116 SHEAR TIE BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 AFT CARGO PIT B-STA 807 IB OF STRINGER 27L FRAME TO SKIN SHEAR TIE AFT FACE CORROSION FOUND AS MARKED. REMOVED AND REPLACED SHEAR TIE IAW SRM. (K) 2L72 4F4 F A16WE E2EA 20050714001762005071400176NM 2005 7 14 ASAA0510181 120050614A53406941885503 BRACKET BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 A BRACKET AT B-STA 847, STRINGER 18R FOUND CORROED. BRACKET REPLACED WITH THE REPAIR PART AT BSTA 847 STRINGER 18R IAW SRM. (K) 2L72 4F4 F A16WE E2EA 20050714001772005071400177NM 2005 7 14 ASAA0510116 120050531A534069353525 STRINGER CLIP BOEING737 737290C 138448VNM AFT CARGO CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 AFT CARGO B-STA 907, STR 20L, TIE CLIP CORRODED. TIE CLIP REPLACED. (K) 2L72 4F A16WE 20050714001792005071400179NM 2005 7 14 ASAA0510138 120050613A531465621251 KEELBEAM BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 KEELBEAM, BS 647-663 LT LWR CHORD CORROSION FOUND UPPER AND LOWER FACE. LT KEELBEAM REPLACED IAW SRM. (K) 2L72 4F4 F A16WE E2EA 20050714001802005071400180NM 2005 7 14 ASAA0510141 120050613A5313655162816 STRINGER BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 STRINGER CORRODED AT BS 967-986. REMOVED AND REPLACED STRINGER IAW SRM. (K) 2L72 4F4 F A16WE E2EA 20050714001812005071400181NM 2005 7 14 ASAA0510154 120050613A531365457769 STRINGER BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 CRACKED STRINGER AT B-STA 789, STRINGER 26R. REMOVED AND REPLACED STRINGER IAW SRM. (K) 2L72 4F4 F A16WE E2EA 20050714001822005071400182NM 2005 7 14 ASAA0510176 120050614A532069412608 STIFFENER BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 CORROSION FOUND ON VERTICAL STIFFENER LOCATED AT BS 328, RBL 14, WL 150, IN E AND E BAY. REMOVED AND REPLACED VERTICAL STIFFENER IAW SRM. (K) 2L72 4F4 F A16WE E2EA 20050714001832005071400183NM 2005 7 14 ASAA0510143 120050613A5311656955059 FRAME BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE FUSELAGE SCRATCHED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 AFT CARGO PIT BS 787, RBL 8 HAS SCRATCHED FRAME. FOUND BEYOND LIMITS AND REPAIRED IAW SRM. (K) 2L72 4F4 F A16WE E2EA 20050714001852005071400185NM 2005 7 14 ASAA0510174 120050614A534069353521 STRINGER CLIP BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 AFT CRGO B-STA 747, STR 22L TIE CLIP CORRODED. REMOVED AND REPLACED TIE CLIP IAW SRM. (K) 2L72 4F4 F A16WE E2EA 20050714001882005071400188NM 2005 7 14 ASAA0510180 120050614A532069421751 SPLICE BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM02742AS 23136 FRAME SPLICE AT BSTA 847, STRINGER 27R FOUND CORRODED. FRAME SPLICE AT BSTA 847, STRINGER 27R REPLACED WITH MADE REPAIR PART IAW SRM. (K) 2L72 4F4 F A16WE E2EA 20050714001892005071400189NM 2005 7 14 ASAA0510110 120050530A53406937460502 SUPPORT ANGLE BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE BSTA630 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 SUPPORT ANGLE CORRODED AT BSTA 630 BETWEEN LT AND RT KEELBEAMS. REPLACED SUPPORT ANGLE. (K) 2L72 4F4 F A16WE E2EA 20050714001902005071400190NM 2005 7 14 ASAA0510112 120050531A5340654653412 SUPPORT ANGLE BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 SUPPORT ANGLE CORRODED AT B-STA 520 RT KEELBEAM. REPLACED SUPPORT ANGLE. (K) 2L72 4F4 F A16WE E2EA 20050714001922005071400192EA 2005 7 14 QXEA200501094 120050706A496021195843 ECU CNDAIRCL600 CL6002C10 1390015EA APU MALFUNCTIONED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09602QX2860 2860 10010 RETURNTED TO GATE. APU ENGINE CONTROL UNIT CAUTION MESSAGE. MAINTENANCE REMOVED AND REPLACED APU ENGINE CONTROL UNIT. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20050714001932005071400193NM 2005 7 14 SWAA052027 120050711A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E + 15, STR 18L. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050714001952005071400195NM 2005 7 14 QXEA200501093 120050705A7720305829301 PROBE DHAV DHC8 DHC8202 2809007NM NR 1 ITT INOPERATIVE A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09369PH 513 RETURNED TO GATE, NR 1 ITT INDICATION FLUCTUATES ERRATICALLY. OTHER INDICATIONS, INCLUDING FUEL FLOW ARE STABLE. MAINTENANCE REMOVED AND REPLACED ITT PROBE AT SEVEN O'CLOCK POSITION. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050714001962005071400196 2005 7 14 PCSA7060501 420050704A3417HG480B100 ADC BOEING727 727212 138407GNM COCKPIT FALSE INDICATIONA PCSACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 SO29598AJ 21947 ON TAKEOFF ROLL, CAPT AIRSPEED INDICATOR WENT TO 300 KNOTS AT AROUND 60 KNOTS INDICATED. CREW ABORTED TAKEOFF AND RETURNED TO BLOCKS. NO FURTHER INCIDENT REPORTED. MAINTENANCE INSPECTED AIRSPEED INDICATION AND FOUND SYSTEM ENCOUNTERED A GLICK FROM NR 1 AIR DATA COMPUTER. CIRCUIT BREAKER RESET PERFORMED OPERATIONAL CHECK OF SYSTEM. NO DEFECTS NOTED. WORK ACCOMPLISHED IAW BOEING 727 MM CH 34-12-00. AIRCRAFT WAS RETURNED TO SERVICE. 2L73 4F A3WE 20050714001972005071400197NE 2005 7 14 HNAA0500063 220050706A72613022383 GARLOCK SEAL DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE NR 2 ENGINE LEAKING A HNAAA UNSCHED LANDING K FLUID LOSS CRCRUISE 1 EA07942HA4250342503 163 NR 2 ENGINE OIL PRESSURE FLUCTUATED IN FLIGHT STAYED BETWEEN 40-55 PSI OVER 3 MINUTES. REMOVED AND REPLACED HYDRAULIC PUMP GARLOCK SEAL. 2H72 4T4 TRTA13NM E20NE 20050714001982005071400198SO 2005 7 14 C2XA05IA085 120050704A3230 LANDING GEAR EMB 145 EMB145LR 3260212SO MALFUNCTIONED A C2XAAD UNSCHED LANDING RETURN TO BLOCK J WARNING INDICATION CLCLIMB 1 SW2713994 145291 CREW REPORTED LANDING GEAR DID NOT RETRACT. LANDING GEAR SELECTOR DID NOT MOVE TO UP POSITION AND MANUAL OVER RIDE WAS NOT USED. DURING THIS TIME, LANDING GEAR AIR/GROUND FAIL MESSAGE DISPLAYED AND AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. INSPECTION OF LANDING GEAR WAS PERFORMED AND AIRCRAFT FERRIED WHERE MAINTENANCE PERFORMED SEVERAL OPERATIONAL CHECKS. NO DEFECTS NOTED DURING OPERATIONAL CHECKS AND AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20050714001992005071400199SO 2005 7 14 C2XA05SH067 120050708A532014521713005 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712900 145511 CORROSION ON CENTER OMEGA BEAM AT FS 20. MAINTENANCE REMOVED AND REPLACED CENTER OMEGA BEAM AT FS 18-23 IAW EMB 145 SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050714002032005071400203EA 2005 7 14 SWIA200515222 120050703A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSBURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07934SW 7722 EMERGENCY OVERHEAD POD LIGHT INOP BY ROW 12. RELAMPED OVERHEAD EMERGENCY LIGHT. OPERATIONAL CHECK OK. 2L72 4F RTA21EA 20050714002072005071400207EA 2005 7 14 SWIA200515226 120050630A2750860D10018ABCD CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 NM07407SW 7034 DURING APPROACH RECEIVED FLAPS HALFSPEED STATUS MSG WITH FLAPS SELECTED. REPLACED FLAP ELECTRONIC CONTROL UNIT IAW 27-51-05. OPERATIONAL CHECK GOOD, SN OFF 753. 2L72 4F RTA21EA 20050714002082005071400208SO 2005 7 14 SWIA200515227 120050625A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO EMERGENCY LIGHTSDISCHARGED A SWIAO OTHER J WARNING INDICATION CRCRUISE 1 NM07189SW 120048 EMERGENCY LIGHT NOT ARMED ILLUM INFLIGHT/CB POPPED, WOULD NOT RESET. REPLACED ALL 3 ELBPS PER MM 33-50-02 AND REPAIRED CHAFED WIRE PER SP MM 20-00-00. OPERATIONAL CHECK GOOD, PN D366-04-001 OFF 140, 984, AND 1260. 2L72 4T RTA31SO 20050714002092005071400209SO 2005 7 14 SWIA200515228 120050701A3350 RELAY EMB 120 EMB120ER 3260203SO EMERGENCY LIGHTSDEFECTIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07582SW 120350 EMERGENCY LIGHTS WILL NOT EXTINGUISH WHEN POWER REMOVED FROM AIRCRAFT. REPLACED RELAY IAW WM 20-00-02. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050714002112005071400211SO 2005 7 14 SWIA200515230 120050702A3397 GROUND WIRE EMB 120 EMB120ER 3260203SO EXIT SIGN LOOSE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07233SW 120307 EMERGENCY EXIT SIGN OVER ROW 9 IS INTERMITTENT. SECURED LOOSE GROUND WIRE AT ROW 9 EXIT SIGN. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050714002132005071400213EA 2005 7 14 SWIA200515232 120050628A274284897 ACTUATOR CNDAIRCL600 CL6002C10 1390015EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION DEDESCENT 1 NM07748SK510 510 10203 ON DESCENT, GOT STAB TRIM CHANNEL 1 INOP STATUS MESSAGE. REPLACED HORIZONTAL STAB TRIM CONTROL ACTUATOR IAW AMM 27-42-01. OPERATIONAL CHECK IAW AMM 27-40-00. 2L72 4F RTA21EA 20050714002152005071400215EA 2005 7 14 SWIA200515234 120050630A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EXTERIOR BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07906SW 7510 EXTERIOR EMERGENCY LIGHT, 2ND FROM FRONT RT SIDE, FAILS TO ILLUMINATE. REPLACED EMERGENCY LIGHT BULB (2ND FROM FRONT ON RT SIDE). OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050714002192005071400219EA 2005 7 14 SWIA200515238 120050707A2740 SWITCH CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07975SW 7951 STAB CH1 INOP AND WON'T RESET. REPLACED STAB CH1 PUSH SWITCH. OPERATIONAL CHECK IAW 27-41-00 GOOD. 2L72 4F RTA21EA 20050714002202005071400220EA 2005 7 14 SWIA200515239 120050704A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 NM07407SW2824 2824 7034 FLAPS FAIL MSG CAME ON DURING CLIMB-OUT WHEN SELECTED FROM 20 TO 8 DEG. REPLACED LT BPSU IAW CRJ MM 27-51-10. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050714002222005071400222EA 2005 7 14 SWIA200515241 120050705A274070609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TOTAKEOFF 1 NM07915SW2272 2272 7615 ON T/O STAB TRIM HAD MOVED SMALL AMOUNT FROM WHERE IT WAS SET. INSTALLED SERVICEABLE HSTCU IAW CRJ MM 27-41-01 AND REPLACED F/O AND CAPT TRIM SWITCHS IAW MM 27-41-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050714002232005071400223EA 2005 7 14 MASA200500288 120050406A2910 HYDRAULIC LINE CNDAIRCL600 CL6002B19 1900309EA NR 1 HYD SYS BROKEN A MASAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 SW0777195 7195 CAPT RETURNED TO FIELD FOR HYDRAULIC SYSTEM NR 1 QUANTITY DROPPED TO 0 PERCENT. MAINTENANCE FOUND HYDRAULIC LINE BROKEN AND REPLACED IT. 2L72 4F RTA21EA 20050712002242005071200224NM 2005 7 12 AWXA200500767 120050608A53206546812 FLOOR SUPPORT BOEING737 7373B7 1384580NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28328AW 23377 DURING C-13 CHECK DISCOVERED CORROSION ON FLOOR SUPPORT JUST FORWARD OF BS 967, BL 18L, WL 204. MAINTENANCE BLENDED OUT CORROSION JUST FORWARD OF BS 967, BL 18L, WL 204 AND FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-51. REMOVED FLOOR SUPPORT JUST FORWARD OF BS 967, BL 18L, WL 204 IAW BOEING 737-300 SRM 51-70-04-0 FIG 1. PREPARED REPLACEMENT FLOOR SUPPORT FOR INSTALLATION IAW BOEING 737-300 SRM 51-40-05-0 FIG 6. INSTALLED REPLACEMENT FLOOR SUPPORT JUST FORWARD OF BS 967, BL 18L, WL 204 IAW BOEING 737-300 SRM 51-70-04-0 FIG 1. 2L72 4F RTA16WE 20050712002262005071200226NM 2005 7 12 CALA0500208 120050701A3260 CIRCUIT BREAKER BOEING737 737524 1384721NM LG INTERMITTENT A CALAO OTHER JN WARNING INDICATION FALSE WARNING TOTAKEOFF 1 SW2733637 27540 WHEN LANDING GEAR RETRACTED AFTER TAKEOFF, CONFIGURATION WARNING HORN SOUNDED AND GEAR HANDLE WOULD NOT MOVE ABOVE OFF. QRH PROCEDURES WERE FOLLOWED AND FLIGHT PROCEEDED NORMALLY WITH NO FURTHER PROBLEMS. MAINTENANCE FOUND LANDING GEAR LEVER LATCH AND PRESSURE WARNING CIRCUIT BREAKER INTERMITTENT. CIRCUIT BREAKER WAS REMOVED AND REPLACED. A LANDING WARNING SYSTEM TEST AND LOCK SOLENOID INSTALL TEST WERE PERFORMED IAW MM 31-26-00-725-040 AND MM 32-31-31 AND BOTH TESTS PASSED. 2L72 4F RTA16WE 20050712002302005071200230EA 2005 7 12 SWIA200515203 120050629A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAD RETURN TO BLOCK F FLT CONT AFFECTED TOTAKEOFF 1 NM07588SW 7069 AFTER T/O RECEIVED A FLAPS FAIL CAUTION MESSAGE. REPLACED RT BPSU IAW CRJ MM 27-51-10. 2L72 4F RTA21EA 20050713000502005071300050EA 2005 7 13 SWIA200515210 120050321A5340 SUPPORT FITTING CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07915SW 7615 SUPPORT FITTING CRACKED AT FS 460, RBL 9, OUTBOARD SIDE, ITEM FOUND AT C-CHECK INSPECTION. REPLACED SUPPORT FITTING IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, 51-21-11, 51-41-02. 2L72 4F RTA21EA 20050713000552005071300055NM 2005 7 13 AWXA200500770 120050629A2560P2070001214 FLASHLIGHT BOEING737 7373S3 1384711NM AFT CABIN INOPERATIVE A AWXAO OTHER L NO TEST TXTAXI/GRND HDL 1 WP28314AW 23733 DURING GROUND HANDLING FLIGHT ATTENDANT REPORTED AFT OUTBOARD CABIN EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED OUTBOARD AFT FLIGHT ATTENDANT FLASHLIGHT. OPERATIONAL CHECKS GOOD. 2L72 4F RTA16WE 20050713000692005071300069SO 2005 7 13 MASA200500473 120050617A3350 LIGHT EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSINOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07853MJ 145464 FIRST FLOOR EMERGENCY FLOOR LIGHT STRIPS INOP. MX OPS CHECKED LIGHTS BUT COULD NOT DUPLICATE PROBLEM. 2L72 4T RTT00011AT 20050713000722005071300072SO 2005 7 13 MASA200500481 120050623A3350744424 LIGHT EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSINOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07853MJ 145464 DURING WALK AROUND, DISCOVERED ROW 12 EMERGENCY EXIT SIGN LIGHT NOT ILLUMINATING. REPLACED LIGHT ASSY AFTER TROUBLESHOOTING. OPERATIONAL CHECK GOOD. 2L72 4T RTT00011AT 20050713000822005071300082NM 2005 7 13 2005UALA00603 120050627A339758781 CABLE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE EMERGENCY LIGHTSDAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29309UA 23670 EMERGENCY EEL LIGHTS INOP FROM ROW 17 AFT TO AND INCLUDING EEL STRIP IN FRONT OF AFT GALLEY CART STOWAGE COMPARTMENT. SUPPLEMENTAL DATA UPDATE EEL CABLE WAS DAMAGED, REPLACED CABLE. 2L72 4F4 FRTA16WE E2GL 20050713000952005071300095NM 2005 7 13 UPS05444780 120050629A5312 PRESSURE PANEL BOEING747 747121 1384871NM NLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 LT NWW SIDE PANEL FOUND CRACK AT BTN BS 260 AND 280 WL 150, CRACK LENGTH 1 INCH. REPAIRED AS PER SRM 53-10-04 FIG 116. 2L74 4F A20WE 20050713000982005071300098NM 2005 7 13 UPS05444783 120050621A5347 SEAT TRACK BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 BS 540-580 LBL 27, SEAT TRACK CORRODED. CORROSION BLEND OUT 0.051 BY .375 BY 4 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A. 2L74 4F A20WE 20050713000992005071300099NM 2005 7 13 UPS05444784 120050622A5320 WEB BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 AFT CARGO LT BS 1900 STR 43L FRAME WEB STRINGER CUTOUT SUSPECTED CRACKED. CRACK LENGTH 0.5 IN. FRAME WEB REPAIRED AS PER SRM 53-10-04 FIG 42. 2L74 4F A20WE 20050713001002005071300100NM 2005 7 13 UPS05444785 120050622A5322 SHEAR TIE BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 AFT CARGO STA 1640 RBL 28 FRAME LWR SHEAR TIE RIVET HOLE EDGE FOUND CRACK. SHEAR TIE REPAIRED AS PER SRM 53-10-04 FIG 3. 2L74 4F A20WE 20050713001012005071300101NM 2005 7 13 UPS05444786 120050621A5320 WEB BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 RT BS 340 U/D FLR BEAM TO FRAME FUNCTION AREA FOUND 1EA HOLE CRACK AT FLOORBEAM WEB THRU THICKNESS RUNNING I/B, CRACK LENGTH 0.125 IN. FLOORBEAM WEB REPAIRED AS PER SRM 53-10-07 FIG 11. 2L74 4F A20WE 20050713001022005071300102NM 2005 7 13 UPS05444787 120050618A5347 SEAT TRACK BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 STA 518-523 LBL 47 INCH SEAT TRACK CORROSION. CORROSION BLEND OUT 0.033 BY 0.5 BY 1.75 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A. 2L74 4F A20WE 20050713001112005071300111WP 2005 7 13 UPS05844750 120050518A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CHAFED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE:C-3. D PIT DOOR CUTOUT AFT SIDE CHAFED AND FASTENER HAS SHORT E.D. AT STA 1440. REMOVED FASTENER AND CUT OUT DAMAGED AREA AND INSTALLED DOUBLER, TRIP AND 2 FILLERS IAW EO DC8 5330-22423-A AND SAASK 840-807058. 2L74 4F RT4A25 20050713001142005071300114WP 2005 7 13 UPS05844758 120050603A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE GOUGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE:C-3. RT FS 70 L31R AND L32R, DEEP GOUGES ON EXTERIOR SKIN. REMOVED DAMAGED SKIN SECTION. FABRICATED AND INSTALLED REPAIR DOUBLER, TRIPLER AND FILLER IAW EO DC8-53-20473 AND SAA SK840-808375. 2L74 4F RT4A25 20050713001172005071300117WP 2005 7 13 UPS05844762 120050605A5511 RIB DOUG DC8 DC871F 302199DWP HORIZONTAL STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01705UP 45949 LT HORIZ STAB L/E 2ND INBD LWR RIB REPAIR HAS DOUBLER AND TRIPLER CRACKED. REMOVED, FABRICATED, AND INSTALLED REPAIR DOUBLER AND TRIPLER IAW SRM 55-2-0, 51-1-21, AND SRM 55-2-0 FIG 2. 2L74 4F RT4A25 20050713001282005071300128NM 2005 7 13 QXEA200501087 120050703A2932 CIRCUIT BREAKER BOMBDRDHC8 DHC8402 1390042NM NR 3 HYD POPPED A QXEAD RETURN TO BLOCK J WARNING INDICATION UKUNKNOWN 1 NM09411QX 4055 NR 3 HYDRAULIC PUMP CAUTION LIGHT ILLUMINATED AFTER ENGINE START. NR 3 HYDRAULIC PRESSURE GAUGE INDICATED ZERO DURING NR 3 ISOLATION CHECK ON AFTER START FLOW. FOUND DCMP CIRCUIT BREAKER CB55 POPPED. RESET BREAKER. NO PARTS REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050713001302005071300130EA 2005 7 13 MASA200500470 120050616A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSBURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0777331 7331 LT INTERIOR OVERWING EMERGENCY EXIT SIGN HAD 1 BULB INOP. OPS CHECKED GOOD. 2L72 4F RTA21EA 20050714000172005071400017EA 2005 7 14 VNAA0506013 120050622A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE DENTED A VNAAK NONE O OTHER ININSP/MAINT 1 GL05250PS 7929 THE CREW REPORTED TWO DENTS ON THE AFT FUSELAGE BELOW THE CARGO DOOR. THE AIRCRAFT WAS FERRIED TO CKB WHERE BOMBARDIER REPAIRED AND INSPECTED THE DAMAGE IAW BOMBARDIER REGIONAL AIRCRAFT SERVICES ENGINEERING ORDER 601R-53-6747. REF AML 4282.27 AND BOMBARDIER REO 601R-53-61-1423. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050714000272005071400027NE 2005 7 14 2005UALA00612 220050704A7200PW40603 ENGINE BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE NR 1 SURGES A UALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 WP29661UA4323711722 27158 724694 RETURNED TO IAD DUE TO NR 1 ENGINE COMPRESSOR STALL. SURGE ON POWER REDUCTION AT 5500 MSL. EPR = 1.128. TWO ADDITIONAL SURGES AT EPR < 1.128. NOT GROUP-3 SURGE. TEST-21 NOT REQUIRED. IAD HPC BSI: OK. IAD REPLACED: 2.9 BLEED SOLENOID & RELAY, HP BLEED CONTROLLER, AND INTERMEDIATE CHECK VALVE. ENGINE CONTINUED TO SURGE ON GROUND RUNS DURING DECEL. ALL SURGES AT < 1.25 EPR. ENGINE REPLACED AT IAD ON 7/9/05. CURRENTLY EN ROUTE TO SFO FOR TEARDOWN. 2L72 4F4 FRTA1NM E24NE 20050714000302005071400030NM 2005 7 14 2005UALA00616 120050705A335020131A BATTERY PACK BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU ROW 17 DISCHARGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29330UA 24191 EEL LIGHT INOP FROM ROW 17ABC THROUGH AFT GALLEY. LOW BATTERY REPLACED, OK. 2L72 4F4 FRTA16WE E21EU 20050714000322005071400032EU 2005 7 14 2005UALA00618 120050706A3350321454 BATTERY AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE EMERGENCY LIGHT DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29431UA 571 NUMEROUS FLOOR PROX EEL LIGHTS INOP THROUGHOUT CABIN. BPOWER SUPPLIES LOW CHARGE. REPLACED MID AND AFT PWR SUPPLIES. 2L72 4F4 FRTA28NM E40NE 20050714000452005071400045NM 2005 7 14 2005UALA00630 120050704A3350362624 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE ROW 44 LT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29116UA 26908 EEL INOPERATIVE ROW 44 LT. EEL LAMP INOP. REPLACED EEL LAMP, OK. 2L74 4F4 FRTA20WE E24NE 20050714000732005071400073EA 2005 7 14 MASA200500491 120050626A3350 LENS CNDAIRCL600 CL6002D24 1390016EA EMGCY EXIT SIGN MISSING A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07916FJ 15016 RED LIGHT LENS COVER ON EMERGENCY EXIT SIGN IS MISSING. MX REPLACED THE LENS COVER. 2L72 4F RTA21EA 20050714000832005071400083NM 2005 7 14 UPS05444799 120050618A5347 SEAT TRACK BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 BS 800 TO 840 LBL 11 SEAT TRACK NECK FOUND CORRODED. CORROSION BLEND OUT 0.052 BY 1.0 BY 2.0 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 14 AT BS 723 TO BS 857 LBL 11 AREA. 2L74 4F A20WE 20050714000842005071400084NM 2005 7 14 UPS05444800 120050618A5347 SEAT TRACK BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 STA 783 LBL 11 SEAT TRACK RT FLANGE CORROSION. CORROSION BLEND OUT 0.019 BY 0.75 BY 1.5 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 14 AT BS 723- BS 857 LBL 11 AREA WORK DETAIL REF NRC NR 6006. 2L74 4F A20WE 20050714001232005071400123EA 2005 7 14 COMAO570077 120050630A2150GG670950091 ACM CNDAIRCL600 CL6002C10 1390015EA CABIN COOLING SMOKE A COMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO01369CA 10079 SMOKE IN CABIN. REPLACED RT ACM. 2L72 4F RTA21EA 20050714001302005071400130NM 2005 7 14 SWAA052016 120050711A53116545815 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME INNER CHORD CRACKED AT BS 348, LBL 50, WL 208. REPAIRED FRAME INNER CHORD PER SRM. 2L72 4F RTA16WE 20050714001352005071400135EA 2005 7 14 COMA0560376 120050702A5210601R386493 PUSHROD CNDAIRCL600 CL6002B19 1900309EA CABIN DOOR BROKEN A COMAA UNSCHED LANDING O OTHER CLCLIMB 1 SO01779CA 7306 AIRCRAFT WOULD NOT PRESSURIZE. REPLACED THE CABIN DOOR PUSH ROD ASSEMBLY. 2L72 4F RTA21EA 20050714001502005071400150NM 2005 7 14 ASAA0510102 120050526A5310655298849 STRUCTURE BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE AFT CARGO AREA CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 AFT CARGO AREA B-STA 940 TO 947, STA 22L CORRODED. CORRODED STR 22L AT B-STA 947 REPLACED WITH FABRICATED REPAIR PART. (K) 2L72 4F4 F A16WE E2EA 20050714001592005071400159NM 2005 7 14 ASAA0510182 120050614A5720655077373 WEB BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE LT WING DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 DENT ON WEB ON LT WING RSS 497 APPROX 10 INCHES AFT OF REAR SPAR. REPAIRED IAW SRM. (K) 2L72 4F4 F A16WE E2EA 20050714001702005071400170EA 2005 7 14 COMA0560381 120050705A3260864808 PSEU CNDAIRCL600 CL6002B19 1900309EA LG MALFUNCTIONED A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01991CA208588315 7216 GEAR DISAGREE WARNING DURING TAXI. REPLACED PSEU FOR TROUBLESHOOTING. 2L72 4F RTA21EA 20050714001782005071400178NM 2005 7 14 ASAA0510118 120050607A531465621252 KEELBEAM BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 CORROSION ON RT KEELBEAM AT B-STA 618. REPLACED KEELBEAM. (K) 2L72 4F4 F A16WE E2EA 20050714001862005071400186NM 2005 7 14 ASAA0510177 120050614A532065495648 SPLICE BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 CORROSION ON STRINGER 26L END SPLICE AT BS 540. REMOVED AND REPLACED END SPLICE IAW SRM. (K) 2L72 4F4 F A16WE E2EA 20050714001942005071400194NM 2005 7 14 QXEA200501096 120050706A2750C1486742003 CONTROL UNIT BOMBDRDHC8 DHC8402 1390042NM TE FLAPS MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09404QX9064 9064 4046 FLAP POWER CAUTION IN FLIGHT. RAN CHECKLIST. CAUTION STILL ILLUMINATED. GPWS CAUTION ALSO ILLUMINATED 15 MINUTES LATER WHILE CHANGING TO LOWER ALTITUDE. REPLACED FLAP CONTROL UNIT. OPERATIONAL CHECK GOOD. NO FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050714002022005071400202EA 2005 7 14 SWIA200515221 120050704A3350 BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSDISCHARGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07980SW 7955 OVERHEAD EMERGENCY EXIT LIGHT AT OVERWING EXITS NOT ILLUMINATED. REPLACED NR 3 EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD IAW 33-51-00. 2L72 4F RTA21EA 20050714002102005071400210EA 2005 7 14 SWIA200515229 120050704A5610 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAO OTHER O OTHER CRCRUISE 1 NM07463SW 7820 CAPT SIDE WINDSHIELD CRACKED IN FLIGHT. REPLACED CAPT SIDE WINDSHIELD IAW MM 56-00-00 AND 56-11-01, PN NR-139321-5; SN OFF 03081H9374. 2L72 4F RTA21EA 20050714002122005071400212SO 2005 7 14 SWIA200515231 120050702A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO EMERGENCY LIGHTSDISCHARGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07197SW8952 8952 120186 EMERGENCY LIGHTS TOWARD FRONT OF CABIN INOP. REPLACED FORWARD ELBP. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050714002142005071400214EA 2005 7 14 SWIA200515233 120050701A2780 SENSOR CNDAIRCL600 CL6002C10 1390015EA SLATS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07707SK 10003 SLAT FAULT STATUS MSG IN FLIGHT. REPLACED RT IB SLAT DISCONNECT SENSOR IAW CRJ 700 AMM 27-81-39, OPERATIONAL CHECK GOOD, P/N OFF 771410C S/N OFF M794. 2L72 4F RTA21EA 20050714002172005071400217EA 2005 7 14 SWIA200515236 120050703A335020131A BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSDISCHARGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07426SW107948178 7468 EMERGENCY LIGHTS ON GALLEY SERVICE DOOR OUT. REPLACED FORWARD EMERGENCY BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050714002242005071400224EA 2005 7 14 MASA200500409 120050526A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0737178 7178 CREW REPORTED PASSENGER DOOR WILL NOT OPEN (REPEAT). AIRCRAFT FERRIED AND MAINTENANCE RE-RIGGED DOOR. 2L72 4F RTA21EA 20050714002252005071400225EA 2005 7 14 MASA200500437 120050604A2610 LOOP CNDAIRCL600 CL6002B19 1900309EA FIRE PROTECTION FAILED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0717175 7175 LT JET LOOP B FAILED. MAINTENANCE REMOVED AND REPLACED LOOP. 2L72 4F RTA21EA 20050714002262005071400226EA 2005 7 14 MASA200500474 120050618A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA CABIN MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07571ML 7209 PAX DOOR WOULD NOT OPEN PROPERLY. DOOR NOW OPENS NORMAL. OPS CHECK GOOD. 2L72 4F RTA21EA 20050715000022005071500002NM 2005 7 15 RYAN200500018 120050612A793356B94 BULB BOEING737 737201 1384454NM PWA JT8 JT8D9 52048NE ENG OIL TEMP FAULTY A RYNAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE07240AU 22355 655811 DURING CLIMB, ENGINE NR 1 HAD HIGH OIL PRESSURE AND SHORTLY THEREAFTER NR 1 OIL TEMPERATURE STARTED CLIMBING TOWARDS REDLINE. ON RETURN, NR 1 ENGINE SHUTDOWN. 2L72 4F4 F A16WE E2EA 20050715000032005071500003NM 2005 7 15 ASAA0510183 120050614A5330654576989 SKIN BOEING737 737290C 138448VNM PWA JT8 JT8D11 52044NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 FUSELAGE SKIN BULGE AT B-STRA 535, STR 28, LT. REPAIRED IAW SRM. (K) 2L72 4F4 F A16WE E2EA 20050715000042005071500004NM 2005 7 15 ASAA0510185 120050614A5313654655216 STRINGER BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 OB SIDE OF STR 26L AT B-STA 986 CORRODED. REMOVED AND REPLACED STRINGER 26L IAW SRM. (K) 2L72 4F4 F A16WE E2EA 20050715000082005071500008NM 2005 7 15 2005UALA00606 120050628A3297 WIRE BOEING757 757222 1384956NM PWA 2037 PW2037 NE MLG DAMAGED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29522UA 24931 RETURNED TO FIELD DUE TO AIR/GROUND SENSOR FAILURE, MANUAL GEAR RETRACTION. FOUND TRIPPED SYS 2 AIR GROUND CB AND CHAFED WIRE IN P37 PANEL (W1270-5852-22).REPLACED CIRCUIT BREAKER AND ACCOMPLISHED REPAIR OF DAMAGED WIRE. 2L72 4F4 FRTA2NM E17NE 20050715000102005071500010EA 2005 7 15 SWIA200515216 120050627A2721 TRIM PANEL CNDAIRCL600 CL6002B19 1900309EA RUDDER CONTROL INOPERATIVE A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07970SW 7881 RUDDER TRIM KNOB INOP. REPLACED RUDDER/AILERON TRIM CONTROL PANEL. OPERATIONAL CHECK GOOD IAW CRJ MM 27-22-00 AND 27-12-10. 2L72 4F RTA21EA 20050715000122005071500012 2005 7 15 AMTA200500257 420050313A25655A33073 SLIDE BOEING737 73783N 13844HINM GE CFM56 CFM56* 13802NE L1 FAILED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11319TZ8465 8465 30643 WHILE COMPLYING WITH WORK CARD 382F2501 L1 SLIDE, SN NG4084, FAILED TO DEPLOY WITH EITHER NORMAL OR MANUAL DEPLOY PROCEDURES. SLIDE WAS REPLACED AND OPS CHECK NORMAL. (K) 2L72 4F4 FRTA16WE E2GL 20050715000142005071500014NM 2005 7 15 SWAA052028 120050711A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D + 15, STR 19R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050715000172005071500017NM 2005 7 15 SWAA052030 120050711A52306545871 DOOR FRAME BOEING737 7373H4 1384600NM AFT CARGO DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 DURING SCHEDULED C1 CHECK, FOUND AFT CARGO DOOR FWD FRAME CRACKED BETWEEN 2ND & 3RD STOP FITTING CUTOUT. REMOVED AND REPLACED AFT CARGO DOOR PER MM. 2L72 4F RTA16WE 20050715000252005071500025NM 2005 7 15 SWAA052035 120050711A53306545765 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29664WN 23495 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 12R. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050715000262005071500026NM 2005 7 15 SWAA052036 120050711A53306545774 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29664WN 23495 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 22L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050715000362005071500036EU 2005 7 15 AALA20050424 120050706A3350321441 BATTERY PACK AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW2118066 509 JFK - FOUND LEFT 4 DOOR EXIT EMERGENCY EGRESS LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT LEFT 4 DOOR FOR EMERGENCY EGRESS LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20050715000382005071500038CE 2005 7 15 DXTA200500828 120050708A2720991455811 ACTUATOR CESSNA750 750 2076810CE RUDDER FAILED E DXTAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL07906QS5219 7500206 RUDDER LIMIT FAIL -B- CAS MESSAGE ILLUMINATED DURING FLIGHT. RUDDER LIMIT WAS 28 PERCENT T/S TO BAD ACTUATOR REMOVED AND REPLACED LOWER RUDDER LIMIT ACTUATOR SYSTEM OP'S CHECKS SATISFACTORY AT THIS TIME. ALL WORK DONE IAW CE 750 M/M 27-23-00. 2L72 4J RTT00007WI 20050715000402005071500040NM 2005 7 15 05FDEA01823 120050707A5753 STRUCTURE DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 LT WING, O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. REPAIR CARRIED OUT AS PER EA1-5750-87587. 2L73 4F RTA22WE 20050715000422005071500042NM 2005 7 15 05FDEA01827 120050707A5753 STRUCTURE DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 LT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. SUPPORT BRACKET REPAIRED AS PER EA1-5750-87587 LT OUTBD FLAP INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20050715000432005071500043NM 2005 7 15 05FDEA01829 120050707A5753 STRUCTURE DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 LT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. REPAIRED AS PER EA1-5750-87587. 2L73 4F RTA22WE 20050715000502005071500050EA 2005 7 15 MASA200500511 120050702A3250 STEERING SYS CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A MASAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SW0777195 7195 CREW REJECTED TAKEOFF BECAUSE F/O HAD NO DIRECTIONAL CONTROL OF RUDDER. MAINTENANCE INSPECTED NOSE WHEEL STEERING SYSTEM AND PERFORMED 2 HIGH SPEED TAXI TESTS. MAINTENANCE COULD NOT DUPLICATE FAULT. 2L72 4F RTA21EA 20050715000512005071500051EU 2005 7 15 UPS05144842 120050706A3350 LIGHT AIRBUSA300 A300F4622R 3930360EU EMERGENCY LIGHTSMALFUNCTIONED A IPXAO OTHER O OTHER NRNOT REPORTED 1 SO01166UP 0805 SUPERNUMERARY LIGHT SYSTEM CAME ON AT LIFT OFF. LIGHTS REMAINED ON REGARDLESS OF SWITCH POSITION. LIGHTS CAME BACK ON AT LANDING. ITEM DEFERRED M305518. PLACARD INSTALLED. OPS CHECKED EMERGENCY LIGHTING SYSTEM AND OPS CHECK GOOD. THIS CLEARS M305518. PLACARD REMOVED. 2L72 4F RTA35EU 20050715000522005071500052NM 2005 7 15 UPS05444807 120050618A5330 SKIN BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C LH BS 914 STR -39L FOUND OUTER SKIN CORROSION AT TOP ROW FASTENER LOCATION MATER LOSE APPROX 15 PERCENT. CORROSION BLEND OUT 0.010 BY 1.0 BY 25 IN. EXCEED SRM 53-30-01 FIG 1 LIMITS. SKIN REPAIR AS PER SRM 53-30-03 FIG 11. 2L74 4F A20WE 20050715000552005071500055NM 2005 7 15 UPS05444811 120050617A5311 FRAME BOEING747 747123F NM FWD CARGO CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C. FWD CARGO FRAME AT BS 760 STR 34R FOUND UPPER CHORD CRACKED. CRACK LENGTH 0.5 IN. FRAME REPAIRED AS PER SRM 53-10-04 FIG 52. 2L74 4F A20WE 20050715000592005071500059NM 2005 7 15 UPS05444816 120050617A531165B0174083 FRAME BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C. BS940 S22L FRAME FOUND CRACKED, CRACK LENGTH 0.5 IN. CABIN BS 940 BETWEEN STR 22L - 23L FRAME O/B FLANGE REPAIRED AS PER HX RS NR R53-22-35322 AND UPS ENGINEERING FILE NR 747-53-20258. 2L74 4F A20WE 20050715000602005071500060NM 2005 7 15 UPS05444817 120050629A5347 CARGO TRACK BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C. M/D BS 640-770 LBL 98 TIE DOWN TRACK CROWN AREA FOUND CORRODED AS MARKED. CORROSION BLEND OUT 0.060 BY 1 BY 5 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, TRACK REPAIRED AT BS 640-770 LBL 98 AS PER SRM 53-10-05 FIG 1A. 2L74 4F A20WE 20050715000642005071500064NM 2005 7 15 UPS05444821 120050621A5347 SEAT TRACK BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C. U/D, BS 540 TO 630 RBL 28 SEAT TRACK CROWN AND FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.049 BY 0.5 BY 4 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, U/D SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A AT BS 540-630 RBL 28 AREA. 2L74 4F A20WE 20050715000652005071500065NM 2005 7 15 UPS05444822 120050621A5315 FLOORBEAM BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C. U/D BS 400 RBL 11-14 FLOORBEAM UPPER CHORD FOUND SLIGHT CORROSION. CORROSION BLEND OUT 0.038 BY 0.5 BY 2 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, U/D FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 1 AT BS 400 RBL 7 - 18"AREA. 2L74 4F A20WE 20050715000662005071500066NM 2005 7 15 UPS05444823 120050622A5311 FRAME BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C. AFT CARGO, LT BS 1560 WL 118 LBL 33 TO LBL 50 FRAME UPPER CHORD LWR SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.036 BY 2 BY 2 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS. UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 2. 2L74 4F A20WE 20050715000672005071500067NM 2005 7 15 UPS05444824 120050620A5311 FRAME BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C. FWD CARGO BAY LT SUPPORT FRAME INNER CHORD FOUND CRACKED AT STA 940 STR 34L HI LOCK CUTOUT AREA, CRACK LENGTH 0.625 IN. FRAME REPAIRED AS PER SRM 53-10-04 FIG 52. 2L74 4F A20WE 20050715000682005071500068NM 2005 7 15 UPS05444825 120050617A5311 FRAME BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C M/D BS 640 STR 24L FRAME FOUND CRACKED, CRACK LENGTH 0.5 IN. M/D BS 640 FRAME REPAIRED AT S23L TO S26L AREA AS PER RS NR R53-22-35316 AND UPS ENGINEERING FILE NR 747-53-20254. 2L74 4F A20WE 20050715000702005071500070NM 2005 7 15 MWEA050069 120050712A5313 STRINGER BOEING717 717200 1383700NM FUSELAGE DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31904ME 55168 LONGERON 18 LEFT (CUSP) IS DISTORTED AT STATION 275 DO TO DENT IN FUSELAGE SKIN. FABRICATED AND INSTALLED DOUBLER. 2L72 4F TRA6WE 20050715000732005071500073NM 2005 7 15 UPS05444827 120050622A5311 FRAME BOEING747 747123F NM AFT CARGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C, AFT CARGO STA 1600 RBL 42 FRAME UPPER CHORD LWR SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.022 BY 1.5 BY 1.5 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, CHORD REPAIRED AS PER SRM 51-40-04 FIG 2. 2L74 4F A20WE 20050715000752005071500075NM 2005 7 15 UPS05444829 120050621A5320 FLOOR SUPPORT BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C, LT BS 340 UPPER DECK FLOORBEAM TO FRAME JUNCTION AREA FOUND 1 EA HOLE CRACK AT FLOORBEAM WEB THRU THICKNESS RUNNING I/B, CRACK LENGTH 0.040 IN. FLOORBEAM WEB REPAIRED AT LBL 45 IN TO LT O/B AREA AS PER SRM 53-10-07 FIG 11. 2L74 4F A20WE 20050715000762005071500076SO 2005 7 15 SIMA200516402 120050611A2621346000731 FIRE BOTTLE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL CARGO BAY DISCHARGED A SIMAF ACTIVATE FIRE EXT. N FALSE WARNING CRCRUISE 1 SW21636AE 145160 CARGO FIRE EXTINGUISHER LIGHT ILLUMINATED IN FLIGHT, FIRE BOTTLES WERE DISCHARGED. MAINTENANCE FOUND NO EVIDENCE OF FIRE OR SMOKE. MAINTENANCE REPLACED BOTH FIRE BOTTLES. OPERATION CHECK OF FIRE DETECTION, GOOD. AC RETURNED TO SERVICE. (K) 2L72 4T4 FRTT00011ATTE6CH 20050715000792005071500079NM 2005 7 15 UPS05444831 120050618A5347 SEAT TRACK BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C, U/D STA 521-522 LBL 66 SEAT TRACK CORROSION. CORROSION BLEND OUT 0.030 BY 0.375 BY 1 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, U/D TRACK REPAIRED AT BS 480-610 LBL 66 AREA AS PER SRM 53-10-05 FIG 1A. 2L74 4F A20WE 20050715000802005071500080NM 2005 7 15 UPS05444832 120050618A5347 SEAT TRACK BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C, U/D STA 544-562 LBL 66 SEAT TRACK CORROSION. CORROSION BLEND OUT 0.059 BY 0.5 BY 3 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, U/D BS 480-610 LBL 66 TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A. 2L74 4F A20WE 20050715000812005071500081NM 2005 7 15 UPS05444833 120050621A532269B033844 SHEAR TIE BOEING747 747123F NM AFT CARGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C, AFT CARGO, LT BS 1520 FRAME SHEAR TIE FOUND CORRODED AT STR 33L TO STR 34L. CORROSION BLEND OUT 0.029 BY 0.75 BY 1.5 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, SHEAR TIE ATTACH BRACKET REPLACED AS PER SRM 51-10-01 PG 9 AT BS 1520 STR 33L - 34L AREA. 2L74 4F A20WE 20050715000822005071500082NM 2005 7 15 UPS05444834 120050621A5313 STRINGER BOEING747 747123F NM AFT CARGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C, AFT CARGO BAY BS 1680 STR 30R LWR AREA FOUND CORRODED. CORROSION BLEND OUT 0.032 BY 1 BY 3 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 2 AT BS 1671 TO BS 1690 STR 30R AREA. 2L74 4F A20WE 20050715000832005071500083NM 2005 7 15 UPS05444835 120050621A5313 STRINGER BOEING747 747123F NM AFT CARGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C , AFT CARGO, LT BS 1596 TO 1602 STR -35L STRINGER FOUND CORRODED. CORROSION BLEND OUT 0.038 BY 0.5 BY 2 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1 JUST BETWEEN BS 1590 AND 1610 STR 35L AREA. 2L74 4F A20WE 20050715000842005071500084NM 2005 7 15 DHL2005770007 120050709A7711 INDICATOR BOEING727 7272B7 138407LNM NR 1 EPR MALFUNCTIONED A DHLAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01770AT 21953 REJECTED TAKEOFF FOR NR 1 ENGINE PARAMETERS SIGNIFICANTLY LOWER THAN NR 2 AND NR 3 ENGINES AT TARGET EPR. AMBIENT TEMP 27DEG G/W 141,600LB MAX IAS APPROX 75KTS. NR 1 EPR GAUGE DEFERRED PER MEL 77-1-1. DMI CONTROL 21585 CXAT A BY RPR, PLACARD INSTALLED. CLEARED CLOGGED P-2 LINE PERFORM ENG RUN JRH CHAP 7 OPS CK NORMAL ENG. RUN SHEET COMPLETE THIS CLEARS DMI 21585 PLACARD REMOVED. 2L73 4F A3WE 20050715000862005071500086NM 2005 7 15 AWXA200500804 120050712A3350321431 BATTERY AIRBUSA319 A319132 3930340NM EMERGENCY LIGHT DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28819AW 1395 PHX - EEL - SEVERAL EMERGENCY EXIT LIGHTS IN AFT CABIN FAILED DURING EMERGENCY LIGHTS TEST DURING 4 DAY CHECK. MAINTENANCE REMOVED AND REPLACED THE BATTERY IN THE EPSU 13WL IAW AMERICA WEST AIRLINES TASKCARD A1C33302. 2L72 4F RTA28NM 20050715000882005071500088NM 2005 7 15 AWXA200500806 120050711A7714 CONNECTOR BOEING757 7572G7 1384963NM TACH LOOSE A AWXAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 WP28909AW 24522 LAX - ABORTED TAKEOFF - FLT 0033 - DURING TAKEOFF HAD NO N3 INDICATION AT 90 KNOTS. ABORTED TAKEOFF, RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND CONNECTOR D1338 LOOSE, N3 TACH TRANSMITTER. TIGHTENED LOOSE CONNECTOR, D1338, IAW BOEING 757 FIM 77-12-00 FIG 105. PERFORMED OPERATIONAL CHECK IAW BOEING 757 AMM 71-00-00-2. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA2NM 20050715000902005071500090NM 2005 7 15 DXTA200500830 120050709A3241 WARNING LIGHT AMD FALC50FALCON2000 2730170NM BRAKES ILLUMINATED E DXTAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL07218QS 118 BRAKE LIGHT ILLUMINATED IN FLIGHT, DOWNLOADED FAULT CODE 335. RESEARCHED COOL CODE: CHECK RT WHEELS. WHEELS CHECK GOOD. NO DEFECTS DETECTED. WORK PERFORMED IAW CHAPTERS 45-308 AW 32-404 OF THE FALCON 2000 M/M. 2K73 4F RTA50NM 20050715000922005071500092EU 2005 7 15 UPS05144867 120050711A5210 DOOR AIRBUS300 A300B4622R 3930312EU CREW DEPLOYED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01141UP 0824 INSPECTION TYPE: PS9, EMERGENCY OPERATION ON CREW DOOR DEPLOYED. REMOVED AND REPLACED DIAPHRAGM ON PERCUSSION MECHANISM AND SERVICED CYLINDER PRESSURE IAW AIRBUS MM 52-10-14-3. 2L72 4F RTA35EU 20050715000942005071500094NM 2005 7 15 UPS05444863 120050626A5311 SPAR BOEING747 747123 1384873NM FUSLEAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE: C, RT SIDE OF BS 1241 UPPER REAR SPAR SIDE OF BODY SPLICE PLATE AREA NR 5 HOLE FOUND CORRODED CRACKED AT SPAR CHORD HORIZONTAL FLANGE LWR SURFACE WITH DEPTH 0.060 INCH & LENGTH 0.050 INCH APPROX. RIGHT BS 1241 UPPER CHORD BOLT HOLE NR 5 REPAIRED AS PER EO B747-5740-17032-C. 2L74 4F A20WE 20050715000962005071500096NM 2005 7 15 UPS05444868 120050621A5340 FITTING BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C FX - LT STA 1241 FORGING TO KICK FITTING BOLT HOLES FOUND CORRODED (FINAL HOLE SIZE: 1.173 INCH). FORGING BOLT HOLE REPAIRED AS PER HX RS R53-43-35324 & UPS ENGINEERING FILE 747-53-20264. 2L74 4F A20WE 20050715000992005071500099NM 2005 7 15 UPS05444836 120050615A575365B078276 RIB BOEING747 747123F NM TE FLAPS CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C, RHW NR 22 VC FLAP I/B ARM I/B SUPPORT RIB CRACKED AT D HOLE AREA. CRACK LENGTH 0.4375 IN. SUPPORT RIB LINKAGE ATT BOSS TIME LIMITED REPAIRED CARRIED OUT AS PER RS NR R57-41-35323 AND UPS EO NR B747-5740-22465-A. 2L74 4F A20WE 20050715001012005071500101NM 2005 7 15 UPS05444877 120050618A532069B821943 BRACKET BOEING747 747123 1384873NM KEELBEAM BOX CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE: C, FX KEELBEAM BOX INTERIOR SUPPORT ROD ATTACH BRACKET FOUND CORROSION AT STA 1240 LBL 3 BOX TOP AREA. CORROSION BLEND OUT 0.051 X .5 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. BRACKET REPLACED AS PER SRM 51-10-01 PG 9 AT BS 1240 LBL 3 AREA. 2L74 4F A20WE 20050715001042005071500104NM 2005 7 15 UPS05544881 120050713A2780 FLAP SYSTEM BOEING757 75724APF 1384969NM WING MALFUNCTIONED A IPXAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 SO01407UP 23729 EMERGENCY DECLARED. TRAILING EDGE FLAP ASYMMETRY ICAS COMING INTO SDF. RAN CHECK LIST LANDED WITH SLATS ONLY 172 KTS. NO PROBLEMS. R/R'D FLAP POS XMTR IAW MM 27-58-03-4. OPS CKS GOOD. ALSO CK'D C/P PINS FOR SECURITY & CLEARED MEM N BOXES. A/C OK FOR SERVICE. 2L72 4F RTA2NM 20050715001072005071500107WP 2005 7 15 UPS05844803 120050620A53135750198501 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01705UP 45949 INSPECTION TYPE:C-2, LONGERON 24L CRACKED ON O/B FLANGE. REMOVED AND REPLACED LONGERON 24L IAW SRM 51-3-2, 51-1-8, AND 51-1-20D. 2L74 4F RT4A25 20050715001092005071500109EA 2005 7 15 SIMA200517108 120050618A3350110049 BATTERY CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE EMERGENCY LIGHT DISCHARGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21503AE 10021 ALL EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED ALL 4 BATTERY PACKS AND ALL 4 BATTERY CHARGERS. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (K) 2L72 4F4 FRTA21EA EOOO63EN 20050715001112005071500111NM 2005 7 15 F3LA200500031 120050704A270047145133 ACTUATOR AIRBUSA319 A319111 3930336NM FLT CONTROLS UNSERVICEABLE A F3LAK NONE F FLT CONT AFFECTED ININSP/MAINT 1 NM03928FR 3937 2236 THS FAILED SECTION -A- OF TASK CARD TC 27400-1. THS LOCKED IN FULL NOSE DOWN POSITION. REPLACED THS ACTUATOR PER MM 27-44-51-400-001. PERFORMED REQUIRED SYSTEM TEST PER MM 27-41-00-730-001 AND CHECKED GOOD. 2L72 4F RTA28NM 20050715001142005071500114 2005 7 15 HNAA0500070 420050713A3440 TRANSCEIVER DHAV DHC8 DHC8311 1386006EA WX RADAR SYS MALFUNCTIONED A HNAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA07331EN 274 AFTER TAKEOFF, RADAR PAINTED SOLID RED LINE AT 10 MILES AND TILT HAD NO EFFECT THEN RADAR WENT TOTAL INOP. REMOVED AND REPLACED RECEIVER TRANSMITTER AND ANTENNA. 2H72 4T RTA13NM 20050715001152005071500115SO 2005 7 15 SIMA200516001 120050604A2150 ACM EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL NR 1 ODOR A SIMAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW21724AE 145301 CREW GOT A SMOKE ODOR WITH A HINT OF VISIBLE SMOKE IN COCKPIT AFTER STARTING THE APU AND TURNING ON PACKS ON THE GROUND. INSPECTED/ TROUBLESHOT FOR DISCREPANCY IAW MM. ISOLATED TO NR 1 ACM. NR 1 PACK DEFERRED IAW MEL. (K) 2L72 4F4 FRTT00011ATTE6CH 20050715001162005071500116WP 2005 7 15 0500989881 120050705A2910 PACKING DOUG DC9 DC951 3022051WP HYD SYSTEM LEAKING A NWAAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL01676MC 47652 WHILE INBOUND FOR LANDING AT MYR, THE LEFT HYDRAULIC SYSTEM FLUID QUANTITY WENT TO ZERO AND THE PRESSURE DROPPED. COM PROCEDURES WERE COMPLIED WITH AND THE RIGHT HYDRAULIC SYSTEM FUNCTIONED NORMALLY. NO EMERGENCY DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT AT MYR. CONTRACT MAINTENANCE CONFIRMED THE LOSS OF HYDRAULIC FLUID AND FOUND A FAILED PACKING ON THE LEFT THRUST REVERSER CONTROL VALVE AS THE CAUSE FOR THE LEAK. NWA TECHNICIANS SENT FROM ORD FOR REPAIR. AIRCRAFT HAS RETURNED TO SERVICE. 2L72 4F RTA6WE 20050715001172005071500117NM 2005 7 15 UPS05444806 120050620A5210 STRUCTURE BOEING747 747123F NM CREW DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C, U/D CREW DOOR LWR BEAM WEB CTR CRACKED, CRACK LENGTH 0.375 IN. U/D CREW DOOR LOWER BEAM WEB CENTER AREA REPAIRED AS PER SRM 51-40-03 FIG 1. 2L74 4F A20WE 20050715001182005071500118EU 2005 7 15 SF20050708 120050708A2612 WARN PANEL SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE RT ENGINE FIRE WARNING A UHLAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL1735SZ 35 AT 2000 FT RT ENGINE CENTRAL WARNING PANEL RED FIRE LIGHT CAME ON AND FIRE BELL SOUNDED. DISCHARGED 1 BOTTLE AND SHUT DOWN ENGINE IAW QRH. ESTIMATED LANDING WEIGHT 27,000 LBS. AIRCRAFT RETURNED AND IS AWAITING MAINTENANCE. 2L72 4T4 TRTA52EU E8NE6 20050715001212005071500121NM 2005 7 15 ASMF200507004 120050706A2410696233B CSD DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE LT ENGINE FAILED W ASMFA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW23169PL3454 53175 725748 DURING CLIMB, LT ENGINE CSD REACHED RED RANGE AND APU WAS OUT OF SERVICE. CHIP DETECTOR WAS VERIFIED AND OIL LEVEL WAS ON YELLOW RANGE. CSD, OIL RADIATOR AND CENTRIFUGAL SWITCH WERE REPLACED IAW MM 24-20-00, 24-10-01 AND 24-10-03. APU WAS TESTED IAW MM 49-60-01. DURING OVERNIGHT SERVICE, THE APU WAS REPLACED IAW MM 49-10-00, TESTED CORRECT. 2L72 4F4 FRTA6WE E9NE 20050715001222005071500122NE 2005 7 15 ASMF200507005 220050707A7230JT8D219 COMPRESSOR DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE LT ENGINE DAMAGED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23204AM2784914488 49404 725695 DURING BOROSCOPIC INSPECTION TO LT ENGINE, DAMAGE OUT OF LIMITS ON 1 BLADE OF COMPRESSOR SEVENTH STAGE WITH 0.150 DEPTH. ENGINE REPLACED. DURING TESTS FUEL LEAK DETECTED IN A LINE FROM CSD. LINE TIGHTENED CORRECTING THE LEAK. TESTS WERE PERFORMED IAW MM 71-00-02 AND 71-00-00, ALL CORRECT. 2L72 4F4 FRTA6WE E9NE 20050715001232005071500123 2005 7 15 PCSA708051 420050708A341869485938 MODULE BOEING727 727233 138408ANM STALL WARNING MALFUNCTIONED A PCSAJAD DUMP FUEL UNSCHED LANDING RETURN TO BLOCK JN WARNING INDICATION FALSE WARNING TOTAKEOFF 1 SO29395AJ 21100 ON DEPARTURE, CREW REPORTED STALL WARNING STICK SHAKER CAME ON AT ROTATION. CREW DUMPED FUEL, RETURNED AND LANDED WITHOUT ANY FURTHER INCIDENT. MAINTENANCE TROUBLESHOT STALL WARNING SYSTEM. OPERATIONAL CHECK NORMAL IAW B-727 MM CH 34-18-01, UNABLE TO DUPLICATE DISCREPANCY. AS A PRECAUTION, MAINTENANCE REMOVED AND REPLACED STALL WARNING MODULE IAW B-727 MM CH 34-18-41, OPERATIONAL CHECK GOOD IAW B-727 MM CH 34-18-01. AIRCRAFT RETURNED TO SERVICE. 2L73 4F RTA3WE 20050715001252005071500125EU 2005 7 15 07062005 120050706A2121 SMOKE SAAB SF340 340B 7860101EU CABIN DETECTED A NSVAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA27315CE 343 SMOKE IN CABIN CONFIRMED. NO MORE SMOKE WITH RECIRC FAN OFF. 2L72 4T RTA52EU 20050715001272005071500127EU 2005 7 15 F3LA200500030 120050705A2750 FLAP SYSTEM AIRBUSA319 A319112 3930323EU MALFUNCTIONED A F3LAO OTHER F FLT CONT AFFECTED APAPPROACH 1 NM03915FR 1851 DURING ARRIVAL IN ANC, FLIGHT CREW REPORTED FLT CONTROL FLAPS FAULT ON ECAM. SLATS TRAVELED TO THE 2 POSITION, FLAPS DID NOT MOVE FROM THE ZERO POSITION. AIRCRAFT LANDED WITHOUT INCIDENT. PERFORMED BITE TEST OF SFCC 1 AND SFCC 2. NO FAULTS NOTED. OPERATED FLAPS ON GROUND. INSPECTED FLAP DRIVE MECHANISMS AND FLAPS. NO DEFECTS FOUND. OPERATION OF FLAPS/SLATS NORMAL. 2L72 4F RTA28NM 20050715001292005071500129WP 2005 7 15 UPS05844880 120050713A2150 CONTROL VALVE DOUG DC8 DC873F 302199FWP LEFT CLOSED A IPXAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO01818UP 46108 BTB DUE TO SMOKE IN COCKPIT DURING PUSHBACK. SUSPECT LEFT PACK OPEN DUE TO DMI ON LEFT PACK. LEFT PACK SWITCH WAS IN THE OFF POSITION. FOUND LEFT PACK FLOW CONTROL VLV OPEN CLOSE VLV PER MEL ITEM 7 STEP 1 OPS CK LEFT AND RIGHT PACKS ON GROUND LEFT PACK IS CLOSED AND WIRED RT PACK IS OPERATIONAL. 2L74 4F RT4A25 20050715001692005071500169EU 2005 7 15 07102005 120050710A32465006227 WHEEL SAAB SF340 340B 7860101EU NLG DEFECTIVE A NSVAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 EA27239CJ 239 NOSE WHEEL SHIMMY ON TAKEOFF. REMOVED AND REPLACED NOSE WHEELS. 2L72 4T RTA52EU 20050715001752005071500175NM 2005 7 15 SB05080 120050711A3350 SOCKET BOEING737 737301 1384611NM EMERGENCY LIGHTSDIRTY A USAAK NONE O OTHER ININSP/MAINT 1 EA19577US 23742 MAINTENANCE REPORTED EMERGENCY LIGHT IN SEAT ROW 21 INOPERATIVE. MAINTENANCE CLEANED CONNECTION ON EMERGENCY LIGHT SOCKET AND REPLACED BULB. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050715001772005071500177NM 2005 7 15 AT0500021 120050707A3350 CONNECTOR BOEING717 717200 1383700NM EMERGENCY LIGHTSLOOSE A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15956AT 55018 SEAT 31D E PATH LIGHTS WILL NOT ILLUMINATE. SECURED LOOSE FLOOR TRACK TO SEAT HARNESS CONNECTOR AS REQUIRED. OPS CHECK GOOD. 2L72 4F TRA6WE 20050715001782005071500178NE 2005 7 15 C8GA20050016 220050708A7261 OIL FILTER BOEING727 727223 1384074NM PWA JT8 JT8D NE NR 3 ENGINE CONTAMINATED A C8GAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SO29899AA 22015 700799 IN CRUISE, NR 3 ENGINE LOW OIL PRESSURE/FILTER BYPASS LIGHT ILLUMINATED. REDUCED ENGINE POWER PER AOM PROCEDURES AND LIGHT EXTINGUISHED. LIGHT ILLUMINATED AGAIN. CREW SHUTDOWN ENGINE AS PRECAUTION. AIRCRAFT CONTINUED AND LANDED WITHOUT INCIDENT. FOUND DEBRIS IN NR 3 ENGINE OIL FILTER. REPLACED FILTER. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. PERFORMED OIL CHANGE AND REPLACED FILTER AGAIN AFTER NEXT FLIGHT. NO DEBRIS NOTED. 2L73 4F4 F A3WE E2EA 20050715001792005071500179SO 2005 7 15 C2XA05SH065 120050706A532014530628003 FLOOR SUPPORT EMB 145 EMB145 3260210SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716961 145103 DURING C-CHECK, MAINTENANCE FOUND CORROSION ON LT AND CENTER OMEGA BEAM FLOOR BOARD MATTING SURFACE FRAMES 33 TO FRAMES 38. MAINTENANCE REPAIRED CENTER OMEGA BEAM AT FRAME 33 IAW EC 5320-01251 AND LT OMEGA BEAM AT FRAME 33 I/A/W EC 5320-01242. AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2L72 4F RTT00011AT 20050715001852005071500185EA 2005 7 15 VTZA200500135 120050709A2740 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A VTZAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 EA27627BR 7233 STAB CHANNEL 1 STATUS MSG, NOT ABLE TO RESET. RETURN TO FIELD. REMOVED AND REPLACED HSTCU AND MACH TRIM PANEL. NO FURTHER DEFECTS NOTED AT THIS TIME. REF MM CH 27-41-01. 2L72 4F RTA21EA 20050715001862005071500186EU 2005 7 15 SF200506171 120050617A243232848001 BATTERY SAAB SF340 SF340A 7850100EU ELEC POWER DISCHARGED A UHLAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL17121CQ 293 121CQ IN FLIGHT LT HOT BATTERY LIGHT ILLUMINATED WITH ALL ASSOCIATED RELAYS OPEN. AIR CREW DIVERTED AIRCRAFT. MAINTENANCE ARRIVED AND FOUND LT BATTERY BAD. REMOVED AND REPLACED LT BATTERY. 2L72 4T RTA52EU 20050715001872005071500187EU 2005 7 15 20050627SF 120050627A2600 WARN PANEL SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE NR 2 ENGINE FIRE WARNING A UHLAAD UNSCHED LANDING RETURN TO BLOCK J WARNING INDICATION CLCLIMB 1 GL1735SZ 35SZ ON CLIMB-OUT, AIRCREW RECEIVED FIRE INDICATION ON NR 2 ENGINE. AIRCREW RETURNED. 2L72 4T4 TRTA52EU E8NE6 20050713000522005071300052EA 2005 7 13 SWIA200515213 120050321A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07915SW 7615 FS 621 FLOOR SUPPORT ANGLE RBL 42 CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED ANGLE IAW CRJ REO 601R-53-61-117. 2L72 4F RTA21EA 20050713000602005071300060NM 2005 7 13 UPS05444741 120050621A5315 FLOORBEAM BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 LT BS 340 UPPER DECK FLOORBEAM TO FRAME FUNCTION AREA FOUND 1EA HOLE CRACK AT FLOORBEAM UPPER CHORD APPROX 0.040 IN RUNNING DOWNWARD. CRACK LENGTH 0.040 INCH. CORROSION BLEND OUT N/A. LT BS 340 UPPER DECK FLOORBEAM UPPER CHORD REPAIRED AT LBL 35 TO LT MOST O/B AREA AS PER SRM 53-10-07 FIG 23. 2L74 4F A20WE 20050713000632005071300063WP 2005 7 13 UPS05844748 120050602A5313S2597424 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 AFTER REMOVAL OF L33R END FITTING STA 8 FOUND L33R CORRODED OUT OF LIMITS STA 8. REF N/R 807385. REMOVED AND REPLACED LONGERON 33R STA 8 TO 70 IAW SRM 51-1-21, 1-1-21D AND 51-3-2. 2L74 4F RT4A25 20050713000682005071300068EA 2005 7 13 MASA200500471 120050616A3350 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSLOOSE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07593ML 7465 EMERGENCY FLOOR LIGHTING STRIPS FROM ROW 7 TO ROW 12 INOPERATIVE. MX SECURED CONNECTOR AT FLOOR LIGHTING ASSEMBLY. 2L72 4F RTA21EA 20050713000832005071300083EU 2005 7 13 2005UALA00609 120050630A3350 LIGHT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE ROWS 12,13,14,18INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29409UA 462 CABIN EMERGENCY LIGHTS IN ROW 12-13-14 AND ROWS 18-19 AND 20 INOP. 2L72 4F4 FRTA28NM E40NE 20050713000862005071300086 2005 7 13 2005UALA00303 420050114A2565D30664105 SLIDE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE GAUGE & BAG TORN A UALAK NONE O OTHER ININSP/MAINT 1 WP29411UA 464 PREDEPLOYED, FOUND BOTTLE GAUGE BROKEN AND BAG TORN. ASPIRATOR BENT. ALL FLANGABLE LINKS POPPED A HOLE IN THE TOP TUBE, BLOWN OUT SEAM AND TORN FABRIC. DEFECTS REPORTED BY THE OSV SHOP (WINSLOW) ARE OF A SLIDE/RAFT PREVIOUSLY INADVERTENTLY DEPLOYED BY CREW ON 12/17/2004 (IAD). THERE WAS NO REPORTED ABNORMALITY DURING SLIDE DEPLOYMENT, HENCE THE REPORTED MULTIPLE DAMAGE ON THE SLIDE/RAFT ASSY FOUND IN THE SHOP ARE PROBABLY DUE TO MISHANDLING DURING SLIDE REMOVAL AND/OR TRANSPORTATION. 2L72 4F4 FRTA28NM E40NE 20050713000892005071300089EU 2005 7 13 2005UALA00610 120050630A5532 SKIN AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE VERTICAL STAB LIGHTNING STRIKEA UALAK NONE O OTHER ININSP/MAINT 1 WP29456UA 1128 LIGHTNING STRIKE ON VERT FIN RT SIDE BETWEEN RIB 10 AND UPPER LEADING EDGE. MAJOR REPAIR ACCOMPLISHED PER EVA 50378A 2L72 4F4 FRTA28NM E40NE 20050713001062005071300106NM 2005 7 13 UPS05444791 120050621A5347 SEAT TRACK BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 BS 520-600 RBL 47 SEAT TRACK CROWN AND FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.048 BY 0.5 BY 3.5 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A. 2L74 4F A20WE 20050713001252005071300125WP 2005 7 13 UPS05844770 120050608A5311 FRAME DOUG DC8 DC871F 302199DWP CARGO BAY CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01705UP 45949 INSPECTION TYPE:C-2. MAIN CARGO STA 1700 RBL 24 SEVERE CORROSION AT TOP OF FRAME ON UNDERSIDE AND CONTINUES OUTBD TO RBL48. CUT OUT DAMAGED AREA PER SRM 51-2-1 FIG 1, SHEET 7. FABRICATED REPAIR REPAIR DOUBLER AND REPAIR ANGLES IAW SRM 51-1-21 FIG 1, AND INSTALLED IAW SRM 51-2-1 FIG 7, SHEET 7. 2L74 4F RT4A25 20050713001342005071300134EA 2005 7 13 SWIA200515214 120050630A2740 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB STICKS A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07431SW 7536 F/O TRIM STICKS IN DOWN POSITION. REPLACED F/O TRIM SWITCH IAW CRJ MM27-41-05. OPERATIONAL CHECK GOOD IAW CRJ MM27-40-00-710-801. 2L72 4F RTA21EA 20050714000052005071400005CE 2005 7 14 CIEA200500008 120050701A534450430043547 HINGE BEECH BEECH 200 B200 1152922CE CABIN DOOR CRACKED E CIEAK NONE O OTHER ININSP/MAINT 1 NM03203LG7511 BB926 AFT LANDING ATTEMPTED TO CLOSE MAIN CABIN ENTRY DOOR & HAD DIFFICULTY. A 5 INCH CRACK NEAR AFT, BOTTOM END OF DOOR, WHERE HINGE IS ATTACHED. DAMAGED - ENTRY DOOR HINGE HALF FOUND 8 INCH CRACK RESULTING IN CRACK GOING THRU 8 RIVETS AFT OF DOOR FWD. DOOR CHANNEL, 5 INCH CRACK EXTENDING FROM 1ST RIVET FWD OF AFT END OF DOOR FWD THRU 5 RIVETS. DOOR SKIN HAD OVERSIZED RIVET HOLES, SMALL CRACKS, LESS THAN .125 INCH. OUTER SKIN .040 THICK. DOOR HINGE .065 THICK. DOOR CHANNEL .050 THICK. FLEXING HINGE, ROTATES AROUND SINGLE ROW OF RIVETS, UNTIL IT FAILS. HINGE IS BETWEEN .040 SKIN & .050 CHANNEL. HINGE FAILS, POSSIBILITY OF LOOSING PRESSURIZATION. REVIEW OF RECORDS, HINGE HAD NEVER BEEN REPLACED. 1L72 4T A24CE 20050714000122005071400012NM 2005 7 14 RYAN200500020 120050703A7830MS25235 SPEED BRAKE BOEING737 737201 1384454NM THRUST REVERSER WORN A RYNAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 CE07225US 21667 SPEED BRAKE TAKEOFF WARNING SWITCH WORN/BROKEN. SWITCH NOT MAKING CONTACT WHEN SPEED BRAKE ARMED, CAUSING A FALSE TAKEOFF WARNING TO SOUND WHEN THROTTLES ARE ADVANCED. 2L72 4F A16WE 20050714000152005071400015NM 2005 7 14 05FDEA01839 120050707A5753 HINGE DOUG MD11 MD11 3023602NM LT WING TE FLAPSCORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 LT WING - O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. FABRICATED BUSHING AND INSTALLED AS PER EA 1-5750-87588. 2L73 4F RTA22WE 20050714000232005071400023EA 2005 7 14 VNAA0507001 120050702A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT WING TIP LIGHTNING STRIKEA VNAAK NONE O OTHER ININSP/MAINT 1 GL05220PS 7887 AFTER LANDING MAINTENANCE DISCOVERED EVIDENCE OF LIGHTNING DAMAGE ON THE LT WING TIP. A DETAILED LIGHTNING STRIKE INSPECTION WAS PERFORMED IAW CRJ200 AMM 05-51-05-220-801. ALL DAMAGE WAS REPAIRED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050714000342005071400034NM 2005 7 14 2005UALA00620 120050705A3350582233 BATTERY BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29187UA 26877 EEL INOPERATIVE, MAIN STAIRS. BATTERY NOT HOLDING CHARGE. EEL LIGHT BATTERY REPLACED. 2L74 4F4 FRTA20WE E24NE 20050714000392005071400039NM 2005 7 14 2005UALA00625 120050701A3350362624 LAMP BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29660UA 27115 EEL LIGHT RIGHT OF MID GALLEY INOPERATIVE. EEL LAMP WAS DAMAGED. REPLACED EEL LAMP, OK. 2L72 4F4 FRTA1NM E24NE 20050714000422005071400042NM 2005 7 14 2005UALA00628 120050704A3350209 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE DOOR 4L AFT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29116UA 26908 EMERGENCY EXIT SIGN EEL INOPERATIVE, DR 4L AFT. REPLACED BURNED OUT LAMP. 2L74 4F4 FRTA20WE E24NE 20050714000462005071400046NM 2005 7 14 2005UALA00631 120050704A3350362624 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE SEAT 5E INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29116UA 26908 EEL INOP SEAT 5E AFT SECTION. EEL LAMP INOP. REPLACED EEL LAMP, OK. 2L74 4F4 FRTA20WE E24NE 20050714000562005071400056 2005 7 14 2005UALA00604 420050628A3442 TRANSCEIVER AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE WX RADAR SYS FAILED A UALAA UNSCHED LANDING O OTHER CRCRUISE 1 WP29410UA 463 WX RADAR FAILED INFLIGHT. WEATHER RADAR RECEIVER / TRANSMITTER WAS DEFECTIVE. SHOP FINDINGS INDICATED A R/T FAULT. WXR R/T WAS REPLACED, AND NO FURTHER ASSOCIATED PROBLEMS OCCURRED. 2L72 4F4 FRTA28NM E40NE 20050714000692005071400069 2005 7 14 07042005 420050704A61228210410 GOVERNOR BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE PROP MALFUNCTIONED A NSVAA UNSCHED LANDING O OTHER CRCRUISE 1 EA27243CJ UE43 114172 LT ENGINE SURGING. REMOVED AND REPLACED PROPELLER GOVERNOR. 2L72 4T4 TRTA24CE E26NE 20050714000722005071400072EA 2005 7 14 SWIA200515219 120050630A2760C13045BA03 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07706SK561 561 10149 SSCU - NR 2 FAULT STATUS MESSAGE IS DISPLAYED. REPLACED NR 2 SSCU IAW CRJ MM 27-61-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050714000812005071400081NM 2005 7 14 UPS05444797 120050617A5347 SEAT TRACK BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 TIE DOWN TRACK BS 1483 RBL 97 CORRODED. CORROSION BLEND OUT 0.080 BY 0.75 BY 1.25 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS. TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A. 2L74 4F A20WE 20050714000872005071400087WP 2005 7 14 UPS05844796 120050705A33506012235 BATTERY DOUG DC8 DC873F 302199FWP EMERGENCY LIGHTSDISCHARGED A IPXAO OTHER L NO TEST ININSP/MAINT 1 SO01874UP 46074 EMERGENCY EXIT LIGHTS FAIL PRE-DEPARTURE CHECK. SWITCH NOT LEFT ENGAGED OVER W/E. REPLACED BATTERY PER MM 33-50-01-2. 2L74 4F RT4A25 20050714001032005071400103NM 2005 7 14 QXEA200501089 120050705A33506104781 BATTERY PACK DHAV DHC8 DHC8202 2809007NM ZONE 200 DISCHARGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09353PH126322012 496 SEVERAL EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK AT PS3 POSITION. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050714001172005071400117SO 2005 7 14 LR7A05096 120050705A2910M832482910 PACKING LKHEED382 382G 526414USO HYD LINE SPLIT A LR7AE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 AL03405LC 460 5025 VISIBLE FLUID LEAK NR 2 ENGINE. SHUTDOWN IAW AFM. RESEALED NR 2 ENGINE HYD PUMP PRESSURE LINE FITTING. OPS CHECK GOOD SMP581 CHAP 29-11 PG 201, NO LEAK. 2H74 4T A1SO 20050714001212005071400121EA 2005 7 14 COMA0560370 120050630A2750 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ACTIVATED A COMAO OTHER JN WARNING INDICATION FALSE WARNING TXTAXI/GRND HDL 1 SO01779CA 7306 FLAPS FAIL CAUTION. RESET FLAPS AND DEFERRED MAINTENANCE PER AD 98-20-01. 2L72 4F RTA21EA 20050714001322005071400132NM 2005 7 14 SWAA052018 120050711A53116516301 FRAME BOEING737 7373H4 1384600NM COCKPIT FLOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED D-CHECK, FOUND 2 EA FUSELAGE STUB FRAMES CRACKED AT BS 188, LT & RT SIDE, WL 208. REMOVED AND REPLACED STUB FRAMES PER SRM. 2L72 4F RTA16WE 20050714001512005071400151NM 2005 7 14 ASAA0510127 120050607A5340654659616 BRACKET BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 AFT CARGO PIT B-STA 727B FRAME TO KEELBEAM (STA 27R) ATTACH ANGLE HAS CORROSION. REPLACED ATTACH ANGLE. (K) 2L72 4F4 F A16WE E2EA 20050714001532005071400153NM 2005 7 14 ASAA0590029 120050329A5320146A7501163 SUPPORT BOEING737 737990 NM GE CFM56 CFM567B24 NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02307AS 30015 DURING C-CHECK, FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT AT BS 500A. REPAIRED IAW SRM. (K) 2L74 4F4 FRTA16WE E00055EN 20050714001842005071400184NM 2005 7 14 ASAA0510157 120050613A531465621251 KEELBEAM BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 KEELBEAM B-STA 707-747 LT LOWER CHORD CORRODED. REMOVED AND REPLACED KEELBEAM IAW SRM. (K) 2L72 4F4 F A16WE E2EA 20050714001912005071400191NM 2005 7 14 ASAA0510115 120050531A53306545866648 SKIN BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 B-STA 597 TO B-STA 618 BETWEEN LT AND RT KEELBEAMS PANEL CORRODED. REPLACED KEELBEAM PANEL. (K) 2L72 4F4 F A16WE E2EA 20050714002042005071400204EA 2005 7 14 SWIA200515223 120050630A27604916406 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 NM07595SW 7292 FLT SPLRS AND OB GND SPLR FAULT STATUS MSG ON ED2 SELECTION TO FLAPS 8. REPLACED BOTH SECUS IAW MM 27-61-05, PN OFF 49164-06 SN 01562 AND SN 01544 2L72 4F RTA21EA 20050714002052005071400205EA 2005 7 14 SWIA200515224 120050701A5610 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAO OTHER O OTHER DEDESCENT 1 NM07440SW 7589 LT COCKPIT WINDOW CRACKED DURING DESCENT. REMOVED AND INSTALLED NEW WINDSHIELD IAW MM 56-12-01, PN NP139322-5 SN OFF 02014H6536. 2L72 4F RTA21EA 20050714002162005071400216EA 2005 7 14 SWIA200515235 120050627A2932 TRANSDUCER CNDAIRCL600 CL6002C10 1390015EA NR 2 HYDRAULIC MALFUNCTIONED A SWIAAE UNSCHED LANDING ENGINE SHUTDOWN M OVER TEMP CRCRUISE 1 NM07752SK 10209 RECEIVED HYD 2 HI TEMP CAUTION MSG AT FL370. TEMP WAS AT 98 DEGREES AND CLIMBED TO 107 DEGREES. CLOSED HYD 2 SOV AND PRECAUTIONARY SHUT DOWN OF ENG NR 2 AS PER QRH. REPLACED NR 2 HYDRAULIC TEMP TRANSDUCER. OPERATIONAL CHECK GOOD IAW 29-36-03. 2L72 4F RTA21EA 20050715000012005071500001NM 2005 7 15 UPS05444747 120050618A5311 FRAME BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 BS 900 LT FRAME O/B FLANGE FOUND CRACKED BTN S-12L AND S-13L. CRACK LENGTH 0.4375 IN. CORROSION BLEND OUT N/A. BS 900 LT FRAME O/B FLANGE BETWEEN STR 12L AND 13L AREA REPAIRED AS PER SRM 53-10-04 FIG 4. 2L74 4F A20WE 20050715000062005071500006NM 2005 7 15 HNAA0500069 120050712A2460 WARNING LIGHT DHAV DHC8 DHC8102 2809003NM DC BUSS FALSE INDICATIONA HNAAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 EA07810EX 308 DC BUSS CAUTION LIGHT ILLUMINATED AFTER TAKEOFF FOLLOWED BY ASSOCIATED CAUTION LIGHTS. CREW CONFIRMED PRIMARY INVERTER HAS SLIGHT FISH SMELL. LGA MAINTENANCE GOING TO REMOVE AND REPLACE INVERTER FOR PRECAUTION. DUE TO PREVIOUS HISTORY AIRCRAFT WILL FERRY TO MDT FOR FURTHER MAINTENANCE ACTIONS. INSPECTED DC CONTACTOR BOX AND OPS CHECKED ELECTRICAL SYSTEM, INSPECTED BOTH DC GENERATORS AND AC CONTACTOR BOXES. NO DISCREPANCIES NOTED. 2H72 4T RTA13NM 20050715000182005071500018NM 2005 7 15 SWAA052031 120050712A33506104781 BALLAST BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29359SW 26596 DURING SCHEDULED RON CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BALLAST ASSY PER MM. 2L72 4F RTA16WE 20050715000242005071500024 2005 7 15 SWAA052034 420050712A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29746SW 29798 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050715000272005071500027NM 2005 7 15 SWAA052037 120050711A53306545774 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29664WN 23495 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 757, STR 24L. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050715000282005071500028CE 2005 7 15 ACE070805 120050708A731210585K FUEL HEATER BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA ENGINE CRACKED E YADAK NONE K FLUID LOSS ININSP/MAINT 1 AL03113AX 955 UC41 97546 MAINTENANCE NOTICED OIL RESIDUE ON ENGINE COWLING. LOCATED ENGINE OIL LEAK AT OIL / FUEL HEATER. REPLACED CRACKED HEATER. 2L72 4T4 TRTA24CE E4EA 20050715000322005071500032NM 2005 7 15 05FDEA01819 120050707A5753 STRUCTURE DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 LT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. FABRICATED BUSHING AND INSTALLED AS PER EA1-5750-87587. 2L73 4F RTA22WE 20050715000392005071500039NM 2005 7 15 05FDEA01821 120050707A5753 STRUCTURE DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 LT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. FABRICATED BUSHING AND INSTALLED AS PER EA1-5750-87587. 2L73 4F RTA22WE 20050715000442005071500044NM 2005 7 15 05FDEA01831 120050707A5753 STRUCTURE DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 LT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. REPAIRED AS PER EA1-5750-87587. 2L73 4F RTA22WE 20050715000452005071500045NM 2005 7 15 05FDEA01833 120050707A5753 STRUCTURE DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 LT WING, O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. FABRICATED BUSHING AND INSTALLED A PER EA 1-5750-87588. 2L73 4F RTA22WE 20050715000492005071500049NM 2005 7 15 05FDEA01841 120050707A5751 SKIN DOUG MD11 MD11 3023602NM AILERON DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 RT WING I/B AILERON BOTTOM SURFACE HAS MULTIPLE SHARP ABRASIONS. 2L73 4F RTA22WE 20050715000582005071500058NM 2005 7 15 UPS05444815 120050617A5311 FRAME BOEING747 747123F NM FWD CARGO CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C. FWD CARGO FRAME AT BS 920 STR 34L FOUND UPPER CHORD CRACKED, CRACK LENGTH 2.75 IN. FWD CARGO BAY FRAME REPAIRED AT BS 920 STR 34L - 37L AREA AS PER SRM 53-10-04 FIG 52. 2L74 4F A20WE 20050715000742005071500074NM 2005 7 15 UPS05444828 120050622A5311 FRAME BOEING747 747123F NM AFT CARGO CHAFED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C, AFT CARGO STA 1600 RBL 37 FRAME UPR CHORD LWR SURFACE CHAFING. REFER NRC NR 6784 FOR WORK DETAIL BS 1600 RBL 8. RT O/B FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 2. 2L74 4F A20WE 20050715000912005071500091EU 2005 7 15 DHL2005362008 120050713A2612 FIRE LOOP AIRBUS300 A300B4203 3930306EU ZONE 100 WILL NOT TEST A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01362DH 84 NR 2 ENGINE FIRE LOOP -B- WILL NOT TEST. DEFERRED LOOP -B- ON ENGINE NR 2 IAW MEL 26-13-03. DMI 21642. PLACARD INSTALLED. 2L72 4F RTA35EU 20050715000932005071500093EU 2005 7 15 UPS05144871 120050708A3350 BULB AIRBUS300 A300B4622R 3930312EU EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01128UP 0812 INSPECTION TYPE:N/A LAV EMERGENCY LIGHT INOP. RELAMPED, WORKED OK. 2L72 4F RTA35EU 20050715000952005071500095NM 2005 7 15 UPS05444864 120050625A5740 FITTING BOEING747 747123 1384873NM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE: C, RIGHT WING UPPER REAR SPAR SIDE OF BODY SPLICE PLATE AREA NR 5 FASTENER HOLE FOUND CRACK AT INTERNAL SPLICE FITTING (CRACK LENGTH .25 INCH). RIGHT WING INTERNAL SPLICE FITTING BOLT HOLE NR 5 REPAIRED AS PER HX RS R57-18-35333 & UPS EO B747-5710-22476-A. 2L74 4F A20WE 20050715000972005071500097NM 2005 7 15 UPS05444869 120050628A5730 SKIN BOEING747 747123 1384873NM LT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE: C, AFT T/E PANEL REMOVED FOR RECTIFICATION WING UPPER SKIN LWR SURFACE FOUND CORRODED AT WS 390. CORROSION BLEND OUT 0.131 X 1.25 X 2.5 INCHES EXCEED SRM 57-30-01 FIG 1 LIMITS, LEFT WING UPPER SKIN LOWER SURFACE REPAIRED AT WS 390 AREA AS PER HX RS R57-25-35337 & UPS EO B747-5730-22494-A. 2L74 4F A20WE 20050715001002005071500100NM 2005 7 15 UPS05444876 120050709A5320BAC15171558 STIFFENER BOEING747 747SR46 1384816NM NLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01680UP 20923 INSPECTION TYPE: C, SECONDARY INSPECTION FOUND OUT LT NLG WW TUNNER S/W AT BS 280 WL 150 STIFFENER FWD O/B FASTENER HOLE CRACKED. NLG LT WW TUNNER INTERIOR STIFFENER AT BS 280-300 WL 150 REPLACED AS PER SRM 51-10-01 PG 8. 2L74 4F RTA20WE 20050715001022005071500102NM 2005 7 15 UPS05444878 120050622A5740 FITTING BOEING747 747123 1384873NM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C RIGHT WING STA 1241 UPPER REAR SPAR SIDE OF BODY SPLICE FITTING NR 4 HOLE FOUND CRACK & COR AT INTERNAL SPLICE FITTING. RIGHT WING BS 1241 BOLT HOLE NR 4 HOLE REPAIRED AS PER SB B747-5740-17032. 2L74 4F A20WE 20050715001032005071500103NM 2005 7 15 UPS05444837 120050621A5311 FRAME BOEING747 747123F NM AFT CARGO CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C, AFT CARGO BS 1500 FRAME FOUND CRACKED JUST BELOW MOST RT HAND ROLLER TRACK AS MARKED. CRACK LENGTH 3 IN. AFT CARGO BAY FRAME AT BS 1500 STR 40R AREA REPAIRED AS PER HX RS NR R53-62-35329 AND UPS EO NR B747-5310-22463-A. 2L74 4F A20WE 20050715001082005071500108NE 2005 7 15 UPS05644717 220050618A7230 FAN BOEING767 76734AF 1385212NM GE CF6 CF680C2B7 NE RT ENGINE VIBRATION A IPXAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 SO01327UP 27753 INSPECTION TYPE: ETOP ATB - R-FAN & LPT ENG VIBRATION HIGH. DURING CLIMB AT 103.5 PERCENT N1 R ENG VIBRATION AT 5.0 FAN LPT. SLIGHT AIRFRAME SHUTTER WHEN POWER REDUCED. PERFORMED FIM 71-05-00, FIG 13, PERFORMED BLOCK 1 ANSWER IS NO BLOCK 2 ANSWER NO; BLOCK 2 ANSWER NO; BLOCK 3 ANSWER NO; BLOCK 4 ANSWER NO; BLOCK 5 ANSWER NO; BLOCK 45 SENDS US TO BLOCK 6 ANSWER YES; AT THIS POINT TECH RECOMMENDS SPINNER BALANCE AT THIS TIME. 2L72 4F4 FRTA1NM E13NE 20050715001102005071500110NM 2005 7 15 ASAA0590030 120050329A5320146A7510 INTERCOSTAL BOEING737 737990 NM GE CFM56 CFM567B24 NE FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02307AS 30015 DURING C-CHECK, FOUND CRACKED INTERCOSTAL AT 500F-500G. REPAIRED IAW SRM. (K) 2L74 4F4 FRTA16WE E00055EN 20050715001122005071500112WP 2005 7 15 UPS05844805 120050625A5320 INTERCOSTAL DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01705UP 45949 INSPECTION TYPE:C-2, INTERCOSTAL AT STA 980 HAS CORROSION. CORROSION OUT OF LIMITS PER SRM 53-2-0. FABRICATED AND INSTALLED INTERCOSTAL IAW SRM 51-1-21, AND SRM 51-1-20D. 2L74 4F RT4A25 20050715001132005071500113EU 2005 7 15 XN0A1248 120050714A2910 O-RING AIRBUS300 A300B4203 3930306EU HYD SYSTEM FAILED A XN0AD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 GL23370PC 134 YELLOW HYDRAULIC SYSTEM LOST FLUID. FOUND O-RING BROWN ON YELLOW SYSTEM FILTER HOUSING MANIFOLD. REMOVED AND REPLACED O-RING OPP & LEAK CHECK GOOD. 2L72 4F RTA35EU 20050715001242005071500124NM 2005 7 15 FX7A200500007 120050704A2781 CONNECTOR BOEING737 737231 1384079NM PWA JT8 JT8D15A 52051NE LE FLAPS DIRTY A FX7AAD UNSCHED LANDING RETURN TO BLOCK JN WARNING INDICATION FALSE WARNING CLCLIMB 1 SO1964346 21633 NR 3 LEADING EDGE FLAPS INDICATES INTRANSIT ON FLIGHT ENGINEER PANEL. FORWARD PANEL HAS LEADING EDGE AMBER LIGHT ILLUMINATED. RECYCLED TWICE WITH SAME RESULTS. AIRCRAFT COMPLETED AND AIR RETURN BACK TO MAIN BASE. MAINTENANCE CLEANED CONNECTOR ON NR 2 AND NR 3 LEADING EDGE FLAPS IAW MM REF 20-11-0. OPS CHECKED NORMAL IAW MM REF 27-82-1. 2L72 4F4 FRTA16WE E2EA 20050715001262005071500126EU 2005 7 15 07082005 120050708A26131734362450 WARNING LIGHT SAAB SF340 340B 7860101EU OVERHEAT PROTECTILLUMINATED A NSVAE ENGINE SHUTDOWN JN WARNING INDICATION FALSE WARNING TXTAXI/GRND HDL 1 EA27308CE 210 TAIL PIPE HOT LIGHT ILLUMINATED ON GROUND. 2L72 4T RTA52EU 20050715001812005071500181NM 2005 7 15 RYNA200500021 120050629A5754114N4004165A SKIN 0 BOEING757 757236 1384971NM NR 3 LE SLAT DENTED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07526NA 24794 LT WING NR 3 LEADING EDGE SLAT TRAILIING EDGE WEDGE OUTBOARD FORWARD SURFACE HAS A DENT AT APPROX WS 560. REPAIRED DENT AT NR 3 SLAT TRAILING EDGE OUTBOARD LOWER SURFACE AT WS 560 IAW B757-SRM 51-70-10 AND 57-43-01. 2L72 4F RTA2NM 20050715001822005071500182NM 2005 7 15 RYNA200500022 120050706A7933 OIL SYSTEM BOEING737 737201 1384454NM PWA JT8 JT8D9 52048NE NR 2 ENGINE OVERTEMP A RYNAE ENGINE SHUTDOWN JM WARNING INDICATION OVER TEMP CLCLIMB 1 CE07225US 21667 DURING CLIMB-OUT, NR 2 ENGINE OIL TEMP INCREASED TO 122 DEG C. DURING DESCENT, OIL TEMP INCREASED TO 140 DEG C. OIL TEMP IN YELLOW BAND FOR 5 MINUTES. OIL PRESSURE WAS NORMAL IN CLIMB AND CRUISE. NR 2 ENGINE SHUTDOWN AS A PRECAUTION BECAUSE OIL TEMP COULD NOT BE CONTROLLED BY THROTTLE. 2L72 4F4 F A16WE E2EA 20050715001892005071500189NM 2005 7 15 QXEA200501100 120050707A33506038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007NM EMERGENCY LIGHTSDISCHARGED A QXEAK NONE O OTHER UKUNKNOWN 1 NM09366PH15701 510 EMERGENCY EXIT SIGN AND LT FORWARD EGRESS LIGHTS INOP. MAINTENANCE REPLACED BATTERY PACKS AND POWER SUPPLIES AT PS-1, PS-2, PS-3 AND PS-4, AND REPAIRED RECESSED PIN AT CONNECTOR 3351-P1 OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050718000252005071800025NM 2005 7 18 ASAA0510075 120050416A5330654576989 SKIN BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 FOUND CORROSION ON FUSELAGE SKIN IN FORWARD BILGE AT BS 500B PLUS 17 INCHES OUTBOARD OF STRINGER 28 RT. REPAIRED IAW EA 5330-01925. (M) 2L72 4F A16WE 20050718000262005071800026NM 2005 7 18 ASAA0510083 120050420A53226546532540 SHEAR TIE BOEING737 737290C 138448VNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 YXX - FOUND NDT CRACK INDICATION AT FASTENER HOLE ON SHEAR TIE ANGLE AT BS 480, BETWEEN STRINGER 18L AND 19L. REPLACED SHEAR TIE AND CRACK REMOVED IAW B737-200 SRM. (M) 2L72 4F A16WE 20050718000272005071800027WP 2005 7 18 ASAA0580278 120050516A5320993053875 CUSP WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02968AS 53016 OKC - FOUND DURING HV CHECK, RIGHT FLOOR CUSP WEB CORRODED AT STATION 389-503. REMOVED DAMAGED SECTION. INSTALLED WEB AND DOUBLER. (M) 2L72 4F RTA6WE 20050718000312005071800031NM 2005 7 18 ASAA0510073 120050416A531166221611 FRAME BOEING737 737290C 138448VNM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 YXX - FORWARD CARGO FRAME ANGLE AT BS 4600, 3 INCHES BELOW STRINGER 20L HAS GOUGE. REPAIRED IAW B737-200 SRM 53-10-04 FIG 10 AND EA 5330-01923. (M) 2L72 4F A16WE 20050718000332005071800033WP 2005 7 18 ASAA0580242 120050509A5320993053875 CUSP WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - FOUND DURING C-CHECK, CUSP WEB CORRODED AT STATION 399. REMOVED CORROSION AND INSTALLED SEGMENT AND DOUBLER. (M) 2L72 4F RTA6WE 20050718000352005071800035NM 2005 7 18 ASAA0510142 120050613A5340654655218 STRINGER CLIP BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX - AFT CARGO PIT BS 827 STRINGER 26L TIE CLIP HAS CORROSION. REMOVED AND REPLACED TIE CLIP IAW B737-200 SRM. (M) 2L72 4F A16WE 20050718000362005071800036NM 2005 7 18 ASAA0540183 120050316A533065C2668531 SKIN BOEING737 7374Q8 138447QNM NR 3 SLAT DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02764AS 25101 OKC - FOUND LEFT WING NR 3 L/E SLAT T/E WEDGE IS DELAMINATED AT INBOARD AND OUTBOARD ENDS WITH EDGE POTTING DETERIORATED. REMOVED DAMAGE FABRICATED AND INSTALLED REPAIR CORES AND DOUBLERS IAW B737 SRM. 2L72 4F RTA16WE 20050718000382005071800038WP 2005 7 18 ASAA0580266 120050517A53135936071503 LONGERON DOUG DC9 DC983 3022083WP FUSLEAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - FOUND DURING C-CHECK, LONGERON 29L IS CORRODED ON THE LOWER SURFACE OF THE INBOARD FLANGE AT STATION 1206. REMOVED AND REPLACED DAMAGED LONGERON AND INSTALLED SPLICE. (M) 2L72 4F RTA6WE 20050718000392005071800039 2005 7 18 QXEA200501097 420050704A3420 SYMBOL GENERATOR DHAV DHC8 DHC8202 2809007NM ZONE 100 INOPERATIVE A QXEAO OTHER O OTHER UKUNKNOWN 1 NM09357PH 504 SYMBOLOGY GENERATOR NR 1 WAS OPEN WHEN PERFORMING ORIGINATING CHECKLIST. MAINTENANCE RESET CIRCUIT BREAKER FOR NR 1 SYMBOLOGY GENERATOR. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050718000402005071800040WP 2005 7 18 UPS05844813 120050523A5315SK8408017575 FLOORBEAM DOUG DC8 DC873 302199CWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE:C3, MAIN CABIN FLOORBEAM, EXISTING REPAIR UNDER AREA HAS HEAVY CORROSION AT STA 940 RBL 65. REMOVED EXISTING 2 FLOORBEAM REPAIRS, 1 FILLER AND FLOORBEAM. FABRICATED AND INSTALLED FLOORBEAM AND 4 REPAIR ANGLES IAW EO DC8-53-20466 AND SAA SK840-807575. 2L74 4F RT4A25 20050718000422005071800042CE 2005 7 18 DJFA2005120 120050703A32301288200281 LANDING GEAR BEECH MU300 400A 1155402CE NLG UNWANTED DEPLOY E DJFAO OTHER O OTHER CRCRUISE 1 EA23749TA4844 RK149 WHILE IN CRUISE FLT AT FL 260 AT 300 KTS, NLG DROPPED OUT OF WW. CREW SLOWED A/C TO BELOW 200 KTS AND REQUESTED A LOWER ALT. L/G WAS CYCLED UP AND ALL GEAR REMAINED RETRACTED. A/C WAS LANDED W/O FURTHER INCIDENT. GEAR WAS INSPECTED FOLLOWING LANDING AND A GEAR DOOR FOUND TO BE TWISTED. MX REMOVED, RESEALED AND REINSTALLED NLG STRUT ASSY. UPLOCK RIGGING WAS CHECKED AND L/G LUBRICATED. PHASE I AND II INSPECTIONS WERE COMPLETED FOR A NLG AFTER OVERSPEED EXTENSION. NO FAULTS FOUND. NLG AFT DOOR ADJUSTED AND SEVERAL WORKING RIVETS REPLACED. 5 CYCLES OF L/G COMPLETED WITH NO NOTED DISCREPANCIES. A/C WAS RETURNED TO SERVICE. 2H72 4F RTA16SW 20050718000432005071800043GL 2005 7 18 2004606202005 120050620A3200302270302 PSEU BOMBDRBD700 BD7001A10 1390006GL LG MALFUNCTIONED E J7SAA UNSCHED LANDING EFJVIBRATION/BUFFET FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 SW05518FX 20046 AT 41,000 FT, 0.80 MACH, AMBER SPOILER FAULT ILLUMINATED. INBOARD SPOILER BOARDS 4 AND 5 AND INBD GRND SPOILERS DEPLOYED TO 1ST HASH MARK. AMBER AND AURAL WARNING GEAR DISAGREE ALERTED WITH GEAR MOVEMENT AND WHITE GEAR INDICATIONS. MAINTENANCE REPLACED PSEU, LANDING GEAR CONTROL PANEL, AND GEAR INDICATION SWITCH PER FSR REQUEST. GEAR SWINGS PERFORMED WITH NO DEFECTS NOTED. 2L72 4F RTT00003NY 20050718000442005071800044NM 2005 7 18 ASAA0510080 120050419A53106545785521 WINDOW FRAME BOEING737 737290C 138448VNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 YXX - FOUND LOWER AFT CORNER OF WINDOW FRAME CRACKED IN FASTENER HOLE AT BS 500A PLUS 15 INCHES RT. REPAIRED IAW ERO 3774 CRACK REMOVED ERO 3774 STEP 1.1. (M) 2L72 4F A16WE 20050718000462005071800046WP 2005 7 18 ASAA0580283 120050516A53209932816503 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02968AS 53016 OKC - DURING HV-CHECK, FOUND E3 FLOOR PANEL HAS A CRACKED SUPPORT. REMOVED DAMAGED SECTION. INSTALLED REPLACEMENT HAT CHANNEL SECTION AND SPLICE. (M) 2L72 4F RTA6WE 20050718000472005071800047EA 2005 7 18 548706022005 120050602A2120 UNKNOWN CNDAIRCL604 CL604 1900301EA COCKPIT ODOR E J7SABA EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW05330FX 5487 PILOT REPORTED DURING CLIMB-OUT, PASSING THROUGH FL260, SMELLED STRONG ELECTRICAL ODOR IN COCKPIT. ACCORDING TO PILOT, ODOR WOULD DISSIPATE THEN RETURN STRONG. RAN CHECKLIST AND SHUTOFF LT PACK AND ODOR APPEARED TO DISSIPATE. COPILOT THOUGHT HE SAW PILOTS MFD FLICKER DURING FLIGHT, PILOT DID NOT. EMERGENCY DECLARED. NO PAX ON BOARD ACFT AT TIME OF EMERGENCY. NO SMOKE IN CABIN/COCKPIT. ENGINE PERIMETERS ALL GOOD. NO CAS MESSEGE. ENGINE/APU FIRE BOTTLES NOT DISCHARGED. INSPECTED AND CLEANED COALESCER SOCKS, EFIS DISPLAYS, COOLING VENTS AND TRU COOLING VENTS. CLEANED SOCKS AND FAN SCREENS AND NO DEFECTS NOTED. UNABLE TO FIND CAUSE OF ODOR. 2L72 4F RTA21EA 20050718000482005071800048WP 2005 7 18 ASAA0580284 120050516A5320 CHANNEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02968AS 53016 OKC - FOUND DURING HV CHECK, LEFT OUTBOARD CABIN FLOOR PANEL AT STATION 465-541 HAS CRACKED HAT CHANNEL. REMOVED DAMAGED SECTION. INSTALLED REPLACEMENT HAT CHANNEL SECTION AND SPLICE. (M) 2L72 4F RTA6WE 20050718000512005071800051WP 2005 7 18 ASAA0580292 120050516A573059304973 SKIN DOUG DC9 DC983 3022083WP WING DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02968AS 53016 OKC - DURING HV-CHECK, FOUND LEFT ANTI-FLOAT TAB HAS A COMPOSITE REPAIR ON TRAILING EDGE, LOWER SURFACE IS DELAMINATING. REMOVED DAMAGE AND INSTALLED A REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050718000532005071800053NM 2005 7 18 ASAA0510132 120050613A531469414601 KEELBEAM BOEING737 737290C 138448VNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX - BS 727 LEFT KEEL BEAM FOUND CRACKED. REMOVED AND REPLACED KEEL BEAM IAW B737-200 SRM. (M) 2L72 4F A16WE 20050718000542005071800054NE 2005 7 18 ASMF200507006 220050708A7240PW2037 COMBUST CHAMBER BOEING757 757200 1384950NM PWA 2037 PW2037 NE LT ENGINE DAMAGED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23703AM3133513539 27203 726736 DURING LT ENGINE BOROSCOPIC INSPECTION, DETECTED COMBUSTION CHAMBER DAMAGED WITH 2 AXIAL CRACKS INTERSECTED WITH CIRCUMFERENTIAL CRACK OUT LIMITS. LT ENGINE REPLACED AND TESTED IAW MM 71-00-02 AND MM 71-00-00, RESPECTIVELY. ALL CORRECT. 2L72 4F4 FRTA2NM E17NE 20050718000552005071800055NM 2005 7 18 ASAA05400221 120050504A5340693535214 STRINGER CLIP BOEING737 737490 1384715NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02792AS 28887 PAE - FOUND STRINGER CLIP HAS 1 EXTRA HOLE. REMOVED AND REPLACED STRINGER CLIP. (M) 2L72 4F RTA16WE 20050718000582005071800058 2005 7 18 X6PA200500006 420050711A6113 BULKHEAD PIPER PA34 PA34200 7103405SO LYC O360 IO360C1E6 41514EA HARTZLHCC2Y HCC2YK2 GL PROP SPINNER CRACKED E X6PAK NONE O OTHER ININSP/MAINT 1 SO33152BW 347250187 L1164551A AU955 LT SPINNER BULKHEAD FOUND CRACKED, PIPER P/N 453-978. 1.5 IN CRACK EXTENDING FROM LAST SPINNER ATTACH FASTENER AT 10 O’CLOCK POSITION AND ANOTHER AT 2 O’CLOCK POSITION. BOTH CRACKS RUN INWARD TOWARD BULKHEAD/PROPELLER ATTACH POINT. 1L72 3O3 O A7SO 1E10 5 CP920 20050718000592005071800059CE 2005 7 18 71222 120050711A2750 FLAP SYSTEM BEECH 1900 1900D 1154162CE MALFUNCTIONED A AMWAAD UNSCHED LANDING RETURN TO BLOCK O OTHER CLCLIMB 1 CE07155YV 155YV AFTER TAKEOFF, CREW NOT ABLE TO RETRACT FLAPS TO ZERO. RETURNED TO FIELD AND LANDED SAFELY WITH NO FURTHER INCIDENT. STILL AWAITING MORE INFORMATION. 2L72 4T RTA24CE 20050718000602005071800060EU 2005 7 18 XN0A1246 120050708A5610 LATCH AIRBUS300 A300B4203 3930306EU CAPT SIDE WINDOWLACK OF LUBE A XN0AD RETURN TO BLOCK P NO WARNING INDICATION TXTAXI/GRND HDL 1 GL23474AS 219 CAPT SIDE WINDOW WILL NOT INDICATE CLOSED. LUBED LATCH PIN ON CAPT SLIDING WINDOW. OPS CHECK GOOD IAW A300 MM 56-12-11. 2L72 4F RTA35EU 20050718000612005071800061WP 2005 7 18 ASAA0580237 120050509A5320 CHANNEL DOUG DC9 DC983 3022083WP FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - FOUND DURING C-CHECK, CABIN FLOORBOARD HAT CHANNEL IS GOUGED. REMOVED AND REPLACED DAMAGED HAT CHANNEL. (M) 2L72 4F RTA6WE 20050718000632005071800063WP 2005 7 18 ASAA0580270 120050517A53009936639501 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - DURING C-CHECK, FOUND CABIN FLOORBOARD STATION 886 TO 946 RBL 22 TO LBL 22 HAS FIBER DAMAGE ON UPPER FACE AD TORN OUT INSERTS. REMOVED AND REPLACED FLOORBOARD. (M) 2L72 4F RTA6WE 20050718000662005071800066WP 2005 7 18 ASAA0580290 120050516A523059101419 SKIN DOUG DC9 DC983 3022083WP CARGO DOOR CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02968AS 53016 OKC - DURING HV CHECK, FOUND MID CARGO DOOR, AFT INBOARD SKIN NEAR DOOR HANDLE IS CHAFFED. REMOVED DAMAGE AND REPLACED WITH FILLER AND DOUBLER. (M) 2L72 4F RTA6WE 20050718000672005071800067WP 2005 7 18 ASAA0580291 120050516A5753591004242 SKIN DOUG DC9 DC983 3022083WP LT WING TE FLAP GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02968AS 53016 OKC - DURING HV CHECK, FOUND LEFT WING OUTBOARD FLAP VANE INBOARD LEADING EDGE IS GOUGED. REMOVED DAMAGE AND REPLACED WITH FILLER AND DOUBLER. (M) 2L72 4F RTA6WE 20050718000702005071800070WP 2005 7 18 ASAA0580249 120050509A53219936688503 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - DURING C-CHECK, FOUND RIGHT OVERWING FLOORBOARD AT STATION 807 IS DELAMINATED. REMOVED AND REPLACED FLOORBOARD. (M) 2L72 4F RTA6WE 20050718000712005071800071WP 2005 7 18 ASAA0580250 120050509A532199365831 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - DURING C-CHECK, FOUND OVERWING FLOORBOARD AT STATION 827 IS DELAMINATED. REMOVED AND REPLACED FLOORBOARD. (M) 2L72 4F RTA6WE 20050718000742005071800074NM 2005 7 18 ASAA0540174 120050312A5320654769015 SUPPORT BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02794AS 28889 PAE - AFT CARGO BAY, FLOOR TO SIDEWALL SUPPORT CORRODED. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT. (M) 2L72 4F RTA16WE 20050718000752005071800075NM 2005 7 18 ASAA0510082 120050420A531365622684 STRINGER BOEING737 737290C 138448VNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 YXX - NDT CRACK INDICATIONS AT FASTENERS HOLES ON STRINGER 19 LEFT, BS 460-480. CRACK REMOVED IAW B737-200 SRM 53-10-3 FIGURE 1. (M) 2L72 4F A16WE 20050718000762005071800076NM 2005 7 18 HNAA0500062 120050703A2910DSC252B40124 LINE DHAV DHC8 DHC8102 2809003NM NR 2 HYD SYS LEAKING A HNAAAD UNSCHED LANDING RETURN TO BLOCK K FLUID LOSS CLCLIMB 1 EA07328HA2265922659 281 WHEN GEAR SELECTED UP, NR 2 HYD ISO C.L. ILLUMINATED AND QUANTITY DROPPED TO 0.5 QTS. REMOVED AND REPLACED NOSE GEAR DRAG STRUT UP LINE. INSPECTED CASE DRAIN FILTER. NO CONTAMINATION FOUND. REPLACED NOSE LANDING GEAR DRAG STRUT "UP" LINE. 2H72 4T RTA13NM 20050718000772005071800077NM 2005 7 18 ASAA0510084 120050420A5313 STRINGER BOEING737 737290C 138448VNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 YXX - NDT CRACK INDICATION AT FASTENER HOLE BS 470, STRINGER 22L. REPAIRED AND REMOVED CRACK IAW B737-200 SRM 53-10-3 FIG 1. (M) 2L72 4F A16WE 20050718000782005071800078WP 2005 7 18 ASAA0580282 120050516A5320 CHANNEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAO OTHER O OTHER NRNOT REPORTED 1 NM02968AS 53016 OKC - DURING HV CHECK, E12 FLOOR PANEL HAS A CRACKED STIFFENER ON THE LOWER SIDE. REMOVED DAMAGED SECTION. INSTALLED REPLACEMENT HAT CHANNEL SECTION AND SPLICE. (M) 2L72 4F RTA6WE 20050718000792005071800079NM 2005 7 18 ASAA0540173 120050311A5320654769020 SUPPORT BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02794AS 28889 PAE - AFT CARGO BAY, FLOOR TO SIDEWALL SUPPORT AT BS 930-947, RBL 23 HAS CORROSION AT NUTPLATE LOCATIONS. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT AT BS 930-947, RBL 23. (M) 2L72 4F RTA16WE 20050718000802005071800080WP 2005 7 18 ASAA0580274 120050516A5320993053811 CUSP WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02968AS 53016 OKC - DURING HV-CHECK, FOUND LEFT CUSP WEB CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050718000812005071800081NM 2005 7 18 ASAA0540248 120050512A5320654795731 SUPPORT BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02705AS 29318 PAE - AFT CARGO BAY, FRAME TO FLOOR TO SIDEWALL SUPPORT PLATE CORRODED. REMOVED FABRICATED AND INSTALLED NEW SUPPORT PLATE PER SRM. (M) 2L72 4F RTA16WE 20050718000852005071800085NM 2005 7 18 ASAA0510086 120050420A5320654659212 CHANNEL BOEING737 737290C 138448VNM FS CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 YXX - AFT CARGO PIT FLOOR SUPPORT CHANNEL ANCHOR NUT HOLES HAVE CORROSION AT BS 847 PLUS 15 INCHES RBL 8. AFT CARGO PIT FLOOR SUPPORT CHANNEL ANCHOR NUT HOLES CORROSION REMOVED AT BS 847 PLUS 15 INCHES RBL 8 PER B737-200 SRM 53-10-5 FIG 5. (M) 2L72 4F A16WE 20050718000862005071800086NM 2005 7 18 ASAA0510087 120050420A5330654577646 SKIN BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 YXX - AROUND CARGO SKIN AT STRINGER 27L BS 817-837 CORROSION FOUND UPON REMOVAL OF STRINGER. CORROSION REMOVED IAW B737-200 SRM 53-30-3 FIG 48. (M) 2L72 4F A16WE 20050718000882005071800088WP 2005 7 18 ASAA0580174 120050404A532199365841 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE BROKEN A ASAAK NONE O OTHER ININSP/MAINT 1 NM02950AS 53023 OKC - FOUND DURING C-CHECK, CABIN FLOOR PANEL BROKEN. REPLACED PANEL. (M) 2L72 4F RTA6WE 20050718000892005071800089WP 2005 7 18 ASAA0580175 120050404A53219936582503 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02950AS 53023 OKC - FOUND DURING C-CHECK, CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL. (M) 2L72 4F RTA6WE 20050718000902005071800090WP 2005 7 18 ASAA0580177 120050404A53219936651515 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02950AS 53023 OKC - FOUND DURING C-CHECK, CABIN FLOOR PANEL PUNCTURED. REPLACED PANEL. (M) 2L72 4F RTA6WE 20050718000912005071800091NM 2005 7 18 ASAA0540247 120050512A5340654795724 BRACKET BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02705AS 29318 PAE - FOUND AFT CARGO BAY, FRAME TO FLOOR TO SIDEWALL SUPPORT BRACKET CORRODED. FABRICATED AND INSTALLED NEW SIDEWALL SUPPORT BRACKET PER SRM. (M) 2L72 4F RTA16WE 20050718000922005071800092NM 2005 7 18 ASAA0540167 120050313A5340693532Y1 STRINGER CLIP BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02764AS 25101 OKC - FOUND RIGHT STRINGER 12R AT BS 1007 STRINGER CLIP IS CRACKED. REMOVED DAMAGED STRINGER CLIP, ORDERED AND INSTALLED A NEW STRINGER CLIP IAW B737 SRM. (M) 2L72 4F RTA16WE 20050718000932005071800093NM 2005 7 18 ASAA0540169 120050311A524165535954 SEAL DEPRESSOR BOEING737 737490 1384715NM GALLEY DOOR CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02791AS 28886 PAE - FORWARD GALLEY DOOR CUTOUT UPPER SEAL DEPRESSOR IS CRACKED. REPLACED SEAL DEPRESSOR. (M) 2L72 4F RTA16WE 20050718000942005071800094WP 2005 7 18 ASAA0580185 120050404A532199366401 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02950AS 53023 OKC - FOUND DURING C-CHECK, CABIN FLOOR PANEL HAS SEVERAL DELAMINATED EDGES. REPLACED PANEL. (M) 2L72 4F RTA6WE 20050718000952005071800095NM 2005 7 18 ASAA0540216 120050501A5240 GUIDE ARM BOEING737 7374Q8 138447QNM L1 DOOR OUT OF ADJUST A ASAAK NONE O OTHER ININSP/MAINT 1 NM02756AS 25097 SEA - L1 DOOR IS DIFFICULT TO CLOSE. ADJUSTED GUIDE ARM. (M) 2L72 4F RTA16WE 20050718000962005071800096NM 2005 7 18 ASAA0540188 120050317A53136552928166 STRINGER BOEING737 737490 1384715NM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02794AS 28889 PAE - FOUND STRINGER IS GOUGED AT AFT CARGO BAY. REMOVED DAMAGED SECTION OF STRINGER, FABRICATED REPAIR PARTS AND INSTALLED. (M) 2L72 4F RTA16WE 20050718000992005071800099WP 2005 7 18 ASAA0580192 120050404A5320 CHANNEL DOUG DC9 DC983 3022083WP FUSLEAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02950AS 53023 OKC - FOUND DURING C-CHECK, CABIN FLOOR PANEL HAT CHANNEL IS CRACKED, 3 PLACES. REPLACED HAT CHANNEL. (M) 2L72 4F RTA6WE 20050718001052005071800105NM 2005 7 18 ASAA0540170 120050311A52416552870501 SEAL DEPRESSOR BOEING737 737490 1384715NM GALLEY DOOR CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02791AS 28886 PAE - FOUND CORROSION ON AFT GALLEY DOOR SEAL DEPRESSOR UPPER FORWARD STATION 959. REPLACED SEAL DEPRESSOR. (M) 2L72 4F RTA16WE 20050718001072005071800107WP 2005 7 18 ASAA0580186 120050404A532099579162 CHANNEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02950AS 53023 OKC - FOUND DURING C-CHECK, FLOOR PANEL HAT CHANNEL BENT AND CRACKED. REPLACED DAMAGED HAT CHANNEL SECTION. (M) 2L72 4F RTA6WE 20050718001092005071800109WP 2005 7 18 ASAA0580225 120050509A53219936547503 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - FOUND DURING C-CHECK, CABIN FLOORBOARD IS DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050718001102005071800110WP 2005 7 18 ASAA0580229 120050509A532199365371 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - FOUND DURING C-CHECK, CABIN FLOORBOARD IS DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050718001112005071800111WP 2005 7 18 ASAA0580232 120050509A532199366541 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - FOUND DURING C-CHECK, CABIN FLOORBOARD IS DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050714000752005071400075SO 2005 7 14 C2XA05SH059 120050630A532014521713005 BEAM EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716961 145103 CENTER OMEGA BEAM CORROSION AT FS 20. MAINTENANCE REMOVE AND REPLACED CENTER OMEGA BEAM AT FS 18-23 IAW EMB SRM 51-40-02. AIRCRAFT APPROVED TO RETURNED FOR SERVICE. 2L72 4F RTT00011AT 20050714000802005071400080NM 2005 7 14 HNAA0500061 120050630A2611473054 SMOKE DETECTOR DHAV DHC8 DHC8101 2809002NM CARGO BAY INTERMITTENT A HNAAO OTHER JN WARNING INDICATION FALSE WARNING CRCRUISE 1 EA07827EX2672826728 390 INTERMITTENT SMOKE WARNING IN FLIGHT. REMOVED AND REPLACED CARGO BAY SMOKE DETECTORS. 2H72 4T RTA13NM 20050714000822005071400082NM 2005 7 14 UPS05444798 120050621A5320BAC1505100312 FLANGE BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 BS 910 RBL 11-33 LATERAL HAT SECTION FWD FLANGE FOUND CRACKED. CORROSION BLEND OUT 0.020 BY 1.0 BY 1.5 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, LATERAL HAT SECTION REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050714001282005071400128 2005 7 14 SWAA052014 420050711A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050714001382005071400138NM 2005 7 14 SWAA052024 120050710A53306545774 SKIN BOEING737 7373TO 138447GNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29697SW 23838 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 18L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050714001422005071400142NM 2005 7 14 ASAA0510117 120050531A53146546547109 KEELBEAM BOEING737 737290C 138448VNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 B-STA 727 BETWEEN LT AND RT KEELBEAM SUPPORT ANGLE FOUND CRACKED. SUPPORT ANGLE REPLACED. (K) 2L72 4F A16WE 20050714001442005071400144NM 2005 7 14 ASAA0510103 120050527A531465621252 KEELBEAM BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 KEELBEAM AT B-STA 648-662 RT LOWER SECTION CORROSION FOUND AT UPPER GATE. REPLACED KEELBEAM. (K) 2L72 4F4 F A16WE E2EA 20050714001492005071400149NM 2005 7 14 ASAA0510100 120050519A5315654659210 FLOORBEAM BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 AFT CARGO FLOOR SUPPORT BEAM ANCHOR NUTS HOLES HAS CORROSION AFT OF B-STA 767, RBL 3. AFT CARGO PIT FLOOR SUPPORT BEAM AFT OF B-STA 767, RBL 3 REPAIRED WITH FABRICATED REPAIR PARTS. (K) 2L72 4F4 F A16WE E2EA 20050714001572005071400157NM 2005 7 14 ASAA0510108 120050530A5313654577542 STRINGER BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 STRINGER CRACKED AT B-STA 868, STR 25R. REPAIRED IAW SRM WITH MADE REPAIR PARTS. (K) 2L72 4F4 F A16WE E2EA 20050714001612005071400161EA 2005 7 14 COMA0560378 120050704A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01981CA132341550 7163 FLAPS FAIL CAUTION. REPLACED LT BPSU. 2L72 4F RTA21EA 20050714001622005071400162EA 2005 7 14 COMA0570078 120050705A532067053110521 WEB CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01317CA7613 10055 FS 280 BULKHEAD LOWER WEBS CORRODED BEYOND LIMITS FROM LBL 36 TO RBL 36. REPLACED FS 280 BULKHEAD LOWER WEBS IAW BOMBARDIER REO 670-53-11-052 REV A REPAIR 2. 2L72 4F RTA21EA 20050714001692005071400169EA 2005 7 14 COMA0560380 120050704A7910 OIL TANK CNDAIRCL600 CL6002B19 1900309EA ENG OIL SYS OVERSERVICED A COMAEA ENGINE SHUTDOWN UNSCHED LANDING JW WARNING INDICATION INADEQUATE Q C CRCRUISE 1 SO01819CA 7415 RECEIVED RT ENGINE HIGH OIL TEMP WARNING. CREW DECLARED EMERGENCY. PERFORMED AN I.F.S.D. AND LANDED WITHOUT INCIDENT. ENGINE OIL OVERSERVICED. REMOVED 5 QTS OF OIL. NO OTHER DEFECTS NOTED. 2L72 4F RTA21EA 20050714001712005071400171EA 2005 7 14 VTZA200500129 120050706A53206013501219 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27662BR 7526 INTERCOSTAL ON AFT SIDE OF FS 621 LT SIDE AT STRINGER 14 CRACKED .854 IN. 2L72 4F RTA21EA 20050714001732005071400173NM 2005 7 14 ASAA0510175 120050614A534069353521 STRINGER CLIP BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 AFT CARGO B-STA 747, STR 21L TIE CLIP CORRODED. REMOVED AND REPLACED TIE CLIP IAW SRM. (K) 2L72 4F4 F A16WE E2EA 20050714001742005071400174NM 2005 7 14 ASAA0510130 120050613A53156554907501 FLOORBEAM BOEING737 737290C 138448VNM PWA JT8 JT8D217 52053NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 CORROSION ON FLOORBEAM AT B-STA 727B, RBL 10-21. CORROSION REPAIRED IAW SRM. (K) 2L72 4F4 F A16WE E9NE 20050714001872005071400187NM 2005 7 14 ASAA0510178 120050614A5330654576989 SKIN BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 FUSELAGE SKIN BULGING AT BS 535, STR 28 LT KEELBEAM. KEELBEAM REPLACED AND SKIN REPAIRED. (K) 2L72 4F4 F A16WE E2EA 20050714002002005071400200EU 2005 7 14 05FDEA01853 120050707A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25656FE16517 745 SEAT TRACK HAS CORROSION FS 40 3, RBL 37.5 SEAT TRACK. FABRICATED ON TRAVELER NR T5/529929 W/O 29203 NR N00439. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-10-16 FIG 201. 2L72 4F RTA35EU 20050714002012005071400201EA 2005 7 14 SWIA200515220 120050706A274270745 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07748SK 10203 STAB CH 1 INOP STATUS MSG AT FL390. REPLACED HORIZONTAL STAB MOTOR CONTROL UNIT IAW 27-42-07, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050714002062005071400206EA 2005 7 14 SWIA200515225 120050701A2740 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA COCKPIT INTERMITTENT A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07407SW 7034 FOS PITCH TRIM SWITCH INTERMITTENT. REPLACED SWITCH IAW 27-41-05. OPERATIONAL CHECK IAW 27-41-15 GOOD. 2L72 4F RTA21EA 20050714002182005071400218EA 2005 7 14 SWIA200515237 120050702A3350 BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSDISCHARGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07426SW 7468 CEILING LEVEL EMERGENCY FLOOD LIGHTS INOP. REPLACED FORWARD EMERGENCY BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050714002212005071400221SO 2005 7 14 SWIA200515240 120050701A3350 RELAY EMB 120 EMB120ER 3260203SO EMERGENCY LIGHTSMALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07565SW 120340 EMERGENCY LIGHTS WILL NOT TURN OFF. INSTALLED NEW K0201 RELAY. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050715000112005071500011 2005 7 15 SWIA200515217 420050630A2220 SWITCH CNDAIRCL600 CL6002B19 1900309EA AUTOPILOT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED DEDESCENT 1 NM07923SW 7664 ON DESCENT AUTOPILOT ON STAB/MACH TRIM 1 AND 2 AND DISCONNECTED. REPLACED CAPT STAB DISCONNECT SWITCH IAW CRJ MM27-41-30. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050715000132005071500013NM 2005 7 15 ASA0510184 120050614A53106547959502 DOOR FRAME BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 DOOR FRAME ON FUSELAGE IS CRACKED (AFT END FWD FRAME. REPLACED IAW SRM. (K) 2L72 4F4 F A16WE E2EA 20050715000152005071500015NM 2005 7 15 AWXA200500773 120050701A21337110033 OUTFLOW VALVE BOEING737 7373G7 1384595NM MALFUNCTIONED A AWXAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 WP28311AW4558610107 24712 CREW REPORTED SMOKE IN CABIN. MX INSP ACFT & FOUND SMOKE COMING FROM SHORTED WIRES JUST BEHIND WALL IN AFT CARGO BAY. FOUND OUTFLOW VALVE DC MOTOR BAD. MX R & R OUTFLOW VALVE. DAMAGED WIRING REPAIRED IAW MM & WIRING DIAGRAM. CABIN PRESSURE CONTROLLER REPLACED FOR POPPING DC MOTOR C/B AND HEATER C/B. OVERHEAD PRESSURE CONTROL PANEL ALSO REPLACED FOR PRECAUTIONARY REASONS IAW MM. OPS CHKS GOOD. TEAR DOWN REPORT OF OUTFLOW VALVE SHOWS AC MOTOR & GEARBOX NOISY & SLUGHISH, SAME WITH DC MOTOR. BEARING FOUND DRY & BINDING. UNIT OVERHAULED IAW CMM, TEAR DOWN OF PRESSURE CONTROLLER SHOWS SHORTED COMPONENTS. UNIT REPAIRED IAW CMM. TEAR DOWN OF PRESSURE CONTROL PANEL SHOWS NO FAULTS. UNIT TESTED IAW CMM. 2L72 4F RTA16WE 20050715000162005071500016NM 2005 7 15 SWAA052029 120050711A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E + 15, STR 18R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050715000202005071500020NM 2005 7 15 SWAA052033 120050712A335065C27093 LIGHT BOEING737 7377H4 1384404NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29739GB 29275 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20050715000332005071500033EA 2005 7 15 A6WA200540223 120050625A5210 DRAG ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31419AW 7633 PAX DOOR AFT DRAG ANGLE CRACKED NEAR UPPER SUPPORT PULLEY. REPAIRED AFT DRAG ANGLE BY REMOVING DAMAGE, PERFORMED EDDY CURRENT INSPECTION, FABRICATED AND INSTALLED REPAIR PIECES IAW REO. (K) 2L72 4F4 FRTA21EA E15NE 20050715000342005071500034NM 2005 7 15 AALA20050426 120050706A3350 CONNECTOR BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21352AA 24033 SFO - EMERGENCY LIGHT AT SEATS 39AB INOPERATIVE. REPAIRED CONNECTOR AT SEAT 39A FOR EMERGENCY LIGHTS AT SEATS 39AB. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050715000352005071500035WP 2005 7 15 AALA20050425 120050706A3220 O-RING DOUG DC9 DC983 3022083WP SCHRADER VALVE LEAKING A AALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW21438AA 49456 STL INFLIGHT T0456/6JUL - NOSE GEAR WILL NOT RETRACT. RED LIGHT REMAINED ON AFTER GEAR RETRACTION. FOUND NOSE STRUT FLAT. SERVICED NOSE STRUT AFTER REPLACING SCHRADER VALVE O-RING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050715000372005071500037NM 2005 7 15 05FDEA01820 120050707A5753 STRUCTURE DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 LT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. REPAIR CARRIED OUT AS PER EA1-5750-87587. 2L73 4F RTA22WE 20050715000412005071500041NM 2005 7 15 05FDEA01825 120050707A5753 STRUCTURE DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 LT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. SUPPORT BRACKET REPAIRED AS PER EA1-5750-87587 LT OUTBD FLAP INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20050715000462005071500046NM 2005 7 15 05FDEA01834 120050707A5753 STRUCTURE DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 LT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. 2L73 4F RTA22WE 20050715000532005071500053NM 2005 7 15 UPS05444808 120050622A5310 STRUCTURE BOEING747 747123F NM AFT CARGO BAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C. AFT CARGO - STA 1580 RBL 7 FRAME UPPER CHORD JUST UNDER ROLLER TRACK FOUND CRACKED. CRACK LENGTH 0.75. AFT CARGO BAY BS 1580 LBL 16 TO RBL 16 FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 2. 2L74 4F A20WE 20050715000542005071500054NM 2005 7 15 UPS05444809 120050622A5315 FLOORBEAM BOEING747 747123F NM AFT CARGO DEFORMED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C . AFT CARGO - STA 1580 BL 0 FRAME UPPER CHORD DEFORMED. AFT CARGO BAY, BS 1580 LBL 16 TO RBL 16 FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 2 REF NRC NR 6699. 2L74 4F A20WE 20050715000572005071500057NM 2005 7 15 UPS05444814 120050617A5311 FRAME BOEING747 747123F NM FWD CARGO CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C. FWD CARGO, FRAME AT BS 880 STR 34L FOUND UPPER CHORD CRACKED, CRACK LENGTH 1.875 IN. FRAME REPAIRED AS PER SRM 53-10-04 FIG 52. 2L74 4F A20WE 20050715000632005071500063NM 2005 7 15 UPS05444820 120050621A5347 SEAT TRACK BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C. U/D, BS 520 TO 600 RBL 10 SEAT TRACK CROWN AND FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.045 BY 0.5 BY 2.75 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, U/D SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 4 AT BS 520 TO 610 RBL 10 INCH AREA. 2L74 4F A20WE 20050715000692005071500069CE 2005 7 15 DELA200500008 120050709A7500460200 SEAL LEAR 55 55LEAR 5170702CE BLEED AIR SYS LEAKING E DELAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03550HG 083 RIGHT ENGINE FIRE TEE HANDLE ILLUMINATED DURING CLIMB OUT. AFM PROCEDURE FOLLOWED. POWER LEVER PLACED TO IDLE AND FIRE LIGHT EXTINGUISHED. REPLACED RIGHT PYLON BLEED AIR SEALS. GROUND AND FLIGHT CHECKED SATISFACTORY. 2L72 4F A10CE 20050715000782005071500078SO 2005 7 15 SIMA200516401 120050611A3397 WIRE EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL AC INVERTER BROKEN A SIMAO OTHER O OTHER NRNOT REPORTED 1 SW21737MW 145396 EMERGENCY EXIT LIGHT JUST AFT OF GALLERY FAILS TO ILLUMINATE. REPAIRED BROKEN WIRE ON NR 2 AC TO AC INVERTER CONNECTOR PLUG IAW SRM. OPS CHECK GOOD IAW MM. AC RETURNED TO SERVICE. (K) 2L72 4F4 FRTT00011ATTE6CH 20050715000982005071500098NM 2005 7 15 UPS05444870 120050630A5711 SPAR BOEING747 747123 1384873NM LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE: C, LT WING REAR SPAR UPPER CHORD HORIZONTAL FLANGE FWD FASTENER HOLE AT WS 392 CRACK RUNNING AFT APPROX 0.080 INCH. LEFT WING REAR SPAR UPPER CHORD HORIZONTAL FLANGE FWD FASTENER HOLE REPAIRED AT WS 392 AREA AS PER HX RS R57-25-35337 & UPS EO B747-5730-22494-A. 2L74 4F A20WE 20050715001312005071500131NM 2005 7 15 UPS05M44875 120050710A3240 VALVE DOUG MD11 MD11F 3023600NM NR 3 BRAKE SYS FAILED A IPXAO OTHER O OTHER LDLANDING 1 SO01252UP 48768 ANTI SKID R FAIL W/SUBSEQUENT DEACTIVATION OF NR 3 BRAKE. LANDING ROLL REQUIRED EXCESSIVE BRAILING WITH SHUDDER FAVORING RIGHT SIDE. REMOVED AND REPLACED NR 3 BRAKE SYS A/S VLV. PERFORMED ANTI SKID SYS OPS TEST ON 10 BRAKES BOTH SYS. A/S TEST NORMAL. 2L73 4F RTA22WE 20050715001802005071500180SO 2005 7 15 C2XA05SH066 120050706A532014530627001 FLOOR SUPPORT EMB 145 EMB145 3260210SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716961 145103 DURING C-CHECK, MAINTENANCE FOUND LT OMEGA BEAM HAS CORROSION FROM FRAME 23 TO JUST AFT OF FRAME 29. MAINTENANCE REPAIRED LT OMEGA BEAM AT FRAME 29 IAWEC 5320-01242. AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2L72 4F RTT00011AT 20050715001832005071500183NM 2005 7 15 CALA0500215 120050710A5315BAC1506210 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714334 23572 INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 967, RBL 38 TO LBL 0. REPLACED FLOORBEAM UPPER CHORD IAW ECRA 5311-01231. 2L72 4F RTA16WE 20050718000282005071800028NM 2005 7 18 ASAA0540218 120050504A5340654587514 ANGLE BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02792AS 28887 PAE - FOUND CORROSION ON GALLEY DOOR THRESHOLD SUPPORT ZEE ANGLE. REMOVED AND REPLACED ZEE ANGLE. (M) 2L72 4F RTA16WE 20050718000412005071800041 2005 7 18 BB05050 420050710A2565140N27669 LOCK BOEING757 757225 1384959NM ESCAPE SLIDE MISSING A USAAK NONE O OTHER ININSP/MAINT 1 EA19605AU 22201 PRIOR TO FLIGHT, CREW FOUND DOOR 1R SLIDE BUSTLE PARTIALLY OPEN AND GIRT DISLODGED. MAINTENANCE REPLACED AFT BAR LOCK AND INSTALLED SLIDE BUSTLE. OK FOR SERVICE. 2L72 4F RTA2NM 20050718000652005071800065EU 2005 7 18 XN0A1247 120050712A2780 SLAT AIRBUS300 A300B4203 3930306EU LE SLAT CONTROL OUT OF ADJUST A XN0AD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL23372PC 196 DURING TAXI, OUT SLATS WOULD NOT EXTEND. ADJUSTED SLAT ASSY APU IAW A300 AMM 27-83-00. OPS CHECK GOOD IAW A300 AMM 27-83-00. 2L72 4F RTA35EU 20050718001012005071800101NM 2005 7 18 HNAA0500067 120050711A771210167N02W00 INDICATOR DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE NR 1 ENGINE INOPERATIVE A HNAAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 EA07816EX3298732987 329 NO TORQUE INDICATION ON NR 1 ENGINE. REMOVED AND REPLACED TORQUE INDICATOR. 2H72 4T4 TRTA13NM E20NE 20050718001032005071800103NM 2005 7 18 ASAA0510005 120050222A335086210144 BATTERY PACK BOEING737 7372X6C 1384552NM RT OVERWING EXITINOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM02746AS 23123 ANC - FOUND RIGHT OVERWING EXIT SIGN INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. (M) 2L72 4F RTA16WE 20050718001122005071800112WP 2005 7 18 ASAA0580203 120050404A5230 STRUCTURE DOUG DC9 DC983 3022083WP CARGO DOOR CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02950AS 53023 OKC - DURING C-CHECK, FOUND FORWARD CARGO BAY DOOR LOWER FORWARD CORNER IS CHAFED. REMOVED DAMAGE. TREATED AND PRIMED PER EA 52-30-01260. (M) 2L72 4F RTA6WE 20050718001132005071800113WP 2005 7 18 ASAA0580205 120050330A552359304973 TAB DOUG DC9 DC983 3022083WP RT ELEVATOR DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02950AS 53023 OKC - FOUND DURING C-CHECK, RIGHT ELEVATOR ANTI-FLOAT TAB IS DELAMINATED. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLERS AND DOUBLERS. (M) 2L72 4F RTA6WE 20050810002332005081000233WP 2005 8 10 ASAA0580236 120050509A5320993061221 CUSP WEB DOUG DC9 DC983 3022083WP FS 1174-1250 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02968AS 53016 OKC - DURING C-CHECK, FOUND CABIN FLOOR CUSP WEB IS CORRODED. REMOVED DAMAGE AND INSTALLED DOUBLER. (M) 2L72 4F RTA6WE 20050718001152005071800115WP 2005 7 18 ASAA0580238 120050509A5320 CHANNEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - FOUND DURING C-CHECK, CABIN FLOORBOARD HAT CHANNEL IS CRACKED. REMOVED AND REPLACED DAMAGED HAT CHANNEL. (M) 2L72 4F RTA6WE 20050718001162005071800116WP 2005 7 18 ASAA0580176 120050404A53219936651515 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02950AS 53023 OKC - FOUND DURING C-CHECK, FLOOR PANEL DELAMINATED. REPLACED PANEL. (M) 2L72 4F RTA6WE 20050718001172005071800117NM 2005 7 18 ASAA0510131 120050613A5314 KEELBEAM BOEING737 737290C 138448VNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX - BS 727 RT KEELBEAM FOUND CRACKED. REMOVED AND REPLACED KEEL BEAM IAW B737-200 SRM. (M) 2L72 4F A16WE 20050718001182005071800118NM 2005 7 18 ASAA0510133 120050613A575369786651 RAMP BOEING737 737290C 138448VNM TE FLAP DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX - LEFT WING OUTBOARD FORE FLAP OUTBOARD RAMP DAMAGED. LEFT WING OUTBOARD FORE FLAP OUTBOARD RAMP REPLACED WITH NEW PART PER IAW B737-200 SRM. (M) 2L72 4F A16WE 20050718001192005071800119NM 2005 7 18 HNAA0500064 120050707A6120MS3474L2255S CONNECTOR DHAV DHC8 DHC8201 2809001NM PWA PW120 PW123 NE HAMSTD14SF 14SF23 NE PROP CONTROL SYSSHORTED A HNAAE ENGINE SHUTDOWN O OTHER CLCLIMB 1 EA07969HA1471814718 468 NR 2 ENGINE AUTO FEATHERED AT 1000 FT AGL ON TAKEOFF. MAX TQ REACHED WAS 114 PERCENT. REPLACED CONNECTOR 9811-J14. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20050718001202005071800120SO 2005 7 18 SWIA200515242 120050701A27523431001001 ACTUATOR EMB 120 EMB120ER 3260203SO NACELLE FLAP MALFUNCTIONED A SWIAO OTHER FKJFLT CONT AFFECTED FLUID LOSS WARNING INDICATION APAPPROACH 1 NM07292UX9446 9446 120292 ON APPROACH, FLAP DISAGREEMENT. REPLACED LT NACELLE FLAP ACTUATOR. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050718001212005071800121EA 2005 7 18 SWIA200515243 120050706A5210 COUNTERBALANCE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR OUT OF RIG A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07590SW 7077 PAX DOOR SLOW TO OPEN. ADJUSTED AND RIGGED PAX DOOR COUNTER BALANCE SYSTEM IAW MM 52-11-17. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050718001222005071800122EA 2005 7 18 SWIA200515244 120050630A2720 TRANSMITTER CNDAIRCL600 CL6002B19 1900309EA RUDDER CONTROL MALFUNCTIONED A SWIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM07455SW 7760 ON PUSHBACK LOST RUDDER INDICATION ON EICAS. REPLACED RUDDER POSITION CONTROL TRANSMITTER IAW MM 27-24-05 OF THE MAINTENANCE MANUAL. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050718001242005071800124EA 2005 7 18 SWIA200515246 120050703A27507805013 CONTROL LEVER CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07403SW1187 1187 7028 FLAPS FAIL CAUTION MESSAGE. REPLACED CONTROL LEVER IAW 27-51-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050718001252005071800125SO 2005 7 18 SWIA200515247 120050705A3397 WIRE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHTSBROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07250YV 120250 ONE FLOOR EMERGENCY LIGHT INOP AT ROW 9. REPAIRED WIRE TO FLOOR LIGHT AT ROW 9. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050718001292005071800129WP 2005 7 18 ASAA0580243 120050509A5310591008517 DOOR FRAME DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - FOUND DURING C-CHECK, FORWARD ENTRY DOOR LEFT DOOR FRAME LOWER FINGER CRACKED. REMOVED DAMAGE INSTALLED FILLER AND DOUBLER. (M) 2L72 4F RTA6WE 20050718001312005071800131WP 2005 7 18 ASAA0580188 120050404A532099579185 CHANNEL DOUG DC9 DC983 3022083WP FLOOR PANEL CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02950AS 53023 OKC - FOUND DURING C-CHECK, CABIN FLOOR PANEL HAT CHANNEL IS CHAFED. REPLACED DAMAGED HAT CHANNEL. (M) 2L72 4F RTA6WE 20050718001322005071800132WP 2005 7 18 ASAA0580190 120050404A53219936651505 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02950AS 53023 OKC - FOUND DURING C-CHECK, CABIN FLOOR PANEL IS DELAMINATED. REPLACED PANEL. (M) 2L72 4F RTA6WE 20050718001332005071800133WP 2005 7 18 ASAA0580193 120050404A5320993663913 CHANNEL DOUG DC9 DC983 3022083WP FLOOR PANEL CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02950AS 53023 OKC - FOUND DURING C-CHECK, CABIN FLOOR PANEL HAT CHANNEL IS CRACKED. REPLACED HAT CHANNEL. (M) 2L72 4F RTA6WE 20050718001352005071800135NM 2005 7 18 ASAA0540217 120050504A534065B783930 SUPPORT FITTING BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02792AS 28887 PAE - FOUND CORROSION ON LOWER SUPPORT FITTING. REMOVED AND REPLACED FITTING. (M) 2L72 4F RTA16WE 20050718001372005071800137NM 2005 7 18 ASAA0540176 120050313A5320655384422 FLOOR SUPPORT BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02794AS 28889 PAE - FOUND AFT CARGO BAY, FLOOR SUPPORT CORRODED AT BS 794 TO 847. REMOVED AND REPLACED FLOOR SUPPORT. (M) 2L72 4F RTA16WE 20050718001402005071800140EA 2005 7 18 SWIA200515248 120050704A2731 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA ELEVATOR MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07936SW 7726 CAPT ELEVATOR TRIM INOP. REPLACED ELEVATOR TRIM SWITCH IAW 27-41-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050718001412005071800141NM 2005 7 18 SB05081 120050711A523010608211 DOOR SEAL BOEING737 737301 1384611NM FWD CARGO DOOR OUT OF POSITION A USAABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19353US 23556 DURING CRUISE, AT APPROX FL320, CABIN PRESSURE WENT TO 10,000 FT WITH CABIN ALT WARNING HORN SOUNDING. CREW ACCOMP EMERGENCY DESCENT TO 10,000 FT AND RETURNED TO FIELD. FLT LANDED W/O FURTHER INCIDENT. NO OXYGEN MASKS WERE DEPLOYED. FLT WAS MX FERRIED FOR MX, FOUND FWD CARGO DOOR SEAL SECTION OUT OF ITS RETAINER APPROX 8 INCHES. REINSTALLED LOOSE SEAL SECTION IN RETAINER. PERFORMED OPS TEST OF PRESSURIZATION CONTROL SYSTEM PER MM 21-31-00. OPS TEST GOOD. ALSO, PRESSURIZED A/C AND LEAK CHECKED DOORS AND WINDOWS PER PCI 2897, JOB CARD J321-00-01. LEAK CHECK GOOD. A/C OK FOR SERVICE. 2L72 4F RTA16WE 20050718001422005071800142WP 2005 7 18 MWEA050068 120050708A2150 ACM DOUG DC9 DC982 3022082WP CABIN SMOKE A MWEAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL31809ME 48071 CREW REPORTED HAZE IN CABIN AND BOTH AFT LAVATORY SMOKE DETECTORS ANNUNCIATED. AIR CYCLE MACHINE (ACM) OIL OVER-SERVICED. SUSPECT ACM OIL BURNED OFF IN GASEOUS STATE. IN ADDITION, REMOVED AND REPLACED WATER SEPARATOR SOCKS. COMPLIED WITH CARRY-OVER C1034 TO INSPECT CONTRACTED LABOR CORRECTIVE ACTION. 2L72 4F A6WE 20050718001452005071800145WP 2005 7 18 ASAA0580196 120050404A5330 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02950AS 53023 OKC - FOUND DURING C-CHECK, FUSELAGE SKIN DENTED. REPLACED DAMAGED SECTION USING FINGER DOUBLER, STRAPS, AND DOUBLERS. (M) 2L72 4F RTA6WE 20050718001462005071800146WP 2005 7 18 ASAA0580178 120050404A532199365841 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02950AS 53023 OKC - FOUND DURING C-CHECK, CABIN FLOOR PANEL PUNCTURED. REPLACED PANEL. (M) 2L72 4F RTA6WE 20050718001482005071800148NM 2005 7 18 ASAA0510079 120050419A53306561252 DOUBLER BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 YXX - UPON REMOVAL OF PREVIOUS REPAIR AT BS 500B PLUS 17 INCHES CORROSION ON RT KEEL BEAM AT BS 535. REPAIRED IAW ERO 3838 AND 3846 AND EA 5310-02458. CORROSION REMOVED IAW ERO 3838 STEP 1.1 PARA 74. (M) 2L72 4F A16WE 20050718001492005071800149WP 2005 7 18 ASAA0580181 120050404A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02950AS 53023 OKC - FOUND DURING C-CHECK, CABIN FLOOR PANEL HAS PULLED RIVETS AND CRACKED SKIN. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER AND FILLER. (M) 2L72 4F RTA6WE 20050718001512005071800151WP 2005 7 18 ASAA0580179 120050404A532199366881 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02950AS 53023 OKC - FOUND DURING C-CHECK, CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL. (M) 2L72 4F RTA6WE 20050718001522005071800152WP 2005 7 18 ASAA0580180 120050404A532199365821 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02950AS 53023 OKC - FOUND DURING C-CHECK, CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL. (M) 2L72 4F RTA6WE 20050718001532005071800153WP 2005 7 18 ASAA0580239 120050509A53219936584501 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - DURING C-CHECK, FOUND CABIN FLOORBOARD DELAMINATED. REMOVED AND REPLACED FLOORBOARD. (M) 2L72 4F RTA6WE 20050718001542005071800154WP 2005 7 18 ASAA0580245 120050509A5330 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - FOUND DURING C-CHECK, FUSELAGE HAS TWO DENTS AT STATION 233 LONGERON 17 AND 18L. REMOVED DAMAGE, INSTALLED SKIN AND DOUBLER. (M) 2L72 4F RTA6WE 20050718001552005071800155WP 2005 7 18 ASAA0580199 120050404A53105936038501 BEAM DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02950AS 53023 OKC - DURING C-CHECK, AFT CARGO BAY DOOR CUTOUT BEAM IS CORRODED UNDER REPAIR DOUBLER. REPLACED CUTOUT BEAM. (M) 2L72 4F RTA6WE 20050718001562005071800156NM 2005 7 18 ASAA0540223 120050505A534069773083 ATTACH FITTING BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02792AS 28887 PAE - FOUND CORROSION AT LAVATORY ATTACH FITTING. REMOVED AND REPLACED ATTACH FITTING. (M) 2L72 4F RTA16WE 20050718001582005071800158WP 2005 7 18 ASAA0580297 120050526A217017946081 COALESCER BAG DOUG DC9 DC982 3022082WP RT A/C PACK FAILED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02935AS 49236 ATB - FAILED RIGHT AIR CONDITIONING SYSTEM WATER SEPARATOR CAUSED CABIN TO FILL WITH SMOKE. REPLACED WATER SEPARATOR, AND PERFORMED PNEUMATIC DUCTS BURN OUT PROCEDURE. (M) 2L72 4F A6WE 20050718001602005071800160NM 2005 7 18 ASAA0540232 120050508A5755654645245 SKIN BOEING737 7374Q8 138447QNM NR 5 SPOILER DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02783AS 25114 OKC - FOUND NR 5 INBOARD SPOILER SKIN IS DENTED. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW BOEING 737-400 SRM 51-770-10 REPAIR 21. (M) 2L72 4F RTA16WE 20050718001622005071800162NM 2005 7 18 ASAA0510069 120050415A53206547973506 WEB BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 YXX - FOUND FLOOR WEB AT RT BS 578-597 CORRODED. REPLACED FLOOR WEB RT BS 578-597 WITH MADE REPAIR PART IAW B737-200 SRM 51-20-1 AND 51-30-2 FIGURE 3. (M) 2L72 4F A16WE 20050718001632005071800163NM 2005 7 18 ASAA0510071 120050414A53136573744 STRINGER BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 YXX - FOUND CORROSION IN AFT CARGO PIT ON STRINGER 21L AT BS 940. REPAIRED PER B737-200 SRM 53-10-3 FIGURE 1. (M) 2L72 4F A16WE 20050718001662005071800166NM 2005 7 18 ASAA0540224 120050505A5320695141112 SUPPORT ANGLE BOEING737 737490 1384715NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02792AS 28887 PAE - FOUND CARGO BAY, BS 500F, STRINGER 26R SUPPORT ANGLE IS CRACKED. REMOVED, FABRICATED AND INSTALLED NEW SUPPORT ANGLE. (M) 2L72 4F RTA16WE 20050718001682005071800168WP 2005 7 18 ASAA0580288 120050516A53209923667 WEB DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02968AS 53016 OKC - DURING HV CHECK, FOUND FLOOR WEB STATION 190 RBL 30 HAS A CRACK ABOVE THE RACK ON THE RIGHT SIDE OF E/E BAY. REMOVED DAMAGE AND REPLACED WITH DOUBLER. (M) 2L72 4F RTA6WE 20050718001692005071800169NM 2005 7 18 ASAA0510070 120050415A33508821004 BATTERY PACK BOEING737 7372X6C 1384552NM EMERGENCY LIGHT DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM02746AS 23123 ANC - FOUND RIGHT OVERWING LOWER EMERGENCY LIGHT LENS WILL NOT STAY SECURED. LIGHT ALSO INOPERATIVE. REPLACED BATTERY PACK AND LENS ASSEMBLY. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20050718001712005071800171WP 2005 7 18 ASAA0580189 120050404A532099579185 CHANNEL DOUG DC9 DC983 3022083WP FLOOR PANEL WORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM02950AS 53023 OKC - DURING C-CHECK, FOUND CABIN FLOOR PANEL HAT CHANNEL IS WORN. REPLACED HAT CHANNEL. (M) 2L72 4F RTA6WE 20050718001732005071800173WP 2005 7 18 ASAA0580200 120050404A532059364421 SILL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02950AS 53023 OKC - DURING C-CHECK, AFT CARGO BAY DOOR LOWER SILL WEB IS CORRODED. REMOVED DAMAGED SECTION AND INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050718001752005071800175WP 2005 7 18 ASAA0580142 120050228A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 OKC - DURING HV CHECK, SEAT TRACK GOUGED AT LUGS. REMOVED DAMAGED SECTION. INSTALLED REPAIR SECTION. (M) 2L72 4F RTA6WE 20050718001762005071800176WP 2005 7 18 ASAA0580267 120050517A5313 LONGERON DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - FOUND DURING C-CHECK, LONGERON 30 IS CORRODED ON THE TOWER SURFACE OF THE INBOARD FLANGE AT STATION 1198 TO 1203. REMOVED DAMAGED PERFORMED HFEC INSPECTION, AND INSTALLED REPAIR STRAPS LONGERON. (M) 2L72 4F RTA6WE 20050718001782005071800178NM 2005 7 18 ASAA0510078 120050415A53146545435501 KEELBEAM BOEING737 737290C 138448VNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 YXX - RIGHT KEEL BEAM SUPPORT ANGLE AT BS 520 TO 535 HAS PREVIOUS DAMAGE. REPLACED WITH FABRICATED REPAIR PART IAW B737-200 SRM 51-20-1 AND 51-10-1 PARAGRAPH 5A. (M) 2L72 4F A16WE 20050718001792005071800179WP 2005 7 18 ASAA0580234 120050509A532099579182 CHANNEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - FOUND DURING C-CHECK, CABIN FLOORBOARD HAT CHANNEL IS CRACKED. REPLACED HAT CHANNEL. (M) 2L72 4F RTA6WE 20050718001812005071800181NM 2005 7 18 05FDEA01869 120050709A5730 PANEL DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 LT WING, UPPER WING, CORROSION FOUND ON FIXED PANEL AND MARKED ON REAR SPAR SECTION AT STA 948. REPAIRED AS PER FEDEX EA 1-5710-90068. 2L73 4F RTA22WE 20050718001822005071800182NM 2005 7 18 05FDEA01871 120050709A5753 HINGE DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 RT WING, O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR PIN ATTACHMENT I/B BORE FOUND CORRODED. 2L73 4F RTA22WE 20050718001832005071800183NM 2005 7 18 05FDEA01872 120050709A5753 HINGE DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 RT WING, O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR PIN ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. REPAIR CARRIED OUT AS PER EA1-5750-87590. 2L73 4F RTA22WE 20050718001842005071800184NM 2005 7 18 05FDEA01873 120050709A5753 HINGE DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 RT WING, O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR PIN ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED IAW CMM 20-11-02. FABRICATED BUSHING AND INSTALLED AS PER EA1-5750-87590. 2L73 4F RTA22WE 20050718001902005071800190NM 2005 7 18 05FDEA01879 120050709A5753 HINGE DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 RT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. REPAIRED AS PER EA1-5750-87591. 2L73 4F RTA22WE 20050718001912005071800191NM 2005 7 18 05FDEA01880 120050709A5753 HINGE DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 RT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. REPAIRED AS PER EA1-5750-87591. 2L73 4F RTA22WE 20050718001942005071800194WP 2005 7 18 ASAA0580269 120050517A534759305661 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - DURING C-CHECK, FOUND CABIN SEAT TRACK LBL 44 STATION 1174 IS EXFOLIATED. REMOVED AND REPLACED SEAT TRACK. (M) 2L72 4F RTA6WE 20050718001962005071800196WP 2005 7 18 ASAA0580273 120050516A5320993061217 CUSP WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02968AS 53016 OKC - DURING HV CHECK, LEFT CUSP WEB CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050718001992005071800199NM 2005 7 18 05FDEA01885 120050709A5753 HINGE DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 RT WING, O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. REMOVED IAW CMM 20-11-02. FABRICATED BUSHING AND INSTALLED IAW EA1-5750-87591. 2L73 4F RTA22WE 20050718002022005071800202NM 2005 7 18 05FDEA01888 120050709A5313 STRINGER DOUG MD11 MD11 3023602NM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 AFT CARGO BAY AT STA 1967, AFT CENTER CEILING TOP STRINGER ASSY FOUND DAMAGED AS MARKED. DAMAGED FLOOR SUPPORT REMOVED. NEW FLOOR SUPPORT REWORKED FROM S2922781- 1X2024T42 AS PER DWG ACA 7149 AND INSTALLED AS PER SRM 51-31-01 VOL.II. CLASSIFIED MINOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050718002032005071800203NM 2005 7 18 05FDEA01889 120050710A5753 HINGE DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 LT WING, O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. REPAIRED AS PER EA1-5750-87592A. 2L73 4F RTA22WE 20050718002052005071800205NM 2005 7 18 05FDEA01894 120050711A5753 HINGE DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 LT WING O/B FLAP O/B HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-09 PG 402-407. REPAIR CARRIED OUT AS PER CMM 57-44-09. 2L73 4F RTA22WE 20050718002062005071800206CE 2005 7 18 DXTA200500824 120050708A2750 CONNECTOR BEECH MU300 400A 1155402CE TE FLAPS CORRODED E DXTAA UNSCHED LANDING F FLT CONT AFFECTED APAPPROACH 1 GL07117QS RK391 ON APPROACH INTO ASE FLAPS LOCKED UP AT 10 DEGREES. DIVERTED TO GJT FOR LANDING AT FLAPS 10. TROUBLESHOT FAULT BY OPENING THROTTLE QUAD AND CLEANED, LUBED. INSPECTION FLAP LEVER AND FOUND NO FAULT. INSPECTED 10 DEG FLAP SWITCH AND ACTUATOR SWITCH. BOTH CHECKED OUT GOOD ON DVM. CLOSED THROTTLE QUAD. INSPECTED LT AND RT FLAP FOLLOW UP SWITCHES. FOUND BAD CORROSION IN CONNECTOR P&J 268 CLEANED CONNECTOR SYS OPS TEST GOOD. RESTORED A/C FOR FLIGHT ALL WORK DONE IAW THE HAWKER 400XP WDM AND AMM CHP 27-51-01. 2H72 4F RTA16SW 20050718002072005071800207 2005 7 18 DXTA200500831 420050711A3400701700098803 COMPUTER CESSNA560 560XL 2076702CE FAILED E DXTAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL07607QS822 5605340 WHILE IN FLIGHT AT FL 410, NR 1 PFD AND MFD WENT BLANK AND THEN A RED X APPEARED ACROSS EACH SCREEN. SG2 WAS SELECTED AND INFORMATION WAS REDISPLAYED TO EACH SCREEN. AMBER SG2 APPEARED ON NR 1 PFD. REPLACED NR 1 IC615 IAW 34-25-02, OPS CHECKS GOOD. 2L72 4F RTA22CE 20050718002092005071800209NM 2005 7 18 05FDEA01896 120050712A5280 HINGE DOUG MD11 MD11 3023602NM MLG DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 LT MLG WHEEL WELL DOOR CENTER HINGE HALVES FOUND CRACKED. CRACKED CENTER HINGE AT LEFT HAND MAIN LANDING GEAR WHEEL WELL DOOR REMOVED AND REPLACED WITH NEW HINGE AS PER SRM 51-35-01 VOLUME II. THIS REPAIR IS CLASSIFIED MINOR PER GMM 6-2-100. 2L73 4F RTA22WE 20050718002122005071800212NM 2005 7 18 USAA200507003 120050711A5311 FRAME BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19392US 23314 1.5 IN CRACK FOUND AT FRAME 767, STR 24L. INSTALLED REPAIR DOUBLER PER SRM 53-00-01 FIG 229. 2L72 4F RTA16WE 20050718002142005071800214 2005 7 18 BA05013 420050712A25657A1508115 SLIDE AIRBUS330 A330323 3930335EU 4L DOOR FAULTY A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW9074 8180 333 DURING EMERGENCY POWER SUPPLY UNIT SYSTEM TEST, RECEIVED FAULT MESSAGE FOR 4L DOOR ESCAPE SLIDE. MAINTENANCE REPLACED 4L DOOR ESCAPE SLIDE. OK FOR SERVICE. 2L72 4F RTA46NM 20050718002162005071800216NM 2005 7 18 QXEA200501101 120050706A2750C1486742003 CONTROL UNIT BOMBDRDHC8 DHC8402 1390042NM TE FLAPS MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09404QX9063 4046 FLAP POWER CAUTION IN FLIGHT. RAN CHECKLIST. CAUTION STILL ILLUMINATED. GPWS CAUTION ALSO ILLUMINATED 15 MINUTES LATER WHILE CHANGING TO LOWER ALTITUDE. REPLACED FLAP CONTROL UNIT AS A PRECAUTIONARY MEASURE. NO FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050718002192005071800219NM 2005 7 18 HNAA0500068 120050711A792245E041 VALVE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE ENGINE OIL TEMP STICKING A HNAAA UNSCHED LANDING M OVER TEMP CRCRUISE 1 EA07907HA5180751807 011 NR 1 ENGINE OIL TEMPERATURE REACHED 120 DEGREES C AND REDUCED TO 115 DEGREES C WHEN FUEL AUXILLARY PUMP SELECTED ON. REMOVED AND REPLACED OIL COOLER THERMAL VALVE. 2H72 4T4 TRTA13NM E20NE 20050714002272005071400227EA 2005 7 14 MASA200500480 120050622A2722 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA RUDDER MALFUNCTIONED A MASAO OTHER F FLT CONT AFFECTED CRCRUISE 1 SW07652ML 7036 RUDDER UNCOMMANDED MOVEMENT IN FLIGHT. REMOVED AND REPLACED NR 1 AND NR 2 LINEAR ACTUATOR. 2L72 4F RTA21EA 20050715000052005071500005NM 2005 7 15 2005UALA00595 120050624A2497 WIRE AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE NR 2 GENERATOR CHAFED A UALAA UNSCHED LANDING HGJELECT. POWER LOSS-50 PC MULTIPLE FAILURE WARNING INDICATION CRCRUISE 1 WP29847UA 1627 LOST NR 2 GENERATOR AND APU AUTO SHUTDOWN. REPAIRED 4 CHAFED WIRES BEHIND NR 2 GCU BENCH PLUG, LOCATED AT FIRST TIE WRAP. 2L72 4F4 FRTA28NM E40NE 20050715000072005071500007NM 2005 7 15 2005UALA00601 120050627A5743 HINGE FITTING BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FLAPS DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29657UA 27112 LT INBD FLAP CENTER HINGE FITTING LINE INBD SIDE DAMAGED. LEFT INBOARD FLAP CENTER HINGE FITTING FOUND DAMAGED ON INBOARD SIDE. REPAIRED PER SRM 57-53-02. 2L72 4F4 FRTA1NM E24NE 20050715000092005071500009WP 2005 7 15 UPS05844757 120050528A53205641006501 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE:C-3. WING BOX BOOT FITTING CRACKED APPROX 5 IN LONG STA 759 BETWEEN L17L-L18L. CUT OUT CRACKS, FABRICATED AND INSTALLED REPAIR PARTS IAW SAASK 840-808203 AND EO DC853-20469. 2L74 4F RT4A25 20050715000192005071500019NM 2005 7 15 SWAA052032 120050712A3350D71701100 BATTERY PACK BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29710SW 27844 DURING SCHEDULED HC1 CHECK, FOUND L1 & R1 DOOR UPPER EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACKS PER MM. 2L72 4F RTA16WE 20050715000472005071500047NM 2005 7 15 05FDEA01835 120050707A5753 STRUCTURE DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 LT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. FABRICATED BUSHING AND INSTALLED AS PER EA 1-5750-87588. 2L73 4F RTA22WE 20050715000482005071500048NM 2005 7 15 05FDEA01836 120050707A5753 STRUCTURE DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 LT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. 2L73 4F RTA22WE 20050715000562005071500056NM 2005 7 15 UPS05444812 120050617A5311 FRAME BOEING747 747123F NM FWD CARGO CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C. FWD CARGO, FRAME AT BS 900 STR -34L FOUND UPPER CHORD TO FRAME WEB CRACKED, CRACK LENGTH 0.75 IN. FRAME REPAIRED AS PER SRM 53-10-04 FIG 52. 2L74 4F A20WE 20050715000612005071500061NM 2005 7 15 UPS05444818 120050621A5315 FLOORBEAM BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C. U/D, BS 400, RBL 0-6 FLOORBEAM UPPER CHORD FOUND SLIGHTLY CORRODED. CORROSION BLEND OUT 0.040 BY 0.875 BY 1.5 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 1. 2L74 4F A20WE 20050715000622005071500062NM 2005 7 15 UPS05444819 120050621A5347 SEAT TRACK BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C. U/D, BS 530-580 RBL 65 IN SEAT TRACK CROWN FOUND CORRODED. CORROSION BLEND OUT 0.042 BY 0.3750 BY 3 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, U/D SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A AT BS 530-590 RBL 65 AREA. 2L74 4F A20WE 20050715000712005071500071NM 2005 7 15 MWEA050070 120050712A53305924802163 SKIN BOEING717 717200 1383700NM FUSELAGE DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31904ME 55168 DENT IN FUSELAGE SKIN STATION 275 AND LONGERON 18 (CUSP) LEFT HAND SIDE. FABRICATED AND INSTALLED DOUBLER. 2L72 4F TRA6WE 20050715000722005071500072NM 2005 7 15 UPS05444826 120050622A5311 FRAME BOEING747 747123F NM AFT CARGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C, AFT CARGO STA 1600 RBL 35 FRAME UPPER CHORD LWR SURFACE FOUND CORROSION. CORROSION BLEND OUT 0.022 BY 1.5 BY 2 IN. EXCEEDED SRM 53-10-01 FIG 1 LIMITS, UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 2. 2L74 4F A20WE 20050715000772005071500077NM 2005 7 15 UPS05444830 120050617A5347 SEAT TRACK BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C, U/D BS 520 TO 670 LBL 10 SEAT TRACK CORRODED. CORROSION BLEND OUT 0.040 BY 1 BY 3 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, U/D BS 520 TO BS 670 LBL 10 TRACK REPAIRED AS PER SRM 53-10-05 FIG 4. 2L74 4F A20WE 20050715000852005071500085EU 2005 7 15 AWXA200500803 120050711A3397D9299200900200 WIRE HARNESS AIRBUS320 A320232 3930326EU EMERGENCY LIGHT SEVERED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28656AW 1079 PHX - EEL - DURING 8 DAY CHECK FOUND EMERGENCY EXIT LIGHT AT SEAT 24 INOPERATIVE. MAINTENANCE REPLACED WIRING HARNESS UNDER SEAT AT ROW 24L. OPERATIONAL CHECKS GOOD. 2L72 4F RTA28NM 20050715000872005071500087NM 2005 7 15 AWXA200500805 120050711A3234 HANDLE BOEING737 7373S3 1384711NM MLG STUCK A AWXAA UNSCHED LANDING O OTHER CLCLIMB 1 WP28312AW 24060 DURING CLIMB OUT OF DFW EN ROUTE TO PHX GEAR HANDLE WOULD NOT GO PAST CENTER POSITION AFTER DEPARTURE, GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO DFW WITHOUT FURTHER INCIDENT. AIRCRAFT WAS FERRIED BACK TO PHX AND IS CURRENTLY BEING TROUBLESHOT. MAINTENANCE FOUND THE AIR/GROUND CABLE OUT OF RIG ON THE RT GEAR. RIGGED CABLE IAW BOEING 737-300 AMM 27-62-51. CYCLED GEAR, OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20050715000892005071500089CE 2005 7 15 DXTA200500829 120050708A215073838433 COOLING TURBINE CESSNA750 750 2076810CE AFT SERVICE BAY FAILED E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07956QS4221 7500156 SMOKE BURNT OIL SMELL COMING FROM ENVIRONMENTAL SYSTEM. WORSE ON DESCENT. REMOVED AND REPLACED FAILED ACM TURBINE. OPERATIONAL CHECK GOOD IAW CE-750 M/M CH 21-51-00. 2L72 4J RTT00007WI 20050715001052005071500105NM 2005 7 15 UPS05444838 120050617A5311 FRAME BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C, M/D, BS 2320 RT STR 26R TO 28R FRAME INNER CHORD FOUND CRACKED, CRACK LENGTH 3 IN. FRAME REPAIRED AS PER HX RS NR R53-82-35327 AND UPS EO NR B747-5310-22462-A. 2L74 4F A20WE 20050715001062005071500106NM 2005 7 15 UPS05444839 120050617A531165B0717639 FRAME BOEING747 747123F NM FWD CARGO CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C, FWD CARGO FRAME AT BS 960 STR 40R FOUND UPPER CHORD CRACKED, ALSO EXTEND TO WEB, CRACK LENGTH 3 IN. FWD CARGO BAY BS 960 S40R AREA FRAME REPAIRED AS PER HX RS NR R53-22-35325 AND UPS ENGINEERING FILE NR 747-53-20259. 2L74 4F A20WE 20050715001192005071500119NM 2005 7 15 ASMF200507002 120050705A2720833605 PSEU DOUG MD80 MD83 3023681NM RUDDER FAILED W ASMFA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 SW23881LF228 53051 AIRCRAFT RETURNED TO PLATFORM DUE TO RUDDER TRAVEL UNRESTRICTED, FLAP SLAT DISAGREE AND BOTH MAIN LANDING GEAR RED LIGHTS TURNED ON. BITE TO SWC AND PSEU PERFORMED, NOT CONFIRMING FAILURE. TECHNICAL PERSONNEL SENT TO STATION AND PSEU REPLACED IAW MM 32-60-04, FLAP-SLAT OPERATIONAL TESTS AND ENGINE RUNNING TEST IN FLIGHT MODE WERE PERFORMED, ALL CORRECT. ADDITIONALLY, RUDDER RESTRICTION TEST PERFORMED AND BOTH WING PROXIMITY SENSORS CLEANED, TESTED CORRECT. OVERWEIGHT LANDING CHECK PERFORMED IAW MM 05-51-04, ALL CORRECT. 2L72 4F RT 20050715001202005071500120NM 2005 7 15 ASMF200507003 120050706A5330 SKIN DOUG MD80 MD83 3023681NM FUSELAGE DENTED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23861LF 49826 DURING TRANSIT CHECK CAPT REPORTED 2 HITS ON FUSELAGE. ONE BELOW 45 RT LIGHT AND OTHER IN AFT RT RVSM AREA. INSPECTION PERSONNEL SENT TO PLATFORM AND CHECK DAMAGE. DENT AT STATION 571 WITHIN LIMITS IAW SRM 53-04 CONDITION B AND DENT IN RVSM AREA WITHIN LIMITS IAW SRM 51-50-00 FIG 18. 2L72 4F RT 20050715001282005071500128WP 2005 7 15 UPS05844874 120050712A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 1 INCH FUSELAGE SKIN CRACK AFT OF OUTFLOW VLV. REMOVED DAMAGE FROM A/C DRHODES 0557647 DAMAGE REMOVAL VERIFIED OK TO FABRICATE & INSTALL REPAIR. 2L74 4F RT4A25 20050715001302005071500130NM 2005 7 15 UPS05M44872 120050709A2560 SMOKE GOGGLES DOUG MD11 MD11F 3023600NM COCKPIT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP 48579 INSPECTION TYPE:N/A COURIER SEAT NEAR REFRIG, SMOKE GOGGLES LENS CRACKED. REMOVED AND REPLACED SMOKE GOGGLES. 2L73 4F RTA22WE 20050715001562005071500156EU 2005 7 15 7135052405 120050524A52301172420213 DOOR BOLKMS117 BK117B1 5626012EU LT CARGO BLEW OUT E A1UAB EMER. DESCENT DJEINFLIGHT SEPARATION WARNING INDICATION VIBRATION/BUFFET AAAIR AMBULANCE 1 CE03770SL5512 S7135 AFTER DROPPING OFF CREW AT HOSPITAL, PILOT WAS REPOSITIONING TO BASE FOR FUEL. 1 MINUTE OUT FROM LANDING AT BASE, MASTER CAUTION LIGHT AND DOOR SEGMENT LIGHT CAME ON. 2 SECONDS LATER THERE WAS A LOAD BANG, AND A/C YAWED LT AND THERE WAS SEVERE VIBRATION. AFTER PILOT ENSURED STILL HAD TAIL ROTOR AUTHORITY AND FULL CONTROL OF A/C, PILOT DECLARED EMERGENCY WITH DISPATCH AND DIVERTED TO LOCAL AIRPORT WHERE PILOT MADE EMERGENCY LANDING. PILOT INSPECTION OF A/C SHOWED LT CARGO DOOR MISSING AND DAMAGE TO MAIN AND TAIL ROTOR BLADES. A/C INSPECTED BY MX AND FOUND UPPER DOOR TRACK BENT OUT AT PINS (WHERE EMERGENCY RELEASE PINS ENGAGE). DOOR HAD SLID BACK APPROX 2.5 IN FROM LOCKED POSITION BEFORE DEPARTING AIRFRAME. 1G72 3U H13EU 20050715001882005071500188NM 2005 7 15 QXEA200501098 120050707A3350 CONNECTOR DHAV DHC8 DHC8202 2809007NM EMERGENCY LIGHTSDIRTY A QXEAK NONE O OTHER UKUNKNOWN 1 NM09366PH 510 FLOOR EMERGENCY LIGHTING AT ROWS 1-4 INOP. MAINTENANCE CLEANED CONNECTORS 3352-P4 AND J4. REPINNED WIRES 3352-11D70 AND 3352-27F20N IAW WIRING DIAGRAM 33-50-01. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2H72 4T RTA13NM 20050715001902005071500190NM 2005 7 15 QXEA200501099 120050707A5210 DOOR BOMBDRDHC8 DHC8402 1390042NM AFT CABIN OUT OF ADJUST A QXEAO OTHER O OTHER TXTAXI/GRND HDL 1 NM09400QX 4030 AFT PASSENGER DOOR HARD TO OPEN. AIRCRAFT FERRIED. RESTACKED WASHERS ON MAIN HINGE IAW EA 6-52-391 AND ADJUSTED AFT PASSENGER DOOR STABILIZER ROD ASSEMBLY AND SECONDARY HINGE ASSEMBLY IAW MAINTENANCE MANUAL TASK 52-00-00-820 PARAGRAPH 4F. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050718000292005071800029NM 2005 7 18 ASAA0540222 120050505A534069773082 ATTACH FITTING BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02792AS 28887 PAE - FOUND CORROSION AT LAV ATTACH FITTING, BS 947. REMOVED AND REPLACED ATTACH FITTING. (M) 2L72 4F RTA16WE 20050718000322005071800032NM 2005 7 18 ASAA0510072 120050416A28106545428504 FUEL TANK BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 YXX - FUEL CENTER TANK CORRODED AT UPPER SURFACE BS 578 RBL 67. REPAIRED IAW EA 5710-01118. (M) 2L72 4F A16WE 20050718000572005071800057NM 2005 7 18 ASMF200507009 120050710A2424947F9453 GCU DOUG MD88 MD88 3023688NM APU FAILED W ASMFD RETURN TO BLOCK HJ ELECT. POWER LOSS-50 PC WARNING INDICATION TXTAXI/GRND HDL 1 SW23160PL14296 49763 A/C RETURNED TO PLATFORM. DURING ENGINES STARTING, LT GENERATOR LIGHT TURNED ON. DETECTED THAT RT GENERATOR AND APU GENERATOR DID NOT GET THEIR BARS. CROSS FEED SUPPLY OUT OF SERVICE. LT GEN OFF LIGHT TURNED ON. GCU OF APU REPLACED IAW MM 24-20-00 CORRECTING THE FAILURE. BCU REPLACED BUT FAILURE CONTINUED IN CROSS FEED SUPPLY AND LT GENERATOR LIGHT. RT GENERATOR DEFERRED IAW MEL 24-8. DURING OVERNIGHT SERVICE, RELAY R2-33 WIRING WAS REPAIRED IAW WDM 30-27-00. ENGINE, APU GENERATOR AND EXTERNAL POWER WERE TESTED AND RELAY R2-37 REPLACED IAW MM 24-20-06, MM 24-40-00 AND MM 24-20-00 RESPECTIVELY. DEFERRED REPORT CLOSED. 2L72 4F RTA6WE 20050718000622005071800062WP 2005 7 18 ASAA0580240 120050509A5320993053813 CUSP WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - FOUND DURING C-CHECK, CUSP WEB CORRODED AT STATION 416 TO 419. REMOVED CORROSION AND INSTALLED DOUBLER. (M) 2L72 4F RTA6WE 20050718000642005071800064WP 2005 7 18 ASAA0580272 120050516A5320993053812 CUSP WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02968AS 53016 OKC - DURING HV-CHECK, RIGHT CUSP WEB CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050718000682005071800068WP 2005 7 18 ASAA0580233 120050509A532199366521 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - FOUND DURING C-CHECK, FLOORBOARD HAS INSERTS PULLED OUT. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050718000692005071800069WP 2005 7 18 ASAA0580241 120050509A5320993061269 CUSP WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - FOUND DURING C-CHECK, CUSP WEB CORRODED AT STATION 1158 TO 1166. REMOVED CORROSION AND INSTALLED SEGMENT AND DOUBLER. (M) 2L72 4F RTA6WE 20050718000722005071800072WP 2005 7 18 ASAA0580277 120050516A5320 CUSP WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02968AS 53016 OKC - DURING HV CHECK, FOUND LEFT FLOOR CUSP WEB CORRODED AT STATION 465-389. REMOVED DAMAGED SECTION. INSTALLED WEB AND DOUBLER. (M) 2L72 4F RTA6WE 20050718000822005071800082NM 2005 7 18 ASAA0510092 120050503A33508821004 BATTERY PACK BOEING737 7372X6C 1384552NM OVERWING EXITS DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM02746AS 23123 ANC - AFTER PAX CABIN RECONFIG, LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED LEFT AND RIGHT OVERWING EXIT EMERGENCY EXIT LIGHT BATTERY PACKS. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20050718000872005071800087NM 2005 7 18 ASAA0510134 120050613A5753 SKIN BOEING737 737290C 138448VNM FLAP DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX - FOUND IMPACT DAMAGE ON OUTBOARD T/E OF RIGHT INBOARD MID FLAP. RIGHT INBOARD MID FLAP IMPACT DAMAGE LOCATION REPAIRED IAW B737-200 SRM. (M) 2L72 4F A16WE 20050718000982005071800098NM 2005 7 18 ASAA0540165 120050310A5320654769016 SUPPORT BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02794AS 28889 PAE - FOUND AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED. REMOVED, FABRICATED AND INSTALLED FLOOR TO SIDEWALL SUPPORT. (M) 2L72 4F RTA16WE 20050718001002005071800100WP 2005 7 18 ASAA0580194 120050404A5320 CHANNEL DOUG DC9 DC983 3022083WP FUSELAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02950AS 53023 OKC - FOUND DURING C-CHECK, CABIN FLOOR PANEL HAT CHANNEL IS CHAFED. REPLACED HAT CHANNEL. (M) 2L72 4F RTA6WE 20050718001042005071800104NM 2005 7 18 ASAA0510093 120050505A5340653535213 STRINGER CLIP BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX - AFT CARGO BS 767 STRINGER 23L TIE CLIP CORRODED. REMOVED AND REPLACED TIE CLIP AT BS 767. (M) 2L72 4F A16WE 20050718001062005071800106WP 2005 7 18 ASAA0580286 120050516A5320 CHANNEL DOUG DC9 DC983 3022083WP FS CUT A ASAAK NONE O OTHER ININSP/MAINT 1 NM02968AS 53016 OKC - DURING HV-CHECK, FOUND FLOOR PANEL 4-E HAT SECTION HAS .25 INCH LONG CUTS AT THE END OF THE HAT SECTION. REMOVED DAMAGED SECTION OF HAT CHANNEL. INSTALLED REPLACEMENT HAT CHANNEL SECTION AND SPLICE. (M) 2L72 4F RTA6WE 20050718001142005071800114WP 2005 7 18 ASAA0580299 120050604A575359304944 VANE DOUG DC9 DC983 3022083WP RT TE FLAP GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02961AS 53075 OKC - FOUND DURING HV-CHECK, RIGHT FLAP VANE GOUGED. REPAIRED DAMAGED SECTION PER SRM 51-70. (M) 2L72 4F RTA6WE 20050718001302005071800130NM 2005 7 18 ASAA0540171 120050315A5330 SKIN BOEING737 737490 1384715NM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02791AS 28886 PAE - FOUND DENT AT BS 385 STRINGER 24R. REPAIRED DENT PER EA. (M) 2L72 4F RTA16WE 20050718001342005071800134WP 2005 7 18 ASAA0580197 120050404A5330 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02950AS 53023 OKC - DURING C-CHECK, FOUND FUSELAGE SKIN DENTED. REPLACED DAMAGED SECTION USING FINGER DOUBLER, STRAPS, AND DOUBLERS. (M) 2L72 4F RTA6WE 20050718001432005071800143EU 2005 7 18 BA05012 120050712A3350321431 BATTERY PACK AIRBUS330 A330323 3930335EU EMERGENCY LIGHTSDISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19672UW 0333 MAINTENANCE REPORTED BATTERY PACKS 2L (13WL) AND 3R (16WL) FAILED CAPACITANCE TEST. MAINTENANCE REMOVED AND REPLACED BATTERY PACKS. OPERATIONAL CHECK GOOD. 2L72 4F RTA46NM 20050718001442005071800144WP 2005 7 18 ASAA0580191 120050404A532199366401 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02950AS 53023 OKC - FOUND DURING C-CHECK, CABIN FLOOR PANEL IS DELAMINATED AND CRACKED. REPLACED PANEL. (M) 2L72 4F RTA6WE 20050718001472005071800147NM 2005 7 18 ASAA0510076 120050417A531465621251 KEELBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 YXX - FOUND LEFT KEEL BEAM CORROSION AT BS 535 ON LOWER FLANGE. REPAIRED IAW RO 3838 AND EA 5310-02458. (M) 2L72 4F A16WE 20050718001572005071800157NM 2005 7 18 ASAA0540225 120050505A532065566552 WEB BOEING737 737490 1384715NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02792AS 28887 PAE - FOUND WEB DAMAGED AT AFT CARGO DOOR CUTOUT. REMOVED, FABRICATED AND INSTALLED WEB. (M) 2L72 4F RTA16WE 20050718001642005071800164NM 2005 7 18 ASAA0540237 120050511A53206545406529 STIFFENER BOEING737 737490 1384715NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02792AS 28887 PAE - FOUND CENTER FUEL STIFFENER IS CRACKED. INSTALLED NEW STIFFENER. (M) 2L72 4F RTA16WE 20050718001672005071800167NM 2005 7 18 ASAA0540226 120050505A5320655572685 BRACKET BOEING737 737490 1384715NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02792AS 28887 FOUND STATION 727 BULKHEAD BRACKET IS CRACKED AT BS 727, RBL 5, WL 145. REMOVED AND REPLACED. (M) 2L72 4F RTA16WE 20050718001892005071800189NM 2005 7 18 05FDEA01878 120050709A5753 HINGE DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 RT WING, O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. REPAIRED AS PER EA1-5750-87590. 2L73 4F RTA22WE 20050718001932005071800193NM 2005 7 18 05FDEA01882 120050709A5753 HINGE DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 RT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. REPAIRED AS PER EA1-5750-87591. 2L73 4F RTA22WE 20050718001952005071800195NM 2005 7 18 05FDEA01883 120050709A5753 HINGE DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 RT WING, O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. REPAIRED AS PER EA1-5750-87591. 2L73 4F RTA22WE 20050718002002005071800200NM 2005 7 18 05FDEA01886 120050709A5753 HINGE DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 RT WING, O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. REPAIRED AS PER EA1-5750-87591. 2L73 4F RTA22WE 20050718002042005071800204NM 2005 7 18 05FDEA01890 120050710A5753 HINGE DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 LT WING, O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. REPAIRED AS PER CMM 57-44-09 P402-407 AND EA 1-5750-87592A. 2L73 4F RTA22WE 20050718002082005071800208CE 2005 7 18 DXTA200500827 120050708A2720 ACTUATOR CESSNA750 750 2076810CE RUDDER FAILED E DXTAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL07908QS5219 7500108 AMBER "RUB LIMIT FAIL B" CAS MESSAGE WITH A AMBER "RUDDER LIMIT 18%" MESSAGE IN EICAS CNTRL POSITION PAGE. EVENT MARKER PUSHED. COULD NOT DUP FLT CREWS DISCREPANCY ON ARRIVAL. RANG OUT WIRING FROM LOGIC MODULE TO LWR RUDDER LIMIT ACT WITH NO DISCREPANCYS FOUND. CLEANED CONNECTOR'S & RE-TORQUED ALL GROUND POINT'S. R/R`D LWR "B" RUDDER LIMIT ACT IAW CR 750 M/M 27-23-00 OPS CHECK'S BAD, "RUDDER LIMIT FAIL B" EICAS MESSAGE ILLUMINATED ON PWR UP. AT NETJETS LMCC REQUEST REPOSITIONED UPPER RUDDER LIMIT "A" TO LWR "B" POSITION P/N EM4070-6/9914558-6 S/N 189THEN INSTALLED RECEIVED OVERHAULED ACT IN UPPER "A" POSITION IAW CE 750 M/M 27-23-00. BOTH UPPER "A" & LWR "B" ACT`S OPS CHECK GOOD. 2L72 4J RTT00007WI 20050718002212005071800221EA 2005 7 18 VTZA200500136 120050711A5712601R107091 RIB CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27654BR 7454 LT BATTERY RIB CRACKED 1.5 IN. 2L72 4F RTA21EA 20050718002242005071800224EA 2005 7 18 VTZA200500138 120050711A53116013600130 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27654BR 7454 RT FS 640 FRAME DOUBLER CRACKED IN RADIUS AT 3.0 IN LENGTH. 2L72 4F RTA21EA 20050718002262005071800226EA 2005 7 18 VTZA2005140 120050711A5346601R536066 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA RT ENGINE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27654BR 7454 RT ENGINE SUPPORT BEAM CRACKED IN LOWER WEB AT 0.75 IN. 2L72 4F RTA21EA 20050718002272005071800227EA 2005 7 18 VTZA200500141 120050711A5310601R5211680 DOOR FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27654BR 7454 PAX DOOR FRAME TOP RADIUS CRACKED AT 1.0 IN LENGTH FORWARD OF DATUM 1 AT FS 338.90. 2L72 4F RTA21EA 20050718002292005071800229 2005 7 18 DXTA200500819 420050707A3410 ODOR CESSNA560 560XL 2076702CE COCKPIT DETECTED E DXTAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 GL07687QS 5605187 UPON DESCENT THROUGH 14000 FT, MFD SCREEN WENT BLANK ABRUPTLY. STRONG ODOR OF BURNED PLASTIC FILLED COCKPIT, BUT NO SMOKE DETECTED. PERFORMED USER INITIATED SELF TEST. ALL ITEMS DISPLAY PASS AND VALID. SWITCH SG FROM NORM TO SG1 AND SG 2. SELF TEST ALSO PASS/VALID. INSPECTED MFD FOR OVERHEAT/BURN ODOR. CHECKS GOOD. ALL WORK PERFORMED IAW CE 560 XL MM 34-25-01 AND 34-25-02 .SYSTEM RAN APPROX 2 HRS. NO DEFECTS FOUND. 2L72 4F RTA22CE 20050719000032005071900003NM 2005 7 19 05FDEA01868 120050709A5714AYB703512 BRACKET DOUG DC10 DC10 N/A-SDRNM CENTER WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25313 CTR WING LOWER STRUCTURE; RT BARREL STA 1277 INTERCOSTAL PRIMARY ATTACH BRACKET CRACKED. AS MARKED. ACCESS THRU CLG OR CAC. REMOVED AND REPLACED CRACKED BRACKET P/N AYB7035-12 AS PER S.R.M. 51/00/01, 51/33/01. REF.N/R N00612 2L73 4F RTA22WE 20050719000052005071900005SO 2005 7 19 SIMA200516802 120050605A5330 SKIN EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21647AE11585 145222 DENT IN THE FUSELAGE BETWEEN STRINGER 20R AND 21R AT FRAME 15. REMOVED THE DENT BY MAKING CUTOUT. FABRICATED A FILLER AND DOUBLER. REPAIR DONE IAW SRM. (K) 2L72 4T4 FRTT00011ATTE6CH 20050719000082005071900008SO 2005 7 19 SIMA200516803 120050606A5330 SKIN EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21647AE 145222 HAIL DAMAGE BETWEEN FRAMES 30-31 AND STRINGER 21L AND 21R. PERFORMED CUT OUT OF DAMAGE. FABRICATED A DOUBLER AND FILLER. REPAIR DONE IAW SRM. (K) 2L72 4T4 FRTT00011ATTE6CH 20050719000092005071900009NM 2005 7 19 S2YA05035 120050526A21204068B000002 VALVE DORNERDO32 DO328300 NM FLOW CONTROL INOPERATIVE A S2YAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL13360SK9880 52 3136 BEFORE TAKEOFF ROLL THE CREW GOT A BLEED SOV CAS MESSAGE, THEY CONSULTED WITH MECHANIC AND WERE ABLE TO GET IT TO CLEAR. CREW ATTEMPTED TAKEOFF AGAIN RECEIVED A BLEED SOV CAS MESSAGE. THE AC RETURNED TO THE GATE. MECHANIC REPLACED THE FLOW CONTROL VALVE. WITH NO FURTHER DISCREPANCIES NOTED THE AC WAS RETURNED TO SERVICE. (K) 2H72 4T RTA55NM 20050719000122005071900012NM 2005 7 19 S2YA05022 120050307A5610001A561A0000214 WINDSHIELD DORNERDO32 DO328300 NM PWA 306 PW306B NE COCKPIT FAILED A S2YAA UNSCHED LANDING O OTHER CLCLIMB 1 GL13351SK2898 3108 SHORTLY AFTER TAKEOFF, THE CREW REPORTED THE LT AFT WINDSHIELD HAD SHATTERED IN FLIGHT. CREW MADE AN AIR-TURN-BACK. MECHANIC REPLACED THE WINDSHIELD AND RETURNED THE AC TO SERVICE. (K) 2H72 4T4 FRTA55NM E35NE 20050719000152005071900015NM 2005 7 19 S2YA05025 120050412A51003283074 CONTROL PANEL DORNERDO32 DO328300 NM PWA PT6 PT6A67D NE COCKPIT INOPERATIVE A S2YAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL13351SK9888 1167 3108 DURING TAXI THE CREW GOT A LAVATORY SMOKE DETECTOR INDICATION. CRASH-FIRE-RESCUE MET THE AC AT THE GATE AND THE PASSENGERS WERE DEPLANED. MECHANIC INSPECTED THE AC AND FOUND NO INDICATION OF FIRE OR SMOKE. MECHANIC REPLACED THE OXYGEN/ECS WITH APU PANEL AND RETURNED THE AC TO SERVICE. (K) 2H72 4T4 TRTA55NM E26NE 20050719000162005071900016NM 2005 7 19 S2YA05033 120050519A2400230G02Y04 PANEL DORNERDO32 DO328300 NM PWA 306 PW306B NE LEFT FAILED A S2YAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL13356SK6393 3163 DURING FLIGHT, THE CREW REPORTED A LT GENERATOR FAIL MESSAGE. CREW CONSULTED WITH DISPATCH AND MADE AN AIR-TURN-BACK. MECHANIC SWAPPED LT AND RT GENERATORS AND ALL OPERATIONAL CHECKS WERE GOOD. DURING TAXI OUT FOR THE NEXT FLIGHT THE LT GENERATOR FAILED. MECHANIC SWAPPED THE LT AND RT HALLEFECT DEVICES AND REPLACED THE 1VE PANEL. PROBLEM HAS NOT RETURNED. 2H72 4T4 FRTA55NM E35NE 20050719000172005071900017NM 2005 7 19 S2YA05028 120050424A36004067B000004 SHUTOFF VALVE DORNERDO32 DO328300 NM PWA 306 PW306B NE BLEED SYSTEM INOPERATIVE A S2YAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL13359SK10021 3202 DURING TAKEOFF OF FLIGHT, THE CREW REPORTED LOW PRESSURE BLEED SOV FAIL CAS MESSAGE AFTER POWER UP FOR TAKE OFF. THE CREW ABORTED THE TAKEOFF AND RETURNED TOT HTE GATE. MECHANIC INSPECTED THE SYSTEM AND REPLACED LT PACK FLOW CONTROL VALVE BUT THE SYSTEM STILL OPS CHECKED BAD. MECHANIC THEN SWAPPED THE LT AND RT LOW PRESSURE VALVES (PRSOV) AND OPS CHECKED GOOD. MECHANIC RETURNED THE AC TO SERVICE. AS OF 05/11/05, PROBLEM HAS NOT RETURNED. (K) 2H72 4T4 FRTA55NM E35NE 20050719000182005071900018NM 2005 7 19 S2YA05027 120050412A2150 A/C PACK DORNERDO32 DO328300 NM PWA 306 PW306B NE CABIN AIR INOPERATIVE A S2YAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL13360SK 3136 DURING FLIGHT, THE CREW REPORTED BOTH LT AND RT PACKS WHERE INOPERATIVE. AFTER DISCUSSING THE SITUATION WITH MECHANIC AND DISPATCH THE PACK WERE STILL INOPERATIVE. THE DISPATCHER DETERMINED THAT AC WOULD HAVE TO MAKE A FUEL STOP TO MAKE IT, SO THE CREW PERFORMED AN AIR-TURN-BACK. MECHANIC WERE UNABLE TO DUPLICATE THE PROBLEM HAS NOT RETURNED. (K) 2H72 4T4 FRTA55NM E35NE 20050719000202005071900020 2005 7 19 S2YA05026 420050412A34226226136002 GYRO BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE NR 2 MALFUNCTIONED A S2YAA UNSCHED LANDING O OTHER CLCLIMB 1 GL13801S 1561 UE80 AFTER TAKEOFF, THE CREW REPORTD THE FO EHSI AND THE CA RMI FROZEN AT 320 DEGREE HEADING. THE CREW PERFORMED AN AIR-TURN-BACK. MECHANIC INSPECTED THE AC BUT COULD NOT DUPLICATE THE PROBLEM. MECHANIC REPLACED THE NR 2 DIRECTIONAL GYRO FOR TROUBLESHOOTING AND RETURNED THE AC TO SERVICE. (K) 2L72 4T4 TRTA24CE E26NE 20050719000212005071900021NM 2005 7 19 S2YA05031 120050511A329747051 CONNECTOR DORNERDO32 DO328300 NM PWA 306 PW306B NE NLG FAILED A S2YAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 GL13352SK 3111 DURING APPROACH, CREW REPORTED A CAS MESSAGE (NWS POWER UP FAIL) AND EXECUTED A MISSED APPROACH. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT WITH FREE CASTERING NOSE WHEEL. OUTSTATION MECHANIC VISUALLY INSPECTED THE NOSE GEAR, RERACKED THE NWS ECU AND REPLACED BULBS ON THE NWS CAPSULE SWITCH. WITH OPS CHECKS GOOD THE AC WAS RETURNED TO SERVICE. DURING THE NEX FLIGHT, CREW REPORTED BOTH NWS FAIL AND NWS POWER UP FAIL ON LANDING. MECHANIC INSPECTED THE SYSTEM, CLEANED THE FEEDBACK POTENTIOMETER AND FOUND THE A3 PIN AT THE NEW NWS SWITCH WAS BAD. MECHANIC REPLACED THE CONNECTOR AND OPERATIONALLY CHECK AC WITH NO FURTHER DEFECTS. (K) 2H72 4T4 FRTA55NM E35NE 20050719000242005071900024NM 2005 7 19 ASMF200507010 120050712A274095906 MOTOR DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE STAB TRIM FAILED W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23831LF 53050 DURING TRANSIT SERVICE, IN GROUND TEST THE HORIZONTAL STABILIZER MOTOR DID NOT MOVE. THE ACTUATOR AND PRIMARY MOTOR WERE REPLACED IAW MM 27-40-01, BUT FAILURE CONTINUED. AIRCRAFT WAS SENT TO THE HANGAR AND ANOTHER ACTUATOR AND PRIMARY MOTOR WAS INSTALLED, THE CONDITION OF P10-63 WAS CHECKED, THE OPERATION OF RELAYS R20-15, R20-17 AND R20-18 WERE VERIFIED, CONTINUITY AND ISOLATION TO GROUND WERE VERIFIED IAW MM 27-40-01 AND WDM 27-041-01 RESPECTIVELY, TESTED CORRECT. 2L72 4F4 FRT E9NE 20050719000252005071900025WP 2005 7 19 ASMF200507007 120050708A5270 PROXIMITY SWITCH DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE PAX DOOR OUT OF ADJUST W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23803ML 49726 AIRCRAFT RETURNED TO PLATFORM, PASSENGER DOOR LIGHT COME ON. PASSENGER DOOR TEST WAS PERFORMED WITH A COMPLETE OPEN/CLOSE CYCLE IAW MM, BEING CORRECT. DURING OVERNIGHT SERVICE, THE GAP BETWEEN PRINTED CIRCUIT AND PROXIMITY SWITCH OF PASSENGER DOOR WAS VERIFIED IAW MM 52-70-03, BEING CORRECT. 2L72 4F4 FRTA6WE E9NE 20050719000262005071900026NM 2005 7 19 ASAA0510165 120050614A5320654795710 ANGLE BOEING737 737290C 138448VNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX - FOUND U-CHANNEL AT AFT CARGO PIT DOOR SILL HAS ELONGATED HOLES FROM PREVIOUS REPAIR. REMOVED AND REPLACED U-CHANNEL IAW B737-200 SRM. (M) 2L72 4F A16WE 20050719000272005071900027NM 2005 7 19 ASAA0510159 120050613A5753 SKIN BOEING737 737290C 138448VNM TE FLAP DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 129 23136 YXX - IMPACT DAMAGE ON OUTBOARD T/E O RIGHT INBOARD MID FLAP. RIGHT INBOARD MID FLAP IMPACT DAMAGE LOCATION REPAIRED IAW B737-200 SRM 51-40-20 REPAIR NR 2. (M) 2L72 4F A16WE 20050719000282005071900028NM 2005 7 19 ASAA0510151 120050613A5320654795715 FLOOR SUPPORT BOEING737 737290C 138448VNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX - FOUND FLOOR SUPPORT FORMER AT BS 801 RBL 21 ELONGATED HOLES. REMOVED AND REPLACED FORMER IAW B737-200SRM. (M) 2L72 4F A16WE 20050719000292005071900029NM 2005 7 19 ASAA0510153 120050613A5320654795717 FLOOR SUPPORT BOEING737 737290C 138448VNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX - FOUND FLOOR SUPPORT FORMER AT BS 813 RBL 21 ELONGATED HOLES. REMOVED AND REPLACED FORMER IAW B737-200 SRM. (M) 2L72 4F A16WE 20050719000302005071900030NM 2005 7 19 ASAA0510164 120050614A531365457769 STRINGER BOEING737 737290C 138448VNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX - FOUND CRACKED STRINGER AT BS 836 STRINGER 26R. REMOVED AND REPLACED STRINGER 26R IAW B737-200 SRM. (M) 2L72 4F A16WE 20050719000312005071900031NM 2005 7 19 ASAA0510163 120050614A57546546421228A WEDGE BOEING737 737290C 138448VNM NR 6 SLAT DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX - FOUND RIGHT NR 6 SLAT T/E WEDGE UPPER SURFACE HAS A DENT AT SLAT STATION 346.53 AND 4.5 INCH FROM T/E. PERMANENT REPAIR COMPLETED IAW B737-200 SRM 51-40-20 REPAIR 7 FIG 16. (M) 2L72 4F A16WE 20050719000352005071900035NM 2005 7 19 ASAA0510146 120050613A532269353501 SHEAR TIE BOEING737 737290C 138448VNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX- SHEAR TIE CRACKED AT BS 787 STRINGER 26R AT HOLE. REPLACED SHEAR TIE IAW B737-200 SRM. (M) 2L72 4F A16WE 20050719000372005071900037NM 2005 7 19 ASAA0510147 120050613A5753 SKIN BOEING737 737290C 138448VNM FLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX - FOUND RIGHT INBOARD FLORE FLAP DENTED AND DELAMINATED AT OLD REPAIR AT BL 118. RIGHT INBOARD FORE FLAP AT WBL 118 DENTED AND DELAMINATED LOCATIONS REPAIRED IAW 737-200SRM. (M) 2L72 4F A16WE 20050719000392005071900039NM 2005 7 19 ASAA0510162 120050614A57546546421228A WEDGE BOEING737 737290C 138448VNM NR 6 SLAT DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX - FOUND RIGHT NR 6 SLAT T/E WEDGE UPPER SURFACE HAS A DENT AT SLAT STATION 359.03 AND 1.5 INCHES FROM T/E. PERMANENT REPAIR COMPLETED IAW B737-200 SRM 51-40-20 REPAIR 11 FIG 20. (M) 2L72 4F A16WE 20050719000402005071900040NM 2005 7 19 ASAA0510148 120050613A53406547957503 ATTACH ANGLE BOEING737 737290C 138448VNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX - FOUND INTERCOSTAL ATTACH ANGLE AT BS 791 CRACKED BETWEEN STRINGER 25-26 RT. ATTACH ANGLE REPLACED FROM BS 767-867. (M) 2L72 4F A16WE 20050719000412005071900041NM 2005 7 19 ASAA0510150 120050613A5320654795714 FLOOR SUPPORT BOEING737 737290C 138448VNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX - FOUND FLOOR SUPPORT FORMER AT BS 793 RBL 21 ELONGATED HOLES. REMOVED AND REPLACED FORMER IAW B737-200SRM. (M) 2L72 4F A16WE 20050719000422005071900042NM 2005 7 19 ASAA0510152 120050613A5320654795716 FLOOR SUPPORT BOEING737 737290C 138448VNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX - FOUND FLOOR SUPPORT FORMER AT BS 810 810 RBL 21 ELONGATED HOLES. REMOVED AND REPLACED FORMER IAW B737-200 SRM. (M) 2L72 4F A16WE 20050719000432005071900043NM 2005 7 19 ASAA0510169 120050614A534069353501 STRINGER CLIP BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX - FOUND AFT CARGO PIT TIE CLIP HAS CORROSION AT BS 747 AND STRINGER 26R. REMOVED AND REPLACED TIE CLIP AT AFT CARGO BS 747 AND 26R IAW B737-200 SRM. (M) 2L72 4F A16WE 20050719000442005071900044WP 2005 7 19 ASAA0580184 120050404A532199365831 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSLEAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02950AS 53023 OKC - FOUND C-CHECK, CABIN FLOOR PANEL IS PUNCTURED AND CRACKED. REPLACED PANEL. (M) 2L72 4F RTA6WE 20050719000452005071900045WP 2005 7 19 DXTA200500823 220050707A720030751604 ENGINE RAYTHNDH125 HAWKER800XP 7150012CE GARRTTTFE731TFE7315BR WP NR 1 VIBRATION E DXTAEAD ENGINE SHUTDOWN UNSCHED LANDING RETURN TO BLOCK EB VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07864QS3053 258564 P107672 ENG NR 1 SHUTDOWN INFLIGHT DUE TO ENGINE VIBRATION, BUZZING AND A STRONG ODOR OF SMOKE. REMOVED NR 1 ENGINE P/N TFE731-5BR-IH S/N P-107672 WITH TOTAL TIME 3052.8 AND TOTAL CYCLES 2099. INSTALLED SERVICEABLE ENGINE P/N TFE731-5BR-IH S/N P-107777 WITH TOTAL TIME 1895.8 AND TOTAL CYCLES 1289. COMPLIED WITH POST INSTALLATION NS AND CHECKS IAW TFE731-5BRL MM 72-02-96 REV 7 AND AIRCRAFT FLIGHT MANUAL. NO DEFECTS NOTED. 2L72 4F4 FRTA3EU E6WE 20050719000462005071900046NM 2005 7 19 ASAA0540219 120050504A5340693535214 STRINGER CLIP BOEING737 737490 1384715NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02792AS 28887 PAE - FOUND STRINGER CLIP CRACKED. REMOVED AND REPLACED STRINGER CLIP. (M) 2L72 4F RTA16WE 20050719000472005071900047WP 2005 7 19 ASAA0580279 120050516A5320 CUSP WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02968AS 53016 OKC - FOUND DURING HV CHECK, RIGHT FLOOR CUSP WEB CORRODED AT STATION 1102-1105. REMOVED DAMAGED SECTION. INSTALLED WEB AND DOUBLER. (M) 2L72 4F RTA6WE 20050719000482005071900048WP 2005 7 19 ASAA0580281 120050516A53209957918523 CHANNEL DOUG DC9 DC983 3022083WP FUSELAGE BROKEN A ASAAK NONE O OTHER ININSP/MAINT 1 NM02968AS 53016 OKC - DURING HV-CHECK, RIGHT FLOORBOARD 4 E HAT CHANNEL HAS BROKEN FASTENER HOLE. REMOVED DAMAGED SECTION. INSTALLED REPLACEMENT HAT CHANNEL SECTION AND SPLICE. (M) 2L72 4F RTA6WE 20050719000492005071900049WP 2005 7 19 ASAA0580141 120050228A53475930565 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 OKC - FOUND DURING HV CHECK, FALSE SEAT TRACK CORRODED. REPLACED TRACK. (M) 2L72 4F RTA6WE 20050719000502005071900050NM 2005 7 19 ASAA0510088 120050420A2810654542854 FUEL TANK BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 YXX - FOUND FUEL CENTER TANK CORRODED AT UPPER STRUCTURE AT BS 578 LBL 67. CORROSION REMOVED IAW EA 5710-01119. (M) 2L72 4F A16WE 20050719000512005071900051NM 2005 7 19 ASAA0510129 120050413A531165465647 FAILSAFE BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX - FRAME FAILSAFE CORRODED AT BS 986 STRINGER 21L. REPAIRED IAW B737-200 SRM 51-40-3 FIG 1. (M) 2L72 4F A16WE 20050719000522005071900052WP 2005 7 19 ASAA0580275 120050516A53119919603507 FRAME DOUG DC9 DC983 3022083WP FS CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02968AS 53016 OKC - DURING HV-CHECK, FRAME AT STATION 1231 LONGERON 30 AND 29R IS CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLER, WEB, AND ANGLES. (M) 2L72 4F RTA6WE 20050719000542005071900054NM 2005 7 19 ASAA0540163 120050516A532065479577 THRESHOLD BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02794AS 28889 PAE - AFT CARGO BAY, DOOR THRESHOLD CORRODED UPPER SURFACE BS 794-834, RBL 25 TO 34, WL 156. REPLACED AFT CARGO BAY DOOR THRESHOLD UPPER SURFACE BS 794-834, RBL 25-34, WL 156. (M) 2L72 4F RTA16WE 20050719000562005071900056NM 2005 7 19 ASAA0540184 120050316A575465C2668537 WEDGE BOEING737 7374Q8 138447QNM NR 2 SLAT DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02764AS 25101 OKC - FOUND LEFT WING NR 2 L/E NR 2 SLAT T/E WEDGE IS DELAMINATED AT OUTBOARD END AND EDGE POTTING DETERIORATED AT THE INBOARD END. REMOVED DAMAGE FABRICATED AND INSTALLED A REPAIR CORE AND DOUBLER IAW B737 SRM 51-70-10 REPAIR 7. (M) 2L72 4F RTA16WE 20050719000592005071900059NM 2005 7 19 ASAA0510135 120050613A5753657194034 SKIN BOEING737 737290C 138448VNM FORE FLAP CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX - FOUND RIGHT INBOARD FORE FLAP CHAFED ON INBOARD TOP SURFACE AT WBL 83. RIGHT INBOARD FORE FLAP INBOARD TOP SURFACE CHAFED LOCATION REPAIRED IAW B737-200 SRM 51-40-20 REPAIR 7 FIG 16 WBL 83. (M) 2L72 4F A16WE 20050719000612005071900061NM 2005 7 19 ASAA0510145 120050613A5313654655116 STRINGER BOEING737 737290C 138448VNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX- CRACKED FRAME AT BS 805 OUTBOARD STRINGER 26R. REPAIRED IAW B737-200SRM. (M) 2L72 4F A16WE 20050719000632005071900063NM 2005 7 19 ASAA0540187 120050317A5230H41423 CASTING BOEING737 737490 1384715NM CARGO DOOR GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02791AS 28886 PAE - FOUND AFT CARGO DOOR EXTERNAL DOOR HANDLE HOUSING IS GOUGED. REMOVED AND REPLACED HOUSING. (M) 2L72 4F RTA16WE 20050719000652005071900065NM 2005 7 19 ASAA0540242 120050512A5311 FRAME BOEING737 737490 1384715NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02792AS 28887 PAE - FOUND FRAME CRACKED AT HAT RACK ATTACH POINT. REPAIRED FRAME AT HAT RACK ATTACH POINT. (M) 2L72 4F RTA16WE 20050719000672005071900067NM 2005 7 19 ASAA0540215 120050427A53306545776 SKIN BOEING737 737490 1384715NM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02799AS 29270 SEA - FOUND DENT AT BS 787 STRINGER 27L TO 27R. DENT IS OUT OF LIMITS IAW WITH THE 737 SRM 53-00-01 FIG 101. DENT IS COMMON TO A STRINGER A=4, Y=.126, A/Y=31.75. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW ASA EA 5330-01929 AND AAR EA 10927. (M) 2L72 4F RTA16WE 20050719000692005071900069WP 2005 7 19 ASAA0580202 120050404A53305910382511 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02950AS 53023 OKC - DURING C-CHECK, FOUND AIRSTAIR EXTERIOR SKIN IS DENTED. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050719000712005071900071WP 2005 7 19 ASAA0580246 120050509A53305911408545 SKIN DOUG DC9 DC983 3022083WP FUSELAGE LIGHTNING STRIKEA ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - DURING C-CHECK, FOUND FUSELAGE SKIN HAS LIGHTNING STRIKE AT STATION 275 BETWEEN L1 AND L2. REMOVED DAMAGE INSTALLED SKIN AND DOUBLER. (M) 2L72 4F RTA6WE 20050719000732005071900073NM 2005 7 19 ASAA0540168 120050313A5340693532Y1 STRINGER CLIP BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02764AS 25101 OKC - FOUND RIGHT STRINGER 11R AT BS 1007 STRINGER CLIP IS CRACKED. REMOVED DAMAGED STRINGER CLIP, ORDERED AND INSTALLED A NEW STRINGER CLIP IAW B737 SRM. (M) 2L72 4F RTA16WE 20050719000752005071900075NM 2005 7 19 ASAA0510090 120050502A5322654659519 SHEAR TIE BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX - AFT CARGO BS 727A STRINGER 19L TO STRINGER 20L SHEAR TIE CORRODED. REPLACED CORRODED SHEAR TIE. (M) 2L72 4F A16WE 20050719000762005071900076WP 2005 7 19 ASAA0580271 120050516A532099305388 CUSP WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02968AS 53016 OKC - DURING HV CHECK, RIGHT CUSP WEB CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050719000772005071900077NM 2005 7 19 ASAA0540182 120050316A5754 WEDGE BOEING737 7374Q8 138447QNM NR 4 SLAT DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02764AS 25101 OKC - FOUND RIGHT WING NR 4 L/E SLAT INBOARD SIDE OF TRAILING EDGE WEDGE HAS SLIGHT DELAMINATION AND INBOARD AND OUTBOARD EDGE POTTING IS DETERIORATED. REMOVED DAMAGE FABRICATED AND INSTALLED A REPAIR CORE AND DOUBLER IAW B737 SRM 51-70-10 REPAIR 7. (M) 2L72 4F RTA16WE 20050719000782005071900078NM 2005 7 19 ASAA0510166 120050614A531469374601 KEELBEAM BOEING737 737290C 138448VNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX - FOUND BS 535 BETWEEN LEFT AND RIGHT KEEL BEAMS SUPPORT ANGLES HAS LOW EDGE MARGIN AT FASTENER HOLE. REMOVED AND REPLACED ANGLE IAW B737-200 SRM. (M) 2L72 4F A16WE 20050719000792005071900079NM 2005 7 19 ASAA0540185 120050317A52306547952358 SKIN BOEING737 737490 1384715NM CARGO DOOR CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02791AS 28886 PAE - AFT CARGO DOOR HAS AREAS OF CORROSION ON INTERNAL SKIN. REPAIRED INTERNAL SKIN. (M) 2L72 4F RTA16WE 20050719000802005071900080NM 2005 7 19 ASAA0540233 120050510A53206517688U180 SILL BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02792AS 28887 PAE - FOUND CORROSION FORWARD ENTRY DOOR MOP SILL AT BS 310-344, LBL 56, WL 208. REMOVED AND REPLACED FORWARD ENTRY DOOR MOP SILL. (M) 2L72 4F RTA16WE 20050719000812005071900081NM 2005 7 19 ASAA0540238 120050511A53226546549509 SHEAR TIE BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02792AS 28887 PAE - FOUND CORROSION ON SHEAR TIE. BLENDED SHEAR TIE, FOUND TO BE OUT OF LIMITS, FABRICATED AND INSTALLED A REPAIR PER SRM. (M) 2L72 4F RTA16WE 20050719000832005071900083NM 2005 7 19 ASAA0540243 120050512A531165465265 FRAME BOEING737 737490 1384715NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02792AS 28887 PAE - FOUND FRAME CRACKED AT HAT RACK ATTACH POINT. REMOVED DAMAGED ARM, FABRICATED REPAIR PARTS AND INSTALLED. (M) 2L72 4F RTA16WE 20050719000852005071900085NM 2005 7 19 ASAA0510167 120050614A532069353521 STRINGER CLIP BOEING737 737290C 138448VNM FUSELAGE CRACKED A ASAAO OTHER O OTHER NRNOT REPORTED 1 NM02742AS 23136 YXX - FOUND AFT CARGO TIE CLIP CRACKED AT BS 787 STRINGER 24R. REMOVED AND REPLACED TIE CLIP IAW B737-200 SRM. (M) 2L72 4F A16WE 20050719000872005071900087WP 2005 7 19 ASAA0580183 120050404A532199366401 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02950AS 53023 OKC - FOUND DURING C-CHECK, CABIN FLOOR PANEL IS DELAMINATED. REPLACED PANEL. (M) 2L72 4F RTA6WE 20050719000892005071900089WP 2005 7 19 ASAA0580251 120050509A5311993607317 FRAME DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - FOUND DURING C-CHECK, FRAME CORRODED AT STATION 1212. REMOVED DAMAGE AND INSTALLED A REPAIR ANGLE. (M) 2L72 4F RTA6WE 20050719000912005071900091WP 2005 7 19 ASAA0580252 120050509A532199365491 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - DURING C-CHECK, FOUND FLOORBOARD STATION 160 IS DELAMINATED. REMOVED AND REPLACED FLOORBOARD. (M) 2L72 4F RTA6WE 20050719000932005071900093WP 2005 7 19 ASAA0580222 120050509A53219936537501 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - FOUND DURING C-CHECK, CABIN FLOOR PANEL DELAMINATING. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050719000952005071900095WP 2005 7 19 ASAA0580276 120050516A5320993053886 CUSP WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02968AS 53016 OKC - FOUND HV CHECK, RIGHT FLOOR CUSP WEB CORRODED AT STATION 256-275. REMOVED DAMAGED SECTION. INSTALLED WEB AND DOUBLER. (M) 2L72 4F RTA6WE 20050719000972005071900097NM 2005 7 19 ASAA0540175 120050312A5320654769020 SUPPORT BOEING737 737490 1384715NM FS CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02794AS 28889 PAE - FOUND AFT CARGO BAY, FLOOR TO SIDEWALL SUPPORT CORRODED. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT. (M) 2L72 4F RTA16WE 20050719001002005071900100NM 2005 7 19 ASAA0540244 120050512A5320654795731 INTERCOSTAL BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02705AS 29318 PAE - AFT CARGO BAY, INTERCOSTAL UPPER FLANGE CORRODED. REMOVED AND REPLACED INTERCOSTAL PER SRM. (M) 2L72 4F RTA16WE 20050719001032005071900103NM 2005 7 19 ASAA0510066 120050404A534065465349 ATTACH FITTING BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 YXX - FRAME ATTACHMENT CORRODED AT BS 520 BETWEEN STRINGER 28L AND 28R. REPLACED SKIN TO FRAME ATTACHMENT IAW B737-200 SRM 51-10-1 PARAGRAPH 9A AND 51-30-2 FIGURE 3. (M) 2L72 4F A16WE 20050719001042005071900104NM 2005 7 19 SB05082 120050713A335020131A BATTERY PACK BOEING737 737301 1384611NM EMERGENCY LIGHTSDISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19558AU 23512 MAINTENANCE REPORTED FORWARD SERVICE DOOR EXTERIOR EMERGENCY EXIT LIGHT AND FIRST CLASS EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED FORWARD EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050719001052005071900105NM 2005 7 19 ASAA0510068 120050415A532265221611 SHEAR TIE BOEING737 737290C 138448VNM FS DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 YXX - BS 520 FRAME TO SKIN ATTACHMENT AT STRINGER 28L TO STRINGER 27 HAS LOW EDGE MARGIN. REPLACED ATTACHMENT PER B737-200 SRM 53-10-4 FIGURE 6. (M) 2L72 4F A16WE 20050719001072005071900107WP 2005 7 19 ASAA0580231 120050509A532199365851 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - FOUND DURING C-CHECK, CABIN FLOORBOARD IS PUNCTURED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050718000302005071800030WP 2005 7 18 ASAA0580289 120050516A53305953050513 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02968AS 53016 OKC - FOUND HV CHECK, FOUND DENT IN FUSELAGE NEAR FORWARD LAV SERVICE DOOR, LENGTH 1.640625 BY 1.390625 WIDE BY .171875 DEEP. REMOVED DAMAGE AND REPLACED WITH FILLER AND DOUBLER. (M) 2L72 4F RTA6WE 20050718000342005071800034NM 2005 7 18 ASAA0510139 120050613A531565538446 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX - AFT CARGO PIT FLOOR SUPPORT BEAM TIE DOWN AREA AND ANCHOR NUT HOLES HAVE CORROSION AT BS 787 RBL 14. FLOORBEAM SECTION REPLACED IAW B737-200 SRM. (M) 2L72 4F A16WE 20050718000372005071800037NM 2005 7 18 ASAA0540186 120050317A5230 SKIN BOEING737 737490 1384715NM CARGO DOOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02791AS 28886 PAE - AFT CARGO DOOR REQUIRES RE-SKIN DO TO NUMEROUS DENTS. REPLACED SKIN. (M) 2L72 4F RTA16WE 20050718000452005071800045WP 2005 7 18 ASAA0580280 120050516A5320993051225 CUSP WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02968AS 53016 OKC - FOUND DURING HV CHECK, RIGHT FLOOR CUSP WEB CORRODED AT STATION 1057-1060. REMOVED DAMAGED SECTION. INSTALLED A REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050718000492005071800049SW 2005 7 18 PNSA050702 120050709A5280 HINGE BRACKET FRCHLDSA227 SA227DC 3377521SW NLG OUT OF ADJUST A PNSAL ABORTED APPROACH SW AFFECT SYSTEMS INADEQUATE Q C DEDESCENT 1 AL03892DC DC892B ON DESCENT FOR LANDING, NLG WOULD NOT COME OUT OF GEAR WELL. AFTER SEVERAL ATTEMPTS, GEAR CAME DOWN AND LOCKED. MAINTENANCE FOUND LT NLG CATCHING AND NOT ALLOWING NOSE GEAR TO COME DOWN. AIRCRAFT FERRIED WITH GEAR DOWN. PRECEDING NIGHT, LT NOSE GEAR HINGE BRACKETS REPLACED DURING A SCHEDULED 5L GEAR CHECK. AFTER AIRCRAFT FERRIED, HINGE BRACKETS AND NOSE GEAR DOOR REPLACED AND AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA18SW 20050718000502005071800050WP 2005 7 18 ASAA0580223 120050509A532199365441 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - FOUND DURING C-CHECK, FORWARD ENTRY FLOOR PANEL CORE DAMAGED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050718000522005071800052WP 2005 7 18 ASAA0580244 120050509A532199365521 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - FOUND DURING C-CHECK, FLOORBOARD HAS THREE CORRODED INSERTS. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050718000562005071800056WP 2005 7 18 ASAA0580235 120050509A53219936550501 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - FOUND DURING C-CHECK, CABIN FLOORBOARD HAS TWO PUNCTURES AND IS DELAMINATED. REMOVED AND REPLACED FLOORBOARD. (M) 2L72 4F RTA6WE 20050718000732005071800073NM 2005 7 18 ASAA0540179 120050316A575365521411 WEDGE BOEING737 7374Q8 138447QNM TE FLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02764AS 25101 OKC - FOUND RIGHT INBOARD TE MID FLAP WEDGE DENTED WITH A CRACK. REMOVED DAMAGE FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW B737 SRM 51-70-10. (M) 2L72 4F RTA16WE 20050718000832005071800083NM 2005 7 18 ASAA0510091 120050427A521069391821 GUIDE BOEING737 737298C 1384490NM R2 DOOR DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02745AS 20794 ANC - R2 DOOR NEEDS TO BE LIFTED TO CLOSE PROPERLY. REPLACED ROLLER GUIDE PLATE ASSEMBLY, BEARING AND GUIDE ARM REF BMM 52-41-0, P/N 69391821, 66145111, 66145266. (M) 2L72 4F RTA16WE 20050718000842005071800084NM 2005 7 18 HNAA0500065 120050711A528083231027001 ROD DHAV DHC8 DHC8102 2809003NM MLG DOOR OUT OF ADJUST A HNAAO OTHER O OTHER CLCLIMB 1 EA07805EX3638336383 228 LT MAIN FRONT GEAR DOOR REMAINS OPEN ABOUT 2 IN WITH GEAR RETRACTED. ADJUSTED DOOR ROD. 2H72 4T RTA13NM 20050718000972005071800097NM 2005 7 18 ASAA0510089 120050420A5313654576625 STRINGER BOEING737 737290C 138448VNM FS CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 YXX - FOUND STRINGER 13R AT BS 500A PLUS 15 INCHES CRACKED. CRACK REMOVED AT STRINGER 13R BS 500A PLUS 15 INCHES PER EA 5330-01918. (M) 2L72 4F A16WE 20050718001022005071800102WP 2005 7 18 ASAA0580201 120050404A53132913044507 GUSSET DOUG DC9 DC983 3022083WP LONGERON CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02950AS 53023 OKC - DURING C-CHECK, FOUND LONGERON GUSSET CORRODED. REPLACED LONGERON GUSSET. (M) 2L72 4F RTA6WE 20050718001082005071800108WP 2005 7 18 ASAA0580187 120050404A53219932816504 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02950AS 53023 OKC - FOUND DURING C-CHECK, CABIN FLOOR PANEL CORRODED, DISBONDED, AND CRACKED. REPLACED DAMAGED SECTION. REBONDED, STOP DRILLED CRACK, AND INSTALLED A REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050718001232005071800123EA 2005 7 18 SWIA200515245 120050707A2750865D1007 PDU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07409SW 7056 DURING TAXI, AFTER SELECTING FLAPS TO 8 DEGREES FLAPS HALFSPEED STATUS MESSAGE ILLUMINATED. REPLACED PDU IAW 27-52-00 AND FECU IAW 27-50-00. OPERATIONAL CHECK GOOD PN 865D100-7, SN/OFF 162 PN 860D100-18 SN/OFF 768. 2L72 4F RTA21EA 20050718001262005071800126NM 2005 7 18 ASAA0510140 120050613A534065505369 ATTACH ANGLE BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX - AFT CARGO PIT BS 727 BUTT AND STRINGER 26L ATTACHED ANGLE HAS CORROSION. REPAIRED BY REMOVAL AND REPLACEMENT WITH FABRICATED REPAIR PART IAW B737-200 SRM. (M) 2L72 4F A16WE 20050718001272005071800127WP 2005 7 18 ASAA0580226 120050509A53219936545503 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - FOUND DURING C-CHECK, CABIN FLOORBOARD IS CRACKED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050718001392005071800139WP 2005 7 18 ASAA0580287 120050516A532199365811 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02968AS 53016 OKC - DURING HV CHECK, FOUND FLOOR PANEL 6-C IS MISSING SEVERAL INSERTS. REMOVED AND REPLACED FLOORBOARD. (M) 2L72 4F RTA6WE 20050718001612005071800161NM 2005 7 18 ASAA0510067 120050415A532265221611 SHEAR TIE BOEING737 737290C 138448VNM FS DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 YXX - FOUND SHEAR TIE AT BS 480 BETWEEN STRINGER 20L AND 21L HAS LOW EDGE MARGIN. REPLACED WITH FABRICATED REPAIR PART IAW B737-200 SRM 51-30-2 PARA 4. 2L72 4F A16WE 20050718001742005071800174WP 2005 7 18 ASAA0580206 120050404A5330591140733 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02950AS 53023 OKC - FOUND DURING C-CHECK, FUSELAGE SKIN IS CREASED AT REPAIR DOUBLER ON RIGHT SIDE. REPLACED DOUBLER PER EA 5330-01914. (M) 2L72 4F RTA6WE 20050718001872005071800187NM 2005 7 18 05FDEA01876 120050709A5753 HINGE DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 RT WIN, O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. REPAIRED AS PER EA1-5750-87590. 2L73 4F RTA22WE 20050718001882005071800188NM 2005 7 18 05FDEA01877 120050709A5753 HINGE DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 RT WING, O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. REPAIRED AS PER EA1-5750-87590. 2L73 4F RTA22WE 20050718001922005071800192NM 2005 7 18 05FDEA01881 120050709A5753 HINGE DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 RT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. REPAIRED AS PER EA1-5750-87591. 2L73 4F RTA22WE 20050718001982005071800198NM 2005 7 18 05FDEA01884 120050709A5753 HINGE DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 RT WING, O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. REPAIR CARRIED OUT ASPER EA1-5750-87591. 2L73 4F RTA22WE 20050718002012005071800201NM 2005 7 18 05FDEA01887 120050709A5320 BRACKET DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 AFT CARGO BAY STA 1841 LOWER FRAME FWD FLOOR PANEL SUPPORTING BRACKET FOUND CORRODED AS MARKED. AFT CARGO COMPARTMENT, STA 1841 LOWER FRAME FWD FLOOR PANEL SUPPORTING BRACKET REMOVED AS PER SRM 51-33-01 VOL II. NEW STIFFENER FABRICATED AS PER DRAWING AGA 7170 AND NEW STIFFENER INSTALLED AS PER SRM 51-33-01 VOL II. MINOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050718002102005071800210NM 2005 7 18 USAA200507001 120050709A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19385US 22958 CRACK AT BS 767 BETWEEN STRINGERS 21 RT AND 22 RT ON FUSELAGE SKIN. REMOVED DAMAGED FUSELAGE SKIN AND INSTALLED REPAIR DOUBLER PER SRM 53-00-01 FIG 229, DETAIL X. 2L72 4F RTA16WE 20050718002132005071800213NM 2005 7 18 USAA200507004 120050712A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19392US 23314 5 IN CRACK FOUND BETWEEN FRAME 727D AND 727E STR 24L. INSTALLED DOUBLER PER SRM 53-00-01 FIG 229. 2L72 4F RTA16WE 20050718002282005071800228EU 2005 7 18 SA05083 120050711A3350 LIGHT AIRBUSA321 A321211 3930370EU EMERGENCY LIGHTSINOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19179UW 1521 DURING EMERGENCY LIGHT TEST, GREEN LIGHT WOULD NOT ILLUMINATE ON PROGRAMMING AND TEST PANEL. MAINTENANCE REPLACED THE LEFT HAND, AFT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20050718002302005071800230CE 2005 7 18 DXTA200500821 120050707A324199121663 PUMP CESSNA560 560XL 2076702CE BRAKE MALFUNCTIONED E DXTAO OTHER O OTHER LDLANDING 1 GL07610QS1690 5605210 ANTI-SKID AND POWER BRAKE FAILURE. PUMP RUNNING CONTINUOUSLY (BOTH LIGHTS ON). REMOVED BRAKE PUMP AND INSTALLED NEW PUMP. OPERATIONAL CHECKS GOOD. LEAK CHECK GOOD. WORK PERFORMED IAW CH 32-42-06 OF CESSNA 560XL MM. 2L72 4F RTA22CE 20050719000012005071900001NM 2005 7 19 UPS05444910 120050715A3510SR3BJ REGULATOR BOEING747 747SR46 1384816NM OXYGEN SYS INOPERATIVE A IPXAO OTHER O OTHER NRNOT REPORTED 1 SO01680UP 20923 F/O'S 02 REG INOP. R/R F/O REGULATOR PER AMM 35-11-07 OPS CK GOOD 2L74 4F RTA20WE 20050719000022005071900002NM 2005 7 19 05FDEA01867 120050709A5714AYB703512 BRACKET DOUG DC10 DC10 N/A-SDRNM CENTER WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25313 CTR WING LOWER STRUCTURE; RT BARREL STRUCTURE STA 1237 INTERCOSTAL PRIMARY ATTACH BRACKET CRACKED THRU AS MARKED IN RED. ACCESS THRU CLG WHEEL WELL OR CAC0. REMOVED AND REPLACED CRACKED BRACKET P/N AYB7033-10 AS PER S.R.M. 51/00/01, 51/33/01, REF N/R N00611. 2L73 4F RTA22WE 20050719000112005071900011SO 2005 7 19 SIMA200516801 120050602A532014522178005 SILL EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL SERVICE DOOR CORRODED A SIMAO OTHER O OTHER NRNOT REPORTED 1 SW21851AE4916 145734 THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. BLENDED THE CENTER SILL TO REMOVE THE CORROSION. PERFORMED EDDY CURRENT WITH NO REJECTABLE INDICATIONS. FABRICATED 2 DOUBLERS FOR REPAIR. REPAIR DONE IAW SRM. (K) 2L72 4F4 FRTT00011ATTE6CH 20050719000142005071900014CE 2005 7 19 S2YA05023 120050310A32301013880083 VALVE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE MLG INOPERATIVE A S2YAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 GL1391SK 23728 UE91 DURING APPROACH, THE CREW REPORT THEY WHERE UNABLE TO EXTEND THE GEAR. THE CREW EXECUTED A MISSED APPROACH AND MANUALLY EXTENDED THE GEAR ACHIEVED 3 GREEN AND PROCEEDED TO LAND WITHOUT INCIDENT. THE AC WAS INSPECTED AND MECHANIC WAS UNABLE TO DUPLICATE THE PROBLEM. MECHANIC REPLACED THE GEAR SERVICE VALVE FOR TROUBLESHOOTING AND RETURNED AC TO SERVICE. (K) 2L72 4T4 TRTA24CE E26NE 20050719000332005071900033CE 2005 7 19 DXTA200500822 120050707A3260D45C24 SWITCH CESSNA560 560XL 2076702CE NLG FAILED E DXTAAD UNSCHED LANDING RETURN TO BLOCK J WARNING INDICATION CLCLIMB 1 GL07618QS753 5605506 AFTER GEAR RETRACTION, UNLOCK LIGHT REMAINED ILLUMINATED. HYD PRESS AND STAB MISCOMPARE LIGHTS ALSO REMAINED ILLUMINATED. GEAR EXTENDED NORMALLY. UNLOCK LIGHT EXTINGUISHED. STAB MISCOMPARE LIGHT EXTINGUISHED. REMOVED AND REPLACED STBY AIRSPEED SWITCH AND TESTED IAW 27-40-00. LEAK TESTED STANDBY STATIC/PITOT SYSTEM IAW 34-11-09. GEAR OPERATES PROPERLY. PITOT/STATIC SYSTEM LEAK CHECK PERFORMED IAW FAR 91.411 ON 7-9-05. 2L72 4F RTA22CE 20050719000992005071900099CE 2005 7 19 DXTA200500826 120050708A2721S38951 BEARING CESSNA560 560XL 2076702CE RUDDER WORN E DXTAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 GL07636QS 5605304 AIRFRAME VIBRATION ABOVE 260 KIA APPEARS TO BE COMING FROM RUDDER. RUDDER PEDALS DANCING BACK AND FORTH. CAN BE FELT IN YOKE AS WELL. VIBRATION GOES AWAY BELOW 250 KIAS. CHECKED WITH YAW DAMP OFF AND VIBRATION STILL PRESENT. FOUND ELEVATOR AND RUDDER TRIM TAB HORN BEARINGS WORN EXCESSIVELY. BEARINGS REPLACED. 2L72 4F RTA22CE 20050719001152005071900115WP 2005 7 19 ASAA0580227 120050509A532199365531 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE TORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - FOUND DURING C-CHECK, FLOORBOARD HAD TORN OUT INSERTS. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050719001172005071900117NM 2005 7 19 ASAA0540178 120050316A5330654577870 SKIN BOEING737 7374Q8 138447QNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02764AS 25101 OKC - FOUND RIGHT EXIT FUSELAGE SKIN HAS SEVERAL AREAS OF DAMAGE, FS 1007-1010 BETWEEN STRINGER 12R AND 14R CREASE AT FS 1010 AND DENT AT STATION 1007. REMOVED DAMAGED SKIN, FABRICATED AND INSTALLED A REPLACEMENT SKIN PANEL IAW AS EA 5330-01905 AND AAR EA 10857. (M) 2L72 4F RTA16WE 20050719001182005071900118SO 2005 7 19 SIMA200517102 120050608A532014521700007 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21802AE 145471 DURING INSPECTION FOUND LT OMEGA BEAM CORRODED AT FRAME 20. REPAIRED LT OMEGA BEAM AT FRAME 20 IAW SRM, DOUBLER REPAIR. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4F4 FRTT00011ATTE6CH 20050719001202005071900120SO 2005 7 19 SIMA200517104 120050610A532014000421001 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21802AE 145471 DURING INSPECTION, FOUND LT OMEGA BEAM CORRODED BETWEEN FRAMES 22 AND 25. REPAIRED LT OMEGA BEAM BETWEEN FRAMES 22 AND 25 IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4F4 FRTT00011ATTE6CH 20050719001222005071900122SO 2005 7 19 SIMA200517103 120050609A532014000421001 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21802AE 145471 DURING INSPECTION, FOUND RT OMEGA BEAM CORRODED BETWEEN FRAMES 22 AND 25. COMPLETED REPAIR TO OMEGA BEAM IAW SRM DOUBLER REPAIR. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4F4 FRTT00011ATTE6CH 20050719001232005071900123SO 2005 7 19 SIMA200517802 120050624A27303621005009 CONTROL UNIT EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL HORIZONTAL STAB INOPERATIVE A SIMAO OTHER F FLT CONT AFFECTED CRCRUISE 1 SW21824AE 145584 DUAL PITCH TRIM FAILURE. PERFORMED RESET PROCEDURES IN AOM AND PROCEEDED ON WITH NO INCIDENT. REPLACED THE HSCU. OPS CHECK GOOD. AC RETURNED TO SERVICE. (K) 2L72 4F4 FRTT00011ATTE6CH 20050719001242005071900124CE 2005 7 19 DXTA200500832 120050710A2720 RUDDER CESSNA560 560XL 2076702CE FLIGHT CONTROLS MALFUNCTIONED E DXTAAD UNSCHED LANDING RETURN TO BLOCK F FLT CONT AFFECTED CLCLIMB 1 GL07635QS 5605358 ON TAKEOFF ROTATION ACFT YAWED HARD TO LEFT. INSPECTED RIGGING OF RUDDER AND RUDDER TRIM SYSTEM. CHECKED CABLE TENSIONS AND TRAVELS. CHECK GOOD. INSPECTED RUDDER BIAS SYSTEM. OPS CHECKED GOOD. NO DEFECTS NOTED IAW C560XL MM 27-20-05. 2L72 4F RTA22CE 20050719001282005071900128 2005 7 19 SA05084 420050710A2565D30665105 SLIDE AIRBUS320 A320214 3930316EU PAX CABIN READS LOW A USAAK NONE O OTHER ININSP/MAINT 1 EA19104UW157237268 863 DURING INSPECTION, MAINTENANCE FOUND AFT RT SLIDE PRESSURE LOW. MAINTENANCE REPLACED AFT RT DOOR ESCAPE SLIDE. OK FOR SERVICE. 2L72 4F RTA28NM 20050719001292005071900129EA 2005 7 19 SWIA200515249 120050711A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSINOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07709BR 7850 EMERGENCY LIGHTS INOP ROWS 2-5. REPLACED ELECTROLUMINESCENT STRIP AT ROW 2, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050719001302005071900130EA 2005 7 19 SWIA200515250 120050712A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07441SW6998 6998 7602 SPOILERON FAULT MESSAGE ON TAXI. REPLACED RT SPOILERON INBOARD PCU IAW MM 27-62-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050719001312005071900131EA 2005 7 19 SWIA200515251 120050709A2711 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA AILERON TAB MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07953SW 7813 RT WING DOWN AILERON TRIM INTERMITTENT. REPLACED AILERON TRIM SWITCH AS REQUIRED, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050719001342005071900134EA 2005 7 19 SWIA200515254 120050708A274070609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07975SW1152 1152 MACH TRIM CAUTION MSG IN FLIGHT. REPLACED HSTCU REF AMM 27-41-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050719001362005071900136EA 2005 7 19 SWIA200515256 120050707A2750860D10018ABCD CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07443SW6637 6637 7638 FLAPS HALFSPEED STATUS MESSAGE. REPLACED FLAP ELECTRONIC CONTROL UNIT IAW MM 27-51-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050719001382005071900138EA 2005 7 19 SWIA200515258 120050711A5210 FITTING CNDAIRCL600 CL6002B19 1900309EA CABIN DOOR OUT OF ADJUST A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07916SW 7634 MAIN CABIN DOOR WOULD NOT CLOSE. ADJUSTED SPIGOT FITTING IAW AMM TASK 52-11-00-730-801. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050719001402005071900140EA 2005 7 19 SWIA200515260 120050708A27505332D1007 MOTOR-BRAKE UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07959SW 7840 ON TAXI IN, FLAPS 45 TO 30 FOR FLAPS HALFSPEED STATUS MSG. REPLACED RT FLAP BRAKE/MOTOR. OPERATIONAL CHECK GOOD IAW MM 27-24-02. 2L72 4F RTA21EA 20050719001412005071900141EA 2005 7 19 SWIA200515261 120050708A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07951SW 7795 ON TAXI OUT, SPOILERON FAULT STATUS MSG. REPLACED RT INBOARD SPOILERON PCU IAW CRJ MM 27-61-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050719001442005071900144SO 2005 7 19 SWIA200515264 120050704A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO EMERGENCY LIGHTSDISCHARGED A SWIAO OTHER L NO TEST NRNOT REPORTED 1 NM07578SW1041610416 120346 EMERGENCY LIGHTS ALONG ROW 3-5 NOT ILLUMINATING WHILE TESTED. REPLACED CENTER EMERGENCY LIGHT BATTERY PACK IAW 24-33-01. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050719001452005071900145EA 2005 7 19 SWIA200515265 120050705A2750860D10018 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 NM07947SW 7786 ON APPROACH FLAPS SELECTED 30 DEGREES, OVERSPEED FLAP CLACKER SOUNDED. REPLACED FECU. OPERATIONAL CHECK GOOD IAW 27-50-00. 2L72 4F RTA21EA 20050719001462005071900146EA 2005 7 19 SWIA200515266 120050708A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSINOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07426SW 7468 EXIT LIGHT AT GALLEY SERVICE DOOR INOP. RELAMPED EXIT LIGHT AT GALLEY SERVICE DOOR. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050719001472005071900147SO 2005 7 19 SWIA200515267 120050707A27503075001007 CONTROL UNIT EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07268UE3120 3120 120207 FLAP DISAGREEMENT WHEN FLAPS WERE SELECTED TO 45 DEGREES. REPLACED FLAP CONTROL UNIT. OPERATIONAL CHECK GOOD IAW 27-50-00. 2L72 4T RTA31SO 20050719001482005071900148EA 2005 7 19 SWIA200515268 120050709A2740 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAAD UNSCHED LANDING RETURN TO BLOCK FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07597SW 7293 STAB TRIM CH 1 AND CH 2 AND MACH TRIM CAUTION MESSAGES INFLIGHT. REPLACED HSTCU IAW MM 22-41-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050719001492005071900149 2005 7 19 SWIA200515269 420050708A34178220372445 ADC CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07947SW3399 3399 7786 WHEN SELECTED FLAPS TO 30 OR 45 OVERSPEED CLACKER COMES ON UNTIL FLAPS SELECTED TO 20 OR LESS. REPLACED NR 1 ADC IAW 34-13-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050719001502005071900150SO 2005 7 19 SWIA200515270 120050707A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO EMERGENCY LIGHTSDISCHARGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07291SW1084110841 120318 AFT 1/3 OF FLOOR EMERGENCY LIGHTING INOPERATIVE. REPLACED AFT BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050719001522005071900152EU 2005 7 19 SIMA200518604 120050623A53117253814417 FRAME SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE FUSLEAGE DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21301AE 340B301 THE CARGO SIDEWALL FRAME AT STA 686.888 WAS FOUND BENT AND DENTED. RECONTOURED THE FRAME. PREPARED AND INSTALLED REPAIR SECTION OF NEW FRAME. REPAIR DONE IAW SRM. (K) 2L72 4T4 TRTA52EU E8NE 20050719001532005071900153EU 2005 7 19 SIMA200518606 120050623A53157253814451 FLOORBEAM SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE FUSLEAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21301AE21203 340B301 FLOORBEAM AT STA 225.0 WAS FOUND CORRODED. PERFORMED A CUT OUT TO REMOVE THE CORROSION. FABRICATED A FILLER, DOUBLER AND 2 SHIMS. REPAIR DONE IAW SRM. (K) 2L72 4T4 TRTA52EU E8NE 20050719001542005071900154EU 2005 7 19 SIMA200518603 120050622A53117253814417 FRAME SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE FUSLEAGE DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21301AE 340B301 THE CARGO SIDEWALL FRAME AT STA 640 WAS FOUND DENTED. RECONTOURED THE DENT. FABRICATED AND INSTALLED REPAIR SECTION OF NEW FRAME. REPAIR DONE IAW SRM. (K) 2L72 4T4 TRTA52EU E8NE 20050719001552005071900155EU 2005 7 19 USAA050754 120050614A5315D531128120201 FLOORBEAM AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19107US 1052 PIT - S2 - CABIN FLOORBEAM, 2 INCH X 2 INCH AREA, CORROSION; LEVEL 2; TASK JA-220-53500 CABIN FLOORBEAM AT FR 21-23 AT +Y254. REPLACED FLOORBEAM IAW SRM. (K) 2L72 4F4 FRTA28NM E38NE 20050719001562005071900156EU 2005 7 19 SIMA200518602 120050622A53117253813039 FRAME SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21301AE21203 340B301 THE RT SIDEWALL CARGO FRAME AT STA 677 WAS FOUND DENTED. RECONTOURED THE DENT. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SRM. (K) 2L72 4T4 TRTA52EU E8NE 20050719001572005071900157EU 2005 7 19 SIMA200518605 120050623A53157253819039 FLOORBEAM SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21301AE21203 340B301 THE GALLEY FLOOR FRAME AT STA 272 WAS FOUND CORRODED. BLENDED THE DAMAGED AREA TO REMOVE THE CORROSION. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SRM. (K) 2L72 4T4 TRTA52EU E8NE 20050719001582005071900158EU 2005 7 19 SIMA200518607 120050621A53157253813143 FLOORBEAM SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE FUSELAGE DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21301AE21203 340B301 THE CARGO FLOOR FRAME AT STA 710.0 WAS FOUND BENT IN 2 AREAS. RECONTOURED BOTH DENTS. FABRICATED AND INSTALLED 2 DOUBLERS AND 2 ANGLES. REPAIR DONE IAW SRM. (K) 2L72 4T4 TRTA52EU E8NE 20050719001592005071900159EU 2005 7 19 USAA050755 120050614A5320 FLOOR SUPPORT AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19107US18257 1052 PIT- CS1 - FLOOR SUPPORT, 1 INCH DIA X .050 INCH DEEP (6 SPOTS) CORROSION; NO LEVEL OR TASK, FLOOR SUPPORT AT Y765 AND FRAME 67. REPAIRED IAW EA 95741 FOR INTERM REPAIR, THEN FINAL RESTORATION TO REPLACE PART WAS ACCOMPLISHED. (K) 2L72 4F4 FRTA28NM E38NE 20050719001602005071900160EU 2005 7 19 SIMA200518608 120050629A5414AL2024T3 SKIN SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LT NACELLE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21301AE21203 340B301 THE LT IB NACELLE WAS FOUND CHAFED AT THE FILLET FAIRING SEAL CONTACT POINT. BLENDED THE DAMAGED AREA. FABRICATED AND INSTALLED A REPAIR DOUBLER. WORK DONE IAW SRM. (K) 2L72 4T4 TRTA52EU E8NE 20050719001612005071900161NM 2005 7 19 USAA050737 120050607A5754 SKIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU KREUGER FLAP CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19445US40360 24863 CLT - Q3/QX4 - WING L/E SKIN, .2500 INCH CRACK AND DENT; L/E SKIN ABOVE IB KREUGER FLAP. REMOVED DAMAGE AND INSTALLED DOUBLER IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050719001622005071900162EU 2005 7 19 USAA050763 120050614A5315 FLOORBEAM AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19107US 1052 PIT - S2 - FLOORBEAM .5 INCH AREA; CORROSION; LEVEL 2; TASK JA-260-53500, FRAME 16, Y-50. INSTALLED DOUBLED ANGLE AND FILLER IAW SRM. 2L72 4F4 FRTA28NM E38NE 20050719001632005071900163NM 2005 7 19 USAA050736 120050607A5320 ANGLE BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19445US40360 24863 CLT - Q3/QX4 - Z ANGLE, .25 INCH X .25 INCH CORROSION; LEVEL 1; TASK C53-107-01, LBL 60, STA 951-986. REMOVED AND REPLACED REPAIR PARTS IAW EA. (K) 2L72 4F4 FRTA16WE E21EU 20050719001642005071900164SO 2005 7 19 SIMA200517803 120050622A532014522178005 SILL EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21853AE4779 145742 THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED EXISTING SERVICE DOOR SILL, AND INSTALLED NEW SILL IAW SRM. (K) 2L72 4F4 FRTT00011ATTE6CH 20050719001652005071900165SO 2005 7 19 SIMA200517804 120050621A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21853AE4779 145742 THE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. PERFORMED A CUTOUT TO REMOVE THE CORROSION. FABRICATED A DOUBLER, FILLER , PLATE AND 2 SHIMS. REPAIR DONE IAW SRM. (K) 2L72 4F4 FRTT00011ATTE6CH 20050719001662005071900166EU 2005 7 19 SIMA200518601 120050622A53207253721283 WEB SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21301AE21203 340B301 THE REINFORCEMENT WEB AT STA 294 WAS FOUND CORRODED. BLENDED THE DAMAGED AREA TO REMOVE THE CORROSION. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW REPAIR. (K) 2L72 4T4 TRTA52EU E8NE 20050719001672005071900167NM 2005 7 19 ASAA0510121 120050607A532069412608 STIFFENER BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX - FOUND CORROSION ON VERTICAL STIFFENER AT BS 328, RBL 14, WL 150. REPLACED VERTICAL STIFFENER. (M) 2L72 4F A16WE 20050719001682005071900168NM 2005 7 19 ASAA0510173 120050614A531465621252 KEELBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX - FOUND CORROSION ON RIGHT KEEL BEAM AT BS 636. RIGHT KEEL BEAM REPLACED IAW B737-200 SRM. (M) 2L72 4F A16WE 20050719001692005071900169NM 2005 7 19 ASAA0510122 120050607A5753657194034 SKIN BOEING737 737290C 138448VNM FORE FLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX - RIGHT INBOARD FORE FLAP DENTED AND DELAMINATED AT OLD REPAIR AT WBL 118. RIGHT INBOARD FORE FLAP AT WBL 118 DENTED AND DELAMINATED LOCATIONS REPAIRED IAW B737-200 SRM CHAPTER 51-40-20 REPAIR 7 FIGURE 16. (M) 2L72 4F A16WE 20050719001702005071900170NM 2005 7 19 ASAA0510124 120050607A5753657194034 SKIN BOEING737 737290C 138448VNM FORE FLAP CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX - FOUND RIGHT INBOARD FORE FLAP CHAFED DAMAGED ON OUTBOARD TOP SURFACE AT WBL 83. RIGHT INBOARD FORE FLAP, OUTBOARD TOP SURFACE AT WBL 83 CHAFED LOCATIONS REPAIRED IAW B737-200 SRM CHAPTER 51-40-20 REPAIR 7 FIGURE 16. (M) 2L72 4F A16WE 20050719001712005071900171NM 2005 7 19 ASAA0510123 120050607A5753657194034 SKIN BOEING737 737290C 138448VNM FORE FLAP CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX - FOUND RIGHT INBOARD FORE FLAP CHAFED DAMAGED ON OUTBOARD TOP SURFACE AT WBL 181. RIGHT INBOARD FORE FLAP, OUTBOARD TOP SURFACE AT WBL 181 CHAFED LOCATION REPAIRED IAW B737-200 SRM CHAPTER 51-40-20 REPAIR 4 FIGURE 13. (M) 2L72 4F A16WE 20050719001722005071900172NM 2005 7 19 ASAA0510125 120050607A531565465929 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX - FOUND AFT CARGO PIT FLOORBEAM HAS CORROSION ON ANCHOR NUT HOLE AFT OF BS 727B AND LBL 3. REPLACED SUPPORT BEAM. (M) 2L72 4F A16WE 20050719001732005071900173NM 2005 7 19 ASAA0510171 120050614A533065458601138 SKIN BOEING737 737290C 138448VNM FUSLEAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX - FUSELAGE SKIN LEFT BS 262 3.5 INCHES ABOVE NLG DOOR CUTOUT CHAFED. SKIN CHAFED REPAIRED IAW B737-200 SRM. (M) 2L72 4F A16WE 20050719001742005071900174NM 2005 7 19 ASAA0510119 120050607A53226546598138 SHEAR TIE BOEING737 737290C 138448VNM FUSLEAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX - AFT CARGO PIT BS 727A RBL 10 FRAME TO SHEAR TIE CORRODED. REPLACED SHEAR TIE. (M) 2L72 4F A16WE 20050719001752005071900175NM 2005 7 19 ASAA0510120 120050607A53226546548112 SHEAR TIE BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX - FOUND AFT CARGO PIT SHEAR TIE HAS CORROSION OUTBOARD OF RIGHT KEEL BEAM, STRINGER 27R AND BS 747. REPLACED SHEAR TIE. (M) 2L72 4F A16WE 20050719001762005071900176NM 2005 7 19 ASAA0510126 120050607A5340654659616 ATTACH ANGLE BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX - FOUND AFT CARGO PIT BS 727B INBOARD OF RIGHT KEEL BEAM STRINGER 27R, FRAME ATTACHED ANGLE TO FLOOR SUPPORT BEAM HAS CORROSION. ATTACH ANGLE REPLACED. (M) 2L72 4F A16WE 20050719001822005071900182NM 2005 7 19 AALA20050430 120050708A3350BPS73 BATTERY PACK BOEING767 767323 1385205NM EMERGENCY LIGHTSDISCHARGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21381AN 25450 EMERGENCY LIGHTS AT SEAT ROWS 22 TO 24 RT HAND SIDE INOPERATIVE. REPLACED BATTERY PACK FOR SEAT ROWS 22 TO 24 RT HAND SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050719001902005071900190NM 2005 7 19 72300220 120050602A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 CORROSION ON STRINGER ANGLE. 2L73 4F4 FRTA3WE E2EA 20050719001912005071900191NM 2005 7 19 72300221 120050608A5320 TEE FITTING BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 CORROSION ON T-ANGLE. 2L73 4F4 FRTA3WE E2EA 20050719001922005071900192NM 2005 7 19 0500996745 120050428A5420 WEB BOEING747 747222B 1384904NM NR 3 PYLON CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01645NW 23736 DURING H-CHECK, FOUND CRACK IN NR 3 PYLON OB AFT FRAME WEB. REPAIRED PER EA 67-165208. 2L74 4F RTA20WE 20050719001962005071900196NM 2005 7 19 UPS05444885 120050629A534069B620491 FITTING BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 BS 760 LBL 80 HANDLING SUPPORT FTG FOUND CORRODED. CORROSION BLEND OUT 0.020 BY 1.0 BY 1.75 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS. FTG REPLACED AS PER MM 20-51-01. 2L74 4F A20WE 20050719001972005071900197NM 2005 7 19 UPS05444886 120050620A5320 SHEAR PLATE BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 SHEAR PNL AT BS 1170 TO BS 1260, LBL 11 - RBL 11 EDGE CORRODED AND DELAMINATION. CORROSION BLEND OUT 83 BY 22 BY 0.010 IN. SHEAR PNL REPAIRED AS PER HX RS NR R-53-20-35335 AND UPS EO NR B747-5320-22500-A. 2L74 4F A20WE 20050719002002005071900200WP 2005 7 19 UPS05844893 120050625A53154888828501 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 FLOORBEAM VERT ATTACH FITTING CRACKED STA 64 RBL 48. REMOVED CRACKED FITTING AND REPLACED IAW DC-8 SRM 51-1-21D. 2L74 4F RT4A25 20050719002022005071900202WP 2005 7 19 UPS05844895 120050625A534097540242 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE C-1, VERTICAL LEG CRACKED BETWEEN FASTENERS STA 1220 AT LONGERON 27R. REMOVED CRACKED VERT LEG FITTING AND REPLACED IAW DC-8 SRM 51-1-20D AN D 51-1-21. 2L74 4F RT4A25 20050719002042005071900204WP 2005 7 19 UPS05844897 120050626A5312 PRESSURE BLKHD DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE C-1, AFT PRESSURE BULKHEAD IS CRACKED 0.5 IN LONG AT LBL 35 AND 66 IN FROM FLOOR. CUT OUT DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR FILLER IAW DC-8 SRM 53-2-5 FIG 14. THE -27 AND -25 DOUBLERS INSTALLED BY PREVIOUS REPAIR. 2L74 4F RT4A25 20050719002052005071900205WP 2005 7 19 UPS05844899 120050627A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE C-1, RT WING L/E UPPER RIB CRACKED AT XFS 734. STOP DRILL CRACK, FABRICATED, AND INSTALLED REPAIR ANGLE DOUBLER IAW DC -8 SRM 57-2-0 FIG 2 AND 57-3-3 FIG 7. 2L74 4F RT4A25 20050719002242005071900224WP 2005 7 19 UPS05844902 120050628A53203779874512 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE C-1, CRACKED FITTING AT F/S 760 BETWEEN LONGERONS 17 AND 18L. REMOVED CRACKED FITTING AND INSTALLED REPLACEMENT FITTING IAW DC-8 51- 1-20D. 2L74 4F RT4A25 20050719002282005071900228NM 2005 7 19 SWAA052073 120050715A55536547450 FITTING BOEING737 7373H4 1384600NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29613SW 27931 DURING SCHEDULED D-CHECK, FOUND LT & RT VERTICAL STAB ATTACH FITTING FWD & AFT PRIMARY CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER. 2L72 4F RTA16WE 20050719002292005071900229WP 2005 7 19 UPS05844903 120050628A53203779658U502 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE C-1, LT MAIN CABIN INTERIOR LONGERON 10L SPLICE FITTING CRACKED AT FS 860. REMOVED CRACKED SPLICE FITTING AND INSTALLED REPLACEMENT FITTING IAW DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20050719002312005071900231NM 2005 7 19 SWAA052075 120050715A53156546811 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29613SW 27931 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 986, LBL 45 TO RBL 45. REPAIRED FLOORBEAM PER BFG ER. 2L72 4F RTA16WE 20050719002392005071900239WP 2005 7 19 UPS05844904 120050628A53203779659U501 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE C-1, MAIN CABIN INTERIOR LT SIDE F/S 900 LONG 6L SPLICE FITTING CRACKED. REMOVED CRACKED SPLICE FITTING AND INSTALLED REPLACEMENT FITTING IAW DC-8 SRM 51-120D. 2L74 4F RT4A25 20050719002422005071900242WP 2005 7 19 UPS05844905 120050628A53203779659U501 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE C-1, MAIN CABIN STA 900 LONGERON 9R FITTING CRACKED APROX 3.0 IN. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D AND 51-1-21. 2L74 4F RT4A25 20050719002452005071900245NM 2005 7 19 UPS05M44889 120050617A5347 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01255UP 48404 CORROSION ON SEAT TRACK BETWEEN STA 929-STA 969 X=75 SEAT TRACK REPAIR CARRIED OUT BETWEEN STA 909-STA 969 X=75 AS PER SRM 53-70-00 FIG 1 VOL 1 REV 37. 2L73 4F RTA22WE 20050719002482005071900248NM 2005 7 19 05FDEA01920 120050713A531065453132 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 FUSELAGE UPPER LOBE, STRINGER CLIP IS CRACKED, BS 660, STR 8R. REMOVED FABRICATED AND INSTALLED STR. CLIP AT BS 660 STR 8R IAW SRM 51-20-1 & 51-30- 02. 2L73 4F RTA3WE 20050719002512005071900251NM 2005 7 19 DHL2005751002 120050719A3350 LIGHT BOEING727 727264 138408MNM COCKPIT INOPERATIVE A DHLAK NONE O OTHER ININSP/MAINT 1 SO01751DH 22982 FLIGHT DECK EMERG LIGHT INOP. R/R FLIGHT DECK EMERG LIGHT ASSY IAW ASTAR B727 MM 33-50-0 OPS CHECK OK. 2L73 4F A3WE 20050719002532005071900253NM 2005 7 19 UPS05M44906 120050608A5754 SKIN DOUG MD11 MD11 3023602NM LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01255UP 48404 LT WING L/E AT NR 12 SLAT TRACK LOWER SKIN CUTOUT AREA FOUND CRACKED AS MARKED. REPAIR DOUBLER FABRICATED AS PER SRM 57-10-00 FIG 21 VOL 1 REV 37. 2L73 4F RTA22WE 20050719002542005071900254NM 2005 7 19 05FDEA01923 120050713A534065453132 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 FUSELAGE UPPER LOBE, STRINGER CLIP IS CRACKED, BS 680, STR 7R. REMOVED, FABRICATED AND INSTALLED STRINGER CLIP AT BS 680 STR 7R IAW SRM 51-30-02 AND DRAWING 65-45313. 2L73 4F RTA3WE 20050719002552005071900255NM 2005 7 19 UPS05M44907 120050527A5347 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01255UP 48404 CABIN CORROSION ON SEAT TRACK AT STA 919-989 X=8. SEAT TRACK BETWEEN STA 909-989 X=8. REPAIR CARRIED OUT AS PER SRM 53-70 -00 FIG 1 VOL 1 REV 37. 2L73 4F RTA22WE 20050719002562005071900256NM 2005 7 19 UPS05M44908 120050714A3230 LANDING GEAR DOUG MD11 MD11 3023602NM NLG MALFUNCTIONED A IPXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01254UP 48406 NOSE GEAR DOES NOT LOCK IN UP POS. INSPECTED NOSE GEAR AND SHER WELL. NIL DAMAGE NOTED ALL LINKAGE CHK'D AND LUBED. NOSE WHEEL OPERATING OPS NORMAL PER KD-11 AMM 32-50-00 PSEU TEST IN PRIMARY AND ALT ILLE PER MD AMM 32-60-00 2L73 4F RTA22WE 20050719002762005071900276EA 2005 7 19 SWIA200515275 120050714A2740 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07407SW 7034 STAB TRIM FAILED. REPLACED MCU AND HSTA IAW CRJ MM 27-41-0. OPERATIONAL CHECK GOOD, PN 7062-3 SN/OFF 1095 PN 8396-3 SN/OFF 969. 2L72 4F RTA21EA 20050719002772005071900277NM 2005 7 19 SWAA052063 120050715A57536546430189 SKIN BOEING737 7373H4 1384600NM LT WING FOREFLAPDELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29356SW 25251 DURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM. 2L72 4F RTA16WE 20050719002782005071900278NM 2005 7 19 SWAA052064 120050717A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29368SW 26579 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR FWD LOWER CORNER CUTOUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050719002792005071900279 2005 7 19 SWAA052065 420050715A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29395SW 27689 R1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20050719002802005071900280NM 2005 7 19 SWAA052066 120050715A53116546529 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29613SW 27931 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 24R. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20050719002822005071900282EA 2005 7 19 SWIA200515277 120050713A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY MALFUNCTIONED A SWIAO OTHER JN WARNING INDICATION FALSE WARNING NRNOT REPORTED 1 NM07446SW 7666 SMOKE CARGO WARNING AT GATE WHILE LOADING BAGS. CLEARED ON ITS OWN. REPLACED NR 2 CARGO SMOKE DETECTOR IAW 26-15-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050719002832005071900283EA 2005 7 19 SWIA200515278 120050709A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA LAVATORY FALSE INDICATIONA SWIAD RETURN TO BLOCK JN WARNING INDICATION FALSE WARNING TOTAKEOFF 1 NM07969SW AFTER T/O RECEIVED SMOKE/LAV CAUTION MESSAGE. RAN BOTH PACKS FOR 1.5 HOURS ON GROUND. OPERATED ALL CABIN LIGHTS. INSPECTED BALLASTS AND OPERATIONAL CHECK OF LAV SMOKE DETECTORS. NO MESSAGES APPEARED ON EICAS. NO DEFECTS NOTED. 2L72 4F RTA21EA 20050719002842005071900284EA 2005 7 19 SWIA200515279 120050708A2760 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION LDLANDING 1 NM07441SW 7602 SPOILERONS FAULT STATUS MESSAGE AFTER LANDING. REPLACED NR 1 AND NR 2 SECU IAW 27-60-05. OPERATIONAL CHECK GOOD, PN 49-164-05 SN/OFF 343 AND 1052. 2L72 4F RTA21EA 20050719002852005071900285EA 2005 7 19 QXEA200501106 120050712A281079888211 CONTROL PANEL CNDAIRCL600 CL6002C10 1390015EA FUEL SMOKE A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM09605QX5573 2161 10022 SMOKE AND ELECTRICAL ODOR COMING FROM FUEL CONTROL PANEL, RT WING ROOT. REPLACED REFUEL/DEFUEL PANEL IAW 28-25-00-801-A01. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20050719002862005071900286EA 2005 7 19 QXEA200501107 120050711A3600 ODOR CNDAIRCL600 CL6002C10 1390015EA ZONE 300 DETECTED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM09604QX 10019 CREW REPORTS FOUL ODOR IN AIRCRAFT. MAINTENANCE INSPECTED WATER SEPARATION, MIXING MANIFOLD FOR WATER AND SCUM. FOUND POOLED WATER IN BOTTOM. CLEANED OUT WATER. NO OTHER DEFECTS NOTED. NO SCUM NOTED. OPERATIONAL CHECK AND LEAK CHECK OF DUCTING GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20050719002872005071900287SO 2005 7 19 C2XA05CL058 120050717A3260852701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212SO NLG FAILED A C2XAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SW2714920 145380 LOUD RUMBLING SOUND FROM NOSE. CAME SUDDENLY DURING CLIMB-OUT. SOUNDED LIKE NOSE GEAR DOOR OPENED UP. MAINTENANCE INSPECTED AND FOUND NOSE GEAR DOORS WOULD NOT CLOSE ON GEAR RETRACTION. REPLACED NOSE GEAR DOOR PROXIMITY SWITCH. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20050720000032005072000003NM 2005 7 20 USAA050816 120050629A5320 FLOOR SUPPORT BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19441US 24812 CLT - Q5 - FLOOR SUPPORT, 2 INCH X 2 INCH CORROSION, STA 312-328, RBL 13. DEFECTIVE PART REPLACED WITH IDENTICAL PART, REMOVED AND REPLACED STIFFENER SUPPORT IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050720000042005072000004WP 2005 7 20 AMTA200500298 120050322A32331535927109 ACTUATOR LKHEED1011 10113853 5265020WP RROYCERB211 RB211524* NE LT MLG UNSERVICEABLE A AMTAO OTHER J WARNING INDICATION LDLANDING 1 GL11161AT12062 1219 WHEN GEAR WAS LOWERED, AIRCRAFT SHUDDERED AND A LOUD BANG HEARD, LOST C HYD SYSTEM, LT MLG DOWN AND LOCKED LIGHT NEVER CAME ON. RAN APPROPRIATE CHECKLIST A ND LANDED, STOPPED ON RUNWAY 7R TO BE TOWED OFF. FOUND MULTIPLE ITEMS BADLY DAMAGED. REMOVED AND REPLACED MLG RETRACTION ACTUATOR IAW MM. REPLACED DOWNLOCK INDICATOR BRACKET AND CABLE, UPPER UNIVERSAL JURY BRACE BRACKET STRUT HOSE ADAPTER BRACKET. (K) 2L73 4F4 F A23WE E12EU 20050720000082005072000008NM 2005 7 20 USAA050809 120050629A5320 ANGLE BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU52779 23861 CLT - Q2 - L-ANGLE, 6 INCH FRETTING, L-ANGLE AT BS 1016 FORWARD OF THE RT FWD VERTICAL FIN MOUNT. FABRICATED AND REPLACED NEW L ANGLE. (K) 2L72 4F4 FRTA16WE E21EU 20050720000092005072000009NM 2005 7 20 USAA050817 120050629A5414 SKIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU RT PYLON CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19430US 24552 CLT - C3 - SKIN, .75 INCH CRACK, RT PYLON AT CORNER OF CUTOUT FOR PANEL NR 5828R, NAC, STA 166.5. INSTALLED DOUBLER IAW TYPICAL REPAIR SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050720000112005072000011NM 2005 7 20 USAA050804 120050629A5320 THRESHOLD BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU52779 23861 CLT - Q2 - WEB, 48 INCHES, CORROSION FWD ENTRY DOORWAY THRESHOLD WEB. FABRICATED WEB AND ASSOCIATED REPAIR PARTS AND INSTALLED DRWG IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050720000132005072000013NM 2005 7 20 USAA050812 120050629A5320 SUPPORT ANGLE BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU52779 23861 CLT - Q2 - SUPPORT ANGLE, 1 INCH, CRACK, STA 540 AND STR 22R. FABRICATED AND INSTALLED REPAIR PART. (K) 2L72 4F4 FRTA16WE E21EU 20050720000142005072000014NM 2005 7 20 USAA050801 120050627A575365C2632011A SKIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU TE FLAP GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19441US40664 24812 CLT - Q5 - FLAP SKIN, .500 X 3 INCH GOUGE, I/H OB MID FLAP BOTTOM SKIN 53 INCHES FROM IB END. REPAIRED DAMAGED SKIN IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050720000152005072000015NM 2005 7 20 USAA050810 120050629A5342 SKATE ANGLE BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU STAB TO FUSELAGEWORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU52779 23861 CLT - Q2 - SKATE ANGLE, 2 INCHES X 4 INCHES, WORN AREA, AFT END OF THE RT SKATE ANGLE AT THE BASE OF THE VERTICAL FIN TO FUSELAGE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS. (K) 2L72 4F4 FRTA16WE E21EU 20050720000172005072000017NM 2005 7 20 USAA050814 120050629A5320 FLOOR SUPPORT BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19441US40664 24812 CLT - Q5 - STA 328-344, LBL9, 2 INCH X 2 INCH, CORROSION, FLOOR SUPPORT. DEFECTIVE PART REPLACED WITH IDENTICAL PART, REMOVED AND REPLACED STIFFENER IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050720000182005072000018NM 2005 7 20 USAA050802 120050627A5712 RIB BOEING737 737401 1384701NM CFMINTCFM56 CFM563B2 13802EU RT WING GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19421US45275 23988 CLT - C4 - RIB, 4 INCHES X .5 INCH, GOUGE, RT WING, WBL 417 JUST OB OF OB FOREFLAP. CUTOUT DAMAGE AND INSTALLED DOUBLER IAW EA. (K) 2L72 4F4 FRTA16WE E21EU 20050720000212005072000021NM 2005 7 20 USAA050803 120050629A5313 STRINGER BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU52779 23861 CLT - Q2 - CARGO FLOOR STRINGER, 6 INCH, CORROSION, AFT CARGO FLOOR STRINGERS AT STA 736 FROM LBBL 17.2 TO RBBL 13.8. REMOVED AND TREATED CORROSION IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050720000232005072000023NM 2005 7 20 USAA050806 120050629A5320 INTERCOSTAL BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE DENTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU 23861 CLT - Q2 - INTERCOSTAL, 2 INCHES X 1 INCH, DENT, STR 25L BETWEEN FRAMES 440 AND 420. FABRICATED AND INSTALLED NEW INTERCOSTAL IAW DRWG. (K) 2L72 4F4 FRTA16WE E21EU 20050720000252005072000025EU 2005 7 20 Y2PA05008 120050610A28222060B PUMP AMD FALC20FALCOND 2720304EU GE CF700 CF7002D2 30010NE NR 1 FUEL BOOST INTERMITTENT E Y2PAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 GL23811AA 187 DURING CLIMB OUT NR 1 ENG STARTED TO SURGE. NR 1 FUEL PRESSURE DROPPED TO ZERO. OPENED CROSSFEED THEN NR 2 ENG LOST 50 PERCENT POWER, FUEL PRESSURE DROPPED TO NEAR ZERO AND NR 2 FUEL PRESSURE LIGHT CAME ON. CREW DECLARED EMERGENCY, TURNED BACK TOWARDS FIELD. ENGINES NR 1 AND NR 2 THEN BOTH STABILIZED WITH THE CROSSFEED VALVE OPEN. AIRCRAFT LANDED BACK WITHOUT FURTHER INCIDENT. DURING GROUND RUN, FOUND NR 1 BOOST PUMP PRESSURE DROP, OPENED CROSSFEED VALVE AND NR 2 BOOST PUMP, PRESSURIZED BOTH SIDES. REMOVED AND REPLACED NR 1 ENG BOOST PUMP IAW MM. RAN BOTH ENGINES AT TAKE OFF POWER. BOTH ENG OPS WERE GOOD DURING RUN AND AT NO TIME ROLLED BACK. AC WAS TEST FLOWN SATISFACTORY AND RETURNED TO SERVICE.(K) 2L72 4F4 F A7EU E7EA 20050720000262005072000026SO 2005 7 20 GUU2005F00028 120050619A5610NP1513111 WINDSHIELD EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE COCKPIT CRACKED A GUUAA UNSCHED LANDING O OTHER CRCRUISE 1 SO29268AS 120202 DURING FLIGHT AT 13,000 FEET, CAPTAINS WINDSHIELD CRACKED AND SHATTERED, DIVERTED. REMOVED AND REPLACED CAPTAINS WINDSHIELD. (K) 2L72 4T4 TRTA31SO E20NE 20050718001282005071800128NM 2005 7 18 ASAA0540177 120050331A5230 SKIN BOEING737 737490 1384715NM CARGO DOOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM025200 28886 PAE - FOUND FORWARD CARGO DOOR REQUIRES OUTER SKIN REPLACED DO TO NUMEROUS DENTS. REPLACED OUTER SKIN. (M) 2L72 4F RTA16WE 20050718001362005071800136NM 2005 7 18 ASAA0540220 120050504A5340693535214 STRINGER CLIP BOEING737 737490 1384715NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02792AS 28887 PAE - FOUND STRINGER CLIP HAS FIGURE 8 HOLE. REMOVED AND REPLACED STRINGER CLIP. (M) 2L72 4F RTA16WE 20050718001502005071800150NM 2005 7 18 ASAA0510137 120050613A534065429012 STRINGER CLIP BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX - TIE CLIP A BS 847 STRINGER 27R FOUND CORRODED. TIE CLIP REPLACED WITH FABRIATED REPAIR PART AT BS 847 STRINGER 27R IAW B737-200 SRM 51-30-02 FIG 11. (M) 2L72 4F A16WE 20050718001592005071800159NM 2005 7 18 ASAA0540230 120050510A53206547690 SUPPORT BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02792AS 28887 PAE - FOUND CORROSION ON LEFT FLOOR TO SIDEWALL SUPPORT. REMOVED AND REPLACED SIDEWALL SUPPORT. (M) 2L72 4F RTA16WE 20050718001652005071800165NM 2005 7 18 ASAA0540235 120050510A5754 SKIN BOEING737 7374Q8 138447QNM NR 5 SLAT DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02783AS 25114 OKC - NR 5 SLAT OUTBOARD TRAILING EDGE IS DELAMINATING. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER, AND DOUBLER IAW BOEING 737-400 SRM 51-70-10 PAGE 8. (M) 2L72 4F RTA16WE 20050718001702005071800170NM 2005 7 18 ASAA0540 120050312A5320654769020 SUPPORT BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02794AS 28889 PAE - FOUND AFT CARGO BAY, FLOOR TO SIDEWALL SUPPORT CORRODED. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT. (M) 2L72 4F RTA16WE 20050718001722005071800172WP 2005 7 18 ASAA0580198 120050404A524059360215 DOOR DOUG DC9 DC983 3022083WP SERVICE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02950AS 53023 OKC - DURING C-CHECK, FOUND FORWARD LAVATORY SERVICE DOOR LANDING IS CORRODED. REPLACED DAMAGED SECTION USING REPAIR FILLER, DOULER, AND STRAP PER EA 5330-01010. (M) 2L72 4F RTA6WE 20050718001772005071800177WP 2005 7 18 ASAA0580268 120050517A5320 CHANNEL DOUG DC9 DC983 3022083WP FLOORBOARD CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - FOUND DURING C-CHECK, CABIN FLOORBOARD STATION 1155 TO 1250 LBL 44 TO 54 HAT CHANNEL IS CRACKED. COMPLETED A FIBERGLASS REPAIR. (M) 2L72 4F RTA6WE 20050718001802005071800180NM 2005 7 18 ASAA0540234 120050510A575465C266867 SKIN BOEING737 7374Q8 138447QNM NR 2 SLAT DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02783AS 25114 OKC - FOUND NR 2 SLAT OUTBOARD UPPER/AFT EDGE IS DELAMINATING. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR CORE, FILLER, AND DOUBLER IAW BOEING 737-400 SRM 51-70-10 PAGE 8. (M) 2L72 4F RTA16WE 20050718001852005071800185NM 2005 7 18 05FDEA01874 120050709A5753 HINGE DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 RT WING, O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR PIN ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. REPAIRED AS PER EA1-5750-87590. 2L73 4F RTA22WE 20050718001862005071800186NM 2005 7 18 05FDEA01875 120050709A5753 HINGE DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 RT WING, O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. REPAIRED AS PER EA1-5750-87590. 2L73 4F RTA22WE 20050718001972005071800197NM 2005 7 18 ASAA0540181 120050316A57536546486131 WEDGE BOEING737 7374Q8 138447QNM TE FLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02764AS 25101 OKC - FOUND LEFT INBOARD TRAILING EDGE FLAP HAS SEVERAL DENTS. REMOVED DAMAGE FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 SRM 51-70-10 PAGE 8. (M) 2L72 4F RTA16WE 20050718002112005071800211EU 2005 7 18 USAA200507002 120050709A5330 SKIN AIRBUSA319 A319112 3930323EU CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19755US 1331 2.25 IN CRACK FOUND BETWEEN STA 539 AND 594 STR 36 RT TO 37 RT ON SKIN. REMOVED DAMAGED SKIN AND INSTALLED REPAIR DOUBLER PER EA 81165. 2L72 4F RTA28NM 20050718002152005071800215NM 2005 7 18 AT0500022 120050710A35205D00271 RELAY BOEING717 717200 1383700NM PAX OXYGEN SYS MALFUNCTIONED A ZZDAO OTHER O OTHER CRCRUISE 1 SO15994AT 55138 PAX O2 ALT REL C/B NR L33 POPPED AFTER 1 RESET. REMOVED AND REPLACED RELAY R2-5152 AND C/B B1-870. PERFORMED O2 MASK DROP CHECK PER M/M 35-23, OPS CHECK GOOD. 2L72 4F TRA6WE 20050719000042005071900004NM 2005 7 19 S2YA05034 120050521A280060330201 CONTROL PANEL DORNERDO32 DO328300 NM PWA 306 PW306B NE FUEL SYSTEM MALFUNCTIONED A S2YAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL13359SK3996 1418 3202 DURING FLIGHT, CREW REPORTED AN AMBER CAS MESSAGE FOR BOTH LT AND RT FUEL QUANTITY INDICATORS. THE CREW CONSULTED WITH MECHANIC AND MADE AN AIR-TURN-BACK. MECHANIC REPLACED THE FUEL CONTROL PANEL AND ALL OPERATIONAL CHECKS WHERE GOOD. (K) 2H72 4T4 FRTA55NM E35NE 20050719000062005071900006SO 2005 7 19 SIMA200516002 120050605A21508152403 ACM EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 1 SMOKE A SIMAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW21906AE 14500894 CREW REPORTED BURNING SMELL IN COCKPIT JUST PRIOR TO PUSH BACK. REPLACED NR 1 AIR CYCLE MACHINE (ACM) IAW AMM. AC RETURNED TO SERVICE. (K) 2L72 4T4 FRTT00011ATTE6CH 20050719000072005071900007CE 2005 7 19 S2YA05024 120050314A3230MS2417101 RELAY BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE MLG MALFUNCTIONED A S2YAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL1391SK UE91 AFTER TAKEOFF, THE CREW WAS UNABLE TO RETRACT THE GEAR. THE CREW PERFORMED AN AIR TURNBACK. MECHANIC INSPECTED THE AC AND REPLACED THE LANDING GEAR RELAY AND THE POWER PACK MOTOR. (K) 2L72 4T4 TRTA24CE E26NE 20050719000102005071900010EU 2005 7 19 SIMA200517101 120050620A27306225027002 SERVO SAAB SF340 340B 7860101EU GE CT7TS CT71 30030NE ELEVATOR FAILED A SIMAO OTHER F FLT CONT AFFECTED CRCRUISE 1 SW21370AM 340B370 WHILE HAND FLYING AC WITH NO AUTOPILOT ENGAGED, THE AIRCRAFT PITCHED UP WITH NO PILOT INPUT. REPLACED ELEVATOR SERVO. OPS CHECK GOOD. PERFORMED FUNCTIONAL CHECK FLIGHT WITH NO DISCREPANCIES NOTED. (K) 2L72 4T4 URTA52EU E8NE 20050719000132005071900013EU 2005 7 19 SIMA200517109 120050617A2730R24086 PUSHROD SAAB SF340 340B 7860101EU GE CT7TS CT71 30030NE ELEVATOR TRIM WORN A SIMAO OTHER F FLT CONT AFFECTED CLCLIMB 1 SW21370AM 340B370 WHILE HAND FLYING AC WITH AUTOPILOT OFF THE AC EXPERIENCED AN UNCOMMANDED PITCH UP OF 5 TO 7 DEGREES. AFTER CORRECTION AND RETRIM THE AC THEN EXPERIENCED AN UNCOMMANDED PITCH DOWN. REPLACED LT ELEVATOR TRIM TAB IB PUSH ROD AND ADJUSTED RT ELEVATOR TRIM TAB IB AND OB PUSH ROD ENDS. OPS CHECK GOOD. AC RETURNED TO SERVICE. (K) 2L72 4T4 URTA52EU E8NE 20050719000322005071900032NM 2005 7 19 2005UALA00600 120050627A5714 SKIN BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE CENTER WING CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29657UA 27112 BS 955 CENTER WING BOX UPPER SKIN AT RBL 3 AT AFT SPAR CORRODED, SKIN SPLICE FITTING AND AFT SPAR. CORROSION CAUSED BY MOISTURE IN THE AREA. BLENDED WING SKIN, FABRICATED REPAIR SHIM BETWEEN SKIN AND FITTING, BLENDED SPAR CHORD, AND FABRICATED MODIFIED FITTING P/N 145T8657-2 PER TIMCO REO (EVA) G10657, REV C, AND UA-EVA-50419 ON NON ROUTINES J7557R, G4070J, G4036J, G4043J AND G7128I. 2L72 4F4 FRTA1NM E24NE 20050719000342005071900034NM 2005 7 19 ASAA0510160 120050613A57546546421228A SKIN BOEING737 737290C 138448VNM NR 6 SLAT DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX - FOUND RIGHT NR 6 SLAT FOUND WITH DELAMINATION ON UPPER SURFACE MID-SPAN AT SLAT STATION 327, 359.03, 346.53 AND FS 540. PERMANENTLY REPAIRED IAW B737-200 SRM. (M) 2L72 4F A16WE 20050719000362005071900036NM 2005 7 19 ASAA0510170 120050614A5712655077367 RIB BOEING737 737290C 138448VNM LT WING WORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX - FOUND LEFT WING RIB BETWEEN AILERON AND FORE FLAP T/E ANGLE SUPPORT CHANNEL HAS WEAR DAMAGE. REMOVED AND REPLACED SUPPORT ANGLE IAW B737-200 SRM. (M) 2L72 4F A16WE 20050719000382005071900038NM 2005 7 19 ASAA0510161 120050614A57546546421228A SKIN BOEING737 737290C 138448VNM NR 6 SLAT DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX - FOUND RIGHT NR 6 SLAT FS 540, UPPER EDGE HAS DAMAGE. PERMANENT REPAIR COMPLETED IAW B737-200 SRM 51-40-20 REPAIR 14 FIG 23. (M) 2L72 4F A16WE 20050719000532005071900053CE 2005 7 19 DXTA200500825 120050708A3240MP50B1 MOTOR CESSNA500 560CESSNA 2076750CE NOSE FAILED E DXTAO OTHER J WARNING INDICATION LDLANDING 1 GL07354QS8940 5600356 WHILE ATTEMPTING TO LAND AFTER GEAR LOWERED POWER BRAKE PRESSURE AND ANTI-SKID INOP LIGHTS ILLUMINATED. FOUND BRAKE POWER PACK FILTER HOUSING CRACKED ON THREADS. REPLACED MOTOR/PUMP ASSY IAW C560MM 32-42-06. 2L72 4F RTA22CE 20050719000552005071900055NM 2005 7 19 ASAA0540164 120050310A5320654769015 FLOOR SUPPORT BOEING737 737490 1384715NM FUSLEAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02794AS 28889 PAE - FOUND AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED. REMOVED, FABRICATED AND INSTALLED FLOOR TO SIDEWALL SUPPORT. (M) 2L72 4F RTA16WE 20050719000572005071900057NM 2005 7 19 ASAA0540239 120050511A5320 SILL BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02792AS 28887 PAE - FOUND CORROSION AT L2 DOOR MOPSILL. REMOVED AND REPLACED. (M) 2L72 4F RTA16WE 20050719001062005071900106NM 2005 7 19 ASAA0510077 120050415A532265465348 SHEAR TIE BOEING737 737290C 138448VNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 YXX - FOUND BS 520 SKIN TO FRAME ATTACH ANGLE BETWEEN STRINGER 27R AND 28R DISPLACED FROM PREVIOUS REPAIRS. REPLACED ATTACH ANGLES IAW B737-200 SRM 53-10-4 FIGURE 6. (M) 2L72 4F A16WE 20050719001082005071900108WP 2005 7 19 ASAA0580247 120050509A53305936435503 SKIN DOUG DC9 DC983 3022083WP FUSLEAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - DURING C-CHECK, FOUND FUSELAGE SKIN HAD DENT AT STATION 1220 LEFT 6 INCHES ABOVE CUSP LINE. COLD WORKED DENT AND INSTALLED SKIN AND DOUBLER. (M) 2L72 4F RTA6WE 20050719001102005071900110WP 2005 7 19 ASAA0580204 120050404A5532591216610N SKIN DOUG DC9 DC983 3022083WP VERTICAL STAB CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02950AS 53023 OKC - FOUND DURING C-CHECK, VERTICAL STABILIZER SKIN CHAFED AT HORIZONTAL STABILIZER FAIRING. REPLACED DAMAGED SECTION. (M) 2L72 4F RTA6WE 20050719001122005071900112WP 2005 7 19 ASAA0580143 120050228A5347593056675 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 OKC - DURING HV-CHECK, FOUND SEAT TRACK CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR PLUG. (M) 2L72 4F RTA6WE 20050719001142005071900114NM 2005 7 19 ASAA0540189 120050318A53136552928604 STRINGER BOEING737 737490 1384715NM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02794AS 28889 PAE - FOUND STRINGER IS GOUGED AT AFT CARGO BAY. REMOVED DAMAGED SECTION OF STRINGER, FABRICATED REPAIR PARTS AND INSTALLED. (M) 2L72 4F RTA16WE 20050719001262005071900126CE 2005 7 19 DXTA200500834 120050625A2720991455811 ACTUATOR CESSNA750 750 2076810CE RUDDER FAILED E DXTAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL07908QS5577 3177 7500108 RUD LIMIT FAIL B AMBER CAS MESSAGE IN CRUISE FLIGHT, FAILED AT 18%. INSTALLED OVERHAULED LWR RUDDER TRAVEL LIMITER ACTUATOR IAW 750 M/M 27-23-00, AND 27-20-00-720. OPS CHECK GOOD. 2L72 4J RTT00007WI 20050719001332005071900133EA 2005 7 19 SWIA200515253 120050708A274070623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07975SW STAB TRIM CH 1 WILL NOT ENGAGE. REPLACED MCU IAW MM 27-42-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050719001372005071900137EA 2005 7 19 SWIA200515257 120050709A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSINOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07447SW 7677 AFT CEILING LEVEL CABIN EMERGENCY LIGHT INOP. RELAMPED CEILING LIGHT IN AFT CABIN. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050719001422005071900142EA 2005 7 19 SWIA200515262 120050708A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSINOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07929SW 7703 FORWARD CABIN EMERGENCY LIGHT, CEILING LEVEL FLOODLIGHT INOP. RELAMPED FORWARD EMERGENCY LIGHT IN CEILING. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050719001772005071900177SO 2005 7 19 SWIA200515271 120050709A27503472001001 CONTROL UNIT EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07215SW3716 1837 120281 FLAP CONTROL FAULT AT ALTITUDE. REPLACED FLAP CONTROL COMPUTER IAW EMB 120 MM 27-50-06. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050719001782005071900178WP 2005 7 19 AALA20050431 120050709A3350P4010049 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHTSDISCHARGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21964TW 53614 ALL SEAT MOUNTED AND FIRST CLASS GALLEY EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT CONTROL MODULE AB5 1 AND AB5 3 FOR SEAT MOUNTED EMERGENCY LIGHTS. INSERTED LOOSE WIRES AT SEAT 17D AND CHARGED BATTERY FOR FIRST CLASS GALLEY EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050719001792005071900179NM 2005 7 19 AALA20050433 120050710A3350P4010049 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHTSINOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21697AN 26977 EMERGENCY LIGHTS IN AFT CABIN WOULD NOT TURN OFF. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050719001842005071900184WP 2005 7 19 AALA20050432 120050709A3222 STRUT DOUG DC9 DC983 3022083WP NLG UNDERSERVICED A AALAA UNSCHED LANDING O OTHER CLCLIMB 1 SW21592AA 53255 NLG WOULD NOT RETRACT. LANDED WITHOUT INCIDENT. SERVICED NOSE STRUT WITH NITROGEN AND OIL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050719001932005071900193SO 2005 7 19 C2XA05CL057 120050708A21508152403 ACM EMB 145 EMB145LR 3260212SO NR 1 PACK FAILED A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW27215378598 145523 CREW REPORTED SMALL AMOUNT OF SMOKE ALONG WITH STRONG ODOR OUT OF VENTS WITH APU RUNNING NR 1 PACK. MAINTENANCE INSPECTED AND REPLACED NR 1 AIR CYCLE MACHINE. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20050719002582005071900258WP 2005 7 19 0501009758 120050712A4990GTCP8598DCA APU DOUG DC9 DC941 302207NWP APU BAY LEAKING A NWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL01758NW719341568 47286 DURING CLIMB, AFT RT LAV SMOKE DETECTOR SOUNDED AND FLIGHT ATTENDANT REPORTED VISIBLE SMOKE IN AREA. NO FIRE DETECTED. FLIGHT CREW RETURNED A/C TO DEPARTURE AIRPORT. MAINTENANCE FOUND APU OIL LEAK AND REPLACED APU. 2L72 4F A6WE 20050720000072005072000007NM 2005 7 20 USAA050807 120050629A5320 FLOOR SUPPORT BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSLEAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU 23861 CLT - Q2 - FLOOR SUPPORT, 1 INCH CRACK, FLOOR SUPPORT AT STA 500D IN A/C DISTRIBUTION BAY. REMOVED DAMAGED WEB, FABRICATED NEW WEB IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050720000302005072000030EU 2005 7 20 YENA200540 120050716A3350324130 BATTERY AIRBUS320 A320232 3930326EU EMERGENCY LIGHT DISCHARGED A YENAK NONE L NO TEST ININSP/MAINT 1 EA15522JB9866 8093 1464 DURING TEST OF EMERGENCY LIGHTING SYSTEM, RECEIVED "EPSU BATTERY, AFT L" MESSAGE ON PTP. VERIFIED AND REPLACED EPSU BATTERY AT AFT LOCATION (13WL) PER AMM 33-51-38. 2L72 4F RTA28NM 20050720000312005072000031NM 2005 7 20 AWXA200500819 120050615A5330654576653 SKIN BOEING737 7373G7 1384595NM FUSLEAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 DURING C16 CHECK FOUND FUSELAGE SKIN CRACK 2.0 INCHES IN LENGTH LOCATED AT BS 518, STRINGER 12L. MAINTENANCE REMOVED DAMAGED AREA FROM SKIN AT BS 518, STRINGER 12L IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NO. 03-5331-05193-SS3. FABRICATED FILLER, DOUBLER AND TRIPLER REPAIR PARTS IAW AWA E.R. NO. 03-5331-05193-SS3. INSTALLED FABRICATED REPAIR PARTS AT BS 518, STRINGER 12L 3INCHES BELOW WINDOW IAW AWA E.R. NO. 03-5331-05913-SS3. 2L72 4F RTA16WE 20050720000322005072000032NM 2005 7 20 AWXA200500820 120050629A5320651768564 INTERCOSTAL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED INTERCOSTAL WEB CRACKED .38 INCHES IN LENGTH LOCATED AT BS 359, STR 16L. REMOVED CRACKED INTERCOSTAL WEB FROM BS 359, STR 16L IAW BOEING 737-300 SRM 51-40-02-0 FIG 8. FABRICATED REPAIR FILLER, TEE, STRAP AND INTERCOSTAL WEB IAW BOEING 737-300 SRM 53-10-04-2 FIG 202. MAINTENANCE INSTALLED FABRICATED REPAIR PARTS T BS 359, STR 16L IAW BOEING 737-300 SRM 53-10-04-2. 2L72 4F RTA16WE 20050720000342005072000034NM 2005 7 20 AWXA200500822 120050628A534765538441 CARGO TRACK BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED CORROSION ON AFT CARGO FLOOR CHANNEL BS 772, BL 17L. REMOVED CORROSION AT BS 772, BL 17L AND FOUND CORROSION TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-53-12 FIG 101. MAINTENANCE REMOVED CORRODED SECTION OF FLOOR CHANNEL IAW AMERICA WEST AIRLINES ENGINEERING REQUEST NO. 03-5300-05191-SS1. FABRICATED REPAIR ANGLE IAW AWA ER 03-5300-05191-SS1. INSTALLED FABRICATED REPAIR PARTS AT BS 772, BL 17L IAW AWA ER 03-5300-05191-SS1. 2L72 4F RTA16WE 20050720000362005072000036WP 2005 7 20 UPS05844764 120050603A5313 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01705UP 45949 INSPECTION TYPE C-2, CORROSION BETWEEN TOP OF L24L AND REPAIR DOUBLER STACK IN LT W/W NEAR STA 906. REMOVED CORROSION OUT OF LIMITS IAW SRM 51-1-8 AND 53-2-0 FIG 1F. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 53-02-02 FIG 005 SHEET 8. 2L74 4F RT4A25 20050720000382005072000038NM 2005 7 20 05FDEA01925 120050713A534065453132 STRINGER CLIP BOEING727 727233 138408ANM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 FUSELAGE UPPER LOBE, STRINGER CLIP IS CRACKED, BS 950C, STR 8R. REPLACED CRACKED STRINGER CLIP PER SRM 51-30-2. 2L73 4F RTA3WE 20050720000412005072000041NM 2005 7 20 05FDEA01926 120050713A534065453132 STRINGER CLIP BOEING727 727233 138408ANM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 FUSELAGE UPPER LOBE, STRINGER CLIP IS CRACKED, BS 950B, STR 8R. REPLACED CRACKED STRINGER CLIP PER SRM 51-30-2. 2L73 4F RTA3WE 20050720000432005072000043EU 2005 7 20 SF200507151 120050715A2611 SMOKE DETECTOR SAAB SF340 SF340A 7850100EU LAVATORY MALFUNCTIONED A UHLAH DEACTIVATE SYST/CIRCUITS N FALSE WARNING CRCRUISE 1 GL1714XS 340A014 FLT 7537 IAD DAY LAV SMOKE ILLUMINATED IN FLIGHT, CREW FOLLOWED QRH PROCEDURES. FLIGHT ATTENDANT NOTICED NO DESCREPENCIES, SENT MECHANIC FROM FWA TO MEET A/C INSPECTED LAV, NO DEFECTS NOTED DEFERRED LAV SMOKE SYSTEM PER MEL 26-13-1. FOLLOWED MAIN/OPS PROCEDURES, A/C FLOWN PART 91 TO FWA. 2L72 4T RTA52EU 20050720000452005072000045NM 2005 7 20 DLM90050333 120050624A3510359001020 BOTTLE DOUG MD90 MD9030 3023690NM CREW UNSERVICEABLE A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27902DA 53382 CREW OXYGEN PRESSURE DROPPED TO ZERO ON CLIMB. REPLACED CREW OXYGEN BOTTLE AND REGULATOR. NO LEAKS. 2L72 4F RTA6WE 20050720000472005072000047NM 2005 7 20 SWAA052094 120050718A3350101114 COVER BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29358SW 26595 FWD GALLEY EMERGENCY EXIT LIGHT COVER LOOSE. SECURED COVER PER MM. 2L72 4F RTA16WE 20050720000482005072000048 2005 7 20 SWAA052095 420050718A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29384SW 26590 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050720000492005072000049NM 2005 7 20 SWAA052096 120050715A5315141A5170 FLOORBEAM BOEING737 7373H4 1384600NM COCKPIT FLOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29613SW 27931 DURING SCHEDULED D-CHECK, FOUND COCKPIT FLOORBEAM UPPER CHORD CORRODED AT BS 259.5, LBL 6 TO RBL 11. REPAIRED FLOORBEAM PER BFG ER. 2L72 4F RTA16WE 20050720000502005072000050NM 2005 7 20 SWAA052097 120050715A53206545806 FLOOR SUPPORT BOEING737 7373H4 1384600NM CABIN FLOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29613SW 27931 DURING SCHEDULED D-CHECK, FOUND CABIN LONGITUDINAL UPPER CHORD CORRODED AT BS 270, BL 0, WL 208. REPAIRED UPPER CHORD PER SRM. 2L72 4F RTA16WE 20050720000512005072000051 2005 7 20 SWAA052098 420050715A256565659723 BRACKET BOEING737 7373H4 1384600NM L1 DOOR SLIDE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29613SW 27931 DURING SCHEDULED D-CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD & AFT FLOOR ATTACH BRACKETS CORRODED. REMOVED AND REPLACED ATTACH BRACKETS PER SRM. 2L72 4F RTA16WE 20050720000522005072000052NM 2005 7 20 SWAA052101 120050718A534465237737 HINGE BOEING737 7373L9 1384470NM R1 DOOR BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 R1 DOOR UPPER HINGE ASSY BROKEN. REMOVED AND REPLACED UPPER HINGE ASSY PER MM. 2L72 4F RTA16WE 20050720000552005072000055 2005 7 20 SWAA052104 420050717A256563550 SLIDE BOEING737 7377H4 1384404NM L2 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29796SW 27889 L2 DOOR SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20050720000562005072000056NM 2005 7 20 SWAA052086 120050718A53206545409 WEB BOEING737 7373H4 1384600NM LH MLG W/W CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE BEADED WEB CRACKED AT BS 665, LBL 40. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050720000572005072000057NM 2005 7 20 SWAA052087 120050718A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 907, LBL 3 TO RBL 3. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050720000582005072000058NM 2005 7 20 SWAA052088 120050718A53306545775 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 843, STR 18L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050720000662005072000066GL 2005 7 20 CHQA200500123 220050625A7200AE3007A1P ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 2 UNSERVICEABLE A CHQAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 GL11568RP9460 9460 145800 CAE312008 DURING POST ENGINE CHANGE HIGH POWER RUN, LAV SMOKE OCCURRED ON EICAS AFTER ABOUT 1.5 MINUTES AT 88 PERCENT N2. ENGINE REPLACED DUE TO PREVIOUSLY INSTALLED ENGINE CAUSING LAV SMOKE ON EICAS AND SMOKE IN COCKPIT AND CABIN. SEE SDR CHQA200500122 FOR DETAILS. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE IAW EMB 145 J/C 72-00-01. OPS CHECK AND LEAK CHECK GOOD. NO EICAS MESSAGES OR SMOKE NOTED. 2L72 4T4 FRTT00011ATTE6CH 20050720000682005072000068EU 2005 7 20 KBM2005F00116 120050621A6420350A3321501 BALL END SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE T/R SPIDER WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19115SH657 3141 T/R SPIDER END BEARING WORN. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050720000702005072000070EA 2005 7 20 ASOA05521 120050614A5210 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27908EV 7654 DURING A C-CHECK IN MCN, THE TOP STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE TOP STEP ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20050720000712005072000071EA 2005 7 20 ASOA05520 120050614A5344 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA CENTER ENGINE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27908EV 7654 DURING A C-CHECK IN MCN, THE CENTER ENGINE SUPPORT BEAM WAS FOUND TO BE CRACKED BEYOND LIMITS UNDER THE FIRE LOOP CLIP. MAINTENANCE IS REPAIRING THE ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW ASA EO 600-53-0072B. (M) 2L72 4F RTA21EA 20050720000722005072000072EA 2005 7 20 ASOA05512 120050613A3350BR9279232 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27820AS 7188 DURING A GROUND INSPECTION IN ATL, THE EMERGENCY FLOODLIGHT AT THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOODLIGHT ASSEMBLY AT THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050720000782005072000078EA 2005 7 20 ASOA05511 120050613A25602616 FLASHLIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27873AS 7549 DURING A GROUND INSPECTION IN ATL, THE BULB IN THE FLIGHT ATTENDANTS EMERGENCY FLASHLIGHT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE FLIGHT ATTENDANTS EMERGENCY FLASHLIGHT. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050720000792005072000079EA 2005 7 20 ASOA05517 120050614A5340 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27908EV 7654 DURING A C-CHECK IN MCN, THE FS 280 AFT INBOARD BRACKET AT LBL 9 AND THE AFT OUTBOARD BRACKET AT RBL 9 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FS 280 AFT INBOARD BRACKET AT LBL 9 AND THE AFT OUTBOARD BRACKET AT RBL 9. (M) 2L72 4F RTA21EA 20050720000802005072000080EA 2005 7 20 ASOA05513 120050613A2120504300 SEAL CNDAIRCL600 CL6002B19 1900309EA ACM DUCT WORN A ASOAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DEDESCENT 1 SO27839AS 7284 DURING DESCENT INTO BNA FROM ATL, THE FLIGHT ATTENDANT NOTICED AN ODOR IN THE BACK OF THE CABIN FOLLOWED BY THE SYNOPTIC PAGE SHOWING THE RT PACK BEGINNING TO OVERTEMP. CREW TURNED OFF THE RT PACK AND THE ODOR SUBSEQUENTLY DISSIPATED. THE AIRCRAFT LANDED SAFELY IN BNA. UPON INSPECTION OF THE ACM, MAINTENANCE FOUND THE DUCT DETACHED FROM THE ACM. MAINTENANCE REMOVED AND REPLACED THE SEAL AND REATTACHED THE DUCT TO THE ACM. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050720000832005072000083EA 2005 7 20 ASOA05524 120050615A5210600250087 STRAP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BINDING A ASOAK NONE O OTHER ININSP/MAINT 1 SO27916EV 7757 FLT 4370 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WAS FOUND HARD TO OPEN FROM THE INSIDE. MAINTENANCE READJUSTED THE PASSENGER DOOR INNER HANDLE RESTRAINT STRAP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050720000852005072000085EA 2005 7 20 ASOA05510 120050611A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27830AS 7236 DURING A C-CHECK IN MCN, THE FS 484 LEFT INBOARD AND OUTBOARD CLIP ON THE PRESSURE FLOOR WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FS 484 LT INBOARD AND OUTBOARD CLIP ON THE PRESSURE FLOOR IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20050720000882005072000088NM 2005 7 20 05FDEA01866 120050708A2750 FLAP BOEING727 7272S2F 1384O81NM TE FLAPS JAMMED A FDEAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO25204FE 22926 ASYMETRICAL INBOARD TRAILING EDGE FLAPS AT 2 DEGREES UPON FLAP RETRACTION. RAN APPROPRIATE QRH PROCEDURES, FOUND LT INBD FLAP COCKED AND JAMMED INTO INBD AILERON. UPON FURTHER TROUBLESHOOTING FOUND BEARING WALKED OUT OF SCREWSHAFT END OF LT INBD TRANSMISSION. REMOVED AND REPLACED REPLACEMENT I/B J/S PER 727-200 M/M 27-51-041-4 . STILL REQUIRES UP-STOPS SET TORQUE TUBES SAFETY, OPS AND RII BUY BACK. 2L73 4F A3WE 20050720000892005072000089EA 2005 7 20 ASOA05523 120050615A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27908EV 7654 DURING A C-CHECK IN MCN, THE FLOOR SUPPORT ANGLES AT FS 621 LT/RT WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FLOOR SUPPORT ANGLES AT FS 621 LT/RT IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20050720000902005072000090NM 2005 7 20 05FDEA01895 120050711A5320 SPLICE DOUG MD11 MD11 3023602NM CTR CARGO BAY DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 CENTER CARGO BAY RT STA 5-113, LONGERON 44 SPLICE FITTING FOUND WITH EXISTING ENLONGATED HOLE AFTER REMOVAL SPLICE FITTING. REMOVED AND REPLACED NEW SPLICE FITTING AS PER SRM 51-33-01 VOL. II. MINOR REPAIR AS GMM 6-2-100. 2L73 4F RTA22WE 20050720000962005072000096NM 2005 7 20 F3LA200500029 120050711A27003945128102 COMPUTER AIRBUSA319 A319111 3930336NM NR 2 ELAC MALFUNCTIONED A F3LAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM03912FR 2049 1803 AIR RETURN. AFTER DEPARTURE AT 8500 FT, ACFT PFD DISPLAYED ALTN LAW, AMBER XXS AND ECAM VERIFIED LANDING WT 130,400 PER POST FLIGHT REPORT. NR 2 ELAC REPLACED. OPS CHECKED GOOD PER AMM 27-93-34-401 AND 27-93-00-710-001. GROUND SCAN DETECTED NO FAULTS PER AMM 27-96-00-740-001. PERFORMED AFS TEST PER WORK CARD MP 22900-1. TESTED GOOD. COMPLIED WITH WORK CARD TC 22200-1, CAT 3B LAND VERIFY. CAT 3B RETAINED. 2L72 4F RTA28NM 20050720000972005072000097SW 2005 7 20 YTRR104514 120050711A6220406310405101 BEARING BELL 407 407 1182206SW PITCH LINK WORN B YTRAO OTHER O OTHER NRNOT REPORTED 1 SW03595RL948 53595 PITCH LINK BEARING WORN BEYOND ALLOWABLE LIMITS. 1G71 3U O H2SW 20050720000982005072000098SW 2005 7 20 ALGA104691 120050715A2510206033167105 FITTING BELL 407 407 1182206SW SEAT BROKEN B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03617AL6201 53265 TAB ON CASTING THAT HAS A NUTPLATE FOR THE SEAT PANEL SUPPORT IS CRACKED AND BROKEN / REPLACED WITH NEW FITTING 1G71 3U O H2SW 20050720000992005072000099SW 2005 7 20 ALGA104612 120050629A6220406310405101 PITCH LINK BELL 407 407 1182206SW MAIN ROTOR WORN B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03404AL340 53479 AXIAL PLAY BEYOND MAX. AND RATCHETY / REPLACED WITH NEW BY FIELD MAINTENANCE. 1G71 3U O H2SW 20050720001012005072000101NM 2005 7 20 05FDEA01982 120050717A5330 SKIN DOUG MD11 MD11 3023602NM ZONE 700 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 LT MLG - DURING CARRYING OUT WHEEL WELL DOOR HINGE REPAIR, FOUND INTERNAL SKIN IPPER AFT AREA WITH A NEW CRACK PROPAGATING FROM FASTENER HOLES AT EXISTING DOUBLER REPAIR. REPAIRED AS PER FEDEX EA 1-3210-89958. 2L73 4F RTA22WE 20050720001032005072000103NM 2005 7 20 05FDEA01984 120050718A5311 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RT MAIN DECK AFT FUSELAGE FRAME AT STA 1661, BETWEEN LONGERONS L12 AND L13 FOUND WITH DENT. DENT MARK REPAIRED PER SRM 53-30-00 VOLUME I FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI: 53-10/2983 AND FEDEX EA 1-5330-87561 2L73 4F RTA22WE 20050720001042005072000104NM 2005 7 20 05FDEA01985 120050718A5310 DOOR FRAME BOEING727 727200 138407ENM E/E BAY CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 CORROSION ON E-BAY DOOR FRAME BS 423 BL 0. BLENDED CORROSION FROM E-BAY FRAME BS 423 BL 0 FOUND TO BE WITHIN LIMITS PER SRM 53-10-1 2L73 4F RTA3WE 20050720001052005072000105NM 2005 7 20 05FDEA01986 120050718A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 NBS 580 MULTIPLE FRAME DENTS ABOVE AND BELOW STRINGER 23L AT BS 580. DENT FOUND TO BE OUT OF LIMITS, REMOVED DAMAGE PER SRM 53-40-3 FABRICATED REPAIR DOUBLER, DRILLED, ALLODINED, PAINTED AND INSTALLED PER SRM 51-40-3, 51-10-2, 51-40-3. 2L73 4F RTA3WE 20050720001062005072000106NM 2005 7 20 05FDEA01987 120050718A5310 STRUCTURE BOEING727 727200 138407ENM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 BS 1352 IS GOUGED AT 3 O'CLOCK, WORN FROM 5-6 O'CLOCK AND MISSING RUBSTRIP FROM 1-6 O'CLOCK. (OPEN) 2L73 4F RTA3WE 20050720001072005072000107NM 2005 7 20 05FDEA01988 120050718A5220 DOOR BOEING727 727200 138407ENM EMERGENCY EXIT DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 REWORK REQUIRED, LT AFT OVERWING EMERGENCY ESCAPE DOOR EXTERNAL SKIN REPAIR DOUBLER UPPER EDGE BENT AT 2 LOCATIONS. REJECTED DUE TO NO BLEND LIMITS ON REPAIR DOUBLER. REPAIRED LT AFT EMERGENCY ESCAPE DOOR EXTERNAL SKIN PER SRM 52-00-3. 2L73 4F RTA3WE 20050720001102005072000110EU 2005 7 20 05FDEA01952 120050714A5730 SKIN AIRBUS300 A300F4605R 3930327EU ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25671FE 778 LT WING FIXED TE UPPER SKIN CRACKED/CUT LOC 5 IN FROM INBD END 2.5 IN FROM AFT END. 2L72 4F RTA35EU 20050720001132005072000113NM 2005 7 20 05FDEA01945 120050714A5340 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 FUSELAGE UPPER LOBE, STRINGER CLIP IS CRACKED, BS 950E, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM 51-30-02 2L73 4F RTA3WE 20050720001172005072000117NM 2005 7 20 ASMF200507011 120050714A2150 A/C PACK DOUG MD88 MD88 3023688NM MALFUNCTIONED W ASMFA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW23XATPM 49671 UNSCHEDULED LANDING AT SAT DUE TO PRESSURIZATION FAILURE IN BOTH A/C PACKS WHEN USING ENGINES ANTI-ICE. ENGINES ANTI-ICE SET UP BOTH A/C PACKS CUT OUT. ACCOMPLISHED ABNORMAL PROCEDURE & OXYGEN MASKS DEPLOYED. MECHANIC PERFORMED PRESSURIZATION TESTS TO BOTH A/C PACKS, WORKED CORRECTLY. RELEASED TO SERVICE. FDR CHANGED IN ORDER TO ACCOMPLISH THE READ OUT AND TEST PROCEDURE. ACFT FERRIED TO MEX. FAILURE DID NOT PRESENT AGAIN DURING THE FT, THE A/C PACKS & PRESSURIZATION OPS CORRECTLY. DURING OVERNIGHT CHECK IN MEXICO, A/C PACKS TESTED IN AUTOMATIC & MANUAL MODE, ANTI-ICE SYS & A/C WERE TESTED IN MODE 1 & MODE 2. ENGINE ANTI-ICE TESTED IAW APPLICABLE MM. BEING ALL CORRECT. NOCOMPONENTS REPLACED. 2L72 4F RTA6WE 20050720001192005072000119NM 2005 7 20 05FDEA01956 120050714A5730 SKIN DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 LT WING FORWARD FIXED LEADING EDGE INNER SKIN FOUND CRACKED, ADJACENT TO REFUELING PANEL AT STA 522. FABRICATED REPAIR DOUBLER AS PER SRM 57-10-00 FIGURE 25 VOLUME I AND INSTALLED REPAIR DOUBLER AT LEFT HAND WING FORWARD LEADING EDGE INNER SKIN, ADJACENT TO REFUELING PANEL AT STA 522 AS PER SRM 51-35-01 VOLUME II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050720001212005072000121NM 2005 7 20 05FDEA01976 120050717A5753 HINGE DOUG MD11 MD11 3023602NM RT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 RT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03 PG 442-443. FABRICATED BUSHING AND INSTALLED AS PER EA 1-5750-87612. 2L73 4F RTA22WE 20050720001222005072000122NM 2005 7 20 05FDEA01978 120050717A5320 FLOOR SUPPORT DOUG MD11 MD11 3023602NM FUSLEAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 CABIN, ALONG STA 1887 TO STA 2007 RBL 24 FLOOR SUPPORT STRUCTURE FOUND CORRODED. REMOVED AND REWORKED NEW FLOOR SUPPORT FROM S3932107-12400 AS PER DWG AGA 7497. NEW FLOOR SUPPORT PAINTED, PART MARKED AND INSTALLED AS PER SRM 51-31-01 VOL II. CLASSIFIED MINOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050720001252005072000125NM 2005 7 20 05FDEA01958 120050714A5320 WEB DOUG MD11 MD11 3023602NM ZONE 100 TORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 CENTER CARGO COMPARTMENT, FOUND FLOOR LEVEL WEB TORN AT STA 1841, RBL 1. TRIMMED OUT , REPAIR DOUBLERS FABRICATED AND INSTALLED IAW SRM 53-00-01 FIG. 10 VOL. I. THIS REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050720001272005072000127NM 2005 7 20 05FDEA01960 120050715A5347ACA7104511 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 MAIN DECK CARGO COMPARTMENT, FLOOR SEAT TRACK AT STA 635, X= - 8.5 FOUND CRACKED APPROXIMATELY 3 INCHES LONG. REPAIRED AS PER SRM 53-70-00 VOLUME I, FIGURE 1. REPAIR CLASSIFID AS MAJOR PER GMM 6-2-100. 2L73 4F RTA22WE 20050720001282005072000128EU 2005 7 20 05FDEA01963 120050715A2432 BATTERY AIRBUS310 A310 EU NR 2 OVERHEATED A FDEAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CRCRUISE 1 SO25450FE 162 NR 2 BATTERY OVERHEATED DURING CRUISE. NR 2 BATT SHOWED 21V AND WAS SWITCHED OFF FOR DURATION OF FLIGHT. VERIFIED BATTERY WAS HOT, AND PERFORMED BATT CHARGE CONT BITE TEST. ALL NORMAL. FOUND RED AND BLUE WIRES 195 AND 196 AT BAT2 SHUNT 19PE DAMAGED AND CHAFING TOGETHER. REPAIRED BOTH WIRES AND REPLACED BATTERY PER PRECAUTIONARY DUE TO OVERHEATING, TESTED BATT CONT BITE TEST AGAIN ALL NORMAL. LET BATTERIES CHARGE FOR 2 HOURS AND OPERATED NORMALLY REF SMP, MM 24-31-11-4 AND WDM 24-31-02. 2L72 4F RTA35EU 20050720001302005072000130NM 2005 7 20 05FDEA01954 120050714A5730 SKIN DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 LEFT WING, FORWARD FIXED LEADING EDGE INNER SKIN FOUND CRACKED, ADJACENT TO NR 4 SLAT STA 540. FABRICATED REPAIR DOUBLER AS PER SRM 57-10-00 FIG. 25 VOL.I AND INSTALLED REPAIR DOUBLER AT LH WING FORWARD FIXED LEADING EDGE INNER SKIN ADJACENT TO NR 4 SLAT STA 540 AS PER SRM 51-35-01 VOL. II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050720001312005072000131NM 2005 7 20 05FDEA01955 120050714A5730 SKIN DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 LEFT WING, FORWARD FIXED LEADING EDGE INNER SKIN FOUND CRACKED, ADJACENT TO REFUELING PANEL AT STA 512. FABRICATED REPAIR DOUBLER AS PER SRM 57-10-00 FIG. 25 VOL.I AND INSTALLED REPAIR DOUBLER AT LH WING FORWARD FIXED LEADING EDGE INNER SKIN, ADJACENT TO REFUELING PANEL AT STA 512 AS PER SRM 57-10-00 FIG. 25 VOL.I AND SRM 51-35-01 VOL.II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050720001332005072000133NM 2005 7 20 05FDEA01933 120050713A5315 FLOORBEAM DOUG MD11 MD11 3023602NM FUSELAGE BROKEN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 CABIN, AT STA 1986 RBL 61 FLOORBEAM STRUCTURE FOUND BROKEN. DISPREPANT FLOOR SUPPORT REMOVED. NEW FLOOOR SUPPORT REWORKED FROM S2929169X7075T6511 AS PER DRAWING AGA 7091 AND INSTALLED AS PER SRM 51-31-01 VOL II. CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050720001352005072000135NM 2005 7 20 05FDEA01935 120050713A5315 FLOORBEAM DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 CABIN, ALONG STA 1887 TO 2007 RBL 19 FLOOR SUPPORT STRUCTURE FOUND CORRODED. FLOOR SUPPORT REMOVED AND REWORKED. 2L73 4F RTA22WE 20050720001362005072000136NM 2005 7 20 05FDEA01936 120050713A5315 FLOORBEAM DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 AT STA 1964 LBL 10 FLOOR SUPPORT STRUCTURE FOUND CORRODED. FLOOR SUPPORT REMOVED. NEW FLOOR SUPPORT REWORKED FROM S2929169X7075T6511 AS PER DRAWING AGA 7091 AND INSTALLED AS PER SRM 51-31-01 VOL II. CLASSIFIED MINOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050720001412005072000141NE 2005 7 20 SA05085 220050715A7250 TURBINE AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE NR 1 ENGINE DAMAGED A USAAEA ENGINE SHUTDOWN UNSCHED LANDING EMYVIBRATION/BUFFET OVER TEMP ENGINE STOPPAGE CLCLIMB 1 EA19738US 1254 779756 EN-ROUTE, CLT TO PHL. AFTER DEPARTURE, THE NR 1 ENGINE HAD A DOUBLE COMPRESSOR STALL, FOLLOWED BY AN IMMEDIATE EGT OVERTEMP. THE CREW FOLLOWED PROCEDURE AND SHUT DOWN THE NR 1 ENGINE. FLIGHT RETURNED TO FIELD CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND TURBINE DAMAGE IN THE NR 1 ENGINE AND THAT IT WILL NOT TURN. THE NR 1 ENGINE WAS REPLACED. FURTHER ACTION PENDING. 2L72 4F4 FRTA28NM E37NE 20050720001422005072000142WP 2005 7 20 05FDEA01754 120050630A5100S392945221 INSULATION DOUG DC10 DC1030 3023501WP ZONE 100 BURNED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25313FE 48311 IN CENTER ACCESSORY COMPARTMENT RT AND LT SIDE OF FUSELAGE INSULATION BLANKET IS SEVERLY BURNED AROUND 1-2 AND 1-3 SYSTEM PNEUMATIC AIR DUCT. BLANKETS ARE REMOVED FOR BLANKETS MOD WILL BE INSTALLED AND SECURED ON EA 8-2580-86498, SEQ NR 780, EMP.97433, QC.98577. 2L73 4F A22WE 20050720001442005072000144NM 2005 7 20 05FDEA01942 120050714A5340 STRINGER CLIP BOEING727 727233 138408ANM FUSLAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 FUSELAGE UPPER LOBE, STRINGER CLIP IS CRACKED, BS 950A, STR 7L . REMOVED AND REPLACED STR CLIP PER SRM 51-30-2. 2L73 4F RTA3WE 20050720001452005072000145NM 2005 7 20 05FDEA01943 120050714A5340 STRINGER CLIP BOEING727 727233 138408ANM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 FUSELAGE UPPER LOBE, STRINGER CLIP IS CRACKED, BS 950B, STR 6L. REMOVED AND REPLACED STR CLIP PER SRM 51-30-2. 2L73 4F RTA3WE 20050720001472005072000147NM 2005 7 20 05FDEA01965 120050715A5311 FRAME BOEING727 727233 138408ANM FUSELAGE CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 FUSELAGE UPPER LOBE, FRAME REPAIR IS CHAFED, BS 970, STR 9R. REPAIRED FRAME PER SRM 51-40-3. 2L73 4F RTA3WE 20050720001512005072000151 2005 7 20 RAIA00507002 420050701A34427021450601 TRANSCEIVER EMB 145 EMB145LR 3260212SO WX RADAR SYS INOPERATIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03846HK 14500855 FLT 8070- IAD- WEATHER RADAR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE WEATHER RADAR R/T ASSEMBLY. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050720001532005072000153NE 2005 7 20 05FDEA01967 220050715A7532 BLEED VALVE AIRBUS310 A310 EU PWA JT9 JT9D7R4E1 52054NE NR 2 MALFUNCTIONED A FDEAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO25417FE 333 AFTER TAKEOFF FROM LISBON HAD NR 2 BLEED VALVE FAULT. DURING RETURN TO LISBON RESET NR 2 BLEED AND FOUND FOLLOWING CONDITIONS: AT 3000 FT NR 1 BLEED TEMP 175 / NR 2 BLEED TEMP 175. THE OVERHEAT WITHIN 2 MINS AT 210 - 220 WITH SUBSEQUENT BLEED VALVE NR 2 FAULT. ON GROUND WITH HP VALVE SELECTED OFF, EVEN AT INCREASE POWER SETTINGS NO PROBLEM NOTED. FAN AIR VALVE REPLACED IAW AMM 36-11-16-4. NO FAULD FOUND ON ENGINE RUN-UP,PERFORMED IAW AMM 71-00-00-5. 2L72 4F4 FRTA35EU E3NE 20050720001552005072000155NM 2005 7 20 05FDEA01969 120050717A53476065491 SEAT TRACK BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25280FE 22347 SEAT TRACK BL 0 STA 600-720 IS CORRODED. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2 2L73 4F RTA3WE 20050720001562005072000156CE 2005 7 20 DXTA200500835 120050712A2710 YOKE CESSNA650 650 2076802CE COCKPIT OUT OF RIG E DXTAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 GL07791QS 6507091 IN LEVEL FLIGHT, LT CONTROL YOKE DEFLECTED 10 DEG - 15 DEG. LT CO-PILOTS YOKE LEVEL/ CENTERED. REMOVED FWD YOKE COVERS L/R YOKES. REMOVED AILERON BELLCRANK PANELS L/R WING. INSTALLED RIG PINS AT YOKES. BOTH YOKES VERIFIED AT NEUTRAL. GAINED ACCESS TO AILERON/ROLL SPOILER MIX ASSY AND C/W CE-650 TASK NR A27-10-10 SPOILER AILERON DISENGAGE AND TASK NR B27-10-10 AILERON SPOILER OPS CK. ALL CHECKED GOOD. REASSEMBLED A/C. L/R YOKES VERIFY NEUTRAL IN GROUND CONDITION. 2L72 4F A9NM 20050720001572005072000157NM 2005 7 20 05FDEA01970 120050717A53476065491 SEAT TRACK BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25280FE 22347 SEAT TRACK BL 0 STA 480-600 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2 2L73 4F RTA3WE 20050720001592005072000159NM 2005 7 20 05FDEA01972 120050717A5347606549 SEAT TRACK BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25280FE 22347 SEAT TRACK 344-480 RBL 24 IS CORRODED. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2 2L73 4F RTA3WE 20050720001622005072000162NM 2005 7 20 0501096717 120050714A2612 FIRE LOOP BOEING747 747251F 1384898NM APU BAY MALFUNCTIONED A NWAAO OTHER N FALSE WARNING CRCRUISE 1 GL01617US 21121 DURING CRUISE, APU FIRE LIGHT B LOOP ILLUMINATED WITH BELL. THEN SELECTED LOOP A. AIRCRAFT CONTINUED ON TO ANC AND LANDED WITHOUT INCIDENT. ANC MAINTENANCE PUT APU FIRE LOOP B ON MEL. 18JUL05 SIN MAINTENANCE R&R UPPER FIRE DETECTOR ELEMENTS LOOP A & B. OPERATIONAL CHECKS OK. 2L74 4F A20WE 20050720001652005072000165NM 2005 7 20 05FDEA01931 120050713A5315 FLOORBEAM DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 CABIN AT STA 1887 RBL 35 FLOORBEAM STRUCTURE FOUND CORRODED. CORROSION REMOVED AND REPROTECTED AS PER SRM 51-21-01 VOL II. MATERIAL THK: 0.080" ,THK REMAINED: 0.072" AND MATERIAL REMOVED: 0.008" FOUND WITHIN LIMIT AS PER SRM 53-00-01 FIG 4 VOL I. REWORKED AREA PAINTED AS PER SRM 51-21-01 VOL II. CLASSIFIED MINOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050720001682005072000168NM 2005 7 20 DHL2005764003 120050715A5522 SKIN BOEING727 727264 138408MNM ELEVATOR DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01764AT 22984 RT. ELEVATOR LOWER SURFACE IS DENTED AT ELEVATOR STA 121. FOUND DENT OUT OF LIMITS. CUT OUT DAMAGE AREA IAW B727 SRM 55-20-1. FABRICATED DOUBLER REPAIR IAW B727 SRM 55-20-3. ALODINED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED DOUBLER IAW B727 SRM 55-20-3 FIG.5. 2L73 4F A3WE 20050720001732005072000173 2005 7 20 KBM2005F00144 420050701A34215040017901 GYRO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE ATTITUDE INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19751H 283 3403 ATTITUDE GYRO INOPERATIVE. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050720001752005072000175EU 2005 7 20 KBM2005F00127 120050625A6720704A34130184 CONTROL CABLE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1B 6OO30NE TAIL ROTOR BINDING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19250SH269 3874 CONTROL ROTOR CABLE, BINDING. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050720001782005072000178NE 2005 7 20 KBM2005F00120 220050527A74209550168600 CABLE SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE IGNITER CHAFED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P 2347 IGNITER CABLE, CABLE IS CHAFED AND SPARKING. REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20050720001842005072000184EU 2005 7 20 KBM2005F00128 120050530A2912806966 FILTER SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1B 6OO30NE HYD SYSTEM BYPASSING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19250SH 3874 HYD FILTER, BYPASS INDICATOR POPPED. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050720001852005072000185EU 2005 7 20 KBM2005F00135 120050623A242523093620010 AMMETER SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1B 6OO30NE COCKPIT READS HIGH E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH 2957 AMPMETER, UNIT READS 30 AMP HIGH AND NEEDLE FLUCTUATING. REMOVED AND REPLACED. DONE AT B2 CONVERSION. (K) 1G71 3U3 U H9EU E19EU 20050720001862005072000186EU 2005 7 20 KBM2005F00136 120050623A63229696 MOTOR SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1B 6OO30NE OIL COOLER RATCHETING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH3871 2957 MOTOR, MAKING RACHETING NOISE. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050720001882005072000188SW 2005 7 20 KBM2005F00141 120050606A3230MS24171D1 RELAY BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL MLG INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1973DP 811 2513 RELAY INOPERATIVE, REMOVED AND REPLACED. (K) 1G71 3U3 U H2SW E4CE 20050720001892005072000189 2005 7 20 KBM2005F00143 420050701A3422200DCL28 GYRO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE DIRECTIONAL PRECESSES A KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19751H 3403 DIRECTIONAL GYRO PRESSESES. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050720001912005072000191EU 2005 7 20 KBM2005F00130 120050710A6720350A21136324 BELLCRANK SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 60053NE TAIL ROTOR CRACKED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV 3296 BELLCRANK, RT T/R BELLCRANK LOWER BRACKET TIE BAR IS CRACKED. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050720001922005072000192EU 2005 7 20 KBM2005F00132 120050604A6410355A09103601 BEARING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE TAIL ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV853 3296 HALF SHELL BEARINGS, WORN. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050720001942005072000194EU 2005 7 20 KBM2005F00148 120050613A6410355A09103601 CASE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE TAIL ROTOR CRACKED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH841 2884 HALF SHELL, UNIT HAS MULTIPLE CRACKS. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050720001962005072000196NE 2005 7 20 P5CA0501376 220050624A7200JT9D7A ENGINE BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE NR 1 FAILED A P5CAEA ENGINE SHUTDOWN UNSCHED LANDING JM WARNING INDICATION OVER TEMP CLCLIMB 1 EA15858FT 20109 662503 AFTER TAKEOFF, NR 1 ENGINE FELT LARGE BANG ALONG WITH EGT OFF SCALE HIGH. SHUT DOWN ENGINE. REMOVED AND REPLACED NR 1 ENGINE MM 71-00-02. 2L74 4F4 F A20WE E20EA 20050720002002005072000200NM 2005 7 20 UPS05444888 120050712A5320 WEB BOEING747 747123F NM NLG W/W CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 NLG RT SIDE WEB FOUND CRACKED AT STA 300 WL 150. CRACK LENGTH 0.25 IN. NLG W/W RHS SIDE WEB REPAIRED AT BS 300 WL 150 AREA AS PER SRM 53-10-04 FIG 116. 2L74 4F A20WE 20050720002012005072000201NE 2005 7 20 UPS05444898 220050714A7200 ENGINE BOEING747 747212B 1384886NM PWA JT9 JT9D7Q 52054NE NR 3 FAILED A IPXAA UNSCHED LANDING Y ENGINE STOPPAGE UKUNKNOWN 1 SO01521UP 21944 NR 3 ENGINE FAILED. REPLACED NR 3 ENGINE IAW TASK CARD 5000, 5016. OPS CHECK GOOD. 2L74 4F4 F A20WE E3NE 20050720002022005072000202NM 2005 7 20 05FDEA01914 120050713A5320 FLOOR SUPPORT DOUG MD11 MD11 3023602NM CABIN CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 CABIN, AT STA 1887 ALONG RBL 38.5 TO RBL 53.5 FLOOR SUPPORT STRUCTURE FOUND CORRODED. SUPPORT REPLACED AS PER DWG AGA8027 AND SRM 51-31-01 VOL2. 2L73 4F RTA22WE 20050720002032005072000203NM 2005 7 20 05FDEA01915 120050713A5320 FLOOR SUPPORT DOUG MD11 MD11 3023602NM CABIN CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 CABIN STA 1887 RBL 54 FLOOR SUPPORT STRUCTURE FOUND CORRODED. CORROSION REMOVED AND REPROTECTED AS PER SRM 51-21-01 VOL II. MATERIAL THK: 0.125", MATERIAL REMAINED: 0.113" AND MATERIAL REMOVED: 0.012" FOUND WITHIN LIMIT AS PER SRM 53-00-01 FIG 4 VOL I. REWORKED AREA PAINTED AS PER SRM 51-21-01 VOL II. CLASSIFIED MINOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050720002042005072000204EA 2005 7 20 SWIA200515272 120050422A5340 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07962SW 7859 FUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH ANGLES ARE CRACKED. INBOARD AND OUTBOARD; FS 280.00; LBL - 9.0. REPLACED ATTACH ANGLES IAW CRJ SRM 51-40-11, 51-42-06, 51-23-00, 51-42-21, 51-25-16, 51-21-11, 57-42-13. 2L72 4F RTA21EA 20050720002052005072000205EA 2005 7 20 SWIA200515273 120050422A5340 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07962SW FUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH ANGLE IS CRACKED, OUTBOARD SIDE FS280.00 RBL 9.0. REPLACED ATTACH ANGLE IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-21-11, 51-42-13. 2L72 4F RTA21EA 20050720002062005072000206EA 2005 7 20 SWIA200515274 120050714A2740 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA COCKPIT STICKS A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07587SW 7062 CAPT YOKE PITCH TRIM SWITCH STICKS. REPLACED SWITCH IAW MM 27-41-05. OPERATIONAL CHECK GOOD IAW MM 27-41-00. 2L72 4F RTA21EA 20050720002082005072000208NM 2005 7 20 QXEA200501105 120050712A7930 OIL SYSTEM BOMBDRDHC8 DHC8402 1390042NM PWC 150 PW150A EA NR 1 ENGINE OVERTEMP A QXEAO OTHER M OVER TEMP CLCLIMB 1 NM09409QX 4051 ABOUT 5 MIN AFTER TAKEOFF, NR 1 OIL TEMP CLIMBED TO 114 DEG C. CLOSED ENGINE INTAKE BYPASS DOORS IAW CHECKLIST. ABOUT 5 MINUTES LATER, TEMP DROPPED TO 107 DEG C AND KEPT DECREASING SLOWING TO ABOUT 77 DEG C WHERE IT REMAINED FOR REST OF FLIGHT. MAINTENANCE INTERROGATED CDS IAW Q400 AMM TASK 45-00-73-742-801. NO CURRENT FAULT MOT 114.5 DEG C FOR 515 SECONDS OK FOR SERVICE IAW Q400 AMM 05-11-992-802. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E00062EN 20050718002202005071800220NM 2005 7 18 HNAA0500066 120050712A2400 WARNING LIGHT DHAV DHC8 DHC8102 2809003NM DC BUSS ILLUMINATED A HNAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA07810EX 308 DC BUSS CAUTION LIGHT ILLUMINATED AFTER TAKEOFF FOLLOWED BY ASSOCIATED CAUTION LIGHTS. INSPECTED DC CONTACTOR BOX, TRU AREA, NR 1 AND 2 DC GENERATORS GROUND RAN AIRCRAFT WITH NO DEFECTS NOTED 2H72 4T RTA13NM 20050718002232005071800223EA 2005 7 18 VTZA2005137 120050711A5712601R102328 RIB CNDAIRCL600 CL6002B19 1900309EA RT WING CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27654BR 7454 RT BATTERY RIB CRACKED 0.75 IN BETWEEN ATTACHING FASTENERS. 2L72 4F RTA21EA 20050718002252005071800225EA 2005 7 18 VTZA200500139 120050711A5346601R536066 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA LT ENGINE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27654BR 7454 LT ENGINE SUPPORT BEAM CRACKED IN LOWER WEB AT 0.75 IN. 2L72 4F RTA21EA 20050719000192005071900019NE 2005 7 19 S2YA05032 220050514A7261 ENGINE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE RIGHT LOW A S2YAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL13831SK232063333 UE83 DURING FLIGHT, CREW REPORT THE RT OIL PRESSURE WAS FLUCTUATING BETWEEN 70 AND 80 PSI AND OCCASIONALY DROPPING TO 50 TO 60 PSI AND THEY WERE GETTING A RED WARNING LIGHT. THE CREW PERFORMED AN AIR-TURN-BACK. OUTSTATION MECHANIC INSPECTED ENGINE CHEC THE CHIP DETECTOR AND ADDED OIL. AC WAS FERRIED BACK. MECHANIC REPLACED THE ENGINE AND RETURNED THE AC TO SERVICE. (K) 2L72 4T4 TRTA24CE E26NE 20050719000222005071900022NM 2005 7 19 USAA050738 120050607A575465C2660399A CHANNEL BOEING737 737301 1384611NM CFMINTCFM56 CFM563B2 13802EU NR 3 SLAT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19589US53594 23934 CLT - C4- CHANNEL, 1 INCH CRACK, NR 3 SLAT JUST BELOW ROD END ACTUATOR ATTACHMENT POINT (L) CHANNEL. FABRICATED AND INSTALLED NEW CHANNEL. (K) 2L72 4F4 FRTA16WE E21EU 20050719000582005071900058NM 2005 7 19 ASAA0540236 120050511A5330653576813 SKIN BOEING737 7374Q8 138447QNM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02783AS 25114 OKC - FUSELAGE SKIN IS DENTED AND GOUGED AT BS 390-410 STRINGER 19R OUT OF LIMITS IAW 737-400 SRM 53-00-01, DUE TO PROXIMITY TO FLAP SEAM. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW AS EA 5330-01930 AND AAR EA 10936. (M) 2L72 4F RTA16WE 20050719000602005071900060NM 2005 7 19 ASAA0510136 120050613A5753657194034 SKIN BOEING737 737290C 138448VNM FORE FLAP CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX - FOUND RIGHT INBOARD FORE FLAP CHAFE DAMAGE ON OUTBOARD TOP SURFACE AT WBL 181. RIGHT OUTBOARD FORE FLAP OUTBOARD TOP SURFACE AT WBL 181 CHAFED LOCATION REPAIRED IAW B737-200 SRM 51-40-20 REPAIR 4 FIG 13 WBL 181. (M) 2L72 4F A16WE 20050719000622005071900062NM 2005 7 19 ASAA0510144 120050613A5753657192682 SKIN BOEING737 737290C 138448VNM TE FLAP DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX - IMPACT DAMAGE ON OUTBOARD TRAILING EDGE OF RIGHT INBOARD MID FLAP. RIGHT INBOARD MID FLAP IMPACT DAMAGE LOCATION REPAIRED IAW B737-200 SRM 51-40-20 REPAIR 1. (M) 2L72 4F A16WE 20050719000642005071900064NM 2005 7 19 ASAA0540240 120050511A53206552878122 SILL BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02792AS 28887 PAE - FOUND CORROSION AT R2 DOOR MOPSILL. REMOVED AND REPLACED. (M) 2L72 4F RTA16WE 20050719000662005071900066NM 2005 7 19 ASAA0540214 120050427A575565464525 SKIN BOEING737 737490 1384715NM SPOILER DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02799AS 29270 SEA - DENT ON BOTTOM OF INBOARD SPOILER ON AFT EDGE AFT OF INBOARD ACTUATOR A=.250, Y=.027, A/Y=9.25. OUT OF LIMITS PER B737 SRM 57-50-01. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW B737 SRM 51-70-10 REPAIR 21. (M) 2L72 4F RTA16WE 20050719000682005071900068WP 2005 7 19 ASAA0580195 120050404A5320 CHANNEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02950AS 53023 OKC - FOUND DURING C-CHECK, CABIN FLOOR PANEL HAT CHANNEL IS CRACKED AND WORN THROUGH. REPLACED HAT CHANNEL. (M) 2L72 4F RTA6WE 20050719000702005071900070NM 2005 7 19 ASAA0510149 120050613A5320654795713 FLOOR SUPPORT BOEING737 737290C 138448VNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX - FOUND FLOOR SUPPORT FORMER AT BS 790 RBL 21 ELONGATED HOLES. REMOVED AND REPLACED FORMER IAW B737-200 SRM. (M) 2L72 4F A16WE 20050719000722005071900072NM 2005 7 19 ASAA0510156 120050613A53226546549511 SHEAR TIE BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX - AFT CARGO PIT SHEAR TIE HAS CORROSION OUTBOARD OF RIGHT KEELBEAM, STRINGER 27R BS 767. REMOVED AND REPLACED SHEAR TIE IAW B737-200 SRM. (M) 2L72 4F A16WE 20050719000742005071900074NM 2005 7 19 ASAA0540172 120050315A531165C323946 FRAME BOEING737 737490 1384715NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02791AS 28886 PAE - PASSENGER CABIN, BS 601 FRAME CHORD IS CRACKED AT RBL 64, WL 204. REPAIRED FRAME CHORD PR EA 5310-02449. (M) 2L72 4F RTA16WE 20050719000822005071900082NM 2005 7 19 ASAA0540241 120050512A53206549631996 SUPPORT ANGLE BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02792AS 28887 PAE - FOUND CORROSION AT FORWARD CARGO BAY, FLOOR TO AFT BULKHEAD SUPPORT ANGLE. REMOVED AND REPLACED BULKHEAD SUPPORT ANGLE. (M) 2L72 4F RTA16WE 20050719000842005071900084NM 2005 7 19 ASAA0540231 120050508A53306548240504 SKIN BOEING737 7374Q8 138447QNM FUSELAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02783AS 25114 OKC - FOUND AFT FUSELAGE SKIN CHAFED BETWEEN FS 1138 AN 1156, JUST BELOW THE LEFT HORIZ STAB LOWER MOUNT. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND SKIN IAW BOEING 737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20050719000862005071900086NM 2005 7 19 ASAA0510168 120050614A5330654576989 SKIN BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX - FOUND FUSELAGE SKIN BULGING AT BS 535 STRINGER 28 LEFT KEEL BEAM. REMOVED AND REPLACED KEEL BEAM AND REPAIRED SKIN IAW B737-200 SRM. (M) 2L72 4F A16WE 20050719000882005071900088WP 2005 7 19 ASAA0580248 120050509A533059114063 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAO OTHER O OTHER NRNOT REPORTED 1 NM02968AS 53016 OKC - FOUND DURING C-CHECK, FUSELAGE SKIN HAS DENT AT STATION 211 BELOW 14R. RECONDITIONED SKIN AND INSTALLED DOUBLER. (M) 2L72 4F RTA6WE 20050719000902005071900090WP 2005 7 19 ASAA0580263 120050517A53209958212 INTERCOSTAL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - FOUND DURING C-CHECK, LONGERON 28R INTERCOSTAL IS CORRODED BETWEEN STATION 1003 AND 1022. REMOVED AND REPLACED INTERCOSTAL. (M) 2L72 4F RTA6WE 20050719000922005071900092WP 2005 7 19 ASAA0580300 120050604A575359304944 VANE DOUG DC9 DC983 3022083WP TE FLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02961AS 53075 OKC - FOUND HV-CHECK, RIGHT FLAP VANE DENTED ON LOWER SURFACE. REMOVED DAMAGED SECTION. INSTALLED FILLER AND DOUBLER. (M) 2L72 4F RTA6WE 20050719000942005071900094WP 2005 7 19 ASAA0580264 120050517A533059360041 SKIN DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - FOUND DURING C-CHECK, MID CARGO COMPARTMENT STATION 731 LONGERON 30 SKIN AROUND DRAIN COVER IS CORRODED. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050719000962005071900096WP 2005 7 19 ASAA0580182 120050404A532199365851 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02950AS 53023 OKC - FOUND DURING C-CHECK, CABIN FLOOR PANEL HAS DAMAGED INSERTS AND EDGE POTTING DAMAGE. REPLACED PANEL. (M) 2L72 4F RTA6WE 20050719000982005071900098WP 2005 7 19 ASAA0580228 120050509A532199365451 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - FOUND DURING C-CHECK, FLOORBOARD IS DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050719001012005071900101WP 2005 7 19 ASAA0580221 120050509A532199365441 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - FOUND DURING C-CHECK, CABIN FLOOR PANEL EDGES SEPARATING, DELAMINATING. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050719001022005071900102NM 2005 7 19 ASAA0510094 120050511A534065353524 STRINGER CLIP BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 UXX - AFT CARGO BS 907 CORRODED TIE CLIP AT STRINGER 21L. REMOVED AND REPLACED TIE CLIP. (M) 2L72 4F A16WE 20050719001252005071900125NM 2005 7 19 DXTA200500833 120050711A2751244142 POTENTIOMETER AMD FALC50FALCON2000 2730170NM COCKPIT FAILED E DXTAA UNSCHED LANDING O OTHER CRCRUISE 1 GL07298QS4857 98 FLAP CONTROL CIRCUIT BREAKER POPPED IN CRUISE FLIGHT. FLAP HANDLE WAS NOT MOVED AND REMAINED IN UP POSTION. INSTALLED REPAIRED LT POTENTIOMETER IAW FALCON 2000 M/M 27-509. 2K73 4F RTA50NM 20050719001272005071900127NM 2005 7 19 PIDA20050058 120050712A33503114981 REFLECTOR BOEING737 7373G7 1384595NM EMERGENCY LIGHTSDEFECTIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05390WL 23219 L2 DOOR EXTERIOR EMERGENCY LIGHT INOP. FOUND REFLECTOR ASSEMBLY LIGHT SOCKET BAD. REPLACED REFLECTOR ASSEMBLY. OPS CHECKS NORMAL PER MM 33-51. 2L72 4F RTA16WE 20050719001512005071900151NM 2005 7 19 ASAA0510172 120050614A531465621252 KEELBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX - FOUND CORROSION ON RIGHT KEEL BEAM AT BS 636. LEFT KEEL BEAM REPLACED IAW B737-200 SRM. (M) 2L72 4F A16WE 20050719001882005071900188NM 2005 7 19 72300218 120050218A5347 SEAT TRACK BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 CORROSION ON SEAT TRACK. 2L73 4F4 FRTA3WE E2EA 20050719001892005071900189NM 2005 7 19 72300219 120050525A5320 INTERCOSTAL BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 CORROSION ON INTERCOSTAL REPLACEMENT. 2L73 4F4 FRTA3WE E2EA 20050719001982005071900198WP 2005 7 19 UPS05844891 120050623A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE C-1, LT FUSELAGE EXTERIOR SKIN CRACKED 1 IN LONG AT STA 1746 BETWEEN L14L TO L15L. REMOVED DAMAGED AREA OF SKIN, FABRICATED, AND INSTALLED REPAIR DOUBLER, FINGER DOUBLERS, AND FILLERS IAW DC-8 SRM 53-2-1 FIG 7. 2L74 4F RT4A25 20050719002062005071900206WP 2005 7 19 UPS05844900 120050627A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE C-1, RT WING L/E UPPER RIB CRACKED AT XFS 721. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR ANGLE DOUBLE IAW DC-8 SRM 57-2-0 FIG 2 AND 57-3-3 FIG 7. 2L74 4F RT4A25 20050719002092005071900209NM 2005 7 19 SWAA052040 120050713A3350OL3071BPEGL BULB BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29333SW 23697 DURING SCHEDULED A2 CHECK, FOUND RT AFT CABIN BULLNOSE EMERGENCY LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050719002112005071900211NM 2005 7 19 SWAA052042 120050712A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29382SW 26588 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050719002132005071900213NM 2005 7 19 SWAA052044 120050712A3350MS155721 BULB BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29445WN 29841 DURING SCHEDULED MV2 CHECK, FOUND EXTERNAL EMERGENCY EXIT LIGHT INOP FWD OF AFT CARGO DOOR. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050719002152005071900215NM 2005 7 19 SWAA052046 120050713A3350MS155721 BULB BOEING737 737301 1384611NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR EXTERNAL EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050719002172005071900217NM 2005 7 19 SWAA052048 120050713A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29332SW 23696 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 777, STR 24R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050719002192005071900219NM 2005 7 19 SWAA052050 120050714A3350D71702001 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT WILL NOT TEST A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29412WN 29818 DURING SCHEDULED HC2 CHECK, 3 EACH CABIN EMERGENCY LIGHT BATTERIES FAILED TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2L72 4F RTA16WE 20050719002212005071900221NM 2005 7 19 SWAA052052 120050713A53306545774 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 18R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050719002232005071900223NM 2005 7 19 SWAA052054 120050713A5313BAC1498 STRINGER BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 500D, STR 23L. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20050719002252005071900225NM 2005 7 19 SWAA052068 120050715A53116546549 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29613SW 27931 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 767, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050719002262005071900226NM 2005 7 19 SWAA052069 120050715A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29613SW 27931 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 767, BETWEEN LBL 6 TO RBL 6. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050719002272005071900227NM 2005 7 19 SWAA052070 120050715A53116546551 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29613SW 27931 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 807, LBL 17. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050719002302005071900230NM 2005 7 19 SWAA052074 120050715A53116546539 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29613SW 27931 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, LBL 65 & RBL 65, WL 200. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20050719002322005071900232 2005 7 19 SWAA052076 420050715A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29626SW 27702 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050719002342005071900234EU 2005 7 19 USAA050761 120050614A5315 FLOORBEAM AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19107US 1052 PIT - S2 - FLOORBEAM, 2 INCH X 2 INCH, CORROSION; FLOORBEAM FR 16Y, 22 INCH. REPLACED FLOORBEAM IAW SRM. (K) 2L72 4F4 FRTA28NM E38NE 20050719002362005071900236EU 2005 7 19 USAA050757 120050614A5315D53472172201 FLOORBEAM AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19107US18257 1052 PIT - S2 - FLOORBEAM, 1INCH X 6 INCHES AREA, CORROSION; NO LEVEL OR TASK, FLOORBEAM RT SIDE AT Y1162.5. DEFECTIVE PART REPLACED WITH IDENTICAL PART IAW SRM AND EA. (K) 2L72 4F4 FRTA28NM E38NE 20050719002382005071900238EU 2005 7 19 USAA050759 120050614A5315D53472172200 FLOORBEAM AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19107US 1052 PIT - S2 - FLOORBEAM, 1 INCH X 6 INCHES, CORRODED. FLOORBEAM LT SIDE AT STA 1162.5. DEFECTIVE PART REPLACED WITH IDENTICAL PART IAW SRM AND EA. (K) 2L72 4F4 FRTA28NM E38NE 20050719002432005071900243EU 2005 7 19 05FDEA01916 120050713A2821 FILTER AIRBUS310 A310 EU FUEL SYSTEM CLOGGED A FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25402FE 201 REJECTED TAKE OFF AS 95 KNOTS DUE TO ECAM WARNING 'ENG FUEL FILTER CLOG' WARNING WAS RESOLVED AS SOON AS THROTTLES WERE RETARDED. TOGA POWER WAS USED (104.7 PERCENT N1) MESSAGE DISAPPEARED QUICKLY AND WE WERE UNC ERTAIN OF WHICH ENGINE WAS AFFECTED. PULLED BOTH MAIN FUEL FILTERS. BOTH WERE CLEANED. REPLACED WITH NEW FILTERS, RAN BOTH ENGS FOR LEAK CHECK AND TO CHECK CLOG LIGHTS. NO LEAK,NO LIGHTS, RELEASED A/C FOR SERVICE. AMM 73-12-03 REMOVED & REPLACED FUEL FILTERS. 2L72 4F RTA35EU 20050719002442005071900244NM 2005 7 19 05FDEA01917 120050713A534066118099 STRINGER CLIP BOEING727 727200 138407ENM FUSLAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 N01123 E & E BAY STA 460, RBL 6, WL 145 STR CLIP IS CRACKED. REMOVED FABRICATED AND INSTALLED STRINGER CLIP BS 460 RBL 6 WL 145 PER SRM 51-20-1 AND SRM 51-30-2 2L73 4F RTA3WE 20050719002462005071900246NM 2005 7 19 05FDEA01918 120050713A534065453132 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 FUSELAGE UPPER LOBE, STRINGER CLIP CRACKED, BS 640, STR. 9 RT. 2L73 4F RTA3WE 20050719002472005071900247NM 2005 7 19 05FDEA01919 120050713A534065453132 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 FUSELAGE UPPER LOBE, STRINGER CLIP IS CRACKED, BS 700, STR 6. REMOVED FABRICATED AND REPLACED STRINGER CLIP AT BS 700 STR 6R PER SRM 51-30-02, 51-20-1, 51-10-02 2L73 4F RTA3WE 20050719002502005071900250NM 2005 7 19 PIDA20050059 120050715A335020131A BATTERY PACK BOEING737 73739A 138447PNM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05375PA 23812 AFT CENTER AISLE EMERGENCY LIGHT INOP. REPLACED AFT RIGHT BATTERY PACK PER MM 33-50. 2L72 4F RTA16WE 20050719002522005071900252NM 2005 7 19 05FDEA01922 120050713A534065453132 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE MISSING A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 FUSELAGE UPPER LOBE STRINGER CLIP MISSING FRAME ATTACH FASTENERS BS 680, STR 6L. REMOVED, FABRICATED AND INSTALLED STRINGER CLIP AT BS 680 STR 6L IAW SRM 51-20-1, 51- 30-02 AND 51-10-02. 2L73 4F RTA3WE 20050719002572005071900257NM 2005 7 19 UPS05M44909 120050714A3230 LANDING GEAR DOUG MD11 MD11 3023602NM NLG MALFUNCTIONED A IPXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01254UP 48406 NOSE GEAR DOES NOT LOCK IN UP POS. INSPECTED NOSE GEAR LINKAGES, DOORS WHEEL WELL AND NOSE WHEEL STEERING NIL DEFECTS FOUND. JACKED A/C PER MD11 AMM 07-11-00-2 AND ILLEG NOSE GEAR PER AMM 32-30-00 FOUND NORMAL. 2L73 4F RTA22WE 20050719002592005071900259NM 2005 7 19 SWAA052077 120050716A57536546435274 SKIN BOEING737 7373G7 1384595NM RT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29670SW 23784 DURING SCHEDULED C2 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM. 2L72 4F RTA16WE 20050719002602005071900260NM 2005 7 19 SWAA052078 120050716A3350311500 LENS BOEING737 7373G7 1384595NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29670SW 23784 DURING SCHEDULED C2 CHECK, FOUND BULLNOSE LIGHT LENS LOOSE AT ROW 21 ABC. SECURED LENS PER MM. 2L72 4F RTA16WE 20050719002612005071900261NM 2005 7 19 SWAA052079 120050716A3350D71702001 BATTERY BOEING737 7373G7 1384595NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29670SW 23784 DURING SCHEDULED C2 CHECK, AFT CABIN EMERGENCY EXIT LIGHTS BATTERY FAILED TEST. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20050719002622005071900262NM 2005 7 19 SWAA052080 120050716A21317638106 CONTROLLER BOEING737 7373T5 1384608NM CABON PRESSURE INOPERATIVE A SWAAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SW29692SW 23062 AIR TURNBACK, AUTO STANDBY & DC FUNCTION INOP ON PRESSURIZATION CONTROL PANEL. REMOVED AND REPLACED AUTO PRESSURIZATION CONTROLLER PER MM. 2L72 4F RTA16WE 20050719002632005071900263NM 2005 7 19 SWAA052081 120050717A335065C27093 LIGHT BOEING737 7377H4 1384404NM R2 DOOR INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29720WN 27854 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20050719002642005071900264NM 2005 7 19 SWAA052082 120050715A3350101073 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29746SW 29798 FWD ENTRY EMERGENCY EXIT LOWER SIGN BROKEN. REMOVED AND REPLACED LENS ASSY PER MM. 2L72 4F RTA16WE 20050719002652005071900265NM 2005 7 19 SWAA052083 120050716A3350D71701100 BATTERY PACK BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29748SW 29800 DURING SCHEDULED MV2 CHECK, FOUND LT FWD & AFT GALLEY EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACKS PER MM. 2L72 4F RTA16WE 20050719002662005071900266 2005 7 19 SWAA052084 420050717A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29755SA 27871 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20050719002672005071900267 2005 7 19 SWAA052085 420050715A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29771SA 27879 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050719002682005071900268NM 2005 7 19 SWAA052055 120050717A3350101331 COVER BOEING737 7373H4 1384600NM EMERGENCY LIGHT CRAZED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED 1/4D CHECK, FOUND RT EXTERIOR EMERGENCY EXIT DOOR LIGHT COVER CRAZED. REMOVED AND REPLACED COVER PER MM. 2L72 4F RTA16WE 20050719002692005071900269NM 2005 7 19 SWAA052056 120050717A53226546529 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE BELTFRAME SHEAR TIE CORRODED AT BS 500D, BL 0. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050719002702005071900270NM 2005 7 19 SWAA052057 120050715A33506104781 BATTERY PACK BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29325SW 23689 DURING SCHEDULED RON CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT ILLUMINATED WITH SWITCH IN ARMED POSITION. RESEATED CONNECTOR TO BATTERY PACK PER MM. 2L72 4F RTA16WE 20050719002712005071900271NM 2005 7 19 SWAA052058 120050715A335090083 BATTERY BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29332SW 23696 DURING SCHEDULED C1 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20050719002722005071900272NM 2005 7 19 SWAA052059 120050715A55236959227 BUSHING BOEING737 7373H4 1384600NM LT ELEVATOR TAB WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29332SW 23696 DURING SCHEDULED C1 CHECK, LT ELEVATOR TAB FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR TAB NR 1 HINGE BUSHING & HARDWARE PER MM. 2L72 4F RTA16WE 20050719002732005071900273NM 2005 7 19 SWAA052060 120050716A531265458197 PRESSURE PANEL BOEING737 7373H4 1384600NM NLG WW CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29344SW 24152 DURING SCHEDULED SERVICE CHECK, FOUND RT NLG W/W FWD PRESSURE SIDE PANEL CRACKED AT BS 243.7, WL 168.5. REPAIRED PANEL PER SWA EA. 2L72 4F RTA16WE 20050719002742005071900274NM 2005 7 19 SWAA052061 120050715A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29356SW 25251 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 887, STR 25R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050719002752005071900275NM 2005 7 19 SWAA052062 120050715A53126546568 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29356SW 25251 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE WEB CRACKED AT AFT PRESSURE BULKHEAD, BS 1016, STR 6L. REPAIRED AFT PRESSURE BULKHEAD WEB PER SRM.. 2L72 4F RTA16WE 20050719002812005071900281EA 2005 7 19 SWIA200515276 120050711A2741 TRANSMITTER CNDAIRCL600 CL6002C10 1390015EA STAB POSITION MALFUNCTIONED A SWIACD ABORTED TAKEOFF RETURN TO BLOCK FJ FLT CONT AFFECTED WARNING INDICATION TOTAKEOFF 1 NM07744SK 10200 ELEVATOR SPLIT CAUTION MESSAGE DISPLAYED. RETURN TO FIELD PER QRH. REMOVED AND REPLACED ELEVATOR POSITION TRANSMITTER PER MM 27-34-10. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050720000012005072000001NM 2005 7 20 SWAA052067 120050715A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29613SW 27931 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 294, STR 13L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050720000022005072000002NM 2005 7 20 USAA050815 120050629A5320 STIFFENER BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19441US 24812 CLT - Q5 - FLOOR STIFFENER, 2 INCH X 16 INCH CORROSION, STA 312-328, LBL12. DEFECTIVE PART REPLACED WITH IDENTICAL PART, REMOVED AND REPLACED STIFFENER IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050720000062005072000006NM 2005 7 20 USAA050800 120050627A575365C2632011A SKIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU LT OB MID FLAP WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19441US 24812 MID FLAP SKIN, .500 WIDE X 4 INCHES LONG, WORN AREA, LT OB MID FLAP BOTTOM SIDE 68 INCH FROM IB END. REMOVED DAMAGE AND INSTALLED NEW TRIPLER DOUBLER IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050720000202005072000020NM 2005 7 20 USAA050818 120050629A5240654587139 DOOR FRAME BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU SERVICE DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19430US42737 24552 CLT - C3 - FWD SERVICE DOOR, .6 INCH CRACK, FWD SERVICE DOOR FRAME LOWER AFT CORNER AFT LIGHTING HOLE. INSTALLED DOUBLER IAW EA. (K) 2L72 4F4 FRTA16WE E21EU 20050720000222005072000022NM 2005 7 20 USAA050805 120050629A5340 MOUNT BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU AFT LAVATORY CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU52779 23861 CLT - Q2 - LAV MOUNT, 1 INCH X 3 INCHES, CORROSION, LT AFT LAV OB MOUNT. FABRICATED AND INSTALLED NEW MOUNT IAW WITH DRWG. (K) 2L72 4F4 FRTA16WE E21EU 20050720000332005072000033NM 2005 7 20 AWXA200500821 120050714A2560P4010021 BATTERY BOEING737 7373G7 1384595NM FLASHLIGHT DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 MCN - EES - DURING C16 CHECK DISCOVERED THE AFT FLIGHT ATTENDANTS EMERGENCY FLASHLIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE AFT FLIGHT ATTENDANTS EMERGENCY FLASHLIGHT BATTERY PACK. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20050720000372005072000037NM 2005 7 20 05FDEA01924 120050713A5340 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 CRACKED STRINGER CLIP BS 990 AT STRINGER 28L FWD SIDE OF FRAME. REPLACED CRACKED STRINGER CLIP PER SRM 51-10-1. 2L73 4F RTA3WE 20050720000392005072000039WP 2005 7 20 UPS05844769 120050605A5343 FITTING DOUG DC8 DC871F 302199DWP RT WW CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01705UP 45949 INSPECTION TYPE C-2, CORNER FITTING CRACKED AND HEAVILY CORRODED, RT W/W STA 980 CEILING O/B CORNER NEXT TO L24R. REMOVED FITTING IAW SRM 51-1-20D. FABRICATED DOUBLER, REPAIR ANGLE AND FILLERS IAW SRM 53-02-00-0, INSTALLED DOUBLER REPAIR ANGLE AND FILLERS IAW SRM51-1-20D, AND 51-1-15. 2L74 4F RT4A25 20050720000642005072000064EA 2005 7 20 VTZA200500127 120050623A2750 FCU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A VTZAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 EA27642BR 7406 FLAP FAIL AT "0" ON CLIMB-OUT. PERFORMED BITE AND SYSTEM TEST ON FECU. TEST GOOD. 2L72 4F RTA21EA 20050720000652005072000065NM 2005 7 20 UPS05M44724 120050623A3350 LIGHT DOUG MD11 MD11F 3023600NM COCKPIT WILL NOT TEST A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01253UP 48439 EMERGENCY POWER LIGHT TEST FAIL ILLUM ON PREFLIGHT. ACCOMPLISHED OPERATIONAL TEST OF EMERGENCY POWER TEST FAIL ALERT. CHECK OK REF MM 24-00-01-5. 2L73 4F RTA22WE 20050720000672005072000067NM 2005 7 20 ASMF200506030 120050629A32465930594547 WHEEL DOUG MD88 MD88 3023688NM MLG DAMAGED W ASMFED ENGINE SHUTDOWN RETURN TO BLOCK EJ VIBRATION/BUFFET WARNING INDICATION TXTAXI/GRND HDL 1 SW23158PL117998129 49761 DURING TAXI A STRONG NOISE AND VIBRATION DETECTED AT MLG AREA. ENGINES SHUTDOWN. TROUBLESHOOTING DETERMINED THAT NOISE WAS PROMOTED BY HYDRAULIC PULSING OF ELECTRICAL PUMPS AND GCU. GCU PLACED IN APU POSITION AND PROBLEM WAS CORRECTED. DURING OVERNIGHT SERVICE, A REVISION PERFORMED TO BOTH MLG, DETECTING WHEEL CAP INCRUSTED IN WHEEL NR 2 OF LT MLG. WHEELS NUMBER 1 AND 2 REPLACED IAW MM 32-40-01. BRAKES CORRECT. REGARDING THE GCU, THE UVC, OIL LEVEL AND CHIP DETECTOR WERE CHECKED IAW MM 24-10-01 AND BEING CORRECT. GENERATION TEST PERFORMED IAW MM 24-2-00, ALL CORRECT. 2L72 4F RTA6WE 20050720000732005072000073NM 2005 7 20 ANCF200400052 120050709A2110 CABIN PRESSURE DOUG MD80 MD83 3023681NM MALFUNCTIONED W ANCFA UNSCHED LANDING O OTHER CRCRUISE 1 SO23583AN 53183 UNABLE TO MAINTAIN CABIN PRESSURE AT FL 330 WITH 0.78 MACH. REQUESTED FL 290 WITH SAME SET OF PWR. FLOW LIGHT REMAINED ON AND CABIN ALT CONTINUED INCREASING. NECESSARY TO SELECT ENGINE AND AIRFOIL ANTI-ICE DUE WEATHER CONDITIONS. CABIN RATE INCREASED AND NECESSARY TO REQUEST LOWER LEVEL AND RETURN TO FIELD. WITH POWER SETTINGS OF N1 86 PERCENT, CABIN CONTINUED INCREASING. AS PER MEL 21-1 CATEGORY C, RT PACK INOPERATIVE, ADJUSTED CLAMPS AND REINSTALLED HOSE IN ACM. 2L72 4F RT 20050720000742005072000074EA 2005 7 20 ASOA05529 120050617A335060206 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27838AS 7276 FLT 4906 - DURING AN OVERNIGHT MAINTENANCE VISIT TO CAE, THE FLOOR LEVEL EMERGENCY LIGHT BY THE PASSENGER DOOR WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE INOPERATIVE EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050720000762005072000076EA 2005 7 20 ASOA05531 120050604A5712 RIB CNDAIRCL600 CL6002B19 1900309EA RT WING CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27909EV 7658 DURING A C-CHECK IN HOT, THE RIGHT BATT RIB ASSEMBLY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RIGHT BATTERY RIB ASSEMBLY AT WS 53.60 IAW ASA EO 600-57-039A. (M) 2L72 4F RTA21EA 20050720000812005072000081EA 2005 7 20 ASOA05514 120050610A5320 SILL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAO OTHER O OTHER NRNOT REPORTED 1 SO27830AS 7236 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT FLOOR SILL ASSEMBLY, AROUND THE NUT PLATES, FINGER DOUBLERS, ATTACH ANGLES AND TRANSVERSE BEAMS, BETWEEN FS 424 AND FS 559 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT FLOOR SILL ASSEMBLY BETWEEN FS 424 AND FS 559 IAW ASA EO 600-53-0271. (M) 2L72 4F RTA21EA 20050720000842005072000084EA 2005 7 20 ASOA05515 120050612A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA BULKHEAD CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27830AS 7236 DURING A C-CHECK IN MCN, THE PILOT`S BULKHEAD FS 280 FRAME AT RBL 11 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE PILOTS BULKHEAD FS 280 FRAME AT RBL 11 IAW ASA EO 600-53-0123. (M) 2L72 4F RTA21EA 20050720000872005072000087EU 2005 7 20 ASOA05525 120050616A33503012000 POWER SUPPLY AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT DISCHARGED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27633AS 344 DURING A GROUND INSPECTION IN MGM, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTS POWER SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20050720000932005072000093EA 2005 7 20 ASOA05516 120050614A5320 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27908EV 7654 DURING A C-CHECK IN MCN, THE FS 484 AFT BRACKETS AT LBL 36 AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FS 484 AFT BRACKETS AT LBL 36 AND RBL 36 IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20050720001022005072000102NM 2005 7 20 05FDEA01983 120050718A5311 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 RT MAIN DECK AFT FUSELAGE FRAME AT STA 1641, BETWEEN LONGERONS L12 AND L13 FOUND WITH DENT. REPAIRED PER SRM 53-30-00 VOLUME I FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2L73 4F RTA22WE 20050720001182005072000118NM 2005 7 20 P9RA20050094 120050716A2910211C223519 PRESSURE SWITCH BOEING757 757231 1384950NM HYD SYSTEM INTERMITTENT A P9RAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO11708TW 28480 AT BEGINNING OF TAKE OFF ROLL, CENTER HYDRAULIC SYSTEM PRESSURE LOW MESSAGE APPEARED ON EICAS. RETURNED TO GATE. ASSIGNED MEL 29-31-2-01. REMOVED AND REPLACED CENTER HYDRAULIC SYSTEM PRESSURE SWITCH IAW THE M/M. GROUND CHECKED GOOD AND CLEARED MEL. 2L72 4F RTA2NM 20050720001322005072000132NM 2005 7 20 05FDEA01932 120050713A5320 FLOOR SUPPORT DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 CABIN, AT STA 1908 ALONG LBL 60 TO LBL 86.5 FLOOR SUPPORT STRUCTURE FOUND CORRODED. SUPPORT REMOVED AND REPLACED. 2L73 4F RTA22WE 20050720001342005072000134NM 2005 7 20 05FDEA01934 120050713A5315 FLOORBEAM DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 CABIN, AT STA 1887 ALONG RBL 60 TO RBL 88 FLOORBEAM STRUCTURE FOUND CORRODED. 2L73 4F RTA22WE 20050720001542005072000154NM 2005 7 20 05FDEA01968 120050717A5347606549124 SEAT TRACK BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25280FE 22347 SEAT TRACK LBL 45 STA 480-690 IS CORRODED. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2 2L73 4F RTA3WE 20050720001772005072000177GL 2005 7 20 KBM2005F00123 220050612A73146899253 PUMP BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL FUEL SYSTEM LEAKING E KBMAO OTHER K FLUID LOSS NRNOT REPORTED 1 WP19188TV3663 2704 FUEL PUMP, UNIT LEAKING AT VENT SEAL. REMOVED AND REPLACED. (K) 1G71 3U3 U H2SW E4CE 20050720001792005072000179EU 2005 7 20 KBM2005F00146 120050712A243216061 BATTERY SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE DISCHARGED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH352 2884 BATTERY, LOW VOLTAGE. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050720001812005072000181EU 2005 7 20 KBM2005F00118 120050623A2150050143 MOTOR SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE BLOWER WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P1109 2347 5 INCH BLOWER MOTOR, COMMUTATOR WORN. REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20050720001832005072000183EU 2005 7 20 KBM2005F00145 120050712A2110SD507 COMPRESSOR SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE AIR CON DAMAGED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH 2884 COMPRESSOR, AC BLOWS WARM AIR. REMOVED AND REPLACED ALSO WITH NEW COIL PN 050034 AND PULLEY (PN 3003552). (K) 1G71 3U3 U H9EU E19EU 20050720001932005072000193EU 2005 7 20 AWXA200500810 120050713A2730 COMPUTER AIRBUS320 A320232 3930326EU NR 1 ELAC MALFUNCTIONED A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28655AW 1075 ABORTED TAKEOFF. DURING TAKEOFF RECEIVED ELAC 1 FAULT. ABORTED TAKEOFF AT 30 KNOTS AND RESET ELAC 1 PUSH BUTTON PER MAINTENANCE CONTROL. AIRCRAFT CONTINUED WITHOUT FURTHER INCIDENT. 2L72 4F RTA28NM 20050720001952005072000195 2005 7 20 P5CA0501374 420050619A221037600521 YAW DAMPER BOEING747 747249F 1384849NM RUDDER MALFUNCTIONED A P5CAO OTHER I FLT. ATTITUDE INST. ININSP/MAINT 1 EA15920FT 22237 RUDDER WOULD NOT DEFLECT. REPLACED UPPER AND LOWER YAW DAMPER COMPUTERS PER AMM 22-16-02. 2L74 4F A20WE 20050720001992005072000199NM 2005 7 20 UPS05444887 120050707A5320 WEB BOEING747 747123F NM A/C BAY CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 FX AIR CONDITIONING BAY REAR FIXED FAIRING INTERIOR ANGLE FOUND CORROSION AT STA 1241 LBL 50 O/B GROUND AIR SUPPLY VALVE AREA. CORROSION BLEND OUT 0.090 BY 0.75 BY 2.5 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS, WEB AND INTERIOR ANGLE REPAIRED AS PER SRM 51-40-02 FIG 1 AND 51-40-04 FIG 1. 2L74 4F A20WE 20050720002112005072000211 2005 7 20 YENA200539 420050706A2330 ODOR AIRBUS320 A320232 3930326EU CABIN DETECTED A YENAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15517JB 1327 F/A NOTICED ODOR OF BURNT WIRES STARTING AT ROW 12ABC AND STRONGEST AT ROW 14ABC. LIVE TV AND CABIN FANS TURNED OFF AND PUT AC FLOW TO HIGH AND ODOR DISSIPATED. A/C WAS DIVERTED. GROUND INSPECTION OF SUSPECT AREA REVEALED NO DEFECTS. SEVERAL SEB'S, DPCU'S AND CABLES FROM SUSPECT AREA REMOVED AS A PRECAUTION AND EXAMINED IN SHOP WITH FAA PRESENT. REVEALED NO DEFECTS. 2L72 4F RTA28NM 20050720002152005072000215NM 2005 7 20 ASMF200507013 120050717A5610 WINDOW BOEING757 7572Q8 1384972NM COCKPIT OPEN W ASMFC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SW23806AM 26273 AIRCRAFT REJECTED TAKEOFF AT 90 KTS AS A CONSEQUENCE OF LT WINDSHIELD OPENED WITHOUT APPARENT REASON. WINDSHIELD ADJUSTMENT CHECKED IAW MM56-11-01, TESTED CORRECT. REJECTED TAKEOFF INSPECTION WAS PERFORMED IAW MM 05-51-14, ALL CORRECT. 2L72 4F RTA2NM 20050721000042005072100004 2005 7 21 KBM2005F00155 420050702A34215040017901 GYRO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE ATTITUDE INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19751H 5 3403 ATTITUDE GYRO INOPERATIVE. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050721000072005072100007EU 2005 7 21 KBM2005F00154 120050629A6720350A33215001 BALL END SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE TAIL ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19966SH 3787 BEARING WORN ON T/R PITCH CHG DRIVE POST. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050721000092005072100009EU 2005 7 21 KBM2005F00150 120050702A7712305731365 INDICATOR SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE TORQUE STICKING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH 2884 TORQUE GAUGE STICKING, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050721000122005072100012EU 2005 7 21 KBM2005F00119 120050527A2435150SG122Q STARTER GEN SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE ENGINE SLOW E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P 2347 STARTER/GEN, AIRCRAFT STARTS SLOW. REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20050721000132005072100013EU 2005 7 21 KBM2005F00126 120050711A7931642790041 TRANSMITTER SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1B 6OO30NE OIL PRESSURE ERRATIC E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19250SH352 3874 OIL PRESSURE GAUGE NEEDLE FLUCTUATES-ERRATIC BETWEEN 4 AND 8 BAR, DURING FLIGHT. ALL OTHER GAUGES, OK. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050721000142005072100014EU 2005 7 21 KBM2005F00129 120050623A2400374GC014 ELECTRICAL BOX SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1B 6OO30NE FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19215LA 2143 GENERATOR LIGHT COMES ON IN FLIGHT. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050721000192005072100019SW 2005 7 21 KBM2005F00140 120050606A243210008921 BATTERY BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL FUSELAGE DISCHARGED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1973DP 64 2513 BATTERY DISCHARGED. REMOVED AND REPLACED. (K) 1G71 3U3 U H2SW E4CE 20050721000202005072100020NM 2005 7 21 DL764050335 120050624A3350 BATTERY BOEING767 767432ER 1385134NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27834MH 29707 FOUND AFT RT PAX EMERGENCY LIGHTS INOP ROW 42-48. REPLACED BATTERY PACK ROW 48, ALL CHECK OK. 2L72 4F RTA1NM 20050721000212005072100021NM 2005 7 21 DLM88050337 120050625A7830NAS1612906 O-RING DOUG MD88 MD88 3023688NM THRUST REVERSER WORN A DALAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SO27965DL 49984 ON SHORT FINAL AFT LAV SMOKE DETECTORS WENT OFF WITH ASSOCIATED ELEC SMELL AFTER LANDING WITHIN 5 MINS, LOST LT HYD FLUID WITH ASSOCIATED LOW QTY LIGHTS. FOUND O-RING FOR LT HYD T/REV DEACTIVATION VLV LEAKING. REPLACED O-RING LEAK CKS NORM. TURNED ON ALL CABIN LIGHTS AND COFFEE DISPENSERS NO ELEC, SMELL NOTED. ENGINE RUN AND DUCT BURNOUT IN PROGRESS. 2L72 4F RTA6WE 20050721000222005072100022NM 2005 7 21 DL78K050338 120050625A3350 BULB BOEING737 737832 13844CFNM EMERGENCY LIGHT BURNED OUT A DALAK NONE L NO TEST ININSP/MAINT 1 SO27398DA 30774 EMERGENCY EXIT LIGHT HAS BULBS AND LIGHT ASSY BROKEN AT SEAT 15E. RELAMPED EMERGENCY LIGHT. 2L72 4F RTA16WE 20050721000232005072100023NM 2005 7 21 DL76L050339 120050626A2120 SMOKE BOEING767 767332 1382001NM CABIN DETECTED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27196DN 28453 FLIGHT ATTENDANTS REPORT ELEC SMOKE IN MID CABIN AFTER T/O. RETURN TO ATL. RAN BOTH ENG AT TAKEOFF POWER FOR 10 MINS. RAN PACKS AT FULL HOT, HAD CABIN / GALLEYS POWERED OPS CK IFE SYSTEM. NO ELEC SMOKE ODOR FOUND ANYWHERE ON A/C. A/C OK FOR SERVICE. 2L72 4F RTA1NM 20050721000242005072100024NM 2005 7 21 DLM88050340 120050627A3260 PROXIMITY SWITCH DOUG MD88 MD88 3023688NM MLG FAILED A DALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27919DE 53422 AFTER RETRACTION OF LANDING GEAR RED UNSAFE LIGHT ON LEFT GEAR APPEARED. REPLACED UPLOCK PROX SWITCH. 2L72 4F RTA6WE 20050721000252005072100025NM 2005 7 21 DL75K050341 120050627A2120 ODOR BOEING757 757232 1384965NM CABIN DETECTED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO276715C 30486 SMOKE AND HAZE NOTED AT ROW 7 BOTH SIDES ELECTRICAL ODOR. SIDE WALL LIGHTS OFF OVERHEAD LIGHTS ON LOW. IFE TURNED OFF AND SMOKE REOCCURRED TWICE DURING DESCENT. NO EICAS MSG INBOUND. NO C/BS POPPED IN COCKPIT OR EE OR CARGO COMPTS. RAN ALL LIGHTS AND IFE AND GALLEY EQUIPMENT CHECKED. CEILING/PSU AREAS AND UNDER SEATS AND FLOOR GRILLS. ALL OPS /ODORS NORMAL. UNABLE TO DUPLICATE. ATL MA NOTIFIED. ALSO CHECKED FWD/AFT CARGO COMPT AND FWD EE COMPTS. RAN APU AIR ENTIRE GROUND TURN. 2L72 4F RTA2NM 20050721000312005072100031NM 2005 7 21 DL757050349 120050701A3244 TIRE BOEING757 757232 1384965NM NR 2 FAILED A DALAC ABORTED TAKEOFF D INFLIGHT SEPARATION TOTAKEOFF 1 SO27660DL 24422 NR 2 MAIN TIRE RECAP SEPARATED FROM TIRE. PUNCTURED SMALL LOWER WING PANEL MFG P/N 113N1622-9. ALSO DAMAGED NR 6 MAIN WHEEL HEAT SHIELDS. REPAIRED AND REPLACED AS NECESSARY. 2L72 4F RTA2NM 20050721000322005072100032 2005 7 21 DL75A050350 420050703A2565 RING BOEING757 757212 1384951NM ESCAPE SLIDE OUT OF POSITION A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27752AT 23128 RIGHT AFT ENTRY DOOR DIFFICULT TO CLOSE AND ARM DURING PREFLIGHT. RT AFT ENTRY LIGHT ILLUMINATED AFTER AIRBORNE. REPOSITIONED RT AFT ENTRY DOOR ESCAPE SLIDE SKIRT AND SURVIVAL PACK D-RING. DOOR OPN NORMAL. 2L72 4F RTA2NM 20050721000332005072100033NM 2005 7 21 DL757050351 120050701A5754MS190700653 WASHER BOEING757 757232 1384965NM NR 8 SLAT BROKEN A DALAO OTHER O OTHER DEDESCENT 1 SO27662DN 24991 LEADING EDGE SLAT DISAGREE MESSAGE ON INITIAL FLAP EXTENSION. FOUND RETAINING NUT LOOSE AND LOCK WASHER BROKEN ON NR 8 SLAT INBOARD ROTARY ACTUATOR. REPLACED WASHER AND RE-TORQUED NUT. 2L72 4F RTA2NM 20050721000342005072100034NE 2005 7 21 DLM88050352 220050707A7200JT8D219 ENGINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 MAKING METAL A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27926DL33972 49713 725812 RIGHT ENGINE OIL STRAINER CLOG MSG. REPLACED ENGINE FOR METAL IN STRAINER. 2L72 4F4 FRTA6WE E9NE 20050721000352005072100035NE 2005 7 21 DL76L050353 220050707A7200PW40603 ENGINE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 2 ODOR A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27178DN52940 724178 25143 724178 ON CLIMBOUT CABIN CREW REPORTED SMOKE DETECTORS SOUNDING. PERFORMED TASK 21-00-21-102-030 NOTHING ABNORMAL FOUND. INSPECT APU BLEED VALVE APU BLEED DUCT RT LT FLOW CONTROL VALVES INSPECTED CABIN INTERIOR NO ODOR. RAN BOTH ENGINES AT HIGH POWER SETTING 1.3 EPR DURING AN HOUR WITH BLEED ON OR OFF AND CABIN SELECTOR FROM COLD TO WARM UNABLE TO DUPLICATE ANYTHING ABNORMAL. MTC FERRY TO ATL. 2L72 4F4 FRTA1NM E24NE 20050721000362005072100036NM 2005 7 21 DL76L050354 120050707A3244UKN TIRE BOEING767 767332 1382001NM MLG FAILED A DALAA UNSCHED LANDING O OTHER CLCLIMB 1 SO27179DN 25144 ON CLIMBOUT HAD A LT GEAR SIDE BRACE MSG / MLG TIRE FAILED 6 TIRE TREAD THROWN REPLACED 6 MAIN WHEEL ASSY PER MM LT SIDE BRACE PROX SWITCH BRACKET FOUND TO HAVE BEEN MOVED BY TREAD DAMAGE REFITTED BRACKET ALL GEAR INDICATIONS NOW NORMAL. SIX TIRE PX WAS GOOD ON ARRIVAL. 2L72 4F RTA1NM 20050721000392005072100039NM 2005 7 21 DL777050358 120050709A253072077500 OVEN BOEING777 777232 1385232NM FWD GALLEY UNSERVICEABLE A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27861DA 29952 CREW REPORTED FWD GALLEY OVEN HAD ELEC SMELL AND SMOKE C/BS FOR OVEN PULLED BY FLT ATTENDANT SMELL STOPPED. FWD TO MCO AND PLACARD PER MEL M25-20-01H. AREA BEHIND THE OVEN INSPECTED FOR SHORTS/ELEC BURNS ALL OK. 2L72 4F RTT00001SE 20050721000402005072100040NM 2005 7 21 DL777050359 120050110A3350 SWITCH BOEING777 777232 1385232NM EMERGENCY LIGHT MALFUNCTIONED A DALAO OTHER O OTHER CRCRUISE 1 SO27866DA 29738 EMERGENCY LIGHT SWITCH AT 4RT INTERMITTANT CAUSING EMERGENCY LIGHTS TO FLICKER. REPLACED SWITCH. 2L72 4F RTT00001SE 20050721000422005072100042NM 2005 7 21 DL764050362 120050711A2780114T01151 CONTROL ROD BOEING767 767432ER 1385134NM NR 7 SLAT DAMAGED A DALAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO27831MH 29702 L/E SLAT ASYM MSG CAME ON AFTER T/O FLAPS SELECTED. FOUND A CONTROL ROD AT NR 7 SLAT DAMAGED. REPLACED SAME. 2L72 4F RTA1NM 20050721000442005072100044NM 2005 7 21 DL76L050366 120050713A2150211080107 ACM BOEING767 767332 1382001NM LEFT FAILED A DALAC ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SO27189DN 25990 STRONG FUMES IN CABIN AND COCKPIT ON TAKEOFF. REPLACED LEFT ACM. 2L72 4F RTA1NM 20050721000462005072100046 2005 7 21 QXEA200501121 420050717A34257003360941 COMPUTER DHAV DHC8 DHC8202 2809007NM AHRS INOPERATIVE A QXEAO OTHER O OTHER CRCRUISE 1 NM09369PH161887268 513 SEA - ON FLIGHT 2276, HSI HEADING MISMATCH MESSAGE DISPLAYED. C/W CHECKLIST, NO HELP. REMOVED AND REPLACED NR 2 AHRS COMPUTER. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050721000502005072100050NM 2005 7 21 DL76L050370 120050715A2750 FLAP SYSTEM BOEING767 767332 1382001NM TRAIL EDGE MALFUNCTIONED A DALAO OTHER F FLT CONT AFFECTED LDLANDING 1 SO27179DN 25144 CREW REPORTS T/E FLAP DISAGREE WITH FLAPS AT 15 EMERGENCY DECLARED INTO CDG. PERFORMED SEVERAL RETRACTION/EXTENSION WITH HYDRAULIC AND ELECTRIC POWER ALTERNATE. NO FAULT DUPLICATED. PERFORMED FSEU BITE TEST, TEST PASSED. 2L72 4F RTA1NM 20050721000522005072100052NE 2005 7 21 DL73S050372 220050517A7200 ENGINE BOEING737 737232 1384475NM PWA JT8 JT8D15 52051NE NR 1 BIRD INGESTION A DALAA UNSCHED LANDING C F.O.D. CLCLIMB 1 SO27321DL 23093 717129 SUSPECT BIRD INGESTION ON TAKEOFF FELT SMALL SHUDDER AND HEARD SOUND FOLLOWED BY FOUL ODOR. ENGINE PARAMETERS NORMAL. PERFORMED MTC INSPECTION PER MM 05-51-201-201. PS 3 FILTER NR 1 ENG CLEAN. RAN ENGINE TO T/O PWR ALL PARAMETERS NORMAL. NO ODORS IN A/C. A/C OK FOR SERVICE. 2L72 4F4 FRTA16WE E2EA 20050721000532005072100053NE 2005 7 21 DL757050373 220050717A7200 ENGINE BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 2 MAKING METAL A DALAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 SO27616DL15628 22823 728761 FL380 LEVEL FLT .79 MACH RT ENGINE CHUGGED AND RT OIL TEMP ROSE TO 166 THROTTLED BACK OIL TEMP RECOVERED EICAS MSG RT OIL FILTER APPROX 5 MINUTES LATER ENGINE CONTINUALLY CHUGGED SHUT IT DOWN. NO METAL FOUND IN TAILPIPE. ALL CHIP DETECTORS HAVE METAL STATUS MSG R ENGINE SEC SEL AND RT OIL FILTER. EPCS MSG DIS/EEC AND OIL P YELLOW. ENGINE EXCD NONE OIL QTY 20. ENGINE CHANGE IN PROGRESS. 2L72 4F4 FRTA2NM E17NE 20050719001092005071900109WP 2005 7 19 ASAA0580265 120050517A5322 SHEAR TIE DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - DURING C-CHECK, FOUND SHEAR TIE CORRODED AT STATION 1219 BETWEEN LONGERON 29 AND 30R. REMOVED AND REPLACED DAMAGED SHEAR TIE. (M) 2L72 4F RTA6WE 20050719001112005071900111NM 2005 7 19 ASAA0510158 120050613A57546546423273 SKIN BOEING737 737290C 138448VNM NR 3 SLAT DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 YXX - NR 3 SLAT DELAMINATED AT OUTBOARD END LOWER SURFACE SLAT STATION 124.27. PERMANENT REPAIR COMPLETED. (M) 2L72 4F A16WE 20050719001132005071900113WP 2005 7 19 ASAA0580298 120050604A575499194441 SKIN DOUG DC9 DC983 3022083WP NR 2 SLAT DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02961AS 53075 OKC - FOUND DURING HV-CHECK, LEFT NR 2 SLAT L/E DENTED. REPAIRED DAMAGED SECTION PER SRM 57-09. (M) 2L72 4F RTA6WE 20050719001162005071900116WP 2005 7 19 ASAA0580230 120050509A53219936582503 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - FOUND DURING C-CHECK, CABIN FLOORBOARD HAS UPPER FACE FIBER DAMAGE. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050719001192005071900119SO 2005 7 19 SIMA200517106 120050610A53131453388801 STRINGER EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FUSLAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21802AE 145471 DURING INSPECTION FOUND EXTERNAL STRINGER 19 RT HAS CHAFE DAMAGE BETWEEN FRAMES 52 AND 53. REPAIRED DAMAGE IAW SRM REINFORCEMENT REPAIR. AIRCARAFT WAS RETURNED TO SERVICE. (K) 2L72 4F4 FRTT00011ATTE6CH 20050719001212005071900121SO 2005 7 19 SIMA200517105 120050610A53131453388801 STRINGER EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL CABIN CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21802AE 145471 DURING INSPECTION, FOUND EXTERNAL STRINGER 19 LT HAS CHAFE DAMAGE BETWEEN FRAMES 52 AND 53. REPAIRED DAMAGE IAW SRM REINFORCEMENT REPAIR. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4F4 FRTT00011ATTE6CH 20050719001322005071900132EA 2005 7 19 SWIA200515252 120050629A2741 TRANSMITTER CNDAIRCL600 CL6002B19 1900309EA RUDDER POSITION MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07947SW 7786 LT RUDDER TRAVEL DOES NOT INDICATE FULL RANGE. REPLACED RUDDER POSITION TRANSMITTER IAW MM 27-24-05, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050719001352005071900135SO 2005 7 19 SWIA200515255 120050712A27523430001007 ACTUATOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07295SW 120322 LT OUTBOARD FLAP FAILED ON TAXI TO GATE. REPLACED LT OUTBOARD FLAP ACTUATOR IAW MM 27-50-00. OPERATIONAL CHECK SATISFACTORY. 2L72 4T RTA31SO 20050719001392005071900139EA 2005 7 19 SWIA200515259 120050705A27505913163 DETECTOR CNDAIRCL600 CL6002C10 1390015EA TE FLAPS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07701SK3673 3673 10133 FLAPS HALFSPEED STATUS MESSAGE ON TAXI OUT. REPLACED LT INBOARD FLAP SKEW DETECTOR AND RIGGED IAW MM 27-52-45. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050719001432005071900143SO 2005 7 19 SWIA200515263 120050707A2611 SMOKE EMB 120 EMB120ER 3260203SO LAVATORY DETECTED A SWIAO OTHER BJNSMOKE/FUMES/ODORS/SPARKS WARNING INDICATION FALSE WARNING CRCRUISE 1 NM07236SW 120312 LAV SMOKE DETECTOR WENT OFF IN FLIGHT, F/A NOTICED SMOKEY ODOR. INSPECTED LAVATORY AND GALLEY LIGHT ASSYS. NO DEFECTS NOTED. ALSO INSPECTED CARGO AREA. NO PROBLEMS FOUND. NO SMOKE ODOR FOUND PRESENT. 2L72 4T RTA31SO 20050719001812005071900181WP 2005 7 19 AALA20050427 120050707A3350 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHTSDISCHARGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21597AA 53287 AFT STAIRWAY EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN AFT STAIRWAY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050719001832005071900183NM 2005 7 19 AALA20050428 120050707A3040 SENSOR BOEING777 777223 1385213NM WINDSHIELD HEAT MALFUNCTIONED A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21757AN 32636 SMOKE IN COCKPIT DURING CRUISE. NOTED F/O WINDOW HEAT SENSOR SMOKING. TURNED OFF WINDOW HEAT. LANDED WITHOUT INCIDENT. FOUND F/O RT WINDOW HEAT J5 SENSOR TERMINAL END BURNT AND MELTED. ALSO, FOUND CRACK IN WINDOW. REPLACED RT NUMBER 1 WINDOW, WINDOW HEAT CONTROLLER, AND RT AND PRIMARY WIRE CONNECTOR LUG. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20050719001852005071900185NM 2005 7 19 AALA20050429 120050707A3350 CONNECTOR BOEING767 767323 1385205NM EMERGENCY LIGHTSNOT SEATED A AALAK NONE O OTHER ININSP/MAINT 1 SW21353AA 24034 EMERGENCY LIGHTS AT SEATS 31HJ INOPERATIVE. SECURED SEAT CONNECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050719001942005071900194SO 2005 7 19 C2XA05SH068 120050713A3260355022002MOD4 CONTROL UNIT EMB 145 EMB145ER 3260211SO LG MALFUNCTIONED A C2XAO OTHER J WARNING INDICATION CRCRUISE 1 SW2714940 145033 DURING CRUISE, FLIGHT CREW OBSERVED LANDING GEAR AIR/GROUND FAIL MESSAGE ON EICAS. FLIGHT CONTINUED TO DESTINATION AND MADE UNEVENTFUL LANDING. MAINTENANCE REMOVED AND REPLACED LANDING GEAR ELECTRONIC UNIT IAW EMB 145 AMM 32-32-01. OPERATIONAL CHECK GOOD. AIRCRAFT APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050719001952005071900195NM 2005 7 19 UPS05444883 120050618A532065B0174166 STRAP BOEING747 747123F NM FWD CARGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 FWD CARGO FRAME AT BS 960 STR 34L FOUND UPPER REINFORCEMENT STRAP CORRODED. CORROSION BLEND OUT 0.52 BY 0.5 BY 1.5 IN. EXCEED SRM 53-10-01 FIG 1 LIMITS. FWD CARGO BAY BS 960 FRAME ATTACH STRAP REPLACED AT BETWEEN STR 31L TO 39L AREA AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050719001992005071900199WP 2005 7 19 UPS05844892 120050625A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE C-1, RT WING UPPER L/E RIB CRACKED 0.5 IN LONG AT XFS 584. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR ANGLES IAW DC-8 SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20050719002012005071900201WP 2005 7 19 UPS05844894 120050625A53135750540502 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE C-1, LONG 11L CRACKED STA 670. REMOVED CRACKED LONGERON FITTING, FABRICATED, AND INSTALLED REPLACEMENT FITTING IAW DWG 5750540 AND DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20050719002032005071900203WP 2005 7 19 UPS05844896 120050626A5312 PRESSURE BLKHD DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE C-1, AFT PRESSURE BULKHEAD CRACKED 1.75 IN LONG AT RBL 26 AND 66 IN FROM FLOOR. CUT OUT DAMAGE SECTION, FABRICATED REPAIR DOUBLER, FINGER DOUBLER, AND FILLER AND INSTALLED IAW SRM 53-2-5 FIG 14A. 2L74 4F RT4A25 20050719002072005071900207WP 2005 7 19 UPS05844901 120050627A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE C-1, RT WING L/E UPPER RIB CRACKED AT XFS 671. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR ANGLE DOUBLER IAW DC-8 SRM 57-2-0 FIG 2 AND 57-3-3 FIG 7. 2L74 4F RT4A25 20050719002082005071900208 2005 7 19 SWAA052039 420050713A25651061323433 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF LIMITS A SWAAK NONE O OTHER ININSP/MAINT 1 SW29333SW 23697 DURING SCHEDULED A2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATING OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20050719002102005071900210NM 2005 7 19 SWAA052041 120050713A3350MS155721 BULB BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29333SW 23697 DURING SCHEDULED A2 CHECK, FOUND R1 DOOR LOWER EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050719002122005071900212 2005 7 19 SWAA052043 420050712A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29382SW 26588 DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050719002142005071900214NM 2005 7 19 SWAA052045 120050713A253041600019 COFFEEMAKER BOEING737 7377H4 1384404NM AFT GALLEY FAULTY A SWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW29445WN 29841 DIVERSION, SMOKE SMELL IN AFT GALLEY. FOUND AFT INBOARD COFFEEMAKER CIRCUIT BREAKER TRIPPED. RESET CIRCUIT BREAKER AND REMOVED AND REPLACED AFT COFFEEMAKERS PER MM. 2L72 4F RTA16WE 20050719002162005071900216NM 2005 7 19 SWAA052047 120050714A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050719002182005071900218NM 2005 7 19 SWAA052049 120050713A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29332SW 23696 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D + 10, STR 19R. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050719002202005071900220NM 2005 7 19 SWAA052051 120050714A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29613SW 27931 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 1064, STR 8R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050719002222005071900222 2005 7 19 SWAA052053 420050714A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29771SA 27879 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050719002332005071900233EU 2005 7 19 USAA050756 120050614A5310 BEAM AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19107US 1052 PIT - S2 - BEAM; 2 INCH CORROSION; NO LEVEL OR TASK; -30 INCHES AT FRAMES 64-65. REMOVED AND REPLACED BEAM. (K) 2L72 4F4 FRTA28NM E38NE 20050719002352005071900235EU 2005 7 19 USAA050760 120050614A5340D5347112420100 FITTING AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE FUSLEAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19107US18257 1052 PIT - S2 - FITTING, 5 INCHES X 2 INCHES AND 2 INCHES X 2 INCHES, CORROSION; LEVEL TASK JA-260-53500, BETWEEN FR 69 AND 70 AT Y48 ON SHEAR PLATE. REPLAED SHEARTIE LT SIDE. (K) 2L72 4F4 FRTA28NM E38NE 20050719002372005071900237EU 2005 7 19 USAA050758 120050614A5315D53472172204 FLOORBEAM AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19107US18257 1052 PIT - S2 - FLOORBEAMS, 1 INCH X 6 INCHES, CORROSION, FLOORBEAMS LT SIDE AT STA Y1292, FR C66. DEFECTIVE PART REPLACED WITH IDENTICAL PART IAW SRM AND EA. (K) 2L72 4F4 FRTA28NM E38NE 20050719002402005071900240EA 2005 7 19 ASOA05533 120050604A5310 BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 SO27909EV 7658 DURING A C-CHECK IN HOT, THE FS 621 RIGHT BEAM WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FS 621 RT BEAM IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20050719002412005071900241EA 2005 7 19 ASOA05532 120050604A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 SO27909EV 7658 DURING A C-CHECK IN HOT, THE FS 621 LEFT/RIGHT OBLIQUE ANGLE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FS 621 LT/RT OBLIQUE ANGLE IAW CRJ SRM 2L72 4F RTA21EA 20050719002492005071900249NM 2005 7 19 UPS05M44890 120050608A5347 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01255UP 48404 CABIN STA 1341 TO 1361 LBL 75 SEAT TRACK CROWN, BASE AND FLANGE FOUND CORROSION AS MARKED. SEAT TRACK REPAIR CARRIED OUT BETWEEN STA 1341 TO 1361 LBL 75 AS PER SRM 51-31-01 VOL II REV 37. 2L73 4F RTA22WE 20050719002882005071900288NM 2005 7 19 0501016717 120050708A2612 WIRE BOEING747 747251F 1384898NM FIRE DETECT SYS CHAFED A NWAAO OTHER JN WARNING INDICATION FALSE WARNING CRCRUISE 1 GL01617US 21121 DURING CRUISE, APU FIRE LIGHT ILLUMINATED WITH BELL. LIGHT AND BELL EXTINGUISHED WHEN FAULT TEST WAS ACCOMPLISHED. AIRCRAFT CONTINUED ON TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE PUT APU FIRE LOOP B ON MEL. MAINTENANCE FOUND CHAFED WIRE AND REPAIRED. OPERATIONAL CHECKS OK. 2L74 4F A20WE 20050720000052005072000005SO 2005 7 20 GUU2005F00027 120050609A3350AGC1 FUSE EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE EMERGENCY LIGHT FAILED A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO29280AS 120231 EMERGENCY FLOOR LIGHTING IN FRONT OF THE GALLEY, INOPERATIVE. REMOVED AND REPLACED EMERGENCY FLOOR LIGHT FUSE. (K) 2L72 4T4 TRTA31SO E20NE 20050720000102005072000010EU 2005 7 20 USAA050764 120050605A53151160851 FLOORBEAM AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19107US18257 1052 PIT - S2 - FLOOR SUPPORT ANGLE, 1 INCH X 1 INCH X .040 INCH DEEP, CORROSION; LEVEL 1; TASK JA-220-53500-004, FRAME 16, +Y65. DEFECTIVE PART REPLACED WITH IDENTICAL. (K) 2L72 4F4 FRTA28NM E38NE 20050720000122005072000012NM 2005 7 20 USAA050808 120050629A5320 ANGLE BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU52779 23861 CLT - Q2 - HORIZONTAL ANGLE, 1 INCH CRACK, STA 695 LT OF BL0. REMOVED FABRICATED AND INSTALLED NEW L ANGLE IAW DWG. (K) 2L72 4F4 FRTA16WE E21EU 20050720000162005072000016NM 2005 7 20 USAA050811 120050629A5740 BRACKET BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU WING WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU52779 23861 CLT - Q2 - ANGLE BRACKET, 2 INCHES X 3 INCHES, WORN AND CHAFED AREA, LWR WING PANEL OB OF NR 2 FLAP TRACK. FABRICATED AND INSTALLED NEW ANGLE IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050720000192005072000019NM 2005 7 20 USAA050813 120050629A533065458001128 SKIN BOEING737 737401 1384701NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE DENTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19425US42809 23992 CLT - Q - SKIN, 2 INCH X 3 INCH DENT, BS328 AND S23R. REPAIR DOUBLER IAW SRM. 2L72 4F4 FRTA16WE E21EU 20050720000292005072000029NE 2005 7 20 SF20050717 220050717A7200 ENGINE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE NR 1 SHUTDOWN A UHLAEC ENGINE SHUTDOWN ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 GL1743SZ 340A043 FLT 7574 FROM BGM TO IAD, 7-17-2005. ON CLIMBOUT, AIRCRAFT HAD AN UNCOMMANDED REDUCTION IN NR 1 PROP'S RPM. AIRCREW FOLLOWED QRH AND PUT INTO TORQUE MOTOR LOCKOUT. THE REDUCTION CONTINUED. AIRCREW CONTINUED TO FOLLOW QRH AND SHUT THE ENGINE DOWN AND RETURNED TO FIELD. 2L72 4T4 TRTA52EU E8NE6 20050720000352005072000035NM 2005 7 20 DHL2005750003 120050719A7931SRL04L INDICATOR BOEING727 7272M7 138407SNM OIL PRESS MALFUNCTIONED A DHLAED ENGINE SHUTDOWN RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01750DH 21951 PRIOR TO REACHING RUNWAY NR 3 OIL PRESS. WAS 25 PSI.REFERED TO ABNORMAL PROCEDURE AND SHUT DOWN ENGINE. R & R NR 3 OIL PRESSURE INDICATOR OPS CHECK GOOD WITH ENGINE RUN IAW ASTAR JRH 5.2 & MM CH 79-32-0. 2L73 4F A3WE 20050720000462005072000046NM 2005 7 20 SWAA052093 120050717A5344BAC1507 HINGE FITTING BOEING737 7373H4 1384600NM R1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29344SW 24152 R1 DOOR UPPER HINGE BOX HOUSING CRACKED. REMOVED AND REPLACED UPPER HINGE BOX PER SRM. 2L72 4F RTA16WE 20050720000532005072000053NM 2005 7 20 SWAA052102 120050718A56105893543129 WINDOW BOEING737 7377H4 1384404NM COCKPIT ARCED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29724SW 27856 L1 COCKPIT WINDOW ARCED & CRACKED. REMOVED AND REPLACED L1 COCKPIT WINDOW PER MM. 2L72 4F RTA16WE 20050720000592005072000059NM 2005 7 20 SWAA052089 120050718A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C + 3, STR 15L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050720000602005072000060NM 2005 7 20 SWAA052090 120050718A53306545775 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 780, STR 18L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050720000612005072000061NM 2005 7 20 SWAA052091 120050718A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 383, STR 15R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050720000622005072000062NM 2005 7 20 SWAA052092 120050717A53306545777 SKIN BOEING737 7373K2 13844BANM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29340LV 23738 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050720000632005072000063NM 2005 7 20 UPS05244732 120050612A5342 FITTING BOEING727 72731C 1384011NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 CLEAT CRACKED O/B OF S26R AT BS 600 LWR SECTION OF CLEAT ADJACENT TO S 26. REMOVED DAMAGED CLEAT IAW SRM 51-30-2. FABRICATED CLEAT IAW SRM 51-20-1. INSTALLED CLEAT IAW SRM 51-30-2. 2L73 4F A3WE 20050720000692005072000069 2005 7 20 KBM2005F00117 420050624A2312064105430 RADIO SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE VHF SYS WEAK A KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P 2347 VHF RADIO, UNIT WEAK AND SCRATCHY. REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20050720000752005072000075EA 2005 7 20 ASOA05530 120050604A5210601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27846AS 7328 DURING A HANGAR VISIT IN BTR, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. (M) 2L72 4F RTA21EA 20050720000822005072000082EU 2005 7 20 ASOA05526 120050616A33507012210 LAMP AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT LOOSE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27632AS 338 FLT 4733 - DURING A GROUND INSPECTION IN PFN, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE RESEATED THE LAMP IN THE EMERGENCY LIGHT ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20050720000922005072000092EA 2005 7 20 ASOA05518 120050614A5320 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27908EV 7654 DURING A C-CHECK IN MCN, THE FS 280 AFT OUTBOARD BRACKET AT LBL 9 AND THE AFT INBOARD BRACKET AT RBL 9 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FS 280 AFT OUTBOARD BRACKET AT LBL 9 AND THE AFT INBOARD BRACKET AT RBL 9. (M) 2L72 4F RTA21EA 20050720000942005072000094CE 2005 7 20 71813 120050717A3240 BRAKE ASSY BEECH 1900 1900D 1154162CE MLG MALFUNCTIONED A AMWAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE07163YV UE163 UPON TAXI INTO DUJ, CREW EXPERIENCED RIGHT BRAKE SPONGY. PARKED AND CHOCKED AIRCRAFT WITH NO FURTHER INCIDENT. MAINTENANCE BLED BRAKES. THEREFORE THERE WERE NO PARTS USED. 2L72 4T RTA24CE 20050720000952005072000095NM 2005 7 20 2005UALA00599 120050625A5210BPAS101 POWER UNIT BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE DOOR 4R MALFUNCTIONED A UALAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP29786UA2241 26938 4R EPAS BATTERY INDICATOR LIGHTS INTERMITTENT WHILE TAXIING. POSSIBLE SWITCH FAILURE. TEST LIGHT CHECKED DURING OPERATIONAL TESTING OF EPAS FOR BATTERY CHARGE AT CHECK INTERVALS PER EC 20-5211-000AA-A. UNIT CYCLED TO SHOP FOR BATTERY REPLACEMENT AT INTERVALS NOT EXCEEDING 19 MONTHS PER EC 20-5220-000LA-A. TROUBLESHOOTING AT SHOP WILL DETERMINE FAULT SOURCE. 2L72 4F4 FRTT0001SE E46NE 20050912002052005091200205NM 2005 9 12 SWAA052673 120050904A29106544548 LINE BOEING737 7373H4 1384600NM MLG WW CHAFED A SWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW29332SW 23696 AIR TURNBACK/DECLARED EMERGENCY, LOST A-SYSTEM HYDRAULICS. REMOVED AND REPLACED A-SYSTEM HYDRAULIC SUPPLY LINE PER MM. 2L72 4F RTA16WE 20050720001002005072000100NM 2005 7 20 05FDEA01981 120050717A5330 SKIN DOUG MD11 MD11 3023602NM ZONE 700 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 LT MLG - DURING CARRYING OUT WHEEL WELL DOOR HINGE REPAIR, FOUND NEW CRACK AT INTERNAL SKIN UPPER FORWARD AREA ADJACENT TO CENTER HINGE. STOP DRILL REPAIR CARRIED OUT AT LEFT HAND MAIN GEAR DOOR FORWARD AREA AS PER SRM 52-10-00 FIGURE 13 VOLUME I. REPAIR DOUBLER FABRICATED AS PER SRM 52-10-00 FIGURE 13 VOLUME I. PROTECTIVE TREATMENT CARRIED OUT AS PER SRM 51-21-01 VOLUME II. REPAIR DOUBLER PAINTED AS PER SRM 51-21-01 VOLUME II. THIS REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100. CLOSED 2L73 4F RTA22WE 20050720001112005072000111NM 2005 7 20 05FDEA01953 120050714A5730 SKIN DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 LEFTWING, FORWARD FIXED LEADING EDGE INNER SKIN FOUND CRACKED, ADJACENT TO NR 5 SLAT STA 590 TO STA 600. FABRICATED REPAIR DOUBLER AS PER SRM 57-10-00 FIG. 25 VOL.I AND INSTALLED REPAIR DOUBLER AT LH WING FORWARD FIXED LEADING EDGE INNER SKIN ADJACENT TO NR 5 SLAT AT STA 590 TO STA 600 AS PER SRM 51-35-01 VOL. II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2- 100. 2L73 4F RTA22WE 20050720001152005072000115NM 2005 7 20 P5CA0501375 120050711A282065B9301425 LINE BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE FUEL SYSTEM LEAKING A P5CAK NONE K FLUID LOSS ININSP/MAINT 1 EA15858FT 20109 662599 NR 2 ENGINE FUEL LEAK. REPLACED NR 2 ENGINE FUEL LINE (DRY BAY AREA). LEAK CHECK OK PER MM 28-22-00. 2L74 4F4 F A20WE E20EA 20050720001232005072000123NM 2005 7 20 05FDEA01979 120050717A5340 SUPPORT BRACKET DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 CABIN AT STA 2007 LBL 59 SUPPORT BRACKET ATTACHED TO BULKHEAD FOUND CORRODED. DISPREPANT SUPPORT BRACKET REMOVED. NEW SUPPORT BRACKET REWORKED FROM S2272071X7075T6511 AS PER DRAWING NJC6040. NEW SUPPORT PAINTED, PART MARKED AND INSTALLED AS PER SRM 51-22-01 VOL II. CLASSIFIED MINOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050720001242005072000124NM 2005 7 20 05FDEA01957 120050714A5730 SKIN DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 LEFT WING, FORWARD FIXED LEADING EDGE INNER SKIN FOUND CRACKED, ADJACENT TO REFUELING PANEL AT STA 530. FABRICATED REPAIR DOUBLER AS PER SRM 57-10-00 FIG. 25 VOL.I AND INSTALLED REPAIR DOUBLER AT LT WING FORWARD FIXED LEADING EDGE INNER SKIN, ADJACENT TO REFUELING PANEL AT STA 530 AS PER SRM 51-35-01 VOL.II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2- 100. 2L73 4F RTA22WE 20050720001292005072000129NE 2005 7 20 ANCF200400053 220050715A7261 ENGINE DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE RIGHT LEAKING W ANCFE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 SO23190AN 53190 P725722D RIGHT ENGINE OIL QUANTITY DECREASED SLOWLY FROM 13 QTS TO 2 QTS IN FLT ( OIL PRESS AND TEMPERATURE WERE NORMAL), ENGINE SHUTDOWN 4 MIN BEFORE LANDING AS OIL REACHED 2 QTS & OIL TEMP STARTED TO INCREASED. ENGINE INITIALLY OPERATED IN IDLE THRUST FOR ABOUT 15 MINUTES. AS PER AMM 78-36-01. OIL SENSE LINE OIL PRESS DIFFERENTIAL SWITCH TO PORT LP5 IN RT ENGINE R & R. AS PER AMM 79-20-05 & 79-20-05. MAGNETIC CHIP DETECTORS WERE CHECKED & REPLACED OIL FILTER, FOUND NO METAL PARTICLES, AS PER AMM 72-00-00. GROUND RUN UP PERFORMED AS PER AMM 72-00-00. ENGINE PARAMETERS WERE EPR 1,05, N1 29, EGT 390, N2 57 OIL PRESS 47 OIL TEMPERATURE 72. 2L72 4F4 FRT E9NE 20050720001382005072000138NM 2005 7 20 05FDEA01938 120050713A5744 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 RT WING, O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT O/B BORE, FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 PG 402-407. FABRICATED BUSHING AND INSTALLED AS PER EA 1-5750-87608. 2L73 4F RTA22WE 20050720001432005072000143NM 2005 7 20 05FDEA01941 120050713A5347ACA7399501 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 ELONGATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 MAIN DECK CARGO COMPARTMENT, FLOOR SEAT TRACK CROWN AT STA 645, X= -47 FOUND ELONGATED. 2L73 4F RTA22WE 20050720001502005072000150SO 2005 7 20 RAIA00507001 120050702A2432480CC01 CONTACTOR EMB 145 EMB145 3260210SO BATTERY FAILED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03804HK 145082 FLT 3523- PIT- BACKUP BATTERY OFF BUSS MESSAGE ON EICAS. MAINTENANCE REPLACED THE BACKUP BATTERY CONTACTOR. OPS CHECKED GOOD. 2L72 4F RTT00011AT 20050720001672005072000167NM 2005 7 20 DHL2005764004 120050715A5330 SKIN BOEING727 727264 138408MNM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01764AT 22984 FUSELAGE SKIN DENTED ABOVE L-2 DOOR AT STR. 5L. - EVALUATED DENT BE OUT OF LIMITS IAW 53-30-1 FIG.1. OPENED CABIN LINING ABOVE L2 DOOR FOR ACCESS IAW B727 SRM 51-30-2. REMOVED PREVIOUS REPAIR FOR INCORPORATION IAW B727 SRM 51-30-2 CUTOUT DAMAGE AREA DIM 1 X 1 AND 1.250 X 1 2 EA IAW B727 SRM 53-30-1 FIG.1. FABRICATED DOUBLER REPAIR IAW B727 SRM 53-30-2 FIG.2. ALODINE AND PRIMED IAW B727 SRM 51-10-2. INSTALLED DOUBLER IAW B727 SRM 53-30-2 CLOSED LINER PANELS IAW B727 SRM 51-30-2 2L73 4F A3WE 20050720001702005072000170NM 2005 7 20 20059 120050714A2611 SMOKE DETECTOR DHAV DHC8 DHC8103 1386005NM INOPERATIVE A KPVAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP13811WP 366 (PIREP) SMOKE WARNING LIGHT ILLUMINATED IN FLIGHT. (MX) INSPECTED AFFECTED SYSTEM AND DEFFERED IAW MEL 26-8-2 CAT C. BULKHEAD DETECTOR INOP, MAINT. PROCEDURES C/W. PLACARDS INSTALLED. (MX) CLEARED MEL 26-8-2. PREFORMED OPS CHECK GOOD IAW DHC -8 MM 26-12-00 PG. 201. NO DEFECTS FOUND, PLACARDS REMOVED. 2H72 4T RTA13NM 20050720001742005072000174NM 2005 7 20 AWXA200500809 120050706A5320654583523 INTERCOSTAL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 DURING C-16 CHECK, FOUND INTERCOSTAL CRACKED ON FORWARD SIDE OF BS 312 FLOORBEAM AT BL 0, WL 208. MAINTENANCE REMOVED INTERCOSTAL LOCATED AT BS 312, BL 0, WL 208 IAW BOEING 737-300 SRM 510-40-02-0 FIG 12. RECEIVED NEW INTERCOSTAL AND PREPPED FOR INSTALLATION IAW BOEING 737-300 SRM 51-40-05-0. INSTALLED INTERCOSTAL IAW BOEING 737-300 SRM 51-40-02-0. 2L72 4F RTA16WE 20050720001762005072000176 2005 7 20 KBM2005F00124 420050712A3422103002201 GYRO SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE DIRECTIONAL FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH 2337 DIRECTIONAL GYRO, DOES NOT HOLD COURSE. REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20050720001822005072000182 2005 7 20 KBM2005F00121 420050612A34225050010902 GYRO SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE DIRECTIONAL SPINNING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P89 2398 DIRECTIONAL GYRO, UNIT SPINNING CONTINUOUSLY. REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20050720001872005072000187 2005 7 20 KBM2005F00139 420050618A2312NPX138N050 RADIO SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1D NE VHF SYSTEM INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1953SH 2009 VHF FM, UNIT INOPERATIVE. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050720001902005072000190 2005 7 20 KBM2005F00142 420050711A34242060702745 INDICATOR SNIAS 350 AS350B2 8680813EU TURN AND BANK STUCK E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19751H 3403 TURN AND BANK, UNIT SLIP NEEDLE STUCK WILL NOT MOVE AT ALL. AIRCRAFT MEL UNTIL 7/20/05. (K) 1G71 3U H9EU 20050720001982005072000198 2005 7 20 KBM2005F00149 420050615A34215040017901 GYRO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE ATTITUDE MALFUNCTIONED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH855 2884 ATTITUDE GYRO, UNIT WILL NOT CAGE PROPERLY. MEL (K) 1G71 3U3 U H9EU E19EU 20050720002092005072000209NM 2005 7 20 QXEA200501104 120050711A7921 DOOR ACTUATOR BOMBDRDHC8 DHC8402 1390042NM PWC 150 PW150A EA ENGINE OIL FAILED A QXEAO OTHER M OVER TEMP CLCLIMB 1 NM09414QX 4061 NR 1 OIL TEMP AT 114 DEG C DURING CLIMB. REFERENCED EMERGENCY CHECKLIST (CLOSED #2 BYPASS DOOR) OIL TEMP REDUCED TO 109 DEGREE C AT LEVEL OFF (FL 230) OIL TEMP NORMAL AT 90 DEGREES C. INTERROGATED CDS FOUND EXCEEDANCE TO BE 114.5 DEGREE C FOR 836 SECONDS. DETERMINED TO BE AREA A AS PER S-11-00-992-802. COMPLIED WITH ENGINE INSPECTION AFTER SUSTAINED RUNNING AT TEMP OUTSIDE OF SPECIFIED LIMITS. IAW TASK 05-33-00-210-814. FOUND ACOC FLAP DOOR ACTUATOR FAILED OPS TEST. REPLACED ACOC DOOR IAW DHC-8-400 MM TASK 79-21-31-000-801 AND 79-21-31-000-8021. GROUND RAN AIRCRAFT AT HIGH POWER FOR 15 MINUTES. OPERATIONAL CHECK AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E00062EN 20050720002102005072000210NM 2005 7 20 QXEA200501102 120050711A2611 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM CARGO BAY FALSE INDICATIONA QXEAA UNSCHED LANDING JN WARNING INDICATION FALSE WARNING CLCLIMB 1 NM09363PH 520 ON CLIMB-OUT GOT INTERMITTENT SMOKE CAUTION LIGHT. RETURNED TO FIELD. UPON OPENING CARGO BAY DISCOVERED A RAMP RADIO/CELL PHONE HAD BEEN LEFT BY GROUND CREW IN ON POSITION. PERFORMED OPERATION CHECK OF BAGGAGE COMPARTMENT SMOKE DETECTION SYSTEM PER AMM TASK 26-15-00-710-801. OPERATION CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050721000022005072100002NE 2005 7 21 KBM2005F00153 220050610A72619560137520 MAGNETIC SEAL SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE ENGINE LEAKING A KBMAO OTHER K FLUID LOSS NRNOT REPORTED 1 WP19966SH305 3787 9910 ENGINE INPUT MAGNETIC SEAL IS LEAKING OIL. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050721000102005072100010EU 2005 7 21 KBM2005F00131 120050710A6730123668P BEARING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE ROD END EXCESS PLAY E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV 3296 ROD END BEARING. UNIT HAS EXCESSIVE PLAY. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050721000152005072100015EU 2005 7 21 KBM2005F00125 120050529A2435524031 STARTER GEN SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE ENGINE VIBRATION E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH1586 2337 STARTER/GEN, HIGH VIBRATION. REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20050721000292005072100029NM 2005 7 21 DL76G050347 120050630A2120 ODOR BOEING767 767332 1382001NM AFT GALLEY DETECTED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO271611B 30595 FLT ATTENDANTS REPORTED UNIDENTIFIED ELECTRICAL ODOR IN AFT GALLEY, CAPTS SIDE. NO SMOKE OR HEAT SOURSE NOTED. ODOR SEEMED TO LESSEN WITH LIGHT, OVENS, AND COFFEEMAKERS OFF. ODOR WAS STILL NOTICEABLE TO SOME OF THE FLT ATTENDANTS. RAN AND INSPECTED ALL AFT GALLEY EQUIPMENT FOR AN HOUR COULD NOT DUPLICATE ODOR. ALL COFFEEMAKERS, OVENS, CHILLER, LIGHTS OPS CHECK OK. A/C OK FOR SERVICE. 2L72 4F RTA1NM 20050721000412005072100041 2005 7 21 DL76L050360 420050711A3460341002292 DISPLAY BOEING767 767332 1382001NM COCKPIT INOPERATIVE A DALAA UNSCHED LANDING O OTHER CLCLIMB 1 SO27196DN 28453 F/O CDU DISPLAY BLANK. SELECTING ALT SOURCE DID NOT CORRECT THE PROBLEM. REPLACED F/O FMC CDU PER MM, GROUND TEST NORMAL. 2L72 4F RTA1NM 20050721000432005072100043NM 2005 7 21 DL75K050363 120050711A361053330AB6 COUPLING BOEING757 757232 1384965NM LT WING LEAKING A DALAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO27639DL 23993 L BLEED DUCT LK EICAS MSG AND OVERHEAD DUCT LEAK LIGHT ON LEFT SIDE ILLUMINATED AFTER T/O. FOUND BUSTED CLAMP ON DUCT LEADING TO LT WING A/I VALVE ON TOP OF LT PYLON. INSTALLED CLAMP AND SEAL ON WING A/I DUCT AND LEAK CHECKED PER M/M. LEAK CHECKS GOOD. AIRCRAFT DIVERTED TO ORLANDO. 2L72 4F RTA2NM 20050721000472005072100047NM 2005 7 21 QXEA200501124 120050719A3241 WARNING LIGHT BOMBDRDHC8 DHC8402 1390042NM ZONE 200 ILLUMINATED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09401QX 4031 GEG - ON FLIGHT 2367, RETURNED TO GATE. OUTBOARD ANTI SKID CAUTION LIGHT ILLUMINATED DURING TAXI, PLACED ON MEL. 2H72 4T RTA13NM 20050721000492005072100049NM 2005 7 21 DLM88050369 120050714A2910 LINE DOUG MD88 MD88 3023688NM HYD SYSTEM LEAKING A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO27948DL 49879 AFTER T/O AND T/O CHECKLIST STEP WHERE HYD AUX AND TRANS PUMPS OFF. ACFT LOST RT HYD SYSTEM PSI AND QTY, DID CHECKLISTS INCLUDING ALTERNATE GEAR EXT CONFIGURED AND LANDED NORMALLY. GEAR DOOR OPEN, LAND WEIGHT 134,000 SINK RATE AT LANDING APPROX 50 FT PER MIN. MX INSTALLED GEAR PINS AND RESTORED DOORS TOWED TO GATE. FOUND FLEX LINE TO SYS PRESS FILTER HOUSING LEAKING. REMOVED AND REPLACED FLEX LINE, RAN ENG. FLEX LINE, LEAK CHECKS GOOD. 2L72 4F RTA6WE 20050721000542005072100054NM 2005 7 21 DL76L050374 120050718A2530 COFFEEMAKER BOEING767 767332 1382001NM AFT GALLEY BURNED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27181DN 25986 ELECTRICAL ODOR WAS DETECTED INFLIGHT AROUND THE AFT GALLEY AREA ON THE COPILOTS SIDE OF THE AIRCRAFT. F/A'S PULLED CB'S FOR THE 2 COFFEEMAKERS ON THAT SIDE AND ODOR WENT AWAY CB'S LEFT OUT FOR REMAINDER OF THE FLIGHT. UPON ARRIVAL FOUND ALL CB'S IN/RESET. FOUND NO WATER AT BOTH COFFEEMAKERS ON RT SIDE AFT GALLEY, BLED AIR FROM LINES, BREWED SEVERAL POTS AND ALL CKS GOOD. INSPECTED COMPTS, CHILLER AND OVENS. 2L72 4F RTA1NM 20050721000552005072100055NM 2005 7 21 DL76L050375 120050718A3150285T025921 CIRCUIT CARD BOEING767 767332 1382001NM E/E BAY MALFUNCTIONED A DALAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO27174DN 24802 ON TAKEOFF POWERUP TO 1.20, GOT A TAKEOFF CONFIG WARNING AND FLAPS EICAS MESSAGE. RAN ENGINES UP AGAIN W/ FLAP 5 AND 15 SAME PROBLEM. REPLACED TAKEOFF CONFIG WARNING CARD, OPS OKAY. 2L72 4F RTA1NM 20050721000572005072100057NM 2005 7 21 DL76G050377 120050718A339760341427 WIRE HARNESS BOEING767 767332 1382001NM EXTERNAL LIGHT BURNED A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO2716065 30199 DURING MTC WALK AROUND FOUND CHAFED WIRES IN LEFT WHEEL WELL FWD BULKHEAD JUST INBOARD OF WHEEL WELL LT SW. REPLACED LOWER BEACON HARNESS, BEACON OPS OK. WHEN LEFT MLG DOOR WAS LOWERED DURING THE TURN AROUND INSPECTION THE TECH AT THAT TIME NOTICED ARCING FROM THE CABLE HARNESS. REPAIRED WIRING. 2L72 4F RTA1NM 20050721000592005072100059NM 2005 7 21 05FDEA01902 120050713A5753 SKIN DOUG MD11 MD11 3023602NM TE FLAPS DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 RT I/B FLAP UPPER SKIN BETWEEN XIFN 151.300 TO 159.300, FOUND WITH EXISTING DENTS, 3 PLACES, AS MARKED. DENT AREA TRIMMED AND REPAIR DOUBLER FABRICATED AND MATERIAL USED AS PER SRM 57-10-00 FIG 34 VOL I AND DRAWING ARC 2740. REPAIR DOUBLER INSTALLED AS PER SRM 51-35-01 VOL II. MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050721000642005072100064NM 2005 7 21 05FDEA01946 120050714A5320 WEB BOEING727 727233 138408ANM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 FIG 8 HOLE AT BS 640 STR 5R FRAME WEB. REPLACED FRAME PER SRM 51-30-2. 2L73 4F RTA3WE 20050721000652005072100065NM 2005 7 21 05FDEA01947 120050714A5311 FRAME BOEING727 727233 138408ANM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 3 FIGURE 8 HOLES AT BS 460 FRAME VERTICAL FLANGE STR 5R. REPLACED FRAME PER SRM 51-30-2. 2L73 4F RTA3WE 20050721000702005072100070NM 2005 7 21 UPS05444912 120050717A7714 INDICATION SYS BOEING747 747123F NM N2 MALFUNCTIONED A IPXAEJA ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING O OTHER CLCLIMB 1 SO01675UP 20390 NR 3 ENG N2 REACH 112 PERCENT DURING DEPARTURE. THRUST REVERSE LEVERS IDLE AND N2 WAS 10 PERCENT OR HIGHER THAN OTHER ENGS. NR 3 ENG SHUTDOWN AND RETURNED TO FIELD. DUMPED FUEL AND DECLARED EMERGENCY. ATB, INTERCHANGED ENG NR 2 AND 3 N2 INDS. ENG GRND RUN UP PERFORMED BY FLT CREW. AT IDLE PWR ENG NR 2 N2 IND WAS READING APPROX 1.5 PERCENT HIGHER THAN ENG NR 3 WITH AN INCREASE OF RPM. ENG NR 2 INDICATION DIFFERENCE BECAME GREATER 10 PERCENT TLA DIFFERENCE BECAME GREATER. 10 PERCENT TLA DIFFERENCE APPROX 4 PERCENT BOTH N1 MATCHED INDICATION ENG NR 2 HIGHER ENG NR 3 N2 INDS RETURNED TO POS M306224. 2L74 4F A20WE 20050721000712005072100071NM 2005 7 21 UPS05544914 120050715A2510111711905 STRAP BOEING757 75724APF 1384969NM SEAT HARNESS FRAYED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01467UP 25483 BOTH F/O SEAT HARNESS/INERTIAL REEL STRAPS WORN AND FRAYED. REMOVED AND REPLACED F/O SEAT HARNESS INERTIAL REEL IAW M/M 24-11-04. PERFORMED OPERATION, OPS CK OK. 2L72 4F RTA2NM 20050721000742005072100074NM 2005 7 21 05FDEA01928 120050713A5340 STRINGER CLIP BOEING727 727233 138408ANM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 FUSELAGE UPPER LOBE, CRACKED STRINGER CLIP, BS 560, STR 7R. REPLACED CRACKED STRINGER CLIP PER SRM 51-30-. 2L73 4F RTA3WE 20050721000762005072100076CE 2005 7 21 DXTA200500841 120050715A335099131 BATTERY PACK CESSNA750 750 2076810CE EMERGENCY LIGHTSINTERMITTENT E DXTAK NONE O OTHER ININSP/MAINT 1 GL07936QS4165 7500036 EMERGENCY LIGHTING SYSTEM NOT WORKING PROPERLY. WITH SWITCH IN ARM, EXTERIOR LIGHTS ILLUMINATE AND BACK HALF OF CABIN LIGHTS ILLUMINATE. FOUND 5G SWITCH ACTIVATED. REPLACED AFT BATTERY PACK DUE TO SW BEING TO SENSITIVE. OPS OK IAW CE750 M/M 33-50-01. 2L72 4J RTT00007WI 20050721000772005072100077CE 2005 7 21 DXTA200500837 120050705A499038003041 OIL SYSTEM CESSNA650 650 2076802CE APU OVERSERVICED E DXTAO OTHER B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 GL07794QS4843 6507094 AFTER STARTING APU AND BLEED AIR ON, COULD NOT CONTROL COCKPIT HEAT AUTO OR MANUAL. BLUE SMOKE FILLED COCKPIT. DUCT TEMPERATURE WAS 210 AND RISING WHEN BLEED AIR WAS TURNED OFF. SMOKE THEN DISAPPEARED. INVESTIGATED AND FOUND APU OVER SERVICED WITH OIL. SERVICED APU OIL TO PROPER LEVEL IAW 650 M/M 12-10-66. REMOVED AND REPLACED COCKPIT AND CABIN WATER SEPARATOR COALESCERS DUE TO OIL CONTAMINATION IAW 650 M/M12-10-01. OPS CHECKS GOOD. 2L72 4F A9NM 20050721000782005072100078NM 2005 7 21 P5CA0501379 120050718A5743BACB30US1442 BOLT BOEING747 747123 1384873NM MLG SHEARED A P5CAK NONE O OTHER ININSP/MAINT 1 EA15858FT 20109 RIGHT WING LANDING GEAR SUPPORT BEAM GATE BEARING ATTACHMENT SUPPORT UPPER VERTICAL BOLT SHEARED AND MIGRATED. REF IPC 57-15-05-0 ITEM 290. SHEARED BOLT REMOVED AND NEW BOLT /WASHERS/ NUT INSTALLED AND TORQUED IAW SRM 51-30-04 FIG 1 SHT 2 TABLE AND MM 57-15-00 FIG 201. 2L74 4F A20WE 20050721000802005072100080NM 2005 7 21 WRLA2005138 120050720A2597 BUSS DOUG MD11 MD11 3023602NM PWA 4460 PW4460 NE GALLEY SPARKS A WRLAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11803DE 48474 SPARKS/FUMES AFT OF MID GALLEY PARTITION AT FLOOR CABIN BUSS. SPARKS CEASED 1 HOUR REMAINING IN FLIGHT. PULLED ALL BREAKERS TO POWER SEATS & LAPTOPS AND TRANSFERRED ITEM TO DMI M25JL1905-139 CAT 'D' PER MEL 25-22-1, ITEM DUE ON 11/16/05. 2L73 4F4 FRTA22WE E24NE 20050721000812005072100081CE 2005 7 21 DXTA200500844 120050717A3260327 BULB BEECH MU300 400A 1155402CE MLG INDICATOR BURNED OUT E DXTAO OTHER J WARNING INDICATION APAPPROACH 1 GL07115QS RK383 LOWERED GEAR HANDLE AND ONLY LEFT MAIN GEAR ILLUMINATED DOWN. RAN GEAR EXTENSION CHECKLIST AND STILL ONLY INDICATED LEFT MAIN DOWN. LANDING WAS UNEVENTFUL. REPLACED INDICATOR LIGHT BULBS WITH NEW AND PERFORMED LANDING GEAR RETRACTION TEST IAW HAWKER 400XP MM CHAPTERS 32-20 AND 32-00. 2H72 4F RTA16SW 20050721000822005072100082CE 2005 7 21 DXTA200500848 120050720A2130 WARNING LIGHT CESSNA500 560CESSNA 2076750CE EMERGENCY PRESS ILLUMINATED E DXTAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 GL07342QS 5600324 ON CLIMBOUT, EMERGENCY PRESS LIGHT CAME ON FOLLOWED BY AN AIR DUCT OVERHEAT LIGHT, AND THE ODOR OF SOMETHING BURNING. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20050721000842005072100084NM 2005 7 21 F3LA200500033 120050713A3150 WARNING LIGHT AIRBUSA319 A319111 3930336NM COCKPIT ILLUMINATED A F3LAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM03905FR 1583 ABORTED TAKEOFF. FLIGHT CREW REPORTED ECAM FAULTS ON TAKEOFF ROLL. AIR PACK 1 AND 2 FAULT, VENT AVIONICS SYS FAULT, VENT BLOWER FAULT, AND VENT EXTRACT FAULT. HOT BRAKES - HIGHEST TEMP WAS 470 DEG. PERFORMED BITE TEST ON VENT SYSTEM (AEVC) AFTER RESET AEVC C/B. SYSTEM BITE CHECK OKAY. NO FAULTS PRESENT. REF AMM 21-26-00-710-001. COMPLIED WITH F9 JOB CARD MP05510, INSPECTION AFTER BRAKE OVERHEAT, AND NO DEFECTS FOUND. 2L72 4F RTA28NM 20050721000862005072100086NM 2005 7 21 QXEA200501114 120050715A242011522184 GENERATOR BOMBDRDHC8 DHC8402 1390042NM ZONE 100 MALFUNCTIONED A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09414QX9036 9036 4061 BOI - ON FLIGHT 2302, RETURNED TO GATE, JUST AS POWER WAS BEING ADDED FOR TAKEOFF (10 PERCENT TORQUE), NR 1 AC GENERATOR LIGHT ILLUMINATED. RAN CHECKLIST. DID NOT RESET. REPLACED NR 1 AC GENERATOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050721000912005072100091NM 2005 7 21 QXEA200501118 120050718A33506104781 BATTERY DHAV DHC8 DHC8202 2809007NM ZONE 200 MALFUNCTIONED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH136 136 528 PSC - TWO RED EMERGENCY LIGHTS ON NR 2 FLOOR STRIP INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK PS6. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050721000922005072100092NM 2005 7 21 QXEA200501120 120050718A5210 ROLLER BOMBDRDHC8 DHC8402 1390042NM ZONE 200 LACK OF LUBE A QXEAK NONE W INADEQUATE Q C ININSP/MAINT 1 NM09415QX 4081 PDX - ON FLIGHT 2422, REAR PASSENGER DOOR DIFFICULT TO OPEN. LUBED DOOR ROLLERS. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050721000942005072100094WP 2005 7 21 0501069623 120050610A5330 SKIN DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01623NW 47591 DURING L-CHECK, FOUND CRACK IN FUSELAGE SKIN AT BS 69.5 LBL 18. REPAIRED PER EA 96-203594. 2L72 4F A6WE 20050721000952005072100095NM 2005 7 21 0501076740 120050702A5311 FRAME BOEING747 747251F 1384898NM FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01640US 23888 DURING L-CHECK FOUND CRACK IN FRAME AT BS 460 S14L. REPAIRED PER EA 67-165222. 2L74 4F A20WE 20050721000962005072100096NM 2005 7 21 0501086740 120050704A5311 FRAME BOEING747 747251F 1384898NM FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01640US 23888 DURING L-CHECK FOUND CRACK IN FRAME WEB AT BS 460 S12L. REPAIRED PER EA 67-165219. 2L74 4F A20WE 20050721000972005072100097CE 2005 7 21 71722 120050711A2750 SWITCH BEECH 1900 1900D 1154162CE TE FLAPS OUT OF RIG A AMWAC ABORTED TAKEOFF FJ FLT CONT AFFECTED WARNING INDICATION TOTAKEOFF 1 CE07155YV 155YV AFTER TAKEOFF, CREW WAS NOT ABLE TO RETRACT FLAPS TO ZERO. RETURNED TO FIELD AND LANDED SAFELY WITH NO FURTHER INCIDENT. THE CORRECTIVE ACTION WAS THE FLAP LIMIT CAM SWITCH S-4 WAS RIGGED. THEREFORE NO PARTS WERE USED. 2L72 4T RTA24CE 20050721000982005072100098CE 2005 7 21 20030865 120050718A61205038912147 SWITCH BEECH 1900 1900D 1154162CE HARTZLHCE4A HCE4A3I NE LOW PRESSURE DEFECTIVE A GLBAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION DEDESCENT 1 NM03254GL UE254 ON APPROACH RT ENGINE POWER WAS REDUCED AND FLT CREW REPORTED THE ENGINE AUTOFEATHERED. AIRCRAFT LANDED SAFELY. MAINTENANCE TROUBLESHOT TO RT LOW PRESSURE SWITCH, REPLACED OP/CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA24CE 5 CP10NE 20050721000992005072100099NM 2005 7 21 USAA050840 120050707A5320 ANGLE BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU 23861 CLT - FOUND TRANSITION ANGLE CORRODED, TRANSITION ANGLE IN AFT CARGO BETWEEN STATION 727C AND STATION 827. REMOVED DAMAGE, INSTALLED TRANSITION ANGLE IAW SRM 51-10-02. (M) 2L72 4F RTA16WE 20050721001002005072100100NM 2005 7 21 USAA050838 120050707A5320 STIFFENER BOEING737 7373B7 1384580NM FUSLEAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU 23861 CLT - FOUND STIFFENER CORRODED 2 INCHES, STATION 227.8, BL 0 ON VERTICAL STIFFENER. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR PARTS IAW EA 69945. (M) 2L72 4F RTA16WE 20050721001012005072100101CE 2005 7 21 DXTA200500820 120050707A3230 CONTROL CABLE CESSNA750 750 2076810CE RT MLG OUT OF ADJUST E DXTAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 GL07984QS 7500084 INFLIGHT, CLIMBING THROUGH 35,000 FT, 3 LOUD AUDIBLE THUMPS HEARD AND FELT EMITTNG FROM LT FORWARD NOSE COMPARTMENT. FOUND RT MAIN FREE FALL CABLE W/TENSION CAUSING RT MAIN GEAR HOOK TO BE UNSEATED IN EXTEND POSITION. READJUSTED RT MAIN GEAR FREEFALL TENSION TO RESLACK IAW THE 750MM 32-30-05 FREEFALL CHECK GOOD IAW 750 M/M 32-00-01. 2L72 4J RTT00007WI 20050721001032005072100103EA 2005 7 21 ASOA05541 120050606A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27838AS 7276 DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY FLOOR LIGHT STRIP WAS FOUND TO BE DAMAGED IN SEVERAL PLACES. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT STRIP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050721001042005072100104NM 2005 7 21 USAA050846 120050707A5522 SKIN BOEING737 7373B7 1384580NM ELEVATOR DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU52779 23861 CLT - FOUND ELEVATOR TOP SKIN CRACKED 3 INCHES TOP SURFACE. MAJOR, COMPOSITE REPAIR IAW EA 96681. (M) 2L72 4F RTA16WE 20050721001062005072100106CE 2005 7 21 DXTA200500839 120050713A3243991205017 MASTER CYLINDER CESSNA500 560CESSNA 2076750CE BRAKES MALFUNCTIONED E DXTAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07334QS1228 5600434 CAPT LT BRAKE INTERMITTENTLY MUSHY WHEN BRAKE APPLIED. BRAKE OPERATING NORMALLY FOR APPROX 2 SECONDS. AFTER THAT TIME, BRAKE PRESSURE DROP. REMOVED AND REPLACED PILOT LT BRAKE MASTER CYLINDER IAW CE 560 M/M CHAP 32-42-02. OPS CHECKED GOOD. 2L72 4F RTA22CE 20050721001092005072100109NM 2005 7 21 USAA050847 120050707A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19505AU54520 23380 CLT - FOUND SKIN CRACKED 3 INCHES, FUSELAGE AT STATION 727E AT STRINGER 25R. INSTALLED DOUBLER AND TRIPLER IAW SRM 53-00-01. (M) 2L72 4F RTA16WE 20050721001132005072100113EA 2005 7 21 ASOA05534 120050618A5210601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR SEPARATED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27883AS 7504 DURING A GROUND INSPECTION IN FLO, THE ACTUATOR ROD WAS FOUND TO BE SEPARATED FROM THE BOTTOM STEP ON THE PASSENGER DOOR. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR AND RECONNECTED THE ACTUATOR ROD TO THE BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050721001142005072100114EU 2005 7 21 USAA050789 120050609A5320D5311281820201 FLOOR SUPPORT AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19721UW 1095 PIT - FOUND FLOOR SUPPORT CORRODED .5 INCH BY .5 INCH AREA, CABIN FLOOR SUPPORT Y254 AT FRAME 16. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 53-11-14. (M) 2L72 4F RTA28NM 20050721001172005072100117 2005 7 21 ASOA05540 420050619A34183995100208 COMPUTER CNDAIRCL600 CL6002B19 1900309EA STALL WARNING MALFUNCTIONED A ASOAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DEDESCENT 1 SO27672BR 7594 FLT 4534 - DURING DESCENT INTO ATL FROM SNB, AT APPROXIMATELY 14,000 FEET A CAUTION STALL FAIL ILLUMINATED, EXTINGUISHED AND REAPPEARED. DURING COMPLIANCE WITH THE QRH, A STRONG ELECTRICAL SMELL/ODOR/SMOKE WAS NOTICED IN THE COCKPIT WHICH DISSIPATED AFTER APPROXIMATELY FIVE MINUTES. THE CREW IMMEDIATELY PUT ON THEIR OXYGEN MASKS AND DECLARED AN EMERGENCY. THE AIRCRAFT DIVERTED TO CHA AND LANDED SAFELY. EMERGENCY VEHICLES WERE DISPATCHED AS A PRECAUTION AND THE AIRCRAFT TAXIED TO THE GATE SAFELY. AN EMERGENCY EVACUATION OF THE AIRCRAFT WAS NOT PERFORMED. MAINTENANCE REMOVED AND REPLACED THE STALL PROTECTION UNIT (COMPUTER). OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050721001182005072100118EU 2005 7 21 ASOA05504 120050609A33507012210 LAMP AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT LOOSE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27633AS 344 FLT 4733 - DURING A GROUND INSPECTION IN PFN, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE RESEATED THE LAMP IN THE EMERGENCY LIGHT ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20050721001192005072100119CE 2005 7 21 DXTA200500842 120050714A3260 WARNING LIGHT CESSNA750 750 2076810CE LG FALSE INDICATIONE DXTAA UNSCHED LANDING JN WARNING INDICATION FALSE WARNING CLCLIMB 1 GL07997QS 7500208 DURING CLIMB-OUT, HAD NOSE DOWN LIGHT NO GEAR UNSAFE LIGHT. THEN WENT OUT. DIVERT TO LAX. POSITIONED AIRCRAFT INTO HANGAR AND JACKED. HOOKED UP HYDRAULIC MULE AND SWING GEAR SEVERAL TIMES. NO FAULTS NOTED. OPERATIONAL CHECK OF GEAR INDICATIONS SATISFACTORY. DOWNJACKED AIRCRAFT AND DISCONNECTED HYDRAULIC MULE. A SYSTEM HYDRAULIC RESERVOIR SERVICED TO FULL. ALL WORK IAW CH 32-30-00 OF THE CE750 MM. 2L72 4J RTT00007WI 20050721001212005072100121EA 2005 7 21 ASOA05505 120050609A33102LA00516320 LIGHT CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27841AS 7300 FLT 4537 - DURING CRUISE FROM SHV-ATL, THE CREW NOTICED A STRONG BURNING ODOR FROM THE CAPTAINS MAP LIGHT WHEN IT AS TURNED ON WITH THE LIGHT OPERATING INTERMITTENTLY. THE ODOR DISSIPATED WHEN THE LIGHT WAS TURNED OFF. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS MAP LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050721001232005072100123EA 2005 7 21 ASOA05539 120050619A52102R5206B MOTOR CNDAIRCL600 CL6002B19 1900309EA ACTUATOR INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27871AS 7537 FLT 4282 - DURING A GROUND INSPECTION IN ABE, THE PASSENGER DOOR WAS FOUND JAMMED CLOSED TAKING OVER FIFTEEN MINUTES TO OPEN. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR ACTUATOR MOTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050721001252005072100125EU 2005 7 21 USAA050795 120050623A5321D5367175302700 FLOORBOARD AIRBUS320 A320214 3930316EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19107US18257 1052 PIT - FOUND FLOORBOARD CRACKED AND DELAMINATED, FLOOR PANEL 262 HG FRAME 64-66/6 INCH FORWARD OF FRAME 66. DOUBLER REPAIR BONDED COMPOSITE PER SRM 53-02-00. (M) 2L72 4F RTA28NM 20050721001262005072100126NM 2005 7 21 USAA050793 120050623A5330 SKIN BOEING757 757225 1384959NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19606AU65095 22202 BFM - FOUND DOOR OUTER SKIN CRACKED .25 INCH, UNDER LOWER HINGE CUTOUT STATION 700-710 L2 DOOR. CUT OUT DAMAGE AREA, FABRICATED FILLER, DOUBLER AND SUPPORT ANGLE AND INSTALLED PER EA 96646. (M) 2L72 4F RTA2NM 20050721001272005072100127EA 2005 7 21 ASOA05508 120050611A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27830AS 7236 DURING A C-CHECK IN MCN, THE PASSENGER DOOR MIDDLE THRESHOLD ANGLE WAS FOUND TO BE CORRODED BEYOND LIMITS AND THE HOLES IN THE ANGLE WERE ELONGATED. MAINTENANCE IS REMOVING AND REPLACING THE PASSENGER DOOR MIDDLE THRESHOLD ANGLE. (M) 2L72 4F RTA21EA 20050721001282005072100128EU 2005 7 21 USAA050797 120050623A5315D5347209200000 FLOORBEAM AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19108UW18429 1061 PIT - FOUND FLOORBEAM CORRODED 2 INCHES BY 36 INCHES, Y765 PLUS FRAME 66-70. REPLACED FLOORBEAM PER SRM 51-72-11 TYPICAL 51-40-01. CORROSION LEVEL 1, TASK JA-260-53500. (M) 2L72 4F RTA28NM 20050721001312005072100131NM 2005 7 21 USAA050842 120050707A5320 INTERCOSTAL BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU52779 23861 CLT - FOUND INTERCOSTAL SUPPORT CRACKED 1.4 INCHES, FS 295 AT STRINGER S16L. FABRICATED AND INSTALLED NEW INTERCOSTAL IAW SRM 53-10-15M SRM 51-10-02. (M) 2L72 4F RTA16WE 20050721001332005072100133EA 2005 7 21 ASOA05502 120050608A3397 SPLICE CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT DISCONNECTED A ASOAK NONE O OTHER ININSP/MAINT 1 SO273350 10212 DURING A GROUND INSPECTION IN SLC, THE OVERWING EMERGENCY EXIT LIGHT AT THE TRAILING EDGE OF THE WING WAS FOUND TO BE INOPERATIVE. MAINTENANCE FOUND A LOOSE CONNECTOR ON THE INTERIOR PANEL SPLICE TO THE OVERWING EMERGENCY EXIT LIGHT AT THE TRAILING EDGE OF THE WING AND RECONNECTED THE SPLICE CONNECTORS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050721001352005072100135EA 2005 7 21 ASOA05538 120050619A521060R13189661 ROLLER CNDAIRCL600 CL6002B19 1900309EA PAX DOOR DIRTY A ASOAK NONE O OTHER ININSP/MAINT 1 SO27916EV 7757 DURING A GROUND INSPECTION IN ATL, THE FLIGHT ATTENDANT REPORTED THE PASSENGER DOOR DIFFICULT TO OPEN. MAINTENANCE CLEANED AND LUBRICATED THE PASSENGER DOOR HANDLE ROLLER AND TRACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050721001372005072100137EA 2005 7 21 ASOA05506 120050610A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27830AS 7236 DURING A C-CHECK IN MCN, THE FS 484 INTERCOSTAL AT RBL 36 OUTBOARD WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FS 484 INTERCOSTAL AT RBL 36 OUTBOARD IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20050721001392005072100139EA 2005 7 21 COMA0560384 120050707A5210 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR OUT OF ADJUST A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01999CA 7230 FLIGHT 5639 - DURING CLIMBOUT OF CVG RECEIVED A CABIN DOOR OUTER HANDLE WARNING. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. FLIGHT LANDED WITHOUT INCIDENT. FOUND CABIN DOOR NOT FLUSH WITH FUSELAGE, PERFORMED OPERATIONAL CHECK OF DOOR HANDLE, NO DISCREPANCIES NOTED. 2L72 4F RTA21EA 20050721001412005072100141EA 2005 7 21 COMA0560386 120050709A2910AE7120311 HOSE CNDAIRCL600 CL6002B19 1900309EA LT ENGINE LEAKING A COMAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO01988CA 7204 FLIGHT 5234 - NR 1 HYDRAULIC SYSTEM CAUTION. REPLACED LEAKING HYDRAULIC LINE. 2L72 4F RTA21EA 20050721001422005072100142EA 2005 7 21 COMA0560387 120050709A5270840534 PROXIMITY SWITCH CNDAIRCL600 CL6002B19 1900309EA CABIN DOOR UNRELIABLE A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01409CA 7441 FLIGHT 5611 - CABIN DOOR OUTER HANDLE CAUTION. REPLACED HANDLE PROXIMITY SENSOR. 2L72 4F RTA21EA 20050721001432005072100143EA 2005 7 21 COMA0560383 120050706A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE THRUST REVERSER ILLUMINATED A COMAE ENGINE SHUTDOWN J WARNING INDICATION DEDESCENT 1 SO01457CA 7612 873283 FLIGHT 5549 - EN ROUTE BOS-PWM DURING DESCENT RECEIVED A LEFT THRUST REVERSER UNLOCK MESSAGE. CREW DECLARED AN EMERGENCY AND SHUTDOWN THE LEFT ENGINE. AIRCRAFT LANDED WITHOUT INCIDENT. DEFERRED THE LEFT THRUST REVERSER PER MEL. 2L72 4F4 FRTA21EA E15NE 20050721001442005072100144SO 2005 7 21 RAIA00507004 120050708A21332097K011100 OUTFLOW VALVE EMB 145 EMB145 3260210SO CABIN PRESSURE INOPERATIVE A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03802HK16618 145066 FLT 3547 - PVD - NO CABIN PRESSURIZATION INDICATION ON CLIMB AFTER DEPARTURE. MAINTENANCE REMOVED AND REPLACED ELECTRO - PNEUMATIC VALVE AND OPS CHECK OK. 2L72 4F RTT00011AT 20050721001462005072100146SO 2005 7 21 RAIA00507006 120050711A3260 PROXIMITY SWITCH EMB 145 EMB145 3260210SO MLG OUT OF ADJUST A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03821HK 145068 FLT 5488 - STL - LANDING GEAR AIR/GND FAIL INDICATION. MAINTENANCE ADJUSTED LT MLG PROX SWITCH AND OPS CHECKED OK. 2L72 4F RTT00011AT 20050721001492005072100149SO 2005 7 21 RAIA00507010 120050714A3150 WARNING LIGHT EMB 145 EMB145LR 3260212SO ILLUMINATED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03829HK 145281 FLT 3542 - STL - STALL PROTECTION SYSTEM FLAP LOW STEER WARNING INDICATION. MAINTENANCE REMOVED AND REINSTALLED AURAL WARNING CONTROL BOW AND OPS CHECKED SYSTEM WITH NO DEFECTS NOTED. 2L72 4T RTT00011AT 20050721001502005072100150NM 2005 7 21 DXTA200500846 120050719A2750 FLAP SYSTEM GULSTM200 200 4500308NM MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07721QS 092 SLATS AND FLAPS INTERMITTANT AFTER TAKEOFF, SELECTED FLAPS, SLATS & KRUEGERS UP. FLAPS STAYED AT 20 DEGREES, SLATS STAYED DOWN AND KRUEGER'S RETRACTED. ALSO HAD THE FOLLOWING ICAS MSG SLAT/FLAP MAINTEN. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA53NM 20050720000272005072000027EU 2005 7 20 USAA050762 120050614A5340D5347112420100 FITTING AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19107US18257 1052 PIT - S2 - FITTING, 6 INCH X 2 INCH AND 2 INCH X 2 INCH, CORROSION; LEVEL 1; TASK JA-260-53500, BETWEEN FR 69 AND 70 AT -Y48 INCH ON SHEAR PLATE (TIE). REPLACED SHEAR TIE, RT SIDE IAW SRM. (K) 2L72 4F4 FRTA28NM E38NE 20050720000422005072000042WP 2005 7 20 0501041236 120050717A2830AV16B1926C CONTROLLER DOUG DC10 DC1030 3023501WP FILL VALVE MALFUNCTIONED A NWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL01236NW6266530827 46934 EN ROUTE FROM FCO TO DTW CREW NOTICED FUEL CONSUMPTION MUCH HIGHER THAN FLIGHT PLAN PREDICTION. APPROX 2000 LBS/HR. FLIGHT DIVERTED TO AMS AND LANDED WITHOUT INCIDENT. REPLACED FILL VALVE CONTROLLER AND FUEL DUMP VALVE. OPERATION CHECKS GOOD. 2L73 4F A22WE 20050720000442005072000044NE 2005 7 20 SF2005071505 220050715A7261 ENGINE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE NR 2 OIL CONSUMPTION A UHLAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL1743SZ 340A043 RIGHT ENGINE OIL PRESSURE LIGHT COMING ON FREQUENTLY IN FLIGHT, 30 PSI & SLIGHT FLUCTUATIONS STARTED COMING ON MORE FREQUENTLY. DECLARED EMERGENCY & MADE A PRECAUTIONARY LANDING IN PIT, WARNING WENT OFF 63 TIMES. FOUND NR 2 ENGINE OIL LEVEL LOW, SERVICED OIL IAW M/M 12-10-79, CREW GROUND RAN FULL POWER FOR 10 MINS, NO LEAKS NOTED. FOUND OIL CONSUMPTION TO BE OUT OF LIMITS, SERVICED NR 2 ENGINE OIL. FERRIED A/C 43SZ FROM PIT TO FWA WITH STOP IN CMH FOR OIL CHECK. 2L72 4T4 TRTA52EU E8NE6 20050720000542005072000054 2005 7 20 SWAA052103 420050718A256565659723 BRACKET BOEING737 7377H4 1384404NM R1 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29745SW 29491 R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR BRACKET LOOSE. SECURED BRACKET PER MM. 2L72 4F RTA16WE 20050720000772005072000077EA 2005 7 20 ASOA05528 120050616A5210601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR DEBONDED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27844AS 7317 FLT 4638 - DURING A GROUND INSPECTION IN CVG THE SIDE ATTACH ROD TO THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND DISCONNECTED. MAINTENANCE FOUND THE BOTTOM STEP INSERTS DISBONDED FROM THE SIDE ATTACH ROD AND REMOVED AND REPLACED THE BOTTOM STEP ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050720000862005072000086EU 2005 7 20 ASOA05527 120050616A33507012210 LAMP AEROSPATR72 ATR72 EU EMERGENCY LIGHT CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27631AS 362 DURING A GROUND INSPECTION IN PFN, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE CLEANED CORROSION OFF THE LAMP AND RESEATED IT IN THE EMERGENCY LIGHT ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20050720000912005072000091EA 2005 7 20 ASOA05522 120050614A2612 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA APU FIRE MALFUNCTIONED A ASOAO OTHER N FALSE WARNING DEDESCENT 1 SO27833AS 7246 FLT 4319 - DURING DESCENT INTO BQK FROM ATL, APPROXIMATELY ONE MINUTE AFTER STARTING THE AUXILIARY POWER UNIT AN APU FIRE FAIL AMBER CAUTION MESSAGE WAS RECEIVED. APPROX TWO SECONDS LATER THAT MESSAGE EXTINGUISHED AND THEN AN APU FIRE RED WARNING MESSAGE AND THE FIRE BELL WERE RECEIVED WHICH WENT OUT APPROXIMATELY ONE SECOND LATER, FOLLOWED BY THE APU AUTOMATICALLY SHUTTING DOWN. THE QRH WAS COMPLIED WITH AND THE AIRCRAFT LANDED SAFELY IN BQK. UPON INSPECTION MAINTENANCE FOUND NO INDICATIONS OF AN APU FIRE. MAINTENANCE DEFERRED THE APU UNDER MEL NR 49-10-01B, CAT C, EXPIRING 6/24/05. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050720001082005072000108SW 2005 7 20 ALGA104481 120050708A6230412040101129 MAST BELL 412 412EP 1182205SW MAIN ROTOR CORRODED B ALGAK NONE O OTHER ININSP/MAINT 1 SW03XATXV2294 36317 FIRST TIME DISASSEMBLY; EXCESSIVE CORROSION PITTING AT AND DEBONDING OF ADAPTER SLEEVE. / INSTALLED NEW MAST POLE BY O/H SHOP 1G72 4U H4SW 20050720001122005072000112NM 2005 7 20 05FDEA01944 120050714A5340 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 FUSELAGE UPPER LOBE, STRINGER CLIP IS CRACKED, BS 950E, STR 4L. REMOVED & REPLACED STR. CLIP PER SRM 51-30-02 2L73 4F RTA3WE 20050720001202005072000120NM 2005 7 20 05FDEA01975 120050717A5744 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 RT WING, O/B FLAP I/B HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. 2L73 4F RTA22WE 20050720001262005072000126NM 2005 7 20 05FDEA01959 120050714A5347ACA7399501 SEAT TRACK DOUG MD11 MD11 3023602NM FUSLEAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 MAIN DECK CARGO COMPARTMENT, FLOOR SEAT TRACK AT STA 635, X= 47 FOUND CRACKED APPROXIMATELY 3 INCHES LONG. REPAIRED AS PER SRM 53-70-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 2L73 4F RTA22WE 20050720001372005072000137NM 2005 7 20 05FDEA01937 120050713A5744 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 RT WING, O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 PG 402-407. FABRICATED BUSHING AND INSTALLED AS PER EA 1-5750-87609. 2L73 4F RTA22WE 20050720001392005072000139NM 2005 7 20 05FDEA01939 120050713A5744 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 RT WING , O/B FLAP O/B HINGE (WING SIDE), SIDE LINK ATTACHMENT BARREL NUT BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. FABRICATED BUSHING AND INSTALLED AS PER EA 1-5750-87608. 2L73 4F RTA22WE 20050720001402005072000140NM 2005 7 20 05FDEA01940 120050713A5744 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 RT WING, O/B FLAP O/B HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED IAW CMM 57-44-09 PG 402-407. 2L73 4F RTA22WE 20050720001462005072000146NM 2005 7 20 05FDEA01964 120050715A5311 FRAME BOEING727 727233 138408ANM FUSELAGE CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 FUSELAGE UPPER LOBE, FRAME IS CHAFED, BS 990, STR 9R. REPAIRED FRAME PER SRM 51-40-3. 2L73 4F RTA3WE 20050720001482005072000148SO 2005 7 20 RAIA00506035 120050629A3610 FILTER EMB 145 EMB145LR 3260212SO FAN AIR VALVE DIRTY A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03849HK 145002 FLT 7954- TYS- BLEED NR 2 OVERTEMP. MAINTENANCE CLEANED THE FAN AIR VALVE FILTER. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050720001492005072000149SO 2005 7 20 RAIA00506036 120050630A2844 WARNING LIGHT EMB 145 EMB145LR 3260212SO FUEL SYSTEM ILLUMINATED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03817HK 145058 FLT 5754- STL- E-1 LOW FUEL PRESSURE. MAINTENANCE DEFERRED ITEM PER MEL. 2L72 4T RTT00011AT 20050720001522005072000152SO 2005 7 20 RAIA00507003 120050703A801231253581 START VALVE EMB 145 EMB145LR 3260212SO NR 1 ENGINE FAILED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03810HK 145231 FLT 3535- PIT- NR 1 ENGINE WOULD NOT START. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE START CONTROL VALVE. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050720001582005072000158NM 2005 7 20 05FDEA01971 120050717A5347602351124 SEAT TRACK BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25280FE 22347 SEAT TRACK RBL 45 STA 740-757 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2 2L73 4F RTA3WE 20050720001602005072000160NM 2005 7 20 05FDEA01973 120050717A5744 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 RT WING-O/B FLAP I/B HINGE (WING SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 PG 602-607. FABRICATED BUSHING AND INSTALLED AS PER EA 1-5750-87610. (CLOSED) 2L73 4F RTA22WE 20050720001612005072000161NM 2005 7 20 05FDEA01974 120050717A5744 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 RT WING-O/B FLAP I/B HINGE (WING SIDE), LWR ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PG 602-607. REPAIR CARRIED OUT AS PER CMM 57-44-08. 2L73 4F RTA22WE 20050720001712005072000171GL 2005 7 20 CHQA200500126 220050712A7200AE3007A1P ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 1 UNSERVICEABLE A CHQAE ENGINE SHUTDOWN BX SMOKE/FUMES/ODORS/SPARKS ENGINE FLAMEOUT DEDESCENT 1 GL11280SK136451916 145381 CAE311281 AFTER STARTING DESCENT OUT OF 16,000 FT, HEAT-TYPE ODOR NOTED SHORTLY AFTER MAKING INITIAL POWER REDUCTION. ODOR SUBSIDED AND ATTRIBUTED TO OCCASIONAL PACK SMELL. SOP UNTIL AFTER PASSING APPROX 400 AGL. A/C CONFIGURED AND SET FOR NORMAL VMC ILS. NR 1 ENGINE ITT SURGED TO 1096 BEFORE LOSING INDICATIONS AND COMPRESSOR-STALL LIKE BANG FELT FOLLOWED BY N1 UNSPOOLING RAPIDLY. QUICK YAW AND SPEED DEGRADING QUICKLY. FLAPS SET TO 22 WITH 10 KNOT BUMP TO VREF. EMERGENCY DECLARED. FLT LANDED W/O INCIDENT. NO FIRE OR SMOKE IN CABIN. NO EVACUATION NEEDED. MX FOUND LARGE CHUNKS OF METAL IN INTAKE. R & R NR 1 ENGINE IAW J/C. OPS CHECK AND LEAK CHECK GOOD. 2L72 4T4 FRTT00011ATTE6CH 20050720001722005072000172 2005 7 20 KBM2005F00122 420050618A34215040017901 GYRO SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE ATTITUDE INTERMITTENT E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P9 2347 AG, UNIT FLAG POPS ON/OFF INTERMITTENTLY. REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20050720001802005072000180 2005 7 20 KBM2005F00137 420050609A3160704A47270102 GAUGE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE CLUSTER INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19351WM43 2167 CLUSTER GUAGE, OIL TEMP, OIL PRESSURE, AND FUEL PRESSURE PEGS OUT. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050720001972005072000197 2005 7 20 P5CA0501378 420050710A34604052508952 FMC BOEING747 74747UF 1384949NM COCKPIT FAILED A P5CAK NONE O OTHER CRCRUISE 1 EA15496MC 29257 CREW REPORTED RT FMC INOP. REPLACED RT FMC- MM 34-61-01. ALL OPS NORMAL. 2L74 4F RT1384945 20050720002072005072000207NE 2005 7 20 QXEA200501103 220050713A7200 WARNING LIGHT DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE ENGINES ILLUMINATED A QXEAD RETURN TO BLOCK JN WARNING INDICATION FALSE WARNING TXTAXI/GRND HDL 1 NM09374PH 528 PCE123077 NR 1 AND NR 2 ENGINE MANUAL CAUTION LIGHTS ILLUMINATED. MAINTENANCE RESET CIRCUIT BREAKER FOR BETA LOCKOUT. CAUTION WENT AWAY. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20050720002132005072000213WP 2005 7 20 NACA20050017 120050712A3230533693 LATCH DOUG DC6 DC6 3021702WP LT MLG DAMAGED A NACAO OTHER O OTHER CLCLIMB 1 AL032907F 533265 LT MAIN GEAR WILL NOT STAY UP WITH GEAR SELECTOR IN NEUTRAL. REPLACED LATCH MECHANISM LINK ASSEMBLY. OPS CHECKED GOOD. 2L74 4R A781 20050720002142005072000214 2005 7 20 ASMF200507012 420050716A3443HG1103BA01 IRU DOUG MD88 MD88 3023688NM NR 2 FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23161PL444116279 49764 AIRCRAFT ARRIVED TO PLATFORM WITH CAPTAIN REPORT INERTIAL NR 2 OUT OF SERVICE. INERTIAL AIRFLOW WAS CHECKED. FUNCTIONING CORRECTLY. OPERATIONAL TESTS WERE CORRECT IAW MM 34-43-00. AIRCRAFT DISPATCHED AND RETURNED TO PLATFORM AS A CONSEQUENCE OF SAME PROBLEM. INERTIAL WAS REMOVED, COOLED AND REINSTALLED, TESTED CORRECT. DURING TRANSIT CHECK INERTIAL NR 2 REPLACED IAW MM 34-43-01, TESTED CORRECT. 2L72 4F RTA6WE 20050721000112005072100011EU 2005 7 21 KBM2005F00152 120050711A21210500847 MOTOR SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE CONDENSOR FLUCTUATES E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19966SH469 3787 7 INCH CONDENSOR MOTOR, SPEED FLUCUATES, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050721000172005072100017EU 2005 7 21 KBM2005F00138 120050609A6410355A09103601 BEARING SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE HALF SHELL WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1937SH 940 2300 HALF SHELLS, WORN. REMOVED AND REPAIRED. (K) 1G71 3U3 UNCH9EU E19EU 20050721000182005072100018EU 2005 7 21 KBM2005F00133 120050703A6720350A33105803 BELLCRANK SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE TAIL ROTOR DEBONDED A KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19345SH965 3345 BUSHING UNBONDED FROM T/R BELLCRANK. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050721000262005072100026NM 2005 7 21 DLM90050342 120050627A240034B1353 CONTROL UNIT DOUG MD90 MD9030 3023690NM E/E BAY INOPERATIVE A DALAO OTHER H ELECT. POWER LOSS-50 PC CLCLIMB 1 SO27906DA 53386 MOMENTARY POWER INTERRUPTION INFLT. EMERGENCY LTS FLICKER. INSTS FLICKER. HAPPENED IMMEDIATELY AFTER T/O AND TWO MORE TIMES IN CLIMBOUT. APU STARTED AS PRECAUTION. NO EPCU FAULTS, VSCF FANS TEST OK. REPLACED EPCU PER MM, NEEDS FUNCTIONAL TEST TASK 24-21-03-720-801. C/W FUNCTIONAL CHECK OF EPCU/ELECT SYSTEM PER M/M, ALL INDICATION AND OPERATION NORMAL. 2L72 4F RTA6WE 20050721000282005072100028NE 2005 7 21 DL76L050346 220050629A7311 COOLER BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 1 ENGINE MALFUNCTIONED A DALAK NONE K FLUID LOSS ININSP/MAINT 1 SO27185DN32879 27961 727678 HISTORY OF LEFT ENG HOC USED 10 PTS ON LAST FLIGHT FROM GRU IN 9.2 HRS. PREV REPLACED DEOILER SEAL AND FUEL OIL COOLER. ATL MTC UNABLE TO FIND LEAK. REPLACED THE LEFT ENGINE. 2L72 4F4 FRTA1NM E24NE 20050721000482005072100048NM 2005 7 21 DL757050368 120050712A2920 RAM AIR TURB BOEING757 757232 1384965NM MALFUNCTIONED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27668DN 25141 DURING HMV3PSV19 ROUTINE OPN 6002 WAS BEING PERFORMED TO TEST THE RAM AIR TURBINE DEPLOYMENT SYSTEM. THE RAT FAILED TO DEPLOY TO FULL EXTEND AND LOCK POSITION. MTC CLEANED AND LUBED LINKAGE, DOOR HINGES AND ADJUSTED COMPARTMENT DOOR LINKAGE PER MM. RAT WAS RETESTED PER MM 29-21-00-735-143, OPERATION WAS NORMAL. 2L72 4F RTA2NM 20050721000512005072100051NE 2005 7 21 DLM88050371 220050716A7210 GEARBOX DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 ENGINE CRACKED A DALAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO27960DL34511 49979 725452 NR 2 ENGINE INFLT SHUTDOWN DUE TO LOSS OF ENGINE OIL AND PRESSURE. FOUND OIL LEAK AT OIL FILTER CAP. GEARBOX CRACK AT STUD HOLDING CAP - NDS ENG CHANGE. 2L72 4F4 FRTA6WE E9NE 20050721000602005072100060NM 2005 7 21 05FDEA01901 120050713A5730 SKIN DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 RT WING, LEADING EDGE SKIN AT STA XORS 797 FOUND WITH 17 IN CRACKED. REPAIR CARRIED OUT AS PER SRM 57-10-00 VOLUME I, FIGURE 37. 2L73 4F RTA22WE 20050721000632005072100063NM 2005 7 21 05FDEA01930 120050713A5320 FLOOR SUPPORT DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 CABIN, AT STA 1887 RBL 30.5 FLOOR SUPPORT STRUCTURE FOUND CORRODED. CORROSION REMOVED AND REPROTECTED AS PER SRM 51-21-01 VOL II. MATERIAL THK 0.070", MATERIAL REMAINED 0.063" AND MATERIAL REMOVED 0.007" FOUND WITHIN LIMIT AS PER SRM 53-00-01 FIG 1A VOL I. REWORKED AREA PAINTED AS PER SRM 51-21-01 VOL II. CLASSIFIED MINOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050721000722005072100072 2005 7 21 0501029959 420050715A256513621228 SLIDE DOUG DC9 DC931 3022065WP TAIL CONE MALFUNCTIONED A NWAAO OTHER O OTHER NRNOT REPORTED 1 GL01919RW 47162 DUE TO WEATHER EN ROUTE, AIRCRAFT DIVERTED. WHILE ON GROUND, PERSONNEL ATTEMPTED TO LOWER AFT STAIRWAY, INSTEAD THEY INADVERTENTLY RELEASED TAIL CONE. EMERGENCY ESCAPE SLIDE FOR TAIL DID NOT DEPLOY WHEN TAIL CONE SEPARATED FROM AIRCRAFT. VELCRO CLOSURE AND LANYARD WERE OILY AND MAY HAVE CONTRIBUTED TO DEPLOYMENT FAILURE. AIRCRAFT INSPECTED AND FERRIED AFTER TAIL CONE REINSTALLATION. MAINTENANCE REPLACED TAIL CONE AND SLIDE AND RETURNED AIRCRAFT TO REVENUE SERVICE. 2L72 4F A6WE 20050721000792005072100079CE 2005 7 21 DJFA2005121 120050718A3260 DOWNLOCK SWITCH BEECH MU300 400A 1155402CE MLG OUT OF ADJUST E DJFAO OTHER J WARNING INDICATION LDLANDING 1 EA23731TA RK273 THE CREW REPORTED THAT THE NOSE WHEEL DID NOT INDICATE DOWN WHEN THE GEAR WAS EXTENDED FOR LANDING IN KDAL. THE LIGHT DID ILLUMINATE WHEN TESTED. WHEN THE FLAPS WERE EXTENDED TO 30 DEGREES, AND THE THROTTLES REDUCED TO IDLE THE GEAR WARNING HORN DID NOT SOUND OFF. THE TOWER INFORMED THE CREW THAT THE GEAR APPEARED TO BE DOWN WHEN A GO-AROUND WAS PERFORMED. THE AIRCRAFT WAS LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ADJUSTED THE NOSE GEAR DOWN AND LOCK SWITCH. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4F RTA16SW 20050721000852005072100085NM 2005 7 21 QXEA200501116 120050718A2430400SG163Q GENERATOR BOMBDRDHC8 DHC8402 1390042NM ZONE 100 MALFUNCTIONED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09405QX 4047 SMF - ON FLIGHT 2410, NR -2 DC GENERATOR FAILED TO COME ONLINE AFTER ENGINE START. REMOVED AND REPLACED NR 2 DC GENERATOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050721001052005072100105NM 2005 7 21 USAA050844 120050707A5320 ANGLE BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU52779 23861 FOUND CHORD ANGLE CORRODED .8 INCHES, LOWER CHORD ANGLE AT BS 227.8. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR PARTS IAW EA 96645 AND BOEING DWG 69-38740. (M) 2L72 4F RTA16WE 20050721001162005072100116EA 2005 7 21 ASOA05543 120050620A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27851AS 7360 DURING A C-CHECK IN MCN, THE AVIONICS BAY FS 280 CLIP AT LBL 9 AFT OUTBOARD SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AVONICS BAY FS 280 CLIP AT LBL 9 AFT OUTBOARD SIDE IAW CRJ 200 SRM 51-42-21. (M) 2L72 4F RTA21EA 20050721001242005072100124NM 2005 7 21 USAA050841 120050707A5315 FLOORBEAM BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU 23861 CLT - FOUND FLOORBEAM TEE CAP CORRODED 1 INCH, AT BS 986.5, LBL 31. REMOVED AND REPLACED UPPER T-CAP OF FLOORBEAM IAW TYPICAL REPAIR 53-10-05, SRM 53-00-51. (M) 2L72 4F RTA16WE 20050721001302005072100130NM 2005 7 21 USAA050845 120050707A5320 INTERCOSTAL BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU 23861 CLT - FOUND INTERCOSTAL CORRODED 6 INCHES, AFT OF FORWARD E/E DOOR AT BL 0, BS 219.8 TO 227.8. REMOVED CORRODED INTERCOSTAL. FABRICATED AND INSTALLED NEW PART IAW EA 96645 AND BOEING DWG 69-38740. (M) 2L72 4F RTA16WE 20050721001342005072100134EU 2005 7 21 USAA050792 120050623A5315D5347209001100 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19721UW 1095 PIT - FOUND FLOORBEAM CORRODED .5 INCH BY .75 INCH, Y1292 FRAME 64-67. DEFECTIVE PART REPLACED WITH IDENT PART. (M) 2L72 4F RTA28NM 20050721001382005072100138EA 2005 7 21 ASOA05503 120050609A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27873AS 7549 FLT 4191 - DURING A GROUND INSPECTION IN ATL, THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE LEFT OVERWING EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050721001402005072100140EA 2005 7 21 COMA0560385 120050709A3230750005000 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA MLG MALFUNCTIONED A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01960CA 7117 FLIGHT 5521 - GEAR DISAGREE WARNING. REPLACED THE MLG SELECTOR VALVE. 2L72 4F RTA21EA 20050721001482005072100148SO 2005 7 21 RAIA00507009 120050714A2840 WARNING LIGHT EMB 145 EMB145LR 3260212SO LOW FUEL ILLUMINATED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03817HK 145058 FLT 5487 - BDL - FUEL LOW LEVEL WARNING INDICATION. MAINTENANCE DEFERRED FUEL LEVEL WARNING INDICATION PER MEL. SUBSEQUENTLY CLEARED DEFERRAL WITH A SYSTEM, OPS CHECK WITH NO DEFECTS NOTED. 2L72 4T RTT00011AT 20050721001512005072100151CE 2005 7 21 DXTA200500847 120050720A3260 INDICATION SYS CESSNA560 560XL 2076702CE MLG MALFUNCTIONED E DXTAO OTHER N FALSE WARNING APAPPROACH 1 GL07639QS 5605139 ON FINAL APPROACH LEFT GEAR GREEN LIGHT AND RED GEAR LIGHT FLICKERING. DID CHECKLIST, ACTIVATED EMERGENCY GEAR SYSTEM GOT 3 GREEN LIGHTS, NO RED. GEAR WAS BLOWN DOWN. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20050721001522005072100152EA 2005 7 21 COMA0560388 120050710A2430 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA DC BUSS ILLUMINATED A COMAB EMER. DESCENT J WARNING INDICATION DEDESCENT 1 SO01915CA 7013 FLIGHT 5607- DC BUSS 2 CAUTION MESSAGE. CND, SYSTEM OPERATIONAL CHECKS NORMAL. 2L72 4F RTA21EA 20050721001542005072100154NM 2005 7 21 SWAA052106 120050719A335065C27093 LIGHT BOEING737 7373H4 1384600NM AFT CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED SERVICE CHECK, FOUND SEVERAL LIGHT BULBS INOP AT EMERGENCY EXIT LIGHT NEAR AFT F/A STA. RELAMPED LIGHT AASY PER MM. 2L72 4F RTA16WE 20050721001552005072100155NM 2005 7 21 SWAA052107 120050718A53306545772 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 912, STR 4R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050721001632005072100163EA 2005 7 21 COMA0560390 120050710A5297K601R507474 WIRE HARNESS CNDAIRCL600 CL6002B19 1900309EA CABIN DOOR UNRELIABLE A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01716CA 7250 FLIGHT 5823 - CABIN DOOR OUTER HANDLE CAUTION. REPLACED THE DOOR WIRE HARNESS. 2L72 4F RTA21EA 20050721001642005072100164SO 2005 7 21 RAIA00507011 120050716A324431590 TIRE EMB 145 EMB145LR 3260212SO MLG SEPARATED A RAIAA UNSCHED LANDING D INFLIGHT SEPARATION CLCLIMB 1 CE03816HK 145055 FLT 5519 - STL - TOWER REPORTED TIRE RECAP DEPARTED NR 2 TIRE DURING TAKEOFF. RETURNED TO STL. MAINTENANCE REMOVED AND REPLACED NR 2 MAIN WHEEL AND TIRE. 2L72 4T RTT00011AT 20050721001672005072100167SO 2005 7 21 RAIA00507008 120050714A2910 WARNING LIGHT EMB 145 EMB145LR 3260212SO NR 1 HYD SYSTEM ILLUMINATED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03811HK 145256 FLT 3545 - PIT - HYD 1 LOW FLUID WARNING INDICATION. MAINTENANCE BLEED AND SERVICED NR 1 HYDRAULIC SYSTEM. 2L72 4T RTT00011AT 20050721001682005072100168EA 2005 7 21 COMA0560391 120050713A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01814CA 7387 FLIGHT 5384 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2L72 4F RTA21EA 20050721001702005072100170SW 2005 7 21 DXTA200500791 120050618A5415MS21030L3 NUT PLATE GULSTM680 680 0141602SW RT PYLON DEFECTIVE E DXTAK NONE O OTHER ININSP/MAINT 1 GL07349QS29 6800029 FUSELAGE FAIRING PANEL ATTACH NUTPLATES FAIL DRAG TORQUE OF 12-15 IN POUNDS. NO NOTED TORQUE ON NUTPLATES. EVALUATED ACFT ACCESS PANEL NUTPLATES FOR DEFECTS. INSTALLED NUT PLATES IAW 680 MM 51-40-03. INSTALLED PANELS IAW 680 MM. INSTALLED NUTPLATES IN RT LWR PYLON IAW 680 MM. INSTALLED RT PYLON LWR ACCESS PANELS IAW 680 MM. CLOSED RT ENGINE COWLING. 16 NUTPLATE SCREWS INSTALLED IAW ENGINEERING ORDER 680-0100, 15 CR NUMBER 099500 REF DRAWING 6900056. 1H72 3O 2A4 20050721001732005072100173EA 2005 7 21 COMA0570084 120050715A5320SH67032172 SILL CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01317CA7613 10055 FLOOR SILL CORROSION BEYOND LIMITS APPROXIMATELY 3 INCHES AFT OF FS 280 ON THE RIGHT HAND SIDE. REPAIRS CARRIED OUT IAW BOMBARDIER EO 601R-53-6796. 2L72 4F RTA21EA 20050721001742005072100174EA 2005 7 21 COMA0560392 120050714A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01937CA 7044 FLIGHT 5321 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2L72 4F RTA21EA 20050721001762005072100176WP 2005 7 21 DHLA200587302 120050717A322027713801 BOLT DOUG DC8 DC873F 302199FWP NOSE GEAR CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ 46091 DURING B-CHECK INSPECTED NOSE LANDING GEAR REMOVED RED SEAL PER NON-ROUNTINE 009836 FOUND BOLT RUSTED THROUGH AND FELL OFF. LOG PAGE OF B-CHECK 057634 2L74 4F RT4A25 20050721001782005072100178SO 2005 7 21 CHQA200500128 120050719A2612902081 CONTROL MODULE EMB 135 EMB135LR 3260305SO FIRE DETECTION UNSERVICEABLE A CHQAF ACTIVATE FIRE EXT. N FALSE WARNING TXTAXI/GRND HDL 1 GL11832RP7576 7576 145676 FLIGHT 6385 TLH-MIA - PILOT REPORTS AFTER PULLING OFF RUNWAY, AN E2 FIRE INDICATION APPEARED ON EICAS. THE FIRST ENGINE FIRE BOTTLE WAS BLOWN AND THE INDICATION REMAINED. THE SECOND ENGINE FIRE BOTTLE WAS BLOWN AND THE INDICATION REMAINED. THE FIRE DEPT FOUND NO EVIDENCE OF FIRE. MAINTENANCE VERIFIED THAT FIRE INDICATION CONTINUALLY GOES OFF. OHMED OUT BOTH ENG AND PYLON LOOPS AND OPS CHECKED GOOD. INSPECTED FIRE LOOP AND ENGINE DUCTING FOR BLOWN DUCTS. NO DEFECTS NOTED. REMOVED AND REPLACED NR 2 FIRE DETECTOR CONTROL MODULE. OPS CHECK GOOD. REMOVED AND REPLACED BLOWN FIRE BOTTLES NOW. OPS CHECK GOOD. MAINTENANCE PERFORMED HIGH POWER ENGINE RUNS. OPS CHECK GOOD. NO EICAS MESSAGES PRESENT. 2L72 4F RTT00011AT 20050721001812005072100181CE 2005 7 21 DXTA200500840 120050714A3240AHA1897 BRAKE RAYTHNDH125 HAWKER800XP 7150012CE LG WEAK E DXTAK NONE O OTHER ININSP/MAINT 1 GL07898QS 258593 BRAKES SEEM MUSHY, PERFORMED TAXI ON ACFT FOR BRAKE SYSTEM TROUBLESHOOTING. BRAKING PERFORMANCE NORMAL. COULD NOT DUPLICATE. RESEARCHED FOR RECENT HISTORY RELATED. NOT FOUND. 2L72 4F RTA3EU 20050721001822005072100182NM 2005 7 21 CALA0500216 120050711A53306545774 SKIN BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714358 23943 WALK AROUND FOUND 3.5 IN CRACK IN STA 767 LOWER LAP SKIN, S25L. REPAIRED IAW SRM 53-00-01, FIGURE 229. DIP WAS ISSUED TO REINSPECT REPAIR EVERY 60,000 CYCLES. 2L72 4F RTA16WE 20050721001842005072100184CE 2005 7 21 DXTA200500843 120050715A2720ACA1218 STRUT RAYTHNDH125 HAWKER800XP 7150012CE RUDDER INOPERATIVE E DXTAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 GL07893QS5562 258393 RUDDER BIAS ACTIVATES WITH BOTH POWER LEVERS AT T/O POWER. GOT FULL RIGHT DEFLECTION OF THE RUDDER, ABORTED AT 50 KTS. - REMOVED AND REPLACED RIGHT HAND RUDDER BIAS STRUT PERFORMED FUNCTION TEST. FUNCTION TESTED GOOD ALL WORK PERFORMED IAW HAWKER 800XP MM 27-20-51. 2L72 4F RTA3EU 20050721001852005072100185NM 2005 7 21 CALA0500218 120050711A5315BAC1505100849 FLOORBEAM BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716217 28777 AFT GALLEY FLOORBEAM CORRODED AT SEVERAL AREAS UNDER NUT PLATE AREA AT STA 986.5, LBL 54 TO RBL 54. REPAIRED FLOORBEAM IAW ECRA 5321-01246. 2L72 4F RTA16WE 20050721001872005072100187NM 2005 7 21 CALA0500220 120050715A531565C339502 FLOORBEAM BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2719623 27527 INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, LBL 0 TO RBL 43. STRAP REPAIR INSTALLED IAW SRM 53-00-51. 2L72 4F RTA16WE 20050721001882005072100188NM 2005 7 21 CALA0500221 120050715A53146562125U25 KEELBEAM BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714334 23572 INSPECTION FOUND 1.0 IN CRACK IN LT KEEL BEAM AT STA 727 ON O/B SIDE, LBL 6.5. CRACKED SECTION OF KEEL BEAM LOWER CHORD CUT OUT AND NEW SECTION SPLICED IN IAW ECRA 5311-01230. 2L72 4F RTA16WE 20050721001902005072100190NM 2005 7 21 CALA0500223 120050717A5414301A31091 SKIN BOEING737 7373T0 1384582NM NR 1 PYLON CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714334 23572 INSPECTION FOUND A 0.5 IN CRACK AT EDGE OF NR 1 PYLON SKIN PANEL OPENING NR 5724L UPPER FORWARD CORNER. SKIN REPAIRED IAW ECRA 5430-01204. 2L72 4F RTA16WE 20050721001922005072100192NM 2005 7 21 AALA20050440 120050712A3350BPS73 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHTSDISCHARGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21635AA 24593 RT OVERWING INTERIOR EMERGENCY EXIT LIGHT AND EMERGENCY EXIT LOCATOR LIGHT ABOVE 14ABC INOPERATIVE. REPLACED BOTH BATTERY PACKS AND CHARGERS FOR RT OVERWING INTERIOR EMERGENCY EXIT LIGHT AND EMERGENCY EXIT LOCATOR LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050721001982005072100198WP 2005 7 21 AALA20050446 120050717A2913314195 PUMP DOUG DC9 DC983 3022083WP RT ENG HYDRAULICINOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW21592AA 53255 RT ENGINE PUMP INOPERATIVE. RT HYDRAULIC PRESSURE LOW LIGHT ON. LANDED ORD WITHOUT INCIDENT. REPLACED RT ENGINE HYDRAULIC PUMP AND FILTERS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050721001992005072100199WP 2005 7 21 AALA20050439 120050712A3397P4010049 WIRE DOUG DC9 DC983 3022083WP EMERGENCY LIGHTSSHORTED A AALAK NONE O OTHER ININSP/MAINT 1 SW219403W 53139 EMERGENCY EXIT LIGHTS AT SEAT 20D AND BACK INOPERATIVE. FOUND WIRE SHORTED AT 280. REPLACED LIGHT ASSEMBLY FOR EMERGENCY EXIT LIGHTS AT SEAT 20D AND BACK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050721002012005072100201EA 2005 7 21 COMA0560393 120050715A2720601R5122623 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA RUDDER MALFUNCTIONED A COMAO OTHER F FLT CONT AFFECTED CRCRUISE 1 SO01920CA 7022 FLIGHT 5662- RUNAWAY RUDDER TRIM. REPLACED THE TRIM SWITCH PANEL. 2L72 4F RTA21EA 20050721002032005072100203NM 2005 7 21 QXEA200501126 120050719A3620 DUCT BOMBDRDHC8 DHC8402 1390042NM BLEED AIR LEAKING A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09402QX 4032 BOI FLIGHT 2405 ON CLIMBING OUT OF PORTLAND, PASSING THROUGH 5000 FT, NR 2 BLEED HOT CAUTION LIGHT CAME ON. ACCOMPLISHED THE E/A CHECKLIST BY TURNING THE NR 2 BLEED SWITCH OFF. AFTER A FEW MINUTES THE NR 2 BLEED HOT CAUTION LIGHT EXTINGUISHED. REPLACED NACELLE DUCT LEAK OVER TEMP SWITCH IAW AMM 36-11-21. GROUND RAN IAW AMM 36-11-00. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050721002052005072100205WP 2005 7 21 AALA20050435 120050710A3231 BRACKET DOUG DC9 DC982 3022082WP LG INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21446AA 49472 DURING CLIMB, GEAR DOOR OPEN LIGHT ILLUMINATED WITH GEAR RETRACTED AND ALL OTHER LIGHTS OUT. GEAR DOOR LIGHT REMAINED ON WITH GEAR DOWN AND 3 GREEN LIGHTS. RAN PROCEDURE AND LANDED SAT WITH GEAR DOORS OPEN. LT AND RT DOOR DAMAGE DUE TO CONTACT WITH GROUND. REPLACED RT MLG DOOR AND REPLACED SKID ON LT MLG DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050721002072005072100207NM 2005 7 21 AWXA200500811 120050715A3350 WIRE BOEING757 7572G7 1384963NM EMERGENCY LIGHTSDAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28909AW 24522 DURING 4 DAY CHECK, FOUND EMERGENCY PATH LIGHTS FROM SEAT ROW 1 TO ROW 8 INOPERATIVE. MAINTENANCE REPAIRED WIRING PER CAP 20. REMOVED AND REPLACED SEAT HARNESS AT ROW 5. ALSO, REMOVED AND REPLACED POWER SUPPLY AND BATTERY. 2L72 4F RTA2NM 20050721002082005072100208NM 2005 7 21 AWXA200500812 120050715A2410735511A GENERATOR BOEING737 7373S3 1384711NM CFMINTCFM56 CFM563B2 13802EU NR 1 ENGINE MALFUNCTIONED A AWXAAD UNSCHED LANDING RETURN TO BLOCK J WARNING INDICATION CRCRUISE 1 WP28315AW20037 23734 NR 1 ENGINE GENERATOR HAD LOW OIL PRESSURE AND HIGH OIL TEMP. DISCONNECTED GENERATOR AND RETURNED TO GEG. APU WAS ON MEL. MX R & R APU BLEED VALVE, CLEARED APU MEL. ISSUED MEL FOR NR 1 ENGINE GENERATOR. VENDOR TEAR DOWN REPORT SHOWS THAT CSD HAD VERY HIGH TIME AND WAS A JUSTIFIED REMOVAL. UNIT WAS OVERHAULED WITH ALL WORN GEARS, DAMAGED GROMMETS, DAMAGED SLEEVES, MOTOR PUMP PISTONS AND BLOCKS BEING REPLACED. 2L72 4F4 FRTA16WE E21EU 20050721002092005072100209NM 2005 7 21 AWXA200500813 120050717A3260 BULB BOEING737 7373S3 1384711NM LG POSITION BURNED OUT A AWXAO OTHER O OTHER DEDESCENT 1 WP28315AW 23734 ON DESCENT, WHEN GEAR EXTENDED, LT MLG LIGHTS WOULD NOT ILLUMINATE. AIRCRAFT FLEW BY TOWER AND MANUALLY CHECKED GEAR TO ENSURE GEAR WAS DOWN AND LOCKED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED BULBS AND CYCLED GEAR SEVERAL TIMES. ALL INDICATIONS WERE NORMAL. 2L72 4F RTA16WE 20050721002112005072100211NM 2005 7 21 AWXA200500815 120050714A532065479576 WEB BOEING737 7373G7 1384595NM AFT CARGO BAY CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 FOUND CORROSION ON WEB LOCATED AT BS 787 + 6 TO BS 847, BETWEEN STRINGER 25R AND 26R, UNDER NUT PLATES IN AFT CARGO BAY. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-15-1 FIG 101. MAINTENANCE REMOVED WEB LOCATED AT BS 787 TO BS 847, BETWEEN STRINGER 25R AND 26R. RECEIVED NEW WEB AND PREPPED FOR INSTALLATION IAW BOEING 737-300 SRM 51-40-05-0 FIG 3 SHEET 1. INSTALLED REPAIR PARTS AT BS 787 + 6 TO BS 847, BETWEEN STRINGER 25R AND 26R IAW BOEING 737-300 SRM 51-40-02-0 FIGS 8 AND 12. 2L72 4F RTA16WE 20050721002122005072100212NM 2005 7 21 AWXA200500816 120050627A5320654795711 STRAP BOEING737 7373G7 1384595NM CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 DISCOVERED CORROSION LOCATED ON STRAP AT BS 787 +6 TO BS 847 +12 BETWEEN STRINGERS 25R AND 26R IN THE AFT CARGO BAY. MAINTENANCE REMOVED CORROSION AT BS 787 +6 TO BS 847 +12 AND FOUND CORROSION TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-15-1 FIG 101. MAINTENANCE REMOVED STRAP AT BS 787 +6 TO BS 847 +12, STR 25R TO 26R. RECEIVED NEW STRAP AND PREPPED FOR INSTALLATION IAW BOEING 737-300 SRM 51-40-05-0 FIG 3, SHEET 1. INSTALLED REPAIR PARTS FROM BS 787 +6 TO BS 847 +12. BETWEEN STRINGERS 25R AND 26R IN THE AFT CARGO COMPARTMENT IAW BOEING 737-300 SRM 51-40-02-0 FIG 3, 4, 8 AND 12. 2L72 4F RTA16WE 20050721002132005072100213NM 2005 7 21 AWXA200500817 120050625A53136946877128 STRINGER BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 FOUND STRINGER 18A CRACKED AT STA 727 ON RT SIDE. MAINTENANCE REMOVED DAMAGED AREA FROM STRINGER 18A AT STA 727 IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5361-05193-SS1. FABRICATED FILLER AND GUSSET IAW AWA E.R. 03-5361-05193-SS1. INSTALLED FABRICATED REPAIR PARTS AT STA 727, RT STRINGER 18A IAW AWA ER 03-5361-05193-SS1. 2L72 4F RTA16WE 20050722000012005072200001EU 2005 7 22 BA05014 120050717A3350321431 EPSU AIRBUS330 A330323 3930335EU CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19678US 388 PHL - THE EPSU CAPACITY TEST FOR EPSU'S AT DOORS 1L AND 3L FAILED TEST. MAINTENANCE REPLACED FAILED BATTERIES IN EPSU'S AT DOORS 1L AND 3L. OPERATIONALLY CHECKS OK. 2L72 4F RTA46NM 20050722000022005072200002NM 2005 7 22 BB05051 120050708A2497 WIRE BOEING767 7672B7 1385107NM APU GENERATOR BURNED A USAAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 EA19655US 25257 DUB FLT 307 EN-ROUTE DUB TO PHL, DURING TAXI OUT, THE APU GENERATOR FAILED. THE FLIGHT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE A-PHASE FEEDER WIRE BURNT FROM THE APU GENERATOR TO THE APU FIREWALL. THE APU GENERATOR WAS PLACED ON MEL. MAINTENANCE REPLACED THE BURNED APU GENERATOR FEEDER WIRE AND REMOVED THE MEL FOR THE APU GENERATOR. OPERATIONALLY CHECKS OK. 2L72 4F RTA1NM 20050722000032005072200003EA 2005 7 22 VNAA0507009 120050710A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE FUSELAGE LIGHTNING STRIKEA VNAAK NONE O OTHER ININSP/MAINT 1 GL05720PS 10178 EVIDENCE OF A LIGHTNING STRIKE WAS FOUND DURING THE 50HR SERVICE CHECK. MAINTENANCE COMPLIED WITH A DETAILED LIGHTNING STRIKE INSPECTION IAW CRJ700 AMM 05-51-07-220-801-A01. ALL LIGHTNING DAMAGE WAS REPAIRED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050722000042005072200004EA 2005 7 22 COMA0560389 120050710A2620346000371 FIRE BOTTLE CNDAIRCL600 CL6002B19 1900309EA CARGO BAY DISCHARGED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01931CA173635739 7037 FLIGHT 5372 - CARGO FIRE BOTTLE LOW CAUTION. REPLACED THE CARGO FIRE BOTTLES. 2L72 4F RTA21EA 20050722000052005072200005EA 2005 7 22 VNAA0507007 120050707A3230750006000 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE MLG FAILED A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL05226JS3037 7895 THE NOSE DOOR OPEN WARNING ILLUMINATED AND SOUNDED AFTER GEAR RETRACTION. THE FLIGHT RETURNED TO SDF. THE AIRCRAFT WAS FERRIED TO PHL WHERE MAINTENANCE REMOVED & REPLACED THE NLG DOOR SELECTOR VALVE IAW CRJ200 AMM 32-22-20-000-801 AND 32-22-20-400-801. LEAK AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050722000062005072200006EA 2005 7 22 VNAA0507006 120050706A3260895304 PSEU CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE MLG FAILED A VNAAO OTHER J WARNING INDICATION CLCLIMB 1 GL05703PS158 10137 DURING CLIMBOUT THE LANDING GEAR INDICATION SYMBOLS AND 9 CAS MESSAGES ILLUMINATED AT THE SAME TIME. THE AIRCRAFT MADE AN UNEVENTFUL LANDING. MAINTENANCE REMOVED AND REPLACED THE PROXIMITY SYSTEM ELECTRONICS UNIT IAW CRJ700 AMM 32-61-01-400-801-A01. THE LANDING GEAR WAS OPERATIONALLY CHECKED IAW CRJ700 AMM 32-30-00-710-801-A01. ALL OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050810002992005081000299EA 2005 8 10 VNAA0507010 120050715A29136619003 PUMP CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE HYD SYSTEM LEAKING A VNAAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL05708PS2560 10160 DURING CRUISE THE CREW REPORTED TOTAL LOSS OF THE NR 1 HYDRAULIC SYSTEM PRESSURE AND FLUID QUANTITY. MAINTENANCE FOUND THE LEFT ENGINE DRIVEN HYDRAULIC PUMP LEAKING. THE LEFT EDP WAS REMOVED & REPLACED IAW CRJ700 AMM 29-11-01-400-801-A01. ALL OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050722000072005072200007EA 2005 7 22 VNAA0507005 120050706A3260 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NLG DOOR ILLUMINATED A VNAAO OTHER J WARNING INDICATION APAPPROACH 1 GL05226JS 7895 THE NOSE DOOR OPEN WARNING ILLUMINATED AND SOUNDED ON SHORT FINAL. MAINTENANCE INSPECTED THE NLG DOORS IAW CRJ200 AMM 32-20-00-210-801. OPERATIONAL CHECKS WERE NORMAL. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050722000082005072200008EU 2005 7 22 05FDEA01990 120050718A5753 FAIRING AIRBUS300 A300F4605R 3930327EU NR 4 FLAP TRACK DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25656FE 745 RH WING NR 4 FLAP TRACK FAIRING AT FWD O/B LWR SURFACE HAS DELAM. 2L72 4F RTA35EU 20050722000092005072200009NM 2005 7 22 05FDEA01992 120050719A5320 BRACKET DOUG MD11 MD11 3023602NM A/C BAY CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 LT NR 1 AIR CONDITIONING BAY, LOWER LONGITUDINAL BRACKET ASSY FOUND WITH CORROSION AS MARKED. INTERCOSTAL FABRICATED AND INSTALLED AS PER DWG ACA3816 AND SRM 51-31-01 VOL 2 RESPECTIVELY. 2L73 4F RTA22WE 20050722000102005072200010WP 2005 7 22 05FDEA01994 120050719A5311 FRAME DOUG DC10 DC1010 3022110WP FUSELAGE DAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25571FE 47830 DURING AIRPLANE'S CONVERSION ROM P TO F FOUND PROCURED HOLE ON RADIUS FRAME DIM 4,00''. INSTALLED REPAIR ANGLE ON FRAME PER SRM 53-30-00 FIG 4A. 2L73 4F A22WE 20050722000112005072200011WP 2005 7 22 05FDEA01995 120050719A5313 LONGERON DOUG DC10 DC1010 3022110WP FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25571FE 47830 DURING AIRPLANE'S CONVERSION FROM P TO F FOUND: ON FWD CARGO COMPARTMENT BTW STA 808-821 L 52, CORROSION ON SHOVEL END AND LONGERON. ACCOMPLISHED REMOVAL OF SHOVEL END, SPLICES. REMOVED CORROSION. REPAIRED IAW SRM 51-33-01 PAGE 34-47 AND SRM 51-35-01 PAG 1-12. 2L73 4F A22WE 20050722000122005072200012WP 2005 7 22 2005000004 120050518A3350EMBS1392 POWER SUPPLY DOUG DC10 DC1030 3023501WP EMERGENCY LIGHT FAILED A CNMAK NONE L NO TEST ININSP/MAINT 1 SW0717085 1408 47957 ON PRE-FLIGHT, FOUND EMERGENCY LIGHT TEST LAMP INOP (GREEN LIGHT ON OVERHEAD PANEL). REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY PER MM 33-51. 2L73 4F A22WE 20050722000132005072200013EU 2005 7 22 USAA050787 120050623A5315D5311281520200 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19721UW17844 1095 PIT - FOUND FLOORBEAM CORRODED 1.5 INCH BY 4 INCHES, CABIN FLOORBEAM Y1292 AT FRAME 18. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-42-00, 51-43-00, 51-72-11. CORROSION LEVEL 1, TASK JA-220-53500. (M) 2L72 4F RTA28NM 20050722000152005072200015WP 2005 7 22 UPS05844915 120050623A5230 SKIN DOUG DC8 DC873F 302199FWP C-4 DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE:C1 C-4 DOOR UPPER FWD CORNER HAS A STEEL DOUBLER REPAIR AND MUST BE REPLACED WITH AN APPROVED REPAIR. REMOVED DOUBLER AND FILLER, FOUND CRACK AT PREVIOUS CUT OUT, CUT OUT DAM AGED AREA, FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0 FIG 21 , 53-2-0 FIG 1D, AND DWG 5616674. 2L74 4F RT4A25 20050722000162005072200016WP 2005 7 22 UPS05844916 120050625A5312 BULKHEAD DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE:C1 683 BULKHEAD CRACKED LBL 10 - RBL 24. CUT OUT DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 53 -2-5 FIG 13. 2L74 4F RT4A25 20050722000182005072200018WP 2005 7 22 UPS05844918 120050627A5730 SKIN DOUG DC8 DC873F 302199FWP NR 2 STUBWING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE: C1, LW NR 2 STUBWING UPPER OB CORNER HAS A CRACK IN SKIN. STOP DRILLED THREE CRACKS, FABRICATED, AND INSTALLED REPAIR IAW DC-8 S RM 57-2-0, 57-5-0, AND 57-2-1 FIG 18. 2L74 4F RT4A25 20050722000192005072200019WP 2005 7 22 UPS05844919 120050627A5730 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 C1 RT WING LE LWR SKIN CRACKED 1 INCH LONG AROUND FASTENER HOLE AT XW 257. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR IAW EO DC8-5720 -4087-B APPENDIX C. 2L74 4F RT4A25 20050722000202005072200020WP 2005 7 22 UPS05844921 120050628A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE: C1, CRACKED APPROX .5 INCH ON LONG 15 UPPER FLANGE 2ND CANTED FRAME FROM STA 1766 INSIDE MAIN CABIN RH SIDEWALL. REMOVED DAMAGE SECTION OF LONGERON, FABRICATED, AND INSTALLED REPAIR I AW DC-8 SRM 53-2-2 FIG 10. 2L74 4F RT4A25 20050722000252005072200025WP 2005 7 22 UPS05844926 120050628A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 C1 LONG 15L AT APPROX STA 1744 HAS A CRACK AT UPPER FRAME ATTACH POINT. REMOVED DAMAGED SECTION OF LONGERON, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 53-2-2 FIG 10. 2L74 4F RT4A25 20050722000302005072200030NM 2005 7 22 QXEA200501112 120050716A2923 PUMP DHAV DHC8 DHC8202 2809007NM HYD AUX SYSTEM INOPERATIVE A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09346PH 477 PDX - NR 1 STANDBY HYDRAULIC PUMP INOP. UPON INSPECTION, FOUND CIRCUIT BREAKER POPPED OPEN IN AC CONTACTOR BOX (2921-CB8). CLOSED CIRCUIT BREAKER IAW GMM 5-18-0. GROUND RAN ENGINE. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050722000322005072200032 2005 7 22 QXEA200501111 420050715A3418501177003 SERVO CNDAIRCL600 CL6002C10 1390015EA STICK PUSHER MALFUNCTIONED A QXEAK NONE O OTHER TXTAXI/GRND HDL 1 NM09606QX4980 10023 PDX- FLIGHT NR 2509 - DURING FLIGHT CONTROL CHECK OF ELEVATORS, ELEVATOR MOVEMENT TO UP O=POSITION (NOSE DOWN) REQUIRES MORE THAN NORMAL PRESSURE WITH PRESSURE FELT AGAINST CONTROL COLUMN AND A NOTICEABLE CLICKING. RATCHETING SOUND ASSOCIATED WITH CONTROL COLUMN MOVEMENT. MAINTENANCE REPLACED THE STICK PUSHER SERVO. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20050722000332005072200033EA 2005 7 22 QXEA200501113 120050716A3610GG670800011 VALVE CNDAIRCL600 CL6002C10 1390015EA NR 1 ENGINE MALFUNCTIONED A QXEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM09611QX7121 10041 DEN - FLIGHT NR 4327 ITT 840 C. - MAINTENANCE REPLACED NR 1 ENGINE HIGH PRESSURE SHUTOFF VALVE. OPERATION CHECK GOOD AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20050722000342005072200034EA 2005 7 22 COMA0560397 120050711A3241 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA ANTI SKID SYS ILLUMINATED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01471CA 7655 FLIGHT 5877- LEFT OUTBD ANTI SKID CAUTION. CND, SYSTEM CHECKS NORMAL, NO FAULTS FOUND. 2L72 4F RTA21EA 20050722000352005072200035NM 2005 7 22 CALA0500228 120050720A5347143A531033 SEAT TRACK BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2726215 28775 INSPECTION FOUND SEAT TRACK CORRODED AT STA 360-380, LBL 22. A REPAIR WAS INSTALLED IAW ECRA 5321-01253. 2L72 4F RTA16WE 20050722000362005072200036NM 2005 7 22 CALA0500229 120050721A3350D71701100 BATTERY PACK BOEING737 737724 13844BYNM EMERGENCY LIGHT INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2724729 28945 SEVERAL EMERGENCY LIGHTS ON SEATS AND OVERHEAD WERE FOUND INOPERATIVE DURING AN "S" CHECK AT SNA. THE FORWARD AND AFT GALLEY EMERGENCY BATTERY PACKS WERE REMOVED AND REPLACED IAW MM 33-51-00. 2L72 4F RTA16WE 20050722000372005072200037SO 2005 7 22 SWIA200515290 120050717A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT DISCHARGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07226SW9307 9307 120296 NUMEROUS EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED CENTER ELBP PER MM 33-10-02. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050722000382005072200038EA 2005 7 22 SWIA200515291 120050719A2751855D10011 SENSOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION LDLANDING 1 NM07461SW6005 6005 7811 AFTER LANDING "FLAPS FAIL" CAUTION MSG. REPLACED RIGHT BPSU. RIGGED BPSU IAW 27-51-10. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050722000412005072200041EA 2005 7 22 SWIA200515294 120050719A2760C13045BA03 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07712SK3427 3427 10172 SSCU 1 FAULT STATUS MSG.REPLACED NR 1 SSCU IAW MM 27-61-05. OPERATIONAL CHECK GOOD IAW MM 27-61-05. 2L72 4F RTA21EA 20050722000422005072200042EA 2005 7 22 SWIA200515295 120050718A274070744 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA STAB MOTOR MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07702SK2559 2559 10136 STAB CH1 INOP STATUS. REPLACED HORIZONTAL STAB MOTOR CONTROL UNIT. IAW CRJ MM 27-42-07. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050722000432005072200043EA 2005 7 22 SWIA200515296 120050717A2750860D10018ABCD CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 NM07919SW886 886 7657 DURING CLEAN UP ON OUR CLIMB OUT, WE RECEIVED "FLAPS FAIL" MESSAGE ON ED 1. REPLACED FLAP ELECTRONIC CONTROL UNIT IAW 27-50-01. OPERATIONAL CHECK OK. 2L72 4F RTA21EA 20050722000442005072200044EA 2005 7 22 SWIA200515297 120050718A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07405SW 7029 STAB TRIM CH 1 WILL NOT ENGAGE. REPLACED HSTA IAW MM 27-40-00, 27-42-01, 27-42-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050722000472005072200047EU 2005 7 22 05FDEA02002 120050720A5320 WEB AIRBUS300 A300F4605R 3930327EU ZONE 100 CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25656FE16518 745 NR AFT CARGO DOOR FWD UPPER CORNER OPENING WEB CRACKED AND BENT. REMOVED WEB IAW SRM 51-40-21. LOCATED AND DRILLED NEW WEB AND ANGLE IAW SRM 51- 40-40 INSTALLED NEW WEB & ANGLE IAW SRM 51-40-21 2L72 4F RTA35EU 20050722000492005072200049EA 2005 7 22 COMA0560399 120050718A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ILLUMINATED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01978CA 7158 FLIGHT 5237- LEFT THRUST REVERSER UNLOCKED CAUTION. DEFERRED MAINTENANCE ON THRUST REVERSER PER MEL 2L72 4F RTA21EA 20050722000522005072200052NM 2005 7 22 BB05053 120050720A2120 ODOR BOEING757 7572B7 1384964NM RROYCERB211 RB211535E4 54555NE COCKPIT DETECTED A USAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA19620AU 27199 CLT FLIGHT 791 EN-ROUTE SJU TO CLT - DURING TAKE-OFF, FROM ROTATION UNTIL INITIAL CLIMB, A STRONG ODOR OF JET FUEL WAS NOTICED IN THE COCKPIT. AFTER FIVE SECONDS, THE ODOR WENT AWAY. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED FOR FUEL LEAKS AND FOUND NONE. ACCOMPLISHED THE APPROPRIATE FIM PROCEDURE. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA2NM E12EU 20050722000532005072200053NM 2005 7 22 QXEA200501125 120050719A3010 SWITCH DHAV DHC8 DHC8202 2809007NM DE ICE SYSTEM MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION DEDESCENT 1 NM09354PH 498 SEA - DE-ICE PRESSURE ON DURING DESCENT (9 PSI) DURING TAXI PRESSURE RETURNED TO NORMAL (SELECTED BOOT AIR TO ISO AS PER CHECKLIST). REPLACED NR 1 & 2 LOW PRESSURE SWITCHES (55) PERFORMED FUNCTIONAL CHECK OF BLEED AIR SYSTEM IAW AMM 21-11-00, PAGES 501-503. OPERATIONAL CHECK GOOD. NO DE-ICE PRESSURE CAUTION NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050722000552005072200055NM 2005 7 22 QXEA200501128 120050720A2611302313 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM CARGO BAY FAULTY A QXEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM09365PH320614224 526 SEA FLIGHT 2030 INTERMITTENT SMOKE WARNING LIGHT ILLUMINATED IN CLIMB THROUGH 12,000 FEET. TROUBLESHOT, FOUND NR 2 SMOKE DETECTOR ON THE FORWARD BULKHEAD IN THE BAGGAGE COMPARTMENT FAULTY. REPLACED NR 2 SMOKE DETECTOR. OPERATIONAL CHECK GOOD. NO FURNTER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050722000592005072200059WP 2005 7 22 0501109601 120050717A2130 CONTROL SYSTEM DOUG DC9 DC932 3022066WP CABIN PRESSURE MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL01601NW 47038 IN LEVEL FLIGHT AT FL340 THE CABIN ALTITUDE ROSE ABOVE 10,000 FEET. CREW PERFORMED AN EMERGENCY DESCENT, COMPLIED WITH COM, UTILIZED THE RED BORDERED CHECKLIST, AND DIVERTED TO DEN. CABIN PRESSURE WAS REGAINED AT FL180 BUT CABIN MASKS HAD DEPLOYED. LANDING WAS UNEVENTFUL AND MAINTENANCE AT DEN REPLACED THE LEFT TURBINE NOZZLE SHUTOFF VALVE, THE LEFT AUGMENTATION VALVE, AND BOTH WATER SEPARATOR ICE SCREENS. THE AIRCRAFT HAS RETURNED TO SERVICE. 2L72 4F A6WE 20050722000602005072200060SO 2005 7 22 CHQA200500127 120050718A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11285SK 145435 RIGHT HAND OVERWING EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED RIGHT HAND OVERWING EMERGENCY EXIT LIGHT BULB IAW EMB 145 AMM 33-50-07-4. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050722000612005072200061EU 2005 7 22 DHL2005365004 120050720A3030 WARNING LIGHT AIRBUS300 A300B4203 3930306EU AOA PROBE ILLUMINATED A DHLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01365DH 149 ON CLIMB OUT AT JFK ANGLE OF ATTACK PROBE HEAT LIGHT CAME ON. THIS WAS ON THE CAPTAINS SIDE ONLY. THE LIGHT WENT OUT AFTER 5 SEC. COULD NOT DUPLICATE. SYSTEM OPS CKS GOOD IAW MM 22-23-00. 2L72 4F RTA35EU 20050722000622005072200062EU 2005 7 22 DHL2005362009 120050720A5270 WARNING SYSTEM AIRBUS300 A300B4203 3930306EU PAX DOOR ACTIVATED A DHLAO OTHER N FALSE WARNING CRCRUISE 1 SO01362DH 84 DOOR LIGHT CAME ON IN FLIGHT ON MWP WITH CHIME AND NO ASSOCIATED LIGHTON S/O DOOR PANEL. EMERGENCY CHECKLIST FOR DOOR LIGHT COMPLETED. PERFORMED DOOR WARNING SYSTEM TEST IAW M/M 52-70-00. OPS CK GOOD. COULD NOT DUPLICATE DISCREPANCY. 2L72 4F RTA35EU 20050722000632005072200063EA 2005 7 22 GBHA0507001 220050712A741476337 IDLER GEAR BELL 47 47G5A 1181034SW LYC O435 VO435A1B 41516EA MAGNETO BROKEN E GBHAO OTHER Y ENGINE STOPPAGE NRNOT REPORTED 1 GL27715BH 25105 MAGNETO DRIVE IDLER GEAR SHAFT FAILED CAUSING BOTH MAGNETOS TO BECOME INOPERATIVE AND THE ENGINE FAILED. THE FAILURE APPEARED TO ORIGINATE AT THE OIL HOLE. TOTAL TIME ON THE ENGINE WAS 4600 HOURS AND TOTAL TIME ON THE PART PROBABLY WAS 4600 HOURS AND THE ENGINE TSO 220 HOURS. THERE WAS NO VERFICATION THE PART WAS MAGNAFLUX AT OVERHAUL. RECOMMEND FOLLOWING THE MANUFACTURERS RECOMMENDATION AND MAGNAFLUX ALL STEEL PARTS. FURTHER THE OIL HOLE DID NOT APPEAR TO HAVE ADEQUETE RELIEF WHEN MANUFACTURED. 1G71 3O3 O 2H3 E279 20050722000642005072200064NM 2005 7 22 05FDEA02004 120050720A7160 NOSE COWL DOUG MD11 MD11 3023602NM NR 1 ENGINE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 NR 1 ENGINE, NOSE INLET COWL INNER BARREL FROM 3, 9 AND 12 O' CLOCK POSITION FOUND DOUBLER WITH SHEARED RIVETS. NR 1 ENGINE, NOSE INLET COWL REMOVED AND REPLACED AS PER AMM 71- 11-01-4. 2L73 4F RTA22WE 20050722000652005072200065NM 2005 7 22 05FDEA02005 120050721A5347606549 SEAT TRACK BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25280FE 22347 SEAT TRACK LBL 45 690-740 IS CORRODED. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2 2L73 4F RTA3WE 20050722000672005072200067EU 2005 7 22 05FDEA02007 120050721A5330 SKIN AIRBUS300 A300F4605R 3930327EU ZONE 100 DENTED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25670FE12779 777 FUSELAGE BOTTOM SKIN PANEL, FR 1-10 AREA -A- FOUND DENTED SKIN DURING ALI INSPECTION. REMOVED DAMAGED AREA OF SKIN, FAB'D REPAIR DOUBLER AND FILLER FROM 2024-T3 .071 AND .050 INSTALLED THE REPAIR IAW SRM 53-11-12 FIG 201. PAINTED REPAIRED AREA IAW MM 51-75-10-8 MAJOR REPAIR. 2L72 4F RTA35EU 20050722000682005072200068EU 2005 7 22 05FDEA02008 120050721A3260837101A PROXIMITY SENSOR AIRBUS310 A310 EU MLG FAILED A FDEAA UNSCHED LANDING G MULTIPLE FAILURE CLCLIMB 1 SO25401FE2492 2492 191 TAT HEAT FAULT. TAT FAULT & ALL THREE PITOT HEAT FAULT ILLUMINATED ON OVERHEAD. REMOVED PROXIMITY SENSOR UNIT AND INSTALLED LANDING GEAR RELAY SIMULATOR SET IAW A310-200 MM 32-00-00-5. LANDING GEAR HANDLE WOULD GO TO FULL UP WITHOUT INTERLOCK AS IT SHOULD. ALL SYSTEMS ASSOCIATED WITH THE ATB OPERATED NORMALLY. 2L72 4F RTA35EU 20050722000692005072200069EU 2005 7 22 05FDEA02009 120050721A3243BDM3003 PROXIMITY SENSOR AIRBUS300 A300F4605R 3930327EU MLG BRAKES MALFUNCTIONED A FDEAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO25674FE1054710547 781 WITH GEAR DOWN AND LOCKED BRAKES INDICATED LOCKED WHILE IN FLIGHT. BRAKE ACCUMULATOR PRESS INDICATED NORMAL IN ALL THREE POSITIONS. R & R PROX BOX PER TSM FAULT CODE INDICATES FAULTY CHANNEL IN BOX (BOX 31 FAULT) OPS CHECKED NORMAL PER AIRBUS M/M 32-31-71-4, CHANGED BRAKE CONTROL UNIT AS PROCAUTIONARY PER AIRBUS M/M 32-42-72-4. 2L72 4F RTA35EU 20050722000712005072200071EA 2005 7 22 COMA0570086 120050717A3250530133 TILLER CNDAIRCL600 CL6002C10 1390015EA COCKPIT MALFUNCTIONED A COMAO OTHER J WARNING INDICATION LDLANDING 1 SO01642CA4782 10125 FLIGHT 5197- STEERING INOP CAUTION DURING LANDING. REPLACED THE STEERING TILLER. 2L72 4F RTA21EA 20050722000722005072200072WP 2005 7 22 MWEA050071 120050719A2120 HAZE DOUG DC9 DC982 3022082WP CABIN DETECTED A MWEAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 GL31809ME 48071 LIGHT HAZE IN CABIN AND RIGHT AFT LAVATORY SMOKE DETECTOR WENT OFF. NO FIX AT THIS TIME 2L72 4F A6WE 20050722000742005072200074SO 2005 7 22 SWIA200515299 120050714A27503472001001 CONTROL UNIT EMB 120 EMB120ER 3260203SO TE FLAP MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07578SW 120346 FLAPS AND SWS LIGHT ON MAP. REPLACED FLAP CONTROL UNIT IAW 27-50-06. OPERATIONAL CHECK GOOD. PN: 347200-1001, SNOFF: 211 2L72 4T RTA31SO 20050722000752005072200075EA 2005 7 22 SWIA200515300 120050713A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07709BR 7850 EMERGENCY LIGHT STRIPS FOUND INOP. REPLACED LIGHT STRIP (2ND WHITE STRIP). OPERATIONAL CHECK GOOD AT THIS TIME. 2L72 4F RTA21EA 20050722000772005072200077NM 2005 7 22 AWXA200500833 120050715A53206561461 SUPPORT ANGLE BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 MCN - MAJOR REPAIR - DISCOVERED, DURING C16 CHECK, L1 DOOR CUTOUT SIDEWALL LINER SUPPORT ANGLE CRACKED AT BS 344, ST 14L. MAINTENANCE REMOVED THE DAMAGED AREA ON THE SUPPORT ANGLE FOR THE L1 DOOR CUTOUT SIDEWALL LINER IAW BOEING 737-300 SRM 51-70-11-0 FIG. 1. FABRICATED REPAIR ANGLE AND FILLER FOR L1 SIDEWALL LINER IAW BOEING 737-300 SRM 51-70-11-0. INSTALLED FABRICATED REPAIR PARTS IAW BOEING 737-300 SRM 51-70-11-0 FIG 1. 2L72 4F RTA16WE 20050722000792005072200079NM 2005 7 22 AWXA200500835 120050711A534069353521 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED STRINGER TIE CRACKED AT BS 380, STR 14L. MAINTENANCE REMOVED DAMAGED TIE AT BS 380, STR 14L IAW BOEING 737-300 SRM 51-40-02-0. PREPPED NEW STRINGER TIE FOR INSTALLATION IAW BOEING 737-300 SRM 51-40-05-0 FIG. 2. INSTALLED REPAIR PARTS AT BS 380, STR 14L IAW BOEING 737-300 SRM 51-40-02 FIGS 8, 4, AND 12. 2L72 4F RTA16WE 20050722000802005072200080NE 2005 7 22 AWXA200500836 220050719A72008249722010 EEC AIRBUSA319 A319132 3930340NM IAE V2524 V2524A5 NE NR 1 ENGINE MALFUNCTIONED A AWXAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 WP28802AW156 924 NR 1 ENG STALLED. CREW RETURNED TO LAS WITHOUT INCIDENT. ENG BORESCOPED & FERRIED BACK TO PHX. MX R & R NR 1 ENG 7TH STAGE BLEED VALVE, 7A & 7C BLEED VALVE, & 7C BLEED VALVE SOLENOID. LUBED VSV ON NR 1 ENG & R & R NR 1 EEC. PERFORMED POWER RUNS IAW TASK CARD. TEARDOWN REPORT OF EEC CONFIRMS REMOVAL. TEARDOWN SHOWS THAT 3 PRESSURE TRANSDUCERS, PAMB, P2 & P5, FAILED BEYOND CMM LIMITS. EEC REPAIRED & TESTED IAW CMM. BLEED VALVE TEARDOWN REVEALED EXCESSIVE LEAKAGE CAUSING VALVE OPENING & CLOSING PRESSURES EXCEEDED LIMITS. UNIT OVERHAULED & TESTED IAW CMM. OPS TESTS GOOD. TEARDOWN OF BLEED VALVE CONFIRMED UNIT FAILED TO FUNCTION. FOUND ALL PISTON SEALS & SHIMS DISTORTED DUE TO HEAT. PLUNGER VALVE REPLACED. 2L72 4F4 FRTA28NM E40NE 20050720002122005072000212EU 2005 7 20 NACA20050016 120050616A575155761015601401 AILERON AEROSPATR42 ATR42* 8680900EU LT WING LIGHTNING STRIKEA NACAO OTHER O OTHER CRCRUISE 1 AL0342NC 067 LIGHTNING STRIKE KNOCKED OUT NR 1 ACW AND NR 1 ECU. BOTH WERE RESET SUCCESSFULLY. UPON INSPECTION, DISCOVERED THERE WAS DAMAGE TO LT AILERON. REPLACED LEFT AILERON ASSEMBLY AND OPS CHECKED GOOD. 2H72 4T RTA53EU 20050721000082005072100008EU 2005 7 21 KBM2005F00151 120050713A21200500847 MOTOR SNIAS 350 AS350B2 8680813EU CONDENSOR MALFUNCTIONED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH 2884 7 INCH CONDENSOR MOTOR, AC 11 AMP. RESET CIRCUIT BREAKER POPPED SEVERAL TIMES. REMOVED AND REPLACED. (K) 1G71 3U H9EU 20050721000272005072100027NM 2005 7 21 DLM88050344 120050629A2497 WIRE HARNESS DOUG MD88 MD88 3023688NM CABIN BURNED A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO27906DL 49537 PRIMARY STAB TRIM C/B POPPED. SIMULTANEOUS TAIL CONE UNSAFE LIGHT ON OAP. FOUND WIRE BUNDLE BURNED IN MID CABIN CEILING AREA. REPAIRED WIRING. 2L72 4F RTA6WE 20050721000302005072100030NM 2005 7 21 DL757050348 120050701A21701942784 COALESCER BAG BOEING757 757232 1384965NM LT A/C BAY CRACKED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27681DA 26957 DURING CLIMBOUT NOTICED A/C WAS NOT COOLING OR PRESSURIZING. REPLACED BLOWN DUCT ON LEFT WATER SEPARATOR. 2L72 4F RTA2NM 20050721000372005072100037NM 2005 7 21 DL76L050355 120050708A3244767300ERM TIRE BOEING767 767332 1382001NM MLG FAILED A DALAA UNSCHED LANDING D INFLIGHT SEPARATION CLCLIMB 1 SO27183DN DL1484 27110 MLG TIRE RECAP FAILED. FOUND DAMAGE TO NR 1 AND NR 5 MLG TIRES. REMOVED AND REPLACED NR 1 AND NR 5 WHEEL ASSYS. LEFT I/B AFT FLAP DAMAGE FROM NR 1 MAIN TIRE FOD. REPAIRED DAMAGE PER ERA 099530-14. 2L72 4F RTA1NM 20050721000382005072100038NM 2005 7 21 DL738050357 120050709A2120 ODOR BOEING737 737832 13844CFNM CABIN DETECTED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO273743H 30836 FIVE MINS AFTER T/O A BURNING ODOR NOTICED IN COCKPIT. ODOR WAS ACRID ELECTRICAL SMELL WITH A LIGHT HAZE IN THE COCKPIT. SMOKE CLEARED WITH PACKS ON HIGH. RAN ENGINES AND PACKS AT ALL PWR SETTING. CK'D OPERATION OF LT AND RT RECIRCULATION FANS. ALL NORMAL. INSPECTED COCKPIT OVERHEAD, C/B PANELS AND BEHIND DISPLAYS. ALSO CK'D GALLEY, LAVS AND PASS COMPARTMENT OVERHEAD. VISUALLY INSPECTED FWD AND MAIN E/E. ALSO BOTH BAG BINS. NO ABNORMAL ODORS OR SMOKE NOTED. A/C OK FOR SERVICE. 2L72 4F RTA16WE 20050721000452005072100045NM 2005 7 21 DLM88050367 120050713A2910 LINE DOUG MD88 MD88 3023688NM HYD SYSTEM LEAKING A DALAO OTHER K FLUID LOSS LDLANDING 1 SO27939DL 49812 DURING DESCENT, LEFT HYDRAULIC QTY DECREASED TO 4 QTS. RECEIVED AN AMBER WARNING LIGHT BUT NO OAP MESSAGE. RAN HYD QTY LOW OR DECREASING CHECKLIST AND DECLARED AN EMERGENCY WITH CVG APPROACH CONTROL. RECEIVED GOOD GEAR INDICATION DOORS UP, ND AFTER LANDING PRESSURE ON LEFT SIDE DROPPED TO 0. LT T/R WAS STUCK IN UNLOCKED. AFTER LANDING BUT STOWED ITSELF DURING TAXI IN. GEAR PINNED BY MTC. INSP LT HYD SYSTEM. FOUND CRACK IN LINE COMING OFF THE TOP OF THE LT HYD BRAKE ACCUMULATOR. RING LOCKED LINE AND REMOVED AND REPLACED ACCUMULATOR PER AMM. SVCD LT HYD LEAK CK. 2L72 4F RTA6WE 20050721000562005072100056NM 2005 7 21 DL76G050376 120050718A335020131A BATTERY PACK BOEING767 767324 1385203NM EMERGENCY LIGHT DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27394DL 27394 ON SQUIB TEST FOUND LEFT SIDE AND RT SPOILER WILL NOT TEST. REPLACED BATTERIES M962 AND M961 OFF WING BATTERY PACKS. OPS CKD NORMAL. 2L72 4F RTA1NM 20050721000582005072100058NM 2005 7 21 05FDEA01900 120050713A5280 HINGE FITTING DOUG MD11 MD11 3023602NM LT MLG W/W DOOR WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 UPON REMOVAL OF LT MLG WHEEL WELL DOOR, FOUND AFT HINGE FITTING WORN. REMOVED AND REPLACED AS PER SRM 51-35-01 VOLUME II. THIS REPAIR IS CLASSIFIED MINOR PER GMM 6-2-100. 2L73 4F RTA22WE 20050721000612005072100061NM 2005 7 21 05FDEA01921 120050713A534065453132 STRINGER CLIP BOEING727 727233 138408ANM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 FUSELAGE UPPER LOBE STRINGER CLIP CRACKED BS 680 STR-5L. REMOVED FABRICATED AND INSTALLED STRINGER CLIP AT BS 680 STR 5L IAW SRM 51-20-1, 51- 30-02, 51-10-02. 2L73 4F RTA3WE 20050721000662005072100066NM 2005 7 21 05FDEA01948 120050714A5312 BULKHEAD BOEING727 727233 138408ANM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 BS 870 BULKHEAD HAS CORROSION ON FWD AND AFT SIDE AT WIRE CONNECTOR ATTACH PLATE, LBL 42. REMOVED CORROSION, FABRICATRED, ALODINED, PRIMED AND INSTALLED REPAIR PARTS PER SRM 53-10-1, 51-30-2 AND 53-10-9. 2L73 4F RTA3WE 20050721000672005072100067WP 2005 7 21 05FDEA01949 120050714A5313AFA30781 LONGERON DOUG DC10 DC1010 3022110WP ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25373FE 46611 CORROSION FOUND IN VERTICAL LEG OF LONGERON 47L STATION 1764, LEAVING A HOLE .5 HIGH BY 3.0 LONG AFTER CORROSION REMOVAL WITH REDUCED MATERIAL THICKNESS ON BOTH SIDES OF SUBJECT HOLE. COMPLIED WITH FED EX EA 8-5310-91240 FUSELAGE LONGERON 47L STA 1764 CORROSION, REPAIR. 2L73 4F A22WE 20050721000732005072100073NM 2005 7 21 05FDEA01927 120050713A53406545136 STRINGER CLIP BOEING727 727233 138408ANM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 FUSELAGE UPPER LOBE, CRACKED STRINGER CLIP, BS 580, STR 7R. REPLACED CRACKED STRINGER CLIP PER SRM 51-30-2. 2L73 4F RTA3WE 20050721000752005072100075EU 2005 7 21 05FDEA01966 120050715A2497 WIRE AIRBUS310 A310 EU NR 2 BATTERY DAMAGED A FDEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO25450FE 162 NR 2 BATTERY OVERHEATED DURING CRUISE. NR 2 BATT SHOWED 21V AND SWITCHED OFF FOR DURATION OF FLIGHT. VERIFIED BATTERY WAS HOT, AND PERFORMED BATT CHARGE CONT BITE TEST. ALL NORMAL. FOUND RED AND BLUE WIRES 195 AND 196 AT BAT2 SHUNT 19PE DAMAGED AND CHAFING TOGETHER. REPAIRED BOTH WIRES AND REPLACED BATTERY PER PRECAUTIONARY DUE TO OVERHEATING, TESTED BATT CONT BITE TEST AGAIN ALL NORMAL. LET BATTERIES CHARGE FOR 2 HOURS AND OPERATED NORMALLY. 2L72 4F RTA35EU 20050721000872005072100087CE 2005 7 21 DXTA200500838 120050706A3260 UPLOCK SWITCH CESSNA750 750 2076810CE LG OUT OF ADJUST E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07912QS 7500012 AFTER TAKEOFF, LANDING GEAR FAILED TO RETRACT NORMALLY. UNLOCK LIGHT STAYED ILLUMINATED FOR ABOUT 2 MINUTES. FELT LIKE NOSE WHEEL WAS TRYING TO CYCLE UP. AFTER SEVERAL ATTEMPTS GEAR STOWED AND UNLOCK WENT OUT. PRIOR TO LANDING, GEAR EXTENDED NORMALLY. ADJUSTED RT MLG AND NOSE UPLOCK SWITCHES TO SPEC IAW CE-750 M/M CHAPTER 32-30-05. ACCOMPLISH GEAR SWITCH AND FREE OPERATIONAL CHECK ALL GOOD. VERIFIED A-SYSTEM PRESSURE IAW CE-750 M/M CHAPTER 29-10-02. OPERATIONAL CHECKS GOOD. 2L72 4J RTT00007WI 20050721000882005072100088NM 2005 7 21 QXEA200501115 120050716A2420 ELECTRICAL SYS BOMBDRDHC8 DHC8402 1390042NM ZONE 100 MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION LDLANDING 1 NM09405QX 4047 RNO - ON FLIGHT 2444, AFTER LANDING NR 1 AC GENERATOR CAUTION LIGHT ILLUMINATED. RESET PER CHECKLIST. RE-ILLUMINATED APPROXIMATELY THREE MINUTES LATER. PROP RPM 600 ON BOTH ENGINES. POWERED AIRCRAFT DOWN, REPOWERED. GROUND RAN AND PERFORMED ADJUSTMENT TEST OF AC POWER SYSTEM. NO PARTS REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050721000892005072100089 2005 7 21 QXEA200501117 420050718A2310CDU3933AE04 DISPLAY BOMBDRDHC8 DHC8402 1390042NM ZONE 100 MALFUNCTIONED A QXEAO OTHER O OTHER CLCLIMB 1 NM09409QX4539 1257 4051 SEA - ON FLIGHT 2383, CAPTAIN'S ARCDU FAILED SHORTLY AFTER TAKEOFF AND REVERTED TO EMERGENCY MODE OF OPERATION. FAILURE SEEMED TO COINCIDE WITH FIRST OFFICERS ATTEMPT TO TRANSMIT TO ATC. CYCLED POWER ON CAPTAINS ARCDU RESTORED NORMAL OPERATION. PROBLEM REOCCURRED TWICE ON APPROACH. REPLACED NR 1 ARCDU. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050721000902005072100090NM 2005 7 21 QXEA200501119 120050718A33506104781 BATTERY DHAV DHC8 DHC8202 2809007NM ZONE 200 MALFUNCTIONED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09365PH123 123 526 PSC - EMERGENCY ESCAPE PATH LIGHTING, 2 RED LIGHTS INOPERATIVE ON TRACK 2. REMOVED AND REPLACED EMERGENCY BATTERY PACK PS6. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050721000932005072100093NM 2005 7 21 P5CA0501377 120050610A3610 CLAMP BOEING747 747283B 1384867NM PWA JT9 JT9D70A 52054NE PNEUMATIC SYS FAILED A P5CAE ENGINE SHUTDOWN MJ OVER TEMP WARNING INDICATION TXTAXI/GRND HDL 1 EA15921FT 21575 689167 CREW REPORTED NR 1 ENGINE FIRE WARNING SOUNDED ON DESCENT. CLOSED THRUST AND START LEVER, LIGHT WENT OUT. FIRE HANDLE WAS NOT PULLED. REPLACED CLAMP TO HIGH STAGE VALVE, MM 36-13-00. OPS AND LEAK CHECK OK MM 71-00-00. 2L74 4F4 F A20WE E3NE 20050721001072005072100107EU 2005 7 21 USAA050796 120050623A5311 FRAME AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19108UW18429 1061 FOUND FRAME CORRODED 6 INCHES BY 2 INCHES, FRAME 66 LEFT AT NUT PLATE HOLES. SPLICE AND DOUBLER REPAIR PER SRM 53-41-14 FIG 201. CORROSION LEVEL 1, TASK JA-26-53500. (M) 2L72 4F RTA28NM 20050721001082005072100108NM 2005 7 21 USAA050839 120050707A575165C252752 BEAM BOEING737 7373B7 1384580NM RT AILERON CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU 23861 CLT - FOUND BEAM CRACKED 1.25 INCH, AFT OF RIGHT AILERON AT TRAILING EDGE. INSTALLED A NEW BEAM IAW SRM 57-51-02. (M) 2L72 4F RTA16WE 20050721001102005072100110CE 2005 7 21 DXTA200500836 120050712A272067604461 BUNGEE CORD CESSNA750 750 2076810CE RUDDER STIFF E DXTAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 GL07900QS4962 7500123 AFTER DEPARTURE, FULL RUDDER TRIM TO LT REQUIRED IN ORDER TO KEEP ACFT COORDINATED. CLIMBING THRU FL 200 AT 250 KIAS, RUDDER KICKED BACK TO NORMAL. HAD TO TRIM RUDDER BACK TO CENTER. OPS CK OF RUDDER SYSTEM ON GROUND REVEALED NO DEFECTS. REMOVED ACCESS PANELS AND PERFORMED VISUAL CHECK OF AREA. NO DEFECTS NOTED. REMOVED RUDDER INPUT BUNGEE AND FOUND BUNGEE STIFF AND STICKING IN COMPRESSED POSITION. REPLACED RUDDER BUNGEE WITH NEW BUNGEE, OPS CK OF RUDDER SYSTEM GOOD. CLOSED ACCESS PANELS. ALL WORK PERFORMED IAW M/M CH 27-24-00. 2L72 4J RTT00007WI 20050721001152005072100115EA 2005 7 21 ASOA05642 120050620A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27826AS 7210 DURING A GROUND INSPECTION IN ATL, FIVE SECTIONS OF EMERGENCY FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE. (M) 2L72 4F RTA21EA 20050721001222005072100122EA 2005 7 21 ASOA05501 120050608A5320BC50393106 COVER CNDAIRCL600 CL6002B19 1900309EA GALLEY CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27830AS 7236 DURING A C-CHECK IN MCN, THE FS 280 LT/RT CLIPS INBOARD AND OUTBOARD WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FS 280 LT/RT CLIPS INBOARD AND OUTBOARD IAW RJ200 SRM 51-42. (M) 2L72 4F RTA21EA 20050721001292005072100129NM 2005 7 21 USAA050794 120050623A5340US415N4112 FITTING BOEING757 757225 1384959NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19606AU65095 22202 BFM - FOUND FITTING CORRODED 4 INCHES BY 3 INCHES BY .100 INCH, STATION 1690, RBL 5 LBL 5. REMOVED AND REPLACED WITH NEW PART PER SRM 53-60-51, 53-00-51. (M) 2L72 4F RTA2NM 20050721001322005072100132EA 2005 7 21 ASOA05509 120050610A5320 SILL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27830AS 7236 DURING A C-CHECK IN MCN, THE CARGO DOOR SILL WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE CARGO DOOR SILL IAW ASA EO 600-53-0117. (M) 2L72 4F RTA21EA 20050721001362005072100136EU 2005 7 21 USAA050791 120050623A5322 SHEAR TIE AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19721UW 1095 PIT - FOUND SHEAR TIE CORRODED 1 INCH BY 1 INCH AREA, BETWEEN FRAME 69 RIGHT, FRAME 70 RIGHT. DEFECTIVE PART REPLACED WITH IDENT PART. CORROSION LEVEL 2, TASK JA-260-53500. (M) 2L72 4F RTA28NM 20050721001452005072100145SO 2005 7 21 RAIA00507005 120050710A3610S2U2226 O-RING EMB 145 EMB145ER 3260211SO BLEED AIR SYSTEMLEAKING A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03808HK 145157 FLT 3505 - PIT - BLEED 2 LEAK INDICATION. MAINTENANCE REMOVED AND REPLACED O-RINGS AT LOCATIONS NR 5, 11, AND 17. 2L72 4F RTT00011AT 20050721001472005072100147SO 2005 7 21 RAIA00507007 120050712A32608005701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212SO MLG MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03813HK 145044 FLT 5493 - STL - LANDING GEAR AIR/GRN FAIL INDICATION. MAINTENANCE REMOVED AND REPLACED PROX SWITCH RT MLG. 2L72 4T RTT00011AT 20050721001582005072100158NM 2005 7 21 SWAA052110 120050719A53126545409 PRESSURE PANEL BOEING737 7373H4 1384600NM MLG WW CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESS WEB CRACKED AT BS 665, RBL 38 & RBL 40. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050721001612005072100161NM 2005 7 21 SWAA052113 120050719A53306546767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29364SW 26575 FUSELAGE SKIN CRACKED AT BS 522, ABOVE STR 19R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050721001622005072100162NM 2005 7 21 SWAA052114 120050719A53306546767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29364SW 26575 FUSELAGE SKIN CRACKED AT BS 520, ABOVE STR 10R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050721001662005072100166EU 2005 7 21 RAIA00507012 120050718A243523095002 STARTER GEN JETAIRJETSTMJETSTM4101 1500501EU ENGINE INOPERATIVE A RAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03566HK10985355 41084 FLT 5449 - STL - RT GENERATOR FAIL WARNING INDICATION. MAINTENANCE REMOVED AND REPLACED NR 2 STARTED GENERATOR. 2L72 4T RTA41NM 20050721001832005072100183NM 2005 7 21 CALA0500217 120050704A53306545774 SKIN BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769351 23589 2.0 IN CRACK IN FUSELAGE SKIN BELOW RT EMERGENCY LIGHT AFT OF WING TO BODY FAIRING, STA 727E, S23R. SKIN REPAIRED IAW ECRA 5330-03461. DIP ISSUED TO REINSPECT REPAIR WITHIN 60,000 CYCLES AND MAKE SUBSEQUENT INSPECTIONS EVERY 25,000 CYCLES. 2L72 4F RTA16WE 20050721001862005072100186NM 2005 7 21 CALA0500219 120050713A53206545875U70 ANGLE BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2719623 27527 INSPECTION FOUND R-1 DOOR CUTOUT Z-ANGLE CORRODED AT STA 294-328, RBL 45. NEW Z-ANGLE INSTALLED IAW SRM 51-40-02. 2L72 4F RTA16WE 20050721001892005072100189NM 2005 7 21 CALA0500222 120050716A5414301A31091 SKIN BOEING737 7373T0 1384582NM NR 1 PYLON CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714334 23572 INSPECTION FOUND 0.5 IN CRACK IN 2 PLACES ON NR 1 ENGINE PYLON SKIN ON EXTERNAL SURFACE ACCESS PANEL NR 5724 CUTOUT. PYLON SKIN REPAIRED IAW ECRA 5430-01204. 2L72 4F RTA16WE 20050721001912005072100191WP 2005 7 21 AALA20050442 120050715A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHTSDISCHARGED A AALAK NONE O OTHER ININSP/MAINT 1 SW2116545 53027 CEILING EMERGENCY LIGHTS CENTER WING SECTION OF CABIN INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS CENTER WING SECTION OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050721001942005072100194WP 2005 7 21 AALA20050441 120050714A3350P4010049 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHTSDISCHARGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21442AA 49468 EMERGENCY PATH LIGHTING AT ROWS 3 THROUGH 20 INOPERATIVE. REPLACED BATTERY PACKS AND CONTROLLERS FOR EMERGENCY PATH LIGHTING AT ROWS 3 THROUGH 20. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050721001962005072100196NM 2005 7 21 AALA20050444 120050717A3397 WIRE BOEING737 737823 13844BZNM EMERGENCY LIGHTSDAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21913AN 29514 FORWARD RT OUTSIDE EMERGENCY LIGHTS INOPERATIVE. REPAIRED WIRING FOR FORWARD RT OUTSIDE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20050721001972005072100197WP 2005 7 21 AALA20050445 120050715A2822 PUMP DOUG DC9 DC982 3022082WP CENTER FUEL INOPERATIVE A AALAA UNSCHED LANDING O OTHER CRCRUISE 1 SW2170504 49798 AFT CENTER FUEL PUMP CIRCUIT BREAKER POPPED AND WAS UNABLE TO RESET. LANDED DTW WITHOUT INCIDENT. REPLACED AFT CENTER FUEL BOOST PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050721002002005072100200NM 2005 7 21 PCSA0719051 120050719A273068000501 PCU BOEING727 727233 138408ANM ZONE 300 MALFUNCTIONED A PCSAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 SO29994AJ 20942 ON TAXI OUT, ACFT ELEVATOR NOSE DOWN STIFF, NOSE UP NORMAL. TAXIED ACFT BACK TO RAMP. VISUAL INSP & TEST OF LT & RT ELEVATOR CABLE SYS & PERFORMED CK OF ELEVATOR CONTROL SYS. OP’S & LEAK CHECK OF ELEVATOR FEEL CONTROL UNIT ACCOMPLISHED, NO DEFECTS NOTED. INSP OF LT & RT ELEVATOR LINKAGES & PUSHRODS IN HORIZONTAL STAB, NO DEFECTS NOTED. INSP REVEALED A FROZEN PULLEY AT FS 280, FROZEN PULLEY LUBED & FREED, OP’S CKD NORMAL. INSP REVEALED LT ELEVATOR PCU HAD A BUMPY FEEL. LT ELEVATOR PCU R & R, OPS & LEAKED CKD NORMAL. INSP OF LT & RT ELEVATOR HINGES ACCOMPLISHED, NO DEFECTS NOTED. LUBED LT & RT ELEVATOR HINGES. ELEVATOR SYS FRICTION TEST. FINAL OPS CK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2L73 4F RTA3WE 20050721002022005072100202NM 2005 7 21 SB05083 120050721A335020131A BATTERY PACK BOEING737 7373B7 1384580NM EMERGENCY LIGHT DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU 23706 PVD MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT OVER THE AFT LEFT ENTRY DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050721002102005072100210NM 2005 7 21 AWXA200500814 120050712A532065479573 WEB BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 FOUND CORROSION ON AFT PIT THRESHOLD WEB FROM BS 787 THROUGH BS 847, STR 25R TOP AND BOTTOM SURFACES. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-30-53-1. MAINTENANCE REMOVED WEB FROM BS 787 THROUGH BS 847, STR 25R AND RECEIVED NEW WEB IAW BOEING DWG 65-47957. PREPPED WEB TO BE INSTALLED IAW BOEING 737-300 SRM 51-40-02-0 FIG 1. INSTALLED NEW THRESHOLD FROM BS 787 THROUGH BS 847, STR 25R WEB IAW BOEING 737-300 SRM 51-40-02-0 FIGS 9 AND 10. 2L72 4F RTA16WE 20050722000172005072200017WP 2005 7 22 UPS05844917 120050627A5730 SKIN DOUG DC8 DC873F 302199FWP NR 2 STUBWING SCRATCHED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 C1 DEEP SCRATCHS IN SKIN L/W UPPER SPAR CAP IB CORNER OF NR 2 STUB WING. SCRATCHS FOUND OUT OF LIMITS, CUT OUT DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1 FIG 26. 2L74 4F RT4A25 20050722000222005072200022WP 2005 7 22 UPS05844923 120050628A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 C1 CRACKED APPROX .5 ON LONG 14 UPPER FLANGE 2ND CANTED FRAME FROM STA 1766 INSIDE MAIN CABIN RT SIDE WALL. REMOVED DAMAGED SECTION OF LONGERON, FABRICATED, AND INSTALLED IAW DC-8 SRM 53-2-2 FIG 10. 2L74 4F RT4A25 20050722000232005072200023WP 2005 7 22 UPS05844924 120050628A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 C1 LONG 16 AT APPROX STA 1745 IS CRACKED AT LWR FRAME TO LONG ATTACH POINT AT RADIUS, (LT CANTED FRAME). REMOVED DAMAGED SECTION OF LONGERON, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 53-2-2 FIG 10. 2L74 4F RT4A25 20050722000272005072200027EU 2005 7 22 05FDEA01899 120050712A5730 ACCESS PANEL AIRBUS310 A310 EU RT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25411FE 359 ACCESS PANEL 650GB HAS 1 ELONGATED HOLE, COMPLIED WITH EA6-5710-90863. 2L72 4F RTA35EU 20050722000292005072200029NM 2005 7 22 AWXA200500818 120050705A52106926552 CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 MCN - MAJOR REPAIR - DURING C16 CHECK FOUND SEVERAL SUB-STRUCTURES DAMAGED ON THE L1 FOWARD ENTRY DOOR CUTOUT SURROUND STRUCTURES. INTERCOSTAL CLIP AT SILL, LOCATED AT BS 350 AND STRINGER 16 RT, CRACKED .30 INCHES IN LENGTH. MAINTENANCE REMOVED CRACKED INTERCOSTAL CLIP AT BS 350, STR 16R. FORMED CLIP IAW AMERICA WEST AIRLINES ENGINEERING REQUEST 03-5301-05193-SS2. PREPPED NEW ANGLE FOR INSTALLATION AT BS 350, STR 16R, SILL IAW AWA ER 03-5301-05193-SS2. INSTALLED FABRICATED REPAIR PARTS AT SILL BS 350 AND STR 16 IAW AWA ER 03-5301-05193-SS2. 2L72 4F RTA16WE 20050722000312005072200031NM 2005 7 22 QXEA200501109 120050713A3150 WARNING LIGHT DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE ENGINES ILLUMINATED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09374PH 528 PCE123077 SEA FLIGHT NR 2298, NR 1, NR 2 ENGINE MANUAL CAUTION LIGHT ILLUMINATED. RESET CIRCUIT BREAKER FOR BETA LOCKOUT. CAUTION WENT AWAY. NO DEFECT NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20050722000402005072200040EA 2005 7 22 SWIA200515293 120050718A2740 TRIM SYSTEM CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07917SW 7641 CAPT STAB TRIM INOPERATIVE. REPLACED CAPT'S TRIM SWITCH. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050722000452005072200045EA 2005 7 22 COMA0560394 120050715A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ILLUMINATED A COMAO OTHER J WARNING INDICATION CRCRUISE 1 SO01786CA 7333 FLIGHT 5456- LEFT THRUST REVERSER UNLOCK CAUTION. DEFERRED MAINTENANCE ON THRUST REVERSER PER MEL 78-30-01. 2L72 4F RTA21EA 20050722000542005072200054 2005 7 22 QXEA200501127 420050719A2210 WARNING LIGHT BOMBDRDHC8 DHC8402 1390042NM ILLUMINATED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09411QX 4055 SEA FLT 2427 WHEN YD WAS SELECTED ON, LIGHTS CAME ON MOMENTARILY THEN WENT OUT AND -YD NOT CENTERED- WAS ILLUMINATED ON BOTH PFD'S. MAINTENANCE NOTES, FAULT UPON ARRIVAL WITH NR 2 ENGINE STILL RUNNING. NO FAULTS IN CDS. FAULT DOES NOT CLEAR, 20 MINUTES AFTER SHUTDOWN FAULT EXTINGUISHES AND DOES NOT RETURN. COMPLIED WITH OPERATIONAL TEST OF YD IAW D8-400 MM TASK 22-11-36-710-801 BEFORE REMOVING POWER FROM AIRCRAFT. OPERATIONAL CHECK GOOD. CYCLED SHIP'S POWER AND AGAIN TESTED YD. OPERATIONAL CHECK AGAIN IS GOOD. NO CAUTION MESSAGES. NO FAULTS IN CDS. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050722000572005072200057EA 2005 7 22 COMA0560395 120050716A2910AE7090052 LINE CNDAIRCL600 CL6002B19 1900309EA LEFT HYD SYS LEAKING A COMAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO01937CA 7044 FLIGHT 5667- NR 1 HYDRAULIC SYSTEM LOW PRESSURE WARNING. REPLACED LEAKING HYDRAULIC LINE. 2L72 4F RTA21EA 20050722000762005072200076EA 2005 7 22 SWIA200515301 120050713A274170609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07983SW9 9 7961 DURING FLIGHT, STAB TRIM AND MACH TRIM CAUTION MESSAGES. REPLACED HSTCU. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050722000812005072200081NM 2005 7 22 AWXA200500837 120050709A532069165004 INTERCOSTAL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED INTERCOSTAL CRACKED .250 INCHES IN LENGTH, LOCATED AT BS 727A TO BS 727B, STR 25R. MAINTENANCE REMOVED INTERCOSTAL AT BS 727A TO BS 727B AND STR 25R IAW BOEING 737-300 SRM 51-40-02-0 FIG 8. RECEIVED AND PREPPED NEW INTERCOSTAL FOR INSTALLATION IAW BOEING 737-300 SRM 51-40-05. INSTALLED REPAIR PARTS AT BS 727A TO BS 727B AND STR 25R IAW BOEING 737-300 SRM 51-40-02-0 FIG 3, 4, 6, 7, AND 8. 2L72 4F RTA16WE 20050722000832005072200083NM 2005 7 22 AWXA200500839 120050707A5312651630086 BULKHEAD BOEING737 7373G7 1384595NM FUSLEAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED 178 BULKHEAD WEB CRACKED AT 4 FASTENERS LOCATED AT WL 234, FROM BL 9L TO BL 13.5L. MAINTENANCE REMOVED DAMAGED AREA ON BULKHEAD WEB IAW BOEING 737-300 SRM 53-10-08. FABRICATED FILLER AND DOUBLER IAW BOEING 737-300 SRM 53-10-08-2 FIG 209. INSTALLED FABRICATED REPAIR PARTS IAW BOEING 737-300 SRM 53-10-08-2 FIG 209. 2L72 4F RTA16WE 20050722000842005072200084NM 2005 7 22 AWXA200500840 120050711A5755655213210 BRACKET BOEING737 7373G7 1384595NM ZONE 600 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED SMALL CRACK LOCATED ON RIGHT WING INBOARD HINGE BRACKET FOR INBOARD GROUND SPOILER. MAINTENANCE REMOVED CRACKED HINGE BRACKET FROM RT WING INBOARD GROUND SPOILER IAW BOEING 737-300 SRM 51-40-02-0 FIG 8. PREPPED NEW HINGE BRACKET FOR INSTALLATION IAW BEOING737-300 SRM 51-10-02-0. INSTALLED R/H WING INBOARD GROUND SPOILER HINGE BRACKET IAW BOEING 737-300 SRM 51-40-02-0 FIGS 3, 4, 8, 12, 13 AND 14. 2L72 4F RTA16WE 20050722000872005072200087NM 2005 7 22 PU3R200500001 120050721A3233273T4118 PISTON BOEING BOEING767 767 UTILUSENM ACTUATOR CRACKED B PU3RO OTHER O OTHER NRNOT REPORTED 1 WP23 6771 PISTON CRACKED AT ROD END. ROD END AND PART OF PISTON ALMOST COMPLETELY SEPARATED FROM THE REST OF THE ACTUATOR. 2L72 4F RTA1NM 20050722000882005072200088WP 2005 7 22 ASMF200507014 120050718A300012294411 ANTI-ICE VALVE DOUG DC9 DC987 3022087WP FAILED W ASMFBA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW23216AM8400 49586 ACFT PERFORMED AN UNSCHEDULED LANDING DUE TO PRESSURIZATION FAILURE, AFTER 45 MIN OF USING ANTI-ICE, AT 350 FLT LEVEL, FLOW & CABIN ALT LIGHT TURNED ON. CAPTAIN ACCOMPLISHED THE ABNORMAL PROCEDURE & PERFORMED AN UNSCHEDULED LANDING. DURING REVISION OXYGEN GENS DETECTED ACTIVED, WINGS & TAIL ANTI-ICE VALVES OPS TESTED CORRECT. PRESSURIZATION & ANTI-ICE TEST PERFORMED IN MANUAL AND AUTO MODE IAW MM. THE OXYGEN GENS DEFERRED & ACFT FLEW TO MEX. DURING OVERNIGHT CHECK, PRESSURIZATION & ANTI-ICE TEST WERE PERFORMED IN MANUAL AND AUTO MODE IAW MM, OXYGEN GENS REPLACED IAW MM & WING ANTI-ICE VALVE REPLACED IAW MM, TESTED CORRECT. DEFERRED REPORT WAS CLOSED. 2L72 4F RTA6WE 20050722000892005072200089NM 2005 7 22 ASMF200507015 120050718A361012911021 THERMOSTAT DOUG MD80 MD83 3023681NM LEFT FAILED W ASMFA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW23881LF12249 53051 THE AIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT HERMOSILLO (HMO) DUE TO LEFT ICE PROTECT TEMP HIGHT LIGHT TURNED ON AND USTB LEGEND IN RADAR COME ON SEVERAL TIMES. THE LEFT PNEUMATIC SYSTEM THERMOSTAT AND ANTICIPATOR WERE REPLACED IAW MM 36-10-06 AND TRANSCEIVER WX RADAR WAS REPLACED IAW 34-41-04, TESTED CORRECT. 2L72 4F RT 20050722000952005072200095SW 2005 7 22 AC2A100890 120050513A5410427065316108 STRUT BELL 427 427 1182207SW NR 2 ENGINE CHAFED B AC2AK NONE O OTHER ININSP/MAINT 1 SO07427CK428 56043 CHAFED ON NR 2 ENGINE EXHAUST BLANKET/ REPLACED STRUT ASSY. AND APPLIED HIGH TEMP RTV TO BLANKET AS PER BELL 1G71 3U R00001RC 20050722000982005072200098NE 2005 7 22 TSAA0575029 220050712A7532 BLEED VALVE BOEING737 7372Y5 1384554NM PWA JT8 JT8D9A 52048NE NR 2 ENGINE DEFECTIVE A TSAAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP13810AL 24031 RUNNING UP ENGINES FOR TAKE-OFF, GOT STEADY BANGING. RPM BARELY PAST IDLE. FLIGHT ATTENDANTS GUESS THE NR 2 ENGINE. TAKE-OFF ABORTED. R&R PRBC IAW MM 75-31-11 OPS CHECK OK ON NR 2 ENGINE. BLEED VALVE SCHEDULING COMPLETED PER PWA MM 72-00-00. LUBED 8TH AND 13TH STAGE BLEED VALVES ON NR 1 AND 2 ENGINES PER PWA MM 75-30-00. NO FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4U4 FRTA16WE E2EA 20050722000992005072200099NM 2005 7 22 05FDEA01758 120050701A5510ALC80552 BULKHEAD DOUG MD11 MD11 3023602NM ZONE 300 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25619FE 48770 EMPENNAGE, TO TRIM RIGHT HAND OPERATING BULKHEAD FOR NR 35R BARREL NUT BORE REWORK ACCESS. RT OPERATING BULKHEAD TRIMMED OUT AS PER SRM 51-31-01 VOL II AND FOUND EXCEEDED LIMIT AS PER FEDEX EO NR 1-5510-7-5000. REPAIR CARRIED OUT ON TRIMMED AREA AT RT OPERATING BULKHEAD AS PER FEDEX EA NR 1-5510-87552. THIS REPAIR IS CLASSIFIED MAJOR PER GMM 6-2-100. 2L73 4F RTA22WE 20050722001002005072200100NM 2005 7 22 AWXA200500825 120050718A2131 SWITCH BOEING737 7373S3 1384711NM PRESS CONTROLLERFAILED A AWXAGA O2 MASK DEPLOYED UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP28312AW52939 24060 DURING FLT AUTO FAIL LIGHT ON PRESSURE CONTROLLER ILLUMINATED WITH CABIN HORN COMING ON. SWITCHED TO STANDBY AND DESCENDED. MASKS DID DEPLOY. EMERGENCY NOT DECLARED AND AIRCRAFT LANDED IN LAS WITHOUT FURTHER INCIDENT. MX TROUBLESHOT AND FOUND AIR/GROUND SWITCH ON PRESSURE CONTROLLER PANEL TO BE BAD. R & R PRESSURE CONTROLLER PANEL, P5-6, IAW BOEING 737-300 MM 21-31-25-4. OPS CHECKS GOOD IAW AMWEST TASK CARD F1B21001. VENDOR REPORTED, VIA EMAIL, THAT UNIT PASSED INCOMING TESTS. TEAR DOWN REPORT SHOWS THAT UNIT WAS TESTED AND OVERHAULED, FOR PRECAUTIONARY PURPOSES, IAW CMM 21-31-00 REV 33. OPS TESTS ON UNIT GOOD. 2L72 4F RTA16WE 20050722001022005072200102EU 2005 7 22 AWXA200500830 120050718A2560P4010021000 BATTERY AIRBUS320 A320232 3930326EU FLASHLIGHT DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28604AW 1196 LAS - EES - DURING 4 DAY CHECK, FOUND THE AFT RT EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT RT EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA28NM 20050722001042005072200104NM 2005 7 22 AWXA200500832 120050716A3150 WARNING SYSTEM BOEING737 7373S3 1384711NM FALSE ACTIVATIONA AWXAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 WP28316AW 23713 DURING TAKEOFF RECIEVED TAKEOFF CONFIGURATION WARNING. ABORTED TAKEOFF. CREW TAXIED BACK AND DEPARTED NORMALLY. AWAITING SAFTEY EVENT REPORT, FROM PILOT, TO DETERMINE CAUSE OF T/O CONFIG WARNING AND SPEED THAT AIRCRAFT ABORTED T/O AT. THIS IS THE SECOND OCCURANCE OF A TAKEOFF CONFIGURATION WARNING WITH 72 HOURS, A FUP IS BEING GENERATED TO ADDRESS THIS ISSUE. FUP COMPLIED WITH & NO DEFECTS NOTED. RECIVED REPORT FROM PILOT. STATES THAT AFTER APPLYING T/O POWER RECIEVED CONFIG HORN, HADN'T EVEN BEGAN TO ROLL YET. AFTER THROTTLING BACK & PULLING OFF THE RUNWAY SAW SPEED BRAKE HANDLE SLIGHTLY ELEVATED. RESET SPEEDBRAKE HANDLE & ATTEMPTED T/O AGAIN. T/O WAS UNEVENTFUL. PILOT ERROR. 2L72 4F RTA16WE 20050722001052005072200105 2005 7 22 2005000005 420050522A34144039891903 INDICATOR BOEING757 75728A 1384976NM COCKPIT FAILED A CNMAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SW07369AX 28161 CAPTIANS AIRSPEED FAILED TO RISE ON TAKEOFF ROLL REJECTED T/O AT 100 KNOTS. REPLACED CAPTIANS AIRSPEED INDICATOR PER AMM 34-13. 2L72 4F RTA2NM 20050722001072005072200107NM 2005 7 22 2005000007 120050604A7700144957000 ACCELEROMETER BOEING757 75728A 1384976NM ENGINE FAULTY A CNMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW07459AX 25621 N1 ENG VIB HIGH ON CLIMB OUT (YELLOW) READ 2.7, ENG INDICATIONS NORMAL. VIBRATION RETURNED BELOW 2.5 WITH THRUST LEVER RETARDED ENG WAS NOT SHUT DOWN. TROUBLE SHOT ENG VIBRATION PER 757 FIM 77-31-00 RT ENG VIBRATION CONTROLLER BOX HAD FAULT CODE B8 DISPLAYED. REMOVED AND REPLACED ACCELEROMETER PER MM 77-31-01. PERFORMED ENG VIB OPS CHECKS OK. 2L72 4F RTA2NM 20050722001102005072200110WP 2005 7 22 UPS05844927 120050628A532237558271N FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 DURING X-RAY INSPECTION AND VERIFIED BY HFEC, A CRACK WAS FOUND ON ZEE FITTING, STA 340, BETWEEN LONG 30-31R. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20050722001122005072200112WP 2005 7 22 UPS05844929 120050630A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE: C1, STA 1756 L4R CRACKED .250 INCH LONG. REMOVED DAMAGED SECTION OF LONGERON, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 53-2-2 FIG 10. 2L74 4F RT4A25 20050722001132005072200113WP 2005 7 22 UPS05844930 120050630A53405894282502 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE: C1, CRACKED FITTING APPROX 2 INCHES ON LONGERON 32R STA 1200 C-PIT ENTRY WAY. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20050722001142005072200114WP 2005 7 22 UPS05844931 120050629A5230 SKIN DOUG DC8 DC873F 302199FWP CARGO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE:C1 C-PIT DOOR LOWER AFT CORNER REPAIR DOUBLER IS NOT PER SRM 53-2-0 FIG 22 AND THERE IS A CRACK IN THE REPAIR FILLER. REMOVED EXISTING REPAIR, CUT OUT DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0 FIG 22. 2L74 4F RT4A25 20050722001152005072200115WP 2005 7 22 UPS05844933 120050720A2910 HYDRAULIC SYSTEM DOUG DC8 DC871F 302199DWP LEAKING A IPXAO OTHER KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO01702UP 45902 ATB - HYDRAULIC FLUID LOSS, EMERGENCY DECLARED. FOUND LEFT MAIN GEAR DOWNLOCK BUNGEE CYLINDER PRESSURE LINE LEAKING/ DAMAGED. R/R LINE PER MM 30-12-2. SVCD HYD SYSTEM PER MM 12-30-01-3 LEAK CK O.K. 2L74 4F RT4A25 20050722001172005072200117NM 2005 7 22 05FDEA01989 120050718A5310 DOOR FRAME BOEING727 727227 1384078NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 E-BAY BODY DOOR FRAME AT BS 449 LBL 2-RBL 2 CORRODED. REPLACED E-BAY BODY DOOR FRAME AT BS 449, PER SRM 51-30-2 AND 51-10-3 AND 51-30-5 2L73 4F A3WE 20050722001182005072200118NM 2005 7 22 05FDEA01961 120050715A5310ACA7106505 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 MAIN DECK CARGO COMPARTMENT, FLOOR SEAT TRACK AT STA 635, X= -27 FOUND WITH CRACKED APPROXIMATELY 3 INCHES LONG. REPAIRED AS PER SRM 53-70-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2L73 4F RTA22WE 20050722001222005072200122NM 2005 7 22 AWXA200500823 120050629A53156545808179 FLOORBEAM BOEING737 7373G7 1384595NM FUSLEAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 DURING C16 CHECK DISCOVERED CORROSION ON THE TOP OF FLOORBEAM, UPPER CHORD AT BS 294, BL 16.7, AND WL 208, WAS PREVIOUS BLEND OUT. AFTER REMOVAL OF CORROSION, MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-10-51-1 FIG 101. REMOVED FLOORBEAM UPPER CHORD SECTION AT BS 294 FROM BL 60R TO BL 20L IAW BOEING 737-300 SRM 51-40-02-0. FABRICATED UPPER CHORD SECTION IAW BOEING 737-300 SRM 51-40-05-0 FIG 2 AND 53-10-51-2 FIG 205. INSTALLED FABRICATED REPAIR PARTS AT BS 294, WL 208, FROM BL 60R TO BL 20L IAW BOEING 737-300 SRM 51-40-02-0 FIG 12 AND 53-10-51-2 FIG 205. 2L72 4F RTA16WE 20050722001242005072200124NM 2005 7 22 AWXA200500826 120050629A531465C385023 KEELBEAM BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 PHX - MAJOR REPAIR - DURING 8 DAY CHECK REPORTED CENTER KEEL BEAM PANEL BULGING WITH PULLED FASTENERS LOCATED AT STA 582, JUST RIGHT OF CENTER TANK SUMP ACCESS PANEL. MAINTENANCE BLENDED OUT CORROSION AT KEEL BEAM RT SIDE STA 576-582, BL 6.5R. INTERGRANULAR CORROSION ON LOWER KEEL BEAM VERTICAL LEG IS OUT OF SRM LIMITS IAW BOEING 737-300 SRM 53-60-12. REMOVED AND INSTALLED NEW SECTION OF KEEL BEAM FROM STA 520-625 IAW BOEING 737-300 SRM 53-60-12 FIG 203. 2L72 4F RTA16WE 20050722001252005072200125 2005 7 22 AWXA200500827 420050716A3420 ADIRU AIRBUSA319 A319132 3930340NM NR 2 FAILED A AWXAC ABORTED TAKEOFF GJ MULTIPLE FAILURE WARNING INDICATION TOTAKEOFF 1 WP28805AW 1049 DURING TAKEOFF RECEIVED MULTIPLE FAULTS BEGINNING TAKE OFF ROLL. ACFT ABORTED T/O & RETURNED TO GATE WITHOUT INCIDENT. MX R & R FAC 1 IAW AMWEST TASK CARD R2A22301. OPS TESTS GOOD. ATTEMPTED ANOTHER TAKEOFF & RECEIVED AUTO FLT RUD TRV LIM SYS ECAM MSG DURING TAKEOFF ROLL. AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MX R & R NR 2 ADIRU IAW AMERICA WEST AIRLINES TASK CARD R2A34304. OPS TESTS GOOD. VENDOR TEAR DOWN REPORT CONFIRMS FAILURE. VENDOR INCOMING TESTS SHOWS PRIMARY FAULT OF GYRO. GYRO WAS REPLACED WITH ALL WORK AND OPERATIONAL TESTS BEING DONE IAW AT261847-01, CMM TP1011 REV 24. 2L72 4F RTA28NM 20050722001272005072200127EU 2005 7 22 0501033247 120050717A2530 CONTROLLER AIRBUS320 A320212 3930322EU OVEN FAILED A NWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL01347NW 408 DURING CLIMB, A BURNING ODOR WAS NOTED IN THE COCKPIT AND SMOKE/HAZE REPORTED IN CABIN. DECLARED YELLOW EMERGENCY AND RETURNED TO MEM AND LANDED UNEVENTFULLY. FOUND ROW 25 LEFT OVERHEAD FLUORESCENT LAMP INOP. FOUND NO EVIDENCE OF BURNED PINS. RELAMPED AND CHECKED OK. NOTED BURNED CONNECTOR PIN ON NR 1 OVEN CONTROLLER. REPLACED NR 1 OVEN CONTROLLER AND CHECKED GOOD. REPLACED AVIONICS VENTILATION FILTER. PRESSURIZED AIRCRAFT, RAN ALL ELECTRICS AND LIGHTS, CHECKED OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA28NM 20050722001282005072200128EU 2005 7 22 2005UALA00644 120050711A3230664700500A4D CONTROLLER AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE MLG FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29431UA 571 NR 1 LGCIU FAULT FOLLOWED BY LOSS OF VH2 RADIO AND THRUST REVERSER. LGCIU FAULT DISPLAYED DURING CRUISE. ACP LGCIU SYSTEM GRND TEST REF MM 32-69-00. TEST OKNO FAULTS FOUND. 2L72 4F4 FRTA28NM E40NE 20050722001292005072200129NM 2005 7 22 2005UALA00645 120050711A335020131A BATTERY PACK BOEING737 737322 1384676NM DOOR 1R DISCHARGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29343UA 24247 EXTERIOR EMERGENCY LIGHT NEXT TO DOOR 1R WON`T ILLUMINATE. BATTERY PACK NOT HOLDING CHARGE. REPLACED OK. 2L72 4F RTA16WE 20050722001302005072200130NM 2005 7 22 2005UALA00646 120050620A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE LIGHTNING STRIKEA UALAK NONE O OTHER ININSP/MAINT 1 WP29574UA 26686 TOP OF FUSELAGE HAS 2 LIGHTNING STRIKES. REMOVED DAMAGE AND MANUFACTURED REPAIR REF SRM 53-00-01. 2L72 4F4 FRTA2NM E17NE 20050722001312005072200131NE 2005 7 22 2005UALA00647 220050711A7200 ENGINE BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE NR 2 OVERHEATED A UALAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION NRNOT REPORTED 1 WP29657UA 27112 724633 RETURNED TO THE FIELD DUE TO HIGH OIL TEMPERATURE ON NR 2 ENGINE. REPLACED FUEL/OIL COOLER BYPASS VALVE SOLENOID. TESTED OK AFTER REPLACEMENT. 2L72 4F4 FRTA1NM E24NE 20050722001362005072200136NM 2005 7 22 2005UALA00652 120050712A3350362624 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT BURNED OUT A UALAK NONE O OTHER ININSP/MAINT 1 WP29178UA 24385 EEL LIGHTS INOP AT ROW 58 LT, ROW 35 LT, LT MID GALLEY, ROW 56 RT, ROW 4A AFT SECTION, ROW 5F AFT SECTION. EEL LIGHTS BURNED OUT, REPLACED OK. 2L74 4F4 FRTA20WE E24NE 20050722001392005072200139NM 2005 7 22 2005UALA00655 120050627A2121 FAN BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN FAILED A UALAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 WP29519UA 24872 STRONG ODOR IN REAR OF CABIN ON TAXI OUT. RIGHT RECIRC FAN FAILED. DEFERRED PER MEL, THEN REPLACED FAN. OPS CHECK OK. RETURNED AIRCRAFT TO SERVICE. 2L72 4F4 FRTA2NM E17NE 20050722001402005072200140EU 2005 7 22 2005UALA00656 120050713A3350321454 EPSU AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE ROW 12, 13, 14, INOPERATIVE A UALAO OTHER L NO TEST ININSP/MAINT 1 WP29436UA 638 SEAT MOUNTED EMERGENCY LIGHTS INOP AT SEATS 12,13, 14, 18, 19 AND 20. POWER SUPPLIES LOW CHARGE, REPLACED. 2L72 4F4 FRTA28NM E40NE 20050722001412005072200141NM 2005 7 22 2005UALA00657 120050713A4900 APU BOEING757 757222 1384956NM PWA 2037 PW2037 NE APU BAY INOPERATIVE A UALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 WP29596UA 28749 RETURNED TO THE FIELD AT SFO AFTER THE APU WOULD NOT START AT TOP OF CLIMB. APU WAS REMOVED FROM AIRCRAFT AND TESTED IN APU TEST CELL. NO FAULT FOUND WITH APU S/N 61832. PASSED ALL TEST AND RETURNED TO SERVICE. AFTER APU REPLACEMENT, MECHANIC FOUND APU BATTERY LOW AND APU BATTERY CHARGER CIRCUIT BREAKER BROKEN. APU BATTERY WAS REPLACED AND OPERATION CHECKED OK. 2L72 4F4 FRTA2NM E17NE 20050722001432005072200143NM 2005 7 22 2005UALA00659 120050713A3397210013 CONNECTOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE EMERGENCY LIGHT BROKEN A UALAK NONE O OTHER ININSP/MAINT 1 WP29504UA 24625 EEL TEST SWITCH ABOVE 2L DOOR BROKEN CONNECTOR. BROKEN CONNECTOR ON EEL TEST SWITCH. REPLACED SWITCH. 2L72 4F4 FRTA2NM E17NE 20050722001442005072200144NM 2005 7 22 2005UALA00660 120050713A335020131A POWER SUPPLY BOEING757 757222 1384956NM PWA 2037 PW2037 NE EMERGENCY LIGHT DISCHARGED A UALAO OTHER O OTHER NRNOT REPORTED 1 WP29542UA 25276 EMERGENCY LIGHTS INOP AT FOLLOWING LOCATIONS: AISLE LIGHT IN BULLNOSE AT ROW 25, CEILING EXIT SIGN AT ROW 16 AND EXTERIOR SLIDE LIGHT ON AFT CARGO DOOR. POWER SUPPLIES LOW CHARGE, REPLACED. 2L72 4F4 FRTA2NM E17NE 20050722001452005072200145NM 2005 7 22 2005UALA00661 120050715A5322 SHEAR TIE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29504UA 24625 SHEAR TIES AT FUSELAGE STA 600 STR 16L-18L HAS OVERSIZE FASTENER HOLES. FABRICATE AND REPLACE SHEAR TIES PER TIMCO EA REO-G10727 AND MM 51-40-02. 2L72 4F4 FRTA2NM E17NE 20050722001472005072200147NM 2005 7 22 2005UALA00663 120050714A2910 PACKING BOEING757 757222 1384956NM PWA 2037 PW2037 NE HYD SYSTEM LEAKING A UALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP29509UA 24763 RETURNED TO FIELD DUE TO INDICATION OF LOSS OF HYDRAULIC FLUID. HYDRAULIC FLOW LIMITER PACKINGS WERE LEAKING AT THE UNIONS, THE PACKINGS WERE REPLACED. THE LEFT HYDRAULIC SYSTEM WAS SERVICED AND LEAK CHECKED OK. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA2NM E17NE 20050722001482005072200148NM 2005 7 22 05FDEA01997 120050719A5322 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 N00923 AFT CARGO FRAME SHEAR TIE IS CORRODED BS 1130 LBL 9. FABRICATED DRILLED ALODINED AND INSTALLED SHEAR TIE REPAIR PER SRM 53-10-4 2L73 4F RTA3WE 20050722001492005072200149NM 2005 7 22 05FDEA01998 120050719A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 N01117 FUSELAGE UPPER LOBE, IS CHAFED ON INNER FLANGE , BS 1030, STR 9L. CUT OUT DAMAGE ON FRAME INNER FLANGE AT BS 1030 STR 9L AND INSTALLED REPAIR PARTS PER SRM 51-40-3. 2L73 4F RTA3WE 20050722001502005072200150NM 2005 7 22 05FDEA02015 120050721A5340 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 WHILE WORKING NR00631 FOUND STRINGER CLIP AT BS 540 STR 22R CRACKED. REPLACED STRINGER CLIP PER SRM 51-30-2. 2L73 4F RTA3WE 20050722001512005072200151 2005 7 22 05FDEA02010 420050721A3418 SENSOR DOUG DC10 DC1010 3022110WP NR 2 AOA MALFUNCTIONED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO2568053 47807 AFTER T/O WHEN WE WERE RETRACTING SLATS WE GOT THE STICK SHAKER STALL WARNING & FLASHING SLAT RESET LIGHT. RETURNED TO SLATS EXTEND THE WARNING STOPPED HAD TO FLY WITH SLATS EXTENDED AND RETURNED TO IND, NORMAL CONFIGURATION LANDING. PERFORMED AT/SC TEST FOUND AT/SC BAD & AOAS VANE BAD. CHANGED NR 2 AOA SENSOR. 2L73 4F A22WE 20050722001522005072200152NM 2005 7 22 05FDEA02011 120050721A5311 FRAME BOEING727 727200 138407ENM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 AFT CARGO FRAME IS GOUGED TOP OF FRAME AT NUTPLATE HOLE BS 1148 BETWEEN STR 25L-26L. REPAIRED AFT CARGO FRAME AT NUTPLATE HOLE BS 1148 STR 25L-26L IAW SRM 51-30-2, 53- 10-1, 51-40-3. 2L73 4F RTA3WE 20050722001532005072200153NM 2005 7 22 05FDEA02012 120050721A5340 STRINGER CLIP BOEING727 727200 138407ENM FUSLAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 FUSELAGE UPPER LOBE STRINGER CLIP IS CRACKED BS 950B STR-6R. REMOVED AND REPLACED UPPER LOBE STR. CLIP BS 950B, STR 6R IAW SRM 51-30-2. 2L73 4F RTA3WE 20050722001542005072200154NM 2005 7 22 05FDEA02013 120050721A5340654531314 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 FUSELAGE UPPER LOBE, STRINGER CLIP IS CRACKED, BS 950D, STR 9R. REPLACED STRINGER CLIP PER SRM 51-30-2. 2L73 4F RTA3WE 20050722001552005072200155NM 2005 7 22 05FDEA02014 120050721A5320 FLOOR SUPPORT BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 FUSELAGE UPPER LOCE, LONGITUDINAL FLOOR SUPPORT, HAS CORROSION ON I/B AND O/B UPPER FLANGES, UNDER NUT PLATES FROM BS 760 TO 850, LBL 25. REPLACED BEAM PER SRM 51-30-2. 2L73 4F RTA3WE 20050722001562005072200156NM 2005 7 22 CALA0500230 120050720A5320147A57104 FLOOR SUPPORT BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2726215 28775 INSPECTION FOUND AFT GALLEY FLOOR SUPPORT AFT OF RT GALLEY MOUNT CORRODED AT STA 986.5 TO 1016. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND BOEING DRAWING 3147A5710. 2L72 4F RTA16WE 20050722001572005072200157NM 2005 7 22 CALA0500231 120050721A5320141A54105 INTERCOSTAL BOEING737 737824 13844BZNM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2726215 28775 INSPECTION FOUND A 1 INCH CRACK AT FASTENER HOLE IN INTERCOSTAL BETWEEN STA 312 AND 328, RBL 30. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20050722001582005072200158NM 2005 7 22 CALA0500232 120050721A5320141A541010 INTERCOSTAL BOEING737 737824 13844BZNM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2726215 28775 INSPECTION FOUND A 1 INCH CRACK AT FASTENER HOLE IN INTERCOSTAL BETWEEN STA 270-294, RBL 2. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 511-20-01 AND 51-40-02. 2L72 4F RTA16WE 20050722001592005072200159NM 2005 7 22 CALA0500233 120050721A5320141A541012 INTERCOSTAL BOEING737 737824 13844BZNM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2726215 28775 INSPECTION FOUND A 1 INCH CRACK IN INTERCOSTAL BETWEEN STA 312 AND 320, LBL 64, NEAR L-1 DOOR. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-20-01 AND SRM 51-40-02. 2L72 4F RTA16WE 20050722001602005072200160NM 2005 7 22 CALA0500234 120050721A5320141A541012 INTERCOSTAL BOEING737 737824 13844BZNM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2726215 28775 INSPECTION FOUND A 1 INCH CRACK IN INTERCOSTAL BETWEEN STA 328 AND 344 NEAR L-1 DOOR. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20050722001612005072200161NM 2005 7 22 05FDEA02016 120050721A5340 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 FUSELAGE UPPER LOBE STRINGER CLIP IS CRACKED BS 950C STR-3R. REPLACED STRINGER CLIP BS950C STR 3R IN UPPER FUSELAGE PER SRM 51-30-2, 51-10-2, 51- 20-1, 51-30-5, 51-30-6. 2L73 4F RTA3WE 20050722001622005072200162EU 2005 7 22 05FDEA01996 120050719A7797 WIRE HARNESS AIRBUS310 A310 EU PWA JT9 JT9D* NE EGT CHAFED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25456FE 318 716121 ENG NR 2 EGT ANALOG INDICATION CONSTANTLY SWINGS BETWEEN 440 DEG C TO 460 DEG C IN CRZ. NR 1 EGT STABLE AT 450 DEG C. ENG NR 2 EGT INDICATION ERRATIC AS WELL DURING APPROACH. T/S IN PROGRESS. PERFORMED T/S ACC TO TSM 77-21-00 AND AMM 77-21-03-5-A. FOUND EGT HARNESS CHAFING WITH COWLING AT POSITION 6 O'CLOCK. TEMPORARY REPAIRED WITH ELEC PLASTIC TA PE IAW ESMP. NR 2 ENG RUN UPPER JRH ALL PARAMETERS READ NORMAL BY AMT 418749. NR 2 ENG COWLING OPENED/CLOSED PER AMM 71-13-00. 2L72 4F4 FRTA35EU E20EA 20050722001632005072200163EU 2005 7 22 05FDEA01999 120050719A7830 ANGLE AIRBUS300 A300F4605R 3930327EU TRUST REVERSER CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25656FE 632019 745 NR 1 ENG TRUST REVERSER ASSY INNER BODY LWR ANGLE CHAFED. 2L72 4F RTA35EU 20050722001642005072200164NM 2005 7 22 05FDEA01903 120050713A5744 HINGE DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 LT WING-O/B FLAP I/B HINGE (WING SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 PG 602-607. FABRICATED BUSHING AND INSTALLED AS PER EA 1-5750-87605. 2L73 4F RTA22WE 20050722001652005072200165NM 2005 7 22 05FDEA01904 120050713A5744 HINGE DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 LEFT WING-O/B FLAP I/B HINGE (WING SIDE), ACTUATOR ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 PG 602-607. REPAIR CARRIED OUT AS PER EA 1-5750-87605. 2L73 4F RTA22WE 20050722001662005072200166NM 2005 7 22 05FDEA01905 120050713A5744 HINGE DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 LT WING-O/B FLAP I/B HINGE (WING SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 PG 602-607. FABRICATED BUSHING AND INSTALLED AS PER EA 1-5750-87605. 2L73 4F RTA22WE 20050722001682005072200168NM 2005 7 22 05FDEA01907 120050713A5744 HINGE DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 LT WING-O/B FLAP I/B HINGE (WING SIDE), LWR ATTACHMENT SPOT FACE FOUND CORRODED. REPAIR CARRIED OUT IAW EA 1-5750-87605. 2L73 4F RTA22WE 20050722001722005072200172NM 2005 7 22 05FDEA01911 120050713A5315 FLOORBEAM DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 AT STA 1821 ALONG LBL 10 TO LBL 25.5 FLOORBEAM STRUCTURE FOUND CORRODED. DISCREPANT FLOOR SUPPORT REMOVED, NEW FLOOR SUPPORT REWORKED FROM S2929169X7075T6511 AS PER DRAWING AGA 3814 AND INSTALLED AS PER SRM 51-31-01 VOL II. CLASSIFIED MINOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050722001742005072200174NM 2005 7 22 05FDEA01913 120050713A5315 FLOORBEAM DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 CABIN, AT STA 1986 ALONG LBL 1 TO LBL 19 FLOOR SUPPORT STRUCTURE FOUND CORRODED. 2L73 4F RTA22WE 20050722001762005072200176NM 2005 7 22 CALA0500224 120050718A53206546547108 FRAME BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714334 23572 INSPECTION FOUND STA 727 BULKHEAD FRAME FLANGE CORRODED BETWEEN LEFT AND RIGHT KEELBEAM AS SEEN FROM AFT CARGO COMPARTMENT, LBL 6.3. REPAIRED IAW ECRA 5311-01232. 2L72 4F RTA16WE 20050722001782005072200178NM 2005 7 22 CALA0500226 120050719A5347140N20692 SEAT TRACK BOEING757 757224 1384958NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713110 27300 INSPECTION FOUND O/B SEAT TRACK CORRODED AROUND NUT PLATE HOLES BETWEEN STA 760 AND 780, RBL 36. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-20-01 AND 51-40-02. 2L72 4F RTA2NM 20050722001812005072200181NM 2005 7 22 QXEA200501108 120050717A2120 ODOR DHAV DHC8 DHC8202 2809007NM COCKPIT DETECTED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM09362PH 518 SEA FLIGHT NR 2108, WHEN CREW PICKED UP THE AIRCRAFT, UPON OPENING THE DOOR THERE WAS AN OVERPOWERING ODOR OF SOMETHING ROTTEN. MAINTENANCE INSPECTED INTERIOR OF AIRCRAFT, COCKPIT, CABIN AND BAGGAGE PIT. CLEANED FLOOR VINYL COVERING IN COCKPIT, GALLEY AND LAVATORY AREAS. VENTILATED AIRCRAFT WITH GROUND FAN AND MAIN CABIN DOOR, CABIN TO BAGGAGE PIT DOORS OPEN FOR 30 MINUTES. NO OTHER DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050722001842005072200184EA 2005 7 22 SWIA200515282 120050714A2750 PDU CNDAIRCL600 CL6002C10 1390015EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07719SK 10188 FLAPS FAIL CAUTION MESSAGE ON GROUND. REPLACED FLAP PDU IAW MM 27-52-37. OPERATIONAL CHECK GOOD, PN 766359B, SNOFF 0543. 2L72 4F RTA21EA 20050722001862005072200186SO 2005 7 22 SWIA200515284 120050713A3397 CONTACTOR EMB 120 EMB120ER 3260203SO EMERGENCY LIGHTSMALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07271YV 120271 EMERGENCY LIGHTS STAY ON AFTER FA'S TEST. REPLACED EMERGENCY BUSS CONTACTOR NR 2 K0519. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050722001892005072200189EA 2005 7 22 SWIA200515287 120050716A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLIGHT SPOILER MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07449SW4442 4442 7699 "SPOILERONS FAULT" STATUS MESSAGE DISPLAYED PRIOR TO TAKEOFF. REPLACED RIGHT OUTBOARD SPOILERON PCU. OPERATIONAL CHECK GOOD IAW MM 27-62-01. 2L72 4F RTA21EA 20050722001912005072200191EA 2005 7 22 SWIA200515289 120050715A5210601R317659 LOCK CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07916SW 7634 MAIN CABIN DOOR WILL NOT OPEN FROM INSIDE CABIN. REPLACED LATCH LOCK ASSY IAW MM 52-11-25. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050722001922005072200192EU 2005 7 22 F3LA200500032 120050715A21312079002AC CONTROLLER AIRBUSA318 A318111 3940019EU CABIN PRESSURE UNSERVICEABLE A F3LAG O2 MASK DEPLOYED J WARNING INDICATION CLCLIMB 1 NM03803FR 2521 2017 FLT CREW REPORTED CABIN PRESSURIZATION FLUCTUATING FOLLOWED BY NR 2 CONTROLLER FAILURE. ECAM EXCESS CABIN ALT. AT APPROX 30,000 FT & CLIMBING. NOTICED CABIN ALT SHOWING IN EXCESS OF 29,000 FT, CABIN MODE NR 1 CONTROLLER LATER ASSUMED CONTROL & CABIN PRESSURE RETURNED TO BELOW 10,000 FT. CABIN O2 MASKS DID NOT AUTOMATICALLY DROP. MANUALLY DEPLOYED OXYGEN MASKS FROM FLT DECK. DECLARED AN EMERGENCY & PERFORMED AN OVERWEIGHT LANDING PER CHECKLIST. LANDING NORMAL. REPLACED PRESSURE CONTROLLER 11 HL PER LEAK LESS THAN 0.78 PSI/MIN. PERFORMED FUNCTIONAL CHECK OF AUTOMATIC MASK RELEASE PER AMM 35-23-00-720-003. OPS CHECK NORMAL. 2L72 4F RT 20050722001972005072200197 2005 7 22 HCM2005F00000 420050722A31970301057900 WIRE HARNESS SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE CHIP DETECTOR INTERMITTENT E HCMAO OTHER O OTHER NRNOT REPORTED 1 WP13193BH 2894 PILOT EXPERIENCED AN ENGINE CHIP LIGHT INDICATION. HE CHOSE TO MAKE LANDING. UPON INVESTIGATION BY THE MECHANIC, A SMALL SILVER OF METAL WAS FOUND. THE PLUG WAS CLEANED. THE SYSTEM WAS FLUSHED AND THE OIL FILTER WAS INSPECTED WITH NO EVIDENCE OF METAL AND REPLACED. FOLLOWING GROUND RUN AFTER MAINTENANCE PRESENTED AN ADDITIONAL ENGINE CHIP LIGHT INDICATION WITH NO EVIDENCE OF METAL. ENGINE CHIP PLUG WIRING HARNESS WAS REPLACED. THE AIRCRAFT WAS GROUND RUN AND FLIGHT CHECKED WITH NO FURTHER INCIDENCE. (K) 1G71 3U3 U H9EU E19EU 20050722001992005072200199NM 2005 7 22 P5CA0501380 120050720A21003247051 EXHAUST VALVE BOEING747 74746NF 13848BTNM E/E COOLING FAILED A P5CAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA15450PA 30808 EICAS MSG "EQUIP COOLING" AFTER ENGINE START. PERFORMED QRH PROCEDURE "EQUP COOLING" MSG REMAINED DISPLAYED. RETURNED TO GATE. CHECKED COUND CMC MSG 21404 E/E COOLING GROUND EXHAUST VALVE FAILED PART REPLACED IAW MM 21-58-12 2L74 4F RTA20WE 20050722002012005072200201NE 2005 7 22 MASA200500518 220050705A7200324485318 MFC DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE ENGINE FAILED A MASAO OTHER O OTHER CRCRUISE 1 SW07988HA4250 426 TM123316 NR 1 ENGINE SHUT DOWN IN FLIGHT BY IT SELF. MX REPLACED FUEL PUMP WITH NO FIX AND FINALLY REPLACED THE MFC AND OPS CK'D NORMAL. 2H72 4T4 TRTA13NM E20NE 20050722002092005072200209CE 2005 7 22 GNB2005F00006 120050525A2700500000895CR CONTROL CABLE CESSNA402 402C 207590RCE CONT O520 TSIO520* 17040SO LT WNG WORN E GNBAO OTHER O OTHER NRNOT REPORTED 1 SW01305AT 402C0030 CABLE BLENDED AT PULLEY. PROBABLE CAUSE, SOFTER NEW STYLE STAINLESS STEEL CABLE MATERIAL. SERVICE LIFE IS ONLY FRACTIONS OF OLD STYLE STEEL CABLES. (K) 1L72 3O3 O A7CE E8CE 20050722002172005072200217 2005 7 22 SA05086 420050721A2565 LANYARD AIRBUS320 A320214 3930316EU ESCAPE SLIDE MISSING A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19106US 1044 PIT - THE AFT LEFT EMERGENCY EXIT DOOR ESCAPE SLIDE SURVIVAL KIT LANYARD WAS FOUND NOT IN VIEW. MAINTENANCE INSTALLED SURVIVAL KIT LANYARD. OK FOR SERVICE. 2L72 4F RTA28NM 20050722002182005072200218 2005 7 22 SA05087 420050721A2565 LANYARD AIRBUS320 A320214 3930316EU ESCAPE SLIDE MISSING A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19106US 1044 PIT - THE AFT RIGHT DOOR ESCAPE SLIDE SURVIVAL KIT LANYARD WAS FOUND INCORRECTLY ROUTED. MAINTENANCE CORRECTLY ROUTED THE AFT RIGHT DOOR ESCAPE SLIDE SURVIVAL KIT LANYARD. 2L72 4F RTA28NM 20050722002192005072200219 2005 7 22 SA05088 420050721A2565 LANYARD AIRBUS320 A320214 3930316EU ESCAPE SLIDE MISSING A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19106US 1044 PIT - THE LEFT FORWARD DOOR ESCAPE SLIDE SURVIVAL KIT LANYARD WAS FOUND INCORRECTLY ROUTED. MAINTENANCE CORRECTLY ROUTED THE SURVIVAL KIT LANYARD. OK FOR SERVICE. 2L72 4F RTA28NM 20050721000622005072100062NM 2005 7 21 05FDEA01929 120050713A5320 FLOOR SUPPORT DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 CABIN, AT STA 2003 RBL 57 FLOOR SUPPORT STRUCTURE FOUND CORRODED. CORROSION REMOVED AND REPROTECTED AS PER SRM 51-21-01 2L73 4F RTA22WE 20050721000682005072100068EU 2005 7 21 05FDEA01950 120050714A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25656FE 745 SEAT TRACK CORROSION ON SEVERAL LOCATIONS BETWEEN FR 63-FR-71 BLO. 2L72 4F RTA35EU 20050721000692005072100069EU 2005 7 21 05FDEA01951 120050714A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25656FE 745 MCD SEAT TRACK CORRODED BETWEEN FR71 - FR73 BL O. 2L72 4F RTA35EU 20050721000832005072100083CE 2005 7 21 DXTA200500845 120050717A499038007221 APU CESSNA560 560XL 2076702CE APU BAY OVERSERVICED E DXTAD RETURN TO BLOCK BW SMOKE/FUMES/ODORS/SPARKS INADEQUATE Q C TXTAXI/GRND HDL 1 GL07687QS1680 5605187 AIRCRAFT APU RUNNING ON GROUND / CABIN FILLED UP WITH BLUE SMOKE, CUT APU BLEED AIR OFF, AND SMOKE SLOWED BUT DID NOT STOP, AIRCRAFT HAD BEEN SITTING IN HEAVY RAIN. STARTED BOTH ENGINES, AC DID NOT SMOKE. FOUND APU OIL OVERSERVICED. REMOVED EXCESS OIL, RAN APU . OPS CHECK GOOD. NO SMOKE W/ APU BLEED AIR. WORK PERFORMED IAW HONEYWELL RE-100(XL) APU MM CHAP 49-90-00 . 2L72 4F RTA22CE 20050721001022005072100102EA 2005 7 21 ASOA05535 120050618A335020131A BATTERY PACK CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27702EV 10035 DURING A GROUND INSPECTION IN ATL, THE EMERGENCY LIGHTS WOULD NOT ILLUMINATE WITH THE SWITCH IN THE ON POSITION. MAINTENANCE REMOVED AND REPLACED AN EMERGENCY LIGHTS BATTERY PACK IAW CRJ700/900 AMM 33-51-17. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050721001112005072100111NM 2005 7 21 USAA050843 120050707A5320 STIFFENER BOEING737 7373B7 1384580NM FUSLEAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU52779 23861 CLT - FOUND STIFFENER CORRODED 2 INCHES, STATION 227.8, BL 0 ON VERTICAL STIFFENER. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR PARTS IAW EA 69945. (M) 2L72 4F RTA16WE 20050721001122005072100112EA 2005 7 21 ASOA05536 120050610A5320 SILL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27830AS 7236 DURING A C-CHECK IN MCN, THE FLOOR SILL AT FS 559 PLUS 16 TO FS 621 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE FLOOR SILL AT FS 559 PLUS 16 TO FS 621 IAW ASA EO 600-53-0278. (M) 2L72 4F RTA21EA 20050721001202005072100120EA 2005 7 21 ASOA05507 120050610A3350487190 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT LOOSE A ASOAK NONE L NO TEST ININSP/MAINT 1 NM01820AS 7188 FLT 4249 - DURING A GROUND INSPECTION IN ATL, THE EMERGENCY EXIT LIGHT AT ROW 8A WAS FOUND TO BE INOPERATIVE. MAINTENANCE FOUND LOOSE CONNECTOR TO THE EMERGENCY EXIT LIGHT AT ROW 8A AND RESECURED IT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050721001532005072100153NM 2005 7 21 SWAA052105 120050718A3350100031 SIGN BOEING737 7377H4 1384404NM EMERGENCY EXIT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29476WN 32475 DURING SCHEDULED RON, FOUND R2 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED EXIT SIGN PER MM. 2L72 4F RTA16WE 20050721001772005072100177NM 2005 7 21 DHL2005745010 120050721A3320 ODOR BOEING727 727224 1384076NM LIGHT DETECTED A DHLAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO01745DH 20665 AT FL 300 CREW NOTICED BURNING ODOR IN COCKPIT AND NOTED L-1 OVERHEAT LIGHT ILLUMINATED TURNED OFF L-1 OVERHEAT LIGHT BURNING ODOR WENT AWAY. TRANSFERRED TO DMI 21743 PER 727 MEL 30-15 CAT C PLACARDS INSTALLED. REF DMI CONTROL 21743 AT FL 300 CREW NOTICED L-1 WINDOW O/H LIGHT & BURNING ODOR. L1 WINDOW & RESISTANCE CKS WITHIN LIMITS. SWAPPED OVERHEAT SENSORS TO PRIMARY IAW MM 30-41-42 OPS CK GOOD. NO BURNING ODOR NOTED. THIS CLEARS DMI 21743. 2L73 4F A3WE 20050721001932005072100193 2005 7 21 AALA20050438 420050712A2330 MONITOR BOEING757 7572Q8 1384972NM CABIN ODOR A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21712TW 27624 ELECTRICAL FUMES IN CABIN DURING FLIGHT. DIVERTED TO MOB. FIRE DEPARTMENT REPORTS VIDEO SCREEN BETWEEN ROWS 9 AND 10 LT SIDE AS SOURCE. INSPECTED AND NO DAMAGE TO CONNECTORS NOTED. REPLACED MONITOR AND RESET CIRCUIT BREAKERS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050722000142005072200014EU 2005 7 22 UPS05144932 120050715A3350 LAMP AIRBUSA300 A300F4622R 3930360EU EMERGENCY EXIT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01152UP 0835 LAVATORY EMERGENCY EXIT INOPERATIVE, RELAMPED. 2L72 4F RTA35EU 20050722000212005072200021WP 2005 7 22 UPS05844922 120050706A5712 RIB DOUG DC8 DC873F 302199FWP XF CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 RT WING L/E UPPER RIB CRACKED .25 INCHES LONG AT XF693. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2, DWG 5769470 AND SRM 51-1-20D. 2L74 4F RT4A25 20050722000242005072200024WP 2005 7 22 UPS05844925 120050628A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 C1 LONG 14L AT APPROX STA 1743 IS CRACKED AT BOTH UPPER AND LOWER FRAME ATTACH POINTS. REMOVED DAMAGED SECTION OF LONGERON, FABRICATED, AND INSTALLED IAW DC- 8 SRM 53-2-2 FIG 10. 2L74 4F RT4A25 20050722000262005072200026EU 2005 7 22 05FDEA01898 120050712A5730 ACCESS PANEL AIRBUS310 A310 EU WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25411FE 359 ACCESS PANEL 650 FB HAS 1 ELONGATED HOLE, COMPLIED WITH EA6-5710-90863. 2L72 4F RTA35EU 20050722000462005072200046EA 2005 7 22 COMA0560398 120050717A32304622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01487CA7349 7729 FLIGHT 5170- GEAR DISAGREE WARNING. REPLACED THE NLG PRIORITY VALVE. 2L72 4F RTA21EA 20050722000482005072200048NM 2005 7 22 05FDEA02003 120050720A7160 NOSE COWL DOUG MD11 MD11 3023602NM NR 3 ENGINE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 NR 3 ENGINE, NOSE INLET COWL INNER BARREL FROM 6 TO 9 O' CLOCK POSITION FOUND WITH CORROSION. NR 3 ENGINE, NOSE INLET COWL REMOVED AND REPLACED PER AMM 71-11- 01-4. 2L73 4F RTA22WE 20050722000502005072200050NM 2005 7 22 BB05054 120050720A2120 ODOR BOEING757 7572B7 1384964NM RROYCERB211 RB211535E4 54555NE COCKPIT DETECTED A USAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA19620AU 27199 DURING TAKE-OFF, FROM ROTATION UNTIL INITIAL CLIMB, A STRONG ODOR OF JET FUEL WAS NOTICED IN THE COCKPIT. AFTER FIVE SECONDS, THE ODOR WENT AWAY. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED FOR FUEL LEAKS AND FOUND NONE. ACCOMPLISHED THE APPROPRIATE FIM PROCEDURE. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA2NM E12EU 20050722000512005072200051NM 2005 7 22 BB05052 120050720A335020121 CHARGER BOEING767 767201 1385125NM ZONE 200 FAULTY A USAAK NONE L NO TEST ININSP/MAINT 1 EA19648US 23900 SNN - DURING INSPECTION, MAINTENANCE FOUND THE EMERGENCY EXIT LIGHTS ON THE OVER-WING ESCAPE DOORS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER ASSEMBLY AND BATTERY AT LOCATION M1209 IN THE CABIN CENTER AREA. 2L72 4F RTA1NM 20050722000662005072200066NM 2005 7 22 05FDEA02006 120050721A5347606549 SEAT TRACK BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25280FE 22347 SEAT TRACK STA 690-740 IS CORRODED LBL 24. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2 2L73 4F RTA3WE 20050722000702005072200070EA 2005 7 22 COMA0560396 120050716A2170 COALESCER BAG CNDAIRCL600 CL6002B19 1900309EA ACM DIRTY A COMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO01819CA 7415 FLIGHT 5855- BURNING SMELL IN CABIN. CND, CLEANED COALESCERS, OPERATIONAL CHECKS NORMAL. 2L72 4F RTA21EA 20050722000732005072200073EA 2005 7 22 SWIA200515298 120050717A27604916405 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION LDLANDING 1 NM07441SW 7602 SPOILERON FAULT STATUS MSG ON LANDING IN HLN.REPLACED SECU 1 AND 2. OPERATIONAL CHECK GOOD. REF CL600 MM 27-61-01. PN 49-164-06 SN OFF: 1137 SN OFF: 0772 2L72 4F RTA21EA 20050722000852005072200085EU 2005 7 22 U30A200500006 120050720A2560PL22412LH055 GLOWSTRIP AIRBUS320 A320214 3930316EU AFT CABIN CRACKED A U30AK NONE O OTHER ININSP/MAINT 1 EA17264AV 1867 AFTER FLT 631 IN ORD, MAINTENANCE WAS PERFORMING A "DAILY INSP." AND FOUND THE PHOTOLUMINESCENT EMERGENCY FLOOR PATH LIGHTING STRIP BROKEN (CRACKED). THE CRACK WAS APPROXIMATELY 6" FROM THE END OF THE STRIP IN THE AFT OF THE AIRCRAFT BY LAV "D". (NOTE: THE PHOTOLUMINESCENT STRIP STILL FUNCTIONS WITH THIS TYPE OF DAMAGE.) MAINTENANCE REPLACED A 6" SECTION OF THE PHOTOLUMINESCENT STRIP PER AMM 33-51-21 PB401. 2L72 4F RTA28NM 20050722000932005072200093SO 2005 7 22 BSYA200500012 220050721A8500 ENGINE BEECH 58 58 1152740CE CONT O520 IO520C 17032SO FAILED E BSYAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 GL079044V TH216 823888R AIRCRAFT WAS ENROUTE FROM BDL TO PHL WHEN HE SEEN SPARKS AND LOST ALL OIL PRESSURE, THEN DIVERTED TO TEB DECLARED AN EMERGENCY, LANDED NO PROBLEMS. FOUND NR 2 ROD THRU ENGINE CASE. CAUSE UNKNOWN AT THIS TIME, R&R ENGINE 1L72 3O3 O 3A16 E5CE 20050722001012005072200101NM 2005 7 22 AWXA200500829 120050718A53306545774 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28334AW 23747 PHX - FUSELAGE CRACK AFT OF LEFT WING JUST BELOW EMERGENCY LIGHT AND AFT OF WING TO BODY FAIRING, APPROX 1.2 INCHES LONG. MAINTENANCE TRIMMED CRACK OUT OF SKIN IAW BOEING 737-300 SRM 53-00-01 REPAIR 31. REQUIRES OEM APPROVAL. FABRICATED EXTERNAL DOUBLER AND TRIPLER IAW ENGINEERING REPAIR NO. 03-5361-05196-ES2. INSTALLED REPAIR PARTS IAW AWA ER 03-5361-05196-ES2. 2L72 4F RTA16WE 20050722001062005072200106 2005 7 22 2005000006 420050522A3414 INDICATOR BOEING757 75728A 1384976NM COCKPIT FAILED A CNMAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SW07369AX 28161 CAPTIANS AIRSPEED FAILED TO RISE BY 80 KNOTS REJECTED T/O 95 KNOTS. DISCONNECTED CAPTIANS PITOT LINE FROM ADC. CLEANED OUT LINE FOUND LINE TO BE BLOCKED BY A BUG. RECONNECTED PITOT LINE AND ADC. PERFORMED PITOT/STATIC TEST PER 757 MM 34-11-10. 2L72 4F RTA2NM 20050722001112005072200111WP 2005 7 22 UPS05844928 120050628A534037540252 FITTING DOUG DC8 DC873F 302199FWP FUSELAEG CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE: C1, STA 1220 BETWEEN L27R-L26R SPIDER FITTING HAS A CRACK RUNNING FROM BOLT HOLE TO LOWER RIVET. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20050722001202005072200120NE 2005 7 22 2005000009 220050711A7314925708 PUMP DOUG DC10 DC1030 3023501WP GE CF6 CF650C2B 30018NE ENGINE FUEL DEFECTIVE A CNMAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SW07270AX 48318 530403 NR 1 ENGINE WOULD NOT MAKE TAKEOFF POWER. REMOVED AND REPLACED MAIN ENGINE FUEL PUMP NR 1 ENG IAW 73-12. REMOVED AND REPLACED MAIN FUEL FILTER IAW 73-11. REMOVED AND REPLACED MEC IAW 73-20 RAN ENGINE PER OMNI JET RUN HANDBOOK, OPS CHECKS GOOD AT THIS TIME. 2L73 4F4 F A22WE E23EA 20050722001332005072200133NM 2005 7 22 2005UALA00649 120050712A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29504UA 24625 FUSELAGE STATION 1595, STR 19R IS DAMAGED. THE REPAIR WAS MODIFIED PER EVA IND-3213A TO REPLACE RIVETS WITH HILOCKS ON THE STRINGER ROW. PERMANENT REPAIR PER SRM 53-00-01 PG 206-208. 2L72 4F4 FRTA2NM E17NE 20050722001382005072200138NM 2005 7 22 2005UALA00654 120050713A3397794640 WIRE BOEING747 747422 1384935NM PWA 4056 PW4056 NE LAV 110 DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29178UA 24385 EEL INOP AFT SIDE LAV 110. DAMAGED FEEDER CABLE WAS REPAIRED OK. 2L74 4F4 FRTA20WE E24NE 20050722001772005072200177NM 2005 7 22 CALA0500225 120050718A5315BAC1505338 FLOORBEAM BOEING757 757224 1384958NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713110 27300 INSPECTION FOUND FLOORBEAM CORRODED IN FRONT OF RT I/B SEAT TRACK AT STA 720, RBL 20 TO RBL 26. THE CORRODED SECTION OF FLOORBEAM WAS CUT OUT AND A NEW SECTION WAS SPLICED IN IAW SRM 53-00-51. 2L72 4F RTA2NM 20050722001792005072200179NM 2005 7 22 CALA0500227 120050719A3350D71702001 BATTERY BOEING737 737724 13844BYNM EMERGENCY LIGHT INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW2723721 28940 POWER DROPPED OFF LINE AND SEVERAL AISLE PATH EMERGENCY LIGHTS WOULD NOT ILLUMINATE. A NEW M1676 BATTERY PACK WAS INSTALLED AND OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20050722001802005072200180EU 2005 7 22 USAA050790 120050623A5320D5347217220390 FLOOR SUPPORT AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19721UW 1095 PIT - FOUND FLOOR SUPPORT BEAM CORRODED 1.5 INCH BY .75 INCH AREA, -Y1050 FRAME 67 AND 68. DEFECTIVE PART REPLACED WITH IDENT PART. CORROSION LEVEL 2, TASK JA-260-53500. (M) 2L72 4F RTA28NM 20050722001822005072200182SO 2005 7 22 SWIA200515280 120050502A5713 STRINGER EMB 120 EMB120ER 3260203SO LT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07227SW 120304 LEFT WING NR 2 FUEL BAY ACCESS LOWER FWD STRINGER CRACKED. DETERMINED TO BE A MAJOR REPAIR, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED STRINGER IAW EMB 120 SRM 57-20-03 P 203 FIG 21 SHEET 7. 2L72 4T RTA31SO 20050722001832005072200183EA 2005 7 22 SWIA200515281 120050714A5210 SLIDING SLEEVE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR HANDLE BINDING A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07409SW 7056 PAX - DOOR DIFFICULT TO STOW FROM THE INSIDE AND HARD TO OPEN FROM THE OUTSIDE. INSPECTED LINKAGE AND REINSTALLED OUTER HANDLE PUSH LATCH PIN. LUBED SLIDER. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050722001852005072200185EA 2005 7 22 SWIA200515283 120050714A2760C13045BA03 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07705SK 10145 STAB CHANNEL NR 2 FAULT MESSAGE. INSTALLATION OF NR 2 SSCU PER 27-61-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050722001872005072200187EA 2005 7 22 SWIA200515285 120050713A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLIGHT SPOILER MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07447SW8070 8070 7677 LEFT SPOILERON FAULT. REPLACED NR 1 HYD SPOILERON PCU IAW MM 27-62-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050722001882005072200188SO 2005 7 22 SWIA200515286 120050715A27503472001001 CONTROL UNIT EMB 120 EMB120ER 3260203SO TE FLAP MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07295SW1187011870 120322 CONTROL FAULT FLAPS EXTEND TO 7 DEGREES. REPLACED FLAP COMPUTER IAW 27-50-06. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050722001902005072200190EA 2005 7 22 SWIA200515288 120050712A2720 TRANSMITTER CNDAIRCL600 CL6002B19 1900309EA RUDDER INOPERATIVE A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07437SW 7564 AFTER ENGINE START, RUDDER INDICATION SHOWED NO MOVEMENT DURING TEST. REPLACED RUDDER POSITION TRANSMITTER IAW CRJ MM 27-24-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050722001932005072200193NE 2005 7 22 2005UALA00641 220050708A7200 VALVE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 1 ENGINE MALFUNCTIONED A UALAEFA ENGINE SHUTDOWN ACTIVATE FIRE EXT. UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29483UA 1586 V10402 RECEIVED ECAM AND A FIRE ALARM FOR ENG NR 1. SHUT DOWN ENGINE. NR 1 ENGINE PRESSURE REGULATING VALVE FOR LEAKAGE AROUND SPINDLE SHAFT. 2L72 4F4 FRTA28NM E40NE 20050722002232005072200223NM 2005 7 22 AT0500023 120050720A3350 BATTERY BOEING717 717200 1383700NM EMERGENCY LIGHT INOPERATIVE A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15910AT 55086 EMERG LIGHTS AT ROWS 123&10 WILL NOT ILLUMINATE. REMOVED AND REPLACED EMERG LIGHT BATTERY SUPPLY ASSY AND REMOVED AND REPLACED PROXIMITY LIGHT ASSY ROW 10 FWD IN REF TO MM 33-51 2L72 4F TRA6WE 20050722002252005072200225SO 2005 7 22 T042005F00000 120050614A321040288000 PLATE PIPER PA31 PA31350 7103110SO LYC O540 TIO540* 41532EA LT MLG CRACKED E T04AO OTHER O OTHER NRNOT REPORTED 1 AL032791721020 317952007 FOUND CRACKS IN REINFORCING WEB. PART TT THOUGHT TO BE SAME AS AC TT. OPERATED THIS AIRCRAFT FOR APPROXIMATELY 2,100 HOURS AND OTHERS FOR A TOTAL OF 5,000 HOURS. FIRST ONE WE HAVE SEEN CRACK. (K) 1L72 3O3 O A20SO E14EA 20050725000052005072500005CE 2005 7 25 SD92005F00000 120050622A3240220000145 LINE CESSNA182 TR182 2072735CE LYC O540 O540L3C5 41532EA LT BRAKE INOPERATIVE E SD9AO OTHER O OTHER NRNOT REPORTED 1 WP07851DE6693 R18201494 L2348440 PILOT REPORTED LT BRAKE INOPERATIVE ON LANDING. INSP OF AIRCRAFT FOUND LOW HYDRAULIC FLUID LEVEL IN LT MASTER CYLINDER. AFTER SERVICING BRAKES AND CHECKING SYSTEM, FOUND B-NUT ON LT BRAKE CALIPER TO BE SLIGHTLY LOOSE. THIGHT END BRAKE LINE, CLEANED AREA AND LEAK CHECKED, FOUND NO LEAKS. PROBABLE CAUSE OF LT BRAKE FAILURE WAS LOW FLUID LEVEL MAGNIFIED BY NORMAL LINING WEAR. AIRCRAFT LANDED WITHOUT INCIDENT OR DAMAGE. (K) 1H71 3O3 O 3A13 E295 20050725000082005072500008EU 2005 7 25 RAIA0050714 120050714A3260 WARNING HORN JETAIRJETSTMJETSTM4101 1500501EU NLG FALSE ACTIVATIONA RAIAO OTHER N FALSE WARNING DEDESCENT 1 CE03562HK 41078 FLT 3651 - SYR - NOSE GEAR STBY IND INOP - GEAR HORN SOUNDED - DECLARED EMERGENCY. LANDED SAFELY WITH OUT INCIDENT. FERRIED TO RIC FOR REPAIRS. MAINTENANCE INSPECTED WIRE HARNESS AND WOW SWITCHES AND PERFORMED MULTIPLE GEAR OPERATIONAL CHECKS BUT WAS UNABLE TO DUPLICATE. NO DEFECTS NOTED. 2L72 4T RTA41NM 20050725000142005072500014NM 2005 7 25 UPS05544944 120050720A2560 SMOKE GOGGLES BOEING757 75724APF 1384969NM COCKPIT MISSING A IPXAK NONE O OTHER ININSP/MAINT 1 SO01409UP 23731 SMOKE GOGGLE MISSING FROM SUPERNUMARY POSITION 1, INSTALLED 1 SMOKE GOGGLE AT POSITION 1 SUPERNUMARY SEAT 2L72 4F RTA2NM 20050725000152005072500015WP 2005 7 25 UPS05844935 120050607A532046461634501 FITTING DOUG DC8 DC871F 302199DWP FUSLEAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01705UP 45949 INSPECTION TYPE: C2, B-PIT BETWEEN STA 460-440 L28R SPLICE FITTING CRACKED. REMOVED AND REPLACED SPLICE FITTING IN B-PIT AT STA 460-440, L28R IAW SRM 51-1-21D AND SRM 51-1-21 2L74 4F RT4A25 20050725000162005072500016WP 2005 7 25 UPS05844936 120050711A5310 FINGER DOUBLER DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE:C1 HEAVY CORROSION BETWEEN COCKPIT SUBFLOOR SKIN AND 2ND FINGER DOUBLER, SEVERAL POPPED RIVIT HEADS,-52 TO -62 LH SIDE AT CUSP. REMOVED FINGER DOUBLERAND REMOVED CORROSION .004 FROM SUBFLOOR SKIN FOUND TOBE WITHIN LIMITS. FABRICATED AND REPLACED FINGER DOUBLER. IAW SRM 51-1-21, 53-2-0, 53-3-3, 51-1-8, 51-1-15, AND 51-1-20D. 2L74 4F RT4A25 20050725000172005072500017WP 2005 7 25 UPS05844937 120050711A53204750419U501 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE:C1 FRAME TO INTERCOSTAL FITTING CRACKED STA.1160 L18R. REMOVE AND REPLACE INTERCOSTAL FITTING IAW SRM 51-3-0 AND 51-1-20D. 2L74 4F RT4A25 20050725000182005072500018WP 2005 7 25 UPS05844938 120050709A5347 SPLICE DOUG DC8 DC873F 302199FWP SEAT TRACK CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE:C1 MAIN CABIN IN BETWEEN FS 980-1000 RBL 60 HAS LIGHT CORROSION ON SEAT TRACK SPLICES. REMOVED, FABRICATED AND INSTALLED 2 EA. SEAT TRACK SPIICES. IAW 51-3-0 ,53-02-03 FIG 006A, AND 51-1-21. 2L74 4F RT4A25 20050725000212005072500021 2005 7 25 20050708 420050708A3160 DISPLAY EMB ERJ170ERJ170100LR EU COCKPIT INOPERATIVE A UHLAO OTHER G MULTIPLE FAILURE CRCRUISE 1 GL17631RW 17000007 ON 07-08-2005, A/C 631RW, FLT 7573 ORD-HPN. DURING FLIGHT AT FL390, ALL FIVE DISPLAY UNITS WENT BLANK. THE AUTOPILOT AND AUTOTHROTTLES DISENGAGED AND MULTIPLE FLIGHT CONTROL FAULT/FAIL MESSAGES WERE PRESENT. MX RESET POWER IAW FIM 45-45-00-810-939, NO DEFECTS NOTED AT THIS TIME. 2L74 4F RTA56NM 20050725000352005072500035NM 2005 7 25 ASMF200507016 120050721A2730 ELEVATOR BOEING757 7572Q8 1384972NM OUT OF RIG W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23804AM 26271 CAPTAIN REPORTED THAT THE MESSAGE -ELEV ASYM- WAS SHOWN IN EICAS. THE FIM 27-09-00 FIG. 106 PROCEDURE WAS PERFORMED AND DURING CONTROLS TESTS REPEATED THE MESSAGE. DURING ELEVATOR SURFACE INSPECTION WAS DETECTED ASYMMETRY IN ELEVATORS. AIRCRAFT WAS SENT TO THE HANGAR AND FIM 27-09-00 PROCEDURE WAS PERFORMED, TESTED CORRECT. 2L72 4F RTA2NM 20050725000382005072500038CE 2005 7 25 07152005A 120050715A5270 WARNING LIGHT BEECH 1900 1900D 1154162CE CARGO DOOR ILLUMINATED A NSVAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA27221CJ UE221 CARGO DOOR WARNING LIGHT ILLUMINATED ON TAKEOFF. 2L72 4T RTA24CE 20050725000392005072500039CE 2005 7 25 DXTA200500851 120050721A323499141961 SELECTOR CESSNA650 650 2076802CE MLG INOPERATIVE E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07797QS4633 6507097 GEAR WOULD NOT RETRACT AFTER TAKEOFF. REMOVED AND REPLACED LANDING GEAR SELECTOR PER CESSNA 650 MM 32-30-01, OPS CHECK GOOD. 2L72 4F A9NM 20050725000402005072500040CE 2005 7 25 DXTA200500849 120050714A275199145104 POSITION SENSOR CESSNA750 750 2076810CE TE FLAPS FAULTY E DXTAO OTHER N FALSE WARNING CRCRUISE 1 GL07934QS 7500034 FLAPS FAIL CAS ILLUMINATED IN CRUISE AT FL450. FLAP INDICATOR CYCLED CONTINOUSLY FROM 0 DEGRRES TO 15 DEGREES INDICATION. FLAPS WERE NOT MOVING. FLAPS WON'T RESET. DUPLICATED DISCREPANCY. NO BITE CODES ON FLAP CONTROLLER. INSTALLED FLAP BREAK OUT BOX. TROUBLESHOT TO FAULTY LT FLAP POSITION SENSOR. REMOVED AND REPLACED SENSOR. ADJUSTED SENSOR. C/W SATISFACTORY OPERATIONAL CHECK OF FLAP SYSTEM. ALL WORK IAW CE750 MM 27-50-00. 2L72 4J RTT00007WI 20050725000412005072500041CE 2005 7 25 DXTA200500850 120050720A3240 BRAKE ASSY CESSNA500 560CESSNA 2076750CE MLG MALFUNCTIONED E DXTAO OTHER S AFFECT SYSTEMS LDLANDING 1 GL07319QS 5600519 DURING LANDING MINOR APPLICATION OF THE BRAKES WOULD LOCK UP TIRES. IT TOOK 6000 FT OF RUNWAY TO STOP. ANTI-SKID TESTS NORMALLY. ALL FLUIDS FULL. WHEN THE TIRES WOULD LOCK UP THE ANTI-SKID WOULDN'T RELEASE LOCK UP. TAXIED AIRCRAFT AND TESTED BRAKING SYSTEM WITH ANTI-SKID BOTH ON AND OFF. BRAKING SYSTEM APPEARED NORMAL. ACCOMPLISHED FUNCTIONAL TEST OF ANTI-SKID SYSTEM. BRAKES RELEASED AND REAPPLIED NORMAL. ACCOMPLISHED BRAKE BLEEDING AND RESERVICED RESERVOIR. ALL WORK DONE IAW CE560 MM CH 32-42-00. 2L72 4F RTA22CE 20050725000432005072500043EU 2005 7 25 07172005A 120050717A6120 PROPELLER SAAB SF340 340B 7860101EU LEFT MALFUNCTIONED A NSVAD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 EA27305CE 202 LEFT PROP WILL NOT FEATHER. OIL PRESSURE 0 PSI. TEMP 175. 2L72 4T RTA52EU 20050725000442005072500044EU 2005 7 25 07182005 120050718A3260 CIRCUIT BREAKER SAAB SF340 340B 7860101EU MLG INDICATOR TRIPPED A NSVAO OTHER P NO WARNING INDICATION APAPPROACH 1 EA27339CJ 339 NO LANDING GEAR INDICATION ON FINAL APPROACH. F7 CIRCUIT BREAKER WAS POPPED, RESET AND CONTINUED OPERATION. 2L72 4T RTA52EU 20050725000452005072500045NE 2005 7 25 07192005 220050719A73108346001 PRESSURE SWITCH SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RT ENGINE LEAKING A NSVAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 EA27312CE 334 RT ENGINE APPEARS TO BE LEAKING FUEL FROM PRESSURE SWITCH. 2L72 4T4 TRTA52EU E8NE 20050725000462005072500046EA 2005 7 25 548707212005 120050721A5610 TERMINAL BLOCK CNDAIRCL604 CL604 1900301EA WINDSHIELD BURNED E J7SAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW05330FX 5487 CREW SAW WISP OF SMOKE AND BURNING ELECTRICAL ODOR IN COCKPIT. MADE UNSCHEDULED LANDING IN ABQ (EMERGENCY DECLARED FOR CLEARANCE PURPOSES). MAINTENANCE FOUND TERMINAL STRIP ON PILOTS WINDSHIELD BURNED OUT (TERMINAL STRIP IS FOR WINDSHIELD HEAT). NO OTHER DEFECTS NOTED. ITEM DEFERRED PER MEL 2L72 4F RTA21EA 20050725000472005072500047EU 2005 7 25 07152005B 120050715A26131734362450 FIRE DETECTOR SAAB SF340 340B 7860101EU RT TAILPIPE ILLUMINATED A NSVAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27305CE 202 RT TAILPIPE HOT LIGHT ILLUMINATED AFTER TAKEOFF AND REMAINED ON UNTIL APPROACH 2L72 4T RTA52EU 20050725000482005072500048EU 2005 7 25 07202005 120050720A3234 INDICATOR SAAB SF340 340B 7860101EU MLG INOPERATIVE A NSVAO OTHER P NO WARNING INDICATION CLCLIMB 1 EA27314CE 335 LANDING GEAR IN TRANSIT LIGHT DOES NOT ILLUMINATE WHEN GEAR IS SELECTED UP. 2L72 4T RTA52EU 20050725000492005072500049CE 2005 7 25 07212005 120050721A3250 STEERING SYS BEECH 1900 1900D 1154162CE NLG MALFUNCTIONED A NSVAO OTHER O OTHER TXTAXI/GRND HDL 1 EA27155CJ UE55 DURING TAXI, AIRCRAFT MAINTAINS STRAIGHT LINE WHEN EITHER RUDDER PEDAL IS DEFLECTED FULL TRAVEL. 2L72 4T RTA24CE 20050725000532005072500053NM 2005 7 25 SB05085 120050724A3397 WIRE BOEING737 7374B7 1384702NM LIGHT ASSY SHORTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19781AU 25020 CLT MAINTENANCE REPORTED THREE OVERWING EXIT HATCH HANDLE LIGHTS INOPERATIVE ON RIGHT-HAND SIDE. MAINTENANCE REPAIRED SHORTED HATCH HANDLE LIGHT L751 WIRE BEHIND EXIT LIGHT ASSEMBLY. ALSO, REPLACED FUSE IN M1497 POWER SUPPLY. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050725000562005072500056EU 2005 7 25 07232005B 120050723A33506013211 BATTERY SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A NSVAK NONE L NO TEST ININSP/MAINT 1 EA27346CJ 346 DURING OPERATIONAL CHECK OF EMERGENCY LIGHT SYSTEM, TWO FLOOR PROXIMITY LIGHTS WERE INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY 24LN 2L72 4T RTA52EU 20050725000602005072500060EU 2005 7 25 07232005A 120050723A2750 FLAP SYSTEM SAAB SF340 340B 7860101EU TE MALFUNCTIONED A NSVAO OTHER F FLT CONT AFFECTED APAPPROACH 1 EA279CJ 224 NO MOVEMENTS WHEN FLAPS SELECTED TO 15 DEGREES 2L72 4T RTA52EU 20050725000672005072500067WP 2005 7 25 GTIA050197 120050623A2497 WIRE DOUG DC9 DC982 3022082WP RT GENERATOR FAILED A GTIAO OTHER O OTHER TXTAXI/GRND HDL 1 GL23817NK 49141 RIGHT ENGINE GENERATOR FEEDER FAULT ON TAXI, AIRCRAFT TAIL SWAP WITH 835. REMOVED AND REPLACED RIGHT ENGINE GENERATOR. OPS AND LEAK CHECK GOOD. (M) 2L72 4F A6WE 20050725000682005072500068WP 2005 7 25 GTIA050195 120050619A3250 ACTUATOR DOUG DC9 DC983 3022083WP NLG STEERING WORN A GTIAO OTHER O OTHER LDLANDING 1 GL23814NK 49619 FLT 461, AFTER LANDING ROLL OUT, AIRCRAFT SHOOK VERY HARD UNTIL AIRCRAFT REACHED 5 TO 10 KTS, UNABLE TO TELL IF IT WAS NOSE OR MAIN WHEEL SHIMMY, AIRCRAFT TAIL SWAP WITH 802. INSPECTED NLG FOUND BOTH STEERING ACTUATORS HAD PLAY. REMOVED AND REPLACED BOTH STEERING ACTUATORS. OPS CHECK NORMAL. 2L72 4F RTA6WE 20050725000722005072500072WP 2005 7 25 GTIA050196 120050621A7797 WIRE DOUG DC9 DC983 3022083WP EPR INDICATOR FAILED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23808NK 49504 FLT 461 - DURING CREW PREFLIGHT, FOUND NR 2 EPR GAUGE FLAG IN VIEW, AIRCRAFT TAIL SWAP WITH 829. REPAIRED WIRES AND REMOVED AND REPLACED TRI CONNECTOR, OPS CHECK GOOD. (M) 2L72 4F RTA6WE 20050725000732005072500073NE 2005 7 25 GTIA050194 220050618A7200 ENGINE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE LEFT FAILED A GTIAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 GL23815NK 49415 FLT 304 - DURING CLIMB-OUT, LEFT ENGINE EGT BEGAN TO CLIMB JUST BELOW MAX TEMP, REDUCED POWER TO MAINTAIN MAX TEMP. FLIGHT ATTENDANT REPORTED LOUD NOISE FROM LEFT ENGINE AND RETURNED TO MCO, AIRCRAFT TAIL SWAP WITH 832. REMOVED AND REPLACED LEFT ENGINE, OPS AND LEAK CHECK GOOD. (M) 2L72 4F4 FRTA6WE E9NE 20050725000752005072500075WP 2005 7 25 GTIA050193 120050603A5313 STRINGER DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23830NK 49932 FUSELAGE FRAME STATION 1418 AT STRINGER 2L CRACKED. STOPPED DRILLED CRACK AT STATION 1418 AT STRINGER 26. FABRICATED REPAIR DOUBLERS. TREATED, PRIMED AND INSTALLED REPAIR DOUBLERS. (M) 2L72 4F A6WE 20050725000772005072500077WP 2005 7 25 GTIA050186 120050603A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23830NK 49932 FLOOR SUPPORT CORRODED AT STATION 180 LBL 50. REMOVED CORROSION, FOUND OUT OF LIMITS. FABRICATED FLOOR SUPPORT. TREATED AND PRIMED. (M) 2L72 4F A6WE 20050725000792005072500079EU 2005 7 25 AJC2005F00007 120050630A2822IC552 PUMP ISRAEL1125 ASTRASPX 4500205EU GARRTTTFE731TFE731* 01518WP FUEL FAILED E AJCAK NONE O OTHER ININSP/MAINT 1 EA25387PA 386 145 THE RT TANK STANDBY FUEL PUMP (BOOST PUMP) DID NOT OPERATE WHEN SELECTED (ON) DURING PREFLIGHT INSPECTION. MAINTENANCE DEFUELED AIRCRAFT AND REPLACED THE RT TANK FUEL PUMP AND INSTALLED NEW GASKET. OPERATIONAL CHECK GOOD IAW MM. AIRCRAFT WAS RETURNED TO SERVICE ON JULY 01, 2005. (EA25200509171) (K) 2L72 4F4 FRTA16NM E6WE 20050725000802005072500080CE 2005 7 25 072405 120050724A2120 SMOKE BEECH 1900 1900C 1154161CE COCKPIT DETECTED E YADAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 AL03111AX UC81 ODOR OF SMOKE IN COCKPIT - SHUT OFF BLEED AIR AND EVIRONMENTAL AIR, ODOR WENT AWAY - MAINTENANCE COULD NOT LOCATE ANY SOURCE OF THE ODOR - OPS CHECK FLIGHT SCHEDULED. 2L72 4T RTA24CE 20050725000822005072500082WP 2005 7 25 GTIA050187 120050607A5320 STRUCTURE DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23830NK 49932 RIGHT PAX CABIN SUB FLOOR AT 18R FS 850 BEHIND VENT GRILL IS CRACKED. CORROSION FOUND OUT OF LIMITS AT WEB 18R FS 850. CUTOUT DAMAGED SECTION OF WEB. FABRICATED REPAIR DOUBLER AND FILLER. TREATED, PRIMED AND PAINTED REPAIR PARTS. INSTALLED REPAIR DOUBLER AND FILLER AT 18R CUSP MEMBRANE. (M) 2L72 4F A6WE 20050725000842005072500084NM 2005 7 25 GTIA050178 120050504A5330 SKIN DOUG MD80 MD83 3023681NM FUSELAGE DENTED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23827NK 49793 FOUND DENT AT STRINGER 236 BETWEEN LONGERONS 18L AND 19L. CHEMICALLY REMOVED PAINT. CUT OUT DAMAGED AREA. FABRICATED REPAIR IAW. TREATED AND PRIMED REPAIR PARTS. INSTALLED REPAIR IAW. ITEM TRANSFERRED TO LOG PATE NR 0300548-1. (M) 2L72 4F RT 20050725000852005072500085WP 2005 7 25 GTIA050190 120050603A5313 LONGERON DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23830NK 49932 CRACKED AT LONGERON 2R STATION 1418. REMOVED 4 RADIUS BLOCKS, 1 LONGERON END STRAP AND 1 LONGERON TO FRAME ANGLE. REMOVED DAMAGED LONGERON 2R FROM 1405-1418. FABRICATED NEW LONGERON, TREATED AND PRIMED. INSTALLED LONGERON AND SPLICE. (M) 2L72 4F A6WE 20050725000882005072500088NM 2005 7 25 GTIA050179 120050518A5320 CUSP WEB DOUG MD80 MD83 3023681NM FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23827NK 49793 FOUND CORROSION -C- AT CUSP WEB LINE. REMOVED CORROSION FROM WEB/MEMBRANE. TREATED AND PRIMED CUSP WEB. CUT OUT DAMAGED AREA. FABRICATED REPAIR, DOUBLER AND FILLER. TREATED AND PRIMED REPAIR PARTS. INSTALLED REPAIR. (M) 2L72 4F RT 20050725000892005072500089CE 2005 7 25 DXTA200500856 120050723A2731 WHEEL CESSNA560 560XL 2076702CE ELEVATOR TRIM JAMMED E DXTAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL07675QS 5605275 ELEVATOR TRIM JAMMED DURING FINAL APPROACH. HAD TO USE EXCESSIVE FORCE ON TRIM WHEEL TO TRIM AIRCRAFT. TRIM WHEEL REMAINS TIGHT WITH ALL POWER OFF AIRCRAFT. - ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20050726000012005072600001NM 2005 7 26 UPS05M44956 120050722A3240 BRAKE ASSY DOUG MD11 MD11F 3023600NM LANDING GEAR FAILED A IPXAO OTHER O OTHER LDLANDING 1 SO01270UP 48576 DURING LANDING AUTOBRAKES FAILED TO DECELERATE THE A/C. AUTOSPOILERS DEPLOYED NORMALLY AND FULL REVERSE THRUST WAS APPLIED IMMEDIATELY MANUAL BRAKING, FULL SPOILERS AND FULL THRUST REVERSE WERE MAINTAINED. PERFORMED AUTO BRACK SYS IAW 32-44-00. NO DEFECT NOTED. SUSPECT FAULTY LT IBCW SEE L/ 414386. PERFORMED MAINT TAXI NO DEFECT NOTED SYS OPS CK SAT. OK FOR FURTHER FLIGHT. "BRAKE TEMP EVEN ACROSS LEFT/RIGHT." 2L73 4F RTA22WE 20050726000032005072600003WP 2005 7 26 ABXA050173 120050627A52205912995503 PAN DOUG DC9 DC941 302207NWP OVERWING EXIT CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23978AX 47628 RIGHT AFT OVERWING EXIT DOOR HAD CRACKED DOOR PAN, UPPER FORWARD CORNER. FABRICATED DOUBLER IAW DC-9 SSRM DWG K07390. INSTALLED IAW DC-9 SSRM DWG K07390. REINSTALLED WEB IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 20050726000062005072600006WP 2005 7 26 ABXA050176 120050628A53133925966 LONGERON DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23978AX 47628 CRACKED LONGERON STA 617, LONGERON 24 LEFT, THROUGH KIDNEY PANEL. REMOVED AND REPLACED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5. 2L72 4F A6WE 20050726000072005072600007WP 2005 7 26 ABXA050177 120050629A528059101617 RIB DOUG DC9 DC941 302207NWP MLG DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23978AX 47628 INNER RIB CRACKED ON LEFT MAIN LANDING GEAR DOOR. REPAIRED AREA IAW DC-9 SSRM NR K05159 AND DC-9 SRM 51-30-1. 2L72 4F A6WE 20050726000102005072600010WP 2005 7 26 ABXA050172 120050627A52205912995503 PAN DOUG DC9 DC941 302207NWP OVERWING EXIT CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23978AX 47628 RIGHT FORWARD OVERWING EXIT DOOR HAD CRACKED DOOR PAN, LOWER AFT CORNER. REPLACED RIGHT FORWARD OVERWING EXIT DOOR IAW DC-9 SRM. 2L72 4F A6WE 20050726000112005072600011 2005 7 26 ABXA050165 420050722A2565 SLIDE BOEING767 767281 1385109NM PAX DOOR DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23767AX 22785 EMERGENCY SLIDE ON MAIN PASSENGER DOOR WOULD NOT STAY IN POSITION. REMOVED AND REPLACED DOOR ESCAPE SLIDE IAW B767 AMM 25-66-01-4. PLACARD REMOVED. 2L72 4F RTA1NM 20050726000122005072600012WP 2005 7 26 ABXA050166 120050708A555359397111 ANGLE DOUG DC9 DC931 3022065WP EMPENNAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23943AX 47528 LEFT DORSAL FIN ATTACH ANGLE CRACKED DURING ROUTINE LINE MAINTENANCE. REPAIRED IAW EA53420010-103 FOR ANGLE REPLACEMENT. 2L72 4F A6WE 20050726000132005072600013WP 2005 7 26 ABXA050167 120050712A534029140251 FITTING DOUG DC9 DC932 3022066WP FUSLEAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23986AX 47543 NR 4 BEAM FORWARD END FITTING CRACKED ON AFT LOWER CARGO DOOR. REMOVED AND REPLACED FITTING AT NR 4 FORWARD BEAM IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20050726000142005072600014NM 2005 7 26 GTIA050174 120050504A5330 SKIN DOUG MD80 MD83 3023681NM FUSELAGE DENTED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23827NK 49793 FOUND DENT AT STATION 1224 BETWEEN LONGERONS 25R AND 26R. REMOVED PAINT AND PRIMER. DENT FOUND TO BE OUT OF LIMITS. COLD WORKED DENT. TREATED AND PRIMED. INSTALLED DOUBLER. PAINT DONE. (M) 2L72 4F RT 20050726000152005072600015NM 2005 7 26 GAIA0521OP 120050623A2170 COALESCER BAG BOEING727 727251 138408HNM PWA JT8 JT8D5 52046NE A/C PACK DIRTY A GAIAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW07252US 19971 DURING CLIMB OUT, FUEL ODOR, LANDING WAS MADE WITHOUT INCIDENT. CHECKED AFT SPAR ENGINE FUEL FEED LINE SHROUDS, NO LEAKS NOTED. REMOVED AND REPLACED BOTH WATER SEPARATOR BAGS, RAN BOTH PACKS, NO FUEL ODOR NOTED. OPS AND LEAK CHECKED OK. AIRCRAFT WAS RETURNED TO SERVICE. ODOR DETERMINED TO BE RELATED TO PREVIOUS REPAIR. (K) 2L73 4F4 F A3WE E2EA 20050726000162005072600016 2005 7 26 BB05056 420050722A2565D30654122 SLIDE BOEING757 7572B7 1384964NM ZONE 200 DEFECTIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19620AU4062 27199 MCO - THE L-1 DOOR "SLIDE ARMED" LIGHT FAILED TO ILLUMINATE WHEN THE DOOR WAS ARMED. MAINTENANCE FOUND THE SPRING ON THE GIRT BAR DEFORMED AND INTERFERING WITH ARMING. MAINTENANCE REPLACED THE GIRT BAR AND ESCAPE SLIDE ON THE L-1 DOOR. OK FOR SERVICE. 2L72 4F RTA2NM 20050726000182005072600018WP 2005 7 26 ABXA050168 120050712A52302914025501 FITTING DOUG DC9 DC932 3022066WP AFT CARGO DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23986AX 47543 NR 2 BEAM AFT END FITTING CRACKED ON AFT LOWER CARGO DOOR. REMOVED AND REPLACED FITTING IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20050726000202005072600020NM 2005 7 26 GTIA050172 120050509A5260 SKIN DOUG MD80 MD83 3023681NM AIRSTAIR DOOR DENTED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23827NK 49793 FOUND DENT AFT AIRSTAIR DOOR. REMOVED PAINT. CUT OUT DAMAGED AREA. FABRICATED ONE EACH FAIRING AND ONE REPAIR DOUBLER. PRIMED REPAIR PARTS. INSTALLED REPAIR PARTS. TREATED AND PRIMED BARE METAL AREAS. PAINTED AFT AIR STAIR DOOR. (M) 2L72 4F RT 20050726000212005072600021NM 2005 7 26 GTIA050171 120050515A5320 FLOOR SUPPORT DOUG MD80 MD83 3023681NM FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23827NK 49793 FOUND FORWARD ENTRY AREA FLOOR SUPPORT IS CORRODED. REMOVED FLOOR SUPPORT. FOUND FLOOR SUPPORT TO BE OUT OF LIMITS USING CALIPERS. LOCATED AND DRILLED NEW FLOOR SUPPORT. TREATED AND PRIMED. TOPCOAT FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2L72 4F RT 20050726000222005072600022NM 2005 7 26 GTIA050169 120050505A5514 STIFFENER DOUG MD80 MD83 3023681NM HORIZONTAL STAB CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23827NK 49793 FOUND LEFT HORIZONTAL STABILIZER REAR SPAR STIFFENER CRACKED ON UPPER EDGE. REMOVED DAMAGED STAB REAR SPAR STIFFENER. FABRICATE STIFFENER SEAL. LOCATED AND DRILLED FABRICATED STIFFENER. TREATED AND PRIMED FABRICATED STIFFENER. TOP COATED FABRICATED STIFFENER. INSTALLED FABRICATED STIFFENER. (M) 2L72 4F RT 20050726000262005072600026NM 2005 7 26 GTIA050170 120050515A5320 FLOOR SUPPORT DOUG MD80 MD83 3023681NM FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23827NK 49793 FOUND FORWARD ENTRY AREA FLOOR SUPPORT CORRODED. REMOVED FLOOR SUPPORT. FOUND FLOOR SUPPORT TO BE OUT OF LIMITS USING CALIPERS. MATERIAL ID CHECK FOR FLOOR SUPPORT. LOCATED AND DRILL NEW FLOOR SUPPORT. TREATED AND PRIMED. TOP COAT FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. APPLIED DINITROL TO FORWARD ENTRY AREA. (M) 2L72 4F RT 20050726000282005072600028WP 2005 7 26 GTIA050165 120050612A3610 AUGMENT VALVE DOUG DC9 DC982 3022082WP NR 1 ENGINE STUCK A GTIAO OTHER J WARNING INDICATION CRCRUISE 1 GL23804NK 49104 NR 1 ENGINE AUGMENTATION VALVE APPEARS TO STICK OPEN AT HIGHER POWER SETTINGS, AIRCRAFT TAIL SWAP WITH N821NK. FOUND LINE BEHIND AUG VALVE ON DUCT TO PNEUMATIC PRESSURE REGULATOR LOOSE, FOUND CRUSH GASKET WORN. REPLACED GASKET AND SECURED LINE. ENGINE RUN ACCOMPLISHED, OPS CHECK NORMAL. (M) 2L72 4F A6WE 20050726000292005072600029NE 2005 7 26 GUU2005F00031 220050705A7200 ENGINE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE NR 2 FAILED A GUUAF ACTIVATE FIRE EXT. XJ ENGINE FLAMEOUT WARNING INDICATION TXTAXI/GRND HDL 1 SO2981556 UE239 PSPS0041 LOUD BANG FROM NR 2 ENGINE UPON INITIAL POWER ADVANCEMENT, ABORTED TAKEOFF. NR 2 ENGINE FIRE T-HANDLE, BLEW BOTTLE. EVACUATED PASSENGERS. DETERMINED RT POWER SECTION TO BE SEIZED. EVIDENCE OF DEBRIS DAMAGE TO INSIDE OF EXHAUST STACKS. INVESTIGATION IN PROCESS. SUSPECT RT POWER SECTION MODULE 2ND STAGE POWER TURBINE BLADE FAILURE. (K) 2L72 4T4 TRTA24CE E26NE 20050726000342005072600034WP 2005 7 26 AALA20050448 120050718A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21498AA 49736 SFO OVERHEAD EMERGENCY LIGHT FROM SEAT 28D AFT INOPERATIVE. REPLACED BATTERY PACK B5 27 AND B5 107 FOR OVERHEAD EMERGENCY LIGHT FORM SEAT 28D AFT. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F A6WE 20050726000362005072600036WP 2005 7 26 AALA20050451 120050719A5280 BOLT DOUG DC9 DC983 3022083WP MLG DOOR MISSING A AALAO OTHER J WARNING INDICATION CLCLIMB 1 SW21593AA 53256 PHX INFLIGHT T1007/19JULY GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR EXTENSION. VERIFIED LEFT HAND GEAR DOOR OPEN. LANDED WITH DOORS OPEN. INSTALLED MISSING BOLT FROM LEFT HAND GEAR DOOR FOLLOW UP MECHANISM. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA6WE 20050726000372005072600037EU 2005 7 26 AALA20050452 120050720A3350P4010051124 POWER SUPPLY AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217083A 645 JFK EMERGENCY LIGHTS AT SEATS 6G TO 18G INOPERATIVE. REPLACED POWER SUPPLY FOR EMERGENCY LIGHTS AT SEATS 6G TO 18G. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA35EU 20050726000392005072600039WP 2005 7 26 AALA20050454 120050721A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21499AA 49737 DTW FORWARD EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F A6WE 20050726000402005072600040NM 2005 7 26 AALA20050455 120050720A3397 WIRE BOEING757 757231 1384950NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21711ZX 28481 DFW EMERGENCY PATH LIGHT AT MID LAV AND BETWEEN SEAT ROWS 12 AND 13 INOPERATIVE. REPLACED FEEDER CABLE FROM FORWARD ENTRY TO NUMBER 2 DOOR AND REPLACED LIGHT SEGMENT BETWEEN ROWS 12 AND 13. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA2NM 20050726000412005072600041WP 2005 7 26 AALA20050458 120050721A3350 CONNECTOR DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21593AA 53256 JFK AFT OVERWING EMERGENCY EXIT SIGN LIGHT AT ROW 21 LEFT AND RIGHT INOPERATIVE. RESECURED LOOSE CONNECTION ON BATTERY PACK FOR AFT OVERWING EMERGENCY EXIT SIGN LIGHT AT ROW 21 LEFT AND RIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA6WE 20050726000422005072600042WP 2005 7 26 AALA20050459 120050723A3350 CHARGER DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21435AA 49453 LAX EMERGENCY TRACK LIGHTS AT AFT EXIT SIGNS INOPERATIVE. REPLACED BATTERY CHARGER FOR EMERGENCY TRACK LIGHTS AT AFT EXIT SIGNS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA6WE 20050726000432005072600043WP 2005 7 26 AMTA200500567 120050709A33505165741 LIGHT LKHEED1011 10113853 5265020WP RROYCERB211 RB211524B4 54555NE SLIDE INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11164AT 1238 AFT 2 LT EXTERIOR SLIDE EGRESS LIGHTS, INOPERATIVE. REMOVED AND REPLACED AFT LT CHARGER, OPS CHECK NORMAL. (K) 2L73 4F4 F A23WE E12EU 20050726000462005072600046EA 2005 7 26 A6WA200540233 120050711A2410755469D IDG CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 1 ENGINE FAILED A A6WAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL31402AW8810 7281 IDG NR 1 CAUTION MESSAGE ON TAKEOFF ROLL, ABORTED TAKEOFF, IDG MESSAGE EXTINGUISHED AND REPLACED WITH GEN NR1 OFF CAUTION MESSAGE. FOLLOWED QRH, MESSAGE CLEARED ALL. ABORTED TAKEOFF AT 40 KNOTS. REMOVED AND REPLACED IDG NR 1, OP CHECK AND LEAK CHECK GOOD. (K) 2L72 4F4 FRTA21EA E15NE 20050726000482005072600048EA 2005 7 26 A6WA200540227 120050709A27604916420 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE SPOILERS MALFUNCTIONED A A6WAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL31429AW2918 7711 (CONFIG SPOILER) CAS MESSAGE ILLUMINATED ON TAKEOFF, ABORTED TAKEOFF. PERFORMED BELOW 20 KNOTS. REMOVED AND REPLACED SECU NR 1 IAW AMM. OPS CHECK GOOD. (K) 2L72 4F4 FRTA21EA E15NE 20050726000512005072600051 2005 7 26 GTIA050161 420050601A3417 CADC DOUG DC9 DC981 3022081WP NR 2 FAILED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23811NK 48017 CLIMBING THROUGH FL260 LOST ALL AUTO FLIGHT PARAMETERS, F/O ALT WAS 300 FT OFF, NO ALTITUDE ALERT. PASS THROUGH 250 DESCENT EVERYTHING STARTED TO COME BACK BUT WOULDN’T STAY ON, NO C/B`S POPPED, NO ANNUNCIATORS. AIR RETURN BACK TO DTA, AIRCRAFT TAIL SWAP WITH N804NK. REMOVED AND REPLACED NR 2 CADC. OPS CHECK GOOD. RTS AND AUTOLAND CHECKS OK. (M) 2L72 4F A6WE 20050726000522005072600052EA 2005 7 26 A6WA200540231 120050422A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAO OTHER O OTHER NRNOT REPORTED 1 GL31417AW 7610 MWC 134 LT FS 621 FLOOR SUPPORT ANGLE IS CRACKED. REPAIRED BY REMOVING DAMAGED SECTION OF ANGLE, FABRICATING AND INSTALLING REPAIR ANGLES IAW MFG REO. (K) 2L72 4F4 FRTA21EA E15NE 20050726000622005072600062SO 2005 7 26 SWIA200515308 120050716A3350 BULB EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07227SW 120304 FLOOR LEVEL EMERGENCY LIGHT AT 10A INOP. REPLACED LIGHT BULB FOR FLOOR LEVEL EMERGENCY LIGHT AT ROW 10A. OPS CHECK GOOD. 2L72 4T RTA31SO 20050726000662005072600066WP 2005 7 26 GTIA050160 120050528A2782 ACTUATOR DOUG DC9 DC983 3022083WP SLATS MALFUNCTIONED A GTIAO OTHER O OTHER TXTAXI/GRND HDL 1 GL23802NK 53168 DURING TAXI OUT, SELECTING FLAPS TO 11 FT THE AUTO-SLAT FAIL LIGHT ILLUMINATED AND THE DISAGREEMENT LIGHT REMAINED ON, RETURNED TO THE GATE AD AIRCRAFT TAIL SWAP WITH N811NK. ADJUSTED S1-467 NO HELP, REMOVED AND REPLACED S1-467 WITH SERVICEABLE UNIT FROM STOCK, STILL NO CURE. REMOVED AND REPLACED AUTO-SLAT ACTUATORS, BOTH AND ADJUSTED S1-467. OPS CHECK GOOD. (M) 2L72 4F RTA6WE 20050726000672005072600067NM 2005 7 26 GTIA05152005 120050515A5347 SEAT TRACK DOUG MD80 MD83 3023681NM FUSLEAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23 49793 FOUND CABIN SEAT TRACK CORRODED. REMOVED FLOOR PANELS. REMOVED DAMAGED SEAT TRACK AND FORWARD AND AFT GIRT MOUNTS. FABRICATED FORWARD AND AFT GIRT MOUNTS. LOCATED AND DRILLED NEW HOLES ON FABRICATED FORWARD AND AFT GIRT MOUNTS. LOCATED AND DRILLED NEW SEAT TRACK. TREATED AND PRIMED AND TOP COATED SEAT TRACK. INSTALLED NEW FABRICATED SEAT TRACK. INSTALLED FLOORBOARD. HEAT TREATED 2 GIRT BAR MOUNTS. TREATED AND PRIMED TWO GIRT BAR MOUNTS. TOP COATED TWO GIRT BAR MOUNTS. INSTALLED TWO GIRT BAR MOUNTS. INSTALLED LEFT SIDE OUTBOARD WEB FLOOR PANELS. (M) 2L72 4F RT 20050726000682005072600068NE 2005 7 26 GUU2005F00029 220050704A7261 ENGINE EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE RIGHT OVERSERVICED A GUUAA UNSCHED LANDING WBJINADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SO29280AS 120231 AFTER TAKEOFF, MAIN HYDRAULIC PUMP PRESSURE LIGHT ILLUMINATED. NOTICED A SMELL AND SMOKE ENTERED THE COCKPIT AND CABIN. RETURNED AND LANDED WITHOUT INCIDENT. DETERMINED RT ENGINE TO BE OVERSERVICED. SERVICED TO PROPER LEVEL. OPERATIONAL CHECKS OF BOTH COOLING PACKAGES NORMAL. NO SMOKE NOTED. 2L72 4T4 TRTA31SO E20NE 20050726000712005072600071CE 2005 7 26 DXTA200500857 120050724A324199123052 TRANSDUCER CESSNA560 560XL 2076702CE RT MLG INOPERATIVE E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07696QS2475 5605296 ON TAKEOFF ROLL, APPROACHING 60K MASTER CAUTION LIGHT ILLUMINATED WITH ANTI-SKID ANNUNCIATOR LIGHT SWITCHES PROPER POSITION, TAKEOFF ABORTED. T/S TO BAD RT WHEEL TRANSDUCER. INSTALLED NEW TRANSDUCER OP'S CHECKS SATISFACTORY AT THIS TIME. ALL WORK DONE IAW CE 560 XL M/M 32-40-00. 2L72 4F RTA22CE 20050721001562005072100156NM 2005 7 21 SWAA052108 120050718A27106960081 ROD BOEING737 7373H4 1384600NM RT AILERON WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED C2 CHECK, RT WING AILERON FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED RT AILERON CONTROL ROD PER MM. 2L72 4F RTA16WE 20050721001572005072100157NM 2005 7 21 SWAA052109 120050716A5330BAC15123364 STRAP BOEING737 7373H4 1384600NM FUSELAGE SKIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29613SW 27931 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN STRAP CRACKED AT BS 440, STR 24R. REMOVED AND REPLACED SKIN STRAP SECTION PER SRM. 2L72 4F RTA16WE 20050721001592005072100159NM 2005 7 21 SWAA052111 120050719A53126545409 PRESSURE PANEL BOEING737 7373H4 1384600NM MLG WW CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESS WEB CRACKED AT BS 664, LBL 39. REPAIRED WEB PER SWA EA. 2L72 4F RTA16WE 20050721001602005072100160NM 2005 7 21 SWAA052115 120050719A53126546568 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED 1/4D CHECK, FOUND 4 EA CRACKS AT BS 1016 PRESS BULKHEAD WEB, STR 1 TO STR 7R. REPAIRED WEB PER SWA EA. 2L72 4F RTA16WE 20050721001652005072100165SO 2005 7 21 RAIA00507013 120050719A36108151131 DUCT EMB 145 EMB145 3260210SO BLEED AIR SYSTEMLEAKING A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03805HK 145096 FLT 3524 - STL - BLEED 2 LEAK INDICATION. MAINTENANCE REMOVED AND REPLACED BLEED HOSE DUCT. 2L72 4F RTT00011AT 20050721001692005072100169EA 2005 7 21 COMA0570083 120050711A7830 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA THRUST REVERSER ILLUMINATED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01653CA 10129 FLIGHT 5430 - LEFT REVERSER UNSAFE. DEFERRED MAINTENANCE PER MEL. 2L72 4F RTA21EA 20050721001722005072100172EA 2005 7 21 COMA0570085 120050715A5320 STRIKER CNDAIRCL600 CL6002C10 1390015EA FUSELAGE BENT A COMAK NONE O OTHER ININSP/MAINT 1 SO01317CA7613 10055 PASSENGER DOOR SEAL STRICKER IS DENTED. REPAIRS CARRIED OUT IAW BOMBARDIER REO 670-53-22-001 REV E REPAIR TYPE 1. 2L72 4F RTA21EA 20050721001752005072100175NM 2005 7 21 TSAA0532028 120050715A3230 LANDING GEAR BOEING737 7372T4 1384492NM MALFUNCTIONED A TSAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13807AL 23443 GEAR WOULD NOT RETRACT ON T/O FROM KONA. ISOLATION VALVE LIGHT CAME ON AND GEAR HANDLE COULD NOT BE RAISED PAST THE OFF POSITION. WITH GEAR HANDLE DOWN, WE HAD NO GEAR LIGHTS. VISUALLY CHECKED GEAR DOWN AND LANDED AT KONA. INSPECTED LANDING GEAR SYSTEM AND FOUND LANDING GEAR LIGHTS CIRCUIT BREAKER OPEN. RESET CIRCUIT BREAKER AND CHECKED OK. NO FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A16WE 20050721001792005072100179SO 2005 7 21 CHQA200500129 120050720A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11279SK 145379 REAR CEILING EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED THE AFT CEILING EMERGENCY LIGHT BULB IAW EMB 145 MM 33-50-08. OPS CHECK GOOD IAW EMB 145 J/C E33-50-00-710-001. 2L72 4T RTT00011AT 20050721001952005072100195NM 2005 7 21 AALA20050443 120050715A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHTSDISCHARGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21930AN 29529 EMERGENCY LIGHT AT ROWS 14, 16, 17 AND 20 INOPERATIVE. REPLACED BATTERY PACK AT ROW 19 FOR EMERGENCY LIGHT AT ROWS 14, 16, 17, AND 20. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20050721002042005072100204NE 2005 7 21 AALA20050437 220050711A7314 PUMP DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE NR 1 ENGINE FUELMALFUNCTIONED A AALAO OTHER JY WARNING INDICATION ENGINE STOPPAGE APAPPROACH 1 SW21490AA 49683 728109 ABOUT 2000 FT ABOVE GROUND LEVEL ON FINAL APPROACH, GOT LT FUEL INLET LOW LIGHT. SHORTLY AFTER THAT NR 1 ENGINE FAILED. REPLACED LT WING TANK PROBES NUMBER 5 THROUGH 12, LT WING TANK COMPENSATOR, RT WING TANK PROBES NUMBERS 6, 5, 9, 10, AND 11 AND RT WING TANK COMPENSATOR. PERFORMED BIOBORE TO ALL FUEL TANKS AND REPLACED LT ENGINE FUEL CONTROL AND FUEL PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 F A6WE E9NE 20050721002062005072100206WP 2005 7 21 AALA20050436 120050710A2150 SHUTOFF VALVE DOUG DC9 DC982 3022082WP PRESS REGULATINGINOPERATIVE A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SW217543A 53025 DURING TAKEOFF AND INITIAL CLIMB WITH TAKEOFF POWER, HOT AIR CONDITIONING PACK ODOR WITH HAZE FILLED CABIN AND COCKPIT. HAZE AND ODOR DISSIPATED A FEW MINUTES AFTER CLIMB POWER SELECTED AND REST OF FLIGHT NORMAL. APU WAS OFF. ACCOMPLISHED REPLACEMENT OF LT AND RT AIR CONDITIONING PRESSURE REGULATING SHUT OFF VALVE. PERFORMED PACK BURN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050722000282005072200028NM 2005 7 22 HNAA0500071 120050718A79318D1437 TRANSMITTER DHAV DHC8 DHC8201 2809001NM OIL PRESSURE CONTAMINATED A HNAAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 EA07996HA1640316403 509 NR 1 ENGINE OIL FLUX IN FLIGHT. CLEANED CONNECTOR ON NR 1 OIL PRESSURE TRANSMITTER, SERVICED ENGINE WITH 2 QTS OF OIL. REMOVED AND REPLACED OIL PRESSURE INDICATOR AS A PRECAUTION. GROUND RUN A/C NO FLUX NOTED. 2H72 4T RTA13NM 20050722000392005072200039SO 2005 7 22 SWIA200515292 120050717A3320 LIGHT EMB 120 EMB120ER 3260203SO SEAT 7A SMOKE A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM07581SW 120349 CABIN FLUORESCENT LIGHT AT SEAT 7A PRODUCED SMOKE. REPLACED CABIN LIGHT RECEPTACLE AT ROW 7A. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050722000582005072200058NM 2005 7 22 TSAA0557027 120050718A57546546423277A SLAT BOEING737 7372T4 1384492NM NR 3 INFLT SEPARATIONA TSAAO OTHER D INFLIGHT SEPARATION NRNOT REPORTED 1 WP13808AL 23445 AFTER ARRIVAL IN LIH A PASSENGER ADVISED THE FLIGHT ATTENDANT THAT PART OF THE WING SEPARATED IN FLIGHT. CAPTAIN THEN OBSERVED A SECTION OF THE NUMBER THREE LEADING EDGE SLAT MISSING. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE LEADING EDGE SLAT ASSEMBLY AND VERIFIED GROUND OPERATION OK. 2L72 4F A16WE 20050722000782005072200078NM 2005 7 22 AWXA200500834 120050606A53126546568520 ANGLE BOEING737 7373G7 1384595NM BULKHEAD CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED CORROSION ON AFT PRESSURE BULKHEAD CENTER STIFFENER ANGLE AT BS 1016, FROM WL 150 TO WL 180, BL 0. MAINTENANCE REMOVED CORROSION ON STIFFENER ANGLE AT BS 1016, FROM WL 150 TO WL 180, BL 0 AND FOUND TO BE OUT OF LIMITS IAW BOEING 737-300. DAMAGED SECTION OF THE ANGLE WAS REMOVED FROM STIFFENER ANGLE AT BS 1016, FROM WL 150 TO WL 180, BL 0 IAW BOEING 737-300 SRM 51-70-11-0 FIG. 1. FABRICATED REPAIR ANGLE AND FILLER IAW BOEING 737-300 SRM 51-70-11-0 FIG. 1. FABRICATED REPAIR PARTS WERE INSTALLED AT AFT PRESSURE BULKHEAD CENTER STIFFENER ANGLE AT BS 1016, FROM WL 150 TO WL 180, BL 0 IAW BOEING 737-300 SRM 51-70-11-0 FIG 1.IAW BOEING 737-300 SRM 51-70-11-0 FIG 1.2L72 4F RTA16WE 20050722000822005072200082NM 2005 7 22 AWXA200500838 120050706A534069353521 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED STRINGER TIE 25R CRACKED ON AFT SIDE OF BS 947. MAINTENANCE REMOVED CRACKED STRINGER TIE IAW BOEING 737-300 SRM 51-40-02-0 FIG 8. FABRICATED NEW STRINGER TIE IAW BOEING 737-300 SRM 51-40-05-0 FIG 2 AND BOEING DRAWING 69-35352. INSTALLED FABRICATED STRINGER TIE AT STR 25R, AFT SIDE OF BS 947 IAW BOEING 737-300 SRM 51-40-02-0 FIG 8, AND 12. 2L72 4F RTA16WE 20050722000862005072200086 2005 7 22 SF20050721 420050721A3417 ADC SAAB SF340 SF340A 7850100EU COCKPIT MALFUNCTIONED A UHLAA UNSCHED LANDING S AFFECT SYSTEMS CRCRUISE 1 GL17123XS 123 FLIGHT 9003 FWA-DAY, PILOT CALLED ON THE RADIO REPORTING THE CAPTAIN'S ALTIMETER AND VERTICAL SPEED INDICATOR WERE FLUCTUATING 20-40 FT, CAUSING THE AUTO-PILOT TO FOLLOW WITH A PITCH UP AND DOWN FLUCTUATION. AIRCRAFT WAS TOLD TO RETURN TO FWA. AIR DATA COMPUTER WAS REPLACED. 2L72 4T RTA52EU 20050722001032005072200103NM 2005 7 22 AWXA200500831 120050719A3350 LIGHT BOEING737 737301 1384611NM EMERGENCY EXIT INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 DEN - EEL - DURING 4 DAY CHECK DISCOVERED THE EMERGENCY EXIT LIGHT AT ROW 19C IS INOPERATIVE. MAINTENANCE PLACED ON MEL. REQUIRES NEW LIGHT ASSEMBLY. 2L72 4F RTA16WE 20050722001092005072200109EU 2005 7 22 05FDEA01991 120050718A7830 ANGLE AIRBUS300 A300F4605R 3930327EU THRUST REVERSER CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25656FE R632020 745 NR 2 ENGINE THRUST REVERSER CHAFED AREA ON INNER BODY LOWER ANGLE. 2L72 4F RTA35EU 20050722001192005072200119EU 2005 7 22 05FDEA01962 120050715A2910AE2463774G0164 HOSE AIRBUS310 A310 EU HYD SYSTEM LEAKING A FDEAG O2 MASK DEPLOYED KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO25425FE 264 AT APPROXIMATELY 1000 FT ON CLIMB-OUT RECEIVED ECAM WARNING FOR GREEN HYD SYSTEM RESERVOIR LOW. THIS CONFIRMED ON OVERHEAD PANEL ACCOMPLISHED ECAM ITEMS AND RED TABS. GEAR EXTENDED BY GRAVITY EXTENSION METHOD SYSTEM QTY DID NOT GO TO ZERO. FOUND RUPTURED LINE ON LEFT MAIN GEAR SIDE STRUT LOCK ACTUATOR. ROBBED LINE OFF ACFT 402 TO RETURN 425 TO SERVICE. ALSO, RESTORED GEAR SYSTEM TO NORM AFTER EMERGENCY EXTENSION PER MM REF 32-33-00-2 AND SERVICED HYD FLUID PER MM REF CHPTR 12 ACFT GOOD FOR CONTINUE SERVICE. 2L72 4F RTA35EU 20050722001232005072200123NM 2005 7 22 AWXA200500824 120050701A5542 SKIN BOEING737 7373G7 1384595NM RUDDER DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 0155 23777 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED FIBER DAMAGE ON LT SIDE OF RUDDER SKIN PANEL AT RUDDER STA 103. MAINTENANCE CUT OUT DAMAGED PLIES ON THE LT SIDE OF THE RUDDER AT STA 103 IAW BOEING 737-300 SRM 51-70-04-0 FIG 10. SANDED, CLEANED AND PREPPED AREA ON RUDDER SKIN FOR BONDED REPAIR. BONDED REPAIR PLYS TO RUDDER SKIN PANEL IAW BOEING 737-300 SRM 51-70-04-0 FIG 10. PERFORMED BALANCING OF THE RUDDER ON JIG IAW BOEING 737-300 SRM 51-60-07-0 FIG 2, 0 WEIGHT WAS ADDED. JIG WAS ALSO BALANCED IAW BOEING 737-300 SRM 51-60-07-0. 2L72 4F RTA16WE 20050722001262005072200126 2005 7 22 AWXA200500828 420050716A2565D31516313 SLIDE AIRBUSA319 A319132 3930340NM L1 DOOR FAILED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28804AW18103236 1043 DURING 4 DAY CHECK DISCOVERED L1 DOOR ESCAPE SLIDE PRESSURE INDICATING ZERO. MAINTENANCE REMOVED AND REPLACED L1 DOOR SLIDE IAW AMERICA WEST AIRLINES TASK CARD R1C25304. VENDOR TEAR DOWN REPORT CONFIRMS REASON FOR REMOVAL. UNIT WAS RECEIVED AND FOUND RESERVOIR ASSEMBLY WITH LOW PRESSURE, DAMAGED GAGE AND DAMAGED SAFETY PIN. RESERVOIR ASSEMBLY WAS REPAIRED WITH THE GAGE, SAFETY PIN AND GAGE WINDOW BEING REPLACED. SERVICE BULLETIN A320 004-25-72 WAS PERFORMED AND EO 2561-01018 WAS COMPLIED WITH. ALL WORK WAS PERFORMED IAW CMM 25-60-56 REV 11. 2L72 4F RTA28NM 20050722001322005072200132NM 2005 7 22 2005UALA00648 120050712A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29504UA 24625 FUSELAGE STATION 1598, STR 19R HAS DAMAGE. SUPPLEMENTAL DATA UPDATE, REMOVED AND REPLACE REPAIRED DOUBLER AT FUSE STA 1598, STR 19R PER TIMCO EA REO-G10703 AND UA-EVA-50446. 2L72 4F4 FRTA2NM E17NE 20050722001342005072200134NM 2005 7 22 2005UALA00650 120050712A339759193 WIRE BOEING757 757222 1384956NM PWA 2037 PW2037 NE EMERGENCY LIGHT DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29504UA 24625 EEL JUMPER AND FEEDER DAMAGED AT STA 895. DAMAGED EEL CABLE WAS REPLACED 2L72 4F4 FRTA2NM E17NE 20050722001352005072200135NM 2005 7 22 2005UALA00651 120050712A3350582240 POWER SUPPLY BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE EMERGENCY LIGHT DISCHARGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29657UA 27112 EMERGENCY LIGHTS L900, L908 AND L976 ON WITH SW IN ARMED POSITION. BATTERY PACK NOT HOLDING CHARGE. REPLACED OK. 2L72 4F4 FRTA1NM E24NE 20050722001422005072200142EU 2005 7 22 2005UALA00658 120050713A5320 FLOOR SUPPORT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29457UA 1146 CABIN FLOOR SUPPORT CORRODED IN 5EA PLACES BETWEEN FRAME 66 AND FRAME 68. SUPPORT IS BETWEEN FLOOR PNL 262EF AND 262FF. SEAT TRACK FLOORBEAMS CORRODED AND REPLACED. REPLACEMENT OF A PSE IS CONSIDERED MAJOR REPAIR. 2L72 4F4 FRTA28NM E40NE 20050722001752005072200175EU 2005 7 22 USAA050788 120050623A5320 SILL AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19721UW17844 1095 FOUND SILL PLATE CORRODED 1 INCH BY 3 INCH AREA, FRAME 66, COMMON TO SILL PLATE. ACCOMPLISHED SRM REPAIR 53-41-14 FIG 201 SHT 4, REPAIR PRINCIPLE 6. CORROSION LEVEL 2, TASK JA-260-53500. (M) 2L72 4F RTA28NM 20050722001942005072200194 2005 7 22 2005UALA00642 420050708A3442 RADAR BOEING757 757222 1384956NM PWA 2037 PW2037 NE WX SYSTEM FAILED A UALAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 WP29575UA 26689 WEATHER RADAR FAILED JUST AFTER TAKEOFF. FLIGHT DIVERTED DUE TO THUNDERSTORMS. MAINTENANCE REPLACED THE RADAR ANTENNA ASSY (P/N 2041444-0401). THE COMPONENT SHOP TESTING DID NOT REVEAL ANY FAILURES, HOWEVER THE AZIMUTH GEAR ASSY WAS FOUND WITH WATER CONTAMINATION. THE GEAR ASSY WAS DRIED AND THE ANTENNA DRIVE ASSY OPERATIONALLY CHECKED GOOD. THE AIRCRAFT HAS FLOWN WITHOUT RADAR PROBLEMS SINCE 9 JULY. 2L72 4F4 FRTA2NM E17NE 20050722001952005072200195EU 2005 7 22 2005UALA00643 120050711A3350 LIGHT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE 1L DOOR SLIDE WILL NOT TEST A UALAK NONE L NO TEST ININSP/MAINT 1 WP29402UA 439 WHILE PERFORMING EMERGENCY LIGHT TEST FAILED WITH MESSAGE EXT LOADS FWD LEFT. REPLACED SLIDE. 2L72 4F4 FRTA28NM E40NE 20050722001982005072200198NM 2005 7 22 MASA200500560 120050718A324221599 BRAKE ASSY DHAV DHC8 DHC8202 2809007NM MLG FAILED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07437YV423 437 ASH 6934 PSP. CREW REPORTED RT BRAKES FAILED DURING TAXI AND RT OB MLG TIRE FLAT. MX REPLACED THE #4 BRAKE. 2H72 4T RTA13NM 20050722002002005072200200NM 2005 7 22 SB05084 120050722A335020121 POWER SUPPLY BOEING737 7374B7 1384702NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19430US 24552 MAINTENANCE REPORTED THE AFT LEFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050725000022005072500002CE 2005 7 25 VJ32005F00001 120050623A55343364000039 FITTING BEECH 33 F33A 1151425CE CONT O520 IO520* 17032SO VERTICAL STAB CRACKED B VJ3RO OTHER O OTHER NRNOT REPORTED 1 WP075530A17445 CE1342 WHILE PERFORMEING UNSCHEDULED MAINTENANCE. VERTICAL STABILIZER WAS REMOVED, WHILE THE MECHANIC WAS INSPECTING THE FITTINGS FOR REINSTALLATION OF THE VERTICAL STABILIZER NOTICED A CRACK COMING FROM BOTTOM RT LOWER MOUNTING HOLE ON FORWARD FITTING. AT THIS TIME NO PROBABLE CAUSE OR RECOMMENDATION. (K) 1L71 3O3 O 3A15 E5CE 20050725000122005072500012EU 2005 7 25 UPS05144942 120050720A5210 BOTTLE AIRBUSA300 A300F4622R 3930360EU DOOR ASSIST LOW A IPXAK NONE O OTHER ININSP/MAINT 1 SO01135UP 0818 PREFLIGHT FOUND ESCAPE BOTTLE NITROGEN BELOW LIMITS SERVICED TO PSI. 2L72 4F RTA35EU 20050725000202005072500020WP 2005 7 25 UPS05844940 120050709A53476015176S277266 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C1, MAIN CABIN SEAT TRACK PLUGS HAVE CORROSION AT STA 500 BL0. REMOVED DAMAGED SEAT TRACK, FABRICATED AND INSTALLED SEAT TRACK SECTION IAW SRM 53-2-3 FIG 8A, FIG 12, AND 51-3-0. 2L74 4F RT4A25 20050725000362005072500036NM 2005 7 25 PIDA20050060 120050719A3350 BULB BOEING757 757236 1384971NM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05757BJ 22176 R4 AND L2 EXTERIOR EMERGENCY EXIT LIGHTS INOP. REPLACED BULBS AT R4 AND L2 EXTERIOR EMERGENCY EXIT LIGHTS PER MM 33-50. OPS CHECKS GOOD. 2L72 4F RTA2NM 20050725000422005072500042EU 2005 7 25 07152005C 120050715A2611 WARNING LIGHT SAAB SF340 340B 7860101EU SMOKE DETECTOR ILLUMINATED A NSVAFA ACTIVATE FIRE EXT. UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27312CE 334 5 MINUTES AFTER TAKEOFF GOT INTERMITTENT CARGO WARNING FOLLOWED BY STEADY WARNING. 2L72 4T RTA52EU 20050725000522005072500052NM 2005 7 25 CALA0500237 120050722A5320143N584570 FLOOR SUPPORT BOEING757 757224 1384958NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713110 27300 INSPECTION FOUND FLOOR SUPPORT CORRODED BETWEEN STA 700 AND 720, RBL 16. REPAIRED IAW ECRA 5310-04482. 2L72 4F RTA2NM 20050725000552005072500055EU 2005 7 25 ALG2005F00036 120050630A6730 ACCUMULATOR UROCOPEC120 EC120B 8680987EU TMECA ARRIUSARRIUS2B1 NE MALFUNCTIONED E ALGAO OTHER O OTHER HOHOVERING 1 SW03524AL 1263 34281 AT HOVER FOR TAKEOFF, PICKED AIRCRAFT UP TO A HOVER 2 TIMES AND BOTH TIMES AT A STEADY HOVER, AIRCRAFT OSCILLATED FORE AND AFT WITH NO PILOT INPUT (NOSE UP AND DOWN). MAINTENANCE INSPECTED SERVO INPUTS FOR WEAR, NO DEFECTS FOUND, SERVICED SERVO CONTROL ACCUMULATOR IAW THE EC-120 MM. THE GROUND RUN AND HOVER CHECK WAS GOOD. (K) 1G72 3U3 UNCR0001RD E34NE 20050725000582005072500058CE 2005 7 25 07242005A 120050724A28101183890051 SHUTOFF VALVE BEECH 1900 1900D 1154162CE FIREWALL STUCK A NSVAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA27220CJ UE20 RIGHT ENGINE STANDBY BOOST PUMP INOP. FOUND FIREWALL VALVE STUCK IN CLOSED POSITION 2L72 4T RTA24CE 20050726000192005072600019WP 2005 7 26 ABXA050169 120050624A531199118603 FRAME DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23978AX 47628 FRAME CRACKED 3 PLACES - FS 1185 AT LONGERON 6 AND 7 LEFT. REMOVED AND REPLACED FRAME IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20050726000302005072600030EA 2005 7 26 SWIA200515305 120050719A2750855D1007 SENSOR CNDAIRCL600 CL6002B19 1900309EA BRAKE POSITION MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07416SW8 8 7089 FLAPS FAIL .17 DEGREES ON APPROACH INTO SLC. REMOVED AND REPLACED NR 1 BPSU AND RIGGED LEFT AND RIGHT BPSU IAW CRJ 27-51-10. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050726000312005072600031NM 2005 7 26 AALA20050450 120050719A3350 LIGHT BOEING757 7572Q8 1384972NM CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21707TW 27625 DFW FLOOR EMERGENCY ESCAPE PATH LIGHTING SEGMENT AT SEAT 1AB INOPERATIVE. REPLACED FLOOR EMERGENCY ESCAPE PATH LIGHTING SEGMENT ASSEMBLY AT SEAT 1AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA2NM 20050726000322005072600032EU 2005 7 26 AALA20050456 120050720A3520 OXYGEN MASK AIRBUS300 A300B4605R 3930308EU CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217082A 643 JFK OXYGEN MASKS AT SEATS 11FG INOPERATIVE. SECURED OXYGEN MASK PANEL AT SEATS 11FG. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA35EU 20050726000332005072600033NM 2005 7 26 AALA20050447 120050717A3350 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21780AN 29956 DFW EMERGENCY PATH LIGHTING IN COACH INOPERATIVE. REPLACED BATTERY PACK M33401 FOR EMERGENCY PATH LIGHTING IN COACH. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTT00001SE 20050726000352005072600035WP 2005 7 26 AALA20050449 120050718A3350 CONNECTOR DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21498AA 49736 SFO EMERGENCY LIGHT ON SEAT 15D AND OVERHEAD EMERGENCY LIGHT I VENTRAL STAIRWELL INOPERATIVE. RECONNECTED CONNECTOR FOR EMERGENCY LIGHT ON SEAT 15D AND OVERHEAD EMERGENCY LIGHT IN VENTRAL STAIRWELL. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F A6WE 20050726000492005072600049 2005 7 26 GTIA050164 420050610A3454 RECEIVER DOUG DC9 DC982 3022082WP VOR-ILS FAILED A GTIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL23803NK 48087 GPR POS FAIL EN ROUTE, HEADING INDICATION ON RADAR DISPLAY, AIRCRAFT TAIL SWAP WITH N814NK. PERFORMED OPERATIONAL CHECK OF UNS1K SYSTEM, OPS CHECK GOOD. REMOVED AND REPLACED NR 1 RECEIVER VOR/ILS. OPS CHECK GOOD. (M) 2L72 4F A6WE 20050726000502005072600050NE 2005 7 26 GTIA050162 220050601A7200 ENGINE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE NR 2 FAILED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23834NK 49847 RT ENGINE FAILURE DURING CLIMB THROUGH 22,000 FT, COMPRESSOR STALLED, EGT 710 FEET ENGINE ROLLED BACK AND SHUTDOWN. FOUND TURBINE SECTION FAILED. REMOVED AND REPLACED NR 2 ENGINE. OPS CHECK AND LEAK CHECK GOOD. (M) 2L72 4F4 FRTA6WE E9NE 20050726000542005072600054WP 2005 7 26 GTIA050163 120050604A7810 NOZZLE DOUG DC9 DC982 3022082WP NR 1 ENGINE CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23803NK 48087 NR 1 ENGINE NOZZLE HAS A 1 INCH CRACK AT 7 O`CLOCK POSITION NEAR EDGE OF NOZZLE, AIRCRAFT TAIL SWAP WITH N811NK. ACCOMPLISHED EA 7830-0501 IN LEFT THRUST REVERSER OUTBOARD EXTERNAL NOZZLE, INTERIM STOP DRILL REPAIR INSTALLED. LP NR 0299826-2. REMOVED AND REPLACED LEFT THRUST REVERSER ASSEMBLY, OPS CHECK AND LEAK CHECK GOOD. (M) 2L72 4F A6WE 20050726000552005072600055NE 2005 7 26 2005000011 220050719A7314 PUMP DOUG DC10 DC1030 3023501WP GE CF6 CF650C2B 30018NE FUEL SYSTEM FAILED A CNMAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 SW0717085 47957 455132 REJECTED TAKE OFF AT 80 KNOTS NR 2 ENGINE WILL NOT MAKE POWER ONLY WENT TO 110 PERCENT N1 LOWER THAN 1&3. CORRECTIVE ACTION REMOVED AND REPLACED THE FUEL PUMP AND M.E.C. STILL IN WORK. 2L73 4F4 F A22WE E23EA 20050726000562005072600056SO 2005 7 26 CHQA200500131 120050722A27513633501003 VELOCITY SENSOR EMB 135 EMB135LR 3260305SO TE FLAPS UNSERVICEABLE A CHQAO OTHER J WARNING INDICATION DEDESCENT 1 GL11842RP5795 5795 145661 WHILE DESCENDING OUT OF 12,000 FT, FLAP FAIL EICAS MESSAGE ASSOCIATED WITH SPS ADV MESSAGE APPEARED ON EICAS. RAN QRH & ADJUSTED LANDING SPEEDS. NOTIFIED APPROACH CONTROL & DECLARED AN EMERGENCY. RAN CHECKLISTS, DESCENT & APPROACH. LANDING NORMAL, LONGER THAN USUAL. ROLLED OUT TO THE END OF THE RUNWAY, 18R. FIRE DEPART ASKED A/C TO PARK ON A PERPENDICULAR TAXIWAY & EXAMINED OUR BRAKES. ALL FOUR BRAKE SENSORS WERE INDICATING HIGH BRAKE TEMPS. FIRE DEPART MADE AWARE THAT RT BRAKE TEMP INDICATING 400 DEGREES & CHOCKED A/C UNTIL COOL BRAKES DOWN WITH A FAN. BRAKES COOLED DOWN RAPIDLY AND TAXIED TO THE GATE. MX REMOVED AND REPLACED THE NR 1 FLAP VELOCITY SENSOR IAW EMB 135 AMM 27-51-12. OPS CHECK GOOD. 2L72 4F RTT00011AT 20050726000632005072600063SO 2005 7 26 SWIA200515309 120050720A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT DISCHARGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07227SW9809 9809 120304 ONE SECTION OF EMERGENCY EXIT LIGHTS DIM. REPLACED MIDDLE ELBP IAW MM 33-50-02. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050726000652005072600065EA 2005 7 26 SWIA200515311 120050720A5230 HANDLE CNDAIRCL600 CL6002B19 1900309EA CARGO DOOR OUT OF ADJUST A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07916SW 7634 FA REPORTS THAT MCD HANDLE WAS VERY HARD TO OPEN. ADJUSTED LOWER TENSION TIES IAW MM 52-11-49. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050726000692005072600069NM 2005 7 26 GTIA050173 120050504A5330 SKIN DOUG MD80 MD83 3023681NM FUSELAGE DENTED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23827NK 49793 FOUND DENT AT FS 278 BETWEEN LONGERONS 17L AND 18L. CHEMICALLY REMOVED PAINT. CUT OUT DAMAGED AREA. FABRICATED TWO STRAPS, 2 FINGER DOUBLER, TWO DOUBLERS, AND 1 FILLER. TREATED AND PRIMED REPAIR PARTS. INSTALLED REPAIR. PAINT DONE. (M) 2L72 4F RT 20050726000782005072600078NM 2005 7 26 AWXA200500846 120050722A2420 GENERATOR AIRBUSA319 A319132 3930340NM NR 2 FAILED A AWXAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 WP28816AW 1350 IAD - EMERGENCY LANDING - FLT 859 - DURING CLIMB-OUT OF IAD, NR 2 GEN DROPPED OFF LINE. APU WAS ON MEL, INOPERATIVE. CREW RESET THE GENERATOR AND DIVERTED INTO CMH FOR PRECAUTIONARY REASONS, LANDING WAS UNEVENTFUL. MAINTENANCE RE-ISSUED APU MEL FOR BLEED AIR AND DIFFERED NR 2 ENGINE GENERATOR. CONTINUED ONTO PHX WITHOUT FURTHER EVENTS. . 2L72 4F RTA28NM 20050726000792005072600079WP 2005 7 26 ARWA20050701 120050719A3230ACG7328503 BUNGEE CORD DOUG DC10 DC1030 3023501WP NLG BROKEN A ARWAK NONE O OTHER ININSP/MAINT 1 SO19524MD 46999 DURING PRE-FLIGHT, FOUND NOSE GEAR, ONE OF THE SPRINGS FOUND BROKEN (RT NOSE SPRING BUNGEE). REMOVED AND REPLACED RT BUNGIE SPRING IN ACCORDANCE WITH M/M 32-22-01. NO ADJUSTMENT REQUIRED. 2L73 4F A22WE 20050726000832005072600083WP 2005 7 26 0501059996 120050716A217017946081 COALESCER BAG DOUG DC9 DC931 3022065WP LEFT DIRTY A NWAAI CABIN DEPRESSURIZATION BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DEDESCENT 1 GL018932E 47141 DURING INITIAL DESCENT AT ABOUT 1000 FPM, THE CABIN BEGAN A RAPID CLIMB OF OVER 1500 FPM. COM PROCEDURES WERE COMPLIED WITH BUT DID NOT HELP. WITH CABIN ALTITUDE CLIMBING ABOVE 10,000, CREW DONNED OXYGEN MASKS, DECLARED AN EMERGENCY, AND PERFORMED A RAPID DESCENT. ONCE AIRCRAFT WAS LEVEL AT 9000 FT AND ADDED POWER SETTINGS, THE CABIN PRESSURE RETURNED TO NORMAL CONTROL AND MADE A NORMAL DESCENT UNTIL LANDING. MAINTENANCE COULD NOT FIND ANY POSITIVE FAULT WITH THE SYSTEM AND REPLACED THE COALESCER BAGS. 2L72 4F A6WE 20050726000842005072600084EU 2005 7 26 DAT2005F00005 120050609A3244 TIRE STBROSSD3 SD360 8100606EU PWA PT6 PT6A65R 52043EA LT MAIN WHEEL FAILED E DATAO OTHER O OTHER NRNOT REPORTED 1 GL13360SA 226 SH3601 DURING DEPARTURE ON TAKEOFF ROLL, ACCELERATION WAS NORMAL THROUGH 85 KNOTS, FLIGHT CREW HEARD A NOISE OUTSIDE OF THE AIRCRAFT. AC STARTED TO PULL TO LT AND THERE WAS CORRECTION MADE TO STRAIGHTEN THE AIRCRAFT. FLIGHT CREW NOTICED DURING THE CORRECTION THE AC ROLLED MORE THAN USUAL. AT THIS POINT, AC WAS 5 KNOTS BELOW V-1 AND IT WAS DECIDED TO ABORT TAKEOFF. AC CONTINUED TO ROLL UNTIL IT CLEARED THE TAXIWAY. AC WAS PARKED TIL HSV MECHANIC COULD ARRIVE. REMOVED DAMAGED LT MAIN WHEEL AND REPLACED. DAMAGED HONEYCOMB LANDING GEAR POD ASSY WAS REPAIRED FOR INTENDED FERRY FLIGHT IN ORDER TO COMPLETE PERMANENT REPAIR. COMPLETED FERRY FLIGHT AND IS CURRENTLY STILL UNDERGOING THE REPAIR. (K) 2H72 4T4 T A41EU E4EA 20050726000882005072600088 2005 7 26 DAT2005F00006 420050615A6122 LINE STBROSSD3 SD360 8100606EU PWA PT6 PT6A65R 52043EA HARTZLHCB5M HCB5MP3 GL PROP GOVERNOR CONTAMINATED E DATAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION APAPPROACH 1 GL13360RW SH3613 PCE97068 EVA2711 DURING FINAL APPROACH AND FINAL CHECKS, THE PROPS FWD THE RT ENGINE STARTED TO SURGE. POWER BROUGHT BACK ON RT ENGINE TO SLOW UP SURGE AND IT STOPPED SURGING MOMENTARILY AND THE GENERATOR AND OIL RT LIGHT ON THE CWP. THE NG`S WERE BELOW 50 PERCENT AND EMERGENCY CHECKLIST WAS FOLLOWING LEADING TO SHUTTING DOWN RT ENGINE. AC LANDED WITHOUT INCIDENT. AC WAS TAXIED BACK TO THE RAMP. MECHANIC REMOVED AND REPLACED THE PROP GOVERNOR IAW MM. THE PY LINE SYS WAS CHECKED AND WATER WAS FOUND IN IT. MECHANIC BLEW OUT THE WATER. GROUND OPS CHECKED, ENGINE AND PERFORMANCE RUNS WERE OK. AC WAS RETURNED TO SERVICE. (K) 2H72 4T4 T A41EU E4EA 6 CP44GL 20050726000932005072600093NM 2005 7 26 UPS05M44950 120050617A5347 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01255UP 48404 INSPECTION TYPE: C-CK , CORROSION ON SEAT TRACK AND FLANGE AT STA 919-957 X=-75. REMOVE CABIN CORROSION ON SEAT TRACK AND FLANGE AT STA 919-957 X=-75 AND FOUND EXCEED LIMIT AS PER SRM 53-70-00 FIG 3 VOL 1 REV 37, CARRY OUT HFEC IAW DAC NDT SPM REV 12. FABRICATION OF SPLICE PLATE AS PER SRM 53-70-00 FIG 1 VOL 1 REV 37, REWORKED AREA NEW SEAT TRACK, SPLICE HAT AND SPLICE PLATES REPROTECTED AS PER SRM 51-21-01 VOL II REV 37. 2L73 4F RTA22WE 20050726000942005072600094NM 2005 7 26 UPS05M44951 120050621A5347 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01255UP 48404 INSPECTION TYPE: C-CK, CORROSION ON SEAT TRACK AT STA 806-910 X=-75. REMOVED CABIN CORROSION ON SEAT TRACK AT STA 806-910 X=-75 AND FOUND EXCEED LIMIT AS PER SRM 53-70-00 FIG 3 VOL I REV 37. MANILFOLD FAILURE SENSING ELEMENT IN THE VICINITY OF CORRODED SEAT TRACK REMOVED AS PER AMM 36-23-07 REV 52 FOR SM ACCESS. CARRY OUT HFEC IAW DAC NDT SPM REV1 2, FABRICATED SPLICE PLATE AS PER SRM 53-70-00 FIG 1 VOL 1 REV 37. 2L73 4F RTA22WE 20050726001022005072600102NM 2005 7 26 GTIA050182 120050524A5320 CUSP WEB DOUG MD80 MD83 3023681NM FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23833NK 49449 FOUND CARGO COMPARTMENT FS 484-515 L18R CUSP WEB HAS CORROSION. REMOVED RT OUTBOARD FLOOR PANEL. CUT WEB OUT OF LIMIT 2 LOCATIONS 6 INCHES BY 8 INCHS BAND 16 INCHES BY 6 INCHES. FABRICATED REPAIR DOUBLERS AND FILLERS. TREATED AND PRIMED. INSTALLED DOUBLER AND FILLERS. (M) 2L72 4F RT 20050726001042005072600104EU 2005 7 26 TRBA2005043 120050613A2700 CONNECTOR AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE AILERONS/RUDDER DAMAGED A TRBAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO29355AT 355 WHILE TAXIING, AILERON AND RUDDER TRIM INDICATORS HAVE NO ELECTRICAL POWER. AIRCRAFT RETURNED TO BLOCKS. REPOSITIONED PIN C-13 IN CONNECTOR PLUG 15 AX. (K) 2H72 4T4 TRTA53EU E20NE 20050726001052005072600105NM 2005 7 26 GTIA050167 120050509A5320 CUSP WEB DOUG MD80 MD83 3023681NM FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23827NK 49793 FOUND CABIN STRINGER 18L CUSP CORRODED. REMOVED RETURN-AIR GRILL ASSEMBLY. REMOVED CABIN FLOORBOARDS. REMOVED FRAME TO FLOOR FITTINGS. REMOVED CUSP MEMBRANE. FABRICATED, LOCATED AND DRILLED REPLACEMENT WEB. TREATED, PRIMED AND TOPCOATED WEB. INSTALLED CUSP MEMBRANE AND FRAME TO FLOOR FITTINGS. INSTALLED RETURN AIR GRILL ASSEMBLY. INSTALLED CABIN FLOORBOARDS. (M) 2L72 4F RT 20050726001082005072600108EA 2005 7 26 SWIA200515304 120050720A274283963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07915SW5692 5692 7615 STAB TRIM CHANNEL 2 STATUS MESSAGE. REMOVED AND REPLACED HORIZONTAL STAB TRIM ACTUATOR AND MCU IAW CRJ 200 MM 27-42-01. OPERATIONAL CHECK GOOD, PN 7062-3, SN/OFF 851. 2L72 4F RTA21EA 20050726001092005072600109CE 2005 7 26 DXTA200500861 120050724A3234 HANDLE CESSNA750 750 2076810CE MLG LOCKED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07982QS 7500182 GEAR WOULD NOT RETRACT AFTER T/O HANDLE LOCKED IN DOWN POSITION T/O INDICATORS ON N1 STAYED ON AFTER POWER REDUCTION THEY WERE WHITE. ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20050726001102005072600110CE 2005 7 26 DXTA200500853 120050722A2130 WARNING LIGHT RAYTHNDH125 HAWKER800XP 7150012CE CABIN PRESSURE ILLUMINATED E DXTAB EMER. DESCENT J WARNING INDICATION CLCLIMB 1 GL07867QS 258576 DURING CLIMB-OUT, A LOUDER THAN NORMAL WIND NOISE WAS HEARD ON THE RIGHT SIDE OF THE COCKPIT. THE CABIN ALTITUDE CLIMBED AS HIGH AS 11500'. THE CABIN ALT LIGHT CAME ON AND THE HORN SOUNDED. KNOB PULLED MASKS DROPPED. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA3EU 20050726001132005072600113EU 2005 7 26 TRBA2005045 120050620A3220D227030721 SPRING AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE NLG DRAG BRACE BROKEN A TRBAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO29425MJ13728 425 (REF SDR2005045) ON GROUND, AFTER ENGINE START, AN UNSAFE LANDING GEAR INDICATION ON NR 2 PANEL WAS ON. FOUND NOSE GEAR SPRING BROKEN. REPLACED NOSE LANDING GEAR DRAG BRACE ASSEMBLY. 2H72 4T4 TRTA53EU E20NE 20050726001142005072600114NM 2005 7 26 GTIA050158 120050524A3610 SEAL DOUG MD80 MD83 3023681NM ACM DUCT LEAKING A GTIAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 GL23822NK 49392 TAIL COMPARTMENT TEMP HIGH LIGHT CAME ON AFTER TAKEOFF, AIR RETURN BACK TO FLL AND AIRCRAFT TAIL SWAP WITH N815NK. REMOVED AND REPLACED SEALS ON LEFT AND RIGHT ACM DUCTS, SECURED TWO LOOSE CLAMPS, RAN ENGINES AT ALL PARAMETERS. OPS AND LEAK CHECKS GOOD. (M) 2L72 4F RT 20050726001152005072600115WP 2005 7 26 GTIA050156 120050521A4920 CHECK VALVE DOUG DC9 DC982 3022082WP APU FAILED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23803NK 48087 ON APU START UP BOTH ENGINES WOULD GET ONLY 12 PERCENT N2, APU OIL TEMP HIGH LIGHT CAME ON, TAIL COMPARTMENT HIGH CAME ON, AIRCRAFT TAIL SWAP WITH N834NK. REMOVED AND REPLACED AIRSTART CHECK VALVE, LEAK CHECK GOOD. (M) 2L72 4F A6WE 20050726001172005072600117WP 2005 7 26 GTIA050152 120050501A3000 METER DOUG DC9 DC983 3022083WP COCKPIT FAILED A GTIAO OTHER N FALSE WARNING DEDESCENT 1 GL23814NK 49619 METER SEL AND HEAT INDICATION GOES RANDOMLY FROM FULL CURRENT (PEGGED) ON ALL SETTINGS EXCEPT "CAPT" "FO" AND "AUX" TO SOMETIMES JUST "RUD LIM" TO SOMETIMES JUST OFF PEGGED, AIRCRAFT TAIL SWAP WITH N835NK. REMOVED AND REPLACED METER SEL AND HEAT SWITCH, OPS CHECK GOOD. NO OTHER DEFECTS NOTED. (M) 2L72 4F RTA6WE 20050726001182005072600118EA 2005 7 26 ASOA05542 120050620A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT SHORTED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11826AS 7210 FLT 4408 - DURING A GROUND INSPECTION IN ATL, FIVE SECTIONS OF EMERGENCY FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE. UPON INSPECTION MAINTENANCE FOUND ONE SECTION OF EMERGENCY FLOOR LIGHTS SHORTED OUT CAUSING ALL FIVE SECTIONS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE SHORTED OUT EMERGENCY FLOOR LIGHT STRIP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050726001212005072600121NE 2005 7 26 MALA050582 220050716A7320230348403 SENSOR BAC 146 AVRO146RJ85A1500097EU PWA JT8 JT8D219 52053NE FADEC FAILED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15526XJ E2351 NR 1 ENGINE FADEC FAILED IN FLIGHT. REMOVED AND REPLACED NR 1 ENG T1 SENSOR, PN 2-303-484-03 IAW 75-30-01 OPS CHECK GOOD 2H74 4F4 FRTA49EU E9NE 20050726001222005072600122EU 2005 7 26 MALA050584 120050719A3234 BUSHING BAC 146 AVRO146RJ85A1500097EU MLG HANDLE FAILED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15505XJ E2313 AFTER DEPARTING LT AND RT MAIN GEAR INDICATORS DID NOT INDICATE UP AND THE GEAR INTRANSIT LIGHT REMAINED ON. RT MAIN LIGHT WENT OUT WHEN SLOWED TO 190. REPLACED BUSHINGS ON THE LT AND RT LEVER ASSY AND SHIMED LT FWD UPPER DOOR HINGE MOUNT POINT FUNCTIONAL CHECKS GOOD. NO INTRANSIT LIGHT GEAR INDICATES UP AND LOCKED WHEN SELECTED UP. 2H74 4F RTA49EU 20050726001232005072600123EU 2005 7 26 MALA050587 120050720A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15437XJ 340B437 DURING 4Y/2Y CHECK IN BNA FOUND LAV SEAT TRACK PROFILE PN 7253721-495 IS CORRODED AND HAS BEEN REPLACED IAW SRM 51-40-21. REF: EAMS WORK ORDER 212613 TASK 2526. 2L72 4T RTA52EU 20050726001262005072600126EU 2005 7 26 MALA050585 120050720A324450104882 TIRE SAAB SF340 340B 7860101EU MLG FLAT A MALAO OTHER O OTHER LDLANDING 1 GL15417XJ 340B417 RT MAIN TIRE MAY BE FLAT. PERFORMED A FLY BY AND A EMERGENCY LANDING AGTER A CONTRACT MECHANIC REPORTED TO THE CREW THAT HE OBSERVED A RT MAIN TIRE BLEW OUT ON THE TAKEOFF ROLL OUT OF SUX. POST FLIGHT IN MSP MAINTENANCE INSPECTED AND FOUND NOTHING WRONG. REPLACED RT MAIN TIRES AS A PRECAUTION. 2L72 4T RTA52EU 20050726001272005072600127EU 2005 7 26 MALA050588 120050720A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15437XJ 340B437 DURING 4Y/2Y CHECK IN BNA FOUND SEAT TRACK AT LBL18.3 IS CORRODED FROM FS297 TO FS319 AND HAS BEEN REPAIRED IAW MESABA EO#S53066. REF: EAMS WORKORDER 212613 TASK 2514 2L72 4T RTA52EU 20050726001282005072600128EU 2005 7 26 MALA050589 120050720A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15437XJ 340B437 DURING 4Y/2Y CHECK IN BNA FOUND SEAT TRACK AT BL 0 IS CORRODED FROM FS 297 TO FS 319 AND HAS BEEN REPAIRED IAW MESABA EO S53060. REF: EAMS WORK ORDER 212613 TASK 2513 2L72 4T RTA52EU 20050726001302005072600130EU 2005 7 26 MALA050594 120050718A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15438XJ 340B438 DURING 4Y/2Y CHECK IN BNA FOUND SEAT TRACK AT LBL 18.3 FROM FS 297 TO FS 319 IS CORRODED AND HAS BEEN REPAIRED IAW MESA EO S53060. REF. EAMS WORK ORDER 212646 TASK 1502 2L72 4T RTA52EU 20050726001332005072600133EU 2005 7 26 GTIA050157 120050521A3350 LAMP AIRBUSA321 A321211 3930370EU EMERGENCY LIGHT BURNED OUT A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23583NK 1195 SEVERAL LIGHTS BURNED OUT IN EMERGENCY EXITS SIGNS ABOVE L1, R1 AND R4 DOORS, AIRCRAFT TAIL SWAP WITH N825NK. RELAMPED EMERGENCY EXIT SIGNS IN CABIN AS REQUIRED, OPS CHECK GOOD. (M) 2L72 4F RTA28NM 20050726001352005072600135NM 2005 7 26 ASMF200507017 120050723A7400 IGNITION UNIT BOEING737 737724 13844BYNM NR 2 INOPERATIVE W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23904AM 28262 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF RIGHT ENGINE IGNITION DID FAILURE. MCDU SHOWED IGNITION 2 OUT OF SERVICE MESSAGE. THE FIM 74-21 PROCEDURE, TASKS 806 AND 807 AND BREAKER RESEAT WERE PERFORMED IAW MM 74-00-00, TESTED CORRECT. 2L72 4F RTA16WE 20050726001362005072600136EU 2005 7 26 DHL2005365005 120050723A2510 CALL HORN AIRBUS300 A300B4203 3930306EU MALFUNCTIONED A DHLAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01365DH 149 RTO RWR 27 MECHANIC CALL HORN ACTIVATED. MECHANIC CALL CURRENTLY DEFERRED. REF DMI 21755. NO PROVISIONS TO DEACTIOVATE CALL. BREIFED CREW. AC OK FOR SERVICE 2L72 4F RTA35EU 20050726001372005072600137NM 2005 7 26 DHL2005788003 120050723A3260 WARNING SWITCH BOEING727 727214 138407RNM NLG OUT OF ADJUST A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01788AT 21958 RED NOSE GEAR DOOR LIGHT FWD PANEL COMES ON AT 320 KT IAS. ADJUSTED NOSE GEAR DOOR WARNING SWITCHES. OPS CKS GOOD ON GROUND IAW 32-62-11. 2L73 4F A3WE 20050726001412005072600141EA 2005 7 26 A6WA200540226 120050701A3230 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA MLG FALSE INDICATIONA A6WAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL31458AW 7816 DURING GEAR RETRACTION, RECEIVED RED WARNING NOSE DOOR OPEN, GEAR DISAGREE LIGHT AND CAUTION STEERING INOPERATIVE WOW INPUT STATES MESSAGE WOW OUTPUT FAIL. RECONNETED TORQUE LINKS PERFORMED GEAR RETRACTIONS SWINGS IAW AMM CH23-30-00. NO DEFECTS OR WARNING NOTED SWINGS PERFORMED AFTER BOTH NLG TIRES CHANGED. INSPECTED NOSE FOR DAMAGE, NONE FOUND. (M) 2L72 4F RTA21EA 20050726001422005072600142WP 2005 7 26 ASMF200507018 120050724A5270 WARNING LIGHT DOUG DC9 DC982 3022082WP AIRSTAIR DOOR ILLUMINATED W ASMFA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW231003Y 48068 CAPTAIN REPORTED THAT AFTER TAKE OFF AFT STAIRWAY DOOR LIGHT TURN ON. DURING REVISION LEFT HOOK WAS DETECTED NOT SECURED AT AFT STAIRWAY DOOR. REPORT WAS DEFERRED IAW MEL 52-3, CAT D. AFTER, DURING PUSH BACK AT MEX THE AFT STAIRWAY DOOR LIGHT TURN ON. IT WAS NECESSARY TO VERIFY THROUGH TAIL CONE THAT THE STAIRWAY WAS CLOSED AND SECURED AND THE LIGHT TURN OFF IAW MM 52-70-00. 2L72 4F A6WE 20050726001432005072600143NE 2005 7 26 A6WA200540224 220050628A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE RIGHT FLAMED OUT A A6WAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION LDLANDING 1 GL31402AW 7281 RIGHT ENGINE FLAMED OUT ON LANDING ROLL, WHILE ATTEMPTING TO USE REVERSE THRUST. CHECKED RIGGING, ADJUSTED TO TOP OF LIMITS, CHECKED ATR, RIGGED, SET IDLE SPEED, PERFORMED POWER ASSURANCE ATR, N1 DISABLE TO ACCEL/DECEL IAW CRJ AMM CHP 71, 76, 78. (M) 2L72 4F4 FRTA21EA E15NE 20050726001442005072600144EU 2005 7 26 A6WA200560008 120050611A4920 APU BAC 146 146200A 1500266EU APU BAY SMOKE A A6WAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL31291UE E2084 APU AIR PUTS SMOKE IN CABIN COMPLIED WITH EO E04/022/621 REV C DETERMINED APU SOURCE OF OIL REF TO WO85137 FOR ALL DISCREPANCIES AND WORK PERFORMED. MAINTENANCE REMOVED AND REPLACED APU ASSEMBLY. (M) 2H74 4F A49EU 20050726001462005072600146NM 2005 7 26 USAA050770 120050616A5320 SUPPORT ANGLE BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU 23861 CLT - FOUND SUPPORT ANGLE CRACKED 1 INCH, LOWER EDGE OF INTERCOSTAL AT FORWARD SIDE OF STATION 328, RBL 32. REMOVED DAMAGED STIFFENER, FABRICATED REPLACEMENT PART, AND INSTALLED. (M) 2L72 4F RTA16WE 20050726001472005072600147NM 2005 7 26 USAA050769 120050616A5315 FLOORBEAM BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU52779 23861 CLT - FOUND FLOORBEAM T-CAP CORRODED 1 INCH, AT BS 986.5, LBL 31. REMOVED AND REPLACED UPPER T-CAP OF FLOORBEAM IAW TYPICAL REPAIR 53-10-05 AND SRM 53-00-51. (M) 2L72 4F RTA16WE 20050726001482005072600148NM 2005 7 26 USAA050765 120050616A5330 SKIN BOEING737 7374B7 1384702NM FUSELAGE DAMAGED A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19782AU 25021 CLT - FOUND SKIN AND TEAR STRAP 2 INCHES, BS 344 BETWEEN STRINGER S22 AND S23R. FABRICATED FROM 2024T3 DOUBLER .032, TRIPLER .050, STRUCTURAL FILLER .071 IAW SRM 53-00-01 FIG 231. (M) 2L72 4F RTA16WE 20050726001502005072600150NM 2005 7 26 USAA050767 120050616A5330 SKIN BOEING737 737301 1384611NM FUSELAGE PUNCTURED A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19354US 23557 CLT - FOUND SKIN PUNCTURED 1 INCH BY 2.5 INCH, BS 312-322 AT S23R. INSTALLED DOUBLER IAW SRM 53-00-01 FIG 229. (M) 2L72 4F RTA16WE 20050726001532005072600153NM 2005 7 26 USAA050766 120050616A5315 FLOORBEAM BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19784AU 25023 CLT - FOUND FLOORBEAM CORRODED .5 INCH BY .5 INCH, BS 986.5, WL 208, RBL 24.75 TO SIDE OF BODY. CLEANED CORROSION, BLENDED, TREATED, PRIMED AND PAINTED PER SRM 53-60-51 AND IN-59-81613-2. (M) 2L72 4F RTA16WE 20050726001552005072600155NM 2005 7 26 72400001 120050619A5311 FRAME BOEING727 727225 1384077NM PWA JT8 JT8D7A 52053NE FUSELAGE CRACKED A K11AK NONE O OTHER ININSP/MAINT 1 GL23724CK 20383 2 INCH CRACK ON FUSE FRAME CHORD REPLACEMENT 2L73 4F4 F A3WE E2EA 20050726001562005072600156NM 2005 7 26 72400002 120050619A5311 FRAME BOEING727 727225 1384077NM PWA JT8 JT8D7A 52053NE FUSELAGE CRACKED A K11AK NONE O OTHER ININSP/MAINT 1 GL23724CK 20383 1 INCH CRACK ON FRAME REPLACEMENT 2L73 4F4 F A3WE E2EA 20050726001572005072600157NM 2005 7 26 72400003 120050620A5347 SEAT TRACK BOEING727 727225 1384077NM PWA JT8 JT8D7A 52053NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23724CK 20383 1 X 1 AREA OF CORROSION SEAT TRACK. 2L73 4F4 F A3WE E2EA 20050726001592005072600159NE 2005 7 26 ALG2005F00037 120050701A2432407612 BATTERY SKRSKYS76 S76 8143010NE ALLSN 250C 250C30S 03013GL MASTER INOPERATIVE E ALGAO OTHER M OVER TEMP NRNOT REPORTED 1 SW03705AL 760267 DURING FLIGHT, THE BATTERY HOT LIGHT CAME ON, THEN THE BTTERY OFF LIGHT CAME ON. THE PILOT FOLLOWED THE EMERGENCY CHECK LIST AND LANDED. THE MECHANIC REMOVED AND REPLACED THE BATTERY, OPS CHECKED PERFORMED AND THE AC WAS RETURNED TO SERVICE. (K) 1G72 3U3 U H1NE E1GL 20050726001622005072600162NM 2005 7 26 USAA050778 120050620A5310 TEAR STRAP BOEING737 7373B7 1384580NM FUSELAGE DEBONDED A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU 23861 CLT - FOUND TEAR STRAP DISBOND 8 INCHES, BS 857, S16R-S17R. INSTALLED RIVETS TO SECURE IAW SRM 53-00-01, FIG 225 DET 3. (M) 2L72 4F RTA16WE 20050726001632005072600163NM 2005 7 26 72300225 120050601A5320 STIFFENER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 6 X 3 AREA OF CORROSION ON STIFFENER 2L73 4F4 FRTA3WE E2EA 20050726001642005072600164NM 2005 7 26 72300224 120050324A5330 LAP JOINT BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 3 X 200 INCH AREA OF CORROSION ON LAP SEAM 2L73 4F4 FRTA3WE E2EA 20050726001652005072600165NM 2005 7 26 72300223 120050323A5330 SKIN BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 10 X 5 INCH AREA OF CORROSION ON SKIN SPLICE. 2L73 4F4 FRTA3WE E2EA 20050726001682005072600168NM 2005 7 26 USAA050780 120050620A5342 CHANNEL BOEING737 7373B7 1384580NM VERTICAL STAB WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU 23861 CLT - FOUND L-CHANNEL FRETTING WEAR .5 INCH BY 3 INCHES, FORWARD OF THE LEFT FORWARD VERTICAL FIN MOUNT AT BS 1016 NR 2412. FABRICATED NEW ANGLE AND INSTALLED IAW SRM 53-20-05. (M) 2L72 4F RTA16WE 20050726001692005072600169NM 2005 7 26 05FDEA02019 120050722A534065453132 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 FUSE UPR LOBE STRINGER CLIP IS CRACKED BS 950A STR-7R. REMOVED AND REPLACED UPPER LOBE STR CLIP AT 950A, STR 7R IAW SRM 51-20-1, 51-10-3, 51-30-2, 51-10-2. 2L73 4F RTA3WE 20050726001702005072600170NM 2005 7 26 05FDEA02020 120050722A534065453132 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 FUSELAGE UPPER LOBE STRINGER CLIP IS CRACKED BS 950C STR-7R. REMOVED AND REPLACED UPPER LOBE STR CLIP AT BS 950C STR 7R. IAW SRM 51-20-1, 51-10- 3, 51-30-2, 51-10-2. 2L73 4F RTA3WE 20050726001722005072600172NM 2005 7 26 05FDEA02022 120050722A5340 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 FUSELAGE UPPER LOBE STRINGER CLIP IS CRACKED BS 990 STR-9R. FABRICATED NEW STR CLIP AND INSTALLED STR CLIP AT BS 990 STR-9R IAW SRM 51-30-2. 2L73 4F RTA3WE 20050726001732005072600173NM 2005 7 26 05FDEA02023 120050722A5340 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 FUSELAGE UPPER LOBE STRINGER CLIP IS CRACKED BS 990 STR-6R. REMOVED AND REPLACED CRACKED STR. CLIP AT BS 990 STR 6R IAW SRM 51-30-2. 2L73 4F RTA3WE 20050726001752005072600175EU 2005 7 26 05FDEA02025 120050723A5321 FLOOR PANEL AIRBUS300 A300F4605R 3930327EU FUSELAGE CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25670FE12779 777 MAIN CABIN FLOOR PANEL 242MF CRACKED. FABBED FLOOR PANEL 242MF ON MAE TRAVELER T5/532594 REF SRZ-25-005 MAJOR REPAIR. 2L72 4F RTA35EU 20050726001762005072600176EU 2005 7 26 05FDEA02026 120050723A5321 FLOOR PANEL AIRBUS300 A300F4605R 3930327EU FUSELAGE CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25670FE12779 777 MAIN CABIN FLOOR PANEL 241MF CRACKED. FABBED FLOOR PANEL 241MF ON MAE TRAVELER T5/532595 REF SRZ-25-005 MAJOR REPAIR. 2L72 4F RTA35EU 20050726001772005072600177EU 2005 7 26 05FDEA02027 120050723A5321 FLOOR PANEL AIRBUS300 A300B4605R 3930308EU FUSELAGE CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25670FE12779 777 MAIN DECK FLOOR PANEL 261AH CRACKED. FABBED FLOOR PANEL 261AH ON MAE TRAVELER T5/532924 REF SRZ-25-005 MAJOR REPAIR. 2L72 4F RTA35EU 20050726001782005072600178NM 2005 7 26 USAA050773 120050616A5753 SKIN BOEING737 7373B7 1384580NM TE FLAP GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU 23861 CLT - FOUND SKIN GOUGED .125 INCH BY 1 INCH BY .060 INCH, LEADING EDGE RADIUS OF LEFT FOR FLAP .22 INCH FROM INBOARD END. REMOVED DAMAGED AREA, 2.5 INCH BY 1 INCH, INSTALLED EXTERNAL DOUBLER 7.5 INCH BY 6 INCHES IAW SRM 57-53-01 FIG 201. (M) 2L72 4F RTA16WE 20050726001792005072600179NM 2005 7 26 USAA050776 120050620A5330 SKIN BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19449US 24893 FOUND SKIN CRACKED 1 INCH, BS 727D. INSTALLED DOUBLER IAW SRM 53-00-01, FIG 231 DETAIL XI. (M) 2L72 4F RTA16WE 20050726001802005072600180NM 2005 7 26 SB05086 120050726A33501012623 LIGHT BOEING737 7374B7 1384702NM OVERWING EXIT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19440US 24811 MAINTENANCE REPORTED THE EMERGENCY LIGHT ASSEMBLY AT THE LEFT OVERWING EXIT ROW INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050726001812005072600181EA 2005 7 26 71936 220050725A7261 OIL FILTER BEECH 1900 1900D 1154162CE PWA PT6 PT6A65B 52043EA ENGINE OIL FOULED A AMWAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE07155YV 155YV AFTER DEPARTURE FROM PITTSBURGH, PA RIGHT ENGINE OIL PRESSURE WENT TO RED LINE, 30 MILES OUT OF DUBOIS, PA. MAINTENANCE REQUESTED THE AIRCRAFT TO LAND IN DUBOIS, PA FOR FURTHER INSPECTION. THE CORRECTIVE ACTION WAS AS FOLLOWED: MAINTENANCE INSTALLED A NEW OIL FILTER. 2L72 4T4 TRTA24CE E4EA 20050726001822005072600182NM 2005 7 26 USAA050783 120050622A5730 SKIN BOEING737 737401 1384701NM WING CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19418US 23985 CLT - FOUND WING UPPER SURFACE WITH CORROSION 2 INCH BY 3 INCH, 2 INCH BY 4 INCH, 2 INCH BY 2 INCH, 4 INCH BY 6 INCH, 1 INCH BY 3 INCH, BETWEEN WBL 117 AND WBL 133 AFT OF FWR SPAR, STRINGER 10 STRINGER 15. REMOVED CORROSION IAW SRM 57-20-01. (M) 2L72 4F RTA16WE 20050726001832005072600183NM 2005 7 26 USAA050771 120050616A5320 ANGLE BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19526AU 23861 CLT - FOUND TRANSITION ANGLE CORRODED 3 INCHES, RT TRANSITION ANGLE AT BS 492.4. REMOVED DAMAGED PART. FABRICATED AND INSTALLED NEW PART IAW 737 SRM 51-10-02. (M) 2L72 4F RTA16WE 20050726001842005072600184NM 2005 7 26 USAA050774 120050616A5315 FLOORBEAM BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU52779 23861 FOUND FLOORBEAM CORRODED 3 INCHES, BS 967, LBL 43. FABRICATED NEW T-CAP FOR FLOORBEAM PER SRM 53-00-51, SAME AS PREVIOUS REPAIR. (M) 2L72 4F RTA16WE 20050726001852005072600185NM 2005 7 26 USAA050775 120050620A5311 FRAME BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU52779 23861 CLT - FOUND FRAME CRACKED .25 INCH, STATION 827 STRINGER 9L. CUT OUT CRACK, INSTALLED NEW REPAIR ANGLES IAW 53-10-20B. (M) 2L72 4F RTA16WE 20050726001862005072600186NM 2005 7 26 05FDEA02018 120050722A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 BS 600 MULTIPLE FRAME DENTS ABOVE & BELOW STRINGER 23L AT BS 600. REPAIRED FRAME BS 600, ABOVE AND BELOW STR 23L, INSTALLED REPAIR IAW SRM 51-40-3, 53- 10-1. 2L73 4F RTA3WE 20050726001872005072600187EU 2005 7 26 05FDEA02028 120050723A5320 WEB AIRBUS300 A300B4605R 3930308EU ZONE 200 CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25670FE12779 777 MAIN DECK REAR CARGO COMPT BET FRAME 79 AND 80 AT FLOOR LEVEL LT SIDE FUSELAGE TO FRAME WEB HAS CRACK. REMOVED WEB IAW SRM 51-40-21, FABRICATED NEW WEB ON MAE TRAVELER T5/533479. INSTALLED NEW WEB IAW SRM 51-40-21. 2L72 4F RTA35EU 20050726001882005072600188EU 2005 7 26 05FDEA02029 120050723A5753 SKIN AIRBUS300 A300F4605R 3930327EU TE FLAP DENTED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25670FE12779 777 RT WING T/E INBD FLAP LOWER SURFACE INBD SECTION HAS DENT (31" FROM INBD END AND 7" FROM T/E). CHECKED ALLOWABLE DENT LIMIT FOUND OT OF LIMIT ACTUAL DENT 0.1405, ALLOWED IS ONLY 0.14" PER SRM 57-50-00 PAGE 105. REMOVED DAMAGE IAW SRM 57-50-00 FIG 205 PAGE 220. FABRICATED DOUBLER MATERIAL 2024T3 .050 BATCH 952611 IAW SRM 57-50-00 FIG 205 PAGE 220. INSTALLED DOUBLER IAW SRM 57-50-00. 2L72 4F RTA35EU 20050726001892005072600189EU 2005 7 26 05FDEA02030 120050723A5315 FLOORBEAM AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25671FE12695 778 MAIN CARGO DECK UNDERNEATH LAVATORY FS 12 TO 13C LBL20 FLOORBEAM HAS CORROSION. REMOVED FLOORBEAM UPPER TEE IAW SRM 51-40-20. FABRICATED NEW PART ON TRAVELER T5/534141 REF SRM 53-12-15 FIG 19 BATCH NR 000823785, DRILL AND LOCATED IAW SRM 51-40-44. INSTALLED NEW PART IAW SRM 51-40-20, PAINTED AREA IAW SRM 51-23-10. 2L72 4F RTA35EU 20050726001902005072600190EU 2005 7 26 05FDEA02031 120050723A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU ZONE 200 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25671FE12695 778 MAIN DECK CARGO SEAT TRACK AT FRAME 41 TO 44 RBL 20, HAS CORROSION ALONG LENGTH NOTED. REMOVED SEAT TRACK, LOCATED AND DRILLED IAW SRM 53-10-16. INSTALLED NEW SEAT TRACK IAW SRM 53-10-16. 2L72 4F RTA35EU 20050726001912005072600191EU 2005 7 26 05FDEA02032 120050724A5320 FLOOR SUPPORT AIRBUS300 A300F4605R 3930327EU ZONE 200 CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25671FE12695 778 MAIN CARGO DECK SUPPORT BETWEEN F38.1 AND F38.2 AT STR 26 RT IS CRACKED. REMOVED DAMAGED SUPPORT, FABBED AND RECEIVED NEW PART ON TRAVELER NR T5/534370 (REF SRM 53-14-15/SRM 51-26-10) AND INSTALLED NEW SUPPORT IAW SRM 51-40-21. 2L72 4F RTA35EU 20050726001922005072600192EU 2005 7 26 05FDEA02033 120050724A5321 FLOOR PANEL AIRBUS300 A300F4605R 3930327EU FUSELAGE BROKEN A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25671FE 778 MAIN CARGO COMPT FLOOR PANEL 251WG IS BROKEN AT FWD INBD CUTOUT. REPLACED FLR PNL ON TRAVELER NR T5/530573 REF SRZ-25-005. 2L72 4F RTA35EU 20050726001932005072600193EU 2005 7 26 05FDEA02034 120050724A5321 FLOOR PANEL AIRBUS300 A300F4605R 3930327EU FUSELAGE CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25671FE 778 MCD FLOOR PANEL 231CF PUNCTURED AND CRACKED. REPLACED FLR PNL ON TRAVELER NR T5/3001556 REF SRZ-25-005. 2L72 4F RTA35EU 20050722000942005072200094NM 2005 7 22 QXEA200501129 120050719A261247387202 AMPLIFIER BOMBDRDHC8 DHC8402 1390042NM FIRE LOOP MALFUNCTIONED A QXEAO OTHER N FALSE WARNING CRCRUISE 1 NM09414QX9422 4061 "CHECK FIRE DETECT" WARNING LIGHT ILLUMINATED IN CRUISE AT 23000. NR 2 ENGINE FAULT A-LIGHT WAS ILLUMINATED ON FIRE PANEL. BOTH LIGHTS EXTINGUISHED AFTER ABOUT 15 SECONDS. NO FIRE. UNEVENTFUL LANDING. MX REPLACED FIRE DETECT CONTROL AMP IAW MM TASK 26-10-01-000-801 AND 26-10-01-400-801. ALSO REPLACED NR 2 ENGINE PEC FIRE LOOP IAW TASK 26-11-03-000-801 AND 26-11-03-400-801. OPS CHECK GOOD. NO FAULTS FOUND. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050722000962005072200096SW 2005 7 22 AC2A100746 120050506A6240901375909101 PRESSURE SWITCH BELL 427 427 1182207SW TRANSMISSION OILMALFUNCTIONED B AC2AO OTHER N FALSE WARNING CRCRUISE 1 SO07427CK407 56043 SWITCH WAS GIVING INDICATION OF LOW TRANSMISSION OIL PRESSURE. / REPLACED SWITCH 1G71 3U R00001RC 20050722001082005072200108NE 2005 7 22 2005000008 220050702A72009068M40G01 DUCT DOUG DC10 DC1030 3023501WP GE CF6 CF650C2B 30018NE NR 2 ENGINE RUPTURED A CNMAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SW07630AX 46596 517140 NR 2 ENGINE ON T/O LOST POWER FROM 111.5 PERCENT TO 92.1 PERCENT ENGINE FAIL LIGHT CAME ON ABORTED T/O DUE TO LOSS OF N1 POWER. INSPECTED NR 2 ENGINE FOUND 14TH STAGE HIGH PRESSURE DUCT RUPTURED. REMOVED AND REPLACED PER MM 75-20 PERFORMED HIGH POWER RUN PER JRH, OPS CHECKED NORMAL. 2L73 4F4 F A22WE E23EA 20050722001162005072200116 2005 7 22 UPS05M44934 420050719A2210 COMPUTER DOUG MD11 MD11F 3023600NM AUTOPILOT INOPERATIVE A IPXAO OTHER S AFFECT SYSTEMS CRCRUISE 1 SO01273UP 48574 ATB - BOTH AUTO PILOTS FAILED SIMULTANEOUSLY. TRIED NUMEROUS TIMES TO RE-ENGAGE, FINALLY ONE OF THEM WAS BACK ON LINE, AND IT LATER FAILED AGAIN REMOVED AND REPLACED NR 2 FCC, BOTH FCC'S PASSED RTS TEST PER MM 22-01-03-4. 2L73 4F RTA22WE 20050722001212005072200121WP 2005 7 22 2005000010 120050715A2741SB1027020823 MOTOR DOUG DC10 DC1030 3023501WP STAB TRIM FAILED A CNMAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0749082 47927 NR 1 SYSTEM HYDRAULIC FAIL LOST ALL FLUID IND ZERO. FOUND PRIMARY HORIZONTAL TRIM MOTOR LEAKING, REMOVED AND REPLACED PER 27-43 CHECKS NORMAL. REPLACED NR 1 HYD SYSTEM FILTERS ON EDPS AND ACMPS LEAK CHECK GOOD IAW 29-12. 2L73 4F A22WE 20050722001372005072200137NM 2005 7 22 2005UALA00653 120050713A3350582240 POWER SUPPLY BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT DISCHARGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29178UA 24385 EEL INOP, ALL LT C ZONE ROWS 22-26. BATTERY PACK NOT HOLDING CHARGE, REPLACED OK. 2L74 4F4 FRTA20WE E24NE 20050722001462005072200146NM 2005 7 22 2005UALA00662 120050715A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29504UA 24625 FRAME 600 IS DENTED AT STRINGER 23L. TRIM OUT DAMAGE, ACP HEFC INSP, NO CRACK NOTED. REPAIRED PER GSO EA G10674 REV B. 2L72 4F4 FRTA2NM E17NE 20050722001672005072200167NM 2005 7 22 05FDEA01906 120050713A5744 HINGE DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 LT WING-O/B FLAP I/B HINGE (WING SIDE), FWD ATTACHMENT O/B BORE FOUND CORRODED. REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. FABRICATED BUSHING AND INSTALLED IAW EA 1-5750-87605. 2L73 4F RTA22WE 20050722001692005072200169NM 2005 7 22 05FDEA01908 120050713A5744 HINGE DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 LT WING-O/B FLAP I/B HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PG 612-615. 2L73 4F RTA22WE 20050722001702005072200170NM 2005 7 22 05FDEA01909 120050713A5753 HINGE DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 LT WING - I/B FLAP O/B HINGE (FLAP SIDE ), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03 PG 442-443. FABRICATED BUSHING AND INSTALLED AS PER EA 1-5750-87606. 2L73 4F RTA22WE 20050722001712005072200171NM 2005 7 22 05FDEA01910 120050713A5315 FLOORBEAM DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 AT STA 1821 ALONG LBL 38.5 TO LBL 65 FLOORBEAM STRUCTURE FOUND CORRODED. REMOVED AND REPLACED. NEW FLOOR SUPPORT REWORKED IAW DWG AGA 7028. NEW SUPPORT PAINTED, PART MARKED AND INSTALLED IAW SRM 51-35-01 VOL.II. CLASSIFIED MINOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050722001732005072200173NM 2005 7 22 05FDEA01912 120050713A5315 FLOORBEAM DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 AT STA 1836 ALONG LBL 10.5 TO LBL 26 FLOOR SUPPORT STRUCTURE FOUND CORRODED. FLOOR SUPPORT REMOVED. NEW FLOOR SUPPORT REWORKED FROM S2929348X7075T6511 AS PER DRAWING AGA 7975 AND INSTALLED AS PER SRM 51-31-01 VOL.II. CLASSIFIED MINOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050722002022005072200202NM 2005 7 22 MASA200500519 120050705A2434GC1010245DIII GENERATOR DHAV DHC8 DHC8202 2809007NM NR 1 DC FAILED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07449YV2436 449 NR 1 DC GEN LIGHT IN FLIGHT. NR 1 DC GENERATOR REPLACED. 2H72 4T RTA13NM 20050722002032005072200203NM 2005 7 22 MASA200500513 120050702A213121178041 CONTROLLER DHAV DHC8 DHC8202 2809007NM CABIN PRESSURE FAILED A MASAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 SW07446YV7587 446 THE CREW RETURNED TO THE FIELD AND DECLARED AND EMERGENCY. THE AIRCRAFT WOUDL NOT PRESSURIZE ABOVE 18000 FT. MAINTENANCE PLACED THE AUTO PRESSURIZATION CONTROL ON MEL. - MX REPLACED PRESSURE CONTROL ON 7/3/05 FOR FINAL FIX. 2H72 4T RTA13NM 20050722002052005072200205CE 2005 7 22 GNB2005F00005 120050628A2710500000895CR CONTROL CABLE CESSNA402 402C 207590RCE CONT O520 TSIO520* 17040SO AILERON WORN E GNBAO OTHER O OTHER NRNOT REPORTED 1 SW013292M 402C0304 WEAR FROM BLENDING DUE TO SOFTER MATERIAL USED IN NEW STYLE CABLE. 1L72 3O3 O A7CE E8CE 20050722002062005072200206EU 2005 7 22 NXT2005F00001 120050614A6210709010301109 BLADE AGUSTAA109 A109E 0260119EU MAIN ROTOR CRACKED E NXTAO OTHER O OTHER NRNOT REPORTED 1 SW19145CF1172 11149 A CRACKED IN THE M/R BLADE EROSION STRIP AT APPROXIMATELY MID-SPAN. BOTH UPPER AND LOWER SURFACES WERE CRACKED. (K) 1G72 3U RTH7EU 20050725000112005072500011EA 2005 7 25 O2G2005F00010 120050705A2830601621453 DRAIN CNDAIRCL600 CL6002B16 1900305EA GE CF34 CF34* NE FUEL LIGHTNING STRIKEE O2GAO OTHER C F.O.D. DEDESCENT 1 NE03601VH 5043 C/W LIGHTNING STRIKE INSPECTION. REPLACED FUEL DRAIN MASK. (NE03200509277) 2L72 4F4 FRTA21EA E15NE 20050725000192005072500019WP 2005 7 25 UPS05844939 120050709A53476015176 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE:C1 MAIN CABIN SEAT TRACK PLUGS HAVE CORROSION AT STA.420 AND RBL 25. REMOVED CORROSION AND FOUND SEAT TRACK OUT OF LIMITS. REMOVED DAMAGED SEAT TRACK,FABRICATED AND REPLACED. IAW SRM 53-02-03-0, 53-2-3 FIG 12 , 51-3-0, AND 53-21-01. 2L74 4F RT4A25 20050725000252005072500025WP 2005 7 25 UPS05844941 120050709A5340 SPLICE DOUG DC8 DC873F 302199FWP FS LBL45 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C1, MAIN CARGO AT FS 990 LBL45 HAS LIGHT CORROSION ON SEAT TRACK SPLICE. REMOVED, FABRICATED AND REPLACED SEAT TRACK SPLICE. IAW SRM 51-3-0, D WG 5910152, 51-3-2 AND 51-1-11. 2L74 4F RT4A25 20050725000372005072500037NE 2005 7 25 07172005B 220050717A7230 COMPRESSOR SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE NR 2 ENGINE STALLED A NSVAEC ENGINE SHUTDOWN ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 EA27251CJ 251 NR 2 ENGINE SHUTDOWN ON TAKEOFF AFTER SUSPECTED COMPRESSOR STALL. 2L72 4T4 TRTA52EU E8NE 20050725000502005072500050NM 2005 7 25 CALA0500235 120050722A5310BAC1505100849 BEAM BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2719623 27527 INSPECTION FOUND BEAM (E&E DOOR CUTOUT SUPPORT STRUCTURE) CORRODED AT STA 986.5, LBL 10 TO LBL 46. REPAIRED IAW ECRA 5310-01233. 2L72 4F RTA16WE 20050725000512005072500051NM 2005 7 25 CALA0500236 120050722A5320143N584570 FLOOR SUPPORT BOEING757 757224 1384958NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713110 27300 INSPECTION FOUND FLOOR SUPPORT CORRODED BETWEEN STA 720 AND 740, RBL 16. A REPAIR WAS PERFORMED IAW ECRA 5310-04482. 2L72 4F RTA2NM 20050725000592005072500059EU 2005 7 25 07242005B 120050724A3260 WARNING LIGHT SAAB SF340 340B 7860101EU MLG ILLUMINATED A NSVAO OTHER J WARNING INDICATION APAPPROACH 1 EA279CJ 2245 EMERGENCY GEAR EXTENSION REQUIRED DUE TO NOSE LANDING GEAR LIGHT NOT ILLUMINATED AND IN TRANSIT LIGHT STILL ILLUMINATED 2L72 4T RTA52EU 20050725000662005072500066WP 2005 7 25 GTIA050198 120050624A7160 PACKING DOUG DC9 DC983 3022083WP NR 1 ENGINE DETERIORATED A GTIAO OTHER O OTHER CLCLIMB 1 GL23802NK 53168 AT CLIMB, EPR LEFT THROTTLE 1 AND ONE-HALF KNOB WIDTHS FORWARD OF RIGHT THROTTLE AT 210 CL, AIRCRAFT TAIL SWAP WITH 802. FOUND NOSE INLET BULLET PACKING AND GROMMET DETERIORATED. REMOVED AND REPLACED PACKINGS. THROTTLES STAGGER WITHIN LIMIT, LEAK CHECKED PT7 PROBES AND BELLOWS. NO DEFETS NOTED. (M) 2L72 4F RTA6WE 20050725000782005072500078EA 2005 7 25 O2G2005F00011 120050628A2711600561553 SUPPRESSOR CNDAIRCL600 CL6002B16 1900305EA GE CF34 CF34* NE PITCH TRIM LIGHTNING STRIKEE O2GAO OTHER O OTHER CRCRUISE 1 NE03601VH 5043 C/W LIGHTNING STRIKE INSPECTION. REPAIRED PITCH TRIM SUPPRESSOR. (K) 2L72 4F4 FRTA21EA E15NE 20050725000812005072500081WP 2005 7 25 GTIA050191 120050605A5310 DOOR FRAME DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23830NK 49932 AFT CARGO DOOR FUSELAGE JAMB, BEAM STATION 1155-1211, L25R CORRODED. REMOVED PANEL FOR ACCESS. REMOVED CORROSION, FOUND MATERIAL IS OUT OF LIMITS. FABRICATED DOUBLER. TREATED AND PRIMED. INSTALLED REPAIR DOUBLER. INSTALLED ACCESS PANELS. (M) 2L72 4F A6WE 20050725000832005072500083NM 2005 7 25 GTIA050181 120050525A5320 WEB DOUG MD80 MD83 3023681NM FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23833NK 49449 FOUND CRACK AT WEB JUST AFT OF L1 DOOR AT LONGERON 15. CUT OUT DAMAGED SECTION OF WEB. FABRICATED REPAIR DOUBLER AND FILLER. TREATED AND PRIMED REPAIRED DOUBLER AND FILLER. FABRIATED PARTS INSTALLED AT LONGERON 152 AFT L1 DOOR. (M) 2L72 4F RT 20050725000862005072500086NM 2005 7 25 GTIA050185 120050507A5320 CUSP WEB DOUG MD80 MD83 3023681NM FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23827NK 49793 FOUND CABIN STRINGER 18R CUSP CORRODED FS 1098-1117. REMOVED CORROSION AT CUSP WEB STATION 1098-1117. FOUND OUT OF LIMITS. REMOVED FLOOR BOARDS AND PANELS FOR ACCESS. REMOVED CUSP WEB STRINGER 18 RT STATION 1059 TO STATION 1174. FABRICATED CUSP WEB. TREATED AND PRIMED, INSTALLED FABRICATED PARTS. RE-INSTALLED FLOOR BOARDS AND PANELS FOR ACCESS. (M) 2L72 4F RT 20050725000872005072500087NM 2005 7 25 GTIA050180 120050524A5320 FLOOR SUPPORT DOUG MD80 MD83 3023681NM FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23833NK 49449 FOUND CORROSION ON FLOOR STATION 200 BL 0. REMOVED CORROSION FLOOR SUPPORT STATION 200 BL 0 MATERIAL LOSS OUT OF LIMITS. FABRICATED FLOOR SUPPORT. LOCATED AND DRILLED HOLES. TREATED AND PRIMED AND INSTALLED FLOOR SUPPORT. (M) 2L72 4F RT 20050726000042005072600004WP 2005 7 26 ABXA050174 120050627A52205912995503 PAN DOUG DC9 DC941 302207NWP OVERWING EXIT CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23978AX 47628 LEFT FORWARD OVER WING EXIT DOOR HAD CRACKED PAN, UPPER AFT CORNER. REPLACED LEFT FORWARD OVER WING EXIT DOOR IAW DC-9 SRM. 2L72 4F A6WE 20050726000052005072600005WP 2005 7 26 ABXA050175 120050627A52205912995503 PAN DOUG DC9 DC941 302207NWP OVERWING EXIT CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23978AX 47628 LEFT AFT OVERWING EXIT DOOR HAD CRACKED DOOR PAN, LOWER AFT CORNER. REPLACED LEFT AFT OVERWING EXIT DOOR IAW DC-9 SRM. 2L72 4F A6WE 20050726000082005072600008WP 2005 7 26 ABXA050170 120050624A53115913595 FRAME DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23978AX 47628 FRAME CRACKED - FS 1152 AT LONGERON 12 RIGHT. REPAIRED IAW DC-9 SRM 53-03. 2L72 4F A6WE 20050726000092005072600009WP 2005 7 26 ABXA050171 120050627A5280591078387 DOOR DOUG DC9 DC941 302207NWP MLG CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23978AX 47628 LEFT MAIN LANDING GEAR DOOR CRACKED JUST FORWARD OF ACTUATOR ATTACH POINT. REPAIRED CRACK IAW DC-9 SRM. 2L72 4F A6WE 20050726000472005072600047EA 2005 7 26 A6WA200540232 120050422A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31417AW 7610 MWC 135 RT FS621 FLOOR SUPPORT ANGLE IS CRACKED. REPAIRED BY REMOVING SECTION OF DAMAGED ANGLE, FABRICATING AND INSTALLING REPAIR ANGES IAW MFG REO. (K) 2L72 4F4 FRTA21EA E15NE 20050726000532005072600053WP 2005 7 26 GTIA050159 120050530A2120 SEAL DOUG DC9 DC982 3022082WP HEAT EXCHANGER LEAKING A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23804NK 49104 AFTER TAKEOFF LEFT AC SUPPLY PRESSURE DROPS TO ZERO, QRH FAILS TO RESTORE SUPPLY PRESSURE, LEFT PACK IS INOPERATIVE. UPON ENTERING ICING CONDITIONS A 2ND ATTEMPT TO RESET THE PACK RESULTED IN A TEMP RESTORATION OF LEFT PACK, SUBSEQUENT OPERATION OF ENGINE AND AIRFOIL ANTI-ICE SYSTEMS CAUSED AN ABNORMAL SURGE IN LEFT SUPPLY PRESSURE, AIRFOIL ICE PRESSURE ABNORMAL LIGHT ILLUMINATED, PACK FAILED, DIVERTED INTO MYR. FOUND CONNECTOR PERI-SEAL LEAKING ON DUCTING AT SECONDARY HEAT EXCHANGER. REMOVED AND REPLACED PERI-SEALS AT LEFT HEAT EXCHANGER. OPS AND LEAK CHECK GOOD. NO OTHER DEFECTS NOTED. (M) 2L72 4F A6WE 20050726000592005072600059EA 2005 7 26 ASOA05544 120050620A5340601R53611001 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE BULKHEAD CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27851AS 7360 DURING A C-CHECK, THE CLIP AT FS 625 LT AFT PRESSURE BULKHEAD WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIP AT FS 625 LT AFT PRESSURE BULKHEAD IAW SRM. (K) 2L72 4F4 FRTA21EA E15NE 20050726000602005072600060EA 2005 7 26 SWIA200515306 120050718A2750 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS OUT OF RIG A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07906SW 7510 "FLAPS FAIL" CAUTION MESSAGE. FLAPS FAILED AT 0 DEGREES. INTERROGATED FECU AND FOUND BOTH LEFT AND RIGHT BPSU'S OUT OF TOLERANCE. RE-RIGGED BOTH LEFT AND RIGHT BPSU'S IAW CRJ 200 MM 27-51-10. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050726000612005072600061EA 2005 7 26 SWIA200515307 120050718A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07437SW 7564 FWD CEILING EMERGENCY LIGHT NOT ILLUMINATING. REMOVED AND REPLACED BULB IAW 33-10-02. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050726000642005072600064SO 2005 7 26 SWIA200515310 120050720A3350 LIGHT EMB 120 EMB120ER 3260203SO CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07227SW 120304 A SECTION OF EMERGENCY LIGHT STRIP INOPERATIVE. REPLACED EMERGENCY LIGHT IAW WM 20-21-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050726000722005072600072CE 2005 7 26 DXTA200500859 120050718A275145AS86805033 TRANSMITTER BEECH MU300 400A 1155402CE TE FLAPS INOPERATIVE E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07117QS RK391 AFTER TAKEOFF, AFTER SELECTING FLAPS 0 " FLAP ASSM " ANNUNICATOR ILLUMINATED. FLYING PILOT NOTICED NO CONTROL PROBLEMS. ANNUNICATOR EVENTULLY EXTINGUISHED. TROUBLESHOT SYSTEM AS PER WDM IN 400 XP MM CM 27-50-00, REMOVED AND REPLACED LT AND RT FLAP POSITION TRANSMITTERS IAW 400XP MM CH 27-50-00. OPS CHECK GOOD. 2H72 4F RTA16SW 20050726000742005072600074CE 2005 7 26 DXTA200500852 120050721A215073838433 ACM CESSNA750 750 2076810CE SEIZED E DXTAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL07971QS791 7500071 DURING TAXI IN AFTER OPERATIONAL CHECK FLIGHT, SMOKE AND ODOR NOTICED COMING THROUGH COCKPIT GASPERS. BY THE TIME AIRCRAFT WAS PARKED AND SHUTDOWN, SMOKE AND ODOR FILLED THE COCKPIT AND CABIN. ARFF CALLED TO THE SCENE. NO NOTICEABLE FIRE OR FLAMES. TROUBLESHOT, FOUND CABIN ACM SEIZED. REPLACED CABIN ACM (AIR CYCLE MACHINE) WITH OVERHAULED UNIT IN ACCORDANCE WITH CESSNA 750 MAINTENANCE MANUAL CHAPTER 21-51-00. OPERATIONAL CHECK GOOD. 2L72 4J RTT00007WI 20050726000752005072600075NE 2005 7 26 DXTA200500854 220050723A7200 ENGINE CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE RIGHT POWER LOSS E DXTAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 GL07344QS9361 5600344 PCE500184 DURING POWER UP FOR TAKEOFF RIGHT ENGINE WOULD NOT MAKE TAKEOFF POWER. PUSHED RIGHT POWER LEVER TO STOP ONLY GOT 96.0 PERCENT N1, NEEDED 96.7 PERCENT N1 FOR TAKEOFF. RAN A/C FOR POWER OF THE DAY RUN COMPUTED P.O.D FOR 94.9 ENG MADE POWER. PUSHED THROTTLE TO STOP GOT 97.8. TEMP OF THE DAY AT TIME OF RUN WAS 35 C. SYSTEM OP'S CHECKS SATISFACTORY AT THIS TIME ALL WORK DONE IAW CE560 M/M 72-00-00 AND CE560 ULTRA FLIGHT MANUAL. 2L72 4F4 FRTA22CE E25EA 20050726000772005072600077NE 2005 7 26 AALA20050457 220050721A7200 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE RIGHT STALLED A AALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SW21402A 49313 718485 BOS INFLIGHT T509/21JUL - AFTER TAKEOFF, RIGHT ENGINE EXPERIENCED MULTIPLE COMPRESSOR STALLS. CREW SHUT DOWN ENGINE AND RETURNED TO BOS AND LANDED WITHOUT INCIDENT. FLIGHT DATA RECORDER REVEALED ENGINE EXHAUST GAS TEMPERATURE EXCEEDED 667C. REPLACED NUMBER 2 ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 F A6WE E9NE 20050726000802005072600080WP 2005 7 26 GTIA050192 120050604A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23830NK 49932 LEFT SUB FLOOR HAS CORROSION, BARE METAL AT 18L FS 320, FS 850 AND FS 1085. REMOVED CORROSION AT WEB AREA 18L, STATION 320-850. FOUND WEB IS OUT OF LIMITS. FABRICATED DOUBLERS AND FILLERS. REMOVED CORROSION AT 18L STATION 1085. FABRICATED REPAIR DOUBLER. TREATED AND PRIMED FABRICATED DOUBLERS AND FILLERS. INSTALLED FABRICATED PARTS. (M) 2L72 4F A6WE 20050726000922005072600092WP 2005 7 26 UPS05844949 120050712A5340 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C1, EXFOILIATED CORROSION ON VERTICAL L-FITTING FWD BULKHEAD RT NOSE TUNNEL. REMOVED VERTICAL L-FITTING, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-21, DWG 4642086,S-2506104 AND 51-1-20D. 2L74 4F RT4A25 20050726001002005072600100WP 2005 7 26 GTIA050189 120050603A5730 SKIN DOUG DC9 DC982 3022082WP LT WING DAMAGED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23830NK 49932 EXTERNAL REPAIR LEFT WING L/E XIS 241.081 IS DAMAGED. DOUBLER OUT OF LIMITS. REMOVED DAMAGED DOUBLER FROM LEFT WING. FABRICATED REPAIR DOUBLER TREATED, PRIMED AND INSTALLED DOUBLER. (M) 2L72 4F A6WE 20050726001062005072600106EA 2005 7 26 SWIA200515302 120050721A274283963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07432SW8513 8513 7548 "STAB CH 2" STAB TRIM WILL NOT ENGAGE. REPLACED BOTH HSTCA AND HSTMC IAW AMM 27-40-00, 27-42-01, AND 27-42-05. OPERATIONAL CHECK GOOD, PN 7062-3, SN/OFF 799. 2L72 4F RTA21EA 20050726001292005072600129EU 2005 7 26 MALA050593 120050718A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15438XJ 340B438 DURING 4Y/2Y CHECK IN BNA FOUND SEAT TRACK AT BL 0 FROM FS 297 TO FS 319 IS CORRODED AND HAS BEEN REPAIRED IAW MESABA EO S53060. REF: EAMS WORK ORDER 212645 TASK 2526 2L72 4T RTA52EU 20050726001382005072600138EU 2005 7 26 XN0A1249 120050726A2910 HYDRAULIC SYSTEM AIRBUS300 A300B4203 3930306EU LOW A XN0AD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL23372PC 196 GREEN & YELLOW HYDRAULIC SYSTEM AIR PRESSURE LOW LIGHT REMAINS ON AFTER BOTH ENGINES STARTED. SERVICED GREEN SYSTEM RESEVOIR HEAD PRESSURE CKS NORMAL PER MM 29-14-00. YELLOW SYSTEM - X-FERRED TO DMI LIST IAW A300 MEL 29-32-03 ASSIGNED 5587 S.P. 29-32-03. C/W PLACARD INSTALL. (ORIG/OPEN) 2L72 4F RTA35EU 20050726001542005072600154EA 2005 7 26 A6WA200540221 120050625A3510 PBE CNDAIRCL600 CL6002B19 1900309EA CABIN DAMAGED A A6WAO OTHER O OTHER NRNOT REPORTED 1 GL31421ZW 7346 GALLEY PBE FALLING APART. REMOVED AND REPLACED FLIGHT ATTENDANT PBE WHOLE ASSEMBLY IAW 35-30-00. (M) 2L72 4F RTA21EA 20050726001952005072600195NM 2005 7 26 USAA050784 120050622A5330 SKIN BOEING737 7374B7 1384702NM FUSELAGE DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19430US 24552 CLT - FOUND SKIN WITH HOLE 10 INCH BY 2 INCH, STATION 887 TO STATION 908 BETWEEN STRINGER 21R AND STRINGER 22R. DOUBLER AND TRIPLER INSTALLED IAW SRM 53-00-01 FIG 231 DETAIL VIII. (M) 2L72 4F RTA16WE 20050726001972005072600197EU 2005 7 26 05FDEA02037 120050724A5321 FLOOR PANEL AIRBUS300 A300F4605R 3930327EU FUSELAGE BROKEN A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25671FE 778 MCD FLOOR PANEL 242DF IS BROKE AFT END OF BOARD. REPLACED FLR PNL ON TRAVELER NR T5/530576 REF SRZ-25-005. 2L72 4F RTA35EU 20050726001992005072600199EU 2005 7 26 MALA050601 120050722A5753 ACCESS PANEL SAAB SF340 340B 7860101EU RT TE FLAP CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15439XJ 340B439 DURING 4Y/2Y CHECK IN BNA FOUND RT FLAP ACCESS PANEL 641AT IS CHAFED AT THE INBOARD END AND HAS BEEN REPAIRED IAW MESABA EO#S57095. REF: EAMS WORKORDER 212650 TASK 6503 2L72 4T RTA52EU 20050726002002005072600200EU 2005 7 26 MALA050602 120050722A5320 FLOOR SUPPORT SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15439XJ 340B439 FLOOR FLANGE AT FS258 IS CORRODED AND HAS BEEN REPAIRED IAW MESABA EO S53102. REF: EAMS WORK ORDER 212650 TASK 2509. 2L72 4T RTA52EU 20050726002062005072600206NM 2005 7 26 USAA050779 120050620A5310 TEAR STRAP BOEING737 7373B7 1384580NM FUSELAGE DEBONDED A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU52779 23861 CLT - FOUND TEAR STRAP DISBOND 15 INCHES, BS 867-887, S17-19 RT. INSTALLED RIVETS THROUGH SKIN AND STRAPS AS REQUIRED IAW SRM 53-00-01 FIG 225. (M) 2L72 4F RTA16WE 20050726002142005072600214NM 2005 7 26 QXEA200501132 120050721A2750 FLAP SYSTEM BOMBDRDHC8 DHC8402 1390042NM TE FLAPS INOPERATIVE A QXEAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 NM09403QX 4037 SEA-ON FLIGHT 2348, RETURNED TO GATE, WHEN SETTING FLAPS FOR TAKEOFF, THE FLAP POWER CAUTION LIGHT ILLUMINATED AND THE FLAPS DID NOT MOVE. NO FAULTS FOUND IN CDS. CLEARED NVM IN CDS, RESET FLAP CONTROL CIRCUIT BREAKER. RAN FLAPS UP AND DOWN TO 35 DEGREES. FLAP CAUTION EXTINGUSHED. AIRCRAFT RETURNED TO SERVICE AS PER SERVICE LETTER DH8-400-SL-27=002A. NO PARTS WERE REPLACED. 2H72 4T RTA13NM 20050726002212005072600221EU 2005 7 26 05FDEA02040 120050724A5321 FLOOR PANEL AIRBUS300 A300F4605R 3930327EU FUSELAGE CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25671FE 778 MAIN CARGO DECK FLOOR PANEL 241PF IS CRACKED IN MIDDLE SECTION OF BOARD. REPLACED FLR PNL ON TRAVELER NR T5/530577 REF SRZ-25-005. 2L72 4F RTA35EU 20050726002232005072600223EU 2005 7 26 F3LA200500035 120050720A3230215TS07YOO CONTROL UNIT AIRBUSA319 A319112 3930323EU MLG UNSERVICEABLE A F3LAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM03909FR 2631 1761 AIR TURNBACK. ON TAKEOFF, FLIGHT CREW REPORTED LGCIU NR 1 FAULT ON WHEEL PAGE. HAD X'S ON WHEEL PAGE. REVERSER 1 FAULT ON STATUS PAGE. REPLACED NO. 1 LGCIU PER AMM 32-31-71, PB 401. PERFORMED BITE TEST PER AMM 32-69-00-740-001. PERFORMED SIMULATION OF FLIGHT PER AMM 32-69-00-860-001. PERFORMED OPS TEST OF THE NORMAL BRAKING SYSTEM PER AMM 32-42-00-710-001. REPLACED LANDING GEAR CONTROL LEVER PER AMM 32-31-11, PB 401. PERFORMED CAT III LAND TEST PER 22-97-00-710-001. CAT IIIB STATUS RETAINED. 2L72 4F RTA28NM 20050726002252005072600225NM 2005 7 26 USAA050777 120050620A5310 TEAR STRAP BOEING737 7373B7 1384580NM DEBONDED A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU 23861 CLT - FOUND DEBONDED TEAR STRAP 11 INCHES, BS 877, S16R-17R. ADDED RIVETS IAW SRM 53-00-01 FIG 225 DET 3. (M) 2L72 4F RTA16WE 20050726002272005072600227NM 2005 7 26 USAA050782 120050621A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19532AU50215 24479 CLT - FOUND SKIN CRACKED 2.25 INCH, BS 727D AT S23R RT SIDE. INSTALLED DOUBLER IAW 53-00-01 FIG 229. (M) 2L72 4F RTA16WE 20050726002282005072600228NM 2005 7 26 2005UALA00664 120050715A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29504UA 24625 APPROX 8 INCH FWD OF C2 DOOR CUTOUT NEAR UPPER CORNER, AIRCRAFT SKIN HAS LARGE DENT. CUT OUT DAMAGE AREA, ACP NDT HFEC INSPECTION, NO CRACK FOUND. FABRICATE AND INSTALL DOUBLER REPAIR PER TIMCO EA REO-G10749, REV A, UA-EVA-50463. 2L72 4F4 FRTA2NM E17NE 20050726002302005072600230NM 2005 7 26 2005UALA00666 120050716A3020 ANTI-ICE VALVE BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE RT ENGINE MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 WP29206UA 30212 RIGHT ENGINE ANTI-ICE VALVE PROBLEM. ANTI-ICE VALVE AND CONTROLLER WERE REPLACED AT JFK, JULY 18. NO FURTHER WRITE-UPS. SHOP PERFORMED INCOMING TEST & CONFIRMED THAT EAI VALVE DID FAIL. VALVE ASSY LARGE PISTON RING INSIDE DIAMETER COATING WAS FOUND WORN TO BASE METAL. NOTE: OUR RECORDS DO NOT SHOW THAT THIS VALVE HAS EVER BEEN REPLACED BEFORE. 2L72 4F4 FRTT0001SE E46NE 20050726002312005072600231 2005 7 26 2005UALA00668 420050716A2565 BOTTLE AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE DOOR 2L SLIDE DISCHARGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29810UA 843 DOOR 2L PRESSURE LOW. SERVICED DOOR CYLINDER TO 1800 PSI. NO HISTORY EXCEPT ROUTINE SERVICING AT A-CHECK. 2L72 4F4 FRTA28NM E40NE 20050726002322005072600232NM 2005 7 26 2005UALA00669 120050715A2530 COFFEEMAKER BOEING757 757222 1384956NM PWA 2037 PW2037 NE GALLEY SHORTED A UALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP29520UA 24890 COFFEEMAKER DELIVERED SHOCK TO FLIGHT ATTENDANT IN REAR GALLEY. UNIT TESTED ONLY AFTER BURST HEATER WAS REPLACED. CAN ONLY SPECULATE BURST HEATER CARTRIDGE IN WATER MAY HAVE BEEN SOURCE OF STRAY CURRENT. UNIT BONDING OK. 2L72 4F4 FRTA2NM E17NE 20050726002332005072600233NM 2005 7 26 2005UALA00670 120050718A4920 SWITCH BOEING757 757222 1384956NM PWA 2037 PW2037 NE APU MALFUNCTIONED A UALAB EMER. DESCENT HJ ELECT. POWER LOSS-50 PC WARNING INDICATION DEDESCENT 1 WP29517UA 24861 LANDED SFO UNDER AMBER ALERT DUE TO LOSS OF GENERATOR AND APU NO-START. GENERATOR DELTA-P SWITCH REPLACED. OPS CHECK GOOD. NO METAL FOUND ON CHIP DET. IN ADDITION TO REPLACEMENT OF GEN DELTA P SWITCH, CH ITEM INCLUDED TO REPLACE APU GENERATOR DUE TO MULTIPLE GRIPES OF CHARGING SYSTEM. THE IDG REQUIRED FLUID SERVICING. INITIALLY THE IDG WAS SERVICED, BUT WAS THEN REPLACED WITH A NEW UNIT DUE TO EXCESS FLUID SERVICING REQUIRED. 2L72 4F4 FRTA2NM E17NE 20050726002342005072600234NM 2005 7 26 2005UALA00672 120050717A335078941 LAMP BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE SEAT 1F INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29787UA 26939 SEAT 1F AFT EMERGENCY PROX FLOOR LIGHT INOP. REPLACED LIGHT ASSY. 2L72 4F4 FRTT0001SE E46NE 20050726002372005072600237NM 2005 7 26 2005UALA00675 120050719A5311 FRAME BOEING737 737522 138449FNM FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29914UA 25381 FUSELAGE FRAME AT STA 663 IS CRACKED IN TWO PLACES AT STR 3R CUTOUT. MAJOR REPAIR ACP'D PER SRM 51-10-02 & SRM51-10-07 FIG 209 PG 225 REPAIR ANGLE INSTALLED, APPROX SIZE 16" X 4" 2L72 4F RTA16WE 20050726002392005072600239NM 2005 7 26 2005UALA00677 120050720A5314 KEELBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29542UA 25276 KEEL BEAM CORROSION. EXT CHORD BS 1180 TO 1176, APPROXIMATELY 6 LBL TO 6 RBL. REMOVE CORROSION AND CK LIMIT PER SRM 53-30-12. ORIGINAL THICKNESS=.130", AFTER REPAIR THI CKNESS=.124", LOSS OF MATERIAL IS WITHIN LIMIT PER SRM 53-30-12 2L72 4F4 FRTA2NM E17NE 20050726002612005072600261NM 2005 7 26 05FDEA02051 120050724A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 TO PROVIDE ACCESS AT HORIZONTAL STAB UPPER TORQUE BOX TO REPAIR HORIZONTAL STAB BARREL NUT HOLE NR 36R. REPAIRED PER EA 1-5310-87589. [CLOSED] 2L73 4F RTA22WE 20050726002622005072600262EU 2005 7 26 MALA050605 120050724A2913521449 PUMP BAC 146 AVRO146RJ85A1500097EU HYD SYSTEM INOPERATIVE A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15535XJ E2371 GREEN HYD HIGH TEMP ILLUMINATED. REMOVED AND REPLACED NR 3 GREEN HYD EDP PN 521449 SN OFF MX651419, SN ON F9911203 2H74 4F RTA49EU 20050726002632005072600263EU 2005 7 26 MALA050603 120050722A2422PC251123C INVERTER SAAB SF340 340B 7860101EU NR 1 FAILED A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL15423XJ 340B423 INFLIGHT ELECTRICAL WIRE BURNING SMELL IN COCKPIT AND CABIN, NO SMOKE. FA REPORTS GRINDING NOISE FROM FLOOR MID CABIN. COCKPIT TEMP INCREASES. FOLLOWED QRH, SHUT OFF HP & BLO. DIVERTED TO RST. REMOVED AND REPLACED NR 1 INVERTER PN PC251-123C, SN OFF 8429, SN ON 8828. NR 1 INVERTER OPS CHECKS GOOD 2L72 4T RTA52EU 20050726002662005072600266NM 2005 7 26 05FDEA02053 120050724A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE NR 36R FOUND WITH CORROSION. REPAIRED IAW EA 1-5510-87597. [CLOSED] 2L73 4F RTA22WE 20050726002682005072600268NM 2005 7 26 2005UALA00671 120050718A3350321454 EPSU AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE EMERGENCY LIGHT FAILED A UALAK NONE J WARNING INDICATION ININSP/MAINT 1 WP29810UA 843 "INTERNAL LOAD FAULT FWD L" DISPLAYED ON PTP DURING EMER LIGHT SYS TEST. SWAPPED FWD AND AFT EPSU'S AND ALL TESTED OK. INTERNAL LOAD FAULTS WILL APPEAR IF THE LOAD ON THE EPSU IS DIFFERENT THAN WHAT THE UNIT "LEARNED" AT IT'S ORIGINAL LOCATION DURING "TEACH-IN". MOVING THE EPSU TO A POSITION WHERE THE LOAD MATCHES WHAT THE UNIT EXPECTED IS ACCEPTABLE. 2L72 4F4 FRTA28NM E40NE 20050726002692005072600269NM 2005 7 26 05FDEA02061 120050725A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE RT NR 10 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. 2L73 4F RTA22WE 20050726002712005072600271NM 2005 7 26 05FDEA02060 120050725A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE RT NR 08 FOUND WITH CORROSION EXCEEDING LIMITS. OPEN 2L73 4F RTA22WE 20050726002722005072600272NM 2005 7 26 05FDEA02055 120050724A5730 SKIN DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 RIGHT HAND WING UPPER SURFACE TRAILING EDGE FORWARD OF NR 2 SPOILER 4 EACH SKIN BULGE FOUND AS MARKED. CORROSION REMOVED AND FOUND WITHIN LIMIT REFER TO SNRM N1237 FOR WORK DETAILS AND 03 EA AREA CORROSION REMOVED AND FOUND EXCEED LIMIT REFER TO SNRM N1236, SNRM N1238 AND N1240 FOR WORK DETAIL. 2L73 4F RTA22WE 20050726002742005072600274NM 2005 7 26 05FDEA02057 120050724A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE RT NR 06 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. [CLOSED] 2L73 4F RTA22WE 20050726002752005072600275EU 2005 7 26 05FDEA02058 120050725A5347A53612518200 SEAT TRACK AIRBUS300 A300F4605R 3930327EU MAIN DECK CARGO CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25670FE 777 SEAT TRACK AT Y450 FR 15 IS CORRODED 2L72 4F RTA35EU 20050726002792005072600279NM 2005 7 26 05FDEA02064 120050725A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE LT NR 13 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. [CLOSED] 2L73 4F RTA22WE 20050726002822005072600282NM 2005 7 26 05FDEA02067 120050725A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE RT NR 22 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. [CLOSED] 2L73 4F RTA22WE 20050726002932005072600293NM 2005 7 26 05FDEA02075 120050725A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE LT NR 29 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. [CLOSED] 2L73 4F RTA22WE 20050726002962005072600296NM 2005 7 26 05FDEA02073 120050725A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE LT NR 25 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. [CLOSED] 2L73 4F RTA22WE 20050726002982005072600298NM 2005 7 26 05FDEA02077 120050725A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE LT NR 31 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. [CLOSED] 2L73 4F RTA22WE 20050726003012005072600301NM 2005 7 26 05FDEA02080 120050725A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE RT NR 30 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. 2L73 4F RTA22WE 20050726003042005072600304NM 2005 7 26 05FDEA02088 120050725A527065284498 STRIKER BOEING727 727200 138407ENM ZONE 800 WORN A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25221FE 20932 AIR RETURN FOR AFT AIRSTAIR LIGHT ILLUMINATED WHEN AIRBORNE AFTER SECOND PACK WAS TURNED ON. INSPECTED AFT AIRSTAIR "UP LOCK" SWITCH AND STRIKER PLATE.FOUND STRIKER PLATE HAS A HOLE WORN THROUGH IT.APPLIED AERODYNAMIC TAPE TO AREA. 2L73 4F RTA3WE 20050726003052005072600305NM 2005 7 26 05FDEA02083 120050725A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE RT NR 1 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA1-5510-87597. [CLOSED] 2L73 4F RTA22WE 20050726003072005072600307NM 2005 7 26 05FDEA02085 120050725A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE LT NR 3 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. [CLOSED] 2L73 4F RTA22WE 20050726003082005072600308NM 2005 7 26 05FDEA02086 120050725A278010608199 SWITCH BOEING727 727200 138407ENM ZONE 600 INOPERATIVE A FDEAE ENGINE SHUTDOWN N FALSE WARNING CLCLIMB 1 SO25221FE 20932 NR 7 SLAT FAILED TO RETRACT FROM FLAPS 2 DEGREE TO FLAPS UP. AIRCRAFT ROLLED LEFT DURING RETRACTION. PERFORMED QRH PROCEDURES. LED REMAINED OUT. OPERATED SLATS NUMEROUS TIMES - EXTEND AND RETRACT FUNCTION CK'S GOOD. FOUND NR 7 SLAT EXTEND SWITCH INOP. REPLACED PER MM 27-82-011-4. OPS CK GOOD. 2L73 4F RTA3WE 20050726003092005072600309NE 2005 7 26 05FDEA02087 220050725A7230 COMPRESSOR BOEING727 727100 1384036NM PWA JT8 JT8D7B 52053NE NR 3 ENGINE STALLED A FDEAC ABORTED TAKEOFF ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS TOTAKEOFF 1 SO25194FE 19143 DURING T/O THROTTLE UP THE NR 3 ENG HAD A COMPRESSOR S TALL . RAN NR 3 ENG UP INDIVIDUALY AND AT A VERY LOW EPR NR 3 EXPERIENCED ANOTHER COMPRESSOR STALL. WINDS CALM. INSP INLET & EXH AREA. ALL NORMAL CKED FOR BLEED VALVE OPERATION, NORMAL, HEARD ALL 3 CLANKS SCREEN IS CLEAR. ADJUSTED P&D VALVE PER P/W 72-00-00 PAGE124. RAN NR 3 ENG PER JRH CHAP 5 ALL CK NORMAL. WENT TO 90 PERCENT THREE TIMES SLOW AND FAST.. NO COMPRESSOR STALLS. 2L73 4F4 FRTA3WE E2EA 20050726003102005072600310NM 2005 7 26 USAA050834 120050705A5320 WEB BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU52779 23861 CLT - FOUND WEB CORRODED 10 INCHES, UNDER STRAP AT THE AFT CARGO COMPARTMENT DOOR OPENING. REMOVED DAMAGE, FABRICATED AND INSTALLED NEW PART IAW BOEING DWG 65-47957 AND SRM 51-10-02. (M) 2L72 4F RTA16WE 20050726003112005072600311NM 2005 7 26 USAA050835 120050705A5313 STRINGER BOEING737 7373B7 1384580NM FUSELAEG CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU 23861 CLT - FOUND STRINGERS CORRODED 12 INCHES, CARGO FLOOR STRINGERS AT STATION 773. REPLACE OUT OF LIMITS STRINGER SECTION IAW SRM 53-60-53 AND TR 53-10-06B. (M) 2L72 4F RTA16WE 20050726003122005072600312NM 2005 7 26 USAA050836 120050705A5320 FLOOR SUPPORT BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19441US 24812 CLT - FOUND FLOOR SUPPORT CORRODED 1 INCH BY 1 INCH, FORWARD CABIN FLOOR STRUCTURE STATION 310 RBL 13 TOP OF SUPPORT INBOARD SCREW HOLE. REMOVED DAMAGED STIFFENER, FRILLED UP AND INSTALLED PART IAW SRM 53-10-51 FIG 101, PAGE 105. (M) 2L72 4F RTA16WE 20050726003132005072600313EA 2005 7 26 A6WA200540229 120050708A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE DENTED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31461AW 7870 MWC 1 DENT IN AFT FUSELAGE AT FS 672 BETWEEN STRINGERS 26L AND 27L. CUT OUT DAMAGED AREA AND INSTALLED FABRICATED FILLER PARTS IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050726003152005072600315EA 2005 7 26 A6WA200540228 120050708A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT WING CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31461AW 7870 MWC 59 WING PLANK, RT WING, UNDER FUEL ACCESS PANEL 650EB IS SEVERLY CORRODED AROUND ENTIRE CIRCUMFERENCE OF OPENING, .150 INCH WIDE X .005 INCH DEEP. BLENDED LOWER WING PLANK IAW MFG REO. (K) 2L72 4F4 FRTA21EA E15NE 20050727000012005072700001NM 2005 7 27 USAA050828 120050705A5330 SKIN BOEING737 7374B7 1384702NM FUSELAGE LIGHTNING STRIKEA USAAK NONE O OTHER ININSP/MAINT 1 EA19441US40664 24812 CLT - FOUND SKIN WITH LIGHTNING STRIKE .125 INCH BY .125 INCH, STATION 500B, 2 INCHES BELOW STRINGER 18L AND 12 AFT. FASTENER INSTALLED IN SKIN IAW 53-00-01 FIG 219. (M) 2L72 4F RTA16WE 20050727000022005072700002EU 2005 7 27 07252005A 120050725A2750 FLAP SYSTEM SAAB SF340 340B 7860101EU TE FLAPS LACK OF LUBE A NSVAO OTHER F FLT CONT AFFECTED APAPPROACH 1 EA27304CE 198 WITH AUTOPILOT ENGAGED THE FLAPS DO NOT MOVE. FOUND MINOR STICKING BETWEEN FLAP AND COVE WHERE FRESHLY PAINTED. SMOOTHED SURFACE AND LUBRICATED. 2L72 4T RTA52EU 20050727000042005072700004NM 2005 7 27 USAA050832 120050705A5313 STRINGER BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU52779 23861 CLT - FOUND STRINGER CORRODED 12 INCHES, CARGO FLOOR STRINGERS AT STATION 773. REPLACED OUT OF LIMITS STRINGER SECTIONS IAW SRM 53-60-53 AND TR 53-10-06B. (M) 2L72 4F RTA16WE 20050727000052005072700005NM 2005 7 27 C7WA200400072 120050107A2613 WARNING LIGHT BOEING727 727222 1384073NM PWA JT8 JT8D1 52044NE BODY OVERHEAT ILLUMINATED A C7WAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO177638U 19911 LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED THEN EXTINGUISHED ON ITS OWN INFLIGHT. INSPECTED DUCTING IN AFT AIRSTAIR AREA AND RAN ENGINES AT TAKEOFF POWER. UNABLE TO DUPLICATE PROBLEM, NO LEAKS NOTED. SYSTEM OPERATIONAL, CHECK GOOD IAW MM. (K) 2L73 4F4 F A3WE E2EA 20050727000102005072700010SW 2005 7 27 KBM2005F00160 120050719A7410106149501 IGNITER BOX BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19188TV 2704 IGNITER BOX, UNIT POPS CIRCUIT BREAKER, REMOVED AND REPLACED. (K) 1G71 3U3 U H2SW E4CE 20050727000122005072700012NM 2005 7 27 C7WA200400073 120050107A2613356802255 SENSING ELEMENT BOEING727 727222 1384073NM PWA JT8 JT8D1 52044NE AFT BODY OVRHT ERRATIC A C7WAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO177638U 19911 IN FLIGHT, LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED, RT DUCT PRESSURE INDICATED 80 PSI. MADE PRECAUTIONARY LANDING. TIGHTENED ALL CLAMPS IN AIRSTAIR AREA. REPLACED LT AND RT PURGE LINE COUPLING SEALS. REMOVED AND REPLACED LOWER AFT BODY OVERHEAT LOOP DETECTOR. SYSTEM OPS CHECK GOOD IAW MM. (K) 2L73 4F4 F A3WE E2EA 20050727000132005072700013SO 2005 7 27 GUU2005F00035 120050701A3397 WIRE EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE GALLEY EXPOSED A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO17266AS 120188 EMERGENCY FLOOR LIGHT TRACK IN FRONT OF GALLEY IS INOPERATIVE WITH WIRES EXPOSED. REPLACED FUSE AND SPLICED WIRE. (K) 2L72 4T4 TRTA31SO E20NE 20050727000142005072700014NE 2005 7 27 KBM2005F00156 220050718A7323704A34130141 CONTROL CABLE SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1 60030NE ENGINE GOVERNOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19215LA 2143 ENGINE GOVERNOR CABLE WORN, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050727000162005072700016 2005 7 27 KBM2005F00157 420050721A2312064105430 RADIO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE VHF SYSTEM INTERMITTENT A KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19115SH1276 3141 VHF RADIO, UNIT CUS OUT AFTER 5 SECONDS OF TRANSMISSION. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050727000172005072700017SW 2005 7 27 KBM2005F00159 120050720A7410106149501 IGNITER BOX BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19188TV3 2704 IGNITER BOX, UNIT POPPED WHEN STARTER BUTTON PRESSED. (K) 1G71 3U3 U H2SW E4CE 20050727000182005072700018EU 2005 7 27 KBM2005F00165 120050715A771456337078012 INDICATOR SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE ENG NG INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH 2337 NG GAUGE, UNIT AUCTUATION 89-72 PERCENT. INDICATED W/NO POWER CHANGE. REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20050727000212005072700021EA 2005 7 27 ASOA05545 120050621A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE MAIN PAX STIFF A ASOAK NONE O OTHER ININSP/MAINT 1 SO27821AS 7194 DURING A GROUND INSPECTION, FA REPORTED THE PASSENGER DOOR DIFFICULT TO CLOSE FROM INSIDE. MAINTENANCE OPENED AND CLOSED THE PASSENGER DOOR SEVERAL TIMES WITH NO DEFECTS NOTED. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050727000232005072700023EA 2005 7 27 ASOA05546 120050622A5320 SILL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27851AS 7360 DURING C-CHECK, THE CARGO COMPARTMENT FLOOR SILL PLATE WAS FOUND TO BE CRACKED AND CORRODED AROUND THE SCREW HOLES BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CARGO COMPARTMENT FLOOR SILL PLATE. (K) 2L72 4F4 FRTA21EA E15NE 20050727000252005072700025 2005 7 27 KBM2005F00161 420050718A3422103002201 GYRO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE DIRECTIONAL SPINNING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19115SH93 3141 DIRECTIONAL GYRO, UNIT SPINS IN FLIGHT. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050727000262005072700026EA 2005 7 27 ASOA05550 120050623A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE ENGINE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27852AS 7369 DURING HANGAR MAINTENANCE, THE ENGINE SUPPORT BEAM WAS FOUND TO BE CRACKED IN THE TOP WEB AT THE FIRE LOOP BRACKET BEYOND LIMITS. MAINTENANCE REPAIRD THE ENGINE SUPPORT BEAM UPPER WEB AT THE FIRE LOOP BRAKCET IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050727000272005072700027EU 2005 7 27 KBM2005F00163 120050710A6520350A33215300 BEARING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE TAIL ROTOR CRACKED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV729 3296 LAMINATED BEARING, UNIT HAS CRACKED AND BULGE AROUND THE RUBBER. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050727000282005072700028EA 2005 7 27 ASOA05549 120050623A33501317 LAMP BRUCE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27902EV 7620 DURING A GROUND INSPECTION, AN EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN AN EXTERIOR EMERGENCY LIGHT. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050727000292005072700029WP 2005 7 27 DHL2005802500 120050622A5347SE085300063 CARGO TRACK DOUG DC8 DC873 302199CWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH84803 46076 UPPER CARGO COMPT NR 2 TRACK CORRODED, STA 780.000 - 786.000. REMOVED CORROSION FROM TRACK NR 2 IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-3 FIG. 12. CUT OUT NR 2 TRACK DAMAGED SEGMENT IAW SRM 53-2-3 PG. 49-50 FIG. 14. FABRICATED SPLICES IAW SRM 53-2-3 PG. 49-50 FIG. 14. CLEANED, TREATED AND PRIMED AREA AND SPLICES IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT AND SPLICES IAW SRM 53-2-3 PG. 49-50 FIG. 14, SRM 51-3-0 PG. 1. TORQUED IAW SRM 51-3-1 PG. 3. 2L74 4F RT4A25 20050727000302005072700030WP 2005 7 27 DHL2005802501 120050627A5753 SKIN DOUG DC8 DC873 302199CWP RT WING TE FLAP DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH84803 46076 RT INBD FLAP UPPER EXTERNAL SKIN INTERIM REPAIR, STA XW 104.000-110.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG.1, SRM 57-7-1 FIG. 1. REMOVED PLATING WITH EXISTING INTERIM REPAIR IAW SRM 51-1-21 PG.1. FABRICATED NEW PLATING (AL2024Y3 0.040) IAW SRM 57-7-1 FIG. 1 ITEM D. CLEANED, TREATED AND PRIMED NEW PLATING INTERNAL PART AND AREA IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED NEW PLATING IAW SRM 51-1-21 PG.1, SRM 51-3-0 PG. 1. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050727000312005072700031WP 2005 7 27 DHL2005802526 120050715A5330 DOUBLER DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH84803 46076 EXTERIOR FUSELAGE NOSE SECTION ESTRUCTURAL MODIFICATION DOUBLER (ACS) CRACKED 0.250 AT AFT UPPER CORNER OF PRIMARY HEAT EXCHANGER STA -12.000 L-24L (MAJOR REPAIR). CORR.: PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 07-11-05, DWG Z20-R02 REV. IR DATED 06-24-05. REMOVED FASTENERS IAW SRM 51-1-21 PG. 1, SRM 51-1-20D PG. 21. CUT OUT DAMAGED SECTION IAW DWG Z20-R02. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER, TRIPLER, AND FILLER (AL2024T3 0.100) IAW DWG Z20-R02- CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG. 9. INSTALLED REPAIR PARTS IAW DWG Z20-R02, SRM 51-1-21 PG.1, SRM 51-1-20D PG.9. TORQUED IA2L74 4F RT4A25 20050727000372005072700037 2005 7 27 KBM2005F00164 420050716A34215040017901 GYRO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE ATTITUDE INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19751H 71 3403 ATTITUDE GYRO, FLAG WILL NOT DISAPPEAR WHEN POWER IS ON, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050727000402005072700040WP 2005 7 27 DHL2005802536 120050715A572037048412 FITTING DOUG DC8 DC873 302199CWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH84803 46076 NR 2 MAIN TANK INTERIOR OUTBD FWD FITTING CRACKED STA XRS 74.869 S-61 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG.1. REMOVED CRACKED FITTING IAW SRM 51-1-21 PG.1, SRM 51-1-20D PG. 21. CLEANED AND APPLIED TOP COATING MATERIAL TO AREA IAW SRM 51-1-12 PG. 7. APPLIED SEALANT TO FAYING SURFACE IAW SRM 51-1-12. INSTALLED NEW FITTING IAW SRM 51-1-20D PG. 9, SRM 51-1-23 (PLI WASHER) TORQUED IAW SRM 51-3-1. REFER TO NR. 030838 FOR LEAK CHECK. 2L74 4F RT4A25 20050727000422005072700042WP 2005 7 27 DHL2005802539 120050718A533057552713N SKIN DOUG DC8 DC873 302199CWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH84803 46076 FUSELAGE INTERNAL SKIN CORRODED STA 220.000 L-35L TO L-36 (FWD CARGO COMPT. BILGE) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 07-15-05 DWG Z20-R06 REV. IR DATED 06-24-05. REMOVED FASTENERS IAW SRM 51-1-21 PG. 1, SRM 51-1-20D PG. 21. REMOVED CORROSION IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG. 2P. CUT OUT DAMAGED SECTION IAW DWG Z20-R06. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED NEW SKIN SEGMENT INTERNAL DOUBLER 16EA STRAPS 12EA INTERNAL SPLICES 4 EA INTERNAL FINGER DOUBLER AND EXTERNAL SPLICE DOUBLER IAW DWG Z20-R06. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG. 9. INS2L74 4F RT4A25 20050727000452005072700045WP 2005 7 27 DHL2005802542 120050723A5543 SUPPORT BRACKET DOUG DC8 DC873 302199CWP RUDDER TAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH84803 46076 RUDDER TAB HINGE SUPPORT BRACKET CRACKED. REMOVED RUDDER TAB IAW MM 27-21-2 PG. 201. REMOVED CRACKED BRACKET IAW SRM 51-1-21. FABRICATED BRACKET IAW JC EA55100013-001-D, DWG DOUGLAS 4701452 AND BOEING COMPANY MSG 1-109638692-2. PERFORMED NDT INSP IAW DC8 NDT SPM PART 08-00-02/07. CLEANED AND PRIMED AREA AND BRACKET IAW SRM 51-1-8B. INSTALLED NEW BRACKET IAW SRM 51-1-21. REINSTALLED RUDDER TAB IAW MM 27-21-2 PG. 202-203. REFER TO NR 030703 FOR OPS CHECK. 2L74 4F RT4A25 20050727000462005072700046WP 2005 7 27 DHL2005802543 120050718A5311 FRAME DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH84803 46076 RT MLG WW FRAME CRACK 5.000 STA 868.000 RBL 50 (MAJOR REPAIR). CORR.: PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG. 2 SHEET 3,6. REMOVED FASTENERS IAW SRM 51-1-21 PG. 1, SRM 51-1-20D PG. 21. CUT OUT DAMAGED FRAME SEGMENT IAW SRM 53-2-0 FIG. 2 SHEET 3. PERFORMED DETAIL VISUAL INSP. NO CRACK OR CORROSION FOUND. FABRICATED NEW FRAME SEGMENT 2 EA SPLICE DOUBLER IAW SRM 53-2-0 FIG. 2 SHEET 3-6, SRM 51-1-4 PG. 1. HEAT TREATED FROM IAW SRM 51-1-1 PG. 1-13-17. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG. 9. INSTALLED REPAIR PARTS IAW SRM 53-2-0 FIG. 2 SHEET 3,6, SRM 51-1-21 PG. 1, SRM 51-1-20D PG. 9. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050727000472005072700047WP 2005 7 27 DHL2005802544 120050718A5311377307325P FRAME DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH84803 46076 CARGO COMPT. FRAME 3.000 CRACK STA 278.000 L-20L (MAJOR REPAIR). CORR.: PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9 DATED 27 JUN 05, BOEING MSG 1-105552361-2, 1-105552361-3 DATED 27 JUN 05. REMOVED SUB FLOOR IAW SRM 51-1-21A PG. 1-4. REMOVED FITTING IAW SRM 51-1-20D PG. 21. PERFORMED STOP HOLE OF 0.250 ON FRAME CRACK END IAW BOEING MSG 1-105552361-2. NDT INSPECTED AREA IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED MODIFIED FITTING IAW BOEING MSG 1-105552361-2 AND SHIM. NDT INSPECTED NEW FITTING IAW NDT SPM PART 08-00-02 TO 07. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG. 9. INSTALLED MODIFIED FITTING IAW BOEING MSG 1-105552361-2, SRM 512L74 4F RT4A25 20050727000482005072700048WP 2005 7 27 DHL2005802545 120050717A5310 DOOR FRAME DOUG DC8 DC873 302199CWP CARGO BAY CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH84803 46076 CARGO DOOR AFT LWR JAMB CORNER 0.500 CRACKED STA 1440.000 L-32R TO L-33R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9 BOEING MESSAGE 1-106666113-2, 1-106666113-3 DATED 07-01-03. REMOVED FASTENERS IAW SRM 51-1-21 PG. 1, SRM 51-1-20D PG. 21. CUT OUT DAMAGED SECTION IAW BOEING MSG 1-106666113-2 (SEMAN DRAWING ED-4019 DATED 06-29-05) SRM 53-2-0 FIG. 2, TR 53-188 SHEET 5,6,7,8. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED EXTERNAL REPAIR DOUBLER, EXTERNAL REPAIR TRIPLER AND FILLER IAW BOEING MSG 1-106666113-2 (SEMAN DRAWING ED-4019) SRM 53-2-0 FIG. 21, TR 53-188 SHEET 5,6,7,8. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW S2L74 4F RT4A25 20050727000492005072700049WP 2005 7 27 DHL2005802502 120050627A5753 SKIN DOUG DC8 DC873 302199CWP RT WING TE FLAP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH84803 46076 RT OUTBD FLAP UPPER SKIN CRACKED 0.500 APPROX. AT STA XF 304.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG.1, SRM 57-7-1 FIG. 4, TR 57-94. REMOVED CRACKED PLATING IAW SRM 51-1-21 PG.1. FABRICATED NEW PLATING IAW SRM 57-7-1 FIG. 4, TR 57-94 ITEM C. CLEANED, TREATED AND PRIMED NEW PLATING INNER PART AND AREA IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG. 9. INSTALLED NEW PLATING IAW SRM 51-1-21 PG. 1. 2L74 4F RT4A25 20050727000512005072700051SO 2005 7 27 GUU2005F00032 120050626A3350D3660401 BATTERY PACK EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE EMERGENCY LIGHT INOPERATIVE A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO17261AS 120141 AT SCHEDULED ROUTINE MAINTENANCE, AFT EMERGENCY LIGHTS INOPERATIVE. REMOVE AND REPLACED AFT BATTERY PACK. (K) 2L72 4T4 TRTA31SO E20NE 20050722002242005072200224NE 2005 7 22 BB05055 220050720A7200 ENGINE BOEING757 757225 1384959NM RROYCERB211 RB211535E4 54555NE LEFT FAILED A USAAO OTHER BXJSMOKE/FUMES/ODORS/SPARKS ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 EA19608AU283858458 22204 31411 PVD FLT 208 EN-ROUTE, CLT TO PVD - DURING THE FLIGHT, THE LAVATORY SMOKE DETECTORS ALARMED FOR SMOKE, AND THEN SHUT OFF. AFTER LANDING, THE GROUND CREWS NOTED AN OIL ODOR IN THE JETWAY OF THE TERMINAL. MAINTENANCE NOTED THAT THERE WAS AN OIL MIST IN THE INTAKE OF THE LEFT ENGINE DURING INSPECTION. THE AIRCRAFT WAS MAINTENANCE FERRIED TO CLT WHERE THE ENGINE WAS REPLACED. 2L72 4F4 FRTA2NM E12EU 20050725000132005072500013 2005 7 25 UPS05144946 420050720A2565 WARNING SYSTEM AIRBUSA300 A300F4622R 3930360EU PAX DOOR SLIDE INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01146UP 0829 BUZZER DOES NOT SOUND DURING TESTING ENTRY DOOR EMERGENCY ESCAPE SLIDE PLACED BUZZER ON DEF M306464 PER MEL 52-73-01-2 PLACARD INSTALLED. R&R EMER ESCAPE SLIDE TEST SWITCH 39WN. POS CK NORMAL IAW MM 25-61-21-4 THIS CLEARS M306464 2L72 4F RTA35EU 20050725000262005072500026NM 2005 7 25 UPS05M44943 120050721A3350 BATTERY DOUG MD11 MD11F 3023600NM EMERGENCY LIGHT DISCHARGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01272UP 48571 EMERGENCY BATTERY 1 LOW. BATTERY CHARGED UP AFTER 45 MIN OF CHARGING. EMERGENCY BATTERY TEST GO OD 2L73 4F RTA22WE 20050725000332005072500033NM 2005 7 25 AWXA200500841 120050707A57546546431279 SKIN BOEING737 7373G7 1384595NM FORE FLAP DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 MCN - MAJOR REPAIR - DURING C16 CHECK FOUND UPPER SURFACE OF THE L/H OUTBOARD FORE FLAP DISBONDED 12 INCHES FROM INBOARD END FROM WBL 219L TO WBL 221L. MAINTENANCE REMOVED DISBONDED AREA FROM UPPER SURFACE OF THE L/H OUTBOARD FORE FLAP DISBONDED AND CLEANED AREA IAW BOEING 737-300 SRM 51-70-10-0 REPAIR 22. FABRICATED REPAIR FILLER AND DOUBLER IAW BOEING 737-300 SRM 51-70-10-0 REPAIR 22. BONDED REPAIR PARTS TO UPPER SURFACE OF THE L/H OUTBOARD FORE FLAP DISBONDED 12 INCHES FROM INBOARD END FROM WBL 219L TO WBL 221L IAW BOEING 737-300 SRM 51-70-10-0 REPAIR 22. 2L72 4F RTA16WE 20050726000022005072600002SO 2005 7 26 GUU2005F00030 120050702A245044B258051002 RELAY EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE APU SHORTED A GUUAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO29261AS 120141 VERY STRONG ODOR IN COCKPIT. REPLACED APU RELAY. (K) 2L72 4T4 TRTA31SO E20NE 20050726000242005072600024NM 2005 7 26 GTIA050166 120050505A5313 STRINGER DOUG MD80 MD83 3023681NM FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23827NK 49793 FOUND CABIN STRINGER 18R CUSP CORRODED. REMOVED CORROSION AT STRINGER 18R CUSP MEMBRANE. CUT OUT DAMAGED SECTION OF CUSP. FABRICATED REPAIR DOUBLER. TREATED AND PRIMED DOUBLER. INSTALLED REPAIR DOUBLER AT STRINER 18R MEMBRANE. APPLIED TOP COAT. (M) 2L72 4F RT 20050726000272005072600027NM 2005 7 26 GTIA050168 120050507A5320 CUSP WEB DOUG MD80 MD83 3023681NM FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23827NK 49793 FOUND CABIN STRINGER 18R CUSP CORRODED. INSTALLED NEW SECTION OF CUSP. AND REPAIR ANGLES. INSTALLED WEB. INSTALLED REPAIR ANGLES. INSTALLED TWO AIR GRILLS. INSTALLED RIGHT OUTBOARD FLOORBOARDS. INSTALLED FRAME FITTINGS. INSTALLED WEB STATION. (M) 2L72 4F RT 20050726000382005072600038NE 2005 7 26 AALA20050453 220050718A7200 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE LEFT STALLED A AALAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 SW21432AA 49350 725576 PHX INFLIGHT T436/18JUL PASSING 5000 FT ON DEPARTURE EXPERIENCED SINGLE LOUD BAND AND FAILURE OF LT ENGINE. RETURNED TO PHX AND LANDED WITHOUT INCIDENT. REPLACED NUMBER ONE ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F4 F A6WE E9NE 20050726000572005072600057SO 2005 7 26 CHQA200500130 120050722A3350RPS1B BATTERY PACK EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCHARGED A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11286SK7324 2506 145443 OVERHEAD FLIGHT ATTENDANT CEILING EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED NR 1 BATTERY POWER SUPPLY IAW EMB 145 AMM 33-50-04. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050726000582005072600058GL 2005 7 26 CHQA200500132 220050723A7200 ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 1 FAILED A CHQAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 GL11561RP 145447 CAE311837 FL350, THRUST SET TO CLIMB, NR 1 ITT YELLOW RANGE AT APPROX 903-904 CELSIUS. POWER RETARDED & ITT REDUCED TO GREEN. ITT REMAINED 80-90 DEGREES HOTTER THAN NR 2 ENG ITT, A HIGHER FUEL FLOW OBSERVED, & VIBRATIONS ON HP SPOOL OF NR 1 NOTABLY HIGHER (STILL WITHIN LIMITS) THAN VIBRATIONS ON NR 2. OIL INDS ON TAKEOFF BOTH NORMAL, & NO MESSAGES PRESENTED. PERFORMED PRECAUTIONARY ENG SHUTDOWN & LANDED AT NEAREST AIRPORT. ATC NOTIFIED. PRECAUTIONARY ENGINE SHUTDOWN PROCEDURE FOLLOWED. ATTEMPTED APU START, FAILED TO ACCELERATE. APPEARED IT WAS NOT LIGHTING PROPERLY, NO RISING EGT NOTED. ACCOMP, & AT LOWER ALTITUDES & WITHIN LIMITS OF APU STARTER, ATTEMPTED TO START 2 TIMES, SAME RESULT. LANDED W/O INCIDENT. 2L72 4T4 FRTT00011ATTE6CH 20050726000732005072600073CE 2005 7 26 DXTA200500858 120050724A326065430087 DOWNLOCK SWITCH CESSNA500 560CESSNA 2076750CE MLG INOPERATIVE E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07347QS 5600357 ON TAKEOFF, RIGHT MAIN GEAR WOULD NOT COME UP (HANDLE DID). FOUND ACTIVATING SIDE OF RT UPLOCK SWITCH BAD. REMOVED AND REPLACED SWITCH IAW 560M/M CHPT 32-31-05. ADJUSTED SWITCH IAW CE-560 CHPT 32-61-00. PERFORMED LANDING GEAR FUNCTIONAL CHECK, AND DOWNLOCK, UPLOCK PARALLELING CIRCUIT TEST. PERFORMED LANDING GEAR TIMED CYCLE TEST IAW CE-560 M/M CHPT 32-01-00. OPERATIONAL CHECKS SATISFACTORY. 2L72 4F RTA22CE 20050726000762005072600076NE 2005 7 26 AALA20050460 220050723A7200 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE RIGHT MAKING METAL A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21430AA 49342 718267 DFW INFLIGHT T563/23JUL - ON CLIMB-OUT APPROXIMATELY 1400 FEET RIGHT ENGINE LOW OIL PRESSURE LIGHT ON. RIGHT OIL QUANTITY NORMAL. RIGHT OIL TEMPERATURE DECREASING. REDUCED POWER ON RIGHT ENGINE TO IDLE. APROXIMATELY 5 MINUTES LATER INCREASED POWER ON RIGHT ENGINE AND VIBRATION BEGAN. SHUTDOWN RIGHT ENGINE. FOUND OIL PRESSURE OUT OF LIMITS AND METAL IN OIL. REPLACED RIGHT HAND ENGINE. 2L72 4F4 F A6WE E9NE 20050726000812005072600081NM 2005 7 26 GTIA050184 120050527A5320 CUSP WEB DOUG MD80 MD83 3023681NM FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23833NK 49449 AFT PIT SUBFLOOR AT LEFT CUSP CORRODED FROM STATION 1022-1041. REMOVED PANELS FOR ACCESS. REMOVED CORROSION FOUND IS OUT OF LIMITS. CUT OUT DAMAGED AREA, FABRICATED WEB AND DOUBLER. TREATED AND PRIMED, INSTALLED REPAIR TWO FITTINGS. RE-INSTALLED REMOVED ACCESS PANELS. (M) 2L72 4F RT 20050726000892005072600089NM 2005 7 26 UPS05544954 120050722A2560MXP21000 SMOKE GOGGLES BOEING757 75724APF 1384969NM COCKPIT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01423UP 25325 CO-PILOT SMOKE GOGGLES LENS CRACKED. REPLACED SMOKE GOGGLES. 2L72 4F RTA2NM 20050726000912005072600091WP 2005 7 26 UPS05844948 120050711A5340 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE:C1 STA 834.500 L19L FRAME TO INTERCOSTAL FITTING CRACKED. REMOVED, FABRICATED AND INSTALLED FRAME FITTING IAW 51-1-20D AND DWG 3779874. 2L74 4F RT4A25 20050726000972005072600097NM 2005 7 26 GTIA050183 120050524A5320 CUSP WEB DOUG MD80 MD83 3023681NM FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23833NK 49449 FOUND FORWARD CARGO COMPARTMENT CORROSION ON CUSP WEB FS 450-475 L18L. REMOVED FLOORBOARDS AND PANELS FOR ACCESS. REMOVED CORROSION. FOUND CUSP-WEB IS OUT OF LIMITS. FABRICATED CUSP WEB 17 INCHES BY 5.5 INCHES. TREAT AND PRIMED CUSP WEB AND INSTALLED FABRICATED PARTS. REINSTALLED ACCESS PANELS AND FLOORBOARDS. (M) 2L72 4F RT 20050726001112005072600111CE 2005 7 26 DXTA200500855 120050723A3234 HANDLE CESSNA560 560XL 2076702CE MLG LOCKED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07605QS 5605321 LANDING GEAR HANDLE WILL NOT RELEASE FROM DOWN POSITION TO RETRACT GEAR AFTER TAKEOFF. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20050726001122005072600112CE 2005 7 26 DXTA200500860 120050724A2720 FITTING CESSNA750 750 2076810CE ACCUMULATOR LOOSE E DXTAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL07921QS 7500241 "RUD STBY SYS FAIL" CAS MESSAGE ILLUMINATED TWICE IN FLIGHT. RSS PRESSURE FLUCTUATED 2200 TO 3800 PSI. DUPLICATED SQK ON GROUND. FOUND RUDDER STANDBY ACCUMULATOR PRESSURE LOW SERVICED ACCUMULATOR IAW 750 MM CHAP 12-10-16. TIGHTENED LOOSE FITTING ON ACCUMULATOR GAUGE. OPS CHECK GOOD. 2L72 4J RTT00007WI 20050726001192005072600119 2005 7 26 GTIA050153 420050504A3417 CADC DOUG DC9 DC983 3022083WP NR 2 INOPERATIVE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 NR 2 CADC INOPERATIVE, F/O`S AIRSPEED INDICATOR AND VSI INOPERATIVE, TAIL SWAP WITH AIRCRAFT 804. RESET C/B ON NR 2 CADC, PERFORMED BITE CHECK, OPS CHECK NORMAL. (M) 2L72 4F RTA6WE 20050726001202005072600120 2005 7 26 GTIA050154 420050513A2210 PUSH-PULL ROD DOUG DC9 DC983 3022083WP NR 1 THOTTLE DISCONNECTED A GTIAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 GL23836NK 53045 AFTER INITIAL LEVEL OFF, THE NR 1 ENGINE AT NEAR CLIMB POWER STOPPED RESPONDING TO AUTO-THROTTLE POWER REDUCTION, THROTTLES BECAME SPLIT AND A/T DISCONNECTED. FULL THROTTLE GAVE NO INCREASE IN POWER AND FULL IDLE WOULD DROP NO LOWER THAN 1.64 EPR, ENGINE WAS SHUT-DOWN ON APPROACH WITH EPR AT 1.53 AND ABOUT 9000 FEET. FOUND NR 1 ENGINE THROTTLE PUSH-PULL CONTROL ROD DISCONNECTED AT AFT CONTROL SECTOR, RE-CONNECTED AS REQUIRED AND RIGGED THROTTLE SYSTEM NR 1. BOTH ENGINE PART POWR STOPS WERE INSTALLED AND THEN STOWED, RUN-UP AND TRIM AS REQUIRED. GROUND CHECKS GOOD. (M) 2L72 4F RTA6WE 20050726001312005072600131EU 2005 7 26 MALA050590 120050720A53477253721459 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15437XJ 340B437 DURING 4Y/2Y CHECK IN BNA FOUND LAV SEAT TRACK PN 7253721-459 IS CORRODED AND HAS BEEN REPLACED IAW SRM 51-40-27. REF: EAMS WORK ORDER 212613 TASK 2515 2L72 4T RTA52EU 20050726001392005072600139EA 2005 7 26 A6WA200540225 120050701A7900 CHECK VALVE CNDAIRCL600 CL6002B19 1900309EA LT ENGINE MALFUNCTIONED A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31449AW 7818 LEFT ENGINE OIL PRESSURE MASTER WARNING IN FLIGHT. REMOVED LEFT ENGINE OIL REPLENISHMENT CHECK VALVE. INSTALLED CHECK VALVE TAGGED REPAIR, P/N 2810044-101, S/N 972. ADDED 5 QUARTS TO LEFT ENGINE. OIL TANK SERVICED TO 5 1/2 FULL RED AMM 79-12-13. NO LEAKS NOTED. (M) 2L72 4F RTA21EA 20050726001452005072600145EA 2005 7 26 A6WA200540222 120050627A261147359719 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY MALFUNCTIONED A A6WAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL31431AW 7256 SMOKE CARGO MESSAGE AFTER PUSHBACK, GROUND INSPECTION OF CARGO HOLD. NO SMOKE FOUND. MEL`D NR 1 CARGO SMOKE DETECTOR. REMOVED AND REPLACED CARGO SMOKE DETECTOR. OPS CHECK GOOD IAW CRJ MM 26-15-00. REMOVED OFF MEL. S/N OFF 1719, S/N ON 2222. (M) 2L72 4F RTA21EA 20050726001492005072600149NM 2005 7 26 DHL2005788004 120050726A3260 SWITCH BOEING727 727214 138407RNM NLG DOOR OUT OF ADJUST A DHLAO OTHER N FALSE WARNING DEDESCENT 1 SO01788AT 21958 NOSE GEAR RED LIGHT FDW PANEL COMES ON AT 320 KTS IAS DURING DESCENT (DOOR LIGHT). CLEAN AND RE-ADJUSTED LEFT NOSE GEAR DOOR SWITCH IAW MM 32-62-11, OPS CK OK. 2L73 4F A3WE 20050726002362005072600236NM 2005 7 26 2005UALA00674 120050718A5230 DOOR FRAME BOEING737 737522 138449FNM CARGO BAY DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29914UA 25381 FWD CARGO DOOR LOWER AFT CORNER FRAME AT LOWER INBOARD FASTENER DAMAGED. MAJOR REPAIR ACP'D BY FRAME SECTION REPLACEMENT. 2L72 4F RTA16WE 20050726002382005072600238NM 2005 7 26 2005UALA00676 120050720A5330141W1325 SKIN BOEING777 777222 1385219NM PWA PW4077PW4077 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29780UA36438 26944 LT UPPER FUSELAGE EXTERNAL SKIN STA 398, STR 1L HAS PREVIOUS BLEND-OUT AND REQUIRES VERIFICATION OF MATERIAL LOSS WITHIN LIMIT OF SRM. PRE-EXISTING BLEND REPAIR. BLEND WAS CUT OUT AND REPAIRED PER 777 SRM 53-00-01, REPAIR 7. 2L72 4F4 FRTT0001SE E46NE 20050726002452005072600245NM 2005 7 26 2005UALA00680 120050719A5312 PRESSURE PANEL BOEING737 737522 138449FNM FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29914UA 25381 LT MLGWW UPPER PRESSURE DECK HAS CRACK AT STA 664 LBL 32. MAJOR REPAIR ACP'D PER MM53-21-98, INSTALLED DOUBLER REPAIR. 2L72 4F RTA16WE 20050726002482005072600248 2005 7 26 2005UALA00683 420050720A2565 SLIDE AIRBUS320 A320232 3930326EU DOOR 2L FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29409UA 462 DURING SLIDE TEST DEPLOYMENT DOOR 2LH SLIDE INFLATION WAS NOT COMPLETE, SIDE WALLS WERE NOT FULL AND 5 OUT OF 6 POSTS DID NOT INFLATE. EVERYTIME A SLIDE DEFECT IS FOUND DURING THE MAINTENANCE OF SLIDE IN THE SHOP, A SHOP SDR IS ISSUED. HOWEVER DURING THE OVERHUAL OF THIS UNIT AFTER THIS SDR INCIDENT, THERE WAS NO SHOP SDR REPORTED TO SHOW ABNORMAL CONDITION OF THE SLIDE/RAFT. SEVERAL PROBABLE CAUSES COULD RESULT IN UNDER INFLATION. IT COULD BE DUE TO LOW BOTTLE PRESSURE BEFORE DEPLOYMENT OR PERHAPS THE ASPIRATOR MALFUNCTIONED OR MAYBE ASPIRATOR WAS PARTIALLY BLOCKED BY A FOREIGN OBJECT ON THE AIRCRAFT. NOT ENOUGH DATA TO PINPOINT THE PROBABLE CAUSE. 2L72 4F RTA28NM 20050726002512005072600251 2005 7 26 2005UALA00686 420050719A256562620468U1 SLIDE BOEING737 737522 138449FNM L1 DOOR DISLODGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29913UA 25291 DOOR 1 LEFT SLIDE PACK CAME COMPLETELY OFF. THE CAUSE FOR THIS EVENT IS UNKNOWN. THE CORRECTIVE ACTION WAS INSPECTION OF THE SLIDE AND RE-INSTALLATION ON SAME AIRCRAFT. 2L72 4F RTA16WE 20050726002542005072600254NM 2005 7 26 2005UALA00689 120050717A335020131A BATTERY BOEING757 757222 1384956NM PWA 2037 PW2037 NE DOORS 1R INOPERATIVE A UALAO OTHER L NO TEST ININSP/MAINT 1 WP29596UA 28749 EMERGENCY EXIT LIGHTS AT DOOR 1R INOPERATIVE. REPLACED BATTERY PACK AT M730. REPLACED BATTERY PACK AT M730. 2L72 4F4 FRTA2NM E17NE 20050726002572005072600257NM 2005 7 26 05FDEA02048 120050724A5320 INTERCOSTAL DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 SNRM N0706: MAIN DECK CARGO - ATTIC AREA STATION 1906 RIGHT HAND LONGERON 4 FOUND INTERCOASTAL DAMAGED. REMOVED AND REPLACED AS PER SRM 51-35-01 VOL. II. THIS REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050726002772005072600277NM 2005 7 26 05FDEA02062 120050725A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE RT NR 12 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. 2L73 4F RTA22WE 20050726002802005072600280NM 2005 7 26 05FDEA02065 120050725A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE RT NR 16 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. [CLOSED] 2L73 4F RTA22WE 20050726002872005072600287NM 2005 7 26 USAA050799 120050623A5315 FLOORBEAM BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19590US 23935 FOUND FLOORBEAM CORRODED 48 INCHES LONG BY 2 INCHES WIDE BY .035 INCH DEEP, 2.5 INCHES LONG BY 2 INCHES WIDE BY .033, FLOORBEAM, BS 328, RBL 12 INCHES-50 INCHES AND LBL 50 INCHES. FABRICATED PARTS, INSTALLED NEW T-CHORD AND REPAIR ANGLE PER SRM 53-00-51, FIG 201, 51-40-02. (M) 2L72 4F RTA16WE 20050726002912005072600291NM 2005 7 26 05FDEA02072 120050725A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE LT NR 23 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. [CLOSED] 2L73 4F RTA22WE 20050727000032005072700003 2005 7 27 SA05089 420050723A2565 SLIDE AIRBUS320 A320214 3930316EU LEFT DAMAGED A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19113UW 1141 PIT - THE AFT LEFT REPLACEMENT SLIDE WAS FOUND SEPARATED FROM ITS BACKING PLATE. MAINTENANCE INSTALLED THE AFT LEFT SLIDE/RAFT TO THE BACKING PLATE AND THEN BACK ONTO THE AIRCRAFT. OK FOR SERVICE. 2L72 4F RTA28NM 20050727000072005072700007SO 2005 7 27 GUU2005F00033 120050628A335012021299501 LIGHT EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE EXTERIOR INOPERATIVE A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO17261AS 120141 LOWER EXTERIOR EMERGENCY LIGHTS ON LT AND RT SIDES NOT WORKING. DETERMINED RT LIGHT ASSEMBLY TO BE TRIPPING THE CIRCUIT BREAKER. REPLACED RT LOWER EXTERIOR EMERGENCY LIGHT ASSY. LT AND RT SIDES OPERATE PROPERLY. (K) 2L72 4T4 TRTA31SO E20NE 20050727000202005072700020 2005 7 27 KBM2005F00162 420050718A34215040017901 GYRO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE ATTITUDE INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19751H 88 3403 ATTITUDE GYRO, FLAG STAYS ON, AIRCRAFT, MEL UNIT. (K) 1G71 3U3 U H9EU E19EU 20050727000362005072700036WP 2005 7 27 DHL2005802533 120050719A532046143972N FITTING DOUG DC8 DC873 302199CWP FUSELAGE BROKEN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH84803 46076 FWD ACCY COMPT. FITTING BROKEN 0.500 STA 70.000 L-31R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG. 1. REMOVED DAMAGED FITTING IAW SRM 51-1-20D PG. 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG. 9. INSTALLED NEW FITTING IAW SRM 51-1-20D PG. 9, SRM 51-1-21 PG. 1. TORQUED IAW SRM 51-3-1 2L74 4F RT4A25 20050727000382005072700038NM 2005 7 27 C7WA200400081 120050303A326065609472 ACCESSORY UNIT BOEING727 727222 1384073NM PWA JT9 JT9D* NE E/E BAY INOPERATIVE A C7WAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO17764OU 19913 RT MLG UNSAFE LIGHT ILLUMINATED IN FLIGHT. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT. OPERATIONAL CHECK IAW MM. OPS CHECK NORMAL. (K) 2L73 4F4 F A3WE E20EA 20050727000542005072700054SO 2005 7 27 GUU2005F00036 120050622A3397 WIRE EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE EMERGENCY LIGHT UNSECURE A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO17266AS 120188 EMERGENCY FLOOR LIGHTING IN FRONT OF GALLEY INOPERATIVE. SECURED WIRE AT GALLEY AREA FLOOR LIGHTING. (K) 2L72 4T4 TRTA31SO E20NE 20050727000552005072700055NM 2005 7 27 USAA050829 120050705A5330 SKIN BOEING737 7374B7 1384702NM FUSELAGE LIGHTNING STRIKEA USAAK NONE O OTHER ININSP/MAINT 1 EA19441US 24812 CLT - FOUND SKIN WITH LIGHTNING STRIKE, STATION 469, 4 INCHES ABOVE STRINGER 21L. FASTENER INSTALLED IN SKIN IAW 737 SRM 53-00-01 FIG 219. (M) 2L72 4F RTA16WE 20050727000562005072700056NM 2005 7 27 USAA050831 120050705A5320 SPLICE BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19441US40664 24812 CLT - FOUND SPLICE CRACKED .5 INCH, BS 907, STRINGER S4L. REPLACED SPLICE WITH NEW PART IAW SRM 51-10-02. (M) 2L72 4F RTA16WE 20050727000572005072700057EA 2005 7 27 ASOA05548 120050622A5321 PRESSURE PANEL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27851AS 7360 DURING A C-CHECK, THE PRESSURE FLOOR AT LBL 36, RBL 36 FROM FS 409+128 TO FS 559 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE PRESSURE FLOOR AT LBL 36, RBL 36 FROM FS 409+128 TO FS 559 IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050727000582005072700058WP 2005 7 27 DHL2005802504 120050629A5347SE085300063 CARGO TRACK DOUG DC8 DC873 302199CWP FUSELAGE BROKEN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH84803 46076 UPPER CARGO COMPT NR 6 TRACK LUGS BROKEN STA 310.000 - 370.000. CUT OUT NR 6 TRACK DAMAGED SEGMENT IAW SRM 53-2-3 PG 49-50 FIG 14. FABRICATED SPLICES IAW SRM 53-2-3 PG 49-50 FIG 14. CLEANED, TREATED AND PRIMED AREA AND APLICES IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT AND SPLICES IAW SRM 53-2-3 PG 49-50, SRM 51-3-0 PG 1. TORQUED IAW SRM 51-3-1 PG 2A-3. 2L74 4F RT4A25 20050727000592005072700059WP 2005 7 27 DHL2005802506 120050706A5320 STIFFENER DOUG DC8 DC873 302199CWP BULKHEAD CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH84803 46076 ITEM REF. NR. 030754: FWD ACCESSORY COMPT. FWD PRESSURE BULKHEAD STIFFENER CRACK 1.500" STA 8.000 RBL 20. CORR.: REMOVED CRACKED STIFFENER IAW SRM 51-1-21 PG.1. FABRICATED NEW STIFFENER IAW SRM 53-3-3 FIG. 3 ITEM A. HEAT TREATED STIFFENER IAW SRM 51-1-1 PG. 1, 13,17. CLEANED, TREATED AND PRIMED AREA AND STIFFENER IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11. INSTALLED NEW STIFFENER IAW SRM 51-1-21 PG.1, SRM 51-1-20D PG. 9. TORQUED IAW SRM 51-3-1 PG. 2A (NUT). 2L74 4F RT4A25 20050727000602005072700060WP 2005 7 27 DHL2005802507 120050706A5312 STIFFENER DOUG DC8 DC873 302199CWP BULKHEAD CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH84803 46076 ITEM REF. NR 030753: FWD ACCESSORY COMPT. FWD PRESSURE BULKHEAD STIFFENER CRACK 2.000 STA 8.000 LBL 20. REMOVED CRACKED STIFFENER IAW SRM 51-1-21 PG.1. FABRICATED NEW STIFFENER IAW SRM 53-3-3 FIG. 3. HEAT TREATED IAW SRM 51-1-1 PG. 1,13,17. INSTALLED NEW STIFFENER IAW SRM 51-1-21 PG.1, SRM 51-1-20D PG. 9, SRM 51-3-0 PG.1. TORQUED IAW SRM 51-3-1. (CLEANED, TREATED AND PRIMED NEW STIFFENER IAW SRM 51-1-8B AFTER HEAT TREATMENT). 2L74 4F RT4A25 20050727000672005072700067WP 2005 7 27 DHL2005802516 120050715A57305611002501 PANEL DOUG DC8 DC873 302199CWP LT WING DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH84803 46076 LT WING T/E UPPER PANEL DELAMINATED (STA XW 5.000 - 47.000). REMOVED AND REPLACED LT WING TE UPPER PANEL (STA XW 5.000-47.000) IAW SRM 51-3-0 PG. 1. TORQUED IAW3 SRM 51-3-1. 2L74 4F RT4A25 20050727000692005072700069WP 2005 7 27 DHL2005802524 120050715A57405754705501N FITTING DOUG DC8 DC873 302199CWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH84803 46076 LT STUB WING INTERIOR FITTING CRACKED 2.000 (MAJOR REPAIR)STA XOLDO 67.750 PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG.1. REMOVED CRACKED FITTING IAW SRM 51-1-21 PG.1, SRM 51-1-20D PG.21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG. 9. INSTALLED NEW FTTING IAW SRM 51-1-20D PG. 9, SRM 51-1-21 PG.1. TORQUED IAW SRM 51-3-1 2L74 4F RT4A25 20050727000722005072700072EA 2005 7 27 ASOA05552 120050623A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27851AS 7360 DURING A C-CHECK, THE FS 280 FRAME AT RBL 9 LOWER ANGLE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FS 280 FRAME AT RBL 9 LOWER ANGLE IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050727000732005072700073 2005 7 27 2005072301 420050723A2565 SLIDE EMB ERJ170ERJ170100LR EU L1 DOOR DEPLOYED A UHLAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 GL17648RW 17000068 ON 07-23-05 FLT 7602 ORD-GRR, DEF L1 SLIDE PARTIALLY DEPLOYED WHILE OPENING. AIRCRAFT FERRIED FROM GRR TO ORD. 2L74 4F RTA56NM 20050727000742005072700074NM 2005 7 27 QXEA200501131 120050723A27202379003001 REGULATOR DHAV DHC8 DHC8202 2809007NM RUDDER MALFUNCTIONED A QXEAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 NM09365PH157241709 526 SEA FLIGHT NR 2180, AFTER TAKEOFF, NR 2 RUDDER HYDRAULIC PRESSURE AND RUDDER FULL PRESSURE CAUTION LIGHTS ILLUMINATED. MAINTENANCE REPLACED THE RUDDER DUAL PRESSURE REGULATOR IAW -8(200) AMM 27-20-38, PAGES 40-405. PERFORMED OPERATIONAL TEST. NO DEFTECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050727000772005072700077EU 2005 7 27 F3LA200500036 120050725A2751 WARNING LIGHT AIRBUSA319 A319112 3930323EU TE FLAPS ILLUMINATED A F3LAO OTHER J WARNING INDICATION APAPPROACH 1 NM03915FR 1851 UPON APPROACH, FLIGHT CREW REPORTED F/CTL FLAPS FAULT WHEN SELECTING FLAPS TWO. FLAPS STAYED AT ZERO. DECLARED AN EMERGENCY. AIRCRAFT LANDED WITHOUT INCIDENT. PERFORMED ROUTINE TROUBLESHOOTING OF FLAPS AND SLATS PER AMM 27-81-00-740-002. NO CURRENT FAULTS. PERFORMED MANUAL CHECK OF SLATS AND FLAPS. ALL POSITIONS NO FAULTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA28NM 20050727000792005072700079EU 2005 7 27 AWXA200500843 120050724A2910S43500272 MANIFOLD AIRBUS320 A320231 3930325EU HYD SYSTEM LEAKING A AWXAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP28634AW50316 091 DURING CLIMB HAD GREEN HYDRAULIC FAILURE. AIRCRAFT RETURNED TO PHX, CREW DECLARED AND PREPARED CABIN FOR EMERGENCY. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE GROUND LEAKAGE MEASUREMENT MODULE LEAKING. REMOVE AND REPLACED THE GROUND LEAK MEASUREMENT MANIFOLD IAW AIRBUS MM 29-19-41-04. LEAK MEASUREMENT MANIFOLD WAS B.E.R. 2L72 4F RTA28NM 20050727000802005072700080NM 2005 7 27 AWXA200500844 120050723A3350100865 POWER SUPPLY BOEING737 7373G7 1384595NM EMERGENCY LIGHT DISCHARGED A AWXAO OTHER O OTHER TXTAXI/GRND HDL 1 WP28302AW 24009 CREW REPORTEDT RT EMERGENCY EXIT LIGHT OVER 23R FLICKERING AND THE EMERGENCY EXIT LIGHT OVER DOOR 2L FLICKERING. MAINTENANCE REMOVED AND REPLACED THE RIGHT AFT POWER SUPPLY. OPERATIONAL CHECKS GOOD. 2L72 4F RTA16WE 20050727000812005072700081 2005 7 27 AWXA200500845 420050723A256560592101 RESERVOIR AIRBUS320 A320232 3930326EU ESCAPE SLIDE FAILED A AWXAO OTHER O OTHER TXTAXI/GRND HDL 1 WP28657AW15501364 1083 BOS - EES - INBOUND WRITE UP INTO BOS, CREW REPORTED CIDS PANEL CAUTION LIGHT ON POST FLT MX REPORT INDICATES SLIDE BOTTLE EMER R. MAINTENANCE FERRIED AIRCRAFT TO PHX FOR REPAIR. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND OVERWING ESCAPE SLIDE RESERVOIR IAW AIRBUS MM 25-62-46-04. 2L72 4F RTA28NM 20050727000832005072700083EU 2005 7 27 AWXA200500848 120050725A3350321454 EPSU AIRBUS320 A320232 3930326EU EMERGENCY LIGHT FAILED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28663AW 1419 ORD - EEL - DURING 4 DAY CHECK, FOUND THE EPSU AND BATTERY LEFT SIDE OVER WING EXIT FAILED OPERATIONAL CHECK. MAINTENANCE REMOVED AND REPLACED THE LEFT OVERWING EPSU IAW AMERICA WEST AIRLINES TASK CARD R1C33303. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA28NM 20050727000852005072700085SO 2005 7 27 1341062005 120050620A32501159SCH4023 STEERING SYS GULSTMG1159 GIV 3980115SO NLG FAILED E N93AO OTHER O OTHER TXTAXI/GRND HDL 1 SO13441QS6568 1341 WHEN TURNING STEERING TO RIGHT CLUNKING NOISE IS HEARD 2L72 4F RTA12EA 20050727000862005072700086WP 2005 7 27 IXXA0500082O 120050722A7797C65039ATI1 WIRE HARNESS DOUG DC8 DC871F 302199DWP NR 2 EGT DEFECTIVE A IXXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW11828BX83768272 45993 DURING TAKEOFF FROM KTOL TO KATL AFTER V1 NR 2 EGT STARTED TO FLUX FROM 860 TO MAX EGT 1000 (DIGITAL AND POINTER) CONTINUED TO FLUX ON CLIMB-OUT. ALL OTHER ENGINE INDICATIONS WERE NORMAL. THE CREW ELECTED TO OVERFLY INTERIM STOP ATL AND FLY DIRECT TO KMCO. MAINTENCE FOUND THE NR 2 ENGINES EGT HARNESS READING HIGH RESISTANCE. REMOVED AND REPLACED THE EGT HARNESS. ENGINE RUN WAS COMPLETE AND NO OTHER DEFECTS WERE NOTED PER ALL APPLICABLE MANUALS AND AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20050727000872005072700087WP 2005 7 27 IXXA0500083O 120050726A7797C65039ATI1 WIRE HARNESS DOUG DC8 DC871F 302199DWP NR 2 EGT DEFECTIVE A IXXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW11828BX83772276 45993 DURING TAKEOFF FROM KTOL BOTH EGT INDICATIONS ON NR 2 ENG BECAME ERRATIC. INFLT-ANALOG WENT OFF SCALE HIGH AND DIGITAL SHOWS 1000 INTERMITTENTLY. THE CREW RETURNED THE AIRCRAFT TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED EGT HARNESS, RAN ENGINES AND THE OPERATIONAL TEST WAS GOOD ON GROUND PER ALL APPLICABLE MANUALS. NO OTHER DEFECTS WERE NOTED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20050727000922005072700092NM 2005 7 27 USAA050825 120050701A5320 INTERCOSTAL BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19441US 24812 CLT - FOUND INTERCOSTAL CORRODED 1 INCH BY 1 INCH, BS 306 LBL 11 FORWARD CABIN FLOOR SUPPORT. INSTALLED NEW INTERCOSTAL IAW SRM 53-10-51, 51-10-02, 51-40-02. (M) 2L72 4F RTA16WE 20050727000952005072700095NM 2005 7 27 USAA050824 120050701A5315 FLOORBEAM BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19441US40664 24812 CLT - FOUND FLOORBEAM CORRODED 1.5 INCH BY 1.5 INCH, STATION 312 RBL 10. NEW TEE CAP INSTALLED IAW SRM 53-10-01, AND SRM 53-00-51. (M) 2L72 4F RTA16WE 20050727000962005072700096NM 2005 7 27 USAA050823 120050701A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE DENTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU 23861 PIT - FOUND SKIN DENTED 2 INCHES BY 2 INCHES, DENT ONE BS 500-500A, S20R-S21R, DENT 2 AND 3 AT BS 500A-500B S19R-S20R. CUT OUT THREE DENTS, FABRICATED TRIPLERS, SIZE OF REPAIR IS 44.5 INCH BY 23 AT 10.22 LBS IAW SRM 53-00-01. (M) 2L72 4F RTA16WE 20050727000972005072700097SO 2005 7 27 C2XA05SH069 120050716A532014521713005 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717524 145399 SHV-DURING C-CHECK THE CENTER OMEGA BEAM AT FR 20 HAS VARIOUS AREAS OF CORROSION. MAINTENANCE REMOVE AND REPLACED CENTER OMEGA BEAM AT FR 18-23 IAW EMB 145 SRM 51-40-02.AIRCRAFT WAS APPROVE FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050727001012005072700101SO 2005 7 27 C2XA05SH082 120050721A533014566202006 SKIN PANEL EMB 145 EMB145EP 3260221SO FUSELAGE LIGHTNING STRIKEA C2XAK NONE O OTHER ININSP/MAINT 1 SW2714943 145040 SHV-DURING C-CHECK MAINTENANCE FOUND LIGHTNING STRIKES AT LOWER RT WING, NEAR PNL 631 AB. MAINTENANCE REPAIRED LIGHTNING STRIKES AT LOWER RT WING, NEAR PNL 631 AB I/A/W EC 5330-01480, REPAIR FIGURES NR 5 7 & 6. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050727001022005072700102SO 2005 7 27 C2XA05SH083 120050721A532014530644403 FLOOR SUPPORT EMB 145 EMB145EP 3260221SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714943 145040 SHV-DURING C-CHECK MAINTENANCE FOUND LT OMEGA BEAM HAS CORROSION AT VARIOUS AREAS BETWEEN FRAMES 38-46. MAINTENANCE REPAIRED LT OMEGA BEAM BETWEEN FRAMES 38 & 46 I/A/W EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050727001032005072700103SO 2005 7 27 C2XA05SH084 120050721A532014521713005 FLOOR SUPPORT EMB 145 EMB145EP 3260221SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714943 145040 SHV-DURING C-CHECK MAINTENANCE FOUND CENTER OMEGA BEAM HAS CORROSION AT FRAME 20. MAINTENANCE REMOVED AND REPLACED CENTER OMEGA BEAM FROM FRAMES 11-23 I/A/W EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050727001052005072700105SO 2005 7 27 C2XA05SH086 120050721A532014521700007 FLOOR SUPPORT EMB 145 EMB145EP 3260221SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714943 145040 SHV-DURING C-CHECK MAINTENANCE FOUND LT OMEGA BEAM FLOOR SUPPORT FLANGE HAS CORROSION BETWEEN FRAMES 20-24. MAINTENANCE REMOVED & REPLACED LT OMEGA BEAM FROM FRAMES 20-23 I/A/W EC 5320-01229. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050727001072005072700107SO 2005 7 27 C2XA05SH088 120050721A551012060867005 HINGE EMB 145 EMB145EP 3260221SO RUDDER WORN A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714943 145040 SHV-DURING C-CHECK MAINTENANCE FOUND HAT BUSHING HOUSING AT ATTACHMENT FITTING FOR UPPER HYDRAULIC ACTUATOR ON RUDDER I IS WORN. MAINTENANCE REPAIRED HAT BUSHING HOUSING FOR UPPER HYDRAULIC ACTUATOR ON RUDDER I I/A/W EC 5540-01043 REV A. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050727001102005072700110NM 2005 7 27 USAA050820 120050630A5320 WEB BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU 23861 CLT - FOUND WEB CORRODED 10 INCHES, WEB UNDER STRAP AT THE AFT CARGO COMPARTMENT DOOR OPENING. REMOVED DAMAGE, FABRICATED AND INSTALLED NEW PART IAW BOEING DWG 65-47957 AND SRM 51-10-02. (M) 2L72 4F RTA16WE 20050727001112005072700111SO 2005 7 27 C2XA05SH070 120050717A491014526850401 FIREWALL EMB 145 EMB145LR 3260212SO AFT APU CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715986 145254 SHV-DURING C-CHECK CRACKS (2) AT RIVETS FWD SIDE OF APU FIEWALL RT SIDE PLUS UPPER RT SIDE. MAINTENANCE REPAIRED APU FIREWALL CRACK FWD SIDE R/H 3 OCLOCK POSITION IAW EC5330-01477 AND REPAIRED APU RIRE WALL AT UPPER R/H SIDE IAW EMB 145 SRM 53-32-13 AND IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVE FOR RETURN TO SERVICE 2L72 4T RTT00011AT 20050727001142005072700114SO 2005 7 27 C2XA05SH073 120050717A532014530644405 FLOOR SUPPORT EMB 145 EMB145EP 3260221SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714943 145040 SHV-DURING C-CHECK LT OMEGA BEAM HAS VARIOUS AREAS OF CORROSION BTW FR 45-52.MAINTENANCE BLENDED LT OMEGA BEAM BTW FR 45-52. FR 49 IS OUT OF LIMIT ALL OTHER FRMS WITHIN LIMIT IAW EMB SRM 53-23-10. REPAIR OMEGA BEAM AT FR 49 IAW EMB 145 SRM 53-00-10 FIGURE 202, SHEET 2.INSTALLED NUTPLATES IAW EC 5320-01137. THE AIRCRAFT WAS APPROVE FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050727001152005072700115SO 2005 7 27 C2XA05SH074 120050717A532014530644401 FLOOR SUPPORT EMB 145 EMB145EP 3260221SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714943 145040 SHV-DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT VARIOUS AREAS BTW FRM 35-39. MAINTENANCE BLENDED LT OMEGA BEAM BTW FRMS 35-39. FR 38 IS OUT OF LIMIT ALL OTHER FRMS ARE WITH IN LIMITS IAW EMB 145 SRM 53-23-10. REPAIRED L/H OMEGA BEAM AT FRM 38 IAW EMB 145 SRM 53-00-10 SECTION 3 FIGURE 202 SHEET 1. INSTALLED NUTPLATE IAW EC 5320-01137. THE AIRCRAFT WAS APPROVE FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050727001162005072700116SO 2005 7 27 C2XA05SH075 120050717A532014530644403 FLOOR SUPPORT EMB 145 EMB145EP 3260221SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714943 145040 SHV DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT VARIOUS AREAS BTW FRMS 38-46. MAINTENANCE BLENDED LT OMEGA BEAM BTW FRMS 38-46. FR 44 IS OUT OF LIMIT ALL OTHER FRMS WITHIN LIMIT IAW EMB 145 SRM 53-23-10.REPAIRED LT OMEGA BEAM AT FR 44 IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVE FOR RETURN TO SERVICE 2L72 4F RTT00011AT 20050727001172005072700117SO 2005 7 27 C2XA05SH076 120050717A532014530642403 FLOOR SUPPORT EMB 145 EMB145EP 3260221SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714943 145040 SHV DURING C-CHECK LT OMEGA BEAM HAS CORROSION BTW FR 28-33.MAINTENANCE BLENDED LT OMEGA BEAM FRMS 28-33. FR 33 IS OUT OF LIMITS ALL OTHER FRMS WITHIN LIMITS IAW EMB 145 SRM 53-22-10.REPAIRED LT OMEGA BEAM AT FR 33 IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVE FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050727001182005072700118SO 2005 7 27 C2XA05BT047 120050719A323074555033 MODULE EMB 145 EMB145LR 3260212SO MLG FAULTY A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW27139944354 4354 145291 CREW REPORTED, LANDING GEAR AIR/GROUND FAIL CAUTION LIGHT ON TAKEOFF, LANDING GEAR LEVER WOULD NOT RETRACT AIRCRAFT AIR RETURNED TO BOSTON, AIRCRAFT MAINTENANCE FERRIED TO BTV, MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL MODULE IAW EMB145 AMM #32-32-02, OPS.CHECKED GOOD. 2L72 4T RTT00011AT 20050727001192005072700119SO 2005 7 27 C2XA05BT048 120050719A21214611028900 FAN EMB 145 EMB145LR 3260212SO CABIN FAULTY A C2XAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW27265451127 1127 145558 CREW REPORTED CABIN SMOKE ONCE AIRBORNE WITH ENGINE BLEED SELECTED ON, MAINTENANCE REMOVED AND REPLACED CABIN RECIRCULATION FAN IAW EMB145 MM AT 21-24-01. OPS.CHECKED GOOD. NO SMELL NOTED. 2L72 4T RTT00011AT 20050727001202005072700120SO 2005 7 27 C2XA05SH077 120050721A533014520571001 SKIN PANEL EMB 145 EMB145EP 3260221SO FUSELAGE DENTED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714943 145040 SHV-DURING C-CHECK MAINTENANCE FOUND R/H FUSELAGE SKIN HAS A DENT BETWEEN FRAMES 19 AND FRAME 20 AT STR 17R. MAINTENANCE REPAIRED DENT AT R/H FUSELAGE SKIN AT FRAME 19 -20, STR 18R (INSTEAD OF 17R) I/A/W EC 5330-01480, REPAIR FIGURES 4 AND 7. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050727001212005072700121SO 2005 7 27 C2XA05SH078 120050721A533014520571001 SKIN PANEL EMB 145 EMB145EP 3260221SO FUSELAGE LIGHTNING STRIKEA C2XAK NONE O OTHER ININSP/MAINT 1 SW2714943 145040 SHV- DURING C-CHECK MAINTENANCE FOUND LIGHTENING STRIKES FROM FRAMES 19-20, STR 18R (MID) & 18R(AFT). MAINTENANCE REPAIRED LIGHTENING STRIKES AT FRAMES 19-20, STR 18R MID & 18R AFT I/A/W EC 5330-01480, REPAIR FIGURES 4 & 7. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050727001242005072700124NE 2005 7 27 ALG2005F00039 120050716A2697MS3476110 CONNECTOR SKRSKYS76 S76 8143010NE ALLSN 250C 250C30S 03013GL FIRE DETECTION FAULTY E ALGAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SW03701AL 760238 ON PRE START, NR 1 ENGINE FIRE TEE HANDLE LIGHTS WOULD NOT TEST IN FORWARD POSITION. THE MECHANIC REMOVED AND REPLACED THE FAULTY CONNECTOR AND THE AIRCRAFT WAS RETURNED TO SERVICE AFTER OPERATIONAL CHECK OF THE SYSTEM. (K) 1G72 3U3 U H1NE E1GL 20050727001262005072700126EA 2005 7 27 A6WA200540203 120050613A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31419AW 7633 CLIP AT FS 280, LBL 9, OUTBOARD SIDE, IS CRACKED IN RADIUS APPROX .50 INCH LONG. REMOVED CRACKED CLIP AT FS 280 LBL 9 OUTBOARD SIDE AND REPLACED WITH NEW CLIP P/N 601R31113-57 IAW CRJ200 SRM 51-42-06 AND 51-42-21. (M) 2L72 4F RTA21EA 20050727001272005072700127NE 2005 7 27 ALG2005F00038 220050714A7261 CHIP DETECTOR SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL1S1 60030NE NR 1 ENGINE INOPERATIVE E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03863AL 760536 PRIOR TO REACHING DESTINATION, NR 1 ENGINE CHIP LIGHT CAME ON. AC LANDED AND MAINTENANCE CHECKED NR 1 ENGINE CHIP PLUG AND NO DEFECTS WERE NOTED. THE AC WAS RETURNED TO SERVICE AFTER OPERATIONAL CHECKS WERE COMPLETED. (K) 1G72 3U3 UNCH1NE E19EU 20050727001282005072700128WP 2005 7 27 0501129981 120050725A2120 CLAMP DOUG DC9 DC931 3022065WP LT ACM LEAKING A NWAAO OTHER J WARNING INDICATION CRCRUISE 1 GL01994Z 47097 DURING CRUISE FLIGHT AT FL290 WITH AIRFOIL ANTI-ICE SYSTEM ON, THE CABIN STARTED CLIMBING AT 300 FT/MIN. INITIATED DESCENT AND COMPLIED WITH THE RED BORDERED CHECK LIST. WHEN THE ANTI-ICE SYSTEM WAS SWITCHED OFF THE CREW WAS ABLE TO CONTROL CABIN PRESSURE BUT WHEN IT WAS SWITCHED BACK ON AS NEEDED THEY LOST CABIN PRESSURE. FLIGHT CONTINUED TO DESTINATION AT 10,000 FEET AND LANDED WITHOUT INCIDENT. MAINTENANCE AT PHL FOUND A LEAKING CLAMP ON THE ACM TO HEAT EXCHANGER CONNECTION BUT DID NOT HAVE A CLAMP TO REPLACE IT WITH. LOG PAGE WAS DEFERRED AND THE AIRCRAFT HAS RETURNED TO SERVICE. 2L72 4F A6WE 20050727001292005072700129EA 2005 7 27 A6WA200540204 120050614A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31419AW 7633 LT SIDE FLOOR SUPPORT ANGLE AT FS 621 CRACKED APPROX 1.1 INCH LONG LBL 41.5, WL 73. CUT AWAY DAMAGED SECTION OF ANGLE AND INSTALLED REPAIR ANGLE IAW BOMBARDIER, INC REO 601R-53-61-117 REV C. (M) 2L72 4F RTA21EA 20050727001302005072700130CE 2005 7 27 ALG2005F00040 120050715A7714206075681101 TACHOMETER CESSNASTC STC206C 1182107CE ALLSN 250C 250C28B 03013GL ENGINE INOPERATIVE E ALGAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW033185P 45775 ON LIFT OFF PILOT NOTICED TURBINE TACH INDICATOR IS ZERO, LANDED THE AIRCRAFT. THE MECHANIC REMOVED AND REPLACED THE ROTOR TACH INDICATOR AND THE AC WAS RETURNED TO SERVICE. (K) 1H71 3O3 UNTA4CE E1GL 20050727001312005072700131GL 2005 7 27 ALG2005F00041 220050714A7261 ENGINE BELL 206 206L4 1182110SW ALLSN 250C 250C30 03013GL OIL CONSUMPTION E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03180AL 52104 CAE890398 DURING HOT REFUELING AT BASE, THE PILOT WAS INFORMED THAT SMOKE COMING FROM THE EXHAUST STACK, HE SHUT THE AIRCRAFT DOWN. POST INSPECTION REVEALED THAT ENGINE OIL LEVEL WAS LOW (TWO LEVEL MARKS). THE MECHANIC REMOVED AND REPLACED THE ENGINE ASSY AND THE AIRCRAFT WAS RETURNED TO SERVICE. (K) 1G71 3U3 UNCH2SW E1GL 20050727001332005072700133NE 2005 7 27 ALG2005F00045 120050712A5210 DOOR SKRSKYS76 S76C 8143008NE ALLSN 250C 250C30 03013GL RT PAX UNSECURE E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03866AL 760562 UPON ARRIVAL, DURING PASSENGER UNLOADING, ONE OF THE PASSENGERS PULLED THE RED EMERGENCY DOOR RELEASE AND JETTISON THE RT PASSENGER DOOR. WHEN THE COPILOT ATTEMPTED TO CLOSE THE DOOR, HE NOTICED THAT THE DOOR WAS LOOSE AND NOT SECURED. AC WAS SHUTDOWN AND OPS WAS NOTIFIED. THE MECHANIC PUT THE DOOR BACK ON AND SECURED IT IAW MM AND AC WAS RETURNED TO SERVICE. (K) 1G72 3U3 UNCH1NE E1GL 20050727001342005072700134EA 2005 7 27 A6WA200540202 120050614A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31419AW 7633 RIGHT SIDE FLOOR SUPPORT ANGLE AT FS 621 CRACKED APPROX 1.1 INCH LONG, RBL 41.5 WL 73. REPAIRED RIGHT SIDE FLOOR SUPPORT ANGLE AT FS 621 BY CUTTING AWAY DAMAGED AREA AND INSTALLED MG REPAIR PARTS IAW BOMBARDIER REO 601R-53-61-117 REV C. (M) 2L72 4F RTA21EA 20050727001402005072700140SO 2005 7 27 C2XA05BT042 120050623A335020131A BATTERY PACK EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT FAULTY A C2XAK NONE O OTHER ININSP/MAINT 1 SW271855662 62 145595 CREW REPORTED, "THAT THE OVERWING EMERGENCY EXIT ROW LIGHT DID NOT WORK." MAINTENANCE REMOVED AND REPLACED NR 4 EMERGENCY EXIT LIGHT BATTERY PACK IAW EMB145 AMM 33-50-04. OPS.CHECKED GOOD. 2L72 4T RTT00011AT 20050727001412005072700141SO 2005 7 27 C2XA05IA084 120050628A3350 LIGHT EMB 145 EMB145LR 3260212SO PAX DOOR INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713992 145284 IAH 0 FLIGHT 2749, DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE PAX DOOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE EMERGENCY LIGHTS WITH NO DEFECTS FOUND, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.(NOTE: NO PARTS WERE CHANGED OR FOUND DEFECTIVE) 2L72 4T RTT00011AT 20050727001452005072700145SO 2005 7 27 C2XA05IA082 120050616A335078241 INVERTER EMB 145 EMB145XR 3260214SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2711106 145650 DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHT ON OVERHEAD PANEL IS INOP. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT INVERTER FOR THE AFFECTED LIGHT, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20050727001472005072700147EA 2005 7 27 ASOA05553 120050623A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27851AS 7360 DURING A C-CHECK, THE FORWARD AND AFT FLOOR SUPPORT ANGLES AT FS 280 BETWEEN LBL 9 AND RBL 9 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FORWARD AND AFT FLOOR SUPPORT ANGLES AT FS 280 BETWEEN LBL 9 AND RBL 9 IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050727001482005072700148EA 2005 7 27 A6WA200540199 120050613A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31419AW 7633 CLIP AT FS 280, RBL 9, INBOARD SIDE IS CRACKED IN RADIUS APPROX .40 INCH LONG. REMOVED CRACKED CLIP AT FS 280 RBL 9 LEFT SIDE AND INSTALLED NEW CLIP IAW CRJ 200 SRM 51-40-11, 51-23-00, 51-42-06 AND 51-42-21. (M) 2L72 4F RTA21EA 20050727001492005072700149EA 2005 7 27 ASOA05554 120050623A5312 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27851AS 7360 DURING A C-CHECK, THE PILOTS BULKHEAD WEB AT FS 280 BETWEEN LBL 9 AND RBL 9 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE PILOTS BULKHEAD WEB AT FS 280 BETWEEN LBL 9 AND RBL 9 IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050727001512005072700151CE 2005 7 27 AJC2005F00008 120050619A32341223820381 CONTROL PANEL BEECH MU300 400A 1155402CE PWA JT15 JT15D5 52112NE MLG DEFECTIVE E AJCAO OTHER O OTHER CLCLIMB 1 EA25400HS1923 RK314 AFTER TAKEOFF, CREW REPORTED THAT LANDING GEAR HANDLE WAS LOCKED IN DOWN POSITION AND THEY COULD NOT RETRACT GEAR. LANDING GEAR DOWNLOCK OVERRIDE WAS ENGAGED AND THE GEAR RETRACTED NORMALLY. ON DESCENT THE CREW REPORTED THAT THE SPEED BRAKES WOULD NOT DEPLOY ON THE LANDING ROLL. THE CREW DID NOT DECLARE AN EMERGENCY. T/S RESPECTIVE SYSTEMS AND CORRECTED AST FOLLOWS: FOUND GROUND SAFETY OVERRIDE (WOW) SOLENOID IN LANDING GEAR CONTROL PANEL ASSY DEFECTIVE. FOUND LOOSE CONNECTOR PLUG AT THE PC 161 CONNECTION, RESEATED AND SECURED CONNECTOR PLUG. JACKED AIRCRAFT, PERFORMED GEAR EXTENSION/RETRACTION OF GEAR DOWNLOCK OVERRIDE CHECK AND FUNCTION CHECK OF THE SPEED BRAKES. ALL CHECK PERFORMED SATISFACTORY. (K)2H72 4F4 FRTA16SW E25EA 20050727001572005072700157WP 2005 7 27 JRAA587062305 120050623A5414 SKIN PANEL CVAC 640 640340D 2422814WP RROYCEDART DART5424 54522EU RT NACELLE CORRODED A JRAAK NONE O OTHER ININSP/MAINT 1 GL11587CA43490 463 SURFACE CORROSION WAS FOUND ON THE RT IB SKIN PANEL AT APPROX STA 96.91. THIS CORRODION WAS NOTED UNDER THE INSULATION PANEL LOWER SIDE. REPLACEMENT OF SKIN PANEL IN PROGRESS. (K) 2L72 4T4 TRTA793 E5EU 20050727001592005072700159GL 2005 7 27 RAIA00507018 220050725A75328166061 BLEED VALVE EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL NR 2 ENGINE MALFUNCTIONED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03821HK16189 145068 NR 2 ENGINE N2 WOULD NOT GO ABOVE 26 PERCENT DURING START. NO ROTATION ON DRY MOTOR. MAINTENANCE REMOVED AND REPLACED THE CROSS BLEED VALVE. OPS CHECKED GOOD. 2L72 4F4 FRTT00011ATTE6CH 20050727001612005072700161SO 2005 7 27 RAIA00507017 120050725A3244 TIRE EMB 145 EMB145 3260210SO NLG CONTAMINATED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03804HK 145082 FLT #3622- PIT- AT GATE, PLANE WAS PARKED OR PUSHED THROUGH AREA OF RAMP THAT WAS RECENTLY PATCHED WITH TAR LEAVING A LARGE AMOUNT OF TAR ON THE TIRES. MAINTENANCE REMOVED AND REPLACED THE NOSE WHEEL TIRES. 2L72 4F RTT00011AT 20050727001622005072700162SO 2005 7 27 RAIA00507019 120050725A3244 TIRE EMB 145 EMB145LR 3260212SO NR 2 MAINS FAILED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03822HK 145069 NR 2 MAIN TIRE TREAD SHREDDED ON TAKEOFF. MAINTENANCE REMOVED AND REPLACED THE NR 2 MAINT TIRE. 2L72 4T RTT00011AT 20050727001632005072700163EU 2005 7 27 TXH2005F00000 120050619A5542SD3336321XB SKIN STBROSSD3 SD360 8100606EU PWA PT6 PT6A60A 52043NE RUDDER CRACKED E TXHAO OTHER O OTHER NRNOT REPORTED 1 WP13827BE SH3746 DEFECT WAS NOTED DURING INSPECTION OF HORIZONTAL AND VERTICAL STABILIZERS. SKIN AND RIB, TOP SIDE OF RUDDER BALANCE WEIGHT ATTACHMENT AND STRUCTURAL AREA CRACKED AND CORRODED. (WP13200509006) (K) 2H72 4T4 T A41EU E4EA 20050727001642005072700164WP 2005 7 27 MWEA050072 120050726A71605930645105 SUPPORT ANGLE DOUG DC9 DC981 3022081WP NOSE COWL CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 RIGHT ENGINE NOSE COWL SUPPORT ANGLE CRACKED, FORWARD OF CIRCULAR WEB. -- FABRICATED AND INSTALLED CUP AND INSTALLED NEW CLIP. 2L72 4F A6WE 20050727001652005072700165EU 2005 7 27 UPS05144961 120050712A5320A5341076522300 BRACKET AIRBUSA300 A300F4622R 3930360EU FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01121UP 0806 INSPECTION TYPE:5 YR AFT CARGO PIT, AFT BULKHEAD, UPPER LEFT ANGLE STRUCTURE IS CRACKED. REMOVED & REPLACED ANGLE BRACKET IAW A300-600 SRM 51-40-21. 2L72 4F RTA35EU 20050727001662005072700166EU 2005 7 27 UPS05144962 120050712A5320A5341076522200 BRACKET AIRBUSA300 A300F4622R 3930360EU FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01121UP 0806 INSPECTION TYPE: 5YR, AFT CARGO PIT, UPPER RIGHT ANGLE STRUCTURE IS CRACKED. REMOVED & REPLACED ANGLE BRACKET IAW A300-600 SRM 51-40-21. 2L72 4F RTA35EU 20050727001672005072700167EU 2005 7 27 UPS05144963 120050712A5320A5341076521700 BRACKET AIRBUSA300 A300F4622R 3930360EU FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01121UP 0806 INSPECTION TYPE: 5YR, AFT CARGO PIT, CENTER UPPER ANGLE STRUCTURE IS CRACKED. REMOVED & REPLACED ANGLE BRACKET IAW A300-600 SRM 51-40-21. 2L72 4F RTA35EU 20050727001692005072700169NM 2005 7 27 UPS05544959 120050726A2560 SMOKE GOGGLES BOEING757 75724APF 1384969NM COCKPIT DEFECTIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01456UP 25477 SMOKE GOGGLES ON CAPT'S SIDE ARE DEFECTIVE. REPLACED DAMAGED SMOKE GOGGLES W/ NEW IN REF TO MM CH 25-00. 2L72 4F RTA2NM 20050727001702005072700170NM 2005 7 27 UPS05544960 120050723A2560 SMOKE GOGGLES BOEING757 75724APF 1384969NM COCKPIT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01443UP 27388 COURIER SEAT HAS ONE SMOKE GOGGLE WITH CRACKED LENS R&R COURIER SEAT SMOKE GOGGLES 2L72 4F RTA2NM 20050727001712005072700171NM 2005 7 27 UPS05644976 120050726A3220 DOOR BOEING767 767300 1385204NM RT MLG OPEN A IPXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01334UP ATB - GEAR DOOR LIGHT AND MESSAGE ON TAKE OFF NO LIMITS EXCEEDED. UPON LANDING FOUND THE RIGHT GEAR DOOR DOWN. FOUND MANUAL RELEASE HANDLE TO NOT BE FULLY STOWED. STOWED HANDLE FULLY AND DOOR CLOSED. OPERATED GEAR DOOR MULTIPLE TIMES WITH DOOR LEVER SEATED. GEAR DOOR AND INDICATION OPERATED NORMALLY. WORK DONE PER MM 32-15-2. 2L72 4F RTA1NM 20050727001722005072700172WP 2005 7 27 UPS05844958 120050724A3350 BATTERY DOUG DC8 DC871F 302199DWP COCKPIT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01715UP 45915 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. R&R BATTERY AND RELAY UNIT W/REF TO MM 33-50-01-2. OPS CHECK GOOD. 2L74 4F RT4A25 20050727001732005072700173WP 2005 7 27 UPS05844965 120050716A53133646937U1 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE:C1 AFTER REMOVAL OF INTERCOSTAL ON N/R 858794 FS 1473 L34R FOUND CORROSION AT LONGERON UNDER STRAP REMOVED LONGERON 34R STA 1350 TO 1490 IAW DC8 SRM 53-2-2 FABRICATED AND INSTALLED LONGERON 34R AT STA 1350-1490 IAW DRWG 3646937 2L74 4F RT4A25 20050727001742005072700174WP 2005 7 27 UPS05844966 120050713A5340 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE:C1 SPLICE FITTING CRACKED AT STA 610, L35L REMOVED CRACKED SPLICE FITTING AT STA 610, LONG 35L IAW SRM 51-1-20D. FABRICATED REPLACEMENT FITTING AND INSTALLED FITTING IAW DRWG 3750330 2L74 4F RT4A25 20050727001752005072700175WP 2005 7 27 UPS05844967 120050707A5340 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE:C1 STA 675 L2L LONGERON SPLICE FITTING CRACKED REMOVED AND REPLACED SPLICE FITTING AT STA 675 L2L IAW SRM 51-1-20D AND 51-3-0 2L74 4F RT4A25 20050727001762005072700176NM 2005 7 27 DHL2005788005 120050726A3260656021132 ACCESSORY UNIT BOEING727 727214 138407RNM MLG FAILED A DHLAO OTHER P NO WARNING INDICATION APAPPROACH 1 SO01788AT 21958 BROUGHT THRUST LEVER BACK ON APPROACH NO RED RT GEAR LT. WITH GEAR SELECTED DOWN RED RT GEAR LT WOULD NOT ILLUMINATE OR PRESS TO TEST. R & R LANDING GEAR ACCESSORY UNIT IAW 727 MM CH 32-09-121 OPS CHECK GOOD 2L73 4F A3WE 20050727001772005072700177NM 2005 7 27 DHL2005754004 120050727A3350 LIGHT BOEING727 727223 1384074NM COCKPIT DISLODGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01754DH 22008 COCKPIT ENTRY EMERGENCY EXIT LIGHT ASSY FELL OUT ONTO FLOOR. REINSTALLED EXIT LIGHT ASSY BACK IN SOCKET IAW BMM 33-50-71OPS CHK'D GOOD. 2L73 4F A3WE 20050727001812005072700181WP 2005 7 27 UPS05844971 120050711A5320 FINGER DOUBLER DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE:C1 HEAVY CORROSION UNDER FINGER DOUBLER LT SIDE OF COCKPIT SUBFLOOR STA -12 TO -32 REMOVED DOUBLER AT STA -12 TO -32 IAW 53-02-03 FABRICATED 3 EA FILLERS, 1 EA DOUBLER, AND 1 EA FINGER DOUBLER AND INSTALLED IAW DWG SRO 8530026 SRM 51-1-20D, AND 51-2-1 2L74 4F RT4A25 20050727001842005072700184WP 2005 7 27 UPS05844974 120050705A5240 SKIN DOUG DC8 DC873F 302199FWP SERVICE DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C1, LT AFT SERVICE DOOR AFT UPPER CORNER HAS CRACK APPROX 3/8 EMITTING FROM FASTNER. REMOVED DAMAGED AREA IAW DC8 SRM 53-02-0 FABRICATED FILLER DOUBLER AND TRIPLER IAW DC8 SRM 53-02-0 FIG 18, AND SRM 53-04-00 INSTALLED FILLER DOUBLER AND TRIPLER AT LT AFT SERVICE DOOR AFT UPPER CORNER IAW SRM 53-02-0 FIG 18 2L74 4F RT4A25 20050728000032005072800003EA 2005 7 28 ASOA05556 120050625A2150GG670950091 ACM CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE LEFT SMOKE A ASOAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DEDESCENT 1 SO27702EV971 10035 DURING CRUISE, AT APPROXIMATELY 37,000 FT CREW RECEIVED A SMOKE AFT LAV WARNING WHICH EXTINGUISHED A FEW SECONDS LATER AND THEN RETURNED A FEW SECONDS AFTERWARDS. FA PERFORMED AN INSP OF THE AFT LAV AND DID NOT NOTE ANYTHING UNUSUAL. APPROX 5 MINUTES FOLLOWING WARNING MESSAGE, SMOKE OCCURRED IN COCKPIT. CREW DONNED OXYGEN MASK, COMPLIED WIHT QRH. EMERGENCY WAS DECLARED, AC DIVERTED. SMOLE LEVEL STABILIZED, BEGAN DISIPATING ENROUTE. AC LANDED SAFELY. MAINT REMOVED AND REPLACED LT AIR CYCLE MACHINE. DURING OPS CHECK, A BELLOWS WAS FOUND LEAKING. MAONT REMOVED AND REPLACED LT BELLOWS ON ACM. OPS CHECK GOOD. AC OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA EOOO63EN 20050728000112005072800011CE 2005 7 28 DXTA200500864 120050725A2741 WARNING LIGHT CESSNA750 750 2076810CE STAB TRIM ILLUMINATED E DXTAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL07939QS 7500193 PRIMARY STAB TRIM FAIL CAS MESSAGE. ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20050728000122005072800012CE 2005 7 28 DXTA200500866 120050726A5610 WINDSHIELD CESSNA750 750 2076810CE COCKPIT FAILED E DXTAA UNSCHED LANDING J WARNING INDICATION DEDESCENT 1 GL07936QS 7500036 DESCENDING THROUGH APPROXIMATELY 37000 FT WINDSHIELD HEAT INOP RT CAS MESSAGE ILLUMINATED SHORTLY AFTERWARDS A LAMINATE LAYER OF THE RIGHT WINDSHIELD SHATTERED. ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20050728000142005072800014NE 2005 7 28 TSAA0575031 220050720A75321058V04002 BLEED VALVE BOEING737 7372Y5 1384554NM PWA JT8 JT8D9A 52048NE NR 2 ENGINE DEFECTIVE A TSAAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 WP13810AL 24031 ON TAKE-OFF NR 2 ENGINE COMPRESSOR STALL ON INITIAL RUN-UP FROM IDLE. R & R NR 2 ENG PRBC IAW MM 75-31-11. BLEED VALVE SCHEDULING COMPLETED PER P&W MM 72-00-00. R.I.I. COMPLETED FOR NR 2 ENG PRBC VALVE CHANGE IAW MM 75-31-11. DID NOT FIX OFF IDLE STALL. LUBRICATED 8TH & 13TH STAGE BLEED VALVES ON NR 2 ENG PER 75-30-00. R&R START BLEED CONTROL VALVE OPERATIONAL CHECK NORMAL. BLEED VALVE SCHEDULING COMPLETED OK PER PWA MM 72-00-00. R & R NR 2 ENG PRBC FOR PRECAUTIONARY IAW MM 75-31-11. BLEED VALVE SCHEDULING COMPLETED, OPS & LEAK CHECK OK. RII COMPLETED FOR PRBC CHECK. NO FAULTS NOTED. AIRCRAFT RETUNED TO SERVICE. 2L72 4U4 FRTA16WE E2EA 20050728000172005072800017NM 2005 7 28 QXEA200501136 120050726A2923 SWITCH DHAV DHC8 DHC8202 2809007NM NR 2 STNDBY PUMPMALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09369PH 513 NR 2 STANDBY PUMP HOT CAUTION LIGHT ILLUMINATED AFTER STANDBY HYDRAULIC PRESSURE WAS SELECTED "NORM" AFTER TAKEOFF. MASTER CAUTION UNABLE TO RESET WHEN CAUTION LIGHT WAS ILLUMINATED. CAUTION LIGHT DARK IN CRUISE AND RE-ILLUMINATED INTERMITTENTLY ON APPROACH AFTER FLAP ACTIVATION. COMPLIED WITH E/A CHECKLIST. MAINTENANCE SWITCHED NR 2 STANDBY HYDRAULIC PUMP OVER TEMP SWITCH TO ITS SECONDARY SWITCH IAW -8(200) AMM 29-11-17, PAGE 1, GROUND RAN AIRCRAFT. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050728000182005072800018NM 2005 7 28 AWXA200500850 120050725A3040 WIRE BOEING737 7374Y0 1384705NM HEAT CONTROLLER FAILED A AWXAO OTHER O OTHER TXTAXI/GRND HDL 1 WP28323AW278916537 23684 PHX - SMOKE - FLT 0075 - PILOT REPORTED ON GROUND THAT THE A1 CB POPPING AND WONT RESET. MAINTENANCE REMOVED AND REPLACED THE PITOT STATIC WINDOW HEAT MODULE ON P5. ALSO, SEVERAL WIRES WERE BURNED IN THAT VICINITY. REMOVED AND REPLACED WIRES ON WINDOW HEAT CONTROLLER PANEL IAW BOEING 737-300 AMM 30-41-00-5. OPERATIONAL CHECKS GOOD. VENDOR COULD NOT VERIFY FAULT DUE TO ARCING FROM AN EXTERNAL SOURCE WHICH BURNED A HOLE IN THE RIGHT REAR VERTICAL EDGE OF COVER. THREE LAMPS WERE FOUND DIM AND THE TOGGLE SWITCH, S7, CAP CUSHION WAS MISSING. THE UNIT WAS INSPECTED, REPAIRED AND TESTED IAW OHM 30-01-06 REV.11. 2L72 4F RTA16WE 20050728000192005072800019EU 2005 7 28 AWXA200500851 120050726A3350321454 POWER SUPPLY AIRBUS320 A320232 3930326EU EMERGENCY LIGHT MALFUNCTIONED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28605AW 543 SNA - EEL - DURING OPERATIONAL TEST OF OVERWING "SLIDE ARMED" LIGHTS THE AFT LEFT WING EXIT LIGHT IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT LEFT EPSU IAW AWA TASKCARD R1C33303. OPERATIONAL CHECKS GOOD. 2L72 4F RTA28NM 20050728000222005072800022NM 2005 7 28 TSAA0534030 120050722A3411 PITOT HEAD BOEING737 73776N 13844CHNM CAPTAINS SIDE OBSTRUCTED A TSAAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 WP13742AL 30830 ETOPS FLT 441 (LAS) CAPTAIN AND FIRST OFFICER’S AIRSPEED DISAGREE; ABORTED TAKEOFF. FOUND DEBRIS IN CAPTAIN SIDE PITOT TUBE. CLEANED DEBRIS FROM PITOT; OPERATIONS CHECKED PITOT TUBES AND RETURN TO SERVICE. 2L72 4F RTA16WE 20050728000272005072800027CE 2005 7 28 39TW070405JC 120050704A3260 WARNING LIGHT LEAR 35 31A 5170531CE GARRTTTFE731TFE731* 01518WP MLG FALSE ACTIVATIONE AOQAO OTHER O OTHER NRNOT REPORTED 1 EA1139TW 047 NR 2 MAIN GEAR UNSAFE LIGHTS DID NOT EXTINGUISH DEPARTING. PREVIOUS GEAR CYCLES WERE UNEVENTFUL. LAST GEAR CYCLE INTO ISP WAS NORMAL. JACKED AIRCRAFT, INSPECTED MAIN LANDING GEAR ASSEMBLIES, UPLOCK AND DOWNLOCK SWITCHES AND DOOR SWITCHES AND MECHANISMS, FOUND NO FAULTS. LUBRICATED MAIN GEAR ASSEMBLIES. ACCOMPLISHED 20 PLUS GEAR SWINGS AND PERFORMED SATISFACTORY OPERATIONAL CHECKS. (EA11200504903) (K) 2L72 4F4 FRTA10CE E6WE 20050726000902005072600090NM 2005 7 26 UPS05544955 120050724A2560 SMOKE GOGGLES BOEING757 75724APF 1384969NM COCKPIT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01458UP 25479 SUPERNUMERARY SMOKE GOGGLES LENS CRACKED. REPLACED WITH SERVICEABLE SMOKE GOGGLES. 2L72 4F RTA2NM 20050726000982005072600098NM 2005 7 26 GTIA050176 120050504A5330 SKIN DOUG MD80 MD83 3023681NM FUSELAGE DENTED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23827NK 49793 FOUND DENT AT STATION 228.5 BETWEEN LONGERON 17R AND 18R. STRIPPED AREA. CUTOUT DAMAGED SECTION. FABRICATED -5 DOUBLER. FABRICATED -0 FINGER DOUBLER. FABRICATED -15 NEW SECTION OF SKIN. TREATED AND PRIMED -5, -9, -15 REPAIR PARTS. FABRICATED TWO -3 STRAPS. FABRICATED -7 STRAP. TREATED 7 PRIMED -3 AND -7 REPAIR PARTS. INSTALLED REPAIR PARTS. PAINT DONE. (M) 2L72 4F RT 20050726001032005072600103 2005 7 26 YENA200541 420050720A23303042865102 ELECTRICAL BOX AIRBUS320 A320232 3930326EU CABIN ODOR A YENAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA15536JB105227416 1784 BURNING ODOR FROM OVERHEAD AT A/C RIGHT ROW 19 RUBBER TYPE OF SMELL. ACCOMPLISHED INFO NOTICE 2004-T023TR. NO ABNORMALITIES FOUND. REPLACED SEB AT SUSPECT ROW 19DEF PER INFO NOTICE IAW 23-39-00. LIVE TV SYSTEM OPERATION CHECKED NORMAL. 2L72 4F RTA28NM 20050726001072005072600107EA 2005 7 26 SWIA200515303 120050721A5610 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAO OTHER O OTHER DEDESCENT 1 NM07590SW 7077 DESCENDING THROUGH APPROX 27000' HEARD A LOUD POP. REPLACED RIGHT WINDSHIELD IAW CRJ 200 MM 56-11-01, PN/OFF 601R33033-2 , SN/OFF 951038635T. 2L72 4F RTA21EA 20050726001162005072600116NM 2005 7 26 GTIA050155 120050516A2421 STATOR AIRBUSA319 A319132 3930340NM ALTERNATOR FAILED A GTIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL23501NK 2424 UPON ENGINE START A31 ENGINE HAD `ENGINE 1 OVSP PROT FAULT` WARNING MESSAGE, AIRCRAFT TAIL SWAP WITH 810. REMOVED AND REPLACED NR 1 ENGINE ALTERNATOR STATOR. OPS CHECK GOOD. CHECKED WIRING, ALL CHECKED GOOD. (M) 2L72 4F RTA28NM 20050726001242005072600124EU 2005 7 26 MALA050581 120050718A7500 BLEED BAND BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071H 41580NE NR 3 ENGINE FAILED A MALAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 GL15512XJ E2326 ON DEPARTURE NR 3 ENGINE TEMP OUT AT 649 DEG APPROXIMATE TURNED AUT THROTTLE OFF AND BROUGHT EGT BACK TO 613 DEG. N2 WAS HIGHER THAN OTHER 3 ENG. N1 WAS LOWER THAN OTHER 3 ENG. TURNING FADEC OFF DID NOT CHANGE SITUATION. RETURNED TO MSP. DOWNLOADED FDR, BOROSCOPED NR 3 ENGINE, REPLACED NR 3 ENGINE BLEED BAND AND PERFORMED TAKEOFF POWER ASSURANCE CHECK. ALL CHECKS GOOD. REF. 409 CARD 274727 FOR DETAILS. 2H74 4F4 FRTA49EU E6NE 20050726001252005072600125EU 2005 7 26 MALA050586 120050720A2920 O-RING BAC 146 AVRO146RJ85A1500097EU HYD SYSTEM LEAKING A MALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL15518XJ E2337 IN CRUISE AT 30K THE GREEN HYD SYSTEM LOST QUANTITY. TURNED OFF GREEN SYSTEM AND DID AN EMERGENCY GEAR EXTENSION. STOPPED OFF RUNWAY AND WAS TOWED TO THE GATE. FOUND O-RING ON PTU PRESSURE MANIFOLD NO RETURN VALVE LEAKING. REMOVED AND REPLACED O-RING. ALL CHECKS GOOD 2H74 4F RTA49EU 20050726001322005072600132EU 2005 7 26 MALA050591 120050720A5321 FLOOR PANEL SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15437XJ 340B437 DURING 4Y/2Y CHECK IN BNA FOUND FLOOR FLANGE AT FS272 IS CORRODED AND HAS BEEN REPAIRED IAW MESABA EO#S53102. REF: EAMS WORK ORDER 212613 TASK 2517 2L72 4T RTA52EU 20050726001342005072600134EU 2005 7 26 MALA050592 120050721A5753 ACCESS PANEL SAAB SF340 340B 7860101EU RT TE FLAP CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15437XJ 340B437 DURING 4Y/2Y CHECK FOUND RT FLAP ACCESS PANEL 641AT IS CHAFED OUT OF LIMITS ON THE INBOARD END AND HAS BEEN REPAIRED IAW MESABA EO#S57094 REF: EAMS WORK ORDER 612613 TASK 6507 2L72 4T RTA52EU 20050726001402005072600140EU 2005 7 26 MALA050583 120050715A2750 COMPUTER BAC 146 AVRO146RJ85A1500097EU FLAP SYSTEM FAILED A MALAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL15520XJ 143592 E2345 AFTER TAKEOFF FLAP STUCK AT 18 WITH FLAP INOP AND FLAP FAULT. REMOVED AND REPLACED COMPUTER PN 676801007 SN OFF UEL/DRG/1435-92, SN ON UEL/DEG/1121-85 IAW AMM 2750-17. OPS CHECK GOOD. 2H74 4F RTA49EU 20050726001512005072600151NM 2005 7 26 USAA050768 120050616A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19354US49460 23557 CLT - FOUND SKIN CRACKED 4 INCHES, STATION 727D, S23R. INSTALLED DOUBLER IAW SRM 53-00-01, FIG 229 DETAIL XI. (M) 2L72 4F RTA16WE 20050726001522005072600152EA 2005 7 26 A6WA200540220 120050624A2121 DUCT CNDAIRCL600 CL6002B19 1900309EA CABIN FAN CLOGGED A A6WAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL31454AW 7842 ELECTRIC SMELL IN CABIN FROM ROW 9 AFT. FOUND CABIN FAN DUCT CLOGGED WITH DUST AND DEBRIS. CLEANED FAN AND DUCT ABOVE ROW 8. OPS CHECK GOOD. ALSO, FOUND BALLAST B130 ABOVE ROW 11 GROUND PIN IN CONNECTOR NOT SEATED CAUSING BALLAST INTERMITTENTLY FLICKERING. RESEATED PER PIN IAW STANDARD PRACTICES, OPS CHECK GOOD. (M) 2L72 4F RTA21EA 20050726001712005072600171NM 2005 7 26 05FDEA02021 120050722A5310 DOOR FRAME BOEING727 727200 138407ENM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 FWD ENTRY DOOR, UPPER FRAME UPPER SURFACE IS GOUGED WHERE 3 BRACKETS WERE IMPROPERLY REMOVED AND REMAINS OF BRACKETS ARE STILL UNDER HILOCK HEADS. REMOVED AND REPLACED UPPER FRAME PER SRM 51-30-2. 2L73 4F RTA3WE 20050726001742005072600174NM 2005 7 26 05FDEA02024 120050722A3411 STATIC PORT DOUG MD11 MD11 3023602NM FUSELAGE FAILED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 FUSELAGE INTERIOR, LT PRIMARY STATIC PORT FAILED WAVINESS TEST. REMOVED AND REPLACED AS PER AMM 34-11-03-4. 2L73 4F RTA22WE 20050726002052005072600205NM 2005 7 26 USAA050772 120050616A5320 ANGLE BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU 23861 CLT - FOUND TRANSITIONAL ANGLE CORRODED 2 SQUARE INCHES, UNDERSIDE OF NUTPLATE OF RIGHT TRANSITION ANGLE AT DOOR FRAME BS 496. REMOVED DAMAGE, FABRICATED REPAIR AND REPLACEMENT PART INSTALLED IAW 737 SRM 51-10-02. (M) 2L72 4F RTA16WE 20050726002072005072600207CE 2005 7 26 71931 120050725A5210 ROLLER BEECH 1900 1900D 1154162CE PAX DOOR OBSTRUCTED A AMWAO OTHER C F.O.D. LDLANDING 1 CE07162ZV UE162 AFTER LANDING IN DUBOIS, PA ON REPOSITIONING FLIGHT 9415, THE PASSENGER DOOR FAILED TO OPEN DUE TO THE DOOR TRIM STUCK IN CAM ROLLER ON DOOR FRAME. THE CORRECTIVE ACTION WAS AS FOLLOWED: MAINTENANCE REINSTALLED THE TRIM. THEREFORE NO PARTS WERE USED. 2L72 4T RTA24CE 20050726002082005072600208EU 2005 7 26 05FDEA02038 120050724A5321 FLOOR PANEL AIRBUS300 A300F4605R 3930327EU FUSELAGE CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25671FE 778 MAIN CARGO FLOOR PANEL 251AH IS CRACKED AT TRACK MAIN ATTACH POINT. REPLACED FLR PNL ON TRAVELER NR T5/530786 REF SRZ-25-005. 2L72 4F RTA35EU 20050726002102005072600210EU 2005 7 26 05FDEA02044 120050724A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU ZONE 200 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25671FE 778 SEAT TRACK BL 0 FROM FRAME STA 45 TO 53 CORRODED IN SEVERAL AREAS. REMOVED DAMAGED SEAT TRACK SECTION, FABRICATED DRILLED AND DEBURRED HOLES IN SEAT TRACK REPLACEMENT AND SPLICE SET. TREATED AND PRIMED ALL PARTS IAW SRM 51-23-10. INSTALLED NEW SEAT TRACK SECTON AND SPLICE SET IAW SRM 53-10-16. 2L72 4F RTA35EU 20050726002132005072600213EU 2005 7 26 05FDEA02041 120050724A5320 FLOOR SUPPORT AIRBUS300 A300F4605R 3930327EU ZONE 200 BROKEN A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25671FE 778 MAIN CARGO DECK BETWEEN FS 13 TO FS 13B RBL 26 FLOOR SUPPORT DAMAGED (BROKEN). REMOVED DAMAGED FLOOR SUPPORT IAW SRM 51-40-20. RECEIVED NEW SUPPORT FROM FAB SHOP AND TRAVELER NR T5/534444 REF SRM 51-26-10 SRM 53-12-15 FIG 19 LOCATED AND DRILLED SUPPORT (NEW) IAW SRM 51-40-44. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-40- 20. TOUCHED UP PAINT COATING ON SUPPORT AND FASTENERS IAW SRM 51-23-10. 2L72 4F RTA35EU 20050726002162005072600216EA 2005 7 26 CVU2005F00001 220050715A8520 CAMSHAFT BEECH 80 65B80 1152812CE LYC O720 IO720A1B 41546EA ENGINE WORN E CVUAO OTHER O OTHER NRNOT REPORTED 1 WP1344MA 720 LD412 SMALL METAL FLAKES KEPT RE-APPEARING IN THE OIL SCREENS. FOUND WORN CAM NR 5 AND NR 6 CYLINDER INTAKE VALVES. ENGINES REMOVED FOR REPAIR. USE MFG ENGINE OIL ADDITIVE FROM TIME OF OVERHAUL. RUN ENGINES FREQUENTLY. (K) 1L72 3O3 O 3A20 1E15 20050726002182005072600218NM 2005 7 26 USAA050785 120050623A5740 ATTACH ANGLE BOEING737 737401 1384701NM WING CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19421US 23988 CLT - FOUND ATTACH ANGLE CRACKED .75 INCH, WING STATION 60.9735. FABRICATED AND INSTALLED A NEW ANGLE IAW BOEING DRAWING 65-50820-362 AND SRM 51-40-02. (M) 2L72 4F RTA16WE 20050726002432005072600243WP 2005 7 26 05FDEA02045 120050722A3230 LANDING GEAR DOUG MD10 MD1010F 3022112WP MALFUNCTIONED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25388FE 46622 AFTER T/O RW 22L JFK. LT MAIN GEAR FAILED TO RETRACT. INDICATIONS WRE LEFT UNSAFE LIGHT AND A RED DOT LEFT GEAR ON CONFIG PAGE. ALSO NOTICED YAW WITH 1GEAR STILL DOWN. R & R LT TRIM CYLINDER PER MM 32-37-01-2. REMOVED AND REPLACED NR 2 SYS BRAKE LINES ON NR 5 & 6 BRAKES. BLEED BRAKES AS PER M.M. 32-43-01-3. REPLACED ALL BROKEN SUPPORTS, AND CLAMPS SUPPORTING HYD LINES USING STANDARD MAINT PRACTICES. LEAK CHECK OK OF HYD LINES AND BRAKES. BLED BOGIE TRIM CYCLINDER. LEAK CHECKS NORMAL. A/C JACKED PER MM 07-11-00-2. PERFORMED GEAR SWING SWING PER MM 32-30-00-5. OPS CK'S OK.GEAR INDICATION CK'S OK PER MM 32-60-00-5. 2L73 4F RTA22WE 20050726002442005072600244EU 2005 7 26 2005UALA00679 120050720A5313 STRINGER AIRBUS320 A320232 3930326EU FUSLEAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29418UA 485 STRINGER 42L HAS CORROSION BETWEEN FRAME 57 AND 58. REPLACEMENT OF STRINGER (PSE) ACCOMPLISHED. 2L72 4F RTA28NM 20050726002462005072600246NM 2005 7 26 2005UALA00681 120050719A5330 SKIN BOEING737 737522 138449FNM FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29914UA 25381 EXTERNAL FUSELAGE SKIN HAS DENT AT STA 897 STR 19L. MAJOR REPAIR ACP'D PER SRM 53-00-01 FIG 229. TRIPLER INSTALLED APPROX 12 X 11. 2L72 4F RTA16WE 20050726002472005072600247NM 2005 7 26 2005UALA00682 120050719A5330 SKIN BOEING737 737522 138449FNM FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29914UA 25381 FUSELAGE SKIN HAS DENT AT STATION 855 BELOW STR 20L SKIN LAP. MAJOR REPAIR ACP'D PER SRM 53-00-01 FIG 229 TRIPLER INSTALLED 14 X 16. 2L72 4F RTA16WE 20050726002492005072600249EU 2005 7 26 2005UALA00684 120050719A3350321454 BATTERY PACK AIRBUS320 A320232 3930326EU EMERGENCY LIGHT FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29402UA 439 EMERGENCY LIGHTS BITE TEST FAILS "BATT FWD L". REPLACED FWD LT EMERGENCY BATTERY PACK. 2L72 4F RTA28NM 20050726002502005072600250 2005 7 26 2005UALA00685 420050720A2565 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE L5 SLIDE INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29122UA 29168 L5 DOOR SLIDE LIGHT INOP. REPLACED LAMP. 2L74 4F4 FRTA20WE E24NE 20050726002522005072600252NM 2005 7 26 2005UALA00687 120050720A5330 SKIN BOEING737 737522 138449FNM FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29914UA 25381 EXTERIOR FUSELAGE SKIN DENTED AT STA 378-380 BTWN STR 17L & 18L, AND STA 376 BTWN STR 16L & 17L ALSO HAS A DENT. MAJOR REPAIR ACP'D PER SRM 53-00-01 TO BOTH DENT AREAS. TRIPLER REPAIR SCHEME USED PER FIG 101 APPROX SIZE 13"X20" 2L72 4F RTA16WE 20050726002532005072600253NM 2005 7 26 2005UALA00688 120050720A5311 FRAME BOEING737 737522 138449FNM FUSELAGE GOUGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29912UA 25290 STA 211 FRAME IS GOUGED APPROXIMATELY 6 FEET ABOVE STRINGER 17R. REPAIRED WEB WITH DOUBLER PER SRM 51-70-13 FIG 1 DETAIL 1 2L72 4F RTA16WE 20050726002552005072600255NM 2005 7 26 05FDEA02046 120050724A5210 SKIN DOUG MD11 MD11 3023602NM ZONE 200 CHIPPED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 FORWARD CABIN - R1 DOOR EXTERIOR UPPER EDGE FOUND CHIPPED. CORRECTIVE ACTION: SNRM N0241: EXISTING REPAIR ON FWD CABIN - R1 DOOR EXTERIOR EVALUATED AND FOUND NOT IAW SRM 52-10-00, FIG.4, SHT 1, VOL. I CHIPPED EXISTING REPAIR DOUBLER REMOVED AS PER SRM 51-35-01 VOL. II AND NEW REPAIR CARRIED OUT AS PER SRM 52-10-00, FIG. 4, SHT 1, VOL. I. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050726002562005072600256NM 2005 7 26 05FDEA02047 120050724A5311 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 MAIN DECK CARGO - LEFT HAND FRAME FOUND DENTED MARK AT STATION 1701 LONGERON 12. CORRECTIVE ACTION: SNRM N0599: MAIN DECK CARGO - LH FRAME AT STA 1701 LONGERON 12 CARRIED OUT REPAIR AS PER SRM 53-30-00 VOL. I. REFER TO FEDEX EA 1-5330-87565 - FUSELAGE - FRAME - TRACKING SRM FRAME REPAIR AT STA Y = 1701 AT LONGERON 12 LEFT HAND FOR REPETITIVE INSPECTION TRACKING. 2L73 4F RTA22WE 20050726002582005072600258NM 2005 7 26 05FDEA02049 120050724A5730 SKIN DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 LT WING UPPER SURFACE FORWARD OF FUEL TANK PANEL 533AT 1 EACH SKIN BULGE FOUND AS MARKED. CORROSION ON LTW UPPER SURFACE FWD OF FUEL TANK PANEL 533AT REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL THICKNESS: 0.749"; THK. REMOVED: 0.033"; THK. REMAINED: 0.716". AREA FOUND WITHIN LIMIT AS PER FEDEX 1-5730-89960 (TITLE: WINGS - LT WING UPPER SKIN BLEND AT XORS 281, STRINGER 9). THIS REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2- 100. 2L73 4F RTA22WE 20050726002592005072600259NM 2005 7 26 05FDEA02050 120050724A5730 SKIN DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 RIGHT HAND WING UPPER SURFACE TRAILING EDGE FORWARD OF OUTBOARD AILERON SEVERAL SKIN BULGE FOUND AS MARKED. CORROSION REMOVED AND FOUND WITHIN LIMIT - REFER TO SNRM N1244, N1245, N1246 AND N1247 FOR WORK DETAILS AND 03 EA AREA CORROSION REMOVED AND FOUND EXCEED LIMIT REFER TO SNRM 1241, N1242 AND N1243 FOR WORK DETAILS. 2L73 4F RTA22WE 20050726003002005072600300NM 2005 7 26 05FDEA02079 120050725A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE RT NR 28 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. [CLOSED] 2L73 4F RTA22WE 20050726003022005072600302NM 2005 7 26 05FDEA02081 120050725A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE LT NR 36 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA1-5510-87597. [CLOSED] 2L73 4F RTA22WE 20050727000062005072700006NM 2005 7 27 USAA050830 120050705A5320 SPLICE BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19441US40664 24812 FOUND SPLICE CRACKED .5 INCH, BS 907, STRINGER S4R. REPLACED SPLICE WITH NEW PART IAW SRM 51-10-02. (M) 2L72 4F RTA16WE 20050727000152005072700015EU 2005 7 27 KBM2005F00158 120050720A21500500521 MOTOR SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE EVAPORATOR INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH3143 2337 FWD EVAPORATOR MOTOR, UNIT DOES NOT BLOW ANY AIR. REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20050727000192005072700019EU 2005 7 27 KBM2005F00166 120050714A21210500847 BLOWER SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE CABIN AIR INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P265 2347 7 INCH BLOWER, A/C BLOWS WARM AIR. REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20050727000242005072700024EA 2005 7 27 ASOA05547 120050622A5347601R3103215 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27851AS 7360 DURING A C-CHECK, THE SEAT RAIL FLOOR AT FS 379, LBL 9 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE SEAT RAIL FLOOR AT FS 379, LBL 9. (K) 2L72 4F4 FRTA21EA E15NE 20050727000322005072700032WP 2005 7 27 DHL2005802527 120050715A57203704841501 FITTING DOUG DC8 DC873 302199CWP NR 2 TANK CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH84803 46076 NR 2 MAIN TANK INTERIOR LOWER SECTION INBD FWD FITTING CRACK, STA XRS 74.869 S-61 (MAJOR REPAIR). CORR.: PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG.1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG. 21. CLEANED AND APPLIED TOP COATING MATERIAL TO AREA IAW SRM 51-1-12 PG. 7. APPLIED SEALANT TO FAYING SURFACE IAW SRM 51-1-12. INSTALLED NEW FITTING IAW SRM 51-1-20D PG. 9, SRM 51-1-23 (PL1 WASHER) TORQUED IAW SRM 51-3-1. REFER TO NR 030838 FOR LEAK CHECK. 2L74 4F RT4A25 20050727000332005072700033WP 2005 7 27 DHL2005802530 120050715A572037048411 FITTING DOUG DC8 DC873 302199CWP NR 2 TANK CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH84803 46076 NR 2 MAIN TANK INTERIOR LWR SECTION OUTBD AFT FITTING CRACKED STA XRS 74.869 S-61 (MAJOR REPAIR). CORR.: PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG.1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG. 21. CLEANED AND APPLIED TOP COATING MATERIAL TO AREA IAW SRM 51-1-12 PG. 7. APPLIED SEALANT TO FAYING SURFACE IAW SRM 51-1-12. INSTALLED NEW FITTING IAW SRM 51-1-20D PG. 9, SRM 51-1-23 (PLI WASHER). TORQUED IAW SRM 51-3-1. REFER TO NR 030838 FOR LEAK CHECK. 2L74 4F RT4A25 20050727000342005072700034WP 2005 7 27 DHL2005802531 120050713A5313S1616757 LONGERON DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH84803 46076 FUSELAGE TAIL SECTION L-17L CRACKED 2.000 (STA 1766.000-1786.000) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG.1, SRM 53-5-3 PG. 16 FIG. 5. REMOVED CRACKED LONGERON IAW SRM 51-1-21 PG. 1, SRM 51-1-20D PG. 21. FABRICATED NEW LONGERON P/N S1616757 IAW SRM 53-5-3 PG. 16 FIG. 15, SRM 51-2-6 FIG. 50. HEAT TREATED NEW LONGERON IAW SRM 51-1-1 PG. 1-13-17. PERFORMED NDT INSP IAW NDT SPM PART 08-00-02 TO07. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG. 9. INSTALLED NEW LONGERON IAW SRM 51-1-20D PG. 9. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050727000352005072700035WP 2005 7 27 DHL2005802532 120050715A5330 DOUBLER DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH84803 46076 EXTERIOR FUSELAGE NOSE SECTION STRUCTURAL MODIFICATION DOUBLER (ACS) CRACKED 0.750 AT AFT LWR CORNER OF RT PRIMARY HEAT EXCHANGER STA -12.000 L-27R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 07-13-05, DWG Z20-R01 REV. IR DATED 06-24-05. REMOVED FASTENERS IAW SRM 51-1-21 PG. 1, SRM 51-1-20D PG. 21. CUT OUT DAMAGED SECTION IAW DWG Z20-R01. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER REPAIR TRIPLER AND 2 EA FILLERS IAW DWG Z20-R01. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG. 9. INSTALLED REPAIR PARTS IAW DWG Z20-R01, SRM 51-1-21 PG.1, SRM 51-1-20D PG. 9, SRM 51-3-0 PG.1, SRM 51-32L74 4F RT4A25 20050727000392005072700039WP 2005 7 27 DHL2005802535 120050718A5330 DOUBLER DOUG DC8 DC873 302199CWP FUSELAGE BROKEN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH84803 46076 EXTERIOR FUSELAGE NR 2 ACCESS DOOR INTERNAL DOUBLER BROKEN STA -165.000 TO -156.000 MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 07-15-05 DWG Z20-R15 REV IR DATED 06-24-05. REMOVED INTERNAL REPAIR DOUBLER AND EXTERNAL PLATING IAW SRM 51-1-21 PG.1. PERFORMED DETAIL VISUAL INSP. NO CRACK OR CORROSION FOUND. FABRICATED EXTERNAL DOUBLER FILLER AND 3 EA STIFFENERS AND INTERNAL STIFFENER PLATE IAW DWG Z20-R15. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG. 9. INSTALLED REPAIR PARTS IAW DWG Z20-R15 SRM 51-1-21 PG.1. 2L74 4F RT4A25 20050727000502005072700050WP 2005 7 27 DHL2005802503 120050628A2750 DRIVE LINK DOUG DC8 DC873 302199CWP TE FLAPS CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH84803 46076 RT OUTBD FLAP DRIVE LINK ASSY CRACKED 0.500 INCH LENGTH AT POINT J STA XF 219.498. REMOVED AND REPLACED RH OUTBD FLAP DRIVE LINK ASSY AT STA XF 219.498 IAW MM 27-51-4 PG. 201-204. REFER TO NR 030703 FOR OPS CHECK. 2L74 4F RT4A25 20050727000622005072700062WP 2005 7 27 DHL2005802509 120050712A5320 ANGLE DOUG DC8 DC873 302199CWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH84803 46076 MAIN CARGO COMPT. PNEU. DUCT COVER SUPPORT ANGLE CORRODED STA 8.000 - 17.000, RBL 59. REMOVED CORROSION FRON SUPPORT ANGLE IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-3 PG. 2P. FABRICATED NEW SUPPORT ANGLE IAW SRM 53-2-0 PG.1. CLEANED, TREATED AND PRIMED AREA AND SUPPORT ANGLE IAW SRM 51-1-8B. INSTALLED SUPPORT ANGLE IAW SRM 51-1-21 PG.1. 2L74 4F RT4A25 20050727000662005072700066WP 2005 7 27 DHL2005802515 120050706A5313 LONGERON DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH84803 46076 FWD CARGO COMPT. CROSS SLIDE DOOR AREA L-35L CRACKED 1.000 STA 300.000-310.000 MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG. 1B. REMOVED FASTENERS IAW SRM 51-1-20D PG. 21. PERFORMED STOP HOLE IAW SRM 53-2-0 FIG. 1B SHEET 3. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED ANGLE DOUBLER IAW SRM 53-2-0 FIG. 1B SHEET 3, SRM 53-4-1 FIG. 28. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG. 9. INSTALLED ANGLE DOUBLER IAW SRM 53-2-0 FIG. 1B SHEET 3, SRM 51-1-220D PG. 9. TORQUED IAW SRM 51-3-1 PG. 2A. 2L74 4F RT4A25 20050727000702005072700070WP 2005 7 27 DHL2005802525 120050715A5330 SKIN DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SO01802DH84803 46076 FUSELAGE EXTERNAL SKIN AFT OF HOLD OPEN HOOK PIN CRACKED 0.375 STA 1610.000 L-14L TO L-15L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 07-11-05, DWG Z20-R04 REV IR DATED 06-24-05. REMOVED FASTENERS IAW SRM 51-1-21 PG. 1, SRM 51-1-20D PG. 21. CUT OUT DAMAGED SECTION IAW DWG Z20-R04. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED TRIPLER DOUBLER AND FILLER AND FINGER DOUBLER IAW DWG Z20-R04. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG. 9. INSTALLED REPAIR PARTS IAW DWG Z20-R04, SRM 51-3-0 PG.1, SRM 51-1-21 PG 1, SRM 51-1-20D PG. 9, SRM 51-3-1 PG. 2A (TORQUED) 2L74 4F RT4A25 20050727000712005072700071EA 2005 7 27 ASOA05551 120050623A5210601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27865AS 7507 DURING AN A-CHECK, THE PASSENGER DOOR BOTTOM STEP WAS FOUND BROKEN AT THE ATTACH LINK. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPS CHECK GOOD. (K) 2L72 4F4 FRTA21EA E15NE 20050727000762005072700076NM 2005 7 27 QXEA200501134 120050724A2910 HYDRAULIC SYSTEM DHAV DHC8 DHC8202 2809007NM NR 2 MALFUNCTIONED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09347PH 480 SEA FLIGHT NR 2203 - RIGHT OUTBOARD SPOILER DOES NOT INDICATE DEFLECTION ON PFCS, APPEARS TO DEFLECT NORMALLY FROM COCKPIT. MAINTENANCE BLED NR 2 HYDRAULIC SYSTEM IAW 29-00-00-870-805. PERFORMED OPERATIONAL TEST OF ROLL SPOILER CONTROL SYSTEM IAW -8(200) AMM 27-14-00-710-801. NO DEFECTS NOTED. ALL SPOILERS INDICATIONS NORMAL AND DEFLECTION OKAY. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050727000882005072700088WP 2005 7 27 DHL2005802505 120050630A5730 DOUBLER DOUG DC8 DC873 302199CWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH84803 46076 RT OUTER WING INBD L/E LWR DOUBLER CRACKED 0.250. REMOVED CRACKED DOUBLER IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. FABRICATED DOUBLER (AL7075T6 0.050) IAW SRM 57-3-3. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050727000912005072700091NM 2005 7 27 USAA050826 120050705A5320 ANGLE BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19441US 24812 CLT - FOUND ANGLE CRACKED .750 INCH, STATION 616 LT SIDE BODY WING TERMINAL FORGING ANGLE, CRACKED ON FORWARD SIDE. REMOVED DAMAGE AND INSTALLED REPAIR ANGLES IAW RT 53-62-01. (M) 2L72 4F RTA16WE 20050727000982005072700098SO 2005 7 27 C2XA05IA081 120050616A3350RPS1B POWER SUPPLY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712569 145630 MCI - DURING MAINTENANCE INSPECTION, THE MAINTENANCE DISCOVERED THAT THE EMEGENCY EXIT SIGN ON THE AFT WALL OF THE GALLEY WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO EMERGENCY LIGHT POWER SUPPLY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (THIS PART IS NOT TRACKED BY SERIAL NUMBER AND NO TIMES ARE AVAILABLE) 2L72 4T RTT00011AT 20050727001002005072700100SO 2005 7 27 C2XA05SH081 120050721A533014520551001 SKIN PANEL EMB 145 EMB145EP 3260221SO FUSELAGE LIGHTNING STRIKEA C2XAK NONE O OTHER ININSP/MAINT 1 SW2714943 145040 SHV-DURING C-CHECK MAINTENANCE FOUND LIGHTNING STRIKE AT FRAME 23 STR 17R. MAINTENANCE REPAIRED LIGHTNING STRIKE AT FRAME 23 STR 17R I/A/W EC 5330-01480, REPAIR FIGURE #1. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050727001042005072700104SO 2005 7 27 C2XA05SH085 120050721A532014530631001 FLOOR SUPPORT EMB 145 EMB145EP 3260221SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714943 145040 SHV-DURING C-CHECK MAINTENANCE FOUND LT OMEGA BEAM LOWER FLANGE IS CORRODED BETWEEN FRAMES 53-59. MAINTEANACE REPAIRED LOWER FLANGE AT FRAME 54 I/A/W EMB 145 SRM 53-00-10 & EC 5320-01140. INSTALLED NEW NUTPLATES I/A/W EC 5320-01137. PREPPED, PRIMED & PAINTED ALL BLEND OUTS ON LT OMEGA BEAM LOWER FLANGE BETWEEN FRAMES 53-59 I/A/W EMB 145 CPM 51-21-06. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050727001252005072700125NM 2005 7 27 USAA050819 120050630A5320 ANGLE BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU 23861 CLT - FOUND TRANSITION ANGLE CORRODED 8 INCHES, IN AFT CARGO BETWEEN STATION 727C AND AND STATION 827. REMOVED CORRODED ANGLE AND INSTALLED NEW ANGLE IAW SRM 51-10-02. (M) 2L72 4F RTA16WE 20050727001362005072700136SO 2005 7 27 C2XA05BT040 120050614A335020131A BATTERY PACK EMB 145 EMB145XR 3260214SO EMERGENCY LGIHT FAULTY A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714180 145900 EWR---CO2129, CREW REPORTED, EMERGENCY EXIT LOCATOR FOR EMERGENCY DOOR WILL NOT LIGHT UP.....MAINTENANCE REMOVED AND REPLACED BATTERY PACK FOR EMERGENCY EXIT LOCATOR IAW EMB145 AMM #33-50-04, OPS.CHECKED GOOD. 2L72 4F RT 20050727001372005072700137SO 2005 7 27 C2XA05SD023 120050616A2560A1140001002 FLASHLIGHT EMB 145 EMB145XR 3260214SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716178 14500889 COCKPIT EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED EMERGENCY FLASHLIGHT OPS CHECK GOOD AIRCRAFT RELEASED AND RETURNED TO SERVICE. 2L72 4F RT 20050727001392005072700139SO 2005 7 27 C2XA05CL053 120050621A3350110049 CHARGER EMB 145 EMB145LR 3260212SO CABIN FAULTY A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2718556 145595 THE CREW REPORTED A MID CABIN OVERHEAD EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY AND CHARGER. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20050727001432005072700143EA 2005 7 27 A6WA200540201 120050613A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31419AW 7633 LEFT SIDE INTERCOSTAL AT FS 484, LBL S7, IS CRACKED IN RADIUS APPROX .30 INCH LONG. (M) REMOVED CRACKED ANGLE FABED NEW ANGLE USING PREFORMED ANGLE. ETCHED, ALODINED, PRIMED, AND TOP COATED FABED ANGLE. INSTALLED FABED ANGLE ON LT SIDE INTERCOSTAL FS 484, LBL 27, IAW MFG REO. (K) 2L72 4F RTA21EA 20050727001602005072700160EU 2005 7 27 RAIA00507016 120050725A2612ES3029 PANEL JETAIRJETSTMJETSTM4101 1500501EU FIRE CAUTION MALFUNCTIONED A RAIAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 CE03560HK163996441 41076 RIGHT FIRE CAPTION FLASHES ON AT RANDOM. MAINTENANCE REMOVED AND REPLACED THE CAPTION PANEL. OPS CHECKED GOOD. 2L72 4T RTA41NM 20050727001682005072700168EU 2005 7 27 UPS05144964 120050709A5740A5724199320200 ANGLE AIRBUSA300 A300F4622R 3930360EU LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01121UP 0806 INSPECTION TYPE: 5YR, LEFT WING INSIDE KRUGER FLAP WELL, CURVED SUPPORT STRUCTURE IS CRACKED IN RADIUS OF 2ND RIB. REMOVED & REPLACED SUPPORT STRUCTURE ANGLE IAW A300-600 SRM 51-40-00. 2L72 4F RTA35EU 20050727001782005072700178NM 2005 7 27 DHL2005788006 120050727A3260 BULB BOEING727 727214 138407RNM MLG INDICATOR BURNED OUT A DHLAO OTHER P NO WARNING INDICATION APAPPROACH 1 SO01788AT 21958 RED "RIGHT GEAR" UNSAFE LIGHT DID NOT ILLUMINATE DURING LANDING GEAR EXTENSION. FOUND RIGHT GEAR RED CORRY LIGHT OUT OF POSITION & LAMP CONTACTS DEFORMED. RELAMPED & REPOSITIONED LAMPS IAW 33-10-0. P/N 387. OPS GOODIAW 32-61-01. 2L73 4F A3WE 20050727001802005072700180WP 2005 7 27 UPS05844969 120050711A53403779762U1 A/C PACK DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C1, LONGERON END FITTING CRACKED AT STA 690 L2L. REMOVED AND REPLACED LONGERON END FITTING AT STA 690 L2L IAW SRM 53-2-2, 51-1-20D, AND 51-3-0. 2L74 4F RT4A25 20050727001822005072700182WP 2005 7 27 UPS05844972 120050711A5340 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE:C1 FRAME TO INTERCOSTAL FITTING CRACKED STA 1200 L18R REMOVED FITTING AT STA 1200 L18R IAW SRM 51-1-20D FABRICATED AND INSTALLED FITTING AT STA 122 L18R IAW SRM51-1-8 AND 51-1-20D 2L74 4F RT4A25 20050728000082005072800008CE 2005 7 28 DXTA200500862 120050723A2741CS402186 POSITION SWITCH CESSNA560 560XL 2076702CE LT STAB INOPERATIVE E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07603QS3986 5605203 STAB MIS COMP LIGHT CAME ON AFTER T/O AND FLAPS SELECTED UP CYCLED FLAPS LIGHT WENT OUT AND ACCELERATED TO 250 KNOTS LIGHT CAME BACK ON AGAIN, SLOWED TO 200 KTS. ON GROUND LIGHT COMES ON WHEN FLAPS SELECTED UP, REMOVED AND REPLACED LT STAB POSITION SWITCH P/N CS402-186 S/N 541 WITH NEW SWITCH P/N CS402-1865 S/N 897. REGGIS AND OPS CHECK GOOD. WORK PERFORMED IAW CE560 MM 27-48-00 REF FAS W/O NR 05-1555. 2L72 4F RTA22CE 20050728000232005072800023WP 2005 7 28 ZJ62005F00000 220050608A7321897780X21 FUEL CONTROL BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE331* 01514WP INTERNAL LEAKING E ZJ6AO OTHER K FLUID LOSS NRNOT REPORTED 1 EA11404GJ8648 3109 754 P633201 DURING CLIMB OUT, LT TORQUE WAS OBSERVED DECREASING. POWER LEVER WAS ADVANCED AND CHARTED TORQUE VALVE COULD NOT BE REACHED AT ALTITUDE 5,000 MSL MAXIMUM OF 80 PERCENT TORQUE BE ATTAINED ON LT ENGINE TROUBLESHOT FOUND FUEL CONTROL LEAKING INTERNALLY, REPLACED FUEL CONTROL. (K) 2L72 4T3 TRTA21EU E2WE 20050728000302005072800030EU 2005 7 28 TRB2005F00002 120050604A2612 WARNING LIGHT AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE RT ENGINE ILLUMINATED A TRBAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SO29377AT 377 DURING GROUND OPERATION, THE RIGHT ENGINE HAD A NACELLE OVERHEAT LIGHT ON, FOLLOWED BY A FIRE WARNING ON AND AN INCREASE IN ITT. TAIL WIND OF 10 TO 14 KNOTS WERE PRESENT. PERFORMED A VISUAL CHECK THE RIGHT ENGINE AND FOUND NO EVIDENCE OF FIRE NOR DAMAGE. (M) 2H72 4T4 TRTA53EU E20NE 20050728000322005072800032EA 2005 7 28 A6AW200540237 120050713A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31409AW 7447 LT FS 280 AT LBL 9 IB CLIP ANGLE IS CRACKED .5 INCH LONG. (K) 2L72 4F4 FRTA21EA E15NE 20050728000342005072800034EA 2005 7 28 A6WA200540236 120050713A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31409AW 7447 RT FS 280 AT RBL 9 IB CLIP ANGLE IS CRACKED .5 INCH LONG. (K) 2L72 4F4 FRTA21EA E15NE 20050728000362005072800036EA 2005 7 28 A6WA200540251 120050716A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31420AW 7640 FS 280, RBL 9, OB ATTACH CLIP CRACKED. (K) REPLACED ANGLE P/N 601R31113-58 IAW CRJ SRM 51-42-06 AND BRAS EO 601R-53-6888. (M) 2L72 4F4 FRTA21EA E15NE 20050728000372005072800037EU 2005 7 28 TRB2005F00004 120050613A2910NTA152504 O-RING AEROSPATR72 ATR72212 8680945EU HYD SYSTEM DAMAGED A TRBAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SO29448AM 448 ON FINAL APPROACH, HYDRAULIC BLUE SYSTEM LOW PRESSURE INDICATION CAME ON. AIRCRAFT LANDED WITHOUT PROBLEM. REPLACED HYDRAULIC MODULE PRESSURE SWITCH O-RING THAT WAS FOUND LEAKING. (M) 2H72 4T RTA53EU 20050728000382005072800038EA 2005 7 28 A6WA200540235 120050713A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31409AW 7447 RT FS 280 AT RBL 9 OB CLIP ANGLE IS CRACKED .5 INCH LONG. (K) 2L72 4F4 FRTA21EA E15NE 20050728000392005072800039SO 2005 7 28 CHQA200500133 120050727A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11565RP 145679 LEFT OVERWING EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED LIGHT BULB IAW EMB 145 AMM 33-50-10-000-801-A. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050728000402005072800040NM 2005 7 28 0501136718 120050707A2120 ODOR BOEING747 747251F 1384898NM CABIN DETECTED A NWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL01618US 21122 DURING ROTATION AT TAKE-OFF, THERE WAS A STRONG SMELL OF FUEL ODOR. SMELL CLEARED IN 2-3 MINUTES AFTER PACK ACTIVATION. AIRCRAFT CONTINUED ON TO DESTINATION AND LANDED WITHOUT INCIDENT. SIN MAINTENANCE CHECKED FOR FUEL LEAKS, NONE FOUND. AIRCRAFT OK FOR RETURN TO SERVICE. 2L74 4F A20WE 20050728000412005072800041EA 2005 7 28 A6WA200540250 120050715A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE DENTED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31420AW 7640 PROTRUDING DENT AT FS 679, BETWEEN STR 23 AND STR 24, RT MEASURES .5 INCH X .020 INCH DEEP. PERFORMED REPAIR TO FUSELAGE SKIN FROM FS 672 TO 682 BETWEEN STRING STR 23 AND 24 BY CUTTING OUT DAMAGED AREA, PERFORMED NDT OF CUT LINE FAB AND DOUBLER AND INSTALLED IAW SRM. (K) 2L72 4F4 FRTA21EA E15NE 20050728000462005072800046NM 2005 7 28 CALA0500238 120050727A335010107451K SIGN BOEING757 757224 1384958NM EMERGENCY LIGHT INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2714107 27297 INSPECTION FOUND THE RT HALF OF CENTER AISLE EMERGENCY LIGHT EXIT SIGN AT OVERWING AREA INOPERATIVE. THE EXIT SIGN WAS REMOVED AND REPLACED. 2L72 4F RTA2NM 20050728000472005072800047NM 2005 7 28 USAA050741 120050608A5311 FRAME BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU 23861 CLT - FOUND FRAME CRACKED 1.3 INCH, 1978 FRAME AT STATION 616 BELOW CREASE BEAM. FABRICATED REPAIR ANGLE, INSTALLED WET PER TYPICAL REPAIR IAW TR 53-61-02. (M) 2L72 4F RTA16WE 20050728000482005072800048NM 2005 7 28 USAA050752 120050610A5414 SKIN BOEING737 7373B7 1384580NM RT PYLON CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19389US55016 23311 CLT - FOUND SKIN CRACKED .75 INCH, RT PYLON SKIN AT NACELLE STATION 216 ACCESS PANEL 5827R. ACCOMPLISHED DOUBLER REPAIR IAW EA 96659. (M) 2L72 4F RTA16WE 20050728000502005072800050NM 2005 7 28 P5CA0501382 120050726A3610 CONTROLLER BOEING747 74746NF 13848BTNM NR 3 ENGINE MALFUNCTIONED A P5CAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP23451PA 30809 STATUS MESSAGE NR 3 ENG PRV / OVHT. (RETURN TO BLOCK) DEFERRED PER MEL 36-11-8C. 2L74 4F RTA20WE 20050728000512005072800051NM 2005 7 28 USAA050746 120050608A5320 SUPPORT BOEING737 7374B7 1384702NM FUSELAGE DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19445US 24863 CLT - FOUND SUPPORT WITH 6 INCHES VARIOUS DAMAGE, BS 685. REPAIR DOUBLER INSTALLED IAW SRM 51-70-11. (M) 2L72 4F RTA16WE 20050728000522005072800052NM 2005 7 28 USAA050745 120050608A5320 INTERCOSTAL BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU52779 23861 CLT - FOUND INTERCOSTAL SUPPORT CRACKED .750 INCH, FUSELAGE STATION 295 AT STRINGER S-16L. FABRICATED AND INSTALLED NEW INTERCOSTAL IAW SRM 53-10-15, SRM 51-10-02. (M) 2L72 4F RTA16WE 20050728000532005072800053EA 2005 7 28 A6WA200540195 120050613A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31419AW 7633 RIGHT SIDE INTERCOSTAL AT FS 484, RBL 36, IS CRACKED IN FLANGE FROM TOP RIVET HOLE TO EDGE, APPROX .35 INCH LONG. REPAIRED RIGHT SIDE INTERCOSTAL AT FS 484 RBL 36 IAW BOMBARDIER REO 601R-53-41-059 REV A AND BRAS STANDARD REPAIR 601R-53-0030. (M) 2L72 4F RTA21EA 20050728000562005072800056NE 2005 7 28 COMA0560407 220050724A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE LEFT FAILED A COMAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01916CA10705 7014 807645 FLIGHT 5378- ENROUTE OKC-CVG RECEIVED A ZERO PSI OIL PRESSURE WARNING ON THE LEFT ENGINE. CREW DECLARED AN EMERGENCY, DIVERTED TO TUL AND LANDED WITHOUT INCIDENT. 2L72 4F4 FRTA21EA E15NE 20050728000572005072800057NM 2005 7 28 USAA050744 120050608A5754 WEDGE BOEING737 7374B7 1384702NM NR 1 SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19445US 24863 CLT - FOUND NR 1 LE SLAT WEDGE DELAMINATED 5 INCHES BY 3 INCHES, OUTBOARD END OF SLAT TRAILING EDGE WEDGE. COMPOSITE REPAIR IAW EA NR 96573. (M) 2L72 4F RTA16WE 20050728000622005072800062EA 2005 7 28 COMA0560402 120050719A3350364911AT LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A COMAO OTHER O OTHER NRNOT REPORTED 1 SO01957CA 7109 FLIGHT 5108- EMERGENCY FLOOR PATH LIGHTS INOPERABLE. REPLACED FLOOR TRACK LIGHTING ASSEMBLY. 2L72 4F RTA21EA 20050728000632005072800063EA 2005 7 28 COMA0560403 120050720A5610NP1393219 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A COMAA UNSCHED LANDING O OTHER CLCLIMB 1 SO01484CA7816 7702 FLIGHT 5657- PILOT WINDSHIELD SHATTERED. REPLACED WINDSHIELD. 2L72 4F RTA21EA 20050728000652005072800065EA 2005 7 28 COMA0560409 120050725A2410M5280343 BULB CNDAIRCL600 CL6002B19 1900309EA IDG TEMP FAILED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01496CA1 7791 FLIGHT 5315- NR 2 IDG CAUTION DURING T/O. REPLACED THE IDG TEMP BULB. 2L72 4F RTA21EA 20050728000672005072800067NM 2005 7 28 USAA050747 120050608A5340 STRINGER CLIP BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU 23861 CLT - FOUND TIE CLIP CRACKED .5 INCH, STATION 440 STRINGER 4L. DEFECTIVE PART REPLACED WITH IDENTICAL PART, REPLACED TIE CLIP IAW SRM 51-10-02. (M) 2L72 4F RTA16WE 20050728000692005072800069NM 2005 7 28 USAA050743 120050608A5340 STRINGER CLIP BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU 23861 CLT - FOUND TIE CLIP CRACKED .5 INCH, STATION 480 STRINGER 15R. REPLACED TIE CLIP IAW SRM 51-10-02. (M) 2L72 4F RTA16WE 20050728000702005072800070EA 2005 7 28 A6WA200540196 120050613A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31419AW 7633 LEFT SIDE INTERCOSTAL AT FS 484, LBL 36 IS CRACKED IN RADIUS APPROX .20 INCH LONG. REPAIRED LEFT SIDE INTERCOSTAL AT FS 484 LBL 36 IAW BOMBARDIER REO 601R-53-41-059 REV A AND BRAS STANDARD REPAIR 601R-53-0030. (M) 2L72 4F RTA21EA 20050728000722005072800072EA 2005 7 28 COMA0560404 120050723A3240 OVERHEAT SENSOR CNDAIRCL600 CL6002B19 1900309EA BRAKES MALFUNCTIONED A COMAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 SO01721CA 7259 FLIGHT 5580- BRAKE OVERHEAT MESSAGE. INSPECTED BRAKE AND FOUND NO DEFECTS. 2L72 4F RTA21EA 20050728000732005072800073WP 2005 7 28 0501159950 120050726A4990GTCP8598DCA APU DOUG DC9 DC932 3022066WP SMOKE A NWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL019346 6634832 47376 DURING CRUISE FLIGHT LEFT AFT LAV SMOKE DETECTOR SOUNDED AND CREW REPORTED SMOKE/SMELL. FLIGHT CREW DIVERTED AC TO MKE AND PERFORMED AN UNEVENTFUL LANDING. MAINTENANCE FOUND AN OIL LEAK AT APU GENERATOR DRIVE PAD SEAL. APU AREA CLEANED AND APU PLACED ON MEL. PACK BURNOUT PROCEDURES FOLLOWED AND COALESCER BAGS REPLACED. 2L72 4F A6WE 20050728000742005072800074EA 2005 7 28 COMA0560405 120050723A335020131A BATTERY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCHARGED A COMAO OTHER O OTHER NRNOT REPORTED 1 SO01483CA12571817 7689 FLIGHT 5595- AFT SECTION OF EMERGENCY FLOOR PATH LIGHTING INOPERABLE. REPLACED THE NR 4 EMERGENCY BATTERY. 2L72 4F RTA21EA 20050728000762005072800076EA 2005 7 28 COMA0560410 120050726A2133 OUTFLOW VALVE CNDAIRCL600 CL6002B19 1900309EA CABIN PRESSURE FAILED A COMAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 SO01929CA 7035 FLIGHT 5499- OVERBOARD COOL CAUTION. AIRCRAFT DID NOT PRESSURIZE. FOUND OVERBOARD AND INBOARD EXHAUST VALVES IN WRONG POSITION. PREVIOUS DEFERRAL ITEM. 2L72 4F RTA21EA 20050728000772005072800077EA 2005 7 28 A6WA200540200 120050613A5320601R3117117 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31419AW 7633 LEFT INTERCOSTAL AT FS 484, LBL 27, IS CRACKED IN RADIUS APPROX .30 INCH LONG. REMOVED CRACKED ANGLE, P/N 601R31171-17. FABRICATED NEW ANGLE USING PERFORMED ANGLE P/N S6444-14 ETCHED, PRIMED, TOP COATED FABRICATED ANGLE. INSTALLED FABRICATED ANGLE ON LEFT SIDE, INTERCOSTAL FS 484, RBL 27, IAW BOMBARDIER REO 601R-53-41-059 AND BR. (M) 2L72 4F RTA21EA 20050728000782005072800078EA 2005 7 28 COMA0560411 120050726A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01937CA 7044 FLIGHT 5043- FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2L72 4F RTA21EA 20050728000792005072800079EA 2005 7 28 A6WA200540207 120050620A261147359719 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA AFT CARGO BAY MALFUNCTIONED A A6WAO OTHER N FALSE WARNING NRNOT REPORTED 1 GL31439AW5960 7753 UPON CARGO SMOKE DETECTOR TEST, SMOKE DETECTOR MESSAGE WOULD NOT GO OUT. REMOVED AND REPLACED CARGO FIRE SMOKE DETECTOR IAW AMM 26-15-01, OPS CHECK GOOD AT THIS TIME. (M) 2L72 4F RTA21EA 20050728000802005072800080EA 2005 7 28 A6WA200540208 120050617A21707536893 COALESCER BAG CNDAIRCL600 CL6002B19 1900309EA AFT FUSELAGE DIRTY A A6WAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NRNOT REPORTED 1 GL31413AW 7585 JET FUEL ODOR IN COCKPIT. SUSPECT DIRTY COALESCER BAG FOR NR 1 PACK, PLACED ON MEL AND PLACARDED. REMOVED AND REPLACED NR 1 COALESCER SOCK IAW 21-51-13. OPS CHECK GOOD. REMOVED FROM MEL AND REMOVED PLACARD. (M) 2L72 4F RTA21EA 20050729000022005072900002NM 2005 7 29 AWXA200500862 120050708A53106516300169 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED FRAME WEB CRACKED .950 INCHES IN LENGTH, AT BS 178, WL 230 AND BL 17.1R. MAINTENANCE REMOVED DAMAGED AREA FROM THE FRAME WEB AT BS 178, WL 230, BL 17.1R. FABRICATED FILLER AND WEB IAW BOEING 737-300 SRM 53-10-08-2 FIG.12. MAINTENANCE INSTALLED FABRICATED REPAIR PARTS IAW BOEING 737-300 SRM 53-10-08-2 FIG 12. 2L72 4F RTA16WE 20050729000032005072900003NM 2005 7 29 AWXA200500863 120050703A5330654577885 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 MCN - MAJOR REPAIR - DURING C16 CHECK FOUND THE R2 DOOR CUTOUT, AT THE LOWER HINGE, CRACKED IN THE RADIUS OF THE FORWARD LOWER CORNER. MAINTENANCE CUTOUT THE DAMAGED PART OF THE LOWER SKIN PANEL IAW BOEING 737-300 SRM 53-60-01-2. FABRICATED FILLER, DOUBLER AND TRIPLER IAW BOEING 737-300 SRM 53-60-01-2 FIG 207. INSTALLED FABRICATED REPAIR PARTS ON R2 DOOR CUTOUT, AT THE LOWER HINGE, IAW BOEING 737-300 SRM 51-40-02-0 FIG 12 AND 13. 2L72 4F RTA16WE 20050729000052005072900005NM 2005 7 29 AWXA200500865 120050712A534066241701 CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 MCN - MAJOR REPAIR - DURING C16 CHECK FOUND CRACK, .275 INCHES IN LENGTH, ON SUPPORT CLIP LOCATED BELOW R/H ZEE ANGLE AT BS 947, STR 26R. MAINTENANCE REMOVED SUPPORT CLIP LOCATED BELOW R/H ZEE ANGLE AT BS 947, STR 26R IAW BOEING 737-300 SRM 51-40-02-0. FABRICATED NEW SUPPORT CLIP IAW BOEING 737-300 SRM 51-30-01-0. INSTALLED FABRICATED REPAIR PARTS BELOW R/H ZEE ANGLE AT BS 947, STR 26R IAW BOEING 737-300 SRM 51-40-02-0 FIGURES 12 AND 14. 2L72 4F RTA16WE 20050729000062005072900006NM 2005 7 29 AWXA200500866 120050711A532069434562 STRAP BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 MCN - MAJOR REPAIR - DURING C16 CHECK FOUND EXFOLIATION CORROSION IN THREE AREAS ON THE LOWER SIDE OF STRAP, LOCATED AT BS 847, STR 25R. MAINTENANCE REMOVED CORROSION FROM LOWER SIDE OF STRAP, LOCATED AT BS 847 AND STR 25R IAW BOEING 737-300 SRM 51-10-02-0. FOUND OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-15-1. STRAP WAS REMOVED FROM BS 847 AND STR 25R, NEW STRAP WAS FABRICATED IAW BOEING 737-300 SRM 51-40-05-0. INSTALLED REPAIR PARTS IAW BOEING 737-300 51-40-02-0 AT BS 847, STR 25R. 2L72 4F RTA16WE 20050729000072005072900007NM 2005 7 29 AWXA200500867 120050705A53306545774 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED THREE CRACKS, 1ST CRACK 2.0 INCHES IN LENGTH, SECOND CRACK 2.0 INCHES IN LENGTH, AND THIRD CRACK 1.5 INCHES IN LENGTH. CRACKS LOCATED ON THE SKIN AT STATION BS 727C + 9.90 AND BS 756.90, STRINGER 22L TO 25L. MAINTENANCE TRIMMED OUT DAMAGED AREA'S ON THE SKIN IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NO. 03-5361-05203-ES1. RE-INSPECTED AREA TO ENSURE ALL DAMAGED SKIN WAS REMOVED AND THERE WERE NO OTHER STRUCTURES DAMAGED IN THE AREA, IAW AWA ER 03-5631-05203-ES1. MAINTENANCE FABRICATED DOUBLER, TRIPLER, THREE FILLERS, AND TWO TEAR STRAP DOUBLERS IAW AWA ER 03-5361-05203-ES1. FABRICATED REPAIR PARTS WERE INSTALLED AT STATION BS 727C + 9.90 AND BS 756.90 AND2L72 4F RTA16WE 20050729000092005072900009EA 2005 7 29 QXEA200501137 120050722A7500GG670800025 SHUTOFF VALVE CNDAIRCL600 CL6002C10 1390015EA BLEED SYSTEM MALFUNCTIONED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09604QX882 10019 ONT- ON FLIGHT 2512, DURING TAXI OUT, THE LEFT BLEED CAUTION MESSAGE ILLUMINATED. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE PLACED THE NR 1 PRSOV ON MEL. MEL CLEARED ON 7/23 BY REPLACING THE LEFT PRSOV. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20050729000112005072900011NE 2005 7 29 ASMF200507019 220050725A7200 ENGINE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE LEFT FAILED W ASMFO OTHER EJ VIBRATION/BUFFET WARNING INDICATION TXTAXI/GRND HDL 1 SW23583MD416648812 49659 718412 CAPTAIN REPORTED THAT DURING LEFT ENGINE STARTING AND SHUT OFF, VIBRATION WAS FELT IN THE HOLE AIRCRAFT. THE LEFT ENGINE VIBRATION ABSORBERS, BARS AND ACCESSORIES WERE INSPECTED, BEING ALL CORRECT. THE LEFT ENGINE WAS STARTED DETECTING VIBRATION. THE UVC WAS DECOUPLED AND THE LEFT ENGINE WAS STARTED CONTINUING THE FAILURE. AIRCRAFT WAS SENT TO THE HANGAR AND THE LEFT ENGINE WAS REPLACED AND TESTED IAW MM 71-00-02 MM 24-20-00 RESPECTIVELY, ALL CORRECT. 2L72 4F4 FRTA6WE E9NE 20050729000132005072900013 2005 7 29 QXEA20051139 420050727A22108220259001 MOUNT CNDAIRCL600 CL6002C10 1390015EA SERVO MALFUNCTIONED A QXEAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM09610QX9545 10033 AFTER AUTOPILOT DISENGAGED, AILERONS WERE IMMOVEABLE (STUCK) FOR SEVERAL SECONDS. ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE REPLACED THE AILERON SERVO MOUNT. PERFORMED OPERATIONAL CHECKS ON THE AILERON SERVO, SERVO MOUNT, FLIGHT CONTROL COMPUTER, AUTOPILOT DISCONNECT SWITCHES, AILERON AND ELEVATOR SERVO ERROR VOLTAGES AND SERVO SLIP CLUTCH.CHECKS GOOD WITH NO DEFECTS. ALSO PERFORMED A GENERAL VISUAL INSPECTION OF THE AILERON MECHANICAL CONTROL SYSTEM AND CABLE RUNS IN NON-PRESSURIZED AREAS. BOMBARDIER AND ROCKWELL-COLLINS DECIDED A DETAILED VISUAL INSPECTION WAS NOT REQUIRED IN THE PRESSURIZED AREAS. NO DISCREPANCIES FOUND. AIRCRAFT RELEASED FOR TEST FLIGHT. TEST FLIGHT OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20050729000142005072900014WP 2005 7 29 ASMF200507021 120050725A53502919845 CABLE DOUG DC9 DC987 3022087WP TAILCONE DAMAGED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23753RA 49587 DURING TRANSIT SERVICE, THE TAILCONE WAS LOOSED. DURING OVERNIGHT CHECK, THE TAILCONE KEVLAR CABLE WAS REPLACED AND THE TAILCONE RELEASE MECHANISM CAM WAS ADJUSTED IAW MM 53-53-02 PAGE 203, BEING ALL CORRECT. 2L72 4F RTA6WE 20050729000162005072900016NM 2005 7 29 05FDEA02089 120050723A34119B810201 ADC BOEING727 727200 138407ENM COCKPIT MALFUNCTIONED A FDEAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 SO25242FE 21178 ON T/O NO AIRSPEED ON CAPT'S AIRSPEED IND. REJECTED T/O. 90 KNOTS RED TABS C/W. REPLACED DADC CPN 3400104 IAW M/M CHP 34-11-051-4 OPS CK GOOD 2L73 4F RTA3WE 20050729000172005072900017NM 2005 7 29 05FDEA02090 120050725A5330 SKIN BOEING727 727200 138407ENM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 GOUGE IN FUSELAGE SKIN AT BS 430, JUST BELOW STR. 18R. CUT OUT DAMAGE IN SKIN BS 430 R, STR 18 IAW SRM 53-30-3 FABRICATED, INSTALLED PARTS PER SRM 53-30-3. (CLOSED) 2L73 4F RTA3WE 20050729000192005072900019NE 2005 7 29 ARWA20050702 220050722A7510431599 ANTI-ICE VALVE DOUG DC8 DC862F 3021972WP PWA JT3D JT3D7 52039NE NR 1 ENGINE MALFUNCTIONED A ARWAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO19791AL 46150 671003 DURING TAXI OUT, NR 1 ENGINE ANTI-ICE VALVE LIGHT ILLUMINATED; FOLLOWED ABNORMAL PROCEDURE; RETURN TO RAMP. REMOVED AND REPLACED NR 1 ENGINE RT ANTI-ICE VALVE IN ACCORDANCE WITH MM 75-10-1; OPERATIONAL CHECK IN ACCORDANCE WITH MM 75-10-0 AND MM 71-0 FOUND NORMAL. 2L74 4F4 F 4A25 1E8 20050729000212005072900021EU 2005 7 29 05FDEA02103 120050726A5321 FLOOR PANEL AIRBUS300 A300F4605R 3930327EU CABIN DELAMINATED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25671FE 778 FWD CGO PIT FLOOR PNL 131MG DELAMINATED AND HAS EDGE DAMAGE. FLOOR PANEL FABRICATED ON TRAVELER T5/530781 IAW SRZ -25-005 2L72 4F RTA35EU 20050729000232005072900023EA 2005 7 29 ASOA05593 120050711A3230 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA MLG MALFUNCTIONED A ASOAO OTHER J WARNING INDICATION APAPPROACH 1 SO11919EV 7780 FLT 4647 - DURING APPROACH INTO ATL FROM APF, UPON SELECTING GEAR DOWN A GEAR UNSAFE WARNING WAS RECEIVED. THE QRH WAS COMPLIED WITH AND THE GEAR WAS LOWERED MANUALLY. THE CREW THEN RECEIVED A THREE GREEN DOWN AND LOCKED INDICATION. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE MAIN LANDING GEAR (MLG) SELECTOR VALVE. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050729000242005072900024EA 2005 7 29 ASOA05588 120050710A335020131A BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT MALFUNCTIONED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11902EV 7620 DURING A GROUND INSPECTION IN CVG, THE EMERGENCY LIGHTS WOULD ONLY TEST FOR A FEW SECONDS. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTS BATTERY PACKS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050729000252005072900025EU 2005 7 29 DHAL200536400 120050728A3260 ROLLER AIRBUS300 A300B4203 3930306EU NLG DOOR LOOSE A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01364DH 141 ON DEPARTURE FROM CVG. NOSE GEAR DOORS LIGHT REMAINED ON. PERFORMED ABNORMAL PROCEDURE AND CONTINUED TO DESTINATION RII REQUIRED. FOUND RT NOSE GEAR DOOR UPLATCH ROLLER LOOSE AND OUT OF RIG. TIGHTENED AND ADJUSTED PER MM 32-22-11. OPS CK GOOD RII JLUTZ 33605 2L72 4F RTA35EU 20050729000272005072900027EA 2005 7 29 ASOA05592 120050711A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11873AS 7549 FLT 4175 - DURING A GROUND INSPECTION IN ATL, THE EMERGENCY FLOOR LIGHTS BETWEEN ROWS 1-3 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT STRIP BETWEEN ROWS 1-3. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050729000292005072900029EU 2005 7 29 05FDEA02092 120050725A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU MCD FLOOR CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25670FE 777 SEAT TRACK AT BL-0 FR 70.5 IS CORRODED OUT OF LIMITS. CUT OUT THE DAMAGED SEAT TRACK SECTION IAW SRM 53-10-16. FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 53-10-16 REF TRAVELER T5/533029. 2L72 4F RTA35EU 20050729000312005072900031EU 2005 7 29 05FDEA02094 120050725A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU MCD FLOOR CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25670FE 777 SEAT TRACK AT R-2, -Y953 FR 55 TO 56 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED WITH NEW SEAT TRACK IAW SRM 53-10-16 FIG 201 REF TRAVELER T5/533734. 2L72 4F RTA35EU 20050729000322005072900032NM 2005 7 29 05FDEA02095 120050726A5753 SKIN DOUG MD11 MD11F 3023600NM TE FLAPS DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 RIGHT WING, INBOARD FLAP, FLAP VANE INBOARD LOWER SKIN FOUND DELAMINATED. DELAMINATION MEASURES 40.00 INCHES IN LENGTH BY 17.00 INCHES IN WIDTH. REPAIRED IN ACCORDANCE WITH FEDEX EA 1-5750-87555. 2L73 4F RTA22WE 20050729000332005072900033NM 2005 7 29 05FDEA02096 120050726A5320 SPLICE DOUG MD11 MD11F 3023600NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 CENTER CARGO LEFT SIDEWALL STATION 1531 L34 LONGERON SPLICE. SUSPECT CRACKED AS MARKED. NEW LONGERON SPLICE FABRICATED AS PER DWG A5A7112. CRACKED LONGERON SPLICE ON CTR CARGO LH SIDEWALL LONGERON 34 LH REMOVED AND REPLACED AS PER SRM 51-33-01 VOL. II. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050729000342005072900034EU 2005 7 29 05FDEA02097 120050726A5321 FLOOR PANEL AIRBUS300 A300F4605R 3930327EU CABIN CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25671FE 778 FLOOR PANEL 231VG PUNCTURED AND CRACKED. FABRICATED FLOOR PANEL ON TRAVELER NR T5/531063 IAW SRZ-25-005. 2L72 4F RTA35EU 20050729000352005072900035NM 2005 7 29 05FDEA02098 120050726A5311 FRAME BOEING727 727227 1384078NM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 DENT IN FRAME STA 970 STR 23L. REPAIRED FRAME AT STA 970 STR. 23L PER SRM 51-40-3 FIG 1. 2L73 4F A3WE 20050729000382005072900038EU 2005 7 29 05FDEA02101 120050726A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25671FE 778 MDCC SEAT TRACK FROM FRAME 54.2-54.3, BL-0 HAS 2 PLACES OF CORROSION REMOVED CORROSION IAW SRM 53-10-16 FOUND SEAT TRACK TO BE OUT OF LIMITS. FABRICATED SEAT TRACK ON TRAVELER NR T5/532242 IAW SRM 53-10-16 TREATED AND PRIMED IAW SRM 51-21-10. FABRICATED SEAT TRACK SPLICES ON TRAVELER T5/532244 IAW SRM 53-10-16. TREATED AND PRIMED SPLICES IAW SRM 51-21-10. REMOVED AND REPLACED SEAT TRACK SPLICES IAW SRM 53-10-16, TOUCHED UP PAINT IAW SRM 51-23-10. 2L72 4F RTA35EU 20050729000392005072900039EA 2005 7 29 ASOA05587 120050707A5312 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11832AS 7243 DURING A C-CHECK IN MCN, THE CO-PILOTS BULKHEAD WEB AT FS 280 WAS FOUND TO BE CRACKED BEYOND LIMITS APPROXIMATELY TWO INCHES OUTBOARD OF RBL 9. MAINTENANCE IS REPAIRING THE CO-PILOTS BULKHEAD WEB AT FS 280 OUTBOARD OF RBL 9 IAW BOMBARDIER REO 601R-53-11-627. (M) 2L72 4F RTA21EA 20050729000402005072900040EA 2005 7 29 ASOA05586 120050707A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11832AS 7243 DURING A C-CHECK IN MCN, THE FS 280 FLOOR SUPPORT ANGLE BETWEEN LBL 9 AND RBL 9 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FS 280 FLOOR SUPPORT ANGLE BETWEEN LBL 9 AND RBL 9. (M) 2L72 4F RTA21EA 20050729000432005072900043EU 2005 7 29 05FDEA02108 120050726A5315A53781947 FLOORBEAM AIRBUS300 A300F4605R 3930327EU FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25656FE 745 COMPLIED WITH EA 6-5310-82098 FUSELAGE MAIN FRAME 31 FLOORBEAM CRACK REPAIR, Y=1707.5. 2L72 4F RTA35EU 20050729000442005072900044EA 2005 7 29 ASOA05583 120050707A3350362624 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11820AS 7188 DURING A GROUND INSPECTION IN ATL, THE FORWARD SECTION OF EMERGENCY FLOOR LIGHTING WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD SECTION EMERGENCY FLOOR LIGHT STRIP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050729000472005072900047EU 2005 7 29 05FDEA02105 120050726A5321 FLOOR PANEL AIRBUS300 A300F4605R 3930327EU CABIN CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25671FE 778 MCD FLR PNL NR 262AH CRACKED. FABRICATED FLOOR PANEL ON TRAVELER NR T5/531328 IAW SRZ-25-005. 2L72 4F RTA35EU 20050729000482005072900048NM 2005 7 29 05FDEA02106 120050726A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE RH NR 14 FOUND WITH CORROSION EXCEEDING LIMITS. REMOVED AND REPLACED WITH NEW SPLICE FITTING PER SRM 51-38-01. 2L73 4F RTA22WE 20050726001942005072600194EU 2005 7 26 05FDEA02035 120050724A5321 FLOOR PANEL AIRBUS300 A300F4605R 3930327EU FUSELAGE PUNCTURED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25671FE 778 MDC FLOOR PANEL 231EF PUNCTURED AND CRACKED. REPLACED FLR PNL ON TRAVELER NR T5/531062. 2L72 4F RTA35EU 20050726001962005072600196EU 2005 7 26 05FDEA02036 120050724A5321 FLOOR PANEL AIRBUS300 A300F4605R 3930327EU FUSELAGE CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25671FE 778 MAIN CARGO FLOOR PANEL 241KJ IS CRACKED AT SEAT TRACK ATTACH POINT. REPLACED FLR PNL ON TRAVELER NR T5/530789 REF SRZ-25-005. 2L72 4F RTA35EU 20050726002012005072600201EU 2005 7 26 MALA050597 120050721A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15439XJ 340B439 DURING 4Y/2Y CHECK IN BNA FOUND SEAT TRACK AT BLO BETWEEN FS 297 AND 316 IS CORRODED AND HAS BEEN REPAIRED IAW SRM 53-70-60. REF: EAMS WORK ORDER 212650 TASK 2513. 2L72 4T RTA52EU 20050726002022005072600202EU 2005 7 26 MALA050598 120050721A52607253710871 RAIL SAAB SF340 340B 7860101EU AIRSTAIR CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15439XJ 340B439 DURING 4Y/2Y CHECK IN BNA FOUND PAX STAIR SLIDE RAIL ASSEMBLY PN 7253710-871 IS CORRODED AND HAS BEEN REPLACED IAW SRM 51-40-21/22. REF: EAMS WORKORDER 212650 TASK 2515 2L72 4T RTA52EU 20050726002032005072600203EU 2005 7 26 MALA050595 120050721A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15439XJ 340B439 DURING 4Y/2Y CHECK IN BNA FOUND LAV SEAT TRACK PN 7253721-459 IS CORRODED AND HAS BEEN REMOVED AND REPLACED IAW SRM 51-40-27 REF: EAMS WORKORDER 212650 TASK 2511 2L72 4T RTA52EU 20050726002042005072600204EU 2005 7 26 MALA0596 120050721A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15439XJ 340B439 DURING 4Y/2Y CHECK IN BNA FOUND SEAT TRACK AT LBL 18.3 AND BETWEEN FS297 AND 310 IS CORRODED AND HAS BEEN REPAIRED IAW SRM 53-70-60. REF: EAMS WORK ORDER 212650 TASK 2512 2L72 4T RTA52EU 20050726002092005072600209EU 2005 7 26 05FDEA02042 120050719A2612 FIRE LOOP AIRBUS310 A310 EU NR 2 ENGINE DAMAGED A FDEABA EMER. DESCENT UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25420FE 339 AFTER T/O AT 15000FT, RECEIVED FIRE WARNING ON ENGINE NR 2. DID PROCEDURES AND RETURNED TO LLBG. TLV U-INSPECTION & T/S PERFORMED ON MTSI 26-10/9536. FIXED DIFFERED LOOP-B, FOUND TWO PLUGS ON LOOP-A SENSING ELEMENTS IN BAD CONDITION (ONE WITH RUBBER ISOLATION CRACKED & ONE WITH CERAMIC INSULATION BROKEN, SIGN OF CORROSION AND ONE PIN PUSHED IN AND THE OTHER NOT LOCKED PROPERLY). DAMAGED PLUGS WERE REPLACED. FOUND ALSO PLUGS ON PYLONE LOOPS CROSSED, FOR MORE DETAILS SEE WRI:26-10/9536 2L72 4F RTA35EU 20050726002112005072600211EA 2005 7 26 CVU2005F00002 220050715A8520 LIFTER BEECH 80 65B80 1152812CE LYC O720 IO720A1B 41546EA ENGINE WORN E CVUAO OTHER O OTHER NRNOT REPORTED 1 WP1344MA 720 LD412 SMALL METAL FLAKES KEPT RE-APPEARING IN THE OIL SCREENS. FOUND WORN CAM NR 5 AND NR 6 CYLINDER INTAKE VALVES. ENGINES REMOVED FOR REPAIR. USE MFG ENGINE OIL ADDITIVE FROM TIME OF OVERHAUL. RUN ENGINE FREQUENTLY. (K) 1L72 3O3 O 3A20 1E15 20050726002152005072600215EA 2005 7 26 MK92005F00000 220050705A8530 STUD PIPER PA31 PA31350 7103110SO LYC O540 LTIO540J2BD 41533EA HARTZLHCE3Y HCE3YR2 GL NR 3 CYLINDER DESTROYED E MK9AO OTHER O OTHER NRNOT REPORTED 1 WP134110N 318252063 RL259568A DJ10143A THE FORWARD EXHAUST STUD BECAME LOOSE AND WAS FORCED OUT OF POSITION BY THE EFFECTS OF EXHAUST PRESSURES WORKING AGAINST IT. WHEN THE THREADS WERE COMPLETELY DESTROYED, BOTH ON THE STUD AND IN THE CYLINDER HEAD, THE EXHAUST WAS ALLOWED TO EXIT THE HEAD FROM A POSITION DIRECTLY UNDER THE EXHAUST VALVE PUSHROD HOUSING. THE RESULTING HEAT BURNED A HOLE IN THE TUBE ALLOWING OIL TO ESCAPE AND CREATE A LOT OF SMOKE. THE FLIGHT WAS NOT INTERUPTED AS THE SMOKE WAS NOT DETECTED UNTIL LANDING, AT WHICH TIME THE ENGINE WAS SECURED AND THE PASSENGERS DEPLANED. RECOMMEND AT EACH 50 HR/OIL CHANGE THE TORQUE BE TESTED ON THESE STUDS. (K) 1L72 3O3 O A20SO E14EA 5 CP33EA 20050726002172005072600217WP 2005 7 26 0501119601 120050725A2120 DUCT DOUG DC9 DC932 3022066WP RT ACM SEPARATED A NWAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL01601NW 47038 WHILE AT CRUISE AT FL350 THE RED "CABIN PRESS" LIGHT ILLUMINATED. COM COMPLIED WITH, FOLLOWED RED BORDERED CHECKLIST, AND A POWER DESCENT WAS INITIATED. CREW WAS ABLE TO RECOVER CONTROL OF CABIN PRESSURE AS THEY PASSED THROUGH FL290 BUT THEN LOST CONTROL AGAIN PERFORMED ANOTHER POWERED DESCENT TO FL230. FLIGHT CONTINUED ON TO DTW AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND A DUCT SEPARATED FROM THE RIGHT AIR CYCLE MACHINE AND REPLACED IT. LEAK CHECK WAS GOOD AND THE AIRCRAFT HAS RETURNED TO SERVICE. 2L72 4F A6WE 20050726002202005072600220EU 2005 7 26 05FDEA02039 120050724A5321 FLOOR PANEL AIRBUS300 A300F4605R 3930327EU FUSELAGE DELAMINATED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25671FE 778 DURING OK TO INSTALLED FOUND PANEL 162EF DELAMINATED. REPLACED FLR PNL ON TRAVELER NR T5/534022 REF SRZ-25-005. 2L72 4F RTA35EU 20050726002222005072600222NM 2005 7 26 F3LA200500034 120050721A21501298A00001 CHECK VALVE AIRBUSA319 A319111 3930336NM RT A/C PACK BROKEN A F3LAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 NM03908FR 2271 1759 FLIGHT CREW REPORTED STRONG, SMOKY/BURNING ELECTRICAL FUMES ON DESCENT AND WAS STRONGER IN AFT CABIN. REPLACED RT PACK CHECK VALVE (19HM) PER AMM 21-63-42, PB 401. NO LEAKS OR ODOR NOTED. 2L72 4F RTA28NM 20050726002262005072600226NM 2005 7 26 USAA050781 120050620A5320 SPLICE BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU52779 23861 CLT - FOUND STRINGER SPLICE CRACKED, .4 INCH AND .3 INCH, STATION 908, S4L. REMOVED OLD STRINGER SPLICE, INSTALL NEW SPLICE IAW SRM 53-00-01 FIG 229. (M) 2L72 4F RTA16WE 20050726002292005072600229NM 2005 7 26 2005UALA00665 120050715A5322 SHEAR TIE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29504UA 24625 SHEAR TIE AT FS 580, STR 14L-15L HAS OVERSIZE FASTENER HOLE. MANUFACTURED SHEAR TIE PER TIMCO EA REO-G10727, REV 1R, UA-EVA-50456. 2L72 4F4 FRTA2NM E17NE 20050726002352005072600235 2005 7 26 2005UALA00673 420050719A2565 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE SLIDE INOPERATIVE A UALAO OTHER O OTHER NRNOT REPORTED 1 WP29122UA 29168 SLIDE LIGHT INOP ON DOORS 4R AND 1L. REPLACED LAMPS. 2L74 4F4 FRTA20WE E24NE 20050726002402005072600240EU 2005 7 26 2005UALA00678 120050720A5313 STRINGER AIRBUS320 A320232 3930326EU FUSLEAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29418UA 485 STRINGER 43L HAS CORROSION AT FRAME 58. REPLACEMENT OF STRINGER (PSE) ACCOMPLISHED. 2L72 4F RTA28NM 20050726002602005072600260NM 2005 7 26 05FDEA02052 120050724A5710 SKIN DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 LEFT HAND WING UPPER SURFACE MOST INBOARD FOUND 1 EACH SKIN BULGE. LH WING UPPER SURFACE MOST INBD 01 EA. SKIN BULGE AREA CORROSION REMOVED AND REPROTECTED AS PER SRM 51-21-01 VOL. II. MAT'L REMOVED 0.042"; ORIG. THICKNESS 0.241"; MAT'L REMAINED 0.199"; FOUND EXCEEDED LIMIT AS PER SRM 57-10-00 FIG. 32 VOL. I. AREA REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-87558 - WINGS - LEFT HAND UPPER WING SKIN - CORROSION REPAIR AT XORS 108 AND STRINGER 13. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050726002642005072600264EU 2005 7 26 MALA050604 120050723A7931230386402 PROBE BAC 146 AVRO146RJ85A1500097EU OIL PRESSURE FAILED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15522XJ E2347 ON CLIMBOUT RECEIVED CONTINUOUS FLASHING LOW OIL PRESS WARNING ON ENG NR 1 OIL PRESS INDICATED 85 PSI WITH NO FLUCTUATION. OIL QTY WAS JUST BELOW HALF. ENGINE PARAMETERS WERE NORMAL WITH NG N2 BELOW 90 PERCENT. LIGHT STOPPED FLASHING. LIGHT DID NOT REILLUMINATE ON DESCENT OR APPROACH INTO MSP. ON SHUT DOWN AT THE GATE LIGHT DID NOT ILLUMINATE. REPLACED OIL PRESS PROCESSOR PN 2-303-864-02, SN OFF 040130700517, SN ON 040130700511. ALSO REPLACED NR 1 ENGINE OIL PRESS TRANSDUCER 2-303-8691, SN OFF 99153380045, SN 981533800029. LEAK CHECK GOOD 2H74 4F RTA49EU 20050726002672005072600267NM 2005 7 26 05FDEA02054 120050724A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE RT NR 02 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA1-5510-87597. [CLOSED] 2L73 4F RTA22WE 20050726002702005072600270SW 2005 7 26 IIF2005F00000 120050617A6310406040943101 CAP BELL 407 407 1182206SW ALLSN 250C 250C47B GL COUPLING BROKEN E IIFAO OTHER O OTHER NRNOT REPORTED 1 SW03407PR2639 139 53232 CAE847290 AIRCRAFT IN FOR INSPECTION, MECHANICAL INSPECTING AREA OF ROTOR BRAKE NOTICED BLACK LINE ACROSS EAR WHERE BOLT GOES THROUGH HOLE. REMOVED BOLT AND EAR FELL OFF. POSSIBLE CAUSE, VIBRATION. (K) 1G71 3U3 UO H2SW E1GL 20050726002732005072600273NM 2005 7 26 05FDEA02056 120050724A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE RT NR 04 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. [CLOSED] 2L73 4F RTA22WE 20050726002762005072600276EU 2005 7 26 05FDEA02059 120050725A5320A53781038214 WEB AIRBUS300 A300B4605R 3930308EU MAIN DECK CARGO CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25670FE 777 MAIN CARGO AT FR 38.1 38.2 AT -Y2462 RT SIDE SUPPORT WEB IS CRACKED. 2L72 4F RTA35EU 20050726002782005072600278NM 2005 7 26 05FDEA02063 120050725A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE LT NR 07 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. [CLOSED] 2L73 4F RTA22WE 20050726002812005072600281NM 2005 7 26 05FDEA02066 120050725A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE RT NR 20 FOUND WITH CORROSION EXCEEDING. REPAIRED IAW EA 1-5510-87597. [CLOSED] 2L73 4F RTA22WE 20050726002832005072600283NM 2005 7 26 USAA050798 120050623A5320 INTERCOSTAL BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19590US 23935 BFM - FOUND WEB/INTERCOSTAL CRACKED .125 INCH, STATION 294.5 STRINGER 7L. INSTALLED ANGLE REPAIR OVER CRACKED AREA PER SRM 53-10-15, 51-70-13. (M) 2L72 4F RTA16WE 20050726002852005072600285NM 2005 7 26 USAA050786 120050623A5312 BULKHEAD BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19446US 24873 FOUND BULKHEAD WEB WITH TWO CRACKS .125 INCH, WL 234, RBL 10.0 BS 178. INSTALLED DOUBLER PER EO 5300V153 AND SRM 53-10-08. (M) 2L72 4F RTA16WE 20050726002862005072600286NM 2005 7 26 05FDEA02069 120050725A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE LT NR 15 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. [CLOSED] 2L73 4F RTA22WE 20050726002882005072600288NM 2005 7 26 05FDEA02070 120050725A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE LT NR 19 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. [CLOSED] 2L73 4F RTA22WE 20050726002892005072600289SO 2005 7 26 UG82005F00004 120050711A3244217K221 TIRE GULSTMG1159 G1159A 3970109SO RROYCESPEY SPEY5118 54523EU NR 2 NLG MISMANUFACTURED E UG8AO OTHER O OTHER NRNOT REPORTED 1 GL23473KT312 438 NR 2 NOSE LANDING GEAR TIRE HAS A BULGE (INDICATING TREAD SEPARATION) BETWEEN THE SIDEWALL CHINE AND THE TREAD OF THE TIRE. BULGE IS APPROXIMATELY 7 INCHES LONG. SUSPECT MANUFACTURING DEFECT IN TIRE. TIRE AND WHEEL ASSY REMOVED FROM AIRCRAT AND OVERHAULED WHEEL WITH NEW TIRE INSTALLED ON AIRCRAFT. (K) 2L72 4F4 F A12EA E2EU 20050726002902005072600290NM 2005 7 26 05FDEA02068 120050725A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE RT NR 24 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. [CLOSED] 2L73 4F RTA22WE 20050726002922005072600292NM 2005 7 26 05FDEA02071 120050725A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE LT NR 21 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. [CLOSED] 2L73 4F RTA22WE 20050726002942005072600294NM 2005 7 26 05FDEA02074 120050725A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE LT NR 27 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED AS PER EA1-5510-87597. [CLOSED] 2L73 4F RTA22WE 20050726002952005072600295NM 2005 7 26 05FDEA02076 120050725A7830 FRAME DOUG MD11 MD11 3023602NM THRUST REVERSER CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 NR 1 ENGINE, RIGHT HAND THRUST REVERSER COWL T-FRAME AT LOWER 2 BUMPER AREA FOUND WITH CHAFING MARK. CARRIED OUT REPAIR PER FEDEX EA 1-7830-87557. ENGINE THRUST REVERSER - NR 1 ENGINE, RIGHT HAND TEE FRAME WEAR AT 4 AND 5 O' CLOCK POSITIONS - REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2L73 4F RTA22WE 20050726002972005072600297NM 2005 7 26 USAA050837 120050705A5510 FITTING BOEING737 7374B7 1384702NM HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19441US40664 24812 FOUND FITTING CORRODED .25 BY .25, HORIZONTAL STAB CTR SECTION, RT SIDE, FORWARD SPAR. SPOT FACED FORWARD FACE OF FORWARD LUG IAW 55-10-10. (M) 2L72 4F RTA16WE 20050726002992005072600299NM 2005 7 26 05FDEA02078 120050725A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE LT NR 33 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. [CLOSED] 2L73 4F RTA22WE 20050726003032005072600303NM 2005 7 26 05FDEA02082 120050725A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE LT NR 14 FOUND WITH CORROSION EXCEEDING LIMITS. FITTING REMOVED AND NEW FITTING INSTALLED PER SRM 57-38-01. (CLOSED) 2L73 4F RTA22WE 20050726003062005072600306NM 2005 7 26 05FDEA02084 120050725A5510 WEB DOUG MD11 MD11 3023602NM HORIZONTAL STAB DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 TO PROVIDE ACCESS AT HORIZONTAL STABILIZER CUT OUT UPPER TORQUE BOX WEB FOR REPAIR OF 36L BARREL NUT HOLE. REPAIRED PER EA 1-5310-87589. [CLOSED] 2L73 4F RTA22WE 20050727000082005072700008EU 2005 7 27 DAT2005F00007 120050707A3244 TIRE STBROSSD3 SD360 8100606EU PWA PT6 PT6A65R 52043EA MLG FAILED E DATAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 GL13601CA 39 SH3623 AC HAD NORMAL STARTUP, TAXI OUT AND WAS CLEARED FOR TAKEOFF. FO WAS FLYING, CAPTAIN SET THE POWER, MADE THE CALLOUTS AND HAD JUST FINISHED SAYING (AIRSPEED ALIVE) WHEN FLIGHT CREW HEARD AN EXPLOSION, FELT THE LT WING DIP JUST AFTER A SLIGHT LT YAW. FLIGHT CREW CALLED (ABORT). TOOK THE POWER BACK TOP BETA. PLANE NEVER MADE IT TO (70 KNOTS) CALL SO AC WAS ABOUT 60 KNOTS WHEN IT HAPPENED. NEVER LOST CENTERLINE AND NEVER USED BRAKES BUT COASTED OFF THE RUNWAY AT DELTA. MECHANIC WAS DISPATCHED, AND REMOVED DAMAGED LT MAIN WHEEL AND REPLACED WITH A SERVICEABLE MAIN WHEEL ASSY. DAMAGED HONEYCOMB LANDING GEAR POD ASSY WILL BE REPAIRED FOR THE INTENDED FERRY FLIGHT TO COMPLETE THE REQUIRED PERMANENT REPAIR. (K) 2H72 4T4 T A41EU E4EA 20050727000092005072700009NE 2005 7 27 DAT2005F00008 320050630A6111A10460EK BLADE STBROSSD3 SD360 8100606EU PWA PT6 PT6A67R 52043NE HARTZLHCA6A HCA6A3A NE LT PROPELLER CRACKED E DATAK NONE O OTHER ININSP/MAINT 1 GL13263GA11644583 SH3754 PCE106087 GP37 DURING THE SCHEDULED COMPLIANCE OF AD ON THE LT PROPELLER IT WAS FOUND 1 OF 6 PROPELLER BLADES WERE CRACKED. MECHANIC REMOVED AND REPLACED THE PROPELLER IAW MM. OPS CHECK GOOD. AC WAS RETURNED TO SERVICE. (K) 2H72 4T4 T A41EU E26NE 6 CP14NE 20050727000112005072700011NE 2005 7 27 KBM2005F00167 220050712A7321 LINE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE FUEL CONTROL LEAKING E KBMAO OTHER K FLUID LOSS NRNOT REPORTED 1 WP19350SH878 1290M 2957 FUEL CONTROL UNIT ASSY REAR SPLIT LINE IS SEEPING FUEL STATICLY, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050727000222005072700022 2005 7 27 QXEA20051135 420050723A2210C18112AA YAW DAMPER BOMBDRDHC8 DHC8402 1390042NM ZONE 300 FAILED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09410QX8891 4053 YAW DAMPER FAILED DURING CLIMB, RESET AND FAILED AGAIN WITH 15 SECONDS. RUDDER TRIM EXCESSIVE TO THE RIGHT DURING ALL PHASES OF FLIGHT. MAINTENANCE PERFORMED OPEATIONAL TEST OF THE RUDDER TRIM SYSTEM IAW Q400 AMM 27-22-00-71-801. OPS CHECKED GOOD. REMOVED AND REPLACED YAW DAMPER ACTUATOR IAW Q400 AMM 22-11-36, PAGES 401-408. PERFORMED OPERATIONAL TEST OF THE YAW DAMPER ACTUATOR IAW Q400 AMM 22-11-36, PAGES 501-503. OPS CHECK GOOD AND RII COMPLIED WITH. AIRCRAFT RETURN TO SERVICE. 2H72 4T RTA13NM 20050727000412005072700041WP 2005 7 27 DHL2005802538 120050719A5330 SKIN DOUG DC8 DC873 302199CWP FUSLEAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH84803 46076 ITEM REF. NR. 045009: FWD ACCY COMPT. FUSELAGE INTERNAL SKIN CORRODED, STA 20.000 L-31R TO L-32R (STA 20.000-70.000) MAJOR REPAIR. CORR.: PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 07-18-05 DWG Z20-R14 REV IR DATED 06-24-05. REMOVED EXISTING REPAIR IAW SRMK 51-1-21 PG. 1, SRM 51-1-20D PG. 21. REMOVED CORROSION (INTERNAL PART) IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG. 2P. CUT OUT CORRODED SECTION IAW DWG Z20-R14. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED FILLER (AL7075T6 0.050) 2EA FINGER DOUBLER (AL7075T6 0.032) REPAIR DOUBLER (AL7075T6 0.063) IAW DWG Z20-R14. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES2L74 4F RT4A25 20050727000432005072700043WP 2005 7 27 DHL2005802540 120050717A5311S2537716 FRAME DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH84803 46076 RT UPPER CUSP EXTRUSION FRAME FWD FLANGE CRACK 0.750 STA 240.000 L-20R TO L-21R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG. 2 SHEET 1,2,6, SRM 53-2-0 FIG. 2 SHEET 7-8, TR 53-110, SRM 53-2-0 FIG. 2 SHEET 1, SRM 53-4-1 FIG. 40 SHEET 7-9, SRM 51-2-0 FIG. 50. REMOVED FASTENERS IAW SRM 51-1-20D PG. 21. CUT OUT DAMAGED FRAME SEGMENT IAW SRM 53-2-0 FIG. 2 SHEET 2-6. PERFORMED DETAIL VISUAL INSP. NO CRACK OR CORROSION FOUND. FABRICATED SPLICE AND ANGLE IAW SRM 53-2-0 FIG. 2 SHEET 2-6, SRM 53-2-0 FIG. 2 SHEET 7, TR 53-110, SRM 51-1-4 PG. 1. HEAT TREATED SPLICE AND ANGLE AND FRAME SEGMENT IAW SRM 51-1-1 PG. 1-13-17. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 512L74 4F RT4A25 20050727000442005072700044WP 2005 7 27 DHL2005802541 120050718A5541570055629SP WEB DOUG DC8 DC873 302199CWP RUDDER CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH84803 46076 RUDDER L/E FRONT SPAR FWD NOSE RIB WEB CRACK 1.500 STA ZR 71.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DOUGLAS DWG 5700556, JC EA55100012-001-D. REMOVED DAMAGED RIB IAW SRM 51-1-21 PG. 1. FABRICATED NEW RIB (AL2024"O" 0.063) IAW DWG 5700556, EA SEMAN 20051035, SRM 55-6-1 FIG. 2 SHEET 2 ITEM R, SRM 51-1-4. HEAT TREATED IAW SRM 51-1-1 PG. 1,13,17 TO T4. PERFORMED NDT INSP IAW NDT SPM PART 08-00-02 TO 07. CLEANED, TREATED AND PRIMED AREA AND NEW RIB IAW SRM 51-1-8B. INSTALLED NEW RIB IAW SRM 51-1-21 PG.1. FOR RIB FABRICATION REFER TO JC EA55100012-001-D. 2L74 4F RT4A25 20050727000632005072700063WP 2005 7 27 DHL2005802510 120050711A5320 FLOOR SUPPORT DOUG DC8 DC873 302199CWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH84803 46076 AFT ACCY COMPT. FLOOR SUPPORT ANGLE CORRODED, STA 1710.000 RBL 19. REMOVED CORROSION FROM SUPPORT ANGLE IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG. 2P. FABRICATED REINFORCING ANGLE IAW SRM 53-7-3 FIG. 5A, SRM 53-2-0 PG. 2E/2F. CLEANED, TREATED AND PRIMED AREA AND REINFORCING ANGLE IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE IAW SRM 51-1-20D PG. 9, SRM 51-3-1 (TORQUE). 2L74 4F RT4A25 20050727000752005072700075NM 2005 7 27 QXEA200501133 120050723A2910 RELAY DHAV DHC8 DHC8202 2809007NM HYD PUMP FAILED A QXEAA UNSCHED LANDING O OTHER APAPPROACH 1 NM09354PH 498 NR 1 STANDBY HYDRAULIC PRESSURE READS ZERO AFTER SWITCH SELECTED TO NR 1. MAINTENANCE REPLACED RELAY 292-K5, NR 1 STANDBY HYDRAULIC PUMP OPERATES NORMALLY AS PER AMM 29-11-17-710-801. CIRCUIT BREAKER REMAINED SET. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050727000822005072700082EU 2005 7 27 AWXA200500847 120050723A3800Z160H0068110 MODULE AIRBUS320 A320232 3930326EU WATER AND WASTE FAILED A AWXAO OTHER O OTHER CRCRUISE 1 WP28648AW 770 IN CRUISE LAV SMOKE EMERGENCY LIGHTS ILLUMINATE ON FOWARD PANEL. MAINTENANCE REMOVED AND REPLACED THE WATER AND WASTE LOWER MODULE. 2L72 4F RTA28NM 20050727000842005072700084 2005 7 27 AWXA200500849 420050723A2565DHE1141 WARNING LIGHT AIRBUSA319 A319132 3930340NM OVERWING SLIDE FALSE ACTIVATIONA AWXAK NONE O OTHER ININSP/MAINT 1 WP28830AW 1565 DURING 8 DAY CHECK, THE RT OVERWING EMER EXIT 'SLIDE ARM' LIGHT WOULD NOT EXTINGUISH WHEN THE RT OVERWING EMER EXIT ARM/DISARM LATCH PIN WAS DISENGAGED. MAINTENANCE REMOVED AND REPLACED THE RT EMERGENCY EXIT OVERWING PROXIMITY SWITCH, 6WN2 IAW AIRBUS MM 52-73-11-05. OPERATINAL CHECKS WERE GOOD. 2L72 4F RTA28NM 20050727000892005072700089WP 2005 7 27 DHL2005802523 120050717A57203704841502 FITTING DOUG DC8 DC873 302199CWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH84803 46076 MAIN TANK INTERIOR LWR SECTION INBD AFT FITTING CRACK STA XRS 74.689 S-61. PERFORMED MAJOR RELPAIR IAW SRM 57-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. CLEANED AND APPLIED TOP COATING MATERIAL TO AREA IAW SRM 51-1-12 PG 7. APPLIED SEALANT TO FAYING SURFACE IAW SRM 51-1-12. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9. TORQUED IAW SRM 51-3-1. REFER TO NR 030838 FOR LEAK CHECK. 2L74 4F RT4A25 20050727001132005072700113SO 2005 7 27 C2XA05SH072 120050517A532014530646401 FLOOR SUPPORT EMB 145 EMB145EP 3260221SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714943 145040 SHV-DURING C- CHECK LT OMEGA BEAM LOWER FLANGE IS CORROED BTWN FR 53-59. MAINTENANCE BLENDED LT OMEGA BEAM BTWN FR 53-59. FR 54 OUT OF LIMIT ALL OTHER FRMS WITHIN LIMIT IAW EMB 145 SRM 53-24-10. PERFORMED OMEGA BEAM REPAIR ON LT OMEGA BEAM LWR FLANGE AT FR 54 IAW EMB 145 SRM 53-00-10 AND EC 5320-01140.INSTALLED NEW NUTPLATES IAW EC 5320-01137.THE AIRCRAFT WAS APPROVE FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050727001382005072700138SO 2005 7 27 C2XA05IA083 120050618A3320BR90002 BALLAST EMB 135 EMB135LR 3260305SO GALLEY INOPERATIVE A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW2714514 145303 THE CREW REPORTED A BURNED/HOT ELECTRICAL ODOR COMING FROM THE GALLEY. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE LIGHT BALLAST FOR THE GALLEY LIGHT, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050727001442005072700144NE 2005 7 27 ALG2005F00043 120050707A6520 CHIP DETECTOR SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30 03013GL T/R GEARBOX MALFUNCTIONED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03518AL 760134 IN CRUISE FLIGHT, THE T/R CHIP/HOT CAUTION LIGHT CAME ON, PILOT FOLLOWED EMERGENCY CHECK LIST AND LANDED. THE MECHANIC CLEANED AND INSPECTED THE CHIP PLUG AND COMPLIED WITH PENALTY RUN IAW MM AND AIRCRAFT WAS RETURNED TO SERVICE. (K) 1G72 3U3 U H1NE E1GL 20050727001532005072700153EA 2005 7 27 A6WA200540198 120050613A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31419AW 7633 CLIP AT FS 280, RBL 9, OUTBOARD SIDE IS CRACKED IN RADIUS APPROX .70 INCH LONG. (M) 2L72 4F RTA21EA 20050727001582005072700158WP 2005 7 27 I5HA0558004 120050608A24212CM353C1J GENERATOR CVAC 340 340CVAC 242270AWP ALLSN 501D 501D13 03004GL RT AC SYSTEM FAILED A I5HAO OTHER O OTHER NRNOT REPORTED 1 GL23584E 2854 24 500963 WHILE ON TRAINING FLIGHT, RT AC GENERATOR (MECHANICAL FAIL) LIGHT ILLUMINATED. THE CAPTAIN PERFORMED AN IN-FLIGHT PRECAUTIONARY SHUTDOWN OF THE RT ENGINE IAW PROCEDURES IN THE EMERGENCY PROCEDURES CHECKLIST. THE AIRCRAFT RETURNED TO BASE AND MADE AN UNEVENTFUL LANDING. RT AC GENERATOR WAS REMOVED AND INSPECTED. THERE WAS NO OBVIOUS DAMAGE TO THE GENERATOR. THE REDUCTION GEARBOX DRIVE GEAR WAS ALSO INSPECTED FOR DAMAGE. NONE WAS FOUND. A SERVICEABLE GENERATOR WAS INSTALLED AND THE AC WAS RETURNED TO SERVICE. (K) 2L72 4R4 T 6A6 E282 20050727001882005072700188NM 2005 7 27 BB05057 120050725A335020121 CHARGER BOEING767 767201 1385125NM PASSENGER CABIN FAILED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19650US 23902 THE FIRST CLASS, RIGHT SIDE FLOOR EMERGENCY AISLE LIGHTS WERE FOUND INOPERATIVE DURING TEST. MAINTENANCE REPLACED THE BATTERY CHARGER ASSEMBLY AND BATTERY FOR THE RIGHT SIDE FIRST CLASS. OPERATIONALLY CHECKS NORMAL. 2L72 4F RTA1NM 20050728000102005072800010CE 2005 7 28 DXTA200500867 120050727A3240 BRAKE CESSNA560 560XL 2076702CE MLG MALFUNCTIONED E DXTAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07625QS 5605319 PILOT AND COPILOT BRAKES SPONGY. ITEM IS UNDER INVESTIGATION 2L72 4F RTA22CE 20050728000212005072800021EU 2005 7 28 AWXA200500853 120050725A3260848401 SENSOR AIRBUS320 A320231 3930325EU LT MLG FAILED A AWXAO OTHER J WARNING INDICATION LDLANDING 1 WP28620AW 052 RNO - EMERGENCY LANDING - FLT 522 - DURING FINAL, RECEIVED GEAR DOWN LOCKED INDICATION BUT HAD GEAR WARNING. DID A FLY BY OF TOWER FOR VISUAL. LANDED IN RNO WITHOUT NOSEWHEEL STEERING AND WAS TOWED TO THE GATE. MAINTENANCE FOUND 15GAA AND 17GAA CONNECTORS ON LT MAIN LANDING GEAR DAMAGED. REMOVED AND REPLACED CANNON PLUGS 15GAA AND 17GAA IAW AIRBUS MM 20-44-00. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA28NM 20050728000422005072800042NM 2005 7 28 USAA050753 120050614A5512 SKIN BOEING737 7373B7 1384580NM HORIZONTAL STAB CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19531AU50176 24478 PIT - FOUND H/S LOWER SKIN CRACKED 2 INCHES, RT HORIZ STAB LOWER SURFACE AFT SPAR STATION 124. ACCOMPLISHED REPAIR PER TYPICAL REPAIR 55-10-08 AND SRM 55-10-01 PAGE 212. (M) 2L72 4F RTA16WE 20050728000452005072800045NM 2005 7 28 USAA050740 120050608A5330 DOUBLER BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU52779 23861 CLT - FOUND DOUBLER CORRODED 3.5 INCH, DOUBLER ON THE WEB ATTACHED TO AFT FLANGE AT STATION 986.5 RBL 43. REPLACED DOUBLER IAW SRM 51-70-13. (M) 2L72 4F RTA16WE 20050728000592005072800059EA 2005 7 28 COMA0570087 120050723A5320CC67034175701 CROSSBEAM CNDAIRCL600 CL6002C10 1390015EA CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01354CA7620 10064 THE TRANSVERSE BEAM AT FS 280 IS CORRODED. REMOVED AND REPLACED TRANSVERSE BEAM P/N CC670-34175-7-01 I/A/W BOMBARDIER REO 670-53-11-047 REV C. 2L72 4F RTA21EA 20050728000662005072800066NM 2005 7 28 USAA050748 120050608A5340 STRINGER CLIP BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU52779 23861 CLT - FOUND TIE CLIP CRACKED .250 INCH, STATION 480 STRINGER 15R. REPLACED TIE CLIP IAW SRM 51-10-02. (M) 2L72 4F RTA16WE 20050728000712005072800071EA 2005 7 28 COMA0560401 120050719A325016480101 MODULE CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01966CA5014 7132 FLIGHT 9474- NLG STEERING INOPERATIVE. REPLACED THE ELECTROHYDRAULIC MODULE. 2L72 4F RTA21EA 20050729000152005072900015NE 2005 7 29 ASMF200507022 220050726A72007958537501 HOSE DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE LT ENGINE DAMAGED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23204AM 49404 725491 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF WHEN LEFT ENGINE WAS STARTED, IT DID NOT REACH THE MINIMUM IDLE VALUES. DURING TAXING, ENGINE WAS ACCELERATED TO 80% OF RPM AND IT ONLY REACHED EPR 1.00, N1 18 PERCENT, N2 43 PERCENT, EGT 520 AND FF 400 KGPM. TWO CLICKS OF ADJUSTMENT WAS PERFORMED TO FCU AND THE LEFT ENGINE WAS STARTED REACHING N2 54 PERCENT, N1 28 PERCENT AND EGT 400, STARTING THE RIGHT ENGINE WITH SIMILAR PARAMETERS. THE ENGINES WERE TESTED IAW 71-00-01, ALL CORRECT. DURING OVERNIGHT CHECK, THE PT2 AND PT7 HOSES WERE REPLACED IAW MM 72-00-03, THE EPRS SYSTEM WAS VERIFIED IAW MM 77-11-01, ACCELERATORS ADJUSTMENT WAS CHECKED AND TRIM TO BOTH ENGINES WAS PERFORMED IAW MM 76-11-00 AND MM 71-00-00 2L72 4F4 FRTA6WE E9NE 20050729000202005072900020EU 2005 7 29 05FDEA02102 120050726A5321 FLOOR PANEL AIRBUS300 A300F4605R 3930327EU CABIN CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25671FE 778 MCD FLOOR PANEL 232NG PUNCTURED AND CRACKED. FABRICATED NEW FLOOR PANEL ON TRAVELER T5/531061 IAW SRZ -25-005. 2L72 4F RTA35EU 20050729000222005072900022EU 2005 7 29 05FDEA02104 120050726A5321 FLOOR PANEL AIRBUS300 A300F4605R 3930327EU CABIN DELAMINATED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25671FE 778 W/O 29493, NR# N00484, BULK CARGO PIT FLOOR PNL 161GF DENTED AND DELAMINATED NEW FLOOR PANEL FABRICATED ON T5/530783 IAW SRZ-25-005 2L72 4F RTA35EU 20050729000372005072900037 2005 7 29 05FDEA02100 420050726A3460 FMC AIRBUS310 A310222 3930315EU NR 1 FAILED A FDEAA UNSCHED LANDING GJ MULTIPLE FAILURE WARNING INDICATION CLCLIMB 1 SO25456FE 318 DURING T/O FMC NR 1 FAILED AND RETURNED ON INITIAL FOLLOWED BY NUMEROUS FAULTS ON OVERHEAD PANEL, SLATS/FLAP 1 AND 2 FAULTED, ATS 1 AND 2 FAILED, PITCH NR 1 AND YAW DAMP NR 1 DROPPED OFF, FOLLOWED BY FUEL PUMPS ON NR 1. RT OUTER AND LT NR 2 OUTER PUMPS FAILED AND LEFT WINDOWS HEAT FAILED. NR 1 GEN FAILED AND APU WAS OFF ACN RELEASED FOR SERVICE PER MEL/CDL: 24-11-01CATEGORY: B EXPIRATION: 28JUL05 "MEL 24-11-01: GEN (IDENTIFY 1 OR 2) 1 INOP. TROUBLESHOT PER TSM 24-00-00 PG 155. CHECKED GEN FEEDER CABLE AND FOUND CABLE TERMINAL BLOCK TO IDG LOOSE. CLEANED, RETORQUED TERMINALS/CLEARED MEL. 2L72 4F RTA35EU 20050729000422005072900042NM 2005 7 29 DU4R0507163 120050728A5311 FRAME BOEING757 757232 1384965NM FUSELAGE DENTED B DU4RK NONE O OTHER ININSP/MAINT 1 SO15624DL 22914 DENT IN AFT CARGO COMPARTMENT BS 1520 FRAME UPPER FLANGE BETWEEN S-25 TO S-26L. 2L72 4F RTA2NM 20050729000492005072900049NM 2005 7 29 05FDEA02107 120050726A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE RT NR 26 FOUND WITH CORROSION EXCEEDING LIMITS. CORRODED FITTING REMOVED AND NEW FITTING INSTALLED PER SRM 51-38-01 VOL II AND SRM 51-33-01 VOL II. MINOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050729000522005072900052NM 2005 7 29 DU4R0507167 120050728A5315 FLOORBEAM BOEING757 757232 1384965NM FUSELAGE CRACKED B DU4RK NONE O OTHER ININSP/MAINT 1 SO15624DL 22914 CRACKED CAP ON FLOORBEAM AT BS 900 BL 54L TO 64L WL 208.1. 2L72 4F RTA2NM 20050729000532005072900053NM 2005 7 29 DU4R0507162 120050728A5311 FRAME BOEING757 757232 1384965NM FUSELAGE CRACKED B DU4RK NONE O OTHER ININSP/MAINT 1 SO15624DL 22914 CRACK IN FRAME UPPER SURFACE IN AFT CARGO COMPARTMENT BS 1540. 2L72 4F RTA2NM 20050729000542005072900054EU 2005 7 29 05FDEA02109 120050726A5410 SPAR AIRBUS300 A300F4605R 3930327EU NR 1 PYLON CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25656FE 745 PYLON STRUCTURE CANTILEVER BEAM LWR SPAR WEB CRACK. COMPLIED WITH EA 6-5450-82109, PYLON STRUCTURE CANTILEVER BEAM LWR SPAR WEB CRACK. 2L72 4F RTA35EU 20050729000562005072900056NM 2005 7 29 05FDEA02111 120050727A5313 LONGERON DOUG MD11 MD11F 3023600NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 FORWARD CARGO: BILGE AREA STA 6-10 L51L LONGERON FOUND CORRODED. CORROSION AT LONGERON END FWD CARGO BILGE STA 6-10 L51R TRIMMED OUT AND CARRIED OUT REPAIR AS PER SRM 53-10-00 VOL. I FIG. 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2L73 4F RTA22WE 20050729000572005072900057NM 2005 7 29 05FDEA02112 120050727A5320 SPLICE DOUG MD11 MD11F 3023600NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 CENTER CARGO, STA 1531 L44R LONGERON SPLICE FOUND CRACKED. CRACKED LONGERON SPLICE ON CENTER CARGO STA 1531 LONGERON 44R REMOVED AND REPLACED AS PER SRM 51-33-01 VOL. II. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2- 100. 2L73 4F RTA22WE 20050729000612005072900061NM 2005 7 29 05FDEA02116 120050727A5311 FRAME BOEING727 727227 1384078NM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 FWD CARGO PIT FRAME AT BS 500 HAS A DENT BETWEEN STRINGER 23R AND 25R. REPAIRED FRAME IAW SRM 51-40-3 THIS IS A MAJOR REPAIR. 2L73 4F A3WE 20050729000662005072900066EA 2005 7 29 ASOA05584 120050707A5320 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11832AS 7243 DURING A C-CHECK IN MCN, THE FS 718 LEFT FORWARD BRACKET, UPPER DOUBLER, WAS FOUND TO BE CRACKED IN THE RADIUS BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FS 178 LEFT FORWARD BRACKET, UPPER DOUBLER. (M) 2L72 4F RTA21EA 20050729000692005072900069EA 2005 7 29 ASOA05580 120050705A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA RT WING CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11832AS 7243 DURING A C-CHECK IN MCN, THE LOWER WING PLANK AT WS 148.019 RT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LOWER WING PLANK AT WS 148.019 RT IAW ASA EO 600-57-0134A. (M) 2L72 4F RTA21EA 20050729000702005072900070EA 2005 7 29 ASOA05581 120050705A5242 HANDLE CNDAIRCL600 CL6002B19 1900309EA E/E BAY DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11832AS 7243 DURING A C-CHECK IN MCN, THE AVIONICS BAY DOOR EXTERIOR HANDLE WAS FOUND CRACKED AROUND THE INTER BOSS. MAINTENANCE REMOVED AND REPLACED THE AVIONICS BAY DOOR HANDLE IAW SRM 51-42-06 AND 51-21. (M) 2L72 4F RTA21EA 20050729000712005072900071NM 2005 7 29 TAMF20050004O 120050727A5610141T4835507 WINDOW BOEING767 767200 1385120NM COCKPIT MALFUNCTIONED W TAMFA UNSCHED LANDING O OTHER CLCLIMB 1 SO23770QT 23802 AFTER TAKE OFF A HEAVY NOISE IN THE LEFT SLIDE WINDOW WAS HEARD WITH THE LATCH HANDLE IN LOCK POSITION. THE AIRPLANE RETURNED TO BOGOTA.NR 2 OPENABLE WINDOW WAS INSPECTED AND OPERATIONAL CHECK WAS PERFORMED IAW AMM 56-11-02 PAGE 601-604 WITH NORMAL RESULTS. OVERWEIGHT LANDING (NOT HARD LANDING) INSPECTION WAS PERFORMED IAW AMM 05-51-35 PAGE 202 (PHASE I INSPECTION, STEP A)AND NO DAMAGE WAS FOUND. THE AIRPLANE RETURNED TO COMMERCIAL OPERATION. 2L72 4F RTA1NM 20050729000752005072900075EU 2005 7 29 MALA050609 120050725A7120 BUSHING BAC 146 AVRO146RJ85A1500097EU ENGINE YOKE MIGRATED A MALAK NONE O OTHER ININSP/MAINT 1 GL15501XJ E2208 WHILE ACCOMPLISHING REPAIRS ON THE NR 4 PYLON, NOTED ENGINE YOKE BUSHINGS HAVE MIGRATED OUT. 2H74 4F RTA49EU 20050729000772005072900077EU 2005 7 29 MALA050606 120050725A5753 ACCESS PANEL SAAB SF340 340B 7860101EU TE FLAPS DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15370PX 340B300 LT FLAP ACCESS PANEL 541AT IS DENTED AND HAS BEEN REPAIRED IAW MESABA EO NR S57060. REF: EAMS WORK ORDER 212675 TASK 5504. 2L72 4T RTA52EU 20050729000792005072900079EU 2005 7 29 MALA050611 120050726A5320 FLOOR SUPPORT SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15370PX 340B300 FLOOR SUPPORT FLANGE IS CORRODED ON RT SIDE BETWEEN FS 272 AND FS 288. DAMAGE HAS BEEN REPAIRED IAW MESABA EO NR S53102. REF: EAMS WORK ORDER 212675, TASK 2525. 2L72 4T RTA52EU 20050729000802005072900080NE 2005 7 29 SF20050726 220050726A7200 ENGINE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE NR 1 MALFUNCTIONED A UHLAE ENGINE SHUTDOWN MJ OVER TEMP WARNING INDICATION NRNOT REPORTED 1 GL17121CQ 121 FLT 7539 IAD-DAY STARTED NR 1 ENGINE NORMALLY, AFTER TURNING ON NR 1 GENERATOR, LT ITT INCREASED TO 1068, MOTORED NR 1 ENGINE DOWN & SHUTOFF NR 1 GENERATOR. 2L72 4T4 TRTA52EU E8NE6 20050729000812005072900081NM 2005 7 29 AWXA200500854 120050706A53206545834107 STRAP BOEING737 7373G7 1384595NM FLOORBEAM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 DURING C16 CHECK DISCOVERED 2 CRACKS, .500 INCHES LONG ON STABILIZER STRAP LOCATED AT THE BOTTOM OF BS 328 FLOORBEAM AT BL 11L, WL 200. MAINTENANCE STOP DRILLED CRACKS ON STRAP AT BS 328, BL 11L, WL 200 IAW BOEING 737-300 SRM 53-10-51-2 FIG 204. FABRICATED REPAIR PLATE IAW BOEING 737-300 SRM 53-10-51-2 FIG 204. INSTALLED FABRICATED REPAIR PARTS AT BS 328, BL 11L, WL 200 IAW BOEING 737-300 SRM 53-10-51-2 FIG 204. 2L72 4F RTA16WE 20050729000822005072900082NM 2005 7 29 AWXA200500855 120050707A57536546431280 SKIN BOEING737 7373G7 1384595NM FORE FLAP DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 DURING C16 CHECK DISCOVERED DISBOND AREA ON THE BOTTOM SURFACE OF THE RT OUTBOARD FORE FLAP, 87 INCHES FROM OUTBOARD END. MAINTENANCE REMOVED AND CLEANED THE DISBOND AREA ON THE BOTTOM OF THE RT OUTBOARD FORE FLAP IAW BOEING 737-300 SRM 51-70-10-0. FABRICATED FILLER AND DOUBLER IAW BOEING 737-300 SRM 51-70-10-0. BONDED AND SEALED FABRICATED REPAIR PARTS TO THE BOTTOM SURFACE OF THE RT OUTBOARD FLAP IAW BOEING 737-300 SRM 51-70-10-0. 2L72 4F RTA16WE 20050729000832005072900083NM 2005 7 29 AWXA200500856 120050701A57536546435277 SKIN BOEING737 7373G7 1384595NM ZONE 500 - LEFT DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 DURING C16 CHECK DISCOVERED DELAMINATED AREA ON THE BOTTOM SURFACE OF THE LEFT OUTBOARD AFT FLAP, APPROXIMATELY 20 INCHES FROM INBOARD END AND 6 INCHES FROM THE TRAILING EDGE. MAINTENANCE REMOVED AND CLEANED DELAMINATED AREA FROM THE BOTTOM SURFACE OF THE LEFT OUTBOARD AFT FLAP, APPROXIMATELY 20 INCHES FROM INBOARD END AND 6 INCHES FROM THE TRAILING EDGE IAW BOEING 737-300 SRM 51-70-10-0. FABRICATED FILLER AND DOUBLER IAW BOEING 737-300 SRM 51-70-10-0. BONDED AND SEALED FABRICATED REPAIR PARTS TO THE BOTTOM SURFACE OF THE L/H OUTBOARD AFT FLAP APPROXIMATELY 20 INCHES FROM INBOARD END IAW BOEING 737-300 SRM 51-70-10-0. 2L72 4F RTA16WE 20050729000842005072900084NM 2005 7 29 AWXA200500857 120050708A5322654583311 SHEAR TIE BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED SHEAR TIE CRACKED 1.1 INCHES IN LENGTH AT STA 196.5, WL 207, BL 28R. MAINTENANCE REMOVED CRACKED SHEAR TIE FROM STA 196.5, WL 207, BL 28R IAW BOEING 737-300 SRM 51-40-02-0. FABRICATED NEW SHEAR TIE IAW BOEING 737-300 SRM 51-30-01-0 AND BAC DWG 65-45833. INSTALLED FABRICATED REPAIR PARTS AT STA 196.5, WL 207, BL 28R IAW BOEING 737-300 SRM 51-40-02-0 FIGS 8 AND 12. 2L72 4F RTA16WE 20050729000852005072900085NM 2005 7 29 AWXA200500858 120050708A5320654583311 SHEAR TIE BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 DURING C16 CHECK DISCOVERED SHEAR TIE CRACKED, 1.2 INCHES IN LENGTH, AT STA 196.5, WL 207, BL 28L. MAINTENANCE REMOVED CRACKED SHEAR TIE AT STA 196.5, WL 207, BL 28L IAW BOEING 737-300 SRM 51-40-02-0. FABRICATED REPLACEMENT SHEAR TIE IAW BOEING 737-300 SRM 51-40-05-0 AND BAC DWG 65-45833. INSTALLED FABRICATED REPAIR PARTS AT STA 196.5, WL 207, BL 28L IAW BOEING 737-300 SRM 51-40-02-0 FIGS 8 AND 12. 2L72 4F RTA16WE 20050729000872005072900087NM 2005 7 29 AWXA200500860 120050703A575465C26601127 SKIN BOEING737 7373G7 1384595NM ZONE 500 - LEFT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 DURING C16 CHECK DISCOVERED A CRACK, .9 INCHES IN LENGTH, ON THE BOTTOM OF THE NR 1 SLAT LOWER SKIN, BELOW CENTER AUXILIARY TRACK, AT SS 339. MAINTENANCE REMOVED THE DAMAGED PART OF SKIN FROM THE BOTTOM OF THE NR 1 SLAT LOWER SKIN AT SS 339 IAW BOEING 737-300 SRM 57-43-01-2. FABRICATED FILLER AND SPLICE PLATE IAW BOEING 737-300 SRM 57-43-01-2. INSTALLED FABRICATED REPAIR PARTS AT BOTTOM OF THE NR 1 SLAT LOWER SKIN, BELOW CENTER AUXILIARY TRACK, AT SS 339 IAW BOEING 737-300 SRM 57-43-01-2. 2L72 4F RTA16WE 20050729000942005072900094SW 2005 7 29 ALGA104923 120050722A6400406012108107 PITCH HORN BELL 407 407 1182206SW TAIL ROTOR CORRODED B ALGAK NONE O OTHER ININSP/MAINT 1 SW03557AL2469 53243 EXCESSIVE PITTING FROM CORROSION BEYOND LIMITS / INSTALLED 2EA NEW PITCH HORNS BY OVERHAUL SHOP. 1G71 3U O H2SW 20050729000972005072900097GL 2005 7 29 YTRR104953 220050725A753223053176 BLEED VALVE BELL 206 206B3 1181506SW ALLSN 250C 250C20B 03013GL ENGINE DEFECTIVE B YTRAO OTHER O OTHER NRNOT REPORTED 1 SW03255RA 2255 ENGINE POWER TREND CHECK GOING DOWN ON CHART. REPLACED BLEED-VALVE ON ENGINE. 1G71 3U3 U H2SW E4CE 20050729000992005072900099SW 2005 7 29 YTRR104956 120050725A282122366621103 FUEL FILTER BELL 206 206L1 1182107SW ALLSN 250C 250C28 03013GL FUEL SYSTEM CRACKED B YTRAO OTHER O OTHER NRNOT REPORTED 1 SW03397RL 45397 FILTER HEAD WEBBING INSIDE WAS CRACKED. REPLACED FILTER HEAD ASSY. 1G71 3U3 U H2SW E1GL 20050729001002005072900100EA 2005 7 29 A6WA200540238 120050713A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31409AW 7447 LT SIDE FS 484 INTERCOSTAL IS CRACKED AT LBL 36. CRACK IS APPROX 1.1 INCH LONG. REPAIRED LT SIDE FS 484 INTERCOSTAL AT LBL 36 IAW MFGREO. (K) 2L72 4F4 FRTA21EA E15NE 20050729001032005072900103EA 2005 7 29 ASOA05591 120050711A2560 LAMP CNDAIRCL600 CL6002B19 1900309EA FLASHLIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11875AS 7559 DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY FLASHLIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY FLASHLIGHT. OPERATIONAL CHECKS GOOD. (M) 2L72 4F RTA21EA 20050729001042005072900104WP 2005 7 29 ARWA20050703 120050724A2910 LINE DOUG DC10 DC1030 3023501WP HYD SYSTEM LEAKING A ARWAO OTHER K FLUID LOSS CRCRUISE 1 SO19526MD 46998 FOUND HYDRAULIC LINE LEAKING; LOCATED ON TOP OF RIGHT LANDING GEAR WHEEL WELL. REPAIRED HYDRAULIC LINE IN ACCORDANCE WITH DC-10 M/M 20-10-01. NO LEAKS FOUND IN ACCORDANCE WITH DC-10 M/M 29-00-00 2L73 4F A22WE 20050729001052005072900105SW 2005 7 29 ALGA104871 120050717A6220406310405101 PITCH LINK BELL 407 407 1182206SW MAIN ROTOR BINDING B ALGAK NONE O OTHER ININSP/MAINT 1 SW036386Z568 53381 BINDING, RATCHETY, AND AXIAL PLAY BEYOND MAX/REPLACED WITH NEW BY FIELD MAINTENANCE 1G71 3U O H2SW 20050729001082005072900108EA 2005 7 29 ASOA05572 120050630A5610 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT BIRD STRIKE A ASOAO OTHER F FLT CONT AFFECTED DEDESCENT 1 SO11865AS 7507 DURING TAKEOFF FROM SHV-CVG, THE AIRCRAFT EXPERIENCED A BIRD STRIKE ON THE FIRST OFFICERS WINDSHIELD WITH NO KNOWN PROBLEMS OCCURRING. DURING DESCENT INTO CVG, THE CREW NOTICED SPORADIC UNCOMMANDED FLIGHT CONTROL DEFLECTIONS WITH O WITHOUT THE AUTO PILOT ENGAGED. NO RUDDER PEDAL DEFLECTION WAS NOTED. THE TOWER DECLARED AN EMERGENCY AND THE AIRCRAFT LANDED SAFELY IN CVG. MAINTENANCE REMOVED AND REPLACED THE NR 1 ACTUATOR LINEAR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050729001092005072900109EA 2005 7 29 ASOA05567 120050630A2120 ODOR CNDAIRCL600 CL6002B19 1900309EA CABIN DETECTED A ASOAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 SO11672BR 7594 FLT 4570 - DURING CRUISE FROM YUL-ATL, AT APPROX 32,000 FEET, THE CREW NOTICED A VERY STRONG BURNING ODOR IN THE COCKPIT WHICH CONTINUED APPROXIMATELY THREE TO FIVE MINUTES AND DISSIPATED. NO VISIBLE SIGNS O SMOKE WERE EVER PRESENT. THIS WAS SUBSEQUENTLY FOLLOWED BY AN INTERMITTENT STALL FAIL CAUTION WHICH WENT AWAY. THE AIRCRAFT LANDED SAFELY IN ATL. WHILE ON THE GROUND PROX SYSTEM FAIL STATUS MESSAGE WAS RECEIVED. MAINTENANCE RAN THE PACKS WITH NO VISIBLE SIGNS OF SMOKE OR ODORS. THE STALL SYSTEM OPERATIONAL CHECKS WERE GOOD. MAINTENANCE ALSO REMOVED AND REPLACED THE PS11MB PROXIMITY SWITCH ON THE SERVICE DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050729001102005072900110EA 2005 7 29 ASOA05575 120050701A5210601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11871AS 7537 DURING HANGAR MAINTENANCE IN MCN, THE BOTTOM STEP ON PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20050729001112005072900111EA 2005 7 29 ASOA05571 120050624A5330 DOUBLER CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11906EV 7642 DURING A C-CHECK IN HOT, THE RT FS 718 DOUBLER WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RT FS 718 DOUBLER IAW SRM 51-42-06 AND BOMBARDIER SERVICE BULLETIN 601R-53-055. (M) 2L72 4F RTA21EA 20050729001132005072900113EA 2005 7 29 ASOA05577 120050704A5210601R3170767 STEP CNDAIRCL600 CL6002C10 1390015EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11755EV 10185 DURING AN A-CHECK IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ASSEMBLY ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20050729001172005072900117EA 2005 7 29 ASOA05573 120050630A3244 TIRE CNDAIRCL600 CL6002B19 1900309EA MLG FAILED A ASOAA UNSCHED LANDING O OTHER CLCLIMB 1 SO11907EV 7648 FLT 4456 - DURING CLIMB-OUT FROM ATL-ICT, THE TOWER ADVISED THE CREW THAT TIRE DEBRIS WERE FOUND ON THE RUNWAY FOLLOWING THEIR TAKEOFF. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO ATL AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED BOTH RIGHT MAIN LANDING GEAR (MLG) WHEEL ASSEMBLIES AND THE RIGHT INBOARD MAIN FLAP ASSEMBLY. MAINTENANCE ALSO BOROSCOPED THE RIGHT ENGINE FOR POSSIBLE FOD. NO SIGNS OF ANY FOD WAS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050729001182005072900118EA 2005 7 29 ASOA05570 120050623A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11906EV 7642 DURING A C-CHECK IN HOT, THE LT OUTBOARD FS 280 CLIP WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LT OUTBOARD FS 280 CLIPS IAW SRM 51-42-06, 51-42-21 AND 51-42-136. (M) 2L72 4F RTA21EA 20050729001202005072900120EU 2005 7 29 DHL2005362007 120050713A5242 DOOR AIRBUS300 A300B4203 3930306EU E/E BAY UNSECURE A DHLAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CRCRUISE 1 SO01362DH 84 THE DOORS LIGHT ON THE MWP ILLUMINATED IN FLIGHT. THE FWD COMPT LIGHT WAS OBSERVED ILLUMINATED ON THE SECOND OFFICERS DOORS PANEL. FOUND LT AVIONICS ACCESS DOOR AJAR. SECURED DOOR. OPS CKS GOOD IAW MM 52-71-00 2L72 4F RTA35EU 20050729001212005072900121NM 2005 7 29 07260501 120050725A21317638101 CONTROLLER BOEING727 7272F9 138407DNM CABIN PRESSURE MISOVERHAULED A PCSAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 SO29199AJ 21426 FLIGHT 711 KMIA/MMMX, DURING CLIMB AUTO PRESSURIZATION FAILED, WENT TO STANDBY, OUTFLOW VALVE WENT FULL OPEN. UNABLE TO HOLD CABIN PRESSURE IN MANUAL AC OR DC. AIRCRAFT RETURNED TO KMIA AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND CABIN PRESSURE CONTROLLER SENSE PORTS CAPPED. REMOVED CAPS AND PERFORMED OPS CHECK PER "B" CHECK WORK CARD 7-29 AND B-727 MM 21-30-0. AIRCRAFT RETUNED TO SERVICE. 2L73 4F RTA3WE 20050729001232005072900123CE 2005 7 29 DXTA200500868 120050727A3297M24308215F PIN CESSNA500 560CESSNA 2076750CE MLG BROKEN E DXTAO OTHER J WARNING INDICATION LDLANDING 1 GL07320QS 5600321 ANIT-SKID INOP LIGHT ILLUMINATED IN FLIGHT AS GEAR RETRACTED, EMERGENCY BRAKES USED ON LANDING. FOUND ONE BROKEN PIN, THE CONNECTOR CORRODED ON THE BITE BOX. REPINNED NEW CONNECTOR WIRE FOR WIRE FROM OLD CONNECTOR TO NEW CONNECTOR. OPERATIONAL CHECK OF ANTI-SKID SYSTEM SATISFACTORY. IAW MODEL 560 M.M. 32-42-00. 2L72 4F RTA22CE 20050729001252005072900125EA 2005 7 29 ASOA05565 120050629A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11847AS 7335 DURING A GROUND INSPECTION IN CAE, THE AFT EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE AFT EMERGENCY CEILING LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050729001262005072900126EA 2005 7 29 ASOA05562 120050628A3397M2275935229 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11830AS 7236 DURING A C-CHECK IN MCN, THE FORWARD EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE REPAIRED BROKEN WIRE ON THE FORWARD OVERHEAD CURVED EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. (M) 2L72 4F RTA21EA 20050729001272005072900127EA 2005 7 29 ASOA05563 120050628A5210601R3167013 STEP CNDAIRCL600 CL6002C10 1390015EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11723EV 10132 DURING A C-CHECK IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE BOTTOM STEP ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20050729001282005072900128EA 2005 7 29 ASOA05561 120050628A5210601R3198045 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11830AS 7236 DURING A C-CHECK IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. (M) 2L72 4F RTA21EA 20050729001292005072900129NE 2005 7 29 C7WA200500109 220050712A7261479175 CONNECTOR BOEING727 7272M7 138407SNM PWA JT8 JT8D15 52051NE NR 2 ENGINE LOOSE A C7WAO OTHER K FLUID LOSS NRNOT REPORTED 1 SO17742RW 21952 688220 AIR TURNBACK; ENGINE SHUTDOWN, NR 2 EGT FLUCTUATES AT FLIGHT LEVEL 27,000. OIL PRESSURE DROPPED TO ZERO, OIL QUANTITY FOLLOWED TO ZERO. DURING INSPECTION OF NR 2 ENGINE FOUND INLET CASE TUBE CONNECTOR ASSEMBLY LOOSE AND LEAKING. TIGHTENED LOOSE BOLTS. LEAK CHECK GOOD MM. EGT OPERATIONAL CHECK GOOD MM. (K) 2L73 4F4 F A3WE E2EA 20050729001312005072900131EA 2005 7 29 ASOA05564 120050629A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11832AS 7243 DURING HANGAR MAINTENANCE IN BTR, THE RIGHT AFT MOST EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE RIGHT AFT MOST EXTERIOR EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. (M) 2L72 4F RTA21EA 20050729001332005072900133CE 2005 7 29 AOQ2005F00002 120050616A770030710272 GASKET LEAR 35 31A 5170531CE GARRTTTFE731TFE73123B WP N1 MONOPOLE WORN E AOQAK NONE J WARNING INDICATION CLCLIMB 1 EA1139TW 4133 047 P99204 DURING CLIMB, AT ALTITUDE, THE NR 2 ENGINE FIRE WARNING ILLUMINATED, ITT INDICATED 801 DEGREES, WARNING CEASED WITHIN 10 SECONDS AFTER THRUST WAS REDUCED BELOW 780 DEGREES ITT. ALL ENGINE INDICATIONS WERE NORMAL. MAINTENANCE TROUBLESHOT NR 2 ENGINE FIRE WARNING LIGHT ILLUMINATION TO A LEAKING N1 MONOPOLE GASKET. MAINTENANCE REPLACED MONOPOLE GASKET. A SATISFACTORY OPERATIONAL AND LEAK TET WAS CONDUCTED AND THE AIRCRAFT WAS RTS. (K) 2L72 4F4 FRTA10CE E6WE 20050729001372005072900137EA 2005 7 29 ASOA05560 120050626A3260173401 UPLOCK ROLLER CNDAIRCL600 CL6002B19 1900309EA NLG FROZEN A ASOAO OTHER J WARNING INDICATION DEDESCENT 1 SO11829AS3940 7232 DURING A DESCENT INTO BTR FROM CVG, UPON SELECTING GEAR DOWN THE NOSE WHEEL WAS SLOW TO DEPLOY AND RED INDICATIONS WITH A MASTER WARNING AND A GEAR DISAGREE ORAL WARNING WERE RECEIVED. THE AIRCRAFT PERFORMED A GO AROUND TO COMPLY WITH THE QRH. INITIAL ATTEMPTS TO EXTEND THE GEAR MANUALLY WERE UNSUCCESSFUL. UPON REMOVING THE HYDRAULIC PRESSURE FROM SYSTEM NR 3 THE GEAR EXTENDED. DURING ROLLOUT, THE NOSE WHEEL STEERING WAS LOST. THE AIRCRAFT WAS TOWED TO THE GATE SAFELY. UPON INSPECTION MAINTENANCE FOUND THE UPLOCK ROLLER FROZEN AND ADJUSTED THE ROLLER. MAINTENANCE ALSO REMOVED AND REPLACED THE NOSE LANDING GEAR (NLG) SELECTOR VALVE. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050801000022005080100002NM 2005 8 1 DHL2005754005 120050729A2741 WARNING HORN BOEING727 727223 1384074NM STAB TRIM ACTIVATED A DHLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01754DH 22008 T/O WARNING HORN SOUNDS WITH STAB TRIM SET AT 2.6 ON CAPT SIDE F/O STAB TRIM INDICATES .5 HIGHER THAN CAPTAIN`S SIDE. CHECKED STAB TAKEOFF WARNING SWITCHES IAW M/M 31-26-24, CHECKED NOSE- UP AND NOSE DOWN STAB JACKSCREW DIMENSION, CHECKED STAB TRIM POSITION IND. IAW B727 M/M 27-40-0 NO DEFECTS NOTED. 2L73 4F A3WE 20050801000052005080100005WP 2005 8 1 UPS05844979 120050628A53403779659U501 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE: C1, MAIN CABIN STA 900 LONGERON 3L FITTING CRACKED APPROX. 4 INCHES. REMOVED AND REPLACED LONGERON FITTING IAW DC-8 SRM 51-1-20D AND 51-1-2 1. 2L74 4F RT4A25 20050801000072005080100007WP 2005 8 1 UPS05844981 120050702A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE:C1 RH WING UPPER AFT SKIN PANEL AT XCW 69.500 CRACKED 1 INCH LONG. CUT OUT DAMAGE,FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-02-01 FIG. 20. 2L74 4F RT4A25 20050801000092005080100009WP 2005 8 1 UPS05844983 120050701A5310 FINGER DOUBLER DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE: C1, COCKPIT SUBFLOOR STA -32 TO -12 RBL 48 FINGER DOUBLER HAS SEVERAL SHEA R HEAD FASTENERS AND POSSIBLE CORROSION. REMOVED FINGER DOUBLER, CORROSION ON FINGER DOUBLER FOUND OUT OF LIMIT S, FABRICATED, AND INSTALLED REPLACEMENT FINGER DOUBLER IAW DC-8 SRM 5 1-1-21 AND DWG SRO8530026. 2L74 4F RT4A25 20050801000102005080100010WP 2005 8 1 UPS05844984 120050701A5310 FINGER DOUBLER DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE: C1, COCKPIT SUBFLOOR AT STA -32 TO -52 RBL 60 FINGER DOUBLER CORRODED. REMOVED FINGER DOUBLER, CORROSION FOUND OUT OF LIMITS, FABRICATED, AND INSTALLED REPLACEMENT FINGER DOUBLER IAW DWG 5612298 AND DC-8 SRM 51- 1-20D AND 51-1-15. 2L74 4F RT4A25 20050801000122005080100012WP 2005 8 1 UPS05844986 120050720A33505708458503 BATTERY PACK DOUG DC8 DC871F 302199DWP EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 DURING LIGHT CK EMERGENCY EXIT LIGHT BY FWD ENTRY DOOR DID NOT COME ON. PEANUT LIGHT UNDER FRONT INSTRUMENTS DO NOT COME ON AS WELL. REPLACED BATTERY PACK/ RELAY UNIT IAW MM SEC 33-50-01. OPS CHK GOOD. 2L74 4F RT4A25 20050801000152005080100015EU 2005 8 1 05FDEA02119 120050727A5753 FLAP TRACK AIRBUS300 A300F4605R 3930327EU LT T/E FLAP DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25656FE 745 LT WING OB TE FLAP LE HAS DENT BET TRACKS NR 5. 2L72 4F RTA35EU 20050801000172005080100017EU 2005 8 1 05FDEA02121 120050727A5321 FLOOR PANEL AIRBUS300 A300F4605R 3930327EU CARGO BAY CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25670FE 777 MAIN DECK FLOOR PANEL 232CF CRACKED. 2L72 4F RTA35EU 20050801000182005080100018EU 2005 8 1 05FDEA02122 120050727A5321 FLOOR PANEL AIRBUS300 A300F4605R 3930327EU CARGO BAY CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25670FE 777 MAIN DECK FLOOR PANEL 232CF CRACKED. 2L72 4F RTA35EU 20050727000522005072700052NM 2005 7 27 USAA050833 120050705A5320 ANGLE BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU 23861 CLT - FOUND TRANSITION ANGLE CORRODED 8 INCHES, IN AFT CARGO BETWEEN STATION 727C AND STATION 827. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-10-02. (M) 2L72 4F RTA16WE 20050727000612005072700061WP 2005 7 27 DHL2005802508 120050705A53204758514512 FITTING DOUG DC8 DC873 302199CWP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH84803 46076 AFT CARGO COMPT. INTERCOSTAL FITTING 2.000 CRACK STA 1300.000 L-33R. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG. 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG. 9. TORQUED IAW SRM 51-3-1 PG. 2A. 2L74 4F RT4A25 20050727000642005072700064SO 2005 7 27 GUU2005F00034 120050628A33500L3071BPEGPL LAMP EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE EMERGENCY LIGHT INOPERATIVE A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO17268AS 120202 EMERGENCY FLOOR ESCAPE LIGHTS INOPERATIVE IN FRONT OF GALLEY, ROW 3A AND 6A. REPLACED LAMPS AT ROW 3A AND 6A AND SECURED LOOSE WIRE AT FUSE. (K) 2L72 4T4 TRTA31SO E20NE 20050727000652005072700065WP 2005 7 27 DHL2005802513 120050706A5313 LONGERON DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH84803 46076 FWD CARGO COMPT CROSS SLIDE DOOR AREA L-35L CRACKED STA 280.000-300.000 MAJOR REPAIR. CORR.: PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG. 1B. REMOVED FASTENERS IAW SRM 51-1-20D PG. 21. PERFORMED STOP HOLE IAW SRM 53-2-0 FIG. 1B (SHEET 3). PERFORMED NDT INSPECTION IAW DC8 NDT PART 06-10-01-001. FABRICATED ANGLE DOUBLER IAW SRM 53-2-0 FIG. 1B (SHEET 3) SRM 53-4-1 FIG. 28. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG. 9. INSTALLED ANGLE DOUBLER IAW SRM 53-2-0 FIG. 1B SHEET 3, SRM 51-1-20D PG. 9. TORQUED IAW SRM 51-3-1 PG. 2A. 2L74 4F RT4A25 20050727000682005072700068WP 2005 7 27 DHL2005802520 120050715A53204772397U1 FITTING DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH84803 46076 FUSELAGE TAIL SECTION L-17R FITTING CRACKED 0.250 STA 1766.000-1782.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21, SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9, SRM 561-1-21 PG 1, SRM 51-3-0, SRM 51-1-23. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050727000782005072700078EU 2005 7 27 1308061705 220050617A753239889631 BLEED VALVE GULSTMG1159 GIV 3980115SO RROYCETAY TAY6118 EU ENGINE MALFUNCTIONED E N93AK NONE O OTHER CLCLIMB 1 SO13408QS7674 1308 ON CLIMB AUTO THROTTLES VARY EPR +/- .04 FROM TARGET EPR 2L72 4F4 FRTA12EA E25NE 20050727000932005072700093CE 2005 7 27 K2A2005F00000 120050224A5280458100903 DOOR BEECH 58 58 1152740CE CONT O520 IO520* 17032SO HARTZLHCJ3Y PHCJ3YF1 GL MLG BROKEN E K2AAO OTHER O OTHER NRNOT REPORTED 1 WP13300TH TH266 IT APPEARS THE AFT HINGE ON THE LT INNER GEAR DOOR BROKE FIRST AND WHEN THE GEAR WAS SELECTED THE DOOR JAMMED THE LT GEAR AND STRESSED THE BRAZE ASSY WHICH BROKE THE GEAR ACTUATOR ARM. THE GEAR DOOR HINGES SHOULD BE EXAMINED FRO CRACKS AND CORROSION REGULARLY AS THIS CRACK SEEMS TO HAVE BEEN DEVELOPING FOR SOME TIME. (K) 1L72 3O3 O 3A16 E5CE 5 CP36EA 20050727000942005072700094EA 2005 7 27 YAX2005F00001 220050711A7314RG17980 PUMP PIPER PA32 PA32300 7103212SO LYC O540 IO540K1A5 41532EA HARTZLHCC2Y HCC2YK1 GL FUEL SYSTEM FLUCTUATES E YAXAO OTHER O OTHER NRNOT REPORTED 1 AL058991N 1273 3240874 L1642048A CH35655B FUEL FLOW FLUCUATION AND SURGING. SOME CASES ENGINE QUITING. (K) 1L71 3O3 O A3SO 1E4 5 CP920 20050727000992005072700099SO 2005 7 27 C2XA05SH080 120050721A533014520571001 SKIN PANEL EMB 145 EMB145EP 3260221SO FUSELAGE LIGHTNING STRIKEA C2XAK NONE O OTHER ININSP/MAINT 1 SW2714943 145040 SHV-DURING C-CHECK MAINTENANCE FOUND LIGHTENING STRIKE AT FRAMES 21-22, STR 18R. MAINTENANCE REPAIRED LIGHTENING STRIKES AT FRAMES 21-22, STR 18R I/A/W EC 5330-01480, REPAIR FIGURE NR 2. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050727001062005072700106SO 2005 7 27 C2XA05SH087 120050721A551012007254607 HINGE EMB 145 EMB145EP 3260221SO RUDDER CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714943 145040 SHV-DURING C-CHECK MAINTENANCE FOUND RUDDER II UPPER MIDDLE ATTACHMENT BRACKET CRACKED. MAINTENANCE REMOVED AND REPLACED RUDDER II UPPER MIDDLE ATTACHMENT BRACKET (HINGE FITTING) I/A/W EC 5540-01028. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050727001082005072700108SO 2005 7 27 C2XA05SH089 120050525A554012007255605 FITTING EMB 135 EMB135LR 3260305SO RUDDER WORN A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717524 145399 SHV C-CHECK RUDDER NR 2 UPPER HINGE BRACKET IS WORN. MAINTENANCE REMOVED AND REPLACED RUDDER NR 2 UPPER HINGE BRACKET IAW EC 5540-01028.THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2L72 4F RTT00011AT 20050727001092005072700109SO 2005 7 27 C2XA05SH90 120050727A532014530642401 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717524 145399 SHV DURING C-CHECK LT OMEGA BEAM AT FR 24 ARE CORROED. MAINTENANCE REPAIRED LT OMEGA BEAM IAW EMB 145 SRM 53-22-10.THE AIRCRAFT WAS APPROVE TO RETURN FOR SERVICE. 2L72 4F RTT00011AT 20050727001122005072700112SO 2005 7 27 C2XA05SH071 120050717A491014526850401 FIREWALL EMB 145 EMB145EP 3260221SO AFT APU CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714943 145040 SHV-DURING C-CHECK APU FIREWALL HAS MULTIPLE CRACKS (4) AROUND RIVETS. MAINTENANCE STOP DRILL CRACKS PER SRM 51-10-02 AND INSTALL DOUBLER SIZE TO ENCOMPASS CRACKS USING PRINCIPLES DESCRIBE IN SRM 53-32-12 ITEM 6 AND USING EC 5330-01473.THE AIRCRAFT WAS APPROVE FOR RETURN TO SERVICE 2L72 4F RTT00011AT 20050727001232005072700123SO 2005 7 27 C2XA05SH079 120050721A533014520571001 SKIN PANEL EMB 145 EMB145EP 3260221SO FUSELAGE LIGHTNING STRIKEA C2XAK NONE O OTHER ININSP/MAINT 1 SW2714943 145040 SHV-DURING C-CHECK MAINTENANCE FOUND LIGHTENING STRIKES AT FRAME 13, STRS 19R - 20R. MAINTENANCE REPAIRED LIGHTENING STRIKES AT FRAME 13, STRS 19R-20R IAW EC 5330-01480, REPAIR FIGURE 3. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050727001322005072700132NE 2005 7 27 ALG2005F00044 120050711A261230326E7 AMPLIFIER SKRSKYS76 S76 8143010NE ALLSN 250C 250C30 03013GL FIRE DETECTOR MALFUNCTIONED E ALGAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SW03702AL 760243 PRIOR TO TAKEOFF THE PILOT NOTICED NR 1 ENGINE FIRE LIGHT AND TONE ACTIVATED. AFTER SHUTDOWN, PASSENGERS WERE EVACUATED AND THE PILOT AND COPILOT VISUALLY CHECKED ENGINE COMPARTMENTS, NO SIGN OF FIRE WAS DETECTED. MAINTENANCE WAS NOTIFIED. TROUBLESHOOTING REVEALED THAT NR 1 ENGINE FIRE DETECTOR AMPLIFIER HAS MALFUNCTIONED. THE MECHANIC REMOVED AND REPLACED NR 1 ENGINE FIRE DETECTOR AMPLIFIER AND AIRCRAFT RETURNED TO SERVICE. (K) 1G72 3U3 U H1NE E1GL 20050727001352005072700135SO 2005 7 27 C2XA05SD022 120050613A2560P2070011120 FLASHLIGHT EMB 145 EMB145ER 3260211SO CABIN BROKEN A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714943 145040 FO'S FLASHLIGHT BROKEN. REPLACED BROKEN FLASHLIGHT OPS CHECK GOOD AIRCRAFT RELEASED AND RETURNED TO SERVICE 2L72 4F RTT00011AT 20050727001422005072700142SO 2005 7 27 C2XA05CL055 120050629A3350P4010030 BATTERY EMB 145 EMB145LR 3260212SO COCKPIT DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712552 145583 DURING ROUTINE MAINTENANCE THE FIRST OFFICER'S EMERGENCY FLASHLIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE BATTERY. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20050727001462005072700146GL 2005 7 27 ALG2005F00042 220050711A7421CH34187A IGNITER BELL 206 206L4 1182110SW ALLSN 250C 250C30 03013GL ENGINE INOPERATIVE E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03188AL 52082 DURING START, THE ENGINE FLAMED OUT. SECOND ATTEMPT WAS UNSUCCESSFUL. UPON INSPECTION, THE MECHANIC REMOVED AND REPLACED THE IGNITER PLUG AND THE AC WAS RETURNED TO SERVICE. (K) 1G71 3U3 UNCH2SW E1GL 20050727001552005072700155NE 2005 7 27 RAIA00507015 220050722A73206945059010 SENSOR JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114GR 01514NE TOTAL TEMP MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03563HK 41079 FLT # 3663- RIC- LEFT HAND IEC FAULT. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND TT2 SENSOR AND PERFORMED AN ENGINE RUN. OPS CHECKED GOOD. 2L72 4T4 TRTA41NM E18NE 20050727001792005072700179WP 2005 7 27 UPS05844968 120050707A534037797926501 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE:C1 STA 675 L3L SPLICE FITTING CRACKED. REMOVED AND REPLACED SPLICE FITTING AT STA 675 L3L IAW SRM 51-1-20D AND 51-3-0 2L74 4F RT4A25 20050727001832005072700183WP 2005 7 27 UPS05844973 120050711A5320 FINGER DOUBLER DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C1, FINGER DOUBLER BLOWN OUT COCKPIT SUBFLOOR AT STA -12 T0-32R REMOVED CORRODED FINGER DOUBLER IAW SRM51-1-21, FABRICATED REPLACEMENT FIGER DOUBLER AND INSTALLED IAW SRM53-03-03AND SRM 53-2-0 FIG 1F 2L74 4F RT4A25 20050728000092005072800009CE 2005 7 28 DXTA200500865 120050725A2910 HYDRAULIC SYSTEM CESSNA750 750 2076810CE B-SYSTEM LEAKING E DXTAC ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 GL07987QS 7500087 WHILE WAITING FOR CLEARANCE FOR T/O, SMELLED A VERY BAD ODOR FOLLOWED BY THE HYD PRESS B LOW AND THE HYD PUMP B-SYSTEM FAIL, THEN THE RUDDER STANBY SYSTEM FAIL LIGHT. LEAKING APPEARED TO COMING FROM THE PYLON AREA. ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20050728000132005072800013CE 2005 7 28 DXTA200500863 120050725A3230 DOWNLOCK SWITCH CESSNA560 560XL 2076702CE MLG OUT OF RIG E DXTAO OTHER J WARNING INDICATION APAPPROACH 1 GL07639QS 5605139 ON APPROACH LOWERED GEAR LT MAIN LIGHT WAS FLICKERING, UNSAFE LIGHT FLICKERING ALSO. DID GO AROUND RAISED GEAR. LOWERED GEAR 2ND TIME SAME INDICATION. BLEW GEAR DOWN PER CHECKLIST. FLICKER LIGHTS DID NOT STOP UNTIL LANDING GEAR WENT TO SAFE INDICATIONS. PERFORMED GEAR SWING OP'S CK. DUPLICATED DISCREPANCY REMOVED AND REPLACED LT DOWNLOCK SWITCH. PERFORMED SWITCH RIGGING AND NUMEROUS GEAR SWING OP'S CKS. OP'S CK GOOD AT THIS TIME. WORK REF 560XL MM 32-01-00 AND 32-60-01. 2L72 4F RTA22CE 20050728000202005072800020EU 2005 7 28 AWXA200500852 120050724A2597 WIRE HARNESS AIRBUS320 A320232 3930326EU L1 DOOR SLIDE DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28659AW36061762 1166 DURING EMERGENCY LIGHT OPERATIONAL CHECK, THE FORWARD LEFT EPSU FAULTED EXTERNAL LIGHT. MAINTENANCE REMOVED AND REPLACED THE L1 SLIDE IAW AMERICA WEST AIRLINES TASK CARD R1C25305. FOUND LAMP HARNESS DAMAGED. LAMP HARNESS WAS REPLACED IAW CMM 53-60-56 REV. 11. 2L72 4F RTA28NM 20050728000252005072800025WP 2005 7 28 DHL2005806001 120050727A2910NAS1611213 O-RING DOUG DC8 DC873F 302199FWP HYD SYSTEM LEAKING A DHLAB EMER. DESCENT KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 SO01806DH 46002 DURING CLIMB OUT,HYD PRESS DROPPED TO ZERO AND HYD QTY DROPPED TO AUX LEVEL. DURING ABN PROC SYSTEM LEVEL DROPPED WELL BELLOW AUX LEVEL WHEN CONFIGURING TO LAND. FOUND WING SLOT CNTL VALVE IN R. W/W LEAKING AT RETAINING PLUG/STUD. R & R UPPER AND LOWER O-RINGS & PACKING. SLOT CONTROL VALVE INSTALLED IAW MM 27-80-4. OPS AND LEAK CHECK OK. SERVICED HYD SYS. GRND RAN, BLED ALL SYS, ALL OPS. 2L74 4F RT4A25 20050728000262005072800026NM 2005 7 28 P9RA20050095 120050718A2750 FLAP SYSTEM BOEING727 727231 1384079NM TE FLAPS OUT OF ADJUST A P9RAO OTHER E VIBRATION/BUFFET DEDESCENT 1 SO1154344 21631 DURING DESCENT BACK INTO SFB, CREW NOTED VIBRATION IN AIRCRAFT ABOVE 270KIAS. LOW FREQUENCY VIBRATION. SUSPECT RIGHT FLAP AREA. MAINTENANCE ADJUSTED RIGHT INBD. FLAP IAW M/M. OPS CHECKED GOOD. NOTE. NO FURTHER VIBRATION NOTED AS OF 7/28/2005. 2L73 4F A3WE 20050728000312005072800031EU 2005 7 28 TRB2005F00003 120050608A2612PR17100 SENSOR AEROSPATR72 ATR72212 8680945EU NR 2 ENGINE INTERMITTENT A TRBAC ABORTED TAKEOFF MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 SO29399AT 399 DURING TAKEOFF ROLL, THE RIGHT ENGINE NACELLE OVERHEAT WARNING LIGHT CAME ON. TAKEOFF ABORTED. REPLACED RIGHT ENGINE NACELLE OVERHEAT SENSOR. (M) 2H72 4T RTA53EU 20050728000352005072800035EU 2005 7 28 TRB2005F00001 120050604A2612 WARNING LIGHT AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FIRE WARNING FALSE INDICATIONA TRBAED ENGINE SHUTDOWN RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SO29434AT 434 WHILE TAXIING WITH PROPELLER IN FEATHER POSITION, WITH A TAIL WIND, THE LEFT ENGINE FIRE WARNING CAME ON MOMENTARILY. ENGINE WAS SHUT-DOWN. PERFORMED VISUAL CHECK AND FOUND NO EVIDENCE OF FIRE NOR DAMAGE. (M) 2H72 4T4 TRTA53EU E20NE 20050728000442005072800044NM 2005 7 28 USAA050751 120050609A5330 SKIN BOEING737 7374B7 1384702NM FUSELAGE WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19445US40360 24863 CLT - FOUND FUSELAGE SKIN WITH WORN .300 INCH LONG BY L.004 INCH WIDE BY .0135 INCH DEEP, AT BASE OF VERTICAL FIN, AFT END BODY CLOSURE ANGLE BODY STATION 1088. BLEND AREA OUT PER EA 96634 AND TREAT AREA. (M) 2L72 4F RTA16WE 20050728000612005072800061EA 2005 7 28 A6WA200540211 120050417A5730 PANEL CNDAIRCL600 CL6002B19 1900309EA WING DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31460AW 7867 ATTACHMENT HOLE ENLARGED ON OUTBOARD SIDE OF PANEL 684BB, DAMAGED WHILE REMOVING SCREW HOLE DIA WAS .193 NOW .265. INSTALLED FABRICATED 100 COUNTERSINK FREEZE PLUG IAW BRAS EO NR 601-57-6666. (M) 2L72 4F RTA21EA 20050728000642005072800064NM 2005 7 28 USAA050742 120050608A5412 SKIN BOEING737 7373B7 1384580NM NR 2 PYLON CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU 23861 CLT - FOUND SKIN CRACKED 1 INCH, NR 2 PYLON LEADING EDGE SKIN. TRIMMED OUT DAMAGE FABRICATED AND INSTALLED FILLER AND DOUBLER. (M) 2L72 4F RTA16WE 20050729000012005072900001NM 2005 7 29 AWXA200500861 120050705A52106545871523 DOOR FRAME BOEING737 7373G7 1384595NM R1 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED R1 DOOR CRACKED 1.380 INCHES IN LENGTH, ON THE FRAME AT THE AFT STOP CUTOUT. MAINTENANCE TRIMMED OUT THE CRACK ON THE FRAME AT THE AFT STOP CUTOUT IAW AMERICA WEST AIRLINES ENGINEERING REPAIR 03-5200-05201-ES1. FABRICATED A REPAIR DOUBLER IAW AWA ER 03-5200-05201-ES1. INSTALLED FABRICATED REPAIR PARTS IAW AWA ER 03-5200-05201-ES1. 2L72 4F RTA16WE 20050729000042005072900004NM 2005 7 29 AWXA200500864 120050707A5320654795711 STRAP BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 MCN - MAJOR REPAIR - CORROSION ON STRAP LOCATED ON INBOARD END OF TORQUE BOX, FROM BS 797 TO BS 847. MAINTENANCE REMOVED CORROSION AND DETERMINED TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-15-1 FIG 101. REMOVED STRAP ON INBOARD END OF TORQUE BOX, FROM BS 797 TO BS 847 AND PREPARED NEW STRAP FOR INSTALLATION IAW BOEING 737-300 SRM 51-40-05-0 FIG 2 AND FIG 3. INSTALLED REPAIR PARTS ON INBOARD END OF TORQUE BOX FROM BS 797 TO BS 847 IAW BOEING 737-300 SRM 51-40-02-0 FIGS 3, 8 AND 12. 2L72 4F RTA16WE 20050729000082005072900008NM 2005 7 29 AWXA200500868 120050708A53206517583503 VERTICAL BEAM BOEING737 7373G7 1384595NM BULKHEAD CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 MCN - MAJOR REPAIR - DURING C16 FOUND THE VERTICAL BEAM WEB CRACKED. 700 INCHES IN LENGTH. WEB LOCATED AT BS 178, FROM WL 175 TO WL 185 AND BL 5.7L. MAINTENANCE CUT OUT DAMAGE ON VERTICAL BEAM WEB FROM WL 175 TO WL 185, BS 178 AND BL 5.7L IAW BOEING 737-300 SRM 53-10-08-2. FABRICATED WEB, SHIMS AND DOUBLER IAW BOEING 737-300 SRM 53-10-08-2 FIG 212. INSTALLED FABRICATED REPAIR PARTS IAW BOEING 737-300 SRM 53-10-08-2 FIG 212. 2L72 4F RTA16WE 20050729000282005072900028EA 2005 7 29 ASOA05589 120050710A2613 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA BRAKE OVERHEAT FALSE INDICATIONA ASOAA UNSCHED LANDING J WARNING INDICATION DEDESCENT 1 SO11730EV 10141 DURING DESCENT FROM SLC-SAT, AT APPROXIMATELY 18,000 FEET THE CREW RECEIVED A BRAKE OVERHEAT WARNING MESSAGE ON EICAS WITH THE LEFT OUTBOARD BRAKE INDICATOR GOING TO TWENTY AND FLUCTUATED ERRATICALLY. AFTER COMPLYING WITH THE QRH ALL INDICATIONS RETURNED TO NORMAL. UPON LOWERING THE GEAR FOR FINAL APPROACH, THE OVERHEAT MESSAGE ACTIVATED AGAIN WITH LEFT OUTBOARD MAIN BRAKE INDICATOR SHOWING RED AND ALL OTHERS SHOWING GREEN AND THE TEMP INDICATOR SHOWING ONE. EMERGENCY VEHICLES WERE REQUESTED AS A PRECAUTION. THE AIRCRAFT LANDED SAFELY IN SAT. MAINTENANCE DEFERRED THE EICAS BRAKE TEMP MONITORING INDICATION UNDER MEL NR 32-46-01, CAT B EXPIRING 7/13/2005. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050729000362005072900036NM 2005 7 29 05FDEA02099 120050726A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 BS 1263 LWR RT TORQUE BOX FRAME ANGLE CRACKED RBL 20 WL 192. REPAIRED FRAME ANGLE PER SRM 51-30-2. (CLOSED) 2L73 4F RTA3WE 20050729000632005072900063NM 2005 7 29 05FDEA02118 120050727A3230656021132 ACCESSORY UNIT BOEING727 727227 1384078NM MLG MALFUNCTIONED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25492FE6235 6235 21530 AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RAISE PAST THE OFF POSITION. JACKED A/C REF 727 MM 07-11-000-2, ATTEMPTED TO RETRACT LANDING GEAR BUT WE WERE UNABLE TO RAISE THE HANDLE PAST THE OFF POSITION WITHOUT PULLING THE OVERIDE. REMOVED AND REPLACED THE LANDING GEAR ACCY UNIT REF 727 MM 32-09-121-4, OPS CHK GOOD, OK FOR SERVICE. 2L73 4F A3WE 20050729000682005072900068EA 2005 7 29 ASOA05579 120050705A5712 RIB CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11832AS 7243 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT BATT RIB ASSEMBLY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT BATT RIB ASSEMBLY AT WS 53.60 IAW ASA EO 600-57-039A. (M) 2L72 4F RTA21EA 20050729000782005072900078EU 2005 7 29 MALA050610 120050725A5312 BULKHEAD BAC 146 AVRO146RJ85A1500097EU MLG WW WORN A MALAK NONE O OTHER ININSP/MAINT 1 GL15501XJ E2208 WHILE ACCOMPLISHING TASK CARD 0638, NOTED WEAR MARKS ON THE FORWARD WALLS OF THE MAIN LANDING GEAR BAYS LEFT AND RIGHT SIDES. 2H74 4F RTA49EU 20050729000862005072900086NM 2005 7 29 AWXA200500859 120050703A57406938865505 ATTACH ANGLE BOEING737 7373G7 1384595NM ZONE 500 - LEFT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 DURING C16 CHECK DISCOVERED CRACK, 1.1 INCHES LONG, LOCATED ON ATTACH ANGLE ON BOTTOM OF LT WING, FORWARD SPAR, TERMINAL FITTING. MAINTENANCE STOP DRILLED CRACKS AND FABRICATED REPAIR DOUBLER IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5712-05196-DF1. INSTALLED FABRICATED REPAIR PARTS ON ATTACH ANGLE AT THE BOTTOM OF LT WING, FORWARD SPAR IAW AWA ER 03-5712-05196-DF1. 2L72 4F RTA16WE 20050729000892005072900089GL 2005 7 29 ALGA104484 220050707A725023032280 TURBINE WHEEL CLARK 1000 1000CLARK 2230102SW ALLSN 250C 250C30 03013GL NR 2 DAMAGED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03 WHEEL ASSY RAN ON TEST CELL WITH TURBINE ASSY S/N CAT-90323 FOUND TO HAVE HEAVY N1 RUB AT SHUT DOWN FROM 25-28 SEAL BOAR WARP. DISASSEMBLED TO REPAIR FOUND NR 2 WHEEL TO HAVE RAW BLADE TIP. ENDS ARE NOT ROUND AND HAVE DEEP INDENTIONS CAUSING SLAG ON TOP OF BLADES. / SENT BACK TO AVIALL FOR WARRANTY CREDIT. 1Q71 3R3 U 2A6 E1GL 20050729001022005072900102EA 2005 7 29 A6WA200540247 120050713A5340601R3HB58 STRINGER CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT FS280 CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31409AW 7447 RT FS 280 AT RBL 9, OB CLIP ANGLE IS CRACKED .5 INCH LONG. REPLACED CLIP IAW SRM. (K) 2L72 4F4 FRTA21EA E15NE 20050729001152005072900115EU 2005 7 29 ASOA05578 120050705A3350 LAMP AEROSPATR72 ATR72 EU PAX DOOR INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11631AS 362 FLT 4223 - DURING A GROUND INSPECTION IN MGM, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY LIGHT ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20050729001222005072900122EA 2005 7 29 ASOA05568 120050622A5340 FITTING CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11906EV 7642 DURING A C-CHECK IN HOT, THE BATHTUB FITTING AT FS 461 RBL 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE BATHTUB FITTING AT FS 461 RBL 9 IAW SRM 51-42-06 AND 51-42-21. (M) 2L72 4F RTA21EA 20050729001242005072900124EA 2005 7 29 ASOA05566 120050629A3350 RELAY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT FAILED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11908EV 7654 FLT 4494 - DURING A GROUND INSPECTION IN ATL, THE EMERGENCY LIGHTS REMAINED ON WHEN IN THE ARMED POSITION. MAINTENANCE REMOVED AND REPLACED THE RELAY K1XD. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050729001322005072900132NM 2005 7 29 C7WA200500108 120050705A3240211473 BRAKE BOEING727 727222 1384073NM PWA JT8 JT8D5 52046NE LT MLG SEIZED A C7WAO OTHER MJ OVER TEMP WARNING INDICATION NRNOT REPORTED 1 SO177643U 20037 AIR RETURN, ON CLIMBOUT AT 14,000 FT WHEEL WELL FIRE LIGHT ILLUMINATED. RAN CHECK LIST FIRE LIGHT WENT OUT. FOUND NR 2 BRAKE ASSEMBLY. SEIZED. REMOVED AND REPLACED NR 2 BRAKE ASSEMBLY. (SO29200506401) (K) 2L73 4F4 F A3WE E2EA 20050801000012005080100001EA 2005 8 1 A6WA200540240 120050713A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31409AW 7447 LT FS 280 AT LBL 9 OB CLIP ANGLE IS CRACKED .5 INCH LONG. REPLACED CLIP IAW SRM. (K) 2L72 4F4 FRTA21EA E15NE 20050801000062005080100006WP 2005 8 1 UPS05844980 120050629A534037794981 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE: C1, MAIN CARGO STA 860 LONGERON 19R FITTING CRACKED APPROX. 2 INCHES ON FWD SIDE OF FRAME. REMOVED AND REPLACED LONGERON FITTING IAW DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20050801000082005080100008WP 2005 8 1 UPS05844982 120050625A53404888829502 ATTACH FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE: C1, FLOORBEAM VERTICAL ATTACH FITTING HAS HEAVY CORROSION. ALSO APPEARS TO BE CRACKED. STA 69 RBL 48. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-3-0. 2L74 4F RT4A25 20050801000132005080100013EU 2005 8 1 RAIA00507020 120050727A2422PC125123B STATIC INVERTER JETAIRJETSTMJETSTM4101 1500501EU LEFT FAILED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03559HK170164933 41075 FLT 5437- STL- LT INVERTER FAIL LIGHT ILLUMINATED. REPLACED THE LT STATIC INVERTER. OPS CHECKED GOOD. 2L72 4T RTA41NM 20050801000202005080100020NM 2005 8 1 ASMF200507023 120050727A27114640880 DRIVE ASSY DOUG MD88 MD88 3023688NM AILERON TRIM DAMAGED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23161PL 49764 DURING TRANSIT SERVICE, CAPTAIN REPORTED AILERON TRIM OUT OF SERVICE. DURING REVISION WAS DETECTED THE PLATE PEDESTAL AILERON TRIM SPIRAL DRIVE DAMAGED. THE SPIRAL DRIVE WAS REPLACED IAW MM 27-10-01, TESTED CORRECT. 2L72 4F RTA6WE 20050801000212005080100021NM 2005 8 1 DU4R0507172 120050729A5330 SKIN BOEING737 737300 1384610NM FUSELAGE DENTED B DU4RK NONE O OTHER ININSP/MAINT 1 SO15387UA 24662 DENT IN LT SIDE FUSELAGE SKIN IN AREA OF S-20L BS 465. 2L72 4F RTA16WE 20050801000232005080100023NE 2005 8 1 MWEA050073 220050727A7200 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE RIGHT ODOR A MWEAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 GL31809ME 48071 REAR CABIN BEGAN TO FILL WITH SOME HAZE AND RIGHT SMOKE DETECTOR WENT OFF. REMOVED AND REPLACED RIGHT ENGINE. 2L72 4F4 F A6WE E9NE 20050801000242005080100024WP 2005 8 1 RYNA200500023 120050720A3600AYLF206 GASKET DOUG DC9 DC982 3022082WP TAIL FAILED A RYNAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE07932RD 49233 TAIL COMPARTMENT TEMPATURE HIGH LIGHT ILLUMINATED DURING CLIMB. REMOVED AND REPLACED TWO GASKETS ON THE PNEUMATIC ICE CONTROL ANTICIPATOR AND BLEED AIR SUPPLY HIGH TEMPERATURE SENSOR. OPERATIONALLY CHECKED NORMAL, NO LEAKS NOTED 2L72 4F A6WE 20050801000272005080100027EU 2005 8 1 SA05090 120050728A335032145410 EPSU AIRBUSA319 A319112 3930323EU PASSENGER CABIN FAILED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19715UW6714 1065 PIT - DURING THE EMERGENCY LIGHTS TEST, RECEIVED 'EPSU INT LOAD EMER R' FAULT. MAINTENANCE REPLACED THE RIGHT EMERGENCY POWER SUPPLY UNIT. SYSTEM OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20050801000302005080100030WP 2005 8 1 AALA20050461 120050725A2797 WIRE DOUG DC9 DC982 3022082WP RUDDER SENSOR SHORTED A AALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW21513AA 49890 TPA INFLIGHT T2247/25JUL CLIMBING THROUGH FLIGHT LEVEL 220 AUTO PILOT DISENGAGED. CAPTAIN SAYS FLIGHT WAS HARD TO CONTROL IN THE ROLL AND YAW MODE. CAPTAIN DECLARED AND EMERGENCY AND RETURNED TO TPA. FLT LANDED WITHOUT INCIDENT. FOUND SHORTED WIRE IN TAIL COMPARTMENT GOING TO RUDDER POSITON SENSOR. REPAIRED SHORTED WIRE IN TAIL COMPARTMENT GOING TO RUDDER POSITION SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F A6WE 20050801000332005080100033WP 2005 8 1 050116996 120050727A21332075401AA OUTFLOW VALVE DOUG DC9 DC931 3022065WP CABIN PRESSURE LEAKING A NWAAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 GL018932E 47141 AT FL310, WITH POWER AT CRUISE SETTING AND AIRFOIL ANTI-ICE ON, THE RED "CABIN PRESS" WARNING LIGHT ILLUMINATED. CABIN WAS JUST ABOVE 10,000 FEET AND CLIMBING AT 800-900 FPM. CREW COMPLIED WITH COM AND THE RED BORDERED CHECKLIST BUT COULD NOT REGAIN CONTROL OF CABIN PRESSURE. AN EMERGENCY DESCENT WAS PERFORMED AND THE AIRCRAFT LANDED UNEVENTFULLY AT DTW. MAINTENANCE DID BITE OF THE PRESSURE CONTROLLERS, FOUND PREVIOUS FAULTS, AND REPLACED THE OUTFLOW VALVE. THE AIRCRAFT HAS RETURNED TO SERVICE. 2L72 4F A6WE 20050801000342005080100034WP 2005 8 1 0501169996 120050727A21332075401AA OUTFLOW VALVE DOUG DC9 DC931 3022065WP CABIN PRESSURE LEAKING A NWAAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 GL018932E 47141 AT FL310, WITH POWER AT CRUISE SETTING AND AIRFOIL ANTI-ICE ON, THE RED "CABIN PRESS" WARNING LIGHT ILLUMINATED. CABIN WAS JUST ABOVE 10,000 FEET AND CLIMBING AT 800-900 FPM. CREW COMPLIED WITH COM AND THE RED BORDERED CHECKLIST BUT COULD NOT REGAIN CONTROL OF CABIN PRESSURE. AN EMERGENCY DESCENT WAS PERFORMED AND THE AIRCRAFT LANDED UNEVENTFULLY AT DTW. MAINTENANCE DID BITE OF THE PRESSURE CONTROLLERS, FOUND PREVIOUS FAULTS, AND REPLACED THE OUTFLOW VALVE. THE AIRCRAFT HAS RETURNED TO SERVICE. 2L72 4F A6WE 20050801000352005080100035EU 2005 8 1 AALA20050464 120050723A2550 LOCK AIRBUS300 A300B4605R 3930308EU CONTAINER ROLLERINOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2111060 470 AFT CARGO COMPARTMENT SMOKE WARNING RIGHT AFTER TAKEOFF. FIRED BOTH BOTTLES ALTHOUGH DID NOT GET AGENT 2 DISCHARGE LIGHT. AFTER LANDING GOT CARGO LOOP B. FOUND LEFT AFT CONTAINER ROLLER RUNS CONTINUOUSLY. REPAIRED JAMMED LOCK 511MY. REPAIRED JOYSTICK AND CARGO CONTROL BOX. REPLACED BOTH FIRE BOTTLES. REPLACED CED 44WH AND 8WH AS PRECAUTION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20050801000362005080100036NE 2005 8 1 AALA20050463 220050722A7200 ENGINE AIRBUS300 A300B4605R 3930308EU GE CF6 CF680C2A5 NE ZONE 500 STALLED A AALAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 SW217082A 643 695439 ON TAKEOFF NUMBER ONE ENGINE COMPRESSOR STALLED. RETUNED TO JFK AND LANDED WITHOUT INCIDENT. REPLACED NUMBER 1 ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA35EU E13NE 20050801000392005080100039WP 2005 8 1 ARWA20050704 120050727A2612 FIRE LOOP DOUG DC8 DC863F 302198FWP NR 4 ENGINE CHAFED A ARWAE ENGINE SHUTDOWN N FALSE WARNING CLCLIMB 1 SO19661AV 45969 NR 4 ENGINE FIRE WARNING ON CLIMB-OUT, MROL SECURED ENGINE IN ACCORDANCE WITH ARROW PROCEDURES "NOTED HIGH OIL TEMPERATURE AFTER SHUTDOWN, OIL PRESSURE 20 PSI IN-CRUISE, 10 PSI ON APPROACH. INSPECTED NR 4 ENGINE; FOUND NR 4 FIRE LOOP CHAFING AGAINST ENGINE COWLING. PROVIDED CLEARANCE, REPOSITIONED FIRE LOOP IN ACCORDANCE WITH M/M 26-2-1 AND M/M 72-00. PERFORMED ENGINE RUN-UP WITH CREW, NO LEAKS OR DEFECTS NOTED IN ACCORDANCE WITH M/M 71-00. ALL INDICATIONS NORMAL. 2L74 4F 4A25 20050801000402005080100040NM 2005 8 1 05FDEA02124 120050728A2913378001 PUMP BOEING727 7272S2F 1384O81NM HYD SYSTEM FAILED A FDEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO25204FE 22926 HYD SYS B OVERHEAT LIGHT IN FLT TURNED ELEC PUMP NR 1 OFF AND LIGHT WENT OUT. REMOVED AND REPLACED NR 1 B PUMP PER MM-29-12-011-2. OPS CKS AND LEAK CKS GOOD. CYCLED ALL FLIGHT CONTROLS ON B SYS TO ENSURE NO AIR IN SYSTEM. NOTE, CASE DRAIN ALSO REMOVED AND REPLACED PER MM, CKS GOOD. 2L73 4F A3WE 20050801000412005080100041NM 2005 8 1 05FDEA02125 120050728A5310 SUPPORT BOEING727 727227 1384078NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 CORROSION ON 740, LBL 8, WL 148, UNDER ACCESS PANEL 3348L. SKIN SUPPORT WAS FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED SKIN SUPPORT BS 740, LBL 8, WL 148 PER SRM 51-30-2 AND SRM 53-10-1 2L73 4F A3WE 20050801000442005080100044GL 2005 8 1 05FDEA02128 220050728A7200 ENGINE DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL NR 1 FIRE A FDEAFE ACTIVATE FIRE EXT. ENGINE SHUTDOWN BAJSMOKE/FUMES/ODORS/SPARKS FLAME/FIRE WARNING INDICATION TXTAXI/GRND HDL 1 SO25397FE 46631 NR 1 ENG FIRE ON GROUND-LOUD BANG, FOLLOWED BY SMOKE, FOLLOWED BY NR 1 ENGINE FIRE WARNING ENGINE FIRE AND SEVERE QRH COMPLIED WITH AS WELL AS ALL APPLICABLE CHECKLISTS. NR 1 FIRE BOTTLE FIRED, NR 1 PACK ON-TEMP 38C GOOD FIRE TEST. REMOVED AND REPLACED NR 1 ENG PER MX WORKCARD 71T0701-1 RAN ENG PER JRH, OPS CHECKS AND LEAK CHECKS NORMAL. 2L73 4F4 F A22WE E23EA 20050801000462005080100046EU 2005 8 1 05FDEA02130 120050728A5742 FITTING AIRBUS300 A300F4605R 3930327EU NR 1 PYLON CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25671FE 778 NR 1 PYLON TO WING ATTACHMENT FITTING SHACKLE OUTBD/INBD LOWER BUSHING HAS CORROSION CHROME PLATING WORN. 2L72 4F RTA35EU 20050801000472005080100047EU 2005 8 1 05FDEA02131 120050728A5742 SLEEVE AIRBUS300 A300F4605R 3930327EU NR 1 PYLON CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25671FE 778 NR 1 PYLON TO WING ATTACH FITTING SLEEVE (OUTBD LUG/LWR) HAS GOUGED MARK AND HAS CORROSION ON THE HEAD END INNER COLLAR. 2L72 4F RTA35EU 20050801000492005080100049EU 2005 8 1 05FDEA02133 120050728A5744 GUSSET AIRBUS300 A300F4605R 3930327EU LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25670FE 777 LT WING BELOW NR 5 SPOILER INBD ATTACH POINT HAS A GUSSET CRACKED. 2L72 4F RTA35EU 20050801000502005080100050EU 2005 8 1 05FDEA02134 120050728A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25670FE 777 SEAT TRACK AT Y953 FR 17-19 IS CORRODED. 2L72 4F RTA35EU 20050801000522005080100052NM 2005 8 1 05FDEA02137 120050729A2612 WARNING SYSTEM BOEING727 727227 1384078NM COCKPIT ACTIVATED A FDEAO OTHER J WARNING INDICATION APAPPROACH 1 SO25490FE 21493 APPROX 1 00 INTO THE FLT APPROX 2000' AGL ON FINAL APPROACH, THE AFT MOST LIGHT IN THE MAIN CARGO SMOKE ILLUMINATED WITH CORRESPONDING FIRE BELL AND LIGHT INTERMITTENTLY SOUNDED AND LIT RAN QRH FOR MAIN CARGO SMOKE AS WELL AS FIRE. NO SMOKE OR FUMES IN COCKPIT, NO HIGH ENERGY STOP, TAXIED CLEAR OF RUNWAY. EVACUATED A/C USING CREW ENTRY SLIDE PULLED CVR FDR. UPON ENTRY ON ACFT THE SMOKE DETECTOR NR 6 WAS ILLUMINATING WITH CORRESPONDING BELL. DISCONNECTED NR 6 SMOKE DETECTOR C/P; INDICATION EXTINGUISHED AND BELL SILENCED. SUSPECT BAD DETECTOR. REMOVED AND REPLACED NR 6 SMOKE DETECTOR OPS CHECKED NORMAL REF AMM 26-16-011-4 & 26-16-00-5. 2L73 4F A3WE 20050801000532005080100053EU 2005 8 1 05FDEA02138 120050729A1430 FASTENER AIRBUS300 A300F4605R 3930327EU AILERON TRIM MISSING A FDEAA UNSCHED LANDING O OTHER CLCLIMB 1 SO25651FE 728 PASSING 5500FT MSL AND LEVELING AT 6000 FT, HAND FLYING USING AUTO THROTTLES, ATTEMPTED TO TRIM AIRCRAFT MANUALLY WITH TRIM BUTTON ON YOKE. DURING TRIM A VIBRATION WAS FELT ON THE A/C. NEEDED MORE TRIM TO LEVEL, AGAIN VIBRATION OCCURRED DURING TRIMMING, 250 KTS, 6000 FT MSL, CG 27.8 PERCENT, AUTOTHROTTLES ON & ENGINES NEAR IDLE. INSPECTED TRIMMABLE HORIZONTAL STABILIZER. ON STABILIZER APRON, FOUND ON BOTH SIDES BOTTOM HALF SEVERAL FINGER SKIRTS MISSING RIVETS (55-10/8938). FOUND MANY PIECES OF PAPER WEDGE IN AND AROUND PITCH TRIM CONTROL WHEEL CHAIN. REMOVED ALL DEBRIS. PERFORMED ADJ/TEST PER MM 22-27-00-5 OP'S 2L72 4F RTA35EU 20050801000552005080100055 2005 8 1 05FDEA02140 420050729A3442 RADAR BOEING727 727227 1384078NM WX SYSTEM MALFUNCTIONED A FDEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO25485FE 21488 ON CLIMB-OUT, TURNING RADAR ON AND GOT A FAIL LT ALONG WITH SPOKING IN ALL RANGES. TURNED OFF, PULLED AND RESET CB'S, SAMETHING WHEN RADAR TURNED ON. REMOVED AND REPLACED WEATHER RADAR R/T. SYS OPS CKD NORMAL. REF B727-200 MM 34-41-41. 2L73 4F A3WE 20050801000572005080100057NM 2005 8 1 DHL2005788007 120050729A3350 BATTERY BOEING727 727214 138407RNM EMERGENCY LIGHT DISCHARGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01788AT 21958 DURING PDC, FOUND EMERGENCY LIGHTS ARMED AND COCKPIT AND FOWARD ENTRY BATTERIES DEAD. RESECURED COCKPIT AND FWD ENTRY EMERGENCY LIGHTS AND TESTED SERVICEABLE REF 33.50.01. 2L73 4F A3WE 20050801000622005080100062NE 2005 8 1 WRLA2005139 220050731A7200 ENGINE DOUG MD11 MD11 3023602NM PWA 4460 PW4460 NE NR 2 FLAMED OUT A WRLAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION LDLANDING 1 SO11801DE 48472 P723949 ON ROLLOUT, NR 2 ENGINE FLAMED OUT, ENGINE WAS IN REVERSE THRUST. PERFORMED T/S AS PER FIM 71-01-02. ALL CHECKS OK PERFORMED EXTENDED DURATION ENGINE RUN IN FWD AND REVERSE THRUST CONDITIONS. ENGINE RUNS ALL NORMAL. 2L73 4F4 FRTA22WE E24NE 20050801000642005080100064EU 2005 8 1 MALA050620 120050727A5753 SKIN BAC 146 AVRO146RJ85A1500097EU TE FLAP DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15504XJ E2311 WHILE ACCOMPLISHING C1 INSPECTION, FOUND A DENT ON THE RIGHT OUTBOARD FLAP TAB, ON THE BOTTOM SIDE, 24 INCHES FROM INBOARD END. 2H74 4F RTA49EU 20050801000652005080100065EU 2005 8 1 SF20050727 120050727A2497 CONNECTOR SAAB SF340 SF340A 7850100EU LT P3 SWITCH DAMAGED A UHLAC ABORTED TAKEOFF J WARNING INDICATION CLCLIMB 1 GL1719XS 340A019 ON TAKEOFF ABOUT 70KTS, AUTOCOARSEN LIGHT ILLUMINATED ON CWP DURING TAKEOFF ROLL. AIRCREW REJECTED TAKEOFF AND RETURN TO THE GATE. APPLIED MODERATE BRAKING. MAINTENANCE FOUND BAD CONNECTION ON LT P3 SWITCH PIN. REPAIRED P3 SWITCH PIN. 2L72 4T RTA52EU 20050801000662005080100066EU 2005 8 1 MALA050621 120050729A3210 CONTROL SYSTEM BAC 146 AVRO146RJ85A1500097EU MLG MALFUNCTIONED A MALAO OTHER J WARNING INDICATION CLCLIMB 1 GL15502XJ E2307 AFTER TAKEOFF, THE LT MLG NO UP AND LOCKED, AUTOPILOT AND AUTO THROTTLES FAILED AND THE MANUAL SPOILER LIGHT ILLUMINATED. NO FURTHER INFORMATION AT THIS TIME 2H74 4F RTA49EU 20050801000672005080100067EU 2005 8 1 MALA050619 120050727A5753 SKIN BAC 146 AVRO146RJ85A1500097EU TE FLAP DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15504XJ E2311 WHILE ACCOMPLISHING C1 INSPECTION, FOUND A DENT ON THE RIGHT OUTBOARD FLAP TAB ABOUT 6 INCHES FROM INBOARD END AND 5 INCHES FROM BOTTOM OF THE TAB. 2H74 4F RTA49EU 20050801000752005080100075SO 2005 8 1 C2XA05IA087 120050712A335078241 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714950 145061 STL - DURING SCHEDULED MAINTENANCE, THE EMERGENCY EXIT SIGN AT ROW 3BC WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT SIGN INVERTER, OPERATIONALLY TESTED THE EMERGENCY LIGHTING SYSTEM AND CLEARED THE DISCREPANCY. 2L72 4T RTT00011AT 20050801000762005080100076NM 2005 8 1 QXEA200501140 120050728A21607786848 MIXER BOX DHAV DHC8 DHC8202 2809007NM CONDENSER MALFUNCTIONED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM09356PH32925792 502 LMT FLIGHT NR 2240, UNABLE TO CONTROL CABIN TEMPERATURE, ALSO NOTED FAINT TAR/ELECTRICAL SMELL THROUGH AIR VENT WHICH DIMINISHED WITH BLEED OFF. MAINTENANCE INSPECTED ECS SYSTEM AND FOUND URBINE SEIZED. REPLACED CONDENSER MIXER AND ACM. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050801000772005080100077NM 2005 8 1 QXEA200501142 120050724A242011522184 GENERATOR BOMBDRDHC8 DHC8402 1390042NM ZONE 200 MALFUNCTIONED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09410QX2743 2743 4053 MSO - AFTER START NR 2 AC GENERATOR CAUTION LIGHT ILLUMINATED. RESET PER ABNORMAL CHECKLIST, STILL REMAINED ILLUMINATED. REPLACED NR 2 AC GENERATOR AND CHECKED SCAVENGE FILTER FOR CONTAMINATION. NO DEFECTS NOTED. BOTH AC GENERATOR AND SCAVENGE FILTER LEAK CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050801000792005080100079EA 2005 8 1 A6WA200540245 120050621A53206013501252 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31419AW 7633 RT OBLIQUE ANGLE AT FS 625 CRACKED ON AFT EDGE APPROX 1 INCH LONG. REMOVED OBLIQUE ANGLE RT FS 625, INSTALLED NEW SERVICEABLE ANGLE IAW SRM. (K) 2L72 4F4 FRTA21EA E15NE 20050811001152005081100115EA 2005 8 11 A6WA200540244 120050715A53406013501252 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT FS 625 CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31420AW 7640 RT FS 625, OBLIQUE ANGLE IS CRACKED. REMOVED CRACKED OBLIQUE ANGLE AND REPLACED WITH NOW IAW SRM. (K) 2L72 4F4 FRTA21EA E15NE 20050801000832005080100083EA 2005 8 1 A6WA200540252 120050716A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31420AW 7640 FS 280, RBL 9, IB ATTACH CLIP CRACKED. REPLACED ANGLE IAW SRM AND EO. (K) 2L72 4F4 FRTA21EA E15NE 20050802000012005080200001EA 2005 8 2 A6WA200540264 120050724A5753 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT WING TE FLAP DENTED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31405AW 7362 LT WING IB FLAP INNER SKIN IS DENTED BETWEEN FLAP STATION 142 AND 147 AT THE INTERCOSTAL SPAR AREA. DEN MEASURES .850 INCH LT X .800 INCH X .067 INCH DEEP. PERFORMED REPAIR BY CUTTING OUT DAMAGE AND INSTALLING 11.5 INCH X 3 INCH FLUSH REPAIR IAW SRM REPAIR AND EO. (K) 2L72 4F4 FRTA21EA E15NE 20050802000032005080200003EA 2005 8 2 A6WA200540265 120050724A5753 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT WING FLAP CHAFED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31405AW 7362 LT WING IB FLAP, IB END AT FLAP STA 50.498 IB BELOW THE LEADING EDGE IS CHAFED FROM THE STUB FAIRING. CHAFE MEASURES 1.50 INCH LONG X .50 INCH WIDE X .035 INCH DEEP. (K) 2L72 4F4 FRTA21EA E15NE 20050802000052005080200005EA 2005 8 2 A6WA200540254 120050715A5320 SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31420AW 7640 WO 84084, MWC 131, RT SIDE UNDERFLOOR SUPPORT STRUCTURE IS CRACKED 1.0 INCH AT FS 621, RBL 40, WL 73. REPAIRED BY REMOVING DAMAGED SECTION OF ANGLE, FABRICATING AND INSTALLING REPAIR ANGLES IAW REO. (K) 2L72 4F4 FRTA21EA E15NE 20050802000102005080200010WP 2005 8 2 CLC2005F00002 120050720A2497 WIRE DOUG DC10 DC1030 3023501WP GE CF6 CF650* 30018NE NR 2 GENERATOR BURNED A CLCAD RETURN TO BLOCK BH SMOKE/FUMES/ODORS/SPARKS ELECT. POWER LOSS-50 PC TXTAXI/GRND HDL 1 SO29279AX 47816 ON TAXI OUT THE NR 2 AC BUSS CIRCUIT BREAKERS POPPED OUT. SMELLED SMOKE IN COCKPIT TAXIED BACK TO THE RAMP. FOUND BURNED WIRES AND FEEDER CABLES BELOW LAVATORY FLOOR FOR THE NR 2 GENERATOR, ALL 3 PHASES. GENERATOR FEEDER CABLES FOR NR 1 AND 3 GENERATORS ARE ALSO DETERIORATED. (K) 2L73 4F4 F A22WE E23EA 20050802000142005080200014EA 2005 8 2 A6WA200540253 120050716A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31420AW 7640 FS 280, LBL 9, OB ATTACH CLIP CRACKED. (K) REPLACED ANGLE P/N 601R31113-58 IAW CRJ CRM 51-42-06 AND BRAS EO 601R-53-6888. (M) 2L72 4F4 FRTA21EA E15NE 20050802000152005080200015EA 2005 8 2 A6WA200540259 120050719A2820722514 SENSOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUEL SYSTEM INOPERATIVE A A6WAO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 GL31459AW3938 7863 RT FUEL HIGH LEVEL SENSOR INOPERATIVE PLACARD AND PLACED ON MEL. CODE ON COMPUTER SHOWS 140 (LT TANK HIGH LEVEL SENSOR). REMOVED AND REPLACED RT FUEL LEVEL SENSOR IAW AMM. OPS AND LEAK CHECK GOOD. (K) 2L72 4F4 FRTA21EA E15NE 20050802000172005080200017NM 2005 8 2 CLC2005F00005 120050711A7160ATL71033 SEAL DOUG DC10 DC1040F 3023507NM PWA JT9 JT9D* NE NR 2 ENG INLET DAMAGED A CLCAK NONE O OTHER ININSP/MAINT 1 SO29140WE59475 46920 DURING PREFLIGHT CHECK, DAMAGE WAS FOUND TO NR 2 ENGINE INTAKE AND FAN BLADES. ENGINE INTAKE HAS DAMAGE TO UPPER AND LWR BELLMOUTH ADAPTOR RINGS, INTAKE INLET LIP HAD SECTION OF SKIN BLOWN OUT, NUMEROUS CRACKS FOUND ALONG CIRCUMFERENCE AT ATTACH FASTENERS. INLET SEAL TORN AT FWD END OF TOP ADAPTER RING AND L/E CHANNEL OF UPPER SEGMENT OF ADAPTER RING HAS SEVERAL CRACKS, 1 LG HOLE ON LT SIDE, ACOUSTIC MATERIAL DAMAGED FWD OF FAN BLADES. BORESCOPE INSP OF NR 2 ENGINE FOUND FOD DAMAGE TO LPC AND HPC BEYOND MM LIMITS, REQUIRING ENG REMOVAL. REPLACED NR 2 ENGINE. REPLACING DAMAGED PIECES OF INTAKE L/E, BELL MOUTH ADAPTOR RINGS AND ACOUSTIC MATERIAL. INSTRUCTED FLIGHT CREWS ON PROPER THROTTLE MANAGEMENT. (K) 2L73 4F4 FRTA22WE E20EA 20050802000192005080200019SO 2005 8 2 N382005F00004 120050719A801138370213 STARTER GULSTMG1159 G1159B 3953535SO RROYCESPEY SPEY5118 54523EU LT ENGINE MELTED E N38AO OTHER O OTHER TXTAXI/GRND HDL 1 EA0595SJ 9436 064 8568 LT ENGINE WILL NOT START; NO START VALVE OR IGNITION LIGHT WHEN STARTER BUTTON PRESSED. A REPLACEMENT STARTER WAS INSTALLED AND THE AIRCRAFT WAS FLOWN BACK TO ITS HOME BASE. (K) 2L72 4F4 FRTA12EA E2EU 20050802000202005080200020NM 2005 8 2 CLC2005F00007 120050711A7160ATL7107 RING DOUG DC10 DC1040F 3023507NM PWA JT9 JT9D* NE BELLMOUTH ADAPT DAMAGED A CLCAK NONE O OTHER ININSP/MAINT 1 SO29140WE59475 46920 DURING PREFLIGHT CHECK, DAMAGE WAS FOUND TO NR 2 ENGINE INTAKE AND FAN BLADES. ENGINE INTAKE HAS DAMAGE TO UPPER AND LOWER BELL MOUTH ADAPTOR RINGS, INTAKE INLET LIP HAD SKIN BLOWN OUT, NUMEROUS CRACKS FOUND ALONG CIRCUMFERENCE AT ATTACH FASTENERS. INLET SEAL TORN AT FWD END OF TOP ADAPTER RING, L/E CHANNEL OF UPPER SEGMENT OF ADAPTER RING HAS SEVERAL CRACKS AND 1 LARGE HOLE ON LT SIDE, ACOUSTIC MATERIAL DAMAGED FWD OF FAN BLADES. BORESCOPE INSP OF NR 2 ENGINE FOUND FOD DAMAGE TO LPC AND HPC BEYOND MM LIMITS REQUIRING ENGINE REMOVAL. REPLACED NR 2 ENGINE. REPLACING PIECES OF INTAKE L/E, BELL MOUTH ADAPTOR RINGS AND ACOUSTIC MATERIAL. INSTRUCTED FLIGHT CREWS ON PROPER THROTTLE MANAGEMENT. (K) 2L73 4F4 FRTA22WE E20EA 20050802000212005080200021EU 2005 8 2 Y2PA05009 120050614A793111346AA TRANSMITTER AMD FALC20FALCOND 2720304EU GE CF700 CF7002D 30010NE OIL PRESSURE FAILED E Y2PABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION LDLANDING 1 GL23823AA 228 304296B DURING DESCENT, CREW NOTICED NR 1 ENGINE OIL PRESSURE GAUGE MAXED OUT. REDUCED NR 1 THROTTLE AND GAUGE DIDN`T MOVE. CREW SHUTDOWN NR 1 ENGINE, DECLARED AN EMERGENCY WITH APPROACH AND DIRECTED THAT THEY NEEDED TO RETURN TO DEPARTURE. CREW EXECUTED ENGINE FAILURE/ SHUTDOWN CHECK LIST, RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MAINT REMOVED AND REPLACED THE NR 1 OIL PRESSURE TRANSMITTER IAW MM. ENGINE WAS RUN FOR OPERATIONAL AND LEAK CHECKS PERFORMED A GROUND RUN ON NR 1 ENGINE IAW WORK CARD. ALL PARAMETERS CHECKED GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4F4 F A7EU E7EA 20050802000252005080200025NM 2005 8 2 AALA20050482 120050722A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21943AN 30599 TUL - EMERGENCY LIGHTS AT FORWARD GALLEY OVERHEAD STATION 328 FAILED TEST IN ACCORDANCE WITH WORK CARD 2311. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD GALLEY OVERHEAD STATION 328. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20050802000272005080200027NM 2005 8 2 AALA20050479 120050716A5311 FRAME BOEING767 767323 1385205NM FUSELAGE DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21366AA 25193 AFW - FUSELAGE FRAME WEB IN FORWARD CARGO COMPARTMENT HAD HEAT DAMAGE CAUSED BY FIRE. AREA AFFECTED WAS 31 INCHES BY 16 INCHES AT STATION 654 AND 88. REPAIRED FRAME PER MRB 767-2717. 2L72 4F RTA1NM 20050802000282005080200028NM 2005 8 2 AALA20050483 120050727A3830141N86313 PAN BOEING757 7572Q8 1384972NM LAVATORY CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21702TW 28162 MCI - CORROSION FOUND AROUND FORWARD LAVATORY DUMP CHUTE BETWEEN FORWARD LAVATORY SERVICE PAN AND UPPER PAN IN AREA 12 INCHES BY 12 INCHES. REPLACED FORWARD LAVATORY SERVICE PANEL UPPER PAN. 2L72 4F RTA2NM 20050802000292005080200029WP 2005 8 2 AALA20050484 120050801A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW219302B 49528 SFO - FOUR EACH EMERGENCY LIGHTS IN OVERHEAD TAIL CONE AND SLIDE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK B528 FOR FOUR EACH EMERGENCY LIGHTS IN OVERHEAD TAIL CONE AND SLIDE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050802000312005080200031NM 2005 8 2 AALA20050481 120050719A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21942AN 30084 TUL - EMERGENCY LIGHT IN MID CABIN AT STATIONS 322 AND 559 FAILED TEST. REPLACED BATTERY PACK FOR EMERGENCY LIGHT IN MID CABIN AT STATIONS 322 AND 559. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20050802000332005080200033EU 2005 8 2 SA05092 120050731A33501012881 LIGHT AIRBUS320 A320214 3930316EU SEAT 23 INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19111US 1114 DCA - THE SEAT MOUNTED EMERGENCY LIGHT AT SEAT 23 ABC WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE FLOOR LEVEL EMERGENCY LIGHT ASSEMBLY AT SEAT 23ABC. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20050802000362005080200036NM 2005 8 2 TSAA0532032 120050727A3230BACC18Z2R CIRCUIT BREAKER BOEING737 7372T4 1384492NM MLG FAILED A TSAAH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CLCLIMB 1 WP13807AL 23443 FLT 71 OGG-HNL, AFTER DEPARTURE, CREW WAS UNABLE TO MOVE LANDING GEAR LEVER TO THE UP POSITION. CREW FOUND CIRCUIT BREAKER POPPED OUT AND THEN RESET IT. GEAR HANDLE WAS THEN MOVED TO THE UP POSITION. THE FLIGHT CONTINUED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE CIRCUIT BREAKER AND PERFORMED A GEAR SWING TEST AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F A16WE 20050802000382005080200038NM 2005 8 2 QXEA200501144 120050730A2510 LOCK DHAV DHC8 DHC8202 2809007NM COCKPIT SEAT LACK OF LUBE A QXEAO OTHER O OTHER LDLANDING 1 NM09351PH 490 SEA FLIGHT NR 2105, AFTER LANDING, WHEN THE BRAKES WERE APPLIED, THE CAPTAIN'S SIDE SEAT MOVED TO THE FULL FORWARD POSITION. MAINTENANCE LUBRICATED CAPTAINS SEAT LOCK MECHANISM. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050802000392005080200039NM 2005 8 2 QXEA200501145 120050730A2720 PRESSURE SWITCH DHAV DHC8 DHC8202 2809007NM RUDDER MALFUNCTIONED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09365PH 526 BOI FLIGHT NR 2204, RUDDER FULL PRESSURE CAUTION LIGHT AFTER TAKEOFF. THIS WAS ACCOMPAINIED BY A RUDDER PRESSURE CAUTION LIGHT. MAINTENANCE REPLACED NR 1 AND NR 2 RUDDER PRESSURE SWITCHES. GROUND RAN AIRCRAFT. OPERATED RUDDER THRU SEVERAL CYCLES. ALSO, C/W -8 200 AMM 27-20-38 TR 27-053, STEPS 1-6A. ALL CHECKS NORMAL NO FURTHER DEFECT NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050802000402005080200040EU 2005 8 2 USAA050857 120050708A5320 FLOOR SUPPORT AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19108UW18429 1061 PIT - FOUND FLOORBEAM CORRODED 4 INCHES BY 18 INCHES BY .050 INCH, FLOOR SUPPORT Y1732 FRAME 69-70. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 53-00-15 FIG 201. (M) 2L72 4F RTA28NM 20050802000422005080200042EU 2005 8 2 USAA050860 120050708A5347D5311278220201 SEAT TRACK AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19108UW18429 1061 PIT - FOUND FLOOR SUPPORT SEAT TRACK CORRODED 2 FT BY .5 INCH, BETWEEN C18 AND C20. REPLACED BEAM SECTION PER DWG D53110900. CORROSION LEVEL 1, TASK JA-220-53500. (M) 2L72 4F RTA28NM 20050802000432005080200043EU 2005 8 2 USAA050854 120050708A5315D5311281820401 FLOORBEAM AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19108UW18429 1061 PIT - FOUND BEAM CORRODED .5 INCH BY 3 INCH AREA, FLOORBEAM Y254 BETWEEN CROSSBEAMS C-16 AND C-20. REMOVED AND REPLACED WITH NEW PART PER SRM 53-11-14 FIG 202. CORROSION LEVEL 1, TASK JA-222-53500. (M) 2L72 4F RTA28NM 20050802000442005080200044EA 2005 8 2 ASOA05559 120050628A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11673BR 7599 DURING A GROUND INSPECTION IN CAE, THE AFT EMERGENCY CEILING LIGHT AS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE AFT EMERGENCY CEILING LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050802000452005080200045EU 2005 8 2 USA2005F00001 120050801A1100 PLACARD AIRBUS320 A320214 3930316EU FUEL FILTER LOOSE A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19115US 1171 AFTER TAKEOFF, THE NR 1 ENGINE FUEL FILTER CLOG MESSAGE ILLUMINATED ON ECAM. ENGINE FUEL FILTER SHOWED EVIDENCE OF PLACARD/LABEL MATERIAL. AIRCRAFT WAS MAINTENANCE FERRIED TO A MAINTENANCE BASE FOR FUEL TANK ENTRY. IN THE LEFT WING, 14 LOOSE PLACARD WERE FOUND AND 6 WERE MISSING. 8 PLACARDS WERE FOUND IN THE LEFT VENT/SURGE TANK. IN THE RIGHT WING, 11 LOOSE PLACARDS WERE FOUND AND 9 WERE MISSING. MAINTENANCE ACCOMPLISHED AIRBUS MANDATORY SERVICE BULLETIN A320-57-1117 AND REMOVED ALL WING TANK PLACARDS/LABELS. (M) 2L72 4F RTA28NM 20050802000462005080200046EU 2005 8 2 USAA050856 120050708A5320D5311281520200 FLOOR SUPPORT AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19108UW18429 1061 PIT - FOUND FLOOR SUPPORT CORRODED 1 INCH IN DIAMETER IN SEVERAL SPOTS, Y1292 BETWEEN C16 AND C20. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M) 2L72 4F RTA28NM 20050802000492005080200049EU 2005 8 2 USAA050862 120050708A53201160852 FLOOR SUPPORT AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19108UW18429 1061 PIT - FOUND FLOOR SUPPORT CORRODED 1 INCH BY 1 INCH BY .070 INCH DEEP, Y495 ABOVE CROSSBEAM C16. REMOVED AND REPLACED IDENTICAL FLOOR SUPPORT PER SRM 51-72-11. CORROSION LEVEL 1, TASK JA-220-53500. (M) 2L72 4F RTA28NM 20050802000502005080200050EU 2005 8 2 USAA050858 120050708A5320D5348004320501 SILL AIRBUS320 A320214 3930316EU DOOR CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19108UW18429 1061 PIT - FOUND DOOR SILL CORRODED 1 INCH, -1732 FLOORBEAM/DOORSILL AT FRAME 66. REMOVED AND REPLACED DOORSILL/FLOORBEAM PER SRM 51-72-11. CORROSION LEVEL 1, TASK JA-260-53500. (M) 2L72 4F RTA28NM 20050802000522005080200052EU 2005 8 2 USAA050873 120050713A5315 FLOORBEAM AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19109UW19030 1065 PIT - FOUND FLOORBEAM CORRODED 1 INCH BY 1.5 INCH AREA, FRAME 66 LEFT SIDE OF DOOR CUTOUT. INSTALLED REPAIR ANGLES AND FILLER PER SRM 53-41-14 REPAIR PRINCIPLE 6. CORROSION LEVEL 1, TASK JA-260-53500. (M) 2L72 4F RTA28NM 20050802000542005080200054EU 2005 8 2 USAA050859 120050708A5315 FLOORBEAM AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19108UW18429 1061 PIT - FOUND FLOORBEAMS CORRODED .5 INCH DIAMETER AROUND 12 NUTPLATES, STATION Y1292 FRAME 66-68. REPLACED FLOORBEAM SECTIONS FROM FRAME 64-70 PER SRM 51-72-11. (M) 2L72 4F RTA28NM 20050802000552005080200055EU 2005 8 2 USAA050855 120050708A5315 FLOORBEAM AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19108UW18429 1061 FOUND FLOORBEAM CORRODED 21 HOLES WITH 1 INCH OF CORROSION, FRAME 66-68 FLOORBEAM Y1292. REMOVED AND REPLACED PER SRM 53-00-15 FIG 201. (M) 2L72 4F RTA28NM 20050802000582005080200058NM 2005 8 2 AWXA200500871 120050707A5311651630086 FRAME BOEING737 7373G7 1384595NM BULKHEAD CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 DURING C16 CHECK DISCOVERED BULKHEAD 178 CHORD CRACKED, 2.2 INCHES IN LENGTH, AT WL 207, BL 27L. MAINTENANCE REMOVED CRACKED CHORD LOCATED AT BULKHEAD 178, WL 207 IAW BOEING 737-300 SRM 51-40-02-0 FIG 8. RECEIVED NEW CHORD AND PREPARED FOR INSTALLATION IAW BOEING 737-300 SRM 51-40-05-0 FIG 2. INSTALLED NEW CHORD AT BULKHEAD 178, WL 207, BL 27L IAW BOEING 737-300 SRM 51-40-02-0 FIGURES 8 AND 12. 2L72 4F RTA16WE 20050802000592005080200059NM 2005 8 2 AWXA200500872 120050708A5312651758351 FRAME BOEING737 7373G7 1384595NM BULKHEAD CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 DURING C16 CHECK, DISCOVERED 178 BULKHEAD CHORD CRACKED IN TWO PLACES, 1.1 INCHES IN LENGTH AND 1.3 INCHES IN LENGTH, AT BS 178, WL 184, BL 5.7L. MAINTENANCE REMOVED BOTH CRACKS ON CHORD LOCATED AT BS 178 BULKHEAD, WL 184, BL 5.7L IAW BOEING 737-300 SRM 53-10-08-2 FIG 205. FABRICATED FOUR REPAIR ANGLES AND TWO REPAIR STRAPS IAW BOEING 737-300 SRM 53-10-08-2 FIG 205. INSTALLED FABRICATED REPAIR PARTS IAW BOEING 737-300 SRM 53-10-08-2 FIG 205. 2L72 4F RTA16WE 20050802000612005080200061EU 2005 8 2 AWXA200500874 120050727A304006282 WINDOW AIRBUS320 A320232 3930326EU COCKPIT FAILED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28669AW12093 1792 PHX - AIR TURN BACK - FLT 570 - DURING TAKEOFF, CREW REPORTED FORWARD WINDSHIELD HEAT INOPERATIVE. RETURNED TO PHX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FORWARD FIXED WINDOW IAW AIRBUS MM 56-11-11-04, OPERATIONAL CHECKS WERE NORMAL. PRIOR TO AIR TURN BACK AND REPLACEMENT OF CAPTAINS WINDOW, WINDOW HEAT CONTROLLER WAS REPLACED IN PHX, FLT 285. WINDSHIELD WAS SCRAPPED AT REPAIR FACILITY. 2L72 4F RTA28NM 20050802000622005080200062NM 2005 8 2 AWXA200500875 120050730A3350D9026 CONNECTOR BOEING737 7373G7 1384595NM EMERGENCY LIGHT LOOSE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 MCN - EEL - DURING C16 CHECK, DISCOVERED SEAT MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROWS 13 THROUGH 26. MAINTENANCE TROUBLESHOT IAW AIRBUS WIRING DIAGRAM MANUAL 33-51-42 AND FOUND LOOSE WIRE CONTACT ON CONNECTOR D9026. RE-INSERTED CONTACT ON CONNECTOR D9026 AS NEEDED. OPERATIONAL CHECKS WERE GOOD IAW TASKCARD A1C33006. 2L72 4F RTA16WE 20050802000652005080200065EU 2005 8 2 AWXA200500878 120050730A3397ABS0374A24 TERMINAL AIRBUS320 A320232 3930326EU EMERGENCY LIGHT INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28640AW 448 ONT - EEL - CREW REPORTED SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING, AT 10D, INOPERATIVE. MAINTENANCE REPLACED TERMINAL IAW STANDARD PRACTICES. OPERATIONAL CHECKS GOOD. 2L72 4F RTA28NM 20050802000702005080200070NM 2005 8 2 UPS05444989 120050722A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 AFT CARGO RT SIDEWALL BS 1620 FRAME WEB FOUND DENT AT RT STA 36 AREA AS MARKED, CRACK LENGTH .750. FRAME WEB REPAIRED AS PER SRM 53-10-04 FIG 66. 2L74 4F A20WE 20050802000712005080200071NM 2005 8 2 UPS05444990 120050725A5347 SEAT TRACK BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 STA 700-710 LBL 66 SEAT TRACK FOUND CORRODED. CORROSION BLEND OUT 0.042 X 1 X 4 EXCEED SRM 53-10-01 FIG 1 LIMIT, SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A. 2L74 4F A20WE 20050802000722005080200072NM 2005 8 2 UPS05444991 120050725A5315 FLOORBEAM BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 BS 360 FLOORBEAM UPPER STRUCTURE HORIZONTAL AFT FLANGE 1EA MOUNTING HOLE CRACK, CRACK LENGTH .125. BS 360 RBL 45 AFTER FLANGE OF FLOORBEAM UPPER STRUCTURE REPAIRED AS PER UPS EO NR B747-5320-12407 APPENDIX 'D' PLAN C. 2L74 4F A20WE 20050802000752005080200075NM 2005 8 2 UPS05544998 120050730A5730 PANEL BOEING757 75724APF 1384969NM RT WING DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01421UP 25281 JUST AFT OF RIGHT WING JACK PAD LWR SURFACE PANEL HAS DELAM. PANEL HAS A 3X4 AREA OF DELAM OUT OF LIMITS PER 57-51-01-1A. SECOND, REMOVED PANEL TO S/M SHOP. THIRD, REMOVED DAMAGE, INSTALLED NEW CORE, INSTALLED PLIES & STARTED CURE SRM 51-70-05-06. REMOVED BAGGING MATERIAL AND HEAT BLANKET, SANDED, PAINTED RESTORED ORIGINAL FINISH PER SRM 51-70-05. INSTALLED PANEL REF SRM 51-40-02. 2L72 4F RTA2NM 20050802000762005080200076WP 2005 8 2 UPS05844995 120050712A53131415997 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 FS 1488 LONG 32L CRACKED ON BACKSIDE OF SPLICE END. REMOVED LONG 32L AND SPLICE END FITTING AT FS 1488 IAW SRM 51-1-21, FABRICATED LONG 32L AND SPLICE END FITTING IAW SRM 53-02-02 FIG 010 AND INSTALLED LONG 32L AND SPLICE END FITTING IAW SRM 51-1-21. 2L74 4F RT4A25 20050802000782005080200078WP 2005 8 2 UPS05845000 120050801A5312 BULKHEAD DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 STAB ACCESS COMPT FWD BULKHEAD LEDGE NR 3 CRACKED AT ANGLE ATTACH, LWR (MARKED). REMOVED LT AFT BULKHEAD WALL PANEL OF MAIN CARGO DECK TO FACILITATE SHEET METAL REPAIR. CONT. TO LP 414978 NR 2: REMOVED RIVETS AND BOLTS FROM PRESS BULKHEAD TO FACILITATE REPAIR. BEGAN FABRICATION OF REPAIR PARTS PER EO DC8-5310-6598C. REPAIRED IN STAB COMP AFT PRESS BULKHEAD "J" BEAM PER EO DC8-5310-6598C. 2L74 4F RT4A25 20050802000792005080200079WP 2005 8 2 UPS05845001 120050729A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 LT UPPER WING PANEL AT T/E IN FRONT OF NR 4 SPOILER HAS SKIN ROLLED UP APPROX 18 - 24 INCHES ALONG AFT EDGE W/APPROX 30 RIVETS PULLED. ROLLED APPX 1.5 - 2 INCHES FWD AT DEEPEST SPOT. REMOVED DAMAGED MATERIAL, INSTALLED REPAIR DOUBLER & ANGLE & SEAL PER EO DC8-5720-22601A. CK'D SPOILER OPERATION PER MM 27-61-01-2. CK'D OK. A/C OK FOR RETURN TO SERVICE. 2L74 4F RT4A25 20050802000802005080200080WP 2005 8 2 AALA20050470 120050726A30202028TP ANTI-ICE SYSTEM DOUG DC9 DC982 3022082WP NR 2 ENGINE INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21275AA 49272 RIGHT ENGINE LOOP-B LIGHT ILLUMINATED APPROXIMATELY 2 TO 3 MINUTES AFTER TAKEOFF. LIGHT STAYED ON FOR VARIOUS AMOUNTS OF TIME ON SEVERAL OCCASIONS. THE RIGHT ENGINE FIRE WARNING LIGHT AND BELL OCCURRED WHEN CONDUCTING THE SINGLE LOOP TEST. LOOP B TESTED OK. MOST OF THE WARNINGS OCCURRED AT HIGH POWER SETTINGS. REPLACED ANTI-ICE TUBE ON NR 2 ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050802000812005080200081WP 2005 8 2 AALA20050473 120050721A3350 LIGHT DOUG DC9 DC982 3022082WP ROW 23-26 INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21499AA 49737 DTW - EMERGENCY EXIT CEILING LIGHTS AT SEAT ROWS 23 TO 26 INOPERATIVE. REPAIRED EMERGENCY EXIT CEILING LIGHTS AT SEAT ROWS 23 TO 26. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050802000822005080200082NM 2005 8 2 AALA20050476 120050614A3397 WIRE BOEING767 767323 1385205NM EMERGENCY LIGHTSBURNED A AALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW21387AM 27184 AFW - CEILING FORWARD OVERHEAD AND MID CABIN LIGHTING PANELS HAD BURNED WIRE, BURNED TERMINALS, AND BURNED TRANSFORMER AT T180. REPLACED TRANSFORMER AND TERMINAL LUGS FOR CEILING FORWARD OVERHEAD AND MID CABIN LIGHTING PANELS AT T180. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050802000852005080200085EU 2005 8 2 AALA20050472 120050712A3350 LIGHT AIRBUS300 A300B4605R 3930308EU ROW 29 INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW2125071 514 MIA - EMERGENCY LIGHTS AT ROW 29 AND AFT INOPERATIVE. REPAIRED EMERGENCY LIGHTS AT ROWS 29 AND AFT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20050802000872005080200087NM 2005 8 2 AALA20050475 120050520A5330 SKIN BOEING767 767323 1385205NM FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21368AA 25195 AFW - FUSELAGE SKIN AT STATION 1219 AND 537 LEFT HAS CRACK. AREA IS 2 INCHES BY 11.7 INCHES. CUT OUT CORROSION AND FABRICATED AND INSTALLED DOUBLERS. 2L72 4F RTA1NM 20050802000922005080200092EU 2005 8 2 AWXA200500884 120050712A5320D53471124201 WEB AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28627AW 66 DURING C4 CHECK DISCOVERED EXFOLIATION CORROSION ON WEB, LOCATED AT -Y1180, FROM FS 69 TO FS 70. MAINTENANCE REMOVED CORRODED WEB FROM FS 69 TO FS 70, -Y1180 IAW AIRBUS SRM 51-72-11 PAGE 1 AND 2. INSTALLED NEW WEB IAW AIRBUS SRM 51-72-11 PAGES 1 AND 2. 2L72 4F RTA28NM 20050802000942005080200094EU 2005 8 2 AWXA200500886 120050712A5320D533112712200 FLOOR SUPPORT AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28627AW 66 DURING C4 CHECK, DISCOVERED CORROSION AT LONGITUDINAL FLOOR SUPPORT, LOCATED AT -Y81, FR 14. NO ALLOWABLE LIMITS FOUND. MAINTENANCE REMOVED FLOOR SUPPORT AT -Y81, FR 14 IAW AIRBUS SRM 51-42-11. INSTALLED NEW FLOOR AT -Y81, FS 14 BEAM IAW AIRBUS SRM 51-42-11. 2L72 4F RTA28NM 20050728000332005072800033NM 2005 7 28 0501146718 120050708A2810 FUEL CELL BOEING747 747251F 1384898NM LEAKING A NWAAC ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 GL01618US 21122 DURING TAKE-OFF THERE WAS A STRONG FUEL ODOR IN COCKPIT. SMELL CLEARED ONCE PACKS WERE TURNED ON. AIRCRAFT CONTINUED ON TO DESTINATION AND LANDED WITHOUT INCIDENT. ANC MAINTENANCE FOUND LEAK ON SEAM 15 INCHES AHEAD OF NR 2 SUMP DRAIN, AND SEALED EXTERNAL TANK AREA LEAK. FUELED TANKS TO 30,000LBS NO LEAKS FOUND. AIRCRAFT OK FOR RETURN TO SERVICE. 2L74 4F A20WE 20050728000432005072800043NM 2005 7 28 USAA050739 120050608A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU 23861 CLT - FOUND SKIN GOUGED 1 INCH BY 5 INCH, BS 500C BETWEEN S 1-S 2R. INSTALLED DOUBLER IAW SRM 53-00-01 FIG 29. (M) 2L72 4F RTA16WE 20050728000492005072800049NM 2005 7 28 P5CA0501381 120050724A242028B2631B GENERATOR BOEING747 74746NF 13848BTNM NR 1 INOPERATIVE A P5CAO OTHER O OTHER TXTAXI/GRND HDL 1 EA15452PA 30810 NR 1 GEN ON APU INOP. "CORRECTIVE ACTION": REPLACED NR 1 GENERATOR. OPS CHECK OK PER MM 24-21-03. 2L74 4F RTA20WE 20050728000542005072800054NM 2005 7 28 USAA050750 120050609A5240 SKIN BOEING737 737301 1384611NM SERVICE DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19575US 23740 CLT - FOUND FORWARD SERVICE DOOR SKIN CRACKED .620 INCH, UPPER HINGE CUTOUT. REPAIR DOUBLER INSTALLED IAW TR 52-10-13. (M) 2L72 4F RTA16WE 20050728000552005072800055EU 2005 7 28 YENA200542 120050720A2121EVT3454H FAN AIRBUS320 A320232 3930326EU AVIONICS BAY FROZEN A YENAA UNSCHED LANDING EB VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA15524JB16370 1528 IT WAS REPORTED SLIGHT VIBRATION AND FAINT ODOR, POSSIBLY ELECTRICAL. VENT BLOWER FAN FAULT. THE AIRCRAFT RETURNED TO MCO. THE VENT BLOWER FAN WAS PLACED ON MEL 21-26-01 C AND REPLACED AT LGB. 2L72 4F RTA28NM 20050728000582005072800058NM 2005 7 28 USAA050749 120050609A5320 ANGLE BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU 23861 CLT - FOUND L-ANGLE CRACKED 4 INCHES, RT SIDE STATION 291.5-295.5 AT FLOOR LEVEL. REMOVED DAMAGED. FABRICATED AND INSTALLED REPAIR PART IAW BOEING DWG 69-37402. (M) 2L72 4F RTA16WE 20050728000602005072800060EA 2005 7 28 COMA0560406 120050724A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01975CA 7150 FLIGHT 5497- FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2L72 4F RTA21EA 20050728000682005072800068EA 2005 7 28 COMA0560408 120050725A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01976CA 7151 FLIGHT 5137- RECEIVED A FLAP FAIL CAUTION DURING CVG APPROACH. AIRCRAFT LANDED WITHOUT INCIDENT. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE FIRST ENVENT MAINTENANCE ACTION PARAGRAPH (B) 1,2,3, (A,B,C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2L72 4F RTA21EA 20050728000752005072800075NM 2005 7 28 PIDA20050061 120050725A5330 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05390WL 23219 CRACK IN FUSELAGE SKIN JUST BELOW STR.18LT AT APROXIMATE BS797. REPAIRED IN ACCORDANCE WITH SRM 53-00-01. 2L72 4F RTA16WE 20050729000102005072900010EA 2005 7 29 QXEA20051138 120050722A2750 FLAP SYSTEM CNDAIRCL600 CL6002C10 1390015EA TE FLAPS MALFUNCTIONED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09611QX 10041 DEN- ON FLIGHT 4277, DURING TAXI OUT, THE FLAP FAULT STATUS MESSAGE ILLUMINATED. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE RESET THE SYSTEM PER THE PROCEDURES IN THE AMM. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2L72 4F RTA21EA 20050729000122005072900012WP 2005 7 29 ASMF200507020 120050725A3220 STRUT DOUG DC9 DC987 3022087WP NLG UNDERSERVICED W ASMFD RETURN TO BLOCK E VIBRATION/BUFFET TXTAXI/GRND HDL 1 SW231075T 49724 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF STRONG NOISE IN THE NOSE LANDING GEAR. THE NOSE LANDING GEAR INSPECTION WAS PERFORMED IAW 32-20-00, ALL CORRECT. THE STRUT WAS SERVICED IAW MM 32-21-02, TESTED CORRECT. 2L72 4F RTA6WE 20050729000182005072900018NM 2005 7 29 05FDEA02091 120050725A5330 SKIN BOEING727 727200 138407ENM N/A CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 PREVIOUS REPAIR IS CHAFED AT BS 720D 12, STRINGER 19 LEFT. REPLACED CHAFFED REPAIR AT BS 720D 12, STR 19L, IAW SRM 51-10-1 AND 51-10-2. (CLOSED) 2L73 4F RTA3WE 20050729000262005072900026EA 2005 7 29 ASOA05590 120050711A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11847AS 7335 FLT 4637 - DURING A GROUND INSPECTION IN DSM, THE EMERGENCY FLOOR TRACK LIGHTING FROM THE GALLEY TO ROW 6 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR TRACK LIGHTING POWER STRIP FROM THE GALLEY TO ROW 6. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050729000302005072900030EU 2005 7 29 05FDEA02093 120050725A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU MCD FLOOR CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25670FE 777 SEAT TRACK BL-0 FR 72.5 CORRODED OUT OF LIMITS. CUT OUT THE DAMAGED SEAT TRACK SECTION IAW SRM 53-10-16. FABRICATED NEW SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW SRM 53-10-16 REF TRAVELER T5/533030. 2L72 4F RTA35EU 20050729000412005072900041EA 2005 7 29 ASOA05585 120050708A33506100976 LAMP CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11705EV 10051 DURING HANGAR MAINTENANCE IN BTR, THE AFT MOST EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE AFT MOST EMERGENCY CEILING LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050729000502005072900050NM 2005 7 29 DU4R0507164 120050728A5320 SHEAR WEB BOEING757 757232 1384965NM FUSELAGE CORRODED B DU4RK NONE O OTHER ININSP/MAINT 1 SO15624DL 22914 CORROSION IN SHEAR WEB SURFACE FROM BS 1681.8 - 1720 BL 0 - BL 60R INCLUDING FASTENERS. 2L72 4F RTA2NM 20050729000552005072900055NM 2005 7 29 05FDEA02110 120050727A5320 SPLICE DOUG MD11 MD11F 3023600NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 FORWARD CARGO: BILGE AREA STA 830 L52 LONGERON SPLICE FOUND CORRODED. REMOVED AS PER SRM 51-33-01 VOL. II. NEW SPLICE MACHINED AS PER DWG ADA7225. FPI CARRIED OUT AS PER DPS 4.707 AND NO CRACK INDICATION FOUND ON NEW SPLICE. NEW SPLICE INSTALLED AS PER SRM 51-33-01 VOL.II. THIS REPAIR CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050729000582005072900058NM 2005 7 29 05FDEA02113 120050727A5320 SPLICE DOUG MD11 MD11F 3023600NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 CENTER CARGO, STA 1531 L45L LONGERON SPLICE FOUND CRACKED. CORRECTIVE ACTION: SRNM N1037: NEW LONGERON SPLICE FABRICATED AS PER DRAWING NO. A5A7116. CRACKED LONGERON SPLICE ON CTR CARGO STA. 1531 LONGERON 45 LH REMOVED AND REPLACED AS PER SRM 51-33-01 VOL. II. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050801000322005080100032EA 2005 8 1 A6WA200540239 120050713A5310 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT FS 484 CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31409AW 7447 RT SIDE FS 484 INTERCOSTAL IS CRACKED AT RBL 36. CRACK IS APPROX 0.4 INCH LONG. REPAIRED RT SIDE FS 484 INTERCOSTAL IAW MFG REO. (K) 2L72 4F4 FRTA21EA E15NE 20050729000882005072900088GL 2005 7 29 ALGA104485 220050706A7230230765591 SPLINE ADAPTER CLARK 1000 1000CLARK 2230102SW ALLSN 250C 250C30 03013GL ENGINE DAMAGED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03 INTERNAL SPLINES OVER MAX SPECS. / REPLACED WITH NEW PART 1Q71 3R3 U 2A6 E1GL 20050729000902005072900090GL 2005 7 29 ALGA104483 220050707A725023053299 TURBINE WHEEL CLARK 1000 1000CLARK 2230102SW ALLSN 250C 250C30 03013GL ENGINE CRACKED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03PARTO WHEEL ASSY WAS RUN ON TEST CELL WITH TURBINE ASSY S/N CAT-90323, FOUND TO HAVE HEAVY N1 RUB AT SHUT DOWN FROM 25-28 SEAL BOAR WARP. DIASSEMBLE TO REPAIR, FOUND WHEEL TO HAVE CRACKS IN COATING ON TE AND RAW END ON LE OF BLADE. FOUND BLADE TIP ARE NOT ROUND. / REMOVED TURBINE ASSY SENT BACK TO AVIALL FOR WARRANTY. 1Q71 3R3 U 2A6 E1GL 20050729000952005072900095EU 2005 7 29 MHIA104942 120050721A5302355A1405220202 SKIN AEROSPAS355 AS355F1 8680810EU TAILBOOM CRACKED B MHIAK NONE O OTHER ININSP/MAINT 1 EA25406LH 5111 DURING INSPECTION FOUND THE UPPER STABILIZER FIN, RIGHT HAND LOWER DOUBLER AND NOSE SKIN CRACKED FROM THE 2ND FORWARD RIVIT OF THE DOUBLER ACCROSS THE NOSE SKIN. REPLACED STABILIZER WITH SERVICEABLE STABILIZER. 1G72 3U H11EU 20050729000982005072900098GL 2005 7 29 YTRR104954 220050721A732323065121 GOVERNOR BELL 206 206B3 1181506SW ALLSN 250C 250C47B GL ENGINE UNSERVICEABLE B YTRAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 SW03209RA564 2091 CAE847645 CANNOT ADJUST RPM. REPLACED GOVERNOR. 1G71 3U3 U H2SW E1GL 20050729001012005072900101EA 2005 7 29 A6WA200540234 120050713A4990 A/C PACK CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RIGHT LEAKING A A6WAO OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL31408AW 7568 CABIN FILLED WITH SMOKE WHILE AT GATE WITH ENGINES OFF, APU AND BOTH PACKS RUNNING. INSPECTED AFT EQUIPMENT BAY AND FOUND AIR LEAK RT PACK WATER SEPARATOR PIPE. NO EVIDENCE OF SMOKE WITH APU AND BOTH PACK ON. (K) 2L72 4F4 FRTA21EA E15NE 20050729001122005072900112EA 2005 7 29 ASOA05576 120050702A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA MAIN PAX LACK OF LUBE A ASOAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO11830AS 7236 FLT 4455 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WAS FOUND EXTREMELY DIFFICULT TO OPEN. MAINTENANCE LUBRICATED THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050801000112005080100011WP 2005 8 1 UPS05844985 120050710A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE: C1, CORROSION ON FLOORBEAM AT STA 60 RBL 45. REMOVED DAMAGE ON UPPER TEE CAP OF FLOORBEAM, FABRICATED AND INSTALLED REPAIR IAW SAA SK 851-857217. 2L74 4F RT4A25 20050801000162005080100016NM 2005 8 1 05FDEA02120 120050727A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25280FE 22347 FLOORBEAM AT STA. 720A RBL 18-22 HAS CORROSION ON UPPER CAP. REPAIRED FLOORBEAM IAW SRM 53-10-8 FIG 3 THIS IS A MAJOR REPAIR. 2L73 4F RTA3WE 20050801000192005080100019NM 2005 8 1 05FDEA02123 120050727A5347606549 SEAT TRACK BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25280FE 22347 SEAT TRACK STA 344-480 RBL 45 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2. 2L73 4F RTA3WE 20050801000282005080100028NE 2005 8 1 AALA20050465 220050723A7261 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE ZONE 600 LEAKING A AALAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 SW217519A 49896 725705 CLT INFLT T2288/23JUL ON DECENT TO CLT RT ENGINE OIL QUANTITY DROPPED TO ZERO. OIL TEMPERATURE BEGAN TO RISE INTO AMBER. N1 AND N2 APPEARED NORMAL. FOUND OIL LEAK IN NUMBER 6 BEARING COMPARTMENT. REPLACED RIGHT ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F4 F A6WE E9NE 20050801000312005080100031 2005 8 1 AALA20050462 420050701A2565D30656126 SLIDE BOEING757 757223 1384957NM L4 DOOR DISCHARGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21622AA 24580 SFO LT NR 4 DOOR EMERGENCY SLIDE BOTTLE PRESSURE NOT IN GREEN ZONE. REPLACED EMERGENCY SLIDE FOR LT NR 4 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA2NM 20050801000372005080100037WP 2005 8 1 ABXA050178 120050726A3297 WIRE DOUG DC8 DC863 302198AWP MLG CONNECTOR BROKEN A ABXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL23817AX 45928 PLACING GEAR HANDLE DOWN, NOSE GEAR LIGHT WOULD NOT COME ON WITH NO RED UNSAFE LIGHT. PERFORMED GEAR RECYCLE, VERIFIED. FOUND BROKEN WIRE AT CONNECTOR P1-215, PIN 6 WIRE NO G323G20 AT NOSE LANDING GEAR DOWN LIMIT SWITCH. REPLACED RECEPTICAL AT P1-215 IAW DC-8 WDM 32-61-01. OPS CHECKED GOOD. 2L74 4F 4A25 20050801000542005080100054NM 2005 8 1 05FDEA02139 120050729A3230 ACCESSORY UNIT BOEING727 727227 1384078NM MLG MALFUNCTIONED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25492FE 21530 AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RAISE PAST THE OFF POSITION. JACKED A/C REF 727 MM 07-11-000-2, ATTEMPTED TO RETRACT LANDING GEAR BUT UNABLE TO RAISE THE HANDLE PAST THE OFF POSITION WITHOUT PULLING THE OVERIDE. REMOVED AND REPLACED THE LANDING GEAR ACCY UNIT REF 727 MM 32-09-121-4, OPS CHK GOOD, OK FOR SERVICE. 2L73 4F A3WE 20050801000592005080100059EU 2005 8 1 MALA050612 120050726A28100733053 SEAL BAC 146 AVRO146RJ85A1500097EU FUEL SYSTEM LEAKING A MALAK NONE K FLUID LOSS ININSP/MAINT 1 GL15501XJ E2208 LEFT WING, FUEL TANK WATER DRAINS AT RIBS 20 AND 18 ARE LEAKING FUEL. REPLACED SEALS P/N'S 0733053 ANS FRS40101A018 IAW AMM 28-11-24 201 AND 28-11-27 201. LEAK CHECK TRANSFERRED TO 409 NR 220349. 2H74 4F RTA49EU 20050801000602005080100060EU 2005 8 1 MALA050614 120050727A5522 SKIN SAAB SF340 340B 7860101EU RT ELEVATOR DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15370PX 340B300 WARRANTY, 4Y/2Y RT ELEVATOR UPPER SURFACE HAS COMPOSITE DAMAGE 68 INCHES FROM I/B END. REPAIRED IAW MESABA EO NR S51031. REMOVED AND REINSTALLED ELEVATOR. 2L72 4T RTA52EU 20050801000632005080100063NM 2005 8 1 SB05087 120050801A3397 WIRE BOEING737 7374B7 1384702NM SEAT ROW 5 BROKEN A USAAK NONE O OTHER ININSP/MAINT 1 EA19432US 24554 PHL - MAINTENANCE REPORTED, THE EMERGENCY EXIT SIGN, AT SEAT ROW 5, INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050801000682005080100068EU 2005 8 1 MALA050618 120050726A5320 FLOOR SUPPORT BAC 146 AVRO146RJ85A1500097EU FUSELAGE DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15504XJ E2311 WHILE ACCOMPLISHING C2 INSPECTION, FOUND A FLOOR SUPPORT ANGLE CRACKED AT FRAME 14 AND CENTER LINE IN THE ELECTRICAL EQUIPMENT BA. 2H74 4F RTA49EU 20050801000692005080100069EU 2005 8 1 MALA050617 120050729A5220 DOOR SAAB SF340 340B 7860101EU EMERGENCY EXIT LOOSE A MALAK NONE O OTHER ININSP/MAINT 1 GL15368PX 340B274 6C EMERGENCY EXIT LOOSE IN FRAME. 2L72 4T RTA52EU 20050801000702005080100070EU 2005 8 1 MALA050616 120050728A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15452XJ 340B452 SEAT TRACK AT BL 0 FROM FS 294 TO FS 310 IS CORRODED AND HAS BEEN REPAIRED IAW SRM 53-70-60. REF EAMS WORK ORDER 212637 TASK 1509. 2L72 4T RTA52EU 20050801000712005080100071SO 2005 8 1 C2XA05SD024 120050702A2560 BATTERY EMB 145 EMB145XR 3260214SO FLASHLIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2734110 145658 AFT FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY. OPS CK GOOD AIRCRAFT RELEASED AND RETURNED TO SERVICE. 2L72 4F RT 20050801000782005080100078NM 2005 8 1 QXEA200501141 120050722A7921D2887355C VALVE BOMBDRDHC8 DHC8402 1390042NM ZONE 100 INOPERATIVE A QXEAO OTHER MJ OVER TEMP WARNING INDICATION CLCLIMB 1 NM09409QX 4051 SEA-ON FLIGHT 2328, NR 2 OIL TEMPERATURE ROSE TO 108 DEGREES. CLOSED BYPASS DOOR PER CHECKLIST AND TEMPERATURE LOWERED TO 104 DEGREES. TEMPERATURE DECREASED A LITTLE MORE DURING CRUISE BUT KEPT A 15 DEGREE TO 20 DEGREE SPLIT FROM NR 1 OIL TEMERATURE. REMOVED AND REPLACED NR 2 OIL COOLER VALVE. GROUND RAN AIRCRAFT AT DIFFERENT POWER SETTINGS. ALL INDICATIONS WERE FOUND TO BE NORMAL. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050801000812005080100081EU 2005 8 1 05FDEA02135 120050728A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25670FE 777 SEAT TRACK AT Y953 FR 17-19 IS CORRODED 2L72 4F RTA35EU 20050802000082005080200008EA 2005 8 2 A6WA200540242 120050714A3260764808 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE MLG FAILED A A6WAO OTHER N FALSE WARNING CLCLIMB 1 GL31467AW3905 7900 ON GEAR RETRACTION, GEAR DISAGREE WARNING MESSAGE. COMPLIED WITH QRH. DOWNLOADED FDR AND FOUND BOTH LT AND RT MLG UPLOCKS INTERMITTENT UPA AND LOCKED. SUSPECT BAD PSEU, REMOVED AND REPLACED PSEU IAW MM. OPS CHECK GOOD. PERFORMED FUNCTION CHECKS OF LANDING GEAR EXTENSION AND RETRACTION IAW MM. CHECK GOOD. (K) 2L72 4F4 FRTA21EA E15NE 20050802000092005080200009NM 2005 8 2 CLC2005F00003 120050721A2720S4913803CS19320 CONTROL CABLE DOUG DC10 DC1040F 3023507NM PWA JT9 JT9D* NE RUDDER CORRODED A CLCAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 SO29140WE 46920 DURING PREFLIGHT, FOUND RUDDER NOSE RIGHT CABLE 2D BROKEN. FOUND RT RUDDER CONTROL CABLE 2D CORRODED AND BROKEN. REMOVED AND REPLACED RUDDER CONTROL CABLE NOSE RT 2D IAW AMM. ACCOMPLISHED RUDDER CONTROL SYSTEM OPERATIONAL, CHECK AND FOUND NORMAL. AIRCRAFT RETURNED TO REVENUE SERVICE. (K) 2L73 4F4 FRTA22WE E20EA 20050802000112005080200011EA 2005 8 2 A6WA200540261 120050725A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31405AW 7362 FS 280, RBL 9, IB CLIP ANGLE IS CRACKED 1 INCH LONG. REMOVED AND REPLACED FS 280, RBL9, IB CLIP IAW SRM. (K) 2L72 4F4 FRTA21EA E15NE 20050802000232005080200023SO 2005 8 2 Z8T2005F00000 220050716A8500TSIO520E ENGINE CESSNA402 402B 207590PCE CONT O520 TSIO520E 17040SO MCAULY3AF32C3AF32C87 GL SEIZED E Z8TAO OTHER O OTHER NRNOT REPORTED 1 WP133949C 23 402B0826 182962R 780701 DURING ENGINE GROUND RUN ENGINE QUIT OPERATING. POST RUN-UP INSPECTION MECHANIC WAS UNABLE TO ROTATE PROPELLER. AIRPLANE WAS FERRIED AND HAD BEEN FLOWN FOR A FEW HOURS PRIOR TO FERRY. ENGINE HAD VIBRATION WHEN RECEIVED FROM FERRY PILOT. 1L72 3O3 O A7CE E8CE 5 CP22EA 20050802000412005080200041EA 2005 8 2 ASOA05557 120050627A5210601R3177351 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11846AS 7328 DURING HANGAR MAINTENANCE IN BTR, THE TOP STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLIED THE TOP STEP ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20050802000482005080200048CE 2005 8 2 AOQ2005F00004 120050720A260024407235 FIRE DETECTOR LEAR 35 31A 5170531CE NR 1 ENGINE MALFUNCTIONED A AOQAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA1139TW 047 DURING CLIMB, NR 1 ENGINE FIRE WARNING LIGHT ILLUMINATED AT ITT 802 DEGREES, REDUCED TO 760 DEGREES, LIGHT EXTINGUISHED. ENGINE INDICATIONS WERE NORMAL. VISUALLY INSPECTED BLEED AIR PLUMBING AND ELECTRICALLY RUNG OUT FIRE WARNING CIRCUIT. FOUND AFT FIRE ELEMENT BELOW MFG. REQUIREMENTS. REPLACED AFT FIRE ELEMENT. ALL CHECKS NORMAL. (M) 2L72 4F RTA10CE 20050802000642005080200064EU 2005 8 2 AWXA200500877 120050729A3350321431 BATTERY AIRBUS320 A320231 3930325EU EMERGENCY LIGHT DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28634AW 091 LAS - EEL - DURING 8 DAY CHECK, DISCOVERED AFT LEFT EMERGENCY LIGHT BATTERY PACK INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT LEFT EMERGENCY BATTERY PACK IAW AMM 33-51-38. OPERATIONAL CHECKS GOOD. 2L72 4F RTA28NM 20050802000672005080200067EU 2005 8 2 AWXA200500880 120050713A5340D5311X1982005 FITTING AIRBUS320 A320231 3930325EU DOOR SILL CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28627AW 66 DURING C4 CHECK, DISCOVERED CORROSION AROUND HOLES ON R1 DOOR LOWER SILL FROM FS 16 TO FS 20. NO ALLOWABLE LIMITS EXIST. MAINTENANCE REMOVED AND REPLACED THE FITTINGS ON R1 DOOR LOWER SILL IAW AIRBUS 320 SRM 51-72-11. 2L72 4F RTA28NM 20050802000832005080200083EU 2005 8 2 AALA20050468 120050727A3350 LIGHT AIRBUS300 A300B4605R 3930308EU EMERGENCY EXIT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2170079 619 JFK - EMERGENCY EXIT SIGN AT ONE LEFT DOOR INOPERATIVE. RESET EMERGENCY LIGHT EXIT SIGN SYSTEM AT ONE LEFT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20050802000892005080200089NE 2005 8 2 HXSA0508001 220050725A7250 TURBINE WHEEL SNIAS 350 AS350B 8680801EU TMECA ARRIELARRIEL1B 6OO30NE ENGINE FAILED G HXSABA EMER. DESCENT UNSCHED LANDING XAJENGINE FLAMEOUT FLAME/FIRE WARNING INDICATION CLCLIMB 1 AL0557958 1512 909 AS-350 CRASHED IN BOGGY TERRAIN WHILE DEPARTING JUNEAU AIRPORT. AIRCRAFT HAD SUBSTANTIAL DAMAGE. IT APPEARS THAT AFTER TAKEOFF THE TURBINE BLADE OR BLADES CAME APART IN THE ENGINE AND SMOKE/FIRE WAS OBSERVED FROM PERSONS ON THE GROUND RESULTING IN AUTOROTATION, EMERGENCY HARD LANDING. THIS HAPPENED JUST AFTER THE INITIAL LIFTOFF FROM THE HELIPORT AND ATTAINING ABOUT 100 FEET ALTITUDE. ENGINE SENT TO TMECA FOR REPORT OF DAMAGE/REASON. SOME UNKNOWNS AT THIS TIME. 1G71 3U3 U H9EU E19EU 20050802000932005080200093EU 2005 8 2 AWXA200500885 120050712A5320D53475575208 THRESHOLD AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28627AW 66 DURING C4 CHECK DISCOVERED CORROSION ALONG LOWER SILL THRESHOLD SHEET IN THE AFT CARGO COMPARTMENT FROM FS 52+9.5 TO FS 56. MAINTENANCE REMOVED LOWER SILL THRESHOLD SHEET IN THE AFT CARGO COMPARTMENT IAW AIRBUS SRM 51-42-11 PAGE 2. FABRICATED NEW THRESHOLD SHEET IAW AIRBUS DRAWING NR D53475575. INSTALLED FABRICATED REPAIR PARTS AT LOWER SILL IN THE AFT CARGO COMPARTMENT FROM FS 52+9.5 TO FS 56 IAW AIRBUS SRM 51-42-11. 2L72 4F RTA28NM 20050802000952005080200095EU 2005 8 2 AWXA200500887 120050712A5320D53472189202 DUMMY RAIL AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28627AW 66 DURING C4 CHECK DISCOVERED GALVANIC CORROSION ON DUMMY RAIL FROM FS 66+5 TO FS 68-5, FROM -Y1170 TO -Y1292. REMOVED CORROSION FROM DUMMY RAIL, FROM FS 66+5 TO FS 68-5, FROM -Y1170 TO -Y1292 IAW AIRBUS 320 SRM 51-74-00. REWORK FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-14. REMOVED DUMMY RAIL FROM FS 66+5 TO FS 68-5, FROM -Y1170 TO -Y1292 IAW AIRBUS 320 SRM 51-42-11. PREPARED NEW DUMMY RAIL FOR INSTALLATION IAW AIRBUS 320 SRM 51-49-11. REPAIR PARTS INSTALLED FROM FS 66+5 TO FS 68-5, FROM -Y1170 TO -Y1292 IAW AIRBUS 320 SRM 51-42-11. 2L72 4F RTA28NM 20050802000982005080200098EU 2005 8 2 AWXA200500890 120050712A5320D53472189202 FLOOR SUPPORT AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28627AW 66 DURING C4 CHECK, DISCOVERED CORROSION ON LONGITUDINAL BEAM BETWEEN FS 65-5 TO FS 69+4, -Y1170. REMOVED CORROSION IAW A320 SRM 51-74-00 AND WAS FOUND TO BE OUT OF LIMITS. REMOVED BEAM BETWEEN FS 65-5 TO FS 69+4 IAW AIRBUS 320 SRM 51-42-11. NEW BEAM WAS PREPARED FOR INSTALLATION IAW A320 SRM 51-44-11. INSTALLED REPAIR PARTS BETWEEN FS 65-5 TO FS 69+4 IAW A320 SRM 51-42-11 AND 51-21-11. 2L72 4F RTA28NM 20050802000992005080200099EU 2005 8 2 AWXA200500891 120050801A3397A9299304600600 WIRE HARNESS AIRBUS320 A320231 3930325EU EMERGENCY LIGHT SHORTED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28636AW 098 ORD - EEL - DURING 4 DAY CHECK, DISCOVERED EMERGENCY EXIT LIGHTING AT LT FORWARD EXIT ROW INOP. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY AND WIRING HARNESS IAW AIRBUS MM 33-51-19-04. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA28NM 20050802001002005080200100EU 2005 8 2 AWXA200500892 120050712A5320D5348004800104 STRUCTURE AIRBUS320 A320231 3930325EU R2 DOOR WAY CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28627AW 66 DURING C4 CHECK, DISCOVERED CORROSION ON EXTRUSION AT R2 DOOR CUTOUT, BETWEEN FS 66 +5, AND FS 68 -5, BL -Y1465. MAINTENANCE REMOVED CORRODED EXTRUSION AT R2 DOOR CUTOUT BETWEEN FS 66 +5 AND FS 68 -5 IAW AIRBUS 320 SRM 51-42-11. INSTALLED NEW EXTRUSION AT R2 DOOR CUTOUT BETWEEN FR 66 +5 AND FR 68 -5 IAW SRM 51-42-11. 2L72 4F RTA28NM 20050802001012005080200101EU 2005 8 2 AWXA200500893 120050712A5320D347218820200 FLOOR SUPPORT AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28627AW 66 DURING C4 CHECK, DISCOVERED CORROSION ON LONGITUDINAL BEAM BETWEEN FS 68 TO FS 69, BL +Y1170. REMOVED CORROSION IAW A320 SRM 51-74-00 AND WAS FOUND TO BE OUT OF LIMITS. REMOVED BEAM BETWEEN FS 68 TO FS 69 IAW AIRBUS 320 SRM 51-42-11. NEW BEAM WAS PREPARED FOR INSTALLATION IAW A320 SRM 51-44-11. INSTALLED REPAIR PARTS BETWEEN FS 68 TO FS 69, BL +Y1170 IAW A320 SRM 51-42-11 AND 51-21-11. 2L72 4F RTA28NM 20050802001022005080200102NM 2005 8 2 0501176302 120050730A2520E65EFR5156B CONTROL UNIT BOEING747 747451 1384940NM SEAT BURNED A NWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL01662US 23720 FLIGHT ATTENDANT REPORTED A BURNING ELECTRICAL ODOR BY ROW 80. MEL`D SEATS 80J&K. DTW - MAINTENANCE 01AUG05, REMOVED AND REPLACED ECU (SEAT ELECTRONIC CONTROL UNIT), AND RECALIBRATED SEATS. OPERATIONAL CHECKED GOOD, REMOVED MEL'S. 2L74 4F RTA20WE 20050802001052005080200105NM 2005 8 2 CALA0500239 120050730A53306545744 SKIN BOEING737 7373TO 138447GNM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770353 23591 A 2 INCH CRACK WAS FOUND IN FUSELAGE SKIN BELOW THE LT REAR EXTERIOR EMERGENCY EXIT LIGHT, STA 727D - 727E, S23L DURING WALKAROUND. DOUBLERS WERE INSTALLED IAW ECRA 5330-03469. A DIP WAS ISSUED TO PERFORM AN INITIAL INSPECTION WITHIN 60,000 FLIGHT CYCLES FROM REPAIR INSTALLATION AND TO ACCOMPLISH SUBSEQUENT REPEAT INSPECTIONS EVERY 25,000 FLIGHT CYCLES. 2L72 4F RTA16WE 20050802001062005080200106NM 2005 8 2 CALA0500240 120050730A5320141A541012 INTERCOSTAL BOEING737 737724 13844BYNM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2725705 28766 INSPECTION FOUND A 1INCH CRACK IN INTERCOSTAL BETWEEN FLOORBEAM AT STA 312-328, RBL 40. A REPAIR WAS PERFORMED IAW SRM 51-40-02. 2L72 4F RTA16WE 20050802001112005080200111NM 2005 8 2 CALA0500245 120050731A5320147A56602 FLOOR SUPPORT BOEING737 737724 13844BYNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2725705 28766 INSPECTION FOUND FLOOR SUPPORT BETWEEN FLOORBEAM AT STA 947-967, RBL 62 (LAV E) CORRODED. REPAIRED FLOOR SUPPORT IAW ECRA 5321-01265. 2L72 4F RTA16WE 20050802001122005080200112NM 2005 8 2 CALA0500246 120050731A5320147A56601 INTERCOSTAL BOEING737 737724 13844BYNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2725705 28766 INSPECTION FOUND INTERCOSTAL CORRODED AROUND TWO NUTPLATES I/B OF L-2 DOOR AT STA 947.5-967, LBL 62. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20050802001132005080200113NM 2005 8 2 CALA0500247 120050731A5320147A56765 FLOOR SUPPORT BOEING737 737724 13844BYNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2725705 28766 INSPECTION FOUND FLOOR SUPPORT CORRODED AT SEVERAL FASTENER HOLES I/B OF L-2 DOOR AT STA 947.5-967, LBL 45 TO LBL 62. REPLACED FLOOR SUPPORT IAW ECRA 5321-01263. 2L72 4F RTA16WE 20050802001152005080200115WP 2005 8 2 ASMF200507025 120050731A291039271012 VALVE DOUG DC9 DC987 3022087WP RIGHT AUGMENTATIFAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION CLCLIMB 1 SW23751RA44366357 49779 ACFT RETURNED OF FLT AS A CONSEQUENCE OF RT VELOCIMETER OSCILLATED FROM 0-400 KTS & ALARM ACTIVATED. DIRECTOR BUSS DISAPPEARED IN BOTH PFD AND FMA W/O IND, AUTOMATIC ACCELERATORS DISCONNECTED, MACH TRIM LIGHT TURNED ON INFLT, AUTOPILOT DISENGAGED FREQUENTLY & "R AIR COND TEMP HI" LIGHT TURNED ON AFTER T/O. DURING MX REVISION DETECTED THAT DYNAMIC HOSE LOOSE, TIGHTENED & TESTED IAW MM, ALL CORRECT. DIRECTOR OF FLT SYS, AUTO ACCELERATORS, MACH TRIM SYS, AUTOPILOT SYS CHECKED IAW MM. AIR COND TEMP HI LIGHT DEFERRED IAW MEL 21-01. DURING OVERNIGHT SERVICE, AUGMENTATION VALVE, HI SENSOR, THERMAL SWITCH AND THERMOSTAT WERE REPLACED IAW MM 36-10-01, TESTED CORRECT. DEFERRED REPORT WAS CLOSED. 2L72 4F RTA6WE 20050802001172005080200117 2005 8 2 IXXA0500089O 420050801A344220671570153 TRANSCEIVER DOUG DC8 DC862F 3021972WP WX RADAR SYS NO INDICATION A IXXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW11799AL76548136 45922335 IN CLIMB FROM KWRI, THE AIRCRAFT'S WEATHER RADAR WOULD NOT PAINT WEATHER OR GROUND. CREW RETURNED AIRCRAFT TO KWRI AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE WEATHER RADAR TRANCEIVER AND WEATHER RADAR ANTENNA. THE SYSTEMS OPERATIONAL CHECK AND SELF-TEST WERE GOOD PER ALL APPLICABLE MANUALS AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F 4A25 20050802001212005080200121NM 2005 8 2 CLC2005F00004 120050711A7160ATL7105 ADAPTER RING DOUG DC10 DC1040F 3023507NM PWA JT9 JT9D* NE NR 2 BELLMOUTH DAMAGED A CLCAK NONE O OTHER ININSP/MAINT 1 SO29140WE59475 46920 DURING PREFLIGHT CHECK, DAMAGE WAS FOUND TO NR 2 ENGINE INTAKE AND FAN BLADES. ENGINE INTAKE HAS DAMAGE TO UPPER AND LOWER BELL MOUTH ADAPTOR RINGS, INTAKE INLET LIP HAD SKIN BLOWN OUT, NUMEROUS CRACKS FOUND ALONG CIRCUMFERENCE AT ATTACH FASTENERS. INLET SEAL TORN AT FWD END OF TOP ADAPTER RING, L/E CHANNEL OF UPPER SEGMENT OF ADAPTER RING HAS SEVERAL CRACKS AND 1 LARGE HOLE ON LT SIDE, ACOUSTIC MATERIAL DAMAGED FWD OF FAN BLADES. BORESCOPE INSPECTION OF NR 2 ENGINE FOUND FOD DAMAGE TO LPC AND HPC BEYOND MM LIMITS REQUIRING ENGINE REMOVAL. REPLACED NR 2 ENGINE. REPLACING PIECES OF INTAKE L/E, BELL MOUTH ADAPTOR RINGS AND ACOUSTIC MATERIAL. INSTRUCTED FLIGHT CREWS ON PROPER THROTTLE MANAGEMENT. (K) 2L73 4F4 FRTA22WE E20EA 20050802001222005080200122EU 2005 8 2 USAA050869 120050713A5315D5311461100200 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19722US17743 1097 PIT - FOUND BEAM CORRODED 2 INCHES BY 1 INCH, FLOORBEAM FRAME 16, FRAME 16-Y254. REPLACED BEAM PER SRM 51-72-11. (M) 2L72 4F RTA28NM 20050802001232005080200123EU 2005 8 2 USAA050871 120050713A5315D5347217220400 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSLEAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19722US17743 1097 PIT - FOUND FLOORBEAM CORRODED 4 INCHES BY 5 FEET, TOP OF BEAM FRAME 66 THROUGH FRAME 69. REPLACED FLOORBEAM AND A SPLICE PART PER SRM 51-72-11. (M) 2L72 4F RTA28NM 20050802001242005080200124EU 2005 8 2 USAA050870 120050713A5300 BEAM AIRBUSA319 A319112 3930323EU FUSLEAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19722US17743 1097 PIT - FOUND BEAM CORRODED 10 INCHES BY 2 INCHES, BETWEEN FRAME 16 AND 20 Y254. INSTALLED BEAM PER SRM 51-72-11. (M) 2L72 4F RTA28NM 20050802001252005080200125EU 2005 8 2 USAA050868 120050713A5310D531182600101 BEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19722US 1097 FOUND BEAM CORRODED 8 INCHES BY 2 INCHES, BETWEEN FRAME 14 AND 16 Y 503.2. REPLACED BEAM BEAM PER SRM 51-72-11. (M) 2L72 4F RTA28NM 20050802001272005080200127EU 2005 8 2 USAA050867 120050713A5320D5347209001100 FLOOR SUPPORT AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19722US17749 1097 PIT - FOUND FLOOR SUPPORT CORRODED 1 INCH DIAMETER HOLES AROUND NUT PLATES, -Y1200 BETWEEN FRAME 66/69. REPLACED 3 SECTIONS OF FLOORBEAM PER SRM 51-72-11. (M) 2L72 4F RTA28NM 20050802001282005080200128NE 2005 8 2 HNAA0500073 220050801A72003022375 GARLOCK SEAL DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE ZONE 400 LEAKING A HNAAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA07808EX3441234412 299 120990 MASTER WARNING LIGHT AND NR 2 ENGINE OIL PRESSURE WARNING LIGHT FLICKERED ONCE EVERY 35 SECONDS TO A MINUTE. OIL PRESSURE FLUCTUATED BETWEEN 40 AND 55 PSI. PERFORMED ABNORMAL CHECKLIST. WITH P/L AT F/I AND C/L AT MIN OIL PRESSURE STABILIZED AT 55 PSI. REMOVED STARTER/GEN. REMOVED AND REPLACED GARLOCK SEAL AND O-RING ON CARRIER. INSTALLED GENERATOR RAN A/C OPS AND LEAK CHECK GOOD. 2H72 4T4 TRTA13NM E20NE 20050802001292005080200129NM 2005 8 2 DHL2005751003 120050801A3350 COVER BOEING727 727264 138408MNM EMERGENCY LIGHT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01751DH 22982 EMERGENCY EXIT LIGHT COVER OVER FWD ENTRY DOOR CRACKED AND BROKEN. REMOVED AND REPLACED EMERGENCY EXIT LIGHT COVER ASSY AND TESTED EMERGENCY LIGHT SYS IAW B727 M/M 33-50-01. OPS CKS NORMAL. P/N: 11-0368-25NF INSTALLED. 2L73 4F A3WE 20050802001332005080200133NM 2005 8 2 HNAA0500072 120050728A5755A44700009 ACTUATOR DHAV DHC8 DHC8102 2809003NM SPOILERS LEAKING A HNAAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 EA07982HA2910129101 380 NR 1 HYDRAULIC ISOLATION VALVE CAUTION LIGHT ILLUMINATED WHEN TAKING RUNWAY FOR TAKEOFF. NR 1 HYDRAULIC QUANTITY WENT TO 1.0 NORMAL BRAKING FAILED. CREW SHUT DOWN NR 1 ENGINE AND RETURNED TO GATE. REMOVED AND REPLACED THE LEFT WING INBOARD ROLL SPOILER PER LOG BOOK WRITE-UP. RECONNECTED HYDRAULIC LINES AND ACTIVATED SYSTEM, FOUND RIGHT WING INBOARD ROLL SPOILER AEROSPACE ACTUATOR LEAKING. REMOVED AND REPLACED ACTUATOR. PLEASE NOTE: ACTUATOR MANUFACTURER IS SMITH AEROSPACE, DID NOT FIND OPTION IN DROP DOWN FOR SMITH AEROSPACE. 2H72 4T RTA13NM 20050802001352005080200135SW 2005 8 2 YTRR104994 120050728A6220406310405101 BEARING BELL 407 407 1182206SW ALLSN 250C 250C47B GL MAIN ROTOR OUT OF LIMITS B YTRRK NONE O OTHER ININSP/MAINT 1 SW03594RL1097 53594 M/R PC LINK BEARING AXIAL AND RADIAL MOVEMENT BEYOND ALLOWABLE LIMITS 1G71 3U3 UO H2SW E1GL 20050802001362005080200136SW 2005 8 2 YTRR104995 120050728A6220406310405101 BEARING BELL 407 407 1182206SW ALLSN 250C 250C47B GL MAIN ROTOR OUT OF LIMITS B YTRAK NONE O OTHER ININSP/MAINT 1 SW03594RL1392 53594 M/R PC LINK BEARING AXIAL AND RADIAL MOVEMENT BEYOND LIMITS 1G71 3U3 UO H2SW E1GL 20050802001402005080200140NM 2005 8 2 05FDEA01457 120050524A5753ARC24443 SKIN DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE TE FLAP NICKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25631FE 48454 LT IB FLAP LOWER SIDE OB SEGMENT XIFH 237.32/266.00 RIVETS INSTALLED ON EXISTING NICKS. LT IB FLAP LOWER SIDE OB SEGMENT XIFH 237.32/266.00 NICKS SKIN. REPAIRED IAW ISRM 57-10-00 FIG 2 VOL I AND SRM 51-35-01 VOL I. CLASSIFIED AS MAJOR REPAIR IAW GMM 6-2-100. 2L73 4F4 FRTA22WE E24NE 20050802001472005080200147SO 2005 8 2 SWIA200515314 120050717A3350 SIGN EMB 120 EMB120ER 3260203SO EMERGENCY EXIT CRACKED A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07227SW ILLUMINATED EXIT SIGN ASSEMBLY ADJACENT TO SEAT 6A IS CRACKED, AND LARGELY MISSING. REMOVED AND REPLACED ILLUMINATED EXIT SIGN AT SEAT 6A WITH A SERVICEABLE ASSEMBLY. OPS CHECK GOOD AT THIS TIME. 2L72 4T RTA31SO 20050802001482005080200148EA 2005 8 2 SWIA200515315 120050720A2751601R590141 DETECTOR CNDAIRCL600 CL6002B19 1900309EA SKEW MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION DEDESCENT 1 NM07923SW 7664 FLAPS DEGRADED MESSAGE ON DESCENT INTO LAX. TROUBLESHOOT FLAPS DEGRADED MESSAGE. REMOVED AND REPLACED SKEW DETECTOR IAW CRJ 200 MM 27-50-00. FLAPS OPERATE NORMALLY. NO DEFECTS, PN 601R59014-1; SN OFF A312. 2L72 4F RTA21EA 20050802001492005080200149SO 2005 8 2 SWIA200515316 120050719A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO ROW 6 INOPERATIVE A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07188SW1004210042 120039 EMERGENCY LIGHTS IN ROW 6 ARE NOT WORKING. REPLACED EMERG LIGHT BATTERY PACK. SYSTEM OPS CHECK GOOD. 2L72 4T RTA31SO 20050802001512005080200151EA 2005 8 2 SWIA200515319 120050719A27604916405 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION LDLANDING 1 NM07919SW 7657 UPON LANDING AT LAX "SPOILERON FAULT" MESSAGE. NO MESSAGES PRIOR TO LANDING IN OAK. REMOVED AND REPLACED NR 1 SPOILER CONTROL UNIT WITH SERVICEABLE UNIT. FAULT D-7 ON UNIT, PN 49-164-05, SN/OFF 3149. 2L72 4F RTA21EA 20050802001532005080200153EA 2005 8 2 SWIA200515321 120050722A5210 ROLLER CNDAIRCL600 CL6002B19 1900309EA PAX DOOR OUT OF ADJUST A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07916SW 7634 MAIN CABIN DOOR STICKS. MOVED FWD SPIGOT ON PAX DOOR AFT .032". ADJUSTED AS NECESSARY TOP FWD SPIGOT AND FWD TEFLON ROLLER ON PAX DOOR. ALSO, REMOVED AND REPLACED BOTH PAX DOOR GAS SPRING IAW AMM 92-11-17, OPS CHECK GOOD AT THIS TIME. 2L72 4F RTA21EA 20050802001552005080200155EU 2005 8 2 05FDEA02143 120050730A5311 FRAME AIRBUS300 A300F4605R 3930327EU FUSELAGE GOUGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25670FE 777 COMPLY WITH EA 6-5310-82112, COMPLIED WITH EA 6-5310-82112 FUSELAGE-MAIN FRAME, FRAME 28 GOUGE REPAIR STR 10L THROUGH STR 11L. 2L72 4F RTA35EU 20050802001572005080200157NM 2005 8 2 05FDEA02153 120050801A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE RT NR 35 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. [CLOSED] 2L73 4F RTA22WE 20050802001592005080200159NM 2005 8 2 05FDEA02155 120050801A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE RT NR 09 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA1-5510-87597. 2L73 4F RTA22WE 20050802001602005080200160WP 2005 8 2 MWEA050074 120050730A2120 ODOR DOUG DC9 DC982 3022082WP COCKPIT DETECTED A MWEAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 GL31810ME 48072 PILOT SMELLED AN ODOR LIKE ELECTRICAL WIRING COMING FROM COCKPIT (NO SMOKE OR FUMES). INSPECTED THE ELETRICAL ELETRONICS COMPARTMENT AND FORWARD ACCESSORY COMPARTMENT, LOWERED CENTER OVERHEAD COCKPIT COMPARMENT PANELS AND INSPECTED WIRING, NO FAULTS NOTED. VISUALLY INSPECTED WIRING UNDER GLARE SHIELD AND OPERATED ALL COCKPIT LIGHTING, INSPECTED WIRING AT LOWER ELECTRICAL POWER CENTER, INSPECTED FORWARD GALLEY OVENS AND, INSPECTED WINDSHIELD HEAT CONNECTORS AND WIRING, NO FAULTS NOTED. 2L72 4F A6WE 20050802001622005080200162EU 2005 8 2 05FDEA02145 120050730A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU ZONE 200 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25671FE 778 MAIN DECK CARGO SEAT TRACK AT FRAME 41 TO 45 RBL 40 HAS CORROSION ALONG LENGTH NOTED. REMOVED CORRODED SEAT TRACK SECTION IAW SRM 53-10-16. FABRICATED NEW SEAT TRACK SECTION ON TRAVELER T5/534306. LOCATED AND DRILLED SECTION IAW SRM 53-10-16 AND 51-40-44. TREATED AND PRIMED IAW SRM 51-21-10. INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-16. PREP AND PAINT IAW AMM 51-75-10-8. 2L72 4F RTA35EU 20050802001642005080200164EU 2005 8 2 05FDEA02147 120050730A53405381290020001 FITTING AIRBUS300 A300F4605R 3930327EU SEAT TRACK CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25671FE 778 UPON REMOVAL OF SEAT TRACK AT RBL40 FITTING AT I/B SIDE OF WEB FOUND CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-40-21 AND PAINTED IAW SRM 51-23-10 FITTING LOCATED AT RBL 40, FRAME 40. 2L72 4F RTA35EU 20050802001662005080200166NM 2005 8 2 05FDEA02149 120050731A5313 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 CENTER CARGO BILGE STATION 1661 LONGERON 48L FOUND CORRODED. CORROSION AT CENTER CARGO BILGE STATION 1661 LONGERON 48L CARRIED OUT REPAIR AS PER SRM 53-10-00 FIG. 2 SHT 5 VOL. II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050802001682005080200168NM 2005 8 2 05FDEA02151 120050731A5313 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 CENTER CARGO BILGE STATION 1601 LONGERON 45R CORROSION FOUND AS MARKED. CORRODED LONGERON ON CENTER CARGO STATION 1601 LONGERON 45RH TRIMMED OUT AT STATION 1591 AND STATION 1611 AND REPAIR CARRIED OUT AS PER SRM 53-10-00 FIGURE 1 VOLUME I AND FEDEX EA 1-5310-87566 2L73 4F RTA22WE 20050802001702005080200170NM 2005 8 2 05FDEA02159 120050801A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE LT NR 32 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA1-5510-87597. 2L73 4F RTA22WE 20050802001722005080200172NM 2005 8 2 05FDEA02161 120050801A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE LT NR 28 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA1-5510-87597. 2L73 4F RTA22WE 20050802001742005080200174NM 2005 8 2 05FDEA02163 120050801A5315 FLOORBEAM DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25631FE 48454 FWD CARGO COMPARTMENT AT STA 939 APPROXIMATELY RBL 60 FLOORBEAM LOWER CHORD DENTED AND WEB CRACK AS MARKED. REPAIRED AS PER EA 1-5310-87607. 2L73 4F RTA22WE 20050802001842005080200184EU 2005 8 2 RAIA00507014 120050714A3260 INDICATOR JETAIRJETSTMJETSTM4101 1500501EU NLG INOPERATIVE A RAIAO OTHER P NO WARNING INDICATION DEDESCENT 1 CE03562HK 41078 FLT 3651 - SYR - NOSE GEAR STBY IND INOP. GEAR HORN SOUNDED, DECLARED EMERGENCY. LANDED SAFELY WITHOUT INCIDENT. FERRIED TO RIC FOR REPAIRS. MAINTENANCE INSPECTED WIRE HARNESS AND WOW SWITCHES AND PERFORMED MULTIPLE GEAR OPERATIONAL CHECKS BUT WAS UNABLE TO DUPLICATE. NO DEFECTS NOTED. 2L72 4T RTA41NM 20050802001862005080200186SO 2005 8 2 LR7A05097 120050801A5312 FLANGE LKHEED382 382G 526414USO BULKHEAD CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03405LC 2470 5025 DURING SCHEDULED C-5 INSPECTION PER JOB CARD HC3215, FOUND FS 93 BULKHEAD LOWER FLANGE CRACKED 2.5 INCH IN RADIUS AT RBL 22, WL 146. REPAIRED IAW SRM SMP 583 53-30-11, NR 2002. 2H74 4T A1SO 20050803000032005080300003EA 2005 8 3 ASOA05594 120050711A3350487190 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT DISCONNECTED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27878AS 7590 DURING A GROUND INSPECTION, THE AFT SECTION OF EMERGENCY FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE RECONNECTED THE AFT SECTION OF EMERGENCY FLOOR TRACK LIGHTS. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050803000042005080300004NE 2005 8 3 ASOA05598 220050713A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RIGHT MALFUNCTIONED A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27871AS 7537 873409 DURING CLIMB OUT, AT APPROXIMATELY 12,000 FEET THE CREW RECEIVED A (RT ENGINE OIL PRESSURE) WARNING WITH THE OIL TEMPERATURE INCREASING TO 153 DEGREES CENTIGRADE AND THE OIL PRESSURE FLUCTUATING BETWEEN 24-36 PSI. QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT DIVERTED AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE RT ENGINE. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050803000122005080300012EA 2005 8 3 ASOA05602 120050714A3350362624 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27672BR 7594 DURING A GROUND INSPECTION, EMERGENCY FLOOR LIGHTS FROM ROW 6 FORWARD WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED 4 EMERGENCY FLOOR LIGHT STRIPS FROM ROW 6 FORWARD AND ALSO DRIED OUT THE EMERGENCY FLOOR LIGHT TRACKS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050803000142005080300014CE 2005 8 3 RU32005F00002 120050727A79311013890235 TRANSDUCER BEECH 300 300BEECH 1152930CE PWA PT6 PT6A60 52043NE OIL PRESSURE FAILED E RU3AE ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW1574 FF9 RT ENGINE OIL PRESSURE INDICATION WAS ABOVE 200 PSI. CREW NOTICED SLIGHT OIL SMELL IN AC. PRECAUTIONARY SHUTDOWN OF RT ENGINE IN FLIGHT. ALL OTHER INDICATIONS WERE NORMAL. REPLACED OIL PRESSURE TRANSDUCER. (K) 2L72 4T4 T A24CE E4EA 20050803000152005080300015EA 2005 8 3 ASOA05595 120050712A7900 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT ENGINE ILLUMINATED A ASOAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27871AS 7537 873409 DURING CRUISE, AT APPROX 30,000 FT, CREW RECEIVED A (R ENG OIL PRESS) WARNING MESSAGE. QRH WAS COMPLIED WITH AND THE POWER LEVER WAS BROUGHT TO IDLE WITH THE OIL PRESSURE STABILIZING AT 25-30 PSI. DURING DESCENT THROUGH 10, 000 FEET THE OIL PRSSURE STABILIZED AT 45 PSI AND REMAINTED THROUGH LANDING. AN EMERGENCY WAS DECLARED, AC DIVERTED, LANDING SAFELY. MAINTENANCE INSPECTD RT ENGINE FOR OIL LEAKAGE, SERVICED IT WITH 1.5 QUARTS OF OIL AND RAN THE ENGINE THROUGH ALL POWER SETTINGS. NO DEFECTS WERE FOUND. OPERATIONAL AND LEAK CHECKS GOOD. AC OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050803000192005080300019NM 2005 8 3 2005UALA00699 120050722A3350362624 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT BURNED OUT A UALAK NONE L NO TEST ININSP/MAINT 1 WP29118UA 28811 SEAT 5A FWD EMERGENCY LAMP INOP. REPLACED LAMP. 2L74 4F4 FRTA20WE E24NE 20050803000232005080300023NM 2005 8 3 2005UALA00703 120050723A5210 GUIDE ARM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE PAX DOOR DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29386UA 24661 DOOR 2L EXTERIOR DOOR HANDLE RAISES IN SLIPSTREAM AND PARTIALLY ROTATES NO SPRING IN DOOR HANDLE, HANDLE HAS NO RESISTANCE WHEN PULLING OUT OR PUTTING BACK. SECURED EXTERNAL HANDLE, REPLACED GUIDE ARM, ADJUSTED STOP PIN. 2L72 4F4 FRTA16WE E2GL 20050803000242005080300024NM 2005 8 3 2005UALA00704 120050723A339758781 WIRE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE ROW 15 AFT DAMAGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29347UA 24251 EMERGENCY EXIT PATH LIGHTS STRIP INOP FROM ROW NR 15 AFT. REPLACED CABLE. 2L72 4F4 FRTA16WE E2GL 20050803000252005080300025NM 2005 8 3 2005UALA00705 120050724A2421 WARNING LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE LT GENERATOR ILLUMINATED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29544UA 25322 RETURNED TO FIELD DUE TO THE LEFT GENERATOR DRIVE LIGHT. SHOP FINDINGS INDICATED THAT NO FAULT WAS FOUND. THE IDG OIL PRESSURE SWITCH WAS REPLACED PRECAUTIONARY. 2L72 4F4 FRTA2NM E17NE 20050803000272005080300027NM 2005 8 3 2005UALA00707 120050725A2120 ODOR BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN DETECTED A UALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP29332UA 24193 FLIGHT DIVERTED DUE TO ODOR IN CABIN. TOOK OFF AND RETURNED A SECOND TIME WITH SAME ODOR. 2L72 4F4 FRTA16WE E2GL 20050803000302005080300030NM 2005 8 3 2005UALA00711 120050722A2120 SMOKE BOEING777 777222 1385219NM PWA PW4077PW4077 NE CABIN DETECTED A UALAA UNSCHED LANDING EB VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP29214UA 30220 SMOKE AND SMOKE ODOR IN FWD CABIN AND FLT DECK WITH VIBRATION IN FLOOR MID CABIN. LT PACK AIR CYCLE MACHINE BLADES FOUND TO BE DAMAGED UPON INSPECTION. ACM WAS SEIZED. THE ACM AND DIFFUSER HOUSING WERE REPLACED. HAMILTON REPORTED ROTOR FAN BLADES BROKEN AT ROOT. ROOT CAUSE IS PENDING. 2L72 4F4 FRTT0001SE E46NE 20050803000312005080300031NM 2005 8 3 2005UALA00712 120050726A5330 SKIN BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29912UA 25290 STATION 807 IS DENTED AT STR 28R. CUT OUT DAMAGE AND INSTALLED A TRIPLER REPAIR REF SRM 53-00-01 FIG 229. 2L72 4F4 FRTA16WE E2GL 20050803000322005080300032 2005 8 3 2005UALA00713 420050726A3442 RADAR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE WX SYSTEM MALFUNCTIONED A UALAA UNSCHED LANDING S AFFECT SYSTEMS CRCRUISE 1 WP29401UA 435 FLIGHT DIVERTED DUE TO WEATHER RADAR MALFUNCTION ALONG WITH FUEL AND WEATHER CONSIDERATIONS. 2L72 4F4 FRTA28NM E40NE 20050803000352005080300035NM 2005 8 3 2005UALA00693 120050722A5240 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FWD GALLEY DOOR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29914UA 25381 FWD GALLEY DOOR, FWD SIDE LOWER END FRAME CRACKED 1 EA FASTENER HOLE. MAJOR REPAIR ACP'D, REPLACED FRAME REF SRM 51-40-02 AND BACO DRAW 69-69430. 2L72 4F4 FRTA16WE E2GL 20050803000362005080300036EU 2005 8 3 2005UALA00714 120050703A5330 SKIN AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29418UA 485 DAMAGE TO FRAME 34 AT BELLY PANEL. DENT IN SKIN 4" FWD OF FS 34 AND JUST OTBD OF STR 43R. MAJOR REPAIR TO ADD DOUBLER OVER SKIN. 2L72 4F4 FRTA28NM E40NE 20050803000382005080300038NM 2005 8 3 AWXA200500894 120050731A3397BMS13311122 WIRE BOEING737 7373G7 1384595NM R2 SLIDE LIGHT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 MCN - EEL - DURING C16 CHECK DISCOVERED, THE R2 DOOR EXTERNAL EMERGENCY SLIDE LIGHT INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AT THE R2 DOOR EXTERNAL EMERGENCY SLIDE LIGHT IAW BOEING SWPM 20-10-13. OPERATIONAL CHECKS GOOD. 2L72 4F RTA16WE 20050803000392005080300039NM 2005 8 3 CALA0500249 120050731A5753654642944 FLAP TRACK BOEING737 737524 1384721NM NR 8 FLAP CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2719621 27334 INSPECTION FOUND THE NR 8 FLAP TRACK CORRODED IN AFT O/B HOLE WHERE THE TRANSMISSION IS ATTACHED. THE AREA WAS REWORKED IAW CMM 57-53-15. 2L72 4F RTA16WE 20050803000402005080300040NM 2005 8 3 CALA0500250 120050731A5753654642945 FLAP TRACK BOEING737 737524 1384721NM NR 2 FLAP CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2719621 27334 INSPECTION FOUND THE NR 2 FLAP TRACK CORRODED IN THE AFT LOWER HOLE WHERE THE TRANSMISSION IS ATTACHED. THE AREA WAS REWORKED IAW CMM 57-53-15. 2L72 4F RTA16WE 20050803000422005080300042NM 2005 8 3 2005UALA00694 120050724A5330 SKIN BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSLEAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29912UA 25290 STATION 203 HAS A SCRATCH BETWEEN STR 24 AND 25 LT. CUT-OUT DAMAGED AREAS AND INSTALLED TRIPLER REPAIR REF SRM 53-10-01 FIG 211 DETAIL XII AND XIII. 2L72 4F4 FRTA16WE E2GL 20050803000442005080300044NM 2005 8 3 2005UALA00696 120050722A33501317 LAMP BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE ROW 10 BULLNOSE BURNED OUT A UALAK NONE L NO TEST ININSP/MAINT 1 WP29902UA 25002 AISLE ILLUMINATION EMERGENCY LIGHT INOP AT ROW 10 BULLNOSE. REPLACED BURNED OUT LAMP. 2L72 4F4 FRTA16WE E2GL 20050803000452005080300045NM 2005 8 3 2005UALA00710 120050725A335058781 WIRE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE ROW 12 INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29307UA 23668 ALL EEL LIGHTS AFT OF ROW 12 INOPERATIVE. REPAIRED POWER CABLE AND FEEDER CABLE. 2L72 4F4 FRTA16WE E2GL 20050803000462005080300046NM 2005 8 3 2005UALA00715 120050726A3350ADD71701100 BATTERY PACK BOEING777 777222 1385219NM PWA PW4077PW4077 NE DOOR 3L DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29780UA 26944 DOOR 3L AFT EMERGENCY EXIT LIGHT INOP. REPLACED POWER SUPPLY. 2L72 4F4 FRTT0001SE E46NE 20050803000472005080300047NM 2005 8 3 2005UALA00716 120050706A3233273T41182 PISTON ROD BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE NLG ACTUATOR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29671UA19693 30026 CRACKED PISTON IN NOSE LANDING GEAR RETRACT ACTUATOR. ON WALKAROUND FOUND NOSE LANDING GEAR ACTUATOR ROD NEAR ROD END CRACKED. CONFIRMED WITH EDDY CURRENT. REPLACED NOSE GEAR ACTUATOR PER MM 32-34-01. HYDRAULIC QUANTITY WAS OK. 2L72 4F4 FRTA1NM E24NE 20050803000482005080300048NM 2005 8 3 2005UALA00717 120050721A3233273T41182 PISTON ROD BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE NLG ACTUATOR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29670UA20207 29240 CRACKED PISTON IN THE NOSE LANDING GEAR RETRACT ACTUATOR. ON WALKAROUND FOUND NOSE LANDING GEAR ACTAUTOR ROD NEAR ROD END CRACKED. CONFIRMED WITH EDDY CURRENT. REPLACED NOSE GEAR ACTUATOR PER MM 32-34-01. HYDRAULIC QUANTITY WAS OK. 2L72 4F4 FRTA1NM E24NE 20050803000492005080300049EU 2005 8 3 2005UALA00718 120050727A5610 WINDSHIELD AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE COCKPIT CRACKED A UALAA UNSCHED LANDING O OTHER CRCRUISE 1 WP29417UA 483 FIRST OFFICER'S WINDSHIELD CRACKED. REPLACED WINDOW DUE TO CRACKING AND DELAMINATION. 2L72 4F4 FRTA28NM E40NE 20050803000502005080300050NM 2005 8 3 2005UALA00719 120050727A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29308UA 23669 APPROXIMATE 1.5 INCH CRACK IN FUSELAGE AT LOWER AFT RADIUS OF DOOR 1R. REPAIRED DOOR 1R LOWER AFT CORNER REF SRM 53-10-01 PAGE 207. 2L72 4F4 FRTA16WE E2GL 20050803000512005080300051NM 2005 8 3 2005UALA00720 120050722A33977956323 WIRE BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT LOOSE A UALAO OTHER O OTHER CRCRUISE 1 WP29173UA 24380 EMERGENCY EXIT LIGHTS ZONE D AND E FLASHING ON AND OFF INFLIGHT. SECURED LOOSE EMERG LIGHT CABLE CONNECTOR AT ZONE D & E. 2L74 4F4 FRTA20WE E24NE 20050803000522005080300052NM 2005 8 3 2005UALA00721 120050727A5411 FRAME BOEING777 777222 1385219NM PWA PW4077PW4077 NE NR 2 PYLON CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29780UA 26944 NR 2 PYLON INSIDE PNL 444DL, CENTER LOWER FRAME IS CRACKED. PYLON FITTING WAS REPLACED DUE TO A STRESS RELATED CRACK. 2L72 4F4 FRTT0001SE E46NE 20050803000542005080300054NM 2005 8 3 2005UALA00723 120050727A335020131A BATTERY BOEING757 757222 1384956NM PWA 2037 PW2037 NE DOOR 1L DISCHARGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29510UA 24780 EXTERIOR EMERGENCY SLIDE LIGHT IS INOP. REPLACE EEL BATTERY CHARGER AT DOOR 1L. 2L72 4F4 FRTA2NM E17NE 20050803000562005080300056NM 2005 8 3 2005UALA00725 120050728A3350362624 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE ROW 38 INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29182UA 25279 EEL INOP, ROW 38 LT. REPLACED EEL LAMP. 2L74 4F4 FRTA20WE E24NE 20050729000592005072900059NM 2005 7 29 05FDEA02114 120050727A5320 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 CENTER CARGO, STA 1531 L46L LONGERON SPLICE FOUND CRACKED. NEW LONGERON SPLICE FABRICATED AS PER DWG A5A7114 AND FEDEX EA 1- 5310-89959 (TITLE: FUSELAGE - MAIN FRAME - LONGERON 46L SPLICE REPLACEMENT AT STA. 1531) CRACKED LONGERON SPLICE ON CENTER CARGO STA. 1531 LONGERON 46 LH AREA REMOVED AND REPLACED AS PER SRM 51-33-01 VOL. II. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050729000602005072900060NM 2005 7 29 05FDEA02115 120050727A5311 FRAME BOEING727 727227 1384078NM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 BS 360 FRAME HAS MECHANICAL DAMAGE FWD OF STR 5L. REPAIRED DAMAGED FRAME PER SRM 51-40-3. (CLOSED) 2L73 4F A3WE 20050729000622005072900062NM 2005 7 29 05FDEA02117 120050727A3620 CLAMP DOUG MD11 MD11F 3023600NM HEAT EXCHANGER BROKEN A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25592FE 48550 APPROX 10 MINUTES AFTER T/O, EXPERIENCED MANIF FAIL LIGHT NR 2 ON AIR PNEU WITH ASSOCIATED AUTOMATIC SHUTDOWN OF PACK 2 AND ISOLATION OF MANIFOLD. NEVER GOT ANY LEVEL 1 OR 2 ALERT OR WARNING. RETURNED TO KIX. INSPECTED PACK, COMPARTMENT AREA AND FOUND ONE HOSE FOR HEAT EXCHANGER BROKEN. ALSO, CLAMP BROKEN. REPLACED HOSE AND CLAMP PER SMP. RAN PACK, ABOUT ONE HOUR, FOUND NORMAL AND DECAY CHECKED WITH APU AIR GOOD. RETURNED TO SERVICE. 2L73 4F RTA22WE 20050729000642005072900064EA 2005 7 29 ASOA05582 120050706A5210601R3198067 STEP CNDAIRCL600 CL6002C10 1390015EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11724EV 10138 DURING A C-CHECK IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE BOTTOM STEP ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20050729000762005072900076EU 2005 7 29 MALA050608 120050725A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15370PX 340B300 SEAT TRACK AT FS640 AND BL 0 IS CORRODED AND HAS BEEN REPAIRED IAW MESABA EO NR S53079. 2L72 4T RTA52EU 20050729000962005072900096SW 2005 7 29 YTRR104952 120050304A8011A1077V STARTER BELL 206 206L1 1182107SW ENGINE INOPERATIVE B YTRAO OTHER O OTHER NRNOT REPORTED 1 SW03397RL 45397 ENGINE WOULD NOT START. REPLACED STARTER RELAY. 1G71 3U H2SW 20050729001072005072900107EA 2005 7 29 ASOA05569 120050623A5340 STRINGER CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11906EV 7642 DURING A C-CHECK IN HOT, THE RT INBOARD FS 280 CLIP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT INBOARD FS 280 CLIP IAW SRM 51-24-21 AND 51-42-136. (M) 2L72 4F RTA21EA 20050729001162005072900116EA 2005 7 29 ASOA05574 120050701A5210 FITTING CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11871AS 7537 DURING HANGAR MAINTENANCE IN MCN, THE AFT ANCHOR FITTING ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFT ANCHOR FITTING ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20050729001342005072900134CE 2005 7 29 AOQ2005F00003 120050717A770030710272 GASKET LEAR 35 31A 5170531CE GARRTTTFE731TFE73123B WP NI MONOPOLE WORN E AOQAK NONE J WARNING INDICATION CLCLIMB 1 EA1139TW 4119 047 P99200 DURING CLIMB, AT ALTITUDE, THE NR 1 ENGINE FIRE WARNING ILLUMINATED, ITT INDICATED 805 DEGREES. THRUST REDUCED BELOW 790 DEGREES ITT, AND LIGHT WENT OUT. ALL ENGINE INDICATIONS WERE NORMAL. MAINTENANCE TROUBLESHOT NR 1 ENGINE FIRE WARNING LIGHT ILLUMINATION TO A LEAKING N1 MONOPOLE GASKET. MAINTENANCE REPLACED MONOPOLE GASKET. A SATISFACTORY OPERATIONAL AND LEAK TEST WAS CONDUCTED AND THE AIRCRAFT WAS RTS. (K) 2L72 4F4 FRTA10CE E6WE 20050801000032005080100003WP 2005 8 1 UPS05844977 120050625A53409754022502 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE:C1 LWR FLOOR BEAM CRACKED ABOVE A-CARGO DOOR FRAME AT CUSP SAT 340. REMOVED AND REPLACED FLOORBEAM TO CUSP FITTING IAW DC-8 SRM 51-3-0. 2L74 4F RT4A25 20050801000042005080100004WP 2005 8 1 UPS05844978 120050627A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 INSPECTION TYPE:C1 RH WING L/E UPPER RIB CRACKED AT XFS 728. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 57-3-3 AND 57-2-0 FIG 2. 2L74 4F RT4A25 20050801000142005080100014EU 2005 8 1 RAIA00507021 120050728A2710 CONTROL SYSTEM JETAIRJETSTMJETSTM4101 1500501EU AILERONS LACK OF LUBE A RAIAD RETURN TO BLOCK W INADEQUATE Q C TXTAXI/GRND HDL 1 CE03560HK 41076 FLT 5404- STL- RESISTANCE IN RIGHT AILERON NOTICED ON TAXI OUT. MAINTENANCE LUBED AILERON CONTROL SYSTEM. OPS CHECKED GOOD. 2L72 4T RTA41NM 20050801000222005080100022NE 2005 8 1 A6WA200540241 220050713A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 1 ODOR A A6WAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL31457AW 7854 INFLIGHT DETECTED OILY ODOR AFTER BLEED AIR CHANGE OVER FROM APU TO ENGINE AIR IN COCKPIT. FERRIED FOR ENGINE NR 1 CHANGE. (K) REMOVED AND REPLACED COALESCER SOCKS IN LEFT AND RIGHT WATER SEPARATORS, NO FURTHER ODOR NOTED. (M) 2L72 4F4 FRTA21EA E15NE 20050801000292005080100029WP 2005 8 1 AALA20050466 120050725A3397 CONNECTOR DOUG DC9 DC982 3022082WP EMERGENCY LIGHT DISCONNECTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW2173444 49470 DFW AFT AIRSTAIR LEFT HAND UPPER SIDEWALL MOUNTED EMERGENCY LIGHT INOPERATIVE. RESECURED CONNECTION FOR EMERGENCY LIGHT AT AFT AIRSTAIR LEFT HAND UPPER SIDEWALL. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F A6WE 20050801000422005080100042NM 2005 8 1 05FDEA02126 120050728A5315 FLOORBEAM BOEING727 727227 1384078NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 BS 344 FLOORBEAM CORROSION FOUND ALONG TOP OF FLANGE IN VARIOUS PLACES. 2L73 4F A3WE 20050801000452005080100045EU 2005 8 1 05FDEA02129 120050728A5415 FITTING AIRBUS300 A300F4605R 3930327EU NR 1 PYLON CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25671FE 778 NR 1 PYLON TO WING ATTACHMENT FITTING SHACKLE OUTBD/INBD LOWER BUSHING HAS CORROSION CHROME PLATING WORN. 2L72 4F RTA35EU 20050801000482005080100048EU 2005 8 1 05FDEA02132 120050728A7830 BLOWOUT DOOR AIRBUS300 A300F4605R 3930327EU THRUST REVERSER GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25670FE 777 EXHAUST THRUST REVERSE R BLOWOUT DOOR EDGE REPAIR. COMPLIED WITH EA 6-7830-82111, EXHAUST THRUST REVERSER BLOWOUT DOOR EDGE WEAR REPAIR. 2L72 4F RTA35EU 20050801000582005080100058NM 2005 8 1 DHL2005750004 120050730A274130363803 SERVO BOEING727 7272M7 138407SNM STAB TRIM INOPERATIVE A DHLAAB UNSCHED LANDING EMER. DESCENT J WARNING INDICATION CLCLIMB 1 SO01750DH 21951 CRUISE TRIM INOP NOSE DOWN. STAB TRIM INOP NOSE DOWN BELOW '0'. NO ABNORMAL APPLICABLE, RETURN TO SAN. RII REQUIRED. REMOVED AND REPLACED A/P STAB TRIM SERVO IAW B727 M/M 22-11-21. INSP ALL WIRING AND CONN ON STAB SERVO AND MAIN ELEC ACTUATOR AND JACKSCREW. NO DEFECTS NOTED. LUBED JACKSCREW IAW B727 M/M 27-40-102, PERFORMED ADJ/TEST ON STAB IA. 2L73 4F A3WE 20050801000722005080100072SO 2005 8 1 C2XA05BT045 120050707A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT FAULTY A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713965 145125 BTV---CO2366, DURING 1A INSPECTION, MAINTENANCE FOUND AFT AISLE PATHWAY EMERGENCY LIGHT TO BE NOT OPERATING. REMOVED AND REPLACED BULB IAW EMB145 AMM NR 33-50-08, OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050802000022005080200002EA 2005 8 2 A6WA200540260 120050719A2750855D10011 BPSU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS INOPERATIVE A A6WAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL31426AW4954 7669 FLAPS FAIL CAS APPROACH, MYR FLAPS SELECTED NOT MOVE QAR C/W FLAPS ZERO LANDING. ACCOMPLISHED -30 DEGREES. REMOVED AND REPLACED LT BPSU IAW AMM. OPS CHECK GOOD. (K) 2L72 4F4 FRTA21EA E15NE 20050802000062005080200006EA 2005 8 2 A6WA200540255 120050716A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31420AW7548 7640 FS700, LBL 9 IB ATTACH CLIP CRACKED. REPLACED ANGLE IAW CRM AND EO. (K) 2L72 4F4 FRTA21EA E15NE 20050802000132005080200013EA 2005 8 2 A6WA200540249 120050716A5730 ACCESS PANEL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT WING DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31420AW 7640 RT LOWER WING PLANK AT WS 45, FUEL ACCESS PANEL 640BB CUT OUT, RAS FRETTING DAMAGE 2 INCH LONG X .175 INCH WIDE. (K) 2L72 4F4 FRTA21EA E15NE 20050802000182005080200018CE 2005 8 2 YDA2005F00001 120050718A2435230481360 COVER BEECH 99 99 1154002CE PWA PT6 PT6A27 52043EA RT STARTER GEN BURNED E YDACO OTHER O OTHER NRNOT REPORTED 1 AL0314MV 137 U59 11654 THE RT ENGINE WAS REPORTED TO BE THROWING SPARKS OUT THE LOWER PORTION OF THE COWL. UPON INVESTIGATION, THE STARTER GEN WAS FOUND TO HAE BURN SPOTS ON THE BRUSH BAND COVER. THE STARTER GEN WAS REMOVED AND A SERVICEABLE STARTER GEN WAS INSTALLED. UPON FURTHER INVESTIGATION OF THE REMOVED STARTER GEN, IT WAS DETERMINED THAT THE BAND WAS MISSING THE INSULATION STRIP. BRUSH WIRES WERE SHORTED TO THE BAND. STARTER GEN WAS LOW TIME. IT IS LIKELY THAT THE INSULATION WAS NOT INSTALLED AT THE OVERHAUL FACILITY. (K) 1L72 3T4 T A14CE E4EA 20050802000222005080200022NM 2005 8 2 CLC2005F00006 120050711A7160AJC7559119 INLET DOUG DC10 DC1040F 3023507NM PWA JT9 JT9D* NE NR 2 ENG INTAKE DAMAGED A CLCAK NONE O OTHER ININSP/MAINT 1 SO29140WE59475 46920 DURING PREFLIGHT CHECK, DAMAGE WAS FOUND NR 2 ENGINE INTAKE AND FAN BLADES. ENG INTAKE HAS DAMAGE TO UPPER AND LWR BELL MOUTH ADAPTOR RINGS, INTAKE INLET LIP HAD SECTION OF SKIN BLOWN OUT, NUMEROUS CRACKS FOUND ALONG CIRCUMFERENCE AT ATTACH FASTENERS. INLET SEAL TORN AT FWD END OF TOP ADAPTER RING AN L/E CHANNEL OF UPPER SEGMENT OF ADAPTER RING HAS SEVERAL CRACKS AND 1 LARGE HOLE ON LT SIDE, ALSO ACOUSTIC MATERIAL DAMAGED FWD OF FAN BLADES. BORESCOPE INSP OF NR 2 ENG FOUND FOD DAMAGE TO LPC AND HPC BEYOND MM LIMITS. REPLACED NR 2 ENGINE. REPLACING DAMAGED PIECES OF INTAKE L/E, BELL MOUTH ADAPTOR RINGS AND ACOUSTIC MATERIAL. INSTRUCTED FLIGHT CREWS ON PROPER THROTTLE MANAGEMENT. (K) 2L73 4F4 FRTA22WE E20EA 20050802000242005080200024NE 2005 8 2 AALA20050485 220050731A7200 ENGINE BOEING757 757223 1384957NM RROYCERB211 RB211535E4 54555NE LEFT FOD A AALAA UNSCHED LANDING C F.O.D. CLCLIMB 1 SW21605AA 27056 31161 CCS INFLIGHT T1522/31JUL - LEFT ENGINE INGESTED LARGE VULTURE AND ENGINE EXHAUST GAS TEMPERATURE WAS 934 C. ENGINE SHUTDOWN. FOUND THREE FAN BLADES DAMAGED. AIRCRAFT OUT OF SERVICE. 2L72 4F4 FRTA2NM E12EU 20050802000262005080200026NM 2005 8 2 AALA20050478 120050617A5740 FITTING BOEING767 767223 1385123NM LT WING CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21319AA 22320 AFW - LT WING REPAIR OF OUTBOARD SIDE LOAD FITTING BORE HAS CORROSION BLEND IN AN AREA OF .25 INCH BY 0.4 INCH BY .005 INCH DEEP. REPAIRED PER SRM 57 20 90 FIGURE 202 WITH THE FOLLOWING EXCEPTION. PERFORMED A LOCALIZED BLEND REPAIR. 2L72 4F RTA1NM 20050802000372005080200037NM 2005 8 2 QXEA200501143 120050731A3610 O-RING DHAV DHC8 DHC8202 2809007NM SPEED SENSOR LEAKING A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM09347PH 480 PDX FLIGHT NR 2036, STARTED NR 2 ENGINE, TURNED ON NR 2 BLEED, GOT HAZE IN COCKPIT AND CABIN. SMELLED LIKE DIRTY GYM SOCKS. REMOVED, CLEANED AND REINSTALLED NR 2 ENGINE P2.5/P3.0 AIR PRESSURE SWITCHING VALVE. NO DEFECT FOUND. REPLACED DAMAGED O-RINGS ON NL SPEED SENSOR PROBE AND NL SENSOR PORT SEALING TUBE. GROUND RAN NR 2 ENGINE WITH BLEED ON AT FEATHER FOR 15 MINUTES AND 70 PERCENT TORQUE/1050 RPM FOR 15 MINUTES WITH CABIN. COCKPIT TEMP SELECTIONS BETWEEN HOT AND FULL COLD. NO ABNORMAL ODORS OR VISIBLE HAZE NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050802000512005080200051EU 2005 8 2 USAA050861 120050708A5315D53472106203 FLOORBEAM AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19108UW18429 1061 PIT - FOUND FLOORBEAM CORRODED 1 INCH BY .75 INCH, FRAME 68 Y 254. REMOVED OLD FLOORBEAM AND INSTALLED NEW PER AIRBUS DWG 18D53472780. (M) 2L72 4F RTA28NM 20050802000602005080200060NM 2005 8 2 AWXA200500873 120050703A575465C26602217 WEDGE BOEING737 7373G7 1384595NM ZONE 500 - LEFT DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 DURING C16 CHECK, DISCOVERED DISBOND AREA ON THE TOP SURFACE OF NR 2 SLAT WEDGE, OUTBOARD END, FROM SLAT STATION 251.27 TO 253.27. MAINTENANCE CUT OUT DISBOND AREA AND CLEANED IAW BOEING 737-300 SRM 51-70-10-0 FIGURE 16. FABRICATED REPAIR CORE AND REPAIR DOUBLER IAW BOEING 737-300 SRM 51-70-10-0 FIG 16. BONDED REPAIR CORE AND DOUBLER TO THE TOP SURFACE OF THE NR 2 SLAT WEDGE, OUTBOARD END, FROM SLAT STATION 251.27 TO 253.27 IAW BOEING 737-300 51-70-10-0 FIG 16. 2L72 4F RTA16WE 20050802000662005080200066EU 2005 8 2 AWXA200500879 120050712A5315ASNA2222 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28627AW 66 DURING C4 CHECK, DISCOVERED CORROSION ON FLOORBEAM Y-254, FROM FS 16 TO FS 19. MAINTENANCE REMOVED CORRODED SECTION OF FLOORBEAM AT Y -254, FROM FS 16 TO FS 19 IAW AIRBUS SRM 53-11-14 FIG 202. PREPARED NEW FLOORBEAM FOR INSTALLATION IAW AIRBUS SRM 53-11-14 AND 51-47-00. INSTALLED FABRICATED REPAIR PARTS AT Y -254, FS 16 TO FS 19 IAW AIRBUS SRM 51-42-11. 2L72 4F RTA28NM 20050802000682005080200068EU 2005 8 2 AWXA200500881 120050712A5320D53112067200 WEB AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28627AW 66 DURING C4 CHECK, DISCOVERED CORROSION ON WEB NEXT TO R1 DOOR, FRAME 20, -Y1584. NO ALLOWABLE DAMAGE LIMITS FOUND IN AIRBUS SRM 53-11-14. MAINTENANCE REMOVED CORRODED NEXT TO R1 DOOR, FS 20 IAW AIRBUS SRM 51-72-11. PREPARED NEW WEB FOR INSTALLATION IAW AIRBUS SRM 51-25-00. INSTALLED REPAIR PARTS NEXT TO R1 DOOR, FR 20 IAW AIRBUS SRM 51-72-11. 2L72 4F RTA28NM 20050802000692005080200069NM 2005 8 2 UPS05444987 120050725A5320 FLOOR SUPPORT BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 U/D BS 400-402 RBL 76 LONGITUDINAL FLOOR SUPPORT FOUND CRACKED, CRACK LENGTH 2". U/D BS 400-402 RBL 76 LONGITUDINAL FLOOR SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 1. 2L74 4F A20WE 20050802000732005080200073NM 2005 8 2 UPS05444992 120050725A5320 SUPPORT BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 BS 415-420 BL 0 TO RBL 40 LATERAL SUPPORT FWD FLANGE FOUND CRACKED AT O/B AREA. BS 415-420 BL 0 TO RBL 40 LATERAL SUPPORT AT O/B AREA FWD FLANGE REPAIRED AS PER SRM 51-40-03 FIG 1. 2L74 4F A20WE 20050802000772005080200077WP 2005 8 2 UPS05844997 120050722A5330 FINGER DOUBLER DOUG DC8 DC873F 302199FWP L31L-31R CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C1, SKIN SPLICE AT FS 1350 INTERIOR FINGER DOUBLER HAS PITTED CORROSION FROM L31R TO L31L. REMOVED FINGER DOUBLER AT FS 1350 IAW SRM 51-1-21 AND 51-1-20D. FABRICATED AND INSTALLED FINGER DOUBLER AT FS 1350 L31L TO 31R IAW SRM 51-1-21. 2L74 4F RT4A25 20050802000912005080200091EU 2005 8 2 AWXA200500883 120050712A5320D5347112320300 SUPPORT AIRBUS320 A320231 3930325EU FUSLEAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28627AW 66 DURING C4 CHECK, DISCOVERED CORROSION ON SUPPORT, LOCATED AT FR 70 - 4, -Y 1180, UNDER STRINGER 23R. MAINTENANCE REMOVED CORRODED SUPPORT AT FR 70 - 4, -Y1180, UNDER STRINGER 23R. PREPARED NEW SUPPORT FOR INSTALLATION IAW AIRBUS MM 51-25-00. INSTALLED REPAIR PARTS AT FR 70 - 4" AND -Y 1180, UNDER STRINGER 23R IAW AIRBUS MM 51-72-11 PAGES 1 AND 2. 2L72 4F RTA28NM 20050802000962005080200096EU 2005 8 2 AWXA200500888 120050712A5347D53472133200 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28627AW 66 DURING C4 CHECK, DISCOVERED CORROSION ON SEAT RAIL BETWEEN FS 64 AND FS 66+5, -Y1292. MAINTENANCE REMOVED CORROSION FROM SEAT RAIL AND FOUND RE-WORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-15. REMOVED CORRODED SEAT RAIL FROM FS 64 TO FS 66+5 IAW AIRBUS 320 SRM 51-42-11. INSTALLED NEW SEAT RAIL AND FASTENERS FROM FS 64 TO FS 66+5, -Y1292 IAW AIRBUS 320 SRM 51-42-11. 2L72 4F RTA28NM 20050802001072005080200107NM 2005 8 2 CALA0500241 120050730A5320141A541014 INTERCOSTAL BOEING737 737724 13844BYNM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2725705 28766 INSPECTION FOUND A 1" CRACK IN INTERCOSTAL BETWEEN FLOORBEAM AT STA 277-294, BL 0. A REPAIR WAS INSTALLED IAW SRM 51-40-02. 2L72 4F RTA16WE 20050802001082005080200108NM 2005 8 2 CALA0500242 120050730A5320141A541016 INTERCOSTAL BOEING737 737724 13844BYNM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2725705 28766 INSPECTION FOUND A 1INCH CRACK IN INTERCOSTAL BETWEEN FLOORBEAM AT STA 328-344, LBL 50. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20050802001092005080200109NM 2005 8 2 CALA0500243 120050730A5320141A541016 INTERCOSTAL BOEING737 737724 13844BYNM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2725705 28766 INSPECTION FOUND A 12 INCH CRACK IN INTERCOSTAL TWELVE INCHES I/B OF THRESHOLD PLATES BETWEEN STA 312 AND 328, LBL 50. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20050802001162005080200116CE 2005 8 2 72066 120050801A7712 INDICATION SYS BEECH 1900 1900D 1154162CE ENGINE TORQUE MALFUNCTIONED A AMWAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 CE07155YV 155YV ON TAKEOFF ROLL OUT, CREW OBSERVED RIGHT ENGINE TORQUE NOT ABOVE 500LBS. RETURN TO GATE WITH NO FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED INDICATOR AND TRANSMITTER. 2L72 4T RTA24CE 20050802001322005080200132NM 2005 8 2 AMTA200500602 120050706A5330 SKIN BOEING757 75723N 1384973NM RROYCERB211 RB211* 54555NE TAIL DAMAGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11519AT 27975 NOTICED SCRAPE ON LOWER TAIL SKIN DURING WALK AROUND. COMPLIED WITH ERA. (K) 2L72 4F4 FRTA2NM A12EU 20050802001392005080200139NM 2005 8 2 05FDEA01429 120050524A5347AFA7789547 SEAT TRACK DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25631FE 48454 AFT INTERMEDIATE FUSELAGE STA 1964, X = 107.25 LT OB EXISTING REPAIR ON CORRODED SEAT TRACK. FOR WORK ACCOMPLISHED REFER TO SNRM N0198, DISCREPANT SEAT TRACK TRIM OUT FROM STA 1751 LBL 107. NEW SEAT TRACK REPLACED FROM AFA 7789-545 AND CARRIED OUT REPAIR IAW SRM 53-70-00 FIG 1 VOL I. NEW SEAT TRACK AND REPAIR PARTS LOCATED AND INSTALLED IAW SRM 53-70-00 FIG 1 VOL I AND SRM 51-31-01VOL II. CLASSIFIED AS MAJOR REPAIR IAW GMM 6-2-100. 2L73 4F4 FRTA22WE E24NE 20050802001412005080200141NM 2005 8 2 05FDEA02141 120050729A5315 FLOORBEAM BOEING727 727277 138408SNM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25244FE 21647 FLOORBEAM AT STA 620 RBL 0-24.5 HAS CORROSION ON UPPER CAP. REMOVED DAMAGED AREA IAW SRM 53-10-8. FAB REPAIR PARTS, T-ANGLE, SUPPORT ANGLE, STRAP, IAW SRM 53-10-3 FG 3 PG 18. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED PARTS IAW SRM 53-10-8 FIG 3 PG 18. 2L73 4F RTA3WE 20050802001422005080200142SO 2005 8 2 SWIA200515312 120050715A3350 BULB EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT INOPERATIVE A SWIAK NONE L NO TEST TXTAXI/GRND HDL 1 NM07288SW 120316 LAST EMERGENCY LIGHT IN BACK OF CABIN IS OUT. INSTALLED BULB INTO SOCKET OF EMERGENCY LIGHT IN THE BACK OF THE CABIN. OPS CHECKS GOOD. 2L72 4T RTA31SO 20050802001502005080200150 2005 8 2 SWIA200515318 420050720A22166225027101 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA ELEVATOR MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION APAPPROACH 1 NM07983SW 7961 AUTOPILOT PITCH TRIM CAUTION ON APPROACH WITH FLAP AT 45 DEGREES, THEN WENT AWAY. REMOVED AND REPLACED ELEVATOR SERVO WITH A SERVICEABLE UNIT. OPS CHECK GOOD ON ALL GROUND OPERATIONS AT THIS TIME IAW MM 22-11-24. 2L72 4F RTA21EA 20050802001522005080200152EA 2005 8 2 SWIA200515320 120050720A27604916406 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA LT SPOILER MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CLCLIMB 1 NM07433SW6151 6151 7550 AFTER TAKEOFF IN YYC, HAD A SPOILERON FAULT STATUS MESSAGE WHICH STAYED ON THE ENTIRE FLIGHT. REPLACED LEFT SECU IAW 27-61-05. OPS CHECK GOOD. 2L72 4F RTA21EA 20050802001542005080200154EA 2005 8 2 SWIA200515322 120050720A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLT SPOILERS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION LDLANDING 1 NM07916SW8136 8136 FLT SPLRS FAULT STATUS MESSAGE ON ED2 UPON TOUCHDOWN. FLT CONTROL PAGE VERIFIED THE LEFT FLT SPOILER WAS AT FAULT. REMOVED AND REPLACED LEFT FLIGHT SPOILER INBOARD PCU PER 27-62-01. PERFORMED OPS CHECK PER 27-64-00-710-801. OPS CHECK GOOD, NO LEAKS NOTED. 2L72 4F RTA21EA 20050802001562005080200156NM 2005 8 2 05FDEA02152 120050731A2840 INDICATION SYS DOUG MD11 MD11 3023602NM FUEL SYSTEM MALFUNCTIONED A FDEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO25582FE 48420 6 HOURS INTO FLIGHT GOT "FUEL MANF DRAIN" AND"TANK 2 FUEL QTY LO" LEVEL. FUEL READ 700 IN 1, 0IN 2, 700 IN 3, 500 AUX, 14000 IN TAIL. AFTER ACCOMPLISHING QRH PROCEDURE. MCDU INDICATED NR 19,000 FUEL REMAINING. RJAA 90 MILES AWAY. DECLARED EMERGENCY AND PROCEEDED TO LAND AT NRT. ON DESCENT AT APP X 14,000 ON DESCENTFUL QTY IND RETURNED 11000 IN 1, 19000 IN 2, 11000 IN 3,500 AUX, 4000 TAIL. RELEASED FOR SERVICE PER MEL/CDL: 28-01-01-02 . 2L73 4F RTA22WE 20050802001582005080200158NM 2005 8 2 05FDEA02154 120050801A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE RT NR 19 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA1-5510-87597. 2L73 4F RTA22WE 20050803000172005080300017NM 2005 8 3 2005UALA00691 120050722A5320 ANGLE BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE STA 996 RBL 53, CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29914UA 25381 AFT CABIN FLOOR ANGLE CAP IS CORRODED AT STA 996 RPL 53, WL208. REPLACED ZEE ANGLE ASSY AT HMV3. 2L72 4F4 FRTA16WE E2GL 20050803000222005080300022NM 2005 8 3 2005UALA00702 120050722A3397W2818 WIRE HARNESS BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT DISCONNECTED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29118UA 28811 RIGHT UPPER DECK DOOR EMERGENCY EXIT SIGN INOP. FOUND WIRES TIED UP IN CEILING AND PULLED BACK. RECONECTED WIRES AND GRD CHECKED NORMAL. 2L74 4F4 FRTA20WE E24NE 20050803000342005080300034NM 2005 8 3 2005UALA00692 120050722A5240 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FWD GALLEY DOOR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29914UA 25381 FWD GALLEY DOOR, AFT SIDE LOWER END FRAME CRACKED 1 EA FASTENER HOLE. MAJOR REPAIR ACP'D, AFT FRAME REPLACED PER SRM 51-40-02 AND BACO DRAW 65-45871. 2L72 4F4 FRTA16WE E2GL 20050803000572005080300057NM 2005 8 3 2005UALA00726 120050728A3350362624 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29182UA 25279 EMERG LT INOP, MAIN STAIRS ILLUM. REPLACED EEL LAMP. 2L74 4F4 FRTA20WE E24NE 20050803000592005080300059NM 2005 8 3 2005UALA00728 120050728A3350 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29182UA 25279 EMERGENCY LIGHT INOPERATIVE, DOOR 1 SLIDE ILLUMINATED. REPLACED LAMP. 2L74 4F4 FRTA20WE E24NE 20050803000632005080300063NM 2005 8 3 2005UALA00732 120050728A335078941 LAMP BOEING777 777222 1385219NM PWA PW4077PW4077 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29773UA 26929 AFT EEL LIGHT 1E INOP. REPLACED BURNED OUT LAMP. 2L72 4F4 FRTT0001SE E46NE 20050803000652005080300065EU 2005 8 3 AWXA200500895 120050801A3397 WIRE AIRBUS320 A320231 3930325EU EMERGENCY LIGHT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 LAS - EEL - DURING 8 DAY CHECK, DISCOVERED ROW 12 SEAT MOUNTED EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AT ROW 12. OPERATIONAL CHECKS WERE GOOD IAW TASK CARD F1C33301. 2L72 4F RTA28NM 20050803000672005080300067NM 2005 8 3 AWXA200500897 120050728A3397BMS13311122 WIRE BOEING737 7373G7 1384595NM EMERGENCY LIGHT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 MCN - EEL - DURING C16 CHECK, DISCOVERED WIRES BROKEN AT THE L1 DOOR EMERGENCY EXIT LIGHT. MAINTENANCE REPAIRED BROKEN WIRES AT THE L1 EMERGENCY EXIT LIGHT IAW SWPM 20-10-13, OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20050803000682005080300068EU 2005 8 3 AWXA200500898 120050730A3350 LIGHT AIRCRUISERS AIRBUS320 A320232 3930326EU L1 DOOR SLIDE INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28651AW A9093 866 PHX - EEL - DURING PHASE 4 CHECK, OPERATIONAL TEST OF EMERGENCY LIGHTS FAILED EXTERNAL LOAD FAULTING FORWARD LEFT. MAINTENANCE REMOVED AND REPLACED THE L1 DOOR ESCAPE SLIDE IAW AMERICA WEST TASK CARD R1C25305. VENDOR TEAR DOWN REPORT SHOWS SLIDE PASSING ALL INCOMING TESTS. SLIDE WAS OVERHAULED IAW CMM 25-60-56 REV11. ALSO S.B. 320 004-25-72 & SIL 25-181 WERE PERFORMED IN ADDITION TO COMPLYING WITH EO 2561-01018.MFG PN WAS CHANGED FROM D31516-313 TO D31516-317. 2L72 4F RTA28NM 20050803000692005080300069NM 2005 8 3 AWXA200500899 120050801A4990 APU AIRBUSA319 A319132 3930340NM APU BAY LACK OF LUBE A AWXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP28830AW 1565 MEM - DIVERSION - FLT 844 - EN ROUTE TO PHX APU SHUT DOWN IN FLIGHT, WITH THE NR 2 ENGINE DRIVEN GENERATOR ON MEL. AIRCRAFT DIVERTED TO MEMPHIS AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT APU AND FOUND THE OIL LEVEL WAS LOW. APU WAS SERVICED AND OPERATIONAL CHECKS WERE GOOD. MAINTENANCE ALSO RAN ENGINES AND CYCLED NR 2 ENGINE GENERATOR NUMEROUS TIMES WITH OPERATIONAL TESTS GOOD, CLEARED MEL ON THE NR 2 ENGINE DRIVEN GENERATOR. A PRECAUTIONARY REMOVAL AND REPLACEMENT OF THE NR 2 GENERATOR PUSH BUTTON SWITCH HAS BEEN SCHEDULED TO BE ACCOMPLISHED WITHIN THE NEXT 24 HOURS. 2L72 4F RTA28NM 20050803000702005080300070NM 2005 8 3 AWXA200500900 120050729A3150 WARNING SYSTEM BOEING737 737301 1384611NM COCKPIT FALSE ACTIVATIONA AWXAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 WP28326AW 23258 SJC - ABORTED TAKEOFF - FLT 165 - ABORTED TAKEOFF FOR UNSPECIFIED WARNING. CLEARED RUNWAY THEN RE-ATTEMPTED T/O. TAKEOFF WAS UNEVENTFUL. 2L72 4F RTA16WE 20050803000722005080300072 2005 8 3 TCA005 420050801A23127926657003 TRANSCEIVER SWRNGNSA226 SA226TC 8780404SW COMMS INOPERATIVE E E18AA UNSCHED LANDING GS MULTIPLE FAILURE AFFECT SYSTEMS CLCLIMB 1 GL23629E TC396 DOCUMENTED ON FL241 BY PILOT, LOST ALL RADIO CONTACT SHORTLY AFTER DEPARTURE, NR 1 AND NR 2 COMM NO AUDIO FROM ANY RADIOS. PILOT RETURNED TO TOL WITHOUT INCIDENT AFTER DECLARING EMERGENCY WITH TOL TOWER. 2L72 4T RTA8SW 20050803000752005080300075EU 2005 8 3 07252005B 120050725A2710 CENTERING CAM SAAB SF340 340B 7860101EU RT AILERON MALFUNCTIONED A NSVAO OTHER F FLT CONT AFFECTED APAPPROACH 1 EA27304CE 198 GET AN AIL FLAG WITH AUTOPILOT ENGAGED. ACFT VERY HARD TO TURN TO THE RT, ACFT AUTOMATICALLY BANKS 30 DEGREES TO THE LT WHEN CONTROLS RELEASED. INSTALLED RT AILERON CENTERING MECHANISM. OPS CHECK GOOD. 2L72 4T RTA52EU 20050803000762005080300076EU 2005 8 3 06022005B 120050602A324050128093 BRAKE ASSY SAAB SF340 340B 7860101EU LEFT WEAK A NSVAO OTHER O OTHER TXTAXI/GRND HDL 1 EA27299CJ 299 ACFT PULLS SIGNIFICANTLY TO THE LT DURING BRAKING, RT BRAKE APPEARS TO BE WEAK. REMOVED AND REPLACED RT BRAKE ASSY. 2L72 4T RTA52EU 20050803000772005080300077EU 2005 8 3 06112005A 120050611A2701 CONTROL COLUMN SAAB SF340 340B 7860101EU COCKPIT STICKING A NSVAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 EA27303CE 194 ELEVATOR MOMENTARILY FROZE DURING TAXI. TIGHTENED CONTROL COLUMN HARDWARE. 2L72 4T RTA52EU 20050803000782005080300078EU 2005 8 3 06222005B 120050622A6123 AUTOFEATHER SYS SAAB SF340 340B 7860101EU LT ENGINE ACTIVATED A NSVAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 EA27341CJ 341 ON TAKEOFF ROLL, LEFT ENGINE WENT INTO AUTOFEATHER. PERFORMED CWC AUTOCOARSEN TEST, OPS CHECK GOOD. 2L72 4T RTA52EU 20050803000792005080300079EU 2005 8 3 06222005C 120050622A7931 CONNECTOR SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE OIL PRESS XMITERLOOSE A NSVAO OTHER N FALSE WARNING CRCRUISE 1 EA27242CJ 242 LEFT OIL PRESSURE READS 0 PSI IN FLIGHT. FOUND LOOSE CONNECTOR ON OIL PRESSURE TRANSMITTER. CLEANED AND SECURED. 2L72 4T4 TRTA52EU E8NE 20050803000802005080300080EU 2005 8 3 06232005B 120050623A7931IPTE119100020 TRANSDUCER SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE OIL PRESSURE MALFUNCTIONED A NSVAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 EA27242CJ 242 RT ENGINE OIL PRESSURE LIGHT ILLUMINATED AFTER TOUCHDOWN, PROP PSI READS 0. REMOVED AND REPLACED TRANSDUCER, OPS CHECK GOOD. 2L72 4T4 TRTA52EU E8NE 20050803000812005080300081EU 2005 8 3 06152005B 120050615A2910 LINE SAAB SF340 340B 7860101EU HYD SYSTEM LEAKING A NSVAO OTHER KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 EA27252CJ 252 UPON LANDING, NO HYDRAULIC PRESSURE OR FLUID. REMOVED AND REPLACED RT MLG DOWN HYDRAULIC LINE. 2L72 4T RTA52EU 20050803000832005080300083CE 2005 8 3 06272005B 120050627A2711 ACTUATOR BEECH 1900 1900D 1154162CE AILERON TRIM LACK OF LUBE A NSVAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 EA27172MJ UE72 AILERON STIFF TO OPERATE. LUBED AILERON TRIM ACTUATOR. 2L72 4T RTA24CE 20050803000842005080300084CE 2005 8 3 06072005B 120050607A32331143800417 ACTUATOR BEECH 1900 1900D 1154162CE MLG MALFUNCTIONED A NSVAO OTHER O OTHER APAPPROACH 1 EA27155CJ UE55 LANDING GEAR EXCESSIVELY SLOW TO EXTEND. CHANGED RT MLG ACTUATOR. 2L72 4T RTA24CE 20050803000872005080300087EU 2005 8 3 MALA050627 120050731A5753 ACCESS PANEL SAAB SF340 340B 7860101EU LT TE FLAP CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15452XJ 340B452 LT FLAP IB END ACCESS PANEL S41AT IS CHAFED AND HAS BEEN REPAIRED IAW MESABA EO 57098 REF EAMS WORK ORDER 212638 TASK 5504. 2L72 4T RTA52EU 20050803000882005080300088EU 2005 8 3 MALA050623 120050802A2910 HYDRAULIC SYSTEM BAC 146 AVRO146RJ85A1500097EU GREEN FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15504XJ E2311 CREW RETURNED TO MEM FOLLOWING FAILURE OF THE GREEN HYDRAULIC SYSTEM. EMERGENCY NOT DECLARED BUT ARFF ON STANDBY. FLIGHT LANDED WITHOUT FURTHER INCIDENT. 2H74 4F RTA49EU 20050803000892005080300089EU 2005 8 3 MALA050624 120050731A5753 ACCESS PANEL SAAB SF340 340B 7860101EU RT TE FLAP CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15452XJ 340B452 RT FLAP IB END ACCESS PANEL S41AT IS CHAFED AND HAS BEEN REPAIRED IAW MESABA EO 57098 REF EAMS WORK ORDER 212638 TASK 6502. 2L72 4T RTA52EU 20050803000932005080300093NM 2005 8 3 SWAA052131 120050720A53226546549 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29609SW 27929 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME SHEAR TIE CORRODED AT BS 747, RBL 10. REMOVED AND REPLACED SHEAR TIE SECTION PER SRM. 2L72 4F RTA16WE 20050803000942005080300094NM 2005 8 3 SWAA052132 120050718A53126545819 PRESSURE PANEL BOEING737 7373H4 1384600NM NLG WW CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED C2 CHECK, FOUND NLG W/W RT SIDE WEB CRACKED AT BS 259, WL 174. REPAIRED WEB PER SWA EA. 2L72 4F RTA16WE 20050803001002005080300100 2005 8 3 SWAA052121 420050720A256565C19901 CABLE BOEING737 7373H4 1384600NM L2 DOOR SLIDE MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29387SW 26602 DURING SCHEDULED A1 CHECK, FOUND L2 DOOR EVACUATION SLIDE LATCH CABLE MISROUTED. REROUTED CABLE PER MM. 2L72 4F RTA16WE 20050803001012005080300101NM 2005 8 3 SWAA052123 120050720A55516551524 FITTING BOEING737 7373H4 1384600NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29609SW 27929 DURING SCHEDULED D CHECK, FOUND LT AND RT HORIZONTAL STAB ATTACH FITTING LUG FACE CLEVICES CORRODED. REPAIRED LUG FACE CLEVICES PER SRM. 2L72 4F RTA16WE 20050803001042005080300104NM 2005 8 3 SWAA052126 120050720A53226546558 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29609SW 27929 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME SHEAR TIE CORRODED AT BS 907, LBL 19 TO RBL 12. REMOVED AND REPLACED SHEAR TIE SECTION PER SRM. 2L72 4F RTA16WE 20050803001052005080300105NM 2005 8 3 SWAA052127 120050720A53226546548 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29609SW 27929 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME SHEAR TIE CORRODED AT BS 767, LBL 10 TO RBL 20. REMOVED AND REPLACED SHEAR TIE SECTION PER SRM. 2L72 4F RTA16WE 20050803001062005080300106NM 2005 8 3 SWAA052128 120050720A53226546549 SHEAR TIE BOEING737 7373H4 1384600NM FUSLEAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29609SW 27929 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME SHEAR TIE CORRODED AT BS 787, LBL 10 TO RBL 22. REMOVED AND REPLACED SHEAR TIE SECTION PER SRM. 2L72 4F RTA16WE 20050803001072005080300107NM 2005 8 3 SWAA052129 120050720A53226546596 SHEAR TIE BOEING737 7373H4 1384600NM FUSLEAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29609SW 27929 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME SHEAR TIE CORRODED AT BS 727B, LBL 8. REMOVED AND REPLACED SHEAR TIE SECTION PER SRM. 2L72 4F RTA16WE 20050803001112005080300111NM 2005 8 3 SWAA052244 120050728A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500A + 4, STR 16R. REPAIRED SKIN PER SWA EA AND SRM. 2L72 4F RTA16WE 20050803001122005080300112NM 2005 8 3 SWAA052245 120050728A575465C26686 SKIN BOEING737 7373H4 1384600NM RT NR 5 SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND RT WING NR 5 L/E SLAT INBD UPPER SKIN CRACKED. REPAIRED SLAT PER SRM. 2L72 4F RTA16WE 20050803001132005080300113NM 2005 8 3 SWAA052246 120050728A53116546546 BELTFRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE BELTFRAME CORRODED AT BS 847, BETWEEN STR 27L TO STR 27R. REPAIRED BELTFRAME PER SRM. 2L72 4F RTA16WE 20050803001142005080300114NM 2005 8 3 SWAA052247 120050728A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 807, STR 26L. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050803001162005080300116NM 2005 8 3 SWAA052249 120050728A53306545775 SKIN BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 847, BETWEEN STR 27L TO STR 27R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050803001172005080300117NM 2005 8 3 SWAA052250 120050728A53306545777 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 968 TO BS 971, STR 21L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050803001222005080300122NM 2005 8 3 SWAA052257 120050729A3350D71702001 BATTERY PACK BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29478WN 33989 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050803001242005080300124NM 2005 8 3 SWAA052259 120050729A324426066712 TIRE BOEING737 737301 1384611NM LT MLG SEPARATED A SWAAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SW29659SW 23229 AIR TURNBACK, NR 2 MAIN TIRE TREAD SEPARATED AND LOST A SYSTEM HYDRAULICS DURING MAIN GEAR RETRACTION. FOUND LT INBD GROUND SPOILER, LT AILERON BUS CABLE , 4 HYDRAULIC LINES AND LT INBD T/E AFT FLAP DAMAGED. REMOVED AND REPLACED MAIN TIRE ASSY, LT INBD T/E AFT FLAP, HYDRAULIC LINES AND LT INBD GROUND SPOILER PER MM. 2L72 4F RTA16WE 20050803001252005080300125NM 2005 8 3 SWAA052260 120050729A53306545774 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 765, STR 24R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050803001292005080300129 2005 8 3 SWAA052264 420050729A2565D31354 SLIDE BOEING737 7373Y0 1384671NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050803001302005080300130NM 2005 8 3 SWAA052265 120050730A323065446915 PRIORITY VALVE BOEING737 7373A4 1384585NM RT MLG FAULTY A SWAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW29680AA 23505 RT MLG EXTENDED UNCOMMANDED WITH RED RIGHT GEAR LIGHT ILLUMINATING FOR 5 MINUTES BEFORE GREEN RIGHT GEAR LIGHT ILLUMINATED. RETRACTED GEAR NORMALLY. MX FERRY TO PHX FOR REPAIRS. REMOVED AND REPLACED MLG PRIORITY MODULAR VALVE, MLG TRANSFER VALVE AND CONNECTOR PER MM. 2L72 4F RTA16WE 20050803001312005080300131NM 2005 8 3 SWAA052266 120050728A324426066712 TIRE BOEING737 7373G7 1384595NM RT MLG SEPARATED A SWAAO OTHER D INFLIGHT SEPARATION LDLANDING 1 SW29690SW 23783 NR 4 MAIN TIRE TREAD SEPARATED. FOUND RT MAIN FLYING AND FIXED DOORS, RT WING PANEL, RT WING INBD T/E FOREFLAP AND RT WING NR 5 GROUND SPOILER DAMAGED. REMOVED AND REPLACED NR 4 MAIN TIRE ASSY PER MM. MX FERRY TO DAL FOR REPAIRS. REMOVED AND REPLACED RT MLG WING PANEL AND FOREFLAP PER MM. 2L72 4F RTA16WE 20050803001332005080300133NM 2005 8 3 SWAA052268 120050728A3350311500 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29763SW 27877 BULLNOSE EMERGENCY LIGHT LENS LOOSE AT ROW 9 ABC. SECURED LENS PER MM. 2L72 4F RTA16WE 20050803001392005080300139NM 2005 8 3 SWAA052227 120050728A53306545775 SKIN BOEING737 7373K2 13844BANM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29345SA 23786 DURING WALKAROUND INSP, FOUND FUSELAGE SKIN CRACKS AT BS 769 AND BS 783, STR 22R. REPAIRED SKIN PER SWA EA AND SRM. 2L72 4F RTA16WE 20050803001402005080300140NM 2005 8 3 SWAA052239 120050728A2560PH22300L GLOWSTRIP BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29641SW 27714 DURING SCHEDULED RON CHECK, FOUND FWD CABIN PHOTOLUMINESCENT STRIP LOOSE AT FWD END. REMOVED AND REPLACED STRIP PER MM. 2L72 4F RTA16WE 20050803001412005080300141NM 2005 8 3 SWAA052242 120050728A53306545775 SKIN BOEING737 7377H4 1384404NM FUSELAGE DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29777QC 30592 DURING SCHEDULED 5Y CHECK, FOUND FUSELAGE SKIN CREASED AT BS 812, BETWEEN STR 27L AND STR 26R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050803001422005080300142 2005 8 3 SWAA052219 420050728A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. SLIDE DID NOT DEPLOY. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20050803001442005080300144NM 2005 8 3 SWAA052221 120050728A53306545775 SKIN BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 847, BETWEEN STR 27R AND STR 27L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050803001472005080300147NM 2005 8 3 SWAA052224 120050728A531165C22910 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 20R. REPAIRED FRAME PER SWA EA. 2L72 4F RTA16WE 20050803001502005080300150SO 2005 8 3 GYW2005F00000 220050728A741410391586 BLOCK CONT CESSNA421 421C 2076016CE CONT O520 GTSIO520L 17032SO RT MAGNETO DESTROYED D GYWAO OTHER O OTHER NRNOT REPORTED 1 SW13421WT497 F02IA065R 421C0620 WHILE PERFORMING THE MAGNETO 500 HOUR INSPECTION, BRASS SHAVINGS WERE FOUND INSIDE THE MAGNETO HOUSING. FURTHER INVESTIGATION RVEALED EXCESSIVE (ROCKING) IN DISTRIBUTOR GEAR IN BLOCK CAUSED BY CENTER BEARING BEING LOOSE IN BLOCK. LOOSENESS AND PLAY ALLOWED GEAR FINGER TO CONTACT BLOCK POSTS. (K) 1L72 3O3 O A7CE E7CE 20050803001532005080300153 2005 8 3 TRBA2005032A 420050513A3460ALATR282 CIRCUIT BOARD AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FDAU UNIT BURNED A TRBAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO29355AT 355 DURING FLIGHT, CREW NOTED HEAVY ODOR OF ELECTRICAL WIRE BURNED. AIRCRAFT RETURNED TO DEPARTURE. REPLACED FDAU UNIT AS A PRECAUTIONARY METHOD. FURTHER INVESTIGATION REVEALED THAT AN INTERNAL PC BOARD (ALATR28-2) WAS BURNED. (K) 2H72 4T4 TRTA53EU E20NE 20050803001552005080300155EA 2005 8 3 ASOA05603 120050714A3350362624 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27844AS 7317 DURING A GROUND INSPECTION, THE EMERGENCY FLOOR LIGHTS ON THE RT SIDE FROM ROW 6 TO THE GALLEY WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT STRIPS FROM ROW 2 TO 5. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050803001562005080300156EA 2005 8 3 ASOA05604 120050714A5330 DOUBLER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27915EV 7754 DURING AN A-CHECK, THE FS 640 RT DOUBLER AT STRINGER 10 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FS 640 RT DOUBLER AT STRINGER 10. (K) 2L72 4F4 FRTA21EA E15NE 20050803001572005080300157SO 2005 8 3 CHQA200500135 120050802A2120 SMOKE EMB 145 EMB145MP 3260216SO CABIN DETECTED A CHQAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL11973RP 145444 ON T/O 1ST TIME ABORTED T/O AROUND 70KTS FOR A BRAKE OVERHEAT MESSAGE. RT INBD BRAKE PEGGED AT TOP OF SCALE, ALL OTHERS IN GREEN. ALL INDS IN GREEN BEFORE TAKING RUNWAY. MX R & R BRAKE TEMP SENSOR. OPS CHK GOOD. 2ND ATTEMPT, ROTATED & RECEIVED A CALL FROM FA NEAR 600 FT WITH A REPORT OF SMOKE. LEVELED OFF AT 5,000 FT. FA STATED SMOKE COMING FROM FLOOR NEAR ROW 7. IT SMELLED FAINTLY OF SMOKE. CONTINUE FLT. ON FINAL, ABOUT 20 MILES OUT, REPORTED SMOKE AGAIN, HEAVIER IN GALLEY & FLOOR VENT NEAR SEAT 3D, DISSIPATING. LANDED & FA SAID IT STOPPED BEFORE LANDING. GALLEY AREA & BINS SMELLED OF SMOKE AT GATE. BRAKES NORM TEMP & UNRELATED TO SMOKE. MX COULD NOT DUPLICATE SMOKE ODOR. 2L72 4F RTT00011AT 20050803001582005080300158WP 2005 8 3 ARWA20050706 120050731A5610NBA60451 WINDSHIELD DOUG DC10 DC1030F 3023504WP COCKPIT CRACKED A ARWAO OTHER O OTHER LDLANDING 1 SO19478CT 47819 AFTER LANDING CAPTAIN'S WINDSHIELD OUTSIDE CRACKED. REMOVED AND REPLACED CAPT WINDSHIELD IN ACCORDANCE WITH M/M 56-11-00; OPERATIONAL CHECK IN ACCORDANCE WITH M/M 30-41-00 AND M/M 30-42-00 FOUND NORMAL. 2L73 4F RTA22WE 20050803001632005080300163NM 2005 8 3 SWAA052233 120050728A53116546559 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29610WN 27696 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L TO STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050803001642005080300164NM 2005 8 3 SWAA052234 120050728A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29610WN 27696 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050803001662005080300166NM 2005 8 3 SWAA052236 120050728A53106547978 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29610WN 27696 DURING SCHEDULED D CHECK, FOUND FUSELAGE CREASE BEAM CORRODED AT BS 727E AND BS 864, STR 17L. REPAIRED BEAM SECTIONS PER SRM. 2L72 4F RTA16WE 20050803001672005080300167NM 2005 8 3 SWAA052237 120050728A55516551524 FITTING BOEING737 7373H4 1384600NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29610WN 27696 DURING SCHEDULED D CHECK, FOUND LT AND RT HORIZONTAL STAB FITTING LUG FACES CORRODED. REPAIRED LUG FACES PER SRM. 2L72 4F RTA16WE 20050803001692005080300169NM 2005 8 3 SWAA052226 120050727A53306545775 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29330SW 23694 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKS BETWEEN BS 727E + 3 AND BS 747, STR 19R. REPAIRED SKIN PER SWA EA AND SRM. 2L72 4F RTA16WE 20050803001712005080300171NM 2005 8 3 SWAA052158 120050724A53306545765 SKIN BOEING737 737317 138447PNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29661SW 23173 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 500A, STR 26R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050803001732005080300173NM 2005 8 3 SWAA052160 120050722A53306545765 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29694SW 23061 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 15L. REPAIRED SKIN PER SWA EA AND SRM. 2L72 4F RTA16WE 20050803001742005080300174NM 2005 8 3 SWAA052161 120050722A53306545765 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29694SW 23061 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 12R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050803001762005080300176 2005 8 3 SWAA052163 420050721A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29767SW 29807 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050803001782005080300178NM 2005 8 3 SWAA052165 120050722A3350MS155721 BULB BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29777QC 30592 DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY LIGHT INOP AT ROW 13 DEF. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050803001792005080300179NM 2005 8 3 SWAA052166 120050722A33506104781 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29777QC 30592 DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20050803001802005080300180 2005 8 3 SWAA052167 420050724A256563550101 SLIDE BOEING737 7377H4 1384404NM R1 DOOR MALFUNCTIONED A SWAAA UNSCHED LANDING O OTHER NRNOT REPORTED 1 SW29791SW 27886 R1 DOOR EMERGENCY EVAC SLIDE MALFUNCTIONED DURING EMERGENCY DEPLOYMENT. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20050803001812005080300181 2005 8 3 SWAA052168 420050724A2565940CW207 STRAP BOEING737 7377H4 1384404NM L1 DOOR SLIDE BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29791SW 27886 DURING SCHEDULED RON CHECK, L1 DOOR EMERGENCY EVAC SLIDE CASE BONDING STRAPS BROKEN. REMOVED AND REPLACED BONDING STRAPS PER MM. 2L72 4F RTA16WE 20050804000042005080400004NM 2005 8 4 UPS05445022 120050723A5313 STRINGER BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 BS 1958-1960 STR 1L STRINGER END FOUND CRACKED, CRACK LENGTH 3.875 INCH. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4 JUST AT STR - 1L BETWEEN BS 1930 AND 1960. 2L74 4F A20WE 20050804000052005080400005NM 2005 8 4 UPS05445023 120050723A5313 STRINGER BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 BS 1958-1960 STR 3L STRINGER END FOUND CRACKED, CRACK LENGTH 1.625 INCH. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4 JUST AT STR 3L BETWEEN BS 1930 AND 1960. 2L74 4F A20WE 20050804000062005080400006NM 2005 8 4 UPS05445024 120050723A5313 STRINGER BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 BS 1940-1960 STR 3R STRINGER END FOUND CRACKED, CRACK LENGTH 1.25 INCH. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4 JUST AT STR 3R BETWEEN BS 1930 AND 1960. 2L74 4F A20WE 20050804000082005080400008NM 2005 8 4 UPS05445026 120050725A532065B402133 FLOOR SUPPORT BOEING747 747121 1384871NM FUSLEAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 BS 400-420 LBL 52 LONGITUDINAL FLOOR SUPPORT FOUND CORROSION. CORROSION BLEND OUT 0.042 BY 1 BY 2 EXCEED SRM 53-10-01 FIG 1 LIMITS. FLOOR SUPPORT REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050804000092005080400009NM 2005 8 4 UPS05445027 120050723A5311 FRAME BOEING747 747121 1384871NM RT MLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 RT MLG WW STA 1394-1416 LOWER FRAME AT WEB FOUND CRACKED, UPPER OF LONGERON BOX, CRACK LENGTH .750. WEB REPAIRED AS PER SRM 51-40-03 FIG 1. 2L74 4F A20WE 20050804000112005080400011NM 2005 8 4 UPS05645031 120050802A4930 B-NUT BOEING767 767300 1385204NM FUELFLOW DIVIDERLEAKING A IPXAO OTHER KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO01311UP 27741 NOTICED FUEL FUMES DURING PREFLIGHT AND INITIAL CLIMB-OUT. RAN BOTH PACKS ON GRD, SMELLED FUMES IN COCKPIT. FOUND FUEL LEAKING AT APU FUEL FLOW DIVIDER INLET B NUT. REMOVED FROM INLET UNION, INSPECTED AND RESECURED PER 20-11-00-2. LEAK CHECKS GOOD. NO FUMES IN COCKPIT WITH APU PNEUMATICS. 2L72 4F RTA1NM 20050804000132005080400013WP 2005 8 4 UPS05845003 120050723A5320 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 A/C COMPT LONGERON END FITTING CORRODED AROUND FASTENER HOLE AT STA 70 L32R. REMOVED AND REPLACED LONG END FITTING AT STA 70 L32R IAW SRM 57-1-20D, AND 51-3-2. 2L74 4F RT4A25 20050801000252005080100025 2005 8 1 ASMF200507024 420050728A3423258733513 GYRO DOUG MD80 MD83 3023681NM VERTICAL FAILED W ASMFA UNSCHED LANDING O OTHER CRCRUISE 1 SW23881LF11468 53051 AIRCRAFT PERFORMED A TECHNICAL LANDING AT CUL DUE TO WHEATEAR CONDITIONS AT HMO. AT CUL CAPTAIN REPORTED THAT DURING TURNS THE RADAR GOES OUT OF SERVICE, SO VERTICAL GYRO NR 2 WAS REPLACED IAW MM 34-23-00, TESTED CORRECT. AIRCRAFT WAS DISPATCHED AND CAPTAIN REPORTED THAT DURING TURNS ADI GOES OUT OF SERVICE, SPHERE AT 90 GRADES WITH FAIL FLAG, AUTOMATIC PILOT DISENGAGE, FMA WITH NO AUTO-LAND LIGHTS, AND NO ECHO’S WERE REGISTERED AT 40 MILES OR LEAST. VERTICAL GYRO NR 2 AND RADAR TRANSCEIVER WERE REPLACED IAW MM 34-23-00 AND 34-41-00 RESPECTIVELY, TESTED CORRECT. 2L72 4F RT 20050801000382005080100038WP 2005 8 1 ABXA050179 120050728A793141800141 TRANSMITTER DOUG DC8 DC863 302198AWP OIL PRESS INDICADEFECTIVE A ABXAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL23825AX 46115 NR 3 ENGINE OIL PRESSURE PEGGED OFF SCALE HIGH. ENGINE WAS SECURED AND FLIGHT CONTINUED ON TO IAD. OIL PRESSURE REMAINED PEGGED OUT HIGH. PERFORMED ENGINE INSPECTION IAW P&W JT3D MM 72-00. OIL FILTER FOUND CLEAN. REMOVED AND REPLACED OIL PRESSURE TRANSMITTER IAW DC-8 AMM. GROUND RUN CHECKED GOOD. 2L74 4F 4A25 20050801000432005080100043WP 2005 8 1 05FDEA02127 120050728A2750AEH72733 BRACKET DOUG MD10 MD1010F 3022112WP ZONE 500 BROKEN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25391FE 46625 COMPLY WITH EA 8-2750-82100A FLIGHT CONTROL-FLAP-REPLACMENT OF FLAP CONTROL BRACKET. COMPLIED WITH EA 8-2750-82100A. FLIGHT CONTROL FLAP REPLACMENT OF LWR CONTROL BRACKET. 2L73 4F RTA22WE 20050801000512005080100051EU 2005 8 1 05FDEA02136 120050729A5742A5461004200200 FITTING AIRBUS300 A300F4605R 3930327EU NR 1 PYLON CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25671FE 778 FOUND THE NR 1 ENG PYLON, INBD MOUNT OUTBD SHACKLE HAS PITTING CORROSION IN THE FACE SIDE OF THE SHACKLE. 2L72 4F RTA35EU 20050801000562005080100056CE 2005 8 1 DJFA2005122 120050728A3260MS243311 DOWNLOCK SWITCH BEECH MU300 400A 1155402CE NLG FALSE INDICATIONE DJFAO OTHER N FALSE WARNING LDLANDING 1 EA23898TA RK295 ON APPROACH, CREW RECEIVED 2 GREEN & NO RED GEAR INDICATIONS. NLG LIGHT WOULD NOT ILLUMINATE, BUT LIGHT WOULD TEST. NO CHANGE IN GEAR DOWN INDICATION WHEN CREW CYCLED MLG TWICE. TOWER HAD CONFIRMED NLG DOWN DURING A LOW APPROACH, BUT AURAL "TOO LOW GEAR" WARNING CAME ON. NLG GREEN INDICATION DID NOT ILLUMINATE WHEN USING THE "EMERGENCY LANDING GEAR DOWN" HANDLE. AFTER PUSHING THE "EMERGENCY DOOR CLOSE" HANDLE BACK IN, RED LIGHT DID EXTINGUISH. "TOO LOW GEAR" AURAL WARNING SOUNDED THROUGHOUT FINAL APPROACH & ALL THE WAY TO TOUCHDOWN. AFTER STOWING THRUST REVERSERS, BOTH THRUST REVERSER ARM LIGHTS REMAINED ILLUMINATED. MX R & R NLGE DOWNLOCK SWITCH. ALL OPS CHECKS WERE GOOD AND THE A/C TURNED TO SERVICE.2H72 4F RTA16SW 20050801000612005080100061NM 2005 8 1 USAA200507005 120050729A5752 SKIN BOEING737 7373B7 1384580NM TRIM TAB DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19531AU 24478 3 INCH BY 4 INCH AREA OF DELAMINATION ON TRAILING EDGE OF TAB, 18 INCH FROM OUTBOARD END. WET COMPOSITE LAYUP PER SRM 51-70-16. 2L72 4F RTA16WE 20050801000732005080100073SO 2005 8 1 C2XA05RI014 120050710A3350 SIGN EMB 145 EMB145ER 3260211SO EMERGENCY EXIT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713936 145025 RIC - DURING ROUTINE INSPECTION, EXIT ROW SIGN IN FRONT OF SEAT 3BC WAS FOUND INOP. MAINTENANCE CHECK THE BULBS AND CLEANED THE CONTACTS. OPERATIONAL TEST WAS PERFORMED SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20050801000742005080100074EU 2005 8 1 MALA050615 120050728A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15452XJ 340B452 SEAT TRACK AT LBL18.3 FROM FS 294 TO FS 310 IS CORRODED AND HAS BEEN REPAIRED IAW SRM 53-70-60 REF: EAMS WORK ORDER 21-26-37 TASK 1510. 2L72 4T RTA52EU 20050801000802005080100080EA 2005 8 1 A6WA200540246 120050713A5320601R3HB58 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31409AW 7447 RT FS 280 AT RBL 9 IB CLIP ANGLE IS CRACKED .5 INCH LONG. REPLACED CLIP IAW SRM. (K) 2L72 4F4 FRTA21EA E15NE 20050802000072005080200007EA 2005 8 2 A6WA200540256 120050720A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE ENGINE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31418AW 7618 ENGINE SUPPORT BEAM LOWER WEB IS CRACKED AT FWD IB CORNER OF THE RT ACCESS PANEL CUT OUT. ENGINE SUPPORT BEAM LOWER WEB WAS REMOVED AND REPLACED BY MODIFICATION OF BEAM UNDER WO 81584 JOB CARD 4EOMFG08364, SEG NR 14, EO2/081/453. (K) 2L72 4F4 FRTA21EA E15NE 20050802000162005080200016EA 2005 8 2 A6WA200540257 120050702A5320601R31058381 CHANNEL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31462AW 7875 CHANNEL OF MAIN UNDERCARRIAGE AND UPLOCK APRON BENT AND CRACKED. REPAIRED IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050802000302005080200030NM 2005 8 2 AALA20050480 120050715A5711 SPAR BOEING767 767323 1385205NM WING CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21386AA 27060 AFW - REAR SPAR WEB WING CENTER SECTION OUTBOARD SIDE OF THE INBOARD LEG OF THE PICKLE FORK HAS BLEND IN AREA APPROXIMATELY 3 INCH BY 0.5 INCH WITH A DEPTH OF 0.067 INCH. REMOVED EXPOSED CORROSION FROM THE REAR SPAR SURFACE. UNDERCUT THE SPAR AND PICKLE FORK APPROXIMATELY ONE EIGHTH INCH TO REMOVE ANY POSSIBLE CORROSION UNDER THE PICKLE FORK. PERFORMED A DETAILED VISUAL INSPECTION TO ENSURE CORROSION WAS REMOVED. ALODINED, PRIMED, AND APPLIED LIBERAL AMOUNTS OF BMS 335. 2L72 4F RTA1NM 20050802000322005080200032EU 2005 8 2 SA05091 120050729A335032145410 EPSU AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT FAULTY A USAAK NONE L NO TEST ININSP/MAINT 1 EA19748UW13740832 1311 PHL - THE FORWARD EMERGENCY POWER SUPPLY UNIT FAULTED DURING THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE FORWARD EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20050802000342005080200034WP 2005 8 2 ARWA20050705 120050730A2612 WIRE DOUG DC8 DC863F 302198FWP NR 4 FIRE LOOP DAMAGED A ARWAO OTHER N FALSE WARNING LDLANDING 1 SO19661AV 45969 AFTER LANDING, FIRE WARNING CAME ON; ENGINE NR 4. COMPLETED APPROPIATE CHECKLIST. REPAIRED WIRING ON NR 4 FIRE WARNING LOOP CONNECTOR (AFT) IN ACCORDANCE WITH M/M 20-50-1. CHECK GOOD IN ACCORDANCE WITH M/M 26-10-0 AND M/M 71-00. 2L74 4F 4A25 20050802000352005080200035NM 2005 8 2 PCSA07300501 120050730A2130 CONTROL SYSTEM BOEING727 7272D3 138407NNM CABIN PRESSURE UNCONTROLLABLE A PCSAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO17804AJ 21021 FLIGHT 8316 - AFTER TAKEOFF FROM BAQ AIRCRAFT UNABLE TO PRESSURIZE, FLIGHT CREW COMPLETED ALTERNATE PROCEDURE WITH NO SUCCESS AND RETURNED BACK TO BAQ WITHOUT FURTHER INCIDENT. MAINTENANCE VISUALLY INSPECTED MAIN CARGO DOOR FOR LEAKS, CHECKED C1, C2, AND AFT ENTRY DOOR FRAME AND SEALS FOR LEAKS. PERFORMED AMERIJET 7-29 PRESSURIZATION WORK CARD, OPERATIONAL CHECK OK. PERFORMED DECAY CHECK IAW B-727 MM CH 5-51-101, DECAY CHECK WITHIN LIMITS. COULD NOT DUPLICATE PROBLEM, AIRCRAFT RETURNED TO SERVICE. 2L73 4F A3WE 20050802000472005080200047EA 2005 8 2 ASOA05558 120050627A33506100976 LAMP CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11723EV 10132 DURING A C-CHECK IN MCN, THE EMERGENCY CEILING LIGHT AT ROW 17 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY CEILING LIGHT AT ROW 17. OPERATIONAL CHECKS GOOD. (M) 2L72 4F RTA21EA 20050802000532005080200053EU 2005 8 2 USAA050872 120050713A5315D5311281820401 FLOORBEAM AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19109UW19030 1065 PIT - FOUND FLOORBEAM CORRODED .5 INCH DIAMETER BY .050 DEEP AREA, FLOORBEAM AT C16 Y254. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-72-11. CORROSION LEVEL 1, TASK JA-220-53500. (M) 2L72 4F RTA28NM 20050802000562005080200056NM 2005 8 2 AWXA200500869 120050708A53206517583504 VERTICAL BEAM BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 DURING C16 CHECK, DISCOVERED TWO CRACKS, .7 INCHES AND .6 INCHES IN LENGTH, LOCATED AT VERTICAL BEAM WEB AT BS 178, BL 5.7R, FROM WL 175 TO WL 185. MAINTENANCE CUT AND REMOVED SECTION OF CRACKED WEB AT BS 178, BL 5.7R AND WL 175 TO 185 IAW BOEING 737-300 SRM 53-10-08-20 FIG 212. FABRICATED DOUBLER AND WEB IAW BOEING 737-300 SRM 53-10-08-2. INSTALLED FABRICATED REPAIR PARTS AT BS 178, BL 5.7R, FROM WL 175 TO WL 185 IAW BOEING 737-300 SRM 53-10-08-2 FIG 212. 2L72 4F RTA16WE 20050802000572005080200057NM 2005 8 2 AWXA200500870 120050708A53126516300510 BULKHEAD BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 DURING C16 CHECK, DISCOVERED BULKHEAD AT BS 178, CENTER WEB, CRACKED 1.1 INCHES IN LENGTH AT BL 6.5R, WL 201. MAINTENANCE REMOVED DAMAGED SECTION OF WEB, LOCATED AT BS 178, BL 6.5R, WL 201, IAW BOEING 737-300 SRM 53-10-08-2 FIG 212. FABRICATED THREE FILLERS, DOUBLER AND STIFFENER IAW BOEING 737-300 SRM 53-10-08-2 FIGURES 1 AND 209. MAINTENANCE INSTALLED FABRICATED REPAIR PARTS AT BS 178 BULKHEAD, BL 6.5R, WL 201 IAW BOEING 737-300 SRM 53-10-08-2 FIG 209. 2L72 4F RTA16WE 20050802000632005080200063NM 2005 8 2 AWXA200500876 120050731A5330 SKIN BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 DURING B4 CHECK, DISCOVERED CRACK IN FUSELAGE STA 947.5, STRINGER 23R, FORWARD OF THE OUTFLOW VALVE. MAINTENANCE REMOVED DAMAGED AREA AT STA 947.5, STR 23R IAW BOEING 737-300 SRM 53-00-01. FABRICATED DOUBLER IAW BOEING 737-300 SRM 53-00-01. INSTALLED FABRICATED REPAIR PARTS IAW BOEING 737-300 SRM 53-00-01. A MONITOR WAS INSTALLED TO RE-INSPECT 60,000 CYCLES FROM REPAIR INSTALLATION. PART AND CRACK LENGTH INFO UPDATED. 2L72 4F RTA16WE 20050802000742005080200074NM 2005 8 2 UPS05544993 120050730A2560 SMOKE GOGGLES BOEING757 75724APF 1384969NM COCKPIT BROKEN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01405UP 23727 GOGGLES BROKEN IN COCKPIT. REMOVED AND REPLACED GOGGLES IN COCKPIT. OK FOR SERVICE. 2L72 4F RTA2NM 20050802000862005080200086EU 2005 8 2 AALA20050469 120050726A3350BR964814 LIGHT AIRBUS300 A300B4605R 3930308EU SEAT 14G - 28G INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2114065 508 JFK - EMERGENCY LIGHT AT SEAT 14G AND 28G INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEATS 14G AND 28G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20050802000882005080200088NM 2005 8 2 AALA20050477 120050617A5415 FITTING BOEING767 767223 1385123NM SPAR OUT OF LIMITS A AALAK NONE O OTHER ININSP/MAINT 1 SW21319AA 22320 AFW - LEFT HAND STRUT OUTBOARD MIDSPAR FITTING HAS BEEN MACHINED TO 1.871 INCH DIAMETER ON NR 1 LUG. REPAIRED LEFT HAND STRUT OUTBOARD MIDSPAR FITTING ON NR 1 LUG PER SRM 54 51 90 2 FIGURE 203 SERVICE BULLETIN 767 54 0059. 2L72 4F RTA1NM 20050802000902005080200090EU 2005 8 2 AWXA200500882 120050713A5340D53112198200 FITTING AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28627AW 66 DURING C4 CHECK DISCOVERED CORROSION ON LOWER SILL OF L1 DOOR, FROM FS 16 TO FS 20, Y 1584. NO ALLOWABLE LIMITS FOUND. MAINTENANCE REMOVED AND REPLACED THE FITTINGS ON L1 DOOR, LOWER SILL, FROM FS 16 TO FS 20, Y 1584, IAW AIRBUS 320 SRM 51-72-11. 2L72 4F RTA28NM 20050802000972005080200097EU 2005 8 2 AWXA200500889 120050713A5347D5337111200 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28627AW 66 DURING C4 CHECK, DISCOVERED CORROSION ON THE RT OUTBOARD SEAT TRACK FS 41+10, -Y1292. MAINTENANCE REMOVED CORROSION IAW A320 SRM 51-75-00 AND FOUND REWORK TO BE OUT OF LIMITS IAW A320 SRM 53-31-15. RT OUTBOARD SEAT TRACK, AT FR 41+10, -Y1292, WAS REMOVED IAW A320 SRM 51-47-11 AND NEW SEAT TRACK WAS PREPARED FOR INSTALLATION IAW A320 SRM 51-44-11. INSTALLED REPAIR PARTS, AT FR 41+10, -Y1292, IAW A320 SRM 51-42-11 AND DRAWING NR D53370500. 2L72 4F RTA28NM 20050802001042005080200104CE 2005 8 2 AMWA72057 120050801A7712 CONNECTOR BEECH 1900 1900D 1154162CE TORQUE INDICATORDIRTY A AMWAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 CE07155YV 155YV ON TAKEOFF ROLL OUT, CREW OBSERVED RIGHT ENGINE UNABLE TO ACHIEVE TAKEOFF POWER. RETURNED TO GATE WITH NO FURTHER INCIDENT. THE CORRECTIVE ACTION WAS AS FOLLOWED: MAINTENANCE CLEANED AND SECURED CONNECTOR AT TORQUE INDICATOR. THEREFORE NO PARTS WERE USED. 2L72 4T RTA24CE 20050802001102005080200110NM 2005 8 2 CALA0500244 120050730A5320141A8310U31 STRAP BOEING737 737724 13844BYNM FLOORBEAM CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2725705 28766 INSPECTION FOUND LIGHT CORROSION ON STRAP/FLOORBEAM I/B OF R-1 DOOR THRESHOLD PLATE FROM STA 294.5 - 344. THE STRAP AND FLOOR CHORD WERE REMOVED AND REPLACED IAW SRM 51-10-02, 51-40-02, AND 53-10-15. 2L72 4F RTA16WE 20050802001192005080200119NM 2005 8 2 KPVA200511 120050723A5730 SKIN DHAV DHC8 DHC8103 1386005NM LT WING TIP DAMAGED A KPVAO OTHER O OTHER TXTAXI/GRND HDL 1 WP13806WP 357 LT WING TIP IS TORN ALMOST ALL THE WAY OFF. REPAIRED LT WING TIP IAW RD8-57-3143. REMOVED AND REPLACED LT AILERON IAW DHC MM 27-12-11 PG 201-204. RIGGED AILERON CONTROL SYSTEM IAW DHC-8 MM 27-12-00 PG 201-213. NO DEFECTS NOTED. REMOVED AND REPLACED LT WING TIP IAW RD 8-57-3143. OPERATIONAL CHECK OF LT POSITION AND ANTI-COLLISION LIGHT IAW DHC-8 MM 33-40-31 PG 201 AND DHC-8 MM 33-40-27 PG 206. NO DEFECTS NOTED. 2H72 4T RTA13NM 20050802001612005080200161EU 2005 8 2 05FDEA02144 120050730A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU ZONE 200 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25671FE 778 MAIN DECK CARGO SEAT TRACK AT FRAME 41 TO 44 BL0 HAS CORROSION ALONG LENGTH NOTED. REMOVED SEAT TRACK, FABRICATED NEW SEAT TRACK ON TRAVELER NR T5/534305 IAW SRM 53-15-16. LOCATED AND DRILLED IAW SRM 53-10-16. TREATED AND PRIMED IAW SRM 51-21-10. INSTALLED NEW SEAT TRACK IAW SRM 53-10-16. PAINTED SEAT TRACK IAW SRM 51-23-10. 2L72 4F RTA35EU 20050802001632005080200163EU 2005 8 2 05FDEA02146 120050730A5311 FRAME AIRBUS300 A300F4605R 3930327EU FUSELAGE GOUGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25671FE 778 COMPLY WITH EA 6-5310-82108, FUSELAGE MAIN FRAME, FRAME 28, GOUGE REPAIR STR 18L THROUGH STR 22L. COMPLIED WITH EA 6-5310-82108 FUSELAGE, MAIN FRAME, FRAME 28, GOUGE REPAIR STR 18L THROUGH STR 22L. 2L72 4F RTA35EU 20050802001652005080200165EU 2005 8 2 05FDEA02148 120050730A3230GA559411 ROD AIRBUS300 A300B4622 3930401EU NLG BROKEN A FDEAA UNSCHED LANDING GJ MULTIPLE FAILURE WARNING INDICATION CLCLIMB 1 SO25716FD 358 AFTER T/O, LANDING GEAR WOULD NOT RETRACT. SELECTED SYS 2 ON POSITION SELECTOR AND ATTEMPTED TO RETRACT. GEAR WOULD NOT RETRACT, NEXT PITCH TRIM 1&2 TRIPPED OFF AND WOULD NOT RESET. AUTOTHROTTLES 1&2 TRIPPED OFF AND WOULD NOT RESET. CREW DECLARED EMERG, RETURNED. ALL ELEC/HYD INDICATIONS WERE NORMAL. NO C/B`S OPEN. AFTER LANDING, ALL SWITCHES WOULD RESET. SYS ACTED LIKE A/C NEVER LEFT GROUND. CHECKED PROX BOX FOUND SN INDICATION FOR NOSE SHOCK ABSORBER. FOUND BEARING WORN ON NOSE SHOCK EXTENSION TARGET ARM. REPLACED BROKEN ROD ASSY ON CONNECTING ARM FOR NOSE GEAR PROX DETECTOR SWITCH ASSY IAW A300AMM 32-00-00. GEAR SWING OPS CHECK NORMAL. 2L72 4F RTA35EU 20050802001672005080200167NM 2005 8 2 05FDEA02150 120050731A5313 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 CENTER CARGO BILGE STATION 1751 LONGERON 46R CORROSION FOUND AS MARKED. CORROSION ON CENTER CARGO BILGE STATION 1751 LONGERON 46 R/H REMOVED AS PER SRM 51-21-01 VOL II AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-01, FIG 3, VOL I. ORIGINAL THICKNESS=0.145", THICKNESS REMOVED=0.053" & THICKNESS REMAINING=0.092". REPAIR CARRIED OUT ON EXCEEDED LIMIT AREA AS PER SRM 53-10-00, FIG 2A, VOL I. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050802001692005080200169NM 2005 8 2 05FDEA02158 120050801A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE LT NR 30 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA1-5510-87597. 2L73 4F RTA22WE 20050802001712005080200171NM 2005 8 2 05FDEA02160 120050801A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE LT NR 26 FOUND WITH CORROSION EXCEEDING LIMITS. CORRODED FITTING REMOVED AND NEW FITTING INSTALLED PER SRM 51-38-01 VOL II AND SRM 51-33-01 VOL II. MINOR REPAIR PER GMM 6-2-100. 2L73 4F RTA22WE 20050802001732005080200173NM 2005 8 2 05FDEA02162 120050801A5313 LONGERON DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 CENTER CARGO COMPARTMENT HAS STA 1787 RT LONGERON 45 CRACKED. REMOVED AND REPLACED AS PER DRAWING AFA7097 AND SRM 51-31-01. 2L73 4F RTA22WE 20050802001752005080200175NM 2005 8 2 05FDEA02164 120050801A574065327348 ATTACH FITTING BOEING727 727233 138408ANM NR 8 FLAP TRACK CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 CORROSION (27X5710-02) NR 8 FLAP TRACK FWD ATTACH FTG ON WING IS CORRODED ON I/B FACE. REPAIRED FITTING PER EA 7-5750-92237 2L73 4F RTA3WE 20050802001762005080200176EU 2005 8 2 05FDEA02165 120050730A3230 ROD AIRBUS300 A300B4622 3930401EU NLG BROKEN A FDEAA UNSCHED LANDING JG WARNING INDICATION MULTIPLE FAILURE CLCLIMB 1 SO25716FD 358 AFTER T/O LANDING GEAR WOULD NOT RETRACT. SELECTED SYSTEM 2 ON POSITION SELECTOR AND ATTEMPTED TO RETRACT. GEAR WOULD NOT RETRACT. NEXT PITCH TRIM 1&2 TRIPPED OFF AND WOULD NOT RESET. AUTOTHROTTLES 1&2 TRIPPED OFF AND WOULD NOT RESET. CREW DECLARED EMERGENCY, RETURNED AND LANDED. FOUND BEARING WORN ON NOSE SHOCK EXTENSION TARGET ARM. REPLACED BROKEN ROD ASSY ON CONNECTING ARM FOR NOSE GEAR PROX DETECTOR SWITCH ASSY IAW A300AMM 32-00-00. GEAR SWING OPS CHECK NORMAL. 2L72 4F RTA35EU 20050802001772005080200177WP 2005 8 2 05FDEA02166 120050801A5740 ATTACH FITTING DOUG DC10 DC1010 3022110WP ZONE 600 BROKEN A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25367FE 46605 RT I/B FLAP, I/B ACTUATOR AFT ATTACH FITTING BROKEN. REMOVED RT I/B FLAP I/B ACTUATOR SUPPORT FITTING PER MM 27-52-01-2 STEPS A1 THRU ALL. INSTALLED NEW R/H I/B FLAP I/B ACTUATOR SUPPORT FITTING PER MM 27-52-1-2. ENLARGED & REAMED FOUR HOLES IN FITTING PER SERVICE BULLETIN 57-76. DAMAGED LOCK FASTENERS ON LOWER BOTTOM SIDE OF ACTUATOR SUPPORT. STRUCTURE TO BE REPLACED AT NEXT C-CHECK PER EA 8-5750-86513. INSTALLED NEW HYD LINES PER MM 27-52-01-2. LEAK & OPERATIONAL CHECKS COMPLIED WITH PER MM 27-52-01-2 2L73 4F A22WE 20050802001782005080200178WP 2005 8 2 ABXA050180 120050725A5311S27779223 FRAME DOUG DC9 DC931 3022065WP E/E BAY CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23907AX 47203 LONGERON 23 LEFT CRACKED AT FRAME, FS 200. REPAIRED AREA IAW DC-9 SRM 53-02. 2L72 4F A6WE 20050802001792005080200179WP 2005 8 2 ABXA050181 120050726A52303914025501N FITTING DOUG DC9 DC931 3022065WP CARGO DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23907AX 47203 AFT LOWER BAG BIN DOOR NR 1 BEAM FORWARD END FITTING CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-1. 2L72 4F A6WE 20050802001802005080200180NM 2005 8 2 RYNA200500024 120050624A5522 SKIN BOEING757 757236 1384971NM ELEVATOR SEPARATED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07526NA 24794 TRAILING EDGE OF LEFT ELEVATOR AT STATION 76.547 IS SEPARATED APPROXIMATELY 1 INCH. ELEVATOR REPAIRED PER B757 SRM 51-70-04. 2L72 4F RTA2NM 20050802001812005080200181NM 2005 8 2 0501185805 120050801A2120 ODOR BOEING757 757351 1384991NM CABIN DETECTED A NWAAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL01585NW 32985 DURING TAXI , PASSENGER AND CREW SMELLED ELECTRICAL ODOR NEAR ROW 6. AIRCRAFT RETURNED TO BLOCKS AND FLIGHT CHANGED TO A/C5643. CHECK SEAT BOXES IN 1ST CLASS AND NOTHING FOUND. RAN NR 1 ENGINE AND PACKS AND THERE WAS A STRONG OIL SMELL IN THE COCKPIT AND CABIN. REPLACED THE EQUIPMENT COOLING FILTER AND BURNED OFF OIL SMELL BY RUNNING BOTH ENGINES, PACKS AND APU. 2L72 4F RTA2NM 20050802001822005080200182NM 2005 8 2 05FDEA02156 120050801A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE RT NR 29 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA1-5510-87597. [CLOSED] 2L73 4F RTA22WE 20050802001832005080200183NM 2005 8 2 05FDEA02157 120050801A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE RT NR 31 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA1-5510-87597. 2L73 4F RTA22WE 20050802001852005080200185EU 2005 8 2 05FDEA02142 120050729A5753 SKIN AIRBUS300 A300F4605R 3930327EU LT WING TE FLAP DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25671FE 778 LT WING I/B T/E FLAP LWR SKIN MID O/B SECTION HAS CREASE. FOUND CREASE TO BE OUT OF LIMITS IAW SRM 57-50-00 FIG 101. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS ON MAE TRAVELER T5/532877 LOCATED, DRILLED, AND INSTALLED IAW SRM 57-50-00 FIG 206. TREATED/PRIMED IAW SRM 51-21-10. PREPPED AND PAINTED IAW MM 51-75-10-8. 2L72 4F RTA35EU 20050802001872005080200187SO 2005 8 2 LR7A05098 120050801A5312 PRESSURE PANEL LKHEED382 382G 526414USO LT MLG WW CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03405LC 2470 5025 DURING SCHEDULED C-5 INSPECTION PER JOB CARD HC5323, FOUND FS 576 LT MLG WHEEL WELL CHINE ANGLE TO CHINE CAP WEB CRACKED .125 INCH AT BOLT HOLE, LBL 62, WL 145. REPAIRED IAW SRM SMP 583 51-140-17, NR 2059. 2H74 4T A1SO 20050803000162005080300016NM 2005 8 3 2005UALA00690 120050724A2913693335 MOTOR AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE PUMP FAILED A UALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 WP29840UA 1522 RETURN TO FIELD WITH A BLUE HYDRAULIC OVERHEAT INDICATION. BLUE HYD ELECT OVERHEAT. SHUTDOWN BLUE PUMP. WARNING CLEARED AFTER 5 MINS. CYCLED CB C12 PER SAMC AND RESTARTED BLUE PUMP. FAULT THEN RETURNED. QTY NORMAL. PUMP JUST REPLACED DUE TO POPPED CB AB9:RAN PUMP BEFORE REMOVAL. PUMP FAILED. CKED HP FILTER. NO DEBRIS. REPLACED BLUE PUMP REF 29-12-51. OPS NORMAL. CREW REPORTS WITH BOTH ENGINES RUNNING BLUE SYSTEM ELECTRIC PUMP FAULT. FOUND BLUE ELEC PUMP CB ON THE VU123 PANEL POPPED GRID AB9. RESET CB AND CB POPPED AGAIN. REPLACED BLUE ELECTRIC PUMP REF MM 29-12-51. OPS NORMAL. 2L72 4F4 FRTA28NM E40NE 20050803000262005080300026NM 2005 8 3 2005UALA00706 120050723A33501317 LAMP BOEING757 757222 1384956NM PWA 2037 PW2037 NE ROW 5 BURNED OUT A UALAK NONE L NO TEST ININSP/MAINT 1 WP29513UA 24810 EMERGENCY AISLE ILLUMINATION LIGHT INOP AT ROW 5. REPLACED LAMP. 2L72 4F4 FRTA2NM E17NE 20050803000282005080300028NM 2005 8 3 2005UALA00708 120050725A5230 SKIN BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE AFT CARGO DOOR DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29914UA 25381 AFT CARGO DOOR EXT SKIN HAS 8 EA DENTS. REPAIR ACP'D PER SRM 52-00-01, 41" BY 23" DOUBLER INSTALLED. 2L72 4F4 FRTA16WE E2GL 20050803000292005080300029NM 2005 8 3 2005UALA00709 120050725A5311 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29914UA 25381 FUSELAGE FRAME STA 663 IS CRACKED AT STR 1 CUTOUT. MAJOR REPAIR ACP'D PER SRM 53-00-07 AND BACO DRAW 65-73740. 2L72 4F4 FRTA16WE E2GL 20050803000332005080300033EU 2005 8 3 MALA050625 120050731A5410 STRUCTURE SAAB SF340 340B 7860101EU RT NACELLE CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15452XJ 340B452 RT NACELLE ATNS 197 OB SIDE IS CHAFED AND HAS BEEN REPAIRED IAWS MESABA EO 54124 REF EAMS WORK ORDER 212637 TASK 4508. 2L72 4T RTA52EU 20050803000582005080300058NM 2005 8 3 2005UALA00727 120050728A3350276005 FUSE BOEING747 747422 1384935NM PWA 4056 PW4056 NE LT OVERWING BURNED OUT A UALAK NONE L NO TEST ININSP/MAINT 1 WP29182UA 25279 EMERG LTS INOP, LT OVERWING 2 EA AFT MOST ASSY'S. REPLACED FUSE IN PWR SUPPLY. 2L74 4F4 FRTA20WE E24NE 20050803000912005080300091EU 2005 8 3 YENA200543 120050728A5210FE240004 CYLINDER DAMPER AIRBUS320 A320232 3930326EU R1 DOOR LEAKING A YENAK NONE O OTHER ININSP/MAINT 1 EA15558JB10494 1915 R1 DOOR EMERGENCY CYLINDER, DAMPER LEAKING. REPLACED R1 DOOR EMERGENCY CYLINDER, DAMPER IAW A320 MM 52-13-14-000-001. 2L72 4F RTA28NM 20050803000962005080300096 2005 8 3 SWAA052117 420050720A2565D31354 SLIDE BOEING737 7375H4 138449DNM R2 DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29507SW 24184 R2 DOOR EVACUATION SLIDE OUT OF POSITITON. REPOSITIONED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20050803000982005080300098NM 2005 8 3 SWAA052119 120050720A53116546525 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 18R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050803000992005080300099 2005 8 3 SWAA052120 420050719A2565416A2200 SLIDE BOEING737 7377H4 1384404NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29795SW 30606 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20050803001032005080300103NM 2005 8 3 SWAA052125 120050720A53126517583 VERTICAL BEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29609SW 27929 DURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD RT VERTICAL BEAM WEB CRACKED AT RBL 17, WL 227. REPAIRED BEAM PER SRM. 2L72 4F RTA16WE 20050803001202005080300120NM 2005 8 3 SWAA052254 120050729A33507003661 BALLAST BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29362SW 26573 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BALLAST PER MM. 2L72 4F RTA16WE 20050803001212005080300121 2005 8 3 SWAA052256 420050731A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29450WN 32470 R2 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. SLIDE DID NOT DEPLOY. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20050803001282005080300128 2005 8 3 SWAA052263 420050729A256565659723 BRACKET BOEING737 7373Y0 1384671NM GIRT BAR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR BRACKET LOOSE. SECURED BRACKET PER MM. 2L72 4F RTA16WE 20050803001382005080300138NM 2005 8 3 DHL2005754006 120050802A3350 LIGHT BOEING727 727223 1384074NM CABIN INOPERATIVE A DHLAK NONE O OTHER ININSP/MAINT 1 SO01754DH 22008 EMERGENCY EXIT LIGHT ABOVE DOOR 1 LEFT IS INOP. REMOVED AND REPLACED EMERGENCY EXIT ASSY ABOVE ENTRY DOOR 1L AS PER MM 33-50-01. PERFORMED OPS CHECK. OPS CHECKED OK. 2L73 4F A3WE 20050803001452005080300145NM 2005 8 3 SWAA052222 120050728A531165C22908 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKS AT BS 500B, BETWEEN STR 20R AND STR 20L. REPAIRED FRAME PER SWA EA. 2L72 4F RTA16WE 20050803001602005080300160NM 2005 8 3 SWAA052230 120050727A335090083 BATTERY PACK BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29475WN 32474 DURING SCHEDULED MV2 CHECK, FOUND RT CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050803001612005080300161NM 2005 8 3 SWAA052231 120050728A53306545765 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 522, STR 10R. REPAIRED SKIN PER SWA EA . 2L72 4F RTA16WE 20050803001622005080300162NM 2005 8 3 SWAA052232 120050728A5315BAC15171489 FLOORBEAM BOEING737 7373H4 1384600NM COCKPIT CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29610WN 27696 DURING SCHEDULED D CHECK, FOUND COCKPIT FLOORBEAM CORRODED AT BS 270, BL 0 TO RBL 14. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20050803001682005080300168NM 2005 8 3 QXEA200501146 120050801A7930 ENGINE BOMBDRDHC8 DHC8402 1390042NM PWC 150 PW150A EA NR 1 MALFUNCTIONED A QXEAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 NM09411QX8346 1509 4055 PCEFA0098 MSO FLIGHT NR 383 - DURING CRUISE, MASTER WARNING NR 1 OIL PRESSURE GAUGE SHOWED NO PRESSURE AND OIL TEMPERATURE WAS INCREASING. SHUT-DOWN ENGINE AS PER E/A CHECKLIST. ADVISED F/A'S TO PREPARE CABIN FOR NORMAL LANDING AT MSO. AIRCRAFT STILL OUT OF SERVICE. MAINTENANCE CHANGED ENGINE. 2H72 4T4 TRTA13NM E00062EN 20050803001722005080300172NM 2005 8 3 SWAA052159 120050722A53306545774 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29694SW 23061 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 741, STR 23L. REPAIRED SKIN PER SWA EA AND SRM. 2L72 4F RTA16WE 20050803001752005080300175 2005 8 3 SWAA052162 420050722A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29756SA 27872 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050804000102005080400010NM 2005 8 4 UPS05445029 120050722A5320 WEB BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 BS 2320-2340 S26R WEB FOUND CRACKED AT AFT PORTION AREA, CRACK LENGTH .375. BS 2337 TO BS 2340 WEB REPAIRED AS PER SRM 51-40-03 FIG 1. 2L74 4F A20WE 20050804000122005080400012WP 2005 8 4 UPS05845002 120050113A5340 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 CORROSION UNDER SMALL CHAFF PAD IN C-PIT TORQUE BOX STA 1200 L34R. REMOVED CORROSION FROM UNDER CHAFF PAD IAW SRM 51-1-8 53-2-0. CORROSION OUT OF LIMITS IAW SRM 53-2-0. FABRICATED REPAIR DOUBLER AND INSTALLED DOUBLER AT STA 1200 L34R IAW SRM 51-1-8 AND DWG 3753772 AND SRM 53-2-0. 2L74 4F RT4A25 20050804000352005080400035WP 2005 8 4 UPS05845004 120050707A5340 SPLICE DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 MAIN CABIN STA 680 L2R LONG SPLICE FITTING CRACKED. REMOVED AND REPLACED LONG SPLICE FITTING AT STA 680 L2R IAW SRM 51-1-20D. 2L74 4F RT4A25 20050804000392005080400039EA 2005 8 4 SWIA200515323 120050727A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCONNECTED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07954SW 7815 FLOOR LEVEL EMERGENCY LIGHTING NEXT TO SEAT ROWS 6, 7, AND 8 INOP. CLEANED AND DRIED OUT MOISTURE, RECONNECTED EMERGENCY LIGHT STRIPS. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050804000402005080400040SO 2005 8 4 SWIA200515324 120050728A2797 SOCKET EMB 120 EMB120ER 3260203SO FLAP ACT CONNECTDAMAGED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07215SW 120281 "CONTROL FAULT" IN CRUISE PORTION OF FLIGHT OF BOTH OUTBOARD AND NACELLE FLAPS. REPLACED ALL SOCKETS IN ALL 6 FLAP ACTUATOR CONNECTORS. OPERATIONAL CHECK GOOD. REF EMB 120 WDM 20-21-00 AND 20-50-00 AND MM 27-50-00. 2L72 4T RTA31SO 20050804000412005080400041SO 2005 8 4 SWIA200515325 120050730A27513471001001 ANNUNCIATOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER FN FLT CONT AFFECTED FALSE WARNING CLCLIMB 1 NM07214SW116637872 120280 ON CLIMB-OUT, GOT A FLAP DISAGREEMENT INDICATION. REPLACED FLAP ANNUNCIATOR PANEL IAW EMB 120 MM 27-50-00. OPERATIONAL CHECK GOOD, PN ON 306900-1017; PN OFF 347100-1001; SN ON 0015; SN OFF 0089. 2L72 4T RTA31SO 20050804000422005080400042SO 2005 8 4 SWIA200515326 120050730A27523430001001 ACTUATOR EMB 120 EMB120ER 3260203SO NACELLE FLAP MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07270YV9323 9323 120270 FLAP DISAGREEMENT ON INBOARD PAIR ON FLAP RETRACTION. REPLACED LT INBD FLAP ACTUATOR IAW AMM 27-50-00. 2L72 4T RTA31SO 20050804000442005080400044SO 2005 8 4 SWIA200515328 120050731A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07188SW9032 9032 120039 ROW 6, LEFT SIDE EXIT ROW LIGHT OUT. REPLACED CENTER ELBP FOR ROW 6, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050804000452005080400045EA 2005 8 4 SWIA200515329 120050729A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07438SW 7574 CEILING MOUNT EMERGENCY LIGHT NEXT TO LAV INOP. RELAMPED AFT MOST CEILING LIGHT. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050804000492005080400049SO 2005 8 4 SWIA200515333 120050730A2611 SMOKE DETECTOR EMB 120 EMB120ER 3260203SO LAVATORY ACTIVATED A SWIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM07296SW 120325 ON TAKEOFF FROM LAS VEGAS, THE LAV SMOKE ALARM WENT OFF. SMOKE WAS NOT VISIBLE. RAN BOTH PACKS OFF APU FOR 34 MINS AND NO SIGN OF SMOKE/SMOKE ODOR WAS PRESENT. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050804000522005080400052EA 2005 8 4 SWIA200515334 120050729A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07463SW 7820 2ND AFT OVHD EMERGENCY LIGHT INOP. RELAMPED 2ND AFT OVHD EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050804000532005080400053NM 2005 8 4 SWAA052146 120050723A53146545866 KEELBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON FUSELAGE KEELBEAM, RT SIDE, BS 727A. REPAIRED KEELBEAM PER SWA EA. 2L72 4F RTA16WE 20050804000552005080400055NM 2005 8 4 SWAA052148 120050724A53226546569 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 967, BETWEEN STR 27L AND STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050804000562005080400056NM 2005 8 4 SWAA052149 120050724A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 807, STR 26L. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050804000572005080400057NM 2005 8 4 SWAA052150 120050724A53206551698 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 907, STR 24L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20050804000582005080400058NM 2005 8 4 SWAA052151 120050724A53306545777 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR UPPER HINGE CUTOUT, FWD UPPER CORNER. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050804000592005080400059NM 2005 8 4 SWAA052152 120050724A3350101331 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 LT OVERWING EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20050804000612005080400061NM 2005 8 4 SWAA052154 120050724A3350D71702001 BATTERY BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29368SW 26579 DURING SCHEDULED RON CHECK, FOUND RT AFT CABIN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20050804000622005080400062NM 2005 8 4 SWAA052155 120050724A335010107451 SIGN BOEING737 7377H4 1384404NM L2 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29444WN 29839 L2 DOOR EMERGENCY EXIT SIGN CRACKED. REMOVED AND REPLACED SIGN PER MM. 2L72 4F RTA16WE 20050804000632005080400063NM 2005 8 4 SWAA052156 120050723A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29474WN 33861 FWD CABIN EEPLS TRACK LOOSE AT FWD END. REMOVED AND REPLACED EEPLS TRACK SECTION PER MM. 2L72 4F RTA16WE 20050804000842005080400084EU 2005 8 4 AWXA200500904 120050712A5320D53480048 SILL AIRBUS320 A320231 3930325EU ZONE 200 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28627AW 66 SAL - DURING C4 CHECK DISCOVERED SILL SHAPE LOCATED AT FS 68-8" ON CABIN FLOOR STRUCTURE. MAINTENANCE REMOVED SILL SHAPE LOCATED AT FR 68-8" ON CABIN FLOOR STRUCTURE IAW AIRBUS 320 SRM 51-42-11. INSTALLED NEW FASTENERS AND SILL SHAPE AT FS 68-8", CABIN FLOOR STRUCTURE, IAW AIRBUS 320 SRM 51-42-11. 2L72 4F RTA28NM 20050804000852005080400085EU 2005 8 4 AWXA200500905 120050714A5313D53480047200 STRINGER AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28627AW 66 SAL - DURING C4 CHECK DISCOVERED CORROSION AT STRINGER 31R, FS 65, INTERNAL STRUCTURE UNDER FLOOR COMPARTMENT. MAINTENANCE REMOVED CORROSION AND NO ALLOWABLE DAMAGE WAS FOUND IN SRM. MAINTENANCE REMOVED STRINGER 31R FROM FS 64 TO FS 67 IAW AIRBUS SRM 51-42-11. INSTALLED NEW STRINGER AND FASTENERS FROM FS 64 TO FS 67 IAW AIRBUS 320 SRM 51-42-11. 2L72 4F RTA28NM 20050804000872005080400087SO 2005 8 4 RAIA00507022 120050729A324021582 BRAKE ASSY EMB 145 EMB145 3260210SO MLG MALFUNCTIONED A RAIAD RETURN TO BLOCK M OVER TEMP TXTAXI/GRND HDL 1 CE03806HK12799256 145112 FLT NR 3533- BOS - BRAKE OVERTEMP NR 1 TIRE FLAT. MAINTENANCE REMOVED AND REPLACED THE NR 1 BRAKE ASSY AND NR 1 AND NR 2 TIRES. OPS CHECKED GOOD. 2L72 4F RTT00011AT 20050804000882005080400088SO 2005 8 4 RAIA00507025 120050802A3150 RELAY EMB 145 EMB145 3260210SO WARNING SYS MALFUNCTIONED A RAIAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 CE03804HK 145082 FLT NR 3622- PIT- TAKEOFF CONFIGURATION WARNING WITH THRUST LEVERS ADVANCED. MAINTENANCE RESEATED RELAY NR K0212. PERFORMED HIGH SPEED TAXI. OPS CHECKED GOOD. 2L72 4F RTT00011AT 20050804000902005080400090SO 2005 8 4 RAIA00507024 120050730A325012302328403 CONTROL HANDLE EMB 145 EMB145LR 3260212SO NLG STEERING INOPERATIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03833HK12343 145240 FLT NR 8018 - STL- WHILE MAKING LEFT TURN, STEERING INOP MESSAGE DISPLAYED ON THE EICAS. MAINTENANCE REMOVED AND REPLACED THE STEERING CONTROL HANDLE. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050804000922005080400092EA 2005 8 4 SWIA200515336 120050731A2751 DETECTOR CNDAIRCL600 CL6002C10 1390015EA TE FLAPS OUT OF RIG A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07716SK 10180 FLAPS FAIL CAUTION MSG. PERFORMED RIGGING OF FLAP SKEW DETECTOR IAW CRJ AMM 27-52-45. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050804000932005080400093EA 2005 8 4 SWIA200515337 120050728A5210 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR OUT OF ADJUST A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07720SW 7297 MAIN CABIN DOOR HARD TO OPEN. ADJUSTED PAX DOOR INNER LEVER TO OUTER HANDLE MECHANISM IAW MM 52-11-0. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050804000952005080400095EA 2005 8 4 SWIA200515339 120050724A2720 PEDAL CNDAIRCL600 CL6002B19 1900309EA RUDDER BLOCKED A SWIAO OTHER F FLT CONT AFFECTED LDLANDING 1 NM07431SW 7536 RUDDER ON LANDING JAMMED ON RIGHT SIDE 1/4 TRAVEL ONLY. FOUND CAMLOCK ON RT SIDE OF CENTER CONSOLE OUT AND INHIBITING RUDDER PEDAL DEFLECTION. SECURED CAMLOCK AND RAN RUDDER PEDALS IN BOTH DIRECTIONS AT FULL DEFLECTION WITH NO DEFECTS NOTED. 2L72 4F RTA21EA 20050804000962005080400096EA 2005 8 4 SWIA200515340 120050727A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLIGHT SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07426SW5839 5839 7468 SPOILERON FAULT STATUS MESSAGE ON GROUND. REPLACED RT SPOILERON IB PCU IAW CRJ MM 27-62-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050804000982005080400098EA 2005 8 4 SWIA200515342 120050724A27515913164 DETECTOR CNDAIRCL600 CL6002C10 1390015EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07709SK2594 2594 10159 FLAPS HALF SPEED STATUS MESSAGE. REPLACED SKEW DETECTOR IAW AMM 27-52-45. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050804000992005080400099EA 2005 8 4 SWIA200515343 120050725A2760C13045BA03 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07709SK1217 1217 10159 SPLR/STAB FAULT STATUS MSG. REPLACED NR 2 SSCU IAW CRJ MM 27-61-00. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050804001012005080400101EA 2005 8 4 SWIA200515345 120050725A2781 SENSOR CNDAIRCL600 CL6002C10 1390015EA SLATS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07706SK 10149 'SLAT FAULT' STATUS MESSAGE. REPLACED RIGHT WING INBOARD SKEW DISCONNECT SENSOR IAW MM 27-81-39. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050804001022005080400102EA 2005 8 4 SWIA200515346 120050725A27604916406 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAD RETURN TO BLOCK FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07441SW 7602 RIGHT SPOILERON STATUS MESSAGE ON TAXI OUT. REPLACED NR 1 AND NR 2 SECU'S. OPERATIONAL CHECKS GOOD IAW 27-61-05, PN OFF 49-164-06; SN OFF 01786, SN OFF 01544. 2L72 4F RTA21EA 20050804001052005080400105SO 2005 8 4 SWIA200515349 120050717A215022045404 ACM EMB 120 EMB120ER 3260203SO ACM BAY SMOKE A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM07583SW4242 4242 120351 "AFTER SHUT DOWN, POSITIONED PACK FROM LOW TO NORM, OVERWHELMING SMELL OF SMOKE IN COCKPIT. REMOVED AND REPLACED ACM (TURBINE). OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050804001062005080400106SO 2005 8 4 SWIA200515350 120050731A3350 BULB EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07224SW 120294 ONE WHITE FLOOR EMERG LIGHT INOP. REPLACED LIGHT BULB TO WHITE EMERG ROW LIGHT STRIPE BY ROW 7. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050804001082005080400108EA 2005 8 4 SWIA200515352 120050722A274170609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07934SW 7722 BOTH STAB TRIM CHANNELS WON'T ENGAGE. REPLACED USING HSTCU. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050804001092005080400109EA 2005 8 4 SWIA200515353 120050720A5210 STOP CNDAIRCL600 CL6002C10 1390015EA PAX DOOR OUT OF ADJUST A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07706SK 10149 FORWARD DOOR STICKS DURING CLOSING AND IS HARD TO OPEN. ADJUSTED FORWARD UPPER MCD STOP PIN. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050804001132005080400113EU 2005 8 4 UPS05145032 120050729A3350 LIGHT AIRBUSA300 A300F4622R 3930360EU LAVATORY INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01160UP 0005 LAV EMERG EXIT LIGHT INOP. RELAMPED. 2L72 4F RTA35EU 20050804001142005080400114NM 2005 8 4 UPS05445008 120050723A531065B38600153 STRINGER CLIP BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 BS 1780 S-12R STRINGER TIE CLIP FOUND CRACKED, CRACK LENGTH .750. TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050804001162005080400116NM 2005 8 4 UPS05445010 120050725A5311 FRAME BOEING747 747121 1384871NM BLG W/W CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE: C, LT BLG WW LT STA 1416 FRAME FOUND CRACKED IN BTN STR 29 AND STR 30, CRACK LENGTH 0.25". LT BLG W/W LT BS 1416 BETWEEN STR 29 AND 30 FRAME REPAIRED AS PER SRM 53-10-04 FIG 4. 2L74 4F A20WE 20050804001172005080400117NM 2005 8 4 UPS05445011 120050725A5315 FLOORBEAM BOEING747 747121 1384871NM FUSLAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 BS 360 FLOORBEAM FWD FLANGE 6EA MOUNTING HOLES CRACK. BS 360 FLOORBEAM UPPER CHORD HORIZ FWD FLANGE AT RBL 29 - 60 AREA REPAIRED AS PER UPS EO NR B747-5320-12407 APPENDIX 'D' PLAN 'C'. 2L74 4F A20WE 20050804001192005080400119NM 2005 8 4 UPS05445017 120050725A5315 FLOORBEAM BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 BS 400 RBL 3 TO 24 FLOORBEAM FOUND CORRODED AS MARKED. CORROSION BLEND OUT 0.043" BY 2" BY 2" EXCEED SRM 53-10-01 FIG 1 LIMITS. BS 400 LBL 7" TO RBL 35" FLOORBEAM REPAIRED AS PER SRM 53-10-07 FIG 10. 2L74 4F A20WE 20050804001232005080400123NM 2005 8 4 UPS05445021 120050723A5313 STRINGER BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 BS 1940-1960 S1R STRINGER END FOUND CRACKED, CRACK LENGTH 1.125. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4 JUST AT STR 1R BETWEEN BS 1930 & 1960. 2L74 4F A20WE 20050802001142005080200114NM 2005 8 2 CALA0500248 120050731A3260MS250112 SWITCH BOEING737 737924 13848A1NM MLG OUT OF ADJUST A CALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW2738403 30120 THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM EWR. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED FIM TASK 32-30-00-810-815 AND FOUND THE MANUAL EXTENSION SWITCH(S1060) OUT OF ADJUSTMENT. THE SWITCH WAS ADJUSTED AND A REPAIR CONFIRMATION RETRACT TEST WAS PERFORMED WITH NO DEFECTS NOTED. 2L74 4F RTA16WE 20050802001182005080200118NM 2005 8 2 200510 120050730A7712 INDICATOR DHAV DHC8 DHC8103 1386005NM NR 2 ENG TORQUE STUCK A KPVAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 WP13805WP 353 ON TAKEOFF, NR 2 TQ GAUGE STUCK AT 68 PERCENT TQ INDICATION ON BOTH ANALOG AND DIGITAL INDICATIONS. GAUGE STUCK EVEN AFTER ENGINE SHUT DOWN. PERFORMED POWER RUN AND OPS CHECK OF TORQUE INDICATION SYSTEM IAW DHC PSM 1-8-2, 77-10-00 PG 2-3. OPS CHECK GOOD. 2H72 4T RTA13NM 20050802001202005080200120SO 2005 8 2 CHQA200500134 120050728A33507287580509 LIGHT EMB 145 EMB145MP 3260216SO CABIN INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11976RP 145322 AFT MOST EMERGENCY LIGHT FLOOR STRIP INOP. REMOVED AND REPLACED AFT MOST EMERGENCY LIGHT FLOOR STRIP IAW EMB 145 AMM 33-50-08-4. OPS CHECK GOOD. 2L72 4F RTT00011AT 20050802001262005080200126NM 2005 8 2 USAA050853 120050708A5312 PRESSURE PANEL BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19441US40664 24812 CLT - FOUND PRESSURE DECK CRACKED .750 INCH, STATION 664 LBL 32.5. REMOVED DAMAGED DAMAGED AREA, INSTALLED REPAIR IAW SRM 53-60-04. (M) 2L72 4F RTA16WE 20050802001302005080200130NM 2005 8 2 DHL2005788008 120050802A3260 BULB BOEING727 727214 138407RNM MLG INDICATOR LOOSE A DHLAO OTHER P NO WARNING INDICATION NRNOT REPORTED 1 SO01788AT 21958 RIGHT GEAR "RED" LIGHT ON FWD PANEL DOESN'T ILLUMINATE ON GEAR EXTENSION. RE-SEATED RT MLG RED LIGHT IN SOCKET. OPS CHECK GOOD IAW MM 32-61-01. 2L73 4F A3WE 20050802001312005080200131NM 2005 8 2 DHL2005788009 120050802A3260 SWITCH BOEING727 727214 138407RNM NLG DOOR OUT OF ADJUST A DHLAO OTHER N FALSE WARNING CRCRUISE 1 SO01788AT 21958 RED "DOORS" LIGHT ON FWD PANEL AND "NOSE GEAR DOOR" AMBER LIGHT ON S'OFFICER'S PANEL FLICKERS DURING TURBULANCE. ADJUSTED NOSE GEAR DOOR LIGHTS SWITCHES, OPS CKECK GOOD IAW MM 32-62-00. 2L73 4F A3WE 20050802001372005080200137NM 2005 8 2 NACA20050018 120050802A7331 INDICATION SYS BOEING727 72722C 138400FNM PWA JT8 JT8D7B 52053NE FUEL FLOW INOPERATIVE A NACAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 AL03792A 19195 654518 NR 2 ENGINE FUEL FLOW INDICATION INOPERATIVE. ENGINE SLOW TO ACCELERATE. FUEL FLOW INDICATION DEFERRED IAW MEL 73-7. PERFORMED ACCELERATION CHECK, FOUND TO BE WITHIN LIMITATIONS. 2L73 4F4 F A3WE E2EA 20050802001432005080200143SO 2005 8 2 SWIA200515313 120050716A3350 BULB EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT INOPERATIVE A SWIAK NONE L NO TEST TXTAXI/GRND HDL 1 NM07227SW 120304 FLOOR LEVEL EMERGENCY LIGHT AT 10A INOP. REPLACED LIGHT BULB FOR FLOOR LEVEL EMERGENCY LIGHT AT ROW 10A. OPS CHECK GOOD. 2L72 4T RTA31SO 20050802001442005080200144NM 2005 8 2 USAA050852 120050708A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19505AU54520 23380 CLT - FOUND SKIN CRACKED 1.75 INCH, FS 745 AT STRINGER 24L. INSTALLED REPAIRED DOUBLER IAW SRM 53-00-01 DETAIL XI. (M) 2L72 4F RTA16WE 20050802001452005080200145NM 2005 8 2 USAA050850 120050707A5321 SPLICE BOEING737 7374B7 1384702NM FLOOR PANEL CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19441US40664 24812 CLT - FOUND SPLICE STRAP CORRODED .5 INCH, AFT CARGO FLOOR PANEL SPLICE STRAP. FABRICATED NEW STRAP AND INSTALLED IAW SRM 51-10-02. (M) 2L72 4F RTA16WE 20050802001462005080200146NM 2005 8 2 USAA050851 120050707A5311 FRAME BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19441US 24812 CLT - FOUND FRAME CRACKED .5 INCH, CENTER AISLE FRAME BETWEEN STATION 380 AND 400. FABRICATED AND INSTALLED NEW PART IAW SRM 51-10-02. (M) 2L72 4F RTA16WE 20050803000062005080300006EA 2005 8 3 ASOA05596 120050712A79301153P0012 PRESSURE SWITCH CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT ENGINE OIL MALFUNCTIONED A ASOAO OTHER J WARNING INDICATION CLCLIMB 1 SO27871AS 7537 873409 DURING CLIMB OUT, AT APPROXIMATELY 16,000 FEET, THE CREW RECEIVED A (R ENG OIL PRESS) MESSAGE. QRH WAS COMPLIED WITH AND POWER WAS BROUGHT BACK TO IDLE ON THE RT ENGINE. OIL PRESSURE STABILIZED AND THE AC CONTINUED ON. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE RT ENGINE OIL PRESSURE SWITCH AND TRANSDUCER. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050803000182005080300018NM 2005 8 3 2005UALA00698 120050726A5754 SKIN BOEING777 777222 1385219NM PWA PW4077PW4077 NE NR 11 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29768UA41484 26919 NR 11 SLAT OUTBD EDGE UPPER AND LOWER SURFACES DELAMINATED. REPAIRED AND NDT INSPECTED IAW 777 AMM 57-43-99-803. INITIAL INSP REQUIRED AT 50 CYCLES AND EVERY 500 CYCLES THEREAFTER UNTIL A PERMANENT REPAIR IS ACCOMPLISHED AT NEXT HMV. THIS LOCALIZED DELAM IS SYSTEMIC TO THE 777 FLEET ON ALL OF THE OUTBOARD SLATS. BOEING HAS COMMITTED TO A RE-DESIGN OF THE TRAILING EDGE WEDGES ON THESE SLATS WHICH ARE PLANNED TO BE READY FOR USE DURING THE LAST QUARTER OF 2006. THE REDESIGNED SLATS WILL ELIMINATE THIS DELAMINATION PROBLEM BY INCORPORATING A MACHINED ONE-PIECE RIB/SPAR DESIGN. 2L72 4F4 FRTT0001SE E46NE 20050803000202005080300020NM 2005 8 3 2005UALA00700 120050722A33509F19948501 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE R1 DOOR INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29118UA 28811 DOOR 1 RIGHT SLIDE EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY. 2L74 4F4 FRTA20WE E24NE 20050803000212005080300021NM 2005 8 3 2005UALA00701 120050722A3350362624 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE SEAT 8B BURNED OUT A UALAK NONE L NO TEST ININSP/MAINT 1 WP29118UA 28811 SEAT 8B AFT EMERGENCY LAMP INOP. REPLACED LAMP. 2L74 4F4 FRTA20WE E24NE 20050803000372005080300037NM 2005 8 3 RYNA200500025 120050624A5320 SHEAR PLATE BOEING757 757236 1384971NM FUSELAGE CORRODED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07526NA 24794 SHEAR SKIN HAS CORRISION AT BS 1720 TO 1681 RBL 50 TO LBL 50 AFT CABIN. CLEANED CORROSION BELOW SHEAR PLATE AND FLOORBEAM IAW B757 SRM 51-40-2 (LIGHT CORRISION). ALODINED AND PRIMED AREA AND REINSTALLED FASTENERS. 2L72 4F RTA2NM 20050803000412005080300041NM 2005 8 3 CALA0500251 120050731A5753654642943 FLAP TRACK BOEING737 737524 1384721NM NR 1 FLAP CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2719621 27334 INSPECTION FOUND THE NR 1 FLAP TRACK CORRODED IN THE AFT UPPER HOLE WHERE THE TRANSMISSION IS ATTACHED. THE AREA WAS REWORKED IAW CMM 57-53-15. 2L72 4F RTA16WE 20050803000432005080300043NM 2005 8 3 2005UALA00695 120050723A5754 SKIN BOEING777 777222 1385219NM PWA PW4077PW4077 NE NR 9 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29768UA 26919 NR 9 SLAT OB EDGE DELAMINATED ON UPPER AND LOWER SURFACE. REPAIRED AND NDT INSPECTED IAW 777 AMM 57-43-99-803. INITIAL INSP REQUIRED AT 50 CYCLES AND EVERY 500 CYCLES THEREAFTER UNTIL A PERMANENT REPAIR IS ACCOMPLISHED AT NEXT HMV. THIS LOCALIZED DELAM IS SYSTEMIC TO THE 777 FLEET ON ALL OF THE OUTBOARD SLATS. BOEING HAS COMMITTED TO A RE-DESIGN OF THE TRAILING EDGE WEDGES ON THESE SLATS WHICH ARE PLANNED TO BE READY FOR USE DURING THE LAST QUARTER OF 2006. THE REDESIGNED SLATS WILL ELIMINATE THIS DELAMINATION PROBLEM BY INCORPORATING A MACHINED ONE-PIECE RIB/SPAR DESIGN. 2L72 4F4 FRTT0001SE E46NE 20050803000532005080300053NM 2005 8 3 2005UALA00722 120050727A5541 RIB BOEING777 777222 1385219NM PWA PW4077PW4077 NE RUDDER LIGHTNING STRIKEA UALAK NONE O OTHER ININSP/MAINT 1 WP29780UA 26944 ELECTRICAL DISCHARGE ON RT OUTBD ANCHOR NUT HOLE ON RIB FITTING ASSY STA 522.702. RUDDER RIB FITTING WAS DAMAGED FROM A LIGHTNING STRIKE AND WAS REPLACED PER BAC DWG 175W5109, SRM 51-40-02. 2L72 4F4 FRTT0001SE E46NE 20050803000552005080300055NM 2005 8 3 2005UALA00724 120050728A33501317 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE ROW 14 BURNED OUT A UALAK NONE L NO TEST ININSP/MAINT 1 WP29182UA 25279 EMERGENCY LIGHTS INOP AT ROW 14, ROW 17 CEILING, AND DR 3L CEILING. REPLACED LAMP. 2L74 4F4 FRTA20WE E24NE 20050803000612005080300061NE 2005 8 3 2005UALA00730 220050728A7297 PIN AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE CONNECTOR BENT A UALAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 WP29843UA 1573 V11052 CREW REPORTED R ENGINE OVERTEMP. THE 2.5 BLEED VALVE MASTER ACTUATOR WAS FOUND TO HAVE A BENT CONNECTOR PIN. THIS DEFECT LEAD TO THE 2.5 BLEED VALVE BEING INTERMITTENTLY SET TO THE FAIL-SAFE (OPEN) POSITION LEADING TO AN EGT OVER-TEMP. 2L72 4F4 FRTA28NM E40NE 20050803000622005080300062EU 2005 8 3 2005UALA00731 120050727A2913 PUMP AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE GREEN HYD SYS LEAKING A UALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP29464UA 1290 LOST GREEN HYDRAULIC SYSTEM. CREW SECURED PUMP AND PTU. 2L72 4F4 FRTA28NM E40NE 20050803000642005080300064 2005 8 3 2005UALA00733 420050729A2565 BOTTLE AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE ESCAPE SLIDE LOW A UALAK NONE O OTHER ININSP/MAINT 1 WP29812UA 850 ESCAPE SLIDE HAS LOW BOTTLE PRESSURE. SLIDES BEING REMOVED DUE TO LOW BOTTLE PRESSURE IS NOT TOTALLY AN UNCOMMON EVENT. THE OPERATING ENVIRONMENT OF SLIDES (VIBRATION, DOOR OPENING/CLOSING, CARTS IMPACTING DOORS, TEMPERATURE & PRESSURE CHANGES) ARE AMONG THE FACTORS THAT COULD RESULT IN BOTTLE LEAKS. SEALS HOWEVER SHOULD AS MUCH AS POSSIBLE KEEP THE PRESSURE DURING THE 36-MONTH SERVICE LIFE OF THE SLIDE ASSEMBLY. ANY BOTTLE THAT IS FOUND LEAKING IS REQUALIFIED IN THE SHOP AS REQUIRED BY THE 49CFR. DURING BOTTLE REQUALIFICATION, ALL SEALS ARE REPLACED WITH NEW ONES. SINCE SLIDE BOTTLES ARE NOT 100% RELIABLE, THEY ARE CHECKED BEFORE EACH FLIGHT TO ENSURE THAT THE PRESSURE IS NORMAL. 2L72 4F4 FRTA28NM E40NE 20050803000662005080300066EU 2005 8 3 AWXA200500896 120050801A3397 WIRE AIRBUS320 A320231 3930325EU EMERGENCY LIGHT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 LAS - EEL - DURING 8 DAY CHECK DISCOVERED ROW 17 SEAT MOUNTED EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AT ROW 17. OPERATIONAL CHECKS WERE GOOD IAW TASK CARD F1C33301. 2L72 4F RTA28NM 20050803000712005080300071SO 2005 8 3 LR7A05099 120050801A215020343041 COOLING TURBINE LKHEED382 382G 526414USO AIR CON SYS FAILED A LR7AH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 AL03403LC 4590 FLIGHT CREW REPORTED, FLIGHT STATION AIR CONDITIONING SYSTEM HOWLING AND SMELL BAD. SHUT DOWN AIR CONDITIONING SYSTEM. FOUND FLIGHT STATION COOLING TURBINE FAILED. REPLACED COOLING TURBINE IAW MM SMP 581 21-50. OPS AND LEAK CK NORMAL. LP 18732, ITEM 1. 2H74 4T A1SO 20050803000732005080300073NM 2005 8 3 USAA050848 120050707A533065C80736354 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19505AU54520 23380 CLT - FOUND SKIN CRACKED 1.3 INCH, MAIN ENTRY LOWER HINGE CUTOUT AT LOWER RADIUS. INSTALLED DOUBLER IAW TYPICAL REPAIR NR 52-10-12. (M) 2L72 4F RTA16WE 20050803000742005080300074NM 2005 8 3 USAA050849 120050707A53306545871523 SKIN BOEING737 7373B7 1384580NM CRACKED CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19505AU54520 23380 CLT - FOUND SKIN CRACKED .25 INCH, FORWARD SERVICE DOOR, LOWER HINGE CUTOUT ON THE SKIN. INSTALLED DOUBLER IAW EA 96719. (M) 2L72 4F RTA16WE 20050803000862005080300086EU 2005 8 3 MALA050626 120050731A5410 STRUCTURE SAAB SF340 340B 7860101EU RT NACELLE CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15452XJ 340B452 RT LOWER NACELLE DESK IS CHAFED AND HAS BEEN REPAIRED IAW MESABA EO 54095. REF EAMS WORK ORDER 212637 TASK 4507. 2L72 4T RTA52EU 20050803000902005080300090NM 2005 8 3 P5CA0501383 120050724A528065B1091739 DOOR BOEING747 747283B 1384867NM MLG MISSING A P5CAK NONE D INFLIGHT SEPARATION TXTAXI/GRND HDL 1 EA15921FT 21575 ON POSTFLIGHT WALKAROUND, FOUND LEFT BODY GEAR O/B SHOCK STRUT DOOR MISSING. REPLACED DOOR PER MM 32-14-06. 2L74 4F A20WE 20050803000922005080300092NM 2005 8 3 SWAA052130 120050720A53226546594 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29609SW 27929 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME SHEAR TIE CORRODED AT BS 727E, LBL 5 TO RBL 10. REMOVED AND REPLACED SHEAR TIE SECTION PER SRM. 2L72 4F RTA16WE 20050803000952005080300095NM 2005 8 3 SWAA052116 120050720A32606544810 UPLOCK SENSOR BOEING737 7373H4 1384600NM RT MLG FAULTY A SWAAO OTHER J WARNING INDICATION CLCLIMB 1 SW29604SW 27955 RT MLG UNSAFE LIGHT INDICATION, RECYCLED GEARS AND LIGHT EXTINGUISHED. REMOVED AND REPLACED RT MLG UPLOCK SENSOR PER MM. 2L72 4F RTA16WE 20050803001082005080300108NM 2005 8 3 SWAA052255 120050728A3350207377 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29450WN 32470 CABIN EEPLS LENS LOOSE AT FWD END. SECURED LENS PER MM. 2L72 4F RTA16WE 20050803001092005080300109NM 2005 8 3 AT0500024 120050723A3350 BATTERY PACK BOEING717 717200 1383700NM EMERGENCY LIGHT INOPERATIVE A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15948AT 55011 EMERGENCY LIGHTS IN AFT ACCESSORY COMPT INOPERATIVE. REPLACED BATTERY PACK IN OVERHEAD FWD OF AFT ACCESSORY COMPT DOOR REF 33-00. NOW CKS OK. 2L72 4F TRA6WE 20050803001102005080300110NM 2005 8 3 SWAA052243 120050728A53306545766 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 485, STR 16L. REPAIRED SKIN PER SWA EA AND SRM. 2L72 4F RTA16WE 20050803001182005080300118NM 2005 8 3 SWAA052252 120050729A53226546529 SHEAR TIE BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29317WN 24068 DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 500D, STR 12R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050803001232005080300123NM 2005 8 3 SWAA052258 120050729A3350MS155721 LAMP BOEING737 7375H4 138449DNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29519SW 25318 DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EXTERNAL EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050803001272005080300127NM 2005 8 3 SWAA052262 120050729A53306545774 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 735, STR 25R. REPAIRED SKIN PER SWA EA AND SRM. 2L72 4F RTA16WE 20050803001322005080300132NM 2005 8 3 SWAA052267 120050729A53116545808 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29691WN 23781 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 303, L1 DOOR LOWER STOP FITTING CUTOUT. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050803001352005080300135EU 2005 8 3 XN0A1250 120050802A2134 WARNING LIGHT AIRBUS300 A300B4203 3930306EU CABIN AIR MALFUNCTIONED A XN0AO OTHER O OTHER TXTAXI/GRND HDL 1 GL23224KW 073 ON TAXI, GROUND AUX VALVE FAULT LIGHT REMAINED ON. DMI GROUND AUX LIGHT REF MEL 21-34-05 AND DMI 5606 CAT "C". PLACARDS INSTALLED. 2L72 4F RTA35EU 20050803001432005080300143NM 2005 8 3 SWAA052220 120050728A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 330, STR 11R. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20050803001482005080300148NM 2005 8 3 SWAA052225 120050728A53306545775 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE CRACKS AT BS 792 AND BS 812, STR 18L. REPAIRED SKIN PER SWA EA AND SRM. 2L72 4F RTA16WE 20050803001492005080300149EU 2005 8 3 TRBA2005049 120050713A3213D61384 BOLT AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE STRUT ASSY BROKEN A TRBAK NONE O OTHER ININSP/MAINT 1 SO29377AT 377 REF: (SDR2005049) WHILE PERFORMING A WALK-AROUND INSPECTION, FOUND THE LT MAIN CYLINDER OUT OF PLACE. REPLACED LT MAIN GEAR SHOCK ABSORBER BOLT. (K) 2H72 4T4 TRTA53EU E20NE 20050803001772005080300177NM 2005 8 3 SWAA052164 120050723A5753113A270016 SKIN BOEING737 7377H4 1384404NM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29767SW 29807 DURING SCHEDULED RON CHECK, FOUND RT WING INBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM. 2L72 4F RTA16WE 20050804000462005080400046EA 2005 8 4 SWIA200515330 120050728A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07432SW 7548 1 BULB IN FIRST POD WILL NOT ILLUM IN EMERGENCY EXIT SIGN. REPLACED EMERGENCY LIGHT BULB AT NR 1 CEILING POSITION. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050804000472005080400047EA 2005 8 4 SWIA200515331 120050728A2751855D10011 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07920SW7458 7458 7660 FLAPS FAIL MESSAGE WILL NOT RESET. REPLACED LEFT BPSU AND RIGGED PER MM 27-51-10. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050804000482005080400048EA 2005 8 4 SWIA200515332 120050726A274170609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07909SW4668 4668 7558 STATUS MESSAGE STAB CH2 INOP. REPLACED HSTCU IAW CRJ 200 MM 27-41-01 AND 27-41-00. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050804000892005080400089SO 2005 8 4 RAIA00507023 120050730A801035059106 STARTER EMB 145 EMB145 3260210SO NR 2 ATS FAILED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03803HK115373571 145077 FLT NR 3503- PIT- ENGINE 2 WOULD NOT SPIN WITH APU OR CROSSBLEED. MAINTENANCE REMOVED AND REPLACED THE NR 2 AIR TURBINE STARTER. OPS CHECKED GOOD. 2L72 4F RTT00011AT 20050804000912005080400091EA 2005 8 4 SWIA200515335 120050730A2752 SPRING CNDAIRCL600 CL6002C10 1390015EA FLAP ACTUATOR MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07719SK 10188 "FLAPS FAIL" MESSAGES. RESET FLAP ACTUATOR (RT) SPRING TYPE INDICATOR IAW CRJ MM 27-52-09-610-802-A01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050804001102005080400110EA 2005 8 4 SWIA200515354 120050724A274170609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07597SW2082 2082 7293 HORIZONTAL TRIM AND MACH TRIM KICKED OFF IN FLIGHT REPEATEDLY. REMOVED AND REPLACED HSTCU. OPERATIONAL CHECK GOOD IAW CRJ MM 27-41-01. 2L72 4F RTA21EA 20050804001122005080400112EA 2005 8 4 SWIA200515356 120050728A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07418SW 7446 SECOND OVERHEAD EMERGENCY LIGHT INOP. REPLACED LAMP. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050805000192005080500019EA 2005 8 5 COMA0560413 120050727A3350BF10011101 LIGHT CNDAIRCL600 CL6002B19 1900309EA ROW 8 MALFUNCTIONED A COMAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01995CA 7229 FLIGHT 4954 - CABIN EMERGENCY LIGHTS FLICKER OFF AND ON. REPLACED LIGHT ASSEMBLY AT ROW 8. 2L72 4F RTA21EA 20050805000202005080500020EA 2005 8 5 COMA0560414 120050727A21331037707 OUTFLOW VALVE CNDAIRCL600 CL6002B19 1900309EA CABIN PRESSURE MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01941CA26498 7050 FLIGHT 5553 - CABIN ALTITUDE CAUTION MESSAGE. REPLACED THE PRIMARY OUTFLOW VALVE. 2L72 4F RTA21EA 20050805000212005080500021SO 2005 8 5 C2XA05RI016 120050728A213122250N0300301 CONTROLLER EMB 145 EMB145LR 3260212SO CABIN PRESSURE FAILED A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW27149508925 145061 FLIGHT 2442 EWR TO GSP: DURING CLIMBING OUT OF EWR, CREW REPORTED PRESSURIZATION PROBLEMS. FLIGHT WAS DIVERTED TO RIC. RIC MAINTENANCE REMOVED AND REPLACED DIGITAL PRESSURIZATION CONTROLLER. MAINTENANCE PERFORMED OPERATIONAL CHECK SUCCESFULLY. ACFT WAS THEN APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20050805000232005080500023NM 2005 8 5 SWAA052214 120050727A56105893543130 WINDOW BOEING737 7373G7 1384595NM COCKPIT LOOSE A SWAAA UNSCHED LANDING O OTHER CLCLIMB 1 SW29670SW 23784 DIVERSION, LOUD SQUEAL IN COCKPIT COMING FROM R1 WINDOW. RETORQUED COCKPIT R1 WINDOW PER MM. 2L72 4F RTA16WE 20050805000242005080500024NM 2005 8 5 SWAA052215 120050721A53126545409306 PANEL BOEING737 7373Y0 1384671NM LT MLG WW CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED C4 CHECK, FOUND LEFT MLG W/W UPPER FWD CEILING PANEL CRACKED AT BS 664, LBL 39. MX FERRY TO DAL, REPAIRED PANEL PER SWA EA. 2L72 4F RTA16WE 20050805000262005080500026 2005 8 5 SWAA052217 420050725A256563550 SLIDE BOEING737 7377H4 1384404NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29727SW 27859 DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050805000272005080500027NM 2005 8 5 SWAA052218 120050727A2560PH22300L GLOWSTRIP BOEING737 7377H4 1384404NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29730SW 27862 CABIN PHOTOLUMINESCENT STRIP LOOSE AT ROW 8 DEF. SECURED STRIP PER MM. 2L72 4F RTA16WE 20050805000302005080500030NM 2005 8 5 SWAA052176 120050724A335020121 BATTERY PACK BOEING737 7373H4 1384600NM EMERGENCY LIGHT FAILED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29361SW 26572 DURING SCHEDULED RON CHECK, RIGHT AFT CABIN EMERGENCY LIGHTS BATTERY FAILED TEST. REMOVED AND REPLACED RIGHT AFT BATTERY PACK PER MM. 2L72 4F RTA16WE 20050805000312005080500031NM 2005 8 5 SWAA052177 120050724A53306545776 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29514SW 25153 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050805000342005080500034NM 2005 8 5 SWAA052181 120050725A3260806002 UPLOCK SENSOR BOEING737 7373A4 1384585NM RT MLG FAULTY A SWAAO OTHER J WARNING INDICATION CLCLIMB 1 SW29680AA 23505 RIGHT MLG TRANSIT LIGHT ILLUMINATED, CYCLED GEAR HANDLE & LIGHT EXTINGUISHED. REMOVED AND REPLACED RIGHT MLG UPLOCK SENSOR & UPLOCK CARD PER MM. 2L72 4F RTA16WE 20050805000352005080500035 2005 8 5 SWAA052182 420050725A2565D31354433 SLIDE BOEING737 737317 138447PNM R2 DOOR DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 R2 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATING LOW. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20050805000392005080500039SO 2005 8 5 C2XA05SH091 120050801A521014533413401 HANDLE EMB 135 EMB135LR 3260305SO PAX DOOR DETACHED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711526 145410 MAIN CABIN DOOR WILL NOT OPEN FROM INSIDE CABIN. MAINTENANCE INSTALLED MAIN CABIN DOOR INTERNAL HANDLE IAW EMB 135 AMM 52-18-05, OPS CHECK GOOD. AIRCRAFT WAS RETURNED FOR SERVICE. 2L72 4F RTT00011AT 20050805000402005080500040SO 2005 8 5 C2XA05BT054 120050802A2120 ODOR EMB 145 EMB145LR 3260212SO COCKPIT DETECTED A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2713975 145163 CREW REPORTED, ODOR OF BURNING PLASTIC OCCURRED IN CRUISE, TURNED OFF RECIRCULATING FAN, ODOR WENT AWAY. ODOR ONLY IN COCKPIT. INSPECTED CABIN AND COCKPIT FOR BURNING ODOR. NO UNUSUAL ODOR. PERFORMED OPERATIONAL CHECK OF RECIRCULATION FAN IAW EMB145 MM 21-00-00. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. CREW REPORTED STRONG ODOR IN COCKPIT ON DESCENT, SIMILAR TO THAT AS DISCRIBED IN LAST ENTRY. ODOR COULD ALSO BE DESCRIBED AS AN INTENSE MILDEW. MAINTENANCE PERFORMED ENGINE RUNS IAW EMB MM 71-00-01. ALSO RAN APU AND ALL BLEED SYSTEM IAW EMB145 MM 49-00-00 AND 36-00-00. COULD NOT DUPLICATE ODOR. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20050805000412005080500041SO 2005 8 5 C2XA05SH092 120050803A533014520571001 SKIN EMB 145 EMB145LR 3260212SO FUSELAGE LIGHTNING STRIKEA C2XAK NONE O OTHER ININSP/MAINT 1 SW2711536 145520 SHV - DURING C-CHECK LIGHTNING STRIKE INDICATION AT FR 16 STR 19R. MAINTENANCE REPAIR DAMAGE LIGHTNING STRIKE AT FR 16 STR 19R IAW EC 5330-01486. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2L72 4T RTT00011AT 20050805000422005080500042SO 2005 8 5 C2XA05CL060 120050726A2611FAU751A4 SMOKE DETECTOR EMB 145 EMB145LR 3260212SO LAVATORY INTERMITTENT A C2XAO OTHER N FALSE WARNING CLCLIMB 1 SW2714570 145632 CLE FLIGHT 2469 THE CREW REPORTED A LAV SMOKE WARNING ON CLIMBOUT AFTER SHUTTING DOWN THE APU. NO SMOKE OR FUMES WERE NOTICED AFTER VISUAL INSPECTION. THE SYSTEM WAS RESET AND NO INDICATION WAS NOTICED. MAINTENANCE INSPECTED AND REPLACED THE FORWARD GALLEY SMOKE DETECTOR PANEL. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20050805000432005080500043SO 2005 8 5 C2XA05BT051 120050728A494023080013A STARTER GEN EMB 145 EMB145LR 3260212SO APU FAILED A C2XAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW27139651439 721 145125 CREW REPORTED ON TAXI, APU FAILED AND BURNING ODOR IN THE COCKPIT, AIRCRAFT WAS INSPECTED AND RELEASED IAW MEL 49-00-00 CATEGORY C-CONTROL 057571. IN RIC, REMOVED AND REPLACED APU STARTER/GENERATOR OPS CHECKED GOOD, NO DEFECTS NOTED, MEL ITEM CLEARED AND AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20050805000462005080500046NM 2005 8 5 SWAA052133 120050721A3350101114 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29365SW 26576 FWD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2L72 4F RTA16WE 20050805000482005080500048NM 2005 8 5 SWAA052135 120050721A561058935578 WINDOW BOEING737 7377H4 1384404NM COCKPIT ARCED A SWAAK NONE O OTHER APAPPROACH 1 SW29738CB 27870 R2 COCKPIT WINDOW ARCED. REMOVED AND REPLACED R2 COCKPIT WINDOW ASSY PER MM. 2L72 4F RTA16WE 20050805000502005080500050NM 2005 8 5 SWAA052137 120050721A53116546558 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29609SW 27929 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, BETWEEN STR 8R -STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050805000512005080500051 2005 8 5 SWAA052138 420050721A25656557463 FITTING BOEING737 7373H4 1384600NM GIRT BAR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29609SW 27929 DURING SCHEDULED D-CHECK, FOUND L1 DOOR AFT GIRT BAR FLOOR ATTACH FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM. 2L72 4F RTA16WE 20050805000522005080500052NM 2005 8 5 SWAA052139 120050721A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM CABIN FLOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29609SW 27929 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CRACKED AT BS 947.5, LBL 53, WL 208. REPAIRED FLOORBEAM PER BFG ER. 2L72 4F RTA16WE 20050805000532005080500053NM 2005 8 5 SWAA052140 120050721A53106547978 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29609SW 27929 DURING SCHEDULED D-CHECK, FOUND LEFT CREASE BEAM CORRODED AT BS 847 TO BS 867. REPAIRED CREASE BEAM SECTION PER SRM. 2L72 4F RTA16WE 20050805000542005080500054NM 2005 8 5 SWAA052143 120050721A55306546874 ANGLE BOEING737 7373H4 1384600NM VERT STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29609SW 27929 DURING SCHEDULED D-CHECK, FOUND VERTICAL STAB LEFT FWD AND RIGHT AFT DRAG ANGLES FACES CORRODED. REMOVED AND REPLACED DRAG ANGLES PER SRM. 2L72 4F RTA16WE 20050805000552005080500055NM 2005 8 5 SWAA052144 120050721A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29443WN 29838 DURING SCHEDULED HC1 CHECK, FOUND EEPLS TRACK COVER DAMAGED AT ROW 14 ABC. REMOVED AND REPLACED COVER SECTION PER MM. 2L72 4F RTA16WE 20050805000562005080500056NM 2005 8 5 SWAA052145 120050718A53306552988 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29687SW 23388 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 931, ABOVE STR 25R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050805000572005080500057NM 2005 8 5 SWAA052294 120050802A53306545768 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29691WN 23781 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050805000582005080500058NM 2005 8 5 SWAA052295 120050802A53306545800 BEAR STRAP BOEING737 7373G7 1384595NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29691WN 23781 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN BEAR STRAP CORRODED AT BS 493, RBL 13. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050805000592005080500059NM 2005 8 5 SWAA052296 120050802A335010126211 BULB BOEING737 7373T5 1384608NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR VERTICAL EMERGENCY LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050805000602005080500060 2005 8 5 SWAA052297 420050801A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29733SA 27865 R1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. SLIDE DID NOT DEPLOY. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20050805000612005080500061NM 2005 8 5 SWAA052298 120050802A335090083 BATTERY PACK BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29793SA 27888 DURING SCHEDULED MV3 CHECK, FOUND COCKPIT EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050805000632005080500063NM 2005 8 5 SWAA052300 120050801A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29315SW 23337 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 361, BETWEEN STR 6R & STR 7R. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050805000672005080500067NM 2005 8 5 SWAA052202 120050727A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 727D + 5, LBL 13. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20050805000682005080500068NM 2005 8 5 SWAA052203 120050727A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 767 + 5, RBL 3 & RBL 8. REPAIRED FLOORBEAMS PER SWA EA. 2L72 4F RTA16WE 20050805000712005080500071 2005 8 5 SWAA052206 420050727A25651061323433 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF LIMITS A SWAAK NONE O OTHER ININSP/MAINT 1 SW29355SW 25250 R2 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATOR OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20050805000722005080500072NM 2005 8 5 SWAA052207 120050726A53306545775 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29522SW 26564 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 774, STR 25L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050805000782005080500078NM 2005 8 5 SWAA052186 120050725A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING WALKAROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 480, STR 16L. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050805000802005080500080NM 2005 8 5 SWAA052188 120050725A3350101073 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29435WN 32455 EMERGENCY EXIT FLOOR LIGHT LENS LOOSE. SECURED LENS PER MM. 2L72 4F RTA16WE 20050805000822005080500082 2005 8 5 SWAA052190 420050725A256561621468 SLIDE BOEING737 7375H4 138449DNM R2 DOOR DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 DURING SCHEDULED RON CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATING LOW. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20050805000832005080500083NM 2005 8 5 SWAA052191 120050725A335010107451 LIGHT BOEING737 7373H4 1384600NM FWD GALLEY INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29357SW 26594 DURING SCHEDULED SERVICE CHECK, FOUND FWD GALLEY LOWER EMERGENCY EXIT LIGHT INOP. SECURED LIGHT PER MM. 2L72 4F RTA16WE 20050805000842005080500084NM 2005 8 5 SWAA052192 120050724A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29369SW 26580 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 12R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050805000852005080500085NM 2005 8 5 SWAA052193 120050726A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29610WN 27696 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050805000862005080500086CE 2005 8 5 DJFA2005124 120050802A2910 HYDRAULIC SYSTEM CESSNA525 525 2076601CE LEAKING E DJFAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 EA23247CW 5250247 AFTER TAKEOFF CREW REPORTED HEARING A CAVITATION SOUND FROM THE REAR OF THE AIRCRAFT. AROUND 10,000 FT HYDRAULIC FLOW LOW LEFT AND RIGHT ANNUNCIATORS AND MASTER CAUTION LIGHTS WERE FLICKERING ON AND OFF. AFTER APPROXIMATELY 30 SECONDS, THE HYDRAULIC FLOW AND MASTER CAUTION LIGHTS WERE ON STEADY. THE CREW DIVERTED THE AIRCRAFT TO KAZO AND BLEW THE GEAR DOWN FOR LANDING. A ZERO DEGREE FLAP LANDING WAS PERFORMED WITH NO OPERATIONAL HYDRAULIC SYSTEM ON THE AIRCRAFT. FOLLOWING LANDING THE CREW HAD FOUND A SUBSTANTIAL AMOUNT OF HYDRAULIC FLUID ON THE REAR OF THE AIRCRAFT. 1L72 4F RTA1WI 20050803000602005080300060NM 2005 8 3 2005UALA00729 120050708A2910 WARNING LIGHT AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE GREEN HYD SYS ILLUMINATED A UALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP2945UA 1585 LOST GREEN SYSTEM HYDRAULIC QTY INDICATION. CREW HAS SHUTDOWN EDP AND PTU. WILL REQUIRE TOW OFF RUNWAY. GREEN HYD QTY LOSS, CREW HAS SHUTDOWN EDP AND PTU. NO SIGNS TH AT PUMP WAS RUN DRY. WILL REQUIRE TOW OFF RUNWAY. INDLM/AFTER MEETING ACFT ON RUNW AY FOUND LEFT MLG DOOR UPLOCK ACTUATOR LEAKING AT THE SUPPLY LINE B-NUT FITTING. FITTING WAS LOOSE APPROX ONE HALF TURN. SECURED FITTING LINE. 2L72 4F4 FRTA28NM E40NE 20050803000822005080300082CE 2005 8 3 06172005B 120050617A2710 TRIM SYSTEM BEECH 1900 1900D 1154162CE AILERONS LACK OF LUBE A NSVAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 EA27172MJ UE72 AILERON TRIM NOT MOVING. INSPECTED AND LUBED TRIM KNOB. 2L72 4T RTA24CE 20050803000852005080300085 2005 8 3 06092005A 420050609A61228210410 GOVERNOR BEECH 1900 1900D 1154162CE PROPELLER MALFUNCTIONED A NSVAO OTHER O OTHER LDLANDING 1 EA27124CJ UE24 NOTICED RIGHT YAW WHEN POWER REDUCED DURING LANDING FLARE. REMOVED AND REPLACED PROP GOVERNOR. 2L72 4T RTA24CE 20050803000972005080300097 2005 8 3 SWAA052118 420050720A2210162300103 COMPUTER BOEING737 7373H4 1384600NM ELEVATOR FEEL FAULTY A SWAAD RETURN TO BLOCK F FLT CONT AFFECTED CLCLIMB 1 SW29336SW 23940 AIR TURNBACK, ELEVATORS FELT BINDING DURING ROTATION. REMOVED AND REPLACED ELEVATOR FEEL COMPUTER PER MM. 2L72 4F RTA16WE 20050803001022005080300102NM 2005 8 3 SWAA052124 120050720A55536547450 FITTING BOEING737 7373H4 1384600NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29609SW 27929 DURING SCHEDULED D CHECK FOUND, LT AND RT VERTICAL STAB ATTACH FITTING LUG FACES CORRODED. REPAIRED LUGS PER SRM. 2L72 4F RTA16WE 20050803001152005080300115NM 2005 8 3 SWAA052248 120050728A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 805, STR 26L. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20050803001192005080300119NM 2005 8 3 SWAA052253 120050729A2497W4707420 WIRE BOEING737 7373H4 1384600NM CONTROL PANEL CHAFED A SWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW29328SW 23692 DIVERSION/DECLARED EMERGENCY, A LARGE ELECTRIC SPARK OCCURRED IN COCKPIT OVERHEAD PANEL AND SHOWERED CENTER CONSOLE WITH SPARKLER LIKE FRAGMENTS. FOUND CHAFFED WIRE BUNDLE IN OVERHEAD PANEL, REPAIRED WIRE PER MM. 2L72 4F RTA16WE 20050803001262005080300126NM 2005 8 3 SWAA052261 120050729A53306545774 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 22R. REPAIRED SKIN PER SWA EA AND SRM. 2L72 4F RTA16WE 20050803001342005080300134NM 2005 8 3 DHL2005788010 120050802A3260387 BULB BOEING727 727214 138407RNM MLG INDICATOR INTERMITTENT A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01788AT 21958 LEFT MAIN GEAR LIGHT ILLUMINATES INTERMITTENTLY. RELAMPED LEFT GEAR GREEN LIGHT BULB. CKS GOOD IAW MM 32-61-01, (BULB NR387). 2L73 4F A3WE 20050803001362005080300136SO 2005 8 3 02062105 120050621A3260922AA2YA6PZ722A PROXIMITY SWITCH EMB 120 EMB120ER 3260203SO MLG OVERHEATED E HSYAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 NM05125AM 120017 PILOT ADVISED THAT DURING DEPARTURE, AFTER SELECTING GEAR UP, COCKPIT INDICATION SHOWED RT MLG DID NOT RETRACT. GEAR DOWN SELECTED AND COCKPIT INDICATIONS SHOWED GEAR UNSAFE CONDITION. GEAR EXTENDED BY EMERGENCY PROCEDURES AND RETURNED TO CPR. T/S SYSTEM AND FOUND RELAY BOX OVERHEATING. REPLACED RELAY BOX WITH SERVICEABLE RELAY BOX. PERFORMED RETRACT CHECKS AND GEAR FAILED TO EXTEND. FURTHER TROUBLESHOOTING REVEALED AN INTERNALLY FAILED A-SYSTEM DOWNLOCK PROXIMITY SENSOR ON RT MLG. REPLACED RT MLG A-SYSTEM DOWNLOCK PROX SENSOR. MLG RETRACT/EXTEND CHECKS GOOD. A/C RELEASED FOR TEST FLT WITH SATISFACTORY RESULTS. A/C RETURNED FOR SERVICE. W 2L72 4T RTA31SO 20050803001462005080300146NM 2005 8 3 SWAA052223 120050728A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR CUTOUT, UPPER AFT CORNER. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050803001592005080300159NM 2005 8 3 SWAA052228 120050727A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29403WN 29815 DURING SCHEDULED MV2 CHECK, FOUND EEPLS STRIP MISSING COVER AT EMERGENCY EXIT. INSTALLED COVER PER MM. 2L72 4F RTA16WE 20050803001652005080300165NM 2005 8 3 SWAA052235 120050728A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29610WN 27696 DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 827, BETWEEN RBL 8 TO RBL 12. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050803001702005080300170NM 2005 8 3 SWAA052157 120050724A3350101073 LENS BOEING737 7373H4 1384600NM L1 DOOR MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29632SW 27707 L1 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20050804000072005080400007NM 2005 8 4 UPS05445025 120050723A5313 STRINGER BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 BS 1940-1960 STR 11R STRINGER END FOUND CRACKED, CRACK LENGTH 1 INCH. BS 1930 TO BS 1960 STR 11R REPAIRED AS PER SRM 53-10-03 FIG 4. 2L74 4F A20WE 20050804000382005080400038NE 2005 8 4 UPS05845033 220050803A7200 ENGINE DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE NR 4 SHUTDOWN A IPXAEA ENGINE SHUTDOWN UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO01813UP 46059 NR 4 ENG SHUT DOWN IN FLT DUE TO OVER TEMP AND LOUD THUD. FROM LP 427064 ITEM 1 AND LP 427065 ITEM 3: PERFORMED THRUST LEVER STATIC TRIM IAW AMM 71-00-00 PG 595.23 TEST 9A. PERFORMED PART POWER TRIM AND INCREASED BY 10 CLICKS. PERFORMED ENG HIGH PWR RUN-UP. R & R NR 4 ENG PER TC 9071-1,2,3. OPS AND LEAK CK GOOD. 2L74 4F4 FRT4A25 E2GL 20050804000602005080400060NM 2005 8 4 SWAA052153 120050723A53306545777 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED BELOW DORSAL FIN AT BS 967, STR 2R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050804000832005080400083EU 2005 8 4 AWXA200500903 120050707A5320D53471124200 WEB AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28627AW 66 SAL - DURING C4 CHECK DISCOVERED CORROSION ON WEB IN CABIN LOCATED AT FS 69+16", STRINGER 23L, Y1200. NO ALLOWABLE DAMAGE LIMITS WERE FOUND IN THE AIRBUS 320 SRM. MAINTENANCE REMOVED AND REPLACED THE WEB LOCATED AT FR 69+16", STRINGER 23L, Y1200 IAW AIRBUS 320 SRM 51-44-11. ALSO, APPLIED SEALANT TO NEW WEB IAW AIRBUS 320 SRM 51-76-11. 2L72 4F RTA28NM 20050804000862005080400086EU 2005 8 4 AWXA200500906 120050713A5347D5713014720302 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28627AW 66 SAL - DURING C4 CHECK DISCOVERED CORROSION ON SEVERAL SECTION OF SEAT TRACK LOCATED BETWEEN FS 36 AND FS 47, BUTT LINE Y765 AND Y-1292. MAINTENANCE REMOVED ALL CORROSION FROM SEAT TRACKS BETWEEN FS 36 AND FS 47, BL Y765 AND Y-1292 IAW AIRBUS 320 SRM 51-74-00. FOUND RE-WORK ON SEAT TRACKS TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15. REMOVED SEAT TRACK SECTIONS FROM VARIOUS LOCATION BETWEEN FS 36 TO FS 47 AND BETWEEN BUTT LINE Y765 TO Y-1292 IAW AIRBUS 320 SRM 51-42-11. INSTALLED NEW SEAT TRACK SECTIONS FROM FS 36 TO FS 47, BUTT LINE Y765 TO Y-1292 AND APPLIED PROTECTIVE TREATMENT IAW AIRBUS 320 SRM 51-42-11 AND A320 SRM 51-21-11. 2L72 4F RTA28NM 20050804000972005080400097EA 2005 8 4 SWIA200515341 120050726A3350 BATTERY PACK CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT DISCHARGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07703SK 10139 EMERGENCY LIGHTS SWITCH ON F/A PANEL LEFT IN "ON" POSITION, EMERGENCY LIGHTS INOP. REPLACED FOUR ELBP'S IAW CRJ 700 MM 33-51-17. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050804001182005080400118NM 2005 8 4 UPS05445016 120050725A5315 FLOORBEAM BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 BS 360 LBL 40 FLOORBEAM FOUND CORRODED. CORROSION BLEND OUT 0.035 BY 2 BY 2 EXCEED SRM 53-10-01 FIG 1 LIMITS. BS 360 LBL 21" TO LT O/B END FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 53-10-07 FIG 23. 2L74 4F A20WE 20050804001202005080400120NM 2005 8 4 UPS05445018 120050723A5313 STRINGER BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 BS 1958-1960 STR 2L STRINGER END FOUND CRACK, CRACK LENGTH 1.5". STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4 JUST AT STR-2L BETWEEN BS 1930 AND 1960. 2L74 4F A20WE 20050804001212005080400121NM 2005 8 4 UPS05445019 120050726A5313 STRINGER BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 BS 560 S9L STRINGER END FOUND CRACK, CRACK LENGTH 7/16". BS 560 STR 9L STR END REPAIRED AS PER SRM 53-10-03 FIG 2. 2L74 4F A20WE 20050804001222005080400122NM 2005 8 4 UPS05445020 120050726A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 BS 560, BETWEEN STR 6L - 8L FRAME AFT FACE O/B AREA 2EA CRACK FOUND, CRACK LENGTH 1.125 & 3/4". BS 560 FRAME REPAIRED AS PER SRM 53-10-04 FIG 54 AT BTN STR 6L TO 8L AREA. 2L74 4F A20WE 20050805000182005080500018EA 2005 8 5 COMA0560412 120050727A5270 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA PAX DOOR ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01716CA 7250 FLIGHT 5429 - CABIN DOOR OUTER HANDLE CAUTION MESSAGE. DEFERRED MAINTENANCE ON DOOR WARNING PER MEL. 2L72 4F RTA21EA 20050805000222005080500022NM 2005 8 5 SWAA052213 120050727A3350101073 LENS BOEING737 7373H4 1384600NM EMERTENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29639SW 27712 L1 DOOR LOWER EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM. 2L72 4F RTA16WE 20050805000252005080500025NM 2005 8 5 SWAA052216 120050722A53126545819 PRESSURE PANEL BOEING737 7373Y0 1384671NM NLG WW CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED SERVICE CHECK, FOUND NLG WW LEFT UPPER ACCESS CUTOUT, AFT INBOARD CORNER CRACKED AT BS 249, LBL 2. REPAIRED WEB PER SWA EA. 2L72 4F RTA16WE 20050805000662005080500066NM 2005 8 5 SWAA052201 120050727A53126546568 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT DOME CAP, 1 O'CLOCK POSITION. REPAIRED WEB PER SWA EA. 2L72 4F RTA16WE 20050805000702005080500070NM 2005 8 5 SWAA052205 120050727A3350101331 LIGHT BOEING737 7373H4 1384600NM MID CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29330SW 23694 RIGHT OVERWING EMERGENCY EXIT DOOR LIGHT LOOSE. SECURED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20050805000742005080500074NM 2005 8 5 SWAA052209 120050727A53116558280 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29610WN 27696 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050805000752005080500075NM 2005 8 5 SWAA052211 120050727A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29610WN 27696 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 767, LBL 9. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050805000882005080500088NM 2005 8 5 SWAA052285 120050801A33506104789 BATTERY BOEING737 7373K2 13844BANM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29345SA 23786 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHTS INOP AT AFT ENTRY DOORS. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050805000892005080500089NM 2005 8 5 SWAA052286 120050802A3350207377 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29450WN 32470 EEPLS TRACK LENS MISSING AT ROW 2 ABC. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20050805000902005080500090NM 2005 8 5 SWAA052287 120050802A335065C27093 LIGHT BOEING737 7377H4 1384404NM EMERGENCY EXIT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29496WN 32478 R2 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20050805000952005080500095NM 2005 8 5 SWAA052171 120050722A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 687, STR 10L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050805000962005080500096NM 2005 8 5 SWAA052172 120050722A53126546568 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE WEB CRACKED AT AFT PRESSURE BULKHEAD, BS 1016, STR 6R. REPAIRED AFT PRESSURE BULKHEAD WEB PER SRM. 2L72 4F RTA16WE 20050805000972005080500097NM 2005 8 5 SWAA052269 120050801A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 907, BETWEEN STR 25L TO STR 25R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050805000982005080500098NM 2005 8 5 SWAA052270 120050801A53116545808 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303, L1 DOOR LOWER FWD STOP FITTING CUTOUT. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050805001012005080500101NM 2005 8 5 SWAA052273 120050730A33501010427 COVER BOEING737 7373H4 1384600NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 BULLNOSE LIGHT COVER MISSING AT ROW 6 ABC. INSTALLED COVER PER MM. 2L72 4F RTA16WE 20050805001042005080500104NM 2005 8 5 SWAA052276 120050801A335020131 BATTERY BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29333SW 23697 DURING SCHEDULED A1 CHECK, FOUND RIGHT AFT EXTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20050805001052005080500105 2005 8 5 SWAA052277 420050801A256563550101 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF LIMITS A SWAAK NONE O OTHER ININSP/MAINT 1 SW29427WN 29831 R1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATES OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20050805001072005080500107NM 2005 8 5 SWAA052279 120050731A53306545776 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29519SW 25318 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 924, STR 24L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050805001082005080500108 2005 8 5 SWAA052280 420050731A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29608SW 27928 DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050805001092005080500109NM 2005 8 5 SWAA052281 120050731A2897 WIRE BOEING737 7373H4 1384600NM FUEL SHUTOFF VLVDAMAGED A SWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW29648SW 27718 DIVERSION, EVIDENCE OF ELECTRICAL ODOR IN COCKPIT. FOUND WIRES DAMAGED IN OVERHEAD P-5 PANEL, NR 1 ENGINE FUEL SHUT-OFF VALVE & MLG POSITION SENSOR CIRCUIT BREAKERS POPPED. REPAIRED WIRES PER SWPM. REMOVED AND REPLACED P52 FUEL MODULE & T492 LEFT MLG POSITION SENSOR PER MM. 2L72 4F RTA16WE 20050805001132005080500113NM 2005 8 5 05FDEA02215 120050803A5753 SKIN DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 RIGHT HAND WING UPPER SURFACE TRAILING EDGE FORWARD OF OUTBOARD AILERON SKIN BULGE FOUND AT XORS 850.33. RHW UPPER SURFACE T/E FWD OF O/B AILERON XORS 850.33 SKIN BULGE AREA CORROSION REMOVED. MAT'L REMOVED: 0.023"; ORIG. THK:0.150"; MAT'L REMAINED: 0.127" FOUND EXCEED LIMIT PER SRM 57-10-00 FIG 32 VOL I.AREA REPAIR C/O PER FEDEX EA: 1-5710-87559-WINGS RT UPPER WING SKIN CORROSION REPAIRS AT XORS 845, XORS 979,AND XORS 989 COMMON TO THE T/E. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2L73 4F RTA22WE 20050805001142005080500114NM 2005 8 5 05FDEA02216 120050803A5755 SKIN DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 RIGHT HAND WING UPPER SURFACE TRAILING EDGE FORWARD OF NR 2 SPOILER SKIN BULGE AT XORS 538.49 STRINGER 4. RT WING UPPER SURFACE TRAILING EDGE FORWARD OF NR 2 SPOILER XORS 538.49 STRINGER 4 SKIN BULGE AREA CORROSION REMOVED. MAT'L REMOVED: 0.024"; ORIG. THICKNESS: 0.330"; MAT'L REMAINED: 0.306"; AREA REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-87562 - WINGS - RT UPPER WING SKIN - CORROSION REPAIRS AT XORS = 531 THRU XORS = 536 & XORS = 540. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050805001172005080500117WP 2005 8 5 05FDEA02193 120050802A5312 BULKHEAD DOUG MD10 MD1010F 3022112WP FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25381FE 46615 RIGHT AIR CONDITIONING COMPT LOWER BULKHEAD FOUND 1 EACH CRACK 0.5 INCH LONG ON WEB AT STA 540. REPAIR PER SRM 53-00-01 FIG 7-9 VOL 1. 2L73 4F RTA22WE 20050805001182005080500118WP 2005 8 5 05FDEA02174 120050802A5312 BULKHEAD DOUG MD10 MD1010F 3022112WP FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25381FE 46615 AIR CONDITIONING COMPT RIGHT SIDE FOUND 6 EACH CRACKS 0.5 INCH LONG ON BULKHEAD SKIN STA 500. REPAIR PER SRM 53-30-00 FIG 6 VOL 1. 2L73 4F RTA22WE 20050805001192005080500119WP 2005 8 5 05FDEA02175 120050802A5313 LONGERON DOUG MD10 MD1010F 3022112WP FUSLEAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25381FE 46615 ONE CRACK 1 INCH LONG ON LONGERON INSIDE APU COMPT STA 2050. REPAIRED CRACK PER SRM 53-17-01 FIG 4 VOL 3, SRM 54-00-01 FIG 2B VOL 1, SRM 51-35-01 PG 1-13 VOL 2. 2L73 4F RTA22WE 20050805001212005080500121WP 2005 8 5 05FDEA02177 120050802A5711 FRAME DOUG MD10 MD1010F 3022112WP LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25381FE 46615 ONE CRACK 0.25 INCH LONG INSIDE FRAME LEADING EDGE LT WING AT XORS 368. REPAIR CRACK IAW SRM 57-20-00 FIG 1 VOL 1. 2L73 4F RTA22WE 20050805001222005080500122WP 2005 8 5 05FDEA02178 120050802A5347 SEAT TRACK DOUG MD10 MD1010F 3022112WP FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25381FE 46615 ONE CRACK 2 INCHES LONG INSIDE TRACK AND FORMED PART AT STA 1019 X=-27 MAIN CABIN FLOOR PANEL. REPAIR SEAT TRACK PER SRM 53-70-00 FIG 1 VOL 1. 2L73 4F RTA22WE 20050805001232005080500123WP 2005 8 5 05FDEA02179 120050802A5320 ANGLE DOUG MD10 MD1010F 3022112WP FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25381FE 46615 AIR CONDITIONING COMPT LT TEE ANGLE WITH CORROSION ON INTERNAL LOWER STRUT FROM STA 560 TO STA 580. INSTALLED NEW SECTION OF LONGERONS AND SPLICE REPAIR PER SRM 53-10-00 FIG 7 VOL 1. 2L73 4F RTA22WE 20050805001252005080500125WP 2005 8 5 05FDEA02182 120050802A5313 LONGERON DOUG MD10 MD1010F 3022112WP FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25381FE 46615 ONE CRACK 4 INCHES LONG ON LONGERON INSIDE APU COMPT RT SIDE STA 2050. REPAIRED CRACK PER SRM 53-17-01 VOL 3 FIG 4, SRM 54-00-01 FIG 2B VOL 1, SRM 51-35-01 PG 1-13 VOL 2. 2L73 4F RTA22WE 20050805001292005080500129WP 2005 8 5 05FDEA02170 120050802A5340AYB70002 TEE FITTING DOUG MD10 MD1010F 3022112WP ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25381FE 46615 AT STA Y=1156 ON TEE CAP INTERNAL RT SIDE BETWEEN LONGERONS 39-40 FOUND CRACK 3 INCHES LONG. REMOVED TEE ANGLE AND INTERNAL DOUBLER IAW SRM 53-40-00 FIG 8 VOL 1. PERFORMED NDT INSPECTION FOUND CRACK 4.3 INCHES LONG. REPAIRED PER SRM 53-40-00 FIG 8 VOL 1. 2L73 4F RTA22WE 20050805001312005080500131WP 2005 8 5 05FDEA02172 120050802A5414 SKIN DOUG MD10 MD1010F 3022112WP NR 3 NACELLE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25381FE 46615 ONE EACH CRACK 1 INCH LONG ON EXTERNAL CORE COWL SKIN RIGHT SIDE ENGINE NR 3. REPAIR IAW SRM 54-10-00 FIG 16 VOL 1. 2L73 4F RTA22WE 20050805001322005080500132WP 2005 8 5 05FDEA02173 120050802A5711 FRAME DOUG MD10 MD1010F 3022112WP LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25381FE 46615 ONE EACH CRACK .5 INCH LONG, ON LEADING EDGE FRAME LT WING AT XORS 372. REPAIR IAW SRM 57-20-00 FIG 1 VOL 1. 2L73 4F RTA22WE 20050805001332005080500133CE 2005 8 5 CIEA200500011 120050724A7830451230 LATCH LEAR 55 55C 5170706CE THRUST REVERSER OUT OF ADJUST E CIEAO OTHER N FALSE WARNING CRCRUISE 1 NM03113YS102594 55071 AFTER TAKEOFF, THE LEFT THRUST REVERSER LIGHT FLASHED ON THEN WENT OUT. THE PILOT ELECTED TO LAND AND HAVE IT LOOKED AT. THERE WAS NO EVIDENCE THAT THERE WAS A PROBLEM. THE UNIT WORKED GOOD ON THE GROUND. THE T/R'S WERE PINNED AND DEFERRED AND THE FLIGHT CONTINUED. THE AIRCRAFT WAS THEN INSPECTED BY MAINTENANCE AND WERE UNABLE TO DUPLICATE THE PROBLEM. AN ADJUSTMENT WAS MADE TO THE INBOARD PNEUMATIC LATCH AND SYSTEM WAS RUN ON THE GROUND AND NO DEFECTS WERE NOTED. 2L72 4F RTA10CE 20050805001392005080500139NM 2005 8 5 SWAA052304 120050803A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 795, STR 26R. REPAIRED STRINGER PER SWA EA. 2L72 4F RTA16WE 20050805001412005080500141EU 2005 8 5 05FDEA02211 120050802A7711 INDICATOR AIRBUS310 A310222 3930315EU NR 2 EPR FAILED A FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25421FE 342 AFTER SETTING 40 N1 AND ADVANCING THROTTLES FOR TAKEOFF THE 2 EPR GAUGE FAILED. REJECTED TAKEOFF AND RETURNED TO THE RAMP, NEEDED EPR'S FOR MANUAL THROTTLE SETTING. TROUBLESHOOTING IN PROGRESS. AWAITING PARTS. PERFORMED WIRING CHECK BETWEEN 2 ENG EEC TO 2 EPR INDICATOR FOUND WIRE R77150029 AND SHIELDED WIRE AT 2 EPR IND CONNECTOR SHORTED. REPAIRED AS PER SMP. AWAITING EEC AND ENG RUN. ENG RAN CARRIED OUT AS PER A310 JRH BY AMT 439456 EPR AND ALL OTHER PARAMETERS NORMAL. ACFT OK FOR SERVICE. 2L72 4F RTA35EU 20050805001422005080500142EU 2005 8 5 05FDEA02212 120050802A5753 SKIN AIRBUS300 A300B4605R 3930308EU TE FLAP DAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25671FE 778 LEFT WING I/B FLAP BOTTOM SKIN HAS CREASE AT MID SECTION REPAIRED DAMAGED SECTION OF LEFT I/B TRAILING EDGE FLAP LOWER SURFACE SKIN AND 2 EA STRINGERS IAW SRM 57-50-00 FIG 206. PREPPED AND PAINTED IAW MM 51-75-10-8. 2L72 4F RTA35EU 20050805001442005080500144NM 2005 8 5 05FDEA02214 120050803A5710 SKIN DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 RIGHT HAND WING UPPER SURFACE TRAILING EDGE FORWARD OF OUTBOARD AILERON SKIN BULGE FOUND AT XORS 979. RTW UPPER SURFACE T/E FWD OF O/B AILERON XORS 979 SKIN BULGE AREA CORROSION REMOVED. MAT'L REMOVED:0.031"; ORIGINAL THK: 0.150"; MAT'L REMAINED: 0119"; FOUND EXCEED LIMIT PER SRM 57-10-00 FIG 32 VOL I. AREA REPAIR C/O PER FEDEX EA:1-5710-87559 - WINGS R/H UPPER WING SKIN CORROSION REPAIRS AT XORS 845,XORS 979, XORS 989, COMMON TO THE T/E. REPAIR CLASSIFIED AS MAJOR PER GMM6-2-100. 2L73 4F RTA22WE 20050805001452005080500145NM 2005 8 5 SWAA052305 120050803A53306545775 SKIN BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 787, STR 26R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050805001472005080500147NM 2005 8 5 SWAA052307 120050803A335010107451 LIGHT BOEING737 7373H4 1384600NM R1 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29375SW 26583 R1 DOOR EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT PER MM. 2L72 4F RTA16WE 20050805001512005080500151NM 2005 8 5 SWAA052311 120050802A57546573714 SKIN BOEING737 7375H4 138449DNM RT WING SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29523SW 26565 DURING SCHEDULED C4 CHECK, FOUND RT WING NR 5 L/E SLAT T/E WEDGE DELAMINATED. REPAIRED SLAT PER SWA EA. 2L72 4F RTA16WE 20050805001532005080500153 2005 8 5 SWAA052313 420050803A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050805001542005080500154NM 2005 8 5 SWAA052314 120050803A53306545765 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29691WN 23781 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C + 17, STR 10L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050805001572005080500157NM 2005 8 5 DL757050379 120050719A2121216001013 COOLING FAN BOEING757 757232 1384965NM C-1 CARGO BAY ODOR A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27686DA 27589 EQUIPMENT COOLING OVERHEAT WITH ODOR, NOT VISIBLE SMOKE. PLACED IN ALTN, ODOR DISSIPATED. REPLACED FWD EQUIPMENT COOLING FAN. 2L72 4F RTA2NM 20050805001592005080500159NM 2005 8 5 DLM88050381 120050718A53119911859121 FRAME DOUG MD88 MD88 3023688NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27915DL 49546 DAMAGE FOUND WHILE ACOMPLISHING EO 9-62073-12 AT HMV, CRACK IN STA 1446 LONGERON 5R. REPAIRED PER SRM 53-03 FIG 30 AS PER EO 9-62073-12. OPERATION 103 INSTRUCTIONS. 2L72 4F RTA6WE 20050805001602005080500160NM 2005 8 5 DL757050382 120050720A34117077603 STATIC INVERTER BOEING757 757232 1384965NM FAILED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27680DA 26956 STATUS MESSAGE STBY INVERTER, INV POWER TRU BREAKER POPPED ONP6 PANEL. ELECTRICAL BURNING ODOR IN CABIN AND COCKPIT. REPLACED STATIC INVERTER PER AMM. OPS CK OK. CONFIRMED STATIC INVERTER CAUSED SMELL IN CABIN. 2L72 4F RTA2NM 20050805001612005080500161NM 2005 8 5 DLM88050383 120050720A3244 TIRE DOUG MD88 MD88 3023688NM NR 3 MLG FAILED A DALAC ABORTED TAKEOFF C F.O.D. TOTAKEOFF 1 SO27935DL 49722 ON T/O FLT ATTENDANT REPORTED NOISE FOLLOWED BY SMELL OF BURNT RUBBER. CREW HAD RETRACTED GEAR AND ON EXT HAD RED UNSAFE LIGHT. MAIN TIRE THREW A CAP. TIRE WAS STILL INFLATED 200PSI SOME DAMAGE TO FLAP, MLG DOWN LOCK CONDUIT AND SENSOR/BRACKET, BUTE DOOR AND NR 2 ENGINE FAN. REPLACED WHEEL AND REPAIRED DAMAGE. 2L72 4F RTA6WE 20050805001632005080500163 2005 8 5 DL767050386 420050720A2220 YAW DAMPER BOEING767 767232 1385132NM RUDDER MALFUNCTIONED A DALAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SO27102DA 22214 UNCOMMANDED RUDDER INPUT AT ROTATION, THOROUGHLY CHECKED SYSTEM. UNABLE TO DUPLICATE OR FIND FAULT. 2L72 4F RTA1NM 20050805001652005080500165NM 2005 8 5 DL76L050389 120050721A5730114T2400305 PANEL BOEING767 767332 1382001NM LT WING MISSING A DALAK NONE O OTHER ININSP/MAINT 1 SO27189DN 25990 LEFT WING PANEL (NR 521EB) COMPLETELY MISSING FROM WING WHEN AIRCRAFT ARRIVED IN LGW. REPLACED SAME. 2L72 4F RTA1NM 20050808000012005080800001NM 2005 8 8 MASA200500524 120050707A52104100S00901 PRESSURE VALVE DHAV DHC8 DHC8202 2809007NM PAX DOOR MALFUNCTIONED A MASAO OTHER J WARNING INDICATION APAPPROACH 1 SW07437YV10813 437 ASH 6259 PSP, THE AIRCRAFT DECLARED AN EMERGENCY ON ITS WAY INTO PHX WITH A PAX DOOR WARNING MESSAGE. MAINTENANCE REPLACED THE PASSENGER DOOR PRESSURE VALVE. 2H72 4T RTA13NM 20050808000022005080800002NM 2005 8 8 MASA200500574 120050719A7931APT761000100DW TRANSDUCER DHAV DHC8 DHC8202 2809007NM NR 1 OIL PRESS DAMAGED A MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW07454YV10523 454 ASH 7081 DEN , NR 1 ENGINE OIL PRESSURE INDICATED 100 PSI. MX REPLACED NR 1 ENGINE OIL PRESSURE TRANSDUCER AND REPAIRED WIRING TO CONNECTOR. 2H72 4T RTA13NM 20050808000032005080800003NM 2005 8 8 UPS05445034 120050727A5310 PRESSURE PANEL BOEING747 747121 1384871NM NLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 LT WLG WW SIDEWALL PANEL FOUND CRACK AT BTN BS 260 AND 280 WL 170 APPROX 1 INCH. LT NLG WW SIDEWALL PANEL REPAIRED AT BS 260 TO BS 280 WL 170 AREA AS PER SRM 53-10-04 FIG 116. 2L74 4F A20WE 20050808000042005080800004NM 2005 8 8 UPS05445035 120050723A5320 WEB BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 BS 1920-1940 S26R FLOOR WEB I/B EDGE FOUND CRACKED, CRACK LENGTH 0.75. WEB REPAIRED AS PER SRM 51-40-03 FIG 1. 2L74 4F A20WE 20050808000052005080800005NM 2005 8 8 UPS05445036 120050725A532065B140561 KEELBEAM BOEING747 747121 1384871NM FUSLEAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 FX KEELBEAM PANEL SUPPORT FOUND CORROSION AT BS 1405. CORROSION BLEND OUT 0.054 BY .750 BY 1.5 EXCEED SRM 53-10-01 FIG 1 LIMITS, SUPPORT REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050808000072005080800007NM 2005 8 8 UPS05445038 120050723A532269B031464 SHEAR TIE BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 BS 2160 BETWEEN STR 20-22L FRAME AFT FACE SHEAR TIE FOUND CRACK, CRACK LENGTH .750. SHEAR TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050808000082005080800008NM 2005 8 8 UPS05445039 120050723A532269B028032 SHEAR TIE BOEING747 747121 1384871NM FUSLEAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 BS 1860 S10-11R STRINGER SHEAR TIE FOUND CRACKED, CRACK LENGTH .50. SHEAR TIE CLIP REPLACED AS PER SRM 51-10-01. 2L74 4F A20WE 20050808000102005080800010NM 2005 8 8 UPS05445041 120050725A532069B035204 FLOOR SUPPORT BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 STA 710 LBL 47 TO LBL 66 FLR SUPPORT FOUND CORRODED. CORROSION BLEND OUT 0.023 BY .50 BY 1 EXCEED SRM 53-10-01 FIG 1 LIMITS, FLR SUPPORT REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050808000112005080800011NM 2005 8 8 UPS05445042 120050723A5315 FLOORBEAM BOEING747 747121 1384871NM FWD CARGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 FWD CARGO RT STA 800 RBL 33 FLOORBEAM UPPER CHORD FOUND CORRODED AND CRACKED. CORROSION BLEND OUT 0.080" BY 1" BY 2.5" EXCEED SRM 53-10-01 FIG 1 LIMITS, FLOORBEAM REPAIRED AT BS 800 RBL 26 TO RBL 42" AREA AS PER SRM 51-40-04 FIG 2. 2L74 4F A20WE 20050808000122005080800012NM 2005 8 8 UPS05445043 120050722A5311 FRAME BOEING747 747121 1384871NM AFT CARGO CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 AFT CARGO LT BS 1900 FRAME WEB FOUND CRACKED BETWEEN LT STR 36 AND LT STR 37, CRACK LENGTH .500. AFT CARGO LT BS 1900 FRAME REPAIRED AT BETWEEN LT STR 36 & 37 AREA AS PER SRM 53-10-04 FIG 4. 2L74 4F A20WE 20050808000132005080800013NM 2005 8 8 UPS05445044 120050722A5311 FRAME BOEING747 747121 1384871NM AFT CARGO CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 AFT CARGO RT BS 1500 FRAME WEB FOUND CRACKED BETWEEN RT STR 28 & STR 29, CRACK LENGTH .4375. AFT CARGO RT BS 1500 BETWEEN S28 TO S29 AREA FRAME REPAIRED AS PER SRM 53-10-04 FIG 4. 2L74 4F A20WE 20050808000142005080800014NM 2005 8 8 UPS05445045 120050722A5311 FRAME BOEING747 747121 1384871NM AFT CARGO CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 AFT CARGO RT BS 1520 FRAME WEB FOUND CRACKED AT RT STR 31, CRACK LENGTH .500. AFT CARGO RT BS 1520 FRAME REPAIRED AT STR 31 RT AREA AS PER SRM 53-10-04 FIG 4. 2L74 4F A20WE 20050808000152005080800015NM 2005 8 8 UPS05445047 120050725A5315 FLOORBEAM BOEING747 747121 1384871NM FUSLEAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 BS 340 LBL 40-50 FLOORBEAM FOUND CLR. CORROSION BLEND OUT 0.047 BY 2 BY 5 EXCEED SRM 53-10-01 FIG 1 LIMITS, U/D BS 340 LBL 8 TO LT O/B END FLOORBEAM REPAIRED AS PER SRM 53-10-07 FIG 23. 2L74 4F A20WE 20050808000162005080800016 2005 8 8 BB05058 420050801A2565130104233 SLIDE BOEING767 7672B7 1385107NM RT OFF WING READS LOW A USAAK NONE O OTHER ININSP/MAINT 1 EA19653US16317975 24894 PHL - RIGHT OFF THE WING SLIDE PRESSURE WAS FOUND LOW. MAINTENANCE REPLACED THE RIGHT WING SLIDE BOTTLE. OK FOR SERVICE. 2L72 4F RTA1NM 20050808000212005080800021NM 2005 8 8 0501196744 120050803A2910BACH8A10EE0380B HOSE BOEING747 747212F 1384851NM NR 4 HYD SYSTEM FAILED A NWAAH DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL01644NW 24177 AFTER TAKEOFF, HAD A TOTAL LOSS OF NR 4 HYDRAULIC SYSTEM. COM WAS FOLLOWED, AN EMERGENCY WAS DECLARED WITH ATC AND RETURNED TO SIN, LANDING WAS UNEVENTFUL. FOUND LEFT HAND WING GEAR ACTUATOR UP FLEX LINE BROKEN AND REPLACED. REPLACED (EDP) ENGINE DRIVEN HYDRAULIC PUMP DUE TO A TOTAL LOSS OF HYD FLUID. NO CONTAMINATION WAS FOUND IN THE EDP AND ADF CASE DRAIN FILTERS. INSPECTION COMPLETED AND AIRCRAFT RETURNED TO SERVICE. 2L74 4F RTA20WE 20050808000252005080800025SO 2005 8 8 CHQA200500136 120050804A33501317 BULB EMB 135 EMB135KL 3260302SO EMERGENCY LIGHTSBURNED OUT A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11295SK 145513 LEFT AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BULB IAW EMB 140 MM 33-50-10. OPS CHECK GOOD. 2L72 4F RTT00011AT 20050808000262005080800026NM 2005 8 8 QXEA200501148 120050802A7540 WARNING LIGHT BOMBDRDHC8 DHC8402 1390042NM BLEED AIR SYS ILLUMINATED A QXEAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 NM09404QX 4046 RDD FLIGHT NR 2308: BOTH BLEED HOT CAUTION LIGHTS CAME ON DURING ROTATION ON TAKEOFF. RAN CHECKLIST. LIGHTS STAYED ON. RETURNED TO FIELD. ACCOMPLISHED UNEVENTFUL LANDING. NO PARTS REPLACED. MAINTENANCE RESET WITH FIM. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050808000272005080800027NE 2005 8 8 CALA0500253 220050804A7200 ENGINE BOEING757 757224 1384958NM RROYCERB211 RB211535E4 54555NE NR 2 FAILED A CALAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 SW2714106 27296 31269 NR 2 ENGINE BEGAN TO VIBRATE AT LEVEL OFF AFTER DEPARTING LAX. A RETURN TO LAX WAS INITIATED AND ENG WAS SHUTDOWN ON APPROACH. THE ACFT LANDED WITHOUT INCIDENT. INITIAL EXAMINATION OF THE ENGINE REVEALED METAL IN THE TAILPIPE. THE NR 2 ENGINE WAS R & R IAW MM. LEAK AND OPS CHECKS WERE GOOD. ENGINEERING INVESTIGATION REVEALED FAILURE OF IPT LOCK PLATES. THE IP COUPLING HAD BECOME UNLOCKED CAUSING REARWARD MOVEMENT OF THE IPT SYSTEM RESULTING IN CONTACT WITH THE IPNGV SEAL CARRIER. THIS CONTACT TREPANNED AND RELEASED IPTB RETAINING PLATES THAT CAUSED DAMAGE TO IPT BLADE T/E. AND LED TO SUBSEQUENT DOWNSTREAM DAMAGE TO THE LP NGV'S AND BLADES. 2L72 4F4 FRTA2NM E12EU 20050808000292005080800029NM 2005 8 8 SWAA052317 120050803A53206545409 WEB BOEING737 7373G7 1384595NM LT MLG WW CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29691WN 23781 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE BEADED WEB CRACKED AT BS 663, BETWEEN LBL 39.5 & LBL 42. REPAIRED BEADED WEB PER SWA EA. 2L72 4F RTA16WE 20050808000302005080800030NM 2005 8 8 CALA0500252 120050804A3350MISC062 BATTERY BOEING767 767424ER 1385270NM EMERGENCY LIGHT INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2766056 29451 THE COCKPIT EMERGENCY LIGHT DID NOT ILLUMINATE DURING TEST. TWO BATTERIES ON THE COCKPIT EMERGENCY LIGHT PACK WERE REMOVED AND REPLACED IAW MM 33-51-01. 2L72 4F RTA1NM 20050808000312005080800031WP 2005 8 8 0501209851 120050802A2760 LINK ASSY DOUG DC9 DC951 3022051WP LT SPOILER BINDING A NWAAO OTHER F FLT CONT AFFECTED TOTAKEOFF 1 GL01760NC 47708 THE AIRCRAFT ROLLED LEFT ON TAKEOFF. AILERON TRIM WAS SET AT ZERO AND CREW HAD TO INPUT EXCESSIVE RIGHT TRIM TO MAINTAIN LEVEL FLIGHT. INCREASING RIGHT TRIM REQUIRED FOR EACH STAGE OF REMAINDER OR FLIGHT. AIRCRAFT MADE AN UNEVENTFUL LANDING AT DTW AND MAINTENANCE FOUND THAT THE LEFT INBOARD SPOILER PANEL WOULD NOT RETRACT FULLY. A BOLT ON THE SPOILER ACTUATOR LEVER LINK ASSEMBLY WAS FOUND TO BE BINDING IN THE OFF STOP POSITION. RETORQUING THE LINK ATTACH NUT ALLOWED PROPER OPERATION AND THE AIRCRAFT WAS RETURNED TO SERVICE AFTER ALL CHECKS WERE SATISFACTORY. 2L72 4F RTA6WE 20050808000322005080800032NE 2005 8 8 SF20050730 220050730A7200 ENGINE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE NR 1 OVERTEMP A UHLAC ABORTED TAKEOFF MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 GL1714XS 340A014 FLT NR 7531 FROM CRW TO IAD, ON TAKEOFF ROLL, NR 1 ENGINE OVERTEMP. TEMP REACHED 933 FOR APPROX 2 SECONDS. AIRCREW REJECTED TAKEOFF AND RETURNED TO GATE. 2L72 4T4 TRTA52EU E8NE6 20050808000332005080800033EU 2005 8 8 SF20050801 120050801A7603 SWITCH SAAB SF340 SF340A 7850100EU ENGINE CONTROLS DIRTY A UHLAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL1735SZ 035 FLIGHT 7579, FLIGHT IDLE STOP OPENED IN FLIGHT, A/C RETURNED TO FIELD. INSPECTED AND FOUND CONTROL QUADRANT MICROSWITCHES TO BE DIRTY, CLEANED MICRO-SWITCHES IAW SAAB M/M 76-10-60-2, PERFORMED OPERATIONAL CHECKS, IAW SAAB M/M 76-10-60-5, ALL OPS CHECKS GOOD. 2L72 4T RTA52EU 20050808000342005080800034EU 2005 8 8 200508041 120050804A2611 WARNING LIGHT SAAB SF340 SF340A 7850100EU CARGO SMOKE ILLUMINATED A UHLAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL17121CQ 121 FLT 7566 HPN-IAD, DURING ENGINE START, CARGO SMOKE LIGHT ON CWP ILLUMINATED. CREW PERFORMED VISUAL INSPECTION CONTRACT MAINTENANCE CALLED IN TO DEFER SYSTEM. 2L72 4T RTA52EU 20050808000372005080800037EA 2005 8 8 COMA0570089 120050729A3222521011 CYLINDER CNDAIRCL600 CL6002C10 1390015EA NLG CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01354CA7620 10064 NLG OUTER CYLINDER P/N 52101-1 S/N BA0027 IS CORRODED. CORROSION REPAIRED IAW BOMBARDIER REO 670-32-21-062 AND GOODRICH SCR 0008-04 REV C. 2L72 4F RTA21EA 20050808000392005080800039NM 2005 8 8 DL73S050393 120050722A3397 WIRE BOEING737 737232 1384475NM SEATS 12-13 DEF BROKEN A DALAK NONE L NO TEST ININSP/MAINT 1 SO27332DL 23104 SEAT MOUNTED EMERGENCY PATH LIGHTS INOP FROM ROW 2 THRU 14. REPLACED FUSES IN SEAT TRACK POWER SUPPLY AND REPAIRED WIRING IN RT SEAT TRACK BETWEEN 12-13 DEF. 2L72 4F RTA16WE 20050808000422005080800042 2005 8 8 DLM88050396 420050723A25655940163505 LANYARD DOUG MD88 MD88 3023688NM TAILCONE SLIDE STRETCHED A DALAO OTHER O OTHER TXTAXI/GRND HDL 1 SO27913DL 49544 OPS AGENT WALKED DOWN THE CATWALK AND MISTAKENLY PULLED THE RED DEPLOY HANDLE FOR TAILCONE AND SLIDE DEPLOYMENT. THE TAILCONE RELEASED BUT DID NOT FULLY DROP. IT WAS STILL HANGING ABOUT A FT ABOVE THE GND BY THE KEVLAR CABLE. THE SLIDE NEVER DEPLOYED. REINSTALLED TAILCONE AND REPLACED STRETCHED LANYARD. 2L72 4F RTA6WE 20050808000432005080800043NM 2005 8 8 DL75K050398 120050722A2120 ODOR BOEING757 757232 1384965NM CABIN DETECTED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO276706Q 30422 DURING CRUISE, FA ADVISED OF ELECTRICAL SMELL IN FWD GALLEY. CONTRACT MTC THOROUGHLY INSPECTED AIRCRAFT AND RAN PACKS. 2L72 4F RTA2NM 20050808000452005080800045NM 2005 8 8 DLM88050400 120050723A3610 BOOT DOUG MD88 MD88 3023688NM TAIL FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27912DE 49997 TAIL COMPT HIGH TEMP MSG ON CLIMB-OUT. REPLACED FAILED BOOT ON MIX MANIFOLD. 2L72 4F RTA6WE 20050808000462005080800046 2005 8 8 DLM90050401 420050723A2397AFA3520360 CABLE DOUG MD90 MD9030 3023690NM SEAT FRAYED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27902DA 53382 SEAT CABLE SPARKING AT SEAT LEG. FOUND CABLE FRAYED. REPLACED SAME. 2L72 4F RTA6WE 20050808000482005080800048NE 2005 8 8 DL75K050403 220050726A7200PW2037RTC ENGINE BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 1 MAKING METAL A DALAC ABORTED TAKEOFF A FLAME/FIRE TOTAKEOFF 1 SO27650DL18580 24390 728734 LEFT ENGINE FAILED ON TAKEOFF ROLL, ABORTED T/O. REPLACED ENGINE. 2L72 4F4 FRTA2NM E17NE 20050808000502005080800050NM 2005 8 8 DL73G050406 120050726A324026066724 BRAKE BOEING737 7373L9 1384470NM NR 4 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27231DN 23717 ON TRANSIT CHECK, FOUND METAL SHARDS UNDERNEATH NR 4 BRAKE ASSY, SHARDS ARE FROM OUTER DISK. REPLACED NBR 4 MAIN BRAKE ASSY PER MM. 2L72 4F RTA16WE 20050808000512005080800051NM 2005 8 8 DLM88050407 120050727A3260R2295 RELAY DOUG MD88 MD88 3023688NM MLG FAILED A DALAO OTHER J WARNING INDICATION APAPPROACH 1 SO27919DL 49584 UPON LANDING GEAR EXTENSION, ALL GEAR NORMAL, BUT COULD NOT EXTINGUISH THE GEAR HORN AT FLAPS 28 AND 40. REPLACED R2-295 RELAY. 2L72 4F RTA6WE 20050808000522005080800052NM 2005 8 8 DL76L050408 120050726A3397 WIRE HARNESS BOEING767 767332 1382001NM SEAT ASSY DAMAGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27180DN 25985 32F AND G PAX SEAT EMERGENCY LIGHT INOP. REPLACED SEAT EMER LIGHT HARNESS. 2L72 4F RTA1NM 20050808000542005080800054NM 2005 8 8 DL738050410 120050721A3350 POWER SUPPLY BOEING737 737832 13844CFNM EMERERNCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27391DA 30560 EMERGENCY ESCAPE LIGHT ABOVE SEAT 10D INOP. REPLACED POWER SUPPLY FUSE. LIGHT OP CKS GOOD. 2L72 4F RTA16WE 20050808000562005080800056NM 2005 8 8 DLM88050412 120050728A2910 TUBE DOUG MD88 MD88 3023688NM HYD SYSTEM LEAKING A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27965DL 49984 LEFT AFT LAV SMOKE DETECTOR ACTIVATED WITH SLIGHT ODOR PRESENT. REPAIRED HYDRAULIC LINE AT LEFT THRUST REVERSER CONTROL VALVE. PERFORMED DUCT BURNOUT PROCEDURE. CHECKS GOOD. 2L72 4F RTA6WE 20050808000572005080800057 2005 8 8 DL76G050413 420050729A3410856LU5 PROBE BOEING767 767332 1382001NM LEFT FAILED A DALAA UNSCHED LANDING I FLT. ATTITUDE INST. CRCRUISE 1 SO271603 29695 CAPT PROBE LIGHT ILLUMINATED IN FLT FOLLOWED BY UNRELIABLE AIRSPEED, SELECTED ALT AIR DATA ALL OK. HOWEVER, HAD TO FLYNO-RVSM AND DID HAVE ENOUGH FUEL TO CONTINUE. REPLACED LEFT PROBE. 2L72 4F RTA1NM 20050808000592005080800059NM 2005 8 8 DL76K050417 120050730A2781 TARGET BOEING767 767332 1382001NM NR 10 SLAT OUT OF POSITION A DALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27178DZ 30596 LE EDGE SLAT ASSYMETRY BETWEEN 1 AND UP. FOUND NO 10 SLAT INBOARD TARGET OUT OF PROX. ADDED SHIM TO SWITCH PER AMM TO S302. RECHECKED BIT ON PSEU. ALL CHKS GOOD. 2L72 4F RTA1NM 20050808000612005080800061NM 2005 8 8 DL76S050419 120050730A1430 BOLT BOEING767 767332 1382001NM GE CF6 CF680A 30025NE NR 2 ENGINE LOOSE A DALAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 SO27130DL 24080 580255 RT ENG FIRE IND INTERMIT DURING CLM. S/D ENG AND ATB TO ATL.C/A FOUND 4 BOLTS LOOSE ON HPT NOZZLE COOLING DUCTS AT HPC CASE 230 AND 330 POSITION. TIGHTENED SAME. REINSTALLED RMVD LOOPS. CKD SECURITY OF ALL LOOPS. RAN ENG AT 90 PCT FOR 5 MIN AND 103 PCT FRO 5 MIN. ALL CKS GOOD. 2L72 4F4 FRTA1NM E13NE 20050808000622005080800062 2005 8 8 DL76S050420 420050731A23307001117009 PROJECTOR BOEING767 767332 1382001NM CABIN ODOR A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27130DL 24080 FLT 683 ATL - MBJ DIVERSION TO MCO, STRONG ODOR MID CABIN. ELECTRICAL SMELL. FOUND MID CABIN MOVIE PROJECTOR SOURCE OF SMELL. REPLACED PROJECTOR. ALL CKS OK. NO FURTHER SMELL NOTED. 2L72 4F RTA1NM 20050808000682005080800068NM 2005 8 8 DL75K050427 120050804A2910AS11508K0322 LINE BOEING757 757232 1384965NM LT HYD SYSTEM LEAKING A DALAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SO27650DL 24390 COMPLETE LOSS OF LEFT HYD SYSTEM AFTER CONFIGURING FOR LANDING IN BDL. DECLARED EMERGENCY. LANDED UNEVENTFULLY. WAS TOWED TO GATE DUE TO LOSS OF NOSE WHEEL STEERING. FOUND HYD LINE TO NOSE WHEEL STEERING LEAKING AT COUPLING. INSTALLED APPROVED HYD LINE, LEAK CKS GOOD. 2L72 4F RTA2NM 20050808000712005080800071NM 2005 8 8 UPS05445048 120050725A5315 FLOORBEAM BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 BS 380 LBL 30-40 FLOORBEAM FOUND CORROSION. CORROSION BLEND OUT 0.045 BY 1 BY 2.5 EXCEED SRM 53-10-01 FIG 1 LIMITS, U/D BS 380 LBL 24 TO LT O/B END FLOORBEAM REPAIRED AS PER SRM 53-10-07 FIG 10. 2L74 4F A20WE 20050808000722005080800072WP 2005 8 8 UPS05845005 120050711A5230 FITTING DOUG DC8 DC873F 302199FWP CARGO DOOR CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C1, MAIN CARGO DOOR JAMB AFT LATCH SPOOL FITTING FWD ANGLE HAS INTERGRANULAR CORROSION. REMOVED AND REPLACED MCD LATCH SPOOL FITTING IAW 51-3-0, 51-3-2, 51-1-21, AND 51-3-1. 2L74 4F RT4A25 20050808000742005080800074WP 2005 8 8 UPS05845049 120050710A5340SAA3779498501 ATTACH ANGLE DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 LT CENTER MAIN CABIN STA 857.125 L19L INBD INTERCOSTAL ATTACH ANGLE CRACKED .500" LONG BETWEEN FASTENERS AT FRAME IN RADIUS. REMOVED ATTACH ANGLE, FABRICATED AND INSTALLED IAW SRM 51-1-20D AND DWG 3779498. 2L74 4F RT4A25 20050808000752005080800075WP 2005 8 8 UPS05845050 120050711A53403779659U501 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 LONGERON END FITTING CRACKED AT STA 902 L7L. REMOVED AND REPLACED LONGERON END FITTING IAW 51-1-20D, 51-1-21 AND 51-3-0. 2L74 4F RT4A25 20050808000762005080800076WP 2005 8 8 UPS05845051 120050707A53403779762U501 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 STA 675 L8L LONGERON SPLICE FITTING CRACKED. REMOVED AND REPLACED SPLICE FITTING IAW SRM 51-1-21,51-1-20D AND 51-1-23. 2L74 4F RT4A25 20050808000782005080800078WP 2005 8 8 UPS05845053 120050804A3350 BATTERY DOUG DC8 DC871 302199AWP EMERGENCY LIGHT MALFUNCTIONED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01715UP 45915 EMERG EXIT LIGHTS ARE SLOW TO DISARM WHEN ACTIVATED. REMOVED AND REPLACED EMERG BATTERY AND RELAY UNIT SYS OPS CHECK NORMAL PER MM 33-50-01-2 PARA 2,4 & 5. 2L74 4F 4A25 20050804000362005080400036WP 2005 8 4 UPS05845006 120050711A5310 FINGER DOUBLER DOUG DC8 DC873F 302199FWP SUB FLOOR CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 FINGER DOUBLER BLOWN OUT IN COCKPIT SUBFLOOR AT STA -67 TO -81. REMOVED FINGER DOUBLER AT STA -67 TO -81. FABRICATED FINGER DOUBLER AND INSTALLED IAW SRM 53-3-1, AND 51-1-21, 51-1-20D. 2L74 4F RT4A25 20050804000372005080400037WP 2005 8 4 UPS05845012 120050710A5312 BULKHEAD DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 RT AFT PRESS BULKHEAD FWD SIDE CRACKED HORIZONTALLY .375 LONG AT RBL 35 AT APPROX 55 INCHES ABOVE FLOOR LINE AT EXISTING REPAIR DOUBLER. CUT OUT DAMAGED AREA ON BULKHD IAW SRM53-2-5 FIG 14A. FABRICATED FILLER AND INSTALLED IAW SRM 53-2-5 FIG 14A, LOCATION OF CRACK ON FS 1766 PRESS BULKHD WITH EXISTING REPAIR DOUBLER IS IN COMPLIANCE WITH AFT PRESS BULKHD WEB CRACK REPAIR IAW SRM 53-2-5 FIG 14A SHEET 4. 2L74 4F RT4A25 20050804000432005080400043EA 2005 8 4 SWIA200515327 120050723A2751601R590141 DETECTOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07923SW 7664 'FLAPS DEGRADED' STATUS MSG. REPLACED SKEW DETECTOR UNIT IAW MM 27-51-15. OPERATIONAL CHECK GOOD, PN 601R59014-1 OFF A381. 2L72 4F RTA21EA 20050804000542005080400054NM 2005 8 4 SWAA052147 120050723A3350311500 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED C1 CHECK, FOUND 2 EMERGENCY BULLNOSE LIGHT LENSES LOOSE AT ROW 8 DEF AND ROW 16 ABC. SECURED BOTH LIGHT LENSES PER MM. 2L72 4F RTA16WE 20050804000822005080400082EU 2005 8 4 AWXA200500902 120050712A5315D5347217220290 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28627AW 66 SAL - DURING C4 CHECK DISCOVERED CORROSION ON FLOORBEAM LOCATED AT +Y1180 AND BETWEEN FR 66+4" AND FR 68-5". MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-14 FIG 102. MAINTENANCE REMOVED FLOORBEAM AT +Y1180 AND BETWEEN FR 66+4" AND FR 68-5" AND INSTALLED NEW FLOORBEAM IAW AIRBUS 320 SRM 51-42-11. 2L72 4F RTA28NM 20050804000942005080400094EA 2005 8 4 SWIA200515338 120050727A2750860D10018 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07416SW 7089 FLAPS HALFSPEED STATUS MSG IN FLIGHT. REPLACED FECU IAW CRJ 200 MM 27-50-00. OPERATIONAL CHECK GOOD, PN 860D100-18 SNOFF 251. 2L72 4F RTA21EA 20050804001002005080400100EA 2005 8 4 SWIA200515344 120050720A2740 SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07597SW 7293 STAB TRIM AND MACH TRIM CAUTION MESSAGES WILL NOT RESET. REPLACED FO'S STAB TRIM SWITCH IAW MM 27-41-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050804001032005080400103SO 2005 8 4 SWIA200515347 120050725A2797 WIRE EMB 120 EMB120ER 3260203SO TE FLAP HANDLE BROKEN A SWIAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 NM07295SW 120322 AFTER DEPARTURE AND MOVING FLAP HANDLE TO 0 RECIEVED A FLAP CONTROL FAULT. REPAIRED BROKEN WIRE AT LEFT OUTBOARD FLAP ACTUATOR. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050804001042005080400104SO 2005 8 4 SWIA200515348 120050724A27523203001007 ACTUATOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07268UE2 2 120207 FLAP CONTROL FAULT DURING EXTENSION. REPLACED LEFT OUTBOARD FLAP ACTUATOR IAW MM 27-50-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050804001072005080400107EA 2005 8 4 SWIA200515351 120050727A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07963SW 7865 LEFT AFT EXTERIOR EMERGENCY LIGHT INOP. REPLACED LEFT EXTERIOR EMERGENCY LIGHT BULB. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050804001112005080400111EA 2005 8 4 SWIA200515355 120050801A27507455001 LEVER CNDAIRCL600 CL6002B19 1900309EA FLAP CONTROL MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07919SW 7657 "FLAP FAIL" CAUTION MESSAGE. REPLACED FLAP SELECTOR LEVER IAW MM 27-50-00. OPERATIONAL CHECK GOOD, PN 7-45500-1, SN/OFF 764. 2L72 4F RTA21EA 20050804001152005080400115NM 2005 8 4 UPS05445009 120050723A5414 SKIN BOEING747 747121 1384871NM NR 2 PYLON DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 NR 2 PYLON NAC STA 240 LOWER EDGE O/B SIDE DOUBLER HOLE CHAFED REVEALED AS MARK. NR 2 PYLON NAC STA 240 LOWER EDGE REPAIRED AS PER SRM 54-30-03 FIG 36. 2L74 4F A20WE 20050805000322005080500032NM 2005 8 5 SWAA052178 120050724A3350MS155721 BULB BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29600WN 27694 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050805000372005080500037NM 2005 8 5 SWAA052170 120050722A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 934, STR 25L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050805000382005080500038NM 2005 8 5 SWAA052196 120050726A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29610WN 27696 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 767, BETWEEN LBL 3 & RBL 49. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050805000452005080500045NM 2005 8 5 SWAA052199 120050726A53116546550 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29610WN 27696 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 787, RBL 8. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050805000472005080500047 2005 8 5 SWAA052134 420050721A2565D31354 SLIDE BOEING737 7375H4 138449DNM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29527SW 26569 L1 DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20050805000492005080500049NM 2005 8 5 SWAA052136 120050721A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29315SW 23337 DURING SCHEDULED SERVICE CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS BETWEEN BS 740 AND BS 750, STR 18L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050805000622005080500062NM 2005 8 5 SWAA052299 120050801A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29315SW 23337 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 359, BETWEEN STR 5R & STR 6R. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050805000652005080500065 2005 8 5 SWAA052200 420050727A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050805000692005080500069 2005 8 5 SWAA052204 420050727A256565659723 BRACKET BOEING737 7373H4 1384600NM GIRT BAR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR FWD BRACKET LOOSE. SECURED BRACKET PER MM. 2L72 4F RTA16WE 20050805000932005080500093NM 2005 8 5 SWAA052291 120050802A57126545445 RIB BOEING737 7373H4 1384600NM LT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29610WN 27696 DURING SCHEDULED D-CHECK, FOUND LEFT WING LOWER RIB CHORD CRACKED AT WBL 135.5, BETWEEN STR 2 & STR 3. REPAIRED RIB PER SWA ACO. 2L72 4F RTA16WE 20050805001022005080500102NM 2005 8 5 SWAA052274 120050726A335065C34691 LIGHT BOEING737 7373H4 1384600NM ROW 1ABC BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29324SW 23414 FWD CABIN LEFT OVERHEAD BIN BULLNOSE LIGHT BROKEN AT ROW 1 ABC. REMOVED AND REPLACED LIGHT PER MM. 2L72 4F RTA16WE 20050805001032005080500103NM 2005 8 5 SWAA052275 120050801A335020121 BATTERY PACK BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29330SW 23694 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY INTERIOR & EXTERIOR LIGHTS INOP AT BOTH ENTRY DOORS. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050805001102005080500110NM 2005 8 5 SWAA052282 120050801A53306545765 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29691WN 23781 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 498, STR 16L. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050805001122005080500112NM 2005 8 5 05FDEA01430 120050524A5347AFA7789548 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25631FE 48454 AFT INTERMEDIATE FUSELAGE STA 1964 X = 107.25 RIGHT O/B EXISTING REPAIR ON CORRODED SEAT TRACK. DISCREPANT SEAT TRACK TRIM OUT AT STA 1831 RBL 107. NEW SEAT TRACK REPLACED FROM AFA 7789-542 AND CARRIED OUT REPAIR AS PER SRM 53-70-00 FIG 1 VOL I. NEW SEAT TRACK AND REPAIR PARTS LOCATED AND INSTALLED AS PER SRM 53-70-00 FIG 1 VOL I AND SRM 51-31-01 VOL II. CLASSIFIED MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050805001152005080500115NM 2005 8 5 05FDEA02217 120050803A5755 SKIN DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 RIGHT HAND WING UPPER SURFACE TRAILING EDGE FORWARD OF NR 2 SPOILER SKIN BULGE AT XORS 538.49 STRINGER 1. RT WING UPPER SURFACE TRAILING EDGE FORWARD OF NR 2 SPOILER XORS 538.49 STRINGER 1 SKIN BULGE AREA CORROSION REMOVED. MAT'L REMOVED: 0.035"; ORIG. THICKNESS: 0.310"; MAT'L REMAINED: 0.275"; FOUND EXCEED LIMIT AS PER SRM 57-10-00 FIG. 32 VOL.I. AREA REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-87562 - WINGS - RH UPPER WING SKIN - CORROSION REPAIRS AT XORS = 531 THRU XORS = 536 & XORS = 540. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6 -2-100. 2L73 4F RTA22WE 20050805001242005080500124WP 2005 8 5 05FDEA02180 120050802A5711 FRAME DOUG MD10 MD1010F 3022112WP RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25381FE 46615 ONE CRACK 0.5 INCH LONG ON FRAME SIDE RT WING AT STA XORS 623. REPAIRED CRACK IAW SRM 57-20-00 FIG 1 VOL 1. 2L73 4F RTA22WE 20050805001272005080500127EU 2005 8 5 05FDEA02168 120050802A5320 WEB AIRBUS300 A300F4605R 3930327EU MAIN DECK CARGO CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25671FE 778 AFT MAIN DECK REAR CARGO COMPT FR 79 WITH STR 26 WEB IS CRACKED. 2L72 4F RTA35EU 20050805001282005080500128EU 2005 8 5 05FDEA02169 120050802A5320 WEB AIRBUS300 A300F4605R 3930327EU MAIN DECK CARGO CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25671FE 778 AFT MAIN DECK REAR CARGO COMPT FR 79 WITH STR 26 WEB IS CRACKED. 2L72 4F RTA35EU 20050805001352005080500135CE 2005 8 5 CIEA200500013 120050803A32601CH25 DOWNLOCK SWITCH BEECH 200 B200 1152922CE RT MLG FAILED E CIEAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 NM03203LG707 86 BB926 DURING APPROACH, RT MAIN GEAR DID NOT INDICATE IT WAS DOWN AND LOCKED. DUE TO SERV AT DESTINATION AIRPORT, A/C RETURNED TO ORIG AIRPORT. PILOT CYCLED GEAR SEVERAL TIMES, UNABLE TO GET A DOWN AND LOCK IND ON RT MAIN GEAR. PILOT DID A MANUAL EXTENSION OF GEAR AND RT GEAR LIGHT CAME ON. A/CT LANDED W/O INCIDENT. A/C WAS THEN JACKED AND AFTER RESETTING MANUAL GEAR SYSTEM GEAR WAS CYCLED AND PROBLEM WAS DUPLICATED. RT MAIN GEAR DOWN AND LOCK SWITCH WAS FOUND TO BE INTERMITTENT. SWITCH WAS REPLACED AND SYS CHECKED GOOD. THE SWITCH WAS MANUFACTURED BY MICRO-SWITCH OUT OF FREEPORT, IL. THE SWITCH HAS TWO PART NUMBERS. RAYTHEON NUMBER IS 100-381006-1, MANUF P/N 1CH25. MFR CODE ON SWITCH IS 91929 0335. 1L72 4T A24CE 20050805001462005080500146NM 2005 8 5 SWAA052306 120050803A5315BAC15171489 FLOORBEAM BOEING737 7373Q8 1384670NM COCKPIT FLOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29317WN 24068 DURING SCHEDULED D CHECK, FOUND COCKPIT FLOORBEAM CORRODED AT BS 270, LBL 10 TO RBL 10, WL 208. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20050805001492005080500149NM 2005 8 5 SWAA052309 120050803A335010107451 LIGHT BOEING737 7373H4 1384600NM L1 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29397SW 27691 DURING SCHEDULED RON CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT PER MM. 2L72 4F RTA16WE 20050805001502005080500150NM 2005 8 5 SWAA052310 120050803A33506556633 LIGHT BOEING737 7377H4 1384404NM MID CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29400WN 27891 LT OVERWING EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT PER MM. 2L72 4F RTA16WE 20050805001552005080500155 2005 8 5 SWAA052315 420050803A25656557463 FITTING BOEING737 7373G7 1384595NM GIRT BAR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29691WN 23781 DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FLOOR FITTING LOOSE. SECURED FITTING PER MM. 2L72 4F RTA16WE 20050805001562005080500156NM 2005 8 5 DL76L050378 120050719A2510 SWITCH BOEING767 767332 1382001NM COCKPIT SEAT SHORTED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27180DN 25985 F/O SEAT CAUSING BURNING ODOR. FOUND SWITCH FOR HORIZONTAL POWER ADJUSTMENT MAKING CONTACT AT ALL TIMES AND CAUSING DRIVE MOTOR TO BURN. REPLACED SEAT ASSY. 2L72 4F RTA1NM 20050808000182005080800018EA 2005 8 8 COMA0560418 120050729A32347455025 SELECTOR SWITCH CNDAIRCL600 CL6002B19 1900309EA MLG MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01471CA8956 7655 FLIGHT 5026 - WHEN LANDING GEAR SELECTED UP, ANTI-SKID AND PARKING BRAKE CAUTION. GEAR DID NOT RETRACT. REPLACED THE LANDING GEAR SELECTOR SWITCH. 2L72 4F RTA21EA 20050808000192005080800019EU 2005 8 8 MALA050628 120050801A5311 FRAME SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15452XJ 340B452 DURING 4K CHECK IN BNA, FOUND LOWER FUSELAGE AND FRAME AT FS 686.888 JUST TO THE LEFT OF BL 0 IS DENTED, DAMAGE IS ACCEPTABLE IAW MESABA EO S53307. REF: EAMS WORK ORDER 212637 TASK 1546. 2L72 4T RTA52EU 20050808000202005080800020EU 2005 8 8 MALA050629 120050804A3350 POWER SUPPLY SAAB SF340 340B 7860101EU EMERGENCY LIGHTSFAILED A MALAK NONE O OTHER ININSP/MAINT 1 GL15452XJ 340B452 DURING 4K CHECK IN BNA, FOUND EMERGENCY POWER SUPPLY 21LN FAILED CAUSING RT AND LT HORIZONTAL SIDEWALL LIGHTS AND THE VERY FIRST FLOOR PROXIMITY ESCAPE PATH LIGHT 41LN NOT TO ILLUMINATE. REF: EAMS WO NR 212638 TASK 1508. 2L72 4T RTA52EU 20050808000222005080800022 2005 8 8 SA05058 420050801A2565130104233 SLIDE BOEING757 7572B7 1384964NM RT OFF WING READS LOW A USAAK NONE O OTHER ININSP/MAINT 1 EA19653US16317975 24894 PHL - RIGHT OFF THE WING SLIDE PRESSURE WAS FOUND LOW. MAINTENANCE REPLACED THE RIGHT WING SLIDE BOTTLE. OK FOR SERVICE. 2L72 4F RTA2NM 20050808000242005080800024NM 2005 8 8 USAA200508001 120050729A52306547952524M SKIN BOEING737 7373B7 1384580NM CARGO DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19504AU 23379 1/2" CRACK AT AFT CARGO DOOR LOWER FWD CORNER OF OUTER SKIN, REPAIR: INSTALLED FILLER, DOUBLER, TRIPLER PER EA 96770. 2L72 4F RTA16WE 20050808000352005080800035EA 2005 8 8 COMA057088 120050729A5313 STRINGER CNDAIRCL600 CL6002C10 1390015EA FUSELAGE DENTED A COMAK NONE O OTHER ININSP/MAINT 1 SO01354CA 10064 AFT RT FUSE AT FS1057 STR 14R-15R HAS 2.6L X 1.6W X .040D DENT. TRIMMED OUT DAMAGED AREA, LPI OR EDDY CURRENT TO ENSURE NO CRACKS EXIST. FABRICATE AND INSTALL DOUBLER (2024-T3 .063) IAW BRAS EO 601R-53-6952. 2L72 4F RTA21EA 20050808000472005080800047NM 2005 8 8 DLM88050402 120050724A3397 WIRE DOUG MD88 MD88 3023688NM CABIN FLOOR BROKEN A DALAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO27935DL 49722 DURING TAXI OUT AND WHILE ON TAXIWAY PASSENGER AT SEAT ROW 28 NOTICED LOOSE WIRING UNDER SEAT ROW 27. AIRCRAFT RETURNED TO RAMP AREA AND MTC DISCOVERED EMERG TRACK LIGHTING WIRE PULLED AWAY FROM SIDEWALL WITH ONE WIRE BROKEN. MADE APPROVED REPAIR TO WIRING AND SECURED SAME BEHIND SIDEWALL. EMERG TRACK LIGHTING OPERATES NORMALLY THROUGHOUT CABIN. 2L72 4F RTA6WE 20050808000492005080800049NM 2005 8 8 DL76L050404 120050726A2530811150417 COFFEEMAKER BOEING767 767332 1382001NM GALLEY SMOKE A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27190DN 28447 JUMPSEAT 4L COFFEE MAKER CB POPPED WITH SMOKE FROM COFFEEMAKER. REPLACED MAKER. CKS OK. MCO REMOVED, CKD WIRING FOR SHORTING/DAMAGE, NO TROUBLE FOUND. 2L72 4F RTA1NM 20050808000532005080800053NM 2005 8 8 DL76L050409 120050726A3350 BULB BOEING767 767332 1382001NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27183DN 27110 EMERGENCY LIGHT INOP LOCATED LT FUSELAGE AFT OF T/E OF LT WING, RELAMPED. 2L72 4F RTA1NM 20050808000582005080800058NM 2005 8 8 DLM88050415 120050729A2120 ODOR DOUG MD88 MD88 3023688NM CABIN DETECTED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO27929DL 49716 ELECTRICAL BURNING POPCORN ODOR ON APPROACH INTO ATL. AFT GALLEY. INSPECTED AIRCRAFT AND RAN PACKS, PERFORMED DUCT BURNOUT. 2L72 4F RTA6WE 20050808000642005080800064NM 2005 8 8 DL757050422 120050731A2150211080107 ACM BOEING757 757232 1384965NM LEFT SEIZED A DALAC ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SO27679DA 26955 LEFT PACK RUNNING HOT AND MAKING SMELL, REPLACED SEIZED ACM. 2L72 4F RTA2NM 20050808000662005080800066NM 2005 8 8 DL76L050425 120050731A2530811150417 COFFEEMAKER BOEING767 767332 1382001NM FWD GALLEY SPARKS A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27174DN 24802 FWD GALLEY COFFEE MKR INOP/SPARKING, REPLACED SAME. 2L72 4F RTA1NM 20050808000672005080800067NM 2005 8 8 DL76L050426 120050804A324226124121A BRAKE BOEING767 76733AER 1385230NM NR 2 MLG LEAKING A DALAO OTHER A FLAME/FIRE TXTAXI/GRND HDL 1 SO27180DN 25985 LEFT BRAKE REPORTED SMOKING BY RAMP ON ARRIVAL. FOUND NR 2 BRAKE LEAKING AT LOWER PISTON CAUSING BRAKE FIRE. FLT DECK BRAKE TEMP INDICATES 4. REPLACED NR 2 MAIN BRAKE AND WHEEL ASSY PER MM. PERFORMED HEAT DAMAGE INSP PER MM 05-51- 14 PAGE 201. NO FURTHER MAINTENANCE ACTION REQUIRED. 2L72 4F RTA1NM 20050808000692005080800069NM 2005 8 8 DL73S050428 120050804A3350 FUSE BOEING737 737232 1384475NM SEAT ROW 25 BLOWN A DALAK NONE L NO TEST ININSP/MAINT 1 SO27310DA 23082 PASSENGER SEAT 25C AND 25D EMERGENCY TRACK LIGHTING INOP. REMOVED AND REPLACED FUSES IN BATTERY PACK CRADLE. OPS CK OK. 2L72 4F RTA16WE 20050808000792005080800079WP 2005 8 8 UPS05845054 120050628A5340SAA47504201 FITTING DOUG DC8 DC873F 302199FWP FUSLEAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 MAIN CABIN INTERIOR LT SIDE FS 860 AFT SIDE L18L ATTACH FITTING CRACKED. REMOVED AND REPLACED ATTACH FITTING IAW SRM 51-1-20D. 2L74 4F RT4A25 20050808000802005080800080WP 2005 8 8 UPS05845055 120050625A53405641006501 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 STA 759 BOOT FITTING CRACKED BETWEEN L17L AND L18L. REPAIRED BOOT FITTING IAW UPS EO DC8-53-2048 AND SAA SK 851-856307. 2L74 4F RT4A25 20050808000852005080800085NE 2005 8 8 AALA20050488 220050730A7310 O-RING BOEING757 757223 1384957NM RROYCERB211 RB211535E4 54555NE ZONE 500 LEAKING A AALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW21675AN 29425 31016 LEFT ENGINE BEGAN TO USE FUEL AT INCREASED RATE. LANDED JAX WITHOUT INCIDENT. FOUND LEFT HAND FUEL LEAKING FROM FUEL CONTROL SUPPLY LINE. REPLACED O-RING ON FUEL CONTROL SUPPLY LINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA2NM E12EU 20050808000862005080800086WP 2005 8 8 AALA20050490 120050730A4990 OIL TANK DOUG DC9 DC982 3022082WP APU LEAKING A AALAA UNSCHED LANDING KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SW21244AA 49256 RIGHT AIR CONDITION SUPPLY TEMPERATURE HIGH. CAUTION LIGHT ON TAKEOFF. FLIGHT ATTENDANT REPORTED BLUE COLOR SMOKE IN CABIN. TURNED OFF RIGHT PACK. LANDED SAT WITHOUT INCIDENT. FOUND OIL LEAK IN APU OIL TANK WITH APU OPERATING. REPLACED APU DUE TO OIL LEAK AND OIL INGESTION. REPLACED RIGHT AIR CONDITION SUPPLY TEMPERATURE SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050808000882005080800088NE 2005 8 8 AALA20050489 220050730A7261 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE RIGHT LEAKING A AALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW21465A 49595 718530 RIGHT ENGINE OIL QUANTITY WENT TO ZERO. RIGHT OIL PRESSURE STARTED SOEN TO 20 PSI. STAYED AT 20 PSI FOR ONE TO TWO MINUTES THEN WENT TO ZERO. OIL TEMPERATURE WAS NORMAL THE ENTIRE TIME. SHUT DOWN ENGINE PER CHECKLIST. REPLACED RIGHT HAND ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 F A6WE E9NE 20050808000902005080800090NM 2005 8 8 BB05060 120050803A335020131A BATTERY BOEING757 757225 1384959NM PASSENGER CABIN DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19606AU 22202 BOS - THE FORWARD, LEFT SECTION OF EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE BATTERY, M731. OPERATIONALLY CHECKS OK. 2L72 4F RTA2NM 20050808000932005080800093EU 2005 8 8 05FDEA02225 120050802A2170 COALESCER BAG AIRBUS310 A310 EU CONTAMINATED A FDEAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SO25409FE 273 ON TAXI OUT MEM, SMELLED A STRONG SMELL THEN A FULL MAIN DECK SMOKE WARNING WHICH LASTED FOR SEVERAL MINUTES. DECLARED EMERGENCY. DETECTION CLEARED ITSELF. RETURNED TO GATE. REPLACED NR 1 AND 2 PACK WATER SEPARATOR BAGS AS PRECAUTIONARY REF A310 AMM 21-51-16-3. BAGS DID NOT APPEAR VERY DIRTY. CLOSED ALL A/C DOORS AND RAN BOTH NR 1 AND 2 ENG AT IDLE FOR ABOUT 10 MINS WITH APU BLEED ISOLATED AND BOTH PACKS RUNNING. THERE WAS A STRONG ODOR THAT WAS NOTICED ALMOST INSTANTLY WHEN PACKS TURNED ON. RAN ENGINES AT HIGH POWER FOR EXTENDED PERIOD RAN PACKS AT SEVERAL DIFFERENT SETTINGS FROM HOT TO COLD ALL INDICATIONS NORMAL, NO ODOR OR SMOKE WAS NOTICED IN FLT DECK OR ON MAIN DECK OF AC. 2L72 4F RTA35EU 20050808000942005080800094NE 2005 8 8 05FDEA02226 220050803A7200CF680C2A5F POWERPLANT AIRBUS300 A300F4605R 3930327EU GE CF6 CF680 30025NE FLANGE CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25671FE12658 778 705241 W/O 29493, NR N00177, ENGINE NR 1 AT FORWARD INBOARD LOWER HOIST POINT, THE FLANGE IS CRACKED AT IT'S BASE. FPI IAWM NTM 51-91-00 CRACK IS CONTAINED BY STOP DRILL. SWAB ETCHED DAMAGED AREA IAW TASK 70-24-01-110-34 PER GESPM STOP DRILL ACCEPTABLE PER EA 6-7223-82106 AND PER AMM 72-23-00-8-F REMOVED AND REPLACED HOIST BRKTS IAW GE MM 72-23-01 2L72 4F4 FRTA35EU E13NE 20050808000952005080800095NE 2005 8 8 05FDEA02227 220050803A7200 GE CF680 AIRBUS300 A300F4605R 3930327EU GE CF6 CF680 30025NE A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25671FE 705241 778 705241 NR 1 ENG FAN CASE HAS 2 PREVIOUSLY STOP DRILLED CRACK ON AFT DOLLY MOUNT AT APPROX 8 O'CLOCK POSITION. FPI IAW NTM 51-91-00 CRACK CONTAINED BY STOP DRILL. SWAB ETCHED DAMAGED AREA IAW TASK 70-24-01-110-34 OF SPM. STOP DRILLS ACCEPTABLE PER EA 6-7223-82106-NRS00008 AND PER AMM 72-23-00-8-F REMOVED AND REPLACED HANDLING HOIST BRACKETS IAW MM 72-23-01. 2L72 4F4 FRTA35EU E13NE 20050808000962005080800096NE 2005 8 8 05FDEA02228 220050803A7200 GE AIRBUS300 A300F4605R 3930327EU GE CF6 CF680 30025NE A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25671FE 705241 778 705241 NR 1 ENG FAN CASE HAS 2 PREVIOUSLY STOP DRILLED CRACKS ON FWD DOLLY MOUNTS AT APPROX 8 O'CLOCK. FPI IAW NTM 51-91-00 CRACK IS CONTAINED BY STOP DRILL. SWAB ETCHED DAMAGED AREA IAW TASK 70-24-01-110-34 SPM. STOP DRILL ACCEPTABLE PER EA 6-7223-82106 AND PER AMM 72-23-00-8-F. REMOVED AND REPLACED HOIST BRACKETS IAW GE MM 72-23-01. 2L72 4F4 FRTA35EU E13NE 20050808000982005080800098NM 2005 8 8 05FDEA02230 120050803A5230 SILL BOEING727 727227 1384078NM CARGO DOOR CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 NR 2 LOWER CARGO DOOR, CORROSION AROUND NUTPLATES STA 950E-990 ON PRESSURE SEAL SILL. REPAIRED PER EA 7-5310-91351. 2L73 4F A3WE 20050808001012005080800101NM 2005 8 8 QXEA200501149 120050804A2750756158 TORQUE SENSOR DHAV DHC8 DHC8202 2809007NM MALFUNCTIONED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09352PH18236 494 SEA FLIGHT NR 2078 - RECEIVED FLAP DRIVE CAUTION LIGHT WHEN SELECTING FLAPS TO 5 DEGREES ON AFTER START PRIOR TO TAXI. MAINTENANCE REPLACED TORQUE SENSOR UNIT IAW DHC-8-200 AMM TASK 27-52-51-000-801 AND 27-52-51-400-801. FUNCTIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050808001182005080800118EA 2005 8 8 VNAA0507021 120050725A2150GG670950093 ACM CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE RIGHT FAILED A VNAAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL05706PS2753 10150 WHEN THE CREW ATTEMPTED A CROSS BLEED START ON THE NR 1 ENGINE, THE SMOKE AFT LAV WARNING MESSAGE ILLUMINATED AND A FLIGHT ATTENDANT REPORTED FUMES FROM FLOOR VENTS. THE CREW DECLARED AN EMERGENCY AND EVACUATED THE AIRCRAFT. MAINTENANCE FOUND THE RT AIR CYCLE MACHINE TURBINE SEIZED. THE ACM WAS REMOVED & REPLACED IAW CRJ700 AMM 21-51-08-400-801-A01. OPERATIONAL AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050808001192005080800119EA 2005 8 8 VNAA0507019 120050726A29136619003 PUMP CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE HYD SYSTEM FAILED A VNAAO OTHER O OTHER NRNOT REPORTED 1 GL05725PS1348 10186 THE CREW REPORTED A HYD EDP 2A CAUTION MESSAGE EN ROUTE TO DTW. MAINTENANCE REMOVED AND REPLACED THE RT ENGINE DRIVEN HYDRAULIC PUMP IAW CRJ700 AMM 29-11-01-000-801-A01 & 29-11-01-400-801-A01. OPERATIONAL AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050808001212005080800121EU 2005 8 8 05FDEA02243 120050804A2550 BEARING AIRBUS300 A300B4605R 3930308EU CARGO FLOOR PNL DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25671FE 778 MCD FLOOR PNL 232FG HAS BALL BEARING DAMAGE. 2L72 4F RTA35EU 20050808001222005080800122EU 2005 8 8 05FDEA02244 120050804A5321 FLOOR PANEL AIRBUS300 A300B4605R 3930308EU MDC DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25671FE 778 MDC FLOOR PNL 232TG DAMAGED. 2L72 4F RTA35EU 20050808001232005080800123EU 2005 8 8 05FDEA02245 120050804A5321 FLOOR PANEL AIRBUS300 A300F4605R 3930327EU MDC DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25671FE 778 MDC FLOOR PNL 231FG DAMAGE. 2L72 4F RTA35EU 20050808001252005080800125EU 2005 8 8 05FDEA02234 120050803A5411 SPAR AIRBUS300 A300F4605R 3930327EU NR 1 PYLON CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25656FE 745 NR 1 PYLON INSIDE PNL 411CL UPPER SPAR WEB HAS CRACK. 2L72 4F RTA35EU 20050808001292005080800129NM 2005 8 8 05FDEA02238 120050803A5755651928061 DEPRESSOR BOEING727 727200 138407ENM NR 5 SPOILER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 LEFT WING UPPER T/E ACCESS PANEL SUPPORT PLATE O/B OF NR 5 SPOILER IS CRACKED. REMOVED AND REPLACED PLATE IAW SRM 51-30-2. 2L73 4F RTA3WE 20050808001332005080800133EU 2005 8 8 05FDEA02251 120050804A5321 FLOOR PANEL AIRBUS300 A300B4605R 3930308EU MDC CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25670FE 777 MDC FLOOR PNL 252AH CRACKED. 2L72 4F RTA35EU 20050808001352005080800135EU 2005 8 8 05FDEA02246 120050804A5321 FLOOR PANEL AIRBUS300 A300B4605R 3930308EU MDC DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25671FE 778 MDC FLOOR PNL 232FF IS DAMAGED. 2L72 4F RTA35EU 20050808001362005080800136NM 2005 8 8 05FDEA02272 120050805A5720 WEB DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25624FE 48443 LEFT WING L/E CRACK LONG 2 INCHES ON INTERNAL WEB AT STA XORS 525. REPAIR IAW SRM 57-10-00 FIG 25 VOL I. 2L73 4F RTA22WE 20050808001372005080800137NM 2005 8 8 05FDEA02274 120050805A5730 ACCESS PANEL DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25624FE 48443 ACCESS PANEL ON RIGHT WING FOUND CRACK 1 INCH LONG ON L/E AT STA XORS 455. REPAIRED DOUBLER IAW SRM 57-10-00 FIG 18 VOL I. 2L73 4F RTA22WE 20050808001382005080800138NM 2005 8 8 05FDEA02275 120050805A5710 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25624FE 48443 ON LEFT WING FOUND CRACK 1 INCH ON L/E AT STA XORS 455. REPAIR IAW SRM 57-10-00 FIG 18 VOL I. 2L73 4F RTA22WE 20050808001402005080800140EU 2005 8 8 05FDEA02239 120050804A5321 FLOOR PANEL AIRBUS300 A300F4605R 3930327EU MAIN DECK CARGO CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25671FE 778 MAIN CARGO COMPT FLOOR PANEL 242EK IS CRACKED AT SEAT TRACK ATTACH POINT. 2L72 4F RTA35EU 20050808001412005080800141EU 2005 8 8 05FDEA02240 120050804A5321 FLOOR PANEL AIRBUS300 A300F4605R 3930327EU MCD CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25671FE 778 MAIN CARGO COMPT FLOOR PNL 262ZF IS CRACKED AT ATTACH POINT. 2L72 4F RTA35EU 20050808001452005080800145EU 2005 8 8 05FDEA02253 120050804A5321 FLOOR PANEL AIRBUS300 A300B4605R 3930308EU MDC DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25670FE 777 MDC FLOOR PNL 231BH DELAMINATED. 2L72 4F RTA35EU 20050808001492005080800149NM 2005 8 8 05FDEA02257 120050804A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 UPPER CARGO SEAT TRACK LBL 11 CRACKED AT STA 633. UPPER CARGO SEAT TRACK LBL 11 AT STA 633 CARRIED OUT REPAIR AS PER SRM 53-70- 00 VOLUME I FIGURE 1. REPAIR IS CLASSIFIED MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050808001502005080800150SO 2005 8 8 RAIA00508002 120050802A324631551 WHEEL EMB 145 EMB145LR 3260212SO MLG FAILED A RAIAO OTHER E VIBRATION/BUFFET CLCLIMB 1 CE03835HK 145670 LOUD NOISE AND VIBRATION FROM NOSE TIRE AREA AFTER LIFTOFF. MAINTENANCE FOUND LEFT NLG WHEEL BEARING FAILURE. REMOVED WHEEL AND TIRE. REMOVED NOSE STRUT DUE TO AXEL DAMAGE. 2L72 4T RTT00011AT 20050808001522005080800152EU 2005 8 8 RAIA00508004 120050803A3260AIR135704 DOWNLOCK SWITCH JETAIRJETSTMJETSTM4101 1500501EU MLG INOPERATIVE A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03561HK 41077 FLT 5393 - STL - TAKEOFF CONFIGURATION WARNING INDICATION WITH LOSS OF TAT AND TCAS. MAINTENANCE REMOVED AND REPLACED NLG DOWN LOCK SWITCH. 2L72 4T RTA41NM 20050808001532005080800153NM 2005 8 8 05FDEA02258 120050804A5347 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 UPPER CARGO SEAT TRACK RBL 47 CRACKED AT STA 1309. REPAIRED AS PER SRM 53-700-00. 2L73 4F RTA22WE 20050808001542005080800154NM 2005 8 8 05FDEA02259 120050804A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 UPPER CARGO SEAT TRACK LBL 11 CORRODED AT STA 1791. CORROSION REMOVED AS PER SRM 51-21-01. 2L73 4F RTA22WE 20050808001582005080800158NM 2005 8 8 05FDEA02263 120050804A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 MAIN DECK CARGO COMPARTMENT, FLOOR SEAT TRACK AT STA 635, X= 27 FOUND CRACKED APPROXIMATELY 3 INCHES LONG. REMOVED AND REPAIR SEAT TRACK AND SPLICES FABRICATED. HFEC INSPECTION CARRIED OUT AS PER NDT SPM 06-10-01-001. FOUND NO CRACKED. REPAIR PARTS TREATED. SEAT TRACK AND SPLICES INSTALLED. 2L73 4F RTA22WE 20050808001592005080800159NM 2005 8 8 05FDEA02264 120050805A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 UPPER CARGO SEAT TRACK RBL 47 CORRODED AT STATION 1441. CARRIED OUT REPAIR AS PER SRM 53-70-00. 2L73 4F RTA22WE 20050808001602005080800160NM 2005 8 8 05FDEA02265 120050805A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 UPPER CARGO SEAT TRACK RBL 47 CRACKED AT STATION 6-20. UPPER CARGO SEAT TRACK RBL 47 CRACKED AT STATION 6-20 REPAIRED AS PER SRM 53- 70-00 FIGURE 1 VOLUME I. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100. 2L73 4F RTA22WE 20050808001622005080800162WP 2005 8 8 05FDEA02267 120050805A5420AUB75647 WEB DOUG MD10 MD1010F 3022112WP ZONE 400 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25381FE 46615 CRACK 1.5 INCH ON PYLON NR 1 UPPER VERTICAL WEB AT STA YN268. REPAIR IAW 54-00-01 FIG 3 VOL I. 2L73 4F RTA22WE 20050808001632005080800163NM 2005 8 8 05FDEA02268 120050805A5420AUB75647 WEB DOUG MD11 MD11 3023602NM ZONE 400 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25624FE 48443 CRACK 1.5 INCH PYLON NR 1 UPPER VERTICAL WEB AT STA YN268. REPAIR IAW 54-00-01 FIG 3 VOL I. 2L73 4F RTA22WE 20050808001642005080800164WP 2005 8 8 05FDEA02201 120050802A5710 STRUCTURE DOUG MD10 MD1010F 3022112WP LT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25381FE 46615 WING LT LOWER SIDE AT XORS=391 TO XORS=433 OLD REPAIR QTY 3 EACH DOUBLER. ACCOMPLISH FEDEX EA 8-5710-84114. 2L73 4F RTA22WE 20050808001652005080800165WP 2005 8 8 05FDEA02202 120050802A5710 STRUCTURE DOUG MD10 MD1010F 3022112WP RT WING UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25381FE 46615 RIGHT WING TIP AT STA YW=756 LOWER SURFACE FOUND DOUBLER REPAIR. REMOVED REPAIRED WING TIP IAW AMM 57-23-01-2 DWG ARB2208 ARB2209 AND SRM 51-30-00. 2L73 4F RTA22WE 20050808001672005080800167NM 2005 8 8 05FDEA02269 120050805A5730 DOUBLER DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25624FE 48443 RIGHT WING L/E NR 7 CRACKS ON INTERNAL DOUBLER AT STA XORS 552. REPAIR IAW SRM 57-10-00 FIG 25 VOL I. 2L73 4F RTA22WE 20050808001682005080800168NM 2005 8 8 05FDEA02270 120050805A5720 SPLICE DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25624FE 48443 RIGHT WING L/E CRACK .5 INCH LONG ON INTERNAL HORIZONTAL SPLICE AT STA XORS 552. REPAIR IAW SRM 51-00-01 VOL I FIG 100. 2L73 4F RTA22WE 20050808001692005080800169NM 2005 8 8 05FDEA02271 120050805A5720 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25624FE 48443 LEFT WING L/E CRACK ON CHORD FIXED PANEL AT STA XORS 450. REPAIR IAW SRM 57-10-00 FIG 18. 2L73 4F RTA22WE 20050808001712005080800171NM 2005 8 8 P5CA0501384 120050803A2120 ODOR BOEING747 747341 13848AMNM CABIN UNKNOWN A P5CAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 EA15355MC 23395 INBOUND CREW REPORTED SMELL OF ELECTRICAL SMOKE IN COCKPIT DURING APPROACH. PERFORMED VISUAL INSPECTION OF ELECTRONIC COMPARTMENT SHELVES. NO EVIDENCE OF SMOKE OR DAMAGE NOTED. VISUALLY INSPECTED AREA UNDER PILOT'S YOKE AND CENTER PEDESTAL, NO DAMAGE FOUND. 2L74 4F RTA20WE 20050808001722005080800172WP 2005 8 8 IXXA05SMN89S 120050623A5340 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING C-CHECK INSPECT, MLG WW FRAME FITTING CORRODED, STA 940.000, L-24. PERFORMED MAJOR REPAIR IAW DC-8 SRM 53-2-0, EO SEMAN NR 2005844. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FOUND OUT OF LIMITS IAW DC-8 SRM 53-2-0. REMOVED CORRODED FRAME FITTING IAW DC-8 SRM 51-1-20D. FAB`D NEW FRAME FITTING IAW DWG DOUG 3646956, EO SEMAN 2005841, 4 SPLICE , DOUBLER (ALCLAD 7075 T6 0.190), (02 EA) FILLERS (ALCLAD 7075 T6 0.160) IAW DC-8 SRM 53-2-0 FIG 8 (SHEET 1,2,5,6. PERFORMED HEAT TREATMENT TO NEW FRAME FITTING, FILLER, DOUBLER IAW DC-8 SRM 51-1-1 PAGES 1, 13, 17. PERFORMED NDT INSPECTION TO NEW FRAME FITTING IAW DC-8 NDT SPM PART 08-00-02 TO 07. CLEANED, TREATED AND PRIMED AREA , REPAIR PARTS IAW DC-8 SRM 51-1-8B2L74 4F RT4A25 20050808001742005080800174CE 2005 8 8 DJFA2005123 120050802A273145AS61023143 ACTUATOR BEECH MU300 400A 1155402CE TAIL UNSERVICEABLE E DJFAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 EA23708TA 31 RK178 THE CREW REPORTED, AFTER LEVELING OFF AT 11,000 FT, ATTEMPTED TO TRIM THE NOSE OF THE A/C DOWN. WHILE PASSING 200 KTS, IT WAS NOTED THAT NO FURTHER TRIM WAS AVAILABLE AND THE CREW HAD REDUCED POWER. THE CO-PILOT HAD ATTEMPTED TO TRIM THE NOSE DOWN WITH THE SAME RESULTS. THE CAPTAIN HAD FULL TRIM AUTHORITY WHEN USING THE EMERGENCY PITCH TRIM WITH THE AUTOPILOT ON, BUT NOT WITH THE PRIMARY PITCH TRIM. THE AIRCRAFT WAS RETURNED TO KMCC AND HAD LANDED W/O FURTHER INCIDENT. MX REPLACED THE PITCH TRIM ACTUATOR. OP`S CHECKS WERE NORMAL AND THE TEST FLIGHT WAS SATISFACTORY. THE A/C WAS RETURNED TO SERVICE. 2H72 4F RTA16SW 20050808001752005080800175NM 2005 8 8 SB05088 120050807A335020131A BATTERY PACK BOEING737 7373B7 1384580NM FORWARD CABIN DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19396US 23318 PIT - MAINTENANCE REPORTED THE FORWARDED EMERGENCY LIGHTS NOT ILLUMINATING. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050808001782005080800178WP 2005 8 8 IXXA05SMN61S 120050623A5330 ANTENNA DOUG DC8 DC871F 302199DWP FUSELAGE DETERIORATED B IXXAO OTHER O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING C CHECK INSPECT, RT AFT FUS STA FS 1346.000, L-35.5R. ONLY 2 ROWS OF RIVETS IN OLD ANTENNA DOUBLER ADD 3RD ROWS OF RIVETS UTILIZING SRM RIVET SPACING OR UPGRADE REPAIR DOUBLER, STA 1346.000 L-35.5R (REF 822BX-R14). PERFORMED MAJOR REPAIR IAW DC-8 SRM 53-2-1 FIG 7 SHEET 1, 3, EO SEMAN # 2005868 DATE 06-13-05. REMOVED EXISTING REPAIR DOUBLER IAW DC-8 SRM 51-1-21 PG 1. FAB`D REPAIR DOUBLER (ALCLAD 7075 T6 0.090) + (02 EA) INTERNAL FINGER DOUBLER (ALCLAD 7075 T6 0.050”) IAW DC-8 SRM 53-2-1 FIG 7 SHEET 1,3, DC-8 SRM 53-4-1 FIG 16 SHEET 1 ITEM E, DC-8 SRM 51-10-0 FIG 2 SHEET 5, DC-8 SRM 51-9-0 FIG 68A, DC-8 SRM 51-1-4 PG 1. CLEANED, TREATED AND PRIMED AREA, REPAIR PARTS IAW DC-8 SRM 51-1-8B. APPLIED SEALANT2L74 4F RT4A25 20050808001792005080800179EU 2005 8 8 DHL2005367002 120050806A5230 DOOR AIRBUS300 A300B4203 3930306EU CARGO BAY STICKING A DHLAO OTHER N FALSE WARNING CRCRUISE 1 SO01367DH 265 DOOR LIGHT CAME ON IN FLIGHT ON MWP WITH CHIME AND NO INDICATION ON S/O PANEL. EMERGENCY CHECKLIST PERFORMED. LIGHT WENT OUT WITH NO CREW ACTION. PERFORMED DOOR WARNING SYSTEM TEST. FOUND SWITCH ON BULK CARGO COMPARTMENT DOOR STICKING. CLEANED AND LUBED IAW M/M 52-71-00, OPS CK GOOD. 2L72 4F RTA35EU 20050808001802005080800180WP 2005 8 8 IXXA05SMN57S 120050623A5330 SKIN DOUG DC8 DC871F 302199DWP CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING C CHECK INSPEC, LWR FWD FUS BELLY AFT NLG W/W SIDE 2 AND 4 EXCEED AVG PITCH, SIDE 2 AND 3 EXCEED MAX PITCH, STA 15.000 L-36. ADD RIVETS TO BRING AVG AND MAX PITCH INTO LIMITS PER SRM OR REWORK. PERFORMED MAJOR REPAIR IAW DC-8 SRM 53-1-0 PG 1, DC-8 SRM 53-3-1 FIG 1 ITEM A, EO SEMAN # 2005864 DATE 06-13-05. REMOVED CORROSION IAW DC-8 SRM 51-1-8 PGS 17, 18, FOUND OUT OF LIMITS IAW DC-8 SRM 53-2-0 PG 2P. REMOVED CORRODED PLATING SEMENT IAW DC-8 SRM 51-1-21 PG 1. FAB`D EXTERNAL SPLICES (02 EA) (ALCLAD 7075 T6 0.063), (02 EA) INTERNAL FINGER DOUBLER (ALCLAD 7075 T6 0.032), (02 EA) INTERNAL DOUBLER (ALCLAD 7075 T6 0.050) IAW SEMAN DC-8 SRM 53-2-1 (SHEET 1,2), DC-8 SRM 53-2-1 FIG 8 SHEET 3, TR # 53-173, DC-8 S2L74 4F RT4A25 20050808001822005080800182WP 2005 8 8 IXXA05SMN60S 120050623A5330 ANTENNA DOUG DC8 DC871F 302199DWP FUSELAGE DETERIORATED B IXXAO OTHER O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING C CHECK INSPECT, RT AFT FUS AFT FS 1290.000, L-35.5R; ONLY 2 ROWS OF RIVETS IN OLD OMEGA ANTENNA DOUBLER ADD THIRD ROW OF RIVETS UTILIZING SRM RIVET SPACING OR UPGRADE REPAIR DOUBLER (REF 822BX-R13). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 # 05259 DATE 06-24-05, SEMAN DWG ED 4000 DATE 06-20-05, EO SEMAN # 2005902 DATE 06-24-05. REMOVED EXISTING REPAIR DOUBLER IAW DC-8 SRM 51-1-21 PG 1, DC-8 SRM 51-1-20D PG 21. REMOVED DAMAGED AREA IAW SEMAN DWG NR EO 4000. PERFORMED NDT INSPECT IAW DC-8 NDT SPM PART 06-10-01-001. NO CRACK, CORROSION FOUND. FAB`D REPAIR DOUBLER (ALCLAD 7075 T6 0.063”), REPAIR TRIPLER (ALCLAD 7075 T6 0.071), (05 EA) INTERNAL FINGER DOUBLER (ALCLAD 7075 T6 0.032) AND (02 EA) FOLLERS (AL2L74 4F RT4A25 20050808001842005080800184WP 2005 8 8 IXXA05SMN86S 120050623A5340 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED B IXXAO OTHER O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, MLG W/W FITTING FRAME CORRODED, STA 879.375 AND L-24. PERFORMED MAJOR REPAIR IAW DC-8 SRM 53-2-0 FIG. 8, EO SEMAN NR 2005843 DATE 06-23-05. REMOVED CORROSION IAW DC-8 SRM 51-1-8 PAGES 17, 18. FOUND OUT OF LIMITS IAW DC-8 SRM 53-2-0 PAGE 2P. REMOVED CORRODED FITTING IAW DC-8 SRM 51-1-20D PAGE 21. FABRICATED SPLICES (02 EA) (ALCLAD 7075 T7 351), (02 EA) SHIMS (ALCLAD 7075 T6 0.071”) IAW DC-8 SRM 53-2-0 FIG 8 (SHEET 1, 3, 6). CLEANED, TREATED AND PRIMED AREA + REPAIR PARTS IAW DC-8 SRM 51-1-8B. INSTALLED NEW FRAME FITTING (PN 3641 00 4 U 504) + NEW DOUBLER (PN 5802677-7N) + (04 EA) SPLICES + (06 EA) SHIMS IAW DC-8 SRM 53-2-0 FIG 8 SHEET 1, 3, 6, DC-8 SRM 51-1-20D PAGE 9. 2L74 4F RT4A25 20050808001852005080800185WP 2005 8 8 IXXA05SMN71S 120050623A5330 SKIN DOUG DC8 DC871F 302199DWP FUSLEAGE DAMAGED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, EXTERNAL DOUBLER ON FWD FUSELAGE BELLY SKIN, MUST BE UPGRADED, REPAIR MUST HAVE THREE ROWS OF RIVETS AT STA FS 401.000 L-35.75 (REF. 822BX-R47). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05271 DATE 06-29-05, SEMAN DWG ED 3997 DATE 06-24-05, EO SEMAN NR 2005899 DATE 06-29-05. REMOVED EXISTING REPAIR DOUBLER IAW DC-8 SRM 51-1-21 PAGE 1 AND DC-8 SRM 51-1-20D PAGE 21. REMOVED DAMAGED AREA IAW SEMAN DKW ED 3997. PERFORMED NDT INSPECTION IAW DC-8 NDT SPM 06-10-01-001. NO CRACK, CORROSION FOUND. FABRICATED REPAIR DOUBLER (ALCLAD 7075 T6 0.080”) + INTERNAL FINGER DOUBLER (ALCLAD 7075 T6 0.032”) IAW SEMAN DWG ED 3997. CLEANED, TREATED AND PRIMED AREA + REPAIR PARTS IAW DC-8 S2L74 4F RT4A25 20050808001862005080800186WP 2005 8 8 IXXA05SMN72S 120050623A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE DAMAGED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING C CHECK INSPECTION, EXTERNAL DOUBLER ON FWD FUSELAGE BELLY SKIN MUST BE UPGRADED, REPAIR MUST HAVE THREE ROWS OF RIVETS, STA FS 543.000 L-3.75R (REF. 822BX-R50). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05271 DATE 06-29-05, SEMAN DWG ED 3998 DATE 06-22-05, EO SEMAN NR 2005900 DATE 06-29-05. REMOVED EXISTING REPAIR DOUBLER IAW DC-8 SRM 51-1-21 PAGE 1 AND DC-8 SRM 51-1-20D PAGE 21. PERFORMED DETAILED VISUAL INSPECTION NO CRACK FOUND, NO CORROSION FOUND. FAB`D REPAIR DOUBLER (ALCLAD 7075 T6 0.100”) + INTERNAL FINGER DOUBLER (ALCLAD 7075 T6 0.032”) IAW SEMAN DWG ED 3998. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW DC-8 SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-12L74 4F RT4A25 20050808001872005080800187WP 2005 8 8 IXXA05SMN73S 120050623A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE DAMAGED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, EXTERNAL DOUBLER ON FWD FUSELAGE BELLY SKIN, MUST BE UPGRADED, REPAIR MUST HAVE THREE ROWS OF RIVETS AT STA FS 1135.000 L-35.5R. PERFORMED MAJOR REPAIR IAW DC-8 SRM 53-2-1 FIG 7 EO SEMAN Nº 2005870 DATE 06-13-05. REMOVED EXISTING REPAIR DOUBLER IAW DC-8 SRM 51-1-21 PAGE 1. REMOVED DAMAGED AREA IAW DC-8 SRM 53-2-1 FIG. 7 (SHEET 1,3). FABRICATED REPAIR DOUBLER (ALCLAD 7075 T6 0.160”) + (02 EA) INTERNAL FINGER DOUBLER (ALCLAD 7075 T6 0.050”) IAW DC-8 SRM 53-2-1 FIG 7 SHEET 1, 3, DC-8 SRM 53-4-1 FIG 16 SHEET 1, ITEM D, DC-8 SRM 51-1-4 PAGE 1. CLEANED, TREATED AND PRIMED AREA + REPAIR PARTS IAW DC-8 SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11. INSTA2L74 4F RT4A25 20050805000282005080500028NM 2005 8 5 SWAA052173 120050725A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 727E, BETWEEN STR 26L & STR 27L. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050805000292005080500029NM 2005 8 5 SWAA052175 120050725A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 947.5, STR 23L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050805000332005080500033NM 2005 8 5 SWAA052179 120050724A55236959227 BUSHING BOEING737 7373H4 1384600NM LT ELEVATOR TAB WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29600WN 27694 DURING SCHEDULED C4 CHECK, LEFT ELEVATOR TAB FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED LEFT ELEVATOR TAB NR 1 & NR 2 HINGE BUSHINGS & HARDWARE PER MM. 2L72 4F RTA16WE 20050805000362005080500036NM 2005 8 5 SWAA052169 120050722A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727C, STR 14R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050805000442005080500044NM 2005 8 5 SWAA052197 120050726A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29610WN 27696 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 727E, RBL 10. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050805000642005080500064NM 2005 8 5 SWAA052301 120050801A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29315SW 23337 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 15L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050805000732005080500073NM 2005 8 5 SWAA052208 120050727A53156546811 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29610WN 27696 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 986, RBL 25 TO RBL 44. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20050805000762005080500076NM 2005 8 5 SWAA052212 120050727A3350101114 COVER BOEING737 7373H4 1384600NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 L1 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED COVER PER MM. 2L72 4F RTA16WE 20050805000772005080500077NM 2005 8 5 SWAA052185 120050726A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 727E, BETWEEN STR 25L & STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050805000792005080500079NM 2005 8 5 SWAA052187 120050725A3350D71702001 BATTERY PACK BOEING737 7373K2 13844BANM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29340LV 23738 L1 & R1 DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050805000812005080500081NM 2005 8 5 SWAA052189 120050726A335007912 COVER BOEING737 7377H4 1384404NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29457WN 33856 CABIN EEPLS COVER CRACKED AT FWD END. REMOVED AND REPLACED COVER PER MM. 2L72 4F RTA16WE 20050805000922005080500092NM 2005 8 5 SWAA052290 120050802A53306545775 SKIN BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29610WN 27696 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 767, BETWEEN STR 27L TO STR 27R. REPAIRED SKIN PER SRM & BFG ER. 2L72 4F RTA16WE 20050805001002005080500100NM 2005 8 5 SWAA052272 120050801A53156546805 FLOORBEAM BOEING737 7373H4 1384600NM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND 2 EACH LONGITUDINAL FLOORBEAMS CORRODED AT BS 847 + 10, LBL 7 & LBL 12. REPAIRED FLOORBEAMS PER SWA EA. 2L72 4F RTA16WE 20050805001112005080500111 2005 8 5 SWAA052283 420050801A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29712SW 27846 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050805001162005080500116NM 2005 8 5 05FDEA02218 120050803A5755 SKIN DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 RIGHT HAND WING UPPER SURFACE TRAILING EDGE FORWARD OF NR 2 SPOILER SKIN BULGE AT XORS 536 STRINGER 1. RHW UPPER SURFACE TRAILING EDGE FORWARD OF NR 2 SPOILER XORS 536 STRINGER 1 SKIN BULGE AREA CORROSION REMOVED. MAT'L REMOVED: 0.032"; ORIG. THICKNESS: 0.310"; MAT'L REMAINED: 0.278"; FOUND EXCEED LIMIT AS PER SRM 57-10-00 FIG. 32 VOL.I. AREA REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-87562 - WINGS - RH UPPER WING SKIN - CORROSION REPAIRS AT XORS = 531 THRU XORS = 536 & XORS = 540. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6 -2-100. 2L73 4F RTA22WE 20050805001202005080500120WP 2005 8 5 05FDEA02176 120050802A5320 WEB DOUG MD10 MD1010F 3022112WP APU BAY CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25381FE 46615 ONE CRACK 1 INCH LONG ON WEB INSIDE APU COMPT STA 2033. REPAIR CRACK IAW SRM 53-17-01 VOL 3 FIG 4, SRM 54-00-01 FIG 2B VOL 2, SRM 51-35-01 PG 1-13 VOL 2. 2L73 4F RTA22WE 20050805001262005080500126NM 2005 8 5 05FDEA02167 120050801A5313 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 CENTER CARGO STATION 5-93 TO STATION 5-113 LONGERON 46R CORROSION FOUND AT TWO LOCATION AS MARKED. CORRODED LONGERON AT 46R CTR CARGO STA 5-93 TO STA 5-113 ON TWO LOCATION CARRIED OUT REPAIR AS PER SRM 53-10-00 FIG. 2. VOL. I. AND FEDEX EA 1-5310-87568 (TITLE: FUSELAGE - LONGERON L46 RH - INSTALLATION OF AN SRM TYPE SPLICE REPAIR WITH BOEING APPROVAL). REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050805001342005080500134CE 2005 8 5 CIEA20050012 120050729A7830 WARNING LIGHT LEAR 55 55LEAR 5170702CE THRUST REVERSER ILLUMINATED E CIEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM03113YS 55071 THE LEFT THRUST REVERSER UNLOCK FLASHED ON AFTER ROTATION. THE AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. THE T/R'S WERE PINNED AND THE FLIGHT WAS DISPATCHED. AT THIS TIME A REASON HAS NOT BEEN FOUND. 2L72 4F A10CE 20050805001362005080500136 2005 8 5 CIEA200500010 420050722A3421161E1 COUPLER BEECH 200 200BEECH 1152920CE ATTITUDE IND UNSECURE E CIEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM035ST 10846 BB289 DURING CLIMB TO ALTITUDE, THE PILOT ATTITUDE INDICATOR DISPLAYED A GYRO FLAG, THEN THE INDICATOR ROLLED TO THE OFF POSITION. THE AIRCRAFT RETURNED TO THE AIRPORT AND LANDED WITHOUT INCIDENT. MAINTENANCE WERE UNABLE TO FULLY DUPLICATE THE PROBLEM. WHILE WORKING ON THE SYSTEM AND MOVING THE 161E-1 MODE COUPLER, THE GYRO FLAG WOULD COME INTO VIEW INTERMITTENTLY. THE MODE COUPLER WAS REMOVED AND THE CANNON PLUG WAS CLEANED, AND THE UNIT WAS REINSTALLED. THE SYSTEM CHECKED GOOD AND WERE NO LONGER ABLE TO GET THE GYRO FLAG INTO VIEW. IT HAS BEEN DETERMINED THAT THE MODE COUPLER WAS NOT FULLY SEATED IN THE RACK ORIGINALLY. 1L72 4T A24CE 20050805001372005080500137NM 2005 8 5 SWAA052302 120050803A53106935371 VERTICAL BEAM BOEING737 7373H4 1384600NM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CORRODED BETWEEN BS 767 TO BS 787, STR 25R TO STR 26R. REMOVED AND REPLACED WEB SECTION PER SRM. 2L72 4F RTA16WE 20050805001402005080500140EU 2005 8 5 05FDEA02210 120050802A2700 FLAP SYSTEM AIRBUS310 A310203 3930313EU WINGS STUCK A FDEAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 SO25414FE 400 DURING SLAT/FLAP RETRACT FLAPS STUCK AT 15 DEG SLATS OK FLAPS SYS 1 & 2 LIGHTS ILLUMINATED AS WELL AS FLAPS LIGHT ON SFDI FLAPS STUCK RAN CHECKLIST LANDED UNEVENTFULLY. FAULT CODE NOT APP TO THIS A/C, ENGINEERING HAS CONTACTED AIRBUS. CYCLED FLAPS AND SLATS 6 TIMES WITHOUT ANY FAULTS. CHECKED TORQUE LIMITERS AND NO FAULTS NOTED. REF THE AIRBUS M/M 27-51-18-4, REMOVED AND REPLACED BOTH SFCC'S FOR PRECAUTIONARY REASONS. REF THE AIRBUS M/M 27-51-00-5, PERFORMED OPS CHECK. SYSTEM OPS CHECKS NORMAL. RAN ENGINES AGAIN AND CYCLED FLAPS AND SLATS 6 MORE TIMES AND NO FAULTS NOTED. 2L72 4F RTA35EU 20050805001482005080500148NM 2005 8 5 SWAA052308 120050802A143018A80101 BOLT BOEING737 7373H4 1384600NM LT ELEVATOR TAB WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29396SW 27690 DURING SCHEDULED C1 CHECK, LT ELEVATOR TAB FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR TAB CONTROL PUSHROD BOLT AND HARDWARE PER MM. 2L72 4F RTA16WE 20050805001622005080500162NM 2005 8 5 DL76G050384 120050720A4920 TURBINE BOEING767 7673P6 1385105NM APU FAILED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27154DL31368 25241 I1542 RAN APU ENTIRE FLT, AFTER LDG WHEN SWITCHED BLEEDS TO APU TO RUN PACKS SMELLED AC SMOKE. REPLACED APU. 2L72 4F RTA1NM 20050808000062005080800006NM 2005 8 8 UPS05445037 120050723A532265B071793 SHEAR TIE BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 BS 2120 BETWEEN S13-14L FRAME ATT SHEAR TIE FOUND BROKEN, CRACK LENGTH .5. SHEAR TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050808000092005080800009NM 2005 8 8 UPS05445040 120050723A532269B028033 SHEAR TIE BOEING747 747121 1384871NM M/D CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 BS 1780 S4-5R STRINGER SHEAR TIE FOUND CRACKED, CRACK LENGTH .3750. SHEAR TIE REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050808000282005080800028 2005 8 8 SWAA052316 420050803A25656557463 FITTING BOEING737 7373G7 1384595NM GIRT BAR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29691WN 23781 DURING SCHEDULED 1/4D CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD AND AFT GIRT BAR FLOOR FITTINGS WORN. REMOVED AND REPLACED FITTINGS PER MM. 2L72 4F RTA16WE 20050808000362005080800036NM 2005 8 8 DL777050391 120050721A3397 WIRE BOEING777 777232 1385232NM EMERGENCY LIGHTSDAMAGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27862DA 29734 EMERGENCY LIGHTS FOR SEATS IN C ZONE INOP, REPAIRED WIRING. 2L72 4F RTT00001SE 20050808000382005080800038NM 2005 8 8 DL75K050392 120050722A3350 WIRE BOEING757 757232 1384965NM EMERGENCY LIGHT BROKEN A DALAK NONE L NO TEST ININSP/MAINT 1 SO276703D 30234 SEAT 18 RT EMERGENCY PATH LIGHT INOP. REPAIRED BROKEN WIRE IN SIDEWALL. 2L72 4F RTA2NM 20050808000402005080800040NM 2005 8 8 DL757050394 120050721A3260 UPLOCK SENSOR BOEING757 757232 1384965NM MLG MALFUNCTIONED A DALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27604DL 22811 AFTER TAKEOFF, GEAR DISAGREE ON EICAS ILLUMINATED ALONG WITH GEAR LIGHT ABOVE HANDLE. RETURNED TO CVG WHEN GEAR LOWERED ALL INDICATIONS RETURNED TO NORMAL. FOUND FAULT CARD ON SYS 2 069 ON PSEU. REPLACED PSEU PER M/M CHKS GOOD. GEAR SWING CKS OK. REPLACED RT GEAR UP SENSORS S10069 AND S10239. SWUNG GEAR SEVERAL TIMES OPS NORMAL EACH TIME. NO EICAS MSG, NO FAULTS ON PSEU AFTER GEAR SWING. 2L72 4F RTA2NM 20050808000412005080800041NM 2005 8 8 DL764050395 120050723A7500 DUCT BOEING767 767424ER 1385270NM GE CF6 CF680C2* GL NR 2 ENGINE LEAKING A DALAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 SO27833MH14262 29706 706120 DURING CLIMB-OUT, GOT RIGHT ENGINE FIRE WARNING WITH ALL THE LIGHTS AND CHIMES. CANCELLED WARNING TWICE. THEN DECIDED TO SHUT THE ENGINE DOWN PER QRH AND FIRED 1 BOTTLE AND ALL INDICATIONS SILENCED. REPAIRED LOOP WIRING AND REPLACED HP DUCT. 2L72 4F4 FRTA1NM E23EA 20050808000552005080800055NM 2005 8 8 DLM88050411 120050728A7830789101198 LINE DOUG MD88 MD88 3023688NM THRUST REVERSER LEAKING A DALAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27936DL 49723 STRONG BURNING ODOR DURING TAXI, REPLACED LEAKING LINE AT LEFT THRUST REVERSER CONTROL VALVE. PERFORMED DUCT BURNOUT. 2L72 4F RTA6WE 20050808000832005080800083NM 2005 8 8 MASA200500575 120050720A2913570347 PUMP DHAV DHC8 DHC8202 2809007NM HYD SYSTEM FAILED A MASAO OTHER J WARNING INDICATION TOTAKEOFF 1 SW07455YV2928 455 ASH 7055 ASE, NR 1 HYD SYSTEM WENT TO ZERO QTY AND ZERO PRESSURE ON TAKEOFF. CONTRACT MX REMOVED AND REPLACED THE PRESSURE MANIFOLD HYDRAULIC PUMP EDP. 2H72 4T RTA13NM 20050808000872005080800087NM 2005 8 8 AALA20050487 120050731A3350 LIGHT BOEING777 777223 1385213NM CABIN BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21759AN 32638 NRT EMERGENCY LIGHT COVER AND FRAME ON BOTTOM RIGHT CORNER OF FIRST CLASS COAT CLOSET BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT ON BOTTOM RIGHT CORNER OF FIRST CLASS COST CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20050808000892005080800089NM 2005 8 8 BB05059 120050802A2611PU90461R3 SMOKE DETECTOR BOEING757 757225 1384959NM PASSENGER CABIN FAULTY A USAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA19608AU 22204 CLT FLT 422 - EN ROUTE TPA TO CLT, THE CABIN CREW REPORTED THE 2L LAV SMOKE DETECTOR WAS GOING OFF WHILE AN ODOR WAS PRESENT. MAINTENANCE REPLACED THE 2L LAV SMOKE DETECTOR. 2L72 4F RTA2NM 20050808000922005080800092NM 2005 8 8 05FDEA02219 120050803A7711JG298A5 INDICATOR BOEING727 72722 1384002NM COCKPIT SPINNING A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25180FE 18867 NR 3 EPR GAUGE ERRATIC SPINNING RAPIDLY WHEN T/O POWER SET. AFTER RTO, OPERATELY NORMALLY ON SECOND ATTEMPT. INFO NOTED PER CREW, OPS CHECK GOOD ON GROUND, NO DEFECTS NOTED OK TO CONTINUE. 2L73 4F A3WE 20050808001022005080800102NM 2005 8 8 PIDA20050062 120050805A3350 LAMP BOEING737 7373G7 1384595NM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05390WL 23219 EMERGENCY EXIT LIGHT IN OVERHEAD BIN AT SEAT 4RT IS INOP. RELAMPED, OPS NORMAL. 2L72 4F RTA16WE 20050808001242005080800124NM 2005 8 8 05FDEA02233 120050803A2612774001 SMOKE DETECTOR BOEING727 727200 138407ENM ZONE 200 MALFUNCTIONED A FDEAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO25203FE 22925 MAIN CARGO SMOKE ALARM NR 4 ILLUMINATED WITH ASSOCIATED BELL .WENT OUT 2 MIN AFTER ILLUMINATION , NO OTHER INDICATIONS OF FIRE WERE PRESENT. REMOVED AND REPLACED THE NR 4 SMOKE DETECTOR PER B727-200 MM 26-16-001-4, OPS CHECK GOOD, OK FOR SERVICE. *S/D* REMOVED AND REPLACED THE NR 4 SMOKE DETECTOR PER B727-200 M/M 26-16-001-4. OP'S CHECK GOOD OK FOR SERVICE. 2L73 4F RTA3WE 20050808001312005080800131NM 2005 8 8 05FDEA02249 120050804A3234 HANDLE BOEING727 727200 138407ENM MLG MALFUNCTIONED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25466FE 21292 AFTER GEAR RETRACTION, WITH GEAR HANDLE IN OFF POSITION, R GEAR DOOR LIGHT ON SO PANEL AND RED DOOR LIGHT ILLUMINATED. LIGHTS WENT OUT WHEN GEAR HANDLE WAS PUT BACK UP. RECYCLED ONCE THEN GEAR HANDLE LT UP PER QRH. ADJUSTED RT GEAR DOOR WARNING SWITCH REF M/M 32-62-011-4. A/C OK FOR SERVICE. 2L73 4F RTA3WE 20050808001442005080800144EU 2005 8 8 05FDEA02252 120050804A5321 FLOOR PANEL AIRBUS300 A300B4605R 3930308EU MDC CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25670FE 777 MDC FLOOR PNL 252WG CRACKED. 2L72 4F RTA35EU 20050808001462005080800146NM 2005 8 8 05FDEA02254 120050804A5347 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 MAIN DECK, SEAT TRACK LBL 47 CRACKED AT STA 939. REPAIR CARRIED OUT AS PER SRM 53-70-00. 2L73 4F RTA22WE 20050808001562005080800156NM 2005 8 8 05FDEA02261 120050804A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 MAIN DECK CARGO COMPARTMENT, FLOOR SEAT TRACK AT STA 635, X= 8.5 FOUND CRACKED APPROXIMATELY 3 INCHES LONG. REMOVED AS PER SRM 53-70-00 VOLUME I, FIGURE 1. REPAIR SEAT TRACK AND SPLICES FABRICATED AS PER SRM 53-70-00 VOLUME I, FIGURE 1. HFEC INSPECTION CARRIED OUT AS PER NDT SPM 06-10-01-001 REV. 12 FOUND NO CRACK. REPAIR PARTS TREATED AS PER SRM 57-21-01 VOLUME II. NEW SEAT TRACK AND SPLICES INSTALLED AS PER SRM 53-70-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2L73 4F RTA22WE 20050808001662005080800166WP 2005 8 8 05FDEA02203 120050802A5533 STRUCTURE DOUG MD10 MD1010F 3022112WP VERTICAL STAB UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25381FE 46615 VERTICAL STABILIZER RT SIDE OLD REPAIR AT XAR=417.800. REPAIR IAW SRM 55-00-01 FIG 3 VOL 1. 2L73 4F RTA22WE 20050808001732005080800173WP 2005 8 8 IXXA05SMN70S 120050623A5330 SKIN DOUG DC8 DC871F 302199DWP DAMAGED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING C CHECK INSPECT, EXT DOUBLER FWD LWR BASKET DOOR OPENING FWD EDGE REPAIR LACKS ENOUGH RIVETS ALL SIDES OF CUT OUT STA FS 279.000 L-31.5R. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 # 05270 DATE 06-29-05, SEMAN DWG ED 3995 DATE 06-25-05, EO SEMAN # 2005897 DATE 06-29-05. REMOVED EXISTING REPAIR DOUBLER IAW DC-8 SRM 51-1-21 PG 1. REMOVED DAMAGED AREA IAW SEMAN DKW ED 3995. PERFORMED NDT INSPECT IAW DC-8 NDT SPM 06-10-01-001. NO CRACK, CORROSION FOUND. FAB`D EXT REPAIR DOUBLER (ALCLAD 7075 T6 0.080), EXTERNAL REPAIR TRIPLER (ALCLAD 7075 T6 0.100), FILLER (ALCLAD 7075 T6 0.071) IAW SEMAN DWG ED 3995 AND DC-8 SRM 51-1-4 PG 1. CLEANED, TREATED AND PRIMED AREA, REPAIR PARTS IAW DC-8 SRM 51-1-8B. APPLIED PRC SE2L74 4F RT4A25 20050808001812005080800181WP 2005 8 8 IXXA05SMN59S 120050623A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE DETERIORATED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING C CHECK INSPECT, REPAIR ON UAL DRAIN DOUBLER MUST BE UPGRADED. REPAIR MUST HAVE 3 ROWS OF RIVETS STA 1270.000, L-35.5L. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 # 05259 DATE 06-24-05, SEMAN DWG ED 4000 DATE 06-20-05, EO SEMAN # 2005902 DATE 06-24-05. REMOVED EXISTING REPAIR DOUBLER IAW DC-8 SRM 51-1-21 PG 1, DC-8 SRM 51-1-20D PG 21. TRIMMED OUT DAMAGED AREA IAW SEMAN DWG NR EO 4000. PERFORMED NDT INSPECT IAW DC-8 NDT SPM PART 06-10-01-001. NO CRACK, CORROSION FOUND. FAB`D REPAIR DOUBLER (ALCLAD 7075 T6 0.063), REPAIR TRIPLER (ALCLAD 7075 T6 0.071), (05 EA) INTERNAL FINGER DOUBLER (ALCLAD 7075 T6 0.032) AND (02 EA) FOLLERS (ALCLAD 7075 T6 0.125) IAW SEMAN ED 4000, DC-8 SRM 51-1-4 PG 1. CLEANED, TREATED2L74 4F RT4A25 20050808001882005080800188WP 2005 8 8 IXXA05SMN74S 120050623A5730 SKIN DOUG DC8 DC871F 302199DWP RT WING DAMAGED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, RT WING INBD L/E UPPER SKIN NON STANDARD REPAIR BETWEEN STA XFS 113.750 - XF 120.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-2-1 FIG. 2J, EO SEMAN NR 2005970 DATE 06-23-05. REMOVED DAMAGED PLATING IAW DC-8 SRM 57-2-1 FIG. 2J. PERFORMED NDT INSPECTION IAW DC-8 NDT SPM PART 06-10-01-001. FABRICATED INTERNAL REPAIR DOUBLER (ALCLAD 2024 T3 0.090”) + FILLERS (ALCLAD 2024 T3 0.063”) IAW DC-8 SRM 57-2-1 FIG. 2J. CLEANED, TREATED AND PRIMED AREA + REPAIR PARTS INTERNAL PART IAW DC-8 SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-12 PAGE 9. INSTALLED REPAIR PARTS IAW DC-8 SRM 57-2-1 FIG. 2J, DC-8 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050808001912005080800191NM 2005 8 8 TSAA0577033 120050727A7711LG80AC TRANSMITTER BOEING737 7372X6C 1384552NM NR 1 EPR DEFECTIVE A TSAAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 WP13817AL 23292 FLT 850 HNL - ITO. ON TAKEOFF, NUMBER 1 ENGINE PRESSURE RATIO INDICATION STOPPED INCREASING AT 170 WHILE THE NUMBER 2 ENGINE INDICATION OPERATED NORMALLY. CREW ABORTED TAKEOFF AT 80 KNOTS. AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 ENGINE EPR TRANSMITTER AND PERFORMED AN ENGINE HIGH POWER RUN UP WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA16WE 20050808001922005080800192WP 2005 8 8 IXXA05SMN76S 120050623A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE INADEQUATE B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING C CHECK INSPECT, EXTERNAL DOUBLER FWD FUSELAGE BELLY SKIN MUST BE UPGRADED, REPAIR MUST HAVE THREE ROWS OF RIVETS, STA FS 543.000 L-3.75R (REF. 822BX-R50). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05271 DATE 06-29-05, SEMAN DWG ED 3998 DATE 06-22-05, EO SEMAN NR 2005900 DATE 06-29-05. REMOVED EXISTING REPAIR DOUBLER IAW DC-8 SRM 51-1-21 PAGE 1 DC-8 SRM 51-1-20D PAGE 21. PERFORMED DETAILED VISUAL INSPECT NO CRACK FOUND, NO CORROSION FOUND. FABRICATED REPAIR DOUBLER (ALCLAD 7075 T6 0.100”) + INTERNAL FINGER DOUBLER (ALCLAD 7075 T6 0.032”) IAW SEMAN DWG ED 3998. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW DC-8 SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11. INS2L74 4F RT4A25 20050808001932005080800193WP 2005 8 8 IXXA05SMN77S 120050623A5730 SKIN DOUG DC8 DC871F 302199DWP RT WING CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING C CHECK INSPECT, RT WING INBD OUTER L/E LWR SKIN CRACKED 1/2", XFS 591.250. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05270 DATE 06-29-05, SEMAN DWG ED 4017 DATE 06-28-05, EO SEMAN NR 2005969 DATE 06-29-05. REMOVED FASTENERS IAW DC-8 SRM 51-1-21 PAGE 1. REMOVED DAMAGED AREA IAW SEMAN DWG ED 4017. PERFORMED NDT INSPECT IAW DC-8 NDT SPM PART 06-60-01-001. NO CRACK, CORROSION FOUND. FAB`D EXTERNAL REPAIR DOUBLER (ALCLAD 7075 T6 0.063”) + FILLER (ALCLAD 7075 T6 0.050”) IAW SEMAN DWG ED 4017. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW DC-8 SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11 PAGE 9. INSTALLED REPAIR PARTS IAW SEMAN DWG ED 4017, DC-8 SRM 51-1-21 PAGE2L74 4F RT4A25 20050808001942005080800194WP 2005 8 8 IXXA05SMN78S 120050623A5230 DOOR DOUG DC8 DC871F 302199DWP FUSELAGE WORN B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING C CHECK INSPECT, EXTERNAL FUS "C" BELLY DOOR LWR PART WORN. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05283 DATE 07-06-05, SEMAN DWG ED 4002 DATE 07-01-05, EO SEMAN NR 2005971 DATE 07-06-05. REMOVED FASTENERS IAW DC-8 SRM 51-1-21 PAGE 1, DC-8 SRM 51-1-21 PAGE 1, DC-8 SRM 51-1-20D PAGE 1. REMOVED DAMAGED AREA IAW SEMAN DWG ED 4020. PERFORMED NDT INSPECT IAW DC-8 NDT SPM PART 06-60-01-001. FAB`D NEW SKIN SEGMENT (ALCLAD 7075 T6 0.071”) + (05 EA) INTERNAL SPLICE DOUBLER (ALCLAD 7075 T6 0.071”) + INTERNAL STRAP DOUBLER (TITANIUM GAL-UV 0.032”) IAW SEMAN DWG ED 4020, DC-8 SRM 52-4-1 FIG 1 ITEM “Q”. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW DC-8 SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING S2L74 4F RT4A25 20050808001952005080800195WP 2005 8 8 IXXA05SMN79S 120050623A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE DAMAGED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING C CHECK INSPECT, EXT DOUBLER LT AFT FUSELAGE MUST BE UPGRADED REPAIR MUST HAVE THREE ROWS OF RIVETS, STA FS 1695.000 L-30.5L (REF. 822BX-R67). PERFORMED MAJOR REPAIR IAW DC-8 SRM 53-2-1 FIG 7, EO SEMAN NR 2005872 DATE 06-13-05. REMOVED EXISTING REPAIR DOUBLER IAW DC-8 SRM 51-1-21 PAGE 1, DC-8 SRM 51-1-20D PAGE 21. TRIMMED OUT DAMAGED AREA IAW DC-8 SRM 53-2-1 FIG 7 (SHEET 1, 5) PERFORMED DETAILED VISUAL INSPECT. NO CRACK, CORROSION FOUND. FAB`D REPAIR DOUBLER (ALCLAD 7075 T6 0.063”) + INTERNAL FINGER DOUBLER (ALCLAD 7075 T6 0.032”) + FILLER (ALCLAD 7075 T6 0.050”) IAW DC-8 SRM 53-2-1 FIG 7 (SHEET 1,5), DC-8 SRM 53-5-1 FIG 1 ITEM E, DC-8 SRM 51-1-4 PAGE 1. CLEANED, TREATED AND PRIMED AREA + REPAIR PAR2L74 4F RT4A25 20050808001962005080800196WP 2005 8 8 DHL2005803002 120050806A32600080004002 PROXIMITY SENSOR DOUG DC8 DC873 302199CWP MLG MALFUNCTIONED A DHLAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SO01803DH 46123 DURING PREFLIGHT PERFORMED GEAR UNSAFE LIGHT CHECK LEFT DOOR UNSAFE LIGHT WOULD NOT ILLUMINATE DURING CHECK. ITEM TRANSF TO DMI NR 21967 IAW MEL 32-14 CAT "A"3.) REF DMI #21967 DURING PREFLIGHT PERFORMED GEAR UNSAFE LIGHT CHECK LEFT DOOR UNSAFE LIGHT WOULD NOT ILLUMINATE DURING CHECK. REMOVED AND REPLACED GEAR DOOR PROX BOX IAW 32-60-0, OPS CHECK IS GOOD THIS CLEARS DMI NR 21967 PLACARD REMOVED. 2L74 4F RT4A25 20050808001972005080800197WP 2005 8 8 IXXA05SMN82S 120050623A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE DAMAGED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING C CHECK INSPECTION, EXTERNAL DOUBLER LEFT AFT FUSELAGE BELOW L-2 DOOR. REPAIR FAILED ASSESSMENT DOUBLER NOT THICK ENOUGH, SIDES 2 UPPER AND 4 LOWER EXCEED AVERAGE RIVET SPACING SIDES 1 FWD, 2 UPPER, 3 AFT, 4 LOWER EXCEED MAX RIVET SPACING. UPGRADE REPAIR PER DACO DC-8 SRM (STA FS 1670). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05283 DATE 07-06-05, SEMAN DWG ED 4002 DATE 07-01-05, EO SEMAN NR 2005904 DATE 07-06-05. REMOVED EXISTING REPAIR DOUBLER IAW DC-8 SRM 51-1-21 PAGE 1. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND, NO CORROSION FOUND. FABRICATED REPAIR DOUBLER (ALCLAD 7075 T6 0.050”) + INTERNAL FINGER DOUBLER (ALCLAD 7075 T6 0.032”) IAW SEMAN DWG ED 4002, DC-8 SRM 51-1-4 PAGE 1. C2L74 4F RT4A25 20050808001982005080800198WP 2005 8 8 IXXA05SMN67S 120050623A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE DAMAGED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING C CHECK INSPECT, EXTERNAL DOUBLER ON FWD LOWER FUSELAGE, STA FS 173, L-35.5R REPAIR MUST BE UPGRADED. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05271 DATE 06-29-05, SEMAN DWG ED 3993 DATE 06-22-05, EO SEMAN NR 2005862 DATE 06-29-05. REMOVED EXISTING REPAIR DOUBLER IAW DC-8 SRM 51-1-21 PAGE 1. FAB`D DOUBLER (ALCLAD 7075 T6 0.063”) + (02 EA) INTERNAL FINGER DOUBLER (ALCLAD 7075 T6 0.032) IAW SEMAN ED 3993 AND DC-8 SRM 51-1-4 PAGE 1. CLEANED, TREATED AND PRIMED AREA ALSO REPAIR PARTS IAW DC-8 SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11. INSTALLED REPAIR PARTS IAW SEMAN DWG ED 3993, DC-8 SRM 51-1-21 PAGE 1, DC-8 SRM 51-1-20D PAGE 9. TORQUED IAW DC-8 SRM 51-3-1. 2L74 4F RT4A25 20050808001992005080800199WP 2005 8 8 IXXA05SMN63S 120050623A5330 SKIN DOUG DC8 DC871F 302199DWP DAMAGED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING C CHECK INSPECT, EXTERNAL DOUBLER ON AFT LOWER FUSELAGE, STA FS 1540.000, L-35.5L REPAIR MUST BE UPGRADED. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05271 DATE 06-29-05, SEMAN DWG ED 4001 DATE 06-22-05, EO SEMAN NR 2005903 DATE 06-29-05. REMOVED EXISTING REPAIR DOUBLER IAW DC-8 SRM 51-1-21 PAGE 1, DC-8 SRM 51-1-20D PAGE 21. PERFORMED DETAILED VISUAL INSPECT NO CRACK, CORROSION FOUND. FAB`D REPAIR DOUBLER (ALCLAD 7075 T6 0.080”) + INTERNAL FINGER DOUBLER (ALCLAD 7075 T6 0.032”) IAW SEMAN ED 4001. CLEANED, TREATED AND PRIMED AREA + REPAIR PARTS IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11 PAGE 9. INSTALLED REPAIR PARTS IAW SEMAN DWG ED 40001 DC-8 SRM 51-1-21 PAGE 1, 2L74 4F RT4A25 20050808002002005080800200WP 2005 8 8 IXXA05SMN65S 120050623A5330 SKIN DOUG DC8 DC871F 302199DWP DAMAGED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECT, UAL DRAIN DOUBLER AT FWD LWR FUSELAGE FS 77, L-35.5R MUST BE UPGRADED, REPAIR MUST HAVE THREE ROWS OF RIVETS (REF. 822BX-R29). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05258 DATE 06-24-05, SEMAN DWG ED 3992 DATE 06-21-05, EO SEMAN NR 2005896 DATE 06-24-05. REMOVED EXISTING REPAIR DOUBLER IAW DC-8 SRM 51-1-21 PAGE 1, DC-8 SRM 51-1-20D PAGE 21. TRIMMED OUT DAMAGED AREA IAW SEMAN DWG NR EO 3992. PERFORMED NDT INSPECTION IAW DC-8 NDT SPM PART 06-10-01-001. NO CRACK, CORROSION FOUND. FAB`D REPAIR DOUBLER (ALCLAD 7075 T6 0.063) + (02 EA) INTERNAL FINGER DOUBLER (ALCLAD 7075 T6 0.032”) IAW SEMAN ED 3992. CLEANED, TREATED AND PRIMED AREA + REPAIR PARTS IAW DC-8 SRM 51-1-8B. APPLIED2L74 4F RT4A25 20050809000012005080900001EU 2005 8 9 MALA050631 120050728A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15452XJ 340B452 DURING 4K INSPECTION IN BNA, SEAT TRACK AT LBL 18.3 FROM FS 294-FS 310 IS CORRODED AND HAS BEEN REPAIRED IAW MESABA EO NR 212637 TASK 110. 2L72 4T RTA52EU 20050809000032005080900003EU 2005 8 9 MALA050635 120050807A3230 LANDING GEAR BAC 146 AVRO146RJ85A1500097EU RIGHT MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15513XJ E2329 RT MAIN GEAR RED IN TRANSIT LIGHT STAYED ON AFTER GEAR WAS SELECTED UP. REMAINED EXTENDED ALL LANDING GEAR IAW PQM CHECKLIST 7. AIR RETURN TO BGR. MAINTENANCE CLEANED AND LUBED GEAR SWUNG GEAR ALL CHECKS GOOD. IAW AVRO MM CHAP 32 DURING GEAR CHECKS FOUND RT OB BRAKE NO RELEASING REMOVED AND REPLACED BRAKE IAW JOBCARD 3240-501. ALL CHECKS GOOD. 2H74 4F RTA49EU 20050809000062005080900006WP 2005 8 9 IXXA05SMN94S 120050627A5730 SKIN DOUG DC8 DC871F 302199DWP ZONE 800 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 4813 DURING C CHECK INSPECTION, RT MLG REMOVE AND INSTALL CTR DOOR (LWR SKIN CRACKED). REMOVED AND REPLACED CTR MAIN PANEL ON RT MLG IN ACCORDANCE WITH DC-8 MM 32-12-1 PAGE 401. FOR OPS CHECK SEE J/C 74204. 2L74 4F RT4A25 20050809000082005080900008WP 2005 8 9 IXXA05SMN92S 120050623A5730 SKIN DOUG DC8 DC871F 302199DWP RT WING DELAMINATED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, RT WING UPPER T/E PANEL EXTERNAL SKIN DELAMINATED, XA 613.000 - XA 681.000. REMOVED AND REPLACED UPPER T/E PANEL ON RT WING XA 613.000 XA 681.000 IAW DC-8 SRM 51-3-0, DC-8 SRM 51-1-21 PAGE 1. TORQUED IAW DC-8 SRM 51-3-1. 2L74 4F RT4A25 20050809000092005080900009WP 2005 8 9 IXXA05SMN93S 120050627A5730 SKIN DOUG DC8 DC871F 302199DWP ZONE 600 DELAMINATED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, RT WING, T/E LWR PANEL EXTERNAL , INTERNAL SKIN DELAMINATED, XW 0.000 - XW 90.000. REMOVED AND REPLACED PANEL ON RT WING T/E, XW 0.000 XW 90.000 IAW DC-8 SRM 51-3-0 PAGE 1, DC-8 SRM 51-1-21 PAGE 14. TORQUED IAW DC-8 SRM 51-3-1. 2L74 4F RT4A25 20050809000112005080900011WP 2005 8 9 IXXA05SMN99S 120050627A5730 SKIN DOUG DC8 DC871F 302199DWP LT WING CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING C CHECK INSPECT, LT WING, SKIN UPPER PART WITH 02 CRACKS 1", 1/2", XRS 74.000 S-9 - S10. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-2-1 FIG 10, EO SEMAN NR 2005833 DATE 06-14-05. REMOVED DAMAGED AREA IAW DC-8 SRM 57-2-1 FIG 10 (SHEET 3). PERFORMED NDT INSPECT IAW DC-8 NDT SPM PART 06-10-01-001. NO CRACK, CORROSION FOUND. FAB`D REPAIR DOUBLER (ALCLAD 7075 T6 0.125), (02 EA) FILLERS PLUG (ALCLAD 7075 T6 0.175) PART DOUBLER FROM 0.125 TO 0.080 OVER 4 LENGTH (TYP BOTH ENDS) IAW DC-8 SRM 57-2-1 FIG 10 (SHEET 3). CLEANED, TREATED AND PRIMED AREA, REPAIR PARTS IAW DC-8 SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW DC-8 SRM 57-2-1 FIG 10 (SHEET 3), DC-82L74 4F RT4A25 20050809000122005080900012NM 2005 8 9 CALA0500254 120050805A531565C339501 FLOORBEAM BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718622 27526 INSPECTION FOUND THE AFT CABIN FLOORBEAM UPPER CHORD CORRODED AT STA 986.5, LBL 48 TO RBL 48. REPAIRED IAW ECRA 5311-01234. 2L72 4F RTA16WE 20050809000142005080900014NM 2005 8 9 CALA0500256 120050807A5330654576987 SKIN BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769351 23589 INSPECTION FOUND A 1" CRACK AND BULGING IN LOWER VHF ANTENNA SKIN AT AFT SIDE, STA 500 TO 500A, S28L TO S 28R. A REPAIR WAS INSTALLED IAW ECRA 5330-03471 AND A DIP WAS ISSUED TO PERFORM AN INITIAL INSPECTION WITHIN 60,000 CYCLES AND TO ACCOMPLISH REPETITIVE INSPECTIONS AT INTERVALS NOT TO EXCEED 30,000 FLIGHT CYCLES AFTER ACCOMPLISHMENT OF INITIAL INSPECTION. 2L72 4F RTA16WE 20050809000182005080900018WP 2005 8 9 IXXA05SMN91S 120050623A5752 SKIN DOUG DC8 DC871F 302199DWP AILERON TAB DAMAGED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, LT AILERON REMOVE AND REINSTALL TRIM TAB (UPPER SKIN HAS HOLES). REMOVED TRIM TAB FROM LT ALEIRON IAW DC-8 MM 27-13-1 PAGES 201-203. INSTALLED TRIM TAB ON LT AILERON IAW DC-8 MM 27-13-1 PAGES 203-208 (REPAIRED CONDITION). FOR OPS CHECK SEE NR 0818. 2L74 4F RT4A25 20050809000252005080900025WP 2005 8 9 IXXA05SMN58S 120050623A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED B IXXAO OTHER O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, EXTERNAL DOUBLER/TRIPLER FWD BASKET DOOR FWD LEFT UPPER CORNER. REPAIR DOES NOT CONFORM TO EVA 33-2614 USED FOR INSTALLATION. EVALUATE REPAIR FOR SRM CONFORMITY (53-2-0 FIG. 19, SHEET 1). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05270 DATE 06-29-05, SEMAN DWG ED 3996 DATE 06-27-05, EO SEMAN NR 2005898 DATE 06-29-05. REMOVED EXISTING REPAIR DOUBLER + TRIPLER IAW DC-8 SRM 51-1-21 PAGE 1, DC-8 SRM 51-1-20D PAGE 9. PERFORMED NDT INSPECTION IAW DC-8 NDT SPM PART 06-10-01-001. NO CRACK, CORROSION FOUND. FAB`D EXISTING REPAIR DOUBLER (ALCLAD 7075 T6 0.090), EXISTING REPAIR TRIPLER (ALCLAD 7075 T6 0.125) IAW SEMAN ED 3996, DC-8 SRM 51-1-4 PAGE 1. CLEANED, TREATED AND PRIMED ARE2L74 4F RT4A25 20050809000262005080900026EU 2005 8 9 DHL2005366500 120050715A5347 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAO OTHER O OTHER ININSP/MAINT 1 SO01366DH 249 DURING "C" CHECK, REPLACEMENT OF SECTIONS OF SEAT TRACKS. REF FOLLOWING N/R'S 1) 021484, " MAIN DECK, FLOOR SUPPORT PNLS 11-4R/11-5R HAS SEVERAL SPOTS OF CORROSION, BETWEEN FR 50 / FR 54, 2) N/R 021490 " MAIN DECK FLOOR SUPPORT ( PNL 10-4L) HAS CORROSION FWD OF FR 50, 3) N/R 021399 "MAIN CABIN FLOOR SEAT FLANGES HAVE SPOTS OF CORROSION BETWEEN FR 27 AND FR 34 AND BETWEEN B.L. "0" AND L.B.L 18". 4) N/R 021516 " MAIN DECK FLOOR STRUCTURE BELOW FLOOR PNL 1-5R HAS SEVERAL SPOTS OF CORROSION BETWEEN FR 19/FR 21. 5) N/R 021888 " MAIN CABIN FLOOR SEAT TRACK FLANGES HAVE SPOTS OF CORROSION BETWEEN FR 47 AND FR 49 AND RBL 18" 6) N/R 021487 "MAIN DECK FLOOR SUPPORT ( PNLS 10-2L) HAS CORROSION BETWEEN FR 47 / FR 50. 7) N/2L72 4F RTA35EU 20050809000282005080900028WP 2005 8 9 IXXA05SMN80S 120050623A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE DAMAGED B IXXAO OTHER O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING C CHECK INSPECT, EXTERNAL DOUBLER SKIN SPLICE FROM LONG 28 LT TO 28 RT; AFT EDGE RIVET SPACING EXCEEDS SRM LIMITS AFT SKIN SPLICE NON DOUG SRM UPGRADE REPAIR TO CONFORM TO DACO DC-8 SRM; FS 1696 L-36. (REF. 822BX-R68). PERFORMED MAJOR REPAIR IAW DC-8 SRM 53-2-1 FIG 8 (SHEET 1,2), EO SEMAN # 2005905 DATE 06-27-05. REMOVED EXISTING REPAIR DOUBLER IAW DC-8 SRM 51-1-21 PG 1. REMOVED DAMAGED AREA IAW DC-8 SRM 53-2-1 FIG 8 (SHEET 1,2) PERFORMED NDT INSPECT IAW NDT SPM PART 06-10-01-001. FAB`D NEW SKIN SEGMENT (ALCLAD 7075 T6 0.050) IAW DC-8 SRM 53-5-1 PG 2, FIG 1 ITEM “E”, EXTERNAL SPLICE DOUBLER (ALCLAD 7075 T6 0.063), (08 EA) INTERNAL FINGER DOUBLER (ALCLAD 7075 T6 0.032), (08 EA) INTERNAL DOUBLER (ALCLAD 72L74 4F RT4A25 20050809000302005080900030NM 2005 8 9 AWXA200500908 120050716A534069374118 STRINGER CLIP BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 DURING C18 CHECK DISCOVERED STRINGER TIE CRACKED, .200 INCHES IN LENGTH, AT BS 312, STR 28R. MAINTENANCE REMOVED STRINGER TIE AT BS 312, STR 28R, IAW BOEING 737-300 SRM 51-40-02. INSTALLED NEW STRINGER TIE AT BS 312, STR 28R IAW BOEING 737-300 SRM 51-40-02-0. 2L72 4F RTA16WE 20050809000312005080900031NM 2005 8 9 AWXA200500909 120050713A5320654587411 CLIP BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 DURING C18 CHECK DISCOVERED CLIP CRACKED, .375 INCHES IN LENGTH, AT BS 336 STRINGER 6R. MAINTENANCE REMOVED CRACKED CLIP AT BS 336 STRINGER 6R IAW BOEING 737-300 SRM 51-40-02-0 FIG 8. FABRICATED NEW CLIP IAW BOEING 737-300 DWG 65-45874 AND BOEING 51-30-01-0 FIG 3, 7, 8. INSTALLED FABRICATED REPAIR PARTS IAW BOEING 737-300 SRM 51-40-02-0 FIG 5, 8 , 12 AND BAC DWG 65-45874. 2L72 4F RTA16WE 20050809000322005080900032NM 2005 8 9 BB05062 120050803A2120 ODOR BOEING757 757225 1384959NM CABIN UNKNOWN A USAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA19608AU 22204 RDU FLT 274 EN ROUTE CLT TO BWI - DURING FLIGHT, THE MID CABIN SMOKE ALARM ACTIVATED. THE CABIN CREW REPORTED AN ELECTRICAL/SMOKE ODOR IN THE CABIN AT THE SAME TIME OF THE ALARM. THE FLIGHT DIVERTED TO RDU AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE. OK FOR SERVICE. 2L72 4F RTA2NM 20050809000332005080900033EU 2005 8 9 SA05094 120050804A335032145410 EPSU AIRBUSA319 A319112 3930323EU PASSENGER CABIN FAULTY A USAAK NONE O OTHER ININSP/MAINT 1 EA19708UW19626 972 CLT - THE RIGHT OVERWING EXIT LIGHT FLASHES DURING TEST. MAINTENANCE REPLACED THE RIGHT SIDE, MID CABIN EMERGENCY POWER SUPPLY UNIT AND BATTERY. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20050809000362005080900036EA 2005 8 9 SWIA200515358 120050623A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07905SW 7437 EMERGENCY FLOOR LIGHTING AFT OF OVERWING EXITS INOP. INSTALLED SERVICEABLE CONNECTOR ON AFT EMERGENCY FLOOR LIGHTING. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050809000372005080900037EA 2005 8 9 SWIA200515359 120050803A2750 FCU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED LDLANDING 1 NM07919SW 7657 FLAPS FAIL IN FLIGHT. REPLACED AND RERIGGED LEFT AND RIGHT BPSU AND FECU IAW 27-50-00. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050809000382005080900038EA 2005 8 9 SWIA200515360 120050730A2751855D10011 POSITION SENSOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07920SW1681 1681 7660 FLAPS FAIL MESSAGE IN FLIGHT. REPLACED BRAKE POSITION SENSOR UNIT ON LEFT SIDE REF 27-52-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050809000392005080900039SO 2005 8 9 SWIA200515361 120050729A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07250YV9131 9131 120250 EMERGENCY LIGHTS EXIT SIGN INOP AT ROW 6. REPLACED MIDDLE ELBP. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050809000422005080900042EA 2005 8 9 SWIA200515364 120050731A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLIGHT SPOILERS MALFUNCTIONED A SWIAC ABORTED TAKEOFF FJ FLT CONT AFFECTED WARNING INDICATION TOTAKEOFF 1 NM07915SW8001 8001 7615 DURING ROLL OUT IN DEN A "SPOILERONS FAULT" STATUS MESSAGE. REPLACED LEFT OUTBOARD SPOILERON PCU IAW CRJ 200 AMM 27-62-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050809000432005080900043EA 2005 8 9 SWIA200515365 120050730A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLIGHT SPOILERS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07982SW 7956 RIGHT SPOILERON FAILED FFOD TEST. REPLACED INBOARD PCU IAW CRJ MM 27-62-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050809000452005080900045EA 2005 8 9 SWIA200515367 120050620A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TOTAKEOFF 1 NM07970SW3772 3772 7881 UPON T/O RECEIVED A STAB CH 1 INOP STATUS MSG. INSTALLED A SERVICEABLE HSTCA & MCU IAW MM 27-40-00. MCU P/N: 7062-3 S/N OFF: 1212. 2L72 4F RTA21EA 20050809000462005080900046EA 2005 8 9 SWIA200515368 120050629A5610 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT FAILED A SWIAO OTHER O OTHER DEDESCENT 1 NM07965SW 7871 OUTER LAYER OF CAPTAIN WINDSHIELD SHATTERED. REPLACED CAPTAIN'S WINDSHIELD IAW MM 56-11-0. 2L72 4F RTA21EA 20050809000472005080900047NM 2005 8 9 AT0500025 120050803A29107972148501 LINE BOEING717 717200 1383700NM RROYCEBR700 BR700710A110 NE HYD SYSTEM CRACKED A ZZDAC ABORTED TAKEOFF K FLUID LOSS TOTAKEOFF 1 SO15977AT 55036 LOSS OF HYD PRESSURE AND QUANTITY AFTER TAKE OFF. FOUND CRACKED END ON GROUND SRV RETURN/PRESS LINE. REPAIRED END OF TUBING WITH PERM-A-SWAGE FITTING REF M/M 20-10 SERVICED HYD LEAK AND OPS CK GOOD. RAN NR 2 ENG, OPS CK EDP, OPS CK GOOD. 2L72 4F4 FTRA6WE E00057EN 20050809000502005080900050WP 2005 8 9 IXXA05SMN90S 120050623A5522 SKIN DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE RT ELEVATOR DELAMINATED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C-CHECK INSPECTION, RT ELEVATOR. REMOVE AND REINSTALL GEARED TAB (EXTERNAL SKIN DELAMINATED). REMOVED GEARED TAB FROM RT ELEVATOR IAW MM 27-30-3. INSTALLED GEARED TAB (OVERHAULED CONDITION) IAW MM 27-30-3. FOR OPS CHECK SEE NR 0818. 2L74 4F4 FRT4A25 E2GL 20050809000522005080900052EA 2005 8 9 ASOA05601 120050714A335020131A BATTERY CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 1 BATTERY DISCHARGED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27820AS 7188 DURING A GROUND INSPECTION, THE EMERGENCY FLOOR LIGHTS AT ROWS 2-4 WERE FOUND INOPERATIVE. MAINTENANCE CHARGED THE EMERGENCY LIGHT BATTERIES, CLEANED AND RESECURED THE CONNECTIONS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050809000572005080900057WP 2005 8 9 IXXA05SMN85S 120050623A5340 FITTING DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE FUSELAGE CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, MLG W/W FITTING CRACKED 4 INCHES, STA 940.000, RBL 5 INCHES. REMOVED CRACKED FITTING IAW SRM 51-1-20D. FABRICATED NEW FITTING IAW DWG NR 3643758 (ALCLAD 7075 T6 51). PERFORMED HEAT TREATMENT IAW SRM 51-1-11. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02 TO 07. CLEANED, TREATED AND PRIMED AREA + NEW FITTING IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11. INSTALLED NEW FITTING IAW SRM 51-1-20D. TORQUED IAW SRM 51-3-1. 2L74 4F4 FRT4A25 E2GL 20050809000602005080900060EU 2005 8 9 ALGA105148 120050724A6510C651A2001101 TAIL WHEEL UROCOPEC120 EC120B 8680987EU TMECA ARRIUSARRIU2F NE CRACKED B ALGAK NONE O OTHER ININSP/MAINT 1 SW03524AL837 1263 CRACKED LAMINATE / REPLACED WITH NEW BY FIELD MAINTENANCE. 1G72 3U3 UNCR0001RD E34NE 20050809000662005080900066CE 2005 8 9 2005F00091 120050726A2910S1236C40134 HOSE CESSNA177 177RG 2073709CE LYC O360 IO360A1B6 41514EA HYD SYSTEM FAILED G A UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA01545PZ5746 177RG1023 HYDRAULIC HOSE TO NOSE LANDING GEAR CYLINDER FAILED IN FLIGHT. THIS CAUSED TOTAL DEPLETION OF HYDRAULIC FLUID AND SUBSEQUENT HYDRAULIC PUMP FAILURE. PILOT WAS UNABLE TO EXTEND LANDING GEAR MANUALLY BECAUSE OF NOT ENOUGH FLUID. A GEAR UP LANDING WAS MADE WITH MINOR DAMAGE TO AIRCRAFT. 1H71 3O3 O A20CE 1E10 20050809000682005080900068NM 2005 8 9 176 120050805A5347 SEAT TRACK BOEING757 757232 1384965NM PWA 2037 PW2037 NE FUSELAGE CORRODED B DU4RO OTHER O OTHER ININSP/MAINT 1 SO15624DL 22914 CORROSION ON SEAT TRACKS LT SIDE IB AND OB AT BS 780 - 800. S/O 283001, DELTA NR NR21386. 2L72 4F4 FRTA2NM E17NE 20050809000712005080900071NM 2005 8 9 172 120050805A5320 THRESHOLD BOEING757 757232 1384965NM PWA 2037 PW2037 NE FUSELAGE CORRODED B DU4RO OTHER O OTHER ININSP/MAINT 1 SO15624DL 22914 CORROSION AT STA. 1440 ON MAIN STRUCTURE UNDER THRESHOLD Z-ANGLE CORROSION AT 6 FASTENERS. S/O 283001, DELTA N//R NR22456 2L72 4F4 FRTA2NM E17NE 20050809000722005080900072NM 2005 8 9 173 120050805A5313 STRINGER BOEING757 757232 1384965NM PWA 2037 PW2037 NE FUSELAGE CORRODED B DU4RO OTHER O OTHER ININSP/MAINT 1 SO15624DL 22914 CORROSION AT STR. 28R AT BS 650. S/O 283001, DELTA N//R NR 22590 2L72 4F4 FRTA2NM E17NE 20050809000742005080900074NM 2005 8 9 175 120050805A5320 CLIP BOEING757 757232 1384965NM PWA 2037 PW2037 NE FUSELAGE CORRODED B DU4RO OTHER O OTHER ININSP/MAINT 1 SO15624DL 22914 CORROSION, AFT CARGO ACCS AREA SHEAR CLIP BS 1681 S-22-S-23. S/O 283001, DELTA N//R NR 21000. 2L72 4F4 FRTA2NM E17NE 20050809000752005080900075NM 2005 8 9 ASMF200508001 120050803A3241 SOCKET HYDROAIRE DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE ANTISKID CONTROLDAMAGED W ASMFK NONE J WARNING INDICATION ININSP/MAINT 1 SW23831LF D887C 53050 DURING TRANSIT SERVICE, PERFORMED ANTISKID TEST, THE CIRCUIT BREAKER R-41 WAS ACTIVATED AND WOULD NOT RESEAT IT. ANTISKID VALVES CONNECTORS WERE DISCONNECTED AND TRANSDUCERS WERE CHECKED OF 4 MAIN WHEELS AND FAIL CONTINUE. ANTISKID CONTROL BOX WAS REPLACED IAW MM 32-43-00 AND FAIL CONTINUE. THE (WHEEL NOT TURNING) SOCKET WAS CHECKED IAW WDM 32-41-00, AND WAS DETECTED DAMAGED. SOCKET WAS REPAIRED AND TESTED IAW MM 32-43-00, ALL CORRECT. 2L72 4F4 FRT E9NE 20050809000902005080900090NE 2005 8 9 ASMF200508002 220050803A7200 BLADE GE CFM567B22 BOEING737 73776N 13844CHNM CFMINTCFM567CFM567B22 13802NE ENGINE DAMAGED W ASMFD RETURN TO BLOCK C F.O.D. CLCLIMB 1 SW23850AM 890620 33786 AIRCRAFT RETURNED TO DEPARTURE, BIRD STRIKE ON RT ENGINE. DURING MAINTENANCE REVISION, 3 ENGINE BLADES WERE DETECTED DAMAGED. AIRCRAFT WAS SENT TO THE HANGAR AND INSPECTION WAS ACCOMPLISHED IAW MM 71-00-00, 4 PAIRS OF ENGINE BLADES WERE REPLACED IAW MM 72-21-02 AND TEST WAS PERFORMED IAW MM 71-00-00, ALL CORRECT. 2L72 4F4 FRTA16WE E00055EN 20050809000952005080900095SO 2005 8 9 SIMA200519301 120050701A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FRAME 25 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21854AE4798 145743 THE CENTER OMEGA BEAM AT FRAME 25 WAS FOUND TO BE CORRODED. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED A DOUBLER, FILLER AND SHIMS. REPAIR DONE IAW SRM. (K) 2L72 4F4 FRTT00011ATTE6CH 20050809000962005080900096SO 2005 8 9 SIMA200519303 120050629A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FRAME 20 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21854AE 145743 THE LT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. REMOVED THE COROSION BY MAKING A CUT OUT. FABRICATED A FILLER EXTERNAL ANGLE, PLATE AND 2 SHIMS. REPAIR DONE IAW SRM. (K) 2L72 4F4 FRTT00011ATTE6CH 20050809000982005080900098SO 2005 8 9 SIMA200519308 120050626A531014533888001 STRUCTURE EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21809AE 145521 DURING INSPECTION, FOUND STRINGER 19 LT CHAFED BETWEEN FRAMES 52, 53. REPLACED DAMAGED STRINGER IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4F4 FRTT00011ATTE6CH 20050809000992005080900099SO 2005 8 9 SIMA200519309 120050626A532014521700005 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO ALLSN AE3007AE3007A 03030GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21809AE 145521 DURING INSPECTION, FOUND FWD CABIN FLOOR OMEGA SHAPE HAS CORROSION AT FRAME 20. INSTALLED NEW DOUBLER IAW SRM. AC WAS RETURNED TO SERVICE. (K) 2L72 4F4 FRTT00011ATTE6CH 20050809001002005080900100SO 2005 8 9 SIMA200519302 120050630A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FRAME 25 LT CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21854AE4798 145743 THE LT OMEGA BEAM AT FRAME 25 WAS FOUND TO BE CORRODED. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED A FILLER, DOUBLER AND 2 SHIMS. REPAIR DONE IAW SRM. (K) 2L72 4F4 FRTT00011ATTE6CH 20050809001032005080900103SO 2005 8 9 SIMA200519310 120050705A532014525381003 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FRAME 20 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21649PP11879 145234 PREVIOUS REPAIR ON THE LT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. REMOVED THE CORRODED REPAIR PART. FABRICATED A FILLER, EXTERNAL ANGLE, 2 SHIMS AND PLATE. REPAIR DONE IAW SRM. (K) 2L72 4T4 FRTT00011ATTE6CH 20050809001042005080900104NM 2005 8 9 USAA050899 120050721A5330 SKIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19441US 24812 CLT - Q - SKIN, 12 INCHES X .250 INCH X .015 INCH, SKIN WEAR, BS870, WL306.5, LBL3. INSTALLED REPAIR DOUBLER AND INSTALLED NEW RUB STRIPS IAW EA, WEIGHT CHANGE OF 1.5 LBS. (K) 2L72 4F4 FRTA16WE E21EU 20050809001062005080900106NM 2005 8 9 USAA050901 120050721A5743 SUPPORT FITTING BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU MLG BEAM ATTACH CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19441US40664 24812 CLT - Q5 - AFT SUPPORT FITTING, 1 INCH, CRACKED, FASTENER HOLE AT MLG BEAM ATTACH PT TO AFT SPAR ON AFT SUPPORT FITTING UP CHRD. REPAIR OF FITTING INCLUDED REAMING OF DISCREP HOLE, SHIMMING IAW EA. (K) 2L72 4F4 FRTA16WE E21EU 20050809001102005080900110EA 2005 8 9 ASOA05605 120050715A33501317 LAMP BRUCE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27905EV 7632 DURING AN A-CHECK, THE RT FWD EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE RT FWD EXTERIOR EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050809001132005080900113EA 2005 8 9 ASO2005F00005 120050713A5340601R3119992 FAIRING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT WING DAMAGED A ASOAK NONE O OTHER TOTAKEOFF 1 SO27902EV 7620 DURING TAKEOFF, TOWER INFORMED CREW THAT TIRE DEBRIS WAS NOTIED ON RUNWAY AFTER DEPARTURE. THERE WERE NO INDICATIONS OF ENGINE DAMAGE AND AC CONTINUED. EMERGENCY WAS DECLARED AND EMERGENCY VEHICLES WERE REQUESTED TO BE ON STANDBY AS PRECAUTION. AC LANDED SAFELY. UPON TOUCHDOWN, FIRE AND RESCUE CONFIRMED IB RT MAIN TIRE WAS SHREDDED. MAINT REMOVED AND REPLACED RT MLG IB AND OB WHEEL AND TIRE ASSEMBLIES. ALSO, FOUND RT IB FLAP ASSEMBLY, RT WING TRAILING EDGE FAIRING AND RT SIDE AFT BELLY FARING DAMAGED. MAINTENANCE REMOVED AND REPLACED RT IB FLAP ASSY AND T WING T/E FAIRING. MAINT REPAIRED THE RT SIDE AFT BELLY FAIRING IAW SRM. OPS CHECKS GOOD. AC OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050809001172005080900117NM 2005 8 9 USAA050880 120050714A5314 FLANGE BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU KEELBEAM WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19526AU 23861 CLT - Q2 - KEELBEAM FLANGE, 60 INCHES SURFACE WEAR. FUSELAGE KEELBEAM LT OB FLANGE STA 664-727. INSTALLED REPAIR STRAP IAW EA. (K) 2L72 4F4 FRTA16WE E21EU 20050809001222005080900122NM 2005 8 9 USAA050886 120050718A5320 WEB BOEING737 737301 1384611NM CFMINTCFM56 CFM563B2 13802EU AIRFRAME DENTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19590US52349 23935 BFM - Q6 - WEB SKIN, 18 INCH X 2.0 INCH X .040 INCH DENT. BS 1016, BTW STR 24R-27R. FAB DOUBLER, FILLER, NEW SKIN SECTION, INSTALLED IAW EA AND SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050809001232005080900123NM 2005 8 9 USAA050885 120050718A532069620146 VERTICAL SUPPORT BOEING737 737301 1384611NM CFMINTCFM56 CFM563B2 13802EU AIRFRAME CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19590US 23935 BFM - Q6 - VERTICAL STIFFENER, 1.0 INCH RACK, CRACKED, WHEEL WELL FWD BULKHEAD 663 LBL 6.15. REPLACED STIFFENER IAW EA AND SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050809001282005080900128SO 2005 8 9 SIMA200517805 120050624A3350 WIRE EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT BROKEN A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21841AE 145667 DISC - EMERGENCY LIGHT AT OVERHEAD SERVICE DOOR INOPERATIVE. FOUND WIRE SPLICE BROKEN. REPAIRED WIRING. OPERATIONAL CHECKED GOOD. AC RETURNED TO SERVICE. (K) 2L72 4F4 FRTT00011ATTE6CH 20050809001292005080900129NM 2005 8 9 05FDEA02232 120050803A5230 DOUBLER BOEING727 727233 138408ANM CARGO DOOR GOUGED A FDEAO OTHER O OTHER ININSP/MAINT 1 SO25218FE 21101 MAIN CARGO DOOR FORWARD SIDE FRAME GOUGED ON REPAIR DOUBLER MIDWAY UP DOOR. INSTALLED NEW RAPAIR DOUBLER PER FED EX EZA 7-5230-92257 2L73 4F RTA3WE 20050809001302005080900130CE 2005 8 9 DJFA2005125 120050803A324345AS38401012 MASTER CYLINDER BEECH MU300 400A 1155402CE BRAKES LEAKING E DJFAO OTHER K FLUID LOSS LDLANDING 1 EA23793TA RK244 THE CREW REPORTED UPON LANDING, THERE WERE NO BRAKES. USED THE EMERGENCY BRAKE SYSTEM TO STOP THE AIRCRAFT. THE CREW TRIED THE NORMAL BRAKES AFTER ROLLOUT ONTO THE TAXIWAY AND THE BRAKES WERE AVAILABLE BUT WERE JERKY. MAINTENANCE FOUND THE PILOTS RIGHT MASTER CYLINDER TO BE LEAKING. THE MASTER CYLINDER WAS REPLACED AND THE SYSTEM WAS BLED. WHILE TESTING THE ANTI-SKID SYSTEM, THERE WAS NO RESPONSE FROM THE RIGHT SIDE AND THE LEFT SIDE WAS INTERMITTANT. PIN CONNECTIONS FOR THE LEFT AND RIGHT WHEEL TRANSDUCER, AND THE ANTI-SKID CONTROL BOX WERE REPAIRED. THE ANTI-SKID CONTROL BOX WAS REPLACED WHEN NO RESPONSE WAS RECEIVED FROM THE RIGHT SIDE. OPERATIONAL TESTS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERV2H72 4F RTA16SW 20050809001312005080900131NM 2005 8 9 05FDEA02220 120050803A5340 STRINGER CLIP BOEING727 727227 1384078NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 STRINGER CLIP AT BS 950B STR 7LT IS CRACKED. REPLACED STRINGER CLIP AT BS 950B STR 7LT PER SRM 51-30-2 2L73 4F A3WE 20050809001322005080900132NM 2005 8 9 05FDEA02221 120050803A5340 STRINGER CLIP BOEING727 727227 1384078NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 STRINGER CLIP AT BS 950C STR 7 LT IS CRACKED. REPLACED STRINGER CLIP AT BS 950C, STR 7LT PER SRM 51-30-2. 2L73 4F A3WE 20050809001332005080900133NM 2005 8 9 05FDEA02222 120050803A5340 STRINGER CLIP BOEING727 727227 1384078NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 STRINGER CLIP AT BS 950D STR 7L IS CRACKED. REPLACED STRINGER CLIP AT BS 950D, STR. 7LT PER SRM 51-30-2. 2L73 4F A3WE 20050809001342005080900134NM 2005 8 9 05FDEA02223 120050803A5340 STRINGER CLIP BOEING727 727227 1384078NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 STRINGER CLIP AT BS 950F STR 7LT IS CRACKED. REPLACED STRINGER CLIP AT BS 950F, STR 7LT PER SRM 51-30-2 2L73 4F A3WE 20050809001352005080900135NM 2005 8 9 05FDEA02224 120050803A5330 SKIN BOEING727 727227 1384078NM FUSELAGE UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 EVALUATE TO DETERMINE IF REPAIR IS MAJOR OR MINOR AND IF REPAIR IS IN ACCORDANCE WITH FAA APPROVED DATA, EXTERNAL REPAIR B/S 1105 STR 25-26L. INSTALLED EXTERNAL REPAIR DOUBLER PER SRM 53-30-3 MINOR REPAIR. 2L73 4F A3WE 20050809001392005080900139WP 2005 8 9 ASAA0580358 120050628A561059644201 WINDOW DOUG DC9 DC983 3022083WP COCKPIT DISENGAGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM02979AS31926 53471 PREFLIGHT CHECK, FOUND COCKPIT LEFT SLIDING WINDOW COULD NOT BE OPENED. REPOSITIONED FORWARD UPPER LATCH PIN IN CHANNEL TRACK. WINDOW THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20050810003002005081000300EA 2005 8 10 A6WA200540258 120050721A53466013500625 BEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FS 625 DENTED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31420AW 7640 NESTED ANGLE ON FWD WEB OF ENGINE BEAM HAS A DEEP GOUGE IN RADIUS APPROX .300 INCH LONG X .075 INCH WIDE AND .050 DEEP. REMOVED DAMAGED SECTION OF NESTING ANGLE. FABRICATED AND INSTALLED REPAIR PARTS IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050809001402005080900140WP 2005 8 9 ASAA0580356 120050626A561059644201 WINDOW DOUG DC9 DC983 3022083WP COCKPIT DISENGAGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM02979AS31906 53471 PREFLIGHT CHECK, COCKPIT LEFT SLIDING WINDOW COULD NOT BE OPENED. REPOSITIONED FORWARD UPPER LATCH PIN IN CHANNEL TRACK. WINDOW THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20050809001412005080900141WP 2005 8 9 ASAA0580359 120050628A561059644201 WINDOW DOUG DC9 DC983 3022083WP COCKPIT DISENGAGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM02979AS31926 53471 PREFLIGHT CHECK, FOUND COCKPIT LEFT SLIDING WINDOW COULD NOT BE OPENED, 2ND OCCURRENCE ON SAME DAY AND 4TH OCCURRENCE IN LAST THREE DAYS. REPOSITIONED FORWARD UPPER LATCH PIN IN CHANNEL TRACK. WINDOW THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20050805000872005080500087NM 2005 8 5 SWAA052284 120050801A551265C25727 SKIN BOEING737 7373H4 1384600NM HORIZONTAL STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29315SW 23337 DURING SCHEDULED C2 CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED AT INBOARD AFT SPAR. REPAIRED HORIZONTAL STAB PER SRM. 2L72 4F RTA16WE 20050805000912005080500091NM 2005 8 5 SWAA052289 120050802A53116545808 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29610WN 27696 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303, STR 16L. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20050805000942005080500094NM 2005 8 5 SWAA052292 120050802A55536546874 ATTACH FITTING BOEING737 7373H4 1384600NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29610WN 27696 DURING SCHEDULED D-CHECK, FOUND LEFT & RIGHT VERTICAL STAB PRIMARY & FAIL-SAFE ATTACH FITTINGS FWD & AFT CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER. 2L72 4F RTA16WE 20050805000992005080500099NM 2005 8 5 SWAA052271 120050801A53156546806 FLOORBEAM BOEING737 7373H4 1384600NM FUSLEAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 867, LBL 7. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20050805001062005080500106NM 2005 8 5 SWAA052278 120050801A53306545776 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29512SW 24189 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 945, STR 24R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050805001302005080500130WP 2005 8 5 05FDEA02171 120050802A5320ARB03232 STIFFENER DOUG MD10 MD1010F 3022112WP BULKHEAD CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25381FE 46615 INTERNAL LOWER FUSELAGE CAC BULKHEAD RT SIDE FOUND 1 EACH CRACK 6 INCHES LONG ON VERTICAL STIFFENER STA 1159 X=-81 Z=-29. PERFORMED REPAIR IAW SRM 57-00-01 FIG 11 VOL 1. 2L73 4F RTA22WE 20050805001382005080500138NM 2005 8 5 SWAA052303 120050803A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 301.2, STR 17R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050805001432005080500143NM 2005 8 5 05FDEA02213 120050803A5710 SKIN DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 RIGHT HAND WING UPPER SURFACE TRAILING EDGE FORWARD OF OUTBOARD AILERON SKIN BULGE FOUND AT XORS 989. RTW UPPER SURFACE T/E FWD OF O/B AILERON XORS 989 SKIN BULGE AREA CORROSION REMOVED. MAT'L REMOVED:0.035"; ORIGINAL THK: 0.150"; MAT'L REMAINED: 0.115"; FOUND EXCEED LIMIT PER SRM 57-10-00 FIG 32 VOL I. AREA REPAIR C/O PER FEDEX EA:1-5710-87559 - WINGS R/H UPPER WING SKIN CORROSION REPAIRS AT XORS 845,XORS 979, XORS 989, COMMON TO THE T/E. REPAIR CLASSIFIED AS MAJOR PER GMM6-2-100. 2L73 4F RTA22WE 20050805001522005080500152NM 2005 8 5 SWAA052312 120050801A5344BAC1507 HINGE BRACKET BOEING737 7373H4 1384600NM L1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29604SW 27955 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR UPPER HINGE BOX FITTING CRACKED. REMOVED AND REPLACED UPPER HINGE BOX PER SRM. 2L72 4F RTA16WE 20050805001582005080500158NM 2005 8 5 DL738050380 120050720A49201319B APU BOEING737 737832 13844CFNM APU BAY SMOKE A DALAK NONE A FLAME/FIRE ININSP/MAINT 1 SO27373DA8993 29621 ON L/O, FOUND APU LOW ON OIL. SERVICED APU. ON APU START ATTEMPT, FOUND HEAVY SMOKING IN APU COMPARTMENT WITH TORCHING FROM APU EXHAUST. REPLACED APU. 2L72 4F RTA16WE 20050805001642005080500164GL 2005 8 5 DL764050388 220050721A7200CF680C2B8F ENGINE BOEING767 767432ER 1385134NM GE CF6 CF680C2* GL NR 2 FAILED A DALAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 SO27836MH1484114841 29709 706225 DURING APPROACH, THROTTLES WERE PLACED AT IDLE FOR A SPEED REDUCTION. WHEN THROTTLES WERE ADVANCED HEARD A NOISE, RIGHT ENGINE STARTED TO SLOWLY ROLL BACK, SHUT DOWN ENG PER QRH. REPLACED NR 2 ENGINE. 2L72 4F4 FRTA1NM E23EA 20050808000172005080800017EA 2005 8 8 COMA0560417 120050728A2750860D10018BCD FCU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO01937CA3178 7044 FLAPS FAIL CAUTION. REPLACED THE FECU. 2L72 4F RTA21EA 20050808000232005080800023 2005 8 8 SA05093 420050802A2565D30665105 SLIDE AIRBUS320 A320214 3930316EU PASSENGER CABIN DAMAGED A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19113UW15048 1141 BOS - DURING A SLIDE TIME CHANGE, THE REPLACEMENT SLIDE WAS FOUND DEFECTIVE FROM STOCK WITH LANYARDS FOR THE GIRT BARS TORN IN HALF. THE SLIDE WAS NOT INSTALLED. MAINTENANCE RETURNED THE SLIDE FOR REPAIR. THE SLIDE TIME CHANGE OCCURRED THREE DAYS LATER WITH A SERVICEABLE SLIDE. 2L72 4F RTA28NM 20050808000442005080800044NE 2005 8 8 DL73S050399 220050723A751065581232 DUCT BOEING737 737232 1384475NM PWA JT8 JT8D15A 52051NE NR 2 ENGINE PERFORATED A DALAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO27331DL 23103 717155 ON T/O AT 3500FT, NR 2 ENG OVHT LIGHT ILLUMINATED. WHEN THRUST LEVER PULLED TO IDLE IAW QRK PROCEDURE LIGHT WENT OUTMADE RETURN LANDING AT CVG. REPLACED BLOWN ANTI-ICE DUCT. 2L72 4F4 FRTA16WE E2EA 20050808000602005080800060NM 2005 8 8 DL76S050418 120050729A7500UNKN BALL JOINT BOEING767 767332 1382001NM GE CF6 CF680A 30025NE NR 2 ENGINE UNKNOWN A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27130DL 24080 580255 ON TAKEOFF GOT VERY RAPID INTERMITTENT R ENG FIRE WARNING. ALSO, GOT INTERMITTENT R ENG FIRE LOOP 1 STATUS MSG. FIRE WARNING GOES AWAY WHEN BELOW ABOUT 85 PERCENT N1. T/S PER FIM. FIRE AND O/H LOOP RESISTANCE VALUES NORM. RAN ENG TO TAKEOFF POWER PER PFHB. RT ENG FIRE LOOP 1 MSG AT 80 % N1. FIRE WARNING AT 103 PERCENT N1. OPENED RT ENG EVIDENCE OF DUCT LEAK JUST UPSTREAM OF PRECOOLER. BACK PRESSURED WITH APU AIRFOUND MULTIPLE DUCT LEAKS. REPLACED CLAMP AND SEAL 8TH STAGE DUCT TO PRECOOLER. REPLACED BALL JOINT AT 8TH STAGE CHECK VALVE. TIGHTENED BALL JOINTS AT HPSOV AND 8TH STAGE CK VLV. 2L72 4F4 FRTA1NM E13NE 20050808000632005080800063NM 2005 8 8 DLM88050421 120050731A4990 CAP DOUG MD88 MD88 3023688NM PWA JT8 JT8D* NE APU OIL LEAKING A DALAA UNSCHED LANDING KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27981DL16106 53268 P80308 SMOKE IN THE CABIN REPORTED BY FLIGHT ATTEND. ATB TO CVG. FOUND PACKING ON APU OIL CAP LEAKING. REPLACED AND PERFORMED DUCT BURNOUT WITH APU INLET WASH. 2L72 4F4 FRTA6WE E2EA 20050808000652005080800065NM 2005 8 8 DL764050424 120050731A2781 TARGET BOEING767 767432ER 1385134NM NR 8 SLAT BROKEN A DALAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 SO27829MH 29700 LE SLATS WOULD NOT EXTEND. FOUND S304 NR 8 OUTBOARD SENSOR TARGET BROKEN. REPLACED BOLT OPS CK OK. 2L72 4F RTA1NM 20050808000702005080800070 2005 8 8 DL764050429 420050804A3130230001487 RECORDER BOEING767 767432ER 1385134NM COCKPIT OVERHEATED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27832MH 29704 UPON ARRIVAL AT A/C, COCKPIT HAD ELECTRICAL ODOR. REPLACED OVERHEATED TAPE REPRODUCER. 2L72 4F RTA1NM 20050808000732005080800073WP 2005 8 8 UPS05845046 120050713A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 F/S 960 LBL 60 FLOORBEAM AT LIGHTING HOLE ON VERT FLANGE AT CENTER OF HOLE HAS A 5" CRACK GOING AT HORIZ ANGLE. STOP DRILLED CRACKED FLOORBEAM, FABRICATED AND INSTALLED 2. REPAIR ANGLES IAW SAA SK 807-858978 AND UPS EODC8-53-20486. 2L74 4F RT4A25 20050808000772005080800077WP 2005 8 8 UPS05845052 120050706A5320SAA58903142 INTERCOSTAL DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 STA 70 RBL 48 UNDER THE SEAT TRACK INTERCOSTAL HAS HEAVY CORROSION. REMOVED, FABRICATED AND INSTALLED INTERCOSTAL IAW SRM 51-1-20D, 51-3-2 AND DWG 5890314. 2L74 4F RT4A25 20050808000812005080800081EA 2005 8 8 COMA0560415 120050728A262047359719 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY UNRELIABLE A COMAF ACTIVATE FIRE EXT. N FALSE WARNING DEDESCENT 1 SO01959CA9979 6246 7116 SMOKE CARGO WARNING, BOTTLES DISCHARGED. REPLACED SMOKE DETECTORS AND FIRE BOTTLES. 2L72 4F RTA21EA 20050808000822005080800082EA 2005 8 8 COMA0560416 120050728A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01473CA 7668 FLIGHT 5877 - LEFT ENGINE THRUST REVERSER UNLOCKED WARNING. DEFERRED MAINTENANCE ON THRUST REVERSER PER MEL. 2L72 4F RTA21EA 20050808000912005080800091NM 2005 8 8 BB05061 120050803A3350 LIGHT BOEING767 767201 1385125NM CABIN INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19648US 23900 PHL - THE FLOOR EMERGENCY ESCAPE PATH LIGHTING ON THE AIRCRAFT RIGHT SIDE, FROM SEAT 19 TO 27, WERE FOUND INOPERATIVE. MAINTENANCE REPAIRED THE FLOOR WIRING. OPERATIONALLY CHECKS OK. 2L72 4F RTA1NM 20050808001002005080800100NM 2005 8 8 QXEA200501147 120050803A216078279018 ACM DHAV DHC8 DHC8202 2809007NM SEIZED A QXEAO OTHER O OTHER CLCLIMB 1 NM09347PH317693203 480 SEA FLIGHT NR 2044 UNABLE TO CONTROL COCKPIT/CABIN TEMPERATURE. EMERGENCY CHECKLIST FAILED TO CONTROL TEMPS BELOW 60 DEGREES DUCT TEMP. DUCT TEMP REDUCED TO 40 DEGREES AFTER UNPRESSURIZING AND RAM VENTILATION. MAINTENANCE INSPECTED AND FOUND AIR CYCLE MACHINE TURBINE SEIZED. REPLACED AIR CYCLE MACHINE IAW D8 AMM 21-50-11, PAGES 401-406. FUNCTIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050808001262005080800126NM 2005 8 8 05FDEA02235 120050803A5330 SKIN DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 EXTERIOR FUSELAGE SKIN HAS CORROSION AT STA 1674 LONGERON 52 BELOW ANTENNA MOUNT. EXTERIOR FUSELAGE SKIN AT STA 1674 LONGERON 52 BELOW LIGHT MOUNT INNER DOUBLER FINGER REMOVED AS PER SRM 51-35-01 VOL II. NEW INNER DOUBLER FINGER FABRICATED AS PER DRAWING AFA 3088 AND INSTALLED AS PER SRM 51-38-01 VOL II. NEW REPAIR DOUBLER AND FILLER INSTALLED AS PER SRM 53-20-00 VOL I FIG 2. MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050808001282005080800128NM 2005 8 8 05FDEA02237 120050803A5230BAC45A BUMPER BLOCK BOEING727 727200 138407ENM FWD LWR CARGO CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 FORWARD LWR CARGO DOOR HANDLE BUMPER STOP BRACKET IS CRACKED. REMOVED AND REPLACED BUMPER IAW SRM 51-30-2. 2L73 4F RTA3WE 20050808001342005080800134EA 2005 8 8 VNAA0507017 120050721A2810 CAP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUEL CELL MISSING A VNAAO OTHER C F.O.D. NRNOT REPORTED 1 GL05261PS 7959 DURING PREFLIGHT, BEFORE FIRST FLIGHT OF THE DAY, THE CREW DISCOVERED THE SINGLE POINT FUEL CAP MISSING. UPON FURTHER INSPECTION THE RIGHT ENGINE INLET COWL WAS FOUND DAMAGED. AFTER INSPECTION THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE INSTALLED A NEW SINGLE POINT FUEL CAP AND COMPLIED WITH A TEMPORARY REPAIR TO THE RT ENGINE INLET COWL IAW BOMBARDIER REO 601R-71-61-2990. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050808001432005080800143EA 2005 8 8 VNAA0507020 120050728A5320 RADOME CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE LIGHTNING STRIKEA VNAAO OTHER O OTHER APAPPROACH 1 GL05223JS 7892 THE CREW REPORTED A POSSIBLE LIGHTNING STRIKE. MAINTENANCE COMPLIED WITH LIGHTNING STRIKE INSPECTIONS IAW CRJ200 AMM 05-51-05-210-801 & 05-51-05-220-801. MINOR PAINT DAMAGE ON THE RADOME WAS DAI'D. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050808001472005080800147NM 2005 8 8 05FDEA02255 120050804A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 MAIN DECK, SEAT TRACK LBL 11 CORRODED AT STA 859. 2L73 4F RTA22WE 20050808001512005080800151SO 2005 8 8 RAIA00508003 120050803A7830 WARNING LIGHT EMB 145 EMB145 3260210SO THRUST REVERSER ILLUMINATED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03820HK 145064 FLT 3587 - PIT - ENGINE 2 THRUST REVERSER DISAGREE WARNING. MAINTENANCE DEFERRED NR 2 T/R PER MEL. 2L72 4F RTT00011AT 20050808001552005080800155NM 2005 8 8 05FDEA02260 120050804A5320 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 UPPER CARGO SEAT TRACK RBL 47 CORRODED AT STA 1696. CARRIED OUT REPAIR AS PER SRM 53-70-00. 2L73 4F RTA22WE 20050808001702005080800170EA 2005 8 8 SWIA200515369 120050731A274070623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA MOTOR MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07934SW4108 4108 7722 STAB CHANNEL 1 WOULD NOT ENGAGE. REPLACED MCU IAW MM 27-42-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050808001832005080800183WP 2005 8 8 IXXA05SMN84S 120050623A5340 FITTING DOUG DC8 DC871F 302199DWP FUSLEAGE CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING C CHECK INSPECT, MLG W/W FRAME FITTING CORRODED, STA 960.000 L-24. PERFORMED MAJOR REPAIR IAW DC-8 SRM 53-1-0 PG 1, DC-8 SRM 53-2-0 FIG. 8 (SHEET 1), EO SEMAN # 2005845 DATE 06-27-05. REMOVED CORROSION IAW DC-8 SRM 51-1-8 PG 17, 18, FOUND OUT OF LIMITS IAW DC-8 SRM 53-2-0 FIG 1F (SHEET 3) PAGE 2P. REMOVED CORRODED FRAME FITTING IAW DC-8 SRM 51-1-20D PG 21. FAB`D FRAME FITTING (NEW) (ALCLAD 7075 T6 51) IAW DWG DOUGLAS NR 3647117, EO SEMAN # 2005842. PERFORMED HEAT TREATMENT IAW DC-8 SRM 51-1-1 PG 1, 13, 17. PERFORMED NDT INSPECT IAW DC-8 SPM PART 08-00-02 TO 07. CLEANED, TREATED AND PRIMED AREA, NEW FRAME FITTING IAW DC-8 SRM 51-1-8B. TRIMMED OUT NEW FITTING TO INSTALL IAW DC-8 SRM 53-2-0 FIG 8 (SHEE2L74 4F RT4A25 20050808001892005080800189WP 2005 8 8 IXXA05SMN75S 120050623A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE DAMAGED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING C CHECK INSPECTION, EXTERNAL DOUBLER ON WINDOW BELT AREA ABOVE C-PIT BASKET DOOR OLD UNITED AIRLINES INSUFFICIENT SIZE OF LOWER EXTENSION UPGRADE DOUBLER TO CONFORM TO THE CURRENT DACO DC-8 SRM REQUIREMENTS (REF. 822BX-R59), STA FS 1400.000 L-15.5R. PERFORMED MAJOR REPAIR IAW DC-8 SRM 53-2-0 FIG 22A TR # 53-170 DATE 09-20-03, EO SEMAN NR 2005878 DATE 06-13-05. REMOVED EXISTING REPAIR DOUBLER IAW DC-8 SRM 51-1-21 PAGE 1, DC-8 SRM 51-1-20D PAGE 21. FABRICATED REPAIR DOUBLER (ALCLAD 7075 T6 0.190”) IAW DC-8 SRM 53-2-0 FIG 22A SHEET 1, 7, TR NR 53-170, DC-8 SRM 53-4-1 FIG 19 ITEM B, DC-8 SRM 51-1-4 PAGE 1. CLEANED, TREATED AND PRIMED AREA + REPAIR DOUBLER IAW DC-8 SRM 51-1-8B. APPLIED PRC SEALANT TO FAY2L74 4F RT4A25 20050809000132005080900013NM 2005 8 9 CALA0500255 120050805A531565C339502 FLOORBEAM BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2719621 27334 INSPECTION FOUND FLOORBEAM CORRODED AT ALL NUT CLIPS TOP AND BOTTOM AT STA 986.5, S18L TO S18R. REPAIRED IAW ECRA 5311-01235. 2L72 4F RTA16WE 20050809000202005080900020WP 2005 8 9 IXXA05SMN96S 120050627A5730 SKIN DOUG DC8 DC871F 302199DWP ZONE 500 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, LT WING NR 5 SPOILER LWR SKIN WITH 02 CRACKS 2", XRS 367.000 - XRS 421.000. REMOVED REPLACED NR 5 SPOILER PANEL ON LT WING XRS 367.000 XRS 421.000 IN ACCORDANCE WITH DC-8B MM 27-61-1 PAGES 201-205. 2L74 4F RT4A25 20050809000232005080900023WP 2005 8 9 IXXA05SMN88S 120050623A5340 FITTING DOUG DC8 DC871F 302199DWP MLG WW CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, MLG W/W FITTING CRACKED 4", STA 857.725 , RBL 46". REMOVED CRACKED FITTING IAW DC-8 SRM 51-1-20D PAGE 21. CLEANED, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8B. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D PAGE 9. TORQUED IAW DC-8 SRM 51-3-1. 2L74 4F RT4A25 20050809000242005080900024WP 2005 8 9 AALA20050491 120050802A3240 BRAKE DOUG DC9 DC982 3022082WP MLG DRAGGING A AALAK NONE O OTHER LDLANDING 1 SW21483A 49676 NUMBER FOUR BRAKE OVER TEMPERATURE. REPLACED NUMBER FOUR WHEEL, BRAKE, AND AXLE SLEEVE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050809000352005080900035EA 2005 8 9 SWIA200515357 120050804A274070623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA MOTOR MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07410SW6751 6751 7066 FFOD CHECKS STAB TRIM CH 1 INOPERATIVE. REPLACED HSTA AND MCU IAW 33-27-415 AND MM 27-40-00, 27-42-01, 27-42-05. OPERATIONAL CHECK GOOD, PN 8396-3 SN OFF 1087. 2L72 4F RTA21EA 20050809000412005080900041EA 2005 8 9 SWIA200515363 120050803A274170609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07934SW126 126 7722 WHILE ON THE GROUND, "STAB CH 1 INOP" AND "MACH TRIM" MSG'S APPEARED. REMOVED AND REPLACED HSTCU. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050809000532005080900053EA 2005 8 9 ASO2005F00003 120050714A335020131A BATTERY CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 4 BATTERY DISCHARGED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27820AS7280 1216 7188 DURING A GROUND INSPECTION, THE EMERGENCY FLOOR LIGHTS AT ROWS 2-4 WERE FOUND TO BE INOPERATIVE. MAINTENANCE CHARGED THE EMERGENCY LIGHT BATTERIES, CLEANED AND RESECURED THE CONNECTIONS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050809000552005080900055NE 2005 8 9 XSF2005F00000 220050728A73100292208230 MANIFOLD SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE ENGINE FUEL CARBONED E XSFAK NONE O OTHER ININSP/MAINT 1 WP13702SA 1455 3551 DURING PREFLIGHT ENGINE WASH, ENGINE WOULD NOT ROTATE DURING STARTER ENGAGEMENT. FOUND ENGINE COMPRESSOR DIFFICULT TO TURN BY HAND, BUT COULD TURN USING FORCE. SUSPECTED FUEL COKING OF THE FUEL MANIFOLD LABRYNTH SEAL. DISASSEMBLED ENGINE, CONFIRMED COKING OF THE LABRYNTH SEAL. INSTALLED OVERHAULED FUEL MANIFOLD, REASSEMBLED ENGINE. ENGINE FUNCTIONED NORMAL WITH NO FURTHER PROBLEMS. PROBABLE CAUSE UNKNOWN. (K) 1G71 3U3 U H9EU E19EU 20050809000562005080900056WP 2005 8 9 IXXA05SMN83S 120050623A5320 CLIP DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE FUSELAGE CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C-CHECK INSPECTION, MLG W/W CLIP CRACKED 5 INCHES , STA 857.725 AND RBL 46 INCHES. REMOVED CRACKED FITTING IAW SRM 51-1-21 PAGE 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PAGE 9. 2L74 4F4 FRT4A25 E2GL 20050809000672005080900067 2005 8 9 LR7A05100 420050803A6122582855 HOUSING LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL NR 4 PROP VALVE FAILED A LR7AEA ENGINE SHUTDOWN UNSCHED LANDING O OTHER CRCRUISE 1 AL03405LC 1454 5025 FLIGHT CREW REPORTED NR 4 PROPELLER RPM FLUX OUT OF LIMITS IN BOTH NORMAL AND MECHANICAL GOVERNING. SHUTDOWN NR 4 ENGINE AT 1953Z IAW AOM ESP. REPLACED NR. 4 PROPELLER VALVE HOUSING IAW HN61135. OPS AND LEAK CHECK NORMAL IAW HN7101. LP 16472, ITEM 1. 2H74 4T4 T A1SO E282 20050809001092005080900109EA 2005 8 9 ASOA05610 120050718A3350BR9279232 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27832AS 7243 DURING C-CHECK, EMERGENCY EXIT FLOODLIGHT ASSEMBLY BY THE FLIGHT ATTENDANTS STATION WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT FLOODLIGHT ASSEMBLY BY FLIGHT ATTENDANTS STATION. OPERATIONAL CHECKS GOOD. (K) 2L72 4F4 FRTA21EA E15NE 20050809001112005080900111EA 2005 8 9 ASOA05599 120050713A324450105711 TIRE MESSIER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE SEPARATED A ASOAK NONE O OTHER TOTAKEOFF 1 SO27902EV DCL633 7620 DURING TAKEOFF, TOWER INFORMED CREW THAT TIRE DEBRIS WAS NOTICED ON RUNWAY AFTER DEPARTURE. THERE WERE NO INDICATIONS OF ENGINE DAMAGE AND AC CONTINUED. EMERGENCY WAS DECLARED AND EMERGENCY VEHICLES WERE REQUESTED TO BE ON STANDBY AS PRECAUTION. AC LANDED SAFELY. UPON TOUCHDOWN, FIRE AND RESCUE CONFIRMED IB RT MAIN TIRE WAS SHREDED. MAINT REMOVED AND REPLACED RT MLG IB AND OB WHEEL AND TIRE ASSEMBLIES. ALSO, FOUND RT IB FLAP ASSEMBLY, RT WING TRAILING EDGE FAIRING AND RT SIDE AFT BELLY FARING DAMAGED. MAINTENANCE REMOVED AND REPLACED RT IB FLAP ASSY AND RT WING T/E FAIRING. MAINT REPAIRED THE RT SIDE AFT BELLY FAIRING IAW SRM. OPS CHECKS GOOD AC OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050809001152005080900115NM 2005 8 9 USAA050883 120050718A5330 SKIN BOEING737 737401 1384701NM CFMINTCFM56 CFM563B2 13802EU BL0,WL148. CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19404US 23886 CLT - C1 - SKIN, .75 INCH CRACK, BS530 BL0, WL148.5 FUSELAGE SKIN AT THE GROUND CONDITIONED AIR CUT OUT. INSTALLED DOUBLER IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050809001162005080900116NM 2005 8 9 USAA050900 120050721A5340 ANGLE BOEING737 737301 1384611NM CFMINTCFM56 CFM563B2 13802EU AFT CARGO CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US50585 23933 CLT - Q6 - TRANSITION ANGLE, 12 INCH X 1 INCH, CORROSION, AFT CARGO STA 737-767. REMOVED DAMAGE, FABRICATED NEW PART AND INSTALLED IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050809001182005080900118SO 2005 8 9 GUU2005F00037 120050709A3350AGC1 FUSE EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE FWD CLOSET OPEN A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO17268AS 120202 EMERGENCY LIGHTS ON THE RT SIDE, AND AFT LT SIDE INOPERATIVE. REPLACED FUSES. (K) 2L72 4T4 TRTA31SO E20NE 20050809001192005080900119SO 2005 8 9 SIMA200517801 120050623A3350110049 BATTERY EMB 135 EMB135KL 3260302SO ALLSN AE3007AE3007C GL CABIN DISCHARGED A SIMAK NONE O OTHER TXTAXI/GRND HDL 1 SW21817AE 145554 CREW DISCOVERED ON PREFLIGHT THAT EMERGENCY STRIP LITES IN FLOOR FROM ROW 11 AFT WILL NOT ILLUMINATE. REPLACED NR 4 BATTERY POWER SUPPLY IAW MM. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (K) 2L72 4F4 FRTT00011ATTE6CH 20050809001242005080900124NM 2005 8 9 USAA050898 120050720A5720 VERTICAL SUPPORT BOEING737 737401 1384701NM CFMINTCFM56 CFM563B2 13802EU RT WING CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19419US45806 23986 CLT - C6 - VERTICAL STIFFNER, .5 INCH CRACK, WS 537 VERTICAL STIFFNER FWD NR 2 ARERON HINGE, RT WING. DRILLED NEW ANGLE AND INSTALLED IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050809001252005080900125NM 2005 8 9 USAA050884 120050718A5414 SKIN BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE LT NACELLE STRUTCRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19393US 23315 CLT - C - SKIN, .75 CRACKED, LT NACELLE STRUT AT NACELLE STATION 218.840. STOP DRILLED AND OVERSIZED HOLE IAW SRM. (K) 2L72 4F4 FRTA16WE E2GL 20050809001272005080900127NM 2005 8 9 USAA050881 120050718A5540 BALANCE ARM BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU RUDDER WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19441US 24812 CLT - Q5 - RUDDER BALANCE ARM, 1.6 INCH WEAR, RUDDER BALANCE ARM. BLENDED AREAS OF WEAR ON RUDDER BALANCE ARM SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050809001542005080900154SO 2005 8 9 SIMA200519312 120050705A531514521721009 FLOORBEAM EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21649PP11879 145234 THE FORWARD DIGITAL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED FORWARD DIGITAL. INSTALLED NEW DIGITAL IAW SRM. (K) 2L72 4T4 FRTT00011ATTE6CH 20050809001562005080900156WP 2005 8 9 ASAA0580357 120050627A561059644201 WINDOW DOUG DC9 DC983 3022083WP COCKPIT DISENGAGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM02979AS31916 53471 PREFLIGHT CHECK, FOUND COCKPIT LEFT SLIDING WINDOW COULD NOT BE OPENED. REPOSITIONED FORWARD UPPER LATCH PIN IN CHANNEL TRACK. WINDOW THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20050809001582005080900158EU 2005 8 9 SIMA200520301 120050715A2910AE7064588 LINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE HYDRAULIC SYS RUPTURED A SIMAA UNSCHED LANDING K FLUID LOSS CLCLIMB 1 SW21301AE 340B301 DISC, UPON GEAR SELECTION UP THE HYDRAULIC QUANTITY STARTED DROPPING TO -0-, MANUAL PUMP OVERRIDE FAILURE. REPLACED RUPTURED NOSE LANDING GEAR RETRACT/EXTENSION ACTUATOR HYDRAULIC LINE. LEAK AND OPS CHECK GOOD. AC RETURNED TO SERVICE. (K) 2L72 4T4 TRTA52EU E8NE 20050809001602005080900160SO 2005 8 9 SIMA200519315 120050707A531514521721009 FLOORBEAM EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21712AE12012 145247 THE GALLEY AREA FORWARD DIGITAL PREVIOUS REPAIR WAS FOUND CORRODED. REMOVED THE EXISTING REPAIR, BLENDED THE DAMAGE AREA OF THE FORWARD DIGITAL TO REMOVE THE CORROSION FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SRM. (K) 2L72 4F4 FRTT00011ATTE6CH 20050809001622005080900162SO 2005 8 9 SIMA200519313 120050701A532014522178005 SILL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21649PP11879 145234 THE RT CENTER SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED RT CENTER SILL. INSTALLED SERVICEABLE SILL IAW SRM. (K) 2L72 4T4 FRTT00011ATTE6CH 20050809001642005080900164SO 2005 8 9 SIMA200519317 120050711A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FR 25 LT CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21811AE8527 145529 THE LT OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. PERFORMED CUT OUT OF THE LT OMEGA BEAM TO REMOVE THE CORROSION. FABRICATED A DOUBLER, FILLER AND 2 SHIMS. REPAIR DOEN IAW SRM. (K) 2L72 4F4 FRTT00011ATTE6CH 20050810000022005081000002NM 2005 8 10 DHL2005746506 120050630A5347 SEAT TRACK BOEING727 727224 1384076NM FUSELAGE DAMAGED A DHLAO OTHER O OTHER ININSP/MAINT 1 SO01746DH 22252 MAIN CABIN SEAT TRACK DAMAGED AT BS 480 TO 580 RBL 45.5. REMOVED DAMAGED SEAT TRACK FROM 480-720 RBL 45.5 IAW B727 SRM 51-30-2 AND SRM 53-10-5 FIG 1, FABBED NEW SEAT TRIM 480-720 RBL 45.5 MAT USED BAC 1520-792 PO 9002389 61" 100" & 109 1/2" 2 SPLICES P/N BAC 1510-100 PO 20093107 SIZE 16 INCH EA IAW B727 SRM 53-10-5 FIG 1. TREATED & PRIMED SEAT TRACK IAW B727 SRM 51-10-2, INSTALLED SEAT TRACKS FROM BS 480-720 RBL 45.5 IAW B727 SRM 53-10-5 FIG 1. 2L73 4F A3WE 20050810000052005081000005NM 2005 8 10 DHL2005746500 120050629A5330 SKIN BOEING727 727224 1384076NM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01746DH 22252 FWD ENTRY DOOR LWR HINGE SUPPORT SKIN CRACKED. REMOVED FASTENERS & CUT OUT DAMAGED SKIN & DOUBLER IAW B727 SRM 51-30-2 AND S/B 727-53A0198 REV 2 FIG 3 SHEET 1 & 2 (3.75 X 1 .375 INCH). FABRICATED DOUBLER FROM 2024-T3, .100 PO 441290, 19.625 X 10.125 INCHES & FILLER MAT. 2024-T3, .080, PO 9002017, 3.75 X 1.375 INCH IAW S/B 727-53A0198, REV 2. TREATED & PRIMED REPAIR PARTS IAW 51-10-2 AND S/B 727-53A 0198, REV 2 FIG 5 DETAIL IV. INSTALLED REPAIR PARTS IAW S/B 727-53A0198 REV 2 FIG 5. THIS REPAIR IS CATEGORY-B. 2L73 4F A3WE 20050810000072005081000007NM 2005 8 10 05FDEA02304 120050807A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25590FE 48505 MAIN DECK CARGO COMPARTMENT, FLOOR SEAT TRACK CROWN AT STA 1139, X= -47 FOUND ELONGATED. MAIN DECK CARGO COMP'T FLOOR SEAT TRACK REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG. 1 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050810000092005081000009NM 2005 8 10 05FDEA02306 120050807A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 CENTER CARGO - UPPER DECK SEAT TRACK X = -75.25 FROM STA 5-73 TO STA 1681 FOUND METAL CLIP NUTS AND SURROUNDING STRUCTURE WITH CORROSION. CARRIED OUT REPAIR AS PER SRM 53-70-00. 2L73 4F RTA22WE 20050810000102005081000010NM 2005 8 10 05FDEA02307 120050807A5347 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 CENTER CARGO - UPPER DECK SEAT TRACK X = -8.50 FROM STA 5-73 TO STA 1681 FOUND METAL CLIP NUTS AND SURROUNDING STRUCTURE CORRODED. CARRIED OUT REPAIR AS PER SRM 53-70-00. 2L73 4F RTA22WE 20050810000112005081000011NM 2005 8 10 05FDEA02308 120050807A5321 FLOOR PANEL DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 CENTER CARGO - UPPER DECK FLOOR PANEL SUPPORT AT STA 1561 X = 58 FOUND CORRODED. 2L73 4F RTA22WE 20050810000122005081000012NM 2005 8 10 05FDEA02309 120050807A7830683L219G07 COWLING GE CF680 DOUG MD11 MD11 3023602NM THRUST REVERSER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 702854 48505 NR 2 ENGINE, RIGHT HAND THRUST REVERSER COWL FORWARD UPPER FRAME FOUND CRACKED. FRAME REPAIRED AS PER DWG SRZ-78-002. 2L73 4F RTA22WE 20050810000132005081000013EU 2005 8 10 05FDEA02310 120050807A5420 WEB AIRBUS300 A300F4605R 3930327EU NR 2 PYLON CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25670FE 777 NR 2 PYLON L/E AREA INSIDE PNL 421CL AFT HORIZONTAL WEB HAS CRACK. 2L72 4F RTA35EU 20050810000162005081000016NM 2005 8 10 05FDEA02303 120050807A5730 SKIN PANEL DOUG MD11 MD11 3023602NM ZONE 600 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT WING - DROOP L/E SKIN PANEL OUTBOARD EDGE FOUND CHAFED MARK. FOUND WITHIN LIMITS AS PER SRM 57-00-01. TRIMMED AND FIGURE 1A VOLUME I. MATERIAL REMOVED 0.375 FROM EDGE. NDT INSPECTED AND VERIFIED CRACK FREE CONDITION. OPERATION CHECKED AND FOUND 'SAT' AS PER AMM 27-80-00. 2L73 4F RTA22WE 20050810000172005081000017NM 2005 8 10 05FDEA02276 120050805A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25624FE 48443 SEAT TRACK AT STA 720 X= 57 FOUND CRACK .5 INCH. REPAIR IAW SRM 53-70-00 FIG 4A VOL I. 2L73 4F RTA22WE 20050810000182005081000018NM 2005 8 10 05FDEA02277 120050805A5310 STRUCTURE DOUG MD11 MD11 3023602NM CARGO BAY CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25624FE 48443 CTR CARGO COMPT CRACK 2 INCHES ON LONG 50 LT BETWEEN STA 1521 AND STA 5-11. REPAIR IAW SRM 51-33-01 PAR 6-10, REPAIR IAW SRM 53-10-00 FIG 1-2. 2L73 4F RTA22WE 20050810000192005081000019NM 2005 8 10 05FDEA02278 120050805A5313 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25624FE 48443 FWD CARGO COMPT FOUND SEVERE CORROSION ON LONGERON 48 LEFT AT STA 6-60. REPAIR IAW SRM 53-10-00 FIG 2 VOL I. 2L73 4F RTA22WE 20050810000202005081000020NM 2005 8 10 05FDEA02279 120050805A5320 WEB DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25624FE 48443 RIGHT FUSELAGE AT STA 1257 BETWEEN LONGERON 15 AND LONGERON 16 FOUND 1 CRACK 1 INCH LONG ON WEB. REPAIRED DOUBLER IAW SRM 53-50-00 FIG 11 SHEET 4. 2L73 4F RTA22WE 20050810000222005081000022NM 2005 8 10 05FDEA02281 120050805A5313 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25624FE 48443 CENTER CARGO FOUND EXFOLIATION CORROSION ON LONG 48 LT SIDE BETWEEN STA 1601 AND 1621. REPAIR IAW SRM 53-10-00 FIG 2 VOL 1. 2L73 4F RTA22WE 20050810000232005081000023NM 2005 8 10 05FDEA02282 120050805A5310 BEAM DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25624FE 48443 FWD CARGO COMPT FOUND CRACK 1 INCH LONG ON BEAM AT STA 6-70 STRINGER 42 RT SIDE. CUTTED DAMAGE AND INSTALL NEW SPLICE REPAIR IAW SRM 53-00-01 FIG 7 VOL I. 2L73 4F RTA22WE 20050810000242005081000024NM 2005 8 10 05FDEA02283 120050805A3246 NUT BOEING727 727200 138407ENM MLG WHEEL LOOSE A FDEAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 SO25281FE 22348 ON TAKEOFF ROLL WITH MAX POWER, AIRCRAFT HAD A LOUD THUMP FELT IN TILLER WHEEL, RUDDERS AND FLOOR.ALL ENGINE INDICATIONS APPEARED NORMAL WITH NO INDICATION OF COMPRESSOR STALL. R-T-O AT APPROX 40-50 KNOTS. PER CREW A/C WOULD PULL TO THE LEFT ON TAXI TO THE GATE. REMOVING NR 2 MLG TIRE TO INSPECT FOUND THE WHEEL NUT HAND TIGHT, MAYBE 5-10 FOOT POUNDS. ALSO FOUND LOCK BOLT LOOSE. REMOVED NR 2 MLG TIRE. INSPECTED NR 2 BRAKE PER M/M. REPLACED NR 2 TIRE RETORQUED NR 1 TIRE AS PRECAUTIONARY. 2L73 4F RTA3WE 20050810000262005081000026EU 2005 8 10 05FDEA02285 120050805A5311A5381231120101 FRAME AIRBUSA300 A300F4622R 3930360EU ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25718FD 365 RIGHT MAIN CABIN FRAME 45 FOUND CRACKED. REMOVED AND REPLACED FRAME SECTION IAW A300-600 SRM 51-40-21 FIG 9, STR 22 TO STR 27. 2L72 4F RTA35EU 20050810000282005081000028NM 2005 8 10 05FDEA02287 120050805A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 EVALUATE TO DETERMINE IF REPAIR IS MAJOR OR MINOR AND IF REPAIR IS IN ACCORDANCE WITH FAA APPROVED DATA, (STRINGER REPAIR STR 28L, BS 700, WL 148). REMOVED PREVIOUS STR. REPAIR SPLICE AND REPAIR SECTION BS 700 720 2" STR 28L WL 148, PER SRM 51-30-2. FABRICATED, ALODINE, PRIMED PAINTED AND INSTALLED NEW STR REPAIR AND REPAIR STR. SECTION BS 700-720 2, STR 28L PER 53-10-3, SHT 1-4, DETAIL 1 AND TABLE II SRM 51-10-2 AND SRM 51-30-2. 2L73 4F RTA3WE 20050810000312005081000031NM 2005 8 10 05FDEA02290 120050805A5340 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 FUSELAGE, UPPER LOBE, STA 680 STR 4L, STRINGER CLIP DAMAGED. REMOVED, FABRICATED AND INSTALLED CLIP PER SRM 51-40-1, 51-10-1, 53-10-2 & FED EX MM 51-20-151-7. 2L73 4F RTA3WE 20050810000322005081000032NM 2005 8 10 05FDEA02291 120050806A534760654924 SEAT TRACK BOEING727 727200 138407ENM MAIN CARGO UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 SEAT TRACK BL 0 STA 360-480 REQUIRES EXTENSION FOR EO 7-5340-7-5002. INSTALLED NEW SEAT TRACK IAW SRM 51-30-2 MAJOR REPAIR. 2L73 4F RTA3WE 20050810000332005081000033NM 2005 8 10 05FDEA02292 120050806A53476023511 SEAT TRACK BOEING727 727200 138407ENM MAIN CARGO CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 PHANTOM SEAT TRACK STA 740-757.5 LBL-45 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2. 2L73 4F RTA3WE 20050810000342005081000034NM 2005 8 10 05FDEA02293 120050806A5314 DOUBLER DOUG MD11 MD11 3023602NM KEELBEAM CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 CTR LANDING GEAR FWD BULKHEAD, LT SIDE WALL, KEEL BEAM DOUBLER FOUND CRACKED. CTR LANDING GEAR FWD BULKHEAD LH SIDEWALL KEEL BEAM DOUBLER REMOVED AND REPLACED AS PER SRM 51-33-01 VOL.II. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2- 100. 2L73 4F RTA22WE 20050810000362005081000036NM 2005 8 10 05FDEA02295 120050806A5347 SEAT TRACK BOEING727 727200 138407ENM MAIN CARGO CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 MCD SEAT TRACK STA 1140-1176 BL-0 HAS CORRODED AREAS. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2. 2L73 4F RTA3WE 20050810000412005081000041NM 2005 8 10 05FDEA02302 120050807A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 AFT CARGO - RIGHT SEAT TRACK AT STA 1954 FOUND CORRODED. REMOVED AND REPLACED AS PER SRM 51-31-01. 2L73 4F RTA22WE 20050810000432005081000043NM 2005 8 10 05FDEA02314 120050808A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE LEFT NR 24 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA1-5510-87597. 2L73 4F RTA22WE 20050810000442005081000044NM 2005 8 10 05FDEA02315 120050808A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE LEFT NR 02 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA1-5510-87597. 2L73 4F RTA22WE 20050810000472005081000047NM 2005 8 10 05FDEA02318 120050808A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE RIGHT NR 03 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. 2L73 4F RTA22WE 20050810000502005081000050NM 2005 8 10 05FDEA02321 120050808A5340 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 STRINGER CLIP AT BS 1010 STR 7 LEFT IS DAMAGED. REMOVED AND REPLACED STR CLIP BS 1010 STR 7L IAW SRM 51-30-02 2L73 4F RTA3WE 20050810000512005081000051NM 2005 8 10 05FDEA02322 120050808A5330 SKIN BOEING727 727200 138407ENM FUSELAGE UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 EVALUATE TO DETERMINE IF REPAIR IS MAJOR OR MINOR AND IF REPAIR IS IN ACCORDANCE WITH FAA APPROVED DATA, (EXTERNAL REPAIR BS 1015, STR 29L, BL 0, 9 X 8 INCHES). REMOVED EXISTING REPAIR, INSTALLED FABRICATED REPAIR PER SRM 53-30-3 FIG 3A. 2L73 4F RTA3WE 20050810000522005081000052NM 2005 8 10 05FDEA02323 120050808A5330 SKIN BOEING727 727200 138407ENM FUSELAGE UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 EVALUATE TO DETERMINE IF REPAIR IS MAJOR OR MINOR AND IF REPAIR IS IN ACCORDANCE WITH FAA APPROVED DATA, (EXTERNAL REPAIR BS 1158, STR 29R, BL 0, 7.5 X 5 INCHES). 2L73 4F RTA3WE 20050810000542005081000054NM 2005 8 10 05FDEA02301 120050807A5310 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 MAIN DECK SEAT TRACK X = 8.5 FROM STA 5-73 TO STA 1681 FOUND METAL CLIP NUTS AND SURROUNDING STRUCTURE CORRODED. CARRIED OUT REPAIR AS PER SRM 53-70-00. 2L73 4F RTA22WE 20050810000552005081000055SO 2005 8 10 LR7A050101 120050806A215020343041 COOLING TURBINE LKHEED382 382G 526414USO AIR CON FAILED A LR7AH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 AL03401LC 730 4606 FLIGHT CREW REPORTED FLIGHT STATION AIR CONDITIONING SYSTEM PRODUCING SMOKE AND FUMES. SHUT DOWN AIR CONDITIONING SYSTEM IAW AFM. FOUND FLIGHT STATION COOLING TURBINE FAILED. REPLACED COOLING TURBINE IAW MM SMP 581-21-50. OPS AND LEAK CHECK NORMAL. 2H74 4T A1SO 20050810000562005081000056NM 2005 8 10 0501216730 120050721A5311 FRAME BOEING747 7472J9F 1384806NM FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01630US 21668 DURING L-CHECK FOUND CRACK IN FRAME WEB AT BS 460 S12L. REPAIRED PER EA 67-165223. 2L74 4F RTA20WE 20050810000572005081000057NM 2005 8 10 0501226730 120050722A5315 FLOORBEAM BOEING747 7472J9F 1384806NM FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01630US 21668 DURING L-CHECK FOUND CRACK IN LONGITUDINAL FLOORBEAM AT BS 1000 LBL 11.33. REPAIRED PER EA 67-165227. 2L74 4F RTA20WE 20050810000582005081000058NE 2005 8 10 SWAA052351 220050804A7230P33P05 BLADE BOEING737 7377H4 1384404NM CFMINTCFM567CFM567B22 13802NE NR 2 ENGINE DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29725SW 27857 875569 DURING SCHEDULED HC2 CHECK, NR 2 ENGINE HAS 2 EACH COMPRESSOR SPOOL BLADE TIP CORNERS MISSING MATERIAL BEYOND LIMITS. REMOVED AND REPLACED NR 2 ENGINE PER MM. 2L72 4F4 FRTA16WE E00055EN 20050810000632005081000063NM 2005 8 10 SWAA052331 120050804A53306545774 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29507SW 24184 DURING WALKAROUND INSP, FOUND FUSELAGE SKIN CRACKED AT BS 757, STR 19L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050810000652005081000065NM 2005 8 10 SWAA052333 120050802A552365C2638425M TAB BOEING737 7373H4 1384600NM LT ELEVATOR DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29637SW 27710 LEFT ELEVATOR TAB DELAMINATED. REMOVED AND REPLACED LT ELEVATOR TAB PER MM. 2L72 4F RTA16WE 20050810000672005081000067NM 2005 8 10 SWAA052335 120050803A53306545766 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 440, BL 0. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050810000692005081000069NM 2005 8 10 SWAA052337 120050804A53226546546 SHEAR TIE BOEING737 737317 138447PNM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 847, LBL 4. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050810000702005081000070NM 2005 8 10 SWAA052338 120050803A53146545866 KEELBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE KEEL BEAM CORRODED AT BS 536, LBL 6.5. REPAIRED KEEL BEAM PER SRM. 2L72 4F RTA16WE 20050810000762005081000076NM 2005 8 10 SWAA052344 120050805A53116546533 FRAME BOEING737 7373H4 1384600NM FWD CARGO CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29613SW 27931 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 492, STR 24R TO STR 26R. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20050810000772005081000077NM 2005 8 10 SWAA052345 120050805A53116520722 FRAME BOEING737 7373H4 1384600NM FWD CARGO CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29613SW 27931 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 24R. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20050810000782005081000078NM 2005 8 10 SWAA052346 120050806A3350D71702001 BATTERY PACK BOEING737 7373T5 1384608NM AFT CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29667SW 23063 DURING SCHEDULED RON CHECK, FOUND LT & RT AFT CABIN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050810000822005081000082NM 2005 8 10 SWAA052350 120050805A335010107451 SIGN BOEING737 7373Q8 1384670NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 L1 DOOR EMERGENCY EXIT LOWER SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM. 2L72 4F RTA16WE 20050810000832005081000083NM 2005 8 10 SWAA052318 120050803A57536546435273 FLAP BOEING737 7373H4 1384600NM LT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED C2 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM. 2L72 4F RTA16WE 20050810000842005081000084NM 2005 8 10 SWAA052319 120050804A53206547980 WEB BOEING737 7373Q8 1384670NM CABIN FLOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29317WN 24068 DURING SCHEDULED D-CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 400 TO BS 420 & BETWEEN BS 847 TO BS 867. REMOVED AND REPLACED CREASE BEAM WEB SECTIONS PER SRM. 2L72 4F RTA16WE 20050810000852005081000085NM 2005 8 10 SWAA052320 120050804A53156547980 WEB BOEING737 7373Q8 1384670NM CABIN FLOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29317WN 24068 DURING SCHEDULED D-CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 400 TO BS 480 & BETWEEN BS 887 TO BS 907. REMOVED AND REPLACED CREASE BEAM WEB SECTIONS PER SRM. 2L72 4F RTA16WE 20050810000862005081000086 2005 8 10 SWAA052321 420050804A25656557463 BRACKET BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29317WN 24068 DURING SCHEDULED D-CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FLOOR BRACKET CORRODED. REMOVED AND REPLACED AFT BRACKET PER SRM. 2L72 4F RTA16WE 20050810000872005081000087NM 2005 8 10 SWAA052322 120050804A53116545874 FRAME BOEING737 7373Q8 1384670NM CABIN FLOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29317WN 24068 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 294, RBL 55, WL 209. REPAIRED STUB FRAME PER BFG ER & SRM. 2L72 4F RTA16WE 20050810000892005081000089NM 2005 8 10 SWAA052324 120050804A53116546554 FRAME BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29317WN 24068 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 807, BS 827, BS 847, BS 867, BS 887 & BS 907, STR 8R TO STR 9R. REPAIRED FRAMES PER SRM. 2L72 4F RTA16WE 20050810000922005081000092EA 2005 8 10 VNAA0507015 120050721A29136619003 PUMP CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE HYD SYS FAILED A VNAAO OTHER O OTHER APAPPROACH 1 GL05723PS1281 10181 THE HYD EDP 2A CAUTION MESSAGE ILLUMINATED ONE MINUTE PRIOR TO LANDING AT CLT. MAINTENANCE DEFERRED THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP AND COMPLIED WITH THE M FUNCTION IAW CRJ700 MEL 29-11-01-2, CODE A. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. ON 07/22/05 MAINTENANCE CLEARED THE MEL BY INSTALLING A SERVICEABLE UNIT ON THE NR 2 ENGINE IAW CRJ700 AMM 29-11-01-400-801-A01. OPERATIONAL AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS AGAIN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050810000942005081000094EA 2005 8 10 VNAA0507014 120050720A2750 FLAP CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF343B1 NE UNKNOWN A VNAAL ABORTED APPROACH F FLT CONT AFFECTED APAPPROACH 1 GL05209PS 7874 ON APPROACH THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED. MAINTENANCE CLEARED THE CAUTION MESSAGE IAW BOMBARDIER SERVICE LETTER RJ-SL-00-001. THE FLAPS OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050810000952005081000095EA 2005 8 10 VNAA0507016 120050722A5200 DOOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF348C1 NE OPEN A VNAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL05719PS 10177 THE CREW REPORTED A LOUD NOISE ABOVE 210KTS DURING CLIMBOUT. THE FLIGHT RETURNED TO CLT WHERE MAINTENANCE DISCOVERED THE EXTERNAL SERVICE PANEL DOOR OPEN. THE DOOR WAS INSPECTED AND OPERATIONALLY CHECKED. NO DAMAGE WAS FOUND AND THE LATCHES FUNCTIONED PROPERLY. THE DOOR WAS SECURED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050810000962005081000096EA 2005 8 10 VNAA0507023 120050729A710022850081142 COWLING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT LOWER DAMAGED A VNAAO OTHER O OTHER LDLANDING 1 GL05226JS3187 7895 AFTER POSTFLIGHT INSPECTION THE CREW REPORTED THAT THE RIGHT ENGINE LOWER NOSE ACCESS COWL WAS MISSING. THE COWL WAS FOUND ON THE RUNWAY. MAINTENANCE INSTALLED A SERVICEABLE NOSE ACCESS COWL IAW CRJ200 AMM 71-14-01-400-802. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050810000982005081000098EA 2005 8 10 VNAA0507012 120050715A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE UNKNOWN A VNAAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 GL05221PS 7889 ON FINAL APPROACH WITH FLAPS 20° THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED. THE CREW FOLLOWED THE QRH AND LANDED WITHOUT INCIDENT. MAINTENANCE COMPLIED WITH THE FLAP FAIL RESET PROCEDURES IAW CRJ200 RJ-SL-00-001. THE FLAPS OPERATIONALLY CHECK GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050810001022005081000102CE 2005 8 10 08022005B 120050802A2730130610000613 ELEVATOR BEECH 1900 1900D 1154162CE STUCK A NSVAK NONE F FLT CONT AFFECTED TOTAKEOFF 1 EA27136MJ 136MJ AT ROTATION SPEED (100 KIAS) CONTROL COLUMN WAS TEMPORARILY STUCK UNTIL EXTREME BACK PRESSURE WAS APPLIED. CONTROL COLUMN THEN MOVED RAPIDLY AFT AND A/C JUMPED OFF RUNWAY. IN FLIGHT A/C ELEVATOR TRIM VERY SLOWLY MOVED TO NOSE UP, REQUIRING APPROX 1/2 UNIT CHANGE NOSE DOWN EVERY 1-2 MINUTES. FLIGHT CONTROLS DON'T SEEM TO BIND ON SUBSEQUENT GROUND CHECKS. 2L72 4T RTA24CE 20050810001032005081000103EU 2005 8 10 08032005A 120050803A2701 YOKE SAAB SF340 340B 7860101EU COCKPIT OUT OF ADJUST A NSVAO OTHER F FLT CONT AFFECTED CRCRUISE 1 EA27306CE 203 BOTH YOKES ARE CANTED RIGHT IN STRAIGHT AND LEVEL FLIGHT. COMPLETED WING AND AILERON RIGGING, OPS CHECK GOOD. 2L72 4T RTA52EU 20050810001052005081000105EU 2005 8 10 08042005B 120050804A1420 CONNECTOR SAAB SF340 340B 7860101EU TORQUE DIRTY A NSVAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 EA27303CE 194 ABORTED T/O, RT TORQUE GAUGE FAILED. NO OTHER ASSOCIATED INDICATIONS. FOUND LOOSE AND DIRTY CANNON PLUG ON TORQUE SENSOR. CLEANED AND SECURED. 2L72 4T RTA52EU 20050810001072005081000107CE 2005 8 10 08072005A 120050807A781011891006229 TUBE BEECH 1900 1900D 1154162CE EXHAUST UNKNOWN A NSVAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 EA27220CJ UE20 LT ENGINE FIRE HANDLE ILLUMINATED MOMENTARILY. REMOVED AND REPLACED EXHAUST STACK BLAST TUBE AND FIRE LOOP. 2L72 4T RTA24CE 20050810001102005081000110CE 2005 8 10 08082005C 120050807A2730130610000613 ELEVATOR BEECH 1900 1900D 1154162CE DAMAGED A NSVAO OTHER F FLT CONT AFFECTED ININSP/MAINT 1 EA27172MJ UE72 LT ELEVATOR, ONE LOOSE RIVET ON THE OUTBOARD HINGE BRACKET AND ONE LOOSE RIVET ON THE CENTER HINGE BRACKET. 2L72 4T RTA24CE 20050810001112005081000111CE 2005 8 10 08082005D 120050805A2730130610000613 ELEVATOR BEECH 1900 1900D 1154162CE DAMAGED A NSVAO OTHER F FLT CONT AFFECTED ININSP/MAINT 1 EA27220CJ UE20 LT ELEVATOR, OUTBOARD ATTACH POINT LOWER SURFACE HAS ONE WORKING RIVET. 2L72 4T RTA24CE 20050810001122005081000112CE 2005 8 10 08082005E 120050805A27301145240595 CLAMP BEECH 1900 1900D 1154162CE TRIM CABLE OBSTRUCTED A NSVAO OTHER F FLT CONT AFFECTED ININSP/MAINT 1 EA27220CJ UE20 BRIDLE CABLE CLAMP CONTACTING UPPER BULKHEAD AND PASSING INTO VERTICAL STAB AREA. 2L72 4T RTA24CE 20050810001142005081000114CE 2005 8 10 08082005H 120050809A2730130610000613 ELEVATOR BEECH 1900 1900D 1154162CE LOOSE A NSVAO OTHER F FLT CONT AFFECTED ININSP/MAINT 1 EA27221CJ UE221 LT ELEVATOR, OUTBOARD HINGE HAS LOOSE RIVET ON BOTTOM SIDE OF ELEVATOR. 2L72 4T RTA24CE 20050810001172005081000117NM 2005 8 10 UPS05445065 120050723A541165B903082 FRAME BOEING747 747121 1384871NM NR 4 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 NR 4 PYLON NAC STA 240 I/B SIDE FWD OF ACCESS PANEL CUTOUT 483EL VERT FRAME LIGHTEN HOLE CRACKED, CRACK LENGTH 2". NR 4 PYLON NAC STA 240 I/B SIDE VERTICAL FRAME REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050810001192005081000119NM 2005 8 10 UPS05445067 120050726A5320654U662464 PANEL BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 BS 440 S14/S15 1R DOOR CUTOUT REVEAL CRACKED BETWEEN NR 8/9 DOOR STOP FTG, CRACK LENGTH 1". REVEAL PANEL REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050810001202005081000120NM 2005 8 10 UPS05445068 120050725A5312 BULKHEAD BOEING747 747121 1384871NM TUNNEL CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 FX BS 260 CANTED BULKHEAD WEB FOUND CRACKED AT WL 176 LBL 67, CRACK LENGTH 1/4". FX BS 260 CANTED BULKHEAD WEB REPAIRED AT WL 176 LBL 67 AREA AS PER SRM 53-10-04 FIG 6. 2L74 4F A20WE 20050810001252005081000125NM 2005 8 10 UPS05545080 120050805A2560 SMOKE GOGGLES BOEING757 75724APF 1384969NM COCKPIT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01452UP 25473 OBSERVERS SMOKE GOGGLES CRACKED. REPLACED OBSERVERS SMOKE GOGGLES. 2L72 4F RTA2NM 20050810001262005081000126WP 2005 8 10 UPS05845056 120050628A5711 SPAR DOUG DC8 DC873F 302199FWP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 FS 855 AFT SIDE OF REAR SPAR LOWER CHORD UPPER SURFACE FROM RBL36.5 -45.00 HAS 8.5" CRACK. REPAIRED REAR SPAR IAW SRO 8570009. 2L74 4F RT4A25 20050810001282005081000128NM 2005 8 10 QXEA200501155 120050806A2720 REGULATOR DHAV DHC8 DHC8202 2809007NM RUD DUAL PRESS UNKNOWN A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09365PH1522974 526 PDX FLIGHT NR 2169 - RUDDER PRESSURE AND RUDDER FULL PRESSURE AT SPEEDS ABOVE 140 KTS. REPLACED RUDDER DUAL PRESSURE REGULATOR AND ACTUATOR ISOLATE SOLNOID VALVES FOR PRECAUTIONARY MEASURES. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050808000842005080800084NM 2005 8 8 05FDEA02231 120050803A5330 SKIN BOEING727 727227 1384078NM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 GOUGES IN FUSELAGE SKIN STA 215, 5 ABOVE STR 17L. REPAIRED DAMAGE IN FUSELAGE SKIN AT STA. 251.5, ABOVE STR 17R IAW SRM 51-30-1, SRM 53- 30-3, 51-10-02, 51-30-02. 2L73 4F A3WE 20050808000972005080800097NM 2005 8 8 05FDEA02229 120050803A5340 STRINGER CLIP BOEING727 727227 1384078NM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 STRINGER CLIP AT BS 1010 STR 7 RT HAS 2 PREVIOUSLY DRILLED HOLES. REPAIRED PER SRM 51-20-1, 51-30-2. 2L73 4F A3WE 20050808000992005080800099 2005 8 8 QXEA200501151 420050804A2220311851201A FLOW DIVIDER DHAV DHC8 DHC8202 2809007NM FUEL MALFUNCTIONED A QXEAO OTHER O OTHER TXTAXI/GRND HDL 1 NM09369PH139826608 513 SEA - NR 2 ITT TAKES UP TO 9 SECONDS TO LIGHT OFF FROM THE POINT OF FUEL INTRODUCTION OF ENGINE START. IT IS WITHIN THE TEN SECOND GUIDANCE IN THE ABNORMAL CHECKLIST BUT FOUR TO FIVE SECONDS LONGER THAN THE NR 1 ITT. MAINTENANCE REPLACE NR 2 ENGINE FUEL FLOW DIVIDER IAW MTC 9731001. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050808001202005080800120EU 2005 8 8 05FDEA02242 120050804A5321 FLOOR PANEL AIRBUS300 A300F4605R 3930327EU FUSELAGE PUNCTURED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25671FE 778 MDC FLOOR PNL 251YG HAS SEVERAL PUNCTURES ON LWR SURFACE AND 1 ON UPPER SURFACE. 2L72 4F RTA35EU 20050808001272005080800127NM 2005 8 8 05FDEA02236 120050803A5540 WEB BOEING727 727200 138407ENM LT HORZ STAB CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 LEFT SIDE OF HORIZONTAL STAB REMOVABLE SPAR WEB IS CRACKED IN 3 SPOTS. REMOVED AND REPLACED WEB IAW SRM 51-30-2. 2L73 4F RTA3WE 20050808001302005080800130NM 2005 8 8 05FDEA02248 120050804A5322 SHEAR TIE BOEING727 727200 138407ENM FUSLEAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 CORROSION ON SHEAR TIE STA 1166 BETWEEN STR 27L & 29L. REPAIRED PR SRM 51-10-1, 51-10-3, 51-20-1, 51-30-2. 2L73 4F RTA3WE 20050808001322005080800132EU 2005 8 8 05FDEA02250 120050804A5321 FLOOR PANEL AIRBUS300 A300B4605R 3930308EU MDC CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25670FE 777 MDC FLOOR PNL 252BH IS CRACKED. 2L72 4F RTA35EU 20050808001392005080800139NM 2005 8 8 05FDEA02273 120050805A5347 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25624FE 48443 MAIN CABIN SEAT TRACK FROM STA 1381 TO 1701 AND AT STA 1951 X= -107 CORRODED. REPAIR IAW SRM 53-70-00 FIG 5 VOL I. 2L73 4F RTA22WE 20050808001422005080800142EU 2005 8 8 05FDEA02241 120050804A5321 FLOOR PANEL AIRBUS300 A300F4605R 3930327EU MDC DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25671FE 778 MDC FLOOR PNL 231FF DAMAGED. 2L72 4F RTA35EU 20050808001482005080800148NM 2005 8 8 05FDEA02256 120050804A5320 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 MAIN DECK, SEAT TRACK RBL 11 CORRODED AT STA 795 TO STA 879. CORROSION REMOVED AS PER SRM 51-21-01. 2L73 4F RTA22WE 20050808001572005080800157NM 2005 8 8 05FDEA02262 120050804A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 MAIN DECK CARGO COMPARTMENT, FLOOR SEAT TRACK AT STA 635, X= - 8.5 FOUND CRACKED APPROXIMATELY 3 INCHES LONG. REMOVED AS PER SRM 53-70-00. REPAIR SEAT TRACK AND SPLICES FABRICATED, HFEC INSPECTION CARRIED OUT. FOUND NO CRACK FOUND. INSTALLED AS PER SRM 53-70-00. REPAIR SEAT TRACK AND SPLICES FABRICATED AS PER SRM 53-70-00 VOLUME I, FIGURE 1 USING S493914-7075T6 AND S4932154-7075T6 RESPECTIVELY. HFEC INSPECTION CARRIED OUT AS PER NDT SPM 06-10- 01-001 REV. 12 FOUND NO CRACK. REPAIR PARTS TREATED AS PER SRM 57-21-01 VOLUME II. FABRICATED SEAT TRACK AND SPLICES INSTALLED AS PER SRM 53-70-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2L73 4F RTA22WE 20050808001612005080800161NM 2005 8 8 05FDEA02266 120050805A5420AUB75647 WEB DOUG MD11 MD11 3023602NM ZONE 400 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25624FE 48443 CRACK 1 INCH LONG ON INTERNAL VERTICAL WEB AT STA YN298. REPAIR IAW SRM 54-00-01 FIG 3 VOL I. 2L73 4F RTA22WE 20050808001762005080800176WP 2005 8 8 IXXA05SMN87S 120050623A5310 STRUCTURE DOUG DC8 DC871F 302199DWP MLG WW CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING C CHECK INSPECT, MLG W/W L-24 CRACKED 2", STA 980.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 53-2-2 FIG 5 TR NR 53-123 DATE 05-15-01, EO SEMAN NR 2005831 DATE 06-16-05. REMOVED FASTENERS IAW DC-8 SRM 51-1-20D PAGE 21. PERFORMED SLOP HOLE ON CRACK END IAW DC-8 SRM 53-2-2 FIG 5 SHEET 21. PERFORMED NDT INSPECT IAW DC-8 NDT SPM PART 06-10-01-001. NO CRACK, CORROSION FOUND. FAB`D REPAIR ANGLE (ALCLAD 2024 T3 0.125”) + WASHERS (ALCLAD 2024 T3 0.090) IAW DC-8 SRM 53-2-2 FIG 5 SHEET 24 IAW DC-8 SRM 51-1-4 PAGE 1. CLEANED, TREATED AND PRIMED AREA + REPAIR PARTS IAW DC-8 SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11 PAGE 9. INSTALLED REPAIR PARTS IAW DC-8 SRM 53-2-2 FIG 5 SHEET 21, 24,2L74 4F RT4A25 20050808001772005080800177NM 2005 8 8 SB05089 120050808A335020121 CHARGER BOEING737 7374B7 1384702NM MID CABIN INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19447US 24874 PIT - MAINTENANCE REPORTED FOUR EMERGENCY LIGHTS AT SEAT ROWS 7 THROUGH 10 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED CHARGER ASSEMBLY M1134 AND THE BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050808002012005080800201WP 2005 8 8 IXXA05SMN66S 120050623A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE DAMAGED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING C CHECK INSPECT, EXTERNAL DOUBLER FWD LOWER FUSELAGE, STA FS 114.000, L-35.5L MUST BE UPGRADED. PERFORMED MAJOR REPAIR IAW DC-8 SRM 53-2-1 FIG. 7, EO SEMAN NR 2005869 DATE 06-13-05. REMOVED EXISTING REPAIR DOUBLER IAW DC-8 SRM 51-1-21 PAGE 1. TRIMMED OUT DAMAGED AREA IAW DC-8 SRM 53-2-1 FIG. 7 (SHEET 1,3). PERFORMED DETAILED VISUAL INSPECT NI CRACK, CORROSION FOUND. FAB`D REPAIR DOUBLER (ALCLAD 7075 T6 0.080”) + (02 EA) INTERNAL FINGER DOUBLER (ALCLAD 7075 T6 0.050”) IAW DC-8 SRM 53-2-1 FIG 7 SHEET 1,3, DC-8 SRM 53-4-1 FIG 16 SHEET 2 ITEM B, DC-8 SRM 51-9-0 FIG 68A, DC-8 SRM 51-1-4 PAGE 1. CLEANED, TREATED AND PRIMED AREA + REPAIR PARTS IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC-8 S2L74 4F RT4A25 20050809000022005080900002EU 2005 8 9 MALA050634 120050805A3230HP848430721 CONTROL VALVE SAAB SF340 340B 7860101EU MLG MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION DEDESCENT 1 GL15452XJ LANDING GEAR WOULD NOT EXTEND WHEN SELECTED DOWN INBOUND TO MCW, AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL VALVE PN HP848430-721 SN/ON 0011 SN/OFF 2054 IAW SF340 AMM 32-31-15, OPS CHECK GOOD. CYCLED GEAR 15 TIMES IN HANGER LEAK CHECK GOOD. 2L72 4T RTA52EU 20050809000102005080900010WP 2005 8 9 IXXA05SMN95S 120050627A5730 SKIN DOUG DC8 DC871F 302199DWP ZONE 500 DELAMINATED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, LT LWR WING T/E NR 546 ACCESS DOOR EXTERNAL SKIN DELAMINATED. REMOVED AND REPLACED EXTERNAL PANEL IN LT LWR WING T/E NR 546 ACCESS DOOR IN ACCORDANCE WITH DPS 367-15. 2L74 4F RT4A25 20050809000152005080900015NM 2005 8 9 CALA0500257 120050807A5330654580033 SKIN BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718350 23588 INSPECTION FOUND THE FUSELAGE SKIN AT LT NOSE WHEEL WELL CRACKED OUT AND MISSING, STA 259.5, S27L. REPAIRED IAW ECRA 5330-03472 2L72 4F RTA16WE 20050809000192005080900019WP 2005 8 9 IXXA05SMN98S 120050627A5313 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING C CHECK INSPECT, AFT CARGO CMPT L-36 CORRODED, STA 1540.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 53-2-2 FIG 4A, EO SEMAN NR 2005846 DATE 06-18-05. REMOVED CORROSION IAW DC-8 SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW DC-8 SRM 53-2-0 PAGE 2P. REMOVED CORRODED LONG SEGMENT IAW DC-8 SRM 53-2-2 FIG 4A. PERFORMED DETAILED VISUAL INSPECT. NO CRACK, CORROSION FOUND FAST LONGERON SEGMENT CUT. FAB`D NEW LONGERON SEGMENT (PN 52597242-3-14400 EXTRUSION) IAW DC-8 SRM 53-2-2 FIG 4A, DC-8 SRM 53-4-1 FIG 42 (SHEET 2) ITEM “Q”, SPLICE (02 EA) (ALCLAD 7075 T651) IAW DC-8 SRM 53-2-2 FIG 10 (SHEET 4), TR # 53-193 IAW DC-8 SRM 53-2-2 FIG 10 (SHEET 2) TR # 53-153. CLEANED, TREATED AND PRIMED AREA, REPAIR PARTS IAW DC-8 SR2L74 4F RT4A25 20050809000222005080900022WP 2005 8 9 IXXA05SMN81S 120050623A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE DAMAGED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING C CHECK INSPECT, EXTERNAL DOUBLER UAL DRAIN DOUBLER, RT AFT FUSELAGE SIDE. REPAIR MUST BE UPGRADED, REPAIR MUST HAVE 3 ROWS OF RIVETS STA FS 1693, L-30.5R (REF.- 822BX-R71). PERFORMED MAJOR REPAIR IAW DC-8 SRM 53-2-1 FIG 7, EO SEMAN NR 2005871 DATE 06-13-05. REMOVED EXISTING REPAIR DOUBLER IAW DC-8 SRM 51-1-21 PAGE 1. FAB`D REPAIR DOUBLER (ALCLAD 7075 T6 0.063”) + INTERNAL FINGER DOUBLER (ALCLAD 7075 T6 0.032”) IAW DC-8 SRM 53-2-1 FIG 7 (SHEET 1,5), DC-8 SRM 53-5-1 FIG 1 ITEM E, DC-8 SRM 51-1-4 PAGE 1. CLEANED, TREATED AND PRIMED AREA + REPAIR PARTS IAW DC-8 SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11. INSTALLED REPAIR PARTS IAW DC-8 SRM 53-2-1 FIG 7, DC-8 SRM 51-1-21 PAGE 2L74 4F RT4A25 20050809000402005080900040SO 2005 8 9 SWIA200515362 120050801A3397 WIRE EMB 120 EMB120ER 3260203SO EMERGENCY SIGN BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07220SW 120288 EMERGENCY EXIT SIGN OVER ROW 9 INOP. REPAIRED BROKEN WIRE AT ROW 9 EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050809000442005080900044EA 2005 8 9 SWIA200515366 120050803A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07455SW 7760 FWD CABIN CEILING EMERGENCY POD LIGHT BULB BURNED OUT. REPLACED BULB AT OVERHEAD EMERGENCY LIGHT IAW MM 33-00-00. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050809000612005080900061 2005 8 9 GUU2005F00038 420050705A34406227236012 DISPLAY EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE FWD INSTR PANEL SHORTED A GUUAO OTHER O OTHER CRCRUISE 1 SO17283AS 120236 DURING FLIGHT, A MOMENTARY SMELL OF ELECTRICAL SMOKE. MULTI-FUNCTION DISPLAY BLANKED OUT, FLIGHT CONTINUED. REPLACED MULTI-FUNCTION DISPLAY. (K) 2L72 4T4 TRTA31SO E20NE 20050809000642005080900064NM 2005 8 9 200512 120050801A2611 SMOKE DETECTOR DHAV DHC8 DHC8103 1386005NM PWA PW121 PW121 52124NE UNKNOWN A KPVAO OTHER J WARNING INDICATION APAPPROACH 1 WP13811WP 366 SMOKE WARNING CAME ON IN FLIGHT. MAINTENANCE INSPECTED SMOKE DETECTORS AND PERFORMED SMOKE WARNING TEST IAW MM 26-12-00 PG. 201 PAR. 1A. OPS CHECK GOOD. 2H72 4T4 TRTA13NM E20NE 20050809000732005080900073NM 2005 8 9 174 120050805A5320 SHEAR WEB BOEING757 757232 1384965NM PWA 2037 PW2037 NE FUSLEAGE CORRODED B DU4RO OTHER O OTHER ININSP/MAINT 1 SO15624DL 22914 CORROSION ON SHEAR WEB SURFACE FROM BS 1681.8 TO 1720 BL 0 TO BL60L INCLUDING FASTENER HOLES. S/O 283001, DELTA N//R NR 21000. 2L72 4F4 FRTA2NM E17NE 20050809000972005080900097SO 2005 8 9 SIMA200519306 120050626A532014522178005 CHANNEL EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21809AE 145521 DURING INSPECTION, FOUND SERVICE DOOR CHANNEL HAS CORROSION AROUND NUT PLATES. REPLACED SERVICE DOOR CHANNEL IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4F4 FRTT00011ATTE6CH 20050809001022005080900102SO 2005 8 9 SIMA200519307 120050626A533014522461011 DOUBLER EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL STA 22, 23 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21809AE 145521 DURING INSPECTION, FOUND FWD CABIN FLOOR DOUBLER HAS CORROSION AROUND NUT PLATES. INSTALLED NEW FORWARD CABIN FLOOR DOUBLER IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4F4 FRTT00011ATTE6CH 20050809001072005080900107EA 2005 8 9 ASO2005F00002 120050714A335020131A BATTERY CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 3 BATTERY DISCHARGED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27820AS7280 1216 7188 DURING GROUND INSPECTION, THE EMERGENCY FLOOR LIGHTS AT ROWS 2-4 WERE FOUND TO BE INOPERATIVE. MAINTENANCE CHARGED THE EMERGENCY LIGHT BATTERIES, CLEANED AND RESECURED THE CONNECTIONS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050809001122005080900112EA 2005 8 9 ASO2005F00004 120050713A5753601R140022 FLAP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE WING DAMAGED A ASOAK NONE O OTHER TOTAKEOFF 1 SO279023V 7620 DURING TAKEOFF, TOWER INFORMED CREW THAT TIRE DEBRIS WAS NOTICED ON RUNWAY AFTER DEPARTURE. THERE WERE NO INDICATIONS OF ENGINE DAMAGE AND AC CONTINUED. EMERGENCY WAS DECLARED AND EMERGENCY VEHICLES WERE REQUESTED TO BE ON STANDBY AS PRECAUTION. AC LANDED SAFELY. UPON TOUCHDOWN, FIRE AND RESCUE CONFIRMED IB RT MAIN TIRE WAS SHREDDED. MAINT REMOVED AND REPLACED RT MLG IB AND OB WHEEL AND TIRE ASSEMBLIES. ALSO, FOUND RT IB FLAP ASSEMBLY, RT WING T/E FAIRING AND RT SIDE AFT BELLY FARING DAMAGED. MAINT REMOVED AND REPLACED RT IB FLAP ASSY AND RT WING T/E FAIRING. MAINT REPAIRED THE RT SIDE AFT BELLY FAIRING IAW SRM. OPS CHECKS GOOD AC OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050809001142005080900114NM 2005 8 9 USAA050882 120050718A5340 ANGLE BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU LT SIDE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19441US40664 24812 CLT - Q5 - ANGLE, .375 INCH, CRACKED AT STA 601LT SIDE BODY WING TERMINAL FORGING ANGLE CRACKED ON AFT SIDE. REMOVED DAMAGED AND INSTALLED REPAIR ANGLE IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050809001212005080900121NM 2005 8 9 USAA050897 120050720A5710 SUPPORT ANGLE BOEING737 737401 1384701NM CFMINTCFM56 CFM563B2 13802EU T/E PANEL CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19419US 23986 CLT - C-6 - SUPPORT ANGLE, .75 INCH CRACK. SUPPORT ANGLE FOR UPPER FIXED T/E PANEL OB OF NACELLE, LT WING. FABRICATED AND INSTALLLED NEW ANGLE, SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050809001262005080900126EA 2005 8 9 ASOA05606 120050715A5320CC670341441 BRACKET CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27703EV 10038 DURING A C-CHECK, THE FS 280 BRACKETS AT LBL 9 AND RBL 9 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FS 280 BRACKETS AT LBL 9 AND RBL 9. (K) 2L72 4F4 FRTA21EA EOOO63EN 20050810000142005081000014NM 2005 8 10 05FDEA02311 120050808A5340 FITTING DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HFEC CARRIED OUT FOUND CRACKS 2 EACH AT LEFT NR 4 BANJO FITTING ON AFT LOWER HOLE 5 O'CLOCK (LOOKING I/B) APPROX .1875 INCH LONG AS MARKED. REPAIRED AS PER SRM 55-20-00. 2L73 4F RTA22WE 20050810000212005081000021NM 2005 8 10 05FDEA02280 120050805A5313 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25624FE 48443 FWD CARGO COMPT FOUND EXFOLIATION CORROSION ON LONG 52 AT STA 1039. REPAIR SRM 53-10-00 FIG 1 & 2 VOL 1. 2L73 4F RTA22WE 20050810000272005081000027EU 2005 8 10 05FDEA02286 120050805A5311A5381231220101 FRAME AIRBUS300 A300B4622R 3930312EU ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25718FD 365 MAIN CABIN RT FRAME 46 CRACKED. REMOVED AND REPLACED RT FRAME 46 AT STR 27 IAW A300-600 SRM 51-40-21 FIG 9. 2L72 4F RTA35EU 20050810000352005081000035NM 2005 8 10 05FDEA02294 120050806A57206521658 CHANNEL BOEING727 727100 1384036NM RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25107FE 19202 RIGHT WING TRAILING EDGE AT AFT SPAR AREA 3 EA CLOSE OUT PANEL SUPPORTS ARE CRACKED LOCATED UNDER NR 12 & 13 SPOILER PANELS. REMOVED AND REPLACED 3 EACH CHANNEL SUPPORTS IAW SRM 51-30-2. 2L73 4F RTA3WE 20050810000372005081000037NM 2005 8 10 05FDEA02296 120050806A534760501824 SEAT TRACK BOEING727 727200 138407ENM MAIN CARGO CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 MCD SEAT TRACK HAS CORROSION BS 870 TO 950 RBL 26. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2. 2L73 4F RTA3WE 20050810000402005081000040NM 2005 8 10 05FDEA02299 120050807A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARRREL NUT HOLE RT NR 27 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. 2L73 4F RTA22WE 20050810000452005081000045NM 2005 8 10 05FDEA02316 120050808A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE LEFT NR 22 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA1-5510-87597. 2L73 4F RTA22WE 20050810000642005081000064 2005 8 10 SWAA052332 420050804A2565D31354433 SLIDE BOEING737 7375H4 138449DNM R2 DOOR OUT OF LIMITS A SWAAK NONE O OTHER ININSP/MAINT 1 SW29508SW 24185 DURING SCHEDULED A1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE PRESSURE OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20050810000802005081000080 2005 8 10 SWAA052348 420050803A2565D31354 SLIDE BOEING737 7373G7 1384595NM L1 & R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29671SW 23785 DURING SCHEDULED C3 CHECK, FOUND L1 & R1 DOOR EMERGENCY EVAC SLIDES OUT OF ADJUST. ADJUSTED SLIDES PER MM. 2L72 4F RTA16WE 20050810000912005081000091NM 2005 8 10 SWAA052326 120050804A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 DURING WALKAROUND INSP, FOUND FUSELAGE SKIN CRACKED AT BS 727C + 8, STR 14R. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050810000932005081000093EA 2005 8 10 VNAA0507013 120050716A5240 ACCESS DOOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE OXYGEN SERVICE OPEN A VNAAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 GL05237PS 7906 DURING CLIMB A LOUD NOISE WAS HEARD COMING FROM THE RIGHT SIDE OF THE AIRCRAFT. SUSPECTING AN OPEN DOOR THE CREW DIVERTED TO PIT. MAINTENANCE FOUND THE OXYGEN SERVICING ACCESS PANEL (212BR) OPEN. THE PANEL AND FUSELAGE WERE INSPECTED IAW CRJ200 AMM 05-51-03-210-004. NO DEFECTS WERE FOUND. THE PANEL OPERATIONALLY CHECKED GOOD. THE PANEL WAS SECURED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050810000992005081000099EA 2005 8 10 VNAA0507022 120050725A2620365000183 FIRE BOTTLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LEFT DISCHARGED A VNAAFA ACTIVATE FIRE EXT. UNSCHED LANDING O OTHER NRNOT REPORTED 1 GL05221PS2034 7889 THE CARGO BTL LOW CAUTION MESSAGE ILLUMINATED IN FLIGHT. THE CREW RETURNED TO CLT WHERE MAINTENANCE DEFERRED THE CARGO FIRE EXTINGUISHING SYSTEM IAW MEL 26-25-01C AND RELEASED THE AIRCRAFT FOR SERVICE. MAINTENANCE IN TYS REMOVED & REPLACED THE LT CARGO COMPARTMENT FIRE BOTTLE IAW CRJ200 AMM 26-25-01-400(000)-801. THE OPERATIONAL CHECK WAS GOOD. THE MEL WAS CLEARED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050810001002005081000100 2005 8 10 YENA200544 420050804A23305040210001 DISPLAY AIRBUS320 A320232 3930326EU CABIN BURNED A YENADH RETURN TO BLOCK DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA15618JB 2489 DURING TAXI OUT FROM GATE, SMOKE WAS COMING OUT OF VDU AT SEAT ROW 7A. RETURNED TO GATE. INITIALLY THE ITEM WAS PLACED ON MEL AND WAS REPLACED ON 8/05/05. 2L72 4F RTA28NM 20050810001152005081000115WP 2005 8 10 IXXA05SMN109S 120050627A5730 WING DOUG DC8 DC871F 302199DWP XS ELONGATED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING C CHECK INSPECT, LT WING, NR 2 STUB WING VANE SLOT HOLE ELONGATED, XS 247.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 # 05270 DATE 06-29-05, SEMAN DWG # 3986 DATE 06-28-05, EO SEMAN # 2005849 DATE 06-29-05. REMOVED DAMAGED AREA IAW SEMAN DWG ED 3986. PERFORMED NDT INSPECT IAW DC-8 NDT SPM PART 06-10-01-001. FAB`D EXISTING REPAIR DOUBLER (ALCLAD 7075 T6 0.071”), FILLER (ALCLAD 7075 T6 0.063”) IAW SEMAN DWG # 3986. CLEANED, TREATED AND PRIMED AREA, REPAIRS INTERNAL PART IAW DC-8 SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW SEMAN DWG # 3986, DC-8 SRM 51-3-0 PG 1, DC-8 SRM 51-1-21 PG 1, DC-8 SRM 51-1-20D PG 9. TORQUED IAW DC-8 SRM 51-3-1. 2L74 4F RT4A25 20050810001162005081000116WP 2005 8 10 IXXA05SMN110S 120050627A5730 SKIN DOUG DC8 DC871F 302199DWP XRS CRACKED B IXXAO OTHER O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING C CHECK INSPECT, RT WING UPPER SKIN HAS 2 CRACKS OF 1" EACH AT XRS 74. 869, S-15 AND S-16. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 # 05280 DATE 07-04-05, SEMAN DWG # ED 3981 DATE 06-29-05, EO SEMAN NR 2005834 DATE 07-04-05. REMOVED EXISTING REPAIR DOUBLERS IAW DC-8 SRM 51-1-20D PAGE 21. REMOVED DAMAGED AREA IAW SEMAN DWG ED 3981. PERFORMED NDT INSPECT IAW DC-8 SPM PART 06-10-01-001. FAB`D EXTERNAL REPAIR DOUBLER (ALCLAD 7075 T6 0.160”), (03 EA) FILLER PLUG (ALCLAD 7075 T6) IAW SEMAN DWG ED 3981. CLEANED, TREATED AND PRIMED AREA, REPAIR PARTS (INTERNAL PART) IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11 PAGE 9. INSTALLED REPAIR PARTS IAW SEMAN DWG ED 3981, DC-8 SRM 2L74 4F RT4A25 20050810001212005081000121NM 2005 8 10 UPS05445069 120050726A5240 FRAME BOEING747 747121 1384871NM L2 DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 L2 DOOR AFT FRAME LOWER CORNER CRACKED, CRACK LENGTH 1. L2 DOOR AFT FRAME LOWER CORNER REPAIRED AS PER SRM 52-10-02 FIG 10. 2L74 4F A20WE 20050810001222005081000122NM 2005 8 10 UPS05445070 120050719A5340BAC1505100849 TEE FITTING BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 BELOW CENTER SECTION SURFACE BS 1241 RBL 104 'T' CHORD FOUND CRACKED, CRACK LENGTH 2.125". 'T' CHORD REWORKED AND INSTALLED AS PER SRM 51-10-01 AND 51-30-02. 2L74 4F A20WE 20050810001272005081000127WP 2005 8 10 UPS05845059 120050630A5711 SPAR CAP DOUG DC8 DC873F 302199FWP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 LT AFT LWR WING SPAR CAP F/S 857 IS CRACKED IN THREE PLACES FROM LBL27-LBL45. REPAIRED LT LWR SPAR CAP IAW SRO DWG 8570009, SRM 51-1-20D, 51-1-24. 2L74 4F RT4A25 20050810001312005081000131NM 2005 8 10 DHL2005746501 120050629A5330 SKIN BOEING727 727224 1384076NM DAMAGED A DHLAO OTHER O OTHER ININSP/MAINT 1 SO01746DH 22252 PILLOWING AT AFT AIRSTAIR LT CUT OUT SKIN BETWEEN STA 1223 AND 1229 STR 27L (MARKED). REMOVED FASTENERS FROM AREA. REMOVED CORROSION FROM CHORD AT STR 27L MATT LOSS .017 ORIG THICKNESS .125 FABED NEW ANGLE FROM 7075 T6 .040 PO NR 9002219 27.3" X 1.25" X 3" IAW B727 SRM 51-40-3 FIG 1 MATT LOSS ON CHORD WITHIN LIMITS IAW B727 SRM 53-10-1 FIG 1. TREATED AND PRIMED NEW ANGLE AND AFFECTED AREA IAW B727 SRM 51-10-2. INSTALLED NEW ANGLE AND ATTACHING PARTS AND SKIN IAW B727 SRM 51-30-2. 2L73 4F A3WE 20050810001322005081000132WP 2005 8 10 IXXA05SMN114S 120050627A5730 SKIN PANEL DOUG DC8 DC871F 302199DWP LT WING DENTED B IXXAO OTHER O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING C CHECK INSPECTION, LT OTBD FLAP L/E DENTED, XF 213.000 (UPPER PART. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-1-0 PG 1, DC-8 SRM 57-7-1 FIG 4, TR NR 57-94, EO SEMAN NR 2005852 DATE 06-18-05. REMOVED DAMAGED PLATING IAW DC-8 SRM 51-1-21 PG 1, DC-8 SRM 51-3-0 PG 1. FAB`D NEW PLATING (ALCLAD 2024 T3 0.040”) IAW DC-8 SRM 57-7-1 FIG 4, TR 57-94 ITEM “C”. CLEANED, TREATED AND PRIMED AREA, NEW PLATING INTERNAL PART IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11 PG 9. INSTALLED NEW PLATING IAW DC-8 SRM 51-1-21 PG 1, DC-8 SRM 51-3-0 PG 1. TORQ`D IAW DC-8 SRM 51-3-1. 2L74 4F RT4A25 20050810001332005081000133NM 2005 8 10 DHL2005746502 120050629A5330 SKIN BOEING727 727224 1384076NM FUSELAGE DENTED A DHLAO OTHER O OTHER ININSP/MAINT 1 SO01746DH 22252 DENT LT FUSELAGE SKIN STA 1233 BETWEEN STR 23L AND 24L (MARKED). CUT OUT DAMAGE AREA FOUND OUT OF LIMITS DIM CUT OUT 1" BY 3/4" IAW B727 SRM 53-30-3 FIG 1. FABBED DOUBLER REPAIR MAT USED 2024 T3 .063 PO NR 9002199 DIM 8" BY 6" IAW B727 SRM 53-30-3 FIG 1 AND 53-30-2 FIG 3. TREATED AND PRIMED IAW B727 SRM 51-10-2 AND INSTALLED DOUBLER IAW 727 SRM 53-30-3 FIG 1. 2L73 4F A3WE 20050810001342005081000134NM 2005 8 10 QXEA200501157 120050807A2430 RELAY DHAV DHC8 DHC8202 2809007NM DC GENERATOR MALFUNCTIONED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09367PH 511 PDX FLIGHT NR 2272 - NR 2 DC GENERATOR CAUTION LIGHT ILLUMINATED. REPLACED RELAY 2431K-12. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050810001352005081000135 2005 8 10 QXEA200501158 420050806A3420 UNKNOWN DHAV DHC8 DHC8202 2809007NM UNKNOWN UNKNOWN A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09366PH 510 PDX FLIGHT NR 2149 - DURING TAXI, THE FIRST OFFICER'S EADI SHOWED ON 8 DEGREE PITCH DOWN WITH 10-15 DEGREES BACK. NO MESSAGES WERE DISPLAYED ON THE EADI OR ADVISORY PANEL. REINITIALIZED NR 2 AHRS, FIRST OFFICER'S ADI POWER UP SELF TEST NORMAL. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050810001362005081000136NM 2005 8 10 QXEA200501152 120050806A2611 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM MALFUNCTIONED A QXEAK NONE J WARNING INDICATION LDLANDING 1 NM09352PH 494 PUW FLIGHT NR 2028 - SMOKE WARNING ON DESCENT, NO SIGN OF SMOKE NOTED. DEFERRED IAW -8(200) MEL 26-8(B). 2H72 4T RTA13NM 20050810001372005081000137NM 2005 8 10 QXEA200501153 120050806A2611302313 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM MALFUNCTIONED A QXEAK NONE J WARNING INDICATION LDLANDING 1 NM09352PH10534925 494 SEA FLIGHT NR 2027 - SMOKE WARNING ON SHORT FINAL, FLASHED FOR APPROXIMATELY TWO SECONDS AND EXTINGUISHED. 10-15 SECONDS LATER IT FLASHED AGAIN FOR TWO SECONDS AND EXTINGUISHED. ON TAXI IN IT FLASHED THREE MORE TIMES ALL LASTING 1-2 SECONDS. REPLACED NR 1 AND NR 2 SMOKE DETECTORS. NR 1 SMOKE DETECTOR PART NUMBER 473054, SERIAL NUMBER 0554, TSN 17043.5, CSN 24703. NR 2 SMOKE DETECTOR INFORMATION LISTED BELOW. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050810001402005081000140NM 2005 8 10 QXEA200501159 120050806A2760 PRESSURE SWITCH DHAV DHC8 DHC8202 2809007NM SPOILERS MALFUNCTIONED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09364PH 524 SEA FLIGHT NR 2022 - NR 1 ROLL SPOILER INBOARD HYDRAULIC CAUTION FLICKERED ON AND OFF INTERMITTENTLY 8-10 TIMES, REMAINED OFF FOR FIVE MINUTES, THEN STAYED ON REMAINDER OF FLIGHT. REPLACED NR 1 INBOARD SPOILER PRESSURE SWITCH AND COMPLIED WITH FUNCITONAL CHECK OF THE ROLL SPOILER CONTROL SYSTEM. OPERATIONAL CHECKS GOOD. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050810001462005081000146NM 2005 8 10 UPS05245076 120050713A5320 SUPPORT BOEING727 72722C 138400FNM CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01941UP 19196 FWD LAV SUPPORT TOP HAT EXTRUSION IS CORRODED AT BS 328RBL 13. REPLACED FWD LAV SUPPORT/TOP HAT IAW SRM 51-20-1 FIG 7. 2L73 4F A3WE 20050810001472005081000147NM 2005 8 10 UPS05245077 120050713A5315 FLOORBEAM BOEING727 72722C 138400FNM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01941UP 19196 REPLACE UPPER CHORD OF FLOORBEAM BS 344 FROM LBL 12 RBL 30 IAW SRM DUE CORROSION. REPLACED UPPER CHORD IAW SRM 53-10-8. 2L73 4F A3WE 20050810001482005081000148NM 2005 8 10 UPS05245078 120050713A5320 SHEAR WEB BOEING727 72722C 138400FNM MCD SILL CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01941UP 19196 NUMEROUS AREAS OF LIGHT SURFACE CORROSION ON MAIN CARGO DOOR SILL SHEAR WEB IN UPPER SURFACE AREAS OF CORROSION CLEANED AND REPROTECTED. WITHIN LIMITS PER SRM 51-1 0-6. 2L73 4F A3WE 20050810001522005081000152NM 2005 8 10 DHL2005746503 120050629A5330 SKIN BOEING727 727224 1384076NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01746DH 22252 PILLOWING AT STA 1213 BETWEEN STR 28L AND 29L LT SIDE FUSELAGE SKIN (MARKED). REMOVED FASTENERS AT STA 1213 STR 28L TO 29L IAW B727 SRM 51-30-2. EVALUATED AREA SKIN DAMAGED (CREASES) AND DENTS OUT LIMITS IAW B727 SRM 53-30-1 FIG 1. REMOVED LOWER SKIN BS 1203 TO BS 1225 LT SIDE IAW B727 SRM 51-30-2. FABBED NEW SKIN MAT USED 2024 T3 .040 PO NR 9002219 DIM 41 1/2 X 28 3/4 IAW B727 SRM 53-30-2 FIG 3. TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED NEW SKIN AT 1213 BETWEEN STR 28L AND 29L IAW B727 SRM 53-30-2 FIG 3 AND 51-30-2. 2L73 4F A3WE 20050810001532005081000153NM 2005 8 10 DHL2005746504 120050629A5330 SKIN BOEING727 727224 1384076NM DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01746DH 22252 PILLOWING AT STA 1208 STR 29R RT SIDE FUSELAGE SKIN (MARKED). REMOVED FASTENERS AT BS 1208 IAW B727 SRM 51-30-2. EVALUATED SKIN CREASES AREA BS 1208 IAW B727 SRM 53-30-1 FIG 1 AND 51-30-2. FOUND TO BE OUT OF LIMITS. SKIN REMOVED LWR SKIN BS 1208 TO BS 1225 IAW B727 SRM 51-30-2. FABBED SKIN MAT USED 2024 T3 .040 PO#9002219 SIZE 41 1/2" BY 28 3/4" IAW B7272 SRM 53-30-2 FIG 3. TREATED AND PRIMED PART AND AREA IAW B727 SRM 51-10-2. INSTALLED NEW SKIN AT BS 1208 STR 29R IAW B727 SRM 53-30-2 FIG 3 AND SRM 51-30. 2L73 4F A3WE 20050810001542005081000154NM 2005 8 10 DHL2005746505 120050630A5347 SEAT TRACK BOEING727 727224 1384076NM DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01746DH 22252 MAIN CABIN SEAT TRACK DAMAGED AT BS 760 TO 850 RBL 45.5. REMOVED SEAT TRACK AT BS 760 TO 850 RBL 45.5 IAW 727 SRM 53-10-1 FIG 3 AND 51-30-2. FABBED NEW SEAT TRACK P/N BAC 1520-841 DIM 8FT IAW 727 SRM 53-10-2 FIG 7 AND 53-10-5 FIG 2. TREATED AND PRIMED SEAT TRACK AND AREA IAW 727 SRM 51-10-2. INSTALLED NEW SEAT TRACK AT STA 760 TO 850 RBL 45.5 IAW 727 SRM 53-10-5 FIG 2 AND 51-30-2. 2L73 4F A3WE 20050810001562005081000156EA 2005 8 10 SWIA200515370 120050719A5315 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAO OTHER O OTHER ININSP/MAINT 1 NM07406SW 7030 FS 280 RT FLOORBEAM RBL 9 OB ATTACH ANGLE CRACKED, ITEM FOUND AT C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-23-00, 51-21-11, 51-42-21 2L72 4F RTA21EA 20050810001582005081000158EA 2005 8 10 SWIA200515372 120050719A5210 DOOR FRAME CNDAIRCL600 CL6002B19 1900309EA CRACKED A SWIAO OTHER O OTHER ININSP/MAINT 1 NM07406SW 7030 PAX DOOR FRAME FS 338.9 CRACKED, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR IAW CRJ REO 601R-52-11-402 REV "C" 2L72 4F RTA21EA 20050810001592005081000159EA 2005 8 10 SWIA200515373 120050719A5210 DOOR FRAME CNDAIRCL600 CL6002B19 1900309EA CRACKED A SWIAO OTHER O OTHER ININSP/MAINT 1 NM07406SW 7030 PAX DOOR SUB FRAME, FS 335.7 CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED FRAME FS 335.7 IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, 2L72 4F RTA21EA 20050810001602005081000160EA 2005 8 10 SWIA200515374 120050719A5210 SKIN CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A SWIAO OTHER O OTHER ININSP/MAINT 1 NM07406SW 7030 PAX DOOR INNER SKIN FS 3389 BELOW BOTTOM STEP CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED SKIN IAW REO 601R-52-11-765 REV --, 2L72 4F RTA21EA 20050810001612005081000161EA 2005 8 10 SWIA200515375 120050719A5210 STRUCTURE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CORRODED A SWIAO OTHER O OTHER ININSP/MAINT 1 NM07406SW 7030 PAX DOOR CORNER CORRODED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED DOOR CORNERS & ANGLES IAW MOD SUM TC 601R16876, TC 601R16637 CRJ SRM 51-40-11, 51-42-06, 51-42-13, 51-42-21, 51-23-00 REO 601R-52-11-770, 2L72 4F RTA21EA 20050810001622005081000162EA 2005 8 10 SWIA200515376 120050719A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAO OTHER O OTHER ININSP/MAINT 1 NM07406SW 7030 FUSELAGE, REMOTE ANGLE ON PULLEY INTERCOSTAL IS CRACKED FS 484.00 - RBL 36.0, ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ REO 601R-53-41-059 REV "A", 2L72 4F RTA21EA 20050810001642005081000164EA 2005 8 10 SWIA200515378 120050719A5744 BOLT CNDAIRCL600 CL6002B19 1900309EA CORRODED A SWIAO OTHER O OTHER ININSP/MAINT 1 NM07406SW 7030 LT OB FLAP OB ACTUATOR HINGE TRUNNION BLOCK BOLT CORRODED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED BOLT IAW AMM 27-54-05-400-801. 2L72 4F RTA21EA 20050810001652005081000165EA 2005 8 10 SWIA200515379 120050719A5310 STRUCTURE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAO OTHER O OTHER ININSP/MAINT 1 NM07406SW 7030 CRACK EMITTING FROM RIVET HOLE AT FS 605 FRAME AND STRINGER 9 INTERSECTION TOP SIDE OF STRINGER, ITEM FOUND AT C-CHECK INSPECTION. FRAME REPAIRED IAW 601R-53-61-1469 2L72 4F RTA21EA 20050810001662005081000166EA 2005 8 10 SWIA200515380 120050719A5310 STRUCTURE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAO OTHER O OTHER ININSP/MAINT 1 NM07406SW 7030 CRACK EMITTING FROM RIVET HOLE AT FS 605 FRAME AND STRINGER 9 INTERSECTION BOTTOM SIDE OF STRINGER, ITEM FOUND AT C-CHECK INSPECTION. FRAME REPAIRED IAW REO 601R-53-61-1469. 2L72 4F RTA21EA 20050810001672005081000167EA 2005 8 10 SWIA200515381 120050709A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA CRACKED A SWIAO OTHER O OTHER ININSP/MAINT 1 NM07426SW 7468 FS 484 CABIN FLOOR LT INTERCOSTAL INBOARD AND OUTBOARD ANGLES LBL 27 AND LBL 36 CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED INTERCOSTAL IAW CRJ REO 601R-53-41-059 REV "A". 2L72 4F RTA21EA 20050810001692005081000169EU 2005 8 10 2005UALA00667 120050715A3350321454 EPSU AIRBUS320 A320232 3930326EU IAE V2527 V2527EA5 NE 112WL2-111WL2-11MALFUNCTIONED A UALAO OTHER L NO TEST ININSP/MAINT 1 WP29402UA 439 EMERGENCY EXIT PATHWAY LIGHTS WILL NOT EXTINGUISH. REPLACED EMERGENCY POWER SUPPLIES 112WL2, 111WL2 AND 110WL2. OPS CHECK GOOD. 2L72 4F4 FRTA28NM E40NE 20050810001712005081000171EA 2005 8 10 SWIA200515384 120050709A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAO OTHER O OTHER ININSP/MAINT 1 NM07426SW 7468 FS 280 CABIN FLOOR TRANVERSE BEAM LOWER FLANGE CRACKED, ITEM FOUND AT C-CHECK. REPAIRED BEAM IAW CRJ REO 601R-53-11-171 REV "B". 2L72 4F RTA21EA 20050810001742005081000174EA 2005 8 10 SWIA200515387 120050709A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA CRACKED A SWIAO OTHER O OTHER ININSP/MAINT 1 NM07426SW 7468 FS 625 AFT EQUIPMENT COMPARTMENT LT ANGLE STR 14L CRACKED, ITEM FOUND AT C-CHECK. REPAIRED ANGLE IAW CRJ REO 601R-53-61-100 "REV NC", REO 601R-53-61-422 REV "NC". 2L72 4F RTA21EA 20050810001752005081000175EA 2005 8 10 SWIA200515388 120050709A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA CRACKED A SWIAO OTHER O OTHER ININSP/MAINT 1 NM07426SW 7468 FS 625 AFT EQUIPMENT COMPARTMENT RT ANGLE ST 14R CRACKED, ITEM FOUND AT C-CHECK. REPAIRED ANGLE IAW CRJ REO 601R-53-100 "REV NC", REO 601R-53-61-422 REV "NC". 2L72 4F RTA21EA 20050810001812005081000181NM 2005 8 10 2005UALA00735 120050729A5340 STRINGER CLIP BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE STA 639 STR 4LT CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29914UA 25381 CABIN UPPER LOBE STRINGER CLIP IS CRACKED AT STA 639 STR 4 LT. REPLACED STRINGER CLIP. 2L72 4F4 FRTA16WE E2GL 20050810001822005081000182NM 2005 8 10 2005UALA00736 120050729A5320 WEB BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE CABIN CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29914UA 25381 CABIN FLOOR WEB CORRODED AT STATION 749 JUST INBD OF STR 17R CREASE BEAM. REMOVED AND REPLACED WEB. 2L72 4F4 FRTA16WE E2GL 20050810001832005081000183EU 2005 8 10 2005UALA00737 120050708A5330 SKIN AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE AFT FUSELAGE JACBUCKLED A UALAK NONE O OTHER ININSP/MAINT 1 WP29495UA 1842 SKIN BUCKLED AROUND AFT FUSELAGE JACK PAD FITTING. MAJOR REPAIR TO REPLACE SKIN IN AREA OF THE JACK PAD. REPLACED SKIN IN AREA OF THE JACK PAD. 2L72 4F4 FRTA28NM E40NE 20050810001842005081000184EU 2005 8 10 2005UALA00738 120050729A2133 OUTFLOW VALVE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CABIN PRESSURE FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29481UA 1559 FLIGHT DIVERTED DUE TO AN AIR CONDITIONING FAULT. SKIN AIR OUTLET VALVE FAILED. VALVE WAS REPLACED, SYSTEM OPS CHECKED AND AIRCRAFT WAS RETURNED TO SERVICE. MOTOR WAS FOUND SHORTED. 2L72 4F4 FRTA28NM E40NE 20050810001852005081000185NE 2005 8 10 2005UALA00739 220050630A7200 ENGINE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 1 STALLED A UALAC ABORTED TAKEOFF RC PARTIAL RPM/PWR LOSS F.O.D. TOTAKEOFF 1 WP29492UA 1755 V10748 NR 1 ENG STALL ON TAKEOFF ROLL. 2L72 4F4 FRTA28NM E40NE 20050810001882005081000188NM 2005 8 10 2005UALA00742 120050731A5310 FAILSAFE BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE STA 1395 LWR FLADAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29667UA23223 29239 STATION 1395 FAIL/SAFE CHORD LOWER FLANGE IS DAMAGED BETWEEN STRINGERS 37L AND 38L AND ALSO BETWEEN STRINGERS 38R AND 39R. LOWER AFT FUSELAGE STRUCTURE DAMAGED BY MOVING BAGGAGE CART. DAMAGED STRUCTURE INCLUDED SKIN, STRINGERS, FRAME, TEAR STRAP. COMBINATION MAJOR REPAIR ACCOMPLISHED BY MAJOR REPAIR AUTHORITY NUMBER 1048 (EVA 50478A) AND MAJOR REPAIR AUTHORITY NR 1049 (EVA 50482A). ANY INSPECTION REQUIREMENTS FROM THE SUBMITTED DAMAGE TOLERANCE ASSESSMENT WILL BE INCORPORATED. 2L72 4F4 FRTA1NM E24NE 20050810001892005081000189NM 2005 8 10 2005UALA00743 120050728A3250 STEERING SYS AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE NLG INOPERATIVE A UALAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 WP29825UA 980 ON ROLLOUT GOT LANDING GEAR NOT DOWN ECAM , THEN GOT NW STEER FAULT. NWS DID NOT WORK. 2L72 4F4 FRTA28NM E40NE 20050810001902005081000190NM 2005 8 10 2005UALA00744 120050729A5320 WEB BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE AFT CARGO DOOR SCORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29914UA 25381 AFT CARGO DOOR SILL WEB HAS NUMEROUS AREAS OF CORROSION WL 141 STATION 800 TO 847 RBL 20" TO RBL 24". REMOVED AND INSTALLED NEW WEB REPAIR. 2L72 4F4 FRTA16WE E2GL 20050810001932005081000193EU 2005 8 10 2005UALA00747 120050802A5330 SKIN AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE RT FUSELAGE AFT DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29419UA 487 RT FUSELAGE DENTED AFT OF FS 64 AT STR 20R. MAJOR REPAIR TO ADD DOUBLER OVER SKIN. 2L72 4F4 FRTA28NM E40NE 20050810001972005081000197NM 2005 8 10 2005UALA00751 120050803A5230 SKIN BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE AFT MANUAL PIT DPUNCTURED A UALAK NONE O OTHER ININSP/MAINT 1 WP29674UA 29242 RAMP REPORTED A PUNCTURE IN THE AFT MANUAL PIT DOOR. MEASURES APPROXIMATELY .5 BY .25 IN AN "L" SHAPE. AFTER INTERIM REPAIR WAS REMOVED, A HFEC INSPECTION WAS ACPL AND NO CRACKS WERE FOUND. REPAIR DOUBLER WAS INSTALLED PER SRM 51-20-05 AND 51-40-02. WORK WAS ACPL ON WU-Z5237L BY GSO AMT 110080, 4550, AND INSP BY QC 400, 385. 2L72 4F4 FRTA1NM E24NE 20050810001982005081000198NM 2005 8 10 2005UALA00752 120050803A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE STA 1723 AT STR DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29594UA 28145 EXTERNAL FUSELAGE SKIN DENTED STA 1723 AT STR 21L. MAJOR REPAIR ACCOMPLISHED PER EVA-40245A. 2L72 4F4 FRTA2NM E17NE 20050810001992005081000199NM 2005 8 10 2005UALA00753 120050803A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE STA 490, STR 15LDENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29587UA 26713 EXTERNAL FUSELAGE SKIN AT STA 490, STR 15L HAS DENT. REMOVE DAMAGE AND INSTALL REPAIR DOUBLER PER SRM 53-00-01, REPAIR 4, P201. REPAIR IS A CATEGORY A REPAIR. 2L72 4F4 FRTA2NM E17NE 20050810002002005081000200NM 2005 8 10 C1HA200592003 120050808A2913AS19570C PUMP BOEING727 727212 138407GNM FAILED A C1HAA UNSCHED LANDING S AFFECT SYSTEMS CRCRUISE 1 GL15292AS 5555 21458 NR 2 B PUMP FAILED INFLIGHT, REPLACED NR 2 B HYD PUMP, CASE DRAIN AND PRESSURE FILTER, OP'S CHECK GOOD. LEAK CK GOOD REF MM 29-12-3. 2L73 4F A3WE 20050810002012005081000201NM 2005 8 10 2005UALA00754 120050802A5230 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE AFT CARGO DOOR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29351UA 24319 AFT CARGO DOOR HAS A VERTICAL CRACK APPROX 2 INCHES LONG, 6 T0 8 INCHES DOWN FROM DOOR HANDLE. REMOVED EXISTING DOUBLERS AND INSTALLED NEW DOUBLER APPROX 48" BY 48" PER SRM 52-30-01 AND SRM 52-00-01. 2L72 4F4 FRTA16WE E2GL 20050810002052005081000205NM 2005 8 10 2005UALA00758 120050804A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29177UA 24384 EMERGENCY LT INOP, CEILING ROW 18. REPLACED LAMP. 2L74 4F4 FRTA20WE E24NE 20050907000312005090700031CE 2005 9 7 DXTA200500944 120050831A3240 BRAKE CESSNA500 560CESSNA 2076750CE MLG FAILED E DXTAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07302QS 5600402 ON TAXI OUT DURING BRAKE CHECK CAPTAINS LEFT BRAKE WENT ALL THE WAY TO THE FLOOR. UPON ACTIVATION OF THE CO-PILOTS LEFT BRAKE, BOTH BECAME SPONGY. RESET BRAKE SHUTTLE VALVES, BLED BRAKE SYSTEM. PERFORMED SEVERAL BRAKE CHECKS STILL AND WHILE TAXIING WITH POWER BRAKE SELECTED ON AND OFF. NEVER GOT BRAKES TO FAIL. SOLID BRAKE PEDALS AT ALL TIMES IAW MODEL 560 MM 32-42-00. 2L72 4F RTA22CE 20050810002072005081000207NM 2005 8 10 2005UALA00761 120050729A3350 LIGHT BOEING777 777222 1385219NM PWA PW4077PW4077 NE INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29780UA 26944 1R AND 4R EXTERIOR EMERGENCY LIGHTS INOP. RELAMPED BOTH EMERGENCY LIGHTS. 2L72 4F4 FRTT0001SE E46NE 20050810002082005081000208NM 2005 8 10 2005UALA00762 120050804A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29177UA 24384 EEL INOP, ROW 44. REPLACED LIGHT ASSY. 2L74 4F4 FRTA20WE E24NE 20050810002092005081000209NM 2005 8 10 2005UALA00763 120050804A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29177UA 24384 EMERGENCY LTS INOP, LT OVERWING 2 FWD ASSY'S. 2L74 4F4 FRTA20WE E24NE 20050810002102005081000210NM 2005 8 10 2005UALA00764 120050804A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29177UA 24384 EEL INOP, AFT GALLEY FWD WALL CROSS AISLE. REPLACED LIGHT ASSY. 2L74 4F4 FRTA20WE E24NE 20050810002152005081000215 2005 8 10 2005UALA00769 420050727A2200 LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE UNKNOWN A UALAK NONE O OTHER ININSP/MAINT 1 WP29329UA 24149 MACH TRIM FAIL LIGHT ON RECALL, VERY CHRONIC. AFTER TROUBLESHOOTING & PARTS REPLACEMENT, REVIEW OF BITE DATA REVEALED INTERMITTENT MOMENTARY LOSS OF POWER TO MACH TRIM SYS. CIRCUIT BREAKER C1064, B-MACH TRIM DC, REPLACED & TEST FLT PERFORMED. INTERMITTENT NATURE OF FAILURE DUE TO IMPROPER SEQUENCING OF RESET OF CB & OTHERS, BY MX AFTER LONG LAY-OVERS, RESULTED IN FAILURE OF FCC TO POWER-UP IN TIME FOR MACH TRIM TEST. WHEN CREW PERFORMED MASTER CAUTION RECALL, MACH TRIM LIGHT ILLUMINATED INDICATING A SINGLE CHANNEL FAULT. AIRCRAFT HAS ACCUMULATED 71 FLT HRS WITHOUT A REOCCURENCE SINCE BREAKER REPLACED. 2L72 4F4 FRTA16WE E2GL 20050810002172005081000217NE 2005 8 10 20030874 220050807A732078639016 HMU EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE DEFECTIVE A GLBAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS CRCRUISE 1 NM03297UX7689 120297 115635 DURING CRUISE, NR 1 ENG PROP RPM STARTED TO FLUCTUATE +/- 12 PERCENT, A FEW SECONDS LATER, TORQUE SLOWLY DROPPED TO ZERO. ALL ENGINE GUAGES ALSO DROPPED THEN CLIMBED BACK TO ABOUT 50 PERCENT THEN DROPPED AGAIN. FLT CREW FEATHERED PROP BUT DID NOT SHUTDOWN ENGINE. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED LT HMU. AIRCRAFT RETURNED TO SERVICE. 2L72 4T4 TRTA31SO E20NE 20050810002202005081000220WP 2005 8 10 IXXA05SMN117S 120050627A5730 SKIN DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE XF304.000-309.00MISREPAIRED A IXXAO OTHER O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, LT OB FLAP NON STANDARD REPAIR, XF 304.000 -XF 309.000 (UPPER PART). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PAGE 1, SRM 57-7-1 FIG. 4, TR NR 57-94, EO SEMAN NR 2005854 DATE 06-18-05. REMOVED PLATING WITH IMPROPER REPAIR IAW SRM 51-1-21 PAGE 1. FABRICATED NEW PLATING (ALCLAD 2024 T3 0.050”) IAW SRM 57-7-1 FIG. 4, TR 57-94 ITEM A. CLEANED, TREATED AND PRIMED AREA + NEW PLATING INTERNAL PART IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PAGE 9. INSTALLED NEW PLATING IAW SRM 51-1-21 PAGE 1. 2L74 4F4 FRT4A25 E2GL 20050810002222005081000222WP 2005 8 10 IXXA05SMN119S 120050628A5340 FITTING DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE 220.000 240.000 CRACKED B IXXAO OTHER O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, FWD CARGO COMPT, FITTING CRACKED 1 INCH AT STA 220.000 - 240.000 L-31R. REMOVED DAMAGED FITTING IAW SRM 51-1-20D PAGE 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PAGE 1. TORQUED IAW SRM 51-3-1. 2L74 4F4 FRT4A25 E2GL 20050810002262005081000226NM 2005 8 10 AT0500026 120050804A33508039251 POWER SUPPLY BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE STA 312 INOPERATIVE A ZZDAK NONE O OTHER ININSP/MAINT 1 SO37933AT 55071 FIRST CLASS SEAT EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACKS AT STA 312 IAW MM 33-51. OPS CK GOOD. 2L72 4F4 FTRA6WE E00061EN 20050810002272005081000227WP 2005 8 10 IXXA05SMN128S 120050629A5340 FITTING DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE 1690.00 L-36 CORRODED B IXXAO OTHER O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, MAIN CARGO CMPT. FITTING CORRODED AT STA. 1690.00, L-36 REMOVED CORROSION IAW SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PAGE 21. REMOVED CORRODED FITTING IAW SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING IAW DWG NR 4641324 (ALCLAD 7075 T6 51). PERFORMED HEAT TREATMENT IAW SRM 51-1-11 PAGES 1,13,17. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02 TO 07. CLEANED, TREATED AND PRIMED AREA + NEW FITTING IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PAGE 9. TORQUED IAW SRM 51-3-1. 2L74 4F4 FRT4A25 E2GL 20050810002282005081000228WP 2005 8 10 IXXA05SMN130S 120050629A5340 FITTING DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE 8.000 L33L CRACKED A IXXAO OTHER O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, NOSE SECTION FITTING CRACKED 5 INCHES, STA. 8.000 L-33L. REMOVED CRACKED FITTING IAW SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING IAW DWG NR 4645453 (ALCLAD 7075 T6 51), EO SEMAN NR 2005939. PERFORMED HEAT TREATMENT IAW SRM 51-1-11 PAGS 1,13,17. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02 TO 07. CLEANED, TREATED AND PRIMED AREA + NEW FITTING IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PAGE 9. TORQUED IAW SRM 51-3-1. AT STA 8.000 L-33L. 2L74 4F4 FRT4A25 E2GL 20050810002292005081000229WP 2005 8 10 IXXA05SMN131S 120050629A5313 LONGERON DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE 1726.000 L-28R CORRODED B IXXAO OTHER O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, MAIN CARGO CMPT.- L-28R CORRODED, STA. 1726.000. REMOVED CORROSION IAW SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PAGE 2. REMOVED CORRODED LONGERON IAW SRM 51-1-20D PAGE 1, DC-8 SRM 51-1-21 PAGE 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW LONGERON IAW SRM 51-1-21 PAGE 1, SRM 51-1-20D PAGE 9. TORQUED IAW SRM 51-3-1. 2L74 4F4 FRT4A25 E2GL 20050810002302005081000230WP 2005 8 10 IXXA05SMN133S 120050629A5753 ANGLE DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE XW129.000 CRACKED B IXXAO OTHER O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, RT IB FLAP INTERNAL ANGLE CRACKED 3 INCH, STA XW 129.000. REMOVED CRACKED ANGLE IAW SRM 51-1-21. FABRICATED NEW ANGLE (A EXTRUSION S-1656396) IAW SRM 57-2-0 PAGE 1. CLEANED, TREATED AND PRIMED AREA + NEW ANGLE IAW SRM 51-1-8B. INSTALLED NEW ANGLE IAW SRM 51-1-21 PAGE 1. 2L74 4F4 FRT4A25 E2GL 20050810002342005081000234NM 2005 8 10 AWXA200500919 120050808A335020131A BATTERY BOEING737 7373B7 1384580NM LOW A AWXAK NONE O OTHER ININSP/MAINT 1 WP28332AW 23384 PHX - EEL - DURING 4 DAY CHECK, THE EXTERIOR EMERGENCY ESCAPE LIGHT AT L2 DOOR WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY AND BATTERY ABOVE AFT GALLEY IAW BOEING 737-300 AMM 33-51-51-201. POWER SUPPLY; RADIANT ILLUM; PN 100865, SN UNK; INOPERATIVE. 2L72 4F RTA16WE 20050810002352005081000235EA 2005 8 10 SWIA200515393 120050807A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA OUT OF ADJUST A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07923SW 7664 MAIN CABIN DOOR VERY HARD TO OPEN. READJUSTED FWD AND AFT UPPER SPIGOT'S IAW AMM 52-11-21. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050810002382005081000238SO 2005 8 10 SWIA200515396 120050805A3350 TERMINAL EMB 120 EMB120ER 3260203SO LOOSE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07576SW 120345 ROW 6A EMERGENCY EXIT ROW LIGHT DOES NOT ILLUMINATE. CONNECTED RING TERMINALS TO SIGN. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050810002392005081000239EA 2005 8 10 SWIA200515397 120050803A2611 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA DIRTY A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07932SW 7714 FALSE SMOKE CARGO WARNING AT THE GATE. CLEANED CANNON PLUGS. OPERATIONAL CHECK GOOD IAW 25-15-01. 2L72 4F RTA21EA 20050810002402005081000240 2005 8 10 SWIA200515398 420050801A34183995100208 COMPUTER CNDAIRCL600 CL6002B19 1900309EA MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TOTAKEOFF 1 NM07588SW422 422 7069 "STALL FAIL" CAUTION MSG CAME ON AFTER T/O. REPLACED STALL PROTECTION COMPUTER IAW AMM 27-35-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050810002462005081000246WP 2005 8 10 AALA20050496 120050803A3350 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217541A 49995 DTW - EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK AND CHARGER ASSEMBLY FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050810002472005081000247EU 2005 8 10 AALA20050493 120050803A3350P4010049 BATTERY PACK AIRBUS300 A300B4605R 3930308EU CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW2118066 509 JFK - EMERGENCY LIGHTS AT SEATS 29 TO 33C AND 35 TO 37C INOPERATIVE. REPLACED LEFT NUMBER 4 BATTERY PACK FOR EMERGENCY LIGHTS AT SEATS 29 TO 33C AND 35 TO 37C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20050810002482005081000248WP 2005 8 10 AALA20050503 120050806A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21968TW 53618 ORD - EMERGENCY LIGHTS AT OVERHEAD ROWS 19 TO 21 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD ROWS 19 TO 21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050810002502005081000250WP 2005 8 10 AALA20050497 120050802A3350P4010049 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21442AA 49468 LGA - EMERGENCY LIGHT AT CABIN SEAT INOPERATIVE. REPLACED MID AND AFT AND FORWARD BATTERY PACKS FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050810002522005081000252WP 2005 8 10 AALA20050499 120050728A3350201720003 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21574AA 53151 TUL - EMERGENCY PATH LIGHTING AT SEATS 14DEF INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY PATH LIGHTING AT SEATS 14DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050810002532005081000253WP 2005 8 10 AALA20050504 120050807A3213 STRUT DOUG DC9 DC982 3022082WP LACK OF LUBE A AALAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 SW21258AA 49288 ORD - INFLIGHT AFTER TAKEOFF NOSE WHEEL WOULD NOT RETRACT. PERFORMED FULL NOSE STRUT SERVICE AND LUBED NOSE GEAR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050810002552005081000255NM 2005 8 10 AWXA200500921 120050712A5320654583469 STRAP BOEING737 7373S3 1384711NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 DURING C18 CHECK DISCOVERED STABILIZER STRAP CRACKED, .65 INCHES IN LENGTH, ON CABIN FLOOR AT BS 330, BL 15L, WL 204. MX STOP DRILLED CRACK IN STABILIZER STRAP AT BS 330, BL 15L, WL 204 IAW BOEING 737-300 SRM 53-10-51-2. FABRICATED REPAIR PLATE IAW BOEING 737-300 SRM 53-10-51-2 FIG 204. INSTALLED REPAIR PLATE ON STABILIZER STRAP AT BS 330, BL 15L, WL 204 IAW BOEING 737-300 SRM 51-40-02-0. 2L72 4F RTA16WE 20050810002562005081000256NM 2005 8 10 AWXA200500922 120050713A521065458076 FRAME BOEING737 7373S3 1384711NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 DURING C18 CHECK DISCOVERED ANGLE CRACKED, .375 INCHES IN LENGTH, AT FORWARD UPPER CORNER OF THE R1 DOOR, CUTOUT. MAINTENANCE CUT OUT CRACKED AREA OF FRAME ANGLE IAW BOEING 737-300 SRM 51-70-11-0. FABRICATED FILLER AND DOUBLER IAW BOEING 737-300 SRM 51-70-11-0. INSTALLED FABRICATED REPAIR PARTS AT FORWARD UPPER CORNER OF THE R1 DOOR, CUTOUT, IAW BOEING 737-300 SRM 51-70-11-0 FIG. 1. 2L72 4F RTA16WE 20050810002582005081000258NM 2005 8 10 AWXA200500924 120050714A5755654645262A SPOILER BOEING737 7373S3 1384711NM ZONE 500 - LEFT DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 DURING C18 CHECK FOUND A DISBOND AREA ON THE UPPER SURFACE OF THE NR 4 SPOILER, 36" FROM INBOARD END FROM WBL 123.75 TO WBL 135.75. MAINTENANCE REMOVED DISBOND AREA FROM THE UPPER SURFACE OF THE NR 4 SPOILER, 36" FROM INBOARD END IAW BOEING 737-300 SRM. FABRICATED FILLER AND DOUBLER IAW BOEING 737-300 SRM 81-70-10-0. BONDED AND SEALED REPAIR PARTS TO THE UPPER SURFACE OF THE NR 4 SPOILER FROM WBL 123.75 TO WBL 135.75 IAW BOEING 737-300 SRM 51-70-10-0 FIG 31. 2L72 4F RTA16WE 20050810002592005081000259NM 2005 8 10 AWXA200500925 120050713A552365C2638415A TAB BOEING737 7373S3 1384711NM ZONE 300 - STABIDELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 DURING C18 CHECK DISCOVERED, THE LT HORIZONTAL ELEVATOR TAB DELAMINATED, AT OUTBOARD END, TOP SURFACE FROM ES 127L TO ES 129L. MAINTENANCE CUT OUT DELAMINATED AREA ON THE LT HORIZONTAL ELEVATOR TAB IAW BOEING 737-300 SRM 51-70-17-0 FIG 11. SANDED AND CLEANED AREA ON THE LT HORIZONTAL ELEVATOR TAB IAW BOEING 737-300 SRM 51-70-17-0. OBTAINED REPAIR PLIES AND BONDED TO SURFACE OF THE LT HORIZONTAL ELEVATOR, OUTBOARD END, TOP SURFACE, FROM ES 127L TO ES 129L IAW BOEING 737-300 SRM 51-70-17-0 FIG 11. NO WEIGHT WAS ADDED TO THE ELEVATOR IAW BOEING 737-300 SRM 51-60-06-0. 2L72 4F RTA16WE 20050810002612005081000261NM 2005 8 10 AWXA200500927 120050728A3350P4010021 POWER UNIT BOEING737 7373S3 1384711NM INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 DURING C18 CHECK DISCOVERED AFT FLIGHT ATTENDANT SEAT FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT FLIGHT ATTENDANT SEAT FLASHLIGHT POWER UNIT AS REQUIRED. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20050810002622005081000262NM 2005 8 10 AWXA200500928 120050718A5740656717218 FITTING BOEING737 7373S3 1384711NM ZONE 600 - RIGHTCORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 DURING C18 CHECK DISCOVERED CORROSION ON THE RT MLG STABILIZER BEAM, AFT ATTACH FITTING. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 57-20-30-1. MAINTENANCE REMOVED AND REPLACED THE AFT ATTACH FITTING ON THE RT MLG STABILIZER BEAM IAW BOEING 737-300 AMM 57-15-00-4. 2L72 4F RTA16WE 20050810002642005081000264NM 2005 8 10 AWXA200500930 120050712A521065458715 FRAME BOEING737 7373S3 1384711NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 DURING C18 CHECK DISCOVERED R1 DOOR FORWARD STOP CUTOUT, FOURTH FROM TOP, CRACKED, .60 INCHES IN LENGTH. MAINTENANCE TRIMMED OUT CRACK AREA AT R1 DOOR FORWARD STOP CUTOUT, FOURTH FROM TOP IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5200-5214-SS1. FABRICATED DOUBLER IAW AWA ER 03-5200-5214-SS1. INSTALLED FABRICATED REPAIR PARTS AT R1 DOOR FORWARD STOP CUTOUT, FOURTH FROM TOP IAW BOEING 737-300 SRM 51-40-02-0 FIG 3 AND AWA ER 03-5200-5214-SS1. 2L72 4F RTA16WE 20050810002662005081000266NM 2005 8 10 AWXA200500932 120050707A5320 STRUCTURE BOEING737 7373S3 1384711NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 DURING C18 CHECK DISCOVERED SEVERAL SUBSTRUCTURES CRACKED AT THE L1 FWD ENTRY DOOR CUTOUT FROM STR 15L TO STR 16L, BS 348.20. MX REMOVED ALL DAMAGED PARTS, (1) CLIP CRACKED .5", (2) CLIP CRACKED .5", (3) CLIP CRACKED .5", (4) CLIP CRACKED .5" IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5312-05215-SS2. FAB`D REPAIR CLIPS IAW AWA ER 03-5312-05215-SS2. MX INSTALLED FABRICATED REPAIR PARTS AT THE L1 FWD ENTRY DOOR CUTOUT FROM STRINGER 15L TO STRINGER 16L, BS 348.20 IAW AMERICA WEST AIRLINES ER 03-5312-05215-SS2. (1)CLIP, PN 69-16970-501; NSN; BOEING; CRACKED (2)CLIP, PN 69-26555-2; NSN; BOEING; CRACKED (3)CLIP, PN 69-26555-3; NSN; BOEING; CRACKED(4)CLIP, PN 65-16509-6; NSN; BOEING; CRACKED. 2L72 4F RTA16WE 20050810002672005081000267WP 2005 8 10 AALA20050509 120050808A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21296AA 49308 DTW - EMERGENCY LIGHTS AT FORWARD OVERHEAD GALLEY AND IN COACH INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD OVERHEAD GALLEY AND IN COACH. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050810002692005081000269NE 2005 8 10 AALA20050500 220050805A7200 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE SHUTDOWN A AALAO OTHER Y ENGINE STOPPAGE DEDESCENT 1 SW21587AA 53250 726017 DFW - INFLIGHT LEFT ENGINE FAILED DURING DESCENT. N1 AND N2 CONTINUED TO WINDMILL. EXHAUST GAS TEMPERATURE OVER 800 DEGREES. TIME ON SINGLE ENGINE APPROXIMATELY 10 MINUTES. LANDED WITHOUT INCIDENT. REPLACED LEFT ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 F A6WE E9NE 20050810002712005081000271WP 2005 8 10 AALA20050502 120050805A3350 CONNECTOR DOUG DC9 DC982 3022082WP CABIN LOOSE A AALAK NONE O OTHER ININSP/MAINT 1 SW21423AA 49335 DFW - EMERGENCY LIGHT AT SEAT 12D INOPERATIVE. RESECURED CONNECTOR UNDER SEAT FOR EMERGENCY LIGHT AT SEAT 12D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050810002722005081000272NM 2005 8 10 AALA20050505 120050807A3350 CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE O OTHER ININSP/MAINT 1 SW21345AN 33084 DFW - SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 22 TO 25HJ INOPERATIVE. SECURED LOOSE CONNECTOR AT SEAT 25HJ FOR SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 22 TO 25HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050810002742005081000274EU 2005 8 10 AWXA200500934 120050714A5753D57570050010 FLAP AIRBUS320 A320231 3930325EU ZONE 500 - LEFT DETERIORATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28627AW 66 DURING C4 CHECK DISCOVERED COMPOSITE DETERIORATED AT TRAILING EDGE OF THE INBOARD FLAP ON THE LT WING. MAINTENANCE GROUND DOWN AND CLEANED THE SURFACE OF THE INBOARD FLAP, TRAILING EDGE, L/H WING IAW AIRBUS A320 SRM 57-52-00. APPLIED GLASS FABRIC AND LAMINATING RESIN TO TRAILING EDGE INBOARD FLAP, LT WING, IAW AIRBUS A320 SRM 57-52-00 AND AMERICA WEST AIRLINES ENGINEERING REPAIR NR 26-5752-05213-RC2. 2L72 4F RTA28NM 20050810002762005081000276EU 2005 8 10 AWXA200500936 120050712A5320D53112094203 WEB AIRBUS320 A320231 3930325EU CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28627AW 66 DURING C4 CHECK DISCOVERED CORROSION ON WEB NEXT TO FORWARD FRAME OF THE R1 DOOR, FS 16 TO FS 14, -Y1379.5. MAINTENANCE REMOVED CORROSION IAW AIRBUS 320 SRM 51-74-00. NO ALLOWABLE DAMAGE LIMITS AVAILABLE. MAINTENANCE FABRICATED DOUBLER IAW AMERICA WEST ENGINEERING REPAIR NR 26-5312-05204-ES1. INSTALLED FABRICATED REPAIR PARTS FROM FS 14 TO FS 16, -Y1379.5 IAW AWA ER NR 26-5312-05204-ES1. 2L72 4F RTA28NM 20050810002772005081000277EU 2005 8 10 AWXA200500937 120050712A5320D53475565212 COVER AIRBUS320 A320231 3930325EU CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28627AW 66 DURING C4 CHECK DISCOVERED CORROSION ALONG LOWER SILL COVER SHEET, UPPER SURFACE, FROM FS 52A TO FS 56 IN THE AFT CARGO COMPARTMENT. MAINTENANCE MECHANICALLY REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-41-49. REMOVED COVER SHEET AND INSTALLED NEW COVER SHEET FROM FS 52A TO FS 56 IN THE AFT CARGO COMPARTMENT IAW AIRBUS 320 SRM 51-42-11. 2L72 4F RTA28NM 20050810002812005081000281SO 2005 8 10 SIMA200520603 120050720A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FR 20 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21813AE 145539 THE LT OMEGA BEAM AT FR 20 WAS FOUND CORRODED. PERFORMED A CUT OUT TO REMOVE THE CORROSION. FABRICATED A DOUBLER, FILLER, PLATE, AND 2 SHIMS. REPAIR DONE IAW SRM. (K) 2L72 4F4 FRTT00011ATTE6CH 20050808001902005080800190NM 2005 8 8 DHL2005740011 120050804A3150 WARNING HORN BOEING727 7272Q9 138448MNM ACTIVATED A DHLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01740DH 21930 AURAL TAKEOFF WARNING ON TAKEOFF ROLL COMPLETED W/ RTO FLOW CHART A/C SPEED NOT ABOVE 10 KNOTS. LUBED FLAP TAKEOFF SWITCH, OPS CKS GOOD IAW MM 31-26-00. 2L73 4F RTA3WE 20050809000042005080900004WP 2005 8 9 IXXA05SMN68S 120050623A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE DAMAGED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING C CHECK INSPECT, UAL DRAIN DOUBLER ON FWD LOWER FUSELAGE, STA FS 224.000, L-35.75R REPAIR MUST BE UPGRADED. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05258 DATE 06-24-05, SEMAN DWG ED 3994 DATE 06-22-05, EO SEMAN NR 2005832 DATE 06-24-05. REMOVED EXISTING REPAIR DOUBLER IAW DC-8 SRM 51-1-21 PAGE 1, DC-8 SRM 51-1-20D PAGE 21. FABRICATED REPAIR DOUBLER (ALCLAD 7075 T6 0.080”) + (02 EA) INTERNAL FINGER DOUBLER (ALCLAD 7075 T6 0.032”) IAW SEMAN ED 3994 AND DC-8 SRM 51-1-4 PAGE 1. CLEANED, TREATED AND PRIMED AREA + REPAIR PARTS IAW DC-8 SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11. INSTALLED REPAIR PARTS IAW SEMAN DWG ED 3994, DC-8 SRM 51-1-21 PAGE 1, DC-8 SRM 51-1-20D PAGE 2L74 4F RT4A25 20050809000052005080900005WP 2005 8 9 IXXA05SMN69S 120050623A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE DAMAGED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING C CHECK INSPECT, EXTERNAL DOUBLER LWR FUSELAGE, STA FS 238.000, L-31R REPAIR EXCEEDS MAX RIVETS SPACING ON SIDES 1 FWD, 2 UPPER AND 4 LOWER ADD ADDITIONAL RIVETS OR REWORK SIDES 1,2 AND 4 TO BRING INTO LIMITS PER SRM BELOW 1.400” SPACING (REF. 822BX-R35). PERFORMED MAJOR REPAIR IAW DC-8 SRM 53-2-1 FIG 7 EO SEMAN NR 2005866 DATE 06-13-05. REMOVED EXISTING REPAIR DOUBLER IAW DC-8 SRM 51-1-20D PAGE 21, DC-8 SRM 51-1-21 PAGE 1. FAB`D REPAIR DOUBLER (ALCLAD 7075 T6 0.080”) + (02 EA) INTERNAL FINGER DOUBLER (ALCLAD 7075 T6 0.050”) IAW DC-8 SRM 53-2-1 FIG 7 SHEET 1, 4, DC-8 SRM 53-4-1 FIG 1. ITEM “B”, DC-8 SRM 51-9-0 FIG 68A, DC-8 SRM 51-1-4 PAGE 1. CLEANED, TREATED AND PRIMED AREA + REPAIR PARTS IAW DC-8 SR2L74 4F RT4A25 20050809000162005080900016NM 2005 8 9 CALA0500258 120050806A335020131A BATTERY BOEING737 737524 1384721NM FWD CABIN INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2713624 27528 THE EMERGENCY LIGHTS IN FORWARD CABIN WOULD NOT ILLUMINATE DURING TEST WHILE IN SERVICE CHECK. THE BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51-51. 2L72 4F RTA16WE 20050809000172005080900017NM 2005 8 9 CALA0500259 120050806A3350D71702001 POWER SUPPLY BOEING737 737724 13844BYNM LH OVRWG EXIT INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2717719 28938 THE LT OVERWING EXIT EMERGENCY LIGHTS WERE FOUND INOPERATIVE DURING SERVICE CHECK TEST. THE POWER SUPPLY AND BATTERY PACK WERE REMOVED AND REPLACED IAW MM 33-51-06. 2L72 4F RTA16WE 20050809000212005080900021WP 2005 8 9 IXXA05SMN97S 120050627A5311 FRAME DOUG DC8 DC871F 302199DWP ZONE 100 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, NOSE SECTION, DOUPLER ANTENNA FRAME WITH 02 CRACKS 2" EACH ONE. REMOVED DOUPLER ANTENNA FRAME (CRACKED) IAW DC-8 SRM 51-1-21 PAGE 1. FABRICATED NEW DOUPLER ANTENNA CAP IAW DWG DOUGLAS NR 561601 (ALCLAD 7075 T6 0.125). PERFORMED HEAT TREATMENT IAW DC-8 SRM 51-1-1 PAGES 1,13,17. CLEANED, TREATED AND PRIMED IAW DC-8 SRM 51-1-8B. INSTALLED NEW CAP IAW DC-8 SRM 51-1-2 PAGE 1. 2L74 4F RT4A25 20050809000272005080900027WP 2005 8 9 IXXA05SMN56S 120050623A5330 DOUBLER DOUG DC8 DC871F 302199DWP FUSELAGE OUT OF LIMITS B IXXAO OTHER O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING C CHECK INSPECT, LT FWD FUS ABOVE AND AFT TURBO COMPRESSOR, SIDE 1 (FWD) BELOW, MIN EDGE DISTANCE FOR RIVETS, REPAIR DOUBLER RATIO ABOVE LIMITS TO THICK, STA FS 116.000 L-21.5L. UPGRADE REPAIR BY REPLACING EXISTING DOUBLER WITH 0.071AND ENSURE MIN EDGE DISTANCE IS WITHIN SRM LIMITS ON SIDE 1. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 # 05280 DATE 07-04-05, SEMAN DWG # ED 3991 DATE 06-28-05, EO SEMAN NR 2005895 DATE 07-04-05. REMOVED EXISTING REPAIR DOUBLERS IAW DC-8 SRM 51-1-21 PAGE 1, DC-8 SRM 51-1-20D PAGE 21. PERFORMED NDT INSPECT IAW DC-8 SPM PART 06-10-01-001. FAB`D REPAIR DOUBLER (ALCLAD 7075 T6 0.071”) + REPAIR TRIPLER (ALCLAD 7075 T6 0.080”) + (03 EA) INTERNAL FINGER DOUBLER (ALCLAD 7075 T6 0.032L74 4F RT4A25 20050809000292005080900029NM 2005 8 9 AWXA200500907 120050713A534069366001 STRINGER CLIP BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 DURING C18 CHECK DISCOVERED STINGER CLIP CRACKED, .200 INCHES IN LENGTH, AT BS 277, STRINGER 10R. MAINTENANCE REMOVED STRINGER CLIP AT BS 277, 10RT IAW BOEING 737-300 SRM 51-40-02-0 FIG 8. FABRICATED NEW STRINGER CLIP IAW BOEING DWG 65-45805. MAINTENANCE INSTALLED FABRICATED REPAIR PARTS IAW BOEING 737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050809000342005080900034 2005 8 9 BA05015 420050803A25657A1508115 SLIDE AIRBUS330 A330323 3930335EU PASSENGER CABIN FALSE INDICATIONA USAAK NONE O OTHER ININSP/MAINT 1 EA19676UW2314910377 375 PHL - PRIOR TO FLIGHT, RECEIVED "SLIDE LOW PRESSURE 4L" MESSAGE. MAINTENANCE RELEASED THE AIRCRAFT ON MEL FOR A SLIDE INDICATION PROBLEM. MAINTENANCE REPLACED THE 4L DOOR EMERGENCY ESCAPE SLIDE. OK FOR SERVICE. 2L72 4F RTA46NM 20050809000512005080900051 2005 8 9 ASO2005F00007 420050711A83005018T49P01 CARBON SEAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE ACCY GB WORN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27875AS SAPL0831 7559 872776 STARTER CARBON SEAL, WORN. (K) 2L72 4F4 FRTA21EA E15NE 20050809000762005080900076SW 2005 8 9 PNSA050703 120050729A2910 LINE SWRNGNSA227 SA227AC 8780603SW HYDRAULIC SYS FAILED A PNSAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 AL032719H 713B DURING CRUISE ENROUTE, 100 MILES WEST, LT HYDRAULIC LIGHT CAME ON FOLLOWED WITH RT WARNING LIGHT. CREW CONFIRMED ON HYD PRESSURE GAUGE LOSS OF PRESSURE. CREW DECLARED AN EMERGENCY WITH CENTER AND DIVERTED WHERE MAINT WAS AVAILABLE. MAINT FOUND HARD HYDRAULIC PRESSURE LINE IN ENGINE COMPARTMENT HAD FAILED. FABRICATED LINE AND RELEASED AIRCRAFT FOR SERVICE. ON RETURN TO HOME BASE FABRICATED LINE WAS REPLACED WITH FACTORY LINE. 2L72 4T RTA8SW 20050809000782005080900078NM 2005 8 9 ASMF200508003 120050804A3241426071 CONTROL BOX DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE ANTI-SKID SYS INOPERATIVE W ASMFC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW23831LF3557 3557 53050 AIRCRAFT REJECTED TAKEOFF (WHEEL NOT TURNING) LIGHT TURNED ON. ANTISKID CONTROL BOX WAS REPLACED IAW MM 32-43-00, TESTED CORRECT. 2L72 4F4 FRT E9NE 20050809000942005080900094SO 2005 8 9 SIMA200518101 120050627A3350602024 LIGHT EMB 145 EMB145LR 3260212SO ALLSN AE3007AE3007C GL CABIN FAILED A SIMAK NONE L NO TEST TXTAXI/GRND HDL 1 SW21671AE 145793 DISC - EMERGENCY EXIT SIGN LIGHT AT THE COCKPIT DOOR STEP INOPERATIVE. REPLACED EMERGENCY EXIT SIGN LIGHT. OPERATIONAL CHECK GOOD. RETURNED TO SERVICE. (K) 2L72 4T4 FRTT00011ATTE6CH 20050809001012005080900101SO 2005 8 9 SIMA200519305 120050626A532014524110009 SILL EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21809AE 145521 DURING INSPECTION, FOUND FORWARD CABIN SILL LT HAS SMALL AREA OF CORROSION ON UPPER FORWARD SIDE. REMOVED AND REPLACED LT SILL IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4F4 FRTT00011ATTE6CH 20050809001052005080900105EA 2005 8 9 ASO2005F00001 120050714A335020131A BATTERY CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 2 BATTERY DISCHARGED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27820AS5031 1882 7188 DURING GROUND INSPECTION, THE EMERGENCY FLOOR LIGHTS AT ROWS 2-4 WERE FOUND TO BE INOPERATIVE. MAINTENANCE CHARGE THE EMERGENCY LIGHT BATTERIES, CLEANED AND RESECURED THE CONNECTIONS. OPERTIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050809001082005080900108EA 2005 8 9 ASOA05609 120050715A5242H34455 HANDLE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE AVIONICSBAY DOO CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27703EV 10038 10038 DURING A C-CHECK, THE AVIONICS BAY DOOR EXTERIOR HANDLE WAS FOUND CRACKED AROUNG THE BASE. MAINTENANCE IS REMOVING AND REPLACING THE AVIONICS BAY DOOR HANDLE. (K) 2L72 4F4 FRTA21EA EOOO63EN 20050809001202005080900120EA 2005 8 9 ASO2005F00006 120050713A5350 FAIRING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE DAMAGED A ASOAK NONE O OTHER TOTAKEOFF 1 SO27902EV 7620 DURING TAKEOFF, TOWER INFORMED CREW THAT TIRE DEBRIS WAS NOTICED ON RUNWAY AFTER DEPARTURE. THERE WERE NO INDICATIONS OF ENGINE DAMAGE AND AC CONTINUED. EMERGENCY WAS DECLARED AND EMERGENCY VEHICLES WERE REQUESTED TO BE ON STANDBY AS PRECAUTION. AC LANDED SAFELY. UPON TOUCHDOWN, FIRE AND RESCUE CONFIMED IB RT MAIN TIRE WAS SHREDDED. MAINT REMOVED AND REPLACED RT MLG IB AND OB WHEEL AND TIRE ASSEMBLIES. ALSO, FOUND RT IB FLAP ASSEMBLY, RT WING T/E FAIRING AND RT SIDE AFT BELLY FARING DAMAGED. MAINTENANCE REMOVED AND REPLACED RT IB FLAP ASSY AND RT WING TRAILING EDGE FAIRING. MAINT REPAIRED THE RT SIDE AFT BELLY FAIRING IAW SRM. OPS CHECK GOOD. AC OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050809001362005080900136NM 2005 8 9 TSAA0552034 120050801A5270 WARNING LIGHT BOEING737 73776N 13844CHNM COCKPIT ILLUMINATED A TSAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP13748AL 30050 ETOPS FLT 468 (OGG - SMF), DOOR ANNUNCIATOR LIGHT ILLUMINATED TWICE DURING TAKEOFF ROLL THEN EXTINGUISHED DURING ABORT AND REMAINED OFF.MTX: INSPECTED ALL DOORS; DOORS HAVE POSITIVE LOCK; NO DEFECTS NOTED; INDICATION STAYED OFF A/C RETURNED TO SERVICE. 2L72 4F RTA16WE 20050809001382005080900138SO 2005 8 9 SIMA200519311 120050702A5330AL2024T3 SKIN EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FR 72, 74 DENTED A SIMAO OTHER O OTHER NRNOT REPORTED 1 SW21649PP 145234 AIRCRAFT ARRIVED FOR REPAIR OF A DENT WITH A SCRATCH BETWEEN FRAMES 72 AND 74 AND STRINGERS14L AND 15L. REMOVED THE DAMAGE BY MAKING A CUT OUT. FABRICATED AN EXTERNAQL DOUBLER AND FILLER. REPAIR DONE IAW SRM. (K) 2L72 4T4 FRTT00011ATTE6CH 20050809001432005080900143NM 2005 8 9 AWXA200500910 120050807A3350321431 BATTERY AIRBUSA319 A319132 3930340NM FAULTY A AWXAK NONE O OTHER ININSP/MAINT 1 WP28818AW 1375 PHX - EEL - DURING 4 DAY CHECK DISCOVERED EPSU COMM EMER L MESSAGE ON CIDS PANEL DURING FUNCTIONAL TEST. MAINTENANCE REMOVED AND REPLACED THE BATTERY FROM THE FORWARD LEFT EMERGENCY PACK. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA28NM 20050809001452005080900145 2005 8 9 AWXA200500912 420050806A3414 INDICATOR BOEING737 7373S3 1384711NM AIRSPEED INOPERATIVE A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28312AW 24060 LAS - ABORTED TAKEOFF - FLT 831 - DURING TAKEOFF, CAPTAINS AIRSPEED INDICATOR FLAGGED. REJECTED TAKEOFF AT 90 KNOTS. CREW RESET ADC NR 1 CIRCUIT BREAKER PER MAINTENANCE CONTROL. FLIGHT CONTINUED ON WITHOUT FURTHER INCIDENT. A FOLLOW UP HAS BEEN WRITTEN TO REMOVE AND REPLACE THE CAPTAIN'S AIRSPEED INDICATOR. 2L72 4F RTA16WE 20050809001472005080900147NM 2005 8 9 AWXA200500914 120050711A57536546435277 WEDGE BOEING737 7373S3 1384711NM FLAP DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 MCN - DURING C18 CHECK, DISCOVERED THE LT OUTBOARD AFT FLAP DELAMINATED AT THE INBOARD END OF THE UPPER AND LOWER SURFACES AT WBL 23.68 TO WBL 235.68. MAINTENANCE REMOVED DAMAGED AREA ON THE LT OUTBOARD AFT FLAP AND PREPARED FOR REPAIR IAW BOEING 737-300 SRM 51-70-10-0 FIG 16. FABRICATED REPAIR DOUBLERS AND FILLER IAW BOEING 737-300 SRM 51-70-10-0 FIG 16. INSTALLED, BONDED AND SEALED REPAIR PARTS TO THE LT OUTBOARD AFT FLAP, THE INBOARD END OF THE UPPER AND LOWER SURFACES AT WBL 23.68 TO WBL 235.68 IAW BOEING 737-300 SRM 51-70-10-0 FIG 16. 2L72 4F RTA16WE 20050809001492005080900149NM 2005 8 9 AWXA200500916 120050714A532069353502 CLIP BOEING737 7373S3 1384711NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 DURING C18 CHECK DISCOVERED ATTACH CLIP AT BS 500A, STRINGER 16R CRACKED .275 INCHES IN LENGTH. MAINTENANCE REMOVED CRACKED CLIP AT BS 500A, STRINGER 16R. RECEIVED AND PREPARED NEW STRINGER CLIP FOR INSTALLATION IAW BOEING 737-300 SRM 51-40-05-0 FIG 2 & 3. INSTALLED NEW STRINGER CLIP IAW BOEING 737-300 SRM 51-40-02-0 FIG 8 & 12. 2L72 4F RTA16WE 20050809001512005080900151EU 2005 8 9 MALA050632 120050802A5311 FRAME SAAB SF340 SF340A 7850100EU CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15110XJ 340A110 DURING 4Y/2Y INSPECTION IN BNA, FRAME 686.888 RT SIDE OF FUSELAGE HAS BEEN CHAFED BY CARGO DOOR CABLE. DAMAGE HAS BEEN REPAIRED IAW MESABA EO#53308. REFER EAMS WORK ORDER #212691 TASK 2505. 2L72 4T RTA52EU 20050809001532005080900153NM 2005 8 9 AWXA200500918 120050714A5340 CLIP BOEING737 7373S3 1384711NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 DURING C18 CHECK FOUND SEVERAL CLIPS CRACKED LOCATED AT BS 380, STRINGER 1 (1.5" LONG), STRINGER 2R (1.5" LONG) AND STRINGER 8L (.26" LONG). MAINTENANCE REMOVED CRACKED CLIPS AT BS 380, STRINGER 1, STRINGER 2R AND STRINGER 8L IAW BOEING 737-300 SRM 51-40-02-0 FIG 8. RECEIVED NEW CLIPS AND PREPARED FOR INSTALLATION IAW BOEING 737-300 SRM 51-40-05-0. INSTALLED REPAIR PARTS AT BS 380, STRINGER 1, STRINGER 2R AND STRINGER 8L IAW BOEING 737-300 SRM 51-40-02-0 FIGS 3, 8 AND 12. 2L72 4F RTA16WE 20050809001592005080900159SO 2005 8 9 SIMA200519201 120050708A335020131A BATTERY EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL CABIN DISCHARGED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21820AE 145576 DISC SEVERAL EMERGENCY EXIT SIGNS IN THE FORWARD CABIN WILL NOT ILLUMINATE. REPLACED BATTERY CHARGER AND BATTERY PACK IAW WC 33-700-19. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. CHARGER ASSEMBLY PN OFF IS 110049 AND SN OFF IS 17435. (K) 2L72 4F4 FRTT00011ATTE6CH 20050809001612005080900161SO 2005 8 9 SIMA200519316 120050705A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FRAME 20 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21811AE 145529 A PREVIOUS REPAIR ON THE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. REMOVED THE EXISTING REPAIR AND CLEANED THE AREA. FABRICATED AN EXTERNAL ANGLE, FILLER REPAIR PLATE AND 2 SHIMS. REPAIR DONE IAW SRM. (K) 2L72 4F4 FRTT00011ATTE6CH 20050809001632005080900163SO 2005 8 9 SIMA200519314 120050707A532014521713005 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FR 25 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21712AE 145247 THE CENTER OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE CENTER OMEGA BEAM TO REMOVE CORROSION FABRICATED A FILLER DOUBLER AND 2 SHIMS. REPAIR DONE IAW SRM. (K) 2L72 4F4 FRTT00011ATTE6CH 20050810000012005081000001NM 2005 8 10 DHL2000746509 120050630A5754 FRAME BOEING727 727224 1384076NM NR 5 SLAT BROKEN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01746DH 22252 LWR AFT CORNER OF ATTACH FRAME INBOARD OF 1439 SLAT ATTACH POINT ON NR 5 SLAT BROKEN. REMOVED NR 5 SLAT TO REPAIR IAW B727 MM 27-81-1, REMOVED INNER PANELS AND I/B & O/B RIBS FOR REPLACEMENT IAW B727 SRM 51-30-2, DRILLED, TREATED AND PRIMED PARTS AND AREA IAW B727 SRM 51-10-2. INSTALLED I/B & O/B RIBS IAW B727 SRM 51-30-2, REINSTALLED INNR PANELS IAW B727 SRM 51-30-2, REINSTALLED NR 5 SLAT IAW B727 MM 27-81-1. OPS CHECK GOOD IAW B727 MM 27-81-0 PO 5070101 P/N 65-17276-11, PO 5070101, P/N 65-17276-9. 2L73 4F A3WE 20050810000382005081000038NM 2005 8 10 05FDEA02297 120050807A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE RIGHT NR 15 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. 2L73 4F RTA22WE 20050810000462005081000046NM 2005 8 10 05FDEA02317 120050808A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE LEFT NR 04 FOUND WITH CORROSION EXCEEDING LIMITS. BARREL NUT BORE REAMED TO 0.974 DIAMETER. BOTTOM BORED THRU FOUND CLEAN HOLE COND. C3 AND ACCEPTABLE PER EO 1-5510-7-5000 D1 PT1. INSP/REPAIR HORIZONTAL STAB.BARREL NUT HOLES AD 2003-22-08/SB MD11-55-023. (BUCKET BUSHING INSTALLED) MINOR REPAIR PER GMM 6-2-100. 2L73 4F RTA22WE 20050810000492005081000049NM 2005 8 10 05FDEA02320 120050808A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE RIGHT NR 05 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. 2L73 4F RTA22WE 20050810000622005081000062NM 2005 8 10 SWAA052330 120050803A33509250071 BULB BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29456WN 32463 EEPLS TRACK LIGHT INOP AT FWD END. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050810000682005081000068 2005 8 10 SWAA052336 420050804A2565D31354 SLIDE BOEING737 7373TO 138447GNM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29697SW 23838 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20050810000722005081000072NM 2005 8 10 SWAA052340 120050805A3350BR2013 LIGHT BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29361SW 26572 DURING SCHEDULED C2 CHECK, FOUND EEPLS STRIP INOP AT ROW 1 DEF & ROW 8 DEF. REMOVED AND REPLACED EEPLS STRIP PER MM. 2L72 4F RTA16WE 20050810000732005081000073NM 2005 8 10 SWAA052341 120050805A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29361SW 26572 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050810000742005081000074NM 2005 8 10 SWAA052342 120050804A5753 SKIN BOEING737 7373H4 1384600NM LT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29390SW 2447 26593 DURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED FLAP PER MM. 2L72 4F RTA16WE 20050810000752005081000075NM 2005 8 10 SWAA052343 120050805A3350101331 COVER BOEING737 7377H4 1384404NM MID CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29444WN 29839 EMERGENCY OVERWING EXIT LOWER LIGHT COVER LOOSE. SECURED COVER PER MM. 2L72 4F RTA16WE 20050810000792005081000079NM 2005 8 10 SWAA052347 120050803A5753 SKIN BOEING737 7373G7 1384595NM RT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29671SW 23785 DURING SCHEDULED C3 CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED FLAP PER MM. 2L72 4F RTA16WE 20050810000812005081000081NM 2005 8 10 SWAA052349 120050805A5753BACB10BH60F11 BEARING BOEING737 7373A4 1384585NM RT WING TE FLAP WORN A SWAAO OTHER O OTHER NRNOT REPORTED 1 SW29680AA 23505 VIBRATION FELT DURING FLAPS OPERATION. FOUND 5 EACH RIGHT INBOARD T/E FOREFLAP TRACK BEARINGS WORN & ONE BEARING BROKEN. REMOVED AND REPLACED BEARINGS PER MM. 2L72 4F RTA16WE 20050810000882005081000088NM 2005 8 10 SWAA052323 120050804A534065C27314 CLIP BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29317WN 24068 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 420, STR 4R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050810000902005081000090NM 2005 8 10 SWAA052325 120050804A53116546552 FRAME BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29317WN 24068 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 747, BS 807, BS 827, BS 847 & BS 867, STR 8L TO STR 9L. REPAIRED FRAMES PER SRM. 2L72 4F RTA16WE 20050810000972005081000097 2005 8 10 VNAA0507011 420050715A34406229302004 RADAR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE WX SYS FAILED A VNAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL05259PS2206 7945 DURING CLIMB THE CREW REPORTED THAT THE WEATHER RADAR WAS PAINTING A LARGE RETURN ON THE RIGHT SIDE OF THE SCREEN WHEN THE AIRCRAFT BANKED. DUE TO WEATHER EN ROUTE AND AT DESTINATION THE CREW ELECTED TO RETURN TO CAK. MAINTENANCE REMOVED AND REPLACED THE WEATHER RADAR RECEIVER/TRANSMITTER/ANTENNA UNIT IAW CRJ200 AMM 34-41-01-400-801. FUNCTIONAL AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050810001042005081000104EU 2005 8 10 08042005A 120050804A2711 AILERON SAAB SF340 340B 7860101EU OUT OF RIG A NSVAO OTHER F FLT CONT AFFECTED CRCRUISE 1 EA27306CE 203 A/C HAS EXCESSIVE ROLL TO THE LEFT. REQUIRES 1.5 UNITS OF AILERON TRIM. PERFORMED AILERON TRIM RIGGING. 2L72 4T RTA52EU 20050810001132005081000113CE 2005 8 10 08082005G 120050806A2730130610000614 ELEVATOR BEECH 1900 1900D 1154162CE DAMAGED A NSVAO OTHER F FLT CONT AFFECTED ININSP/MAINT 1 EA27243CJ UE43 RT ELEVATOR, OUTBOARD HINGE CLEVIS AND STABILIZER HINGE BRACKET HAS NO CLEARANCE. 2L72 4T RTA24CE 20050810001232005081000123NM 2005 8 10 UPS05545057 120050723A3210 BEARING BOEING757 75724APF 1384969NM LT MLG CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01447UP 27736 LEFT MLG FWD TRUNNION BEARING CORRODED NEAR TRUNNION LINK FWD PIN HOLES. REMOVED AND REPLACED LT MLG FWD TRUNNION BEARING IAW MM 57-54-05-4 STEPS 4 AND 5. 2L72 4F RTA2NM 20050810001242005081000124NM 2005 8 10 UPS05545062 120050807A3510MC1025104 OXYGEN MASK BOEING757 75724APF 1384969NM COCKPIT LEAKING A IPXAG O2 MASK DEPLOYED N FALSE WARNING NRNOT REPORTED 1 SO01409UP 23731 "A" CPTS OXYGEN MASK HARNESS "POPPED" AND STARTED LEAKING ON A CHECK TEST, CARD 0101. REMOVED AND REPLACED CPTS O2 MASK/REGULATOR ASSY IAW AMM 35-11-51-4. OPS CHECK GOOD . 2L72 4F RTA2NM 20050810001382005081000138NM 2005 8 10 QXEA200501154 120050805A243523088008 STARTER GEN DHAV DHC8 DHC8202 2809007NM MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION TOTAKEOFF 1 NM09367PH14109261 511 SEA FLIGHT NR 2272 - NR 1 DC GENERATOR CAUTION LIGHT ILLUMINATED FOLLOWED BY A NR 2 DC GENERATOR CAUTION LIGHT. DUAL DC GENERATOR CHECKLIST WAS RUN. LIGHT REMAINED ILLUMINATED. MAINTENANCE REPLACED NR 1 AND NR 2 STARTER-GENERATORS IAW MTC 98-01-001. PERFORMED FUNCITONCAL CHECK IAW AMM 24-31-00-720-801. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. NR 2 STARTER/GENERATOR P/N 23088-008, S/N 95006, TSN 9929.1, CSN 14330 AND TSR 264.3. 2H72 4T RTA13NM 20050810001412005081000141NM 2005 8 10 UPS05245071 120050711A5340 FITTING BOEING727 72722C 138400FNM CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01941UP 19196 RT MLG W/W, BS 870 FITTING HAS EVIDENCE OF CORROSION AT LOWER O/B FLANGE. REPAIRED IAW UPS EO 727-53-20186. (M) 2L73 4F A3WE 20050810001502005081000150NM 2005 8 10 UPS05445063 120050723A5313 STRINGER BOEING747 747121 1384871NM M/D CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 BS 2180-2200 S25R STRINGER FOUND CRACKED, CRACK LENGTH 5/8". BS 2180 TO BS 2208 STR 25R STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. 2L74 4F A20WE 20050810001552005081000155EA 2005 8 10 QXEA200501150 120050802A2410766277B IDG CNDAIRCL600 CL6002C10 1390015EA MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09603QX7017 3918 10011 DEN - ON FLIGHT 2456, THE ESSENTIAL AC CAUTION LIGHT CAME ON IN CRUISE AT 39,000. AUTOMATIC BUS TRANSFER DID NOT TAKE PLACE. RAN CHECKLIST WITH NO CHANGES. TURNED GENERATOR 1 TO OFF, RESET, THEN ON. THEN BUS TRANSFER TOOK PLACE. MAINTENANCE FOUND INTERNAL FAULT OF THE NR 1 IDG. REPLACED NR 1 IDG, AND PERFORMED A OPERATIONAL CHECK OF THE BUS AUTO TRANSFER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20050810001572005081000157EA 2005 8 10 SWIA200515371 120050719A5210 DOOR FRAME CNDAIRCL600 CL6002B19 1900309EA CRACKED A SWIAO OTHER O OTHER ININSP/MAINT 1 NM07406SW 7030 PAX DOOR FRAME FS 320.10 CRACKED, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR IAW CRJ REO 601R-52-11-402 REV "C". 2L72 4F RTA21EA 20050810001632005081000163EA 2005 8 10 SWIA200515377 120050719A5210 STRUCTURE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A SWIAO OTHER O OTHER ININSP/MAINT 1 NM07406SW 7030 PAX DOOR EDGE MEMBER FS319 CRACKED, ITEM FOUND AT C-CHECK INSPECTION. PAX DOOR EDGE MEMBER REPAIRED IAW CRJ REO 601R-52-11-279. 2L72 4F RTA21EA 20050810001722005081000172EA 2005 8 10 SWIA200515385 120050709A5320 BRACKET CNDAIRCL600 CL6002B19 1900309EA CORRODED A SWIAO OTHER O OTHER ININSP/MAINT 1 NM07426SW 7468 PAX DOOR CUT-OUT LOWER LONGERON BRACKETS AND CLEATS AT FS 316 AND 343 - CORRODED, ITEM FOUND AT C-CHECK. CORROSION REMOVED IAW CRJ SRM 51-21-06, 53-00-00. .002 MAT LOSS, .063 NOM .061 REMAINING WITHIN LIMITS IAW CRJ SRM 53-00-00. 2L72 4F RTA21EA 20050810001732005081000173EA 2005 8 10 SWIA200515386 120050709A5415 TRACK CNDAIRCL600 CL6002B19 1900309EA CRACKED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07426SW 7468 RT ENG INBOARD LOWER MAIN TRACK ASSEMBLY IS CRACKED, ITEM FOUND AT C-CHECK. MAIN TRACK ASSEMBLY REPLACED IAW CRJ AMM 78-34-11-400-801 & 78-34-11-000-801. 2L72 4F RTA21EA 20050810001762005081000176EA 2005 8 10 SWIA200515389 120050729A27515913163 DETECTOR CNDAIRCL600 CL6002C10 1390015EA MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07713SK1845 1845 10174 FLAPS HALFSPEED STATUS MSG DURING TAXI TO THE GATE. REPLACED RIGHT INBOARD FLAP, OUTBOARD ACTUATOR SKEW DETECTOR IAW CRJ MM 27-52-45. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050810001922005081000192NE 2005 8 10 2005UALA00746 220050801A7200 ENGINE BOEING757 757222 1384956NM PWA 2037 PW2037 NE CONTAMINATED A UALAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 WP29595UA 28748 RETURNED TO FIELD UNDER AMBER ALERT DUE TO FUMES IN THE COCKPIT. ODOR DISSAPATED DURING RETURN TO GATE. THE DETERGENT WASH OF THE ENGINES IS THE SORCE OF THE ODOR. PER MM 72-05-99 PAGE 701, ENGINE NEEDS HIGH POWER RUN AFTER WASH TO REMOVE ANY DETERGENT RESIDUAL FROM PNUEMATIC SYSTEM. 2L72 4F4 FRTA2NM E17NE 20050810002022005081000202NM 2005 8 10 2005UALA00755 120050801A5553 ATTACH FITTING BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE LT & RT VERT STACORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29912UA 25290 VERTICAL STABILIZER LT AND RT AFT PRIMARY ATTACH LUG FITTINGS ON FUSELAGE HAD CORROSION REMOVAL BEYOND LIMITS. REPLACED LT AND RT AFT PRIMARY ATTACH LUGS AND INSTALLED NEW BUSHINGS PER BACO DRAWING 65-52274. 2L72 4F4 FRTA16WE E2GL 20050810002062005081000206NM 2005 8 10 2005UALA00759 120050730A3350 LIGHT BOEING777 777222 1385219NM PWA PW4077PW4077 NE INOPERATIVE A UALAO OTHER L NO TEST ININSP/MAINT 1 WP29780UA 26944 SEAT 12D FWD EMERGENCY LIGHT ASSY BROKEN. REPLACED EEL LIGHT. 2L72 4F4 FRTT0001SE E46NE 20050810002112005081000211NM 2005 8 10 2005UALA00765 120050730A3350 INVERTER BOEING777 777222 1385219NM PWA PW4077PW4077 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29780UA 26944 SEAT 1F EMERGENCY LIGHTS INOP. REPLACED INVERTER. 2L72 4F4 FRTT0001SE E46NE 20050810002162005081000216WP 2005 8 10 IXXA05SMN142S 120050630A5720 VANE DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE XOLDI6.235 MISREPAIRED A IXXAO OTHER O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, LT WING SLOT VANE NON STANDARD REPAIR, STA XOLDI 6.235. REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-1-21 PAGE 1. REMOVED DAMAGED AREA IAW SEMAN DWG ED 4003, PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. FABRICATED EXTERNAL REPAIRS DOUBLER (ALCLAD 7075 T6 0.071) + FILLER (ALCLAD 7075 T6 0.063) + INTERNAL FINGER DOUBLER (ALCLAD 7075 T6 0.063”) IAW SEMAN DWG ED 4003, DC-8 SRM 51-1-4 PAGE 1. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PAGE 9. INSTALLED REPAIR PARTS IAW SEMAN DWG ED 4003, SRM 51-1-21 PAGE 1, SRM 51-3-0 PAGE 1, SRM 51-1-20D PAGE 9. TORQUED IAW SRM 51-3-1. 2L74 4F4 FRT4A25 E2GL 20050810002182005081000218WP 2005 8 10 IXXA05SMN111S 120050627A5730 WING DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE XRS 74. 869 S-10CRACKED A IXXAO OTHER O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, RT WING UPPER SKIN CRACKED 1INCH, STA. XRS 74. 869, S-10. REMOVED EXISTING REPAIR DOUBLERS SRM 51-1-20D PAGE 21. REMOVED DAMAGED AREA IAW SEMAN DWG ED 3981. PERFORMED NDT INSPECTION IAW SPM PART 06-10-01-001. FABRICATED EXTERNAL REPAIR DOUBLER (ALCLAD 7075 T6 0.160”) + (03 EA) FILLER PLUG (ALCLAD 7075 T6) IAW SEMAN DWG ED 3981. CLEANED, TREATED AND PRIMED AREA + REPAIR PARTS (INTERNAL PART) IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PAGE 9. INSTALLED REPAIR PARTS IAW SEMAN DWG ED 3981, SRM 51-1-20D PAGE 9. TORQUED IAW SRM 51-3-1. 2L74 4F4 FRT4A25 E2GL 20050810002372005081000237EA 2005 8 10 SWIA200515395 120050804A27604916405 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA MALFUNCTIONED A SWIAD RETURN TO BLOCK FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07928SW1076410760 7701 FLIGHT SPOILER FAULT ON TAXI OUT. REPLACED SECU IAW MM 27-61-00. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050810002412005081000241SO 2005 8 10 SWIA200515399 120050802A27523203001007 ACTUATOR EMB 120 EMB120ER 3260203SO MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED LDLANDING 1 NM07190SW1380 1380 120050 AFTER ADDING FLAPS TO 25 DEGREES ON FINAL APPROACH, NOTICED RIGHT ROLLING TENDANCY. REPLACED RIGHT OUTBOARD FLAP ACTUATOR. OPERATIONAL CHECK GOOD IAW MM 27-50-00. 2L72 4T RTA31SO 20050810002422005081000242EA 2005 8 10 SWIA200515400 120050727A2150GG670950091 ACM CNDAIRCL600 CL6002C10 1390015EA SEIZED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 NM07706SK 10149 ON TAKEOFF, STRONG SMELL OF SMOKE. REPLACED LEFT AIR CYCLE MACHINE IAW AMM 21-51-08. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050810002432005081000243EA 2005 8 10 SWIA200515401 120050722A2741 SWITCH CNDAIRCL600 CL6002B19 1900309EA INOPERATIVE A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07437SW 7564 FOS STAB TRIM SWITCH IS STICKY. REPLACED FO STAB TRIM DISC SWITCH IAW 27-41-30. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050810002702005081000270WP 2005 8 10 AALA20050501 120050805A3350P201003131S LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21485AA 49678 LGA - EMERGENCY DOOR EXIT LIGHT AT RIGHT NUMBER ONE DOOR INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050810002782005081000278SO 2005 8 10 SIM2005F00010 120050720A573014566207013 SKIN EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL LT WING DAMAGED A SIMAO OTHER O OTHER ININSP/MAINT 1 SW21925AE 14500908 LT AILERON AND WING WERE DAMAGED BY A CATERING TRUCK. MAINTENANCE REPLACED LT WING SPAR SEGMENT AND WING SKIN. REPLACED LT AILERON IAW EO. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4T4 FRTT00011ATTE6CH 20050810002832005081000283SO 2005 8 10 SIMA200520601 120050720A571014569100403 AILERON EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL LT WING DAMAGED A SIMAO OTHER O OTHER ININSP/MAINT 1 SW21925AE 14500908 LT AILERON AND WING WERE DAMAGED BY A CATERING TRUCK. MAINTENANCE REPLACED LT WING SPAR SEGMENT AND WING SKIN. REPLACED LT AILERON IAW EO. AC WAS RETURNED TO SERVICE. (K) 2L72 4T4 FRTT00011ATTE6CH 20050810002842005081000284SO 2005 8 10 SIM2005F00011 120050720A571114567124013 SPAR EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL LT WING DAMAGED A SIMAO OTHER O OTHER ININSP/MAINT 1 SW21925AE 14500908 LT AILERON AND WING WERE DAMAGED BY A CATERING TRUCK. MAINTENANCE REPLACED LT WING SPAR SEGMENT AND WING SKIN. REPLACED LT AILERON IAW EO. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4T4 FRTT00011ATTE6CH 20050810002872005081000287SO 2005 8 10 SIMA200520606 120050723A21508152403 ACM EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL NR 1 SEIZED A SIMAAB UNSCHED LANDING EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21612AE 145079 AFTER A NORMAL TAKEOFF AND CLIMB AT 9000 FT, CREW REPORTED SMOKE IN THE COCKPIT AND CABIN. SHORTLY BEFORE LANDING, CREW RECEIVED A PACK 1 OVERLOAD AND PACK 1 OVERHEAT EICAS MESSAGE. MAINTENANCE REPLACED NR 1 AIR CYCLE MACHINE OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (K) 2L72 4F4 FRTT00011ATTE6CH 20050810002882005081000288EA 2005 8 10 A6WA200540263 120050725A5340 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LBL 9 OB CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31405AW 7362 FS 280, LBL 9, CLIP ANGLE IS CRACKED, 1 INCH LONG. REMOVED AND REPLACED CLIP ANGLE FS 280, LBL 9, OB, IAW SRM. (K) 2L72 4F4 FRTA21EA E15NE 20050810002902005081000290EA 2005 8 10 A6WA200540273 120050725A5340601R3111358 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RBL9,OB CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31405AW 7362 FS 280, RBL 9, OB, CLIP ANGLE IS CRACKED 1 INCH LONG. REMOVED AND REPLACED ANGLE IAW EO AND SRM. (K) 2L72 4F4 FRTA21EA E15NE 20050810002922005081000292EA 2005 8 10 A6WA200540267 120050724A5210601R317725 DRAG ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PASSENGER DOOR CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31420AW 7640 PASSENGER DOOR STAIR AFT DRAG ANGLE IS CRACKED, .5 INCH LONG IN RADIUS (ADJACENT TO MOUNT FOR PASSENGER DOR ASSIST CABLE PULLEY). REMOVED DAMAGED SECTION OF ANGLE, FABRICATED REPAIR ANGLE AND INSTALLED ANGLE IAW REO. (K) 2L72 4F4 FRTA21EA E15NE 20050810002942005081000294EA 2005 8 10 A6WA200540262 120050725A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LBL 9, IB CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31405AW 7362 FS 280, LBL 9, IB CLIP ANGLE IS CRACKED, 1 INCH LONG. REMOVED AND REPLACED FS 280, LBL 9, IB CLIP IAW SRM. (K) 2L72 4F4 FRTA21EA E15NE 20050810002962005081000296WP 2005 8 10 AALA20050506 120050807A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21560AA 53090 BOS - EMERGENCY LIGHT AT FORWARD LEFT NUMBER 1 DOOR AND AISLE WAY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT FORWARD LEFT NUMBER 1 DOOR AND AISLE WAY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050810003012005081000301NM 2005 8 10 DHL2005746524 120050711A5730 SKIN BOEING727 727224 1384076NM RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01746DH 22252 C-CHECK CRACK ON R/W TRAILING EDGE UPPER SURFACE AT NR 12 SPOILER NR 2 HINGE CUTOUT. STOP DRILLED CRACK AT NR 12 SPOILER CUTOUT IAW B727 SRM 57-30-04 FIG 10, C/W HFEC IAW NDT M PT6, 51-00-00 FIG 23, CRACK IS CONTAINED. FABBED REPAIR PLATE FROM .071 7075T6 PO 9001737, DIM. 6 1/2"X 3 3/4" IAW B727 SRM 57-30-04 FIG 10, TREATED & PRIMED IAW B727 SRM 51-10-2, INSTALLED REPAIR IAW B727 SRM 57-30-04 FIG 10 AND 51-30-2. 2L73 4F A3WE 20050810003022005081000302NM 2005 8 10 DHL2005746525 120050711A5512 SKIN BOEING727 727224 1384076NM BULGED A DHLAO OTHER O OTHER ININSP/MAINT 1 SO01746DH 22252 LT HORIZONTAL UPPER SURFACE REAR CHORD SKIN BULGING OFF FASTENERS STAB 188, MARKED. CUT HORIZONTAL STAB UPPER SKIN FOR ACCESS AT STAB 188 DIM 17 1/2" X 3" IAW B727 SRM 55-10-3 FIG 3. CUT OUT FWD FLANGE OF UPPER T/E SPAR CHORD IAW B727 SRM 55-10-5 FIG 1. REMOVED 2EA -T- ANGLES AND FABBED NEW -T- ANGLES P/N BAC1505-29111 DIM 7 1/2" PO 9002342 CHORD FILLER DIM 1.25 7075 T6 12"X2" PO 9912445 AND REPAIR ANGLES 7075 T6 .071 DIM 20"X1" X1" PO900489 AND SKIN DOUBLER FROM 2024 T3 .080 25" X 51/2" PO 9002255 IAW B727 SRM 55-10-5 FIG 1 AND 55-10-3 FIG 3. TREATED AND PRIMED REPAIR PARTS AND AREA IAW B727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B727 SRM 55-10-5 FIG 1, 55-10-3 FIG 3. 2L73 4F A3WE 20050810003032005081000303NM 2005 8 10 DHL2005746512 120050705A5320 ANGLE BOEING727 727224 1384076NM AIRSTAIR CRACKED A DHLAO OTHER O OTHER ININSP/MAINT 1 SO01746DH 22252 AFT AIRSTAIRS RT TORQUE BOX ACTUATOR ANGLE SUPPORT FITTING STRUCTURE IS CRACKED ALONG RADIUS. REMOVED I/B WEB DOUBLER AND ANGLE AT AFT AIRSTAIR TORQUE BOX AREA IAW B727 S/B 727-53-0129. DRILLED, INSTALLED, TREATED AND PRIMED ANGLE IAW B727 S/B 727-53-0129. REINSTALLED I/B WEB DOUBLER IAW B727-53-0129 REV 5 FIG 4. 2L73 4F A3WE 20050810003042005081000304NM 2005 8 10 DHL2005746522 120050705A5530 STRUCTURE BOEING727 727224 1384076NM VERTICAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01746DH 22252 VERTICAL STAB FIN STA 180 LT STR 9 IS CRACKED AT ATTACH BOLT TO FRAME. CUT OUT CRACKED SECTION OF STR 9 DI 4 1/2". FABBED FILLER P/N BAC1517-1367 PO 501963 4 1/2" 2EA ANGLE DOUBLERS P/N AND 10134-1201 PO 601952 18" IAW B727 SRM 55-30-4 FIG 1. TREATED AND PRIMED REPAIR PARTS IAW B727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B727 SRM 55-30-4 FIG 1. 2L73 4F A3WE 20050810003052005081000305NM 2005 8 10 DHL2005746521 120050705A5530 STRUCTURE BOEING727 727224 1384076NM VERTICAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01746DH 22252 C-CHECK VERTICAL FIN STA 133 LT STR 9 IS CRACKED AT ATTACH BOLT TO FRAME. REMOVE FASTENERS IAW B727 SRM 51-30-2, CUT OUT DAMAGE AREA DIM 9 1/2"X 3" AND FABBED FILLER FROM BAC15171367 PO 501963 DIM 9 1/2"X 3" AND ANGLE FROM 10134-1201 PO 501962 DIM 23"X 1 1/4"X 3/4" (2EA) & PLATE FROM 7075T6 .080 PO 9002012 DIM 23"X1" (2EA) IAW B727 SRM 55-30-4 FIG 1. TREATED AND PRIMED IAW B727 SRM 51-10-2 AND INSTALLED REPAIR PARTS ON VERTICAL STAB STA 133 STR 9 IAW B727 SRM 55-30-4 FIG 4. 2L73 4F A3WE 20050810003122005081000312NM 2005 8 10 DHL2005788011 120050809A3260 CAP BOEING727 727214 138407RNM MLG INDICATOR LOOSE A DHLAO OTHER P NO WARNING INDICATION DEDESCENT 1 SO01788AT 21958 LEFT GEAR GREEN LIGHT DID NOT COME ON DURING EXTENTION. APPLIED APPROPRIATE ABNORMAL PROCEDURE AND LANDED SAFELY. FOUND L/MLG GREEN LIGHT CAP ASSEMBLY NOT FULLY ENGAGED IN LIGHT ASSY. PROPERLY INSTALLED PER MM 33-10-51 & L/MLG GREEN LIGHT OPS CKS NORMAL. 2L73 4F A3WE 20050810003132005081000313NM 2005 8 10 DHL2005788012 120050810A3260 WIRE BOEING727 727214 138407RNM MLG INDICATOR LOOSE A DHLAO OTHER P NO WARNING INDICATION DEDESCENT 1 SO01788AT 21958 LEFT GEAR LIGHT DID NOT COME ON DURING EXTENSION. APPLIED APPROPRIATE ABNORMAL PROCEDURES AND LANDED SAFELY. TIGHTEND LOOSE WIRE ON BACK OF KOREY LIGHT ASSY. SYSTEM CHECKED NORMAL ON SEVERAL DUMMY GEAR RETRACTIONS IAW B727 M/M 32-61-01. 2L73 4F A3WE 20050810003142005081000314NM 2005 8 10 DHL2005746513 120050701A5320 SPLICE BOEING727 727224 1384076NM STRINGER INCORRECT A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01746DH 22252 INCORRECT STRINGER SPLICE INSTALLED AT PREVIOUS REPAIR STR 28R STA 480. REMOVED INCORRECT STR SPLICE AT STR 28R STA 480 IAW B727 SRM 51-30-2. FABBED NEW STR SPLICE MAT USED BAC 1498-145 PO 422371 DIM 13" IAW B727 SRM 53-10-3 FIG 1 AND 53-10-20 FIG 9. TREATED AND PRIMED PART AND AREA IAW B727 SRM 51-10-2. INSTALLED NEW STR SPLICE AT STA 480 STR 28R IAW B727 SRM 53-10-3 FIG 1. 2L73 4F A3WE 20050810003152005081000315NM 2005 8 10 DHL2005746515 120050701A5313 STRINGER BOEING727 727224 1384076NM CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01746DH 22252 STRINGER 27R CORRODED AT BS 700. CUT OUT DAMAGED SECTION OF STR 27R BS 700 3.5", REPLACED WITH FILLER MAT ID BAC1498-131 PO9001873 3.5" AND STR DOUBLER BAC1498-144 PO 335792 10.5" IAW B727 SRM 53-10-3 FIG 1. TREATED & PRIMED REPAIR PARTS IAW B727 SRM 51-10-2, INSTALLED REPAIR PARTS IAW B727 SRM 53-10-3 FIG 1. 2L73 4F A3WE 20050810003172005081000317NM 2005 8 10 DHL2005746511 120050701A573059948502 SKIN BOEING727 727224 1384076NM RT WING GOUGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01746DH 22252 RT WING LOWER WS 770 FWD HAS EDGE OF SKIN GOUGED. CUT OUT DAMAGED SECTION OF SKIN AT WS 770 LWR SKIN DIM 3/4"X 2.5" IAW B727 SRM 57-30-4 FIG 1. FABBED REPAIR DOUBLER FROM .080 2024 T3 PO 9002255 DIM 3 1/8" X 6 3/4" IAW B727 SRM 57-30-4 FIG 1. TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED REPAIR IAW B727 SRM 57-30-4 FIG 1 & 51-30-2. 2L73 4F A3WE 20050810003192005081000319WP 2005 8 10 ASAA0580302 120050613A5321993654763 FLOOR PANEL DOUG DC9 DC983 3022083WP FS 160-180 DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - DURING HV-CHECK, FOUND CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050810003202005081000320WP 2005 8 10 ASAA0580315 120050613A53209936534101 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FS 185-194 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL SUPPORT CORRODED. REPLACED FLOOR PANEL SUPPORT. (M) 2L72 4F RTA6WE 20050810003212005081000321WP 2005 8 10 ASAA0580293 120050523A532059360717 INTERCOSTAL DOUG DC9 DC983 3022083WP FS 1212-1231 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - DURING CHECK, INTERCOSTAL CORRODED ON LOWER HORIZONTAL AND VERTICAL FLANGES. REPLACED INTERCOSTAL. (M) 2L72 4F RTA6WE 20050810003232005081000323WP 2005 8 10 ASAA0580256 120050515A5310 STRUCTURE DOUG DC9 DC983 3022083WP CARGO BAY CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - DURING C-CHECK, AFT CARGO COMPARTMENT LONGERON IS CORRODED ON BETWEEN 27R AND 27L. REMOVED AND REPLACED DAMAGED FRAME SEGMENT AND REPAIR ANGLES. (M) 2L72 4F RTA6WE 20050810003242005081000324WP 2005 8 10 ASAA0580259 120050515A575399359406 SKIN DOUG DC9 DC983 3022083WP FLAP GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - DURING C-CHECK, RIGHT WING INBOARD FLAP GOUGED OUTBOARD OF BUTT JOINT BOTTOM SURFACE. REMOVED DAMAGE, AND INSTALLED DOUBLER IN FLAP SKIN. (M) 2L72 4F RTA6WE 20050810003252005081000325WP 2005 8 10 ASAA0580303 120050613A532199365445 FLOOR PANEL DOUG DC9 DC983 3022083WP FS 185-200 DELAMINATED A ASAAO OTHER O OTHER NRNOT REPORTED 1 NM02981AS 53472 OKC - FOUND HV CHECK, CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050810003262005081000326WP 2005 8 10 ASAA0580305 120050613A5321993655211 FLOOR PANEL DOUG DC9 DC983 3022083WP FS 200-256 DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - FOUND HV CHECK, CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050810003272005081000327WP 2005 8 10 ASAA0580301 120050612A5321993654721 FLOOR PANEL DOUG DC9 DC983 3022083WP FS 180-200 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - DURING HV-CHECK, CABIN FLOOR PANEL CORRODED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050810003292005081000329WP 2005 8 10 ASAA0580310 120050613A5321993653739 FLOOR PANEL DOUG DC9 DC983 3022083WP FS 148-160 DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL TORN AND DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050810003322005081000332WP 2005 8 10 ASAA0580349 120050621A5322993607410 SHEAR TIE DOUG DC9 DC983 3022083WP FS 1150 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - DURING HV-CHECK, FOUND SHEAR TIE CORRODED. REPLACED SHEAR TIE. (M) 2L72 4F RTA6WE 20050810003342005081000334WP 2005 8 10 ASAA0580257 120050515A5330593666751 BEAR STRAP DOUG DC9 DC983 3022083WP FS 1210 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - DURING C-CHECK, AFT CARGO COMPARTMENT DOOR CUTOUT BEAR STRAP IS CORRODED AT STATION 1210. REMOVED DAMAGE AND INSTALLED REPAIR INTERNAL FILLER, EXTERNAL DOUBLERS. AFT CARGO DOOR P/N 5936667-51, BEAR STRAP P/N 59364335. (M) 2L72 4F RTA6WE 20050810003362005081000336WP 2005 8 10 ASAA0580348 120050621A5322993607329 SHEAR TIE DOUG DC9 DC983 3022083WP FS 1193 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - DURING HV-CHECK, FOUND SHEAR TIE CORRODED. REPLACED SHEAR TIE. (M) 2L72 4F RTA6WE 20050810003392005081000339WP 2005 8 10 ASAA0580351 120050621A5320991015127 CUSP WEB DOUG DC9 DC983 3022083WP FS 927-946 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - DURING HV-CHECK, LEFT CUSP WEB IS CORRODED ON UPPER SURFACE. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050810003402005081000340WP 2005 8 10 ASAA0580354 120050621A5523591041449 STRUCTURE DOUG DC9 DC983 3022083WP ELEVATOR TAB DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - DURING HV-CHECK, FOUND RIGHT ELEVATOR GEARED TAB LOWER INBOARD SURFACE IS DENTED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050810003422005081000342WP 2005 8 10 ASAA0580304 120050613A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP CABIN CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - DURING HV-CHECK, CABIN FLOOR PANEL INSERTS CORRODED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050810003432005081000343WP 2005 8 10 ASAA0580306 120050613A5321993653711 FLOOR PANEL DOUG DC9 DC983 3022083WP FS 148 -160 DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050810003442005081000344WP 2005 8 10 ASAA0580350 120050621A5320 INTERCOSTAL DOUG DC9 DC983 3022083WP CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - DURING HV-CHECK, FOUND INTERCOSTAL CORRODED. REPLACED INTERCOSTAL. (M) 2L72 4F RTA6WE 20050810003452005081000345WP 2005 8 10 ASAA0580295 120050523A531159624501 FRAME DOUG DC9 DC983 3022083WP FS 1079 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - DURING C-CHECK, FOUND FRAME CORRODED AROUND FASTENERS. REMOVED DAMAGED SECTIONS. INSTALLED REPAIR DOUBLER AND FILLER. (M) 2L72 4F RTA6WE 20050810003462005081000346WP 2005 8 10 ASAA0580254 120050515A531199360734 FRAME DOUG DC9 DC983 3022083WP FS 1155 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - DURING C-CHECK, FOUND FRAME AT STATION 1155 CORRODED. REMOVED AND REPLACED DAMAGED FRAME. (M) 2L72 4F RTA6WE 20050810003482005081000348WP 2005 8 10 ASAA0580352 120050621A5330595305077 SKIN DOUG DC9 DC983 3022083WP FS 313-351 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - DURING HV-CHECK, FOUND FUSELAGE SKIN DENTED AND CREASED. REMOVED DAMAGED SECTION. INSTALLED SKIN REPAIR SECTION, FINGER DOUBLER, LONGERON STRAPS, INTERNAL REPAIR DOUBLERS, LONGERON STRAPS, INTERNAL REPAIR DOUBLERS AND FILLERS. (M) 2L72 4F RTA6WE 20050810003492005081000349WP 2005 8 10 ASAA0580307 120050613A5321993653911 FLOOR PANEL DOUG DC9 DC983 3022083WP FS 148-160 DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050810003512005081000351WP 2005 8 10 ASAA0580323 120050613A5320993653471 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FS 162-196 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - DURING HV-CHECK, FOUND CABIN FLOOR PANEL SUPPORT CORRODED AROUND INSERT. REPLACED FLOOR PANEL SUPPORT. (M) 2L72 4F RTA6WE 20050810003522005081000352WP 2005 8 10 ASAA0580322 120050613A5320993653425 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FS 200 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - DURING HV-CHECK, FOUND CABIN FLOOR SUPPORT CORRODED AROUND INSERT. REPLACED FLOOR PANEL SUPPORT. (M) 2L72 4F RTA6WE 20050810003532005081000353WP 2005 8 10 ASAA0580321 120050613A5320993653443 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FS 180 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL SUPPORT CORRODED. REPLACED FLOOR PANEL SUPPORT. (M) 2L72 4F RTA6WE 20050810003542005081000354WP 2005 8 10 ASAA0580309 120050613A5321993654721 FLOOR PANEL DOUG DC9 DC983 3022083WP FS 180-200 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL DELAMINATED AND CORRODED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050810003592005081000359WP 2005 8 10 ASAA0580317 120050613A5320993653411 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FS 157 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - DURING HV-CHECK, FOUND CABIN FLOOR PANEL SUPPORT CORRODED. REPLACED FLOOR PANEL SUPPORT. (M) 2L72 4F RTA6WE 20050810003602005081000360WP 2005 8 10 ASAA0580296 120050523A531159624501 FRAME DOUG DC9 DC983 3022083WP FS 1060 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - FOUND DURING C-CHECK, FRAME CORRODED AROUND FASTENERS. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER AND FILLER. (M) 2L72 4F RTA6WE 20050810003612005081000361WP 2005 8 10 ASAA0580255 120050515A531359360501 LONGERON DOUG DC9 DC983 3022083WP FS 1237-1297 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - DURING C-CHECK, FOUND LONGERON 30 IS CORRODED ON FLANGES AT STATION 1237-1241. REMOVED AND REPLACED DAMAGED LONGERON. (M) 2L72 4F RTA6WE 20050810003632005081000363WP 2005 8 10 ASAA0580319 120050613A5320993653415 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FS 196 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - DURING HV-CHECK, CABIN FLOOR PANEL SUPPORT CORRODED. REPLACED FLOOR PANEL SUPPORT. (M) 2L72 4F RTA6WE 20050810003642005081000364NM 2005 8 10 DHL2005746514 120050703A5510 WEB BOEING727 727224 1384076NM TORQUE BOX CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01746DH 22252 POSSIBLE CRACK IN UPPER TORQUE BOX WEB BS 1303 AT LWR RT CORNER ACCESS BY PNL 9504 MARKED RED. STOP DRILLED CRACK IAW B727 SRM 51-10-1. HFEC VERIFIED STOP DRILL IAW B727 NDT MANUAL PH 4 51-00-00 FIG 23. COMPLIED WITH COTNEY AEROSPACE EAZ04.3 07-26-05. 2L73 4F A3WE 20050810003672005081000367NM 2005 8 10 DHL2005746519 120050703A5330 SKIN BOEING727 727224 1384076NM BS 1090 DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01746DH 22252 C-CHECK DENT LT SIDE FUSELAGE SKIN STA 1090 BETWEEN STR. 26L & 27L. CUT OUT DAMAGE ON FUSELAGE SKIN AT STA 1090 BETWEEN STR 26L & 27L 1"X 1.5" IAW B727 SRM 53-30-3 FIG 1. FABRICATED REPAIR DOUBLER 7.5"X 9" 2024T3 .063 PO 9002199 IAW B727 SRM 53-30-3 FIG 1. TREATED & PRIMED DOUBLER AND ALL AFFECTED AREAS IAW B727 SRM 51-10-2. INSTALLED REPAIR DOUBLER IAW B727 SRM 53-30-3 FIG 1. THIS REPAIR IS CAT-A. 2L73 4F A3WE 20050810003692005081000369WP 2005 8 10 05FDEA02357 120050809A5230 SKIN DOUG MD10 MD1010F 3022112WP ZONE 100 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25564FE 46984 AFTER CARGO DOOR STA 1791 EXTERNAL SKIN EXISTING 1EA REPAIR DOUBLER ON LWR FWD CORNER. REPAIR PER SRM 52-10-00 FIG 17 VOL 1. 2L73 4F RTA22WE 20050810003712005081000371WP 2005 8 10 05FDEA02359 120050809A5312 BULKHEAD DOUG MD10 MD1010F 3022112WP FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25564FE 46984 UPPER FUSELAGE STA 265 UPPER FWD PRESSURE BULKHEAD EXISTING 1EA REPAIR DOUBLER ON EXTERNAL SKIN. REPAIR PER SRM 53-00-01 VOL 1 FIG 4 SHEET 2. 2L73 4F RTA22WE 20050810003722005081000372EU 2005 8 10 05FDEA02328 120050808A5321 FLOOR PANEL AIRBUS300 A300B4605R 3930308EU MDC BROKEN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25670FE 777 MDC FLOOR PNL 241LK BROKEN. 2L72 4F RTA35EU 20050810003732005081000373EU 2005 8 10 05FDEA02329 120050808A5321 FLOOR PANEL AIRBUS300 A300B4605R 3930308EU MDC CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25670FE 777 MDC FLOOR PNL 252UF CRACKED. 2L72 4F RTA35EU 20050810003752005081000375WP 2005 8 10 05FDEA02361 120050809A5753 SKIN DOUG MD10 MD1010F 3022112WP ZONE 600 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25564FE 46984 RIGHT WING T/E OUTBOARD FLAP I/B HINGE XORS 562 EXISTING EXTERNAL REPAIR DOUBLER ON LWR SKIN. REPAIR PER SRM 57-00-01 FIG 4 SHEET 2 VOL 1. 2L73 4F RTA22WE 20050810003762005081000376WP 2005 8 10 05FDEA02362 120050809A5312 PRESSURE PANEL DOUG MD10 MD1010F 3022112WP ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25564FE 46984 ON STA 1510 CTR W/W ON WEB X=31.5 Z=-36 FOUND CRACK 1,75". REPAIR PER SRM 53-00-01 FIG 10 SHEET 5, 6, 7 VOL 1. 2L73 4F RTA22WE 20050810003772005081000377WP 2005 8 10 05FDEA02363 120050809A5754 SKIN DOUG MD10 MD1010F 3022112WP ZONE 500 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25564FE 46984 LEFT WING SLAT 1 XORS 130 EXISTING FLUSH REPAIR DOUBLER ON LWR SKIN. ACCOMPLISH EA 8-5710-84123. 2L73 4F RTA22WE 20050811000012005081100001NM 2005 8 11 UPS05445132 120050722A531165B0172345 FRAME BOEING747 747121 1384871NM M/D CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE:C M/D BS 600 LT STR 25L - 24L FRAME FOUND CRACKED (CRACK LENGTH .75" & 1"). M/D BS 600 LT STR 23 TO STR 26 AREA FRAME REPAIRED AS PER HX RS R53-22-35339 & UPS EO B747-5310-22627-A. 2L74 4F A20WE 20050811000052005081100005NM 2005 8 11 UPS05445144 120050724A575365B020984 STRUCTURE BOEING747 747121 1384871NM TE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE:C RIGHT WING I/B MID FLAP T/E WEB UPPER CHORD CORRODED REVEALED AT 104"- 108" AS MARKED (COUNT FROM I/B). CORROSION BLEND OUT 0.054" X 3/4" X 3" EXCEED SRM 57-50-01 FIG 3 LIMITS, CHORD REPAIRED AS PER HX RS R57-55-35354 & UPS ENGINEERING FILE 747-57-20081. 2L74 4F A20WE 20050811000062005081100006WP 2005 8 11 05FDEA02350 120050809A5730 SKIN DOUG MD10 MD1010F 3022112WP ZONE 500 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25564FE 46984 LEFT WING DROOP L/E FLUSH REPAIR SKIN ON EXTERNAL SKIN. REPLACED OLD REPAIR PER SRM 57-00-01 FIG 4 VOL 1 SHEET 2. 2L73 4F RTA22WE 20050811000072005081100007WP 2005 8 11 05FDEA02352 120050809A5754 SKIN DOUG MD10 MD1010F 3022112WP ZONE 600 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25564FE 46984 RIGHT WING SLAT 6 CENTRAL TRACK EXISTING EXTERNAL REPAIR DOUBLER ON LWR SKIN. REPAIR PER SRM 57-10-00 FIG 31 VOL 1. 2L73 4F RTA22WE 20050809001422005080900142WP 2005 8 9 ASAA0580347 120050618A5311991224672 FRAME DOUG DC9 DC983 3022083WP CHAFED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM02949AS 53022 OKC - DURING HV CHECK, FRAME WEB CHAFED. REPAIRED WEB SECTION PER SRM 51-70-4. (M) 2L72 4F RTA6WE 20050809001442005080900144NM 2005 8 9 AWXA200500911 120050805A3350276005 FUSE BOEING757 7572S7 1384962NM INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW 23323 PHX - EEL - DURING A3 CHECK DISCOVERED FORWARD ESCAPE PATH LIGHTING, LEFT AND RIGHT EXITS FOR EMERGENCY LIGHTS, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED FUSE AT THE FORWARD EMERGENCY LIGHT POWER SUPPLY M730. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA2NM 20050809001462005080900146NM 2005 8 9 AWXA200500913 120050807A3397BR963180 WIRE HARNESS BOEING737 7373Y0 1384671NM DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 DEN - EEL - DURING 4 DAY CHECK DISCOVERED ROW 22L, SEAT MOUNTED, EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHTING SEAT HARNESS AT ROW 22L. OPERATIONAL CHECKS GOOD. 2L72 4F RTA16WE 20050809001482005080900148NM 2005 8 9 AWXA200500915 120050713A53306545775594 SKIN BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 DURING C18 CHECK DISCOVERED FUSELAGE SKIN CRACK, 1.43 INCHES IN LENGTH, AT BS 727E+4 INCHES, STRINGER 24R. MAINTENANCE CUT OUT DAMAGED AREA OF SKIN AT BS 727E+4 INCHES, STRINGER 24R IAW BOEING 737-300 SRM 53-00-01-3 FIG 229. FABRICATED DOUBLER, TRIPLER AND FILLER IAW BOEING 737-300 SRM 53-00-01-3 FIG 229. INSTALLED AND SEALED FABRICATED REPAIR PARTS AT BS 727E+4 INCHES, STRINGER 24R IAW BOEING 737-300 SRM 53-00-01-3 FIG 229. 2L72 4F RTA16WE 20050809001502005080900150EU 2005 8 9 MALA050630 120050728A5347 SEAT TRACK SAAB SF340 340B 7860101EU CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15452XJ 340B452 DURING 4K INSPECTION IN BNA, SEAT TRACK AT BLO FROM FS 294-FS 310 IS CORRODED AND HAS BEEN REPAIRED IAW MESABA EO NR 53309. REF: EAMS WORK ORDER #212637 TASK 1509. 2L72 4T RTA52EU 20050809001522005080900152NM 2005 8 9 AWXA200500917 120050711A5753654643099 WEDGE BOEING737 7373S3 1384711NM ZONE 500 - LEFT DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 DURING C18 CHECK DISCOVERED LT INBOARD FORE FLAP LOWER SURFACE DELAMINATED, AT THE INBOARD TRACK ATTACHMENT. MAINTENANCE REMOVED DAMAGED AREA ON THE LT INBOARD FORE FLAP LOWER SURFACE AND CLEANED AREA IAW BOEING 737-300 SRM 51-70-10. FABRICATED FILLER AND DOUBLER IAW BOEING 737-300 SRM 51-70-10-0 FIG 30. INSTALLED, BONDED AND SEALED FABRICATED REPAIR PARTS TO THE LT INBOARD FORE FLAP LOWER SURFACE IAW BOEING 737-300 SRM 51-70-10-0 FIG 30. 2L72 4F RTA16WE 20050809001552005080900155WP 2005 8 9 ASAA0580253 120050509A3350 WIRE DOUG DC9 DC983 3022083WP LIGHT LOOSE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM02958AS 53024 ANC LINE CHECK, FOUND AFT EXIT CATWALK SIDE PANEL EMERGENCY LIGHT INOPERATIVE. RESECURED LOOSE WIRE CONNECTOR. LIGHT THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20050809001572005080900157EA 2005 8 9 VNAA0507018 120050724A5240 DOOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN OPEN A VNAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL05218PS 7885 DURING CLIMB PASSING 10,500 FT THE FLIGHT ATTENDANT NOTICED AN INCREASE IN NOISE LEVEL AROUND THE SERVICE DOOR. THE F/A REPORTED THAT THE GREEN INDEX MARKS ON THE INDICATOR WINDOW WERE NOT ALIGNED. COCKPIT INDICATIONS WERE NORMAL. THE FLIGHT RETURNED TO PHL WHERE MAINTENANCE OPERATIONALLY CHECKED THE SERVICE DOOR IAW CRJ200 AMM 52-41-00-710-801. OPS CHECKS WERE GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050810000042005081000004NM 2005 8 10 DHL2005746508 120050630A5347 SEAT TRACK BOEING727 727224 1384076NM DAMAGED A DHLAO OTHER O OTHER ININSP/MAINT 1 SO01746DH 22252 MAIN CABIN SEAT TRACK DAMAGED AT BS 1110 TO 1130 LBL 45.5. CUT OUT DAMAGED SEAT TRACK FROM STA 1020 TO 1135 LBL 45.5 IAW B727 SRM 53-10-5 FIG 1, FABBED NEW SEAT TRACK DIM (117 1/2") MAT USED BSC 520-792 PO 900-203 SPLICE 7075 T6 0.25 PO 900-1189 DIM (9") 2 ANGLER SPLICE AND 10134-1407 PO 449666 DIM (15"X3") IAW B727 SRM 53-10-1 FIG 1, TREATED AND PRIMED IAW B727 SRM 51-10-2, INSTALLED NEW SEAT TRACK IAW B727 SRM 53-10-1 FIG 1. 2L73 4F A3WE 20050810000062005081000006CE 2005 8 10 DJFA2005126 120050806A2810 SUMP BEECH MU300 400A 1155402CE FUEL DRAIN OPEN E DJFAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 EA23792TA RK264 KSGR - KHOU DURING CLIMB THE CREW NOTICED FUEL LEAKING FROM THE RIGHT WING TIP. THE FUEL WAS COMING FROM TWO AREAS. THE FIRST BEING THE WING TIP AREA WHICH PRODUCED A FIVE FOOT VAPOR TRAIL. THE SECOND AREA WAS FROM THE SPOILER, ABOUT ONE FOOT IN FROM THE OUTBOARD TIP. THE AIRCRAFT WAS DIVERTED TO KHOU WHERE AN UNEVENTFUL LANDING WAS MADE. FOLLOWING THE LANDING THE CREW NOTED FUEL POOLING UNDER THE SPOILER. MAINTENANCE FOUND THE DRAIN SUMP ON THE SURGE TANK TO BE OPEN. THE DRAIN SUMP WAS CLOSED AND FUEL WAS CLEANED FROM THE ACCESS PANEL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4F RTA16SW 20050810000082005081000008NM 2005 8 10 05FDEA02305 120050807A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 CENTER CARGO CEILING UPPER DECK SEAT TRACK RBL 8.0 FOUND CORRODED AT STA 1561. REPAIR CARRIED OUT AS PER SRM 53-70-00. 2L73 4F RTA22WE 20050810000152005081000015NM 2005 8 10 05FDEA02312 120050808A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE RIGHT NR 13 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA1-5510-87597. 2L73 4F RTA22WE 20050810000252005081000025NM 2005 8 10 05FDEA02284 120050805A5322 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 AFT CARGO COMP SHEAR TIE HAS CORROSION BS 985 RBL 9. REPAIRED PER SRM 53-10-1, 53-10-3 FIG. 1. 2L73 4F RTA3WE 20050810000292005081000029NM 2005 8 10 05FDEA02288 120050805A5330 SKIN BOEING727 727200 138407ENM FUSELAGE UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 EVALUATE TO DETERMINE IF REPAIR IS MAJOR OR MINOR AND IF REPAIR IS IN ACCORDANCE WITH FAA APPROVED DATE, (EXTERNAL REPAIR BS 690, STR 28R 18 X 12 INCHES). REMOVED AND REPLACED EXTERNAL REPAIR BS690, STR. 28R, IAW SRM 53-30-3. FIG 3A. 2L73 4F RTA3WE 20050810000302005081000030NM 2005 8 10 05FDEA02289 120050805A5340 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 FUSELAGE, UPPER LOBE, STA 680 STR 3L, STRINGER CLIP DAMAGED. OUT OF LIMITS, REMOVED, FABRICATED AND INSTALLED CLIP PER SRM 51-40-1, 51-10-1, 53-10-1, 51-30-2 & FED EX MM 51-20-151-7. 2L73 4F RTA3WE 20050810000392005081000039NM 2005 8 10 05FDEA02298 120050807A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE LT NR 35 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. 2L73 4F RTA22WE 20050810000422005081000042NM 2005 8 10 05FDEA02313 120050808A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE RIGHT NR 11 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA1-5510-87597. 2L73 4F RTA22WE 20050810000482005081000048NM 2005 8 10 05FDEA02319 120050808A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE RT NR 07 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA1-5510-87597. 2L73 4F RTA22WE 20050810000532005081000053NM 2005 8 10 05FDEA02300 120050807A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STABILIZER BARREL NUT HOLE LEFT NR 34 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. 2L73 4F RTA22WE 20050810000592005081000059NM 2005 8 10 SWAA052327 120050803A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29375SW 26583 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050810000602005081000060NM 2005 8 10 SWAA052328 120050804A335007912 COVER BOEING737 7377H4 1384404NM MID CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29428WN 29844 EEPLS STRIP COVER LOOSE AT ROW 12 ABC. INSTALLED COVER PER MM. 2L72 4F RTA16WE 20050810000612005081000061NM 2005 8 10 SWAA052329 120050804A335007912 COVER BOEING737 7377H4 1384404NM MID CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29449WN 32469 EEPLS STRIP COVER LOOSE AT ROW 12 ABC. SECURED COVER PER MM. 2L72 4F RTA16WE 20050810000662005081000066NM 2005 8 10 SWAA052334 120050803A53306545765 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29680AA 23505 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500B, STR 19L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050810000712005081000071NM 2005 8 10 SWAA052339 120050806A53156546806 FLOORBEAM BOEING737 7373Q8 1384670NM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29317WN 24068 DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED BETWEEN BS 727D TO BS 867, LBL 8. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20050810001012005081000101WP 2005 8 10 IXXA05SMN108S 120050627A5720 WING DOUG DC8 DC871F 302199DWP XFS 212.000 CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING C CHECK INSPECT, LT WING NR 2 STUB WING UPPER PART CORRODED, XFS 212.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-2-1 FIG 38. TR NR 57-85, EO SEMAN NR 2005848 DATE 06-18-05. REMOVED FASTENERS IAW DC-8 SRM 51-1-21 PG 1, DC-8 SRM 51-1-20D PG 21. REMOVED CORROSION IAW DC-8 SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW DC-8 SRM 57-2-1 PG 11-12. REMOVED CORRODED AREA IAW DC-8 SRM 57-2-1 FIG 38. PERFORMED VISUAL INSPECT NO CRACK FOUND, NO CORROSION FOUND. FAB`D REPAIR DOUBLER (ALCLAD 7075 T6 0.071”), FILLER (ALCLAD 7075 T6 0.063) IAW DC-8 SRM 57-2-1 FIG 38, DC-8 SRM 57-3-1 FIG 3. CLEANED, TREATED AND PRIMED AREA, REPAIR PARTS INTERNAL PART IAW DC-8 SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW 2L74 4F RT4A25 20050810001062005081000106CE 2005 8 10 08042005C 120050804A3297 WIRE BEECH 1900 1900D 1154162CE MLG DOWNLOCK BROKEN A NSVAO OTHER O OTHER APAPPROACH 1 EA27124CJ UE24 NO DOWNLOCK INDICATION WHEN GEAR DOWN. REPAIRED BROKEN WIRE. 2L72 4T RTA24CE 20050810001082005081000108CE 2005 8 10 08082005A 120050805A2730130610000613 ELEVATOR BEECH 1900 1900D 1154162CE DAMAGED A NSVAO OTHER F FLT CONT AFFECTED ININSP/MAINT 1 EA27124CJ UE24 LT ELEVATOR, THREE RIVETS NEED REPLACED ON OUTBOARD ELEVATOR ATTACH POINT. 2L72 4T RTA24CE 20050810001092005081000109CE 2005 8 10 08082005B 120050805A2730130610000614 ELEVATOR BEECH 1900 1900D 1154162CE DAMAGED A NSVAO OTHER F FLT CONT AFFECTED ININSP/MAINT 1 EA27124CJ UE24 RT ELEVATOR, OUTBOARD HINGE POINT HAS THREE LOOSE RIVETS. 2L72 4T RTA24CE 20050810001182005081000118NM 2005 8 10 UPS05445066 120050724A5720 WEB BOEING747 747121 1384871NM RT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 RHW I/B MID FLAP T/E WEB UPR AREA SEVERAL AREA CORROSION REVEAL BETWEEN NR 3 AND NR 4 ARM, COUNT FROM O/B. CORROSION BLEND OUT 0.039" BY 0.5" BY 2" EXCEED SRM 57-50-01 FIG 3 LIMITS, WEB REPAIRED AS PER SRM 51-40-02 FIG 1. 2L74 4F A20WE 20050810001292005081000129CE 2005 8 10 08082005I 120050809A2730130610000614 ELEVATOR BEECH 1900 1900D 1154162CE LOOSE A NSVAO OTHER F FLT CONT AFFECTED ININSP/MAINT 1 EA27221CJ UE221 RT ELEVATOR, OUTBOARD HINGE HAS LOOSE RIVET ON BOTTOM SIDE OF ELEVATOR. 2L72 4T RTA24CE 20050810001442005081000144NM 2005 8 10 UPS05245074 120050718A5347 SEAT TRACK BOEING727 72722C 138400FNM BROKEN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01941UP 19196 SEAT TRACK HORIZ FLANGE UPPER, BROKEN AT BS870 RBL 24.75. REPAIRED IAW UPS EO 727-53-20184. 2L73 4F A3WE 20050810001452005081000145NM 2005 8 10 UPS05245075 120050713A5320 INTERCOSTAL BOEING727 72722C 138400FNM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01941UP 19196 ON REMOVAL OF FLOOR PANEL OUTSIDE FWD LAV, INTERCOSTAL FOUND CORRODED. LOCATION BETWEEN BS312-328 LBL 29. REPLACED INTERCOSTAL IAW SRM 53-10-02 AND 53-30-2. 2L73 4F A3WE 20050810001492005081000149NM 2005 8 10 UPS05445060 120050725A532065B1506931 ANGLE BOEING747 747121 1384871NM CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSIDE KEEL BEAM BOX AT BS 1329 LBL 9- RBL 9 ATT ANGLE FOUND CORROSION. CORROSION BLEND OUT 0.062" BY 1" BY 2" EXCEED SRM 53-10-01 FIG 1 LIMITS, ANGLE REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050810001512005081000151NM 2005 8 10 UPS05445064 120050722A5311 FRAME BOEING747 747121 1384871NM M/D CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 BS 940 BETWEEN S14-15R FRAME FOUND CRACK, CRACK LENGTH 7/16". BS 940 BETWEEN STR 14-15R FRAME REPAIRED AS PER SRM 53-10-04 FIG 4. 2L74 4F A20WE 20050810001682005081000168EA 2005 8 10 SWIA200515382 120050709A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA CRACKED A SWIAO OTHER O OTHER ININSP/MAINT 1 NM07426SW 7468 FS 484 CABIN FLOOR RT INTERCOSTAL OB ANGLE RBL36 CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED INTERCOSTAL IAW CRJ REO 601R-53-41-059 REV "A". 2L72 4F RTA21EA 20050810001702005081000170EA 2005 8 10 SWIA200515383 120050709A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07426SW 7468 FS 280 FLOOR SUPPORT ANGLE LBL 13 CRACKED, ITEM FOUND AT C-CHECK. REPAIRED ANGLE IAW CRJ REO 601R-53-11-138 REV "NC". 2L72 4F RTA21EA 20050810001792005081000179SO 2005 8 10 SWIA200515392 120050807A27513069001017 ANNUNCIATOR EMB 120 EMB120ER 3260203SO MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07578SW2913 2913 120346 DURING CRUISE FLT, RECEIVED A "FLAP" AND "ADVANCED SWS" ON THE MAP. REPLACED FLAP ANNUNCIATOR PANEL IAW 27-50-05. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050810001862005081000186NM 2005 8 10 2005UALA00740 120050801A3350321454 EPSU AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE R BATTERY FAULTY A UALAO OTHER L NO TEST ININSP/MAINT 1 WP29836UA 1460 EMERGENCY LIGHT TEST FAULTED. REPLACED EPSU. 2L72 4F4 FRTA28NM E40NE 20050810001872005081000187NM 2005 8 10 2005UALA00741 120050731A5100 PDU BOEING757 757222 1384956NM PWA 2037 PW2037 NE TE FLAPS VIBRATION A UALAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 WP29502UA 24623 RETURNED TO FIELD DUE TO AIRCRAFT VIBRATION. TE FLAP PDU DID NOT FUNCTION PROPERLY. REPLACED SUBJECT PDU. 2L72 4F4 FRTA2NM E17NE 20050810001952005081000195NM 2005 8 10 2005UALA00749 120050802A3350 LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE ROWS 15-21 INOPERATIVE A UALAO OTHER L NO TEST ININSP/MAINT 1 WP29351UA 24319 EEL FLOOR LIGHTING ROWS 15-21 INOPERATIVE. REPLACED CABLE AND SECURED TRACKS. REPLACED CABLE AND SECURED TRACKS. 2L72 4F4 FRTA16WE E2GL 20050810001962005081000196NM 2005 8 10 2005UALA00750 120050802A3350 LIGHT BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29784UA 26951 EEL LIGHTS AT 1E INOP. REPLACED EEL LIGHT. 2L72 4F4 FRTT0001SE E46NE 20050810002032005081000203NM 2005 8 10 2005UALA00756 120050803A3350 LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FLOOR AT AFT CABINOPERATIVE A UALAO OTHER L NO TEST ININSP/MAINT 1 WP29365UA 24534 EEL LIGHTS INOPERATIVE ON FLOOR AT AFT CABIN. CLEANED AND DRIED RACEWAY, PWR CABLE AND LIGHTS. 2L72 4F4 FRTA16WE E2GL 20050810002122005081000212NM 2005 8 10 2005UALA00766 120050730A3350 LIGHT BOEING777 777222 1385219NM PWA PW4077PW4077 NE INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29780UA 26944 M2 GALLEY FWD LT EMERGENCY LIGHT INOP. REPLACED EEL LIGHT ASSEMBLY. 2L72 4F4 FRTT0001SE E46NE 20050810002132005081000213NM 2005 8 10 2005UALA00767 120050731A3350 LIGHT BOEING777 777222 1385219NM PWA PW4077PW4077 NE INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29780UA 26944 A-4 GALLEY LT EMERGENCY LIGHTS INOP. REPLACED EEL LIGHT ASSEMBLY. 2L72 4F4 FRTT0001SE E46NE 20050810002142005081000214NM 2005 8 10 2005UALA00768 120050805A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29196UA 28715 EMERGENCY LT AT 39 ABC INOP. REPLACED LIGHT ASSY. 2L74 4F4 FRTA20WE E24NE 20050810002232005081000223WP 2005 8 10 IXXA05SMN120S 120050629A5340 FITTING DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE STA 70.000 CORRODED B IXXAO OTHER O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, ACND. CMPT. LT FITTING CORRODED STA 70.000, L-31R. REMOVED CORROSION IAW SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PAGE 2P. REMOVED CORRODED FITTING IAW SRM 51-1-20D PAGE 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PAGE 9. TORQUED IAW SRM 51-3-1. 2L74 4F4 FRT4A25 E2GL 20050810002312005081000231NM 2005 8 10 ASMF200508004 120050806A215020495055 COOLING TURBINE HONEYWELL DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE LEFT INOPERATIVE W ASMFK NONE J WARNING INDICATION ININSP/MAINT 1 SW23861LF370441590 116227 49826 DURING TRANSIT SERVICE, LT AIR CONDITIONING SYSTEM WAS DETECTED INOPERATIVE. REPORT WAS DEFERRED IAW MEL 21-1. DURING OVERNIGHT SERVICE, COOLING TURBINE WAS REPLACED IAW MM 21-51-01, TESTED CORRECT. DEFERRED REPORT WAS CLOSED. 2L72 4F4 FRT E9NE 20050810002362005081000236SO 2005 8 10 SWIA200515394 120050730A3350 SIGN EMB 120 EMB120ER 3260203SO BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07290SW 120317 EXIT ROW SIGN AT ROW 9 BROKEN. REPAIRED EXIT ROW SIGN AT ROW 9. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050810002492005081000249EU 2005 8 10 AALA20050492 120050803A3350BR964814 LIGHT AIRBUS300 A300B4605R 3930308EU CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW2118066 509 JFK - EMERGENCY LIGHT AT SEATS 31G AND 34G BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHTS AT SEATS 31G AND 34G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20050810002512005081000251NM 2005 8 10 AALA20050498 120050729A3350D71701100 BATTERY PACK BOEING737 737823 13844BZNM CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21920AN 29521 TUL - THREE BATTERY PACKS IN CABIN FAILED TEST PER CARD 2311. REPLACED THREE BATTERY PACKS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20050810002602005081000260NM 2005 8 10 AWXA200500926 120050717A53136545765125 STRINGER BOEING737 7373S3 1384711NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 DURING C18 CHECK DISCOVERED STRINGER 8L CRACKED, 1.125 INCHES IN LENGTH, AT BS 380. MAINTENANCE CUT OUT CRACK ON STRINGER 8L, BS 380, IAW BOEING 737-300 SRM 53-00-03-2 FIG 203. FABRICATED TWO ZEE ANGLES AND FILLER IAW BOEING 737-300 SRM 53-00-03-2 FIG 203. INSTALLED FABRICATED REPAIR PARTS AT STRINGER 8L, BS 380 IAW BOEING 737-300 SRM 53-00-03-2 FIG 203. 2L72 4F RTA16WE 20050810002732005081000273NM 2005 8 10 AWXA200500933 120050715A5320654581094 BEAM BOEING737 7373S3 1384711NM CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 DURING C18 CHECK DISCOVERED CORROSION ON BS 312 BEAM FROM BL 0 TO BL 21R, WL 208. PREVIOUS BLEND OUT PRESENT, MATERIAL LOSS GREATER THAN ALLOWED, IAW BOEING 737-300 SRM 53-10-51-1. MX CUT OUT DAMAGED SECTION OF BEAM IAW BOEING 737-300 SRM, 53-10-51-2 FIG 205. FABRICATED TWO ANGLES IAW BOEING 737-300 SRM 53-10-51. RECEIVED AND PREPARED CHORD AND SHIMS FOR INSTALLATION IAW BOEING 737-300 SRM 53-10-51-2. INSTALLED FABRICATED REPAIR PARTS AT BS 312 BEAM FROM BL 0 TO BL 21R, WL 208 IAW BOEING 737-300 SRM 53-10-51-2 FIG 205. 2L72 4F RTA16WE 20050810002752005081000275EU 2005 8 10 AWXA200500935 120050713A5320D5347049200 WEB AIRBUS320 A320231 3930325EU CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28627AW 66 DURING C4 CHECK DISCOVERED CORROSION ON WEB LOCATED IN THE AFT CARGO COMPARTMENT BETWEEN FS 58 AND FS 59, Y700. WEB WAS REMOVED FROM AFT CARGO COMPARTMENT, BETWEEN FS 58 AND FS 59, Y700 IAW AIRBUS 320 SRM 51-72-11. INSTALLED REPAIR PARTS IAW AIRBUS 320 SRM 51-72-11. 2L72 4F RTA28NM 20050810002792005081000279SO 2005 8 10 SIMA200520604 120050720A531314533888001 STRINGER EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL STR 19R CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21813AE 145539 A PREVIOUS REPAIR ANGLE ON STRINGER 19R WAS FOUND CHAFED. REMOVED THE EXISTING REPAIR ANGLE AND CLEANED THE AREA. FABRICATED AN INSTALLED A NEW REPAIR ANGLE. REPAIR DONE IAW SRM. (K) 2L72 4F4 FRTT00011ATTE6CH 20050810002802005081000280SO 2005 8 10 SIMA200520602 120050720A571014522178005 SILL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL SERVICE DOOR CORRODED A SIMAO OTHER O OTHER ININSP/MAINT 1 SW21811AE4752 14500908 THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED DAMAGED SILL AND CLEANED THE AREA. INSTALLED NEW SILL IAW SRM. (K) 2L72 4T4 FRTT00011ATTE6CH 20050810002862005081000286EA 2005 8 10 A6WA200540269 120050726A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FS 484,LBL 27 CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31405AW 7362 LT FS 484, LBL27, ANGLE IS CRACKED APPROX 1.25 INCH L THRU THICKNESS OF MATERIAL AT UPPER END OF RADIUS. REMOVED CRACKED ANGLE, FABED NEW ANGLE FROM ANGLE TO SMPLE AND INSTALLED IAW SRM. (K) 2L72 4F4 FRTA21EA E15NE 20050810002912005081000291EA 2005 8 10 A6WA200540243 120050318A2711 AILERON CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT AILERON TRIM OUT OF RIG A A6WAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL31412AW 7582 WITH AILERON TRIM CENTERED, AIRCRAFT HAS A STRONG ROLL TO THE RT. WITH LARGE AMOUNT OF LT WING DOWN TRIM, THE AIRCRAFT CAN BE MADE TO FLY LEVEL. AUTO-PILOT WAS OFF. FOUND RT AILERON SLIGHTLY OUT OF RIG. RE-RIGGED RT AILERON IAW AMM. (K) 2L72 4F4 FRTA21EA E15NE 20050810002982005081000298NM 2005 8 10 AALA20050508 120050807A3350 BATTERY PACK BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21755AN 30263 DFW - FIRST CLASS GALLEY FLOOR EMERGENCY EXIT LIGHTS. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN FIRST GLASS GALLEY FLOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20050810003112005081000311NM 2005 8 10 DHL2005746528 120050728A5754 SKIN BOEING727 727224 1384076NM NR 4 SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01746DH 22252 C-CHECK NR 4 SLAT SKIN CRACKED AT I/B SLAT HOOK (ON RIVET). ROUTED OUT CRACKED SIZE 1/4" ON NR 4 SLAT AT I/B SLAT HOOK IAW B727 SRM 57-50-3 FIG 10. FABBED REPAIR PLATE FROM 2024T3 .125 SIZE 3 3/4"X 4 1/4" PO 9002329 IAW B727 SRM 57-50-3 FIG 10. TREATED AND PRIMED PART & AREA IAW B727 SRM 51-10-2, INSTALLED PLATE REPAIR IAW B727 SRM 57-50-3 FIG 10. 2L73 4F A3WE 20050810003222005081000322WP 2005 8 10 ASAA0580353 120050621A5523591041449 SKIN DOUG DC9 DC983 3022083WP ELEVATOR TAB DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - DURING HV-CHECK, FOUND LEFT ELEVATOR GEARED TAB UPPER INBOARD SURFACE IS DELAMINATED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050810003312005081000331WP 2005 8 10 ASAA0580294 120050523A53205936071611 INTERCOSTAL DOUG DC9 DC983 3022083WP FS 1153 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - DURING C-CHECK, FOUND INTERCOSTAL CORRODED. REPLACED INTERCOSTAL. (M) 2L72 4F RTA6WE 20050810003332005081000333WP 2005 8 10 ASAA0580262 120050516A5320993051225 CUSP WEB DOUG DC9 DC983 3022083WP FS 1067 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02968AS 53016 OKC - FOUND HV-CHECK, FOUND RIGHT CUSP WEB CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050810003372005081000337WP 2005 8 10 ASAA0580311 120050613A5321993654513 FLOOR PANEL DOUG DC9 DC983 3022083WP FS 180-218 DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050810003382005081000338WP 2005 8 10 ASAA0580261 120050515A531359360501 LONGERON DOUG DC9 DC983 3022083WP FS 1203-1243 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - DURING C-CHECK, FOUND LONGERON 30 IS CORRODED AT STATION 1220. REMOVED AND REPLACED STRAP. (M) 2L72 4F RTA6WE 20050810003562005081000356WP 2005 8 10 ASAA0580320 120050613A532099365347 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FS 162-196 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - FOUND DURING HV CHECK, CABIN FLOOR PANEL SUPPORT CORRODED. REPLACED FLOOR PANEL SUPPORT. (M) 2L72 4F RTA6WE 20050810003682005081000368WP 2005 8 10 05FDEA02365 120050809A5710 CAP DOUG MD10 MD1010F 3022112WP ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25564FE 46984 LT WING XORS 402 BULKHEAD CAP CRACKED FWD OF STR 15. REPAIR IAW EA 8-5710-84859. 2L73 4F RTA22WE 20050810003742005081000374WP 2005 8 10 05FDEA02360 120050809A5320 CHANNEL DOUG MD10 MD1010F 3022112WP ZONE 100 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25564FE 46984 FWD CARGO COMPT RT SIDE ON CHANNEL AT X=-58 FOUND AN EXISTING SPLICE REPAIR Y=1019 Z=-100. REPAIR PER SRM 53-70-00 FIG 8, SHEET 1-3 VOL 1. 2L73 4F RTA22WE 20050811000092005081100009WP 2005 8 11 05FDEA02336 120050809A5322991960443 SHEAR TIE DOUG DC10 DC1010 3022110WP FS 1741 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25564FE 46984 CTR CARGO COMPT BILGE FOUND CORROSION ON SHEAR CLIP AT STA 1741 FROM STR 52 TO 51 LT. REMOVED CORROSION PER SRM 51-21-01 VOL 2 PAGE 28. TREATED AREA PER SRM 51-21-01 PG 21-24-25 VOL 2. REPAIRED SHEAR CLIP PER SRM 53-30-00 VOL 1 FIG 10, SRM 51-35-01 PG 1/13 AND SRM 51-33-01 PG 34-47 VOL 2. 2L73 4F A22WE 20050811000102005081100010WP 2005 8 11 05FDEA02337 120050809A5512 SKIN DOUG DC10 DC1010 3022110WP LT STAB DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25564FE 46984 LT STAB, XE 101 I/B ELEV, EXISTING 1 EXT REPAIR DOUBLER ON UPPER SKIN. REPLACE REPAIR PER SRM 55-00-01 VOL 1 SHT 2A, 2B FIG 3 SHT 2. 2L73 4F A22WE 20050811000132005081100013WP 2005 8 11 05FDEA02364 120050809A5310 BEAM DOUG MD10 MD1010F 3022112WP ZONE 100 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25564FE 46984 FWD CARGO COMPT RIGHT SIDE STA 1099 FOUND EXISTING SPLICE REPAIR WITH NEW SECTION OF BEAM X=-46 Z=-100. REPAIR PER SRM 53-60-01 FIG 3 VOL 1. 2L73 4F RTA22WE 20050811000152005081100015WP 2005 8 11 05FDEA02369 120050809A5730 ACCESS PANEL DOUG MD10 MD1010F 3022112WP ZONE 500 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25564FE 46984 LEFT WING ACCESS PANEL PRESSURE REFUEL AREA AT XOS 611 EXISTING EXTERNAL REPAIR DOUBLER ON SKIN. REPAIR IAW SRM 57-10-00 FIG 68 VOL 1. 2L73 4F RTA22WE 20050811000182005081100018WP 2005 8 11 05FDEA02341 120050809A5315 FLOORBEAM DOUG MD10 MD1010F 3022112WP FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25564FE 46984 AT STA 919, X=58, Z=-97 AFTER REMOVED OLD CHANNEL WITH NRC N01214, FOUND FLOORBEAM DAMAGED ON OLD REPAIR. REPAIR BEAM PER SRM 53-60-01 VOL 1 FIG 3. 2L73 4F RTA22WE 20050811000192005081100019WP 2005 8 11 05FDEA02342 120050809A5310AFA00433 BEAM DOUG MD10 MD1010F 3022112WP CARGO BAY DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25564FE 46984 CTR CARGO COMPT ON BEAM AT STA 1701 RT SIDE FOUND OLD REPAIR AT X=-38 BROKEN. REPLACED BEAM PER DWG AFA0043-3 AND SRM 51-33-01 PG 34/47 AND SRM 51-35-01 PG 1/13. 2L73 4F RTA22WE 20050811000222005081100022WP 2005 8 11 05FDEA02345 120050809A5313AEA034423 LONGERON DOUG MD10 MD1010F 3022112WP CARGO BAY CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25564FE 46984 CTR CARGO COMPT ON STA 1521 X=-50 RT SIDE 1EA CRACK LONG 10" ON EXISTING REPAIR AT Z=97.350. REPLACE TEE LONGERON IAW SRM 51-35-01 PG 1-13 VOL 2 AND DWG AEA0344 AND SRM 51-33-01 PG 34-47 VOL 2. 2L73 4F RTA22WE 20050811000232005081100023WP 2005 8 11 05FDEA02346 120050809A5320 ANGLE DOUG MD10 MD1010F 3022112WP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25564FE 46984 PERFORMED PENETRANT INSPECTION ON LT LWR CAP ANGLE AT STA 2122.881 FOUND 2 INCH CRACK LONG. REPAIRED ANGLE IAW SRM 53-40-00 FIG 6 PG 25 VOL 1. 2L73 4F RTA22WE 20050811000252005081100025WP 2005 8 11 05FDEA02348 120050809A5730 SKIN DOUG MD10 MD1010F 3022112WP LT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25564FE 46984 LEFT WING XOS UPPER EXT L/E SIDE, EXISTING REPAIR DOUBLER ON SKIN. REMOVED SLAT TRACK DOOR AND REMOVED AND REPLACED AND REINSTALLED TRACK SLAT DOOR IAW MM 57-21-01-2, SRM 51-35-02 VOL 2 AND SRM 57-10-00 FIG 68 VOL 1. 2L73 4F RTA22WE 20050811000262005081100026WP 2005 8 11 05FDEA02366 120050809A5313AFA30401 LONGERON DOUG MD10 MD1010F 3022112WP ZONE 100 BROKEN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25564FE 46984 CTR CARGO COMPT BILGE AREA ON STA 1671 RT SIDE LONGERON SPLICE BROKEN 6 INCHES LONG ON L44. REPAIR FRAME CAP BETWEEN L45-46 RT IAW SRM 53-30-00 FIG 5 VOL 1 AND REPLACED LONGERON IAW DWG NFA6074. 2L73 4F RTA22WE 20050811000272005081100027WP 2005 8 11 05FDEA02367 120050809A5320 STIFFENER DOUG MD10 MD1010F 3022112WP ZONE 100 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25564FE 46984 AFT CARGO COMPT BILGE AREA RT SIDE ON L49 ONE EXISTING SPLICE ON STIFFENER AT STA 1781 TO 1801. REPAIR PER SRM 53-10-00 FIG 2A SHT 1-3 VOL 1. 2L73 4F RTA22WE 20050811000282005081100028SO 2005 8 11 CHQA200500137 120050807A21508166042 REGULATOR VALVE EMB 135 EMB135KL 3260302SO CABIN COOLING BURNED A CHQAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL11375SK9793 9793 145569 FLIGHT 5282 - STL - ATL - ON CLIMB-OUT, RECEIVED BLEED 1 CLOSED MESSAGE AND A BURNING SMELL AROUND ROW 5A. FOUND THE PACK VALVE CIRCUIT BREAKER POPPED AND FOUND THE PACK VALVE WAS BURNT UP CAUSING THE CIRCUIT BREAKER TO POP. REMOVED AND REPLACED THE PACK VALVE. OPS CHECKED BOTH PACKS WITH ENGINE AND APU BLEEDS. NO SMELL NOTED. 2L72 4F RTT00011AT 20050811000302005081100030EU 2005 8 11 08012005B 120050801A261172111211000 SMOKE DETECTOR SAAB SF340 340B 7860101EU AVIONICS FALSE ACTIVATIONA NSVAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 EA27237MJ 237 AVIONICS SMOKE LIGHT ILLUMINATED ON GROUND. CLEANED SMOKE DETECTOR. 2L72 4T RTA52EU 20050811000312005081100031NM 2005 8 11 AT0500027 120050808A3520 OXYGEN MASK BOEING737 73776N 13844CHNM LAVATORY DEPLOYED A ZZDAO OTHER O OTHER CRCRUISE 1 SO15173AT 32661 AFT LEFT LAV O2 MASK DEPLOYED IN FLIGHT. RESTOWED AFT LAV O2 MASKS REF 35-22. 2L72 4F RTA16WE 20050811000332005081100033WP 2005 8 11 05FDEA02354 120050809A5310 STRUCTURE DOUG MD10 MD1010F 3022112WP ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25564FE 46984 LWR FUSELAGE LT SIDE AIR CONDITION COMPT ON INLET EXHAUST VALVE SYS NR 2 DOUBLER WITH CORROSION AT Y=515 LONGERON 46. REMOVED CORROSION PER SRM 51-21-001 VOL 2 PAR 34 AND REPAIRED PER SRM 53-20-00 FIG 2 VOL 1. 2L73 4F RTA22WE 20050811000342005081100034WP 2005 8 11 05FDEA02351 120050809A5730 SKIN DOUG MD10 MD1010F 3022112WP ZONE 500 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25564FE 46984 LT WING SLAT 2 XORS 231 EXISTING FLUSH REPAIR DOUBLER ON LWR SKIN. REPAIR PER SRM 57-10-00 FIG 29 VOL 1. 2L73 4F RTA22WE 20050811000402005081100040CE 2005 8 11 DXTA200500878 120050802A3250MS1656230 PIN CESSNA750 750 2076810CE TILLER SHEARED E DXTAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL07967QS 7500067 DURING TAXI, TILLER KNOB DEVELOPED SLACK WHEN TURNING THEN FINALLY POPPED AND ROTATES FREELY. UNABLE TO STEER THE AIRCRAFT WITH THE TILLER. ROLL PIN IN TILLER KNOB SHEARED OFF. INSTALLED NEW PIN, P/N MS16562-30. WORK DONE IAW CE-750 MM. CH. 32-50-00. OPS CHECK GOOD. 2L72 4J RTT00007WI 20050811000412005081100041CE 2005 8 11 DXTA200500879 120050802A3240 BRAKE ASSY CESSNA500 560CESSNA 2076750CE MLG FAILED E DXTAO OTHER S AFFECT SYSTEMS LDLANDING 1 GL07333QS 5600333 UPON LANDING F/O RT BRAKE PEDALS WHEN PRESSED TP APPLY BRAKES WENT TO THE FLOOR-POWER BRAKE LOW PRESSURE LIGHT AND ANTI-SKID INOP LIGHT ILLUMINATED. CAPTAIN CHECKED BRAKES ON LEFT SIDE,TEMPORARY BRAKES WERE ESTABLISHED AND THEN COMPLETE FAILURE, EMERGENCY BRAKES APPLIED. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20050811000442005081100044CE 2005 8 11 DXTA200500882 120050804A3240 BRAKE CESSNA500 560CESSNA 2076750CE MLG INTERMITTENT E DXTAO OTHER S AFFECT SYSTEMS LDLANDING 1 GL07317QS 5600317 PON - LANDING RIGHT BRAKE PEDAL FOR RIGHT SIDE PILOT WAS SOFT (APPROX 3"- 4" TRAVEL) MUCH FIRMER ON SECOND APPLICATION. SAME SEQUENCE EXPERIENCED DURING TAXI. LEFT SIDE BRAKES OPERATE NORMALLY. 2L72 4F RTA22CE 20050811000452005081100045 2005 8 11 DXTA200500884 420050803A34607014300901 DISPLAY CESSNA750 750 2076810CE NR 1 FAILED E DXTAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07921QS218 7500241 NR 1 DU DISPLAY FAILED INFLIGHT. SLIGHT SMELL OF ELECTRIC SHORT OCCURRED BUT DISAPPEARED AFTER DESELECTING NR 1 DU AS THE PFD DISPLAY. VERIFIED DU870 DEAD. REMOVED AND REPLACED NR 1 PFD AND OPS CHECKED FUNCTIONS NORMAL IAW CESSNA 750 MM CHAP 34-25-01. 2L72 4J RTT00007WI 20050811000472005081100047 2005 8 11 XN0A1252 420050809A3442 DISPLAY AIRBUS300 A300B4203 3930306EU RADAR INOPERATIVE A XN0AO OTHER O OTHER NRNOT REPORTED 1 GL23474AS 219 CAPT'S RADAR DISPLAY INOP. REMOVED AND REPLACED RADAR IND IAW A300 MM 34-41. OPS CHECK GOOD. 2L72 4F RTA35EU 20050811000482005081100048NE 2005 8 11 XN0A1253 220050809A7412 EXCITER BOEING727 727227 1384078NM PWA JT8 JT8D9A 52048NE NR 2 ENGINE FAILED A XN0AD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL2376752 21248 ON ENGINE START NR 2 ENGINE WOULD NOT START, START VALVE OPENS PRESSURE DROP NO EGT. REMOVED AND REPLACED NR 2 ENG EXCITER BOX IAW MM 74-11-1, OPS GOOD. 2L73 4F4 F A3WE E2EA 20050811000492005081100049NM 2005 8 11 XN0A1254 120050810A3241 BRAKE ASSY BOEING727 727227 1384078NM MLG VIBRATES A XN0AD RETURN TO BLOCK E VIBRATION/BUFFET TXTAXI/GRND HDL 1 GL2376752 21248 ON TAXIOUT, BRAKES VIBRATE WHEN APPLIED. BLED BRAKES AS REQ'D IAW B727 MM REF 32-41-0, SYSTEM OPS CHECKS GOOD. 2L73 4F A3WE 20050811000512005081100051WP 2005 8 11 05FDEA02371 120050809A5330 SKIN DOUG MD10 MD1010F 3022112WP FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25564FE 46984 ON EXTERNAL SKIN AT STA 1139 LONGERON 47-48 LT SIDE FOUND TWO RIVETS LOOSE. REPAIR SKIN IAW EA 8-5330-84901A PT 2. 2L73 4F RTA22WE 20050811000552005081100055SW 2005 8 11 M3XA2005508MT 120050806A3150407375015105 ANNUNCIATOR BELL 407 407 1182206SW COCKPIT BURNED E M3XABA EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP07508MT2911 53326 DURING CRUISE FLIGHT RETURNING TO BASE, THE PILOT SMELLED SMOKE AND NOTICED PUFFS OF SMOKE COMING FROM THE INSTRUMENT PANEL/CAUTION AND WARNING PANEL AREA. IMMEDIATELY LANDED AND EVACUATED THE AIRCRAFT. AFTER SHUTDOWN, NOTICED THE CIRCUIT BREAKER FOR THE CAUTION AND WARNING PANEL HAD OPENED. MAINTENANCE WAS CONTACTED FOR FURTHER INSTRUCTIONS AND REPAIR. 1G71 3U O H2SW 20050811000572005081100057CE 2005 8 11 DXTA200500872 120050728A3260S31063 DIODE CESSNA560 560XL 2076702CE MLG INDICATOR INOPERATIVE E DXTAO OTHER J WARNING INDICATION APAPPROACH 1 GL07639QS 5605139 GEAR UNSAFE INDICATION FOR LEFT MAIN WHEEL, LIGHT FLICKERING AND UNLOCK LIGHT ON FLICKERING. RAN 'LANDING GEAR WILL NOT EXTEND' CHECKLIST WITH GEAR MANUAL BLOW DOWN, NO CHANGE IN INDICATION. REMOVED AND REPLACED INOP DIODE WITH A NEW DIODE AS REQUIRED OPS CHECK GOOD. ALL WORK PERFORMED IAW CE-560XL MM CHAPTER 32-30-00 AND 32-01-00. 2L72 4F RTA22CE 20050811000592005081100059NM 2005 8 11 DXTA200500873 120050729A2497C752F20 WIRE GULSTM200 200 4500308NM DAMAGED E DXTAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 GL07708QS 069 STRONG SMOKE SMELL IN THE COCKPIT, THAT SMELLED LIKE BURNING WIRES ON APPROACH. TURNED OFF ALL LIGHTS AND AUDIO IN THE CABIN THE SMELL WENT AWAY SHORTLY AFTER. THE SMELL WAS MUCH STRONGER IN THE COCKPIT THAN THE CABIN. FOUND SCREW IN WIRE BUNDLE, REPAIRED WIRE C752F20 WD 27-40-12, MM 20-30-02, 20-50-03. OPS CHECKED AFFECTED SYSTEM HORIZONTAL TRIM SECONDARY CHANNEL MM 27-40-00. 2L72 4F RTA53NM 20050811000622005081100062CE 2005 8 11 DXTA200500875 120050731A2821 FILTER CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL FUEL SYSTEM BYPASSING E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07964QS 7500164 CAE330346 FUEL FILTER BYPASS LIGHT (R) ILLUMINATED ON T/O ROLL. LOW SPEED ABORT AT 40KTS. 2L72 4J4 FRTT00007WITE6CH 20050811000632005081100063CE 2005 8 11 DXTA200500874 120050731A3230 LINK CESSNA500 560CESSNA 2076750CE MLG OUT OF ADJUST E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07304QS 5600408 AFTER GEAR RETRACTION NOTED EXCESSIVE AIR NOISE, EXTENDED GEAR, UPON RETRACTION HYD PRESS LIGHT REMAINED ON ALSO GEAR UNLOCK LIGHT STAYED ON. RE-EXTENDED GEAR AND HYD PRESS LIGHT WENT OUT AND GEAR UNLOCK LIGHT WENT OUT. ADJUSTED NOSE LANDING GEAR DOWN LINKAGE IAW CE560 M/M CHAP 32-21-01, LANDING GEAR EXTENDS AND RETRACTED TEN TIME WITH NO DEFAULT. 2L72 4F RTA22CE 20050811000642005081100064EU 2005 8 11 05FDEA02330 120050808A5321 FLOOR PANEL AIRBUS300 A300F4605R 3930327EU MDC CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25670FE 777 MDC FLOOR PNL 231EF IS CRACKED. 2L72 4F RTA35EU 20050811000672005081100067WP 2005 8 11 05FDEA02333 120050809A5754 SKIN DOUG MD10 MD1010F 3022112WP NR 1 SLAT DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25564FE 46984 RIGHT WING, SLAT NR 1, EXT TRACK FITTING, ONE EXT REPAIR DOUBLER ON LWR SKIN. REPAIR PER SRM 57-10-01 FIG 4 SHT 2 VOL 1, SRM 51-35-02 VOL 2 PG 3/9. 2L73 4F RTA22WE 20050811000682005081100068WP 2005 8 11 05FDEA02334 120050809A5753 SKIN DOUG MD10 MD1010F 3022112WP TE FLAP DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25564FE 46984 LEFT WING O/B FLAP XOF 513 EXT REPAIR DOUBLER ON LWR SKIN. REPLACE REPAIR PER SRM 57-10-00 FIG 85 VOL 1. 2L73 4F RTA22WE 20050811000722005081100072WP 2005 8 11 ASAA0580328 120050613A5320995576317 INTERCOSTAL DOUG DC9 DC983 3022083WP FS 185 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - DURING HV CHECK, FOUND L1 DOOR INTERCOSTAL CRACKED. REPLACED DAMAGED INTERCOSTAL. (M) 2L72 4F RTA6WE 20050811000732005081100073WP 2005 8 11 ASAA0580324 120050613A532059364423 WEB DOUG DC9 DC983 3022083WP FS 1155-1212 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - DURING HV CHECK, FOUND AFT CARGO BAY DOOR JAMB LOWER TORQUE BOX WEB CORRODED. REPLACED WEB. (M) 2L72 4F RTA6WE 20050811000742005081100074WP 2005 8 11 ASAA0580334 120050613A532259360759 SHEAR TIE DOUG DC9 DC983 3022083WP FS 1219 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - FOUND DURING HV CHECK, SHEAR TIE CORRODED. REPLACED DAMAGED SHEAR TIE. (M) 2L72 4F RTA6WE 20050811000762005081100076WP 2005 8 11 ASAA0580326 120050613A5313593666713 LONGERON DOUG DC9 DC983 3022083WP FS 1238-1296 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - FOUND HV-CHECK, LONGERON 30 CORRODED. REPLACED DAMAGED SECTION. (M) 2L72 4F RTA6WE 20050811000792005081100079WP 2005 8 11 ASAA0580327 120050613A532299360737 SHEAR TIE DOUG DC9 DC983 3022083WP FS 1155 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - DURING HV CHECK, AFT CARGO BAY SHEAR TIE CORRODED. REPLACED DAMAGED SHEAR TIE. (M) 2L72 4F RTA6WE 20050811000852005081100085WP 2005 8 11 ASAA0580336 120050613A532059360392 STRAP DOUG DC9 DC983 3022083WP FS 1147 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - DURING HV CHECK, AFT CARGO BAY STRAP BETWEEN FRAMES 1136 AND 1155 CORRODED. REPLACED DAMAGED STRAP. (M) 2L72 4F RTA6WE 20050811000872005081100087WP 2005 8 11 ASAA0580337 120050613A5322991960443 SHEAR TIE DOUG DC9 DC983 3022083WP FS 1250 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - DURING HV CHECK, FOUND SHEAR TIE CORRODED. REPLACED DAMAGED SHEAR TIE. (M) 2L72 4F RTA6WE 20050811000882005081100088WP 2005 8 11 ASAA0580338 120050613A5311SR0953005725 FRAME DOUG DC9 DC983 3022083WP FS 1250 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - FOUND DURING HV CHECK, AFT CARGO BAY FRAME CORROSION. REPLACED DAMAGED FRAME. (M) 2L72 4F RTA6WE 20050811000912005081100091NE 2005 8 11 HALA0500801 220050802A7200 ENGINE BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE LEFT MALFUNCTIONED A HALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13486HA 55131 13242 LT ENGINE PARAMETERS STARTED TO FLUCTUATE APPROX 7000 FT ON CLIMBOUT. WENT FROM CLB1 TO MCT PWR, IGN SYMBOL CAME ON. FMS PAGE CHANGED TO CONFIRM ENG OUT ALL FLUCTUATIONS WERE SMALL AND DID NOT SHUTDOWN ENGINE. ACCOMPLISHED FIM 73-22, TASK 807 EEC, INPUTS FRM FXX BLEED WORD FAULT CROSS CHECK FML (CH B) DUE EEC NR 1 BITE INFO, NO FAULTS NOTED. DFDR DOWNLOADED AND GIVE TO ENGINEERING FOR ANALYSIS. REF LOG PGS 114675 & 114801, ITEMS 70,71,72, AND 73. (WP13200509843) (K) 2L72 4F4 FTRA6WE E00061EN 20050811000942005081100094EA 2005 8 11 ASOA05615 120050722A5210H341433 HANDLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PASSENGER DOOR BINDING A ASOAK NONE O OTHER ININSP/MAINT 1 SO27842AS 7305 7304 DURING A GROUND INSPECTION, THE FLIGHT ATTENDANT REPAORTED THE PASSENGER DOOR DIFFICULT TO OPEN. MAINTENANCE REMOVED, REBUILT, AND REINSTALLED THE PASSENGER DOOR HANDLE ASSY. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050811000992005081100099EA 2005 8 11 ASOA05612 120050720A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE MAIN PAX LACK OF LUBE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27846AS 7328 AFTER PARKING THE AIRCRAFT, THE PASSENGER DOOR COULD NOT BE OPENED FROM THE INSIDE. MAINTENANCE CLEANED AND LUBRICATED THE TRACK AND ROLLER ASSEMBLY ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. NO FURTHER DEFECTS NOTED. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050811001002005081100100EA 2005 8 11 ASOA05616 120050705A5320601R3501153 PLATE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27852AS 7369 DURING C-CHECK, THE CARGO DOOR FLOOR LANDING PLATE WAS FOUND TO BE CRACKED FROM THE CENTER 2 RIVETS BEYOND LIMITS. MAINTENANCE REPAIRED THE CARGO DOOR FLOOR LANDING PLATE IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050811001012005081100101EA 2005 8 11 ASOA05619 120050722A5730 PANEL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE WING CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27833AS 7246 DURING A C-CHECK, THE LOWER WING PLANK AT WS 148.019 LT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LOWER WING PLANK AT WS 148.019 LT SIDE IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050811001022005081100102EA 2005 8 11 ASOA05626 120050723A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27833AS 7246 DURING A C-CHECK, THE AFT FLOOR SUPPORT ANGLES FS 280 BETWEEN LBL 9 AND RBL 9 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE CORRODED FLOOR SUPPORT ANGLE IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050811001032005081100103 2005 8 11 ASOA05627 420050723A3140350A53000100 COMPUTER AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE COCKPIT INOPERATIVE A ASOAK NONE O OTHER DEDESCENT 1 SO27632AS195717 338 DURING DESCENT, THE CREW NOTICED A CLIMB IN CABIN PRESSURE, SHORTLY FOLLOWED BY AN MFC 2B FAULT. THE CREW DECLARED AN EMERGENCY AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE NR 2 MFC. OPERATIONAL CHECKS GOOD AC OK FOR SERVICE. (K) 2H72 4T4 TRTA53EU E20NE 20050811001042005081100104EA 2005 8 11 A6WA200540271 120050728A5712 RIB CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT FS 523.8 CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31405AW 7362 LT MLG WHEEL WELL BATT RIB AT WS 48.30, FS 523.8 IS CRACKED AT UPPER RADIUS APPROX 1.25 INCH LONG. REPAIRED IAW REO. (K) 2L72 4F4 FRTA21EA E15NE 20050811001052005081100105EA 2005 8 11 ASOA05617 120050707A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27852AS 7369 DURING A C-CHECK, THE LT OB FS 484 ANGLE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRE THE LT OB FS 484 ANGLE IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050811001062005081100106SO 2005 8 11 YNT2005F00000 120050719A53131159BH20547 STRINGER GULSTMG1159 G1159 3953505SO RROYCESPEY SPEY511* 54523EU FS336,355 CORRODED E YNTAO OTHER O OTHER NRNOT REPORTED 1 SW05188JS12763 029 CORROSION ON STRINGER L17, FS 336, CORROSION REMOVED AND A REPAIR STRAP INSTALLED OVER REPAIRED AREA. (SW05200510589) (K) 2L72 4F4 FRTA12EA E2EU 20050811001072005081100107EA 2005 8 11 ASOA05614 120050722A335059257 INVERTER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 2 MALFUNCTIONED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27820AS 7188 DURING A GROUND INSPECTION, THE EMERGENCY LIGHTS FROM ROWS 2 TO 4 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 INVERTER FOR THE EMERGENCY LIGHTS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050811001092005081100109EA 2005 8 11 ASOA05623 120050722A3350CANAC7B LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27833AS 7246 DURING A C-CHECK, THE LT AND RT OVERWING EMERGENCY EXIT BETA LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT AND RT OVERWING EMERGENCY EXIT BETA LIGHTS. OPS CHECK GOOD. (K) 2L72 4F4 FRTA21EA E15NE 20050811001112005081100111EA 2005 8 11 ASOA05625 120050723A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27833AS 7246 DURING A C-CHECK, THE FORWARD FLOOR SUPPORT ANGLE FS 280 BETWEEN LBL 9 AND RBL 9 WAS FOUND CORRODED BEYOND LIMITS. (K) 2L72 4F4 FRTA21EA E15NE 20050811001122005081100112EA 2005 8 11 ASOA05628 120050724A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27833AS 7246 DURING A C-CHECK, THE LT IB AND RT OB FS 280 CLIPS WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LT OB AND RT IB FS 280 CLIPS IAW SRM. (K) 2L72 4F4 FRTA21EA E15NE 20050811001202005081100120NM 2005 8 11 UPS05M45082 120050524A5347 SEAT TRACK DOUG MD11 MD11F 3023600NM AFT CABIN CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01255UP 48404 INSPECTION TYPE:C-CHECK AFT CABIN - CORROSION ON SEAT TRACK AT X=-107 STA 1841, 1901 & 1961. AFT CABIN CORROSION ON SEAT TRACK REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-70-00 FIG 3 VOL 1 REV 37, SPLICE HATS REWORKED CARRIED OUT AND SPLICE PLATES FABRICATE AS PER SRM 53-70-00 FIG 1 VOL I REV 37. 2L73 4F RTA22WE 20050811001212005081100121NM 2005 8 11 UPS05M45083 120050527A5347 SEAT TRACK DOUG MD11 MD11F 3023600NM CABIN CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01255UP 48404 INSPECTION TYPE:C-CHECK CABIN - CORROSION ON SEAT TRACK FLANGE AT SPLICE END STA 929 X=-8. CABIN SEAT TRACK BETWEEN STA 849-929 X=-8 REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG 1 VOL I REV 37. 2L73 4F RTA22WE 20050811001222005081100122NM 2005 8 11 UPS05M45085 120050602A5311 FRAME DOUG MD11 MD11F 3023600NM FWD CGO COMPT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01255UP 48404 INSPECTION TYPE:C-CHECK FWD CARGO UNDER FLOOR AREA TRANSVERSE AT STA 755 LONGERON 52 (CENTERLINE ) FOUND WITH CORROSION AS MARKED. CORROSION REMOVED & TREATED AS PER SRM 51-21-01 VOL II REV 37 ON FWD CARGO UNDER FLOOR AT STA 755 LONGERON 52, FOUND WITHIN LIMIT AS PER SRM 53-00-01 VOL I REV 37. 2L73 4F RTA22WE 20050811001232005081100123NM 2005 8 11 UPS05M45086 120050603A5311 FRAME DOUG MD11 MD11F 3023600NM CTR CGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01255UP 48404 INSPECTION TYPE:C-CHECK CTR CARGO AT STA 1721 LONGERON 51 LT TO 51 RT TRANSVERSE FRAME FOUND WITH CORROSION AS MARKED. CORROSION REMOVED AS PER SRM 53-30-00 VOL I FIG 7 REV 37 ON CTR CARGO AT STA 1721 LONGERON 51 LT TRANSVERSE FRAME FOUND WITHIN LIMIT AS PER SRM 53-00-01 VOL I FIG 1A REV 37 AND REWORKED AREA REPROTECTED AS PER SRM 51-21-01 VOL II REV 37. 2L73 4F RTA22WE 20050811001242005081100124NM 2005 8 11 UPS05M45087 120050603A5311 FRAME DOUG MD11 MD11F 3023600NM CTR CARGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01255UP 48404 INSPECTION TYPE:C-CHECK CTR CARGO AT STA 1741 LONGERON 52 TRANSVERSE FRAME FOUND WITH CORROSION AS MARKED. CORROSION REMOVED AS PER SRM 53-30-00 VOL 1 FIG 7 REV 37 ON CTR CARGO AT STA 1741 LONGERON 52 FOUND WITHIN LIMIT AS PER SRM 53-00-01 VOL I REV 37 AND REWORKED AREA REPROTECTED AS PER SRM 51-21-01 VOL II REV 37. 2L73 4F RTA22WE 20050811001252005081100125NM 2005 8 11 UPS05M45095 120050603A5311 FRAME DOUG MD11 MD11F 3023600NM CTR CARGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01255UP 48404 INSPECTION TYPE:C-CHECK CTR CARGO AT STA 1741 LONGERON 52 AFT SIDE OF TRANSVERSE FRAME FOUND WITH CORROSION AS MARKED. CORROSION REMOVED & TREATED AS PER SRM 51-21-01 VOL II REV 37 ON CTR CARGO AT STA 1741 LONGERON 52 AFT SIDE TRANSVERSE AND FOUND WITHIN LIMIT AS PER SRM 53-00-01 VOL I FIG 1A REV 37. 2L73 4F RTA22WE 20050811001262005081100126NM 2005 8 11 UPS05M45096 120050603A5311 FRAME DOUG MD11 MD11F 3023600NM CTR CARGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01255UP 48404 INSPECTION TYPE:C-CHECK CTR CARGO AT STA 1781 LONGERON 52 TRANSVERSE FRAME FOUND WITH CORROSION AS MARKED. CORROSION REMOVED AS PER SRM 53-30-00 VOL I FIG 7 REV 37 ON CTG CARGO STA 1781 LONGERON 52 FOUND WITHIN LIMIT AS PER SRM 53-00-01 VOL 1 FIG 1A REV 37, REWORKED AREA REPROTECTED AS PER SRM 51-21-01 VOL II REV 37. 2L73 4F RTA22WE 20050811001272005081100127NM 2005 8 11 UPS05M45097 120050604A5340 MOUNT DOUG MD11 MD11F 3023600NM FWD CARGO COMPT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01255UP 48404 INSPECTION TYPE:C-CHECK FWD CARGO MOUNTING CORRODED AT INNER AREA WHERE MOUNT BOLTS ARE LOCATED AS MARKED. CORROSION REMOVED AS PER SRM 53-00-01 VOL 1 FIG 1A REV 37. MINOR CORROSION ON 3EA LATERAL GUIDE FLOOR MOUNTING FOUND WITHIN LIMIT AND REPROTECTED AS PER SRM 51-21-01 VOL II REV 37. 2L73 4F RTA22WE 20050811001282005081100128NM 2005 8 11 UPS05M45098 120050604A5340 MOUNT DOUG MD11 MD11F 3023600NM FWD CGO COMPT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01255UP 48404 INSPECTION TYPE:C-CHECK FWD CARGO AT STA 999 4EA LATERAL GUIDE FLOOR MOUTING CORRODED AT INNER AREA WHERE MOUNT BOLTS ARE LOCATED AS MARKED. CORROSION REMOVED & TREATED AS PER SRM 51-21-01 VOL II REV 37 ON FWD CARGO AT STA 999 4EA LATERAL GUIDE MINOR CORROSION AND FOUND WITHIN LIMIT AS PER SRM 53-00-01 VOL I FIG 1A REV 37. 2L73 4F RTA22WE 20050811001322005081100132NM 2005 8 11 UPS05445094 120050725A5315 FLOORBEAM BOEING747 747121 1384871NM U/D CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE:C U/D BS 380 FLOORBEAM UPPER CHORD HORIZONTAL AFT FLANGE 1EA MOUNTING HOLE CRACK (CRACK LENGTH 0.040"). U/D BS 380 FLOORBEAM UPPER CHORD REPAIRED AT BTN LBL 24" TO LT O/B AS PER SRM 53-10-07 FIG 10. 2L74 4F A20WE 20050811001352005081100135NM 2005 8 11 UPS05445128 120050722A542065B09031077 WEB BOEING747 747121 1384871NM NR 1 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE:C NR 1 PYLON REAR MOUNT BULKHEAD FOUND CRACK AT FWD FRAME WEB (CRACK LENGTH 7/16"). NR 1 PYLON REAR MOUNT BULKHEAD FRAME WEB REPAIRED AS PER HX RS R54-53-35353 & UPS ENGINEERING FILE 747-54-20052, CONTINUE TO CONDUCT DETAIL VISUAL & HFEC INSPECTION OF THE REAR ENGINE MOUNT LOWER B/H ASSY, PER THE REQUIREMENT OF SB 747-54A2202, EVERY 1200 FLT CYC OR 18 MONTHS. 2L74 4F A20WE 20050811001362005081100136NM 2005 8 11 UPS05445131 120050723A5730 SKIN BOEING747 747121 1384871NM LHW CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE:C, LEFT WING UPPER WING SKIN L/E RABBIT AREA 2 PLACES BULGED UP AT WS 1470-1515 AFT OF NR 1 VC FLAP AREA. CORROSION THROUGH WHOLE THICKNESS AREA 7.3" X 4.3". LEFT WING UPPER WING SKIN REPAIRED AS PER HX RS R57-25-35357 & UPS ENGINEERING FILE 747-57-20080. 2L74 4F A20WE 20050811001382005081100138NM 2005 8 11 AWXA200500940 120050715A5320654587512 ANGLE BOEING737 7373S3 1384711NM CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 DURING C18 CHECK DISCOVERED CORROSION ON THE R1 INNER CHORD, UPPER ANGLE AT BS 305 TO BS 324, BL 58R, WL 209. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-10-13-1 FIG 101. MAINTENANCE REMOVED ANGLE AT BS 305 TO BS 324, BL 58R, WL 209 IAW BEING 737-300 SRM 51-30-01. PREPARED NEW ANGLE FOR INSTALLATION IAW BOEING 737-300 SRM 51-40-02-0. INSTALLED REPAIR PARTS AT BS 305 TO BS 324, BL 58R, WL 209 IAW BOEING 737-300 SRM 51-40-02-0 FIG 3. 2L72 4F RTA16WE 20050810001392005081000139NM 2005 8 10 QXEA200501156 120050805A243523088002B STARTER GEN DHAV DHC8 DHC8202 2809007NM MALFUNCTIONED A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09345PH11473983 476 BLI FLIGHT NR 2249 - ON START UP (AFTER DISCONNECTING EXTERNAL POWER), NR 2 DC GENERATOR CAUTION LIGHT DID NOT EXTINGUISH. REPLACED STARTER/GENERATOR. OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050810001422005081000142NM 2005 8 10 UPS05245072 120050719A7830 BULKHEAD BOEING727 72722C 138400FNM THRUST REVERSER CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01941UP 19196 ENGINE NR 3 THRUST REVERSER AFT BULKHEAD CRACKED AT 11 O`CLOCK POS. REPAIRED IAW SRM 51-40-2 AND SRM 51-30-2. 2L73 4F A3WE 20050810001432005081000143NM 2005 8 10 UPS05245073 120050718A5754 SUPPORT ANGLE BOEING727 72722C 138400FNM NR 1 LE SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01941UP 19196 LE SLAT CRACKED ON SUPPORT ANGLE BENEATH TELESCOPIC DUCT, REPAIR. REPAIRED IAW SRM 51-40-3 AND SRM 57-50-2 FIG 2. 2L73 4F A3WE 20050810001772005081000177EA 2005 8 10 SWIA200515390 120050805A27604916406 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION LDLANDING 1 NM07446SW4960 4960 7666 ON SHORT FINAL, GOT WHITE SPOILERON FAULT AND WHITE INBOARD GROUND SPOILER FAULT. REPLACED NR 2 SECU WITH A SERVICEABLE UNIT IAW 27-00-00. 2L72 4F RTA21EA 20050810001782005081000178SO 2005 8 10 SWIA200515391 120050807A5753 FLAP EMB 120 EMB120ER 3260203SO CRACKED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07576SW 120345 LEFT NACELLE FLAP IS IN THE DOWN POSITION ROUGHLY 10 DEGREES IN THE FLAPS 0 DEGREE SETTING. REPLACED LT NACELLE FLAP ASSY IAW MM 27-50-02. 2L72 4T RTA31SO 20050810001802005081000180NM 2005 8 10 2005UALA00734 120050729A5313 STRINGER CLIP BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE STA 685, STR 4LTCRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29914UA 25381 CABIN UPPER LOBE STRINGER CLIP IS CRACKED AT STA 685, STR 4 LT. REMOVED AND REPLACED STRINGER CLIP. 2L72 4F4 FRTA16WE E2GL 20050810001912005081000191NM 2005 8 10 2005UALA00745 120050731A5330 SKIN BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE STA 837 BTWN STRDENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29912UA 25290 STA 837 IS DENTED BETWEEN STR 25L AND 26L. CUT OUT DAMAGE AND INSTALLED DOUBLER AND TRIPLER REPAIR PER SRM 53-00-01 FIG 229. 2L72 4F4 FRTA16WE E2GL 20050810001942005081000194NM 2005 8 10 2005UALA00748 120050802A52306547952136 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE AFT CARGO DOOR LGOUGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29351UA 24319 AFT CARGO DOOR LOWER AFT FRAME HAS .035 GOUGE WITH 15" LONG CRACK. REMOVED LOWER AFT FRAME. REMOVED INNER SUPPORT ANGLE. REINSTALLED ANGLE AND NEW FRAME. REF SRM 51-40-02. FRAME PN 65-47952-136. 2L72 4F4 FRTA16WE E2GL 20050810002042005081000204NM 2005 8 10 2005UALA00757 120050804A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29177UA 24384 EMERGENCY LT INOP, DR 1L SLIDE AND DR 4R SLIDE. REPLACED LIGHT ASSY. 2L74 4F4 FRTA20WE E24NE 20050810002192005081000219CE 2005 8 10 CIEA200500014 120050809A261261423473275 FIRE DETECTOR BEECH 200 200BEECH 1152920CE PWA PT6 PT6A60A 52043NE SHORTED E CIEAO OTHER O OTHER TXTAXI/GRND HDL 1 NM035ST BB289 AFTER THE PILOT GOT INTO THE AIRCRAFT TO PERFORM A TRIP AND TURNED ON THE MASTER SWITCH, THE ENGINE FIRE WARNING CIRCUIT BREAKER POPPED AND WOULD NOT RESET. THE TRIP WAS CANCELED AND THE AIRCRAFT WAS TURNED OVER TO MAINTENANCE. MAINTENANCE TROUBLESHOT AND FOUND THE LT AFT FIRE PROBE ON THE LEFT ENGINE TO BE SHORTED INTERNALLY. THE CONDITION OF THE PROBE WAS LOOKED AT AND WHERE THE WIRES FEED INTO THE PROBE APPEARS TO HAVE NO SEALANT AROUND THEM. THERE WAS MINOR EVIDENCE OF OIL IN THE AREA BUT NOT EXCESSIVE. THERE WAS NO EVIDENCE OF ANYTHING DRIPPING FROM THE UNIT ITSELF. 1L72 4T4 T A24CE E4EA 20050810002212005081000221WP 2005 8 10 IXXA05SMN118S 120050627A5730 SKIN DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE XF 345.000 MISREPAIRED A IXXAO OTHER W INADEQUATE Q C ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, LT OB FLAP, NON STANDARD REPAIR, XF 345.000 (UPPER PART) PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PAGE 1, SRM 57-7-1 FIG. 4, TR NR 57-94, EO SEMAN NR 2005856 DATE 06-18-05. REMOVED PLATING WITH IMPROPER REPAIR IAW SRM 51-1-21 PAGE 1. FABRICATED NEW PLATING (ALCLAD 2024 T3 0.063”) IAW SRM 57-7-1 FIG. 4 ITEM B. CLEANED, TREATED AND PRIMED AREA + NEW PLATING INTERNAL PART IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PAGE 9. INSTALLED NEW PLATING IAW SRM 51-1-21 PAGE 1, SRM 51-3-0 PAGE 1. TORQUED IAW SRM 51-3-1. 2L74 4F4 FRT4A25 E2GL 20050810002442005081000244WP 2005 8 10 AALA20050494 120050802A3233 ACTUATOR DOUG DC9 DC982 3022082WP INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 SW21410AA 49321 DFW - INFLIGHT UNABLE TO RETRACT NOSE GEAR. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. LUBED TRUNNION PIROTS. REPLACED BUNGEE OVER CENTER ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050810002452005081000245WP 2005 8 10 AALA20050495 120050803A3230 VALVE DOUG DC9 DC982 3022082WP INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21410AA 49321 DFW - INFLIGHT NOSE LANDING GEAR DID NOT RETRACT AFTER TAKEOFF. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR CONTROL VALVE AND ACCOMPLISHED NOSE GEAR STRUT REPACK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050810002542005081000254NM 2005 8 10 AWXA200500920 120050717A5753BACB30NR6K BOLT BOEING737 7373S3 1384711NM ZONE 500 - LEFT CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 MCN - DURING C18 CHECK DISCOVERED CORROSION ON RETAINING BOLTS FOR THE LT INBOARD MID FLAP GIMBAL SUPPORT. NO CORROSION REMOVAL LIMITS AVAILABLE FOR RETAINING BOLTS FOR THE LT INBOARD MID FLAP GIMBAL SUPPORT. MAINTENANCE REMOVED AND REPLACED BOLTS ON THE LT INBOARD MID FLAP INBOARD GIMBAL SUPPORT IAW AMERICA WEST AIRLINES TASK CARD I3L57057. ADDITIONAL BOLT WAS FOUND WITH CORROSIN THAT SHOULD HAVE BEEN INCLUDED IN THE ORIGINAL SDR. ADDED INFORMATION TO SDR. 2L72 4F RTA16WE 20050810002572005081000257NM 2005 8 10 AWXA200500923 120050724A5320654797322 WEB BOEING737 7373S3 1384711NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 DURING C18 CHECK DISCOVERED WEB CRACKED, 2.3 INCHES IN LENGTH, IN THE CABIN AREA AT BS 616, BL 60R, WL 208. MAINTENANCE REMOVED CRACKED WEB AT BS 616, BL 60R, WL 208 IAW BOEING 737-300 SRM 51-40-02-0 FIG 8. RECEIVED NEW WEB AND PREPARED FOR INSTALLATION IAW BOEING 737-300 SRM 51-40-02-0 FIG 1. INSTALLED REPAIR PARTS AT BS 616, BL 60R, WL 208 IAW BOEING 737-300 SRM 51-40-02-0 FIGS 8 AND 12. 2L72 4F RTA16WE 20050810002632005081000263NM 2005 8 10 AWXA200500929 120050718A5740656717217 FITTING BOEING737 7373S3 1384711NM ZONE 500 - LEFT CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 DURING C18 CHECK DISCOVERED CORROSION ON THE LT MLG STABILIZER BEAM, AFT ATTACH FITTING. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 57-20-30-1. MAINTENANCE REMOVED AND REPLACED THE AFT ATTACH FITTING ON THE LT MLG STABILIZER BEAM IAW BOEING 737-300 AMM 57-15-00-4. 2L72 4F RTA16WE 20050810002652005081000265NM 2005 8 10 AWXA200500931 120050731A5311654653932 FRAME BOEING737 7373S3 1384711NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 DURING C18 CHECK, FOUND FUSELAGE FRAME CRACKED, .50 INCHES IN LENGTH, AT BS 616, BL 65R BELOW STRINGER 17, CABIN AREA. MAINTENANCE REMOVED CRACK FROM INNER CHORD FRAME AT BS 616, BL 65R BELOW STRINGER 17, CABIN AREA IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5311-01143-DD1. FABRICATED STIFFENING ANGLE AND FILLER IAW AWA ER 03-5311-01143-DD1. INSTALLED FABRICATED REPAIR PARTS IAW AWA ER 03-5311-01143-DD1. 2L72 4F RTA16WE 20050810002682005081000268WP 2005 8 10 AALA20050510 120050808A3397 WIRE DOUG DC9 DC982 3022082WP CABIN BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21296AA 49308 DTW - EMERGENCY LIGHTS ON SEAT 21DEF INOPERATIVE. REPAIRED BROKEN WIRE UNDER SEAT FOR EMERGENCY LIGHTS ON SEAT 21DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050810002932005081000293SO 2005 8 10 SIMA200520901 120050723A3241742093 BRAKE ASSY EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL LOWER FUSELAGE FAILED A SIMAO OTHER O OTHER LDLANDING 1 SW21847AE 145707 DURING LANDING, ANTI SKID CYCLED ABNORMALLY. AIRCRAFT WOULD NOT STOP IN NORMAL DISTANCES. REPLACED BRAKE CONTROL UNIT. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (K) 2L72 4F4 FRTT00011ATTE6CH 20050810002972005081000297WP 2005 8 10 AALA20050507 120050807A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217533A 49987 SAT - AFT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK ON OVERHEAD BIN AFT SECTION FOR AFT OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050810003072005081000307NM 2005 8 10 DHL2005746527 120050712A5311 GUSSET BOEING727 727224 1384076NM FRAME CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01746DH 22252 BS 825 FRAME GUSSET ON RT SIDE I/B AT EDGE IS CRACKED. REMOVED GUSSET ON BS 825 FRAME ON RT SIDE I/B IAW B727 SRM 51-30-2. FABBED GUSSET FROM 7075 T6 .090 SIZE 4.3"X5.6" PO 9001777 IAW B727 S/B 53-0197 SRM 51-10-2. INSTALLED GUSSET IAW B727 S/B 53-0197 REV 1 FIG 11. 2L73 4F A3WE 20050810003082005081000308NM 2005 8 10 DHL2005746526 120050712A5320 STIFFENER BOEING727 727224 1384076NM CARGO BAY CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01746DH 22252 C-CHECK LOWER CARGO COMPT BS 1183 VERTICAL STIFFENER RBL 7.6 SHOWS CRACK FROM LOWER END IS ABOUT 3 INCHES LONG (NDT VERIFIED). REMOVED FASTENERS FOR ACCESS IAW S/B 727-53-0175. STOP DRILLED CRACK IAW B727 SRM 51-10-1. HFEC VERIFIED STOP DRILL IAW B727 NDT MANUAL PT6 51-00-00 FIG 23. LOCATED & DRILLED PARTS P/N 65C29080 -3 PO 522887 (ANGLE) P/N 65C29080-5 PO 522887 (ANGLE) P/N 65C29080-8 PO 5228138 (RADUIS FILLER) P/N 65C29080-7 PO 5228102 (RADUIS FILLER) IAW SB 727-53-0175. TREATED AND PRIMED PARTS & WORK AREA IAW B727 SRM 51-10-2. INSTALLED PARTS IAW SB 727-53-0175 REV 3 FIG 3. 2L73 4F A3WE 20050810003102005081000310EU 2005 8 10 AWXA200500938 120050713A5320D53470489000 WEB AIRBUS320 A320231 3930325EU CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28627AW 66 DURING C4 CHECK DISCOVERED CORROSION ON FLANGE OF WEB LOCATED IN THE AFT CARGO COMPARTMENT BETWEEN FS 56 AND FS 57, Y700. NO ALLOWABLE DAMAGE LIMITS FOUND IN THE AIRBUS SRM. MAINTENANCE REMOVED WEB IN THE AFT CARGO COMPARTMENT BETWEEN FS 56 AND FS 57, Y700 IAW SRM. INSTALLED NEW WEB AND FASTENERS IN THE AFT CARGO COMPARTMENT BETWEEN FR56 AND FR57, Y700 IAW AIRBUS 320 SRM 51-42-11. 2L72 4F RTA28NM 20050810003282005081000328WP 2005 8 10 ASAA0580355 120050621A575359304943 VANE DOUG DC9 DC983 3022083WP TE FLAP PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - DURING HV-CHECK, FOUND LEFT INBOARD FLAP INBOARD FLAP VANE PUNCTURED AND DELAMINATED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER AND FILLER. (M) 2L72 4F RTA6WE 20050810003302005081000330WP 2005 8 10 ASAA0580312 120050613A532199365465 FLOOR PANEL DOUG DC9 DC983 3022083WP FS 160-200 DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050810003352005081000335WP 2005 8 10 ASAA0580260 120050515A5320993607314 SPLICE DOUG DC9 DC983 3022083WP FS 1155 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - DURING C-CHECK, FOUND STATION 1155 FRAME SPLICE STRAP IS CORRODED. REMOVED AND REPLACED STRAP. (M) 2L72 4F RTA6WE 20050810003412005081000341WP 2005 8 10 ASAA0580308 120050613A5321993653915 FLOOR PANEL DOUG DC9 DC983 3022083WP FS 148-160 DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050810003552005081000355WP 2005 8 10 ASAA0580285 120050516A532199579181 FLOORBOARD DOUG DC9 DC983 3022083WP FS 693-617 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02968AS 53016 OKC - DURING HV CHECK, FOUND FLOOR PANEL E-8 IS MISSING SPACER IN SUPPORT. REMOVED DAMAGED SECTION OF HAT CHANNEL DUE CRACK. INSTALLED REPLACEMENT HAT CHANNEL SECTION AND SPLICE. (M) 2L72 4F RTA6WE 20050810003662005081000366NM 2005 8 10 DHL2005746520 120050705A5311 FRAME BOEING727 727224 1384076NM BS 700 DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01746DH 22252 FRAME DENTED AT BS 700 STR 24R. REMOVED NESSARY FASTENERS IAW B727 SRM 51-30-2. REMOVED DAMAGED SEC FROM FRAME AT BS 700 STR 24R IAW B727 SRM 51-40-3 FIG 1, 51-30-2 FABBED DOUBLER FROM 7075 T6 .063 PO 900226 10" X 3.5" X .75" DRILLED, DEBURRED, TREATED & PRIMED AFFECTED AREA DOUBLER IAW B727 SRM 51-40-3 FIG 1, 51-10-2. INSTALLED DOUBLER IAW B727 SRM 51-30-2 51-40-3 FIG 1. 2L73 4F A3WE 20050811000032005081100003NM 2005 8 11 UPS05445142 120050726A5310 DOUBLER BOEING747 747121 1384871NM M/D CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE:C M/D BS 1980-2000 S20-22L WINDOW FORGING MATTING SURFACE SKIN FOUND CORROSION DUE FORGING REMOVED. CORROSION BLEND OUT 0.022" X 1.5" X 3" EXCEED SRM 53-30-01 FIG 1 LIMITS. M/D BS 1983 LT WINDOW CUTOUT DOUBLER CORROSION REPAIRED AS PER HX RS R53-61-35356 & UPS ENGINEERING FILE 747-53-20276. 2L74 4F A20WE 20050811000042005081100004NM 2005 8 11 UPS05445143 120050724A575365B020984 STRUCTURE BOEING747 747121 1384871NM RT WING TE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE:C RIGHT WING I/B MID FLAP T/E WEB UPPER CHORD CORROSION REVEALED AT 73" - 78" AS MARKED (COUNT FROM I/B). CORROSION BLEND OUT 0.083" X 3/4" X 3" EXCEED SRM 57-50-01 FIG 3 LIMITS. CHORD REPAIRED AS PER HX RS R57-55-35354 & UPS ENGINEERING FILE 747-57-20081. 2L74 4F A20WE 20050811000142005081100014WP 2005 8 11 05FDEA02368 120050809A5730 ACCESS PANEL DOUG MD10 MD1010F 3022112WP ZONE 500 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25564FE 46984 LEFT WING ACCESS PANEL SLAT DRIVE MECHANISM LOWER EXTERNAL L/E XOS 487 EXISTING EXTERNAL REPAIR DOUBLER ON SKIN. REPAIR PER SRM 57-10-00 FIG 68 VOL 1. 2L73 4F RTA22WE 20050811000162005081100016WP 2005 8 11 05FDEA02339 120050809A5730 SKIN DOUG MD10 MD1010F 3022112WP RT WING DAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25564FE 46984 RIGHT WING XORS 506 L/E TRACK NR 8 EXISTING 1EA EXT REPAIR DOUBLER ON SKIN. REPLACED REPAIR PER SRM 57-10-00 FIG 68 SHT 1-3 VOL 1. 2L73 4F RTA22WE 20050811000292005081100029EU 2005 8 11 08012005A 120050801A2711 SWITCH SAAB SF340 340B 7860101EU ROLL TRIM FAILED A NSVAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 EA27305CE 202 MAIN ROLL TRIM INOP BOTTOM HALF OF SWITCH WON'T OPERATE TOWARD DOWN POSITION. PERFORMED OPERATIONAL CHECK, OPS CHECK GOOD. 2L72 4T RTA52EU 20050811000322005081100032WP 2005 8 11 05FDEA02370 120050809A5710991960443 SHEAR TIE DOUG MD10 MD1010F 3022112WP ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25564FE 46984 RT WING XORS 130 ABOVE STR 36 BEHIND A LOWER PIPE SUPPORT BRACKET THE BULKHEAD WEB HAS A 1.250" CRACK LONG. REPAIR IAW SRM 57-00-01 FIG 12 SHT 4 VOL 1. 2L73 4F RTA22WE 20050811000352005081100035WP 2005 8 11 05FDEA02353 120050809A5320 CHANNEL DOUG MD10 MD1010F 3022112WP ZONE 100 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25564FE 46984 FWD CARGO COMPT LT SIDE ON CHANNEL AT STA 999 , X=28, Z=-100 FOUND 1EA SPLICE REPAIR. REPAIR PER SRM 53-70-00 FIG 7 SHEET 3, 6 VOL 1. 2L73 4F RTA22WE 20050811000392005081100039CE 2005 8 11 DXTA200500869 120050722A3230 LANDING GEAR CESSNA560 560XL 2076702CE INTERMITTENT E DXTAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 GL07601QS 5605301 LANDING GEAR FAILED TO RETRACT ON T/O. HANDLE WAS DIFFICULT TO MOVE OUT OF DOWN POSITION; THEN, WHEN ABLE TO MOVE IT UP, NOSE GEAR GREEN LIGHT REMAINED ON WITH MAIN GEAR GREEN LIGHTS OFF AND INTRANSIT LIGHT ON. SELECTED DOWN POSITION AND GOT NORMAL INDICATION. PERFORMED SEVERAL GEAR SWINGS AND FOUND ALL LANDING GEAR OPERATIONS AND INDICATIONS TO BE NORMAL WORK PERFORMED IAW CE560XL MM 32-30-00. 2L72 4F RTA22CE 20050811000422005081100042CE 2005 8 11 DXTA200500880 120050803A2120 ODOR CESSNA750 750 2076810CE COCKPIT DETECTED E DXTAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 GL07956QS 7500156 OILY SMELL COMING FROM COCKPIT PAC, MORE SO DURING DESCENT. IT GOT SO BAD, SHUT OFF THE COCKPIT PAC DURING DESCENT INTO SFO, AND THE SMELL WENT AWAY. 2L72 4J RTT00007WI 20050811000522005081100052WP 2005 8 11 05FDEA02372 120050809A5330 SKIN DOUG MD10 MD1010F 3022112WP FUSELAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25571FE 47830 DURING AIRPLANE'S CONVERSION FROM P TO F FOUND ON EXTERNAL SKIN AT STA 1119 STR 40 LT, BULGING WITH HEAD FASTENER BROKEN AND CRACK ON SKIN; ON STR 38 ONE FASTENER WITH HEAD BROKEN. ON STR 38, REPLACE FASTENERS PER SRM 51-35-01 PG 1-12; ON STR 40 REPAIR SKIN PER SRM 53-20-00 FIG 6 SHEET 3. 2L73 4F RTA22WE 20050811000532005081100053NM 2005 8 11 05FDEA02373 120050809A5313 STRINGER BOEING727 727227 1384078NM CARGO BAY DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 FORWARD CARGO BAY, FRAME IS DENTED AT BS 500 BETWEEN STRINGER LT 26 AND LT 23. REPAIRED FWD CARGO BAY FRAME PER SRM 51-40-3. 2L73 4F A3WE 20050811000562005081100056EU 2005 8 11 BA05017 120050809A3350321431 BATTERY AIRBUS330 A330323 3930335EU PASSENGER CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19674UW 341 PHL - THE EMERGENCY POWER SUPPLY UNIT AT DOOR 4L FAILED THE SYSTEM TEST. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT BATTERY AT DOOR 4L. SYSTEM OPERATIONALLY CHECKS OK. 2L72 4F RTA46NM 20050811000612005081100061CE 2005 8 11 DXTA200500877 120050731A2720 YAW DAMPER CESSNA750 750 2076810CE MALFUNCTIONED E DXTAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 GL07912QS 7500012 IN FLIGHT YAW DAMPER DOES NOT APPEAR TO OPERATE IN COORDINATION WITH FLIGHT CONTROLS. LAGS AND OVERCORRECTS. SEVERAL TIMES IN FLIGHT, BOTH ON AUTO-PILOT AND WHEN HAND FLOWN, YAW DAMPER APPEARS TO OPERATE UNCOMMANDED. OVERCOMPENSATING APPEARS WORSE ON B FGC. RUDDER TRIM INDICATOR ALMOST OUT OF TAKEOFF SCALE TO THE LEFT IN COORDINATED LEVEL FLIGHT. AMBER CAS MESSAGE RETRIM WING DOWN TWICE. 2L72 4J RTT00007WI 20050811000652005081100065EU 2005 8 11 05FDEA02331 120050808A5321 FLOOR PANEL AIRBUS300 A300B4605R 3930308EU MDC DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25670FE 777 MDC FLOOR PNL 242CF IS DAMAGED. 2L72 4F RTA35EU 20050811000662005081100066NM 2005 8 11 05FDEA02332 120050809A5313 STRINGER BOEING727 727227 1384078NM CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 STRINGER 28R IS CORRODED AT STA 480. REMOVED AND REPLACED STRINGER SPLICE AT STA 480 STRINGER 28R IAW SRM 53-10-3 FIG 1. 2L73 4F A3WE 20050811000702005081100070EA 2005 8 11 ASOA05621 120050722A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27833AS 7246 DURING A C-CHECK, THE LT OB AND RT IB FS 280 CLIPS WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LT OB AND RT IB FS 280 CLIPS IAW SRM. (K) 2L72 4F4 FRTA21EA E15NE 20050811000782005081100078WP 2005 8 11 ASAA0580314 120050613A5320 FLOOR SUPPORT DOUG DC9 DC983 3022083WP CABIN CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - FOUND DURING HV-CHECK, CABIN FLOOR PANEL SUPPORT CORRODED. REPLACED FLOOR PANEL SUPPORT. (M) 2L72 4F RTA6WE 20050811000802005081100080WP 2005 8 11 ASAA0580332 120050613A5313591143289 LONGERON DOUG DC9 DC983 3022083WP FS 1429-1430 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - FOUND DURING HV CHECK, LONGERON 2R CRACKED. REPLACED DAMAGED SECTION OF LONGERON. (M) 2L72 4F RTA6WE 20050811000832005081100083WP 2005 8 11 ASAA0580330 120050613A5322991960383 SHEAR TIE DOUG DC9 DC983 3022083WP FS 1231 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - FOUND DURING HV CHECK, AFT CARGO BAY SHEAR TIE CORRODED. REPLACED DAMAGED SHEAR TIE. (M) 2L72 4F RTA6WE 20050811000842005081100084WP 2005 8 11 ASAA0580335 120050613A5322993607317 SHEAR TIE DOUG DC9 DC983 3022083WP FS 1212 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - DURING HV CHECK, FOUND SHEAR TIE CORRODED. REPLACED DAMAGED SHEAR TIE. (M) 2L72 4F RTA6WE 20050811000982005081100098EA 2005 8 11 A6WA200540274 120050716A5340601R3111357 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FS 280 CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31420AW 7640 FS 280, LBL 9, IB ATTACH CLIP CRACKED. REPLACED ANGLE IAW SRM AND EO. (K) 2L72 4F4 FRTA21EA E15NE 20050811001102005081100110EA 2005 8 11 ASOA05622 120050722A3350BF60390901 LENS CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE GALLEY CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27833AS 7246 DURING C-CHECK, THE EMERGENCY EXIT LIGHT LENS COVER ABOVE THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT LENS COVER ABOVE THE SERVICE DOOR. (K) 2L72 4F4 FRTA21EA E15NE 20050811001142005081100114EA 2005 8 11 ASOA05629 120050724A5312 PRESSURE PANEL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27833AS 7246 DURING A C-CHECK, CORROSION WAS FOUND BEYOND LIMITS ON THE PRESSURE FLOOR SKIN RT SIDE BETWEEN 409 AND 128 TO 559 RBL 36 AND 45. MAINTENANCE HAS SUBMITTED A DAMAGE REPORT AND IS AWAITING REO FOR REPAIR. THIS MRR WILL REMAIN OPEN UNTIL THE PROPER DOCUMENTATION IS OBTAINED AND THE REPAIR CAN BE COMPLIED WITH. (K) 2L72 4F4 FRTA21EA E15NE 20050811001182005081100118WP 2005 8 11 UPS05845125 120050711A5310 STRUCTURE DOUG DC8 DC873F 302199FWP DPIT DOOR JAMB ELONGATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE: C1, D-PIT DOOR AFT WEB HAS SEVERAL ELONGATED HOLES AND LITE CORROSION AROUND FASTENER. REMOVED DAMAGED WEB IAW SRM 51-1-21, FABRICATED DOOR JAMB SKIN AND WEB IAW DWG 5616674 AND SRM 51-1-21 AND INSTALLED JAMB SKIN AND WEB IAW DWG 5616674 AND SRM 53-2-0. 2L74 4F RT4A25 20050811001292005081100129EU 2005 8 11 UPS05145124 120050806A3350 LIGHT AIRBUSA300 A300F4622R 3930360EU EXIT DOOR INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01130UP 0814 INSPECTION TYPE:N/A EMERGENCY EXIT DISARM LIGHT BLOWN OUT. RELAMPED, OPS CHECK GOOD. 2L72 4F RTA35EU 20050811001312005081100131NM 2005 8 11 UPS05445093 120050725A5315 FLOORBEAM BOEING747 747121 1384871NM U/D CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE:C U/D BS 360 FLOORBEAM UPPER CHORD HORIZONTAL AFT FLANGE 1EA MOUNTING HOLE CRACK AT LBL 46" (CRACK LENGTH 1/16"). U/D BS 360 LBL 21" TO LT O/B END AREA FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 53-10-07 FIG 23. 2L74 4F A20WE 20050811001372005081100137NE 2005 8 11 AWXA200500939 220050809A7200 ENGINE BOEING757 7572S7 1384962NM RROYCERB211 RB211535E4 54555NE LEFT SURGES A AWXAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 WP28904AW 23566 DURING CLIMB, LT ENG SURGED. A/C DIVERTED. LANDED WITHOUT INCIDENT. SEVERAL COMPONETS CHANGED INCLUDING NR 1 EEC, BVCU, AND SEVERAL OPERATIONAL TESTS PREFORMED. DISCOVERED TUBE MISSING FROM PF RAKE ON THE NR 1 ENGINE. A/C FERRIED FOR REPAIR. R & R PF RAKE ON NR 1 ENG. OPS TEST GOOD. COULD NOT CONFIRM FAILURE OF ESC. UNIT TESTED ONLY & PASSED ALL TESTS IAW CMM. NO FAULTS FOUND. BLEED VALVE CONTROLLER FAILED INCOMING TESTS. FOUND H1 FAULTY ON SIGNAL PROCESSOR BOARD. ALSO FOUND FATIGUED JOINTS ON TR4 & TR9 ON PUS2 BOARD. H1 PROCESSOR BOARD REPLACED & UNITED REPAIRED. UNIT PASSED OPS CHKS. ALL WORK ACCOMPLISHED IAW CMM. 2L72 4F4 FRTA2NM E12EU 20050811001392005081100139NM 2005 8 11 AWXA200500941 120050715A53206545833151 ANGLE BOEING737 7373S3 1384711NM CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 DURING C18 CHECK DISCOVERED CORROSION ON FLOOR WEB ANGLE AT BS 270, FROM BL8L TO BL8R. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-10-51-1 FIG 101. MAINTENANCE REMOVED DAMAGED SECTION ON ANGLE AT BS 270, BL8L TO BL8R IAW BOEING 737-300 SRM 51-70-11-0. FABRICATED REPLACEMENT ANGLE, REPAIR ANGLE AND FILLER IAW BOEING 737-300 SRM 53-10-51-0 FIG 1, 51-70-11-0 FIG 1, AND BOEING DWG 65-45833. INSTALLED FABRICATED REPAIR PARTS IAW BOEING 737-300 SRM 51-70-11-0 FIG 1. 2L72 4F RTA16WE 20050811001402005081100140NM 2005 8 11 UPS05445140 120050723A531165B04346168 FRAME BOEING747 747121 1384871NM M/D CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 BS 2180 STR 25R STRINGER AREA FRAME FOUND CRACK, CRACK LENGTH 0.75" AND 0.5". BS 2180 STR 23R TO STR 26R FRAME REPAIRED AS PER HX RS NR R53-62-35345 AND UPS EO NR B747-5310-22631-A. 2L74 4F A20WE 20050811001412005081100141NM 2005 8 11 QXEA200501163 120050809A6123 AUTOFEATHER SYS BOMBDRDHC8 DHC8402 1390042NM UNKNOWN A QXEADC RETURN TO BLOCK ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM09405QX 4047 GEG FLIGHT NR 2439: TAKEOFF ABORTED AT 60 KNOTS DUE TO AUTO FEATHER NOT ARMING. MAINTENANCE COMPLIED WITH FIM TASK 61-20-09-810-806. CLEARED FAULT. COMPLIED WITH OPS CHECK. NO DEFECTS NOTED AND NO COMPONENTS WERE CHANGED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050811001422005081100142 2005 8 11 CHQA200500139 420050809A23127510700766 RADIO EMB 145 EMB145LR 3260212SO COCKPIT VHF COMMINOPERATIVE A CHQAK NONE B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 GL11280SK118989077 145381 FLIGHT 3143 - GSP-LGA - DURING DESCENT, AN ODOR SIMILAR TO ELECTRICAL BURNING WAS NOTICED FOLLOWED BY COM 1 FAILING. REMOVED AND REPLACED THE NR 1 INTEGRATED COM UNIT IAW EMB 145 AMM 23-00-01. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050811001452005081100145CE 2005 8 11 DXTA200500888 120050809A2780 SLAT CESSNA750 750 2076810CE INOPERATIVE E DXTAO OTHER S AFFECT SYSTEMS APAPPROACH 1 GL07921QS 7500241 GOT "FLAP FAIL" AMBER EICAS MESSAGE DURING APPROACH. FOLLOWED CHECKLIST BUT COULDN'T CLEAR. GOT SLATS AND NO FLAPS. 2L72 4J RTT00007WI 20050811001462005081100146CE 2005 8 11 DXTA200500889 120050806A3210 LANDING GEAR CESSNA750 750 2076810CE UNSECURE E DXTAO OTHER E VIBRATION/BUFFET CLCLIMB 1 GL07984QS 7500084 GEAR BUMP WAS EXPERIENCED NUMEROUS TIMES DURING CLIMB TO CRUISE ALTITUDE AND OCCASIONALLY ON DESCENT; NOT AT ALL DURING CRUISE FLIGHT. ACCOMPLISHED "GEAR BUMP" TROUBLESHOOTING IAW 750 TEAM X ENGINEERING CHECKLIST. NO DEFECTS NOTED. SERVICED NLG STRUT IAW CE 750 TEM X ENGINEERING CHECKLIST, 750MM 12-10-38 DMU INSTALLED AND WILL BE CHECKED ON OCF. 2L72 4J RTT00007WI 20050811001492005081100149CE 2005 8 11 DXTA200500891 120050808A2820661631155 PIPE CESSNA500 560CESSNA 2076750CE FUEL SYS CHAFED E DXTAK NONE O OTHER ININSP/MAINT 1 GL07825QS 5600655 PERFORM VISUAL INSPECTION OF THE RT LINE ASSY P/N 6516311-19 (REFUEL/DEFUEL FLOW) FOR SIGNS OF CHAFFING BY FLAP CROSS OVER CABLE BEHIND PANEL 172BB. (CHAPT. 6 ACCESS PLATES AND PANELS INDENTIFICATION. CE-560E MM 6-20-02 FIG 2 PG 12 OF 14). GAINED ACCESS FOR INSPECTION AND FOUND THAT SINGLE POINT FUEL LINE CHAFFED BEYOND LIMITS. 8/7 REMOVED FUEL LINE. 8/8 OK TO INSTALL NEW FUEL LINE 8/8 INSTALLED NEW FUEL LINE IAW 560 MM 20-10-13. 8/8 OK TO CLOSE AND SEAL ACCESS PANELS. 8/8 CLOSED ALL PANELS, SEALED OVERWING FILLET PANEL IAW 560 MM 20-32-00. 8/8 SEALANT NEEDS PAINT APPLIED TOUCH UP PAINT AS REQ. 8/8 LEAK CHECKED GOOD 8/8. 2L72 4F RTA22CE 20050811001542005081100154NM 2005 8 11 UPS05445090 120050725A5315 FLOORBEAM BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 BS 340 FLOORBEAM UPPER CHORD HORIZONTAL AFT FLANGE ONE MOUNTING HOLE CRACK, CRACK LENGTH 1/16. BS 240 LBL 8" TO LT O/B CORRODED FLOORBEAM REPAIRED AS PER SRM 53-10-07 FIG 23 REFER NRC NR 6532 FOR WORKING DETAIL. 2L74 4F RTA20WE 20050811001552005081100155NM 2005 8 11 UPS05445091 120050725A5315 FLOORBEAM BOEING747 747121 1384871NM U/D CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 BS 340 FLOORBEAM UPPER CHORD HORIZONTAL FWD FLANGE ONE MOUNTING HOLE CRACK, LENGTH 1/16". BS 340 LBL 8" TO LT O/B CORRODED FLOORBEAM REPAIRED AS PER SRM 53-10-07 FIG 23. 2L74 4F A20WE 20050811001562005081100156NM 2005 8 11 UPS05445092 120050725A5315 FLOORBEAM BOEING747 747121 1384871NM U/D CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 BS 360 FLOORBEAM UPPER CHORD HORIZONTAL FWD FLANGE ONE MOUNTING HOLE CRACK AT LBL 54, CRACK LENGTH 0.030". BS 360 LBL 21" TO LT O/B END AREA FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 53-10-07 FIG 23. 2L74 4F A20WE 20050811001572005081100157NM 2005 8 11 ASAA0580343 120050613A533059670412 SKIN DOUG MD80 MD83 3023681NM FS 1485-1497 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - DURING HV-CHECK, FUSELAGE SKIN DENTED. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RT 20050811001582005081100158NM 2005 8 11 ASAA0580342 120050613A5320993653473 TRACK DOUG MD80 MD83 3023681NM FS 148.5-200 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02981AS 53472 OKC - DURING HV CHECK, FOUND CABIN FLOOR FALSE TRACK CORRODED. REPLACED FLASE TRACK. (M) 2L72 4F RT 20050811001592005081100159NM 2005 8 11 USAA050895 120050718A534065B578392 MOUNT BOEING757 7572B7 1384964NM FS 324 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19628AU36199 27806 BFM - FOUND LAV MOUNT CORROSION 1.5 INCH BY .075 INCH BY .05 INCH, MAIN CABIN STATION 324 LBL 12. REMOVED AND REPLACED WITH NEW PART PER SRM 53-00-51, 51-40-02. (M) 2L72 4F RTA2NM 20050811001632005081100163NM 2005 8 11 USAA050894 120050718A5340415N400217 SUPPORT BOEING757 7572B7 1384964NM FS 368 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19628AU36199 27806 PIT - FOUND GAL SUPPORT FITTING CORRODED 2 INCH BY .75 INCH BY .03 INCH, MAIN CABIN STATION 368 RBL 12. REMOVED AND REPLACED WITH NEW PART PER SRM 53-00-51, 51-40-02. (M) 2L72 4F RTA2NM 20050811001642005081100164EA 2005 8 11 ASOA05635 120050725A5210601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PASSENGER DOOR SEPARATED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27834AS 7254 DURING A GROUND INSPECTION, THE PASSENGER DOOR BOTTOM STEP WAS FOUND TO HAVE A BROKEN ATTACH BRACKET. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050811001692005081100169EA 2005 8 11 ASOA05633 120050725A33508GH00247308 LAMP CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE EMERGENCY LIGHT BURNED OUT A ASOAO OTHER O OTHER NRNOT REPORTED 1 SO27748EV 396497 10158 DURING MAINTENANCE, THE LEFT EXTERIOR EMERGENCY LIGHT NEAREST THE OVERWING EMERGENCY EXIT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT EXTERIOR EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA EOOO63EN 20050811001702005081100170WP 2005 8 11 UPS05845114 120050710A5340 FITTING DOUG DC8 DC873F 302199FWP FS1738 L18R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE:C1 RIGHT AFT MAIN CABIN FS 1738 LONG 18R UPPER FLANGE TO LONG FITTING CRACKED .250" LONG. REMOVED LONGERON SPLICE FITTING IAW SRM 53-2-2 FIG 10. FABRICATED 2EA REPAIR SPLICES AND LONGERON SECTION AND INSTALLED REPAIR PARTS IAW SRM 53-2-2 FIG 10, 53-02-02 FIG 010. 2L74 4F RT4A25 20050811001712005081100171WP 2005 8 11 UPS05845115 120050713A5340 FITTING DOUG DC8 DC873F 302199FWP FS1200 L33R-L34RCRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE:C1 BATHTUB FITTING CRACKED AT C-PIT DOOR JAMB STA 1200 L33R-L34R. REMOVED AND REPLACED BATHTUB FITTING IAW SRM 53-2-0 AND SRM 53-2-0 FIG 02G. 2L74 4F RT4A25 20050811001732005081100173WP 2005 8 11 UPS05845117 120050709A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP FS 55 BL 0 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE:C1 FLOORBEAM CORRODED AT STA 55 BL 0, FWD SIDE, SEEN FROM A/C COMPARTMENT. REMOVED CORROSION IAW SRM 51-2-1 FIG 1 SHEET 7. FABRICATED REPAIR ANGLE DOUBLER AND FILLER IAW SRM 53-07-03 FIG 006A, AND 51-02-00-0 FIG 050. INSTALLED FILLER AND ANGLE DOUBLER IAW SRM 51-1-20D AND 51-1-15. 2L74 4F RT4A25 20050811001742005081100174WP 2005 8 11 UPS05845118 120050707A534056410072 FITTING DOUG DC8 DC873F 302199FWP FS 781 L18R-19R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE:C1 STA 781 BETWEEN LONG 19R AND 18R BOOT FITTING IS CRACKED. REMOVED AND REPLACED FUSELAGE FWD CENTER SPAR FRAME FITTING (BOOT FITTING) AT STA 781 LONG 19R AND 18R IAW SAA SK 807-858138 AND UPS EO DC8-53-20482. 2L74 4F RT4A25 20050811001752005081100175WP 2005 8 11 UPS05845119 120050710A5313 LONGERON DOUG DC8 DC873F 302199FWP FS 1730 L15R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE:C1 RIGHT AFT MAIN CABIN FS 1730 LONG 15R CRACKED LWR SIDE AT RADIUS .500" LONG. REMOVED DAMAGED AREA AT STA 1730 L15R IAW SRM 53-2-2 FIG 10. FABRICATED AND INSTALLED LONGERON SECTION AND SPLICE FITTING AT FS 1730 L15R IAW SRM 53-02-02 FIG 10 AND SRM 53-2-2 FIG 1D. 2L74 4F RT4A25 20050811001762005081100176WP 2005 8 11 UPS05845120 120050713A53303750257U1 FITTING DOUG DC8 DC873F 302199FWP FS 1040 L31R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE:C1 LONG 31R SPLICE FITTING CRACKED FROM 1040-1060. REMOVED AND REPLACED LONG SPLICE FITTING IAW SRM 53-1-0 AND 51-1-20 AT STA 1040-1060 LONG 31R. 2L74 4F RT4A25 20050811001772005081100177WP 2005 8 11 UPS05845121 120050716A5330561537271N SKIN DOUG DC8 DC873F 302199FWP FS1395-1445 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE:C1 UPON REMOVAL OF D-PIT SCUFF PLATE TO FOM FOR NDT INSPECTION TO COMPLY WITH EO DC8-5330-20206 FOUND CORROSION ON FUSELAGE SKIN FS 1395 TO 1445 L34R-L32R. REMOVED AND REPLACED FUSELAGE SKIN AT STA 1395-1445 L34R-L32R IAW SRM 51-1-21, 51-1-20D AND DWG 65615372. 2L74 4F RT4A25 20050811001792005081100179NM 2005 8 11 UPS05M45099 120050606A5320 FLOOR SUPPORT DOUG MD11 MD11F 3023600NM FWD CGO COMPT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01255UP 48404 INSPECTION TYPE:C-CHECK FWD CARGO COMPT AT STA 1119 RT FLOOR SUPPORT NEAR CENTERLINE FOUND WITH CORROSION AS MARKED. CORROSION REMOVED & TREATED AS PER SRM 51-21-01 VOL II REV 37 ON FWD CARGO AT STA 1119 RT FLOOR SUPPORT FOUND WITHIN LIMIT AS PER SRM 53-00-01 VOL 1 REV 37. 2L73 4F RTA22WE 20050811001812005081100181NM 2005 8 11 UPS05M45101 120050606A5320 FLOOR SUPPORT DOUG MD11 MD11F 3023600NM FWD CARGO COMPT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01255UP 48404 INSPECTION TYPE:C-CHECK FWD CARGO COMPT AT STA 6-73.5 RT FLOOR SUPPORT NEAR CENTERLINE FOUND WITH CORROSION AS MARKED. CORROSION REMOVED AND TREATED AS PER SRM 51-21-01 REV 37 FOUND WITHIN LIMIT AS PER SRM 53-00-01 VOL I REV 37. 2L73 4F RTA22WE 20050811001852005081100185NM 2005 8 11 UPS05M45105 120050608A5313 LONGERON DOUG MD11 MD11F 3023600NM CTR CGO COMPT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01255UP 48404 INSPECTION TYPE:C-CHECK CTR CARGO COMPT AT STA 1841 LONGERON 50 LT TO 50 RT TRANSVERSE AREA FOUND WITH CORROSION AS MARKED. CORROSION REMOVED AS PER SRM 53-30-00 VOL 1 FIG 7 REV 37 ON CTR CARGO A T STA 1841 LONGERON 50 LT TO 50 RT TRANSVERSE AREA AND FOUND WITHIN LIMIT AS PER SRM 53-00-01 VOL I REV 37 AND REPROTECTED AS PER SRM 51-21-01 VOL II REV 37. 2L73 4F RTA22WE 20050811001872005081100187NM 2005 8 11 UPS05M45107 120050609A5330 SKIN PANEL DOUG MD11 MD11F 3023600NM AFT CARGO COMPT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01255UP 48404 INSPECTION TYPE:C-CHECK AFT CARGO COMPT AT STA 1962 AFT TRANSVERSE TO SKIN PANEL CENTERLINE AREA FOUND WITH CORROSION AS MARKED. CORROSION REMOVED ON AFT CARGO AT STA 1962 AFT TRANSVERSE TO SKIN PANEL CENTERLINE AREA, FOUND WITHIN LIMIT AS PER SRM 53-30-00 VOL I REV 37 AND REWORKED AREA REPROTECTED AS PER SRM 51-21-01 VOL II REV 37. 2L73 4F RTA22WE 20050811001882005081100188NM 2005 8 11 UPS05M45108 120050609A5311 FRAME DOUG MD11 MD11F 3023600NM AFT WASTE TANK CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01255UP 48404 INSPECTION TYPE:C-CHECK AFT WASTE TANK COMPT AT STA 1997 FROM CENTERLINE TO X-6 INCHES FOUND WITH CORROSION ON AFT TRANSVERSE FRAME AS MARKED. CORROSION REMOVED ON AFT WASTE TANK AT STA 1997 FROM CENTERLINE TO X-6 INCHES AND FOUND WITHIN LIMIT AS PER SRM 53-30-00 VOL I FIG 7 REV 37 AND REWORKED AREA REPROTECTED AS PER SRM 51-21-01 VOL II REV 37. 2L73 4F RTA22WE 20050811001902005081100190NM 2005 8 11 UPS05M45110 120050613A5311 FRAME DOUG MD11 MD11F 3023600NM CAC COMPT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01255UP 48404 INSPECTION TYPE:C-CHECK CAC COMPT STA 6-70 LONG 52 CORROSION FOUND ON AFT OF FRAME AS MARKED. CORROSION REMOVED & TREATED AS PER SRM 51-21-01 VOL II REV 37, FOUND WITHIN LIMIT AS PER SRM 53-00-01 VOL II REV 37. 2L73 4F RTA22WE 20050811001912005081100191NM 2005 8 11 UPS05445133 120050723A531165B04346167 FRAME BOEING747 747121 1384871NM M/D CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE:C M/D BS 2180 BETWEEN S25-26L FRAME FOUND CRACK (CRACK LENGTH 1/2"). M/D BS 2180 BETWEEN STR 24L - 26L FRAME REPAIRED AS PER HX RS R53-62-35345 & UPS EO B747-5310-22631-A. 2L74 4F A20WE 20050811001942005081100194NM 2005 8 11 UPS05445136 120050722A531165B0173082 FRAME BOEING747 747121 1384871NM M/D CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE:C M/D BS 740 RT STR 25R FRAME FOUND CRACK (CRACK LENGTH 0.75"). M/D BS 740 STR 24R-26R FRAME REPAIRED AS PER HX RS R53-22-35340 & UPS EO B747-5310-22628-A. 2L74 4F A20WE 20050811002012005081100201WP 2005 8 11 IXXA05SMN113S 120050627A5730 SKIN DOUG DC8 DC871F 302199DWP XF 415.000 IMPROPER B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, LT IB FLAP REPAIR IMPROPER, XF 415.000 (UPPER PART) PERFORMED MAJOR REPAIR IAW SRM 57-2-5 FIG. 1. EO SEMAN NR 2005858 DATE 06-18-05. REMOVED DAMAGED PLATING IAW SRM 57-2-5 FIG. 1(SHEET 1,2). PERFORMED DETAILED VISUAL INSPECTION TO AREA, NO CRACK FOUND, NO CORROSION FOUND. FABRICATED NEW PLATING (ALCLAD 2024 T3 0.050”) + FILLER (ALCLAD 2024 T3 0.020”) IAW DC-8 SRM 57-2-5 FIG. 1 (SHEET 1,2), SRM 57-7-1 FIG. 4 ITEM Q AND U. CLEANED, TREATED AND PRIMED AREA + REPAIR PARTS INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PAGE 9. INSTALLED REPAIR PARTS IAW SRM 57-2-7 FIG. 1, SRM 51-1-21 PAGE 1, SRM 51-3-0 PAGE 1. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050811002022005081100202WP 2005 8 11 IXXA05SMN121S 120050629A5340 FITTING DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE 1766.000 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, AFT. ACCESSORY COMPARTMENT FITTING CRACKED L-28R, STA 1766.000 REMOVED CRACKED FITTING IAW SRM 51-1-20D PAGE 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PAGE 1. TORQUED IAW SRM 51-3-0. 2L74 4F4 FRT4A25 E2GL 20050811002032005081100203WP 2005 8 11 IXXA05SMN155S 120050706A5330 SKIN DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE STA665.000 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, MID ACCESSORY COMPARTMENT L-31R CORRODED, STA 665.000. PERFORMED MAJOR REPAIR IAW SRM 53-2-2 FIG. 11, EO SEMAN NR 20051003 DATE 06-27-05. REMOVED FASTENERS IAW SRM 51-1-20D PAGE 21. REMOVED CORROSION IAW SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PAGE 2P. FABRICATED REPAIR ANGLE DOUBLER (EXTRUSION 7075 T6 511 0.130”) IAW SRM 53-2-2 FIG. 11. CLEANED, TREATED AND PRIMED AREA + REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PAGE 9. INSTALLED REPAIR PARTS IAW SRM 53-2-2- FIG. 11 SHEET 3,4,5,6, SRM 51-1-20D PAGE 9. TORQUED IAW SRM 51-3-1. 2L74 4F4 FRT4A25 E2GL 20050811002052005081100205WP 2005 8 11 IXXA05SMN157S 120050706A5730 SKIN DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE XS250.000-240.00CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, LT WING. STUB WING UPPER SURFACE STA XS 250.000 XS 240.000 HAS TWO CRACKS OF .5 INCH. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG. 38, TR NR 57-85, EO SEMAN NR 2005983 DATE 06-18-05. REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1. TRIMMED OUT DAMAGED AREA IAW SRM 57-2-1 FIG. 38. PERFORMED VISUAL INSPECTION, NO CRACK, CORROSION FOUND. FABRICATED REPAIR DOUBLER (ALCLAD 7075 T6 0.071) + FILLER (ALCLAD 7075 T6 0.063) IAW SRM 57-2-1 FIG. 38, SRM 57-3-1 FIG. 3. CLEANED, TREATED AND PRIMED AREA AND REPAIR DOUBLER INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11. INSTALLED REPAIR PARTS IAW SRM 57-2-1 FIG. 38, SRM 51-3-0 PAGE 1, SRM 51-1-20D PAGE 9. TOR2L74 4F4 FRT4A25 E2GL 20050811002062005081100206WP 2005 8 11 IXXA05SMN127S 120050629A5340 FITTING DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE 1215.000 L-31L CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, AFT. LWR. CARGO BILGE INTERIOR. NR 3 DOOR HOUSING LWR FITTING CORRODED (INTERNAL STRUCTURE), STA. 1215.000, L-31LREMOVED CORROSION IAW SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PAGE 2P. REMOVED CORRODED FITTING IAW SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING IAW DWG DOUGLAS NR 3750248 (ALCLAD 7075 T6 51). PERFORMED HEAT TREATMENT IAW SRM 51-1-11 PAGES 1,13,17. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02 TO 07. NO CRACK, CORROSION FOUND. CLEANED, TREATED AND PRIMED AREA + NEW FITTING IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PAGE 9. TORQUED IAW SRM 51-3-1. 2L74 4F4 FRT4A25 E2GL 20050811002082005081100208WP 2005 8 11 IXXA05SMN123S 120050629A5340 FITTING DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE 1690.000 L-30L CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, AFT ACCESSORY COMPARTMENT BATHTUB FITTING CRACKED, STA 1690.000 L - 30L. REMOVED CRACKED BATHTUB FITTING IAW SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING (ALCLAD 7075 T6 51) IAW DWG 4641324. PERFORMED HEAT TREATMENT IAW SRM 51-1-1 PAGES 1,13,17. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02 TO 07. CLEANED, TREATED AND PRIMED AREA + NEW FITTING IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PAGE 9. TORQUED IAW SRM 51-3-1. 2L74 4F4 FRT4A25 E2GL 20050811002092005081100209WP 2005 8 11 IXXA05SMN124S 120050629A5340 FITTING DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE 1690.000 L-34R CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, AFT ACCESSORY COMPARTMENT BATHTUB FITTING CRACKED, STA 1690.000 L-34R. REMOVED CRACKED BATHTUB FITTING IAW SRM 51-1-20D PAGE 21. FABRICATED NEW BATHTUB FITTING (ALCLAD 7075 T6 51) IAW DWG 4641324. PERFORMED HEAT TREATMENT IAW SRM 51-1-1 PAGES 1,13,17. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02 TO 07. CLEANED, TREATED AND PRIMED AREA + NEW FITTING IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PAGE 9. TORQUED IAW SRM 51-3-1. 2L74 4F4 FRT4A25 E2GL 20050811002102005081100210WP 2005 8 11 IXXA05SMN125S 120050629A5313 LONGERON DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE 1690.000 L-34R CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, AFT ACCESSORY COMPARTMENT, L -34R CRACKED STA 1690.000. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PAGE 1, SRM 53-5-1 FIG. 7, EO SEMAN NR 2005863 DATE 06-18-05. REMOVED CRACKED LONGERON SEGMENT + EXISTING SPLICES IAW SRM 51-1-20D PAGE 21. CLEANED, TREATED AND PRIMED AREA + SPLICES IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PAGE 9. INSTALLED NEW LONGERON SEGMENT (PN 51415997) REINSTALLED SPLICES IAW SRM 53-5-1 FIG. 7 PAGE 22 ITEM A, SRM 51-1-20D PAGE 9. TORQUED IAW SRM 51-3-1. 2L74 4F4 FRT4A25 E2GL 20050811002122005081100212EU 2005 8 11 05FDEA02324 120050808A5230FXEA6523082117 FITTING AIRBUS330 A300* EU GE CF6 CF6* 30020GL CARGO DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25656FE 745 MDIS 656 52-30 0008568 03AUG05 BFM CLOSE R C/W EA 6-5230-82117 DOORS - MAIN CARGO DOOR BEARING FITTING CRACKED ENT BY: 575463 RPT BY: 575463 FACT 04AUG05 23:50 BFM R COMPLIED WITH EA 6-5230-82117 DOORS MAIN CARGO DOOR BEARING FITTING CRACKED. RII:497234 ENT BY: 573371 RPT BY: 573371. 2L72 4F4 FRTA26NM E23EA 20050811002152005081100215CE 2005 8 11 08082005F 120050806A2730130610000613 ELEVATOR BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA LOOSE A NSVAO OTHER F FLT CONT AFFECTED ININSP/MAINT 1 EA27243CJ UE43 LT ELEVATOR: OB BRACKET HAS 2 LOOSE RIVETS ON BOTTOM AND 1 AT AFT END WITH ELONGATED HOLE. 2L72 4T3 TRTA24CE E2NE 20050811002162005081100216GL 2005 8 11 EVCA105166 220050802A7200250C30P ENGINE BELL 206 206L1 1182107SW ALLSN 250C 250C28B 03013GL FUSELAGE TOP MAKING METAL E EVCAO OTHER O OTHER NRNOT REPORTED 1 CE0359AE 1875 45291 ENGINE CAUTION WARNING CHIP DETECTOR LIGHT ILLUMINATED IN FLIGHT. CHIP DETECTOR WAS REMOVED AND NO SIGNIFIGANT CHIP WAS FOUND. REINSERTED CHIP PLUG AND RAN AIRCRAFT LIGHT ILLUMINATED AGAIN. MINTENANCE FOUND EXTENSIVE METAL ON BOTH UPPER AND LOWER ENGINE CHIP DETECTORS. EXTERNAL ENGINE OIL FILTER SHOWED LARGE AMOUNT OF METAL. ENGINE REMOVED FOR REPAIR. 1G71 3U3 U H2SW E1GL 20050811002182005081100218SW 2005 8 11 ALGA105176 120050725A6220406310405101 PITCH LINK BELL 407 407 1182206SW ALLSN 250C 250C47B GL RATCHETING E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03477AL273 53203 RATCHETY AND ROUGH / REPLACER WITH NEW BY FIELD MAINTENANCE. 1G71 3U3 UO H2SW E1GL 20050811002202005081100220WP 2005 8 11 IXXA05SMN138S 120050630A5730 SKIN DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE XF415.000 IMPROPER A IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSP, RT OB FLAP FWD UPPER PLATING NON STANDARD REPAIR AT STA XF 415.000. PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PAGE 1, SRM 57-7-1 FIG. 4 TR NR 57-94, EO SEMAN NR 2005914 DATE 06-18-05. REMOVED DAMAGED PLATING IAW SRM 51-1-21 PAGE 1. FABRICATED NEW PLATING (ALCLAD 2024 T3 0.032”) IAW SRM 57-7-1 FIG. 4 ITEM P. CLEANED, TREATED AND PRIMED AREA AND NEW PLATING INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11. INSTALLED NEW PLATING IAW SRM 51-1-21 PAGE 1. 2L74 4F4 FRT4A25 E2GL 20050811002212005081100221WP 2005 8 11 IXXA05SMN139S 120050630A5330 DOUBLER DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE 35.000-70.000 CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, FUSELAGE EXTERIOR INTERNAL DOUBLER CORRODED , STA 35.000 - 70.000 BETWEEN L - 28 TO L 31. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PAGE 1, SRM 53-3-1 FIG. 1, EO SEMAN NR 2005877 DATE 06-22-05. REMOVED CORROSION IAW SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PAGE 2P. REMOVED CORRODED INTERNAL DOUBLER IAW SRM 51-1-21 PAGE 1. FABRICATED NEW INTERNAL DOUBLER (ALCLAD 7075 T6 0.025”) IAW SRM 53-3-1 FIG. 1 ITEM D. CLEANED, TREATED AND PRIMED AREA AND INTERNAL DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11. INSTALLED NEW INTERNAL DOUBLER IAW SRM 51-1-21 PAGE 1. 2L74 4F4 FRT4A25 E2GL 20050811002222005081100222WP 2005 8 11 IXXA05SMN136S 120050630A5730 SKIN DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE XF197.000-213.00DAMAGED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, RT OB FLAP FWD UPPER PLATING NON STANDARD REPAIRS (03 EA) AND WEAR DAMAGES BETWEEN STA XF 197.000 - XF 213.000PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PAGE 1, SRM 57-7-1 FIG. 4 TR NR 57-94, EO SEMAN NR 2005912 DATE 06-18-05. REMOVED DAMAGED PLATING WITH INTERIM REPAIR IAW SRM 51-1-21 PAGE 1. FABRICATED NEW PLATING (ALCLAD 2024 T3 0.040”) IAW SRM 57-7-1 FIG. 4 ITEM C. CLEANED, TREATED AND PRIMED AREA AND NEW PLATING INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11. INSTALLED NEW PLATING IAW SRM 51-1-21 PAGE 1, SRM 51-3-0 PAGE 1. TORQUED IAW SRM 51-3-1. 2L74 4F4 FRT4A25 E2GL 20050811002232005081100223WP 2005 8 11 IXXA05SMN140S 120050630A5730 SKIN DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE XFS51.250-57.500BROKEN A IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, LT WING IB L/E UPPER SURFACE BROKEN, STA XFS 51.250 - 57.500. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG. 25, EO SEMAN NR 2005908 DATE 06-15-05. REMOVED DAMAGED AREA IAW SRM 57-2-1 FIG. 21. PERFORMED NDT INSPECTION IAW NDT SPM PART 06-10-01-001. FABRICATED INTERNAL REPAIR DOUBLER (ALCLAD 2024 T3 0.090”) + FILLER (ALCLAD 2024 T3 0.063”) IAW SRM 57-2-1 FIG. 21. CLEANED, TREATED AND PRIMED AREA + REPAIR PARTS INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-12. INSTALLED REPAIR PARTS IAW SRM 57-2-1 PAGE 21, SRM 51-1-21 PAGE 1. 2L74 4F4 FRT4A25 E2GL 20050811002242005081100224SO 2005 8 11 1392080205 120050802A7732241273000011 MONITOR GULSTMG1159 GIV 3980115SO RROYCETAY TAYMK6118 NE LT ENGINE FAULTY E N93AA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO13492QS 1392 WHILE ENROUTE, LT ENGINE EXCEEDANCE CAS MESSAGE. DIVERTED TO HPN. TROUBLESHOT TO ENGINE VIBRATION MONITORING UNIT. 2L72 4F4 FRTA12EA A25NE 20050812000012005081200001NM 2005 8 12 SWAA052293 120050801A5753 SKIN BOEING737 7373A4 1384585NM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 1354 23251 DURING SCHEDULED C3 CHECK, FOUND RIGHT WING INBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED AFT FLAP PER MM. 2L72 4F RTA16WE 20050812000022005081200002WP 2005 8 12 UPS05845112 120050729A5230 FRAME DOUG DC8 DC873F 302199FWP MAIN CARGO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE:C1 WHILE ACCOMPLISHMENT OF MCD FWD HINGE REPLACEMENT AFTER REMOVAL OF THE ACTUATOR CLOSE OUT PNL FOUND A 1" CRACK ON THE FWD UPPER MAIN FRAME CRACK ON "Z" FRAME STOPPED AT EXISTING HOLE NDT HFEC CRACK TERMINATES AT EXISTING HOLE IAW NDTSPM06-10-01. FABRICATED REPAIR ANGLE AND DOUBLER IAW SRM 52-2-0 FIG 2 AND 51-3-0. 2L74 4F RT4A25 20050812000032005081200003SO 2005 8 12 C2XA05SH093 120050805A533014520170403 SKIN EMB 145 EMB145LR 3260212SO FUSELAGE DENTED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711536 145520 SHV - DURING C-CHECK MAINTENANCE FOUND RT EXTERNAL FUSELAGE HAS DENT AT FRAME 4, NEAR TOP FWD CORNER OF PANEL 114 CR. MAINTENANCE REPAIRED DENT IAW EC 5330-01488. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050812000052005081200005SO 2005 8 12 C2XA05SH095 120050807A532014532638401 FLOOR SUPPORT EMB 145 EMB145 3260210SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713958 145085 SHV - DURING C-CHECK MAINTENANCE FOUND CORROSION ON LT OMEGA BEAM AT FRAME 25- FRAME 29. MAINTENANCE REPAIRED LT OMEGA BEAM AT FRAME 29 IAW EMB 145 SRM 53-00-10, SECTION 3, FIGURE 202, SHEET 2. INSTALLED NUT PLATES IAW EC 5320-01137 & PAINTED REPAIR AREA IAW EC 5320-01140. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050812000072005081200007GL 2005 8 12 C2XA05BT055 220050808A7200AE3007A1E ENGINE EMB 145 EMB145XR 3260214SO ALLSN AE300 AE3007A GL NR 2 ODOR A C2XAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW27131236924 6924 145688 CAE312329 CREW REPORTED, SMOKE IN CABIN. TURNED OFF PACK NUMBER 2 AND SMOKE CLEARED. ERW MAINTENANCE TROUBLESHOT, DETERMINED ENGINE NR 1 CAUSING SMOKE IN CABIN. AIRCRAFT MAINTENANCE FERRIED TO BTV WITH NR 1 BLEED OFF. BTV MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE. OPS CHECKED AND LEAKED CHECKED GOOD. AIRCRAFT RELEASED FOR SERVICE IAW TASKCARD 6271001. 2L72 4F4 FRT TE6CH 20050812000102005081200010SO 2005 8 12 C2XA05CL061 120050809A521014531389401 ROD EMB 145 EMB145EP 3260221SO DOOR OUT OF ADJUST A C2XAK NONE O OTHER TXTAXI/GRND HDL 1 SW2713929 145009 CLE - THE CREW REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO CLOSE AND LATCH. MAINTENANCE INSPECTED AND ADJUSTED THE MAIN CABIN DOOR FOLDING FLAP RODS. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20050812000112005081200011SO 2005 8 12 C2XA05SH99 120050811A531514522215407 FLOORBEAM EMB 145 EMB145 3260210SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713958 145085 SHV - DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION AT FR 61. MAINTENANCE REPAIRED THE CENTER OMEGA BEAM AT FR 61 IAW EC 5320-01255. THE AIRCRAFT WAS APPROVED TO RETURNED FOR SERVICE. 2L72 4F RTT00011AT 20050812000122005081200012SO 2005 8 12 C2XA05SH100 120050511A531514521700007 FLOOR SUPPORT EMB 145 EMB145 3260210SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713958 145085 SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION BETWEEN FR 22-23. MAINTENANCE REPAIRED LT OMEGA BEAM BETWEEN FR 22-23 IAW EMB 145 SRM 53-21-10 SECTION 8 FIGURE 207. THE AIRCRAFT WAS APPROVED FOR RETURN FOR SERVICE. 2L72 4F RTT00011AT 20050812000132005081200013SO 2005 8 12 C2XA05SH101 120050511A532014521700007 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715527 145413 SHV - DURING C-CHECK CORROSION ON RT OMEGA BEAM AT FR 18. MAINTENANCE REPAIRED RT OMEGA BEAM AT FR 18 IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050812000162005081200016NE 2005 8 12 DHL2005801013 220050810A7200 ENGINE DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C1 13802NE NR 1 FAILED A DHLAO OTHER O OTHER APAPPROACH 1 SO01801DH 46033 ENGINE FAILURE NR 1. R&R NR 1 ENGINE DRIVEN FUEL PUMP IAW DC8 MM 73-10-1. NO LEAKS NOTED. OPS CKS GOOD ON ENGINE RUN IAW MM 71-00 & ASTAR JRH. PARTS INFO ON LP 056593. EVIDENCE OF CORROSION REPORTED IN AREA OF 3 REMOVED FASTENERS L WING STATION 519.00. REF. ITEM 1W LP063739; #4 ALT TANK PLATE 505B & BAFFLE (INNER) 560A REMOVED FOR ACCESS. OK TO INSTALL 560A BAFFEL NR 4 ALT TANK PLATE. INSTALLED 560A BAFFLE AND505B TANK PLATE IAW MM 78-10-0 LEAK CK OK INSTALLED 3 EA HI-LOCS IN NR 1 ALT TANK IAW MM CH 28 AND SRM CHAPTER 51-3-0 AT STRINGER 63 PER NAAS W/O 250713 FOUND CORROSION TO NEGILIBLE, BLENDED OUT AREA. NO SUFFICANT METAL REMOVED. WORK DONE IAW SRM 51-1-8C, BY NAAS PER NAAS W/O 250713. 2L74 4F4 FRT4A25 E2GL 20050812000192005081200019NM 2005 8 12 05FDEA02374 120050809A5754 SKIN DOUG MD11 MD11 3023602NM ZONE 600 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT WING, FIXED LEADING EDGE UPPER SURFACE FOUND CHAFED MARK AT OUTBOARD OF NR 19 SLAT TRACK. CHAFED MARKED REMOVED FOUND OUT OF LIMIT AS PER SRM 57-10-00 FIGURE 3 VOLUME I. REPAIR CARRIED OUT AT RIGHT HAND WING FIXED LEADING EDGE UPPER SURFACE AREA AT OUTBOARD OF NR 19 SLAT TRACK AS PER SRM 57-10-00 FIGURE 14 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050812000202005081200020NM 2005 8 12 05FDEA02375 120050809A5313 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 CENTER ACCESSORY COMPARTMENT LONGERON 51L, STA 1112 SUSPECTED CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. LONGERON FABRICATED AS PER DRAWING AAA7088 AND FEDEX EA 1-5310-89966. 2L73 4F RTA22WE 20050812000232005081200023WP 2005 8 12 05FDEA02377 120050806A3260 WARNING LIGHT DOUG DC10 DC1010F 3022111WP MLG FALSE ACTIVATIONA FDEAO OTHER J WARNING INDICATION CLCLIMB 1 SO25357FE 46939 UNSAFE GEAR-UP IND DURING GEAR RETRACT ON TAKEOFF. BOTH PRI AND SEC IND SHOWERED OR UNSAFE. LOWERED GEAR IAW RED-TAB PROC AND ALL IND GREEN. RAISED GEAR AGAIN AND GOT A GOOD GEAR UP IND. GEAR RETRACT SOUNDED NORM AND CAME UP AS USUAL BUT HANDLE MECH INSIDE OR BEHIND PANEL FEELS SLACK OR LOOSE. PERFORMED VISUAL CHK OF L/G CONTROL MECHANISM, NO FAULTS NOTED. OPERATED HANDLE THRU FULL MOTION, ALL GEAR LIGHTS OPERATED AS DESIGNED. PERFORMED INSPECT OF PROX SENSORS AND TARGETS (32-61-1 5-4) CHECKED NORMAL. INSPECTED GEAR AND DOORS FOR OBVIOUS IRREGS, NONE NOTED. NO FAULTS DISPLAYED FOR PREV FLIGHT OR CURRENT. PERFORMED PSEU RTS (31-71-01-2). (OPEN) 2L73 4F A22WE 20050812000242005081200024NM 2005 8 12 05FDEA02378 120050810A5314 KEELBEAM BOEING727 727227 1384078NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 AFT CARGO COMP KEEL BEAM HAS CORROSION ON OB FLANGE BS 950B-970 STR-29R. FABRICATED & INSTALLED REPAIR STRAP PER FED EX SR-27-53-023, REV. A., SR27-53-013A, SRM 53-10-4. 2L73 4F A3WE 20050812000262005081200026NM 2005 8 12 05FDEA02380 120050810A5311 FRAME BOEING727 727227 1384078NM CARGO BAY DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 FORWARD CARGO BAY, FRAME IS DENTED AT BS 580 BETWEEN STRINGER LT 24 AND LT 23. REPAIRED PER SRM 51-40-3. [CLOSED] 2L73 4F A3WE 20050815000012005081500001NM 2005 8 15 05FDEA02381 120050810A2750MS9391130ZE4C MOTOR BOEING727 727233 138408ANM TE FLAPS MALFUNCTIONED A FDEAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO25277FE4654 784 22042 O/B T/E FLAPS WOULD NOT POSITION WITH FLAP HANDLE. FLT CREW C/W QRH PROCEDURES AND HAVE A C/B PULLED. INSPECTED O/B FLAPS FOR POSSIBLE JAM AND NONE NOTED. WITH HYD ON, THE O/B FLAP CONTROL VALVE IS BYPASSING FLUID. REMOVED AND REPLACED O/B FLAP HYD MOTOR IN REF TO B-727-200 M/M 27-51-062-4. ALL OPS CHECKS GOOD AND NO LEAKS NOTED. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION OFF MFG MS9-3911-30ZE4C. 2L73 4F RTA3WE 20050815000042005081500004NM 2005 8 15 05FDEA02384 120050810A5230 FRAME BOEING727 727227 1384078NM CARGO DOOR PUNCTURED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 MAIN CARGO DOOR AFT SIDE FRAME PUNCTURED, 15" FROM LOWER CORNER. REPAIRED PER SRM 52-30-2. 2L73 4F A3WE 20050815000052005081500005NM 2005 8 15 05FDEA02385 120050810A5313 STRINGER BOEING727 727227 1384078NM CARGO BAY DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 FORWARD CARGO BAY, FRAME IS DENTED AT BS 600 BETWEEN STRINGER LT 24 AND LT 23. REPAIRED DENTED FRAME AT BS 600 STR 23LH TO 24LH IAW SRM 51-40-3. [CLOSED] 2L73 4F A3WE 20050815000062005081500006NM 2005 8 15 05FDEA02386 120050810A5313 STRINGER BOEING727 727227 1384078NM CARGO BAY DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 FORWARD CARGO BAY, FRAME IS DENTED AT BS 520 BETWEEN STRINGER LT 25 AND LT 22. REPAIRED FRAME AT FWD CARGO BAY BS 520 BETWEEN STR 25L & 22L IAW SRM 51-40-3, 51-10-2. 2L73 4F A3WE 20050815000072005081500007NM 2005 8 15 05FDEA02388 120050810A5754 RIB BOEING727 727227 1384078NM LT WING SLAT CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 LT WING NR 3 SLAT INTERNAL STRUCTURE AT O/B ACTUATOR MOUNTING SUPPORT RIB CRACKED. REMOVED AND REPLACED SUPPORT RIB IAW SRM 51-40-3 FIG 1. 2L73 4F A3WE 20050815000092005081500009NM 2005 8 15 05FDEA02390 120050811A5280 COVER DOUG MD11 MD11 3023602NM ZONE 700 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT MAIN LANDING GEAR DOOR, DURING REPLACE, FORWARD AND UPPER COVER ASSEMBLY FOUND EXTRA FASTENER HOLES ON THE DOOR OUTER SKIN. LEFT HAND MAIN LANDING GEAR DOOR OUTER SKIN EXTRA FASTENER HOLES AREA REPAIR CARRIED OUT AS PER SRM 52-00-01 FIGURE 7 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2 -100. 2L73 4F RTA22WE 20050815000102005081500010NM 2005 8 15 05FDEA02391 120050811A5320 CHANNEL DOUG MD11 MD11 3023602NM CARGO BAY DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25624FE 48443 FWD CARGO COMPT FOUND CORROSION ON CHANNEL FROM STA 1113 TO STA 6-10 X=-56. FABRICATE REPAIR DOUBLER IAW SRM 53-00-01 FIG 7 SHT 7 VOL 1. 2L73 4F RTA22WE 20050815000112005081500011NM 2005 8 15 05FDEA02392 120050811A5320 CHANNEL DOUG MD11 MD11 3023602NM CARGO BAY DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25624FE 48443 REPAIR ASSESSMENT (E.O. 1-5100-7-5001) FOUND DOUBLER ON FWD CARGO COMPT AT STA 1039 X=50 Z=-97 3" BY 3" ON CHANNEL. PERFORMED REPAIR CHANNEL IAW SRM 53-70-00 FIG 6 VOL 1. 2L73 4F RTA22WE 20050815000132005081500013WP 2005 8 15 05FDEA02395 120050811A5730 SKIN DOUG MD10 MD1010F 3022112WP FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25564FE 46984 RT WING DROP L/E XW=332 EXISTING FLUSH REPAIR DOUBLER ON EXT SKIN. REMOVED OLD REPAIR AND INSTALL NEW REPAIR IAW SRM 57-10-00 FIG 39 VOL 1. 2L73 4F RTA22WE 20050815000152005081500015WP 2005 8 15 05FDEA02397 120050811A5310 BEAM DOUG DC10 DC1010 3022110WP CARGO BAY DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25564FE 46984 FWD CARGO COMPT LT SIDE ON BEAM AT STA 1099 FOUND SPLICE REPAIR WITH NEW SECTION FROM INB'D TO OUT'B AT X=46 Z=-100. REPAIR IAW EA 8-5310-87665. 2L73 4F A22WE 20050815000162005081500016NM 2005 8 15 05FDEA02398 120050811A5313 STRINGER BOEING727 727227 1384078NM CARGO BAY DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 FORWARD CARGO BAY, FRAME IS DENTED AT BS 720 AT STRINGER LT 24. REPAIRED FRAME AT BS 720, STR 24L PER SRM 51-40-3 2L73 4F A3WE 20050815000182005081500018NM 2005 8 15 05FDEA02400 120050811A5330 SKIN BOEING727 727227 1384078NM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 FUSELAGE SKIN HAS A DENT AT BS 1171, 1 INCH ABOVE STRINGER 23L. REPAIRED PER SRM 53-30-3. 2L73 4F A3WE 20050815000202005081500020NM 2005 8 15 05FDEA02402 120050811A5330 SKIN BOEING727 727227 1384078NM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 FUSELAGE SKIN HAS A DENT AT BS 1141, 1 INCH ABOVE STRINGER 20L. REPAIRED FUSELAGE SKIN AT BS 1141 1 INCH ABOVE STR 20L PER SRM 53-30-3 2L73 4F A3WE 20050815000222005081500022NM 2005 8 15 05FDEA02404 120050811A5320 CHANNEL DOUG MD11 MD11 3023602NM CARGO BAY CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25624FE 48443 FWD CARGO COMPT FOUND CRACK LONG 1" ON CHANNEL AT STA 999 X=-50. REPAIR IAW SRM 53-70-00 FIGURE 6 SHT 6 VOL 1. 2L73 4F RTA22WE 20050815000232005081500023NM 2005 8 15 05FDEA02405 120050811A5714 SKIN DOUG MD11 MD11 3023602NM WING BOX CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25624FE 48443 UPPER CARGO COMPT FOUND CORROSION WITH EXFOLIATION ON CTR WING UPPER PANEL AT STA 1235 X=-100. ACCOMPLISH EA 1-5720-88880. 2L73 4F RTA22WE 20050815000252005081500025NM 2005 8 15 05FDEA02407 120050811A5100 NONE DOUG MD11 MD11 3023602NM NONE NONE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25624FE 48443 THIS INSTRUCTION TO REPLACE BOTH EXISTING ILS RECEIVERS WITH MMR AND ASSOCIATED WIRING. ACCOMPLISH EA 1-3431-82825. 2L73 4F RTA22WE 20050815000262005081500026NE 2005 8 15 IXXA0500092O 220050811A7320806312 MEC DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C1 13802NE NR 4 ENGINE OUT OF ADJUST A IXXAO OTHER X ENGINE FLAMEOUT DEDESCENT 1 SW11823BX880071979 46064 693379 DURING DESCENT FROM MPDC TO KTOL FLIGHT LEVEL 38.0, NR 4 ENGINE FLAMED OUT WHEN THROTTLE WAS RESTARTED. ALL ENGINE PARAMETERS WERE NORMAL CREW ACCOMPLISHED FLAME OUT IN FLIGHT START. WHEN A IGNITER WAS USED FOR IN-FLIGHT START ENGINE STARTED NORMALLY NO OTHER PROBLEMS OCCURRED DURING FLIGHT AND LANDED AT KTOL WITHOUT INCIDENT. MAINTENANCE PERFORMED FAULT 51 TROUBLE SHOOTING PROCEDURE AND FOUND THE SPECIFIC GRAVITY WAS OFF. IT WAS ADJUSTED, THE FLIGHT IDLE WAS LOW AND WAS ALSO ADJUSTED. PERFORMED A POWER ASSURANCE RUN PER ATI ERH & GMM NO DEFECTS WERE NOTED PER ALL APPLICABLE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE 2L74 4F4 FRT4A25 E2GL 20050815001632005081500163EA 2005 8 15 COMA0560421 120050801A5240 DOOR CNDAIRCL600 CL6002B19 1900309EA SERVICE OPEN A COMAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 SO01484CA 7702 FLIGHT 5498 - EXTREMELY LOUD SQUEAL FROM RT SIDE OF A/C. FOUND O2 SERVICE DOOR OPEN. CLOSED SERVICE DOOR, NO DEFECTS NOTED. 2L72 4F RTA21EA 20050815001652005081500165NM 2005 8 15 CALA0500262 120050811A5315147A5506 FLOORBEAM BOEING737 737724 13844BYNM STA 986.5 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2724706 28767 INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, LBL 35 TO RBL 35. THE FLOORBEAM WAS REPAIRED IAW ECRA 5321-01268. 2L72 4F RTA16WE 20050815001702005081500170 2005 8 15 SWAA052396 420050811A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29431WN 29845 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050815001742005081500174NM 2005 8 15 SWAA052400 120050811A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29612SW 27930 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 685, STR 11R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050815001752005081500175NM 2005 8 15 SWAA052401 120050811A53116546526 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29612SW 27930 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 380, BS 400 AND BS 440, STR 8L TO STR 9L. REPAIRED FRAMES PER SRM. 2L72 4F RTA16WE 20050815001762005081500176NM 2005 8 15 SWAA052402 120050811A53116546529 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29612SW 27930 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 360, BS 400, BS 440 AND BS 500A, STR 8R TO STR 9R. REPAIRED FRAMES PER SRM. 2L72 4F RTA16WE 20050815001822005081500182NM 2005 8 15 SWAA052408 120050811A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM AFT CARGO BAY CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29612SW 27930 DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 807, RBL 5 TO LBL 5. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050816000022005081600002EU 2005 8 16 AWXA200500943 120050810A3510 OXYGEN SYSTEM AIRBUS320 A320232 3930326EU READS LOW A AWXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP28653AW 1003 CMH - DIVERSION - FLT 0064 - DURING FLIGHT, EN ROUTE TO BOS FROM LAS, CREW NOTICED THE FLIGHT DECK OXYGEN PRESSURE READING LOW, 350 PSI. CREW DIVERTED TO CMH AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE SERVICED FLIGHT DECK OXYGEN IAW AMERICA WEST AIRLINES TASK CARD S2A35301 AND PERFORMED LEAK CHECK OF CREW MASKS AND OXYGEN SYSTEM. COULD NOT FIND ANY LEAKS AND PRESSURE HELD. AIRCRAFT CONTINUED ON TO BOS. OXYGEN WAS SERVICED PREVIOUSLY ON THE 7TH OF AUGUST BUT AIRCRAFT HAS NO PRIOR HISTORY. 2L72 4F RTA28NM 20050816000112005081600011EA 2005 8 16 SWIA200515409 120050803A2740 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA COCKPIT STICKING A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07934SW 7722 FO'S STAB TRIM SWITCH STICKS. REPLACED F/O'S STAB DISCONNECT SWITCH PER MM 27-41-30. 2L72 4F RTA21EA 20050816000212005081600021EU 2005 8 16 AALA20050486 120050730A7500 DUCT AIRBUS300 A300B4605R 3930308EU GE CF6 CF680C2A5 NE NR 2 BLEED SYS LEAKING A AALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW217083A 645 690243 MIA - INFLIGHT ON MAX POWER TAKEOFF ENGINE EXHAUST TEMPERATURE REACHED 1000. AFTER LIFT OFF ATTEMPTED TO RETARD NUMBER 2 THROTTLE BUT IT WAS STUCK FORWARD. RECEIVED INTERMITTENT OVERTEMP AND FIRE INDICATION. RAN FIRE PROCEDURE AND SHOT BOTH FIRE BOTTLES IN FLIGHT. RIGHT SIDE MAIN BRAKES REACHED 685 TO 700 DEGREES. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. FIRE CHIEF REPORTED NO FIRE AFTER LANDING. FOUND BLOWN DUCT. FRACTURED BLEED BIAS SENSOR. REPLACED NUMBER 2 ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA35EU E13NE 20050816000332005081600033NM 2005 8 16 DHL2005746510 120050630A523059948502 RETAINER BOEING727 727224 1384076NM CARGO DOOR SEAL CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01746DH 22252 FWD CARGO DOOR LWR AFT CORNER CRACK. REMOVED AND REPLACED SEAL RETAINER (FRAME) AT C1 DOOR IAW B727 SRM 51-30-2 P/N 65-59948-502 PO522885, LEAK CHECK GOOD IAW B727 MM 21-31-0. 2L73 4F A3WE 20050816000492005081600049NM 2005 8 16 05FDEA02451 120050811A2751 WARNING LIGHT DOUG MD11 MD11 3023602NM TE FLAPS ILLUMINATED A FDEAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 SO25606FE 48602 ON FINAL APPROACH GOT FLAP DISAG ALERT WHILE EXTENDING FLAPS FROM 35 TO 50. RETURNED FLAPS TO 35 AND ALERT CLEARED MOMENTARILY THEN CAME BACK ON, MISSED APPROACH ACCOMPLISHED AND RAN QRH PROCEDURES. ABLE TO RETURN FLAPS TO 35/EXT WITH NO ALERTS. NORMAL APPROACH AND LANDING ACCOMPLISHED. REMOVED AND REPLACED XMTR INBOARD FLAP RT POS. AS PER MD11 MM 27-54-04, OPS CHECK SATIS. 2L73 4F RTA22WE 20050816000532005081600053SO 2005 8 16 C2XA05IA090 120050714A335078241 INVERTER EMB 135 EMB135LR 3260305SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2728529 145512 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY EXIT SIGN AT THE PASSENGER DOOR WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE INVERTER, OPERATIONALLY CHECKED THE LIGHTING SYSTEM, AND CLEARED THE DISCREPANCY. 2L72 4F RTT00011AT 20050816000582005081600058NM 2005 8 16 05FDEA02457 120050812A5754 SKIN BOEING727 727200 138407ENM NR 6 SLAT UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 RIGHT NR 6 SLAT L/E HAS A PREVIOUS REPAIR THAT IS A MAJOR REPAIR IAW SRM 57-50-3 FIG 1. 2L73 4F RTA3WE 20050816000612005081600061WP 2005 8 16 05FDEA02460 120050813A3260 BULB DOUG MD10 MD1010F 3022112WP NLG INDICATOR INOPERATIVE A FDEAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 SO25560FE 46938 PER FLIGHT CREW DEBRIEF (EMP 66912). ON INITIAL GEAR EXTENSION, DID NOT GET GREEN LIGHT FOR NLG ON THE PRIMARY LANGING GEAR INDICATION. CHANGED THE BULBS FOR THE NLG GREEN IND. THEN GOT THE NLG GREEN INDICATION, AND HAD A NORMAL LANDING. PERFORMED FUNCTIONAL TEST IAW MM 31-12-04-2 PAR 5. OPS CHECK NORMAL AT THIS TIME. DUE TO FLIGHT CREW REMOVED AND REPLACED BULBS OF THE PRIMARY NOSE LANDING GEAR IND. 2L73 4F RTA22WE 20050816000632005081600063NM 2005 8 16 05FDEA02462 120050813A5330 SKIN BOEING727 727200 138407ENM FUSELAGE UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 PREVIOUS REPAIR AT STA 712 TO 724 STR 22L AND 23L IS A MAJOR REPAIR IAW SRM 53-30-3 FIG 1. 2L73 4F RTA3WE 20050816000672005081600067NM 2005 8 16 DHL2005747505 120050710A5753 SKIN BOEING727 727224 1384076NM TE FLAP DEBONDED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01747DH 22253 RT WING INBD MID FLAP T/E APPROX 1/2" FROM INBD END IS DISBONDED. CUT OUT DELAM AREA, FAB FILLER AN DOUBLERS ON TRAVELER NR T-828368. CLEANED UP AN PREP REPAIR AREA AN PARTS FAB. BONDED REPAIR PARTS, TREATED AND PRIMED. COMPLETED REPAIR ON RT WING I/B MID FLAP T/E WEDGE APPROX 1/2" FROM INBD END OUTER SURFACE IAW B727 SRM 57-50-2 FIG 3, 51-40-20,51-40-24, 51-10-2. 2L73 4F A3WE 20050816000782005081600078NM 2005 8 16 SWAA052435 120050812A5753 SKIN BOEING737 7373H4 1384600NM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29625SW BN858 27701 RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2L72 4F RTA16WE 20050816000922005081600092NM 2005 8 16 SWAA052446 120050813A33509250071 BULB BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29776WN 30591 DURING SCHEDULED MV3 CHECK, FOUND RT AFT EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050816000952005081600095NM 2005 8 16 SWAA052421 120050813A27506573271 TORQUE TUBE BOEING737 7373H4 1384600NM LT WING TE FLAP WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 DURING SCHEDULED SERVICE CHECK, FOUND NR 4 T/E FLAP TRANSMISSION TORQUE TUBES WORN. REMOVED AND REPLACED TORQUE TUBES PER MM. 2L72 4F RTA16WE 20050816001042005081600104NM 2005 8 16 SWAA052440 120050814A53126516300 BULKHEAD BOEING737 7373T5 1384608NM BS 178 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29696SW 23064 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE VERTICAL BEAM WEB CRACKED AT BS 178 BULKHEAD, BETWEEN LBL 17.1 TO RBL 17.1, BETWEEN WL 212 TO WL 227. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050816001612005081600161SO 2005 8 16 LR7A05102 120050813A5330 SKIN LKHEED382 382G 526414USO FS 440 DENTED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 647 4763 DURING SCHEDULED B2 INSPECTION PER JOB CARD HB5301 FOUND DENT IN FS 440 FUSELAGE SKIN AT WL 200, RBL 70. REPAIRED IAW SRM SMP 583 51-140-10. 2H74 4T A1SO 20050816002202005081600220EU 2005 8 16 USAA050889 120050718A53151160851 FLOORBEAM AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19109UW19030 1065 FOUND FLOORBEAM CORRODED .040 INCH DEEP BY .5 INCH DIAMETER, 41 INCHES LT OF CENTER LINE A C16. CORROSION LEVEL 1, TASK JA-220-53500. REMOVED AND REPLACED BEAM IAW SRM 51-40-00. (M) 2L72 4F RTA28NM 20050817000102005081700010WP 2005 8 17 MWEA050076 120050812A53205936038501 FILLER DOUG DC9 DC981 3022081WP DOOR SILL CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 AFT PIT LOWER DOOR JAMB HAS CORROSION ON FORWARD FACE OF SILL AND AROUND SCREW. FABRICATED AND AND INSTALLED FILLER. 2L72 4F A6WE 20050817000202005081700020EU 2005 8 17 RAIA00508015 120050810A3350 LIGHT JETAIRJETSTMJETSTM4101 1500501EU RT WING MALFUNCTIONED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03574HK 41093 FLT 5392 - STL - RT WING EMERGENCY LIGHTS INOP. MAINTENANCE CYCLED POWER AND OPS CHECK OK. 2L72 4T RTA41NM 20050817000252005081700025EA 2005 8 17 ASOA05600 120050713A29105018T49P01 SEAL CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM WORN A ASOAO OTHER KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO11875AS 7559 FLT 4508 - DURING CLIMB-OUT FROM TUP-ATL, AT APPROX 18,000-19,000 FT, THE CREW RECEIVED AN INTERMITTENT ENG OIL PRESSURE AURAL AND A R ENG OIL PRESSURE WARNING FOR APPROXIMATELY TEN SECONDS. IT THEN WENT OUT AND REOCCURRED THREE TIMES WITH THE OIL PRESSURE FLUCTUATING FROM 32-75 PSI. THE CREW LEVELED THE AIRCRAFT OFF AND MOVED THE RIGHT ENGINE POWER LEVER TO IDLE AND THE OIL PRESSURE STABILIZED BETWEEN 32-38 PSI. THE QRH HAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT PERFORMED A SINGLE ENGINE LANDING SAFELY INTO ATL. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE HYDRAULIC PUMP AND STARTER CARBON SEALS, RUNNERS, PACKINGS AND O-RINGS. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SER2L72 4F RTA21EA 20050817000342005081700034WP 2005 8 17 ASAA0580362 120050718A532199365493 FLOOR PANEL DOUG DC9 DC983 3022083WP FS 160-200 TORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM02944AS 53019 OKC - DURING HV CHECK FOUND CABIN FLOOR PANEL TORN AT CORNER. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050817000362005081700036CE 2005 8 17 800GF080905 120050809A2741 WARNING HORN BEECH MU300 400A 1155402CE ACTIVATED E UVCAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03800GF RK96 TAKEOFF CONFIGURATION WARNING HORN SOUNDED ON TAKEOFF ROLL, THE CREW ABORTED THE TAKEOFF. ONCE CLEAR OF THE RUNWAY THE TAKEOFF CONFIGURATION WAS CHECKED AND RESET, WITH NO FURTHER PROBLEM. 2H72 4F RTA16SW 20050817000412005081700041WP 2005 8 17 ASAA0580367 120050717A532199365811 FLOOR PANEL DOUG DC9 DC983 3022083WP FS 389-465 DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02944AS 53019 OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050817000422005081700042WP 2005 8 17 ASAA0580368 120050717A532199366885 FLOOR PANEL DOUG DC9 DC983 3022083WP FS 674-693 PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02944AS 53019 OKC - DURING HV-CHECK, FOUND CABIN FLOOR PANEL PUNCTURED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050817000502005081700050WP 2005 8 17 UPS05845192 120050801A5310 SEAL DOUG DC8 DC873F 302199FWP STA 20 RBL 60 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 INSPECTION TYPE:C1 HEAVY CORROSION AROUND EXTERNAL POWER CABLE PRESSURE SEAL BELOW EPC RA CK STA 20 RBL 60. REMOVED, FABRICATED, AND INSTALLED PRESSURE SEAL DOUBLER IAW DWG 56122 78 AND DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20050817000662005081700066NM 2005 8 17 AALA20050516 120050809A3350 SOCKET BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21387AM 27184 MIA - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 23H INOPERATIVE. FOUND BROKEN WIRE AT SOCKET OF EMERGENCY LIGHT CONNECTOR UNDER SEAT 23J. INSTALLED NEW SOCKET FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 23H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050817000692005081700069WP 2005 8 17 AALA20050527 120050814A3397 WIRE DOUG DC9 DC983 3022083WP CABIN SHORTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21931TW 49527 ORD - EMERGENCY LIGHTS AT SEAT ROWS 30 TO 32 INOPERATIVE. FOUND WIRES AT SEAT 30 SHORTED. REPAIRED WIRING FOR SEAT MOUNTED LIGHTS AND REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050817000792005081700079WP 2005 8 17 IXXA05SMN150S 120050630A5730 SKIN DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE XW2.000-20.000 DENTED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING C CHECK INSPECTION, LT IB FLAP UPPER PART WITH SEVERAL DENTS XW 2.000 - XW 20.000. PERFORMED MAJOR REPAIR IAW SRM 57-2-5 FIG. 1, EO NR 20051013 DATE 06-29-05. REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1, SRM 51-3-0PAGE 1. REMOVED PLATING SEGMENT (DAMAGED) IAW SRM 57-2-5 FIG. 1. PERFORMED NDT INSPECTION IAW NDT SPM PART 06-10-01-001. NO CRACK, CORROSION FOUND. FABRICATED NEW PLATING (ALCLAD 2024 T3 0.050”) + INTERNAL SPLICE (ALCLAD 2024 T3 0.063”) IAW SRM 57-2-5 FIG. 1 (SHEET 1,3), SRM 57-7-1 FIG. 1 ITEM A. CLEANED, TREATED AND PRIMED AREA + NEW PLATING INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PAGE 9. INSTALLED REPAIR PARTS IAW SRM. TORQUED IAW SRM 51-3-1. 2L74 4F4 FRT4A25 E2GL 20050817000962005081700096CE 2005 8 17 GUU2005F00039 120050725A3240 BRAKE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE RT MLG INADEQUATE A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO1787557 UE246 DURING TAXI, RT BRAKE INEFFICIENT. BLED RT BRAKES. (K) 2L72 4T4 TRTA24CE E26NE 20050817001002005081700100NE 2005 8 17 AWXA200500954 220050812A7250 BLADES AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE NR 2 ENGINE FAILED A AWXAO OTHER O OTHER CLCLIMB 1 WP28646AW453946459 271 V0037 DURING CLIMBOUT, 500 AGL, LOUD BANG ACCOMPANIED WITH ACFT YAWING LT 5-10 FT. ENG RECOVERED IMMEDIATELY. ACFT CONTINUED & LANDED WITHOUT FURTHER EVENT. NO EMERGENCY ACTION TAKEN/DECLARED. MX BORESCOPED BOTH ENGINES TO ENSURE INTEGRITY. NO DEFECTS NOTED ON NR 1 , BUT FOUND NR 2 DAMAGED INTERNALLY. MX R & R NR 2 ENGINE IAW AWA TC R5M71302. CONFIRMED FAILURE. INCOMING INSPECTION REVEALED TWO BROKEN STAGE 5 BLADES WITH MISSING AIRFOIL MATERIAL CAUSING SECONDARY DAMAGE TO OTHER AIRFOILS. ENGINE WAS REPAIRED AND RESTORED IAW EM 71/72-00-00/CD-EM E-V2500-1IA/A5 REV. 60. ENGINE WAS SATISFACTORILY TEST IAW EM 71-00-00 TEST 10. 2L72 4F4 FRTA28NM E311NE 20050817001032005081700103NM 2005 8 17 TSAA0521036 120050814A21200123FA2 SENSOR BOEING737 73776N 13844CHNM CABIN AIR FAILED A TSAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13744AL 32582 FLIGHT 493 SNA-OGG. AFTER DEPARTURE FROM SNA CREW NOTED EQUIPMENT COOLING SUPPLY OFF LIGHT ILLUMINATED STEADY IN NORMAL POSITION FLICKERING IN ALTERNATE POSITION. CREW RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LOW AIRFLOW SENSOR, OPS AND LEAK CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. FLIGHT CREW CONDUCTED IN-FLIGHT VERIFICATION OF EQUIPMENT COOLING AND FOUND SYSTEM OPERATING NORMALLY. 2L72 4F RTA16WE 20050817001082005081700108WP 2005 8 17 ASAA0580377 120050717A532199365853 FLOOR PANEL DOUG DC9 DC983 3022083WP FS 864-886 PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02944AS 53019 OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL PUNCTURED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050817001112005081700111WP 2005 8 17 ASAA0580380 120050717A5321993664740 FLOOR PANEL DOUG DC9 DC983 3022083WP FS 1193-1250 DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02944AS 53019 OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050817001162005081700116WP 2005 8 17 ASAA0580383 120050717A532199365479 FLOOR PANEL DOUG DC9 DC983 3022083WP FS 180-200 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02944AS 53019 OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL HAS CORRODED INSERTS. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050817001202005081700120CE 2005 8 17 AJC2005F00010 120050727A32601EN18 DOWNLOCK SWITCH LEAR 60 60LEAR 5170707CE PWA 305 PW305 NE RT MLG FAILED E AJCAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 EA25706CR754 168 UPON GEAR EXTENSION FOR LANDING, 3 GREEN GEAR LIGHTS ILLUMINATED AND INNER GEAR DOORS OPEN RED LIGHT REMAINED (ON). CREW CYCLED LANDING GEAR TO NO AVAIL, EXECUTED TOWER FLY BY FOR CONFIRMATION AND WAS INSTRUCTED TO RETURN, WHERE ANOTHER ATC TOWER FLY BY WAS MADE AND LANDED UNEVENTFULLY. MAINTENANCE DETERMINED THAT THE RT MAIN GEAR DOWNLOCK SWITCH TO BE DEFECTIVE. REPLACED SAME, PERFORMED LANDING GEAR RETRACTION AND EXTENSION IAW MM. SYSTEM SERVICED, CHECKED SATISFACTORY, AND AIRCRAFT RETURNED TO SERVICE. (K) 2L72 4F4 FRTA10CE E35NE 20050817001242005081700124NM 2005 8 17 BB05066 120050810A2120 HAZE BOEING757 7572B7 1384964NM RROYCERB211 RB211535E4 54555NE CABIN DETECTED A USAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 EA19608AU 22204 EN-ROUTE, THE MID LAV SMOKE DETECTOR BEGAN TO ALARM DURING FLIGHT. THE CABIN CREW NOTED A LIGHT HAZE THROUGHOUT THE CABIN. THE FLIGHT CREW SHUT DOWN THE LT PACK AND CONTINUED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACTION PENDING. 2L72 4F4 FRTA2NM E12EU 20050817001312005081700131WP 2005 8 17 ASAA0580392 120050718A5512593614318 SKIN DOUG DC9 DC983 3022083WP HORIZONTAL STAB PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02944AS 53019 OKC - DURING HV CHECK, FOUND VERTICAL STABILIZER HAS PUNCTURE ON RIGHT SIDE AT RADIUS FOR HORIZONTAL STABILIZER. REPLACED DAMAGED SKIN SECTION. (M) 2L72 4F RTA6WE 20050817001612005081700161NM 2005 8 17 CALA0500265 120050731A5320141N620046 INTERCOSTAL BOEING757 757224 1384958NM R-1 DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713110 27300 INSPECTION FOUND A .5 INCH CRACK IN R-1 DOOR INTERCOSTAL JUST FORWARD OF THE TORQUE BOX. A REPAIR WAS INSTALLED IAW ECRA 5240-01471. 2L72 4F RTA2NM 20050817001642005081700164WP 2005 8 17 0501279877 120050812A2120 ODOR HONEYWELL DOUG DC9 DC951 3022051WP CABIN DETECTED A NWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL01786NC P103DCA 48148 AFTER TAKEOFF FLIGHT ATTENDANT REPORTED SMELL IN AFT AIRCRAFT CABIN. FLIGHT CREW RETURNED AC TO DEPARTURE AIRPORT. MAINTENANCE PLACED APU ON MEL AND REPLACED THE WATER SEPARATORS. 2L72 4F RTA6WE 20050817001682005081700168EU 2005 8 17 KBM2005F00170 120050728A7931642790041 INDICATION SYS SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1 60030NE ENG OIL PRESS FLUCTUATES A KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19215LA1653 2143 ENGINE OIL PRESS, UNIT FLUCTUATES IN FLIGHT. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050817001752005081700175EU 2005 8 17 KBM2005F00172 120050804A2120050085 MOTOR SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1 60030NE BLOWER INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19215LA663 2143 5 INCH MOTOR, UNIT INOPERATIVE, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050817001782005081700178 2005 8 17 KBM2005F00173 420050726A34241234T100372 INDICATOR SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE TURN & BANK NOISY A KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH 2337 TURN AND BANK, UNIT MAKING LOUD NOISE, REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20050817001822005081700182EU 2005 8 17 DAT2005F00009 120050714A3246AHA1236 WHEEL STBROSSD3 SD330 8100602EU PWA PT6 PT6* 52043EA MLG DEFLATED E DATAO OTHER O OTHER NRNOT REPORTED 1 GL13334AC 223 SH3029 THE LT MAIN WHEEL ASSY DEFLATED DURING TAXI AFTER LANDING. MECHANIC WAS DISPATCHED AND REMOVED THE DEFLATED LT MAIN WHEEL AND REPLACED WITH A SERVICEABLE MAIN WHEEL ASSY IAW MM. THE AIRCRAFT WAS RETURNED TO SERVICE. (K) 2H72 4T3 T A41EU E2NE 20050817001862005081700186NM 2005 8 17 ASAA0540334 120050703A57536546430190 SKIN BOEING737 7374Q8 138447QNM TE FLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02775AS 25108 OKC - FOUND RIGHT INBOARD FLAP LOWER SKIN IS DENTED AND DELAMINATED JUST OUTBOARD OF CENTER TRACK. REMOVED DAMAGED AREA, FABRICATED SKIN FILLER AND DOUBLER AND INSTALLED REPAIR PIECES IAW 737-400 SRM 51-70-10 REPAIR 21. (M) 2L72 4F RTA16WE 20050817001872005081700187NM 2005 8 17 ASAA0540335 120050703A57536546430190 SKIN BOEING737 7374Q8 138447QNM TE FLAP DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02775AS 25108 OKC - FOUND RIGHT INBOARD FORE FLAP UPPER IS DELAMINATED 34 INCHES FROM OUTBOARD END AND 8 INCHES FROM T/E. REMOVED DAMAGED AREA, FABRICATED SKIN FILLER AND DOUBLER AND INSTALLED REPAIR PIECES IAW 737-400 SRM 51-70-10 REPAIR 21. (M) 2L72 4F RTA16WE 20050817001882005081700188NM 2005 8 17 ASAA0540336 120050703A57536546430190 SKIN BOEING737 7374Q8 138447QNM FORE FLAP DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02775AS 25108 OKC - FOUND RIGHT INBOARD FORE FLAP UPPER SKIN IS DELAMINATED 60 INCHES FROM INBOARD END AND 8 INCHES FROM T/E. REMOVED DAMAGED AREA, FABRICATED SKIN FILLER AND DOUBLERS AND INSTALLED REPAIR PIECES IAW 737-400 SRM 51-70-10 REPAIR 21. (M) 2L72 4F RTA16WE 20050817001892005081700189EU 2005 8 17 KBM2005F00175 120050726A7931350A67402301AA INDICATION SYS SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE OIL PRESS FLUCTUATES E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19250SH444 3874 OIL PRESSURE HARDNESS, UNIT FLUCTUATING FROM 5 BAR TO 8 BAR AND PEG OUT. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050817001902005081700190 2005 8 17 KBM2005F00176 420050804A310056375600010 GAUGE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE T4 FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19250SH 3874 T-4 GAUGE, DURING START T4 GAUGE NEEDLE WILL NOT RISE AND KEEP BLOWING T-4 FUSE, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050817001932005081700193EU 2005 8 17 KBM2005F00178 120050731A21204900171 MOTOR SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE BLOWER INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV 3296 5 INCH BLOWER MOTOR, INOPERATIVE, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050817001942005081700194EU 2005 8 17 KBM2005F00179 120050803A21200500847 MOTOR SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE BLOWER FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV 3296 7 INCH MOTOR, FAILED, CAUSED AIRCRAFT 50 A FUSE TO FAIL. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050817001952005081700195EU 2005 8 17 KBM2005F00180 120050803A2150540028C2A CONTROL BOX SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE AIR CONDITIONINGUNKNOWN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV61107 3296 CONTROL BOX, UNIT REQUIRES LOAD CHECK, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050817001972005081700197NE 2005 8 17 KBM2005F00181 220050414A74219550175400 IGNITER SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE RT ENGINE WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19345SH 3345 CENTER ELECTRODE ON RT ENGINE IGNITER WORN. (K) 1G71 3U3 U H9EU E19EU 20050817002032005081700203NM 2005 8 17 ASAA0540342 120050703A575465C26602311 WEDGE BOEING737 7374Q8 138447QNM NR 2 SLAT DEBONDED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02775AS 25108 OKC - FOUND NR 2 SLAT T/E WEDGE PREVIOUSLY INSTALLED REPAIR IS DISBONDED AT AFT OUTBOARD CORNER. PREPARED DAMAGED AREA, FABRICATED AND INSTALLED A REPAIR DOUBLER AND BONDED, IAW 737-400 SRM 51-70-10 REPAIR 8. (M) 2L72 4F RTA16WE 20050817002072005081700207NM 2005 8 17 2005UALA00772 120050806A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE STR 20R, STA 171DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP2987UA 26713 FUSELAGE SKIN IS DENTED AT STR 20R, STA 1719. REMOVE DAMAGE, ACP HEFC INSP, NO CRACK FOUND. FABRICATE AND INSTALL DOUBLER PER TIMCO REO-G10787, AND UA EVA 50524. 2L72 4F4 FRTA2NM E17NE 20050817002082005081700208NM 2005 8 17 2005UALA00773 120050806A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE STA 580, STR 24LDENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29587UA 26713 DENT IN FRAME AT STA 580, STR 24L. TRIMMED OUT DAMAGE, ACP HFEC INSP, NO CRACK FOUND. FABRICATE ANGLE REPAIR PER TIMCO REO-G10764 AND UA EVA-50105. 2L72 4F4 FRTA2NM E17NE 20050817002132005081700213NE 2005 8 17 2005UALA00778 220050805A7297 WIRE BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE ENGINE FRAYED A UALAO OTHER O OTHER NRNOT REPORTED 1 WP29798UA 26928 PANEL OPENED AT POTABLE WATER COMPRESSOR IN AFT BULK PIT. FOUND WIRING AND CONNECTOR TO COMPRESSOR FRYED. FOUND COMPRESSOR NOT RUNNING AND VERY HOT. ON AUGUST 1, LAX CLEANED COMPRESSOR ELEC CONNECTOR TO CLEAR W/U FOR LOW H2O PRESS. REPEAT W/U ON AUG 4, SFO REPLACED COMPRESSOR AND REPLACED CONNECTOR. STILL NO HELP, DEFERRED TO DEN. COMPRESSOR REPLACED AGAIN AUG 6. NO SUBSEQUENT W/U'S TO DATE. FINDINGS FOR COMPRESSEOR REMOVED AUG 6: WILL NOT BUILD PRESSURE. VALVE DAMAGED. NUT, O-RINGS AND BEARINGS WORN. REPLACED ALL WORN AND DEFECTIVE PARTS AS NOTED, ASSEMBLED AND TESTED IN ACCORDANCE WITH OEM SPECIFICATIONS. 2L72 4F4 FRTT0001SE E46NE 20050817002142005081700214NM 2005 8 17 2005UALA00779 120050806A335020131A BATTERY PACK BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE ROW 13 INOPERATIVE A UALAO OTHER L NO TEST ININSP/MAINT 1 WP29938UA 26671 EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 13 TO AFT CABIN. REPLACED BATTERY AND AFT GALLEY STRIP. 2L72 4F4 FRTA16WE E2GL 20050912000722005091200072NE 2005 9 12 SWAA052707 220050906A72301590M21P01 FAN BLADE BOEING737 7373H4 1384600NM GE CFM56 CFM56* 13802NE NR 2 ENGINE SHINGLED A SWAAO OTHER EJ VIBRATION/BUFFET WARNING INDICATION LDLANDING 1 SW29391SW 27378 VIBRATION FELT THROUGHOUT FLIGHT - NOTICEABLY LOUD UPON LANDING DURING REVERSE THRUST OPERATIONS. FOUND SEVERAL FAN BLADES ON NR 2 ENGINE DAMAGED & SHINGLED. REMOVED AND REPLACED NR 2 ENGINE FAN BLADE SET PER MM. 2L72 4F4 FRTA16WE E2GL 20050817002152005081700215NM 2005 8 17 2005UALA00781 120050807A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE STA 620 DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP2987UA 26713 FUSELAGE SKIN IS CREASED AT STA 620 LT AND STR 17L. REMOVED DAMAGE SKIN AND REPLACED PER MM 53-30-92- SKIN SPLICE REPAIR, AND REF UA-EVA- 50527. 2L72 4F4 FRTA2NM E17NE 20050817002202005081700220NM 2005 8 17 2005UALA00786 120050806A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE OVERWING INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29120UA 29166 TWO AFT OVERWING EMERGENCY LIGHT ASSYS, RIGHT SIDE INOP. 2L74 4F4 FRTA20WE E24NE 20050817002212005081700221NM 2005 8 17 2005UALA00787 120050806A3350362624 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE SEAT 5F INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29120UA 29166 AFT SEAT EEL LIGHT AT SEAT 5F MISSING. REPLACED LIGHT ASSY. 2L74 4F4 FRTA20WE E24NE 20050817002222005081700222NM 2005 8 17 2005UALA00788 120050806A335080541 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE MID LAV INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29120UA 29166 MID LAV CROSS AISLE EEL LIGHT FWD LEFT SIDE INOP. REPLACED LIGHT ASSY. 2L74 4F4 FRTA20WE E24NE 20050817002232005081700223NM 2005 8 17 2005UALA00789 120050808A2432 BATTERY BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FAILED A UALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 WP29919UA 25386 RETURNED TO THE FIELD DUE TO A BATTERY SYSTEM FAILURE. SHOP FINDINGS REVEALED BAD CELLS IN THE BATTERY. THE BATTERY HAS BEEN SCRAPPED. 2L72 4F4 FRTA16WE E2GL 20050817002242005081700224WP 2005 8 17 DHL05805002 120050817A2121 FAN DOUG DC8 DC873F 302199FWP LT A/C PACK FAILED A DHLAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO01805DH 46125 LT PACK TRIP LIGHT COME ON ON THE GROUND AND LIGHT SMOKE IN COCKPIT, DEFERRED LT AC PACK PER MEL 21-38 CAT C SPECIAL PROCEDURE 21-38 CW A/C RESTRICTED TO FL 250 PLACARD INST DMI 22107. LT PACK TRIP LIGHT CAME ON ON THE GROUND & LIGHT SMOKE IN COCKPIT. R&R LT PACK COOLING FAN. UPON FURTHER SYSTEM INSPECTION FOUND ACM TURBINE DISCHARGE DUCT CLAMP MISSING INSERTS & SLEEVE, R&R CLAMP ASSY P/N CF15-250.PACK CKS OK IAW 21-55-00 DMI CLEARED. 2L74 4F RT4A25 20050818000012005081800001NM 2005 8 18 QXEA200501175 120050812A36208209712 SHUTOFF VALVE BOMBDRDHC8 DHC8402 1390042NM NR 2 BLEED SYS FAULTY A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09408QX9915 4050 GEG FLIGHT 2314: NR 2 BLEED HOT CAUTION LIGHT ILLUMINATED. TURNED NR 2 BLEED AIR OFF IAW PERTINENT CHECKLIST. CAUTION LIGHT REMAINED ILLUMINATED FOR ABOUT MINUTES THEN WENT OFF. LEFT NR 2 BLEED OFF FOR REMAINDER OF FLIGHT. NO FURTHER INCIDENT. MAINTENANCE INTERROGATED CDS. FOUND FAULT CODES 1102-R HPSOV AND 7005 R BLD ANA OT. REMOVED AND REPLACED NR 2 PRECOOLER TEMP SWITCH AND REMOVED AND REPLACED NR 2 HPSOV IAW AMM 36-11-09. OPS CHECK GOOD. CDS SHOWED NO FAULT CODES. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050818000022005081800002NM 2005 8 18 USAA200508003 120050815A5330 SKIN BOEING737 7373B7 1384580NM CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19384US 22957 A 2 INCH CRACK BETWEEN BS 753.5 & BS 755.5 AT S-21R. INSTALLED DOUBLER PER SRM 53-00-01 FIG 201 REPAIR 31. 2L72 4F RTA16WE 20050818000032005081800003NM 2005 8 18 USAA200508002 120050813A5312 PRESSURE PANEL BOEING737 737301 1384611NM MLG WW CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19353US 23556 A .75 INCH CRACK FOUND IN LT MLG WHEEL WELL PRESSURE FLOOR WEB STA 665/LBL 30. INSTALLED DOUBLER PER TYPICAL REPAIR 53-60-04A & EA 81311. 2L72 4F RTA16WE 20050818000062005081800006NM 2005 8 18 DHL2005747507 120050814A5340 ATTACH ANGLE BOEING727 727224 1384076NM FS 990 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01747DH 22253 CORROSION ON SKIN ATTACH ANGLE FS 990 FROM STR 27R TO STR 29R. REMOVED CORROSION OFF SKIN ATTACH ANGLE FS 990 STR 27R TO 29R. PERFORMED ULT INSP ON BLENDED AREA. ATTACH ANGLE BEYOND LIMITS IAW B727 SRM 51-20-1. FABRICATED AND INSTALLED NEW ATTACH ANGLE SKIN 7 X 2 X 6.5 INCHES FROM 7075-T6 .080 IAW B727 SRM 51-10-2, 51-10-6, 51-30-2 AND 51-20-1. 2L73 4F A3WE 20050818000082005081800008NM 2005 8 18 DHL2005747509 120050814A5320 SHEAR WEB BOEING727 727224 1384076NM BS 950F CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01747DH 22253 CORRODED AFT CARGO INTERCOSTAL FROM STA 950F TO 970 STR 28R. REMOVED FLOOR SUPPORT CLIPS, REMOVED SHEAR WEB. FABRICATED AND INSTALLED NEW SHEAR WEB 19.5 X 7 INCHES FROM 7075-T6 .040 WEB, FLOOR SUPPORT CLIPS IAW B727 SRM 51-30-5, 51-10-2, 53-10-2 AND 51-30-2. 2L73 4F A3WE 20050818000092005081800009GL 2005 8 18 C2XA05BT058 220050809A7200AE3007A1P ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 2 LEAKING A C2XAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW27145706891 6891 145632 CAE312207 CREW REPORTED, LAV SMOKE WARNING. EWR MAINTENANCE INSPECTED THE AIRCRAFT AND MAINTENANCE FERRIED AIRCRAFT TO BTV MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE IAW TASKCARD 6271001, OPS CHECKED AND LEAKS CHECKS GOOD. 2L72 4T4 FRTT00011ATTE6CH 20050818000102005081800010SO 2005 8 18 C2XA05TY048 120050812A532014525480003 SILL EMB 145 EMB145XR 3260214SO CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714158 145791 DURING A SCHEDULED 1C INSPECTION THE CARGO DOOR CUTOUT SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SILL ASSEMBLY AS PER THE EMB 145XR SRM AND EC5330-01458. ACFT WILL BE RELEASED TO SERVICE FOLLOWING COMPLETION OF THE 1C INSPECTION. 2L72 4F RT 20050818000112005081800011 2005 8 18 WRLA2005140 420050816A2565AWD9822503 SLIDE DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE L-3 DOOR TWISTED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278 48746 DURING C1 CHECK IN HEL, L-3 EVACUATION SLIDE WAS TEST DEPLOYED PER WOA TC 1095 CARD. THE SLIDE FULLY INFLATED BUT FAILED TO REGAIN THE PROPER DIRECTION FOR USE. REMOVED AND REPLACED SLIDE PER MM PROCEDURES. 2L73 4F4 FRTA22WE E24NE 20050818000122005081800012NM 2005 8 18 SWAA052452 120050815A335020131A BATTERY PACK BOEING737 7373H4 1384600NM CABIN FAILED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29325SW 23689 EMERGENCY EXIT INTERIOR & EXTERIOR LIGHTS FAILED TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050818000142005081800014 2005 8 18 SWAA052454 420050815A256565C19901 CABLE BOEING737 7373G7 1384595NM R2 DOOR BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29690SW 23783 DURING SCHEDULED 1/4D CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE CABLE BROKEN. REMOVED AND REPLACED CABLE PER MM. 2L72 4F RTA16WE 20050818000152005081800015NM 2005 8 18 SWAA052455 120050815A53116517684 FRAME BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29696SW 23064 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303, STR 10L. REPAIRED FRAME PER SWA EA. 2L72 4F RTA16WE 20050818000162005081800016NM 2005 8 18 SWAA052456 120050815A53116517685 FRAME BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29696SW 23064 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME INNER CHORD CRACKED AT BS 348.2, STR 15L. REMOVED AND REPLACED INNER FRAME CHORD PER SRM. 2L72 4F RTA16WE 20050818000182005081800018NM 2005 8 18 SWAA052450 120050815A3260189915 SENSOR BOEING737 7373H4 1384600NM NLG FAULTY A SWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW29315SW 23337 AIR TURNBACK/DECLARED EMERGENCY. LG POSITION INDICATING LIGHTS ILLUMINATED AFTER GEAR RETRACTION. RECYCLED GEARS, NO HELP. REMOVED AND REPLACED NLG PRIMARY DOWN PROX SENSOR PER MM. 2L72 4F RTA16WE 20050818000202005081800020SO 2005 8 18 C2XA05TY049 120050816A531314521722017 STRINGER EMB 135 EMB135LR 3260305SO DAMAGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716525 145403 TYS, DURING A SCHEDULED INSPECTION, STRINGER 2L, JUST FORWARD OF FRAME 75 WAS FOUND DAMAGED. MAINTENANCE CUT OUT THE DAMAGED SECTION, FABRICATED A NEW SECTION, -J- AND -L- ANGLES, PRIMED, PAINTED AND INSTALLED IAW EMB-135/145 SRM 53-00-03 AND CPM 51-21-04/05/06. 2L72 4F RTT00011AT 20050818000232005081800023NM 2005 8 18 QXEA200501176 120050813A32509451693 MANIFOLD BOMBDRDHC8 DHC8402 1390042NM NLG STEERING MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION LDLANDING 1 NM09412QX5474 4059 SMF FLIGHT 2415: THE NOSE STEERING CAUTION LIGHT CAME ON JUST AFTER LANDING. RAN THE CHECKLIST AND THE NOSE STEERING CAUTION LIGHT CAME BACK ON. MAINTENANCE REMOVED AND REPLACED NOSE WHEEL STEERING MANIFOLD IAW Q400 TASK 32-51-16-000-801 AND -400-801. OPS CHECK IAW TASK 32-51-00-710-801 GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050818000242005081800024NM 2005 8 18 DHL2005747512 120050717A5753 SKIN BOEING727 727224 1384076NM LEADING EDGE GOUGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01747DH 22253 LT WING INBOARD TRAILING EDGE FORE FLAP OUTBOARD LOWER LEADING EDGE REPAIR DOUBLER IS GOUGED THRU. REMOVED EXISTING REPAIR IAW B727 SRM 51-30-2. FABRICATED NEW REPAIR DOUBLER 3.95 X 4.55 INCH FROM 2024-T3 .063 IAW B727 SRM 57-50-4. ALODINED AND PRIMED, INSTALLED NEW REPAIR DOUBLER ON TO LT WING I/B TRAILING EDGE FORE FLAP, O/B LWR LEADING EDGE IAW B727 SRM 57-50-4. SEALED FAYING EDGE OF NEW REPAIR DOUBLER USING PS870B-1/2 IAW B727 SRM 57-50-4. 2L73 4F A3WE 20050818000262005081800026NM 2005 8 18 SWAA052464 120050815A53306545775 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STR 19L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050818000272005081800027NM 2005 8 18 SWAA052463 120050815A53306545776 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 23L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050818000292005081800029NM 2005 8 18 SWAA052461 120050816A79331122514 BULB BOEING737 7373H4 1384600NM NR 1 ENG INDICATFAULTY A SWAAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 SW29326SW 23690 INFLIGHT SHUTDOWN/DECLARED EMERGENCY. NR 1 ENGINE OIL TEMPERATURE INDICATED ABOVE RED LINE. REMOVED AND REPLACED NR 1 ENGINE OIL TEMP BULB PER MM. 2L72 4F RTA16WE 20050818000302005081800030NM 2005 8 18 SWAA052460 120050816A2750693923617 PUSHROD BOEING737 7373H4 1384600NM LT WING TE FLAP BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED RON CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DRIVE PUSHROD BROKEN. REMOVED AND REPLACED PUSHROD PER MM. 2L72 4F RTA16WE 20050818000312005081800031NM 2005 8 18 SWAA052459 120050815A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 750 TO BS 757, STR 18L TO STR 20L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050818000322005081800032NM 2005 8 18 SWAA052458 120050815A57536546435273 SKIN BOEING737 7373H4 1384600NM LT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED C4 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2L72 4F RTA16WE 20050818000342005081800034NE 2005 8 18 08122005E 220050812A7200 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LEFT SURGES A NSVAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 EA27308CE 210 ABORTED TAKEOFF DURING POWER UP LT ENGINE SURGED. MAINTENANCE INSPECTION FOUND NO FAULT. 2L72 4T4 TRTA52EU E8NE 20050818000352005081800035 2005 8 18 08152005C 420050810A2210 SERVO SAAB SF340 340B 7860101EU AUTOPILOT MALFUNCTIONED A NSVAO OTHER O OTHER APAPPROACH 1 EA27303CE 194 DURING COUPLED ILS APPROACH YELLOW ELV LIGHT ON EADI FOLLOWED BY YOKE VIBRATION AND A STRONG RATTLING SOUNDED UNDER CAPT'S FLOORBOARD. PERFORMED OPERATIONAL CHECK OF A/P SYSTEM. ABLE TO DUPLICATE YOKE VIBRATION WHEN SIMULATING APPROACH. SERVO RATTLES UNDER FLOORBOARD (CLUTCH IS RATTLING). CHECKED ALL FLIGHT CONTROLS FOR SMOOTH OPERATION AND TRIM SWITCHES. OPS CHECKS GOOD. DETERMINED PROBLEM TO BE INDUCED WITH A/P ENGAGED. DEFERRED A/P. 2L72 4T RTA52EU 20050818000362005081800036EU 2005 8 18 08112005D 120050811A5310 STRUCTURE SAAB SF340 340B 7860101EU NOSE BIRD STRIKE A NSVAO OTHER O OTHER CRCRUISE 1 EA27339CJ 339 BIRD STRIKE ON NOSE OF A/C. PERFORMED VISUAL INSPECTION OF NOSE, ENG INLETS, LEADING EDGES, & PROBE, NO DEFECTS NOTED. 2L72 4T RTA52EU 20050818000402005081800040NM 2005 8 18 AWXA200500959 120050714A53116546561509 FRAME BOEING737 7373S3 1384711NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 DURING C18 CHECK DISCOVERED FRAME CRACKED, .17 INCHES IN LENGTH, UNDER DOOR ASSIST HANDLE AT THE R2 DOOR, BS 954, STR14R. MAINTENANCE TRIMMED OUT CRACK AT DOOR ASSIST HANDLE AT THE R2 DOOR, BS 954, STR 14R IAW AMERICA WEST AIRLINES (AWA) ENGINEERING REPAIR (ER) 03-5362-05224-DF2. FABRICATED FILLER, STRAP, AND FRAME SPLICE STRAP IAW AWA ER 03-5362-05224-DF2. INSTALLED FABRICATED REPAIR PARTS UNDER DOOR ASSIST HANDLE AT THE R2 DOOR, BS 954, STR14R IAW AWA ER 03-5362-5224-DF2. 2L72 4F RTA16WE 20050818000422005081800042NM 2005 8 18 AWXA200500961 120050816A2781 WARNING SYSTEM BOEING757 7572S7 1384962NM SLATS ACTIVATED A AWXAO OTHER J WARNING INDICATION DEDESCENT 1 WP28905AW 23567 FLT 563 - WHILE DEPLOYING FLAPS CREW REPORTED LEADING EDGE SLAT DISAGREE EICAS MESSAGE. MESSAGE CLEARED WITH ALTERNATE EXTENSION. EMERGENCY LANDING FOR PRECAUTIONARY PURPOSES. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED OPERATIONAL CHECK IAW TASK CARD F1B27629, OPERATIONAL CHECKS GOOD. NO FAULTS FOUND. 2L72 4F RTA2NM 20050818000432005081800043NM 2005 8 18 2005UALA00802 120050810A2781 WARNING SYSTEM BOEING757 757222 1384956NM PWA 2037 PW2037 NE SLATS ACTIVATED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29507UA 24743 RETURNED TO FIELD DUE TO LE SLAT DISAGREE EICAS MESSAGE. FOUND FSCU HAD INTERMITTE FAULT ON SLAT PDU XMIT. CLEANED CONNECTOR. ACP SYSTEM CYCLE OPS NORMAL. 2L72 4F4 FRTA2NM E17NE 20050818000442005081800044NM 2005 8 18 2005UALA00790 120050708A3350 LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE R1 DOOR INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP2987UA 26713 EEL AT 1-R DOOR INTERIOR AND EXTERIOR INOP. REPLACED EXIT LIGHT. 2L72 4F4 FRTA2NM E17NE 20050818000482005081800048EU 2005 8 18 2005UALA00794 120050809A2910 HYDRAULIC SYSTEM AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE GREEN SYS LEAKING A UALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP29484UA 1609 FLIGHT EXPERIENCED GREEN HYD QTY LOSS AND ECAM INDICATION. 2L72 4F4 FRTA28NM E40NE 20050818000492005081800049NM 2005 8 18 2005UALA00795 120050810A3260 LANDING GEAR BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE NOSE MISALIGNED A UALAC ABORTED TAKEOFF WJ INADEQUATE Q C WARNING INDICATION TOTAKEOFF 1 WP29226UA 30226 GEAR WARNING MESSAGE. HAD GEAR CONFIG WARNING DUE TO MAIN GEAR STEERING NOT CENTERED AND LOCKED PRIOR TO APPLICATION OF TAKEOFF POWER. ITEM IS CURRENTLY DEFERRED. HISTORICALLY THIS PROBLEM IS CAUSED BY CREW APPLYING TAKE OFF POWER BEFORE MAIN GEAR COMPLETELY CENTERED AFTER TURNING ONTO RUNWAY. 2L72 4F4 FRTT0001SE E46NE 20050818000502005081800050NM 2005 8 18 2005UALA00796 120050809A3350 LIGHT BOEING777 777222 1385219NM PWA PW4077PW4077 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29779UA 26941 2F AFT FLOOR EMERGENCY LIGHT INOP. REPLACED EEL LIGHT ASSEMBLY. 2L72 4F4 FRTT0001SE E46NE 20050818000532005081800053 2005 8 18 2005UALA00799 420050718A2565D31101205 SLIDE BOEING757 757222 1384956NM PWA 2037 PW2037 NE 4L DOOR LEAKING A UALAK NONE O OTHER ININSP/MAINT 1 WP29513UA 24810 TUBE ASSY FAILED AIR RETENTION TEST DUE TO EXCESSIVE POROSITY LEAKING THROUGH TUBE FABRIC NOTED ON VARIOUS LOCATIONS. DURING COMPONENT SHOP MAINTENANCE SLIDE FAILED AIR RETENTION TEST DUE TO FABRIC POROSITY. POROSITY WAS BEYOND CMM LIMITS. SLIDE WAS RETURNED TO OEM FOR INFLATABLE REPLACEMENT. 2L72 4F4 FRTA2NM E17NE 20050818000552005081800055NE 2005 8 18 2005UALA00801 220050810A72617T0526 CARBON SEAL BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 1 ENGINE DAMAGED A UALAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP2990UA 7422 28708 726649 DIVERTED TO OGG UNDER AMBER ALERT WITH NR 1 ENGINE SHUTDOWN DUE TO LOW OIL QUANTITY INDICATION. ROOT CAUSE WAS THE FAILURE OF THE DE-OILER CARBON SEAL. THIS IS AN ANOMALY, AS THERE WAS NO HISTORY OF HOC PRIOR TO THE EVENT. ALSO IT WAS NOT DUE TO INFANT MORTALITY. CORRECTIVE ACTION WAS THE REPLACEMENT OF THE CARBON SEAL, AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA2NM E17NE 20050818000562005081800056NM 2005 8 18 2005UALA00803 120050811A5242 SKIN BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE E/E DOOR GOUGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29674UA 29242 FWD LOWER FUSELAGE, E/E DOOR SKIN IS GOUGED ON THE FWD RT CORNER. THE GOUGE IS AN ISOLATED INCIDENT AND NOT SYSTEMIC TO FLEET. PRODUCTION BLENDED AND FOUND IT TO BE OUT OF THE SRM, SRM 52-40-01 LIMITS. A DOUBLER WAS FABRICATED PER SRM 52-40-01 AND INSTALLED PER SRM 51-40-02. 2L72 4F4 FRTA1NM E24NE 20050818000572005081800057NM 2005 8 18 2005UALA00804 120050811A5315 STIFFENER BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE FLOORBEAM CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29674UA 29242 FWD NOSE SECTION, BS 246 FLOORBEAM, FWD SIDE APPROX LBL 17, VERTICAL STIFFENER CRACKED. ROUTINE INSPECTION IN PLACE TO FIND AND FIX THESE CRACKED STIFFENERS. THIS IS A KNOWN ISSUE ADDRESSED BY BOEING SERVICE BULLETIN AND UA MAINTENANCE PROGRAM. 2L72 4F4 FRTA1NM E24NE 20050818000582005081800058NM 2005 8 18 2005UALA00805 120050811A5330 SKIN BOEING747 747422 1384935NM PWA 4056 PW4056 NE STR 28L STA 490 DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29178UA 24385 CRACK FOUND ADJACENT TO FASTENER HOLE STR 28L STA 490. OUTER SKIN CRACKED AT FASTENER HOLE AND TRIMMED AWAY. SKIN'S INNER BONDED DOUBLER ALSO CRACKED AND TRIMMED AWAY. ALSO, FOUND INTERCOSTAL BRACKET ATTACHED TO SKIN AND INTERCOSTAL WEB BUT NOT ATTACHED TO FRAME WEB. SUSPECT THIS PRODUCTION ERROR TO BE RESPONSIBLE FOR SKIN AND BONDED DOUBLER CRACKS. 2L74 4F4 FRTA20WE E24NE 20050818000592005081800059NM 2005 8 18 2005UALA00806 120050810A33509F19948501 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE R4 DOOR INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29121UA 29167 DOOR 4 RT INSIDE DOOR MOUNTED SLIDE LIGHT INOP. REPLACED LIGHT ASSY. 2L74 4F4 FRTA20WE E24NE 20050818000622005081800062NM 2005 8 18 2005UALA00809 120050812A33509F19948501 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE 3R DOOR INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29104UA 26902 EMERG LT INOP, DR 3 RT SLIDE. REPLACED LIGHT ASSY. 2L74 4F4 FRTA20WE E24NE 20050818000632005081800063NM 2005 8 18 2005UALA00810 120050812A33501317 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT BURNED OUT A UALAK NONE L NO TEST ININSP/MAINT 1 WP29104UA 26902 EMERGENCY LIGHT INOP, CEILING MID GALLEY. REPLACED LAMP. 2L74 4F4 FRTA20WE E24NE 20050818000652005081800065EU 2005 8 18 2005UALA00812 120050812A3220 LANDING GEAR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NOSE MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29428UA 523 NOSE GEAR WOULD NOT LOCK IN UP POSITION. 2L72 4F4 FRTA28NM E40NE 20050818000672005081800067NM 2005 8 18 DHL2005747510 120050814A5313 STRINGER BOEING727 727224 1384076NM 950F CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01747DH 22253 CORROSION FOUND ON STR 28R, STA 950F TO 970 AT SKIN ATTACHMENTS. REMOVED STR 28R FROM 950F TO 1010, FRAME STA 987 RT CLIPS AND ANGLE SUPPORT STA 950F, 985, 990. FABRICATED AND INSTALLED STR SPLICE 13.5 INCH FROM BAC1498-131, SPLICE 1.08 X .810 X .19R FROM 7075-T651, FORMED SECTION REPAIR 6.0 X 1.0 FROM 301 .080" 1/4 HD AND STR 49 FROM BAC1509-100204 IAW TIMCO REO-L00957 AND REO-L00960. 2L73 4F A3WE 20050818000682005081800068NM 2005 8 18 DHL2005747511 120050814A5330 BEAR STRAP BOEING727 727224 1384076NM 990 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01747DH 22253 CORROSION FOUND AFT PIT INTERNAL SKIN STA 990 STR 28R AFT OF BEAR STRAP DOUBLER. REMOVED CORROSION, FABRICATED AND INSTALLED DOUBLER 20.25 X 15.5 INCH FROM 2024-T3 .160 IAW B737 SRM 53-30-3 FIG 3. 2L73 4F A3WE 20050818000732005081800073NM 2005 8 18 AWXA200500964 120050731A53156546812170 FLOORBEAM BOEING737 7374Y0 1384705NM CABIN CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28334AW 23747 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED CORROSION ON UPPER SURFACE OF FLOOR SUPPORT BS 965, BL 18R, WL 208. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-51-1. REMOVED FLOOR SUPPORT AT BS 965, BL 18R, WL 208 IAW BOEING 737-300 SRM 51-40-02-0. RECEIVED AND PREPARED NEW FLOOR SUPPORT FOR INSTALLATION IAW BOEING 737-300 SRM 51-40-05-0 FIG 2. INSTALLED REPAIR PARTS AT BS965, BL 18R, WL 208 IAW BOEING 737-300 SRM 51-40-02-0 FIGS 12 AND 14. 2L72 4F RTA16WE 20050818000772005081800077NM 2005 8 18 USAA050915 120050729A531596722217368LF FLOORBEAM BOEING757 7572B7 1384964NM RROYCERB211 RB211535E4 54555NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19628AU36199 27806 BFM - C3 - FLOORBEAM CAP 4.2 INCH X .020 INCH, 2 INCH X 2 INCH X .027 INCH, 2 INCH X 3 INCH X .020 INCH, 3.5 INCH X 2 INCH X .020 INCH, CORROSION; NO LEVEL OR TASK, STA 365, RBL 4 INCH/ RBL, 14 INCH/RBL 55 INCH/RBL 61. REPAIRED IAW EA. (K) 2L72 4F4 FRTA2NM E12EU 20050818000782005081800078NM 2005 8 18 USAA050918 120050729A532014IN31703CLF CHANNEL BOEING757 7572B7 1384964NM RROYCERB211 RB211535* NE STA324-345,LBL18CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19628AU 27806 BFM - C3 - U CHANNEL, 14 INCH X 2.5 INCH X .04 INCH, CORROSION; NO LEVEL OR TASK STA 324-345, LBL 18 INCH. REPLACED FLOOR SUPPORT U CHANNEL IAW SRM. (K) 2L72 4F4 FRTA2NM E12EU 20050818000802005081800080EA 2005 8 18 A6WA200540276 120050803A5753 VANE CNDAIRCL600 CL6002B19 1900309EA CFMINTCFM56 CFM563B2 13802EU RT TE FLAP WORN A A6WAK NONE O OTHER ININSP/MAINT 1 GL31405AW 7362 RT OB FLAP VANE, OB FLAP VANE FITTING WORN EVEN WORN LEADING EDGE OF VANE .030 INCH IS MINIMUM CLEARANCE ALLOWED IAW REO. REMOVED OLD VANE FITTING FROM RT OB FLAP AS WS296.073 AND INSTALLED NEW VANE FITTING IAW REO. (K) 2L72 4F4 FRTA21EA E21EU 20050818000822005081800082CE 2005 8 18 DBC2005F00000 120050810A5610991407147 WINDSHIELD CESSNA650 650 2076802CE GARRTTTFE731TFE731* 01518WP COCKPIT DISTORTED E DBCAO OTHER O OTHER NRNOT REPORTED 1 GL13202JK 6500100 (DBCA122D) DISTORTION OF WINDSHIELD NOTED IN LT CORNER. REMOVED WINDSHIELD AND SENT FOR EVALUATION. WINDSHIELD COULD NOT BE REPAIRED, REQUIRES REPLACEMENT. SUSPECTS WINDSHIELD DAMAGE DUE TO OVERHEATING CAUSED BY SITTING ON RAMP WITH REFLECTIVE WINDSHIELD SCREEN IN PLACE. (K) 2L72 4F4 F A9NM E6WE 20050816002052005081600205NM 2005 8 16 BB05054A 120050721A2530 COFFEEMAKER BOEING757 757225 1384959NM GALLEY ODOR A USAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA19607AU 22203 LAS FLT 697 EN-ROUTE PHL TO LAS. THE CABIN CREW NOTICED A BURNING ODOR, LIKE BURNING COFFEE, COMING FROM THE AIRCRAFT LEFT GALLEY AIR VENT. THE APPROPRIATE CIRCUIT BREAKERS WERE PULLED AND THE ODOR DISSIPATED. FLIGHT CONTINUED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED THE LEFT AFT COFFEE MAKERS. FOUND EVIDENCE OF BURNED COFFEE. CLEANED AREA AND INSTALLED THE ORIGINAL COFFEE MAKERS. OPERATIONALLY CHECKS OK. 2L72 4F RTA2NM 20050816002062005081600206NM 2005 8 16 DHLA05740016 120050811A3231 DOOR BOEING727 7272Q9 138448MNM NLG OUT OF ADJUST A DHLAO OTHER J WARNING INDICATION DEDESCENT 1 SO01740DH NOSE GEAR DOOR LIGHT ILLUMINATED DURING DESCENT. PERFORMED ABNORMAL LIGHT REMAINED EXTINGUISHED WITH GEAR HANDLE IN UP POSTION. ADJUSTED NOSE GEAR DOORS, SWUNG NOSE GEAR, CK NORMAL PER MM 32-22-1 2L73 4F RTA3WE 20050816002192005081600219EA 2005 8 16 ASOA05620 120050722A53006003603031 FRAME CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27833AS 7246 DURING C-CHECK, THE FUSELAGE FRAME AND DOUBLER AT FS 718, STRINGER 10-12 LT SIDE WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FUSELAGE FRAME AND DOUBLER AT FS 718, STRINGER 10-12 LT SIDE IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050817000132005081700013WP 2005 8 17 MWEA050078 120050815A5347593056673 SEAT TRACK DOUG DC9 DC981 3022081WP CABIN CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 MAIN CABIN, LEFT OUTBOARD SEAT TRACK STATION 1105 TO 1117 IS CORRODED. FABRICATED AND INSTALLED SEAT TRACK. 2L72 4F A6WE 20050817000162005081700016WP 2005 8 17 MWEA050081 120050815A5320993653437 FLOOR SUPPORT DOUG DC9 DC981 3022081WP STA 1155 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 MAIN CABIN, FRAME FLOOR SUPPORT BETWEEN INBOARD AND OUTBOARD, SEAT TRACK AT STATION 1155 CORRODED. FABRICATED AND INSTALLED FLOOR. 2L72 4F A6WE 20050817000242005081700024CE 2005 8 17 DJFA2005129 120050812A2997 WIRE HARNESS BEECH MU300 400A 1155402CE TRANSDUCER BROKEN E DJFAA UNSCHED LANDING O OTHER DEDESCENT 1 EA23440CW 67839132 RK40 ON DESCENT, CREW NOTICED HYDRAULIC SYSTEM PRESSURE WAS INDICATING TOO HIGH. THE HIGH HYDRAULIC SYSTEM PRESSURE CHECKLIST REQUIRES A NO FLAP LANDING AND USE OF EMERGENCY BRAKES TO STOP THE AIRCRAFT. EMERGENCY DECLARED. DUE TO IT'S LONGER RUNWAY LENGTH, ACFT DIVERTED TO KORF FOR LANDING. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE HYDRAULIC PRESSURE TRANSDUCER AND REPAIRED A BROKEN WIRE IN THE TRANSDUCER WIRING HARNESS. THE LANDING GEAR WAS CYCLED SEVERAL TIMES TO BLEED THE HYDRAULIC SYSTEM. THE BRAKES WERE BLED AND THE NITROGEN BOTTLE WAS SERVICED. OPERATIONAL CHECKS OF THE HYDRAULIC INDICATION SYSTEM AND LANDING GEAR SYSTEMS WERE NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4F RTA16SW 20050817000322005081700032WP 2005 8 17 ASAA0580360 120050717A532199365485 FLOOR PANEL DOUG DC9 DC983 3022083WP FS 200-237 DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02944AS 53019 OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL DELAMINATED. REBONDED FIBERGLASS. (M) 2L72 4F RTA6WE 20050817000492005081700049WP 2005 8 17 UPS05845188 120050720A52302772981 HINGE PIN DOUG DC8 DC873F 302199FWP CARGO DOOR WORN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE:C1 REMOVE MAIN CARGO DOOR HINGE TO ACCOMPLISH FWD HINGE REPLACEMENT, CRACKED, FOUND DURING DOUBLER REMOVAL. REMOVED MAIN CARGO DOOR AND HINGE, MAG PARTICAL, HFEC AND FPI INSPECT IONS ACCOMPLISHED, NO CRACKS NOTED. REINSTALLED HINGE, REPLACED HINGE PINS 2 EA AND INSTALLED DOOR IAW MM 52-36-01-4, SRM 51-3-0, 51-1-21, DPS 4.704, NDTSPM 06-10-01.001 AND DPS4.707. 2L74 4F RT4A25 20050817000522005081700052WP 2005 8 17 UPS05845194 120050802A53404758514519 FITTING DOUG DC8 DC873F 302199FWP FS1230 L34-35R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 INSPECTION TYPE:C1 -C- PIT STA 1230 BETWEEN L34R TO L35R FITTING CRACKED AROUND FASTENERS . REMOVED, FABRICATED, AND INSTALLED FITTING IAW DWG 4758514 AND DC-8 SR M 51-1-20D. 2L74 4F RT4A25 20050817000542005081700054 2005 8 17 BAQ2005F00002 420050721A3400 ANTENNA AGUSTAA109 A109E 0260119EU TMECA ARRIUSARRIUS2K1 NE NAVIGATIONAL FAILED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA037YL 11502 FAILURE MODE OF ANTENNA IS (RT ELEMENT BECOMES EXTREMELY WEAK) WHICH CAUSES NAV INDICATOR DISPLAY ERRORS OF UP TO 5 DEGREES. VISUAL INSPECTION INDICATES THAT RT NAV ANTENNA ELEMENT IS EXPOSED TO A MUCH HIGHER TEMPERATURE THEN LT ELEMENT. RECENT FLIGHT PERFORMED WITH TEMPERATURE STRIPS AFFIXED TO AIRCRAFT PROVE THIS AS FACT. TEMP STRIPS ON RT SIDE OF AIRCRAFT INDICATE A TEMPERATURE (IN FLIGHT) IN EXCESS OF 199 DEGREES F. DESIGN LIMIT FOR THIS ANTENNA IS 185 DEGREES F, PER THE MFG. (SEE ATTACHED PHOTOS AND EMAIL). RECOMMENDATIONS INCLUDE USING AN ANTENNA SUITABLE FOR HIGHER TEMP EXPOSURE OR RELOCATING ANTENNAS TO FUSELAGE, AWAY FROM EXHAUST. (K) 1G72 3U3 URTH7EU E34NE 20050817000572005081700057NE 2005 8 17 H3V2005F00000 220050719A7230566281 STATOR SKRSKYS64 CH54A 8142501NE PWA JFTD12JFTD12A4A 52047NE COMPRESSOR DAMAGED L H3VLO OTHER O OTHER NRNOT REPORTED 1 WP1744094 6718421 FOD DAMAGE FROM RIVETS OF THE 1ST STAGE STATOR REAR AIRSEAL (2ND STAGE) DAMAGED THE COMPRESSOR BLADES. THIS CAUSED A STALL AND THE T5 TEMP ROSE TO 1000 DEGREES C INSTANTLY, CAUSING SEVERE TURBINE AND FREE TURBINE BLADES, VANES, AND SEALS DAMAGE. THE AIRCRAFT ENGINE WAS REMOVED, DISASSEMBLED, AND INSPECTED. DURING THIS DISASSEMBLY AND INSPECTION, THE DAMAGE WAS DISCOVERED. THE INCIDENT HAPPENED UPON LANDING. (K) 2G72 4U4 U H16NM E15EA 20050817000612005081700061WP 2005 8 17 ASAA0580372 120050717A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP CABIN DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02944AS 53019 OKC - DURING HV-CHECK, FOUND CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050817000702005081700070NM 2005 8 17 AALA20050524 120050812A3350 BATTERY PACK BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21344AN 33083 DFW - RIGHT HAND EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT M731 FOR RIGHT HAND EXTERIOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050817000712005081700071NM 2005 8 17 AALA20050519 120050811A3350 LIGHT BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21622AA 24580 DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT 36D INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT 36D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050817000722005081700072WP 2005 8 17 AALA20050521 120050810A3350 CHARGER DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21271AA 49293 DFW - CEILING EMERGENCY LIGHTS ABOVE AFT STAIR DOOR INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY FOR CEILING EMERGENCY LIGHTS ABOVE AFT STAIR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050817000752005081700075NM 2005 8 17 AALA20050515 120050804A3350D71701100 BATTERY PACK BOEING737 737823 13844BZNM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21944AN 29535 TUL - EMERGENCY LIGHT BATTERY PACK IN RIGHT HAND FORWARD CABIN OF OVERWING ESCAPE HATCH AT STATION 569 RIGHT INOPERATIVE. REPLACED BATTERY PACK 5826 FOR EMERGENCY LIGHT IN RIGHT HAND FORWARD CABIN OF OVERWING ESCAPE HATCH. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20050817000802005081700080WP 2005 8 17 AALA20050517 120050810A3250NAS110420D BOLT DOUG DC9 DC982 3022082WP NLG STEERING SHEARED A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21415AA 49326 LAX - INFLIGHT UNABLE TO RAISE LANDING GEAR AFTER TAKEOFF. NOSE STEERING WAS MOVABLE BOTH DIRECTIONS. AIRPLANE GROUND SHIFT DID NOT OCCUR. GEAR HANDLE WOULD NOT RAISE. FOUND NOSE LANDING GEAR GROUND SENSING MECHANISM ATTACH BOLT SHEARED AT LOWER SPRING BRACKET. REPLACED BOLT AND CYCLED GEAR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050817000812005081700081GL 2005 8 17 HDNR200500001 220050804A726023008021 HOUSING ALLSN C20B BOLKMS105 BO105CBS 5626008EU ALLSN 250C 250C20B 03013GL GEARBOX DEBONDED B HDNAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SW03911E CAG38994 S812 CAE836263 OIL NOT SCAVENGING. OIL EMPTIED FROM AIRCRAFT TANK TO ENGINE GEARBOX DURING GROUND OPERATION. FOUND THAT THE SEALANT THAT SOME OVERHAUL VENDORS PUT IN THE BACK OF THE LOWER RIGHT COMPRESSOR MOUNT INSERT, INSIDE THE GEARBOX HOUSING, HAD FALLEN OUT AND PLUGGED THE SCAVENGE PICK-UP IN THE BOTTOM OF THE GEARBOX. HOUSING HAD 284.7 HRS TSO. 1G72 3U3 UNCH3EU E4CE 20050817000832005081700083SO 2005 8 17 CHQA200500140 120050813A3260 PROXIMITY SENSOR EMB 145 EMB145LR 3260212SO NLG CONTAMINATED A CHQAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL11291SK 145486 FLIGHT 3320 CHS-CLT - ON TAKEOFF, RIGHT AT ROTATION, RECEIVED AN LND AIR/GND/FAIL EICAS MESSAGE. THE LANDING GEAR WOULD NOT RETRACT. THE EICAS INDICATED THREE GEAR DOWN AND LOCKED. TOWER CHECKED THE UNDERCARRIAGE TO CONFIRM ALL THE GEAR WAS DOWN. RETURNED FOR LANDING IN CHS WITHOUT EVENT. AN EMERGENCY WAS DECLARED, HOWEVER THE RESPONSE WAS CANCELLED ONCE THE AIRCRAFT LANDING SAFELY AND EXITED THE RUNWAY. MAINTENANCE INSPECTED ALL FIVE PROXIMITY SENSORS AND CONNECTORS. ALL LOOKED GOOD EXCEPT FOR THE NLG PROXIMITY SENSOR WAS COVERED IN A VERY THICK GREASE. CLEANED THE SENSOR AND TOOK THE AIRCRAFT ON A TEST FLIGHT. AIRCRAFT PASSED ALL CHECK FLIGHT TESTS. 2L72 4T RTT00011AT 20050817000862005081700086WP 2005 8 17 IXXA05SMN151S 120050630A5730 SKIN PANEL DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE XFS38.750-70.000CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, LT WING. SLANT PANEL UPPER PART CORRODED, XFS 38.750 - XFS 70.000. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG. 37, EO NR 20051004 DATE 06-16-05. REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1, SRM 51-1-20D PAGE 21. SMOOTHED AND PERFORMED BLEND OUT TO CORRODED AREA IAW SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1. FABRICATED REPAIR DOUBLER (ALCLAD 7075 T6 0.125) IAW SRM 57-2-1 FIG. 37. CLEANED, TREATED AND PRIMED AREA AND REPAIR DOUBLER INTERNAL PART (NEW) IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-12. INSTALLED REPAIR DOUBLER AND NEW FASTENERS IAW SRM 57-2-1 FIG. 37, SRM 51-1-21 PAGE 1, SRM 51-1-20D PAGE 9. TORQUED IAW SRM 51-3-1. 2L74 4F4 FRT4A25 E2GL 20050817000942005081700094CE 2005 8 17 DXTA200500897 120050811A2170 COALESCER BAG CESSNA750 750 2076810CE CONTAMINATED E DXTAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL07979QS 7500079 APPROX 2 MINUTES AFTER THE APU WAS STARTED ON THE GROUND, THE COCKPIT AND CABIN BEGAN FILLING WITH ENVIROMENTAL TYPE SMOKE THE COCKPIT PAC WAS IN THE OFF POSTION AS REQUIRED BY THE MEL. THE CABIN PAC WAS ON AND THE ISOLATION VALVE WAS OPEN. THE COCKPIT SUPPLY TEMP WAS NOTICED TO BE 187 AND CLIMBING RAPIDLY THE PAC AND APU ANS ENTIRE AIRCRAFT WERE ALL QUICKLY SHUT DOWN. REMOVED WATER SEPARATOR COALESCER CLOTH AND CLEANED. REINSTALLED RAN APU AND OPS CHECKED. NORMAL OPS WORK IAW CESSNA 750 M/M CHPT 49-10-00. 2L72 4J RTT00007WI 20050817001122005081700112EU 2005 8 17 BMAC050010 120050806A7712 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33110UG 01514WP RT ENGINE DIRTY A B16AO OTHER N FALSE WARNING CLCLIMB 1 SO29530PA 732 ERATIC TORQUE +/- 4 PERCENT RT ENGINE INDICATION. MAINTENANCE CLEANED PLUG AT DELTA P/P TRANSDUCER IAW J31 MM 76-10-21, PERFORMED ENGINE RUN, OPS CHECKED GOOD AT THIS TIME. 2L72 4T4 TRTA41NM E4WE 20050817001182005081700118WP 2005 8 17 ASAA0580386 120050718A5210995576317 INTERCOSTAL DOUG DC9 DC983 3022083WP FS 185 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02944AS 53019 OKC - DURING HV CHECK, FOUND MAIN PASSENGER L1 DOOR INTERCOSTAL CRACKED IN RADIUS. REPLACED INTERCOSTAL. (M) 2L72 4F RTA6WE 20050817001232005081700123 2005 8 17 SF200508121 420050812A3460 BATTERY SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE COCKPIT ODOR A UHLAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 GL17121CQ 121 VERY STRONG ELEC ODOR COMMING FROM COCKPIT BATTS/EXT POWER AND AVIONICS ON, MFD C/B G18 POPPED AFTER 30 SECS OF NOTICING ODOR. CONTRACTED MAINTENANCE, PULLED AND CAPPED C/B. MAINT CONFIRMED SMELL COMING FROM MFD. 2L72 4T4 TRTA52EU E8NE6 20050817001262005081700126WP 2005 8 17 ASAA0580388 120050718A532059101419 PAN DOUG DC9 DC983 3022083WP FS 425 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02944AS 53019 OKC - DURING HV CHECK, FOUND FORWARD CARGO BAY DOOR PAN CRACKED IN AFT SIDE. STOP DRILLED CRACK. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050817001272005081700127NE 2005 8 17 AJC2005F00011 220050722A73213587502 BEARING ISRAEL1125 ASTRASPX 4500205EU GARRTTTFE731TFE73140 29001NE NR 6 FAILED E AJCAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 EA25387PA800 145 P113241 CREW REPORTED DEPARTURE, ENROUTE, RT ENGINE DEEC COMPUTER TRIPPED TO MANUAL MODE, FOLLOWED BY THE LOSS OF THE N1 GGE INDICATION. FLIGHT CONTINUED NORMALLY, THEN EXPERIENCED A RT ENGINE VIBRATION WHICH CLIMBED TO .8 ON THE VIBRATION INDICATOR. REDUCED PWR ON RT ENG TO 75 PERCENT. VIBRATION STOPPED. FLEW AC AT REDUCED PWR AND DIVERTED FOR MAINT WHERE THEY LANDED SAFELY WITHOUT INCIDENT. CREW DID NOT DECLARE EMERGENCY. ENG WAS SENT TO MFG FOR REPAIR, DETERMINED THAT THE NR6 BEARING FAILED DUE TO OIL STARVATION. NR 6 BEARING WAS REPLACED WITH OTHER COMPONENTS AND ENG WAS RETURNED TO SERVICE. 2L72 4F4 FRTA16NM E1NM 20050817001352005081700135WP 2005 8 17 ASAA0580397 120050725A5320993053866 CUSP WEB DOUG DC9 DC983 3022083WP FS 237-313 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02947AS 53020 OKC - DURING C-CHECK, FOUND RIGHT CUSP WEB CORRODED. REMOVED CORRODED SECTION. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050817001492005081700149NM 2005 8 17 USAA050970 120050803A5330 SKIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU STA 727D, S23L CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19449US 24893 CLT - Q1 - SKIN, 1 INCH CRACK, STA 727D, BELOW S-23L (NEAR LIGHT). CUT OUT CRACK, FABRICATED DOUBLER AND FILLER, INST 12 INCH X 12 INCH DOUBLER IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050817001512005081700151WP 2005 8 17 ASAA0580404 120050719A532199579185 FLOOR PANEL DOUG DC9 DC983 3022083WP FS 465-541 CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02947AS 53020 OKC - DURING C-CHECK, FOUND CABIN FLOOR PANEL HAS CHAFE MARKS ON LOWER SURFACE BONDED STIFFENER. REPLACED STIFFENER. (M) 2L72 4F RTA6WE 20050817001522005081700152NM 2005 8 17 USAA050987 120050805A5315 FLOORBEAM BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU CABIN CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19444US 24886 BFM, Q2, TEE CHORD, .5 INCH CRACK, CABIN FLOORBEAM AT STA 312 RBL 35. FABRICATED NEW UPPER CHORD, LOCATED DRILLED AND INSTALLED ALL REPAIR PARTS IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050817001542005081700154NM 2005 8 17 USAA050903 120050727A5330 SKIN BOEING737 737401 1384701NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19404US46134 23886 CLT - C1 - FUSELAGE SKIN, .75 INCH CRACK, GROUND AIR SERVICE CONNECTION DOOR CUTOUT AT AREA BETWEEN BS 520-BS 540. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED IAW EA. (K) 2L72 4F4 FRTA16WE E21EU 20050817001552005081700155NM 2005 8 17 USAA050904 120050727A5322 SHEAR TIE BOEING737 737401 1384701NM CFMINTCFM56 CFM563B2 13802EU STA 867 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19404US46134 23886 CLT - C1 - SHEAR TIE, .3125 INCH HOLE, 4.5 INCH CORROSION, STA 867 BOTTOM OF FUSELAGE BETWEEN SHEAR TIE AND SKIN. REMOVED CORRODED SHEAR TIE AND REPLACED WITH NEW SHEAR TIE. (K) 2L72 4F4 FRTA16WE E21EU 20050817001592005081700159EU 2005 8 17 MAC8501 120050812A243430E221G GENERATOR FOKKERF27 F27MK500 4990629EU NR 2 FAILED A MTNAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO33713FE 1194 10615 ON TAKEOFF FROM POA, THE NR 2 GENERATOR OVERHEAT LIGHT ILLUMINATED. THE PIC DECLARED AN EMERGENCY AND RETURNED TO POA WITHOUT INCIDENT. THE A/C LANDED 100 LBS OVERWEIGHT WITH A SMOOTH LANDING. AFTER LANDING AND TAXIING TO THE RAMP, THE RIGHT NACELLE WAS INSPECTED AND NO SIGNS OF FIRE WERE FOUND. THE GENERATOR WAS CHANGED AND THE A/C RETURNED TO SERVICE. 2H72 4T A817 20050817001762005081700176WP 2005 8 17 ABXA050182 120050803A573059205212 PANEL DOUG DC9 DC933F 302207AWP PWA JT8 JT8D7B 52053NE LT WING DEBONDED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23933AX 47291 LT WING OB UPPER TRAILING EDGE PANEL HAD SKIN DAMAGE AT STA. XRS 516. SKIN DEBONDED AND ROLLED BACK FROM THE LEADING EDGE PANEL. DAMAGED AREA MEASURED 6 INCHES LONG BY 18 INCHES WIDE. DEFERRED: NR 45199. TEMP REPAIRED IAW REA D957-52280. CLEARED: DI NR 45199. REPAIRED BONDED PANEL IAW SRM 57-30-2 AND 57.01 FIG 3 SHEET 2. 2L72 4F4 F A6WE E2EA 20050817001772005081700177EU 2005 8 17 USAA050891 120050718A53101160852 BEAM AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19109UW 1065 FOUND BEAM CORRODED 1 INCH BY 1 INCH BY .100 INCH DEEP, FORWARD CABIN TOP OF BEAM AT CENTER LINE A C16. CORROSION LEVEL 1, TASK JA-220-53500. REMOVED AND REPLACED BEAM, REPLACED WITH IDENTICAL PART NR. (M) 2L72 4F4 FRTA28NM E38NE 20050817001852005081700185EU 2005 8 17 KBM2005F00174 120050421A2910POLYV597K41619 BELT SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE HYD SYS CRACKED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH 2337 HYDRAULIC BELT, CRACKED AND SPLIT (LONGITUDE) OVER HALF CIRCUMFERENCE, REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20050817001982005081700198NM 2005 8 17 ASAA0540338 120050703A57536546430129 SKIN BOEING737 7374Q8 138447QNM TE FLAPS DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02775AS 25108 OKC - FOUND LEFT INBOARD FORE FLAP HAS 2 EACH GROUPS OF DENTS ON LOWER SURFACE. FILLED DENTS, FABRICATED AND INSTALLED SKIN DOUBLERS IAW 737-400 SRM 51-70-10 REPAIR 2. (M) 2L72 4F RTA16WE 20050817002002005081700200 2005 8 17 KBM2005F00182 420050627A34225050010902 GYRO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1B 6OO30NE DIRECTIONAL MALFUNCTIONED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH 2957 DIRECTIONAL GYRO FLAG ON. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050817002042005081700204NM 2005 8 17 2005UALA00614 120050705A5330 SKIN BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE MISREPAIRED A UALAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP29175UA 24382 EXISTING DOUBLER NOT PER SRM OR MM, STATION 1720-1740 AND STRINGER 38R-40R. MJR RPR, EXISTING DOUBLER NOT PER SRM OR MM, STA 1720- 1740, AND STR 38R-40R. DOUBLER REMOVED; ACCOMP HFEC INSP, NO CRACKS NOTED, REF NDT PART 6, 53-00-01. FABBED DOUBLER AND INSTALLED PER SRM 53-00-01, FIG 201. LESS THAN 5 LB SKIN TRIM OUT 3 BY 5 INCH, 2 INCH ABOVE SKIN LAP AT STR 40R. 2L74 4F4 FRTA20WE E24NE 20050817002052005081700205NE 2005 8 17 2005UALA00770 220050805A7230 COMPRESSOR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 2 ENGINE STALLED A UALAEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 WP29409UA 462 V10670 ON CLIMB-OUT, NR 2 ENGINE COMPRESSOR STALLED. SHUT DOWN NR 2 ENGINE. 2L72 4F4 FRTA28NM E40NE 20050817002092005081700209NM 2005 8 17 2005UALA00774 120050806A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE STA 1400, STR 26DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29587UA 26713 AFT PIT FRAME DENTED STA 1400, STR 26L. TRIMMED OUT DAMAGE, ACP HFEC INSP, NO CRACK FOUND. FABRICATE REPAIR ANGLE PER TIMCO REO- G10758, REV B, AND UA EVA-50516. 2L72 4F4 FRTA2NM E17NE 20050818000052005081800005NM 2005 8 18 DHL2005747506 120050814A5322 SHEAR TIE BOEING727 727224 1384076NM BS 970 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01747DH 22253 CORROSION ON AFT PIT FRAME AT BS 970 STR 28R - 29R. REMOVED FLOOR SUPPORT AND VERTICAL STIFFENER BS 930 - 990. ANGLE SHEAR TIE FOUND 100 PERCENT MATERIAL LOSS. CUT OUT CORRODED AREA OF ANGLE SHEAR TIE. FABRICATED AND INSTALLED SHEAR TIE REPAIR 6 X 1 X 1 INCH FROM 7075-T6 .063 IAW B727 SRM 51-10-2, 51-30-2, 53-10-4 FIG 13. 2L73 4F A3WE 20050818000832005081800083SW 2005 8 18 ALG2005F00047 120050718A7712407375003107 INDICATOR BELL 407 407 1182206SW ALLSN 250C 250C47B GL TORQUE ODOR E ALGAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW03436AL 53069 IN CRUISE FLIGHT, 4 MINUTES FROM LANDING, THE TORQUE INDICATOR WENT BLANK, 1 MINUTE LATER THE PILOT COULD SMELL PLASTIC BURNING IN THE COCKPIT. THE PILOT LANDED AND NOTIFIED MAINTENANCE. MECHANIC REMOVED AND REPLACED THE TORQUE GAUGE AND AC WAS RETURNED TO SERVICE, UPON COMPLETION OF THE OPERATIONAL CHECK. (K) 1G71 3U3 UO H2SW E1GL 20050818000842005081800084SW 2005 8 18 ALG2005F00050 120050721A6210 BLADE BELL 206 206L1 1182107SW ALLSN 250C 250C30P 03013GL MAIN ROTOR BIRD STRIKE E ALGAO OTHER C F.O.D. TXTAXI/GRND HDL 1 SW035759M 45555 PRIOR TO TAKEOFF, AFTER INCREASING THE COLLECTIVE FOR TAKEOFF, A SEAGULL STRUCK THE LEADING EDGE OF THE M/R BLADE, THE PILOT SHUT THE AC DOWN AND NOTIFIED MAINTENANCE. THE MECHANIC INSPECTED THE M/R BLADES IAW MM. AC WAS RETURNED TO SERVICE. (K) 1G71 3U3 U H2SW E1GL 20050818000872005081800087SW 2005 8 18 ALG2005F00049 120050717A28222C271 PUMP BELL BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL LT FUEL BOOST INTERMITTENT E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03343AL 51372 IN CRUISE FLIGHT, PILOT NOTICED THAT LT BOOST PUMP IS INTERMITTENT. UPON LANDING THE MECHANIC REMOVED AND REPLACED THE LT FUEL BOOST PUMP AND AC WAS RETURNED TO SERVICE AFTER COMPLETION OF OPERATIONAL CHECKS IAW MM. (K) 1G71 3U3 U H2SW E1GL 20050818000882005081800088SO 2005 8 18 TZR2005F00029 220050712A8530AEC520TI CYLINDER CESSNA401 401A 207590DCE CONT O520 TSIO520EB 17040SO ENGINE CRACKED E TZRAO OTHER O OTHER NRNOT REPORTED 1 SW05409TE1200 401A0118 CRACKED BETWEEN SPARK PLUG BOSS AND EXHAUST CYLINDER. TYPICAL OF THE CYLINDERS. (K) 1L72 3O3 O A7CE E8CE 20050818000902005081800090EU 2005 8 18 KBM2005F00190 120050421A2910704A34412033 LINE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE HYDRAULIC SYS LEAKING E KBMAO OTHER K FLUID LOSS NRNOT REPORTED 1 WP19751H 3403 HYDRAULIC LINE LEAKING. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050818000972005081800097NM 2005 8 18 USAA050916 120050729A5315 FLOORBEAM BOEING757 7572B7 1384964NM RROYCERB211 RB211535* NE STA324, RBL40-46CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19628AU 27806 BFM - C3 - FLOORBEAM CAP, 6 INCHES L X 2.5 INCHES W X .05 INCH, CORROSION; NO LEVEL OR TASK, STA 324, RBL 40-46. REPAIRED IAW SRM AND EA. (K) 2L72 4F4 FRTA2NM E12EU 20050818001002005081800100SW 2005 8 18 ALG2005F00051 120050723A3212209075323001 RELAY BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL FLOAT SYSTEM FAULTY E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW031078Y 2924 DURING THE SECOND TOUCH DOWN OF THE DAY, FLOATS INFLATED WITHOUT ANY INPUT FROM THE PILOT. THE MECHANIC REMOVED AND REPLACED THE FAULTY RELAY AND THE AC WAS RETURNED TO SERVICE UPON COMPLETION OF SYSTEM CHECKS. (K) 1G71 3U3 U H2SW E4CE 20050818001022005081800102SW 2005 8 18 ALG2005F00048 120050720A6340407040006103 TRANSMISSION BELL 407 407 1182206SW ALLSN 250C 250C47B GL MAIN ROTOR MAKING METAL E ALGAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW03796RV 53037 IN FLIGHT TRANSMISSION, CHIP LIGHT ILLUMINATED, UPON LANDING THE MECHANIC CLEANED THE TRANSMISSION CHIP PLUGS IAW MM AND DURING THE GROUND RUN AND LEAK CHECK TRANSMISSION CHIP LIGHT ILLUMINATED ONCE AGAIN. THE MECHANIC REMOVED AND REPLACED THE TRANSMISSION. (K) 1G71 3U3 UO H2SW E1GL 20050818001032005081800103GL 2005 8 18 ALG2005F00052 220050724A7230 COMPRESSOR BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL ENGINE STALLED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03351AL 51431 DURING TAKEOFF AT 95 PERCENT TORQUE, OAT +34, WINDS CALM, AC HAD A COMPRESSOR STALL FOLLOWED BY A LOUD BANG, YAW, AND A DROP IN TORQUE. THE PILOT REDUCED POWER LEVELED AT 50 FT AT 70 KNOTS 50 PERCENT TORQUE, FLEW 8 MINUTES TO A LARGER PLATFORM AND LANDED. THE MECHANIC INSPECTED THE ENGINE INTAKE AREA, COMPRESSOR BLADES, BLEED VALVE NO DEFECTS WERE NOTED. SUBSEQUENT FLIGHT CHECK WAS UNEVENTFUL AND THE AC WAS RETURNED TO SERVICE. (K) 1G71 3U3 U H2SW E1GL 20050818001062005081800106 2005 8 18 KBM2005F00183 420050726A233010000 ENTERTAIN SYS SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE DMP100 INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19250SH439 3874 DMP-100, UNIT INOPERATIVE, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050818001082005081800108EU 2005 8 18 KBM2005F00184 120050724A2842647510033 PROBE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE FUEL SYS INACCURATE A KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19351WM 2167 FUEL PROBE, FUEL GAUGE READS INACCURATE. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050818001102005081800110EU 2005 8 18 KBM2005F00189 120050421A2910704A34412036 LINE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE HYDRAULIC SYS LEAKING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19751H 2459 3403 HYDRAULIC LINE LEAKING, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050818001152005081800115SW 2005 8 18 ALG2005F00056 120050730A2910 LINE BELL 214 214ST 1182106SW GE CT7TS CT72A 30030NE NR 1 HYD SYS LEAKING E ALGAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW03390AL 28198 ENROUTE, A HOWLING NOISE STARTED AND BECAME LOUDER, THE PILOT NOTICED NR 1 HYD PRESSURE FLUCTUATED BETWEEN 200-300 PSI. THE PILOT TURNED OFF NR 1 HYD NOISE WENT AWAY. UPON LANDING THE MECHANIC FOUND NR 1 PRESSURE LINE TO THE COLLECTIVE SERVO IS LEAKING. HE TIGHTENED THE LINE AND REPLACED THE HYD PUMP ASSY AND THE AC WAS RETURNED TO SERVICE UPON COMPLETION OF FUNCTION CHECKS IAW MM. (K) 2G72 4U4 U H10SW E8NE 20050818001162005081800116NM 2005 8 18 ASAA0540327 120050626A5330654653120 SKIN BOEING737 7374Q8 138447QNM FS 500F CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 YXX - BS 500F CORROSION ON SKIN TO FRAME ATTACHMENT AT STRINGER 27 AND 28 RT. BLEND AND CHECK LIMITS REPAIRED IAW 737-400 SRM 53-00-07 FIG 203. (M) 2L72 4F RTA16WE 20050818001182005081800118NM 2005 8 18 ASAA0540352 120050706A533065C323591 SKIN BOEING737 7374Q8 138447QNM FS 467-470 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 YXX - FOUND CORROSION AT ANTENNA LOCATION ON INSIDE OF SKIN AT BS 490, BL 0. REMOVED CORROSION AND REPAIRED PER EA 5330-01962. (M) 2L72 4F RTA16WE 20050818001202005081800120NM 2005 8 18 ASAA0540328 120050626A5330654659320 SKIN BOEING737 7374Q8 138447QNM FS 500A CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 YXX - FOUND BS 500A CORROSION ON SKIN TO FRAME ATTACH ANGLE BETWEEN 28L AND 28R CORRODED. ATTACH ANGLE REPLACED WITH FABRICATED REPAIR PART IAW 737-400 SRM. (M) 2L72 4F RTA16WE 20050818001212005081800121NM 2005 8 18 ASAA0540329 120050626A5330654653120 SKIN BOEING737 7374Q8 138447QNM FS 500B CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 YXX - FOUND BS 500B CORROSION ON SKIN TO FRAME ATTACHMENT BETWEEN 28L AND 28R CORRODED. REPAIRED IAW B737400 SRM 53-00-07 FIG 203. (M) 2L72 4F RTA16WE 20050819000032005081900003NM 2005 8 19 ASAA0540331 120050626A575465C3262012 SKIN BOEING737 7374Q8 138447QNM FORE FLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 YXX - FOUND RIGHT INBOARD FORE FLAP LOWER SIDE DENTED MID-SPAN. RIGHT INBOARD FORE FLAP LOWER SIDE REPAIRED IAW B737-400 SRM 51-70-10 REPAIR NR 7. (M) 2L72 4F RTA16WE 20050822000052005082200005EU 2005 8 22 USAA050983 120050805A53151161084 FLOORBEAM AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE C18, C24-Y1292 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19110UW13254 1112 PIT - S2 - FLOORBEAM, 2 INCH X 2 INCH, 2 INCH X 2 INCH, 1.5 INCH X .5 INCH, CORROSION; LEVEL 1; TASK JA-220-53500, BETWEEN C18 AND C24 - Y1292. DEFECTIVE PART REPLACED WITH IDENTICAL PART IAW SRM. (K) 2L72 4F4 FRTA28NM E38NE 20050822000102005082200010EU 2005 8 22 USAA050976 120050805A5320D5311141420000 FLOOR SUPPORT AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE 8INRT CTR,C20C21CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19110UW13254 1112 PIT - S2 - FLOOR SUPPORT, 1 INCH DIA, CORROSION; LEVEL 1; TASK JA-220-53500, FLOOR SUPPORT, 8 INCHES RT OF CENTER AT C-20 AND C-21. DEFECTIVE PART REPLACED WITH IDENTICAL PART IAW SRM. (K) 2L72 4F4 FRTA28NM E38NE 20050822000122005082200012EU 2005 8 22 KBM2005F00197 120050520A2120 MOTOR SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1 60030NE BLOWER BROKEN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19215LA460 2143 5 INCH BLOWER MOTOR, ONE BLOWER MOTOR BLADE BROKEN. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050822000142005082200014EU 2005 8 22 KBM2005F00206 120050521A21210500844 MOTOR SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE BLOWER UNSERVICEABLE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1937SH 2300 BRUSHES WORN BEYOND LIMITS, ARMATURE BEYOND LIMITS. REPLACED BLOWER MOTOR WITH SERVICEABLE UNIT. (K) 1G71 3U3 UNCH9EU E19EU 20050822000152005082200015EU 2005 8 22 KBM2005F00201 120050430A5510355A1305200303 STRUCTURE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE HORIZONTAL STAB CRACKED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19345SH 3345 HORIZONTAL STABILIZER, RT SIDE TOP IS CRACKED 5 INCHES IN LENGTH, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050822000162005082200016 2005 8 22 KBM2005F00195 420050521A310012444412 INDICATOR BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL TOT ERRATIC E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19188TV 2704 TOT INDICATOR INDICATING ERRATICALLY. REMOVED AND REPLACED. (K) 1G71 3U3 U H2SW E4CE 20050822000212005082200021NE 2005 8 22 KBM2005F00193 220050316A7210642790041 CONNECTOR SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE OIL PRESS TRANS LEAKING E KBMAO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 WP19115SH 3141 OIL PRESSURE TRANS, LEAKING FROM CONNECTOR PLUG. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050822000252005082200025EU 2005 8 22 KBM2005F00202 120050522A71601206502A ACTUATOR SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE ALT AIR DOOR FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19345SH 3345 ENGINE ALT AIR DOOR WILL NOT OPEN. INSTALLED NEW MOTOR. (K) 1G71 3U3 U H9EU E19EU 20050822000272005082200027EU 2005 8 22 KBM2005F00207 120050520A21210500846 MOTOR SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE BLOWER INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1937SH 1075 2300 7 INCH BLOWER MOTOR, BLOWING WARM AIR. REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20050822000292005082200029EU 2005 8 22 KBM2005F00210 120050416A3210350A38104020 CROSSBEAM SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1D NE ROTATED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1953SH 2009 CROSSBEAM ROTATING, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050822000302005082200030EU 2005 8 22 KBM2005F00211 120050423A7997 WIRE SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1D NE OIL TEMP PROBE BROKEN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1953SH 1620 2009 OIL TEMP PROBE TERMINAL BROKEN. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050822000392005082200039NM 2005 8 22 ASAA0540349 120050706A5320654653170 ANGLE BOEING737 7374Q8 138447QNM FS 500B CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 YXX - FOUND BS 500B SKIN TO FRAME ATTACHMENT CORRODED BETWEEN STRINGER 27L AND 28L. FABRICATED AND REPLACED REPAIR PART IAW B737-400 SRM 53-00-07 FIGURE 203. (M) 2L72 4F RTA16WE 20050822000402005082200040NM 2005 8 22 ASAA0540351 120050706A5322654653120 SHEAR TIE BOEING737 7374Q8 138447QNM FS 500B CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 YXX - FOUND BS 500B FRAME TO SKIN ATTACHMENT BETWEEN STRINGER 27R-28R IS CORRODED. REPAIRED IAW B737-400 SRM 53-00-07 FIG 203. (M) 2L72 4F RTA16WE 20050822000412005082200041NM 2005 8 22 ASAA0540332 120050626A53306545767193 SKIN BOEING737 7374Q8 138447QNM FS 370 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02775AS 25108 OKC - FOUND DENT IN FUSELAGE EXTERIOR SKIN AT BS 370 BELOW STRINGER 17L. REMOVED DAMAGED SKIN, FABRICATED AND INSTALLED DOUBLER IAW 737-400 SRM 53-00-01 FIG 23L. (M) 2L72 4F RTA16WE 20050822000422005082200042NM 2005 8 22 ASAA0540325 120050626A531057176917 WINDOW POST BOEING737 7374Q8 138447QNM FS 219.8 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 YXX - F/O`S NR 1 WINDOW OUTBOARD POST UPPER CORNER CRACKED. REPAIRED IAW 737-400 SRM 53-10-01 FIGURE 202. (M) 2L72 4F RTA16WE 20050822000432005082200043NM 2005 8 22 ASAA0540344 120050706A532069429494 SUPPORT BRACKET BOEING737 7374Q8 138447QNM FS 807 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 YXX - AFT CARGO PIT SUPPORT BRACKET CRACKED ON UPPER FLANGE AT BS 807 RBL 20. REPAIRED IAW B737-400 SRM 51-30-01. (M) 2L72 4F RTA16WE 20050822000462005082200046NM 2005 8 22 ASAA0540323 120050626A53476553844 CARGO TRACK BOEING737 7374Q8 138447QNM BS 847 CHIPPED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 YXX - AFT CARGO PIT FLOOR SUPPORT BEAM TIE DOWN TRACK CHIPPED OFF AT BS 847 LBL 18. REPAIRED IAW B737-400 SRM 53-00-53 FIGURE 202. (M) 2L72 4F RTA16WE 20050822000502005082200050NM 2005 8 22 QXEA200501180 120050816A5240 DOOR BOMBDRDHC8 DHC8402 1390042NM AFT SERVICE MALFUNCTIONED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09415QX 4081 PDX FLIGHT #2308: AFT SERVICE DOOR WILL NOT OPEN. MAINTENANCE OPENED DOOR AND OPS CHECKED NUMEROUS TIMES PER AMM TASK 54-41-00-720-802. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050822000512005082200051NM 2005 8 22 QXEA200501173 120050813A6120 AUTOFEATHER SYS DHAV DHC8 DHC8202 2809007NM NR 2 ENGINE OUT OF RIG A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09353PH 496 NR 2 PROP WILL NOT AUTO FEATHER FOR AUTO FEATHER TEST. TORQUE DROPS BUT NO POWER UPTRIM OR ALTERNATE FEATHER LIGHT. MAINTNEANCE CHECKED NR 2 ENGINE HARNESS FOR LOOSE CONNECTIONS. NONE NOTED. CHECKED ENGINE CONDITION PANEL FOR FAULTS. NONE NOTED. COMPLIED WITH AUTO FEATHER AND POWER UPTRIM TEST IAW DHC8/200 ENGINE RIGGING MANUAL, PART 3, PAGES 3-63 THROUGH 3-65. AUTO FEATHER AND POWER UPTRIM TEST NORMAL. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050822000532005082200053NM 2005 8 22 QXEA200501174 120050814A2920 WARNING LIGHT DHAV DHC8 DHC8202 2809007NM HYD PRESSURE ACTIVATED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09345PH 476 DURING AFTER START CHECKLIST "STBY HYD 1" GAUGE DID NOT SHOW PRESSURE. RECYCLED SWITCH, STILL NO PRESSURE. BROUGHT THE FLAPS UP, NR 1 SHOWED FULL PRESSURE. RECYCLED SWITCH, SHOWED NO PRESSURE. MAINTENANCE INSPECTED AIRCRAFT CONTACTOR BOX WIRING FOR ANY NOTICEABLE CHAFING OR LOOSE CONNECTIONS. NO DEFECTS NOTED. GROUND RAN AIRCRAFT, CYCLED NR 1 STANDBY HYDRAULIC PUMP SWITCH AND CYCLED FLAPS. ALL INDICATIONS CHECK NORMAL. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050822000542005082200054NM 2005 8 22 QXEA200501179 120050816A2497 WIRE DHAV DHC8 DHC8202 2809007NM NR 2 AC GEN CHAFED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09348PH 484 NR 2 AC GENERATOR CAUTION LIGHT ILLUMINATED ON TAXI OUT. MAINTENANCE INSPECTED AIRCRAFT CONTATOR BOX. FOUND WIRE CHAFED BARE AT 2421 TB2-1A AND EXPOSED WIRE AT TERMINAL END OF CB8 WIRE 2005DA22A-1. REPAIRED CHAFFED TERMINAL BLACK WIRE PER AMM 20-45-04. REPAIRED TERMINAL END PER AMM 20-45-05. COMPLIED WITH OPERATION CHECK OF AC SYSTEM PER AMM 24-21-00, PAGES 501-503. CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050822000642005082200064NM 2005 8 22 DU4R0508177 120050809A5315 FLOORBEAM BOEING757 757232 1384965NM CABIN CORRODED B DU4RK NONE O OTHER ININSP/MAINT 1 SO15624DL 22914 CORROSION RUNNING UNDER REPAIR DOUBLER AT STA. 377.7 LBL 59. 2L72 4F RTA2NM 20050822000652005082200065NM 2005 8 22 SWAA052476 120050816A324426123012 TIRE BOEING737 7377H4 1384404NM MLG WHEEL SEPARATED A SWAAO OTHER D INFLIGHT SEPARATION CLCLIMB 1 SW29725SW 27857 NR 3 MAIN TIRE TREAD SEPARATED. FOUND NR 3 KRUEGER FLAP, RIGHT INBOARD T/E AFT FLAP & RIGHT INBOARD T/E MIDFLAP DAMAGED. REMOVED AND REPLACED NR 3 & NR 4 MAIN TIRE/WHEEL ASSY, NR 3 KRUEGER FLAP & RIGHT INBOARD T/E AFT FLAP PER MM. REPAIRED RIGHT INBOARD T/E MIDFLAP PER SWA EA & SRM. 2L72 4F RTA16WE 20050822000662005082200066NM 2005 8 22 SWAA052477 120050817A3350MS155721 BULB BOEING737 7377H4 1384404NM FUSELAGE INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29755SA 27871 DURING SCHEDULED MV2 CHECK, FOUND LT AFT EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050822000672005082200067 2005 8 22 SWAA052478 420050817A2565NAS60426P FASTENER BOEING737 7377H4 1384404NM L1 DOOR SLIDE MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29781WN 30601 DURING SCHEDULED 5Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE COVER MISSING FASTENERS. INSTALLED FASTENERS PER SRM. 2L72 4F RTA16WE 20050822000682005082200068NM 2005 8 22 SWAA052466 120050817A3350101331 LENS BOEING737 7377H4 1384404NM MID CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29214WN 32486 DURING SCHEDULED RON CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM. 2L72 4F RTA16WE 20050822000692005082200069NM 2005 8 22 SWAA052467 120050817A2560PH22300L GLOWSTRIP BOEING737 7373H4 1384600NM CABIN DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29351SW 24572 DURING SCHEDULED SERVICE CHECK, FOUND FWD SECTION EEPLS PHOTO LUMINESCENT STRIP DAMAGED. REMOVED AND REPLACED STRIP PER MM. 2L72 4F RTA16WE 20050822000712005082200071 2005 8 22 SWAA052469 420050817A25655A33075 SLIDE BOEING737 7377H4 1384404NM R1 DOOR DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29471WN 32471 R1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATING LOW. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20050822000722005082200072NM 2005 8 22 SWAA052470 120050817A53116546539 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29612SW 27930 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CHORD CRACKED AT BS 616, LBL 65, WL 200. REPAIRED FRAME CHORD PER BFG ER. 2L72 4F RTA16WE 20050822000732005082200073NM 2005 8 22 SWAA052471 120050816A2560BR2013 GLOWSTRIP BOEING737 7373H4 1384600NM ROW 8 DEF WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29637SW 27710 DURING SCHEDULED C2 CHECK, FOUND EEPLS STRIP WORN AT ROW 8 DEF. REMOVED AND REPLACED STRIP PER MM. 2L72 4F RTA16WE 20050822000742005082200074NM 2005 8 22 SWAA052472 120050816A3350101073 LENS BOEING737 7373H4 1384600NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29645SW 28330 DURING SCHEDULED C4 CHECK, FOUND EMERGENCY EXIT LIGHT LENS MISSING ABOVE ROW 2 DEF. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20050822000752005082200075 2005 8 22 SWAA052473 420050817A2565D31354 SLIDE BOEING737 7373A4 1384585NM R2 DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 R2 DOOR EMERGENCY EVAC SLIDE COVER INTERFERING WITH RECYCLE BIN COMPARTMENT DOOR. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20050822000772005082200077NM 2005 8 22 USAA050986 120050805A5330 SKIN BOEING757 7572B7 1384964NM RROYCERB211 RB211535E4 54555NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19624VJ 27246 BFM - C3 - SKIN, 2.5 INCH X 2.0 INCH X .048 INCH, 2.0 INCH X 2.5 INCH X .037 INCH, CORROSION; NO TASK OR LEVEL, STA 490-493, S-27 TO S-28L, STA 500, S27-S28L. INSTALLED DOUBLER IAW EA AND SRM. (K) 2L72 4F4 FRTA2NM E12EU 20050822000832005082200083EA 2005 8 22 ASO2005F00008 120050722A53206003603023 DOUBLER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27833AS 7246 DURING A C-CHECK, THE FUSELAGE FRAME AND DOUBLER AT FS 718, STRINGER 10-12 LT SIDE WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FUSELAGE FRAME AND DOUBLER AT FS 718, STRINGER 10-12 LT SIDE IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050822000932005082200093WP 2005 8 22 IXXA05RNG028S 120050721A5740 SUPPORT FITTING DOUG DC8 DC862F 3021972WP ZONE 600 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW1171CX 670243317 45961 DURING ROUTINE "C" CHECK, RT WING OUTBOARD FLAP SUPPORT FITTING STA XF 219.498 WAS FOUND CRACKED (0.177"). REPAIR ACCOMPLISHED, STOP HOLE WAS DRILLED, ANGLE WAS FABRICATED AND INSTALLED IAW EWO ATI 57-018 & EO ATI-070405. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR. 2L74 4F 4A25 20050822000942005082200094EU 2005 8 22 IXXA0500096O 220050818A7261 LINE DOUG DC8 DC871F 302199DWP CFMINTCFM56 CFM563C1 13802EU OIL PRESSURE BROKEN A IXXAE ENGINE SHUTDOWN O OTHER CRCRUISE 1 SW11828BX89301405 45993 692264 DURING CRUISE FROM KBFI TO KTOL THE NR 2 ENGINE HAD LOSS OF OIL QUANTITY FOLLOWED BY LOSS OF OIL PRESSURE. CREW PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN. AIRCRAFT MAINTAINED OIL PRESSURE DURING DURATION OF FLIGHT AND THE CREW LANDED IN KTOL WITHOUT INCIDENT. MAINTANENCE FOUND BROKEN LINE AT OIL TRANSMITTER. MAINTENANCE REMOVED AND REPLACED THE OIL PRESSURE TRANMSMITTER LINE AND THEN RAN ENGINES. THE OPERATIONAL AND LEAK CHECK WERE GOOD IN ACCORDANCE WITH THE ERH AND GMM. AIRCRAFT WAS RETURNED TO SERVICE 2L74 4F4 FRT4A25 E21EU 20050822000952005082200095WP 2005 8 22 IXXA0500097O 120050818A7900D51P5410115 TUBE DOUG DC8 DC871F 302199DWP CFMINTCFM56 CFM563C1 13802EU ENGINE OIL BROKEN A IXXAE ENGINE SHUTDOWN O OTHER CLCLIMB 1 SW11828BX83903406 45993 692264 !DURING CLIMBOUT FROM KTOL TO KPHL THE NR 2 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED. PRESSURE WAS AT 14 PSI AND FLUCTUATING AND OIL QUANTITY DEPLETING SLOWLY. THE CREW PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN. CREW LANDED IN KPHL WITHOUT INCIDENT. MAINTENANCE FOUND OIL PRESSURE TRANSMITTER OIL SUPPLY TUBE BROKE AT FLANGE. MAINTENANCE REMOVED AND REPLACED TUBE. THE OPERATIONAL CHECK AND LEAK CHECK WERE GOOG PER ALL APPLICABLE MANUALS AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F4 FRT4A25 E21EU 20050822000972005082200097NE 2005 8 22 IXXA0500103O 220050819A7200 ENGINE DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE NR 2 MALFUNCTIONED A IXXAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SW11828BX83904408 45993 DURING CRUISE FROM KPHL TO KTOL THE NR 2 ENGINE FLUCTUATED EGT FOLLOWED BY A INSTANTANEOUS EGT TEMPERATURE INCREASE. OIL PRESSURE FLUCTUATED BUT NO LOSS. THE CREW PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN THEN LANDED IN KTOL WITHOUT INCIDENT. AN INSPECTION IS ON GOING. AS SOON AS INFORMATION IS AVAILABLE IT WILL BE PROVIDED. 2L74 4F4 FRT4A25 E2GL 20050822001032005082200103WP 2005 8 22 IXXA05RNG025S 120050721A5740 SUPPORT FITTING DOUG DC8 DC862F 3021972WP XF CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW1171CX 670243317 45961 DURING ROUTINE "0C" CHECK, RT WING INBOARD FLAP SUPPORT FITTING STA XF 97.6090 WAS FOUND CRACKED (0.2740"). REPAIR ACCOMPLISHED, STOP HOLE WAS DRILLED, ANGLE WAS FABRICATED AND INSTALLED IAW EWO ATI 57-015 & EO ATI-070105. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR. 2L74 4F 4A25 20050822001062005082200106WP 2005 8 22 IXXA05RNG031S 120050721A5740 SUPPORT FITTING DOUG DC8 DC862F 3021972WP PWA JT3D JT3D* 52039NE XF 409.664 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW1171CX 670243317 45961 DURING ROUTINE "0C" CHECK, RT WING OUTBOARD FLAP SUPPORT FITTING STA XF409.664 WAS FOUND CRACKED (LONG 1.570"). REPAIR ACCOMPLISHED, STOP HOLE WAS DRILLED, ANGLE WAS FABRICATED AND INSTALLED IAW EWO ATI 57-021 & EO ATI-070705. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR. 2L74 4F4 F 4A25 1E8 20050822001072005082200107WP 2005 8 22 IXXA05RNG039S 120050720A5730 SKIN DOUG DC8 DC862F 3021972WP XFA 603.750 CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW1171CX 670243317 45961 DURING A ROUTINE C CHECK INSPECTION FOUND SKIN CORROSION DAMAGE ON THE RT OUTER WING AT INBD EXTENDED L/E AROUND STA XFS 603.750REMOVED CORROSION DAMAGE, FABRICATED REPAIR DOUBLER AND INSTALLED IAW EWO ATI 57-031 & EO ATI-071405. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR. 2L74 4F 4A25 20050822001112005082200111 2005 8 22 BB05063 420050805A2565D31041147 SLIDE BOEING757 7572B7 1384964NM PASSENGER CABIN READS LOW A USAAK NONE O OTHER ININSP/MAINT 1 EA19620AU34204821 27199 PHL - THE R-3 DOOR EMERGENCY ESCAPE SLIDE BOTTLE PRESSURE WAS FOUND LOW. MAINTENANCE REPLACED THE R-3 DOOR EMERGENCY ESCAPE SLIDE. OK FOR SERVICE. 2L72 4F RTA2NM 20050822001132005082200113NM 2005 8 22 QXEA200501161 120050807A3097697071268 WIRE HARNESS BOMBDRDHC8 DHC8402 1390042NM PROP DE ICE SYS BROKEN A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09402QX 4032 SEA FLIGHT 2391: INTERMITTENT PROP DEICE CAUTION LIGHT WHILE IN ICING CONDITIONS AND PROP SELECTOR ON. ATTEMPTED ONE RESET PER E&A CHECKLIST. PROP DEICE CAUTION CONTINUED TO ILLUMINATE INTERMITTENTLY.RESCHEDULED PER MEL 30-60-1, CAT C, RSI 351658. MAINTENANCE FOUND NR 2 TMCU CD'S FAULTS; OPEN PHASE B/OPEN PHASE C AND OPEN HEATER. ON FURTHER INSPECTION FOUND R5 BLADE DEICER WIRE HARNESS DAMAGED WITH ONE WIRE BROKEN. REMOVED AND REPLACED R5 DEICER WIRE HARNESS IAW Q400 AMM TASK 61-10-06-000-805 AND -400-805. FUNCTIONAL TEST GOOD. FAULTS DID NOT RETURN. CLEARS MEL/RSI. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050822001152005082200115WP 2005 8 22 IXXA05SMN100S 120050627A5730 PANEL DOUG DC8 DC871F 302199DWP XW 6.000 CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, LH WING.- SLANT PANEL UPPER PART CORRODED, XW 6.000 PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-2-1 FIG. 37, EO SEMAN Nº 2005847 DATE 06-16-05. REMOVED FASTENERS IAW DC-8 SRM 51-1-21 PAGE 1, DC-8 SRM 51-1-20D PAGE 21. SMOOTHED, PERFORMED BLEND OUT TO CORRODED AREA IAW DC-8 SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW DC-8 SRM 57-2-1 PAGES 11, 12. FABRICATED REPAIR DOUBLER (ALCLAD 7075 T6 0.125”) IAW DC-8 SRM 57-2-1 FIG. 37. CLEANED, TREATED AND PRIMED AREA NEW REPAIR DOUBLER INTERNAL PART IAW DC-8 SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-12. INSTALLED REPAIR DOUBLER WITH NEW FASTENERS IAW DC-8 SRM 57-2-1 FIG. 37, DC-8 SRM 51-1-20D PAGE 9, DC-8 SRM 512L74 4F RT4A25 20050822001162005082200116WP 2005 8 22 IXXA05SMN101S 120050627A5720 WEB DOUG DC8 DC871F 302199DWP XCW 69.000 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, LT WING T/E WEB UPPER PART CRACKED 1/2, XCW 69.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-2-6 FIG. 15, EO SEMAN NR 2005836 DATE 06-25-05. REMOVED FASTENERS IAW DC-8 SRM 51-1-20D PAGE 21. REMOVED DAMAGED AREA IAW DC-8 SRM 57-2-6 FIG. 15. PERFORMED NDT INSPECTION IAW NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER, FILLERS (02 EA) IAW DC-8 SRM 57-2-6 FIG. 15. CLEANED, TREATED AND PRIMED AREA + REPAIR PARTS INTERNAL PART IAW DC-8 SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11 PAGE 9. INSTALLED REPAIR PARTS IAW DC-8 SRM 57-2-6 FIG. 15, DC-8 SRM 51-3-0 PAGE 1, DC-8 SRM 51-1-20D PAGE 9. TORQUED IAW DC-8 SRM 51-3-1. 2L74 4F RT4A25 20050822001182005082200118WP 2005 8 22 IXXA05SMN103S 120050627A5340 FITTING DOUG DC8 DC871F 302199DWP 1215.000 L-31L CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C-CHECK INSPECTION, AFT LOWER CARGO COMPT. INTERIOR.- FITTING CORRODED IN NR 3 DOOR HOUSING , STA 1215.000 NEAR TO L-31L. REMOVED CORROSION IAW DC-8 SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW DC-8 SRM 53-2-0 PAGE 2P. REMOVED CORRODED FITTING IAW DC-8 SRM 51-1-20D PAGE 21. FABRICATED NEW FITTING IAW DWG DOUGLAS 3750248 (ALCLAD 7075 T651) PERFORMED HEAT TREATMENT IAW DC-8 SRM 51-1-11 PAGES 1, 13, 17. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02 TO 07. NO CRACK CORROSION FOUND. CLEANED, TREATED AND PRIMED AREA + NEW FITTING IAW DC-8 SRM 51-1-8B. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D PAGE 9. TORQUED IAW DC-8 SRM 51-3-1. 2L74 4F RT4A25 20050822001202005082200120WP 2005 8 22 IXXA05SMN105S 120050627A5340 FITTING DOUG DC8 DC871F 302199DWP 440.000-460.000 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, FWD CARGO CMPT.- SPLICE FITTING CRACKED 2", STA 440.000 - 460.000 L-31R. REMOVED CRACKED SPLICE FITTING IAW DC-8 SRM 51-1-20D PAGES 21. CLEANED, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8B. INSTALLED SPLICE FITTING IAW DC-8 SRM 51-1-20D PAGE 9, DC-8 SRM 51-1-15 PAGE 1, DC-8 SRM 51-3-0 PAGE 1. TORQUED IAW DC-8 SRM 51-3-1. 2L74 4F RT4A25 20050822001282005082200128WP 2005 8 22 IXXA05SMN153S 120050630A5730 SKIN PANEL DOUG DC8 DC871F 302199DWP XF 134.000 IMPROPER B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C-CHECK INSPECTION, RH. INBD. FLAP.- FWD UPPER PLATING HAS INTERIN REPAIR, XF 134.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-1-0 PAGE 1, DC-8 SRM 57-7-1 FIG. 1, EO SEMAN 20051009 DATE 06-28-05. REMOVED PLATING WITH INTERIM REPAIR IAW DC-8 SRM 51-1-21 PAGE 1. FABRICATED NEW PLATING (ALCLAD 2024 T3 0.050”) IAW DC-8 SRM 57-7-1 FIG. 1 ITEM F. CLEANED, TREATED AND PRIMED AREA AND NEW PLATING INTERNAL PART IAW DC-8 SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11 PAGE 9. INSTALLED NEW PLATING IAW DC-8 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050822001302005082200130NE 2005 8 22 RAIA00508006 220050805A7200 ENGINE JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114HR 01514NE RIGHT OUT OF ADJUST A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03563HK 41079 FLT 3679 - PIT - RT ENGINE TORQUE LOW. MAINTENANCE ADJUSTED MAX FUEL FLOW AND TORQUE BRIDGE. 2L72 4T4 TRTA41NM E18NE 20050822001332005082200133SO 2005 8 22 RAIA00508009 120050807A324339807 VALVE EMB 145 EMB145LR 3260212SO BRAKE ASSY MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03811HK12041 145256 FLT 3558 - PIT - OUTBOARD BRAKE INOP WARNING INDICATION. MAINTENANCE REMOVED AND REPLACED OUTBOARD BRAKE CONTROL VALVE. 2L72 4T RTT00011AT 20050822001342005082200134WP 2005 8 22 IXXA05SMN147S 120050630A5730 SKIN DOUG DC8 DC871F 302199DWP -17.500-11.000 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C-CHECK INSPECTION, LT WING INTERIOR ANGLE DEFORMED, STA XFS -17.500 TO XFS -11.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 # 05259 DATE 06-24-05, SEMAN DWG ED 4016 DATE 06-20-05, EO SEMAN NR 2005948 DATE 06-24-05. 2L74 4F RT4A25 20050822001382005082200138EU 2005 8 22 USAA050890 120050718A53151161201 FLOORBEAM AIRBUS320 A320214 3930316EU FR 66 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19109UW19030 1065 FOUND FLOORBEAM CORRODED 2 INCH BY 4 INCH, FORWARD FRAME 66, 31 INCHES RIGHT OF CENTER LINE. CORROSION LEVEL 1, TASK JA-220-53500. REMOVED AND REPLACED FLOORBEAM PER SRM 51-40-00. (M) 2L72 4F RTA28NM 20050822001392005082200139EU 2005 8 22 YENA200545 120050807A27504917011 COMPUTER AIRBUS320 A320232 3930326EU TE FLAPS MALFUNCTIONED A YENALA ABORTED APPROACH UNSCHED LANDING F FLT CONT AFFECTED APAPPROACH 1 EA15589JB6740 1238 2215 ECAM MSG FLAPS LOCKED FLT CNTRL - ALIGNMENT FAULT. DURING FINAL APP TO BUR, FLAP HANDLE MOVED TO FLAP 2 POSITION. FLAPS LOCKED BETWEEN POS 1 AND POS 2. SLATS EXTENDED NORMALLY: DIVERTED TO LAX. PERFORMED WTB RESET OF FLAP SYS PER AMM 27-50-00-02. REMOVED AND REPLACED SFCC NR 1 PER AMM 27-51-34. 2L72 4F RTA28NM 20050822001442005082200144EU 2005 8 22 08082005K 120050808A61238210153 PCU SAAB SF340 340B 7860101EU RT PROPELLER MALFUNCTIONED A NSVAK NONE O OTHER TXTAXI/GRND HDL 1 EA27347CJ 347 DISCREPANCY: RH PROPELLER FEATHERS WITH CONDITION LEVER IN UNFEATHER POSITION, POWER LEVER AT 5 PERCENT AND INTAKE LIGHT ILLUMINATES. R&R'D PCU 2L72 4T RTA52EU 20050822001492005082200149NM 2005 8 22 SWAA052479 120050818A55516551524 FITTING BOEING737 7373Q8 1384670NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29317WN 24068 DURING SCHEDULED D-CHECK, FOUND LT & RT HORIZONTAL STAB ATTACH FITTING LUG FACES CORRODED. REPAIRED LUG FACES PER SRM. 2L72 4F RTA16WE 20050822001522005082200152NM 2005 8 22 SWAA052482 120050818A55516551524 FITTING BOEING737 7373H4 1384600NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29612SW 27930 DURING SCHEDULED D-CHECK, FOUND LT & RT HORIZONTAL STAB FITTING LUG FACES CORRODED. REPAIRED LUG FACES PER SRM. 2L72 4F RTA16WE 20050822001542005082200154NM 2005 8 22 SWAA052484 120050818A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29617SW 27700 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 767, LBL 19. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050822001572005082200157EA 2005 8 22 COMA0560427 120050805A32307300500 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA MLG MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01416CA 7450 FLIGHT 5247 - GEAR DISAGREE WARNING. REPLACED THE MLG SELECTOR VALVE. 2L72 4F RTA21EA 20050822001582005082200158EA 2005 8 22 COMA0560430 120050805A5240 DOOR CNDAIRCL600 CL6002B19 1900309EA SERVICE OPEN A COMAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 SO01951CA 7091 FLIGHT 5692 - STALL FAIL, MACH TRIM CAUTION. FOUND O2 SERVICE DOOR OPEN. CLOSED DOOR. 2L72 4F RTA21EA 20050822001602005082200160EA 2005 8 22 COMA0570091 120050804A2150GG670950091 ACM CNDAIRCL600 CL6002C10 1390015EA LEFT OVERTEMP A COMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO01669CA2253 10176 FLIGHT 6647 - DURING CLIMBOUT OF CVG NOTED SMOKE IN THE CABIN, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE LT AIR CYCLE MACHINE. 2L72 4F RTA21EA 20050822001622005082200162EA 2005 8 22 COMA0560428 120050805A7110 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LEFT SURGES A COMAA UNSCHED LANDING O OTHER CLCLIMB 1 SO01484CA 7702 FLIGHT 5063 - LEFT ENGINE SURGE 5-6 PERCENT. DEFERRED MAINTENANCE PER MEL. 2L72 4F4 FRTA21EA E15NE 20050822001632005082200163EA 2005 8 22 COMA0570092 120050805A2780 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA SLAT ILLUMINATED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01390CA 10106 FLIGHT 5104 - SLAT FAULT MESSAGE. SLATS FAILED AT 0. CND NO DEFECTS FOUND. 2L72 4F RTA21EA 20050817000182005081700018CE 2005 8 17 6019307142005 120050714A32601EN18 DOWNLOCK SWITCH LEAR 60 60LEAR 5170707CE MLG MALFUNCTIONED E J7SAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW05249FX 60193 AFTER LANDING GEAR SELECTED UP, GEAR STAYED DOWN WITH TWO UNSAFE MAIN LIGHTS AND THREE GREEN LIGHTS INDICATION. AIRCRAFT DIVERTED TO RSW FOR MAINTENANCE. MAINTENANCE TROUBLESHOOTING FOUND THE RIGHT GEAR DOOR DOWN AND LOCKED SWITCHES HARD FAILED. REPLACED SWITCHES AND RIGGED. GEAR SWINGS PERFORMED WITH NO DEFECTS NOTED. 2L72 4F RTA10CE 20050817000232005081700023CE 2005 8 17 DJFA2005128 120050810A32971283640681 CIRCUIT BOARD BEECH MU300 400A 1155402CE MLG INTERMITTENT E DJFAL ABORTED APPROACH O OTHER LDLANDING 1 EA23457CW RK57 ON VISUAL APPROACH GEAR WAS SELECTED DOWN, NO GEAR MOVEMENT. APPROACH WAS MISSED, GEAR SELECTED UP. EMERGENCY DECLARED, ACFT RETURNED. ON RETURN GEAR LEVER WAS CYCLED SEVERAL TIMES WITH NO GEAR MOVEMENT. ON APPROACH GEAR SELECTED DOWN & APPROX 5 SEC GEAR EXTENDED. UNEVENTFUL LANDING. MX PERFORMED OPS CHECKS OF LANDING GEAR WITH NO DEFECTS. BENCH CHECK OF PRINTED CIRCUIT BOARD 162 PERFORMED WITH NO DEFECTS FOUND. GEAR CONTROL UNIT, SOLENOIDS ON VALVE PACK, GEAR DOOR & DOOR SWITCHES ALL CHECKED WITH NO DEFECTS. PCB 162 REPLACED DUE TO SUSPICION OF K1 RELAY BEING INTERMITTENT. OPERATIONAL CHECKS OF GEAR AND A TEST FLIGHT WERE PERFORMED WITH NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4F RTA16SW 20050817000272005081700027EU 2005 8 17 TRB2005F00005 120050717A2121011494500 FAN AEROSPATR72 ATR72212 8680945EU LT A/C RECIRC BURNED A TRBAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO29431AT 431 AFTER TURNING THE AIRCRAFT BATTERY ON, A STRONG ELECTRICAL SMELL, SMOKE AND FUMES SPREAD INTO THE CABIN AND COCKPIT. EMERGENCY EVACUATION CONDUCTED. REPLACED LEFT AIR CONDITIONING RECIRCULATING FAN. (M) 2H72 4T RTA53EU 20050817000332005081700033WP 2005 8 17 ASAA0580361 120050717A532199365859 FLOOR PANEL DOUG DC9 DC983 3022083WP FS 927-1003 DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02944AS 53019 OKC - FOUND DURING HV CHECK, CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050817000372005081700037WP 2005 8 17 ASAA0580364 120050717A532199365813 FLOOR PANEL DOUG DC9 DC983 3022083WP FS 541-579 DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02944AS 53019 OKC - DURING HV CHECK, FOUND FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050817000402005081700040WP 2005 8 17 ASAA0580366 120050717A532199365813 FLOOR PANEL DOUG DC9 DC983 3022083WP F 617-693 DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02944AS 53019 OKC - FOUND DURING HV CHECK, CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050817000442005081700044WP 2005 8 17 ASAA0580370 120050717A5321993665113 FLOOR PANEL DOUG DC9 DC983 3022083WP FS 769-807 DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02944AS 53019 OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050817000872005081700087CE 2005 8 17 DXTA200500894 120050810A3240 BRAKE CESSNA560 560XL 2076702CE MLG MALFUNCTIONED E DXTAD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07664QS 5605264 PILOT'S AND COPILOT'S -L- PEDALS HAVE EXCESSIVE TRAVEL FORWARD BEFORE BRAKE ACTUATES. -L- PEDALS ARE ALSO SPONGY CAUSING ACFT TO PULL HARD RIGHT WHEN BRAKES ARE APPLIED. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20050817000922005081700092EU 2005 8 17 DXTA200500898 120050814A3230 LANDING GEAR BRAERO1000 HAWKER1000 7450005EU RT MLG INOPERATIVE E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07546QS 259046 RED LANDING GEAR LIGHT ON THE RIGHT SIDE (RIGHT MAIN) STAYED ON AFTER GEAR RETRACTION, WITNESS ON THE GROUND REPORTED THAT THE RIGHT MAIN GEAR NEVER RETRACTED. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA3EU 20050817001042005081700104 2005 8 17 F3LA200500037 420050812A233020092455101 COOLING FAN AIRBUSA318 A318111 3940019EU LIVE TV UNIT FAILED A F3LAO OTHER J WARNING INDICATION CRCRUISE 1 NM03801FR 4121 1939 FLIGHT CREW REPORTED LIVE TV SMOKE DETECTION WARNING HORN SOUNDED DURING FLIGHT. LIVE TV FAN C/B 2000VU POPPED AND WOULD NOT RESET. REPLACED AFT RACK COOLING FAN PER AMM 44-25-00, PAGE 471. OPS CHECK GOOD. 2L72 4F RT 20050817001172005081700117WP 2005 8 17 ASAA0580384 120050717A532199365851 FLOOR PANEL DOUG DC9 DC983 3022083WP FS 380 DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02944AS 53019 OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050817001282005081700128WP 2005 8 17 ASAA0580389 120050718A523059101413 SKIN DOUG DC9 DC983 3022083WP FS 399 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02944AS 53019 OKC - DURING HV CHECK, FOUND FORWARD CARGO BAY DOOR DENTED. RE-COLD FORMED SKIN AND INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050817001292005081700129WP 2005 8 17 ASAA0580390 120050718A523059101413 DOOR DOUG DC9 DC983 3022083WP FS 1204 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02944AS 53019 OKC - DURING HV CHECK, FOUND AFT CARGO BAY DOOR DENTED. RE-COLD FORMED SKIN AND INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050817001392005081700139EA 2005 8 17 A6WA200540278 120050804A219775065916 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT A/C PACK UNSECURE A A6WAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL31429AW 7711 SHORTLY AFTER TAKEOFF, STRONG SMELL OF SMOKE IN COCKPIT AND CABIN. NO VISUAL SMOKE, PACK TEMP NORMAL. (AIR RETURN) DURING TAXI PACK NR 2 HI TEMP INDICATION. INSPECTED AFT EQUIPMENT BAY AREA AND FOUND RT PACK ACM TEMP SWITCH HANGING FROM CONNECTOR PLUG. NO NOTICE OF OIL OR OTHER CONTAMINANTS. SECURED PLUG, RAN ENGINES WITH RT PACK (OFF) AND LT PACK OPERATING, NO ODOR OR VISUAL SMOKE NOTED. (K) 2L72 4F4 FRTA21EA E15NE 20050817001422005081700142SO 2005 8 17 CHQA200500143 120050815A2120 ODOR EMB 145 EMB145LR 3260212SO CABIN DETECTED A CHQAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 GL11266SK 145241 FLIGHT 3385 RDU-LGA - UPON DESCENT THE CREW SMELLED AN ELECTRICAL BURNING SMELL COMING FROM THE LEFT HAND SIDE OF THE COCKPIT. NO VISIBLE SMOKE WAS NOTED. DURING PREVIOUS ENGINE START IN RDU, THE GPU OVERRATED AND WENT OFF LINE DURING START. MAINTENANCE INSPECTED GPU RECEPTACLE AND BATTERY COMPARTMENT FOR EVIDENCE OF BURNING. POWERED AIRCRAFT WITH GPU. NO DEFECTS WERE NOTED. NO EVIDENCE OF SMOKE OR BURNING SMELL WAS DETECTED. 2L72 4T RTT00011AT 20050817001462005081700146WP 2005 8 17 ASAA0580401 120050725A53209930538U12 CUSP WEB DOUG DC9 DC983 3022083WP FS 522-579 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02947AS 53020 OKC - DURING C-CHECK, FOUND RIGHT CABIN FLOOR CUSP WEB IS CORRODED. REPLACED WEB. (M) 2L72 4F RTA6WE 20050817001502005081700150WP 2005 8 17 ASAA0580403 120050725A5320993061225 CUSP WEB DOUG DC9 DC983 3022083WP FS 1060-1079 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02947AS 53020 OKC - DURING C-CHECK, FOUND RIGHT CABIN FLOOR CUSP WEB IS CORRODED. REMOVED DAMAGED SECTION OF WEB AND INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050817001562005081700156WP 2005 8 17 ASAA0580406 120050725A53305920323509 SKIN DOUG DC9 DC983 3022083WP FS 569-588 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02947AS 53020 OKC - DURING C-CHECK, FOUND FUSELAGE IS DENTED. COLD-WORKED DAMAGED AREA AND INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050817001572005081700157NM 2005 8 17 USAA050905 120050727A5322 SHEAR TIE BOEING737 737401 1384701NM CFMINTCFM56 CFM563B2 13802EU STA 867 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19404US 23886 CLT - C1 - SHEAR TIE, 5.5 INCH X 1.0 INCH CORROSION, BETWEEN SHEAR TIE AND SKIN AT STA 867 BOTTOM OF FUSELAGE. REMOVED CORRODED SHEAR TIE AND INSTALLED NEW SHEAR TIE IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050817001672005081700167EU 2005 8 17 KBM2005F00169 120050728A6730AC67244 SERVO SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE MAIN ROTOR BINDING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P 2347 SERVO/ LAT, UNIT BINDING. REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20050817001702005081700170CE 2005 8 17 AJC2005F00009 120050727A21609795583 VALVE BEECH MU300 400A 1155402CE PWA JT15 JT15D1 52060NE CABIN TEMP FAILED E AJCAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA25127BW2168 RK105 AIR RETURNED DUE TO AIR CONDITIONING FAIL LIGHT ILLUMINATED AND CABIN REVERTED TO EMERGENCY PRESSURIZATION MODE. AIRCRAFT ISSUED SPECIAL FLIGHT PERMIT, FOR MAINTENANE AT SERVICE CENTER. MAINTENANCE FOUND THE CABIN TEMPERATURE CONTROL VALVE TO BE DEFECTIVE. REPLACED SAME AND FUNCTIONALLY TESTED SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (EA25200509515) (K) 2H72 4F4 FRTA16SW E1NE 20050817001792005081700179WP 2005 8 17 ASAA0580408 120050725A5330593600731 SKIN DOUG DC9 DC983 3022083WP FS 1305 GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02947AS 53020 OKC - FOUND DURING C-CHECK, FUSELAGE IS GOUGED. REPLACED EXISTING REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050817001922005081700192EU 2005 8 17 KBM2005F00177 120050727A21200500844 BRUSHES SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE BLOWER MOTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV 3296 7 INCH BLOWER MOTOR, UNIT HAS WORN BRUSHES AND EVIDENCE OF OVERHEAT ON THE ARMATURE, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050817001962005081700196NM 2005 8 17 ASAA0540337 120050703A57536546434370 SKIN BOEING737 7374Q8 138447QNM TE FLAP DEBONDED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02775AS 25108 OKC - FOUND RIGHT WING INBOARD AFT FLAP LOWER SKIN AT PREVIOUS REPAIR IS DISBONDED ON FORWARD END AT SECOND TRACK. REMOVED DISBONDED AREA, REPAIRED AREA WITH FIBERGLASS OVERLAY VIA HOTBOND IAW 737-400 SRM 51-70-06 PARAGRAPH 3A. (M) 2L72 4F RTA16WE 20050817001992005081700199NM 2005 8 17 ASAA0540339 120050703A5512657378351 SKIN BOEING737 7374Q8 138447QNM HORIZONTAL STAB DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02775AS 25108 OKC - FOUND LEFT HORIZONTAL STAB LEADING EDGE STAB STATION 131.54 HAS NUMEROUS CREASES. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW 737-400 SRM 55-10-01 FIGURE 203. (M) 2L72 4F RTA16WE 20050817002012005081700201NM 2005 8 17 ASAA0540340 120050703A5512657378352 SKIN BOEING737 7374Q8 138447QNM HORIZONTAL STAB DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02775AS 25108 OKC - FOUND SPEED TAPE INSTALLED AT THE L/E IN THE RIGHT HORIZONTAL STABILIZER. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED A REPAIR DOUBLER AND FILLER IAW 737-400 SRM 55-10-01 FIG 203. (M) 2L72 4F RTA16WE 20050817002102005081700210NM 2005 8 17 2005UALA00775 120050806A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FWD PIT STA 600 DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29587UA 26713 FWD PIT FRAME STA 600, LT 2 EACH DENT STR 24L. TRIMMED OUT DAMAGE, ACP HFEC INSP, NO CRACK FOUND. FABRICATE AND INSTALL REPAIR PER TIMCO REO-G10763, REV B, AND UA EVA-50518. 2L72 4F4 FRTA2NM E17NE 20050817002122005081700212NM 2005 8 17 2005UALA00777 120050806A3350 LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE ROW 15 INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP2987UA 26713 EEL FLOOR LIGHT AT SEAT ROW 15 INOP. REPLACE LIGHT STRIP. 2L72 4F4 FRTA2NM E17NE 20050817002162005081700216EU 2005 8 17 2005UALA00782 120050804A3350 BATTERY PACK AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29427UA 512 EMERGENCY LIGHTS FAIL TEST. REPLACED BATTERY PACK AT DOOR 1L. 2L72 4F4 FRTA28NM E40NE 20050818000042005081800004WP 2005 8 18 DHL2005806501 120050812A5312 FINGER DOUBLER DOUG DC8 DC873F 302199FWP -67.0 TO -80.0 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH87034 46002 COCKPIT SUBFLOOR PRESSURE PANEL FINGER DOUBLER CORRODED (STA -67.000 TO -80.000). REMOVED CORROSION FROM FINGER DOUBLER IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED FINGER DOUBLER IAW SRM 51-1-21 PG 1. FABRICATED FINGER DOUBLER (AL2024T3 0.040) IAW SRM 53-3-3 FIG 6. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-14. INSTALLED FINGER DOUBLER IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050818000072005081800007NM 2005 8 18 DHL2005747508 120050814A5340 SPLICE BOEING727 727224 1384076NM STRINGER CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01747DH 22253 CORRODED STRINGER SPLICE 28R IN AFT CARGO COMPT BS 1010. REMOVED CORRODED SPLICE. FABRICATED AND INSTALLED REPAIR STRINGER SPLICE 12.5 INCHES FROM BAC1498-131 IAW B727 SRM 51-30-2 AND DWG 65-16341. 2L73 4F A3WE 20050818000172005081800017NM 2005 8 18 SWAA052457 120050815A53206517583 VERTICAL BEAM BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29696SW 23064 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE VERTICAL BEAM WEB CRACKED AT BS 183.5, RBL 5.7, WL 185. REPAIRED WEB PER SWA EA & SRM. 2L72 4F RTA16WE 20050818000192005081800019 2005 8 18 SWAA052451 420050815A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29315SW 23337 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050818000222005081800022NM 2005 8 18 QXEA200501177 120050816A5230 HANDLE BOMBDRDHC8 DHC8402 1390042NM CARGO DOOR UNSECURE A QXEAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 NM09414QX 4061 PDX FLIGHT 2415: CLIMBING THROUGH 3000 FT, MASTER WARNING FUSELAGE LIGHT ILLUMINATED. MFD DOOR PAGE SHOWED BAGGAGE LIGHT ILLUMINATED. RETURNED TO FIELD. MAINTENANCE INSPECTED AND FOUND AFT CARGO DOOR HANDLE EXTENDED. SEATED HANDLE, NO DEFECTS FOUND. SUSPECT DOOR HANDLE NOT COMPLETELY STOWED. NO DEFECTS FOUND ON LATCH ASSY. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050818000522005081800052 2005 8 18 2005UALA00798 420050802A2565D31096201 SLIDE BOEING757 757222 1384956NM PWA 2037 PW2037 NE L1 DOOR LEAKING A UALAK NONE O OTHER ININSP/MAINT 1 WP29542UA 25276 TUBE ASSY FAILED AIR RETENTION TEST DUE TO EXCESSIVE POROSITY LEAKING THROUGH TUBE FABRIC NOTED ON VARIOUS LOCATIONS. DURING COMPONENT SHOP MAINTENANCE SLIDE FAILED AIR RETENTION TEST DUE TO FABRIC POROSITY. POROSITY WAS BEYOND CMM LIMITS. SLIDE WAS RETURNED TO OEM FOR INFLATABLE REPLACEMENT. 2L72 4F4 FRTA2NM E17NE 20050818000542005081800054NM 2005 8 18 2005UALA00800 120050810A3350362624 LAMP BOEING777 777222 1385219NM PWA PW4077PW4077 NE SEAT 3E INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29774UA 26936 EMERGENCY LIGHTING COMING OFF AT SEAT 3E. 3E IS BROKEN AND AFT LIGHT DOES NOT ILLUMINATE. REPLACED LIGHT ASSY. 2L72 4F4 FRTT0001SE E46NE 20050818000662005081800066NM 2005 8 18 DHL2005747513 120050717A5320 WEB BOEING727 727224 1384076NM CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01747DH 22253 CORROSION ON WEB AT STR 27L STA 950 TO STA 950A. REMOVED CORROSION ON WEB AT STA. 950 TO 950A LONGERON 27L. FOUND OUT OF LIMITS IAW B727 SRM 53-10-1 AND 51-10-6. REMOVED WEB AND INSTALLED NEW WEB P/N 69-44877-13, ALODINED AND PRIMED IAW B727 SRM 51-10-2, INSTALLED NEW WEB IAW B727 SRM 51-30-2, REINSTALLED PANEL 3365 IAW B27 SRM 51-30-2 USED DRAWING 69-44877. 2L73 4F A3WE 20050818000692005081800069NM 2005 8 18 AWXA200500956 120050815A3350321431 BATTERY AIRBUSA319 A319132 3930340NM EMERGENCY LIGHT DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28816AW 1350 LAS - EES - DURING 4 DAY CHECK THE EMERGENCY LIGHT TEST FAULTED L EPSU BATTERY. MAINTENANCE REMOVED AND REPLACED THE LEFT OVERWING EPSU BATTERY IAW AIRBUS AMM 33-51-38-000-001. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA28NM 20050818000702005081800070 2005 8 18 AWXA200500957 420050815A2565D30664105 SLIDE AIRBUS320 A320231 3930325EU L1 DOOR LOOSE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW323396837 055 PHX - EES - DURING 4-DAY CHECK WHILE REMOVING GIRT BAR FROM THE L1 DOOR, THE SLIDE DROPPED OUT OF THE BOTTOM. MAINTENANCE REMOVE AND REPLACED THE L1 DOOR SLIDE IAW AMERICA WEST AIRLINES TASK CARD R1C25304. VENDOR FOUND NO FAULTS WITH SLIDE. UNIT WAS OVERHAULED IAW CMM 25-61-20 REV. 9. 2L72 4F RTA28NM 20050818000852005081800085GL 2005 8 18 ALG2005F00058 220050804A753223073353 BLEED VALVE BELL 407 407 1182206SW ALLSN 250C 250C47B GL ENGINE FAILED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03547AL 53240 CAE847271 DURING OPS FLIGHT CHECK, WHILE ACCELERATING, (CHECK INSTRUMENT LIGHT) ILLUMINATED, THE PILOT IMMEDIATELY REDUCED POWER AND THE COMPRESSOR STALLED. PILOT RETURNED TO BASE AND NOTIFIED MAINTENANCE. THE MECHANIC REMOVED AND REPLACED THE BLEED VALVE AND THE AC WAS RETURNED TO SERVICE UPON COMPLETION OF FUNCTION CHECKS IAW MFG. (K) 1G71 3U3 UO H2SW E1GL 20050818000942005081800094 2005 8 18 KBM2005F00191 420050726A2312064105430 RADIO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE VHF FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH2955 2884 VHF RADIO FAILED. (K) 1G71 3U3 U H9EU E19EU 20050818001232005081800123NM 2005 8 18 ASAA0540330 120050626A53156553844 FLOORBEAM BOEING737 7374Q8 138447QNM FS 947 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 YXX - AFT CARGO PIT FLOOR SUPPORT BEAM TIE DOWN TRACK HAS CORROSION FORWARD OF BS 947 LBL 18. REPAIRED IAW 737-400 SRM 53-00-53 FIG 209. (M) 2L72 4F RTA16WE 20050819000012005081900001NM 2005 8 19 ASAA0540297 120050626A533065C323591 SKIN BOEING737 7374Q8 138447QNM FS 460 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 OKC - FOUND DENT AT STATION 460 BETWEEN STRINGERS 26 AND 27 RIGHT, A=.750 Y=19.73. TRIMMED OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW AAR EA 11020 AND ASA EA 5330-01954. (M) 2L72 4F RTA16WE 20050819000042005081900004NM 2005 8 19 ASAA0540296 120050626A575465C26603202 SKIN BOEING737 7374Q8 138447QNM NR 4 SLAT CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 OKC - FOUND NR 4 SLAT INBOARD LOWER SKIN T/E IS CHAFED TO THE COMPOSITE. REMOVED DAMAGE, FABRICATED SKIN AND DOUBLER AND INSTALLED REPAIR PIECES IAW 737-400 SRM 51-70-10. (M) 2L72 4F RTA16WE 20050822000012005082200001NM 2005 8 22 USAA050939 120050729A5320US14IN8322263LF FLOORBEAM BOEING757 7572B7 1384964NM RROYCERB211 RB211535* NE STA303-379RBL55 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19628AU36199 27806 BFM - C3 -CHORD, 11 INCH X .90 INCH, CORROSION, STA 303-379, RBL 55. REPLACED FLOOR SUPPORT CHORD IAW SRM. (K) 2L72 4F4 FRTA2NM E12EU 20050822000032005082200003EU 2005 8 22 USAA050985 120050805A5315D5347208900400 FLOORBEAM AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE FR 68-66 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19110UW 1112 PIT - S2 - FLOORBEAM, 2 INCH X 36 INCH, CORROSION; LEVEL 1; TASK JA-260-53500, FLOOR SUPPORT BEAM FROM FR 68-66, IB AFT ENTRY DOOR. DEFECTIVE PART REPLACED WITH IDENTICAL PART. (K) 2L72 4F4 FRTA28NM E38NE 20050822000072005082200007EU 2005 8 22 USAA050981 120050805A5315D5311281520200 FLOORBEAM AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE Y765, FR C16 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19110UW13254 1112 A .7500 INCH DIA AREA OR LEVEL 1 CORROSION ON FLOORBEAM AT Y765 FR C-16. DEFECTIVE PART REPLACED WITH IDENTICAL PART IAW SRM. (K) 2L72 4F4 FRTA28NM E38NE 20050822000132005082200013EU 2005 8 22 KBM2005F00198 120050520A2121050143 MOTOR SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1 60030NE BLOWER INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19215LA460 2143 5 INCH BLOWER MOTOR, INOPERATIVE. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050822000172005082200017EU 2005 8 22 KBM2005F00196 120050519A33400107704402 LIGHT SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1 60030NE ANTI-COLLISION INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19215LA 2143 ANTI-COLLISION LIGHT INOPERATIVE. REMOVED AND RELACED. (K) 1G71 3U3 U H9EU E19EU 20050822000192005082200019EU 2005 8 22 KBM2005F00203 120050421A7700 CHIP DETECTOR SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE ENGINE MALFUNCTIONED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19351WM 2167 ENGINE CHIP LIGHT ILLUMINATED IN FLIGHT. REMOVED, INSPECTED AND CLEANED ENG ELECTRICAL CHIP DETECTORS. NO METAL FOUND, GROUND RUN FOR 1 HOUR. CHIP LIGHT NOT ILLUMINATED, CHECK GOOD. (K) 1G71 3U3 U H9EU E19EU 20050822000232005082200023 2005 8 22 KBM2005F00200 420050521A34215040111920 INDICATOR SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE ATTITUDE INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV958 3296 ATTITUDE INDICATOR WILL NOT RESET (CAGE). MEL`D (K) 1G71 3U3 U H9EU E19EU 20050822000242005082200024NE 2005 8 22 KBM2005F00204 220050520A75329550161210 BLEED VALVE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE ENGINE STUCK E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19351WM710 2167 BLEED VALVE STUCK OPEN. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050822000282005082200028EU 2005 8 22 KBM2005F00209 120050416A6320579069G BEARING SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1D NE MAIN ROTOR ROTATED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1953SH 2009 LAMINATED BEARINGS ARE ROTATING, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050822000332005082200033SW 2005 8 22 KBM2005F00214 120050523A6340206075188001 INDICATOR BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL XMSN OIL TEMP INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1973DP 2513 TRANSMISSION OIL TEMP LIGHT ILLUMINATED AT 90 DEGREES C. REMOVED AND REPLACED. (K) 1G71 3U3 U H2SW E4CE 20050822000342005082200034EU 2005 8 22 USAA050980 120050805A5315D5347219208 FLOORBEAM AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE FR66, Y765 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19110UW13254 1112 1 INCH OF CORROSION. NO LEVEL OR TASK, FRAME 66 Y-765 AT ATTACH FITTING. DEFECTIVE PART REPLACED WITH IDENTICAL PART IAW SRM. (K) 2L72 4F4 FRTA28NM E38NE 20050822000442005082200044NM 2005 8 22 ASAA0540343 120050703A57536546430190 SKIN BOEING737 7374Q8 138447QNM TE FLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02775AS 25108 OKC - FOUND RIGHT INBOARD FORE HAS A DENT ON THE LOWER SIDE ABOVE INBOARD TRACK. PREPARED DAMAGED AREA, FABRICATED AND INSTALLED A REPAIR DOUBLER AND BONDED, IAW 737-400 SRM 51-70-30 REPAIR 2. (M) 2L72 4F RTA16WE 20050822000472005082200047NM 2005 8 22 ASAA0540324 120050626A552265C25746141A SKIN BOEING737 7374Q8 138447QNM LT ELEVATOR DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 YXX - FOUND LT ELEVATOR LOWER SURFACE DELAMINATED. REMOVED DAMAGE AND REPAIRED IAW B737-40 SRM 51-70-04. (M) 2L72 4F RTA16WE 20050822000552005082200055NE 2005 8 22 QXEA200501178 220050816A72003038400 ENGINE DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE NR 2 MALFUNCTIONED A QXEAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM09347PH167863291 480 PCEAG0044 CREW REPORTED SMOKE IN CABIN AFTER ENGINE START UP. ISOLATED TO NR 2 BLEED. MAINTENANCE REPLACED THE NR 2 ENGINE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20050822000812005082200081CE 2005 8 22 DEL2005F00000 120050807A3244PW184F102 TIRE LEAR 55 55LEAR 5170702CE GARRTTTFE731TFE7313A 01518WP NLG FAILED B DELRO OTHER O OTHER NRNOT REPORTED 1 CE03273MG 119 NOSE TIRE FAILED ON TAKEOFF RUN. REPLACED NOSE TIRE (WHEEL ASSY WITH NEW TIRE AND OVERHAULED WHEEL ASSY. (K) 2L72 4F4 F A10CE E6WE 20050822000962005082200096WP 2005 8 22 IXXA0500095O 120050817A7900 LINE DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C1 13802NE BROKEN A IXXAE ENGINE SHUTDOWN O OTHER CRCRUISE 1 SW11828BX83892396 45993 692264 DURING CRUISE FROM KDFW TO KTOL CREW SHUTDOWN THE #2 ENGINE DUE TO LOSS OF OIL QUANTITIY PRESSURE. CREW LANDED IN KTOL WITHOUT INCIDENT. MAINTENANCE FOUND A BROKEN LINE AT THE OIL PRESSURE TRANSMITTER. THEY REMOVED AND REPLACED THE PRESSURE TRANSMITTER LINE AND PERFORMED A LOSS OF OIL PRESSURE INSPECTION CHECK. THE OPERATIONAL AND LEAK CHECK WAS GOOD IN ACCORDANCE WITH THE ERH AND GMM. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F4 FRT4A25 E2GL 20050822000992005082200099WP 2005 8 22 IXXA05RNG044S 120050723A5330 SKIN DOUG DC8 DC862F 3021972WP 1440-1530 CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW1171CX 670243317 45961 DURING A ROUNTINE C CHECK INSPECTION FOUND CORROSION ON LOWER SKIN STA 1440-1530 LONGERON 31RH- 31LH. SKIN STA 1440-1530 LONGERON 31R-31L WAS REMOVED AND REPLACED IAW DOUGLAS DRAWING 5615374, AND EXTERNAL SPLICE, INTERNAL SPLICE, FINGER DOUBLER AND LONGERON STRAP WERE INSTALLED BETWEEN STA 1420-1440 LONGERON 31RH - 31LH IAW EWO ATI 53-009 & SRM 53-2-1 FIGURE 4. 2L74 4F 4A25 20050822001002005082200100WP 2005 8 22 IXXA05RNG046S 120050717A5730 SKIN DOUG DC8 DC862F 3021972WP XRS 795 MISDRILLED B IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW1171CX 670243317 45961 DURING A ROUTINE C CHECK INSPECTION FOUND A MISS DRILL HOLE ON PLATING STA XRS 795 LONGERON 3-RHD. REPAIR WAS MADE AND DOUBLER WAS INSTALLED IAW EWO ATI 57-036 & EO ATI-071705.FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR. 2L74 4F 4A25 20050822001192005082200119WP 2005 8 22 IXXA05SMN104S 120050627A5230 FITTING DOUG DC8 DC871F 302199DWP STA 1420.000 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, AFT LWR CARGO BILGE INTERIOR.- NR 4 DOOR INTERNAL SUPPORT CTR FITTING CRACKED, STA 1420.000. REMOVED CRACKED FITTING IAW DC-8 SRM 51-1-21 PAGES 1 CLEANED, TREATED AND PRIMED AREA DC-8 SRM 51-1-8B. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-21 PAGE 21. 2L74 4F RT4A25 20050822001212005082200121WP 2005 8 22 IXXA05SMN106S 120050627A5730 SKIN DOUG DC8 DC871F 302199DWP XW104.000 WORN B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, LH INBOARD FLAP UPPER PART SKIN WORN, XW 104.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-1-0 PAGE 1, DC-8 SRM 57-7-1 FIG. 1, EO SEMAN NR 2005850 DATE 06-18-05. REMOVED DAMAGED PLATING IAW DC-8 SRM 51-1-21 PAGE 1. FABRICATED NEW PLATING (ALCLAD 2024 T3 0.040”) IAW DC-8 SRM 57-7-1 FIG. 1 ITEM “D”. CLEANED, TREATED AND PRIMED AREA + NEW PLATING INTERNAL PART IAW DC-8 SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11 PAGE 9. INSTALLED NEW PLATING IAW DC-8 SRM 51-1-21 PAGE 1, DC-8 SRM 51-3-0 PAGE 1. TORQUED IAW DC-8 SRM 51-3-1. 2L74 4F RT4A25 20050822001222005082200122WP 2005 8 22 IXXA05SMN107S 120050627A5720 SKIN DOUG DC8 DC871F 302199DWP XW 132.000 IMPROPER A IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, LH INBD FLAP UPPER PART SKIN NON STANDARD REPAIR, XW 132.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-1-0 PAGE 1, DC-8 SRM 57-7-1 FIG. 1, EO SEMAN NR 2005851 DATE 06-18-05. REMOVED PLATING WITH IMPROPER REPAIR IAW DC-8 SRM 51-1-21 PAGE 1. FABRICATED NEW PLATING (ALCLAD 2024 T3 0.050”) IAW DC-8 SRM 57-7-1 FIG. 1 ITEM “F”. CLEANED, TREATED AND PRIMED AREA + NEW PLATING INTERNAL PART IAW DC-8 SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11 PAGE 9. INSTALLED NEW PLATING IAW DC-8 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050822001552005082200155NM 2005 8 22 SWAA052485 120050818A532065C27314 CLIP BOEING737 7373H4 1384600NM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29617SW 27700 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CORRODED AT BS 787, STR 26R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050822001592005082200159EA 2005 8 22 COMA0570093 120050805A32306619501 MOTOR CNDAIRCL600 CL6002C10 1390015EA SYSTEM 3 MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01656CA3781 10143 FLIGHT 5438 - GEAR DISAGREE WARNING. REPLACED THE 3B ACMP. 2L72 4F RTA21EA 20050822001642005082200164EA 2005 8 22 COMA0560429 120050805A3241140153 TRANSDUCER CNDAIRCL600 CL6002B19 1900309EA LT MLG MALFUNCTIONED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01917CA28703 7017 FLIGHT 5553 - ANTI SKID CAUTION DURING T/O. REPLACED WHEEL SPEED TRANSDUCER. 2L72 4F RTA21EA 20050822001662005082200166EA 2005 8 22 COMA0560433 120050807A32304622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG UNRELIABLE A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01487CA16431176 7729 FLIGHT 5333 - GEAR DISAGREE WARNING. REPLACED THE NLG PRIORITY VALVE. 2L72 4F RTA21EA 20050822001702005082200170NE 2005 8 22 COMA0560436 220050809A7314887055 PUMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE RT ENGINE FAILED A COMAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO01712CA102295946 7244 FLIGHT 4998 - NR 2 HYDRAULIC SYSTEM HIGH TEMP AND LOW PRESSURE WARNING. REPLACED THE RT ENGINE HYDRAULIC PUMP. 2L72 4F4 FRTA21EA E15NE 20050822001712005082200171NE 2005 8 22 COMA0560437 220050811A7297601R577921PE WIRE HARNESS CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE RT ENGINE CHAFED A COMAE ENGINE SHUTDOWN AYJFLAME/FIRE ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 SO01956CA 7105 807604 FLIGHT 5164 - EN ROUTE FSD - CVG RECEIVED A NR 2 ENGINE FIRE MESSAGE, SHUTDOWN NR 2 ENGINE. FLIGHT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 ENGINE ASSEMBLY AND IDG HARNESS ASSEMBLY DUE TO CHAFED BLUE WIRE ARCING AGAINST THE FUEL CONTROL. 2L72 4F4 FRTA21EA E15NE 20050822001732005082200173EA 2005 8 22 COMA0570095 120050805A5320CC670341755 CROSSBEAM CNDAIRCL600 CL6002C10 1390015EA FS 280 CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01331CA7693 10061 THE TRANSVERSE BEAM AT FS 280 IS CORRODED FROM LBL 36 TO RBL 36. REMOVED THE CORRODED TRANSVERSE BEAM AND INSTALLED A NEW TRANSVERSE BEAM IAW BOMBARDIER REO 670-53-11-047 REV C. 2L72 4F RTA21EA 20050822001742005082200174EA 2005 8 22 COMA0560400 120050718A304016591 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA WINDSHIELD HEAT MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01436CA12293 7482 FLIGHT 5484 - RIGHT WINDSHIELD HEAT CAUTION. REPLACED THE WINDSHIELD HEAT CONTROLLER. 2L72 4F RTA21EA 20050822001752005082200175EA 2005 8 22 COMA0560423 120050802A27508575D100101 COUPLING CNDAIRCL600 CL6002B19 1900309EA LT TE FLAP MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01989CA 7215 FLIGHT 5454 - FLAP FAIL CAUTION. REPLACED THE LT NR 1 FLEY DRIVE SHAFT. 2L72 4F RTA21EA 20050822001762005082200176EA 2005 8 22 COMA0570090 120050729A531267053110521 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA FS 280 CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01354CA7620 10064 FS 280 BULKHEAD LOWER WEBS ARE CORRODED BEYOND LIMITS FROM LBL 36 TO RBL 36. REPLACED THE FS 280 BULKHEAD LOWER WEBS IAW BOMBARDIER REO 670-53-11-052 REV A REPAIR 2. 2L72 4F RTA21EA 20050822001772005082200177EA 2005 8 22 COMA0560434 120050808A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAP MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01976CA 7151 FLIGHT 5178 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2L72 4F RTA21EA 20050823000012005082300001EA 2005 8 23 COMA0560452 120050818A27419660013 SWITCH CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A COMAO OTHER O OTHER APAPPROACH 1 SO01489CA 7755 FLIGHT 5386 - STAB AND MACH TRIM WILL NOT DISENGAGE. REPLACED THE PILOTS STAB TRIM DISCONNECT SWITCH ON CONTROL YOKE. 2L72 4F RTA21EA 20050823000022005082300002EA 2005 8 23 COMA0560444 120050812A2913848847 PUMP CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM MALFUNCTIONED A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01981CA150102755 7163 FLIGHT 5428 - GEAR DISAGREE WARNING. REPLACED HYDRAULIC PUMP 3A. 2L72 4F RTA21EA 20050823000062005082300006NM 2005 8 23 UPS05245205 120050802A5320 SUPPORT BOEING727 72730C 1384009NM BS 302-344 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919UP 19012 INSPECTION TYPE:C FWD LAV PARTITION SUPPORT STRUCTURAL EXTRUSION CORRODED BS 302 - 344 DOOR THRESHOLD AREA. PARTITION SUPPORT STRUCTURE EXTRUSION REPLACED IAW SRM 51-10-2, 51-20- 2 & 51-30-2. 2L73 4F A3WE 20050823000072005082300007NM 2005 8 23 UPS05245206 120050731A5320 WEB BOEING727 72730C 1384009NM BS 294.5 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919UP 19012 INSPECTION TYPE:C RT SIDE AFT OF RT 294.5 FWD ATTACHMENT ANGLE OF NWW BOX AND RT HAS EVIDENCE OF CORROSION. REPAIR CARRIED OUT IAW SRM 51-10-6, 53-10-1 & 51-40-2. 2L73 4F A3WE 20050823000082005082300008NM 2005 8 23 UPS05245207 120050803A5320 INTERCOSTAL BOEING727 72730C 1384009NM BS 294.5 - 312 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919UP 19012 INSPECTION TYPE:C, CORROSION ON INTERCOSTAL BS 294.5 - BS 312 LBL 33. INTERCOSTAL REPLACED IAW BOEING DWG 65-17593 AND SRM 51-30-02. 2L73 4F A3WE 20050823000092005082300009NM 2005 8 23 UPS05545209 120050720A5347146N52191 SEAT TRACK BOEING757 75724APF 1384969NM MCD CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01401UP 23723 INSPECTION TYPE:C SEAT TRACK CORRODED BS 1180 - 1200 RBL 46. REMOVED AND REPLACED SEAT TRACK BS 1180 - 1329.5 RBL 46 IAW SRM 53-00-52 FIG 201. 2L72 4F RTA2NM 20050823000102005082300010 2005 8 23 SWAA052488 420050817A256565C16820 HOOK BOEING737 7373H4 1384600NM R2 DOOR SLIDE LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29642WN 27715 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER MM. 2L72 4F RTA16WE 20050823000112005082300011 2005 8 23 SWAA052489 420050817A2565D31354418 SLIDE BOEING737 7373H4 1384600NM L2 DOOR DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29654SW 28399 DURING SCHEDULED RON CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATING LOW. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20050823000122005082300012 2005 8 23 SWAA052490 420050818A25656557450 COVER BOEING737 7373T5 1384608NM L1 DOOR SLIDE LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29694SW 23061 L1 DOOR EMERGENCY EVAC SLIDE COVER LOOSE. SECURED SLIDE COVER PER MM. 2L72 4F RTA16WE 20050823000152005082300015NM 2005 8 23 CALA0500267 120050818A5311654653949 FRAME BOEING737 7373T0 1384582NM STA 616 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714335 23573 INSPECTION FOUND A .5 INCH CRACK IN LT MAIN FRAME BELOW MAIN DECK FLOOR AT STA 616, S18L TO S19L. A FILLER AND ANGLE REPAIR WAS INSTALLED IAW ECRA 5311-01158, PAGE 1-9. 2L72 4F RTA16WE 20050823000162005082300016NM 2005 8 23 CALA0500268 120050818A53206517688175 CHANNEL BOEING737 737524 1384721NM STA 277-360 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2746625 27529 INSPECTION FOUND L-1 DOOR ENTRY Z-CNANNEL CORRODED AT STA 277-360, LBL 39. A NEW Z-CHANNEL WAS INSTALLED IAW SRM 51-40-02. 2L72 4F RTA16WE 20050823000172005082300017 2005 8 23 SWAA052493 420050817A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29796SW 27889 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050823000192005082300019WP 2005 8 23 AALA20050533 120050818A21216054578 FAN DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21402A 49313 DFW - INFLIGHT ACRID SMELL ACCOMPANIED BY MODEST AMOUNT OF SMOKE REPORTED BY FLIGHT ATTENDANTS. SECURED RECIRCULATION FAN AND SMOKE AND SMELL DISSIPATED QUICKLY. REPLACED RECIRCULATION FAN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050823000202005082300020WP 2005 8 23 AALA20050534 120050818A3350P4010049 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE K FLUID LOSS ININSP/MAINT 1 SW217509 49803 LGA - FORWARD EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK FOR AFT EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050823000212005082300021NM 2005 8 23 AALA20050528 120050817A3350BPS73 BATTERY PACK BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21361AA 24042 EZE - EMERGENCY LIGHTS AT ROWS 20HJ AND 21HJ INOPERATIVE. REPLACED BATTERY PACK AT ROW 20 FOR EMERGENCY LIGHTS AT ROWS 20HJ AND 21HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050823000222005082300022WP 2005 8 23 AALA20050530 120050816A3260 DOWNLOCK SENSOR DOUG DC9 DC982 3022082WP NLG INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21225AA 49175 DFW - INFLIGHT NOSE GEAR UNSAFE LIGHT ILLUMINATED. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND DOWNLOCK SENSOR INOPERATIVE. REPLACED NOSE LANDING GEAR LOCK SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050823000242005082300024WP 2005 8 23 AALA20050532 120050818A3222 STRUT DOUG DC9 DC983 3022083WP NLG INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21566AA 49348 SEA - INFLIGHT LANDING GEAR HANDLE STUCK HALF WAY UP ON GEAR RETRACTION ON TAKEOFF. FOUND NOSE STRUT BINDING. SERVICED NOSE STRUT WITH OIL AND NITROGEN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050823000262005082300026NM 2005 8 23 AALA20050535 120050818A2910271N61191 LINE BOEING757 757223 1384957NM HYDRAULIC SYS RUPTURED A AALAO OTHER K FLUID LOSS TXTAXI/GRND HDL 1 SW21603AA 27054 BOS - AT PUSHBACK WHEN BRAKES WERE RELEASED HYDRAULIC FLEX LINE IN LEFT WHEEL WELL RUPTURED. REPLACED LEFT HAND GEAR WHEEL WELL HYDRAULIC LINE IN UPPER SECTION OF LEFT HAND GEAR AFT OF REAR SPAR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050823000282005082300028 2005 8 23 AALA20050538 420050808A25655A330730 LIGHT BOEING737 737823 13844BZNM SLIDE INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21945AN 30085 TUL - EMERGENCY LIGHT ON FORWARD SERVICE DOOR ESCAPE SLIDE INOPERATIVE NOT HOOKED UP. INSTALLED SERVICEABLE SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20050823000292005082300029NM 2005 8 23 AALA20050539 120050812A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21946AN 30600 TUL - EMERGENCY LIGHT BATTERY PACKS IN CABIN FAILED TEST. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20050823000302005082300030EA 2005 8 23 COMA0560447 120050815A2913848847 PUMP CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01819CA225903200 7415 FLIGHT 5003 - HYDRAULIC SYSTEM 3 LOW PRESSURE CAUTION. REPLACED THE NR 3A ACMP. 2L72 4F RTA21EA 20050823000312005082300031EA 2005 8 23 COMA0570097 120050819A3222521011 CYLINDER CNDAIRCL600 CL6002C10 1390015EA NLG CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01331CA7694 10061 NLG OUTER CYLINDER P/N 52101-1, S/N BA0003 IS CORRODED. CORROSION REPAIRED IAW REO 670-32-21-064 AND GOODRICH SCR 0008-04 REV C. 2L72 4F RTA21EA 20050823000322005082300032EA 2005 8 23 COMA0560448 120050816A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ILLUMINATED A COMAO OTHER J WARNING INDICATION DEDESCENT 1 SO01798CA 7348 FLIGHT 5130 - LEFT THRUST REVERSER UNLOCK CAUTION. DEFERRED MAINTENANCE PER MEL. 2L72 4F RTA21EA 20050823000362005082300036EA 2005 8 23 COMA0560440 120050811A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA LEFT UNRELIABLE A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01937CA1624810828 7044 FLIGHT 5208 - FLAPS FAIL CAUTION. REPLACED THE LT BPSU. 2L72 4F RTA21EA 20050823000382005082300038EA 2005 8 23 COMA0560442 120050812A3297173060000001 WIRE HARNESS CNDAIRCL600 CL6002B19 1900309EA RT MLG MALFUNCTIONED A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01468CA 7649 FLIGHT 5182 - ANTI-SKID CAUTION DURING TAKEOFF. REPLACED THE RT MLG WHEEL SPEED WIRE HARNESS. 2L72 4F RTA21EA 20050823000392005082300039EA 2005 8 23 COMA0560443 120050812A5240 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA ACCESS DOOR OPEN A COMAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 SO01954CA 7100 FLIGHT 5383 - GROUND POWER SWITCH PANEL OPENED IN FLIGHT. INSPECTED FOR DAMAGE AND CLOSED DOOR. 2L72 4F RTA21EA 20050823000432005082300043NE 2005 8 23 DL76G050445 220050811A72611978M64G01 MANIFOLD BOEING767 767332 1382001NM GE CF6 CF680C2B6F 30025NE NR 1 ENGINE UNSERVICEABLE A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO271608 30573 706113 FLT CREW REPORTED NR 1 ENG OIL LOSS DIVERTED TO DXB FOR REPAIRS. ENG WAS NOT SHUTDOWN. ENG OIL TANK SERVICED. ENGINE MOTORED. LEAK TRACED TO OIL LINE TO PRESSURE TRANSMITTER AND LOW PRESSURE SWITCH. LINE AND CLAMP REPLACED AND ENGINE GROUND RUN CARRIED OK. NO LEAKAGE EVIDENT. 2L72 4F4 FRTA1NM E13NE 20050823000442005082300044NM 2005 8 23 DL73S050446 120050810A3350 FUSE BOEING737 737232 1384475NM POWER SUPPLY BLOWN A DALAK NONE L NO TEST ININSP/MAINT 1 SO27327DL 23099 SEAT MOUNTED EMERGENCY EXIT LIGHTS INOP ROWS 11 THRU 15 DEF. REPLACED FUSES ON POWER SUPPLY, CHECK OK. 2L72 4F RTA16WE 20050823000462005082300046NM 2005 8 23 DL76L050448 120050811A2530828450407 OVEN BOEING767 767332 1382001NM AFT GALLEY SMOKE A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27173DN 24800 BOTH AFT GALLEY OVENS PRODUCED SMOKE. C/BS PULLED. CKD OVENS FOUND BUN BEHIND THE TRAY. OPERATED FOR 30 MINS. OPS NORM, OVEN CLEANED. 2L72 4F RTA1NM 20050823000472005082300047NM 2005 8 23 DL73S050449 120050812A7830 TRANSMITTER BOEING737 737247 138448DNM THRUST REVERSER LEAKING A DALAA UNSCHED LANDING KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27243WA 23517 ODOR IN CABIN, DIVERSION TO CLT. FOUND HYDRAULIC LEAK AT RT THRUST REVERSER PRESSURE TRANSMITTER LEAKING INTO RT PACK INLET. SECURED LEAK. CLEANED PACK INLET. REPLACED COALESCER. 2L72 4F A16WE 20050823000492005082300049EA 2005 8 23 COMA0560425 120050804A5297601R576891 WIRE HARNESS CNDAIRCL600 CL6002B19 1900309EA CARGO DOOR FAULTY A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01915CA 7013 FLIGHT 5687 - DURING CLIMBOUT OF ERI RECEIVED A CARGO DOOR CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE CARGO DOOR WIRING HARNESS. 2L72 4F RTA21EA 20050823000512005082300051EA 2005 8 23 COMA0560451 120050817A3030 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA ADS FAILED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01492CA 7763 FLIGHT 5395 - LEFT PITOT HEAT, AOA HEAT, STATIC AND PITOT HEAT CAUTIONS. CND, RESET THE ADS CONTROLLER, SYSTEM CHECKS GOOD. 2L72 4F RTA21EA 20050823000532005082300053NM 2005 8 23 CALA0500270 120050820A5313BAC1498161 STRINGER BOEING737 7373T0 1384582NM STA 867-887 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714335 23573 INSPECTION FOUND STRINGER 25R IN THE AFT BAGGAGE BIN CORRODED AT STA 867-887, RBL 27. A SECTION OF STRINGER AND DOUBLERS WAS INSTALLED IAW SRM 53-00-03. 2L72 4F RTA16WE 20050823000562005082300056NM 2005 8 23 CALA0500273 120050821A5320141A541012 INTERCOSTAL BOEING737 737824 13844BZNM BS 312-328 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712216 28776 INSPECTION FOUND A 2 INCH CRACK IN INTERCOSTAL BETWEEN BS 312 AND 328, LBL 44. A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-40-02 AND 53-00-51. 2L72 4F RTA16WE 20050823000572005082300057NM 2005 8 23 CALA0500274 120050821A5320141A541012 INTERCOSTAL BOEING737 737824 13844BZNM STA 312-328 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712216 28776 INSPECTION FOUND A 2 INCH CRACK IN INTERCOSTAL BETWEEN STA 312 AND 328, RBL 44. A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-80-02 AND 53-00-51. 2L72 4F RTA16WE 20050823000582005082300058NM 2005 8 23 CALA0500275 120050821A5315141A5506 FLOORBEAM BOEING737 737824 13844BZNM STA 360 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712216 28776 INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 360, LBL 8. REPAIRED IAW ECRA 5321-01277. 2L72 4F RTA16WE 20050823000592005082300059EU 2005 8 23 SF200508122 120050812A2914 COUPLING SAAB SF340 SF340A 7850100EU HYD HAND PUMP SPLIT A UHLAO OTHER O OTHER NRNOT REPORTED 1 GL1719XS 340A019 8-12-2005, FLT 7556 IAD-ABE, ON PREFLIGHT OF AIRCRAFT, AIRCREW NOTICED THE HYD HAND PUMP FEMALE COUPLING SPLIT IN HALF. AIRCREW NOTIFIED MAINTENANCE. MAINTENANCE REMOVED AND REPLACED HYD HAND PUMP HANDLE FEMALE RECEPTACLE. 2L72 4T RTA52EU 20050823000632005082300063CE 2005 8 23 HSYA01081205 120050812A79311013890233 TRANSMITTER BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA OIL PRESSURE FAILED E HSYAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM05318BH UB36 ON CLIMBOUT, NR 2 ENGINE OIL PRESSURE DROPPED TO ZERO. ENGINE WAS SECURED AND SHUT DOWN AND AIRCRAFT RETURNED TO SJU, EMERGENCY DECLARED. PROPELLER FEATHERED. APPARENT CAUSE OF PROBLEM - RT ENGINE OIL PRESSURE TRANSMITTER FAILURE. TROUBLESHOT AND FOUND OIL PRESSURE TRANSMITTER FAILED. REMOVED AND REPLACED TRANSMITTER. OPS CHECKED GOOD IAW BEECH 1900 MM 79-30-50 ON WAR CARD 222512. 2L72 4T4 TRTA24CE E4EA 20050823000642005082300064 2005 8 23 YENA200546 420050807A23303042865102 ELECTRICAL BOX AIRBUS320 A320232 3930326EU LIVE TV ODOR A YENAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15587JB5944 2177 RUBBER SMELL REPORTED IN VICINITY OF ROWS 13-16 ON LEFT SIDE OF A/C. LIVE TV TURNED OFF AND SMELL WENT AWAY. INITIALLY LIVE TV SYSTEM WAS DEFERRED PER MEL 25-22-03D. LATER AT JFK, ISPECTION PER JB INFO NOTICE 2004-T023TR, JB WC 233900-J1-17 AND LTV MM 23-39-00 REVEALED NO FAULT. AS A PRECAUTIONARY MEASURE SEB AT 14B REPLACED. 2L72 4F RTA28NM 20050823000652005082300065NM 2005 8 23 UPS05245199 120050815A33501000679 BATTERY BOEING727 72722C 138400FNM COCKPIT INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01941UP 19196 WITH EMERGENCY EXIT SWITCH ON, COCKPIT AND MAIN ENTRY DOOR LIGHTS DO NOT COME ON REPLACED BATERIES 2L73 4F A3WE 20050823000662005082300066NM 2005 8 23 UPS05445208 120050816A5220 SKIN BOEING747 747212B 1384886NM ESCAPE HATCH DENTED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01526UP 21937 INSPECTION TYPE:N/A SEVERAL DENTS IN CREW EMERGENCY ESCAPE HATCH OUTER SKIN S/M. DOOR REMOVED FOR REPAIR S/M SHOP. FABRICATED NEW SKIN IAW 52-20-01 OK TO INSTALL INNER AND OUTER SKIN. INSTALLED OUTER SKIN PER SRM 51-36-02. FINISHED INSTALLATION OF INNER SKIN PER SRM 51-40-02. REF LP 4440326. 2L74 4F A20WE 20050823000672005082300067WP 2005 8 23 UPS05845201 120050729A33505708458503 BATTERY PACK DOUG DC8 DC873F 302199FWP COCKPIT INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01840UP 46140 INSPECTION TYPE:PNT EMERGENCY EXIT LIGHTS FAILED TEST REMOVED AND REPLACED BATTERY PACK. OPS CHECK NORMAL 2L74 4F RT4A25 20050823000682005082300068WP 2005 8 23 UPS05845202 120050811A53403779762U501 FITTING DOUG DC8 DC871F 302199DWP STA 680 L2R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 INSPECTION TYPE:C1 MAIN CABIN LONGERON END FITTING CRACKED (2 INCHES) STA 680 L2R. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D,51-1-21,AND 51-1-23 . 2L74 4F RT4A25 20050823000692005082300069WP 2005 8 23 UPS05845203 120050811A5320 FINGER DOUBLER DOUG DC8 DC871F 302199DWP FS960-980 RBL 65CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 INSPECTION TYPE:C1 MAIN CABIN SUB FLOOR FINGER DOUBLER CORRODED AND SHEAR HEAD FASTENER A T STA 960 TO 980 RBL 65. REMOVED, FABRICATED, AND INSTALLED FINGER DOUBLER IAW DWG 5645332 AND DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20050823000712005082300071 2005 8 23 YENA200547 420050816A233020092455101 COOLING FAN AIRBUS320 A320232 3930326EU AVIONICS COMP FAILED A YENAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 EA15598JB3320 3320 2314 JUST PRIOR TO DESCENT AFT AVIONICS COMPARTMENT INDICATED SMOKE. RESET SYSTEM AND TESTED OK. LEFT SYSTEM OFF FOR REST OF FLIGHT. R&R COOLING FAN ASSY IAW LTV MM 23-39-00, OPS CHECK GOOD. 2L72 4F RTA28NM 20050823000722005082300072 2005 8 23 YENA200548 420050816A2397 WIRE AIRBUS320 A320232 3930326EU CONTROL UNIT BROKEN A YENAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15583JB 2150 F/A INFORMED COCKPIT OF BURNING ODOR TYPE SMELL EMINATING FROM AFT CABIN. ODOR DISSIPATED WHEN LIVE TV SWITCH WAS PLACED OFF. PERFORMED INFO NOTICE 2004-TO23TR, FOUND DPCU CABLE WITH TWO (2) BROKEN WIRES. PLACED ON MEL REF 25-22-03, CAT D CONTROL L02110. INSTALLED PLACARD. NOTIFIED MCC. 2L72 4F RTA28NM 20050823000732005082300073NM 2005 8 23 XN0A1257 120050817A2420 GENERATOR BOEING727 727227 1384078NM NR 2 OVERTEMP A XN0AO OTHER MJ OVER TEMP WARNING INDICATION NRNOT REPORTED 1 GL23793A 20774 AC GEN DRIVE OIL TEMP IN CAUTION RANGE GEN NR 2. CLEANED CONNECTORS AT BOTH TEMP BULB. CHECKED MAG PLUG - NO CONTAMINATION. CHANGED CSD OIL & OPS CHECK GOOD IAW MM 24-10-0 & 24-20-0. (ORIG/CLOSED). 2L73 4F A3WE 20050823000752005082300075SO 2005 8 23 RAIA00508022 120050815A3350 LIGHT EMB 145 EMB145EP 3260221SO CABIN INOPERATIVE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03826HK 145016 FLT 5558-MSP-CREW REPORTED THAT EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE PERFORMED OPS CHECK OF EMERGENCY LIGHT SYSTEM. NO DEFECTS NOTED. 2L72 4F RTT00011AT 20050823000762005082300076SO 2005 8 23 RAIA00508025 120050816A3397 CONTACT EMB 145 EMB145EP 3260221SO EMERGENCY LIGHT DIRTY A RAIAK NONE O OTHER ININSP/MAINT 1 CE03826HK 145016 FLT 5501-STL-EMERGENCY EXIT LIGHTS ON THE FLOOR INOPERATIVE. MAINTENANCE CLEANED THE CONTACTS ON THE EMERGENCY LIGHTS TRACK. 2L72 4F RTT00011AT 20050823000772005082300077SO 2005 8 23 RAIA00508019 120050813A2910AE7138001 LINE EMB 145 EMB145LR 3260212SO HYD SYSTEM BROKEN A RAIAD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 CE03811HK 145256 FLT 3537-PIT-NR 4 BRAKE INBOARD HYDRAULIC QUICK DISCONNECT LINE BROKEN. MAINTENANCE REMOVED AND REPLACED THE BRAKE HOSE ASSEMBLY. 2L72 4T RTT00011AT 20050823000782005082300078GL 2005 8 23 RAIA00508020 220050814A7313 FUEL NOZZLE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL ENGIN ODOR A RAIAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 CE03850HK 145003 FLT 8063-STL-FLIGHT CREW REPORTED NOXIOUS ODOR WHEN ANTI-ICE SYSTEM WAS ACTIVATED. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE FUEL NOZZLES. 2L72 4T4 FRTT00011ATTE6CH 20050823000792005082300079SO 2005 8 23 RAIA00508021 120050815A3350RPS1B POWER SUPPLY EMB 145 EMB145EP 3260221SO EMERENCY LIGHT INOPERATIVE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03827HK7099 847 145021 FLT 5493-CLT-EMERGENCY FLOOR LIGHTING INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY. 2L72 4F RTT00011AT 20050823000812005082300081NM 2005 8 23 AWXA200500965 120050803A5320655287873 WEB BOEING737 7373Y0 1384671NM DOOR SILL CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28334AW 23747 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED CORROSION AROUND AFT DRAIN TUBE HOLE IN THE L2 DOOR SILL WEB AT BS 987, BL 65L, AND WL 208. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-15-1 FIG 107. REMOVED L2 DOOR SILL WEB AT BS 986, BL 65L, WL 208 IAW BOEING 737-300 SRM 51-40-02-0. FABRICATED REPLACEMENT SILL WEB IAW BOEING 737-300 SRM 51-40-05-0 FIG 2. INSTALLED REPAIR PARTS AT BS 987, BL 65L, AND WL 208 IAW BOEING 737-300 SRM 51-40-02-0 FIGS 8, 13 AND BAC DWG 65-52878. 2L72 4F RTA16WE 20050823000822005082300082NM 2005 8 23 AWXA200500966 120050731A5320655287897 SILL BOEING737 7373Y0 1384671NM CABIN CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28334AW 23747 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED CORROSION ON THE L2 DOOR SILL INNER CHORD, UPPER SURFACE AT BS 951, BL 50L AND WL 208. REMOVED CORROSION AT L2 DOOR SILL INNER CHORD, UPPER SURFACE AND FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-8-1. MAINTENANCE REMOVED L2 DOOR SILL INNER CHORD IAW BOEING 7370-300 SRM 51-40-02-0. RECEIVED NEW INNER CHORD AND PREPARED FOR INSTALLATION IAW BOEING 737-300 SRM 51-40-05-0 FIG 4. INSTALLED NEW INNER CHORD AT BS 951, BL 50L AND WL 208 IAW BOEING 737-300 SRM 51-40-02-0 FIG 3, 4, 6, 7 AND 12. 2L72 4F RTA16WE 20050823000832005082300083NM 2005 8 23 AWXA200500967 120050802A532069366565 SHEAR WEB BOEING737 7373Y0 1384671NM INTERCOSTAL CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28334AW 23747 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED CORROSION ON UPPER FLANGE OF INTERCOSTAL LOCATED AT BS 940, BL 0, WL 208. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-51-1 FIG 101. REMOVED INTERCOSTAL SHEAR WEB FROM BS 940, BL 0 AND WL 208 IAW BOEING 737-300 SRM 51-40-02. FABRICATED REPLACEMENT SHEAR WEB IAW BOEING 737-300 SRM 51-30-01-0. INSTALLED FABRICATED REPAIR PARTS AT BS 940, BL 0, WL 208 IAW BOEING 737-300 SRM 51-40-02-0 FIGURES 3, 8, 12, 13 AND BAC DWG 69-36656. 2L72 4F RTA16WE 20050817001802005081700180WP 2005 8 17 ASAA0580409 120050725A52305910141129 SKIN DOUG DC9 DC983 3022083WP FS 1174 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02947AS 53020 OKC - FOUND DURING C-CHECK, AFT CARGO BAY DOOR SKIN IS DENTED. REMOVED DAMAGED AREA. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050817001842005081700184NM 2005 8 17 ASAA0540333 120050703A5311654655138 FRAME BOEING737 7374Q8 138447QNM FS 807 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02775AS 25108 OKC - FRAME 807 FORWARD FACE CORRODED BETWEEN STRINGERS 27L AND 27R. REMOVED DAMAGED SHEAR TIES. FABRICATED AND INSTALLED REPAIR PIECES IAW 737-400 SRM 53-00-07 FIGURE 210. (M) 2L72 4F RTA16WE 20050817001912005081700191WP 2005 8 17 IXXA05SMN126S 120050629A5330 SKIN PANEL DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE 70.000-115.000 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, EXTERNAL FUS CORRODED, STA. 70.000 STA. 115.000, L-35L - L-35R. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PAGE 1, SRM 53-3-1 FIG. 1 ITEM A, EO NR 2005864 DATE 06-13-05. REMOVED CORROSION IAW SRM 51-1-8 PAGES 17, 18, FOUND OUT OF LIMITS IAW SRM 53-2-0 PAGE 2P. REMOVED CORRODED PLATING SEMENT IAW SRM 51-1-21 PAGE 1. FABRICATED EXTERNAL SPLICES (02 EA) (ALCLAD 7075 T6 0.063”) + (02 EA) INTERNAL FINGER DOUBLER (ALCLAD 7075 T6 0.032”) + (02 EA) INTERNAL DOUBLER (ALCLAD 7075 T6 0.050) IAW SRM, CLEANED, TREATED AND PRIMED AREA + REPAIR PARTS IAW SRM. APPLIED SEALANT TO FAYING SURFACES IAW SRM. INSTALLED NEW PLATING SEGMENT (PN 5613862-15N1) + REPAIR PARTS AND TORQUED IAW SRM. 2L74 4F4 FRT4A25 E2GL 20050817002022005081700202NM 2005 8 17 ASAA0540341 120050703A5512657378351 SKIN BOEING737 7374Q8 138447QNM HORIZONTAL STAB DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02775AS 25108 OKC - FOUND LEFT HORIZONTAL STAB L/E STAB STATION 192.54 HAS 2 EACH CREASES. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW 737-400 SRM 55-10-01 FIGURE 203. (M) 2L72 4F RTA16WE 20050817002062005081700206NM 2005 8 17 2005UALA00771 120050806A5311 SPLICE BOEING757 757222 1384956NM PWA 2037 PW2037 NE STA 1420 FRAME DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29587UA 26713 FRAME SPLICE AT STA 1420 BETWEEN STR 24L AND 25L IS DENTED ON TOP IN AFT CARGO PIT. TRIMMED OUT DAMAGE, ACP HEFC NDT INSP, NO CRACK FOUND. REPAIR PER TIMCO REO-G10762, REV B, AND UAL EVA 50517. 2L72 4F4 FRTA2NM E17NE 20050817002112005081700211NM 2005 8 17 2005UALA00776 120050808A5350 SKIN BOEING747 747422 1384935NM PWA 4056 PW4056 NE RADOME BIRD STRIKE A UALAK NONE O OTHER ININSP/MAINT 1 WP29121UA 29167 CREW REPORT STRIKING TWO LARGE BIRDS ON CLIMB-OUT FROM ORD. STRUCK THE LOWER NOSE OR BELLY OF THE AIRCRAFT PASSING THROUGH 4800 FT. BIRD IMPACT DAMAGE TO RADOME AND SKIN FLANGE STRUCTURE FWD OF FWD PRESSURE BHD. RADOME REPLACED; STRUCTURE REPAIRED PER UA EVA 50523A WITH FAA FORM 8100-9 APPROVAL. 2L74 4F4 FRTA20WE E24NE 20050817002172005081700217NM 2005 8 17 2005UALA00783 120050808A2800 TOTALIZER BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE FUEL SYS MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29786UA 26938 CREW REPORTED FUEL IMBALANCE, INCORRECT TOTALIZER & FMC CALCULATED TO CONTINUE TO LHR. KICKED OFF A-P & ACFT LT WING HEAVY. MX REPLACED FUEL QTY PROCESSING UNIT. FAULT REPEATED INBOUND. FUEL TANK PROBES R13 & R14 REPLACED. NO FURTHER FUEL IMBALANCE OR INDICATION PROBLEMS NOTED. PRIOR, ACFT PROBLEM WITH RT TANK UNDERWING FUEL GAUGE INOP & REFUELING VALVE NOT OPENING. REPLACEMENT OF FQPU & FUEL TANK PROBES R13 & R14 AS A RESULT OF THIS EVENT DID NOT CORRECT THIS PROBLEM. THE PROBLEM WAS FINALLY CORRECTED WHEN THE INTEGRATED REFUEL PANEL REPLACED ON 8/30/05. NO FAULTS FOUND ON REPLACED FQPU & FUEL TANK PROBES R13 & R14. REPLACED IRP FAILED TEST AT VENDOR & REPAIRED. 2L72 4F4 FRTT0001SE E46NE 20050817002182005081700218NM 2005 8 17 2005UALA00784 120050807A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE L1 DOOR INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29194UA 26892 DOOR 1L EMERGENCY LIGHT INOP. 2L74 4F4 FRTA20WE E24NE 20050817002192005081700219NM 2005 8 17 2005UALA00785 120050806A33501317 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE ROW 22 & 37 BURNED OUT A UALAK NONE L NO TEST ININSP/MAINT 1 WP29120UA 29166 CEILING EMERGENCY LIGHT AT ROW 22 LT AND 37 RT INOP. REPLACED LAMP. 2L74 4F4 FRTA20WE E24NE 20050823000852005082300085NM 2005 8 23 AWXA200500969 120050731A53156546568122 FLOORBEAM BOEING737 7373Y0 1384671NM CABIN CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28334AW 23747 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED CORROSION UNDER SURFACE OF BEAM LOCATED AT BS 1016, BL 6R, AND WL 208. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-51-1. MAINTENANCE FABRICATED REPAIR STRAP IAW BOEING 737-300 SRM 53-00-57-2 FIG 203. INSTALLED FABRICATED REPAIR PARTS AT BS 1016, BL 6R, AND WL 208 IAW BOEING 737-300 SRM 53-00-51-20 FIG 203. 2L72 4F RTA16WE 20050823000872005082300087NM 2005 8 23 AWXA200500971 120050728A531565613181161 FLOORBEAM BOEING737 7373Y0 1384671NM CABIN CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28334AW 23747 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED CORROSION ON FLOOR BEAM SUPPORT AT BL 29L AND BL 14R, BS 995, WL 208. MAINTENANCE REMOVED CORROSION FROM FLOOR BEAM SUPPORTS AND FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-51-1 FIG 101. REMOVED FLOOR BEAM AT BL 29L AND BL 14R, BS 995, WL 208 IAW BOEING 737-300 SRM 51-40-02-0. FABRICATED NEW FLOOR BEAM SUPPORTS IAW BOEING 7 37-300 SRM 51-40-05-0 FIG 2, FIG 4 AND BOEING DWG 65-61381. INSTALLED FABRICATED REPAIR PARTS AT BL 29L AND BL 14R BS 995, WL 208 IAW BOEING 737-300 SRM 51-40-02-0 FIG 12 AND BAC DWG 65-61381. 2L72 4F RTA16WE 20050823000882005082300088NM 2005 8 23 AWXA200500972 120050730A53206546812181 FLOOR SUPPORT BOEING737 7373Y0 1384671NM CABIN CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28334AW 23747 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED CORROSION ON UNDERSIDE OF FLOOR SUPPORT STRUCTURE AT BS 1010, WL 208, BL 7R. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-51-1 FIG 101. REMOVED FLOOR SUPPORT AT BS 101, WL 208, BL 7R IAW BOEING 737-300 SRM 51-40-02. FABRICATED NEW FLOOR SUPPORT IAW BOEING 737-300 SRM 51-40-05-0, BOEING 737-300 SRM 53-60-51-0 FIG 1, AND BOEING DWG 65-46812. INSTALLED FABRICATED REPAIR PARTS AT BS 1010, WL 208, BL 7R IAW BOEING 737-300 SRM 51-40-02-0 FIGS 12, 14. 2L72 4F RTA16WE 20050823000892005082300089NM 2005 8 23 AWXA200500973 120050801A5320654587526 SHEAR WEB BOEING737 7373Y0 1384671NM CABIN CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28334AW 23747 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED CORROSION LOCATED ON MAIN CABIN SHEAR WEB AT BS 288, STR 17, BL 54R, WL 208.1. CORROSION WAS REMOVED AT BS 288, STR 17, BL 54R, WL 208.1 AND FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-10-15-1 FIG 101. REMOVED SHEAR WEB FROM BS 270 TO BS 290, STR 17, BL 54R, WL 208.1 IAW BOEING 737-300 SRM 51-40-02-0 AND FABRICATED REPLACEMENT SHEAR WEB IAW BOEING 737-300 SRM 51-40-02 AND BAC DWG 65-45875. INSTALLED FABRICATED REPAIR PARTS FROM BS 270 TO BS 290, STR 17, BL 54R, WL 208.1 IAW BOEING 737-300 SRM 51-40-02-0. 2L72 4F RTA16WE 20050823000902005082300090NM 2005 8 23 AWXA200500974 120050726A57536546431285 SKIN BOEING737 7373Y0 1384671NM ZONE 500 - LEFT DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28334AW 23747 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED DISBOND AREA ON INBOARD END OF THE LT OUTBOARD FORE FLAP. MAINTENANCE REMOVED DISBONDED SKIN AND CORE FROM LT OUTBOARD FORE FLAP IAW BOEING 737-300 SRM 51-70-10-0. FABRICATED REPAIR CORE, FILLER AND REPAIR DOUBLER IAW BOEING 737-300 SRM 51-70-10-0. BONDED AND SEALED REPAIR PARTS TO INBOARD END OF L/H OUTBOARD FORE FLAP IAW BOEING 737-300 SRM 51-70-10-0 REPAIR 7. 2L72 4F RTA16WE 20050823000932005082300093NM 2005 8 23 AWXA200500977 120050727A534065353501 STRINGER CLIP BOEING737 7373Y0 1384671NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28334AW 23747 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED CRACKED, .2 INCHES IN LENGTH, STRINGER TIE AT BS 727B, STR 26L. MAINTENANCE REMOVED STRINGER TIE AT BS 727B, STR 26L IAW BOEING 737-300 SRM 51-40-02-0. PREPARED REPLACEMENT STRINGER TIE FOR INSTALLATION IAW BOEING 737-300 SRM 51-40-02-0. INSTALLED REPAIR PARTS AT BS 727B, STR 26L IAW BOEING 737-300 SRM 51-40-02-0 FIG 12. 2L72 4F RTA16WE 20050823000962005082300096NM 2005 8 23 AWXA200500980 120050725A53306545800219 SKIN BOEING737 7373Y0 1384671NM L1 DOOR CUTOUT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28334AW 23747 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED CRACK, .150 INCHES IN LENGTH, AT L1 DOOR CUTOUT JUST BELOW AFT CORNER AT FASTENER. MAINTENANCE REMOVED CRACK IAW AMERICA WEST AIRLINES ENGINEERING REPAIR 03-5211-05224-ES1. FABRICATED DOUBLER, TRIPLER, FILLERS AND SCUFF PLATE IAW AWA ER 03-5311-05224-ES1. INSTALLED FABRICATED REPAIR PARTS AT L1 DOOR CUTOUT JUST BELOW AFT CORNER. 2L72 4F RTA16WE 20050823000982005082300098CE 2005 8 23 72383 120050817A77121143800653 INDICATOR BEECH 1900 1900D 1154162CE TORQUE FAILED A AMWAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE07144ZV2058 2058 UE144 UPON TAKE OFF ROLLOUT, CREW NOTICED RIGHT ENGINE TORQUE INDICATOR STUCK AT 3000LBS. ABORTED TAKE OFF AND RETURN TO GATE WITH NO FURTHER INCIDENT. THE CORRECTIVE ACTION WAS AS FOLLOWED: MAINTENANCE REMOVED AND REPLACED TORQUE INDICATOR AND TRANSMITTER. 2L72 4T RTA24CE 20050823001012005082300101NE 2005 8 23 05FDEA02478 220050816A7200 ENGINE BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE NR 3 FAILED A FDEAEA ENGINE SHUTDOWN UNSCHED LANDING MBJOVER TEMP SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SO25241FE 20979 DURING CLIMBOUT S/O NOTICED RT MANIFOLD DROP TO ZERO. THIS WAS FOLLOWED BY NR 3 STRUT OVERHEAT LIGHT & ACRID SMELL. FOLLOWED QRH TO NR 3 ENGINE SHUTDOWN & EMERGENCY RETURN TO ONT. 20 MIN ENGINE WINDMILLING. STRUT EXTINGUISHED AFTER ABOUT 3 MINUTES. (OPEN) 2L73 4F4 FRTA3WE E2EA 20050823001042005082300104NM 2005 8 23 05FDEA02484 120050816A2150 A/C PACK DOUG MD11 MD11 3023602NM NR 1 ODOR A FDEAAJ UNSCHED LANDING DUMP FUEL B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO25599FE 48598 AFTER T/O AT TOP OF CLIMB, NOTICED STRONG ACRID ODOR & SMOKE IN COCKPIT. RETURNED TO ANC. ISOLATED TO NR 1 PACK. PERFORMED AC PACK & DISTRIBUTION DUCT CLEANING. ODOR REMAINS NO SMOKE NOTED. PERFORMED NR 1 AC PACK FUNCTIONAL CHECK. ODOR IS DISSIPATING. UNABLE TO REPRODUCE SMOKE AS DURING INITIAL TS. PACKS WERE OPERATED USING BOTH APU & NR 1 ENGINE PNEUMATIC SUPPLY. REPLACED NR 1 PACK ALESCER BAG, NR 1 ENG PRV. INSPECTED PNEUMATIC DUCT FOR EVIDENCE OF OIL. NONE FOUND. RAN NR 1 ENG PER MD-11 JRH. COULD NOT INDUCE SMOKE COCKPIT. AC RELEASED FOR SERVICE PER MEL/CDL: 36-10-02-A. 2L73 4F RTA22WE 20050823001052005082300105NM 2005 8 23 05FDEA02485 120050816A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 CORROSION ON FUSELAGE SKIN IS BULGED AT BS 1015 STRINGER 30. REMOVED CORROSION SPEC C53-100-03 FUSELAGE SKIN AT B.S. 1015 STR 30 FOUND TO BE OUT OF LIMITS. INSTALLED STRINGER REPAIR PER SMR 51-30-2, 53-10-1. (CLOSED) 2L73 4F RTA3WE 20050823001062005082300106NM 2005 8 23 05FDEA02486 120050816A54136519645156 LONGERON BOEING727 727200 138407ENM NR 2 ENG COWL CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 NR 2 LT FWD ENG COWL IS CRACKED IN THE LOWER FRAME ABOVE EACH ALIGNMENT PIN. REMOVED AND REPLACED LONGERON (FRAME.) 2L73 4F RTA3WE 20050823001122005082300112EA 2005 8 23 SWIA200515418 120050809A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07916SW 7634 CEILING EMERGENCY LIGHT BY LAV INOP. RELAMPED AFT EMERGENCY CEILING LIGHT BY LAV IAW CRJ MM 33-51-16. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050823001152005082300115EA 2005 8 23 SWIA200515421 120050812A274170608 TRIM SYSTEM CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07437SW1069410694 7564 STAB TRIM CH1 INOP. REPLACED HSTCU IAW 27-40-00. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050823001162005082300116EA 2005 8 23 SWIA200515422 120050808A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07439SW 7578 FORWARD MOST OVERHEAD EMERGENCY FLOOD LIGHT INOP. REPLACED LAMP, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050823001242005082300124EA 2005 8 23 SWIA200515430 120050803A27604916420 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07441SW3412 3412 7602 FLT SPLRS FAULT STATUS, OB GND SPLR FAULT STATUS AT GATE. REPLACED NR 1 SECU IAW 27-61-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050823001262005082300126NM 2005 8 23 UPS05545210 120050720A5347146N52181 SEAT TRACK BOEING757 75724APF 1384969NM MCD CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01401UP 23723 SEAT TRACK CORRODED BS 1318 RBL 44 AND 46 WL 208. REMOVED AND REPLACED SEAT TRACK FROM BS 1180 TO BS 1318 RBL 45 WL 208 PER SRM 53-00-52. 2L72 4F RTA2NM 20050823001302005082300130NM 2005 8 23 UPS05545214 120050720A5347146N521801 SEAT TRACK BOEING757 75724APF 1384969NM MCD CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01401UP 23723 SEAT TRACK CORRODED, BS 1180 - 1200, RBL 26 WL 208. REPLACED SEAT TRACK SECTION, BS 1180 - 1225 PER SRM 53-00-52-2R 5 FIG 201. 2L72 4F RTA2NM 20050823001352005082300135NM 2005 8 23 UPS05545223 120050818A3350BP73 BATTERY BOEING757 75724APF 1384969NM EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01471UP 28842 EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY ASSY PWR SUPPLY/EMERGENCY LIGHTS IAW MM 33-51-07-2. SYSTEM OPS CK NORMAL. 2L72 4F RTA2NM 20050823001362005082300136WP 2005 8 23 UPS05845219 120050812A53404750419U502 FITTING DOUG DC8 DC871F 302199DWP FS 1150 L19R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 FITTING CRACKED AT FS 1150 L19R. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20050823001422005082300142EA 2005 8 23 SWIA200515434 120050816A2721 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA TRIM SYSTEM INTERMITTENT A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07953SW 7813 RUDDER TRIM SWITCH INTERMITTENT. REPLACED TRIM CONTROL PANEL FOR AILERON AND RUDDER . OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050823001432005082300143 2005 8 23 SWIA200515435 420050815A22166225734002 SERVO EMB 120 EMB120ER 3260203SO ELEVATOR BINDING A SWIAO OTHER F FLT CONT AFFECTED DEDESCENT 1 NM07235SW1025610256 120310 WHEN AP WAS DISENGAGED, CAPTAIN TRIED TO MANUALLY TRIM NOSE DOWN, BUT TRIM WHEEL WAS BINDING. REMOVED AND REPLACED ELEV TRIM SERVO. OPERATIONAL CHECK GOOD IAW MM 22-11-00. 2L72 4T RTA31SO 20050823001452005082300145SO 2005 8 23 SWIA200515437 120050816A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT DISCHARGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07567SW3240 3240 120342 AFT SECTION OF EMERGENCY LIGHTS INOP. REPLACED AFT ELBP PER MM 33-50-02. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050823001542005082300154WP 2005 8 23 UPS05845226 120050811A53404750521U1 FITTING DOUG DC8 DC871F 302199DWP FS 857 L1 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 LONGERON END FITTING CRACKED AT FS 857.125 L1 FWD SIDE. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20050823001562005082300156WP 2005 8 23 UPS05845228 120050812A5313 LONGERON DOUG DC8 DC871F 302199DWP FS 1746 L14R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 LONGERON 14R CRACKED FS 1746. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 53-2-2 FIG 11. 2L74 4F RT4A25 20050823001602005082300160WP 2005 8 23 UPS05845234 120050808A5330 SKIN DOUG DC8 DC871F 302199DWP FS 1746 L15L CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 FUSELAGE EXTERIOR SKIN CRACKED 1/2 INCH LONG AT STA 1746 L15L. REMOVED DAMAGED AREA FAB`D FILLER, DOUBLER AND FINGER DOUBLER AND INSTALLED IAW SRM 53-2-1 AND 53-2-1 FIG 7. 2L74 4F RT4A25 20050823001622005082300162WP 2005 8 23 UPS05845237 120050811A5320 FINGER DOUBLER DOUG DC8 DC871F 302199DWP FS 925 LBL65 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 MAIN CABIN CENTER SUB FLOOR AT STA 925 LBL 65, FINGER DOUBLER AREA HEAVY CORRODED. REMOVED, FAB`D FINGER DOUBLER AND REPAIRED IAW DWG 5645332 AND SRM 53-0 7-01-0 FIG 010. 2L74 4F RT4A25 20050823001632005082300163WP 2005 8 23 UPS05845238 120050809A5730 SKIN DOUG DC8 DC871F 302199DWP LT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 SEVERE CORROSION BETWEEN OUTER SKIN AND FRAME LOWER SURFACE AT SKIN SEAM IN FRONT OF THE LEFT SIDE FUEL DUMP MANIFOLD. REMOVED EXISTING DOUBLER, REMOVED DAMAGE, FAB`D FILLER AND DOUBLER AND INSTALLED IAW SRM 57-02-00-0, DWG 5649654. 2L74 4F RT4A25 20050823001642005082300164WP 2005 8 23 UPS05845239 120050813A5330 FINGER DOUBLER DOUG DC8 DC871F 302199DWP FS -67 TO -52 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 COCKPIT SUBFLOOR FINGER DOUBLER HAS SHEARED HEAD FASTENERS AND POSSIBLE CORROSION UNDER DOUBLER AT FS -67 TO -52 LBL24. REMOVED AND REPLACED FINGER DOUBLER IAW SRM DWG 5612298 AND SRM 51-1-21 AND 51-1-20D. 2L74 4F RT4A25 20050823001652005082300165WP 2005 8 23 UPS05845240 120050813A5712 RIB DOUG DC8 DC871F 302199DWP XFS 707 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 LT WING LE UPPER RIB CRACKED AT XFS 707. FABED DOUBLER AND REPAIRED RIB IAW DWG 5769466, AND SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20050823001672005082300167WP 2005 8 23 UPS05845242 120050813A5712 RIB DOUG DC8 DC871F 302199DWP XFS 766.250 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 LT LE UPPER RIB CRACKED AT XFS 766.250. FAB`D DOUBLER AND REPAIRED IAW DWG 5769470 AND SRM57-02-00 FIG 2. 2L74 4F RT4A25 20050823001682005082300168EU 2005 8 23 2005UALA00813 120050812A5320 STRAP AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE BTWN FR 33 & FR CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29419UA 487 PREVIOUS STRAP BETWEEN FS 33 AND FS 34 ON STRINGER 42R IS CORRODED. 2L72 4F4 FRTA28NM E40NE 20050823001692005082300169NM 2005 8 23 05FDEA02496 120050817A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 CORROSION ON STR 18A LT SIDE. REPAIRED STR 18A LT SIDE PER SRM 51-30-02, SRM 53-10-01 AND BOEING DWG 65-16334. 2L73 4F RTA3WE 20050823001702005082300170NM 2005 8 23 05FDEA02500 120050817A5320 STRUCTURE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 FOUND CORROSION IN BOLT HOLES AT BS 360, STR 26 LT TO EXCEED THE TOLERANCES ALLOWED BY FEDEX SR27-53-021. REMOVED CORROSION FROM BOLT HOLES AT BS 360, STR 26L AND REPAIRED PER EA 7-5310- 91340. 2L73 4F RTA3WE 20050823001712005082300171NM 2005 8 23 05FDEA02487 120050816A53206517684 INTERCOSTAL BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 FRAME AT STA 303 NEAR 16L IS CRACKED. REMOVED AND REPLACED CRACKED INTERCOSTAL IAW SRM 51-30-2. 2L73 4F RTA3WE 20050823001722005082300172NE 2005 8 23 05FDEA02494 220050817A7200 ENGINE BOEING727 727200 138407ENM PWA JT8 JT8D217C 52053NE NR 1 MALFUNCTIONED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25208FE 22930 REPEAT GRIPE. ON T/O ADVANCED POWER TO STANDARD, NO RESPONSE ON NR 1 ENG. NR 1 ENG SHOWED EPR, N1, EGT, N2 FROZEN. FUEL FLOW MOVED 100PPH. AFTER QRH REJECTING T/O PROCEDURES AND THROTTLES AT IDLE N1=23 PERCENT, EGT 500 C, N2=47 PERCENT. AFTER RETURNING TO THE GATE FOR MAINTENANCE, THROTTLES AT IDLE SHOWED N1 ON NR 1 ENG WAS 10 PERCENT LOWER THAN N1 ON NR 3 ENG. AFTER SEVERAL THROTTLE ADVANCEMENTS NR 1 ENG RETURNED TO NORMAL OPERATION. (OPEN) 2L73 4F4 FRTA3WE E9NE 20050823001742005082300174WP 2005 8 23 05FDEA02558 120050819A5712 RIB DOUG DC10 DC1010 3022110WP RT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 RT WING OUT'B L/E INTERNAL STRUCTURE FOUND 1EA REPAIR ANGLE ON RIB XORS 465. FABRICATED REPAIR ANGLE IAW SRM 57-20-00 FIGURE 1 VOL.1. 2L73 4F A22WE 20050823001792005082300179WP 2005 8 23 05FDEA02563 120050819A5712 RIB DOUG DC10 DC1010 3022110WP RT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 DISCREPANCY: RH WING OUT'B L/E INTERNAL STRUCTURE FOUND 1EA ANGLE REPAIR ON RIB AT XORS 470. CORRECTIVE ACTION: FABRICATED REPAIR ANGLE IAW SRM 57-20-00 FIGURE 1 VOL.1. 2L73 4F A22WE 20050823001812005082300181WP 2005 8 23 05FDEA02565 120050819A5712 RIB DOUG DC10 DC1010 3022110WP RT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 RT WING OUT'B L/E INTERNAL STRUCTURE FOUND 1EA ANGLE REPAIR ON RIB AT XORS 940. FABRICATED REPAIR ANGLE IAW SRM 57-20-00 FIGURE 1 VOL.1. 2L73 4F A22WE 20050823001892005082300189WP 2005 8 23 05FDEA02573 120050819A5712 RIB DOUG DC10 DC1010 3022110WP RT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 RT WING OUT'B L/E INTERNAL STRUCTURE FOUND 1EA ANGLE REPAIR ON RIB XORS 917. REPAIRED IAW SRM 57-00-01 FIGURE 3 VOL.1. 2L73 4F A22WE 20050823001932005082300193EU 2005 8 23 EM05008 120050819A213010014522 CHECK VALVE EMB ERJ170ERJ170100 EU NR 1 A/C PACK INOPERATIVE A USAAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 EA19810MD3046 000026 FLIGHT 1808, DCA TO IAH - UPON REACHING CRUISE ALTITUDE THE CREW RECEIVED "CABIN ALTITUDE HIGH" EICAS MESSAGE. THE FLIGHT LEFT DCA WITH NR 1 PACK ON MEL. THE CREW DECLARED AN EMERGENCY AND DID AN EMERGENCY DESCENT PER QRH. THE OXYGEN MASKS DID NOT DEPLOY. MAINTENANCE - TROUBLESHOT SYSTEM, REMOVED AND REPLACED RT CHECK VALVE. 2L74 4F RTA56NM 20050823001962005082300196NM 2005 8 23 05FDEA02548 120050819A531265291881 RIB BOEING727 727200 138407ENM LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 NR 2 FLAP TRACK CENTER FAIRING AFT FORMER IS CRACKED. REMOVED AND REPLACED RIB IAW SRM 51-30-2 2L73 4F RTA3WE 20050823001972005082300197NM 2005 8 23 05FDEA02549 120050819A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 HORIZONTAL STAB BARREL NUT HOLE LT NR 27 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. [CLOSED] 2L73 4F RTA22WE 20050823001992005082300199NM 2005 8 23 2005UALA00814 120050814A5340 STRINGER CLIP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE AFT PIT STA 727DBENT A UALAK NONE O OTHER ININSP/MAINT 1 WP29327UA 24147 AFT PIT STA 727D STR 20L STRINGER CLIP BENT AND CRACKED. REMOVED AND REPLACED STRINGER CLIP. 2L72 4F4 FRTA16WE E2GL 20050823002002005082300200NM 2005 8 23 2005UALA00815 120050814A5340 STRINGER CLIP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE AFT PIT STA 907 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29327UA 24147 AFT PIT STA 907 STR 24R STRINGER CLIP BENT AND CRACKED. REMOVED AND REPLACED STRINGER CLIP. 2L72 4F4 FRTA16WE E2GL 20050824000022005082400002NM 2005 8 24 05FDEA02502 120050817A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 FORWARD CARGO CEILING AREA, SEAT TRACK AT STA 635, LBL 8.5 FOUND CRACKED. REMOVED AS PER SRM 53-70-00 VOLUME I, FIGURE 1. REPAIR SEAT TRACK AND SPLICES FABRICATED AS PER SRM 53-70-00 VOLUME I, FIGURE 1. HFEC INSPECTION CARRIED OUT AS PER NDT SPM 06-10-01-001 REV. 12 FOUND NO CRACKED. REPAIR PARTS TREATED AS PER SRM 57- 21-01 VOLUME II. SEAT TRACK AND SPLICES INSTALLED AS PER SRM 53-70-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2L73 4F RTA22WE 20050824000052005082400005NM 2005 8 24 05FDEA02507 120050818A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 CABIN SEAT TRACK AT STATION Y1049, -X8.5 FOUND CORRODED. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE I VOLUME I AT STATION Y1009 TO STATION Y1129, -X8.5. 2L73 4F RTA22WE 20050824000062005082400006NE 2005 8 24 05FDEA02503 220050817A7310651670233 DRAIN LINE BOEING727 727200 138407ENM PWA JT8 JT8D17 52049NE NR 1 ENG FUEL CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 NR 1 ENGINE FUEL FEED SHROUD DRAIN LINE IS CRACKED STA 870 LT MLG WW. REMOVED AND REPLACED DRAIN LINE IAW MM 20-10-005-4. 2L73 4F4 FRTA3WE E2EA 20050824000082005082400008NM 2005 8 24 05FDEA02510 120050818A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 MAIN DECK SEAT TRACK AT STATION Y1092, -X8.5 FOUND CORRODED. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE I VOLUME I AT STATION Y1009 TO STATION Y1129, -X8.5. 2L73 4F RTA22WE 20050824000122005082400012NM 2005 8 24 2005UALA00819 120050814A3350767 LAMP BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE DOOR 3L BURNED OUT A UALAK NONE L NO TEST ININSP/MAINT 1 WP29209UA 30215 NR 3 LT DOOR EMERGENCY SLIDE LIGHT INOP. REPLACED LAMP. 2L72 4F4 FRTT0001SE E46NE 20050824000132005082400013NM 2005 8 24 2005UALA00820 120050814A2720 FLT CONTROLS BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE RUDDER MALFUNCTIONED A UALAO OTHER F FLT CONT AFFECTED APAPPROACH 1 WP29784UA 26951 THREE UNCOMMANDED RUDDER MOVEMENTS ON APPROACH. MECHANICS PERFORMED CAT3 CHECKS PER AMM 22-11-00 PG 501, AMM 22-31-00 AND RUDDER ACTUATOR CONFIDENCE CHECK ON MAT, ALL OPS CHECKS NORMAL. ENGINEERING REVIEWED MAINTENANCE RECORDS AND DOWN LINKED CMC FAULT DATA FOR FLIGHT 958. THERE WERE NO REPORTS OF FAULTED FLIGHT CONTROLS, HYDRAULICS OR INSTRUMENT SYSTEMS THAT COULD CAUSE THIS PROBLEM. THERE ARE NO PRIOR REPORTS IN MAINTENANCE HISTORY FOR RUDDER MOVEMENTS. ENGINEERING SUSPECTS THIS REPORT MAY HAVE BEEN DUE TO AN ATMOSPHERIC ANOMALY. AIRPLANE WILL BE MONITORED FOR ANY SYSTEM MALFUNCTIONS. 2L72 4F4 FRTT0001SE E46NE 20050824000162005082400016NM 2005 8 24 2005UALA00823 120050813A33501317 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE ROW 17 BURNED OUT A UALAK NONE L NO TEST ININSP/MAINT 1 WP29116UA 26908 CEILING EMERGENCY LIGHT INOP AT AISLE 17 UPPER DECK. REPLACED LAMP 2L74 4F4 FRTA20WE E24NE 20050824000172005082400017NM 2005 8 24 2005UALA00824 120050813A33501317 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE DOOR 5L BURNED OUT A UALAK NONE L NO TEST ININSP/MAINT 1 WP29116UA 26908 DOOR 5 LEFT FWD SILL LIGHT INOP. REPLACED LAMP. 2L74 4F4 FRTA20WE E24NE 20050824000222005082400022NM 2005 8 24 2005UALA00829 120050815A3397794640 POWER CABLE BOEING747 747422 1384935NM PWA 4056 PW4056 NE DOOR 2R DAMAGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29199UA 28717 DOOR 2 RIGHT LOWER WALL EEL AISLE JUST AFT OF GALLEY INOP. REPAIRED FEEDER CABLE. 2L74 4F4 FRTA20WE E24NE 20050824000282005082400028NM 2005 8 24 2005UALA00835 120050815A2910 HYDRAULIC SYSTEM BOEING747 747422 1384935NM PWA 4056 PW4056 NE NR 4 MALFUNCTIONED A UALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP29196UA 28715 RETURNED TO SFO UNDER AMBER ALERT DUE TO NR 4 HYDRAULIC SYSTEM PROBLEM . 2L74 4F4 FRTA20WE E24NE 20050824000292005082400029NM 2005 8 24 2005UALA00836 120050817A5310 FRAME BOEING747 747422 1384935NM PWA 4056 PW4056 NE MED DOOR 2 R/H UCRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29127UA 28813 MED DOOR 2 RT UPPER FRAME CRACKED AT HINGE ATTACH FASTENER HOLE, MID POINT. DAMAGE REPAIRED FOR HORIZONTAL BEAM PER SM-80-52-10-05-JD. 2L74 4F4 FRTA20WE E24NE 20050824000302005082400030NM 2005 8 24 2005UALA00837 120050817A5310 FRAME BOEING747 747422 1384935NM PWA 4056 PW4056 NE MED DOOR 2 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29127UA 28813 MED DOOR 2 LT HAS CRACKED UPPER FRAME MID POINT, AT HINGE ATTACH FASTENER HOLE. DAMAGE REPAIRED FOR HORIZONTAL BEAM PER SM-80-52-10-05-JD. 2L74 4F4 FRTA20WE E24NE 20050824000322005082400032NM 2005 8 24 2005UALA00839 120050817A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INTERMITTENT A UALAK NONE L NO TEST ININSP/MAINT 1 WP29182UA 25279 EMER LT INTERMITTENT ON/OFF STAIR-LOC 658. 2L74 4F4 FRTA20WE E24NE 20050824000362005082400036NM 2005 8 24 2005UALA00843 120050818A335020131A BATTERY BOEING757 757222 1384956NM PWA 2037 PW2037 NE STA 1243 DISCHARGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29587UA 26713 SECTION OF COACH EMERGENCY LIGHTS INOP, REPLACED BATTERY. 2L72 4F4 FRTA2NM E17NE 20050824000432005082400043NM 2005 8 24 2005UALA00850 120050818A3350 LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE EXTERIOR INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29318UA 23950 LEFT AND RIGHT EMERGENCY EXIT LIGHTS INOP (EXTERIOR). REPLACED LIGHT ASSEMBLY. 2L72 4F4 FRTA16WE E2GL 20050824000462005082400046SO 2005 8 24 SWIA200515443 120050819A3097 WIRE EMB 120 EMB120ER 3260203SO TERMINAL BLOCK LOOSE A SWIAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 NM07562SW 120336 TURNED ON WINDSHIELD CLIMBING THROUGH FL180. BEGAN TO SMELL ELECTRICAL BURNING. SHORTLY THEREAFTER, SAW SMOKE COMING FROM UNDER FORWARD GLARESHIELD. TIGHTENED LOOSE GROUND WIRE ON TERMINAL BLOCK. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050824000472005082400047SO 2005 8 24 SWIA200515444 120050816A3310 LIGHT EMB 120 EMB120ER 3260203SO COCKPIT SMOKE A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM07221SW 120290 SMOKE COMING FROM FO`S STORM LIGHT. REPLACED FO'S STORM LIGHT ASSY. 2L72 4T RTA31SO 20050824000482005082400048EA 2005 8 24 SWIA200515445 120050818A7931 PRESSURE SWITCH CNDAIRCL600 CL6002B19 1900309EA RT ENGINE INACCURATE A SWIAE ENGINE SHUTDOWN N FALSE WARNING CLCLIMB 1 NM07960SW 7853 RIGHT ENGINE OIL PRESSURE BELOW 25 PSI AND INCREASING AND DECREASING ABNORMALLY. REPLACED RT ENGINE OIL PRESSURE SWITCH. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050824000492005082400049EA 2005 8 24 SWIA200515446 120050817A27604916406 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07407SW5572 5572 7034 SPOILERONS FAULT MSG, DURING TAXI OUT. REPLACED SECU NR 1. OPERATIONAL CHECK GOOD IAW MM 27-61-00-720-801. 2L72 4F RTA21EA 20050824000512005082400051SO 2005 8 24 SWIA200515448 120050815A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT DISCHARGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07586SW1076210762 120354 EMERGENCY LIGHTS IN BACK ARE NOT WORKING. REPLACED NR'S 1, 2, AND 3 ELBP'S IAW 33-50-01, OPERATIONAL CHECK GOOD, PN 1 D366-04-001, SN 1 OFF 507, SN 2 OFF 817 SN 3 OFF 1050. 2L72 4T RTA31SO 20050824000522005082400052SO 2005 8 24 SWIA200515449 120050818A3350 BULB EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07270YV 120270 ONE "EMERGENCY FLOOR LIGHT" INOP 1ST RED LIGHT. REPLACED BULB IN 1ST RED EMERGENCY FLOOR LIGHT. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050824000532005082400053NE 2005 8 24 MALA050652 320050815A6140 SENSOR SAAB SF340 340B 7860101EU ROTOL R354 R3544123F13 NE PROP RPM MALFUNCTIONED A MALAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 GL15445XJ 340B445 CREW RETURNED TO MSP DUE TO A PROPELLER RPM CONTROL/INDICATION FAULT. RPM PROP RPM WENT TO ZERO INFLIGHT. REMOVED AND REPLACED PROP RPM SENSOR AS REQUIRED PN 4088T42P01. REMOVED AND REPLACED PROP GAUGE AS REQ SN OFF 9710657 ON 324. OPS CHECKS GOOD. 2L72 4T RTA52EU 6 CP61GL 20050824000552005082400055EU 2005 8 24 MALA050654 120050815A2910711493 VALVE BAC 146 AVRO146RJ85A1500097EU MLG FAILED A MALAO OTHER J WARNING INDICATION CRCRUISE 1 GL15526XJ E2351 LOSS OF GREEN HYD SYSTEM. RAN CHECK LIST AND PERFORMED EMERGENCY GEAR EXTENSION. REPLACED GREEN SYSTEM HYD SELECTOR VALVE NR 3 ENGINE HYD PUMP AND FLUSHED GREEN SYSTEM HYD SYSTEM AND REPLACED FILTERS. REMOVED AND REPLACED SELECTOR 71149-3 SN ON/OFF F9748464 IAW 24-23-31A-D. LEAK AND OPS CHECK GOOD OF SELECTOR VALVE. INSTALLED NEW ENGINE DRIVEN PUMP PN 521449 SN ON MX618453 IAW 29-10. BLED L AND R OVERCENTER JACKS. FLUSHED HYD LINES FROM HYD BAY TO NR 3 EDP. LEAK CHECKS GOOD. REMOVED AND REPLACED NR 3 ENGINE ISOLATION VALVE PN HTE9531-3, SN OFF 190VB115 ON 190VB147IWA AMM 29-10-14. LEAK AND OPS CHECKS GOOD NR 3 ENGINE HYD PUMP. OP AND LEAK CHECK GOOD. 2H74 4F RTA49EU 20050824000562005082400056EU 2005 8 24 MALA050658 120050816A5510 SKIN SAAB SF340 340B 7860101EU STABILIZER DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15362PX 340B258 DURING 4Y/2Y INSPECTION IN BNA, FOUND RT HORIZONTAL STABILIZER UPPER SURFACE IS DENTED. DAMAGE HAS BEEN REPAIRED IAW MESABA EO#$55056. REF: EAMS WORK ORDER 212631, TASK 3503. 2L72 4T RTA52EU 20050824000572005082400057EU 2005 8 24 MALA050637 120050808A2910 HYDRAULIC SYSTEM SAAB SF340 340B 7860101EU FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15361PX 340B249 CREW RETURNED TO MSP AFTER DEPARTURE, DUE TO HYDRAULIC SYSTEM FAILURE. GEAR WAS SUCCESSFULLY EXTENDED AND CFR CALLED. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO FURTHER INFORMATION AT THIS TIME. 2L72 4T RTA52EU 20050824000602005082400060EU 2005 8 24 MALA050646 120050812A5420 COWL DOOR BAC 146 AVRO146RJ85A1500097EU NR 3 NACELLE CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15522XJ E2347 DURING INSPECTION, FOUND NR 3 AFT INBD COWL DOOR HAS CHAFING ON STIFFENERS AT BOTTOM OF COWL DOOR. 2H74 4F RTA49EU 20050824000642005082400064EU 2005 8 24 MALA050638 120050812A7720 INDICATION SYS SAAB SF340 340B 7860101EU ENGINE TEMP FLUCTUATES A MALAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL15457XJ 340B457 CREW RETURNED TO MSP DUE TO ENGINE TEMPERATURE (ITT) FLUCTUATIONS. NO FURTHER INFORMATION AT THIS TIME. 2L72 4T RTA52EU 20050824000652005082400065EU 2005 8 24 MALA050643 120050812A5420 COWL DOOR BAC 146 AVRO146RJ85A1500097EU NR 1 NACELLE DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15522XJ E2347 DURING INSPECTION FOUND DAMAGE TO STIFFENERS ON NR 1 AFT OTBD COWL DOOR CHAFFING ON STIFFENER AT BOTTOM OF COWL DOOR. 2H74 4F RTA49EU 20050824000662005082400066EU 2005 8 24 MALA050644 120050812A5420 COWL DOOR BAC 146 AVRO146RJ85A1500097EU NR 2 NACELLE CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15522XJ E2347 DURING INSPECTION FOUND NR 2 AFT OTBD COWL DOOR HAS CHAFING ON STIFFENER AT BOTTOM OF COWL DOOR. 2H74 4F RTA49EU 20050824000672005082400067NE 2005 8 24 MALA050665 220050818A7320216362040 MANIFOLD BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071H 41580NE FUEL SYS DAMAGED A MALAO OTHER J WARNING INDICATION DEDESCENT 1 GL15516XJ E2334 ON SHORT FINAL, NR 4 FIRE BELL AND CAUTION ILLUMINATED. SECURED ENGINE VIA ENGINE FIRE EMERGENCY CHECK LIST. NO VISUAL INDICATION OF FIRE NR 1 BOTTLE USED. REPLACED FUEL MANIFOLDS IAW TASK CARD 7310-501, PN 2-163-620-40, SN ON 972495400218 AND PN 2-163-620-39, SN ON 14-517. LEAK CHECKS GOOD. REMOVED AND REPLACED NR 1 FIRE BOTTLE. 2H74 4F4 FRTA49EU E6NE 20050824000712005082400071EU 2005 8 24 MALA050642 120050812A5280 SKIN BAC 146 AVRO146RJ85A1500097EU LT MLG DOOR CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15522XJ E2347 WHILE ACCOMPLISHING C1 INSPECTION, FOUND THE LEFT MAIN LANDING GEAR DOOR LOWER SKIN, FORWARD UPPER CUT-OUT CRACKED ON AFT OUTBOARD CORNER. 2H74 4F RTA49EU 20050824000722005082400072EU 2005 8 24 MALA050647 120050812A5420 COWL DOOR BAC 146 AVRO146RJ85A1500097EU CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15522XJ E2347 DURING INSPECTION, FOUND NR 4 AFT INBD COWL DOOR HAS CHAFING ON STIFFENER AT BOTTOM OF COWL DOOR. 2H74 4F RTA49EU 20050824000812005082400081EU 2005 8 24 MALA050659 120050816A5512 SKIN SAAB SF340 340B 7860101EU HORIZONTAL STAB DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15362PX 340B258 DURING 4Y/2Y INSPECTION, FOUND RT HORIZONTAL STABILIZER UPPER SURFACE IS DENTED. DAMAGE HAS BEEN REPAIRED IAW MESABA EO#$55056. REF: EAMS WORK ORDER 212631 TASK 3504. 2L72 4T RTA52EU 20050824000842005082400084NM 2005 8 24 SWAA052524 120050821A55236959227 BUSHING BOEING737 7373H4 1384600NM LT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29398SW 27692 DURING SCHEDULED C4 CHECK, LT ELEVATOR TAB FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR NR 1 HINGE BUSHING & ROD END HARDWARE PER MM. 2L72 4F RTA16WE 20050824000852005082400085NM 2005 8 24 SWAA052525 120050821A3350207377 LENS BOEING737 7377H4 1384404NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29424WN 29828 EEPLS TRACK LENS MISSING AT ROW 2 ABC. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20050824000902005082400090NM 2005 8 24 SWAA052530 120050822A5315BAC1503 FLOORBEAM BOEING737 7373H4 1384600NM CABIN CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29617SW 27700 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FLOORBEAM TEE CORRODED AT BS 270, LBL 11 TO RBL 11. REMOVED AND REPLACED FLOORBEAM T-CHORD PER SRM. 2L72 4F RTA16WE 20050824000932005082400093SW 2005 8 24 PNSA050803 120050819A3397 TERMINAL SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TFE33112UHR WP HAND PUMP LIGHT SHORTED A PNSAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 AL0341NE AC713B PILOT REPORTED SMOKE COMING FROM UNDER LT PILOT SEAT. A/C RETURNED TO BLOCK AND MX FOUND POST LIGHT FOR HYDRAULIC HAND PUMP BROKEN OFF AND SHORTED. SECURED WIRING AND DEFERRED IAW MEL 33-1. 2L72 4T4 TRTA8SW E4WE 20050824000942005082400094EU 2005 8 24 DHL2005366502 120050725A5754 SLAT TRACK AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE CRACKED CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01366DH 249 DURING C-CHECK, DISCREPANCY AS FOLLOWS N/R 021215 DISCREPANCY AS FOLLOWS, RT WING NR 1 SLAT LOWER, IB OF NR 1 TRACK AT EDGE HAS A CRACK. REMOVED SKIN TO REPLACE CRACK ANGLE IAW SRM. MATERIAL USED 2024-0, .063 INCH THICK PO NR 1004297 HEAT TREATED TO 2024-T4 IAW SRM 51-40-30. RE-INSTALLED SKIN PREVIOUSLY REMOVED TO INSTALL ANGLE AS SRM 51-30-30. 2L72 4F4 FRTA35EU E23EA 20050824001022005082400102 2005 8 24 ASMF200508010 420050818A23406861000001 HANDSET DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE CABIN FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23753RA2524 2524 49587 AIRCRAFT RETURNED TO PLATFORM AFTER THE LT ENGINE STARTED, THE FLIGHT ATTENDANT CALLING CAME ON CONSTANTLY. THE BREAKER P37 CALL SYS WAS RESEATED BUT THE FAILURE CONTINUED. THE FRONT HANDSET WAS VERIFIED, ALL CORRECT. THE BACK HANDSET WAS VERIFIED, DETECTING ATT, PILOT AND P/A LIGHTS TURNED ON. THE HANDSET WAS REPLACED IAW MM 23-40-00, ALL CORRECT. 2L72 4F4 FRTA6WE E9NE 20050824001082005082400108NM 2005 8 24 ASMF200508012 120050821A3260833605 PROXIMITY SWITCH DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE RT MLG FAILED W ASMFK NONE N FALSE WARNING ININSP/MAINT 1 SW23169PL1282712827 53175 CAPTAIN REPORTED THAT RT RED MAIN LANDING GEAR LIGHT TURNED ON. THE PROXIMITY SWITCH UNIT WAS TESTED, LIGHT PANEL WAS CHECKED AND SENSORS WERE VERIFIED BUT FAILURE CONTINUED. THE PROXIMITY SWITCH UNIT WAS REPLACED AND FAILURE CODE 310 WAS SHOWN AND RED LIGHTS TURNED ON. THE PROXIMITY SWITCH CARD WAS REPLACED IAW MM 32-60-00, TESTED CORRECT. 2L72 4F4 FRTA6WE E9NE 20050824001142005082400114NM 2005 8 24 CALA0500279 120050821A2810BMS1011 SEAL BOEING757 757224 1384958NM RT CENTER TANK LEAKING A CALAA UNSCHED LANDING KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2714118 27560 A STRONG FUEL ODOR WAS SMELLED IN THE AIRCRAFT CABIN WHILE EN ROUTE FROM BHM TO EWR. THE AIRCRAFT WAS DIVERTED TO SNN WHERE IT LANDED WITHOUT INCIDENT. RT SEAT ROWS 16 AND 17 WERE REMOVED AND THE FLOOR PANELS WERE OPENED. MAINTENANCE NOTED A FUEL LEAK AT THE RT WING TO CENTER SPLICE APPROXIMATELY SIX INCHES FORWARD FROM CENTER TANK AFT BULKHEAD. THE LEAKING AREA WAS RESEALED IAW MM 28-11-00, PAGE 846 AND IAW ECRA 2811-01003. A LEAK CHECK OF THE RT CENTER TANK SEALANT WAS PERFORMED IAW 28-11-00 AND CHECKED GOOD. THE FLOOR PANELS AND SEAT ROWS WERE REINSTALLED IAW STANDARD PRACTICES MANUAL CHAPTER 20 AND MM 25-25-01. 2L72 4F RTA2NM 20050824001212005082400121WP 2005 8 24 ABXA050192 120050804A533059128703 SKIN DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23965AX 47498 FS 1114 RIGHT SKIN CRACKED 8 1/2 INCHES UP FROM ENGINE PYLON. REPAIRED AREA FS 1114 RIGHT IAW DC-9 SRM. 2L72 4F A6WE 20050824001242005082400124WP 2005 8 24 ABXA050199 120050808A5712991707216 RIB DOUG DC9 DC941 302207NWP RIGHT WING CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23965AX 47498 CRACKED RIB AT RIGHT WING TRAILING EDGE, STA XRS 133. REMOVED, REPAIRED AND REINSTALLED RIB AT RIGHT WING STA XRS 133 IAW DC-9 SSRM K05159 AND DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 20050824001272005082400127WP 2005 8 24 MWEA050088 120050823A532099365357 FLOOR SUPPORT DOUG DC9 DC982 3022082WP STA 218 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 UPON REMOVAL OF FLOOR SUPPORT FOUND CORROSION ON WEB BELOW THE SUPPORT, STATION 218 RT SIDE. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20050824001282005082400128WP 2005 8 24 MWEA050090 120050823A534449135932N SUPPORT ANGLE DOUG DC9 DC982 3022082WP NLG DOOR HINGE DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 NOSE LANDING GEAR AFT LEFT DOOR HINGE POINT SUPPORT BOLT HOLES ENLONGATED. FABRICATED AND INSTALLED FRONT SUPPORT ANGLE. 2L72 4F A6WE 20050824001292005082400129WP 2005 8 24 MWEA050091 120050823A532099155705 PANEL DOUG DC9 DC982 3022082WP STAIRWAY CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 VENTRAL STAIRWAY LEFT SIDE JUST FORWARD OF NR 1 ALIGNMENT PIN HAS CORROSION. FABRICATED AND INSTALLED NEW PANEL. 2L72 4F A6WE 20050824001302005082400130WP 2005 8 24 MWEA050092 120050823A532099155707 PANEL DOUG DC9 DC982 3022082WP STAIRWAY CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 VENTRAL STAIR LEFT SIDE JUST FORWARD OF NR 3 ALIGNMENT PIN HAS CORROSION. FABRICATED AND INSTALLED NEW PANEL. 2L72 4F A6WE 20050824001342005082400134WP 2005 8 24 ABXA050190 120050809A5340591472998 ATTACH ANGLE DOUG DC9 DC932 3022066WP BULKHEAD CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 FORWARD LOWER CARGO AFT BULKHEAD LOWER ATTACH ANGLES CRACKED AT LONGERON 24 RIGHT. REPLACED ATTACH ANGLES IAW DC-9 SRM. 2L72 4F A6WE 20050824001392005082400139NM 2005 8 24 AALA20050547 120050821A2910 LINE BOEING757 757223 1384957NM HYD SYSTEM RUPTURED A AALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SW21652AA 24610 BOS INFLIGHT T1752/21AUG - ON FINAL APPROACH, AIRCRAFT UNABLE TO EXTEND RIGHT MAIN GEAR. EXENDED GEAR THROUGH EMERGENCY PROCEDURE AND LANDED WITHOUT INCIDENT. FOUND FLEX LINE AT RIGHT GEAR DOWNLOCK ACTUATOR RUPTURED. REPLACED BOTH FLEX LINES. AIRCRAFT MAINTENANCE FERRIED TO JFK FOR GEAR RETRACTION CHECK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050824001402005082400140NM 2005 8 24 AALA20050540 120050812A5320 SILL BOEING767 767323 1385205NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21355AA 24036 AFW - LOWER MAIN SILL OUTER CHORD HAS CORROSION REMOVAL ON VERTICAL LEG INBOARD SURFACE IN AN AREA OF 1.7 INCH BY 2.8 INCH WITH A DEPTH OF .035 AT STATION 527. REMOVED AND VERIFIED CORROSION HAD BEEN REMOVED. PERFORMED A HIGH FREQUENCY EDDY CURRENT INSPECTION. INSTALLED FASTENERS WET. ALODINED AND APPLIED TWO COATS OF PRIMER. 2L72 4F RTA1NM 20050824001412005082400141 2005 8 24 AALA20050548 420050822A256531564101 STRAP BOEING757 757223 1384957NM CABIN MISSING A AALAK NONE O OTHER ININSP/MAINT 1 SW21697AN 26977 MEX - ON PREFLIGHT INSPECTION, CREW REPORTED SURVIVAL EQUIPMENT D RING STRAP MISSING FROM 2 RIGHT DOOR EMERGENCY SLIDE. REPLACED STRAP AT 2 RIGHT DOOR EMERGENCY SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050824001482005082400148NM 2005 8 24 DL73S050453 120050814A3350 COVER BOEING737 737232 1384475NM SEAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27327DL 23099 PASSENGER SEAT 10D EMERGENCY TRACK LIGHTING FLOOR LIGHT DAMAGED, REPAIRED SAME. 2L72 4F RTA16WE 20050824001502005082400150NM 2005 8 24 DL764050455 120050816A2720 LOCK BOEING767 767432ER 1385134NM RUDDER PEDAL LOOSE A DALAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO27839MH 29712 DURING TAKEOFF NOTICED CAPTAINS RUDDER PEDALS SHIFT FORWARD ABOUT AN INCH, NORMAL T/O. INSPECTED PEDAL MECHANISIM AND TIGHTEND LOCK. PDEAL NOW LOCKS INTO DESIRED POSITION. 2L72 4F RTA1NM 20050824001522005082400152NM 2005 8 24 DL76L050457 120050816A3610361002241 VALVE BOEING767 767332 1382001NM LT ENGINE FAILED A DALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO27171DN 24759 L HPSOV EICAS MSG AT 80 PERCENT N1 ON T/O ROLL. REPLACED VALVE. 2L72 4F RTA1NM 20050824001562005082400156NM 2005 8 24 DL777050461 120050817A3350 FUSE BOEING777 777232 1385232NM CABIN UNSERVICEABLE A DALAO OTHER L NO TEST ININSP/MAINT 1 SO27860DA 29951 SEATS 30 DEF TO 41 DEF EMERGENCY LIGHTS INOP. REPLACED FUSE IN POWER SUPPLY. 2L72 4F RTT00001SE 20050824001582005082400158GL 2005 8 24 DL764050430 220050806A7200CF680C2B8F ENGINE BOEING767 767432ER 1385134NM GE CF6 CF680C2* GL NR 1 FAILED A DALAK NONE O OTHER ININSP/MAINT 1 SO27832MH1330313303 29704 704929 ENGINE FAILED BOROSCOPE 11TH STAGE RAIL LIFTED. OPERATION 5039, REPLACED ENGINE. 2L72 4F4 FRTA1NM E23EA 20050824001622005082400162NM 2005 8 24 DLM88050435 120050808A2130 DUCT DOUG MD88 MD88 3023688NM CRACKED A DALAD RETURN TO BLOCK J WARNING INDICATION CLCLIMB 1 SO27920DE 53423 TAIL COMPARTMENT TEMP HI MSG PASSING THROUGH FL 250 AT CLIMB POWER. REPLACED CRACKED SPYDER DUCT. 2L72 4F RTA6WE 20050824001642005082400164NE 2005 8 24 DL76G050438 220050808A72611978M64G01 LINE BOEING767 767332 1382001NM GE CF6 CF680C2B6F 30025NE NR 1 ENGINE BROKEN A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO271608 30573 706113 AT CRUISE ALT FL320, 3 HOURS INTO FLT, LEFT ENGINE OIL QUANTITY WENT TO ZERO. OIL PRESSURE WAS 45 PSI AND GRADUALLY DECREASED TO 11 PSI TRANSIENT 10 PSI EXPERIENCED ON FINAL APPROACH LEFT THRUST LEVER REDUCED TO IDLE. NO REVERSE. ALL OTHER ENG PARAMETERS NORMAL. OIL PUMP DISCHARGE MANIFOLD PIPE BROKEN. PIPE REPLACED. ENGINE RUN-UP 5 MIN. ALL PARAMETERS NML. NO LEAK DEBRIS. INFO ENG OIL SERVICED 48 PINTS WITH EXXON 2380 ENG OIL, MPN 1978M64G01. 2L72 4F4 FRTA1NM E13NE 20050824001712005082400171SO 2005 8 24 CHQA200500145 120050819A2120 SMOKE EMB 145 EMB145LR 3260212SO LAVATORY DETECTED A CHQAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL11258JQ 145768 AFTER AN HOUR ON THE GROUND, LAV SMOKE IND DURING INITIAL CLIMB AT ABOUT 600 FT. F/A REPORTED SMOKE IN REAR OF CABIN. NO EMERGENCY DECLARED; REQUESTED TO RETURN TO THE FIELD. PRIOR TO PUTTING ON O2 MASKS, SMELLED A PUNGENT SMELL. CLEARED TO LAND AND ATC WANTED TO KNOW THE REASON. REPORTED LAVATORY SMOKE INDICATION WITH SMOKE IN THE REAR OF THE CABIN. ATC CALLED THE TRUCKS. LAV SMOKE INDICATION AND THE SMOKE STOPPED IN ABOUT 1 TO 2 MIN. NO ASSISTANCE REQUIRED ON THE GROUND AND RETURNED TO GATE. PRIOR TO TAKEOFF NUMBER ONE ENGINE WAS BEING RUN DURING THE DELAY WITH BOTH PACKS ON AND APU OFF. DURING THE WAIT ON THE GROUND, PILOT REMEMBERED SMELLING AN ODD SMELL IN THE PACK SYSTEM THAT LASTED ONLY 5 SECON2L72 4T RTT00011AT 20050824001722005082400172 2005 8 24 AT0500028 420050816A2330LSEBUTKB00101 DISPLAY BOEING717 717200 1383700NM SEAT 11AC SHORTED A ZZDAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO15955AT 55017 PAX & F/A REPORTED SMOKE /ELECT ARCHING ASSOCIATED WITH X/M SATELLITE SYSTEM AT SEATS 11/A/C. PULLED SYSTEM BREAKERS SMOKE/ ARCHING CEASED. UNEVENTFUL DIVERT TO RIC. REMOVED AND REPLACED DASDU UNDER SEAT 11 AC. 2L72 4F TRA6WE 20050824001732005082400173 2005 8 24 SWAA052531 420050822A25656557463 FITTING BOEING737 7373H4 1384600NM CABIN FLOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29617SW 27700 DURING SCHEDULED D-CHECK, FOUND CORROSION ON L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR FITTINGS. REMOVED AND REPLACED GIRT BAR FLOOR FITTINGS PER SRM. 2L72 4F RTA16WE 20050824001762005082400176NM 2005 8 24 SWAA052534 120050822A3350101114 COVER BOEING737 7373A4 1384585NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29677AA 23289 LEFT OVERWING EMERGENCY EXIT COVER MISSING. INSTALLED COVER PER MM. 2L72 4F RTA16WE 20050824001802005082400180CE 2005 8 24 DXTA200500899 120050810A3241 WARNING LIGHT CESSNA560 560XL 2076702CE ANTI SKID SYS ILLUMINATED E DXTAO OTHER J WARNING INDICATION LDLANDING 1 GL07609QS 5605522 ON LANDING THE ANTISKID LIGHT ILLUMINATED AND ON TAXI IN THE LOW BRAKE PRESSURE LIGHT ILLUMINATED AND THE PNEUMATIC BRAKES HAD TO BE USED TO STOP THE PLANE. C/W BRAKE SYSTEM BLEED, BIT TEST & AN ANTISKID FUNCTIONAL TEST. NO FAULTS FOUND AT THIS TIME, WORK DONE IAW CE-560XL MM CH 32-42-00 & 32-44-00. 2L72 4F RTA22CE 20050824001812005082400181CE 2005 8 24 DXTA200500900 120050815A783065900171 POSITION SWITCH CESSNA500 560CESSNA 2076750CE THRUST REVERSER INOPERATIVE E DXTAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 GL07351QS 5600451 INFLIGHT NR 2 THRUST REVERSER DEPLOY LT ILLUMINATED. THE T/R ARM & UNLOCK LIGHTS WERE EXTINGUISHED. NR 2 ENG SHUTDOWN IAW CE560 CHECKLIST W/ THROTTLE OFF. TROUBLESHOT RT T/R PROBLEM TO INTERMITTENT DEPLOY SWITCH. REMOVED AND REPLACED DEPLOY SWITCH WITH NEW, P/N 6590017-1. OPERATED RT T/R WITH HYDRAULIC TEST STAND, OPS CHECKS GOOD. OPERATED ENGINES AND OPS CHECK T/R'S OPS CHECK GOOD. WORK PERFORMED PER CE560 M/M, 78-31-02. 2L72 4F RTA22CE 20050824001832005082400183CE 2005 8 24 DXTA200500901 120050815A323025UM981 LINK RAYTHNDH125 HAWKER800XP 7150012CE MLG WORN E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07873QS 258573 ON DEPARTURE LEFT MAIN GEAR WOULD NOT RETRACT WITH ASSOCIATED RED GEAR UNSAFE LIGHT ILLUMINATED ON PANEL. REMOVED AND REPLACED LT SEQUENCE VALVE LINK AND TWO BUSHINGS IAW HAWKER 800XP 32-30-00. OP'S CHECK GOOD. 2L72 4F RTA3EU 20050824001842005082400184NM 2005 8 24 DXTA200500902 120050816A5310 STRUCTURE GULSTM200 200 4500308NM BIRD STRIKE E DXTAC ABORTED TAKEOFF C F.O.D. TOTAKEOFF 1 GL07722QS 093 BIRD STRIKE DURING T/O ROLL OUT OF KSAV. ABORTED AT ABOUT 100 KTS. ACCOMPLISHED BIRD STRIKE INSPECTION IN ACCORDANCE WITH G200 MAINTENANCE MANUAL CHAPTER 05-55-00, NO DISCREPANCIES NOTED. 2L72 4F RTA53NM 20050824001852005082400185CE 2005 8 24 DXTA200500903 120050816A3297EJN3 WIRE CESSNA650 650 2076802CE MLG BROKEN E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07779QS 6507079 GEAR WILL NOT RETRACT. FOUND OPEN WIRE BETWEEN EJN3 AND JPN1 IN NOSE GEAR WELL. INSPECTED WIRE HARNESS, DISCOVERED BROKEN WIRE. REPAIRED BROKEN WIRE IAW THE 650 MAINTENANCE MANUAL 20-10-01. DOWNLOCK SOLENOID OPS CHECK SATISFACTORY. RETRACTION/EXTENSION CHECK SATISFACTORY. 2L72 4F A9NM 20050824001902005082400190NM 2005 8 24 SWAA052497 120050819A53306545775 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 835, STR 20L. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050824001922005082400192NM 2005 8 24 SWAA052499 120050820A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING WALKAROUND INSP, FOUND FUSELAGE SKIN CRACKED AT BS 986, STR 21L. MX FERRY TO PHX FOR REPAIRS. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050824001972005082400197NM 2005 8 24 SWAA052504 120050820A335007912 COVER BOEING737 7377H4 1384404NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29459WN 32497 FWD END OF EEPLS TRACK COVER CRACKED. REMOVED AND REPLACED COVER PER MM. 2L72 4F RTA16WE 20050824001982005082400198NM 2005 8 24 SWAA052505 120050819A53116516301 FRAME BOEING737 7375H4 138449DNM COCKPIT FLOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29503SW 24180 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STUB FRAME CRACKED AT BS 188, RT SIDE, WL 208. REPAIRED STUB FRAME PER SRM. 2L72 4F RTA16WE 20050824001992005082400199NM 2005 8 24 SWAA052506 120050819A53216546833 FLOOR PANEL BOEING737 7375H4 138449DNM COCKPIT FLOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29503SW 24180 DURING SCHEDULED SPECIAL VISIT, FOUND COCKPIT FLOOR WEB CRACKED BETWEEN BS 188 TO BS 196, RBL 29, WL 208. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050824002002005082400200NM 2005 8 24 SWAA052507 120050820A53306545775 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29507SW 24184 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 784, STR 19L. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050825000012005082500001NM 2005 8 25 SWAA052536 120050823A275065505396 SHAFT BOEING737 7373Q8 1384670NM RT WING TE FLAP CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29317WN 24068 DURING SCHEDULED D-CHECK, FOUND RT WING INBOARD T/E MIDFLAP OUTBOARD GIMBLE SHAFT CORRODED. REMOVED AND REPLACED GIMBLE SHAFT PER MM. 2L72 4F RTA16WE 20050825000052005082500005NM 2005 8 25 SWAA052510 120050818A3350D71702001 BATTERY PACK BOEING737 7373H4 1384600NM FWD GALLEY INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED SERVICE CHECK, FOUND LT FWD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050825000062005082500006NM 2005 8 25 SWAA052511 120050818A5753 SKIN BOEING737 7373H4 1384600NM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29644SW 2322 28329 DURING SCHEDULED C4 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT LOWER INBOARD END. REMOVED AND REPLACED FLAP PER MM. 2L72 4F RTA16WE 20050825000102005082500010CE 2005 8 25 DXTA200500908 120050819A32301283640685 PCB BEECH MU300 400A 1155402CE MLG DEFECTIVE E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07116QS RK385 AFTER T/O RED LIGHT IN HANDLE ILLUMINATED. CYCLED GEAR, GOT 3 GR AND 1 RD. RAN ALT GEAR EXT PROCEDURE. JACKED THE AIRCRAFT, SWUNG THE GEAR FOUND THAT THE MAIN GEAR DOORS WILL OPEN BUT WILL NOT CLOSE. TROUBLESHOT SYSTEM AND FOUND RELAY KIT IN PCB 162 BAD. REPLACED CIRCUIT BOARD P/N 128-364068-5 WITH A NEW BOARD FROM RAYTHEON IAW RAYTHEON STANDARD PRACTICES. CYCLES GEAR SEVERAL TIMES AND OBSERVED NORMAL CYCLES AND INDICATION IAW RAYTHEON 400/400A MM 32-30-00. SERVICED BLOW DOWN BOTTLE PER RAYTHEON 400/400A NN 12-00. OPS CHECKED GOOD. 2H72 4F RTA16SW 20050825000122005082500012 2005 8 25 DXTA200500911 420050821A2210 WARNING LIGHT BEECH MU300 400A 1155402CE PITCH TRIM ILLUMINATED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07140QS RK406 AFTER TAKEOFF RED AP PITCH TRIM FAIL LIGHT CAME ON AND AP KICKED OFF. AIRCRAFT CHECKLIST COMPLETED AND LANDED AS SOON AS PRACTICAL. ITEM IS UNDER INVESTIGATION. 2H72 4F RTA16SW 20050825000152005082500015NM 2005 8 25 SWAA052514 120050820A33506104789 BATTERY PACK BOEING737 7373G7 1384595NM AFT CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29683SW 24008 DURING SCHEDULED SERVICE CHECK, FOUND L2 & R2 DOORS EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050825000182005082500018NM 2005 8 25 SWAA052517 120050821A3350MS155721 BULB BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29753SW 29848 DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT AISLE LIGHT INOP AT ROW 18 DEF. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20060221002862006022100286WP 2006 2 21 DHL2005803506 120051118A5720 ANGLE DOUG DC8 DC873 302199CWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 ITEM REF NR 033540: RT WING CTR L/E INTERCOSTAL JOINT ANGLE TO FORMER CRACKED XS 454.976. REMOVED CRACKED ANGLE IAW SRM 51-3-0. FABRICATED NEW ANGLE (AL7075T6 0.063") IAW SRM 57-2-0 PG. 1. CLEANED, TREATED AND PRIMED AREA AND ANGLE IAW SRM 51-1-8B. INSTALLED NEW ANGLE WITH BOLTS IAW SRM 51-3-0. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20060221002882006022100288WP 2006 2 21 DHL2005803508 120051117A53205615530173 STIFFENER DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 ITEM REF NR 033272: FWD ACCY COMPT RT FWD PRESSURE BULKHEAD STIFFENER CRACKED 1.500 INCHES STA 8.000. REMOVED CRACKED STIFFENER IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED NEW STIFFENER (ALCLAD 7075"0" 0.071") IAW SRM 53-3-3 PG. 11. HEAT TREATED FROM 70750" TO 7075 T6 IAW SRM 51-1-1 PG. 1,13,17. CLEANED, TREATED AND PRIMED AREA AND NEW STIFFENER IAW SRM 51-1-8B. INSTALLED NEW STIFFENER IAW SRM 51-1-21, SRM 51-1-20D. TORQUED IAW SRM 51-3-1. FOR STIFFENER FABRICATION REFER TO JC EA53100133-001-D (ATTACHED). 2L74 4F RT4A25 20060221002912006022100291WP 2006 2 21 DHL2005803511 120051117A5320561553025 STIFFENER DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 ITEM REF NR 033271: FWD ACCY COMPT LT FWD PRESSURE BULKHEAD STIFFENER CRACKED 1 INCH STA 8.000. REMOVED CRACKED STIFFENER IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED NEW STIFFENER (ALCLAD 7075"0" 0.071") IAW SRM 53-3-3 PG. 11. HEAT TREATED FROM 7075"0" TO 7075T6 IAW SRM 51-1-1 PG. 1,13,17. CLEANED, TREATED AND PRIMED AREA AND NEW STIFFENER IAW SRM 51-1-8B. INSTALLED NEW STIFFENER IAW SRM 51-1-21, SRM 51-1-20D. TORQUED IAW SRM 51-3-1 PG. 2A. FOR STIFFENER FABRICATION REFER TO JC EA53100132-001-D (ATTACHED) 2L74 4F RT4A25 20060221002922006022100292WP 2006 2 21 DHL2005803539 120051203A5315 FLOORBEAM DOUG DC8 DC873 302199CWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01803DH82180 46123 ITEM REF NR 038741: WING CTR SECTION FLOORBEAM HOLE MISDRILLED STA 980.000 RBL 93750 (MAIN CARGO COMPT.) (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 11/28/05, DWG AA33-53-R07 REV IR DATE 11/11/05. REMOVED FASTENERS IAW SRM 51-1-21. TRIMMED OUT DAMAGED AREA, FABRICATED REPAIR ANGLE (EXTRUSION 7075T6 511 0.140"), FILLER (7075T6511 0.125") IAW DWG AA33-53-R07. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG. 9. INSTALLED REPAIR PARTS IAW DWG AA33-53-R07, SRM 51-1-20D, SRM 51-3-1 2L74 4F RT4A25 20060221003582006022100358EA 2006 2 21 SWIA200516252 120050912A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07408SW 7055 CRACK ON FRAME FLANGE AT FS 640 RT STR 9R, ITEM FOUND AT C CHECK INSPECTION. REPAIRED CRACKED FRAME IAW CRJ REO 601R-53-61-1543 AND RII 53-401. 2L72 4F RTA21EA 20060222000752006022200075EU 2006 2 22 05FDEA04096 120051203A5101 REPAIR AIRBUS310 A310 EU FUSELAGE UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25424FE 241 PREVIOUS REPAIR INSTALLED AT FUSELAGE LT SIDE, L2 REAR DOOR FRAME AT STA 4669, FR75A, STR 20LH TO STR 24LH. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. 2L72 4F RTA35EU 20060222000762006022200076EU 2006 2 22 05FDEA04098 120051203A5101 REPAIR AIRBUS310 A310 EU FUSELAGE UNKNOWN A FDEAO OTHER O OTHER ININSP/MAINT 1 SO25424FE 241 PREVIOUS REPAIR INSTALLED AT FUSELAGE RT SIDE OF TAIL CONE AT STA 5094 TO STA 5122, FR101 TO FR102, STR 07RH TO STR 08RH. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. CORRECTIVE ACTION:**S/D COMING** 2L72 4F RTA35EU 20060222000812006022200081NM 2006 2 22 05FDEA04183 120051208A5315 FLOORBEAM BOEING727 727* NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 AFT PIT MAIN DECK FLOORBEAM HAS CORROSION STA BS 1130 LBL67.0 REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW B727 SRM 51-10-6 AND 53-10-1. FABRICATED REPAIR PARTS IAW B727 SRM 53-10-8 FIGURE 10. ALODINED AND PRIMED REPAIR PARTS IAW B727 SRM 51-10-2.INSTALLED REPAIR PARTS IAW B727 SRM 53-10-8 FIGURE 10 AND 51-30-2.REMOVED SEAT TRACK,1 EACH INTERCOASTAL AND 4 EACH GUSSET AND REINSTALLED AFTER REPAIR WAS COMPLETE IAW B727 SRM 51-30-2. THIS IS A MAJOR REPAIR SIGNED BY MECH #110188 AND QC303 REFERENCE SNRM N00490. 2L73 4F RTA3WE 20060222000832006022200083CE 2006 2 22 BSYA200500026 120051106A3697 WIRE LEAR 35 35A 5170602CE GARRTTTFE731TFE731* 01518WP VALVE CHAFED E BSYAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL0727TT 0122 ON TAKE OFF OUT OF DAL LEFT MOD VALVE STUCK IN EMERGENCY AND POPPED CIRCUIT BREAKER. MAINTENANCE FOUND A CHAFED WIRE ON CONNECTOR ON MOD VALVE, REPAIRED WIRE OPS CHECKS GOOD. 2L72 4F4 F A10CE E6WE 20060222000842006022200084CE 2006 2 22 BSYA200500027 120051206A3260 SQUAT SWITCH BEECH 58 58 1152740CE CONT O520 IO520* 17032SO LT MAIN GEAR FROZEN E BSYAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL072064V TH1004 ON TAKEOFF, PILOT SELECTED GEAR UP AND NOTHING HAPPENED, THEN RETURNED TO DEPARTURE, NO PROBLEMS. MAINTENANCE FOUND LT MAIN GEAR SQUAT SWITCH PACKED WITH SNOW, THAWED OUT SWITCH OPS CHECKS GOOD. 1L72 3O3 O 3A16 E5CE 20060222001042006022200104NM 2006 2 22 05FDEA04339 120051215A5700 REPAIR BOEING727 727200 138407ENM N/A UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25274FE 22039 FOUND PREVIOUS REPAIR ON LEFT WING NR 1 KRUEGER FLAP FWD SURFACE WAS ACCOMPLISHED IAW SRM 57-50-3, FIG 2 BASED ON AN EXTERNAL EVALUATION CONSISTED OF LOCATION, SHAPE, SIZE, FASTENERS SPACING AND NUMBERS, MATERIAL THICKNESS AND GENERAL WORKMANSHIP, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2L73 4F RTA3WE 20060223000072006022300007EA 2006 2 23 SWIA200516277 120051108A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07927SW 7693 MAIN FUSELAGE; FS 280, LBL 9.0, UPPER FLANGE CRACKED ON TRANSVERSE BEAM, ITEM FOUND AT C CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-11-138 REV NC. 2L72 4F RTA21EA 20060223000092006022300009SO 2006 2 23 LR7A05208 120051212A531234258314 CAP LKHEED382 382G 526414USO BULKHEAD CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 650 4763 DURING 'B-3' CHECK PER HB5302, FOUND LOWER FLANGE OF BULKHEAD CAP CRACKED 3 INCHES AT FS902, WL195, RBL64. REPAIRED CAP IAW SMP583 FIG. 53-50-17. N/R NO. 0078. 2H74 4T A1SO 20060223000142006022300014WP 2006 2 23 05FDEA04312 120051214A5754 ANGLE DOUG DC10 DC1030 3023501WP NR 4 SLAT CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 LT WING SLAT NR 4 FOUND 1 CRACK 1" LONG ON ANGLE AT STA XORS 506. REPLACED CLIP IAW MD-10-30 M/M 27-80-01-7 FIG 401 SHT 1 AND PERFORMED ADJUSTMENT IAW MD-10-30 M/M 27-80-01-7 FIG 408 SHT 1. 2L73 4F A22WE 20060223000212006022300021WP 2006 2 23 05FDEA04354 120051216A5101 REPAIR DOUG DC10 DC1030 3023501WP FUSELAGE UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 FOUND DOUBLER LENGTH 9" WIDTH 8" ON RT EXT FUSELAGE AT STA 879 LONG 36. REMOVED AND REPLACED REPAIR IAW 1-109812697-7 AND SRM 53-20-00 FIG 6 SHT 5- 6 VOL 1 AND FEDEX EA# 8-5310-93218. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F160401-2 INNER EXTERNAL DOUBLER AND F160401-4 OUTER EXTERNAL DOUBLER IAW SRM 52-20-00 FIG 6 SHT 5-6 VOL 1. 2L73 4F A22WE 20060223000242006022300024WP 2006 2 23 05FDEA04357 120051216A5753 SKIN DOUG DC10 DC1010 3022110WP ZONE 500 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25359FE 46635 LEFT WING INBOARD FLAP LOWER SKIN DENT FILLED WITH SEALANT AT XW234-238, 31" FWD OF TRAILING EDGE. FOUND DENT TO BE OUT OF LIMITS, REPAIRED SKIN IAW DC10 SRM 57-00-00 VOL I. SEE FEDEX NONROUTINE NR N00295 OF WORK ORDER 00031297. 2L73 4F A22WE 20060223000282006022300028WP 2006 2 23 05FDEA04304 120051214A5101 REPAIR DOUG DC10 DC1010 3022110WP FUSELAGE NONE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25563FE 46948 UPPER LIP AIR CONDITIONING DOOR RT SIDE PACK NR 3 HAS AN EXTERNAL DOUBLER REPAIR DIM 31 INCHES BY 2 INCHES. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 52-10-00 FIG 2 VOL 1 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2. 2L73 4F A22WE 20060223000322006022300032WP 2006 2 23 05FDEA04308 120051214A5101 REPAIR DOUG DC10 DC1030 3023501WP GE CF6 CF650C2 30018NE FUSELAGE NONE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 LT WING L/E EXT SKIN FOUND FLUSH DOUBLER DIM 2.75 INCHES BY 2.75 INCHES AT STA XORS 521. PERFORMED A GVI OF REPAIR IAW SRM 57-10-00 FIG 39 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001-2P E3. 2L73 4F4 F A22WE E23EA 20060223000432006022300043NM 2006 2 23 NOCA2905 120051206A3350ML3071 BULB BOEING757 75728A 1384976NM RROYCERB211 RB211535E4 54555NE EMERGENCY LIGHTSINOPERATIVE G NOCAK NONE L NO TEST ININSP/MAINT 1 EA15752NA 28174 E PATH AT DOOR 4 ONE RED LIGHT AT END INOP. 2L72 4F4 FRTA2NM E12EU 20060223000502006022300050NM 2006 2 23 05FDEA04361 120051216A5270 INDICATION SYS BOEING727 727233 138408ANM DOORS OUT OF RIG A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25257FE 20939 LIGHT ILLUMINATED, PASSING 16K MSL (MCD A LIGHT WAS OUT AND TESTED GOOD). DESCENDED TO 10K MSL. LIGHT EXTINGUISHED AT 12K MSL, BULB TESTED GOOD. RELEASED FOR SERVICE PER MEL/CDL: 52-15-01 CATEGORY: C EXP: 26DEC05 "MEL 52-15-01: MCD WARN LIGHT SYS B INOP. VERIFY DOOR CLOSED AND LOCKED PRIOR TO EACH BLOCK OUT." FOUND MCD 'B' LIGHT RIGGED OUT OF SEQ WITH 'A' (PREMATURE TO INDICATE), ADJ CONTACT, IND NORMAL AND IN SEQ WITH SW 'A'. 2L73 4F RTA3WE 20060223001132006022300113NM 2006 2 23 05FDEA04348 120051215A5311 FRAME BOEING727 727227 1384078NM PWA JT8 JT8D9A 52048NE BS660, STR6 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 RT FUSELAGE INTERNAL FRAME REPAIR DOUBLER 12 INCHES BY 2.5 INCHES, LOCATED AT BS 660, STRINGER 6 REQUIRES EVALUATION TO DETERMINE IF THE REPAIR IS MAJOR OR MINOR AND IF REPAIR IS IAW APPROVED DATA. REPAIRED FRAME DOUBLER BS 660 STR 6 SRM 53-10-4. 2L73 4F4 F A3WE E2EA 20060223001162006022300116 2006 2 23 HEEA107317 420051201A2297C52A20 WIRE BELL 214 214ST 1182106SW GE CT7TS CT72A 30030NE SCAS CHAFED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0359806 28140 SCAS FAILED IN FLIGHT. ATTEMPTED TO RESET IT BUT IT BLEW THE CIRCUIT BREAKER. SECURED OFF AND CONTINUED TO BASE WITHOUT INCIDENT. MAINTENANCE REPAIRED CHAFED WIRE WHICH RUNS BETWEEN THE SCAS AMP AND THE YAW ACTUATOR. 2G72 4U4 U H10SW E8NE 20060223001182006022300118 2006 2 23 HEEA107320 420051211A22157690001802106 ACTUATOR SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL1S1 60030NE YAW INOPERATIVE E HEEAO OTHER O OTHER CRCRUISE 1 SW03761P 537 760588 DURING CRUISE FLIGHT, THE AIRCRAFT STARTED FISH TAILING. RETURNED TO DEPARTURE. MAINTENANCE REPLACED THE NR 1 AFCS YAW ACTUATOR. 1G72 3U3 UNCH1NE E19EU 20060223001192006022300119EU 2006 2 23 HEEA107316 120051129A2900350A27310728 PLATE SNIAS 350 AS350B3 8680954EU OVERTORQUED B HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03973AE4032 3229 DURING THE GROUND TEST OF THE HYDRAULIC SYSTEM, THE HYD TEST BUTTON ON THE LOWER CONSOLE WAS DEPRESSED AND THE CHECK INITIATED. THE COLLECTIVE LOCKING DEVICE DISENGAGED AND THE AIRCRAFT BECAME AIRBORNE. AIRCRAFT CONTROL WAS REESTABLISHED AND AIRCRAFT WAS LANDED. ON SHUTDOWN VEMD SHOWED OVER LIMIT DETECTED. VEMD SHOWED OVERTORQUE OF 110 FOR 17 SECONDS. 1G71 3U H9EU 20060223001212006022300121NE 2006 2 23 HEEA107323 220050822A73233040654 TUBE BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE GOVERNOR FAILED B HEEAO OTHER J WARNING INDICATION CRCRUISE 1 SW032258F 33073 IN CRUISE FLIGHT AT 1200' AT 70% TORQUE, OBSERVED LARGE TORQUE SPLIT. NR 1 HIGH, NR 2 HAD DROPPED TO ZERO. N1 ON NR 2 WAS NOTED AT 58%. IDENTIFIED NR 2 ENGINE GOVERNOR FAILURE. SELECTED NR 2 ENGINE MANUAL THROTTLE, DIVERTED TO MANASSAS. LANDED WITH NO INCIDENT. REPLACED TUBE ASSY AND NO OTHER DEFECTS NOTED. 1G72 4U4 U H4SW E22EA 20060223001232006022300123GL 2006 2 23 HEEA107326 220050904A720023053999 ENGINE BELL 230 230 1182149SW ALLSN 250C 250C30G2 03013GL NR 2 POWER LOSS B HEEAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SW03230H 3876 23004 ON TAKEOFF, THE NR 2 ENGINE LOST POWER. PILOT PERFORMED SINGLE ENGINE LANDING. REPLACED ENGINE ASSEMBLY. 1G72 3U3 UNCH9SW E1GL 20060223001252006022300125NE 2006 2 23 HEEA107328 120051005A3210EWS22741 BOLT SKRSKYS76 S76A 8143006NE MLG FROZEN B HEEAO OTHER J WARNING INDICATION CLCLIMB 1 SW03762P 760060 AFTER TAKEOFF, LANDING GEAR WAS RETRACTED. RED UNSAFE LIGHT DID NOT GO OUT. LANDING GEAR WAS EXTENDED, GOT THREE GREEN AND LANDED AT LFT. MAINTENANCE FOUND MAIN LANDING GEAR TIEDOWN RING ATTACHMENT BOLT FROZEN, CAUSING TIEDOWN RING TO NOT BE FREE TO SPRING AND LAY AGAINST LANDING GEAR STRUT, CAUSING INTERFERENCE WITH LANDING GEAR DOOR DURING RETRACTION. REPLACED BOLT. 1G72 3U H1NE 20060223001282006022300128SW 2006 2 23 HEEA107334 120050612A6210206015001115 BLADE BELL 206 206L1 1182107SW MAIN ROTOR PEELING B HEEAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 SW035000K1762 45167 AT CRUISE SPEED AT 105 KTS, PILOT FELT SOMETHING IN CONTROLS AND AIRCRAFT STARTED SHAKING UP AND DOWN SEVERLY. PILOT IMMEDIATELY LOWERED COLLECTIVE AND REDUCED AIRSPEED. THE AMOUNT OF SHAKING SUBSIDED WITH THE CHANGE IN AIRSPEED. AIRCRAFT WAS FLYABLE WITH VERTICAL VIBRATION. PILOT RETURNED AND LANDED AND PERFORMED EMERGENCY SHUTDOWN. UPON POSTFLIGHT INSPECTION IT WAS DETERMINED THAT AN OUTSIDE TRIM TAB LOWER BONDING HAD PEELED AWAY FROM BLADE. NO DAMAGE ELSEWHERE. REPLACED MAIN ROTOR BLADE. 1G71 3U H2SW 20060223001292006022300129NE 2006 2 23 HEEA107338 120050816A26126555004023103 AMPLIFIER SKRSKYS76 S76A 8143006NE NR 1 FIRE WARN FAILED B HEEAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW035435V 760158 DURING CRUISE AT 6500 FT, NR 1 ENGINE FIRE CAPSULE, WARNING HORN AND T HANDLE ACTIVATED. BEGAN EMERGENCY PROCEDURES AND SIC STATED HE SMELLED SOMETHING BURNING, PIC CONCURRED. EMERGENCY PROCEDURES COMPLIED DURING DESCENT. SINGLE LANDING PERFORMED. REPLACED AMPLIFIER. 1G72 3U H1NE 20060223001322006022300132NE 2006 2 23 HEEA107342 120050408A53447620508001133 HINGE SKRSKYS76 S76A 8143006NE ACCESS DOOR MISSING B HEEAO OTHER O OTHER CRCRUISE 1 SW03762P 760060 DURING CRUISE FLIGHT A LOUD NOISE WAS HEARD. RETURNED TO CAMERON. MAINTENANCE FOUND THE ACCESS DOOR AND HINGE PIN MISSING FROM THE FRONT OF THE FORWARD COWLING. REPLACED HINGE. 1G72 3U H1NE 20060223001352006022300135SW 2006 2 23 HEEA107347 120050222A2910214076764101 TUBE BELL 214 214ST 1182106SW HYD SYSTEM LEAKING B HEEAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0359806 28140 IN CRUISE FLIGHT UTILITY HYDRAULIC AND OIL COOLER SEGMENT LIGHTS ILLUMINATED. FOLLOWED APPROPRIATE EMERGENCY CHECKLISTS AND RETURNED TO MCY. MAINTENANCE FOUND PIN HOLE IN TUBE UNDER ADEL CLAMP. 2G72 4U H10SW 20060223001362006022300136EU 2006 2 23 HEEA107349 120050428A29106920 SOLENOID VALVE BOLKMS105 BO105S 5626006EU HYD SYSTEM WARNING LIGHT B HEEAO OTHER J WARNING INDICATION CRCRUISE 1 SW0381832 S828 DURING CRUISE FLIGHT, THE HYDRAULIC BLOCK LIGHT CAME ON. RETURNED TO BASE AND MAINTENANCE REPLACED SOLENOID VALVE. 1G72 3U H3EU 20060223001382006022300138NE 2006 2 23 HEEA107351 220050722A7200CT72A ENGINE BELL 214 214ST 1182106SW GE CT7TS CT72A 30030NE NR 1 MALFUNCTIONED B HEEAO OTHER J WARNING INDICATION CRCRUISE 1 SW033897N8083 28106 IN CRUISE, NR 1 ENGINE NR AND NG AND MGT WENT HIGH, TORQUE AND NP SHOWED ZERO, REDUCED NR 1 THROTTLE AND PERFORMED CHECKLIST AND SHUT ENGINE DOWN. ROTOR RPM WENT TO 107 FOR 10 SECONDS. INSPECTED ENGINE AND REPLACED YELLOW ENGINE HARNESS AND ECU. 2G72 4U4 U H10SW E8NE 20060223001402006022300140NE 2006 2 23 HEEA107358 120050713A52467630207014057 DOOR SKRSKYS76 S76C 8143008NE EXTERIOR MISSING B HEEAO OTHER D INFLIGHT SEPARATION NRNOT REPORTED 1 SW03505PH4522 760505 DURING POST FLIGHT, OIL LEVEL CHECK FOUND DOOR MISSING. REPLACED DOOR. 1G72 3U NCH1NE 20060223001412006022300141NE 2006 2 23 HEEA107359 120050708A67307665005801112 SERVO SKRSKYS76 S76A 8143006NE TAIL ROTOR MALFUNCTIONED B HEEAO OTHER J WARNING INDICATION CRCRUISE 1 SW03776P 2510 760275 AFTER CRUISE CHECK, THE NR 1 HYDRAULIC LIGHT CAME ON; FOLLOWED CHECKLIST AND WERE UNABLE TO CLEAR LIGHT. RETURNED TO MCY FOR MAINTENANCE. REPLACED TAIL ROTOR SERVO. 1G72 3U H1NE 20060223001422006022300142SW 2006 2 23 HEEA107360 120050216A6340412075008111 INDICATOR BELL 412 412 1182202SW TORQUE FAILED B HEEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW032261D 33076 COPILOT NR 1 TORQUE INDICATOR FAILED IN FLIGHT. MAINTENANCE REPLACED THE TORQUE INDICATOR. 1G72 4U H4SW 20060223001582006022300158NE 2006 2 23 PCSA12070501 220051207A7230 COMPRESSOR BOEING727 7272F9 138407DNM PWA JT8 JT8D15 52051NE NR 2 ENGINE STALLED A PCSAEA ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CRCRUISE 1 SO29199AJ383397722 21426 708908 FLIGHT 723 DEPARTED MIA AND CLIMBED TO 34,000 FT CRUISE ALTITUDE, CREW REPORTED NUMBER 2 ENG COMPRESSOR STALLED, POWER WAS REDUCED AND NR 2 ENG CONTINUED TO COMPRESSOR STALL. THE CREW PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN, ALL FLIGHT CONDITIONS WERE NORMAL, THE NR 2 ENGINE WINDMILLED FOR 15 MINUTES. THE A/C RETURNED BACK TO MIA AND LANDED WITHOUT ANY FURTHER INCIDENT. MX INSPECTED & REPLACED NR 2 ENG MAIN OIL STRAINER. LEAK CHECK GOOD. MX ACCOMPLISHED A HIGH POWER TAKE-OFF RUN/STEADY STATE CRUISE, AND SURGE TROUBLESHOOTING, NO DEFECTS NOTED. ENGINE HIGH POWER RUN, OPERATIONALLY CHECKED NORMAL. A BLEED SCHEDULE CHECK, A T/A ANTI-ICE VALVE CHECKED NORMAL. 2L73 4F4 FRTA3WE E2EA 20060223001592006022300159NM 2006 2 23 SPAA0500047 120051215A2560P4010021 BATTERY BOEING737 7372Y5 1384554NM FLASHLIGHT DISCHARGED A SPAAK NONE L NO TEST ININSP/MAINT 1 WP28712S 23038 EMERGENCY FLASHLIGHT BATTERY DEAD AT AFT FLIGHT ATTENDANT STATION. REPLACED EMERGENCY FLASHLIGHT BATTERY IAW B737MM 25-69-0 & 20-50-11, OPS CHECK NORMAL. 2L72 4U RTA16WE 20060223001602006022300160NM 2006 2 23 SPAA0500048 120051216A3350900835A BATTERY PACK BOEING737 7372Y5 1384554NM CABIN DISCHARGED A SPAAK NONE L NO TEST ININSP/MAINT 1 WP28712S 23038 SCHEDULED MAINTENANCE VISIT, FWD DOOR AREA CEILING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK IAW B737MM 33-51-02. OPERATIONAL CHECK NORMAL. 2L72 4U RTA16WE 20060223001712006022300171CE 2006 2 23 DJFA2005182 120051226A3260327 BULB BEECH MU300 400A 1155402CE MLG INDICATOR BURNED OUT E DJFAA UNSCHED LANDING P NO WARNING INDICATION APAPPROACH 1 EA23442CW RK42 CREW REPORTED, LT GREEN GEAR LIGHT DID NOT ILLUMINATE WHEN THE GEAR WAS EXTENDED FOR LANDING INTO KASE. GEAR LEVER WAS RECYCLED ONCE AND LEFT GEAR INDICATION STILL DID NOT ILLUMINATE. THE APPROACH TO KASE WAS ABORTED, A/C WAS DIVERTING TO KEGE. CREW EXCHANGED THE RT GEAR INDICATION BULB FOR THE LT AND EXTENDED LANDING GEAR. LT GEAR INDICATION ILLUMINATED, BUT NOT THE RT. TOWER NOTIFIED ATC THAT A/C WAS IN AN EMERGENCY CONDITION AND CREW DECLARED MINIMUM FUEL. WHILE ON SHORT FINAL INTO KEGE, TOWER CONFIRMED THAT ALL THREE LANDING GEAR APPEARED TO BE DOWN. AN UNEVENTFUL LANDING WAS MADE IN KEGE. MX REPLACED LT LANDING GEAR INDICATION LIGHT. OPS CHECKS WERE GOOD AND A/C WAS RETURNED TO SERVICE. 2H72 4F RTA16SW 20060223001732006022300173SW 2006 2 23 HEEA107419 120051213A243523046020 STARTER GEN BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE NR 2 FAILED E HEEAK NONE O OTHER NRNOT REPORTED 1 SW032261D20048 33076 NR 2 GENERATOR FAILED IN FLIGHT. REPLACED NR 2 STARTER GENERATOR. 1G72 4U4 U H4SW E22EA 20060223001742006022300174NM 2006 2 23 DHL2005786003 120051125A7711LG14C14 TRANSMITTER BOEING727 727214 138407RNM NR 2 EPR FAILED A DHLAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO01786AT 21692 NR 2 EPR GAUGE HAD NO INDICATION AS TAKEOFF THRUST APPLIED. TAKEOFF WAS REJECTED. ALL ENG INDICATIONS WERE NORMAL BEFORE LOSS OF EPR GAUGE. N1, N2, FUEL FLOW AND EGT FUNCTIONING NORMAL. DEFERRED NR 2 EPR PER MEL 77-1-1. CAT A. KPS CONTROL NR 23343 AT 0953. ITEM TRANSFERRED TO DMI LOG AT THIS LOCATION-IAH. PLACARD INSTALLED, REF: DMI 23343 - NR 2 EPR GAUGE HAD NO IND AS T/O THRUST APPLIED. REMOVED AND REPLACED NR 2 EPR TRANSMITTER REF: B727-200 MM CHPT 77-11-11. OPS CK GOOD PER ASTAR J.R.H. CHPT 5. THIS CLEARS DMI #23343. PLA REMOVED. 2L73 4F A3WE 20060223001762006022300176NM 2006 2 23 05FDEA04397 120051221A5315 REPAIR BOEING727 727227 1384078NM FLOORBEAM MISINSTALLED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 REPAIR ON MAIN DECK FLOORBEAM UPPER FLANGE BS 480, LBL 5 TO RBL 24. REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED TO NOT BE IAW SRM 53-10-8. REMOVED AND REPLACED REPAIR IAW SRM 53-10-8 FIG 1. 2L73 4F A3WE 20060223001772006022300177NM 2006 2 23 05FDEA04413 120051227A5310 CREASE BEAM BOEING727 727227 1384078NM BS 1120-1130 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 FOUND CORROSION ON CREASE BEAM ANGLE, BS 1120 TO BS 1130, LBL 65, WL 208. 2L73 4F A3WE 20060223001792006022300179NM 2006 2 23 05FDEA04415 120051227A5101 REPAIR BOEING727 727227 1384078NM FUSELAGE UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 FUSELAGE FLUSH REPAIR AT BS 1150, BL0, REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIRED SKIN PER SRM 53-30-3. 2L73 4F A3WE 20060223001952006022300195SW 2006 2 23 HEEA107416 120051217A7931222375077113 TRANSMITTER BELL 222 222U 1182140SW LYC LTS101LTS101750C1 41560NE OIL PRESSURE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036992 47521 NR 1 ENGINE OIL PRESSURE GAUGE PEGGED OUT ON THE HIGH SIDE. MAINTENANCE REPLACED THE ENGINE OIL PRESSURE TRANSMITTER. 1G72 3U3 U H9SW E5NE 20060223001962006022300196EU 2006 2 23 05FDEA04105 120051203A5101 REPAIR AIRBUS310 A310203 3930313EU T/E FLAP UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25424FE 241 COMPLY WITH AGING 9-AGING-INSP, PREVIOUS REPAIR INSTALLED AT LEFT HAND OUTBOARD FLAP (TOP TRAILING EDGE WEDGE SECTION - COMPOSITE) AT WS 823 TO WS 835. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIRED IAW SRM 57-53-12 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR. 2L72 4F RTA35EU 20060223001982006022300198EU 2006 2 23 MAC120501 120051221A3246 BEARING LORAL AEROSPATR42 ATR42320 8680930EU PWA PW121 PW121 52124NE WHEEL ASSY MISSING A MTNAK NONE O OTHER ININSP/MAINT 1 SO33906FX SEP9457 280 ON POST FLT WALK AROUND INSP. A MECHANIC DISCOVERED A PROBLEM WITH THE RT NOSE WHEEL ASSEMBLY. AFTER REMOVING THE WHEEL ASSEMBLY THE OUTER BEARING WAS MISSING PARTS CAUSING UNREPAIRABLE DAMAGE TO THE AXLE ASSEMBLY. THE WHEEL ASSEMBLY IS MFG BY AIRCRAFT BRAKING SYSTEMS (ABS). 2H72 4T4 TRTA53EU E20NE 20060223001992006022300199EU 2006 2 23 05FDEA04106 120051203A5101 REPAIR AIRBUS310 A310203 3930313EU LT WING UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25424FE 241 COMPLY WITH AGING 9-AGING-INSP, PREVIOUS REPAIR INSTALLED AT LEFT HAND WING ROOT (LEADING EDGE ABOVE KRUEGER FLAP) AT WS 57 TO WS 77. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIRS CONFORMS TO EXISTING FEDEX ENG EA 6-5710-94660. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR. 2L72 4F RTA35EU 20060223002052006022300205CE 2006 2 23 122105N317CS1 120051221A291674593 RESERVOIR CESSNA500 550 2076604CE HYD SYSTEM UNKNOWN E Z5FAA UNSCHED LANDING EKJVIBRATION/BUFFET FLUID LOSS WARNING INDICATION CLCLIMB 1 NE03317CS3389 5501019 AFTER T/O ATTEMPTED TO RETRACT MLG, HEARD A LOUD NOISE & HAD CAUTION LIGHTS ILLUMINATE. GEAR UNSAFE, HYD PRESSURE , & LOW FLUID LIGHTS CAME ON. SELECTED GEAR DOWN & PULLED EMERGENCY BLOWDOWN HANDLE. GEAR WENT INTO DOWN & LOCKED POSITION & GEAR INDICATORS NORMAL, HYD LOW LEVEL LIGHT STAYED ON. CREW DECLARED AN EMERG & DIVERTED, LANDING UNEVENTFUL. A/C FOUND TO HAVE NO HYD FLUID, CAUSE BEING INVESTIGATED. COMPLETE CHK OF HYD SYS; ALL VALVES, ACTUATORS & PLUMBING COMPLETED, NO DEFECTS FOUND. FILTERS & PUMPS INSPECTED, NO DEFECTS NOTED. HYD RESERVOIR SUSPECTED FAILED, ALLOWING FLUID TO VENT OVERBOARD. RESERVOIR REPLACED & REMOVED COMPONENT IS BEING SENT TO OEM FOR EVALUATION. A/C RETURNED TO SERVICE. 1L72 4F A22CE 20060223002072006022300207CE 2006 2 23 DJFA2005181 120051226A2120 ODOR BEECH MU300 400A 1155402CE COCKPIT DETECTED E DJFAO OTHER B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 EA23709TA RK180 DURING T/O A HEAVY ODOR SIMILAR TO MELTING PLASTIC COMING FROM PAX COMPT AT TIME OF DISCOVERY, TEMP CONTROL WAS SET ON AUTO, TEMP KNOB IN HOT POSITION. CREW DONNED THEIR OXYGEN MASKS & TURNED OFF ALL CABIN HEAT. APPROX 10 MINS ODOR DISSIPATED. A NORMAL LANDING. MX INSPECTED CABIN TEMP CONTROL VALVES FOR PROPER OPERATION & LEAKS, AND CHECKED TEMP SENSOR RESISTANCE. NO DEFECTS NOTED. AFTER CLEANING CABIN TEMP SENSOR, AND OPERATIONALLY CHECKING TEMP CONTROLS, AFT HEAT VENT WAS FOUND TO BE VERY HOT. BEECHCRAFT SB 21-3289 FOR REDUCING HEAT VENT TEMPERATURE INSTALLED USING KIT 128-5043-1. OPS CHECKS AFTER KIT INSTALLATION WERE GOOD. A/C WAS RETURNED TO SERVICE. 2H72 4F RTA16SW 20060228000592006022800059SO 2006 2 28 SIMA200534501 120051208A332011049 CHARGER EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL CABIN LIGHTS INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21739AE 145402 DISC FLOOR PROXIMITY LIGHTS COME ON BY THEMSELVES AND WOULD NOT EXTINGUISH. REPLACED NR 3 BATTERY CHARGER. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (K) 2L72 4F4 FRTT00011ATTE6CH 20060228001042006022800104WP 2006 2 28 IXXA05SMN304S 120051229A5330 SKIN DOUG DC8 DC872 302199BWP FUSLEAGE DENTED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11722CX 46130 DURING ROUTINE C-CHECK INSPECTION, EXTERNAL FUS FWD CARGO COMPT AFT CARGO DOOR SKIN WITH (06EA) DENTS. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-0 FIG 2A (SHEET 1), TR 57-84 DATED 08-01-00. REMOVED NON STANDARD REPAIR IAW DC8 SRM 51-1-21. REMOVED DAMAGED SECTION IAW DC-8 SRM 57-2-0 FIG 2A (SHEET 1). FABRICATED NEW EXT REPAIR DOUBLER , FILLER IAW DC8 SRM 57-2-0 FIG 2A (SHEET 1), DC-8 SRM 57-3-2 FIG 31. CLEANED, TREATED AND PRIMED AREA INNER SIDE IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACE IAW DC8 SRM 51-1-11. INSTALLED REPAIR PARTS IAW DC8 SRM 57-2-0 FIG 2A (SHEET 1), DC-8 SRM 51-1-21. 2L74 4F RT4A25 20060228001222006022800122EA 2006 2 28 SWIA200516278 120051108A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07927SW 7693 FS 280 LT FLOORBEAM LBL 9.0 I/B AND O/B ATTACH ANGLES CRACKED, ITEM FOUND AT C CHECK INSPECTION. ANGLES AT FS 280, LBL 9 I/B AND O/B REPLACED IAW CRJ SRM 51-42-06, 51-23-00, 51-40-11 AND 51-42-21. 2L72 4F RTA21EA 20060228001232006022800123EA 2006 2 28 SWIA200516279 120051108A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA BS 484 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07927SW 7693 CABIN FLOOR FS 484 LT INTERCOSTAL LBL 27 AND LBL 36 CRACKED, ITEM FOUND AT C CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-41-059 REV "A". 2L72 4F RTA21EA 20060228001242006022800124EA 2006 2 28 SWIA200516280 120051108A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA BS 625 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07927SW 7693 LT INTERCOSTAL (CLIP) CRACKED AT FS 625 AND STRINGER 14L, ITEM FOUND AT C CHECK INSPECTION. REPLACED CLIP IAW CRJ SRM 51-42-06. 2L72 4F RTA21EA 20060228001252006022800125EA 2006 2 28 SWIA200516281 120051108A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA CRACKED CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07927SW 7693 FS 280 RT FLOORBEAM RBL 9.0 I/B AND O/B ATTACH ANGLES CRACKED, ITEM FOUND AT C CHECK INSPECTION. REPLACED ANGLES AT FS 280, RBL 9 I/B AND O/B IAW CRJ SRM 51-42-06, 51-23-00, 51-40-11 AND 51-42-21. 2L72 4F RTA21EA 20060228001262006022800126EA 2006 2 28 SWIA200516282 120051108A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA BS 460 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07927SW 7693 CABIN FLOOR RT SUPPORT FITTING FS 460 RBL 9.0 CRACKED, ITEM FOUND AT C CHECK INSPECTION. REPLACED FITTING IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, 51-21-11. 2L72 4F RTA21EA 20060228001272006022800127EA 2006 2 28 SWIA200516283 120051108A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA BS 484 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07927SW 7693 CABIN FLOOR FS 484 RT INTERCOSTAL INBD CLIP RBL 27 CRACKED ITEM FOUND AT C CHECK INSPECTION. CLIP REPLACED IAW CRJ REO 601R-53-41-059 REV "A" AND AMM 20-24-00. 2L72 4F RTA21EA 20060228001282006022800128EA 2006 2 28 SWIA200516284 120051108A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA BS 625 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07927SW 7693 RT INTERCOSTAL (CLIP) CRACKED AT FS 625 AND STRINGER 14R, ITEM FOUND AT C CHECK INSPECTION. REPLACED CLIP IAW CRJ SRM 51-42-06. 2L72 4F RTA21EA 20060228001442006022800144EA 2006 2 28 SWIA200516309 120051115A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA BS 625 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07416SW 7089 AFT EQUIPMENT COMPARTMENT FS 625 STR 14L LT INTERCOSTAL CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED INTERCOSTAL IAW CRJ REO 601R-53-61-100, 601R-53-61-422. 2L72 4F RTA21EA 20060228001452006022800145EA 2006 2 28 SWIA200516310 120051209A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07930SW 7713 FS 280.00 AT RBL 9 , I/B FLOORBEAM ATTACH ANGLE IS CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ SRM 51-22-00, 51-42-21, 51-41-01, -51-21-11, 51-40-11 PARA 4. 2L72 4F RTA21EA 20060228001462006022800146EA 2006 2 28 SWIA200516311 120051209A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07930SW 7713 FS 280.00 AT LBL 9 - O/B FLOORBEAM ATTACH ANGLE IS CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED ATTACH ANGLE IAW CRJ 51-22-00, 51-42-21, 51-41-02, 51-21-11 AND 51-40-11 PARA 4. 2L72 4F RTA21EA 20060228001472006022800147EA 2006 2 28 SWIA200516312 120051209A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA BS 625 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07930SW 7713 FS 625.00 AT STRINGER 14R ATTACH CLIP CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-61-442 AND REO 601R-53-61-100. 2L72 4F RTA21EA 20060228001482006022800148EA 2006 2 28 SWIA200516313 120051209A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07930SW 7713 FS 280.00 AT RBL 9, O/B FLOORBEAM ATTACH ANGLE IS CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ SRM 51-22-00, 51-42-21, 51-41-02, 51-21-11, 51-40-11 PARA 4. 2L72 4F RTA21EA 20060228001492006022800149EA 2006 2 28 SWIA200516314 120051209A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA BS 484 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07930SW 7713 FUSELAGE, PULLEY INTERCOSTAL HAS CRACKED I/B ANGLE FS 484.00; LBL 27.0, ITEM FOUND AT C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ REO 601R-53-41-059 REV A. 2L72 4F RTA21EA 20060228001502006022800150EA 2006 2 28 SWIA200516315 120051209A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA BS 625 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07930SW 7713 FS 625.00 AT STRINGER 14L ATTACH CLIP CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-61-422 AND REO 601R-53-61-100. 2L72 4F RTA21EA 20060228001512006022800151EA 2006 2 28 SWIA200516316 120051209A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 621 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07930SW 7713 FS 621.00, LBL 40, FLOORBEAM ANGLE IS CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-61-117 REV C. 2L72 4F RTA21EA 20060228001522006022800152EA 2006 2 28 SWIA200516317 120051117A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA BS 621 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07449SW 7699 AFT CARGO FS621 LT SIDE OTBD FRAME CRACKED, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR ANGLES PER REO 601R-53-61-117 SHTS 1 THRU 3 REV 'B'. 2L72 4F RTA21EA 20060228001532006022800153EA 2006 2 28 SWIA200516318 120051117A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA BS 623 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07449SW 7699 AFT CARGO FS623 RT OTBD SIDE FRAME CRACKED, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR TO FS 621 RIGHT OTBD SIDE FRAME IAW REO 601R-53-61-117. 2L72 4F RTA21EA 20060228001542006022800154EA 2006 2 28 SWIA200516319 120051117A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA BS 640 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07449SW 7699 FS 640 FRAME RT SIDE HAS 2' CRACK IN REINFORCEMENT ANGLE, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED FRAME SECTION REPAIR PARTS TO RT FS 640 IAW CRJ200 SRM 51-42-6; 51-42-20; AND 51-42-21. 2L72 4F RTA21EA 20060228001552006022800155EA 2006 2 28 SWIA200516320 120051117A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA BS 640 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07449SW 7699 FS 640 FRAME LT SIDE HAD 3' CRACK IN REINFORCEMENT ANGLE, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED AT LT FS 640 BETWEEN LT STRINGER 6-12 FRAME SECTION SPLICE ANGLE AND FILLER IAW REO 601R 53-61-487 REV 'C'. 2L72 4F RTA21EA 20060228001562006022800156EA 2006 2 28 SWIA200516321 120051117A5340 BRACKET CNDAIRCL600 CL6002B19 1900309EA BS 625 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07449SW 7699 STA 625 STR 14 LT AND RT BRACKETS CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED CRACKED INTERCOSTALS IAW CRJ200 SRM 51-40-11/51-42-21/51-25-16 AND REO 601R 53-81-422. 2L72 4F RTA21EA 20060228001572006022800157EA 2006 2 28 SWIA200516322 120051129A5340 STRINGER CLIP CNDAIRCL600 CL6002B19 1900309EA BS 625 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07427SW 7497 LT SIDE FS 625 STR 14L CLIP CRACKED, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW CLIP PART IAW CRJ200 SRM 51-42-06 PG 9-14 . 2L72 4F RTA21EA 20060228001582006022800158EA 2006 2 28 SWIA200516323 120051129A5340 STRINGER CLIP CNDAIRCL600 CL6002B19 1900309EA BS 625 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07427SW 7497 RT SIDE FS 625 STR 14R CLIP CRACKED, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW CLIP IAW CRJ200 SRM 51-42-06 PG 9-14. 2L72 4F RTA21EA 20060228001592006022800159EA 2006 2 28 SWIA200516324 120051129A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07427SW 7497 FS 280 LBL 9 INNER AND OUTER FLOORBEAM ANGLES CRACKED, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW INNER FLOOR SPORT ANGLE AT FS 280.0 LBL9 IAW REO 601R F53-11-136. 2L72 4F RTA21EA 20060228001602006022800160EA 2006 2 28 SWIA200516325 120051129A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07427SW 7497 FS 280 RBL 9 INNER AND OUTER FLOORBEAM ANGLES CRACKED, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW CLIPS AT FS 280 RBL 9 INNER AND OUTER FLOOR SUPPORT ANGLES IAW REO 601R-53-11-136. 2L72 4F RTA21EA 20060302000112006030200011EU 2006 3 2 SDR2005089 120051221A7712AIR985 TORQUE SENSOR AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE RT ENGINE INOPERATIVE A TRBAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO29322AC 320 AFTER TAKEOFF AND DURING CLIMBING, THE RT ENGINE STARTED TO FLUCTUATE ABOUT 10 PERCENT. REPLACED NR 2 TORQUE SENSOR. (K) 2H72 4T4 TRTA53EU E20NE 20060302000342006030200034WP 2006 3 2 IXXA05SMN319S 120051229A5542 REPAIR DOUG DC8 DC872 302199BWP RUDDER CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11722CX71621 46130 DURING ROUTINE C-CHECK INSPECTION, RIGHT RUDDER REPAIR DOUBLER EDGES CORRODED, STA ZR 61.156. PERFORMED MAJOR REPAIR IAW DC-8 SRM 55-6-1 FIG 1, EO SEMAN 20051480 DATED 12-20-05. REMOVED CORROSION IAW DC8 SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW SEMAN DC-8 SRM 55-2-0 PAGE 12. REMOVED CORRODED PLATING IAW DC-8 SRM 55-1-0, DC-8 SRM 51-1-21. FABRICATED NEW PLATING (AL 2024 T3 0.040) IAW SEMAN DC-8 SRM 5-6-1 FIG 1 ITEM -C-. CLEANED, TREATED; PRIMED AREA & REPAIR DOUBLER IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11. INSTALLED NEW PLATING IAW DC8 SRM 51-1-21. FOR REBALANCE SEE N/R 2849. 2L74 4F RT4A25 20060302000352006030200035WP 2006 3 2 IXXA05SMN320S 120051229A5340 FITTING DOUG DC8 DC872 302199BWP BS 822.500 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11722CX71621 46130 DURING ROUTINE C-CHECK INSPECTION, MAIN CARGO CMPT - WING CENTER SECTION FITTING CRACKED 3, AT STA 822.500, L-22R. REMOVED CRACKED FITTING IAW DC-8 SRM 51-1-20D. FABRICATED NEW FITTING IAW ATI REPAIR SPECIFICATION 2003-05, DOUGLAS DWG 4753360. PERFORMED NDT INSP IAW DC-8 NDT SPM PART 08-00-02-07. CLEANED, TREATED AND PRIMED AREA & NEW FITTING IAW DC-8 SRM 51-1-8B. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D, DC-8 SRM 51-3-1. 2L74 4F RT4A25 20060310000662006031000066NM 2006 3 10 UPS06M46278 120051207A5510 STRUCTURE DOUG MD11 MD11F 3023600NM EMPENNAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01282UP 48452 INSPECTION TYPE:C EMPENNAGE - BARREL NUT HOLE 02 LEFT FOUND BEARING WITH SURFACE CORROSION ON SIDE & BOTTOM AREA. CORROSION REMOVAL C/OUT & FOUND BLENDED OUT BEYOND ALLOWABLE LIMIT. BARREL NUT HOLE 02 LEFT BORE & BOTTOM REWORKED PER EN 1640-05. FAB SLEEVE BUSHING PER EO MD11-5510-19409-K. APPLIED SEALANT PR1422B1/2 BLEND OUT AREA & S/BUSHING PER EO MD11-5510-19409-K. REPAIR ACCOMPLISHED AT BARREL NUT HOLE 02 LEFT PER EO MD11-5510-19409-K & EN1640-05, FOUND SATIS. 2L73 4F RTA22WE 20060310000672006031000067NM 2006 3 10 UPS06M46279 120051207A5510 STRUCTURE DOUG MD11 MD11F 3023600NM EMPENNAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01282UP 48452 INSPECTION TYPE:C EMPENNAGE - BARREL NUT HOLE 15 LEFT FOUND BEARING WITH SURFACE CORROSION ON SIDE & BOTTOM AREA. CORROSION REMOVAL C/OUT & FOUND BLENDED OUT BEYOND ALLOWABLE LIMIT. BARREL NUT HOLE 15 LEFT BORE & BOTTOM REWORKED PER EN1635-05. FAB SLEEVE BUSHING PER EO MD11-5510-19409-K,F-5. APPLIED PR1422B1/2 BLEND OUT AREA & S/BUSHING PER EO MD11-5510-19409-K. REPAIR ACCOMPLISHED AT BARREL NUT HOLE 15 LEFT PER EO MD11-5510-19409-K & EN1635-05, FOUND SATIS. 2L73 4F RTA22WE 20060310000682006031000068NM 2006 3 10 UPS06M46280 120051221A5510 STRUCTURE DOUG MD11 MD11F 3023600NM EMPENNAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01282UP 48452 INSPECTION TYPE:C EMPENNAGE - BARREL NUT HOLE 20 LEFT FOUND BEARING WITH SURFACE CORROSION ON SIDE & BOTTOM AREA. CORROSION REMOVAL C/OUT & FOUND BLENDED OUT BEYOND ALLOWABLE LIMIT. BARREL NUT HOLE 20 LEFT BORE & BOTTOM REWORKED PER EN1024-06. FAB SLEEVE BUSHING PER EO MD11-5510-19409-K,FIG-5. APPLIED SEALANT PR1422B1/2 BLEND OUT AREA & S/BUSHING PER MD11-5510-19409-K. REPAIR ACCOMPLISHED AT BARREL NUT HOLE 20 LEFT PER EO MD11-5510-19409-K & EN1024-06, FOUND SATIS. 2L73 4F RTA22WE 20060314000972006031400097EU 2006 3 14 06FDEA0925 120051122A3240 SPACER AIRBUS310 A310203 3930313EU MLG BRAKES MISINSTALLED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25427FE 362 AFTER LANDING NOTED NO RIGHT BRAKES AVAILABLE, BRAKE RELEASE LIGHTS IN VIEW BUT NO BRAKING PRESSURE. REMOVED 3, 4, 7 AND 8 TIRE ASSY AS PER A310 M/M 12-37-32. FOUND SPACER P/N 2606840 (4 EA) INSTALLED INCORRECTLY (SPACER WAS INSTALLED BETWEEN BRAKE AND TIRE ASSY INSTEAD OF BETWEEN TIRE ASSY AND AXLE NUT). INSPECTED ALL RIGHT MLG WHEEL ASSY AND ITS BEARINGS. NO DAMAGE NOTED. REINSTALLED 3, 4, 7 AND 8 TIRE ASSY AND SPACERS AS PER IPC 32-46-18-01A AND M/M 12-37-32. 2L72 4F RTA35EU 20060314001182006031400118SO 2006 3 14 C2XA05BT086 120051207A335020131A POWER SUPPLY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT FAULTY A C2XAK NONE O OTHER ININSP/MAINT 1 SW27129577549 7549 145080 CREW REPORTED, OVERWING EMERGENCY LIGHT NOT WORKING. MAINTENANCE REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY [POWER SUPPLY] AND OPS CHECKED SYSTEM GOOD IAW EMB145 AMM NR 33-50-04. 2L72 4T RTT00011AT 20060322002232006032200223SO 2006 3 22 MASA200501001 120051206A783083990168 SWITCH EMB 145 EMB145LR 3260212SO THRUST REVERSER MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07833MJ1526 145327 ASH 2994 DTW. NR 2 ENG THRUST REVERSER DISAGREE. MAINTENANCE REMOVED AND REPLACED TOP O/B STOW TRANSIT SWITCH. 2L72 4T RTT00011AT 20060322002242006032200224SO 2006 3 22 MASA200501034 120051213A3210M83536 RELAY EMB 145 EMB145LR 3260212SO MLG FAILED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07834MJ 145340 ASH 2925 ROA. CREW REPORTED A LANDING GEAR AIR TO GROUND FAIL MESSAGE AND WERE UNABLE TO RETRACT THE LANDING GEAR. MX REPLACED RELAYS AND PERFORMED GEAR SWINGS, OPS CHECK GOOD. 2L72 4T RTT00011AT 20060322002252006032200225SO 2006 3 22 MASA200501049 120051218A783083990152 SWITCH EMB 145 EMB145LR 3260212SO THRUST REVERSER MALFUNCTIONED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07834MJ12015 145340 ASH 2741 CLT. E1 THRUST REVERSER DISAGREE. MAINTENANCE REMOVED AND REPLACED BOTH STOW SWITCHES. 2L72 4T RTT00011AT 20050818000132005081800013NM 2005 8 18 SWAA052453 120050815A33506042221 LIGHT BOEING737 7373K2 13844BANM CABIN ERRATIC A SWAAK NONE O OTHER ININSP/MAINT 1 SW29345SA 23786 SEVERAL CABIN INTERIOR EMERGENCY EXIT LIGHTS ILLUMINATED. CYCLED EMERGENCY LIGHTS ARM SWITCH PER MM. OPS CHECKED GOOD. 2L72 4F RTA16WE 20050818000212005081800021NE 2005 8 18 FX7A200500008 220050805A7200CFM563B1 ENGINE BOEING737 73733A 1384673NM GE CFM56 CFM563B1 13802NE OVERHEATED A FX7AA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO19371FA 23631 721606 ENGINE NR 2 EGT REACHING 936 DEGREES AFTER TAKEOFF, IT WAS NECESSARY TO REDUCE POWER TO MAINTAIN BELOW 930 DEGREES, FIRST REDUCTION + OR - 2% N1 SECOND REDUCTION + OR - 4.5% N1, SET UP FOR 92.5% OAT 31 DEGRESS. AIRCRAFT TAKEN TO THE BLAST FENCE BY THE FLIGHT CREW AND MAINTENANCE BOTH ENG OPERATIONS TO REDUCE TAKEOFF POWER NR 1 EGT 865, NR 2 EGT 890 VISUALLY INSPECTED ENG INLET AND EXHAUST AND FOUND SAFE FOR THE INTENDED PART 91 MAINTENANCE FERRY FROM MIA TO TUS. MAINTENANCE PERFORMED THE REDUCED POWER CHECK. 2L72 4F4 FRTA16WE E2GL 20050818000252005081800025NM 2005 8 18 SWAA052465 120050815A575365C16950 ROLLER BOEING737 7373Y0 1384671NM RT WING FOREFLAPMISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED C4 CHECK, FOUND RT WING INBOARD T/E FOREFLAP MID-TRACK ROLLER MISSING. INSTALLED ROLLER PER MM. 2L72 4F RTA16WE 20050818000282005081800028NM 2005 8 18 SWAA052462 120050816A531165C22909 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29690SW 23783 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 20R. REPAIRED FRAME PER SWA EA. 2L72 4F RTA16WE 20050818000372005081800037CE 2005 8 18 08152005B 120050810A5610 WINDOW BEECH 1900 1900D 1154162CE COCKPIT SEPARATED A NSVAO OTHER D INFLIGHT SEPARATION CRCRUISE 1 EA27243CJ UE43 OUTER WINDOW PANE FELL OUT. INSTALLED NEW WINDOW. 2L72 4T RTA24CE 20050818000382005081800038NM 2005 8 18 AWXA200500952 120050813A21337110033 OUTFLOW VALVE BOEING737 7373G7 1384595NM CABIN PRESSURE MALFUNCTIONED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28157AW535322483 23779 DURING CLIMB NORMAL & ALTERNATE EQUIPMENT COOLING FAILED. ACFT RETURNED TO PHX, LANDED AND WOULD NOT DEPRESSURIZE. CABIN STAYED AT A DELTA P OF 2.0. MX R & R EQUIPMENT COOLING LOW FLOW SENSOR IAW BOEING MM 21-58-43-4. OPS CHECKS GOOD. ALSO, R & R OUTFLOW VALVE IAW AWA TASK CARD R6A21001. R & R CABIN PRESSURE CONTROLLER IAW AIRBUS MM 21-31-21-4. OPS CHECKS GOOD. VENDOR TEAR DOWN REPORT OF OUTFLOW VALVE CONFIRMS REASON FOR REMOVAL, UNIT FAILED INCOMING TEST. DC SWITCH REQUIRED ADJUSTMENT AND GATE BUMPER SEAL MISSING. UNIT REPAIRED AND TESTED IAW CMM 21-33-00 REV 19. VENDOR SHOWS CABIN PRESSURE CONTROLLER PASSED INCOMING TESTS AND NO FAULTS WERE FOUND. 2L72 4F RTA16WE 20050818000392005081800039NM 2005 8 18 AWXA200500958 120050718A574065494428 FITTING BOEING737 7373S3 1384711NM ZONE 600 - RIGHTCORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 DURING C18 CHECK DISCOVERED CORROSION ON THE RT MLG STABILIZER BEAM, FORWARD ATTACH FITTING. CORROSION WAS REMOVED IAW BOEING 737-300 SRM 51-10-02 AND FOUND TO BE OUT OF LIMITS IAW BOEING 7 37-300 SRM 57-20-90-1 FIG 102. MAINTENANCE REMOVED THE RT MLG STABILIZER BEAM, FORWARD ATTACH FITTING IAW BOEING 737-300 AMM 57-15-00-4. PREPARED NEW ATTACH FITTING FOR INSTALLATION IAW BOEING 737-300 51-40-05. INSTALLED NEW RT MLG STABILIZER BEAM, FORWARD ATTACH FITTING IAW BOEING 737-300 AMM 57-15-00-4 IAW BOEING 737-300 AMM 57-15-00-4. 2L72 4F RTA16WE 20050818000412005081800041NM 2005 8 18 AWXA200500960 120050730A532069505981 INTERCOSTAL BOEING737 7373Y0 1384671NM CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28334AW 23747 DURING C16 CHECK DISCOVERED CORROSION ON THE UNDERSIDE OF FLOOR STRUCTURE AT BS 991, WL 208, BL 17L. MAINTENANCE REMOVED CORROSION IAW BOEING 737-300 SRM 51-10-01. FOUND CORROSION TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-00-04-1 FIG 101. REMOVED FLOOR SUPPORT INTERCOSTAL AT BS 991, WL 208, BL 17L IAW BOEING 737-300 SRM 51-40-07. PREPARED NEW FLOOR SUPPORT, INTERCOSTAL FOR INSTALLATION IAW BOEING 737-300 SRM 51-40-05-0FIG 2. INSTALLED REPAIR PART AT BS 991, WL 208, BL 17L IAW BOEING 737-300 SRM 51-40-02-0 FIG 3 AND FIG 12. 2L72 4F RTA16WE 20050818000452005081800045NM 2005 8 18 2005UALA00791 120050807A3350 SWITCH BOEING757 757222 1384956NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP2987UA 26713 L-2 DOOR EMERGENCY LIGHT TEST SWITCH INOP. REPLACED SWITCH. 2L72 4F4 FRTA2NM E17NE 20050818000462005081800046NM 2005 8 18 2005UALA00792 120050805A3350 LIGHT BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE CABIN INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29657UA 27112 LEFT SIDE FIRST CLASS EEL STRIPS INOP. 2L72 4F4 FRTA1NM E24NE 20050818000472005081800047 2005 8 18 2005UALA00793 420050804A25657A1323113 SLIDE BOEING747 747422 1384935NM PWA 4056 PW4056 NE ESCAPE SLIDE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29128UA 30023 EES RECEIVED FOR SERVICE WITH NO SAFETY PIN IN ONE OF TWO CYLINDERS. ----THIS ITEM IS NOT A SDR REPORTABLE ITEM.---- SLIDE BOTTLES ARE SUPPOSED TO BE UNPINNED WHEN THE UNITS ARE IN THE INSTALLED CONDITION ON THE ACFT. SAFETY PIN IS FOR TRANSPORTATION OR HANDLING OF A CHARGED BOTTLE ASSEMBLY. 2L74 4F4 FRTA20WE E24NE 20050818000512005081800051NM 2005 8 18 2005UALA00797 120050810A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE LT OVERWING INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29187UA 26877 LEFT OVERWING AFT TWO EMERGENCY LIGHTS INOP. 2L74 4F4 FRTA20WE E24NE 20050818000602005081800060NM 2005 8 18 2005UALA00807 120050811A3350 LIGHT BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE SEAT 3F DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29782UA 26948 AFT EEL LIGHT AT 3F RIPPED OUT OF SEAT. REPLACED LIGHT ASSY. 2L72 4F4 FRTT0001SE E46NE 20050818000612005081800061NM 2005 8 18 2005UALA00808 120050812A335080541 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE MID LAV INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29104UA 26902 EEL INOP AT RT AFT MOST CROSS AISLE AND CROSS AISLE MID LAVS. REPLACED LIGHT ASSY. 2L74 4F4 FRTA20WE E24NE 20050818000642005081800064NM 2005 8 18 2005UALA00811 120050811A2130 CLAMP BOEING757 757222 1384956NM PWA 2037 PW2037 NE LT A/C BAY LOOSE A UALABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29546UA 25367 LOST CABIN PRESSURE. FOUND CLAMP LOOSE IN LEFT AC BAY. REPLACED NUMEROUS SEALS IN LT AND RT AC BAY. PRESSURIZED ACFT. PRESSURIZED OK . 2L72 4F4 FRTA2NM E17NE 20050818000712005081800071EU 2005 8 18 AWXA200500962 120050816A3397A9299304600600 WIRE HARNESS AIRBUS320 A320231 3930325EU EMERGENCY LIGHT DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28626AW 65 ORD - EEL - DURING TEST OF EMERGENCY LIGHT SYSTEM, SEAT MOUNTED LIGHT AT SEAT ROW 9R WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT CABLE HARNESS UNDER ROW 9R. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA28NM 20050818000722005081800072NE 2005 8 18 AWXA200500963 220050815A7230 COMPRESSOR AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE NR 2 ENGINE STALLED A AWXAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 WP28631AW 077 CLE - AIR TURNBACK - FLT 281 - DURING TAKEOFF CREW REPORTED COMPRESSOR STALL ON THE NR 2 ENGINE. AIRCRAFT RETURNED TO CLE LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE IS REMOVING AND REPLACING THE NR 2 ENGINE AT THIS TIME. 2L72 4F4 FRTA28NM E311NE 20050818000742005081800074NE 2005 8 18 C7WA0500109 220050712A7261652186713 LINE BOEING727 7272M7 138407SNM PWA JT8 JT8D9A 52048NE NR 1 ENGINE LOOSE A C7WAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 SO29742RW 21952 649229 AIR TURNBACK: ENGINE SHUTDOWN, NR 1 ENGINE OIL FILTER BYPASS LIGHT CAME ON AT 8000 FT, DURING CLIMB OUT. COMPLETED PRECAUTIONARY SHUTDOWN CHECKLIST. DURING INSPECTION OF NR 1 ENGINE, FOUND LOOSE LINE B-NUT AT OIL PRESSURE SWITCH. TIGHTENED B-NUT. OPERATIONAL CHECK GOOD. (K) 2L73 4F4 F A3WE E2EA 20050818000752005081800075EA 2005 8 18 A6WA200560016 220050714A732177390025 FUEL CONTROL BAG BAE146BAE146200A 1500266EU LYC ALF502ALF502* 41580EA NR 1 ENGINE UNSERVICEABLE A A6WAEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 GL31179US4192 E2041 LF05390AC CLIMBING THRU 9000 FT NR 1 ENGINE STARTED TO WIND DOWN. BOTH N1 AND N2 WERE DROPPING, TGT APPEARED TO BE RISING. SECURED ENGINE, PERFORMED IMMEDIATE ACTION CHECKLIST C/W QRH. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE. (K) 2H74 4F4 FRTA49EU E6NE 20050818000762005081800076EU 2005 8 18 A6WA200560017 120050730A492038000864 APU BAG BAE146BAE146200A 1500266EU LYC ALF502ALF502R5 41580NE APU BAY BIRD INGESTION A A6WAK NONE BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION ININSP/MAINT 1 GL31610AW12307 E2082 SMOKE IN CABIN WHEN TURNING ON PACKS. MAINTNANCE C/W EO, BOTH AC PACKS. FOUND BIRD AND OIL IN APU INTAKE. REMOVED AND REPLACED APU, BOTH AC PACKS, JET PUMPS AND WATER INJECTOS IAW EO, SYSTEM OPS CHECK GOOD. (K) 2H74 4F4 FRTA49EU E6NE 20050818000792005081800079NM 2005 8 18 USAA050919 120050729A5320141N516139 CHANNEL BOEING757 7572B7 1384964NM RROYCERB211 RB211535* NE STA326,RBL43 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19628AU 27806 BFM - C3 - U CHANNEL, 1.2 INCH X 1 INCH CRACK, STA 326, RBL43 INCH. REPLACED FLOOR SUPPORT U CHANNEL IAW SRM. (K) 2L72 4F4 FRTA2NM E12EU 20050818000812005081800081EU 2005 8 18 ALG2005F00057 120050730A7712 INDICATOR UROCOPEC120 EC120B 8680987EU TMECA ARRIUSARRIU2F NE TORQUE MALFUNCTIONED E ALGAA UNSCHED LANDING N FALSE WARNING HOHOVERING 1 SW03511AL 1252 AT HOVER, A GUST OF WIND HIT THE AC REQUIRING MORE RT PEDAL AS A RESULT THE TORQUE REACHED 111 PERCENT FOR 1 SECOND. THE TAKEOFF WAS ABORTED AND MAINTENANCE WAS NOTIFIED. THE MECHANIC INSPECTED THE T/R GB, T/R DRIVE SHAFT DISC PACKS AND BEARINGS ALSO INPUT DRIVE SHAFT DISC PACKS AND T/R GB CHIP PLUG, NO DEFECTS WERE NOTED AND THE AC WAS RETURNED TO SERVICE. (K) 1G72 3U3 UNCR0001RD E34NE 20050818000862005081800086SW 2005 8 18 ALG2005F00046 120050725A760304638C80Z382 THROTTLE CABLE BELL 206 206L1 1182107SW ALLSN 250C 250C28B 03013GL SEVERED A ALGAO OTHER O OTHER NRNOT REPORTED 1 SW031067D 45435 UPON LANDING, FOR CARGO TRANSPORT, THROTTLE WAS REDUCED TO FLIGHT IDLE BUT ENG RPM STAYED THE SAME, THROTTLE WAS OPENED AND CLOSED SEVERAL TIMES WITH NO EFFECT ON ENG RPM. FINALLY, PILOT SHUT ENGINE OFF BY TURNING THE MAIN FUEL SHUT OFF AND NOTIFIED MAINTENANCE. MECHANIC, UPON INSPECTION, DISCOVERED THAT INNER CABLE WS SEVERED 2 FT FROM THE THROTTLE IN THE COCKPIT. REMOVED AND REPLACED THE CABLE AND THE AC WAS RETURNED TO SERVICE UPON COMPLETION OF FUNCTION CHECKS IAW MM. (K) 1G71 3U3 U H2SW E1GL 20050818000922005081800092EU 2005 8 18 KBM2005F00185 120050404A801201740078030 DRAIN VALVE SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE START DRAIN LEAKING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1937SH 2300 START/ DRAIN VALVE, LEAKING EXTERNALLY. REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20050818000932005081800093SW 2005 8 18 KBM2005F00188 120050728A2432MS24171D1 RELAY BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL BATTERY INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1973DP 28 2513 BATTERY RELAY INOPERATIVE, REMOVED AND REPLACED. (K) 1G71 3U3 U H2SW E4CE 20050818001012005081800101CE 2005 8 18 TZR2005F00027 120050304A3210 TORQUE LINK CESSNA401 401A 207590DCE CONT O520 TSIO520EB 17040SO MCAULY3AF32C3AF32C* GL LANDING GEAR CRACKED E TZRAO OTHER O OTHER NRNOT REPORTED 1 SW05409TE 401A0118 THE LT AND RT MLG HAD CRACKS ON THE BOSS AREA WHERE THE TORQUE LINKS ATTACH. THE CRACKS WERE ABOUT .2500 INCH LONG AND LOCATED NEXT TO WHERE THE BOSS CONNECTS TO THE TUBE. (K) 1L72 3O3 O A7CE E8CE 5 CP22EA 20050818001042005081800104GL 2005 8 18 ALG2005F00053 220050725A7321 FUEL CONTROL BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL ENGINE OUT OF RIG E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW0335WH 2736 DURING RUN UP THE ENGINE FLAMED OUT, THE PILOT NOTIFIED MAINTENANCE. THE MECHANIC UPON TROUBLESHOOTING FOUND THE FUEL CONTROL OUT OF RIG. HE RIGGED THE FUEL CONTROL IAW MM AND AC WAS RETURNED TO SERVICE UPON COMPLETION OF FUNCTION CHECKS. (K) 1G71 3U3 U H2SW E4CE 20050818001052005081800105CE 2005 8 18 ALG2005F00054 120050727A321213AT2 SWITCH CESSNASTC STC206C 1182107CE ALLSN 250C 250C28B 03013GL FLOAT SYSTEM FAILED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW031078N 45389 DURING RUN UP THE FLOAT WOULD NOT ARM, THE PILOT SHUT THE AC DOWN AND NOTIFIED MAINTENANCE. THE MECHANIC REMOVED AND REPLACED THE FLOAT ARM SWITCH AND THE AC WAS RETURNED TO SERVICE UPON COMPLETION OF THE FUNCTION CHECKS. (K) 1H71 3O3 UNTA4CE E1GL 20050818001092005081800109 2005 8 18 KBM2005F00186 420050415A3421AR850 ENCODER BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL ALTITUDE IDICATOINOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19667JM 3444 ALTITUDE ENCODER, INOPERATIVE, REMOVED AND REPLACED. (K) 1G71 3U3 U H2SW E4CE 20050818001112005081800111NM 2005 8 18 USAA050917 120050729A5330T20243100C SKIN BOEING757 7572B7 1384964NM RROYCERB211 RB211535* NE STA1316STR29-30RCORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19628AU 27806 BFM - SKIN - 2 INCH X 2 INCH X .022 INCH D - CORROSION; NO TASK OR LEVEL STA 1316, BET STR 28R AND 30, REPAIRED 1AW SRM AND EA. (K) 2L72 4F4 FRTA2NM E12EU 20050818001142005081800114NE 2005 8 18 ALG2005F00055 220050727A73202319928930 FUEL CONTROL UROCOPEC120 EC120B 8680987EU TMECA ARRIUSARRIU2F NE ENGINE MALFUNCTIONED E ALGAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 SW03515AL 1165 IN CRUISE FLIGHT, THE TURBINE SURGED WHICH WAS CONFIRMED WITH ENGINE NOISE LEVEL CHANGE. UPON LANDING THE MECHANIC REMOVED AND REPLACED THE FUEL CONTROL AND THE AC WAS RETURNED TO SERVICE UPON COMPLETION OF ALL FUNCTION CHECKS IAW MM. (K) 1G72 3U3 UNCR0001RD E34NE 20050818001172005081800117NM 2005 8 18 ASAA0540347 120050706A531466232541 KEELBEAM BOEING737 7374Q8 138447QNM FS 807 DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 YXX - FOUND AFT CARGO PIT LEFT KEEL BEAM STRINGER 27L, INBOARD ATTACH ANGLE MISSING. FABRICATED AND INSTALLED REPAIR PARTS IAW B737-400 SRM 51-30-01. (M) 2L72 4F RTA16WE 20050818001192005081800119NM 2005 8 18 ASAA0540345 120050706A57536546435282 SKIN BOEING737 7374Q8 138447QNM TE FLAP DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 YXX - FOUND RIGHT OUTBOARD AFT FLAP HAS DELAMINATION ON THE UPPER AND LOWER SURFACES. REMOVED AND REPLACED RIGHT OUTBOARD FLAP IAW B737-400 AMM 27-51-39. (M) 2L72 4F RTA16WE 20050818001222005081800122NM 2005 8 18 ASAA0540346 120050706A575365C3262012 SKIN BOEING737 7374Q8 138447QNM FORE FLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 YXX - FOUND RIGHT INBOARD FORE FLAP LOWER SIDE DENTED MID-SPAN. RIGHT INBOARD FORE FLAP LOWER SIDE REPAIRED IAW B737-400 SRM 51-70-10 REPAIR NR 7. (M) 2L72 4F RTA16WE 20050819000022005081900002NM 2005 8 19 ASAA0540299 120050626A5310693725310 BEAM BOEING737 7374Q8 138447QNM FS 685 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 OKC - THE STUB BEAM 69-37253-10 WAS FOUND TO BE CRACKED AT UPPER CORNER OUTBOARD SIDE DURING 685 FRAME REPLACEMENT. TRIMMED OUT DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED IAW BOEING FAILED REWORK RECORD DD2 UNDER BOEING REPAIR AGREEMENT NR 6-1171-RE-01389. (M) 2L72 4F RTA16WE 20050822000022005082200002EU 2005 8 22 USAA050974 120050804A53151161201 FLOORBEAM AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE FWD FR 66-68 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19109UW19030 1065 PIT - S2 - FLOORBEAM, .5 INCH X .5 INCH AND 3 INCH X 2.5 INCH, CORROSION; LEVEL 1; TASK JA260-53500, FWD OF FRA 66-68, 30 INCHES LT OF CTR. REMOVED AND REPLACED BEAM. DEFECTIVE PART REPLACED WITH IDENTICAL PART. (K) 2L72 4F4 FRTA28NM E38NE 20050822000042005082200004EU 2005 8 22 USAA050982 120050805A5315D5347218820400 FLOORBEAM AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE FR 64-70 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19110UW13254 1112 PIT - S2 - FLOORBEAM, 2 INCH X 96 INCH, CORROSION; LEVEL 1; TASK JA-260-53500, FLOOR SUPPORT FR 64-70 IB AFT ENTRY DOOR. DEFECTIVE PART REPLACED WITH IDENTENTICAL PART IAW SRM. (K) 2L72 4F4 FRTA28NM E38NE 20050822000062005082200006EU 2005 8 22 USAA050979 120050805A5315D5311278220201 FLOORBEAM AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE Y765, C16,C20 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19110UW13254 1112 PIT - S2 - FLOORBEAM, 1 IN DIA AND .7500 INCH DIA AREA, CORROSION; LEVEL 1; TASK JA-220-53500, FLOORBEAM AT Y765 BETWEEN C16 ADN C20. DEFECTIVE PART REPLACED WITH IDENTICAL PART IAW SRM. (K) 2L72 4F4 FRTA28NM E38NE 20050822000092005082200009EU 2005 8 22 USAA050975 120050805A5315D5311282600101 FLOORBEAM AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE FR C16, 20 IN LTCORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19110UW13254 1112 PIT - S2 - FLOORBEAM, 2 INCH X 3 INCH CORROSION, LEVEL 2; TASK: JA-220-53500 20 INCH LT OF CENTER AT FRAME C-16. REMOVED AND REPLACED IAW SRM. (K) 2L72 4F4 FRTA28NM E38NE 20050822000182005082200018NE 2005 8 22 KBM2005F00199 220050506A73205529 BEARING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1B 6OO30NE FCU THROTTLE WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH 2337 FUEL CONTROL THROTTLE CABLE BEARING WORN. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050822000202005082200020NE 2005 8 22 KBM2005F00205 220050420A7200 BEARING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE ENGINE DIRTY E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19351WM 2167 REMOVED ENGINE ASSEMBLY FOR CHIP LIGHT EVACUATION. ENGINE REAR BEARING CLEANED, RIGGED NR1 AND N2 REPLACED WITH NEW OIL. PERFORMED GROUND RUN OPS CHECKED GOOD. (K) 1G71 3U3 U H9EU E19EU 20050822000262005082200026EU 2005 8 22 KBM2005F00208 120050416A6410355A09103601 BEARING SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1D NE TAIL ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1953SH 2009 HALF SHELL LAMINATED BEARINGS, WORN BEYOND LIMITS. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050822000322005082200032 2005 8 22 KBM2005F00213 420050523A3452066106200 TRANSPONDER BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL LORAN SYS INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1973DP 2513 TRANSPONDER SHOWING 5272 IN CONTROL TOWER WHEN SET ON 5252 IN AIRCRAFT. REMOVED AND REPLACED. (K) 1G71 3U3 U H2SW E4CE 20050822000372005082200037NM 2005 8 22 ASAA0540322 120050626A532066232541 ANGLE BOEING737 7374Q8 138447QNM FS 807 MISSING A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 YXX - AFT CARGO PIT KEEL BEAM (STR 27L) INBOARD ATTACHED ANGLE MISSING AT BS 807. REPLACED ANGLE WITH FABRICATED REPAIR PART. (M) 2L72 4F RTA16WE 20050822000382005082200038NM 2005 8 22 ASAA0540348 120050706A5320654653170 ANGLE BOEING737 7374Q8 138447QNM BS 500C CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 YXX - FOUND BS 500C STRINGER 27R TO 28R SKIN TO FRAME ATTACHMENT CORRODED. FABRICATED AND REPLACED REPAIR PART IAW B737-400 SRM 53-00-07 FIGURE 203. (M) 2L72 4F RTA16WE 20050822000482005082200048NM 2005 8 22 ASAA0540326 120050626A53106546531 SHEAR TIE BOEING737 7374Q8 138447QNM FS 500A CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 YXX - FOUND BS 500E CORROSION ON SKIN TO FRAME ATTACHMENT AT STRINGER 27 AND 28 LEFT. BLEND AND CHECK LIMITS REPAIRED IAW 737-400 SRM 53-00-07 FIG 203. (M) 2L72 4F RTA16WE 20050822000592005082200059EA 2005 8 22 2005F00092 220050809A853076620 STUD PIPER PA31 PA31325 7103105SO LYC O540 TIO540F2BD 41532EA NR 2 CYLINDER BROKEN E A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CLCLIMB 1 GL254503L 473 318012031 L683261A AFTER DEPARTURE, @ APPROX 500'AGL, ENGINE LOST POWER. THROTTLE REDUCTION TO 31"MP, RAN SMOOTHLY. RETURN FOR LANDING, DISCOVER 7 OF #2 CYLINDER HOLD DOWN STUDS BROKEN 1L72 3O3 O A20SO E14EA 20050822000702005082200070NM 2005 8 22 SWAA052468 120050817A335057771 CAP BOEING737 7377H4 1384404NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29456WN 32463 EEPLS FWD END CAP BROKEN. REMOVED AND REPLACED END CAP PER MM. 2L72 4F RTA16WE 20050822000762005082200076NM 2005 8 22 DU4R0508178 120050809A5230 SKIN BOEING757 757232 1384965NM CARGO DOOR CORRODED B DU4RK NONE O OTHER ININSP/MAINT 1 SO15624DL 22914 CORROSION ON BELLY SKIN JUST AFT OF MEC DOOR. 2L72 4F RTA2NM 20050822000982005082200098WP 2005 8 22 IXXA05RNG026S 120050721A5740 SUPPORT FITTING DOUG DC8 DC862F 3021972WP XF 219.498 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW1171CX 670243317 45961 DURING ROUTINE "C" CHECK, RT WING INBOARD FLAP SUPPORT FITTING STA XF219.498 WAS FOUND CRACKED (1.599"). REPAIR ACCOMPLISHED, STOP HOLES WERE DRILLED, ANGLE WAS FABRICATED AND INSTALLED IAW EWO ATI 57-017 & EO ATI-070305. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR. 2L74 4F 4A25 20050822001012005082200101WP 2005 8 22 IXXA05RNG047S 120050717A5246 DOOR DOUG DC8 DC862F 3021972WP FUEL CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW1171CX 670243317 45961 DURING A ROUTINE C CHECK INSPECTION A CRACK WAS FOUND AT FUEL ACESS DOOR 506B LH. CORRECTIVE ACTION: ACCESS DOOR # 506B WAS REPAIRED IAW EWO ATI 57-026 & SRM 57-2-1 FIGURE 43. 2L74 4F 4A25 20050822001042005082200104WP 2005 8 22 IXXA05RNG029S 120050721A5740 SUPPORT FITTING DOUG DC8 DC862F 3021972WP ZONE 600 CRACKED B IXXAO OTHER O OTHER ININSP/MAINT 1 SW1171CX 670243317 45961 DURING ROUTINE "C" CHECK, RT WING INBOARD FLAP SUPPORT FITTING STA XF 339.723 WAS FOUND CRACKED (0.703"). REPAIR ACCOMPLISHED, STOP HOLE WAS DRILLED, ANGLE WAS FABRICATED AND INSTALLED IAW EWO ATI 57-019 & EO ATI-070505. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR. 2L74 4F 4A25 20050822001052005082200105WP 2005 8 22 IXXA05RNG030S 120050721A5740 SUPPORT FITTING DOUG DC8 DC862F 3021972WP XF 409.664 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW1171CX 670243317 45961 DURING ROUTINE "C" CHECK, RT WING INBOARD FLAP SUPPORT FITTING STA XF 409.664 WAS FOUND CRACKED (LONG: 3.178"). REPAIR ACCOMPLISHED, STOP HOLE WAS DRILLED, ANGLE WAS FABRICATED AND INSTALLED IAW EWO ATI 57-020 & EO ATI-070605. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR. 2L74 4F 4A25 20050822001082005082200108NE 2005 8 22 200513 220050804A732078639110 HYDROMECH UNIT DHAV DHC8 DHC8103 1386005NM PWA PW121 PW121 52124NE ZONE 500 UNKNOWN A KPVAC ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 WP13806WP 357 PCE120086 ON TAKEOFF ROLL, ABORTED DUE TO NR 1 ENGINE NOT PRODUCING TAKEODD POWER. NR 1 PROP AT 900 AND NR 2 PROP AT 1200 RPM. NR 1 TORQUE AT 40% AND NR 2 @ 60%. REMOVED AND REPLACED HMU/EDP IAW PWC 72-01-40 SEC. 5 PAR. A-D. NO DEFECTS NOTED. 2H72 4T4 TRTA13NM E20NE 20050822001092005082200109EU 2005 8 22 2005080501 120050805A2120 SMOKE EMB ERJ170ERJ170100LR EU CABIN DETECTED A UHLAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 GL17631RW 17000007 ON 08-05-2005, FLT 7587 ORF-ORD, CREW REPORTS THAT ON DESCENT THAT THEY HAD SMOKE IN THE CABIN. 2L74 4F RTA56NM 20050822001102005082200110EA 2005 8 22 VTZA200500142 120050805A531260034017595 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27620BR 7179 RT SIDE PILOTS BULKHEAD AT FS 280 RBL 9.0 IS CRACKED AT 1.0" IN WEB RADIUS 2L72 4F RTA21EA 20050822001242005082200124WP 2005 8 22 IXXA05SMN137S 120050630A5730 SKIN DOUG DC8 DC871F 302199DWP XF226.000 WORN B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, RT OTBD FLAP FWD UPPER PLATING WORN, STA XF 226.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05258 DATE 06-24-05, SEMAN DWG ED 4005 DATE 06-20-05, EO SEMAN 2005913 DATE 06-24-05. REMOVED FASTENERS IAW DC-8 SRM 51-3-0 PAGE 1, C-8 SRM 51-1-21 PAGE 1, DC-8 SRM 51-1-20D PAGE 21. REMOVED DAMAGED PLATING IAW SEMAN DWG ED 4005, PERFORMED NDT INSPECTION. IAW DC-8 NDT SPM PART 06-10-01-001. NO CRACK, NO CORROSION FOUND. FABRICATED NEW PLATING SEGMENT + INTERNAL SPLICE + EXTERNAL DOUBLERS IAW SEMAN DWG ED 4005, DC-8 SRM 51-1-4 PAGE 1. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS INTERNAL PART IAW DC-8 SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW DC-8 S2L74 4F RT4A25 20050822001252005082200125WP 2005 8 22 IXXA05SMN141S 120050630A5730 SKIN DOUG DC8 DC871F 302199DWP XFS-11.250-23.75DEFORMED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, LT WING INBD L/E UPPER SURFACE DEFORMED, STA XFS -11.250 TO XFS -23.750. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 05259, SEMAN DWG ED 4016, EO SEMAN 2005948. 2L74 4F RT4A25 20050822001262005082200126WP 2005 8 22 IXXA05SMN149S 120050630A5730 SKIN DOUG DC8 DC871F 302199DWP XW131.000 DENTED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, LH INBD FLAP UPPER PART DENTED, XW 131.000 PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-1-0 PAGE 1, DC-8 SRM 57-7-1 FIG. 1, EO SEMAN Nº 20051010 DATE 06-28-05. REMOVED DAMAGED PLATING IAW DC-8 SRM 51-1-21 PAGE 1. FABRICATED NEW PLATING (ALCLAD 2024 T3 0.025”) + BONDED DOUBLER (ALCLAD 2024 T3 0.020”) IAW DC-8 SRM 57-7-1 FIG. 1 ITEM “A”, “L”. CLEANED, TREATED AND PRIMED AREA + REPAIR PARTS INTERNAL PART IAW DC-8 SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11 PAGE 9 BONDED DOUBLER. IAW DC-8 SRM 51-1-9 (HYSOL). INSTALLED NEW PANEL IAW DC-8 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050822001312005082200131EU 2005 8 22 RAIA00508007 120050805A243651539019E GCU JETAIRJETSTMJETSTM4101 1500501EU NR 1 MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03569HK2938 41088 FLT 5437 - STL - LEFT GENERATOR FAILURE INDICATION. MAINTENANCE REMOVED AND REPLACED NR 1 GENERATOR CONTROL UNIT. 2L72 4T RTA41NM 20050822001322005082200132SO 2005 8 22 RAIA00508008 120050806A3260 PROXIMITY SWITCH EMB 145 EMB145ER 3260211SO MLG UNKNOWN A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03808HK 145157 FLT 3587 - PVD - LANDING GEAR WILL NOT RETRACT. MAINTENANCE PERFORMED MULTIPLE LANDING GEAR OPERATIONAL CHECKS; INSPECTED PROX SWITCHES BUT WERE UNABLE TO DUPLICATE MALFUNCTION. 2L72 4F RTT00011AT 20050822001352005082200135WP 2005 8 22 ABXA050183 120050808A2131 RELAY DOUG DC9 DC941 302207NWP CABIN PRESSURE INOPERATIVE A ABXAB EMER. DESCENT J WARNING INDICATION CLCLIMB 1 GL23990AX 47493 LOST PRESSURIZATION AT FL 290. PRESSURE CONTROLLER WOULD NOT LOCK. DESCENDED TO 2000, GAINED MANUAL CONTROL. DECLARED AN EMERGENCY. TROUBLESHOOTING DISCOVERED R2-55 RELAY TO BE BAD, REPLACED RELAY. ALSO REPLACED R20227. REPLACED LEFT GROUND SHIFT RELAY R2-4. PERFORMED ADJUST/TEST OF CABIN PRESSURE CONTROL IAW DC-9 AMM 21-32-00, PAGE A & B THROUGH COMPLETION. ALL OPS CHECKED GOOD. SEE WORK PACK 2005990 FOR WORK ACCOMPLISHED. 2L72 4F A6WE 20050822001372005082200137EU 2005 8 22 USAA050892 120050718A5315D5347209001100 FLOORBEAM AIRBUS320 A320214 3930316EU FS 64-69 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19109UW19030 1065 PIT - FOUND FLOORBEAM CORRODED 1 INCH BY 2 INCH ON EACH OF THREE BEAMS, FRAME 64-69, 50 INCHES RIGHT OF CENTER. REMOVED AND REPLACED WITH IDENTICAL PART PER SRM 51-72-11. CORROSION LEVEL 2, TASK JA-260-53500. (M) 2L72 4F RTA28NM 20050822001402005082200140NE 2005 8 22 XN0A1255 220050811A7320 COMPRESSOR AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE NR 2 ENGINE STALLED A XN0AA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 GL23370PC 134 AFTER TAKEOFF NR 1 ENG BEGAN COMPRESSOR STALLING AT 700 FT AGL. (ORIG/OPEN) 2L72 4F4 FRTA35EU E23EA 20050822001412005082200141NE 2005 8 22 V0DR200500001 320050804A6111 BEARING RACE HARTZL BEECH 1900 1900D 1154162CE HARTZLHCE4A HCE4A3A NE PROPELLER ASSY BROKEN B GLBAK NONE O OTHER ININSP/MAINT 1 NM0394GL 3804 3804 HJ1755 UE94 HJ1755 DURING DISASSEMBLY FOR OVERHAUL, FOUND NR 2 AND NR 3 BLADE BEARING RACES CRACKED AND BROKEN. HUB SIDE RACES (P/N) D-7745-A (S/NS) A059 & A075. BLADE SIDE RACES (P/N) D-7745-B (S/NS) A417 & A453. 2L72 4T RTA24CE 5 CP10NE 20050822001422005082200142WP 2005 8 22 ASMF200508005 120050810A2420696233B CSD DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE LEFT MALFUNCTIONED W ASMFB EMER. DESCENT M OVER TEMP CRCRUISE 1 SW23583MD443122868 49659 718220 AIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT HMO AS CONSEQUENCE OF OVERTEMPERATURE ON LEFT CONSTANT SPEED DRIVE (CSD). LEFT CHIP DETECTORS WERE CHECKED, ALL CORRECT. CSD WAS DETECTED OVERFILLED. CSD WAS DRAINED UNTIL CORRECT LEVEL AND LEFT ENGINE RUN WAS CORRECT. CSD TEMPERATURE WAS CORRECT. DURING OVERNIGHT SERVICE, CSD, SEAL, AND HEAT EXCHANGER WERE REPLACED IAW MM 24-10-01, 72-61-59 AND 24-10-03, RESPECTIVELY, TESTED CORRECT. 2L72 4F4 FRTA6WE E9NE 20050822001432005082200143NE 2005 8 22 08082005J 220050808A7200 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LEFT FLAMED OUT A NSVAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 EA27304CE 198 785213 DISCREPANCY: LH ENGINE HAD MOMENTARY FLAMEOUT INFLIGHT AT 21000FT. AND -11 DEGREES PERFORMED BORESCOPE INSPECTION, NO DEFECTS NOTED 2L72 4T4 TRTA52EU E8NE 20050822001462005082200146NM 2005 8 22 05065 120050811A2120 SMOKE BOEING747 747122 1384872NM COCKPIT DETECTED A KCSAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL23716CK 19753 AFTER T/O SMELLED SMOKE BACK SIDE OF P6 PANEL. NO VISUAL - CLEARED ON CLIMB OUT. FOUND AND CLEANED LINT AND DUST. AIRCRAFT REMAINED POWER FOR SEVERAL HOURS ON GROUND. NO SMOKE SMELL NOTICED. 2L74 4F A20WE 20050822001482005082200148NM 2005 8 22 SWAA052475 120050815A53306545776 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947.5, STR 21R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050822001502005082200150NM 2005 8 22 SWAA052480 120050817A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29339SW 24090 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 945.5, STR 25R. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050822001512005082200151NM 2005 8 22 SWAA052481 120050818A55536546874 FITTING BOEING737 7373H4 1384600NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29612SW 27930 DURING SCHEDULED D-CHECK, FOUND LT & RT VERTICAL STAB FWD & AFT FAILSAFE CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER. 2L72 4F RTA16WE 20050822001532005082200153NM 2005 8 22 SWAA052483 120050818A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29617SW 27700 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIES CORRODED AT BS 727E, LBL 9 & LBL 19. REMOVED AND REPLACED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20050822001612005082200161EA 2005 8 22 COMA0560426 120050804A5210601R386317 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR LATCH WORN A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01716CA 7250 FLIGHT 5486 - DURING CLIMBOUT OF HSV RECEIVED A CABIN DOOR WARNING CAUTION MESSAGE. FLIGHT RETURNED TO THE FIELD. REPLACED THE OUTER CABIN DOOR HANDLE LATCH BASE LOWER ASSEMBLY. 2L72 4F RTA21EA 20050822001652005082200165EA 2005 8 22 COMA0560431 120050805A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA CONNECTOR LOOSE A COMAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01973CA 7146 FLIGHT 5890 - EMERGENCY FLOOR LIGHTS INOP AT ROWS 7/8. REPAIRED LOOSE WIRE CONNECTIONS. 2L72 4F RTA21EA 20050822001672005082200167EA 2005 8 22 COMA0560435 120050808A2610356024310 ELEMENT CNDAIRCL600 CL6002B19 1900309EA LT PYLON MALFUNCTIONED A COMAO OTHER J WARNING INDICATION DEDESCENT 1 SO01965CA 7131 FLIGHT 5105 - LT 14TH STAGE DUCT WARNING. REPLACED THE PYLON DUCT LEAK SENSING ELEMENT. 2L72 4F RTA21EA 20050822001682005082200168EA 2005 8 22 COMA0560432 120050806A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01518CA 7816 FLIGHT 5660 - FLAPS FAIL. INSPECTED FLAPS IAW AD 98-20-01. 2L72 4F RTA21EA 20050822001722005082200172EA 2005 8 22 COMA0570094 120050805A532067053110521 WEB CNDAIRCL600 CL6002C10 1390015EA FS 280 CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01331CA7693 10061 THE LT AND RT LOWER WEBS BELOW THE FLOOR AT FS 280 ARE CORRODED FROM LBL 36 TO RBL 36. REMOVED THE CORRODED WEBS AND INSTALLED NEW WEBS IAW REO 670-53-11-052 REV A. 2L72 4F RTA21EA 20050823000042005082300004EA 2005 8 23 COMA0560438 120050810A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ACTIVATED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01409CA 7441 FLIGHT 5243 - RT THRUST REVERSER UNLOCKED MESSAGE. CND FOUND NO DEFECTS WITH RT THRUST REVERSER. 2L72 4F RTA21EA 20050823000132005082300013NM 2005 8 23 SWAA052491 120050817A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 737E, STR 22L. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050823000142005082300014 2005 8 23 SWAA052492 420050816A2565D31354 SLIDE BOEING737 7373TO 138447GNM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29697SW 23838 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20050823000232005082300023NM 2005 8 23 AALA20050531 120050818A3350 BATTERY PACK BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21680AN 29590 DFW - EMERGENCY EXIT SIGN LIGHT AT THE L764 CLASS DIVIDER AT STATION 647 INOPERATIVE. REPLACED THE BATTERY PACK AND CHARGER ASSEMBLY M731 FOR EMERGENCY EXIT SIGN LIGHT AT THE L764 DIVIDER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050823000252005082300025NM 2005 8 23 AALA20050537 120050808A5414 SKIN BOEING767 767223 1385123NM LT PYLON DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21322AA 22323 AFW - LT PYLON INBOARD SIDE STRUT SKIN HAS GOUGE WHICH WAS REWORKED BEYOND LIMIT. DAMAGE WAS INDUCED BY INTERFERENCE FROM THE UPPER FIRE SEAL BRACKET. BLENDED DAMAGE AT SINGLE FASTENER LOCATION. PERFORMED HIGH FREQUENCY EDDY CURRENT INPSECTION. INSTALLED NEW FASTENER AND REMOVED THE SOURCE OF WEAR BY TRIMMING BRACKETS. RESTORED FIRE SHIELD. 2L72 4F RTA1NM 20050823000272005082300027NM 2005 8 23 AALA20050536 120050810A5314 KEELBEAM BOEING767 767223 1385123NM BS 790 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21322AA 22323 AFW - RIGHT HAND KEEL BEAM OUTBOARD FLANGE AT STATION 790 HAD FLANGE REMOVED DUE TO CORROSION. A 3.6 INCH BY 1 INCH SECTION OF KEEL BEAM CHORD FLANGE WAS REMOVED AT APPROXIMATELY STATION 790. PERFORMED OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION ON ALL REMOVED FASTENER HOLES. PERFORMED EDDY CURRENT INSPECTION ON EDGES AND BLENDS TO VERIFY CORROSION COMPLETELY REMOVED. ROTOPEEN EDGES AND BLENDS IN AREA OF THE CUTOUT. FABRICATED A REPAIR ANGLE FROM 7075 T6511 EXTRUSION. FABRICATED FILLER FROM 7075 T6 AND INSTALLED ANGLE AND FILLED WET WITH SEALANT AND FASTENED WITH BACB30MY6. HI-LOKS AND FASTENERS INSTALLED WET MAINTAINING 1.7 DIAMETER EDGE DISTANCE. APPLIED CORROSION INHIBITING COMPOUND. 2L72 4F RTA1NM 20050823000332005082300033EA 2005 8 23 COMA0560449 120050816A5210 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA PAX DOOR FALSE ACTIVATIONA COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01716CA 7250 FLIGHT 5298 - CABIN DOOR OUTER HANDLE CAUTION. CND, FOUND NO DEFECTS WITH DOOR. 2L72 4F RTA21EA 20050823000352005082300035EA 2005 8 23 COMA0560450 120050817A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA LEFT MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01976CA131381516 7151 FLIGHT 5637 - FLAPS FAIL CAUTION. REPLACED THE LT BPSU. 2L72 4F RTA21EA 20050823000372005082300037EA 2005 8 23 COMA0560441 120050812A2750 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS OUT OF RIG A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01814CA 7387 FLIGHT 5207 - FLAPS FAIL CAUTION. RE-RIGGED LT AND RT BPSU. SYSTEM CHECKS NORMAL. 2L72 4F RTA21EA 20050823000422005082300042NM 2005 8 23 DLM88050444 120050808A5350401631 TAIL CONE DOUG MD88 MD88 3023688NM DEPLOYED A DALAO OTHER W INADEQUATE Q C TXTAXI/GRND HDL 1 SO27948DL 49879 EMS SERVICES BLEW TAIL CONE AT PHL. REPLACED TAIL CONE. 2L72 4F RTA6WE 20050823000452005082300045NM 2005 8 23 DL764050447 120050811A2760NAS161210 SEAL BOEING767 767432ER 1385134NM SPOILER ACT DAMAGED A DALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO27839MH 29712 RT HYD QTY WAS .48 AND DROPPED TO .38. REPLACED O-RING ON SPOILER ACTUATOR. 2L72 4F RTA1NM 20050823000482005082300048NE 2005 8 23 COMA0560424 220050802A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE OVERTEMP A COMAE ENGINE SHUTDOWN MEJOVER TEMP VIBRATION/BUFFET WARNING INDICATION DEDESCENT 1 SO01442CA 7483 807582 FLIGHT 5807- LT ENGINE HIGH ITT. SHUDDER AND VIBE IN AIRFRAME. REPLACED ENGINE. 2L72 4F4 FRTA21EA E15NE 20050823000502005082300050EA 2005 8 23 COMA0560446 120050813A32304622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG UNRELIABLE A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01991CA265514585 7216 FLIGHT 5454 - GEAR DISAGREE WARNING. REPLACED THE NLG PRIORITY VALVE. 2L72 4F RTA21EA 20050823000542005082300054NM 2005 8 23 CALA0500271 120050820A5347BAC15202779 SEAT TRACK BOEING737 737824 13844BZNM STA 360 + 12 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712216 28776 INSPECTION FOUND CENTER CLOSET SEAT TRACK CORRODED AT STA 360 PLUS 12 (OUTBOARD TRACK), LBL 41 TO LBL 42. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-40-02, 53-00-52, AND AMM 20-30-11-910-801, AND 20-50-11-910-801. 2L72 4F RTA16WE 20050823000552005082300055NM 2005 8 23 CALA0500272 120050820A5320147A8540U7 THRESHOLD BOEING737 737824 13844BZNM STA 950-975 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712216 28776 INSPECTION FOUND THE L-2 DOOR THRESHOLD FRAME CORRODED FROM STA 950-975, S17L. THE L-2 DOOR THRESHOLD WAS REMOVED AND REPLACED IAW SRM 53-00-51 AND 51-40-02. 2L72 4F RTA16WE 20050823000612005082300061NM 2005 8 23 0501286717 120050618A5312 PRESSURE PANEL BOEING747 747251F 1384898NM NLG WW CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01617US 21121 DURING LINE CHECK FOUND CRACK IN RIGHT HAND NOSE WHEEL WELL SIDE PANEL WEB. REPAIRED PER EA 67-204659. 2L74 4F A20WE 20050823000622005082300062NE 2005 8 23 DJFA2005130 220050816A7200 ENGINE BEECH MU300 400A 1155402CE PWA JT15 JT15D5 52112NE RIGHT ODOR E DJFAG O2 MASK DEPLOYED B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA23696TA RK301 PCEJA0374 DURING CRUISE FLIGHT WHILE AT 28,000 FT BOTH PILOTS NOTICED A STRONG ENVIRONMENTAL ODOR IN THE COCKPIT. THE CREW DONNED OXYGEN MASKS AND REVIEWED THEIR CHECKLIST. WHEN THE LEFT CABIN PRESSURE SOURCE WAS SELECTED THE ODOR HAD IMMEDIATELY DISSIPATED. THE FLT WAS COMPLETED AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. WHILE PERFORMING A GROUND INSPECTION IT WAS NOTED THAT THE RIGHT ENGINE HAD A FISH ODOR TO IT. MAINTENANCE INSPECTED BOTH ENGINES FOR EVIDENCE OF A BIRD STRIKE. NO EVIDENCE WAS FOUND. THE ENGINES WERE OPERATED WITH THE RIGHT BLEED AIR SOURCE SELECTED AND NO ODOR WAS NOTICED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4F4 FRTA16SW E25EA 20050823000702005082300070WP 2005 8 23 UPS05845204 120050810A5712 RIB DOUG DC8 DC871F 302199DWP RT LE XFS 806 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 INSPECTION TYPE: C1, RT WING L/E LWR RIB CRACKED AT XFS 806. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 57-2-0, 51-1-20D, AND 51-1-21. 2L74 4F RT4A25 20050823000742005082300074 2005 8 23 C8GA20050017 420050817A34142083081 INDICATOR BOEING727 727223 1384074NM AIRSPEED INOPERATIVE A C8GAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO29899AA 122 22015 FLT 1828 FROM TOL TO RFD. NO #2 AIRSPEED INDICATION AT THE BEGINNING OF TAKE OFF ROLL. ABORTED TAKE OFF AND RETURNED TO GATE. REPLACED #2 AIRSPEED INDICATOR. LEAK AND OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L73 4F A3WE 20050823000802005082300080SO 2005 8 23 RAIA00508023 120050816A3230 PIN EMB 145 EMB145LR 3260212SO NLG INSTALLED A RAIAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 CE03817HK 145058 FLT 5486-STL-NOSE GEAR WOULD NOT RETRACT. MAINTENANCE REMOVED THE GEAR PIN. 2L72 4T RTT00011AT 20050823000842005082300084NM 2005 8 23 AWXA200500968 120050726A534069353654 ATTACH ANGLE BOEING737 7373Y0 1384671NM CABIN CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28334AW 23747 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED ATTACH ANGLE CRACKED FROM BS 380 TO BS 400, BL 0 IN CABIN. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT BS 380-440 IAW BOEING 737-300 SRM 51-40-02. FABRICATED REPAIR ATTACH ANGLE IAW BOEING DWG 69-35365. INSTALLED FABRICATED REPAIR PARTS AT BS 380-440 IAW BOEING 737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050823000862005082300086NM 2005 8 23 AWXA200500970 120050731A531065498843 BEAM BOEING737 7373Y0 1384671NM CABIN CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28334AW 23747 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED CORROSION ON TRANSVERSE BEAM LOCATED AT BS 967, BL 28R, AND WL 208. MAINTENANCE REMOVED CORROSION FROM BEAM AT BS 967, BL 28R, WL 208 AND FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-51-1 FIG 101. FABRICATED REPAIR ANGLES AND FILLER IAW BOEING 737-300 SRM 53-30-51-2. INSTALLED FABRICATED REPAIR PARTS AT BS 967, BL 28R, AND WL 208 IAW BOEING 737-300 SRM 53-30-51-2 FIG 202. 2L72 4F RTA16WE 20050823000912005082300091NM 2005 8 23 AWXA200500975 120050724A53306545871523 SKIN BOEING737 7373Y0 1384671NM R1 DOOR CUTOUT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28334AW 23747 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED R1 DOOR UPPER HINGE CUTOUT AT UPPER CORNER. MAINTENANCE TRIMMED OUT THE R1 DOOR UPPER HINGE CUTOUT IAW AMERICA WEST AIRLINES (AWA) ENGINEERING REPAIR (ER) NO. 03-5241-05208-ES2. FABRICATED DOUBLER AND REPLACEMENT UPPER HINGE COVER IAW AWA ER 03-5241-05208-ES2. INSTALLED REPAIR PARTS IAW AWA ER 03-5241-05208-ES2. 2L72 4F RTA16WE 20050823000972005082300097NE 2005 8 23 GLBA20050504 220050816A7200 ENGINE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE NR 1 FAILED A GLBAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM03179GL 16487 UE179 114193 LOW OIL PRESSURE WARNING INDICATOR ILLUMINATED ON NR 1 ENGINE WHILE CLIMBING THROUGH 7000 MSL IN A LEFT TURN. OIL PRESSURE DROPPED TO 0 PSI WHILE ENGINE WAS SHUT DOWN WITHIN 45 SECONDS 2L72 4T4 TRTA24CE E26NE 20050823001022005082300102NM 2005 8 23 ABXA050184 120050810A5754114T410126A SLAT BOEING767 767205 1385121NM RT WING L/E MISSING A ABXAK NONE O OTHER ININSP/MAINT 1 GL23713AX 23058 DURING INSPECTION OF AIRCRAFT AT ILN, FOUND RIGHT WING NR 12 LEADING EDGE SLAT OUTER SKIN MISSING. HONEYCOMB EXPOSED AT UPPER INBOARD SIDE, APPROXIMATELY 9.5 WIDE AND 11.0 LENGTH. REMOVED AND REPLACED NR 12 LEADING EDGE SLAT IAW B767 MM 27-81-02-4. 2L72 4F RTA1NM 20050823001102005082300110EA 2005 8 23 SWIA200515416 120050801A27515913163 DETECTOR CNDAIRCL600 CL6002C10 1390015EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07716SK1785 1785 10180 "FLAPS HALFSPEED" STATUS MESSAGE APPEARED ON GROUND. REPLACED RT INBOARD SKEW DETECTOR AND SFECU IAW AMM 27-52-05 AND 27-52-45. OPERATIONAL CHECK GOOD, PN 766389L SN 0617. 2L72 4F RTA21EA 20050823001112005082300111EA 2005 8 23 SWIA200515417 120050808A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLT SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07910SW9696 9696 7566 FLIGHT SPOILERS FAULT STATUS MESSAGE IN FLIGHT. REPLACED INBOARD PCU ON RIGHT FLIGHT SPOILER IAW MM 27-62-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050823001132005082300113EA 2005 8 23 SWIA200515419 120050813A2750855D10011 SENSOR CNDAIRCL600 CL6002B19 1900309EA SPEED BRAKE MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION LDLANDING 1 NM07930SW6767 6767 7713 FLAPS FAIL MSG DURING AFTER LANDING. REPLACED RT FLAP BPSU. OPERATIONAL CHECK GOOD IAW CRJ 200 AMM 27-51-10. 2L72 4F RTA21EA 20050823001192005082300119EA 2005 8 23 SWIA200515425 120050813A3350 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT LOOSE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07909SW 7558 EMERGENCY LIGHT STRIP ON THE FLOOR FROM EMERGENCY EXIT ROW 8 AND BEHIND DOES NOT ILLUMINATE. RESECURED CONNECTOR AT AFT END OF CABIN TRACK. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050823001212005082300121EA 2005 8 23 SWIA200515427 120050812A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07459SW6744 6744 7782 NR 2 STAB TRIM WILL NOT ENGAGE. REPLACED HSTA, AND MCU IAW 27-42-01. OPERATIONAL CHECK GOOD, PN 7062-3, SN/OFF 1067. 2L72 4F RTA21EA 20050823001222005082300122EA 2005 8 23 SWIA200515428 120050812A2781 DETECTOR CNDAIRCL600 CL6002C10 1390015EA SLATS INOPERATIVE A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07712SK 10172 SLAT FAULT STATUS MSG AT GATE. REPLACED LEFT INBOARD SLAT SKEW DETECTOR. OPERATIONAL CHECK GOOD, IAW 27-81-00. 2L72 4F RTA21EA 20050823001272005082300127NM 2005 8 23 UPS05545211 120050718A5315111N52075 FLOORBEAM BOEING757 75724APF 1384969NM CARGO BAY CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01401UP 23723 MAIN CARGO BAY BS 900 RBL 45 FLOORBEAM CORRODED. REPAIRED PER EO 05-3652. 2L72 4F RTA2NM 20050823001282005082300128NM 2005 8 23 UPS05545212 120050720A5347 SEAT TRACK BOEING757 75724APF 1384969NM MAIN CARGO DECK CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01401UP 23723 MAIN CARGO BAY BS 900 LBL 45 FLOORBEAM CORRODED. REPLACED SEAT TRACK IAW 51-40-02. 2L72 4F RTA2NM 20050823001312005082300131NM 2005 8 23 UPS05545215 120050720A5320141N525037 SHEAR WEB BOEING757 75724APF 1384969NM MCD CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01401UP 23723 CORROSION ON SHEAR WEB SURFACE FROM STA 335 TO STA 440 WL 208 FROM LBL 45 TO LBL 63. REPAIRED PER GOODRICH ER 05-3756. 2L72 4F RTA2NM 20050823001322005082300132NM 2005 8 23 UPS05545216 120050720A5347146N52205 SEAT TRACK BOEING757 75724APF 1384969NM MAIN CARGO BAY CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01401UP 23723 SEAT TRACK CORRODED BS 1540, LBL 44, WL 208. REPLACED SEAT TRACK SECTION, BS 1540 - 1550 PER SRM 53-00-52-2R 5 FIG 201. 2L72 4F RTA2NM 20050823001342005082300134NM 2005 8 23 UPS05545218 120050720A5347 SEAT TRACK BOEING757 75724APF 1384969NM BS 900 - 960 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01401UP 23723 STA 900 - 960 LBL 45 CORROSION ON UPPER FLANGE OF SEAT TRACK, SEAT TRACK WAS REMOVED AND REPLACED. 2L72 4F RTA2NM 20050823001372005082300137WP 2005 8 23 UPS05845220 120050811A53404753360U502 FITTING DOUG DC8 DC871F 302199DWP FS 822 L20L CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 FITTING CRACKED FS 822 L20L. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20050823001382005082300138WP 2005 8 23 UPS05845221 120050811A53403779659U501 FITTING DOUG DC8 DC871F 302199DWP FS 907 L8R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 LONGERON END FITTING CRACKED FS 907 L8R. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D AND 51-1-21. 2L74 4F RT4A25 20050823001402005082300140EA 2005 8 23 SWIA200515432 120050815A2721 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA RUDDER STUCK A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07945SW 7770 RUDDER TRIM STUCK. REPLACED TRIM PANEL. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050823001462005082300146SO 2005 8 23 SWIA200515438 120050815A27523430001005 ACTUATOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION LDLANDING 1 NM07393SW1153011530 120330 FLAP DISAGREEMENT DURING FLAP RETRACTION ON AFTER LANDING CHECK. "INBD" LIGHTS FLASHING. REPLACED THE LEFT INBOARD FLAP ACTUATOR IAW MM 27-50-07. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050823001492005082300149EA 2005 8 23 SWIA200515441 120050814A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07590SW 7077 PAX MAIN CABIN DOOR EMERGENCY FLOOD LIGHT HAS A BURNED OUT LIGHT BULB. RELAMPED PAX MAIN CABIN DOOR EMERGENCY FLOOD LIGHT. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050823001522005082300152EU 2005 8 23 UPS05145245 120050819A3350CM82400 LIGHT AIRBUSA300 A300F4622R 3930360EU EXIT SIGN INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01124UP 0808 COURIER ZONE LIGHTED EXIT SIGN INOP, OPS CK NORMAL. 2L72 4F RTA35EU 20050823001552005082300155WP 2005 8 23 UPS05845227 120050812A5312 BULKHEAD DOUG DC8 DC871F 302199DWP FS1766 RBL48 L11CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 AFT PRESSURE BULKHEAD CRACKED 1.5" LONG FS 1766 RBL 48 L11R. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAE DWG SRO 8530007. 2L74 4F RT4A25 20050823001592005082300159WP 2005 8 23 UPS05845233 120050811A5340SAA3779498501 FITTING DOUG DC8 DC871F 302199DWP FS 857.125 L19L CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 FRAME TO INTERCOSTAL ATTACH FITTING CRACKED AT F/S 857.125 L19L. REMOVED AND REPLACED ATTACH FITTING IAW SRM 51-1-21D AND 51-3-2. 2L74 4F RT4A25 20050823001612005082300161WP 2005 8 23 UPS05845236 120050816A53404613574 FITTING DOUG DC8 DC871F 302199DWP FS210 L7R CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 HEAVY CORROSION ON SPLICE FITTING STA 210 L7R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2L74 4F RT4A25 20050823001662005082300166WP 2005 8 23 UPS05845241 120050816A5311 FRAME DOUG DC8 DC871F 302199DWP FS 1890 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 FRAME ON 62 DOOR OPENING IS CRACKED INSIDE OPENING RT SIDE. FAB`D DOUBLER AND REPAIRED IAW SRM 53-05-01 AND 51-1-21A. 2L74 4F RT4A25 20050823001732005082300173WP 2005 8 23 05FDEA02557 120050819A5712 RIB DOUG DC10 DC1010 3022110WP LT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LT WING L/E INTERNAL STRUCTURE FOUND 1 EA ANGLE REPAIR ON RIB XORS 577. FABRICATED REPAIR ANGLE IAW SRM 57-20-00 FIG. 1 VOL.1. 2L73 4F A22WE 20050823001752005082300175WP 2005 8 23 05FDEA02559 120050819A5712 RIB DOUG DC10 DC1010 3022110WP RT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 DISCREPANCY: RH WING OUT'B L/E INTERNAL STRUCTURE FOUND 1EA ANGLE REPAIR ON RIB XORS 572. CORRECTIVE ACTION: FABRICATED REPAIR ANGLE IAW SRM 57-20-00 FIGURE 1 VOL.1. 2L73 4F A22WE 20050823001772005082300177WP 2005 8 23 05FDEA02561 120050819A5712 RIB DOUG DC10 DC1010 3022110WP RT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 RT WING OUT'B L/E INTERNAL STRUCTURE FOUND 1EA ANGLE REPAIR ON RIB AT XORS 577. FABRICATED REPAIR ANGLE IAW SRM 57-20-00 FIGURE 1 VOL.1. 2L73 4F A22WE 20050823001832005082300183WP 2005 8 23 05FDEA02567 120050819A5730 SKIN DOUG DC10 DC1010 3022110WP LT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LT WING OUT'B L/E FOUND 1EA DOUBLER REPAIR ON SKIN AT XORS 506. FABRICATED DOUBLER REPAIR IAW SRM 57-10-00 FIGURE 68 VOL.1. 2L73 4F A22WE 20050823001862005082300186WP 2005 8 23 05FDEA02570 120050819A5512 SKIN DOUG DC10 DC1010 3022110WP HORIZONTAL STAB DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 HORIZONTAL STAB CONSTANT SECTION FOUND 1EA DOUBLER REPAIR ON AFT BLKHD AT STA 2123 X=-40 RT SIDE. REPAIRED IAW SB 55A028 AND DWG SR10550007. 2L73 4F A22WE 20050823001872005082300187WP 2005 8 23 05FDEA02571 120050819A5553 ATTACH ANGLE DOUG DC10 DC1010 3022110WP VERTICAL STAB DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE RT SIDE FOUND 1EA EXTERNAL DOUBLER REPAIR. REPAIRD IAW SRM 55-20-00 FIGURE 3 VOL.1. 2L73 4F A22WE 20050823001912005082300191NM 2005 8 23 05FDEA02575 120050819A5330 SKIN BOEING727 727 UTILSYSNM ZONE 100 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479 FUSELAGE EXTERNAL SKIN DAMAGED AFT OF SECTION 41 AROUND STRINGER 19 LT, REMOVED DAMAGE FABRICATED REPAIR DOUBLER FILLER AND INSTALLED IAW SRM 53-30-3 FIG 24. PREP AND PAINTED AREA I.A.W. M/M 51-20-151-7. THIS IS A CLASS B REPAIR WITH AN INSPECTION THRESHOLD OF 45,000 CYCLES PER SRM 53-30-3 FIG 24 2L73 4J RTA3WE 20050823001922005082300192CE 2005 8 23 10506017007 120050822A5311 FRAME BEECH 1900 1900D 1154162CE FUSELAGE CORRODED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07173YV UE173 CORROSION FOUND ON INSPECTION FOR ABC STRUCTURAL FS 213.25. MORE INFORMATION TO BE ADDED AT A LATER DATE. 2L72 4T RTA24CE 20050823001942005082300194NM 2005 8 23 05FDEA02546 120050819A57536521795284 STIFFENER BOEING727 727200 138407ENM RT WING CUT A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 RT WING NR 5 FLAP TRACK FAIRING STIFFNER IS CUT. REMOVED AND REPLACED STIFFNER IAW SRM 51-30-2 2L73 4F RTA3WE 20050818000892005081800089SW 2005 8 18 KBM2005F00187 120050301A6210206010200133 BLADE BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL MAIN ROTOR DEBONDED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1973DP 1384 2513 MAIN ROTOR BLADE, UPPER DOUBLER DEBONDING. REPAIRED BY ROTOR BLADES, INC. (K) 1G71 3U3 U H2SW E4CE 20050818000982005081800098SO 2005 8 18 TZR2005F00028 220050712A8530AEC520TI CYLINDER CESSNA401 401A 207590DCE CONT O520 TSIO520EB 17040SO MCAULY3AF32C3AF32C* GL NR 5 CRACKED E TZRAO OTHER O OTHER NRNOT REPORTED 1 SW05409TE645 401A0118 RT ENGINE NR 5 CYLINDER. LOW COMPRESSION. (K) 1L72 3O3 O A7CE E8CE 5 CP22EA 20050818000992005081800099NM 2005 8 18 C7WA200500111 120050722A3230 LANDING GEAR BOEING727 7272K5 138004PNM PWA JT8 JT8D17 52049NE MALFUNCTIONED A C7WAO OTHER O OTHER NRNOT REPORTED 1 SO29909PG 21852 AIR RETURN, UNABLE TO RETRACT MAIN LANDING GEAR. PERFORMED GEAR SWING AND MANUAL EXTENSION OF LANDING GEAR IAW MM. MAIN LANDING GEAR OPERATES NORMAL, NO DEFECTS NOTED. (K) 2L73 4F4 FRTA3WE E2EA 20050818001122005081800112EU 2005 8 18 KMB2005F00000 120050723A2910704A34240015 ACCUMULATOR SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1D1 NE HYD SYSTEM LEAKING A KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P 2342 ACCUMULATOR, DURING HYDRAULIC TEST, ACCUMULATOR LEAKED. REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20050818001132005081800113 2005 8 18 KBM2005F00192 420050722A34225050010902 GYRO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE DIRECTIONAL SPINNING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19966SH744 3787 DIRECTIONAL GYRO, UNIT SPINS EVERY 5 MINUTES, IN FLIGHT. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050822000082005082200008EA 2005 8 22 A6WA200540237 120050713A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT FS 280 CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31409AW 7447 LT FS 280.00 AT LBL 9 IB CLIP ANGLE IS CRACKED .5 INCH LONG. REPLACED CLIP IAW SRM. (K) 2L72 4F4 FRTA21EA E15NE 20050822000112005082200011EU 2005 8 22 USAA050978 120050805A5315D5347217220500 FLOORBEAM AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE CABIN CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19110UW13254 1112 PIT - S2 - BEAM, .5 INCHES X .5 INCHES, CORROSION; LEVEL 1; TASK JA-260-53500, FLOOR SUPPORT BEAM FR 66-68, Y1182 TO Y1292. DEFECTIVE PART REPLACED WITH IDENTICAL PART. (K) 2L72 4F4 FRTA28NM E38NE 20050822000222005082200022EU 2005 8 22 KBM2005F00194 120050520A243216061 BATTERY SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE OVERTEMP E KBMAO OTHER MJ OVER TEMP WARNING INDICATION NRNOT REPORTED 1 WP191188P 2347 NICAD BATTERY, BATTERY TEMP LIGHT ON, BATTERY HOT. REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20050822000312005082200031SW 2005 8 22 KBM2005F00212 120050522A6320214040805001 SWITCH BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL M/R XMSN INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1973DP 2513 MAIN ROTOR TRANSMISSION OIL TEMP LIGHT ILLUMINATING AT 85 DEGREES C. REMOVED AND REPLACED. (K) 1G71 3U3 U H2SW E4CE 20050822000352005082200035NM 2005 8 22 ASAA0540298 120050626A531165C356934 FRAME BOEING737 7374Q8 138447QNM FS 685 BROKEN A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 OKC - FOUND RIGHT FRAME BS 685 IS BROKEN ON THE LOWER FLANGE. REMOVED AND REPLACED FRAME ASSEMBLY IAW DWG INSTRUCTIONS 65C36758-41-6. (M) 2L72 4F RTA16WE 20050822000362005082200036NM 2005 8 22 ASAA0540353 120050706A5753 SKIN BOEING737 7374Q8 138447QNM FLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 YXX - FOUND LEFT OUTBOARD FORE FLAP HAS A DENT FROM CHAFING OUTBOARD OF FORE FLAP TRACK. DENT ON OUTBOARD LEFT FORE FLAP OUTBOARD OF NR 1 FORE FLAP TRACK REPAIRED IAW B737-400 SRM 57-53-01 FIGURE 201. (M) 2L72 4F RTA16WE 20050822000452005082200045NM 2005 8 22 ASAA0540367 120050721A5210 GUIDE ARM BOEING737 7374Q8 138447QNM R1 DOOR OUT OF RIG A ASAAK NONE O OTHER ININSP/MAINT 1 NM02775AS 25108 SEA - RIGHT FORWARD SERVICE DOOR R-1 WILL NOT CLOSE. DOOR GUIDE ARM AND HORIZONTAL ROD WERE FOUND OUT OF RIG. RIGGED DOOR PER AMM 53-41-00. ACCOMPLISHED DOOR LUBE. DOOR NOW OPENS AND CLOSES NORMALLY. (M) 2L72 4F RTA16WE 20050822000492005082200049NM 2005 8 22 ASAA0540350 120050706A532069429494 SUPPORT BRACKET BOEING737 7374Q8 138447QNM FS 807 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 YXX - FOUND AFT CARGO PIT SUPPORT BRACKET CRACKED AT BS 807, RBL 20. FABRICATED AND REPLACED REPAIR PART IAW B737-400 SRM 51-40-02 AND 51-30-01. (M) 2L72 4F RTA16WE 20050822000522005082200052NM 2005 8 22 QXEA200501172 120050814A27202379003001 REGULATOR DHAV DHC8 DHC8202 2809007NM RUDDER PRESS MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09379PH5931 530 SEA - THE "RUD FULL PRESS" CAUTION LIGHT ILLUMINATED DURING CRUISE FLIGHT, FOLLOWED IMMEDIATELY BY THE "RUD PRESS" CAUTION LIGHT. COMPLETED EMERGENCY AND ABNORMAL CHECKLIST FOR BOTH LIGHTS. MAINTENANCE REPLACED RUD FULL PRESS SWITCHES NO HELP. TROUBLESHOT TO RUD PRESS REGULATOR. REPLACED PER AMM 27-20-38, PAGES 401-405. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050822000562005082200056NE 2005 8 22 QXEA200501171 220050814A7200 VALVE DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE NR 2 ENGINE MALFUNCTIONED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM09347PH 480 WHEN NR 2 BLEED WAS SELECTED ON, GREY HAZE FILLED COCKPIT AND CABIN. MAINTENANCE REPLACED NR 2 ENGINE P2.5/3.0 SWITCHING VALVE IAW QX MTC 9723001. GROUND RAN NR 2 ENGINE, SELECTED NR 2 BLEED ON. NO HAZE OR ODORS DETECTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20050822000922005082200092WP 2005 8 22 IXXA05RNG027S 120050721A5740 SUPPORT FITTING DOUG DC8 DC862F 3021972WP XF 97.6090 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW1171CX 670243317 45961 DURING ROUTINE "C" CHECK, RT WING OUTBOARD FLAP SUPPORT FITTING STA XF 97.6090 WAS FOUND CRACKED (0.2035"). REPAIR ACCOMPLISHED, STOP HOLES WERE DRILLED, ANGLE WAS FABRICATED AND INSTALLED IAW EWO ATI 57-016 & EO ATI-070205. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR. 2L74 4F 4A25 20050822001022005082200102WP 2005 8 22 IXXA05RNG048S 120050717A5246 DOOR DOUG DC8 DC862F 3021972WP FUEL CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW1171CX 670243317 45961 DURING A ROUTINE C CHECK INSPECTION A CRACK WAS FOUND AT FUEL ACCESS DOO 506A LH.CORRECTIVE ACTION: ACCESS DOOR 506A LH WAS REPAIRED IAW EWO ATI-57-027 & SRM 57-2-1 FIGURE 43. 2L74 4F 4A25 20050822001122005082200112NM 2005 8 22 BB05064 120050808A335020131A BATTERY PACK BOEING757 7572B7 1384964NM PASSENGER CABIN DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19630AU 27808 CLT - THE OVERHEAD EMERGENCY LIGHT AT ROW 13DEF WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONALLY CHECKS OK. 2L72 4F RTA2NM 20050822001142005082200114WP 2005 8 22 IXXA05SMN62S 120050623A5330 SKIN DOUG DC8 DC871F 302199DWP FS 1346.000 DAMAGED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, RT AFT FUSELAGE STA FS 1346.000, L-35.5R. ONLY 2 ROWS OF RIVETS IN OLD ANTENNA DOUBLER ADD THIRD ROWS OF RIVETS UTILIZING SRM RIVET SPACING OR UPGRADE REPAIR DOUBLER, STA 1346.000 L-35.5R (REF 822BX-R14). PERFORMED MAJOR REPAIR IAW DC-8 SRM 53-2-1 FIG. 7 SHEET 1, 3, EO SEMAN 2005868 DATE 06-13-05. REMOVED EXISTING REPAIR DOUBLER IAW DC-8 SRM 51-1-21 PAGE 1. FABRICATED REPAIR DOUBLER (ALCLAD 7075 T6 0.090”) (02 EA) INTERNAL FINGER DOUBLER (ALCLAD 7075 T6 0.050”) IAW DC-8 SRM 53-2-1 FIG. 7 SHEET 1,3, DC-8 SRM 53-4-1 FIG. 16 SHEET 1 ITEM E, DC-8 SRM 51-10-0 FIG. 2 SHEET 5, DC-8 SRM 51-9-0 FIG. 68A, DC-8 SRM 51-1-4 PAGE 1. CLEANED, TREATED AND PRIMED AREA REPAIR PARTS IAW DC-8 S2L74 4F RT4A25 20050822001172005082200117WP 2005 8 22 IXXA05SMN102S 120050627A5720 VANE DOUG DC8 DC871F 302199DWP XW 454.000 ELONGATED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C-CHECK INSPECTION, LT WING.- VANE SLOT REPAIR HOLE ELONGATED, XW 454.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, SEMAN DWG ED 3982, EO SEMAN 2005835. REMOVED FASTENERS IAW DC-8 SRM 51-1-21 PAGE 1, DC-8 SRM 51-1-20D PAGE 21. TRIMMED OUT DAMAGED AREA IAW SEMAN DWG EO 3982. PERFORMED NDT INSPECTION IAW DC-8 NDT SPM. NO CRACK, NO CORROSION FOUND FAST STOP DRILL. FABRICATED EXTERNAL REPAIR DOUBLER, FILLER, INTERNAL DOUBLER IAW SEMAN DWG ED 3982. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW DC-8 SRM. APPLIED PRC SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11 PAGE 9. INSTALLED REPAIR PARTS IAW SEMAN DWG ED 3982, DC-8 SRMS. TORQUED IAW DC-8 SRM. 2L74 4F RT4A25 20050822001232005082200123WP 2005 8 22 IXXA05SMN132S 120050629A5313 LONGERON DOUG DC8 DC871F 302199DWP XS 1690.00 L-36 CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, MAIN CARGO CMPT.- L-36 CORRODED, STA. 1690.00 - STA. 1700.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 53-2-2 FIG. 4A, EO SEMAN Nº 2005937 DATE 06-22-05. REMOVED CORROSION IAW DC-8 SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW DC-8 SRM 53-2-0 PAGE 2P. REMOVED LONGERON SEGMENT IAW DC-8 SRM 53-2-2 FIG. 4. PERFORMED DETAILED VISUAL INSPECTION PAST LONGERON SEGMENT TRIM. NO CRACK, CORROSION FOUND. FABRICATED NEW LONGERON SEGMENT IAW DC-8 SRM 53-2-2 FIG. 4A, DC-8 SRM 53-5-11 FIG. 7, ITEM A, DC-8 SRM 51-2-0 FIG. 50 + SPLICE IAW DC-8 SRM 53-2-2 FIG. 10, TR NR 53-193, DC-8 SRM 53-2-2 FIG. 10 TR NR 53-153. PERFORMED HEAT TREATMENT TO SPLICE IAW DC-8 SRM 51-1-1 PAGES 1,13,7. CLEANED, 2L74 4F RT4A25 20050822001272005082200127WP 2005 8 22 IXXA05SMN152S 120050630A5210 SKIN DOUG DC8 DC871F 302199DWP ZONE 800 IMPROPER B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C CHECK INSPECTION, FWD.- PASSENGER DOOR UPPER PART HAS INTERIN REPAIR. PERFORMED MAJOR REPAIR IAW DC-8 SRM 52-2-0 FIG. 4, EO SEMAN NR 20051011 DATE 06-28-05. REMOVED INTERIM REPAIR IAW DC-8 SRM 51-1-21 PAGE 1. PERFORMED DETAILED VISUAL INSPECTION, NO CRACK, CORROSION FOUND. FABRICATED REPAIR DOUBLER (ALCLAD 2024 T3 0.050”) IAW DC-8 SRM 52-2-0 FIG. 4 (SHEET 3), DC-8 SRM 53-3-1 FIG. 1 ITEM L, DC-8 SRM 51-1-4 PAGE 1. CLEANED, TREATED AND PRIMED AREA AND REPAIR DOUBLER IAW DC-8 SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11 PAGE 9. INSTALLED REPAIR DOUBLER IAW DC-8 SRM 52-2-0 FIG. 4, DC-8 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050822001292005082200129WP 2005 8 22 IXXA05SMN154S 120050706A5311 FRAME DOUG DC8 DC871F 302199DWP STA 55.00 L-24R CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11822BX898902881 45813 DURING ROUTINE C-CHECK INSPECTION, FWD ACCES COMPT. FRAME CRACKED 2” STA 55.000 L-24R. PERFORMED MAJOR REPAIR IAW DC-8 SRM 53-2-0 FIG. 2 SHEET 5, TR 53-125 DATE 08-31-01, DC-8 SRM 53-2-0 FIG. 2 (SHEET 6) EO SEMAN NR 20051015 DATE 06-29-05. REPAIRED PER SRM. 2L74 4F RT4A25 20050822001362005082200136NM 2005 8 22 05FDEA02325 120050808A2752652661458 TRANSMISSION BOEING727 727200 138407ENM TE FLAPS DAMAGED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25482FE 21464 AFTER T/O UPON FLAP RETRACTION ASSYMETRICAL FLAPS ON INBOARD FLAPS RAN RED TABS AND RETURNED TO PVD. RT INBRD TRAILING EDGE FLAP INBRD JACK SCREW GEARBOX DAMAGED AND PULLED APART WHERE JACK SCREW ENTERS GEARBOX AT REAR SPAR. FACT 08AUG05 19:08 PVD R R&R'D RT INBD FLAP, INBD FLAP TRANSMISSION ASSY IAW 27-51-041-4. ALSO, R&R'D RT IB AILERON AND TAB ASSY PER MM 27-10-001-2, PGS 1-3. 2L73 4F RTA3WE 20050822001452005082200145NM 2005 8 22 BB05067 120050811A335020121 CHARGER BOEING767 767201 1385125NM PASSENGER CABIN FAULTY A USAAO OTHER O OTHER CRCRUISE 1 EA19648US 23900 THE EMERGENCY LIGHTS ILLUMINATED IN FLIGHT WITH THE EMERGENCY SWITCH IN THE ARMED POSITION. MAINTENANCE REPLACED THE BATTERY CHARGER ASSEMBLY. OPERATIONALLY CHECKS OK. 2L72 4F RTA1NM 20050822001472005082200147 2005 8 22 SWAA052474 420050817A2565D31354 SLIDE BOEING737 7373A4 1384585NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050822001562005082200156NM 2005 8 22 SWAA052486 120050818A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29617SW 27700 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIES CORRODED AT BS 807, RBL 3, LBL 3 & LBL 9. REMOVED AND REPLACED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20050822001692005082200169EA 2005 8 22 COMA0570096 120050809A2760 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA SPOILERS ILLUMINATED A COMAO OTHER J WARNING INDICATION DEDESCENT 1 SO01368CA 10075 FLIGHT 5289 - SPOILERS CAUTION MESSAGE. LEFT GROUND LIFT DUMP INOPERABLE. RESET SYSTEM NO DEFECTS NOTED. 2L72 4F RTA21EA 20050822001782005082200178NM 2005 8 22 SWAA052487 120050818A53116546569 SHEAR TIE BOEING737 7373H4 1384600NM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29617SW 27700 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 947, RBL 18. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050823000032005082300003EA 2005 8 23 COMA0560445 120050813A339759465 POWER CABLE CNDAIRCL600 CL6002B19 1900309EA CABIN BROKEN A COMAO OTHER O OTHER CRCRUISE 1 SO01995CA 7229 FLIGHT 5610 - CABIN EMERGENCY LIGHTS FLICKER. REPLACED POWER CABLE. 2L72 4F RTA21EA 20050823000052005082300005NE 2005 8 23 COMA0560439 220050810A7200CF343A1 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE LEFT FAILED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01811CA135771324 7380 807607 FLIGHT 5739 - LEFT ENGINE OIL PRESSURE WARNING. REPLACED THE LEFT ENGINE. 2L72 4F4 FRTA21EA E15NE 20050823000182005082300018WP 2005 8 23 AALA20050529 120050817A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21495AA 49733 BOS - AFT CEILING EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050823000342005082300034EA 2005 8 23 COMA0570098 120050815A335020131A BATTERY CNDAIRCL600 CL6002C10 1390015EA CABIN DISCHARGED A COMAO OTHER O OTHER NRNOT REPORTED 1 SO01374CA6308 2291 10090 FLIGHT 5827 - EMERGENCY LIGHTS INOPERABLE. REPLACED THE EMERGENCY LIGHTS BATTERY. 2L72 4F RTA21EA 20050823000402005082300040NM 2005 8 23 DL738050442 120050808A3231162A31051 ROD BOEING737 737832 13844CFNM LT NLG DOOR BROKEN A DALAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO27387DA 30374 DURING ROTATION LOUD POP NEAR COCKPIT. GEAR CAME UP NORMALLY WITH LIGHTS OUT. GEAR LOWERED, GEAR NORMALLY ALL GREEN. RETURNED TO TPA. MTC FOUND L NLG DOOR PUSH ROD BROKEN. REPLACED SAME PER MM. 2L72 4F RTA16WE 20050823000412005082300041NE 2005 8 23 DL764050443 220050807A7200CF680C2B8F ENGINE BOEING767 767432ER 1385134NM GE CF6 CF680 30025NE NR 1 WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO27841MH1531415314 706232 29714 706232 FAILED OPN 5039 11TH STAGE BORO. REPLACED ENGINE. 2L72 4F4 FRTA1NM E13NE 20050823000522005082300052NM 2005 8 23 CALA0500269 120050819A532065C807351 ANGLE BOEING737 737524 1384721NM STA 975-990 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2746625 27529 INSPECTION FOUND R-2 DOOR ZEE ANGLE CORRODED AT STA 975-990, RBL 50 TO RBL 51. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-40-02. 2L72 4F RTA16WE 20050823000942005082300094NM 2005 8 23 AWXA200500978 120050722A5752654645521C TAB BOEING737 737301 1384611NM ZONE 500 - LEFT DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED DISBOND AREA ON UPPER SURFACE OF THE L/H AILERON TAB AT OUTBOARD END. MAINTENANCE REMOVED DISBONDED SKIN ON UPPER SURFACE OF THE L/H AILERON TAB AT THE OUTBOARD END IAW BOEING 737-300 SRM 51-70-07-0. BONDED FIBERGLASS REPAIR TO UPPER SURFACE OF THE L/H AILERON TAB ON OUTBOARD END IAW BOEING 737-300 SRM 51-70-07-0. RE-WEIGHED AILERON TAB AND ADDED NOTE TO DATA PLATE IAW BOEING 737-300 SRM 51-60-03-0 FIG 1. 2L72 4F RTA16WE 20050823000952005082300095NM 2005 8 23 AWXA200500979 120050731A5320655584311 CHANNEL BOEING737 7373Y0 1384671NM CABIN CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28334AW 23747 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED CORROSION ON U CHANNEL AT BS 990, BETWEEN STR23L AND 24L. NO CORROSION REMOVAL LIMITS ARE AVAILABLE FOR CHANNEL. MAINTENANCE REMOVED CHANNEL AT BS 990, STR 23L TO 24L IAW BOEING 737-300 SRM 51-40-02-0. PREPARED REPLACEMENT CHANNEL FOR INSTALLATION IAW BOEING 737-300 SRM 51-40-02-0 FIG 8. INSTALLED REPAIR PARTS IAW BOEING 737-300 SRM 51-40-02-0 FIGURES 4 AND 8. 2L72 4F RTA16WE 20050823000992005082300099SO 2005 8 23 C2XA05TY050 120050817A323214532170401 SEQUENCE VALVE EMB 145 EMB145LR 3260212SO MLG DEFECTIVE A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2713995 145295 TYS AIRCRAFT ON TAKEOFF HAD A LANDING GEAR/LEVER DISAGREE WARNING.AIRCRAFT RETURN TO BLOCK AND WAS CHECKED OUT FOR A SAFE FERRY FLIGHT TO TYS. MAINTENANCE R/R THE LANDING GEAR CONTROL LEVER IAW EMB 145 AMM 32-32002.ALL OPS CHECKS WERE GOOD AND AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4T RTT00011AT 20050823001002005082300100NM 2005 8 23 05FDEA02477 120050816A5320 SILL BOEING727 727200 138407ENM CARGO DOOR DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 N01472 BS 364 - BS 640, STR 3L WHILE WORKING NR N01466, FOUND NUMEROUS HOLES IN MAIN CARGO DOOR UPPER SILL TO BE FIGURE EIGHTED. B.S 634 TO 640 JUST ABOVE STR.3L. (OPEN) 2L73 4F RTA3WE 20050823001032005082300103WP 2005 8 23 05FDEA02483 120050816A5270 WARNING LIGHT DOUG DC10 DC1030 3023501WP A/C DOOR INTERMITTENT A FDEAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO25319FE 47820 DURING CRUISE FLIGHT, WE GOT THE AIR CONDITIONER DOOR OPEN LIGHT THAT CAME ON SEVERAL TIMES. GRADUALLY COMING ON FOR LONGER PERIODS RAN QRH & LANDED AT NEAREST FIELD,KIND. INSPECTED ALL THREE AC BAY DOOR SWITCHES IAW 52-42-01-2 FOUND ALL 3 DOOR SWITCHES TO OPERATE NORMAL. INSPECTED F/E ANNUNCIATOR LIGHT PANEL, FOUND NUMEROUS ANNUCIATOR CONTACT PINS TO BE DAMAGED & COULD CAUSE AC DOOR LIGHT TO FLICKERON & OFF W/ VIBRATION. R&R'D F/E'S ANNUNCIATOR LIGHT PANEL IAW 33-15-02-2 OPS NORMAL. RETURNED A/C TO SERVICE. 2L73 4F A22WE 20050823001082005082300108NM 2005 8 23 05FDEA02466 120050815A5314 KEELBEAM DOUG MD11 MD11 3023602NM ZONE 700 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 CENTER LANDING GEAR FORWARD BULKHEAD, LT KEELBEAM DOUBLER FOUND CRACKED AS MARKED. REMOVED AND REPLACED WITH NEW DOUBLER AS PER SRM 51-31-01. 2L73 4F RTA22WE 20050823001182005082300118SO 2005 8 23 SWIA200515424 120050813A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT DISCHARGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07188SW9055 9055 120039 FORWARD EMERGENCY FLOOR LIGHTS INOP. REPLACED FORWARD BATTERY PACK. OPERATIONAL CHECK GOOD, PN D366-04-001, SN/ON 1169, SN/OFF 049/05-85. 2L72 4T RTA31SO 20050823001232005082300123EA 2005 8 23 SWIA200515429 120050808A2750855D10011 SENSOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07919SW4788 4788 7657 "FLAPS FAIL" CAUTION MSG. REMOVED AND REPLACED RT BPSU IAW CRJ MM 27-51-10 AND READJUSTED LT AND RT BPSU IAW M/M 27-51-10. READJUSTEMENT OF FECU POTENTIOMETER NR 5 AND NR 8. OPERATIONAL CHECK GOOD IAW CRJ M/M 27-51-10. 2L72 4F RTA21EA 20050823001412005082300141SO 2005 8 23 SWIA200515433 120050817A27503472001001 CONTROL UNIT EMB 120 EMB120ER 3260203SO TE FLAP MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 NM07214SW1232412324 120280 FLAP CONTROL FAULT ON CLIMB-OUT. REPLACED THE FLAP CONTROL UNIT. OPERATIONAL CHECK GOOD IAW MM 27-50-00. 2L72 4T RTA31SO 20050823001442005082300144EA 2005 8 23 SWIA200515436 120050815A2720 BEARING CNDAIRCL600 CL6002B19 1900309EA RUDDER PEDAL WORN A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07597SW 7293 AFTER PUSHBACK FROM SLC, HEARD AUDIBLE CLICKING SOUND AS WELL AS BUMPING FEEDBACK FROM PEDALS. REPLACED LEFT RUDDER PEDAL PIVOT BEARINGS AND PEDAL ADJUSTMENT YOKE. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050823001472005082300147 2005 8 23 SWIA200515439 420050815A22106225734002 SERVO EMB 120 EMB120ER 3260203SO AILERONS BINDING A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07236SW1309313093 120312 ROUGHNESS IN CONTROL YOKE WHEN MOVING AILERONS FROM CENTER TO THE LT. REPLACED AILERON AUTO-PILOT SERVO IAW 22-10-05. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050823001502005082300150EU 2005 8 23 UPS05145243 120050819A3350 LAMP AIRBUSA300 A300F4622R 3930360EU EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01149UP 0832 LAV EMERGENCY LIGHT INOP. RELAMPED, OPS NORMAL. 2L72 4F RTA35EU 20050823001532005082300153NM 2005 8 23 UPS05545231 120050820A5610 HANDLE BOEING757 75724APF 1384969NM R2 WINDOW INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01432UP 25463 P3 R2 WINDOW EXT CRANK HANDLE WILL NOT OPEN. INSPECTED R2 FWD STRIKER BRACKET TO VERIFY THAT EO B757-5610-5738 WAS C/W. THIS EO WAS C/W BUT STRIKER BRACKET WAS OUT OF ADJUSTMENT. ADJUSTED STRIKER BRACKET AS PER EO B 757-5610-5738D. OPS CHECKED EXTERNAL CRANK HANDLE IAW TASK CARD 56-001-01 AND OPS CK GOOD. 2L72 4F RTA2NM 20050823001572005082300157WP 2005 8 23 UPS05845229 120050812A53403779762U1 FITTING DOUG DC8 DC871F 302199DWP STA 680 L2L CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 MAIN CABIN LONGERON END FITTING CRACKED AFT SIDE OF STA 680 L2L. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D, 51-1-21, AND 51-3-0 . 2L74 4F RT4A25 20050823001762005082300176WP 2005 8 23 05FDEA02560 120050819A5712 RIB DOUG DC10 DC1010 3022110WP RT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 RT WING OUT'B L/E INTERNAL STRUCTURE FOUND 1EA ANGLE REPAIR ON RIB AT XORS 582. FABRICATED ANGLE IAW SRM 57-20-00 FIGURE 1 VOL.1. 2L73 4F A22WE 20050823001982005082300198CE 2005 8 23 DJFA2005132 120050821A3260 SWITCH RAYTHNDH125 HAWKER800XP 7150012CE MLG MALFUNCTIONED E DJFAO OTHER N FALSE WARNING DEDESCENT 1 EA23720TA 258320 THE CREW SELECTED GEAR DOWN FOR LANDING. THE INDICATION WAS THREE RED OVER THREE GREEN. THREE FLYBYS WERE PERFORMED AND THE TOWER DECLARED AN EMERGENCY FOR THE CREW. THE AIRCRAFT LANDED WITH OUT INCIDENT. 2L72 4F RTA3EU 20050824000012005082400001NM 2005 8 24 05FDEA02501 120050816A2710BACC13AP6D2398 CONTROL CABLE BOEING727 727200 138407ENM AILERONS BROKEN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25467FE 21449 DURING POSTFLIGHT INSPECTION FOUND LEFT INBOARD AILERON CABLE BROKEN. INSPECTED CABLE PULLEYS NO FURTHER DAMAGE FOUND AT THIS TIME. FOUND CABLE BROKE IN HALF HANGING FROM THE LEFT WHEEL WELL JUST ABOVE APU FIRE BOTTLE AREA. A/C ARRIVED WITH INBOARD AILERON IN THE UP POSITION AND ALL OTHER CONTROL SURFACES IN THE DOWN POSITION. REMOVED AND REPLACED LT AILERON BUSS CABLE RUN ABSA(T) PER 727-200 MM 20-10-020-4. PERFORMED ADJUSTMENT AND TEST OF AILERON BUSS SYSTEM PER 727-200 MM 27-10-000- 5. OPS CHECKS GOOD, OK FOR SERVICE. 2L73 4F RTA3WE 20050824000032005082400003NM 2005 8 24 05FDEA02505 120050817A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 PREVIOUS REPAIR AT STA 400 BETWEEN 5L AND 6L IS A MAJOR REPAIR IAW SRM 53-30-3 FIG 1. 2L73 4F RTA3WE 20050824000042005082400004NM 2005 8 24 05FDEA02506 120050818A5315 FLOORBEAM DOUG MD11 MD11 3023602NM CARGO BAY DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 AFT CARGO COMPARTMENT STA 1841 LOWER FRAME FLOORBEAM WEB FOUND DAMAGED, AS MARKED. REMOVED AS PER SRM 51-33-01 AND 51-35-01 VOL II. NEW WEB FABRICATED AS PER DRAWING AGA 7170 AND NEW WEB INSTALLED AS PER SRM 51-33-01 AND 51-35-01 VOL II. MINOR REPAIR AS PER GMMM 6-2-100. 2L73 4F RTA22WE 20050824000072005082400007NM 2005 8 24 05FDEA02509 120050818A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 CABIN SEAT TRACK AT STATION Y1019, -X8.5 FOUND CORRODED. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE I VOLUME I AT STATION Y1009 TO STATION Y1129, -X8.5. 2L73 4F RTA22WE 20050824000092005082400009NM 2005 8 24 05FDEA02512 120050818A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 MAIN DECK SEAT TRACK AT STATION Y1124, -X8.5 FOUND CORRODED. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE I VOLUME I AT STATION Y1009 TO STATION Y1129, -X8.5. 2L73 4F RTA22WE 20050824000102005082400010NM 2005 8 24 2005UALA00816 120050813A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE STA 860, STR 5L LIGHTNING STRIKEA UALAK NONE O OTHER ININSP/MAINT 1 WP29588UA 26717 LIGHTNING STRIKE DAMAGE AT STA 860, STR 5L. DRILLED OUT DAMAGE PER SRM 53-00-01, ACP HFEC INSP, NO CRACK FOUND. INSTALLED SOLID FASTENER PER MM 53-00-01. 2L72 4F4 FRTA2NM E17NE 20050824000192005082400019NM 2005 8 24 2005UALA00826 120050813A3350276005 FUSE BOEING747 747422 1384935NM PWA 4056 PW4056 NE RT OVERWING BLOWN A UALAK NONE L NO TEST ININSP/MAINT 1 WP29116UA 26908 RIGHT OVERWING EMERGENCY LIGHTS INOP. TWO MOST FWD ASSY'S REPLACED FUSE. 2L74 4F4 FRTA20WE E24NE 20050824000212005082400021NM 2005 8 24 2005UALA00828 120050815A3350582233 BATTERY BOEING747 747422 1384935NM PWA 4056 PW4056 NE DOOR 4L DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29199UA 28717 DOOR 4 LEFT LOWER WALL EEL AISLE JUST AFT OF GALLEY INOP. REPLACED BATTERY ASSY. 2L74 4F4 FRTA20WE E24NE 20050824000232005082400023EU 2005 8 24 2005UALA00830 120050809A3350321454 BATTERY PACK AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE SEATS 1C-6C INOPERATIVE A UALAO OTHER L NO TEST ININSP/MAINT 1 WP29422UA 503 SEATS 1C-6C FLOOR PROXIMITY EMERGENCY ESCAPE PATH SYSTEM LIGHTS ARE INOPERATIVE. REPLACED BATTERY PACK. 2L72 4F4 FRTA28NM E40NE 20050824000242005082400024NM 2005 8 24 2005UALA00831 120050816A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE SEAT 34 ABC INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29128UA 30023 SEAT 34 ABC EMERGENCY LIGHT INOP. 2L74 4F4 FRTA20WE E24NE 20050824000252005082400025NM 2005 8 24 2005UALA00832 120050816A5320 STIFFENER BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29674UA 29242 FWD NOSE SECTION BS 246 FLOORBEAM, FWD SIDE AT LBL 40 VERTICAL STIFFENER IS CRACKED. FINDING AND REPLACING CRACKED VERTICAL STIFFENERS IS WITHIN THE SCOPE OF ROUTINE INSPECTION OF THIS AREA, PER FAA-APPROVED BOEING SERVICE BULLETIN 767-53-0093. STIFFENER WAS REPLACED. 2L72 4F4 FRTA1NM E24NE 20050824000272005082400027NM 2005 8 24 2005UALA00834 120050815A5310 STRUCTURE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE BIRD STRIKE A UALAO OTHER O OTHER NRNOT REPORTED 1 WP29378UA 24653 BIRD STRIKE AROUND THE RADOME, VERY LOUD, ALSO, ODOR IN COCKPIT. ON CLIMB, THE AIRCRAFT ENCOUNTERD A BIRDSTRIKE. THE AIRCRAFT RETURNED TO FIELD AND MAINTENANCE PERFORMED A BID STRIKE INSPECTION PER AMM. THERE WAS EVIDENCE OF BIRD INGESTION IN THE NR 1 ENG HOWEVER THERE WERE NO DAMAGE TO THE BLADES OR VANES. THEY CLEANED OUT THE DEBRIS. THERE WERE TWO SEPARATE AREAS ON THE RADOME THAT WAS DAMAGE. AN INTERIM REPAIR WAS ACCOMPLISHED AND THE RADOME WAS REPLACED 4 DAYS LATER. 2L72 4F4 FRTA16WE E2GL 20050824000312005082400031NM 2005 8 24 2005UALA00838 120050816A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE BELOW DOOR 2L CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29305UA 23666 DENT FWD AND BELOW DOOR 2L. 2L72 4F4 FRTA16WE E2GL 20050824000332005082400033NM 2005 8 24 2005UALA00840 120050817A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE 3L DOOR MALFUNCTIONED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29198UA 28716 EMERGENCY LIGHTS AT DOOR 3L REMAIN ON WITH COCKPIT SWITCH IN ARMED POSITION. 2L74 4F4 FRTA20WE E24NE 20050824000342005082400034NM 2005 8 24 2005UALA00841 120050803A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE BS 1701 DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29594UA 28145 EXTERNAL FUSELAGE SKIN DAMAGE AT BS 1701 BTWN STRINGERS 19L-20L. ACCOMPLISH DOUBLER PER EVA-40245. 2L72 4F4 FRTA2NM E17NE 20050824000352005082400035NM 2005 8 24 2005UALA00842 120050815A3210 LANDING GEAR BOEING747 747422 1384935NM PWA 4056 PW4056 NE MAINS COLLAPSED A UALAK NONE O OTHER ININSP/MAINT 1 WP29196UA 28715 BODY GEARS RETRACTED CAUSING AIRCRAFT TO SETTLE ON ITS TAIL. EXTENSIVE MAJOR STRUCTURAL DAMAGE TO LOWER AFT FUSELAGE UP THROUGH FRAMES FROM APPROX STATION 1960-2180. BLG COMPONENTS ALSO DAMAGED. WILL WORK WITH BOEING AOG TEAM TO INSPECT, ASSESS AND REPAIR ALL DAMAGE. 2L74 4F4 FRTA20WE E24NE 20050824000372005082400037NM 2005 8 24 2005UALA00844 120050819A5330 SKIN BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE BELOW R2 DOOR PUNCTURED A UALAK NONE O OTHER ININSP/MAINT 1 WP29930UA 26655 PUNCTURE OF SKIN BELOW AND AFT OF DOOR 2R. 2L72 4F4 FRTA16WE E2GL 20050824000382005082400038NM 2005 8 24 2005UALA00845 120050818A5320 FLOOR SUPPORT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE STA 957-986 CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29327UA 24147 CABIN FLOOR SUPPORT AT AFT ENTRY DOOR HAS CORROSION STA 957-986 LBL 62.5 WL 208 AND LBL 63.0 WL 208. 2L72 4F4 FRTA16WE E2GL 20050824000402005082400040NM 2005 8 24 2005UALA00847 120050818A5230 STRUCTURE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE AFT CARGO DOOR DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29327UA 24147 AFT CARGO DOOR HAS SEVERAL OVERLAPPING DENTS AND SKIN IS DAMAGED ON FWD SIDE. INSTALLED A REPAIR DOUBLER 53 BY 48 INCHES REF SRM 52-00-01 AND SRM 51-00-01 FIG 202. 2L72 4F4 FRTA16WE E2GL 20050824000412005082400041NM 2005 8 24 2005UALA00848 120050819A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29347UA 24251 EXTERNAL FUSELAGE STA 434 STR 2R BLENDED SKIN AROUND A FASTENER IS DAMAGED. 2L72 4F4 FRTA16WE E2GL 20050824000422005082400042NM 2005 8 24 2005UALA00849 120050808A5350 RADOME BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE BIRD STRIKE A UALAK NONE O OTHER ININSP/MAINT 1 WP29121UA 29167 CREW REPORT STRIKING TWO LARGE BIRDS ON CLIMB-OUT FROM ORD. STRUCK THE LOWER NOSE OR BELLY OF THE AIRCRAFT PASSING THROUGH 4800 FT. DAMAGE TO FUSELAGE SKIN AND FWD STRUCTURE REPAIRED PER MAJOR REPAIR EVA'S 50522A AND 50523A. RADOME REPLACED. 2L74 4F4 FRTA20WE E24NE 20050824000452005082400045SO 2005 8 24 SWIA200515442 120050814A3350 LAMP EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07220SW 120288 EMERGENCY LIGHTS BY MCD OUT. INSTALLED SERVICEABLE LAMP. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050824000582005082400058EU 2005 8 24 MALA050641 120050812A5280 SKIN BAC 146 AVRO146RJ85A1500097EU LT MLG DOOR DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15522XJ E2347 WHILE ACCOMPLISHING C1 INSPECTION, FOUND THE LEFT MAIN LANDING GEAR DOOR, LOWER SKIN AFT UPPER CUT-OUT TO BE CRACKED ON THE FORWARD OUTBOARD CORNER. 2H74 4F RTA49EU 20050824000592005082400059EU 2005 8 24 MALA050645 120050812A5420 COWL DOOR BAC 146 AVRO146RJ85A1500097EU NACELLE CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15522XJ E2347 DURING INSPECTION, FOUND NR 3 AFT OTBD COWL DOOR HAS CHAFFING ON STIFFENER AT BOTTOM OF COWL DOOR. 2H74 4F RTA49EU 20050824000632005082400063EU 2005 8 24 MALA050661 120050816A5411 RIB SAAB SF340 340B 7860101EU RT NACELLE CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15362PX 340B258 DURING 4Y/2Y INSPECTION IN BNA, FOUND RT NACELLE RIB NR 2 IS CHAFED AT NS203, LOWER SIDE. DAMAGE HAS BEEN REPAIRED IAW MESABA EO#$54127. REF: EAMS WORK ORDER 212631 TASK 4540. 2L72 4T RTA52EU 20050824000682005082400068EU 2005 8 24 MALA050651 120050814A2120 SMOKE SAAB SF340 340B 7860101EU CABIN DETECTED A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL15411XJ 340B411 CREW REPORTED WITH THE SUPP A/C RUNNING THE CABIN BEGAN TO FILL WITH SMOKE. CREW TURNED OFF SUPP A/C SYSTEM AND EXITED THE AIRCRAFT. AFTER TEN MINUTES OR SO, THE SMOKE WAS GONE. FIRE DEPARTMENT SHOWED UP TO AIRCRAFT AS WELL. NO FURTHER INFORMATION AT THIS TIME. 2L72 4T RTA52EU 20050824000692005082400069EU 2005 8 24 MALA050640 120050812A5280 SKIN BAC 146 AVRO146RJ85A1500097EU MLG DOOR DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15522XJ E2347 WHILE ACCOMPLISHING C1 INSPECTION, FOUND THE LEFT MAIN LANDING GEAR DOOR LOWER SKIN, AFT UPPER CUT-OUT CRACKED INSIDE CUT-OUT ON FORWARD OUTBOARD CORNER. 2H74 4F RTA49EU 20050824000702005082400070EU 2005 8 24 MALA050639 120050811A5320 FLOOR SUPPORT BAC 146 AVRO146RJ85A1500097EU CABIN CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15522XJ E2347 WHILE ACCOMPLISHING C3 INSPECTION, FOUND THE FLOOR SUPPORT BRACKET AT FRAME 35 IN THE AFT CARGO BAY CRACKED AND CORRODED. 2H74 4F RTA49EU 20050824000732005082400073EU 2005 8 24 MALA050648 120050813A5730 SKIN BAC 146 AVRO146RJ85A1500097EU RT WING DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15522XJ E2347 WHILE ACCOMPLISHING C3 INSPECTION, FOUND A CRACK ON THE PANEL BETWEEN THE RIGHT WING AND AILERON HORN JUST AFT OF THE WING TIP, PANEL 691AR. 2H74 4F RTA49EU 20050824000742005082400074EU 2005 8 24 MALA050649 120050813A5753 TAB BAC 146 AVRO146RJ85A1500097EU TE FLAP WORN A MALAK NONE O OTHER ININSP/MAINT 1 GL15522XJ E2347 WHILE ACCOMPLISHING C1 INSPECTION, FOUND WEAR MARKS ON THE UNDERSIDE OF THE RIGHT INBOARD FLAP TAB AT THE INBOARD HINGE. 2H74 4F RTA49EU 20050824000752005082400075EU 2005 8 24 MALA050650 120050816A5320 FLOOR SUPPORT BAC 146 AVRO146RJ85A1500097EU CABIN CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15522XJ E2347 WHILE ACOOMPLISHING C1 INSPECTION, FOUND TWO FLOOR SUPPORT BRACKETS UNDER PANEL 141CL LEFT AND RIGHT ON FRAME 20 CRACKED AND BROKEN. 2H74 4F RTA49EU 20050824000762005082400076EU 2005 8 24 MALA050662 120050816A5730 SKIN SAAB SF340 340B 7860101EU LT WING SCRATCHED A MALAK NONE O OTHER ININSP/MAINT 1 GL15362PX 340B258 DURING 4Y/2Y INSPECTION, FOUND LT WING LOWER SKIN AT WS71.5 IS SCRATCHED. DAMAGE HAS BEEN REPAIRED IAW MESABA EO#$57101. REF: EAMS WORK ORDER 212631 TASK 5509. 2L72 4T RTA52EU 20050824000772005082400077EU 2005 8 24 MALA050663 120050817A2432 BATTERY BAC 146 AVRO146RJ85A1500097EU MASTER FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15533XJ E2367 FAILED CAP CHECK. 2H74 4F RTA49EU 20050824000802005082400080EU 2005 8 24 MALA050660 120050816A5512 SKIN SAAB SF340 340B 7860101EU HORIZONTAL STAB DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15362PX 340B258 DURING 4Y/2Y INSPECTION IN BNA, FOUND RT HORIZONTAL STABILIZER UPPER SURFACE IS DENTED. DAMAGE HAS BEEN REPAIRED IAW MESABA EO#$55056. REF: EAMS WORK ORDER 212631 TASK 3505. 2L72 4T RTA52EU 20050824000832005082400083 2005 8 24 SWAA052523 420050821A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29370SW 26597 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20050824000862005082400086NM 2005 8 24 SWAA052526 120050819A3350417N5213 COVER BOEING737 7377H4 1384404NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29455WN 32462 EEPLS TRACK COVER LOOSE AT ROW 15 DEF. SECURED COVER PER MM. 2L72 4F RTA16WE 20050824000872005082400087NM 2005 8 24 SWAA052527 120050822A3350417N5213 COVER BOEING737 7377H4 1384404NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29458WN 33857 EEPLS TRACK COVER LOOSE. SECURED COVER PER MM. 2L72 4F RTA16WE 20050824000892005082400089NM 2005 8 24 SWAA052529 120050822A53156545805 FLOORBEAM BOEING737 7373H4 1384600NM CABIN CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29617SW 27700 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 312, LBL 1.0. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20050824000912005082400091EU 2005 8 24 SA05097 120050822A3350321430 BATTERY AIRBUSA321 A321211 3930370EU CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19170US 1462 THE EMERGENCY LIGHTS TEST FAILED IN THE MID LT POSITION OF THE CABIN. MAINTENANCE REPLACED THE 15WL BATTERY. SYSTEM TESTS OK. 2L72 4F RTA28NM 20050824001032005082400103WP 2005 8 24 ASMF200508008 120050817A7100JT8D219 ENGINE DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE RIGHT MAKING METAL W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23803ML42477 49726 716784 AIRCRAFT RETURNED TO PLATFORM, DURING RT ENGINE START, THE RT START VALVE OPEN LIGHT FLASHED AT 40 PERCENT RPM, N2 DECREASED TO 35 PERCENT AND RETURNED TO 50-56 PERCENT, 20 SECONDS AFTER THAT ENGINE STOPPED. AIRCRAFT WAS SENT TO THE HANGAR AND DURING MAINTENANCE REVISION WAS DETECTED METAL FLAKES IN THE RT ENGINE GEARBOX. THE RT ENGINE WAS REPLACED IAW MM 71-00-00, TESTED CORRECT. 2L72 4F4 FRTA6WE E9NE 20050824001112005082400111NM 2005 8 24 CALA0500276 120050822A5347143A531039 SEAT TRACK BOEING737 737824 13844BZNM STA 328 + 12 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712216 28776 INSPECTION FOUND CORROSION ON I/B SEAT TRACK AT FORWARD END, BS 328 +12, LBL 30 (CLOSET SUPPORT TRACK). THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20050824001122005082400112NM 2005 8 24 CALA0500277 120050822A5320147A57659 INTERCOSTAL BOEING737 737824 13844BZNM STA 951 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712216 28776 INSPECTION FOUND INTERCOSTAL CORRODED AT STA 951, RBL 26. A NEW INTERCOSTAL WAS INSTALLED IAW ECRA 5321-01276. 2L72 4F RTA16WE 20050824001132005082400113NM 2005 8 24 CALA0500278 120050808A5347BAC15202779 SEAT TRACK BOEING737 737824 13844BZNM STA 360 + 12 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712216 28776 INSPECTION FOUND I/B CLOSET SEAT TRACK CORRODED AT STA 360 + 12, LBL 22.5. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-40-02. 2L72 4F RTA16WE 20050824001172005082400117WP 2005 8 24 MWEA050083 120050818A53479957871502 SEAT TRACK DOUG DC9 DC982 3022082WP COCKPIT DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 FIRST OFFICER'S, INBOARD SEAT TRACK HOLES ARE ENLONGATED. FABRICATED AND INSTALLED SEAT TRACK. 2L72 4F A6WE 20050824001182005082400118WP 2005 8 24 MWEA050086 120050818A534759305478 SEAT TRACK DOUG DC9 DC982 3022082WP CABIN CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 NR 2 SEAT TRACK CORRODED, FORWARD END. FABRICATED AND INSTALLED SEAT TRACK. 2L72 4F A6WE 20050824001192005082400119WP 2005 8 24 ABXA050197 120050808A53105912285509 WINDOW FRAME DOUG DC9 DC941 302207NWP CABIN CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23965AX 47498 TOP FORWARD CORNER OF WINDOW FRAME ON AFT SIDE OF STA 737 RIGHT HAD A SMALL CRACK. REPAIRED AREA IAW DC-9 SSRM K07226. 2L72 4F A6WE 20050824001202005082400120WP 2005 8 24 ABXA050198 120050808A5347S5914913M24000 SEAT TRACK DOUG DC9 DC941 302207NWP CABIN CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23965AX 47498 SEAT TRACK CRACKED AT STA 200, RIGHT BUTT LINE 10. REMOVED AND REPLACED SEAT TRACK RIGHT BUTT LINE 10, FS 200 TO FS 155 IAW DC-9 SRM 51-30-2 AND 51-30-1. 2L72 4F A6WE 20050824001222005082400122WP 2005 8 24 ABXA050193 120050804A57535910041504 VANE DOUG DC9 DC941 302207NWP RT WING TE FLAP CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23965AX 47498 RIGHT FLAP INBOARD FIXED VANE SKIN CRACKED ADJACENT TO REPAIR. REMOVED AND REPLACED INBOARD FIXED VANE IAW DC-9 SRM. 2L72 4F A6WE 20050824001232005082400123WP 2005 8 24 ABXA050194 120050805A5347S4925848M36000 SEAT TRACK DOUG DC9 DC941 302207NWP CABIN CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23965AX 47498 SEAT TRACK RT BUTT LINE 9, FS 200, CRACKED. REMOVED AND REPLACED SEAT TRACK IAW DC-9 SRM 51-30-1. 2L72 4F A6WE 20050824001252005082400125WP 2005 8 24 ABXA050200 120050809A541199581832 SPAR DOUG DC9 DC941 302207NWP RT PYLON CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23965AX 47498 RIGHT AFT PYLON SPAR WEB WAS CRACKED AT LIGHTNING HOLE, LONGERON 13 RIGHT. REPAIRED CRACK IAW DC-9 SRM 53-01. 2L72 4F A6WE 20050824001322005082400132WP 2005 8 24 ABXA050186 120050817A5200 ACCESS DOOR DOUG DC9 DC931 3022065WP FUSELAGE UNLATCHED A ABXAK NONE O OTHER CLCLIMB 1 GL23924AX 47403 ON T/O, NO PRESSURIZATION, CABIN CLIMBED AT SAME RATE AS AIRCRAFT. AC PACKS SHOWED 27 PSI ON BOTH SIDES, CABIN FLOW CONTROL VALVE WAS FULLY CLOSED. INSPECTED A/C FOUND ALL EXTERIOR DOORS CLOSED. FOUND AFT BULKHEAD ACCESS DOOR UNLATCHED. RESECURED DOOR. PRESSURIZED A/C. OPS CHECKED GOOD. 2L72 4F A6WE 20050824001332005082400133NM 2005 8 24 ABXA050187 120050818A5620140T24232A WINDOW BOEING767 767231 1385131NM CABIN MISSING A ABXAK NONE D INFLIGHT SEPARATION ININSP/MAINT 1 GL23709AX 22572 1ST CABIN WINDOW AFT OF OVERWING EMERGENCY EXIT LEFT SIDE WAS MISSING A PIECE OF THE OUTER PANE. REMOVED AND REPLACED BROKEN WINDOW AFT OF LEFT EMERGENCY EXIT DOOR IAW B767 AMM 56-21-01-4. 2L72 4F RTA1NM 20050824001372005082400137WP 2005 8 24 AALA20050545 120050822A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21577AA 53154 ORD - EMERGENCY LIGHT IN CEILING AT ROWS 23 TO 26 INOPERATIVE. REPLACED BATTERY PACK AT B5106 FOR EMERGENCY LIGHT IN CEILING AT ROWS 23 TO 26. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050824001382005082400138NM 2005 8 24 AALA20050546 120050822A3397 CONNECTOR BOEING777 777223 1385213NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21779AN 29955 MIA - EMERGENCY LIGHT AT AFT SEAT 2G INOPERATIVE. FOUND LOOSE CONNECTOR. RESECURED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT AFT SEAT 2G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20050824001422005082400142NM 2005 8 24 AALA20050542 120050811A5320 SILL BOEING767 767323 1385205NM CABIN CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21355AA 24036 AFW - FORWARD CARGO DOOR CUTOUT LOWER MAIN SILL HAS CORROSION. BLEND IS LOCATED APPROXIMATELY AT STATION 570 ON THE LOWER SURFACE OF THE FAIL SAFE STRAP. BLEND IS APPROXIMATELY 2 INCHES BY 5 INCHES WITH A DEPTH OF 0.124 INCH REMAINING. REMOVED AND VERIFIED CORROSION REMOVED. PERFORMED A HIGH FREQUENCY EDDY CURRENT INSPECTION ON ALL REMOVED FASTENER LOCATIONS. INSTALLED FASTENERS WET. APPLIED ALODINE AND TWO COATS OF PRIMER. 2L72 4F RTA1NM 20050824001442005082400144WP 2005 8 24 AALA20050544 120050822A2822 PUMP DOUG DC9 DC982 3022082WP ZONE 100 INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21283AA 49296 DFW INFLIGHT T1296/22AUG - AIRCRAFT WOULD NOT TRANSFER FUEL FROM CENTER TANK. FORWARD BOOST PUMP CIRCUIT BREAKER POPPED ON TAKEOFF. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED CENTER FORWARD TANK BOOST PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050824001452005082400145NM 2005 8 24 DL777050450 120050812A2120 ODOR BOEING777 777232 1385232NM CABIN DETECTED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO27865DA 29737 CHEMICAL/MUSTY SMELL 4 TIMES USUALLY WITH PWR REDUCTION ALSO NOTED IN AFT CABIN, CHKD PER FIM TASK 21-00-00-810-808. CHKD L ENG BLEED AIR FOR OIL CONTAM. CHKD PACKS FOR OIL CONTAM. CHKD HYD RES PRESS MODULES. CHKD RECIRC FANS AND CARGO COMPT. CHKD FOR HYD LEAKS INSP NO TROUBLE FOUND. CONTACTED MCC FOR MORE INFO, HAD CREW RUN ENGS NTF. 2L72 4F RTT00001SE 20050824001462005082400146NM 2005 8 24 DL777050451 120050812A212023415901 CONVERTER BOEING777 777232 1385232NM OZONE FAILED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO27865DA 29737 STRONG OIL SMELL DURING FLT WORSE IN CLB/DESCENT AND PWR CHANGES. SUSPECT FROM PACK L/R. OVERWHELMING ODOR IN C/P ON DESCENT IRRITATED EYES. CHECKED EXH OF LT AND RT PACK. FOUND ODOR COMING FROM LT PACK. CHECKED INSIDE LP AND HP DUCTS LT ENG NO OIL RESIDUE FOUND. CHECKED ALL BLEED VLV EXITS LT ENG NO RESIDUE. CKD APU DUCT NO RESIDUE. RAN LT ENG NOTICED STRONG ODOR IN C/P DURING BLEED SHIFT. BORO LT ENG COMP NO OIL FOUND. PERFORMED CONTAMINATION REMOVAL PER AMM. REPLACED UPPER/LWR RECIRC FILTERS. REPLACED LT OZONE CONV PER AMM. NO FUMES AFTER OZONE CONV REPLACED. 2L72 4F RTT00001SE 20050824001472005082400147NM 2005 8 24 DL73S050452 120050814A335020121 CHARGER BOEING737 737232 1384475NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE O OTHER ININSP/MAINT 1 SO27318DL 23090 EMERGENCY LIGHTS ON SEATS WILL NOT EXTINGUISH. REPLACED BATTERY CHARGER IN CEILING ABOVE 1C RIGHT AFT CHARGER. SYSTEM TEST NORMAL. 2L72 4F RTA16WE 20050824001492005082400149NM 2005 8 24 DL76L050454 120050815A3350201301A BATTERY BOEING767 767332 1382001NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE O OTHER ININSP/MAINT 1 SO27173DN 24800 IR - ON L/O, FOUND EMERGENCY EXIT SIGNS AT DOOR 1L AND 1R. REMOVED AND REPLACED BATTERY PACK FOR DOOR 1L AND 1R EXIT SIGNS, NOW OPS NORMAL. 2L72 4F RTA1NM 20050824001512005082400151NM 2005 8 24 DLM88050456 120050816A3210 LOCK DOUG MD88 MD88 3023688NM MLG MALFUNCTIONED A DALAO OTHER O OTHER LDLANDING 1 SO27942DL 49815 AIRCRAFT DEPARTED HARD SURFACE OF RUNWAY AND TAXIED MOMENTARILY THROUGH GRASS AREA. ALL ENGINE INDICATIONS NORMAL. ON LANDING ROLLOUT, BRAKING SEEMED INEFFECTIVE. CLEANED NLG AND FUSELAGE. PERFORMED HIGH ENERGY INSP. NO EVIDENCE OF HIGH ENERGY STOP CONDITION NOTED. PERFORMED HIGH DRAG/SIDE LOAD INSP PER M/M. NO ITEMS NOTED. FURTHER CHECKS AND TROUBLESHOOTING CURRENTLY IN PROGRESS. 2L72 4F RTA6WE 20050824001532005082400153NM 2005 8 24 DL764050458 120050813A275018195820 TRANSMITTER BOEING767 767432ER 1385134NM NR 5 T/E FLAP OUT OF ADJUST A DALAO OTHER F FLT CONT AFFECTED LDLANDING 1 SO27831MH 29702 T/E FLAP ASYM EICAS MSG, LT FLAP READS 4 RT FLAP READS UP. ADJUSTED NR 5 POSITION TRANSMITTER PER MM. 2L72 4F RTA1NM 20050824001552005082400155 2005 8 24 DL777050460 420050817A23301302004002 CRADLE BOEING777 777232 1385232NM 3A UNSERVICEABLE A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27862DA 0335 29734 UPCU AT 3A SPARKED WHEN CORD PINCHED IN SEAT ASSY. FOUND CORD ON CRADLE SPARKED. REMOVED AND REPLACED CRADLE. 2L72 4F RTT00001SE 20050824001572005082400157NM 2005 8 24 DLM90050464 120050819A2750222010003 CONTROL UNIT DOUG MD900 MD900 3027375NM PYLON FLAPS FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27903DA 53383 ELEVATOR SPLIT MSG AND PYLON FLAP FAULT MSG ILLUM IN FLT. REPLACED ACU, ALL DIAGNOSTIC TESTS PASSED. 1G72 3U NCH19NM 20050824001602005082400160NM 2005 8 24 DL73S050432 120050807A3350 POWER SUPPLY BOEING737 737232 1384475NM EMERGENCY LIGHTSINOPERATIVE A DALAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO27309DL 23081 AFTER PUSHBACK AND NR 2 ENGINE START FLT ATTEND INFORMED US THAT CERTAIN EMERG LIGHTS WERE ILLIMINATED. CYCLED COCKPIT AND AFT FLT ATTEND SWS. LIGHTS REMAINED ON. REPLACED FWD POWER SUPPLY M1132. ALL CKS GOOD. 2L72 4F RTA16WE 20050824001612005082400161NM 2005 8 24 DL76G050433 120050807A4920 APU BOEING767 767332 1382001NM GE CF6 CF680 30025NE APU BAY CONTAMINATED A DALAA UNSCHED LANDING CJ F.O.D. WARNING INDICATION TXTAXI/GRND HDL 1 SO271612T10300 P2631 30575 P2631 APU FAULT ON START OF LEFT ENGINE. APU WOULD NOT RESTART. REMOVED PLASTIC BAG FROM INLET AND REPLACED SURGE VALVE. 2L72 4F4 FRTA1NM E13NE 20050824001632005082400163NM 2005 8 24 DL764050437 120050808A2121 BEARING BOEING767 767332 1382001NM RECIRC FAN FAILED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27825MH 29696 SMOKE FUMES IN THE CABIN. RT RECIRC FAN AND FWD IFE COOLING STATUS MESSAGE. ACCOMPLISHED SMOKE REMOVAL CHECKLIST AND SMOKE DISSIPATED. RT RECIRC FAN C/B POPPED INFLT. REPLACED FAN. 2L72 4F RTA1NM 20050824001662005082400166 2005 8 24 DL76G050441 420050808A3420346001053 ADC BOEING767 7673P6 1385105NM LEFT FAILED A DALAA UNSCHED LANDING I FLT. ATTITUDE INST. CLCLIMB 1 SO27156DL 25354 L ADC COMPUTER FAILED. LGW MTCCA, REPLACED L ADC A/C MM 34-12-01-404-006. OPS CHKS SATISFACTORY. 2L72 4F RTA1NM 20050824001672005082400167NM 2005 8 24 DL76S050465 120050818A3300333780101 BATTERY PACK BOEING767 767332 1382001NM EMERGENCY LIGHTSFAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27132DN 24981 WHILE TS 2R DOOR EXT EMERG LIGHT FOUND RT WING OVERWING EGRESS LIGHTS INOP AND LT SLIDE LIGHTS INOP ALSO FOUND 2L EXT EMERG LIGHT INOP. RELAMPED 2L EXT EMERG LIGHT OPS CKS OK REPLACED M731 AND M738 PWR SUPPLIES AND BATTERIES RT O WING EGRESS LIGHTS AND LT WING SLIDE LIGHTS CKS OK. 2L72 4F RTA1NM 20050824001682005082400168NM 2005 8 24 DL76G050466 120050819A2530828450407 OVEN BOEING767 7673P6 1385105NM AFT GALLEY ODOR A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27155DL 25269 AFT GALLEY OVEN ELEC SMELL. REPLACED SAME. 2L72 4F RTA1NM 20050824001702005082400170WP 2005 8 24 ABXA050188 120050813A5250 KNOB DOUG DC9 DC932F 3022067WP COCKPIT DOOR LOOSE A ABXAK NONE O OTHER NRNOT REPORTED 1 GL23904AX 47040 COCKPIT DOOR LATCH MECHANISM INOP FROM OUTSIDE COCKPIT AND DOOR WAS DIFFICULT TO OPEN AND CLOSE. RESECURED SCREWS IN DOOR HANDLE OPERATES PROPERLY AT THIS TIME. 2L72 4F A6WE 20050824001742005082400174NM 2005 8 24 SWAA052532 120050822A53106545829 CREASE BEAM BOEING737 7373H4 1384600NM CABIN FLOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29617SW 27700 DURING SCHEDULED D-CHECK, FOUND FUSELAGE CREASE BEAM WEB CORRODED BETWEEN BS 294.5 TO BS 360, LBL 70.53. REPAIRED CREASE BEAM PER SRM. 2L72 4F RTA16WE 20050824001752005082400175NM 2005 8 24 SWAA052533 120050822A55516551524 FITTING BOEING737 7373H4 1384600NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29617SW 27700 DURING SCHEDULED D-CHECK, FOUND LT & RT HORIZONTAL STAB FITTING LUG FACES CORRODED. REPAIRED LUG FACES PER SRM. 2L72 4F RTA16WE 20050824001772005082400177NM 2005 8 24 SWAA052535 120050818A3350101114 COVER BOEING737 7373Q8 1384670NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 LEFT OVERWING EMERGENCY EXIT SIGN COVER MISSING. INSTALLED COVER PER MM. 2L72 4F RTA16WE 20050824001782005082400178SO 2005 8 24 CHQA200500144 120050818A2611FDS765A2 SMOKE DETECTOR EMB 145 EMB145LR 3260212SO LAVATORY UNSERVICEABLE A CHQAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL11579RP 14500871 FLIGHT 6410 CMH-BOS - ON TAKEOFF ABOUT 1000 AGL, LAVATORY SMOKE BELL WENT OFF. F/A REPORTED THAT THERE WAS NOT ANY SMOKE IN THE CABIN. DID NOT DECLARE AN EMERGENCY. AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. PASSENGERS WERE NOT PREPARED FOR AN EMERGENCY EVACUATION, AS THERE WAS NO SMOKE, AND NO REASON TO SUSPECT A FIRE. REMOVED AND REPLACED LAVATORY SMOKE DETECTION PANEL AND LAVATORY SMOKE SENSOR. RAN ENGINE AND COULD NOT DUPLICATE. 2L72 4T RTT00011AT 20050824001792005082400179NM 2005 8 24 C1HA200597002 120050814A2750652661452 TRANSMISSION BOEING727 727270 138408PNM FLAP INOPERATIVE A C1HAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 GL15697CA 5430 23052 AFTER LANDING FLAP INDICATOR FLAPS STUCK ON 8 DEG (INBOARD) C/B`S CLOSED. PERFORMED ADJUSTMENT, FOUND SHEERED PIN ON OUTPUT DRIVE GEAR OF NR 5 FLAP TRANSMISSION R@RED NR 5 FLAP TRANSMISSION PER MM 27-51-41. 2L73 4F RTA3WE 20050824001822005082400182CE 2005 8 24 DXTA200500904 120050817A3241 ANTI-SKID SYS CESSNA500 560CESSNA 2076750CE MLG MALFUNCTIONED E DXTAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL07331QS 5600331 ANTI SKID ACTIVATES INTERMITTANTLY BELOW 5KTS. COMPLETELY ACTIVATES WITH MODERATE BRAKE PRESSURE, RESULTING IN NO BRAKES AT ALL. ANTISKID OFF BRAKES NORMAL. ALL ELECTRICAL SIGNALS CHECK OK IAW 560 M/M WIRING 32-48-01. BIT CHECK, CHECKS OK IAW 560 MM 32-40-00, DYNAMIC BIT TEST CHECKS OK IAW 560 MM 32-42-00. ACCOMPLISHED ANTI-SKID BRAKE SYSTEM CHECK IAW 560 MM CH 32-42-00. 2L72 4F RTA22CE 20050824001872005082400187NM 2005 8 24 SWAA052494 120050819A5210507945 DOOR BOEING737 7373H4 1384600NM L1 STIFF A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 L1 DOOR HARD TO OPEN OR CLOSE. ADJUSTED DOOR PER MM. 2L72 4F RTA16WE 20050823000922005082300092NM 2005 8 23 AWXA200500976 120050807A532065176859 SHEAR WEB BOEING737 7373Y0 1384671NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28334AW 23747 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED SHEAR WEB FROM BS 328 TO BS 344, STR 13L TO STR 16L, CRACKED AT REPAIR PLATE. MAINTENANCE REMOVED CRACKED PLATE ON SHEAR WEB FROM BS 328 TO BS 344, STR 13L TO STR 16L IAW BOEING 737-300 SRM 51-40-02-0 FIG 8. FABRICATED REPLACEMENT REPAIR PLATE IAW BOEING 737-300 SRM 51-70-13-0 AND 51-40-05-0. INSTALLED PLATE ON SHEAR WEB FROM BS 328 TO BS 344, STR 13L TO STR 16L IAW BOEING 737-300 SRM 51-40-02-0 AND 51-70-13-0. 2L72 4F RTA16WE 20050823001072005082300107NM 2005 8 23 05FDEA02465 120050815A5314 KEELBEAM DOUG MD11 MD11 3023602NM ZONE 700 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 CENTER LANDING GEAR FORWARD BULKHEAD, RT KEELBEAM DOUBLER FOUND CRACKED AS MARKED. REMOVED AND REPLACED WITH NEW DOUBLER AS PER SRM 51-31-01. 2L73 4F RTA22WE 20050823001092005082300109NM 2005 8 23 05FDEA02467 120050815A5280 DOOR DOUG MD11 MD11 3023602NM ZONE 700 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 SNRM N0364: RIGHT HAND MAIN LANDING GEAR FLIPPER DOOR FOUND WITH CRACK AS MARKED. REMOVED AND REPLACED WITH NEW PART AS PER AMM 32-14-10-4. ADJUSTMENT TEST CARRIED OUT AS PER AMM 32-31-00-5, FOUND SATIS. 2L73 4F RTA22WE 20050823001142005082300114EA 2005 8 23 SWIA200515420 120050813A5610 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT FAILED A SWIAO OTHER O OTHER DEDESCENT 1 NM07956SW 7825 LEFT SIDE WINDOW SHATTERED IN FLIGHT DECK. REPLACED LEFT SIDE WINDOW IAW CRJ MM 56-12-01, PN OFF: 60R33033-11 SN OFF: 03062H7719. 2L72 4F RTA21EA 20050823001172005082300117SO 2005 8 23 SWIA200515423 120050813A3397 CONNECTOR EMB 120 EMB120ER 3260203SO LOOSE LOOSE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07251YV 120251 ONE SECTION OF FLOOR LEVEL EMERGENCY LIGHTS ARE INOP ROW 3, 4, AND 5. RESECURED CONNECTOR FOR EMERGENCY LIGHTS FOR ROW 3, 4, AND 5, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050823001202005082300120EA 2005 8 23 SWIA200515426 120050813A274083963 CABLE CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07431SW1549515495 7536 STAB 2 INOP. REPLACED HSTCA AND MCU IAW MM 27-40-00, 27-42-01, 27-42-05. OPERATIONAL CHECK GOOD, PN 7062-3, SN/OFF 329. 2L72 4F RTA21EA 20050823001252005082300125EA 2005 8 23 SWIA200515431 120050810A2750 FLAP SYSTEM CNDAIRCL600 CL6002C10 1390015EA TE FLAPS OUT OF RIG A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 NM07719SK 10188 FLAPS FAIL MESSAGE ON CLIMB-OUT. CLEARED INHIBITS. ELECTRICALLY RIGGED FLAPS. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050823001292005082300129NM 2005 8 23 UPS05545213 120050720A5347146N52191 SEAT TRACK BOEING757 75724APF 1384969NM MCD CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01401UP 23723 SEAT TRACK CORRODED BS 1320 RBL 46 WL 208. REMOVED AND REPLACED SEAT TRACK BS 1320 - 1349.5 RBL 45 IAW SRM 53-00-52. 2L72 4F RTA2NM 20050823001332005082300133NM 2005 8 23 UPS05545217 120050720A5347143N52785 SEAT TRACK BOEING757 75724APF 1384969NM MCD CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01401UP 23723 CORROSION ON SEAT TRACK AT FASTENERS AFT OF FLOORBEAM, STA 441 WL 208 RBL 45. REPLACED SEAT TRACK SECTION, BS 440 - 490, RBL 45, WL 208 PER SRM 53-00-5202R 5, FIG 201. 2L72 4F RTA2NM 20050823001392005082300139WP 2005 8 23 UPS05845222 120050801A53403755827502 FITTING DOUG DC8 DC873F 302199FWP FS 348 L31R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 A PIT STA 348 L31R ZEE FITTING CRACKED 3 INCHES LONG. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20050823001482005082300148EA 2005 8 23 SWIA200515440 120050814A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY MALFUNCTIONED A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07587SW 7062 CARGO SMOKE MESSAGE ON ED-1 AFTER PERFORMING CARGO SMOKE TEST. REPLACED NR 2 CARGO SMOKE DETECTOR IAW MM 26-15-01. OPERATIONAL CHECK GOOD, PN 473597-19; SN OFF 1727. 2L72 4F RTA21EA 20050823001512005082300151 2005 8 23 UPS05145244 420050821A2565D31023101 SLIDE AIRBUSA300 A300F4622R 3930360EU CABIN DEPLOYED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01134UP 0817 SLIDE INADVERTANTLY DEPLOYED. REMOVED AND REPLACED DOOR SLIDE PER MM 25-61-21. OPS CK OK. 2L72 4F RTA35EU 20050823001582005082300158WP 2005 8 23 UPS05845232 120050811A5340SAA37798742 FITTING DOUG DC8 DC871F 302199DWP FS 834.500 L18L CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 FRAME TO INTERCOSTAL ATTACHED FITTING CRACKED AT F/S 834.500 L18L. REMOVED AND REPLACED INTERCOSTAL ATTACH FITTING IAW SRM 51-1-20D. 2L74 4F RT4A25 20050823001782005082300178WP 2005 8 23 05FDEA02562 120050819A5712 RIB DOUG DC10 DC1010 3022110WP RT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 RT WING OUT;B L/E INTERNAL STRUCTURE FOUND 1EA ANGLE REPAIR ON RIB AT XORS 567. FABRICATED REPAIR ANGLE IAW SRM 57-20-00 FIGURE 1 VOL.1. 2L73 4F A22WE 20050823001802005082300180WP 2005 8 23 05FDEA02564 120050819A5712 RIB DOUG DC10 DC1010 3022110WP RT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 RT WING OUT'B L/E INTERNAL STRUCTURE FOUND 1EA ANGLE REPAIR ON RIB AT XORS 460. FABRICATED REPAIR ANGLE IAW SRM 57-20-00 FIGURE 1 VOL.1. 2L73 4F A22WE 20050823001822005082300182WP 2005 8 23 05FDEA02566 120050819A5712 RIB DOUG DC10 DC1010 3022110WP RT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 RT WING OUT'B L/E INTERNAL STRUCTURE FOUND 1 EA ANGLE REPAIR ON RIB AT XORS 930. FABRICATED REPAIR ANGLE IAW SRM 57-20-00 FIGURE 1 VOL.1. 2L73 4F A22WE 20050823001842005082300184WP 2005 8 23 05FDEA02568 120050819A5730 SKIN DOUG DC10 DC1010 3022110WP LT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LT WING INB'D L/E FOUND 1EA EXTERNAL DOUBLER REPAIR ON SKIN AT XORS 87. REPAIRED IAW SRM 57-10-00 FIGURE 40 VOL.1. 2L73 4F A22WE 20050823001852005082300185WP 2005 8 23 05FDEA02569 120050819A5313 LONGERON DOUG DC10 DC1010 3022110WP FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 UPPER FUSELAGE INTERNAL AFT BODY FOUND 1EA LONGERON REPAIRED BTW STA 2122 TO STA 2163 LONGERON 50 LT SIDE. REPAIRED IAW SRM 53-00-01 FIGURE 7 VOL.1. 2L73 4F A22WE 20050823001882005082300188WP 2005 8 23 05FDEA02572 120050819A5510 BULKHEAD DOUG DC10 DC1010 3022110WP HORIZONTAL STAB DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 DISCREPANCY: HORIZONTAL STABILIZER CONSTANT SECTION FOUND 1EA DOUBLER REPAIR ON AFT BLKHD AT STA 2123 X=40 LH SIDE. CORRECTIVE ACTION: REPAIRED IAW SB 55A028 AND DWG SR10550007. 2L73 4F A22WE 20050823001902005082300190WP 2005 8 23 05FDEA02574 120050819A5730 SKIN DOUG DC10 DC1010 3022110WP LT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LT WING TIP FOUND 1EA EXTERNAL DOUBLER REPAIR ON EXTERNAL SKIN. REPAIRED IAW SB 57-27 2L73 4F A22WE 20050823001952005082300195NM 2005 8 23 05FDEA02547 120050819A57536521796108A FAIRING BOEING727 727200 138407ENM RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 NR 8 FLAP TRACK MOVABLE FAIRING HINGE FITTING IS CRACKED. REPLACED FLAP TRACK FAIRING ON WC 76C001-04 2L73 4F RTA3WE 20050824000112005082400011NM 2005 8 24 2005UALA00818 120050811A2120 SMOKE BOEING757 757222 1384956NM PWA 2037 PW2037 NE COCKPIT DETECTED A UALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP29526UA 24994 STRONG SMOKE ODOR IN FLIGHT DECK AND SMOKE ODOR AT ROW 16. THE SMELL IN THE CABIN WAS CORRECTED BY SEVERAL RELATED ACTIONS DURING THE TROUBLESHOOTING OF THE AIRCONDITIONING SYSTEM. THE PACKS WERE RECYCLED AND SEVERAL FILTERS WERE REPLACED. NOTE: OVEN WAS REMOVED AND SENT TO HOMESHOP FOR INSPECTION AND SERVICE. NO FINDINGS REPORTED TO INDICATE MALFUNCTION WITH AN OVEN. 2L72 4F4 FRTA2NM E17NE 20050824000142005082400014NM 2005 8 24 2005UALA00821 120050813A3350362624 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE R0W 48 INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29116UA 26908 SEAT EEL LIGHT INOP AT ROW 48 HJK. REPLACED LIGHT ASSY. 2L74 4F4 FRTA20WE E24NE 20050824000152005082400015NM 2005 8 24 2005UALA00822 120050813A3350362624 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE ROW 44 INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29116UA 26908 SEAT EEL LIGHT INOP, AT 44 ABC. REPLACED LIGHT ASSY. REPLACED LIGHT ASSY. 2L74 4F4 FRTA20WE E24NE 20050824000182005082400018NM 2005 8 24 2005UALA00825 120050813A33501317 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE COCKPIT BURNED OUT A UALAK NONE L NO TEST ININSP/MAINT 1 WP29116UA 26908 FLIGHT DECK CEILING EMERGENCY LIGHT INOP. REPLACED LAMP. 2L74 4F4 FRTA20WE E24NE 20050824000202005082400020NM 2005 8 24 2005UALA00827 120050815A3350582233 BATTERY BOEING747 747422 1384935NM PWA 4056 PW4056 NE 46 ABC DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29199UA 28717 SEAT EEL LIGHTS INOP FROM ROWS 46 ABC THROUGH 54 ABC. REPLACED BATTERY ASSY. 2L74 4F4 FRTA20WE E24NE 20050824000262005082400026EU 2005 8 24 2005UALA00833 120050815A2910 HYDRAULIC SYSTEM AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE GREEN SYS FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29435UA 613 GREEN HYDRAULIC SYSTEM FAILURE AND YELLOW SYSTEM OVERHEAT. 2L72 4F4 FRTA28NM E40NE 20050824000392005082400039NM 2005 8 24 2005UALA00846 120050818A5320 ANGLE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE AFT GALLEY DOOR CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29327UA 24147 AFT GALLEY DOOR THRESHOLD ZEE ANGLE CORRODED STA 978 TO 984 RBL 62.5 STR 17 WL 208. 2L72 4F4 FRTA16WE E2GL 20050824000442005082400044NM 2005 8 24 2005UALA00851 120050818A2751 WARNING LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE TE FLAPS ILLUMINATED A UALAO OTHER J WARNING INDICATION NRNOT REPORTED 1 WP29318UA 23950 FLT SHOWED LE FLAPS IN TRANSIT LIGHT. AMBER ALERT CALLED IN. A FAILED LEADING EDGE (LE) FLAP AND SLAT CONTROL VALVE INHIBITED FULL EXTENTION OF THE LE FLAPS AND SLATS. SUBJECT FAILURE CONSIDERED AN ISOLATED INCIDENTCORRECTIVE ACTION: REPLACED AND TESTED SUBJECT LE FLAP/SLAT CONTROL VALVE PER MAINTENANCE MANUAL (MM) 737-27-81-81 AND TESTED AUTO SLAT & STANDBY PER 737 MM 27-83-00. AND ALL OPS CHECKS NORMAL.FAILURE FINDINGS : TBDMAINTENANCE PROGRAM: ON-CONDITION 2L72 4F4 FRTA16WE E2GL 20050824000502005082400050EA 2005 8 24 SWIA200515447 120050818A274183963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07431SW3801 3801 7536 STAB TRIM CHANNEL ONE INOP MESSAGE ON DESCENT. REPLACED HORIZONTAL STAB TRIM ACTUATOR AND MOTOR CONTROL UNIT MM 27-42-01 AND 27-42-05, OPERATIONAL CHECK GOOD, PN 7062-3, SN OFF 1212. 2L72 4F RTA21EA 20050824000542005082400054EU 2005 8 24 MALA050653 120050815A7933 GAUGE SAAB SF340 340B 7860101EU PROP TEMP ERRATIC A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15414XJ 340B414 RT PROP TEMP GAUGE ERRATIC, BOUNCING IN AND OUT OF RED ARC. REMOVED AND REPLACED TEMP PRESS GAUGE PER SAAB AMM SN ON 9709661A, SN OFF 9701324A. OPS CHECK GOOD. REMOVED AND REPLACED RT PGB OIL TEMP IAW CT7 79-00-00. OPS CHECK GOOD PN4053T73P01. 2L72 4T RTA52EU 20050824000612005082400061EU 2005 8 24 MALA050655 120050816A2920AIR917621 CONTROL VALVE BAC 146 AVRO146RJ85A1500097EU HYD PTU FAILED A MALAO OTHER F FLT CONT AFFECTED CRCRUISE 1 GL15515XJ E2333 CREW RETURNED TO DTW FOLLOWING FAILURE OF THE YELLOW HYDRAULIC SYSTEM. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. REPLACED PTU FLOW CONTROL VALVE AND ASSOCIATED SEALS. REF AVRO AMM CH 29-20-24 PN AIR91762-1, SN ON LK8505340. SERVICED/BLED SYSTEM. 2H74 4F RTA49EU 20050824000622005082400062EU 2005 8 24 MALA050656 120050816A5753 SKIN SAAB SF340 340B 7860101EU LT TE FLAP DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15362PX 1313 340B258 DURING 4Y/2Y INSPECTION IN BNA, FOUND LT FLAP, L/E HAS HEAT DAMAGE. DAMAGE HAS BEEN REPAIRED IAW MESABA EO#$57100. REF: EAMS WORK ORDER 212767, PN7257800-573, SN 1313. 2L72 4T RTA52EU 20050824000782005082400078EU 2005 8 24 MALA050664 120050817A2432 BATTERY BAC 146 AVRO146RJ85A1500097EU MASTER FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15534XJ E2370 FAILED CAP CHECK. 2H74 4F RTA49EU 20050824000792005082400079EU 2005 8 24 MALA050657 120050816A5311 FRAME SAAB SF340 340B 7860101EU FUSELAGE CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15362PX 340B258 DURING 4Y/2Y INSPECTION IN BNA, FOUND FRAME AT FS 464, RT SIDE IS CHAFED AND HAS BEEN REPAIRED IAW MESABA EO 53310. 2L72 4T RTA52EU 20050824000822005082400082NM 2005 8 24 SWAA052522 120050822A53306545766 SKIN BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29369SW 26580 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 468, BL 0, AT DME ANTENNA NR 1 CUTOUT. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050824000882005082400088NM 2005 8 24 SWAA052528 120050822A53116546539 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29612SW 27930 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CHORD CRACKED AT BS 616, RBL 65, WL 200. REPAIRED FRAME CHORD PER BFG ER. 2L72 4F RTA16WE 20050824000922005082400092NM 2005 8 24 BB05070 120050823A335020121 CHARGER BOEING757 7572B7 1384964NM RROYCERB211 RB211535E4 54555NE CABIN FAULTY A USAAK NONE O OTHER ININSP/MAINT 1 EA19627AU 27805 THE L-2 EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK CHARGER ASSEMBLY. OPERATIONALLY CHECKS OK. 2L72 4F4 FRTA2NM E12EU 20050824001012005082400101 2005 8 24 ASMF200508009 420050818A34214055900905 SYMBOL GENERATOR DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE INOPERATIVE W ASMFA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW23216AM2591125911 49586 AIRCRAFT RETURNED OF FLIGHT, DURING ROTATION HEARD A LOUD NOISE IN THE NOSE LANDING GEAR, LOOSING AHRS 2 WITH HEADING, HORIZON LIGHTS TURNED ON, FMA AND RIGHT ND WITHOUT INFORMATION. AHRS 2 AND 3 WERE SWAPPED IAW MM 34-21-10 AND VISUAL INSPECTION OF NLG WAS PERFORMED WITHOUT DAMAGE DETECTED IAW MM 32-20-00. SYMBOL GENERATOR AND AHRU 2 WERE REPLACED IAW MM 34-21-10, TESTED CORRECT. 2L72 4F4 FRTA6WE E9NE 20050824001042005082400104 2005 8 24 ASMF200508006 420050815A2210 COMPUTER DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE COCKPIT FAILED W ASMFO OTHER J WARNING INDICATION CRCRUISE 1 SW23945AS 49643 AIRCRAFT RETURNED OF FLIGHT, BOTH DFGC OUT OF SERVICE. THE DFGC RTC BITE WERE PERFORMED IAW MM 22-01-05, TESTED CORRECT. THE OVERWEIGHT LANDING CHECK WAS PERFORMED IAW MM 05-51-04, ALL CORRECT. DURING OVERNIGHT CHECK, BOTH DFGC TESTS WERE PERFORMED IAW MM 22-01-00, BEING CORRECT. 2L72 4F4 FRT E9NE 20050824001052005082400105WP 2005 8 24 ASMF200508007 120050816A2620 AUGMENT VALVE KIDDE DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE FIRE BOTTLE OUT OF ADJUST W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23803ML11493 91928EJ 49726 AIRCRAFT RETURNED TO PLATFORM, DURING THE LT ENGINE START, THE FIRE EXTINGUISHER AGENT 2 LOW LIGHT TURNED ON. THE FIRE EXTINGUISHER POSITION 2 WAS REPLACED IAW MM 26-20-01; LT AUGMENTING VALVE WAS ADJUSTED IAW MM 36-10-01; THE CLAMS OF AUGMENTING VALVE AND REGULATOR VALVE WERE REPLACED IAW MM 20-10-11 AND LEAKS CHECK WAS PERFORMED IAW MM 21-10-00, MM 30-10-00 AND MM 36-10-00, TESTED CORRECT. 2L72 4F4 FRTA6WE E9NE 20050824001062005082400106SO 2005 8 24 08222005 220050822A8500536379 BOLT CONT CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO ENGINE SHEARED G HYIAK NONE O OTHER ININSP/MAINT 1 NE016875D2270 2270 828512R 402C0511 828512R PROPELLER FAILED TO TURN ON START. CRANKSHAFT LARGE ATTACH BOLTS SHEARED AND GEAR DISLODGED FROM CRANKSHAFT. ENGINE REMOVED AND REPLACED. 1L72 3O3 O A7CE E8CE 20050824001072005082400107NM 2005 8 24 ASMF200508011 120050820A2910 O-RING DOUG MD88 MD88 3023688NM HYD SYSTEM LEAKING W ASMFK NONE KJ FLUID LOSS WARNING INDICATION ININSP/MAINT 1 SW23158PL 49761 DURING TRANSIT CHECK, DETECTED HYDRAULIC LEAK IN NOSE LANDING GEAR. AIRCRAFT WAS SENT TO THE HANGAR AND NOSE LANDING GEAR STRUT O-RING SEALS WERE REPLACED IAW MM 32-21-02, TESTED CORRECT. 2L72 4F RTA6WE 20050824001152005082400115WP 2005 8 24 MWEA050084 120050818A534759305477 SEAT TRACK DOUG DC9 DC982 3022082WP COCKPIT CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 SEAT TRACK, TWO SCREWS MISSING AT STATION 1270 AND CORROSION AROUND THE HOLE. FABRICATED AND INSTALLED SEAT TRACK. 2L72 4F A6WE 20050824001162005082400116WP 2005 8 24 MWEA050085 120050818A5347800484 SEAT TRACK DOUG DC9 DC982 3022082WP STA 207 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 SEAT TRACK CORRODED AT STATION 207. FABRICATED AND INSTALLED SEAT TRACK. 2L72 4F A6WE 20050824001262005082400126WP 2005 8 24 ABXA050196 120050808A53105912285509 WINDOW FRAME DOUG DC9 DC941 302207NWP CABIN CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23965AX 47498 TOP FORWARD CORNER OF WINDOW FRAME ON AFT SIDE OF STA 737 LEFT WAS CRACKED. REPAIRED AREA IAW DC-9 SSRM K07226. 2L72 4F A6WE 20050824001312005082400131WP 2005 8 24 MWEA050093 120050823A53305911410347 SKIN DOUG DC9 DC982 3022082WP STA 484 DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 DENT IN LEFT SIDE OF FUSELAGE 16 INCHES FROM THE LOWER FORWARD CORNER OF THE POTABLE WATER SERVICE PANEL, STATION 484 BETWEEN LONGERON 22 AND 23. FABRCATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20050824001352005082400135WP 2005 8 24 ABXA050191 120050809A531199118594 FRAME DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 FRAME 1104 CANTED CRACKED AT LONGERON 14 RIGHT AND LONGERON 15 RIGHT. REMOVED AND REPLACED FRAME IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20050824001362005082400136WP 2005 8 24 AALA20050543 120050821A3260 PROXIMITY SENSOR DOUG DC9 DC982 3022082WP MLG INOPERATIVE A AALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW21470AA 49600 DFW INFLIGHT T490/21AUG, NOSE LANDING GEAR INDICATION. TRIED TO RECYCLE GEAR TWO TIMES. SECOND TIME LEFT THE GEAR DOWN AND RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED PROXIMITY SENSOR FOR NOSE LANDING GEAR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050824001432005082400143NM 2005 8 24 AALA20050541 120050811A5310 FAILSAFE BOEING767 767323 1385205NM CARGO DOOR CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21355AA 24036 AFW - LOWER MAIN SILL FAIL SAFE STRAP AT CARGO DOOR HAS CORROSION REMOVED ON LOWER SURFACE. AREA AFFECTED IS 5 INCHES BY 2 INCHES WITH A DEPTH OF .076 INCH. MATERIAL REMAINING BEYOND SRM LIMITS. REMOVED CORROSION AND PERFORMED HIGH FREQUENCY EDDY CURRENT INSPECTION ON SURFACE AND OPEN HOLE. INSTALLED FASTENERS WET. ALODINED AND APPLIED TWO COATS OF PRIMER. 2L72 4F RTA1NM 20050824001542005082400154NM 2005 8 24 DL777050459 120050817A2150TRENT892 A/C PACK BOEING777 777232 1385232NM NR 1 ENGINE ODOR A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO27865DA23089 29737 A/C HAS STRONG OIL SMELL. RAN PACKS FOR 1 HOUR. CHECKED A/C SYSTEMS. NTF. 2L72 4F RTT00001SE 20050824001592005082400159NM 2005 8 24 DL757050431 120050806A2110381702020 COMPRESSOR BOEING757 757232 1384965NM AFT CARGO FAILED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27662DN 24991 DURING DE-PLANING NOTICED SMOKE AND FUMES IN AFT CABIN FROM ROW 20 TO AFT GALLEY. REPLACED POTABLE WATER COMPRESSOR. 2L72 4F RTA2NM 20050824001652005082400165NE 2005 8 24 DL76G050440 220050808A7250CF680C2B6F BLADES BOEING767 767332 1382001NM GE CF6 CF680C2B6F 30025NE NR 1 ENGINE TORN A DALAD RETURN TO BLOCK MJ OVER TEMP WARNING INDICATION TXTAXI/GRND HDL 1 SO271610D2419824198 30594 704824 DURING TAXI AND NR 1 ENGINE START EGT WENT TO 849 ANALOG A/C ADVISED TO RTB. DURING T/S, N2 WENT TO ONLY 42.9 PERCENT AND EGT WAS ABOVE 750 FOR 2.5 MIN DAMAGE FOUND TO 1ST AND 3RD HPC. REPLACED ENGINE. 2L72 4F4 FRTA1NM E13NE 20050824001692005082400169NE 2005 8 24 ABXA050189 220050817A7200 ENGINE DOUG DC8 DC863 302198AWP PWA JT3D JT3D3B 52039NE NR 2 FAILED A ABXAE ENGINE SHUTDOWN Y ENGINE STOPPAGE CRCRUISE 1 GL23813AX4593 46136 669577 LOW OIL PRESSURE LIGHT NR 2 ENGINE OIL PRESSURE DROPPED TO 30 PSI. SHUT DOWN NR 2 ENGINE DOWN AT 0350Z. ZERO OIL PRESSURE AFTER ENGINE SHUT DOWN. REMOVED AND REPLACED NR 2 ENGINE IAW JOB CARD 8090507 AND WORK PACK 600230688. 2L74 4F4 F 4A25 1E8 20050824001862005082400186CE 2005 8 24 DXTA200500905 120050817A2720991455811 ACTUATOR CESSNA750 750 2076810CE RUDDER FAILED E DXTAO OTHER J WARNING INDICATION CRCRUISE 1 GL07982QS918 7500182 RUDDER LIMIT FAIL A EICAS MESSAGE. CONTROL PAGE SHOWS 43 PERCENT RUD LIMIT. REMOVED UPPER RUDDER -A- LINEAR ACTUATOR DUE TO INTERNAL FAILURE. INSTALLED OVERHAULED UNIT. OPERATIONAL CHECK WAS GOOD. WORK WAS DONE IAW CE-750 MM 27-23-00. 2L72 4J RTT00007WI 20050824001882005082400188 2005 8 24 SWAA052495 420050820A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20050824001892005082400189NM 2005 8 24 SWAA052496 120050817A53306545775 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 865 TO BS 872, STR 16L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050824001912005082400191 2005 8 24 SWAA052498 420050821A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29335SW 23939 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20050824001932005082400193NM 2005 8 24 SWAA052500 120050821A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29369SW 26580 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 359, STR 14L. REMOVED AND REPLACED STRINGER PER SRM. 2L72 4F RTA16WE 20050824001942005082400194NM 2005 8 24 SWAA052501 120050821A53306545769 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29369SW 26580 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 378.5, LBL 2.8, AFT SIDE OF E & E COOLING EXHAUST PORT. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050824001952005082400195NM 2005 8 24 SWAA052502 120050819A335007912 COVER BOEING737 7377H4 1384404NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29401WN 29813 EEPLS TRACK COVER BROKEN AT ROW 1 ABC. REMOVED AND REPLACED COVER PER MM. 2L72 4F RTA16WE 20050824001962005082400196NM 2005 8 24 SWAA052503 120050820A33506042221 LIGHT BOEING737 7377H4 1384404NM AFT GALLEY BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29414WN 29820 R2 DOOR LOWER EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20050824002012005082400201 2005 8 24 SWAA052508 420050820A2565D31354 SLIDE BOEING737 7375H4 138449DNM R1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29526SW 26568 DURING SCHEDULED SERVICE CHECK, R1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20050825000212005082500021NM 2005 8 25 SWAA052520 120050817A53306545777 SKIN BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 986.5, BETWEEN STR 26L TO STR 27L. MX FERRY TO DAL FOR REPAIRS. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050825000232005082500023SO 2005 8 25 C2XA05BT052 120050728A335078241 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT FAULTY A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715983 145239 DURING SERVICE ROUTINE CHECK, MAINTENANCE FOUND THE COCKPIT STEP UP AND FORWARD OVERHEAD EMERGENCY LIGHTS NOT WORKING. REMOVED AND REPLACED NR 1 EMERGENCY LIGHT INVERTER IAW EMB AMM NR 33-50-10, OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050825000242005082500024SO 2005 8 25 C2XA05BT053 120050728A335020131A BATTERY EMB 145 EMB145EP 3260221SO EMERGENCY LIGHT FAULTY A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712934 145019 CREW REPORTED, EMERGENCY LIGHT WAS NOT WORKING. MAINTENANCE REMOVED AND REPLACED ALL EMERGENCY LIGHT BATTERIES IAW EMB145 AMM NR 33-50-04, OPS CHECKED GOOD. 2L72 4F RTT00011AT 20050825000252005082500025SO 2005 8 25 C2XA05IA094 120050723A3350110049 POWER SUPPLY EMB 145 EMB145 3260210SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712957 145080 DURING MAINTENANCE INSPECTION, THE RIGHT FORWARD EXTERNAL EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO EMERGENCY LIGHT POWER SUPPLY, OPERATIONALLY TESTED WITHOUT DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050825000262005082500026NM 2005 8 25 AWXA200500990 120050822A3397BMS13311122 WIRE BOEING737 7373Y0 1384671NM EMERGENCY LIGHT INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 PHX - EEL - DURING 8 DAY CHECK, DISCOVERED EMERGENCY ESCAPE PATH LIGHTING FOR SEAT 11 TO 15 ON THE LT SIDE INOPERATIVE. MAINTENANCE REPAIRED A WIRE AT SEAT 15 IAW BOEING 737-300 WDM TR 33-042AW. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20050825000272005082500027SO 2005 8 25 C2XA05RI017 120050808A33977287503519 WIRE HARNESS EMB 145 EMB145LR 3260212SO CABIN LIGHT BURNED A C2XAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW2717984 145246 FLT 2969 - RIC - PRE-FLIGHT - DURING PRE-FLIGHT INSPECTION, SIDE WALL LIGHT AT SEAT 2A WAS SMOKING. RIC MAINTANACE REMOVED AND REPLACED LAMP HARNESS ASSY AND PERFORMED OPERATIONAL TESTS. OPS TEST GOOD. ACFT WAS APPROVED TO RETURNED TO SERVICE. 2L72 4T RTT00011AT 20050825000282005082500028SO 2005 8 25 C2XA05SD026 120050805A2560 DIODE EMB 145 EMB145LR 3260212SO FLASHLIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713903 145479 SDF - REAR CABIN EMERGENCY FLASHLIGHT LED INOP. REMOVED AND REPLACED REAR CABIN FLASHLIGHT ASSY. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050825000302005082500030SO 2005 8 25 C2XA05BT057 120050805A335066903 LIGHT EMB 145 EMB145LR 3260212SO CABIN FAULTY A C2XAO OTHER O OTHER NRNOT REPORTED 1 SW2712563 145612 DURING SERVICE AND ROUTINE CHECK, MAINTENANCE FOUND EMERGENCY EXIT IDENTIFIER ON SERVICE DOOR TO BE FAULTY ALSO, FORWARD FLOOR EMERGENCY LIGHT NR 1 NOT WORKING. REMOVED AND REPLACED EMERGENCY EXIT IDENTIFIER ON SERVICE DOOR IAW EMB145 AMM NR 33-50-06 AND EMERGENCY EXIT AISLE LIGHT IAW EMB145 AMM NR 33-50-08. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050825000312005082500031SO 2005 8 25 C2XA05IA097 120050804A3350BA50933901 CHARGER EMB 145 EMB145XR 3260214SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713123 145688 MCI - DURING MAINTENANCE INSPECTION, THE LEFT AND RIGHT EXTERIOR REAR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT POWER SUPPLY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20050825000322005082500032SO 2005 8 25 C2XA05CL059 120050719A3350744412 SIGN EMB 145 EMB145LR 3260212SO EMERGENCY EXIT INOPERATIVE A C2XAK NONE L NO TEST TXTAXI/GRND HDL 1 SW2713988 145265 CLE FLIGHT NR2715 - THE CREW REPORTED THE MID CABIN EMERGENCY EXIT SIGN DID NOT ILLUMINATE WHEN TESTED. MAINTENANCE REPLACED THE EXIT SIGN AND OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20050825000352005082500035EA 2005 8 25 SWIA200515451 120050820A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA ROW 10C INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07910SW 7566 ELECTROLUMINESCENT FLOOR LIGHT AT ROW 10C INOP. REPLACED PHOTO LUMINESCENT FLOOR LIGHTING AT SEAT 10 CD. OPERATIONAL CHECK GOOD REF 33-51-01. 2L72 4F RTA21EA 20050825000362005082500036EA 2005 8 25 SWIA200515452 120050822A2721 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA RUDDER TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07439SW 7578 RUDDER TRIM WILL NOT ACTUATE NOSE RIGHT. REPLACED RUDDER TRIM/AILERON TRIM CONTROL PANEL. OPERATIONAL CHECK GOOD REF MM 27-12-10. 2L72 4F RTA21EA 20050825000382005082500038EA 2005 8 25 SWIA200515454 120050821A5210 LATCH CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BINDING A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07417SW 7400 MAIN CABIN DOOR WON'T OPEN FROM OUTSIDE. CLEANED PAX DOOR LATCH PINS. CYCLED PAX DOOR HANDLE NUMEROUS CYCLES. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050825000412005082500041EA 2005 8 25 SWIA200515457 120050819A2711 TRIM PANEL CNDAIRCL600 CL6002B19 1900309EA AILERON STUCK A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07446SW 7666 AILERON TRIMS ONE DIRECTION. REPLACED AILERON TRIM PANEL. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050825000432005082500043NM 2005 8 25 DL757050467 120050820A3244326002025 BRAKE BOEING757 757232 1384965NM NR 7 UNSERVICEABLE A DALAK NONE O OTHER ININSP/MAINT 1 SO27692DL 29724 AFT LEFT TIRE ON RT MAIN GEAR MISSING BRAKE WEAR INDICATOR PINS. FOUND NR 7 BRAKE COMING APART. REMOVED AND REPLACED NR 7 BRAKE ASSY PER M/M. 2L72 4F RTA2NM 20050825000442005082500044NM 2005 8 25 DLM88050468 120050820A7160 PACKING DOUG MD88 MD88 3023688NM LT ENG NOSE BUL LEAKING A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27974DL 53242 AFTER TAKEOFF, FLIGHT ATTENDANTS NOTIFIED FLIGHT CREW THAT BOTH AFT LAV SMOKE DETECTORS WERE GOING OFF. REPLACED PACKING IN LEFT ENGINE NOSE BULLET DUE TO OIL LEAK. 2L72 4F RTA6WE 20050825000452005082500045NM 2005 8 25 DL76L050469 120050819A561083081 SEAL BOEING767 767332 1382001NM COCKPIT WINDOW DAMAGED A DALAA UNSCHED LANDING O OTHER CRCRUISE 1 SO27193DN 28450 EXTREMELY LOAD EAR PIERICING SQUEAL AT 8.0 PSID COMING FROM L2 WINDOW. REPLACED L2 WINDOW SEAL PER AMM. PRESSURIZED TO 8.0 PSID. NO SQUEAL NOTED. 2L72 4F RTA1NM 20050825000472005082500047 2005 8 25 DL76G050471 420050820A34604077880908 DISPLAY BOEING767 767332 1382001NM COCKPIT RT FAILED A DALAA UNSCHED LANDING O OTHER CRCRUISE 1 SO271612T 30575 CO-PILOTS CDU WENT BLANK DID NOT COME BACK ON. REPLACED WITH NEW CDU. OPS CKS OK. 2L72 4F RTA1NM 20050825000492005082500049WP 2005 8 25 DHL2005806503 120050815A5754 DOUBLER DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE FLAP DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH87034 46002 INTERIM REPAIR ON RT OB FLAP UPPER PLATING (STA XF 208.000-213.000) (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG. 1, SRM 57-7-1 FIG. 4, TR NR 57-94. REMOVED PLATING WITH INTERIM REPAIR ON IT IAW SRM 51-1-21 PG. 1, SRM 51-3-0 PG. 1. FABRICATED NEW PLATING (AL2024T3 0.040) IAW SRM 57-7-1 FIG. 4, TR 57-94 ITEM (C). CLEANED, TREATED AND PRIMED AREA AND NEW PLATING INNER FACE IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG. 9. INSTALLED NEW PLATING IAW SRM 51-1-21 PG. 1, SRM 51-3-0 PG.1. TORQUED IAW SRM 51-3-1 (STA XF 169.000 - 213.000) 2L74 4F4 FRT4A25 E2GL 20050825000512005082500051WP 2005 8 25 DHL2005806504 120050819A5312 STIFFENER DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE BULKHEAD CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH87034 46002 REF. NR. 041519) FWD ACCY COMPT RT PRESSURE BULKHEAD STIFFENER CRACKED 1 AT STA 8.000. REMOVED CRACKED STIFFENER IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED NEW STIFFENER (AL7075 INCH 0 INCH 0.071INCH) IAW SRM 53-3-3 FIG. 3. HEAT TREATED IAW SRM 51-1-1 PG. 1,13,17. CLEANED, TREATED AND PRIMED AREA AND STIFFENER IAW SRM 51-1-8B. INSTALLED STIFFENER IAW SRM 51-1-21, SRM 51-1-20D. TORQUED IAW SRM 51-3-1. 2L74 4F4 FRT4A25 E2GL 20050825000522005082500052EU 2005 8 25 RAIA00508026 120050819A7930 WARNING LIGHT JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE331* 01514WP LT ENGINE OIL ILLUMINATED A RAIAA UNSCHED LANDING J WARNING INDICATION TXTAXI/GRND HDL 1 CE03556HK 41073 LT ENGINE OIL CONTAMINATION LIGHT ILLUMINATED DURING TAXI. MAINTENANCE INSPECTED AND CLEANED THE MAGNETIC CHIP DETECTOR AND PERFORMED TEST OF INDICATING SYSTEM FOLLOWED BY ENGINE OPERATIONAL CHECK. 2L72 4T3 TRTA41NM E2WE 20050825000532005082500053SO 2005 8 25 RAIA00508027 120050821A2150 A/C PACK EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL FAILED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03805HK 145096 FLT 3544- RIC- PACK OVERLOAD DURING TAKEOFF. MAINTENANCE PLACED ITEM ON MEL. 2L72 4F4 FRTT00011ATTE6CH 20050825000562005082500056CE 2005 8 25 GLBA20050506 120050822A32601003810061 UPLOCK SWITCH BEECH 1900 1900D 1154162CE MLG OUT OF ADJUST A GLBAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 NM03170GL UE170 GEAR INTRANSIT LIGHT ILLUMINATED, CYCLED GEAR ALL GEAR CAME UP, TRANSIT LIGHT REMAINED ILLUMINATED. PERFORMED GEAR SWING, NOSE GEAR UPLOCK SWITCH REQUIRED ADJUSTMENT. 2L72 4T RTA24CE 20050825000582005082500058SO 2005 8 25 LR7A05109 120050822A5310 BEAM LKHEED382 382G 526414USO FS 497 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03406LC 550 4676 DURING SCHEDULED B1 INSPECTION IAW JOB CARD HB3201 FOUND LT MLG WHEEL WELL FS 497 BOW BEAM CRACKED AT UPPER LUG, LBL 60, WL 200. REPAIRED IAW SRM SMP 583 53-40-14. NR 0048. 2H74 4T A1SO 20050825000592005082500059SO 2005 8 25 LR7A05110 120050822A5330 SKIN LKHEED382 382G 526414USO FS 518 SCRATCHED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03406LC 550 4676 DURING SCHEDULED B1 INSPECTION IAW JOB CARD HB5301 FOUND FS 518 FUSELAGE SKIN SCRATCHED AT LBL 24, WL 130. REPAIRED IAW SRM SMP 583 51-140-12. NR 0077. 2H74 4T A1SO 20050825000602005082500060NM 2005 8 25 SB05096 120050821A3397 WIRE BOEING737 7374B7 1384702NM AFT CABIN BROKEN A USAAK NONE O OTHER ININSP/MAINT 1 EA19777AU 24979 MAINTENANCE REPORTED THE LAST 2 ROWS OF FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE RE-SPLICED POWER WIRE IAW WPM 20-10-13. OPS CHECK GOOD. 2L72 4F RTA16WE 20050825000622005082500062GL 2005 8 25 EVC2005F00000 220050802A7200250C30P ENGINE BELL 206 206L1 1182107SW ALLSN 250C 250C30 03013GL FAILED E EVCAK NONE O OTHER ININSP/MAINT 1 CE0359AE 45291 CAE897513 ENGINE CAUTION WARNING CHIP DETECTOR LIGHT ILLUMINATED IN FLIGHT. CHIP DETECTOR WAS REMOVED AND NO SIGNIFICANT CHIP WAS FOUND. REINSERTED CHIP PLUG AND RAN AIRCRAFT LIGHT ILLUMINATED AGAIN. MAINTENANCE FOUND EXTENSIVE METAL ON BOTH UPPER AND LOWER ENGINE CHIP DETECTORS. EXTERNAL ENGINE OIL FILTER SHOWED LARGE AMOUNT OF METAL. ENGINE REMOVED FOR REPAIR. SUSPECT BEARING IN GEARBOX. (K) 1G71 3U3 U H2SW E1GL 20050825000632005082500063NM 2005 8 25 180 120050824A5315 FLOORBEAM BOEING757 757232 1384965NM FUSELAGE CORRODED A K NONE O OTHER ININSP/MAINT 1 SO15672DL 25977 CORROSION ON CABIN FLOORBEAM BS 365 RBL 73. 2L72 4F RTA2NM 20050825000662005082500066 2005 8 25 AWXA200500991 420050820A3417 ADC BOEING737 7373Y0 1384671NM RIGHT MALFUNCTIONED A AWXAC ABORTED TAKEOFF G MULTIPLE FAILURE TOTAKEOFF 1 WP28334AW 23748 ABORTED TAKEOFF C-CHECK NON REVENUE FLT HAD REJECTED TAKEOFF AT 80 KTS FOR CAPTAINS ALTIMETER, MACH AIRSPEED INDICATOR & MACH TRIM FAIL LIGHT ALSO SPEED TRIM FAIL LIGHT. A VARIETY OF EFIS INFORMATION LOST WHEN AUTO THROTTLES DISENGAGED. MX R & R LT & RT ADC IAW AWA TC R2A34007. OPS CHECKS GOOD IAW AWA R2A34007. CONFIRMED FAILURE OF LT ADC, UNIT FAILED INCOMING FUNCTIONAL RATE OF CLIMB TEST. REPLACED SYNCHRO BOARD & RESOLVER BOARD. WORK PERFORMED IAW CMM 34-10-97 REV 10. WAS NOT ABLE TO CONFIRM FAULT ON THE RT ADC, NO FAULTS WERE FOUND WITH UNIT. UNIT INSPECTED & FUNCTIONALLY TESTED IAW CMM 34-10-97 REV 10. 2L72 4F RTA16WE 20050825000672005082500067 2005 8 25 AWXA200500992 420050822A3414 INDICATOR BOEING737 7373Y0 1384671NM AIRSPEED INOPERATIVE A AWXAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 WP28334AW 23748 F/O'S AIRSPEED INDICATOR WAS STICKING AT TAKEOFF. AIRCRAFT ABORTED TAKEOFF AT APPROXIMATELY 80 KNOTS AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE F/O'S AIRSPEED INDICATOR. VENDOR DID NOT CONFIRM FAULT. UNIT WAS OVERHAULED AND SERVICE BULLETIN 2083-34-13 REV.4 AND MODIFICATION "L" PER S.B. 2083-34-15 WERE INCORPORATED. IN ADDITION C7 AND C9 THROUGH C11 WERE REPLACED ON THE POWER SUPPLY. UNIT PASSED FUNCTIONAL TESTS. ALL WORK AND TESTS WERE PERFORMED IAW CMM 34-12-02 REV. 1. 2L72 4F RTA16WE 20050825000682005082500068NM 2005 8 25 AWXA200500993 120050713A575465C267933 SKIN BOEING737 7373S3 1384711NM NR 3 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 DURING C18 CHECK DISCOVERED, THE NR 3 SLAT SKIN AT OUTBOARD END, SS 124, CRACKED .375 INCHES IN LENGTH. MAINTENANCE REMOVED DAMAGED AREA OF THE NR 3 SLAT SKIN IAW BOEING 737-300 SRM 57-43-01-2. FABRICATED FILLER AND SPLICE PLATE IAW BOEING 737-300 SRM 52-43-01-2 FIG 206. INSTALLED FABRICATED REPAIR PARTS IAW BOEING 737-300 SRM 57-43-01-2 FIG 206. 2L72 4F RTA16WE 20050825000692005082500069NM 2005 8 25 AWXA200500994 120050713A575465C267943 SKIN BOEING737 7373S3 1384711NM NR 2 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 MCN - DURING C18 CHECK DISCOVERED, 4 CRACKS IN THE NR 2 SLAT SKIN BELOW THE INBOARD AUXILIARY TRACK, FROM SS 90 TO SS 164. MAINTENANCE REMOVED DAMAGED AREA OF NR 2 SLAT SKIN BELOW THE INBOARD AUXILIARY TRACK, FROM SS 90 TO SS 164 IAW BOEING 737-300 SRM 57-43-01-2. FABRICATED FILLER AND SPLICE PLATE IAW BOEING 737-300 SRM 52-43-01-2 FIG 206. INSTALLED FABRICATED REPAIR PARTS ON THE NR 2 SLAT SKIN BELOW THE INBOARD AUXILIARY TRACK FROM SS 90 TO SS 164 IAW BOEING 737-300 SRM 57-43-01-2 FIG 206. 2L72 4F RTA16WE 20050825000702005082500070NM 2005 8 25 AWXA200500995 120050715A53156545834255 STIFFENER BOEING737 7373S3 1384711NM BS 297-308 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 MCN - DURING C18 CHECK DISCOVERED CORROSION ON THE BOTTOM OF FLOOR SUPPORT STIFFENER AT RBL 11, WL 208, BS 297 TO BS 308. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-10-51-1 FIG 101. REMOVED STIFFENER AND PREPARED NEW STIFFENER FOR INSTALLATION IAW BOEING 737-300 SRM 51-40-05-0. INSTALLED FABRICATED REPAIR PARTS AT RBL 11, WL 208, BS 297 TO BS 308 IAW BOEING 737-300 SRM 51-40-02-0. 2L72 4F RTA16WE 20050825000712005082500071NM 2005 8 25 0501296301 120050816A253040806203 OVEN BOEING747 747451 1384940NM GALLEY SMOKE A NWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL01661US 23719 FLIGHT ATTENDANT REPORTED OVEN 3-50 CAUSED SMOKE IN GALLEY (PULLED HALON). AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. DTW MAINTENANCE MEL'D OVEN. MAINTENANCE REMOVED AND REPLACED OVEN CONTROLLER. OPERATIONAL CHECKED GOOD. 2L74 4F RTA20WE 20050825000722005082500072NM 2005 8 25 05FDEA02497 120050817A5311 FRAME BOEING727 727227 1384078NM FUSELAGE BENT A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 FRAME BENT STA 1070 STR 25L - 2L. REMOVED DAMAGED AREA, FABRICATED REPAIR ANGLE, TREATED AND PRIMED, INSTALLED REPAIR IAW SRM 51-30-2, 51-40-3, 51-10-2. 2L73 4F A3WE 20050825000732005082500073NM 2005 8 25 05FDEA02499 120050817A5340 STRINGER CLIP BOEING727 727227 1384078NM UPPER LOBE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 FUSELAGE, UPPER LOBE, STA 680 STR 2L, STRINGER CLIP DAMAGED. REPLACED STRINGER CLIP AT BS 680, STR 2L PER SRM 51-30-2. 2L73 4F A3WE 20050825000742005082500074NM 2005 8 25 05FDEA02592 120050823A5313 STRINGER BOEING727 727227 1384078NM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 AT STA 435 STR 19R, FOUND CRACK AT FASTENER HOLES, 2ND HOLE FWD OF STRINGER SPLICE. REPAIRED PER SRM 53-10-3, MAJOR REPAIR. [CLOSED] 2L73 4F A3WE 20050825000752005082500075NM 2005 8 25 05FDEA02595 120050823A5313 STRINGER BOEING727 727227 1384078NM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 WHILE WORKING N01449, FOUND STRINGER 20R BS 419 TO BE DENTED. REPAIRED PER SRM 53-10-3 FIG 1. 2L73 4F A3WE 20050825000762005082500076WP 2005 8 25 0501319973 120050820A2150 ACM DOUG DC9 DC931 3022065WP LEFT SMOKE A NWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL019337 47346 AFTER DEPARTURE, THE FLT ATTENDANT REPORTED SMOKE IN THE CABIN. THE SMOKE CLEARED WHEN THE LT PACK WAS SECURED. AN EMERGENCY WAS DECLARED AND THE FLT RETURNED TO A NORMAL SAFE LANDING BACK AT DTW. NO FIRE OR IMMEDIATE SOURCE OF SMOKE WAS FOUND. MAINTENANCE FOUND BOTH OF THE WATER SEPARATOR SOCKS TO BE OILY AND REPLACED THEM. THE LEFT HAND ACM WAS ALSO REPLACED DUE TO HIGH TIME. THE AIRCRAFT RETURNED TO SERVICE ON 26AUG AND HAS NOT EXPERIENCED ANY REPEAT SYSTEM PROBLEMS. 2L72 4F A6WE 20050825000782005082500078EU 2005 8 25 05FDEA02584 120050822A5347 SEAT TRACK AIRBUS310 A310203 3930313EU FR 69-70 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25425FE 264 SEAT TRACK BETWEEN FS 69-70, LBL 37" HAS CORROSION. REMOVED LIGHT SURFACE CORROSION IAW SRM 51-74-10 PG 204 MAT LOSS .001, FOUND TO BE WITHIN LIMITS IAW SRM 53-10-16 PG 103. TREATED AND PRIMED IAW SRM 51-21-10 PG 1 AND TOPCOATED IAW SRM 51-23-00 PG 1. 2L72 4F RTA35EU 20050825000802005082500080NM 2005 8 25 05FDEA02589 120050823A71602242101565 NOSE COWL DOUG MD11 MD11 3023602NM NR 1 ENGINE VIBRATION A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25588FE 48490 ON TAKEOFF RWY 25L VHHH, AFTER POWER REDUCTION TO CLIMB AT 1500 AFL, GOT A YAW "BUMP" AND NOISE AND VIBRATION "BUZZ" IN AIRFRAME. NO ABNORMAL INDICATIONS INITIALLY, THEN NR 1 COMPRESSOR VIBRATION CLIMBED TO 5.0 AMBER, REDUCED NR 1 THROTTLE AND BUZZ DIMINISHED. NOISE QUIET AND INDICATION NORMAL AT IDLE, LEFT ENGINE RUNNING FOR SYSTEMS AVAILABILITY, DUMPED 147,000 POUNDS FUEL, LANDING VHHH. 2L73 4F RTA22WE 20050825000822005082500082WP 2005 8 25 UPS05845257 120050812A5313 LONGERON DOUG DC8 DC871F 302199DWP FS 1746 L7R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 LONGERON 7R CRACKED AT FS 1746. REMOVED DAMAGED AREA IAW SRM 53-02-02 FIG 11, FABRICATED AND INSTALLED REPAIR SPLICE FILLER AND REPAIR ANGLES IAW SRM 53-02-02 FIG 11 AND SRM 51-1-20D. 2L74 4F RT4A25 20050825000842005082500084WP 2005 8 25 UPS05845260 120050823A5610 MECHANISM DOUG DC8 DC873F 302199FWP WINDOW STUCK A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 F/O'S EMERG (CLEAR VIEW, DV WINDOW) WILL NOT OPEN. CLEANED AND LUBED F/O'S WINDOW SLIDE MECH. OPS CK NORMAL. 2L74 4F RT4A25 20050825000862005082500086NM 2005 8 25 AWXA200500996 120050724A5315654797379 FLOORBEAM BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 MCN - DURING C18 CHECK, DISCOVERED INNER CHORD CRACKED, 1 INCH, IN CABIN AREA, BS 616, WL 208, BL 60R. MAINTENANCE CUT OUT DAMAGED SECTION OF INNER CHORD AT BS 616, WL 208, BL 60R IAW AMERICA WEST AIRLINES (AWA) ENGINEERING REPAIR (ER) NUMBER 03-5361-0522-RC1. FABRICATED SPLICE CHANNEL, SPLICE STRAP AND INNER CHORD IAW AWA ER 03-5361-05221-RC1. INSTALLED FABRICATED REPAIR PARTS AT BS 616, WL 208, BL 60R IAW AWA ER 03-5361-5221-RC1. 2L72 4F RTA16WE 20050825000872005082500087NM 2005 8 25 AWXA200500997 120050714A5754 SKIN BOEING737 7373S3 1384711NM ZONE 500 - LEFT DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 0313 23712 MCN - DURING C18 CHECK, DISCOVERED DISBOND AREA ON TOP SURFACE OF THE NR 3 SLAT AT THE INBOARD END. MAINTENANCE REMOVED DISBOND SKIN AND CORE ON THE NR 3 SLAT IAW BOEING 737-300 SRM 51-70-10-0 FIG 16. FABRICATED REPAIR DOUBLER AND CORE IAW BOEING 737-300 SRM 51-70-10-0 FIG 16. BONDED AND SEALED REPAIR PARTS TO THE NR 3 SLAT INBOARD END OF WEDGE IAW BOEING 737-300 SRM 51-70-10-0 FIG 16. 2L72 4F RTA16WE 20050825000882005082500088NM 2005 8 25 AWXA200500998 120050822A52105079454 SKIN BOEING737 7373G7 1384595NM L1 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28311AW 24712 MCN - DURING C18 CHECK, DISCOVERED THE L1 DOOR WEB CRACKED, .950 INCHES IN LENGTH, BELOW HANDLE AT BS 328, STR 14L. MAINTENANCE REMOVED CRACKED SECTION ON THE L1 DOOR WEB BS 328, STR 14L IAW BOEING 737-300 SRM 51-70-13-0G FIG 1. FABRICATED REPAIR PLATE IAW BOEING 737-300 SRM 51-70-13-0G FIG 1. INSTALLED FABRICATED REPAIR PARTS AT L1 DOOR WEB BS 328, STR 14L IAW BOEING 7 37-300 SRM 51-70-13-0G FIG 1. 2L72 4F RTA16WE 20050825000902005082500090EU 2005 8 25 AWXA200501000 120050815A5347D5337111001000 SEAT TRACK AIRBUS320 A320231 3930325EU FR 41-47 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28645AW 238 SAL - DURING C3 CHECK DISCOVERED CORROSION ON SEAT TRACK LOCATED AT RT INBOARD SIDE AT FR 42+17, -Y765. MAINTENANCE REMOVED CORROSION AND FOUND REWORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15. REMOVED SEAT TRACK AT FR 42+17, -Y765 AND INSTALLED NEW SEAT TRACK IAW AIRBUS 320 SRM 53-31-15 FIG 2. 2L72 4F RTA28NM 20050825000922005082500092EU 2005 8 25 AWXA200501002 120050815A5347D57130147202 SEAT TRACK AIRBUS320 A320231 3930325EU FR 36-41 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28645AW 238 SAL - DURING C3 CHECK, DISCOVERED CORROSION ON SEAT TRACK LOCATED ON THE LT OUTBOARD SIDE AT FS 36 +16" Y1292. MAINTENANCE REMOVED CORROSION AND FOUND REWORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15. REMOVED SEAT TRACK AT FR 36 +16" Y1292 AND INSTALLED NEW SEAT TRACK IAW AIRBUS 320 SRM 53-31-15 FIG 2. 2L72 4F RTA28NM 20050825000942005082500094EU 2005 8 25 AWXA200501004 120050815A5347D57130147200 SEAT TRACK AIRBUS320 A320231 3930325EU FR 36-41 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28645AW 238 SAL - DURING C3 CHECK, DISCOVERED CORROSION ON SEAT TRACK LOCATED ON THE LT INBOARD SIDE AT FR 39 +10" Y765. MAINTENANCE REMOVED CORROSION AND FOUND REWORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15. REMOVED SEAT TRACK AT FR 39 +10" Y765 AND INSTALLED NEW SEAT TRACK IAW AIRBUS 320 SRM 53-31-15 FIG 2. 2L72 4F RTA28NM 20050825000962005082500096NM 2005 8 25 AWXA200500981 120050817A2560PW070001101 FLASHLIGHT BOEING757 7572S7 1384962NM CABIN INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28901AW 23321 LAS - EEL - DURING 4 DAY CHECK, DISCOVERED THE FORWARD F/A EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD F/A EMERGENCY FLASHLIGHT. OPERATIONAL CHECKS GOOD. 2L72 4F RTA2NM 20050825000972005082500097NM 2005 8 25 AWXA200500982 120050817A5330 SKIN BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 PHX - DURING 4 DAY CHECK, FOUND SKIN CRACK ON LEFT SIDE OF FUSELAGE APPROX 1' AFT AND 1' BELOW EMERGENCY LIGHT AFT OF MLG WHEEL WELL. MAINTENANCE REMOVED DAMAGED SKIN AT STA JUST FWD OF 747, STR 24L PER BOEING 737-300 SRM 51-00-01. FABRICATED DOUBLER AND INSTALLED IAW BOEING 737-300 SRM 51-00-01. 2L72 4F RTA16WE 20050825000982005082500098NM 2005 8 25 AWXA200500983 120050730A575465C26601173 SKIN BOEING737 7373Y0 1384671NM NR 1 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28334AW 23747 MCN - DURING C16 CHECK, DISCOVERED 5 CRACKS, .250 INCHES IN LENGTH, ON BOTTOM SURFACE OF THE NR 1 SLAT, BELOW OUTBOARD MAIN TRACK AT SS 356L. MAINTENANCE CUT OUT AND REMOVED DAMAGED SKIN FROM THE NR 1 SLAT, BELOW OUTBOARD MAIN TRACK AT SS 356L IAW BOEING 737-300 SRM 57-43-01-2 FIG 206. FABRICATED SPLICE PLATE AND FILLER IAW BOEING 737-300 SRM 57-43-01-2 FIG 206. INSTALLED FABRICATED REPAIR PARTS AT THE NR 1 SLAT, BELOW OUTBOARD MAIN TRACK AT SS 356L IAW BOEING 737-300 SRM 57-43-01-2 FIG 206. 2L72 4F RTA16WE 20050825000992005082500099NM 2005 8 25 AWXA200500984 120050714A575465C26601179 SKIN BOEING737 7373S3 1384711NM ZONE 500 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 MCN - DURING C18 CHECK, DISCOVERED FOUR CRACKS IN THE NR 1 SLAT, .250 INCHES IN LENGTH, LOCATED AT THE LOWER SKIN AT OUTBOARD END SS 385. MAINTENANCE REMOVED AND REPLACED THE NR 1 SLAT IAW BOEING 737-300 AMM 27-81-21-004-001 AND 27-81-21-404-002. OPERATIONAL CHECKS WERE GOOD IAW BOEING 737-300 AMM 27-81-00-825-018. 2L72 4F RTA16WE 20050825001002005082500100NM 2005 8 25 AWXA200500985 120050808A5330 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28311AW 24712 PHX - DURING 4 DAY CHECK, FOUND SKIN CRACK ON LEFT SIDE OF FUSELAGE APPROX 1' AFT AND 1' BELOW EMERGENCY LIGHT AFT OF MLG WHEEL WELL. MAINTENANCE REMOVED DAMAGED SKIN AT STA JUST FWD OF 747, STR 24L PER BOEING 737-300 SRM 51-00-01. FABRICATED DOUBLER AND INSTALLED IAW BOEING 737-300 SRM 51-00-01. 2L72 4F RTA16WE 20050825001012005082500101NM 2005 8 25 AWXA200500986 120050808A5315654593469 STRAP BOEING737 7373G7 1384595NM FLOORBEAM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28311AW 24712 DURING C15 CHECK, DISCOVERED FLOOR STRAP CRACKED, 2.0 INCHES IN LENGTH, ON THE BOTTOM OF BS 328 BEAM AT BL 11L. MAINTENANCE STOP DRILLED CRACK ON FLOORBEAM AT BS 328, BL 11L IAW BOEING 737-300 SRM 53-10-51-2 FIG 204. FABRICATED REPAIR PLATE AND INSTALLED ON FLOOR STRAP LOCATED AT BOTTOM OF BS 328 BEAM AT BL 11L IAW BOEING 737-300 SRM 53-10-51-2 FIG 204. 2L72 4F RTA16WE 20050825001032005082500103NM 2005 8 25 AWXA200500988 120050808A53156545834107 STRAP BOEING737 7373G7 1384595NM FLOORBEAM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28311AW 24712 MCN - DURING C15 CHECK DISCOVERED FLOOR STRAP CRACKED, .7 INCHES IN LENGTH, ON THE BOTTOM OF BS 344 BEAM AT BL 45L. MAINTENANCE STOP DRILLED CRACK ON FLOORBEAM AT BS 344, BL 45L IAW BOEING 737-300 SRM 53-10-51-2 FIG 204. FABRICATED REPAIR PLATE AND INSTALLED ON FLOOR STRAP LOCATED AT BOTTOM OF BS 344 BEAM AT BL 45L IAW BOEING 737-300 SRM 53-10-51-2 FIG 204. 2L72 4F RTA16WE 20050825001052005082500105EU 2005 8 25 UPS05145259 120050717A71602210302521 COWLING AIRBUSA300 A300F4622R 3930360EU PWA 4158 PW4158 NE NR 2 ENG FAN DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01131UP 0815 NR 2 ENG OTBD FAN COWL HAS HEAT DAMAGE. REMOVED AND REPLACED NR 2 ENG OTBD FAN COWL REF MM 71-13-02-4. 2L72 4F4 FRTA35EU E24NE 20050825001072005082500107WP 2005 8 25 UPS05845251 120050812A5320 ANGLE DOUG DC8 DC871F 302199DWP FS 1766 L6R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 C1 ANGLE CRACKED AT FS 1766 LONG 6R. REMOVED CRACKED ANGLE AT FS 1766 L6R IAW SRM 51-1-20D. FABRICATED AND INSTALLED ANGLE AT FS 1766 L6R IAW SRM DWG 5773844 AND SRM 51-1-20D. 2L74 4F RT4A25 20050825001092005082500109WP 2005 8 25 UPS05845253 120050811A5340 FITTING DOUG DC8 DC871F 302199DWP FS 781 L18R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 FRAME TO INTERCOSTAL ATTACH FITTING CRACKED AT FS 781 LONG 18R AFT SIDE. REMOVED AND REPLACED FITTING IAW DWG 3750025 AND SRM 51-1-20D. 2L74 4F RT4A25 20050825001112005082500111WP 2005 8 25 UPS05845255 120050813A5752 SKIN DOUG DC8 DC871F 302199DWP LT AILERON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 LT WING AILERON LE UPPER SURFACE AROUND FASTENER HAS 1/4" LONG CRACK PCU AREA. STOP DRILLED CRACK NDT HFEC VERIFIED CRACK TERMINATES AT STOP DRILL. FABRICATED REPAIR DOUBLER IAW 57-02-00-0 AND INSTALLED REPAIR DOUBLER IAW SRM 57-02-00-0 AND 57-08-00-0. REPAIR DOUBLER CENTERED AT AILERON HINGE LINE "D" VALUE EQUALS ZERO THEREFORE THERE IS NO NET CHANGE IN BALANCE IAW SRM 51-04-08 FIG 59R. 2L74 4F RT4A25 20050825001122005082500112NM 2005 8 25 05FDEA02596 120050823A5311 FRAME BOEING727 727233 138408ANM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 WHILE WORKING FED EX EA 7-5330-72293B PT2, FOUND FASTENER HOLES ON EDGE OF FRAME WITH NO EDGE DISTANCE, BS 620 LBL-9 W/L 302 AND 303 2 EA. REPAIRED FRAME BS 620, LBL 9 PER FED-EX EA 7-5330-92323. 2L73 4F RTA3WE 20050825001132005082500113NM 2005 8 25 QXEA200501184 120050820A21508209251 SHUTOFF VALVE BOMBDRDHC8 DHC8402 1390042NM A/C PACK FAULTY A QXEAO OTHER J WARNING INDICATION DEDESCENT 1 NM09412QX8911 4059 CABIN PACK HOT CAUTION LIGHT ILLUMINATED DURING DESCENT. C/W EMERGENCY/ABNORMAL CHECKLIST. ALL CABIN DUCT TEMPS ZERO (0) INDICATIONS WERE WITHIN THE GREEN RANGE. MAINTENANCE INTERROGATED CDS, FOUND CAB TSOV STATUS MESSAGE IN FAULT HISTORY. REMOVED AND REPLACED CABIN TURBINE SHUTOFF VALVE IAW AMM 21-51-41-000-801 AND -400-801, IAW FIM 21-60-00-810-823. OPS CHECK AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050825001142005082500114NM 2005 8 25 HNAA0500076 120050817A326082400033033 PROXIMITY SENSOR DHAV DHC8 DHC8102 2809003NM NLG FAILED A HNAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA07941HA3560435604 161 WHEN GEAR WAS SELECTED UP THE NOSEGEAR REMAINED UNSAFE AND AMBER MAIN GEAR DOOR LIGHTS ILLUMINATED. SELECTED GEAR DOWN ALL INDICATIONS NORMAL. REMOVED AND REPLACED NLG DRAGSTRUT PROXIMITY SENSOR. 2H72 4T RTA13NM 20050826000022005082600002SO 2005 8 26 RAIA00508032 120050822A3397 WIRE EMB 145 EMB145EP 3260221SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT UNSECURE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03826HK 145016 EMERGENCY LIGHT IN CABIN BELOW COCKPIT DOOR INOPERATIVE. MAINTENANCE SECURED LOOSE WIRE. 2L72 4F4 FRTT00011ATTE6CH 20050825000222005082500022NM 2005 8 25 SWAA052521 120050817A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 986.5, STR 27L. MX FERRY TO DAL FOR REPAIRS. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20050825000292005082500029SO 2005 8 25 C2XA05IA095 120050720A335078241 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713988 145265 STL - DURING MX INSPECTION, THE EMERGENCY LIGHT BY THE LEFT EXIT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050825000332005082500033SO 2005 8 25 C2XA05IA093 120050724A335066367 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713988 145265 IAH - FLIGHT 2553, DURING PREFLIGHT INSPECTION, THE NR 2 EMERGENCY FLOOR PROXIMITY LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE PLACED THE AFFECTED LIGHT STRIP ON MEL 3350-00/2 CAT C CONTROL NUMBER 057514, AND THE AIRCRAFT WAS APPROVED FOR RETURN TOP SERVICE. THE AIRCRAFT LANDED IN CRP WHERE MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050825000342005082500034EA 2005 8 25 SWIA200515450 120050822A2741 SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07932SW 7714 STAB TRIM CH 1 INOP. REPLACED F/O TRIM SWITCH IAW MM 27-41-05, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050825000422005082500042EA 2005 8 25 SWIA200515458 120050722A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07406SW 7030 ANGLE CRACKED IN ADG COMPARTMENT, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED ANGLE IAW CRJ SRM 51-21-16, 51-23-00, 51-24-36, 51-25-06, 51-25-00, 51-40-06, 51-40-11, 51-40-02, 51-42-06. 2L72 4F RTA21EA 20050825000552005082500055SW 2005 8 25 PNSA050801 120050820A5270 SWITCH SWRNGNSA227 SA227AC 8780603SW PAX DOOR OUT OF ADJUST A PNSAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 AL032719H AC713B DURING CLIMB OUT FROM ANC THRU 5,500 FEET, THE CABIN DOOR LIGHT ILLUMINATED. A/C RETURNED TO ANC AND DESCENDING THRU 5,000 FEET THE LIGHT EXTINGUISHED. MAINTENANCE ADJUSTED DOOR SWITCHES IAW 52-70-00. NOTE MECHANIC HAD WORKED ON THE DOOR SYSTEM THE PREVIOUS NIGHT. 2L72 4T RTA8SW 20050825000612005082500061NM 2005 8 25 P5CA0501385 120050516A5320 STRUCTURE BOEING747 747230B 1384889NM FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 EA15509MC 21221 LT FOUND 1 OFF STANDOFF HOLE WITH 2 OFF CRACKS APPROXIMATELY 3MM EACH AT BS 280 WEB. REPAIR CARRIED OUT IAW MFG MSG 1-1ME16G. REFER TO FAA FORM 8100-9 DATED JUNE 2, 2005. THIS REPAIR IS SUBJECT TO CONTINUE INSPECTION IAW SB 747-53A2293. 2L74 4F A20WE 20050825000642005082500064EU 2005 8 25 YENA200550 120050817A212120092455101 FAN AIRBUS320 A320232 3930326EU AVIONICS SMOKE A YENAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 EA15550JB11794 1891 AT FL 360 RECEIVED AFT AVIONICS COMPARTMENT SMOKE WARNING WITH A RED LIGHT SMOKE INDICATION WITH A HORN ON THE OVERHEAD PANEL; THIS HAD NO ASSOCIATED ECAM. SILENCED THE ALARM, AND QRH PROCEDURE CATRRIED OUT. AFTER COMPLETION OF QRH PROCEDURE THE RED LIGHT REMAINED AND THE HORN SOUNDED A SECOND TIME. CAPTAIN DECLARED EMERGENCY AND MADE A UNEVENTFUL UNSCHEDULED LANDING AT OKC. VISUAL INSPECTION OF AFT AVIONICS RACK REVEALED NO DEFECT. REMOVED AND REPLACED AFT AVIONICS RACK COOLING FAN ASSY, OPERATION CHECK NORMAL PER LTV AMM 23-39-00. 2L72 4F RTA28NM 20050825001062005082500106NM 2005 8 25 UPS05545249 120050823A2120 UNKNOWN BOEING757 75724APF 1384969NM COCKPIT FUMES A IPXAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO01451UP 27739 CREW REPORTED FUMES IN THE COCKPIT, NO EMERGENCY DECLARED. STRONG BURNING ODOR FROM ISOLATED PACKS. RAN BOTH ENGINES AND BOTH PACKS IN NORMAL AND ISOLATED CONFIGURATIONS INSPECTED INLETS AND EXHAUST. INSPECTED ALL CARGO COMPARTMENTS. NO UNUSUAL ODORS OR BURNING ODORS NOTED AS ASSOCIATED WITH FIM 21-00-01 A/C OK FOR SERVICE 2L72 4F RTA2NM 20050825001082005082500108WP 2005 8 25 UPS05845252 120050812A5320 ANGLE DOUG DC8 DC871F 302199DWP FS 1766 L6L CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 C1 ANGLE CRACKED AT FS 1766 LONG 6L. REMOVED ANGLE IAW SRM 51-1-20D AT FS 1766 LONG 6L. FABRICATED AND INSTALLED ANGLE AT FS 1766 LONG 6L DWG 5773844 AND SRM 51-1-20D. 2L74 4F RT4A25 20050825001102005082500110WP 2005 8 25 UPS05845254 120050812A5313 LONGERON DOUG DC8 DC871F 302199DWP FS 1726 L15L CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 LONG 15L CRACKED AT FS 1726. REMOVED DAMAGED AREA IAW SRM 53-2-2 FIG 11. FABRICATED REPAIR SPLICE FILLER AND REPAIR ANGLES AND INSTALLED IAW SRM 53-02-02 FIG 11 AND SRM 51-1-20D. 2L74 4F RT4A25 20050826000032005082600003EU 2005 8 26 RAIA00508030 120050822A3260 UPLOCK SWITCH JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114HR 01514NE RT MLG FAILED A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03564HK 41081 RED IN-TRANSIT LIGHT ILLUMINATED AND STAYED ON AFTER GEAR RETRACTION. MAINTENANCE REMOVED AND REPLACED THE RT MLG SECONDARY UPLOCK SWITCH. 2L72 4T4 TRTA41NM E18NE 20050826000052005082600005SO 2005 8 26 RAIA00508033 120050822A3350 LIGHT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL RT OVERWING INOPERATIVE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03812HK 145373 RT OVERWING EMERGENCY EXIT LIGHT IS INOPERATIVE. MAINTENANCE PERFORMED OPS CHECK OF EMERGENCY LIGHTING SYSTEM. OPS CHECKED GOOD. 2L72 4T4 FRTT00011ATTE6CH 20050826000072005082600007WP 2005 8 26 05FDEA02605 120050824A5712 RIB DOUG DC10 DC1010 3022110WP GE CF6 CF66K 30020NE ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 RT WING L/E AT XORS 526 FOUND RIB CRACKED. ACCOMPLISHED WING OB EDGE FORMER REPAIR IAW SRM. 2L73 4F4 F A22WE E23EA 20050826000092005082600009WP 2005 8 26 05FDEA02607 120050824A5310 STRUCTURE DOUG DC10 DC1010 3022110WP GE CF6 CF66K 30020NE ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 MAIN CABIN INTERNAL FUSELAGE FOUND NR 2 HOLES DIAM. 0.25 INCH TOO CLOSE AT STA 1561, LONGERON 8 LT SIDE. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM. 2L73 4F4 F A22WE E23EA 20050826000102005082600010WP 2005 8 26 05FDEA02608 120050824A1430 FASTENER DOUG DC10 DC1010 3022110WP GE CF6 CF66K 30020NE ZONE 100 WRONG PART A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25556FE 46710 AIR COND COMPT LT SIDE FOUND EXISTING REPAIR WITH WRONG FASTENERS (CHERRY AND BOLT) ON NLG BLKHD. REMOVED EXISTING REPAIR, TRIMMED OUT DAMAGED AREA AND REPAIRED IAW SRM. 2L73 4F4 F A22WE E23EA 20050826000132005082600013CE 2005 8 26 DXTA200500914 120050822A3233MS287734 O-RING CESSNA650 650 2076802CE GARRTTTFE731TFE7314R 01518WP NLG ACTUATOR LEAKING E DXTAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL07792QS 6507092 GEAR WOULD NOT RETRACT AFTER TAKEOFF. JACKED AIRCRAFT AND CYCLED LANDING GEAR. FOUND HYDRAULIC FITTING AT NOSE GEAR ACTUATOR LEAKING EXCESSIVELY. REPLACED O-RING AT NOSE GEAR ACTUATOR RETRACT PORT FITTING AND COMPLIED WITH GEAR SWING FUNCTIONAL TESTS IAW MFG MM. SERVICED HYDRAULIC RESERVOIR WITH BRAYCO. 2L72 4F4 F A9NM E6WE 20050826000142005082600014CE 2005 8 26 DXTA200500924 120050825A2432 BATTERY CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE MASTER OVERTEMP E DXTAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL07335QS 5600335 BATTERY OVERTEMP AT 145 DEGREES STEADY, ANNUNCIATOR LIGHT ILLUMINATED, DELARED EMERGENCY AND LANDED SAFELY. ITEM IS UNDER INVESTIGATION. 2L72 4F4 FRTA22CE E25EA 20050826000152005082600015CE 2005 8 26 DXTA200500916 120050823A3240 BRAKE ASSY CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE MLG WEAK E DXTAD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07332QS 5600523 CO-PILOT TAXING TO RUNWAY, RT BRAKE PEDAL GOES APPROXIATELY FIVE INCHES MORE THAN LT PEDAL TO APPLY FULL PRESSURE. ITEM IS UNDER INVESTIGATION. 2L72 4F4 FRTA22CE E25EA 20050826000162005082600016CE 2005 8 26 DXTA200500917 120050823A3210 LANDING GEAR CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE NOISY E DXTAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL07342QS 5600324 AT APPROXIMATELY 240 KTS, INDICATED A SUDDEN LOUD RUSHING AIR NOISE WAS HEARD FROME THE NOSE. A SLIGHT VIBRATION ACCOMPANIED THE SOUND. AFTER DECREASING AIR SPEED SOUND WAS STILL PRESENT. WHEN GEAR WAS EXTENDED, INCREASED VIBRATIONS WERE FELT. ITEM IS UNDER INVESTIGATION. 2L72 4F4 FRTA22CE E25EA 20050826000172005082600017WP 2005 8 26 05FDEA02603 120050824A5311 FRAME DOUG DC10 DC1010 3022110WP GE CF6 CF66K 30020NE ZONE 100 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 AIR COND COMPT LT SIDE FOUND WORN FRAME AT STA 588 X=64. TRIMMED WORN AREA AND REPAIR IAW SRM. 2L73 4F4 F A22WE E23EA 20050826000182005082600018WP 2005 8 26 05FDEA02614 120050824A5712 RIB DOUG DC10 DC1010 3022110WP GE CF6 CF66K 30020NE ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 RT WING FIXED LEADING EDGE AT STA 750 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM AND REPAIR ANGLE. 2L73 4F4 F A22WE E23EA 20050826000202005082600020WP 2005 8 26 05FDEA02616 120050824A5712 RIB DOUG DC10 DC1010 3022110WP GE CF6 CF66K 30020NE ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 RT WING FIXED LEADING EDGE AT XORS 696 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM AND REPAIR ANGLE. 2L73 4F4 F A22WE E23EA 20050826000212005082600021WP 2005 8 26 05FDEA02617 120050824A5712 RIB DOUG DC10 DC1010 3022110WP GE CF6 CF66K 30020NE ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 RT WING FIXED LEADING EDGE AT XORS 733 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM. 2L73 4F4 F A22WE E23EA 20050826000242005082600024NM 2005 8 26 05FDEA02600 120050823A5311 FRAME BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE BS 610 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 PILOT HOLES NEXT TO FASTENER HOLES IN STUB FRAME BS 610 STR3L. REPAIRED FRAME PER FED-EX EA 7-5330-92328. [CLOSED] 2L73 4F4 FRTA3WE E2EA 20050826000272005082600027NM 2005 8 26 QXEA200501183 120050818A2120 HAZE BOMBDRDHC8 DHC8402 1390042NM PWC 150 PW150A EA CABIN DETECTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 AFTER STARTING THE APU AND SELECTING BLEED AIR ON, NOTICED HAZE IN COCKPIT AND CABIN. AFTER SHUTTING OFF APU, HAZE WENT AWAY. MAINTENANCE PERFORMED BORESCOPE INSP OF APU COMPRESSOR IMPELLER AND TURBINE WHEEL IAW AMM TASK 49-00-00-290-801. FOUND TO BE IN SERVICEABLE CONDITION. THEN RAN THE APU WITH BLEED AIR ON FOR 45 MIN, CYCLING RECIRC FAN ON/OFF AND COULD NOT DUPLICATE DISCREPANCY. RAN NR 1 AND NR 2 ENGINE WITH BLEEDS ON AND COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT APU SYSTEM FOUND SERVICEABLE. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E00062EN 20050826000282005082600028NM 2005 8 26 HNAA0500077 120050822A2923SM601BA20A1 CIRCUIT BREAKER DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HYD SYSTEM FAILED A HNAAK NONE J WARNING INDICATION LDLANDING 1 EA07806EX3564035640 263 LOSS OF THE NR1 STBY PUMP PRESSURE INDICATION ON LANDING AND LOSS OF NORMAL BRAKES. REMOVED AND REPLACED RT WHEEL WELL REMOTE CONTROL CIRCUIT BREAKER. 2H72 4T4 TRTA13NM E20NE 20050826000292005082600029 2005 8 26 C8GA20050018 420050815A3417H648B13 ADC BOEING727 727223 1384074NM PWA JT8 JT8D15 52051NE E&E BAY INOPERATIVE A C8GAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO29899AA 1302 22015 ON TAKEOFF ROLL, FO AIRSPEED INDICATION INOPERATIVE. FLAG CAME OUT AFTER STOP. CLEANED NR 2 ADC CONNECTOR PLUG AND RERACKED ADC. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 20050826000302005082600030NM 2005 8 26 SB05094 120050817A33501012623 LIGHT BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU SEAT ROW 11 INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19442US 24841 MAINTENANCE REPORTED THE EMERGENCY LIGHT AT SEAT ROW 11 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY. OPS CHECK GOOD. 2L72 4F4 FRTA16WE E21EU 20050826000312005082600031NE 2005 8 26 IXXA0500104O 220050823A7261CFM562C BLADE DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE NR 2 LEAKING A IXXAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW11828BX319823398 45993 692264 NR 2 ENG SHUTDOWN FOR LOSS OF OIL QTY. OIL PRESS DROPPED. OIL TEMP STABLE. SHUTDOWN NR 2 ENG. WINDMILL OIL PRESS DROPPED & QTY INCREASED. TEMP STABLE. NO WINDMILLING PRESS. LOW PRESS LIGHT ILLUM. LANDED W/OUT INCIDENT. R&R NR 2 ENG, OPS & LEAK CHK GOOD. ACFT RTS. AN FITTING & FLARE OF TUBE INCOMPATIBLE. OIL LINE CLAMP LOOSE. FORWARD OIL TANK MOUNT LOOSE. BORESCOPE REVEALED HALF OF A HPT BLADE MISSING. LOOSE HARDWARE CAUSED BY CORE VIBRATIONS (N2). ENG HAS BEEN RETURNED TO VENDOR FOR REPAIR & ROOT CAUSE ANALYSIS OF BLADE FAILURE. OVERTEMP ANALYSIS RESULTS NEG. ENG BEYOND REPAIR. METALLURGICAL EVALUATION REPORT, HPT BLADE FAILED IN THERMAL FATIGUE MODE DUE TO SEGREGATION OF TITANIUM-HAFNIUM DURING CASTING. 2L74 4F4 FRT4A25 E2GL 20050826000322005082600032WP 2005 8 26 05FDEA02609 120050824A5712 RIB DOUG DC10 DC1010 3022110WP GE CF6 CF66K 30020NE ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 RT WING FIXED LEADING EDGE AT STA XORS 936 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER, FILLER AND DOUBLER REPAIR IAW SRM. 2L73 4F4 F A22WE E23EA 20050826000332005082600033WP 2005 8 26 05FDEA02618 120050824A5712ARB129142 RIB DOUG DC10 DC1010 3022110WP GE CF6 CF66K 30020NE ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 RT WING FIXED LEADING EDGE AT XORS 742 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM. 2L73 4F4 F A22WE E23EA 20050826000342005082600034WP 2005 8 26 05FDEA02619 120050824A5712ARB129242 RIB DOUG DC10 DC1010 3022110WP GE CF6 CF66K 30020NE ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 RT WING FIXED LEADING EDGE AT XORS 831 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM. 2L73 4F4 F A22WE E23EA 20050826000352005082600035WP 2005 8 26 05FDEA02620 120050824A5712 RIB DOUG DC10 DC1010 3022110WP GE CF6 CF66K 30020NE RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 RT WING FIXED LEADING EDGE AT XORS 598 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM AND INSTALLED ANGLE REPAIR. 2L73 4F4 F A22WE E23EA 20050826000362005082600036WP 2005 8 26 05FDEA02621 120050824A5712 RIB DOUG DC10 DC1010 3022110WP GE CF6 CF66K 30020NE RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 RT WING FIXED LEADING EDGE AT XORS 615 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM AND INSTALLED ANGLE REPAIR. 2L73 4F4 F A22WE E23EA 20050826000372005082600037WP 2005 8 26 05FDEA02622 120050824A5712 RIB DOUG DC10 DC1010 3022110WP GE CF6 CF66K 30020NE ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 RT WING FIXED LEADING EDGE AT XORS 490 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM AND INSTALLED ANGLE REPAIR. 2L73 4F4 F A22WE E23EA 20050826000382005082600038WP 2005 8 26 05FDEA02623 120050824A5712 RIB DOUG DC10 DC1010 3022110WP GE CF6 CF66K 30020NE ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 RT WING FIXED LEADING EDGE AT XORS 485 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM AND INSTALLED ANGLE REPAIR. 2L73 4F4 F A22WE E23EA 20050826000412005082600041WP 2005 8 26 05FDEA02626 120050824A5712 RIB DOUG DC10 DC1010 3022110WP GE CF6 CF66K 30020NE ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 RT WING FIXED LEADING EDGE AT XORS 352 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM AND INSTALLED ANGLE REPAIR. 2L73 4F4 F A22WE E23EA 20050826000422005082600042EU 2005 8 26 YENA200551 120050818A25304110001137 COFFEEMAKER AIRBUS320 A320232 3930326EU IAE V2524 V2524A5 NE GALLEY ODOR A YENAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15621JB370 2491 F/A REPORTED ACRID BURNING ODOR (NO SMOKE) FROM FWD GALLEY. ODOR SUBSIDED WHEN COFFEE POTS TURNED OFF. PERFORMED TSM TASK 24-00-00-810-823, CHECKED PINS AND NOSE TERMINALS BEHIND COFFEEEMAKERS. OK TO CONTINUE. PRECAUTIONARY REPLACED BOTH COFFEE MAKERS (S/N 191002510, 191002509). 2L72 4F4 FRTA28NM E40NE 20050826000432005082600043NM 2005 8 26 USAA051044 120050823A5530 FITTING BOEING737 737301 1384611NM VERTICAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US 23933 O/B ATTACH HOLE IN RT AFT DRAG BRACE ATTACH FITTING OFR VERTICAL FIN CORRODED. REMOVED CORROSION, FABRICATED BUSHING AND INSTALLED IAW EA 96816, DEFECT SIZE: 1 X 2 INCH TYPICAL. 2L72 4F RTA16WE 20050826000442005082600044NM 2005 8 26 USAA051045 120050823A5320 STRIP BOEING737 737301 1384611NM CARGO BAY WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US 23933 AFT CARGO CAP STRIP BETWEEN SCUFF PLATE AND ACF-3 DAMAGED. REMOVED DAMAGED STRIP, FABRICATED & INSTALLED NEW STRIP IAW BOEING DWG 65-49613 DEFECT SIZE: 3 X 2 INCH WORN AREA. 2L72 4F RTA16WE 20050826000472005082600047NM 2005 8 26 SWAA052539 120050823A53116520725 FRAME BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29317WN 24068 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 24R. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20050826000522005082600052NM 2005 8 26 SWAA052544 120050822A3350MS155721 BULB BOEING737 7377H4 1384404NM L1 DOOR INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29715SW 27849 DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050826000532005082600053NM 2005 8 26 SWAA052545 120050823A531065458075 DOOR FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29359SW 26596 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE FRAME CRACKED AT R1 DOOR UPPER HINGE CUTOUT. REPAIRED FRAME PER SWA EA. 2L72 4F RTA16WE 20050826000542005082600054NM 2005 8 26 SWAA052546 120050823A5753 SKIN BOEING737 7373H4 1384600NM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29359SW 2166 26596 DURING SCHEDULED C3 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2L72 4F RTA16WE 20050826000552005082600055NM 2005 8 26 SWAA052547 120050824A532269353656 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29369SW 26580 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 360, BETWEEN STR 13L & STR 14L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050826000582005082600058NM 2005 8 26 SWAA052550 120050824A53116545812 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29372SW 26599 DURING SCHEDULED 1/4D CHECK, FOUND BS 328 R1 DOOR CUTOUT FUSELAGE FRAME CRACKED AT NR 4 STOP FITTING. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050826000642005082600064NM 2005 8 26 SWAA052556 120050824A53116520725 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29612SW 27930 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 24R. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20050826000672005082600067NM 2005 8 26 05FDEA02586 120050823A5320 SPLICE DOUG MD11 MD11 3023602NM DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25624FE 48443 CUT DAMAGE AND INSTALL NEW SPLICE REPAIR IAW SRM 53-00-01 FIG 7 VOL I. 2L73 4F RTA22WE 20050826000692005082600069WP 2005 8 26 05FDEA02611 120050824A5712 RIB DOUG DC10 DC1010 3022110WP ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 THE RIGHT WING FIXED LEADING EDGE AT STA 816 FOUND RIB CRACKED. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 4, 6 VOL I. 2L73 4F A22WE 20050826000702005082600070WP 2005 8 26 05FDEA02612 120050824A5712 RIB DOUG DC10 DC1010 3022110WP ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 RT WING FIXED LEADING EDGE AT STA XORS 768 FOUND NR 1 RIB CRACKED. REPAIR IAW SRM 57-20-00 FIG 1 SHEET 4/6 VOL I. 2L73 4F A22WE 20050826000712005082600071WP 2005 8 26 05FDEA02613 120050824A5712 RIB DOUG DC10 DC1010 3022110WP ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 THE RIGHT WING FIXED LEADING EDGE AT STA 756 FOUND NR 1 RIB CRACK. ACCOMPLISHED FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 1, 3, 4 VOL I AND INSTALLED ANGLE REPAIR. 2L73 4F A22WE 20050826000722005082600072WP 2005 8 26 05FDEA02627 120050824A5712 RIB DOUG DC10 DC1010 3022110WP ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LT WING FIXED LEADING EDGE AT XORS 481 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 1, 3, 4 VOL I AND INSTALLED ANGLE REPAIR. 2L73 4F A22WE 20050826000732005082600073WP 2005 8 26 05FDEA02628 120050824A5712 RIB DOUG DC10 DC1010 3022110WP ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LT WING FIXED LEADING EDGE AT XORS 469 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 1, 3, 4 VOL I AND INSTALLED ANGLE REPAIR. 2L73 4F A22WE 20050826000742005082600074WP 2005 8 26 05FDEA02629 120050824A5712 RIB DOUG DC10 DC1010 3022110WP ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LT WING FIXED LEADING EDGE AT XORS 457 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1SHEET 3, 4 VOL I AND INSTALLED ANGLE REPAIR. 2L73 4F A22WE 20050826000752005082600075WP 2005 8 26 05FDEA02630 120050824A5712 RIB DOUG DC10 DC1010 3022110WP ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LT WING FIXED LEADING EDGE AT XORS 457 FOUND NR 1 RIB CRACK. INSTALLED FILLER IAW SRM 57-20-00 FIG 1 SHEET 3, 4 VOL I. 2L73 4F A22WE 20050831000322005083100032WP 2005 8 31 05FDEA02632 120050824A5330 SKIN DOUG DC10 DC10* WP ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25360FE 46636 BARE METAL AT CIRCUMFERENTIAL STRAP BETW. L40L & L41L FS 1871. REMOVED CORROSION,FABRICATED AND INSTALLED SHIM,DOUBLER,TRIPLER AND FINGER DOUBLERS IAW DC10-10/MD10-10 SRM 51-21-01 VOL I & II,53-20-00 VOL I PG.73 FIG. 6 SHT. 3 ,53- 20-00 VOL.I PG. 74 FIG. 6 SHT.4 AND 51-41-01 VOL II. MAJOR REPAIR 2L73 4F A22WE 20050826000772005082600077WP 2005 8 26 05FDEA02633 120050824A5330 SKIN DOUG MD10 MD1010F 3022112WP FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25360FE 46636 LWR FUSELAGE EXT SKIN APPROX STA 1830 AT BL 0 AT THRESHOLD OF AFT BULK PIT DOOR HAS A CREASE WITH DENT APPROX 36 INCHES IN LENGTH. 2L73 4F RTA22WE 20050826000782005082600078WP 2005 8 26 05FDEA02634 120050824A5340AEA04741 ANGLE DOUG MD10 MD1010F 3022112WP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25360FE 46636 CORROSION FOUND ON LEFT REAR SPAR CAP ANGLE APB 7080-1. REPAIRED IN ACCORDANCE WITH FEDEX EA 8-5340-84036 LT SLANT PANEL TEE ANGLE CORROSION REPAIR . 2L73 4F RTA22WE 20050826000792005082600079EU 2005 8 26 05FDEA02635 120050824A5230 SKIN AIRBUS300 A300B4622R 3930312EU ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25729FD 657 BULK CARGO COMPARTMENT DR FWD LWR CORNER HAS A CRACK INDICATION ON EXTERNAL SKIN AT FRAME 67 AREA MARKED. REMOVED DAMAGE AND INSTALLED REPAIR IAW A300-600 SRM 53-17-12, 51-40-21 AND AMM 53-10-18. 2L72 4F RTA35EU 20050826000832005082600083WP 2005 8 26 05FDEA02639 120050825A5712 RIB DOUG DC10 DC1010 3022110WP ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LT WING FIXED LEADING EDGE AT XORS 927 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET, 3, 5 VOL I AND INSTALLED ANGLE REPAIR. 2L73 4F A22WE 20050826000842005082600084WP 2005 8 26 05FDEA02640 120050825A5712 RIB DOUG DC10 DC1010 3022110WP ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LT WING FIXED LEADING EDGE AT XORS 860 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 4; 6 VOL I AND INSTALLED ANGLE REPAIR. 2L73 4F A22WE 20050826000862005082600086WP 2005 8 26 05FDEA02653 120050825A5712 RIB DOUG DC10 DC1010 3022110WP LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LT WING FIXED LEADING EDGE AT XORS 519 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 3, 4 VOL I AND INSTALLED ANGLE REPAIR. 2L73 4F A22WE 20050826000872005082600087WP 2005 8 26 05FDEA02654 120050825A5712 RIB DOUG DC10 DC1010 3022110WP ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LT WING FIXED LEADING EDGE AT XORS 516 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 3, 4 VOL I AND INSTALLED ANGLE REPAIR. 2L73 4F A22WE 20050826000892005082600089WP 2005 8 26 05FDEA02656 120050825A5712 RIB DOUG DC10 DC1010 3022110WP ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LT WING FIXED LEADING EDGE AT XORS 504 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 3, 4 VOL I AND INSTALLED ANGLE REPAIR. 2L73 4F A22WE 20050826000952005082600095WP 2005 8 26 05FDEA02645 120050825A5712 RIB DOUG DC10 DC1010 3022110WP ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LT WING FIXED LEADING EDGE AT XORS 706 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 3, 4 VOL I AND INSTALLED ANGLE REPAIR. 2L73 4F A22WE 20050826000962005082600096WP 2005 8 26 05FDEA02646 120050825A5712 RIB DOUG DC10 DC1010 3022110WP ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LT WING FIXED LEADING EDGE AT XORS 700 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 3, 4 VOL I AND INSTALLED ANGLE REPAIR. 2L73 4F A22WE 20050826000972005082600097WP 2005 8 26 05FDEA02647 120050825A5712 RIB DOUG DC10 DC1010 3022110WP LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LT WING FIXED LEADING EDGE AT XORS 694 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 3, 4 VOL I AND INSTALLED ANGLE REPAIR. 2L73 4F A22WE 20050826000992005082600099NM 2005 8 26 05FDEA02469 120050816A5313 STRINGER BOEING727 727227 1384078NM BS 1090 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 STRINGER AT BS 1090 STR 7LT IS DAMAGED. REPAIRED STRINGER PER SRM 53-10-1, 53-10-3 FIG 3 MAJOR REPAIR. 2L73 4F A3WE 20050826001002005082600100NM 2005 8 26 05FDEA02470 120050816A5340 STRINGER CLIP BOEING727 727227 1384078NM STA 660 BROKEN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 FUSELAGE UPPER LOBE, STA 660, STRINGER CLIP 8L BROKEN. REMOVED AND REPLACED STRINGER CLIP AT STR 8L BS 660 IAW SRM 51-30-2. 2L73 4F A3WE 20050826001022005082600102NM 2005 8 26 05FDEA02472 120050816A5311 FRAME BOEING727 727233 138408ANM BS 620 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 WHILE WORKING FED EX EA 7-5330-72293B PT2, FOUND DOUBLE HOLE IN FRAME "C' CHANNEL AND SUPPORT AT BS 620 LBL 22 WL 300. REPAIRED C-CHANNEL, BS 620, LBL 22 PER FED-EX EA 7-5330-62327. 2L73 4F RTA3WE 20050826001042005082600104NM 2005 8 26 05FDEA02474 120050816A5311 FRAME BOEING727 727233 138408ANM BS 620 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 WHILE WORKING FED EX EA 7-5330-72293B PT2, FOUND DOUBLE HOLES IN FRAME AND C-CHANNEL AT 620 RBL 8 W/L 304. (OPEN) 2L73 4F RTA3WE 20050829000012005082900001NM 2005 8 29 EIA2005131 120050622A3350 LIGHT BOEING747 747212B 1384886NM STA 405 INOPERATIVE A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 UPPER DECK EMERGENCY LIGHT AT LOCATION STA 405 INOP. LIGHT ASSY REPLACED PER MM 33-51-00 OPS CKD OK. 2L74 4F A20WE 20050829000022005082900002NE 2005 8 29 EIA2005132 220050630A7200 ENGINE BOEING747 747273C 1384896NM PWA JT9 JT9D7J 52054NE NR 4 FAILED A EIAAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 NM09471EV 20651 662361 FL 340 IN CRUISE, NO TURBULENCE LOUD BANG WITH YAW TO RIGHT ENG NR 4 N1, N2 EGT PARAMETERS INDICATION EXCEEDENCES (RED) ENGINE FLAMED OUT. SECURED ENG. NO FIRE WARNING. METAL IN TAILPIPE REMOVED AND REPLACED NR 4 ENGINE IAW F7201/9724001. 2L74 4F4 F A20WE E20EA 20050829000042005082900004NM 2005 8 29 EIA2005134 120050709A3350 BULB BOEING747 747273C 1384896NM EMERGENCY LIGHT INOPERATIVE A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 R5 AND L5 AND L1 DOOR EMERGENCY EXIT LIGHTS, SILL LIGHTS, AND EXIT SIGNS WILL NOT ILLUMINATE. REMOVED AND REPLACED BULBS, LIGHT ASSY'S AND POWER SUPPLY BATTERY IAW 33-51-00. OPS CK OK. 2L74 4F A20WE 20050829000052005082900005NM 2005 8 29 EIA2005135 120050713A29133508807 PUMP BOEING747 747212B 1384886NM HYD SYSTEM LEAKING A EIAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 NM09482EV 20713 NR 1 HYD SYS SLOWLY LOST HYD QUANTITY AT TO GAGE SHOWED 9 GAL. GAGE SHOWED SLOW LOSS APPROX 2 HRS AFTER T/O. DID LEAK/LOSS PROCEDURES BUT LEAK CONTINUED, SYSTEM DEPRESSURIZED AND ADP OFF REMAINDER OF FLIGHT. REMOVED AND REPLACED NR 1 ENG HYDRAULIC PUMP PER MM 29-11-05 OPS AND LEAK CHECK OK. FOUND HYD PUMP LEAKING AT PARTING SURFACE. 2L74 4F A20WE 20050829000092005082900009NM 2005 8 29 EIA2005140 120050712A5311 FRAME BOEING747 747230B 1384889NM BS 803 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09487EV 23286 STA 803 WL 215 1.5" BELOW STR 24R DOOR FRAME WEB HAS A CRACK. REMOVED DAMAGE AND REPAIRED DOOR FRAME STA 803 WL 215 STR 24R AREA PER ECRA 487-53-025-2. 2L74 4F A20WE 20050829000102005082900010NM 2005 8 29 EIA2005141 120050712A5210 WEB BOEING747 747230B 1384889NM R1 DOOR PUNCTURED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09487EV 23286 STA 455 WL 247 STR 20R R1 DOOR INTERIOR WEB PUNCTURED. REPAIRED R1 DOOR INTERIOR WEB STA 455 WL 247 STR 20R PER ECRA 487-52-008-2. 2L74 4F A20WE 20050829000112005082900011NM 2005 8 29 EIA2005142 120050712A5320 STIFFENER BOEING747 747230B 1384889NM NLG WW CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09487EV 23286 TOP ON NLG BOX HAS CRACKED LONGITUDINAL STIFFENER AT LBL 26 STA 280-300. REPLACED STIFFENER PER B747 SRM 51-30-02 PGS 8-9 AND 51-30-05 PAGES 6-9. 2L74 4F A20WE 20050829000122005082900012NM 2005 8 29 EIA2005143 120050624A2612 FIRE WARNING BOEING747 747212B 1384886NM APU ACTIVATED A EIAAO OTHER N FALSE WARNING CRCRUISE 1 NM09485EV 20712 APU FIRE DETECTION AND PILOTS FIRE LIGHTS COME ON MOMENTARILY AND INTERMITTENTLY DURING CRUISE. APU FIRE WARNING, OPS CK OK IAW MM 26-11-00. 2L74 4F A20WE 20050829000142005082900014NM 2005 8 29 QXEA200501186 120050823A2530 COFFEEMAKER DHAV DHC8 DHC8202 2809007NM GALLEY ODOR A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM09353PH 496 SEA FLT NR 2276, FLT ATTENDANT REPORTS AN ELECTRICAL ODOR BY THE COFFEEMAKER IN GALLEY. MAINTENANCE DEFERRED NR 1 AND NR 2 WARMERS. BOTH CIRCUIT BREAKER PULLED AND WARMER DEACTIVATED. 2H72 4T RTA13NM 20050829000152005082900015NM 2005 8 29 QXEA200501187 120050823A2120 ODOR DHAV DHC8 DHC8202 2809007NM GALLEY DETECTED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM09353PH 496 SEA FLIGHT NR 2252, FLIGHT ATTENDANT REPORTS AN ELECTRICAL ODOR COMING FROM THE GALLEY AREA IN THE CABIN. MAINTENANCE PERFORMED GENERAL VISUAL INSPECTION OF GALLEY AREA AND PERFORMED OPERATIONAL TEST OF ALL INTERIOR LIGHTS AND HOT JUGS. INSPECTED RELAY PANEL BEHIND WARDROBE CLOSET. NO DEFECTS OF ODORS OF ELECTRICAL NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050829000162005082900016NM 2005 8 29 QXEA200501185 120050819A5210 MECHANISM DHAV DHC8 DHC8202 2809007NM PAX DOOR STIFF A QXEAO OTHER O OTHER TXTAXI/GRND HDL 1 NM09366PH 510 SE FLT NR 2073, FLT ATTENDANT NOT ABLE TO OPEN MAIN CABIN DOOR FROM INSIDE CABIN. ABLE TO OPEN FROM OUTSIDE. MAINTENANCE LUBRICATED THE LIFTING MECHANISM AND OPERATED THROUGH SEVERAL CYCLES. DOOR OPERATES SMOOTHLY. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050829000192005082900019EU 2005 8 29 WRNA200500019 120050818A2910A3233161502000 LINE AIRBUS300 A300B4203 3930306EU HYDRAULIC SYS LEAKING A WRNAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO05505TA 271 LOST GREEN HYD FLUID DURING GEAR RETRACTION. FOUND LT MAIN GEAR DOOR ACTUATOR LINE FAILED. REPLACED WITH TEMPORARY LINE IAW MM 20-23-11. SERVICED HYD'S IAW 12-12-29 OPS CK AND LEAK CK SATISFACTORY. ITEM PLACED ON CI, DMI NR 1927, TO BE REPLACED BY 9-17-05 OR 350 FLT HRS. 2L72 4F RTA35EU 20050829000202005082900020EU 2005 8 29 YENA200549 120050817A335032145410 POWER SUPPLY AIRBUS320 A320232 3930326EU EMERGENCY LIGHT INOPERATIVE A YENAK NONE O OTHER ININSP/MAINT 1 EA15598JB3300 2314 DURING PREFLIGHT, FOUND BOTH FWD CABIN DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EPSU PER 33-51-38, OPERATIONS CHECK NORMAL. 2L72 4F RTA28NM 20050829000222005082900022NM 2005 8 29 DHL2005781002 120050819A7722152BL801E INDICATOR BOEING727 727227 1384078NM EGT MALFUNCTIONED A DHLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01781DH 21996 REJECTED TO RNY 30L STL DUE TO NR 1 EGT EXCEEDING 620 DEGREES AT CALCULATED EPR OF 2.11 GW 178,400, PA 540 A/S 120 KNTS TEMP 25 DEGREES. REPLACED NR 1 EGT INDICATOR AND PERFORMED GROUND CHECK PER JRH 7.1 CHECK NORMAL. 2L73 4F A3WE 20050829000242005082900024EU 2005 8 29 WRNA200500020 120050824A2910221290 SOLENOID VALVE AIRBUS300 A300B4203 3930306EU NR 1 ENGINE LEAKING A WRNAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO05821SC 211 WHILE IN FLT, CLIMB, LOSS OF GREEN HYDRAULIC SYSTEM FLUID. AIRCRAFT RETURNED TO AIRFIELD, LANDING NORMAL. FOUND GREEN SYSTEM EDP SOLENOID VALVE LEAKING. REMOVED AND REPLACED EDP SOLENOID, OP'S CHECK SATISFACTORY IAW 29-11-32. AIRCRAFT LANDED OVERWEIGHT. INSPECTION PERFORMED PER 5-51-11, ALL SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA35EU 20050829000252005082900025CE 2005 8 29 DXTA200500920 120050824A3230 LANDING GEAR CESSNA750 750 2076810CE MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07915QS 7500015 CLIMBING THROUGH APPROX FL270, THE LANDING GEAR UNLOCK LIGHT BEGAN CYCLING ON AND OFF ACCOMPANIED BY THE LANDING GEAR SLAMMING INTO THE UP AND LOCKED POSTION CONTINUOUSLY 1 TO 2 TIMES PER SECOND BEGAN A DESENT AND THE CYCLING STOPPED AT APPROX FL200 WHEN LOW ENOUGH AND SLOW ENOUGH THE GEAR WAS SELECTED DOWN AND GOT 3 GREEN LIGHTS NO RED. 2L72 4J RTT00007WI 20050829000272005082900027SO 2005 8 29 C2XA05CL064 120050814A335078241 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT FAULTY A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715912 145439 MCI FLIGHT NR 2657, THE CREW REPORTED THE GALLEY EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20050829000282005082900028SO 2005 8 29 C2XA05BT059 120050816A335078241 INVERTER EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT FAULTY A C2XAO OTHER O OTHER NRNOT REPORTED 1 SW2713118 145675 STL---CO3279, CREW REPORTED EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED INVERTER, OPS CHECKED AND RETURNED TO SERVICE GOOD. 2L72 4F RT 20050829000292005082900029SO 2005 8 29 C2XA05CL065 120050818A33501317 BULB EMB 135 EMB135ER 3260203SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2717507 145215 DURING ROUTINE MAINTENANCE, THE EMERGENCY CEILING LIGHT AT ROW 6 WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BULB. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20050829000302005082900030CE 2005 8 29 DXTA200500919 120050824A3230 LANDING GEAR CESSNA650 650 2076802CE MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07792QS 6507092 LANDING GEAR WOULD NOT RETRACT ON TAKEOFF. 2L72 4F A9NM 20050829000312005082900031CE 2005 8 29 DXTA200500918 120050823A3260602751 DOWNLOCK SWITCH CESSNA750 750 2076810CE MLG FAULTY E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07935QS 7500135 ON GEAR RETRACTION GREEN LT MAIN GEAR DOWN LIGHT REMAINED ILLUMINATED. GEAR APPEARED FULLY RETRACTED. GEAR EXTENDED NORMALLY FOR LANDING. REMOVED FAULTY DOWN LOCK SWITCH FROM LT POSITION. INSTALLED NEW SWITCH. OPS CHECKS GOOD IAW CESSNA 750 MM 32-30-04. 2L72 4J RTT00007WI 20050829000322005082900032NM 2005 8 29 DXTA200500921 120050822A2780 CONTROL SYSTEM AMD FALC50FALCON2000 2730170NM SLAT/FLAPS MALFUNCTIONED E DXTAO OTHER J WARNING INDICATION CRCRUISE 1 GL07229QS 129 FLAP SLATS NIPS LIGHT OUT IN FLIGHT. LEFT SLAT NOT RETRACTING COMPLETELY, FLAPS/SLATS DEPLOYED AT CRUISE. 2K73 4F RTA50NM 20050829000332005082900033CE 2005 8 29 DXTA200500923 120050824A2120 ODOR CESSNA750 750 2076810CE CABIN DETECTED E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07960QS 7500160 DURING CRUISE AT FL 400, A VERY STRONG ACRID BURNING ODOR WAS DETECTED BY CREW AND PAX. PRECAUTIONARY LANDING MADE. STRONG ODOR ON GROUND WAS AROUND BAGGAGE AND HELL HOLE AREA. NO VISABLE SMOKE. 2L72 4J RTT00007WI 20050829000342005082900034CE 2005 8 29 DXTA200500922 120050824A2750 FLAP SYSTEM CESSNA750 750 2076810CE TE MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION DEDESCENT 1 GL07948QS 7500149 WHEN FLAPS SELECTED TO FIVE, FLAP FAIL CAS MESSAGE APPEARED. FOLLOWED CHECKLIST, ATTEMPTED RESET, FLAPS FALLEN AGAIN IN THE FLAP FIVE POSITION. 2L72 4J RTT00007WI 20050829000362005082900036NM 2005 8 29 DHL2005783003 120050826A2780 SWITCH BOEING727 727227 1384078NM LE FLAPS FAILED A DHLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01783DH 21999 UPON RETRACTING FLAPS FROM 5 TO 2 DEG LED IN TRANSIT LIGHT REMAINED ILLUMINATED. CHECKED SO PANEL, NR 5 LE FLAP IN TRANSIT. PERFORMED ABNORM PROCEDURE, NO CHANGE RETURNED TO CVG. REMOVED AND REPLACED NR 5 L/E FLAP SWITCH IAW MM 27-82-01, OPS CHECK GOOD. 2L73 4F A3WE 20050829000372005082900037NM 2005 8 29 AWXA200501006 120050823A3350 LIGHT BOEING757 7572S7 1384962NM R1 DOOR SLIDE INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28904AW 23566 BWI - EEL - DURING A CHECK INSPECTION IN BWI, FOUND THE R1 DOOR SLIDE LIGHT INOPERATIVE. MAINTENANCE ISSUED AN MEL. 2L72 4F RTA2NM 20050829000392005082900039NM 2005 8 29 AWXA200501008 120050825A2560P2070001214 FLASHLIGHT BOEING737 7373G7 1384595NM CABIN INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 SFO - EEL - FLT 227 - CREW REPORTED, ON OVERNIGHTING AIRCRAFT, THE FORWARD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE ISSUED AN MEL. PHX - MAINTENANCE REPLACED THE FLASHLIGHT AS REQUIRED. 2L72 4F RTA16WE 20050829000422005082900042WP 2005 8 29 05FDEA02650 120050825A5712 RIB DOUG DC10 DC1010 3022110WP ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LT WING FIXED LEADING EDGE AT XORS 638 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 1, 3, 4 VOL I AND INSTALLED ANGLE REPAIR. 2L73 4F A22WE 20050829000432005082900043WP 2005 8 29 05FDEA02651 120050825A5712 RIB DOUG DC10 DC1010 3022110WP LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LT WING FIXED LEADING EDGE AT XORS 594 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 3, 4 VOL I AND INSTALLED ANGLE REPAIR. 2L73 4F A22WE 20050829000452005082900045NM 2005 8 29 DHL2005751004 120050823A3260 PROXIMITY SWITCH BOEING727 727264 138408MNM MLG MALFUNCTIONED A DHLAO OTHER N FALSE WARNING APAPPROACH 1 SO01751DH 22982 ON FINAL WITH GEAR EXTENDED, THE RED LEFT GEAR UNSAFE LIGHT ILLUMINATED ALONG WITH NORMAL 3 GREEN INDICATIONS. CLEANED LEFT MAIN GEAR PROX SWITCH SYSTEM, OPS CK NORMAL IAW M/M 32-61-01. 2L73 4F A3WE 20050829000462005082900046NM 2005 8 29 EIA2005144 120050712A5230 SKIN BOEING747 747230B 1384889NM CARGO DOOR CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09487EV 23286 AFT LOWER CARGO DOOR INNER LOWER SKIN CORRODED SEVERAL PLACES. REMOVED CORROSION FROM FT LOWER C/D INNER SKIN PER B747 SRM 51-10-01 AND REPAIRED INNER LWR SKIN PER ECRA 487-52-002-2. 2L74 4F A20WE 20050829000472005082900047NM 2005 8 29 EIA2005145 120050627A2612 CIRCUIT CARD BOEING747 747212B 1384886NM APU FIRE MALFUNCTIONED A EIAAO OTHER N FALSE WARNING CRCRUISE 1 NM09485EV 20712 INTERMITTENT FIRE WARNING INDICATION ON APU DURING FLIGHT. OCCURS WITH LOOP SELECTOR IN BOTH A OR B. ACCOMPLISHED FIRE TEST ON APU, APU TEST NORMAL. PULLED APU FIRE HANDLE AS PRECAUTIONARY. RERACKED APU FIRE WARNING CARD, OPS CK GOOD. 2L74 4F A20WE 20050829000492005082900049NM 2005 8 29 EIA2005146 120050628A2612 FIRE LOOP BOEING747 747212B 1384886NM APU BAY CHAFED A EIAAO OTHER N FALSE WARNING CRCRUISE 1 NM09485EV 20712 INTERMITTENT FIRE WARNING INDICATION ON APU DURING FLIGHT. PULLED A LOOP CB FOR APU FOR FIRE WARNING SYSTEM WHICH STOPPED INTERMITTENT FIRE WARNING. FOUND WIRING ON APU A LOOP FIRE WARNING CONNECTION CHAFING WITH STRUCTURE. REPAIR PER STANDARD PRACTICE 20-3--22, OPS CHK OK PER MM 26-25-00. 2L74 4F A20WE 20050829000502005082900050NM 2005 8 29 EIA2005148 120050801A3350 LIGHT BOEING747 747230B 1384889NM CABIN INOPERATIVE A EIAAK NONE L NO TEST ININSP/MAINT 1 NM09487EV 23286 5 EA EMERGENCY LIGHTS INOP. REMOVED AND REPLACED 5 EA EMERGENCY LIGHT ASSY PER B747 MM 33-51-07. OPS CHECKED GOOD PER B747 MM 33-51-0. 2L74 4F A20WE 20050829000522005082900052NM 2005 8 29 EIA2005150 120050817A8011 WARNING LIGHT BOEING747 747121 1384871NM START VALVE ILLUMINATED A EIAAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 NM09480EV 20348 NR 4 ENGINE "START VALVE" LIGHT ILLUMINATED IN FLIGHT: ACCOMPLISHED ABNORMAL PROCEDURES AND INFLIGHT ENGINE FAILURE AND SHUTDOWN CHECKLIST. STARTER VALVE FAILURE CW WINDMILL INSP IAW 72-00-00 AND INFLIGHT SHUTDOWN INSPECTION. NO DEFECTS NOTED REINSTALLED ORIGINAL START VALVE AND REOPENED DMI NR 4000 R AND RD STARTER FOR INFLIGHT SHUTDOWN IAW 80-11-01. 2L74 4F A20WE 20050829000542005082900054EA 2005 8 29 QXEA200501189 220050825A7200 WARNING LIGHT BOMBDRDHC8 DHC8402 1390042NM PWC 150 PW150A EA ENGINE ILLUMINATED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09410QX 4053 GEG FLIGHT NR 2371: AFTER PUSHBACK, POWERPLANT MESSAGE ON ED. MAINTENANCE INTERROGATED CDS. FOUND FAULT CODE 132 CHANNEL A OF NR 1 ENGINE. PERFORMED FIM TASK 61-20-03-810-816. FAULT CODE CLEARED. NO FURTHER MAINTENANCE REQUIRED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E00062EN 20050829000562005082900056NE 2005 8 29 05FDEA02544 220050818A7532 BLEED VALVE AIRBUS300 A300B4622 3930401EU PWA 4158 PW4158 NE NR 1 ENGINE FAILED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25716FD 358 SHORTLY AFTER T/O NR 1 ENGINE HP BLEED VALVE FAULTED. TEMP ON ECAM BLEED PAGE SHOWED 255-260 DEGREES. WITHIN 30 SECONDS REGULAR BLEED VALVE FAULTED. REMOVED AND REPLACED NR 1 ENGINE FAN AIR VALVE, ALL CHECKS NORMAL PER MM 36-11-16-4-03. ACCOMPLISHED NR 1 ENGINE RUN PER A300 JRH, NO FAULTS NOTED. 2L72 4F4 FRTA35EU E24NE 20050829000582005082900058EA 2005 8 29 VTZA200500144 120050818A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FS 621 CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27678BR 7653 RT FS 621 FLOOR SUPPORT IS CRACKED AT 1 INCH IN ANGLE. 2L72 4F RTA21EA 20050829000592005082900059EA 2005 8 29 VTZA200500145 120050818A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA BS 624 CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27678BR 7653 RT OBLIQUE ANGLE IS CRACKED AT 1 INCH IN RADIUS. 2L72 4F RTA21EA 20050829000622005082900062EA 2005 8 29 VTZA200500146 120050818A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA BS 621 CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27678BR 7653 LT FS 621 FLOOR SUPPORT IS CRACKED AT 1 INCH IN ANGLE. 2L72 4F RTA21EA 20050829000632005082900063EA 2005 8 29 VTZA200500147 120050818A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA BS 624 CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27678BR 7653 LEFT 624 OBLIQUE ANGLE IS CRACKED AT 1" IN RADIUS. 2L72 4F RTA21EA 20050829000642005082900064WP 2005 8 29 05FDEA02576 120050819A2697 WIRE DOUG DC10 DC1010 3022110WP FIRE BOTTLE PULLED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO2540061 46973 NR 2 ENGINE FIRE BOTTLE HAS 2 WIRES PULLED FROM PRESS SWITCH ON INBOARD BOTTLE. REMOVED AND REPLACED NR 2 FIREBOTTLE SWITCH CONNECTOR P1-1264 IAW BSWPM 20-31-03. REMOVED AND REPLACED TERMINAL STRIP S3-403 IAW BSWPM 20-20-03. REPLACED WIRING 2W253L22 AND 2W258A22N IAW BSWPM 20-10-01 AND DC10-10MM 26-21-01-05, LOW PRESSURE TEST GOOD IAW DC10-10MM 26-21-06-2. 2L73 4F A22WE 20050829000692005082900069EA 2005 8 29 QXEA200501182 120050820A3620 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA ILLUMINATED A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09611QX 10041 BIL, ON PUSH BACK FOR FLIGHT 4311, THE DUCT MON FAULT MESSAGE APPEARED. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE PLACED THE SYSTEM ON MEL 36-21-7B, RSI 349850. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20050829000702005082900070EU 2005 8 29 SF20050827 120050827A2422 INVERTER SAAB SF340 SF340A 7850100EU FAILED A UHLAA UNSCHED LANDING S AFFECT SYSTEMS CRCRUISE 1 GL1714XS 340A014 FLIGHT 7547 IAD-SCE, CREW CALLED MAINTENANCE CONTROL ON THE RADIO REPORTING, MAIN INVERTER FAILED IN FLIGHT. AIRCRAFT RETURNED TO IAD. 2L72 4T RTA52EU 20050829000722005082900072NE 2005 8 29 SF200508161 220050816A7200 ENGINE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE MALFUNCTIONED A UHLAO OTHER J WARNING INDICATION CRCRUISE 1 GL1719XS 340A019 132 FLT NR 7558 FROM IAD-ABE, AIRCRAFT WAS EN ROUTE TO ABE IN CRUISE AT 75 PERCENT WHEN ENGINE WENT TO 101 PERCENT. AIRCREW PULLED POWER BACK TO 35 PERCENT PUT INTO TORQUE MOTOR LOCKOUT AND EVERYTHING STABILIZE. CONTINUED SAFELY TO ABE. 2L72 4T4 TRTA52EU E8NE6 20050829000732005082900073EA 2005 8 29 QXEA200501181 120050819A5230 VENT CNDAIRCL600 CL6002C10 1390015EA CARGO DOOR UNLATCHED A QXEAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 NM09601QX 10009 OKC - ON FLIGHT 4184 ,THE PROX SYSTEM 2 FAULT ILLUMINATED FOR THE FORWARD CARGO DOOR. AIRCRAFT RETURNED TO THE FIELD AND ACCOMPLISHED AN UNEVENTFUL LANDING. MAINTENANCE FOUND THE FORWARD CARGO DOOR VENT NOT PROPERLY LATCHED. LATCHED, AND PERFORMED INSPECTION OF AREA, NO DEFECTS NOTED. PERFORMED OPERATIONAL CHECK OFF DOOR, CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2L72 4F RTA21EA 20050829000742005082900074EU 2005 8 29 MALA050596 120050721A5320 SEAT TRACK SAAB SF340 340B 7860101EU BS 297-310 CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15439XJ 340B439 DURING 4Y/2Y CHECK IN BNA, FOUND SEAT TRACK AT LBL 18.3 AND BETWEEN FS 297 AND 310 IS CORRODED AND HAS BEEN REPAIRED IAW SRM 53-70-60. REF: EAMS WORK ORDER 212650 TASK 2512. 2L72 4T RTA52EU 20050829000752005082900075NM 2005 8 29 UPS05245261 120050801A5330 SKIN BOEING727 72730C 1384009NM BS 355 S8-10 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919UP 19012 AREA OF CORROSION ON SKIN BS 355, BETWEEN STR 8 AND 10 LT. PAINT STRIP AREA IF REQUIRED, REMOVE CORROSION AND RECTIFY. REPAIR CARRIED OUT IAW SRM 51-10-1, 53-30-1 MM 25-21-2 AND AAAE EO 200 5-077-001 UPS ENGINEERING FILE NO. B727-5330-22744-A. 2L73 4F A3WE 20050829000762005082900076NM 2005 8 29 UPS05245262 120050804A5320 STIFFENER BOEING727 72730C 1384009NM BS 870 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919UP 19012 RT MLG W/W, EVIDENCE OF CORROSION ON VERTICAL STIFFENER CEILING AREA BS 870 RBL 45. REPAIR CARRIED OUT IAW SRM 51-40-4. 2L73 4F A3WE 20050829000772005082900077NM 2005 8 29 UPS05245263 120050803A5315 FLOORBEAM BOEING727 72730C 1384009NM BS 328 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919UP 19012 FLOORBEAM TOP CHORD CORROSION OUTSIDE LIMITS BS 328 RBL 12. REPAIR CARRIED OUT IAW SRM 53-10-8 & 51-10-2. 2L73 4F A3WE 20050829000782005082900078NM 2005 8 29 UPS05245264 120050731A5340 ATTACH ANGLE BOEING727 72730C 1384009NM BS 294.5 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919UP 19012 RT SIDE AFT OF BS 294.5 FWD ATTACHMENT ANGLE OF NWW BOX HAS EVIDENCE OF CORROSION. WEB REPAIRED IAW SRM 51-40-2. 2L73 4F A3WE 20050829000802005082900080EU 2005 8 29 SF8202005 120050820A7712 INDICATOR SAAB SF340 SF340A 7850100EU RT TORQUE FAULTY A UHLAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL17121CQ 121 FLIGHT 7558 IAD-ABE, AFTER ARMING CONSTANT TORQUE ON TAKEOFF, RIGHT ENGINE TORQUE INDICATED 20 PERCENT LOWER THEN SELECTED. AIRCRAFT REJECTED TAKEOFF AND RETURNED TO BLOCK. FOUND RIGHT TORQUE INDICATOR TO BE AT FAULT. R/R INDICATOR, OPS CHECK GOOD. 2L72 4T RTA52EU 20050829000822005082900082WP 2005 8 29 ABXA050203 120050824A32600080004003 CONTROL BOX DOUG DC9 DC941 302207NWP MLG PROXIMITY DEFECTIVE A ABXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL23952AX3818 47615 GEAR DOOR OPEN LIGHT ILLUMINATED IN FLIGHT. INSPECTED AIRCRAFT MAIN LANDING GEAR DOOR UPLATCHES AND MECHANISMS IAW DC-9 AMM 32-60-03-2. ALL OKAY, NO DEFECTS NOTED. INSPECTED PROX SENSORS FOR POSITIONING AND ATTACHMENT, NO DEFECTS NOTED. REMOVED AND REPLACED LANDING PROX SWITCH CONTROL BOX IAW DC-9 AMM. OPS CHECKED GOOD. LUBRICATED MAIN LANDING GEAR DOOR UPLATCHES AND ROLLERS. ALL OKAY. (PROBLEM REPORTED OUT OF GEG EN ROUTE TO BIL) DIVERTED AIRCRAFT TO SLC. CREW RECYCLED GEAR INTO SLC, GEAR RECYCLED OKAY. 2L72 4F A6WE 20050829000832005082900083WP 2005 8 29 ABXA050204 120050824A32607000010101ABX DOWNLOCK SWITCH DOUG DC9 DC931 3022065WP LT MLG DEFECTIVE A ABXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23907AX 47203 LEFT MAIN GEAR UNSAFE LIGHT STAYED ON AFTER GEAR RETRACTION, RECYCLED GEAR AND GEAR UNSAFE LIGHT WENT OUT. FOUND NR 5 PIN ON DOWNLOCK SWITCH DIRTY, CLEANED RECEPTACLE AND PIN. CHECKED DOWNLOCK SWITCH, FOUND INTERMITTENT. OPS CHECKED AND VERIFIED PROBLEM. REMOVED AND REPLACED DOWNLOCK SWITCH IAW DC-9 MM 32-60-01-2-0101. OPS CHECKED GOOD. 2L72 4F A6WE 20050829000842005082900084WP 2005 8 29 ABXA050205 120050824A323049245891 ROD END DOUG DC9 DC931 3022065WP LT MLG WORN A ABXAO OTHER J WARNING INDICATION CLCLIMB 1 GL23907AX 47203 LEFT MAIN GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. PLACED GEAR LEVER IN UPLATCH CHECK POSITION AND GEAR DOOR OPEN LIGHT CAME ON. RECYCLED GEAR AND BOTH LIGHTS WENT OUT. INSPECTED LEFT MAIN LANDING GEAR COMPONENT. FOUND LEFT GEAR ACTUATOR END WORN EXCESSIVELY. REMOVED AND REPLACED ROD END IAW DC-9 MM 32-32-04 AND PERFORMED LANDING GEAR EXTENSION AND RETRACTION TEST IAW DC-9 MM 32-30-00. OPS CHECKED GOOD. 2L72 4F A6WE 20050829000852005082900085 2005 8 29 ABXA050206 420050826A34212587335113 GYRO DOUG DC9 DC931 3022065WP VERTICAL DEFECTIVE A ABXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL23906AX7 47072 DURING CLIMB FROM YYC, CAPTAIN'S ADI HAD NUMEROUS INTERMITTENT GYRO FLAGS AND ADI WAS ERRATIC. IN CRUISE, INTERMITTENT ROLL FLAGS. REMOVED AND REPLACED NR 1 VERTICAL GYRO IAW DC-9 AMM 37-27-01-4. SYSTEM OPS CHECKED GOOD. (CACTUS CALL OUT OF YYC ENROUTE TO FAR) THERE WERE NO PARTS IN FAR, SO DECISION WAS MADE TO ROUTE MXA OVER FAR DIRECT TO FSD. 2L72 4F A6WE 20050829000872005082900087WP 2005 8 29 05FDEA02581 120050822A5330 SKIN DOUG MD10 MD1010F 3022112WP BS 1381 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25571FE 47830 DURING AIRPLANE'S CONVERSION FROM P TO F FOUND: ON UPPER SURFACE OF CTR WING BOX AT STA 1381 LT SIDE X = 75'' CORROSION ON SKIN; REMOVED SLANT PANEL LT SIDE IAW MM 20-50-02, CUT ANGLE APB 7081-1 IAW SRM 53-40-00 FIG 11 SH 2. REMOVED CORROSION IAW SRM 51-21-00 PAG 28, CHECKED LIMITS IAW SRM 57-20-00 FIG 8A, COMPLETED WORK PER EA 8-5710-84088. REPLACED GASKET, P/N AEA 0487-1 QTY: 1 2L73 4F RTA22WE 20050829000912005082900091NE 2005 8 29 MALA050666 220050822A7200 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RIGHT ODOR A MALAE ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL15406XJ 340B406 CLIMBING THROUGH 15000 FEET EN ROUTE TO DTW SMELLED A WEIRD ODOR IN FLIGHT DECK. LOOKED DOWN AT THE ENGINE INSTRUMENTS AND NOTED THE RIGHT ENGINE OIL PRESSURE GAUGE FLUCTUATING INTO THE YELLOW ARC, THEN INTO GREEN CONTINUOUSLY ABOUT 30 SEC. AFTER THAT, HEARD A BANG AND THE RIGHT ENGINE FAILED. REPLACED RT ENGINE ASSY IAW JC 7100-301. WO 394760 FOR DETAILS SN ON GE-E785714. CURRENT MARGIN 57C. 2L72 4T4 TRTA52EU E8NE 20050829000922005082900092EU 2005 8 29 MALA050671 120050820A2432 BATTERY BAC 146 AVRO146RJ85A1500097EU MASTER FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15527XJ E2352 FAILED CAP CHECK. 2H74 4F RTA49EU 20050829000932005082900093NE 2005 8 29 MALA050667 220050822A7200 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LEFT FAILED A MALAO OTHER M OVER TEMP CLCLIMB 1 GL15406XJ 340B406 ADVANCING THE POWER ON THE LEFT ENGINE AFTER THE RT FAILED. ACCIDENTALLY PUSHED THE POWER LEVER UP TO MUCH AND THE RED OVER TEMP LIGHT CAME ON AND ITT WAS 1000C. CORRECTED AFTER 5 TO 10 SECONDS. REPLACED LT ENGINE ASSY IAW JC 7100-301. WO 381423 FOR DETAILS SN ON GE-E785664, MARGIN 50C. 2L72 4T4 TRTA52EU E8NE 20050829000952005082900095EU 2005 8 29 MALA050670 120050819A7603 CONDITION LEVER SAAB SF340 340B 7860101EU LT PROPELLER FAILED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15365PX 340B265 NO CONTROL OF LT PROP RPM IN FLIGHT CONDITION LEVER MOVES FREELY WITH NO CHANGE IN RPM. ALL OTHER PARAMETERS NORMAL ENGINE WOULD NOT SHUT DOWN AT GATE. PULLED FIRE HANDLE. REMOVED AND REPLACED LT CONDITION CABLE. PERFORMED ALL RUNS AND OPS CHECK IAW SAAB AMM 76-10-46. 2L72 4T RTA52EU 20050829000992005082900099 2005 8 29 SWAA052560 420050824A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050829001022005082900102NM 2005 8 29 SWAA052563 120050824A33507003661 BALLAST BOEING737 7377H4 1384404NM EMERGENCY EXIT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29425LV 29829 DURING SCHEDULED MV2 CHECK, FOUND RIGHT CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BALLAST PER MM. 2L72 4F RTA16WE 20050829001032005082900103 2005 8 29 SWAA052564 420050824A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29444WN 29839 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050829001072005082900107NM 2005 8 29 SWAA052568 120050825A2750569670 MOTOR BOEING737 7375H4 138449DNM TE FLAPS FAULTY A SWAAO OTHER O OTHER NRNOT REPORTED 1 SW29507SW 24184 LOUD NOISE HEARD WHEN FLAPS ARE EXTENDED & RETRACTED. REMOVED AND REPLACED FLAP HYDRAULIC DRIVE MOTOR PER MM. 2L72 4F RTA16WE 20050829001102005082900110WP 2005 8 29 ROSA2005040 120050415A213354447211 ACTUATOR DOUG DC9 DC915F 3022037WP OUTFLOW VALVE FAILED A ROSAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW01166DE754 47152 LOST CABIN PRESSURE AT 19,000 FEET, RETURNED TO AIRPORT. REMOVED AND REPLACED OUTFLOW VALVE ACTUATOR AND CABIN PRESSURE CONTROLLER SIGNAL AMPLIFIER SYSTEM FUNCTION CHECKS SATISFACTORY AT THIS TIME. 2L72 4F A6WE 20050829001112005082900111CE 2005 8 29 CIEA200500015 120050824A33109036402211 CIRCUIT BOARD BEECH 200 200BEECH 1152920CE LIGHTING SYS SHORTED E CIEAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM03428P 7740 BB745 DURING PILOT PREFLIGHT THE PILOT WAS CHECKING THE FUEL CROSSFEED SYSTEM AND SWITCHED TO CROSSFEED TO THE RT ENGINE. THE PILOT THEN HEARD A CRACKLIN SOUND AND SAW SOME SMOKE COMING FROM THE SWITCH AREA. THE PILOT THEN CANCELED THE TRIP. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THAT THE CROSSFED SYSTEM HAD NOTHING TO DO WITH THE SMOKE. THE EDGE LIGHTED PANEL FOR THE BACK LIGHTENING HAD SHORTED OUT AT ONE OF THE BULBS. 1L72 4T A24CE 20050829001152005082900115EA 2005 8 29 COMA0560456 120050820A2621365000183 FIRE BOTTLE CNDAIRCL600 CL6002B19 1900309EA CARGO LOW A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01926CA276443710 7027 FLIGHT 4949 - CARGO LOW BOTTLE MESSAGE. REPLACED THE CARGO FIRE BOTTLE. 2L72 4F RTA21EA 20050829001172005082900117NM 2005 8 29 05FDEA02666 120050826A5320 INTERCOSTAL DOUG MD11 MD11 3023602NM BS 1621 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 AFT CABIN INTERCOSTAL AT STA 1621 RT LONGERON 7 FOUND CRACK. INTERCOSTAL REMOVED AND FABRICATED FROM 7075-0-0.032 AS PER DRAWING AFA 7761. CARRIED OUT HEAT TREATMENT ON FABRICATED PART, PAINTED AND INSTALLED AS PER SRM 51-35-01 VOL II. CLASSIFIED MINOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050829001212005082900121EA 2005 8 29 COMA0560458 120050821A2750 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS OUT OF RIG A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01965CA 7131 FLIGHT 5858 - FLAPS FAIL CAUTION. ADJUSTED THE RIGGING OF THE RT BPSU. 2L72 4F RTA21EA 20050825000372005082500037SO 2005 8 25 SWIA200515453 120050820A213032144143 VALVE EMB 120 EMB120ER 3260203SO RT A/C PACK SMOKE A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM07568SW1146011460 120343 STRONG SMELL OF SMOKE IN CABIN. RECEIVED A PACK FAIL LIGHT. REPLACED RIGHT PACK PRESSURE REGULATOR SHUT OFF VALVE. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050825000392005082500039SO 2005 8 25 SWIA200515455 120050820A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07561SW9385 9385 120335 EMERGENCY STRIP LIGHTS ADJACENT TO GALLEY INOP. REPLACED FORWARD EMERGENCY BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050825000462005082500046NE 2005 8 25 DL76S050470 220050820A7314 PUMP BOEING767 767332 1382001NM GE CF680 CF680A2 NE NR 1 ENGINE LEAKING A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO27118DL 23277 580405 FUEL IMBALANCE OF 3500LBS, DIVERTED TO OMA, FOUND BOLT AT LT ENGINE FUEL PUMP MISSING AND LEAKING. REPLACED GASKET AND 4 BOLTS. 2L72 4F4 FRTA1NM E13NE 20050825000502005082500050WP 2005 8 25 DHL2005806502 120050816A5754 FRAME DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE RT WING SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH87034 46002 RT WING CTR L/E FORMER UPPER PART CRACKED 0.250 INCH, STA XFS 416.500. PERFORMED STOP HOLE AND FABRICATED 2 THIN FORMED ANGLE DOUBLERS (AL7075T6 0.032 INCH) IAW SRM 57-2-0 PG. 9-10. CLEANED, TREATED AND PRIMED AREA AND 2 THIN FORMED ANGLE DOUBLERS IAW SRM 51-1-8B. INSTALLED 2 THIN FORMED ANGLE DOUBLERS IAW SRM 57-2-0 PG. 9-10. 2L74 4F4 FRT4A25 E2GL 20050825000652005082500065NM 2005 8 25 05FDEA02593 120050823A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 N01510 WHILE WORKING FED EX NON ROUTINE CARD 5184, FOUND THE FRAME TO BE CRACKED AT BODY STATION 420 STRINGER 20R ** SD ** COMING REPAIRED CRACK PER SRM 51-40-3, THIS IS A MAJOR REPAIR. 2L73 4F RTA3WE 20050831000312005083100031NM 2005 8 31 05FDEA02591 120050823A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 CORROSION ON SKIN AT NR 3 VHF ANTENNA MOUNTING BRACKET CUT OUT BS 1042 WL 138.5 (AFT CARGO COMPARTMENT) REMOVED CORROSION ON SKIN AT NR 3 VHF ANTENNA MOUNTING BRACKET CUTOUT BS 1042 BL 0 WL 138.5 FOUND TO BE WITHIN LIMITS ALL WORK DONE IAW SRM 53-30-1, 51-10-1 2L73 4F RTA3WE 20050825000812005082500081WP 2005 8 25 UPS05845256 120050815A5340 FITTING DOUG DC8 DC871F 302199DWP FS 1768 L17R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 END FITTING CRACKED LONG 17R FS 1768. REMOVED AND REPLACED END FITTING AT STA 1768 LONG 17R IAW DWG 4772397 AND SRM51-1-20D. 2L74 4F RT4A25 20050825000832005082500083WP 2005 8 25 UPS05845258 120050811A5340 ANGLE DOUG DC8 DC871F 302199DWP FS 798 LBL48 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 CENTER WING BOX SUB FLOOR "L" ANGLE CRACKED AT FS 798 LBL 48. REMOVED AND REPLACED "L" ANGLE AT FS 798 LBL 48 IAW SRM 51-3-2 AND SRM 51-1-20D. 2L74 4F RT4A25 20050825000852005082500085NM 2005 8 25 UPS05M45248 120050610A5313 LONGERON DOUG MD11 MD11F 3023600NM CABIN CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01255UP 48404 INSPECTION C-CK, CABIN-STA 1239 TO 1249 L-27 LONGERON RT FOUND CORROSION AS MARKED CABIN STA 1239 TO 1249 L27 RT CORRODED LONGERON. FABRICATED AS PER EN13 24-05 AND INSTALLED AS PER SRM 51-31-01VOL II REV 37. 2L73 4F RTA22WE 20050825000892005082500089EU 2005 8 25 AWXA200500999 120050815A5347D533711200500 SEAT TRACK AIRBUS320 A320231 3930325EU FR 41-47 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28645AW 238 SAL - DURING C3 CHECK, DISCOVERED CORROSION ON SEAT TRACK LOCATED AT RT OUTBOARD SIDE AT FR 42+17, -Y1292. MAINTENANCE REMOVED CORROSION AND FOUND REWORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15. REMOVED SEAT TRACK AT FR 42+17, -Y1292 AND INSTALLED NEW SEAT TRACK IAW AIRBUS 320 SRM 53-31-15 FIG 2. 2L72 4F RTA28NM 20050825000912005082500091EU 2005 8 25 AWXA200501001 120050815A5347D5337111008 SEAT TRACK AIRBUS320 A320231 3930325EU FR 41-47 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28645AW 238 SAL - DURING C3 CHECK, DISCOVERED CORROSION ON SEAT TRACK LOCATED AT LT INBOARD SIDE AT FR 44+7, Y765. MAINTENANCE REMOVED CORROSION AND FOUND REWORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15. REMOVED SEAT TRACK AT FR 44+7, Y765 AND INSTALLED NEW SEAT TRACK IAW AIRBUS 320 SRM 53-31-15 FIG 2. 2L72 4F RTA28NM 20050825000932005082500093EU 2005 8 25 AWXA200501003 120050815A5347D53371112004 SEAT TRACK AIRBUS320 A320231 3930325EU FR 41-47 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28645AW 238 SAL - DURING C3 CHECK, DISCOVERED CORROSION ON SEAT TRACK LOCATED ON THE LT OUTBOARD SIDE AT FS 42 +16" Y1292. MAINTENANCE REMOVED CORROSION AND FOUND REWORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15. REMOVED SEAT TRACK AT FS 42 +16" Y1292 AND INSTALLED NEW SEAT TRACK IAW AIRBUS 320 SRM 53-31-15 FIG 2. 2L72 4F RTA28NM 20050825000952005082500095EU 2005 8 25 AWXA200501005 120050815A5347D57130147203 SEAT TRACK AIRBUS320 A320231 3930325EU FR 36-41 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28645AW 238 SAL - DURING C3 CHECK, DISCOVERED CORROSION ON SEAT TRACK LOCATED ON THE RT OUTBOARD SIDE AT FR 39 +3" Y-1292. MAINTENANCE REMOVED CORROSION AND FOUND REWORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15. REMOVED SEAT TRACK AT FR 39 +3" Y-1292 AND INSTALLED NEW SEAT TRACK IAW AIRBUS 320 SRM 53-31-15 FIG 2. 2L72 4F RTA28NM 20050825001022005082500102NM 2005 8 25 AWXA200500987 120050706A57536546431285 WEDGE BOEING737 7373G7 1384595NM ZONE 500 DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28311AW 24712 DURING C15 CHECK DISCOVERED DISBOND AREA ON THE LT OUTBOARD FORE FLAP FROM WBL 310 TO WBL 313.5. MAINTENANCE REMOVED DISBOND SKIN AND CORE ON THE LOWER SKIN OF LT OUTBOARD FORE FLAP IAW BOEING 737-300 SRM 51-70-10-0 REPAIR 7, FIG 16. FABRICATED CORE AND EXTERNAL DOUBLER IAW BOEING 737-300 SRM 51-70-10-0 REPAIR 7, FIG 16. BONDED AND SEALED FABRICATED REPAIR PARTS TO THE LT OUTBOARD FORE FLAP FROM WBL 310 TO WBL 313.5 IAW BOEING 737-300 SRM 51-70-10-0 REPAIR 7, FIG 16. 2L72 4F RTA16WE 20050825001042005082500104NM 2005 8 25 AWXA200500989 120050820A3412 WIRE BOEING757 757225 1384959NM AIR/GROUND SYS INOPERATIVE A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28907AW 22691 PHX - AIR TURN BACK - FLT 277 - TAT PROBE FAULTED AFTER TAKEOFF. CREW RETURNED TO PHX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPAIRED WIRING AT THE AIR/GROUND SYSTEM TWO RELAY (K203) IAW BOEING 757 AMM 20-81-12. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA2NM 20050826000062005082600006WP 2005 8 26 05FDEA02604 120050824A5751 SKIN DOUG DC10 DC1010 3022110WP GE CF6 CF66K 30020NE ZONE 500 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LT WING LOWER SURFACE ON IB AILERON: FOUND NR 1 DENT ( LENGTH 0.87 INCH ; DEPTH 0.094 INCH) AND FOUND NR 1 DENT (LENGTH 0.63 INCH ; DEPTH 0.027 INCH) AT STA XW 343 CUT DAMAGED PORTION OF LOWER SKIN AND REPAIRED IAW SRM. 2L73 4F4 F A22WE E23EA 20050826000112005082600011CE 2005 8 26 DXTA200500915 120050822A2750MP50G4 PDU CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL TE FLAPS INOPERATIVE E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07906QS 7500206 FLAPS FAIL IN FLIGHT, SLATS EXTENDED / FLAPS AT ZERO. ATTEMPTED RESET TO NO AVAIL, DIVERTED. TROUBLESHOT FLAPS WITH TEAM X. TO PDU. REMOVED AND REPLACED PDU WITH OVERHAULED PDU ASSY. RIGGED FLAPS, GOOD. OPS CHECK FLAPS GOOD IAW MM. 2L72 4J4 FRTT00007WITE6CH 20050826000122005082600012CE 2005 8 26 DXTA200500912 120050818A3260 TARGET CESSNA650 650 2076802CE GARRTTTFE731TFE7314R 01518WP MLG UPLOCK OUT OF ADJUST E DXTAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL07797QS 6507097 LANDING GEAR UNLOCK ANNUNCIATOR REMAINED ILLUMINATED AFTER GEAR RETRACTION. VERIFIED SQUAWK, DETERMINED LDG GEAR UPLOCK SWITCH TARGET ON RT MAIN WAS OUT OF ADJUSTMENT. ADJUSTED TARGET TO CONTACT SWITCH. OPERATIONAL CHECK OF GEAR WAS COMPLETED SATSFACTORY. PERFORMED IAW MODEL MM. 2L72 4F4 F A9NM E6WE 20050826000192005082600019WP 2005 8 26 05FDEA02615 120050824A5712 RIB DOUG DC10 DC1010 3022110WP GE CF6 CF66K 30020NE ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 RT WING FIXED LEADING EDGE AT STA XORS702 FOUND NR 1 RIB CRACKED. ACCOMPLISH FORMER REPAIR IAW SRM AND REPAIR ANGLE. 2L73 4F4 F A22WE E23EA 20050826000252005082600025NM 2005 8 26 05FDEA02601 120050823A5311 FRAME BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE BS 620 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 N01449, WHILE WORKING EA 7-5330-72293B PT 2, FOUND DOUBLE HOLE IN FRAME AT 620 LBL 21 WL 302. REPAIRED DOUBLE HOLE IN FRAME, BS 620, LBL 21 PER FED-EX EA 7-5330-92327. 2L73 4F4 FRTA3WE E2EA 20050826000402005082600040WP 2005 8 26 05FDEA02625 120050824A5712 RIB DOUG DC10 DC1010 3022110WP GE CF6 CF66K 30020NE ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 RT WING FIXED LEADING EDGE AT XORS 402 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM AND INSTALLED ANGLE REPAIR. 2L73 4F4 F A22WE E23EA 20050826000462005082600046NM 2005 8 26 SWAA052558 120050824A32301030875 SOLENOID BOEING737 7373G7 1384595NM MLG FAULTY A SWAAO OTHER J WARNING INDICATION LDLANDING 1 SW29671SW 23785 DECLARED EMERGENCY. MLG HANDLE WOULD NOT LOCK DOWN DURING MLG EXTENSION, 3 RED AND 3 GREEN LANDING GEAR POSITION LIGHTS ILLUMINATED. REMOVED AND REPLACED MLG LEVER HANDLE SOLENOID PER MM. 2L72 4F RTA16WE 20050826000482005082600048NM 2005 8 26 SWAA052540 120050823A2560P2070001 FLASHLIGHT BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 AFT OUTBOARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2L72 4F RTA16WE 20050826000512005082600051 2005 8 26 SWAA052543 420050822A256569457352 BRACKET BOEING737 7373L9 1384470NM R2 DOOR SLIDE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD ATTACH BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER MM. 2L72 4F RTA16WE 20050826000602005082600060NM 2005 8 26 SWAA052552 120050824A3350101073 LENS BOEING737 7377H4 1384404NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29449WN 32469 R2 DOOR EMERGENCY EXIT SIGN LENS CRACKED. REMOVED AND REPLACED LENS PER MM. 2L72 4F RTA16WE 20050826000612005082600061NM 2005 8 26 SWAA052553 120050824A53306545774 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29527SW 26569 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 747 TO BS 767, STR 18L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050826000622005082600062NM 2005 8 26 SWAA052554 120050823A5753 SKIN BOEING737 7373H4 1384600NM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29602SW 1047 27953 DURING SCHEDULED C4 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2L72 4F RTA16WE 20050826000662005082600066EU 2005 8 26 05FDEA02598 120050823A3610 DUCT AIRBUS310 A310203 3930313EU BLEED AIR SYS LEAKING A FDEAA UNSCHED LANDING SJ AFFECT SYSTEMS WARNING INDICATION CLCLIMB 1 SO25401FE 191 PASSING FL 330 GOT NR 2 BLEED LEAK LT IAW ECAMS SHUTOFF NR 2 BLEED VALVE. A/C WOULD NOT HOLD CABIN PRESS AT 310,280,OR EVEN 12,000 FT WITH NR 1 PACK. PACK BAY FOUND SENSOR LOOPS TOUCHING THE BLEED AIR SUPPLY DUCT GOING TO THE NR 2 ENG, ALSO FOUND SMALL LEAK AT THE SAME AREA, TIGHTENED BOLTS ON THE FLANGE AND REPOSITIONED LOOPS AND LEAK CHECKED FOUND OK RAN BOTH ENG'S PER 310 JRH. FOUND NO LEAK FAULTS. PERFORMED CABIN PRESS AND CONTROL CK PER MM 21-31-00-5-01. FOUND OK, FOUND WITH BOTH ENG RUNNING THAT THE PRESS WAS NORMAL 32-34 PSI ON EACH ENG, WITH SINGLE PACK OR BOTH PACKS. A/C OK FOR SERVICE. 2L72 4F RTA35EU 20050826000762005082600076WP 2005 8 26 05FDEA02631 120050824A5712 RIB DOUG DC10 DC1010 3022110WP LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LEFT WING FIXED LEADING EDGE AT XORS 452 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 4, 6 VOL I. 2L73 4F A22WE 20050826000812005082600081WP 2005 8 26 05FDEA02637 120050825A5712 RIB DOUG DC10 DC1010 3022110WP ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LT WING FIXED LEADING EDGE AT XORS 1011 FOUND NR 1 RIB CRACK. ACCOMPLISHED FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 5, 6 VOL I. 2L73 4F A22WE 20050826000822005082600082WP 2005 8 26 05FDEA02638 120050825A5712ARB129339 RIB DOUG DC10 DC1010 3022110WP ZONE 500 CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25556FE 46710 LT WING FIXED LEADING EDGE AT XORS 980 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 5, 6 VOL I. 2L73 4F A22WE 20050826000942005082600094WP 2005 8 26 05FDEA02644 120050825A5712 RIB DOUG DC10 DC1010 3022110WP LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LT WING FIXED LEADING EDGE AT XORS 749 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 3,4 VOL I AND INSTALLED ANGLE REPAIR. 2L73 4F A22WE 20050826000982005082600098WP 2005 8 26 05FDEA02648 120050825A5712 RIB DOUG DC10 DC1010 3022110WP LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LT WING FIXED LEADING EDGE AT XORS 677 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 3, 4 VOL I AND INSTALLED ANGLE REPAIR. 2L73 4F A22WE 20050826001012005082600101NM 2005 8 26 05FDEA02471 120050816A5311 FRAME BOEING727 727233 138408ANM STA 620 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 WHILE WORKING FED EX EA 7-5330-72293B PT 2 FOUND DOUBLE HOLE IN FRAME 620 LBL 7 AND LBL 8 W/L 298. FRAME REPLACED PER FED-EX EA 7-5330-92326. 2L73 4F RTA3WE 20050829000062005082900006NM 2005 8 29 EIA2005137 120050712A5340 FITTING BOEING747 747230B 1384889NM BS 990 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09487EV 23286 CRACKED STR 38L AT BS 990 UNDER BATHTUB FITTING. REMOVED DAMAGE, NDT AREA, FABBED AND INSTALLED PARTS PER SRM B747 53-10-03 FIG 1, 51-10-02 AND SOPM 20-41-02. 2L74 4F A20WE 20050829000172005082900017NM 2005 8 29 QXEA200501188 120050822A2120 ODOR BOMBDRDHC8 DHC8402 1390042NM CABIN DETECTED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM09412QX 4059 SEA FLT NR 2309: SLIGHT WHIFF OF BURNING ODOR IN COCKPIT/FORWARD CABIN AREA. SMELLED LIKE BURNING RUBBER. MAINTENANCE INSPECTED THE NOSE GEAR FOR BURNING RUBBER ODOR . NO ODOR NOTED. NOTICED RUBBER ODOR IN COCKPIT AND CABIN WHEN AIRCRAFT LANDED ON RUNWAY. CREW CONFIRMED THAT IT WAS THE ODOR THEY NOTICED. NO OTHER DEFECTS NOTED. NO PARTS WERE REPLACED. MAINTENANCE STATED THAT THE AIRCRAFT WAS OK FOR CONTINUED SERVICE. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050829000182005082900018EU 2005 8 29 YENA200552 120050820A3350321431 BATTERY AIRBUS320 A320232 3930326EU EMERGENCY EXIT DISCHARGED A YENAK NONE O OTHER ININSP/MAINT 1 EA15571JB7885 2125 EMERGENCY EXIT LIGHT FOR OVERWING EXITS RT INOP. REPLACED EMERGENCY LIGHT BATTERY OVERWING RT SIDE. 2L72 4F RTA28NM 20050829000262005082900026SO 2005 8 29 C2XA05CL063 120050813A3350110049 POWER SUPPLY EMB 145 EMB145LR 3260212SO CABIN FAULTY A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712563 145612 DURING ROUTINE MAINTENANCE, THE NR 1 EMERGENCY BATTERY CHARGER WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 EMERGENCY BATTERY POWER SUPPLY. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20050829000512005082900051NM 2005 8 29 EIA2005149 120050803A3350 LIGHT BOEING747 747212B 1384886NM CABIN INOPERATIVE A EIAAK NONE L NO TEST ININSP/MAINT 1 NM09486EV 20888 UPPER DECK EXIT DOOR EMERGENCY FLOOD LIGHT INOP. REPLACED UPPER DECK DOOR EMERGENCY EXIT SIGN ASSY, SYSTEM OPS CHECK NORMAL IAW MM 33-51-00. 2L74 4F A20WE 20050829000532005082900053 2005 8 29 EIA2005151 420050818A2565 SLIDE BOEING747 747230B 1384889NM CABIN UNSECURE A EIAAK NONE O OTHER ININSP/MAINT 1 NM09487EV 23286 UPPER DECK ESCAPE SLIDE NEEDS TO BE REPACKED. SLIDE REMOVED IAW EO 25-747-1780-05 REV B. 2L74 4F A20WE 20050829000552005082900055NM 2005 8 29 05FDEA02543 120050818A3010 PRESSURE SWITCH BOEING727 727233 138408ANM ANTI ICE SYSTEM FAILED A FDEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO25303FE 46802 EN ROUTE AT FL 350, IN AND OUT OF POSSIBLE ICING CONDITIONS, WHEN INITIATING WING A/I ON, RECEIVED AIR SYS 3 OFF (LEVEL 1) ANNUNCIATED, WITH NR 3 BLEED (AMBER) AND NR 3 MANF (RED) LIGHTS ILLUMINATED. QRH PROCEDURES FOLLOWED. DIVERTED INTO TO KDEN. RED MANF LIGHT EXTINGUISHED APPROX 10 MIN FROM LANDING MEL: RELEASED FOR SERVICE PER MEL/CDL: 30-11-01 CATEGORY: C EXPIRATION: 27AUG05 WING A/I SHUTOFF VALVES, INOP. DO NOT OPERATE A/C IN ICING." PERFORMED LEAK DECAY CHECK FOR NR 3 MANIFOLD OK. CHECKED MANIFOLD FAIL DETECTOR UNIT FOR FAULTS. REPLACED NR 3 MAN FAIL DETECTOR PRESS SWITCH AND TESTED OK TO CONTINUE. 2L73 4F RTA3WE 20050829000602005082900060EA 2005 8 29 VTZA200500148 120050821A3397 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT OUT OF ADJUST A VTZAO OTHER L NO TEST ININSP/MAINT 1 EA27643BR 7363 FWD CABIN FLOOR LIGHTING INOP. ADJUSTED CONTACTS ON LIGHT STRIP. 2L72 4F RTA21EA 20050829000672005082900067NM 2005 8 29 05FDEA02579 120050819A5343 FITTING DOUG MD11 MD11 3023602NM ZONE 700 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 EVIDENCE OF MINOR SURFACE CORROSION FOUND ON CENTER LANDING GEAR LEFT TRUNNION FITTING LOWER MATING SURFACE AREA. CORROSION MACHINED OFF AND FOUND WITHIN LIMIT AS PER SRM 53-40-00. 2L73 4F RTA22WE 20050829000712005082900071EU 2005 8 29 SF20050820 120050820A7712 INDICATOR SAAB SF340 SF340A 7850100EU RT TORQUE FAILED A UHLAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL17121CQ 121 FLIGHT 7558 IAD-ABE, AFTER ARMING CONSTANT TORQUE ON TAKEOFF, RIGHT ENGINE TORQUE INDICATED 20 PERCENT LOWER THEN SELECTED. AIRCRAFT REJECTED TAKEOFF AND RETURNED TO BLOCK. FOUND RIGHT TORQUE INDICATOR TO BE AT FAULT. R/R INDICATOR, OPS CHECK GOOD. 2L72 4T RTA52EU 20050829000892005082900089EU 2005 8 29 YENA200553 120050821A212120092455101 COOLING FAN AIRBUS320 A320232 3930326EU E/E BAY FAILED A YENAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA15558JB10802 1915 DURING TAXI, AFT RACK CARGO SMOKE INDICATION. RETURNED TO GATE. GROUND INSPECTION DETERMINED AFT RACK COOLING FAN FAILED. THE ITEM WAS PLACED ON MEL 25-22-03 D AND LATER THE FAN WAS REPLACED PER LTV MM 23-39-00. 2L72 4F RTA28NM 20050829000902005082900090EU 2005 8 29 MALA050669 120050819A2150 ACM SAAB SF340 340B 7860101EU ODOR A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL15441XJ 340B441 UNABLE TO COOL CABIN AND FLIGHT DECK WITH A SULFUR TYPE SMELL FROM AC SYSTEM. AIR RETURN TO DTW. REMOVED AND REPLACED RT ACM AND PERFORMED OPS CHECKS OF BOTH RT AND LT ACM. ALL CHECKS GOOD. 2L72 4T RTA52EU 20050829000942005082900094EU 2005 8 29 MALA050668 120050808A5712 RIB SAAB SF340 340B 7860101EU WING CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15369PX 340B295 LE 6UBR HAS CRACKED RIBS THAT HAVE BEEN REPAIRED IAW MESABA EO NR S57066 AND SRM 57-10-30 REF: EAMS WORK ORDER 212724 TASK 6504. 2L72 4T RTA52EU 20050829000962005082900096EU 2005 8 29 MALA050673 120050825A29104204002 PTU BAC 146 AVRO146RJ85A1500097EU HYD SYSTEM MALFUNCTIONED A MALAO OTHER M OVER TEMP NRNOT REPORTED 1 GL15532XJ E2366 GREEN HIGH TEMP HIGH. REMOVED AND REPLACED PTU PN 4204002, SN OFF LM54 ON BX63. REMOVED AND REPLACED NR 3 EDP PN 521499 SN ON 60010412 OFF F991164 AND GREEN ISO VALVE PN HTE9531-3 SN ON 290VB151, OFF FR020BA IAW AMM 29-10-17-201, 29-10-14. RAN FOR 45 MINUTES. OPS CHECK GOOD. 2H74 4F RTA49EU 20050829000972005082900097EA 2005 8 29 COMA0570099 120050819A5610NP1393226 WINDOW CNDAIRCL600 CL6002C10 1390015EA COCKPIT CRACKED A COMAO OTHER O OTHER NRNOT REPORTED 1 SO01354CA7756 10064 FLIGHT 5186 - COPILOT SIDE WINDOW SHATTERED. REPLACED WINDOW. 2L72 4F RTA21EA 20050829001082005082900108NM 2005 8 29 SWAA052569 120050824A335015AT48 SWITCH BOEING737 7375H4 138449DNM EMERGENCY LIGHT INTERMITTENT A SWAAK NONE O OTHER ININSP/MAINT 1 SW29512SW 24189 DURING SCHEDULED SERVICE CHECK, FOUND COCKPIT EMERGENCY EXIT LIGHTS INTERMITTANT. REMOVED AND REPLACED COCKPIT LIGHT SWITCH PER MM. 2L72 4F RTA16WE 20050829001142005082900114NM 2005 8 29 CALA0500282 120050825A531565C339503 FLOORBEAM BOEING737 737524 1384721NM STA 986.5 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2746625 27529 INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, RBL 9 TO RBL 45. REPAIRED IAW ECRA 5321-01273. 2L72 4F RTA16WE 20050829001162005082900116NM 2005 8 29 05FDEA02665 120050826A5320 INTERCOSTAL DOUG MD11 MD11 3023602NM BS 1741 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 AFT CABIN INTERCOSTAL AT STA 1741 RT LONGERON 7 FOUND CRACK. REMOVED AND FABRICATED AS PER DRAWING AFA 7761. INSTALLED AS PER SRM 51-35-01 VOL.II. CLASSIFIED MINOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050829001192005082900119NE 2005 8 29 COMA0560457 220050821A72616087T04P05 SCAVENGE PUMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE LT ENGINE MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01940CA13571 7048 FLIGHT 5630 - LEFT ENGINE OIL PRESSURE FLUCTUATING. REPLACED THE SCAVENGE LUBE PUMP. 2L72 4F4 FRTA21EA E15NE 20050829001222005082900122NM 2005 8 29 05FDEA02664 120050826A5320 INTERCOSTAL DOUG MD11 MD11 3023602NM BS 1701 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 AFT CABIN INTERCOSTAL AT STA 1701 RT LONGERON 7 FOUND CRACK. REMOVED AND FABRICATED AS PER DRAWING AFA 7761. INSTALLED AS PER SRM 51-35-01 VOL.II. CLASSIFIED MINOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050829001242005082900124NM 2005 8 29 05FDEA02661 120050825A57406521658Y29 BRACKET BOEING727 727100 1384036NM LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25136FE 19855 COVE PANEL BRACKET IS BROKEN ON LOWER WING PANEL BELOW NR 3 SPOILER. REMOVED AND REPLACED 3 EA BRACKET P/N 65-21658Y29, 65-21658-27, AND 65-21658Y30, AND 1 EA ROD P/N 69-17911-18 IAW SRM 51-30-2. 2L73 4F RTA3WE 20050829001252005082900125NM 2005 8 29 05FDEA02491 120050816A5347A5A70821 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 MAIN DECK SEAT TRACK AT STATION Y5-02 TO 5-20, -X8.5 FOUND CORRODED. MAIN DECK SEAT TRACK AT STATION Y5-00 TO STATION Y5-123, -X8.5 REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE I VOLUME I. CLASSIFIED REPAIR AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050829001262005082900126EA 2005 8 29 COMA0560460 120050822A3210 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA LANDING GEAR ILLUMINATED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01986CA 7174 FLIGHT 5414 - GEAR DISAGREE WARNING. OPERATIONAL CHECK OF LANDING GEAR WAS SATISFACTORY. 2L72 4F RTA21EA 20050829001282005082900128NM 2005 8 29 05FDEA02490 120050816A5347ADA83901 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 CABIN SEAT TRACK AT STATION Y1064, -X8.5 FOUND CORRODED. MAIN DECK SEAT TRACK AT STATION Y1009 TO STATION Y1129, -X8.5 REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE I VOLUME I. CLASSIFIED REPAIR AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050829001292005082900129EA 2005 8 29 COMA0560455 120050819A5610NP1393226 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A COMAO OTHER O OTHER CRCRUISE 1 SO01819CA13856 7415 FLIGHT 5166 - COPILOT SIDE WINDOW CRACKED. REPLACED WINDOW. 2L72 4F RTA21EA 20050829001302005082900130NM 2005 8 29 05FDEA02662 120050826A5347 SEAT TRACK DOUG MD11 MD11 3023602NM BS 1349.5-1353.5CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 AFT CABIN SEAT TRACK CROWN AT STA 1349.5 TO 1353.5 RBL 107 FOUND CORROSION. CORRECTIVE ACTION: SNRM N0807: DISCREPANT SEAT TRACK CARRY OUT REPAIR AS PER SRM 53-70-00 FIG.1 VOL.I. CLASSIFIED MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050829001312005082900131NM 2005 8 29 USAA051047 120050823A5330 SKIN BOEING737 737401 1384701NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19420US 23987 FUSELAGE SKIN 2 INCHES AFT OF BS 727D AT S-23R DAMAGED. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER IAW SRM 53-00-01, DEFECT SIZE 3 INCHES. 2L72 4F RTA16WE 20050829001332005082900133NM 2005 8 29 USAA051041 120050823A5530 BUSHING BOEING737 737301 1384611NM VERTICAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US 23933 VERTICAL FIN AFT JUGS RT BUSINGS AFT FACES CORRODED. REMOVED CORROSION, FABRICATED AND INSTALLED BUSHINGS IAW BOEING DWG 69-72039, 65-55274, DEFECT SIZE: 1 X 2 INCH TYPICAL. 2L72 4F RTA16WE 20050829001382005082900138WP 2005 8 29 MWEA050089 120050823A5320991007842 FLOOR SUPPORT DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE STA 218 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 RT SIDE, MOST OB FLOORBOARD ATTACH STRIP HAS HOLE CORRODED, STATION 218. FABRICATED AND INSTALLED FLOOR SUPPORT. 2L72 4F4 F A6WE E9NE 20050829001392005082900139SO 2005 8 29 CHQA200500146 120050823A3260 PROXIMITY SENSOR EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL MLG UNSECURE A CHQAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL11382SK 145624 ON DEPARTURE, LANDING GEAR WAS SELECTED UP. THE LT MAIN DID NOT INDICATE UP AND LOCKED. AN EICAS MESSAGE L/G LEVER DISAGREE APPEARED. GEAR WAS CYCLED IAW THE QRH. RETURNED TO FIELD. DID NOT DECLARE AND EMERGENCY, HOWEVER AN EMERGENCY WAS DECLARED ON OUR BEHALF BY THE TOWER. LANDING GEAR INDICATED DOWN AND LOCKED UPON RETURN. INSPECTED GEAR AND FOUND FORWARD PROXIMITY BACKSHELL UNSECURED. RE-SECURED BACKSHELL. PERFORMED SEVERAL GEAR SWINGS. ALL OPS CHECKED GOOD. 2L72 4F4 FRTT00011ATTE6CH 20050829001402005082900140EU 2005 8 29 XN0A1259 120050819A2720 CONTROL SYSTEM AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE ELEVATOR MALFUNCTIONED A XN0AA UNSCHED LANDING O OTHER CLCLIMB 1 GL23371PC 157 DURING TAKEOFF, FLARE ROLL ELEVATOR CONTROL WAS VERY DIFFICULT TO MANEUVER THE AIRCRAFT. CARRIED OUT INSPECTION PER A300 FIM CHAPTER 27-31-00 FIGURE 101 SHEET NR 1 & 2 NO FAULTS FOUND. CARRIED OUT INSPECTION PER A300 AMM CHAPTER 27-33-14 & 27-33-00 OF THE ARTIFICIAL FEEL UNIT, NO DEFECTS NOTED. CARRIED OUT INSPECTION PER A300 AMM 27-33-00 PAGE 513 & 514 AND FOUND TO BE WITHIN LIMITS. VISULLY INSPECTED THS SYSTEM, ELEVATOR CONTROL SYSTEM CABLES, QUADRANTS, PULLEYS, AND FOUND NO DEFECTS. GROUND OPERATIONAL CHECK NORMAL. (STATUS:SUPP/CLOSED) 2L72 4F4 FRTA35EU E23EA 20050829001412005082900141EA 2005 8 29 COMA0560453 120050819A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01937CA2765 62 7044 FLIGHT 5144 - FLAPS FAIL CAUTION. REPLACED THE LT BPSU. 2L72 4F RTA21EA 20050829001432005082900143NM 2005 8 29 BB05071 120050823A335020131A BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19628AU 27806 CLT - BATTERY FOR THE AFT EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE BATTERY FOR THE AFT EMERGENCY LIGHT. SYSTEM CHECKS OK. 2L72 4F RTA2NM 20050829001442005082900144NM 2005 8 29 BB05072 120050823A335020121 CHARGER BOEING757 7572B7 1384964NM EMERGENCY LIGHT FAULTY A USAAK NONE O OTHER ININSP/MAINT 1 EA19628AU 27806 CLT - THE AFT DOORS EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER. SYSTEM CHECKS OK. 2L72 4F RTA2NM 20050829001462005082900146 2005 8 29 BB05068 420050817A2565 GIRT BAR BOEING757 7572B7 1384964NM CABIN DISLODGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19625VJ 27246 CLT - MAINTENANCE FOUND THE L-4 DOOR SLIDE GIRT BAR PARTIALLY DISLODGED. MAINTENANCE REMOVED THE GIRT BAR, LUBED, AND THEN INSTALLED THE SAME GIRT BAR. OPERATIONALLY CHECKS OK. 2L72 4F RTA2NM 20050829001472005082900147WP 2005 8 29 ARWA20050803 120050817A3220510361 LINK ASSY DOUG DC8 DC863F 302198FWP PWA JT3D JT3D* 52039NE NLG VIBRATION A ARWAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO19441J 45988 AFTER TAKEOFF AND GEAR RETRACTION, EXPERIENCED CONTINUOUS VIBRATION AND NOISE FROM NOSE WHEEL WELL AREA. RETURNED AND LANDED TO INVESTIGATE. REMOVED AND REPLACED RT NOSE DOOR LINK ASSEMBLY IAW MM. PERFORMED ADJUSTMENT TEST SYSTEM IAW M/M. TEST GOOD. 2L74 4F4 F 4A25 1E8 20050829001482005082900148GL 2005 8 29 LR7A05107 220050818A7200 ENGINE LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL NR 4 FLAMED OUT A LR7AE ENGINE SHUTDOWN XJ ENGINE FLAMEOUT WARNING INDICATION APAPPROACH 1 AL03404LC 51 4763 FLIGHT CREW REPORTED DURING APPROACH, NR 4 ENGINE FLAMED OUT ON SHORT FINAL AFTER WAKE TURBULENCE ENCOUNTER. ENGINE WAS AT FLIGHT IDLE. DURING MAINTENANCE EVALUATION GROUND RUN NR 4 RRM AT 105 PERCENT AT FLIGHT IDLE. REPLACED PROPELLER ASSY IAW HN6101 AND 61135. OPS CHECK NORMAL IAW HN7101. 2H74 4T4 T A1SO E282 20050829001502005082900150SO 2005 8 29 RAIA00508024 120050816A3260852701 PROXIMITY SENSOR EMB 145 EMB145ER 3260211SO ALLSN AE300 AE3007A GL MLG INOPERATIVE A RAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03808HK 145157 LANDING GEAR AIR GROUND FAIL MESSAGE DURING FLIGHT. MAINTENANCE REMOVED AND REPLACED THE RT NR 1 WOW PROXIMITY SWITCH. 2L72 4F4 FRTT00011ATTE6CH 20050829001512005082900151NM 2005 8 29 AALA20050551 120050821A3350D71702001 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21756AM 30264 DFW - SEAT EMERGENCY ESCAPE PATH LIGHTS IN D-ZONE IN COACH INOPERATIVE. REPLACED BATTERY PACK FOR SEAT EMERGENCY ESCAPE PATH LIGHTS AT D-ZONE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20050829001522005082900152NM 2005 8 29 AALA20050554 120050817A3350D71702011 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21921AN 29522 TUL - BATTERY PACK FOR EMERGENCY LIGHTING IN CABIN INOPERATIVE. REPLACED BATTERY PACK 8130 FOR EMERGENCY LIGHT IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20050829001552005082900155WP 2005 8 29 AALA20050553 120050823A3350 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHTSBROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW21429AA 49341 ORD - EMERGENCY ARROW LIGHT ALONG WALLBOARD BY FORWARD GALLEY INOPERATIVE. REPAIRED BROKEN WIRE FOR EMERGENCY ARROW LIGHT ALONG WALLBOARD BY FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050829001562005082900156WP 2005 8 29 AALA20050549 120050815A49905940405503 APU DOUG DC9 DC982 3022082WP LEAKING A AALAA UNSCHED LANDING KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21555AN 53085 JFK - INFLIGHT LGA TO DFW, AFTER TAKE OFF STRONG BURNING FLUID SMELL WAS NOTED IN COCKPIT. F/A REPORTED SMOKE IN CABIN. AIR INTERRUPTED TO JFK AND LANDED WITHOUT INCIDENT. FOUND INTERNAL AND EXTERNAL OIL LEAK ON AUXILLARY POWER UNIT. REPLACED APU. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050829001572005082900157NM 2005 8 29 AALA20050550 120050823A3350 LIGHT BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21616AA 24524 MIA - EMERGENCY LIGHT AT SEAT 18D BROKEN. REPLACED EMERGENCY LIGHT ASSEMBLY FOR SEAT 18D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050829001582005082900158EA 2005 8 29 SWIA200515459 120050824A2797 WIRE CNDAIRCL600 CL6002B19 1900309EA RUDDER BROKEN A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07963SW 7865 DURING RUDDER TRIM TEST, RUDDER TRIM STICKS NL. REPAIRED WIRE ON RUDDER TRIM SWITCH, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050829001662005082900166NM 2005 8 29 SB05095 120050818A3350 LIGHT BOEING737 7373B7 1384580NM PASSENGER CABIN BROKEN A USAAK NONE O OTHER ININSP/MAINT 1 EA19531AU 24478 CLT - THE AISLE EMERGENCY EXIT LIGHT WAS FOUND BROKEN. MAINTENANCE REPLACED THE EMERGENCY EXIT IDENTIFIER AND A FUSE IN THE BATTERY PACK. OPERATIONALLY CHECKS OK. 2L72 4F RTA16WE 20050829001672005082900167NM 2005 8 29 RYNA200500026 120050817A53300000 SKIN BOEING737 737201 1384454NM BS 727B+18 CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07242US 22444 DURING WALKAROUND AFTER FLIGHT A SKIN CRACK AT BS 727B+18" AND JUST ABOVE STRINGER 16L WAS NOTICED. AIRCRAFT FERRIED TO FLIGHTSTAR FOR REPAIR. COMPLIED WITH FUSELAGE SKIN REPAIR AT BS 727B+18" AT STRINGER 16L PER SRM 53-30-3 FIG DETAIL VII. 2L72 4F A16WE 20050829001682005082900168NM 2005 8 29 USAA051043 120050823A5530 BUSHING BOEING737 737301 1384611NM VERTICAL FIN CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US 23933 VERTICAL FIN LT MOUNT LUGS, AFT FACE CORRODED. REMOVED CORROSION, FABRICATED & INSTALLED BUSHINGS IAW BOEING DWGS 69-72039 & 65-52274 DEFECT SIZE: 1 X 2 INCH AREA. 2L72 4F RTA16WE 20050829001692005082900169NM 2005 8 29 USAA051034 120050823A5314 KEELBEAM BOEING737 737301 1384611NM BS 664-727 WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US 23933 KEEL BEAM LEFT OUTBOARD FLANGE STA 664 TO 727 DAMAGED. REMOVED DAMAGE, FAB & INSTALLED FILLER PLUGS, REPAIR STRAP AND APPROP SHIMS INCLUDED IAW EA 96777, DEFECT SIZE: 60 INCHES OF SURFACE WEAR AT FAIRING ATTACH HOLES AND STRAP. 2L72 4F RTA16WE 20050829001702005082900170NM 2005 8 29 USAA051035 120050823A5347 SEAT TRACK BOEING737 737301 1384611NM BS 658 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US662 23933 SEAT TRACK VERTICAL LEG HAS 0250 INCH CRACK AT CUTOUTS FOR FASTENERS. STOP DRILL CRACKS, INSTALL REPAIR ANGLES IAW EA 96799, DEFECT SIZE: 0250 INCH, CRACKED AT CUTOUTS FOR FASTENERS. 2L72 4F RTA16WE 20050829001712005082900171NM 2005 8 29 USAA051036 120050823A5347 SEAT TRACK BOEING737 737301 1384611NM BS 662-670, RBL2CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US 23933 BS 662-670, RBL 24 CRACKED. STOP DRILLED CRACKS, INSTALLED REPAIR DOUBLER/CHANNELS IAW EA 96799, DEFECT SIZE: .250 X 2 INCH. 2L72 4F RTA16WE 20050829001732005082900173NM 2005 8 29 USAA051038 120050823A5720 STRUCTURE BOEING737 7374B7 1384702NM WING FUEL CELL CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19449US 24893 INTERNAL FUEL TANK AT BOTTOM SKIN AT WBL 13550 CRACKED. FABRICATED NEW T-SECTION & INSTALLED REPAIR T-SECTION IAW EA 96796, DEFECT SIZE: 2.250 INCH. 2L72 4F RTA16WE 20050829001742005082900174NM 2005 8 29 USAA051039 120050823A5340 ANGLE BOEING737 737301 1384611NM LT PACK BAY CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US 23933 LEFT PACK BAY, AFT RIGHT CORNER CRACKED. FABRICATED ATTACH ANGLE SRM 51-10-02 BOEING DWG 66-24798, DEFECT SIZE: 1 INCH. 2L72 4F RTA16WE 20050829001752005082900175NM 2005 8 29 USAA051040 120050823A5530 BUSHING BOEING737 737301 1384611NM VERTICAL FIN CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US 23933 VERTICAL FIN AFT ATTACH LUGS RT SIDE FWD FACES. REMOVED CORROSION MACHINED & INSTALLED BUSHINGS IAW BOEING DWG 69-72039, 65-52274 DEFECT SIZE: 1 X 2 INCHES TYPICAL. 2L72 4F RTA16WE 20050829001762005082900176NM 2005 8 29 USAA051033 120050823A5320 WEB BOEING737 737301 1384611NM STA 699 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US 23933 STA 699 INSIDE KEEL BEAM STRUT LOWER RT CORNER OF LIGHTENING HOLE IN BULKHEAD. REMOVED DAMAGE, INSTALLED DOUBLER IAW EA 69760 DEFECT SIZE: LOWER RT CORNER OF LIGHTENING HOLE CRACKED .500 INCH. 2L72 4F RTA16WE 20050829001782005082900178SO 2005 8 29 CHQA200500147 120050824A335078241 INVERTER EMB 145 EMB145 3260210SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE O OTHER ININSP/MAINT 1 GL11265SK 145226 THE TWO AFT EMERGENCY FLOOR PROXIMITY STRIPS ARE INOPERATIVE. REMOVED AND REPLACED NR 6 INVERTER IAW EMB 145 MM 33-50-11. 2L72 4F RTT00011AT 20050829001812005082900181SO 2005 8 29 MASA200500543 120050713A3350375924 LAMP EMB 145 EMB145LR 3260212SO ROW 12 INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07851MJ 145572 DURING RON, THE CREW FOUND 12 FWD CEILING PANEL EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT. 2L72 4T RTT00011AT 20050829001822005082900182EA 2005 8 29 MASA200500563 120050718A3397E520005705A CIRCUIT BOARD CNDAIRCL600 CL6002D24 1390016EA EMERGENCY LIGHT FAILED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07921FJ3334 15021 ASH 6213 PHX. EMERGENCY LIGHT SYSTEM TO BE CYCLING ON AND OFF WHEN IN THE ARMED POSITION. MX REMOVED AND REPLACED THE NR 5 PRINTED CIRCUIT CARD AT J11 AND THE SYSTEM FUNCTIONED NORMALLY. 2L72 4F RTA21EA 20050829001842005082900184SO 2005 8 29 MASA200500568 120050719A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07853MJ 145464 DURING THE WALK AROUND IT WAS DISCOVERED THE LEFT FWD EXTERIOR EMERGENCY LIGHT NOT ILLUMINATING. REPLACED THE LIGHT BULB AFTER TROUBLESHOOTING. OPERATIONAL CHECK GOOD. 2L72 4T RTT00011AT 20050829001852005082900185EA 2005 8 29 MASA200500601 120050729A33508GH00247308 LIGHT CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07503MJ 10058 RIGHT OVERWING EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT (P/N: 8GH002473-08). 2L72 4F RTA21EA 20050829001872005082900187SO 2005 8 29 MASA200500608 120050731A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07836MJ 145359 ASH 2722 CLT. FORWARD 2 FLOOR PROXIMITY EMERGENCY EXIT LIGHT STRIPS INOP. MX COULD NOT DUPLICATE THE DISCREPANCY AND IT OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050829001902005082900190SO 2005 8 29 MASA200500635 120050812A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07831MJ 145273 ASH 2805 CLT. CREW REPORTED EMERGENCY EXIT LIGHT BEING INOP. MX RESET THE SYSTEM. 2L72 4T RTT00011AT 20050829001912005082900191SO 2005 8 29 MASA200500641 120050814A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07840MJ 145429 ASH 2749 CLT. EMERGENCY EXIT CEILING LIGHT ROW 12 INOP. MAINTENANCE OPS CHECKED SYSTEM NORMAL. AIRCRAFT DEPARTED WITH NO FURTHER PROBLEMS. 2L72 4T RTT00011AT 20050829001922005082900192NM 2005 8 29 CALA0500280 120050823A5320141A57703 SUPPORT BOEING737 737824 13844BZNM STA 328 +12 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712216 28776 INSPECTION FOUND O/B SEAT TRACK SUPPORT CORRODED AT FORWARD END AT BS 328 + 12 (CLOSET SUPPORT TRACK). THE SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND 53-10-51. 2L72 4F RTA16WE 20050829001932005082900193NM 2005 8 29 CALA0500281 120050822A32106546113 TRUNNION PIN BOEING737 737524 1384721NM LT MLG FRACTURED A CALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2717640 28901 THE LT MLG UNSAFE LIGHT ILLUMINATED AFTER TAKEOFF FROM IAH. THE CREW VERIFIED THAT THE LT MLG HAD NOT RETRACTED. THE CREW PLACED THE GEAR HANDLE IN THE EXTENDED POSITION AND GOT THREE GREEN LIGHTS. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT MLG TRUNNION PIN BROKEN IN TWO AND CORRODED. THE LT MLG TRUNNION PIN WAS REMOVED AND REPLACED. AN FCD WILL BE ISSUED TO INSPECT THE FLEET LG TRUNNION PINS. 2L72 4F RTA16WE 20050829001942005082900194SW 2005 8 29 PNSA050802 120050821A5270 SWITCH SWRNGNSA227 SA227AC 8780603SW PAX DOOR OUT OF ADJUST A PNSAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 AL032719H AC713B DURING CLIMBOUT FROM ANC THE CABIN DOOR LIGHT ILLUMINATED. A/C RETURNED TO ANC AND MX ADJUSTED THE NR 7 BAYONET SWITCH. A/C WAS RELEASED FOR CHECK FLIGHT AND OPS CHECK NORMAL. 2L72 4T RTA8SW 20050829001962005082900196EA 2005 8 29 SWIA200515465 120050822A2120VP0615E00 SHUTOFF VALVE CNDAIRCL600 CL6002B19 1900309EA CABIN AIR MALFUNCTIONED A SWIAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM07431SW 7536 EN ROUTE TO MRY RECEIVED CARGO FAN FAIL AND CARGO SOV FAIL STATUS THEN CARGO SMOKE WARNING. REPLACED CARGO RECIRCULATED AIR SHUT OFF VALVE IAW AMM 21-55-07. REPLACED CARGO FAN AND EXHAUST SOV IAW 21-55-01. P/N VP0615E00, S/N 1888, P/N VP0615E00, S/N OFF J92345, P/N AE0607F00, S/N OFF L0250. 2L72 4F RTA21EA 20050829001972005082900197EA 2005 8 29 SWIA200515466 120050819A27505913164 DETECTOR CNDAIRCL600 CL6002C10 1390015EA FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07719SK1526 1526 10188 FLAPS HALFSPEED STATUS MESSAGE DURING TAXI. REPLACED RIGHT WING OUTBOARD FLAP SKEW DETECTOR FOR NR 1 SFCU IAW MM 27-52-45. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050829002002005082900200EA 2005 8 29 SWIA200515469 120050823A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA ROWS 2-5 LOOSE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07961SW 7857 EMERGENCY LIGHTS ROWS 2, 3, 4, 5 INOP. RECONNECTED STRIP. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050829002012005082900201NM 2005 8 29 SWAA052570 120050825A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29617SW 27700 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 663.75, STR 10R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050829002032005082900203NM 2005 8 29 SWAA052571 120050825A53106546801 CREASE BEAM BOEING737 7373H4 1384600NM BS 380-500B CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29617SW 27700 DURING SCHEDULED D-CHECK, FOUND RIGHT CREASE BEAM WEB CORRODED BETWEEN BS 380 TO BS 500B. REPAIRED CREASE BEAM PER SRM. 2L72 4F RTA16WE 20050829002082005082900208NM 2005 8 29 SWAA052576 120050825A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29369SW 26580 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 727E, RBL 8. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050829002102005082900210NM 2005 8 29 SWAA052578 120050822A53306545775 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29326SW 23690 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 767 TO BS 797, STR 18L TO STR 19L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050829002112005082900211NM 2005 8 29 SWAA052579 120050822A53306545774 SKIN BOEING737 7373H4 1384600NM BS 727D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29326SW 23690 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 19R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050829002122005082900212NM 2005 8 29 SWAA052580 120050822A53306550570 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29326SW 23690 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER BEAR STRAP CUTOUT. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050829002132005082900213NM 2005 8 29 0501326717 120050809A5330 SKIN BOEING747 747251F 1384898NM BS 2060-2080 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01617US 21121 DURING L-CHECK FOUND CRACK IN FUSELAGE SKIN BETWEEN BS 2060 - 2080 S31R-33R. REPAIRED PER EA 67-165234. 2L74 4F A20WE 20050829002142005082900214NM 2005 8 29 0501336717 120050818A5311 FRAME BOEING747 747251F 1384898NM BS 400 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01617US 21121 DURING L-CHECK FOUND CRACK IN FRAME AT BS 400 S23L. REPAIRED PER EA 67-165233. 2L74 4F A20WE 20050829002162005082900216CE 2005 8 29 1050617009 120050824A5311 FRAME BEECH 1900 1900D 1154162CE BS 588 CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07173YV UE173 CENTER CANTED FRAME AT FS 588. LEFT FLANGE CRACKED AT NUT PLATE AND RIVET, STRINGER 7L AND 8L. MORE INFORMATION WILL BE AVAILABLE AT A LATER DATE. 2L72 4T RTA24CE 20050830000012005083000001NM 2005 8 30 PIDA250021A 120050222A5340 SUPPORT ANGLE BOEING737 737228 13844AGNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05252TR 23001 CORROSION AROUND THE FORWARD LAVATORY DUMP VALVE, I/B SIDE. REPLACED CORRODED SUPPORT ANGLE PER BAC DWG 65-55757 AND SRM 51-10-2. 2L72 4F RTA16WE 20050830000052005083000005NM 2005 8 30 05FDEA02676 120050826A5310 SEAT TRACK DOUG MD11 MD11 3023602NM BS 1811-1880 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 AFT CABIN SEAT TRACK CORROSION FOUND ON CROWN, FLANGES AND BASE AT STA 1811 TO 1880 LBL 8.5. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-70-00 FIG.3 VOL.I. CARRIED OUT REPAIR ON DISCREPANT SEAT TRACK AS PER SRM 53-70-00 FIG.1 VOL.I. CLASSIFIED MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050830000062005083000006NM 2005 8 30 05FDEA02677 120050826A5347 SEAT TRACK DOUG MD11 MD11 3023602NM BS 1811-1880 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 AFT CABIN SEAT TRACK CORROSION ON FLANGES, CROWN AND BASE AT STA 1811 TO STA 1880 RBL 8.5 AT VARIOUS LOCATION. SEAT TRACK REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-70-00 FIG.3 VOL.I. CARRY OUT REPAIR ON DISCREPANT SEAT TRACK AS PER SRM 53-70-00 FIG.1 VOL.I. CLASSIFIED MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050830000072005083000007NM 2005 8 30 05FDEA02678 120050826A5347 SEAT TRACK DOUG MD11 MD11 3023602NM BS 1811-1880 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 AFT CABIN SEAT TRACK CORROSION ON FLANGES, CROWN AND BASE AT STA 1811 TO 1880 LBL 27.5. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-70-00 FIG 3 VOL I. CARRIED OUT REPAIR ON DISCREPANT SEAT TRACK AS PER SRM 53-70-00 FIG 1 VOL I. CLASSIFIED MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050830000082005083000008NM 2005 8 30 05FDEA02679 120050826A5347 SEAT TRACK DOUG MD11 MD11 3023602NM BS 1811-1880 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 AFT CABIN SEAT TRACK CORROSION ON FLANGE, CROWN AND BASE AT STA 1811 TO 1880 RBL 27.5. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-70-00 FIG 3 VOL I. CARRIED OUT REPAIR ON DISCREPANT SEAT TRACK AS PER SRM 53-70-00 FIG 1 VOL I. CLASSIFIED MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050830000092005083000009NM 2005 8 30 05FDEA02680 120050826A5347 SEAT TRACK DOUG MD11 MD11 3023602NM BS 1861-1887 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 AFT CABIN SEAT TRACK CORROSION AT CROWN, BASE AND FLANGES AT STA 1861 TO 1887 LBL 65.5. REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-70-00 FIG.3 VOL.I. CARRIED OUT REPAIR AS PER SRM 53-70-00 FIG.1 VOL.I ON DISCREPANT SEAT TRACK. CLASSIFIED MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050830000112005083000011EU 2005 8 30 USAA051060 120050826A5320D5311282720201 FLOOR SUPPORT AIRBUSA319 A319112 3930323EU FRAME 12 TO 16 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19724UW 1122 FRAME 12 TO 16 BETWEEN Y254 TO Y765. FLOOR SUPPORT SECTION REPLACED WITH IDENTICAL PART PER SRM 51-72-11, DEFECT SIZE: 1/2" BY 6" AREA. 2L72 4F RTA28NM 20050830000122005083000012EU 2005 8 30 USAA051059 120050826A5315D531127820201 FLOORBEAM AIRBUSA319 A319112 3930323EU FR 20 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19724UW 1122 RT FLOORBEAM OF FRAME 20 FLOORBEAM 1292. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-72-11, DEFECT SIZE: .5 X 10. 2L72 4F RTA28NM 20050830000132005083000013EU 2005 8 30 USAA051058 120050826A5315 FLOORBEAM AIRBUSA319 A319112 3930323EU FR 66 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19724UW 1122 FLOOR SUPPORT Y1732 AT FRAME 66. INSTALLED REPAIR DOUBLERS PER ASRM 53-41-14, DEFECT SIZE: 1 INCH DIA. 2L72 4F RTA28NM 20050830000142005083000014EU 2005 8 30 USAA051057 120050826A5320D5347209001100 FLOOR SUPPORT AIRBUSA319 A319112 3930323EU FR 64-68 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19724UW 1122 CORROSION AT NUT PLATE HOLES, FLOOR SUPPORT BEAM Y 1292 AT FRAME 64, 67, 68. REPLACED FLOOR SUPPORT BEAMS (3 EA) PER SRM 51-72-11, DEFECT SIZE: .5" DIA. 2L72 4F RTA28NM 20050830000152005083000015EU 2005 8 30 USAA051056 120050826A5347D57130147203 SEAT TRACK AIRBUSA319 A319112 3930323EU FR 40 GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19724UW 1122 RT OTBD SEAT TRACK AT FRAME 40. DEFECTIVE PART REPLACED WITH IDENT PART PER AIRBUS DWG JOD57130147, DEFECT SIZE: .250 X 1 INCH X .020" DEEP. 2L72 4F RTA28NM 20050830000162005083000016EU 2005 8 30 USAA051055 120050826A5753 SKIN AIRBUSA319 A319112 3930323EU TE FLAP DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19724UW 1122 RT O/B FLAP TRAILING EDGE, OUT FLAP SKIN. INSTALLED DOUBLER PER SRM 57-53-00 FIG 213 VERSION 3, DEFECT SIZE: 22" LENGTH OF DELAMINATION. 2L72 4F RTA28NM 20050830000172005083000017NE 2005 8 30 DXTA200500929 220050826A720030358005D ENGINE CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE RIGHT INOPERATIVE E DXTAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07326QS5202 5600526 PCEJCO551 DURING ENGINE START, THE RIGHT ENGINE HAD NORMAL START, LEFT ENGINE STARTED, ENGINE ACCELERATED THRU 52 PERCENT AND WOULD NOT SHUT OFF WITH THRUST LEVER IN CUT OFF. HAD TO SHUT ENGINE DOWN USING FIREWALL SHUTOFF. MAX N1 103.5%, N2 OVERSPEED, DID NOT NOTICE ACTUAL SPEED. ENGINE IS BEING REMOVED AND GOING TO SHOP FOR EVALUATION. 2L72 4F4 FRTA22CE E25EA 20050830000182005083000018CE 2005 8 30 DXTA200500927 120050825A3610S100420PG SENSOR CESSNA750 750 2076810CE PYLON MALFUNCTIONED E DXTAO OTHER J WARNING INDICATION DEDESCENT 1 GL07971QS5683 7500071 ON DESCENT, PYLON BLEED LEAK, ILLUMINATED EMERGENCY PROCEDURES COMPLETED, WARNING LIGHT EXTINGUISHED WHEN IDLE, BUT CAME BACK ON WHEN POWER WAS ADDED. REMOVED PANEL 412DB TO GAIN ACCESS TO SENSOR TT018 AND TT020 VISUALLY INSPECTED BOTH SENSORS, NO DEFECTS NOTED. INSPECTED ALL PNEUMATIC LINES IN PYLON AREA NO DEFECTS NOTED. OPENED PANEL 411FB TO INSPECT FORWARD END OF PNEUMATIC DUCT, NO DEFECTS NOTED. RAN ENGINE AT IDLE, NO LEAKS NOTED AT ANY PNEUMATIC DUCTS. SUSPECT SENSOR NOT OPERATING PROPERLY, REMOVED SENSOR TT020 P/N S100420PG S/N 3987A AND INSTALLED NEW SENSOR P/N S101816PG S/N 1380 PER CE750 MM 30-16-00 OP'S CHECK GOOD. 2L72 4J RTT00007WI 20050830000192005083000019NM 2005 8 30 DXTA200500928 120050826A3260C16262 PCB AMD FALC50FALCON2000 2730170NM MLG INOPERATIVE E DXTAO OTHER J WARNING INDICATION APAPPROACH 1 GL07284QS 185 UPON GEAR EXTENSION, GOT THE FOLLOWING INDICATIONS, THE 3 RED LIGHTS NO GREEN THE EXTENSION PROCESS THEN STOPPED. HEARD A CLICKING SOUND COMING FROM BEHIND US. JUST AS THE GEAR HANDLE STARTED FLASHING THE EXTENSION PROCESS FINISHED. REMOVED PCB 10GW AND INSTALLED SERVICEABLE PCB 10 GW PERFORMED FULL FUNCTIONAL EXTEND/RETRACT TEST OF L/G AND DOORS NUMEROUS TIMES. OPS CHECK GOOD IAW DASSAULT F2000 M/M 32-300. 2K73 4F RTA50NM 20050830000202005083000020CE 2005 8 30 DXTA200500934 120050828A3230 LANDING GEAR CESSNA650 650 2076802CE MAINS MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07792QS 6507092 AFTER TAKEOFF, GEAR WOULD NOT RETRACT, ACCOMPLISHED AIR TURN BACK. 2L72 4F A9NM 20050830000212005083000021CE 2005 8 30 DXTA200500931 120050826A215073838432 ACM CESSNA750 750 2076810CE ACM BAY INOPERATIVE E DXTAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07943QS2470 7500043 IN FLIGHT HEARD A LOUD POP IN THE CABIN FOLLOWED BY AN ELECTRICAL BURNING ODOR, ALSO IN THE CABIN SHEDDING THE CABIN ELECTRICAL LOAD WITH THE INTERIOR MASTER TO THE OFF POSITION TOOK CARE OF THIS ISSUE INTERIOR MASTER WAS LEFT OFF. REMOVED AND REPLACED FWD AIR CYCLE MACHINE REF CE 750 MM 21-51-00. OPS CK AND CK OF FWD CKS GOOD AT THIS TIME REF CE-750 MM 21-51-00. 2L72 4J RTT00007WI 20050830000272005083000027NM 2005 8 30 SCNA05003 120050826A3350 FUSE BOEING737 7378Q8 13844BXNM EMERGENCY LIGHT FAILED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15809SY 30683 MAINTENANCE FOUND FWD EMERGENCY EXITS LOWER SIGNS NOT WORKING. REMOVED AND REPLACED FUSES IN LT FWD EMERGENCY LIGHT POWER PACK PER AMM 33-51-13, OK FOR SERVICE. 2L72 4F RTA16WE 20050830000292005083000029EU 2005 8 30 XN0A1262 120050825A3240 BRAKE AIRBUS300 A300B4203 3930306EU MLG DRAGGING A XN0AD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL23371PC 157 ON TAXI, NORMAL SYS LEFT & RIGHT BRAKES DRAGGING. HYD YELLOW SYS AIR PRESS LOW LIGHT ON. 2L72 4F RTA35EU 20050830000302005083000030SO 2005 8 30 C2XA05BT063 120050820A3350744412 SIGN EMB 145 EMB145LR 3260212SO EMERGENCY EXIT FAULTY A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713968 145138 DURING 5A INSPECTION, MAINTENANCE FOUND THE AFT GALLEY EMERGENCY EXIT SIGN FAULTY. REMOVED AND REPLACED EMERGENCY EXIT SIGN IAW EMB145 AMM 33-50-14. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050830000322005083000032NM 2005 8 30 SWAA052595 120050826A53116546525 FRAME BOEING737 7373H4 1384600NM BS 380 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29617SW 27700 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050830000332005083000033NM 2005 8 30 SWAA052596 120050826A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 380 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29617SW 27700 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050830000352005083000035NM 2005 8 30 SWAA052598 120050828A53306545775 SKIN BOEING737 7373A4 1384585NM BS 791 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 791, STR 19L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050830000372005083000037NM 2005 8 30 SWAA052600 120050826A3350MS155721 BULB BOEING737 7377H4 1384404NM EMERGENCY EXIT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29770SA 30589 DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050830000382005083000038SO 2005 8 30 C2XA05IA098 120050815A3350744412 SIGN EMB 135 EMB135LR 3260305SO EMERGENCY EXIT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2727523 145389 IAH - DURING MAINTENANCE INSPECTION, THE EMERGENCY LIGHT ON THE AFT GALLEY PARTITION WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050830000392005083000039SO 2005 8 30 C2XA05SH105 120050822A335020131A BATTERY EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713123 145688 SHV - RON MAINTENANCE FOUND EMERGENCY LIGHT BATTERY ABOVE SERVICE DOOR NOT WORKING. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY ABOVE SERVICE DOOR IAW EMB 145 XR VCMM 25-60-03. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RT 20050830000412005083000041SO 2005 8 30 C2XA05IA101 120050820A335078241 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713955 145075 MCI - DURING MAINTENANCE INSPECTION, THE NUMBER ONE EMERGENCY LIGHT INVERTER WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050825000402005082500040EA 2005 8 25 SWIA200515456 120050814A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLT SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07459SW 7782 SPOILERON FAULT, STATUS MSG APPEARED ON TAXI. REPLACED RIGHT INBOARD SPOILERON PCU. OPERATIONAL CHECK GOOD IAW 27-64-01. 2L72 4F RTA21EA 20050825000542005082500054WP 2005 8 25 05FDEA02488 120050816A2613 WARNING LIGHT DOUG MD10 MD1010F 3022112WP GE CF6 CF66D 30020GL CARGO BAY ILLUMINATED A FDEAO OTHER J WARNING INDICATION CRCRUISE 1 SO25368FE 46606 AT FL 320 (SEL CARGO HEAT OFF) ALERT DISPLAYED AND CTR AND AFT CARGO TEMPS WERE 99 DEGRESS. TURNED OF CARGO HEAT AND TEMP REMAINED AT 99 DEGREES. OAT AT FL 320 -8C. BOTH CARGO TEMPS REMAINED AT 99 DEGREES. DECLARED EMERGENCY. LANDED. MEL 17AUG05 00:23 ACN RELEASED FOR SERVICE IAW MEL/CDL: 21-63-02. MEL 21-63-02: LWR CARGO COMPT TEMP INDICATION(S) ( INOP) LOWER CENTER CARGO COMPARTMENT TEMP INDICATIONS INOP. (OPEN) 2L73 4F4 FRTA22WE E23EA 20050825000572005082500057SO 2005 8 25 LR7A05108 120050822A5330 SKIN LKHEED382 382G 526414USO FS 682 GOUGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03406LC 550 4676 DURING SCHEDULED B1 INSPECTION IWA JOB CARD HB5301 FOUND FS 682 FUSELAGE SKIN GOUGED AT RBL 65 WL 162. REPAIRED IAW SRM SMP 58351-140-11. NR 0027. 2H74 4T A1SO 20050825000772005082500077NM 2005 8 25 0501306627 120050818A3220 LANDING GEAR BOEING747 747251B 1384892NM NOSE COLLAPSED A NWAAO OTHER SJ AFFECT SYSTEMS WARNING INDICATION LDLANDING 1 GL01627US 21709 AIRCRAFT LANDED WITH NOSE GEAR UP. FAILURE OF THE NLG DOOR ACTUATOR CAUSED THE NOSE GEAR NOT TO DEPLOY. PASSENGERS/CREW DEPLANED VIA SLIDES. ORIGINALLY IT WAS REPORTED THAT THE NOSE GEAR HAD COLLAPSED ON THE RUNWAY AFTER LANDING. 2L74 4F A20WE 20050825000792005082500079EU 2005 8 25 05FDEA02585 120050822A5347 SEAT TRACK AIRBUS310 A310203 3930313EU FR 71-73 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25425FE 264 SEAT TRACK BETWEEN FS 71-73, LBL 32" HAS SEVERAL SPOTS OF CORROSION. REMOVED LIGHT SURFACE CORROSION IAW SRM 51-74-10 PG 204 .002 MAT LOSS FOUND TO BE WITHIN LIMITS IAW SRM 53-10-16 PG 103. TREATED AND PRIMED IAW SRM 51-21-10 PG 1 AND TOP COATED IAW SRM 51-23-00 PG 1. 2L72 4F RTA35EU 20050825001192005082500119CE 2005 8 25 2005F00095 120050810A2497CM358950 CIRCUIT BREAKER CESSNA414 414A 2075907CE MASTER SWITCH BURNED G A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL0936934 414A0486 FLIGHT WAS TERMINATED WHEN THE AVIONICS MASTER CIRCUIT BREAKER/SWITCH OVERHEATED AND FAILED IN THE (ON) POSITION. MECHANICALLY, THE SWITCH COULD BE MOVED TO THE (OFF) POSITION, BUT ELECTRICALLY WOULD REMAIN (ON). DUE TO ELECTRICAL ODOR AND FAILURE OF THE SWITCH, THE FLIGHT WAS TERMINATED EARLIER THAN ANTICIPATED. MAINTENANCE TROUBLESHOOTING INDICATED THAT THE TOTAL CIRCUIT DRAW WAS 14 TO 15 AMPS. THE SWITCH WAS REPLACED AND NO FURTHER DISCREPANCIES WERE NOTED. THIS CIRCUIT BREAKER/SWITCH APPEARS TO BE AN ORIGINAL PART. A REVIEW OF THE SDR DATA BASE INDICATES THERE HAVE BEEN FIVE OTHER SIMILAR INCIDENTS REPORTED. 1L72 3O A7CE 20050826000012005082600001NM 2005 8 26 DU4R0508179 120050824A5315 FLOORBEAM BOEING757 757232 1384965NM PWA 2037 PW2037 NE FUSELAGE GOUGED B DALAK NONE O OTHER ININSP/MAINT 1 SO15672DL 25977 TOP OF FLOORBEAM IS GOUGED AT STA 1400 LBL 51 WL 208.1. S/O 283002, N/R 23803. 2L72 4F4 FRTA2NM E17NE 20050826000082005082600008WP 2005 8 26 05FDEA02606 120050824A5754 SKIN DOUG DC10 DC1010 3022110WP GE CF6 CF66K 30020NE ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 RT WING FIXED L/E AT SLAT TRACK NR 7 FOUND NR 1 CRACK 1 INCH LONG ON SKIN AT XORS 372. CUT DAMAGED AREA AND REPAIRED WITH DOUBLER IAW SRM. 2L73 4F4 F A22WE E23EA 20050826000222005082600022NM 2005 8 26 05FDEA02597 120050823A2913 PUMP DOUG MD11 MD11 3023602NM GE CF6 CF680C2D1F 30025NE HYD SYSTEM MALFUNCTIONED A FDEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO25613FE 48749 AT CRUISE FL 340 GOT (HYD 3 ELEV OFF) LEVEL 1 ALERT. NR 3 QTY DECREASED SLOWLY TO 3.2 GAL. THEN GOT (HYD 3 OFF) LEVEL 1 ALERT. PUMPS TURNED OFF AND QUANTY STABILIZED AT 3.6. AFTER SLATS EXTENDED AND GEAR EXTENDED, QUANTITY DECREASED TO 1.2. COMPLIED WITH CFM. DIVERTED. REMOVED AND REPLACED NR 3 ENG UPPER EDP AND LOWER EDP PER MM 29-11-20.HYD LINES REQ BLEED AND LEAK CHECK AND OPS CHECK OF EDP'S AND COWLS SECURED CLOSED REMOVED AND REPLACED RESERVOIR PER MM29-12-01-4 MOTORED NR 3 ENG TO BLEED AND LEAK CHECK UPPER AND LOWER EDP'S, RAN NR 3 ENG TO OPS CHECK EDP'S PER JRH AND MD11 MM 29-11-00-0, ALL PARAMETERS MET. A/C OK FOR SERVICE. 2L73 4F4 FRTA22WE E31N3 20050826000232005082600023NM 2005 8 26 182 120050824A5347 SEAT TRACK BOEING757 757232 1384965NM BS 365-400 CORRODED A K NONE O OTHER ININSP/MAINT 1 SO15672DL 25977 CORROSION ON RT IB SEAT TRACK BS 365 TO 400. 2L72 4F RTA2NM 20050826000492005082600049NM 2005 8 26 SWAA052541 120050822A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29341SW 24091 DURING SCHEDULED C4 CHECK, FOUND LOWER FUSELAGE SKIN CRACKED AT BS 727D, BL 0. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050826000502005082600050NM 2005 8 26 SWAA052542 120050822A52306547952230 DOOR FRAME BOEING737 7373H4 1384600NM AFT CARGO BAY CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29341SW 24091 DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR FWD VERTICAL FRAME CRACKED AT UPPER OUTBOARD FASTENER. REMOVED AND REPLACED AFT CARGO DOOR PER MM. 2L72 4F RTA16WE 20050826000562005082600056NM 2005 8 26 SWAA052548 120050824A57116545326 SPAR BOEING737 7373H4 1384600NM RT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29369SW 26580 DURING SCHEDULED 1/4D CHECK, FOUND RT WING FWD SPAR PLATE CRACKED AT WBL 70.85. REPAIRED WING SPAR PER SWA EA & SRM. 2L72 4F RTA16WE 20050826000572005082600057NM 2005 8 26 SWAA052549 120050824A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29369SW 26580 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2L72 4F RTA16WE 20050826000592005082600059NM 2005 8 26 SWAA052551 120050823A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29419WN 29824 FWD SECTION OF EEPLS TRACK BROKEN. REMOVED AND REPLACED EEPLS SECTION PER MM. 2L72 4F RTA16WE 20050826000632005082600063 2005 8 26 SWAA052555 420050823A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29602SW 27953 DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050826000682005082600068WP 2005 8 26 05FDEA02610 120050824A5712ARB129242 RIB DOUG DC10 DC1010 3022110WP ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 RT WING FIXED LEADING EDGE AT STA XORS 810 FOUND NR 1 RIB CRACK. REPAIRED FORMER INSTALLED CLIP IAW SRM 57-20-00 FIG 1 SHEET 4, 6 VOL I. 2L73 4F A22WE 20050826000852005082600085WP 2005 8 26 05FDEA02641 120050825A5712 RIB DOUG DC10 DC1010 3022110WP ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LT WING FIXED LEADING EDGE AT XORS 849 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 4, 6 VOL I. 2L73 4F A22WE 20050826000902005082600090WP 2005 8 26 05FDEA02657 120050825A5712 RIB DOUG DC10 DC1010 3022110WP ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LEFT WING FIXED LEADING EDGE AT XORS 487 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 3, 4 VOL I AND INSTALLED ANGLE REPAIR. 2L73 4F A22WE 20050826000912005082600091WP 2005 8 26 05FDEA02658 120050825A5712 RIB DOUG DC10 DC1010 3022110WP ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LT WING TIP AT XW 912 FOUND NR 1 RIB CRACK. ACCOMPLISH ANGLE REPAIR IAW SRM 57-00-01 FIG 3 SHEET 2 VOL I. REMOVED AND REINSTALLED PLUG ON WEB IAW SRM 51-41-01 FIG 5 VOL II. 2L73 4F A22WE 20050826000922005082600092WP 2005 8 26 05FDEA02642 120050825A5712 RIB DOUG DC10 DC1010 3022110WP ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LT WING FIXED LEADING EDGE AT XORS 821 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 4, 6 VOL I. 2L73 4F A22WE 20050826001032005082600103NM 2005 8 26 05FDEA02473 120050816A5311 FRAME BOEING727 727233 138408ANM BS 620 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 WHILE WORKING FED EX EA 7-5330-72293B PT2, FOUND FASTENER HOLES ON EDGE OF C-CHANNEL FRAME BS 620 STR 2 RT. REPAIRED PER SRM 53-10-1. 2L73 4F RTA3WE 20050829000032005082900003NM 2005 8 29 EIA2005133 120050708A3350S1356B37 LIGHT BOEING747 747212B 1384886NM CABIN INOPERATIVE A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 R5 AND L5 DOOR EMERGENCY EXIT LIGHTS WILL NOT ILLUMINATE. RELAMPED R5 AND REMOVED AND REPLACED EMERGENCY LIGHT ASSY ON L5, IAW MM 33-51-07, OPS CK GOOD. 2L74 4F A20WE 20050829000212005082900021NM 2005 8 29 DHL2005749001 120050819A323169295273 LINK BOEING727 7272J0 138407ENM MLG DOOR BROKEN A DHLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01749DH 22013 WITH GEAR HANDLE IN UP POSITION RED DOOR LIGHTS REMAIN ILLUMINATED WITH MODERATE TO SEVERE VIBRATION. REMOVED AND REPLACED BROKEN DOOR LINK. DOORS OP SERVICEABLE IAW MM 32-35-0 AND 32-22-1 P/N: 69-29527-3. 2L73 4F RTA3WE 20050829000232005082900023NM 2005 8 29 EIA2005136 120050719A3350 FUSE BOEING747 747SR46 1384816NM BATTERY PACK FAILED A EIAAK NONE L NO TEST ININSP/MAINT 1 NM09478EV 21033 DOOR EMERGENCY EXIT LIGHT BY THE UPPER DECK ESCAPE SLIDE IS INOP. REPLACED FUSE ON THE BATTERY PACK. 2L74 4F RTA20WE 20050829000382005082900038NM 2005 8 29 AWXA200501007 120050825A2560P4010021 BATTERY AIRBUSA319 A319132 3930340NM FLASHLIGHT INOPERATIVE A AWXAO OTHER L NO TEST TXTAXI/GRND HDL 1 WP28805AW 1049 LAS - EEL - DURING GROUND HANDLING IN LAS, TECH DISCOVERED THE FORWARD FLIGHT ATTENDANT'S JUMPSEAT FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FLASHLIGHT BATTERY AS REQUIRED. 2L72 4F RTA28NM 20050829000442005082900044WP 2005 8 29 05FDEA02652 120050825A5712 RIB DOUG DC10 DC1010 3022110WP ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LT WING FIXED LEADING EDGE AT XORS 531 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1SHEET 4, 6 VOL I. 2L73 4F A22WE 20050829000572005082900057NM 2005 8 29 05FDEA02550 120050819A5730 SKIN DOUG MD11 MD11 3023602NM LT WING DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 LT WING LE PANEL 516EB , FOUND DENT EXTERIOR SURFACE AT STICKER. REPAIR CARRIED OUT AS PER EA1-5710-90127. 2L73 4F RTA22WE 20050829000612005082900061EA 2005 8 29 VTZA200500149 120050821A2751855D1009 POSITION SENSOR CNDAIRCL600 CL6002B19 1900309EA SLAT/FLAPS FAILED A VTZAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 EA27641BR13148 7349 FLAPS FAIL AT 8 DEGREES. REPLACED LEFT BRAKE POSITION SENSOR UNIT. 2L72 4F RTA21EA 20050829000652005082900065NM 2005 8 29 05FDEA02577 120050819A5740698251710 ATTACH FITTING BOEING727 727227 1384078NM NR 7 FLAP TRACK CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 NR 7 FLAP TRACK FWD ATTACH FITTING IS CORRODED. REPLACED NR 7 FLAP TRACK FWD ATTACH FITTING IAW BOEING DWG 65-17357, OHM 20-50-03, MM 28-11-00. 2L73 4F A3WE 20050829000682005082900068NE 2005 8 29 05FDEA02580 220050821A7320 FUEL CONTROL AIRBUS300 A300F4605R 3930327EU PWA 4158 PW4158 NE NR 2 ENGINE FLUCTUATES A FDEAA UNSCHED LANDING GJ MULTIPLE FAILURE WARNING INDICATION CLCLIMB 1 SO25654FE 738 ON INITIAL CLIMB-OUT, PASSING APPROX 11000 FT MSL, A/T SYSTEM DISENGAGED. WHEN THAT HAPPENED, NOTICED A FLUCTUATION IN NR 1 FUEL FLOW. CONTINUED CLIMB WHILE EVALUATING PROBLEM. NR 2 FUEL FLOW WAS APPROX 12000PPH NR 1 WAS FLUCTUATING BETWEEN 7000 PPH AND 15000 PPH. REPLACED THE NR 1 ENGINE, PERFORMED HIGH POWER RUN PER A300 JRH, ALL CHECKS GOOD, OK FOR SERVICE. 2L72 4F4 FRTA35EU E24NE 20050829000862005082900086NM 2005 8 29 ABXA050201 120050823A3230257T110315 MODULE BOEING767 767281 1385109NM MLG DEFECTIVE A ABXAO OTHER O OTHER LDLANDING 1 GL23787AX 23020 WITH GEAR HANDLE DOWN, 3 GREEN LIGHTS. GEAR DISAGREE ILLUMINATED AND GEAR DISAGREE MESSAGE. GEAR RECYCLED. LANDING GEAR HANDLE MODULE WAS REMOVED AND REPLACED IAW BOEING MM. 2L72 4F RTA1NM 20050829000882005082900088NM 2005 8 29 05FDEA02541 120050818A5315AGA71704 FLOORBEAM DOUG MD11 MD11 3023602NM BS 1841 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 AFT CARGO COMPARTMENT, STA 1841 LOWER FRAME FLOORBEAM SKIN FOUND DAMAGED AS MARKED. AFT CARGO COMPARTMENT, LOWER FRAME FLOORBEAM WEB AT STA 1841, REMOVED AS PER SRM 51-33-01 AND 51-35-01 VOL II. NEW WEB FABRICATED AS PER DRAWING AGA 7170 AND NEW WEB INSTALLED AS PER SRM 51-33-01 AND 51-35-01 VOL II. MINOR REPAIR AS PER GMMM 6-2-100. 2L73 4F RTA22WE 20050829001002005082900100NM 2005 8 29 SWAA052561 120050824A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 727C TO BS 727D, STR 14L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050829001042005082900104NM 2005 8 29 SWAA052565 120050823A53216546833 WEB BOEING737 7375H4 138449DNM COCKPIT FLOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29503SW 24180 DURING SCHEDULED SPECIAL VISIT, FOUND COCKPIT FLOOR WEB CRACKED BETWEEN BS 188 TO BS 196, LBL 29, WL 208. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050829001062005082900106NM 2005 8 29 SWAA052567 120050825A53116516301 FRAME BOEING737 7375H4 138449DNM COCKPIT FLOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29503SW 24180 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STUB FRAME CRACKED AT BS 188, LT SIDE, WL 208. REMOVED AND REPLACED STUB FRAME PER SRM. 2L72 4F RTA16WE 20050829001122005082900112NM 2005 8 29 05FDEA02660 120050825A5730 SKIN BOEING727 727200 138407ENM CENTER WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 COMPLY WITH EA 7-5710-82121, WINGS-STRUCTURE- REPAIR OF CENTER SECTION LOWER SKIN CORROSION. COMPLIED WITH EA 7-5710-82121 WINGS STRUCTURE REPAIR OF CENTER SECTION LOWER SKIN CORROSION THIS IS A MAJOR REPAIR RII:497236. 2L73 4F RTA3WE 20050829001132005082900113NM 2005 8 29 05FDEA02659 120050823A362020035012007 SENSOR DOUG MD11 MD11 3023602NM ZONE 400 DEFECTIVE A FDEAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO25578FE4509545095 48458 APPROX 2:40 HOURS INTO FLIGHT, LEVEL THREE AIR MANIFOLD 2 FAIL ALERT ILLUMINATED. CLEARED MASTER WARNING AND RAN APPROPIATE QRH LIST. SYSTEM 2 ON THE AIR SYNOPTIC DISPLAYED AS A RED LINE. MANIFOLD 2 MAINTAINED AIR PRESSURE THROUGHOUT REMAINDER OF FLT AND "BLEED AIR 2 OFF" NEVER ILLUMINATED ON THE AIR SYNOPTIC PAGE. A/C DIVERTED INTO CTS. REPLACED DEFECTIVE SENSORS D1-29 AND D1-28. REPLACED MFC PRECAUTIONARY. 2L73 4F RTA22WE 20050829001182005082900118NM 2005 8 29 05FDEA02669 120050826A5347 SEAT TRACK DOUG MD11 MD11 3023602NM BS 1321-1352 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 AFT CABIN - SEAT TRACK BASE AND CROWN CORRODED AT STA 1321 TO STA 1352 RT RBL 75. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-70-00 FIG.3 VOL I. CARRIED OUT REPAIR AS PER SRM 53-70-00. 2L73 4F RTA22WE 20050829001232005082900123EA 2005 8 29 COMA0560459 120050821A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01984CA 7171 FLIGHT 5606 - LT REVERSER UNLOCKED CAUTION. FOUND NO DEFECTS. T/R WAS ON DEFERRED MAINTENANCE LIST. 2L72 4F RTA21EA 20050829001272005082900127 2005 8 29 PIDA20050066 420050822A2210 AUTOPILOT SYS BOEING757 757236 1384971NM COCKPIT MALFUNCTIONED A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05757BJ 22176 CENTER AUTO PILOT PITCHES NOSE DOWN WHEN ENGAGED. PLACED ON MEL 22-10-1. 2L72 4F RTA2NM 20050829001352005082900135NM 2005 8 29 USAA051049 120050824A5320 FLOOR SUPPORT BOEING737 7374B7 1384702NM BS 794-847 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19449US 24893 RBL 13.80 BETWEEN STA 794.0 AND 847.0 CORRODED. FABRICATED NEW FLOOR SUPPORT STRINGER AND INSTALLED PER TR 53-10-08 AND 51-10-02, DEFECT SIZE: LEVEL 1. 2L72 4F RTA16WE 20050829001372005082900137WP 2005 8 29 MWEA050087 120050823A524259100835 DOUBLER DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE E/E DOOR DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 DENT ON EMERGENCY EXIT DOOR. FABRICATED AND INSTALLED DOUBLER. 2L72 4F4 F A6WE E9NE 20050829001422005082900142NM 2005 8 29 SB05099 120050825A3350606171 SOCKET BOEING737 7373B7 1384580NM SEAT 15L FAILED A USAAK NONE O OTHER ININSP/MAINT 1 EA19512AU 23595 MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT AT SEAT 15L INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT SOCKET. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050829001542005082900154WP 2005 8 29 AALA20050552 120050823A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHTSLOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21429AA 49341 ORD - EMERGENCY LIGHTS ON TAIL CONE SLIDE INOPERATIVE. FOUND LOOSE CONNECTION ON BATTERY PACK. TIGHTENED CONNECTION ON BATTERY PACK FOR EMERGENCY LIGHT ON TAIL CONE SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050829001612005082900161EA 2005 8 29 SWIA200515462 120050824A274070623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA ACTUATOR MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07446SW8631 8631 7666 STAB CH 1 INOP. REPLACED MCU AND HORIZONTAL ACTUATOR. COMPLIED WITH RII 27-415 IAW MM 27-40-00, 27-42-01, 27-42-05. OPERATIONAL CHECK GOOD. P/N 8396-3, S/N OFF 912. 2L72 4F RTA21EA 20050829001622005082900162EA 2005 8 29 SWIA200515463 120050822A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07446SW 7666 REAR, LEFT SIDE EMERGENCY LIGHT INOPERATIVE. INSTALLED A NEW FLOOR LEVEL POWER STRIP IN THE AFT POSITION. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050829001642005082900164EU 2005 8 29 SA05095 120050816A3350 LIGHT AIRBUSA319 A319112 3930323EU CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19701UW 890 BDL - THE AFT RIGHT EXIT ROW EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED THE BROKEN WIRING. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20050829001952005082900195EA 2005 8 29 SWIA200515464 120050823A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY MALFUNCTIONED A SWIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM07431SW 7536 FIVE MINS AFTER T/O REC'D SMOKE CARGO MSG. MSG WENT OUT AFTER 3 SECONDS. REPLACED NR 1 AND NR 2 CARGO SMOKE DETECTORS PER CRJ MM 26-15-01. OPERATIONAL CHECK GOOD. P/N 473597-19, S/N OFF 1747, S/N OFF 1746. 2L72 4F RTA21EA 20050829001982005082900198 2005 8 29 SWIA200515467 420050820A34183995100208 COMPUTER CNDAIRCL600 CL6002B19 1900309EA STALL WARNING MALFUNCTIONED A SWIAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 NM07409SW 7056 AFTER TAKEOFF, STALL FAIL CAUTION MSGS. REPLACED STALL PROTECTION COMPUTER. OPERATIONAL CHECK GOOD IAW MM 27-35-01, P/N ON 3995100208, S/N OFF 247. 2L72 4F RTA21EA 20050829001992005082900199EA 2005 8 29 SWIA200515468 120050823A52102R5206B MOTOR CNDAIRCL600 CL6002B19 1900309EA PAX DOOR MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07438SW1062510625 7574 MCD WILL NOT OPEN. REPLACED PAX DOOR MOTOR ASSY IAW MM 52-11-08. OPERATIONAL CHECK GOOD. P/N 2R5206B OFF 0129. 2L72 4F RTA21EA 20050829002022005082900202 2005 8 29 PIDA20050064 420050814A2210A71882 SERVO VALVE BOEING757 757236 1384971NM AILERONS INOPERATIVE A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05757BJ 22176 CENTER AUTOPILOT INOP, WILL NOT ENGAGE IN FLIGHT. PLACED ON MEL 22-10-1. 08/21/2005, REPLACED CENTER SYSTEM AILERON SERVO VALVE. OPS CHECKS GOOD PER MM 22-13-04. 2L72 4F RTA2NM 20050829002042005082900204NM 2005 8 29 SWAA052572 120050825A53106546803 CREASE BEAM BOEING737 7373H4 1384600NM BS 500-500A CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29617SW 27700 DURING SCHEDULED D-CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 500 TO BS 500A. REPAIRED CREASE BEAM WEB SECTION PER SRM. 2L72 4F RTA16WE 20050829002072005082900207 2005 8 29 SWAA052575 420050824A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29627SW 27935 DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050829002182005082900218NM 2005 8 29 DHL2005781003 120050827A335010604503 RELAY BOEING727 727227 1384078NM EMERGENCY LIGHT FAILED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 EMERGENCY EXIT LIGHTS ON WITH SWITCH IN THE ARMED POSITION. REMOVED AND REPLACED R70 EMERGENCY EXIT RELAY IAW WD 33-51-00, GROUND OPS CHECK NORMAL. P/N 10-60450-3 USED. 2L73 4F A3WE 20050830000032005083000003CE 2005 8 30 DJFA2005131 120050817A213032908001 CONTROL VALVE BEECH MU300 400A 1155402CE PWA JT15 JT15D5 52112NE CABIN INOPERATIVE E DJFAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA23731TA RK273 THE CREW REPORTED THAT WHILE IN CRUISE FLIGHT AT FL 250 THERE WAS EXTREMELY HOT AIR BLOWING FROM THE REAR VENT IN THE LAVATORY. THE AFT CABIN WALL WAS FOUND TO BE EXTREMELY HOT AND WAS SMELLING LIKE BURNING RUBBER. A REQUEST WAS MADE TO DIVERT THE AIRCRAFT, AND AN UNEVENTFUL LANDING WAS MADE. FOLLOWING LANDING, THE CREW ALSO NOTED THAT THE AIRCRAFT WAS PRESSURIZING WHILE ON THE GROUND. MAINTENANCE REPLACED THE CABIN TEMPERATURE CONTROL VALVE AND PERFORMED A CABIN TEMPERATURE SYSTEM TEST. OPERATIONAL AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4F4 FRTA16SW E25EA 20050830000232005083000023NM 2005 8 30 DXTA200500932 120050827A2400 CONTROL BOX GULSTM200 200 4500308NM COCKPIT HOT E DXTAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07703QS 060 AT FL410, CREW DETECTED A STRONG ODOR OF ELECTRICAL BURNING. CABIN MASTER ISOLATED IT AND ODOR WENT AWAY. FOUND AIRSHOW BOX (BLUE) BEHIND DRAWER WITH PLATES WAS VERY HOT. 2L72 4F RTA53NM 20050830000342005083000034NM 2005 8 30 SWAA052597 120050825A5753 SKIN BOEING737 7373H4 1384600NM LH WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29626SW 1558 27702 DURING SCHEDULED C4 CHECK, FOUND LT OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM. 2L72 4F RTA16WE 20050830000362005083000036NM 2005 8 30 SWAA052599 120050825A2560PH22300L GLOWSTRIP BOEING737 7377H4 1384404NM CABIN DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29713SW 27847 DURING SCHEDULED RON CHECK, FOUND 3 SECTIONS OF PHOTOLUMINESCENT STRIPS DAMAGED. REMOVED AND REPLACED STRIPS PER MM. 2L72 4F RTA16WE 20050830000422005083000042GL 2005 8 30 RAIA00508028 220050822A7200 ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 2 MALFUNCTIONED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03830HK 145313 FLT 5525-STL- E2 ATTCS NO MARGIN DISPLAYED ON EICAS DURING TAKEOFF. MAINTENANCE RESET NR 2 ENGINE FADEC CB, PERFORMED CMC DOWNLOAD AND PERFORMED AN OPERATIONAL CHECK. OPS CHECKED GOOD. 2L72 4T4 FRTT00011ATTE6CH 20050830000432005083000043SO 2005 8 30 RAIA00508029 120050822A3397 CONNECTOR EMB 145 EMB145 3260210SO EMERGENCY LIGHT LOOSE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03821HK 145068 DURING PREFLIGHT EMERGENCY ESCAPE PATH LIGHTING WAS FOUND TO BE INOP. MAINTENANCE RESECURED A LOOSE CONNECTION. OPS CHECKED GOOD. 2L72 4F RTT00011AT 20050830000442005083000044SO 2005 8 30 RAIA00508034 120050823A2730 WARNING LIGHT EMB 145 EMB145LR 3260212SO PITCH TRIM ILLUMINATED A RAIAO OTHER J WARNING INDICATION DEDESCENT 1 CE03839HK 14500829 FLT 7989 - IAD - ON ARRIVAL DESCENT AT 210 KNOTS AS F/O TOUCHED TRIM DOWN TO DISCONNECT AP, BOTH PITCH TRIM MAIN AND PITCH TRIM BACKUP WARNING MESSAGES ILLUMINATED. MAINTENANCE CLEANED MAIN AND BACKUP TRIM SWITCHES AND PERFORMED TEST OF ALL SWITCHES RELATED TO PITCH TRIM. NO DEFECTS NOTED. 2L72 4T RTT00011AT 20050830000452005083000045EA 2005 8 30 COMA0560461 120050822A2750860D10018ABC CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01814CA130257486 7387 FLIGHT 5274 - FLAPS FAIL CAUTION. REPLACED THE FECU. 2L72 4F RTA21EA 20050830000462005083000046EA 2005 8 30 COMA0560462 120050822A32971730013000001 WIRE HARNESS CNDAIRCL600 CL6002B19 1900309EA RT MLG MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01457CA 7612 FLIGHT 5084A - ANTI/SKID INOP CAUTION. REPLACED THE RT MLG WIRE HARNESS. 2L72 4F RTA21EA 20050830000472005083000047NE 2005 8 30 COMA0560463 220050823A7261407T95PO1 SCREEN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT ENGINE CLOGGED A COMAEA ENGINE SHUTDOWN UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CRCRUISE 1 SO01868CA 7427 FLIGHT 5653 - LEFT ENGINE OIL PRESSURE WARNING, I.F.S.D. FOUND C-SUMP SCAVENGE PUMP INLET SCREEN CLOGGED. REPLACED SUMP SCREEN FITTING. 2L72 4F4 FRTA21EA E15NE 20050830000482005083000048EA 2005 8 30 COMA0560464 120050823A2752854D10019 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01937CA2454 7044 FLIGHT 5058A - FLAPS FAIL CAUTION. CND, REPLACED THE LT OUTBOARD FLAP ACTUATORS. 2L72 4F RTA21EA 20050830000492005083000049EU 2005 8 30 2005133 120050821A2130 CABIN PRESSURE BRAERODH125 BAE125800A 1500285EU MALFUNCTIONED E DJFAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 EA23811CW 258011 KTTN - KCGF THE CABIN ALTITUDE WAS NOTED AS UNUSUALLY HIGH. THE CABIN RATE CONTINUED TO CLIMB AS THE AIRCRAFT DESCENDED AND THE CABIN ALTITUDE WARNING HORN SOUNDED. THE CREW DECLARED AN EMERGENCY AND PERFORMED AN EMERGENCY DESCENT. THE AIRCRAFT LANDED WITHOUT INCIDENT. 2L72 4F RTA3EU 20050830000502005083000050NE 2005 8 30 NACA20050019 220050825A8530356993 CYLINDER DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE NR 2 GALLED A NACAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CRCRUISE 1 AL032907F732 732 533265 P31426 NR 4 ENGINE FEATHERED DUE TO NR 2 CYLINDER DOUBLE SHORTED SECONDARY. INSPECTED NR 2 CYLINDER SPARK PLUG AND FOUND TO BE PEENED. REPLACED NR 2 CYLINDER. OP CHECK GOOD. 2L74 4R4 R A781 5E8 20050830000512005083000051GL 2005 8 30 C2XA05IA086 220050712A720023058318 BEVEL GEAR EMB 145 EMB145XR 3260214SO ALLSN AE300 AE3007A GL NR 1 ENGINE FAILED A C2XAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION DEDESCENT 1 SW2717159 145792 CAE312354 FLIGHT 2543 - EN ROUTE TO IAH THE CREW REPORTED THAT THE NR 1 ENGINE SHUT DOWN UNCOMMANDED DURING DESCENT AROUND 14,000 FT. ENGINE 1 OUT, MESSAGE WAS DISPLAYED ON THE EICAS SCREEN ALONG WITH SHED BUS 1 AND 2. THE CREW ATTEMPTED TO AIR START THE ENGINE BUT WAS UNABLE TO AND THE NR 1 ENGINE N2 INDICATION WENT TO DASHES. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE ENGINE. NOTE: NO TIMES OR SERIAL NUMBER AVAILABLE FOR BEVEL GEAR. 2L72 4F4 FRT TE6CH 20050830000522005083000052CE 2005 8 30 1050812038AMW 120050824A5320 ANGLE BEECH 1900 1900D 1154162CE FUSELAGE CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07143YV UE143 AT FS 303 RIGHT HEAVY ANGLE CRACKED. MORE INFORMATION WILL BE AVAILABLE AT A LATER DATE. 2L72 4T RTA24CE 20050830000532005083000053NM 2005 8 30 SWAA052581 120050824A53306545775 SKIN BOEING737 7373H4 1384600NM BS 810 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 810, STR 14R. MX FERRY TO DALLAS. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050830000542005083000054NM 2005 8 30 SWAA052582 120050824A53306545767 SKIN BOEING737 7373H4 1384600NM BS 400 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 400, STR 26R. MX FERRY TO DALLAS. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050830000562005083000056NM 2005 8 30 SWAA052584 120050824A53306545767 SKIN BOEING737 7373H4 1384600NM BS 424 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 424, STR 26L. MX FERRY TO DALLAS. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050830000672005083000067SO 2005 8 30 SIMA200521613 120050803A3350BA50933901 POWER SUPPLY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCHARGED A SIMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW21649PP 145234 EVV - FLT 4304 - OVERWING AISLE EMERGENCY EXIT SIGN FAILS TO ILLUMINATE. REPLACED NR 2 EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20050830000702005083000070EA 2005 8 30 A6WA200540282 120050803A5753 VANE CNDAIRCL600 CL6002B19 1900309EA RT TE FLAP WORN A A6WAK NONE O OTHER ININSP/MAINT 1 GL31405AW 7362 RIGHT OUTBOARD FLAP VANE, OUTBOARD FLAP VANE FITTING WORN EVEN WITH LEADING EDGE OF VANE .030 INCH IS MINIMUM CLEARANCE ALLOWED PER BOMBARDIER, INC REO 601R-57-53-195. REMOVED OLD VANE FITTING FROM RIGHT OUTBOARD FLAP AS WS 296.073 AND INSTALLED NEW VANE FITTING P/N 601R14560-6 IAW BOMBARDIER, INC REOS 601R-57-53-019 AND 601R-57-53-195. (M) 2L72 4F RTA21EA 20050830000722005083000072EA 2005 8 30 A6WA200540287 120050815A5210 SKIN CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31465AW 7893 PASSENGER DOOR AFT SKIN DAMAGED AND INTERNAL STIFFENER CRACKED BELOW SKIN RIGHT STIFFENER CRACKED COMPLETELY IN HALF 1.5 INCH. INSTALLED REPAIR FILLER AND DOUBLE IAW BRAS EO 601R-52-7054A. (M) 2L72 4F RTA21EA 20050830000742005083000074EA 2005 8 30 A6WA200540285 120050811A5310 STRUCTURE CNDAIRCL600 CL6002B19 1900309EA MLG WW DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31464AW 7890 WHILE RETRACTING RIGHT MLG DAMAGE OCCURRED TO THE UPLOCK APRON ASSEMBLY BY PUNCHING A HOLE APPROX 1.5 INCH BY 1 INCH. REPAIRED RIGHT MLG WHEEL WELL CHANNEL BY CUTTING OUT DAMAGE FABRICATING AND INSTALLING REPAIR IAW BRAS EO 601R-53-7036. (M) 2L72 4F RTA21EA 20050830000752005083000075NM 2005 8 30 ASAA0540302 120050626A5753 SKIN BOEING737 7374Q8 138447QNM TE FLAP CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 OKC - FOUND RIGHT INBOARD FORE FLAP UPPER SURFACE CHAFED. REPAIRED IAW 737-400 SRM 51-70-10 REPAIR. (M) 2L72 4F RTA16WE 20050830000762005083000076NM 2005 8 30 ASAA0540304 120050626A5330 SKIN BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 OKC - FOUND AFT CARGO DOOR FORWARD INNER SURROUND SKIN IS CORRODED BETWEEN STRINGER 23R AND 26R FUSELAGE STATION 793. REMOVED CORRODED SKIN, FABRICATED AND INSTALLED REPAIR IAW 737-400 SRM 51-40-5 AND 51-40-2. (M) 2L72 4F RTA16WE 20050830000772005083000077NM 2005 8 30 ASAA0540306 120050626A53306546431244 SKIN BOEING737 7374Q8 138447QNM FS 202.6-414.4 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 OKC - RIGHT OUTBOARD FORE FLAP HAS 4 EACH DENTS ON UPPER AFT SURFACE. REPAIRED RIGHT OUTBOARD FORE FLAP UPPER SURFACE IAW 737-400 SRM 51-70-10 REPAIR 21. (M) 2L72 4F RTA16WE 20050830000782005083000078SO 2005 8 30 SIMA200520101 120050717A3350744412 LIGHT EMB 135 EMB135LR 3260305SO CABIN INOPERATIVE A SIMAO OTHER O OTHER NRNOT REPORTED 1 SW21717AE 145272 FORWARD BULKHEAD EMERGENCY LIGHT FAILS TO ILLUMINATE. REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050830000792005083000079SO 2005 8 30 SIMA20051609 120050801A5320 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO FRAME 25 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21815AE 145545 ABI - A PREVIOUS REPAIR ON THE CENTER OMEGA BEAM AT FRAME 25 WAS FOUND TO BE CORRODED. REMOVED THE CORRODED REPAIR PARTS. FABRICATED A DOUBLER AND FILLER. REPAIR DONE IAW EMB IC2005-145/4050 DATED AUGUST 1, 2005. (M) 2L72 4F RTT00011AT 20050830000802005083000080SO 2005 8 30 SIMA200520002 120050719A335020131A POWER SUPPLY EMB 135 EMB135KL 3260302SO EMERGENCY LIGHT DISCHARGED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21808AE 145519 LEFT WING LOWER EMERGENCY LIGHT INOPERATIVE. REPLACED NR 1 BATTERY POWER SUPPLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050830000822005083000082CE 2005 8 30 GUU2005F00041 120050812A3240 BRAKE ASSY BEECH 1900 1900D 1154162CE MLG MALFUNCTIONED A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO1787550 UE205 FLT 9304 - TCB/FLL - POOR BRAKING ACTION ON LEFT BRAKE. BLED LEFT BRAKES. (M) 2L72 4T RTA24CE 20050830000832005083000083NM 2005 8 30 GAIA05022OP 120050811A33501315 BULB BOEING727 7272J0 138407ENM L1 DOOR BURNED OUT A GAIAK NONE O OTHER ININSP/MAINT 1 SW07281KH 21105 L1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED L1 DOOR EMERGENCY EXIT LIGHT. LIGHT OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F RTA3WE 20050830000862005083000086NM 2005 8 30 USAA050952 120050803A5551 BUSHING BOEING737 7373B7 1384580NM HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US 23933 CLT - FOUND LUG/BUSHING CORRODED 2 INCH DIAMETER BY .015 TYPICAL, L3, FORWRD FACE LEFT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED NEW BUSHING IAW SRM 53-10-10. (M) 2L72 4F RTA16WE 20050830000882005083000088CE 2005 8 30 GLBA20050507 120050821A6123 AUTOFEATHER SYS BEECH 1900 1900D 1154162CE LT ENGINE MALFUNCTIONED A GLBAO OTHER J WARNING INDICATION APAPPROACH 1 NM03240GL UE240 LEFT ENGINE SOUNDED LIKE IT CYCLED THROUGH AN AUTOFEATHER, INCREASED POWER AND CONDITION CEASED, LANDED WITHOUT INCIDENT. PERFORMED GROUND RUN-UP, COULD NOT DUPLICATE, RETURNED TO SERVICE. 2L72 4T RTA24CE 20050830000892005083000089 2005 8 30 RYNA200500027 420050825A23106225272001 TRANSCEIVER BOEING757 757225 1384959NM HF SYSTEM INOPERATIVE A RYNAA UNSCHED LANDING O OTHER CRCRUISE 1 CE07930RD 22210 BOTH HF SYSTEMS WOULD NOT TRANSMIT. REMOVED AND REPLACED BOTH HF TRANSCEIVERS, SYSTEM OPERATIONALLY CHECKED GOOD. 2L72 4F RTA2NM 20050830000902005083000090 2005 8 30 ASMF200508013 420050822A3441 INDICATOR DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE RADAR INOPERATIVE W ASMFO OTHER J WARNING INDICATION CRCRUISE 1 SW23838AM9367 9367 204 49397 AIRCRAFT RETURNED, DURING CRUISE RADAR SYSTEM WAS OUT OF SERVICE. DURING MAINTENANCE REVISION WAS DETECTED RADAR INDICATOR OUT OF SERVICE. THE INDICATOR RADAR WAS REPLACED IAW MM 34-41-02, TESTED CORRECT AND THE OVERWEIGHT LANDING CHECK WAS PERFORMED IAW MM 05-51-04, ALL CORRECT. AFTER DISPATCH, AIRCRAFT RETURNED TO PLATFORM, FLIGHT CONTROLS TEST, MOVEMENT OF PEDAL WAS RESTRICTED. THE STEERING MECHANISM SYSTEM WAS CHECK IAW MM 32-50-00 AND THE RUDER CONTROL LEVER WAS POSITIONED CORRECTLY IAW MM 27-20-00, TESTED CORRECT. 2L72 4F4 FRTA6WE E9NE 20050830000912005083000091SO 2005 8 30 CHQA200500149 120050828A33507287580505 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A CHQAK NONE O OTHER ININSP/MAINT 1 GL11298SK 145508 FIRST FLOOR EMERGENCY LIGHT STRIP INOPERATIVE. REMOVED AND REPLACED THE FIRST FLOOR EMERGENCY LIGHT STRIP IAW EMB 145 MM 33-50-12. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050830000922005083000092SO 2005 8 30 CHQA200500152 120050827A335066367 LIGHT EMB 145 EMB145EP 3260221SO NR 3 BURNED OUT A CHQAK NONE O OTHER ININSP/MAINT 1 GL11978RP 145169 NR 3 EMERGENCY FLOOR LIGHT PROXIMITY STRIP INOPERATIVE. REMOVED AND REPLACED NR 3 EMERGENCY FLOOR LIGHT STRIP. OPS CHECK GOOD IAW EMB 145 MM 33-50-12. 2L72 4F RTT00011AT 20050830000932005083000093SO 2005 8 30 CHQA200500150 120050827A33501317 LAMP EMB 135 EMB135KL 3260302SO EMERGENCY LIGHT BURNED OUT A CHQAK NONE O OTHER ININSP/MAINT 1 GL11375SK 145569 LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. RELAMPED EMERGENCY LIGHT IAW EMB 140 MM 33-50-07. 2L72 4F RTT00011AT 20050830000942005083000094SO 2005 8 30 CHQA200500148 120050827A335078241 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSINOPERATIVE A CHQAK NONE O OTHER ININSP/MAINT 1 GL11286SK 145443 EMERGENCY FLOOR LIGHTS NR 6, NR 7, AND NR 8 ARE INOPERATIVE. REMOVED AND REPLACED NR 6 EMERGENCY BATTERY INVERTER. OPS CHECK GOOD IAW EMB 145 MM 33-50-11. 2L72 4T RTT00011AT 20050830000952005083000095SO 2005 8 30 CHQA200500151 120050827A3350 LAMP EMB 135 EMB135KL 3260302SO EMERGENCY LIGHT BURNED OUT A CHQAK NONE O OTHER ININSP/MAINT 1 GL11381SK 145619 AISLE EMERGENCY LIGHT NR 3 LAMP INOPERATIVE. RELAMPED NR 3 AISLE EMERGENCY LIGHT IAW EMB 140 MM 33-50-08. OPS CHECK GOOD. 2L72 4F RTT00011AT 20050830000982005083000098 2005 8 30 BA05016 420050803A25657A1508115 SLIDE AIRBUS330 A330323 3930335EU 4L DOOR LOW A USAAK NONE O OTHER ININSP/MAINT 1 EA19676UW2314910377 375 PHL - PRIOR TO FLIGHT, RECEIVED "SLIDE LOW PRESSURE 4L" MESSAGE. MAINTENANCE RELEASED THE AIRCRAFT ON MEL FOR A SLIDE INDICATION PROBLEM. MAINTENANCE REPLACED THE 4L DOOR EMERGENCY ESCAPE SLIDE. OK FOR SERVICE. 2L72 4F RTA46NM 20050830000992005083000099EA 2005 8 30 A6WA200540286 120050816A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FS 654 LIGHTNING STRIKEA A6WAK NONE O OTHER ININSP/MAINT 1 GL31465AW 7893 FUSELAGE SKIN HAS SUSTAINED LIGHTNING STRIKE DAMAGE AT FS 654.5 BETWEEN STR 26R AND 27R. REPAIRED DAMAGED AREA BY INSTALLING AN EXTERNAL DOUBLER AT FS 654.5 BETWEEN STR 26R AND 27R IAW EO AND SRM. (K) 2L72 4F4 FRTA21EA E15NE 20050830001002005083000100NM 2005 8 30 USAA051062 120050829A5314 KEELBEAM BOEING737 7373B7 1384580NM STA 520 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US 23933 STA 520 S-28/KEEL BEAM. REMOVED DAMAGED, INSTALL FILLERS, SHIMS AND REPAIR ANGLE IAW EA 96839, DEFECT SIZE: 1 X 3. 2L72 4F RTA16WE 20050830001022005083000102 2005 8 30 TSAA0531037 420050822A31004081600930 DISPLAY BOEING737 7377Q8 1384418NM GE CFM56 CFM567B24 NE NR 1 INOPERATIVE A TSAAA UNSCHED LANDING G MULTIPLE FAILURE CRCRUISE 1 WP13751AL4676 30674 DISPLAY SOURCE ILLUMINATED BOTH SIDES SPD L AND M ILLUMINATED CAPTAIN’S SIDE, NO NAVIGATIONAL MAP-SOURCE ALL ON 1 = ALL BLANK; DIVERTED. MTX ACTION, REMOVED AND REPLACED NR1 DEU IAW MM 31-62-2-21-4, OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA16WE E00055EN 20050830001072005083000107EU 2005 8 30 05FDEA02690 120050826A2612 FIRE LOOP AIRBUS310 A310222 3930315EU MALFUNCTIONED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25418FE 343 REPLACED FIRE DET ASSY (H2/H4) FOR BOTH LOOP A AND B, THIS ALSO CLEARED MEL ON "A" LOOP WRI 26-10/9082 PER MM 26-12-12-4. OPS CHECK SATIS AND PERFORMED ENG RUN PER A-310 JRH OK. 2L72 4F RTA35EU 20050830001132005083000113 2005 8 30 05FDEA02695 420050827A3418 WARNING LIGHT DOUG DC10 DC1010 3022110WP STALL WARNING ILLUMINATED A FDEAA UNSCHED LANDING E VIBRATION/BUFFET TOTAKEOFF 1 SO25367FE 46605 ON ROTATE STICK SHAKER ACTIVATED 140KTS A/C FULL BUFFET TO 3000 FT 180 KTS. DID NOT CHANGE T/O CONFIG. A/C STALL AT 15DGS AOB 210 KTS 15DGS FLAP. FLAPS 50, A/C BUFFETED AT 160KTS IN A FULL STALL LANDING, 20KTS FASTER THAN BUG. CKD FOR FULL EXT OF FLAPS /SLATS. INSP ALL FLT CONT SURFACES WERE CONFIG CORRECTLY. CKD SPOILERS FULL UP AND DOWN. NO DEFECTS. PERF STALL ADJ/TST AND AT/SC ADJ/TST IAW DC-10MM'S 22-33-00-2, AND 22-30-00 REF WRI 34-18/7405 FOR WORK ACCOMP, C/W ELEV LOAD FEEL AND MECH TESTS REF DC-10 MM 27-30-00-5. CKD FLAP AND AOA VANE FOR PROPER OP. REMOVED AND REPLACED AT/SC NR 2. REMOVED AND REPLACED NR 2 LAU PER M/M22-11-01-2. PURGED AND LEAK CKD CAPT'S AND F/O'S PITOT SYSTEMS. 2L73 4F A22WE 20050830001152005083000115NM 2005 8 30 05FDEA02697 120050828A5320 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 UPPER CARGO, SEAT TRACK LBL 27 CRACKED AT STA 1338. REPAIRED AS PER SRM 53-70-00 FIG 1 VOL I. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050830001162005083000116NM 2005 8 30 05FDEA02681 120050826A5310 SEAT TRACK DOUG MD11 MD11 3023602NM BS 1964-1966 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 AFT CABIN CURVED SEAT TRACK CORROSION ON FLANGES, CROWN AND BASE AT STA 1964 TO 1966 RBL 107. CARRIED OUT REPAIR AS PER SRM 53-70-00 FIG.1 VOL.I. CLASSIFIED MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050830001182005083000118WP 2005 8 30 05FDEA02683 120050826A5522 SKIN DOUG DC10 DC1010 3022110WP ZONE 300 NICKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 RT I/B ELEVATOR UPPER SURFACE FOUND NICK BETWEEN STA XE 225 AND XE 238. ACCOMPLISH EXTERNAL DOUBLER REPAIR IAW SRM 55-10-00 FIG 8 VOL I. 2L73 4F A22WE 20050830001202005083000120WP 2005 8 30 05FDEA02685 120050826A5730CODE516EB ACCESS PANEL DOUG DC10 DC1010 3022110WP ZONE 500 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LT WING ACCESS PANEL FOUND HARDWARE ON EXTERNAL SKIN WITH HOLE WORN. REPAIR WITH DOUBLER IAW SRM 57-10-00 FIG 10A VOL I. 2L73 4F A22WE 20050830001222005083000122NM 2005 8 30 05FDEA02699 120050828A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 UPPER CARGO, SEAT TRACK 47 CRACKED AT STA 1095 TO STA 6-51. REPAIRED AS PER SRM 53-70-00 FIG 1 VOL I. THIS REPAIR CLASSIFED AS MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050830001242005083000124NM 2005 8 30 05FDEA02701 120050828A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 UPPER CARGO, SEAT TRACK LBL 27 CRACKED AT STA 1169. REPAIRED AS PER SRM 53-70-00 VOLUME I FIGURE 1. THIS REPAIR CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050830001262005083000126NM 2005 8 30 05FDEA02703 120050827A5297 CONNECTOR DOUG MD11 MD11 3023602NM DOOR WARNING DAMAGED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25631FE 48454 AIR CONDITION DOOR LIGHT CAME ON OVER SGF. FOUND PIN NR 2 PUSHED BACK IN S1-255, RESEATED PIN, OPS CHECKS NORMAL. 2L73 4F RTA22WE 20050830001282005083000128NM 2005 8 30 05FDEA02705 120050829A5330 SKIN BOEING727 72722 1384002NM BS 1203-1223 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25192FE 19085 WHILE WORKING ON AIRCRAFT, RAN INTO AIRCRAFT N192FE. DENTED AT BS 1203L TO 1223L IN BETWEEN STRINGERS 19 & 20, GOUGED AT BS 1203L TO 1223L IN BETWEEN STRINGERS 20 & 21. REPAIRED SKIN PER SRM 53-30-3, MAJOR REPAIR. 2L73 4F A3WE 20050830001302005083000130GL 2005 8 30 RAIA00508035 220050822A7200 COMPRESSOR EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 2 ENGINE STALLED A RAIAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 CE03830HK129775841 145313 311264 FLT 5525 - STL - NR 2 ENGINE HAS COMPRESSOR STALLS. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE. 2L72 4T4 FRTT00011ATTE6CH 20050830001342005083000134EA 2005 8 30 REX2005F00014 120050716A3260 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE MLG ILLUMINATED A REXAO OTHER N FALSE WARNING APAPPROACH 1 SO258525B9649 7525 (REF NR: 05-088) GEAR DISAGREE WARNING MESSAGE AFTER TAKEOFF, DURING GEAR RETRACTION, FOLLOWED QRH WITH UNEVENTFUL LANDING. PERFORMED FUNCTIONAL TEST OF LANDING GEAR EXTENSION/ RETRACTION. OPS CHECK GOOD, OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050830001372005083000137GL 2005 8 30 HDNR200500002 220050809A725023073854 TURBINE WHEEL BOLKMS105 BO105CBS 5626008EU ALLSN 250C 250C20B 03013GL ENGINE SEPARATED B HDNAA UNSCHED LANDING DRJINFLIGHT SEPARATION PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SW03911WK377 S753 CAE835284 ENGINE LOST POWER IN FLIGHT. UPON INSPECTION OF THE TURBINE, THE 2ND STAGE TURBINE WHEEL WAS FOUND TO HAVE 1 BLADE MISSING WHICH SUBSEQUENTLY CAUSED SIGNIFICANT FOD DAMAGE TO THE 2ND, 3RD AND 4TH STAGE NOZZLES AND THE 3RD AND 4TH STAGE STAGE WHEELS AS WELL AS OTHER TURBINE SECTION DISTRESS. ALL DAMAGE WAS CONTAINED WITHIN THE TURBINE. THE 1ST AND 2ND STAGE WHEELS AND NOZZLES HAVE BEEN SENT TO MFG FOR INVESTIGATION. 1G72 3U3 UNCH3EU E4CE 20050830001442005083000144NE 2005 8 30 GLBA20050505 220050819A7200PT6A67D ENGINE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE RIGHT SURGES A GLBAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 NM03100GL157943822 UE100 114305 RT ENGINE SURGING 2500-4500 POUND TORQUE ON T/O WITH POWER LEVERS STATIONARY, ABORTED T/O. PERFORMED ENGINE RUN-UP AND OVER TORQUE CHECKS, COULD NOT DUPLICATE ENGINE SURGE, RETURNED TO SERVICE. 2L72 4T4 TRTA24CE E26NE 20050830001452005083000145NE 2005 8 30 REX2005F00039 220050513A7230CF343B1 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 2 FAILED A REXAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 SO258390A8350 7390 (REF NR: 05-064) ON CLIMB OUT, AT ABOUT FL303, THERE WAS A LOUD BANG AND THE NR 2 ENGINE ITT SPIKED. THIS WAS FOLLOWED BY A LOSS OF N1 AND OIL PRESSURE. FLIGHT CREW FOLLOWED THE QRH PROCEDURES AND DECLARED AN EMERGENCY. THE PIC REQUESTED AND RECEIVED PERMISSION TO DIVERT. AN OTHERWISE UNEVENTFUL APPROACH AND LANDING WAS MADE. MAINTENANCE DETERMINED PROBLEM TO BE 2 BROKEN INLET GUIDE VANE ACTUATOR ARMS. THIS ENGINE WAS REMOVED AND WILL BE SENT FOR REPAIR. (K) 2L72 4F4 FRTA21EA E15NE 20050830001472005083000147EU 2005 8 30 XN0A1258 120050818A3610 REGULATOR AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE NR 1 ENGINE FAILED A XN0AA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 GL23224KW 073 ON CLIMBOUT, GOT NR 1 ENGINE TEMP HIGH AND REGUL FAULT LIGHTS. TEMP WAS PEGGED AT 300 DEGREES C. PERFORMED QRH WITH NO CHANGE. LT AND CENTER MANIFOLD LIGHTS CAME ON. REDUCED THROTTLE TO IDLE. TEMP REDUCED AND LIGHTS EXTINGUISHED. REMOVED AND REPLACED NR 1 ENGINE BLEED AIR PNEU REGULATOR IAW MM CHAPTER 36-11-14. LEAK AND OPS CK GOOD. REMOVED AND REPLACED NR 1 ENGINE FAN AIR VALVE IAW MM CHAPTER 36-11-16. LEAK AND OPS CK GOOD. SYSTEM OPS CHECKS GOOD IAW MM CHAPTER 36-11-00. 2L72 4F4 FRTA35EU E23EA 20050830001482005083000148NM 2005 8 30 XN0A1260 120050825A5242 DOOR BOEING727 727227 1384078NM PWA JT8 JT8D9A 52048NE E/E BAY OUT OF ADJUST A XN0AA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL2379754 21363 PILOT REPORT, COULD NOT PRESSURIZE A/C. RE-ADJUSTED EE DOOR IAW MM 52-40-11. 2L73 4F4 F A3WE E2EA 20050830001502005083000150NE 2005 8 30 ASMF200508014 220050825A7200JT8D219 ENGINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE RIGHT MAKING METAL W ASMFO OTHER J WARNING INDICATION APAPPROACH 1 SW23161PL3778924327 49764 CAPTAIN REPORTED THAT DURING APPROACH RT ENGINE REACHED 101 PERCENT OF N1. DURING MAINTENANCE REVISION, WAS DETECTED METAL CHIPS IN THE RT ENGINE GEARBOX. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT CHECK, THE RT ENGINE WAS REPLACED IAW MM 71-00-02, TESTED CORRECT. 2L72 4F4 FRTA6WE E9NE 20050831000042005083100004NM 2005 8 31 2005UALA00860 120050822A33977945243 WIRE BOEING747 747422 1384935NM PWA 4056 PW4056 NE 3A, 34C, 54C & 6INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29198UA 28716 EEL INOPERATIVE AT 3A, 34C, 54C, 61C. REPAIRED CONNECTOR. 2L74 4F4 FRTA20WE E24NE 20050831000052005083100005NM 2005 8 31 2005UALA00861 120050822A3397794640 WIRE BOEING747 747422 1384935NM PWA 4056 PW4056 NE ROW 26B DISCONNECTED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29198UA 28716 EEL INOPERATIVE, AFT MOST LT CROSS AISLE, AT DR 5L & ROW 26B. FOUND CONNECTOR DISCONNECTED. RESECURED CONNECTOR. 2L74 4F4 FRTA20WE E24NE 20050831000062005083100006NM 2005 8 31 2005UALA00862 120050822A33977945243 WIRE BOEING747 747422 1384935NM PWA 4056 PW4056 NE ROW 61R INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29198UA 28716 EEL INOPERATIVE ROW 61R & LT AISLE NEAR DOOR 1L. REPAIRED CONNECTOR. 2L74 4F4 FRTA20WE E24NE 20050831000072005083100007NM 2005 8 31 2005UALA00863 120050822A3350362624 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE RT OVRWING INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29198UA 28716 EMERGENCY LIGHT INOPERATIVE, RIGHT OVERWING TOP ASSY & 1EA STAIR ILLUM AFT CREW REST. REPLACED EEL LAMP. 2L74 4F4 FRTA20WE E24NE 20050831000082005083100008NM 2005 8 31 05FDEA02709 120050829A5320 FLOOR SUPPORT BOEING727 727227 1384078NM BS 268 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 CORROSION ON COCKPIT FLOOR STRUCTURE BS 268 LBL 8 WL 207. REMOVED FABRICATED AND INSTALLED WEB AND TEE CHORD IAW SRM 51-30-3, 51-30-6 AND 51-10-3. 2L73 4F A3WE 20050831000092005083100009NM 2005 8 31 05FDEA02711 120050829A5320 FLOOR SUPPORT BOEING727 727227 1384078NM BS 266 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 CORROSION ON COCKPIT FLOOR STRUCTURE BS 266 LBL 2 WL 207. REMOVED, FABRICATED AND INSTALL REPAIR PER SRM 51-20-1 2L73 4F A3WE 20050831000102005083100010WP 2005 8 31 05FDEA02713 120050829A5330 SKIN DOUG MD10 MD1010F 3022112WP ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25396FE 46630 SKIN BULGING AT RIVETS, POSSIBLE CORROSION AND STRESS CRACK CORROSION. REMOVED FUSELAGE SKIN WITH CORRODED AREAS FROM FS 775-879 STR 50L-50R AND REPLACED WITH NEW SKIN PANEL PER SRM. PASSED LEAK CHECK TEST ON REPLACED AREA. 2L73 4F RTA22WE 20050831000112005083100011NM 2005 8 31 05FDEA02714 120050830A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 UPPER CARGO, SEAT TRACK RBL 27 CRACKED AT STA 630. UPPER CARGO STA 625 TO STA 665 RBL 27 SEAT TRACK REPAIRED AS PER SRM 53-70-00 VOLUME I FIGURE 1. THIS REPAIR IS CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050831000132005083100013NM 2005 8 31 SB05103 120050830A33501012721 LIGHT BOEING737 737301 1384611NM SEAT ROW 13 INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19353US 23556 CLT - MAINTENANCE REPORTED THE CABIN SEAT MOUNTED EMERGENCY LIGHT AT SEAT ROW 13 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050831000142005083100014NM 2005 8 31 2005UALA00864 120050821A33501317 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29121UA 29167 EMERGENCY CEILING LIGHTS INOPERATIVE AT UPPER DECK DOOR AFT, ROW 16, ROW 17 & JUST AFT OF ROW 18. RELAMPED EMERGENCY CEILING LIGHT. 2L74 4F4 FRTA20WE E24NE 20050831000162005083100016NM 2005 8 31 2005UALA00866 120050821A33501317 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE LT OVERWING INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29121UA 29167 LEFT OVERWING EMERGENCY LIGHT ASSEMBLY 2ND FROM FWD INOP. REPLACED LAMP. 2L74 4F4 FRTA20WE E24NE 20050831000172005083100017NM 2005 8 31 2005UALA00867 120050822A5315 FLOORBEAM BOEING737 737322 1384676NM BS 947 CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29327UA 24147 CABIN FLOORBEAM TOP CORRODED IN SEVERAL PLACES. 2L72 4F RTA16WE 20050831000182005083100018NM 2005 8 31 2005UALA00868 120050822A5310 SUPPORT BOEING737 737322 1384676NM E/E DOOR WORN A UALAK NONE O OTHER ININSP/MAINT 1 WP29327UA 24147 EE ACCESS DOOR CUTOUT, RT DOOR CUTOUT, SUPPORT FRAME STR 27R STA 338 IS WORN ABOVE DOOR LATCH FITTING. 2L72 4F RTA16WE 20050831000192005083100019NM 2005 8 31 2005UALA00869 120050822A5315 FLOORBEAM BOEING737 737322 1384676NM BS 294.5 LBL 7 CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29327UA 24147 CABIN FLOOR, STA 294.5 LBL 7, FLOORBEAM UPPER SURFACE, CORROSION. 2L72 4F RTA16WE 20050831000202005083100020NM 2005 8 31 2005UALA00870 120050822A5753 SKIN BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE LT WING FLAP PUNCTURED A UALAK NONE O OTHER ININSP/MAINT 1 WP29217UA 30550 LEFT WING INBOARD FLAP, INBOARD SECTION ON LOWER SURFACE, SKIN IS PUNCTURED ON FOREFLAP. DAMAGE FOUND ON THE LOWER SKIN ON THE FLAP WAS AN ISOLATED INCIDENT BUT WILL BE FILED FOR FUTURE REFERENCE OF SIMILIAR FINDINGS. A 200 DEGREE FAHRENHEIT, WET LAY-UP REPAIR WAS PUT IN PLACE TO REPAIR THE PUNCTURE ON THE FOREFLAP, PER TIMCO REO (EVA) G10875, REV-A. 2L72 4F4 FRTT0001SE E46NE 20050831000212005083100021NM 2005 8 31 2005UALA00871 120050823A3350362624 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29173UA 24380 EMERGENCY LIGHT AT 4A AND 50 ABC INOP. REPLACED EEL LAMP. 2L74 4F4 FRTA20WE E24NE 20050831000232005083100023NM 2005 8 31 2005UALA00873 120050822A2721 TRIM SYSTEM BOEING737 737322 1384676NM RUDDER MALFUNCTIONED A UALAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 WP29304UA 23665 EXCESSIVE RUDDER AND TRIM, NEEDED 4 UNITS LT RUDDER TRIM AND 3 UNITS LWD TRIM PLUS YOKE INPUT, TO MAINTAIN WINGS LEVEL. EMERGENCY EQUIPMENT REQUESTED. A BROKEN NR 6 SPOILER CONTROL CABLE (WSB2-4) INHIBITED FLIGHT SPOILER MOVEMENT OF THE NR 6 SPOILER CREATING AN ASYMMETRICAL AIR LOAD ON THE WING SURFACES. THE SUBJECT CONTROL CABLE WAS REPLACED, RIGGED, AND TESTED PER 737 MM 27-61-00 AND ALL CHECKED GOOD. THIS IS CONSIDERED AN ISOLATED INCIDENT. CLEANED AND LUBRICATED AT EVERY 'C' CHECK AND REPLACED AT A 2 HMV FREQUENCY. THERE IS NO HISTORY OF PREVIOUS FAILURES OF THIS OR OTHER FLIGHT CONTROL CABLES AT SIMILAR LOCATIONS. 2L72 4F RTA16WE 20050826000042005082600004SO 2005 8 26 RAIA00508031 120050822A3397 CONNECTOR EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT UNSECURE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03812HK 145373 EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE SECURED THE CONNECTOR. OPS CHECKED GOOD. 2L72 4T4 FRTT00011ATTE6CH 20050826000262005082600026NM 2005 8 26 SB05097 120050823A335020121 CHARGER BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU AFT CABIN INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU 23706 MAINTENANCE REPORTED THE BATTERY CHARGER FOR THE AFT ENTRY DOOR EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY. OPS CHECK GOOD. 2L72 4F4 FRTA16WE E21EU 20050826000392005082600039WP 2005 8 26 05FDEA02624 120050824A5712ARB128712 RIB DOUG DC10 DC1010 3022110WP GE CF6 CF66K 30020NE ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 RT WING FIXED LEADING EDGE AT XORS 454 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM. 2L73 4F4 F A22WE E23EA 20050826000452005082600045NM 2005 8 26 USAA051046 120050823A53206547952183 THRESHOLD BOEING737 737301 1384611NM CARGO DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US 23933 AFT CARGO DOOR MOST FWD THRESHOLD HAS CRACK. WELDED CRACK IAW BOEING PROCESS SPEC BAC 5975, DEFECT SIZE: .75 INCH. 2L72 4F RTA16WE 20050826000652005082600065NM 2005 8 26 SWAA052557 120050824A53116520723 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29612SW 27930 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 492, STR 24R. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20050826000802005082600080NM 2005 8 26 05FDEA02636 120050824A5314 KEELBEAM BOEING727 727227 1384078NM BS 874 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 UPPER FLANGE ON KEELBEAM, IS CRACKED AT FASTENER HOLE, STA 874, LBL 6. FABRICATED & INSTALLED STEEL DOUBLER AT BS 870 LBL 6 PER ECA 7-5310-70687 AND BOEING SERVICE BULLITEN 727-53-0208. 2L73 4F A3WE 20050826000882005082600088WP 2005 8 26 05FDEA02655 120050825A5712 RIB DOUG DC10 DC1010 3022110WP ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LT WING FIXED LEADING EDGE AT XORS 509 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 3, 4 VOL I AND INSTALLED ANGLE REPAIR. 2L73 4F A22WE 20050826000932005082600093WP 2005 8 26 05FDEA02643 120050825A5712ARB129241 RIB DOUG DC10 DC1010 3022110WP ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LT WING FIXED LEADING EDGE AT XORS 809 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 4, 6 VOL I. 2L73 4F A22WE 20050829000072005082900007NM 2005 8 29 EIA2005138 120050712A5311 FRAME BOEING747 747230B 1384889NM BS 2231 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09487EV 23286 FRAME STA 2231 STR 24L CRACK IN WEB INNER STRAP. REPAIRED CRACK AT STA 2231 WEB CUT OUT BETWEEN STR 24L AND 25L PER B747 SRM 53-10-01 FIG 1 DETAIL 1 AND ECRA 487-53-018-2. 2L74 4F A20WE 20050829000082005082900008NM 2005 8 29 EIA2005139 120050712A5315 FLOORBEAM BOEING747 747230B 1384889NM BS 280 DAMAGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09487EV 23286 FLOORBEAM WEB REPAIR BUCKLED AT STA 280 RBL 45. REPAIRED FLOORBEAM WEB STA 280 RBL 45 PER ECRA 487-53-010-2. 2L74 4F A20WE 20050829000132005082900013 2005 8 29 DXTA200500913 420050818A2210 AUTOPILOT SYS CESSNA750 750 2076810CE MALFUNCTIONED E DXTAO OTHER P NO WARNING INDICATION DEDESCENT 1 GL07913QS 7500113 ARRIVING 180 KNOTS, AUTO-PILOT REPEATEDLY CAME OFF-LINE. ELEV FELT HEAVY ON CONTROLS. AT 140 KNOTS, PRIMARY TRIM WOULD NOT WORK. NO CAS MESSAGES RECEIVED EXCEPT WHEN SECONDARY TRIM ARMED. SECONDARY TRIM NOT ATTEMPTED. DOWNLOADED FAULT HISTORY FROM IAC NR 1&2. FOUND NO AP FAULTS DETECTED. PERFORMED PRIMARY TRIM CHANNEL A & B TRAVEL VERIFICATION OPS CK GOOD IAW MM. PERFORMED AP OPS CHECK IAW MM. OPS CK GOOD. 2L72 4J RTT00007WI 20050829000352005082900035EU 2005 8 29 DHL2005366501 120050725A5347F0581021 SEAT TRACK AIRBUS300 A300B4203 3930306EU COCKPIT CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01366DH 249 DURING C-CHECK, COCKPIT SEAT TRACK WORN OUT OF LIMITS AT COPILOT SEAT AFT O/B, FLIGHT ING AND FWD TRACK FOR FIRST OBSERVER SEAT. REMOVED AND REPLACED COCKPIT TRACKS AT COCKPIT; AFT O/B,FLIGHT ING: O/B TRACK AND FIRST OBSERVER; FWD TRACK AS PER A-300 M/M 53-41-11 P/N F05-810-21, F 06-228-129; F06-159-20. 2L72 4F RTA35EU 20050829000402005082900040EU 2005 8 29 YENA200554 120050824A3350324131 BATTERY AIRBUS320 A320232 3930326EU EMERGENCY LIGHT FAILED A YENAO OTHER O OTHER CRCRUISE 1 EA15571JB45 2125 RIGHT OVERWING EMERGENCY EXIT DOOR LIGHT INOP. REPLACED RIGHT EMERGENCY BATTERY PACK IAW 33-51-38. 2L72 4F RTA28NM 20050829000412005082900041WP 2005 8 29 05FDEA02649 120050825A5712 RIB DOUG DC10 DC1010 3022110WP LT WING CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25556FE 46710 LT WING FIXED LEADING EDGE AT XORS 656 FOUND NR 1 RIB CRACK. ACCOMPLISH FORMER REPAIR IAW SRM 57-20-00 FIG 1 SHEET 1, 3, 4 VOL I AND INSTALLED ANGLE REPAIR. 2L73 4F A22WE 20050829000482005082900048NM 2005 8 29 EIA2005147 120050712A5410 ACCESS PANEL BOEING747 747230B 1384889NM NR 3 NACELLE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09487EV 23286 A CRACK WAS FOUND ON NR 3 ENG, RT CORE COWL AT LOCATION OF ACCESS PANEL 473AR. REMOVED PREVIOUS REPAIRS, FAF0581021BBED NEW REPAIR PARTS AND INSTALLED PER ECRA 487-54-016-2.B 2L74 4F A20WE 20050829000662005082900066NM 2005 8 29 05FDEA02578 120050819A5343 FITTING DOUG MD11 MD11 3023602NM ZONE 700 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 EVIDENCE OF SURFACE CORROSION FOUND ON CENTER LANDING GEAR RIGHT TRUNNION FITTING LOWER MATING SURFACE AREA. SURFACE CORROSION ON CENTER LANDING GEAR RIGHT HAND TRUNNION FITTING LOWER MATING SURFACE AREA REMOVED AS PER SRM 51-21-01 VOLUME II PAGE 27. ORIGINAL THICKNESS = 2.650", MATERIAL REMOVED = 0.011", MATERIAL REMAINING = 2.639" FOUND WITHIN LIMITS AS PER SRM 53-40-00 VOLUME I FIGURE 15. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050829000792005082900079NM 2005 8 29 UPS05245265 120050805A5320 STIFFENER BOEING727 72730C 1384009NM BS 870 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919UP 19012 LT MLG W/W, EVIDENCE OF CORROSION ON BS 870 VERTICAL STIFFENER AND ATTACH CLIP AT LB 145. CEILING AREA. REPAIR CARRIED OUT IAW SRM 51-30-2 & 51-10-2, 51-10-1. 2L73 4F A3WE 20050829000812005082900081NE 2005 8 29 ABXA050202 220050824A73218063505 FUEL CONTROL BOEING767 767281 1385109NM GE CF6 CF680A 30025NE RIGHT ENGINE DEFECTIVE A ABXAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 GL23786AX808 23019 580234 ON TAKEOFF ROLL, RIGHT ENGINE FAILED TO PRODUCE TAKEOFF POWER. WITH LEFT ENGINE ACCELERATING NORMALLY. RIGHT ENGINE STOPPED ACCELERATING AT 58 PERCENT N1. REMOVED AND REPLACED RIGHT ENGINE MAIN ENGINE CONTROL IAW B767 AMM 73-21-01-4. PERFORMED ENGINE RUN, SYSTEM CHECKED GOOD. 2L72 4F4 FRTA1NM E13NE 20050829000982005082900098 2005 8 29 SWAA052559 420050824A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050829001012005082900101NM 2005 8 29 SWAA052562 120050825A335065C34691 LIGHT BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 BULLNOSE EMERGENCY EXIT LIGHT ASSY LOOSE AT ROW 17 ABC. SECURED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20050829001052005082900105NM 2005 8 29 SWAA052566 120050823A53136551698 SPLICE BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29503SW 24180 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER SPLICE CRACKED AT BS 908, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20050829001092005082900109EA 2005 8 29 VTZA200500150 120050823A2751 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS OUT OF RIG A VTZAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 EA27648BR 7406 FLAPS FAIL AT ZERO. PERFORMED RIGGING OF LT AND RT BPSU'S. 2L72 4F RTA21EA 20050829001202005082900120NM 2005 8 29 05FDEA02663 120050826A57406089318 BRACKET BOEING727 727200 138407ENM LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25478FE 21395 LT WING BRACKET BROKEN INSIDE ACCESS PANEL 8405. REMOVED AND REPLACED BROKEN BRACKET IAW SRM 51-10-1 AND SRM 51-30-2. 2L73 4F RTA3WE 20050829001342005082900134NM 2005 8 29 USAA051051 120050824A5542 SKIN BOEING737 7374B7 1384702NM RUDDER DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19449US 24893 RUDDER LT SIDE MID SECTION AREA HAS DELAMINATION. COMPOSITE REPAIR IAW SRM 51-70-05, DEFECT SIZE: 2 INCHES. 2L72 4F RTA16WE 20050829001452005082900145NM 2005 8 29 SB05098 120050824A335020131A BATTERY PACK BOEING737 7373B7 1384580NM EMERGENCY LIGHT DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19389US 23311 PIT - MAINTENANCE REPORTED THE SEAT MOUNTED EMERGENCY LIGHTS FROM SEAT ROWS 11-16, LEFT-HAND SIDE, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050829001492005082900149WP 2005 8 29 ARWA20050804 120050818A27603644322 CRANK ASSY DOUG DC8 DC862F 3021972WP PWA JT3D JT3D7 52039NE LT ACTUATOR BROKEN A ARWAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO19791AL 46150 WHEN POWER SET FOR TAKEOFF, TAKEOFF WARNING HORN SOUNDED AND SPOILER EXTENDED LIGHT ILLUMINATED. REMOVED AND REPLACED BROKEN GROUND SPOILER ACTUATION CRANKS IAW MM; RE-SAFETIED ALL PREVIOUSLY REMOVED HARDWARE. PERFORMED FUNCTIONAL CHECK OF GROUND SPOILERS PANEL, AND WARNING LIGHT FOUND TO OPERATE NORMALLY. 2L74 4F4 F 4A25 1E8 20050829001592005082900159SO 2005 8 29 SWIA200515460 120050823A27503472001001 CONTROL UNIT EMB 120 EMB120ER 3260203SO TE FLAP MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 NM07214SW6538 6538 120280 ABOVE 160 KTS DURING FLAP RETRACTION OUTBOARD FLAPS DISAGREE (FLAP ON MAP, DISAGREEMENT ON OVERHEAD). REPLACED FLAP CONTROL UNIT IAW A/C MM 27-50-06, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050829001602005082900160 2005 8 29 SWIA200515461 420050824A34183995100208 STICK SHAKER CNDAIRCL600 CL6002B19 1900309EA STALL WARNING MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED DEDESCENT 1 NM07948SW 7789 DURING DESCENT THROUGH 10,000 FT, AT 230 KIAS, STICK SHAKER ACTIVATED AND AUTOPILOT DISENGAGED. REPLACED STALL PROTECTION COMPUTER PER MM 27-35-01 TASK 27-35-01-710-801, 27-35-01-750-801, 27-35-01-750-802, 27-35-750-803, 27-35-01-720-801. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050829001772005082900177NM 2005 8 29 USAA051042 120050823A5530 BUSHING BOEING737 737301 1384611NM VERTICAL FIN CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US 23933 VERTICAL FIN, AFT MOUNT LUGS LT SIDE BUSHINGS, FWD FACE CORRODED. REMOVED CORROSION, FABRICATED AND INSTALLED BUSHINGS IAW BOEING DWGS 69-72039 & 65-52274 DEFECT SIZE: 1 X 2 INCH AREA. 2L72 4F RTA16WE 20050829001792005082900179SO 2005 8 29 MASA200500517 120050704A3350 LIGHT EMB 145 EMB145LR 3260212SO ROWS 8-12 INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07835MJ 145353 ASH 2748 CLT. THE CREW HAD THE EMERGENCY FLOOR PROX LIGHTS INOP FROM ROWS 8 TO 12. MX OPERATED THE SYSTEM AND COULD NOT DUPLICATE DISCREPANCY. A/C DEPARTED WITHOUT FURTHER INCIDENT. 2L72 4T RTT00011AT 20050829001832005082900183EA 2005 8 29 MASA200500566 120050718A3397 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT LOOSE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0727172 7172 ASH 2652 PHL. FLOOR LEVEL EMERGENCY LIGHT STRIP INOP. MX SECURED CONNECTOR TO LIGHT STRIP. NO FURTHER DEFECTS NOTED. 2L72 4F RTA21EA 20050829001882005082900188EA 2005 8 29 MASA200500621 120050807A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0717175 7175 ASH 7165 IAD. NUMEROUS EMERGENCY EXIT FLOOR LIGHTING STRIPS INOP. MAINTENANCE RESET AND OPS CHECKED GOOD. 2L72 4F RTA21EA 20050829002052005082900205NM 2005 8 29 SWAA052573 120050824A33507003661 BALLAST BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 DURING SCHEDULED A2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BALLAST PER MM. 2L72 4F RTA16WE 20050829002092005082900209NM 2005 8 29 SWAA052577 120050825A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 767 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29369SW 26580 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 767, STR 27R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050829002172005082900217CE 2005 8 29 1050812038 120050824A5720 STRUCTURE BEECH 1900 1900D 1154162CE LT WING CORRODED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07143YV UE143 LT COLLECTOR TANK CORROSION AND SURFACE CORROSION AROUND DRAINS. MORE INFORMATION WILL BE AVAILABLE AT A LATER DATE. 2L72 4T RTA24CE 20050830000222005083000022NM 2005 8 30 DXTA200500933 120050828A3241606568 TRANSDUCER GULSTM200 200 4500308NM ANTI SKID SYS INOPERATIVE E DXTAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 GL07707QS2090 066 " ANTI-SKID OFF " LIGHT ILLUMINATED DURING TAXI OUT, PRESSED TO RESET AND APPROX 1 MIN LATER IT ILLUMINATED, CYCLED ANTI-SKID CB'S AND IT AGAIN ILLUMINATED AND CONTINUED TO CYCLE ON /OFF APPROX EVERY MIN. REMOVED TRANSDUCER ON NR 4 WHEEL P/N: 606568 S/N: OLT01-0824 AND INSTALLED REPAIRED TRANSDUCER P/N: 606568 S/N: MAR02-0906. OPS CHECK GOOD. 2L72 4F RTA53NM 20050830000242005083000024CE 2005 8 30 DXTA200500930 120050826A3240 BRAKE ASSY CESSNA500 560CESSNA 2076750CE MLG MALFUNCTIONED E DXTAO OTHER S AFFECT SYSTEMS LDLANDING 1 GL07375QS 5600375 FOLLOWING LANDING ROLL OUT AND SEVERAL BRAKE APPLICATIONS BRAKES WILL GO SOFT AND NOT RESPOND. PUMPING BRAKES RESTORES NORMAL BRAKE FUNCTION. BLEED BRAKES IAW CE 560 CHAPTER 32-42-00. OPS CHECK GOOD. 2L72 4F RTA22CE 20050830000252005083000025NM 2005 8 30 DXTA200500925 120050825A2910 HYDRAULIC SYSTEM AMD FALC50FALCON2000 2730170NM NR 1 LEAKING E DXTAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL07277QS 177 COMPLETE LOSS OF THE NR 1 HYDRAULIC SYSTEM IN FLIGHT AT FL410. HYD QTY DROPPED TO 15 PERCENT, PRESSURE FELL TO 100PSI. UPON LANDING HYDRAULIC FLUID NOTED ALL OVER BELLY OF ACFT AND COVERING INSIDE OF "HELLHOLE" COMPLIED WITH NORMAL AND ABNORMAL CHECKLIST PER AFM. 2K73 4F RTA50NM 20050830000552005083000055NM 2005 8 30 SWAA052583 120050824A53306545776 SKIN BOEING737 7373H4 1384600NM BS 920 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 920, STR 25R. MX FERRY TO DALLAS. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050830000572005083000057NM 2005 8 30 SWAA052585 120050824A53306545766 SKIN BOEING737 7373H4 1384600NM BS 460 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 460, STR 17R. MX FERRY TO DALLAS. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050830000662005083000066NM 2005 8 30 SWAA052594 120050826A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 360 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29617SW 27700 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050830000692005083000069SO 2005 8 30 SIMA200521614 120050804A335020131A BATTERY PACK EMB 135 EMB135KL 3260302SO EMERGENCY LIGHTSDISCHARGED A SIMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW21833AE 145629 SGF - FLT 3788 - ENTRY, GALLEY DOOR, ROW 1 THROUGH ROW 8 AND LEFT EMERGENCY LIGHTS DO NOT ILLUMINATE. REPLACED EMERGENCY BATTERY PACKS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050830000712005083000071EA 2005 8 30 A6WA200540283 120050813A5270 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA PAX DOOR ACTIVATED A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31413AW 7585 PASSENGER DOOR MASTER CAUTION AND AURAL `DOOR` CAME ON AFTER TAKEOFF AT APPROXIMATELY 500 AGL. COMPLIED WITH QRH AND RETURNED TO LAND. INTERROGATED PSEU, FOUND CODES D116, D117 AND D113. ALL INDICATIONS NORMAL. ALL ALIGNMENT MARKS NORMAL. NO FAULTS NOTED. (M) 2L72 4F RTA21EA 20050830000732005083000073EA 2005 8 30 A6WA200540288 120050812A5310 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA CARGO DOOR CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31465AW 7893 CARGO DOOR SUPPORT BEAM MEMBER ANGLE, P/N 601R35050-109, CRACKED AT PRESSURE BULKHEAD FS 621, LBL 34.42. FABRICATED NEW CARGO DOOR SUPPORT BEAM ANGLE IAW CRJ200 SRM 51-30-06 AND BOMBARDIER DRAWING NR 601R35050, INSTALLED ANGLE IAW CRJ200SRM 51-42-21. (M) 2L72 4F RTA21EA 20050830001172005083000117WP 2005 8 30 05FDEA02682 120050826A5753 SKIN DOUG DC10 DC1010 3022110WP ZONE 600 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 RT WING I/B FLAP STRUCTURE AT XIFH 195.300 TO XIFH 189.300 FOUND DENT IN THE LWR EXTERNAL SKIN DIAMETER 2.36 INCH BY .275 INCH DEEP AND FOUND DEFORMATION ON STRUCTURE. CUT DAMAGE SECTION OF SKIN; CHECKED AND REPAIR IAW SRM 57-00-01 FIG 4 SHEET 2 VOL I. 2L73 4F A22WE 20050830001192005083000119WP 2005 8 30 05FDEA02684 120050826A5320 CHANNEL DOUG DC10 DC1010 3022110WP BS 959-979 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 FWD CARGO COMPT FOUND HEAVY CORROSION BETWEEN STA 959-979 WITH CRACK LONG 4 INCH. CUT DAMAGE SECTION ON CHANNEL AND REPAIRED IAW SRM 53-70-00 FIG 7 VOL I. 2L73 4F A22WE 20050830001212005083000121NM 2005 8 30 05FDEA02698 120050828A5347 SEAT TRACK DOUG MD11 MD11F 3023600NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 UPPER CARGO, SEAT TRACK RBL 27 CRACKED AT STA 6-30. REMOVED AS PER SRM 53-70-00 VOLUME I FIGURE 1. NEW TRACK AND SPLICE FABRICATED AS PER SRM 53-70-00 VOLUME I FIGURE 1. NEW TRACK AND SPLICE INSTALLED AS PER SRM 53-70-00 VOLUME I FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2L73 4F RTA22WE 20050830001232005083000123NM 2005 8 30 05FDEA02700 120050828A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 UPPER CARGO, SEAT TRACK RBL 11 CORRODED AT STA 1121 TO STA 6-10. REMOVED AS PER SRM 51-31-01 VOL 2. NEW SEAT TRACK AND SPLICE FABRICATED AS PER SRM 53-70-00 VOL 1 FIG1. NEW SEAT TRACK AND SPLICE INSTALLED AS PER SRM 51-35-01 VOL 2. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050830001252005083000125NM 2005 8 30 05FDEA02702 120050828A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 UPPER CARGO, SEAT TRACK RBL 47 CRACKED AT STA 939 TO STA 979. REMOVED AS PER SRM 53-70-00 VOL1 FIG1. NEW TRACK AND SPLICE REWORKED AS PER SRM 53-70-00 VOL 1 FIG1. NEW TRACK AND SPLICE INSTALLED AS PER SRM 53-70-00 VOL1 FIG 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050830001322005083000132EA 2005 8 30 SWIA200515470 120050826A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLT SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07592SW9901 9901 7279 FLIGHT SPOILERS FAULT STATUS MSG ON ED2. REPLACED RIGHT NR 2 OUTBOARD FLIGHT SPOILER PCU IAW MM 29-62-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050830001362005083000136NM 2005 8 30 PCSA823200501 120050823A5210 DOOR BOEING727 727225 1384077NM PWA JT8 JT8D217C 52053NE L-1 MISALIGNED A PCSAA UNSCHED LANDING O OTHER CLCLIMB 1 SO29604AJ 21453 ON CLIMBOUT, AIRCRAFT WOULD NOT PRESSURIZE, CREW REPORTED LOUD AIRFLOW NOISE COMING FROM CABIN. AIRCRAFT RETURNED TO DEPARTURE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE L-1 MAIN CABIN ENTRY DOOR AFT END OF DOOR WITH A GAP, THE L-1 DOOR WAS ADJUSTED AND RIGGED IAW MM CH 52-11-01 OPERATIONAL CHECK NORMAL, DECAY CHECK ACCOMPLISHED IAW. WORKCARD 829, DECAY NORMAL AND PRESSURIZATION CHECK IAW MM CH 5-51-101 WAS NORMAL. A OVERWEIGHT LANDING INSPECTION WAS ACCOMPLISHED IAW MM CH 5-51-271 NO DEFECTS NOTED, AIRCRAFT WAS RETURNED TO SERVICE. 2L73 4F4 F A3WE E9NE 20050830001392005083000139CE 2005 8 30 1050617008 120050823A7830 FLANGE BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA THRUST REVERSER WORN A AMWAK NONE O OTHER ININSP/MAINT 1 CE07173YV UE173 LT UPPER TURTLEBACK FLANGE WORN. CRACKED ON IB EDGE. MORE INFORMATION WILL BE AVAILABLE AT A LATER DATE. 2L72 4T3 TRTA24CE E2NE 20050830001412005083000141NM 2005 8 30 05FDEA02688 120050826A5260 WARNING LIGHT BOEING727 7272S2F 1384O81NM AIRSTAIR ILLUMINATED A FDEAE ENGINE SHUTDOWN J WARNING INDICATION TOTAKEOFF 1 SO25209FE 22931 JUST AT BRAKE RELEASE AN "AFT AIRSTAIR" LIGHT ILLUMINATED. TAKEOFF WAS REJECTED. RTO CHECKLIST WAS ACCOMPLISHED. REJECTED TAKEOFF PARAMETERS, AIRSPEED <50 KIAS, EPR NR 1 NR 3 1.83, NR 2 1.75. TAKEOFF TIME 02:18. RELEASED FOR SERVICE PER MEL/CDL: 52-06-B. CREW COMMENTED NO PROBLEMS WITH AFT A/S WARNING LIGHT SYS LAST TWO LEGS. INSPECTED ALL UP LOCK & INTERIOR HANDLE SWITCHES & TESTED SYS SEVERAL TIMES IAW B727MM 52-70-001-5. 2L73 4F A3WE 20050830001462005083000146WP 2005 8 30 05FDEA02686 120050826A5730CODE515BT ACCESS PANEL DOUG DC10 DC1010 3022110WP ZONE 500 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LEFT WING ACCESS PANEL FOUND HARDWARE ON EXTERNAL SKIN WITH HOLE WORN. REPAIR WITH DOUBLER IAW SRM 57-00-01 FIG 4 SHEET 2 VOL I. 2L73 4F A22WE 20050831000032005083100003NM 2005 8 31 2005UALA00859 120050819A339758781 WIRE BOEING737 737522 138449FNM CFMINTCFM56 CFM562AFR 13802EU ROW 15 FAILED A UALAK NONE O OTHER ININSP/MAINT 1 WP2942UA 26679 EEL LIGHTS FROM ROW 15 BACK INOP. INSTALLED SERVICEABLE EEL LEAD FOR FAILED SECTION. 2L72 4F4 FRTA16WE E21EU 20050831000122005083100012NM 2005 8 31 183 120050824A5347 SEAT TRACK BOEING757 757232 1384965NM BS 460 DAMAGED A K NONE O OTHER ININSP/MAINT 1 SO15672DL480 25977 OB SEAT TRACK HAS SEVERAL ELONGATED HOLES FROM BS 460 TO 480. 2L72 4F RTA2NM 20050831000242005083100024NE 2005 8 31 2005UALA00874 220050819A7200 ENGINE BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 1 SMOKE A UALAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 WP29565UA 26669 727114 OBSERVED SMOKE FROM BOTTOM OF NR 1 ENGINE COWLING ON TAXI INTO ORD. LINE MAINTENANCE DETERMINED THAT HYDRAULIC FLUID WAS LEAKING FROM A LOOSE B-NUT. B-NUT WAS TIGHTENED AND SYSTEM WAS CHECKED. NO OTHER LEAKS NOTED. 2L72 4F4 FRTA2NM E17NE 20050831000262005083100026NM 2005 8 31 05FDEA02715 120050830A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 UPPER CARGO, SEAT TRACK RBL 11 CRACKED AT STA 630. REMOVED AS PER SRM 53-70-00 VOL I FIG 1. NEW TRACK REWORKED AND INSTALLED AS PER SRM 53-70-00 VOL I FIG 1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050831000282005083100028NM 2005 8 31 05FDEA02717 120050830A29106517840492 TUBE BOEING727 727233 138408ANM ZONE 500 CHAFED A FDEABA EMER. DESCENT UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 SO25222FE 20933 HYD SYS A FAILED (W/FLAPS 15) WHILE CONFIGURING TO LAND AT MEM. REPLACED ENGINES NR 1 AND 2 ENGINE DRIVEN HYDRAULIC PUMPS, REF MM29-11-041-2. REPLACED BOTH CASE DRAIN FILTERS. REPLACED SYSTEM "A" HYDRAULIC RETURN FILTER, R/I. REMOVED AND REPLACED SYSTEM A HYDRAULIC PRESS FILTERS. REMOVED AND REPLACED SYSTEM A SPOILER 3 PRESS AND RET LINES IAW SMP. PERFORMED LEAK CK OF ALL CHANGED COMPONENTS. LK CKS GOOD. RAN 12 ENGINES PER JRH CHAP 5 AND PERFORMED OP AND LK CHK OF SYSTEM A ENG DRIVEN PUMPS. OPS AND LK CHECKS GOOD. 2L73 4F RTA3WE 20050831000292005083100029NM 2005 8 31 SWAA052601 120050829A335065C34691 LIGHT BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29315SW 23337 EMERGENCY BULLNOSE LIGHT LOOSE AT ROW 8 DEF. SECURED LIGHT PER MM. 2L72 4F RTA16WE 20050831000302005083100030NM 2005 8 31 SWAA052602 120050828A53306545774 SKIN BOEING737 7373H4 1384600NM BS 750.5 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750.5, STR 19L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050831000332005083100033NM 2005 8 31 05FDEA02710 120050829A5310 SUPPORT BOEING727 727227 1384078NM COCKPIT FLOOR CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 CORROSION ON COCKPIT FLOOR STRUCTURE BS 268 LBL 8 WL 207. REMOVED FABRICATED AND INSTALLED WEB AND TEE CHORD IAW SRM 51-30-3, 51-30-6 AND 51-10-3. 2L73 4F A3WE 20050831000342005083100034NM 2005 8 31 SWAA052610 120050829A53116546593 FRAME BOEING737 7373H4 1384600NM BS 500A CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29617SW 27700 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L TO STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050831000352005083100035NM 2005 8 31 SWAA052611 120050829A53116546555 FRAME BOEING737 7373H4 1384600NM BS 867 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29617SW 27700 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L TO STR 9L AND STR 8R TO STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050831000372005083100037NM 2005 8 31 CALA0500284 120050826A21216454051 FAN BOEING737 737824 13844BZNM FWD BAG BIN INOPERATIVE A CALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW273620716149 30579 ELECTRICAL ODOR & SMOKE FROM THE LT OVERWING EXIT AREA DURING CLIMBOUT OF EWR AND THE ODOR COULD BE SMELLED IN THE COCKPIT. THE AIRCRAFT WAS DIVERTED TO PHL. SMOKE STOPPED ON DESCENT & STARTED AGAIN ON APPROACH. ACFT LANDED WITHOUT INCIDENT. MAINTENANCE UNABLE TO DUPLICATE FAILURE DURING AN ENGINE RUN. THE RT RECIRCULATION FAN (AIR DISTRIBUTION FAN) WAS REMOVED AND REPLACED ALONG WITH THE RT AIR FILTER. THE ELECTRICAL ODOR CONTINUED SO THE LT AIR DISTRIBUTION FAN AND HEPA FILTER WERE ALSO REMOVED AND REPLACED. BOTH AIR DISTRIBUTION FANS WERE TESTED AT THE VENDOR AND PASSED ALL PHASES OF FUNCTIONAL TESTING. NO PROBLEM COULD BE CONFIRMED WITH EITHER UNIT. 2L72 4F RTA16WE 20050831000382005083100038SO 2005 8 31 CHQA200500153 120050830A335078241 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11262SK 145168 FORWARD SIDE OF AFT OVERWING EXIT LOCATOR FAILED TO ILLUMINATE DURING TEST. REMOVED AND REPLACED NR 6 INVERTER IAW EMB 145 MM 33-50-11. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050831000392005083100039SO 2005 8 31 CHQA200500154 120050830A3397 CONNECTOR EMB 145 EMB145LR 3260212SO BATTERY PACK LOOSE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11565RP 145679 ALL EMERGENCY LIGHTS AROUND CABIN ESCAPE HATCHES INOPERATIVE. EMERGENCY FLOOR STRIP LIGHTS NR 3 AND NR 4 INOPERATIVE. FOUND EMERGENCY BATTERY 3 CONNECTOR LOOSE. RECONNECTED IAW EMB 145 MM 33-50-04. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050831000412005083100041NM 2005 8 31 AWXA200501009 120050829A33501012721 LIGHT BOEING737 7373G7 1384595NM SEAT 21 INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 PHX - EEL - FLT 753 - DURING GROUND HANDLING SEAT 21 FLOOR PROXIMITY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PLACED SEAT LIGHT ON MEL. TWO DAYS LATER ON 29AUG05, THE FLOOR PROXIMITY LIGHT ASSEMBLY WAS REPLACED IN LAS. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20050831000422005083100042EU 2005 8 31 AWXA200501010 120050815A5347D571301472000 SEAT TRACK AIRBUS320 A320231 3930325EU FR 36-41 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28645AW 238 SAL - MAJOR REPAIR - DURING C3 CHECK DISCOVERED CORROSION ON SEAT TRACK LOCATED ON THE RT INBOARD SIDE AT FR 36" Y-765. MAINTENANCE REMOVED CORROSION AND FOUND REWORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15. REMOVED SEAT TRACK AT FR 36" Y-765 AND INSTALLED NEW SEAT TRACK IAW AIRBUS 320 SRM 53-31-15 FIG 2. 2L72 4F RTA28NM 20050831000432005083100043EU 2005 8 31 AWXA200501011 120050815A5340D5323127020100 FITTING AIRBUS320 A320231 3930325EU FR 24-25 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28645AW 238 SAL - MAJOR REPAIR - CORROSION FOUND ON C3 CHECK LOCATED AROUND FITTING AT THE LOWER SILL OF THE FORWARD CARGO DOOR CUTOUT. NO ALLOWABLE DAMAGE LIMITS FOUND IN THE AIRBUS 320 SRM. MAINTENANCE REMOVED AND REPLACED THE FITTING LOCATED ON THE LOWER SILL OF FORWARD CARGO DOOR IAW AIRBUS 320 SRM 51-72-11 AND DWG D53231668. 2L72 4F RTA28NM 20050831000442005083100044EU 2005 8 31 AWXA200501012 120050815A5347D53112782200 SEAT TRACK AIRBUS320 A320231 3930325EU FR 20+10-24 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28645AW 238 SAL - MAJOR REPAIR - DURING C3 CHECK DISCOVERED CORROSION ON SEAT TRACK LOCATED ON THE RT INBOARD SIDE AT FR 20+10" Y-765. MAINTENANCE REMOVED CORROSION AND FOUND REWORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15. REMOVED SEAT TRACK AT FR 20+10" Y-765 AND INSTALLED NEW SEAT TRACK IAW AIRBUS 320 SRM 53-31-15 FIG 2. 2L72 4F RTA28NM 20050831000452005083100045NM 2005 8 31 AWXA200501013 120050818A2780 CONTROL SYSTEM BOEING757 7572S7 1384962NM LE FLAPS MALFUNCTIONED A AWXAO OTHER J WARNING INDICATION APAPPROACH 1 WP28905AW 23567 PHX - FLIGHT CONTROL - FLT 0059 - UPON SELECTION OF FLAPS THE CREW REPORTED AN EICAS MESSAGE FOR LEADING EDGE SLAT DISAGREE MESSAGE WITH FLAPS SELECTED IN THE FIRST DETENT. CREW COMPLETED QRH CHECKLIST AND CALLED OUT EMERGENCY EQUIPMENT FOR PRECAUTIONARY PURPOSES. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED, TESTED AND CYCLED FLAPS/SLATS WITH NO DEFECTS OR FAULTS BEING NOTED. AIRCRAFT WAS RETURNED TO SERVICE. AT THE TIME OF THIS INCIDENT THERE WAS A FOLLOW UP CURRENTLY ISSUED AGAINST THIS AIRCRAFT. THE FOLLOW UP WAS COMPLIED WITH ON 19AUG05, WITH SEVERAL ROTARY ACTUATORS BEING REPLACED CLEARING THE FOLLOW UP. 2L72 4F RTA2NM 20050831000462005083100046NM 2005 8 31 AWXA200501014 120050809A5315654681160 FLOORBEAM BOEING737 7373G7 1384595NM BS 986 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28311AW 24712 MCN - MAJOR REPAIR - DURING C15 CHECK DISCOVERED CORROSION LOCATED ON BS 986 FLOORBEAM T-CAP FROM BL 17L TO BL 17R. MAINTENANCE REMOVED CORROSION AT BS 986 FLOORBEAM IAW BOEING 737-300 SRM 51-10-02-0. MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-51-1 FIG 101. FABRICATED REPAIR STRAPS AND SUPPORT ANGLES IAW BOEING 737-300 SRM 53-00-51-2. ALSO RECEIVED NEW T-CAP AND PREPARED FOR INSTALLATION IAW BOEING 7370-300 SRM 53-00-51-2. MAINTENANCE INSTALLED REPAIR PARTS ON BS 986 FLOORBEAM T-CAP FROM BL 17L TO BL 17R IAW BOEING 737-300 SRM 53-00-51-2 FIG 101. 2L72 4F RTA16WE 20050831000502005083100050NM 2005 8 31 SWAA052603 120050828A53306545774 SKIN BOEING737 7373H4 1384600NM BS 762.25 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 762.25, STR 19L. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050831000522005083100052NM 2005 8 31 SWAA052605 120050829A53116546539 FRAME BOEING737 7373H4 1384600NM BS 616 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29617SW 27700 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, STR 17R AND STR 17L. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20050831000542005083100054NM 2005 8 31 SWAA052607 120050829A53116558280 FRAME BOEING737 7373H4 1384600NM BS 360 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29617SW 27700 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R TO STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050831000562005083100056NM 2005 8 31 2005UALA00876 120050824A5330 SKIN BOEING737 737322 1384676NM FUSELAGE BENT A UALAK NONE O OTHER ININSP/MAINT 1 WP29376UA 24641 EXTERNAL FUSELAGE SKIN BENT & DAMAGED AT AFT GALLEY DOOR LOWER HINGE CUTOUT. 2L72 4F RTA16WE 20050831000582005083100058NM 2005 8 31 2005UALA00878 120050823A335060253 LIGHT BOEING737 737322 1384676NM AFT GALLEY DAMAGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29310UA 23671 EMERGENCY EXIT LIGHTS, FLOOR LIGHT DAMAGED AT AFT CABIN. REPLACED EEL LIGHT ASSY. 2L72 4F RTA16WE 20050831000602005083100060EU 2005 8 31 2005UALA00880 120050824A3350 LIGHT AIRBUS320 A320232 3930326EU CABIN WILL NOT TEST A UALAK NONE L NO TEST ININSP/MAINT 1 WP29434UA 592 EMERGENCY LIGHT TEST FAILS EPSU IN LOAD EMERGENCY RIGHT. GLOBAL RESET AIRCRAFT CHECKS OK ON TEST. 2L72 4F RTA28NM 20050831000662005083100066NM 2005 8 31 2005UALA00886 120050825A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE BS 1540 DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29588UA 26717 FRAME DENTED AT STA 1540 AT STR 26L, AFT PIT, INBOARD FLANGE. REPAIRED FRAME WITH NESTED J-ANGLE REPAIR TO EXISTING CHORD PER TIMCO REO (EVA) G10818, REV B 2L72 4F4 FRTA2NM E17NE 20050831000682005083100068NM 2005 8 31 QXEA200501191 120050826A6120699018002 CONTROL UNIT BOMBDRDHC8 DHC8402 1390042NM NR 1 PROPELLER MALFUNCTIONED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09407QX3880 4049 BOI FLIGHT 2303: RETURN TO GATE - POWERPLANT MESSAGE. MAINTENANCE FOUND CDS FAULT CODES 180, 182 AND 184 ON NR 1 ENGINE PRESENT. TROUBLESHOOT PER FIM 61-20-04. REPLACED NR 1 PEC PER AMM TASK 61-20-36-000-801. FAULT CODES CLEARED. POWERPLANT MESSAGE CLEARED. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050831000712005083100071EU 2005 8 31 YENA200555 120050824A335032145410 POWER SUPPLY AIRBUS320 A320232 3930326EU EMERGENCY LIGHT INOPERATIVE A YENAK NONE O OTHER ININSP/MAINT 1 EA15598JB121 2314 L & R FORWARD EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED EPSU 10WL IAW AMM 33-51-38-04. 2L72 4F RTA28NM 20050831000732005083100073EU 2005 8 31 YENA200556 120050825A5210FE240004 CYLINDER DAMPER AIRBUS320 A320232 3930326EU R1 DOOR LEAKING A YENAK NONE O OTHER ININSP/MAINT 1 EA15566JB160625537 2042 R1 DOOR ASSIST CYLINDER LEAKING WILL NOT HOLD NITROGEN. REMOVED AND REPLACED R1 DOOR ASSIST CYLINDER PER AMM 52-11-14. 2L72 4F RTA28NM 20050831000812005083100081NM 2005 8 31 SWAA052613 120050829A53116546550 FRAME BOEING737 7373H4 1384600NM BS 787 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29617SW 27700 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R TO STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050831000832005083100083NM 2005 8 31 SWAA052615 120050829A531165C25229 FRAME BOEING737 7373H4 1384600NM BS 727D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29617SW 27700 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R TO STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050831000852005083100085 2005 8 31 SWAA052617 420050829A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29724SW 27856 R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR STRAP OUT OF POSITION. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20050831000872005083100087NM 2005 8 31 SWAA052619 120050828A3350D71701100 BATTERY PACK BOEING737 7377H4 1384404NM EMERGENCY EXIT FAILED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29726SW 27858 DURING SCHEDULED HC1 CHECK, RT AFT GALLEY EMERGENCY EXIT LIGHT BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050831000882005083100088CE 2005 8 31 1050617008AMW 120050824A5730118120002131 PANEL BEECH 1900 1900D 1154162CE LT WING FAILED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07173YV1701217012 UE173 LEFT WING UPPER BIN EVIDENCE OF DEFORMATION AT TURTLE BACK MOUNT FLANGE AREA. REPAIRED IAW SR-CO-00024. MORE INFORMATION WILL BE AVAILABLE AT A LATER DATE. 2L72 4T RTA24CE 20050831000902005083100090EA 2005 8 31 SWIA200515472 120050826A274170623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07938SW 7741 STAB CHANNEL ONE WILL NOT ENGAGE. REPLACED MOTOR CONTROL UNIT IAW MM27-42-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050831000922005083100092EA 2005 8 31 SWIA200515474 120050824A2720DL2428M9MOD1 ACTUATOR CNDAIRCL600 CL6002C10 1390015EA RUDDER LIMITER MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07740SK 10196 RUDDER LIMIT FAULT STATUS MESSAGE. REPLACED NR 1 RUDDER LIMITER ACTUATOR IAW CRJ MM 27-25-03. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050831000942005083100094EA 2005 8 31 SWIA200515476 120050825A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07591SW8791 8791 7079 STAB TRIM CH 2 WILL NOT ENGAGE. REPLACED THE HSTA ACTUATOR IAW MM 27-42-01 AND MCU IAW MM 27-42-05. OPERATIONAL CHECK GOOD. P/N 7062-3, S/N OFF 215. 2L72 4F RTA21EA 20050831000962005083100096NM 2005 8 31 2005UALA00852 120050819A5330 SKIN BOEING737 737322 1384676NM CFMINTCFM56 CFM562AFR 13802EU BS 1006 DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29347UA 24251 EXT FUSELAGE SKIN IS DENTED 0.75 INCH FWD OF STA 1006 & IMMEDIATELY BELOW SKIN LAP AT S14L. 2L72 4F4 FRTA16WE E21EU 20050831000972005083100097NM 2005 8 31 2005UALA00853 120050821A5340 FITTING BOEING737 737522 138449FNM CFMINTCFM56 CFM562AFR 13802EU BS 616 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29913UA 25291 CRACK IN FUSELAGE MAIN FRAME FITTING UNDER CABIN FLOOR AT STA 616 RBL 70, INNER CHORD AT BOTTOM 2 RIVETS. 2L72 4F4 FRTA16WE E21EU 20050831000982005083100098NM 2005 8 31 2005UALA00854 120050819A5322 SHEAR TIE BOEING757 757222 1384956NM PWA 2037 PW2037 NE STA 1480-1470 CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29588UA 26717 STA 1480 TO 1470 SKIN AND FRAME HAS CORROSION AROUND VHF ANTENNA. REMOVED CORROSION ON SKIN AND FRAME, REPLACED SHEAR TIE PER MM 51-10-02, 51-40-02. MEASURE AFTER DAMAGE REMOVAL, FOUND SKIN AND FRAME ARE WITHIN LIMITS. 2L72 4F4 FRTA2NM E17NE 20050831000992005083100099NM 2005 8 31 2005UALA00855 120050820A5754 SKIN BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE NR 4 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29217UA 30550 NR 4 SLAT HAD LOCAL DELAMINATION AT THE OUTBOARD END LOWER SURFACE OF THE TRAILING EDGE WEDGE. *S/D* THE LOCAL DELAMINATION FOUND IN THE NR 4 SLAT IS SYSTEMIC ON THE TRAILING EDGE WEDGES ON THE 777 SLATS. BOEING IS CURRENTLY WORKING ON A MODIFIED DESIGN TO REPLACE THE CURRENT WEDGE DESIGN. THIS CURRENT SLAT HAD BEEN REPAIRED PER EVA E97-335A WITH AN INTERIM REPAIR THAT HAD REQUIREMENTS FOR INITIAL AND REPETITIVE INSPECTIONS UNTIL A PERMANENT REPAIR COULD BE INSTALLED AT THE NEXT HMV. THEREFORE, GSO INSTALLED A PERMANENT REPAIR DOUBLER PER TIMCO REO-G10847. 2L72 4F4 FRTT0001SE E46NE 20050831001002005083100100NM 2005 8 31 2005UALA00856 120050820A335078941 LAMP BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE SEAT 37G INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29217UA 30550 SEAT 37G EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY. 2L72 4F4 FRTT0001SE E46NE 20050831001012005083100101NM 2005 8 31 2005UALA00857 120050821A335078941 LAMP BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE SEAT 3F INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29217UA 30550 SEAT 3F AFT EMERGENCY LIGHT INOP, BROKEN. REPLACED LIGHT ASSY. 2L72 4F4 FRTT0001SE E46NE 20050831001022005083100102NM 2005 8 31 2005UALA00858 120050821A2120 ODOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN/COCKPIT DETECTED A UALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP29504UA 24625 DIVERTED DUE TO ELECTRICAL ODOR IN THE COCKPIT AND CABIN. ACCORDING TO THE SHOP REPORT, RESISTOR R170 WAS DAMAGED BY OVERHEAT AND CAUSED SOME DISCOLORATION ON THE CIRCUIT BOARD. THIS IS THE TYPE OF FAILURE REPORTED ON BOEING SERVICE LETTER 757-SL-24-069-A. THE UNIT HAS BEEN INSTALLED ON THIS ACFT FOR APPROXIMATELY 1,800 FHRS. 2L72 4F4 FRTA2NM E17NE 20050831001032005083100103NM 2005 8 31 RYNA200500028 120050829A29235718610 PUMP BOEING737 737201 1384454NM B-HYD SYS OVERHEATED A RYNAA UNSCHED LANDING MK OVER TEMP FLUID LOSS CRCRUISE 1 CE07242US 22444 NR 2 B-SYSTEM ELECTRIC HYDRAULIC PUMP OVERHEATED, RETURNED TO ACY DUE TO DECREASING A-SYSTEM HYDRAULIC QUANTITY. REMOVED AND REPLACED NR 2 B-SYSTEM ELECTRIC HYDRAULIC PUMP, AND SERVICED A-SYSTEM. BOTH SYSTEMS LEAKED AND OPERATIONALLY CHECKED GOOD. REF B737 MM 29-12-22. 2L72 4F A16WE 20050831001052005083100105WP 2005 8 31 ARWA20050805 120050828A3231NAS5054 BEARING DOUG DC8 DC862F 3021972WP MLG DAMAGED A ARWAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO19791AL 46150 AFTER TAKEOFF; DOOR NOT LATCHED, LIGHT REMAINED ON; COMPLETED PROPER CHECKLIST AND UNABLE TO HAVE SATISFACTORY UPLATCH CHECKLIST; HAD TO DUMB FUEL AND RETURN TO STATION. ACCOMPLISHED GEAR SWING FOR TROUBLESHOT; FABRICATED DOOR ASSEMBLY AND PERFORMED GEAR SWING OPERATIONAL CHECK NORMAL AS PER DC-8 M/M 12-81-1 AND M/M 32-10-0. REMOVED AND REPLACED FROZEN BEARING IN LT MAIN LANDING GEAR DOOR UPLATCH MECHANISM IN ACCORDANCE WITH M/M 32-31-4. OPERATIONAL CHECK NORMAL. ALSO FOUND LOOSE TARGET ON RT SIDE MAIN LANDING GEAR DOOR UPLATCH SWITCH, TIGHTENED IN ACCORDANCE WITH M/M 32-36-0; OPERATIONAL CHECK NORMAL. 2L74 4F 4A25 20050831001102005083100110 2005 8 31 05105 420050827A31406229820008 DCU CNDAIRCL600 CL6002B19 1900309EA FAILED A REXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO258492C 7492 ON ROTATION ICE CAUTION FOLLOWED BY MASTER CAUTION LEFT ENGINE FIRE FOLLOWED BY ASSORTED OTHER MESSAGES. DECLARED EMERGENCY AND LANDED. UPON INVESTIGATION FOUND DCU'S BAD. REMOVED AND REPLACED DCU 1 AND DCU2 IAW AMM 31-41-00. PERFORMED OPS CHECK GOOD. 2L72 4F RTA21EA 20050831001172005083100117NM 2005 8 31 ASAA0540313 120050626A5311654655055 FRAME BOEING737 7374Q8 138447QNM FS 787 CUT A ASAAK NONE L NO TEST ININSP/MAINT 1 NM02773AS 25106 OKC - FOUND FRAME DAMAGED ON UPPER LIP AT BS 787 BETWEEN STRINGER 25 AND 26 RT. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW 737-400 SRM 53-00-07 FIGURE 201. (M) 2L72 4F RTA16WE 20050831001202005083100120NM 2005 8 31 ASAA0540308 120050626A57536546435282 SKIN BOEING737 7374Q8 138447QNM FS 202.6-414.4 PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 OKC - FOUND RIGHT OUTBOARD AFT FLAP INBOARD END HAS A PUNCTURE IN THE LOWER SURFACE. REMOVED DAMAGE AREA, FABRICATED FILLER AND DOUBLER AND INSTALLED REPAIR PIECES IAW B737-400 SRM 51-70-1 REPAIR 22. (M) 2L72 4F RTA16WE 20050831001232005083100123NM 2005 8 31 ASAA0540310 120050626A575465C26602311 SKIN BOEING737 7374Q8 138447QNM NR 2 SLAT DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 FOUND NR 2 SLAT OUTBOARD T/E DELAMINATED. REMOVED DAMAGE, FABRICATED SKIN AND DOUBLER AND INSTALLED REPAIR PIECES IAW 737-400 SRM 51-70-10. (M) 2L72 4F RTA16WE 20050831001252005083100125NM 2005 8 31 ASAA0540321 120050626A575365C26603202 WEDGE BOEING737 7374Q8 138447QNM TE FLAPS DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 OKC - FOUND LEFT INBOARD MID FLAP T/E WEDGE HAS TWO EACH SHARP DENTS. REMOVED DAMAGE, FABRICATED SKIN AND DOUBLER AND INSTALLED REPAIR PIECES IAW 737-400 SRM 51-70-10. (M) 2L72 4F RTA16WE 20050831001272005083100127NM 2005 8 31 ASAA0540307 120050626A531165C25229081 FRAME BOEING737 7374Q8 138447QNM FS 727D CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 OKC - FOUND FRAME AT BS 727D BETWEEN STRINGER 26 AND 27 LEFT ARE CORRODED. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR IAW 737-400 SRM 53-00-07 FIGURE 208. (M) 2L72 4F RTA16WE 20050831001292005083100129SO 2005 8 31 SIMA200521401 120050730A335066903 LIGHT EMB 135 EMB135KL 3260302SO CABIN INOPERATIVE A SIMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW21833AE 145629 FLT 3472 - BTR - CREW REPORTS EMERGENCY LIGHTS WILL NOT ILLUMINATE. REPLACED 2 FLOOR LIGHT STRIPS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050831001312005083100131SO 2005 8 31 SIMA200521608 120050728A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO FS 20 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21815AE8370 145545 THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED A DOUBLER, FILLER, TWO SHIMS AND PLATE. REPAIR DONE IAW EMB SRM 145/1142 REV 29, CHAPTER 53-00-10 FIG 201. (M) 2L72 4F RTT00011AT 20050831001332005083100133EU 2005 8 31 SIMA200521402 120050801A335066902 LIGHT SAAB SF340 340B 7860101EU CABIN INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21370AM 340B370 ONE SECTION OF FLOOR EMERGENCY LIGHTS WILL NOT ILLUMINATE. REPLACED FLOOR PROXIMITY ESCAPE PATH LIGHT STRIP 44LN. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 20050831001342005083100134EA 2005 8 31 SIMA200522301 120050809A335020131A BATTERY PACK CNDAIRCL600 CL6002C10 1390015EA CABIN DISCHARGED A SIMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW21512AE 10110 THE EMERGENCY LIGHTS WILL NOT ILLUMINATE. REPLACED NUMBER 1, 2, 3 AND 4 BATTERY PACKS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA21EA 20050831001352005083100135NM 2005 8 31 USAA050954 120050803A5510 BEAM BOEING737 7373B7 1384580NM FS 986 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US50 23933 CLT - FOUND BEAM CORRODED 6 INCHES, STATION 986, EXTREME RT END. REPLACED T-CAP IAW TR 53-60-05B. (M) 2L72 4F RTA16WE 20050831001362005083100136NM 2005 8 31 USAA050966 120050803A5320 WEB BOEING737 7373B7 1384580NM CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US50585 23933 CLT - FOUND WEB CRACKED 2 INCHES, AFT CARGO DOOR CUTOUT FRAME, LOWER WEB. REMOVED DAMAGED WEB, FABRICATED AND INSTALLED NEW WEB IAW BOEING DWG 65-20723 AND SRM 51-10-02. (M) 2L72 4F RTA16WE 20050831001372005083100137NM 2005 8 31 USAA050964 120050803A5315 FLOORBEAM BOEING737 7373B7 1384580NM FS 312 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US50585 23933 CLT - FOUND BEAM CORRODED 28 INCHES, T-CAP OF FLOORBEAM STATION 312, LBL 2, RBL 26. REMOVED PREVIOUS T-CAP AND REPLACED WITH NEW CAP EXTENDING SPLICES PER SRM IAW SRM 53-10-51. (M) 2L72 4F RTA16WE 20050831001382005083100138NM 2005 8 31 USAA050967 120050803A5340 ATTACH ANGLE BOEING737 7373B7 1384580NM BS 727 WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US 23933 CLT - FOUND ATTACH ANGLE CRACKED 1 INCH DIAMETER, WORN AREAS, RT WHEEL WELL STATION 727 RBL 14 BOTTOM OF BULKHEAD. REMOVED DAMAGED ANGLE. FABRICATED AND INSTALLED NEW ANGLE IAW BOEING DWG 65-48689 AND SRM 51-10-02 AND 51-40-02. (M) 2L72 4F RTA16WE 20050831001392005083100139NM 2005 8 31 USAA050973 120050804A5313 STRINGER BOEING737 7373B7 1384580NM FS 500 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US50585 23933 CLT - FOUND STRINGER CRACKED .5 INCH, STRINGER 8R AT STATION 500. REMOVED DAMAGED SECTION. FABRICATED AND INSTALLED REPAIR PIECES IAW SRM 53-00-03. (M) 2L72 4F RTA16WE 20050831001412005083100141NM 2005 8 31 USAA050972 120050804A531011323702 CREASE BEAM BOEING737 7373B7 1384580NM BS 576 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US50585 23933 CLT - FOUND CREASE BEAM CRACKED .75 INCH, BS 576, S17R. REPLACED WITH FACTORY NEW PART IAW SRM 51-10-02. (M) 2L72 4F RTA16WE 20050831001432005083100143NM 2005 8 31 USAA050963 120050803A53406935352U14 STRINGER CLIP BOEING737 7373B7 1384580NM BS 847 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US50585 23933 CLT - FOUND STRINGER TIE CRACKED .25 INCH, BS 847, STRINGER 4R. REMOVED CRACKED TIE, BS 847, STRINGER 4R. REMOVED CRACKED TIE CLIP AND INSTALLED NEW CLIP IAW SRM 51-10-02 AND 51-40-02. (M) 2L72 4F RTA16WE 20050831001452005083100145NM 2005 8 31 USAA050959 120050803A5320 STIFFENER BOEING737 7373B7 1384580NM BS 1006-1016 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US 23933 CLT - FOUND STIFFENER CORRODED .5 INCHES BY 6 INCHES, STRINGER 26R BS 1006-1016. REMOVED DAMAGE INSTALLED NEW STRINGER SECTION ATTACH FITTING AND STIFFENER IAW SRM 53-60-03 AND 51-10-02. (M) 2L72 4F RTA16WE 20050831001472005083100147NM 2005 8 31 USAA050955 120050803A5320 INTERCOSTAL BOEING737 7373B7 1384580NM FS 312/394.5 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US50585 23933 CLT - FOUND INTERCOSTAL CORRODED 2 INCHES BY 3 INCHES, STATION 312 AND 394.5 ATL LBL 12. REMOVED PART, FABRICATED NEW AND INSTALLED IAW SRM 51-10-02. (M) 2L72 4F RTA16WE 20050831001492005083100149NM 2005 8 31 USAA050961 120050803A53206545834U69 STRAP BOEING737 7373B7 1384580NM BS 326 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US50585 23933 CLT - FOUND STABILIZER STRAP CRACKED 1 INCH, BS 326, LBL 11. DEF PART REPLACED WITH IDENTICAL PART, IAW SRM 51-10-02 AND 51-40-02. (M) 2L72 4F RTA16WE 20050831001502005083100150NM 2005 8 31 USAA050962 120050803A53206545834U70 STRAP BOEING737 7373B7 1384580NM BS 327 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US 23933 CLT - FOUND STABILIZER STRAP CRACKED 1 INCH, BS 327, BL 0, CABIN FLOOR STRUCTURE. REMOVED CRACKED STRAP AND REPLACE WITH NEW FROM STOCK IAW SRM 51-10-02 AND 51-40-02. (M) 2L72 4F RTA16WE 20050831001522005083100152NM 2005 8 31 USAA050951 120050803A5551 BUSHING BOEING737 7373B7 1384580NM HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US50585 23933 CLT - BUSHING CORRODED, L1, FORWARD FACE LEFT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED NEW BUSHING IAW SRM 53-10-10. (M) 2L72 4F RTA16WE 20050901000012005090100001NM 2005 9 1 USAA050949 120050803A5551 BUSHING BOEING737 7373B7 1384580NM HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US 23933 CLT - FOUND CORROSION ON LUG/BUSHING 2 INCHES BY .015, LEFT STAB, FORWARD LOWER LUG LEFT HORIZ STABILIZER. OVERSIZED LUG, FABRICATED NEW BUSHING IAW SRM 55-10-10. (M) 2L72 4F RTA16WE 20050901000022005090100002NM 2005 9 1 USAA050953 120050803A5551 BUSHING BOEING737 7373B7 1384580NM HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US50585 23933 CLT - FOUND LUG/BUSHING CORRODED 2 INCHES BY .015 TYPICAL, LT STAB CENTER SECTION FORWARD LOWER LUG. REMOVED CORROSION, FABRICATED NEW BUSHING. (M) 2L72 4F RTA16WE 20050901000042005090100004EA 2005 9 1 REX2005F00002 120050802A215078279015 ACM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RIGHT INOPERATIVE A REXAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 SO258698A6274 7698 (REF NR: 05-094) IN FLIGHT CABIN HAD FUMES AND POSSIBLE SMOKE. QRH FOLLOWED DIVERTED WITH UNEVENTFUL LANDING. TROUBLESHOT AIRCRAFT AND ENGINES DOWN TO THE RT AIR CYCLE MACHINE (ACM). REMOVED AND REPLACED RT ACM IAW AMM. OPS CHECKED GOOD. (K) 2L72 4F4 FRTA21EA E15NE 20050901000052005090100005NM 2005 9 1 USAA050902 120050727A5730 PANEL BOEING737 737401 1384701NM CFMINTCFM56 CFM563B2 13802EU LT WING CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19404US46134 23886 CLT - C1 - PANEL, 2 INCH CRACK, TOP OF LT WING PANEL JUST OB OF GROUND SPOILER. REMOVED DAMAGE AND INSTALLED REPAIR SPLICE AND DOUBLER IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050901000072005090100007CE 2005 9 1 GUU2005F00040 120050730A55241016200131 BRACKET BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE RT ELEVATOR CORRODED A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO178153819328 UE199 AT SCHEDULED INSPECTION, RT ELEVATOR CENTER HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REPLACED RT ELEVATOR CENTER HINGE BRACKET. (K) 2L72 4T4 TRTA24CE E26NE 20050901000092005090100009EA 2005 9 1 REX2005F00044 120050502A3260 PROXIMITY SWITCH CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NLG OUT OF ADJUST A REXAO OTHER N FALSE WARNING APAPPROACH 1 SO258587E8275 7587 (REF NR: 05-059) RECEIVED (GEAR DISAGREE) MESSAGE ON APPROACH. QRH FOLLOWED GEAR MANUALLY EXTENDED. EMERGENCY DECLARED UNEVENTFUL LANDING. ADJUSTED NOSE GEAR PROXIMITY SWITCH IAW AMM. GEAR SWINGS PERFORMED. (K) 2L72 4F4 FRTA21EA E15NE 20050901000102005090100010NM 2005 9 1 AMTA200500634 120050805A3610 SEAL BOEING757 75733N 1384931NM LT SHUTOFF VALVEUNSERVICEABLE A AMTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL11555TZ 1574 32589 ON TAKEOFF AND CLIMB OUT, LT HIGH STAGE BLEED LIGHT ILLUMINATED ACCOMPANIED WITH EICAS MESSAGE RETURNED TO DEPARTURE. T/S IAW FIM, FOUND HPSOV BUTTERFLY SEAL BROKEN. REPLACED IAW FIM MM, LEAK CHECK GOOD. (K) 2L72 4F RTA2NM 20050901000112005090100011EA 2005 9 1 REX2005F00000 120050727A3260 PROXIMITY SWITCH CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE MLG LOOSE A REXAO OTHER N FALSE WARNING TOTAKEOFF 1 SO258525B 7525 (REF NR: 05-092) GEAR DISAGREE WARNING AFTER TAKEOFF, DURING GEAR RETRACTION. RT MAIN SHOWS IN TRANSIT. FOLLOWED QRH WITH UNEVENTFUL LANDING. INTERROGATED PSEU, FOUND TARGET FOR RT MLG UPLOCK PROXIMITY SWITCH LOOSE. TIGHTENED TARGET IAW AMM AND PERFORMED GEAR SWING IAW AMM. OPS CHECK GOOD. (K) 2L72 4F4 FRTA21EA E15NE 20050901000122005090100012NM 2005 9 1 USAA050946 120050803A5551 BUSHING BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US50585 23933 CLT - Q6 -LUG/BUSHING, 2 INCH DIA X .015 TYPICAL, CORROSION; NO LEVEL OR TASK, L1,AFT FACE, LT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED NEW BUSHING IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050901000142005090100014EA 2005 9 1 ASOA05653 120050803A5220601R330501 HANDLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE ESCAPE HATCH CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27854AS 7382 DURING A C-CHECK, THE CREW ESCAPE HATCH OUTER HANDLE WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CREW ESCAPE HATCH OUTER HANDLE ASSY IAW SRM. (K) 2L72 4F4 FRTA21EA E15NE 20050901000202005090100020EA 2005 9 1 2005F00094 220050608A7322105217 CARBURETOR CESSNA172 172P 2072436CE LYC O320 O320D2J 41508EA MCAULY1C160 1C160DTM GL ENGINE FAILED D CQNAO OTHER R PARTIAL RPM/PWR LOSS LDLANDING 1 SO0599744 152 17276503 RL1385139A 7557MI ENGINE POWER LOSS DURING LANDING TOUCH 3, GOES. UNABLE TO REGAIN RPMS WITHOUT PUMPING THE THROUGH HOLE. CARBURETOR WAS REBUILT, INSTALLED 7/7/04, 157.2 HOURS SOH. REMOVED AND REPLACED CARBURETOR, FIXED POWERLOSS PROBLEM. (K) 1H71 3O3 ONT3A12 E274 5 NP910 20050901000212005090100021WP 2005 9 1 CLC2005F00009 120050804A2420780002976 CABLE DOUG DC10 DC1030 3023501WP GE CF6 CF650C2 30018NE NR 2 GENERATOR BURNED A CLCAD RETURN TO BLOCK BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TXTAXI/GRND HDL 1 SO29279AX 47816 ON TAXI OUT, THE NR 2 AC BUSS CIRCUIT BREAKERS POPPED OUT. SMELLED SMOKE IN COCKPIT, TAXIED BACK TO THE RAMP. FOUND BURNED WIRES AND FEEDER CABLES BELOW LAVATORY FLOOR FOR THE NR 2 GENERATOR, ALL 3 PHASES. GENERATOR FEEDER CABLES FOR NR 1 AND 3 GENERATORS ARE ALSO ALL 3 PHASES. GENERATOR FEEDER CABLES FOR NR 1 AND 3 GENERATORS ARE ALSO DETERIORATED. ACCOMPLISHED REPLACEMENT, BY SPLICING OF CABLES AT STATIONS 410-492 AND STA 535 IAW MM, 9 EA FOR AC BUSS TIE FOR NR 2 ENGINE. ALL ELECTRICAL SYSTEMS, OPS CHECK NORMAL. AC RETURNED TO REVENUE SERVICE. (K) 2L73 4F4 F A22WE E23EA 20050829001322005082900132NM 2005 8 29 USAA051048 120050823A5512 SKIN BOEING737 737401 1384701NM RT STABILIZER CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19420US 23987 RIGHT STABILIZER LOWER SKIN, ELEV STA 106 (JUST FWD OF PNL 9208R) CRACKED. INSTALLED FILLER AND DOUBLER IAW TYPICAL REPAIR 55-10-07 REV-B, DEFECT SIZE: 1.25 INCH 2L72 4F RTA16WE 20050829001362005082900136NM 2005 8 29 USAA051050 120050824A5320 WEB BOEING737 7374B7 1384702NM BS 344 DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19449US 24893 RIGHT CREASE BEAM WEB AT ATTACHMENT TO FRAME 344 HAS HOLE. COMPLIED WITH EA 9682 AND BOEING DWG 65-45875, DEFECT SIZE .1875 INCH. 2L72 4F RTA16WE 20050829001532005082900153NM 2005 8 29 AALA20050555 120050815A5414 RETAINER BOEING767 767223 1385123NM PYLON SEAL WORN A AALAK NONE O OTHER ININSP/MAINT 1 SW21332AA 22331 MCI - NUMBER ONE AND TWO ENGINE THRUST REVERSER SEAL RETAINER RUBBED INTO PYLON STRUCTURE AT TOP AFT SIDE OF BOTH INBOARD AND OUTBOARD REVERSERS FOR NUMBER TWO ENGINE AND AT TOP AFT SIDE OF INBOARD THRUST REVERSERS FOR NUMBER ONE ENGINE. BLENDED WEAR AND PERFORMED HIGH FREQUENCY EDDY CURRENT INSPECTION. CHECKED AREA FOR MATERIAL LOSS AND CRACKS. TRIMMED REVERSER SEAL RETAINER AND RIGGED REVERSER CLEARANCE. 2L72 4F RTA1NM 20050829001632005082900163NM 2005 8 29 BB05069 120050818A33501000679 LIGHT BOEING767 767201 1385125NM PASSENGER CABIN FAULTY A USAAK NONE L NO TEST ININSP/MAINT 1 EA19650US 23902 SNN - DURING TEST, THE FLIGHT DECK EMERGENCY EXIT SIGN FAILED TO ILLUMINATE. MAINTENANCE REPLACED THE FLIGHT DECK EMERGENCY EXIT SIGN. OPERATIONALLY CHECKS OK. 2L72 4F RTA1NM 20050829001652005082900165EU 2005 8 29 SA05096 120050817A335032145410 EPSU AIRBUSA321 A321211 3930370EU PASSENGER CABIN FAILED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19175US15461 1496 CLT - DURING TEST, RECEIVED FAULT MESSAGE, EPSU INT LOAD FWD L. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT AT THE FORWARD LOCATION. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20050829001722005082900172NM 2005 8 29 USAA051037 120050823A5530 ATTACH FITTING BOEING737 737301 1384611NM VERTICAL FIN CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US 23933 RIGHT AFT O/B VERTICAL FIN ATTACH LUG ON FUSELAGE. MACHINED AFT CHAMFER AND BOR TO CLEAN UP CORROSION & INSTALL NEW BUSHING IAW EA 96788, DEFECT SIZE .080 INCH DEEP. 2L72 4F RTA16WE 20050829001802005082900180SO 2005 8 29 MASA200500539 120050711A3397 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT LOOSE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07836MJ 145359 ASH 2832 CLT. NR 2 AND NR 3 FROM FORWARD EMERGENCY FLOOR PATH LIGHTS WERE INOP. MX RESECURED A CONNECTOR ON THE NR 3 LIGHT STRIP AND OP CHECKED THE LIGHTS. 2L72 4T RTT00011AT 20050829001862005082900186SO 2005 8 29 MASA200500603 120050729A3397 CONTACT EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT FAILED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07836MJ 145359 ASH 2829 GSP. NR 2 AND NR 3 FLOOR PROXIMITY EMERGENCY LIGHTS WOULD NOT ILLUMINATE. CONTACT MX RESET THE EMERGENCY LIGHT SYSTEM AND NO FURTHER DEFECTS WERE NOTED. 2L72 4T RTT00011AT 20050829001892005082900189SO 2005 8 29 MASA200500622 120050807A3350 SIGN EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07829MJ 145228 ASH 2726 CLT. LEFT OVERWING EMERGENCY EXIT SIGN INOP. MX PERFORMED AN OPERATIONAL TEST AND COULD NOT DUPLICATE THE FAULT. 2L72 4T RTT00011AT 20050829002062005082900206 2005 8 29 SWAA052574 420050824A256565C16820 HOOK BOEING737 7373H4 1384600NM L2 DOOR GIRT BARLOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29627SW 27935 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER MM. 2L72 4F RTA16WE 20050829002152005082900215NM 2005 8 29 0501346717 120050818A5311 FRAME BOEING747 747251F 1384898NM BS 380 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01617US 21121 DURING L-CHECK FOUND CRACKS IN FRAME AT BS 380 S24L. REPAIRED PER EA 67-165232. 2L74 4F A20WE 20050830000022005083000002EA 2005 8 30 COMA60454A 120050819A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01937CA2765 62 7044 FLIGHT 5144 - FLAPS FAIL CAUTION. REPLACED THE LT BPSU. 2L72 4F RTA21EA 20050830000042005083000004NM 2005 8 30 SB05100 120050827A3397 WIRE BOEING737 7374B7 1384702NM EMERGENCY EXIT BROKEN A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US 24781 PIT - MAINTENANCE REPORTED THE AFT LEFT EXTERIOR OVERWING EMERGENCY EXIT LIGHT AND THE AISLE EMERGENCY EXIT SIGNS AT ROWS 10 ABC AND 11 ABC WERE INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AT CEILING EMERGENCY EXIT SIGN AT EXIT WINDOWS AND REPLACED FUSES IN CHARGER ASSEMBLY. OPERATIONAL CHECK OF EMERGENCY LIGHTS GOOD. 2L72 4F RTA16WE 20050830000102005083000010EU 2005 8 30 USAA051061 120050826A5315D5347217220400 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19724UW 1122 FROM 3 INCHES FWD OF FS 66 TO 5 INCHES FWD OF FS 68 IN Y1292 BEAM. DEFECTIVE PART REPLACED WITH IDENTICAL PART DEFECT SIZE: 3 X 1.5, 4 X 1.5, 1 X 1, .5 X 1, .5 X 1. 2L72 4F RTA28NM 20050830000262005083000026CE 2005 8 30 DXTA200500926 120050825A2910 LINE CESSNA750 750 2076810CE HYDRAULIC SYS LEAKING E DXTAO OTHER K FLUID LOSS LDLANDING 1 GL07947QS 7500047 EXCESSIVE BRAKE PEDAL PRESSURE NEEDED ON LANDING ROLL OUT. REQUIRED LARGER THAN NORMAL INPUT TO STOP AIRCRAFT. THIS WAS A DRY RUNWAY NOT CONTAMINATED. PERFORMED VISUAL INSPECTION OF BRAKES AND PLUMBING. PERFORMED POWER BRAKE BLEEDING IAW CITATION 750 MM CH 32-42-00-721. FUNCTION AND LEAK CHECK GOOD. 2L72 4J RTT00007WI 20050830000282005083000028EU 2005 8 30 XN0A1261 120050825A2910 HYDRAULIC SYSTEM AIRBUS300 A300B4203 3930306EU YELLOW SYS FAILED A XN0AD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL23371PC 157 ON TAXI, YELLOW HYD AIR PRESS LOW INDICATION AND QTY DECREASE TO YELLOW BAND. VERIFIED YELLOW SYS, FALL AT RESERVOIR. SERVICED HEAD PRESSURE, SYS NORMAL PER A300 MM 29-00-00. 2L72 4F RTA35EU 20050830000312005083000031 2005 8 30 COMA0560465 420050823A341845150340 TRANSDUCER CNDAIRCL600 CL6002B19 1900309EA AOA MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01479CA8645 7675 FLIGHT 5763 - STALL FAIL WARNING. REPLACED THE AOA TRANSDUCER. 2L72 4F RTA21EA 20050830000402005083000040SO 2005 8 30 C2XA05IA099 120050821A3350AD20131A BATTERY PACK EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2717521134644824 145378 IAH - DURING MAINTENANCE INSPECTION, THE AFT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050830000582005083000058NM 2005 8 30 SWAA052586 120050826A335020131A BATTERY PACK BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29330SW 23694 DURING SCHEDULED RON CHECK, FOUND FWD GALLEY EXIT SIGN INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050830000592005083000059NM 2005 8 30 SWAA052587 120050826A53306545765 SKIN BOEING737 7373H4 1384600NM BS 500C CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29338SW 23960 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 15L. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050830000602005083000060NM 2005 8 30 SWAA052588 120050828A53116517684 FRAME BOEING737 7373H4 1384600NM BS 303.9 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29369SW 26580 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303.9, STR 16L. REPAIRED FRAME PER SWA EA & SRM. 2L72 4F RTA16WE 20050830000612005083000061NM 2005 8 30 SWAA052589 120050828A53206545409 WEB BOEING737 7373H4 1384600NM BS 663.75 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29372SW 26599 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE BEADED WEB CRACKED AT BS 663.75, RBL 39. REPAIRED BEADED WEB PER SRM. 2L72 4F RTA16WE 20050830000632005083000063NM 2005 8 30 SWAA052591 120050826A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM BS 787 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29617SW 27700 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, RBL 9. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050830000642005083000064NM 2005 8 30 SWAA052592 120050826A53106545829 CREASE BEAM BOEING737 7373H4 1384600NM BS 294.5-360 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29617SW 27700 DURING SCHEDULED D-CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 294.5 TO BS 360. REPAIRED CREASE BEAM PER SRM. 2L72 4F RTA16WE 20050830000652005083000065NM 2005 8 30 SWAA052593 120050826A53106545807 FRAME BOEING737 7373H4 1384600NM R1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29617SW 27700 DURING SCHEDULED D-CHECK, FOUND R1 DOOR CUTOUT STUB FRAME CRACKED AT FWD UPPER CORNER. REMOVED AND REPLACED STUB FRAME PER SRM. 2L72 4F RTA16WE 20050830000812005083000081NM 2005 8 30 ASAA0540317 120050626A5311654653120 FRAME BOEING737 7374Q8 138447QNM FS 500F CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 OKC - FOUND FRAME AT BS 500F STRINGER 27-28 LEFT ARE CORRODED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW 737-400 SRM 53-00-07 FIGURE 203. (M) 2L72 4F RTA16WE 20050830001142005083000114NM 2005 8 30 05FDEA02696 120050827A5315 FLOORBEAM DOUG MD11 MD11 3023602NM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 AFT CABIN, AFTER REMOVAL OF CORRODED SEAT TRACK, FLOORBEAM WEB UPPER CHORD AT STA 1828 LBL 27.5, FOUND EXTRA HOLE CLOSE TO EDGE AS MARKED. REMOVED AND REPLACED FROM S1464579-7075T6511 AS PER DRAWING AGA 7070. 2L73 4F RTA22WE 20050830001272005083000127EU 2005 8 30 05FDEA02704 120050827A7830 WARNING LIGHT AIRBUS330 A300* EU THRUST REVERSER ILLUMINATED A FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25730FD 659 NR 2 REVERSER UNLOCK CAME ON DURING TAKEOFF IMMEDIATELY AFTER BRAKE RELEASE AFTER 40 PERCENT BUT BEFORE STANDARD POWER. LIGHT WENT OUT WHEN THROTTLES PULLED TO IDLE MEL. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-C CATEGORY: C EXPIRATION: 06SEP05 "MEL 78-30-01-C: ENGINE (IDENTIFY 1 OR 2) NR 2 THRUST REVERSER, INOP. THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POSITION. INSPECTED RIG AND FOUND NORMAL. ADJUSTED PER 78-31-00-5-06. HOLDING MASTER ACTUATORS AGAINST STOP PERLOAD WAS C/W IN THE STOWED DIRECTION AT THE PNEUMATIC DRIVE UNIT. OPS CK'D NORMAL WHEN POWER MOVED OUT OF IDLE 2L72 4F RTA26NM 20050830001292005083000129NM 2005 8 30 05FDEA02706 120050829A5330 SKIN BOEING727 72722 1384002NM BS 1166-1183 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25192FE 19085 EXTERNAL FUSELAGE SKIN HAS POPPED AND CRACKED FASTENERS ALONG STR 25 LEFT, BS 1166 - 1183. REPAIRED DAMAGED FUSELAGE SKIN BS 1166-1183 AT STR 25-STR 27 PER FED EX EA 7-5330-91350. 2L73 4F A3WE 20050830001312005083000131EU 2005 8 30 RAIA00508036 120050825A3397 WIRE JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT DISCONNECTED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03571HK 41090 FLT 5581 - STL - EMERGENCY EXIT LIGHT INOP. MAINTENANCE RECONNECTED EMERGENCY LIGHT. 2L72 4T RTA41NM 20050830001332005083000133NM 2005 8 30 PIDA20050065 120050826A3350 CHARGER BOEING757 757236 1384971NM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05757BJ 22176 R4 DOOR EMERGENCY SLIDE LIGHT INOP. REPLACED M736 BATTERY CHARGER PER MM 33-51. 2L72 4F RTA2NM 20050830001352005083000135EA 2005 8 30 REX2005F00005 120050825A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE TE FLAPS FAILED A REXAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 SO25827AY 8027 ( REF NR: 05-102) FLAP FAILURE ENROUTE, AT 0. QRH FOLLOWED UNEVENTFUL LANING. RESET FLAPS AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K) 2L72 4F4 FRTA21EA E15NE 20050830001382005083000138NM 2005 8 30 ASAA0540303 120050626A5753 SKIN BOEING737 7374Q8 138447QNM GE CFM56 CFM56* 13802NE TE FLAP DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 OKC - FOUND RT OB AFT FLAP DELAMINATED AT IB AFT CORNER. 2L72 4F4 FRTA16WE E2GL 20050830001402005083000140WP 2005 8 30 05FDEA02687 120050826A5712 RIB DOUG DC10 DC1010 3022110WP ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE LT WING FIXED LEADING EDGE AT STA XORS 743 FOUND RIB CRACK. REPAIR IAW SRM 57-20-00 FIG 1 SHEET 3, 4 AND INSTALLED REPAIR ANGLE. 2L73 4F A22WE 20050831000012005083100001NM 2005 8 31 SWAA052608 120050829A53116546529 FRAME BOEING737 7373H4 1384600NM BS 440 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29617SW 27700 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R TO STR 9R AND STR 8L TO STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050831000152005083100015NM 2005 8 31 2005UALA00865 120050821A3350362624 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE 5A AFT, 32 ABC &INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29121UA 29167 EEL INOPERATIVE AT 5A AFT, 32 ABC, 44 ABC & DOOR 4 GALLEY AREA CROSS AISLE WALL. REPLACED EEL LAMP. 2L74 4F4 FRTA20WE E24NE 20050831000252005083100025NM 2005 8 31 2005UALA00875 120050824A5330 SKIN BOEING737 737322 1384676NM STR 10R, BS 377 DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29376UA 24641 EXTERNAL FUSELAGE SKIN DENTED ABOVE STR 10R AT STA 377. 2L72 4F RTA16WE 20050831000272005083100027EU 2005 8 31 05FDEA02716 120050830A2612 FIRE DETECTOR AIRBUS300 A300B4605R 3930308EU GE CF6 CF680 30025NE NR 2 NACELLE FALSE INDICATIONA FDEAFEA ACTIVATE FIRE EXT. ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25652FE 735 705257 DURING CLIMB-OUT AT 20,000 FT, NR 2 ENGINE INDICATED A FIRE: LIGHT IN FIRE CRC AND LIGHT IN FUEL SHUTOFF HANDLE. NO OTHER ANOMALIES NOTED EITHER ON ANALOG GAUGES OR ECAM PAGE. ALL CHECKLISTS COMPLETED TO INCLUDE PULLING FIRE HANDLE & DISCHARGING BOTH BOTTLES. FIRE LIGHT REMAINED ON THROUGH LANDING & ROLL OUT. INSPECTED NR 2 ENGINE INTAKE & EXHAUST, FOUND NO OBVIOUS DEFECTS, OPENED ALL COWLS & INSPECTED FOR LOOSE OR LEAKING DUCT WORK. FOUND FOIL MISSING FROM STARTER DUCT. R & R BOTH NR 2 ENGINE FIRE EXTINGUISHER BOTTLES PER A300 MM. OPS CKS GOOD. REPLACED RELAYS 10WD & 10WE. REPLACED GEARBOX, TURBINE & UPPER RT TURBINE DETECTORS IAW A300 AMM, NR 2 FIRE WARNING TESTS NORMAL. 2L72 4F4 FRTA35EU E13NE 20050831000362005083100036NM 2005 8 31 QXEA200501190 120050828A215078279018 ACM DHAV DHC8 DHC8202 2809007NM ACM BAY SEIZED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09353PH9239 496 YYJ FLIGHT 2074 CABIN BECAME EXCESSIVELY HOT ON CLIMBOUT, UNABLE TO CONTROL CABIN TEMP IN AUTO AND MANUAL MODES. RAN BOTH FLIGHT COMPARTMENT AUTO FAIL AND CABIN COMPARTMENT AUTO FAIL CHECKLISTS AND PULLED AND RESET ASSOCIATED CIRCUIT BREAKERS, NO HELP. CABIN DUCT TEMP WAS STEADY AT 50 DEG CELSIUS AND CABIN TEMPS WERE NEARLY UNBEARABLE. MAINTENANCE REMOVED AIR CYCLE MACHINE IAW DHC-8 200 MM TASKS 21-50-11-000-801 AND 400-801. GROUND RAN NR 2 ENGINE AND SELECTED BLEED ON AIR CONDITIONING SYSTEM OPERATES NORMALLY. DUCT TEMP WENT TO 5 DEGREES CELSIUS WHEN SELECTED FULL COLD, NO LEAKS NOTED AT AIR CYCLE MACHINE. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050831000702005083100070NM 2005 8 31 SB05102 120050830A33973507771 CONNECTOR BOEING737 737301 1384611NM SEAT ROW 12 DISCONNECTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19353US 23556 CLT - MAINTENANCE REPORTED THE CABIN MOUNTED EMERGENCY LIGHTS FROM SEAT ROWS 12 THRU 16 WERE INOPERATIVE. MAINTENANCE SECURED A CONNECTOR BENEATH SEAT ROW 12. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050831000722005083100072CE 2005 8 31 DJFA2005135 120050824A291345AS65020001 PUMP BEECH MU300 400A 1155402CE RIGHT ENGINE WORN E DJFAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA23709TA RK180 THE CREW REPORTED THAT THE HYDRAULIC PRESSURE WAS READING HIGH IN FLIGHT. WHEN THE HYDRAULIC PRESSURE DROPPED TO ZERO THE CREW CLOSED THE EMERGENCY DUMP VALVE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT WAS DIVERTED TO KSAN DUE TO THE HIGHER RUNWAY LENGTH IN THE EVENT THAT THE EMERGENCY BRAKES WOULD HAVE TO BE USED. WHEN THE AIRCRAFT WAS LANDED, THE USE OF NORMAL BRAKES RESULTED IN HYDRAULIC PRESSURE FLUCTUATIONS. MAINTENANCE REPLACED THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP. NEW HYDRAULIC PACK FILTERS WERE INSTALLED FOR THE LEFT AND RIGHT POSITIONS. GROUND RUN OPERATIONAL CHECKS WERE NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4F RTA16SW 20050831000742005083100074NM 2005 8 31 CALA0500283 120050826A53146545866 KEELBEAM BOEING737 7373T0 1384582NM BS 500D-540 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714335 23573 INSPECTION FOUND KEEL BEAM CORRODED AT STA 500D-540, S28R. THE CORRODED SECTION OF KEEL BEAM WAS CUT OUT AND A NEW SECTION OF KEEL BEAM WAS INSTALLED IAW ECRA 5311-01236. 2L72 4F RTA16WE 20050831000762005083100076NM 2005 8 31 2005UALA00889 120050825A2120 SMOKE BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN DETECTED A UALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP29550UA 25398 DIVERTED DUE TO SMOKE IN THE CABIN & COCKPIT. MODERATE SMOKE AND FUMES OF ELECTRICAL TYPE IN CABIN AND COCKPIT. FLIGHT DIVERTED TO DTW. INSPECTED GALLEYS, CABIN, CARGO PITS AND BOTH E&E BAYS FOR ELECTRICAL RELATED PROBLEMS. FOUND AUDIO ACCESSORY UNIT WITH STRONG ELECTRICAL SMELL. CAPT AND FO WRITE-UP ALSO GENERATED SAYING UNABLE TO COMMUNICATE WITH FLT ATTENDANTS ON SERVICE INTERPHONE. REPLACED AUDIO ACCESSORY MR23505-59 UNIT CHECKED GOOD. TWO CIRCUIT BOARD FAILURES OCCURRED WITHIN THE AUDIO ACCESSORY UNIT. BOARD A1 HAD RESISTOR R1 AND CAPACITOR C2 FAILURE. BOARD A2 HAD A FAILURE OF RESISTOR R1. RESISTOR SPECIFICATIONS (R1) FOR BOTH BOARDS IS P/N RL42S100GTX (10 OHM 2WATT). CAPACITOR SPECIFICATION 2L72 4F4 FRTA2NM E17NE 20050831000802005083100080NM 2005 8 31 SWAA052612 120050829A53116546552 FRAME BOEING737 7373H4 1384600NM BS 827 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29617SW 27700 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L TO STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050831000822005083100082NM 2005 8 31 SWAA052614 120050829A53116546559 FRAME BOEING737 7373H4 1384600NM BS 907 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29617SW 27700 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R TO STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050831000842005083100084NM 2005 8 31 SWAA052616 120050829A53306545776 SKIN BOEING737 7373Q8 1384670NM BS 885 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 885, STR 24R. REPAIRED SKIN PER SWA EA AND SRM. 2L72 4F RTA16WE 20050831000862005083100086 2005 8 31 SWAA052618 420050828A256563550101 SLIDE BOEING737 7377H4 1384404NM L1 DOOR OUT OF LIMITS A SWAAK NONE O OTHER ININSP/MAINT 1 SW29725SW 27857 DURING SCHEDULED RON CHECK, L1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATED OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20050831000892005083100089EA 2005 8 31 SWIA200515471 120050826A2741 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07427SW 7497 HORIZONTAL STAB CHANNEL 2 WILL NOT ENGAGE. REPLACED STAB/MACH TRIM ENGAGE PANEL. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050831000912005083100091EA 2005 8 31 SWIA200515473 120050821A27515913163 DETECTOR CNDAIRCL600 CL6002C10 1390015EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07724SK1731 1731 10189 FLAPS HALFSPEED STATUS MSG. REPLACED LT WING INBOARD FLAP, OUTBOARD SKEW DETECTOR IAW MM 27-52-45. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050831000932005083100093EA 2005 8 31 SWIA200515475 120050825A2741 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07915SW 7615 STAB TRIM CH 2 WILL NOT ENGAGE. REPLACED STAB/MACH TRIM PANEL. OPERATIONAL CHECK GOOD IAW MM 27-41-25 AND 27-41-00. 2L72 4F RTA21EA 20050831000952005083100095EA 2005 8 31 SWIA200515477 120050821A5753601R140021 STRUCTURE CNDAIRCL600 CL6002B19 1900309EA TE FLAP DAMAGED A SWIAO OTHER CF F.O.D. FLT CONT AFFECTED LDLANDING 1 NM07936SW6533 6533 7726 LEFT INBOARD FLAP DAMAGE ON UNDERSIDE OF FLAP AFTER NR 1 MAIN BLEW OUT ON LANDING. REPLACED LEFT INBOARD FLAP IAW MM 27-54-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050831001042005083100104WP 2005 8 31 0501369863 120050825A3320 BALLAST DOUG DC9 DC951 3022051WP LIGHT BURNED A NWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL01772NC 47774 DURING DEPLANING AT THE GATE AN ELECTRICAL ODOR AND A LITTLE SMOKE DEVELOPED IN THE AFT CABIN AREA. A PASSENGER REPORTED SPARKS COMING FROM A LIGHT NEAR THE LEFT EXIT ROW. ELECTRICAL POWER WAS REMOVED FROM THE AIRCRAFT AND THE SMOKE STOPPED. THE PASSENGERS WERE ALL OFF OF THE AIRCRAFT A FEW SECONDS LATER AND THE DEPLANED WITHOUT ANY PROBLEMS OR PANIC. MAINTENANCE FOUND THE LOWER SIDEWALL LIGHT BALLAST AT SEAT 14A BURNED. THE BALLAST WAS REPLACED AND THE PANELS THAT WERE DISCOLORED BY THE SMOKE WERE CLEANED. OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050831001122005083100112EA 2005 8 31 A6WA200540280 120050806A215078279015 ACM CNDAIRCL600 CL6002B19 1900309EA RIGHT MALFUNCTIONED A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31411ZW7371 7569 RT PACK OVER PRESSURIZE ON BLEED SWITCH OVER, AND WOULD NOT RESET, AIR RETURN. REMOVED AND REPLACED RT AIR CYCLE MACHINE IAW AMM 21-51-10, OPS CHECK NORMAL. (M) 2L72 4F RTA21EA 20050831001132005083100113EA 2005 8 31 A6WA200540281 120050728A571256144A14 RIB CNDAIRCL600 CL6002B19 1900309EA FS 523.8 CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31405AW 7362 RIGHT MLG WHEEL WELL BATTERY RIB AT WS 48.30, FS 523.8 IS CRACKED AT UPPER RADIUS APPROX 1.25 INCH LONG. REPAIRED IAW REO 601R-57-51-046 REV B. (M) 2L72 4F RTA21EA 20050831001142005083100114NM 2005 8 31 ASAA0540314 120050626A5310654655056 FAILSAFE BOEING737 7374Q8 138447QNM FS 787 CUT A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 OKC - FOUND CORROSION ON FAIL/SAFE CHORD STATION 787 AT STRINGER 26R. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW 737-400 SRM 51-70-11. (M) 2L72 4F RTA16WE 20050831001152005083100115NM 2005 8 31 ASAA0540316 120050626A532065479573 THRESHOLD BOEING737 7374Q8 138447QNM FS 804-845 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 OKC - FOUND AFT PIT DOOR THRESHOLD INNER WEB IS CORRODED. REMOVED WEB, FABRICATED AND INSTALLED WEB IAW 737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20050831001182005083100118NM 2005 8 31 ASAA0540315 120050626A5320652072629 WEB BOEING737 7374Q8 138447QNM FS 440-492.4 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 OKC - FOUND FORWARD PIT THRESHOLD ATTACH WEB HAS CORROSION AT FASTENER HOLES. REMOVED WEB, FABRICATED AND INSTALLED WEB IAW 737-400 SRM 51-40-05 AND 51-40-02. (M) 2L72 4F RTA16WE 20050831001302005083100130SO 2005 8 31 SIMA200521601 120050728A531314533888001 STRINGER EMB 135 EMB135KL 3260302SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21815AE 145545 STRINGER 19R WAS FOUND TO BE CHAFED AT THE AFT BELLY PANEL CUTOUT. BLENDED THE CHAFED AREA. FABRICATED A REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB SRM 145/1142 REV 30, CHAPTER 53-24-02. (M) 2L72 4F RTT00011AT 20050831001322005083100132SO 2005 8 31 SIMA200521603 120050728A531314533888001 STRINGER EMB 135 EMB135KL 3260302SO CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21815AE8370 145545 ABI - STRINGER 19L WAS FOUND TO BE CHAFED AT THE AFT BELLY PANEL CUT OUT. BLENDED THE CHAFED AREA. FABRICATED A REPAIR ANGLE AND SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 29, CHAPTER 53-24-02. (M) 2L72 4F RTT00011AT 20050831001402005083100140NM 2005 8 31 USAA050969 120050803A5551 ATTACH FITTING BOEING737 7373B7 1384580NM HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US 23933 CLT - FOUND STAB LUG CORRODED, R1 LUG AFT FACE RIGHT HORIZONTAL STABILIZER. REMOVED CORROSION AND INSTALLED BUSHING IAW SRM 55-10-10. (M) 2L72 4F RTA16WE 20050831001422005083100142NM 2005 8 31 USAA050958 120050803A5551 BUSHING BOEING737 7373B7 1384580NM HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US 23933 CLT - FOUND LUG/BUSHING CORRODED 2 INCH BY .015 INCH, FORWARD SPAR ATTACH LUG AFT FACE LEFT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED BUSHING IAW SRM 55-10-10. (M) 2L72 4F RTA16WE 20050831001442005083100144NM 2005 8 31 USAA050956 120050803A5315BAC1505100246 FLOORBEAM BOEING737 7373B7 1384580NM BS 344 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US 23933 CLT - FOUND FLOORBEAM UPPER CHORD CORRODED 1 INCH BY 1 INCH, BS 344 BETWEEN LBL 55 - RBL 13. REMOVED UPPER CHORD OF FLOORBEAM. INSTALLED NEW CHORD AND ASSOCIATED REPAIR SPLICES IAW SRM 53-10-51. (M) 2L72 4F RTA16WE 20050831001462005083100146NM 2005 8 31 USAA050960 120050803A5315 FLOORBEAM BOEING737 7373B7 1384580NM FS 360 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US 23933 CLT - FOUND BEAM T-CAP CORRODED 6 INCHES, STATION 360, RBL 55 - RBL 61. REMOVED DAMAGED METAL, INSTALLED NEW T-CAP FROM RBL 35 - RBL 72 IAW SRM 53-00-51. (M) 2L72 4F RTA16WE 20050831001482005083100148NM 2005 8 31 USAA050957 120050803A5414 SKIN BOEING737 7373B7 1384580NM RT PYLON CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US50585 23933 CLT - FOUND PYLON SKIN CRACKED 2 INCHES, RT ENGINE PYLON UNDER PANEL 5858. REMOVED DAMAGE FABRICATED AND INSTALLED DOUBLER IAW TR 57-41-02. (M) 2L72 4F RTA16WE 20050901000062005090100006NM 2005 9 1 USAA050947 120050803A5551 BUSHING BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US50585 23933 CLT - Q6 - LUG/BUSHING, 2 INCH DIA X .015 TYPICAL, CORROSION; NO LEVEL OR TASK, L3, AFT FACE, LT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED NEW BUSHING IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050901000132005090100013EU 2005 9 1 USAA050977 120050805A5315D5347217220400 FLOORBEAM AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE FR 66-68 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19110UW13254 1112 PIT, S2, BEAM, .018, .028, .026, CORROSION; LEVEL 1 ASK JA-260-53500, FLOOR SUPPORT BEAM, FR66-68, Y1182 TO Y1292. DEVECTIVE PART REPLACED WITH IDENTICAL PART NUMBER. (K) 2L72 4F4 FRTA28NM E38NE 20050901000172005090100017NM 2005 9 1 USAA050941 120050803A5551 BUSHING BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US50585 23933 CLT - Q6 - LUG/BUSHING, 2 INCH DIA X .015 TYPICAL, CORROSION; NO LEVEL OR TASK. L5, FWD FACE LT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED BUSHING IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050901000252005090100025NE 2005 9 1 ALG2005F00060 220050806A73210319928730 FUEL CONTROL UROCOPEC120 EC120B 8680987EU TMECA ARRIUSARRIU2F NE ENGINE FAILED E ALGAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION HOHOVERING 1 SW03523AL 1262 ON THE FIRST HOVER FLIGHT OF THE DAY. IN HOVER FLIGHT, THE ROTOR RPM BLEED OFF AND WOULD NO RECOVER. NOTIFIED MAINTENANCE OF THE PROBLEM. FUEL CONTROL WAS REPLACED IAW MM. AC RETURNED TO SEVICE UPON COMPLETION OF ALL FUNCTIONAL CHECKS. (K) 1G72 3U3 UNCR0001RD E34NE 20050901000262005090100026NM 2005 9 1 USAA050942 120050803A5551 BUSHING BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU HORIZONTAL STAB CORRODED A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19588US 23933 CLT - Q6 - LUG/BUSHING, 2 INCH DIA X .015 TYPICAL, CORROSION; NO LEVEL OR TASK, L5, AFT FACE LT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED BUSHING IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050901000292005090100029NM 2005 9 1 HALA0500889 120050804A4997 GROUND WIRE BOEING767 76733AER 1385230NM APU STARTER SHORTED A HALAK NONE O OTHER ININSP/MAINT 1 WP13588HA 492070 33466 REMOVED AND REPLACED APU STARTER IAW AMM. DID NOT FIX DISCREPANCY. (LOANER STARTER FROM DELTA). TROUBLESHOT WIRING TO STARTER AND FOUND STARTER GROUND LEADS SHORTED AT TERMINAL/ AIRFRAME SIDE. REPAIRED, REPLACED GROUND LEADS AND TERMINAL ENDS, AND FABRICATED ATTACHING BRACKET IAW DWG AND SWPM. (K) 2L72 4F RTA1NM 20050901000302005090100030EA 2005 9 1 A6WA200540290 120050818A3230750006000 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NLG INOPERATIVE A A6WAO OTHER J WARNING INDICATION LDLANDING 1 GL31414ZW 7586 ON APPROACH, WHEN SELECTED GEAR DOWN GOR (GEAR DISAGREE AND NOSE DOOR) MASTER WARNING. NLG INDICATED UP AND LOCKED MLG DOWN. CYCLED GEAR WITH SAME INDICATIONS. PERFORMED QRH AND OBTAINED 3 GREEN. REMOVED AND REPLACED NLG SELECTOR VALVE AMM. OPS CHECK GOOD. LEAK CHECK GOOD. (K) 2L72 4F4 FRTA21EA E15NE 20050901000322005090100032NM 2005 9 1 USAA050906 120050728A5320BAC1498156 STIFFENER BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU BS 1006-1016 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US50585 23933 CLT - Q6 - STIFFENER, .5 INCH X 6 INCH CORROSION; NO LEVEL OR TASK. STR 26R, BS 1006-1016. REMOVED DAMAGE INSTALLED NEW STRINGER SECTION, ATTACH FITTING AND STIFFENER IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050901000332005090100033EA 2005 9 1 REX2005F00026 120050622A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A REXAO OTHER J WARNING INDICATION APAPPROACH 1 SO258721B6063 7721 (REF NR 05-077) FLAPS FAIL ON APPROACH AT 30, QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAPS AND PLACED ON 72 HOUR WATCH IAW AD-98-20-01. (K) 2L72 4F4 FRTA21EA E15NE 20050901000412005090100041NM 2005 9 1 AMTA200500637 120050809A2410727792M GENERATOR BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE RIGHT UNSERVICEABLE A AMTAO OTHER J WARNING INDICATION CRCRUISE 1 GL11520AT11248357 27976 EICAS MSG R GEN DRIVE DISPLAYED GEN DRIVE LIGHT ILLUMINATED, GEN DRIVE DISCONNECTED. REMOVED AND REPLACED IDG IAW M57-24-01. 2L72 4F4 FRTA2NM E12EU 20050901000422005090100042NM 2005 9 1 AMTA200500648 120050817A3350 SOCKET BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE EMERGENCY LIGHT DISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11522AT 29330 EGRESS LIGHT INOPERATIVE AT 28D AISLE. FOUND LAMP SOCKET UNPLUGGED. RESECURED AS REQUIRED. OPS CHECK GOOD. (K) 2L72 4F4 FRTA2NM E12EU 20050901000432005090100043NM 2005 9 1 USAA050992 120050808A5311 FRAME BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU BS 616 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US50585 23933 CLT, Q6 FRAME, 1.4 INCH CRACK, BS 616 RT BOTTOM OF FRAME INNER CHORD BS 616 RT. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER IAW TR 53-62-01. (K) 2L72 4F4 FRTA16WE E21EU 20050901000442005090100044EA 2005 9 1 ASOA05636 120050722A5330 DOUBLER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27833AS 7246 DURING C-CHECK, THE RT FS 718 DOUBLER AT STRINGER 10-12 RT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RT FS 718 DOUBLER AT STRINGER 10-12 RT IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050901000452005090100045EU 2005 9 1 KBM2005F00215 120050805A6420350A33214501 PITCH LINK SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE TAIL ROTOR CRACKED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19115SH2360 3141 UNIT HAS MULTIPLE CRACKS IN BUSHING, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050901000472005090100047NM 2005 9 1 USAA050989 120050805A532065528947 FLOOR SUPPORT BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU BS 540 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19444US40668 24862 BFM - Q2 - CHANNEL, 1 INCH AND 1.25 INCH, CRACKS (2), PAX CABIN FLOOR SUPPORT (CHANNEL) AT STA 540 LBL 1. DEFECTIVE PART REPLACED WITH IDENT PART. (K) 2L72 4F4 FRTA16WE E21EU 20050901000502005090100050NM 2005 9 1 USAA050988 120050805A5320BAC149673777075TSUPPORT BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU AFT CARGO CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19444US40668 24862 BFM, Q2, ZEE SUPPORT, 100 INCHES, CORROSION; LEVEL 1 TASK C53-202-01, AFT CARGO COMPT RT SUPPORT ZEE STA 727C-747. FABRICATED AND INSTALLLED NEW ZEE SUPPORT IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050901000512005090100051NM 2005 9 1 AMTA200500647 120050817A3350 BULB BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE EMERGENCY LIGHT LOOSE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11522AT 29330 EGRESS LIGHT INOPERATIVE AT 16D AISLE. RESECURED BULB. OPS CHECK GOOD. (K) 2L72 4F4 FRTA2NM E12EU 20050901000542005090100054NM 2005 9 1 AMTA200500635 120050808A3397 WIRE BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE EMERGENCY LIGHT DISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11522AT 29330 SEVERAL EGRESS LIGHTS INOPERATIVE FWD OF L2 DOOR. FOUND WIRE NOT CONNECTED. RECONNECTED AS REQUIRED. OPS CHECK GOOD. OK FOR SERVICE. (K) 2L72 4F4 FRTA2NM E12EU 20050901000552005090100055EA 2005 9 1 REX2005F00021 120050626A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE TE FLAPS ILLUMINATED A REXAO OTHER O OTHER TXTAXI/GRND HDL 1 SO25827AY497 8027 (REF NR: 05-082) FLAP FAIL CAUTION MESSAGE. QRH FOLLOWED. RESET FLAPS AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K) 2L72 4F4 FRTA21EA E15NE 20050901000562005090100056NE 2005 9 1 KBM2005F00219 220050704A721070BM055020 GEAR SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1D NE GEAR BOX MAKING METAL E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19215LA2911 2143 M05 REDUCTION GEAR, SUSPECTED OF CAUSING CHIP LIGHT. (K) 1G71 3U3 U H9EU E19EU 20050901000572005090100057EU 2005 9 1 KBM2005F00230 120050505A7160350A5410804 INTAKE SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1D NE ENGINE CRACKED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1953SH 2009 ARRIEL ENGINE INTAKE HAS MULTIPLE CRACKS, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050901000582005090100058 2005 9 1 KBM2005F00220 420050812A34225050031904 GYRO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE DIRECTIONAL SPINNING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19345SH588 3345 DIRECTIONAL GYRO, UNIT SPINS IN FLIGHT, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050901000592005090100059EU 2005 9 1 KBM2005F00226 120050505A3210350A41104621 SKID SHOE SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1D1 NE MLG CRACKED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1953SH 2009 RT FWD SKID SHOE CRACKED, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050901000612005090100061EU 2005 9 1 KBM2005F00225 120050627A3340DHS77516040 LIGHT SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1B 6OO30NE EXTERIOR FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH 2957 BODY LIGHT, FAILED. (K) 1G71 3U3 U H9EU E19EU 20050901000652005090100065EU 2005 9 1 KBM2005F00235 120050804A2121050145 BLOWER SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE MALFUNCTIONED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19966SH 3782 5 INCH BLOWER, BLOWING WARM AIR, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050901000692005090100069CE 2005 9 1 CVU2005F00003 120050818A3610442CW SHAFT BEECH 80 65B80 1152812CE LYC O720 IO720A1B 41546EA DRY AIR PUMP SHEARED E CVUAO OTHER O OTHER NRNOT REPORTED 1 WP1346MA 155 LD413 PUMP FAILED UNDER NORMAL OPERATING CONDITIONS (VFR, DAY). 1L72 3O3 O 3A20 1E15 20050901000702005090100070SO 2005 9 1 HYI2005F00005 220050818A8520642399 CONNECTING ROD CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO LT ENGINE UNSERVICEABLE E HYIAE ENGINE SHUTDOWN O OTHER APAPPROACH 1 NE01764EA 402C0237 AT 3000 FT, ON APPROACH, LT ENGINE BEGAN TO RUN ROUGH, PILOT PERFORMED FLOW CHECK, ALL ENGINE INSTRUMENTS APPEARED NORMAL, BOOST PUMPS TO LOW AS A PRECAUTIONARY. LT ENGINE CONTINUED TO RUN ROUGHER THEN SHUTDOWN, PILOT FEATHERED LT PROPELLER, LANDED WITHOUT INCIDENT. MAINT FOUND NR 5 CONNECTING ROD FAILED. (VIVIBLE THRU 8 INCHES IN DIAMETER HOLE IN CASE HALVES. REMOVED AND REPLACED LT ENGINE AND RELEASED AIRCRAFT BACK TO SERVICE. (NE01200505272) 1L72 3O3 O A7CE E8CE 20050901000712005090100071WP 2005 9 1 QOF2005F00002 120050810A7820C16932 MUFFLER ROBSINR44 R44RAVENII 7640122WP LYC O540 IO540* 41532EA EXHAUST SYSTEM CRACKED E QOFAO OTHER O OTHER NRNOT REPORTED 1 AL01144AK 10226 MUFFLER SWELLS AND CRACKS AT TAIL PIPE WELD. (K) 1G71 3O3 O H11NM 1E4 20050901000722005090100072WP 2005 9 1 QOF2005F00001 120050810A5313C04621 STRINGER ROBSINR44 R44RAVENII 7640122WP LYC O540 IO540* 41532EA FUSELAGE CRACKED E QOFAO OTHER O OTHER NRNOT REPORTED 1 AL01144AK 10226 TOP FORE AND AFT STRINGER CRACKED AT AFT MOST TAB AT JUNCTURE OF WELD. TURB TO TAB. (K) 1G71 3O3 O H11NM 1E4 20050901000762005090100076EA 2005 9 1 ASOA05658 120050807A5210601R3196059 STEP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27860AS 7433 7433 DURING AN A-CHECK, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN AND MATERIAL MISSING. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. (K) 2L72 4F4 FRTA21EA E15NE 20050901000772005090100077EA 2005 9 1 ASOA05632S 120050724A5260601R3807413 ANCHOR FITTING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27886AS 7531 DURING HANGAR MAINTENANCE, THE AFT ANCHOR FITTING ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFT ANCHOR FITTING ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050901000782005090100078EA 2005 9 1 REX2005F00009 120050819A2750860D10018ABC FCU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS FAILED A REXAO OTHER O OTHER APAPPROACH 1 SO258524A9727 7524 (REF NR: 05-098) FLAP FAILURE AT 0, QRH FOLLOWED UNEVENTFUL LANDING. REMOVED AND REPLACED FLAP ELECTRONIC UNIT (FECU) IAW AMM. (K) 2L72 4F4 FRTA21EA E15NE 20050901000792005090100079EA 2005 9 1 REX2005F00015 120050716A3220 LANDING GEAR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NOSE MALFUNCTIONED A REXAO OTHER J WARNING INDICATION APAPPROACH 1 SO258458A10934 7458 (REF NR: 05-088) NOSE GEAR WAS NOT DOWN AND LOCKED WITH THE LANDING GEAR SELECTOR IN THE DOWN POSITION, ON APPROACH. THE CREW RECYCLED THE GEAR UP AND DOWN. LANDING GEAR CAME DOWN NORMALLY ON SECOND ATTEMPT. QRH FOLLOWED, LANDING UNEVENTFUL. PERFORMED GEAR SWING IAW AMM. OPS CHECK GOOD. (K) 2L72 4F4 FRTA21EA E15NE 20050901000802005090100080EA 2005 9 1 ASOA05657 120050806A3350BF10044004 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27908EV 7654 DURING A GROUND INSPECTION, THE EMERGENCY EXIT LIGHT BY THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY BY THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050901000812005090100081EA 2005 9 1 ASOA05643 120050729A3350BM10006002 LAMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27842AS 7304 DURING OVERNIGHT MAINTENANCE, THE RT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE RT OVERWING EMERGENCY LIGHT. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050901000822005090100082NM 2005 9 1 AMTA200500650 120050818A3350 WIRE BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE EMERGENCY LIGHT DAMAGED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11514AT 27971 EGRESS LIGHTING OUT FROM 12 DEF FWD TO R2 DOOR. REPAIRED WIRING AS REQUIRED REF STD PRACTICES. CHECKS OK. (K) 2L72 4F4 FRTA2NM E12EU 20050901000852005090100085EA 2005 9 1 ASOA05648 120050804A3350OL3071BPEGPL LAMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE GALLEY BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27912EV 7728 DURING A GROUND INSPECTION, THE LOWER INTERIOR EMERGENCY LIGHT BY THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE LOWER INTERIOR EMERGENCY LIGHT BY THE SERVICE DOOR. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050901000862005090100086NM 2005 9 1 AMTA200500654 120050819A2613579601 DETECTOR BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE RT ENGINE UNSERVICEABLE A AMTAK NONE J WARNING INDICATION TXTAXI/GRND HDL 1 GL11561TZ 33526 AFTER ENGINE SHUTDOWN, STATUS MSG (R ENG OH LP2). REMOVED AND REPLACED RT ENGINE. OVERHEAT DETECTOR (NACELLE) IN A/W AMM. OPS CHECK NORMAL. (K) 2L72 4F4 FRTA2NM E12EU 20050901000872005090100087EA 2005 9 1 ASOA05630S 120050724A5321 FLOOR PANEL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27833AS 7246 DURING C-CHECK, CORROSION WAS FOUND BEYOND LIMITS ON THE PRESSURE FLOOR SKIN LT SIDE BETWEEN 409 AND 128 TO 559, RBL 36 AND 45. MAINTENANCE IS REPAIRING THE PRESSURE FLOOR SKIN LT SIDE BETWEEN 409 AND 128 TO 559, RBL 36 AND 45 IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050901000912005090100091EA 2005 9 1 REX2005F00019 120050628A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS FAILED A REXAO OTHER O OTHER APAPPROACH 1 SO258914A3239 7914 (REF NR: 05-084) FLAPS FAILED AT 8 DEGREES ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAPS AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K) 2L72 4F4 FRTA21EA E15NE 20050901000932005090100093EA 2005 9 1 ASOA05639 120050727A5210H341433 HANDLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR BINDING A ASOAK NONE O OTHER ININSP/MAINT 1 SO27868AS 7417 7417 DURING A GROUND INSPECTION, THE PASSENGER DOOR WAS FOUND HARD TO OPEN FROM THE OUTSIDE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR OUTER HANDLE. OPS CHECK GOOD. AIRCRAFT OF FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050901000942005090100094EA 2005 9 1 ASOA05637 120050726A5347601R3831225 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE BS 559+64 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27833AS 7246 DURING C-CHECK, THE LT SIDE WALL SEAT RAIL (TRACK) AT FS 559 +64 ABOVE THE BLOWOUT PANEL WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LT SIDE WALL SEAT RAIL (TRACK) AT FS 559 +64 IAW SRM. (K) 2L72 4F4 FRTA21EA E15NE 20050901000952005090100095EA 2005 9 1 REX2005F00022 120050625A2750860D10018 FCU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE TE FLAPS FAILED A REXAO OTHER O OTHER CLCLIMB 1 SO25827AY497 8027 (REF NR: 05-081) FLAPS FAIL ON CLIMB-OUT. QRH FOLLOWED UNEVENTFUL LANDING. REMOVED AND REPLACED FLAP ELECTRONIC UNIT (FECU). (K) 2L72 4F4 FRTA21EA E15NE 20050901000982005090100098EA 2005 9 1 UG82005F00006 120050815A3260 WARNING LIGHT CNDAIRCL600 CL6002B16 1900305EA GE CF34 CF343A 30015NE MLG ILLUMINATED E UG8AO OTHER P NO WARNING INDICATION APAPPROACH 1 GL23241FB 5102 (REF CNTRL NR PA05003) THERE WAS NOT GREEN (DOWN AND LOCKED) INDICATION ON THE NOSE GEAR. THERE WAS ALSO NO RED (UNSAFE) INDICATION. THE CREW WENT THROUGH THE REQUIRED CHECKLIST AND DECLARED AN EMERGENCY TO TOWER. (K) 2L72 4F4 FRTA21EA E15NE 20050901000992005090100099EA 2005 9 1 A6WA200540292 120050821A5210 DRAG ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31466AW 7899 PASSENGER DOOR AFT DRAG ANGLE CRAKED APPROX 1 INCH LONG ADJECENT TO DOOR ASSIST CABLE PULLEY BRACKET. CUT OUT DAMAGED AREA, PERFORMED EDDY CURRENT, FABED REPAIR ANGLE, SPLICES AND INSTALLED IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050901001002005090100100EA 2005 9 1 UG82005F00005 120050821A3411 PROBE CNDAIRCL600 CL6002B16 1900305EA GE CF34 CF343B1 NE PITOT/STATIC DAMAGED E UG8AO OTHER J WARNING INDICATION CLCLIMB 1 GL23599DA 5498 (REF CNTRL NR: PA05004) ALTITUDE SPLIT BETWEEN NR 1 AND NR 2 ALTIMETERS OF 250 FT AT 17,000 FT. THE RT PITOT/STATIC PROBE HAS IMPACT DAMAGE. (K) 2L72 4F4 FRTA21EA E15NE 20050901001012005090100101EA 2005 9 1 REX2005F00023 120050624A2750860D10018ABC FCU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS FAILED A REXAO OTHER O OTHER TXTAXI/GRND HDL 1 SO258524A 7524 (REF NR: 05-080) FLAP FAIL ON TAXI, RETURNED TO GATE. REMOVED AND REPLACED FLAP ELECTRONIC UNIT (FECU) IAW AMM, SYSTEM TESTS GOOD. (K) 2L72 4F4 FRTA21EA E15NE 20050901001022005090100102EU 2005 9 1 HAEA200500181 120050814A24203S2060DC168B1 GCU AMD FALC20FALCON 2720302EU GE CF700 CF7002D2 30010NE RADIO CABINET FAILED E HAEAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 SW05158TW4060 158 ENROUTE, AT FL280, BATTERY BUS ANNUNCIATOR LIGHT ILLUMINATED. RESET BUS IAW CHECKLIST AND REDUCED ELECTRICAL LOAD. PROBLEM CORRECTED FOR A FEW MINUTES FOLLOWED BY LOSS OF NR 1 GEN LIGHT. ATTEMPTED RESET OF NR 1 GEN UNSUCCESSFUL. NR 1 GEN WAS SHUT OFF AND ELECTRICAL LOAD FURTHER REDUCED. AFTER A FEW MINUTES NR 2 GEN LIGHT ILLUMINATED. CREW CONTACTED AIRPORT AND INFORMED OF MECHANICAL DIFFICULTIES. AIRCRAFT DIVERTED, NO EMERGENCY DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE DISPATCHED FOR REPAIR. FOUND NR 1 AND NR 2 GCU FAILED AND NR 2 GENERATOR FAULTY. REPLACED AND NR 1 AND NR 2 GCU, REPLACED NR 2 STARTER/GENERATOR. GROUND OPS GOOD. (K) 2L72 4F4 F A7EU E7EA 20050901001032005090100103EA 2005 9 1 ASOA05659 120050808A33506100976 LAMP BRUCE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27744EV 10157 DURING A GROUND INSPECTION, THE 2 AFT EMERGENCY CEILING LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMPS IN THE 2 AFT EMERGENCY CEILING LIGHTS. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA EOOO63EN 20050901001042005090100104EA 2005 9 1 REX2005F00010 120050820A2750860D10018ABC FCU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS FAILED A REXAO OTHER O OTHER APAPPROACH 1 SO258506C 7506 (REF NR: 05-097) FLAP FAILURE AT 30, QRH FOLLOWED UNEVENTFUL LANDING. REMOVED AND REPLACED FLAP ELECTRONIC UNIT (FECU) IAW AMM. (K) 2L72 4F4 FRTA21EA E15NE 20050901001082005090100108WP 2005 9 1 QOF2005F00000 120050808A5311C04621 FRAME ROBSINR44 R44RAVENII 7640122WP LYC O540 IO540* 41532EA FUSELAGE CRACKED E QOFAO OTHER O OTHER NRNOT REPORTED 1 AL01644AK 10364 TOP FORE AND AFT STRINGER CRACKED AT AFT MOST TAB AT JUNCTURE OF WELD. TUBE TO TAB. 2004 MODEL. (K) 1G71 3O3 O H11NM 1E4 20050901001092005090100109NE 2005 9 1 KBM2005F00216 220050805A7421CH34745 IGNITER SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE ENGINE BROKEN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19115SH 3141 9791 IGNITER INSULATOR BROKE LOOSE. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050901001112005090100111EA 2005 9 1 A6WA200540293 120050821A53206013501251 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FS 625 CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31466AW 7899 LT FS 625 OBLIQUE ANGLE CRACKED NEAR RADIUS APPROX 1.0 INCH LONG. REPLACED ANGLE IAW SRM. (K) 2L72 4F4 FRTA21EA E15NE 20050901001132005090100113WP 2005 9 1 CLC2005F00008 120050804A2497780002972 CABLE DOUG DC10 DC1030 3023501WP GE CF6 CF650C2 30018NE FUSELAGE BURNED A CLCAD RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TXTAXI/GRND HDL 1 SO29279AX 47816 ON TAXI OUT THE NR 2 AC BUSS CIRCUIT BREAKERS POPPED OUT. SMELLED SMOKE IN COCKPIT, TAXIED BACK TO THE RAMP. FOUND BURNED WIRES AND FEEDER CABLES BELOW LAVATORY FLOOR FOR THE NR 2 GENERATOR, ALL THREE PHASES. GENERATOR FEEDER CABLES FOR NR 1 AND 3 GENERATORS ARE ALSO ALL 3 PHASES. GENERATOR FEEDER CABLES FOR NR 1 AND 3 GENERATORS ARE ALSO DETERIORATED. ACCOMPLISHED REPLACEMENT, BY SPLICING OF CABLES AT STATIONS 410-492 AND STA 535 IAW MM, 9 EA FOR AC BUS TIE FOR NR 2 ENGINE. ALL ELECTRICAL SYSTEMS, OPS CHECK NORMAL. AC RETURNED TO REVENUE SERVICE. (K) 2L73 4F4 F A22WE E23EA 20050901001142005090100114EA 2005 9 1 REX2005F00020 120050620A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A REXAO OTHER O OTHER APAPPROACH 1 SO25836AY83 8036 (REF NR: 05-083) FLAPS FAILED AT 8 DEGREES ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAPS AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K) 2L72 4F RTA21EA 20050901001172005090100117EA 2005 9 1 ASOA05646 120050802A335020131A BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT DISCHARGED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27919EV6211 2518 7780 DURING A GROUND INSPECTION, THE EXTERIOR EMERGENCY LIGHTS AND THE AFT EMERGENCY FLOOR LIGHTS WERE FOUND TO BE DIM. MAINTENANCE REMOVED AND REPLACED THE FORWARD AND AFT EMERGENCY BATTERY PACKS. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050901001182005090100118WP 2005 9 1 KC82005F00006 220050816A732021011425 COMPUTER LEAR 35 36A 5170603CE GARRTTTFE731TFE73122B 01518WP LT ENGINE ERRATIC E KC8AO OTHER O OTHER NRNOT REPORTED 1 GL2371CK 035 BEFORE TAKEOFF, THE PILOT NOTICED THAT THE ENGINE IDLE AND TAKEOFF RPM ERRATIC IN THE NORMAL ENGINE CONTROL MODE, IN MANUAL ENGINE CONTROL MODE, ENGINE PERFORMANCE AND RPM`S WERE STABLE. REPLACED ENGINE FUEL CONTROL COMPUTER WITH SERVICEABLE REPAIRED COMPUTER AND PERFORMED ALL REQUIRED ENGINE RUNS AND ADJUSTMENTS IAW MM. (K) 2L72 4F4 F A10CE E6WE 20050901001192005090100119EA 2005 9 1 ASOA05644 120050729A3350BM10006002 LAMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27880AS 7606 DURING HANGAR MAINTENANCE, THE RT FWD EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE RT FWD EXTERIOR EMERGENCY LIGHT. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050901001212005090100121NM 2005 9 1 USAA050945 120050803A5551 BUSHING BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US50585 23933 CLT - Q6 - LUG/BUSHING, 2 INCH X .015 TYPICAL, CORROSION; NO LEVEL OR TASK, LT,AFT FACE, LT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED BUSHING IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050901001232005090100123EU 2005 9 1 KBM2005F00221 120050623A63229696 MOTOR SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1B 6OO30NE OIL COOLER RATCHETING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH3871 2957 MOTOR, MAKING RATCHETING NOISE. REMOVED AND REPLACE. (K) 1G71 3U3 U H9EU E19EU 20050901001242005090100124 2005 9 1 KBM2005F00233 420050806A3452066106200 TRANSPONDER SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE COCKPIT MALFUNCTIONED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH5367 2884 TRANSPONDER FREQUENCY OFF, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050901001262005090100126EA 2005 9 1 ASOA05656 120050805A5330 DOUBLER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27878AS 7590 DURING HANGAR MAINTENANCE, THE RT SIDE FS 640 DOUBLER WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RT SIDE FS 640 DOUBLER IAW SRM AND EO. (K) 2L72 4F4 FRTA21EA E15NE 20050901001282005090100128EA 2005 9 1 REX2005F00017 120050714A7830 SWITCH CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE THRUST REVERSER OUT OF ADJUST A REXAO OTHER J WARNING INDICATION APAPPROACH 1 SO258944B 7944 (REF NR: 05-086) ON APPROACH, CREW RECEIVED A LT THRUST REVERSER UNLOCKED MESSAGE WHEN THE THRUST REVERSERS WERE ARMED. FLIGHT CREW DECLARED AN EMERGENCY AND COMPLETED THE MEMORY AND QRH ITEMS. AN OTHERWISE UNEVENTFUL APPROACH AND LANDING WITHOUT THRUST REVERSERS WAS MADE. MAINTENANCE RIGGED THE THRUST REVERSER AND ADJUSTED THE STOW SWITCH. (K) 2L72 4F4 FRTA21EA E15NE 20050901001302005090100130EA 2005 9 1 REX2005F00004 120050824A2750601R930033 LEVER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS FAILED A REXAO OTHER O OTHER TXTAXI/GRND HDL 1 SO258696C6678 7696 ( REF NR: 05-103) FLAP FAILURE ON TAXI OUT. REMOVED AND REPLACED FLAP HANDLE IAW AMM. (K) 2L72 4F4 FRTA21EA E15NE 20050901001322005090100132EA 2005 9 1 REX2005F00003 120050824A2750860D10018 FCU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS FAILED A REXAO OTHER O OTHER APAPPROACH 1 SO258524A9753 7524 ( REF NR: 05-104) FLAP FAILURE. REMOVED AND REPLACED FLAP ELECTRONIC CONTROL UNIT (FECU) IAW AMM. (K) 2L72 4F4 FRTA21EA E15NE 20050901001332005090100133EA 2005 9 1 REX2005F00008 120050819A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS FAILED A REXAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SO258696C6657 7696 ( REF NR 05-099) UPON CLIMBOUT, FLAPS FAIL WHEN SELECTED UP. DECLARED EMERGENCY, DIVERTED. RESET FLAPS AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K) 2L72 4F4 FRTA21EA E15NE 20050901001342005090100134EA 2005 9 1 REX2005F00006 120050823A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS FAILED A REXAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 SO258980A2180 7980 (REF NR: 05-101) FLAP FAILURE MESSAGE ON TAXI. RESET SYSTEM PLACED FLAPS ON 72 HOUR WATCH IAW AD 98-20-01. (K) 2L72 4F4 FRTA21EA E15NE 20050901001352005090100135EA 2005 9 1 REX2005F00007 120050819A215078279015 ACM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LEFT OVERHEATED A REXAO OTHER MJ OVER TEMP WARNING INDICATION TXTAXI/GRND HDL 1 SO258921B3497 7921 (REF NR: 05-100) AT GATE LT AIR CYCLE MACHINE (ACM) PACK OVERHEAT MESSAGE AND SMOKE NOTED IN COCKPIT. DEFERRED LT ACM IAW MEL. (K) 2L72 4F4 FRTA21EA E15NE 20050901001362005090100136EA 2005 9 1 REX2005F00011 120050810A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS FAILED A REXAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SO258505Q10159 7505 (REF NR: 05-096) FLAPS FAILED AT 20 WHEN SELECTED TO 30 ON APPROACH. RESET FLAPS AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K) 2L72 4F4 FRTA21EA E15NE 20050830000622005083000062NM 2005 8 30 SWAA052590 120050827A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29432WN 33715 DURING SCHEDULED RON CHECK, FOUND FWD CABIN EEPLS TRACK LIGHT LOOSE. SECURED TRACK PER MM. 2L72 4F RTA16WE 20050830000842005083000084NM 2005 8 30 ASAA0540305 120050626A532265465542 SHEAR TIE BOEING737 7374Q8 138447QNM FS 847 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 OKC - BS 847 FRAME SHEAR TIE IS CORRODED BETWEEN STRINGER 27L AND 27R. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR SHEAR TIE AND FLOOR SUPPORT CLIP IAW 737-400 SRM 53-00-7, 51-30-01, AND 51-40-1. (M) 2L72 4F RTA16WE 20050830000852005083000085NM 2005 8 30 USAA050950 120050803A5551 BUSHING BOEING737 7373B7 1384580NM HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US 23933 CLT - FOUND LUG/BUSHING CORRODED 2 INCHES IN DIAMETER BY .015 TYPICAL, L6, AFT FACE LEFT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED NEW BUSHING IAW SRM 53-10-10. (M) 2L72 4F RTA16WE 20050830000872005083000087NM 2005 8 30 ASAA0540300 120050626A53306545767193 SKIN BOEING737 7374Q8 138447QNM FS 370 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 OKC - FOUND DENT IN FUSELAGE EXTERIOR SKIN BS 370 BELOW STRINGERS 17R. REMOVED DAMAGED SKIN, FABRICATED AND INSTALLED REPAIR IAW 737-400 SRM 53-00-01 FIGURE 231. (M) 2L72 4F RTA16WE 20050830000962005083000096NM 2005 8 30 AMTA200500633 120050805A3350 WIRE BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE EMERGENCY LIGHT DISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11518AT 27974 FLOOR PATH EMERGENCY INOPERATIVE FROM ROW 9 TO R2 DOOR EXIT MARKER. RECONNECTED LIGHT ASSY AT ROW 9, OPS CHECK GOOD. (K) 2L72 4F4 FRTA2NM E12EU 20050830000972005083000097NM 2005 8 30 05FDEA02708 120050829A5311 FRAME BOEING727 727227 1384078NM BS 580 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 FORWARD CARGO BAY, FRAME IS DENTED AT BS 580 BETWEEN STRINGER LT 24 AND LT 23. REPAIRED FRAME IAW SRM 51-40-3. 2L73 4F A3WE 20050830001042005083000104EA 2005 8 30 REX2005F00001 120050802A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A REXAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO258965E 7965 (REF NR: 05-093) FLAPS FAIL AT 20 WHEN SELECTED ON TAXI. RESET SYSTEM AND PLACED 72 HOUR WATCH IAW AD 98-20-01. (K) 2L72 4F4 FRTA21EA E15NE 20050830001052005083000105EU 2005 8 30 BA05018 120050820A3350321431 BATTERY PACK AIRBUS330 A330323 3930335EU EMERGENCY LIGHTSDISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19673UW 337 PHL - THE L-2 DOOR FAILED THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE BATTERY PACK AT THE L-2 DOOR. SYSTEM TESTS OK. 2L72 4F RTA46NM 20050830001062005083000106NM 2005 8 30 05FDEA02689 120050826A57436519257 FITTING BOEING727 72722 1384002NM ZONE 700 MISDRILLED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25190FE 19083 LEFT AND RIGHT LOWER FORWARD TRUNNION TEE ATTACHED FITTINGS PART NUMBER 65-19257-6 /5/7/8, REQUIRES REWORK, REFERENCE:EO/7-5710-7-2314D PT-4. REWORKED LEFT AND RIGHT LOWER FORWARD TRUNNION ATTACH TEE FITTINGS PART NUMBERS 65-19257-5/6/7/8 IAW FEDEX EA 7-5710-91277 REV A.TITTLE WINGS, MLG TRUNNION FITTINGS OVERSIZED HOLES BUSHING REPAIR AD 2004-18-08. REFERENCE FEDEX N/R N00031 AND N/R N00033. 2L73 4F A3WE 20050830001082005083000108NE 2005 8 30 05FDEA02691 220050825A7200 ENGINE DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE NR 2 FLUCTUATES A FDEAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 SO25616FE279397561 48747 NR 2 ENGINE DISPLAYED GRADUAL OIL LOSS TO AN INDICATION OF 1 QT JUST BEFORE DESCENT TO KIX. OIL PRESSURE BEGAN TO FLUCTUATE A LITTLE AND DURING DESCENT AN ALERT "OIL PRESS LO" DISPLAYED. PRECAUTIONARY SHUTDOWN PER QRH. NR 2 OIL PRESSURE WAS AROUND 35 PSI WITH 1 AND 3 ABOUT 50 PSI. IN IDLE DESCENT PRESSURE WAS SOMEWHERE BELOW 30 PSI WHEN "LO PRESS" ALERT CAME ON. 2L73 4F4 FRTA22WE E13NE 20050830001092005083000109WP 2005 8 30 05FDEA02692 120050825A2697 WIRE HARNESS DOUG MD10 MD1010F 3022112WP FIRE LOOP FAILED A FDEAEFJAENGINE SHUTDOWN ACTIVATE FIRE EXT. DUMP FUEL UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25357FE 46939 AFTER TAKEOFF ON CLIMB-OUT AT 17,000 FEET, GOT INTERMITTENT NR 2 ENG FIRE INDICATION, 1ST IN FUEL LVR THEN PASSING 18,000 GOT FIRE WARNING, ALL INDICATION NR 2 ENG, LIGHTS, BELL FOLLOWED QRH, SHUTDOWN NR 2 ENG. LANDED ASAP AT KATL. FIRED BOTH BOTTLES AND STILL HAD INTERMITTENT INDICATIONS NR 2 ENG REPLACED THE NR 2 RT FIRE BOTTLE PER M/NM 26-21-01-4. REPLACED HARNESS ASSY'S P1-8224 TO P1-8694 AND ASSY. P1-8225 TO P1-8693 REMOVED AND REPLACED THE NR 1 FIRE EXTINGUSHING BOTTLE FOR THE NR 2 ENG. 2L73 4F RTA22WE 20050830001102005083000110 2005 8 30 05FDEA02694 420050827A3418 STALL WARNING BOEING727 72722 1384002NM NR 1 MALFUNCTIONED A FDEAO OTHER NB FALSE WARNING SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO25166FE 18863 ON TAXI OUT, NR 1 STALL WARNING STICK SHAKER ACTIVATED MOMENTARILY THEN STOPPED. ABOUT 3 MINUTES LATER, IT REACTIVATED AND PULLED THE NR 1 STALL WARNING C\B TO DEACTIVATE. ON TAXI IN SMOKE BEGAN TO EMANATE FROM BEHIND GLARE SHIELD. EVACUATED AIRCRAFT. REMOVED AND REPLACED ACM TEMP SWITCH PER M/M REF 21-51-011-4. 2L73 4F A3WE 20050830001112005083000111NM 2005 8 30 UPS05245266 120050806A55326517561 SKIN BOEING727 72730C 1384009NM BS 1385 TO 1485 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919UP 19012 INSPECTION TYPE: C, NR 2 ENG UPPER HORIZ FIREWALL SURFACE TO VERT FIN, LT, ANGLE HAS EVIDENCE OF CORROSION ON INNER SURFACE OF VERT FIN SKIN BETWEEN STA 1385 AND 1425 APPROX. SKIN REMOVED AND FOUND CORRODED O/S LIMITS, CHORD BETWEEN BS 1384 AND 1484 FOUND CORRODED AND CHORD REMOVED. NEW CHORD SPLICE IN WITH REPAIR ANGLES AND SKIN REPLACED IAW UPS AUTH 727-53-20187 AND 727-55-20049. 2L73 4F A3WE 20050830001122005083000112NM 2005 8 30 UPS05645269 120050828A2560 SMOKE GOGGLES BOEING767 76734AF 1385212NM COCKPIT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01334UP 32844 INSPECTION TYPE:N/A CAPTAIN'S SMOKE GOGGLES ARE CRACKED. REMOVED AND REPLACED CAPTAIN'S SMOKE GOGGLES. 2L72 4F RTA1NM 20050831000022005083100002NM 2005 8 31 SWAA052609 120050829A53116546526 FRAME BOEING737 7373H4 1384600NM BS 400 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29617SW 27700 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L TO STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050831000222005083100022NM 2005 8 31 2005UALA00872 120050823A3350582233 BATTERY BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHTSINOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29173UA 24380 EMERGENCY LIGHTS AT LEFT BODY FAIRING 4 EA INOP. REPLACED BATTERY ASSY. 2L74 4F4 FRTA20WE E24NE 20050831000402005083100040 2005 8 31 QXEA200501196 420050829A3418 WARNING LIGHT BOMBDRDHC8 DHC8402 1390042NM STALL WARNING ILLUMINATED A QXEAO OTHER J WARNING INDICATION LDLANDING 1 NM09417QX 4086 SEA FLIGHT 2398: ON LANDING ROLLOUT, PUSHER SYSTEM FAIL CAUTION LIGHT ILLUMINATED. PER CHECKLIST, ACCOMPLISHED STALL WARNING TEST, NO HELP. MAINTENANCE COMPLIED WITH FIM TASK 27-33-00-810-127. OPS CHECK GOOD IAW AMM 27-33-00, PAGE 501. CAUTION LIGHT DID NOT ILLUMINATE. NO FAULTS IN CDS. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050831000472005083100047NM 2005 8 31 AWXA200501015 120050808A5330655298871 SKIN PANEL BOEING737 7373G7 1384595NM BS 956.5 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28311AW 24712 MCN - MAJOR REPAIR - DURING C15 CHECK DISCOVERED SKIN CRACK, .65 INCHES IN LENGTH, ADJACENT TO THE FORWARD LOWER CORNER OF THE L2 DOOR CUTOUT AT BS 956.5 AND STR 17L. MAINTENANCE TRIMMED OUT CRACKED AREA FORWARD LOWER CORNER OF THE L2 DOOR AT BS 956.5 AND STR 17L IAW BOEING 737-300 SRM 53-00-01 FIG 201. FABRICATED FILLER, DOUBLER AND TRIPLER IAW BOEING 737-300 SRM 53-00-01 FIG 201. INSTALLED FABRICATED REPAIR PARTS FORWARD LOWER CORNER OF THE L2 DOOR AT BS 956.5 AND STR 17L IAW BOEING 737-300 SRM 53-00-01 FIG 201. 2L72 4F RTA16WE 20050831001062005083100106NM 2005 8 31 DHL2005741005 120050831A3234 HANDLE BOEING727 7272Q9 138448MNM MLG MALFUNCTIONED A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01741DH 21931 AFTER T/O RED DOOR LIGHT, & AMBER RT GEAR DOOR LIGHTS ILLUMINATED WITH GEAR HANDLE IN OFF POSITION. ACCOMMPLISH AOM PROCEDURES, DOOR LIGHTS EXTINGUISHED WHEN GEAR HANDLE IN UP POSITION. PERFORMED OP'S CHECK OF RT GEAR DOOR, DUMMY RETRACTION, CHECK GOOD PER MM 32-12-01. 2L73 4F RTA3WE 20050831001072005083100107EA 2005 8 31 05106 120050820A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ILLUMINATED A REXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO258800G 7800 AFTER TAKEOFF AND CLIMBOUT FROM XNA, THE FLIGHT CREW RECEIVED A NUMBER 2 ENGINE THRUST REVERSER UNLOCKED MESSAGE AND THE N1 REV ICON APPEARED. THE FLIGHT CREW REDUCED POWER ON NUMBER TWO ENGINE AND ACCOMPLISHED MEMORY ITEMS. THE FLIGHT CREW DECLARED AN EMERGENCY AND RETURNED VFR TO XNA. AN OTHERWISE UNEVENTFUL APPROACH AND LANDING WAS MADE. CONTRACT MAINTENANCE CONFIRMED THAT THE REVERSER WAS UNLOCKED. MAINTENANCE STOWED, PINNED AND DEFERRED THE THRUST REVERSER. AIRCRAFT DEPARTED AND RETURNED TO DTW. 2L72 4F RTA21EA 20050831001082005083100108WP 2005 8 31 0501359949 120050829A2133 SEAL DOUG DC9 DC931 3022065WP OUTFLOW VALVE MIGRATED A NWAABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL018928E 45865 WHEN CLIMBING THROUGH FL250 THE CREW NOTICED THE CABIN ALTITUDE WAS AT 8000 FEET AND CLIMBING AT 500 FPM. THE AIRCRAFT WAS LEVELED AT FL250 BUT THE CABIN CONTINUED TO CLIMB. CREW DECLARED AN EMERGENCY, INITIATED A RAPID DESCENT TO 10,000 FEET, COMPLIED WITH THE EMERGENCY CHECKLIST & COM, AND DIVERTED TO BNA. LANDING WAS UNEVENTFUL AND MAINTENANCE FOUND THE SEAL MIGRATING OUT OF POSITION ON THE NEGATIVE PRESSURE RELIEF VALVE PREVENTING THE VALVE FROM SEATING. THE SEAL WAS REINSTALLED ON THE RELIEF VALVE, A VESSEL LEAK CHECK PERFORMED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F A6WE 20050831001092005083100109WP 2005 8 31 DHL2005873002 120050829A3350 BATTERY DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT DISCHARGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ 46091 EMERGENCY LIGHTS BATTERY DISCHARGED DUE TO LEFT IN ARMED POS. ALLOWED EMERGENCY LIGHT BATTERIES TO CHARGE TO PEAK AND TESTED PER DACO M/M 33-50-0. OP CHECKS SERVICE. 2L74 4F RT4A25 20050831001162005083100116NM 2005 8 31 ASAA0540318 120050626A5313654653120 STRINGER BOEING737 7374Q8 138447QNM FS 500B CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 OKC - FOUND CORROSION AT BS 500B STRINGER 26-27 RT. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PIECES IAW 737-400 SRM 53-00-07 FIG 203. (M) 2L72 4F RTA16WE 20050831001192005083100119NM 2005 8 31 ASAA0540320 120050626A5754 SKIN BOEING737 7374Q8 138447QNM NR 4 SLAT DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS PA625 25106 OKC - FOUND NR 4 SLAT IS DELAMINATED ON T/E AT INBOARD END. REMOVED DAMAGED AREA, FABRICATED SKIN FILLER AND DOUBLER AND INSTALLED REPAIR PIECES IAW B737-400 SRM 51-70-10 REPAIR 21. (M) 2L72 4F RTA16WE 20050831001212005083100121NM 2005 8 31 ASAA0540311 120050626A5322654653120 SHEAR TIE BOEING737 7374Q8 138447QNM FS 500B CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 OKC - FOUND CORROSION AT BS 500B STRINGER 26L-27L. REMOVED CORROSION AND REPAIRED SHEAR TIE AT BS 500B IAW B737-400 SRM 53-00-07 FIG 203. (M) 2L72 4F RTA16WE 20050831001222005083100122NM 2005 8 31 ASAA0540312 120050626A5322654653120 SHEAR TIE BOEING737 7374Q8 138447QNM FS 500B CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 OKC - FOUND CORROSION AT BS 500B STRINGER 26L-27L. REMOVED CORROSION ON SHEAR TIE, FABRICATED AND INSTALLED REPAIR IAW B737-400 SRM 53-00-07 FIG 101 AND 203. (M) 2L72 4F RTA16WE 20050831001242005083100124NM 2005 8 31 ASAA0540319 120050626A575465C26602311 SKIN BOEING737 7374Q8 138447QNM NR 2 SLAT DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 OKC - FOUND NR 2 SLAT INBOARD UPPER CORNER DAMAGED. REMOVED PREVIOUS REPAIR, FABRICATED AND INSTALLED SKIN AND DOUBLER IAW 737-400 SRM 51-70-10. (M) 2L72 4F RTA16WE 20050831001262005083100126NM 2005 8 31 ASAA0540301 120050626A5754 SKIN BOEING737 7374Q8 138447QNM NR 4 SLAT CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 OKC - FOUND NR 4 SLAT, LOWER SURFACE OUTER SKIN CRACKED AT OUTBOARD END. CUT OUT DAMAGE, INSTALLED FILLER AND DOUBLER IAW 737-400 SRM 57-43-01 FIGURE 206. (M) 2L72 4F RTA16WE 20050831001282005083100128NM 2005 8 31 ASAA0540309 120050626A575465C26602311 SKIN BOEING737 7374Q8 138447QNM NR 2 SLAT DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 OKC - FOUND NR 2 SLAT INBOARD T/E DELAMINATED AT CORNER. REMOVED DAMAGE, FABRICATED SKIN AND DOUBLER AND INSTALLED REPAIR PIECES IAW 737-400-SRM 51-70-10. (M) 2L72 4F RTA16WE 20050831001512005083100151NM 2005 8 31 USAA050965 120050803A5320 ANGLE BOEING737 7373B7 1384580NM CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US50585 23933 CLT - FOUND C-ANGLE CORRODED 2 INCHES, UPPER SURFACE OF FORWARD ENTRY DOOR THRESHOLD C-ANGLE. REMOVED DAMAGED ANGLE AND REINSTALLED NEW ANGLE IAW SRM 53-10-15. (M) 2L72 4F RTA16WE 20050901000152005090100015EA 2005 9 1 ASOA05649 120050804A3510S70477 LINE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE COCKPIT OXYGEN LEAKING A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27719EV 10099 DURING CLIMB OUT, AT APPROXIMATELY 4,000 FT, THE CREW HEARD A LOUD NOISE FOLLOWED BY A HISSING SOUND FROM BEHIND THE COCKPIT. THE CREW THEN RECEIVED A LOW OXYGEN MESSAGE ON EICAS. AN EMERGENCY WAS DECLARED AND AIRCRAFT RETURNED TO DEPARTURE, LANDING SAFETLY. MAINTENANCE REMOVED AND REPLACED THE OXYGEN LINE AT THE OBSERVERS MASK BOX. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA EOOO63EN 20050901000272005090100027NM 2005 9 1 USAA050943 120050803A5551 LUG BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US50585 23933 CLT - Q6 - LUGS, CORROSION; NO LEVEL OR TASK, L2/L5 BORES, LT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED BUSHINGS IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050901000282005090100028NM 2005 9 1 USAA050990 120050808A5340 SUPPORT BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU BS 727D,S8L,S9L CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US50585 23933 CLT, Q6, PSU SUPPORT RAIL, 2 CRACKS, .1250 INCH, .1875 INCH, CRACK, BS 727D BETWEEN S8L AND 9L. DAMAGE REMOVED, INSTALLED REPAIR ANGLES IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050901000352005090100035NE 2005 9 1 REX2005F00031 220050530A7261 CARBON SEAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE ENGINE DAMAGED A REXAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 SO258940E 7940 (REF NR: 05-072) ON DECENT, THE RT ENGINE OIL PRESSURE WARNING ILLUMINATED. THE FLIGHT CREW NOTED THAT THE INDICATED PRESSURE WAS LOW, BUT STILL IN THE GREEN ARC. FLIGHT CREW REVIEWED QRH PROCEDURES FOR A POSSIBLE ENGINE FAILURE. MINUTES LATER THE OIL PRESSURE INDICATION DROPPED INTO THE RED ARC. CAPTAIN EXECUTED QRH PROCEDURES, SHUTDOWN ENGINE AND DECLARED AN EMERGENCY. AN OTHERWISE NORMAL APPROACH AND LANDING WAS MADE. MAINTENANCE DETERMINED PROBLEM TO BE OIL LOSS CAUSED BY A DAMAGED EDP CARBON SEAL ON THE ACCY GEARBOX. CARBON SEAL WAS REPLACED, OIL TOPPED OFF AND A LEAKING RUN WAS PERFORMED WITH NO FURTHER LEAKAGE NOTED. AIRCRAFT WAS RELEASED FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050901000522005090100052NM 2005 9 1 USAA050991 120050808A534065516989 SPLICE BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU BS 907 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US50585 23933 CLT, Q6, SPLICE CRACKED AT STA 907, S4R. REMOVED AND REPLACED STRINGER SPLICE IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050901000602005090100060 2005 9 1 KBM2005F00231 420050625A34225050031904 GYRO SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1D NE DIRECTIONAL MALFUNCTIONED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1953SH 490 2009 DIRECTIONAL GYRO FLAG GOES ON IN FLIGHT. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050901000622005090100062EU 2005 9 1 KBM2005F00227 120050505A6220117775P BALL JOINT SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1D NE STARFLEX FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1953SH 2009 BALL JOINTS, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050901000642005090100064EU 2005 9 1 KBM2005F00224 120050627A2121071403701 FAN SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1B 6OO30NE AVIONICS BAY FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH 2957 AVIONICS FAN WAS POPPING CIRCUIT BREAKER, REPLACED WITH NEW. (K) 1G71 3U3 U H9EU E19EU 20050901000752005090100075EA 2005 9 1 ASOA05608 120050717A335058351 STRIP CNDAIR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN MISSING A ASOAK NONE O OTHER ININSP/MAINT 1 SO27878AS 7590 DURING A GROUND INSPECTION, AN EMERGENCY FLOOR LIGHT ORANGE STRIP WAS FOUND MISSING. MAINTENANCE REPLACED AN EMERGENCY FLOOR LIGHT, ORANGE STRIP. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050901000832005090100083EA 2005 9 1 ASOA05607 120050717A5260601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR SEPARATED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27923EV 7731 7826 DURING AN A-CHECK, THE PASSENGER DOOR BOTTOM STEP ATTACH BRACKET TO THE STAY ROD WAS FOUND SEPARATING FROM THE STEP. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. (K) 2L72 4F4 FRTA21EA E15NE 20050901000882005090100088EA 2005 9 1 ASOA05629S 120050724A5321 FLOOR PANEL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE COCKPIT CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27833AS 7246 DURING A C-CHECK, CORROSION WAS FOUND BEYOND LIMITS ON THE PRESSURE FLOOR SKIN RT SIDE BETWEEN 409 AND 128 TOO 559 RBL AND 36 AND 45. MAINTENANCE IS REPAIRING THE PRESSURE FLOOR SKIN RT SIDE BETWEEN 409 AND 128 TO 559, RBL 36 AND 45 IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050901000922005090100092EA 2005 9 1 ASOA05638 120050726A33501317 LAMP BRUCE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27912EV 7728 DURING A ROUTINE OVERNIGHT CHECK, THE LT FORWARD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE LT FORWARD EMERGENCY LIGHT. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050901000962005090100096EA 2005 9 1 ASOA05640 120050727A5210601R3186067 STEP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27839AS 7284 7284 DURING A GROUND INSPECTION, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ASSEMBLY AND STEP RETRACTION ARM ON THE PASSENGER DOOR. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050901001062005090100106CE 2005 9 1 FFS2005F00006 120050725A532011443006019 SPLICE BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA FS 523.5 MISMANUFACTURED G FFSAO OTHER O OTHER NRNOT REPORTED 1 AL01575P UC95 THE FRAME SPLICES ADJACENT TO STRINGER 4L ON FUSELAGE FRAME AT FS 523.5, HAD POOR FIT-UP BETWEEN THE LT FRAME (114-430059-5), THE TOP FRAME (114-430127-3) AND THE LT SPLICE CLIP (114-43006019). THERE WAS A 0.030 TO 0.060 INCH GAP BETWEEN THE FRAME FLANGE AND THE FLANGE OF THE SPLICE CLIP WITH THE RIVET SHANKS VISIBLE. THE GAP BETWEEN THE FRAME FLANGE AND THE SPLICE CLIP WAS SIMILAR ON THE RT SIDE AND ALSO ON LT AND RT OF THE FS 531.0 FRAME AND FS 544.25 FRAME LT AND RT TO A LESSER DEGREE. ONE RIVET HEAD WAS MISSING FROM THE FLANGE AT THE FS 544.25, RT SIDE SPLICE AND SEVERAL HEADS (POPPED OFF) WHEN REMOVING THE RIVETS FOR REPAIR. (K) 2L72 4T4 TRTA24CE E4EA 20050901001102005090100110EU 2005 9 1 ASOA05661 120050809A33503011162 COVER AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE EMERGENCY LIGHT MISSING A ASOAK NONE O OTHER ININSP/MAINT 1 SO27633AS 344 DURING HANGAR MAINTENANCE, THE EMERGENCY FLOOR LIGHT COVER AT ROW 1-D WAS FOUND WITH THE WORK (EXIT) MISSING. MAINTENANCE REMOVE AND REPLACED THE EMERGENCY EXIT FLOOR LIGHT COVER AT ROW 1-D. (K) 2H72 4T4 TRTA53EU E20NE 20050901001162005090100116NE 2005 9 1 ASOA05660 220050808A7261CF343B1 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RIGHT OVERSERVICED A ASOAO OTHER WJ INADEQUATE Q C WARNING INDICATION CRCRUISE 1 SO27871AS 7537 DURING CRUISE, AT APPROX 28,000 FEET, RT ENGINE OIL TEMP INDICATED IN YELLOW RANGE AT APPROX 160 DEGREES C, THEN INCREASED INTO RED RANGE INDICATING A HIGH OF 165 DEGREES C WITH RT ENGINE OIL PRESSURE INDICATING 44-50 PSI. CREW COMPLIED WITH THE QRH AND REDUCED THE RT ENGINE TO IDLE. AFTER SEVERAL MINUTES, RT ENGINE OIL TEMP DECREASED TO NORMAL AND WAS LEFT AT IDLE FOR THE REMAINDER OF FLIGHT. EMERGENCY WAS DECLARED AND AC LANDED SAFELY. MAINTENANCE FOUND RT ENGINE OIL OVER SERVICED. DRAINED THE ACCY GEAR BOX, PROPERLY SERVICE THE ENGINE OIL AND COMPLIED WITH HIGH POWER GROUND RUNS. ENGINE OIL TEMPERATURE AND PSI INDICATIONS WERE NORMAL. OPS CHECK GOOD. AC OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050901001202005090100120EA 2005 9 1 ASOA05647 120050730A5210601R380741 ANCHOR FITTING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27913EV 7731 DURING HANGAR MAINTENANCE, THE AFT ANCHOR FITTING ON THE PASSENGER DOOR WAS FOUND CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFT ANCHOR FITTING ON THE PASSENGER DOOR. (K) 2L72 4F4 FRTA21EA E15NE 20050901001222005090100122NM 2005 9 1 USAA0540944 120050803A5551 BUSHING BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US50585 23933 CLT - Q6 - LUG/BUSHING, 2 INCH X .015 TYPICAL, CORROSION; NO LEVEL OR TASK, L2, FWD FACE LT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED BUSHING IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050901001392005090100139EA 2005 9 1 REX2005F00013 120050720A2751 SENSOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS FAILED A REXAO OTHER O OTHER APAPPROACH 1 SO258560F8790 7560 (REF NR 05-090) FLAPS FAIL AT 4 DEGREES ON FINAL. PERFORMED RIGGING OF LT AND RT BRAKE POSITION SENSING UNIT ( BPSL) IAW AMM. (K) 2L72 4F4 FRTA21EA E15NE 20050901001422005090100142EA 2005 9 1 REX2005F00030 120050611A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS FAILED A REXAO OTHER O OTHER APAPPROACH 1 SO258598B7772 7598 (REF NR 05-073) FLAPS FAIL MESSAGE WHEN GOING FROM 20 TO 30 DEGREES. EMERGENCY DECLARED QRH FOLLOWED UNEVENTFUL LANDING WITH FLAPS 20. RESET FLAPS AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K) 2L72 4F4 FRTA21EA E15NE 20050901001452005090100145EU 2005 9 1 MHI2005F00000 120050721A5532355A1405220202 SKIN AEROSPAS355 AS355F1 8680810EU ALLSN 250C 250C20F 03013GL STABILIZER CRACKED E MHIAO OTHER O OTHER NRNOT REPORTED 1 EA25406LH 5111 840075 (REF NR: 104942) DURING INSPECTION, FOUND THE UPPER STABILIZER FIN, RT LWR DOUBLER AND NOSE SKIN CRACKED FROM THE 2ND FORWARD RIVET OF THE DOUBLER ACCROSS THE NOSE SKIN. REPLACED STABILIZER WITH SERVICEABLE STABILIZER. (K) 1G72 3U3 U H11EU E4CE 20050901001462005090100146EA 2005 9 1 REX2005F00033 120050527A5610601R3303317 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE COCKPIT CRACKED A REXAO OTHER O OTHER APAPPROACH 1 SO258891A3471 7891 (REF NR: 05-070) CAPTAINS WINDSHIELD CRACKED. REMOVED AND REPLACED CAPTAINS LT FRONT WINDSHIELD IAW AMM. (K) 2L72 4F4 FRTA21EA E15NE 20050901001472005090100147EA 2005 9 1 REX2005F00043 120050505A2750855D10011 BPSU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS FAILED A REXAO OTHER O OTHER TXTAXI/GRND HDL 1 SO25826AY 8026 (REF NR: 05-060) FLAP FAIL MESSAGE UPON POWER UP. REMOVED AND REPLACED RT BRAKE POSITION SENSING UNIT (BPSU). (K) 2L72 4F4 FRTA21EA E15NE 20050901001492005090100149EA 2005 9 1 REX2005F00036 120050518A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CARGO BAY FALSE INDICATIONA REXAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO258721B5805 7721 (REF NR: 05-067) RECEIVED (CARGO SMOKE) WARNING IN FLIGHT. EMERGENCY DECLARED, QRH FOLLOWED EXTINGUISHING SYSTEM ACTIVATED WITH UNEVENTFUL LANDING AND PASSENGER EVACUATION ON TAXI WAY. INVESTIGATED, FOUND TO BE FALSE WARNING. SYSTEM DEFERED IAW MEL. (K) 2L72 4F4 FRTA21EA E15NE 20050901001502005090100150EA 2005 9 1 REX2005F00037 120050518A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS OUT OF RIG A REXAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO25825AY262 8025 (REF NR: 05-066) FLAPS FIAL ON TAXI. QRH FOLLOWED, RETURNED TO BLOCKS. FLAP SYSTEM RIGGED IAW AMM. OPS CHECKED GOOD. (K) 2L72 4F4 FRTA21EA E15NE 20050901001512005090100151EA 2005 9 1 REX2005F00034 120050528A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS FAILED A REXAO OTHER O OTHER APAPPROACH 1 SO258942A2515 7942 (REF NR: 05-069) FLAPS FAILED AT 20 ON APPROACH, QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAPS AND PLACED SYSTEM ON 72 HOUR WATCH IAW AD 98-20-01. (K) 2L72 4F4 FRTA21EA E15NE 20050901001532005090100153EA 2005 9 1 REX2005F00038 120050517A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS FAILED A REXAO OTHER O OTHER APAPPROACH 1 SO25800AY1109 8000 (REF NR: 05-065) FLAPS FAILED AT 30 ON APPROACH. RESET SYSTEM, PLACED FLAPS ON 72 HOUR WATCH IAW AD 98-20-01. (K) 2L72 4F4 FRTA21EA E15NE 20050901001542005090100154EA 2005 9 1 REX2005F00042 120050506A2750860D10018ABCD FCU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS FAILED A REXAO OTHER F FLT CONT AFFECTED CLCLIMB 1 SO25826AY125 8026 (REF NR: 05-061) FLAPS FAIL AT ZERO ON CLIMB-OUT. QRH FOLLOWED, EMERGENCY DECLARED RETURNED TO DEPARTURE WITH UNEVENTFUL LANDING. REMOVED AND REPLACED FLAP ELECTRONIC CONTROL UNIT. (FECU) (K) 2L72 4F4 FRTA21EA E15NE 20050901001552005090100155EA 2005 9 1 REX2005F00032 120050528A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS FAILED A REXAO OTHER O OTHER APAPPROACH 1 SO258409N11485 7409 (REF NR: 05071) FLAPS FAIL AT 11 DEGREES ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAPS AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K) 2L72 4F4 FRTA21EA E15NE 20050901001602005090100160EU 2005 9 1 UPS05145288 120050806A3350 LIGHT AIRBUSA300 A300F4622R 3930360EU EMERGENCY EXIT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01146UP 0829 LAV EMERGENCY EXIT LIGHT INOP, RELAMPED. 2L72 4F RTA35EU 20050901001632005090100163NM 2005 9 1 UPS05445271 120050825A5740 FITTING BOEING747 747212B 1384886NM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01526UP 21937 BS 1241 REAR SPAR CRACK INDICATION REVEALED AT UPPER SPLICE FITTING LOWER SURFACE AT NR 6 HOLE. CRACK LENGTH 0.060". RT NR 6 BOLT HOLE BUSHING REPAIRED AS PER EO NR B747-5740-17032. 2L74 4F A20WE 20050901001642005090100164NM 2005 9 1 UPS05445272 120050825A5740 FITTING BOEING747 747212B 1384886NM LT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01526UP 21937 LT WING UPPER REAR SPAR SIDE OF BODY SPLICE NR 6 FASTENER HOLE FOUND CORROSION AT UPPER SPLICE FITTING APPROX 0.030" IN LENGTH RUNNING FORWARD O/B, CORROSION BLEND OUT 0.030" IN LENGTH. LEFT NR 6 BOLT HOLE BUSHING REPAIRED AS PER EO NR B747-5740-17032. 2L74 4F A20WE 20050901001652005090100165NM 2005 9 1 UPS05445290 120050825A5311 FRAME BOEING747 747212B 1384886NM BS 880 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01526UP 21937 FX FRONT BODY FAIRING SUPPORT UPPER SURFACE FOUND SURFACE CORROSION AT STA 880 RBL 0 TO RBL 1". CORROSION BLEND OUT 0.080" BY 1" BY 1" EXCEED SRM 53-50-01 FIG 5 LIMITS, FRAME WEB REPAIRED AT BS 880 BL 0" TO RBL 1" FWD SIDE AREA AS PER SRM 53-50-04 FIG 1. 2L74 4F A20WE 20050901001672005090100167NM 2005 9 1 UPS05545297 120050830A2560 SMOKE GOGGLES BOEING757 75724APF 1384969NM COCKPIT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01431UP 25462 1ST OBSERVER SMOKE GOGGLES LENS CRACKED. REPLACED 1ST OBSERVERS SMOKE GOGGLES. 2L72 4F RTA2NM 20050901001682005090100168WP 2005 9 1 UPS05845274 120050811A5340 FITTING DOUG DC8 DC871F 302199DWP FS 834.5 L18R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 FS 834.500 L18R FRAME ATTACH FITTING CRACKED. REMOVED AND REPLACED FRAME FITTING AT STA 834.500 L18R IAW SRM 51-1-20 D, SRM 51-3-2. 2L74 4F RT4A25 20050902000092005090200009EA 2005 9 2 SWIA200515485 120050819A5310 GUSSET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07442SW 7609 SEVERAL CRACKS TO STRENGTHENING GUSSET ON THE BODY (FUSELAGE) RIB NEXT TO THE ENGINE BEAM, (ITEM FOUND AT ROUTINE INSPECTION.) REMOVED AND REPLACED TWO CLIPS NEAR AFT PRESSURE BULKHEAD IAW CRJ SRM 51-42-21 ON LEFT AND RIGHT SIDE. 2L72 4F RTA21EA 20050902000122005090200012NM 2005 9 2 CALA0500285 120050830A5320 STRUCTURE BOEING737 737824 13844BZNM STA 312-344 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712218 28778 INSPECTION FOUND L-1 DOOR CORRODED IN SEVERAL SPOTS FROM STA 312-344, LBL 51. THE CHORD WAS REMOVED AND REPLACED IAW SRM 51-40-00. 2L72 4F RTA16WE 20050902000132005090200013NM 2005 9 2 CALA0500286 120050829A3210654611325 TRUNNION PIN BOEING737 737524 1384721NM RT MLG FRACTURED A CALAO OTHER O OTHER LDLANDING 1 SW272365719513 SS5515 28918 THE FLIGHT CREW REPORTED A LOUD NOISE UPON LANDING AT ORD. INSPECTION BY MAINTENANCE FOUND THE RT MLG TRUNNION PIN FRACTURED. THE RT MLG WAS REMOVED AND REPLACED. AN FCD WAS ISSUED TO INSPECT THE REMAINDER OF THE FLEET. 2L72 4F RTA16WE 20050902000142005090200014EA 2005 9 2 COMA0560474 120050829A3230750005000 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA MLG FAULTY A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01816CA13201 7398 FLIGHT 5204 - WHEN GEAR WAS SELECTED DOWN FOR LANDING AT CVG, RECEIVED A GEAR DOWN DISAGREEMENT MESSAGE. CREW DECLARED AN EMERGENCY AND ABORTED FIRST APPROACH. CREW PULLED EMERGENCY HANDLE FOR GEAR EXTENSION THEN LANDED WITHOUT INCIDENT ON SECOND ATTEMPT.REPLACED THE MLG SELECTOR VALVE. 2L72 4F RTA21EA 20050902000272005090200027NM 2005 9 2 05FDEA02725 120050831A5311 FRAME DOUG MD11 MD11 3023602NM BS 5-0 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 MAIN DECK CARGO COMPARTMENT FRAME FOUND DENT AT LEFT STA 5-0, LONGERON 11L. REPAIRED AS PER SRM 53-30-00. 2L73 4F RTA22WE 20050902000282005090200028EU 2005 9 2 MALA050676 120050830A7931 ENGINE BAC 146 AVRO146RJ85A1500097EU OIL PRESSURE MALFUNCTIONED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15509XJ E2321 CREW RETURNED TO DTW FOLLOWING LOW ENGINE OIL INDICATION. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO FURTHER INFORMATION AT THIS TIME. 2H74 4F RTA49EU 20050902000302005090200030EU 2005 9 2 MALA050678 120050808A5230 STRUCTURE SAAB SF340 340B 7860101EU CARGO DOOR CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15369PX 0307 340B295 DURING 4Y/2Y INSPECTION IN BNA FOUND CARGO DOOR, P/N 7252300-502, S/N 0307 IS CHAFED AND HAS BEEN REPAIRED IAW MESABA EOS52044. REF EAMS WORK ORDER 212723. TASK 8503 & 8505. 2L72 4T RTA52EU 20050902000312005090200031EA 2005 9 2 COMA0560471 120050827A329717300233 WIRE HARNESS CNDAIRCL600 CL6002B19 1900309EA NLG STEERING FAULTY A COMAO OTHER J WARNING INDICATION LDLANDING 1 SO01507CA 7796 FLIGHT 5291 - EN ROUTE CVG-XNA RECEIVED A STEERING FAIL WARNING, FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE STEERING WIRING HARNESS ON NLG. 2L72 4F RTA21EA 20050902000322005090200032EA 2005 9 2 COMA0560473 120050829A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01420CA 7451 FLIGHT 5850 - AFTER LANDING WHEN SELECTING FLAPS TO 30 DEGREES RECEIVED A FLAP CAUTION MESSAGE. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE FIRST EVENT, MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2L72 4F RTA21EA 20050902000342005090200034WP 2005 9 2 UPS05845279 120050811A534037796594501 FITTING DOUG DC8 DC871F 302199DWP FS 857 L5L CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 LONGERON END FITTING CRACKED AT FS 867.125 L5L. REMOVED AND REPLACED LONGERON END FITTING AT FS 857.125 L5L IAW SRM 51-1-20D, 51-1-21 AND 51-3-0. 2L74 4F RT4A25 20050902000392005090200039WP 2005 9 2 UPS05845285 120050815A53404612650N FITTING DOUG DC8 DC871F 302199DWP FS -8 L33L CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 FS -8 AT L33L BULKHEAD HAS CRACKED END FITTING A/C COMPT. REMOVED AND REPLACED END FITTING AT FS -8 L33L IAW SRM 51-3-0,51-3-2 PG 1 AND 51-1-21. 2L74 4F RT4A25 20050902000402005090200040WP 2005 9 2 UPS05845292 120050813A53403755847U502 FITTING DOUG DC8 DC871F 302199DWP FS1230 L32R CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 LWR CARGO FS 1230 L32R ZEE FITTING CORRODED AND CRACKED .500 INCH LONG AROUND FASTNER HOLE. REMOVED ZEE FITTING IAW SRM 51-1-21 AND 51-1-20D. REPLACED ZEE FITTING AT FS 1230 L32R IAW SRM 51-3-2 AND 51-1-20D. 2L74 4F RT4A25 20050902000422005090200042WP 2005 9 2 UPS05845294 120050812A5320 CUSP WEB DOUG DC8 DC871F 302199DWP BS 1390-1430 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 CUSP HAS SHEAR HEAD FASTENER AND CRACK 1 INCH LONG FS 1420 L21R. REMOVED DAMAGED CUSP FROM BS 1390-1430 L21R IAW SRM 51-1-20D AND 51-1-2. FABRICATED AND INSTALLED REPAIR PARTS AND CUSP ANGLE IAW SRM 53-2-5 FIG 15 AND DWG 9754069 AT BS 1390-1430 L21R. 2L74 4F RT4A25 20050902000432005090200043WP 2005 9 2 UPS05845296 120050831A5610 WINDOW DOUG DC8 DC873F 302199FWP COCKPIT JAMMED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 F/O'S SLIDING WINDOW JAMMED. 2L74 4F RT4A25 20050902000462005090200046EA 2005 9 2 SWIA200515479 120050826A2750 TRANSMITTER CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07923SW 7664 FLAPS DEGRADED STATUS MESSAGE DISPLAYED IN FLIGHT. REPLACED LT FLAP POSITION TRANSMITTER IAW MM 27-55-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050902000472005090200047EA 2005 9 2 SWIA200515480 120050827A3350 BULB CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07750SK 10207 GALLEY FLOOR LEVEL EMERGENCY LIGHT INOP. REPLACED BULB. OPERATIONAL CHECK GOOD. REF AMM 33-24-02. 2L72 4F RTA21EA 20050902000482005090200048EA 2005 9 2 SWIA200515481 120050828A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLT SPOILERS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED APAPPROACH 1 NM07442SW1000710007 7609 WITH FLAPS SELECTED AT 45 DEGREES, GEAR DOWN AND FLIGHT SPOILER SELECTED TO THE 1/4 DETENT, THE AIRPLANE ROLLS ABRUPTLY TO THE RIGHT. REPLACED BOTH LT FLIGHT SPOILERS PCU'S IAW MM 27-62-01. OPERATIONAL CHECK GOOD PN 27000-7 SN/OFF MAL-6876. 2L72 4F RTA21EA 20050902000602005090200060NM 2005 9 2 05FDEA02719 120050830A5330 SKIN DOUG MD11 MD11 3023602NM FUSELAGE CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 LOWER FUSELAGE, FORWARD CARGO DOOR CUT-OUT AFT LOWER SIDE BETWEEN LONGERON 40R AND 41R, FOUND CHAFED SKIN = ABA7030-1. CARRIED OUT REPAIR AS PER SRM 53-50-00. 2L73 4F RTA22WE 20050902000622005090200062NM 2005 9 2 05FDEA02721 120050830A5347 SEAT TRACK DOUG MD11 MD11 3023602NM BS 635 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 MAIN DECK CARGO COMPARTMENT, NR 3 SEAT TRACK COUNTED FROM MOST LEFT, FOUND CRACKED AT STA 635. REPAIRED IAW SRM 53-70-00. 2L73 4F RTA22WE 20050902000632005090200063NM 2005 9 2 05FDEA02722 120050830A5310 STRUCTURE DOUG MD11 MD11 3023602NM BS 1721 CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25597FE 48596 CENTER CARGO COMPARTMENT, BILGE AREA AT STA 1721 LONGERON SPLICE 50R FOUND CRACKED. REMOVED AND REPLACED WITH NEW LONGERON SPLICE AS PER SRM 51-33-01. 2L73 4F RTA22WE 20050902000742005090200074NM 2005 9 2 DU4R0508185 120050824A5310 CREASE BEAM BOEING757 757232 1384965NM BS 460-480 DAMAGED A DU4RK NONE O OTHER ININSP/MAINT 1 SO15672DL 25977 CREASE BEAM HAS ELONGATED HOLES FROM BS 460 TO BS 480. 2L72 4F RTA2NM 20050902000802005090200080NM 2005 9 2 SWAA052634 120050829A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29322SW 23343 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR UPPER HINGE CUTOUT, UPPER RADIUS. REPAIRED SKIN PER SWA EA AND SRM. 2L72 4F RTA16WE 20050902000812005090200081 2005 9 2 SWAA052635 420050830A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29358SW 26595 DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050902000832005090200083NM 2005 9 2 SWAA052637 120050830A57536546435277 SKIN BOEING737 7373H4 1384600NM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29360SW 26571 DURING SCHEDULED C4 CHECK, FOUND LT WING OTBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM. 2L72 4F RTA16WE 20050902000852005090200085NM 2005 9 2 SWAA052639 120050830A335065C53829 CHARGER BOEING737 7375H4 138449DNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29523SW 26565 DURING SCHEDULED SERVICE CHECK, FOUND FWD CABIN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM. 2L72 4F RTA16WE 20050902000902005090200090NM 2005 9 2 SWAA052648 120050831A53116546555 FRAME BOEING737 7373H4 1384600NM BS 867 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050902000912005090200091NM 2005 9 2 SWAA052649 120050830A5312BAC1514413 ANGLE BOEING737 7373G7 1384595NM BS 1016 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29670SW 23784 DURING SCHEDULED 1/4D CHECK, FOUND BS 1016 AFT PRESSURE BLKHD Z-ANGLE CRACKED AT 6:30 O'CLOCK POSITION. REMOVED AND REPLACED Z-ANGLE PER SRM. 2L72 4F RTA16WE 20050902000922005090200092NM 2005 9 2 SWAA052650 120050831A5753 SKIN BOEING737 7373A4 1384585NM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 2302 23288 DURING SCHEDULED SERVICE CHECK, FOUND LT WING OTBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM. 2L72 4F RTA16WE 20050902000932005090200093 2005 9 2 SWAA052651 420050831A256563550101 SLIDE BOEING737 737317 138447PNM R1 DOOR OUT OF LIMITS A SWAAK NONE O OTHER ININSP/MAINT 1 SW29686SW 23175 R1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATED OUT OF LIMITS. REMOVED AND REPLAECD SLIDE PER MM. 2L72 4F RTA16WE 20050902000942005090200094NM 2005 9 2 SWAA052652 120050825A53126545819 PRESSURE PANEL BOEING737 7373Q8 1384670NM NLG WW CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29687SW 23388 DURING SCHEDULED RON CHECK, FOUND NLG W/W RT UPPER ACCESS PANEL CUTOUT, AFT INBD CORNER CRACKED AT BS 251.6, LBL 2.0. REPAIRED WEB PER SWA EA. 2L72 4F RTA16WE 20050902000962005090200096NM 2005 9 2 SWAA052654 120050831A53306545776 SKIN BOEING737 7373H4 1384600NM BS 941 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 941, STR 4R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050902000972005090200097NM 2005 9 2 SWAA052655 120050830A53306545775 SKIN BOEING737 7373H4 1384600NM BS 783 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29336SW 23940 DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 783, STR 20L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050902000982005090200098NM 2005 9 2 SWAA052656 120050831A53306545774 SKIN BOEING737 7373H4 1384600NM BS 727E+12 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29336SW 23940 DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E + 12, STR 18R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050902000992005090200099NM 2005 9 2 SWAA052632 120050831A3230A42006028305 SOLENOID BOEING737 7373H4 1384600NM MLG FAULTY A SWAAO OTHER O OTHER LDLANDING 1 SW29313SW 23335 MOVING LANDING GEAR LEVER TO DOWN POSITION, ALL RED AND GREEN WARNING LIGHTS ILLUMINATED. CYCLED LANDING GEAR LEVER SEVERAL TIMES BEFORE RED WARNING LIGHTS EXTINGUISHED. REMMOVED AND REPLACED LANDING GEAR LEVER SOLENOID PER MM. 2L72 4F RTA16WE 20050902001002005090200100NM 2005 9 2 SWAA052633 120050829A53306545776 SKIN BOEING737 7373H4 1384600NM BS 937 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29322SW 23343 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 937, STR 23R. REPAIRED SKIN PER SWA EA AND SRM. 2L72 4F RTA16WE 20050902001082005090200108EU 2005 9 2 USAA050938 120050729A5310D5347217220390 BEAM AIRBUSA319 A319112 3930323EU FS 66/68 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19723UW17735 1109 PIT - FOUND BEAM CORRODED .5 INCH BY .5 INCH AND .5 INCH BY .5 INCH, ON FLOORBEAM BETWEEN FRAME 66/68 -Y450 INCH. REPLACED BEAM PER SRM 53-41-00. CORROSION LEVEL 1, TASK JA-260-53500. (M) 2L72 4F RTA28NM 20050902001092005090200109EU 2005 9 2 USAA050937 120050729A5315D5347209001000 FLOORBEAM AIRBUSA319 A319112 3930323EU FS 66-68 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19723UW17735 1109 PIT - FOUND FLOORBEAM CORRODED 1 SQUARE INCH, BETWEEN FRAME 66/68 AT Y-48 INCHES LEFT. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-72-11. CORROSION LEVEL 1, TASK JA-260-53500. (M) 2L72 4F RTA28NM 20050902001102005090200110NM 2005 9 2 SWAA052641 120050831A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM BS 767 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 767, BETWEEN BL 0 TO RBL 12. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050906000032005090600003NM 2005 9 6 AWXA200501022 120050805A52106545871515 FRAME BOEING737 7373G7 1384595NM R1 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28311AW 24712 MCN - MAJOR REPAIR - DURING C15 CHECK FOUND R1 DOOR CRACKED, .300 INCHES IN LENGTH, AT THE 3RD AFT DOOR STOP CUTOUT. MAINTENANCE STOP TRIMMED OUT CRACK FROM THE R1 DOOR IAW AMERICA WEST AIRLINES REPAIR NR 03-5210-5238-ES1. FABRICATED REPAIR DOUBLER IAW AWA ER 03-5210-5238-ES1. INSTALLED REPAIR PARTS AT THE R1 DOOR IAW BOEING 737-300 SRM 03-5210-05238-ES1. 2L72 4F RTA16WE 20050831000482005083100048NM 2005 8 31 QXEA200501195 120050828A3620 WARNING LIGHT BOMBDRDHC8 DHC8402 1390042NM NR 1 BLEED SYS FALSE ACTIVATIONA QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09411QX 4055 LAX FLIGHT 2310: NR 1 BLEED HOT CAUTION LIGHT ILLUMINATED IN CRUISE. SHUTOFF NR 1 BLEED PER E/A CHECKLIST. LIGHT EXTINGUISHED. MAINTENANCE COMPLIED WITH FIM TASK 36-20-00-810-801. PERFORMED OPERATIONAL TEST OF THE BLEED AIR SYSTEM PER TASK 36-11-00-710-802. BLEED AIR CAUTION DID NOT RETURN. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050831000492005083100049NM 2005 8 31 P5CA0501386 120050828A5330 SKIN BOEING747 74746NF 13848BTNM BS 1980-2000 DENTED A P5CAK NONE O OTHER ININSP/MAINT 1 EA15450PA 30808 BULK CARGO DOOR B/T STA 1980-2000 RT CLOSE TO LOWER CUT OUT DENT WAS FOUND 2.28 X 1.46 X 0.075 INCHES. WORK ACCOMPLISHED PER ENGINEERING DISPOSITION RFTA-4177-001. DENT STRAIGHTENED, NO CRACK FOUND. 2L74 4F RTA20WE 20050831000512005083100051NM 2005 8 31 SWAA052604 120050819A253041600019 COFFEEMAKER BOEING737 7375H4 138449DNM AFT GALLEY FAULTY A SWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW29506SW 24183 ELECTRICAL ODOR IN AFT GALLEY. REMOVED AND REPLACED BOTH AFT GALLEY COFFEEMAKERS PER MM. 2L72 4F RTA16WE 20050831000532005083100053NM 2005 8 31 SWAA052606 120050829A53156546811 FLOORBEAM BOEING737 7373H4 1384600NM BS 986 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29617SW 27700 DURING SCHEDULED D CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 986, LBL 46. REPAIRED FLOORBEAM PER BFG ER. 2L72 4F RTA16WE 20050831000552005083100055EU 2005 8 31 DJFA2005133 120050821A2133 OUTFLOW VALVE BRAERODH125 BAE125800A 1500285EU CABIN PRESSURE MALFUNCTIONED E DJFAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 EA23811CW 258011 THE CABIN ALTITUDE WAS NOTED AS UNUSUALLY HIGH. THE CABIN RATE CONTINUED TO CLIMB AS THE AIRCRAFT DESCENDED AND THE CABIN ALTITUDE WARNING HORN SOUNDED. THE CREW DECLARED AN EMERGENCY AND PERFORMED AN EMERGENCY DESCENT WHILE DONNING THE OXYGEN MASKS. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ISSUED MEL 21-30-5 FOR THE OUTFLOW VALVES AND THE AIRCRAFT WAS RETURNED TO SERVICE. ON AUGUST 22, 2005 A PRESSURIZATION SYSTEM FUNCTIONAL TEST WAS PERFORMED BY MAINTENANCE. SYSTEM OPERATION WAS SATISFACTORY. THE CABIN OXYGEN MASKS WERE CLEANED AND STOWED AND A SATISFACTORY CHECK FLIGHT WAS PERFORMED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA3EU 20050831000572005083100057NM 2005 8 31 2005UALA00877 120050823A2432 CHARGER BOEING777 777222 1385219NM MASTER BATTERY FAULTY A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29222UA 30553 RECEIVED BATTERY CHARGER FAULT. MECHANICS FOUND CIRCUIT BREAKER FOR MAIN BATTERY CHARGER TRIPPED. THE BATTERY AND CHARGER WERE REPLACED PER MM 24-31-01 AND 24-31-02. REMOVED BATTERY PN 263BA101-2 SN 1049A HAS BEEN SENT TO THE VENDOR FOR REPAIR. BATTERY CHARGER PN 263BC101-2 SN 1088 HAS PASSED ALL SHOP TESTS. ONE PRIOR REPORT ON PREVIOUS LEG 22AUG05 OF MAIN BATTERY LOW VOLTAGE WHERE BATTERY WAS REPLACED. NO OTHER REPORTS IN LAST 12 MONTHS. ENGINEERING CONSIDERS THIS AN ISOLATED CASE. 2L72 4F RTT0001SE 20050831000592005083100059NM 2005 8 31 2005UALA00879 120050824A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE BS 324 CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29505UA 24626 FLOORBEAM AT BS 324 IS CORRODED FROM THE CIRCUMFERENTIAL FRAME TO THE SPLICE AT RBL 50, AND THE T-CAP. FABED REPAIR PARTS PER SRM 53-00-51, ALODINE, PRIME, AND PAINT. INSTALL REPAIR PARTS PER MM 53-00-98. 2L72 4F4 FRTA2NM E17NE 20050831000612005083100061NM 2005 8 31 2005UALA00881 120050824A335058673 INVERTER BOEING737 737322 1384676NM MID CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29365UA 24534 EMERGENCY EXIT FLOOR LIGHTS INOP HALF WAY BACK. REPLACED AFT INVERTER. 2L72 4F RTA16WE 20050831000622005083100062NM 2005 8 31 2005UALA00882 120050824A2121 FAN BOEING757 757222 1384956NM PWA 2037 PW2037 NE GALLEY FAILED A UALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 WP29589UA 28707 STRONG ELECTRICAL ODOR IN MID GALLEY. STRONG ELECTRICAL ODOR IN MID GALLEY AFTER APU GEN FIELD TRIP. REPLACED NR 1 FWD EQUIP SUPPLY FAN. 2L72 4F4 FRTA2NM E17NE 20050831000632005083100063 2005 8 31 2005UALA00883 420050803A2565D31038201 SLIDE BOEING757 757222 1384956NM PWA 2037 PW2037 NE PAX DOOR SEPARATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29503UA 24624 THE RIGHT SLIDE BUMPER SEPARATED DURING OVERPRESSURE. INTERNAL SEAM FAILURE CAUSED BUMPER PROFILE TO DISTORT. ANALYSIS BY OEM OF BUMPER INTERNAL SEAM FAILURE SHOWED PROPER SEAM ASSEMBLY. INFLATABLE WAS REPLACED. 2L72 4F4 FRTA2NM E17NE 20050831000642005083100064NM 2005 8 31 2005UALA00884 120050825A5241 FRAME BOEING737 737322 1384676NM FWD GALLEY DOOR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29327UA 24147 FWD GALLEY DOOR AFT FRAME IS CRACKED AT 3RD AND 4TH STOP FITTING CUTOUTS. 2L72 4F RTA16WE 20050831000652005083100065NM 2005 8 31 2005UALA00885 120050825A5241 FRAME BOEING737 737322 1384676NM FWD GALLEY DOOR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29327UA 24147 FWD GALLEY DOOR FRAME CRACKED AFT SIDE LOWER STOP FITTING. 2L72 4F RTA16WE 20050831000672005083100067NM 2005 8 31 2005UALA00887 120050825A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE BS 1400 DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29588UA 26717 FRAME HAS A DENT AT STA 1400 BETWEEN STR 26L AND STR 27L, AFT PIT, INBOARD FLANGE. REPAIRED FRAME FLANGE WITH NESTED J-ANGLE TO EXISTING CHORD PER TIMCO REO (EVA) G10828, REV B. 2L72 4F4 FRTA2NM E17NE 20050831000692005083100069CE 2005 8 31 DJFA2005134 120050828A7830 WARNING LIGHT BEECH MU300 400A 1155402CE THRUST REVERSER ILLUMINATED E DJFAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA23698TA RK298 THE CREW REPORTED THAT DURING TAKEOFF THE LEFT THRUST REVERSER UNLOCK AND LEFT THRUST REVERSER ARM LIGHTS ILLUMINATED. THIS WAS FOLLOWED BY THE ASSOCIATED MASTER WARNING AND EMERGENCY STOW LIGHTS ILLUMINATING. THE THRUST REVERSER WAS STOWED MANUALLY BY USE OF THE EMERGENCY STOW BUTTON. THE AIRCRAFT WAS RETURNED TO KHIO AND AN UNEVENTFUL LANDING WAS MADE. MAINTENANCE ISSUED MEL 78-1 AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4F RTA16SW 20050831000752005083100075NM 2005 8 31 2005UALA00888 120050825A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE BS 1340 BENT A UALAK NONE O OTHER ININSP/MAINT 1 WP29588UA 26717 STA 1340 LEFT HAND SIDE FRAME BENT AT STR 25L. REMOVED EXISTING PRODUCTION SPLICE AND FABRICATED A NEW PRODUCTION SPLICE ANGLE PER TIMCO REO(EVA) G10831, REV C. 2L72 4F4 FRTA2NM E17NE 20050831000772005083100077NM 2005 8 31 2005UALA00890 120050825A2782 ACTUATOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 6 SLAT FAILED A UALAA UNSCHED LANDING J WARNING INDICATION DEDESCENT 1 WP29507UA 24743 DIVERTED TO EWR WITH A SLAT DISAGREE PROBLEM. FOUND NR 6 SLAT ACTUATORS NR 11 AND 12 OVERLOAD INDICATORS POPPED. REPLACED BOTH NR 11 AND 12 SLAT ACTUATORS. 2L72 4F4 FRTA2NM E17NE 20050831000782005083100078NM 2005 8 31 HNAA0500079 120050826A2910DSC1906 CHECK VALVE DHAV DHC8 DHC8102 2809003NM HYD SYSTEM CRACKED A HNAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 EA07912HA5081450814 040 AT GEAR RETRACTION NR 2 ISOV CAUTION LIGHT ILLUMINATED FOLLOWED BY ROLL SPOILER HYD. CAUTION LIGHT NR 2 QUANTITY DROPPED TO 1/2 QT. SYSTEM PRESSURE REMAINED NORMAL. REPLACED CHECK VALVE. 2H72 4T RTA13NM 20050831000792005083100079NE 2005 8 31 HNAA0500078 220050828A732078639114 HMU DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE ZONE 400 FAILED A HNAAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 EA07825EX3950 3950 388 121354 A 5 INCH POWER LEVER SPLIT IN CRUISE. REMOVED AND REPLACED HYDRO MECHANICAL UNIT AND FUEL PUMP. 2H72 4T4 TRTA13NM E20NE 20050831001112005083100111 2005 8 31 SF20050829 420050829A3425 COMPUTER SAAB SF340 SF340A 7850100EU AHRS FAILED A UHLAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL17123XS 123 7561 IAD-SCE 10 DEGREES PITCH DIFFERENCE BETWEEN CAPT`S & F/O`S SIDE, ASSOCIATED WITH 30 DEGREES DIFFERENCE IN HEADING ON CAPT`S SIDE, WITH YELLOW PITCH FLAG. A/C RETURNED TO FIELD. REMOVED AND REPLACED LT AHRS COMPUTER, IAW SAAB M/M 34-21-05-2. PERFORMED OPERATIONAL CHECKS, IAW SAAB M/M 34-21-00-5. ALL OPS CHECKS GOOD. 2L72 4T RTA52EU 20050901000032005090100003NM 2005 9 1 USAA050968 120050804A5551 CLEVIS BOEING737 7373B7 1384580NM HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US50585 23933 CLT - FOUND ATTACH CLEVIS CORRODED 2 INCHES DIAMETER BY .015 TYPICAL, RIGHT HORIZ STAB FORWARD SPAR ATTACH CLEVIS AFT FACE. REMOVED CORROSION AND BUSHED IAW 55-10-10. (M) 2L72 4F RTA16WE 20050901000082005090100008CE 2005 9 1 VQM2005F00000 120050602A3246313996 WHEEL CESSNA650 650 2076802CE GARRTTTFE731TFE731* 01518WP MLG BROKEN E VQMAO OTHER O OTHER NRNOT REPORTED 1 NM03651PW 6500090 DURING WEEKLY INSPECTION ON AIRCRAFT, IT WAS DISCOVERED THAT ONE THROUGH BOLT ON LT MAIN WHEEL IN NR 1 POSITION WAS BROKEN. AFTER FURTHER INSPECTION NR 2 POSITION WHEEL ON SAME LT LANDING GEAR HAD 2 BROKEN THROUGH BOLTS ADJACENT TO EACH OTHER. ALL BOLTS RETAINED AND AVAILABLE UPON REQUEST. (K) 2L72 4F4 F A9NM E6WE 20050901000162005090100016NM 2005 9 1 USAA050948 120050803A5551 BUSHING BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US50585 23933 CLT - Q6 - LUG/BUSHING, CORROSION, L6 LUG, LT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED BUSHING IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050901000312005090100031 2005 9 1 A6WA200540284 420050816A3414WL102AMS5 INDICATOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE STDBY AIRSPEED INOPERATIVE A A6WAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 GL31459AW5488 7863 TAKEOFF ABORTED DUE TO STANDBY AIRSPEED INDICATION READING ZERO AT 80 KNOTS. TAKEOFF ABORTED AT 90 KNOTS, BRAKE TEMPS 8,8,6,5, NORMAL BRAKING. REMOVED AND REPLACED STANDBY AIRSPEED INDICATOR. (K) 2L72 4F4 FRTA21EA E15NE 20050901000372005090100037NE 2005 9 1 KBM2005F00217 220050806A72009603490601 BEARING SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE DRIVE SHAFT WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P 2347 ENGINE POWER DRIVESHAFT BEARING WORN BEYOND LIMITS. REPLACED WITH NEW. (K) 1G71 3U3 UNCH9EU E19EU 20050901000392005090100039NM 2005 9 1 USAA050993 120050808A5311 FRAME BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU BS 500A CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US 23933 CLT, Q6, FRAME .125 INCH CRACK, STRINGER 9 LT STA 500A. REPAIRED IAW TR 53-10-20B. (K) 2L72 4F4 FRTA16WE E21EU 20050901000402005090100040EA 2005 9 1 ASOA05652 120050723A5210 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27854AS 7382 DURING A C-CHECK, THE PASSENGER DOOR INNER SKIN AND INTERCOSTAL AT TATUM 1, FS 338 FRAME BETWEEN DATUM 1 AND THE UPPER CLOSE OUT WEB WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE PASSENGER DOOR INNER SKIN AND INTERCOSTAL AT DATUM 1, FS 338 FRAME BETWEEN DATUM 1 AND THE UPPER CLOSE OUT WEB IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050901000532005090100053EA 2005 9 1 ASOA05654 120050806A3350BF10044004 SIGN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE GALLEY CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27833AS 7248 DURING C-CHECK, THE EMERGENCY EXIT SIGN OVER THE SERVICE DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT SIGN OVER THE SERVICE DOOR IAW AMM. (K) 2L72 4F4 FRTA21EA E15NE 20050901000632005090100063 2005 9 1 KBM2005F00223 420050627A34225050010902 GYRO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1B 6OO30NE DIRECTIONAL STUCK E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH871 2957 DIRECTIONAL GYRO FLAG WAS STUCK. REPLACED WITH SERVICEABLE UNIT. (K) 1G71 3U3 U H9EU E19EU 20050901000682005090100068SO 2005 9 1 HYI2005F00006 220050818A8520536379 BOLT CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO CRANKSHAFT SHEARED E HYIAO OTHER O OTHER NRNOT REPORTED 1 NE016875D2270 402C0511 828512R LT PROPELLER FAILED TO TURN ON START, MAINTENANCE FOUND CRANKSHAFT LARGE ATTACH BOLTS SHEARED AND GEAR DISLODGED FROM CRANKSHAFT. MAINTENANCE REMOVED AND REPLACED THE ENGINE AND RETURNED THE AIRCRAFT TO SERVICE. (NE01200505271) (K) 1L72 3O3 O A7CE E8CE 20050901000732005090100073EA 2005 9 1 ASOA05651 120050805A1100S157418 PLACARD CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN WORN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27856AS 7404 DURING AN A-CHECK, THE EXIT PLACARD ON THE PASSENGER DOOR WAS FOUND NEEDING REPLACEMENT. MAINTENANCE REMOVED AND REPLACED THE EXIT PLACARD ON THE PASSENGER DOOR. (K) 2L72 4F4 FRTA21EA E15NE 20050901000842005090100084EA 2005 9 1 ASOA05611 120050719A2560111RJ7001 STRIP CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE CABIN DAMAGED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27705EV 10051 DURING HANGAR MAINTENANCE, THE EMERGENCY FLOOR LIGHTING REFLECTIVE STRIP BETWEEN ROW 6 AND THE GALLEY WAS FOUND DAMAGED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHTING REFLECTIVE STRIP BETWEEN ROW 6 AND THE GALLEY. (K) 2L72 4F4 FRTA21EA EOOO63EN 20050901000902005090100090EA 2005 9 1 REX2005F00018 120050706A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS FAILED A REXAO OTHER O OTHER APAPPROACH 1 SO258554A8986 7554 (REF NR: 05-085) FLAP FAILED ON APPROACH. RESET SYSTEM AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K) 2L72 4F4 FRTA21EA E15NE 20050901001372005090100137EA 2005 9 1 ASOA05655 120050722A5210 HANDLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR DAMAGED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27833AS 7246 DURING A C-CHECK, THE EMERGENCY EXIT BETA LIGHT ON THE PASSENGER DOOR HANDLE WAS FOUND DAMAGED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT BETA LIGHT ON THE PASSENGER DOOR. (K) 2L72 4F4 FRTA21EA E15NE 20050901001402005090100140EA 2005 9 1 REX2005F00016 120050715A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS FAILED A REXAO OTHER O OTHER APAPPROACH 1 SO25801AY1521 8001 (REF NR: 05-087) FLAPS FAILED ON APPROACH, QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAPS AND PLACED SYSTEM ON 72 HOUR WATCH IAW AD 98-20-01. (K) 2L72 4F4 FRTA21EA E15NE 20050901001412005090100141EA 2005 9 1 REX2005F00027 120050620A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS FAILED A REXAO OTHER O OTHER APAPPROACH 1 SO258905F3520 7905 (REF NR: 05-076) FLAP FAIL ON APPROACH WHEN GOING FROM 20 TO 30, QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAP SYSTEM AND PLACED ON 72 HOUR WATCH IAW AD-98-20-01. (K) 2L72 4F4 FRTA21EA E15NE 20050901001562005090100156EA 2005 9 1 REX2005F00040 120050509A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS FAILED A REXAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SO258888D3382 7888 (REF NR: 05-063) FLAP FAILED AT 20 ON APPROACH. RESET SYSTEM AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K) 2L72 4F4 FRTA21EA E15NE 20050901001582005090100158EA 2005 9 1 COMA0560472 120050828A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01984CA 7171 FLIGHT 5805 - EN ROUTE LGA-GSP RECEIVED A LEFT THRUST REVERSER UNLOCK MESSAGE. CREW DIVERTED TO JFK, FLIGHT LANDED WITHOUT INCIDENT. DEFERRED THE LEFT THRUST REVERSER PER MEL. 2L72 4F RTA21EA 20050901001692005090100169WP 2005 9 1 UPS05845275 120050816A5330 FINGER DOUBLER DOUG DC8 DC871F 302199DWP FS-67 TO -80 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 COCKPIT SUBFLOOR FINGER DOUBLER HAS SEVERAL SHEAR HEAD RIVETS AND CORRODED AT STA -67 TO -80 RBL 60. REMOVED FINGER DOUBLER IAW SRM 51-1-21 AND 51-3-0. REMOVED CORROSION FROM WEB IAW SRM 51-1-8, FABRICATED AND INSTALLED REPLACEMENT FINGER DOUBLER AT STA -67 TO -80 RBL 60 IAW SRM 53-03-01 PG1 FIG 007, 51-1-8, AND SRM 51-1-20D. 2L74 4F RT4A25 20050902000012005090200001EA 2005 9 2 COMA0560468 120050826A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA LT WING FAULTY A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01814CA19923 7387 FLIGHT 5441 - WHILE AT GATE AT JAX, RECEIVED A FLAP FAIL CAUTION. REPLACED THE RIGHT BRAKE POSITION SENSING UNIT. 2L72 4F RTA21EA 20050902000262005090200026NM 2005 9 2 05FDEA02724 120050831A5311 FRAME DOUG MD11 MD11 3023602NM BS 1661 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 MAIN DECK CARGO COMPARTMENT, FRAME FOUND DENT AT LEFT STA 1661, LONGERON 12L. CARRIED OUT REPAIR AS PER SRM 53-30-00. 2L73 4F RTA22WE 20050902000292005090200029WP 2005 9 2 UPS05845276 120050811A53403649114U FITTING DOUG DC8 DC871F 302199DWP FS 923 L22L CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 MAIN CABIN CENTER SUBFLOOR STA 923 L22L "T" FITTING AROUND FASTNERS AREA HAS HEAVY CORROSION. REMOVED CORROSION FROM "T" FITTING AND VISUALLY FOUND CRACK IAW SRM 51-1-8. REMOVED AND REPLACED "T" FITTING IAW SRM 51-3-2 AND DWG 3649114. 2L74 4F RT4A25 20050902000382005090200038WP 2005 9 2 UPS05845283 120050819A5280 DOUBLER DOUG DC8 DC871F 302199DWP NLG DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 NOSE SECTION FUSELAGE SKIN HAS 3/8" CRACK AT AFT HINGE ACCESS DOOR. REMOVED CRACKED DOUBLER AT NOSE EXTERIOR AFT SKIN IAW SRM 51-1-21. FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW DWG56126127 AND SRM 51-1-20E. 2L74 4F RT4A25 20050902000492005090200049EA 2005 9 2 SWIA200515482 120050823A274070609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07932SW1736 1736 7714 DURING FLIGHT, STAB AND MACH TRIM CAUTION MESSAGES WERE DISPLAYED ON ED-1. RELACED HORIZONTAL STAB TRIM CONTROL UNIT IAW CRJ MM 27-41-01, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050902000522005090200052EA 2005 9 2 COMA0560467 120050826A2751855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA LEFT WING FAULTY A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01783CA7891 7315 FLIGHT 5402 - DURING APPROACH INTO MCO WHEN FLAPS SELECTED TO 20 DEGREES RECEIVED A FLAP FAIL CAUTION. REPLACED THE LEFT BRAKE POSITION SENSING UNIT. 2L72 4F RTA21EA 20050902000572005090200057NM 2005 9 2 UPS05M45289 120050829A2560 SMOKE GOGGLES DOUG MD11 MD11F 3023600NM COCKPIT TORN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01271UP 48572 RT COURIER SEAT SMOKE GOGGLE TORN. ORDERED POUCH TO P1 SHELF REPLACED POUCH FOR SMOKE GOGGLE AT RT COURIER SEAT AS REQ FOR SERVICE. 2L73 4F RTA22WE 20050902000592005090200059 2005 9 2 05FDEA02718 420050830A3442 RADAR BOEING727 72722 1384002NM WX SYSTEM FAILED A FDEAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 SO25166FE 18863 WX RADAR FAILED 5 MIN AFTER T/O CYCLED C/B NO JOY TURNED RT ON AND OFF SEVERAL TIMES REMAINED FAILED. REPLACED WX R/T, GRD OPS CK NORMAL MM 34-41-041. REMOVAL/INSTALLATION, OFF MFG 622-5132-101, POS ONL SRL 2652 TAG A03946 ON MFG 622-5132-101 SRL 3939 TAG A15647. 2L73 4F A3WE 20050902000612005090200061NM 2005 9 2 05FDEA02720 120050830A5310 STRUCTURE DOUG MD11 MD11 3023602NM BS 1110 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 CAC COMPARTMENT INTERIOR, BILGE LOCATION AT STA 1110, LONGERON 51L, FOUND CORRODED. CARRIED OUT REPAIR AS PER SRM 53-10-00. 2L73 4F RTA22WE 20050902000822005090200082NM 2005 9 2 SWAA052636 120050830A3350BR2013 STRIP BOEING737 7373H4 1384600NM EMERGENC LIGHT WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29358SW 26595 DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK STRIP WORN AT ROW 23 DEF. REMOVED AND REPLACED EEPLS STRIP PER MM. 2L72 4F RTA16WE 20050902000862005090200086NM 2005 9 2 SWAA052640 120050831A5320BAC15171489 FLOOR SUPPORT BOEING737 7373H4 1384600NM BS 270 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 DURING SCHEDULED D CHECK, FOUND COCKPIT FLOOR Z-CHORD CORRODED AT BS 270, RBL 11 TO LBL 11, WL 208. REPAIRED Z-CHORD PER SRM. 2L72 4F RTA16WE 20050902000892005090200089NM 2005 9 2 SWAA052647 120050831A53116546550 FRAME BOEING737 7373H4 1384600NM BS 787 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L TO STR 8R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050902000952005090200095NM 2005 9 2 SWAA052653 120050830A3350D71702001 BATTERY PACK BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29783SW 29809 DURING SCHEDULED MV2 CHECK, FOUND RT FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050906000022005090600002NM 2005 9 6 AALA20050560 120050828A3350 LIGHT BOEING737 737823 13844BZNM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21971AN 29547 DFW - EMERGENCY LIGHTS AT AFT RIGHT CABIN PASSENGER DOOR EXIT LIGHT ASSEMBLY MARKER ON THE INTERIOR AFT OF THE DOOR IS BROKEN. REPLACED THE EMERGENCY LIGHT EXIT IDENTIFIER LIGHT ASSEMBLY ON THE INTERIOR AFT OF THE RIGHT AFT CABIN PASSENGER DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20050906000042005090600004NM 2005 9 6 AWXA200501023 120050806A53146562125 KEELBEAM BOEING737 7373G7 1384595NM BS 540 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28311AW 24712 DURING C15 CHECK DISCOVERED CORROSION AND 1.0 INCH CRACK ON THE LT KEEL BEAM LOWER CHORD AT BS 540, WL 150, BL 6.5L. CORROSION WAS DETERMINED TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-12 FIG 101. MAINTENANCE REMOVED CORRODED AND CRACKED SECTION ON KEEL BEAM AT BS 540, WL 150, BL 6.5L IAW BOEING 737-300 SRM 53-60-11. FABRICATED ANGLES, FILLERS AND PREPARED FOR INSTALLATION IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5300-05236-SS2. INSTALLED FABRICATED REPAIR PARTS AT BS 540, WL 150, BL 6.5L IAW AWA ER 03-5300-05236-SS2. 2L72 4F RTA16WE 20050906000052005090600005NM 2005 9 6 AWXA200501024 120050819A521065505611 HOUSING BOEING737 7373G7 1384595NM DOOR HINGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28311AW 24712 DURING C15 CHECK DISCOVERED THE R1 DOOR UPPER HINGE HOUSING CRACKED 1.5 INCHES IN LENGTH AT BS 310, WL 258, STR 10R. MAINTENANCE REMOVED AND REPLACED THE R1 DOOR UPPER HINGE HOUSING IAW BOEING 737-300 SRM 51-40-02-06 FIG 8, 51-40-06 DETAIL 1 TABLE I, 51-40-02-06. 2L72 4F RTA16WE 20050906000382005090600038EA 2005 9 6 SWIA200515489 120050809A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07448SW FS 280 , TRANSVERSE BEAM CRACKED ON UPPER SUPPORT ANGLE LBL 13, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED TRANSVERSE BEAM IAW CRJ REO 601R-53-11-138 REV "NC". 2L72 4F RTA21EA 20050906000392005090600039EA 2005 9 6 SWIA200515490 120050809A5340 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07448SW 7678 FS 280 LBL 9.0 INBD ATTACH ANGLE CRACKED, ITEM FOUND AT C-CHECK INSPECTION. FS 280 ATTACH ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-42-13, 51-21-11, 51-25-16, 51-23-00. 2L72 4F RTA21EA 20050906000412005090600041NM 2005 9 6 AWXA200501016 120050830A335020131A BATTERY BOEING737 73733A 1384673NM EMERGENCY LIGHT INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 PHX - EEL - DURING INSPECTION DISCOVERED EMERGENCY EXIT PATHWAY LIGHTS AT ROWS 1, 2, 3, AND 4 ARE ON DIM WITH SWITCH IN OFF OR ARMED POSITION. MAINTENANCE REPLACED THE POWER SUPPLY AND BATTER IAW MAINTENANCE MANUAL 33-51. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20050906000432005090600043EU 2005 9 6 AWXA200501018 120050830A3230 CONTROL UNIT AIRBUS320 A320231 3930325EU MLG MALFUNCTIONED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28633AW 082 DURING TAKEOFF, LANDING GEAR WOULD NOT RETRACT, ALSO HAD ECAM FAULT FOR MLG SHOCK ABSORBER. AIRCRAFT RETURNED TO PHX AND LANDED WITHOUT FURTHER INCIDENT. EMERGENCY WAS NOT DECLARED, GEAR WAS DOWN AND LOCKED. MAINTENANCE REMOVED AND REPLACED NR 2 LGCIU AND ALSO SERVICED THE RT MLG SHOCK ABSORBER IAW AIRBUS MM 12-14-32. GEAR SWINGS AND OPERATIONAL CHECKS WERE GOOD. TEAR DOWN REPORT CONFIRMS FAILURE. UNIT FAILED THE INTERFACE BOARD NR 2 TESTS, TRANSDUCER 10, ON THE INTERFACE BOARD NR 2 WAS REPLACED. UNIT WAS REPAIRED AND TESTED IAW CMM 32-31-39 REV. 13. 2L72 4F RTA28NM 20050906000442005090600044NM 2005 9 6 SWAA052642 120050831A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM BS 787 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, RBL 14. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050906000452005090600045NM 2005 9 6 SWAA052643 120050831A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM BS 807 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 807, RBL 7. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050906000462005090600046NM 2005 9 6 SWAA052644 120050831A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 807 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CORRODED AT BS 807, RBL 7. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050906000472005090600047NM 2005 9 6 AALA20050557 120050828A3241 CONTROL UNIT BOEING757 757223 1384957NM ANTI SKID SYS INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW21678AN 29428 LAX INFLIGHT T1677 - ANTI-SKID MESSAGE IN FLIGHT. AIRCRAFT DIVERTED FROM SNA TO LAX AND LANDED WITHOUT INCIDENT. REPLACED ANTI-SKID CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050906000492005090600049NM 2005 9 6 AALA20050559 120050827A3350P4010051112 MODULE BOEING767 767223 1385123NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21338AA 22335 JFK- EMERGENCY LIGHTS AT SEAT ROWS 2AB TO 9AB INOPERATIVE. REPLACED MODULE AND BATTERY PACK AT FIRST CLASS POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050906000502005090600050WP 2005 9 6 AALA20050558 120050826A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21465A 49595 SAT - EMERGENCY LIGHTS AT FORWARD ENTRY AND FLIGHT DECK INOPERATIVE. REPLACED BATTERY PACK AT FORWARD ENTRY DOOR CEILING FOR EMERGENCY LIGHTS AT FORWARD ENTRY AND FLIGHT DECK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050906000522005090600052NM 2005 9 6 SWAA052658 120050901A53306545774 SKIN BOEING737 7373H4 1384600NM BS 727B CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29324SW 23414 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727B, STR 14L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050906000532005090600053NM 2005 9 6 SWAA052659 120050831A3350MS155721 BULB BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29355SW 25250 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050906000542005090600054NM 2005 9 6 SWAA052660 120050901A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29423WN 29827 FWD CABIN EEPLS STRIP WORN. REMOVED AND REPLACED STRIP PER MM. 2L72 4F RTA16WE 20050906000552005090600055NM 2005 9 6 SWAA052661 120050901A53116546524 FRAME BOEING737 7373H4 1384600NM BS 360 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050906000562005090600056NM 2005 9 6 SWAA052662 120050901A53116520725 FRAME BOEING737 7373H4 1384600NM BS 440 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050906000582005090600058NM 2005 9 6 SWAA052664 120050831A2560PH22300L GLOWSTRIP BOEING737 7373H4 1384600NM CABIN DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29641SW 27714 DURING SCHEDULED RON CHECK, FOUND FWD CABIN PHOTOLUMINESCENT STRIP DAMAGED. REMOVED AND REPLACED STRIP PER MM. 2L72 4F RTA16WE 20050906000612005090600061NM 2005 9 6 SWAA052667 120050831A57436582770 ANGLE BOEING737 737317 138447PNM LT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED C1 CHECK, FOUND LT MLG STABILIZER BEAM OTBD ATTACH ANGLE CRACKED. REMOVED AND REPLACED ATTACH ANGLE PER SRM. 2L72 4F RTA16WE 20050906000652005090600065NM 2005 9 6 SWAA052623 120050829A52306547953 SKIN BOEING737 7373H4 1384600NM AFT CARGO CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29322SW 23343 DURING SCHEDULED C2 CHECK, FOUND AFT CARGO DOOR SKIN HANDLE CUTOUT CRACKED AT UPPER AFT CORNER. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050906000662005090600066NM 2005 9 6 SWAA052624 120050830A52306545775 SKIN BOEING737 7375H4 138449DNM CARGO DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29503SW 24180 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT AFT CARGO DOOR CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050906000682005090600068 2005 9 6 SWAA052626 420050829A256565C19901 CABLE BOEING737 7373A4 1384585NM L2 DOOR SLIDE MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED A1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE LATCH CABLE MISROUTED. REROUTED CABLE PER MM. 2L72 4F RTA16WE 20050906000692005090600069NM 2005 9 6 SWAA052627 120050830A53306545776 SKIN BOEING737 7373A4 1384585NM BS 940 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 940, STR 21L. REPAIRED SKIN PER SWA EA AND SRM. 2L72 4F RTA16WE 20050906000732005090600073 2005 9 6 SWAA052631 420050829A256563550 SLIDE BOEING737 7377H4 1384404NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29759GS 30544 DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050906000772005090600077NM 2005 9 6 AALA20050564 120050829A3350 LIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21765AN 32879 MIA - MOUNTED EMERGENCY LIGHT AT FORWARD CLOSET BROKEN. REPLACED MOUNTED EMERGENCY LIGHT ASSEMBLY AT FORWARD CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20050906000782005090600078NM 2005 9 6 AALA20050566 120050831A3350P4010051112 MODULE BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21680AN 29590 LGA - EMERGENCY LIGHT AT RIGHT FOUR DOOR INOPERATIVE. REPLACED BATTERY AND CHARGER M736 FOR EMERGENCY LIGHT AT RIGHT FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050906000792005090600079NM 2005 9 6 AALA20050568 120050825A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21913AN 29514 TUL - EMERGENCY LIGHTS IN FIRST CLASS CABIN AT STATION 380 TO 400 AND LEFT REAR SERVICE DOOR AT STATION 927 TO 986 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN FIRST CLASS CABIN AT STATION 380 TO 400 AND LEFT REAR SERVICE DOOR AT STATION 927 TO 986. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20050906000912005090600091WP 2005 9 6 MWEA050095 120050901A53479957871531 SEAT TRACK DOUG DC9 DC982 3022082WP COCKPIT DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 PIOLT SEAT INBOARD SEAT TRACK HOLES ARE ENLONGATED. FABRICATED AND INSTALLED SEAT TRACK. 2L72 4F A6WE 20050906000922005090600092WP 2005 9 6 MWEA050096 120050901A5280 DOUBLER DOUG DC9 DC982 3022082WP GEAR DOOR CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 RIGHT GEAR DOOR EDGES AND AROUND 3 RIVETS HAVE SURFACE CORROSION AND A LARGE AMOUNT OF BARE METAL IS SHOWING. FABRICATED AND INSTALLED REPAIR DOUBLER. 2L72 4F A6WE 20050906000932005090600093WP 2005 9 6 MWEA050097 120050901A53211120817 FLOORBOARD DOUG DC9 DC982 3022082WP STA 160-200 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 RIGHT SIDE OF STATION 160-200 FORWARD CABIN FLOORBOARD ATTACH ANGLE GOING FORWARD AND AFT FIRST INBOARD FROM SERVICE DOOR MANY AREAS OF CORROSION. FABRICATED AND INSTALLED FLOORBOARD SUPPORT ANGLE. 2L72 4F A6WE 20050906000942005090600094WP 2005 9 6 MWEA050098 120050901A5321993653457 FLOORBOARD DOUG DC9 DC982 3022082WP CABIN CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 8 FLOORBOARD ATTACH STRIP FIRST INBOARD OF PASSENGER DOOR HAS CORROSION. FABRICATED AND INSTALLED FLOORBOARD SUPPORT ANGLE. 2L72 4F A6WE 20050906000952005090600095NM 2005 9 6 AWXA200501019 120050830A3350321454 POWER SUPPLY AIRBUSA319 A319132 3930340NM EMERGENCY LIGHT DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28829AW 1563 PHX - EEL - DURING 8 DAY INSPECTION , THE EMERGENCY LIGHT TEST FAILED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY IAW AMERICA WEST AIRLINES TASKCARD R1C33303. OPERATIONAL TESTS GOOD. 2L72 4F RTA28NM 20050906000972005090600097NM 2005 9 6 AWXA200501021 120050831A315035EN144 SWITCH BOEING737 73733A 1384673NM STAB STUCK A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28175AW 23634 LAS - ABORTED TAKEOFF - FLT 162 - AFTER ADVANCING THROTTLES CREW RECEIVED TAKE OFF WARNING CONFIGURATION HORN. EXITED RUNWAY AND TAXIED TO THE GATE. MAINTENANCE TROUBLESHOT AND FOUND THE STABILIZER TAKE OFF WARNING SWITCH STICKING. REMOVED AND REPLACED THE STABILIZER T/O WARNING SWITCH, S132, IAW BOEING 737-300 MM 31-26-24-4. OPERATIONAL TESTS WERE GOOD. 2L72 4F RTA16WE 20050906000992005090600099GL 2005 9 6 YTRR105443 220050811A732323076061 GOVERNOR BELL 206 206B3 1181506SW ALLSN 250C 250C20B 03013GL ENGINE MALFUNCTIONED B HL9FO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 SO232043B369 3355 UNDER HEAVY LOAD IN CRUISE FLIGHT ENGINE WOULD OSCILLATE AND NOT RECOVER. R/R GOVERNOR AND PROBLEM DISAPPEARED 1G71 3U3 U H2SW E4CE 20050906001012005090600101SW 2005 9 6 YTRR105445 120050813A6220412010190103 SPINDLE BELL 412 412 1182202SW M/R HUB DEBONDED B YLYAK NONE O OTHER ININSP/MAINT 1 WP194125C2837 33103 ON ROUTINE INSPECTION FOUND ELASTOMERIC PIVOT BEARING DEBONDED BEYOND LIMITS. 1G72 4U H4SW 20050906001022005090600102SW 2005 9 6 YTRR105446 120050812A6220406310405101 BEARING BELL 407 407 1182206SW MAIN ROTOR WORN B YTRAK NONE O OTHER ININSP/MAINT 1 SW03595RL841 53595 M/R PC BEARING RADILA AND AXIAL LIMITS BEYOND MANUFACTURERS SPECIFICATIONS 1G71 3U O H2SW 20050906001042005090600104GL 2005 9 6 EGRA200501 220050212A725023032941 TUBE ALLSN 250C30S SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL NR 1 TURBINE CRACKED E EGRAK NONE K FLUID LOSS ININSP/MAINT 1 EA17763MH CAT90531 760230 CAE890276S AFTER NORMAL LANDING AND SHUTDOWN AT HOSPITAL A LARGE PUDDLE OF OIL WAS FOUND UNDER THE AIRCRAFT. FURTHER INVESTIGATION SHOWED OIL COVERING NR 1 ENGINE DECK AND OIL QUANTITY WAS DOWN BY THREE QUARTS. OIL TEMP AND PRESS WERE NORMAL AT SHUTDOWN. THE LABYRINTH SEAL SUPPLY TUBE WAS FOUND TO BE CRACKED OFF FROM THE ESHAUST COLLECTOR FLANGE ADAPTER AND MISPLACED ABOUT HALF THE TUBE DIAMETER. THIS RESTRICTED AIR FLOW TO THE LAB SEAL ALLOWED OIL TO FLOW OVER THE LAB SEAL. TURBINE SECTION WAS WITHIN 30 CYCLES OF BEING REMOVED DUE TO TURBINE WHEEL CYCLES. MECHANIC ON DISASSEMBLY REPORTED THAT TUBE MAY HAVE BEEN ORIGINALLY TIGHTENED UNDER A TWISTING LOAD. TURBINE SECTION WAS REPLACED. 1G72 3U3 U H1NE E1GL 20050906001052005090600105SW 2005 9 6 ALGA105522 120050818A6320206040032105 BEARING BELL 206 206L3 1182108SW TRANSMISSION MAKING METAL B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03351AL 51431 TRANSMISSION ASSEMBLY MAKING METAL, DISASSEMBLED AND FOUND DUPLEX BEARING BREAKING DOWN. / REMOVED AND REPLACED DUPLEX BEARING P/N 206-040-032-105 1G71 3U H2SW 20050906001072005090600107SW 2005 9 6 ALGA105532 120050812A6220406310405101 PITCH LINK BELL 407 407 1182206SW MAIN ROTOR WORN B ALGAK NONE O OTHER ININSP/MAINT 1 SW03497AL613 53172 EXCESSIVE BINDING AND AXIAL PLAY / REPLACED WITH NEW BY FIELD MAINTENANCE 1G71 3U O H2SW 20050906001092005090600109EU 2005 9 6 MALA060675 120050826A2760HC579H0351203U SEAL BAC 146 AVRO146RJ85A1500097EU SPOILERS DAMAGED A MALAO OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 GL15508XJ E2318 VIBRATION IN RANGE OF 280 TO 287 KIAS MAINT VERIFIED RIGHT MID SPOILER FLUTTERING. DURING EPISODE NOTED RT MID LIFT SPOILER FLUTTERING IN FLT. OTHER SPOILERS CHECK OK. NOTED MID SPOILER SEAL REQUIRES RE-CONTOURING. RE-CONTOURED T/E SEAL DUE TO SEAL GAP. SEAL IS CONTOURED FLUSH WITH FLAP TAB. AC TO BE FERRIED FROM MEM TO MSP WITH AIRSPEED RESTRICTED TO BELOW 250 KTS. RHOB LIFT SPOILER SEAL TS AND REPAIRS. REPLACED RHOB LIFT SPOILER TE PN HC579HO351-203U IAW SRM 57-72-11 2H74 4F RTA49EU 20050906001102005090600110EU 2005 9 6 MALA050677 120050827A2150 ODOR SAAB SF340 340B 7860101EU AIR CONDITIONER DETECTED A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL15362PX 340B258 IN FLIGHT PAX IN THE REAR OF THE AIRCRAFT NOTICED A METALLIC SMELL COMING FROM THE SUPP A/C VENT. CREW THEN SHUT THE SUPP A/C DOWN. ON THE GROUND CREW THOUGHT THAT THE SMELL WAS FROM THE VENT ALSO. NO FURTHER INFORMATION AT THIS TIME 2L72 4T RTA52EU 20050906001122005090600112WP 2005 9 6 ABXA050208 120050831A2120 DUCT DOUG DC9 DC941 302207NWP RT ACM LOOSE A ABXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL23964AX 47781 AT FL 350 LOST CABIN PRESSURE. LT PACK WAS NOT PROVIDING PRESSURIZATION BUT WAS IN AUTO AND INDICATED 160 PSI. ONLY ABLE TO MAINTAIN FL 210 WITH RIGHT PAC AT 260 PSI. BOTH PAC TEMPS NORMAL. FOUND RIGHT ACM DISCHARGE DUCT LOOSE AND RESECURED. REMOVED AND REPLACED LEFT WATER SEPERATOR BAG. OPS CHECKED GOOD IAW DC-9 AMM 21-00. 2L72 4F A6WE 20050906001142005090600114NM 2005 9 6 QXEA200501198 120050830A3620 WARNING LIGHT BOMBDRDHC8 DHC8402 1390042NM NR 1 BLEED SYS ILLUMINATED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09411QX 4055 SMR FLIGHT 2359: NR 1 BLEED HOT CAUTION LIGHT CAME ON DURING TAXI. MAINTENANCE C/W FIM TASK Q400 36-20-00-810-801 AND C/W OPS TEST BLEED AIR SYSTEM PER Q400 AMM 36-11-00-710-802. NO DEFECTS NOTED. OK TO CONTINUE. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050906001152005090600115CE 2005 9 6 SDR08310526 120050831A2613434422123 OVERHEAT SENSOR BEECH 18 H18 1151012CE RT WING SHORTED E HKGAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW17228A 502 BA629 DURING CLIMB, A RIGHT WING OVERHEAT INDICATION. SELECTED GEAR DOWN, AND CONDITION CONTINUED. SHUT RT ENGINE DOWN, AND RETURN TO KSDF. MX INSPECTED THE RT WING LE AREA, AND FOUND NO INDICATION OF OVERHEAT, BLEED AIR LEAKS, OR ELECTRICAL PROBLEMS. WING OVERHEAT SENSOR TESTED USING A HEAT GUN, AND OPERATION WAS NORMAL. EXTENDED ENGINE RUNS WERE CONDUCTED AND THE CONDITION WAS NOT DUPLICATED. THIS AIRCRAFT HAD BEEN PARKED ON THE RAMP AT KSDF DURING THE PASSING OF THE REMAINS OF HURICANE KATRINA, AND THE PROBLEM IS SUSPECTED TO BE ASSOCIATED WITH AN ACCUMULATION OF MOISTURE IN THE AREA OF THE SENSOR. THE USE OF THE HEAT GUN DURING THE TROUBLESHOOTING PROCESS PROBABLY DRIED THE AREA ELIMINATING THE MOISTURE. 1L72 3R A765 20050906001172005090600117GL 2005 9 6 CHQA200500155 220050829A7200 ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 2 UNSERVICEABLE A CHQAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 GL11561RP5816 1555 145447 CAE312123 FLIGHT 6285 - MCO-CMH - AFTER DEPARTING MCO DURING THE INITIAL CLIMB LAV SMOKE WAS DISPLAYED ON THE EICAS ACCOMPANIED BY A TRIPLE CHIME. CONTACTED THE FLIGHT ATTENDANT SOON AFTER AND ASKED HER TO CHECK THE LAVATORY FOR ANY SIGN OF SMOKE OR FIRE. FLIGHT ATTENDANT REPORTED NO VISIBLE SIGN OF SMOKE OR FIRE BUT INDICATED THAT SHE AND OTHER PASSENGERS NOTICED A BURNING SMELL. ELECTED TO RETURN TO THE FIELD WITHOUT ANY COMPLICATIONS OR DELAY FOR FURTHER INSPECTION. PERFORMED TROUBLESHOOTING AND FOUND ENGINE NR 2 CAUSING SMOKE. REMOVED AND REPLACED NR 2 ENGINE IAW CHQ JOBCARD CE720001. 2L72 4T4 FRTT00011ATTE6CH 20050906001182005090600118SO 2005 9 6 CHQA200500156 120050831A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11260SK 145128 RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY IAW EMB 145 MM 33-50-09. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050906001202005090600120CE 2005 9 6 PNSA050804 120050830A3243 CALIPER CESSNA208 208B 2073701CE RT BRAKE SHEARED E PNSAK NONE S AFFECT SYSTEMS LDLANDING 1 AL039820F 208B0410 ON LANDING AT KCQ RIGHT BRAKE FAILED. MX FOUND TOP ANCHOR PIN OF RT BRAKE CALIBER SHEARED. BRAKE CAUSED DAMAGE TO WHEEL ASSY AND BRAKE TORQUE PLATE. REPLACED BRAKE TORQUE PLATE, ANCHOR PINS, WHEEL ASSY AND BRAKE PADS. AIRCRAFT RETURNED TO SERVICE. 1H71 3T A37CE 20050906001222005090600122CE 2005 9 6 2005F00097 120050830A5740501200742 FITTING BEECH 100 100BEECH 1152916CE WING CRACKED E K NONE O OTHER ININSP/MAINT 1 SO15577D 18421 B22 CRACK DETECTED IN WING FITTING DURING SIRM INSPECTION 1L72 3T A14CE 20050906001272005090600127EA 2005 9 6 HNAA0500080 120050831A242031708001A GENERATOR DHAV DHC8 DHC8311 1386006EA NR 2 FAILED A HNAAE ENGINE SHUTDOWN O OTHER CLCLIMB 1 EA07327EN2325323253 284 AT APPROXIMATELY 400 FEET ON DEPARTURE, NR 2 AC GEN CAUTION LIGHT ILLUMINATED. APPROXIMATELY ONE MINUTE LATER THE MASTER WARNING AND NR 2 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED. CONFIRMED OIL PRESSURE WAS AT 0 AND SHUTDOWN ENGINE. REMOVED AND REPLACED AC GENERATOR. 2H72 4T RTA13NM 20050906001292005090600129NM 2005 9 6 QXEA200501201 120050831A33506104781 BATTERY DHAV DHC8 DHC8202 2809007NM ZONE 200 INOPERATIVE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09379PH294 530 PDX - NR 1 AND NR 2 PASSENGER CEILING EMERGENCY LIGHTS INOPERATIVE AND LEFT EGRESS LIGHT. REMOVED AND REPLACED 3351 PS3 EMERGENCY POWER SUPPLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050906001302005090600130NM 2005 9 6 QXEA200501199 120050831A324483210001077 TIRE DHAV DHC8 DHC8202 2809007NM ZONE 700 BLOWN A QXEAA UNSCHED LANDING O OTHER CLCLIMB 1 NM09355PH34 500 BOI - ON FLIGHT 2204, NR 1 MAIN LANDING GEAR WHEEL BLOWN ON TAKEOFF. TIRE BLEW BEFORE RETRACTING GEAR. BELOW MAX LANDING WEIGHT. VERIFIED WITH CREW AIRCRAFT WAS BELOW MAX LANDING WEIGHT. C/W INSPECTION OF TIRE AND NACELLE/ENGINE AREA, FOUND LEFT OUTBOARD AFT DRAG STRUT FAIRING DAMAGED, NO OTHER DAMAGE NOTED. ALSO, INSPECTED PROPS AND ENGINE INLET AREA WITH NO DEFECTS NOTED. REMOVED AND REPLACED BOTH NR 1 AND NR 2 MAIN TIRES. INSPECTED BRAKES AND HYDRAULIC LINES WHILE TIRES REMOVED WITH NO DAMAGE NOTED. 2H72 4T RTA13NM 20050906001322005090600132NM 2005 9 6 AT0500029 120050712A3350767 BULB BOEING737 737 UTILSYSNM EMERGENCY LIGHT BURNED OUT A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15184AT 32656 RIGHT OUTSIDE AFT EMER LIGHT BY R2 DOOR DOES NOT ILLUMINATE. REMOVED AND REPLACED LIGHT BULB IAW B737 MM 33-51. OPS CHECK GOOD P/N OFF/ON 767 2L72 4F RTA16WE 20050906001332005090600133 2005 9 6 AT0500030 420050731A2330 WIRE BOEING717 717200 1383700NM HANDSET BURNED A ZZDAB EMER. DESCENT O OTHER APAPPROACH 1 SO15936AT 2484 55058 AFT HANDSET CORD MELTED AND PRODUCED STRONG ELECTRICAL ODOR. REMOVED AND REPLACED AFT F/A HANDSET, OPS CHECKS NORMAL, NO OTHER DISCREPANCIES NOTED, REF AMM 23-41. OK FOR SERVICE. 2L72 4F TRA6WE 20050906001362005090600136NM 2005 9 6 USAA200508005 120050830A575569392289 FITTING BOEING737 737301 1384611NM HINGE CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19591US 23936 FOUND 3/8" BY .045" CIRCULAR WEAR AT OUTBOARD HINGE BRACKET FOR NR 5 SPOILER BOARD, WBL 169.25R. DEFECTIVE PART REPLACED WITH IDENTICAL PART. 2L72 4F RTA16WE 20050906001372005090600137EU 2005 9 6 05FDEA02729 120050901A7120 MOUNT AIRBUS300 A300F4605R 3930327EU ZONE 400 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25659FE15605 757 NR 1 ENG FWD MOUNT 0/B AFT HOLE HAS PITTING CORROSION. REAMED HOLE WITHIN LIMITS IAW A300-600 SRM 54-51-81. CAD PLATED HOLE IAW A300-600 SRM 54-51-81 AND A300-600 SRM 51-21-10. 2L72 4F RTA35EU 20050906001382005090600138NM 2005 9 6 05FDEA02730 120050831A278040174 SWITCH BOEING727 7272S2F 1384O81NM K FLAPS DAMAGED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25201FE 22924 AFTER T/O DURING FLAP RETRACTION FROM 5 DEG TO 2 DEG AMBER LED LIGHT REMAINED ILLUMINATED S/O AUX PAN INDICATED NR 5 REMAINED EXT. PERFORMED QRH PROC AND LIGHT REMAINED ILLUM. RET TO LAND. REMOVED AND REPLACED NR 5 KRUEGER FLAP SWITCH AND STRAIGHTENED SWITCH ARM. REF M/M 27-82-001-4 OPERATES NORMAL. 2L73 4F A3WE 20050907000022005090700002SO 2005 9 7 C2XA05IA102 120050822A335078241 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716559 145603 MCI - CURING MAINTENANVE INSPECTION THE FORWARD OVERWING CEILING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 6 EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THA AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050907000032005090700003SO 2005 9 7 C2XA05CL072 120050826A2560P4010030 BATTERY EMB 145 EMB145XR 3260214SO FLASHLIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712166 14500831 CLE FLIGHT3237 THE CREW REPORTED THE F/A FLASHLIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE FLASHLIGHT BATTERY.OPERATIONAL CHECKS WERE GOOD. 2L72 4F RT 20050907000042005090700004SO 2005 9 7 C2XA05CL073 120050829A335078241 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712564 145618 CLE FLIGHT 2617 THE CREW REPORTED THE EMERGENCY FLOOR LIGHTING WAS INOPERATIVE AT ROW 12. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT INVERTER NR 6. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20050907000052005090700005SO 2005 9 7 C2XA05CL074 120050829A3350110049 CHARGER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714558 145598 DURING ROUTINE MAINTENANCE THE EXTERNAL WING EMERGENCY AFT LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE #4 EMERGENCY BATTERY CHARGER ASEMBLY.OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20050901000342005090100034EA 2005 9 1 REX2005F00028 120050613A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A REXAO OTHER O OTHER TXTAXI/GRND HDL 1 SO258936A2871 7936 FLAPS FAILED AFTER LANDING WHEN SELECTED UP DURING TAXI. RESET SYSTEM AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K) 2L72 4F4 FRTA21EA E15NE 20050901000382005090100038NM 2005 9 1 AMTA200500632 120050805A3350 BULB BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE EMERGENCY LIGHT INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11518AT 27974 L4 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. CLEANED SOCKET AND REPLACED BULB, OPS CHECK GOOD. (K) 2L72 4F4 FRTA2NM E12EU 20050901000462005090100046EA 2005 9 1 ASOA05645 120050723A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE BS 280 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27833AS 7246 DURING C-CHECK, THE INTERCOSTAL AT FS 280, RBL 9 OB OF THE CLIP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE INTERCOSTAL AT FS 280, RBL 9 IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050901000482005090100048NM 2005 9 1 USAA050984 120050805A5310 BEAM BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU BS 500 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US50585 23933 CLT - Q6 - BEAM, 3 INCH CRACK, STRINGER 8R, STA 500. ACCOMPLISHED SPLICE REPAIR. (K) 2L72 4F4 FRTA16WE E21EU 20050901000492005090100049NM 2005 9 1 AMTA200500641 120050814A2410727792M GENERATOR BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE RIGHT UNSERVICEABLE A AMTAH DEACTIVATE SYST/CIRCUITS H ELECT. POWER LOSS-50 PC CRCRUISE 1 GL11554TZ1336613366 32588 RT GENERATOR DRIVE DISPLAYED. GEN DRIVE LIGHT ILLUMINATED. GEN DRIVE DISCONNECTED. REMOVED AND REPLACED IDG IAW MM. LK AND OPS CHECK GOOD. (K) 2L72 4F4 FRTA2NM E12EU 20050901000662005090100066 2005 9 1 KBM2005F00222 420050623A310023093620010 AMMETER SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1B 6OO30NE COCKPIT READS HIGH E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH7963 2957 APMMETER, UNIT READS 30 AMP HIGH AND NEEDLE FLUCTUATING. REMOVED AND REPLACED. (DONE AT B2 CONVERSION). (K) 1G71 3U3 U H9EU E19EU 20050901000672005090100067EU 2005 9 1 KBM2005F00232 120050814A7931704A37642043 INDICATOR SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1D NE OIL PRESSURE INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1953SH 472 2009 NO ENGINE OIL PRESSURE INDICATION, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050901000742005090100074EA 2005 9 1 REX2005F00025 120050622A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A REXAO OTHER O OTHER APAPPROACH 1 SO258758D5660 7758 (REF NR: 05-078) FLAPS FAIL ON APPROACH AT 20 ON APPROACH, QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAPS AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K) 2L72 4F4 FRTA21EA E15NE 20050901000972005090100097EA 2005 9 1 ASOA05641 120050726A5210601R3167013 STEP CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27723EV 10132 10132 DURING A GROUND INSPECTION, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA EOOO63EN 20050901001072005090100107EA 2005 9 1 REX2005F00029 120050611A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS FAILED A REXAO OTHER O OTHER CLCLIMB 1 SO258524A9225 7524 (REF NR: 05-074) FLAPS FAIL MESSAGE AT ZERO WHEN RETRACTED. EMERGENCY DECLARED QRH FOLLOWED UNEVENTFUL LANDING WITH FLAPS 0. RESET FLAPS AND PLAED ON 72 HOUR WATCH IAW AD 98-20-01. (K) 2L72 4F4 FRTA21EA E15NE 20050901001252005090100125EU 2005 9 1 KBM2005F00234 120050806A243216061 BATTERY SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE MASTER DISCHARGED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH 2884 BATTERY, LOW VOLTAGE, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050901001292005090100129EA 2005 9 1 REX2005F00024 120050624A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS FAILED A REXAO OTHER O OTHER APAPPROACH 1 SO258524A9321 7524 (REF NR: 05-079) FLAPS FAIL ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAP SYSTEM AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K) 2L72 4F4 FRTA21EA E15NE 20050901001382005090100138EA 2005 9 1 REX2005F00012 120050727A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS FAILED A REXAO OTHER O OTHER APAPPROACH 1 SO258495B10290 7495 (REF NR: 05-091) FLAPS FAIL AT 30 DEGREES ON APPROACH, QRH FOLLOWED. LANDING UNEVENTFUL. FOUND FCL NOT IN 30 DETENT. RESET FLAPS AND COMPLIED WITH AD-98-20-01. MONITORING FLAPS FOR 72 HOURS. (K) 2L72 4F4 FRTA21EA E15NE 20050901001522005090100152EA 2005 9 1 REX2005F00035 120050526A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS FAILED A REXAO OTHER O OTHER TXTAXI/GRND HDL 1 SO258524A9205 7524 (REF NR: 05-068) FLAP FAIL. RESET SYSTEM AND PLACED ON 72 HOUR WATCH IAW AD98-20-01. (K) 2L72 4F4 FRTA21EA E15NE 20050901001592005090100159EU 2005 9 1 MALA050674 120050826A3320005WS00 WEU SAAB SF340 340B 7860101EU CABIN LIGHTS FAILED A MALAO OTHER L NO TEST CRCRUISE 1 GL15424XJ 340B424 BITE LIGHT ON LEFT SIDE OF OVERHEAD LIGHTS DO NOT ILLUMINATE WITH UPPER LAMPS TESTS. REMOVED AND REPLACED WEU PER AMM 31-50-05-4. OPS CHECK GOOD, P/N ON 006WS00, S/N ON 1596, P/N OFF 005WS00, S/N OFF 1464. 2L72 4T RTA52EU 20050901001612005090100161EU 2005 9 1 UPS05145295 120050831A2120 SMOKE AIRBUSA300 A300F4622R 3930360EU COCKPIT DETECTED A IPXAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO01130UP 0814 SMOKE IN THE COCKPIT. 2L72 4F RTA35EU 20050902000082005090200008NM 2005 9 2 DU4R0508184 120050824A5315 FLOORBEAM BOEING757 757232 1384965NM PWA 2037 PW2040 NE BS 480 DAMAGED B DU4RK NONE O OTHER ININSP/MAINT 1 SO15672DL 25977 FLOORBEAM AT BS 480 HAS SEVERAL ELONGATED HOLES FORM OB SEAT TRACK TO CREASEBEAM. 2L72 4F4 FRTA2NM E17NE 20050902000102005090200010EA 2005 9 2 SWIA200515486 120050819A5311 ANGLE CNDAIRCL600 CL6002B19 1900309EA BS 640 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07442SW ANGLE AT FS 640.00 CRACKED BETWEEN STR 9 AND STR 12L, ITEM FOUND AT ROUTINE INSPECTION. REPLACED LT SIDE REINFORCEMENT ANGLE AT FS 640 BETWEEN STR 9 AND 12 IAW SRM 51-42-06 AND 51-42-13. 2L72 4F RTA21EA 20050902000332005090200033WP 2005 9 2 UPS05845277 120050811A534037796631 FITTING DOUG DC8 DC871F 302199DWP FS 680 L1L CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 CRACK ON SPLICE FITTING ON LONG 1L STA 680. REMOVED CRACKED FITTING AND LONGERON SPLICE IAW SRM 51-1-20D, INSTALLED FITTING, SPLICE AND STRAPS IAW SRM 51-1-21,51-1-20D AND 51-01-23 FIG 48. 2L74 4F RT4A25 20050902000372005090200037WP 2005 9 2 UPS05845282 120050815A53409754022U503 FITTING DOUG DC8 DC871F 302199DWP FS 280 RBL50 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 STA 280 RBL 50 END FITTING CRACKED. REMOVED AND REPLACED END FITTING AT STA 280 RBL 50 IAW DWG 9754022 AND SRM 51-1-20D. 2L74 4F RT4A25 20050902000442005090200044 2005 9 2 UPS05845298 420050831A2350 MICROPHONE DOUG DC8 DC873F 302199FWP OXYGEN MASK INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 CAPTAINS O2 MASK MIC INOP. 2L74 4F RT4A25 20050902000502005090200050EA 2005 9 2 SWIA200515483 120050826A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY INTERMITTENT A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07930SW 7713 FWD CARGO SMOKE DETECTOR RED LIGHT STAYS ON AND INTERMITTENTLY GIVES WARNING. REPLACED CARGO BAY FORWARD SMOKE DETECTOR REF AMM 26-15-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050902000512005090200051EA 2005 9 2 SWIA200515484 120050826A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07920SW 7660 EMERGENCY CEILING LIGHT AT ROW 10 INOP. RE-LAMPED CEILING LIGHT AT ROW 10 AS REQUIRED. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050902000562005090200056WP 2005 9 2 ASMF200508015 120050827A801138334211 STARTER DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE LT ENGINE FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23216AM4322817589 49586 AIRCRAFT RETURNED TO PLATFORM DURING LT ENGINE STARTING, THE STARTER VALVE LIGHT TURNED ON BUT IT DID NOT HAVE TURN IN N2. DURING MAINTENANCE REVISION, THE LT STARTER WAS DETECTED DAMAGED. THE LT STARTER AND STARTER VALVE WERE REPLACED IAW MM 80-10-01/02 RESPECTIVELY, TESTED CORRECT. 2L72 4F4 FRTA6WE E9NE 20050902000582005090200058NM 2005 9 2 05FDEA02693 120050826A5753ARC4125502 FITTING DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575 48500 O/B FLAP FOUND CRACK AT UPSTOP BOLT LE STRUCTURE. REMOVED AND REPLACED UP STOP FITTING AS PER SRM 51-33-01 AND 51-31-01 VOL.II. 2L73 4F RTA22WE 20050906000012005090600001NM 2005 9 6 AALA20050562 120050829A3397 WIRE HARNESS BOEING767 767323 1385205NM EMERGENCY LIGHTSINOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21384AA 26996 SFO - EMERGENCY EXIT LIGHT AT SEAT 25B INOPERATIVE. CONNECTED SEAT HARNESS FOR EMERGENCY LIGHT AT SEAT 25B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050906000602005090600060NM 2005 9 6 SWAA052666 120050831A55236959227 BUSHING BOEING737 737317 138447PNM RT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED C1 CHECK, RT ELEVATOR TAB FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB NR 2 HINGE BUSHING AND HARDWARE PER MM. 2L72 4F RTA16WE 20050906000622005090600062NM 2005 9 6 SWAA052620 120050829A53306545765 SKIN BOEING737 7373H4 1384600NM BS 505 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 505, STR 16L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050906000712005090600071NM 2005 9 6 SWAA052629 120050829A3350D71701100 BATTERY PACK BOEING737 7377H4 1384404NM EMERGENCY LIGHT FAILED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29759GS 30544 DURING SCHEDULED HC2 CHECK, EMERGENCY LIGHTS BATTERY PACK FAILED TEST AT ROW 16 ABC. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050906000742005090600074EU 2005 9 6 AALA20050567 120050831A3350P4010049 BATTERY PACK AIRBUS300 A300B4605R 3930308EU CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2190070 513 SJU - EMERGENCY FLOOR LIGHTING BETWEEN ROWS 19 TO 26 INOPERATIVE. REPLACED BATTERY PACK AND CHARGER FOR EMERGENCY FLOOR LIGHTING BETWEEN ROWS 19 TO 26. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20050906000762005090600076NM 2005 9 6 AALA20050565 120050829A3350 LIGHT BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21388AA 27448 MIA - EMERGENCY LIGHT AT RIGHT FOUR DOOR INOPERATIVE. FOUND BAD CONTACT AT LIGHT ASSEMBLY. SECURED CONTACT FOR EMERGENCY LIGHT ASEMBLY AT RIGHT FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050906000902005090600090WP 2005 9 6 MWEA050094 120050901A53479957871502 SEAT TRACK DOUG DC9 DC982 3022082WP COCKPIT DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 CO-PILOT'S CREW SEAT INBOARD SEAT TRACK HOLES ARE ENLONGATED. FABRICATED AND INSTALLED NEW SEAT TRACK. 2L72 4F A6WE 20050906000962005090600096NM 2005 9 6 AWXA200501020 120050831A3260189929 PROXIMITY SENSOR BOEING737 7373G7 1384595NM NLG INOPERATIVE A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28158AW 23780 PHX - AIR TURN BACK - FLT 0032 - AFTER TAKEOFF, DURING CLIMB, NOSE GEAR WOULD NOT RETRACT. NOSE GEAR HAD BOTH RED AND GREEN LIGHTS ILLUMINATED. AIRCRAFT RETURNED TO PHX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE DISCOVERED THE S845 SWITCH, NOSE DOWN SWITCH, WITH HIGH RESISTANCE. REMOVED AND REPLACED THE NOSE DOWN PROXIMITY SWITCH IAW BOEING 737-300 AMM 32-61-00-1 AND 32-61-51-4. OPERATIONAL TESTS WERE GOOD. 2L72 4F RTA16WE 20050906000982005090600098SW 2005 9 6 ALGA105415 120050624A6210212015501115 BLADE BELL 212 212 1181420SW MAIN ROTOR CORRODED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03XATVM2704 30934 DURING ROUTINE MAINTENANCE INSPECTION CORROSION WAS FOUND ON THE SPAR AT LEADING EDGE SPLICE JOINT / BLADE WAS REMOVED FOR FURTHER INSPECTION, DUE TO EXTENT OF DAMAGE TO SPAR BLADE WAS SCRAPPED! 1G71 4U H4SW 20050906001062005090600106SW 2005 9 6 ALGA105536 120050822A5302206031329103S ATTACH FITTING BELL 206 206B3 1181506SW TAILBOOM MISINSTALLED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03158H 2974 WHEN LOCATING NEW FIRRING PILOT FOR BOLT LOCATED TOO HIGH / REPLACED WITH NEW 1G71 3U H2SW 20050906001112005090600111NM 2005 9 6 ABXA050207 120050829A335020131A BATTERY BOEING767 767281 1385109NM EMERGENCY LIGHT DISCHARGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23783AX 23016 EMERGENCY LIGHTS INOPERATIVE. SWAPPED EMERGENCY LIGHT BATTERY WITH SPARE. OPS CHECKED GOOD IAW B767 AMM 33-00. 2L72 4F RTA1NM 20050906001232005090600123EA 2005 9 6 COMA0560469 120050826A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA LEFT WING FAULTY A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01814CA5600 7387 FLIGHT 5441- WHILE AT GATE AT JAX RECEIVED A FLAP FAIL CAUTION MESSAGE. REPLACED THE LEFT BRAKE PPOSITION SENSING UNIT. 2L72 4F RTA21EA 20050906001282005090600128WP 2005 9 6 IXXA0500105O 120050901A3230 LANDING GEAR DOUG DC8 DC871F 302199DWP NOSE FAILED A IXXAO OTHER J WARNING INDICATION CRCRUISE 1 SW11822BX90880117 45813 WHEN LANDING GEAR LEVER IS SELECTED TO UPLATCH CHECK POSITIONS, DOOR LIGHTS AND LANDING GEAR UNSAFE LIGHTS ILLUMINATE. SAME RESULTS AFTER GEAR RECYCLE. THE NOSE GEAR DOOR STAYED CLOSED WHEN GEAR LEVER IS RETURNED TO UP POSITION BOTH LIGHTS GO OUT. ALSO THE LANDING GEAR LEVER IS VERY HARD TO MOVE. MAINTENANCE DEFFERED THIS TO DMI 32746 AND 32747. THE AIRCRAFT WAS RETURNED TO SERVICE. AS MORE INFORMATION BECOMES AVAILABLE IT WILL BE PROVIDED. 2L74 4F RT4A25 20050907000012005090700001SO 2005 9 7 C2XA05CL071 120050825A332072875005XX LIGHT EMB 145 EMB145EP 3260221SO CABIN LOOSE A C2XAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW2712934 145019 ORD FLIGHT 2243 THE CREW REPORTED A ELECTRICAL/SMOKE SMELL IN THE CABIN DURING CLIMB.THE AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND ROW 1A,2A CABIN LIGHTS TO HAVE ELECTRICAL SMOKE ODOR.THE BULBS WERE REMOVED AND THE A/C WAS RELEASED I/A/W MEL 33-20-00/-1.SUPPLEMENT TO FOLLOW. MAINTENANCE INSPECTED AND FOUND CONNECTOR ON LAMP FIXTURE OVER SEAT 2A LOOSE. RESECURED AND RELAMPED.OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20050907000202005090700020EA 2005 9 7 ASOA05642AA 120050729A52104442440105 CABLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE BINDING A ASOAK NONE O OTHER ININSP/MAINT 1 SO27836AS 7263 7263 DURING A GROUND INSPECTION, THE PASSENGER DOOR WOULD NOT OPEN OR LOCK AND TH DOOR ASSIST MOTOR WOULD NOT OPERATE THE DOOR ALL THE WAY. MAINTENANCE FOUND THE DOOR ASSIST CABLE WRAPPED AROUND THE DOOR HINGE AND REMOVED IT FROM AROUND THE HINGE. OPERATIONAL HECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050907000212005090700021NM 2005 9 7 05FDEA02734 120050902A5711ARB74131 SPAR DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 LT WING TOPSIDE FOUND CORROSION UNDER T/E PANEL JUST FWD OF O/B AILERON XORS 917.0 AND XORS 1040.0. REPAIR CARRIED OUT AS PER EA1-5710-87601. 2L73 4F RTA22WE 20050907000222005090700022 2005 9 7 SWAA052690 420050903A2565D31591478 SLIDE BOEING737 7373Q8 1384670NM L1 DOOR OUT OF LIMITS A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 L1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATED OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20050907000262005090700026NE 2005 9 7 DXTA200500936 220050829A7310 O-RING CESSNA560 560XL 2076702CE PWA 545 PW545A NE FUEL FILTER MALFUNCTIONED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07604QS 5605204 PCEDB0413 LEFT FUEL BYPASS ANNUNCIATOR (AMBER) ILLUMINATED ON TAKEOFF ROLL. REMOVED AND REPLACED LT FUEL FILTER AND O-RING'S IAW PWA MM 545A MAINTENANCE MANUAL. RAN A/C LEAK CHECK GOOD FUEL BYPASS AMBER LIGHT DID NOT ILLUMINATE (P/N C31J2404-0R11CA) ASSOCIATED O-RINGS IAW 73-10-05. 2L72 4F4 FRTA22CE E00059EN 20050907000332005090700033NM 2005 9 7 SWAA052692 120050902A53156545410 FLOORBEAM BOEING737 7373G7 1384595NM BS 664 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29670SW 23784 DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 664, LBL 24.75. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20050907000352005090700035NM 2005 9 7 SWAA052694 120050902A53206545410 FLOOR SUPPORT BOEING737 7373G7 1384595NM CABIN FLOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29670SW 23784 DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOOR SUPPORT CRACKED BETWEEN BS 660.5 TO BS 664, RBL 0.5, BL 0. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20050907000362005090700036NM 2005 9 7 SWAA052695 120050902A53126546568 BULKHEAD BOEING737 7373G7 1384595NM BS 1016 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29670SW 23784 DURING SCHEDULED 1/4D CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT DOME CAP, 5 O'CLOCK POSITION. REPAIRED WEB PER SWA EA. 2L72 4F RTA16WE 20050907000382005090700038NM 2005 9 7 SWAA052697 120050902A53306545775 SKIN BOEING737 7373G7 1384595NM R2 DOOR AREA CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29670SW 23784 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050907000432005090700043EA 2005 9 7 VTZA200500155 120050831A5320601R35031239 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA BS 621 CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27679BR 7662 RT FS 621 FLOOR SUPPORT IS CRACKED AT 1' IN ANGLE. 2L72 4F RTA21EA 20050907000442005090700044EA 2005 9 7 VTZA200500156 120050831A5320601R3111358 ANGLE CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27679BR 7662 RT 280 VERTICLE ANGLE IS CRACKED AT .5" BETWEEN FASTENERS. 2L72 4F RTA21EA 20050907000452005090700045NM 2005 9 7 HNAA0500083 120050816A53308533002414 SKIN PANEL DHAV DHC8 DHC8102 2809003NM BS 424-445 DEBONDED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07942HA427387219 163 SKIN WAS FOUND DISBONDED BETWEEN FRAMES AT STATIONS 424 AND 445 ON STRINGERS 24S, 27S, AND 28S. THE SKIN PANEL WAS REPLACED. 2H72 4T RTA13NM 20050907000462005090700046EA 2005 9 7 VTZA200500157 120050831A531260034017595 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27679BR 7662 RT SIDE PILOTS BULKHEAD AT FS 280 RBL 9.0 IS CRACKED AT 1.0" IN WEB RADIUS. 2L72 4F RTA21EA 20050907000472005090700047EA 2005 9 7 VTZA200500158 120050831A5210601R317725 DRAG ANGLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27679BR 7662 PAX DOOR AFT DRAG ANGLE IS CRACKED 1.5". 2L72 4F RTA21EA 20050907000492005090700049EA 2005 9 7 VTZA200500160 120050831A5320601R3111387 ANGLE CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27679BR 7662 LEFT 280 VERTICLE ANGLE IS CRACKED AT .5" BETWEEN FASTENERS. 2L72 4F RTA21EA 20050907000502005090700050EA 2005 9 7 VTZA200500161 120050831A5320601R311719 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA BS 484 CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27679BR 7662 INTERCOSTAL CRACKED AT .250" IN LENGTH ON RT OUTBD SIDE AT FS 484 RIGHT BETWEEN BL 36.00. 2L72 4F RTA21EA 20050907000522005090700052EA 2005 9 7 VTZA200500163 120050831A53206013501251 ANGLE CNDAIRCL600 CL6002B19 1900309EA BS 625 CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27679BR 7662 LT OBLIQUE ANGLE AT FS 625 IS CRACKED. 2L72 4F RTA21EA 20050907000552005090700055EA 2005 9 7 VTZA200500166 120050831A531260034017595 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA BS 280 CORRODED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27622BR 7187 FS 280 BETWEEN LBL AND RBL 9.0 HAS LEVEL 2 CORROSION. 2L72 4F RTA21EA 20050907000572005090700057NM 2005 9 7 AWXA200501025 120050808A5315654583471 STRAP BOEING737 7373G7 1384595NM FLOORBEAM BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28311AW 24712 DURING C15 CHECK DISCOVERED, FLOOR STRAP BROKEN BOTTOM OF BS 312 BEAM AT BL 45R. MAINTENANCE FABRICATED REPAIR PLATE IAW BOEING 737-300 SRM 53-10-51-2. INSTALLED FABRICATED REPAIR PARTS IAW BOEING 737-300 SRM 53-10-51-2. 2L72 4F RTA16WE 20050907000612005090700061NM 2005 9 7 AWXA200501029 120050904A5100 STRUCTURE BOEING737 7373G7 1384595NM FUSELAGE VIBRATION A AWXAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 WP28158AW 23780 LAX - AIR TURN BACK - FLT 106 - AFTER TAKEOFF, CREW REPORTED AIRFRAME VIBRATIONS. AIRCRAFT RETURNED TO LAX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE VISUALLY INSPECTED AND OPERATED ALL FLIGHT CONTROLS. PERFORMED YAW DAMPER BITE TESTS AND CHECKED STANDBY RUDDER. ALL CHECKED OK. AIRCRAFT WAS MAINTENANCE FERRIED TO PHX, WHERE CREW REPORTED NO ABNORMALITIES DURING FERRY FLIGHT. MAINTENANCE PREFORMED BITE CHECKS OF ELEVATOR CONTROL AND AILERON CONTROL, STAB TRIM, MACH TRIM AND FLAPS. INSPECTED MACH TRIM ACTUATOR, FLAPS AND INSPECTED ALL GEAR DOORS AND INSPECTED FOR FLOATING SPOILER. NO DAMAGE, DEFECTS OR FAULTS WERE NOTED. 2L72 4F RTA16WE 20050907000632005090700063EU 2005 9 7 YENA200557 120050828A3350 SIGN AIRBUS320 A320232 3930326EU EMERGENCY EXIT FAILED A YENAK NONE O OTHER CRCRUISE 1 EA15598JB 2314 FWD EMERGENCY EXIT LIGHTS NOT WORKING. REPLACED EXIT SIGN 50WL, CHECKS OK REF 33-51-00. THE 50WL LIGHT HOUSING IS A CONSUMABLE PART WITH NO SERIAL NUMBER. 2L72 4F RTA28NM 20050907000652005090700065SO 2005 9 7 C2XA05CL062 120050812A3230355022002 CONTROL UNIT EMB 145 EMB145LR 3260212SO MLG FAULTY A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW27149528685 4906 145067 CLE FLIGHT NR 2496 - THE CREW REPORTED, THE LANDING GEAR WOULD NOT RETRACT ON CLIMB-OUT. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20050907000672005090700067WP 2005 9 7 MWEA050100 120050902A4900 APU DOUG DC9 DC982 3022082WP APU BAY OVERTEMP A MWEAK NONE O OTHER ININSP/MAINT 1 GL31810ME 48072 TAIL COMPARTMENT HIGH LIGHT CAME ON. FOUND AUXILIARY POWER UNIT CONTROL VALVE LEAKING AND HOIST ACCESS PANEL OFF AND HOT AIR BLOWING OUT. REINSTALLED HOIST PANEL, VERIFIED LEAK AT V BAND CLAMP ON LOAD CONTROL OUTLET DUCT. REMOVED AND INSPECTED CLAMP, NO DEFECTS NOTED. RETURNED TO NORMAL CONFIGURATIONS. 2L72 4F A6WE 20050907000682005090700068NM 2005 9 7 MWEA050102 120050831A52805930583231 DOOR DOUG MD88 MD88 3023688NM MLG CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 LEFT MAIN LANDING GEAR INBOARD DOOR IS CRACKED ON THE INNER SURFACE AT THE FORWARD INBOARD CORNER. FABRICATED AND INSTALLED DOUBLER. 2L72 4F RTA6WE 20050907000722005090700072EU 2005 9 7 RAIA00509005 120050903A3397 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT LOOSE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03559HK 41075 FLT 5446 - JLN - FLOOR LEVEL EMERGENCY LIGHTS FROM ROW 3A-5A INOP. MAINTENANCE RESECURED CONNECTOR. 2L72 4T RTA41NM 20050907000742005090700074EU 2005 9 7 RAIA00508040 120050831A3397 WIRE JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT BROKEN A RAIAK NONE O OTHER ININSP/MAINT 1 CE03561HK 41077 FLT 5581 -STL - EMERGENCY ESCAPE PATH LIGHTING OUT. MAINTENANCE REPAIRED CONNECTION TO THE EMERGENCY LIGHTING AT SEAT 5A. 2L72 4T RTA41NM 20050907000752005090700075SO 2005 9 7 RAIA00508041 120050831A3397 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT LOOSE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03817HK 145058 FLT 5517 - STL - LEFT OVERWING EMERGENCY LIGHT INOP. MAINTENANCE RESEATED CONNECTION TO EMERGENCY LIGHT. 2L72 4T RTT00011AT 20050907000762005090700076SO 2005 9 7 RAIA00509001 120050901A3397 CONNECTOR EMB 145 EMB145 3260210SO EMERGENCY LIGHT LOOSE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03802HK 145066 FLT 3574 - PIT - EMERGENCY EXIT SIGN INOP. MAINTENANCE RESECURED ELECTRICAL CONNECTORS AND OPS CHECKS GOOD. 2L72 4F RTT00011AT 20050907000772005090700077EU 2005 9 7 RAIA00509004 120050902A3397 WIRE JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT BROKEN A RAIAK NONE O OTHER ININSP/MAINT 1 CE03574HK 41093 FLT 5437 - STL - EMERGENCY LIGHT DOES NOT ILLUMINATE. MAINTENANCE REPAIRED BROKEN WIRE TO LIGHT ASSY. 2L72 4T RTA41NM 20050907000782005090700078NM 2005 9 7 P5CA0501388 120050824A5230D20702 ACTUATOR BOEING747 747283B 1384867NM CARGO DOOR HOOK FAILED A P5CAK NONE L NO TEST ININSP/MAINT 1 EA15921FT 21575 SIDE CARGO DOOR HOOK ACTUATOR FAILED IN ELECTRICAL MODE. DEFERRED PER MEL 52-20. 2L74 4F A20WE 20050907000792005090700079EU 2005 9 7 YENA200558 120050829A5730824 ACCESS PANEL AIRBUS320 A320232 3930326EU WING LOOSE A YENAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 EA15517JB19637 1327 ON CLIMBOUT THRU FL220 FELT SIGNIFICANT VIBRATION IN FRONT PART OF AIRCRAFT IN BOTH PILOTS SEATS AND RUDDER PEDALS, REDUCED POWER AND LEVELED OFF AND STILL FELT SAME VIBRATION. ALL ENGINE INDICATIONS NORMAL. PERFORMED PROCESS OF TSM TASK 05-50-00-810-801. NO DEFECTS NOTED. UPON FURTHER INSPECTION FOUND PANEL 127BG AT ACCESS DOOR 824 EXTREMELY LOOSE. RE-SECURED PANEL IAW 53-12-13. 2L72 4F RTA28NM 20050907000812005090700081NM 2005 9 7 P5CA0501389 120050826A7830 SWITCH BOEING747 747283B 1384867NM PWA JT9 JT9D70A 52054NE T/REV STOW OUT OF ADJUST A P5CAO OTHER J WARNING INDICATION NRNOT REPORTED 1 EA15921FT 21575 689169 NR 2 ENGINE REVERSER UNSTOW. ADJUSTED NR 2 REVERSER STOW SWITCH PER MM 78-31-00. 2L74 4F4 F A20WE E3NE 20050907000822005090700082SO 2005 9 7 C2XA05SH102 120050818A491014526850401 FIREWALL EMB 145 EMB145LR 3260212SO APU CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716541 145542 SHV - DURING C-CHECK, APU FIREWALL HAS A CRACK AT 3 O`CLOCK POSITION. MAINTENANCE REPAIRED THE FIREWALL AT 3 O`CLOCK POSITION IAW EC5330-01483. THE AIRCRAFT WAS APPROVE TO RETURN FOR SERVICE. 2L72 4T RTT00011AT 20050907000832005090700083SO 2005 9 7 C2XA05SH103 120050818A532014521700007 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO BS 22-23 CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2721537 145523 SHV - DURING C-CHECK, THE LT OMEGA BEAM HAS CORROSION AT NUT PLATE BETWEEN FS 22-23. MAINTENANCE REPAIRED LT OMEGA BEAM AT NUT PLATE BETWEEN FS 22-23 IAW EC5320-01257. THE AIRCRAFT WAS APPROVE TO RETURN FOR SERVICE. 2L72 4T RTT00011AT 20050907000842005090700084SO 2005 9 7 C2XA05SH104 120050818A532014521700007 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716541 145542 SHV - DURING C-CHECK, THE LT OMEGA BEAM HAS CORROSION AT NUT PLATE BETWEEN FS 22-23. MAINTENANCE REPAIRED THE LT OMEGA BEAM CORROSION BETWEEN FS 22-23 IAW EC5320-01257. THE AIRCRAFT WAS APPROVE TO RETURN FOR SERVICE. 2L72 4T RTT00011AT 20050907000852005090700085SO 2005 9 7 C2XA05CL066 120050820A2611M83726316002P RELAY EMB 145 EMB145XR 3260214SO COCKPIT STICKING A C2XAO OTHER N FALSE WARNING CRCRUISE 1 SW2716183 14500914 CLE - FLIGHT NR 2674, THE CREW REPORTED A BAGGAGE SMOKE INDICATION IN FLIGHT 5 OR 6 TIMES. THE WARNING WENT AWAY AFTER 20-30 SECONDS EACH TIME. MAINTENANCE INSPECTED AND REPLACED RELAYS KO630, KO625, AND KO629. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RT 20050907000872005090700087SO 2005 9 7 C2XA05CL068 120050820A3260355022022 CONTROL UNIT EMB 145 EMB145EP 3260221SO MLG FAULTY A C2XAO OTHER J WARNING INDICATION DEDESCENT 1 SW27129465324 565 145052 CLE - FLIGHT NR 2623, THE CREW REPORTED A AIR/GROUND FAIL MESSAGE WHEN THE LANDING GEAR WAS EXTENDED. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20050907000902005090700090SO 2005 9 7 C2XA05TY051 120050827A329714521495405 WIRE HARNESS EMB 145 EMB145LR 3260212SO NLG PROX SHORTED A C2XAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW2716911 145446 FLT NUMBER 2703, LANDING GEAR AIR/GROUND FAIL EICAS MESSAGE ON CLIMB-OUT. ACFT RETURNED TO FIELD. MAINTENANCE REMOVED AND REPLACED THE NLG PROXIMITY SENSE HARNESS ASSY. ACFT WAS TEST FLOWN WITH NO DISCREPANCIES NOTED AND SUBSEQUENTLY RELEASED TO SERVICE. 2L72 4T RTT00011AT 20050907000922005090700092SO 2005 9 7 C2XA05TY052 120050826A555314504980602 FITTING EMB 145 EMB145LR 3260212SO VERTICAL STAB CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713995 145295 DURING A SCHEDULED 2C INSPECTION, THE VERTICAL STABILIZER RT FITTING WAS FOUND TO HAVE CORROSION INSIDE THE SPHERICAL BEARING HOUSING. THE CORROSION WAS REMOVED AND THE BEARING HOUSING WAS REAMED AND BUSHED AS PER EXPRESSJET EC5510-01124. 2L72 4T RTT00011AT 20050908000042005090800004NM 2005 9 8 05FDEA02745 120050903A5330 SKIN BOEING727 727200 138407ENM BS 1060 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 UPON FURTHER INVESTIGATION FOUND 2EA DENTS ON SKIN AT BS 1060, 2 INCH BELOW STR 29. 2L73 4F RTA3WE 20050908000052005090800005NM 2005 9 8 05FDEA02756 120050905A5347 SEAT TRACK DOUG MD11 MD11 3023602NM BS 872 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 MID CABIN AT STA 872 RBL 75 FOUND SEAT TRACK CROWN INBOARD SIDE CORROSION AS MARKED. CARRIED OUT REPAIR AS PER SRM 53-70-00 FIG.I VOL.I. CLASSIFIED MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050908000062005090800006NM 2005 9 8 05FDEA02757 120050905A5210 RETAINER DOUG MD11 MD11 3023602NM PAX DOOR DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 FWD CABIN DOOR 1 RIGHT AFT SEAL RETAINER FOUND DENTED AS MARKED. FWD CABIN DOOR 1 R/H AFT DENT PAN SEGMENT REMOVED AND NEW PAN INSTALLED AS PER SRM 51-31-01 VOL.II, SRM 51-33-01 VOL.II AND SRM 51-35-01 VOL.II. MINOR REPAIR PER GMM 6-2-100. 2L73 4F RTA22WE 20050908000092005090800009NM 2005 9 8 05FDEA02760 120050906A5753 ATTACH FITTING DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 LEFT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87629. 2L73 4F RTA22WE 20050908000102005090800010NM 2005 9 8 05FDEA02761 120050906A5753 ATTACH FITTING DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 LEFT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. CORROSION REPAIR CARRIED OUT AS PER EA 1-5750-87629. 2L73 4F RTA22WE 20050908000112005090800011SO 2005 9 8 FYO2005F00000 120050822A27206341902 BAR PIPER PA32 PA32301 7103207SO LYC O540 IO540* 41532EA RT RUDDER PEDAL CRACKED E FYOAO OTHER O OTHER NRNOT REPORTED 1 AL058216T11766 328206037 NOTICED EXCESS PLAY BETWEEN RT AND LT PEDALS DUE TO ELONGATED THRU BOLTS IN ASSY. UPON DISASSEMBLY, FOUND TUBE TO HAVE EXTREME CRACK RADIATING FROM THRU BOLT HOLE AND RADIATING AROUND TO BACK SIDE OF TUBE AND GOING OUT TO EACH SIDE IN A SPIRAL FRACTURE. PART WAS VERY NEAR TOTAL FAILURE. THIS PART IS IMPOSSIBLE TO INSPECT WITHOUT TOTALLY REMOVING AND DISASSEMBLING RUDDER BAR ASSY. BELIEVE THIS IS CAUSED BY PRESSING HARD ON PEDALS TO TURN NOSE WHEEL BEFORE AIRCRAFT IS IN MOTION, CAUSING A STRONG RADIAL FORCE BEING APPLIED TO RUDDER BAR. (AL05200502805) (K) 1L71 3O3 O A3SO 1E4 20050908000122005090800012NM 2005 9 8 05FDEA02493 120050817A5710 RIVET DOUG MD11 MD11 3023602NM AILERON LOOSE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25575FE 48500 LEFT WING TOPSIDE FIXED TRAILING EDGE ISLAND FWD AREA BETWEEN O/B FLAP AND I/B AILERON FOUND WORKING RIVETS ON FORWARD I/B CORNER. LEFT WING TOPSIDE FIXED TRAILING EDGE ISLAND FWD AREA BETWEEN O/B FLAP AND I/B AILERON I/B AND O/B CORNER SKIN TRIMMED. REPAIR FILLER AND DOUBLER FABRICATED AND MATERIAL USED AS PER DWG ARC 0583 AND SRM 51-71-00 PARAGRAPH 20B VOL II. HOT BOND REPAIR CARRIED OUT AS PER SRM 51-71-00 VOL II. MINOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050908000132005090800013NM 2005 9 8 UPS05245356 120050823A52806517563 DOOR BOEING727 72722C 138400FNM NLG CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01930UP 19096 NLG FWD LT DOOR HAS CORROSION UNDER SEAL AT I/B END. CORRODED SECTION REPLACED WITH FABRICATED SECTION IAW SRM 51-20-1 AND DWG 65-17563. 2L73 4F A3WE 20050908000142005090800014NM 2005 9 8 UPS05245357 120050825A5330 SKIN BOEING727 72722C 138400FNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01930UP 19096 SUSPECT SKIN CRACK AT UPPER FWD ENTRY DOOR CUT OUT BETWEEN STR 5 AND 6 L. PLEASE CARRY OUT NDI AND RECIFITY. REPAIR CARRIED OUT IAW SRM ADDENDUM EO B727-5330-1460-D OPT 1. 2L73 4F A3WE 20050908000152005090800015NM 2005 9 8 UPS05445355 120050823A532065B15069417 STIFFENER BOEING747 747212B 1384886NM BS 1460 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01526UP 21937 LT KEEL BEAM VERTICAL WEB SURFACE EXTERNAL ATT STIFFENER FOUND CRACKED AT STA 1460 LBL 9, CRACK LENGTH .625. STIFFENER REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050908000162005090800016WP 2005 9 8 UPS05845329 120050828A5712 RIB DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 LT WING LE LOWER RIB IS CRACKED AT XFS 622.500. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2 -0 FIG 2. 2L74 4F RT4A25 20050908000192005090800019WP 2005 9 8 UPS05845332 120050828A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 RT WING LE UPPER RIB IS CRACKED AT XFS 635.000. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2 -0 FIG 2. 2L74 4F RT4A25 20050908000212005090800021WP 2005 9 8 UPS05845334 120050828A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 RT WING LE SKIN IS CRACKED AT FASTENER HOLE XFS 666.250. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1. 2L74 4F RT4A25 20050908000232005090800023WP 2005 9 8 UPS05845336 120050829A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 RT WING LE UPPER RIB CRACKED .3450 LONG AT XFS 379 (MID CENTER LE). STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20050908000242005090800024WP 2005 9 8 UPS05845337 120050829A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 RT WING LE UPPER RIB CRACKED .3750 LONG AT XFS 312 (MID CENTER LE). STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20050908000262005090800026NM 2005 9 8 05FDEA02762 120050906A5753 ATTACH FITTING DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 LT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REPAIR CARRIED OUT AS PER EA 1-5750-87629. 2L73 4F RTA22WE 20050908000322005090800032NM 2005 9 8 05FDEA02767 120050906A5753 ATTACH FITTING DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 RIGHT WING - O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-87630. 2L73 4F RTA22WE 20050908000332005090800033NM 2005 9 8 05FDEA02768 120050906A5753 ATTACH FITTING DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 RIGHT WING - O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR PIN ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87630. 2L73 4F RTA22WE 20050908000342005090800034NM 2005 9 8 05FDEA02769 120050906A5753 ATTACH FITTING DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 RIGHT WING - O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR PIN ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 AND CARRIED OUT AS PER EA 1-5750-87630. 2L73 4F RTA22WE 20050908000352005090800035NM 2005 9 8 05FDEA02770 120050906A5753 ATTACH FITTING DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 RT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR PIN ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-87630. 2L73 4F RTA22WE 20050908000372005090800037NM 2005 9 8 05FDEA02772 120050906A5753 ATTACH FITTING DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 RT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. REPAIR CARRIED OUT AS PER EA 1-5750-87630. 2L73 4F RTA22WE 20050908000382005090800038NM 2005 9 8 05FDEA02773 120050906A5753 ATTACH FITTING DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 RT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. REPAIR CARRIED OUT AS PER EA 1-5750-87630 AND CLASSIFIED AS MINOR PER GMM 6-2-100. 2L73 4F RTA22WE 20050908000492005090800049NM 2005 9 8 05FDEA02774 120050906A5753 ATTACH FITTING DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 RT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. CORROSION REPAIR CARRIED OUT AS PER EA 1-5750-87632. 2L73 4F RTA22WE 20050908000502005090800050NM 2005 9 8 05FDEA02775 120050906A5753 ATTACH FITTING DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 RT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87632. 2L73 4F RTA22WE 20050908000532005090800053NM 2005 9 8 05FDEA02778 120050906A5753 ATTACH FITTING DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 RT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87632. 2L73 4F RTA22WE 20050908000552005090800055NM 2005 9 8 05FDEA02780 120050906A5753 ATTACH FITTING DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 RT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87632. 2L73 4F RTA22WE 20050908000562005090800056NM 2005 9 8 05FDEA02781 120050906A5753 ATTACH FITTING DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 RIGHT WING - O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87632. 2L73 4F RTA22WE 20050908000582005090800058WP 2005 9 8 UPS05845338 120050829A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 RT WING LE UPPER RIB CRACKED .375 LONG AT XFS 322 (MID CENTER LE). STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2 -0 FIG 2. 2L74 4F RT4A25 20050908000602005090800060WP 2005 9 8 UPS05845340 120050828A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 RT WING LE UPPER SKIN IS CRACKED AT XFS 580.000. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1 FIG 33. 2L74 4F RT4A25 20050908000612005090800061WP 2005 9 8 UPS05845342 120050828A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 RT WING LE UPPER SKIN HAS INTERGRANULAR CORROSION AT XFS 622.500. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1 FIG 38. 2L74 4F RT4A25 20050908000632005090800063WP 2005 9 8 UPS05845344 120050829A5712 RIB DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 LT WING LE LOWER RIB PREVIOUS REPAIR IS CRACKED AT XFS 347.750. REMOVED, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20050908000672005090800067WP 2005 9 8 UPS05845348 120050829A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 LT WING LE HAS INTERGRANULAR CORROSION IN SKIN AT XW 257. SKIN IS SPLIT T ALONG EDGE. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1. 2L74 4F RT4A25 20050908000682005090800068WP 2005 9 8 UPS05845349 120050829A5712 RIB DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 LT WING LE UPPER RIB IS CRACKED AT XS 435.789. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2 -0 FIG 2. 2L74 4F RT4A25 20050908000702005090800070WP 2005 9 8 UPS05845352 120050828A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 RT WING LE UPPER RIB IS CRACKED AT XFS 753.750. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2 -0 FIG 2. 2L74 4F RT4A25 20050908000722005090800072NM 2005 9 8 UPS05M45358 120050718A5347AFA7789547 SEAT TRACK DOUG MD11 MD11F 3023600NM BS 1963 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01256UP 48405 CABIN SEAT TRACK AT STA 1963 LBL =107 FOUND CORRODED CABIN SEAT/T AT STA 1963 LBL 107 SEAT/T CROWN 0102 CORROSION REMOVAL C/OUT FOUND MAT REMOVED OUT OF LIMIT (ORI THK 0.145" AND MAT REMOVED 0.0 55") AS PER SRM 53-70-00 FIG 3 V1 R.37. REMOVE SEAT/T FASTENERS AND REMOVED SPLICE CUT PER SRM 53-31-01V1 R1. NEW SEAT/T REPAIR SPLICE HAT AND SPLICE PLATE AND INSTALLED PER SRM 51-31-01.V2.R.37. 2L73 4F RTA22WE 20050908000782005090800078 2005 9 8 UG82005F00009 420050824A830030730422 GEARSHAFT BRAERODH125 HS125700A 4230170EU GARRTTTFE731TFE7313R1H 29001WP LP GEARBOX WORN E UG8AO OTHER O OTHER NRNOT REPORTED 1 GL2348FB 10032 257129 (REF CNTRL NR: PA05005) THE S.O.A.P. LAB REPORT INDICATED HIGH LEVEL OF IRON (STEEL) IN THE ENGINE. THE SAMPLE INDICATED A SPECIFIC (BELLEVILLE) WASHER IN THE LP COMPRESSOR GEARBOX WAS FAILING DUE TO A SHIFTING OF THE LP PLANETARY GEARSHAFT ASSY. AC WAS FERRIED FOR REPAIRS. ENGINE WAS DISASSEMBLED AS NECESSARY AND THE PLANETARY GEARSHAFT ASSEMBLY WAS REPLACED IAW THE 731 LIGHT MM. ALL REQUIRED OPERATIONAL CHECKS WERE CARRIED OUT IAW THE 731 LIGHT MM AND AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4F4 F A3EU E6WE 20050908000792005090800079NM 2005 9 8 SB05104 120050831A3297BACR13CG2AB RELAY BOEING737 7374B7 1384702NM MLG FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19432US 24554 CLT - FLT102 - AFTER TAKEOFF FROM CLT, THE LANDING GEAR HANDLE WOULD NOT MOVE PAST THE OFF POSITION. THE WARNING HORN WAS SOUNDING OFF ALSO. CREW DID NOT ATTEMPT THE OVER-RIDE TRIGGER BUT LOWERED THE LANDING GEAR AND RECEIVED A NORMAL GEAR INDICATION OF THREE GREEN LIGHTS. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE OPERATED LANDING GEAR RETRACTION AND EXTENSION NUMEROUS TIMES AND COULD NOT DUPLICATE PROBLEM. REMOVED AND REPLACED SENSING RELAYS R276 AND R280 AS PRECAUTIONARY. ACCOMPLISHED SATISFACTORY LANDING GEAR OPERATIONAL TEST PER MM 32-32-00. 2L72 4F RTA16WE 20050908000802005090800080NM 2005 9 8 05FDEA02731 120050901A5320 SPLICE DOUG MD11 MD11 3023602NM BS 1119 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 FWD CARGO COMPT, BETWEEN STA 1119 AND STA 6-10 ALONG L-52L, LONGERON SPLICE CORRODED. CORRODED SPLICE REMOVED AND NEW SPLICE INSTALLED AS PER DRAWING ADA8424 AND SRM 51-33-01. 2L73 4F RTA22WE 20050901001442005090100144EA 2005 9 1 PJM2005F00000 120050805A2820MS2874140300 LINE DHAV DHC3 DHC3 2800202EA FUEL SYSTEM LEAKING E PJMAO OTHER K FLUID LOSS NRNOT REPORTED 1 AL056868B 274 INFLIGHT FIRE RESULTED FROM SMALL PIN HOLE IN FUEL PRESSURE LINE MOUNTED TO AFT FACE OF FIREWALL, SPRAYED FUEL ONTO BACK OF INSTRUMENTS IN PILOTS INSTRUMENT PANEL. UNABLE TO DETERMINE IGNITION SOURCE. AC MADE EMERG LANDING, FIRE WAS EXTINGUISHED WITH ONBOARD HANDHELD EXTING. FULE LINE WAS CONSTRUCTED OF .2500 INCH ALUMINUM TUBING. SOURCE OF PIN HOLE WAS NOT IMMEDIATELY APPARENT, MAY HAVE BEEN CAUSED BY CORROSION INSIDE LINE DUE TO WATER CONTAMINATION FROM FUSELAGE, SITTING OUTSIDE FOR AN EXTENDED PERIOD OF TIME. THIS AC WAS RECENTLY REBUILD AFTER ACCIDENT. RECOMMEND THAT ALL OPEN FLUID AND AIR LINES BE PROPERLY PROTECTED DURING PERIODS OF STORAGE, OR REPLACED BEFORE RETURN TO SERVICE.(AL05200502784) (K) 1H71 3R A815 20050901001482005090100148EA 2005 9 1 REX2005F00041 120050509A3260 DOWNLOCK TARGET CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE MLG DIRTY A REXAO OTHER N FALSE WARNING APAPPROACH 1 SO258847A4031 7847 (REF NR: 05-062) ON APPROACH, AFTER SELECTING GEAR DOWN, RECEIVED (GEAR DISAGREE) NOSE NOT GREEN. FOLLOWED QRH. CHECKED AND CLEANED DOWN LOCK TARGETS. PERFORMED GEAR SWING IAW AMM, NO DEFECTS NOTED. (K) 2L72 4F4 FRTA21EA E15NE 20050901001572005090100157EA 2005 9 1 COMA0560470 120050826A2750860D10018ABCD FCU CNDAIRCL600 CL6002B19 1900309EA AVIONICS BAY FAULTY A COMAO OTHER J WARNING INDICATION CRCRUISE 1 SO01814CA2868 7387 FLIGHT 5441 - DURING CRUISE RECEIVED A FLAP HALFSPEED MSG FOLLOWED BY A FLAP FAIL CAUTION MESSAGE. CREW DECLARED AN EMERGENCY AND FLIGHT LANDED AT JAX WITH FLAPS AT ZERO DEGREES. REPLACED THE FLAP ELECTRONIC CONTROL UNIT. 2L72 4F RTA21EA 20050901001622005090100162NM 2005 9 1 UPS05445270 120050825A5740 FITTING BOEING747 747212B 1384886NM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01526UP 21937 RT BS 1241 WING UPPER REAR SPAR SIDE-OF-BODY KICK FITTING AREA FOUND HOLE NR 2 CRACKED AT KICK FITTING APPROX 0.060". RH NR 2 BOLT HOLE BUSHING REPAIRED AS PER EO NR B747-5740-17032. 2L74 4F A20WE 20050901001662005090100166NM 2005 9 1 UPS05545287 120050830A2131 CONTROLLER BOEING757 75724APF 1384969NM CABIN PRESSURE INOPERATIVE A IPXAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO01464UP 28268 RT PACK TRIPPED OFF AND LEFT PACK FAILED TO RESPOND IN FLIGHT. TESTED BOTH PACKS IAW MM 21-31-00-5. RERACK OF CABIN PRESSURE CONTROLLERS TEST PACK TEMP CONTROL IAW 21-51-00-5 AND 21-51-14-5 PLACARD INSTALLED. 2L72 4F RTA2NM 20050902000072005090200007NM 2005 9 2 DU4R0508181 120050824A5347 SEAT TRACK BOEING757 757232 1384965NM BS 368-400 CORRODED A DU4RK NONE O OTHER ININSP/MAINT 1 SO15672DL 25977 CORROSION ON RT OB SEAT TRACK BS 368 TO 400. 2L72 4F RTA2NM 20050902000242005090200024WP 2005 9 2 05FDEA02723 120050831A5712 RIB DOUG DC10 DC1010 3022110WP ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE RIGHT WING FIXED LEADING EDGE, AT XORS 347, ZONE 618, FOUND RIB CRACKED. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-20-00, VOL I, FIG 1, SHT 1, 3 AND 4. 2L73 4F A22WE 20050902000352005090200035WP 2005 9 2 UPS05845280 120050811A5340 FITTING DOUG DC8 DC871F 302199DWP FS 857 L10L CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 LONGERON END FITTING CRACKED AT FS 857.125 L10L. REMOVED AND REPLACED LONG END FITTING AT FS 857.125 L10L IAW SRM 51-1-8,51-1-20, 51-3-01 AND 53-3-0. 2L74 4F RT4A25 20050902000362005090200036WP 2005 9 2 UPS05845281 120050811A534036408874 FITTING DOUG DC8 DC871F 302199DWP FS 980 LBL40 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 MAIN CABIN TEE FITTING CORRODED AT FS 980 LBL 40. REMOVED CORROSION ON TEE FITTING AND FOUND TO BE OUT OF LIMITS IAW SRM 53-2-0. REMOVED AND REPLACED TEE FITTING AT FS 980 LBL 40 IAW SRM 51-3-0, 51-1-21, AND 51-3-2. 2L74 4F RT4A25 20050902000412005090200041WP 2005 9 2 UPS05845293 120050811A5340 FITTING DOUG DC8 DC871F 302199DWP FS 857 L18R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 FITTING CRACKED AT FS 857.125 L18R AFT SIDE. REMOVED AND REPLACED END FITTING AT FS 857.125 L18R IAW SRM 51-1-20D AND DWG 4750420. 2L74 4F RT4A25 20050902000452005090200045EA 2005 9 2 SWIA200515478 120050829A3397 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DIRTY A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07953SW 7813 CENTER STRIP OF EMERGENCY PATHWAY LIGHTING INOP. CLEANED CONNECTOR AS REQUIRED. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050902000732005090200073EA 2005 9 2 ASOA05650 120050804A3240 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE COCKPIT ILLUMINATED A ASOAO OTHER N FALSE WARNING APAPPROACH 1 SO27823AS 7196 DURING APPROACH, THE CREW RECEIVED (PARKING BRAKE SOV) AND (ANTI SKID) CAUTION MESSAGES. CREW EXECUTED A GO-AROUND AND COMPLIED WITH THE QRH. UPON LOWERING THE GEAR FOR LANDING THE MESSAGES EXTINGUISHED. EMERGENCY VEHICLES WERE REQUESTED TO BE ON STANDBY AS A PRECAUTION. THE AIRCRAFT LANDED SAFELY. MAINTENANCE CYCLED THE PARKING BRAKE AND TESTED ANTI-SKID SYSTEM WITH NO DEFECTS NOTED. MAINTENANCE ALSO VERIFIED HYDRAULIC PRESSURE IN THE NR 3 SYSTEM WITH NO DEFECTS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050902000842005090200084NM 2005 9 2 SWAA052638 120050830A3350MS155721 BULB BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29498WN 32480 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EXTERNAL EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050902000872005090200087NM 2005 9 2 SWAA052645 120050831A53116546558 FRAME BOEING737 7373H4 1384600NM BS 907 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L TO STR 8R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050902000882005090200088NM 2005 9 2 SWAA052646 120050831A53116546552 FRAME BOEING737 7373H4 1384600NM BS 827 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L TO STR 8R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050902001012005090200101NE 2005 9 2 COMA0560454B 220050819A7261 OIL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE LT ENGINE OVERSERVICED A COMAEA ENGINE SHUTDOWN UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 SO01940CA 7048 FLIGHT 5786- LEFT ENGINE OIL PRESSURE WARNING. FOUND OIL SYSTEM OVERSERVICED. REMOVED EXCESS OIL AND OPERATIONAL CHECKS WERE NORMAL. 2L72 4F4 FRTA21EA E15NE 20050906000362005090600036 2005 9 6 SWIA200515487 420050823A3418 BUTTON EMB 120 EMB120ER 3260203SO STALL WARNING STUCK A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07299SW 120329 STALL WARNING BUTTON STICKS IN DOWN POSITION. REMOVED AND REPLACED STALL WARNING PANEL. OPERATIONAL CHECKS GOOD IAW 27-00-00. 2L72 4T RTA31SO 20050906000372005090600037EA 2005 9 6 SWIA200515488 120050809A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FLOORBEAM CRACKED A SWIAO OTHER O OTHER ININSP/MAINT 1 NM07448SW 7678 FS 280, RT FLOORBEAM INBOARD AND OUTBOARD ATTACH ANGLES CRACKED, ITEM FOUND AT C-CHECK INSPECTION. FS 280 INBD & OB ATTACH ANGLES REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-42-13, 51-21-11, 51-25-16, 51-23-00. 2L72 4F RTA21EA 20050906000482005090600048WP 2005 9 6 AALA20050556 120050826A2530 OVEN DOUG DC9 DC983 3022083WP GALLEY FIRE A AALAO OTHER A FLAME/FIRE CRCRUISE 1 SW21966TW 53616 IAH INFLIGHT T1383/26AUG - RESIDUE IN LEFT OVEN IN FORWARD GALLEY CAUGHT FIRE. FLIGHT ATTENDANT CLOSED OVEN DOOR AND FIRE EXTENGUISHED. CLEANED LEFT HEAD OVEN IN FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050906000572005090600057NM 2005 9 6 SWAA052663 120050901A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 294 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 294, STR 13L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050906000722005090600072NM 2005 9 6 SWAA052630 120050829A3350D71701100 BATTERY PACK BOEING737 7377H4 1384404NM EMERGENCY LIGHT FAILED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29759GS 30544 DURING SCHEDULED HC2 CHECK, RT AFT GALLEY EMERGENCY LIGHTS BATTERY PACK FAILED TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050906001352005090600135NM 2005 9 6 USAA200508004 120050830A5330 SKIN BOEING737 7373B7 1384580NM BS 867 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19375US 22954 CRACK AT BS867 JUST BELOW S-23R. INSTALLED EXTERNAL DOUBLER PER SRM 53-00-01 FIG 201, DETAIL X. 2L72 4F RTA16WE 20050907000272005090700027CE 2005 9 7 DXTA200500942 120050830A5270 STRIKER CESSNA750 750 2076810CE CARGO DOOR OUT OF ADJUST E DXTAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL07967QS 7500067 DURING T/O ROLL AMBER EICAS MSG. BAGGAGE DOOR SEAL AND MASTER CAUTION ILLUMINATED BEFORE 80 KIAS. ABORTED T/O. ADJUSTED BAGGAGE DOOR SEAL SWITCH AND STRIKER PLATE DUE TO BAGGAGE DOOR SEAL CAS MESSAGE ON T/O ROLL. SYSTEM OPS CHECKED GOOD IAW CE-750 MM CH 52-31-01. 2L72 4J RTT00007WI 20050907000282005090700028CE 2005 9 7 DXTA200500939 120050830A275067183281 CONTROLLER CESSNA750 750 2076810CE TE FLAPS FAULTY E DXTAO OTHER J WARNING INDICATION APAPPROACH 1 GL07921QS2 7500241 AMBER FLAPS FAIL CAS MESSAGE ON FLAP EXTENSION FROM 15-35 DEGREES. RESET AND THEN WORKED NORMAL FOR SECOND APPROACH. FOUND BITE 3 SHOWING ON CONTROLLER. TROUBLESHOT SYSTEM TO A FAULTY CONTROLLER. REMOVED AND REPLACED W/REPAIRED UNIT. OPERATIONAL CHECK NORMAL. MAINTENANCE PERFORMED IAW CITATION 750 MM CH 27-50-00. 2L72 4J RTT00007WI 20050907000292005090700029CE 2005 9 7 DXTA200500945 120050831A323062420357 LINK CESSNA650 650 2076802CE NLG DAMAGED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07715QS 6507105 GEAR WOULD NOT RETRACT AFTER TAKEOFF. REPLACED NLG CENTERING SWITCH AND UPPER TORQUE LINK ASSY P/N 6242035-7 BALL LINK P/N 6242020-13 LINK BEARING P/N AIR6-42AD AND LINK SHAFT P/N 6242035-6 GEAR SWING FT OK CESS 650 MM 32/20/00. 2L72 4F A9NM 20050907000302005090700030CE 2005 9 7 DXTA200500943 120050830A3243991205017 MASTER CYLINDER CESSNA500 560CESSNA 2076750CE MLG BRAKES LEAKING E DXTAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07316QS3876 5600516 RIGHT PILOT'S BRAKE PEDAL SOFT. REMOVED AND REPLACED CO-PILOT'S LT & RT BRAKE MASTER CYLINDERS AND BLED BRAKE SYSTEM IAW 560 ULTRA MM 32-42, OPS CHECK GOOD. 2L72 4F RTA22CE 20050907000342005090700034NM 2005 9 7 SWAA052693 120050902A53206545410 FLOOR SUPPORT BOEING737 7373G7 1384595NM BS 664-668 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29670SW 23784 DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOOR SUPPORT CRACKED BETWEEN BS 664 TO BS 668, RBL 24.75. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20050907000372005090700037NM 2005 9 7 SWAA052696 120050902A5311907804 FRAME BOEING737 7373G7 1384595NM BS 303 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29670SW 23784 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303, L1 DOOR FWD LOWER STOP FITTING. REMOVED AND REPLACED STOP FITTING PER SRM. 2L72 4F RTA16WE 20050907000422005090700042EA 2005 9 7 VTZA200500154 120050831A5712601R102328 RIB CNDAIRCL600 CL6002B19 1900309EA RT WING CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27679BR 7662 RT BATT RIB IS CRACKED .750 BETWEEN THE ATTACHING FASTENERS. 2L72 4F RTA21EA 20050907000532005090700053EA 2005 9 7 VTZA200500164 120050831A5210601R5211680 DOOR FRAME CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27622BR 7187 PAX DOOR FRAME TOP RADIUS CRACKED AT 1 INCH IN LENGTH FORWARD OF DATUM 1 AT FS 338.90. 2L72 4F RTA21EA 20050907000542005090700054EA 2005 9 7 VTZA200500165 120050831A5210601R5211680 DOOR FRAME CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27622BR 7187 PAX DOOR FRAME TOP RADIUS CRACKED AT 1 INCH IN LENGTH FORWARD OF DATUM 1 AT FS 320.90. 2L72 4F RTA21EA 20050907000562005090700056EA 2005 9 7 VTZA200500167 120050831A53206013401251 ANGLE CNDAIRCL600 CL6002B19 1900309EA BS 625 CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27622BR 7187 LT OBLIQUE ANGLE AT FS 625 IS CRACKED. 2L72 4F RTA21EA 20050907000592005090700059NM 2005 9 7 AWXA200501027 120050808A552265C2575371 SKIN BOEING737 7373G7 1384595NM LT ELEVATOR DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28311AW 24712 DURING C15 CHECK DISCOVERED LT ELEVATOR LEADING EDGE DELAMINATED 12 INCHES INBOARD FROM OUTBOARD HINGE. MAINTENANCE REMOVED DELAMINATED PLIES ON THE LEADING EDGE, 12 INCHES FROM OUTBOARD HINGE IAW BOEING 737-300 SRM 55-20-01-2 FIG 201. BONDED REPAIR PLIES TO THE LT ELEVATOR 12 INCHES FROM OUTBOARD HINGE IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5521-05238-RC1. LEFT ELEVATOR WAS BALANCED AND FOUND WITHIN LIMITS IAW BOEING 737-300 SRM 51-60-04-0. 2L72 4F RTA16WE 20050907000602005090700060NM 2005 9 7 AWXA200501028 120050902A5610 SEAL BOEING737 7373G7 1384595NM COCKPIT WINDOW DIRTY A AWXAA UNSCHED LANDING O OTHER CLCLIMB 1 WP28303AW 24010 DFW - AIR TURN BACK - FLT 421 - AFTER DEPARTURE CREW REPORTED LOUD SQUEAL COMING FROM CAPTAIN'S WINDOW. AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE CLEANED AND LUBRICATED THE CAPTAIN'S SLIDING WINDOW SEAL. ALSO, RE-SEALED THE CAPTAIN'S FORWARD, L1, WINDOW. PRESSURIZATION CHECKS WERE GOOD. 2L72 4F RTA16WE 20050907000662005090700066WP 2005 9 7 MWEA050099 120050901A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 FOUR CEILING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERIES IN BATTERY PACK. 2L72 4F A6WE 20050907000732005090700073SO 2005 9 7 RAIA00509003 120050902A3397 WIRE EMB 145 EMB145 3260210SO EMERGENCY LIGHT BROKEN A RAIAK NONE O OTHER ININSP/MAINT 1 CE03820HK 145064 FLT 5575 - STL - EMERGENCY LIGHTING INOP. MAINTENANCE REPAIRED BROKEN WIRE. 2L72 4F RTT00011AT 20050907000912005090700091SO 2005 9 7 C2XA05SH106 120050829A532014521713003 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716541 145542 SHV - DURING C-CHECK MAINTENANCE, FOUND LT OMEGA BEAM LOWER FLANGE HAS CORROSION AT FRAMES 19A TO 23. MAINTENANCE REPAIRED LT OMEGA BEAM LOWER FLANGE IAW EC 5320-01257 REV A. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050908000022005090800002EU 2005 9 8 05FDEA02743 120050902A3260 PROXIMITY SENSOR AIRBUS300 A300F4605R 3930327EU PITCH TRIM MALFUNCTIONED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25651FE 728 ON DEPARTURE KMEM GEAR WOULD NOT RETRACK IN SYSTEM 2 PITCH TRIM TRIPPED OFF, ATS TRIPPED OFF BOTH WOULD NOT RESET. FLIGHT DIRECTOR INOP, A/P INOP, RETURN TO MEM. NOSE GEAR TORQUE LINK PROX DETECTOR 55GB HAD IMPACT DAMAGE REMOVED AND TEMP INSTALLED THE DETECTOR, THE W/U WAS FOR THE NR 2 SYS 55GB IS NR 1 SYS. NO DEF 82 GB INSTALLED 55GB SENSOR, ALSO REMOVED AND REPLACED 82GB FOR SYS NR 2. BOTH W/I LIMITS, NO ADJUSTMENT MADE, REF A300-600 M/M 32-00-0 0-4. SWUNG NOSE GEAR SEVERAL TIMES WITH NO FAULTS IN PROX BOX. 2L72 4F RTA35EU 20050908000072005090800007NM 2005 9 8 05FDEA02758 120050906A5753 ATTACH FITTING DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 LEFT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87629. 2L73 4F RTA22WE 20050908000082005090800008NM 2005 9 8 05FDEA02759 120050906A5753 ATTACH FITTING DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 LEFT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. CORROSION REPAIR CARRIED OUT AS PER EA 1-5750-87629. 2L73 4F RTA22WE 20050908000182005090800018WP 2005 9 8 UPS05845331 120050828A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 RT WING LE UPPER RIB IS CRACKED AT XFS 622.500. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2 -0 FIG 2. 2L74 4F RT4A25 20050908000512005090800051NM 2005 9 8 05FDEA02776 120050906A5753 ATTACH FITTING DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 RT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. CORROSION REPAIR CARRIED OUT AS PER EA 1-5750-87632. 2L73 4F RTA22WE 20050908000712005090800071WP 2005 9 8 UPS05845354 120050902A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 SKIN BULGE AND CRACK. ASSIGNED FERRY PERMIT NR 9148 TO SAA. PER NRC 788843 REPAIRED ON NRC 788844. PERFORMED LOW FREQ EDDY CURRENT INSP IN AREA OF SKIN BULGE AT FS 35 PER NDT SPM 06-10-2.002. MAT LOS S DETECTED AT FS 35 IN AREA BTWN L36 & L34R APPX 8". SKIN REPLACED. 2L74 4F RT4A25 20050908000732005090800073NM 2005 9 8 UPS05M45359 120050718A5347AFA7789542 SEAT TRACK DOUG MD11 MD11F 3023600NM BS 1841-1921 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01256UP 48405 CABIN SEAT TRACK AT STA 1841-1921 RBL = 107 FOUND CORRODED IN SEVERAL PLACES CABIN SEAT/T AT STA 1841-1921 RBL 107 CORROSION REMOVAL C/OUT PER SRM 53-70-00 V1.R.37, FOUND OUT OF LIMIT ORI THK 0.080" AND MAT REMOVED BEYOND ACCEPTED LIMIT. SEAT/T FASTENERS REMOVED AND SEAT/T SPLICE CUT STA 1831 PER SRM 53-70-00 F1,V1.R37. NEW SEAT/TRACK REPAIR SPLICE HAT AND SPLICE PLATE STA 1831-2007 RBL107 INSTALLED SRM 1-31-01V.2.R37. 2L73 4F RTA22WE 20050908000832005090800083NM 2005 9 8 05FDEA02735 120050902A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 UPPER CARGO, SEAT TRACK RBL 27 CORRODED AT STA 1745. UPPER CARGO STA 1745 RBL 27 SEAT TRACK REPAIRED AS PER SRM 53-70-00 VOLUME I FIGURE 1. THIS REPAIR IS CLASSIFIED AS MAJORE REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050908000852005090800085SO 2005 9 8 C2XA05BT065 120050826A323022250100003 SOLENOID VALVE EMB 145 EMB145EP 3260221SO NLG FAULTY A C2XAO OTHER J WARNING INDICATION CLCLIMB 1 SW27169271536415364 145006 CREW REPORTED, "NOSE GEAR DOORS DID NOT CLOSE ON FIRST RETRACTION CYCLE, CLOSED ON SECOND RETRACTION CYCLE ALL INDICATIONS GOOD." MAINTENANCE REMOVED AND REPLACED NOSE LANDING GEAR SOLENOID VALVE IAW EMB145 MM NR 32-53-02 AND OPS CHECKED GOOD IAW EMB145 MM NR 32-30-00. NO FAULTS NOTED. 2L72 4F RTT00011AT 20050908000862005090800086SO 2005 9 8 C2XA05SH107 120050831A491014526850401 FIREWALL EMB 145 EMB145LR 3260212SO APU BAY CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712540 145537 SHV - DURING C-CHECK MAINTENANCE, FOUND APU FIREWALL CRACKED AT 3 O'CLOCK POSITION AROUND RIVETS. MAINTENANCE REPAIRED APU FIREWALL AT 3 O'CLOCK POSITION IAW EC 5330-01496 DISPOSITION 2.0. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050908000892005090800089EU 2005 9 8 08142005A 120050814A2697 WIRE SAAB SF340 340B 7860101EU FIRE DETECTOR BROKEN A NSVAO OTHER N FALSE WARNING CRCRUISE 1 EA27242CJ 242 RT TAIL PIPE HOT LIGHT WILL NOT EXTINGUISH. REPAIRED BROKEN WIRE IN TAIL PIPE COWLING. 2L72 4T RTA52EU 20050908000912005090800091EU 2005 9 8 08152005D 120050815A2697 WIRE HARNESS SAAB SF340 340B 7860101EU FIRE DETECTOR DAMAGED A NSVAO OTHER N FALSE WARNING CRCRUISE 1 EA27242CJ 242 TAIL PIPE HOT LIGHT. REMOVED AND REPLACED 3 DETECTORS AND MIDDLE WIRE HARNESS. 2L72 4T RTA52EU 20050908000962005090800096EU 2005 9 8 08182005C 120050818A7697 CABLE SAAB SF340 340B 7860101EU POWER LEVER DAMAGED A NSVAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 EA27314CE 335 RT POWER LEVER DOES NOT CONTROL TORQUE INFLIGHT OR ON THE GROUND. REMOVED AND REPLACED RT POWER CABLE. 2L72 4T RTA52EU 20050908000972005090800097EU 2005 9 8 08202005A 120050820A2150 A/C PACK SAAB SF340 340B 7860101EU ODOR A NSVAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA27346CJ 346 SMELL OF BURNING WIRES DURING START. INSPECTED BOTH BATTERY COMPARTMENTS, INTERIOR LIGHTS FOR SHORTS, AC PACKS FOR OBVIOUS DAMAGE AND FORWARD ELECTRICAL COMPARTMENT FOR OBVIOUS DAMAGE OR EVIDENCE OF ELECTRICAL SPARKS. THIS A/C HAS BEEN INSPECTED FOR THE PURPOSE OF A FERRY FLIGHT AND DETERMINED TO BE SAFE FOR FLIGHT FROM LGA TO ALB. LEFT A/C PACK DMI'ED. 2L72 4T RTA52EU 20050908001002005090800100CE 2005 9 8 08222005A 120050822A5220 DOOR LATCH BEECH 1900 1900D 1154162CE EMERGENCY DOOR OUT OF ADJUST A NSVAK NONE O OTHER ININSP/MAINT 1 EA27171CJ UE71 EMERGENCY 4F DOOR HANDLE NOT FLUSHED WITH DOOR. RESEALED RT FWD EMERGENCY EXIT HANDLE. 2L72 4T RTA24CE 20050908001032005090800103 2005 9 8 BB05077 420050902A2565 SLIDE BOEING757 757225 1384959NM PASSENGER CABIN READS LOW A USAAK NONE O OTHER ININSP/MAINT 1 EA19602AU 22196 PHL - THE R2 EMERGENCY ESCAPE SLIDE INDICATED LOW PRESSURE. MAINTENANCE REPLACED THE SLIDE ASSEMBLY. OK FOR SERVICE. 2L72 4F RTA2NM 20050908001062005090800106EA 2005 9 8 SWIA200515495 120050829A274170609 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 NM07440SW ON CLIMB-OUT, STAB CH 1 INOP MSG APPEARED ON ED-2. REPLACED HSTCU IAW MM 27-41-01. OPERATIONAL CHECK GOOD, PN 7060-9 SN/OFF 1076. 2L72 4F RTA21EA 20050908001072005090800107EA 2005 9 8 SWIA200515496 120050831A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLT SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07407SW1502715027 7034 SPOILERON FAULT STATUS MESSAGE ON TAXI OUT. REPLACED RIGHT SPOILERON OUTBOARD PCU IAW 27-62-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050908001092005090800109EA 2005 9 8 SWIA200515498 120050829A274170609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07932SW4733 4733 7714 DURING FLIGHT STAB AND MACH TRIM CAUTION MESSAGES WERE DISPLAYED ON ED1. REPLACED HSTCU. OPERATIONAL CHECK GOOD IAW 27-41-01. 2L72 4F RTA21EA 20050908001122005090800112EA 2005 9 8 SWIA200515501 120050828A274170623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07908SW1089910899 7540 STAB CHANNEL 2 INOP, WOULDN'T ENGAGE. REPLACED STAB TRIM MOTOR CONTROL UNIT IAW CRJ MM 27-42-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050908001152005090800115NM 2005 9 8 SB05106 120050901A335020131A BATTERY PACK BOEING737 7373B7 1384580NM EMERGENCY LIGHT DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19515AU 23701 CLT - MAINTENANCE REPORTED THE FORWARD RIGHT EMERGENCY LIGHT AT THE SERVICE DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050908001162005090800116EU 2005 9 8 YENA200559 120050829A273031075440 CONTROL SERVO AIRBUS320 A320232 3930326EU LT ELEVATOR OUT OF RIG A YENAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 EA15517JB19638 1327 CLIMBING THROUGH FL180 FELT VIBRATION IN FLIGHT CONTROLS, RUDDERS AND PILOTS SEAT. AFT F/A'S REPORTED NOTICEABLE VIBRATION IN AFT PART OF AIRCRAFT. VIBRATION ALSO FELT IN LEVEL FLIGHT AND DESCENT. FLIGHT CONTROL STATUS PAGE NORMAL (AP WAS ON AND OFF) ACCOMP TSM 05-50-00-810-801. FOUND ELEVATOR BLUE SERVO LT CONTROL BEYOND LIMITS. REMOVED AND REPLACED SERVO IAW 27-34-00-220-052. ALSO FOUND ELEVATOR BLUE SERVO RT CONTROL WITH JAM NUT LOOSE ON ROD END. ADJUSTED & RETIGHTENED IAW TASK AMM 27-34-51. OK FOR SERVICE. VIBRATION REPORTING SHEET FOR OUTBOUND CREW HAD NO FURTHER REPORT. 2L72 4F RTA28NM 20050908001172005090800117EU 2005 9 8 UPS05145304 120050831A3350 LIGHT AIRBUSA300 A300F4622R 3930360EU EMERGENCY EXIT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01124UP 0808 EMERGENCY LIGHT WILL NOT TEST CORRECTLY. DEFERRED PER EML 33-51-05-2 DMP. COMPLIED WITH 33-51-09 TRANSFERRED TO DMI LOG AND PLACARD. 2L72 4F RTA35EU 20050908001192005090800119NM 2005 9 8 UPS05245313 120050829A5350 CLIP BOEING727 72722C 138400FNM PANEL 3427 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01930UP 19096 RT BODY FAIRING 3427 HAS SMALL CRACK AT FWD ATTACHING END CLIP. ATTACHING END CLIP REPLACED IAW SRM 51-20-04. 2L73 4F A3WE 20050908001202005090800120NM 2005 9 8 UPS05245314 120050830A5330 SKIN BOEING727 72722C 138400FNM BS 364 STR3L CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01930UP 19096 SUSPECT SKIN CRACK AT BS 364 STR 3 LT. DAMAGED AREA CUT OUT AND REPAIRED IAW SRM 53030-3 FIG 3A. 2L73 4F A3WE 20050908001212005090800121NM 2005 9 8 UPS05245316 120050822A5330 SKIN BOEING727 72722C 138400FNM BS 1263 S5L TO 6SCRATCHED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01930UP 19096 LIGHT SURFACE SCRATCHES FOUND ON SKIN AT BS 1263 BETWEEN S5L AND 6L. DAMAGED AREA FOUND OUT OF LIMITS, REPAIRED IAW SRM 53-30-3 FIG 13. 2L73 4F A3WE 20050908001232005090800123NM 2005 9 8 UPS05445311 120050824A5330 SKIN BOEING747 747212B 1384886NM BS 1980-2000 DENTED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01526UP 21937 INSPECTION TYPE:C FX LT LOWER FUSELAGE EXTERNAL SKIN SURFACE SUSPECT DENT MARK AT STA 1980 TO STA 2000 STR 43L TO STR 44L. FX BS 1986 TO BS 1998.5 BETWEEN STR 43L TO STR 44L SKIN REPAIRED AS PER SRM 53-30-03 FIG 1 SUBSEQUENT INSPECTIONS ARE NECESSARY FOR CAT B REPAIR REFER TO SRM 53-30-03 FIG 1 TABLE IV FOR INSP REQUIREMENTS. 2L74 4F A20WE 20050908001242005090800124NM 2005 9 8 UPS05445322 120050826A534065B386005 STRINGER CLIP BOEING747 747212B 1384886NM BS 2060 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01526UP 21937 BULK CARGO BS 2060 STR 28L FOUND 1EA TIE CLIP CRACKED, CRACK LENGTH 3/8". TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050908001252005090800125WP 2005 9 8 UPS05845324 120050827A5730576960036 DOUBLER DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 C3 RT LE LWR INNER DOUBLER CRACKED AROUND DRAIN HOLE (2 EA CRACKS). REMOVED, FABRICATED, AND INSTALLED INNER DOUBLER IAW DC-8 SRM 51-1-21 AND DWG 5769600. 2L74 4F RT4A25 20050908001312005090800131EU 2005 9 8 08262005A 120050826A2711 TRIM SYSTEM SAAB SF340 340B 7860101EU AILERONS MALFUNCTIONED A NSVAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27306CE 203 CONFIG WARNING ON T/O ROLL AT 70 KNOTS. INSPECTED AND FOUND STANDBY TRIM ADJUSTED OUT OF GREEN ARC. PERFORMED OPS CHECK IAW 27-32-10S, OPS CHECK GOOD. 2L72 4T RTA52EU 20050908001322005090800132CE 2005 9 8 08282005A 120050828A2780 STRUCTURE BEECH 1900 1900D 1154162CE LE FLAP WORN A NSVAO OTHER O OTHER TXTAXI/GRND HDL 1 EA27136MJ UE36 RIGHT INBD FLAP HAS A WORN SPOT. RIGHT INBD FLAP WELL HAS A CRACK. STILL WORKING THE DISCREPANCY. 2L72 4T RTA24CE 20050908001332005090800133NE 2005 9 8 08302005B 220050825A7320 CONTROL UNIT SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RT ENGINE MALFUNCTIONED A NSVAB EMER. DESCENT J WARNING INDICATION CLCLIMB 1 EA27321CJ 321 RT ENGINE TORQUE FLUX. REMOVED AND REPLACED DECU. OPS CHECK GOOD. 2L72 4T4 TRTA52EU E8NE 20050908001352005090800135CE 2005 9 8 09012005B 120050831A7603 POWER LEVER BEECH 1900 1900D 1154162CE LT ENGINE FLUCTUATES A NSVAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 EA27220CJ UE20 LT POWER LEVER MIGRATES WITH FRICTION ON TQ FLUCTUATED 2000 LBS DURING TAKEOFF. REPAIRED LT BACKLASH SPRING TENSION. OPS CHECK GOOD. 2L72 4T RTA24CE 20050908001362005090800136EU 2005 9 8 09022005A 120050901A7797 CONNECTOR SAAB SF340 340B 7860101EU DECU LOOSE A NSVAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 EA27305CE 202 DURING NORMAL POWER REDUCTION, RIGHT TORQUE INSTANTLY DROPPED FROM 60 PERCENT TO 20 IGNITION LIGHT COMES ON AND TORQUE RECOVERED. CHECKED AND TIGHTENED CONNECTOR ON DECU, NO DEFECTS NOTED, OPS CHECK GOOD. 2L72 4T RTA52EU 20050908001372005090800137EU 2005 9 8 09022005B 120050901A2612 FIRE LOOP SAAB SF340 340B 7860101EU LT ENGINE OUT OF POSITION A NSVAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 EA27299CJ 299 DURING TAKEOFF, LT ENGINE BLEED AIR LEAK LIGHT CAME ON. FOUND LOOP GROUNDING ON FRAME, RE-POSITIONED, OPS CHECK GOOD. 2L72 4T RTA52EU 20050908001382005090800138NE 2005 9 8 09022005C 220050901A7200 ENGINE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE NR 1 OVERTEMP A NSVABA EMER. DESCENT UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CRCRUISE 1 EA27221CJ UE221 NR 1 ENG OIL OVERTEMP AT 130 DEGREES, AND PSI AT OR BELOW 60. SHUT DOWN ENG IN-FLIGHT AT 7000'. ENGINE CHANGE IN PROGRESS. 2L72 4T4 TRTA24CE E26NE 20050908001392005090800139EU 2005 9 8 09022005D 120050901A3260 CIRCUIT BREAKER SAAB SF340 340B 7860101EU MLG INDICATOR TRIPPED A NSVAO OTHER P NO WARNING INDICATION DEDESCENT 1 EA27294CJ 294 NO GEAR INDICATION WHEN GEAR SELECTED DOWN. PILOT FOUND CIRCUIT BREAKER POPPED AND RESET IT, MEL'D GEAR. 2L72 4T RTA52EU 20050908001402005090800140NM 2005 9 8 SB05110 120050904A335020131A BATTERY PACK BOEING737 7374B7 1384702NM EMERGENCY LIGHT DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19438US 24560 CLT - MAINTENANCE REPORTED THE FORWARD ENTRY AREA EMERGENCY LIGHTS WERE DIM. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050908001452005090800145NM 2005 9 8 2005UALA00896 120050826A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE STA 1380 DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29588UA 26717 FRAME DENTED AT STA 1380 BETWEEN S26L AND S27L. TRIMMED OUT DAMAGES, ACP HEFC INSP, NO CRACK FOUND. FABRICATE, ALODINE, PRIME, AND INSTALL REPAIR PER TIMCO REO-G10819, REV B. 2L72 4F4 FRTA2NM E17NE 20050908001462005090800146NM 2005 9 8 2005UALA00897 120050826A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE STA 1440 DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29588UA 26717 FRAME DENTED AT STA 1440 BETWEEN S26L AND S27L. TRIMMED OUT DAMAGES, ACP HEFC INSP, NO CRACK FOUND. FABRICATE, ALODINE, PRIME, AND INSTALL REPAIR PER TIMCO REO-G10826. 2L72 4F4 FRTA2NM E17NE 20050908001492005090800149NM 2005 9 8 2005UALA00900 120050826A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE STA 1620, STR 25DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29588UA 26717 FRAME DENTED AT STA 1620, STR 25R. TRIMMED OUT DAMAGES, ACP HEFC INSP, NO CRACK FOUND. FABRICATE, ALODINE, PRIME, AND INSTALL REPAIR PER TIMCO REO-G10821, REV B. 2L72 4F4 FRTA2NM E17NE 20050908001522005090800152NM 2005 9 8 2005UALA00903 120050827A335078941 LAMP BOEING777 777222 1385219NM PWA PW4077PW4077 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29774UA 26936 SEAT MOUNTED FLOOR PROXIMITY LIGHT AAT SEAT 1E INOP. REPLACED EEL LAMP ASSY. 2L72 4F4 FRTT0001SE E46NE 20050908001542005090800154NM 2005 9 8 2005UALA00905 120050829A3350582233 POWER SUPPLY BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT DISCHARGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29182UA 25279 EMERGENCY LIGHTS UPPER DECK LEFT SIDE ROWS 16-17 SELF-ILLUM. SELF-TURNED OFF NOW. REPLACED POWER SUPPLY. 2L74 4F4 FRTA20WE E24NE 20050908001562005090800156NM 2005 9 8 2005UALA00907 120050827A3150 WARNING HORN BOEING757 757222 1384956NM PWA 2037 PW2037 NE ACTIVATED A UALAO OTHER J WARNING INDICATION DEDESCENT 1 WP29541UA 25253 ON DESCENT HAD FIRE WARNING HORN GO OFF. 2L72 4F4 FRTA2NM E17NE 20050908001572005090800157NM 2005 9 8 2005UALA00908 120050826A2800 ENGINE BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 2 FLAMED OUT A UALAD RETURN TO BLOCK X ENGINE FLAMEOUT TXTAXI/GRND HDL 1 WP29514UA 24839 727109 ENGINE FLAMEOUT DURING NR 2 ENGINE START. 2L72 4F4 FRTA2NM E17NE 20050912000012005091200001EU 2005 9 12 YENA200561 120050904A3350 BATTERY AIRBUS320 A320232 3930326EU EPSU FAILED A YENAK NONE O OTHER ININSP/MAINT 1 EA15598JB124 2314 FWD EPSU FAILED BATTERY SYSTEM CHECK. REPLACED FWD EPSU FIN 10WL PER AMM 33-51-38-04. 2L72 4F RTA28NM 20050912000022005091200002 2005 9 12 DXTA200500941 420050830A3197 GROUND STUD CESSNA750 750 2076810CE LOOSE E DXTAA UNSCHED LANDING GJ MULTIPLE FAILURE WARNING INDICATION CLCLIMB 1 GL07964QS 7500164 EMERGENCY RETURN DUE TO NUMEROUS FAILURES & CAS MESSAGES. IRS 2 FAULT/ FOLLOWED BY SUSPECTED IAC 2 FAILURE. FMS 2, RMU 2, DU 4 & DU 5 FAILED. AMBER CAS MESSAGES ASSOCIATED WITH IAC 2 FAILURE. CAS MESSAGES FADEC REV ADC L, FADEC FAULT LB, PRI-STAB TRIM FAIL, PITCH ROLL DISC, FLT CONTROL FAULT. CYAN MESSAGES CVR FAIL, FGC FAIL, RUDDER FLT CONTROL SHUT-OFF SWITCH ILLUM & PRIMARY TRIM FAILED RT BUSS SWITCHED TO EMERGENCY & WOULDN`T UNLATCH, X-TIE OPEN. RT T/R WOULDN`T DEPLOY & NLG STEERING FAILED. FLAP & SLAT FAILED & RT ENGINE INSTRUMENTS FAILED. FOUND RT BUSS DROPPING OFF LINE. RT ENGINE CURRENT TRANSFORMER FAILING CIRCUIT RESISTANCE TEST. RETORQUED GROUND NUT, TRANSFORMER PASSED TEST IAW C750 MM. 2L72 4J RTT00007WI 20050912000042005091200004NM 2005 9 12 SB05111 120050905A3260189929 UPLOCK SENSOR BOEING737 7374B7 1384702NM RT MLG FAULTY A USAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19780AU 24997 CLT - FLT415 - ON CLIMB-OUT FROM CLT, CREW REPORTED THE RIGHT MAIN LANDING GEAR RED AND GREEN LIGHT ILLUMINATED WHEN GEAR HANDLE WAS PLACED IN THE UP AND/OR OFF POSITION. CREW MOVED GEAR HANDLE TO DOWN POSITION AND RECEIVED A NORMAL GEAR INDICATION OF THREE GREEN LIGHTS AND NO RED LIGHTS. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE RIGHT MAIN LANDING GEAR UPLOCK SENSOR FAULTY. REMOVED AND REPLACED UPLOCK SENSOR PER MM 32-61-21-4. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050912000052005091200005NM 2005 9 12 TAMF20050005O 120050905A2797 WIRE BOEING767 767200 1385120NM SLATS CHAFED W TAMFA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO23768QT 23803 DURING TAKEOFF EICAS MSG L/E SLAT ASSYM DISPLAYED & LEADING EDGE LIGHT ILLUM WITH THE FLAP LEVER IN 1. BOTH FLAP POINTERS WERE CORRECT. THE AIRPLANE WAS RETURNED TO RNG FRM 27810500. WIRING W176-102-24 IN P-36 WAS REPAIRED IAW WDM 32-09-11 PAGE 1 SH 2. FIM 27-81-00 FIG 107 STEPS 1 TO 20A WAS PERFORMED WITH NORMAL RESULTS. SYSTEM OK. OVERWEIGHT LANDING INSPECTION (PHASE I, STEP A) WAS PERFORMED IAW AMM 05-51-35 PAGES 201 & 202; NO DAMAGES WERE FOUND. 2L72 4F RTA1NM 20050912000072005091200007 2005 9 12 SA05099 420050907A256561639103 BOTTLE AIRBUSA321 A321211 3930370EU ESCAPE SLIDE READS LOW A USAAK NONE O OTHER ININSP/MAINT 1 EA19167US9422 9222 1442 PIT - THE SLIDE BOTTLE PRESSURE AT DOOR R3 WAS LOW. MAINTENANCE REPLACED THE SLIDE BOTTLE AT DOOR R3. OK FOR SERVICE. 2L72 4F RTA28NM 20050912000092005091200009 2005 9 12 P5CA0501392 420050820A341737571835 COMPUTER BOEING747 747341 13848AMNM NR 1 ADC FAILED A P5CAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA15355MC 23395 "A" AUTOPILOT ALTITUDE HOLD INOP. "B" AUTO PILOT WOULD NOT ENGAGE. AIRCRAFT DIVERTED TO AMS. REPLACED NR 1 AIR DATA COMPUTER AND DEFERRED "B" AUTOPILOT MM 34-12-01. 2L74 4F RTA20WE 20050912000152005091200015EA 2005 9 12 SWIA200515508 120050902A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07934SW 7722 2ND OVERHEAD CABIN EMERGENCY LIGHT INOP. REPLACED 2ND OVERHEAD CABIN EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050912000202005091200020EA 2005 9 12 SWIA200515513 120050901A2710 CONTROL CABLE CNDAIRCL600 CL6002B19 1900309EA AILERONS OUT OF ADJUST A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07971SW 7947 AIRCRAFT REQUIRES EXCESSIVE AMOUNT OF RT WING DOWN TRIM. RETENSIONED LT AND RT AILERON CABLES IAW AMM 27-00-00. 2L72 4F RTA21EA 20050912000212005091200021EA 2005 9 12 COMA0560476 120050826A2121 COOLING FAN CNDAIRCL600 CL6002B19 1900309EA FAILED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01926CA 7027 FLIGHT 5523 - DISPLAY COOL CAUTION. DEFERRED MAINTENANCE PER MEL. 2L72 4F RTA21EA 20050912000222005091200022EA 2005 9 12 COMA0560477 120050830A2750865D1007 PDU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01967CA19698679 7134 FLIGHT 5301 - FLAPS FAIL CAUTION. REPLACED THE PDU. 2L72 4F RTA21EA 20050912000232005091200023EA 2005 9 12 COMA0560475 120050825A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01783CA7891 7315 FLIGHT 5212 - FLAPS FAIL CAUTION. REPLACED THE LT BPSU. 2L72 4F RTA21EA 20050912000242005091200024NM 2005 9 12 P5CA0501391 120050826A2620 CONNECTOR BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE FIRE SQUIB LOOSE A P5CAK NONE L NO TEST ININSP/MAINT 1 EA15858FT 20109 662599 NR 2 ENGINE SQUIB TEST FAILED ON FLIGHT ENGINEER PREFLIGHT. CLEANED AND RESEATED NR 2 ENGINE RT FIRE EXTINGUISHER BOTTLE SQUIB PLUG PER MM 26-11-00. 2L74 4F4 F A20WE E20EA 20050912000262005091200026NM 2005 9 12 P5CA0501395 120050906A7830 BALL SCREW HONEYWELL BOEING747 74746NF 13848BTNM T/R GEARBOX LACK OF LUBE A P5CAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA15450PA GRTE8139 30808 LOWER LT T/R ANGLE GEAR BOX FOUND BALL SCREW AT SHOP VISIT FOR LUBRICATION. REPLACED T/R ANGLE GEAR BOX, MM 78-31-22. 2L74 4F RTA20WE 20050912000282005091200028CE 2005 9 12 DJFA2005136 120050831A2731766214 CONTROLLER BEECH MU300 400A 1155402CE CABIN PRESSURE INTERMITTENT E DJFAO OTHER J WARNING INDICATION CLCLIMB 1 EA23455CW RK365 KMEM - KRUS TRIP ID 888513 THE CREW REPORTED THAT THE PITCH TRIM FAILED ON CLIMBOUT AT 10,500 FT 255 KTS. THE PITCH TRIM BEGAN OPERATING AT 30,000 FT, AND THEN FAILED AGAIN AT 12,500 FT DURING DESCENT. WHEN THE EMERGENCY PITCH TRIM WAS USED IT WAS OPERATING PROPERLY. WHILE SLOWING TO 250 KTS AT 7,500 FT THE PITCH TRIM BEGAN WORKING AGAIN. MAINTENANCE REPLACED THE PITCH TRIM CONTROLLER IN THE AFT CABIN. OPERATIONAL CHECKS WERE PERFORMED AND THE SYSTEM OPERATED NORMALLY. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4F RTA16SW 20050912000292005091200029NM 2005 9 12 UPS05M45361 120050719A5347S4929147 SEAT TRACK DOUG MD11 MD11F 3023600NM BS 1621-1521 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01256UP 48405 INSPECTION TYPE:C CABIN STA 1321-1521 LBL=75.25 FOUND SEAT TRACK CORRODED IN SEVERAL PLACES. CORROSION REMOVED & FOUND BEYOND LIMIT PER SRM 53-70-00 F.3.V1.R.37 THK REMAINED 0.050" & ORI THK 0.100" MAT. SEAT/T FASTENERS REMOVED FOR ACCESS & SPICE CUT AT STA 1266 & STA 1391 PER SRM 53-70-00.F1.V1R37.NE W SEAT/T REPAIR SPLICE HATS & SPLICE PLATES BET STA 1266 & 1391 LBL75. 25, INSTALLED PER SRM 53-70-00 F.1 V.1.R.37 & 51-31-01 V2.R37. 2L73 4F RTA22WE 20050912000302005091200030NM 2005 9 12 P5CA0501396 120050906A7830 BALL SCREW HONEYWELL BOEING747 74746NF 13848BTNM T/R GEARBOX CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 EA15450PA 8145 30808 UPPER RT T/R ANGLE GEAR BOX FOUND BALL SCREW CORRODED. REPLACED ANGLE GEAR BOX PER MM 78-31-22. 2L74 4F RTA20WE 20050912000352005091200035EA 2005 9 12 COMA0560487 120050904A3010356124310 ELEMENT CNDAIRCL600 CL6002B19 1900309EA LT PYLON MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01963CA 7127 FLIGHT 5414 - LEFT 14TH DUCT WARNING MESSAGE. REPLACED THE BLEED LEAK SENSE ELEMENT. 2L72 4F RTA21EA 20050912000362005091200036EA 2005 9 12 COMA0570100 120050904A5610NP1393226 WINDOW CNDAIRCL600 CL6002C10 1390015EA COCKPIT FAILED A COMAO OTHER O OTHER CRCRUISE 1 SO01376CA6277 10092 FLT 5841 - COPILOT'S SIDE WINDOW SHATTERED. REPLACED WINDOW. 2L72 4F RTA21EA 20050912000372005091200037EA 2005 9 12 COMA0560488 120050905A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAP FAILED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01956CA 7105 FLT 5805 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2L72 4F RTA21EA 20050912000382005091200038EA 2005 9 12 COMA0560489 120050906A5210 PUSHROD CNDAIRCL600 CL6002B19 1900309EA PAX DOOR OUT OF ADJUST A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01999CA 7230 FLIGHT 5781 - CABIN DOOR OUTER HANDLE CAUTION. ADJUSTED DOOR HANDLE PUSH ROD. 2L72 4F RTA21EA 20050912000402005091200040EA 2005 9 12 REXA200500107 120050901A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A REXAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO258543F 7543 FLAP FAILURE ON TAXI-OUT. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD 98-20-01. 2L72 4F RTA21EA 20050912000412005091200041SO 2005 9 12 SWIA200515514 120050510A5311 FRAME EMB 120 EMB120ER 3260203SO COCKPIT CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07566SW 120341 LT COCKPIT FLOOR PROP CRACKED AT FRAME 13, ITEM FOUND AT C-CHECK INSPECTION. REMOVED LT COCKPIT FRAME 13 AND REPAIRED PER SRM 53-10-10, MM 51-22-00, 51-30-01. 2L72 4T RTA31SO 20050912000442005091200044NM 2005 9 12 SWAA052719 120050906A53116546558 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L & STR 8R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050912000472005091200047NM 2005 9 12 SWAA052722 120050906A53116546555 FRAME BOEING737 7373H4 1384600NM BS 867 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050912000492005091200049 2005 9 12 SWAA052724 420050906A25656557463 GIRT BAR BOEING737 7373H4 1384600NM BS 344 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 DURING SCHEDULED D-CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FLOOR FITTING CORRODED AT BS 344. REMOVED AND REPLACED AFT GIRT BAR FLOOR FITTING PER SRM. 2L72 4F RTA16WE 20050912000502005091200050NM 2005 9 12 SWAA052725 120050906A53116546525 FRAME BOEING737 7373H4 1384600NM BS 380 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050912000512005091200051NM 2005 9 12 SWAA052726 120050906A53116546524 FRAME BOEING737 7373H4 1384600NM BS 360 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050912000522005091200052NM 2005 9 12 SWAA052727 120050906A53116546529 FRAME BOEING737 7373H4 1384600NM BS 440 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050912000552005091200055NM 2005 9 12 SWAA052730 120050905A275065446311 CONTROL VALVE BOEING737 7373G7 1384595NM TE FLAPS FAULTY A SWAAK NONE O OTHER ININSP/MAINT 1 SW29683SW 24008 FLAP LEVER MOVEMENT WAS RESTRICTED & BINDING WAS FELT IN FLAP LEVER. REMOVED AND REPLACED T/E FLAP CONTROL VALVE PER MM. 2L72 4F RTA16WE 20050912000562005091200056 2005 9 12 SWAA052731 420050903A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29706SW 27840 R1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20050912000572005091200057EA 2005 9 12 COMA0560478 120050830A2750855D10011 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS UNRELIABLE A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01506CA6918 7793 FLIGHT 5220A - FLAPS FAIL CAUTION. REPLACED THE RT BPSU. 2L72 4F RTA21EA 20050912000592005091200059NM 2005 9 12 SWAA052732 120050906A3350612825 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29713SW 27847 DURING SCHEDULED MV2 CHECK, FOUND LT FWD BULLNOSE EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20050912000602005091200060NM 2005 9 12 SWAA052733 120050825A3350BR2013 LIGHT BOEING737 7377H4 1384404NM ROW 8 LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29740SW 29276 EEPLS STRIP LOOSE AT ROW 8 DEF. SECURED STRIP PER MM. 2L72 4F RTA16WE 20050912000612005091200061NM 2005 9 12 SWAA052734 120050903A2750113A26101 BELLCRANK BOEING737 7377H4 1384404NM LT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29748SW 29800 DURING SCHEDULED MV2 CHECK, FOUND OUTBOARD AFT FLAP ACTUATING MECHANISM BELLCRANK CASTING CRACKED AT INBOARD SIDE OF LT WING. REMOVED AND REPLACED AFT FLAP ACTUATING MECHANISM BELLCRANK CASTING PER MM. 2L72 4F RTA16WE 20050912000622005091200062NE 2005 9 12 SWAA052735 220050904A7200 ENGINE BOEING737 7377H4 1384404NM CFMINTCFM567CFM567B22 13802NE RIGHT SHUTDOWN A SWAAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION NRNOT REPORTED 1 SW29748SW 29800 875814 INFLIGHT SHUTDOWN/DECLARED EMERGENCY. NR 2 ENGINE SHUTDOWN DUE TO SUSPECTED FUEL LEAK. NR 1 FUEL TANK DECREASED FUEL QUANTITY BY 700 NR IN 20 MINUTES. CHECKED FOR FUEL LEAKS, NONE FOUND. PERFORMED BITE CHECK, NO FAULTS RECORDED. 2L72 4F4 FRTA16WE E00055EN 20050912000632005091200063 2005 9 12 SWAA052698 420050906A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED SERVICE CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050912000652005091200065NM 2005 9 12 SWAA052700 120050905A53306545775 SKIN BOEING737 7373H4 1384600NM BS 863 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 863, STR 16L. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050912000662005091200066NM 2005 9 12 SWAA052701 120050905A52306547952524 DOOR FRAME BOEING737 7373H4 1384600NM AFT CARGO CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR FWD FRAME CRACKED AT BALANCE CABLE PULLEY MOUNT BRACKET. REMOVED AND REPLACED AFT CARGO DOOR PER MM. 2L72 4F RTA16WE 20050912000682005091200068NM 2005 9 12 SWAA052703 120050904A53156545410 FLOORBEAM BOEING737 7373H4 1384600NM BS 668 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29373SW 26581 DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 668, RBL 24.75. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20050912000712005091200071NM 2005 9 12 SWAA052706 120050906A253041600019 COFFEEMAKER BOEING737 7373H4 1384600NM AFT GALLEY FAULTY A SWAAK NONE O OTHER ININSP/MAINT 1 SW29385SW 26600 ELECTRICAL SMELL FROM AFT COFFEEMAKER. REMOVED AND REPLACED AFT COFFEEMAKER PER MM. 2L72 4F RTA16WE 20050906000402005090600040EA 2005 9 6 SWIA200515491 120050809A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA BS 625 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07448SW 7678 AFT EQUIP BAY, INTERCOSTAL CLIP IS CRACKED, FS 625.00 STR 14L ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIP IAW CRJ REO 601R-53-61-100 REV NC. 2L72 4F RTA21EA 20050906000422005090600042NM 2005 9 6 AWXA200501017 120050821A3610312N533811 DUCT BOEING757 757225 1384959NM BLEED AIR SYS DAMAGED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28914AW 22208 PHX - AIR TURN BACK - FLT 0049 - DURING CLIMB, AFTER TAKEOFF CREW RECIEVED NR 2 ENGINE OVERHEAT EICAS DURING CLIMB. CREW FOLLOWED QRH AND ISOLATED BLEED SOURCE. CREW DECIDED TO RETURN TO PHX. LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND DUCT LEAKING ON THE NR 2 ENGINE. REPLACED SEVERAL SEALS ON THE NR 2 ENGINE AND ALSO REPLACED THE Y DUCT ON THE NR 2 ENGINE, OPERATIONAL CHECKS GOOD. RETURNED TO SERVICE. 2L72 4F RTA2NM 20050906000512005090600051NM 2005 9 6 SWAA052657 120050901A53306545774 SKIN BOEING737 7373H4 1384600NM BS 727D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29324SW 23414 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 19R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050906000592005090600059NM 2005 9 6 SWAA052665 120050831A52406969854 GUSSET BOEING737 7373G7 1384595NM R1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29670SW 23784 DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR AFT LOWER GUSSET CRACKED. REMOVED AND REPLACED DOOR PER MM. 2L72 4F RTA16WE 20050906000632005090600063NM 2005 9 6 SWAA052621 120050829A53306545765 SKIN BOEING737 7373H4 1384600NM BS 492 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 492, STR 26L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050906000642005090600064NM 2005 9 6 SWAA052622 120050829A53306545776 SKIN BOEING737 7373H4 1384600NM BS 941 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 941, STR 21L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050906000672005090600067NM 2005 9 6 SWAA052625 120050830A55306549837 ANGLE BOEING737 7373H4 1384600NM VERTICAL STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 DURING SCHEDULED D CHECK, FOUND VERTICAL STABILIZER RT T/E ANGLE CRACKED AT RS 23.37. REMOVED AND REPLACED ANGLE PER SRM. 2L72 4F RTA16WE 20050906000702005090600070 2005 9 6 SWAA052628 420050829A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29701GS 27836 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050906000752005090600075NM 2005 9 6 AALA20050563 120050829A33508100033901 LIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21785AN 30005 JFK - EMERGENCY LIGHT AT ONE LEFT COAT CLOSET INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY FOR NUMBER ONE LEFT COAT CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20050906000802005090600080NM 2005 9 6 AALA20050561 120050828A3350D71702001 LIGHT BOEING737 737823 13844BZNM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21971AN 29547 DFW - SEAT MOUNTED EMERGENCY LIGHT AT SEATS 9D AND 13D AND 18D INOPERATIVE. REPLACED THE SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AT SEATS 9D AND 13D AND 18D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20050906001002005090600100SW 2005 9 6 YTRR105444 120050819A2910212076005101 SERVO BELL 412 412 1182202SW HYD SYSTEM LEAKING B YLYAK NONE O OTHER ININSP/MAINT 1 WP194125C 33103 ON ROUTINE INSPECTION FOUND HYDRAULIC SERVO LEAKING BEYOND ACCEPTABLE LIMITS. 1G72 4U H4SW 20050906001132005090600113NM 2005 9 6 QXEA200501197 120050828A7930800600M02 ACTUATOR BOMBDRDHC8 DHC8402 1390042NM NR 2 ENGINE LEAKING A QXEAO OTHER MJ OVER TEMP WARNING INDICATION CLCLIMB 1 NM09413QX 4060 IDA FLIGHT 2361: DURING CLIMB NR 2 ENGINE OIL TEMP INCREASED TO 112 DEG C. CLOSED ENGINE INTAKE PER CHECKLIST. IN LEVEL FLIGHT OIL TEMP STABILIZED AT 88 DEG C.INTERROGATED CDS, DETERMINED MAXIMUM OIL TEMP 112.3 DEG C FOR 277.3 SECONDS OR 12.88 MINUTES. MAINTENANCE FOUND NR 2 ENGINE OIL COOLER FLAP DOOR ACTUATOR INOP. REMOVED AND REPLACED ACTUATOR IAW AMM TASKS 79-21-31-000-801 AND-400-801. OPS CHECK GOOD. REF TO SUSTAINED RUNNING AT OIL TEMP OUTSIDE SPECIFIED LIMITS. REFERENCE CHART LIMITS AMM 05-11-00, PGA 609. C/W AMM TASK 05-23-00-210-814, SUBTASK 05-53-00-680-002, ITEMS 1-6 FOR MTX PROCEDURES. ENGINE RUN C/W. NO LEAKS NOTED. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050906001162005090600116NM 2005 9 6 USAA051063 120050830A5330 SKIN BOEING737 7373B7 1384580NM BS 869-887 CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US 23933 LOCATION: BS 869- BS 887 ACTION: REMOVED DAMAGE, INSTALLED TRIPLER IAW EA 96764 DEFECT SIZE: APPX 18 INCH AREA OF CHAFING ON SKIN BELOW DORSAL FIN TIP CONTACT AREA, BOTH SIDES 2L72 4F RTA16WE 20050906001192005090600119WP 2005 9 6 IXXA05SMN159S 120050809A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING DELAMINATED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL 46003 DURING ROUTINE C CHECK INSPECTION, LT WING.- T/E UPPER PANEL EXTERNAL SKIN DELAMINATED, XW 0.000 XW 47.000. REMOVED DELAMINATED PANEL AND REPLACED ON LH WING T/E UPPER PANEL EXTERNAL SKIN, XW 0.000 – XW 47.000 IAW DC8 SRM 51-3-0 2L74 4F RT4A25 20050906001212005090600121WP 2005 9 6 DHL2005802008 120050901A2612 FIRE LOOP DOUG DC8 DC873 302199CWP NR 2 ENGINE FAILED A DHLABA EMER. DESCENT UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO01802DH 46076 ENROUTE AT FL 370 WE HAD AN INTERMITTENT NR 2 FIRE INDICATION. AFTER BOTH BOTTLES WERE FIRED THE FIRE INDICATION REMAINED CONSTANT FOR APPROX 10 MIN AND WAS INTERMITTENT THROUGH REMAINDER OF FLT. LOOP-A FAILED TO TEST FOR FIRE WARNING, SHORT TEST GOOD. 2L74 4F RT4A25 20050906001252005090600125NM 2005 9 6 CALA0500287 120050901A5315141A550424 FLOORBEAM BOEING737 737824 13844BZNM STA 328 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712218 28778 INSPECTION FOUND PITTING CORROSION ON FLOORBEAM AT STA 328, RBL 58 IN THE GALLEY AREA. THE FLOORBEAM WAS REPAIRED IAW ECRA 5321-01281. 2L72 4F RTA16WE 20050906001312005090600131NM 2005 9 6 QXEA200501200 120050824A33506104781 BATTERY DHAV DHC8 DHC8202 2809007NM ZONE 200 INOPERATIVE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09349PH354 486 SEA - LEFT AND RIGHT EMERGENCY EGRESS LIGHTS, CENTER AND AFT EMERGENCY CEILING LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY POWER SUPPLIES AND BATTERY PACKS BEHIND CEILING PANEL 235BZ. REMOVED AND REPLACED BATTERY PACK PS4 BEHIND CEILING PANEL 245BZ. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050906001342005090600134SO 2005 9 6 C2XA05CL070 120050824A3350375921 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW2716951 145063 CLE FLIGHT 2748 THE CREW REPORTED THE OVERHEAD EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE FORWARD ISLE OVERHEAD EMERGENCY LIGHT.OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20050907000192005090700019NM 2005 9 7 SB05101 120050829A3260 WARNING LIGHT BOEING737 7373B7 1384580NM MLG FALSE INDICATIONA USAAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 EA19520AU 23706 CLT - UPON LOWERING LANDING GEAR, CREW RECEIVED A GEAR INDICATION OF 3 GREEN AND 3 RED. CREW ACCOMPLISHED A GO-AROUND, CYCLED THE GEAR AND RECEIVED A NORMAL GEAR INDICATION OF 3 GREEN. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE JACKED AIRCRAFT AND TROUBLESHOT SYSTEM. PERFORMED LANDING GEAR EXTENSION/WARNING CHECK PER JOB CARD J332-60-1 AND SWUNG GEAR SEVERAL TIMES. COULD NOT DUPLICATE PROBLEM. CLEANED AND LUBRICATED SWITCHES AT LANDING GEAR CONTROL LEVER. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050907000242005090700024CE 2005 9 7 DXTA200500938 120050830A3241 BRAKE CESSNA560 560XL 2076702CE ANTI-SKID SYS MALFUNCTIONED E DXTAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07637QS 5605137 ON LANDING ROLL AND DURING TAXI THE BRAKES ARE VERY TOUCHY AND APPLY AT DIFFERENT RATES. NOT POSSIBLE TO TAXI WITHOUT CONSTANT PULLING LEFT AND RIGHT. PERFORMED TROUBLESHOOTING OF BRAKE SYSTEM, INCLUDING ANTI-SKID SYSTEM FUNCTIONAL CHECK IS GROUND MODE. FUNCTIONAL CHECK TESTED GOOD. BLED ANTI-SKID BRAKE SYSTEM PERFORMED HIGH SPEED GROUND TAXI, NO DEFECTS NOTED. ALL WORK PERFORMED IAW CESSNA 560XL MM, CH 32-42-00. BRAKES OPERATE PROPERLY AT THIS TIME. 2L72 4F RTA22CE 20050907000412005090700041EA 2005 9 7 VTZA200500153 120050831A53206013501252 ANGLE CNDAIRCL600 CL6002B19 1900309EA BS 625 CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27679BR 7662 RT OBLIQUE ANGLE AT FS 625 IS CRACKED. 2L72 4F RTA21EA 20050907000482005090700048EA 2005 9 7 VTZA200500159 120050831A5320601R35031 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA BS 621 CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27679BR 7662 LT FS 621 FLOOR SUPPORT IS CRACKED AT 1 IN ANGLE. 2L72 4F RTA21EA 20050907000512005090700051EA 2005 9 7 VTZA200500162 120050831A5320601R3117117 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA BS 484 CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27679BR 7662 INTERCOSTAL CRACKED AT .250 IN LENGTH ON LT OUTBOARD SIDE AT FS 484 BETWEEN BL 36.00. 2L72 4F RTA21EA 20050907000642005090700064SO 2005 9 7 C2XA05IA091 120050714A326023092900001 UPLOCK EMB 145 EMB145LR 3260212SO LT MLG INOPERATIVE A C2XAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW27169541605516055 145072 FLT 2657 - CREW REPORTED THAT THE LEFT MAIN LANDING GEAR INDICATION SHOWED RED DASHES UPON TAKEOFF. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR UPLOCK BOX. 2L72 4T RTT00011AT 20050907000692005090700069NM 2005 9 7 SB05107 120050901A335020131A BATTERY PACK BOEING737 7374B7 1384702NM EMERGENCY LIGHT DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19447US 24874 PIT - MAINTENANCE REPORTED THE SEAT MOUNTED EMERGENCY LIGHTS FROM ROWS 12 THROUGH 19 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND FUSE. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050907000802005090700080SO 2005 9 7 C2XA05CL078 120050906A524014531197001 BUSHING EMB 145 EMB145 3260210SO SERVICE DOOR WORN A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712967 145133 CLE - FLIGHT NR 2512 - CREW REPORTED GALLEY SERVICE DOOR HARD TO OPEN. MAINTENANCE INSPECTED AND REMOVED AND REPLACED BUSHINGS ON GALLEY SERVICE DOOR CRANK ASSEMBLY. OPERATIONAL CHECKS REPORTED GOOD. 2L72 4F RTT00011AT 20050907000862005090700086SO 2005 9 7 C2XA05CL067 120050820A2910 B-NUT EMB 145 EMB145LR 3260212SO NR 2 ENGINE LOOSE A C2XABA EMER. DESCENT UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW2713989 145271 CLE - FLIGHT NR 2275, THE CREW REPORTED A HYDRAULIC SYSTEM NR 2 FAIL IN FLIGHT. THE AIRCRAFT DIVERTED INTO BUF AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND TIGHTENED LOOSE "B" NUT ON THE NR 2 ENGINE HYDRAULIC PUMP. SERVICED THE NR 2 HYDRAULIC SYSTEM AND OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20050908000032005090800003NM 2005 9 8 05FDEA02744 120050903A5714 SPAR BOEING727 727200 138407ENM CENTER WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 CRACK FOUND DURING UT & HFEC INSP AT WING CENTER SECTION UPPER REAR SPAR WEB BS 870 LBL 6 - 7.5. REPAIRED UPPER REAR SPAR CHORD AT BS 870, LBL 6-7.5 PER EO 7-5710-7-3325. 2L73 4F RTA3WE 20050908000172005090800017WP 2005 9 8 UPS05845330 120050828A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 RT WING LE UPPER RIB IS CRACKED AT XFS 566.250. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2 -0 FIG 2. 2L74 4F RT4A25 20050908000202005090800020WP 2005 9 8 UPS05845333 120050828A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 RT WING LE UPPER RIB IS CRACKED AT XFS 753.750. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2 -0 FIG 2. 2L74 4F RT4A25 20050908000222005090800022WP 2005 9 8 UPS05845335 120050828A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 RT WING LE UPPER SKIN HAS INTERGRANULAR CORROSION AT XFS 766.250. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1 FIG 38. 2L74 4F RT4A25 20050908000292005090800029NM 2005 9 8 05FDEA02764 120050906A5753 ATTACH FITTING DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 LEFT WING - O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REPAIR CARRIED OUT AS PER EA 1-5750-87629. 2L73 4F RTA22WE 20050908000302005090800030NM 2005 9 8 05FDEA02765 120050906A5753 ATTACH FITTING DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 LEFT WING - O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87629. 2L73 4F RTA22WE 20050908000312005090800031NM 2005 9 8 05FDEA02766 120050906A5753 ATTACH FITTING DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 RIGHT WING - O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR PIN ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-87630. 2L73 4F RTA22WE 20050908000522005090800052NM 2005 9 8 05FDEA02777 120050906A5753 ATTACH FITTING DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 RT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REPAIR CARRIED OUT AS PER EA 1-5750-87632. 2L73 4F RTA22WE 20050908000592005090800059WP 2005 9 8 UPS05845339 120050828A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 LT WING LE UPPER SKIN IS CRACKED IB OF XFS 710.000. NO CRACK NOTED, FOUND TO BE CORROSION, CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1 FIG 38. 2L74 4F RT4A25 20050908000652005090800065WP 2005 9 8 UPS05845346 120050829A5712 RIB DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 LEFT WING LE LOWER RIB IS CRACKED AT XFS 341.500. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2 -0 FIG 2. 2L74 4F RT4A25 20050908000812005090800081NM 2005 9 8 05FDEA02732 120050901A5315 FLOORBEAM DOUG MD11 MD11 3023602NM BS 6-70 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 FWD CARGO COMPT, BETWEEN LBL 3 AND LBL 22, ALONG STA 6-70, FLOORBEAM CRACKED AND CORRODED. CORRECTIVE ACTION: SNRM N1070: FWD CARGO STA 6-70 FLOOR PANEL BEAM CRACK AND CORROSION SUPPORT REMOVED AND NEW SUPPORT INSTALLED AS PER DRAWING ADA 7667, SRM 51-33-01 VOL.II AND SRM 51-35-01 VOL.II. FABRICATE NEW SUPPORT P/N FX ADA 7667-31 PER DRAWING ADA 7667. MINOR REPAIR PER GMM 6-2-100. 2L73 4F RTA22WE 20050908000872005090800087SO 2005 9 8 C2XA05BT066 120050828A32347455503 LEVER EMB 145 EMB145EP 3260221SO MLG INTERMITTENT A C2XAO OTHER J WARNING INDICATION CLCLIMB 1 SW27169274932 4932 145006 CREW REPORTED, "NOSE GEAR DOOR[S] OPENED DURING CLIMB-OUT AT 15000 FT AND 290 KNOTS." MX R & R LGEU AND NLG ACT PROX SWITCHES 2. A/C TEST FLT FOR VERIFICATION TESTED UNSATISFACTORY ON 8/29/2005 AS CO3475, "MLG INDICATES UP NOSE GEAR DOOR VISUALLY VERIFIED OPEN". MX INSPECTED WIRING PER WIRING MANUAL FOUND HIGH RESISTANCE AT PIN 10 AT LEVER TO GS0255DC AND HIGH RESISTANCE AT PLUG P7123. WHEN LEVER CYCLED DURING L/G RETRACTION TEST WAS INTERMITTENT. R/R`D L/G RETRACTION LEVER IAW EMB145 MM NR 32-32-08 AND GROUNDING BLOCK GS025506 IAW EMB145 WIRING MANUAL NR 20-13-05. MLG RETRACTION TEST GOOD, TEST FLEW A/C SATISFACTORILY. A/C RETURNED TO SERVICE. 2L72 4F RTT00011AT 20050908000952005090800095EU 2005 9 8 08182005B 120050818A2697 CONNECTOR SAAB SF340 340B 7860101EU FIRE DETECTOR DAMAGED A NSVAK NONE L NO TEST ININSP/MAINT 1 EA27339CJ 339 LT TAILPIPE HOT LIGHT DOES NOT TEST. REPAIRED CONNECTOR TO LT TAILPIPE SENSOR. 2L72 4T RTA52EU 20050908000982005090800098EU 2005 9 8 08202005B 120050820A5414 COWLING SAAB SF340 340B 7860101EU RT ENGINE DEPARTED A NSVAO OTHER D INFLIGHT SEPARATION CRCRUISE 1 EA27237MJ 237 RT ENG AC SCOOP DEPARTED AIRCRAFT. A/C RELEASED FOR FERRY FLIGHT FROM PIT TO ALB. REMOVED AND REPLACED RT ENG COWLINGS, ROBBED COWLINGS OFF 307CE IN ALB. 2L72 4T RTA52EU 20050908000992005090800099EU 2005 9 8 08212005C 120050821A2612 FIRE DETECTOR SAAB SF340 340B 7860101EU RT TAILPIPE MALFUNCTIONED A NSVAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 EA27294CJ 294 RT TAILPIPE HOT LIGHT ILLUMINATED DURING TAXI OUT. INSPECTED AND CLEANED CONNECTION TO RT TAILPIPE HOT HARNESS. PERFORMED GROUND RUNS AT SEVERAL DIFFERENT POWER SETTINGS. NO DEFECTS NOTED. OPS CHECK GOOD. 2L72 4T RTA52EU 20050908001012005090800101EU 2005 9 8 08232005B 120050823A5753 ATTACH BOLT SAAB SF340 340B 7860101EU TE FLAPS WORN A NSVAO OTHER O OTHER TXTAXI/GRND HDL 1 EA27301CE 191 EXCESSIVE PLAY IN ATTACHMENT POINTS OF RT OUTBOARD FLAP. REMOVED AND REPLACED FWD ROLLER BOLT. ADJUSTED FLAP BUMPERS ON NR 4 FLAP. OPS CHECK GOOD. 2L72 4T RTA52EU 20050908001082005090800108EA 2005 9 8 SWIA200515497 120050821A2780766389L CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA SLAT/FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07743SK 10199 FLAPS HALFSPEED STATUS MESSAGE DURING FLIGHT. REPLACED NR 1 SFECU IAW CRJ 700 MM 27-51-05. OPERATIONAL CHECK OK. 2L72 4F RTA21EA 20050908001102005090800110SO 2005 9 8 SWIA200515499 120050824A3397 WIRE EMB 120 EMB120ER 3260203SO EXIT SIGN BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07576SW 120345 EXIT SIGN ABOVE SEAT 6A INOP. REPAIRED WIRE IAW WAM STANDARD PRACTICES 20-00-00. OPERATIONAL CHECK GOOD IAW AMM 23-50-00. 2L72 4T RTA31SO 20050908001132005090800113EA 2005 9 8 SWIA200515502 120050828A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07913SW 7597 NR 3 OVERHEAD EMERGENCY LIGHT INOP. RELAMPED NR 3 OVERHEAD EMERGENCY LIGHT AS REQUIRED. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050908001182005090800118NM 2005 9 8 UPS05245312 120050829A5350 FRAME BOEING727 72722C 138400FNM BS 1010 S26R CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01930UP 19096 BODY FAIRING 3608 AFT FRAME AT ATTACHING ANGLE IS CORRODED AT BS 1010 ADJACENT TO STR 26R. FRAME REPLACED IAW SRM 51-20-1 FIG 7. 2L73 4F A3WE 20050908001442005090800144NM 2005 9 8 2005UALA00895 120050826A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE STA 1380 DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29588UA 26717 FRAME DENTED AT STA 1540 BETWEEN STR 25R AND STR 26R. TRIMMED OUT DAMAGES, ACP HEFC INSP, NO CRACK. FABRICATE, ALODINE, PRIME AND INSTALL REPAIR PER TIMCO REO-G10820, REV B. 2L72 4F4 FRTA2NM E17NE 20050908001502005090800150NM 2005 9 8 2005UALA00901 120050826A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE STA 1420 DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29588UA 26717 FRAME DENTED AT STA 1420 BETWEEN S26L AND S27L. TRIMMED OUT DAMAGES, ACP HFEC INSP, NO CRACK FOUND. FABRICATE, ALODINE, PRIME, AND INSTALL REPAIR PER TIMCO GEO-10827. 2L72 4F4 FRTA2NM E17NE 20050908001552005090800155NM 2005 9 8 2005UALA00906 120050827A2910 HYDRAULIC SYSTEM BOEING757 757222 1384956NM PWA 2037 PW2037 NE MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29568UA 26674 RETURNED TO ANC UNDER AN AMBER ALERT DUE TO A HYDRAULIC PROBLEM. LEFT HAND ENGINE HYDRAULIC PUMP FAILED. REPLACED LEFT HAND PUMP PER MM29-11-05. ALSO REPLACED PRESSURE FILTER AND CASE DRAIN FILTERS. CHECKED AND REPLACED ELECTRIC HYDRAULIC PUMP CASE DRAIN FILTER PRECAUTIONARY, NO METAL FOUND. RETURNED AIRCRAFT TO SERVICE. 2L72 4F4 FRTA2NM E17NE 20050912000082005091200008SO 2005 9 12 1322090505 120050905A32971159SCAV3856 WIRE HARNESS GULSTMG1159 GIV 3980115SO BRAKE OVERTEMP DEFECTIVE E N93AD RETURN TO BLOCK MJ OVER TEMP WARNING INDICATION TXTAXI/GRND HDL 1 SO13422QS 1322 NR 3 BRAKE OVERTEMP INDICATION DURING TAXI OUT FOR TAKEOFF. 2L72 4F RTA12EA 20050912000102005091200010EA 2005 9 12 SWIA200515503 120050903A2750860D10018 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07953SW 7813 FLAP FAIL CAUTION MSG. REPLACED FECU IAW CRJ MM 27-51-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050912000122005091200012EA 2005 9 12 SWIA200515505 120050902A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07589SW 7072 2ND AFT EMERGENCY LIGHT INOP. REPLACED 2ND AFT OVERHEAD EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050912000142005091200014EA 2005 9 12 SWIA200515507 120050901A3397 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSLOOSE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07908SW 7540 LIGHTED EMERGENCY EXIT SIGN ON LEFT SIDE OF GALLEY SERVICE DOOR IS INOP. RESECURED CONNECTOR. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050912000252005091200025NM 2005 9 12 P5CA0501394 120050906A7830 BALL JOINT HONEYWELL BOEING747 74746NF 13848BTNM T/R GEARBOX CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 EA15450PA 8139 30808 LOWER RT THRUST REVERSER ANGLE GEARBOX FOUND BALL SCREW CORRODES. REPLACED ANGLE GEAR BOX PER MM 78-31-22. 2L74 4F RTA20WE 20050912000422005091200042 2005 9 12 AT0500031 420050905A31604082170912 DISPLAY BOEING717 717200 1383700NM NR 4 FAILED A ZZDAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO15977AT 55036 NR 4 DU FAILED IN FLIGHT WITH SMOKE IN COCKPIT ONLY. REMOVED AND REPLACED NR 4 DU. DISPLAY TESTS PASSED. ALSO CLEANED REMAINING DU COOLING INLETS. INSPECTED INST COOLING FAN & FILTER, NO DEFECTS FOUND. OK FOR SERVICE. REF 31-43, 31-61. P/N OFF/ON 4082170-912, S/N OFF 02770892, S/N ON 31491628. 2L72 4F TRA6WE 20050912000542005091200054NM 2005 9 12 SWAA052729 120050906A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM BS 807 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 807, RBL 7. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050912000582005091200058CE 2005 9 12 ACE082605 120050826A2822 DIAPHRAGM ROMEC RG37060A BEECH 1900 1900C 1154161CE BOOST PUMP RUPTURED E YADAO OTHER KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 AL03113AX 3398 B107019 UC41 PILOT REPORTED LOW FUEL PRESSURE WARNING LIGHT CAME ON IN FLIGHT. MAINTENANCE REPLACED LEAKING LOW PSI BOOST PUMP. VERIFIED DIAPHRAGM HAD FAILED. FUEL WAS OBSERVED IN AGB AREA. 2L72 4T RTA24CE 20050912000732005091200073NM 2005 9 12 SWAA052708 120050906A3350MS155721 BULB BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29495WN 33869 DURING SCHEDULED RON CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050912000742005091200074NM 2005 9 12 SWAA052709 120050905A53306545776 SKIN BOEING737 7375H4 138449DNM BS 947 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 24L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050912000752005091200075NM 2005 9 12 SWAA052710 120050906A335010107451 SIGN BOEING737 7375H4 138449DNM CABIN SEPARATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED A1 CHECK, L1 DOOR EMERGENCY EXIT SIGN FELL OFF. REINSTALLED SIGN PER MM. 2L72 4F RTA16WE 20050912000772005091200077NM 2005 9 12 SWAA052712 120050906A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 294 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 294, STR 13L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050912000782005091200078NM 2005 9 12 SWAA052713 120050906A53156546809 FLOORBEAM BOEING737 7373H4 1384600NM BS 947 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 DURING SCHEDULED D-CHECK, FOUND CABIN FLOORBEAM UPPER CHORD CORRODED AT BS 947, BETWEEN BL 0 TO LBL 45, WL 208. REPAIRED FLOORBEAM PER BFG ER. 2L72 4F RTA16WE 20050912000792005091200079NM 2005 9 12 SWAA052714 120050906A53156546811 FLOORBEAM BOEING737 7373H4 1384600NM BS 986.5 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 DURING SCHEDULED D-CHECK, FOUND CABIN FLOORBEAM UPPER CHORD CORRODED AT BS 986.5, BETWEEN RBL 35 TO RBL 45, WL 208. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20050912000802005091200080NM 2005 9 12 SWAA052715 120050906A53106552878 DOOR FRAME BOEING737 7373H4 1384600NM R2 DOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 DURING SCHEDULED D-CHECK, FOUND R2 DOOR CUTOUT, FWD LOWER FRAME CORRODED AT BS 956, WL 208. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050912000822005091200082NM 2005 9 12 SWAA052717 120050906A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM BS 767 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 767, BL 0 & RBL 12. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050912000842005091200084CE 2005 9 12 GLBA20050516 120050902A561010138402517 WINDSHIELD BEECH 1900 1900D 1154162CE COCKPIT FAILED A GLBAO OTHER O OTHER CLCLIMB 1 NM03247GL2070 UE247 LEFT WINDSHEILD OUTER PLY SHATTERED. REPLACED WINDSHEILD. 2L72 4T RTA24CE 20050912000852005091200085CE 2005 9 12 CIEA200500016 120050901A574323411231 ATTACH FITTING LEAR 35 35A 5170602CE RT MLG CRACKED E CIEAK NONE O OTHER ININSP/MAINT 1 NM03553V 115295764 35A141 DURING COMPLIANCE OF A 6000 MAJOR LANDING GEAR INSPECTION THE RIGHT MAIN GEAR ACTUATOR ATTACH PILLAR WAS FOUND TO HAVE A .25 INCH CRACK IN IT. THE CRACK WAS APPROXIMATELY 3.7 INCHES FROM THE MAIN GEAR ACTUATOR END OF THE PILLAR. THE CRACK WAS IN A CIRCUMFERENTIAL DIRECTION. THE CRACK WAS FOUND DURING THE NDT PART OF THE INSPECTION USING MAGNETIC PARTICLE INSPECTION. THE CRACK ONCE FOUND WAS VISIBLE USING A 10 X MAGNIFYING GLASS. THIS UNIT WAS INSPECTED 5764 LANDING PRIOR TO THIS AS PART OF A 6000 LANDING INSPECTION. THIS UNIT IS A LIFE LIMITED COMPONENT AT 18,000 LANDINGS. 2L72 4F A10CE 20050912000902005091200090EA 2005 9 12 VNAA0508023 120050821A2120 VENT CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE CARGO BAY OBSTRUCTED A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL05723PS 10181 DURING CLIMBOUT WITH LIVE CARGO THE CARGO OVERHEAT CAUTION MESSAGE ILLUMINATED. THE CREW FOLLOWED THE QRH AND RETURNED TO CLT. MAINTENANCE INSPECTED THE AFT CARGO COMPARTMENT AND FOUND BAGGAGE BLOCKING THE CONDITIONED AIR VENT. THE BAGGAGE WAS REPOSITIONED. THE CARGO AIR CONDITIONING SYSTEM OPERATIONALLY CHECKED GOOD IAW CRJ700 AMM 21-55-00-710-801-A02. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050912000912005091200091CE 2005 9 12 DJFA2005137 120050905A2750 FLAP SYSTEM BEECH MU300 400A 1155402CE OUT OF ADJUST E DJFAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA23402CW RK2 KPVD - KCLT TRIP ID 893929 DURING CLIMBOUT WHILE PASSING FL 260 AT A SPEED OF 250 KTS THE FLAP ASYMMETRY LIGHT ILLUMINATED WHILE THE FLAPS WERE SET AT ZERO DEGREES, AND INDICATING ZERO DEGREES. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT WAS DIVERTED TO KBDL. A ZERO FLAPS LANDING WAS MADE IN KBDL WITHOUT FURTHER INCIDENT. MAINTENANCE RERIGGED THE RIGHT FLAP FOLLOW UP SWITCH. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4F RTA16SW 20050912000972005091200097CE 2005 9 12 DXTA200500954 120050905A2612 FIRE DETECTOR RAYTHNDH125 HAWKER800XP 7150012CE CARGO BAY MALFUNCTIONED E DXTAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL07840QS 258340 BAGGAGE FIRE LIGHT ILLUMINATED IN FLIGHT. GAINED ACCESS TO FWD, LAV, AND AFT SMOKE DETECTORS. INSPECTED DETECTORS FOR SECURITY AND INTEGRITY, NO DEFECTS NOTED. POWERED UP ALL ELECTRICAL BUSSES AND TESTED SMOKE DETECTORS, ALL TEST SATISFACTORY. INSPECTED CABIN OF AIRCRAFT TO INCLUDE LAV AND FWD AFT BAG COMPARTMENTS FOR EVIDENCE OF FIRE, NO DEFECTS NOTED. SYSTEM TEST NORMAL. ALL DONE IAW HAWKER 800XP M/M 26-11-00. 2L72 4F RTA3EU 20050912000982005091200098CE 2005 9 12 DXTA200500955 120050905A272099146003 ACTUATOR CESSNA750 750 2076810CE RUDDER FAILED E DXTAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 GL07983QS2169 7500083 AT FL 320 AND .88 MACH THE UPPER RUDDER YD STARTED BOUNCING OFF THE LEFT SIDE OF THE RUDDER LIMITER WITH THE UPPER YD IN THE B-CHANNEL, IT WOULD NOT HAPPEN ON THE A-CHANNEL. AT SPEED & ALTITUDE THE RUDDER HAD TO BE TRIMMED TO THE LEFT EXCESSIVELY. REMOVED UPPER RUDDER ACTUATOR DUE TO INTERNAL LEAKAGE. REPLACEMENT ACTUATOR INSTALLED IAW CE-750 MM CH 27-24-01. OPS CHECK GOOD. 2L72 4J RTT00007WI 20050912000992005091200099CE 2005 9 12 DXTA200500956 120050906A5100 UNKNOWN CESSNA750 750 2076810CE FUSELAGE UNKNOWN E DXTAO OTHER E VIBRATION/BUFFET CRCRUISE 1 GL07900QS 7500123 AT FL400 IN CRUISE A LOUD THUMP WAS HEARD AND FELT IN THE NOSE AREA. ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20050912001002005091200100NM 2005 9 12 DXTA200500946 120050830A3260803682 POSITION SWITCH AMD FALC50FALCON2000 2730170NM MLG MALFUNCTIONED E DXTAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL07284QS 185 AFTER TAKEOFF GEAR HANDLE WAS SELECTED UP, GEAR STARTED TO RETRACT WITH THREE RED LIGHTS, GEAR THEN STOPPED INTRANSIT WITH MAIN GEAR RED AND GREENS SEEN AND GEAR HANDLE FLASHING. AFTER SELECTING GEAR DOWN, GEAR WENT DOWN NORMALLY. TROUBLESHOT FOR LANDING GEAR FAILURE TO RETRACT NORMALLY INTERFACED WITH AIRFRAME SYSTEM COMPUTERS AND FOUND NO FAULTS, OPERATIONALLY TESTED LANDING GEAR SEVERAL TIMES WITH NO FAULTS. AT THE OPERATOR REQUEST THE MLG DOOR ACTUATOR PROXIMITY SWITCHES, LEFT P/N 803602, S/N 1391, RIGHT P/N 803682, S/N 1243 WERE REPLACED WITH NEW SWITCHES OF SAME P/N, LEFT S/N 1224, RIGHT 1220 IN ACCORDANCE WITH FALCON 2000 MM 32-811. PERFORMED MLG OPERATIONAL CHECK AND FOUND T/O OPS CHECK NORMAL. 2K73 4F RTA50NM 20050912001012005091200101CE 2005 9 12 DXTA200500950 120050901A3240 BRAKE ASSY CESSNA750 750 2076810CE MLG MALFUNCTIONED E DXTAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07931QS 7500064 BRAKE PEDALS ON LEFT AND RIGHT GO ALL THE WAY TO THE STOPS WHEN PRESSURE IS APPLIED, BRAKES FELT SPONGEY. PERFORMED VISUAL INSPECTION OF BRAKES, NO DEFECTS NOTED. PERFORMED BLEEDING PROCEDURES, PERFORMED POWER BRAKE PRESSURE CHECK, PRESSURE CHECKS NORMAL. PERFORMED TAXI CHECK ON BRAKE SYSTEM, TAXI CHECK NORMAL. WORK PERFORMED IAW CE-750 MM CHAP 32-42-00. 2L72 4J RTT00007WI 20050912001032005091200103CE 2005 9 12 DXTA200500951 120050902A215022066101 ACM CESSNA560 560XL 2076702CE ACM BAY SEIZED E DXTAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL07630QS1005 5605130 APU RUNNING ON THE GROUND WITH BLEED AIR ON. SMOKE IN CABIN AND COCKPIT SHUTDOWN BLEED AIR AND APU REMOVED BATTERY POWER FROM AIRCRAFT. ACM WAS FOUND SEIZED UP, INSTALLED REPAIRED ACM PACK IAW 560XL M/M 21-51-00. 2L72 4F RTA22CE 20050912001062005091200106NE 2005 9 12 ARWA20050901 220050907A7532563883 BLEED VALVE DOUG DC8 DC862F 3021972WP PWA JT3D JT3D7 52039NE NR 1 ENGINE FAILED A ARWAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SO19791AL 46150 671003 ABORTED TAKEOFF AT 60 KNOTS UPON HEARING A LOUD BANG; NR 1 ENGINE COMPRESSOR STALLED. REMOVED AND REPLACED BLEED VALVE AND CONTROL COMPRESSOR IN ACCORDANCE WITH M/M 75-30-3; OPERATIONAL CHECK NORMAL IN ACCORDANCE WITH 75-30-0. PERFORMED BORESCOPE INSPECTION IN ACCORDANCE WITH TASK CARD DC8-AR-002 ARROW MAINTENANCE CHECK MANUAL, VOLUME III; FOUND NORMAL. CHECKED ON RUN-UP ALL ENGINES; FOUND NORMAL IN ACCORDANCE WITH M/M 71-00. 2L74 4F4 F 4A25 1E8 20050912001072005091200107EA 2005 9 12 COMA0560480 120050901A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01809CA6099 79 7366 FLIGHT 5432 - SPOILER CONFIG MESSAGE DURING T/O. REPLACED THE LT SPOILERON PCU. 2L72 4F RTA21EA 20050912001102005091200110NM 2005 9 12 SWAA052738 120050907A53116546554 FRAME BOEING737 7373H4 1384600NM BS 846 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 846, BETWEEN STR 24R & STR 25R. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20050912001122005091200112NM 2005 9 12 05FDEA02737 120050902A5330 SKIN BOEING727 727200 138407ENM BS 640 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 THREE HOLES, BS 640 STR 2L, BUCKTAILS BEHIND EXISTING STRUCTURE. *S/D* REPAIRED HOLES, BS 640, STR 2L, PER FED-EX EA 7-5330-92260A. 2L73 4F RTA3WE 20050912001132005091200113NM 2005 9 12 05077 120050908A2611 BULB BOEING747 747209B 138489BNM EMERGENCY LIGHT BURNED OUT A KCSAK NONE N FALSE WARNING ININSP/MAINT 1 GL23704CK 22299 MAIN DECK CARGO SMOKE LIGHTS SEGMENTS NR 2 - 5 ILLUMINATED AFTER ETP CARGO EXAMINED. NO FIRE NOTED. AFTER 15 MIN LIGHTS EXTINGUISHED. RELAMPED NR 2 & 5 SMOKE DETECTORS AND OPS CHECKED GOOD IAW B747 MM 26-14-00. 2L74 4F RTA20WE 20050912001152005091200115NM 2005 9 12 QXEA200501213 120050901A3080 PRESSURE SWITCH DHAV DHC8 DHC8202 2809007NM DEICE SYSTEM MALFUNCTIONED A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09362PH 518 SEA FLIGHT 2182 LEFT AND RIGHT DEICE PRESSURE 10 PSI AT FLIGHT IDLE ON THE GROUND. MAINTENANCE REPLACED HIGH PRESSURE SWITCHES AND 2121K6 RELAY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050912001162005091200116 2005 9 12 QXEA200501214 420050906A34207003360941 AHRS DHAV DHC8 DHC8202 2809007NM NR 2 MALFUNCTIONED A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09361PH* 7486 516 SEA FLIGHT 2078 ALTITUDE HEADING FAIL FIRST OFFICERS AHRS. MAINTENANCE REPLACED NR 2 AHRS IAW MTC 93240019. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050912001172005091200117NE 2005 9 12 QXEA200501215 220050902A73142860057101 PUMP DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE FUEL SYS MALFUNCTIONED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09369PH15786 513 SEA FLIGHT 2078 ON CLIMBOUT NR 1 ENGINE FUEL PRESSURE CAUTION LIGHT ACCOMPANIED BY FALLING TORQUE AND FLUCTUATING AND FALLING FUEL FLOW. ACCOMPLISHED NR 1 ENGINE FUEL PRESSURE CAUTION CHECKLIST. UPON SELECTING NR 1 AUX PUMP ON, NOTED A MOMENTARY JUMP IN TORQUE TO APPROXIMATELY 130 PERCENT FOR 1 SECOND. FUEL FLOW WHICH HAD FALLEN TO 750 RETURNED TO NORMAL. ALL OTHER ENGINE INDICATIONS NORMAL WITH AUX PUMP ON. MAINTENANCE REPLACED HP FUEL PUMP. OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20050912001202005091200120NE 2005 9 12 QXEA200501210 220050902A73233037604 PUMP DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE OVERSPEED MALFUNCTIONED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09353PH5446 496 SEA - NR 2 TORQUE ANALOG AND DIGITAL FLUCTUATES FROM 2-30 PERCENT DURING FEATHER OPERATION. MAINTENANCE REPLACED HYDRAULIC OVERSPEED PUMP. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20050912001212005091200121NM 2005 9 12 QXEA200501211 120050904A2430 GENERATOR DHAV DHC8 DHC8202 2809007NM NR 1 MALFUNCTIONED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09350PH 488 RDM FLIGHT 2220, NR 1 DC GENERATOR CAUTION LIGHT ON TAXI. MAINTENANCE DEFERRED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050912001242005091200124CE 2005 9 12 DXTA200500947 120050830A3240387072 SERVO VALVE CESSNA500 560CESSNA 2076750CE BRAKES FAILED E DXTAD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07375QS9111 5600375 UPON LANDING BRAKES RESPONDED NORMALLY, WITH SPEED BELOW 40 KTS, BRAKES WERE RELEASED. WHEN BRAKES WERE REAPPLIED (TRAVELING STRAIGHT) TO SLOW TO TURN-OFF SPEED, PRESSURE WAS PRESENT IN THE PEDALS BUT BRAKES DID NOT RESPOND. REMOVED ANTI SKID SERVO VALVE PER AMCC REQUEST. INSTALLED A NEW VALVE. OPERATIONAL AND LEAK CHECKS GOOD. ANTI-SKID FUNCTIONAL CHECK GOOD. ALL WORK IAW CH'S 32-42-05, 32-42-00 AND 34-23-02 OF THE CE-560 MM. 2L72 4F RTA22CE 20050912001252005091200125EA 2005 9 12 COMA0560482 120050901A3350364911 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A COMAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01507CA 7796 FLIGHT 4999 - EMERGENCY FLOOR PATH LIGHT, FWD SECTION IS INOPERABLE. REPLACED TRACK LIGHT STRIP. 2L72 4F RTA21EA 20050912001312005091200131NM 2005 9 12 ASMF200509001 120050901A2150 ACM BOEING757 7572Q8 1384972NM FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23804AM 26271 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING PUSHBACK, THE AIR CONDITION PACKAGE FAILED WITH EICAS MESSAGES OF RIGHT ENGINE PURGE VALVE DID NOT OPERATE. REPORT WAS DEFERRED IAW MEL 36-11-1. 2L72 4F RTA2NM 20050912001322005091200132NM 2005 9 12 ASMF200509002 120050903A5330 SKIN DOUG MD88 MD88 3023688NM BS 1277 DENTED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23169PL 53175 DURING TRANSIT CHECK AT ONT, IT WAS DETECTED A DENT IN FUSELAGE SKIN OF 2 X 1.875 WITH 0.044 DEPTH, LOCATED AT STA Y=1277 BETWEEN RIGHT LONGERON 22 & 23. DENT WAS EVALUATED AND IT WAS FOUND WITHIN LIMITS IAW SRM 53-04, FIGURE 38, TABLE C, CONDITION 1B. AT MEX, THE NON ROUTINE CARD NUMBER A0081245 WAS ISSUED TO VERIFY THE DENT IN FUSELAGE SKIN LOCATED IN STA Y=1277 BETWEEN RIGHT LONGERON 22 & 23 AND IT WAS DETEMINED TO PERFORM REPETITIVE DYE PENETRANT OR EDDY CURRENT INSPECTION ON A YEARLY BASIS OR EVERY C-CHECK IAW SRM 53-04, FIGURE 38, TABLE C. 2L72 4F RTA6WE 20050912001332005091200133EA 2005 9 12 REXA200500108 120050902A27501104SD100401 DRIVE SHAFT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS STUCK A REXAO OTHER J WARNING INDICATION APAPPROACH 1 SO258495B 7495 FLAPS FAIL ON APPROACH STUCK AT 42 DEGREES. 2L72 4F RTA21EA 20050912001352005091200135NM 2005 9 12 CALA0500303 120050902A2800233N320619 CONTROL PANEL BOEING757 757224 1384958NM FUEL SYSTEM INOPERATIVE A CALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW271911739364 27559 A SMOKY ODOR NOTICED IN COCKPIT WHEN CREW TURNED ON ENGINE ANTI-ICE & IGNITION DUE TO WEATHER WHILE EN ROUTE. CENTER AUTOPILOT TRIPPED OFF & F/O'S AIRSPEED INDICATOR FAILED. ODOR BEGAN TO DISSIPATE. WHEN WEATHER CONDITIONS ABATED IGNITION & ENGINE ANTI-ICE WERE TURNED OFF. OPS OF AUTOPILOT & F/O'S AIRSPEED INDICATOR RETURNED TO NORMAL. FLT CONTINUED & LANDED WITHOUT PROBLEMS. MX INSPECTED ALL C/B OVERHEAD PANEL WIRING, BOTH ADC'S AND BUSS TIE BREAKERS WITH NO TROUBLE FOUND. MX FOUND FUEL PUMP FEED OVERHEAD CONTROL PANEL CENTER PUMP SWITCH GIVING OFF AN ODOR. PANEL REPLACED AS A PRECAUTION. 2L72 4F RTA2NM 20050912001392005091200139 2005 9 12 REXA200500111 420050904A2562 G SWITCH ARTEX CNDAIRCL600 CL6002B19 1900309EA ELT FAILED A REXAK NONE L NO TEST ININSP/MAINT 1 SO258683B7000 4778 01438 7683 ELT FAILS G-SWITCH TEST. REMOVED IN ACCORDANCE WITH PA 25-048D AND FAR 91.207 FOR REPAIR. UNIT MUST BE REPAIRED AND REINSTALLED WITHIN 90 DAYS. REMOVED ELT FOR MAINTENANCE IN ACCORDANCE WITH FAR 91.207. 2L72 4F RTA21EA 20050912001412005091200141NM 2005 9 12 UPS05245372 120050823A5320 WEB BOEING727 72722C 138400FNM BS 290 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01930UP 19096 INSPECTION TYPE: C, NLG W/W CEILING AT BS 290 LBL 0 HAS SUSPECT CRACKS AT FASTENER HEADS. WEB REPLACED IAW SRM 51-20-1 AND DWG 65-18416. 2L73 4F A3WE 20050912001422005091200142NM 2005 9 12 UPS05445374 120050908A3350 LIGHT BOEING747 747123 1384873NM COCKPIT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 EMERGENCY EXIT LIGHTS WILL NOT ARM WITH SAFETY SWITCH CLOSED. REPOSITIONED SWITCH ENGAGE HOOP. CHECKS OK. 2L74 4F A20WE 20050912001442005091200144WP 2005 9 12 UPS05845366 120050811A5340 FITTING DOUG DC8 DC871F 302199DWP BS 759 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 INSPECTION TYPE:C1, FITTING CRACKED AT FS 759 L18R AFT SIDE. REMOVED AND REPLACED FITTING AT FS 759 L18R IAW SRM 51-1-20D,51-1-24, AND 51-1-8 2L74 4F RT4A25 20050912001452005091200145NM 2005 9 12 P5CA0501387 120050826A275065B4750112 MODULE BOEING747 747283B 1384867NM TE FLAPS FAILED A P5CAO OTHER GJ MULTIPLE FAILURE WARNING INDICATION CRCRUISE 1 EA15921FT 21575 DURING CRUISE, LEADING EDGE FLAP GROUP 1, 2, 3, 4 LEFT AND 1 RIGHT DISPLAY AMBER, GROUPS 1 & 2 LEFT ALSO DISPLAY GREEN. REPLACED MODULE OPS CHECK OK PER MM 27-88-00. 2L74 4F A20WE 20050912001462005091200146SO 2005 9 12 C2XA05SH108 120050901A491014526850401 FIREWALL EMB 145 EMB145LR 3260212SO APU DAMAGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712540 145537 SHV - DURING C-CHECK, THE APU COWLING MATING SURFACE TO FUSELAGE (FIREWALL) HAS SEVERAL DAMAGED RIVETS AT 6 O'CLOCK POSITION. MAINTENANCE REPAIRED THE APU MATING SURFACE (FIREWALL) AT 6 O'CLOCK POSITION IAW EC5330-01496. 2L72 4T RTT00011AT 20050912001492005091200149SO 2005 9 12 C2XA05SH111 120050905A575414565300402 SKIN EMB 145 EMB145 3260210SO LEADING EDGE DENTED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714959 145091 SHV - DURING C-CHECK, RT LEADING EDGE NR 3 HAS DENT BETWEEN 2ND AND 3RD VORTILLON. MAINTENANCE REPAIRED RT LEADING EDGE NR 3 BETWEEN 2ND AND 3RD VOTILLON IAW EMB 145 SRM 57-40-00. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2L72 4F RTT00011AT 20050912001512005091200151EU 2005 9 12 2005UALA00910 120050829A5230 MOUNT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CARGO DOOR HANDLCRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29405UA 452 FWD CARGO DOOR HANDLE MOUNT PLATE WHERE IT ATTACHES TO THE DOOR FRAME IS CRACKED AT THE FRAME. 2L72 4F4 FRTA28NM E40NE 20050912001532005091200153EU 2005 9 12 2005UALA00912 120050829A5230 SKIN AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CARGO DOOR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29405UA 452 FWD CARGO DOOR INNER SKIN IS CRACKED AT LWR AFT CORNER. 2L72 4F4 FRTA28NM E40NE 20050912001542005091200154NM 2005 9 12 2005UALA00913 120050829A5310 DOOR FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE R1 DOOR CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29327UA 24147 R1 DOOR FRAME STA 296 RBL 54 CORRODED, S17R, WL 208. 2L72 4F4 FRTA16WE E2GL 20050912001562005091200156NM 2005 9 12 2005UALA00915 120050826A335060253 LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29516UA 24860 EEL STRIP IN FRONT OF MID CABIN LAV IS INOPERATIVE. REPLACED EEL LIGHT ASSEMBLY. 2L72 4F4 FRTA2NM E17NE 20050912001572005091200157NM 2005 9 12 2005UALA00916 120050827A339759193 CABLE BOEING757 757222 1384956NM PWA 2037 PW2037 NE STA 1076 INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29544UA 25322 EMERGENCY PROXIMITY LIGHTS INOPERATIVE. REPLACED CABLE AT STA 1076 AND JUMPER WIRE AT STA 880 TO 902. 2L72 4F4 FRTA2NM E17NE 20050912001582005091200158NM 2005 9 12 2005UALA00917 120050829A2120 ODOR BOEING777 777222 1385219NM PWA PW4077PW4077 NE CABIN DETECTED A UALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP29774UA 26936 ELECTRICAL ODOR IN CABIN. RAN BOTH ENGINES AND APU WITH PACKS AND ALL RECIRC ON; POWERED GALLEYS, PAX ENTERTAINMENT SYSTEM; CHECKED E/E COMPARTMENT AND CABIN CEILING AREA; NO ODORS DETECTED. ROOT CAUSE UNKNOWN. 2L72 4F4 FRTT0001SE E46NE 20050912001602005091200160NM 2005 9 12 2005UALA00919 120050830A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29505UA 24626 OUTSIDE DOOR 1R TO LEFT OF NOSE NUMBER SMALL CREASE AND DENT IN FUSELAGE. 2L72 4F4 FRTA2NM E17NE 20050912001652005091200165NE 2005 9 12 VNAA0508014 220050821A7200 ENGINE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE LEFT VIBRATION A VNAAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 GL05705PS 10144 GEE965531 DURING TAKEOFF LEFT ENGINE FAN VIBRATION LEVEL INDICATED IN THE CAUTION RANGE. THE CREW FOLLOWED THE QRH AND RETURNED TO DAY. MAINTENANCE LUBRICATED THE LT ENGINE FAN BLADE TANGS IAW CRJ700 AMM 72-21-02-640-801-A01. ENGINE OPERATIONAL AND VIBE CHECKS WERE GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050912001662005091200166EA 2005 9 12 VNAA0508015 120050823A2750 DETECTOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A VNAAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 GL05209PS 7874 CLIMBING OUT OF DCA THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED. THE CREW FOLLOWED THE QRH AND LANDED WITHOUT INCIDENT AT IAD. MAINTENANCE RESET THE SKEW DETECTION UNIT, PERFORMED A BITE CHECK, AND OPERATIONALLY CHECKED THE FLAP CONTROL LEVER IAW CRJ200 AMM 27-51-01-740-801 AND 27-51-15-710-802. ALL OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050912001672005091200167EA 2005 9 12 VNAA0508016 120050824A5350 RADOME CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSLEAGE BIRD STRIKE A VNAAO OTHER O OTHER APAPPROACH 1 GL05226JS 7895 AFTER LANDING INSPECTION REVEALED DAMAGE TO THE RADOME FROM A BIRD STRIKE. AFTER INSPECTION THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE REPLACED THE RADOME WITH A SERVICEABLE UNIT IAW CRJ200 AMM 53-81-01-000(400)-801. NO FURTHER DAMAGE WAS NOTED. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050912001682005091200168NE 2005 9 12 0501385506 220050903A73141B6149 PUMP BOEING757 757251 1384970NM PWA 2037 PW2037 NE NR 1 ENGINE FAILED A NWAAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 GL01506US11344 23195 728798 DURING CRUISE FLIGHT ENGINE NR 1 FLAMED OUT. FLIGHT CREW DIVERTED TO OMA PERFORMING AN UNEVENTFUL LANDING. MAINTENANCE REMOVED AND REPLACED ENGINE NR 1 FUEL CONTROL AND FUEL PUMP. 2L72 4F4 FRTA2NM E17NE 20050912001692005091200169CE 2005 9 12 72752 120050905A3233R1143800419 ACTUATOR BEECH 1900 1900D 1154162CE MLG FAILED A AMWAO OTHER J WARNING INDICATION APAPPROACH 1 CE07162ZV634 634 UE162 WHEN GEAR WAS EXTENDED FOR LANDING IN OGDENSBURG, PA RIGHT MAIN GEAR INDICATION DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE MAIN LANDING GEAR ACTUATOR. OPS CHECKED NORMAL. 2L72 4T RTA24CE 20050912001702005091200170NM 2005 9 12 SB05109 120050904A27512061141 INDICATOR BOEING737 737301 1384611NM P2 CENTER PANEL FAULTY A USAAL ABORTED APPROACH F FLT CONT AFFECTED APAPPROACH 1 EA19353US4787047870 23556 ORD - FLT551 - ON APPROACH TO ORD, CREW EXTENDED FLAPS FROM 5 TO 10 UNITS AND A SPLIT FLAP INDICATION OF L-5 AND R-10 WAS DISPLAYED. FLAPS LOCKED OUT. CREW ACCOMPLISHED A GO-AROUND AND ON SUBSEQUENT APPROACH, FLAPS OPERATED NORMAL. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED FLAP TRANSMISSIONS AND TRANSMITTERS. NO DEFECTS NOTED. FLAPS OPERATED NORMAL ON GROUND. HOWEVER, ON NEXT FLIGHT TO PHL (FLT508), A SPLIT FLAP INDICATION OCCURRED AGAIN. MAINTENANCE REMOVED AND REPLACED THE FLAP POSITION INDICATOR. OPERATION CHECK OF FLAPS GOOD. 2L72 4F RTA16WE 20050912001712005091200171NM 2005 9 12 2005UALA00921 120050830A3350321430 BATTERY PACK AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE EMERGENCY LIGHT DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29812UA 850 LT FWD EMERG LIGHT BATTERY PACK LOW. FAILED 3SVC LIGHT TEST. REPLACED FWD EMERG LIGHT BATTERY. 2L72 4F4 FRTA28NM E40NE 20050912001742005091200174NM 2005 9 12 2005UALA00922 120050831A3350321430 BATTERY AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE EMERGENCY LIGHT FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29823UA 952 FWD EMERGENCY BATTERY FAILED 3SVC CK. REPLACED FWD EMERGENCY LIGHT BATTERY. 2L72 4F4 FRTA28NM E40NE 20050912001752005091200175 2005 9 12 2005UALA00923 420050806A2565101651306 SLIDE BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE CABIN DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29664UA 29236 UPON INFLATION OF THE UNIT, UPPER TUBE IS NOTED WITH TEAR ON THE FABRIC ABOUT .25 INCH LOCATED CLOSE TO PRESSURE RELIEF VALVE. HOLE GOES THROUGH ON TOP AND BOTTOM PART OF THE UPPER TUBE. THE PRESSURE RELIEF VALVE BAND CLAMP SCREW IS NOTED WITH SHARP EDGES THAT CUT THROUGH THE CLAMP COVER AND UPPER TUBE FABRIC. INSPECT PRV SCREW FOR SHARP EDGES AND REPLACE AS NECESSARY. 2L72 4F4 FRTA1NM E24NE 20050912001762005091200176NM 2005 9 12 2005UALA00924 120050831A5610 WINDOW AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE COCKPIT CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29817UA 873 FIRST OFFICER'S FWD OUTER PANE WINDOW CRACKED. REPLACED RT WINDSHIELD REF MM56-11-11. ALSO REPLACED RT WINDOW HEAT CONTROLLER. 2L72 4F4 FRTA28NM E40NE 20050912001822005091200182NM 2005 9 12 DU4R20050187 120050817A5320146N852252 TEE FITTING BOEING757 757232 1384965NM BS 1320-1440 CORRODED B DALAK NONE O OTHER ININSP/MAINT 1 SO15672DL 25977 AFT CARGO COMPT THRESHOLD AREA REPAIR TEE CHORD HAS LIGHT CORROSION ON UPPER SURFACE BS 1320 - 1440. REMOVED AND REPLACED THE UPPER TEE CHORD P/N 146N8522-52 IAW B757 SRM 51-40-02, 53-60-16 FIG 102 AND 51-40-05. 2L72 4F RTA2NM 20050912001832005091200183NM 2005 9 12 DU4R20050188 120050825A5340 STRINGER CLIP BOEING757 757232 1384965NM BS 1460 CORRODED B DALAK NONE O OTHER ININSP/MAINT 1 SO15672DL 25977 CORROSION ON S-25L TIE CLIP AT FRAME 1460 IN AFT CARGO. REMOVED, FABRICATED AND INSTALLED REPAIR CLIP 3.50 X 3.20 INCH FROM BAC1518-472 EXTRUSION IAW B757 SRM 51-40-02, 51-20-01 AND DWG 140N2005. 2L72 4F RTA2NM 20050912001842005091200184NM 2005 9 12 DU4R20050189 120050818A5320 ANGLE BOEING757 757232 1384965NM BS 1640 CORRODED B DALAK NONE O OTHER ININSP/MAINT 1 SO15672DL 25977 CORROSION BETWEEN STRINGER 25R AND 26R IN AFT CARGO BULKHEAD FRAME 1640. FABRICATED AND INSTALLED REPAIR ANGLE 21.3 X 3.0 INCH FROM 7075-T6 .050 IAW B757 SRM 51-40-02 PG 1253-00-07, 51-20-01 AND DWG 753N1603-9. 2L72 4F RTA2NM 20050912001862005091200186NM 2005 9 12 CALA0500288 120050901A5320141A5310 DOOR FRAME BOEING737 737824 13844BZNM STA 290-330 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712218 28778 INSPECTION FOUND THE R-1 DOOR FRAME CORRODED FROM STA 290-330. THE CHORD WAS REMOVED AND REPLACED IAW BOEING DRAWING 141A5310. 2L72 4F RTA16WE 20050912001892005091200189NM 2005 9 12 CALA0500291 120050901A5320141A541012 WEB BOEING737 737824 13844BZNM STA 318 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712218 28778 INSPECTION FOUND A 1 INCH CRACK IN WEB AT STA 318, LBL 45. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW GMM 10-90-00 AND SRM 51-10-02. 2L72 4F RTA16WE 20050912001902005091200190NM 2005 9 12 CALA0500292 120050901A5320141A541012 WEB BOEING737 737824 13844BZNM STA 318 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712218 28778 INSPECTION FOUND A 1 INCH CRACK IN WEB AT STA 318, RBL 58. THE WEB WAS REMOVED AND REPLACED IAW GMM 10-90-000 AND SRM 51-40-02. 2L72 4F RTA16WE 20050912001922005091200192NM 2005 9 12 CALA0500294 120050902A5320147A8540U7 DOOR FRAME BOEING737 737824 13844BZNM STA 950-980 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712218 28778 INSPECTION FOUND L-2 DOOR CHORD CORRODED FROM STA 950-980, LBL 51. A NEW CHORD WAS INSTALLED IAW SRM 51-70-11. 2L72 4F RTA16WE 20050912001932005091200193NM 2005 9 12 CALA0500295 120050902A5320147A576213 INTERCOSTAL BOEING737 737824 13844BZNM BS 947.5-967 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712218 28778 INSPECTION FOUND INTERCOSTAL CORRODED BETWEEN 947.5 AND 967, RBL 50. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20050912001952005091200195WP 2005 9 12 MWEA050101 120050906A27503920274525 CONTROL CABLE DOUG DC9 DC982 3022082WP LEFT WING FRAYED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 LEFT WING NR 5 SLAT CABLE HAS A SINGLE STRAND STICKING OUT ADJACENT TO PULLEY BRACKET INBOARD OF SLAT DRIVER. REMOVED AND REPLACED PULLEY ON BRACKET JUST INBOARD OF DRIVE TRACK NR 13. 2L72 4F A6WE 20050912001982005091200198NM 2005 9 12 ABXA050210 120050831A3230 SELECTOR VALVE BOEING767 767281 1385109NM MLG BINDING A ABXAO OTHER J WARNING INDICATION APAPPROACH 1 GL23787AX 23020 INBOUND TO ILN DID A GEAR RECYCLE. GEAR DISAGREE LIGHT WITH THREE GREEN. FOUND SHAFT ON MAIN LANDING SELECTOR VALVE BINDING. REMOVED AND REPLACED MAIN LANDING GEAR SELECTOR VALVE IAW B767 AMM 32-31-02-4. OPS AND LEAK CHECKED GOOD. 2L72 4F RTA1NM 20050912001992005091200199NM 2005 9 12 ABXA050209 120050821A5210 DOOR BOEING767 767281 1385109NM MAIN PAX STIFF A ABXAO OTHER O OTHER LDLANDING 1 GL23767AX 22785 MAIN ENTRY DOOR WOULD NOT OPEN ABOVE FLIGHT. ADJUSTED BUSTLE AS NEEDED. OPS CHECKED DOOR SIX TIMES. OPS CHECKED GOOD. 2L72 4F RTA1NM 20050907000252005090700025CE 2005 9 7 DXTA200500940 120050830A2720 ACTUATOR CESSNA750 750 2076810CE YAW DAMPER MALFUNCTIONED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07961QS 7500061 LOWER YAW DAMP DISENGAGED TWICE DURING TAKEOFF ATTEMPTS. PERFORMED TEST OF LINEAR ACTUATORS FOR YAW DAMP SYSTEM IAW CESSNA 750 MM 27-24-00. OPS CHECK NORMAL. NO MESSAGES. 2L72 4J RTT00007WI 20050907000322005090700032NM 2005 9 7 SWAA052691 120050902A3350101114 LENS BOEING737 7373Y0 1384671NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29664WN 23495 EMERGENCY LIGHT LENS LOOSE AT ROW 12 DEF. SECURED LENS PER MM. 2L72 4F RTA16WE 20050907000392005090700039EA 2005 9 7 VTZA200500151 120050831A5712601R107091 RIB CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27679BR 7662 LEFT BATT RIB IS CRACKED 1.5". 2L72 4F RTA21EA 20050907000402005090700040EA 2005 9 7 VTZA200500152 120050831A531260034017595 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27622BR 7187 LT SIDE BULKHEAD AT FS 280 IBL 9.0 IS CRACKED AT 1.0" IN WEB RADIUS. 2L72 4F RTA21EA 20050907000582005090700058NM 2005 9 7 AWXA200501026 120050807A53136546877188 STRINGER BOEING737 7373G7 1384595NM BS 727 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28311AW 24712 DURING C15 CHECK DISCOVERED STRINGER 18A SHEAR BEAM CRACKED 2.0 INCHES IN LENGTH AT THE AFT END. MAINTENANCE TRIMMED OUT EXISTING CRACK IAW AMERICA WEST AIRLINES ENGINEERING REPAIR 03-5361-05241-RC1. FABRICATED FILLER AND RADIUS FILLER IAW AWA ER 03-5361-05241-RC1. INSTALLED FABRICATED REPAIR PARTS IAW AWA ER 03-5361-05241-RC1. 2L72 4F RTA16WE 20050907000622005090700062NM 2005 9 7 QXEA200501202 120050830A36208209082 SWITCH BOMBDRDHC8 DHC8402 1390042NM OVERTEMP MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09411QX 4055 NR 1 BLEED HOT CAUTION LIGHT ON CLIMB. TURNED OFF NR 1 BLEED AS PER E/A CHECKLIST, LIGHT STAYED ON. AIRCRAFT FERRIED FROM PSP TO PDX. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE NACELLE DUCT LEAK OVERTEMP SWITCH IAW TASK 36-11-21-000-801 AND -400-801. PERFORMED OPERATIONAL TEST OF BLEED AIR SYSTEM IAW TASK 36-11-00-710-802. OPS TEST OK. NR 1 BLEED HOT CAUTION LIGHT NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050907000702005090700070SO 2005 9 7 RAIA00508038 120050829A5210 SEAL EMB 145 EMB145EP 3260221SO PAX DOOR OBSTRUCTED A RAIAA UNSCHED LANDING C F.O.D. CLCLIMB 1 CE03826HK 145016 FLT 5537-STL - CABIN FAILED TO PRESSURIZE AFTER 12000 AND CLIMBING. MAINTENANCE FOUND INTERIOR TRIM PANEL OVER PART OF THE DOOR SEAL. REPOSITIONED TRIM. SYSTEM OPS CHECKED GOOD. 2L72 4F RTT00011AT 20050907000712005090700071SO 2005 9 7 RAIA00509002 120050902A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03836HK 145695 FLT 8004 - ORD - EMERGENCY FLOOR LIGHTING INOP. MAINTENANCE SECURED EMERGENCY FLOOR TRACK SECTION. 2L72 4T RTT00011AT 20050907000882005090700088SO 2005 9 7 C2XA05BT062 120050820A32608005701 SENSOR EMB 145 EMB145LR 3260212SO MLG FAULTY A C2XAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW27155553592 3592 145594 CREW REPORTED, "LANDING GEAR AIR/GROUND FAIL AFTER TAKEOFF, GEAR WOULD NOT RETRACT." MAINTENANCE REMOVED AND REPLACED THE LEFT TRAILING ARM PROXIMITY SWITCH IAW EMB145 MM NR 32-63-01. OPS CHECKED OF LANDING GEAR AIR/GROUND SYSTEM AND LANDING GEAR SWING GOOD IAW EMB145 MM NR 32-63-03. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20050907000892005090700089SO 2005 9 7 C2XA05CL069 120050822A2910368192111 PRESSURE SWITCH EMB 145 EMB145EP 3260221SO HYD SYSTEM CRACKED A C2XAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 SW2712934 145019 ROC - FLIGHT NR 2040, THE CREW REPORTED A NR 1 HYDRAULIC LOW QUANTITY IN FLIGHT. REPORTED LOSS OF ALL NR 1 HYDRAULIC FLUID IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE PRESSURE SUPPLY PRESSURE SWITCH. ALSO, REPLACED THE NR 1 HYDRAULIC PUMP AND FILTER. 2L72 4F RTT00011AT 20050908000282005090800028NM 2005 9 8 05FDEA02763 120050906A5753 ATTACH FITTING DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 LEFT WING - O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. CORROSION REPAIR CARRIED OUT AS PER EA 1-5750-87629. 2L73 4F RTA22WE 20050908000362005090800036NM 2005 9 8 05FDEA02771 120050906A5753 ATTACH FITTING DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 RT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. FABRICATED BUSHING AND INSTALLED AS PER EA 1-5750-87630. 2L73 4F RTA22WE 20050908000542005090800054NM 2005 9 8 05FDEA02779 120050906A5753 ATTACH FITTING DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 RT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87632. 2L73 4F RTA22WE 20050908000572005090800057NM 2005 9 8 05FDEA02782 120050906A5313 LONGERON DOUG MD11 MD11 3023602NM BS 1139 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 CAC COMPT BETWEEN STA 1139 AND STA 1159, LONGERON 51R CRACKED. SPLICE REMOVED AND NEW SPLICE INSTALLED AS PER SRM 51-31-01 VOL.II, SRM 51-33-01 VOL.II, SRM 51-35-01 VOL.II AND DRAWING AAA 7086. NEW SPLICE PART. NR FXAAA 7086-1 FABRICATED AS PER DRAWING AAA 7086. MINOR REPAIR PER GMM 6-2-100. 2L73 4F RTA22WE 20050908000622005090800062WP 2005 9 8 UPS05845343 120050829A5712 RIB DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 LT WING LE LOWER RIB IS CRACKED AT XFS 335.250. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2 -0 FIG 2. 2L74 4F RT4A25 20050908000642005090800064WP 2005 9 8 UPS05845345 120050829A5712 RIB DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 LEFT WING LE LOWER RIB PREVIOUS REPAIR IS CRACKED AT XFS 360.250. REMOVED, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20050908000662005090800066WP 2005 9 8 UPS05845347 120050829A5712 RIB DOUG DC8 DC873F 302199FWP LT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 LT WING LE LOWER RIB IS BULGED AND HAS INTERGRANULAR CORROSION AT XFS 372.750. CUT OUT DAMAGE, FABRICATED, INSTALLED REPAIR IAW DC-8 SRM 57-2-0 FIG. 2. 2L74 4F RT4A25 20050908000692005090800069WP 2005 9 8 UPS05845351 120050828A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 RT WING LE SKIN IS CRACKED AT TWO LOCATIONS XW 257. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1. 2L74 4F RT4A25 20050908000742005090800074NM 2005 9 8 UPS05M45360 120050817A5347 SEAT TRACK DOUG MD11 MD11F 3023600NM BS 824-840 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01256UP 48405 CABIN SEAT TRACK AT STA 824-840 LBL =107.25 FOUND SEVERAL PLACES CORRODED. SEAT/T CORROSION REMOVED FOUND OUT OF LIMIT, (ORI THK 0.080" AND MAT REMOVED THK 0.030", PER SRM 53-70-00.F3.V.1.R37. DAMAGED PORTION OF SEAT/T CUT REMOVED. SPLICE AND NEW SEAT/TRACK INSTALLED PER SRM 53-70-00 .F1.V.1R .37 AT STA765-830,LBL=107.25. 2L73 4F RTA22WE 20050908000842005090800084NM 2005 9 8 05FDEA02736 120050902A5753 SKIN BOEING727 727225 1384077NM FORE FLAP TORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 LEFT WING OUTBORD FORE FLAP UPPER SKIN SECTION MISSING (HONEYCOMB EXPOSED). REMOVED AND REPLACED LEFT WING OUTBORD FORE FLAP ASSEMBLY ON FEDEX SNRM N00079. REFERENCE NON ROUTINE N00007. 2L73 4F A3WE 20050908000882005090800088NM 2005 9 8 SB05108 120050903A29136507506 PUMP BOEING737 737301 1384611NM NR 1 ENGINE LEAKING A USAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 EA19300AU1 1 23228 PHL - FLT803 - ON CLIMB-OUT FROM PHL, CREW REPORTED THE NR 1 ENGINE HYDRAULIC PUMP LOW PRESSURE LIGHT ILLUMINATED ON GEAR RETRACTION. SYSTEM "A" HYDRAULIC QUANTITY DROPPED TO LESS THAN ONE-QUARTER. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP AND INSPECTED AND REPLACED THE NR 1 ENGINE CASE DRAIN FILTER, WHICH CHECKED OK. RESERVICED HYDRAULIC SYSTEM. OPERATIONAL CHECK AND LEAK CHECK GOOD. 2L72 4F RTA16WE 20050908000942005090800094EU 2005 9 8 08182005A 120050818A2750 VALVE SAAB SF340 340B 7860101EU TE FLAPS MALFUNCTIONED A NSVAO OTHER J WARNING INDICATION CRCRUISE 1 EA279CJ 224 FLAPS DEPLOY VIOLENTLY FROM 0 TO 15 DEGREES. REMOVED AND REPLACED FLAP VALVE. 2L72 4T RTA52EU 20050908001052005090800105EA 2005 9 8 SWIA200515494 120050830A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 NM07440SW8004 8004 7589 STAB TRIM CH 1 STATUS MESSAGE AFTER TAKEOFF. REPLACED HSTCA AND HSTMCU IAW 27-40-27. OPERATIONAL CHECK GOOD, PN 7062-3 SN/OFF 1131. 2L72 4F RTA21EA 20050908001262005090800126WP 2005 9 8 UPS05845325 120050828A5712 RIB DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 C3 LT WING L/E LOWER RIB CRACKED AT XFS 822.500. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2 -0 FIG 2. 2L74 4F RT4A25 20050908001282005090800128WP 2005 9 8 UPS05845327 120050828A5712 RIB DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 LT WING L/E LOWER RIB IS CRACKED AT XFS 772.500. CRACK EXTENDS FROM EDGE TO FASTENER HOLE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20050908001422005090800142NM 2005 9 8 2005UALA00893 120050826A5310 DOOR FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FWD GALLEY DOOR CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29327UA 24147 FWD GALLEY DOOR STUB FRAME AT STA 296 AND RBL 54 CORRODED AT STRINGER S-17R AND WL 208. 2L72 4F4 FRTA16WE E2GL 20050908001512005090800151NM 2005 9 8 2005UALA00902 120050827A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE BS 1787.43 DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29588UA 26717 LOWER AFT FUSELAGE LIGHTNING STRIKE AT BS 1787.43 LBL 8 AT FASTENER AND SKIN. REMOVED DAMAGE, ACP HEFC INSP, NO CRACKED NOTED. INSTALL REPAIR DOUBLER PER SRM 53-00-01, AND TIMCO REO-G10914, REV A. 2L72 4F4 FRTA2NM E17NE 20050908001532005090800153NM 2005 9 8 2005UALA00904 120050826A335078941 LAMP BOEING777 777222 1385219NM PWA PW4077PW4077 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29780UA 26944 EEL LIGHT INOP 21G. REPLACED LAMP ASSY. 2L72 4F4 FRTT0001SE E46NE 20050912000032005091200003NM 2005 9 12 QXEA200501205 120050904A36208209082 SWITCH BOMBDRDHC8 DHC8402 1390042NM NR 2 NACELLE FAILED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09402QX 4032 PDX FLIGHT 2405: NR 2 BLEED HOT CAUTION LIGHT CAME ON AFTER START. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE NACELLE DUCT LEAK OVERTEMP SWITCH AND BLEED OVERTEMP SWITCH IAW Q400 AMM 36-11-21-000/400-801 AND 36-11-16-400-801. GROUND RAN AIRCRAFT AT VARIOUS BLEED SETTINGS FOR APPROXIMATELY 10 MINUTES. CAUTION MESSAGE DID NOT REAPPEAR. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050912000112005091200011EA 2005 9 12 SWIA200515504 120050904A2741 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07915SW 7615 STAB CH 2 WILL NOT ENGAGE. REPLACED PILOT STAB TRIM DISCONNECT SWITCH AS REQUIRED. OPERATIONAL CHECK GOOD IAW 27-41-00. 2L72 4F RTA21EA 20050912000132005091200013EA 2005 9 12 SWIA200515506 120050901A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLT SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07928SW 7701 ON TAXI OUT, FLT SPOILER FAULT STATUS MSG APPEARED. REPLACED L FLIGHT SPOILER INBOARD PCU IAW CRJ MM 27-62-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050912000192005091200019EA 2005 9 12 SWIA200515512 120050902A274183963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07437SW1085810858 7564 STAB 1 WILL NOT ENGAGE. REPLACED HORIZONTAL STAB TRIM ACTUATOR AND MOTOR CONTROL UNIT IAW MM 27-40-00, 27-42-01, 27-42-05, P/N: 7062-3; S/N OFF: 1004. 2L72 4F RTA21EA 20050912000392005091200039WP 2005 9 12 0501399921 120050904A2130NW9A21407111 HOSE DOUG DC9 DC932 3022066WP CABIN PRESSURE SEPARATED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01943N 47647 WHILE CRUISING AT FL 350, THE CABIN PRESS WARNING ILLUMINATED AND INDICATION SHOWED THE CABIN CLIMBING THROUGH 9500 FEET. FLT CREW INITIATED AN EMERGENCY DESCENT DOWN TO 10,000 FT AND DIVERTED TO DTW. LOG PAGE STATES THAT THE CABIN PRESSURE CONTROL RETURNED AS THE AIRCRAFT PASSED THROUGH FL 250 FOLLOWING COM PROCEDURE COMPLIANCE. THE LANDING AT DTW WAS UNEVENTFUL AND MAINTENANCE FOUND A HOSE BLOWN OFF DUCTING. THE HOSE WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F A6WE 20050912000452005091200045NM 2005 9 12 SWAA052720 120050906A53116546552 FRAME BOEING737 7373H4 1384600NM BS 827 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L & STR 8R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050912000462005091200046NM 2005 9 12 SWAA052721 120050906A53116546550 FRAME BOEING737 7373H4 1384600NM BS 787 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L & STR 8R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050912000642005091200064NM 2005 9 12 SWAA052699 120050905A53306545768 SKIN BOEING737 7373H4 1384600NM BS 324 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 324, STR 23R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050912000672005091200067NM 2005 9 12 SWAA052702 120050904A53306545765 SKIN BOEING737 7373H4 1384600NM BS 500D + 18 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29373SW 26581 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D + 18, STR 12L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050912000832005091200083NM 2005 9 12 SWAA052736 120050904A53126582671 PRESSURE PANEL BOEING737 7377H4 1384404NM RT MLG WW CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29784SW 29810 DURING SCHEDULED 5Y CHECK, FOUND RIGHT MLG W/W FWD WEB CRACKED AT BS 663, RBL 14. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050912000882005091200088 2005 9 12 P5CA0501393 420050823A22102590622935 COMPUTER BOEING747 747341 13848AMNM AUTOPILOT INOPERATIVE A P5CAK NONE O OTHER ININSP/MAINT 1 EA15355MC 23395 "A" AUTOPILOT ALT HOLD INOP. "B" AUTOPILOT ON DEFERRAL WILL NOT ENGAGE. REPLACED "A" PITCH COMPUTER PER MM 22-12-01. DMI CONTINUES. 2L74 4F RTA20WE 20050912000892005091200089EA 2005 9 12 VNAA0508025 120050826A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A VNAAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL05218PS 7885 ON DOWNWIND THE FLAPS FAIL MESSAGE ILLUMINATED WITH FLAPS AT 8 DEGREES. THE CREW FOLLOWED THE QRH AND LANDED. MAINTENANCE RESET THE FECU IAW CRJ200 SL:00-001. FLAP SYSTEM OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050912000922005091200092WP 2005 9 12 MWEA050104 120050907A5754 SKIN DOUG DC9 DC981 3022081WP WING SLAT CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31804ME 48030 LEADING EDGE AT STATION 375 HAS CORROSION. FABRICATED AND INSTALLED DOUBLER AND FILLER. 2L72 4F A6WE 20050912000932005091200093CE 2005 9 12 DXTA200500952 120050905A7830650162 POSITION SWITCH BEECH MU300 400A 1155402CE THRUST REVERSER INOPERATIVE E DXTAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL07120QS65 RK409 DURING CRUISE FLIGHT AT FL,360/.78 MACH THE LT DEPLOY LIGHT ILLUMINATED (THE DEPLOY ONLY-NO ARM OR UNLOCK.) DESCENDED AND PUSHED EMERGENCY STOW. THE BOTTOM PORTION OF THE EMERGENCY STOW THRUST REVERSER. ARM AND DEPLOY WERE NOW ILLUMINATED. THE DEPLOY LIGHT REMAINED ILLUMINATED UNTIL THE AIRSPEED DROPPED BELOW 200 KTS. REMOVED AND REPLACED LT TR DEPLOY SWITCH IAW NORDAM CMM 78-30-07. OP CHECKS AND RIG CHECKS GOOD. 2H72 4F RTA16SW 20050912000952005091200095CE 2005 9 12 DXTA200500948 120050901A3244 LINE CESSNA680 680CE 2076811CE HYDRAULIC SYS MISINSTALLED E DXTAO OTHER G MULTIPLE FAILURE LDLANDING 1 GL07349QS207 6800029 THE LEFT OUTBOARD MAIN TIRE BLEW ON LANDING THE ANTI-SKID INOP EICAS MESSAGE DISPLAYED ON ROLL OUT AND EXTINGUISHED SHORTLY THEREAFTER. THE SIC (PF) ALSO NOTED THE RIGHT BRAKE PEDAL FELT NORMAL AND THE LEFT BRAKE PEDAL FELT MUSHY. FOUND LT INBOARD + OUTBOARD BRAKE LINES FROM ANTI SKID CONTROL VALVE TO PARKING VAVLE INSTALLED IMPROPERLY. LEFT INBOARD LINE LEFT OUTBOARD PAT ON PART BRAKE VALVE, LEFT OUTBOARD LINE LEFT INBOARD PORT ON PART BRAKE VALVE. CONFIGURED LINES LEFT INBOARD TO LEFT INBOARD, RIGHT INBOARD TO LEFT INBOARD. BLED BRAKES IAW 680 MM CHAPT 32-42-10 LINES INSTALLED IAW 680 MM CHAPT 32-42-20. LEAK CHECK GOOD, OPS CHECK GOOD. 2L72 4F RCT00012WI 20050912001022005091200102CE 2005 9 12 DXTA200500949 120050901A215073838431 ACM CESSNA750 750 2076810CE COCKPIT STIFF E DXTAB EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07923QS4069 7500023 NOTICED A PUNGENT SUFFER ODOR IN THE COCKPIT WHILE AT FL410 IN CRUISE POWER, ODOR SEEMS TO COME AND GO. ACCOMPLISHED AN EMERGENCY DESCENT AND LANDING W/O FURTHER INCIDENT. FOUND COCKPIT ACM VERY STIFF TO TURN. REPLACED ACM IAW 750 MAINTENANCE MANUAL CHPT 21-51-00. 2L72 4J RTT00007WI 20050912001052005091200105NM 2005 9 12 P5CA0501397 120050908A2820MA11A11731 ACTUATOR BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE NR 1 ENGINE MALFUNCTIONED A P5CAK NONE O OTHER ININSP/MAINT 1 EA15858FT 20109 695749 AFTER ENGINE START, NR 1 ENGINE RAN FOR APPROX 3 MINUTES THEN SHUT DOWN. REPLACED NR 1 ENGINE SPAR VALVE ACTUATOR, MM 28-22-01. 2L74 4F4 F A20WE E20EA 20050912001182005091200118NM 2005 9 12 QXEA200501207 120050906A242051608003 GCU DHAV DHC8 DHC8202 2809007NM NR 2 GENERATOR MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09348PH394496055 484 SEA FLIGHT 2172 FROM EUG TO SEA RECEIVED NR 2 AC GENERATOR CAUTION LIGHT FIVE TIMES DURING VARIOUS PHASES OF FLIGHT. RECYCLED PER THE EA CHECKLIST, BUT IT WOULD COME ON AGAIN AFTER A WHILE EACH TIME. MAINTENANCE REPLACED NR 2 ENGINE GCU. OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050912001382005091200138EA 2005 9 12 REXA200500113 120050909A5220H341931 HANDLE CNDAIRCL600 CL6002B19 1900309EA ESCAPE HATCH CORRODED A REXAK NONE O OTHER ININSP/MAINT 1 SO258665A 7665 DURING ROUTINE INSPECTION TASK, CREW ESCAPE HATCH OUTER HANDLE DID NOT EJECT WHEN OPENING ESCAPE HATCH WHEN UTILIZING INSIDE HANDLE. OUTER HANDLE IS RECESSED INTO HATCH FOR AERODYNAMIC PURPOSES. UPON INSPECTION, OUTER HANDLE WAS FOUND FROZEN IN PLACE (FLUSH) DUE TO CORROSION. 2L72 4F RTA21EA 20050912001402005091200140 2005 9 12 UPS05145373 420050908A2565 LIGHT AIRBUSA300 A300F4622R 3930360EU ESCAPE SLIDE INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01151UP 0834 EVACUATION SLIDE WARNING LIGHT INOP. LIGHT DEFERRED PER MEL 52-73-01-1 M-309637 ASSIGNED. PREFORMED EMERG ESCAPE SLIDE RELEASE & RESIDUAL PRESSURE WARNING ADJ/TEST PER MM 52-73-00 & BITE TEST OF ASPW PER MM 52-73-00. NO FAULTS FOUND AT THIS TIME. OPS CK GOOD. [CLOSED] 2L72 4F RTA35EU 20050912001482005091200148SO 2005 9 12 C2XA05SH110 120050901A523014525480003 BEAM EMB 145 EMB145 3260210SO CARGO DOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714959 145091 SHV - DURING C-CHECK, CARGO DOOR LOWER BEAM AT FS 65-68 HAS CORROSION. MAINTENANCE REMOVE AND REPLACED CARGO DOOR LOWER BEAM AT FS 65-68 IAW SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2L72 4F RTT00011AT 20050912001502005091200150NM 2005 9 12 2005UALA00909 120050825A2782 ACTUATOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 6 SLAT FAILED A UALAO OTHER J WARNING INDICATION NRNOT REPORTED 1 WP29507UA 24743 LEADING EDGE SLAT DISAGREE MESSAGE. LEADING EDGE SLAT DISAGREE MSG PER CREW. FOUND NR 6 SLAT ACTUATORS NR 11 AND 12 OVERLOAD INDICATORS POPPED. REPLACED BOTH NR 11 AND 12 SLAT ACTUATORS. 2L72 4F4 FRTA2NM E17NE 20050912001612005091200161NM 2005 9 12 2005UALA00920 120050830A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE BS 1640 CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29505UA 24626 MAIN CABIN FLOORBEAM AT BS 1640, UPPER T-CAP HAS CORROSION IN SEVERAL PLACES AROUND FASTENER HOLES, UPPER AND LOWER SURFACES, LBL 9 TO RBL 60. REMOVED EXISTING SPLICES AND DAMAGED T-CAP SECTION, FABRICATED NEW T-CAP AND SPLICE ANGLES AND STRAPS PER MM 53-00-98. 2L72 4F4 FRTA2NM E17NE 20050912001622005091200162EA 2005 9 12 VNAA0508024 120050826A2751601R590141 DETECTOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS FAILED A VNAAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 GL05244PS3201 7912 ON FINAL APPROACH THE CREW REPORTED A FLAPS FAIL MESSAGE AT 45 DEGREES. MAINTENANCE DETERMINED THAT THE SKEW DETECTION UNIT WAS INOPERATIVE. THE SKEW DETECTION SYSTEM WAS DEFERRED IAW CRJ200 MEL 27-51-03(C). THE AIRCRAFT WAS RELEASED FOR SERVICE. CAK MAINTENANCE INSTALLED A SERVICEABLE SKEW DETECTION UNIT ON 08/30/05 IAW CRJ200 AMM 27-51-15-400-801. OPERATIONAL CHECKS WERE GOOD. THE MEL WAS CLEARED AND THE AIRCRAFT WAS AGAIN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050912001632005091200163EA 2005 9 12 VNAA0508022 120050823A5220SH670505467 LEVER CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE EMERGENCY DOOR WORN A VNAAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 GL05709PS1570 10165 DURING TAKEOFF THE LEFT EMERGENCY DOOR CAUTION MESSAGE ILLUMINATED. THE CREW ABORTED THE TAKEOFF. MAINTENANCE VERIFIED THE DOOR WAS SECURED AND DEFERRED THE INDICATION SYSTEM PER MEL 52-70-03 CODE C. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. AFTER TROUBLESHOOTING THE LEVER ASSEMBLY WAS FOUND WORN MAKING POOR CONTACT WITH THE PROXY SENSOR. PART IS ON ORDER. 2L72 4F4 FRTA21EA EOOO63EN 20050912001732005091200173EA 2005 9 12 SWIA200515493 120050828A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLT SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION LDLANDING 1 NM07919SW7735 7735 7657 SPOILERON FAULT MESSAGE UPON LANDING. REPLACED PCU SPOILERON RT OUTBOARD. OPERATIONAL CHECK GOOD IAW MM 27-60-00. 2L72 4F RTA21EA 20050912001872005091200187NM 2005 9 12 CALA0500289 120050901A5347BAC15202789 SEAT TRACK BOEING737 737824 13844BZNM BS 370-385 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712218 28778 INSPECTION FOUND LT OUTBOARD SEAT TRACK CORRODED FROM STA 370-385, LBL 45.5. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-40-00 AND 53-00-52. 2L72 4F RTA16WE 20050912001882005091200188NM 2005 9 12 CALA0500290 120050901A5347BAC15202789 SEAT TRACK BOEING737 737824 13844BZNM STA 370-385 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712218 28778 INSPECTION FOUND LT INBOARD SEAT TRACK CORRODED FROM STA 370 TO 385, LBL 24.75. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-40-00 AND 53-00-32. 2L72 4F RTA16WE 20050912001972005091200197NM 2005 9 12 UPS05M45320 120050524A5347 SEAT TRACK DOUG MD11 MD11F 3023600NM BS 1961 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01255UP 48404 CK AFT CABIN CORROSION ON SEAT TRACK AT X=107 STA 1961. AFT CABIN CORROSION ON SEAT TRACK AT X=107 STA 1961. REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-70-00 FIG 3 VOL 1 REV 36. REPAIR SLICE HAT REWORKED CARRIED OUT AND REPAIR SPLICE PLATE FABRICATED AS PER SRM 53-7 0-00 FIG 1 VOL 1 REV 37. INSTALLED NEW SEAT TRACK, REPAIR SPLICE HAT AND SPLICE PLATE BETWEEN STA 1831 TO STA 2007 X=107 AS PER SRM 51-31-01. 2L73 4F RTA22WE 20050912002062005091200206NM 2005 9 12 SWAA052674 120050902A531265C28106 STIFFENER BOEING737 7373H4 1384600NM BS 1016 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29373SW 26581 DURING SCHEDULED 1/4D CHECK, FOUND LT CHANNEL STIFFENER CORRODED AT BS 1016 BULKHEAD, BL 0. REPAIRED STIFFENER PER BOEING DRAWING. 2L72 4F RTA16WE 20050912002082005091200208EU 2005 9 12 MALA050689 120050903A5230 SKIN BAC 146 AVRO146RJ85A1500097EU CARGO DOOR CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15507XJ E2316 WHILE ACCOMPLISHING C1 INSPECTION, FOUND A CRACK ON THE REAR CARGO DOOR OUTER SKIN BOTTOM AFT CORNER 6 INCHES FROM BOTTOM OF DOOR. 2H74 4F RTA49EU 20050912002092005091200209EU 2005 9 12 MALA050690 120050903A5420 BUSHING BAC 146 AVRO146RJ85A1500097EU NR 1 PYLON MIGRATED A MALAK NONE O OTHER ININSP/MAINT 1 GL15507XJ E2316 WHILE ACCOMPLISHING C3.IG1 INSPECTION FOUND THE NR 1 ENGINE PYLON TO YOKE LINK BUSHINGS HAVE MIGRATED OUT. 2H74 4F RTA49EU 20050912002112005091200211EU 2005 9 12 MALA050693 120050903A5420 BUSHING BAC 146 AVRO146RJ85A1500097EU NR 4 PYLON MIGRATED A MALAK NONE O OTHER ININSP/MAINT 1 GL15507XJ E2316 WHILE ACCOMPLISHING C3.IG1 INSPECTION FOUND THE NR 4 ENGINE PYLON TO YOKE LINK BUSHINGS HAVE MIGRATED OUT. 2H74 4F RTA49EU 20050912002122005091200212EU 2005 9 12 MALA050694 120050903A5320 SILL BAC 146 AVRO146RJ85A1500097EU PASSENGER DOOR CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15507XJ E2316 WHILE ACCOMPLISHING C2 INSPECTION FOUND CORROSION ON THE LEFT AFT PASSENGER DOOR SILL PLATE ON THE FLANGE THAT FLOORBOARD SIT ON, BETWEEN FRAMES 14 AND 43. 2H74 4F RTA49EU 20050912002132005091200213EU 2005 9 12 MALA050695 120050903A5320 GUSSET BAC 146 AVRO146RJ85A1500097EU FRAME 43 CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15507XJ E2316 WHILE ACCOMPLISHING C2 INSPECTION FOUND CORROSION ON FLOORBEAM INTERCOSTAL GUSSET PLATE BETWEEN FRAMES 41 AND 43, 31 INCHES INBOARD OF LEFT AFT PASSENGER DOOR SILL AT FRAME 43. 2H74 4F RTA49EU 20050912002142005091200214EU 2005 9 12 MALA050700 120050903A5310 DOOR FRAME BAC 146 AVRO146RJ85A1500097EU CARGO DOOR CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15507XJ E2316 WHILE ACCOMPLISHING F1.IG1T INSPECTION FOUND CORROSION ON AFT CARGO DOOR SURROUND AT BOTTOM OF DOOR FRAME INNER SURFACE, 10 TO 25 INCHES AFT OF FORWARD SIDE OF DOOR FRAME. 2H74 4F RTA49EU 20050912002152005091200215EU 2005 9 12 MALA050702 120050903A5320 SILL BAC 146 AVRO146RJ85A1500097EU SERVICE DOOR CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15507XJ E2316 WHILE ACCOMPLISHING C3.IG1 INSPECTION FOUND FORWARD RIGHT SERVICE DOOR SILL PLATE CORRODED. 2H74 4F RTA49EU 20050912002192005091200219EU 2005 9 12 MALA050697 120050903A5320 SILL BAC 146 AVRO146RJ85A1500097EU SERVICE DOOR CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15507XJ E2316 WHILE ACCOMPLISHING C2 INSPECTION FOUND CORROSION ON RIGHT AFT SERVICE DOOR SILL PLATE ON THE FLANGE THAT THE FLOORBOARD SITS ON, BETWEEN FRAMES 41 AND 43. 2H74 4F RTA49EU 20050912002202005091200220EU 2005 9 12 MALA050699 120050903A5313 LONGERON BAC 146 AVRO146RJ85A1500097EU FR 35 CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15507XJ E2316 WHILE ACCOMPLISHING F1.IG1T INSPECTION FOUND CORROSION ON AFT CARGO DOOR SURROUND LOWER LONGERON STRAP AT FRAME 35. 2H74 4F RTA49EU 20050912002402005091200240NM 2005 9 12 USAA200509001 120050906A5330 SKIN BOEING737 737301 1384611NM BS 727D CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19334US 23231 1-7/8 INCH CRACK AT BS 727D AND STRINGER 3L. REMOVED DAMAGED SKIN AND REPAIRED PER SRM 53-00-01. 2L72 4F RTA16WE 20050912002412005091200241EU 2005 9 12 BA05019 120050906A3350321431 BATTERY AIRBUS330 A330323 3930335EU EMERGENCY LIGHT DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW 315 PHL - THE EPSU AT DOOR 3L FAULTED DURING TEST. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT AT DOOR 3L. OPERATIONALLY CHECKS OK. 2L72 4F RTA46NM 20050912002422005091200242NM 2005 9 12 USAA051067 120050906A5330 SKIN BOEING737 7373B7 1384580NM BS 727D CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19397US 23319 15.5 INCHES AFT OF BS 727D, S23L (2) 16.5 INCHES AFT OF BS 727D, S-22L, REMOVED DAMAGE, FAB AND INST DOUBLER, INC 2 CRACKS AND 2 PREEX REPAIRS TO 1 DOUBLER REP IAW 53-00-01 FIG 201. DEFECT SIZE: (1) 15.5 INCHES AFT OF BS 727D, S-23-L, (2) 16.5 INCHES AFT OF BS 727. 2L72 4F RTA16WE 20050912002432005091200243NM 2005 9 12 USAA051066 120050906A5330 SKIN BOEING737 7373B7 1384580NM BS 754 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19397US 23319 CRACK IN FUSELAGE SKIN BS 754, S25L. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER PER SRM 53-00-01 FIG 249. DEFECT SIZE: 4.5 INCH CRACK IN FUSELAGE SKIN. 2L72 4F RTA16WE 20050912002442005091200244NM 2005 9 12 USAA051065 120050906A5320 ANGLE BOEING737 7374B7 1384702NM BS 344 DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19449US 24893 FUESLAGE STATION 344 RIGHT HAS GAP. FABRICATED SHIMS AND FILLERS AND INSTALLED PER EA 96820. DEFECT SIZE: .275 INCH GAP BETWEEN THE RIGHT CREASE BEAM INNER CHORD ANGLE AND FLOORBEAM. 2L72 4F RTA16WE 20050912002472005091200247EA 2005 9 12 SWIA200515516 120050906A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY MALFUNCTIONED A SWIAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 NM07461SW 7811 CARGO SMOKE MESSAGE ON GROUND IN SLC. REPLACED NR 2 CARGO SMOKE DETECTOR. OPERATIONAL CHECK GOOD, PN 473597-19 SN/OFF 2001. 2L72 4F RTA21EA 20050912002502005091200250EA 2005 9 12 SWIA200515519 120050905A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY FAILED A SWIAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 NM07908SW 7540 WHILE HOLDING SHORT OF RUNWAY, RECEIVED A INTERMITTENT "CARGO SMOKE" WARNING WITH ASSOCIATED AURAL WARNING. REPLACED NR 2 CARGO SMOKE DETECTOR. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050912002552005091200255EA 2005 9 12 SWIA200515522 120050905A274170609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07954SW 7815 INFLIGHT STAB TRIM AND MACH TRIM CAUTION MSGS APPEARED. REPLACED HSTCU. OPERATIONAL CHECK GOOD IAW CRJ MM 27-41-01. 2L72 4F RTA21EA 20050912002562005091200256EA 2005 9 12 SWIA200515523 120050831A5514 BUSHING CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB DAMAGED A SWIAO OTHER F FLT CONT AFFECTED CLCLIMB 1 NM07591SW 7079 DURING CLIMB-OUT AT 280KTS AT 25,500 FT, EXPERIENCED AC FLUTTER. REMOVED AND REPLACED HORIZ STABILIZER BUSHINGS IAW SB 601R-55-007. 2L72 4F RTA21EA 20050912002572005091200257 2005 9 12 AWXA200501030 420050907A341746502003030314 ADC AIRBUSA319 A319132 3930340NM NR 1 MALFUNCTIONED A AWXAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 WP28807AW1737215397 1064 FLT 029 - ABORTED TAKEOFF AT 80 KNOTS DUE TO IR NR 1 FAULT. RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ADIRU IAW AMERICA WEST AIRLINES TASK CARD R2A34304. OPERATIONAL CHECKS WERE GOOD. VENDOR TEAR DOWN REPORT SHOWS THAT THE "Y" GYRO TO BE A SLOW STARTER. GYRO WAS REPLACED AND UNIT CALIBRATED. REPAIR AND FUNCTIONAL TESTS WERE PREFORMED IAW AT261847-01, CMM TP1011 REV 24. 2L72 4F RTA28NM 20050912002582005091200258NM 2005 9 12 AWXA200501031 120050907A7722 WARNING LIGHT BOEING737 7373S3 1384711NM NR 1 ENGINE ILLUMINATED A AWXAC ABORTED TAKEOFF MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 WP28314AW 23733 FLT 122 - REJECTED TAKEOFF, AT 70 KNOTS, IN PHX FOR NR 1 ENGINE OVER TEMP. CREW REPORTED THE NR 1 ENGINE EGT REACHED 930 DEG AND RED LIGHT ILLUMINATED FOR LESS THAN A COUPLE SECONDS. AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED POWER ASSURANCE RUNS IAW AMERICA WEST AIRLINES TASK CARD F5M71003. OPERATIONAL TESTS WERE NORMAL. 2L72 4F RTA16WE 20050912002612005091200261NM 2005 9 12 AWXA200501034 120050908A33501012721 LIGHT BOEING737 7373G7 1384595NM CABIN INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 PHX - EEL - DURING 4 DAY CHECK DISCOVERED, SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE AT ROW 14L. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AT ROW 14L OPERATIONAL CHECKS GOOD. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20050912002622005091200262NM 2005 9 12 AWXA200501035 120050831A53206545834107 STRAP BOEING737 7373G7 1384595NM BS 325 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - DURING C18 CHECK DISCOVERED, THE LOWER CABIN FLOOR STRAP CRACKED, 1.15 INCHES IN LENGTH, AT BS 325, BL 32R, AND WL 200. MAINTENANCE STOP DRILLED CRACK FLOOR STRAP AT BS 324, BL 32R, AND WL 200 IAW BOEING 737-300 SRM 53-10-51-2. FABRICATED REPAIR PLATE IAW BOEING 737-300 SRM 53-10-51-2. INSTALLED FABRICATED REPAIR PARTS IAW BOEING 737-300 SRM 51-40-02-0. 2L72 4F RTA16WE 20050912002652005091200265NM 2005 9 12 AWXA200501038 120050828A53206520726502 INTERCOSTAL BOEING737 7373Y0 1384671NM BS 500-500A CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 DURING C16 CHECK DISCOVERED INTERCOSTAL CRACKED AT ZEE CHANNEL ATTACH HOLE, BS 500-500A, STRINGER 26L, BL 25R. MAINTENANCE REMOVED INTERCOSTAL AT BS 500-500A, WL 154, STR 26L IAW BOEING 737-300 SRM 53-30-15-0. FABRICATED FILLER AND REPAIR ANGLE IAW BOEING 737-300 SRM 51-70-11-0. INSTALLED FABRICATED REPAIR PARTS ONTO INTERCOSTAL AND RE-INSTALLED INTERCOSTAL AT BS 500-500A, STRINGER 26L, BL 25R IAW BOEING 737-300 SRM 51-40-02-0. 2L72 4F RTA16WE 20050912002672005091200267EU 2005 9 12 USAA051077 120050909A5315D5311282600101 FLOORBEAM AIRBUSA319 A319112 3930323EU FR 14 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19730US 1182 FLOORBEAM Y503.4 LEFT BETWEEN FRAME 14 DEFECTIVE. DEFECTIVE PART REPLACED WITH IDENTICAL PART PR SRM 51-72-11. DEFECT SIZE: .5 X 8 X .040 INCH DEEP. 2L72 4F RTA28NM 20050912002682005091200268NM 2005 9 12 USAA051069 120050909A321065605795 BUSHING BOEING737 7374B7 1384702NM MLG CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19449US 24893 UNIVERSAL ASSY AND LWR DRAG STRUT BUSHINGS IN RT MAIN GEAR CORRODED. REMOVED CORROSION AND INSTALLED NEW BUSHINGS IAW EA 96880, DEFECT SIZE: 1 X 3 INCH. 2L72 4F RTA16WE 20050912002702005091200270NM 2005 9 12 USAA051071 120050909A5312 BULKHEAD BOEING757 7572B7 1384964NM BS 164.3 DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19628AU 27806 MID BULKHEAD O/B FWD UPPER BOLT HOLE PP STA 164.3 DAMAGED. REAMED HOLE, INSTALLED SLEEVE BUSHING, REAMED PER EA 96822, DEFECT SIZE: .8810. 2L72 4F RTA2NM 20050912002712005091200271EU 2005 9 12 USAA051072 120050909A53151161107 FLOORBEAM AIRBUSA319 A319112 3930323EU FR 66 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19725UW 1135 CORROSION FLOORBEAM FR 66 -Y1500. INSTALLED DOUBLER PER SRM 53-41-14 REPAIR 6. DEFECT SIZE: 1.5 X .75 INCH. 2L72 4F RTA28NM 20050913000012005091300001 2005 9 13 YENA200560 420050902A23303088510101 ENTERTAIN SYS AIRBUS320 A320232 3930326EU CABIN ODOR A YENAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15552JB1013 1861 ELECTRICAL SMELL/ODOR DETECTED AT ROW 26DEF. FLIGHT ATTENDANTS VERIFIED LOCATION FROM UNDER SEAT. INSPECTED ROWS 24, 25, 26 ABC & DEF FOR ELECTRICAL ODOR IAW AMM 24-00-00-810-823 AND INFO NOTICE 2004-T023TR, NO ODORS NOTED. DEACTIVATED LTV SYS PER MEL 25-22-03. REF LOG PG 87601 - EU INTERFACE FOR WAU (WIRELESS AIRBORNE UNIT) DISPLAYED WAU POWER BAD ANTENNA STATE OVER CURRENT. REMOVED AND REPLACED WAU IAW AMM 23-39-00 AND OPERATIONS CHECK OK. REMOVED SEB AS PRECAUTIONARY. 2L72 4F RTA28NM 20050913000022005091300002NM 2005 9 13 BB05074 120050831A2750285T009913 MODULE BOEING767 767201 1385125NM TE FLAPS FAULTY A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19645US59602 23897 PHL FLT 564 EN-ROUTE PHL TO GLA - AFTER TAKE-OFF, FLAPS WOULD NOT RETRACT PAST 1 UNIT WITH THE FLAP HANDLE IN THE UP POSITION. EICAS STATUS MESSAGE, "FLAP/SLAT ELEC", WAS INDICATED. THE FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FLAPS AND STABILIZER POSITION MODULE. OPERATIONALLY CHECKS OK. 2L72 4F RTA1NM 20050913000032005091300003NM 2005 9 13 05FDEA02740 120050902A5340 FITTING BOEING727 727200 138407ENM BS 640 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 ONE HOLE BS 640 BUCKTAIL BEHIND INTERNAL FITTING BETWEEN STR 3L-4L. REPAIRED HOLE, BS 640 BETWEEN STR 3L & 4L PER FED-EX EA. 7-5330-9226A. 2L73 4F RTA3WE 20050913000052005091300005NM 2005 9 13 05FDEA02746 120050904A5330 SKIN BOEING727 727100 1384036NM BS 1166-1183 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25192FE 19085 EXTERNAL FUSELAGE SKIN HAS POPPED AND CRACKED FASTENERS ALONG STR 25 LEFT, BS 1166-1183. REPAIRED DAMAGED FUSELAGE SKIN BS 1166-1183 AT STR 25-STR 27 PER FED EX EA 7-5330-91350. 2L73 4F RTA3WE 20050913000062005091300006NM 2005 9 13 05FDEA02747 120050904A5230 ATTACH FITTING BOEING727 727200 138407ENM CARGO DOOR GOUGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25218FE 21101 GOUGE IN MAIN CARGO DOOR UPPER SKIN ATTACH FITTING, FITTING AT BODY STATION 640 JUST ABOVE STRINGER 2 LEFT. REMOVED AND REPLACED BS 640 ATTACH FITTING ABOVE STR 3 LT CARGO DOOR UPPER SILL PER EA 7-5330-92260A. 2L73 4F RTA3WE 20050913000082005091300008WP 2005 9 13 NACA20050020 120050909A2913PF17L391125ZE PUMP DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE HYD SYSTEM CRACKED A NACAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 AL036174C884 884 44075 P33192 NR 2 ENGINE HYDRAULIC FAILURE ON APPROACH. HAD TO USE EMERGENCY AIR BRAKE UPON LANDING. INSPECTED AND FOUND HYDRAULIC PUMP CASE CRACKED AND TOTAL HYDRAULIC FLUID LOSS. REPLACED NR 2 ENGINE HYDRAULIC PUMP. LEAK AND OP CHECKED GOOD. 2L74 4R4 R 6A3 5E8 20050913000092005091300009NM 2005 9 13 C1HA200581002 120050909A5311 FRAME BOEING727 7272S7 138407ZNM BS 804 CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15681CA 22020 CRACK ON FRAME AT BS 804 STR 15R. CUT OUT DAMAGED SECTION, FABBED NEW FILLER AND SPLICE ANGLE FROM 7075T6 .090 PO 294560 DIM FILLER 6.5" X 1" X 1" AND SPLICE 11.75 X 1 X 1, TREATED, PRIMED AND INSTALLED IAW 727 SRM 51-10-2 AND 51-40-3 FIG 1 RII ACCOMPLISHED. 2L73 4F A3WE 20050913000112005091300011EA 2005 9 13 REX200500114 120050908A215078279015 ACM CNDAIRCL600 CL6002B19 1900309EA RIGHT OVERHEATED A REXAO OTHER MB OVER TEMP SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO258423C11002 7423 AT GATE SMOKE IN CABIN WITH RIGHT AIR CYCLE MACHINE (ACM) INDICATING HIGH TEMP. INVESTIGATED CAUSE DEFERRED RIGHT ACM PACK PER MEL. 2L72 4F RTA21EA 20050913000122005091300012WP 2005 9 13 05FDEA02787 120050905A3260 CONNECTOR DOUG MD10 MD1010F 3022112WP MLG LOOSE A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25357FE 46939 LANDING GEAR INDICATED UNSAFE ON BOTH THE CONFIG PAGE AND GEAR LIGHTS AFTER RETRACTION. RECYCLED IAW CFM PROCEDURE AND ALL INDICATIONS NORMAL. TOWER STATED GEAR "APPEARED" RETRACTED WHILE HAD UNSAFE INDICATIONS. REMOVED AND REPLACED LANDING GEAR CONTROL MECHANISM DURING REPLACEMENT OF THE LANDING GEAR CONTROL HANDLE AND MECH. IT WAS DISCOVERED SWITCH S1-431 CONNECTORS WERE VERY LOOSE AND SWITCH WAS REPLACED. JACKED AIRCRAFT. SWUNG ALL GEAR SEVERAL TIMES. ALL LIGHTS WORKED NORMAL. 2L73 4F RTA22WE 20050913000142005091300014NM 2005 9 13 05FDEA02791 120050907A5753 ATTACH FITTING DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 LT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. CORROSION REPAIR CARRIED OUT AS PER EA 1-5750-87631. 2L73 4F RTA22WE 20050913000152005091300015EA 2005 9 13 VTZA200500170 120050908A5346601R536066 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA RT ENGINE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27624BR 7211 RT ENGINE SUPPORT BEAM IS CRACKED IN LOWER WEB AT .75". 2L72 4F RTA21EA 20050913000162005091300016EA 2005 9 13 VTZA200500168 120050908A5210 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA BS 338 CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27624BR 7211 PAX DOOR INTERCOSTAL TOP RADIUS CRACKED AT 1" IN LENGTH AT DATUM FS 338. 2L72 4F RTA21EA 20050913000182005091300018EA 2005 9 13 VTZA200500172 120050908A5320S6830 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA BS 325-379 CORRODED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27624BR 7211 LBL 9 FLOOR SUPPORT HAS CORROSION AT FS 325 TO 379. 2L72 4F RTA21EA 20050913000192005091300019EA 2005 9 13 VTZA200500169 120050908A5310601R5211680 DOOR FRAME CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27624BR 7211 PAX DOOR FRAME TOP RADIUS CRACKED AT 1" IN LENGTH FORWARD OF DATUM 1 AT FS 338.90. 2L72 4F RTA21EA 20050913000202005091300020EA 2005 9 13 VTZA200500177 120050908A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA BS 280 CORRODED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27624BR 7211 FS 280 BETWEEN LBL 19.0 AND RBL 12.0 HAS LEVEL 2 CORROSION. 2L72 4F RTA21EA 20050913000212005091300021EA 2005 9 13 VTZA200500173 120050908A5320S6830 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA BS 325.5-333.5 CORRODED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27624BR 7211 LBL 27 FLOOR SUPPORT HAS CORROSION AT FS 325.5 AND 333.5. 2L72 4F RTA21EA 20050913000222005091300022EA 2005 9 13 VTZA200500174 120050908A5315601R35031239 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 621 CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27624BR 7211 LT FS 621 FLOOR SUPPORT IS CRACKED AT 1" IN ANGLE. 2L72 4F RTA21EA 20050913000242005091300024EA 2005 9 13 VTZA200500176 120050908A5315S6830 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 337 CORRODED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27624BR 7211 RBL 27 FLOORBEAM HAS CORROSION AT FS 337. 2L72 4F RTA21EA 20050913000282005091300028NM 2005 9 13 05FDEA02803 120050907A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 HORIZONTAL STAB RT BARREL NUT BORE NR 7 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 - EA 1-5510-87628 ATTACHMENT 7. CLASSIFIED AS MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20050913000302005091300030NM 2005 9 13 05FDEA02805 120050907A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 HORIZ STAB RT BARREL NUT BORE NR 13 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 6. MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20050913000312005091300031NM 2005 9 13 05FDEA02806 120050907A575365162082 ATTACH FITTING BOEING727 727227 1384078NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 RIGHT WING, NR 7 FLAP TRACK FWD ATTACH FITTING INBOARD FACE CORRODED (27X5709-02). REPAIRED PER E.A. 7-5710-91348. 2L73 4F A3WE 20050913000332005091300033NM 2005 9 13 05FDEA02808 120050907A5753 ATTACH FITTING DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 LT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87633. 2L73 4F RTA22WE 20050913000352005091300035NM 2005 9 13 05FDEA02793 120050907A5753 ATTACH FITTING DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 LT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. ORROSION REPAIR CARRIED OUT AS PER EA 1-5750-87631. 2L73 4F RTA22WE 20050913000362005091300036NM 2005 9 13 05FDEA02801 120050907A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 HORIZ STAB RT BARREL NUT BORE NR 3 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08. EA 1-5510-87628, ATTACHMENT 3. MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20050913000372005091300037NM 2005 9 13 05FDEA02814 120050908A5230 GUSSET BOEING727 7272S2F 1384O81NM FWD CARGO DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25211FE 22933 FWD CARGO DOOR AFT LOWER GUSSET IS CRACKED. REMOVED AND REPLACED GUSSET IAW SRM 51-30-2. 2L73 4F A3WE 20050913000382005091300038WP 2005 9 13 ABXA050214 120050822A57534912322505 STUD DOUG DC9 DC941 302207NWP FLAP HINGE BROKEN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23956AX 47620 RIGHT WING OUTBOARD FLAP HINGE, STA 333, INBOARD LOWER STUD BROKEN OFF. REMOVED AND REPLACED ALL 4 STUDS IAW JOB CARD 92410004 AND DC-9 SRM. 2L72 4F A6WE 20050913000402005091300040NM 2005 9 13 05FDEA02818 120050908A5744 HINGE DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 LT WING, I/B FLAP O/B HINGE (WING SIDE), PIVOT HOLE SPOT FACE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87635. 2L73 4F RTA22WE 20050913000452005091300045NM 2005 9 13 05FDEA02823 120050909A5313 LONGERON DOUG MD11 MD11 3023602NM BS 5-123 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 CENTER CARGO COMPT, RT STA 5-123 LONGERON SPLICE 45R FOUND CRACKED. SNRM N1594: CENTER CARGO COMPT. R/H STA 5-123 LONGERON 45R CRACK SPLICE REMOVED AND NEW SPLICE P/N FXA5A 7116-503 INSTALLED AS PER DRAWING A5A 7116 AND SRM 51-33-01 VOL.II. NEW SPLICE P/N FX A5A 7117-503 FABRICATED PER DRAWING A5A 7116. CLASSIFIED MINOR REPAIR PER GMM 6-2-100. 2L73 4F RTA22WE 20050913000482005091300048NM 2005 9 13 05FDEA02826 120050909A5220 RETAINER BOEING727 727233 138408ANM EMER EXIT DOOR CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25268FE 21674 CORROSION, RT FWD EMERG EXIT DOOR, PRESSURE SEAL RETAINER AND FASTENERS CORRODED AT LOWER SIDE OF DOOR. REPLACED WITH NEW RETAINER PER FED EX MM 52-21-112-4. 2L73 4F RTA3WE 20050913000502005091300050NM 2005 9 13 05FDEA02828 120050909A5322 SHEAR TIE BOEING727 727233 138408ANM BS 680 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25268FE 21674 FWD CARGO CORROSION FLOOR SHEAR TIE STA 680 LBL 4 TO RBL 4 WL 148. REPAIRED PER SRM 53-10-4. 2L73 4F RTA3WE 20050913000512005091300051NM 2005 9 13 UPS05445379 120050825A531265B100056 BULKHEAD BOEING747 747212B 1384886NM RT MLG WW CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01526UP 21937 INSPECTION TYPE:C L/G - RBLG W/W STA 1480 BULKHEAD FWD FACE FOUND SURFACE CORROSION AROUND L/G RETRACT ACTUATOR UPPER MOUNT AREA. BS 1480 BULKHEAD CORRODED. TIME LIMITED REPAIR AT RBL 85 WL 156 AREA AS PER H HX RS R53-43-35364 AND UPS EO B747-5310-22826-A. BOEING RECOMMEND PERFORMING THE CPC TASK C53-125-01 MORE FREQUENTLY TO REDUCE CORROSION TO LEVEL 1. BOEING WILL PROVIDE THE STATUS IN 12 MONTHS AFTER COMPLETION OF THE DAMAGE TOLERANCE ANALYSIS. 2L74 4F A20WE 20050913000532005091300053NM 2005 9 13 UPS05545375 120050826A5320 FLOOR SUPPORT BOEING757 75724APF 1384969NM STA 320 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01403UP 23725 INSPECTION TYPE:C BS 320 FIVE INCHES I/B OF CREW ENTRY DOOR FRAME CORROSION ON LWR SIDE OF FLOOR SUPPORT STRUCTURE AROUND NUT PLATES. REPLACED THE PART IAW SRM 51-40-05. 2L72 4F RTA2NM 20050913000552005091300055NM 2005 9 13 UPS05645401 120050910A2410 GENERATOR BOEING767 76734AF 1385212NM RT DISCONNECTED A IPXAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 SO01315UP 27743 INSPECTION TYPE: ETOP ATB - DUE RT GEN DRIVE MSG DISPLAYED ON T/O AT 100 KTS. ONE ELEC SOURCE REMAINING. FOUND RT GEN DISCONNECTED AND OIL LEVEL LOW AND FILL UNION LOOSE. RECONNECTED IDG IAW 24-11-01. TIGHTENED FILL UNION AND SERVICED IDG IAW 12-13-03-3 ENG RUN CARRIED OUT SYS NOW SATIS AND NO LEAKS FOUND. 2L72 4F RTA1NM 20050913000572005091300057WP 2005 9 13 UPS05845380 120050705A5312 PRESSURE PANEL DOUG DC8 DC873F 302199FWP BS 979 LBL 40 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 INSPECTION TYPE:C1 LEFT W/W SKIN HEAVILY CORRODED INSIDE HAT CHANNEL STA 979 LBL 40. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW UPS EO DC8-5310 -22753-A AND SAA SK 809-850352. 2L74 4F RT4A25 20050913000582005091300058WP 2005 9 13 UPS05845381 120050727A53204651908 FITTING DOUG DC8 DC873F 302199FWP STA 310 L18L CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 INSPECTION TYPE: C1, MAIN CABIN LONGERON SPLICE FITTING HAS 4 INCH CRACK STA 310 L18L. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FITTING IAW SAA SK 809- 850545 AND UPS ENGINEERING FILE NUMBER DC8-53-20487. 2L74 4F RT4A25 20050913000602005091300060WP 2005 9 13 UPS05845384 120050812A5210 PAN DOUG DC8 DC871F 302199DWP L1-DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 INSPECTION TYPE:C1 L1 DOOR LWR AFT CORNER JAMB INSIDE WEB CRACKED 2 INCHES LONG. REMOVED DOOR JAMB AND WEB CUT OUT DAMAGED AREA IAW DWG 5597646, FABRICATED DOUBLER AND SPLICE AND INSTALLED REPAIR PARTS IAW DWG 5597646. 2L74 4F RT4A25 20050908000822005090800082NM 2005 9 8 05FDEA02733 120050902A5312 BULKHEAD DOUG MD11 MD11 3023602NM MLG WW CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 CENTER WHEEL WELL LEFT FORWARD BULKHEAD SPOILER PUSHROD (MJ) FEED THROUGH CUTOUT REINFORCEMENT DOUBLER FOUND CRACKED. CTR WHEEL WELL LT FWD BULKHEAD SPOILER PUSH ROD (MJ) FEEDTHROUGH CUTOUT REINFORCEMENT DOUBLER REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II. OPERATION CHECK CARRIED OUT ON SPOILER SYSTEM FOUND 'SATIS' AS PER AMM 27-60-00-5. 2L73 4F RTA22WE 20050908000902005090800090EU 2005 9 8 08142005B 120050814A3240 BRAKE ASSY SAAB SF340 340B 7860101EU MLG LEAKING A NSVAO OTHER KJ FLUID LOSS WARNING INDICATION LDLANDING 1 EA27338CJ 338 LOSS OF HYDRAULIC POWER ON LANDING. REMOVED AND REPLACED NR 2 BRAKE AND BRAKE LINE. 2L72 4T RTA52EU 20050908000922005090800092EU 2005 9 8 08152005E 120050815A3230 HOUSING SAAB SF340 340B 7860101EU HAND PUMP BROKEN A NSVAK NONE O OTHER ININSP/MAINT 1 EA27338CJ 338 EMERGENCY PUMP HANDLE HOUSING BROKEN. REMOVED AND REPLACED PUMP HANDLE HOUSING, OPS CHECK GOOD. 2L72 4T RTA52EU 20050908000932005090800093NE 2005 9 8 08092005A 220050809A7200 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LEFT FLAMED OUT A NSVAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 EA27304CE 198 LEFT ENGINE HAD MOMENTARY FLAMEOUT IN FLIGHT AT FL210-11 DEGREES W/TRACE ICE, IGNITION KICKED IN RIGHT AWAY. PERFORMED ENGINE RUN AFTER LT ENGINE BORESCOPE TO VERY PROPER ENGINE PERFORMANCE. ALSO, PERFORMED ENGINE OVERSPEED TEST IAW COLGAN WORKCARD 73-20-01S, OPS CHECK GOOD. 2L72 4T4 TRTA52EU E8NE 20050908001022005090800102EU 2005 9 8 08242005A 120050824A2697 WIRE SAAB SF340 340B 7860101EU RT FIRE DETECTORBROKEN A NSVAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 EA27252CJ 252 RT ENGINE TAILPIPE HOTLIGHT ILLUMINATED. FOUND BROKEN WIRES, REPAIRED AND OPS CHECK GOOD. 2L72 4T RTA52EU 20050908001042005090800104EA 2005 9 8 HNAA0500081 120050903A2434 GENERATOR DHAV DHC8 DHC8311 1386006EA NR 1 MALFUNCTIONED A HNAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA07330EN 274 DC BUSS FAULT ILLUMINATED IN FLIGHT FOLLOWED BY NUMEROUS OTHER CAUTION LIGHTS, AUX INV RUDDER FULL PRESS, GPWS, PAX DOOR, BAG DOOR, FWD EXIT DOOR, SERVICE DOOR. REMOVED AND REPLACED NR 1 DC GENERATOR. 2H72 4T RTA13NM 20050908001112005090800111EA 2005 9 8 SWIA200515500 120050831A2720DL2428M9 ACTUATOR CNDAIRCL600 CL6002C10 1390015EA RUDDER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07730SK 10193 RUD LIMITER FAULT. REPLACED NR 1 RUDDER LIMITER ACTUATOR IAW CRJ MM 27-25-03. OPERATIONAL CHECK GOOD, PN DL2428M9, SNOFF 0534. 2L72 4F RTA21EA 20050908001142005090800114NM 2005 9 8 SB05105 120050901A323027326 CABLE BOEING737 7374B7 1384702NM RT MLG WW OUT OF ADJUST A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19432US 24554 AFTER TAKEOFF FROM CLT, CREW REPORTED MLG HANDLE WOULD NOT MOVE UP TO RETRACT THE GEAR. CREW LOWERED MLG HANDLE TO DOWN POSITION & RECEIVED A NORMAL GEAR INDICATION OF 3 GREEN LIGHTS. FLT RETURNED TO FIELD. DURING APPROACH, CREW REPORTED FLAPS WOULD NOT EXTEND BELOW 15 UNITS & AUTO BRAKES UNARMED LIGHT ILLUMINATED WHEN BRAKES SELECTED. FLT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY DECLARED. MX ADJUSTED GROUND INTERLOCK VALVE CABLE PER MM. CHECKED RESISTANCE OF S106 SENSOR AND ADJUSTED GAP OF SENSOR PER MM. CHECKS GOOD. VISUALLY INSPECTED ALL FLAP & FLAP DRIVE COMPONENTS FOR STRUCTURAL FAILURE OR FOD PER MM. NO DEFECTS NOTED. PERFORMED NORMAL FLAP OPERATIONAL CHECK PER MM. OPERATIONAL CHECK GOOD.2L72 4F RTA16WE 20050908001222005090800122NM 2005 9 8 UPS05245317 120050822A5313 STRINGER BOEING727 72722C 138400FNM BS 304-320 S22R CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01930UP 19096 AREA OF SUSPECT CORROSION BETWEEN SKIN AND INTERNAL STRUCTURE AT BS 295 STR22R. CORROSION FOUND TO BE ON STRINGER 22R BETWEEN BS 204-316. STRINGER SECTION REPLACED BETWEEN BS 304 AND 320 IAW SRM 53-10-3 FIG 1. 2L73 4F A3WE 20050908001272005090800127WP 2005 9 8 UPS05845326 120050828A5712 RIB DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 785.000. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2 -0 FIG 2. 2L74 4F RT4A25 20050908001292005090800129WP 2005 9 8 UPS05845328 120050828A5712 RIB DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 LEFT WING LE LOWER RIB IS CRACKED AT XFS 735.000. STOP DRILLED CRACKED, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57 -2-0 FIG 2. 2L74 4F RT4A25 20050908001342005090800134EU 2005 9 8 09012005A 120050831A2750 CONTROL SYSTEM SAAB SF340 340B 7860101EU TE FLAPS MALFUNCTIONED A NSVAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 EA27251CJ 251 FLAPS DIDN'T MOVE 1ST TIME 15 DEGREES SELECTED. PERFORMED OPERATIONAL CHECK OF FLAP SYSTEM. OP CHECKS GOOD. 2L72 4T RTA52EU 20050908001412005090800141NM 2005 9 8 2005UALA00892 120050826A5313 STRINGER BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE BS 294 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29913UA 25291 STR 10L UPR FLANGE IS CRACKED AT STA 294. 2L72 4F4 FRTA16WE E2GL 20050908001432005090800143NM 2005 9 8 2005UALA00894 120050826A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE STA 1480 DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29588UA 26717 FRAME DENTED AT STATION 1480 BTWN S25L AND S26L. TRIMMED OUT DAMAGES, ACP HEFC INSP, NO CRACK FOUND. FABRICATE, ALODINE, PRIME, AND INSTALL REPAIR PER TIMCO REO G10824, REV B. 2L72 4F4 FRTA2NM E17NE 20050908001472005090800147NM 2005 9 8 2005UALA00898 120050826A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE STA 1460 DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29588UA 26717 FRAME DENTED AT STA 1460 BETWEEN S25L AND S26L. TRIMMED OUT DAMAGES, ACP HEFC INSP, NO CRACK FOUND. FABRICATE, ALODINE, PRIME, AND INSTALL REPAIR PER TIMCO REO-G10825. 2L72 4F4 FRTA2NM E17NE 20050908001482005090800148NM 2005 9 8 2005UALA00899 120050826A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE STA 1500 STR 25DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29588UA 26717 FRAME DENTED AT STA 1500, STR 25L. TRIMMED OUT DAMAGE, ACP HEFC INSP, NO CRACK FOUND. FABRICATE, ALODINE, PRIME, AND INSTALL REPAIR PER TIMCO REO-G10823. 2L72 4F4 FRTA2NM E17NE 20050912000062005091200006EU 2005 9 12 SA05098 120050903A2410740119H IDG AIRBUSA319 A319112 3930323EU RT ENGINE LEAKING A USAAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CLCLIMB 1 EA19756US10072 1340 PHL - FLT 933 - EN ROUTE PHL TO FLL - SHORTLY AFTER TAKEOFF, THE NUMBER TWO IDG LOW OIL PRESSURE LIGHT BEGAN TO COME ON INTERMITTENTLY, CAUSING ECAM WARNINGS. THE NUMBER TWO IDG WAS DISCONNECTED PER ECAM INSTRUCTIONS. WITH THE APU GENERATOR ON MEL, THE FLIGHT RETURNED TO FIELD WITH ONE OPERATIONAL GENERATOR. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NUMBER TWO IDG AND THE APU GENERATOR. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20050912000162005091200016EA 2005 9 12 SWIA200515509 120050902A274183963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 NM07932SW5595 5595 7714 DURING INITIAL CLIMB-OUT, BOTH STAB TRIM CH'S KICKED OFFLINE, FOLLOWED IMMEDIATELY BY MACH TRIM. REPLACED HORIZONTAL STAB TRIM ACTUATOR AND MOTOR CONTROL UNIT PER CRJ 200 M/M 27-42-01; 27-42-05. OPERATIONAL CHECK GOOD, PN 7062-3; SN OFF 786. 2L72 4F RTA21EA 20050912000172005091200017EA 2005 9 12 SWIA200515510 120050902A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07464SW 7827 A SECTION OF EMERGENCY FLOOR LIGHTING INOP. REPLACED EMERGENCY FLOOR PATH LIGHTING POWER STRIP IAW CRJ MM 33-51-01. OPERATIONAL CHECK NORMAL. 2L72 4F RTA21EA 20050912000182005091200018EA 2005 9 12 SWIA200515511 120050829A27515913164 DETECTOR CNDAIRCL600 CL6002C10 1390015EA TE FLAPS MALFUNCTIONED A SWIAO OTHER N FALSE WARNING CLCLIMB 1 NM07746SK1014 1014 FLAPS HALFSPEED STATUS MESSAGE AFTER DEPARTING ORD. REPLACED LEFT OB FLAP, OB SENSOR IAW MM 27-52-45. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050912000272005091200027EA 2005 9 12 REXA200500110 120050904A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA WINGS FAILED A REXAO OTHER J WARNING INDICATION APAPPROACH 1 SO258918B 7918 FLAPS FAIL ON APPROACH. 2L72 4F RTA21EA 20050912000322005091200032EA 2005 9 12 COMA0560484 120050902A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A COMAO OTHER O OTHER NRNOT REPORTED 1 SO01965CA 7131 FLIGHT 5387 - EMERGENCY LIGHTS ROW 1-5 INOPERABLE. RESECURED LIGHT STRIP. 2L72 4F RTA21EA 20050912000332005091200033EA 2005 9 12 COMA0560485 120050902A2750 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01471CA 7655 FLIGHT 5549 - FLAPS FAIL CAUTION. RIGGED THE LEFT AND RIGHT FLAP BPSU TO M/M SPECIFICATIONS. 2L72 4F RTA21EA 20050912000342005091200034EA 2005 9 12 COMA0560486 120050903A5350 SEALANT CNDAIRCL600 CL6002B19 1900309EA FAIRING VIBRATION A COMAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO01489CA 7755 FLIGHT 5564 - UNUSUAL VIBRATION DURING CLIMB. REPLACED THE AERODYNAMIC SEALANT ON BELLY FAIRING. 2L72 4F RTA21EA 20050912000432005091200043NM 2005 9 12 SWAA052718 120050906A53106545829 CREASE BEAM BOEING737 7373H4 1384600NM BS 270-328 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 DURING SCHEDULED D-CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 270 TO BS 328. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM. 2L72 4F RTA16WE 20050912000482005091200048NM 2005 9 12 SWAA052723 120050906A53106545829 CREASE BEAM BOEING737 7373H4 1384600NM BS 294-390 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 DURING SCHEDULED D-CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 294-390. REPAIRED CREASE BEAM WEB PER SRM. 2L72 4F RTA16WE 20050912000532005091200053NM 2005 9 12 SWAA052728 120050906A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM BS 787 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, RBL 14. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050912000692005091200069NM 2005 9 12 SWAA052704 120050904A53156545410 FLOORBEAM BOEING737 7373H4 1384600NM BS 668 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29373SW 26581 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CRACKED AT BS 668, LBL 24.75. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20050912000702005091200070NM 2005 9 12 SWAA052705 120050906A3350D71702001 BATTERY PACK BOEING737 7373H4 1384600NM EMERGENCY LIGHT FAILED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29379SW 26586 DURING SCHEDULED RON CHECK, AFT GALLEY EMERGENCY EXIT LIGHTS BATTERY PACK FAILED TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050912000872005091200087NM 2005 9 12 P5CA0501390 120050902A2810 VALVE BOEING747 747123 1384873NM FUEL SYSTEM LEAKING A P5CAK NONE K FLUID LOSS ININSP/MAINT 1 EA15858FT 20109 FUEL LEAKING OUT OF LEFT WING OUTBOARD FRONT SPAR. RESEATED POPPED VALVE ON LEFT SPAR. INSPECTED OK NO LEAKS, OPS OK PER MM 28-11-04. 2L74 4F A20WE 20050912000962005091200096CE 2005 9 12 DXTA200500953 120050905A2150 A/C PACK CESSNA500 560CESSNA 2076750CE FAILED E DXTAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 GL07375QS 5600375 STRONG BURNING SMELL IN THE COCKPIT AND NOTICED BY PAX IN THE AFT CABIN ON LANDING. ODOR LINGERED UNTIL SHUT DOWN. TROUBLESHOT DISCREPANCY TO INTERNAL FAILURE OF THE FREON AIR CONDITIONING FORWARD EVAPORATOR ASSEMBLY. INSPECTED LOCAL AREA, NO OTHER DISCREPANCY NOTED. DISABLED FREON AC SYSTEM PER MEL 21.18 CAT C. WORK PERFORMED IAW CHAPTER 21-52-01 OF 560MM. 2L72 4F RTA22CE 20050912001042005091200104EA 2005 9 12 COMA0560479 120050901A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01964CA 7129 FLIGHT 5874 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2L72 4F RTA21EA 20050912001082005091200108EA 2005 9 12 COMA0560481 120050901A2750855D10011 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS UNRELIABLE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01506CA6998 11 7793 FLIGHT 5224 - FLAPS FAIL CAUTION. REPLACED THE RT BPSU. 2L72 4F RTA21EA 20050912001142005091200114NM 2005 9 12 QXEA200501206 120050905A2420 GENERATOR DHAV DHC8 DHC8202 2809007NM NR 2 AC MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09348PH 484 PSC FLIGHT 2092 NR 2 AC GENERATOR LIGHT ILLUMINATED ON CLIMB, AS PER CHECKLIST, RESET AC GENERATOR. LIGHT WENT OUT. REMAINED OFF REMAINDER OF FLIGHT. MAINTENANCE INSPECTED ENGINE CONDITION PANEL, AIRCRAFT GENERATOR CHIP DETECTION LIGHT, NO FLAGS NOTED. PERFORMED OPERATIONAL CHECK OF AIRCRAFT GENERATORS IAW AMM SUBTASK 24-21-00-720-001, OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050912001192005091200119NM 2005 9 12 QXEA200501209 120050903A2430 GENERATOR DHAV DHC8 DHC8202 2809007NM NR 1 MALFUNCTIONED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09350PH 488 PDX FLIGHT 2139, NR 1 DC GENERATOR CAUTION LIGHT CYCLES ON/OFF. MAINTENANCE PERFORMED DC GENERATOR OPERATIONAL CHECK AND VISUAL INSPECTION OF NR 1 DC GENERATOR IAW AMM TASK 24-31-00-720-801. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050912001272005091200127NM 2005 9 12 QXEA200501216 120050907A36208209082 SWITCH BOMBDRDHC8 DHC8402 1390042NM BLEED AIR SYSTEMMALFUNCTIONED A QXEAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM09408QX 4050 SEA FLIGHT 2377, NR 2 BLEED HOT CAUTION LIGHT ILLUMINATED IN FLIGHT. NR 2 BLEED SWITCH WAS TURNED OFF PER CHECKLIST BUT THE CAUTION LIGHT STAYED ILLUMINATED FOR THE REST OF THE FLIGHT. MAINTENANCE REMOVED AND INSTALLED NR 2 BLEED OVER TEMPERATURE SWITCH IAW Q400 AMM TASK 36-11-16-000-801 FOR REMOVAL AND TASK 36-11-16-400-801 FOR INSTALLATION. OPS CHECK GOOD IAW Q400 AMM TASK 36-11-00-710-802. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050912001302005091200130SO 2005 9 12 637090205 120050902A29101159SCH5019 ACTUATOR VALVE GULSTMGV GULFSTREAMGV3980116SO HYD SYSTEM DEFECTIVE E N93AA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 SO13509QS4522 637 L-R AIL HYD OFF WARNING ACTIVATED IN FLIGHT, L - AIL CB POPPED ON GROUND. 2L72 4F RTA12EA 20050912001362005091200136NM 2005 9 12 0501416638 120050907A2612 CIRCUIT CARD BOEING747 747251B 1384892NM APU FIRE DETECT MALFUNCTIONED A NWAAO OTHER N FALSE WARNING CRCRUISE 1 GL01638US 23549 AFTER TOP OF CLIMB, APU B-FAULT ILLUMINATED ALONG WITH FIRE HANDLE AND FIRE WARNING. AFTER 2 HOURS INDICATION WAS NORMAL. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. LAX MAINTENANCE RESEATED APU FIRE DETECTION CARD AND CHECKED LOOPS. OPERATIONAL CHECK GOOD. 2L74 4F A20WE 20050912001472005091200147SO 2005 9 12 C2XA05SH109 120050901A491014526850401 FIREWALL EMB 145 EMB145 3260210SO APU BAY CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714959 145091 SHV - DURING C-CHECK, RT APU FIRWALL REINFORCED REGION O/B 3 O'CLOCK POSITION IS CRACK. MAINTENANCE REPAIRED RT APU FIREWALL REINFORCED REGION O/B 3 O'CLOCK POSITION IAW EMB 145 SRM 53-32-13. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2L72 4F RTT00011AT 20050912001522005091200152EU 2005 9 12 2005UALA00911 120050829A5230 MOUNT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CARGO DOOR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29405UA 452 AFT CARGO DOOR HANDLE MOUNT PLATE WHERE IT ATTACHES TO DOOR FRAME IS CRACKED. 2L72 4F4 FRTA28NM E40NE 20050912001642005091200164EA 2005 9 12 VNAA0508011 120050818A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A VNAAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL05218PS 7885 THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED ON APPROACH. THE CREW FOLLOWED THE QRH AND LANDED WITHOUT INCIDENT. MAINTENANCE CYCLED AIRCRAFT POWER. THE FLAP SYSTEM OPERATIONALLY CHECKED GOOD IAW CRJ200 AMM 27-54-00-710-801. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050912001772005091200177NM 2005 9 12 2005UALA00925 120050901A335020131A POWER SUPPLY BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE ROW 14 INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29937UA 26668 THE FOLLOWING EMERGENCY LIGHTS ARE INOP: EEL LIGHTS AFT OF ROW 14, SLIDE LIGHT DOOR 2L. EXIT SIGN DOOR 2R, AFT ENTRY EXIT SIGN, AISLE LIGHT ROW 17. REPLACED POWER SUPPLY AND BATTERY. 2L72 4F4 FRTA16WE E2GL 20050912001782005091200178NM 2005 9 12 2005UALA00926 120050901A5210 BEAM BOEING747 747422 1384935NM PWA 4056 PW4056 NE PAX DOOR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29119UA 28812 NR 2 LT MAIN ENTRY DOOR UPPER GATE CLOSURE BEAM ATTACH HOLE CRACKED. CLOSURE BEAM PROBABLY CRACKED DUE TO FATIGUE. INSTALLED ANGLE DOUBLER REF SM 80-52-10-05-JD AND SRM 51-70-11. WORK ACPD AT DOOR OVERHAUL SHOP BY MECHANIC PARK, HYUN JOON 8004850 AND INSP KIM, KAL 122L. 2L74 4F4 FRTA20WE E24NE 20050912001792005091200179EU 2005 9 12 2005UALA00927 120050817A5320 FLOOR SUPPORT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FRAME 66-70 CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29429UA 539 AFT GALLEY FLOOR SUPPORT 66-70 CORRODED. AMIS STATUS SHOWS THAT THE FLOOR SUPPORT WAS REPAIRED. REPAIRED OR REPLACED FLOOR SUPPORT IN ACCORDANCE WITH THE SRM. 2L72 4F4 FRTA28NM E40NE 20050912001802005091200180WP 2005 9 12 UPS05845353 120050902A383017200382 MOTOR DOUG DC8 DC873F 302199FWP CABIN OVERHEATED A IPXAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO01818UP 46108 LAV FLUSH MOTOR OVERHEATED CAUSING SMOKE IN CABIN. REMOVED AND REPLACED LAV TIMER AND FLUSH MOTOR PER MM 20-10-03, 20-16-00-2. OPS CK NORMAL PER MM 38-30-00-1. NO LEAKS NOTED. 2L74 4F RT4A25 20050912001812005091200181WP 2005 9 12 0501379947 120050810A5240 SKIN DOUG DC9 DC931 3022065WP SERVICE DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018938E 47161 DURING L-CHECK FOUND CRACK IN FUSELAGE SKIN AT FORWARD SERVICE DOOR FRAME LOWER AFT CORNER. REPAIRED PER EA 99-204703. 2L72 4F A6WE 20050912001912005091200191NM 2005 9 12 CALA0500293 120050901A5320141A54103 WEB BOEING737 737824 13844BZNM STA 282 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712218 28778 INSPECTION FOUND TWO 1 INCH CRACKS IN WEB AT STA 282, RBL 10. THE WEB WAS REMOVED AND REPLACED IAW GMM 10-90-00 AND SRM 51-40-02. 2L72 4F RTA16WE 20050912002042005091200204NM 2005 9 12 SWAA052672 120050902A29106544548 LINE BOEING737 7373H4 1384600NM HYD SYSTEM LEAKING A SWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW29332SW 23696 DIVERSION, LOST A-SYSTEM HYDRAULIC PRESSURE & FLUID. REMOVED AND REPLACED A-SYSTEM HYDRAULIC HEAT EXCHANGER LINE & HYDRAULIC CASE DRAIN FILTER PER MM. 2L72 4F RTA16WE 20050912002182005091200218EU 2005 9 12 MALA050704 120050903A5740 TAB BAC 146 AVRO146RJ85A1500097EU TE FLAP CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15507XJ E2316 WHILE ACCOMPLISHING C1. IG1 INSPECTION FOUND LEFT INBOARD FLAP TAB HAS CHAFING MARKS AT ITS MIDDLE ATTACH POINT. 2H74 4F RTA49EU 20050912002212005091200221EU 2005 9 12 MALA050701 120050903A5753 TAB BAC 146 AVRO146RJ85A1500097EU TE FLAP CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15507XJ E2316 WHILE ACCOMPLISHING C3.IG1 INSPECTION FOUND LEFT INBOARD FLAP TAB HAS SEVERAL CHAFING MARKS AT INBOARD ATTACH POINT. 2H74 4F RTA49EU 20050912002462005091200246EA 2005 9 12 SWIA200515515 120050903A2750860D10018 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION LDLANDING 1 NM07917SW6420 6420 7641 AFTER LANDING IN DEN, RECEIVED FLAPS FAIL CAUTION MESSAGE AT FLAPS 20 DEGREES. INSTALLED SERVICEABLE FECU IAW MM 27-51-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050912002522005091200252NM 2005 9 12 USAA051068 120050908A57536546435366A SKIN BOEING737 7374B7 1384702NM TE FLAP DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 UPPER SKIN OF FLAP T/E WEDGE DELAMINATED. REMOVED PREVIOUS REPAIR AND FABRICATED AND INSTALLED NEW REPAIR IAW SRM 51-70-10. DEFECT SIZE: 2 INCH DIAMETER DELAMINATION. 2L72 4F RTA16WE 20050912002592005091200259EU 2005 9 12 AWXA200501032 120050908A335032145410 POWER SUPPLY AIRBUS320 A320231 3930325EU EMERGENCY LIGHT INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28627AW2234318240 66 PHX - EEL - DURING 8-DAY CHECK DISCOVERED, THE LT OVERWING ESCAPE PATH LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT OVERWING EMERGENCY LIGHT POWER SUPPLY IAW AIRBUS 319/320 MM 33-51-38-04. OPERATIONAL CHECKS GOOD. 2L72 4F RTA28NM 20050912002602005091200260EU 2005 9 12 AWXA200501033 120050908A335032145410 POWER SUPPLY AIRBUS320 A320231 3930325EU EMERGENCY LIGHT INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28620AW1634411116 052 PHX - EEL - DURING 8-DAY CHECK DISCOVERED, THE LT AFT EMERGENCY LIGHTING POWER SUPPLY INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT POWER SUPPLY. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA28NM 20050912002632005091200263NM 2005 9 12 AWXA200501036 120050825A575465C26601170 STRUCTURE BOEING737 7373Y0 1384671NM ZONE 500 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 DURING C16 CHECK DISCOVERED, 2 CRACKS, .375 INCHES IN LENGTH, LOCATED ON THE BOTTOM OF THE NR 1 SLAT SKIN BELOW OUTBOARD MAIN TRACK. MAINTENANCE REMOVED CRACKS FROM NR 1 SLAT SKIN IAW BOEING 737-300 SRM 57-43-01-2. FABRICATED FILLER AND SPLICE PLATE IAW BOEING 737-300 SRM 57-43-01-2. INSTALLED FABRICATED REPAIR PARTS AT THE BOTTOM OF THE NR 1 SLAT, BELOW OUTBOARD MAIN TRACK IAW BOEING 737-300 SRM 57-43-01-2. 2L72 4F RTA16WE 20050912002722005091200272EU 2005 9 12 USAA051073 120050909A5315D5347217220500 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19730US 1182 CORROSION FLOORBEAM -Y1292 AT FRAME 66. REMOVED & REPLACED BEAM PER SRM 53-41-14, DEFECT SIZE: 2 X 3 INCH. 2L72 4F RTA28NM 20050913000172005091300017EA 2005 9 13 VTZA200500171 120050908A5320601R35031239 ANGLE CNDAIRCL600 CL6002B19 1900309EA BS 621 CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27624BR 7211 RT FS 621 FLOOR SUPPORT IS CRACKED AT 1" IN ANGLE. 2L72 4F RTA21EA 20050913000252005091300025NM 2005 9 13 05FDEA02797 120050907A5753 ATTACH FITTING DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 LT WING, O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87631. 2L73 4F RTA22WE 20050913000262005091300026NM 2005 9 13 05FDEA02798 120050907A5753 ATTACH FITTING DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 LT WING, O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87631. 2L73 4F RTA22WE 20050913000272005091300027NM 2005 9 13 05FDEA02802 120050907A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 HORIZ STAB RT BARREL NUT BORE NR 5 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 - EA 1-5510-87628 ATTACHMENT 4. CLASSIFIED AS MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20050913000322005091300032NM 2005 9 13 05FDEA02807 120050907A5330 SKIN BOEING727 727223 1384074NM BS 1269 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25268FE 21674 48 SECTION, EXTERNAL SKIN IS GOUGED, 1 INCH BELOW STR 25R. REPAIRED PER SRM 53-30-3, 51-20-4 MINOR REPAIR. 2L73 4F A3WE 20050913000342005091300034NM 2005 9 13 05FDEA02792 120050907A5753 ATTACH FITTING DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 LT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87631. 2L73 4F RTA22WE 20050913000392005091300039NM 2005 9 13 05FDEA02817 120050908A5330 DOUBLER DOUG MD11 MD11 3023602NM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 FWD CABIN, ENTRY DOOR NR 1 RT UPPER EDGE FOUND EXISTING DOUBLER UPPER EDGE BENT AND SEPARATED FROM DOOR. FWD CABIN ENTRY DOOR 1 R/H UPPER EDGE SKIN REPAIRED AS PER SRM 52-10- 00 FIG.4 VOL.I SHT.1. CLASSIFIED MAJOR REPAIR PER GMM 6-2-100. 2L73 4F RTA22WE 20050913000422005091300042NM 2005 9 13 05FDEA02820 120050909A5313 LONGERON DOUG MD11 MD11 3023602NM BS 1641 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 CENTER CARGO COMPT, RT STA 1641 LONGERON 43R FOUND WITH HAIR LINE CRACK. REPAIRED AS PER SRM 53-10-00 FIG.2 VOL.I. CLASSIFIED MAJOR REPAIR PER GMM 6-2-100. 2L73 4F RTA22WE 20050913000462005091300046NM 2005 9 13 05FDEA02824 120050909A5310 SEAT TRACK DOUG MD11 MD11 3023602NM BS 1828-1829 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 AFT CABIN, STA 1828 TO 1829 RBL 107 FOUND SEAT TRACK CROWN WORN. SNRM N1611: AFT CABIN STA 1771 TO STA 1831 RBL 107 CROWN WORN SEAT TRACK REPAIRED AS PER SRM 53-70-00 FIG.1 VOL.I. CLASSIFIED MAJOR REPAIR PER GMM 6-2-100. 2L73 4F RTA22WE 20050913000632005091300063EA 2005 9 13 COMA0560491 120050907A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01941CA 7050 FLIGHT 5089- FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2L72 4F RTA21EA 20050913000642005091300064EA 2005 9 13 COMA0570101 120050907A5310CC670341755 CROSSBEAM CNDAIRCL600 CL6002C10 1390015EA FS 280 CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01355CA7805 10067 THE TRANSVERSE BEAM AT FS 280 IS CORRODED FROM LBL 36 TO RBL 36. THE CORRODED TRANSVERSE BEAM WAS REMOVED AND A NEW TRANSVERSE BEAM WAS INSTALLED IAW BOMBARDIER REO 670-53-11-047 REV C. 2L72 4F RTA21EA 20050913000652005091300065WP 2005 9 13 UPS05845391 120050825A5330 SKIN DOUG DC8 DC873F 302199FWP FS 1746 L15L CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE: C3, FUSELAGE SKIN CRACKED .5 INCH LONG AT FS 1746 L15L. REMOVED DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 53 -2-1. 2L74 4F RT4A25 20050913000732005091300073WP 2005 9 13 UPS05845399 120050902A52305894282502 FITTING DOUG DC8 DC873F 302199FWP CARGO DOOR FRAMECRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE:C3 C-PIT DOOR JAMB FITTING CRACKED I/B OF NR 6 T-BOLT FITTING AT FWD SI DE. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20050913000742005091300074WP 2005 9 13 UPS05845400 120050910A5313 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 LONGERON CORROSION BELLY 30, 31 & 34. LOG PAGES REFERENCED 442142/2,3 & 4441243 REMOVED 52 RIVETS/HI LOKS AT F.S. 70. STA 28R-30R TO VERIFY CORR PERFO RMED LOW FQY, VERIFY MATL LOSS 10-12 SO 05571 QC REF DC8-5330-22862 RE MOVE RIVETS F.S. 35. STA 30R TO VERIFY CORR PERFORMED LOW FQY NO LOSS AT TIME. REMOVE 17 RIVETS FS 25. STR 32R-35R VERIFY CORR, PERFORMED LOW FQY ON STAT 32-32 (R)NO LOS STAT 32-35 20 PERCENT PLUS STAT 35-35 10 PERCENT. 2L74 4F RT4A25 20050913000762005091300076EA 2005 9 13 COMA0560492 120050908A5210601R318723 SEAL CNDAIRCL600 CL6002B19 1900309EA PAX DOOR FOD A COMAA UNSCHED LANDING C F.O.D. CLCLIMB 1 SO01983CA 7169 FLIGHT 5154 - AIRCRAFT WILL NOT PRESSURIZE. AIR LEAK AT CABIN DOOR. REMOVED FOD FROM DOOR AND REPLACED DAMAGED DOOR SEAL. 2L72 4F RTA21EA 20050913000772005091300077NM 2005 9 13 SWAA052740 120050907A53306545774 SKIN BOEING737 7373H4 1384600NM BS 778 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 778, STR 20R. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050913000792005091300079NM 2005 9 13 SWAA052742 120050909A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 727E TO BS 747, STR 18R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050913000812005091300081NM 2005 9 13 SWAA052744 120050911A3350612825 BATTERY PACK BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29330SW 23694 DURING SCHEDULED SERVICE CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050913000822005091300082NM 2005 9 13 SWAA052745 120050907A53226546569 SHEAR TIE BOEING737 7373H4 1384600NM BS 947.5 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 947.5, BETWEEN STR 23L TO STR 24L. REPAIRED SHEAR TIE PER SWA EA. 2L72 4F RTA16WE 20050913000862005091300086NM 2005 9 13 SWAA052749 120050909A3350BR2013 LIGHT BOEING737 7377H4 1384404NM ROW 1 ABC LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29429WN 33658 EEPLS TRACK AT ROW 1 ABC LOOSE. SECURED TRACK PER MM. 2L72 4F RTA16WE 20050913000882005091300088NM 2005 9 13 SWAA052751 120050911A33506104781 BATTERY PACK BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29497WN 32479 DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050913000892005091300089GL 2005 9 13 CHQA200500158 220050908A7200 ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 2 FIRE A CHQAD RETURN TO BLOCK A FLAME/FIRE TXTAXI/GRND HDL 1 GL11267SK 145268 CAE312179 FLIGHT 3163 - BOS-ROC - UPON SHUTDOWN OF ENGINES AT ROC, RAMP PERSONNEL REPORTED THAT THE NR 2 ENGINE WAS ON FIRE. PASSENGERS DEPLANED IMMEDIATELY. THE FIRE WENT OUT BY ITSELF. DID NOT SEE THE FIRE BUT DID OBSERVE SMOKE COMING FROM THE AFT END OF THE AIRCRAFT. RAMP REPORTED THERE WAS A LARGE FIRE BALL OBSERVED. THERE WAS NO FIRE MESSAGE INSIDE THE AIRCRAFT. CONTRACT MAINTENENACE CAME ON SCENE AND DRY MOTORED AND THEN RAN THE ENGINE WITH CFR PRESENT. NO FIRE OBSERVED. NO DEFECTS FOUND. 2L72 4T4 FRTT00011ATTE6CH 20050913000902005091300090SO 2005 9 13 CHQA200500159 120050910A2913PV303211 PUMP EMB 145 EMB145LR 3260212SO HYD SYSTEM LEAKING A CHQAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL11971RP6650 6650 145426 FLIGHT 7835 - CMH-IAD - EN ROUTE FROM CMH TO IAD, RECEIVED HYD 1 LO QTY MESSAGE ON EICAS. LATER, RECEIVED E1 HYD PUMP FAIL AND HYD SYS 1 FAIL ALONG WITH ALL ASSOCIATED MESSAGES. COMPLIED WITH THE QRH AND INFORMED OF ATC OF THE MECHANICAL FAILURE AND DECLARED AN EMERGENCY DUE TO NR 1 HYD SYSTEM FAILURE. ON APPROACH, THE SYSTEM PARTIALLY RESTORED ITSELF AND A/C WAS ABLE TO EXTEND THE GEAR USING NORMAL MEANS. LANDING WAS UNEVENTFUL AND HAD NO PROBLEMS STEERING THE AIRCRAFT ON THE GROUND. REMOVED AND REPLACED NR 1 ENGINE DRIVEN HYDRAULIC PUMP. OPS AND LEAK CHECKS GOOD. 2L72 4T RTT00011AT 20050913000922005091300092SO 2005 9 13 CHQA200500161 120050912A335078241 INVERTER EMB 145 EMB145LR 3260212SO RT OVERWING INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11291SK 145486 RT OVERWING EXIT MARKER FAILED TO ILLUMINATE DURING OPS CHECK. REMOVED AND REPLACED INVERTER NR 5 IAW EMB 145 MM 33-50-11. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050913000932005091300093SO 2005 9 13 CHQA200500163 120050906A33501317 BULB EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT BURNED OUT A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11844RP 145620 LEFT HAND OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED OVERWING EMERGENCY LIGHT BULB IAW EMB 145 MM 33-50-07. OPS CHECK GOOD. 2L72 4F RTT00011AT 20050913000942005091300094SO 2005 9 13 CHQA200500164 120050906A33503025103 BULB EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT BURNED OUT A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11844RP 145620 RIGHT HAND OVERWING EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED THE RIGHT HAND OVERWING EMERGENCY LIGHT IAW EMB 134 MM 33-50-07. OPS CHECK GOOD. 2L72 4F RTT00011AT 20050913000952005091300095 2005 9 13 COMA0560493 420050910A3140601R5120411 LIGHT CNDAIRCL600 CL6002B19 1900309EA COCKPIT FAULTY A COMAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO01492CA 7763 FLIGHT 5177 - DURING TAKEOFF ROLL THE EICAS SCREENS WENT BLANK. REPLACED THE LIGHTING CONTROL PANEL. 2L72 4F RTA21EA 20050913000962005091300096NM 2005 9 13 05FDEA02783 120050906A77102045061 INDICATOR BOEING727 7272S2F 1384O81NM EPR MALFUNCTIONED A FDEAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO25208FE3516 1501 22930 WHILE ADVANCING THROTTLES FOR T/O, NR 3 EPR INDICATOR JUMPED UP TO FROZE AT "2.07" AND REMAINED THERE FOR 5 MIN AFTER RTO WITH NR 3 THROTTLE AT IDLE. RELEASED FOR SERVICE PER MEL/CDL: 77-01-01. NR 3 ENGINE EPR INDICATOR INOP. REMOVED AND REPLACED NR 3 ENG "EPR" IND PER AMM 77-11-002-2. RAN ENGINE PER JRH CHAP 5 OPS CK'S GOOD. 2L73 4F A3WE 20050913000972005091300097NM 2005 9 13 05FDEA02784 120050906A7710 INDICATOR BOEING727 7272S2F 1384O81NM EPR MALFUNCTIONED A FDEAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 SO25205FE 22927 REJECTED TAKEOFF UNDER 70 KNOTS DUE TO NO INDICATION ON NR 3 EPR GAUGE. COMPLIED WITH QRH AND MEL 77-01-01 NR 3 EPR INOP PROCEDURES. SUBSEQUENT TAKEOFF WAS UNEVENTFUL. PURGED MOISTURE FROM PT2 AND PT7 LINES TO NR 3 EPR TRANSMITTER WITH DRY NITROGEN AND RAN ENG'S NR 3 AND NR 2 ( NR 2 FOR COMPARISON). GROUND CHECKS NORMAL. NO 90 DAY HISTORY FOR THIS DISCREPANCY. OK TO CONTINUE. 2L73 4F A3WE 20050913000982005091300098NM 2005 9 13 SWAA052752 120050908A53116520723 FRAME BOEING737 7375H4 138449DNM FWD CARGO CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29503SW 24180 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR NR 5 STOP FITTING. REPAIRED FRAME PER BFG ER & SRM. 2L72 4F RTA16WE 20050913000992005091300099NM 2005 9 13 SWAA052753 120050909A5753 SKIN BOEING737 7375H4 138449DNM RT WING TE FLAPSDELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29525SW 26567 DURING SCHEDULED RON CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER SWA EA & SRM. 2L72 4F RTA16WE 20050913001022005091300102NM 2005 9 13 SWAA052756 120050908A53306545775 SKIN BOEING737 7373H4 1384600NM BS 787 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 787, RBL 10. REPAIRED SKIN PER BFG ER. 2L72 4F RTA16WE 20050913001032005091300103NM 2005 9 13 SWAA052757 120050908A53116520723 FRAME BOEING737 7373H4 1384600NM BS 494 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 494, FWD CARGO DOOR NR 5 STOP FITTING CUTOUT. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20050913001042005091300104 2005 9 13 SWAA052758 420050908A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 DURING SCHEDULED D-CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050913001062005091300106NM 2005 9 13 SWAA052760 120050909A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 1121 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29618WN 28034 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIPS CRACKED AT BS 1121, STR 2L & STR 2R. REMOVED AND REPLACED CLIPS PER SRM. 2L72 4F RTA16WE 20050913001072005091300107NM 2005 9 13 SWAA052761 120050908A53306545774 SKIN BOEING737 7373L9 1384470NM BS 727E CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29658SW 23332 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 24L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050913001082005091300108NM 2005 9 13 SWAA052762 120050909A3350612825 BATTERY PACK BOEING737 7373Y0 1384671NM ROW 5 DEF INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED SERVICE CHECK, FOUND SEVERAL CABIN EEPLS LIGHTS INOP BETWEEN FWD GALLEY & ROW 5 DEF. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050913001112005091300111NM 2005 9 13 SWAA052765 120050909A53206546805 FLOOR SUPPORT BOEING737 7377H4 1384404NM BS 771-773 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29786SW 29811 DURING SCHEDULED 5Y CHECK, FOUND FLOOR SUPPORT CORRODED BETWEEN BS 771 TO BS 773, LBL 3. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20050913001132005091300113NM 2005 9 13 SWAA052766 120050909A53206546805 FLOOR SUPPORT BOEING737 7377H4 1384404NM BS 771-773 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29786SW 29811 DURING SCHEDULED 5Y CHECK, FOUND LONGITUDINAL FLOOR SUPPORT CORRODED BETWEEN BS 771 TO BS 773, LBL 8. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20050913001142005091300114NM 2005 9 13 SWAA052767 120050909A53206546805 FLOOR SUPPORT BOEING737 7377H4 1384404NM BS 771-773 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29786SW 29811 DURING SCHEDULED 5Y CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED BETWEEN BS 771 TO BS 773, LBL 17. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20050913001152005091300115NM 2005 9 13 SWAA052768 120050909A53206546805 FLOOR SUPPORT BOEING737 7377H4 1384404NM BS 771-773 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29786SW 29811 DURING SCHEDULED 5Y CHECK, FOUND LONGITUDINAL FLOOR SUPPORT CORRODED BETWEEN BS 771 TO BS 773, RBL 8. REPAIRED FLOOR SUPPORT PER SWA EA. 2L72 4F RTA16WE 20050913001162005091300116NM 2005 9 13 SWAA052769 120050909A53206546805 FLOOR SUPPORT BOEING737 7377H4 1384404NM BS 771-773 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29786SW 29811 DURING SCHEDULED 5Y CHECK, FOUND LONGITUDINAL FLOOR SUPPORT CORRODED BETWEEN BS 771 TO BS 773, RBL 14. REPAIRED FLOOR SUPPORT PER SWA EA. 2L72 4F RTA16WE 20050913001192005091300119EA 2005 9 13 SWIA200515017 120050513A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07963SW 7865 LEFT OUTBOARD ATTACH CLIP AT FS 280.00 RBL IS CRACKED, ITEM FOUND AT C-CHECK INSPECTION. BRACKET REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21 AND 51-21-11. 2L72 4F RTA21EA 20050913001212005091300121EA 2005 9 13 SWIA200515019 120050513A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 621 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07963SW 7865 FLOORBEAM ANGLE AT FS 621.00 OUTBOARD IS CRACKED, ITEM FOUND AT C-CHECK INSPECTION. FLOOR SUPPORT ANGLE REPAIRED IAW CRJ REO 601R-53-61-117 REV "B". 2L72 4F RTA21EA 20050913001222005091300122SO 2005 9 13 SWIA200515524 120050906A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT DISCHARGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07564SW1141411414 120339 THREE EMERGENCY LIGHTS DO NOT TEST. REPLACED FORWARD EMERGENCY LIGHT BATTERY PACK IAW 73-00-00. OPERATIONAL CHECK GOOD, P/N: D366-04-001, S/N ON: 1139 S/N OFF: 1130. 2L72 4T RTA31SO 20050913001272005091300127NM 2005 9 13 05FDEA02796 120050907A5753 ATTACH FITTING DOUG MD11 MD11 3023602NM TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 LT WING, O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87631. 2L73 4F RTA22WE 20050913001292005091300129NM 2005 9 13 05FDEA02794 120050907A5753 ATTACH FITTING DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 LT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87631. 2L73 4F RTA22WE 20050913001322005091300132NM 2005 9 13 UPS05M45362 120050718A5347S4929147 SEAT TRACK DOUG MD11 MD11F 3023600NM BS 1341-1381 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01256UP 48405 INSPECTION TYPE:C CABIN SEAT TRACK BETWEEN STA 1341-1381 RBL =75.5 FOUND CORRODED. CORROSION REMOVED & FOUND BEYOND LIMIT PER SRM 53-70-00 V1.REV.37.REMAINED THK 0.040" & ORI THK 0.100".SEAT/T FASTENERS REMOVED FOR ACCESS & SPLICE CUT AT STA 1266 & 1391 PER SRM 53-70-00 F1.V1.R.37. REPAIR SPLICE & FAB PLATE PER 53-70-00 F1.V1R.37. NEW SEAT/T REPAIR SPICE HAT & SPLICE INSTALLED BETWEEN 1266 & 1391 PER SRM 5370-00F1V1 R37. 2L73 4F RTA22WE 20050913001332005091300133SO 2005 9 13 SWIA200515529 120050910A27203081401003 ACTUATOR EMB 120 EMB120ER 3260203SO RUDDER MALFUNCTIONED A SWIAC ABORTED TAKEOFF FJ FLT CONT AFFECTED WARNING INDICATION TOTAKEOFF 1 NM07583SW5693 5693 120351 RT RUDDER JAMMED ON TAKEOFF. REPLACED BLUE SYSTEM ACTUATOR IAW MM 27-22-02. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050913001352005091300135EA 2005 9 13 SWIA200515531 120050909A274170608 TRIM SYSTEM CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07720SW1057610576 7297 STAB TRIM CHANNEL 1 OCCASIONALLY WILL NOT ENGAGE. REPLACED HSTCU IAW MM 27-41-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050913001362005091300136EA 2005 9 13 SWIA200515532 120050907A2741 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07407SW 7034 F/O SIDE STAB TRIM WILL NOT TRIM NOSE DOWN. REPLACED FO'S PITCH TRIM SWITCH IAW MM 27-41-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050913001402005091300140EA 2005 9 13 SWIA200515536 120050905A2751 DETECTOR CNDAIRCL600 CL6002C10 1390015EA LE SLATS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07712SK 10172 "SLAT FAULT" STATUS MSG AT GATE. REPLACED LEFT OUTBOARD SLAT SKEW DETECTOR. OPERATIONAL CHECK GOOD IAW MM 27-51-00. 2L72 4F RTA21EA 20050913001592005091300159NM 2005 9 13 05FDEA02816 120050908A5744 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 RT WING, I/B FLAP O/B HINGE (WING SIDE), PIVOT HOLE SPOT FACE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87636. 2L73 4F RTA22WE 20050913001612005091300161NM 2005 9 13 05FDEA02811 120050908A5230 WEB BOEING727 727233 138408ANM CARGO DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25268FE 21674 LOWER CARGO DOOR INNER WEB IS CRACKED 3 INCHES FROM FWD SIDE AFT AND 11 INCHES FROM BOTTOM UP. REPAIRED PER SRM 51-40-2, MINOR REPAIR. 2L73 4F RTA3WE 20050913001622005091300162NM 2005 9 13 05FDEA02833 120050910A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 HORIZ STAB RT BARREL NUT BORE NR 23 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 9. MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20050913001642005091300164NM 2005 9 13 05FDEA02836 120050912A5753 ATTACH FITTING DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 RT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. REPAIR CARRRIED OUT AS PER EA 1-5750-87634. 2L73 4F RTA22WE 20050913001672005091300167EU 2005 9 13 SF20050905 120050905A3230 WARNING LIGHT SAAB SF340 SF340A 7850100EU MLG ILLUMINATED A UHLAO OTHER J WARNING INDICATION LDLANDING 1 GL1735SZ 035 FLIGHT 7539 IAD-DAY, LANDING GEAR SELECTED DOWN WITH NO GREEN LIGHT INDICATION ON NOSE WHEEL. LANDING GEAR WAS CYCLED AS PER QRH AND LIGHT REMAINED OUT. NOSE GEAR LIGHT THEN CAME ON WHILE IN HOLDING PATTERN. 2L72 4T RTA52EU 20050913001682005091300168EU 2005 9 13 USAA051074 120050909A5310D5347218820400 BEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19730US 1182 CORROSION BETWEEN FR 66 & 69 Y1292. REMOVED & REPLACED BEAMS PER SRM 57-72-11, DEFECT SIZE: 2 X 2, 1.5 X 2, 3 X 2 INCH. 2L72 4F RTA28NM 20050913001732005091300173NM 2005 9 13 USAA051080 120050909A574065C2630025 SUPPORT ANGLE BOEING737 7374B7 1384702NM RT WING CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19776AU 24934 RT WING T/E SUPPORT ANGLE, JUST INBOARD OF NR 6 SPOILER CRACKED. NEW PART SUPPORT ANGLE INSTALLED PER SRM 57-53-71 & 51-40-02, DEFECT SIZE: 0.050 INCH. 2L72 4F RTA16WE 20050914000022005091400002NM 2005 9 14 MASA200500687 120050830A21507506594 SWITCH DHAV DHC8 DHC8202 2809007NM A/C PACK MALFUNCTIONED A MASAO OTHER MJ OVER TEMP WARNING INDICATION NRNOT REPORTED 1 SW07446YV8881 446 ASH 7056 DEN. AIR CONDITIONING PACK HOT LIGHT ILLUMINATED IN FLIGHT. R2 OVERTEMP SWITCH. 2H72 4T RTA13NM 20050914000042005091400004WP 2005 9 14 ABXA050213 120050821A532039258121 FLOOR SUPPORT DOUG DC9 DC941 302207NWP BS 718 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23960AX 47762 LEFT VERTICAL FLOOR SUPPORT CRACKED AT FS 718, LEFT BUTT LINE 44. REMOVED AND REPLACED FITTING IAW DC-9 SRM 51-30-2, 51-30-5 AND 51-30-1. 2L72 4F A6WE 20050914000052005091400005NE 2005 9 14 QXEA200501194 220050829A7200 ENGINE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE NR 1 OVERTEMP A QXEAC ABORTED TAKEOFF MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 NM09611QX6741 10041 GEE965279 DEN- ON FLIGHT 4308 DURING TAKEOFF ROLL, NR 1 ENGINE TEMPERATURE INDICATED 939C AND IN THE RED. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO THE GATE. MAINTENANCE IN DENVER FOUND TEMP EXCEEDANCE TO BE 7.3 SECONDS. PERFORMED A POWER ASSURANCE RUN, ENGINE FAILED. OPERATING AT 938-940C WHEN THE LIMIT IS 900C. AIRCRAFT FERRIED TO PORTLAND, WHERE THE NR 1 ENGINE WAS CHANGED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050914000062005091400006NM 2005 9 14 QXEA200501222 120050909A2510 MECHANISM BOMBDRDHC8 DHC8402 1390042NM SHOULDER BELT LACK OF LUBE A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09412QX 4059 SEA FLIGHT NR 2374: CAPTAIN'S SHOULDER HARNESS DOES NOT MOVE. RETURN TO GATE. MAINTENANCE CLEANED AND LUBED HARNESS SPRING MECHANISM SEATBELT ON CAPTAIN'S SEAT. OPERATES NORMALLY. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050914000082005091400008WP 2005 9 14 ABXA050217 120050909A2130 CONTROL SYSTEM DOUG DC9 DC941 302207NWP CABIN PRESSURE FAILED A ABXAG O2 MASK DEPLOYED J WARNING INDICATION DEDESCENT 1 GL23969AX 47464 RAPID DECOMPRESSION AT TOP OF DESCENT WHEN POWER LEVERS RETARDED. UNRECOVERABLE IN MANUAL, POWER LEVELED AT IDLE, OXYGEN USED. PERFORMED PAR 3, DC-9 MM 21-31-09-2, ADJUST/TEST SINGLE ENGINE SECOND SEGMENT CLIMB SWITCHES. OPS CHECKED GOOD. 2L72 4F A6WE 20050912000762005091200076NM 2005 9 12 SWAA052711 120050906A53106547978 CREASE BEAM BOEING737 7373H4 1384600NM BS 616 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 616, RBL 65. REPAIRED CREASE BEAM WEB PER SRM. 2L72 4F RTA16WE 20050912000812005091200081NM 2005 9 12 SWAA052716 120050906A53156545829 FLOORBEAM BOEING737 7373H4 1384600NM BS 328 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 DURING SCHEDULED D-CHECK, FOUND CABIN FLOORBEAM CORRODED AT BS 328, RBL 24. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20050912000942005091200094EA 2005 9 12 REXA200500109 120050902A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA MALFUNCTIONED A REXAO OTHER J WARNING INDICATION APAPPROACH 1 SO258721B 7721 FLAP FAILURE AT 0 WHEN SELECTED DOWN ON APPROACH. 2L72 4F RTA21EA 20050912001092005091200109NE 2005 9 12 SWAA052737 220050905A7200CFM567B ENGINE BOEING737 7377H4 1384404NM CFMINTCFM567CFM567B22 13802NE LEFT FAILED A SWAAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION DEDESCENT 1 SW29211WN 34163 892190 INFLIGHT SHUTDOWN/DECLARED EMERGENCY. HEARD POP FROM NR 1 ENGINE WITH SLIGHT YAW. NR 1 ENGINE SPOOLED DOWN, DID NOT RESTART. REMOVED AND REPLACED NR 1 ENGINE PER MM. 2L72 4F4 FRTA16WE E00055EN 20050912001112005091200111NM 2005 9 12 SWAA052739 120050907A53156545808 FLOORBEAM BOEING737 7373H4 1384600NM BS 294.5 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 DURING SCHEDULED D-CHECK, FOUND CABIN FLOORBEAM UPPER CHORD CRACKED AT BS 294.5, LBL 53. REPAIRED FLOORBEAM UPPER CHORD PER SRM. 2L72 4F RTA16WE 20050912001222005091200122NM 2005 9 12 QXEA200501212 120050906A3310 BULB DHAV DHC8 DHC8202 2809007NM EMERGENCY LIGHT BURNED OUT A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09357PH 504 PDX FLIGHT 2238, NR 2 PROPELLER GROUND RANGE LIGHT NEED RELAMPING. MAINTENANCE REPLACEED BULBS. OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050912001232005091200123NM 2005 9 12 QXEA200501208 120050906A242031708001A GENERATOR DHAV DHC8 DHC8202 2809007NM NR 2 AC MALFUNCTIONED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09348PH* 207 484 SEA FLIGHT 2283 AFTER BRINGING PROPS OUT OF FEATHER AFTER PUSHBACK, RECEIVED THE NR 2 AC GENERATOR CAUTION LIGHT. MAINTENANCE REPLACED NR 2 ENGINE AC GENERATOR IAW Q200 AMM 24-21-00. PERFORMED GENERATOR FUNCTION CHECK. FUNCTIONAL CHECK GOOD. LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050912001262005091200126EA 2005 9 12 COMA0560483 120050902A291673031 RESERVOIR CNDAIRCL600 CL6002B19 1900309EA NR 3 HYD SYSTEM MALFUNCTIONED A COMAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO01960CA24086 7117 FLIGHT 5064 - GEAR DISAGREE WARNING. REPLACED THE NR 3 HYDRAULIC RESERVOIR. 2L72 4F RTA21EA 20050912001282005091200128WP 2005 9 12 ASMF200508016 120050829A532039546421 PLATE DOUG DC9 DC987 3022087WP CONTROL COLLUMN DAMAGED W ASMFC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 SW23755RA 49727 AIRCRAFT REJECTED TAKEOFF AT 60 KTS AND RETURNED TO PLATFORM AS A CONSEQUENCE RUDDER MOVEMENT TO THE RIGHT SIDE WAS VERY HARD, RIGHT PEDAL STOCKS FULLY INSIDE AND THE DIRECTION CONTROL WAS UNABLE WITH PEDALS. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT CHECK, THE CONTROL PEDESTAL COVER AND SPIRAL DRIVE PLATE WERE REPLACED IAW MM 27-20-07, ADJUSTMENT AND RUDDER HYDRAULIC POWER PACKAGE TEST WAS PERFORMED IAW MM 27-20-08, BEING CORRECT. 2L72 4F RTA6WE 20050912001292005091200129NM 2005 9 12 ASMF200508017 120050829A7400 IGNITION UNIT DOUG MD80 MD83 3023681NM RT ENGINE MALFUNCTIONED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23861LF 49826 DURING RIGHT ENGINE STARTED, THE IGNITION FAILED. ONCE THE ENGINE STOPPED TURN, A SECOND START WAS PERFORMED IAW 74-20-02, BEING CORRECT. DURING OVERNIGHT CHECK, THE CABLES, SPARK PLUGS AND IGNITION SYSTEM OF BOTH ENGINES WERE CHECKED IAW MM 74-10-02 AND MM 74-20-02 RESPECTIVELY, TESTED CORRECT. 2L72 4F RT 20050912001342005091200134NM 2005 9 12 0501406717 120050819A5311 FRAME BOEING747 747251F 1384898NM BS 400 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01617US 21121 DURING L-CHECK FOUND CORROSION ON FRAME LOWER CHORD AT BS 400 BETWEEN S40L AND S41L. REPAIRED PER EA 67-165239. 2L74 4F A20WE 20050912001372005091200137 2005 9 12 REXA200500112 420050908A2562 G SWITCH ARTEX CNDAIRCL600 CL6002B19 1900309EA ELT FAILED A REXAK NONE L NO TEST ININSP/MAINT 1 SO258969A2591 2591 07973 7969A ELT FAILS G-SWITCH TEST. REMOVED IN ACCORDANCE WITH PA 25-048D AND FAR 91.207 FOR REPAIR. UNIT MUST BE REPAIRED AND REINSTALLED WITHIN 90 DAYS. REMOVED ELT FOR MAINTENANCE IN ACCORDANCE WITH FAR 91-207. 2L72 4F RTA21EA 20050912001432005091200143WP 2005 9 12 UPS05845364 120050828A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE:C3 RIGHT WING L/E SKIN UPPER I/B OF XFS 710.000 HAS INTERGRANULAR CORROSION AND IS CRACKED. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1 FIG 38. 2L74 4F RT4A25 20050912001552005091200155NM 2005 9 12 2005UALA00914 120050829A5322 SHEAR TIE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE BS 807 DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29327UA 24147 EXTERNAL FUSELAGE STA 807 BETWEEN 28L AND 28R HAS A DENT AND SHEAR TIE BENT AT RADIUS. 2L72 4F4 FRTA16WE E2GL 20050912001592005091200159NE 2005 9 12 2005UALA00918 220050828A7297CTB9000 TERMINAL BLOCK BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE NR 1 ENGINE OVERHEATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29788UA 250 26942 NR 1 ENGINE UPPER IDG TERMINAL BLOCK HAS MELTED AREAS AND MISSING SHRINK WRAP ON WIRES. THE IDG STRUT DISCONNECT TERMINAL BLOCK INSPECTION/TORQUE CHECK ACCOMPLISHED AT THE SEGMENTED 'A' DISCOVERED THE OVERHEATED TERMINAL BLOCK. REVIEW OF IDG WRITE-UPS, LOGBOOK, AND MAINTENANCE MESSAGES PRIOR TO DISCREPANCY DID NOT INDICATE ABNORMAL IDG OPERATING CONDITIONS OR IN-SERVICE DIFFICULTIES. PHASE 'B' INITIALLY OVERHEATED POSSIBLY DUE TO IMPROPER TORQUE CAUSING THE CABLE LUGS TO LOOSEN AND OVERHEAT WITH HIGH RESISTANCE. 2L72 4F4 FRTT0001SE E46NE 20050912001722005091200172EA 2005 9 12 SWIA200515492 120050505A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 409+128 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07423SW 7456 FUSELAGE VERTICAL BEAM IS CRACKED AT BOTTOM FLANGE, FS 409.00 + 128; RBL - 18.0; O/B SIDE, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-41-056 REV "C". 2L72 4F RTA21EA 20050912001942005091200194NM 2005 9 12 CALA0500296 120050903A5320147A56603 INTERCOSTAL BOEING737 737824 13844BZNM BS 947.5-967 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712218 28778 INSPECTION FOUND INTERCOSTAL CORRODED BETWEEN STA 947.5 AND 967, LBL 25 (AT AFT FLOORBOARD ATTACHMENT HOLE). THE INTERCOSTAL WAS REPAIRED IAW ECRA 5321-01285. 2L72 4F RTA16WE 20050912001962005091200196NM 2005 9 12 MWEA050103 120050905A3350 BATTERY PACK BOEING717 717200 1383700NM EMERGENCY LIGHT INOPERATIVE A MWEAK NONE O OTHER ININSP/MAINT 1 GL31909ME 55173 BOTH OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED OVERWING BATTERY PACK. 2L72 4F TRA6WE 20050912002002005091200200 2005 9 12 SWAA052668 420050903A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED RON CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050912002012005091200201NM 2005 9 12 SWAA052669 120050903A3350D71702001 BATTERY PACK BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK HOUSING & CHARGER PER MM. 2L72 4F RTA16WE 20050912002022005091200202NM 2005 9 12 SWAA052670 120050905A3350D71702001 BATTERY PACK BOEING737 7373H4 1384600NM EMERGENCY LIGHT FAILED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29326SW 23690 DURING SCHEDULED RON CHECK, AFT GALLEY EMERGENCY EXIT LIGHTS BATTERY PACK FAILED TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050912002032005091200203NM 2005 9 12 SWAA052671 120050901A53306545775 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29327SW 23691 DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 801 TO BS 805, STR 17L. MX FERRY TO PHX FOR REPAIRS. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050912002172005091200217EU 2005 9 12 MALA050698 120050903A5320 GUSSET BAC 146 AVRO146RJ85A1500097EU FR 41-43 CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15507XJ E2316 WHILE ACCOMPLISHING C2 INSPECTION FOUND CORROSION ON FLOORBEAM INTERCOSTAL GUSSET PLATE BETWEEN FRAMES 41 AND 43, 18 INCHES INBOARD OF RIGHT AFT SERVICE DOOR SILL AT FRAME 43. 2H74 4F RTA49EU 20050912002482005091200248SO 2005 9 12 SWIA200515517 120050905A3350 LIGHT EMB 120 EMB120ER 3260203SO CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07227SW 120304 ONE FLOOR TRACK LIGHT INOP. REPLACED FLOOR TRACK LIGHT ASSY. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050912002532005091200253EA 2005 9 12 SWIA200515520 120050906A3411 PITOT TUBE CNDAIRCL600 CL6002B19 1900309EA OBSTRUCTED A SWIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM07408SW 7055 STALL FAIL, CAUTION MSG AFTER TAKEOFF RETURN TO SLC. REMOVED CONTAMINATION FROM CAPT PITOT TUBE. PURGED PITOT PROBE OF CONTAMINATION. OPERATIONAL CHECK GOOD IAW MM 27-35-05; 27-35-01 AND 34-11-00. 2L72 4F RTA21EA 20050912002542005091200254SO 2005 9 12 SWIA200515521 120050904A213032144143 PRESSURE VALVE EMB 120 EMB120ER 3260203SO LT A/C PACK MALFUNCTIONED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM07223SW4212 4212 120291 LEFT PACK FAIL AND DUCT LEAK MSG, AND COCKPIT FILLED WITH SMOKE. INSTALLED PRESSURE REGULATOR SHUT OFF VALVE, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050912002662005091200266NM 2005 9 12 AWXA200501039 120050823A53306548240504 SKIN BOEING737 7373Y0 1384671NM BS 1140-1156 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 DURING C16 CHECK DISCOVERED SKIN CRACKED BELOW LOWER AFT RT HORIZONTAL STAB ATTACH FITTING FROM BS 1140 TO BS 1156, WL 274, BL 22R. MAINTENANCE REMOVED DAMAGE SKIN FROM RT HORIZONTAL STAB IAW BOEING 737-300 SRM 51-40-02-0. FABRICATED REPLACEMENT SKIN IAW BOEING DWG PL 65-48240. INSTALLED FABRICATED SKIN ON AFT RT HORIZONTAL STAB FROM BS 1140 TO BS 1156, WL 274, BL 22R IAW BOEING 737-300 SRM 51-40-02-0. 2L72 4F RTA16WE 20050912002692005091200269NM 2005 9 12 USAA051070 120050909A5410311N50232 FITTING BOEING757 7572B7 1384964NM NR 2 PYLON GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19628AU 27806 NR 2 PYLON UPPER SPAR, AFT HOLE, OUTER SURFACE GOUGE. SPOT FACED DAMAGED AREA HFEC INSPECTED, SHOT PEENED, TREATED & INSTALLED FASTENER PER EA 96808. DEFECT SIZE: .045 INCH DEEP, 15.5 PERCENT MATERIAL LOSS. 2L72 4F RTA2NM 20050913000042005091300004NM 2005 9 13 05FDEA02741 120050902A5320 SILL BOEING727 727200 138407ENM BS 604 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 OPEN HOLE NEXT TO FASTENER AT BS 604 MCD UPPER SILL O\B CHORD. REPAIRED OPEN HOLE, BS 604 IN MCD UPPER SILL PER FED-EX EA. 7-5310-92265. 2L73 4F RTA3WE 20050913000102005091300010NM 2005 9 13 C1HA200581012 120050912A532065175186 STIFFENER BOEING727 7272S7 138407ZNM BS 1263 CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15681CA 22020 U-CHANNEL SUPPORT IS CRACKED ON AFT SIDE OF WEB INSIDE OF RT LOWER TORQUE BOX, STA 1263 + 10 IN. REMOVED AND REPLACED DAMAGED BEAM P/N 65-17518-8, PO 531836 AT RT LWR TORQUE BOX AT ACTUATOR SUPPORT FITTING IAW SB 727-53-0129 REV 5 FIG 4 RII ACCOMPLISHED. 2L73 4F A3WE 20050913000232005091300023EA 2005 9 13 VTZA200500175 120050908A5320S6830 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA BS 325-392 CORRODED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27624BR 7211 RBL 9 FLOORBEAM HAS CORROSION AT FS 325 TO 392. 2L72 4F RTA21EA 20050913000292005091300029NM 2005 9 13 05FDEA02804 120050907A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 HORIZ STAB RT BARREL NUT BORE NR 11 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 - EA 1-5510-87628 ATTACHMENT 5. CLASSIFIED AS MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20050913000412005091300041NM 2005 9 13 05FDEA02819 120050908A5313 LONGERON DOUG MD11 MD11 3023602NM BS 1801 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 CENTER CARGO COMPT, RT STA 1801 LONGERON 46 FOUND WITH CORROSION CRACKED. ONGERON REMOVED AND NEW LONGERON INSTALLED AS PER SRM 51-31-01 VOL.II, SRM 51-33-01 VOL.II AND SRM 51-35-01 VOL.II. MAJOR REPAIR PER GMM 6-2-100. 2L73 4F RTA22WE 20050913000492005091300049NM 2005 9 13 05FDEA02827 120050909A5322 SHEAR TIE BOEING727 727233 138408ANM BS 640 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25268FE 21674 FWD CARGO CORROSION (C53-113-01) FLOOR SHEAR TIE STA 640 RBL 4 TO LBL 4 WL 148. REPAIRED PER SRM 53-10-4, MINOR REPAIR. 2L73 4F RTA3WE 20050913000592005091300059WP 2005 9 13 UPS05845383 120050814A5320 SPLICE DOUG DC8 DC871F 302199DWP FS 450 L33R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 INSPECTION TYPE:C1 CRACKED SPLICE ANGLE INSIDE CHANNEL AT FS 450 L33R. REMOVED CRACKED SPLICE ANGLE IAW SRM 51-1-21D, MACHINED AND INSTALLED LONGERON SPLICE AT STA 450 L33R IAW DWG 3750330. 2L74 4F RT4A25 20050913000612005091300061WP 2005 9 13 UPS05845385 120050813A5340 FITTING DOUG DC8 DC871F 302199DWP FS 1150 L33R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 INSPECTION TYPE:C1 C-PIT FS 1150 L33R I/B SIDE, FITTING HAS 2EA PLUGGED FASTENERS LOOSE. REMOVED INTERCOSTAL AT FS 1150 L33R IAW SRM 51-1-20D, FABRICATED AND INSTALLED FITTING AND INTERCOSTAL IAW DWG 4758514 AND DWG 9754949. 2L74 4F RT4A25 20050913000622005091300062 2005 9 13 UPS05845389 420050911A2565 SLIDE DOUG DC8 DC873F 302199FWP PAX DOOR MISINSTALLED A IPXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01810UP 46001 UNABLE TO READ PRESSURE ON EMERGENCY SLIDE ON ENTRY DOOR, NEED TO BE REPACKED. REMOVED AND REPLACED COVER. 2L74 4F RT4A25 20050913000662005091300066EA 2005 9 13 COMA0570102 120050907A532067053110521 WEB CNDAIRCL600 CL6002C10 1390015EA FS 280 CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01355CA7805 10067 THE LT AND RT LOWER WEBS ABOVE THE FLOOR AT FS 280 ARE CORRODED FROM LBL 36 TO RBL 36. REMOVED THE CORRODED WEBS AND INSTALLED NEW WEBS IAW REO 670-53-11-052 REV A. 2L72 4F RTA21EA 20050913000702005091300070WP 2005 9 13 UPS05845396 120050828A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE:C3 RIGHT WING L/E UPPER SKIN IS CRACKED IN THREE LOCATIONS (1ST XFS 310.250 ) (2ND 316.250) (3RD 322.750). CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1 FIG 38. 2L74 4F RT4A25 20050913000712005091300071WP 2005 9 13 UPS05845397 120050829A5712576953057 RIB DOUG DC8 DC873F 302199FWP LT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE:C3 LT WING L/E LOWER RIB HAS INTERGRANULARR CORROSION AT XFS 366.500, RIB IS ALSO CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT RIB IAW DC-8 SRM 51-1-2 0D, 51-1-21, AND DWG 5769530. 2L74 4F RT4A25 20050913000722005091300072WP 2005 9 13 UPS05845398 120050829A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE:C3 LT WING L/E UPPER SKIN HAS INTERGRANULAR CORROSION UNDER REPAIR DOUBLER AT XFS 410.250. REMOVED REPAIR DOUBLER, CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1. 2L74 4F RT4A25 20050913000752005091300075 2005 9 13 UPS05845402 420050912A3417 ADC DOUG DC8 DC871F 302199DWP NR 1 FAILED A IPXAA UNSCHED LANDING O OTHER CLCLIMB 1 SO01703UP 45939 INSPECTION TYPE:N/A ATB - AFTER T/O LOST NR 1 ADC, PULLED C/B COULD NOT RESTORE, XFRD TO NR 2 ADC ON CAPT SIDE. ATB DUE TO SLIGHT ELEC BURNING SMELL. REMOVED AND REPLACED AIR DATA COMP IAW MM 34-11-01-4 AND NR 1 ADC SELECT XFR RELAY IAW MM 20-50-16-2. CHECK WIRE FROM C/B'S TO RELAY TO ADC NO DEFECTS NOTED. AIR DATA COMPUTER & XFR RELAY NEEDS OPS CHECK. PERFORMED ADC TEST PER MM 34-11-00. 2L74 4F RT4A25 20050913000802005091300080NM 2005 9 13 SWAA052743 120050909A53306545776 SKIN BOEING737 7373H4 1384600NM BS 938 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 938, STR 21L. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050913000842005091300084NM 2005 9 13 SWAA052747 120050909A5753 SKIN BOEING737 7373H4 1384600NM RT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29352SW 24888 DURING SCHEDULED A1 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM. 2L72 4F RTA16WE 20050913000912005091300091SO 2005 9 13 CHQA200500162 120050910A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11573RP 14500837 RIGHT HAND WING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED WING EMERGENCY LIGHT BULB IAW EMB 145 MM 33-50-09. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050913001002005091300100NM 2005 9 13 SWAA052754 120050909A5753 SKIN BOEING737 7375H4 138449DNM RT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29528SW 26570 DURING SCHEDULED RON CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER SWA EA & SRM. 2L72 4F RTA16WE 20050913001012005091300101NM 2005 9 13 SWAA052755 120050908A53116546539 FRAME BOEING737 7373H4 1384600NM BS 616 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CHORD CRACKED AT BS 616, RBL 65, WL 202. REPAIRED FRAME CHORD PER BFG ER. 2L72 4F RTA16WE 20050913001052005091300105NM 2005 9 13 SWAA052759 120050909A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM BS 787 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29618WN 28034 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, LBL 9. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050913001232005091300123 2005 9 13 SWIA200515525 420050911A3418 CONTROL PANEL EMB 120 EMB120ER 3260203SO STALL WARNING INOPERATIVE A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07288SW 120316 STALL WARNING SYSTEM 2 INOP. REPLACED STALL WARNING TEST PANEL. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050913001262005091300126EA 2005 9 13 SWIA200515528 120050907A3350 BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07961SW 7857 FORWARD SECTION OF EMERGENCY LIGHTS ON CABIN FLOOR INOP. REPLACED FWD BATTERY PACK BALLAST. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050913001342005091300134SO 2005 9 13 SWIA200515530 120050910A27523430001005 ACTUATOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07566SW1203912039 120341 FLAP DISAGREEMENT ON INBOARD PAIR WHEN RETRACTING FLAPS. REPLACED LEFT INBOARD FLAP ACTUATOR IAW MM 27-50-07. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050913001382005091300138EA 2005 9 13 SWIA200515534 120050908A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA ROW 5 INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07455SW 7760 EMERGENCY OVERHEAD POD AT ROW 5 IS OUT. REPLACED ROW 5 EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050913001632005091300163NM 2005 9 13 05FDEA02834 120050912A5753 ATTACH FITTING DOUG MD11 MD11F 3023600NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 RT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. CORROSION REPAIR CARRIED OUT AS PER EA 1-5750-87634. 2L73 4F RTA22WE 20050913001662005091300166NM 2005 9 13 CALA0500306 120050910A3350ADD71701100 BATTERY PACK BOEING737 737724 13844BYNM EMERGENCY LIGHTSINOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2738727 28797 THE L-1 DOOR EXTERIOR AND L-1 DOOR OVERHEAD EMERGENCY LIGHTS WERE FOUND INOPERATIVE. THE M1675 BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51-06. 2L72 4F RTA16WE 20050913001702005091300170NM 2005 9 13 USAA051084 120050909A5320BAC1509100505 SUPPORT BOEING737 7374B7 1384702NM BS 993 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19776AU 24934 CORROSION STA 993 AT LEFT SIDE. FABBED PART AND INSTALLED PER SRM 51-40-25, DEFECT SIZE: 4.6 INCH. 2L72 4F RTA16WE 20050914000012005091400001NM 2005 9 14 MASA200500573 120050719A243551539008D CONTROL UNIT DHAV DHC8 DHC8202 2809007NM NR 1 STARTER GENFAILED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07989HA3065 427 ASH 6201 PHX. NR 1 ENGINE WON'T START. SMOKE CAME OUT OF THE ENGINE. MX REPLACED THE STARTER GENERATOR AND GENERATOR CONTROL UNIT. 2H72 4T RTA13NM 20050914000072005091400007NM 2005 9 14 ABXA050216 120050907A335020131A BATTERY BOEING767 767281 1385109NM EMERGENCY LIGHT DISCHARGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23768AX 22786 AIRCRAFT EMERGENCY LIGHTING SYSTEM INOPERATIVE (SPARE BATTERY). REMOVED AND REPLACED EMERGENCY LIGHT SPARE BATTERY PACK. OPS CHECKED GOOD IAW B767 MM 33-56-35. 2L72 4F RTA1NM 20050914000102005091400010SO 2005 9 14 CHQA200500160 120050909A801135059106 STARTER EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL ENGINE SMOKE A CHQAF ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL11272SK3205 3205 145306 CAE311921 ON PUSHBACK & ENG START, NORMAL UNTIL START OF NR 1 ENG, WHEN START/STOP SELECTOR ENGAGED RECEIVED NO INDICATION OF NORMAL START. NO ROTATION, NO OIL PRESSURE, NO FUEL FLOW, AND NO ITT RISE. ABORTED START, ATTEMPTED A CROSS BLEED START, SAME RESULTS. TAXIED TO GATE TO ATTEMPT A EXTERNAL AIR START. NOTIFIED BY GROUND PERSONNEL OF SMOKE COMING OUT OF ENGINE. BEGAN EMERGENCY EVACUATION MEMORY ITEM & CHECKLIST. CAPTAIN PULLED BOTH FIRE HANDLES. F/O NOTIFIED ATC & VISUALLY VERIFIED CHECKLIST ITEMS. VISUALLY INSPECTED NR 1 ENG & SAW SMOKE. BLEW -A- BOTTLE & WAITED, SMOKE STILL VISIBLE AS STRONG IF NOT STRONGER. BLEW B-BOTTLE AND SMOKE BEGAN TO CEASE. REMOVED & REPLACED TURBINE STARTER. 2L72 4T4 FRTT00011ATTE6CH 20050914000162005091400016NM 2005 9 14 ASMF200509004 120050909A29107936907517 HOSE DOUG MD88 MD88 3023688NM HYDRAULIC SYS DAMAGED W ASMFK NONE K FLUID LOSS ININSP/MAINT 1 SW23162PL 49765 DURING TRANSIT CHECK, IT WAS DETECTED A HYDRAULIC LEAK AT THE SLATS PRESSURE LINE FORWARD ADF ANTENNA. THE SLATS PRESSURE LINE WAS REPLACED IAW MM 29-10-00, TESTED CORRECT. 2L72 4F RTA6WE 20050914000172005091400017NM 2005 9 14 ASMF200509005 120050910A2612 CONNECTOR DOUG MD88 MD88 3023688NM LT FIRE DETECT MISINSTALLED W ASMFK NONE WL INADEQUATE Q C NO TEST ININSP/MAINT 1 SW23162PL 49765 CAPTAIN REPORTED THE LEFT ENGINE FIRE TEST OUT OF SERVICE. DURING REVISION, LOOP-A AND BAND LT ENGINE FIRE SHUT OFF LEVER LIGHTS DID NOT TURN ON. THE CONNECTORS P1-823, P1-822 AND P1-824 WERE CHECKED, BEING CORRECT. DURING REVISION BY CONTINUITY AND ISOLATION, IT WAS DETECTED THE BASKET WIRING OPENED AND THE CONNECTORS P1-824 AND P1-825 WITHOUT CONTINUITY PER TWO LINES INVERTED AT THE INFERIOR BASKET OF CONNECTORS P1-859 AND P1-854. THE CONNECTORS WERE INSTALLED CORRECTLY IAW MM 26-10-00, TESTED CORRECT. DURING OVERNIGHT CHECK, THE FIRE DETECTING SYSTEM WAS TESTED IAW MM 26-10-00, ALL CORRECT. 2L72 4F RTA6WE 20050914000182005091400018CE 2005 9 14 DXTA200500963 120050911A3240 BRAKE ASSY CESSNA560 560XL 2076702CE MLG UNDERSERVICED E DXTAD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07639QS 5605139 LEFT BRAKE ON CAPTAIN'S SIDE MUSHY. BRAKE NEEDS SERVICING. 2L72 4F RTA22CE 20050914000192005091400019CE 2005 9 14 DXTA200500964 120050912A2720 RUDDER PEDAL CESSNA500 560CESSNA 2076750CE RUDDER ERRATIC E DXTAO OTHER F FLT CONT AFFECTED DEDESCENT 1 GL07360QS 5600460 REPEAT WRITE UP. ON DESCENT INTO TEB, RUDDER PEDALS WOULD JERK RIGHT AND LEFT. SEEMS TO BE HAPPENING WHEN AFIS SENDS AND RECEIVES. 2L72 4F RTA22CE 20050914000232005091400023CE 2005 9 14 DXTA200500961 120050909A3411 PITOT SYSTEM CESSNA750 750 2076810CE WARNING LIGHT E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07921QS 7500241 AMBER 'P/S-RAT HEAT OFF' CAS MESSAGE ILLUMINATED DURING TAKEOFF ROLL. T/O ABORTED. SWITCHES WERE IN THE ON POSITION THE ENTIRE TIME. CHECKED FOR MESSAGE ON MAINTENANCE PAGE 60TLS, CHECKED CONNECTION ON LT/RT P/S SWITCHES S1030 AND S1063. SHOOK DOWN ALL ACCESSIBLE WIRING, NO FAULTS NOTED. SYSTEM OP'S CK GOOD PER 750 MM TASK 30-32-00-710 AND 30-30-00-710. 2L72 4J RTT00007WI 20050914000242005091400024CE 2005 9 14 DXTA200500959 120050908A2750 HANDLE CESSNA750 750 2076810CE TE FLAPS DIRTY E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07948QS 7500149 FLAPS FAILED AT 15 DEGREES. FLAPS FAILED AT 15 DEGREES HAD BITES NR 2 AND NR 6 ON CONTROLER REMOVED FLAP HANDLE, REMOVED COVER AND CLEANED LINT FROM INSIDE HANDLE IAW: CE750 M/M 27-50-00. FLAPS OPERATIONALY CHECK GOOD. 2L72 4J RTT00007WI 20050914000262005091400026CE 2005 9 14 DXTA200500962 120050910A282131J240401 FUEL FILTER CESSNA560 560XL 2076702CE PWA 545 PW545A NE RIGHT CLOGGED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07625QS 5605319 PCEDB0652 RIGHT SIDE FUEL FILTER BYPASS ANNUNCIATOR AND MASTER CAUTION LIGHT ILLUMINATED DURING TAKEOFF ROLL. LIGHT ILLUMINATED AS THROTTLES WERE PUT IN TO DETENT. THROTTLES BROUGHT UP SLOWLY. LIGHT EXTINGUISHED WHEN THROTTLES BROUGHT BACK TO IDLE. REMOVED AND REPLACED THE FUEL FILTER AND O-RINGS FOR THE RT ENGINE. CARRIED OUT ENGINE RUN AND ANNUNCIATOR DID NOT REOCCUR. OPS AND LEAK CHECK WAS GOOD. ALL WORK DONE IAW PRATT AND WHITNEY 545A MM CHAP 73-10-05. 2L72 4F4 FRTA22CE E00059EN 20050914000282005091400028NM 2005 9 14 2005UALA00928 120050901A2121 FAN AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE CABIN FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29822UA 948 RETURN TO FIELD DUE TO AN EXTRACT FAN FAULT. ECAM EXTRACT FAN FAULT DISPLAYED AFTER TAKEOFF. REPLACED BLOWER FAN AND AVIONICS FILTER. OPS. TEST PER 21-26-00. OPS CHECKS GOOD. 2L72 4F4 FRTA28NM E40NE 20050914000292005091400029NM 2005 9 14 2005UALA00929 120050902A3234 LEVER AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE MLG FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29827UA 1022 UNABLE TO RETRACT LANDING GEAR. ON TAKE OFF LANDING GEAR HANDLE WOULDN`T MOVE, GEAR STAYED DOWN. LANDING WT-140.8+SINK RATE-100FPM. REPLACED LANDING GEAR LEVER PER MM- 32-31-11, TESTS GOOD. 2L72 4F4 FRTA28NM E40NE 20050914000322005091400032NM 2005 9 14 2005UALA00932 120050903A5315 FLOORBEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE BS 312 CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29327UA 24147 CABIN FLOOR BS 312 LBL 1 AND LBL 6 SMALL AREA OF CORROSION ON UPPER SURFACE OF FLOORBEAM. 2L72 4F4 FRTA16WE E2GL 20050914000382005091400038EU 2005 9 14 2005UALA00938 120050905A5313 STRINGER AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FS 54-56 CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29420UA 489 STR 43L HAS CORROSION BETWEEN FRAMES 54-56. CUT-OUT DAMAGED SECTION ACP SPLICE REPAIR PER SRM 53-00-13 FIG 201. 2L72 4F4 FRTA28NM E40NE 20050914000392005091400039NM 2005 9 14 2005UALA00939 120050902A3350321430 BATTERY AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE EMERGENCY LIGHT FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29835UA 1426 CABIN EMERGENCY LIGHT TEST FAILED WITH MESSAGE: EPSU INT LOAD EMER L. REPLACED BATTERY 11WL. 2L72 4F4 FRTA28NM E40NE 20050914000412005091400041EU 2005 9 14 2005UALA00941 120050903A5330 SKIN AIRBUS320 A320232 3930326EU FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29468UA 1363 APPROX 1 INCH CRACK IN OUTER FUSELAGE SKIN JUST TO THE LEFT OF APU AIR INLET. MANUFACTURED REPAIR DOUBLER AND INSTALLED. REPAIRED PER SRM53-51-11 FIG203. 2L72 4F RTA28NM 20050914000422005091400042 2005 9 14 2005UALA00942 420050901A2565 SLIDE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE DOOR 2R WARNING LIGHT A UALAK NONE L NO TEST ININSP/MAINT 1 WP29433UA 589 DURING CABIN EMERGENCY LIGHTS CHECK, FOUND EXT LOAD AFT LEFT ERROR MSG. REPLACED DOOR 2R SLIDE. 2L72 4F4 FRTA28NM E40NE 20050914000452005091400045NM 2005 9 14 2005UALA00945 120050905A33501317 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29179UA 25158 EMERG LT INOP, CEILING UPPER DECK DOOR AREA. REPLACED LAMP. 2L74 4F4 FRTA20WE E24NE 20050914000462005091400046NM 2005 9 14 2005UALA00946 120050905A335020131A POWER SUPPLY BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29179UA 25158 EMERG LTS INOP 2 EA ASSY AFT LT OVERWING. REPLACED POWER SUPPLY 2L74 4F4 FRTA20WE E24NE 20050914000482005091400048WP 2005 9 14 05FDEA02837 120050911A7797 WIRE HARNESS DOUG MD10 MD1010F 3022112WP NR 1 ENGINE FAILED A FDEAEJA ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25398FE 46634 ENGINE NR 1 EGT EXCEEDING 937 DEGREES ON TAKEOFF ALSO NOTED N1 FLUCTUATION SAME TIME. SHUT DOWN ENGINE AND DUMPED FUEL 22,000 LBS, RETURNED TO SEA. REMOVED AND REPLACED NR 1 ENG EGT THERMOCOUPLE HARNESS PER MD-10-10 AMM 77-21-01-2. OPS CHECKED NORMAL. 2L73 4F RTA22WE 20050914000492005091400049NM 2005 9 14 05FDEA02751 120050904A5730 SKIN DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 CRACK INDICATIONS ON NR 5 BORE HOLES FOUND DURING HFEC INSPECTION AT LEFT HAND WING LOWER SKIN DOOR CUTOUT OF PANEL 536AB. FOUND HOLES CRACK LENGTH APPROXIMATELY 0.100", 1 HOLE CRACK LENGTH APPROXIMATELY 0.187" ON BORE SURFACE. REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-87569. 2L73 4F RTA22WE 20050914000522005091400052NM 2005 9 14 05FDEA02739 120050902A5320 CHANNEL BOEING727 727233 138408ANM BS 620 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 WHILE WORKING FED EX EA 7-5330-72293B PT2 FOUND 2 FASTENER HOLES ON EDGE OF "C" CHANNEL BS 620 LBL-36 W/L 292. REPAIRED C-CHANNEL, BS 620, LBL 36 PER FED-EX EA 7-5330-92321. 2L73 4F RTA3WE 20050914000542005091400054WP 2005 9 14 IXXA05RNG043S 120050717A53205644011501 ANGLE DOUG DC8 DC862F 3021972WP BS 857.000 CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW1171CX 670243317 45961 CORROSION ON LT WHEEL WELL "DOG HOUSE" AREA LOWER SIDE STA 857.000, ANGLE WAS FOUND CORRODED. ANGLE WAS FABRICATED IAW DOUGLAS DRAWING 5644678 AND ASSEMBLED IAW DC8 SRM 53-7-2 FIGURE 4. 2L74 4F 4A25 20050914000562005091400056WP 2005 9 14 IXXA05RNG045S 120050720A5730 SKIN DOUG DC8 DC862F 3021972WP RT WING CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW1171CX 670243317 45961 SKIN CORROSION DAMAGE FOUND ON RIGHT OUTER WING AT UPPER PLATING AROUND WING STATION XRS 727.00 AND STRINGER 3RH DURING A ROUTINE C CHECK INSPECTION. CORRODED AREA WAS BLENDED OUT, DOUBLER WAS FABRICATED AND INSTALLED IAW EWO ATI 57-035 AND EO ATI-071605. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR. 2L74 4F 4A25 20050914000572005091400057WP 2005 9 14 UPS05845367 120050810A5730 SKIN DOUG DC8 DC871F 302199DWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 INSPECTION TYPE:C1 RIGHT WING UPPER SKIN .25 INCH CRACK AT STA XCW 69 REAR SPAR AREA. CUT OUT CRACKED SECTION OF RIGHT WING AT XCW 69, NDT VERIFIED CRACK TERMINATION IAW HFEC INSP PER NDTSPM 06-10-01.001. FABRICATED -4 FILLER, -6 FILLER AND -8 DOUBLER IAW SRM 51-1-8, AND 51-1-26 FIG 1 SHT 1, AND INSTALLED REPAIR PARTS IAW SRM 51-1-20D AND 51-1-15. 2L74 4F RT4A25 20050914000592005091400059WP 2005 9 14 UPS05845369 120050815A5315 FLOORBEAM DOUG DC8 DC871F 302199DWP FS 55 LBL 12 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 INSPECTION TYPE:C1 FLOORBEAM CRACKED AT FS 55 LBL 12. CUT OUT DAMAGED AREA OF FLOORBEAM IAW SRM 53-2-0 TEMP REV 53-152, FABRICATED DOUBLER AND FILLER AND INSTALLED REPAIR PARTS IAW SRM 53-2-0 TEMP REV 53-152 AND 51-1-20D. 2L74 4F RT4A25 20050914000612005091400061NM 2005 9 14 UPS05M45363 120050702A5330 SKIN DOUG MD11 MD11F 3023600NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01255UP 48404 INSPECTION TYPE:C-CHECK AFT CARGO CORROSION BETWEEN DOUBLER & SKIN OF PREVIOUSLY INSTALLED LAV VACUUM PUMP OUTLET AT STA 1959 L38-39 RT. REFER TO SH523-123 EARN FOR WORK CARRIED OUT AND ATTACHED EARN N255UP FOR DISPOSITION. 2L73 4F RTA22WE 20050914000622005091400062NM 2005 9 14 USAA051081 120050909A53206552878 CHANNEL BOEING737 7374B7 1384702NM BS 957-993 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19776AU 24934 CORROSION BETWEEN BS 957-993 LBL 48. REMOVED & REPLACED CHANNEL PER SRM 51-40-02, 51-40-05, DEFECT SIZE: 26"L X 2"W X .030"D. 2L72 4F RTA16WE 20050914000672005091400067EU 2005 9 14 MALA050679 120050825A5320 WEB SAAB SF340 340B 7860101EU BS 294 CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15454XJ 340B454 DURING 4K INSPECTION IN BNA FOUND FLOOR WEB AT STA 294.0 RBL 10 IS CORRODED-OUT OF LIMITS. REMOVED AND REPLACED FLOOR WEB. REF:EAMS WO 212752 TASK 1521. WORK REF SAAB SRM 51-40-21. 2L72 4T RTA52EU 20050914000682005091400068EU 2005 9 14 MALA050682 120050829A5330 SKIN SAAB SF340 340B 7860101EU BS 315-379 DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15454XJ 340B454 DURING 4K CHECK IN BNA FOUND DENTS IN RT SIDE ICE QUARD ARE STA 315-379. REMOVED ICE QUARD. REPAIRED FUSELAGE, OUT OF LIMIT REF: SRM 51-10-101 LOCATION REF: EO S53005. NEW ICE QUARDS. REF: EAMS WO 212753 TASK 2502. 2L72 4T RTA52EU 20050914000692005091400069EU 2005 9 14 MALA050688 120050903A5315 FLOORBEAM BAC 146 AVRO146RJ85A1500097EU FR 18 CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15507XJ E2316 WHILE ACCOMPLISHING C1 INSPECTION, FOUND FLOORBEAM (UNDERSIDE) AT FRAME 18 RBL 30 CORRODED. 2H74 4F RTA49EU 20050914000702005091400070EU 2005 9 14 MALA050685 120050903A5315 GUSSET BAC 146 AVRO146RJ85A1500097EU FLOORBEAM CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15507XJ E2316 WHILE ACCOMPLISHING C1 INSPECTION, FOUND GUSSET PLATE AT FRAME 18 FLOORBEAM LBL 12 CORRODED. 2H74 4F RTA49EU 20050914000712005091400071EU 2005 9 14 MALA050686 120050903A5347 SEAT TRACK BAC 146 AVRO146RJ85A1500097EU FR 18 CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15507XJ E2316 WHILE ACCOMPLISHING C1 INSPECTION, FOUND SEAT RAIL AT FRAME 18 FLOORBEAM RBL 16 CORRODED. 2H74 4F RTA49EU 20050914000732005091400073EU 2005 9 14 MALA050680 120050826A54207254110257 STRAP SAAB SF340 340B 7860101EU CAM LOCK CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15454XJ 340B454 DURING 4K INSPECTION FOUND LT NACELLE FIG 8 INBOARD ATTACH CAM-LOCK STRAP CHAFED OUT OF LIMIT P/N 7254110-257. REMOVED AND REPLACED REF: EAMS WO 212753 TASK 4505 WORK REF: SAAB SRM 51-40-22/21/25. 2L72 4T RTA52EU 20050914000742005091400074EU 2005 9 14 MALA050681 120050826A54207254110257 STRAP SAAB SF340 340B 7860101EU COWL CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15454XJ 340B454 DURING 4K CHECK IN BNA REMOVED AND REPLACED RT NACELLE FIG 8 COWL ATTACH STRAP P/N 7254110-257 CHAFE DAMAGE. REMOVED AND REPLACED REF: EAMS WO 212753 TASK 4501 WORK ORDER SAAB SRM 51-40-22/21/25. 2L72 4T RTA52EU 20050914000772005091400077NM 2005 9 14 AALA20050570 120050902A3350 BATTERY PACK BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21386AA 27060 DFW - ALL FOUR EMERGENCY LIGHT OVERWING EXIT SIGNS INOPERATIVE. REPLACED BATTERY PACK M1209 FOR ALL FOUR EMERGENCY LIGHT OVERWING EXIT SIGNS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050914000782005091400078WP 2005 9 14 AALA20050572 120050903A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21407AA 49318 MSP - EMERGENCY LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT FORWARD ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050914000792005091400079NM 2005 9 14 AALA20050471 120050903A3350 LIGHT BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21194AA 32388 LAX - EMERGENCY LIGHT AT LEFT ONE DOOR BROKEN. REPLACED EMERGENCY LIGHT AT LEFT ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050914000812005091400081WP 2005 9 14 AALA20050574 120050905A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21569AA 49351 DTW - CEILING EMERGENCY EXIT LIGHT AT ROWS 7 TO 9 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY EXIT LIGHT AT SEAT ROWS 7 TO 9. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050914000832005091400083NM 2005 9 14 AALA20050577 120050906A2120 TUBE BOEING757 757223 1384957NM CARGO BAY FAN OBSTRUCTED A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21172AJ 32400 MIA - CAPTAIN REPORTED FIRE INDICATION IN AFT CARGO COMPARTMENT. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. ACCOMPLISHED BITE TEST WITH NO FAULTS NOTED. REMOVED DEBRIS FROM AFT CARGO COMPARTMENT FAN TUBING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050914000862005091400086WP 2005 9 14 AALA20050579 120050906A3350P4010051111 MODULE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21452AA 49553 SFO - EMERGENCY EXIT LIGHT AT PASSENGER DOOR LEFT TWO IN AFT GALLEY INOPERATIVE. REPLACED ELECTRICAL CHARGING MODULE FOR EMERGENCY EXIT LIGHT IN PASSENGER DOOR LEFT TWO IN AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050914000872005091400087WP 2005 9 14 ARWA20050906 120050714A5330 SKIN DOUG DC8 DC863F 302198FWP BS 1690-1734 CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19784AL 46135 DURING C-CHECK INSPECTION, THE FOLLOWING WAS FOUND; FUSELAGE EXTERIOR STA 1690 THROUGH STA 1734, L-29L, SKIN WITH CORROSION. 2L74 4F 4A25 20050914000882005091400088WP 2005 9 14 ARWA20050902 120050623A5330 SKIN DOUG DC8 DC863F 302198FWP BS 1490-1690 CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19784AL 46135 DURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND; LOWER FUSELAGE STA 1490 THROUGH STA 1690, L-31L THROUGH L-31R, SKIN PANEL WITH CORROSION AT SEVERAL PLACES. 2L74 4F 4A25 20050914000892005091400089SO 2005 9 14 RAIA00509006 120050901A335078241 INVERTER EMB 145 EMB145 3260210SO EMERGENCY LIGHT INTERMITTENT A RAIAK NONE O OTHER ININSP/MAINT 1 CE03802HK 145066 FLIGHT 3507 - MHT - FLOOR PROXIMITY OVERWING EMERGENCY EXIT SIGN INTERMITTENT. MAINTENANCE REMOVED AND REPLACED THE NR 6 INVERTER. 2L72 4F RTT00011AT 20050914000902005091400090SO 2005 9 14 RAIA00509007 120050906A3350744412 SIGN EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03830HK 145313 FLT 5584 - RIC - ROW 3 BULKHEAD EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE EXIT SIGN. 2L72 4T RTT00011AT 20050914000922005091400092NM 2005 9 14 USAA051083 120050909A5313US5300022LF STRINGER BOEING737 7374B7 1384702NM BS 380-400 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19776AU 24934 FS 380-400 AT STR 4L CRACKED. FABBED PARTS, INSTALLED REPAIR PER SRM 51-40-02, DEFECT SIZE: 1 INCH CRACK. 2L72 4F RTA16WE 20050914000942005091400094WP 2005 9 14 ARWA20050908 120050718A5751 SKIN DOUG DC8 DC863F 302198FWP RT AILERON CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19784AL 46135 DURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND; RT INBOUND AILERON BETWEEN XA 565 AND XA542 LOWER SKIN WITH CORROSION. 2L74 4F 4A25 20050914000952005091400095NM 2005 9 14 ASMF200509003 120050906A2711R15048 ACTUATOR BOEING737 737* NM AILERON TRIM FAILED W ASMFO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 SW23997AM2206 2196 30283 CAPTAIN REPORTED THAT AILERON TRIM FAILED AND THE SELECTED RATE WAS OVERSHOOT. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT CHECK, THE CONTROL PANEL SWITCH OPERATION AND CONNECTOR ACTUATOR VOLTAGE WERE VERIFIED, DETERMINING THAT THE ACTUATOR NEEDS TO BE REPLACED IAW MM 27-11-11 AND FIM 27-11. TASK 814 WAS PERFORMED, TESTED CORRECT. 2L72 4F RTA16WE 20050914000962005091400096WP 2005 9 14 ARWA20050907 120050712A5420 STRUCTURE DOUG DC8 DC863F 302198FWP NR 2 PYLON CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19784AL 46135 DURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND; NR 2 PYLON FOOT STOOL INBOUND SIDE WITH CRACK, APPROXIMATELY 5/8". 2L74 4F 4A25 20050914000982005091400098NM 2005 9 14 CIHA200581003 120050909A5340 CLIP BOEING727 7272S7 138407ZNM BS 850 CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15681CA 22020 SUPPORT CLIP ON STR 16R CRACKED AT BS 850. REMOVED DAMAGED SPLICE ON STR 16R AT BS 850 IAW 727 SRM 51-30-2. FABBED NEW SPLICE FROM BAC 1498-137 PO 4496178 DIM 6 INCHES IN LENGTH IAW 727 SRM 53-10-2 FIG 9. SPLICE TREATED, PRIMED, AND INSTALLED IAW 727 SRM 51-10-2 AND 51-30-2. 2L73 4F A3WE 20050914000992005091400099NM 2005 9 14 C1HA200581004 120050909A5311 FRAME BOEING727 7272S7 138407ZNM BS 680 DENTED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15681CA 22020 FRAME DENTED IN FWD CARGO PIT OVER BS 680 OVER STRINGER 25R, MARKED. CUT OUT DAMAGED AREA 1.75 X .75 INCH AND FABBED REPAIR DOUBLER FROM 7075T6 .063 PO 9002351 DIM 9.75 X 3.75 INCH IAW 727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1. REPAIR ANGLE TREATED AND PRIMED AND INSTALLED IAW 727 SRM 51-10-2 AND 51-40-3 FIG 1. 2L73 4F A3WE 20050914001002005091400100NM 2005 9 14 CIHA200581005 120050909A5311 FRAME BOEING727 7272S7 138407ZNM BS 520 DENTED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15681CA 22020 FWD CARGO PIT, HAS FRAME 520 DENTED ON STR 26R. DAMAGED AREA OUT OF LIMITS IAW 727 SRM 53-10-1 FIG 1. CUT OUT DAMAGED AREA BS 520 FRAME BETWEEN STR 25R AND 26R DIM 2 X 1 INCH, FABBED REPAIR ANGLE FROM 7075T6 .063 PO 9002351 DIM 9.25 X 4 INCH, TREATED, PRIMED, AND INSTALLED IAW 727 SRM 51-10-2, 53-10-2 FIG 5, 51-40-3 FIG 1. 2L73 4F A3WE 20050914001012005091400101NM 2005 9 14 C1HA200581007 120050909A5330 SKIN BOEING727 7272S7 138407ZNM BS 463 DENTED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15681CA 22020 BS 463 BETWEEN 15RT-16RT STRINGERS HAS LARGE PROTRUDING DENT OIL CANNING. DAMAGE OUT OF LIMITS IAW 727 SRM 53-30-1 FIG 1, CUT OUT DAMAGED AREA, FABBED FILLER FROM 2024 T3 .040 PO 9002416 DIM 4.375 X 4.5 INCH, DOUBLER FROM 2024 T3 .050 PO 9002507 DIM 14.25 X 10.875 INCH IAW SRM 53-30-2 FIG 1 AND 53-30-3 FIG 4, REPAIR PARTS TREATED, PRIMED AND INSTALLED IAW 727 SRM 51-10-2 AND 53-30-3 FIG 4. 2L73 4F A3WE 20050914001022005091400102NM 2005 9 14 C1HA200581009 120050909A5311 FRAME BOEING727 7272S7 138407ZNM RT MLG WW CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15681CA 22020 RIGHT MLG WW LOAD APU CONTROL VALVE CUT OUT HOLE ON STA 870, WEB IS CRACKED. CRACK STOP DRILLED IAW 727 SRM 51-10-1. FABBED AND INSTALLED 2 EA DOUBLERS FROM 301 1/2 HD .050 PO 9912793 DIM 12 X 11 INCHES AND 18.5 X 21 INCHES IAW 727 SRM 53-10-9 FIG 5. 2L73 4F A3WE 20050914001042005091400104NM 2005 9 14 C1HA200581011 120050909A5320 CHANNEL BOEING727 7272S7 138407ZNM BS 1263+10 CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15681CA 22020 U-CHANNEL SUPPORT IS CRACKED ON FWD SIDE OF WEB INSIDE OF RIGHT LOWER TORQUE BOX, STA 1263 + 10 INCHES. REMOVED AND REPLACED DAMAGED GUSSET P/N 69-67881-1 PO 5070544 AND STIFFENER P/N 65-17518-15 PO 531824 AT RIGHT LOWER TORQUE BOX AT ACTUATOR SUPPORT FITTING IAW SB 727-53-0129 REV 5 FIG 4. 2L73 4F A3WE 20050914001052005091400105NM 2005 9 14 CIHA200581006 120050909A5311 FRAME BOEING727 7272S7 138407ZNM BS 520 DENTED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15681CA 22020 FWD CARGO PIT HAS FRAME DENTED AT STA 520 STR 25R (MARKED). DAMAGED AREA OUT OF LIMITS IAW 727 SRM 53-10-1 FIG 1. CUT OUT DAMAGED AREA BS 520. FRAME BETWEEN STR 25R-26R DIM 2 X 1 INCH AND FABBED REPAIR ANGLE FROM 7075T6 .063 PO 9002351 DIM 9.25 X 4 INCHES, TREATED PRIMED, AND INSTALLED IAW 727 SRM 51-10-2, 53-10-2 FIG 5 AND 51-40-3 FIG 1. 2L73 4F A3WE 20050914001062005091400106NM 2005 9 14 C1HA200581013 120050912A532065C138744 ANGLE BOEING727 7272S7 138407ZNM BS 1263+10 CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15681CA 22020 L-ANGLE SUPPORT IS CRACKED AT UPPER INBOARD CORNER OF RIGHT LOWER TORQUE BOX, STA 1263 + 10 INCHES. REMOVED AND REPLACED DAMAGED ANGLE P/N 65C13874-4 PO 3146138 AND FILLER P/N 65C13874-5 PO 3146132 AT RIGHT LOWER TORQUE BOX AT ACTUATOR SUPPORT FITTING IAW SB 727-53-0129 REV 5 FIG 4. 2L73 4F A3WE 20050914001082005091400108NM 2005 9 14 C1HA200581016 120050912A5311 FRAME BOEING727 7272S7 138407ZNM BS 660 DENTED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15681CA 22020 FRAME DENTED IN FWD CARGO -B- STA 660 OVER STRINGER 26R, MARKED. CUT OUT DAMAGED AREA DIM 2.125 X 1 INCH, FABBED REPAIR ANGLE FROM 7075T6 .063 PO 9002126 DIM 13 X 4 INCHES IAW 727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1. REPAIR ANGLE TREATED AND PRIMED INSTALLED IAW 727 SRM 51-10-2 AND 51-40-3 FIG 1. 2L73 4F A3WE 20050914001092005091400109NM 2005 9 14 C1HA200581017 120050912A53146518636378 STIFFENER BOEING727 7272S7 138407ZNM BS 870 CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15681CA 22020 RIGHT MLG KEELBEAM INBOARD SIDE VERTICAL STIFFENER IS CRACKED STA 870 (MARKED). REMOVED AND REPLACED DAMAGED VERTICAL STIFFENER BS 870 AT KEEL BEAM IAW 727 SRM 51-30-2 P/N 65-18036-378 PO 53185. 2L73 4F A3WE 20050914001102005091400110NM 2005 9 14 C1HA200581015 120050912A5311 FRAME BOEING727 7272S7 138407ZNM BS 680 DENTED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15681CA 22020 FRAME DENTED IN FWD CARGO PIT STA 680 OVER STRINGER 25R, MARKED. CUT OUT DAMAGED AREA DIM 1.375 X .875 INCHES AND FABBED ANGLE REPAIR FROM 7075T6 .063 PO9002507 DIM 15.75 X 3.75 IAW 727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1. ANGLE TREATED AND PRIMED INSTALLED IAW 727 SRM 51-10-2 AND 51-40-3 FIG 1. 2L73 4F A3WE 20050914001112005091400111WP 2005 9 14 ABXA050212 120050907A3397 WIRE DOUG DC9 DC941 302207NWP BROKEN A ABXAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL23975AX 47512 WHEN CIRCUIT BREAKER FOR CLEARVIEW & EYEBROW WINDOWS WAS PUSHED IN DURING FLIGHT, CONSIDERABLE ARCHING AND SPARKS CAME FROM CAPTAIN'S CLEARVIEW WINDOW BUY THE TERMINAL BLOCK. REPAIRED A BROKEN WIRE AT THE TERMINAL BLOCK AND REPLACED THE TERMINAL BLOCK IAW DC9 AMM 30-41-00-2. 2L72 4F A6WE 20050914001162005091400116NM 2005 9 14 05FDEA02815 120050908A5744 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 RT WING, I/B FLAP O/B HINGE (WING SIDE), PIVOT BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87636. 2L73 4F RTA22WE 20050914001182005091400118NM 2005 9 14 SWAA052675 120050902A53156546805 FLOORBEAM BOEING737 7373H4 1384600NM BS 845 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29373SW 26581 DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 845, LBL 8. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20050914001202005091400120EA 2005 9 14 REXA200500116 120050911A2780 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA LE FLAPS MALFUNCTIONED A REXAO OTHER J WARNING INDICATION APAPPROACH 1 SO258936A 7936 FLAPS FAILED AT 20 DEG ON APPROACH. PERFORMED AD 98-20-01, UNDER 72 HOURS MONITORING FOR FLAPS FAIL MESSAGES. 2L72 4F RTA21EA 20050914001212005091400121EA 2005 9 14 REXA200500115 120050909A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A REXAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO258886A 7886 FLAP FAIL MESSAGE. INSPECTED PER AD 98-20-01. NO DEFECTS NOTED. RESET FLAPS PER MANUFACTURES FAULT ISOLATION MANUAL (FILM). OPERATIONALLY CHECKS GOOD. 2L72 4F RTA21EA 20050914001222005091400122NM 2005 9 14 05FDEA02830 120050909A5320 FLOOR SUPPORT BOEING727 727200 138407ENM BS 572 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25268FE 21674 FWD CARGO FLOOR SUPPORT DENTED STA 572 WL 156 LBL 9. REPAIRED PER SRM 53-10-1, 51-40-4 FIG 1 MINOR REPAIR. 2L73 4F RTA3WE 20050914001232005091400123EA 2005 9 14 REXA200500117 120050911A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A REXAO OTHER J WARNING INDICATION APAPPROACH 1 SO25827AY 8027 FLAPS FAILED AT 20 DEGREES ON APPROACH. COMPLIED WITH AD 98-20-01. NO DISCREPANCIES NOTED. UNDER 72 HOURS FLAP WATCH. 2L72 4F RTA21EA 20050914001242005091400124EU 2005 9 14 U30A200500007 120050910A2120 ODOR AIRBUS320 A320214 3930316EU CABIN DETECTED A U30AD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA17270AV 2325 AS AIRCRAFT TRANSITIONED FROM RUNWAY TO TAXIWAY AFTER LANDING, RAMP PERSONNEL & TOWER PERSONNEL SAW WHITE SMOKE FROM UNDER PLANE FOR 20 SEC. CREW REPORTED BRIEF LIGHT SMOKE AND UNKNOWN ODOR IN CABIN THAT DISSIPATED QUICKLY, WHICH WAS VERIFIED BY THE F/O. THE AIRCRAFT CONTINUED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE VISUALLY INSPECTED THE APU COMPARTMENT & AIR INLET, BRAKES, AVIONICS COMPARTMENT, CARGO COMPARTMENTS, AIR CONDITIONING PACKS (INLETS & OUTLETS) AND WHEEL WELLS WITH NO DEFECTS NOTED. MAINTENANCE PERFORMED IDLE RUN OF ENGINES PER AMM 71-00-00-710-006, WITH NO DEFECTS NOTED. ACFT RETURNED TO SERVICE. AIRCRAFT HAS OPERATED SEVERAL FLIGHTS SINCE THIS OBSERVATION WITH NO FURTHER INCIDENT. 2L72 4F RTA28NM 20050914001252005091400125EU 2005 9 14 EM05009 120050909A216010007003 ACM EMB ERJ170ERJ170100 EU NR 1 INOPERATIVE A USAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA19817MD3156 000038 FLIGHT 1756, CMH TO PHL - ON CLIMB THRU FL200 THERE WAS A STRONG SMELL OF SMOKE IN THE CABIN. PACK NR 1 SUBSEQUENT FAILED, SMOKE SMELL DISSIPATED AFTER SELECTED OFF. MAINTENANCE FOUND AMBER X ON EICAS PAGE. TRIED TO OPERATE PACK NR 1, PACK FAILED AGAIN WITH SMOKE SMELL IN CABIN. RELEASED PACK NR 1 PER MEL. PACK NR 1 SWITCH IS OFF, A/C IS OK FOR SERVICE. REMOVED AND REPLACED NR 1 AIR CYCLE MACHINE. OPERATIONAL CHECK IS GOOD PER AMM 21-51-00, THIS CLEARS MEL. 2L74 4F RTA56NM 20050914001262005091400126 2005 9 14 EM05010 420050901A2230426000183 CONTROL QUADRANT EMB ERJ170ERJ170100 EU COCKPIT SPLIT A USAAK NONE O OTHER ININSP/MAINT 1 EA19801MA3713 000012 THROTTLE LEVER ANGLE SPLIT IN AUTO THROTTLE MODE. MAINTENANCE RELEASED PER MEL 22-3000, CONTROL 0101BO4. TROUBLESHOT WITH CMC. REMOVED AND REPLACED THRUST CONTROL QUADRANT WITH AUTO. OPERATIONAL TEST IS GOOD, THIS CLEARED MEL. 2L74 4F RTA56NM 20050914001272005091400127NM 2005 9 14 05FDEA02843 120050913A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 CABIN - SEAT TRACK ADJACENT TO STA 635 X-11 LOWER FLANGE FOUND CRACKED. CARRIED OUT REPAIR AS PER SRM 53-70-00 FIG 1 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050914001282005091400128NM 2005 9 14 05FDEA02844 120050913A5330 DOUBLER DOUG MD11 MD11 3023602NM ZONE 100 CHIPPED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 CENTER CARGO - DOOR AFT CUTOUT EDGES EXTERIOR EXISTING REPAIR DOUBLER PATCH CHIPPED EDGES. DAMAGED EXISTING REPAIR DOUBLERS ON CENTER CARGO, DOOR AFT CUTOUT AREA REMOVED AS PER SRM 51-33-01 VOLUME II. AND NEW REPAIR DOUBLERS FABRICATED AS PER SRM 53-50- 00 FIGURE 16 VOLUME I. NEW REPAIR DOUBLER INSTALLED AS PER SRM 51-33-01 VOLUME II. THIS REPAIR CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050914001292005091400129EA 2005 9 14 VTZA200500179 120050910A2910AE4096G0060000 LINE CNDAIRCL600 CL6002B19 1900309EA HYDRAULIC SYS LEAKING A VTZAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA27623BR 7192 HYDRAULIC 3 LOW PRESSURE MESSAGE. REPLACED LINE ON 3A PUMP. 2L72 4F RTA21EA 20050914001362005091400136CE 2005 9 14 4511209112005 120050911A771430707227 TRANSDUCER LEAR 45 45LEAR 5170805CE ALIDSGTPE331TPE331201A 0517 WP N2 FAILED E J7SAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SW05415FX 112 P116216C ENGINE AMBER COMPUTER FAULT LIGHT ILLUMINATED ON T/O ROLL BELOW 80 KNOTS. T/O WAS ABORTED AND THE ENG COMPUTER SWITCH WAS CYCLED TWICE BUT, THE FAULT WOULD NOT CLEAR. PRELIMINARY T/S POINTS TO FAILED N2 TRANSDUCER. 2L72 4F3 TRTT00008WIAEXJ STC 20050914001392005091400139EU 2005 9 14 MAC90501 120050912A5315WASI02A FLOORBEAM AEROSPATR42 ATR42300 8680920EU FR 15 CRACKED A MTNAK NONE O OTHER ININSP/MAINT 1 SO33909FX 275 THE LONGITUDINAL FLOORBEAM BL 0 AT FRAME 15 CRACKED NEAR ATTACH POINT TO THE LATERAL FLOORBEAM. CRACK WAS DISCOVERED DURING TROUBLESHOOTING ANOTHER UNRELATED PROBLEM. REPAIR WAS ACCOMPLISHED PER EO 4225001-42-53-32. THIS PART WAS INSTALLED BY STC ST01189W1. 2H72 4T RTA53EU 20050914001422005091400142NM 2005 9 14 2005UALA00950 120050907A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE BS 580 DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29505UA 24626 FWD PIT FRAME IS DENTED 2 EACH PLACES AT BS 580 BETWEEN STR 22L & STR 24L ON INBOARD FLANGE. REPAIRED FRAME FLANGE WITH NESTED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20050915000022005091500002SW 2005 9 15 ALG2005F00064 120050812A7712222375077119 TRANSMITTER BELL 407 407 1182206SW ALLSN 250C 250C47B GL TORQUE FAILED E ALGAO OTHER N FALSE WARNING CLCLIMB 1 SW03617AL 53265 ON CLIMB OUT FROM BASE, TORQUE GAUGE GRADUALLY DECREASED TO ZERO. MAINTENANCE NOTIFIED. REMOVED TORQUE TRANSMITTER SN 57586518, AND INSTALLED SN 57292141. LEAK AND OPS CHECK GOOD. WORK IAW MM. (K) 1G71 3U3 UO H2SW E1GL 20050912002102005091200210EU 2005 9 12 MALA050691 120050903A5420 BUSHING BAC 146 AVRO146RJ85A1500097EU NR 2 PYLON MIGRATED A MALAK NONE O OTHER ININSP/MAINT 1 GL15507XJ E2316 WHILE ACCOMPLISHING C3.IG1 INSPECTION FOUND THE NR 2 ENGINE PYLON TO YOKE LINK BUSHINGS HAVE MIGRATED OUT. 2H74 4F RTA49EU 20050912002162005091200216EU 2005 9 12 MALA050696 120050903A5320 FLOOR SUPPORT BAC 146 AVRO146RJ85A1500097EU FRAME 14 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15507XJ E2316 WHILE ACCOMPLISHING C1 INSPECTION FOUND A FLOOR SUPPORT ANGLE IN THE ELECTRICAL EQUIPMENT BAY AT FRAME 14 CRACKED. 2H74 4F RTA49EU 20050912002452005091200245NM 2005 9 12 USAA051064 120050906A52306547952183X SKIN BOEING737 7374B7 1384702NM CARGO DOOR GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19449US 24893 AFT CARGO DOOR AT UPPER FWD CORNER AREA. REMOVED DAMAGE AND INSTALLED REPLACEMENT STIFFENER AND REPAIR DOUBLER PER EA 96812 AND DWG 65-47952. DEFECT SIZE: .250 GOUGE INTO THE SKIN DOUBLER AND TEE STIFFENER AND PULLEY BRACKET STICKER NR 1888. 2L72 4F RTA16WE 20050912002492005091200249SO 2005 9 12 SWIA200515518 120050906A275012064207615 SELECTOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 NM07271YV6602 6602 120271 ANNUNCIATOR "FLAPS TOO LOW" SOUNDS ON SHORT FINAL WITH FLAPS. REPLACED FLAP HANDLE IAW MM 27-50-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050912002512005091200251NM 2005 9 12 BB05078 120050908A335020131A BATTERY BOEING757 757225 1384959NM EMERGENCY LIGHT DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19606AU 22202 BOS - THE EMERGENCY LIGHTS WERE FOUND INOPERATIVE DURING AN OPERATIONAL CHECK. MAINTENANCE INSTALLED A NEW BATTERY. OPERATIONALLY CHECKS OK. 2L72 4F RTA2NM 20050912002642005091200264NM 2005 9 12 AWXA200501037 120050825A575465C26602108 SKIN BOEING737 7373Y0 1384671NM ZONE 600 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 DURING C16 CHECK DISCOVERED 1 CRACK, .375 INCHES IN LENGTH, LOCATED ON THE BOTTOM OF THE NR 5 SLAT SKIN BELOW THE OUTBOARD AUXILIARY TRACK. MAINTENANCE REMOVED CRACKS FROM NR 5 SLAT SKIN IAW BOEING 737-300 SRM 57-43-01-2. FABRICATED FILLER AND SPLICE PLATE IAW BOEING 737-300 SRM 57-43-01-2. INSTALLED FABRICATED REPAIR PARTS AT THE BOTTOM OF THE NR 5 SLAT, BELOW OUTBOARD AUXILIARY TRACK IAW BOEING 737-300 SRM 57-43-01-2. 2L72 4F RTA16WE 20050913000072005091300007NM 2005 9 13 05FDEA02832 120050910A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 HORIZONTAL STAB RT BARREL NUT BORE NR 19 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08- EA 1-5510-87628 ATTACHMENT 10. CLASSIFIED AS MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20050913000132005091300013WP 2005 9 13 05FDEA02788 120050907A5100S392945221 INSULATION DOUG DC10 DC1010F 3022111WP FUSELAGE BURNED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568053 47807 CAC, FUSELAGE INSULATION BLANKETS SEVERLY BURNED AROUND SYS 1-2 AND SYS 1-3, PNEUMATIC AIR DUCT. CHECKED PNEUMATIC SYSTEMS PER JRH AND LEAK CHECKED,OP'S AND LEAK CHECHED OK.FOUND INSULTION BLANKETS SECURED & TOUCHING DUCT. NEW INSULTATION BLANKETS INSTALLED IAW MM 25-28-00. 2L73 4F A22WE 20050913000432005091300043NM 2005 9 13 05FDEA02821 120050909A5313 LONGERON DOUG MD11 MD11 3023602NM BS 1641 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 CENTER CARGO COMPT, RT STA 1641 LONGERON SPLICE 44R FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL.II. MINOR REPAIR PER GMM 6-2-100. 2L73 4F RTA22WE 20050913000442005091300044NM 2005 9 13 05FDEA02822 120050909A5313 LONGERON DOUG MD11 MD11 3023602NM BS 1661 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 CENTER CARGO COMPT, RT STA 1661 LONGERON SPLICE 46R FOUND CRACKED. REMOVED AND REPLACED AS PER DRAWING AFA 7113 AND SRM 51-31-01 VOL.II. CLASSIFIED AS MINOR REPAIR PER FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20050913000472005091300047NM 2005 9 13 05FDEA02825 120050909A5330 SKIN BOEING727 727227 1384078NM BS 990-1050 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 FUSELAGE SKIN HAS SEVERAL GOUGES FROM BS 990-1050 STRINGER 27L - 26R. REPAIRED PER SRM 53-30-3 2L73 4F A3WE 20050913000522005091300052NM 2005 9 13 UPS05445390 120050821A533065B072012 BEAR STRAP BOEING747 747212B 1384886NM BS 545 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01526UP 21937 INSPECTION TYPE:C FX LOWER FUSELAGE EXTERNAL SKIN SURFACE FWD LAVATORY SERVICE PAN FWD ATT PLATE FOUND CORRODED AT LT STA 545 STR 46L TO STR 47L. CORROSION BLEND OUT THROUGH WHOLE THICKNESS .5 X 1 INCH. FX BS 540 BETWEEN STR 46L TO STR 47L LAV SVC PAN ATTACHED BEAM STRAP REPAIRED AS PER HX RS R-53-21-35363 & ENGINEERING FILE NUMBER : 747-53-20283. FOLLOW THE INSP INTERVAL AS PER SRM 53-30-03 FIG 1 TABLE IV USING EXTERNAL LFEC INSP METHOD. 2L74 4F A20WE 20050913000542005091300054NM 2005 9 13 UPS05545376 120050826A5315 FLOORBEAM BOEING757 75724APF 1384969NM BS 620 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01403UP 23725 INSPECTION TYPE:C MAIN CARGO BAY FLOORBEAM CORRODED BS 620 LBL 4-10. REPAIR PER SRM 51-20-06 AND ER 05-3962. 2L72 4F RTA2NM 20050913000562005091300056WP 2005 9 13 UPS05845377 120050909A33505708458503 BATTERY PACK DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT FAILED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01808UP 46008 INSPECTION TYPE:N/A DURING ROUTINE MX, EMERGENCY LIGHTING WOULD NOT TEST. REMOVED AND REPLACED BATTERY PACK ASSY IAW AMM 33-50-01-2, EMERGENCY LIGHTING OPS CHECKS NORMAL. 2L74 4F RT4A25 20050913000682005091300068WP 2005 9 13 UPS05845394 120050808A5730 DOUBLER DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE: C3, LT WING L/E LOWER INTERNAL DOUBLER IS CRACKED AT DRAIN HOLE XFS 597.500. REMOVED, FABRICATED, AND INSTALLED INTERNAL DOUBLER IAW DC-8 SRM 57-3- 0, 51-1-20D, AND 51-1-21. 2L74 4F RT4A25 20050913000692005091300069WP 2005 9 13 UPS05845395 120050828A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE: C3, LEFT WING L/E UPPER SKIN IS CRACKED AT XW 485. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1 FIG 38. 2L74 4F RT4A25 20050913000852005091300085NM 2005 9 13 SWAA052748 120050907A335090083 BATTERY PACK BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29382SW 26588 DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT UPPER & LOWER LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050913000872005091300087NM 2005 9 13 SWAA052750 120050909A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29486WN 33852 EEPLS TRACK AT FWD END LOOSE. REMOVED AND REPLACED EEPLS TRACK PER MM. 2L72 4F RTA16WE 20050913001092005091300109NM 2005 9 13 SWAA052763 120050908A3350MS155721 BULB BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29776WN 30591 DURING SCHEDULED MV2 CHECK, FOUND AFT EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050913001102005091300110NM 2005 9 13 SWAA052764 120050908A335010107451 SIGN BOEING737 7377H4 1384404NM AFT GALLEY BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29782SA 29808 R2 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED EXIT SIGN LIGHT ASSY PER MM. 2L72 4F RTA16WE 20050913001202005091300120EA 2005 9 13 SWIA200515018 120050513A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07963SW RIGHT OUTBOARD CLIP AT FS 280.00 RBL IS CRACKED, ITEM FOUND AT C-CHECK INSPECTION. BRACKET REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-21-11. 2L72 4F RTA21EA 20050913001242005091300124 2005 9 13 SWIA200515526 420050905A3418C818022 SERVO EMB 120 EMB120ER 3260203SO STICK SHAKER WEAK A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07224SW7991 7991 120294 FO'S STICK SHAKER VERY WEAK. REPLACED FO'S STICK SHAKER SERVO IAW EMB 120 AMM 27-34-04. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050913001252005091300125EA 2005 9 13 SWIA200515527 120050907A2741 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB TRIM INOPERATIVE A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07463SW 7820 FO SIDE STAB TRIM INOP. REPLACED FO'S STAB TRIM SWITCH IAW 27-41-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050913001282005091300128NM 2005 9 13 05FDEA02799 120050907A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 HORIZONTAL STAB LT BARREL NUT BORE NR 1 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 - EA 1-5510-87628 ATTACHMENT 2. CLASSIFIED AS MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20050913001302005091300130NM 2005 9 13 05FDEA02795 120050907A5753 ATTACH FITTING DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 LT WING, O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. CORROSION REPAIR CARRIED OUT AS PER EA 1-5750-87631. 2L73 4F RTA22WE 20050913001372005091300137EA 2005 9 13 SWIA200515533 120050911A276052C52610A1 MANIFOLD CNDAIRCL600 CL6002B19 1900309EA GROUND SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION LDLANDING 1 NM07465SW 7845 OUTBOARD SPOILER CAUTION ON TOUCHDOWN. REPLACED MANIFOLD IAW MM 27-63-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050913001392005091300139EA 2005 9 13 SWIA200515535 120050906A2760C13045BA04 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07707SK169 169 10003 SPOILER/STAB FAULT STATUS MSG ON TAXI. REPLACED BOTH SSCU'S IAW 27-61-05. OPERATIONAL CHECK GOOD, C13045BA04; SN2OFF 796. 2L72 4F RTA21EA 20050913001412005091300141SO 2005 9 13 SWIA200515537 120050601A5311 FRAME EMB 120 EMB120ER 3260203SO FR 13 CRACKED A SWIAO OTHER O OTHER ININSP/MAINT 1 NM07229SW 120305 ANGLE OPPOSITE FROM COCKPIT LT FLOOR PROP AT FRAME 13 CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE OPPOSITE FROM COCKPIT LT FLOOR PROP AT FRAME 13 IAW SRM 51-40-02. 2L72 4T RTA31SO 20050913001602005091300160NM 2005 9 13 05FDEA02800 120050907A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 HORIZ STAB RT BARREL NUT BORE NR 36 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 - EA 1-5510-87628 ATTACHMENT 1. CLASSIFIED AS MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20050913001652005091300165NM 2005 9 13 CALA0500305 120050910A53226546554 SHEAR TIE BOEING737 7373T0 1384582NM BS 847 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2763305 23356 INSPECTION FOUND SHEAR TIE AT STA 847 BETWEEN S27L AND S27R, LBL 6 TO RBL 6 CORRODED. THE CORRODED SECTION OF SHEAR TIE WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-00-07, FIGURE 208. 2L72 4F RTA16WE 20050914000032005091400003WP 2005 9 14 ABXA050215 120050822A5312991015529 PRESSURE PANEL DOUG DC9 DC941 302207NWP LT MLG WW CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23956AX 47620 AREA OF EXFOLIATION ON UPPER PRESSURE PANEL, MAIN FRAME AREA. REMOVED AND REPLACED DOUBLERS IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20050914000132005091400013EU 2005 9 14 YENA200564 120050905A3350F100055000 SIGN AIRBUS320 A320232 3930326EU EMERGENCY LIGHTSFAILED A YENAO OTHER O OTHER LDLANDING 1 EA15598JB 2314 FWD EMERGENCY EXIT LIGHT INOP WHEN ARMED AND GEAR DOWN. REMOVED AND REPLACED EMERGENCY EXIT SIGN (40 WL) ABOVE R1 DOOR IAW AMM 33-51-16, OPS CHECK GOOD. THE PART IS CONSIDERED EXPENDABLE. 2L72 4F RTA28NM 20050914000152005091400015EA 2005 9 14 QXEA200501220 120050909A2120 ODOR CNDAIRCL600 CL6002C10 1390015EA CABIN DETECTED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM09614QX 10049 DEN - ON FLIGHT 2457, AFTER STARTING FUEL BOOST PUMP TEST, A STRONG SMELL OF JET A WAS NOTICED IN THE BACK OF THE AIRCRAFT. INSPECTED AFT EQUIPMENT BAY AND FOUND A STRONG ODOR OF JET FUEL, BUT NO NOTICEABLE LEAKS. MAINTENANCE INSPECTED THE APU AND FUEL LINES IN THE AFT EQUIPMENT AREA WITH NO DEFECTS NOTED. RAN BOTH ENGINES, NO SMELLS OR LEAKS NOTED. WITH BOOST PUMPS BOTH ON AND OFF NO SMELL OR LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2L72 4F RTA21EA 20050914000212005091400021CE 2005 9 14 DXTA200500957 120050905A215011342402 EVAPORATOR CESSNA500 560CESSNA 2076750CE A/C PACK FAILED E DXTAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07375QS9120 5600375 STRONG BURNING ODOR IN THE COCKPIT AND NOTICED BY PAX IN THE AFT CABIN ON LANDING. ODOR LINGERED UNTIL SHUT DOWN. TROUBLESHOT DISCREPANCY TO INTERNAL FAILURE OF THE FREON AIR CONDITIONING FORWARD EVAPORATOR ASSEMBLY. INSPECTED LOCAL AREA NO OTHER DISCREPANCY NOTED. DISCHARGED AIR CONDITIONING SYSTEM. REMOVED FORWARD EVAPORATOR. INSTALLED A NEW ONE. LEAK CHECKED GOOD, EVACUATED AND SERVICED IT WITH 2.5 LBS OF R-134 A REFRIGERANT. OPERATIONAL CHECK, CHECKED GOOD PER CITATION 560 MM CHAP. 21-52-00. 2L72 4F RTA22CE 20050914000272005091400027NM 2005 9 14 CALA0500307 120050913A3350D71701100 BATTERY PACK BOEING737 737824 13844BZNM EMERGENCY LIGHT INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2724224 28933 SOME EMERGENCY LIGHTS IN REAR OF AIRCRAFT WERE FOUND INOPERATIVE WHILE AIRCRAFT WAS UNDERGOING AN "S" CHECK. THE LT REAR CABIN BATTERY PACK WAS REMOVED AND REPLACED. 2L72 4F RTA16WE 20050914000442005091400044NM 2005 9 14 2005UALA00944 120050905A3397794640 CABLE BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT DAMAGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29179UA 25158 EEL LT INOP LT SIDE WALL LAV 111. REPAIRED FEEDER CABLE. 2L74 4F4 FRTA20WE E24NE 20050914000472005091400047NM 2005 9 14 2005UALA00947 120050905A3350362624 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29179UA 25158 EEL INOP SEAT 38LH. REPLACED EEL LAMP. 2L74 4F4 FRTA20WE E24NE 20050914000502005091400050NM 2005 9 14 05FDEA02752 120050905A5347 SEAT TRACK DOUG MD11 MD11 3023602NM BS 1019 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 UPPER CARGO, SEAT TRACK RBL 47 CRACKED AT STA 1019. REPAIRED AS PER SRM 53-70-00. 2L73 4F RTA22WE 20050914000512005091400051NM 2005 9 14 05FDEA02738 120050902A5330 SKIN BOEING727 727233 138408ANM BS 620 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25218FE 21101 FOUR HOLES BS 620 STR 2L BUCKTAILS BEHIND EXISTING STRUCTURE. REPAIRED HOLES, BS 620, STR 2L PER FED-EX EA 7-5330-92260A. 2L73 4F RTA3WE 20050914000552005091400055WP 2005 9 14 IXXA05RNG049S 120050818A5512 SKIN DOUG DC8 DC862F 3021972WP HORIZONTAL STAB DENTED B IXXAK NONE O OTHER ININSP/MAINT 1 SW1171CX * 3317 45961 DURING INSPECTION CHECK, SKIN DENT AND SCRATCH DAMAGE WAS FOUND ON THE LEFT HORIZONTAL STABILIZER LEADING EDGE AT UPPER PLATING AROUND L/E STATION XFS 146.00. REMOVED DAMAGE AREA AND DOUBLER WAS INSTALLED IAW EWO ATI 55-05 & EO ATI-071905. EDDY CURRENT INSPECTION WAS PERFORMED IAW SPM TP-MDC-093K393 PROCEDURE 06-10-01.001 AND NO CRACKS WERE FOUND. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR. 2L74 4F 4A25 20050914000582005091400058WP 2005 9 14 UPS05845368 120050814A5320375025U1 SPLICE DOUG DC8 DC871F 302199DWP FS 450 L31R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 INSPECTION TYPE:C1 SPLICE FITTING AT FS 450 L31R IS CRACKED. REMOVED AND REPLACED SPLICE FITTING AT FS 450 L31R IAW DWG 5754814 AND SRM 51-1-20D. 2L74 4F RT4A25 20050914000662005091400066WP 2005 9 14 ARWA20050905 120050712A5420 STRUCTURE DOUG DC8 DC863F 302198FWP NR 3 PYLON CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19784AL 46135 DURING C-CHECK INSPECTION, THE FOLLOWING WAS FOUND; NR 3 PYLON FOOT STOOL INBOUND SIDE WITH 1.750 INCH CRACK. 2L74 4F 4A25 20050914000762005091400076EU 2005 9 14 AALA20050569 120050904A2780 DRIVE UNIT AIRBUS300 A300B4605R 3930308EU LE SLATS INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2114061 471 MIA - AIRCRAFT DIVERTED TO MIA WITH DUAL LEADING EDGE INDICATION PROBLEMS. REPLACED POWER DRIVE UNIT AND NUMBER THREE JACKSCREW. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20050914000852005091400085NM 2005 9 14 AALA20050578 120050905A33971703663 SOCKET BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21353AA 24034 SFO - EMERGENCY EGRESS LIGHT AT SEAT ROW 22AB INOPERATIVE. REPLACED CONNECTOR SOCKET FOR EMERGENCY EGRESS LIGHT AT SEAT ROW 22AB. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050914000912005091400091NM 2005 9 14 USAA051082 120050909A5320 PLATE BOEING737 7374B7 1384702NM BS 1016 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19776AU 24934 CORROSION LT DECK PLATE AT STA 1016 FWD OF PRESS BULKHEAD. REMOVED DAMAGED AREA PER SRM 52-70-13, FABBED REPAIR DOUBLER, FILLER, INSTALLED REPAIR, DEFECT SIZE: 2' APPROX EXFOLIATION CORROSION. 2L72 4F RTA16WE 20050914001072005091400107NM 2005 9 14 C1HA200581014 120050912A5230 SKIN BOEING727 7272S7 138407ZNM ZONE 100 CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15681CA 22020 AFT CARGO DOOR HAS CRACK ABOVE THE FWD BLOW OUT PNL BS 950E INNER SKIN. CUT OUT DAMAGED AREA DIM 2 X .5 INCH AND FABBED DOUBLER FROM 7075T6 .050 PO 9002507 DIM 3.5 X 3 INCHES IAW 727 SRM 52-30-1 FIG 5 AND 51-40-2 FIG 1. DOUBLER TREATED, PRIMED AND INSTALLED IAW 727 SRM 51-40-2 FIG 1. 2L73 4F A3WE 20050914001152005091400115NM 2005 9 14 05FDEA02813 120050908A5230 GUSSET BOEING727 7272S2F 1384O81NM FWD CARGO DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25211FE 22933 FWD CARGO DOOR GUSSET IS CRACKED AFT SIDE 3RD BRKT FROM TOP OF DOOR. REMOVED AND REPLACED GUSSET IAW SRM 51-30-2. 2L73 4F A3WE 20050914001332005091400133NM 2005 9 14 MZZA0500005 120050912A3350D71702030 CHARGER BOEING737 737824 13844BZNM EMERGENCY LIGHT INOPERATIVE A MZZAK NONE O OTHER ININSP/MAINT 1 WP1314240 28952 THE EMERGENCY EXIT LIGHTS AT FRONT ENTRY DOOR (L-1) FORWARD EXTERIOR AND OVERHEAD BIN FORWARD OF ROW 2B WERE FOUND INOPERATIVE. THE BATTERY CHARGER WAS REMOVED AND REPLACED IAW MM 33-51-06. 2L72 4F RTA16WE 20050914001352005091400135NE 2005 9 14 05FDEA02842 220050912A7230 CASE BOEING727 727200 138407ENM PWA JT8 JT8D17 52049NE COMPRESSOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25211FE 22933 689876 NR 2 ENG RT FWD FAN FRAME CASE HAS SEVERAL CRACKS. DYE PENETRANT INSPECTION DONE IAW SOPM 20-20-02 FOUND 1EA CRACK AT 3 O'CLOCK POSITION. CRACK STILL WITHIN LIMITS IAW PW JT8D MM72-00-00. STOP DRILLED CRACK IAW PW JT8D MM 72-00-00. REINSPECT CASE EVERY 200 HRS PER MM 72-00-00 PG 662 B (1) (B). 2L73 4F4 FRTA3WE E2EA 20050914001372005091400137NM 2005 9 14 SCNA05004 120050911A3350 BATTERY PACK BOEING737 7378Q8 13844BXNM EMERGENCY LIGHT INOPERATIVE A SCNAK NONE O OTHER ININSP/MAINT 1 GL15809SY 30683 PER WORKCARD 330100000 DISCOVERED FWD OVERWING EMERGENCY LIGHTS INOP (INTERIOR). REMOVED AND REPLACED FWD OVERWING EMERGENCY LIGHT BATTERY PACK & FUSES. OPS CHECKS NORMAL IAW 33-51-66-960-805. 2L72 4F RTA16WE 20050914001412005091400141EU 2005 9 14 2005UALA00949 120050907A2133 OUTFLOW VALVE AIRBUS320 A320232 3930326EU CABIN PRESSURE FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29489UA 1702 LOST CABIN PRESSURE AT FLT LEVEL 270. CABIN PRESSURE PARTIALLY MAINTAINED DOWN TO 12,000 FT. FLIGHT REQUESTED LOWER ALTITUDE AND RETURNED TO GROUND. AT FL270 THE AIRCRAFT LOST CABIN PRESSURE. CABIN PRESSURE MADE IT TO 12,000 FEET. THE FLIGHT REQUESTED LOWER ALT AND RETURNED TO GROUND. ACCOMPLISHED MT21-001, TESTED OK. CABIN PRESSURE SYSTEM 1 & 2 FAULT. CFDS IDENTIFIED VALVES AS FAULTED. REPLACED OUTFLOW VALVE 10HL PER MM-21-31-51. ALSO REPLACED CPC'S 1 & 2 PER MM-21-31-34. 2L72 4F RTA28NM 20050914001442005091400144EU 2005 9 14 2005UALA00952 120050908A5320 FLOOR SUPPORT AIRBUS320 A320232 3930326EU FR 66-70 CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29441UA 751 CORROSION AT AFT GALLEY FLOOR SUPPORT 66-70. 2L72 4F RTA28NM 20050914001462005091400146NM 2005 9 14 2005UALA00954 120050827A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE BS 1715 STR 28 DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29588UA 26717 LOWER AFT FUSELAGE LIGHTNING STRIKE AT STA 1715, S28L. TRIMMED OUT DAMAGES, ACP HEFC INSP, NO CRACK FOUND. FABRICATE, ALODINE, PRIME AND INSTALL REPAIR DOUBLER. 2L72 4F4 FRTA2NM E17NE 20050915000042005091500004EA 2005 9 15 VNAA0508026 120050827A2150VP1240E00 VALVE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT A/C PACK FAILED A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL05230PS3227 7904 DURING CLIMBOUT WITH THE RT PACK DEFERRED PER MEL 21-51-01(C), THE LT PACK TEMP CAUTION MESSAGE ILLUMINATED. THE CREW FOLLOWED THE QRH AND RETURNED TO CLT. MAINTENANCE REMOVED & REPLACED THE DUAL POSITION VALVE IAW CRJ200 AMM 21-21-10-400-801. OPERATIONAL CHECKS WERE GOOD. THE MELS WERE CLEARED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050915000112005091500011NM 2005 9 15 2005UALA00955 120050813A5320 SHEAR WEB BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29588UA 26717 CABIN CORROSION UNDER MIKATA BLOCK AT SHEAR WEB, BS APPROX RBL 56.0. REMOVE CORROSION, ACP HEFC INSP, NO CRACK FOUND. INSTALLED REPAIR DOUBLER PER SRM 41-40-02. 2L72 4F4 FRTA2NM E17NE 20050915000132005091500013NM 2005 9 15 2005UALA00957 120050908A3350276005 FUSE BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT SHORTED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29194UA 26892 TWO FWD EMERGENCY LIGHT ASSY'S AT LT BODY FAIRING INOP. REPLACED FUSE. 2L74 4F4 FRTA20WE E24NE 20050915000152005091500015EU 2005 9 15 USAA050934 120050729A5315 FLOORBEAM AIRBUSA319 A319112 3930323EU CABIN CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19723UW 1109 PIT - FOUND FLOORBEAM CORRODED .75 INCH DIAMETER AREA, FLOORBEAM AT Y1292 LEFT AT C-20. CUT OUT DAMAGE, INSTALLED FILLER AND ANGLES PER SRM 53-10-14. CORROSION LEVEL 1, TASK JA-220-53500. 2L72 4F RTA28NM 20050915000202005091500020NM 2005 9 15 2005UALA00960 120050909A3350362624 LAMP BOEING737 737322 1384676NM ROW 15 BURNED OUT A UALAK NONE L NO TEST ININSP/MAINT 1 WP29333UA 24228 EEL LAMPS AFT OF ROW 15 INOP. REPLACED SHORTED LAMP AT ROW 21. 2L72 4F RTA16WE 20050915000222005091500022NM 2005 9 15 05FDEA02839 120050912A5310 SHEAR TIE BOEING727 727200 138407ENM BS 700 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25268FE 21674 CORROSION FWD CARGO FLOOR SHEAR TIE BS 700, BL 0, WL 148. REMOVE AND REPLACE SHEAR TIE PER SRM 53-10-1 2L73 4F RTA3WE 20050915000242005091500024NM 2005 9 15 05FDEA02848 120050913A5320 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 CENTER CARGO - LONGERON SPLICE ADJACENT TO STA 1541 L-38 RIGHT BRIM AREA FOUND CRACK. STA 1541 LONGERON 38 RT CRACK LONGERON SPLICE REMOVED AS PER SRM 51-33-01 VOL II. NEW LONGERON SPLICE MACHINED AS PER DWG A5A7114. NEW LONGERON SPLICE INSTALLED AS PER SRM 51-33-01 VOL II. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050915000272005091500027NM 2005 9 15 SWAA052773 120050911A3350101073 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR EXTERNAL EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS PER SRM. 2L72 4F RTA16WE 20050915000282005091500028NM 2005 9 15 SWAA052774 120050910A53306545765 SKIN BOEING737 7373H4 1384600NM BS 519 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29335SW 23939 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 519, STR 14L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050915000292005091500029 2005 9 15 SWAA052775 420050912A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29432WN 33715 R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20050915000322005091500032 2005 9 15 SWAA052778 420050809A25656557450 COVER BOEING737 7377H4 1384404NM L1 DOOR SLIDE LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29728SW 27860 L1 DOOR EMERGENCY EVAC SLIDE COVER LOOSE. SECURED COVER PER MM. 2L72 4F RTA16WE 20050915000362005091500036WP 2005 9 15 AALA20050588 120050912A4920 O-RING DOUG DC9 DC982 3022082WP THERMOSTAT VALVEINOPERATIVE A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW217509 49803 EWR INFLIGHT T1147/11SEP ACRID SMOKE IN CABIN IMMEDIATELY AFTER TAKEOFF. PACKS SHUT OFF AND LANDED EWR WITHOUT INCIDENT. REPLACED O-RING AT THERMOSTAT VALVE OF APU. PERFORMED PACK BURN OUT AND ENGINE HIGH POWER RUN UP WITH NO SMOKE NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050915000372005091500037WP 2005 9 15 AALA20050582 120050909A49905940405503 APU DOUG DC9 DC982 3022082WP APU BAY LEAKING A AALAA UNSCHED LANDING KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21214AA 49162 DFW INFLIGHT T2334/9SEPT SMOKE ENTERED CABIN JUST AFTER TAKEOFF ROLL LIFT OFF. SMOKE WAS GREENISH IN COLOR AND LASTED ABOUT FIVE MINUTES AND THEN BEGAN TO DISSIPATE. LANDED AT DFW WITHOUT INCIDENT. FOUND OIL IN APU. REPLACED APU IN ACCORDANCE WITH WORK CARD 21 96 01. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050915000382005091500038NM 2005 9 15 AALA20050592 120050829A5315 FLOORBEAM BOEING767 767323 1385205NM BS 764 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21389AA 27449 AFW FLOORBEAM AT STATION 764 HAS CORROSION REMOVAL BEYOND SRM LIMITS. AREA WAS 1.0 INCH BY .030 INCH WITH A DEPTH OF .030 INCH. FABRICATED REPAIR STRAP FROM 301 AND A HALF HARD STAINLESS STEEL .063 THICK. ALODINED ALL BARE ALUMINUM SURFACES. FINISHED BLEND AND REPAIR PARTS WITH TWO COATS OF BMS 10-11 PRIMER. FILLED BLENDS WITH BMS592. INSTALLED REPAIR STRAP WITH BMS595 SEALANT USING BACB30NW6 FASTENERS. INSTALL BALANCING STRAP ON BOTTOM WITH BACB30MY6 FASTENERS. 4 6D SPACING. 2L72 4F RTA1NM 20050915000392005091500039NM 2005 9 15 AALA20050593 120050902A3350D71702100 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21973AN 29548 TUL EMERGENCY LIGHTS AT AFT LEFT GALLEY (STATION 967), FIRST CLASS SEATS (STATION 328), AND MID CABIN (STATION 727) FAILED OPERATIONAL CHECK. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN AFT LEFT GALLEY, FIRST CLASS SEATS, AND MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20050915000402005091500040NM 2005 9 15 AALA20050581 120050909A495039244421 VALVE DOUG MD80 MD83 3023681NM APU INOPERATIVE A AALAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 SW219630A 53561 DEN INFLT T887/09 SEPT SEVERAL MINUTES AFTER ENGINE WAS ON WING ICE, SMOKE WAS PRESENT IN COCKPIT AND CABIN. DIVERTED TO DEN AND LANDED WITHOUT INCIDENT. TURNED ANTI ICE ON AGAIN AND SMOKE REAPPEARED. PRESSURE ABNORMAL LIGHT ILLUMINATED. REPLACED ANTI ICE PRESSURE REGULATING AND SHUT OFF VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RT 20050915000412005091500041NM 2005 9 15 AALA20050584 120050909A3397MS35659364 WIRE HARNESS BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21389AA 27449 JFK EMERGENCY LIGHT AT SEAT 22H INOPERATIVE. REPLACED SEAT HARNESS FOR EMERGENCY LIGHT AT SEAT 22H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050915000422005091500042NM 2005 9 15 AALA20050594 120050902A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21922AN 29523 TUL EMERGENCY LIGHTS IN CABIN FAILED FUNCTIONAL CHECK. REPLACED BATTERY PACKS AT M1674 AND M1675 FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20050915000432005091500043WP 2005 9 15 AALA20050583 120050909A323039567851 LINK DOUG DC9 DC982 3022082WP MLG INOPERATIVE A AALAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SW21269AA 49292 DFW INFLIGHT T1316/9SEPT SEVERE VIBRATION AFTER LANDING GEAR WAS RETRACTED ON TAKEOFF IN AREA OF LANDING GEAR. FOUND RIGHT NOSE GEAR DOOR EXTENDED. REPLACED RIGHT HAND NOSE LANDING GEAR DOOR LINK ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050915000452005091500045NM 2005 9 15 AALA20050586 120050910A3350 LIGHT BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21371AA 25198 DFW OVERWING EMERGENCY LIGHT FORWARD EXTERNAL INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR OVERWING EMERGENCY LIGHT FORWARD EXTERNAL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050915000462005091500046NM 2005 9 15 P5CA0501398 120050909A750077385619 CHECK VALVE BOEING747 747230B 1384889NM GE CF6 CF650E2 30018NE NR 3 ENGINE FAILED A P5CAB EMER. DESCENT RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 EA15508MC 21644 528420 AT FL 37.0 NR 3 ENGINE COMPRESSOR STALLED, ALL PARAMETERS NORMAL. OPS OK AT LOWER ALTITUDE. BORESCOPE PER MM 72-00-00 PG 680P, NO FINDINGS. FOUND 8TH STAGE CHECK VALVE FAILED. REPLACED SAME, OPS NORMAL PER 36-11-02. 2L74 4F4 F A20WE E23EA 20050915000492005091500049EU 2005 9 15 SF20050904 120050904A3240 BRAKE ASSY SAAB SF340 SF340A 7850100EU MLG MALFUNCTIONED A UHLAO OTHER K FLUID LOSS NRNOT REPORTED 1 GL17121CQ 121CQ A/C 121 FLIGHT 7521 SCE-IAD, 9/4/05. UPON ARRIVAL IN IAD, PILOT REPORTS WHEN PARKING AT THE GATE AND THE BRAKES FELT SOFT. ON POST FLIGHT, FOUND HYDRAULIC PUDDLE UNDER RIGHT GEAR. MAINTENANCE INSPECTED AND FOUND THAT THE NR 3 BRAKE HAD RUPTURED AND DAMAGED THE INSIDE OF THE TIRE WHERE IT IS CONTACT WITH THE BRAKE. 2L72 4T RTA52EU 20050915000502005091500050EU 2005 9 15 SF200509121 120050912A2910 WARNING LIGHT SAAB SF340 SF340A 7850100EU HYD SYSTEM ILLUMINATED A UHLAO OTHER J WARNING INDICATION DEDESCENT 1 GL1743SZ 340A043 9-12-2005, FLIGHT 7571 FROM IAD TO DAY, ON DESCENT, AIRCREW RECEIVED HYD LIGHT ON WITH BOTH MAIN AND EMERGENCY ACCUMULATOR'S LOW. AIRCREW FOLLOWED MEMORY ITEMS AND QRH AND LANDED A/C IN DAY. 2L72 4T RTA52EU 20050915000512005091500051WP 2005 9 15 AALA20050587 120050912A33500200335001 LIGHT DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW219404V 53140 LGA EMERGENCY LIGHT IN AFT TAIL COMPARTMENT INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT IN AFT TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050915000542005091500054NM 2005 9 15 PCSA0906051 120050906A2751HIO10271 PROXIMITY SWITCH BOEING727 727233 138408ANM NR 5 SLAT FAULTY A PCSAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO29994AJ 20942 FLIGHT 713 DURING TAKEOFF ROLL OUT OF MIA CREW REPORTED NUMBER (5) LEADING EDGE SLAT AMBER LIGHT ILLUMINATED ON FLIGHT ENGINEERS PANEL. THE CREW ABORTED THE TAKEOFF & RETURNED TO THE BLOCK WITHOUT ANY FURTHER INCIDENT. MAINTENANCE FOUND NUMBER (5) LEADING EDGE SLAT POSITION INDICATING SWITCH DEFECTIVE, NUMBER (5) L/E SLAT POSITION SWITCH WAS REMOVED AND REPLACED. FUNCTIONALLY CHECKED GOOD IAW BOEING 727 MM CH 27-82-11. A HIGH ENERGY STOP INSPECTION WAS ALSO ACCOMPLISHED IAW BOEING 727 MM CH 5-51-121, NO DEFECTS NOTED. AIRCRAFT WAS RETURNED BACK TO SERVICE. 2L73 4F RTA3WE 20050915000552005091500055NM 2005 9 15 MZZA0500004 120050907A3350D71702030 CHARGER BOEING737 737824 13844BZNM EMERGENCY LIGHT INOPERATIVE A MZZAK NONE O OTHER ININSP/MAINT 1 WP1314240 28952 THE EMERGENCY EXIT LIGHTS ON OVERHEAD BIN AT ROWS 14, 16, 19, 21, AND 26 DEF WERE FOUND INOPERATIVE. THE BATTERY CHARGER WAS REMOVED AND REPLACED IAW MM 33-51-06. 2L72 4F RTA16WE 20050915000572005091500057EA 2005 9 15 VNAA0508027 120050827A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT WINGLET CRACKED A VNAAK NONE O OTHER ININSP/MAINT 1 GL05256PS 7937 DURING THE INTERMEDIATE INSPECTION THE CREW DISCOVERED A CRACK AND DELAMINATION DAMAGE ON THE LEFT WINGLET TRAILING EDGE FAIRING. AFTER INSPECTION THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE PERFORMED A TEMPORARY REPAIR IAW BOMBARDIER REO 601R-57-31-668. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050915000592005091500059EA 2005 9 15 VNAA0508028 120050828A2700 FCU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A VNAAO OTHER F FLT CONT AFFECTED CRCRUISE 1 GL05218PS 7885 DURING CRUISE FLIGHT WITH FLAPS AT 0 DEGREE THE FLAPS FAIL MESSAGE ILLUMINATED. THE CREW FOLLOWED THE QRH AND PERFORMED A NO FLAP LANDING AT DESTINATION. MAINTENANCE INTERROGATED THE MDC, FECU, AND SDU. NO FAULTS WERE DISPLAYED. THE FLAP SYSTEM WAS RESET AND OPERATIONALLY CHECKED GOOD IAW CRJ200 SL 27-084. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050915000612005091500061EA 2005 9 15 VNAA0508030 120050829A2760 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE SPOILERONS MALFUNCTIONED A VNAAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL05708PS 10160 ON FINAL APPROACH, APPLICATION OF THE FLIGHT SPOILER LEVER RESULTED IN I/B SPOILERONS & I/B FLT SPLRS CAUTION MESSAGES. THE CREW FOLLOWED THE QRH AND LANDED SAFELY. MAINTENANCE RESET THE SSCU IAW CRJ700 SL-27-028. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050915000622005091500062EA 2005 9 15 VNAA0509006 120050907A2750 FCU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A VNAAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL05244PS 7912 WITH FLAPS AT 45 DEGREES ON APPROACH THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED. THE CREW MADE A NORMAL LANDING. MAINTENANCE RESET THE FECU IAW CRJ200 SL-00-001. OPERATIONAL CHECKS WERE PERFORMED 5 TIMES AND WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050915000632005091500063EA 2005 9 15 VNAA0509001 120050905A2150 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT A/C PACK ILLUMINATED A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL05246PS 7920 DURING CLIMBOUT, WITH THE LT PACK MEL'D, THE RT PACK HIGH PRESS MESSAGE ILLUMINATED. THE CREW FOLLOWED THE QRH AND RETURNED TO DCA. MAINTENANCE OPERATIONALLY CHECKED THE RT PACK IAW CRJ200 AMM 21-51-00-710-801 AND WAS UNABLE TO DUPLICATE THE DISCREPANCY. NO DEFECTS WERE FOUND. ALL OPS CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050915000642005091500064EA 2005 9 15 VNAA0509003 120050905A3244299K631 TIRE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE MLG FAILED A VNAAO OTHER O OTHER LDLANDING 1 GL05258PS17 7941 AFTER LANDING INSPECTION REVEALED NR 2 MLG TIRE TREAD SEPARATION AND DAMAGE TO THE LT INBOARD FLAP. MAINTENANCE REPLACED THE WHEEL/TIRE ASSY IAW CRJ200 AMM 32-41-01-000(400)-801. THE AIRCRAFT WAS THEN FERRIED TO DAY WHERE MAINTENANCE REMOVED AND REPLACED THE LT INBOARD FLAP IAW CRJ200 AMM 27-54-01-400-801. ALL OPERATIONAL AND RIG CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050915000652005091500065EA 2005 9 15 VNAA0509002 120050905A2750 FCU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A VNAAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL05244PS 7912 WITH FLAPS AT 45 DEGRESS ON FINAL APPROACH THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED. THE CREW REPORTED NO ASYMMETRY AND MADE A NORMAL LANDING. MAINTENANCE RESET THE FECU IAW CRJ200 SL-00-001. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050915000672005091500067EA 2005 9 15 REXA200500118 120050912A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A REXAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO25821AY 8021 FLAP FAIL MESSAGE. COMPLIED WITH AD 98-20-01. NO DISCREPANCIES NOTED. UNDER 72 HOURS FLAP WATCH. 2L72 4F RTA21EA 20050915000682005091500068EA 2005 9 15 REXA200500119 120050912A3260 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA MLG ILLUMINATED A REXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO258477R 7477 GEAR DISAGREE WARNING MESSAGE AND GEAR DISAGREE AURAL WARNING AFTER TAKEOFF. PERFORMED QUICK REFERENCE HANDBOOK (QRH) AND WAS SUCCESSFUL ON LANDING GEAR DOWN. RETURNED TO AIRPORT, LANDING UNEVENTFUL. 2L72 4F RTA21EA 20050915000702005091500070NM 2005 9 15 05FDEA02846 120050913A5320 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 CENTER CARGO LONGERON SPLICE BRIM AREA SUSPECT CRACK AT STA 1541 ADJACENT TO LONGERON 37 RIGHT HAND. SPLICE REMOVED AS PER SRM 51-33-01 VOL II. NEW LONGERON SPLICE MACHINED AS PER DWG A5A7114. NEW LONGERON SPLICE INSTALLED AS PER SRM 51-33-01 VOL II. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050915000712005091500071NM 2005 9 15 05FDEA02847 120050913A5311 FRAME DOUG MD11 MD11 3023602NM ZONE 200 NICKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 MAIN DECK - DVI CARRIED OUT ON INTERIOR FUSELAGE, NICK FOUND ON FRAME 535 LEFT HAND AT G-NET CAUSED BY SUPPORT YOKES. MAIN DECK STATION 535 LEFT HAND FRAME REPAIRED AS PER DWG SRZ-53-503. THIS REPAIR CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050915000722005091500072EU 2005 9 15 DHL2005366003 120050913A2611FSD200500 SMOKE DETECTOR AIRBUS300 A300B4203 3930306EU FAULTY A DHLABA EMER. DESCENT UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01366DH 249 SMOKE LIGHT ILLUMINATED DURING ROTATION EMERGENCY & ABNORMAL PROCEDURES PERFORMED. REPLACED FAULTY 4R SMOKE DETECTOR AND TESTED PER A/B M/M 26-14-0. CHECKS SERVICE. 2L72 4F RTA35EU 20050915000732005091500073NM 2005 9 15 DHL2005780003 120050913A3210 LANDING GEAR BOEING727 727223 1384074NM MAINS VIBRATION A DHLAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 SO01780DH 22006 VIBRATION FELT ON T/O ROLL, SUSPECT DRAGGING BRAKE. REJECTED T/O. INSPECTED BOTH MAIN LANDING GEARS AND RELATED BRAKES AND COMPONENTS AWO NOSE GEAR AND STEERING SYSTEM. NO DEFECTS NOTED. 2L73 4F A3WE 20050915000752005091500075NM 2005 9 15 SWAA052678 120050902A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29424WN 29828 FWD END OF EEPLS STRIP DAMAGED. REMOVED AND REPLACED STRIP PER MM. 2L72 4F RTA16WE 20050915000762005091500076NM 2005 9 15 SWAA052679 120050903A3350207377 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29429WN 33658 EEPLS TRACK LENS MISSING. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20050915000792005091500079EU 2005 9 15 09082005C 120050905A2560 DEFIBRILLATOR SAAB SF340 340B 7860101EU CABIN FAILED A NSVAO OTHER O OTHER TXTAXI/GRND HDL 1 EA27347CJ 347 ON PREFLIGHT, DEFIBRILLATOR SHOWS RED WRENCH INSTEAD OF OK, ON SCREEN. DMI'ED TO MOVE TO PIT (PART 91) AND REMOVED AND REPLACED UNIT IN PIT. 2L72 4T RTA52EU 20050915000802005091500080CE 2005 9 15 09092005A 120050907A2810 DRAIN LINE BEECH 1900 1900D 1154162CE FUEL SYSTEM LEAKING A NSVAO OTHER KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 EA27221CJ UE221 FUEL LEAKING FROM LT WHEEL WELL. REMOVED AND REPLACED DRAIN TUBE ASSY. FUEL LINE, OPS CHECK GOOD. 2L72 4T RTA24CE 20050915000812005091500081CE 2005 9 15 09082005E 120050905A6123 GOVERNOR BEECH 1900 1900D 1154162CE LT ENGINE FAILED A NSVAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA27221CJ UE221 LT ENGINE FAILED AUTO FEATHER. REMOVED AND REPLACED LT OVERSPEED GOVERNOR. OPS CHECKED GOOD. 2L72 4T RTA24CE 20050915000822005091500082CE 2005 9 15 09082005D 120050905A6123 GOVERNOR BEECH 1900 1900D 1154162CE RT ENGINE FAILED A NSVAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA2760MJ UE60 RT ENGINE FEATHERING DURING T/O. PROP AT 500 RPM AND TQ AT 1000 IN GROUND FINE. REMOVED AND REPLACED RT PROP GOVERNOR, OPS CHECK GOOD. 2L72 4T RTA24CE 20050915000842005091500084CE 2005 9 15 09092005C 120050908A2612 FIRE LOOP BEECH 1900 1900D 1154162CE LEFT FAILED A NSVAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 EA27124CJ UE24 LT FORWARD FIRE LOOP TEST FAIL. REMOVED AND REPLACED LEFT FORWARD FIRE LOOP. OPS CHECK GOOD. 2L72 4T RTA24CE 20050915000852005091500085CE 2005 9 15 09092005D 120050908A2730 TRIM SYSTEM BEECH 1900 1900D 1154162CE ELEVATOR BINDING A NSVAO OTHER O OTHER TXTAXI/GRND HDL 1 EA27191CJ UE19 ELEVATOR TRIM RATTLING/BINDING. INSPECTION C/W CABLE TENSION CHECKS DONE, NO DEFECTS NOTED. 2L72 4T RTA24CE 20050915000862005091500086 2005 9 15 09092005G 420050908A3418 STALL WARNING SAAB SF340 340B 7860101EU RIGHT MALFUNCTIONED A NSVAO OTHER N FALSE WARNING CRCRUISE 1 EA27277MJ 277 RT STALL WARNING FAIL LIGHT ILLUMINATED INFLIGHT. CYCLED STALL WARNING CHAN C/B, OPS CHECK GOOD. 2L72 4T RTA52EU 20050915000942005091500094SO 2005 9 15 C2XA05SH112 120050910A491014526850401 FIREWALL EMB 145 EMB145LR 3260212SO APU BAY CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713994 145291 SHV - DURING C-CHECK, APU LOWER FIREWALL HAS SEVERAL CHAFED DAMAGED RIVETS. MAINTENANCE REPAIRED APU LOWER FIREWALL CHAFED DAMAGE RIVETS IAW EC 5330-01500. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE 2L72 4T RTT00011AT 20050915000962005091500096SO 2005 9 15 C2XA05BT067 120050901A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A C2XAK NONE O OTHER ININSP/MAINT 1 SW2726545 145558 DURING SERVICE AND RETURN CHECK IN BTV MAINTENANCE, FOUND THE ROW NR 7 OVERHEAD EMERGENCY EXIT LIGHT NOT WORKING, REMOVED AND REPLACED BULB IAW EMB145 AMM NR 33-50-08, OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050915000982005091500098SO 2005 9 15 C2XA05CL080 120050911A33202LA00727830 LIGHT EMB 145 EMB145XR 3260214SO CABIN SHORTED A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW2726141 145733 MCI FLIGHT NR 2484, THE CREW REPORTED THE PSU READING LIGHT AT SEAT 19B GOT VERY HOT AND OMITTED A HAZE. THE AIRCRAFT WAS RELEASED IAW MEL 25-60-02/4. MAINTENANCE INSPECTED AND REPLACED THE PSU READING LIGHT AT SEAT 19B. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RT 20050915001012005091500101SO 2005 9 15 C2XA05BT064 120050829A335020131A BATTERY EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT FAULTY A C2XAK NONE O OTHER ININSP/MAINT 1 SW27131231039734 145688 CREW REPORTED EMERGENCY LIGHT AT EXIT ROW IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY IAW EMB145 AMM NR 33-50-04. OPS CHECKED GOOD. 2L72 4F RT 20050915001032005091500103EU 2005 9 15 MALA050684 120050901A3350 POWER SUPPLY SAAB SF340 SF340A 7850100EU EMERGENCY LIGHT INOPERATIVE A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15110XJ 340A110 CABIN EMERGENCY LIGHTS ASSOCIATED WITH POWER SUPPLIES 23LN & 21LN INOP. REPLACED SUPPLIES WITH SERVICEABLE UNITS. OPS CHECK GOOD. 2L72 4T RTA52EU 20050915001082005091500108EU 2005 9 15 09072005B 120050902A2720 LIMITER SAAB SF340 340B 7860101EU RUDDER INOPERATIVE A NSVAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 EA27242CJ 242 RUDDER LIMITER INOP. MEL'ED. 2L72 4T RTA52EU 20050915001112005091500111NM 2005 9 15 CALA0500298 120050903A5315BAC1505100849 FLOORBEAM BOEING737 737824 13844BZNM STA 986.5 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712218 28778 INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, LBL 64 TO RBL 64. REPAIRED FLOORBEAM PER ECRA 5321-01283 AND SRM 51-40-02. 2L72 4F RTA16WE 20050915001122005091500112NM 2005 9 15 CALA0500299 120050903A5315147A5505 FLOORBEAM BOEING737 737824 13844BZNM STA 967 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712218 28778 INSPECTION FOUND FLOORBEAM CORRODED AROUND FLOORBOARD HOLES AT STA 967 FROM RBL 30 TO RBL 49. THE CORROSION WAS REMOVED AND THE AREA WAS REWORKED AND REPAIRED IAW ECRA 5321-01282. 2L72 4F RTA16WE 20050915001132005091500113NM 2005 9 15 CALA0500300 120050903A5210655287399 SKIN BOEING737 7373T0 1384582NM L-2 DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2734315 23366 INSPECTION FOUND A 0.6 INCH CRACK IN L-2 DOOR SKIN AT UPPER HINGE. THE CRACKED SKIN WAS TRIMMED OUT AND REPAIR DOUBLERS WERE INSTALLED IAW ECRA 5210-01850. 2L72 4F RTA16WE 20050915001162005091500116SO 2005 9 15 LR7A05111 120050902A5312 BULKHEAD LKHEED382 382G 526414USO FS 858 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03406LC 115 4676 DURING SCHEDULED A-CHECK PER JOB CARD HA1200 FOUND LEFT FS 858 BULKHEAD TEE AND WEB CRACKED AT LBL 69, WL 198. REPAIRED IAW LAC MEA 382-53-05-067, LP 21228 ITEM M3. 2H74 4T A1SO 20050915001182005091500118EU 2005 9 15 09082005A 120050903A6120 CONTROL PANEL SAAB SF340 340B 7860101EU TORQUE STUCK A NSVAB EMER. DESCENT O OTHER CLCLIMB 1 EA27242CJ 242 CONTROL TORQUE ON TAKEOFF SWITCH BROKEN, STUCK IN APR MODE. DEFERRED IN LGA , REMOVED AND REPLACED CTOT PANEL. OPS CHECK GOOD AND CLEARED MEL'S IN HYA. 2L72 4T RTA52EU 20050915001212005091500121CE 2005 9 15 JBGA20050005 120050823A213166002041 REGULATOR LEAR 35 35A 5170602CE TAILCONE INOPERATIVE E JBGAB EMER. DESCENT J WARNING INDICATION CLCLIMB 1 GL07357LJ 357 LOSS OF CABIN PRESS. 2L72 4F A10CE 20050915001222005091500122NM 2005 9 15 QXEA200501203 120050901A5210 MECHANISM BOMBDRDHC8 DHC8402 1390042NM PAX DOOR DIRTY A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09412QX 4059 SEA FLIGHT 2365: MAIN CABIN DOOR HARD TO OPEN FROM INSIDE THE CABIN. MAINTENANCE CLEANED AND LUBED THE INTERNAL DOOR OPEN MECHANISM AS REQUIRED. OPS CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050915001242005091500124SO 2005 9 15 C2XA05CL076 120050905A5210 LEVER EMB 145 EMB145LR 3260212SO PAX DOOR LOOSE A C2XAO OTHER O OTHER NRNOT REPORTED 1 SW2714920 145380 CLE - FLIGHT NR 3264 - THE CREW REPORTED, THE MAIN CABIN DOOR IS VERY HARD TO OPEN. IT STICKS AND CAN TAKE SEVERAL TRIES TO OPEN. MAINTENANCE INSPECTED AND RE-SECURED THE MAIN CABIN DOOR LOCKING LEVER. OPERATIONAL CHECKS WERE REPORTED GOOD. 2L72 4T RTT00011AT 20050915001272005091500127NM 2005 9 15 BB05076 120050831A3260 WARNING LIGHT BOEING757 7572B7 1384964NM MLG FALSE ACTIVATIONA USAAO OTHER J WARNING INDICATION CLCLIMB 1 EA19619AU 27198 CLT - FLT 1123 EN ROUTE, PIT TO CLT, AFTER TAKEOFF, A "GEAR DOORS" EICAS MESSAGE APPEARED WITH THE GEAR HANDLE UP. ALSO, RECEIVED A "DOORS" AMBER LIGHT. THE "GEAR" AMBER LIGHT AND ALL GREEN DOWN LIGHTS EXTINGUISHED. CREW CYCLED THE GEAR AND ALL INDICATIONS WENT TO NORMAL. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED SEVERAL GEAR SWINGS. NO FAULTS FOUND. OK FOR SERVICE. 2L72 4F RTA2NM 20050915001282005091500128EU 2005 9 15 MALA050709 120050903A5210 SILL BAC 146 AVRO146RJ85A1500097EU PAX DOOR CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15507XJ E2316 WHILE ACCOMPLISHING C1 INSPECTION FOUND FORWARD PASSENGER DOOR SILL PLATE CORRODED. 2H74 4F RTA49EU 20050915001302005091500130EU 2005 9 15 MALA050710 120050903A5320 GUSSET BAC 146 AVRO146RJ85A1500097EU FUSELAGE4 CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15507XJ E2316 WHILE ACCOMPLISHING C1 INSPECTION FOUND GUSSET PLATE AT FRAME 15 FLOORBEAM LBL 20 CORRODED. 2H74 4F RTA49EU 20050915001312005091500131EU 2005 9 15 MALA050711 120050903A5240 SLIDE BAC 146 AVRO146RJ85A1500097EU SERVICE DOOR MISINSTALLED A MALAK NONE O OTHER ININSP/MAINT 1 GL15507XJ E2316 WHILE ACCOMPLISHING C1 INSPECTION FOUND THE RIGHT FORWARD SERVICE DOOR EVACUATION SLIDE INCORRECTLY PACKED. 2H74 4F RTA49EU 20050915001332005091500133EU 2005 9 15 MALA050713 120050907A3350 RELAY SAAB SF340 340B 7860101EU EMERGENCY LIGHT FAILED A MALAO OTHER O OTHER CRCRUISE 1 GL15404XJ 340B404 CABIN EMERGENCY LIGHTS FLICKER ON/OFF IN FLIGHT. REPLACED RELAY 16LN IN EMERGENCY LIGHT PANEL. 2L72 4T RTA52EU 20050915001342005091500134EU 2005 9 15 MALA050703 120050903A5730 SKIN BAC 146 AVRO146RJ85A1500097EU RT WING GOUGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15507XJ E2316 WHILE ACCOMPLISHING F1.E INSPECTION FOUND A GOUGE ON THE RIGHT WING LOWER SKIN AFT OF THE AFT SPAR AT RIB 1. IT APPEARS THAT THE DAMAGE WAS CAUSED BY PANEL 284BR. 2H74 4F RTA49EU 20050915001352005091500135EU 2005 9 15 MALA050705 120050903A5320 FLOOR SUPPORT BAC 146 AVRO146RJ85A1500097EU FR 14 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15507XJ E2316 WHILE ACCOMPLISHING C1 INSPECTION FOUND A FLOOR SUPPORT ANGLE AT FRAME 14 IN THE ELECTRICAL EQUIPMENT BAY CRACKED (RT ANGLE). 2H74 4F RTA49EU 20050915001392005091500139NM 2005 9 15 SB05112 120050909A21337110033 OUTFLOW VALVE BOEING737 737301 1384611NM CABIN PRESSURE LEAKING A USAAO OTHER J WARNING INDICATION CRCRUISE 1 EA19352US5609056090 23555 AIRCRAFT WOULD NOT MAINTAIN CABIN PRESSURIZATION. AT FL030, CABIN ALTITUDE CLIMBED 1,200 FEET PER MINUTE WITH OUTFLOW VALVE FULLY CLOSED. CREW DESCENDED BELOW FL020 BEFORE CABIN ALTITUDE WOULD DESCEND BELOW 8,000 FEET. FLIGHT CONTINUED. MX PRESSURIZED AIRCRAFT. FOUND AFT OUTFLOW VALVE LEAKING EXCESSIVELY. REPLACED AFT OUTFLOW VALVE. OPS CHECK GOOD. ALSO FOUND AFT CARGO DOOR SEAL PULLED FROM RETAINER, AFT RIGHT SERVICE DOOR UPPER SEAL LEAKING AND RIGHT PACK BAY FLEX SEAL AT FORWARD BULKHEAD OF PACK BAY LEAKING. REINSTALLED AFT CARGO DOOR SEAL INTO RETAINER, CLEANED AFT RIGHT SERVICE DOOR SEAL AND REPLACED FLEX SEAL AT FORWARD BULKHEAD OF PACK BAY. PRESSURIZATION LEAK RATE WITHIN LIMITS. 2L72 4F RTA16WE 20050915001412005091500141NM 2005 9 15 SWAA052680 120050902A3350207377 LENS BOEING737 7377H4 1384404NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29434WN 32454 EEPLS TRACK LENS BROKEN AT MID CABIN. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20050915001432005091500143NM 2005 9 15 SWAA052681 120050904A3350101114 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29435WN 32455 CABIN EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED COVER PER MM. 2L72 4F RTA16WE 20050915001452005091500145NM 2005 9 15 SWAA052683 120050902A53116516301 FRAME BOEING737 7375H4 138449DNM COCKPIT FLOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29503SW 24180 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STUB FRAMES CRACKED AT BS 188, LT & RT SIDE, WL 208. REPAIRED STUB FRAMES PER SRM. 2L72 4F RTA16WE 20050915001462005091500146NM 2005 9 15 SWAA052684 120050902A53116520723 FRAME BOEING737 7375H4 138449DNM FWD CARGO CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29503SW 24180 DURING SCHEDULED SPECIAL VISIT, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 1 & NR 5 STOP FITTINGS. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050915001472005091500147NM 2005 9 15 SWAA052685 120050902A53206551698 SPLICE BOEING737 7375H4 138449DNM BS 908 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29503SW 24180 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER SPLICE CRACKED AT BS 908, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20050913000672005091300067EA 2005 9 13 COMA0560490 120050906A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A COMAK NONE L NO TEST TXTAXI/GRND HDL 1 SO01965CA 7131 FLIGHT 5565 - EMERGENCY FLOOR LIGHTING INOPERATIVE FROM ROWS 2 THROUGH 5. CLEANED CONTACTORS ON EMERGENCY FLOOR TRACK LIGHT STRIP. 2L72 4F RTA21EA 20050913000782005091300078NM 2005 9 13 SWAA052741 120050907A53306545766 SKIN BOEING737 7373H4 1384600NM BS 455 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 455, STR 16L. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050913000832005091300083NM 2005 9 13 SWAA052746 120050910A3350MS155721 BULB BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29343SW 24151 DURING SCHEDULED SERVICE CHECK, FOUND LT EXTERIOR FUSELAGE LIGHTS INOP. RELAMPED LIGHTS PER MM. 2L72 4F RTA16WE 20050913001122005091300112NE 2005 9 13 05FDEA02786 220050902A7320 HMU AIRBUS310 A310222 3930315EU PWA JT9 JT9D7R4E1 52054NE NR 1 ENGINE FAILED A FDEAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SO25455FE 331 707725 DURING TAKEOFF ROLL, CREW HEARD AT LEAST 3 VERY LOUD BANGS FROM THE LEFT SIDE OF THE AIRCRAFT. THERE WAS ALSO SOME LEFT YAW ASSOCIATED WITH THE NOISE. REJECTED TAKEOFF WAS PERFORMED AT APPROXIMATELY 110 KNOTS. ENGINE INSTRUMENTS INDICATED NOTHING ABNORMAL. REJECTED TAKEOFF WAS PERFORMED ON RUNWAY 25 AT SFS. ALSO, THERE WERE NO ECAM INDICATIONS. PERFORMED WHEELS AND BRAKES ON LT MAIN GEAR INSPECTION CHECK AS PER A310 MM 32-40-00-6. REMOVED AND REPLACED NR 1 ENGINE HMU 73-21-01-4. 2L72 4F4 FRTA35EU E3NE 20050913001172005091300117NM 2005 9 13 SWAA052770 120050909A57436937877 FITTING BOEING737 7377H4 1384404NM LT WING CHAFED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29786SW 29811 DURING SCHEDULED 5Y CHECK, FOUND LT WING WALKING BEAM AFT LOWER HANGER FITTING CHAFED. REPAIRED FITTING PER SWA EA. 2L72 4F RTA16WE 20050913001182005091300118NM 2005 9 13 SWAA052771 120050909A3350101073 LENS BOEING737 7377H4 1384404NM AFT GALLEY MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29797MX 27890 R2 DOOR EMERGENCY EXIT SIGN LENS MISSING. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20050913001692005091300169EU 2005 9 13 USAA051076 120050909A5320D5348004320501 SILL AIRBUSA319 A319112 3930323EU AFT DOOR CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19730US 1182 CORROSION RT AFT DOOR SILL SUPPORT AT FRAME 66. BLENDED, INSTALLED REPAIR ANGLES PER SRM 53-41-14, DEFECT SIZE: .75 INCH DIA AROUND SCREW HOLE. 2L72 4F RTA28NM 20050913001712005091300171NM 2005 9 13 USAA051078 120050909A532065C80735105 CHANNEL BOEING737 7374B7 1384702NM BS 285 - 344 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19776AU 24934 CORROSION BS 285 - BS 344 AT SUPPORT CHANNEL. INSTALLED SUPPORT CHANNEL PER SRM 5T1-40-00, DEFECT SIZE: 1 X 0.050 INCH. 2L72 4F RTA16WE 20050913001722005091300172NM 2005 9 13 USAA051079 120050909A5320US5360045LF INTERCOSTAL BOEING737 7374B7 1384702NM STA 787-807 BENT A USAAK NONE O OTHER ININSP/MAINT 1 EA19776AU 24934 STA 787-807, STR 24L BENT. FABBED PART, INSTALLED INTERCOSTAL PER SRM 51-40-02, DEFECT SIZE: 1.5 INCH BENT. 2L72 4F RTA16WE 20050914000092005091400009EA 2005 9 14 QXEA200501218 120050906A27605120011 PCU CNDAIRCL600 CL6002C10 1390015EA SPOILERS MALFUNCTIONED A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09611QX8678 10041 DEN - DURING TAXI OUT, THE INBOARD SPOILER CAUTION LIGHT ILLUMINATED. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE SPOILER PCU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20050914000112005091400011EU 2005 9 14 YENA200562 120050904A335032145410 POWER SUPPLY AIRBUS320 A320232 3930326EU EMERGENCY LIGHT FAILED A YENAO OTHER J WARNING INDICATION APAPPROACH 1 EA15598JB7354 11 2314 FORWARD ENTRY EXIT LIGHTS BOTH SIDES DID NOT ACTIVATE WITH GEAR EXTENSION NOR ACTIVATE MANUALLY. EPSU FWD -L- FAILS BITE CHECK. REMOVED AND REPLACED EPSU AND EMERGENCY LIGHT BATTERY PER 31-51-38. OPS CHECK GOOD. BATTERY EMERGENCY LIGHT - P/N 3214-31, S/N 044926, T/T 92 HRS & 27 CYCLES. 2L72 4F RTA28NM 20050914000122005091400012EU 2005 9 14 YENA200563 120050904A3350321431 BATTERY PACK AIRBUS320 A320232 3930326EU EMERGENCY LIGHT FAILED A YENAO OTHER O OTHER CRCRUISE 1 EA15571JB142 2125 RIGHT SIDE OVERWING EMERGENCY EXIT LIGHT IS INOPERATIVE. REPLACED BATTERY PACK ON RT EPSU IAW MM 33-51-00, OPS CHECK OK. 2L72 4F RTA28NM 20050914000202005091400020CE 2005 9 14 DXTA200500965 120050912A2710 AILERON CESSNA560 560XL 2076702CE WING LOOSE E DXTAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 GL07694QS 5605194 WHILE IN FLIGHT AILERON HAS 3 TO 4 INCHES OF FREE PLAY WITH NO EFFECT ON MOVEMENT OF AILERONS. 2L72 4F RTA22CE 20050914000252005091400025CE 2005 9 14 DXTA200500958 120050908A2150 A/C PACK CESSNA560 560XL 2076702CE ODOR E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07695QS 5605293 15 MIN PRIOR WITH APU RUNNING AT HPN (NJA FACILITY) OUR A/C WAS TAIL TO TAIL WITH A COMPANY ULTRA. THE ULTRA STARTED IT'S ENGINES AND RAN FOR 10 TO 15 MINS BLOWING ITS FUMES INTO OUR TAIL. AT FL 380, SELECTED A WARMER TEMP AND IMMEDIATELY HAD JET EXHAUST FUMES IN THE COCKPIT AND CABIN. ENOUGH THAT THE PAX COMPLAINED OF FUMES. DON O2 MASK. DIVERTED TO TOL. THE ODOR DISSAPATED AFTER THE A/C WAS SHUT DOWN. LEAK CHECKED APU /RUNNING LEAK CHECK GOOD AT 85 PERCENT N2 AND CABIN FULL HOT LEAK CHECK L/R ENGINES, LEAK CHECK GOOD. NO FUMES NOTED IN CABIN OR COCKPIT DURING RUN. WORK IAW 560 XL CHAPTERS 21-22-00 AND 71-00-04. 2L72 4F RTA22CE 20050914000342005091400034NM 2005 9 14 2005UALA00934 120050904A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29546UA 25367 AFT CARGO PIT DOOR CUTOUT, LOWER SKIN DENTED. REMOVED DAMAGE AND FABRICATED REPAIR DOUBLER AND FILLERS PER TIMCO REO (EVA) G10924, REV.D. 2L72 4F4 FRTA2NM E17NE 20050914000352005091400035EU 2005 9 14 2005UALA00935 120050905A5313 STRINGER AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FR 31-32 CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29420UA 489 STR 41R HAS CORROSION BETWEEN FS 31-32. CUT-OUT DAMAGED SECTION AND SPLICED IN NEW SECTION OF STRINGER PER SRM 53-21-13 FIG 203. 2L72 4F4 FRTA28NM E40NE 20050914000362005091400036EU 2005 9 14 2005UALA00936 120050905A5313 STRINGER AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FR 33-34 CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29420UA 489 STRINGER 41R HAS CORROSION BETWEEN FRAMES 33-34. CUT-OUT DAMAGED SECTION, SPLICED IN NEW SECTION REF SRM 53-21-13 FIG 203 . 2L72 4F4 FRTA28NM E40NE 20050914000402005091400040NM 2005 9 14 2005UALA00940 120050903A3350321430 BATTERY AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE EMERGENCY LIGHT FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29836UA 1460 EMERGENCY LIGHT TEST FAILS. GRIPES 'EPSU AFT L'. REPLACED AFT LEFT BATTERY. 2L72 4F4 FRTA28NM E40NE 20050914000652005091400065WP 2005 9 14 ARWA20050904 120050707A5330 SKIN DOUG DC8 DC863F 302198FWP BS 1620-1640 CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19784AL 46135 DURING C-CHECK INSPECTION, THE FOLLOWING WAS FOUND; AFT ACCESSORY COMPT INTERIOR STA 1620 THROUGH STA 1640, BETWEEN L-32L AND L-33L, SKIN WITH CORROSION. 2L74 4F 4A25 20050914000752005091400075WP 2005 9 14 AALA20050575 120050905A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21205AA 49155 DFW - CEILING EMERGENCY LIGHTS IN FORWARD GALLEY AND MID GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS IN FORWARD GALLEY AND MID GALLEY INOPERATIVE. 2L72 4F A6WE 20050914000802005091400080WP 2005 9 14 AALA20050573 120050904A3397 CONNECTOR DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW219625W 53595 STL - EMERGENCY EGRESS LIGHTS AT AFT CABIN INOPERATIVE. REPAIRED QUICK DISCONNECT IN TAIL SIDEWALL LIGHT FOR EMERGENCY EGRESS LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050914000822005091400082NM 2005 9 14 AALA20050576 120050905A3350 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21692AA 26972 DFW - EMERGENCY LIGHTS AT FIRST CLASS SEATS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIRST CLASS SEATS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050914000932005091400093EU 2005 9 14 USAA051075 120050909A5310D5348004320401 BEAM AIRBUSA319 A319112 3930323EU FR 66 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19730US 1182 FRAME 66 OUTBOARD LT DOOR SILL. REMOVED & REPLACED PER SRM 51-72-11, 53-41-14, DEFECT SIZE: 1 X 2 INCH. 2L72 4F RTA28NM 20050914001032005091400103NM 2005 9 14 C1HA200581010 120050909A5320 WEB BOEING727 7272S7 138407ZNM BS 1243+6 CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15681CA 22020 RIGHT LOWER TORQUE BOX HAS CRACK AT LIGHTNING HOLE WITH STOP DRILL HOLE, STA 1243 +6 IN. ROUTED OUT DAMAGED AREAS, FABBED DOUBLER FROM 7075 T6 .032 PO 900573 DIM 10 X 2 INCHES IAW 727 SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1. DOUBLER TREATED AND PRIMED AND INSTALLED IAW 727 SRM 51-10-2 AND 51-40-3 FIG 1. 2L73 4F A3WE 20050914001122005091400112EU 2005 9 14 MALA050683 120050829A5330 SKIN SAAB SF340 340B 7860101EU BS 322-361 DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15454XJ 340B454 DURING 4K CHECK IN BNA FOUND DENTS IN LT SIDE ICE QUARD AREA STA 322-361. REMOVED ICE QUARDS. REPAIRED FUSELAGE, OUT OF LIMIT REF: SRM 51-10-10. REF: EO S53005, INSTALLED NEW ICE QUARDS REF: EAMS WO 212753, TASK 2503. 2L72 4T RTA52EU 20050914001132005091400113NM 2005 9 14 05FDEA02809 120050907A5753 ATTACH FITTING DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 LT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87633. 2L73 4F RTA22WE 20050914001142005091400114NM 2005 9 14 05FDEA02810 120050907A5330 SKIN DOUG MD11 MD11 3023602NM ZONE 100 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 WHILE PERFORMING REPEATITIVE INSPECTIONS ON EXISTING SKIN EXTERNAL DOUBLER REPAIR AT STA Y1811 LONGERON 36R, FOUND THE REPAIR DOUBLER WITH SEVERAL SUNK IN FASTENER HEADS. REPAIR DOUBLER REMOVED AS PER SRM 51-31-01 VOLUME II. NEW REPAIR DOUBLER FABRICATED AS PER SRM 53-20-00 FIGURE 2 VOLUME I AND REPAIR DOUBLER INSTALLED AS PER SRM 53-20-00 FIGURE 2 VOLUME I. THIS REPAIR CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050914001192005091400119 2005 9 14 SWAA052676 420050905A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29387SW 26602 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20050914001302005091400130NE 2005 9 14 TSAA0571038 220050907A7200 ENGINE BOEING737 73776N 13844CHNM CFMINTCFM567CFM567B2US 13802NE NR 2 MALFUNCTIONED A TSAAED ENGINE SHUTDOWN RETURN TO BLOCK RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TXTAXI/GRND HDL 1 WP13741AL 28641 ETOPS FLT 473 OAK-OGG: ENGINE NR 2 SHUT DOWN AFTER START. ENGINE NR 2 WAS SLOW TO SPOOL AFTER PUSHBACK. ENGINE NR 1 HITS 40 PERCENT BEFORE ENGINE NR 2 HIT 26 PERCENT. RETURNED TO GATE. PERFORMED EEC BITE IAW FIM 74-00-00-810-801-F00, NO FAULTS NOTED. PERFORMED EEC TEST IAW 73-21-00-700-804-F00, NO FAULTS NOTED. PERFORMED TEST 8 - ACCELERATION CHECK PER TASK 71-00-00-700-824-F00, ACCELERATION CHECK OKAY. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA16WE E2GL 20050914001312005091400131EU 2005 9 14 DHL2005366002 120050913A2611 WARNING LIGHT AIRBUS300 A300B4203 3930306EU SMOKE DETECTOR FALSE INDICATIONA DHLABA EMER. DESCENT UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01366DH 249 SMOKE LIGHT ILLUMINATED AFTER BREAKING GROUND. ABNORMAL PROCEDURE & EMERGENCY PROCEDURE PERFORMED. VISUALLY INSPECTED FWD CARGO COMPARTMENT, NO SMOKE OR ABNORMAL SMELL FOUND. SMOKE DET SYSTEM OPS CHECKS NORMAL IAW M/M 26-14-00. 2L72 4F RTA35EU 20050914001322005091400132EA 2005 9 14 VTZA200500178 120050907A2710 IDG CNDAIRCL600 CL6002B19 1900309EA NR 2 UNDERSERVICED A VTZAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA27640BR 7340 IDG 2 CAUTION MSG AND SPOILERON CONFIGURATION MESSAGE ON TAKEOFF. SERVICED NR 2 IDG IAW CRJ AMM 12-13-24 SPOILER SYS HAS NO MESSAGE POSTED AND OPS CHECK GOOD IAW CRJ AMM 27-60-00. 2L72 4F RTA21EA 20050914001342005091400134NM 2005 9 14 05FDEA02841 120050912A5322 SHEAR TIE BOEING727 727200 138407ENM BS 700 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25268FE 21674 CORROSION ON SHEAR TIE, AFT SIDE, BS 700 BL 0. REMOVE AND REPLACE SHEAR TIE PER SRM 53-10-1. 2L73 4F RTA3WE 20050914001382005091400138NM 2005 9 14 SB05113 120050910A27512061141 INDICATOR BOEING737 7374B7 1384702NM TE FLAPS FAULTY A USAAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 EA19783AU4817248172 25022 CLT FLT440 ON CLIMBOUT FROM CLT, AIRCRAFT EXPERIENCED AN ASYMMETRICAL FLAP INDICATION. ONE FLAP INDICATED ZERO UNITS WHILE THE OTHER FLAP INDICATED ONE UNIT. AIRCRAFT DID NOT EXPERIENCE ANY ROLL OR ADVERSE CONDITION ASSOCIATED WITH THE INDICATION. CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD AT CLT. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND TAXIED TO THE GATE. MAINTENANCE REMOVED AND REPLACED THE FLAP POSITION INDICATOR PER MM 27-58-01. FUNCTIONAL TEST OF INDICATING SYSTEM AND OPERATIONAL TEST OF FLAP ASYMMETRY SYSTEM CHECKS GOOD. 2L72 4F RTA16WE 20050914001402005091400140NM 2005 9 14 2005UALA00948 120050906A5330 SKIN BOEING737 737322 1384676NM BS 747 STR 24R DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29348UA 24252 EXTERNAL FUSELAGE SKIN HAS LIGHTNING STRIKE DAMAGE AT STA 747 STR 24R. 2L72 4F RTA16WE 20050914001432005091400143NM 2005 9 14 2005UALA00951 120050907A3350321430 POWER SUPPLY AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE EMERGENCY LIGHT FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29828UA 1031 FWD LT EMERGENCY POWER SUPPLY AND BATTERY FAILS TEST. REPLACED POWER SUPPLY AND BATTERY. 2L72 4F4 FRTA28NM E40NE 20050914001452005091400145NM 2005 9 14 2005UALA00953 120050806A5321 FLOOR PANEL BOEING757 757222 1384956NM PWA 2037 PW2037 NE BS 1680-1720 CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP2987UA 26713 AFT CABIN FLOOR BS 1680 TO 1720, RBL 51 METAL FLOOR CORRODED. REMOVE GALLEY MOUNT FOR ACCESS, REMOVE CORROSION AND INSTALL DOUBLER, ALODINE, PRIME, AND PAINT PER SRM 51-20-01. 2L72 4F4 FRTA2NM E17NE 20050915000012005091500001GL 2005 9 15 YTRR105931 220050905A732123070606 FUEL CONTROL BELL 206 206B3 1181506SW ALLSN 250C 250C20 03013GL ENGINE OUT OF ADJUST B YTRRK NONE O OTHER ININSP/MAINT 1 SW0321RT 2659 AIRCRAFT STARTING HOT. UNABLE TO ADJUST FUEL CONTROL TO CORRECT HOT STARTING. 1G71 3U3 U H2SW E4CE 20050915000092005091500009EA 2005 9 15 VNAA0508032 120050831A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE DAMAGED A VNAAK NONE O OTHER ININSP/MAINT 1 GL05229PS 7898 RAMP EMPLOYEES REPORTED A TWO INCH SCRATCH ON THE FUSELAGE SKIN BELOW THE CARGO DOOR SILL PLATE. MAINTENANCE COMPLIED WITH A TEMP REPAIR IAW BOMBARDIER REO 601R-53-61-1510. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050915000122005091500012NM 2005 9 15 2005UALA00956 120050907A335060253 LIGHT BOEING737 737322 1384676NM AFT GALLEY INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29313UA 23674 AFT GALLEY FLOOR EEL LIGHTS INOP. REPLACED LAMP STRIP AT AFT GALLEY. 2L72 4F RTA16WE 20050915000192005091500019NM 2005 9 15 2005UALA00959 120050908A5321 PRESSURE PANEL BOEING757 757222 1384956NM PWA 2037 PW2037 NE AFT CABIN FLOOR DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29505UA 24626 AFT CABIN FLOOR LEVEL, AFT PRESS DECK PLATE HAS DAMAGE. REPAIRED PER MM 53-60-97. 2L72 4F4 FRTA2NM E17NE 20050915000312005091500031 2005 9 15 SWAA052777 420050912A256565C16820 HOOK BOEING737 7373H4 1384600NM L1 DOOR GIRT BARLOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29642WN 27715 L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED HOOK PER MM. 2L72 4F RTA16WE 20050915000662005091500066EA 2005 9 15 VNAA0509005 120050906A2750 FCU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A VNAAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL05244PS 7912 WITH FLAPS AT 20 DEGREES ON APPROACH THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED. THE CREW FOLLOWED THE QRH AND MADE A FLAPS 20 DEGREES LANDING. MAINTENANCE RESET THE FECU IAW CRJ200 SL-00-001. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050915000892005091500089CE 2005 9 15 09092005F 120050908A2740 STABILIZER BEECH 1900 1900D 1154162CE NOISY A NSVAO OTHER O OTHER TXTAXI/GRND HDL 1 EA27171CJ UE71 STAB MAKING RATTLING NOISE. DMI'ED RATTLE. 2L72 4T RTA24CE 20050915000902005091500090EU 2005 9 15 09072005A 120050902A7714 INDICATOR SAAB SF340 340B 7860101EU RT NG INOPERATIVE A NSVAO OTHER P NO WARNING INDICATION CRCRUISE 1 EA27301CE 191 RT NG GAUGE DROPPED TO ZERO IN FLIGHT. PERFORMED ENGINE RUNS NO DEFECTS NOTED AT THIS TIME. OPS CHECK GOOD. 2L72 4T RTA52EU 20050915000912005091500091SO 2005 9 15 C2XA05CL075 120050831A3350B6245305 LIGHT EMB 145 EMB145EP 3260221SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714942 145037 DURING ROUTINE MAINTENANCE, THE EMERGENCY LIGHT ON THE SERVICE DOOR WAS INTERMITTENT. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY ON THE SERVICE DOOR. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20050915000922005091500092SO 2005 9 15 C2XA05BT068 120050908A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT FAULTY A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712967 145133 DURING SERVICE AND ROUTINE CHECK, MAINTENANCE FOUND THAT THE RIGHT EXTERIOR OVERWING EMERGENCY LIGHT IS NOT FUNCTIONING. REMOVED AND REPLACED BULB IAW EMB145 MM NR 33-50-01; OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050915000932005091500093SO 2005 9 15 C2XA05TY053 120050907A21508152402 ACM EMB 145 EMB145EP 3260221SO NR 1 SMOKE A C2XAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW2713935 145022 FLT NR 2786, PILOT REPORT SMOKE IN COCKPIT AFTER SELECTING PACKS AT 500' AGL. ACFT RETURNED TO FIELD. MTX PLACED NR 1 PACK ON MEL AS PER MEL 21-51-00 CAT C, CONTROL NR 059007 AND WAS RELEASED. NR 1 ACM WAS REMOVED AND REPLACED UPON ACFT'S ARRIVAL INTO CLE, MEL WAS CLEARED AND ACFT WAS RELEASED TO SERVICE. 2L72 4F RTT00011AT 20050915001042005091500104NM 2005 9 15 05FDEA02728 120050901A2782269002917 ACTUATOR BOEING727 727233 138408ANM NR 7 SLAT MALFUNCTIONED A FDEAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 SO25285FE 22622 LOST SYS A QTY DESCENDING OUT OF 12K FT. RAN APPROPRIATE CHECKLISTS INCLUDING MAN FLAP AND GEAR EXT. NR 7 SPOILER FAILED TO EXT DURING FLAP EXT. REMOVED AND REPLACED NR 7 SLAT ACT IAW M/M 27-81-032-4. REMOVED AND REPLACED CASE DRAIN FILTERS IAW M/M29-11-041-2 AND REMOVED AND REPLACED A SYS PRESS FILTERS IAW M/M 29-11-062-3. RAN ENG'S AND LEAK CHECK C/W, NO LEAKS AND IND NORMAL. A/C OK TO CONTINUE. 2L73 4F RTA3WE 20050915001062005091500106EU 2005 9 15 UQR2005F00000 120050801A3244237K232 TIRE BRAERODH125 HS125700A 4230170EU GARRTTTFE731TFE7313R1H 29001WP RT MLG CRACKED B UQRRO OTHER O OTHER NRNOT REPORTED 1 WP01700NW69 NA0246 P80102 DURING PRELIMINARY INCOMING INSPECTION ON 7/11/05 IT WAS NOTED THAT NR3 MAIN WHEEL TIRE HAD CRACKS OR SPLITS RADIALLY IN BETWEEN TREAD. IT WAS DETERMINED THAT THIS TIRE WAS INSTALLED ON THE NR 3 WHEEL (PN AH52788, SN 675/8129 ON 6/8/05 ACTT 11,926.5, ACTL 12,443) AC TIMES ON 7/11/05 (WHEN DEFECT WAS NOTED) WERE ACTT 11996.2, ACTL 12,552. THE TIRE HAS AC MFG TRACKING NR 983290, WO/CONTRACT/INVOICE NR 506021. IT IS SUSPECTED THAT THE CRACKS/SPLITS IN THE TREAD ARE DUE TO POSSIBLE MFG FLAW. IF UNDETECTED THIS COULD HAVE BEEN POTENTIALLY VERY DANGEROUS SITUATION UNDER LANDING LOADS. THE CRACKED/SPLIT TIRE WAS REMOVED AND REPLACED WITH A NEW TIRE AND THE WHEEL/BOLTS WERE NDT INSPECTED. (WP01200512932) (K) 2L72 4F4 F A3EU E6WE 20050915001202005091500120SO 2005 9 15 CHQA200500157 120050903A323122250100003 SOLENOID EMB 145 EMB145LR 3260212SO NLG DOOR UNSERVICEABLE A CHQAO OTHER J WARNING INDICATION CRCRUISE 1 GL11578RP 14500865 FLIGHT 6360 - MCO -LIT - EN ROUTE FROM MCO TO LIT, NOSE GEAR DOORS OPENED UNCOMANDED. ALSO DOOR CMD CIRCUIT BREAKER POPPED. INITIALLY SLOWED TO 210 KTS. FOUND NOTHING IN THE QRH THAT PERTAINED. CONTINUE TO LIT, LANDED WITHOUT INCIDENT. FERRIED FROM LIT TO CMH. REMOVED AND REPLACED NOSE GEAR DOOR SOLENOID VALVE IAW EMB 145 MM 32-33-02. OPS CHECK SATISFACTORY. 2L72 4T RTT00011AT 20050915001372005091500137NM 2005 9 15 05FDEA02829 120050909A5310 SHEAR TIE BOEING727 727233 138408ANM BS 660 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25268FE 21674 FWD CARGO CORROSION FLOOR SHEAR TIE STA 660 RBL 4 TO LBL 4 WL 148. REPAIRED PER SRM 53-10-4. 2L73 4F RTA3WE 20050915001542005091500154NM 2005 9 15 DL75K050494 120050828A2530811150417 COFFEEMAKER BOEING757 757232 1384965NM AFT GALLEY ODOR A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27695DA 29727 FUMES IN AIRCRAFT AT R3 AREA IN CABIN ONLY IN AFT GALLEY FL380 2 HRS INTO FLT / OPENED PANELS IN REAR GALLEY, NTF. CHECKED BEHIND C/B PANEL ALL CONNECTIONS TIGHT CHECKED CONNECTOR ON CURRENT TRANSFORMER, ALL NORMAL. CLEANED OVERHEAD VENT FILTERS. CHECKED BEHIND OVERHEAD LIGHT FIXTURE, ALL GOOD. REPLACED COFFEEMAKER AS PRECAUTIONARY. 2L72 4F RTA2NM 20050915001552005091500155NM 2005 9 15 CALA0500308 120050913A531466621258 KEELBEAM BOEING737 7373T0 1384582NM STA 690-727 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2763305 23356 INSPECTION FOUND RT WHEEL WELL LOWER KEEL BEAM MILDLY CORRODED AT STA 690-727, S28R. REPAIRED IAW ECRA 5311-01237. 2L72 4F RTA16WE 20050915001562005091500156NM 2005 9 15 MASA200500715 120050907A215078279016 ACM DHAV DHC8 DHC8202 2809007NM SMOKE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07987HA9164 25 425 ASH 6377 PHX. SMOKE AND ASH IN THE CABIN AND COCKPIT. MX TROUBLESHOT AND FOUND THAT THE ACM WAS STARTING TO COME APART. MAINTENANCE REPLACED THE ACM. 2H72 4T RTA13NM 20050915001572005091500157NM 2005 9 15 MASA200500352 120050513A612030005000056 TSCU DHAV DHC8 DHC8202 2809007NM TORQUE MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07449YV1638 1638 449 ASH 6106 PHX TO PSP. THE AIRCRAFT RETURNED TO THE GATE WHEN THE CREW REPORTED THAT THE NR 1 ENGINE/PROP TORQUE WENT TO 100 PERCENT TORQUE UNCOMMANDED WHEN ADVANCING THE POWER LEVER. MAINTENANCE REPLACED THE TSCU. 2H72 4T RTA13NM 20050915001602005091500160NM 2005 9 15 AALA20050595 120050912A3350 CONNECTOR BOEING767 767323 1385205NM EMERGENCY LIGHT LOOSE A AALAK NONE O OTHER ININSP/MAINT 1 SW21396AN 29603 LAX - EMERGENCY LIGHT AT LEFT SIDE OF STORAGE COMPARTMENT FORWARD OF SEAT 20B INOPERATIVE. FOUND LOOSE CONNECTOR AT SIDEWALL. SECURED LOOSE CONNECTOR AT SIDEWALL FOR EMERGENCY LIGHT AT LEFT SIDE OF STORAGE COMPARTMENT FORWARD OF SEAT 20B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050915001612005091500161NE 2005 9 15 RAIA00509011 220050910A732031059007 HMU JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114HR 01514NE ENGINE MALFUNCTIONED A RAIAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 CE03566HK100614 41084 76111 FLT 5445 - STL - NR 2 ENGINE LOW TORQUE WILL NOT PRODUCE MORE THAN 40 PERCENT TORQUE. MAINTENANCE REMOVED AND REPLACED THE FUEL CONTROL UNIT. OPS CHECKED GOOD. 2L72 4T4 TRTA41NM E18NE 20050915001632005091500163SO 2005 9 15 RAIA00509009 120050908A3350 CONNECTOR EMB 145 EMB145 3260210SO EMERGENCY LIGHT UNSECURE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03801HK 145053 FLT 3542 - STL - FLOOR EMERGENCY LIGHT INOP. MAINTENANCE RESECURED LOOSE CONNECTOR. 2L72 4F RTT00011AT 20050915001642005091500164EU 2005 9 15 RAIA00509014 120050911A3350 LIGHT JETAIRJETSTMJETSTM4101 1500501EU CABIN INOPERATIVE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03574HK 41093 FLT 5416 - STL - EMERGENCY FLOOR LIGHTS OUT. MAINTENANCE CYCLED POWER TO EMERGENCY LIGHTS. 2L72 4T RTA41NM 20050915001652005091500165 2005 9 15 RAIA00509010 420050908A2312 TRANSPONDER EMB 145 EMB145LR 3260212SO COMMS FAILED A RAIAA UNSCHED LANDING O OTHER CLCLIMB 1 CE03811HK 145256 FLT 3521- PIT - BOTH TRANSPONDERS FAILED IN FLIGHT JUST AFTER TAKEOFF. MAINTENANCE RERACKED THE COMMUNICATION UNITS AND CYCLED AIRCRAFT POWER. 2L72 4T RTT00011AT 20050915001662005091500166SO 2005 9 15 RAIA00509012 120050910A335066903 LIGHT EMB 145 EMB145 3260210SO CABIN INOPERATIVE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03820HK 145064 FLT 5523 - STL - EMEGENCY LIGHT STRIPS PARTIALLY OUT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP. 2L72 4F RTT00011AT 20050915001672005091500167SO 2005 9 15 RAIA00509013 120050911A3397 CONNECTOR EMB 145 EMB145 3260210SO EMERGENCY LIGHT LOOSE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03802HK 145066 FLT 3544 - STL - FWD BULKHEAD EMERGENCY EXIT LIGHT INOP. MAINTENANCE RESECURED LOOSE CONNECTION. 2L72 4F RTT00011AT 20050915001702005091500170NM 2005 9 15 DL76S050474 120050822A2560P4010021SMI BATTERY BOEING767 767332 1382001NM FLASHLIGHT INOPERATIVE A DALAO OTHER O OTHER TXTAXI/GRND HDL 1 SO27120DL 23279 1L DOOR FLASHLIGHT WON`T TEST. REPLACED BATTERY. 2L72 4F RTA1NM 20050915001752005091500175NM 2005 9 15 DL76K050487 120050825A2781 SENSOR BOEING767 767332 1382001NM LE SLATS MALFUNCTIONED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27178DZ 30596 LEADING EDGE WOULD ONLY RETRACT TO 1/2 VISUAL CONFIRMED POSITION. REPLACED PROX SENSOR 302 AND FOUND ALL VALUES OF THE NEW SENSOR WITHIN TOLERANCE. REPLACED SM6 AND ASSOCIATED CONNECTOR PINS. 2L72 4F RTA1NM 20050915001762005091500176NM 2005 9 15 DLM88050488 120050824A36006712152180 SWITCH DOUG MD88 MD88 3023688NM TEMP FAILED A DALAO OTHER M OVER TEMP CRCRUISE 1 SO27964DL 49983 THE 26K TAIL COMPT TEMP HIGH MASTER WARNING CAME ON. FOUND LEFT TEMP SWITCH STUCK IN CLOSED POSITION. REPLACED SAME. 2L72 4F RTA6WE 20050915001772005091500177NM 2005 9 15 DL76L050489 120050825A4930211734220 CONTROLLER BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE APU MALFUNCTIONED A DALAK NONE O OTHER ININSP/MAINT 1 SO27188DN33688 27583 P1044 APU FAILED WITH FAULT LIGHT ILLUMINATED. FOUND ECU WITH ECU FAULT LIGHT ILLUMINATED. REPLACED ECU, CHECKS GOOD. 2L72 4F4 FRTA1NM E24NE 20050915001812005091500181NM 2005 9 15 DL76L050529 120050909A361077328810 SHUTOFF VALVE BOEING767 767332 1382001NM RIGHT FAILED A DALAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO27180DN 25985 RIGHT ENGINE BLEED VALVE WOULD NOT OPEN WHEN SELECTED ON. TRIED NEW PRSOV FILTERS, NO HELP. RERACKED RIGHT ENGINE BLEED CARD, NO HELP. REPLACED RIGHT ENGINE PRSOV, OPS OK. 2L72 4F RTA1NM 20050915001822005091500182NM 2005 9 15 DL76L050530 120050909A3397 WIRE BOEING767 767332 1382001NM EMERGENCY LIGHT CHAFED A DALAK NONE O OTHER ININSP/MAINT 1 SO27188DN 27583 C/B 36 TRIPPED AND WOULD NOT RESET. FOUND WIRES AT THE P22 PNL CHAFED. REPAIRED WIRES. 2L72 4F RTA1NM 20050915001832005091500183NM 2005 9 15 DL76L050532 120050909A2410755359B IDG BOEING767 767332 1382001NM RIGHT FAILED A DALAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO27196DN 28453 RIGHT IDG DROP OFFLINE AND WOULD NOT RESET. BPCU BITE CHECK FAULTS GEN DIODE. REPLACED GCU, NO HELP. REINSTALL ORIGINAL GCU. REMOVED AND REPLACED RIGHT IDG. OPS AND LEAK CHECK OK. 2L72 4F RTA1NM 20050915001842005091500184NM 2005 9 15 DL76L050533 120050909A2910 FILTER BOEING767 767332 1382001NM HYD SYSTEM BYPASSING A DALAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO27195DN 28452 RETURN TO GATE FOR PASSENGER CONCERN OF SURGING SOUND UNDER FLOOR AT MID CABIN AREA. REPLACED MODULATING AIR VALVE, NO HELP. REPLACED CONTROL PRESSURE SWITCH, NO HELP. FOUND FILTER BYPASS POPPED. REPLACED FILTER AND ADP, LEAK CHECK GOOD. OPS CHECK NORMAL. 2L72 4F RTA1NM 20050915001862005091500186NM 2005 9 15 DLM88050538 120050911A4990 APU DOUG MD88 MD88 3023688NM AFT LEAKING A DALAC ABORTED TAKEOFF KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SO27914DE 49957 RIGHT AFTER T/O AFT LAVATORIES SMOKE DETECTORIES WENT OFF WITH WHITE HAZY SMOKE IN THE AFT CABIN AND ODD SMELL. FOUND APU INLET WET WITH OIL FROM INTERNAL LEAK. REPLACED SAME AND PERFORMED DUCT BURNOUT. 2L72 4F RTA6WE 20050915001912005091500191NE 2005 9 15 DL76S050543 220050913A7261CF680AABX ENGINE BOEING767 767332 1382001NM GE CF6 CF680 30025NE NR 1 LEAKING A DALAH DEACTIVATE SYST/CIRCUITS KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO27122DL36365 580339 23436 580339 ODOR DETECTED AND SEVERAL SMOKE DETECTORS WENT OFF. ODOR DISSIPATED WITH UTILITY BUSSES OFF, BUT RETURNED WHEN POWER LEVERS ADVANCED. OIL LEAK NR 1 ENGINE. REPLACED NR 1 BEARING MANIFOLD PKNGS, PERF SAME INSPECTION ON NR 2 ENGINE CKS OK. RAN AT HIGH PWR WITH NO ODOR OR SMOKE. 2L72 4F4 FRTA1NM E13NE 20050915001922005091500192WP 2005 9 15 UPS05845417 120050908A5320 CUSP WEB DOUG DC8 DC873F 302199FWP BS 1535 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE:C3, MAIN DECK STA 1535 WEB AT CUSP AREA IS CRACKED APPROX .5 INCH. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-2-0 FIG 23 AND DWG 9753254. 2L74 4F RT4A25 20050915001942005091500194NM 2005 9 15 MASA200500685 120050829A6123M390166105L RELAY DHAV DHC8 DHC8202 2809007NM AUTO FEATHER MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07988HA 426 ASH 6286 PHX. AUTO FEATHER ARM LIGHT WILL NOT GO OUT. MAINTENANCE CHANGED THE K-5 AUTO FEATHER RELAY. OPERATIONAL CHECK NORMAL. 2H72 4T RTA13NM 20050915001952005091500195NM 2005 9 15 MASA200500719 120050909A6123M390166105L RELAY DHAV DHC8 DHC8202 2809007NM AUTO FEATHERING MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07989HA 427 ASH 6259 PHX. A/F WILL NOT ARM. MX RESET THE SYSTEM AND PERFORMED ENGINE RUN CHECKS AND THE SYSTEM CHECKED GOOD. THE AIRCRAFT THEN RTG A SECOND TIME FOR SAME PROBLEM. MX ADJUSTED THE AUTOFEATHER ARMING POT, REMOVED AND REPLACED K5 RELAY. 2H72 4T RTA13NM 20050919000022005091900002SO 2005 9 19 1262091005 120050914A36101118331 PLUG GULSTMG1159 GIV 3980115SO UNKNOWN E N93AA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO13462QS9919 1262 AIRCRAFT YAWS LEFT AND RIGHT ABRUPTLY DURING ALL PHASES OF FLIGHT. 2L72 4F RTA12EA 20050919000032005091900003EU 2005 9 19 05FDEA02905 120050914A5321242EK FLOOR PANEL AIRBUS310 A310 EU GE CF6 CF680 30025NE CARGO DECK DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25425FE 264 MDCC FLOOR PANEL 242EK IS DELAMINATED. FABED NEW FLOOR PANEL. 2L72 4F4 FRTA35EU E13NE 20050919000092005091900009EU 2005 9 19 05FDEA02912 120050914A5321231JH FLOOR PANEL AIRBUS310 A310 EU GE CF6 CF680 30025NE CARGO DECK CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25425FE 264 MDCC FLOOR PANEL 231JH CRACKED. FABED NEW FLOOR PANEL. 2L72 4F4 FRTA35EU E13NE 20050919000122005091900012EU 2005 9 19 05FDEA02913 120050914A5321231JG FLOOR PANEL AIRBUS310 A310 EU GE CF6 CF680 30025NE CARGO DECK CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25425FE 264 MDCC FLOOR PANEL 231JG IS CRACKED. FABED NEW FLOOR PANEL. 2L72 4F4 FRTA35EU E13NE 20050919000152005091900015EU 2005 9 19 05FDEA02916 120050914A5321232EG FLOOR PANEL AIRBUS310 A310 EU GE CF6 CF680 30025NE CARGO DECK DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25425FE 264 MDCC FLOOR PANEL 232EG IS DELAMINATED. FABED NEW FLOOR PANEL. 2L72 4F4 FRTA35EU E13NE 20050919000172005091900017EU 2005 9 19 05FDEA02918 120050914A5347 SEAT TRACK AIRBUS310 A310 EU GE CF6 CF680 30025NE CARGO DECK NICKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25425FE 264 MDCC SEAT TRACK HAS NICKS. REMOVED NICKED SEAT TRACK AND INSTALLED NEW TRACK IAW SRM 53-10-16, 51-27-00,51-40- 40,AND 51-21-00. 2L72 4F4 FRTA35EU E13NE 20050919000182005091900018EU 2005 9 19 05FDEA02919 120050914A5347 SEAT TRACK AIRBUS310 A310 EU GE CF6 CF680 30025NE CARGO DECK DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25425FE 264 MDCC SEAT TRACK HAS DAMAGED LUGS. REMOVED DAMAGED TRACK AND INSTALLED NEW TRACK IAW SRM 51-40-21, 51-21-10, AND 53-10-16. 2L72 4F4 FRTA35EU E13NE 20050919000212005091900021CE 2005 9 19 ACE091305 120050913A3230MS24171D1 RELAY BEECH 1900 1900C 1154161CE MLG CONTAMINATED E YADAO OTHER S AFFECT SYSTEMS APAPPROACH 1 AL03112AX44 UC45 PIREP - LANDING GEAR FAILED TO EXTEND USING NORMAL SYSTEM. MANUAL EXTENSION PERFORMED. MAINTENANCE REPLACED WATER LOGGED HYDRAULIC POWER PACK RELAY (SUSPECT THAT RELAY WAS FROZEN AFTER FLIGHT AT ALTITUDE). SEALED WING LEADING EDGE GAP TO HELP REDUCE FREE WATER / MOISTURE IN ELECTRICAL BAY. 2L72 4T RTA24CE 20050919000232005091900023WP 2005 9 19 UPS05845410 120050903A5712 RIB DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE: C3, LT WING L/E UPPER RIB IS CRACKED AT XFS 803.750. STOP DRILLED, FABRICATED DOUBLER AND INSTALLED IAW SRM 51-1-21, 51-1-20D AND 57-2-0. 2L74 4F RT4A25 20050919000252005091900025WP 2005 9 19 UPS05845412 120050828A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE: C3, RT WING L/E UPPER SKIN IS CRACKED O/B OF XFS 710.000. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1 FIG 38. 2L74 4F RT4A25 20050919000282005091900028WP 2005 9 19 UPS05845416 120050904A5720 STIFFENER DOUG DC8 DC873F 302199FWP RW XW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE: C3, RIGHT WING L/E, OUTBOARD STUB WING L/E STIFFENER CRACKED 1 INCH LONG AT XW 463.000 NR 4 PYLON UPPER. REMOVED CRACKED STIFFENER, FABRICATED AND INSTALLED REPLACEMENT STIFFENER IAW 51-3-0, 51-1-21A, AND DWG 5769891. 2L74 4F RT4A25 20050919000322005091900032EA 2005 9 19 VTZA200500182 120050914A57406001020428 SUPPORT ANGLE CNDAIRCL600 CL6002B19 1900309EA RT WING CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27655BR 7457 RIGHT BATTERY RIB SUPPORT ANGLE RWS 48.3 IS CRACKED .25 INCH. 2L72 4F RTA21EA 20050919000332005091900033EA 2005 9 19 VTZA200500183 120050914A5346601R536066 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA RT ENGINE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27655BR 7457 RIGHT ENGINE SUPPORT BEAM IS CRACKED IN LOWER WEB AT .75 INCH. 2L72 4F RTA21EA 20050919000362005091900036EA 2005 9 19 VTZA200500186 120050914A57406001020427 SUPPORT ANGLE CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27655BR 7457 LEFT BATTERY RIB SUPPORT ANGLE LWS 48.3 IS CRACKED .25 INCH. 2L72 4F RTA21EA 20050919000392005091900039 2005 9 19 QXEA200501225 420050914A6113 SMOKE DHAV DHC8 DHC8202 2809007NM HAMSTD14SF 14SF23 NE NR 1 SPINNER DETECTED A QXEAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM09347PH 480 PSC FLIGHT 2101 - NOTICED SMOKE COMING FROM BEHIND NR 1 PROP SPINNER. ALL ENGINE NR 1 INDICATIONS NORMAL. MAINTENANCE REMOVED COWL HORSECOLLAR AND LOWER COWL AND OPENED SIDE DOORS AND COMBUSTION SECTION DOORS. VISUALLY INSPECTED ALL FLUID LINES AND WIRING. NO DEFECTS NOTED. VISUALLY INSPECTED PROP DE-ICE SLIP RING AND BRUSH BLOCK. NO DEFECTS NOTED. NO EVIDENCE OF CONTACT BETWEEN PROP SPINNER AND COWLING OR PROP AND HORSECOLLAR. COMPLIED WITH GROUND RUNS AT FEATHER, DISC, FI AND 90 PERCENT TORQUE FOR 5 MINUTES. NO DEFECTS OR SMOKE NOTED. COMPLIED WITH PROP DE-ICE FUNCTIONAL TEST. NO PARTS REPLACED, AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 6 CP7NE 20050919000402005091900040NM 2005 9 19 QXEA200501227 120050914A7600 ECU DHAV DHC8 DHC8202 2809007NM NR 1 ENGINE INACCURATE A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09351PH 490 SEA FLIGHT 2026 - NR 1 ENGINE MANUAL CAUTION LIGHT ILLUMINATED, STAYED ILLUMINATED AFTER CHECKLIST PROCEDURE. MAINTENANCE RESET NR 1 ENGINE ECU PER DHC-8 200 AMM MCN 27631-01. RAN NR 1 AND NR 2 ENGINE AT VARIOUS POWER SETTINGS. NR 1 ECU STAYED ON. CYCLED NR 1 ECU OFF AND ON SEVERAL TIMES WITHOUT ANY DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050919000412005091900041NM 2005 9 19 MASA2005434 120050603A2910DH10201153CS SPU DHAV DHC8 DHC8202 2809007NM NR 2 MALFUNCTIONED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07989HA693 693 427 ASH 6288 PHX. NR 2 SPU AUX POWER LIGHT ON TAKEOFF ROLL. MX REPLACED ANOTHER SPU. TEST FLIGHT CHECKED OUT GOOD. 2H72 4T RTA13NM 20050919000422005091900042NM 2005 9 19 05FDEA02871 120050914A5744 ATTACH BRACKET DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 RIGHT WING - O/B FLAP I/B HINGE (WING SIDE), LWR ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. REPAIR CARRIED OUT AS PER CMM 57-44-08 AND FOUND WITHIN LIMIT AS PER DAC DWG ARC 0502. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2L73 4F RTA22WE 20050919000432005091900043EU 2005 9 19 XNOA1264 120050915A2780 SLAT SYSTEM AIRBUS300 A300B4203 3930306EU MALFUNCTIONED A XN0AA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 GL23307FV 235 AFTER DEPARTURE SLATS WILL NOT RETRACT. PERFORMED CABLE TENSION CHECK OF THE SLAT CONTROLS AND VISUAL CHECK SYSTEM IAW A300 AMM 27-80-00. OPS CHECK GOOD. 2L72 4F RTA35EU 20050919000462005091900046NM 2005 9 19 CALA0500311 120050913A3397W1150513512 WIRE BOEING737 7373T0 1384582NM EMERGENCY LIGHT CHAFED A CALAO OTHER O OTHER CRCRUISE 1 SW2717321 23372 THE EMERGENCY EXIT AISLE PATH LIGHTING ILLUMINATED INTERMITTENTLY WHILE IN CRUISE PORTION OF FLIGHT. MAINTENANCE FOUND WIRES W1150-513 AND -512 CHAFING IN FORWARD CLOSET AREA WHILE REFERENCING WIRING DIAGRAM 33-51-21. THE WIRES WERE REPAIRED AND OPERATION OF THE EMERGENCY LIGHTS CHECKED GOOD. 2L72 4F RTA16WE 20050919000482005091900048EA 2005 9 19 QXEA200501229 120050913A2121 FAN CNDAIRCL600 CL6002C10 1390015EA NR 2 DISPLAY FAILED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09614QX 10049 DEN - ON FLIGHT 2457, AFTER TAKEOFF RECEIVED A DISPLAY COOL CAUTION MESSAGE. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE FOUND THE NR 2 DISPLAY FAN FAILED. PLACED ON MEL 21-24-2, RSI 351876. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20050919000522005091900052NM 2005 9 19 DLM88050495 120050828A2997 WIRE DOUG MD88 MD88 3023688NM HYD PUMP CHAFED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27980DL 53267 SPARKS REPORTED COMING FROM RIGHT MLG WHEEL WELL DURING TAXI IN TO GATE. FOUND AUX HYDRAULIC PUMP POWER C/B POPPED AND WIRE BUNDLE GOING TO PUMP CHAFED AND BURNT IN WHEEL WELL AT HANDLE OF HYD SERVICE HAND PUMP. REPAIRING DAMAGED WIRING. 2L72 4F RTA6WE 20050919000532005091900053NM 2005 9 19 DL73S050496 120050827A5330654577561 SKIN BOEING737 737232 1384475NM FS 727B S-20R CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27308DL 23080 FUSEALGE SKIN CRACKS WAS FOUND AT FS 727B ABOVE STRINGER 20R AT A CHEM MILL LOCATION. THE DAMAGE WAS IDENTIFIED AND REMOVED AN A REPAIR INSTALLED FOLLOWING THE INSTRUCTIONS OF THE B737-200 SRM 53-30-3 FIGURE 48. THE REPAIR IS INSTALLED FOLLOWING INSTRUCTIONS PROVIDED BY ERA 450393-14. 2L72 4F RTA16WE 20050919000542005091900054NM 2005 9 19 DL733050497 120050829A7931SEL0C4W INDICATOR BOEING737 737347 1384647NM CFMINTCFM56 CFM562AFR 13802EU NR 2 ENGINE UNSERVICEABLE A DALAEC ENGINE SHUTDOWN ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO27309WA 141A 23442 721213 DURING T/O ROLL AFTER 80 KTS NR 2 OIL PRESS ROLLED BACK TO BELOW THE RED DIAL. ALL OTHER IND NORMAL. CONTINUED T/O AND PERFORMED LOP CK LIST PROCEDURE PER QRH. ENG SHUTDOWN AND RETURNED TO DTW. SWAP INDICATORS. PROBLEM FOLLOWED. REPLACED NR 2 OIL PRESS IND, OPS CHECK NORMAL. PERFORM WINDMILL INSP, SUPPLY AND SCAVENGE FILTER CLEAN. CHIP DETECTORS CLEAN. PERFORMED POWER ASSURANCE RUN, ENG CHECKS NORMAL. OK FOR SERVICE. 2L72 4F4 FRTA16WE E21EU 20050919000552005091900055NM 2005 9 19 DL76L050498 120050830A361080217010 VALVE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 1 ENGINE MALFUNCTIONED A DALAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO27187DN 27582 724169 RTB - LEFT ENGINE BLEED LIGHT WITH PRV STATUS MSG . REPLACED VALVE. 2L72 4F4 FRTA1NM E24NE 20050919000562005091900056NM 2005 9 19 DLM88050499 120050830A3244MD88M TIRE DOUG MD88 MD88 3023688NM NR 2 DAMAGED A DALAEC ENGINE SHUTDOWN ABORTED TAKEOFF D INFLIGHT SEPARATION TOTAKEOFF 1 SO27991DL 53343 NR 2 TIRE TREAD THROWN ON TAKEOFF. NR 1 ENGINE DAMAGED AND SHUTDOWN. REPLACED TIRE AND ENGINE. 2L72 4F RTA6WE 20050919000572005091900057NE 2005 9 19 DL757050501 220050830A7320DPN286001295 VALVE BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 2 ENGINE FAILED A DALAD RETURN TO BLOCK XJ ENGINE FLAMEOUT WARNING INDICATION TXTAXI/GRND HDL 1 SO27665DN 25013 716363 DURING START OF NR 2 ENGINE, ENGINE SEEMED TO START NORMALLY, THEN RECEIVED ENGINE SPAR VALVE LIGHT AND EICAS MESSAGE. SUBSEQUENTLY RECEIVED ENGINE VALVE LIGHT AND ENGINE FLAMED OUT. REMOVED AND REPLACED NR 2 ENGINE SPAR VALVE PER M/M, RUN AND OPS CHECKS NORMAL. 2L72 4F4 FRTA2NM E17NE 20050919000592005091900059NM 2005 9 19 DL764050506 120050830A3270 CARTRIDGE BOEING767 767432ER 1385134NM TAIL SKID CRUSHED A DALAK NONE O OTHER LDLANDING 1 SO27827MH 29698 ON LANDING NORMAL SINK RATE SPEED BRAKE PARTIALLY DEPLOYED THEN RETRACTED. SUSPECT POSSIBLE TAIL STRIKE. REPLACED TAIL SKID CARTRIDGE. 2L72 4F RTA1NM 20050919000602005091900060NE 2005 9 19 DL76G050508 220050902A7200CF680C2B6F ENGINE BOEING767 767332 1382001NM GE CF6 CF680C2B6F 30025NE NR 2 VIBRATION A DALAC ABORTED TAKEOFF EJ VIBRATION/BUFFET WARNING INDICATION TOTAKEOFF 1 SO27169DZ17860 29689 704751 RIGHT ENGINE FAN VIBS 4.7 HIGH FREQ VIBES FELT. RETURNING TO JFK FOR MTC. 2L72 4F4 FRTA1NM E13NE 20050919000612005091900061NM 2005 9 19 DL764050509 120050903A2121732591F FAN BOEING767 767432ER 1385134NM E/E BAY FAILED A DALAC ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SO27831MH 29702 ATB - FUMES NOTED IN COCKPIT AND 1ST CLASS IN CLIMB. REPLACED FWD EQUIPMENT COOLING FAN. 2L72 4F RTA1NM 20050919000632005091900063NM 2005 9 19 DL76G050511 120050903A2720285T0014104 MODULE BOEING767 767324 1385203NM RUDDER MALFUNCTIONED A DALAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO27394DL UNK 27394 RUDDER RATIO LIGHT AND MSG CAME ON DURING TAXI OUT. UNABLE TO RESET, RETURNED TO GATE. FOUND LEFT RUDDER RATIO MODULE FAULTED. RESET SAME, PERFORMED RUDDER RATIO TEST, CHECKS GODD. OK FOR SERVICE. 2L72 4F RTA1NM 20050919000642005091900064NM 2005 9 19 DLM88050513 120050904A2910 HYDRAULIC SYSTEM DOUG MD88 MD88 3023688NM LEFT CONTAMINATED A DALAO OTHER J WARNING INDICATION DEDESCENT 1 SO27979DL 53266 LEFT HYD PRESS WENT TO 0 QUANTITY, NORMAL ON DESCENT INTO BDL. RECOVERED PRESS WITH TRANS PUMP ON. DECLARED EMERGENCY AND LANDED UNEVENTFULLY. BLED AIR FROM LEFT HYD RESERVIOR, RAN LEFT ENGINE, CYCLED ALL FLT CONTROLS THRU SEVERAL TIMES. SERVICED AND BLED AIR AGAIN. HYD PRESSURE NOW NORMAL WITH LEFT ENGINE OR TRANSFER PUMP. 2L72 4F RTA6WE 20050919000662005091900066NM 2005 9 19 DL73S050516 120050905A2170 COALESCER BAG BOEING737 737232 1384475NM CABIN AIR CONTAMINATED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27308DL 23080 STRONG BURNING RUBBER ODOR ON LIFT OFF. ODOR NOTICED IN COCKPIT AND CABIN. RAN ENGS TO TAKEOFF PWR PER PFHB NTF. REPLACED WATER SEPARATOR BAGS AS PRECAUTIONARY. 2L72 4F RTA16WE 20050919000672005091900067NM 2005 9 19 DL767050518 120050906A5312148T261099 BULKHEAD BOEING767 767232 1385132NM FS 1582 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27103DA 22215 DAMAGE FOUND ON FS 1582 BULKHEAD AT STIFFENER 14L LAPJOINT BETWEEN TEAR STRAPS 4 AND 5. REPAIRED USING DOUBLER/STRUCTURAL SHIMS ON AFT SIDE OF BULKHEAD. BOEING APPROVED WITH AMOC TO AD 2005-03-11. 2L72 4F RTA1NM 20050919000762005091900076NM 2005 9 19 SWAA052779 120050912A53306545776 SKIN BOEING737 7373H4 1384600NM BS 927 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 23L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050919000772005091900077 2005 9 19 SWAA052780 420050912A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29430WN 33659 DURING SCHEDULED RON CHECK, R1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20050919000782005091900078NM 2005 9 19 SWAA052781 120050912A53306545765 SKIN BOEING737 7373Q8 1384670NM BS 510 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29687SW 23388 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510, STR 16L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050919000792005091900079 2005 9 19 SWAA052782 420050913A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29752SW 29804 R2 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20050919000802005091900080NM 2005 9 19 SWAA052783 120050913A3350BR2013 LIGHT BOEING737 7377H4 1384404NM ROW 9 ABC LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29766SW 29806 EEPLS TRACK LOOSE AT ROW 9 ABC. REMOVED AND REPLACED EEPLS TRACK SECTION PER MM. 2L72 4F RTA16WE 20050919000812005091900081NM 2005 9 19 SWAA052784 120050913A3350101073 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29775SW 30590 AFT CABIN EMERGENCY EXIT SIGN LENS MISSING. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20050919000852005091900085EA 2005 9 19 SWIA200515538 120050914A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS INTERMITTENT A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 NM07962SW 7859 ON APPROACH FLAPS FAIL MESSAGE DISPLAYED AT 8 DEGREES. RESET FLAP SYSTEM AND PERFORMED FLAP SYSTEM TEST. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050919000862005091900086EA 2005 9 19 SWIA200515539 120050914A215078279015 ACM CNDAIRCL600 CL6002B19 1900309EA LEFT SMOKE A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM07932SW7133 7133 7714 ON GROUND LEFT PACK TEMP ROSE THROUGH 118 DEGREES WITH SMOKE. REPLACED LT ACM IAW MM 21-51-10. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050919000922005091900092SO 2005 9 19 SWIA200515545 120050905A3350 SIGN EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT MISSING A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07565SW 120340 EMERGENCY EXIT SIGN MISSING FORWARD DOOR. INSTALLED NEW EMERGENCY LIGHT FIXTURE, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050919000962005091900096NM 2005 9 19 PIDA20050076 120050617A5315 FLOORBEAM BOEING737 737228 13844AGNM BS 312 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05237TR 23007 BS 312 FLOORBEAM HAS CORROSION FROM LBL 20 TO RBL 20 AT FASTENER HOLES. REPAIRED FLOORBEAM PER SRM 53-10-9. 2L72 4F RTA16WE 20050919000972005091900097NM 2005 9 19 PIDA20050075 120050623A5315 FLOORBEAM BOEING737 737228 13844AGNM BS 294 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05237TR 23007 BS 294 FLOORBEAM HAS CORROSION FROM LBL 28 TO RBL 45 AT FASTENER HOLES. REPAIRED FLOORBEAM PER SRM 53-10-9. 2L72 4F RTA16WE 20050919001002005091900100NM 2005 9 19 PIDA20050078 120050708A5315 FLOORBEAM BOEING737 737228 13844AGNM BS 986 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05237TR 23007 BS 986 FLOORBEAM HAS CORROSION AT LBL 20 TEE CHORD. REPAIRED FLOORBEAM T-CAP AT LBL 20 PER SRM 53-10-9. 2L72 4F RTA16WE 20050919001022005091900102NM 2005 9 19 PIDA20050087 120050623A5320 INTERCOSTAL BOEING737 737228 13844AGNM BS 312-328 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05237TR 23007 INTERCOSTAL AT LBL 11 FROM BS 312 TO BS 328 HAS CORROSION AT NUT PLATE HOLES. REPLACED INTERCOSTAL PER SRM 51-10-1. 2L72 4F RTA16WE 20050919001032005091900103NM 2005 9 19 PIDA20050093 120050707A5320 INTERCOSTAL BOEING737 737228 13844AGNM BS 1006 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05237TR 23007 INTERCOSTAL WEB AND STRAP HAVE CORROSION AT ATTACH FASTENER AT BS 1006 FLOORBEAM AT LBL 26. REPLACED WEB AND STRAP PER DWG 65-46812 AND SRM 51-10-1 AND SRM 51-10-2. 2L72 4F RTA16WE 20050919001042005091900104NM 2005 9 19 PIDA20050086 120050627A5320 INTERCOSTAL BOEING737 737228 13844AGNM BS 298 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05237TR 23007 INTERCOSTAL FROM RBL 16 TO RBL 31 AT BS 298 HAS CORROSION ON TOP SURFACE. REPLACED INTERCOSTAL PER SRM 51-10-1. 2L72 4F RTA16WE 20050919001072005091900107NM 2005 9 19 PIDA20050094 120050707A5320 INTERCOSTAL BOEING737 737228 13844AGNM BS 1006-1016 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05237TR 23007 DIAGONAL INTERCOSTAL AND OVERLAPING WEB HAVE CORROSION FROM BS 1006 TO BS 1016 AT LBL 4. REPLACED CORRODED SHIM OF INTERCOSTAL PER SRM 51-10-1. 2L72 4F RTA16WE 20050919001092005091900109NM 2005 9 19 PIDA20050103 120050628A5340 ANGLE BOEING737 737228 13844AGNM BS 500A-520 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05237TR 23007 TRANSITION ANGLE IN FWD CARGO BIN IS CORRODED FROM BS 500A TO BS 520. REPLACED TRANSITION ANGLE PER SRM 51-10-1. 2L72 4F RTA16WE 20050919001112005091900111NM 2005 9 19 PIDA20050096 120050707A4910655483830 FITTING BOEING737 737228 13844AGNM APU DOOR HINGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05237TR 23007 AFT ANGLE FOR AFT APU DOOR HINGE CRACKED. REPLACED FITTING AND ATTACH ANGLES PER DWG 65-54838. 2L72 4F RTA16WE 20050919001122005091900112NM 2005 9 19 PIDA20050098 120050706A5340 SUPPORT BRACKET BOEING737 737228 13844AGNM BS 1016 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05237TR 23007 BLEED AIR DUCT SUPPORT BRACKET AND ATTACH ANGLES AT BS 1016 AT LBL 12 HAVE CORROSION. REPLACED DUCT SUPPORT BRACKET AND ANGLES PER SRM 51-10-1. 2L72 4F RTA16WE 20050919001152005091900115NM 2005 9 19 PIDA20050101 120050630A5320 INTERCOSTAL BOEING737 737228 13844AGNM BS 1016-1040 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05237TR 23007 INTERCOSTAL FROM BS 1016 TO BS 1040 CORRODED. REPLACED INTERCOSTAL PER SRM 51-10-1. 2L72 4F RTA16WE 20050919001212005091900121NM 2005 9 19 PIDA20050070 120050713A5330 SKIN BOEING737 737228 13844AGNM BS 500A-520 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05237TR 23007 CORROSION BULGE IN LOWER SKIN AT STRINGER 28 LT (KEELBEAM) AT BS 500A +12 AND BS 520. TRIMMED OUT DAMAGED SECTION AF SKIN AND REPAIRED PER EA 53-170. (KEELBEAM REPAIR ON SDR PIDA20050069.) 2L72 4F RTA16WE 20050919001222005091900122NM 2005 9 19 PIDA20050097 120050629A5340 MOUNT BOEING737 737228 13844AGNM RADAR SYS CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05237TR 23007 SHELF THAT RADAR T/R RACK MOUNTS TO HAS A CRACK IN BOTH AFT CORNERS. REPAIRED MOUNT ANGLES PER SRM 51-40-3. 2L72 4F RTA16WE 20050919001252005091900125EA 2005 9 19 COMA0560495 120050911A3210 LANDING GEAR CNDAIRCL600 CL6002B19 1900309EA MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01924CA 7026 FLIGHT 5425 - DURING APPROACH RECEIVED AN INTERMITTENT GEAR DOWN DISAGREE CAUTION MESSAGE. PERFORMED MULTIPLE GEAR SWINGS ON JACKS, DISCREPANCY COULD NOT BE DUPLICATED. 2L72 4F RTA21EA 20050914000142005091400014EA 2005 9 14 QXEA200501219 120050906A3213 STRUT CNDAIRCL600 CL6002C10 1390015EA NLG DISCHARGED A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09609QX 10031 PDX- ON FLIGHT 4218 DURING TAXI OUT, THE NOSE STRUT BOTTOMED OUT. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE SERVICED THE NOSE STRUT IAW AMM 12-12-32-610-803-A01. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2L72 4F RTA21EA 20050914000222005091400022CE 2005 9 14 DXTA200500960 120050909A215073838433 ACM CESSNA750 750 2076810CE ACM BAY FAILED E DXTAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07920QS435 7500120 ABOUT 1 HOUR INTO OUR FLIGHT AT FL410, DETECTED AN ODOR IN THE COCKPIT THAT SMELLED ELECTRICAL IN NATURE. SYSTEMS WERE OPERATING NORMALLY AND THE SMELL DISSIPATED AFTER ABOUT 5 MINUTES THEN AFTER LANDING WITH THE APU RUNNING, DETECTED THE SAME SMELL. THE A/C THEN FILLED WITH SMOKE ORIGINATING FROM THE COCKPIT. AGAIN, THERE WERE NO OTHER OBVIOUS SIGNS OF SYSTEMS MALFUNCTION. REMOVED AND REPLACED COCKPIT AIR CYCLE MACHINE. ALSO REMOVED, CLEANED AND REINSTALLED COALESCER CLOTH. NO FURTHER DEFECTS NOTED. ALL OPERATIONS NORMAL AT THIS TIME. ALL WORK PERFORMED IAW CE 750 AMM 21-51-00. 2L72 4J RTT00007WI 20050914000302005091400030NM 2005 9 14 2005UALA00930 120050903A5414 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 1 PYLON DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29511UA 24799 NR 1 PYLON OB SKIN DAMAGED. REPAIRED PER SRM 54-31-99. 2L72 4F4 FRTA2NM E17NE 20050914000312005091400031NM 2005 9 14 2005UALA00931 120050903A5312 BULKHEAD BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE BS 1016 GOUGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29327UA 24147 AFT PRESSURE BULKHEAD HAS SEVERAL GOUGES AND SCRATCHES AT UPPER ELECTRICAL CONDUIT THROUGH LT SIDE LBL 5 TO LBL 3 WL 84. 2L72 4F4 FRTA16WE E2GL 20050914000332005091400033NM 2005 9 14 2005UALA00933 120050904A5311 FRAME BOEING747 747422 1384935NM PWA 4056 PW4056 NE BS 1800 PUNCTURED A UALAK NONE O OTHER ININSP/MAINT 1 WP29119UA 28812 AFT CARGO COMPARTMENT BS 1800 LBL 50 LWR LOBE FRAME WEB PUNCTURED. LOCAL DAMAGE TO FRAME WEB; CAUSE UNKNOWN. FAA APPROVED PERMANENT REPAIR INSTALLED. 2L74 4F4 FRTA20WE E24NE 20050914000372005091400037EU 2005 9 14 2005UALA00937 120050905A5313 STRINGER AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FR 58-59 CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29420UA 489 STR 43L HAS CORROSION BETWEEN FS 58-59. CUT-OUT DAMAGED SECTION AND SPLICED IN NEW SECTION REF SRM 53-00-13 FIG 201. 2L72 4F4 FRTA28NM E40NE 20050914000432005091400043NM 2005 9 14 2005UALA00943 120050902A2120 SMOKE BOEING777 777222 1385219NM PWA PW4077PW4077 NE LAVATORY DETECTED A UALAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 WP29774UA 26936 CREW REPORT OF SMOKE SMELL IN THE AREA OF LAV 3L. ODOR REPORTED INSIDE LAV 3L ONLY; FIRE OFFICIALS INSPECTED AREA ABOVE AND INSIDE LAV WITH HEAT DETECTION EQUIPMENT; NO PROBLEMS FOUND. NO FURTHER OCCURRENCES OF SMOKE OR ODOR NOTED SUBEQUENT TO THIS REPORT. ROOT CAUSE UNKNOWN. 2L72 4F4 FRTT0001SE E46NE 20050914000532005091400053WP 2005 9 14 IXXA05RNG040S 120050723A5754 SKIN DOUG DC8 DC862F 3021972WP LT WING SLAT DENTED B IXXAK NONE O OTHER ININSP/MAINT 1 SW1171CX 670243317 45961 DURING INSPECTION CHECK, FOUND A DENT AT WING OUTER INBOARD EXTENDED LEADING EDGE PLATING STA XFS 610 TO SPAR LT. EXTERNAL DOUBLER WAS FABRICATED AND INSTALLED IAW EWO ATI 57-032 AND SRM 57-2-1 FIGURE 2H. 2L74 4F 4A25 20050914000602005091400060WP 2005 9 14 UPS05845371 120050811A5340 FITTING DOUG DC8 DC871F 302199DWP FS 759 LBL 48 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 INSPECTION TYPE:C1 CENTER WING SUB FLOOR FS 759 LBL 48 L-FITTING CRACKED. REMOVED CRACKED L-FITTING IAW SRM 51-1-20D, FABRICATED AND INSTALLED L-FITTING IAW DWG 3643110 AND 51-1-20D. 2L74 4F RT4A25 20050914000632005091400063NM 2005 9 14 QXEA200501217 120050906A3297471515 WIRE HARNESS BOMBDRDHC8 DHC8402 1390042NM WOW DAMAGED A QXEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM09415QX 4081 LAX FLIGHT: AFTER TAKEOFF, LANDING GEAR FAILED TO RETRACT. AIRCRAFT WAS FERRIED TO PDX. MAINTENANCE INTERGATED PSEU AND FOUND NW CENT OPEN IN THE PRESENT FAULTS. REMOVED NLG WOW 2/CENTERING HARNESS IAW MM TASK 32-21-11-000-801. REPLACED AND INSTALLED HARNESS IAW 32-21-11-400-801. PERFORMED A FUNCTIONAL TEST OF THE NOSE WHEEL STEERING SYSTEM AND AN OPERATIONAL TEST OF THE LANDING GEAR EXTENSION AND RETRACTIONAL TEST CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050914000642005091400064WP 2005 9 14 ARWA20050903 120050623A5330 SKIN DOUG DC8 DC863F 302198FWP BS 1690-1720 CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19784AL 46135 DURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND; LOWER FUSELAGE STA 1690 THROUGH STA 1720, L-31L THROUGH L-31R, SKIN PANEL WITH CORROSION AT SEVERAL PLACES. 2L74 4F 4A25 20050914000722005091400072EU 2005 9 14 MALA050687 120050903A5347 SEAT TRACK BAC 146 AVRO146RJ85A1500097EU FR 18 CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15507XJ E2316 WHILE ACCOMPLISHING C1 INSPECTION FOUND SEAT RAIL AT FRAME 18 FLOORBEAM RBL 30 CORRODED. 2H74 4F RTA49EU 20050914000842005091400084EU 2005 9 14 AALA20050580 120050908A4990 APU AIRBUS300 A300B4605R 3930308EU APU BAY LEAKING A AALAA UNSCHED LANDING KBJFLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SW2111060 470 LIR - AIR INTERRUPT INTO LIR DUE TO SMOKE IN CABIN. LANDED LIR WITHOUT INCIDENT. REPLACED WATER SEPARATOR BAGS AND ACCOMPLISHED PACK BURN. PLACARD APU. MIA FOUND OIL IN APU COMPARTMENT. AIRCRAFT OUT OF SERVICE FOR REPAIRS. 2L72 4F RTA35EU 20050914000972005091400097NM 2005 9 14 C1HA200581008 120050909A5311 FRAME BOEING727 7272S7 138407ZNM BS 700 DENTED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15681CA 22020 FRAME DENTED IN FWD CARGO PIT STA 700 OVER STRINGER 25R, MARKED. CUT OUT DAMAGED AREA DIM 3 X .625 INCH AND FABBED REPAIR ANGLE FROM 7075T6 .063 PO 9002351 DIM 11 X 3. .875 INCH IAW 727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1. ANGLE TREATED, PRIMED AND INSTALLED IAW 727 SRM 51-10-2 AND 51-40-3 FIG 1. 2L73 4F A3WE 20050914001172005091400117WP 2005 9 14 ABXA050211 120050909A3397 WIRE DOUG DC9 DC933F 302207AWP COCKPIT LIGHT BROKEN A ABXAK NONE O OTHER NRNOT REPORTED 1 GL23933AX 47291 FIRST OFFICER'S BRIEFCASE LIGHT EMITTED ELECTRICAL SPARKS OUT OF THE LIGHT/LENSE AREA. MAINTENANCE REPAIRED BROKEN WIRE AT BRIEFCASE LIGHT. OPS CHECKED OK IAW ABX MAINTENANCE MANUAL 33-10. 2L72 4F A6WE 20050915000162005091500016EU 2005 9 15 2005UALA00958 120050908A5320 SILL AIRBUS320 A320232 3930326EU RT PAX DOOR CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29420UA 489 AFT RIGHT CABIN DOOR SILL PLATE HAS CORROSION UNDER AFT SLIDE MOUNT. 2L72 4F RTA28NM 20050915000212005091500021NM 2005 9 15 05FDEA02838 120050912A5330 SKIN BOEING727 727200 138407ENM BS 988 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 AFT CARGO COMP PREVIOUS REPAIR SKIN CUTOUT HAS CORRODED BS 988 RBL 11 BILGE. REPAIRED SKIN CUTOUT AT BS 988, RBL 11 PER FED-EX EA 7-5330-91368. 2L73 4F RTA3WE 20050915000232005091500023NM 2005 9 15 05FDEA02840 120050912A5330 SKIN BOEING727 727200 138407ENM BS 700 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25268FE 21674 WHILE WORKING CARD, FOUND CORROSION ON SKIN AT BS 700, BL 0, WL 149.5 BETWEEN STR 28R-STR 28L. REPAIRED PER SRM 53-30-3, MAJOR REPAIR. 2L73 4F RTA3WE 20050915000302005091500030 2005 9 15 SWAA052776 420050912A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29639SW 27712 R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20050915000332005091500033NM 2005 9 15 05FDEA02850 120050913A2750 CONNECTOR BOEING727 727200 138407ENM TE FLAPS LOOSE A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25490FE 21493 ON DEPARTURE GOING FROM FLAPS 5 TO 2 THE INBOARD FLAP INDICATOR SHOWED FLAPS REMAINED AT 5. RAN QRH WITH NO CHANGE. AIRCRAFT HAD NO ADVERSE FLIGHT FEEL. RIGHT I/B FLAP POSITION TRANSMITTER CONNECTOR FOUND LOOSE. RESECURED AND SAFETIED IAW SMP. CYCLED FLAPS SEVERAL TIMES AND INDICATIONS WERE NORMAL. REF: AMM 27-52-000-0. 2L73 4F RTA3WE 20050915000342005091500034NM 2005 9 15 05FDEA02851 120050913A5710 STRUCTURE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25577FE 48469 DURING PASSENGER TO FRIEGHT CONVERSION, FOUND THE SEQUENT PUFFIN CORROSIONS ON THE UPPER RIGHT WING SKIN IN THE FOLLOWING ZONE: FROM WING CROSS-SECTION STA XORS 402 TO XORS 433. NOTE: THE UPPER MENTIONED CORROSIONS HAVE BEEN INDIVIDUALIZED IN 2 POINT. BLENDOUT ALL EVIDENCE OF CORROSION AS PER SRM 57-10-00 FIG 32. MEASURE AND RECORD REWORKED POSITION, DIMENSIONS AND SKIN RESIDUAL THICKNESS. REWORKED IS IN LIMITS FOR SRM 57-10-00 FIG 32. PROTECT AREA PER SRM 51-21-02. 2L73 4F RTA22WE 20050915000352005091500035NM 2005 9 15 05FDEA02852 120050913A5710 STRUCTURE DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25577FE 48469 DURING PASSENGER TO FRIEGHT CONVERSION, FOUND THE SEQUENT PUFFIN CORROSIONS ON THE UPPER LEFT WING SKIN IN THE FOLLOWING ZONES: FROM WING CROSS-SECTION STA XORS 97 TO XORS 1042. NOTE: THE UPPER MENTIONED CORROSIONS HAVE BEEN INDIVIDUALIZED IN 38 POINT. BLENDOUT ALL EVIDENCE OF CORROSION AS PER SRM 57-10-00 FIG 32. MEASURE AND RECORD REWORKED POSITION, DIMENSIONS AND SKIN RESIDUAL THICKNESS. REWORKED AREA ARE ACCEPTABLE PER SRM 57-10-00 FIG 32 AND BOEING MESSAGE N 1-111785997-4. PROTECT AREA PER SRM 51-21-02. 2L73 4F RTA22WE 20050915000442005091500044WP 2005 9 15 AALA20050585 120050910A321359632541 STRUT DOUG DC9 DC982 3022082WP NLG INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21269AA 49292 DFW INFLIGHT T2409/10SEPT LOUD NOISE AND EXCESSIVE VIBRATION FROM NOSE WHEEL AREA AFTER GEAR RETRACTION. CONTINUED AFTER NOSE WHEEL SPINDOWN. NOSE WHEEL INDICATOR LIGHT WAS RED WITH THE GEAR HANDLE UP. REPLACED NOSE GEAR STRUT AND LOWER SCISSOR LINK TORQUE PIN. SERVICED NOSE STRUT WITH OIL AND AIR. REPLACED BOTH LEFT AND RIGHT HAND NOSE TIRES AS PRECAUTION. PERFORMED FUNCTION CHECK FLIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050915000532005091500053WP 2005 9 15 AALA20050590 120050912A33506011779 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW219403W 53139 SFO OVERHEAD EMERGENCY LIGHTS AT ROWS 23, 24B, AND 26 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT ROWS 23, 24B, AND 26. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050915000562005091500056NM 2005 9 15 DHL2005786002 120050903A7931ST104Z TRANSMITTER BOEING727 727214 138407RNM NR 1 ENG OIL MALFUNCTIONED A DHLAED ENGINE SHUTDOWN RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01786AT 21692 DISC - NR 1 ENG OIL PRESSURE BELOW RED LINE DURING TAXI OUT. RAN ABNORMAL PROCEDURE, SHUT ENGINE DOWN. REMOVED AND REPLACED NR 1 ENG OIL PRESSURE TRANSMITTER IAW B727 MM 79-32-01. OPS CHECKS GOOD. 2L73 4F A3WE 20050915000692005091500069NM 2005 9 15 05FDEA02845 120050913A5320 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 CENTER CARGO LONGERON SPLICE FOUND CRACK AT STA 1541 L-32 LEFT HAND. NEW LONGERON SPLICE FABRICATED AS PER DRAWING A5A7112. CRACKED LONGERON SPLICE ON STA 1541 LONGERON 32 REMOVED AND REPLACED AS PER SRM 51-33- 01 VOL II. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050915000742005091500074NM 2005 9 15 SWAA052677 120050901A53306545769 SKIN BOEING737 7373H4 1384600NM BS 379 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29394SW 27380 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 379, STR 27L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050915000772005091500077EU 2005 9 15 09082005B 120050904A3350 LIGHT SAAB SF340 340B 7860101EU PAX DOOR INOPERATIVE A NSVAO OTHER O OTHER TXTAXI/GRND HDL 1 EA27233CJ 233 MAIN CABIN DOOR AND GALLEY EMERGENCY LIGHTS INOP. RECHARGED SYSTEM WITH EXTERNAL POWER, OPS CHECK GOOD. 2L72 4T RTA52EU 20050915000832005091500083CE 2005 9 15 09082005F 120050906A7603 POWER LEVER BEECH 1900 1900D 1154162CE RT ENGINE OUT OF RIG A NSVAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 EA27220CJ UE20 RT POWER LEVER HAS 1 FULL KNOB SPLIT ABOVE LT KNOB. RERIGGED RT ENGINE. 2L72 4T RTA24CE 20050915000872005091500087EU 2005 9 15 09092005B 120050907A7712 INDICATOR SAAB SF340 340B 7860101EU LT TORQUE MALFUNCTIONED A NSVAO OTHER N FALSE WARNING TOTAKEOFF 1 EA27321CJ 321 LT TORQUE GAUGE INDICATED AN ADDITIONAL 7 PERCENT ON T/O WITH APR ENGAGED. MEL'ED SYSTEM. 2L72 4T RTA52EU 20050915000972005091500097SO 2005 9 15 C2XA05BT060 120050817A3220 LANDING GEAR EMB 145 EMB145LR 3260212SO NOSE COLLAPSED A C2XAO OTHER O OTHER TXTAXI/GRND HDL 1 SW2716911 145446 CREW REPORTED, "NOSE LANDING GEAR COLLASPED ON PUSH BACK FROM GATE." MAINTENANCE TROUBLESHOOTING AND REPAIRING AIRCRAFT. 2L72 4T RTT00011AT 20050915000992005091500099SO 2005 9 15 C2XA05CL081 120050909A3350110049 CHARGER EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713123 145688 DURING ROUTINE MAINTENANCE, THE LAST TWO EMERGENCY AISLE PATH LIGHT STRIPS WERE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY AND POWER SUPPLY. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RT 20050915001022005091500102SO 2005 9 15 C2XA05IA100 120050822A243232845001 BATTERY EMB 145 EMB145XR 3260214SO NR 1 MAIN OVERTEMP A C2XAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CRCRUISE 1 SW27111762638 633 14500881 CLE - FLIGHT 2995, THE CREW REPORTED A BATTERY ONE OVERTEMP IN CRUISE. THE AIRCRAFT DIVERTED TO CLE WHERE IT LANDED WITHOUT INCIDENT, AND MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE MAIN BATTERY. OPERATIONAL CHECKS WERE GOOD, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20050915001052005091500105SO 2005 9 15 C2XA05CL077 120050906A21508152403 ACM EMB 135 EMB135ER 3260203SO NR 1 DEFECTIVE A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2714508 135220 CLE FLIGHT NR 2268, CREW REPORTED, SAW AND SMELLED SMOKE IN THE AIRCRAFT WITH PACK NR 1 ON. MAINTENANCE INSPECTED AND REMOVED AND REPLACED NR 1 AIR CYCLE MACHINE. OPERATIONAL CHECKS WERE REPORTED GOOD. 2L72 4F RTT00011AT 20050915001142005091500114NM 2005 9 15 CALA0500301 120050905A53306545775 SKIN BOEING737 7373T0 1384582NM STA 747 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717326 23456 A WALKAROUND FOUND A 4 INCH CRACK IN RT FUSELAGE SKIN AT BS 747, S19R. REPAIRED IAW SRM 53-00-01, FIGURE 229. 2L72 4F RTA16WE 20050915001172005091500117SO 2005 9 15 LR7A05112 120050904A215020343041 COOLING TURBINE LKHEED382 382G 526414USO FS 196 FAILED A LR7AH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 AL03401LC 189 4606 FLIGHT CREW REPORTED FLIGHT DECK AIR CONDITIONING TURBINE BEGAN TO SQUEAL, OUTPUT SMELLED HOT AND OILY. SHUT OFF PACK. REPLACED FLIGHT DECK COOLING TURBINE IAW MM SMP 581 21-50 PG 206. OPS CHECKED NORMAL. LP 17550 ITEM 1. 2H74 4T A1SO 20050915001192005091500119NM 2005 9 15 QXEA200501204 120050903A2751 WARNING LIGHT BOMBDRDHC8 DHC8402 1390042NM TE FLAPS FALSE INDICATIONA QXEAO OTHER N FALSE WARNING LDLANDING 1 NM09409QX 4051 PDX FLIGHT 2815: ON SHORT LANDING APPROACH, WHEN FLAPS SELECTED FROM 10 TO 15 DEG, FLAPS REMAINED AT 10 DEG AND FLAP POWER CAUTION LIGHT ILLUMINATED. ELECTED TO LAND WITH FLAPS AT 10 DEG AND RAN ASSOCIATED E/A CHECKLIST WHEN STOPPED ON TAXIWAY. PERFORMED FLAP CONT C/B RESET IAW CHECKLIST. FLAP POWER CAUTION LIGHT EXTINGUISHED AND RETRACTED FLAPS TO ZERO NORMALLY AND PARKED. MAINTENANCE DETERMINED THIS TO BE NUISANCE CAUTION LIGHT PER BOMBARDIER SERVICE LETTER DHC8-400-SL-27-002A. 2H72 4T RTA13NM 20050915001252005091500125NM 2005 9 15 BB05073 120050831A2750285T004953 FCU BOEING767 767201 1385125NM TE FLAPS FAULTY A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19645US454726642 23897 PHL - FLT 564 - EN ROUTE, PHL TO GLA - AFTER TAKEOFF, FLAPS WOULD NOT RETRACT PAST 1 UNIT WITH THE FLAP HANDLE IN THE UP POSITION. EICAS STATUS MESSAGE, "FLAP/SLAT ELEC", WAS INDICATED. THE FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FLAP SLAT ELECTRONIC UNIT. OPERATIONALLY CHECKS OK. 2L72 4F RTA1NM 20050915001262005091500126NM 2005 9 15 BB05075 120050831A3260 WARNING LIGHT BOEING757 7572B7 1384964NM MLG FALSE ACTIVATIONA USAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19633AU 27811 CLT - FLT 667, EN ROUTE CLT TO LAS - AFTER TAKEOFF, RECEIVED AN EICAS MESSAGE "GEAR DOOR" WITH THE LANDING GEAR HANDLE UP. ALSO, RECEIVED AN AMBER "DOORS" LIGHT. THE GEAR LIGHT AND ALL THREE GREEN DOWN AND LOCKED LIGHTS EXTINGUISHED. THE CREW CYCLED THE GEAR, BUT STILL HAD THE SAME INDICATIONS. THE FLT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED TROUBLESHOOTING PROCEDURES AND NUMEROUS GEAR SWINGS. THE FAULT COULD NOT BE DUPLICATED. OPERATIONALLY CHECKS OK. 2L72 4F RTA2NM 20050915001292005091500129EU 2005 9 15 MALA050692 120050903A5420 BUSHING BAC 146 AVRO146RJ85A1500097EU NR 3 PYLON MIGRATED A MALAK NONE O OTHER ININSP/MAINT 1 GL15507XJ E2316 WHILE ACCOMPLISHING C3.IG1 INSPECTION FOUND THE NR 3 ENGINE PYLON TO YOKE LINK BUSHINGS HAVE MIGRATED OUT. 2H74 4F RTA49EU 20050915001322005091500132EU 2005 9 15 MALA050712 120050903A5240 SEAL BAC 146 AVRO146RJ85A1500097EU DOOR CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15507XJ E2316 WHILE ACCOMPLISHING F1.E INSPECTION FOUND AFT CARGO DOOR SEAL RETAINER CHAFED IN 3 PLACES. 2H74 4F RTA49EU 20050915001362005091500136EU 2005 9 15 MALA050706 120050903A5520 STRUCTURE BAC 146 AVRO146RJ85A1500097EU ELEVATOR CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15507XJ E2316 WHILE ACCOMPLISHING C2 INSPECTION FOUND CORROSION ON THE RIGHT ARM OF THE ELEVATOR DISCONNECT LEVER ASSEMBLY AT FRAME 11 ON ELECTRICAL EQUIPMENT BAY ROOF. 2H74 4F RTA49EU 20050915001382005091500138NM 2005 9 15 05FDEA02831 120050910A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 HORIZONTAL STAB RT BARREL NUT BORE NR 15 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 8. MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20050915001442005091500144NM 2005 9 15 SWAA052682 120050903A3350MS155721 BULB BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29487WN 33854 DURING SCHEDULED MV2 CHECK, FOUND RT EMERGENCY EXTERIOR LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050915001492005091500149NM 2005 9 15 SWAA052686 120050902A53216546833 WEB BOEING737 7375H4 138449DNM COCKPIT FLOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29503SW 24180 DURING SCHEDULED SPECIAL VISIT, FOUND COCKPIT FLOOR WEB CRACKED BETWEEN BS 188 TO BS 196, LBL 29 TO RBL 29, WL 208. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050915001512005091500151NM 2005 9 15 SWAA052688 120050902A53306545775 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29503SW 24180 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT AFT CARGO DOOR CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050915001532005091500153NM 2005 9 15 DL777050492 120050827A3230161W60221 SPRING BOEING777 777232 1385232NM RT MLG UPLOCK FAILED A DALAK NONE S AFFECT SYSTEMS ININSP/MAINT 1 SO27860DA 29951 DURING PDC FOUND RT MLG UPLOCK SPRING MISSING. REPLACED SAME. 2L72 4F RTT00001SE 20050915001692005091500169NM 2005 9 15 DL76S050473 120050822A2611SAAU308C SMOKE DETECTOR BOEING767 767332 1382001NM INOPERATIVE A DALAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 SO27120DL 23279 MID LEFT SMOKE DETECTOR WOULD NOT SILENCE. REPLACED SMOKE DETECTOR. 2L72 4F RTA1NM 20050915001712005091500171NM 2005 9 15 DL767050481 120050823A3350M9008 POWER SUPPLY BOEING767 767232 1385132NM EMERGENCY LIGHT INOPERATIVE A DALAO OTHER O OTHER CRCRUISE 1 SO27101DA 22213 EMERGENCY LIGHTS INOP THROUGHOUT CABIN. REPLACED M9008 POWER SUPPLY, CHECKS OK. 2L72 4F RTA1NM 20050915001722005091500172NE 2005 9 15 DLM88050483 220050823A7200 ENGINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 MALFUNCTIONED A DALAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SO27910DE 53419 725944 ON TAKEOFF ROLL, NR 2 ENGINE WOULD NOT ACCELERATE ABOVE IDLE POWER ABORTED TAKEOFF BELOW 80 KTS. OPENED NR 2 ENG COWL TO INSP FUEL CONTROL LINKAGE, NO OBVIOUS DAMAGE. INSP ALL HARD LINES TO FCU FOR SECURITY - NTF. CHECKED MOISTURE TRAP, TRAP DRY. FOUND BELLOWS UNDER SERVICED. SUPP SAME PER M/M. RAN ENG FOUND PT PWR OUT OF ADJUSTMENT. C/W PFHB TESTS 9077 TEST C, D, AND P, ALL CHECKS GOOD. A/C OK FOR SERVICE. 2L72 4F4 FRTA6WE E9NE 20050915001902005091500190NM 2005 9 15 DL764050542 120050913A3397 CONNECTOR BOEING767 767432ER 1385134NM EMERGENCY LIGHT DISCONNECTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27836MH 29709 EMERGENCY TRACK LIGHTS OUT AT SEATS 19AB-24AB AND 19FG-24FG. FOUND EMERGENCY TRACK LIGHTING CONNECTOR DISCONNECTED AT SEAT 19AB AND SEAT 19FG. 2L72 4F RTA1NM 20050915001932005091500193NM 2005 9 15 MASA200500615 120050805A2611PU90461R2 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM LAVATORY MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07456YV785 456 ASH 7065 DEN. PILOT REPORTS LAV SMOKE DETECTOR STAYS ON AT ALL TIMES. CREW VERIFIED NO SMOKE OR FIRE. MAINTENANCE REPLACED LAV SMOKE DETECTOR. 2H72 4T RTA13NM 20050915001962005091500196NM 2005 9 15 MASA200500631 120050811A2611473054 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM CARGO BAY INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07987HA3389 425 ASH 6370 YUM. THE NR 2 BAGGAGE COMP SMOKE DETECTOR INOP. REPLACED DETECTOR. 2H72 4T RTA13NM 20050919000052005091900005EU 2005 9 19 05FDEA02907 120050914A5321231VG2 FLOOR PANEL AIRBUS310 A310 EU GE CF6 CF680 30025NE CARGO DECK CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25425FE 264 MDCC FLOOR PANEL 231VG-2 IS CRACKED. FABED NEW FLOOR PANEL. 2L72 4F4 FRTA35EU E13NE 20050919000162005091900016EU 2005 9 19 05FDEA02917 120050914A5347 SEAT TRACK AIRBUS310 A310 EU GE CF6 CF680 30025NE CARGO DECK CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25425FE 264 MDCC SEAT TRACK IS CORRODED. REMOVED CORRODED TRACK AND INSTALLED NEW TRACK IAW SRM53-10-16, 51-40-21, AND51- 23-10. 2L72 4F4 FRTA35EU E13NE 20050919000202005091900020WP 2005 9 19 PNSA050904 220050907A7200 ENGINE SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TFE33112UHR WP NR 2 OVERSPEED A PNSAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 AL032719H 713B ON TAKEOFF PILOT NOTICED THAT THE NR 2 ENGINE WAS IN AN OVERSPEED CONDITION. PILOT ABORTED TAKEOFF AND RETURNED TO MAINT HANGAR, MX FOUND THAT THE PROP GOVENOR WAS OUT OFF RIG. ADJUSTMENT WAS MADE AND ENGINE OPS CHECKED NORMAL. NOTE MX HAD WORKED ON SYSTEM THAT AFFECTED THE ENGINE SPEED EARLIER THAT MORNING. 2L72 4T4 TRTA8SW E4WE 20050919000262005091900026WP 2005 9 19 UPS05845413 120050903A5712 RIB DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE: C3, LT WING L/E LOWER RIB IS CRACKED AT XFS 660.000. STOP DRILLED CRACK, FABRICATED AND INSTALLED 2 EA REPAIR DOUBLERS IAW SRM 57-2-0, 51-1-20D AND 51-1-21. 2L74 4F RT4A25 20050919000352005091900035EA 2005 9 19 VTZA200500185 120050914A53116013600130 DOUBLER CNDAIRCL600 CL6002B19 1900309EA FRAME CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27655BR 7457 RIGHT FRAME DOUBLER CRACKED IN RADIUS AT 1 INCH IN LENGTH. 2L72 4F RTA21EA 20050919000382005091900038 2005 9 19 QXEA200501226 420050914A3420 WARNING LIGHT DHAV DHC8 DHC8202 2809007NM FLT DIRECTOR ILLUMINATED A QXEAO OTHER O OTHER TXTAXI/GRND HDL 1 NM09368PH 512 LWS FLIGHT 2023 - FLIGHT DIRECTOR HEADING DATA MESSAGE ON BOTH ADVISORY DISPLAYS. CYCLED AIRCRAFT POWER PER MAINTENANCE CONTROL. ALL INDICATIONS NORMAL. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050919000652005091900065 2005 9 19 DL76G050514 420050904A3444 IRU BOEING767 767332 1382001NM COCKPIT MALFUNCTIONED A DALAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 SO27169DZ 29689 AFTER T/O IRUS DID NOT RADIO UPDATE. IRU POSITION SHOWED APPROX 200 MILES FROM FIRST WAYPOINT. PERFORMED FULL IRU ALIGNMENT. ALL 3 IRUS CHECKS OK PER AMM. PERFORMED FMS TEST, ALL INPUTS OK. FMS MONITOR TEST OK. 2L72 4F RTA1NM 20050919000682005091900068NM 2005 9 19 DLM88050522 120050908A2916 TRANSMITTER DOUG MD88 MD88 3023688NM RT RESERVOIR LEAKING A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO27911DL 49542 RIGHT HYD QTY GAUGE DROPPED TO ZERO AFTER DEPARTURE FROM ATL. REPLACED HARDWARE ON RT RESERVOIR TRANSMITTER. 2L72 4F RTA6WE 20050919000702005091900070NM 2005 9 19 DL733050524 120050906A5330 SKIN BOEING737 737347 1384647NM FS 727E S-24L CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27308WA 23441 CRACK FOUND IN FUSELAGE SKIN AT CHEM-MIL WHILE ACCOMP OPN 57546. CRACK REPORTED TO BE 1.5 INCH LONG, LOCATED AT FS 727E, S-24L. REPAIRED PER SRM 53-00-01, FIGURE 201. RELATED TO AD 2004-18-06, S/B 737-53A1210, & S/B 737-53-1065. 2L72 4F RTA16WE 20050919000752005091900075NM 2005 9 19 QXEA200501223 120050913A2750 FLAP SYSTEM BOMBDRDHC8 DHC8402 1390042NM TE FLAPS MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM09401QX 4031 SEA FLIGHT 2328: FLAP POWER CAUTION LIGHT. RESET C/B PER CHECKLIST. FLAPS STILL AT 5 DEG AND FLAP POWER CAUTION ILLUMINATED. MAINTENANCE C/W Q400 SL-27-022A FOR FLAP POWER CAUTION LIGHT NUISANCE. SYSTEM RESET. NO FAULT CODES NOTED. PERFORMED OPS CK OF FLAP CONTROL SYSTEM IAW Q400 AMM 27-50-00-710-801. NO PROBLEMS NOTED THROUGH 3 FULL OPS CYCLES. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050919000822005091900082NM 2005 9 19 XN0A1263 120050913A2130 CABIN PRESSURE BOEING727 727227 1384078NM MALFUNCTIONED A XN0AO OTHER O OTHER NRNOT REPORTED 1 GL2376752 21248 AIRCRAFT WOULD NOT PRESSURIZE IN ANY MODE - AUTO, STANDBY OR MANUAL AC OR DC. TRANSFERRED TO MEL 5718 IAW MEL 21-16-2D. PLACARDS INSTALLED CAT-C. 2L73 4F A3WE 20050919000832005091900083NM 2005 9 19 PIDA20050084 120050628A534769403521 SEAT TRACK BOEING737 737228 13844AGNM BS 280 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05237TR 23007 SEAT TRACK AT RBL 42 HAS CORROSION ON O/B FLANGE AT BS 280. REPLACED SECTION OF SEAT TRACK PER SRM 51-10-1. 2L72 4F RTA16WE 20050919000892005091900089EA 2005 9 19 SWIA200515542 120050909A2751601R590141 DETECTOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07912SW 7595 FLAP DEGRADED STATUS MESSAGE WILL NOT CLEAR. REPLACED SKEW DETECTION SYSTEM UNIT IAW MM CHATPER 27-51-15. OPERATIONAL CHECK GOOD. P/N 601R59014-1; S/N OFF A-289. 2L72 4F RTA21EA 20050919000942005091900094NM 2005 9 19 PIDA20050089` 120050623A5320 INTERCOSTAL BOEING737 737228 13844AGNM BS 320 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05237TR 23007 INTERCOSTAL AT BS 320 BETWEEN RBL 11 AND RBL 29 HAS CORROSION AT CLIP NUT HOLES. REPLACED CORRODED INTERCOSTAL SHIM PER SRM 51-10-1. 2L72 4F RTA16WE 20050919000992005091900099NM 2005 9 19 PIDA20050077 120050617A5315 FLOORBEAM BOEING737 737228 13844AGNM BS 328 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05237TR 23007 BS 328 FLOORBEAM HAS CORROSION FROM LBL 15 TO RBL 57 AT FASTENER HOLES. SPLICED IN NEW SECTION OF FLOORBEAM T-CAP FROM LBL 35 TO RIGHT O/B END PER SRM 53-10-9. 2L72 4F RTA16WE 20050919001052005091900105NM 2005 9 19 PIDA20050088 120050623A53206545834256 INTERCOSTAL BOEING737 737228 13844AGNM BS 312-328 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05237TR 23007 INTERCOSTAL AT RBL 11 BETWEEN BS 312 TO BS 328 HAS CORROSION AT NUT PLATE HOLES. REPLACED INTERCOSTAL PER SRM 51-10-1. 2L72 4F RTA16WE 20050919001162005091900116NM 2005 9 19 PIDA20050104 120050622A5315 FLOORBEAM BOEING737 737228 13844AGNM BS 787 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05237TR 23007 FLOORBEAM IN AFT CARGO BIN AT RBL 5 HAS CORROSION AROUND NUT PLATE HOLE AT BS 787. REPAIRED DAMAGED AREA OF UPPER LEG PER SRM 51-40-3. 2L72 4F RTA16WE 20050919001182005091900118NM 2005 9 19 PIDA20050100 120050628A5320 INTERCOSTAL BOEING737 737228 13844AGNM BS 500A-500B CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05237TR 23007 INTERCOSTAL FROM BS 500A TO BS 500B AT STR 26 RT IS CRACKED. REPLACED INTERCOSTAL PER DWG 69-41757 AND SRM 51-10-1. 2L72 4F RTA16WE 20050919001282005091900128NM 2005 9 19 05FDEA02857 120050913A5530 WEB BOEING727 727200 138407ENM VERTICAL STAB CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 VERTICAL STABILIZER MAIN BOX WEB IS CRACKED AT FIN STA 133 JUST BELOW ACCESS CUTOUT. *S/D* INSTALLED DOUBLER AT FIN STA 133 PER EA 7-5530-91356. 2L73 4F RTA3WE 20050919001292005091900129NM 2005 9 19 05FDEA02858 120050913A5322 SHEAR TIE BOEING727 727200 138407ENM BS 720 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25268FE 21674 CORROSION FWD CARGO FLOOR SHEAR TIE STA 720 BL 0 WL 148. *S/D* REPAIRED PER SRM 53-10-4, AND 53-10-1 MAJOR REPAIR. 2L73 4F RTA3WE 20050919001312005091900131NM 2005 9 19 05FDEA02855 120050913A5322 SHEAR TIE BOEING727 727200 138407ENM BS 720 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION, FORWARD CARGO BAY ON SHEAR TIE BETWEEN STRINGER 28 RT AND STRINGER 28 LT BS 720 (FWD SIDE OF FRAME). FOUND TO BE OUT OF LIMITS IAW 51-10-1. REMOVED & REPLACED IAW 53-40-4 & 51-20-2. 2L73 4F RTA3WE 20050919001322005091900132EA 2005 9 19 QXEA200501230 120050914A2720 CONTROL SYSTEM CNDAIRCL600 CL6002C10 1390015EA RUDDER LIMITER MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM09610QX 10033 BOI - ON FLIGHT 4276, RECEIVED SPOILER/STAB AND RUDDER LIMIT FAULT MESSAGES. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE C/W CRJ700/900 SL-27-028A TEMP REV 34-0088. COMPLIED WITH TASK CARD R341101. FAULTS CLEARED. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2L72 4F RTA21EA 20050919001332005091900133WP 2005 9 19 05FDEA02865 120050914A5330 SKIN DOUG MD10 MD1010F 3022112WP BS 1953 DENTED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25571FE 47830 DURING AIRPLANE'S CONVERSION FROM P TO F FOUND: DENT ON SKIN LT SIDE STA 1953 LONG 29: 1 INCH LONG * 0.04 DEPTH. LONG 31: 2" LONG * 0.08 DEPTH. REWORK DENT AREA IAW SRM 53-20-00 FIG 13. DYE PENETRANT INSPECT FOR CRACK. INSTALLED REPAIR FINGER DOUBLER IAW SRM 53-20-00 FIG 13. 2L73 4F RTA22WE 20050919001352005091900135WP 2005 9 19 05FDEA02867 120050914A5311 FRAME DOUG MD10 MD1010F 3022112WP BS 469 NICKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25571FE 47830 DURING AIRPLANE' S CONVERSION FROM P TO F FOUND: AVIONIC COMPARTMENT AT STA 469 X= 33 WITH 2EA NICKS ON THE FRAME. BLEND OUT NICK AREA IAW SRM 53-00-01 FIG 1B, AND INSTALL FRAME REPAIR IAW SRM 53-30-00 FIG 4A. 2L73 4F RTA22WE 20050919001412005091900141NM 2005 9 19 PIDA20050072 120050708A5313 STRINGER BOEING737 737228 13844AGNM BS 360 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05237TR 23007 CORROSION ON STRINGER 27 LT AT THE AFT END AT BS 360. REPAIRED PER SRM 53-10-3. 2L72 4F RTA16WE 20050919001422005091900142NM 2005 9 19 PIDA20050073 120050623A5340 STRINGER CLIP BOEING737 737228 13844AGNM BS 540 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05237TR 23007 CORROSION ON STRINGER 27 LT ATTACH CLIP AT BS 540 FRAME. REPAIRED PER DRAWING 65-49564 AND SRM 51-10-1. 2L72 4F RTA16WE 20050919001432005091900143NM 2005 9 19 PIDA20050074 120050708A5313655162829 STRINGER BOEING737 737228 13844AGNM BS 967 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05237TR 23007 CORROSION ON STRINGER 27 LT JUST AFT OF BS 967 FRAME. SPLICED IN NEW SECTION OF STRINGER P/N 65-51628-29 FROM BS 917 TO BS 1016 PER SRM 53-10-3. 2L72 4F RTA16WE 20050919001482005091900148NM 2005 9 19 PIDA20050083 120050628A534769403521 SEAT TRACK BOEING737 737228 13844AGNM BS 269-294 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05237TR 23007 SEAT TRACK AT RBL 15 HAS CORROSION ON FLANGES FROM BS 269 TO BS 294. REPLACED SECTION OF SEAT TRACK PER SRM 51-10-1. 2L72 4F RTA16WE 20050919001492005091900149NE 2005 9 19 ASMF200509006 220050913A7320 EEC BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE RT SIDE FAILED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23806AM30371 26273 726731 CAPTAIN REPORTED RT ENGINE EGT INDICATION WITH OSCILLATIONS OF 100 GRADES IN EICAS. THE RT EEC EBG AND THERMOCOUPLE HARNESS JUNCTION BOX WERE REPLACED IAW MM 73-21-04 AND 77-51-12, RT ENGINE WAS TESTED IAW MM 71-00-01, ALL CORRECT. 2L72 4F4 FRTA2NM E17NE 20050919001502005091900150 2005 9 19 WRLA2005141 420050911A3451 INTERROGATOR DOUG MD11 MD11F 3023600NM PWA 4060 PW4060 52119NE DME INOPERATIVE A WRLAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11381 48523 TPE/ANC AT FIVE HOURS EN ROUTE A SMELL AND VISUAL OBSERVATION OF LITE SMOKE IN COCKPIT. AT SAME TIME DME 2 C/B POPPED, SMOKE AND SMELL DISSIPATED AFTER 20 MIN. INSPECTED NR 2 DME INTERROGATOR AND FOUND UNIT TO BE AT FAULT, NO EVIDENCE OF ANY ELECTRICAL WIRING DAMAGE OR ADJACENT COMPONENTS DAMAGE. TRANSFERRED NR 2 DME TO DMI M34SE1105-84 IAW MEL 34-52-1 CAT D. C/B WAS PULLED AND COLLARED. 2L73 4F4 FRTA22WE E24NE 20050919001512005091900151NM 2005 9 19 SWAA052785 120050914A335020131 BATTERY PACK BOEING737 7373H4 1384600NM EMERGENCY LIGHT FAULTY A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED RON CHECK, RT AFT CABIN EMERGENCY LIGHTS BATTERY PACK WILL NOT HOLD CHARGE. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050919001532005091900153NM 2005 9 19 SWAA052787 120050914A2560P4010021 BATTERY BOEING737 7373H4 1384600NM FLASHLIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29638SW 27711 AFT OUTBOARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2L72 4F RTA16WE 20050919001552005091900155NM 2005 9 19 SWAA052789 120050914A5240MS21042L3 NUT PLATE BOEING737 7373L9 1384470NM R2 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED 1/2D CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE UPPER AFT ANCHOR NUT PLATE CRACKED. REMOVED AND REPLACED NUT PLATE PER MM. 2L72 4F RTA16WE 20050919001602005091900160EU 2005 9 19 05FDEA02900 120050914A5347 SEAT TRACK AIRBUS310 A310 EU FR 61-62 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25425FE 264 MCD SEAT TRACK BET FR 61 AND FR 62 BL 0 HAS CRACK. REPAIRED SEAT TRACK IAW SRM 53-10-16. 2L72 4F RTA35EU 20050919001612005091900161EU 2005 9 19 05FDEA02901 120050914A5511 SPAR AIRBUS310 A310 EU HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25425FE 264 LT HORIZ STAB UPPER REAR SPAR T-CAP LOWER SIDE CORRODED AT NUTPLATES 51 TO 57 IN FROM FUSELAGE. REMOVED NUTPLATES, REMOVED CORROSION, MODIFIED RIB SUPPORT FABED REPAIRS, AND INSTALLED REPAIRS IAW SRM 51-40-21, 55-11-21, AND 51-74-10. 2L72 4F RTA35EU 20050919001632005091900163EU 2005 9 19 05FDEA02903 120050914A5347 SEAT TRACK AIRBUS310 A310 EU FR 79 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25425FE 264 MDCC - SEAT TRACK FR 79 LBL 56 CORRODED. REMOVED CORROSION, REMOVED SEAT TRACK, DRILLED NEW TRACK, INSTALLED TRACK IAW SRM 53-10-16, 51-40-21, 51-40-44, AND 51-40-21. 2L72 4F RTA35EU 20050919001652005091900165NM 2005 9 19 SWAA052804 120050914A53306545776 SKIN BOEING737 7375H4 138449DNM BS 900 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 900, BETWEEN STR 24R TO STR 25R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050919001672005091900167WP 2005 9 19 ABXA050219 120050901A531199196182 FRAME DOUG DC9 DC932 3022066WP BS 718 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23900AX 47380 RIGHT MAIN FRAME STA 718 HAD CRACK IN S/B SECTION. CRACK HAD GROWN INTO ATTACHMENT HOLES FOR REPAIR. FRAME REQUIRED REPLACEMENT PER S/B 53-100. FRAME WAS REMOVED AND REPLACED ON EA 53400324-0021-2. 2L72 4F A6WE 20050919001722005091900172WP 2005 9 19 UPS05845427 120050903A5712 RIB DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE: C3, LT WING L/E UPPER RIB IS CRACKED AT XFS 297.500. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 57-02-00 FIG 2 AND 51-01-20D. 2L74 4F RT4A25 20050919001742005091900174WP 2005 9 19 UPS05845443 120050903A5712 RIB DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE:C3 LEFT WING L/E UPPER RIB IS CRACKED AT XFS 835.000. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-2-0, 51-1-21 AND 51-1-20D. 2L74 4F RT4A25 20050919001762005091900176WP 2005 9 19 UPS05845445 120050903A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE:C3 RIGHT OUTER WING OUTBOURD EXTENDED LEADING EDGE UPPER RIB CRACKED AT XFS 722. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-2-0 FIG 2, 51-1-21 AND 51-1-20D. 2L74 4F RT4A25 20050919001772005091900177WP 2005 9 19 UPS05845446 120050903A5712 RIB DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE:C3 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 772.500. FABRICATED AND INSTALLED DOUBLER IAW SRM 57-2-0, 51-1-20D AND 51-1-21. 2L74 4F RT4A25 20050919001802005091900180WP 2005 9 19 UPS05845449 120050903A5730 DOUBLER DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE:C3 LEFT WING L/E LOWER INTERNAL DOUBLER IS CRACKED AT DRAIN HOLE AT XFS 335.250. REMOVED INTERNAL DOUBLER. FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-3-0, 51-1-20D AND 51-1-21. 2L74 4F RT4A25 20050919001822005091900182NM 2005 9 19 05FDEA02925 120050915A5313 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 CENTER CARGO, LONGERON SPLICE AT BILGE AREA ADJACENT TO STATION 5-113 TO STATION 1541 LONGERON-49 RIGHT BRIM AREA FOUND CRACK. LONGERON SPLICE REMOVED AT BILGE AREA ADJACENT TO STATION 5-113 TO STATION 1541 LONGERON-49 RT AS PER SRM 51-33-01 VOLUME II. NEW LONGERON SPLICE MACHINED AS PER DWG A5A7114. NEW LONGERON SPLICE INSTALLED AS PER SRM 51-33-01 VOLUME II. THIS REPAIR CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050919001832005091900183EU 2005 9 19 F3LA200500040 120050907A5743 FITTING AIRBUSA319 A319112 3930323EU LT WING MLG CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03903FR 2143 1560 INSPECTION REPORTED CORROSION ON FWD FACE, FWD LUG, LT WING RIB 5, LANDING GEAR FITTING. MACHINED CORROSION ON LUG FACE PER SRM 57-26-13. 2L72 4F RTA28NM 20050919001852005091900185EA 2005 9 19 REXA200500123 120050916A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A REXAO OTHER J WARNING INDICATION APAPPROACH 1 SO25827AY 8027 EMERGENCY DELCARED WHEN FLAPS FAILED AT 20 DEGREES ON APPROACH. LANDING UNEVENTFUL. 2L72 4F RTA21EA 20050919001862005091900186EU 2005 9 19 F3LA200500041 120050907A5743 FITTING AIRBUSA319 A319112 3930323EU LT WING MLG CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03903FR 2143 1560 INSPECTION REPORTED CORROSION IN FWD BORE FROM 4 O'CLOCK TO 7 O'CLOCK LT WING, RIB 5, LANDING FITTING. BORED OUT CORROSION PER SRM 57-26-13. 2L72 4F RTA28NM 20050919001872005091900187NM 2005 9 19 05FDEA02884 120050914A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 HORIZ STAB LT NR 36 BARREL NUT BORE AREAS CORRODED. REWORK/REPAIR AD 2003-22-08- EA 1-5510-87628 ATTACHMENT 12. CLASSIFIED AS MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20050919001882005091900188NM 2005 9 19 05FDEA02926 120050915A5313 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 CENTER CARGO, LONGERON SPLICE AT BILGE AREA ADJACENT TO STATION 5-113 TO STATION 1541 LONGERON-52 LEFT BRIM AREA FOUND CRACK. CRACK LONGERON SPLICE AT CENTER CARGO - LONGERON STATION 5-113 TO STATION 1541 LONGERON 52 REMOVED AND REPLACED WITH NEW LONGERON AS PER SRM 51-33-01 VOL II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2L73 4F RTA22WE 20050919001942005091900194EA 2005 9 19 REXA300500117 120050911A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A REXAO OTHER J WARNING INDICATION APAPPROACH 1 SO25827AY 8027 FLAPS FAILED AT 20 DEGEES ON APPROACH. COMPLIED WITH AD98-20-01. NO DISCREPANCIES NOTED. UNDER 72 HOURS FLAP WATCH. 2L72 4F RTA21EA 20050919001952005091900195WP 2005 9 19 05FDEA02860 120050914A5711 SPAR DOUG MD10 MD1010F 3022112WP RT WING DAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25571FE 47830 DURING AIRPLANE'S CONVERSION FROM P TO F FOUND DOUBLE HOLE 0.187* 0.291 ON TE. RT WING LOWER CAP AT STA XORS 728 AND HOLE OVALIZED IN FRG PANEL. NORMALIZED HOLE AND INSTALLED REPAIR BUSHING PER SRM 51-31-01 VOL II, REPAIRED PANEL PER SRM 57-00-01 FIG 4 SH 2. 2L73 4F RTA22WE 20050919001992005091900199CE 2005 9 19 DXTA200500968 120050914A2730 ELEVATOR CESSNA560 560XL 2076702CE MALFUNCTIONED E DXTAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 GL07679QS 5605279 THROUGH 110 KTS ON TAKEOFF ROLL FULL AFT ELEVATOR DID NOT INITIATE ROTATION TAKEOFF ABORTED. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20050919002012005091900201NM 2005 9 19 DXTA200500966 120050914A29107G979 PRESSURE SWITCH AMD FALC50FALCON2000 2730170NM NR 1 HYD SYSTEM LEAKING E DXTAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL07277QS625 177 TOTAL LOSS OF HYDRAULIC FLUID ON THE NR 1 HYD SYSTEM IN FLIGHT. REMOVED NR 1 HYDRAULIC SYSTEM PRESSURE SWITCH CODE (L30GI) P/N 7G979, S/N 1722 AND REPLACED WITH NEW SWITCH P/N 7G979 , S/N 2784. REMOVED NR 1 & NR 2 ENGINE HYDRAULIC PUMPS AND INSPECTED FLUID AND PUMP CONDITION. NO DEFECTS NOTED. RE-INSTALLED NR 1 & NR 2 ENGINE HYDRAULIC PUMPS. PERFORM OPERATIONAL CHECKS AND LEAK CHECKS ON NR 1 & NR 2 ENGINE HYDRAULIC SYSTEM IAW 29-104 & 29-100, NO DEFECTS NOTED. SERVICED HYDRAULIC SYSTEMS 1 & 2 TO CORRECT LEVELS WITH 5606 FLUID IAW 29-112. 2K73 4F RTA50NM 20050919002032005091900203CE 2005 9 19 DXTA200500971 120050916A2150 ACM CESSNA750 750 2076810CE FAILED E DXTAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 GL07982QS 7500182 WHILE DESCENDING OUT OF 410, HEARD A LOUD BANG AND SMELLED SMOKE. THE SMOKE CLEARED, UNABLE TO CONTROL COCKPIT TEMP. SUSPECT COCKPIT ACM BROKEN. ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20050919002052005091900205EA 2005 9 19 REXA200500121 120050915A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A REXAO OTHER J WARNING INDICATION APAPPROACH 1 SO258721B 7721 EMERGENCY LANDING FOR FLAPS FAIL AT 0 DEGREES ON APPROACH. LANDING UNEVENTFUL. COMPLIED WITH AD 98-20-01. RESET PER FAULT ISOLATION MANUAL, OPERATIONALLY CHECKS GOOD. 2L72 4F RTA21EA 20050919002062005091900206SO 2005 9 19 SWIA200515547 120050904A3350 SOCKET EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07233SW 120307 ONE RED LIGHT INOP IN FLOOR LEVEL LIGHTING OVER ROW 6. REPLACED LIGHT SOCKET ON FLOOR LIGHTING AT ROW 6. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050919002082005091900208EA 2005 9 19 SWIA200515549 120050825A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA BS 605 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07413SW 7102 FRAME FLANGE CRACKED AT FS 605 STR 9L ABOVE STRINGER FROM LOWER FASTENER HOLE TO EDGE OF FLANGE. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FLANGE IAW CRJ REO 601R-53-61-1507. 2L72 4F RTA21EA 20050919002102005091900210SO 2005 9 19 SWIA200515551 120050603A5713 STRINGER EMB 120 EMB120 3260201SO RT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07188SW 120039 LOWER STRINGER NR 8 CRACKED AT NR 3 FUEL BAY ACCESS AREA OUTBOARD OF NACELLE, RIGHT WING. ITEM FOUND AT C-CHECK INSPECTION. REPLACED CRACKED STRINGER NR 8 AT NR 3 FUEL BAY ACCESS RIGHT WING AS PER EMB120 SRM 57-20-03 FIG 202 PG 211. 2L72 4T RTA31SO 20050919002112005091900211EA 2005 9 19 REXA200500120 120050914A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A REXAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO258696C 7696 FLAPS FAIL MESSAGE DURING TAXI. SYSTEM RESET AND PLACED ON 72 HRS WATCH PER AD 98-20-01. 2L72 4F RTA21EA 20050919002122005091900212WP 2005 9 19 05FDEA02931 120050915A3411 PITOT TUBE DOUG DC10 DC1010 3022110WP FIRST OFFICERS OBSTRUCTED A FDEAC ABORTED TAKEOFF C F.O.D. TOTAKEOFF 1 SO2568051 47805 REJECTED T/O 5L IND DUE TO ZERO AIRSPEED INDICATION IN F/O INDICATOR TEMP 24 DEG, WT=420,000, AIRSPEED AT REJECT=100KTS, RNWY 57 (FULL LENGHT), BRAKE COOLING TIME=64 MINS, TIME OF REJECT=21:59Z. FOUND F/O'S PITOT TUBE OBSTRUCTED. CLEARED OBSTRUCTION AND PURGED F/O'S PITOT SYSTEM AND PERFORMED LOW LEVEL PITOT STATIC SYSTEM CHECK F/O'S AIRSPEED INDICATOR, OPS CHECKS NORMAL. 2L73 4F A22WE 20050919002132005091900213EU 2005 9 19 05FDEA02908 120050914A5321242UJ FLOOR PANEL AIRBUS310 A310 EU CARGO DECK DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25425FE 264 MDCC FLOOR PANEL 242UJ DELAMINATED. FABED NEW PANEL. 2L72 4F RTA35EU 20050919002142005091900214EA 2005 9 19 VTZA200500188 120050915A5320601R3117117 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA BS 484 CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27653BR 7438 LEFT INTERCOSTAL FLOOR SUPPORT CRACKED .25 INCH AT FS 484. 2L72 4F RTA21EA 20050919002152005091900215EA 2005 9 19 VTZA200500189 120050915A5320301R3117117 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA BS 484 CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27653BR 7438 RIGHT INTERCOSTAL FLOOR SUPPORT CRACKED .25 INCH AT FS 484. 2L72 4F RTA21EA 20050919002202005091900220SO 2005 9 19 RAIA00509017 120050912A3350 FUSE EMB 145 EMB145LR 3260212SO BATTERY PACK FAILED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03839HK 14500829 FLT 7987-SYR- EMERGENCY LIGHTS OUT AT ROW 12. MAINTENANCE REPLACED A FUSE ON BATTERY PACK NR 3. 2L72 4T RTT00011AT 20050919002222005091900222SO 2005 9 19 RAIA0050919 120050912A276014533022405 CONTROL UNIT EMB 145 EMB145 3260210SO SPOILERS FAILED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03802HK3665 3665 145066 FLT 3537-PIT- SPOILER FAIL IN FLIGHT. MAINTENANCE REMOVED AND REPLACED THE SPOILER CONTROL UNIT. 2L72 4F RTT00011AT 20050919002232005091900223EU 2005 9 19 RAIA00509021 120050913A33506134051 POWER SUPPLY JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT INOPERATIVE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03574HK 41093 FLT 5537-STL- FORWARD EMERGENCY LIGHTS IN FLOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT POWER SUPPLY. 2L72 4T RTA41NM 20050919002252005091900225NM 2005 9 19 UPS05245431 120050822A5520 CHANNEL BOEING727 72731C 1384011NM RT ELEVATOR. CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01922UP 19231 INSPECTION TYPE:C SUPPORT CHANNEL CRACKED AT TOP END, JUST I/B OF RT ELEVATOR NR 1 HINGE BEAM, AFT OF ELEVATOR I/B INPUT ROD. CHANNEL FABRICATED IAW SRM 51-20-1 FIG 7. CHANNEL REPLACED IAW SRM 51-30-02. 2L73 4F A3WE 20050919002282005091900228NM 2005 9 19 UPS05245435 120050828A5312 BULKHEAD BOEING727 72731C 1384011NM BS 870 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01922UP 19231 INSPECTION TYPE: C, CORROSION ON LT WHEEL WELL BULKHEAD AT BS 870 - FWD FACE 25 INCH FROM O/B EDGE AND 20 INCH FROM BOTTOM EDGE. REPAIR CARRIED OUT IAW AAAE RO 2005-081-2 -UPS ENG FILE NUMBER 727-53 -20190. 2L73 4F A3WE 20050920000012005092000001NM 2005 9 20 PCSA09170501 120050917A2131 CONTROLLER BOEING727 7272F9 138407DNM CABIN PRESSURE MALFUNCTIONED A PCSAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO29199AJ 21426 FLIGHT 857 DURING CLIMBOUT FROM MIA FLIGHT CREW REPORTED AIRCRAFT WOULD NOT PRESSURIZE & IT SEEMED BOTH PACKS WERE NOT WORKING AT ALL. AIRCRAFT RETURNED TO MIA & LANDED WITHOUT ANY FURTHER INCIDENT. MAINTENANCE CHECKED BOTH LEFT & RIGHT PACKS IAW B-727 MM CH 21-55-0 OPERATION CHECK WAS NORMAL. MAINTENANCE RERACKED THE PRESSURE CONTROLLER & CLEANED PACK VALVES & CLEANED THE CANNON PLUGS & RESECURED, A FULL PRESSURIZATION CHECK OUT WAS ACCOMPLISHED IAW AMERIJET WORK CARD 847 OPERATIONAL CHECK WAS NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. 2L73 4F RTA3WE 20050920000022005092000002NM 2005 9 20 05FDEA02921 120050915A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 CRACK INDICATION AT END OF STRINGER-43 WAS FOUND DURING HFEC INSPECTION AT LEFT SIDE WING TANK. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050920000042005092000004NM 2005 9 20 05FDEA02923 120050915A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 CRACK INDICATION AT END OF STRINGER 10 WAS FOUND DURING HFEC INSPECTION AT LEFT SIDE WING TANK. CRACKED AREA REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050920000062005092000006NM 2005 9 20 05FDEA02896 120050914A5313 STRINGER BOEING727 727225 1384077NM ZONE 100 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 FABRICATE AND INSTALL STRINGER REPAIR AT BODY STATION 500 AND S21R. REMOVED, FABRICATED AND INSTALLED STRINGER CHANNEL IAW FX B727-200 SRM 53-10-3. ALODINED AND PRIMED IAW FX B727-200 SRM 51-10-2. 2L73 4F A3WE 20050920000102005092000010NM 2005 9 20 05FDEA02935 120050915A5713 STRINGER DOUG MD11 MD11F 3023600NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 CRACK INDICATION AT END OF STRINGER-13 WAS FOUND DURING HFEC INSPECTION AT RIGHT SIDE WING TANK. SLOTTED OUT AND REPAIR CARRIED OUT AS PER SRM 57-20-00, FIG 10, VOL I. NEW STRINGER CLIP FABRICATED AS PER FEDEX EA 1-5720-90027, THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050920000112005092000011NM 2005 9 20 05FDEA02936 120050915A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 CRACK INDICATION AT END OF STRINGER-12 WAS FOUND DURING HFEC INSPECTION AT RIGHT SIDE WING TANK. SLOTTED OUT AND REPAIR CARRIED OUT AS PER SRM 57-20-00, FIG 10, VOL I. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050920000142005092000014NM 2005 9 20 05FDEA02939 120050916A5713 STRINGER DOUG MD11 MD11 3023602NM RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 CRACK FOUND ON RT WING UPPER STRINGER ENDS S-11 APPROX 7.5 INCHES (ACCESS FROM LOWER WING FUEL TANK PANEL NR 636AB). SNRM N0949: RH WING STRINGER END S-11 APPROX. 7.5 INCHES CRACK, ACCESS FROM LOWER WING FUEL TANK PANEL NO. 636AB CARRIED OUT REPAIRED AS PER SRM 57-20-00 FIG. 10 VOL.I. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050920000152005092000015NM 2005 9 20 05FDEA02940 120050916A5713 STRINGER DOUG MD11 MD11 3023602NM RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 CRACK FOUND ON RT WING UPPER STRINGER ENDS S-10 APPROX 12 INCHES (ACCESS FROM LOWER WING FUEL TANK PANEL NR 636CB). SNRM N0950: RH WING UPPER STRINGER END S-10 APPROX. 12 INCHES CRACK, ACCESS FROM LOWER WING FUEL TANK PANEL NO. 636CB, CARRIED OUT REPAIRED AS PER SRM 57-20-00 FIG. 10 VOL.I. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050920000162005092000016NM 2005 9 20 05FDEA02941 120050916A5313 LONGERON DOUG MD11 MD11 3023602NM BS 6-90 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 CAC COMPT BETWEEN STA 6-90 AND STA 1139, NR L-44L LONGERON CORRODED. SNRM N1168: CAC COMPT BETWEEN STA 6-90 AND STA 1139 L-44L LONGERON CORROSION REMOVED AND REPROTECTED AS PER SRM 51-21-01 VOL.II. MATERIAL ORIGINAL THK 0.071" REMOVED 0.006" X L=3" REMAIN 0.065 FOUND WITHIN LIMIT AS PER SRM 53-00-01 FIG.1A VOL.I. MINOR REPAIR PER GMM 6-2-100. 2L73 4F RTA22WE 20050920000172005092000017WP 2005 9 20 05FDEA02942 120050916A7160 NOSE COWL DOUG MD10 MD1010F 3022112WP LEFT BIRD STRIKE A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25398FE 46634 AT ROTATION NOTICED BIRD FLOCK LEFT OF NOSE LEVEL AT 2000 FT NOTICED VIBRATION, CONTINUED TO CLIMB VIBRATION WAS NOTICED IN NR 1 START LEVER AND THROTTLE. AT 17000 NR 1 RED REV U/L APPEARS. RAN RED TABS, SHUT DOWN NR 1 ENGINE, RETURNED TO AFW. INSPECTED NR 1 ENGINE AND FOUND SEVERAL CUTS AND GOUGES BETWEEN 1/4" TO 3.5" LONG. NOSE COWL ON ORDER. 2L73 4F RTA22WE 20050915000252005091500025NM 2005 9 15 05FDEA02849 120050913A5320 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 CENTER CARGO - LONGERON SPLICE ADJACENT TO STA 1541 L-40 LEFT HAND BRIM AREA FOUND CRACK. LONGERON SPLICE ADJACENT TO STA 1541 LLONGERON 40 LEFT HAND BRIM AREA REMOVED AS PER SRM 51-33-01 VOL II. NEW LONGERON SPLICE FABRICATED AS PER DRAWING A5A7114 AND INSTALLED AS PER SRM 51-33-01 VOL II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050915000262005091500026NM 2005 9 15 SWAA052772 120050912A335020131 BATTERY PACK BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED RON CHECK, FOUND RT AFT CABIN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050915000472005091500047NM 2005 9 15 P5CA0501399 120050909A2612285100028136 CIRCUIT CARD BOEING747 74746NF 13848BTNM FIRE WARNING SYSFAILED A P5CAF ACTIVATE FIRE EXT. N FALSE WARNING NRNOT REPORTED 1 EA15452PA 30810 FWD CARGO MASTER FIRE WARNING ON GROUND IN MIA. CHECKLIST COMPLETED. FIRE BOTTLES DISCHARGED. FOUND FIRE WARNING CARD A31 AT FAULT. REMOVED A31 CARD PER MM 26-23-00, OPS NORMAL. 2L74 4F RTA20WE 20050915000482005091500048EU 2005 9 15 SF20050913 120050913A7931 WARNING LIGHT SAAB SF340 SF340A 7850100EU ENGINE OIL PRESSFALSE ACTIVATIONA UHLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL1719XS 340A019 FLIGHT 7578 ABE-IAD, RT ENGINE OIL PRESSURE MASTER WARNING CAME ON AFTER 2 SEC. AFTER CTOT ENGAGEMENT, LESS THAN 60 KNOTS INDICATED. LIGHT WENT OUT RIGHT AFTER POWER REDUCTION. ABORTED TAKEOFF. 2L72 4T RTA52EU 20050915000522005091500052NM 2005 9 15 AALA20050589 120050913A3350 MODULE BOEING767 767323 1385205NM EMERGENCY SIGN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21361AA 24042 LAX EMERGENCY LIGHT AT RIGHT ONE EXIT IDENTIFIER SIGN INOPERATIVE. REPLACED MODULE IN EMERGENCY LIGHT EXIT IDENTIFIER SIGN AT RIGHT ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050915000582005091500058EA 2005 9 15 VNAA0508031 120050829A2750 FCU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A VNAAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL05244PS 7912 DURING APPROACH WITH FLAPS 30 DEGREES THE FLAPS HALFSPEED STATUS MESSAGE ILLUMINATED. AT FLAPS 45DEGREES THE FLAPS FAIL MESSAGE ILLUMINATED. THE CREW FOLLOWED THE QRH AND LANDED SAFELY. MAINTENANCE RESET THE FECU IAW CRJ200 SL-00-001. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050915000602005091500060EA 2005 9 15 VNAA0508029 120050829A2751855D10011 BPSU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT TE FLAPS FAILED A VNAAO OTHER J WARNING INDICATION APAPPROACH 1 GL05218PS3531 7885 DURING FINAL APPROACH THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED. THE CREW FOLLOWED THE QRH AND LANDED SAFELY. MAINTENANCE REMOVED & REPLACED THE RT FLAP BRAKE AND POSITION SENSOR UNIT IAW CRJ200 AMM 27-51-10-400-801. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050915000782005091500078EU 2005 9 15 09082005G 120050906A7797 CONNECTOR SAAB SF340 340B 7860101EU INDICATOR DIRTY A NSVAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 EA27301CE 191 DURING START NR 2 ENGINE NG READINGS WERE ERRATIC. DURING SECOND ATTEMPT THE START WAS NORMAL UNTIL 55 PERCENT, THEN NG DROPPED TO 0%. CLEANED AND INSPECTED CONNECTOR ON BACK OF INDICATOR AND ALTERNATOR. OPS CHECK GOOD. 2L72 4T RTA52EU 20050915000882005091500088EU 2005 9 15 09092005E 120050908A3260 CONTROL PANEL SAAB SF340 340B 7860101EU MLG BURNED A NSVAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 EA27339CJ 339 UPON EXTENSION OF LANDING GEAR, IMMEDIATELY GOT 3 GREEN INDICATORS, THEN THE LIGHTS WENT OUT. FOUND M-5 C/B TRIPPED. OBSERVED SMOKE RISING FROM BEHIND LANDING GEAR PANEL, AND SMELLED BURNT INSULATION. REMOVED AND REPLACED LANDING GEAR PANEL, OPS CHECK GOOD. 2L72 4T RTA52EU 20050915000952005091500095SO 2005 9 15 C2XA05IA103 120050902A3350276005 FUSE EMB 145 EMB145LR 3260212SO BATTERY CHARGER BLOWN A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714558 145598 MCI - DURING MAINTENANCE INSPECTION, THE LEFT AND RIGHT EXTERIOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FUSE FOR THE AFFECTED EMERGENCY LIGHTS, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050915001002005091500100SO 2005 9 15 C2XA05CL079 120050910A28232810051102 VALVE EMB 145 EMB145LR 3260212SO RT WING VENT LEAKING A C2XAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW2714977 145175 CLE FLIGHT NR 2293, THE CREW REPORTED A RIGHT WING FUEL LEAK IN FLIGHT. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT WING FUEL VENT VALVE. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20050915001072005091500107NM 2005 9 15 CALA0500297 120050903A5320147A56601 INTERCOSTAL BOEING737 737824 13844BZNM BS 947.5-967 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712218 28778 INSPECTION FOUND INTERCOSTAL BETWEEN STA 947.5 AND 967, LBL 51 AT L-2 DOOR CORRODED AROUND FLOOR PANEL MOUNT HOLES. REPAIRED INTERCOSTAL IAW ECRA 5321-01286. 2L72 4F RTA16WE 20050915001152005091500115NM 2005 9 15 CALA0500302 120050905A3350 CHARGER BOEING737 7373T0 1384582NM SEAT 21 ABC INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2717356 23942 INSPECTION FOUND SEAT 21 ABC EMERGENCY LIGHT INOPERATIVE. THE BATTERY CHARGER ASSEMBLY WAS REMOVED AND REPLACED IAW MM 33-51-81. 2L72 4F RTA16WE 20050915001402005091500140NM 2005 9 15 05FDEA02835 120050912A5753 ATTACH FITTING DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 RT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87634. 2L73 4F RTA22WE 20050915001592005091500159NM 2005 9 15 QXEA200501224 120050910A2730 WARNING LIGHT BOMBDRDHC8 DHC8402 1390042NM ELEVATORS ILLUMINATED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09400QX 4030 BOI FLIGHT 2400: ELEVATOR ASYMMETRY CAUTION LIGHT DURING CRUISE. NO OTHER ABNORMAL INDICATIONS. LIGHT EXTINGUISHED DURING TAXI. MAINTENANCE INTEROGATED CDS SYSTEM. FOUND FAULTS L E2 AND 63 RIGHT E2. COMPLIED WITH Q400 FIM 27-30-00. GROUND RAN AFT AND PERFORMED ELEVATOR CONTROL SYSTEM ADJUSTMENT AND TEST REF Q400 AMM 27-30-00. GROUND OPS CHECK NORMAL. INTEROGATED CDS. NO PRESENT FAULTS. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050915001742005091500174NM 2005 9 15 DLM88050486 120050824A3260833605 PSEU DOUG MD88 MD88 3023688NM MLG MALFUNCTIONED A DALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27911DL 789 49542 AIR TURNBACK DUE TO LEFT GEAR UNSAFE LIGHT WHEN HANDLE RAISED. CYCLED GEAR WITH NO HELP. NO FAULTS FOUND ON PSEU. CYCLED GEAR SEVERAL TIMES, ALL IND CHECKS GOOD. REPLACED PSEU AND D1-26 UPLOCK PROX SENSOR LEFT GEAR, ALL CHECKS GOOD. 2L72 4F RTA6WE 20050915001802005091500180NM 2005 9 15 DL73S050527 120050908A5330 SKIN BOEING737 737232 1384475NM FS 525 S-16R CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27314DA 23086 THE FUSELAGE SKIN WAS FOUND WITH A CRACK JUST ABOVE THE BONDED DOUBLER MILL LINE OF STRINGER 16R AT FS 525. THE CRACK WAS 1 INCH LONG AND TYPICAL OF THOSE DOCUMENTED IN AD 2004-18-06 AND BAC S/B 737-53A1210. THE CRACK WAS REMOVED WITH A CUT OUT AND REPAIRED WITH AN EXTERNAL DOUBLER PER B737 SRM AND ER/A 450574-14AD. 2L72 4F RTA16WE 20050915001852005091500185NM 2005 9 15 DL76G050537 120050910A2530828450407 OVEN BOEING767 767332 1382001NM AFT GALLEY NB7 ARCED A DALAK NONE O OTHER ININSP/MAINT 1 SO271603 29695 OVEN NR 7 AFT GALLEY SPARKED WHEN TURNED ON AND POPPED C/B. REPLACED SAME. 2L72 4F RTA1NM 20050915001882005091500188NE 2005 9 15 DL76L050540 220050912A7200PW40603 ENGINE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 1 MALFUNCTIONED A DALAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO27197DN29672 28454 727775 AT T/O CREW REPORTED LEFT DUCT PSI FLUX ALONG WITH L-2 DOOR AREA HAVING VIBRATION AND VIBRATION WAS FELT IN CONTROL COLUMN ROLL MODE. RETURNED TO JFK FOR REPAIRS. INSPECTED LEFT ENGINE FOR BIRD STRIKE. BOROSCOPED AND VIBE SURVEYED. REPLACED PRSOV FOR HISTORY OF BLEED FLUX. 2L72 4F4 FRTA1NM E24NE 20050915001892005091500189EA 2005 9 15 QXEA200501228 120050913A4920 APU CNDAIRCL600 CL6002C10 1390015EA AFT ODOR A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM09600QX 10005 GEG - ON FLIGHT 2351 NOTICED FUEL SMELL IN CABIN. MAINTENANCE PLACED THE APU ON MEL 49-10-1B, RSI 351878. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20050919000062005091900006EU 2005 9 19 05FDEA02909 120050914A5321231VG FLOOR PANEL AIRBUS310 A310 EU GE CF6 CF680 30025NE CARGO DECK PUNCTURED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25425FE 264 MDCC FLOOR PANEL 231VG IS PUNCTURED. FABED NEW FLOOR PANEL. 2L72 4F4 FRTA35EU E13NE 20050919000082005091900008EU 2005 9 19 05FDEA02911 120050914A5321231KH FLOOR PANEL AIRBUS310 A310 EU GE CF6 CF680 30025NE CARGO DECK CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25425FE 264 MDCC FLOOR PANEL 231KH IS CRACKED. FABED NEW FLOOR PANEL. 2L72 4F4 FRTA35EU E13NE 20050919000132005091900013EU 2005 9 19 05FDEA02914 120050914A5321232NG FLOOR PANEL AIRBUS310 A310 EU GE CF6 CF680 30025NE CARGO DECK DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25425FE 264 MDCC FLOOR PANEL 232NG DELAMINATED. FABED NEW FLOOR PANEL. 2L72 4F4 FRTA35EU E13NE 20050919000142005091900014EU 2005 9 19 05FDEA02915 120050914A5321241WH FLOOR PANEL AIRBUS310 A310 EU GE CF6 CF680 30025NE CARGO DECK CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25425FE 264 MDCC FLOOR PANEL 241WH IS CRACKED. FABED NEW FLOOR PANEL. 2L72 4F4 FRTA35EU E13NE 20050919000192005091900019EU 2005 9 19 05FDEA02920 120050914A5347A5381192320200 SEAT TRACK AIRBUS310 A310 EU GE CF6 CF680 30025NE CARGO DECK CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25425FE 264 MDCC SEAT TRACK BETWEEN FR. 51 ,52 LBL 56 HAS CORROSION . REMOVED AND REPLACED SEAT TRACK DUE TO OUT OF LIMITS CORROSION IAW SRM 53-10-16 AND 51-40-21. 2L72 4F4 FRTA35EU E13NE 20050919000302005091900030 2005 9 19 VTZA200500180 420050912A2210 AUTOPILOT SYS CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A VTZAO OTHER F FLT CONT AFFECTED CRCRUISE 1 EA27623BR 7192 UNCOMMANDED LT ROLL WITH AUTOPILOT ENGAGED. INTERROGATED FCC FOR FAULTS, FOUND NO DEFECTS. PERFORMED YAW DAMP COMMAND AND FEEDBACK TEST W/ NO DEFECTS NOTED REF FIM 22-11-00. PERFORMED AILRON/ELV SERVO SPIN UP TEST, FOUND NO DEFECTS AT THIS TIME REF FIM 22-22-00. AC OK FOR SERVICE. FDR WAS DOWNLOADED, FOUND ROLL TO BE NEGLIGIBLE (3 DEGREES EVERY 2 SEC) CHANGED HDG 11 DEGREES IN 20 SEC. 2L72 4F RTA21EA 20050919000342005091900034EA 2005 9 19 VTZA200500184 120050914A5340601R3111358 ANGLE CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27655BR 7457 RIGHT 280 VERTICAL ANGLE IS CRACKED AT .5 INCH BETWEEN FASTENERS. 2L72 4F RTA21EA 20050919000372005091900037NM 2005 9 19 QXEA200501221 120050909A2130 CABIN PRESSURE DHAV DHC8 DHC8202 2809007NM MALFUNCTIONED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09366PH 510 YLW FLIGHT 2175 - AIRCRAFT FAILED TO PRESSURIZE ON CLIMBOUT WITH PRESSURIZATION SELECTOR SWITCH IN AUTO AND CABIN SET NORM SWITCH IN EIGHT POSITION. MAINTENANCE DEFERRED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050919000452005091900045NM 2005 9 19 CALA0500310 120050914A5315147A5506 FLOORBEAM BOEING737 737724 13844BYNM STA 986.5 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2724702 28763 INSPECTION FOUND FORWARD FLANGE OF FLOORBEAM CORRODED ON NUT PLATE HOLES AT STA 986.6, LBL 23, LBL 26, RBL 4, RBL 12, AND RBL 20. THE FLOORBEAM WAS REPAIRED IAW ECRA 5321-01292. 2L72 4F RTA16WE 20050919000512005091900051NM 2005 9 19 FE5F200500002 120050826A291341022021 HOUSING CURTIS DOUG MD80 MD83 3023681NM HYD PUMP CRACKED W FE5FO OTHER K FLUID LOSS LDLANDING 1 WP03B80377628 1372 53479 THE A/C, LOST BOTH HYD PRESS (BOTH PRESS 0) WHILE TOUCH DOWN AND USE REVERSE THRUST(BOTH SIDE HYD QTY NORMAL.L:15, R:17 PROCEED QRH(L/R)HYD PRESS LOW PROCEDURE:TRANS PUMP SW OFF CHECK PRESSURE AND QTY NORMAL.TAXI BACK TO GATE. ENGINEERS VISUAL CHECKED, FOUND PUMP, HYD TRANSFER (PTU) LEAKAGE. REMOVED DEFECT PART SENT TO SHOP, FOUND HOUSING, DRAIN PORT ASSEMBLY CRACK. 2L72 4F RT 20050919000622005091900062NM 2005 9 19 DL738050510 120050903A25601317 BULB BOEING737 737832 13844CFNM EMERGENCY LIGHT BURNED OUT A DALAK NONE L NO TEST ININSP/MAINT 1 SO27383DN 30346 EMERGENCY LIGHTS OVERHEAD INOP AT 31B 32D 24B 01B. RELAMPED, ALL CHECKS OK. 2L72 4F RTA16WE 20050919000692005091900069NM 2005 9 19 DL733050523 120050906A5330 SKIN BOEING737 737347 1384647NM FS 727E S-22R CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27308WA 23441 CRACK WAS FOUND IN THE FUSELAGE SKIN WHILE DOING OPN 57546 INSPECTIONS. REPAIRED PER SRM 53-00-01, FIGURE 201. REF AD 2004-18-06 / S/B 737-53A1210 / 737-53-1065. 2L72 4F RTA16WE 20050919000912005091900091EA 2005 9 19 SWIA200515544 120050911A2740 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA YOKE INOPERATIVE A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07403SW 7028 CAPTAIN'S YOKE PITCH TRIM INOP. REPLACED CAPTAIN'S YOKE TRIM SWTICH IAW 27-41-05, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050919000932005091900093SO 2005 9 19 SWIA200515546 120050912A27523431001001 ACTUATOR EMB 120 EMB120ER 3260203SO NACELLE FLAPS FAILED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07212SW1277412774 120276 RIGHT NAC FLAP HYD FAILURE. INSTALLED HYDRAULIC ACTUATOR ON RT NACELLE FLAP. OPERATIONAL CHECKS ARE GOOD IAW 27-50-00. 2L72 4T RTA31SO 20050919000952005091900095NM 2005 9 19 PIDA20050090 120050623A5320 INTERCOSTAL BOEING737 737228 13844AGNM BS 320 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05237TR 23007 INTERCOSTAL AT BS 320 BETWEEN RBL 30 AND RBL 56 HAS CORROSION AT CLIP NUT HOLES. REPLACED CORRODED INTERCOSTAL SHIM PER SRM 51-10-1. 2L72 4F RTA16WE 20050919000982005091900098NM 2005 9 19 PIDA20050079 120050708A5315 FLOORBEAM BOEING737 737228 13844AGNM BS 1016 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05237TR 23007 BS 1016 FLOORBEAM HAS CORROSION FROM LBL 3 TO LBL 10. REPAIRED FLOORBEAM UPPER CHORD FROM LBL 3 TO LBL 10 PER EA 53-172. 2L72 4F RTA16WE 20050919001062005091900106NM 2005 9 19 PIDA20050091 120050627A5320 INTERCOSTAL BOEING737 737228 13844AGNM BS 294-312 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05237TR 23007 INTERCOSTAL AT LBL 11 BETWEEN BS 294 AND BS 312 HAS CORROSION AT CLIP NUT HOLES. REPLACED INTERCOSTAL PER SRM 51-10-1. 2L72 4F RTA16WE 20050919001082005091900108NM 2005 9 19 PIDA20050095 120050803A5754693927511 RIB BOEING737 737228 13844AGNM NR 3 SLAT CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05237TR 23007 NR 3 SLAT HAS A CRACK IN THE RIB O/B OF SLAT ACTUATOR. REPLACED SLAT RIB PER SRM 51-10-1 AND SRM 51-30-1. 2L72 4F RTA16WE 20050919001102005091900110NM 2005 9 19 PIDA20050106 120050628A5320 STRAP BOEING737 737228 13844AGNM BS 330 CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05237TR 23007 SONIC VIBRATION STRAP AT LBL 11 AT BS 330 IS CRACKED. REPAIRED STRAP PER SRM 53-10-9. 2L72 4F RTA16WE 20050919001132005091900113NM 2005 9 19 PIDA20050105 120050622A5340 CLIP BOEING737 737228 13844AGNM FLOORBEAM CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05237TR 23007 FLOORBEAM ATTACH CLIP AT BS 867 AT LBL 8 IN AFT CARGO BIN IS CORRODED. REPLACED ATTACH CLIP PER SRM 51-10-1. 2L72 4F RTA16WE 20050919001142005091900114NM 2005 9 19 PIDA20050102 120050628A5320 WEB BOEING737 737228 13844AGNM BS 500B-520 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05237TR 23007 WEB IN RIGHT SIDE OF FWD CARGO BIN IS CORRODED FROM BS 500B TO BS 520. REPLACED CORRODED WEB PER DWG 69-41757-504 AND SRM 51-10-1. 2L72 4F RTA16WE 20050919001172005091900117NM 2005 9 19 PIDA20050099 120050624A53206545875470 ANGLE BOEING737 737228 13844AGNM R1 DOOR CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05237TR 23007 Z-ANGLE AT R-1 DOOR HAS CORROSION AT FASTENER HOLES. REPLACED Z-ANGLE PER SRM 51-10-1. 2L72 4F RTA16WE 20050919001232005091900123NM 2005 9 19 PIDA20050107 120050623A5320 INTERCOSTAL BOEING737 737228 13844AGNM BS 328-344 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05237TR 23007 INTERCOSTAL AT LBL 11 IS CORRODED AT THE NUT PLATE HOLES FROM BS 328 TO BS 344. REPLACED INTERCOSTAL SHIM PER SRM 51-10-1. 2L72 4F RTA16WE 20050919001262005091900126NM 2005 9 19 PIDA20050067 120050819A5414 SKIN BOEING757 757200 1384950NM LT NACELLE DENTED A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05750WL 23928 WITH AIRCRAFT PARKED AT GATE, JETWAY STRUCK LEFT ENGINE NACELLE LEADING EDGE AT APPROX 11:00 POSITION. REPAIRED DENT PER SRM 54-10-01 AND EA NR 54-233. 2L72 4F RTA2NM 20050919001582005091900158EU 2005 9 19 F3LA200500039 120050907A5743 FITTING AIRBUSA319 A319112 3930323EU LT MLG CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03903FR 2143 1560 INSPECTION REPORTED CORROSION ON AFT FACE, FWD LUG, LT WING LANDING FITTING, RIB 5. MACHINED CORROSION PER SRM 57-26-13. 2L72 4F RTA28NM 20050919001592005091900159NM 2005 9 19 SWAA052792 120050914A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM BS 321 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 321, STR 29R. REMOVED AND REPLACED STRINGER PER SRM. 2L72 4F RTA16WE 20050919001642005091900164EU 2005 9 19 05FDEA02904 120050914A5321231NH FLOOR PANEL AIRBUS310 A310 EU CARGO DECK CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25425FE 264 MDCC - FLOOR PANEL 231NH IS CRACKED. FAB`D NEW PANEL. 2L72 4F RTA35EU 20050919001782005091900178WP 2005 9 19 UPS05845447 120050903A5712 RIB DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE:C3 LEFT WING L/E UPPER RIB IS CRACKED AT XFS 822.500. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-2-0, 51-1-21 AND 2-51-1-20D. 2L74 4F RT4A25 20050919001792005091900179WP 2005 9 19 UPS05845448 120050903A5712 RIB DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE:C3 LEFT WING L/E UPPER RIB IS CRACKED AT XFS 816.250. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0, 51-1-21 AND 51-1-20D. 2L74 4F RT4A25 20050919001812005091900181WP 2005 9 19 UPS05845450 120050913A5712 RIB DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE:C3 WHILE WORKING NR 808576, FOUND LT WING I/B FLAP LWR O/B SIDE 3RD RIB FROM LWR AT XW120 CRACKED. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 51-1-21, 57-2-0 FIG 2 SHT 2, 51-1-20D. 2L74 4F RT4A25 20050919001842005091900184EA 2005 9 19 REXA200500122 120050916A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A REXAO OTHER J WARNING INDICATION APAPPROACH 1 SO258721B 7721 FLAPS FAIL MESSAGE AND FLAPS FAILED AT 0 DEGREES. PERFORMED QUICK REFERENCE HANDBOOK. LANDING UNEVENTFUL. 2L72 4F RTA21EA 20050919001912005091900191NM 2005 9 19 05FDEA02929 120050915A5230 DEPRESSOR BOEING727 727227 1384078NM CARGO DOOR DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 NR 1 CARGO DOOR LWR CENTER SEAL DEPRESSOR DENTED AT AFT END. REPAIRED PER SRM 52-00-2. 2L73 4F A3WE 20050919001922005091900192NM 2005 9 19 05FDEA02930 120050915A5340 STRINGER CLIP BOEING727 727225 1384077NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 CORROSION FWD PIT A/C PLENUM AREA FRAME STA 720E BILGE AREA BETWEEN STRINGER 29R AND STRINGER 28R. REMOVED CORROSION IAW FX B727 SRM 51-10-6. FOUND BEYOND LIMITS IAW FX B727 SRM 53-10-1. REMOVED DAMAGED SECTION IAW FX B727 SRM 51-40-3. FAB REPAIR ANGLE IAW FX B727 SRM 53-10-4F15. ALODINED AND PRIMED IAW FX B727 SRM 51-10-2. PAINTED IAW FX B727 MM 51-20-001-17. INSTALLED REPAIR ANGLE IAW FX B727 SRM 51-30-2. 2L73 4F A3WE 20050919002072005091900207EA 2005 9 19 SWIA200515548 120050914A2752766361B ACTUATOR CNDAIRCL600 CL6002C10 1390015EA NR 2 MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED APAPPROACH 1 NM07719SK 10188 FLAPS FAILED AT 20 DEGREES. REPLACED LEFT NR 2 ACTUATOR PER CRJ MM 27-52-09. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050919002172005091900217SO 2005 9 19 RAIA00509015 120050911A3350 LIGHT EMB 145 EMB145LR 3260212SO OVERWING INOPERATIVE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03812HK 145373 FLT 3544-RIC-RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. MAINTENANCE RE-SET RIGHT OVERWING EMERGENCY EXIT SIGN. 2L72 4T RTT00011AT 20050919002192005091900219SO 2005 9 19 RAIA00509016 120050912A3397 CONNECTOR EMB 145 EMB145EP 3260221SO EMERGENCY LIGHT DAMAGED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03826HK 145016 FLT 5479-OKC- EMERGENCY EXIT LIGHTS ALONG FLOOR INTERMITTENT AND LIGHT AT FLIGHT DECK STEP INOP. MAINTENANCE REPAIRED CONNECTION TO STEP EMERGENCY LIGHTS. 2L72 4F RTT00011AT 20050919002262005091900226NM 2005 9 19 UPS05245433 120050902A5330 LAP JOINT BOEING727 72731C 1384011NM BS 1139 STR 4 RTCORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01922UP 19231 INSPECTION TYPE:C 2 BULGES FOUND ON LAP JOINT AT STRINGER 4R BS 1139. DAMAGED AREA CUT OUT IAW SRM 53-30-3 FIG 5 AND REPAIRED IAW SRM 53-30-3 FIG 5. 2L73 4F A3WE 20050919002292005091900229NM 2005 9 19 UPS05245436 120050828A5315 FLOORBEAM BOEING727 72731C 1384011NM BS 1130 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01922UP 19231 INSPECTION TYPE:C SURFACE CORRSION AT BS 1130 JOINT BETWEEN FLOORBEAM TOP AND CREASE WEB AT RBL 62. REPAIR PARTS FABRICATED IAW AAAE EO 2005-081-003 - UPS ENG FILE 72 7-53-20189. DOUBLER INSTALLED IAW SRM 51-30-02. 2L73 4F A3WE 20050919002302005091900230NM 2005 9 19 UPS05245437 120050828A5740 ATTACH FITTING BOEING727 72731C 1384011NM BS 1050 LBL 21 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01922UP 19231 INSPECTION TYPE: C, CRACK IN ZEE SECTION ATTACHED TO FRAME AT BS 1050 LBL 21. Z-SECTION REPAIRED IAW SRM 51-40-4 FIG 2. 2L73 4F A3WE 20050919002322005091900232WP 2005 9 19 UPS05845418 120050903A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE: C3, LEFT WING L/E UPPER SKIN HAS A DAMAGED FASTENER HOLE AT XFS 347.750. FABRICATED AND INSTALLED DOUBLER IAW 57-03-03 FIG 005 PG 1,EO DC8-572 0-7767-A AND SRM 51-1-21. 2L74 4F RT4A25 20050920000032005092000003NM 2005 9 20 05FDEA02922 120050915A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 CRACK INDICATION AT END OF STRINGER 14 WAS FOUND DURING HFEC INSPECTION AT LEFT SIDE WING TANK. SLOTTED OUT AND REPAIR CARRIED OUT AS PER SRM 57-20-00, FIGURE 10 VOLUME I. STRINGER REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050920000192005092000019WP 2005 9 20 ABXA050228 120050517A534059104645 SUPPORT ANGLE DOUG DC9 DC932F 3022067WP BS 660 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23909AX 47148 CENTER TANK UPPER SUPPORT ANGLE WAS CRACKED AT STA 660, LEFT BUTT LINE 42. REMOVED AND REPLACED SUPPORT ANGLE IAW DC-9 SRM. 2L72 4F A6WE 20050920000212005092000021NM 2005 9 20 ABXA050234 120050916A5210 DOOR BOEING767 767200 1385120NM MAIN PAX OPEN A ABXAO OTHER W INADEQUATE Q C CLCLIMB 1 GL23799AX 23432 DURING CLIMB-OUT AT FL260, A MODERATELY LOUD NOISE WAS HEARD AND EICAS MESSAGE LEFT FORWARD ENTRANCE DOOR ILLUMINATED. CABIN PRESSURE CONTROL REMAINED NORMAL. PASSENGER REPORTED THAT THE ENTRY DOOR LOCKING HANDLE HAD POPPED TO THE OPEN POSITION. AIRCRAFT WAS LEVELING AND DOOR HANDLE WAS PUSHED BACK TO THE CLOSED POSITION. EICAS MESSAGE WENT OUT. PROBLEM DID NOT RECUR. PERFORMED OPERATIONAL CHECK OF ENTRY DOOR SEVERAL TIMES, OPS CHECKED GOOD. PERFORMED BITE TEST OF PSEU, NO FAULTS NOTED IAW B767 MM. 2L72 4F RTA1NM 20050920000222005092000022NM 2005 9 20 SWAA052817 120050918A26124735975 FIRE DETECTOR BOEING737 7377H4 1384404NM AFT CARGO FAULTY A SWAAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 SW29497WN 32479 DIVERSION/DECLARED EMERGENCY. AFT CARGO FIRE WARNING LIGHT ILLUMINATED DISCHARGED ONE FIRE EXTINGUISHER BOTTLE. REMOVED AND REPLACED B3 SMOKE DETECTOR & FIRE EXTINGUISHER BOTTLE PER MM. 2L72 4F RTA16WE 20050920000232005092000023NM 2005 9 20 SWAA052818 120050913A53126516300 BULKHEAD BOEING737 7375H4 138449DNM BS 179 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29506SW 24183 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE BULKHEAD WEB CRACKED AT BS 179, LBL 17.1, WL 236. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050920000252005092000025NM 2005 9 20 SWAA052820 120050916A3350101331 LENS BOEING737 7375H4 138449DNM RT OVERWING LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29526SW 26568 RIGHT OVERWING EXIT SIGN LENS LOOSE. SECURED LENS PER MM. 2L72 4F RTA16WE 20050920000272005092000027NM 2005 9 20 SWAA052822 120050916A5315BAC15171489 FLOORBEAM BOEING737 7373H4 1384600NM BS 270 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 DURING SCHEDULED D-CHECK, FOUND COCKPIT FLOORBEAM CORRODED AT BS 270, BETWEEN LBL 6 TO RBL 6. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20050920000292005092000029NM 2005 9 20 SWAA052824 120050916A53106549921 CREASE BEAM BOEING737 7373H4 1384600NM BS 380-400 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 DURING SCHEDULED D-CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 380 TO BS 400. REPAIRED CREASE BEAM WEB PER SRM. 2L72 4F RTA16WE 20050920000302005092000030 2005 9 20 SWAA052825 420050916A25656557463 BRACKET BOEING737 7373H4 1384600NM GIRT BAR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 DURING SCHEDULED D-CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKETS CORRODED. REMOVED AND REPLACED BRACKETS PER SRM. 2L72 4F RTA16WE 20050920000312005092000031NM 2005 9 20 SWAA052826 120050916A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 787 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CORRODED AT BS 787, STR 26R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050920000322005092000032NM 2005 9 20 SWAA052827 120050916A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM BS 787 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, RBL 17. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050920000332005092000033NM 2005 9 20 SWAA052828 120050916A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM BS 767 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 767, BETWEEN LBL 2 TO RBL 12. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050920000342005092000034NM 2005 9 20 SWAA052829 120050916A53116546532 FRAME BOEING737 7373H4 1384600NM BS 480 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050920000352005092000035NM 2005 9 20 SWAA052830 120050916A53116546526 FRAME BOEING737 7373H4 1384600NM BS 400 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050920000392005092000039NM 2005 9 20 05FDEA02944 120050916A5311 FRAME DOUG MD11 MD11 3023602NM BS 577 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 LOWER FUSELAGE, LT AIRCON COMPT NR 1 INTERIOR FUSELAGE FRAME AT STA 577 LT LONGERON 44-48L, FOUND DENTED. DENTED FRAME REMOVED & NEW FRAME INSTALLED AS PER SRM 51-35-01 VOL.II. NEW FRAME FABRICATED AS PER DRAWING ACA 3352 P/N FX ACA 3352-3. MINOR REPAIR PER GMM 6-2-100. 2L73 4F RTA22WE 20050920000412005092000041WP 2005 9 20 UPS05845420 120050812A5320 CUSP WEB DOUG DC8 DC871F 302199DWP FS 1100 L21R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 INSPECTION TYPE:C1 CUSP CRACKED FS 1100 L21R. REMOVED CUSP DOUBLER AT FS 1100 L21R AND REMOVED DAMAGED SECTION OF L21R IAW SRM 51-1-20A AND SRM 53-2-5 FIG 15. FABRICATED AND INSTALLED SPLICE PLATE -3 AND -5, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-2-5 FIG 15 AND TR 53-179 AND BOEING MESSAGE NUMBER 1-115367837-2. 2L74 4F RT4A25 20050920000422005092000042NE 2005 9 20 2005F00099 120050907A6210 STRIP SKRSKY SKRSKYS61 S61N 8142104NE M/R BLADE DEBONDED B ERAAK NONE O OTHER ININSP/MAINT 1 AL03564EH 61M4041380 61365 MAIN ROTOR BLADE OUTBOARD EROSION STRIP DEBONDED. 2G72 4U 1H15 20050920000442005092000044NM 2005 9 20 05FDEA02932 120050915A2781 INDICATOR BOEING727 72722 1384002NM NR 2 K FLAPS INOPERATIVE A FDEAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 SO25191FE 19084 NR 2 KRUGER FLAP LED FAILED TO RETRACT ON SCHEDULE. KRUGER FLAP INDICATION INOP, FO'S AND SO'S PANEL REMOVED AND REPLACED NR 2 POS INDICATION SWITCH PER MM 27-82-001-4 SYS, OPS CHECK NORMAL. 2L73 4F A3WE 20050920000452005092000045 2005 9 20 05FDEA02933 420050915A3442 RADAR BOEING737 737247 138448DNM WX SYSTEM MALFUNCTIONED A FDEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO25237FE 21331 RADAR INOP WITH RANGE AT 40 MILES, 15 LOW TILT, NO GND RETURN, LEVEL FLIGHT 80 MILE RANGE TILT 1.5 UP, RADAR SHOWED NUMEROUS RETURNS WITH VISUALLY NO WEATHER AHEAD. WEATHER RADAR OPS CHKS NORMAL ON GRND IAW 727-200AMM 34-41-000-0. 2L72 4F A16WE 20050920000462005092000046NM 2005 9 20 05FDEA02934 120050915A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 CRACK INDICATION AT END OF STRINGER-14 WAS FOUND DURING HFEC INSPECTION AT RIGHT SIDE WING TANK. SLOTTED OUT AND REPAIR CARRIED OUT AS PER SRM 57-20-00, FIG 10, VOL I. NEW STRINGER CLIP FABRICATED AS PER FEDEX EA 1-5720-90025, THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050920000522005092000052EU 2005 9 20 ASOA05713 120050729A5320S5337129320201 PLATE AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11636AS 375 DURING A C-CHECK, THE SUPPORT PLATES BETWEEN FRAME 13 TO FRAME 17, LBL 47 FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SUPPORT PLATED BETWEEN FRAME 13 TO FRAME 17, LBL 47 IAW ATR-72 SRM 51-25-01. 2H72 4T RTA53EU 20050920000762005092000076NM 2005 9 20 05FDEA02876 120050914A5744 ATTACH FITTING DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 RT WING, O/B FLAP O/B HINGE (WING SIDE), LWR ATTACHMENT O/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87641. 2L73 4F RTA22WE 20050920000782005092000078NM 2005 9 20 05FDEA02878 120050914A5744 ATTACH FITTING DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 RT WING, O/B FLAP O/B HINGE (WING SIDE), SIDE LINK ATTACHMENT LWR AFT BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87641. 2L73 4F RTA22WE 20050920000832005092000083WP 2005 9 20 05FDEA02864 120050914A5330 SKIN DOUG DC10 DC1010 3022110WP BS 979-999 DENTED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25571FE 47830 DURING AIRPLANE'S CONVERSION FROM P TO F FOUND: DENT AND NICK ON LOWER SKIN FUSELAGE AT STA 979-999 LONGERON 45-46 RT, DENT DIMENSION 2.5 X 4.5, 0.08. BLEND OUT NICKS AND VERIFIED LIMIT IAW SRM 53-00-01FIG 1A. REWORKED DENTS AREA IAW SRM 53-20-00 FIG 13, DYE PENETRANT INSP FOR CRACKS. INSTALLED FINGER DOUBLER IAW SRM 53-20-00 FIG 13. 2L73 4F A22WE 20050920000852005092000085NM 2005 9 20 05FDEA02874 120050914A5744 ATTACH FITTING DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 RT WING, O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87641. 2L73 4F RTA22WE 20050920000872005092000087NM 2005 9 20 SWAA052793 120050915A5753 SKIN BOEING737 7373H4 1384600NM LT WING FOREFLAPDELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 DURING SCHEDULED 1/4D CHECK, FOUND LT WING OUTBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM. 2L72 4F RTA16WE 20050920000892005092000089NM 2005 9 20 SWAA052795 120050915A53156546811 FLOORBEAM BOEING737 7373H4 1384600NM BS 986 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 986, BETWEEN LBL 35 TO LBL 45. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20050920000912005092000091NM 2005 9 20 SWAA052797 120050915A53116546555 FRAME BOEING737 7373H4 1384600NM BS 867 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L & STR 8R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050920000932005092000093NM 2005 9 20 SWAA052799 120050915A53116546548 FRAME BOEING737 7373H4 1384600NM BS 747 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L & STR 8R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050920000952005092000095NM 2005 9 20 SWAA052801 120050915A53116546552 FRAME BOEING737 7373H4 1384600NM BS 827 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R TO STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050920000982005092000098NM 2005 9 20 05FDEA02881 120050914A5744 ATTACH FITTING DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 RT WING, O/B FLAP O/B HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87641. 2L73 4F RTA22WE 20050920000992005092000099NM 2005 9 20 05FDEA02882 120050914A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 HORIZONTAL STAB LT NR 26 BARREL NUT BORE AREA CORRODED. CORRODED SPLICE FITTING REMOVED AND NEW FITTING INSTALLED PER SRM 51-32-01, VOL II, SRM 51-38-01 VOL II, SRM 51-33-01 VOL II. MINOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20050920001002005092000100NM 2005 9 20 05FDEA02888 120050914A5210 FRAME BOEING727 727233 138408ANM PAX DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25268FE 21674 FWD ENTRY DOOR, LWR FRAME IS CRACKED, AT THE LWR FWD CORNER. REPLACED FWD ENTRY DOOR LWR FWD CORNER FRAME IAW SRM 51-30-2, 51-30-5. 2L73 4F RTA3WE 20050920001012005092000101NM 2005 9 20 05FDEA02889 120050914A5330 SKIN BOEING727 727225 1384077NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 PREVIOUS REPAIR,SKIN CUT-OUT APPEARS TO HAVE CRACK STA 500 S20R AND S21R. REMOVED, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLERS IAW B727 SRM 51-30-2, 53-30-30 FIG 3. 2L73 4F A3WE 20050920001022005092000102NM 2005 9 20 05FDEA02890 120050914A5310 DOOR FRAME BOEING727 727225 1384077NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 L1 DOOR CUT-OUT UPPER HINGE CAVITY, FRAME IS CRACKED AROUND HOLE. 2L73 4F A3WE 20050920001032005092000103NM 2005 9 20 05FDEA02891 120050914A5315 FLOORBEAM BOEING727 727233 138408ANM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25286FE 22623 FLOORBEAM CORRODED STA 620 FROM BL 0 TO LBL 45. REMOVED, FABBED, HEAT TREATED, CAD PLATED, ALODINED, PRIMED AND INSTALLED FLOORBEAM REPAIR AT STA 620 FROM BL 0 TO LBL45 ALL IAW FX SR 27-53-034E FIG 1 & 4,FX B727 SRM 51-10-2,BAC5619(H) AND BAC5701. 2L73 4F RTA3WE 20050920001042005092000104WP 2005 9 20 05FDEA02892 120050914A5744 BRACKET DOUG MD10 MD1010F 3022112WP TE FLAPS CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25550FE 46521 RT INBD FLAP, OTBD HINGE ASSY UPPER AFT SUPPORT BRACKET WAS FOUND CRACKED. REMOVED FAB AND REPLACED BRACKET IAW SRM 51-35-01, 51-33-01, MINOR REPAIR IAW FEDEX GMM. 2L73 4F RTA22WE 20050920001052005092000105NM 2005 9 20 05FDEA02893 120050914A5315 FLOORBEAM BOEING727 727233 138408ANM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25286FE 22623 FLOORBEAM CORRODED STA 720D FROM RBL 24 TO LBL 45. REMOVED, FABBED, HEAT TREATED, CAD PLATED, ALODINED, PRIMED AND INSTALLED FLOORBEAM REPAIR AT STA 720D FROM RBL 24 TO LBL 45 ALL IAW FX SR27-53-034E FIG. 1 & 4, FX B727 SRM 51-10-2, BAC5619 (H) AND BAC 5701. 2L73 4F RTA3WE 20050920001062005092000106NM 2005 9 20 05FDEA02894 120050914A5330 SKIN BOEING727 727225 1384077NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 FUSELAGE SKIN DENTED BS 370 BETWEEN STR 3-R AND STR 6-R. 2L73 4F A3WE 20050920001082005092000108 2005 9 20 YENA200565 420050914A233020092455101 COOLING FAN AIRBUS320 A320232 3930326EU LIVE TV FAILED A YENAO OTHER J WARNING INDICATION APAPPROACH 1 EA15594JB4034 2284 ON FINAL TO TPA - AFT AVIONICS SMOKE WARNING ACTIVATED. WARNING ACTIVATED AGAIN AT NR 2 ENG SHUT DOWN AND WHEN EXTERNAL A/C POWER APPLIED. NO OTHER SMOKE/HEAT/FIRE WARNINGS. INITIALLY ITEM WAS DEFERRED PER MEL 25-27-03. REPLACED AFT RACK COOLING FAN ASSY PER AMM 23-39-00. 2L72 4F RTA28NM 20050920001102005092000110 2005 9 20 SWAA052816 420050918A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29487WN 33854 R1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20050920001152005092000115NM 2005 9 20 QXEA200501240 120050917A2913 PUMP BOMBDRDHC8 DHC8402 1390042NM NR 3 HYD SYSTEM FAILED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09408QX 4050 BZN FLIGHT 2328: NR 3 HYDRAULIC PUMP CAUTION LIGHT ILLUMINATED ON TAXI OUT. MAINTENANCE RESEATED RELAY 2431 RL4. OPS CHECK GOOD ON GROUND RUN. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050920001162005092000116WP 2005 9 20 UPS05845457 120050917A2560 SMOKE GOGGLES DOUG DC8 DC873F 302199FWP COCK PIT SCRATCHED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 2ND OBSERVERS SMOKE GOGGLES SCRATCHED. REPLACED SMOKE GOGGLES. 2L74 4F RT4A25 20050920001182005092000118NM 2005 9 20 AWXA200501042 120050916A3350BMS13311122 WIRE BOEING737 7373G7 1384595NM EMERGENCY LIGHT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 DEN - EEL - DURING 4 DAY DISCOVERED THE EMERGENCY ESCAPE PATH LIGHTS AT ROW 2 INOPERATIVE. MAINTENANCE RE-SPLICED A BROKEN WIRE UNDER ROW 2L. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20050920001202005092000120NM 2005 9 20 AWXA200501044 120050825A575465C267937 SKIN BOEING737 7373Y0 1384671NM ZONE 600 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED 8 CRACKS ON BOTTOM OF THE NR 4 SLAT SKIN, BELOW ACTUATOR AT SS 61.01. MAINTENANCE REMOVED DAMAGED SKIN ON THE NR 4 SLAT IAW BOEING 737-300 SRM 57-43-01-2R. FABRICATED FILLER AND SPLICE PLATE IAW BOEING 737-300 SRM 57-43-01-2. INSTALLED FABRICATED REPAIR PARTS ON THE NR 4 SLAT SKIN, BELOW ACTUATOR, AT SS 61.01 IAW BOEING 737-300 SRM 57-43-01-2R 6 SHEETS 1-4. 2L72 4F RTA16WE 20050920001222005092000122NM 2005 9 20 AWXA200501046 120050825A575465C266025 SKIN BOEING737 7373Y0 1384671NM SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED 3 CRACKS, .375 INCHES IN LENGTH, FROM SS 167.5L TO SS 172L, ON THE BOTTOM OF THE NR 2 SLAT SKIN, INBOARD OF THE TELESCOPING ANTI ICE TUBE. MAINTENANCE REMOVED THE DAMAGED SKIN ON THE NR 2 SLAT IAW BOEING 737-300 SRM 57-43-01-2. FABRICATED FILLER AND SPLICE PLATE IAW BOEING 737-300 SRM 57-43-01-2R 6 FIG 201. INSTALLED FABRICATED REPAIR PARTS AT THE BOTTOM OF THE NR 2 SLAT, INBOARD OF THE TELESCOPING ANTI ICE TUBE, SS 167.5L TO SS 172L, IAW BOEING 737-300 SRM 57-43-01-2R 6 FIG 201. 2L72 4F RTA16WE 20050920001242005092000124NM 2005 9 20 AWXA200501048 120050823A57536546431280 SKIN BOEING737 7373Y0 1384671NM ZONE 600 DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED DISBOND AREA ON THE UPPER SURFACE OF THE RT OUTBOARD FORE FLAP FROM WBL 197.5 TO WBL 200.5. MAINTENANCE REMOVED DAMAGED AREA ON THE RT OUTBOARD FORE FLAP IAW BOEING 737-300 SRM 51-70-10-2R 4. FABRICATED CORE, SEPTUM, FILLER, AND DOUBLER IAW BOEING 737-300 SRM 51-70-10-2R. BONDED REPAIR PARTS TO UPPER SURFACE OF THE RT OUTBOARD FORE FLAP FROM WBL 197.5 TO WBL 200.5 IAW BOEING 737-300 SRM 51-70-10-2. 2L72 4F RTA16WE 20050920001252005092000125NM 2005 9 20 AWXA200501049 120050826A57536546443128 SKIN BOEING737 7373Y0 1384671NM ZONE 600 DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED DISBOND AREA ON THE UPPER SURFACE OF THE RT OUTBOARD FORE FLAP FROM WBL 301.69 TO WBL 305.69. MAINTENANCE REMOVED DAMAGED AREA ON THE RT OUTBOARD FORE FLAP IAW BOEING 737-300 SRM 51-70-10-2R 4. FABRICATED CORE, SEPTUM, FILLER, AND DOUBLER IAW BOEING 737-300 SRM 51-70-10-2R. BONDED REPAIR PARTS TO UPPER SURFACE OF THE RT OUTBOARD FORE FLAP FROM WBL 301.69 TO WBL 305.69 IAW BOEING 737-300 SRM 51-70-10-2. 2L72 4F RTA16WE 20050920001262005092000126NM 2005 9 20 AWXA200501050 120050825A5755664645155A PANEL BOEING737 7373Y0 1384671NM ZONE 500 - LEFT DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED DISBOND AREA ON THE UPPER AND LOWER SURFACE OF THE NR 3 SPOILER PANEL AT INBOARD AFT CORNER FROM WING STATIONS 291L TO WING STATIONS 297L. MAINTENANCE REMOVED DISBOND AREA FROM THE NR 3 SPOILER PANEL IAW BOEING 737-300 SRM 51-70-10-2R REPAIR 4. FABRICATED FILLER, DOUBLER, AND REPAIR CORE IAW BOEING 737-300 SRM 51-70-10-2R FIG 203. BONDED REPAIR PARTS TO THE NR 3 SPOILER PANEL UPPER AND LOWER SURFACES FROM WING STATIONS 291L TO WING STATIONS 297L IAW BOEING 737-300 SRM 51-70-10-2R4 FIG 203. 2L72 4F RTA16WE 20050920001272005092000127NM 2005 9 20 AT0500032 120050914A3350LP7265001 LAMP BOEING717 717200 1383700NM EMERGENCY LIGHT BROKEN A ZZDAK NONE L NO TEST ININSP/MAINT 1 SO15947AT 55010 EMERGENCY PATH LIGHT 1FWD, 10, AND 20 INOP. RELAMPED, OPS CHECK NORMAL. REF MM 33-00. 2L72 4F TRA6WE 20050920001282005092000128NM 2005 9 20 AT0500033 120050914A3350LP7265001 LAMP BOEING717 717200 1383700NM EMERGENCY LIGHT BROKEN A ZZDAK NONE L NO TEST ININSP/MAINT 1 SO15935AT 55069 ROW 17 EMERGENCY LIGHT INOP. REMOVED & REPLACED EMERGENCY LIGHT BULBS REF AMM 33-51, OPS CHECK GOOD. P/N OFF/ON LP7265-001. 2L72 4F TRA6WE 20050920001292005092000129NM 2005 9 20 AWXA200501040 120050913A2121731376A FAN BOEING757 7572S7 1384962NM CABIN BURNED A AWXAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP28903AW 23323 PILOTS REPORTED A STRONG BURNING ODOR COMING FROM FLT DECK WHILE THE ACFT PARKED AT GATE. PILOTS REPORTED THE CIRCUIT BREAKER FOR THE EQUIPMENT COOLING SUPPLY FAN 1 WAS FOUND POPPED ON THE P6-3 PANEL F-17. MX REMOVED AND REPLACED THE NR 1 EQUIPMENT COOLING FAN PER BMM 21-58-06-4. OPERATIONAL TEST WAS GOOD. VENDOR TEAR DOWN REPORT CONFIRMS REASON FOR REMOVAL. PRETEST WAS PERFORMED AND FAILED INSULATION TEST. FOUND BEARING FAILURE AND STATOR ASSEMBLY BURNED. BEARING, CONNECTOR, KEY AND STATOR ASSEMBLY WERE REPLACED AND UNIT PASSED FUNCTIONAL TEST. ALL WORK AND FUNCTIONAL TESTS WERE PREFORMED IAW CMM 21-58-15 REV 10. 2L72 4F RTA2NM 20050920001332005092000133NM 2005 9 20 AWXA200501051 120050823A5753654643099 WEDGE BOEING737 7373Y0 1384671NM ZONE 500 - LEFT DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED DISBOND AREA ON THE UPPER SURFACE OF THE LT INBOARD FORE FLAP FROM WBL 103.0L TO WBL 111.0L. MAINTENANCE REMOVED DAMAGED AREA ON THE LT INBOARD FORE FLAP FROM WBL 103.0L TO WBL 111.0L IAW BOEING 737-300 SRM 51-70-10-2R 4. FABRICATED CORE, SEPTUM, FILLER, AND DOUBLER IAW BOEING 737-300 SRM 51-70-10-2R. BONDED REPAIR PARTS TO UPPER SURFACE OF THE LT INBOARD FORE FLAP FROM WBL 103.0L TO WBL 111.0L IAW BOEING 737-300 SRM 51-70-10-2. 2L72 4F RTA16WE 20050920001482005092000148EA 2005 9 20 QXEA200501232 220050914A7397312240105 WIRE HARNESS BOMBDRDHC8 DHC8402 1390042NM PWC 150 PW150A EA FADEC FAILED A QXEAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 NM09408QX 4050 SMR FLIGHT: POWERPLANT MESSAGE ON ED FOLLOWED BY NR 1 ENGINE FADEC FAIL MASTER WARNING. ENGINE SHUTDOWN PER CHECKLIST. MAINTENANCE FOUND FAULT CODES 935, 936 AND 360. BOTH A AND B CHANNELS FAILED. REMOVED AND REPLACED FUEL CONTROL ELECTRICAL HARNESS IAW Q400 AMM 73-21-11. CLEARED FAULT CODES. GROUND RAN FOR HARNESS REPLACEMENT IAW TASK 71-00-868-805 (ENGINE REPLACEMENT RUNS). AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E00062EN 20050920001492005092000149NM 2005 9 20 0501426638 120050909A2612 CIRCUIT CARD BOEING747 747251B 1384892NM APU FIRE DETECT FAILED A NWAAO OTHER N FALSE WARNING CRCRUISE 1 GL01638US 23549 DURING CRUISE APU B FIRE DETECTION FAULT LIGHT, AND APU FIRE WARNING LIGHT ILLUMINATED INTERMITTENTLY. COM PROCEDURE ACCOMPLISHED. AIRCRAFT CONTINUED AND LANDED WITHOUT INCIDENT. NRT MAINTENANCE REPLACED APU FIRE CONTROL CARD. OPERATIONAL CHECK GOOD. 2L74 4F A20WE 20050920001512005092000151WP 2005 9 20 P20050099 120050911A3350582011 SIGN DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A P9RAK NONE O OTHER ININSP/MAINT 1 SO11135NJ 49440 FWD LT EMERGENCY EXIT DOOR EXIT LUMINCENT SIGN INOP. REMOVED AND REPLACED FWD LT EXIT SIGN IAW AMM 33-53-01. OPS CHECK GOOD. PART MANUFACTURER: LUMINESCENT SYSTEMS INC. 2L72 4F A6WE 20050920001532005092000153NM 2005 9 20 UPS05445460 120050916A3350 LAMP BOEING747 747123 1384873NM EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 UPPER DECK SERVICE DOOR EMERGENCY LIGHT INOP. RELAMPED PER MM 33-51-05 OPS CK OK. 2L74 4F A20WE 20050920001552005092000155NM 2005 9 20 UPS05445463 120050916A5411 RIB BOEING747 747121 1384871NM NR 2 PYLON DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 L/T SIDE OF THE NR 2 PYLON, DAMAGED RIBS REPAIR. SHOW EVIDENCE OF CRACK INSIDE PYLON OPPOSITE PREVIOUS REPAIR. 11' FROM SLOT SEAL OPENIN G AND 8' FROM BOTTOM EDGE. ACCOMPLISED HI-FREQUENCY EDDY CURRENT SUSPECT AREA NO CRACKS DETECTED 2L74 4F A20WE 20050920001572005092000157WP 2005 9 20 UPS05845452 120050810A5312 PRESSURE PANEL DOUG DC8 DC871F 302199DWP FS 940 L24L CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 POPPED RIVET, PILLOWED SKIN, LT W/W CEILING, STA 940 OB ABOVE L24L. REMOVED CORROSION AND FOUND OUT OF LIMITS AT STA 940 L24L IAW SRM 51-1-8, FABRICATED AND INSTALLED FILLER, SPLICE DOUBLER FINGER DOUBLER AND TAPERED FILLER AT STA 940 L24L IAW SAA SK 750-846380, DWG SRO8530026, BOEING MESSAGE NR 1-117725249, BOEING MESSAG E 1-118905200-4. 2L74 4F RT4A25 20050920001592005092000159WP 2005 9 20 MWEA050106 120050916A26136712152180 OVERHEAT SENSOR DOUG DC9 DC982 3022082WP TAIL INOPERATIVE A MWEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL31810ME 48072 TAIL COMPARTMENT HIGH TEMPERATURE LIGHT CAME ON. REMOVED AND REPLACED OVERHEAT SENSOR AND TIGHTENED RIGHT CLAMP. 2L72 4F A6WE 20050920001612005092000161NM 2005 9 20 CALA0500314 120050912A5330 SKIN BOEING737 7373T0 1384582NM STA 727D CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770352 23590 MAINTENANCE FOUND A 2 INCH CRACK IN RT FUSELAGE SKIN AT STA 727D AND S23R. A REPAIR WAS INSTALLED IAW ECRA 5330-03482. A DIP WAS ISSUED TO REINSPECT THE AREA WITHIN 60,000 FLIGHT CYCLES AND TO ACCOMPLISH SUBSEQUENT REPEAT INSPECTIONS EVERY 25,000 FLIGHT CYCLES THEREAFTER. 2L72 4F RTA16WE 20050920001632005092000163NM 2005 9 20 CALA0500316 120050918A2121731376B FAN BOEING757 757224 1384958NM E&E COMPT INOPERATIVE A CALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2714107 27297 A STRONG ODOR OF ELECTRICAL SMOKE WAS NOTICED IN THE CABIN WHILE EN ROUTE FROM LAX TO EWR. THE ELECTRICAL AND AIR CONDITIONING SMOKE AND FIRE CHECKLISTS WERE RUN AND THE SOURCE COULD NOT BE IDENTIFIED. THE AIRCRAFT WAS DIVERTED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE FORWARD EQUIPMENT COOLING SUPPLY FAN NR 1 CIRCUIT BREAKER POPPED. THE COOLING FAN WAS FOUND INTERNALLY FAILED. THE FAN C/P WAS DISCONNECTED AND STOWE AND THE FAN WAS PLACARD INOPERATIVE DUE TO PART NOT BEING IN STOCK. 2L72 4F RTA2NM 20050920001652005092000165NM 2005 9 20 QXEA200501231 120050915A5210 HANDLE BOMBDRDHC8 DHC8402 1390042NM PAX DOOR UNSECURE A QXEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM09409QX 4051 RNO FLIGHT 2446: FUSELAGE DOOR WARNING LIGHT (FORWARD CARGO) CAME ON AT FL 21,000 - PRESSURIZATION WAS NORMAL. MAINTENANCE, UPON ARRIVAL TO GATE, FOUND DOOR HANDLE NOT SECURE. SECURED HANDLE AND PERFORMED 3 OPERATIONAL TESTS OF BAGGAGE DOOR PER AMM 52-32-00-710-801. EACH OPERATION OF DOOR PRODUCED NO DEFECTS TO NOTE. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050920001672005092000167 2005 9 20 YENA200566 420050915A23973042865102 ELECTRICAL BOX AIRBUS320 A320232 3930326EU LIVE TV FAILED A YENAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15553JB3493 1896 INFLT CREW REPORTED SMELL AROUND SEATS 24-25 A/C LEFT. TURNED LIVE TV OFF SMELL DISSIPATED. PERFORMED INFO NOTICE 2004-T023TR AND TSM 24-00-00. NO DEFECTS NOTED. INITIALLY THE AIRCRAFT FLEW UNDER MEL 25-22-03. FINAL ACTION - REPLACED SEB AT 25B PRECAUTIONARY AS PER INFO NOTICE 2004-T023TR. SEB HAS ONE NUTPLATE SHEARED OFF AND LOOSE INSIDE SEB. FOUND NO EVIDENCE OF BURNING ARCING ELECTRICAL ODOR OR OTHER CONTAMINATION. 2L72 4F RTA28NM 20050920001682005092000168 2005 9 20 P9RA20050100 420050915A3457S67157582 ANTENNA DOUG DC9 DC982 3022082WP GPS FAULTY A P9RAH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION NRNOT REPORTED 1 SO11130NJ 49222 GPS MESSAGE ON CDU, GPS ANTENNA FAIL & DEAD RECONING. FMS PLACED ON MEL 34-42-01 CAT-C. 2L72 4F A6WE 20050920001702005092000170NM 2005 9 20 0501436638 120050909A2612 FIRE DETECTOR BOEING747 747251B 1384892NM APU BAY FALSE INDICATIONA NWAAO OTHER N FALSE WARNING NRNOT REPORTED 1 GL01638US 23549 APU B-FIRE DETECTION FAULT LIGHT, AND APU FIRE WARNING LIGHT ILLUMINATED INTERMITTENTLY. COM PROCEDURE ACCOMPLISHED. AIRCRAFT CONTINUED AND LANDED WITHOUT INCIDENT. LAX COMPLIED WITH MEL. NRT MAINTENANCE REPLACED APU LOWER SENSING ELEMENT 13SEP05. OPERATIONAL CHECK GOOD. 2L74 4F A20WE 20050920001712005092000171EU 2005 9 20 XN0A1266 120050916A2420 GENERATOR AIRBUS300 A300B4203 3930306EU NR 1 FAILED A XN0AD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL23371PC 157 NR 1 GENERATOR OFF LIGHT CAME ON AFTER BLOCK-OUT. ITEM TRANSFERRED TO DMI 5730 IAW ENA MEL 24-11-01 CAT-B. NR 1 GENERATOR DISCONNECTED IAW A300 AMM 24-00-00. PLACARDS INSTALLED. REMOVED AND REPLACED NR 1 GEN AS PER A300 MM 24-21-11, GROUND CHECK NORMAL DMI CLEARED. 2L72 4F RTA35EU 20050920001722005092000172NM 2005 9 20 SWAA052833 120050917A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 578 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29618WN 28034 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 578, STR 11R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050920001742005092000174 2005 9 20 SWAA052835 420050918A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29623SW 27933 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20050920001762005092000176NM 2005 9 20 SWAA052837 120050918A5310573149 POST BOEING737 7373L9 1384470NM COCKPIT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED 1/2D CHECK, FOUND L1 COCKPIT WINDOW POST CRACKED AT UPPER OUTBOARD CORNER. REPAIRED WINDOW POST PER SRM. 2L72 4F RTA16WE 20050920001782005092000178WP 2005 9 20 P9RA20050098 120050915A33506011777 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT DISCHARGED A P9RAK NONE L NO TEST ININSP/MAINT 1 SO1169826 49486 OVERWING EMERGENCY EVACUATION LIGHTS ARE INOP. REMOVED AND REPLACED OVERWING EMERGENCY EVACUATION LIGHTS BATTERY POWER SUPPLY IAW MM 33-53-00. OPS CHECK GOOD. 2L72 4F A6WE 20050915001502005091500150NM 2005 9 15 SWAA052687 120050902A53206551698 SPLICE BOEING737 7375H4 138449DNM BS 360 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29503SW 24180 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER SPLICE CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20050915001522005091500152NM 2005 9 15 SWAA052689 120050902A3350BR2013 LIGHT BOEING737 7373Q8 1384670NM ROW 17 DEF LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 EEPLS TRACK LOOSE AT ROW 17 DEF. SECURED TRACK PER MM. 2L72 4F RTA16WE 20050915001582005091500158NM 2005 9 15 MASA200500502 120050628A213310306814 OUTFLOW VALVE DHAV DHC8 DHC8202 2809007NM CABIN PRESSURE FAILED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07455YV9766 455 ASH 7155 DEN. AIRCRAFT WILL NOT PRESSURIZE IN AUTO OR MANUAL. MX REMOVED AND REPLACED OUTFLOW VALVE. 2H72 4T RTA13NM 20050915001622005091500162EU 2005 9 15 RAIA00509008 120050908A3350 LIGHT JETAIRJETSTMJETSTM4101 1500501EU OVERWING INOPERATIVE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03574HK 41093 FLT 5468 - STL - ESCAPE PATH LIGHTING INOP AT ROWS 3-5 AND AT THE OVERWING EXIT. MAINTENANCE RESET POWER SYSTEMS. OPS CHECKED GOOD. 2L72 4T RTA41NM 20050915001682005091500168NE 2005 9 15 DLM90050472 220050821A7297242710071 TRU DOUG MD90 MD9030 3023690NM IAE V2528 V2528D5 NE NR 1 ENGINE FAILED A DALAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CLCLIMB 1 SO27916DN 53396 020084 APPROX 10 MINS AFTER T/O LEFT GENERATOR TRIPPED OFF LINE AND WOULD NOT RESET. APU WAS STARTED IAW PROCEDURE. LOSS OF CAPTS FLT DIRECTOR, NR 1 VOR, AND ALL ENGINE INSTRUMENTS WERE CONTINUALLY FLICKERING AND DISPLAYING ERRONEOUS DATA. GROUND PROXIMITY C/B WAS DISCOVERED POPPED AND WOULD NOT RESET. OAP SCREEN WOULD DISPLAY FLICKERING MESSAGES THAT WERE UNREADABLE. REPLACED TRU AND COOLING FAN. 2L72 4F4 FRTA6WE E40NE 20050915001732005091500173NM 2005 9 15 DL764050485 120050823A3350 CONNECTOR BOEING767 767432ER 1385134NM EMERGENCY LIGHT DISCONNECTED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27839MH 29712 FOUND EMERGENCY TRACK LIGHTS OUT BEHIND ROW 32CDE. FOUND CONNECTOR DISCONNECTED, RECONNECTED ALL, CHECKS NORMAL. 2L72 4F RTA1NM 20050915001782005091500178 2005 9 15 DL76L050491 420050827A2565233T42464 PANEL BOEING767 767332 1382001NM SLIDE INTERMITTENT A DALAK NONE L NO TEST ININSP/MAINT 1 SO27198DN 28455 LOWER EMERGENCY ESCAPE SLIDE SPOILER SQIB TEST INOP/INTERMITTENT. REPLACED PANEL. 2L72 4F RTA1NM 20050915001792005091500179NM 2005 9 15 DLM90050526 120050907A273059663091 CRANK ASSY DOUG MD90 MD9030 3023690NM LEFT PYLON FLAP CRACKED A DALAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 SO27911DA 53391 LEFT PYLON FLAP ACTUATOR CONTROL ROD BRACKET IPC27-51-00-35 ITEM 145 CRACKED AT SPLINE BOSS CLAMPING AREA RESULTING IN LOSS OF MOVEMENT OF LEFT PYLON FLAP PANEL. MFG P/N 5966309-1. REPLACED SAME. 2L72 4F RTA6WE 20050915001872005091500187NM 2005 9 15 DL757050539 120050912A3233 ACTUATOR BOEING757 757232 1384965NM NLG MALFUNCTIONED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27663DN NA 24992 AFTER RAISING GEAR HANDLE THE DOOR LIGHT REMAINED ILLUM AND GEAR DOORS MSG ON EICAS. FOUND INTERLOCK ACTUATOR INOP. REPLACED SAME. DOOR OPS NOW CHECKS GOOD. 2L72 4F RTA2NM 20050919000012005091900001WP 2005 9 19 05FDEA02895 120050914A7830 HINGE FITTING DOUG DC10 DC1010 3022110WP GE CF6 CF6* 30020GL THRUST REVERSER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568053 47807 NR 3 LT THRUST REVERSER CENTER HINGE SUPPORT EXTRUSION ON INSIDE OF PYLON IS CRACKED AT TOP.**S/D COMING** 2L73 4F4 F A22WE E23EA 20050919000042005091900004EU 2005 9 19 05FDEA02906 120050914A5321232TG FLOOR PANEL AIRBUS310 A310 EU GE CF6 CF680 30025NE CARGO DECK CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25425FE 264 MDCC FLOOR PANEL 232TG IS CRACKED. FABED NEW FLOOR PANEL. 2L72 4F4 FRTA35EU E13NE 20050919000072005091900007EU 2005 9 19 05FDEA02910 120050914A5321231TG FLOOR PANEL AIRBUS310 A310 EU GE CF6 CF680 30025NE CARGO DECK CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25425FE 264 MDCC FLOOR PANEL 231TG CRACKED. FABED NEW FLOOR PANEL. 2L72 4F4 FRTA35EU E13NE 20050919000102005091900010SW 2005 9 19 PNSA050903 120050906A5210 SEAL SWRNGNSA227 SA227AC 8780603SW PAX DOOR BLOWN A PNSAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 AL0341NE AC741B ON FLIGHT AT ALTITUDE CABIN PRESSURIZATION DUMPED. AIRCRAFT RETURNED TO DEPARTING AIRPORT AND LANDED UNEVENTFULLY. MX FOUND THAT PAX DOOR SEAL HAD BLOWNOUT, SEAL WAS REPLACED AND OPS CHECKED NORMAL. 2L72 4T RTA8SW 20050919000112005091900011NE 2005 9 19 ALGA105940 120050825A62207610308010049 HUB SKRSKYS76 S76A 8143006NE MAIN ROTOR CRACKED B ALGAK NONE O OTHER ININSP/MAINT 1 SW03705AL18043 760267 CRACKED DAMPER LUG / REPLACED WITH NEW HUB BY FIELD MAINTENANCE. 1G72 3U H1NE 20050919000222005091900022NM 2005 9 19 UPS05545414 120050914A2121 FAN BOEING757 75724APF 1384969NM COCKPIT FAILED A IPXAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO01466UP 25482 DIVERTED DUE TO SMOKE IN THE COCKPIT. SMELL DISSIPATED SLIGHTLY. SMELL MOS NOTICABLE ON 1ST OFFICERS SIDE AND LATER ALONG UPPER CIRCUIT BREAKER PANEL. FOUND NR 1 FLIGHT DECK EQUIPMENT COOLING FAN TO BE SOURCE OF SMELL. R/R IAW MM 21-58-23-4 SYSTEM OPS CK NORMAL 2L72 4F RTA2NM 20050919000242005091900024WP 2005 9 19 UPS05845411 120050903A5712 RIB DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE: C3, LT WING L/E UPPER RIB IS CRACKED AT XS 461.372. STOP DRILLED, FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 21.1.20D, 57-02-00 FIG 2, 57-03-03 FIG 5. 2L74 4F RT4A25 20050919000272005091900027WP 2005 9 19 UPS05845415 120050903A5712 RIB DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE:C2, LT WING L/E LOWER RIB IS CRACKED AT XFS 653.750. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-2-0, 5 1-1-20D AND 51-1-21. 2L74 4F RT4A25 20050919000312005091900031EA 2005 9 19 VTZA200500181 120050914A5320601R3111387 ANGLE CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27655BR 7457 LEFT 280 VERTICAL ANGLE IS CRACKED AT .5 INCH BETWEEN FASTENERS. 2L72 4F RTA21EA 20050919000442005091900044NM 2005 9 19 CALA0500309 120050914A5315147A5505 FLOORBEAM BOEING737 737724 13844BYNM STA 967 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2724702 28763 INSPECTION FOUND LITE CORROSION UNDER SCREW HOLES ON FLOORBEAM AT STA 967, LBL 30 TO RBL 30. REPAIRED FLOORBEAM IAW ECRA 5321-01291. 2L72 4F RTA16WE 20050919000472005091900047NM 2005 9 19 05FDEA02854 120050913A5320 SPLICE BOEING727 727200 138407ENM STRINGER CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION, FORWARD CARGO BAY ON STRINGER SPLICE 26 RT BS 680 (FWD I/B SIDE). REMOVED CORROSION ON STR SPLICE FOUND TO BE WITHIN LIMITS ALL WORK DONE IAW SRM 51-10-6, 53-10-01, 51-30-2. 2L73 4F RTA3WE 20050919000582005091900058NM 2005 9 19 DLM88050504 120050831A335041B004AD073 BATTERY DOUG MD88 MD88 3023688NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE O OTHER ININSP/MAINT 1 SO27918DL 49583 TAIL COMPARTMENT OVERHEAD EMERGENCY LIGHTS INOP. REPLACED B5-28 POWER SUPPLY BATTERIES, CHECKS GOOD. 2L72 4F RTA6WE 20050919000712005091900071NM 2005 9 19 DL757050525 120050908A5730NONE SKIN BOEING757 757232 1384965NM LT WING WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO27626DL 22916 WEAR DAMAGE WAS FOUND ON THE LEFT HAND SIDE LOWER WING SKIN CAUSED BY CONTACT WITH THE WING-TO-BODY FAIRING SKIN. THE DAMAGE WAS REPAIRED BY ACTS IN VANCOUVER PER ACTS PP B757-57-21136. 2L72 4F RTA2NM 20050919000722005091900072WP 2005 9 19 P9RA20050096 120050902A335060030451 POWER SUPPLY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INTERMITTENT A P9RAK NONE O OTHER ININSP/MAINT 1 SO11130NJ 49222 MAINTENANCE; SFB EMERGENCY LIGHTING INTERMITTENT IN COCKPIT AND MID CABIN. REMOVED AND REPLACED BATTERY POWER SUPPLIES PER M/M. OPS TESTED GOOD. PART INFORMATION FOR MID CABIN. PART, BATTERY POWER SUPPLY. PART NUMBER 60-0304-51. 2L72 4F A6WE 20050919000732005091900073NM 2005 9 19 05FDEA02872 120050914A5744 ATTACH FITTING DOUG MD11 MD11 3023602NM FLAP HINGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 RIGHT WING - O/B FLAP I/B HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08. 2L73 4F RTA22WE 20050919000842005091900084EA 2005 9 19 COMA0560494 120050911A5210 LATCH CNDAIRCL600 CL6002B19 1900309EA PAX DOOR MALFUNCTIONED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01812CA 7381 FLIGHT 5755 - DURING TAKEOFF ROLL RECEIVED A CABIN DOOR HANDLE CAUTION MESSAGE. ABORTED TAKEOFF AND RETURNED TO THE GATE. PERFORMED OPERATIONAL CHECK OF THE CABIN DOOR HANDLE MECHANISM, COULD NOT DUPLICATE DISCREPANCY. 2L72 4F RTA21EA 20050919000872005091900087EA 2005 9 19 SWIA200515540 120050912A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07916SW 7634 EMERGENCY EXTERIOR LIGHT JUST FORWARD LEFT WING BURNED OUT. RELAMPED SAME, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050919000882005091900088EA 2005 9 19 SWIA200515541 120050910A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07913SW 7597 LAST OVERHEAD EMERGENCY LIGHT INOP. REPLACED LAST OVERHEAD EMERGENCY LIGHT BULB, OPERATIONAL CHECK GOOD PER CRJ MM 33-51-16. 2L72 4F RTA21EA 20050919000902005091900090EA 2005 9 19 SWIA200515543 120050913A27604916420 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION LDLANDING 1 NM07465SW 7845 ON TOUCHDOWN, RECEIVED AN OUTBOARD GND SPOILERS CAUTION MESSAGE. REPLACED BOTH NR 1 AND NR 2 SECU IAW MM 27-61-05. OPERATIONAL CHECK GOOD. P/N OFF 49-164-20; S/N OFF 03112; S/N OFF 0817. 2L72 4F RTA21EA 20050919001012005091900101NM 2005 9 19 PIDA20050081 120050705A5320 CHANNEL BOEING737 737228 13844AGNM BS 1016-1030 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05237TR 23007 HAT CHANNEL FROM BS 1026 TO BS 1030 AT BL 0 IS CORRODED. REPLACED CHANNEL PER DWG 65-46816 AND SRM 51-10-1 AND SRM 51-30-0. 2L72 4F RTA16WE 20050919001202005091900120NM 2005 9 19 PIDA20050092 120050711A5320 INTERCOSTAL BOEING737 737228 13844AGNM BS 986-1006 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05237TR 23007 DIAGONAL INTERCOSTAL FROM BS 986 AT LBL 22 TO BS 1006 AT LBL 9 IS CORRODED. REPLACED INTERCOSTAL PER SRM 51-10-1. 2L72 4F RTA16WE 20050919001272005091900127NM 2005 9 19 05FDEA02856 120050913A5322 SHEAR TIE BOEING727 727200 138407ENM BS 720 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION, FORWARD CARGO BAY ON SHEAR TIE BETWEEN STRINGER 27 LT AND STRINGER 28 LT BS 720 (FWD SIDE OF FRAME). REPAIRED SHEAR TIE AT B.S. 720 BETWEEN STR 27L & 28L PER SRM 53-10-4. 2L73 4F RTA3WE 20050919001302005091900130EU 2005 9 19 05FDEA02853 120050913A5511 RIB AIRBUS310 A310203 3930313EU ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25425FE 264 LEFT HORIZONTAL L/E PANEL 331BB RIB NR 1 IS CRACKED AT UPPER AFT CORNER. 2L72 4F RTA35EU 20050919001362005091900136NM 2005 9 19 05FDEA02868 120050914A5744 ATTACH FITTING DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 RIGHT WING - O/B FLAP I/B HINGE (WING SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87638. 2L73 4F RTA22WE 20050919001442005091900144NM 2005 9 19 PIDA20050080 120050708A5320 PAN BOEING737 737228 13844AGNM BS 1016 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05237TR 23007 DRIP PANS AT BS 1016 HAVE CORROSION FROM LBL 45 TO RBL 45. REPLACED LEFT AND RIGHT DRIP PANS PER SRM 51-10-1 AND SRM 51-30-0. 2L72 4F RTA16WE 20050919001452005091900145NM 2005 9 19 PIDA20050071 120050708A5313 STRINGER BOEING737 737228 13844AGNM BS 967 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05237TR 23007 CORROSION ON STRINGER 25 LT JUST AFT OF BS 967 FRAME. REPAIRED PER 53-10-3. 2L72 4F RTA16WE 20050919001472005091900147NM 2005 9 19 PIDA20050082 120050628A5347 SEAT TRACK BOEING737 737228 13844AGNM BS 328-360 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05237TR 23007 SEAT TRACK AT RBL 52 HAS CORROSION ON FLANGES FROM BS 328 TO BS 360. REPLACED SECTION OF SEAT TRACK PER SRM 51-10-1 AND SRM 51-10-2. 2L72 4F RTA16WE 20050919001572005091900157NM 2005 9 19 SWAA052791 120050914A534065C27314 STRINGER CLIP BOEING737 7373L9 1384470NM BS 663 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050919001662005091900166WP 2005 9 19 ABXA050218 120050901A531199196191 FRAME DOUG DC9 DC932 3022066WP BS 718 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23900AX 47380 PREVIOUSLY REPAIRED LEFT WHEEL WELL MAIN FRAME 718 HAD SEPARATION IN PREVIOUS CRACKS WITH CORROSION INSIDE CRACKS. ALSO HAD CORROSION AROUND MAIN FRAME BOTTOM BOLT IN FORWARD FLANGE. REMOVED AND REPLACED MAIN FRAME STA 718 LEFT ON JOB CARD EA 53400323-001-2. 2L72 4F A6WE 20050919001682005091900168NM 2005 9 19 SB05114 120050915A2497BACC47DP4 CONNECTOR BOEING737 737401 1384701NM NR 2 ENGINE BURNED A USAAO OTHER H ELECT. POWER LOSS-50 PC CRCRUISE 1 EA19422US 23989 FLIGHT DEPARTED RDU WITH THE NR 1 ENGINE GENERATOR ON MEL 24-1. EN ROUTE CLT, THE NR 2 AND NR 3 TRANSFORMER RECTIFIER UNIT CIRCUIT BREAKERS TRIPPED. THE APU GENERATOR WAS UNABLE TO PICK UP THE RIGHT GENERATOR BUSS AS THE NR 2 ENGINE GENERATOR HAD TRIPPED OFF LINE WITH VOLTS AND FREQUENCIES INDICATING ZERO. FLIGHT LANDED SAFELY WITHOUT INCIDENT AT CLT. MAINTENANCE FOUND PIN -B- ON CONNECTOR D3026 BURNT CAUSING PHASE LOSS. REPLACED CONNECTOR D3026 PER SPWM 20-61-19. OPERATIONAL CHECK OF NR 2 GENERATOR, NR 2 AND NR 3 TRANSFORMER RECTIFIER UNITS AND APU CHECK NORMAL. CLEARED MEL 24-1 ON NR 1 ENGINE GENERATOR WITH THE REPLACEMENT OF THE NR 1 GENERATOR CONTROL UNIT AND A RESET OF THE NR 1 CSD. OPS CK GOOD. 2L72 4F RTA16WE 20050919001692005091900169WP 2005 9 19 UPS05845421 120050816A5311 SPAR DOUG DC8 DC871F 302199DWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 INSPECTION TYPE:C1 RIGHT KEEL BEAM AT FS 857 2.5 INCH CRACK ON LWR SPAR. STOP DRILLED CRACK AT XCW 4.0 IAW SRM 51-1-20D NDT HFEC IAW NDTSPM 06-10-01.001 NO CRACKS NOTED BEYOND STOP DRILL. FABRICATED FILLERS VERTICAL FILLERS AND -136 ANGLE AND STIFFENERS AND INSTALLED REPAIR PARTS IAW SAA SK 750-847317, UPS ENG FILE NUMBER DC8-57-20134 AND BOEING MESSAGE 1-116364542-2. 2L74 4F RT4A25 20050919001932005091900193SO 2005 9 19 SWIA200515552 120050603A5320 FLOOR SUPPORT EMB 120 EMB120ER 3260203SO CABIN CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07188SW 120039 CABIN FLOOR CENTER FORWARD OMEGA BEAM CORRODED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED CENTER FORWARD OMEGA BEAM IAW 120 SRM 51-10-02 PG 3 SEC 3A. 2L72 4T RTA31SO 20050919002002005091900200CE 2005 9 19 DXTA200500969 120050914A2910 LINE CESSNA650 650 2076802CE HYD SYSTEM BROKEN E DXTAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL07791QS 6507091 HYDRAULIC LINE IN RIGHT MAIN GEAR WELL BROKE AFTER T/O HAD TO BLOW GEAR DOWN AND USE ALL BACKUP SYSTEMS HAD RIGHT AND LEFT HYD LOW VOLUME AND PRESSURE LIGHTS. ITEM IS UNDER INVESTIGATION. 2L72 4F A9NM 20050919002042005091900204CE 2005 9 19 DXTA200500967 120050914A2612 FIRE LOOP CESSNA560 560XL 2076702CE LT ENGINE DIRTY E DXTAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL07625QS 5605319 LEFT FIRE DET SYSTEM INOP, LIGHT ON IN FLIGHT. VERIFIED SQWAWK, T/S SYSTEM BY SWAPPING LT & RT FIRE DETECT CONTROLS, NO HELP. REMOVED UPPER AND LOWER LT ENGINE COWLINGS. INSPECTED FIRE LOOP AND CHECKED RESISTANCE, FOUND WITHIN LIMITS. CHECKED SYSTEM WIRING, NO FAULTS FOUND. CLEANED ALL SYSTEM WIRING CONNECTORS AND FIRE LOOP CONNECTIONS. SYSTEM TEST GOOD IAW THE CE MM & WDM CHAP 26-10-01. RETURNED AIRCRAFT TO NORMAL. 2L72 4F RTA22CE 20050919002092005091900209EA 2005 9 19 SWIA200515550 120050825A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA BS 605 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07413SW 7102 FRAME FLANGE CRACKED AT FS 605 STR 9L - BELOW STRINGER CRACK EMINATING FROM TOP FASTENER HOLE ABOVE & BELOW. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FLANGE IAW CRJ REO 601R-53-61-1507. 2L72 4F RTA21EA 20050919002182005091900218EU 2005 9 19 RAIA00509020 120050913A3350 LIGHT JETAIRJETSTMJETSTM4101 1500501EU CABIN INOPERATIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03574HK 41093 FLT 5537-STL- FORWARD EMERGENCY LIGHTS IN FLOOR INOPERATIVE. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE LIGHTS WITH NO FAULTS FOUND. 2L72 4T RTA41NM 20050919002212005091900221SO 2005 9 19 RAIA00509018 120050912A7830 WARNING LIGHT EMB 145 EMB145 3260210SO THRUST REVERSER ILLUMINATED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03802HK 145066 FLT 3537-PIT- ENGINE 2 THRUST REVERSER DISAGREE MESSAGE IN FLIGHT. MAINTENANCE DEFERRED THE NR 2 THRUST REVERSER. 2L72 4F RTT00011AT 20050919002242005091900224NM 2005 9 19 UPS05245430 120050825A3220 FITTING BOEING727 72731C 1384011NM NLG TRUNNION CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01922UP 19231 INSPECTION TYPE:C CORROSION ON NLG TRUNNION FITTINGS LT AND RT. CORROSION REMOVED FROM LT & RT TRUNNION FITTINGS IAW SRM 53-40-01. NEW BUSHINGS FABRICATED AND INSTALLED IAW MM 53-40-01 AND 53-40-01 FIG 2. 2L73 4F A3WE 20050919002272005091900227NM 2005 9 19 UPS05245434 120050819A5320 STIFFENER BOEING727 72731C 1384011NM BS 870 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01922UP 19231 INSPECTION TYPE:C HORIZONTAL STIFFENER CORRODED IN CABIN AT BS 870 FWD SIDE, RBL 19. REPLACEMENT STIFFENER FABRICATE IAW SRM 51-20-10 AND DRAWING 65-23114. STIFFENER INSTALLED IAW SRM 51-30-02 AND DRAWING 65-16328. 2L73 4F A3WE 20050919002312005091900231NM 2005 9 19 UPS05245442 120050827A5710 SHEAR TIE BOEING727 72731C 1384011NM BS 740 LBL 25.08CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01922UP 19231 INSPECTION TYPE:C SUSPECT CRACK IN CENTER TANK FRONT SPAR TO STIFFENER SHEAR TIE CLIP O/B AFT RADIUS LBL 25-08. SHEAR TIE CLIP REPLACED IAW 51-30-02. 2L73 4F A3WE 20050920000072005092000007WP 2005 9 20 05FDEA02897 120050914A7830 ANGLE DOUG DC10 DC1010 3022110WP THRUST REVERSER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568053 47807 NR 3 ENGINE LT THRUST REVERSER CENTER HINGE SUPPORT EXTRUSION INSIDE PYLON IS CRACKED AT TOP REF: SNRM 798. REMOVED CRACKED HINGE SUPPORT. INSTALLED HINGE SUPPORT EXTRUSION AS REQ., REF SRM 51-31-01 (REF N/R N00798). 2L73 4F A22WE 20050920000092005092000009EU 2005 9 20 SF20050917 120050917A7931 WARNING LIGHT SAAB SF340 SF340A 7850100EU LT ENGINE ILLUMINATED A UHLAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL1735SZ 35 FLIGHT 7582 DAY-IAD, L OIL ENG PRESS ILLUMINATED ON CWP INTERMITTENTLY, ACCOMPANIED BY LEFT ENGINE OIL PRESSURE GAUGE FLUCTUATING APPROXIMATELY 30-50 PSI. AIRCRAFT DIVERTED TO PIT. INSPECTED NR 1 ENGINE AND SERVICED WITH 2.5 QTS OIL. GROUND RAN, NO LEAKS NOTED. 2L72 4T RTA52EU 20050920000122005092000012NM 2005 9 20 05FDEA02937 120050916A5713 STRINGER DOUG MD11 MD11 3023602NM LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 HFEC CARRIED OUT AND CRACK FOUND ON LT WING AT S-40 STRINGER END WITH LENGTH OF APPROX 7 1/2" BY ACCESS FROM FUEL TANK CUTOUT 537AB. REPAIRED AS PER SRM 57-20-00 FIG.10 VOL I. REPAIR CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20050920000132005092000013NM 2005 9 20 05FDEA02938 120050916A5713 STRINGER DOUG MD11 MD11 3023602NM LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 HFEC CARRIED OUT AND CRACK FOUND ON LT WING AT S-11 STRINGER END WITH LENGTH OF APPROX 11" BY ACCESS FROM FUEL TANK CUTOUT 536AB. LT WING FUEL TANK 537AB CUTOUT AT S-11 CRACK STRINGER REPAIRED AS PER SRM 57-20-00 FIG.10 VOL.I. CLASSIFIED MAJOR REPAIR PER GMM 6-2-100. 2L73 4F RTA22WE 20050920000242005092000024 2005 9 20 SWAA052819 420050917A2565D31354 SLIDE BOEING737 7375H4 138449DNM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29525SW 26567 DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050920000372005092000037NM 2005 9 20 SWAA052832 120050916A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 578 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 578, STR 11R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050920000382005092000038NM 2005 9 20 05FDEA02943 120050916A5713 STRINGER DOUG MD11 MD11 3023602NM LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 LT WING UPPER STRINGER NR 13 FOUND CRACK (APPROX. 11.5" LONG) ON THE STRINGER OUTBOARD END RADIUS AREA. SNRM N1427: LH WING UPPER STRINGER #13 ON THE STRINGER OUTBOARD END RADIUS CRACK. STRINGER REPAIRED AS PER SRM 57-20-00 FIG.10 VOL.I. MAJOR REPAIR PER GMM 6-2-100. CLIP REPLACED IAW EA#1-5720-87702 TITLE: WINGS- OUTER WING- STRINGER REPAIR/CLIP FABRICATION. 2L73 4F RTA22WE 20050920000402005092000040NM 2005 9 20 05FDEA02945 120050916A5320 INTERCOSTAL DOUG MD11 MD11 3023602NM BS 1900 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 MAIN DECK, AFT CABIN AT STA 1900 LT INTERCOSTAL AT LONGERON 13L FOUND CRACKED FROM FASTENER HOLES. REMOVED AND FABRICATED FROM 7075.0.0.063" AS PER DRAWING NFA 6374. FABRICATED INTERCOSTAL REPROTECTED, PART MARK AND INSTALLED AS PER SRM 51-33-01 VOL.II. CLASSIFIED MINOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050920000512005092000051EA 2005 9 20 ASOA05666 120050815A2120 ODOR CNDAIRCL600 CL6002B19 1900309EA CABIN DETECTED A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SO11846AS 7328 DURING TAKEOFF, THE CREW NOTICED A STRONG ODOR COMING FROM THE AIR CONDITIONING PACKS IN THE COCKPIT. UPON CHECKING THE ENVIRONMENTAL CONTROL SYSTEM PAGE THE CREW NOTED THE BLEED LINE WAS APPROX 110 PSI WITH ALL OTHER INDICATIONS IN THE NORMAL RANGE. AS THE FLIGHT CONTINUED, THE BLEED LINE PSI RETURNED TO THE NORMAL RANGE AND THE ODOR DISSIPATED. THE ODOR RETURNED WHEN POWER WAS REDUCED FOR DESCENT. THE AIRCRAFT LANDED SAFELY. MAINTENANCE DEFERRED THE CABIN/COCKPIT TEMPERATURE CONTROL SYSTEM LT PACK AUTO MODE UNDER MEL NR 21-61-01-01-A, CAT C EXPIRING 8/25/2005. 2L72 4F RTA21EA 20050920000772005092000077NM 2005 9 20 05FDEA02877 120050914A5313 LONGERON DOUG MD11 MD11 3023602NM BS 1139-1159 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 CAC COMPT BETWEEN STA 1139 AND STA 1159, LONGERON 51L CORRODED. REMOVED AND NEW SPLICE INSTALLED AS PER SRM 51-31-01 VOL.II, SRM 51-33-01 VOL.II SRM 51-35-01 VOL.II AND DRAWING AAA 7086. NEW SPLICE PART. NR AAA 7086-1 FABRICATED PER DRAWING AAA 7086. MINOR REPAIR PER GMM 6-2-100. 2L73 4F RTA22WE 20050920000792005092000079NM 2005 9 20 05FDEA02879 120050914A5744 ATTACH FITTING DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 RT WING, O/B FLAP O/B HINGE (WING SIDE), SIDE LINK ATTACHMENT BARREL NUT BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87641. 2L73 4F RTA22WE 20050920000812005092000081NM 2005 9 20 05FDEA02880 120050914A5744 ATTACH FITTING DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 RT WING, O/B FLAP O/B HINGE (WING SIDE), SIDE LINK ATTACHMENT UPPER FWD BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87641. 2L73 4F RTA22WE 20050920000822005092000082WP 2005 9 20 05FDEA02863 120050914A5330 SKIN DOUG DC10 DC1010 3022110WP BS 555 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25571FE 47830 DURING AIRPLANE'S CONVERSION FROM P TO F FOUND DENT ON UPPER SKIN FUSELAGE AT STA 555 REF LONGERON 26 RT, DENT DIMENSION 2.0 X 2.0, 0.06 THICK. REWORKED DENT AREA IAW SRM 53-20-00 FIG 13. DYE CHECK FOR CRACK AND INSTALLED INT REPAIR DOUBLER IAW SRM 53-70-00 FIG 13. 2L73 4F A22WE 20050920000842005092000084NM 2005 9 20 05FDEA02873 120050914A5744 ATTACH FITTING DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 RT WING, O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87641. 2L73 4F RTA22WE 20050920000862005092000086NM 2005 9 20 05FDEA02875 120050914A5744 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 RT WING, O/B FLAP O/B HINGE (WING SIDE) PIVOT BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87641. 2L73 4F RTA22WE 20050920000882005092000088NM 2005 9 20 SWAA052794 120050915A5315BAC1509 FLOORBEAM BOEING737 7373H4 1384600NM BS 773 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 773, RBL 3 & RBL 14. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20050920000902005092000090NM 2005 9 20 SWAA052796 120050915A531065C26402 CREASE BEAM BOEING737 7373H4 1384600NM BS 727D-727E CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 DURING SCHEDULED D-CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 727D TO BS 727E. REPAIRED CREASE BEAM WEB SECTION PER SRM. 2L72 4F RTA16WE 20050920000922005092000092NM 2005 9 20 SWAA052798 120050915A53116546550 FRAME BOEING737 7373H4 1384600NM BS 787 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L & STR 8R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050920000942005092000094NM 2005 9 20 SWAA052800 120050915A531165C25228 FRAME BOEING737 7373H4 1384600NM BS 727D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8L & STR 8R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050920000962005092000096NM 2005 9 20 SWAA052802 120050915A53116546558 FRAME BOEING737 7373H4 1384600NM BS 907 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R TO STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050920001112005092000111EU 2005 9 20 MALA050714 120050902A2913521449 PUMP BAC 146 AVRO146RJ85A1500097EU HYD SYSTEM FAILED A MALAO OTHER M OVER TEMP NRNOT REPORTED 1 GL15531XJ E2365 CREW SENT ACARS ABOUT LOSING GREEN HYD SYS. RESPONDED BY SAYING YELLOW HYD SYS HOT. DECLARED EMERG & LANDED. REPLACED NR 3 ENG EDP & C/W FCA29004. NO LEAKS NOTED. PERFORMED GREEN HYD SYS CHECK FOR 50 MIN. NO DEFECTS NOTED. DISC NR 1 FOR GREEN SYS HIGH TEMP. DISC NR 2 REPLACE NR 3 ENG EDP FOR T/S OF GREEN SYS HIGH TEMP. R & R NR 3 EDP. LEAKS CHK GOOD. GREEN HYD TEMP LOWER. REPLACED AC HYD PUMP & COMPLETED, NO LEAKS NOTED. PERFORMED YELLOW HYD SYS CHK FOR 50 MIN. NO DEFECTS NOTED. NR 1 COMPLETE FOR YELLOW HI TEMP. DISC NR 2 COMPLETE FOR YELLOW HI TEMP. DISC NR 3 REPLACED AC HYD PUMP FOR T/S YELLOW HYD HIGH TEMP. REPLACED AC HYD PUMP ASSY REF AMM 29-20-11, NO LEAKS NOTED. DISC NR 4. HYD TEMP LOWER.2H74 4F RTA49EU 20050920001132005092000113EU 2005 9 20 N81KA5205 120050502A2910SA7670042020 LINE BRAERODH125 HS125700B 1500205EU HYDRAULIC SYS RUPTURED E KKYAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 NE0381KA 15009484 0307 ON T/O FROM OXC, WITH 0 PAXS, PILOTS ALERTED TO A LOSS OF HYD PRESSURE. INDICATING & HYD SYS CHECKED, & CONFIRMED SYS LOSS OF PRESSURE HAD OCCURRED. A/C RETURNED TO OXC FOLLOWING AFM PROCEDURES. VISUAL INSPECT REVEALED LT ENG COWL WET WITH HYD FLUID. MX ESTABLISHED LT ENG HYD PUMP PRESSURE HOSE RUPTURED. A REVIEW OF A/C RECORDS INDICATED SUBJECT HOSE HAD NOT BEEN REPLACED SINCE 1978, AS WELL A PROTECTIVE FIRE SHEATH COVERING POINT THAT RUPTURED PRECLUDED THAT A VISUAL INSPECT WOULD HAVE FORETOLD AN IMPENDING FAILURE. AS A PRECAUTION, SUCTION HOSE & CASE DRAIN HOSE ASSY REPLACED. SYS FLUSHED & SERVICED, BOTH HYD PUMPS WERE REPLACED. A/C JACKED & AN OPS CHK OF HYD SYS CONDUCTED WITH NO ABNORMALITIES. 2L72 4F A3EU 20050920001802005092000180NM 2005 9 20 SWAA052806 120050916A53306545776 SKIN BOEING737 7373H4 1384600NM BS 934 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29325SW 23689 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 934, STR 24L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050920001822005092000182NM 2005 9 20 SWAA052808 120050918A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 787 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 787, STR 21R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050920001842005092000184NM 2005 9 20 SWAA052810 120050918A53306545765 SKIN BOEING737 7373H4 1384600NM BS 510D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29349SW 24408 DURING WALKAROUND INSP, FOUND FUSELAGE SKIN CRACKED AT BS 510D, STR 16L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050920001862005092000186NM 2005 9 20 SWAA052812 120050916A33506104789 BATTERY PACK BOEING737 7373H4 1384600NM FWD GALLEY FAILED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29352SW 24888 DURING SCHEDULED SERVICE CHECK, L1 & R1 DOOR EMERGENCY EXIT SIGNS BATTERY PACK FAILED TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050920001892005092000189EU 2005 9 20 EM05011 120050918A2150 A/C PACK EMB ERJ170ERJ170100 EU NR 1 SMOKE A USAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA19817MD 000038 FLIGHT 1675, PHL TO ORD - THE CREW REPORTED SMOKE IN THE COCKPIT AND CABIN. ACCOMPLISHED QRH SMOKE/FUMES, LANDED AT DESTINATION ORD (NEAREST SUITABLE AIRPORT). THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. PRIOR EVENT ON 9/9/05. MAINTENANCE PERFORMED PACK NR 1 AND NR 2 OPERATION TEST. PACK NR 1 FAILED AND REPRODUCED SMOKE IN COCKPIT. AC RELEASED ON MEL. MAINTENANCE TROUBLESHOOTING FOR FURTHER ACTION, AC ON ETR. 2L74 4F RTA56NM 20050920001912005092000191NM 2005 9 20 BB05080 120050917A335020121 POWER SUPPLY BOEING767 7672B7 1385107NM EMERGENCY LIGHT UNSERVICEABLE A USAAK NONE O OTHER ININSP/MAINT 1 EA19656US 26847 SNN DURING DAILY CHECK, MAINTENANCE FOUND THE FORWARD LEFT-HAND EMERGENCY PACK INOPERATIVE. MAINTENANCE PERFORMED TROUBLESHOOTING AND FOUND THE POWER SUPPLY AT THE FORWARD LEFT-HAND POSITION UNSERVICEABLE. REPLACED POWER SUPPLY PER MM 33-51-07-02. OPERATIONAL CHECK GOOD. 2L72 4F RTA1NM 20050920001942005092000194SW 2005 9 20 ALG2005F00061 120050825A6220407310104105 SPRING BELL 407 407 1182206SW ALLSN 250C 250C47B GL FRAHM FAILED E ALGAO OTHER E VIBRATION/BUFFET CRCRUISE 1 SW03537AL 53230 AIRCRAFT DEVELOPED A VERTICAL VIBRATION IN FLIGHT. NOTIFIED MAINTENANCE. FRAHM DAMPER SPRING HAD FAILED. REMOVED AND INSTALLED FOUR NEW FRAHM DAMPER SPRINGS IAW MM. (K) 1G71 3U3 UO H2SW E1GL 20050920001962005092000196NM 2005 9 20 UIEA200500124 120050831A542065B9414197 SUPPORT BOEING747 7472D7B 1384803NM GE CF6 CF650E2 30018NE NR 2 PYLON CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15524MC 21784 D-CHECK, NR 2 PYLON, RT LWR AFT SKIRT FAIRING LOWER STIFFENER CRACKED. STOPPED DRILLED THE CRACK. NDT AND HFEC INSPECTED ALL AFFECTED FASTENER HOLES AND REPAIR AREA TO ENSURE CRACKS AND DAMAGE FREE CONDITION. FABRICATED AND INSTALLED 0.050 INCH THICK REPAIR CHANNEL. EO ISSUED TO ACCOMPLISHED A DETAIL VISUAL INSPECTION OF THE REPAIR AREA EVERY C-CHECK OR 18 MONTHS WHICHEVER IS EARLIER FOR DEGRADATION OF THE REPAIR INCLUDING CRACKS OR LOOSE FASTENERS. (K) 2L74 4F4 FRTA20WE E23EA 20050920001972005092000197EA 2005 9 20 ASOA05681 120050820A5340 FITTING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE BS 461 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27839AS 7284 DURING A C-CHECK, THE FITTING UNDER THE FLOOR AT FS 461, RBL 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FITTING UNDER THE FLOOR AT FS 461, RBL 9. (K) 2L72 4F4 FRTA21EA E15NE 20050920001992005092000199CE 2005 9 20 S2Y2005F00000 120050722A32601013645789 PCB BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA MLG SHORTED A S2YAO OTHER N FALSE WARNING APAPPROACH 1 GL13891SK849 849 UE89 DURING APPROACH, THE CREW DID NOT RECEIVE THE DOWN AND LOCK INDICATION FOR THE NOSE LANDING GEAR. THE CREW ALSO NOTED A SMOKE ODOR IN THE COCKPIT. THE CREW MADE A SAFE LANDING. MAINTENANCE INSPECTED THE SYSTEM AND FOUND BOTH THE ANNUNCIATOR FAULT DETECT PCB AND THE ANNUNCIATOR CONTROL PCB HAD SHORTS. MAINTENANCE REPLACED BOTH PCB AND OPS CHECKED THE SYSTEM WITH NO FURTHER DEFECTS NOTED. (K) 2L72 4T3 TRTA24CE E2NE 20050920002002005092000200NM 2005 9 20 USAA051028 120050817A5322US65458053LF SHEAR TIE BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU BS 277 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19444US40668 24862 BFM - Q2 - SHEAR TIE CLIP, .050 INCH CRACKED, STA 277, STR 8L TO 9L SHEAR TIE CLIP. INSTALLED REPAIR PART, SHEAR CLIP, STA 277 IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050920002012005092000201NM 2005 9 20 USAA051030 120050819A5414 SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU PYLON DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US50585 23933 CLT - Q6 - PYLON SKIN, 1.3 INCH, GROOVE IB SIDE OF NR 2 ENGINE PYLON AT WING L/E JUNCTION. REPAIRED IAW TYPICAL REPAIR IAW TR. (K) 2L72 4F4 FRTA16WE E21EU 20050920002032005092000203NM 2005 9 20 USAA051025 120050817A5340US69366002LF STRINGER CLIP BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU BS 277 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19444US40668 24862 BFM - Q2 - STRINGER CLIP, .250 INCH CRACK, STA 277; STR 9 L STR CLIP. INSTALLED REPAIR STRINGER CLIP STA 907 IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050920002052005092000205EA 2005 9 20 ASOA05687 120050820A5330 DOUBLER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE BS 508 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27839AS 7284 DURING A C-CHECK, THE DOUBLER AT FS 508, RBL 44 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO MFG FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. (K) S/D - MAINTENANCE REMOVED THE CORROSION FROM THE DOUBLER AT FS 508, RBL 44 BY COMPLYING WITH ASA EO 600-53-0313. (M) 2L72 4F4 FRTA21EA E15NE 20050920002062005092000206NM 2005 9 20 USAA050995 120050809A5313 STRINGER BOEING757 757225 1384959NM RROYCERB211 RB211535E4 54555NE BS 1340 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19608AU 22204 CLT - RON - STRINGER, 3 INCH, CORROSION, FASTENER PULLED AND SKIN BULGING STA 1340, STRINGER 27R. INSTALLED NEW SECTION OF STR IAW SRM AND EA. (K) 2L72 4F4 FRTA2NM E12EU 20050920002072005092000207NM 2005 9 20 USAA051012 120050817A5313 STRINGER BOEING757 757225 1384959NM RROYCERB211 RB211535E4 54555NE BS 1320 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19600AU 22192 CLT - RON - STRINGER, 6.75 INCH X 1 INCH CORROSION, NO CORROSION LEVEL, STA 1320, STR 30L. REMOVED DAMAGED STRINGER SECTION, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM. (K) 2L72 4F4 FRTA2NM E12EU 20050920002092005092000209GL 2005 9 20 ALG2005F00067 220050813A7230 ENGINE BELL 407 407 1182206SW ALLSN 250C 250C47B GL FOD E ALGAA UNSCHED LANDING EF VIBRATION/BUFFET FLT CONT AFFECTED CLCLIMB 1 SW03697AL 53374 CAE84212 ON TAKE OFF, HIGH PITCH WHINE WAS NOTED. NOTIFIED MAINTENANCE. INSPECTED ENGINE AND FOUND COMPRESSOR FOD DAMAGE. REMOVED AND REPLACED ENGINE ASSY. GROUND RUN, VIBRATION CHECK, AND LEAK CHECK ALL GOOD. WORK IAW MM. (K) 1G71 3U3 UO H2SW E1GL 20050920002102005092000210NM 2005 9 20 USAA051004 120050815A5340 BRACKET BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU BS 360 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19449US41152 24893 CLT - Q1 - BRACKET, 1 INCH, CRACK, STA 360, STR 7L BRACKET. REMOVED DAMAGED BRAKET, FRABRICATED NEW BRACKET AND INSTALLED, ISW SRM AND DWG. (K) 2L72 4F4 FRTA16WE E21EU 20050920002112005092000211SW 2005 9 20 ALG2005F00068 120050813A6340214040805001 SWITCH BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL XMSN TEMP FAILED E ALGAO OTHER J WARNING INDICATION CRCRUISE 1 SW03116AL 2389 ON INBOUND FLIGHT, TRANSMISSION TEMPERATURE LIGHT ILLUMINATED. TRANSMISSION TEMPERATURE GAUGE REMAINED NORMAL. MAINTENANCE NOTIFIED. REMOVED AND REPLACED TEMPERATURE SWITCH. LEAK CHECK AND GROUND RUN C/W, NO DEFECTS NOTED. ALL WORK IAW MM. (K) 1G71 3U3 U H2SW E4CE 20050920002132005092000213NM 2005 9 20 USAA051005 120050815A5512 SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU HORIZONTAL STAB CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US50585 23933 CLT - Q6 - LOWER SKIN, 1.7 INCH CRACK LOWER SKIN APPROX STAB STA 129 AT AFT SPAR, HORIZONTAL STAB. REPAIRED AND INSTALLED DOUBLER AND FILLER IAW EA. (K) 2L72 4F4 FRTA16WE E21EU 20050920002152005092000215NM 2005 9 20 USAA051022 120050817A5311 FRAME BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU BS 500 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19444US40668 24862 BFM - Q2 - FLAME, 2.45 INCH LT, CRACKED FWD CARGO FRAME BS 500 BL 0. TRIM OUT CRACK, FAB REPAIR, INSTALLED DOUBLER IAW EA. (K) 2L72 4F4 FRTA16WE E21EU 20050920002162005092000216NE 2005 9 20 ALG2005F00070 120050810A261265901204103 RELAY SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL FIRE WARNING INOPERATIVE E ALGAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 SW03917QS 760217 DURING THE START PROCEDURE, THE TRANSMISSION FIRE LIGHT AND HORN ACTIVATED. MAINTENANCE WAS NOTIFIED. THE K3 RELAY WAS REMOVED AND REPLACED. AC GROUND CHECKED GOOD. ALL WORK IAW MM. (K) 1G72 3U3 U H1NE E1GL 20050920002182005092000218EA 2005 9 20 ASOA05680 120050820A5210601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27850AS 7355 DURING A GROUND INSPECTION, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050920002212005092000221CE 2005 9 20 ALG2005F00062 120050825A2821174364502 FUEL FILTER CESSNASTC STC206C 1182107CE ALLSN 250C 250C28B 03013GL FUEL SYSTEM DAMAGED E ALGAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW0341GH 45502 ON TAKEOFF FUEL FILTER LIGHT ILLUMINATED. NOTIFIED MAINTENANCE. REMOVED FUEL FILTER AND FOUND FILTER DARKENED APPROXIMATELY 50 PERCENT. NO SEDIMENT IN BOWL. NO CONTAMINATES WERE FOUND IN THE AIRCRAFT FUEL SAMPLE. INSTALLED NEW FUEL FILTER, BLED SYSTEM, C/W GROUND RUN LEAK CHECK AND AFTER FUEL SYSTEM MAINTENANCE CHECK. NO DEFECTS NOTED. IAW MM. OPS CHECK FLT GOOD. (K) 1H71 3O3 UNTA4CE E1GL 20050920002232005092000223EA 2005 9 20 ASOA05684 120050820A5330 DOUBLER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE BS 470 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27839AS 7284 DURING C-CHECK, THE DOUBLER AT FS 470, RBL 34-44 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO MFG FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. (K) S/D - MAINTENANCE REMOVED THE CORROSION FROM THE DOUBLER AT FS 470, RBL 34-44 BY COMPLYING WITH ASA EO 600-53-0313. (M) 2L72 4F4 FRTA21EA E15NE 20050920002242005092000224SO 2005 9 20 IMD2005F00000 220050829A8550CH481081 OIL FILTER CESSNA414 414A 2075907CE CONT O520 TSIO520NB 17040SO RT ENGINE LEAKING E IMDAO OTHER K FLUID LOSS NRNOT REPORTED 1 NE05245DC7 414A0613 PILOT REPORTED FINDING AN OIL LEAK ON RT ENGINE DURING PREFLIGHT. ENGINE WASHED AND RUN, OIL FILTER FOUND CRACKED AND LEAKING AT THE WRENCH LUG FLANGE ON TOP OF THE FILTER. FILTER APPEARED TO BE OVERTORQUED UPON REMOVAL. FILTER RETAINED FOR WARRANTY AND QUALITY INSPECTION BY INSTALLER OR MFG. (K) 1L72 3O3 O A7CE E8CE 20050920002252005092000225EA 2005 9 20 A6WA200540298 120050906A5340 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE BS 621 CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31424AW 7656 LT FS621.0 FLOOR SUPPORT ANGLE HAS A 1 INCH CRACK. MAINTENANCE CUT OUT AND REMOVED DAMAGED ANGLE AT FS 621 LT FITTED AND DRILLED NEW ANGLES AND STRAP AND INSTALLED IAW REO. (K) 2L72 4F4 FRTA21EA E15NE 20050921000012005092100001NM 2005 9 21 P9RA20050097 120050828A3350608884 CONNECTOR BOEING757 757231 1384950NM EMERGENCY LIGHT CONTAMINATED A P9RAK NONE L NO TEST ININSP/MAINT 1 SO11715TW 28483 SFB FORWARD EMERGENCY LIGHTS INOP IN FIRST CLASS CABIN. FOUND MOISTURE IN SEVERAL LIGHT STRIP HOOK UP POINTS. CLEANED CONTACTS. OPS CHECKED GOOD PER MM. NO PART REPLACEMENT AT THIS TIME. 2L72 4F RTA2NM 20050921000032005092100003EU 2005 9 21 2005UALA00987 120050916A5330 SKIN AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29404UA 450 FUSELAGE SKIN IN AREA AROUND DOOR 2L IS DAMAGED. REPAIRED AREA AROUND DOOR 2L WITH DOUBLER PER SRM 53-00-11 PR 313-314. 2L72 4F4 FRTA28NM E40NE 20050921000042005092100004EU 2005 9 21 2005UALA00988 120050915A3350 LIGHT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29430UA 568 EMERGENCY LIGHT TEST FAILED FWD BATTERY LEFT AND COM EMERGENCY AFT L. REPLACED ENERGECY POWER-SUPPLY UNIT 10WL. 2L72 4F4 FRTA28NM E40NE 20050921000052005092100005NM 2005 9 21 2005UALA00989 120050915A2611 WARNING LIGHT AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE CARGO SMOKE ILLUMINATED A UALAFA ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CRCRUISE 1 WP29855UA 1737 CREW REPORTS SMOKE WARNING FOR AFT CARGO PIT. NTERROGATED SYSTEM AND UNABLE TO VERIFY FAULT FOR AFT CARGO COMPARTMENT SMOKE DETECTION. REPLACED SDU PER AMM 26-17-34. REPLACED AFT CARGO COMPARTMENT SMOKE DETECTOR PER AMM 26-16-15. REPLACED AFT CARGO FIRE BOTTLE AND SQUIB AS REQUIRED. 2L72 4F4 FRTA28NM E40NE 20050921000062005092100006NM 2005 9 21 2005UALA00990 120050916A3350 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29127UA 28813 EMERGENCY LIGHT INOP DR3L SILL. REPLACED LAMP. 2L74 4F4 FRTA20WE E24NE 20050921000072005092100007NM 2005 9 21 2005UALA00991 120050916A3350 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE ROW 58 INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29127UA 28813 EMERGENCY LIGHT INOP ROW 58 LEFT CEILING AND ROW 13 LEFT CEILING. REPLACED LAMP. 2L74 4F4 FRTA20WE E24NE 20050921000092005092100009NM 2005 9 21 2005UALA00993 120050916A2120 DUCT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN BURNED A UALAJHA DUMP FUEL DEACTIVATE SYST/CIRCUITSUNSCHED LANDING MB OVER TEMP SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP29182UA 25279 WALL/FLOOR ON LEFT SIDE OF ACFT BY ROW 24 WAS EXTREMELY HOT WITH A BURNING SMELL. DUCT ASSEMBLY SIDEWALL RISER P/N 214U2119-11 FOR ZONE C WAS FOUND WITH HEAT DAMAGE AT THE HOT TRIM AIR INLET INTERFACE (STA 1153.66). THE DUCT ASSY EXHIBITED A DARK BROWN COLOR WITH SIGNIFICANT STRUCTURAL DAMAGE TO THE LOWER SECTION, ADJACENT TO THE CONNECTION TO THE UNDERFLOOR TRIM AIR DUCT ASSY P/N 213U2107-7. THE DAMAGE WHICH INCLUDES A LARGE HOLE, APPEARS TO BE INITIATED AT THE TRANSITION POINT WHERE THE FLOW CHANGES DIRECTION (SMOOTH CURVATURE). IN ADDITION, DURING REMOVAL OF JOINT ASSY P/N CF15-250, SLEEVE P/N 24098-250 WAS FOUND BROKEN IN PIECES. 2L74 4F4 FRTA20WE E24NE 20050921000102005092100010 2005 9 21 QXEA200501235 420050917A2340 HANDSET DHAV DHC8 DHC8202 2809007NM CABIN INOPERATIVE A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09350PH 488 SEA FLIGHT NR 2174, FLIGHT ATTENDANT TELEPHONE INOP, CAN'T CALL COCKPIT OR MAKE PA. MAINTENANCE REPLACED FLIGHT ATTENDANT HANDSET PER Q200 AMM 23-40-03, PAGES 401-405. OPERATIONAL CHECK PER TASK 23-40-00-710-801. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050921000112005092100011NM 2005 9 21 QXEA200501236 120050916A2997 WIRE DHAV DHC8 DHC8202 2809007NM PRESSURE XMITTERBROKEN A QXEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM09362PH 518 SEA FLIGHT NR 2203, NR 2 HYDRAULIC MAIN PRESSURE READ ZERO FOR FIFTEEN MINUTES. MAINTENANCE REPAIRED BROKEN WIRE AT CONNECTOR 2932-P5 (PRESSURE TRANSMITTER FOR NR 2 MAIN HYDRAULIC SYSTEM) IAW AMM 20-45-03 AND 20-45-90 (Q200). GROUND RAN NR 2 ENGINE AND NR 2 HYDRAULIC MAIN PRESSURE CHECK NORMAL ON NR 2 HYDRAULIC PRESSURE INDICATOR. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050921000122005092100012 2005 9 21 QXEA200501237 420050918A34257003110901 EADI DHAV DHC8 DHC8202 2809007NM COCKPIT MALFUNCTIONED A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09366PH1461615 510 SEA FLIGHT NR 2084, ON TAXI OUT, FIRST OFFICER'S ADI SHOWED FIVE DEGREES DOWN PITCH AND FIVE DEGREES RIGHT TURN. ALSO, PITCH/ROLL MISMATCH ON ADVISORY DISPLAY. MAINTENANCE REPLACED FIRST OFFICER'S EADI IAW MTC 9340015. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050921000132005092100013EA 2005 9 21 MASA200500527 120050707A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA MAIN PAX STIFF A MASAO OTHER O OTHER APAPPROACH 1 SW0727172 7172 ASH 2685 ROA. MAIN PAX DOOR DIFFICULT TO OPEN ON ARRIVAL TO PHL. MX PERFORMED OPS CHECK OF DOOR PRESSURIZED CABIN AND COULD NOT DUPLICATE THE DISCREPANCY, ACFT CONTINUED OPERATIONS. 2L72 4F RTA21EA 20050921000142005092100014NM 2005 9 21 05FDEA02953 120050916A5330 SKIN BOEING727 727233 138408ANM BS 1191-1203 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25268FE 21674 WHILE WORKING N00667, FOUND EXTERNAL SKIN REPAIR AT BS 1191 - 1203 AT STR 23 RT TO HAVE INSUFFICIENT ROWS OF FASTENERS AT UPPER AFT CORNER OF REPAIR DOUBLER. REPAIRED PER SRM 53-30-3. 2L73 4F RTA3WE 20050921000172005092100017EA 2005 9 21 MASA200500540 120050710A7720 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA RT ENGINE FALSE INDICATIONA MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW0727185 7185 ASH 2615 MSP. RT ENGINE OVERTEMP ON T/O ROLL. ENGINE FOUND TO BE OPERATING WITHIN LIMITS. 2L72 4F RTA21EA 20050921000192005092100019EA 2005 9 21 MASA200500640 120050812A3510 OXYGEN MASK CNDAIRCL600 CL6002B19 1900309EA ROW 6 DEPLOYED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0727172 7172 ASH 2677 GRR. OXYGEN MASK THAT DROPPED WITH OUT COMMAND IN ROW 6. MX SECURED MASK. 2L72 4F RTA21EA 20050921000222005092100022NM 2005 9 21 2005UALA00963 120050909A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE BS 540 STR 19R DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29505UA 24626 SKIN DENTED STA 540, STR 19R. TRIMMED OUT DAMAGE AND ACCOMP INSURANCE CUT. INSTALLED FILLERS AND DOUBLER. 2L72 4F4 FRTA2NM E17NE 20050921000242005092100024NM 2005 9 21 2005UALA00965 120050909A5330 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE BS 1500 DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29505UA 24626 AFT PIT FRAME IS DENTED AT STA 1500 & STR 25L. TRIMMED DAMAGE, INSURANCE CUT, HECT VERIFY NO CRACKS. FAB NEW PRODUCTION SPLICE, AND INSTALLED WITH REPAIR ANGLE AND NEW STR CLIPS. 2L72 4F4 FRTA2NM E17NE 20050921000262005092100026NM 2005 9 21 2005UALA00967 120050909A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE BS 1400 DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29505UA 24626 AFT PIT FRAME DENTED STA 1400 AT STR 25L. TRIMMED OUT DAMAGE, INSURANCE CUT, HFEC INSP, FABBED J-ANGLE REPAIR AND INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050921000282005092100028NM 2005 9 21 2005UALA00969 120050909A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE BS 540 DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29505UA 24626 FWD PIT FRAME IS DENTED AT STA 540, STR 24L TO 26L. TRIMMED OUT DAMAGE AND INSURANCE CUT, FABBED NEW SPLICE AND REPAIR ANGLE AND INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050921000302005092100030NM 2005 9 21 2005UALA00971 120050910A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE BS 620 DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29505UA 24626 FWD PIT FRAME IS DENTED 2 PLACES AT STA 620 BETWEEN STR 26L AND 24L. *S/D* TRIMMED OUT DAMAGE AND INSURANCE CUT, FAB NEW SPLICE AND REPAIR ANGLE AND INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050921000322005092100032EA 2005 9 21 MASA200500531 120050709A3230864808 PSEU CNDAIRCL600 CL6002B19 1900309EA MLG MALFUNCTIONED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW0747239781 7239 ASH 7168 BNA. PROX SYSTEM CHANNEL IN FLIGHT EXTENDED GEAR, DID NOT RESPOND. EXTENDED GEAR MANUALLY AND LANDED IN BNA. R2 PSEU OPS GOOD. 2L72 4F RTA21EA 20050921000342005092100034EA 2005 9 21 MASA200500580 120050722A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0737228 7228 ASH 6491 PHX. CABIN SERVICE DOOR EXIT LIGHT INOP. MAINTENANCE RELAMPED THE EXIT LIGHT. 2L72 4F RTA21EA 20050921000362005092100036NM 2005 9 21 USAA051088 120050916A5551 FITTING BOEING737 7374B7 1384702NM HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 LT HORIZONTAL STAB FWD SPAR FWD CLEVIS L1 LUG. REMOVED CORROSION FABRICATED AND INSTALLED NEW BUCHING IAW SRM 55-10-10, DEFECT SIZE: 1"X3". 2L72 4F RTA16WE 20050921000382005092100038NM 2005 9 21 USAA051087 120050916A5320 FLOOR SUPPORT BOEING737 7374B7 1384702NM BS 380-400 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 FLOOR SUPPORT CRACKED BETWEEN STATION 380 AND 400, BL0. FABRICATED AND INSTALLED NEW ANGLE, DEFECT SIZE: .125". 2L72 4F RTA16WE 20050921000392005092100039EU 2005 9 21 USAA051090 120050919A5322D5347112420100 SHEAR TIE AIRBUSA319 A319112 3930323EU FR 69-70 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19732US 1203 RT SIDE SHEAR TIE CORRODED BETWEEN FRAMES 69 AND 70. DEFECTIVE PART REPLACED WITH IDENT PART NR, DEFECT SIZE: 2 SQ IN. 2L72 4F RTA28NM 20050921000402005092100040NM 2005 9 21 USAA051091 120050919A5754 SKIN BOEING757 757225 1384959NM FLAP LEADING EDGCHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19609AU 22205 RT WING I/B FLAP O/B EDGE OF L/E CHAFED. CUT OUT DAMAGE AND REPAIRED PER SRM 57-53-01 FIG 201, 51-40-03, DEFECT SIZE: 9.9" X 6.5". 2L72 4F RTA2NM 20050921000412005092100041NM 2005 9 21 TAMF20050006O 120050917A5754 SKIN BOEING767 767200 1385120NM GE CF6 CF680C2B2 30025NE SLAT CRACKED W TAMFO OTHER C F.O.D. CLCLIMB 1 SO23767QT 23804 DURING TAKE OFF, THE CREW FELT A SUSPECTED BIRD STRIKE IN THE RIGHT PART OF THE AIRPLANE. DURING MAINTENANCE INSPECTION WAS FOUND A DENT AND CRACK ON THE NOSE SKIN AT SLAT NR 7. TIME LIMITED REPAIR WAS PERFORMED IAW EWO AND MFG APPROVAL NR 1-124395785-2 IN ORDER TO PERFORM FLIGHT. RIGHT NOW THE AIRPLANE IS PENDING FOR PERMANENT REPAIR. PERMANET REPAIR IN SLAT NR 7 WAS PERFORMED IAW EWO 767-57-005 PART II & BOEING APPROVAL 1-124395785. OPERATIONAL TEST OF LEADING EDGE SLATS WAS PERFORMED IAW AMM 27-81-01 PAGE 430-440 WITH NORMAL RESULTS. THE AIRPLANE RETURNED TO SERVICE ON SEPTEMBER 21, 2005. 2L72 4F4 FRTA1NM E13NE 20050921000422005092100042NM 2005 9 21 UIA0508 120050914A3260833703 SENSOR DOUG MD90 MD9030 3023690NM MLG FAILED Z O OTHER N FALSE WARNING TXTAXI/GRND HDL 1 SW9917923 53534 LANDING GEAR WARNING HORN SOUNDED 2 TIMES DURING ROLL OUT. FOLLOWED BY RT MAIN GEAR RED LIGHT FLASH. AIRCRAFT STOPPED AT TAXIWAY. INSPECTION FOUND R MAIN LANDING GEAR DOWNLOCK PROXIMITY SENSOR NOT GOOD. IAW AMM REPLACED THE SENSOR AND ADJ. CLEARANCE TO 0.070 INCH BETWEEN SENSOR AND TARGET. IAW AMM PERFORM FUNCTIONAL TEST RESULT SATISFY. 2L72 4F RTA6WE 20050921000432005092100043NM 2005 9 21 2005UALA00986 120050914A2120 ODOR BOEING777 777222 1385219NM PWA PW4077PW4077 NE CABIN DETECTED A UALAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 WP29772UA 26930 CREW REPORTED ELECTRICAL ODOR OR SMELL AROUND DOOR 2R. FOOD/DEBRIS BURNT IN WARMING OVEN. OVENS WERE CLEANED. 2L72 4F4 FRTT0001SE E46NE 20050921000442005092100044NM 2005 9 21 QXEA200501238 120050916A2611 SMOKE WARNING DHAV DHC8 DHC8202 2809007NM CARGO BAY FALSE ACTIVATIONA QXEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM09352PH 494 RDM FLIGHT NR 2142, MASTER WARNING AND SMOKE WARNING LIGHTS ILLUMINATED AND EXTINGUISHED. THEN SMOKE WARNING RE-ILLUMINATED. MAINTENANCE INSPECTED CARGO COMPARTMENT. NO EVIDENCE OF SMOKE. INSPECTED BOTH SMOKE DETECTORS. NO DEFECTS NOTED. PERFORMED OPERATIONAL CHECK PER AMM 26-15-00-710-801. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050921000452005092100045NM 2005 9 21 QXEA200501239 120050919A271043501508010 ACTUATOR DHAV DHC8 DHC8202 2809007NM AILERON TRIM MALFUNCTIONED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09358PH171103037 506 SEA FLIGHT NR 2070 AFTER TAKEOFF, THE AIRCRAFT WANTED TO ROLL RIGHT. ALL ENGINE INDICATIONS WERE NORMAL AND MATCHED, THE TURN COORDINATION WAS CENTERED, FULL LEFT AILERON TRIM WAS NEEDED TO RETURN CONTROL TO NEAR NORMAL. MAINTENANCE REPLACED THE RIGHT AILERON TRIM ACTUATOR. OPERATIONAL CHECK FLIGHT GOOD. OPERATION AND FUNCTIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050921000582005092100058EA 2005 9 21 MASA200500725 120050913A2450 GPU CNDAIRCL600 CL6002B19 1900309EA ELECTRICAL FAILED A MASAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 SW0737178 7178 ASH 6775 LAS. AIRCRAFT RETURNED TO GATE FOR FLAPS FAIL AT 8 DEGREES. MX FOUND THAT FAULT WAS DUE TO THE GPU NOT PROVIDING THE POWER REQUIRED TO OPERATE THE HYD PUMPS. MX SWAPPED GPU AND AIRCRACT OPS NORMAL. AIRCRAFT DEPARTED WITH NO FURTHER DEFECTS. 2L72 4F RTA21EA 20050921000612005092100061NM 2005 9 21 ASMF200509007 120050916A212015J85312 CLAMP DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE CABIN PRESSURE LOOSE W ASMFO OTHER J WARNING INDICATION CLCLIMB 1 SW23160PL 49763 AIRCRAFT RETURNED OF FLIGHT DURING CLIMB FLOW LIGHT TURNED ON AND PRESSURIZATION DID NOT WORK IN MANUAL MODE. A LEAK CHECK WAS PERFORMED AND FOUND LEAK IN SLEEVE AIR COOLING TURBINE. A CLAMP WAS TIGHTENED IAW MM. THE LEAK WAS CORRECTED AND PRESSURIZATION CONTROL WAS INTERCHANGED IAW. THE PRESSURIZATION CHECK WAS PERFORMED WITH 2 DIFFERENTIALS IN AUTOMATIC MODE AND 3 DIFFERENTIALS IN MANUAL MODE, OPERATING CORRECTLY. DURING OVERNIGHT CHECK WAS VERIFIED BOTH PACKAGES FOR LEAKS, DETECTING SOME LEAKS DUE TO CLAMP DAMAGE. LEAKS WERE CORRECTED AND CLAMPS WERE REPLACED IAW MM. THE PRESSURIZATION CHECK WAS PERFORMED IN MANUAL AND AUTOMATIC MODE IAW MM, BEING CORRECT. 2L72 4F4 FRTA6WE E9NE 20050919001342005091900134WP 2005 9 19 05FDEA02866 120050914A5532 SKIN DOUG MD10 MD1010F 3022112WP VERTICAL STAB DAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25571FE 47830 DURING AIRPLANE' S CONVERSION FROM P TO F FOUND VERTICAL STABILIZER ON RUDDER RT SIDE STA ZFR 320.125, SEVERAL SWELLING THE SKIN. REPAIRED DAMAGED SECTION OF SKIN IAW 55-10-00 FIG 3 VOL I. 2L73 4F RTA22WE 20050919001372005091900137NM 2005 9 19 05FDEA02869 120050914A5744 ATTACH FITTING DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 RIGHT WING - O/B FLAP I/B HINGE (WING SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87638. 2L73 4F RTA22WE 20050919001382005091900138NM 2005 9 19 05FDEA02870 120050914A5744 ATTACH FITTING DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 O/B FLAP I/B HINGE (WING SIDE), LWR ATTACHMENT I/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87638. 2L73 4F RTA22WE 20050919001392005091900139NM 2005 9 19 PIDA20050069 120050713A5314 KEELBEAM BOEING737 737228 13844AGNM BS 500B CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05237TR 23007 LEFT KEELBEAM HAS SIGNS OF CORROSION 16 INCHES AFT OF BS 500B FRAME. REPLACED SECTION OF KEELBEAM FROM BS 500A +12 TO BS 540 PER EA 53-171. 2L72 4F RTA16WE 20050919001402005091900140NM 2005 9 19 PIDA20050068 120050901A335020131A BATTERY PACK BOEING737 737228 13844AGNM EMERGENCY LIGHTSINOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05237TR 23007 NUMEROUS EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK IN AFT CARGO BIN, IN FWD SECTION OF CABIN, AND AFT CABIN. SYSTEM OPS CHECKS GOOD. 2L72 4F RTA16WE 20050919001462005091900146NM 2005 9 19 PIDA20050085 120050708A5320BAC1520729 SEAT TRACK BOEING737 737228 13844AGNM BS 985-1016 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05237TR 23007 SEAT TRACK AT RBL 40 HAS CORROSION FROM BS 985 TO BS 1016. REPLACED SECTION OF SEAT TRACK PER SRM 51-10-1 AND SRM 53-10-02. 2L72 4F RTA16WE 20050919001522005091900152NM 2005 9 19 SWAA052786 120050914A335010107451 SIGN BOEING737 7373K2 13844BANM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29345SA 23786 FWD EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM. 2L72 4F RTA16WE 20050919001542005091900154NM 2005 9 19 SWAA052788 120050914A53126582671 PRESSURE PANEL BOEING737 7373L9 1384470NM MLG WW CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE BEADED PRESSURE WEB CRACKED AT BS 663, LBL 31 & RBL 39. REPAIRED BEADED WEB PER SRM. 2L72 4F RTA16WE 20050919001562005091900156NM 2005 9 19 SWAA052790 120050914A534065C27314 STRINGER CLIP BOEING737 7373L9 1384470NM BS 663 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050919001622005091900162EU 2005 9 19 05FDEA02902 120050914A5347A0327400584 SEAT TRACK AIRBUS310 A310 EU FR 58-72 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25425FE 264 MAIN DECK SEAT TRACK FR 58 TO 72 CORRODED. REMOVED CORROSION, REMOVED TRACKS, FAB REPAIR PARTS INSTALLED REPAIR PARTS IAW SRM 51-23-10, 51-40-21, AND 53-10-16. 2L72 4F RTA35EU 20050919001702005091900170WP 2005 9 19 UPS05845422 120050903A5712 RIB DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE:C3, LT WING L/E UPPER RIB IS CRACKED AT XFS 778.750. STOP DRILLED, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-2-0. 2L74 4F RT4A25 20050919001712005091900171WP 2005 9 19 UPS05845424 120050904A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CHAFED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE:C3, RT WING L/E LOWER RIB IS CHAFED AT XFS 422.750. BLEND OUT OF LIMITS. FABRICATED AND INSTALLED 2 EA ANGLE REPAIRS IAW SRM 57-2-0 FIG 6, 57-3-3 FIG 5 AND 51-1-20D. 2L74 4F RT4A25 20050919001732005091900173WP 2005 9 19 UPS05845428 120050908A5714 DOUBLER DOUG DC8 DC873F 302199FWP FS 960-980 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE:C3 MAIN CABIN CENTER WING BOX STA 960 TO 980 RBL 65 FINGER DOUBLER HAS CORROSION. REMOVED FINGER DOUBLER, REMOVED CORROSION FROM DOUBLER AND SUBFLOOR FOUND DOUBLER OUT OF LIMITS. FABRICATED AND INSTALLED FINGER DOUBLER IAW SRM 51-1-21, 53-02-0 AND 53-07-03. 2L74 4F RT4A25 20050919001752005091900175WP 2005 9 19 UPS05845444 120050903A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE:C3 RIGHT O/B LEADING EDGE UPPER RIB CRACKED AT XFS 846. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM. 2L74 4F RT4A25 20050919001892005091900189NM 2005 9 19 05FDEA02927 120050915A5313 LONGERON DOUG MD11 MD11F 3023600NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 CENTER CARGO, LONGERON SPLICE AT BILGE AREA ADJACENT TO STATION 5-113 TO STATION 1541 LONGERON -51 LT BRIM AREA FOUND CRACK. CRACK LONGERON SPLICE REMOVED AS PER SRM 51-33-01 VOLUME II. NEW LONGERON SPLICE MACHINED AS PER DWG A5A7114. NEW LONGERON SPLICE INSTALLED AS PER SRM 51-33-01 VOLUME II. THIS REPAIR CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050919001902005091900190 2005 9 19 05FDEA02928 420050914A2230 ENGINE AIRBUS310 A310 EU NR 2 MALFUNCTIONED A FDEAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 SO25417FE 333 ON TAKEOFF ROLL AT 40 PERCENT N1 WHEN TOGA BUTTONS DEPRESSED NR 1 ENG ADVANCED, NR 2 ENG DID NOT. REJECT AT LESS THAN 20 KNOTS. RELEASED FOR SERVICE PER MEL/CDL: 22-30-01-A. R AND I TCC PER MM 22-36-34-4 AND PERFORMED ADJUSTMENT AND TEST PER MM 22-30-00-5 ALL TEST PASSED. 2L72 4F RTA35EU 20050919001962005091900196EU 2005 9 19 SA05100 120050914A77208TC19AAR1 SENSOR AIRBUSA319 A319112 3930323EU NR 1 ENGINE FAULTY A USAAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 EA19725UW1782917829 1135 PIT FLT 268 ON CLIMB OUT FROM PIT, AT FL160, CREW REPORTED THE NR 1 ENGINE AGENT ONE DISCHARGE LIGHT ILLUMINATED. FLIGHT ATTENDANT REPORTED FLAMES OUT THE REAR OF THE ENGINE WHILE A DEADHEAD PILOT REPORTED EXCESSIVE VIBRATION. CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD AT PIT. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND TAXIED TO THE GATE. MAINTENANCE PERFORMED BOROSCOPE INSPECTION OF NR 1 ENGINE. NO DEFECTS NOTED. ACCOMPLISHED TROUBLESHOOTING TASK 73-00-00-02 AND REPLACED NR 1 ENGINE T3 SENSOR PER MM 77-23-10-04. RAN ENGINES AT VARIOUS POWER SETTINGS. ALL OPERATIONS NORMAL. ALSO, REMOVED AND REPLACED NR 1 ENGINE AGENT ONE DISCHARGE BOTTLE. OPS CHECK GOOD. 2L72 4F RTA28NM 20050919001972005091900197NM 2005 9 19 UPS05445406 120050912A5610 WINDSHIELD BOEING747 747200 1384847NM COCKPIT DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 INSPECTION TYPE:N/A F/O R1 WINDOW HAS CHIPPING AND CRACKING IN MAIN GLASS PLIES. COMPLETED R1 REMOVAL & INSTALLED NEW R1 REF TO MM 56-11-01 UP TO STEP 6.D. FIRST TORQUE COMPLETED. ITEM STEPS 6D THRU J NEED TO BE C/W. STEPS ARE FOR INSTALLATION OF SEALANT. WINDSHIELD REQUIRES 3RD FINAL RE-TORQUE PER MM 56-11-01 STEP 9. DFRD 3RD FINAL WINDSHIELD RE-TORQUE PER AMC CONTROL D309948. ASSIGNED RETORQUE TO BE C/W WITHIN 9 DAYS PER AMC. ORIG TORQUE LP 372189 ITEM 1, 2ND TORQUE LP 372192 ITEM 3. ACCOMPLISHED STEPS 6 THRU D. MM 56-11-01 PG 417-419 SEALANT INSTALLATION. 2L74 4F RTA20WE 20050919002022005091900202CE 2005 9 19 DXTA200500970 120050915A2720 RUDDER CESSNA750 750 2076810CE MALFUNCTIONED E DXTAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 GL07902QS 7500002 UPON CLIMBOUT THROUGH 7000 FT THE RUDDER NEEDED MORE AND MORE TRIM TO REMAIN CENTERED. CONTINUED TO ADD LEFT RUDDER TRIM UNTIL THE HALF WAY POINT. IT TOOK MORE RUDDER TRIM AND WOULD NOT CENTER. THE RUDDER THEN VIOLENTLY SWUNG BACK THE OTHER DIRECTION. OPERATION WAS NORMAL AFTER THAT, ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20050920000052005092000005NM 2005 9 20 05FDEA02924 120050915A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 CRACK INDICATION AT END OF STRINGER 09 WAS FOUND DURING HFEC INSPECTION AT LEFT SIDE WING TANK. REPAIR CARRIED OUT AT LT WING TANK AT STRINGER 9 AS PER SRM 57-20-00 FIG 10 VOL I. FABRICATED REPAIR ANGLES AS PER SRM 57-20-00 FIG 10 VOL I AND INSTALLED REPAIR ANLGES AS PER SRM 51-33-01 VOL II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050920000082005092000008NM 2005 9 20 05FDEA02898 120050914A5315 FLOORBEAM BOEING727 727233 138408ANM ZONE 200 MISDRILLED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25286FE 22623 FLOORBEAM STATION 380 HAS PREVIOUS DRILLED HOLES IN RADIUS AND NO EDGE DISTANCE AT LEFT BUTT LINE 50 TO 60. CUT OUT DAMAGE SECTION OF UPPER BEAM CAP IAW FEDEX SR27-53-034E FIGURE 30. REMOVED TIEDOWN, RADIUS STOPS AND VERTICAL STIFFENERS IAW FEDEX SRM 51-30-2. FABRICATED REPAIR FILLER IAW FEDEX SR27-53-03E FIGURE 30. ALODINED AND PRIMED FILLER IAW FX B727 SRM 51-10-2. FABRICATED REPAIR ANGLES IAW FX SR 27-53-034E FIG 30. PRIMED REPAIR ANGLES IAW FX B727 SRM 51-10-20. INSTALLED REPAIR ANGLES AND FILLER IAW FX SR27-53-034E FIG 30. REINSTALLED TIEDOWN RADIUS, STRAPS AND VERTICAL STIFFENER IAW FX SRM B727 SRM 51-30-2. 2L73 4F RTA3WE 20050920000282005092000028NM 2005 9 20 SWAA052823 120050916A53106546956 CREASE BEAM BOEING737 7373H4 1384600NM BS 460-480 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 DURING SCHEDULED D-CHECK, FOUND RIGHT CREASE BEAM WEB CORRODED BETWEEN BS 460 TO BS 480. REPAIRED CREASE BEAM WEB PER SRM. 2L72 4F RTA16WE 20050920000532005092000053NM 2005 9 20 USAA051086 120050914A5751654645528SP SPAR BOEING737 7374B7 1384702NM AILERON DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 INBOARD END OF RT AILERON FRONT SPAR. TRIMMED AND SEALED IAW 57-50-22 DEFECT SIZE: 1 X 3 INCH. 2L72 4F RTA16WE 20050920000542005092000054NM 2005 9 20 USAA051085 120050914A5754 SKIN BOEING737 7374B7 1384702NM NR 1 SLAT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 LOWER SKIN, OUTBOARD END CRACKED. INSTALLED DOUBLER, IAW BOEING 737-400, SRM 57-43-01 DEFECT SIZE: 1.5 INCH. 2L72 4F RTA16WE 20050920000562005092000056WP 2005 9 20 ABXA050229 120050401A531199196182N FRAME DOUG DC9 DC932 3022066WP MLG WW CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23903AX 47427 CENTER OVER WHEEL WELL MAIN FRAME RIGHT SIDE IN WHEEL WELL, HAD CRACK EXTENDING INTO TWO EACH FASTENERS. MAIN FRAME NEEDED REPLACED PER SERVICE BULLETIN DC9-53-100. MAIN FRAME REPLACED ON EA 53400324-001-2. 2L72 4F A6WE 20050920000572005092000057WP 2005 9 20 ABXA050230 120050401A53305911412191 SKIN DOUG DC9 DC932 3022066WP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23903AX 47427 FUSELAGE SKIN FORWARD OF KIDNEY PANEL WAS BULGING AROUND FASTENERS FROM JUST ABOVE SKIN SPLICE AT LONGERON 26 LEFT TO SPLICE AT LONGERON 26 RIGHT. INNER SKIN CORROSION OUT OF LIMITS. FABRICATED AND INSTALLED NEW SKIN AND LONGERON IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 20050920000582005092000058WP 2005 9 20 ABXA050231 120050403A5330591140733 SKIN DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23903AX 47427 FUSELAGE SKIN CRACKED AFT OF SERVICE DOOR CUTOUT, AT LOWER AFT CORNER. REPAIRED AFT LOWER CORNER OF DOOR IAW DC-9 SRM 53-05. 2L72 4F A6WE 20050920000592005092000059WP 2005 9 20 ABXA050232 120050405A5320991007813 CUSP WEB DOUG DC9 DC932 3022066WP SERVICE DOOR CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23903AX 47427 CUSP WEB ANGLE AT SERVICE DOOR THRESHOLD CORRODED. REPAIRED CUSP WEB ANGLE IAW DC-9 SRM 53-05. 2L72 4F A6WE 20050920000602005092000060WP 2005 9 20 ABXA050233 120050405A532059124921 PAN DOUG DC9 DC932 3022066WP SERVICE DOOR CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23903AX 47427 SERVICE DOOR PAN CORRODED. REMOVED AND REPLACED LOWER SECTION OF SERVICE DOOR JAMB PAN IAW DC-9 SRM 53-05. 2L72 4F A6WE 20050920000612005092000061WP 2005 9 20 ABXA050220 120050901A53119919617502 FRAME DOUG DC9 DC932 3022066WP BS 699 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23900AX 47380 RIGHT FORWARD MAIN FRAME, STA 699, CRACKED AT POINTS G AND J, AFT FLANGE REQUIRED 5935650 REPAIR INSTALLED. REPAIRED MAIN FRAME AT FS 699 IAW EA 53400120-001-1. 2L72 4F A6WE 20050920000622005092000062WP 2005 9 20 ABXA050221 120050902A55115918000518 SPAR CAP DOUG DC9 DC932 3022066WP HORIZONTAL STAB CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23900AX 47380 RIGHT HORIZONTAL STABILIZER UPPER REAR SPAR TEE CAP MOST OUTBOARD END CRACKED. REPAIRED HORIZONTAL REAR SPAR CAP IAW DC-9 SRM 55-02. 2L72 4F A6WE 20050920000632005092000063WP 2005 9 20 ABXA050222 120050817A5320571412155 PAN DOUG DC9 DC941 302207NWP PAX DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23965AX 47498 AFT UPPER CORNER OF MAIN ENTRY DOOR PAN WAS CRACKED. REPAIRED AREA IAW DC-9 SRM 52-05. 2L72 4F A6WE 20050920000642005092000064WP 2005 9 20 ABXA050223 120050724A533059114181 SKIN DOUG DC9 DC931 3022065WP BS 680-737 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23907AX 47203 SKIN LONGERON 30, FS 680 TO FS 737 WAS CORRODED. BLENDED CORROSION AND REPAIRED DAMAGED AREAS IAW DC-9 SRM. 2L72 4F A6WE 20050920000652005092000065WP 2005 9 20 ABXA050224 120050726A531199115408 FRAME DOUG DC9 DC931 3022065WP BS 1087 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23907AX 47203 SHEAR TIE CRACKED FS 1087, LONGERON 2 RIGHT. REMOVED AND REPLACED SHEAR TIE IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20050920000662005092000066WP 2005 9 20 ABXA050225 120050613A53403925966501 FITTING DOUG DC9 DC941 302207NWP BS 617 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47492 LONGERON 25 LEFT, END FITTING CRACKED, STA 617. REMOVED AND REPLACED LONGERON 25 LEFT END FITTING IAW DC-9 SRM. 2L72 4F A6WE 20050920000672005092000067WP 2005 9 20 ABXA050226 120050517A571449171351 SHEAR TIE DOUG DC9 DC932F 3022067WP CENTER WING CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23909AX 47148 RIGHT XCW "0" STRINGER 17 - 18, HAD CRACKED SHEAR CLIP. REMOVED AND REPLACED SHEAR CLIPS IAW DC-9 SRM. 2L72 4F A6WE 20050920000682005092000068WP 2005 9 20 ABXA050227 120050517A57144917790502 SHEAR TIE DOUG DC9 DC932F 3022067WP CENTER WING CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23909AX 47148 RIGHT XCW 23 STRINGER 15 - 16, HAD CRACKED SHEAR CLIP. REMOVED AND REPLACED SHEAR CLIP IAW DC-9 SRM. 2L72 4F A6WE 20050920000692005092000069NM 2005 9 20 05FDEA02885 120050914A5313 STRINGER BOEING727 727225 1384077NM ZONE 500 PUNCTURED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 STA 480 SR20R HAS PUNCTURE ON LOWER SIDE. REMOVED DAMAGE ON STRINGER/DYE PENETRANT INSPECTION IAW B727 SRM 53-10-3 FIG 2, NO CRACKS NOTED. FABRICATED AND INSTALLED 3 EACH STRINGER TIES IAW B727 SRM 51-30-2 AND BAC DRAWING NR 66-11809. REMOVED AND REINSTALLED BRACKET, SUPPORT ANGLE, AND STIFFENER IAW B727 SRM 51-30-2. 2L73 4F A3WE 20050920000702005092000070NM 2005 9 20 05FDEA2886 120050914A5240 SKIN BOEING727 727227 1384078NM R1 DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 R-1 DOOR SKIN IS CRACKED AT UPPER HINGE. 2L73 4F A3WE 20050920000712005092000071NM 2005 9 20 05FDEA02887 120050914A5511 RIB BOEING727 727227 1384078NM HORIZONTAL STAB GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 LEFT HORIZONTAL STAB NR 3 BALANCE BAY OB RIB IS GOUGED FROM CONTACT WITH IDLER HINGE PIN. REMOVED AND REPLACED L/HORIZ. STAB NO. 3 BALANCE BAY OUTBD RIB IAW EA 7-5510-70689, PART 1 AND 727 SRM 51-30-2 AND 51-30-5. 2L73 4F A3WE 20050920000972005092000097NM 2005 9 20 SWAA052803 120050915A2560PH22300L GLOWSTRIP BOEING737 7377H4 1384404NM ROW 15-17 DEF CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29761RR 27875 DURING SCHEDULED MV2 CHECK, FOUND PHOTOLUMINESCENT STRIP CRACKED BETWEEN ROW 15 DEF TO ROW 17 DEF. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER MM. 2L72 4F RTA16WE 20050920001122005092000112NM 2005 9 20 MASA200500654 120050818A335061047811 BATTERY PACK DHAV DHC8 DHC8202 2809007NM EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07987HA 425 ASH 6282 PHX. DURING PREFLIGHT, THE RIGHT EXT EMERGENCY LIGHTS WOULD NOT TURN OFF AFTER A SUCCESSFUL TEST WITHOUT THE APPLICATION OF GROUND POWER. MX CHANGED THE BATTERY PACK AND FOUND OPS TO BE NORMAL. 2H72 4T RTA13NM 20050920001142005092000114WP 2005 9 20 UPS05845456 120050902A534037584952N FITTING DOUG DC8 DC873F 302199FWP L35R STA 1140 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 LWR CARGO STA 1140 L35R FWD FITTING CRACKED 2 INCHES LONG. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20050920001502005092000150EU 2005 9 20 XNOA1266 120050916A2420 WARNING LIGHT AIRBUS300 A300B4203 3930306EU NR 1 GENERATOR ILLUMINATED A XN0AD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL23371PC 157 NR 1 GENERATOR OFF LIGHT CAME ON AFTER BLOCK-OUT. ITEM TRANSFERRED TO DMI 5730 IAW ENA MEL 24-11-01 CAT-B. NR 1 GENERATOR DISCONNECTED. PLACARDS INSTALLED. 2L72 4F RTA35EU 20050920001522005092000152NM 2005 9 20 UPS05445459 120050916A3510 STRAP BOEING747 747212B 1384886NM O2 MASK BROKEN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 CAPT'S O2 MASK SUPPORT STRAP BROKEN. REPLACED CAPT'S O2 MASK STRAP. 2L74 4F A20WE 20050920001542005092000154 2005 9 20 UPS05445462 420050916A3416 WARNING SYSTEM BOEING747 747121 1384871NM ALTITUDE INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 ALTITUDE ALERTING SYSTEM INOP. RVSM A POSSIBILITY. R/R ALTITUDE A;ERTER COMPUTER PER MM 34-16-00-PG 207. SYSTEM TEST GOOD PER MM 34-16-00-OR. 2L74 4F A20WE 20050920001562005092000156WP 2005 9 20 UPS05845451 120050903A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 LEFT WING L/E UPPER SKIN HAS INTERGRANULAR CORROSION AT XFS 785.000. REMOVED CORROSION, FOUND OUT OF LIMITS. FABRICATED AND INSTALLED DOUBLER IAW SRM 51-1-8,51-1-21 AND EO DC8-5720-7767-A. 2L74 4F RT4A25 20050920001582005092000158WP 2005 9 20 UPS05845455 120050831A5313 LONGERON DOUG DC8 DC873F 302199FWP L15L STA 1728 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 LONG 15 LT CRACKED AT STA 1728 TOP AND BOTTOM. REMOVED DAMAGED SECTION OF LONGERON, FABRICATED REPLACEMENT SECTION OF LONGERON, AND INSTALLED IAW DC-8 SRM 53-2-2 FIG 10. 2L74 4F RT4A25 20050920001602005092000160NM 2005 9 20 CALA0500313 120050909A5320146N852247 SILL BOEING757 757224 1384958NM CARGO BAY CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718112 27302 MAINTENANCE NOTED SEVERAL AREAS OF CORROSION ON THE AFT CARGO COMPARTMENT O/B LOWER SILL CHORD. THE CHORD SECTION WAS REPLACED IAW ECRA 5310-04487. 2L72 4F RTA2NM 20050920001622005092000162NM 2005 9 20 CALA0500315 120050917A3397 WIRE BOEING757 757224 1384958NM EMERGENCY LIGHT STRIPPED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717139 30352 INSPECTION FOUND EMERGENCY AISLE PATH LIGHTING INOPERATIVE AT ROWS 7-20. A POWER WIRE AT ROW 24 WAS FOUND STRIPPED. THE WIRE WAS SPLICED AND THE LIGHTING CHECKED GOOD. 2L72 4F RTA2NM 20050920001642005092000164 2005 9 20 MAC90502 420050919A31002588423905AF AMPLIFIER FOKKERF27 F27MK500 4990629EU COCKPIT SHORTED A MTNABA EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO33705FE 10367 APPROXIMATELY AN HOUR INTO FLT, THE PIC EXPERIENCED SMOKE IN THE COCKPIT. DECLARED AN EMERGENCY AND RETURNED TO MIA. THE LANDING WAS WITHOUT INCIDENT. AFTER INVESTIGATION, THE CAUSE FOR THE SMOKE WAS AN INTERNAL SHORT IN THE INSTRUMENT AMP RACK. THE INSTRUMENT AMP RACK WAS REPLACED AND THE A/C RETURNED TO SERVICE. 2H72 4T A817 20050920001662005092000166NM 2005 9 20 CALA0500312 120050915A5320147A854007 THRESHOLD BOEING737 737724 13844BYNM STA 937-996 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2724702 28763 INSPECTION FOUND L-2 DOOR LOWER THRESHOLD FRAME CORRODED AT STA 937-996, LBL 52 TO RBL 52. THE L-2 DOOR THRESHOLD WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20050920001692005092000169NE 2005 9 20 XNOA1265 220050916A7320 SOLENOID AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE NR 2 ENGINE FAILED A XN0AC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL23372PC 196 517463 NR 2 ENGINE WOULD NOT ACCELERATE ON TAKEOFF. TROUBLESHOOT GROUND IDLE SOLENOID AND TRANFERRED TO DMI 5726 IAW MEL 73-30-02 CAT-C. CLEARED & RESEATED NR 2 ENG FTL IDLE SOLENOID C/P OPS CHECK NORMAL IAW A300 MM 73-21-00. DMI 5726 CLEARED. 2L72 4F4 FRTA35EU E23EA 20050920001732005092000173NM 2005 9 20 SWAA052834 120050916A57536546435340 SKIN BOEING737 7373H4 1384600NM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED RON CHECK, FOUND RIGHT OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM. 2L72 4F RTA16WE 20050920001752005092000175NM 2005 9 20 SWAA052836 120050918A53306545776 SKIN BOEING737 7373L9 1384470NM BS 957 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 957, STR 17R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050920001772005092000177NE 2005 9 20 SWAA052838 220050916A7314J1215P12 SEAL BOEING737 7377H4 1384404NM CFMINTCFM567CFM567B22 13802NE RT ENGINE TORN A SWAAC ABORTED TAKEOFF XJ ENGINE FLAMEOUT WARNING INDICATION TOTAKEOFF 1 SW29786SW 29811 874116 AIR TURNBACK, INFLIGHT SHUTDOWN, DECLARED EMERGENCY. NR 2 ENGINE FLAMED OUT. FOUND TORN FUEL PUMP SEAL CAUSING FUEL LEAK. REMOVED AND REPLACED SEAL PER MM. 2L72 4F4 FRTA16WE E00055EN 20050920001792005092000179NM 2005 9 20 SWAA052805 120050916A53306545766 SKIN BOEING737 7373H4 1384600NM BS 465-485 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29325SW 23689 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 465 TO BS 485, STR 16R TO STR 17R. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050920001812005092000181 2005 9 20 SWAA052807 420050913A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29326SW 23690 R2 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20050920001832005092000183NM 2005 9 20 SWAA052809 120050918A53126546568 BULKHEAD BOEING737 7373H4 1384600NM BS 1016 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 DURING SCHEDULED 1/4D CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT DOME CAP, 4 O'CLOCK, 5 O'CLOCK & 7 O'CLOCK POSITIONS. REPAIRED WEB PER SWA EA. 2L72 4F RTA16WE 20050920001852005092000185NM 2005 9 20 SWAA052811 120050916A53306545765 SKIN BOEING737 7373H4 1384600NM BS 520 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29352SW 24888 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 15L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050920001872005092000187NM 2005 9 20 SWAA052813 120050917A3350D71701100 BATTERY PACK BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29406WN 27894 EEPLS STRIP INOP AT ROW 11 TO ROW 17. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050920001922005092000192EU 2005 9 20 SA05101 120050916A5210 BOTTLE AIRBUSA321 A321211 3930370EU PAX DOOR ASSIST LOW A USAAO OTHER J WARNING INDICATION CRCRUISE 1 EA19169UW 1455 TPA PILOT REPORTED THE CIDS PANEL CAUTION LIGHTS KEEP ILLUMINATING DURING FLIGHT. LIGHTS WILL RESET IN FLIGHT BUT ONCE ON GROUND THE CAUTION LIGHTS ILLUMINATE AGAIN. MAINTENANCE SERVICED THE LEFT MID DOOR ASSIST BOTTLE TO CORRECT PRESSURE. 2L72 4F RTA28NM 20050920002022005092000202NM 2005 9 20 USAA051031 120050819A5330 SKIN BOEING737 737401 1384701NM CFMINTCFM56 CFM563B2 13802EU BS 727B-737C CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19417US45837 23984 CLT - C5 - SKIN, 3 INCH CRACK, 727B-737C AT STRINGER 23R. INSTALLED DOUBLER IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050920002122005092000212EA 2005 9 20 ASOA05683 120050820A5330 DOUBLER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE BS 427 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27839AS 7284 DURING A C-CHECK, THE DOUBLERS AT FS 427, LBL 34-44 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. (K) S/D - MAINTENANCE REMOVED THE CORROSION ON THE DOUBLERS AT FS 427, LBL 34-44 BY COMPLYING WITH ASA EO 600-53-0314. (M) 2L72 4F4 FRTA21EA E15NE 20050920002142005092000214NM 2005 9 20 USAA051008 120050816A5340 ANGLE BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU BS 727-710 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US 23933 CLT - Q6 - ANGLE, KEEL BEAM HAS FRETTING WEAR ON IT 17 IN X 1 INCH, CORRODED, STA 727-710, LBL 8. REMOVED SURF CORROSION, BLENDED AND TREATED IAW SRM, DWG. (K) 2L72 4F4 FRTA16WE E21EU 20050920002172005092000217EA 2005 9 20 ASOA05679 120050819A5320 WEB CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE BS 559-574 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27839AS 7284 DURING A C-CHECK, THE LT FLOOR ATTACH WEB AT FS 559.80 TO 574 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE WILL DETERMNE THE APPROPRIATE REPAIR UPON FURTHER INSPECTION ON THE LT FLOOR WEB AT FS 559.80 TO FS 574. 2L72 4F4 FRTA21EA E15NE 20050920002192005092000219EA 2005 9 20 ASOA05685 120050820A5330 DOUBLER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE BS 478 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27839AS 7284 DURING C-CHECK, THE DOUBLER AT FS 478, LBL 35-45 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO MFG FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. (K) S/D - MAINTENANCE REMOVED THE CORROSION FROM THE DOUBLER AT FS 476, LBL 35-45 BY COMPLYING WITH ASA EO 600-53-0314. (M) 2L72 4F4 FRTA21EA E15NE 20050920002222005092000222EA 2005 9 20 ASOA05682 120050820A5330 DOUBLER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE BS 422-446 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27839AS 7284 DURING A C-CHECK, THE DOUBLERS AT FS 422 TO FS446, RBL 34-44 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. (K) MAINTENANCE REMOVED THE CORROSION ON THE DOUBLERS AT FS 422 TO FS 446, RBL 34-44 BY COMPLYING WITH ASA EO 600-53-0313. (M) 2L72 4F4 FRTA21EA E15NE 20050921000152005092100015EA 2005 9 21 MASA200500658 120050820A3350316 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07652ML 7036 ASH 2850 PHL. FWD CEILING EMERGENCY FLOOD LIGHT INOP. MAINTENANCE REPLACED THE LAMP. 2L72 4F RTA21EA 20050921000292005092100029NM 2005 9 21 2005UALA00970 120050910A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE BS 520 DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29505UA 24626 FWD PIT FRAME AT STA 520, STR 24L, IS DENTED. TRIMMED OUT DAMAGE AND INSURANCE CUT, FABBED J-ANGLE REPAIR AND INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050921000312005092100031NM 2005 9 21 2005UALA00972 120050911A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE BS 1701 DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29505UA 24626 FUSELAGE SKIN AT BS 1701 AND STR 14L. ACCOMPLISHED EXTERNAL DOUBLER REPAIR PER TIMCO REO G10893 AND UA-EVA- 50622. 2L72 4F4 FRTA2NM E17NE 20050921000332005092100033EA 2005 9 21 MASA200500557 120050717A5210 LATCH CNDAIRCL600 CL6002B19 1900309EA PAX DOOR LACK OF LUBE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0717156 7156 ASH 2628 CLT. THE PAX DOOR WILL NOT OPEN FROM OUTSIDE. MX LUBED DOOR LATCH ASSEMBLY. 2L72 4F RTA21EA 20050921000352005092100035EA 2005 9 21 MASA200500618 120050806A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07715SF 7115 ASH 2635 STL. LEFT AFT EXTERIOR EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOP. MAINTENANCE RELAMPED. 2L72 4F RTA21EA 20050921000372005092100037NM 2005 9 21 USAA051089 120050916A5551 FITTING BOEING737 7374B7 1384702NM HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 LT HORIZONTAL STAB LUG 3 FWD CLEVIS. REMOVED CORROSION FABRICATED AND INSTALLED NEW BUCHING IAW SRM 55-10-10, DEFECT SIZE: 1" X 3". 2L72 4F RTA16WE 20050921000462005092100046NE 2005 9 21 QXEA200501233 220050917A7320 WARNING LIGHT DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE NR 1 ENGINE ILLUMINATED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09348PH 484 PCEAE0009 SEA FLIGHT NR 2232, NR 1 ENGINE MANUAL CAUTION ILLUMINATED. MAINTENANCE COMPLIED WITH RESET AND TEST PROCEDURES PER MCN 27631-01. OPERATIONAL TEST GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20050921000512005092100051NM 2005 9 21 05FDEA02947 120050916A5313 STRINGER BOEING727 727200 138407ENM BS 506.5 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION, FORWARD CARGO BAY ON STRINGER 25 RT BS 506.5. REPAIRED STRINGER AT BS 506.5 STRINGER 25R PER SRM 53-10-3. 2L73 4F RTA3WE 20050921000562005092100056EA 2005 9 21 MASA200500657 120050819A2150 SWITCH CNDAIRCL600 CL6002B19 1900309EA NR 2 A/C PACK FAILED A MASAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 SW0737218 7218 ASH 6239 COS. DIVERTED TO DEN FOR DUAL PACK FAILURE. MX SWAPPED OVER TEMP SWITCH FROM THE NR 1 PACK TO THE NR 2 PACK AND RESTORED THE NR 2 PACK. OPS CHECKED GOOD. 2L72 4F RTA21EA 20050921000622005092100062NM 2005 9 21 USAA200509002 120050915A5330 SKIN BOEING737 737301 1384611NM BS 727E-747 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19300AU 23228 2 INCH CRACK EXTENDING FROM UNDER A PREVIOUS REPAIR AT STA 727E - 747 STRINGER 23L. REMOVED REPAIR DOUBLER, FABRICATED NEW DOUBLER AND FILLERS AND INSTALLED REPAIR PER SRM 53-00-01 FIG 201. 2L72 4F RTA16WE 20050921000642005092100064EA 2005 9 21 MASA200500565 120050718A52101186541 LATCH CNDAIRCL600 CL6002B19 1900309EA PAX DOOR INOPERATIVE A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW0727191 7191 ASH 2631 PHL. A/C WOULD NOT PRESSURIZE IN AUTO OR MANUAL. MX FOUND THE PASSENGER DOOR LATCH ASSY INOPERATIVE, PREVENTING DOOR FROM CLOSING PROPERLY. MAINTENANCE REMOVED AND REPLACED PASSENGER DOOR LATCH MECHANISM. 2L72 4F RTA21EA 20050921000662005092100066NM 2005 9 21 SWAA052840 120050919A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM BS 986 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 DURING SCHEDULED D-CHECK, FOUND CABIN FLOORBEAM CORRODED AT BS 986, LBL 35 TO LBL 45, WL 208. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20050921000682005092100068NM 2005 9 21 SWAA052842 120050919A53116546595 FRAME BOEING737 7373H4 1384600NM BS 727D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 DURING SCHEDULED D-CHECK, FOUND CABIN FUSELAGE FRAME CRACKED AT BS 727D, STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050921000702005092100070NM 2005 9 21 SWAA052844 120050919A531165465526 FRAME BOEING737 7373H4 1384600NM BS 400 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 DURING SCHEDULED D-CHECK, FOUND CABIN FUSELAGE FRAME CRACKED AT BS 400, STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050921000722005092100072NM 2005 9 21 SWAA052846 120050919A53116546549 SHEAR TIE BOEING737 7373H4 1384600NM BS 767 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 DURING SCHEDULED D-CHECK, FOUND CABIN FUSELAGE SHEAR TIE CORRODED AT BS 767, LBL 2 TO RBL 2, WL 156. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050921000732005092100073EA 2005 9 21 MASA200500630 120050810A284273664310 COMPUTER CNDAIRCL600 CL6002B19 1900309EA FUEL QTY MALFUNCTIONED A MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW07372282886 7228 ASH 6493 PHX. LOSS OF FUEL CH 1 & CH 2 ALONG WITH TOTAL FUEL QUANTITY. MAINTENANCE REMOVED AND REPLACED THE FQGC. 2L72 4F RTA21EA 20050921000752005092100075EU 2005 9 21 USAA051120 120050920A5321 FLOOR PANEL AIRBUSA319 A319112 3930323EU CABIN DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19723UW 1109 FASTENER HOLE DAMAGED OD OF PANEL, CABIN FLOOR PANEL 262HG. INSERT PER GILL MANUAL MCGIRM 8701 REV F, AIRBUS SRM 53-02-00, DEFECT SIZE: 1" X 1" AREA. 2L72 4F RTA28NM 20050921000772005092100077EU 2005 9 21 USAA051118 120050920A5315D5347217220400 FLOORBEAM AIRBUSA319 A319112 3930323EU BS 66-68 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19732US 1203 FOUND CORROSION LT BS 66 TO 68 INB OF DOOR SILL -Y1162. REPLACED WITH IDENTICAL PART PER SRM 51-42-00, DEFECT SIZE: 1" X 2". 2L72 4F RTA28NM 20050921000792005092100079EU 2005 9 21 USAA051116 120050920A5315D5347218820400 FLOORBEAM AIRBUSA319 A319112 3930323EU BS 68 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19732US 1203 FOUND CORROSION LT BEAM Y1162 STA 68 AROUND NUT PLATES AT ATTACH HOLES. REPLACED WITH IDENTICAL PART PER SRM 51-42-00, DEFECT SIZE: 1" BY 2". 2L72 4F RTA28NM 20050921000802005092100080EA 2005 9 21 MASA200500679 120050827A26107546911 SENSOR CNDAIRCL600 CL6002B19 1900309EA A/C PACK DUCT FAILED A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW07154SF 7154 ASH 2819 ABE. DIVERTED DUE TO SMOKE VISIBLE IN CABIN. MAINTENANCE FOUND THE RIGHT PACK RUNNING AWAY HOT. THE DUCT TEMP SENSOR WAS REPLACED. 2L72 4F RTA21EA 20050921000822005092100082EA 2005 9 21 MASA200500717 120050908A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA ROW 1 INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0717156 7156 ASH 2733 PHL. ROW 1 EXIT FLOOR STRIP LIGHTING INOPERATIVE. MX REPLACED FORWARD EMERGENCY LIGHT STRIP. 2L72 4F RTA21EA 20050921000842005092100084NM 2005 9 21 SWAA052847 120050919A53126516300 BULKHEAD BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29506SW 24183 DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD WEB CRACKED A LBL 17.1, WL 236. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050922000022005092200002EA 2005 9 22 MASA200500613 120050804A2750860D10018ABC FCU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07154SF1 7154 ASH 2664 PHL. FLAPS FAILING AT ZERO DETENT. MX REMOVED AND REPLACED THE FECU. 2L72 4F RTA21EA 20050922000032005092200003EA 2005 9 22 MASA200500592 120050725A2913887055 PUMP CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM FAILED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07372181381 365 7218 ASH 6264 PHX. LEFT GEAR DISAGREE IN FLIGHT. MX REPLACED NR 3A HYD PUMP. 2L72 4F RTA21EA 20050922000042005092200004EA 2005 9 22 MASA200500612 120050803A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07154SF 7154 ASH 2751 PHL. FLAPS FAILED AT ZERO. MAINTENANCE RESET PER PART A OF AD. 2L72 4F RTA21EA 20050922000062005092200006NM 2005 9 22 05FDEA02986 120050918A5744 ATTACH FITTING DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 LEFT WING, O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-87640. 2L73 4F RTA22WE 20050922000072005092200007NM 2005 9 22 05FDEA02987 120050918A5744 ATTACH FITTING DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 LEFT WING, O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. FABRICATED BUSHING AND INSTALLED AS PER EA 1-5750-87640. 2L73 4F RTA22WE 20050922000082005092200008EU 2005 9 22 05FDEA02976 120050916A5347 SEAT TRACK AIRBUS310 A310 EU FS 62-36 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25425FE 264 MDC - SEAT TRACK AT RBL 58 BETWEEN FS 62-63 HAS SEVERAL DAMAGED LUGS. 2L72 4F RTA35EU 20050922000092005092200009EU 2005 9 22 05FDEA02977 120050916A5347 SEAT TRACK AIRBUS310 A310 EU FR 75-77 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25425FE 264 MDCC - SEAT TRACK BETWEEN FS 75-77 LBL HAS SPOTS OF CORROSION. 2L72 4F RTA35EU 20050922000112005092200011NM 2005 9 22 0509002 120050919A5753 RIB BOEING737 7372H4 138448CNM TE FLAP CRACKED A MJYAK NONE O OTHER ININSP/MAINT 1 SW05733TW 22732 RT WING AT WBL STA 364, OUTBOARD MID FLAP RIB CRACKED. 2L72 4F A16WE 20050922000132005092200013EU 2005 9 22 2005UALA00973 120050911A3350Z120H0072112 CONTROL PANEL AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29448UA 842 LEFT AFT MED EMERGENCY LIGHT SWITCH IS INOPERATIVE. REPLACED CIDS AFT PANEL. 2L72 4F4 FRTA28NM E40NE 20050922000142005092200014EU 2005 9 22 2005UALA00974 120050910A3350 LIGHT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CABIN FAULTY A UALAK NONE L NO TEST ININSP/MAINT 1 WP29479UA 1538 EMERGENCY EXIT LIGHT TEST DOES NOT PASS. REPLACED BATTERY. 2L72 4F4 FRTA28NM E40NE 20050922000152005092200015NM 2005 9 22 2005UALA00975 120050911A3350 LAMP BOEING777 777222 1385219NM PWA PW4077PW4077 NE SEAT 2E INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29777UA 26916 EMERGENCY LIGHT AT SEAT 2E INOP. RELAMPED. 2L72 4F4 FRTT0001SE E46NE 20050922000162005092200016NM 2005 9 22 2005UALA00977 120050911A5210 ROD BOEING737 737322 1384676NM GE CFM56 CFM563US 13802NE R1 DOOR OUT OF ADJUST A UALAO OTHER O OTHER CRCRUISE 1 WP29327UA 24147 DOOR 1R HANDLE MOVES IN FLIGHT. *S/D* ADJUSTED COCKING ROD AND LATCH FITTINGS AND STOP PINS. REF MM 52- 00-96-0100A AND MM 52-41-00. 2L72 4F4 FRTA16WE E2GL 20050922000192005092200019NM 2005 9 22 2005UALA00980 120050912A25302610000101 OVEN AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE GALLEY SMOKE A UALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP29835UA 1426 F/A REPORTS SMOKE COMING OUT OF OVEN. SECURED IT AND DIVERTING FLIGHT. INITIAL INSPECTION REVEALED A DIRTY FILM ON INTERIOR OF OVEN WITH A DISTINCT ODOR THAT COULD HAVE CAUSED "SMOKING" CONDITION. THE OVEN WAS INSPECTED AND CHECKED/TESTED PER MANUFACTURER'S COMPONENT MAINTENANCE MANUAL AND WILL BE RETURNED TO SERVICE. MAINTENANCE RECORDS WILL NOTE THIS INCIDENT FOR FUTURE REFERENCE. 2L72 4F4 FRTA28NM E40NE 20050922000212005092200021EU 2005 9 22 2005UALA00982 120050906A3350 BATTERY AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE EMERGENCY LIGHT FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29411UA 464 LEFT EMERGENCY BATTERY WON'T PASS TEST. REPLACED BATTERY. 2L72 4F4 FRTA28NM E40NE 20050922000232005092200023NM 2005 9 22 2005UALA00984 120050914A3397 CONNECTOR BOEING747 747451 1384940NM PWA 4056 PW4056 NE EMERGENCY LIGHT DAMAGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29105UA 26473 EEL INOP AT SEAT 22 LEFT BOTH SECTIONS AND SEAT 3J FWD SECTION. REPAIRED CONNECTOR AT SEAT. 2L74 4F4 FRTA20WE E24NE 20050922000242005092200024NM 2005 9 22 2005UALA00985 120050914A3350 LIGHT BOEING747 747451 1384940NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29105UA 26473 EEL INOP ON WALL BETWEEN LAVS 111 & 112. REPAIRED FEEDER WIRE ON FLOOR. 2L74 4F4 FRTA20WE E24NE 20050922000252005092200025EA 2005 9 22 MASA200500528 120050708A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA MAIN PAX STIFF A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0717217 7217 ASH 7167 IAD. PAX DOOR THAT WAS DIFFICULT TO OPEN. MX REPOSITIONED THE A/C TO A DIFFERENT GATE AND COULDN'T DUPLICATE ANY FURTHER FAULTS WITH DOOR. 2L72 4F RTA21EA 20050922000262005092200026EA 2005 9 22 MASA200500542 120050712A2612356024310 FIRE LOOP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT ENGINE MALFUNCTIONED A MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW07571ML 7209 872094 ASH 2786 PHL. RIGHT HAND 14TH STAGE DUCT WARNING. CREW SHUTDOWN THE ENGINE AND MX IS CURRENTLY TROUBLESHOOTING THE FAULT. MAINTENANCE REMOVED AND REPLACED THE 14TH STAGE SENSE LOOP. 2L72 4F4 FRTA21EA E15NE 20050922000272005092200027EA 2005 9 22 MASA200500547 120050714A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07570ML 7206 ASH 2638 PHL. THE CREW REPORTED ONE RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. MAINTENANCE RELAMPED THE EXIT LIGHT. 2L72 4F RTA21EA 20050922000282005092200028NM 2005 9 22 05FDEA02981 120050917A5350 FAIRING BOEING727 727225 1384077NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 RIGHT WING TO BODY FAIRING NR 3437 HAS CORROSION (EXFOLIATED). REMOVED ANGLE IAW B727 SRM 51-30-2. FABRICATED ANGLE IAW BAC DRAWING 65-25582. ALODINED AND PRIMED ANGLE IAW B727 SRM 51-10-2. INSTALLED ANGLE IAW B727 SRM 51-30-2. REMOVED TEE CHORD IAW B727 SRM 51-30-2. FABRICATED CHORD IAW BAC DRAWING 65-25582. ALODINED AND PRIMED TEE CHORD IAW B727 SRM 51-10-2. INSTALLED TEE CHORD IAW B727 SRM 51-30-2. 2L73 4F A3WE 20050922000312005092200031NM 2005 9 22 05FDEA02984 120050918A5744 ATTACH FITTING DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 LT WING, O/B FLAP O/B HINGE (WING SIDE), SIDE LINK ATTACHMENT AFT BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-87640. 2L73 4F RTA22WE 20050922000332005092200033CE 2005 9 22 DXTA200500973 120050917A2612 FIRE DETECTOR CESSNA650 650 2076802CE APU BAY MALFUNCTIONED E DXTAH DEACTIVATE SYST/CIRCUITS N FALSE WARNING CRCRUISE 1 GL07710QS 6507100 APU FIRELIGHT CAME ON IN FLIGHT, PUSH THE LIGHT AND BLEW THE BOTTLE AS PER CHECKLIST, INSPECTED APU AND SURROUNDING AREA NO DAMAGE NOTED, MEL PER CE-650 NJA MEL MANUAL. ITEM IS UNDER INVESTIGATION. 2L72 4F A9NM 20050922000392005092200039NM 2005 9 22 SWAA052848 120050919A53146545866 KEELBEAM BOEING737 7373L9 1384470NM BS 727 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED 1/2D CHECK, FOUND KEELBEAM CORRODED AT BS 727, LBL 7. REPAIRED KEELBEAM PER SWA EA & SRM. 2L72 4F RTA16WE 20050922000412005092200041NM 2005 9 22 USAA051097 120050920A5311 FRAME BOEING737 7374B7 1384702NM BS 294 DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 STA 294, S-16L AFT OF FRAME, NEW PART, INSTALLED WITH LOCK FASTENERS IAW SRM 51-10-02, DEFECT SIZE: SHEETMETAL NR 4365, WEB CRACKED (APPROX 1.5 INCHES LONG) S-161, AFT OF BS 294 FRAME. 2L72 4F RTA16WE 20050922000432005092200043EA 2005 9 22 MASA200500507 120050630A2410755469D IDG CNDAIRCL600 CL6002B19 1900309EA NR 2 FAILED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07172319173 7231 ASH 6332 FSD. ABORTED THE TAKEOFF ROLL DUE TO AN IDG 2 CAUTION MESSAGE THAT CLEARED AND WAS REPLACED BY A GEN 2 CAUTION MESSAGE. MAINTENANCE PLACED THIS ON DEFERRAL. MX REPLACED THE NR 2 GENERATOR ON 7/11/05. 2L72 4F RTA21EA 20050922000442005092200044EA 2005 9 22 MASA200500558 120050717A5210 CABLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR OUT OF ADJUST A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0737228 7228 ASH 6493 PHX. A MAIN CABIN DOOR THAT WAS HARD TO OPEN. MX ADJUSTED CABLE TENSION FOR DOOR SUPPORT WHEEL. 2L72 4F RTA21EA 20050922000452005092200045EA 2005 9 22 MASA200500564 120050718A5210601R3189325 ROD CNDAIRCL600 CL6002B19 1900309EA PAX DOOR DAMAGED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0727172 7172 ASH 2652 PHL. COULD NOT OPEN THE PASSENGER DOOR. A/C FERRIED TO PHL. MAINTENANCE REMOVED AND REPLACED PASSENGER DOOR PUSH ROD ASSEMBLY. 2L72 4F RTA21EA 20050922000462005092200046EA 2005 9 22 MASA200500569 120050718A3350316 LIGHT CNDAIRCL600 CL6002B19 1900309EA ROW 5 INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0727185 7185 ASH 5620 ERI. EMERGENCY EXIT FLOOD LIGHT OVER ROW 5 THAT WAS INOPERATIVE. MX RELAMPED. 2L72 4F RTA21EA 20050922000492005092200049EU 2005 9 22 USAA051113 120050920A5315D5347209000200 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19730US 1182 FOUND CORROSION Y 765 AFT OF 640 AND AT FRAME 66 AT BARREL NUT. REMOVED AND REPLACED WITH LIKE PART, DEFECT SIZE: 1/4" X 1/2". 2L72 4F RTA28NM 20050922000502005092200050EU 2005 9 22 USAA051124 120050920A5310 BEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19732US 1203 FOUND CORROSION FR 16 AND BETWEEN FR 19 AND 20 CENTER BEAM. INSTALLED DOUBLERS PER SRM 53-00-14 FIG 206, DEFECT SIZE: 2" X 2" AND 1" X 1". 2L72 4F RTA28NM 20050922000512005092200051NM 2005 9 22 USAA051096 120050920A5340 ATTACH BRACKET BOEING737 7374B7 1384702NM BS 737 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 FOUND CRACK O/H DUCT ATTACH BRACKET AT STA 767 STR 1. FABRICATED AND INSTALLED IAW SRM 51-10-02 AND BOEING DWG 69-47869, DEFECT SIZE: 1/4" CRACK AT BRACKET. 2L72 4F RTA16WE 20050922000522005092200052NM 2005 9 22 USAA051095 120050920A5340 STRINGER CLIP BOEING737 7374B7 1384702NM BS 737 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 FOUND TIE CLIP CRACKED AT STA 767, STR 2L. REPLACED TIE CLIP IAW SRM 51-10-02. 2L72 4F RTA16WE 20050922000532005092200053EU 2005 9 22 05FDEA02975 120050916A2611 CONTROL UNIT AIRBUS310 A310 EU SMOKE DETECTORS MALFUNCTIONED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25409FE 273 ON CLIMB-OUT JUST ABV FL190, MAIN DECK CARGO SMOKE WARNING ANNUNCIATED FOR MID 2. PRIOR TO MAIN DECK WARNING LOOP A MID 2 FAULTED. COMMENCED AIR TURN-BACK TO KGRR, RAN MDC SMOKE PROC IAW QRH. ECAM REQUEST TO NORM ON DESCENT THROUGH APPROX 15000'MSL. NO SMOKE OR FUMES IN COCKPIT AT ANY TIME. NORMAL APPR AND LANDING. MAIN DECK (IDENTIFY MID 2 LOOP A SMOKE DETECTOR(S) - INOP." INSPECTED ALL OF MAIN CARGO DECK FOR SMOKE. NO SMELL OF SMOKE FOUND. REMOVED AND REPLACED MID 2 CARGO SMOKE CONTROL UNIT PER A310-200 MM SUP 26-16-12-4. OPS CK GOOD. 2L72 4F RTA35EU 20050922000542005092200054NM 2005 9 22 05FDEA02978 120050916A575365192507 FLAP TRACK BOEING727 7272S2F 1384O81NM NR 6 FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25211FE 22933 RT WING INBD FLAP OUTBD TRACK NR 6 HAS CORROSION, PITTING, AND CHAFING ON FACES AND ROLLERS SLIDING TRACKS. REPLACED NR 6 FLAP TRACK ASSY IAW MM 27-51-031-4. 2L73 4F A3WE 20050922000552005092200055NM 2005 9 22 05FDEA02979 120050916A575365192509 FLAP TRACK BOEING727 7272S2F 1384O81NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25211FE 22933 RT WING OUTBD FLAP, OUTBD TRACK HAS SURFACE CORROSION AND CHAFING ON FACES AND ROLLERS SLIDING TRACKS. REMOVED AND REPLACED NR 8 FLAP TRACK IAW MM 27-51-031-4. 2L73 4F A3WE 20050922000562005092200056NM 2005 9 22 05FDEA02980 120050917A5330 SKIN BOEING727 7272S2F 1384O81NM BS 190 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25211FE 22933 FUSELAGE SKIN IS DAMAGED, POSSIBLY CRACKED AT FS 190, AT APPROX 7 O'CLOCK POSITION, (NO STRINGERS IN THIS AREA.) MAJOR REPAIR PERFORMED HFEC IAW PTGNTM 51-00-00 CRACKED INDICATED AS MARKED. REMOVED DAMAGE IAW SRM 53-30-1FIG 1. FABRICATED REPAIR DOUBLER FROM 2024T3 .050 BATCH NR 950751 IAW SRM 53-30--1 FIG1 AND FILLER FROM 2024T3 .040 BATCH NR 957207 IAW SRM 53-30-1 FIG 1. INSTALLED REPAIR AND FILLER IAW SRM 53-30-1 FIG1. THIS IS ACATAGORY ""A"" REPAIR. PREP AND PAINTED IAW MM 51-20-151-7. 2L73 4F A3WE 20050922000572005092200057NM 2005 9 22 USAA051093 120050920A53401133482 STRINGER CLIP BOEING737 7374B7 1384702NM BS 827 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 FOUND CRACK STA 827, S4L. REMOVED DAMAGED PART, INSTALLED NEW IAW SRM 51-10-02 3.C (3), DEFECT SIZE: .125" CRACK. 2L72 4F RTA16WE 20050922000592005092200059EU 2005 9 22 USAA051114 120050920A5310D5347217220390 BEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19732US 1203 FOUND CORROSION RT BEAM STA 66-68 INB OF RT DOOR SEAL AT ATTACH HOLES. REPLACED WITH IDENTICAL PART NUMBER PER SRM 51-42-0, DEFECT SIZE: 1" X 2". 2L72 4F RTA28NM 20050922000602005092200060NM 2005 9 22 USAA051104 120050920A5551657378212 ATTACH FITTING BOEING737 7374B7 1384702NM HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 FOUND CORROSION RT HORIZ STAB FORWARD LWR CLEVIS AFT BUSHING AFT FACE. REMOVED CORROSION AND INSTALLED BUSHING IAW SRM 55-10-10, DEFECT SIZE: 1" X 2" AREA OF CORROSION. 2L72 4F RTA16WE 20050922000612005092200061NM 2005 9 22 USAA051129 120050920A5311US5RM5360071 FRAME BOEING737 7374B7 1384702NM BS 907 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19776AU 24934 FOUND CRACK STA 907 STR 1. INSTALLED FRAME ANGLE REPAIR PER SRM 53-00-07, DEFECT SIZE: 1". 2L72 4F RTA16WE 20050922000622005092200062NM 2005 9 22 USAA051128 120050920A5330 SKIN BOEING737 7374B7 1384702NM BS 864 CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19776AU 24934 FOUND CHAFING UPPER FUSELAGE EXT SKIN DBLR UNDER DORSAL FIN STA 864 BL=0. REMOVED DBLR, FILLER, SKIN AND TEAR STRIP, FABBED AND INSTALLED NEW PER EA 96859, DEFECT SIZE: 5-3/4" X 7". 2L72 4F RTA16WE 20050922000632005092200063EU 2005 9 22 USAA051112 120050920A5320D5348004320401 SILL AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19725UW 1135 FOUND CORROSION Y 1500 AND FRAME 6. DEFECTIVE PART REPLACED WITH IDENTICAL PART NUMBER, DEFECT SIZE: 2 SQ IN. 2L72 4F RTA28NM 20050922000652005092200065EU 2005 9 22 USAA051110 120050920A5322D5347112420100 SHEAR TIE AIRBUSA319 A319112 3930323EU FR 69-70 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19733UW 1205 FOUND CORROSION BETWEEN FRAME 69 AND 70 TO RT SIDE. REMOVED AND REPLACED WITH DEFECTIVE PART NR PER SRM 51-72-11, DEFECT SIZE: 3" X 4". 2L72 4F RTA28NM 20050922000662005092200066NM 2005 9 22 USAA051109 120050920A5510657378211 BUSHING BOEING737 7374B7 1384702NM HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 FOUND CORROSION LT HORIZ STAB L14 AFT BUSHING. REWORKED AREA AND INSTALLED BUSHING IAW SRM 55-10-10, DEFECT SIZE: 1" X 2" AREA OF CORROSION. 2L72 4F RTA16WE 20050922000672005092200067NM 2005 9 22 USAA051108 120050920A5551657378211 ATTACH FITTING BOEING737 7374B7 1384702NM HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 FOUND CORROSION LT HORIZ STAB L5 BUSHING LUG FACE. REMOVE CORROSION AND BUSHING IAW SRM 55-10-10, DEFECT SIZE: 1" X 2" AREA OF CORROSION. 2L72 4F RTA16WE 20050920000182005092000018EU 2005 9 20 SF20050918 120050918A7930 WARNING LIGHT SAAB SF340 SF340A 7850100EU LT ENGINE ILLUMINATED A UHLAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL1735SZ 035 FLIGHT 7562 IAD-HPN, LT ENGINE OIL PRESSURE CWP LIGHT ILLUMINATED INTERMITTENTLY, LT ENGINE OIL PRESSURE GAGE FLUX 30-50 PSI, ALL OTHER ENGINE PARAMETERS NORMAL. POST FLIGHT FOUND NO OIL LEAKS OUTSIDE OF ENGINE COWLS OR ON WINGS. 2L72 4T RTA52EU 20050920000262005092000026NM 2005 9 20 SWAA052821 120050916A53226546529 SHEAR TIE BOEING737 7373H4 1384600NM BS 500 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 500, BETWEEN RBL 1 TO RBL 2. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050920000362005092000036NM 2005 9 20 SWAA052831 120050916A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 480 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 480, STR 15R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050920000492005092000049NM 2005 9 20 BB05079 120050911A335020131A BATTERY PACK BOEING757 757225 1384959NM EMERGENCY LIGHT DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19606AU 22202 MCO - THE GALLEY FORWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK IN THE FORWARD GALLEY. OPERATIONALLY CHECKS OK. 2L72 4F RTA2NM 20050920001072005092000107NM 2005 9 20 WRLA2005142 120050909A3260862701 SENSOR DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE MLG INOPERATIVE A WRLAD RETURN TO BLOCK N FALSE WARNING CLCLIMB 1 SO11276 48632 AIR TURNBACK DUE TO ON GEAR RETRACTION, LT MAIN GEAR INDICATED GEAR UNSAFE ON PRIMARY PANEL AND CONFIGURATION PAGE. REPLACED LEFT GEAR UP & LOCKED SENSOR IAW AMM 32-61, PERFORMED RTS OF SENSOR IAW AMM 32-61-17 PG 700-801, NO FAULTS NOTED AT THIS TIME. 2L73 4F4 FRTA22WE E24NE 20050920001092005092000109NM 2005 9 20 SWAA052815 120050918A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29449WN 32469 EEPLS TRACK COVER MISSING AT FWD END. INSTALLED COVER PER MM. 2L72 4F RTA16WE 20050920001172005092000117WP 2005 9 20 UPS05845461 120050915A5512 SKIN DOUG DC8 DC873F 302199FWP HORIZONTAL STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 LT HORIZONTAL LE HAS INTERGRANULAR CORROSION AROUND FASTENER HOLES ON LOWER SURFACE AT IB END OF OB SECTION. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 55-2-1 FIG 4. 2L74 4F RT4A25 20050920001192005092000119NM 2005 9 20 AWXA200501043 120050918A2560P4010021 BATTERY BOEING737 7373G7 1384595NM FLASHLIGHT INOPERATIVE A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28311AW 24712 CREW REPORTED THE EMERGENCY FLASHLIGHT, BY THE L1 DOOR, WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY IN THE FLASHLIGHT NEXT TO THE L1 DOOR. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20050920001212005092000121NM 2005 9 20 AWXA200501045 120050826A53136948948501 STRINGER BOEING737 7373Y0 1384671NM BS 351.2-360 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED GALVANIC CORROSION IN THE E&E COMPARTMENT AT STRINGER 28R FROM BS 351.2 TO BS 360. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-00-03-1A1 FIG 101. MAINTENANCE REMOVED STRINGER 28R IAW BOEING 737-300 SRM 51-40-02-06. RECEIVED AND DRILLED NEW STRINGER IAW BOEING 737-300 SRM 51-40-05-06 FIG 2 & 3. INSTALLED REPAIR PARTS AT STRINGER 28R BETWEEN BS 351.2 AND BS 352 IAW BOEING 737-300 SRM 51-40-02-06. 2L72 4F RTA16WE 20050920001232005092000123NM 2005 9 20 AWXA200501047 120050825A5755664645159A SKIN BOEING737 7373Y0 1384671NM SPOILER DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED DISBOND AREA ON THE UPPER AND LOWER SURFACE OF THE NR 2 SPOILER. SEVENTEEN INCHES FROM THE INBOARD END AND FIVE INCHES FROM THE AFT EDGE FROM WING STATIONS 354.75L TO WING STATIONS 359.2L. MAINTENANCE REMOVED DISBOND AREA FROM THE NR 2 SPOILER IAW BOEING 737-300 SRM 51-70-10-2R REPAIR 4. FABRICATED DOUBLER AND REPAIR CORE IAW BOEING 737-300 SRM 51-70-10-2R FIG 203. BONDED REPAIR PARTS TO THE NR 2 SPOILER UPPER AND LOWER SURFACES FROM WING STATIONS 354.75L TO WING STATIONS 359.2L IAW BOEING 737-300 SRM 51-70-10-2R4 FIG 203. 2L72 4F RTA16WE 20050920001302005092000130EU 2005 9 20 AWXA200501041 120050914A335032145410 POWER SUPPLY AIRBUS320 A320231 3930325EU EMERGENCY LIGHT INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28620AW1604318 052 ATL - EEL- DURING 8-DAY CHECK FOUND THE EMERGENCY EXIT SEAT ROW LIGHTS AT ROWS 13, 17, 19 AND 24 INOP. ALSO EMERGENCY LIGHTS AT PASSENGER ENTRY DOORS R2 & L2 INOP. MAINTENANCE REMOVED AND REPLACED THE LT AFT EMERGENCY POWER SUPPLY UNIT IAW AIRBUS MM 33-51-38. OPERATIONAL CHECKS WERE GOOD. VENDOR CONFIRMED FAUILURE. FOUND FUSE F2 OPEN. REPLACED FUSE AND TESTED UNIT IAW CMM 33-51-12 REV. 2. 2L72 4F RTA28NM 20050920001322005092000132WP 2005 9 20 MWEA050105 120050914A53305930495505 DOUBLER DOUG DC9 DC981 3022081WP INBOARD FLAP DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31805ME 48031 WHILE SWINGING LANDING GEAR, DAMAGED LOWER SURFACE OF INBOARD FLAP AND OUTBOARD VANE. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20050920001342005092000134EA 2005 9 20 SWIA200515553 120050516A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA BS 625 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07592SW 7279 FS 625 LT ANGLE STR 14L CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06. 2L72 4F RTA21EA 20050920001352005092000135EA 2005 9 20 SWIA200515554 120050912A2750 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07930SW 7713 FLAPS HALFSPEED STATUS MSG. REPLACED RIGHT BPSU IAW AMM 27-51-10, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050920001362005092000136EA 2005 9 20 SWIA200515555 120050914A274183963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07445SW6170 6170 7651 IN FLIGHT AT 31,000 FT RECEIVED STAB TRIM AND MACH TRIM CAUTION MSG. REPLACED HSTCU AND MOTOR CONTROL UNIT IAW 27-23-01 AND RII 27-415. P/N 7062-3, S/N OFF 319. 2L72 4F RTA21EA 20050920001372005092000137NM 2005 9 20 AWXA200501052 120050825A5313655292890 STRINGER BOEING737 7373Y0 1384671NM ZONE 200 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED EXFOLIATION CORROSION AT STRINGER 22L FROM BS 894 TO BS 900. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-00-03-1A1 FIG 101. MAINTENANCE REMOVED STRINGER 22L IAW BOEING 737-300 SRM 53-00-03-2R. FABRICATED REPLACEMENT ANGLES AND CHANNEL IAW BOEING 737-300 SRM 53-00-03-2R1. RECEIVED AND DRILLED NEW STRINGER IAW BOEING 737-300 SRM 51-40-02. INSTALLED REPAIR PARTS AT STRINGER 22L BETWEEN BS 894 AND BS 900 IAW BOEING 737-300 SRM 53-00-03-2R. 2L72 4F RTA16WE 20050920001382005092000138NM 2005 9 20 AWXA200501053 120050824A53306545800113 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED FUSELAGE SKIN CRACKED AT THREE FASTENER HOLES LOCATED AT THE R1 DOOR CUTOUT LOWER AFT CORNER. MAINTENANCE REMOVED DAMAGED SKIN AND PREVIOUS REPAIR DOUBLER LOCATED IN SAME AREA IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5311-0521-ES1. FABRICATED REPAIR DOUBLER, TRIPLER, QUADRUPLER AND FILLERS IAW AWA ER 03-5311-0521-ES1. FABRICATED REPAIR PARTS WERE INSTALLED AT THE R1 DOOR CUTOUT LOWER AFT CORNER IAW AWA ER 03-5311-0521-ES1. 2L72 4F RTA16WE 20050920001392005092000139NM 2005 9 20 AWXA200501054 120050824A5330654577881 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED SKIN CRACK AT FASTENER HOLE LOCATED AT THE R2 DOOR CUTOUT LOWER FORWARD CORNER. MAINTENANCE CUT OUT DAMAGED SKIN IAW BOEING 737-300 SRM 53-00-01-2R. FABRICATED DOUBLER, TRIPLER AND FILLER IAW BOEING 737-300 SRM 53-00-01-2R. INSTALLED REPAIR PARTS AT THE R2 DOOR CUTOUT LOWER FORWARD CORNER IAW BOEING 737-300 SRM 53-00-01-2R 32 FIG 201. 2L72 4F RTA16WE 20050920001402005092000140NM 2005 9 20 AWXA200501055 120050824A53476546815101 SEAT TRACK BOEING737 7373Y0 1384671NM ZONE 200 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED CORROSION ON SEAT TRACK AT BS 827, BL 24L, WL 208. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS IAW BOEING 737-30 SRM 53-00-52-1A FIG 101. CUT OUT DAMAGED SECTION OF SEAT TRACK AT BS 827, BL 24L, WL 208 IAW BOEING 737-300 SRM 53-00-52-2R4 FIG 20. RECEIVED AND DRILLED NEW SEAT TRACK AND SPLICES IAW BOEING 737-300 SRM 53-00-52-2R-3 FIG 201. INSTALLED SEAT TRACK AT BS 827, BL 24L, WL 208 IAW BOEING 737-300 SRM 53-00-52-2R 3 FIG 201. 2L72 4F RTA16WE 20050920001412005092000141NM 2005 9 20 AWXA200501056 120050825A53306545800602 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED FUSELAGE SKIN CRACKED AT FASTENER HOLE LOCATED AT L1 DOOR CUTOUT AFT LOWER CORNER. MAINTENANCE CUT OUT DAMAGED SKIN, DOUBLER AND BEAR STRAP AT THE L1 DOOR AFT LOWER CORNER IAW AMERICA WEST AIRLINES ENGINEERING REPAIR 03-5300-05248-SS1. FABRICATED DOUBLER, TRIPLER AND FILLER IAW AWA ER 03-5300-05248-SS1. INSTALLED FABRICATED REPAIR PARTS AT L1 DOOR CUTOUT AFT LOWER CORNER IAW AWA ER 03-5300-05248-SS1. 2L72 4F RTA16WE 20050920001422005092000142NM 2005 9 20 AWXA200501057 120050824A5730654540717 SKIN BOEING737 7373Y0 1384671NM ZONE 500 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED CORROSION ON TOP LEFT WING INTERSPAR SKIN AT BS 616, STR 9L, WS 78L. MAINTENANCE BLENDED OUT CORROSION AND FOUND TO BE OUT OF LIMITS PER BOEING 737-300 SRM 57-20-01 FIG 101. FABRICATED REPAIR ANGLE IAW AMERICA WEST AIRLINES ENGINEERING REQUEST 03-5723-05259-ES1. INSTALLED FABRICATED REPAIR PARTS ON TOP LEFT WING INTERSPAR AT BS 616, STR 9L, WS 78L IAW AWA ER 03-5723-05259-ES1. 2L72 4F RTA16WE 20050920001432005092000143NM 2005 9 20 AWXA200501058 120050909A53206545834377 INTERCOSTAL BOEING737 7373G7 1384595NM ZONE 200 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED INTERCOSTAL CRACKED AT BS 345, BL 0, WL 208. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT BS 345 IAW BOEING 737-300 SRM 51-40-02-0G. RECEIVED NEW INTERCOSTAL AND PREPPED FOR INSTALLATION IAW BOEING 737-300 SRM 51-40-02-0G. INSTALLED REPAIR PARTS IAW BOEING 737-300 SRM 51-40-02-0G PAR 7D, 4A AND FIG 8. 2L72 4F RTA16WE 20050920001442005092000144NM 2005 9 20 AWXA200501059 120050903A532069366565 SHEAR WEB BOEING737 7373G7 1384595NM ZONE 200 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - MAJOR REPAIR - DURING C18 CHECK DISCOVERED INTERCOSTAL LOWER LEG CRACKED IN RADIUS AT BS 933, BL 0, AND WL 202. MAINTENANCE REMOVED CRACKED INTERCOSTAL IAW BOEING 737-300 SRM 51-40-02-0G. RECEIVED NEW INTERCOSTAL AND PREPPED FOR INSTALLATION IAW BOEING 737-300 SRM 51-40-02-0G. INSTALLED REPAIR PARTS IAW BOEING 737-300 SRM 51-40-02-0G FIGS 8, 2, 3, AND 12. 2L72 4F RTA16WE 20050920001452005092000145NM 2005 9 20 AWXA200501060 120050831A57536546435 SKIN BOEING737 7373G7 1384595NM ZONE 500 DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - MAJOR REPAIR - DURING C18 CHECK DISCOVERED AREA OF DISBOND LOCATED ON THE UPPER AND LOWER SURFACE OF THE LEFT HAND OUTBOARD FLAP FROM WS 230.68L TO WS 237.68L. MAINTENANCE REMOVED AREA OF DISBOND FROM LT OUTBOARD FLAP IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED CORE AND DOUBLER IAW BOEING 737-300 SRM 51-70-10-ER4. BONDED REPAIR PARTS TO LOWER SURFACE OF THE LEFT HAND OUTBOARD FLAP FROM WS 230.68L TO WS 237.68L IAW BOEING 737-300 SRM 51-70-10-2 R4 FIG 203. 2L72 4F RTA16WE 20050920001462005092000146NM 2005 9 20 AWXA200501061 120050903A534065C25482515 CLIP BOEING737 7373G7 1384595NM ZONE 200 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - MAJOR REPAIR - DURING C18 CHECK DISCOVERED ATTACH CLIP CRACKED AT BS 696, BL 01L. MAINTENANCE REMOVED CRACKED CLIP IAW BOEING 737-300 SRM 51-40-02-0G. FABRICATED REPLACEMENT CLIP IAW BOEING 737-300 DWG 65C25482. INSTALLED FABRICATED REPAIR PARTS AT BS 696, BL 01L IAW BOEING 737-300 SRM 51-40-02-0G FIGS 8 AND 12. 2L72 4F RTA16WE 20050920001472005092000147NM 2005 9 20 AWXA200501062 120050908A5322654583311 SHEAR TIE BOEING737 7373G7 1384595NM ZONE 200 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - MAJOR REPAIR - DURING C18 CHECK DISCOVERED FLOOR SHEAR TIE CRACKED AT BS 196, BL 29R AND WL 207. MAINTENANCE REMOVED CRACKED SHEAR TIE IAW BOEING 737-300 SRM 51-40-02-0G. FABRICATED NEW SHEAR TIE AND PREPPED FOR INSTALLATION IAW BOEING 737-300 SRM 51-40-05-0G. INSTALLED FABRICATED REPAIR PARTS IAW BOEING 737-300 SRM 51-40-05-0G AND 51-40-02-0G FIG 12. 2L72 4F RTA16WE 20050920002042005092000204CE 2005 9 20 S2YA05048 120050815A2797 WIRE BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA TE FLAPS DAMAGED A S2YAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 GL1391SK UE91 SHORTLY AFTER TAKEOFF, THE CREW REPORTED THE FLAPS WILL NOT RETRACT. AFTER CONSULTING WITH DISPATCH AND MAINTENANCE, THE CREW PERFORMED AN AIR-TURN-BACK. MAINTENANCE FOUND A CHAFED WIRE AT THE LT SAFETY SWITCH. MAINTENANCE REPAIRED THE WIRE, OPS CHECKED THE SYSTEM AND WITH NO FURTHER DEFECTS RETURNED THE AC TO SERVICE. (K) 2L72 4T3 TRTA24CE E2NE 20050920002082005092000208EU 2005 9 20 USAA051014 120050817A53151161432 FLOORBEAM AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19110UW13254 1112 PIT - S2 - FLOORBEAM, 2 INCH X 6 INCH CORROSION, LEVEL 2; TASK JA-220-53500, 9 INCHES RT OF CENTER FROM FRAME C16 TO C21. REPLACED IAW SRM. (K) 2L72 4F4 FRTA28NM E38NE 20050921000082005092100008NM 2005 9 21 2005UALA00992 120050916A3350 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29127UA 28813 EEL INOP AT SEAT 4A FWD, 22B AFT, 5F AFT, AND 3J AFT SECTIONS. REPLACED EEL LAMP. 2L74 4F4 FRTA20WE E24NE 20050921000202005092100020NE 2005 9 21 2005UALA00961 220050909A7230 COMPRESSOR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 2 ENGINE STALLED A UALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 WP29461UA 1266 V10064 NR 2 ENGINE COMPRESSOR STALL. QTY 1 HPC R6 BLADE FRACTURED ON THE AIRFOIL. THIS, ALONG WITH SECONDARY DAMAGE FROM THE RELEASED BLADE, DEGRADED THE COMPRESSOR'S PERFORMANCE WHICH CAUSED THE OPERATIONAL PROBLEMS. 2L72 4F4 FRTA28NM E40NE 20050921000232005092100023NM 2005 9 21 2005UALA00964 120050909A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29505UA 24626 ON ARRIVAL FOUND TWO EA DENTS ON FUSELAGE JUST FWD & BELOW WATERLINE OF DOOR 2L. DENTS ARE ON AN EXISTING DOUBLER. *S/D* FOUND AT RATIO OF 15.5 TO BE BEYOND LIMITS IN SRM 53-00-01 PG 103. DAMAGE IS DEFERRABLE AS PER SRM 53-00-01 PG 102 ITEM I. 2L72 4F4 FRTA2NM E17NE 20050921000252005092100025NM 2005 9 21 2005UALA00966 120050909A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE BS 1420 DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29505UA 24626 DENT ON PIT FRAME STA 1420, STR 24L. TRIMMED OUT DAMAGE, INSURANCE CUT, INSTALLED NEW PRODUCTION SPLICE AND ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20050921000272005092100027NM 2005 9 21 2005UALA00968 120050909A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE BS 600 DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29505UA 24626 FWD PIT FRAME IS DENTED AT STA 600, BETWEEN STR 24L AND 25L. TRIMMED OUT DAMAGE WITH INSURANCE CUT, FAB J-ANGLE AND INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050921000472005092100047 2005 9 21 QXEA200501234 420050918A31309804700001 RECORDER DHAV DHC8 DHC8202 2809007NM CABIN MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09348PH15103 484 SEA FLIGHT NR 2054 INFLIGHT, THE FLIGHT DATA RECORDER CAUTION LIGHT COMES ON INTERMITTENTLY, CIRCUIT BREAKERS VERIFIED IN (A9-AVIONIC, G2-L ESS-H2 L ESS) AS PER EMERGENCY ABNORMAL CHECKLIST. MAINTENANCE REPLACED FDR IAW AMM 31-31-05, PAGES 401-404. COMPLIED WITH ULB FUNCTION TEST IAW MTC 5313001. ALL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050921000492005092100049EU 2005 9 21 05FDEA02956 120050916A2410 GENERATOR AIRBUS300 A300B4605R 3930308EU APU FAILED A FDEAA UNSCHED LANDING HB ELECT. POWER LOSS-50 PC SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO25662FE 761 CLIMBING OUT AT 22,000 FT NR 2 GEN FAULTED WITH IMMEDIATE ACRID ELEC SMOKE SMELL/FUMES. NO OTHER FAULTS. C/W ECAM. DECLARED EMERGENCY AND RETURNED TO KORD IN 19 MIN "MEL 24-23-01: APU GEN SYSTEM INOP." FOUND EVIDENCE OF WATER IN AREA OF NR 2 ENG GEN CONTROL UNIT. CLEANED RESIDUAL MOISTURE FROM AREA AND SWAPPED NR 2 GEN CONT WITH APU GEN CONT, DEFERRED APU GEN CONT UNIT. REF AMM 24-22-12-4. SWAP COMPONENT POSITIONS. 2L72 4F RTA35EU 20050921000542005092100054EA 2005 9 21 MASA200500690 120050901A2721 TRIM SYSTEM CNDAIRCL600 CL6002B19 1900309EA RUDDER OUT OF ADJUST A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07154SF 7154 ASH 2897 PHL. ABORTED A TAKEOFF DUE TO A TAKEOFF CONFIG ISSUE. AFTER BRINGING THE PLANE TO A STOP THE CAPTAIN NOTICED HIS RUDDER TRIM WAS NOT ALIGNED. RE-ALIGNED TRIM AND THE MESSAGE WENT AWAY. 2L72 4F RTA21EA 20050921000572005092100057NE 2005 9 21 MASA200500689 220050902A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 1 MALFUNCTIONED A MASAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 SW0777181 7181 872898 ASH 2828 CLE. ABORTED TAKEOFF DUE TO THE NR 1 ENG WOULD NOT ACCELERATE PAST 70 PERCENT N1. CONTRACT MAINTENANCE PERFORMED A VISUAL INSPECTION OF THE FAN AND ENGINE AREAS AND FOUND NO DEFECTS. PERFORMED ENGINE RUNS AND THE DISCREPANCY COULD NOT BE DUPLICATED. 2L72 4F4 FRTA21EA E15NE 20050922000102005092200010NM 2005 9 22 0509001 120050919A534065244912 STRINGER CLIP BOEING737 7372H4 138448CNM BS 332 CRACKED A MJYAK NONE O OTHER ININSP/MAINT 1 SW05733TW 22732 FORWARD SERVICE DOORWAY AREA, STA 332 STRINGER 8R AREA, T-CLIP IS CRACKED. 2L72 4F A16WE 20050922000202005092200020NM 2005 9 22 2005UALA00981 120050912A2120 ODOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE COCKPIT DETECTED A UALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP29543UA 25698 ACRID OIL SMELL IN COCKPIT THROUGHOUT FLIGHT. ACCOMPLISHED ENGINE BURNOUT PROCEDURE PER MM21-00-01 PG210. SMELL DIMINISHED AFTER ENGINE RUN. RETURNED AIRCRAFT TO SERVICE. 2L72 4F4 FRTA2NM E17NE 20050922000292005092200029NM 2005 9 22 05FDEA02982 120050918A55336517506 WEB BOEING727 727227 1384078NM VERTICAL STAB CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 VERTICAL STABILIZER 1303 WEB IS CRACKED AT LOWER LT CORNER. REPAIRED VERT STAB 1303 WEB IAW SRM 51-40-2. 2L73 4F A3WE 20050922000382005092200038EA 2005 9 22 MASA200500599 120050728A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07571ML 7209 ASH 2772 PHL. CREW REPORTED A SECTION OF EMERGENCY EXIT FLOOR PATH LIGHTING INOP. MAINTENANCE REPLACED THE LIGHT STRIP. 2L72 4F RTA21EA 20050922000482005092200048EU 2005 9 22 USAA051123 120050920A5320 FLOOR SUPPORT AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19733UW 1205 FOUND CORROSION TOP OF FLOOR SUPPORT/BEAM Y254 AT FRAME C19. CUT OUT DAMAGE, INSTALLED FILLER AND REPAIR ANGLES PER SRM 53-00-14 PG 222, 224 FIG 204. 2L72 4F RTA28NM 20050922000702005092200070NM 2005 9 22 USAA051105 120050920A5551657378211 ATTACH FITTING BOEING737 7374B7 1384702NM HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 FOUND CORROSION FWD FACE OF L13 HOR STAB LUG. REMOVED CORROSION AND INSTALLED BUSHING IAW SRM 55-10-10, DEFECT SIZE: 1" X 2" AREA OF CORROSION. 2L72 4F RTA16WE 20050922000712005092200071NM 2005 9 22 USAA051130 120050920A5320US655169821F SPLICE BOEING737 7374B7 1384702NM BS 907 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19776AU 24934 FOUND CRACK FUSELAGE STRINGER SPLICE AT STA 907 STR 4R. INSTALLED STRINGER SPLICE IAW SRM 51-40-02, DEFECT SIZE: .25". 2L72 4F RTA16WE 20050922000722005092200072NM 2005 9 22 USAA051103 120050920A5551657378211 ATTACH FITTING BOEING737 7374B7 1384702NM HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 FOUND FWD FACE OF L4 LUG FWD CLEVIS OF LT HOR STAB. REMOVED CORROSION AND INSTALLED BUSHING IAW SRM 55-10-10, DEFECT SIZE: 1" X 2" AREA OF CORROSION. 2L72 4F RTA16WE 20050922000742005092200074NM 2005 9 22 USAA051101 120050920A5320 WEB BOEING737 7374B7 1384702NM BS 500G CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 FOUND CRACK 500G, S-27R. FAB FILLER AND DOUBLER PER SRM 51-70-11, DEFECT SIZE: 0.25" CRACK IN WEB. 2L72 4F RTA16WE 20050922000752005092200075NM 2005 9 22 USAA051100 120050920A5313 STRINGER BOEING737 7374B7 1384702NM BS 907 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 FOUND CRACK PRODUCTION SEAM AT STA 907 IN STR 4L. REMOVED CRACKED STRINGER SPLICE, INST NEW P/N 1122424 STR SPLICE, CLIP AND LADDER IAW SRM 51-10-02, DEFECT SIZE: PRODUCTION SEAM AT STA 907 IN STR 4L. (MARKED) 2L72 4F RTA16WE 20050922000772005092200077NM 2005 9 22 USAA051098 120050920A5340 BRACKET BOEING737 7374B7 1384702NM BS 500G CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 FOUND CRACK STA 500G, S28R. FAB`D NEW ANGLE FROM 2024-T3 .040 PER DWG 69-73527 IAW SRM 51-10-02, DEFECT SIZE: .250" CRACK IN RADIUS. 2L72 4F RTA16WE 20050922000792005092200079EU 2005 9 22 USAA051126 120050920A5315D5347209300000 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19730US 1182 FOUND CORROSION Y 765 FLOORBEAM. REMOVED AND REPLACED BEAM WITH IDENTICAL PART NR, DEFECT SIZE: 4" X 4". 2L72 4F RTA28NM 20050922000802005092200080EU 2005 9 22 USAA051125 120050920A5315 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19732US 1203 FOUND CORROSION BETWEEN FR 13 AND 15. REPLACED BEAM PER SRM 51-72-11, DEFECT SIZE: 1" X 2". 2L72 4F RTA28NM 20050922000812005092200081NM 2005 9 22 USAA051106 120050920A5510657378211 ATTACH FITTING BOEING737 7374B7 1384702NM HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 FOUND CORROSION AFT FACE OF L6 HORIZ STAB LUG. REMOVED CORROSION AND INSTALLED BUSHING IAW SRM 55-10-10, DEFECT SIZE: 1" X 2" AREA OF CORROSION. 2L72 4F RTA16WE 20050922000842005092200084EA 2005 9 22 MASA200500718 120050909A5270 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA PAX DOOR FALSE INDICATIONA MASAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW07570ML 7206 ASH 6287 STL. PAX DOOR OUTER HANDLE CAUTION MESSAGE IN FLIGHT, OVERBOARD COOL MESSAGE AND UPON LANDING. FERRIED PLANE TO PHL TO COMPLY WITH OVERWEIGHT LANDING INSPECTION AND PAX DOOR RIGGING. MX COULD NOT DUPLICATE. 2L72 4F RTA21EA 20050922000862005092200086EU 2005 9 22 AWXA200501063 120050904A5315D53472188202 FLOORBEAM AIRBUS320 A320231 3930325EU CABIN CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28634AW 091 DURING C4 CHECK, DISCOVERED EXFOLIATION CORROSION LOCATED ON FLOORBEAM AT FR 68, Y1292. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-14. REMOVED FLOORBEAM AT FR68, Y1292 IAW AIRBUS 320 SRM 51-72-11. INSTALLED NEW FLOORBEAM AT FR68, Y1292 IAW AIRBUS 320 SRM 51-72-11. 2L72 4F RTA28NM 20050922000872005092200087EU 2005 9 22 AWXA200501064 120050901A5315D53472189202 FLOORBEAM AIRBUS320 A320231 3930325EU CABIN CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28634AW 091 DURING C4 CHECK DISCOVERED, GALVANIC CORROSION LOCATED ON FLOORBEAM AT FR 68, Y-1292. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-14. REMOVED FLOORBEAM AT FR68, Y-1292 IAW AIRBUS 320 SRM 51-72-11. INSTALLED NEW FLOORBEAM AT FR68, Y-1292 IAW AIRBUS 320 SRM 51-72-11. 2L72 4F RTA28NM 20050922000892005092200089EU 2005 9 22 AWXA200501066 120050904A5315D5347219320000 FLOORBEAM AIRBUS320 A320231 3930325EU CABIN CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28634AW 091 DURING C4 CHECK, DISCOVERED GALVANIC CORROSION LOCATED ON FLOORBEAM FROM FR 66+8 TO FR 68, Y-765. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-14. REMOVED FLOORBEAM FROM FR 66+8 TO FR 70, Y-765 IAW AIRBUS 320 SRM 51-72-11. INSTALLED NEW FLOORBEAM FROM FR 66+8 TO FR70, Y-765 IAW AIRBUS 320 SRM 51-72-11. 2L72 4F RTA28NM 20050922000912005092200091EU 2005 9 22 AWXA200501068 120050904A5315D53472090005 FLOORBEAM AIRBUS320 A320231 3930325EU CABIN CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28634AW 091 DURING C4 CHECK, DISCOVERED GALVANIC CORROSION LOCATED ON FLOORBEAM FROM FR 64 TO FR 66, Y-1292. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-14. REMOVED FLOORBEAM FROM FR 64 TO FR 66, Y-1292 IAW AIRBUS 320 SRM 51-72-11. INSTALLED NEW FLOORBEAM FROM FR 64 TO FR 66, Y-1292 IAW AIRBUS 320 SRM 51-72-11. 2L72 4F RTA28NM 20050922000942005092200094EU 2005 9 22 AWXA200501071 120050904A5320D53112821200 FLOOR SUPPORT AIRBUS320 A320231 3930325EU CABIN CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28634AW 091 DURING C4 CHECK, DISCOVERED EXFOLIATION CORROSION LOCATED ON FLOOR SUPPORT FROM FS 19 TO FS 20, Y-254. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-14. REMOVED FLOOR SUPPORT FROM FS 12 TO FS 24, Y-254 IAW AIRBUS 320 SRM 51-72-11. INSTALLED NEW FLOOR SUPPORT FROM FS 12 TO FS 24, Y-254 IAW AIRBUS 320 SRM 51-72-11. 2L72 4F RTA28NM 20050922000952005092200095EU 2005 9 22 AWXA200501074 120050918A2910AE2463921G0181 LINE AIRBUS320 A320231 3930325EU HYD SYSTEM RUPTURED A AWXAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP28633AW 082 LAS - AIR TURN BACK - FLT 372 - DURING CLIMB, CREW RECEIVED GREEN HYDRAULIC LOW RESERVOIR MESSAGE AFTER SHORTLY RAISING GEAR. RETURNED TO LAS AND LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT WAS TOWED BACK TO THE GATE. MAINTENANCE FOUND THE LT LANDING GEAR DOOR ACTUATOR LINE FAILED. REPLACED LINE AND SERVICED SYSTEM. LEAK CHECKS WERE GOOD. 2L72 4F RTA28NM 20050922001002005092200100EU 2005 9 22 09142005A 120050913A5210 TAB SAAB SF340 340B 7860101EU PAX DOOR MISSING A NSVAO OTHER O OTHER TXTAXI/GRND HDL 1 EA27299CJ 299 LOWER SAFETY DOOR LOCKING TAB MISSING. FOUND INDICATOR IN PLACE, ORANGE COLOR IS FADED, DMI'ED. 2L72 4T RTA52EU 20050922001012005092200101EU 2005 9 22 09152005A 120050914A2420M832481210 PACKING SAAB SF340 340B 7860101EU A/C GENERATOR LEAKING A NSVAB EMER. DESCENT KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA27346CJ 346 RT ENGINE OIL LIGHT, CREW SHUT DOWN ENGINE. FOUND PGB OIL LOW AND OIL AROUND AC GENERATOR, REMOVED AC GEN FOUND O-RING COCKED. REMOVED AND REPLACED O-RING, OPS AND LEAK CHECK GOOD. 2L72 4T RTA52EU 20050922001022005092200102CE 2005 9 22 09152005B 120050914A2621MS21353341 SWITCH BEECH 1900 1900D 1154162CE FIRE TEST FAILED A NSVAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 EA2760MJ UE60 LT ENGINE FIRE BOTTLE DISCHARGE LIGHT ILLUMINATED INTERMITTENTLY THEREAFTER. BOTTLE PRESSURE READS NORMAL. REMOVED AND REPLACED UPPER LT FIRE TEST SWITCH IAW 31-10-00, OPS CHECK GOOD. 2L72 4T RTA24CE 20050922001042005092200104EU 2005 9 22 09192005C 120050918A6123 PROPELLER SAAB SF340 340B 7860101EU MALFUNCTIONED A NSVAO OTHER O OTHER TXTAXI/GRND HDL 1 EA27321CJ 321 LT PROP WILL NOT COME OUT OF FEATHER, MEL'ED. 2L72 4T RTA52EU 20050922001052005092200105EU 2005 9 22 09202005A 120050919A75008957312763 CLAMP SAAB SF340 340B 7860101EU BLEED AIR LEAKING A NSVAC ABORTED TAKEOFF O OTHER TXTAXI/GRND HDL 1 EA27252CJ 252 LT ITT RISING. ABORTED TAKEOFF. REMOVED AND REPLACED LT HP BLEED CLAMP. 2L72 4T RTA52EU 20050922001062005092200106NM 2005 9 22 USAA051131 120050920A5311 FRAME BOEING737 7374B7 1384702NM BS 294.5 DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 BS 294.5, S-17R, CUT OUT DAMAGE, FABRICATED NEW ATTACH ANGLE AND INSTALLED IAW SRM 51-70-11 TABLE 5 OF FIG NR 1, DEFECT SIZE: .5" CRACKED DOOR FRAME. 2L72 4F RTA16WE 20050922001072005092200107NM 2005 9 22 USAA051132 120050920A5312 PRESSURE PANEL BOEING737 7374B7 1384702NM BS 665 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 FOUND CRACK STA 665, LBL 30. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW TR 53-60-04, DEFECT SIZE: 1.0" CRACK. 2L72 4F RTA16WE 20050922001082005092200108SO 2005 9 22 RAIA00509023 120050915A3350 LIGHT EMB 145 EMB145 3260210SO CABIN INOPERATIVE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03802HK 145066 FLT 3537 - BNA - EMERGENCY LIGHT ON FWD BULKHEAD INOP. MAINTENANCE RESEATED CONTACT ON LIGHT STRIP. 2L72 4F RTT00011AT 20050922001102005092200110SO 2005 9 22 RAIA00509024 120050916A3350 LIGHT EMB 145 EMB145LR 3260212SO ROW 12A INOPERATIVE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03817HK 145058 FLT 5517 - STL - EMERGENCY LIGHT INOP AT 12A. MAINTENANCE RESEATED BULB. 2L72 4T RTT00011AT 20050922001112005092200111SO 2005 9 22 RAIA00509025 120050916A326023092900001 UPLOCK EMB 145 EMB145LR 3260212SO RT MLG FAILED A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03814HK1672316723 145046 FLT 5501 - STL - LANDING GEAR LEVER DISAGREE WHEN GEAR IS UP. MAINTENANCE REMOVED AND REPLACED RIGHT MLG UPLOCK UNIT. 2L72 4T RTT00011AT 20050922001122005092200112GL 2005 9 22 RAIA00509028 220050917A7200 ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 1 OVERTEMP A RAIAC ABORTED TAKEOFF MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 CE03817HK 145058 FLT 5503 - DEN - NR 1 ITT AT 920 DEGREES AT TAKEOFF. MAINTENANCE PERFORMED ENGINE OPS CHECK. 2L72 4T4 FRTT00011ATTE6CH 20050922001132005092200113SO 2005 9 22 RAIA0050929 120050918A3397 CONTACT EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT LOOSE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03817HK 145058 FLT 5498 - STL - EMERGENCY EXIT DOOR LIGHT INOP. MAINTENANCE RESEATED CONTACT TO LEFT EMERGENCY EXIT LIGHT ASSEMBLY. 2L72 4T RTT00011AT 20050922001142005092200114SO 2005 9 22 RAIA00509026 120050916A7830 WARNING LIGHT EMB 145 EMB145LR 3260212SO THRUST REVERSER ILLUMINATED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03817HK 145058 FLT 5488 - STL - NR 2 THRUST REVERSER DISAGREE MSG. MAINTENANCE DEFERRED THRUST REVERSER SYSTEM. 2L72 4T RTT00011AT 20050922001152005092200115SO 2005 9 22 RAIA00509022 120050915A3397 WIRE EMB 145 EMB145EP 3260221SO EMERGENCY LIGHT BROKEN A RAIAK NONE O OTHER ININSP/MAINT 1 CE03826HK 145016 FLT 5478 - STL - CENTER FLOOR EMERGENCY LIGHT STRIP INOP. MAINTENANCE REPLACED BROKEN WIRE TO TRACK ASSEMBLY. 2L72 4F RTT00011AT 20050922001162005092200116NM 2005 9 22 SWAA052863 120050920A3350101114 LENS BOEING737 7373Q8 1384670NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT SIDEWALL LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20050922001182005092200118NM 2005 9 22 SWAA052865 120050920A53116545810 FRAME BOEING737 7373L9 1384470NM BS 312 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 312, STR 6R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050922001192005092200119NM 2005 9 22 SWAA052866 120050920A53206551698 SPLICE BOEING737 7373L9 1384470NM BS 359 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER SPLICE CRACKED AT BS 359, STR 15L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20050922001232005092200123NM 2005 9 22 05FDEA02991 120050918A5744 ATTACH FITTING DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 L WING, O/B FLAP I/B HINGE (WING SIDE), FWD ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. CORRECTIVE ACTION: SNRM N1225: LH WING- O/B FLAP I/B HINGE (WING SIDE), FWD ATTACHMENT O/B HOLE SPOT FACE CORROSION REPAIR CARRIED OUT AS PER EA#1-5750-87637 TITLE: WINGS- TRAILING EDGE AND TRAILING EDGE DEVICES- L/H OUTBD FLAP INBD HINGE BRACKET REPAIR. ORIGINAL THK 0.374" REMAINING THK 0.371" MATERIAL REMOVED 0.003". MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20050922001272005092200127NM 2005 9 22 SWAA052851 120050920A53306545767 SKIN BOEING737 7373H4 1384600NM BS 480-518 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT STR 16L, BETWEEN BS 480 & BS 518. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050922001292005092200129 2005 9 22 SWAA052853 420050920A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29352SW 24888 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20050922001322005092200132NM 2005 9 22 SWAA052856 120050920A53306552988 DOUBLER BOEING737 7373H4 1384600NM BS 983 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DOUBLER CORRODED AT BS 983, STR 23R TO STR 24R. REPAIRED SKIN DOUBLER PER SRM. 2L72 4F RTA16WE 20050922001332005092200133NM 2005 9 22 SWAA052857 120050920A53116546564 FRAME BOEING737 7373H4 1384600NM BS 993 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29618WN 28034 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 993, RBL 46, WL 208. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050922001362005092200136NM 2005 9 22 SWAA052860 120050920A53116546533 SHEAR TIE BOEING737 7373H4 1384600NM BS 500 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29618WN 28034 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500, STR 28L TO STR 28R. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050922001372005092200137NM 2005 9 22 SWAA052861 120050920A53116558280 FRAME BOEING737 7373H4 1384600NM BS 360 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29618WN 28034 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R TO STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050922001382005092200138NM 2005 9 22 SWAA052862 120050920A53116546525 FRAME BOEING737 7373H4 1384600NM BS 380 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29618WN 28034 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L TO STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050923000012005092300001NM 2005 9 23 TSAA0577041 120050919A7700 LINE BOEING737 7372X6C 1384552NM PT2 SENSE OBSTRUCTED A TSAAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 WP13817AL 23292 CARGO FLT 820 HNL-OGG. AT CRUISE, CREW NOTED NR 1 ENGINE EPR 0.30 LESS THAN NR 2 ENGINE. N1 AND N2 SAME ON BOTH ENGINES. CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED DEBRIS FROM THE NR 1 PT2 SENSE LINE PER AMM 72-00-00 AND RETURNED THE AIRCRAFT TO SERVICE. 2L72 4F RTA16WE 20050923000022005092300002NM 2005 9 23 PIDA20050114 120050907A5320 SUPPORT BRACKET BOEING737 737228 13844AGNM BS 737 CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 VHF ANTENNA SUPPORT, RIGHT CENTER BRACKET AT BS 767 +12 IS CRACKED. REPLACED BRACKET PER DWG 66-13842 AND SRM 51-10-0. 2L72 4F RTA16WE 20050923000042005092300004 2005 9 23 RAIA00509030 420050918A3140 COMPUTER EMB 145 EMB145 3260210SO MALFUNCTIONED A RAIAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 CE03809HK 145187 FLT 3571 - PIT - AT 20 KTS ON TAKEOFF ROLL RECEIVED CHECK IC 2 CAUTION MESSAGE ON EICAS. MAINTENANCE RERACKED IC 600 CPU. 2L72 4F RTT00011AT 20050923000062005092300006NM 2005 9 23 AWXA200501076 120050903A532065479737 WEB BOEING737 7373G7 1384595NM BS 578 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 DURING C18 CHECK, DISCOVERED SHEAR WEB CRACKED, 2.3 INCHES, JUST FORWARD OF BS 578, WL 204, BL 70L. MAINTENANCE REMOVED CRACKED SHEAR WEB IAW BOEING 737-300 SRM 51-40-02-0G. FABRICATED NEW SHEAR WEB IAW BOEING 737-300 DWG 65-47973. INSTALLED FABRICATED REPAIR PARTS FORWARD OF BS 578, WL 204, AND BL 70L IAW BOEING 737-300 SRM 51-40-02-0G. 2L72 4F RTA16WE 20050923000102005092300010EU 2005 9 23 AWXA200501080 120050903A5347D5337111000800 SEAT TRACK AIRBUS320 A320231 3930325EU FR 41-47 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28634AW 091 DURING C4 CHECK, DISCOVERED GALVANIC CORROSION ON LT INBOARD SEAT TRACK FROM FR 41 TO FR 47, Y765. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 101. MAINTENANCE REMOVED SEAT TRACK FROM FR 41 TO FR 47, Y765 IAW AIRBUS 320 SRM 51-42-11. RECEIVED NEW SEAT TRACK AND INSTALLED FROM FR 41 TO FR 47 AND Y765 IAW AIRBUS 320 SRM 51-42-11 AND 51-72-11. 2L72 4F RTA28NM 20050923000112005092300011EU 2005 9 23 AWXA200501081 120050903A5347D57130147202 SEAT TRACK AIRBUS320 A320231 3930325EU FR 36-41 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28634AW 091 DURING C4 CHECK, DISCOVERED EXFOLIATION CORROSION ON LT OUTBOARD SEAT TRACK AT FR 36+17", Y1292. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 101. MAINTENANCE REMOVED SEAT TRACK FROM FR 36 TO FR 41, Y1292 IAW AIRBUS 320 SRM 51-42-11. RECEIVED NEW SEAT TRACK AND INSTALLED FROM FR 36 TO FR 41 AND Y1292 IAW AIRBUS 320 SRM 51-42-11 AND 51-72-11. 2L72 4F RTA28NM 20050923000122005092300012EU 2005 9 23 AWXA200501082 120050903A5347D5337111200400 SEAT TRACK AIRBUS320 A320231 3930325EU FR 41-47 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28634AW 091 DURING C4 CHECK, DISCOVERED EXFOLIATION CORROSION ON RT INBOARD SEAT TRACK AT FR 42+17", Y1292. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 101. MAINTENANCE REMOVED SEAT TRACK FROM FS 41 TO FS 47, Y1292 IAW AIRBUS 320 SRM 51-42-11. RECEIVED NEW SEAT TRACK AND INSTALLED FROM FR41 TO FR47, Y1292 IAW AIRBUS 320 SRM 51-42-11 AND 51-72-11. 2L72 4F RTA28NM 20050923000132005092300013EU 2005 9 23 AWXA200501083 120050903A5347D5713014720 SEAT TRACK AIRBUS320 A320231 3930325EU FR 36-41 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28634AW 091 DURING C4 CHECK DISCOVERED EXFOLIATION CORROSION ON RT INBOARD SEAT TRACK AT FS 38+18", Y-765. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 101. MAINTENANCE REMOVED SEAT TRACK FROM FS 36 TO FS 41, Y-765 IAW AIRBUS 320 SRM 51-42-11. RECEIVED NEW SEAT TRACK AND INSTALLED FROM FS 36 TO FS 41, Y-765 IAW AIRBUS 320 SRM 51-42-11 AND 51-72-11. 2L72 4F RTA28NM 20050923000192005092300019NM 2005 9 23 UPS05245467 120050823A5720 STIFFENER BOEING727 72731C 1384011NM LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01922UP 19231 INSPECTION TYPE:C-CRACK IN VERTICAL STIFFENER LT WING FRONT SPAR AT STA 557. STIFFENER REPLACED IAW SRM 51-30-2 AND DRW NR 65-16200. 2L73 4F A3WE 20050923000202005092300020NM 2005 9 23 UPS05245468 120050826A5753 FLAP TRACK BOEING727 72731C 1384011NM NR 4 FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01922UP 19231 INSPECTION TYPE:C-CORROSION ON NR 4 FLAP TRACK FWD MOUNTING UPPER AND LWR, ALSO INNER RADIUS OF HOLES. CORROSION REMOVED IAW SOPM 20-10-01 P1 AND EO B727-5742-0651K AND TEMPER ETCHED IAW SOPM 20-10-01. 2L73 4F A3WE 20050923000212005092300021NM 2005 9 23 UPS05245469 120050826A5753 FLAP TRACK BOEING727 72731C 1384011NM NR 4 FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01922UP 19231 INSPECTION TYPE:C-CORROSION FOUND ON FWD MOUNTING PAD OF NR 4 FLAP TRACK. CORROSION REMOVED IAW SOPM 20-10-01 P1 AND EO B727-5742-0651K. SURFACE TEMPER ETCHED 2B (3) IAW SOPM 20-10-01. CAD PLATED IAW OHM 20-42-10. 2L73 4F A3WE 20050923000232005092300023WP 2005 9 23 UPS05845471 120050809A5714 SPAR DOUG DC8 DC873F 302199FWP CENTER TANK CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 INSPECTION TYPE:C1 POSSIBLE CRACK ON LOWER SURFACE SKIN AFT CTR SPAR RT CTR AUX TANK. NDT VERIFIED 2 INCH CRACK AT RT CTR AUX TANK AFT CTR SPAR. REMOVED CRACKED SECTION OF CTR SPAR, FABRICATED REPLACEMENT SECTION OF CTR SPAR AND REPAIR PARTS, AND INSTALLED IAW SAA SK 809-851262. 2L74 4F RT4A25 20050923000252005092300025WP 2005 9 23 UPS05845475 120050911A5322 SHEAR TIE DOUG DC8 DC871F 302199DWP BS 35 L34R-L34L CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 INSPECTION TYPE:SP, AT STA 35 IN BETWEEN L34L AND L34R HAS CORROSION BEYOND LIMITS ON SHEAR TIE. REMOVED, FABRICATED AND INSTALLED SHEER TIE IAW SRM 53-03-01 FIG 003, 51-3-2, 51-1-21 AND 51-1-21. 2L74 4F RT4A25 20050923000292005092300029NM 2005 9 23 AALA20050610 120050909A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21974AN 30098 TUL - EMERGENCY LIGHTS AT SEATS 7F, 13F, 19F, AND AFT RIGHT HAND OVERHEAD AT STATION 967 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEATS 7F, 13F, 19F AND AFT RIGHT HAND OVERHEAD AT STATION 967. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20050923000302005092300030WP 2005 9 23 AALA20050609 120050919A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW213515 49892 DFW - CEILING EMERGENCY LIGHTS AT ROWS 13, 16, 23 AND 32DEF, AND 12, 16, 23, 25, 27AB AND FIRST CLASS AND FLIGHT ATTENDANT JUMP SEAT INOPERATIVE. REPLACED BATTERY PACKS FOR ROWS 13, 16, 23 AND 32DEF, AND 12, 16, 23, 25, 27AB AND FIRST CLASS AND FLIGHT ATTENDANT JUMP SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050923000322005092300032NM 2005 9 23 TSAA0536039 120050913A750032144464 VALVE BOEING737 73776N 13844CHNM NR 1 ENGINE FAILED A TSAAA UNSCHED LANDING S AFFECT SYSTEMS CRCRUISE 1 WP13741AL14241818 28641 ETOPS: FLT. 476 OGG-SAN: DUCT PRESSURE GRADUALLY SPLITS DURING CLIMB, AT CRUISE SPLIT IS 23 PSI, LEFT - 19 PSI, RIGHT - 42 PSI. AIRCRAFT DIVERTED TO HONOLULU AND COMPLETED AN OVERWEIGHT LANDING WITHOUT INCIDENT. FOUND HIGH STAGE VALVE AND PRSOV PRESSURE SENSE LINE LEAKING AIR. REMOVED AND REPLACED HIGH STAGE VALVE IAW AMM 36-11-06-4. OPS AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA16WE 20050923000352005092300035WP 2005 9 23 AALA20050598 120050915A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21584AA 53247 LAX - OVERWING EMERGENCY EXIT SIGNS ON TWO AFT OVERWING EXIT DOORS INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING EMERGENCY EXIT SIGNS ON TWO AFT OVERWING EXIT DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050923000382005092300038NM 2005 9 23 AALA20050599 120050916A3350 LIGHT BOEING777 777223 1385213NM GALLEY DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21776AN 29582 MIA - MOUNTED EMERGENCY LIGHT AT FORWARD GALLEY CLOSET DAMAGED. REPLACED MOUNTED EMERGENCY LIGHT AT FORWARD GALLEY CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20050923000412005092300041EU 2005 9 23 AALA20050597 120050915A3350P4010049 BATTERY PACK AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217055A 462 JFK - EMERGENCY AISLE LIGHT ON RIGHT HAND SIDE FIRST CLASS AND NUMBER ONE RIGHT DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY AISLE LIGHT ON RIGHT HAND SIDE FIRST CLASS AND NUMBER ONE RIGHT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20050923000432005092300043CE 2005 9 23 09212005B 120050919A5220 HANDLE BEECH 1900 1900D 1154162CE EMERGENCY EXIT OUT OF RIG A NSVAO OTHER O OTHER TXTAXI/GRND HDL 1 EA27221CJ UE221 LEFT EMERGENCY EXIT EXTERIOR HANDLE NOT FLUSHED. RIGGED DOOR HANDLE. 2L72 4T RTA24CE 20050923000462005092300046EA 2005 9 23 09212005D 220050920A73218063005 FUEL CONTROL BEECH 1900 1900D 1154162CE PWA PT6 PT6A6 52043EA LT ENGINE FAILED A NSVAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TXTAXI/GRND HDL 1 EA27136MJ UE36 ON LEFT ENGINE START AT 44 PERCENT, ITT ROSE RAPIDLY AND ABORTED START AT 980 DEGREES CELSIUS (ENG AT 980 DEGREES FOR LESS THAN 5 SECS BEFORE SHUTDOWN). REMOVED AND REPLACED LEFT FUEL CONTROL. OPS CHECK GOOD. 2L72 4T3 TRTA24CE E4EA 20050923000492005092300049EU 2005 9 23 09122005C 120050906A2611 SMOKE DETECTOR SAAB SF340 340B 7860101EU E/E BAY MALFUNCTIONED A NSVAB EMER. DESCENT N FALSE WARNING DEDESCENT 1 EA27304CE 198 AVIONICS SMOKE LIGHT ILLUMINATED 50 MILES FROM SJT. FOLLOWED CHECKLIST, LIGHT DID NOT GO OUT, DECLARED EMERGENCY. AT 20 MILES LIGHT WENT OUT. LANDED SAFELY. DEFERRED AVIONICS SMOKE DETECTOR. 2L72 4T RTA52EU 20050923000502005092300050CE 2005 9 23 09122005F 120050911A6123 CIRCUIT BREAKER BEECH 1900 1900D 1154162CE AUTOFEATHER INOPERATIVE A NSVAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 EA27171CJ UE71 PROP OVERSPEED TEST INOP. LOW PITCH TEST INOP. AUTOFEATHER INOP. RESET CB9, OPS CHECK GOOD FOR PROP OVERSPEED, LOW PITCH, AND AUTOFEATHER TEST. 2L72 4T RTA24CE 20050923000512005092300051CE 2005 9 23 09122005E 120050910A5730 SKIN BEECH 1900 1900D 1154162CE LT WING BIRD STRIKE A NSVAO OTHER O OTHER CRCRUISE 1 EA27243CJ UE43 BIRD STRIKE ON LEFT INBOARD LEADING EDGE. REMOVED AND REPLACED LEADING EDGE, ONLY WAITING ON A BOOT. 2L72 4T RTA24CE 20050923000542005092300054EU 2005 9 23 09212005I 120050920A2611 WARNING LIGHT SAAB SF340 340B 7860101EU E/E BAY FALSE ACTIVATIONA NSVAO OTHER N FALSE WARNING CRCRUISE 1 EA27239CJ 239 AVIONICS SMOKE LIGHT ILLUMINATED IN FLIGHT (NO SMELL OR ODOR OF SMOKE). MEL'ED. 2L72 4T RTA52EU 20050923000552005092300055CE 2005 9 23 09132005A 120050912A2797 GROUND WIRE BEECH 1900 1900D 1154162CE FLAP SYSTEM LOOSE A NSVAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 EA2760MJ UE60 FLAP WILL NOT GO DOWN WHEN SELECTED 17 DEGREES. MEL'ED FLAP SYSTEM. C/W MEL ON 9/15/2005 FOUND LOOSE GROUND, RESECURED, OPS CHECK GOOD. 2L72 4T RTA24CE 20050923000562005092300056EU 2005 9 23 09162005B 120050915A2933 INDICATOR SAAB SF340 340B 7860101EU HYD QTY FAILED A NSVAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 EA27347CJ 347 HAD TO PUMP GEAR AND FLAPS DOWN. MEL'ED ELECTRIC QUANTITY INDICATOR. 2L72 4T RTA52EU 20050923000582005092300058EU 2005 9 23 09152005C 120050914A324650104882 WHEEL SAAB SF340 340B 7860101EU NLG VIBRATION A NSVAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 EA27308CE 210 ABORTED TAKEOFF DUE TO NOSEWHEEL SHIMMY (ABORTED TAKEOFF). REMOVED AND REPLACED LT AND RT NOSE WHEELS. PERFORMED HIGH SPEED TAXI TEST. OPS CHECKS GOOD. 2L72 4T RTA52EU 20050923000592005092300059EU 2005 9 23 09192005A 120050916A3240 BRAKE ASSY SAAB SF340 340B 7860101EU MLG MALFUNCTIONED A NSVAO OTHER O OTHER NRNOT REPORTED 1 EA27277MJ 277 LEFT BRAKE DIFFICULT TO ACTUATE. BLED BRAKES, OPS CHECK GOOD. 2L72 4T RTA52EU 20050923000602005092300060 2005 9 23 09192005B 420050917A3418861CAR VANE SAAB SF340 340B 7860101EU AOA MALFUNCTIONED A NSVAK NONE L NO TEST ININSP/MAINT 1 EA27315CE 343 RIGHT STALL WARNING FAILED TEST. REMOVED AND REPLACED AOA VANE. 2L72 4T RTA52EU 20050923000622005092300062NM 2005 9 23 PIDA20050111 120050916A53206545870113 SUPPORT ANGLE BOEING737 7373G7 1384595NM BS 291 CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05370WL 24011 SHELF SUPPORT ANGLE CRACKED AT BS 291 AT STR 14 RT. REPLACED ANGLE PER DWG 65-45870 AND SRM 51-10-2. 2L72 4F RTA16WE 20050923000642005092300064NM 2005 9 23 PIDA20050110 120050915A5320 SUPPORT ANGLE BOEING737 7373G7 1384595NM BS 291 CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05370WL 24011 SHELF SUPPORT ANGLE AT BS 291 CRACKED AT STR 13 RT. REPLACED ANGLE PER SRM 51-10-2. 2L72 4F RTA16WE 20050923000652005092300065CE 2005 9 23 45074 120050913A5346 BEAM CESSNA402 402B 207590PCE ENGINE CRACKED B QTVAK NONE O OTHER NRNOT REPORTED 1 NM116367X20345 402B1330 DURING SID 54-10-04 INSPECTION, CRACKS WERE FOUND ON 3 OF 4 FWD ENGINE SUPPORT BEAMS. CRACKS WERE FOUND AT EDGE OF MOUNT SUPPORT ON OUTBOARD BEAM AND EDGE OF WASHERS ON INBOARD BEAMS. REPAIR PATCHES WERE INSTALLED IAW AERODESIGN AIRCRAFT ENGINEERING, INC ENGINEERING REPORT 5815.1, APPROVED FOR THIS AIRCRAFT ONLY. 1L72 3O A7CE 20050923000662005092300066NM 2005 9 23 CALA0500317 120050919A531465621258 KEELBEAM BOEING737 7373T0 1384582NM BS 663.75-696 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2760312 23363 INSPECTION FOUND THE RIGHT KEEL BEAM CORRODED AT LOWER SURFACE BETWEEN STA 663.75 TO 696, S27R. REPAIRED IAW ECRA 5311-01239. 2L72 4F RTA16WE 20050923000672005092300067NM 2005 9 23 CALA0500318 120050919A531465621257 KEELBEAM BOEING737 7373T0 1384582NM STA 663.75-727 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2760312 23363 INSPECTION FOUND LEFT KEELBEAM LOWER SURFACE CORRODED AT STA 663.75 TO 727. REPAIRED KEEL BEAM LOWER CHORD IAW ECRA 5311-01238. 2L72 4F RTA16WE 20050923000682005092300068NM 2005 9 23 SPAA0500074 120050913A33501000679 LIGHT BOEING737 7372T4 1384492NM L2 DOOR INOPERATIVE A SPAAK NONE L NO TEST ININSP/MAINT 1 WP28703S 22529 ON PREFLIGHT CHECK FOUND EMERGENCY EXIT LIGHT AT CABIN DOOR 2L DIM. REPLACED EMERGENCY EXIT LIGHT/BATTERY PACK ASSEMBLY PER MM 33-51-101, OPERATIONAL CHECK NORMAL. 2L72 4F A16WE 20050923000692005092300069NM 2005 9 23 05FDEA02988 120050918A5744 ATTACH FITTING DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 LT WING, O/B FLAP I/B HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08. 2L73 4F RTA22WE 20050923000702005092300070CE 2005 9 23 1050902038 120050919A532012944004475 INTERCOSTAL BEECH 1900 1900D 1154162CE BS 468-495 CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07135YV2001720017 UE135 INTERCOSTAL ABOVE CARGO DOOR CRACKED AT FS 468, 482 AND 495. MAINTENANCE WAS DOING A STRUCTURAL REPAIR. 2L72 4T RTA24CE 20050923000712005092300071NM 2005 9 23 HNAA0500085 120050918A325086005 MANIFOLD DHAV DHC8 DHC8102 2809003NM NLG STEERING BROKEN A HNAAK NONE O OTHER ININSP/MAINT 1 EA07975HA4182041820 176 STEERING MANIFOLD RETURN OUTLET AND COMPENSATOR ASSY PLATE HAS THREE SHEARED BOLTS. REMOVED AND REPLACED STEERING MANIFOLD. 2H72 4T RTA13NM 20050923000732005092300073EU 2005 9 23 05FDEA03003 120050920A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25681FE 799 MDCC - FR 37-38 SEAT TRACK L3 HAS DAMAGE IN SCALLOPS. FABRICATED AND INSTALLED SEAT TRACK SECTION IAW A300-600 SRM 53-10-16. ALODINED, PRIMED, AND TOPCOATED IAW A300-600 SRM 51-75-10. 2L72 4F RTA35EU 20050923000742005092300074NM 2005 9 23 05FDEA03013 120050920A5315 FLOORBEAM BOEING727 727233 138408ANM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25286FE 22623 FLOORBEAM CORRODED STA 680 FROM BLO TO LBL 45. REMOVED CORROSION IAW FX B727 SRM 51-10-6. FOUND AREA FROM LBL8 TO LBL12 TO BE OUT OF LIMITS IAW FX P-F SRM 53-10-1. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW FX SR27-53-034E FIG 1. ALODINED AND PRIMED REPAIR PARTS IAW FX SRM B727 51-10-2. 2L73 4F RTA3WE 20050923000752005092300075NM 2005 9 23 05FDEA03014 120050920A5347 SEAT TRACK BOEING727 727233 138408ANM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25286FE 22623 SEAT TRACK CORRODED STA 480-690 AT LBL 45. REMOVED SEAT TRACK STA 480-690 AT LBL 45 IAW FX B727 SRM 51-30-2. LOCATED AND DRILLED NEW SEAT TRACK AND SPLICES IAW FX B727 SRM 53-10-5. ALLODINED, PRIMED AND INSTALLED SEAT TRACK IAW FX B727 SRM 53-10-5, 51-30-2, 51-10-2. 2L73 4F RTA3WE 20050923000762005092300076NM 2005 9 23 05FDEA03015 120050920A5347 SEAT TRACK BOEING727 727233 138408ANM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25286FE 22623 SEAT TRACK CORRODED STA 720-740 AT BL0. REMOVED CORRODED SEAT TRACK AT STA 720-740 ON BL 0, LOCATED AND DRILLED NEW SEAT TRACK, ALODINED, PRIMED AND INST NEW SEAT TRACK SECTION STA 720-740 AT BL0 ALL IAW FX B727 SRM 53-10-5, 51-30-2, 51-10-5 AND 51-10-2. 2L73 4F RTA3WE 20050923000772005092300077NM 2005 9 23 05FDEA03016 120050920A5347 SEAT TRACK BOEING727 727233 138408ANM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25286FE 22623 SEAT TRACK CORRODED STA 480-690 AT LBL 24. REMOVED DAMAGED SEAT TRACK STA 480-690 AT LBL24, LOCATED AND DRILLED NEW SEAT TRACK, ALODINED, PRIMED AND INSTALLED NEW SEAT TRACK AT STA 480-690 AT LBL 24 ALL IAW FX B727 SRM 53-10-5, 51-30-2, 51-10-5 AND 51-10-2. 2L73 4F RTA3WE 20050923000782005092300078NM 2005 9 23 05FDEA03017 120050920A5347 SEAT TRACK BOEING727 727233 138408ANM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25286FE 22623 SEAT TRACK CORRODED STA 690-740 AT LBL24. REMOVED SEAT TRACK, LOCATED AND DRILLED, ALODINED, PRIMED AND INSTALLED NEW SEAT TRACK SECTION STA 690-740 AT LBL 24 ALL IAW FX B727 SRM 53-10-5, 51-30-2,51-10-5 AND 51-10-2. 2L73 4F RTA3WE 20050923000792005092300079NM 2005 9 23 05FDEA03018 120050920A5347 SEAT TRACK BOEING727 727233 138408ANM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25286FE 22623 SEAT TRACK CORRODED STA 690-740 AT LBL45. REMOVED SEAT TRACK, LOCATED AND DRILLED, ALODINED, PRIMED AND INSTALLED NEW SEAT TRACK FROM STA 690 TO 740 AT LBL45 ALL IAW FX B727 SRM 53-10-5, 51-30-2, 51-10-5 AND 51-10-2. 2L73 4F RTA3WE 20050923000802005092300080NM 2005 9 23 05FDEA03019 120050920A5320 FLOOR SUPPORT BOEING727 7272S2F 1384O81NM BS 852 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25211FE 22933 MAIN DECK FLOOR SUPPORT AT STA 852 BETWEEN LBL 45.50 AND 62, CORROSION UNDER CLIP NUT HOLES AND MOUNT BOLT AT LBL 45.5. REMOVED CORROSION IAW SRM 51-10-6, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REMOVED CHANNEL IAW 51-30-2. FABED NEW UPPER CAP USING MAT.2024T3 .016 BATCH 122431 IAW 51-20-1. FABED NEW CHANNEL ON TRAVELER TD/000219, INSTALLED CHANNEL IAW SRM 51-30-2. UPPER CAP INSTALLED IAW SRM 51-30-2. 2L73 4F A3WE 20050923000812005092300081NM 2005 9 23 05FDEA03020 120050920A5347 FLOORBEAM BOEING727 727233 138408ANM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25286FE 22623 FLOORBEAM CORRODED STA 480 FROM BL0 TO LBL45. REMOVED, FABRICATED, ALODINED, PRIMED AND INSTALLED FLOORBEAM REPAIR AT STA 480 FROM BL0 TO LBL45 ALL IAW FX B727 SRM 53-10-8, 53-10-1 AND 51-10-2. 2L73 4F RTA3WE 20050923000822005092300082NM 2005 9 23 05FDEA03021 120050920A5315 FLOORBEAM BOEING727 727233 138408ANM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25286FE 22623 FLOORBEAM CORRODED STA 720A FROM BL0 TO LBL45. REMOVED, FABRICATED, HEAT TREATED, CAD PLATED, ALODINED, PRIMED AND INSTALLED FLOORBEAM REPAIR STA 720A BLO TO LBL 45 ALL IAW FX SR 27-53-034E FIG 5, FX B727 SRM 51-10-2, 53-10-1, BAC5619(H) AND BAC 5701. 2L73 4F RTA3WE 20050923000832005092300083NM 2005 9 23 05FDEA03022 120050920A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 UPPER CARGO, SEAT TRACK RBL 77 CORRODED AT STATION 1350. SEAT TRACK REPAIRED AS PER SRM 53-70-00 VOLUME I FIGURE 1. CLASSIFIED AS MAJOR REPAIR PER GMM 6-2-100. 2L73 4F RTA22WE 20050923000842005092300084EU 2005 9 23 05FDEA03004 120050920A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25681FE 799 FR 42- FR 43 SEAT TRACK L3 IS DAMAGED IN SCALLOP AREA. FABRICATED AND INSTALLED SEAT TRACK SECTION IAW A300-600 SRM 53-10-16. ALODINED, PRIMED, AND TOPCOATED IAW A300-600 SRM 51-75-10. 2L72 4F RTA35EU 20050923000852005092300085 2005 9 23 05FDEA03006 420050920A3442 DISPLAY BOEING727 727233 138408ANM WX RADAR INOPERATIVE A FDEAA UNSCHED LANDING JS WARNING INDICATION AFFECT SYSTEMS CLCLIMB 1 SO25222FE 20933 AFTER T/O, SWITCHING FROM TERRAIN TO WX MODE OR RADAR, LOST RANGE MARKER AND DATA DISPLAY. ACTUAL WX RETURNS WORKED. REMOVED AND REPLACED INDICATOR R/T AS PRECAUTIONARY. REF B727-200MM SEC 34-41-031-4 AND 34-41-041-4. 2L73 4F RTA3WE 20050923000862005092300086NM 2005 9 23 05FDEA03007 120050920A5753 STRUCTURE BOEING727 727227 1384078NM NR 7 FLAP TRACK CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 AFTER REMOVAL OF NR 7 FLAP TRACK FWD FITTING ON N00421, FOUND EXISTING DAMAGE IN AFT INBOARD ATTACH FITTING HOLE. REPAIRED PER SRM 51-20-1, 51-30-2. 2L73 4F A3WE 20050923000912005092300091EA 2005 9 23 COMA0560507 120050918A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION LDLANDING 1 SO01409CA 7441 FLIGHT 4991- DURING LANDING RECEIVED A FLAP FAIL CAUTION MESSAGE AT 8 DEGREE FLAP POSITION SETTING. COMPLIED WITH AS 98-20-01 FLAP CAUTION MESSAGE FIRST EVENT MAINTENANCE ACTION PARAGRAPH (B) 1, 2, 3 (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2L72 4F RTA21EA 20050920001882005092000188NE 2005 9 20 SWAA052814 220050916A7261CFM567B ENGINE BOEING737 7377H4 1384404NM CFMINTCFM567CFM567B22 13802NE NR 1 CONTAMINATED A SWAAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 SW29429WN 33658 890303 INFLIGHT SHUTDOWN/DECLARED EMERGENCY. NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. SHUT DOWN NR 1 ENGINE BYPASS LIGHT EXTINGUISHED. FOUND METAL PARTICLES IN OIL FILTER. REMOVED AND REPLACED NR 1 ENGINE PER MM. 2L72 4F4 FRTA16WE E00055EN 20050920001902005092000190NM 2005 9 20 SB05115 120050918A27512061141 INDICATOR BOEING737 737301 1384611NM TE FLAPS FAULTY A USAAL ABORTED APPROACH F FLT CONT AFFECTED APAPPROACH 1 EA19334US5176051760 23231 DFW FLT1262 - DURING FINAL APPROACH TO DFW, CREW SELECTED FLAPS FROM 15 TO 25 UNITS AND NOTICED A DEVELOPING SPLIT IN THE LEFT AND RIGHT FLAP POINTERS. AT 25 UNITS, THERE WAS A NOTICEABLE SPLIT BUT NO APPARENT AIRCRAFT ROLL. CREW EXECUTED A GO-AROUND AND LANDED WITH FLAPS 15 WITHOUT FURTHER INCIDENT. SUBSEQUENT TEST AT THE GATE SHOWED THE FLAPS GOING TO 25 UNITS WITH A 3 TO 4 SPLIT, THEN 30 UNITS WITH NO SPLIT AND 40 UNITS WITH NO SPLIT. MAINTENANCE FOUND THE FLAP POSITION INDICATOR FAULTY. REPLACED INDICATOR PER MM 27-51-00 AND 27-58-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050920001932005092000193EU 2005 9 20 SA05102 120050918A5210 DISC AIRBUSA321 A321211 3930370EU PAX DOOR PUNCTURED A USAAK NONE J WARNING INDICATION ININSP/MAINT 1 EA19169UW 1455 LGA - MAINTENANCE REPORTED THE CIDS PANEL INDICATES MID LEFT ENTRY DOOR ASSIST BOTTLE PRESSURE LOW. LGA MAINTENANCE SERVICED THE MID LEFT DOOR ASSIST BOTTLE PER MM. LEAK CHECK GOOD. ALSO, ACTION FROM A MAINTENANCE TECH SERVICE ITEM REVEALED A PUNCTURED BLOW OUT DISC. PIT MAINTENANCE REPLACED DISC AND O-RINGS. SERVICED BOTTLE AND LEAK CHECKED GOOD. 2L72 4F RTA28NM 20050920001952005092000195EA 2005 9 20 A6WA200540300 120050905A5320 FLANGE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE BS 484 CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31424AW 7656 MWC 138, UNDERFLOOR INTERCOSTAL ATTACHED FLANGE IS CRACKED AT LBL 36, BS 484, WL73. REPAIRED UNDERFLOOR INTERCOSTAL AT LBL 36 IAW 601R-53-41-059 AND 601R-53-0030 BY CUTTING OUT CRACKED ANGLE AND INSTALLING REPAIR ANGLE. (K) 2L72 4F4 FRTA21EA E15NE 20050920001982005092000198NM 2005 9 20 USAA0514007 120050815A5320 CHANNEL BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU BS 360 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19449US41152 24893 CLT - Q1 - SPLICE CHANNEL, 1 INCH CRACK, BS 360, S-15L STRINGER SPLICE CHANNEL. REMOVED DAMAGED SLICE AND INSTALLED NEW SLICE IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050921000022005092100002WP 2005 9 21 UPS05845405 120050912A5712 RIB DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 CRACK IN RIB AT LT INBD GROUND SPOILER INBD MOUNT FITTING (MARKED). STOP DRILLED CRACK REF SRM 57-02-00 1199249 9/12/05. ACCOMPLISHED HFEC OF AREA NO DEFECTS NOTED. REPAIRED RIB AS PER DC8-SRM 57-02-00-51-1-20 SEE LOG PAGE 418971 M-3 FOR FITTING ASSY-END. 2L74 4F RT4A25 20050921000162005092100016EA 2005 9 21 MASA200500673 120050825A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA MAIN PAX MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07571ML 7209 ASH 2786 DCA. PAX DOOR WILL NOT OPEN. CONTRACT MAINTENANCE MOVED THE AIRCRAFT TO LEVEL GROUND AND OPS CHECKED GOOD. 2L72 4F RTA21EA 20050921000182005092100018EA 2005 9 21 MASA200500596 120050726A3260 UPLOCK SENSOR CNDAIRCL600 CL6002B19 1900309EA LT MLG OUT OF ADJUST A MASAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 SW0737218 7218 ASH 6023 LAS. LAS TO FAT DIVERTED TO BFL FOR GEAR DISAGREE MESSAGE IN FLIGHT (FL280). FERRIED TO PHX AND MX ADJUSTED MLG LEFT MAIN GEAR UPLOCK SENSOR. 2L72 4F RTA21EA 20050921000212005092100021NM 2005 9 21 2005UALA00962 120050910A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM563B1 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29203UA 24718 LWR FUSELAGE EXTERNAL SKIN HAS A DENT AT BS 1020.5 AT STRINGER 25L. FABRICATED & INSTALLED EXTERNAL DOUBLER & FILLERS PER SRM 53-80-01. 2L72 4F4 FRTA16WE E2GL 20050921000482005092100048EA 2005 9 21 MASA200500562 120050718A5270840534 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA DOOR HANDLE FAILED A MASAO OTHER P NO WARNING INDICATION NRNOT REPORTED 1 SW0747239 7239 ASH 7025 ORD. THE AIRCRAFT FAILED TO PRESSURIZE. CONTRACT MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR HANDLE PROX SWITCH. 2L72 4F RTA21EA 20050921000502005092100050NM 2005 9 21 05FDEA02946 120050916A5320 SPLICE DOUG MD11 MD11 3023602NM BS 6-90 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 ALONG STA 6-90, LONGERON 44L, LONGERON SPLICE FITTING CORRODED. CAC COMPT. ALONG STA 6-90 LONGERON 44L LONGERON CORROSION SPLICE REMOVED AND NEW SPLICE INSTALLED AS PER SRM 51-31-01 VOL.II, SRM 51-33-01 VOL.II, SRM 51-35-01 VOL.II AND DRAWING AGA 7115. NEW SPLICE FABRICATED PER DRAWING AGA 7115 P/N FX AGA 7116- 511. MAJOR REPAIR PER GMM 6-2-100. 2L73 4F RTA22WE 20050921000522005092100052NM 2005 9 21 05FDEA02948 120050916A5315 FLOORBEAM BOEING727 727200 138407ENM BS 1110 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION, STA 1110 BL 0, CORROSION ON MAIN DECK FLOORBEAM LOWER CHORD. REPAIR FLOOR BEAM LOWER CHORD PER SRM 53-10-8, FIG 2. 2L73 4F RTA3WE 20050921000532005092100053EA 2005 9 21 MASA200500669 120050824A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A MASAO OTHER J WARNING INDICATION APAPPROACH 1 SW07154SF455 7154 ASH 2761 PHL. ON APPROACH TO PHL PILOT DECLARED AN EMERGENCY DUE TO FLAPS FAIL AT 12 DEG. ACFT LANDED WITHOUT INCIDENT. MX REMOVED AND REPLACED BOTH BPSU & RT FLEX SHAFTS. 2L72 4F RTA21EA 20050921000552005092100055 2005 9 21 SB05116 420050919A2565BACS21AP6000W BRACKET BOEING737 7373B7 1384580NM R2 DOOR SLIDE MISSING A USAAK NONE O OTHER ININSP/MAINT 1 EA19394US 23316 ORD - PILOT REPORTED MISSING HARDWARE FOR THE FORWARD BRACKET OF THE R2 SERVICE DOOR ESCAPE SLIDE. MAINTENANCE REPLACED MISSING HARDWARE FOR THE FORWARD BRACKET OF THE R2 SERVICE DOOR ESCAPE SLIDE. 2L72 4F RTA16WE 20050921000592005092100059EA 2005 9 21 MASA200500729 120050914A261147359719 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY MALFUNCTIONED A MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW07154SF3153 7154 ASH 2611 PHL. CARGO SMOKE WARNING MESSAGE IN FLIGHT. MX REPLACED THE SMOKE DETECTOR. 2L72 4F RTA21EA 20050921000632005092100063EA 2005 9 21 MASA200500546 120050713A3320 BULB CNDAIRCL600 CL6002B19 1900309EA GALLEY LIGHT INCORRECT A MASAO OTHER WB INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW0717231 7231 ASH 6078 PHX. AS ACFT WAS BOARDING F/A NOTICED SMOKE IN CABIN NEAR PAX DOOR. MX FOUND GALLEY LIGHTS TO BE LAMPED WITH INCORRECT BULBS, IT CAUSED AN OVERHEAT SITUATION AND DAMAGED 1 OF THE LIGHT ASSY. MX RELAMPED 2 OF 4 BULBS AND PLACED 2 ON NAI. ACFT CONTINUED OPERATIONS. LATER MAINTENANCE REPLACED THE GALLEY LIGHT ASSEMBLY. 2L72 4F RTA21EA 20050921000652005092100065NM 2005 9 21 SWAA052839 120050919A53306545769 SKIN BOEING737 7373H4 1384600NM BS 373 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29395SW 27689 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 373, BETWEEN STR 28L & STR 28R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050921000672005092100067NM 2005 9 21 SWAA052841 120050919A53116546550 FRAME BOEING737 7373H4 1384600NM BS 787 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 DURING SCHEDULED D-CHECK, FOUND CABIN FUSELAGE FRAME CRACKED AT BS 787, STR 9L & STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050921000692005092100069NM 2005 9 21 SWAA052843 120050919A53116546558 FRAME BOEING737 7373H4 1384600NM BS 907 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 DURING SCHEDULED D-CHECK, FOUND CABIN FUSELAGE FRAME CRACKED AT BS 907, STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050921000712005092100071NM 2005 9 21 SWAA052845 120050919A532065C27314 CLIP BOEING737 7373H4 1384600NM BS 480 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 DURING SCHEDULED D-CHECK, FOUND CABIN FUSELAGE STR CLIP CRACKED AT BS 480, STR 15R. REMOVED AND REPLACED STR CLIP PER SRM. 2L72 4F RTA16WE 20050921000742005092100074EU 2005 9 21 USAA051121 120050920A5322 SHEAR TIE AIRBUSA319 A319112 3930323EU FR 69-70 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19733UW 1205 LT SHEAR TIE CORRODED BETWEEN FRAME 69 AND 70. REMOVED AND REPLACED PART WITH NEW PER 51-72-11, DEFECT SIZE: .05" X 1" AREA. 2L72 4F RTA28NM 20050921000762005092100076EU 2005 9 21 USAA051119 120050920A5315D5347219320000 FLOORBEAM AIRBUSA319 A319112 3930323EU CABIN CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19732US 1203 FOUND Y-765 FLOORBEAM CORROSION (RT) 7" AFT OF STA 66 AROUND ATTACH HOLES. REMOVED AND REPLACED BEAM WITH IDENTICAL PART NUMBER PER SRM 51-72-11, DEFECT SIZE: 1 X 1". 2L72 4F RTA28NM 20050921000782005092100078EU 2005 9 21 USAA051117 120050920A5315D5347209001100 FLOORBEAM AIRBUSA319 A319112 3930323EU BS 66 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19732US 1203 FOUND CORROSION RT BEAM Y-1292 STA 66 AT ATTACH HOLE AFT END. REPLACED WITH IDENTICAL PART PER SRM 51-42-00, DEFECT SIZE: 1" X 2". 2L72 4F RTA28NM 20050921000812005092100081NE 2005 9 21 MASA200500716 220050908A73214147T70P02 FUEL CONTROL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 1 ENGINE MALFUNCTIONED A MASAC ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 SW07771811201012010 7181 872898 ASH 2763 GRR. ABORTED TAKEOFF DUE TO THE NR 1 ENG NOT MAKING TAKEOFF POWER. CONTRACT MAINTENANCE PERFORMED A PERFORMANCE RUN OF THE ENGINE AND COULD NOT FIND A FAULT. FERRIED THE PLANE TO PHL WHERE MX REMOVED AND REPLACED NR 1 FUEL CONTROL. 2L72 4F4 FRTA21EA E15NE 20050921000832005092100083EA 2005 9 21 MASA200500656 120050819A3350 SWITCH CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT MALFUNCTIONED A MASAO OTHER L NO TEST NRNOT REPORTED 1 SW0727172 7172 ASH 2942 PHL. EMERGENCY EXIT LIGHTING SYSTEM FAULT. THE LIGHTS TURNED ON WHEN THE EMERGENCY EXIT LIGHT SWITCH WAS SET TO ARM. MX RESET THE EMERGENCY EXIT LIGHT C/B. 2L72 4F RTA21EA 20050922000052005092200005NM 2005 9 22 05FDEA02985 120050918A5744 ATTACH FITTING DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 LEFT WING, O/B FLAP O/B HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-09. REPAIR CARRIED OUT AS PER EA 1-5750-87640. 2L73 4F RTA22WE 20050922000122005092200012NM 2005 9 22 05092003 120050919A5312 BULKHEAD BOEING737 7372H4 138448CNM BS 1016 CRACKED A MJYAK NONE O OTHER ININSP/MAINT 1 SW05733TW 22732 BS 1016 AFT PRESSURE BULKHEAD WEB TO "Y" CHORD ATTACHMENT CRACKED. 2L72 4F A16WE 20050922000172005092200017NE 2005 9 22 2005UALA00978 220050909A7310 WARNING SYSTEM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUEL FLOW ACTIVATED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29521UA 24891 RETURNED TO FIELD DUE TO FUEL FLOW INDICATION. DURING TROUBLESHOOTING FOUND DAMAGE TP WIRE INSULATION AT CONNECTOR D5004 FUEL FILTER DIFFERENTIAL PRESSURE SWITCH APPROXIMATELY A HALF INCH FROOM THE BACKSHELL. REPAIRED WIRING PER MM 71-51-00 PAGES 820/821. 2L72 4F4 FRTA2NM E17NE 20050922000182005092200018EU 2005 9 22 2005UALA00979 120050913A2133 OUTFLOW VALVE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CABIN PRESSURE MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29481UA 1559 AIRCRAFT PRESSURIZATION PROBLEM. CREW STOPPED CLIMB AT 10,000 FT, CABIN ALTITUDE WAS 7,000 FT. AIRCRAFT RETURNED TO FIELD AND LANDED OVERWEIGHT. CREW STOPPED CLIMB AT 10,000 FEET, CABIN ALTITUDE WAS 7,000 FEET. AIRCRAFT RETURNED TO FIELD AND LANDED OVERWEIGHT. REMOVED BORROWED SKIN AIR OUTLET VALVE FROM FRONTIER. INSTALLED NEW SKIN AIR OUTLET VALVE AND TEST FAILED. VALVE INOPPED PER MEL. REPLACED WITH NEW SKIN AIR OUTLET VALVE MR21202, PCN 644-9041 PER MM-21-26-53 AND OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA28NM E40NE 20050922000362005092200036EA 2005 9 22 MASA200500589 120050725A3350316 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0717231 7231 ASH 6713 PHX. FLOOR ELECTROLUMINESCENT PROXIMITY EMERGENCY ESCAPE PATH LIGHT WITHOUT ORANGE OVERLAY WAS FOUND TO BE INOP. MX RELAMPED. 2L72 4F RTA21EA 20050922000372005092200037EA 2005 9 22 MASA200500593 120050726A3260864202 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA NLG FAILED A MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW0737218 7218 ASH 2993 CHA. SPS ADVANCE AND LANDING GEAR AIR GROUND FAIL AFTER TAKEOFF. MX REPLACED THE LT, RT AND NOSE PROX SENSOR. 2L72 4F RTA21EA 20050922000472005092200047EU 2005 9 22 USAA051115 120050920A5315D5347209001000 FLOORBEAM AIRBUSA319 A319112 3930323EU STA 66 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19732US 1203 FOUND CORROSION LT STA 66 AFT END OF FLOORBEAM AT ATTACH HOLES FOR FLOORBOARD. REPLACED WITH IDENTICAL PART PER SRM 51-42-00, DEFECT SIZE: 1" X 2". 2L72 4F RTA28NM 20050922000582005092200058NM 2005 9 22 USAA051092 120050920A5330 SKIN BOEING737 7374B7 1384702NM BS 200-210 DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 STA 200-210, S-22R - S-23R, 10 BY 8 DOUBLER INSTALLED IAW SRM 53-10-01, DEFECT SIZE: AT STA 200-210, S22R THRU S-23R, MEASURES 10 BY 8. 2L72 4F RTA16WE 20050922000642005092200064EU 2005 9 22 USAA051111 120050920A5320D5347218920400 FLOOR SUPPORT AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19732US 1203 FOUND CORROSION FLOOR SUPPORT Y-1162, DEFECTIVE PART REPLACED WITH IDENT PART NUMBER, DEFECT SIZE: 6 SQ IN IN SEVERAL SPOTS. 2L72 4F RTA28NM 20050922000692005092200069NM 2005 9 22 USAA051122 120050920A5310 DOOR FRAME BOEING737 7374B7 1384702NM BS 296 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 FOUND CRACK FWD SVC DOOR, FWD FRAME AT UPPER DOOR STOP FTG LWR O/B CRNR, STA 296 S-8R-10. REMOVED DAMAGED FRAME AND INSTALLED FRAME PIN PER BOEING DWG 65-45807 AND 65C34778, SRM 51-10-02, 51-40-DEFECT SIZE: 1.25". 2L72 4F RTA16WE 20050922000762005092200076NM 2005 9 22 USAA051099 120050920A5340 ATTACH BRACKET BOEING737 7374B7 1384702NM BS 500G CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 FOUND CRACK STA 500G, S28L. FAB NEW ANGLE FROM 2024-T3 .040 PER DWG 65C33472 IAW BOEING DWG 69-73527, SRM 51-10-02, DEFECT SIZE: .250" CRACK IN RADIUS. 2L72 4F RTA16WE 20050922000822005092200082EA 2005 9 22 MASA200500624 120050808A2611 CAGE CNDAIRCL600 CL6002B19 1900309EA SMOKE DETECTOR CONTAMINATED A MASAO OTHER CN F.O.D. FALSE WARNING NRNOT REPORTED 1 SW0737178 7178 ASH 6033 PHX. A CARGO SMOKE INDICATION. MX REMOVED A PLASTIC DRINK CUP FROM THE NR 2 CARGO SMOKE DETECTOR CAGE AND THE SYSTEM OPERATED NORMALLY. A/C DEPARTED WITHOUT FURTHER INCIDENT. 2L72 4F RTA21EA 20050922000882005092200088EU 2005 9 22 AWXA200501065 120050904A5315D5347217220290 FLOORBEAM AIRBUS320 A320231 3930325EU CABIN CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28634AW 091 DURING C4 CHECK, DISCOVERED EXFOLIATION CORROSION LOCATED ON FLOORBEAM FROM FR 66 TO FR 68, Y1292. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-14. REMOVED FLOORBEAM FROM FR 66 TO FR 68, Y1292 IAW AIRBUS 320 SRM 51-72-11. INSTALLED NEW FLOORBEAM FROM FR 66 TO FR 68, Y1292 IAW AIRBUS 320 SRM 51-72-11. 2L72 4F RTA28NM 20050922000902005092200090EU 2005 9 22 AWXA200501067 120050904A5315D53472172203 FLOORBEAM AIRBUS320 A320231 3930325EU CABIN CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28634AW 091 DURING C4 CHECK DISCOVERED GALVANIC CORROSION LOCATED ON FLOORBEAM FROM FR 66+8 TO FR 68, Y-1292. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-14. REMOVED FLOORBEAM FROM FR 66+8 TO FR 68, Y-1292 IAW AIRBUS 320 SRM 51-72-11. INSTALLED NEW FLOORBEAM FROM FR 66+8 TO FR 68, Y-1292 IAW AIRBUS 320 SRM 51-72-11. 2L72 4F RTA28NM 20050922000932005092200093EU 2005 9 22 AWXA200501070 120050904A5315D53472098000 FLOORBEAM AIRBUS320 A320231 3930325EU CABIN CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28634AW 091 DURING C4 CHECK DISCOVERED, GALVANIC CORROSION LOCATED ON FLOORBEAM FROM FR 65 TO FR 67, Y912. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-14. REMOVED FLOORBEAM FROM FR 65 TO FR 67, Y912 IAW AIRBUS 320 SRM 51-72-11. INSTALLED NEW FLOORBEAM FROM FR 65 TO FR 67, Y912 IAW AIRBUS 320 SRM 51-72-11. 2L72 4F RTA28NM 20050922001222005092200122NM 2005 9 22 05FDEA02990 120050918A5744 ATTACH FITTING DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 LT WING, O/B FLAP I/B HINGE (WING SIDE), LWR ATTACHMENT I/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87637. 2L73 4F RTA22WE 20050922001252005092200125NM 2005 9 22 SWAA052849 120050920A335065C34691 LENS BOEING737 7375H4 138449DNM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29503SW 24180 EMERGENCY EXIT BULLNOSE LIGHT LENS MISSING AT ROW 3 ABC. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20050922001262005092200126NM 2005 9 22 SWAA052850 120050920A3350101114 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29624SW 27934 FWD LOWER EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM. 2L72 4F RTA16WE 20050922001282005092200128NM 2005 9 22 SWAA052852 120050920A53306552988 SKIN BOEING737 7373H4 1384600NM BS 930 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29347SW 24374 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STR 24L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050922001312005092200131NM 2005 9 22 SWAA052855 120050920A53226546550 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, LBL 17, WL 149. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050923000052005092300005NM 2005 9 23 AWXA200501075 120050908A5320654583312 WEB BOEING737 7373G7 1384595NM BS 196 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 DURING C18 CHECK DISCOVERED FLOOR WEB CRACKED, 1.3 INCHES IN LENGTH, AT BS 196, WL 207, BL 29L. REMOVED CRACKED FLOOR WEB IAW BOEING 737-300 SRM 51-40-02-06 FIG 8. FABRICATED NEW WEB IAW BOEING 737-300 SRM 51-40-05-06 TABLE I. INSTALLED FABRICATED REPAIR PARTS AT BS 186, WL 207, AND BL 29L IAW BOEING 737-300 SRM 51-40-02-06. 2L72 4F RTA16WE 20050923000072005092300007NM 2005 9 23 AWXA200501077 120050906A5330654577677 SKIN BOEING737 7373G7 1384595NM BS 967 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - MAJOR REPAIR - DURING C18 CHECK DISCOVERED EXFOLIATION CORROSION ON FUSELAGE SKIN, INTERIOR SIDE, AT BS 967 BETWEEN STR 26L AND STR 26R. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW BOEING 7370-300 SRM 53-00-01-1A FIG 101. CUT OUT DAMAGED SKIN AT BS 967 BETWEEN STR 26R AND 26L IAW BOEING 737-300 SRM 53-00-01-2R-31 FIG 201. FABRICATED DOUBLER IAW BOEING 737-300 SRM 53-00-01-2R 31. MAINTENANCE INSTALLED FABRICATED REPAIR PARTS AT BS 967 BETWEEN STR 26L AND STR 26R IAW BOEING 737-300 SRM 53-00-01-2R 31 FIG 201. 2L72 4F RTA16WE 20050923000172005092300017NM 2005 9 23 UPS05245465 120050901A5420 BUSHING BOEING727 72731C 1384011NM NR 1 PYLON CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01922UP 19231 INSPECTION TYPE:C NR 1 ENGINE FWD ENGINE MOUNT PITTING CORROSION IN BORE OF MOUNT HOLES (TW O/B HOLES). BUSHINGS REPLACED IAW SOPM 20-50-03 AND EO B727-5440-1592 APNDX-A. 2L73 4F A3WE 20050923000222005092300022NM 2005 9 23 UPS05245470 120050826A5753 FLAP TRACK BOEING727 72731C 1384011NM NR 4 FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01922UP 19231 INSPECTION TYPE:C-CORROSION ON NR 4 FLAP TRACK AFT MOUNT PAD CORROSION REMOVED IAW SOPM 20-10-01 P1 AND EO B727-5742-0651K & TEMPER ETCHED 2B (3) IAW SOPM 20-10-01. CAD PLATED IAW OHM 20-42-10. 2L73 4F A3WE 20050923000272005092300027WP 2005 9 23 AALA20050601 120050916A3350 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21290AA 49302 ORD - EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACKS FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050923000282005092300028WP 2005 9 23 AALA20050605 120050919A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21498AA 49736 SFO - EMERGENCY LIGHT AT SEAT 15D INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 15D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050923000312005092300031NM 2005 9 23 AALA20050602 120050916A3397 CIRCUIT BREAKER BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21639AA 24597 JFK - SEAT MOUNTED EMERGENCY LIGHTS FROM ROW 16 AFT WOULD NOT TURN OFF FROM COCKPIT OR FLIGHT ATTENDANT STATION. LIGHT WENT OUT AFTER 45 MINUTES. RESET EMERGENCY LIGHT CHARGER CIRCUIT BREAKERS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050923000332005092300033WP 2005 9 23 AALA20050603 120050919A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21483A 49676 LGA - FORWARD AISLE EMERGENCY LIGHTS NEAR FORWARD LAVATORY INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD AISLE EMERGENCY LIGHTS NEAR FORWARD LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050923000342005092300034WP 2005 9 23 AALA20050607 120050920A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21978TW 53628 LGA - CEILING EMERGENCY LIGHTS AT ROWS 2 TO 6 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROWS 2 TO 6. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050923000392005092300039WP 2005 9 23 AALA20050600 120050916A3350P4010049 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21982TW 53632 SFO - SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 3 TO 19 INOPERATIVE. REPAIRED WIRING AT SEAT ROW 14CDE AND REPLACED BATTERY PACKS AT B5103, B523 AND B5107 FOR SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 3 TO 19. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050923000402005092300040NM 2005 9 23 AALA20050596 120050915A5243 SEAL BOEING757 757223 1384957NM FUEL PORT LEAKING A AALAA UNSCHED LANDING O OTHER CLCLIMB 1 SW21611AM 24487 DEN - AFTER TAKEOFF PASSENGER REPORTED FUEL LEAKING FROM RIGHT OVERWING FUEL CAP. LANDED DEN WITHOUT INCIDENT. REPLACED FUEL CAP, O-RING SEALS AT RIGHT WING OVERWING FUEL PORT HOUSING ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050923000452005092300045EU 2005 9 23 09212005E 120050920A7720 INDICATOR SAAB SF340 340B 7860101EU ITT MALFUNCTIONED A NSVAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 EA27239CJ 239 LEFT ITT GAUGE READING DROPPED TO ZERO. SWAPPED GAUGES. WORKING AS ADVERTISED. PLACED GAUGES BACK IN RESPECTIVE SLOTS. OPS CHECK GOOD. 2L72 4T RTA52EU 20050923000532005092300053EU 2005 9 23 09212005H 120050920A2612 FIRE LOOP SAAB SF340 340B 7860101EU LT ENGINE SHORTED A NSVAO OTHER N FALSE WARNING CRCRUISE 1 EA27347CJ 347 LEFT FIRE DETECT FAIL LIGHT ILLUMINATES DURING FLIGHT. FOUND LOOSE PIECE OF SAFETY WIRE TOUCHING FIRE DETECT LOOP INTERMITTENTLY. SECURED WIRE AND RAN PLANE. OP CHECKS GOOD. 2L72 4T RTA52EU 20050923000572005092300057EU 2005 9 23 AWXA200501086 120050904A5347D53772092205 SEAT TRACK AIRBUS320 A320231 3930325EU FS 20-21 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28634AW 091 DURING C4 CHECK, DISCOVERED CORROSION ON SEAT TRACK FROM FS 20 TO FS 21, Y-765. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 101. MAINTENANCE REMOVED SEAT TRACK FROM FR20 TO FR21, Y-765 IAW AIRBUS 320 SRM 51-42-11. RECEIVED NEW SEAT TRACK AND INSTALLED FROM FS 20 TO FS 21 Y-765 IAW AIRBUS 320 SRM 51-42-11 AND 51-72-11. 2L72 4F RTA28NM 20050923000872005092300087 2005 9 23 05FDEA03008 420050920A3414 INDICATOR BOEING727 727233 138408ANM COCKPIT INOPERATIVE A FDEAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO25254FE542 542 20936 CAPTAINS AIRSPEED INDICATOR DID NOT INDICATE AIRSPEED ON T/O. ACN RELEASED FOR SERVICE PER MEL/CDL: 20-01 CATEGORY: X RVSM ITEM "MEL 20-01: DO NOT OPERATE AIRCRAFT WITHIN RVSM AIRSPACE." "NO RVSM OPERATIONS". R/R CADC PER M/M 34-12-011-4, OPS CHECK GOOD. DEF. RVSM ON A/C PER MEL 20-01 CONT NR 248485, NO EXP. NOTE: NO RVSM CADC INSTALLED (NIS) PER M.O.C.C. PREMATURE REMOVAL/INSTALLATION OFF MFG 9B-81020-1 POS 1 SRL 40851 TAG 6A8103 ON MFG HG480B13 SRL 91032048 TAG 830290. 2L73 4F RTA3WE 20050923000892005092300089NM 2005 9 23 05FDEA03009 120050920A5315 FLOORBEAM BOEING727 727233 138408ANM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25286FE 22623 FLOORBEAM CORRODED STA 560 FROM BL0 TO LBL45. CUT OUT DAMAGED SECTION OF FLOORBEAM CAP IAW FX SR27-53-034E FIG 30 SHT 5. FABRICATED, DRILLED AND LOCATED REPAIR "T", SUPPORTS, FILLERS, ANGLES AND "T" CAP REPAIR ANGLES IAW FX SR27-53-034E FIG 30 SHT 5. INSTALLED REPAIR "T" SUPPORT, FILLERS ANGLES AND "T" CAP REPAIR ANGLES IAW FX SR27-53-034E FIG 30 SHT 5. ALODINED AND PRIMED ALL REPAIR PARTS IAW FX SRM B727 51-10-2. 2L73 4F RTA3WE 20050923000952005092300095NM 2005 9 23 05FDEA03023 120050920A5753651920814 FLAP TRACK BOEING727 7272S2F 1384O81NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25211FE 22933 NR 2 FLAP TRACK FWD MOUNT FITTING CORRODED AROUND BUSHINGS. REMOVED AND REPLACED NR 2 FLAP TRACK ASSY IAW MM 27-51-031-4. 2L73 4F A3WE 20050923000962005092300096EU 2005 9 23 YENA200567 120050920A3260848401 PROXIMITY SENSOR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE MLG INOPERATIVE A YENAO OTHER JS WARNING INDICATION AFFECT SYSTEMS CLCLIMB 1 EA15536JB14219 1784 ON TAKE OFF, AT APPROXIMATELY 1500, AGL GOT ECAM. F/O PERFORMED ECAM ACTION, SHOCK ABSORBER FAULT, THAT CLEARED AND THEN GOT ECAM GEAR NOT LOCKED IN UP POSITION. PERFORMED THAT ECAM WHICH CLEARED ALL PROBLEM WITH NO STATUS MESSAGE. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT FLOWN BACK UNDER MEL 32-31-00. T/S 24GA AT FAULT. REPLACED 24GA PROXIMITY SENSOR IAW AMM 32-31-73-04 AND BITE CK OK. 2L72 4F4 FRTA28NM E40NE 20050923000972005092300097NM 2005 9 23 05FDEA03024 120050921A5744 FITTING DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 RIGHT WING, OUTBOARD FLAP INBOARD AFT HINGE FITTING OUTBOARD MOUNT HOLE (HINGE SIDE) CORRODED. CARRIED OUT BUSHING REPAIR AS PER FEDEX EA #1-5750- 90023. 2L73 4F RTA22WE 20050923000992005092300099NM 2005 9 23 05FDEA03026 120050921A5753 FITTING DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 RIGHT WING, OUTBOARD FLAP INBOARD AFT HINGE FITTING AFT MOUNT AFT HOLE (FLAP SIDE) CORRODED. REMOVED AS PER EO 1-5750-7-5008. 2L73 4F RTA22WE 20050923001012005092300101NM 2005 9 23 05FDEA03028 120050921A5311 FRAME BOEING727 727232 1384082NM BS 950B DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 AFT CARGO BAY, BS 950B FRAME BETWEEN STR 25R AND STR 26R HAS A DENT. REPAIRED FRAME AT BS 950B STR 26R PER SRM 51-40-3. 2L73 4F A3WE 20050923001032005092300103NM 2005 9 23 05FDEA03030 120050921A5311 FRAME BOEING727 727232 1384082NM BS 1130 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 FRAME DENTED AT BS 1130, STR 26L. REPAIRED FRAME AT BS 1130 STR 26L PER SRM 51-40-3 2L73 4F A3WE 20050923001052005092300105NM 2005 9 23 05FDEA03032 120050921A5311 FRAME BOEING727 727232 1384082NM BS 1050 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 FRAME DENTED IN 2 PLACES AT BS 1050, STR 23L AND 25L. REPAIRED FRAME AT BS 1050 STR 23L & 25L PER SRM 51-40-3. 2L73 4F A3WE 20050923001072005092300107NM 2005 9 23 05FDEA03035 120050921A5311 FRAME BOEING727 727232 1384082NM BS 950C DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 AFT CARGO BAY, FRAME IS DENTED AT BS 950C BETWEEN STR 25R AND STR 26R. REPAIRED FRAME AT BS 950C, STR 25R-26R PER SRM 51-40-3. 2L73 4F A3WE 20050923001312005092300131NM 2005 9 23 AWXA200501093 120050920A7797HAB14350 TERMINAL BLOCK BOEING737 7373B7 1384580NM NR 2 ENGINE INOPERATIVE A AWXAA UNSCHED LANDING O OTHER CRCRUISE 1 WP28332AW 23384 LAS - DIVERSION - FLT 0282 - DURING CRUISE, EN ROUTE TO SJC, CREW REPORTED THE NR 2 ENGINE EGT WAS FLUCTUATING IN CRUISE WITH ALL OTHER ENGINE PARAMETERS BEING NORMAL. AIRCRAFT DIVERTED INTO LAS AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED TERMINAL BLOCK, T1012. OPERATIONAL CHECKS OF ENGINES WERE GOOD. 2L72 4F RTA16WE 20050923001332005092300133NM 2005 9 23 05FDEA03042 120050922A5313 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 CENTER CARGO, LONGERON CORROSION FOUND AT STA 1701 L50. REPAIR AS PER SRM 53-10-00 FIGURE 2 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2L73 4F RTA22WE 20050923001352005092300135NM 2005 9 23 05FDEA03034 120050921A5311 FRAME BOEING727 727232 1384082NM BS 970 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 FRAME DENTED AT BS 970, ABOVE STR 26L. REPAIRED PER SRM 53-10-1. 2L73 4F A3WE 20050923001372005092300137NM 2005 9 23 PIDA20050128 120050919A5320 INTERCOSTAL BOEING737 737228 13844AGNM BS 312-328 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 INTERCOSTAL AT RBL 11 FROM BS 312 TO BS 328 HAS CORROSION AT CLIP NUT HOLES. REPLACED INTERCOSTAL PER SRM 51-10-1. 2L72 4F RTA16WE 20050923001392005092300139NM 2005 9 23 PIDA20050131 120050921A5320 INTERCOSTAL BOEING737 737228 13844AGNM BS 960 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 INTERCOSTAL AT BS 960 HAS CORROSION FROM RBL 18 TO RBL 45. REPLACED INTERCOSTAL PER SRM 51-10-1. 2L72 4F RTA16WE 20050923001412005092300141NM 2005 9 23 PIDA20050130 120050912A5320 INTERCOSTAL BOEING737 737228 13844AGNM BS 328-344 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 INTERCOSTAL AT LBL 11 FROM BS 328 TO BS 344 HAS CORROSION AT CLIP NUT HOLES. REPLACED INTERCOSTAL PER SRM 51-10-1. 2L72 4F RTA16WE 20050923001432005092300143NM 2005 9 23 PIDA20050136 120050902A534765C3468833 SEAT TRACK BOEING737 737228 13844AGNM BS 519 CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 SEAT TRACK WEB AT LBL 24 HAS A CRACK AT A RIVET HOLE AT BS 519. REPLACED DAMAGED WEB PER SB 737-53-1120 AND SRM 51-10-1. 2L72 4F RTA16WE 20050923001452005092300145 2005 9 23 PIDA20050118 420050906A2565 MOUNT BOEING737 737228 13844AGNM GIRT BAR CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 L1 DOOR GIRT BAR MOUNTS CORRODED AT BS 312 AND BS 344. REPLACED GIRT BAR MOUNTS PER SRM 51-10-1. 2L72 4F RTA16WE 20050923001482005092300148NM 2005 9 23 PIDA20050134 120050921A5320 SEAT TRACK BOEING737 737228 13844AGNM BS 270-294 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 SEAT TRACK AT RBL 42 FROM BS 270 TO BS 294 HAS CORROSION AT CLIP NUT HOLES. REPLACED SECTION OF SEAT TRACK PER DWG 69-40352 AND SRM 51-10-1. 2L72 4F RTA16WE 20050923001512005092300151EA 2005 9 23 COMA0560509 120050918A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01814CA 7387 FLIGHT 5638 - DURING ATL APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE AT 45 DEGREE FLAP POSITION SETTING. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE FIRST EVENT MAINTENANCE ACTION PARAGRAPH (B) 1, 2, 3 (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2L72 4F RTA21EA 20050926000032005092600003EA 2005 9 26 COMA0560511 120050919A3241 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA ANTI SKID SYS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01458CA 7613 FLIGHT 4940 - INBOARD ANTI-SKID CAUTION. RESET THE ANTI-SKID CONTROL UNIT. 2L72 4F RTA21EA 20050926000042005092600004EA 2005 9 26 SWIA200515557 120050402A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA BS 484 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07917SW 7641 FS 484 LT INTERCOSTAL LBL 27 CLIP AND LBL 36 ANGLE CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED INTERCOSTAL CLIP IAW CRJ REO 601R-53-41-059 REV "A". REPAIR INTERCOSTAL FLANGE LBL 36 IAW REO 601R-53-41-059 REV "A". 2L72 4F RTA21EA 20050926000062005092600006SO 2005 9 26 RAIA00509038 120050922A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN LOOSE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03846HK 14500855 FLT 5542 - DSM - EMERGENCY LIGHT STRIP NEEDS TO BE ATTACHED. MAINTENANCE REINSTALLED THE EMERGENCY LIGHT STRIP AT 1A. 2L72 4T RTT00011AT 20050926000122005092600012SO 2005 9 26 RAIA00509039 120050922A3397 WIRE EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DAMAGED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03813HK 145044 FLT 5542 - STL - EMERGENCY LIGHT INOP AT SERVICE DOOR. MAINTENANCE REPAIRED WIRING TO EXIT LIGHT ASSEMBLY. 2L72 4T RTT00011AT 20050926000132005092600013GL 2005 9 26 RAIA00509032 220050920A7320 SENSOR EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 2 ENGINE MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03846HK 14500855 312671 FLT 8030 - DEN - NR 2 ENGINE NO DISPATCH DISPLAYED ON THE EICAS. MAINTENANCE REMOVED AND REPLACED THE NR 4 PO SENSOR. 2L72 4T4 FRTT00011ATTE6CH 20050926000212005092600021NM 2005 9 26 USAA051137 120050921A5320 SPLICE BOEING737 7374B7 1384702NM BS 360 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19443US 24842 FOUND STRINGER CRACKED BS 360 STRINGER 15L. REPLACED WITH IDENTICAL PART, REMOVED AND REPLACED STRINGER SPLICE IAW SRM 51-40-02, DEFECT SIZE: .250". 2L72 4F RTA16WE 20050926000222005092600022NM 2005 9 26 USAA051136 120050921A5320 STRINGER CLIP BOEING737 7374B7 1384702NM STA 500G CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19443US 24842 FOUND TIE CLIP CRACKED STA 500 G STRINGER 8R. DEFECTIVE PART REPLACED WITH IDENTICAL PART, REMOVED AND REPLACED STRINGER TIE CLIP IAW SRM 51-40-02, DEFECT SIZE: .250". 2L72 4F RTA16WE 20050926000242005092600024NM 2005 9 26 USAA051134 120050921A5320 INTERCOSTAL BOEING737 7374B7 1384702NM BS 312-328 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19443US 24842 FOUND INTERCOSTAL CORRODED BETWEEN STATION 312 AND 328. MAJOR REPAIR IAW SRM 51-40-02, DEFECT SIZE: 3/16". 2L72 4F RTA16WE 20050926000252005092600025NM 2005 9 26 USAA051133 120050921A5330 SKIN BOEING737 7374B7 1384702NM BS 380 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 FOUND FUSELAGE CRACKED, BS 380 JUST BELOW S-8L. CUTOUT CRACKED AREA INSTALLED REPAIR PER T/R 53-10-20B, DEFECT SIZE: 1". 2L72 4F RTA16WE 20050926000262005092600026NM 2005 9 26 SWAA052884 120050922A3350101073 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 17 ABC. SECURED LENS PER MM. 2L72 4F RTA16WE 20050926000272005092600027EU 2005 9 26 USAA200509003 120050920A5315D5347219021100 FLOORBEAM AIRBUS320 A320214 3930316EU FS 66 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19115US 1171 1 INCH BY 1 INCH CORROSION AT -Y1292 FLOORBEAM AT FS 66. REPLACED FLOORBEAM PER SRM 51-72-11. 2L72 4F RTA28NM 20050926000292005092600029EU 2005 9 26 USAA200509005 120050920A5315D5347209001000 FLOORBEAM AIRBUS320 A320214 3930316EU FS 66 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19115US 1171 3" BY 3" CORRODED AREA AT LT CABIN FLOORBEAM Y1292 AT FS 66. REPLACED FLOORBEAM PER SRM 51-72-11. 2L72 4F RTA28NM 20050926000322005092600032EA 2005 9 26 SWIA200515561 120050402A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 621 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07917SW 7641 FS 621 FLOORBEAM ANGLE RBL 42 CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED ANGLE IAW CRJ REO 601R-53-61-117 REV "B". 2L72 4F RTA21EA 20050926000332005092600033EA 2005 9 26 SWIA200515562 120050402A5320 WEB CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07917SW 7641 AFT FUSE ESB LWR WEB LBL 38 CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED DAMAGE IAW CRJ REO 601R-53-61-366 REV E. 2L72 4F RTA21EA 20050926000342005092600034EA 2005 9 26 SWIA200515563 120050918A2760C13045BA04 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07719SK294 294 10188 "SSCU 1 FAULT" AND "SPL/STAB FAULT" STATUS MSGS. REPLACED NR 1 SSCU IAW CRJ MM 27-41-00. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050926000352005092600035SO 2005 9 26 SWIA200515564 120050915A3350 LAMP EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07186SW 120034 ROW 9A FLOOR EMERGENCY LIGHTING, ONE RED LIGHT INOP. RELAMPED BULB TO LIGHT SOCKET, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050926000362005092600036EA 2005 9 26 SWIA200515565 120050918A3520 OXYGEN MASK CNDAIRCL600 CL6002B19 1900309EA CABIN DEPLOYED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07597SW 7293 PASSENGER O2 MASKS DEPLOYED WHILE SETTING FIELD ELEVATION FROM 3860' TO 4220'. REINSTALLED MASKS AND ALL DOORS RESET PER MM 35-20-00. 2L72 4F RTA21EA 20050926000372005092600037EA 2005 9 26 SWIA200515566 120050919A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07590SW 7077 3RD CABIN POD EMERGENCY LIGHT INOP. REPLACED LAMP. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050926000382005092600038 2005 9 26 SWIA200515567 420050914A3418 CONTROL PANEL EMB 120 EMB120ER 3260203SO STALL WARNING MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07295SW 120322 STALL WARNING LIGHT ON MAP STAYS ILLUMINATED. REPLACED STALL WARNING PANEL, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050926000392005092600039EA 2005 9 26 SWIA200515568 120050914A2711 TRIM PANEL CNDAIRCL600 CL6002B19 1900309EA AILERON TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07965SW 7871 AILERON TRIM DOESN'T WORK TO THE RIGHT. REPLACED FLIGHT CONTROL TRIM SWITCH PANEL. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050926000412005092600041EA 2005 9 26 SWIA200515570 120050918A3520 OXYGEN MASK CNDAIRCL600 CL6002B19 1900309EA CABIN DEPLOYED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07413SW 7102 O2 MASKS DROPPED (UNCOMMANDED). RESTOWED ALL O2 MASKS. NO DEFECTS NOTED OF PAX O2 SYSTEM. OPERATIONAL CHECK SYSTEM PER CRJ MM 35-20-00. 2L72 4F RTA21EA 20050926000452005092600045EA 2005 9 26 SWIA200515574 120050603A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07710BR FS 280 RT FLOORBEAM INBOARD AND OUTBOARD RBL 9.0 ATTACH ANGLES CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLES IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13, 51-23-00. 2L72 4F RTA21EA 20050926000482005092600048EA 2005 9 26 SWIA200515576 120050921A2741 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB TRIM INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07915SW 7615 STAB TRIM CH. 2 WILL NOT ENGAGE. REPLACED FO'S TRIM SWITCH. OPERATIONAL CHECK GOOD IAW 27-41-05 AND 27-41-30. 2L72 4F RTA21EA 20050926000502005092600050EA 2005 9 26 SWIA200515578 120050916A27604916406 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED LDLANDING 1 NM07958SW6716 6716 7833 SPOILERON FAULT ON TOUCH DOWN. REPLACED NR 1 SECU. OPERATIONAL CHECK GOOD IAW CRJ 200 M/M 27-61-05. 2L72 4F RTA21EA 20050926000522005092600052EA 2005 9 26 SWIA200515580 120050916A3350 POWER SUPPLY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INTERMITTENT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07439SW 7578 FLOOR EMERGENCY LIGHT STRIP INTERMITTENT. REPLACED FWD POWER SUPPLY LIGHTING SECTION ELECTRICAL SUPPLY IAW MM 33-51-00. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050926000562005092600056NM 2005 9 26 USAA051140 120050922A53206545834551 INTERCOSTAL BOEING737 7374B7 1384702NM BS 312-328 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19443US 24842 INTERCOSTAL CRACKED LBL 45 BETWEEN STA 312 AND 328. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-40-02, DEFECT SIZE: .250" CRACK. 2L72 4F RTA16WE 20050926000612005092600061NM 2005 9 26 ASMF200509010 120050918A27205914387509 ACTUATOR DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE RUDDER MALFUNCTIONED W ASMFK NONE J WARNING INDICATION ININSP/MAINT 1 SW23881LF 53051 CAPTAIN REPORTED THAT RUDDER TRAVEL UNRESTRICTED LIGHT TURNED ON. THE RUDDER POSITION SENSOR WAS CHECKED AND CLEANED IAW MM 27-20-00. NON ROUTINE CARD NR A0082196 TO RUDDER TRAVEL UNRESTRICTED LIGHT TURNED ON WAS GENERATED TO REPLACE RUDDER THROW LIMITER. THE RUDDER LIMIT ACTUATOR WAS REPLACED IAW MM 27-20-06, TESTED CORRECT. 2L72 4F4 FRT E9NE 20050926000662005092600066NM 2005 9 26 USAA051094 120050920A53201131305 SPLICE BOEING737 7374B7 1384702NM BS 907 DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 FOUND SPLICE BS907, STRINGER S4R. REMOVED DAMAGED PARTS, AND INSTALLED NEW PARTS IAW SRM 51-10-02, DEFECT SIZE: 1/2" CRACK. 2L72 4F RTA16WE 20050926000692005092600069EA 2005 9 26 COMA0560499 120050913A5210 LATCH CNDAIRCL600 CL6002B19 1900309EA PAX DOOR UNSECURE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01409CA 7441 FLIGHT 5856 - RECEIVED A CABIN DOOR HANDLE CAUTION MESSAGE DURING CLIMBOUT OF SAT. FLIGHT RETURNED TO SAT. FOUND THE OUTER CABIN DOOR HANDLE NOT FULLY STOWED, OPERATIONAL CHECK INDICATED NO DISCREPANCIES. 2L72 4F RTA21EA 20050926000712005092600071EA 2005 9 26 COMA0560501 120050914A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01956CA194919961 7105 FLIGHT 4960 - FLAPS FAIL CAUTION. REPLACED THE LEFT BPSU. 2L72 4F RTA21EA 20050926000722005092600072EA 2005 9 26 COMA0560502 120050914A2750860D10018 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01506CA6992 7793 FLIGHT 5554 - FLAPS FAIL CAUTION. CND, REPLACED THE PDU AND THE FECU. 2L72 4F RTA21EA 20050926000762005092600076EA 2005 9 26 COMA0560504 120050915A2150150T471 THERMOSWITCH CNDAIRCL600 CL6002B19 1900309EA CARGO BAY MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01821CA 7420 FLIGHT 5267 - CARGO OVERHEAT WARNING. REPLACED THE DUCT OVERTEMP SWITCH. 2L72 4F RTA21EA 20050926000772005092600077EA 2005 9 26 COMA0560506 120050917A2910D97C00614 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA NR 2 HYD SYSTEM FAULTY A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01941CA 7050 FLIGHT 5321 - DURING CLIMBOUT OF CVG THE NR 2 HYDRAULIC C/B TRIPPED. REPLACED THE NR 2 HYDRAULIC SOV ACTUATOR. 2L72 4F RTA21EA 20050926000782005092600078NM 2005 9 26 QXEA200501255 120050918A299710962242 CONTACTOR BOMBDRDHC8 DHC8402 1390042NM HYD PUMP DAMAGED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09416QX2078 4083 NR 3 HYDRAULIC PUMP CAUTION ILLUMINATED ON TAXI TO GATE. MAINTENANCE REPLACED DC CONTACTOR K-23 AND RELAY RL4 (P/N M610619-022, QX CODE 6-2431-1-0009). PERFORMED BLEEDING OF THE NR 3 HYDRAULIC SYSTEM IAW Q400 TASK 29-10-00-870-803. PERFORMED FUNCTIONAL TEST OF THE NR 3 HYDRAULIC SYSTEM IAW TASK 29-12-00-720-801. FUNCTIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050926000822005092600082NM 2005 9 26 QXEA200501250 120050917A3240 BRAKE DHAV DHC8 DHC8202 2809007NM MLG CONTAMINATED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM09360PH 515 ON FLIGHT 2219, PASSENGERS AND FUELER REPORTED MODERATE SMOKE COMING FROM RIGHT (FO SIDE) OUTBOARD BRAKE ASSEMBLY. INSPECTED NR 3 AND NR 4 BRAKES. NO LEAKS NOTED. FOUND RESIDUAL HYDRAULIC FLUID FROM ANTI-SKID TEST DONE BEFORE PREVIOUS FLIGHT. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2H72 4T RTA13NM 20050926000862005092600086EA 2005 9 26 MASA200500057 120050125A2120 ODOR CNDAIRCL600 CL6002D24 1390016EA LAVATORY DETECTED A MASAA UNSCHED LANDING JB WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW07907FJ 15007 ASH 6216 PHX-PHX - THE CREW RETURNED THE AIRCRAFT TO THE FIELD DUE TO THE AFT LAVATORY SMOKE DETECTOR SOUNDING FOR APPROXIMATELY 8 SECONDS AND THE FLIGHT ATTENDANT NOTICING AN UNUSUAL ODOR AT THE AFT LAVATORY AREA. MAINTENANCE INSPECTED THE LAVATORY AREA AND PERFORMED ENGINE RUNS WITH NO DEFECTS NOTED. 2L72 4F RTA21EA 20050926000872005092600087NM 2005 9 26 QXEA200501246 120050920A2120 ODOR DHAV DHC8 DHC8202 2809007NM CABIN DETECTED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 NM09350PH 488 PDX FLIGHT NR 2082, AFTER TAKEOFF AND TURNING ON BLEEDS, AIR SMELLED LIKE OLD GYM SOCKS. ALSO, ON DESCENT WITH LOW POWER SETTINGS, SAME SMELL ALL THE WAY TO THE GATE. MINOR ODOR IN CRUISE. MAINTENANCE RAN BOTH ENGINES AT START/FEATHER AND MIN, TURNED ON ENGINE BLEEDS NE AT A TIME. NO SMELLS FOUND COMING FROM AIR CONDITIONING SYSTEM. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050926000932005092600093NM 2005 9 26 SWAA052869 120050920A53306545877 SKIN BOEING737 7373H4 1384600NM BS 328 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29347SW 24374 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 328, STR 19R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050926000952005092600095NM 2005 9 26 SWAA052871 120050920A53306545768 SKIN BOEING737 7373H4 1384600NM BS 445-500B CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 445 & BS 500B, STR 18R TO STR 19R. REPAIRED SKIN PER SRM & SWA EA. 2L72 4F RTA16WE 20050926000972005092600097NM 2005 9 26 SWAA052873 120050921A53116546558 FRAME BOEING737 7373H4 1384600NM BS 907 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907 BETWEEN STR 8L & STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050926000992005092600099NM 2005 9 26 SWAA052875 120050921A53206551698 SPLICE BOEING737 7373H4 1384600NM BS 907 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29618WN 28034 DURING SCHEDULED D-CHECK, FOUND STR SPLICE CRACKED AT BS 907, STR 4R. REMOVED AND REPLACED STR SPLICE PER SRM. 2L72 4F RTA16WE 20050926001012005092600101NM 2005 9 26 SWAA052877 120050921A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM BS 995 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29618WN 28034 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STR CORRODED AT BS 995, STR 21R. REPAIRED STR SECTION PER SRM. 2L72 4F RTA16WE 20050926001022005092600102NM 2005 9 26 SWAA052878 120050921A53306545765 SKIN BOEING737 7375H4 138449DNM BS 482B CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29506SW 24183 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 482B + 3, ABOVE STR 7L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050926001032005092600103NM 2005 9 26 SWAA052879 120050921A53116546531 FRAME BOEING737 7373H4 1384600NM BS 494 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 494, FWD CARGO DOOR CUTOUT LOWER STOP FITTING. REPAIRED FRAME PER SWA EA. 2L72 4F RTA16WE 20050926001052005092600105NE 2005 9 26 QXEA200501245 220050919A73204120T02P02 ACTUATOR CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 30049NE FUEL SYSTEM LEAKING A QXEAO OTHER K FLUID LOSS NRNOT REPORTED 1 NM09613QX5535 10045 PDX - NR 1 ENGINE FUEL LEAK. MAINTENANCE REPLACED THE VG SLAVE ACTUATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E00063EN 20050926001092005092600109NM 2005 9 26 ASMF200509009 120050918A32465930594547 WHEEL DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE MLG DAMAGED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23831LF 53050 DURING TRANSIT CHECK THE MAIN LANDING GEAR WHEELS WERE DETECTED CONTAMINATED WITH RUNWAY RE-COVER MATERIAL. THE WHEELS WERE CHECKED; THE WHEEL POSITION 2 WAS REPLACED AND A GENERAL REVISION WAS PERFORMED AT ENGINES AND FLIGHT CONTROL SURFACES IAW MM 32-40-01, MM 05-55-00, MM 05-50-00 RESPECTIVELY, NONE DAMAGE WERE FOUND, ALL CORRECT. 2L72 4F4 FRT E9NE 20050926001112005092600111EA 2005 9 26 COMA0560496 120050913A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01447CA 7552 FLIGHT 5651- DURING TAXI OUT RECEIVED A FLAP FAIL CAUTION MESSAGE. FLIGHT RETURNED TO GATE. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE FIRST EVENT MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2L72 4F RTA21EA 20050922000012005092200001EA 2005 9 22 MASA200500526 120050707A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA MAIN PAX STIFF A MASAO OTHER O OTHER TXTAXI/GRND HDL 1 SW0727172 7172 ASH 2724 CLE. MAIN PAX DOOR DIFFICULT TO OPEN ON ARRIVAL TO PHL. MX PERFORMED OPS CHECK OF DOOR AND COULD NOT DUPLICATE THE DISCREPANCY, ACFT CONTINUED OPERATIONS. 2L72 4F RTA21EA 20050922000222005092200022EU 2005 9 22 2005UALA00983 120050912A3350 LAMP AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29416UA 479 EMERGENCY EXIT LIGHT OUT AT SEAT 6ABC. RELAMPED EMERGENCY EXIT LIGHT AT SEAT 6ABC 2L72 4F4 FRTA28NM E40NE 20050922000302005092200030NM 2005 9 22 05FDEA02983 120050918A5744 ATTACH FITTING DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 LT WING, O/B FLAP O/B HINGE (WING SIDE), SIDE LINK ATTACHMENT FWD BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. FABRICATED BUSHING AND INSTALLED AS PER EA 1-5750-87640. 2L73 4F RTA22WE 20050922000322005092200032EU 2005 9 22 DXTA200500975 120050918A2721 TRIM SYSTEM ISRAELGALAXYGALAXY 4500307EU MALFUNCTIONED E DXTAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 GL07700QS 052 IMMEDIATELY AFTER TAKEOFF THE NORMAL PITCH TRIM FROZE AT 2.6 DEG SETTING. AFTER SEVERAL MINUTES AND SEVERAL ATTEMPTS AT NOSE DOWN TRIM, SYSTEM WORKED NORMAL, HOWEVER SPEED WAS < 180 KIAS. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA53NM 20050922000342005092200034CE 2005 9 22 DXTA200500974 120050917A3246 WHEEL CESSNA750 750 2076810CE NLG LOOSE E DXTAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 GL07962QS 7500126 TAKEOFF ABORTED UNDER 80 KTS DUE TO SEVERE VIBRATION FROM NOSEWHEEL. INSPECTED BOTH NOSE WHEELS AND TIRES, FOUND LEFT WHEEL LOOSE. REMOVED BOTH WHEELS, CHECKED BALANCE, BALANCE CHECKS GOOD. REINSTALLED BOTH NOSE WHEELS AND RETORQUED WHEELS. INSPECTED WHEEL WELL AND NOSE DOORS. NO DEFECTS. WORK DONE IAW CH 32-41-01 OF THE 750 MM. 2L72 4J RTT00007WI 20050922000352005092200035CE 2005 9 22 DXTA200500977 120050920A2120 ODOR BEECH MU300 400A 1155402CE CABIN DETECTED E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07140QS RK406 WHEN ENGINE, WING, AND TAIL ANTI ICE ON STRONG ODOR WAS PRESENT IN CABIN. ITEM IS UNDER INVESTIGATION. 2H72 4F RTA16SW 20050922000422005092200042EA 2005 9 22 MASA200500637 120050812A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA MAIN PAX STUCK A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0717156 7156 ASH 2611 PHL. UPON ARRIVAL UNABLE TO OPEN PAX DOOR. MAINTENANCE PERFORMED AN OPERATIONAL CHECK AND RETURNED THE AIRCRAFT TO SERVICE. 2L72 4F RTA21EA 20050922000682005092200068NM 2005 9 22 USAA051107 120050920A5510657378211 BUSHING BOEING737 7374B7 1384702NM HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 FOUND CORROSION LT HORIZ STAB, FWD L2 LUG BUSHING. REMOVED CORROSION AND INSTALLED BUSHING IAW SRM 55-10-10, DEFECT SIZE: 1" X 2" AREA OF CORROSION. 2L72 4F RTA16WE 20050922000782005092200078NM 2005 9 22 USAA051127 120050920A5313US654577211F STRINGER BOEING737 7374B7 1384702NM BS 907 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19776AU 24934 FOUND FUSELAGE STR SPLICE AT STA 907 STR 4L. INSTALLED STRINGER SPLICE IAW SRM 51-40-02, DEFECT SIZE: .75" CRACK. 2L72 4F RTA16WE 20050922000852005092200085EA 2005 9 22 MASA200500651 120050817A3250 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA NLG STEERING MALFUNCTIONED A MASAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 SW07571ML 7209 ASH 2780 PHL. ABORTED TAKEOFF DUE TO THE AIRCRAFT TURNED TO THE RIGHT ON TAKEOFF AND WOULD NOT RESPOND TO RUDDER INPUTS. MX PERFORMED OPS CHECK OF NWS. 2L72 4F RTA21EA 20050922000962005092200096CE 2005 9 22 09122005A 120050909A61235038912147 PRESSURE SWITCH BEECH 1900 1900D 1154162CE AUTOFEATHER SYS FAILED A NSVAO OTHER L NO TEST TXTAXI/GRND HDL 1 EA27152MJ UE52 RT AUTOFEATHER FAIL TEST. REMOVED AND REPLACED LOW PRESSURE SWITCH OPS CHECK GOOD. 2L72 4T RTA24CE 20050922000972005092200097CE 2005 9 22 09122005B 120050909A6120 POWER LEVER BEECH 1900 1900D 1154162CE RIGHT OUT OF ADJUST A NSVAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 EA27220CJ UE20 RIGHT ENGINE POWER LEVERS GO INTO REVERSE WHEN POSITION IS GROUND FINE. ADJUSTED LOW PITCH TORQUE (GND IDLE TORQUE.) RUN UP CHECKS NORMAL. REF BMM 76-00-00. 2L72 4T RTA24CE 20050922001172005092200117NM 2005 9 22 SWAA052864 120050920A53116546593 FRAME BOEING737 7373H4 1384600NM BS 500B CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SWA EA. 2L72 4F RTA16WE 20050922001242005092200124NM 2005 9 22 SB05117 120050920A335020121 POWER SUPPLY BOEING737 7374B7 1384702NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US 24781 MCO - MAINTENANCE REPORTED THE EMERGENCY EXIT SIGNS FOR THE AFT GALLEY DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT AFT GALLEY POWER SUPPLY ALONG WITH THE BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050922001302005092200130NM 2005 9 22 SWAA052854 120050920A53116558280 FRAME BOEING737 7373H4 1384600NM BS 360 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050922001342005092200134NM 2005 9 22 SWAA052858 120050920A53116546550 SHEAR TIE BOEING737 7373H4 1384600NM BS 787 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29618WN 28034 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, LBL 18 TO RBL 18. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050922001352005092200135NM 2005 9 22 SWAA052859 120050920A53116546593 SHEAR TIE BOEING737 7373H4 1384600NM BS 500A CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29618WN 28034 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500A, STR 28L TO STR 28R. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050923000032005092300003NM 2005 9 23 TSAA0536040 120050914A361041SG2651 TRANSDUCER BOEING737 73776N 13844CHNM DUCT PRESSURE FAILED A TSAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP13741AL 28641 ETOPS FLIGHT 484 HNL-SNA. DUCT PRESSURE SPLIT ON CLIMB (FL 290) LEFT DUCT AT 26 PSI. RIGHT DUCT AT 46 PSI. N1 AND N2 THE SAME ON BOTH ENGINES. AT FL370 LEFT DUCT AT 20 PSI. RIGHT DUCT AT 44 PSI. N1 AND N2 SAME ON BOTH ENGINES. CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND DUCT PRESSURE TRANSDUCER. MAINTENANCE ALSO REMOVED AND REPLACED THE PRECOOLER CONTROL VALVE SENSOR (P/N: 129666-2, S/N: 8315) AS A PRECAUTION. ALL OPERATIONAL AND LEAK CHECKS GOOD. A TEST FLIGHT WAS CONDUCTED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA16WE 20050923000092005092300009EU 2005 9 23 AWXA200501079 120050903A5347D57130147200 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28634AW 091 DURING C4 CHECK DISCOVERED EXFOLIATION CORROSION ON LT INBOARD SEAT TRACK AT FR 36 AND Y765. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 101. MAINTENANCE REMOVED SEAT TRACK FROM FR 36 TO FR 41 AND Y765 IAW AIRBUS 320 SRM 51-42-11. RECEIVED NEW SEAT TRACK AND INSTALLED FROM FR 36 TO FR 41 AND Y765 IAW AIRBUS 320 SRM 51-42-11 AND 51-72-11. 2L72 4F RTA28NM 20050923000142005092300014EU 2005 9 23 AWXA200501084 120050903A5347D53371100100 SEAT TRACK AIRBUS320 A320231 3930325EU FR 41-47 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28634AW 091 DURING C4 CHECK DISCOVERED EXFOLIATION CORROSION ON RT INBOARD SEAT TRACK AT FS 41+11", Y-765. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 101. MAINTENANCE REMOVED SEAT TRACK FROM FS 41 TO FS 47, Y-765 IAW AIRBUS 320 SRM 51-42-11. RECEIVED NEW SEAT TRACK AND INSTALLED FROM FS 41 TO FS 47, Y-765 IAW AIRBUS 320 SRM 51-42-11 AND 51-72-11. 2L72 4F RTA28NM 20050923000242005092300024WP 2005 9 23 UPS05845474 120050911A5322 SHEAR TIE DOUG DC8 DC871F 302199DWP BS 55 L34L-L34R CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 INSPECTION TYPE:SP AT STA 55 IN BETWEEN L34L AND L34R HAS CORROSION BEYOND LIMIT ON SHEER TIE. REMOVED, FABRICATED AND INSTALLED SHEER TIE IAW SRM 53-03-01, 51-3-2, 51-1-21 AND 51-1-20D. 2L74 4F RT4A25 20050923000362005092300036EU 2005 9 23 AALA20050608 120050920A3350 BATTERY PACK AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2180058 466 JFK - EMERGENCY LIGHTS ON RIGHT HAND SIDE AT ZONE-C INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS ON RIGHT HAND SIDE AT ZONE-C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20050923000372005092300037WP 2005 9 23 AALA20050606 120050920A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21510AM 49804 ATL - OVERWING EMERGENCY LIGHT ON LEFT AND RIGHT HAND SIDES INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING EMERGENCY LIGHTS ON LEFT AND RIGHT HAND SIDES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050923000422005092300042WP 2005 9 23 AALA20050604 120050919A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21435AA 49453 SFO - OVERHEAD EMERGENCY LIGHTS FROM ROWS 23 TO 36 INOPERATIVE. REPLACED BATTERY PACK B5106 FOR OVERHEAD EMERGENCY LIGHTS FROM ROWS 23 TO 36. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050923000522005092300052EU 2005 9 23 09212005G 120050920A3232NAS6404A13 BOLT SAAB SF340 340B 7860101EU MLG DOOR ACT MISSING A NSVAO OTHER O OTHER LDLANDING 1 EA27339CJ 339 RIGHT OUTBOARD LANDING GEAR DOOR WAS OPEN UPON LANDING (DOOR RETRACT ACTUATOR MISSING BOLT). INSTALLED MISSING HARDWARE AS REQUIRED. 2L72 4T RTA52EU 20050923000612005092300061NM 2005 9 23 PIDA20050109 120050914A5320 WEB BOEING737 7373G7 1384595NM BS 986 CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05370WL 24011 CLOSE OUT WEB CRACKED IN AFT CABIN AT BS 986 AND RBL 44. REPAIRED PER SRM 51-70-13. 2L72 4F RTA16WE 20050923000722005092300072NM 2005 9 23 05FDEA02886 120050914A5240 SKIN BOEING727 727227 1384078NM R1 DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 N00364 - R-1 DOOR SKIN IS CRACKED AT UPPER HINGE. 2L73 4F A3WE 20050923001472005092300147NM 2005 9 23 PIDA20050133 120050902A53206546812169 INTERCOSTAL BOEING737 737228 13844AGNM BS 967-987 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 INTERCOSTAL AT LBL 18 FROM BS 967 TO BS 987 HAS CORROSION. REPLACED INTERCOSTAL PER SRM 51-10-1. 2L72 4F RTA16WE 20050923001522005092300152EA 2005 9 23 COMA0560510 120050919A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01984CA 7171 FLIGHT 5795- LEFT ENGINE REVERSER UNLOCK CAUTION. DEFERRED MAINTENANCE ON T/R PER MEL. 2L72 4F RTA21EA 20050926000052005092600005EA 2005 9 26 SWIA200515558 120050402A5340 FITTING CNDAIRCL600 CL6002B19 1900309EA BS 460 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07917SW 7641 FS 460 OB FLOOR FITTING RBL 9.0 CRACKED, ITEM FOUND AT C-CHECK INSPECTION. FITTING REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, 51-21-11. 2L72 4F RTA21EA 20050926001152005092600115EU 2005 9 26 05FDEA02995 120050919A5320 FLOOR SUPPORT AIRBUS310 A310203 3930313EU FR 11-12A CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25425FE 264 FWD MDCC UNDERFLOOR FLOOR PANEL SUPPORT FROM FRAME 11-12A, LBL 30 IS CORRODED AND CRACKED AT LOWER SURFACE. REMOVED AND REPLACED PANEL SUPPORT IAW SRM 51-40-00, PART FABRICATED ON PCT NR T5/546112. 2L72 4F RTA35EU 20050926001162005092600116EU 2005 9 26 05FDEA02996 120050919A5320 FLOOR SUPPORT AIRBUS310 A310203 3930313EU FR 13-15 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25425FE 264 FWD MDCC UNDERFLOOR AREA FLOOR PANEL SUPPORT BETWEEN FRAMES 13-15 LBL 58 IS CORRODED. REMOVED CORROSION IAW SRM 51-22-00 ORIG MAT=.079 AFTER =.042 OUT OF LIMITS IAW SRM 53-12-15. REMOVED DAMAGED SUPPORT IAW SRM 51-40-21. LOCATED AND DRILLED NEW SUPPORT IAW SRM 51-40-44. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-40-21. 2L72 4F RTA35EU 20050926001182005092600118NM 2005 9 26 QXEA200501243 120050919A4920 APU BOMBDRDHC8 DHC8402 1390042NM APU BAY SMOKE A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM09400QX 4030 GEG FLIGHT NR 2395: APU WAS RUNNING ABOUT 2 MINUTES. STARTED TO HEAT CABIN RAPIDLY, THEN SMOKEY HAZE FILLED THE CABIN. TURNED OFF APU. MAINTENANCE DEFERRED PER MEL 49-00-1, RSI 352431. MAINTENANCE REMOVED AND REPLACED THE APU IAW MTC 6492001. OPS CHECK GOOD. RAN BLEEDS FULL HOT. NO HAZE NOTED. CLEARS RSI #352431. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050926001222005092600122EU 2005 9 26 05FDEA03002 120050920A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25681FE 799 MDCC SEAT TRACK R2 FS 54.2 - FS 54.3 HAS DAMAGE IN SCALLOP AREA. FABRICATED SEAT TRACK SECTION AND INSTALLED WITH 2 EA SPLICES IAW A300-600 SRM 53-10-16. ALODINED, PRIMED, AND TOPCOATED IAW A300-600 SRM 51-75-10. 2L72 4F RTA35EU 20050926001232005092600123EA 2005 9 26 MASA200500058 120050125A2760 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA LIFT DUMP ILLUMINATED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07508MJ 10087 ASH 7262 TUS-IAD - THE CREW ABORTED THE TAKEOFF DUE TO A GROUND LIFT DUMP UNSAFE CAUTION MESSAGE DURING TAKEOFF ROLL. MAINTENANCE REST THE SYSTEM AND PERFORMED AN OPERATIONAL CHECK WITH NO DEFECTS NOTED. 2L72 4F RTA21EA 20050926001252005092600125NM 2005 9 26 BB05081 120050921A3397 SOCKET BOEING757 7572B7 1384964NM L4 DOOR FAILED A USAAK NONE O OTHER ININSP/MAINT 1 EA19613AU 27144 CLT - MAINTENANCE REPORTED THE L4 EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT SOCKET ASSEMBLY. OPERATIONAL CHECK GOOD. 2L72 4F RTA2NM 20050926001262005092600126EU 2005 9 26 AWXA200501103 120050903A5320D53480020696 STRUCTURE AIRBUS320 A320231 3930325EU CARGO FLOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28634AW 091 SAL - DURING C4 CHECK, DISCOVERED 7 INCH CRACK ON TRAY LOCATED ON FLOOR STRUCTURE BETWEEN FS 68 AND FS 69, Y1292. NO ALLOWABLE DAMAGE LIMITS WERE FOUND IN THE AIRBUS 320 SRM. MAINTENANCE REMOVED TRAY ON FLOOR STRUCTURE BETWEEN FS 68 AND FS 69, Y1292 IAW AIRBUS SRM 51-72-11. INSTALLED NEW TRAY ON FLOOR STRUCTURE BETWEEN FS 68 AND FS 69 IAW AIRBUS SRM 51-72-11. 2L72 4F RTA28NM 20050926001282005092600128WP 2005 9 26 ASMF200509011 120050920A71105930645503 NOSE COWL DOUG DC9 DC987 3022087WP LT ENGINE DAMAGED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23204AM 49404 DURING TRANSIT CHECK, DETECTED A HIT ON LEFT NOSE COWLING OUT OF LIMITS BY FOREIGN OBJECT DAMAGE. THE LEFT NOSE COWLING WAS REPLACED IAW MM 71-10-01 AND ANTI-ICE TEST WAS PERFORMED IAW MM 36-10-00, BEING CORRECT. 2L72 4F RTA6WE 20050926001292005092600129NM 2005 9 26 AWXA200501094 120050922A3350BR964411 LIGHT BOEING737 73733A 1384673NM CABIN INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 PHX - EEL - DURING 4 DAY CHECK, DISCOVERED PASSENGER ROW NR 18 EMERGENCY EXIT LIGHT FAILED TO ILLUMINATE DURING TEST. MAINTENANCE REMOVED AND REPLACED ROW NR 18 EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONAL TESTS WERE GOOD. 2L72 4F RTA16WE 20050926001302005092600130EU 2005 9 26 AWXA200501095 120050922A2730 CONTROL UNIT AIRBUS320 A320232 3930326EU SERVO CONTROL MALFUNCTIONED A AWXAO OTHER E VIBRATION/BUFFET CRCRUISE 1 WP28602AW 565 DEPARTING PHX, EN ROUTE TO SAN, CREW REPORTED DURING LEVEL OFF GOING THROUGH 330 KTS IAS AT 220K FT MSL AIRPLANE SHOOK ON LONG AXIS AT ABOUT 4-10 CYCLES PER SECOND SHAKING STOPPED BELOW 300KTS IAS. AIRCRAFT DECLARED EMERGENCY AND LANDED IN SAN WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLE SHOT IAW AIRBUS 320 TROUBLE SHOOTING MANUAL 27-34-00-200 AND 05-50-00-810-801. REMOVED AND REPLACED THE RT INBOARD, YELLOW, ELEVATOR SERVO CONTROL PER AIRBUS 320 MM 27-34-51-000-001 AND 27-34-51-400-001. VENDOR CONFIRMED FAILURE. FOUND EXCESSIVE OSCILLATING, AND BOTH SPHERICAL BEARINGS FLATTENED OUT. ALSO FOUND INSULATION RESISTANCE TO LOW. UNIT WAS REPAIRED AND TESTED IAW CMM 27-34-52 REV.9. 2L72 4F RTA28NM 20050926001312005092600131EU 2005 9 26 AWXA200501096 120050904A5347D53112782200 SEAT TRACK AIRBUS320 A320231 3930325EU FR 20 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28634AW 091 SAL - MAJOR REPAIR - DURING C4 CHECK DISCOVERED EXFOLIATION CORROSION ON SEAT TRACK AT FS 20, Y-1292. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 101. MAINTENANCE REMOVED SEAT TRACK FROM FS 16+13 TO FS 24, Y-1292 IAW AIRBUS 320 SRM 51-42-11. RECEIVED NEW SEAT TRACK AND INSTALLED FROM FR16+1 TO FR24, Y-1292 IAW AIRBUS 320 SRM 51-42-11 AND 51-72-11. 2L72 4F RTA28NM 20050926001322005092600132EU 2005 9 26 AWXA200501097 120050903A5347D5337111200500 SEAT TRACK AIRBUS320 A320231 3930325EU FR 41-47 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28634AW 091 SAL - MAJOR REPAIR - DURING C4 CHECK DISCOVERED EXFOLIATION CORROSION ON RT OUTBOARD SEAT TRACK FROM FR 41 TO FR 47, Y-1292. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 101. MAINTENANCE REMOVED SEAT TRACK FROM FR 41 TO FR 47, Y-1292 IAW AIRBUS 320 SRM 51-42-11. RECEIVED NEW SEAT TRACK AND INSTALLED FROM FR 41 TO FR 47, Y-1292 IAW AIRBUS 320 SRM 51-42-11 AND 51-72-11. 2L72 4F RTA28NM 20050926001332005092600133EU 2005 9 26 AWXA200501098 120050903A5347D5323046720 SEAT TRACK AIRBUS320 A320231 3930325EU FR 26-27 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28634AW 091 SAL - DURING C4 CHECK DISCOVERED FILIFORM CORROSION ON RT INBOARD SEAT TRACK AT FS 26+15, Y-765. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-15 FIG 101. MAINTENANCE REMOVED SEAT TRACK FROM FS2 6+9 TO FS 27, Y-765 IAW AIRBUS 320 SRM 51-42-11. TWO L PROFILES WERE MACHINED IAW AIRBUS 320 SRM 53-00-15 FIG 201 AND INSTALLED FROM FS 26+9 TO FS 27, Y-765 IAW AIRBUS 320 SRM 51-42-11 AND 51-72-11. 2L72 4F RTA28NM 20050926001342005092600134 2005 9 26 AWXA200501099 420050903A2565D5211155400140 FITTING AIRBUS320 A320231 3930325EU R1 DOOR SLIDE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28634AW 091 SAL - DURING C4 CHECK DISCOVERED CORROSION ON THE AFT SLIDE SUPPORT FITTING FOR THE R1 DOOR. NO ALLOWABLE DAMAGE LIMITS FOUND IN THE AIRBUS SRM. REMOVED AFT SUPPORT FITTING AT THE R1 DOOR IAW AIRBUS 320 51-42-11. INSTALLED NEW FITTING IAW AIRBUS SRM 51-72-11. 2L72 4F RTA28NM 20050926001352005092600135 2005 9 26 AWXA200501100 420050905A2565D5211155400040 FITTING AIRBUS320 A320231 3930325EU L2 DOOR SLIDE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28634AW 091 SAL - DURING C4 CHECK DISCOVERED CORROSION ON THE AFT SLIDE SUPPORT FITTING FOR THE L2 DOOR. NO ALLOWABLE DAMAGE LIMITS FOUND IN THE AIRBUS SRM. REMOVED AFT SUPPORT FITTING AT THE L2 DOOR IAW AIRBUS 320 51-42-11. INSTALLED NEW FITTING IAW AIRBUS SRM 51-72-11. 2L72 4F RTA28NM 20050926001362005092600136EU 2005 9 26 AWXA200501101 120050905A5320D53112198200 FITTING AIRBUS320 A320231 3930325EU FR 16-20 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28634AW 091 SAL - DURING C4 CHECK, DISCOVERED EXFOLIATION CORROSION ON FITTING LOCATED AT Y1584, BETWEEN FS 16 AND FS 20, NEAR THE L1 LOWER SILL. NO ALLOWABLE DAMAGE LIMITS FOUND IN THE AIRBUS SRM. REMOVED FITTING AT Y1584 BETWEEN FS16 AND FS 20 IAW AIRBUS 320 51-42-11. INSTALLED NEW FITTING AT Y1584 BETWEEN FS 16 AND FS 20 IAW AIRBUS SRM 51-72-11. 2L72 4F RTA28NM 20050926001372005092600137EU 2005 9 26 AWXA200501102 120050903A5320D53471124200 PLATE AIRBUS320 A320231 3930325EU FR 69-70 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28634AW 091 SAL - DURING C4 CHECK DISCOVERED CORROSION ON SHEAR PLATE BETWEEN FS 69 AND FS 70. NO ALLOWABLE DAMAGE LIMITS WERE FOUND IN THE AIRBUS 320 SRM. MAINTENANCE REMOVED THE SHEAR PLATE BETWEEN FS 69 AND FS 70, Y1292 IAW AIRBUS SRM 51-72-11. INSTALLED NEW SHEAR PLATE BETWEEN FS 69 AND FS 70 IAW AIRBUS SRM 51-72-11. 2L72 4F RTA28NM 20050926001402005092600140NM 2005 9 26 UPS05M45479 120050921A2710 WARNING LIGHT DOUG MD11 MD11F 3023600NM PWA 4460 PW4460 NE AILERONS ILLUMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01270UP 48576 AILERON DEFLECTED DISAGREE MESSAGE. A/C WAS DIVERTED AND EMERGENCY WAS DECLARED. FUEL WAS DUMPED BELOW MAXIMUM LANDING WEIGHT TO 57000 POUNDS. REPLACED O/B AILERON DEFLECTION ACTUATOR UP TO SUB TASK 27-16-02-820-001 PG 8 PER MM 27-16-02-4. L/P 474801--COMPLETED STEPS 2, F (3) O FMM 27-16-02-4 TO END. COMPLETED ADJUSTMENT OF RT OB AILERON DEFLECTION ACTUATOR. SAFTIED BOTH JAM NUTS ON AILERON DEFLECTION ACTUATOR. [CLOSED] 2L73 4F4 FRTA22WE E24NE 20050926001432005092600143EU 2005 9 26 AWXA200501104 120050905A5320D5347577400000 WEB AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28634AW 091 SAL - DURING C4 CHECK, DISCOVERED CORROSION, BELOW WEB FLANGE, AROUND NUT PLATE AT FS 59+1.5", Y-680, IN THE AFT CARGO COMPARTMENT. NO ALLOWABLE DAMAGE LIMITS FOUND IN THE AIRBUS 320 SRM. MAINTENANCE REMOVED WEB FROM FS 59+1.5" TO FR60 IAW AIRBUS 320 SRM 51-42-11. NEW WEB INSTALLED FROM FS 59+1.5" TO FS 60, Y-680, IN THE AFT CARGO COMPARTMENT IAW AIRBUS 320 SRM 51-72-11. 2L72 4F RTA28NM 20050926001532005092600153NM 2005 9 26 SWAA052888 120050921A53216546833 WEB BOEING737 7375H4 138449DNM BS 188-196 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29505SW 24182 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FLOOR WEB CRACKED BETWEEN BS 188 TO BS 196, LT & RT SIDE, WL 208. REPAIRED FLOOR WEB PER SRM. 2L72 4F RTA16WE 20050926001542005092600154NM 2005 9 26 SWAA052889 120050921A3350D71702001 BATTERY PACK BOEING737 7375H4 138449DNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29519SW 25318 DURING SCHEDULED SERVICE CHECK, FOUND RT EXTERIOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050926001552005092600155NM 2005 9 26 SWAA052890 120050922A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM BS 787 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29618WN 28034 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, LBL 4. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050926001562005092600156NM 2005 9 26 SWAA052891 120050921A3350BR2013 LIGHT BOEING737 7373H4 1384600NM CABIN DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29632SW 27707 DURING SCHEDULED A1 CHECK, FOUND RT CABIN EEPLS STRIP DELAMINATED. REMOVED AND REPLACED STRIP PER MM. 2L72 4F RTA16WE 20050926001572005092600157NM 2005 9 26 SWAA052892 120050921A335020121 FUSE BOEING737 7373H4 1384600NM BATTERY CHARGER FAILED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29635SW 27708 DURING SCHEDULED C3 CHECK, FOUND RT AFT EXTERIOR EMERGENCY LIGHT INOP. REMOVED & REPLACED BATTERY CHARGER FUSE PER MM. 2L72 4F RTA16WE 20050926001582005092600158NM 2005 9 26 SWAA052893 120050921A3350100031 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29635SW 27708 DURING SCHEDULED C3 CHECK, FOUND FWD GALLEY EMERGENCY EXIT SIGN LENS LOOSE. SECURED LENS PER MM. 2L72 4F RTA16WE 20050926001592005092600159 2005 9 26 SWAA052894 420050921A25656557463 BRACKET BOEING737 7373H4 1384600NM GIRT BAR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29635SW 27708 DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR BRACKETS LOOSE. SECURED BRACKETS PER MM. 2L72 4F RTA16WE 20050926001602005092600160NM 2005 9 26 SWAA052883 120050922A3350BR2013 LIGHT BOEING737 7373H4 1384600NM ROW 10 LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29330SW 23694 EEPLS STRIP LOOSE AT ROW 10. SECURED STRIP PER MM. 2L72 4F RTA16WE 20050926001612005092600161EA 2005 9 26 MASA200500037 120050116A2150 A/C PACK CNDAIRCL600 CL6002C10 1390015EA RIGHT SMOKE A MASAD RETURN TO BLOCK BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TXTAXI/GRND HDL 1 SW07509MJ 10094 ASH 7259 IAD-CLT, THE AIRCRAFT RETURNED TO THE GATE DUE TO LAV SMOKE ON TAXI OUT AND RIGHT PACK FAIL MESSAGE AND THE CREW SMELLED SMOKE. MAINTENANCE MEL'ED THE SYSTEM. MAINTENANCE OPS CHECKED AND THE SYSTEM CHECKED GOOD. 2L72 4F RTA21EA 20050926001632005092600163SO 2005 9 26 C2XA05SH115 120050926A491014526850401 FIREWALL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL APU BAY CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714993 145289 DURING C-CHECK THE APU FIREWALL AT FRAME 81 HAS CHAFE MARKS FROM RIVETS. MAINTENANCE REPAIRED THE APU FIREWALL AT FRAME 81 IAW EC5330-01507. THE AIRCRAFT WAS APPROVED FOR RETURNED TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20050926001642005092600164NM 2005 9 26 XN0A1267 120050921A2910 HYDRAULIC SYSTEM BOEING727 727227 1384078NM PWA JT8 JT8D9 52048NE A-SYSTEM LEAKING A XN0AO OTHER K FLUID LOSS TOTAKEOFF 1 GL23793A 20774 LOSS (A) SYS HYD ON TAKEOFF. (ORIG/OPEN) 2L73 4F4 F A3WE E2EA 20050926001672005092600167EA 2005 9 26 VNAA0509010 120050916A711122850081141 ACCESS PANEL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT NOSE COWL PUNCTURED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL05242JS3227 7911 A BELT LOADER HIT THE LT ENGINE NOSE COWL LOWER ACCESS PANEL. DAMAGE AT THE 5 O'CLOCK POSITION WAS A 6 X 2 HOLE. AFTER INSPECTION AND TEMPORARY REPAIR THE AIRCRAFT WAS FERRIED TO CKB WHERE MAINTENANCE REMOVED & REPLACED THE PANEL WITH A SERVICEABLE UNIT IAW CRJ200 AMM 71-14-01-000(400)-801. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050926001682005092600168EA 2005 9 26 VNAA0509007 120050908A29136619003 PUMP CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE HYD SYSTEM FAILED A VNAAO OTHER J WARNING INDICATION CRCRUISE 1 GL05718PS1687 10175 DURING CRUISE THE HYD 1 LO PRESS AND HYD EDP 1A CAUTION MESSAGES ILLUMINATED. THE CREW FOLLOWED THE QRH AND CONTINUED TO CLT, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP IAW CRJ700 AMM 29-11-01-400-801-A01. OPERATIONAL AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050926001702005092600170EA 2005 9 26 VNAA0509008 120050912A2750860D10018 FCU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS FAILED A VNAAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 GL05244PS2701 7912 AFTER TAKEOFF FROM DCA WITH FLAPS AT 20 DEGREES THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED. THE CREW FOLLOWED THE QRH AND DIVERTED TO PHL, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT IAW CRJ200 AMM 27-51-05-000(400)-801. OPERATIONAL TEST OF FLAP SYSTEM WAS GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050926001712005092600171NM 2005 9 26 S2YA05053 120050831A32502304000001 CONTROL VALVE DORNERDO32 DO328300 NM PWA 306 PW306B NE NLG STEERING FAILED A S2YAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL13358SK8536 1521 3188 DURING FLIGHT, THE CREW REPORTED A CAS MESSAGE INDICATING THE NOSE WHEEL STEERING (NWS) PROXY FAILED. THE CREW PERFORMED AN AIR-TURN-BACK. MAINTENANCE REPLACED NWS CONTROL VALVE, WIRING HARNESS, AND NWS ELECTRICAL CONTROL UNIT (ECU). WITH OPS CHECKS GOOD, AC WAS RETURNED TO SERVICE. (K) 2H72 4T4 FRTA55NM E35NE 20050926001742005092600174EU 2005 9 26 V2J2005F00002 120050919A32501000006635 POTENTIOMETER PIAGIOP180 P180 6960204EU PWA PT6 PT6* 52043EA NLG STEERING FAILED E V2JAO OTHER O OTHER NRNOT REPORTED 1 EA25109SL 1092 STEERING SYSTEM FAILED TO STAY ENGAGED DURING TAXI. SYSTEM WAS ABLE TO RESET BUT FAILED SEVERAL SECONDS LATER. REPEATED ATTEMPTS TO RESET THE SYSTEM HAD NO POSITIVE EFFECT. REPLACEMENT OF UNIT WAS ACCOMPLISHED IAW THE AIRFRAME AND COMPONENT MFG MM. (K) 1H72 3O3 TRTA59EU E2NE 20050926001772005092600177EU 2005 9 26 V2J2005F00003 120050919A2721EM40112 ACTUATOR PIAGIOP180 P180 6960204EU PWA PT6 PT6* 52043EA PITCH TRIM FAILED E V2JAK NONE O OTHER ININSP/MAINT 1 EA25305SL1330 1083 SYSTEM FAILED IN PRIMARY, SECONDARY SYSTEM OPERATION NORMAL TROUBELSHOT SYSTEM IAW THE MM, FOUND PROBLEM TO BE AN INTERNAL FAULT WITH THE ACTURATOR ASSEMBLY. INSTALLED AN O/H UNIT SAME PN, SN-70. SECURITY AND FUNCTION CHECKS PERFORMED WITH NO FAULTS FOUND. SYSTEM AND AIRCRAFT WERE APPROVED FOR SERVICE. (K) 1H72 3O3 TRTA59EU E2NE 20050926001802005092600180NM 2005 9 26 UIEA200500118 120050825A3210 PIN BOEING747 74747UF 1384949NM GE CF6 CF680C2* GL MLG MIGRATED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15409MC 30558 DAILY CHECK, ON WALK AROUND, FOUND LT BODY GEAR JURY STRUT UPPER ATTACHMENT PIN FOUND MIGRATED. RETENTION BOLT AND UPPER CAP STILL WITH CONDUIT. LOWER CAP AND NUT FOUND IN ADJACENT STRUCTURE. ON WALKAROUND, FOUND RT BODY GEAR JURY STRUT UPPER ATTACHMENT RETENTION BOLT NUT LOOSE. NO COTTER PIN EVIDENT. ALL OTHER DETAILS AT LOCATION INTACT. UPPER ATTACH AREA INSPECTED. PIN, CAPS AND RETENTION BOLT INSTALLED AND SAFETIED IAW MM. NUT TIGHTENED AND SAFETIED IAW MM. (K) 2L74 4F4 FRT1384945 E23EA 20050926001822005092600182EA 2005 9 26 A6WA200540299 120050906A5320453170500 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE BS 621 CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31424AW 7656 RT FS 621.0 FLOOR SUPPORT ANGLE HAS A 1 INCH CRACK. CUT OUT AND REMOVED DAMAGED ANGLE. FITTED AND DRILLED UP NEW ANGLE AND STRAP, COUNTER SUNK HOLES. TREATED ALL REPAIR PARTS. INSTALLED PARTS AND PAINTED IAW REO. (K) 2L72 4F4 FRTA21EA E15NE 20050926001862005092600186NM 2005 9 26 S2YA05040 120050704A2400230GC02703 CONTROL PANEL DORNERDO32 DO328300 NM PWA 306 PW306B NE INOPERATIVE A S2YAA UNSCHED LANDING O OTHER CRCRUISE 1 GL13354SK1 3126 DURING FLIGHT, THE CREW REPORTED THEY LOST NR 1, 2, AND 3 DISPLAY UNITS ALONG WITH THE FLIGHT DIRECTOR AND NON-ESSENTIAL BUSS 1 FAIL. THE CREW PERFORMED AN AIR-TURN-BACK. MAINTENANCE REPLACED THE 1VE PANEL AND WITH OPERATIONAL CHECKS GOOD THE AC WAS RETURNED TO SERVICE. NOTE: THIS 1VE PANEL WAS JUST REPLACED THAT DAY TO ELIMINATE AN APUAND DC POWER PROBLEM. (K) 2H72 4T4 FRTA55NM E35NE 20050926001872005092600187CE 2005 9 26 S2YA05036 120050601A3260 UPLOCK SWITCH BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA LT MLG OUT OF ADJUST A S2YAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL13891SK UE89 ON CLIMBOUT OF FLIGHT, THE CREW REPORT THE LANDING GEAR HANDLE LIGHT WAS FLICKERING WITH THE HANDLE IN THE UP POSITION. THE CREW PERFORMED AN AIR-TURN-BACK TO DEPARTURE AIRPORT. MECHANIC ADJUSTED THE LT MAIN UPLOCK SWITCH AND RETURNED THE AC TO SERVICE. (K) 2L72 4T3 TRTA24CE E2NE 20050926001882005092600188NM 2005 9 26 S2YA05037 120050614A5270 WARNING LIGHT DORNERDO32 DO328300 NM CARGO DOOR ILLUMINATED A S2YAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL13355SK 3124 SHORTLY AFTER TAKEOFF, THE CREW REPORTED THE CARGO DOOR WAS INDICATING OPEN. THE CREW CONSULTED WITH MAINTENANCE AND MADE AN AIR-TURN-BACK TO DEPARTURE. WHEN THIS BEING A RETURN PROBLEM, MAINTENANCE CHECKED THE GAP OF THE DOOR SENSORS AND REPLACED LT SIDE AFT 2 INTERIOR FLORESCENT BULBS. A MAINTENANCE FLIGHT WAS PERFORMED WITH DEFECTS NOTES AND THE AC WAS RETURNED TO SERVICE. (K) 2H72 4T RTA55NM 20050926001902005092600190EU 2005 9 26 TRBA2005054 120050821A3260DHE1148 PROXIMITY SWITCH AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE LT MLG INTERMITTENT A TRBAO OTHER N FALSE WARNING CLCLIMB 1 SO29417AT 417 WHILE IN CLIMB, LANDING GEAR DID NOT RETRACT. GEAR HANDLE DID NOT MOVE. AC RETURNED TO DEPARTURE. REPLACED PROXIMITY SWITCH NR 53GB. (K) 2H72 4T4 TRTA53EU E20NE 20050926001912005092600191NM 2005 9 26 S2YA05041 120050711A2400230GC02Y03 CONTROL PANEL DORNERDO32 DO328300 NM PWA 306 PW306B NE GENERATORS INOPERATIVE A S2YAO OTHER HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 GL13355SK978 3124 BEFORE FLIGHT CREW REPORTED A LT GENERATOR FAIL. MAINTENANCE SWAPPED THE LT AND RT GENERATORS WITH OPS CHECKS GOOD THE AC WAS RETURNED TO SERVICE. ON THE NEXT FLIGHT, THE CREW REPORTED A LT GEN FAIL. THE CREW PERFORMED AN AIR-TURN-BACK. MAINTENANCE REPLACED THE 1VE PANEL AND WITH OPERATIONAL CHECKS GOOD THE AC WAS RETURNED TO SERVICE. (K) 2H72 4T4 FRTA55NM E35NE 20050926001942005092600194CE 2005 9 26 UG82005F00007 120050824A293042RT1003 SENSOR CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL LT HYD SYSTEM INTERMITTENT E UG8AO OTHER O OTHER NRNOT REPORTED 1 GL235113S 7500013 HYDRAULIC SYSTEM, A TEMPERATURE FLUCTUATED BETWEEN 80-130 DEGREES C WITH SMALL VARIATION IN PRESSURE. UNLOADED A HYDRAULIC SYSTEM AND TEMPERATURE DECREASED TO 90 DEGREES C BUT CLIMBED TO 119 DEGREES AT SHUTDOWN ON THE RAMP. REPLACED DEFECTIVE TEMPERATURE SENSOR FOR A HYDRAULIC SYSTEM. LT HYDRAULIC SYSTEM OPERATION AND INDICATION NORMAL IAW MM. AIRCRAFT RETURNED TO SERVICE. (K) 2L72 4J4 FRTT00007WITE6CH 20050926001982005092600198SW 2005 9 26 ALG2005F00066 120050821A6321DO1521 BOLT BELL 206 206L4 1182110SW ALLSN 250C 250C30P 03013GL ROTOR BRAKE DEFECTIVE E ALGAK NONE O OTHER ININSP/MAINT 1 SW03265AL 52280 DURING MAINTENANCE SERVICE CHECK, THE LT ROTOR BRAKE CALIPER WAS FOUND TO BE DEFECTIVE. THE FOLLOWING ITEMS WERE REMOVED AND REPLACED WITH SERVICEABLE COMPONENTS: ROTOR BRAKE DISK, BOLTS AND 2 ROTOR BRAKE CALIPERS. IAW MM. (K) 1G71 3U3 UNCH2SW E1GL 20050926002002005092600200SW 2005 9 26 ALG2005F00069 120050813A7712407375003107 INDICATOR BELL 407 407 1182206SW ALLSN 250C 250C47B GL TORQUE FAILED E ALGAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW03617AL 53265 ON CLIMB OUT FROM BASE, TORQUE GUAGE DROPPED TO 2 PERCENT. MAINTENANCE NOTIFIED. REMOVED AND REPLACED ENGINE TORQUE INDICATOR. C/W LEAK CHECK AND GROUND RUN, NOT DEFECTS NOTED. ALL WORK IAW MM. (K) 1G71 3U3 UO H2SW E1GL 20050926002032005092600203NM 2005 9 26 UIEA200500119 120050825A2450 WIRE HARNESS BOEING747 747271C 1384869NM GE CF6 CF650E2 30018NE ELECTRICAL BUSS SHORTED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15537MC 22403 DAILY CHECK, IB PICKUP ITEM BY MAINTENANCE. UNABLE TO POWER CGO HANDLING BUSSES. REMOVED AND REPLACED BPCU NR 1 AND NR 2. ALSO, FOUND WIRE HARNESS W124, 12 WIRES SHORTED OUT. REPAIRED IAW SWPM ACCOMPLISHED, CARGO HANDLING SYSTEM CHECKS NORMAL. (K) 2L74 4F4 F A20WE E23EA 20050927000012005092700001CE 2005 9 27 TAMFAKE111 120050912A321012345 LANDING GEAR BEECH 18 E18S 1151006CE INOPERATIVE W TAMFK NONE O OTHER ININSP/MAINT 1 SO23700W 111 111 BA54 TEST TEST TEST TEST TEST TEST TEST TEST 1L72 3R A765 20050927000042005092700004EA 2005 9 27 ASOA05703 120050821A5210 STEP CNDAIRCL600 CL6002C10 1390015EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11755EV 10185 DURING AN A-CHECK IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR IAW CRJ700 MM 52-00. OPERATIONAL CHECKS GOOD. (M) 2L72 4F RTA21EA 20050927000122005092700012EA 2005 9 27 ASOA05689 120050820A5330 FINGER DOUBLER CNDAIRCL600 CL6002B19 1900309EA BS 449 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11839AS 7284 DURING A C-CHECK IN MCN, THE FINGER DOUBLERS AT FS 449, LBL 44 AND RBL 44 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO BOMBARDIER FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. (M) S/D - MAINTENANCE REMOVED THE CORROSION FROM THE FINGER DOUBLERS AT FS 449, LBL 44 AND RBL 44 BY COMPLYING WTH ASA EO 600-53-0314. (M) 2L72 4F RTA21EA 20050927000142005092700014SO 2005 9 27 SIMA200521605 120050727A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO FS 25 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21813AE 145539 THE LEFT OMEGA BEAM AT FRAME 25 WAS FOUND TO BE CORRODED. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 29, CHAPTER 53-00-10. (M) 2L72 4F RTT00011AT 20050927000202005092700020SO 2005 9 27 SIMA200521612 120050726A531014521713003 BEAM EMB 135 EMB135KL 3260302SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21813AE 145539 THE GALLEY CENTER BEAM WAS FOUND TO BE CORRODED UNDER THE FLOOR RAMP. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED EXTERNAL DOUBLER. REPAIR DONE IAW EMB SRM, SRM EMB145/1142 REV 29, CHAPTER 53-21-10 FIG 202 SHEET 2. (M) 2L72 4F RTT00011AT 20050927000262005092700026EA 2005 9 27 ASO2005F00009 120050820A5330 FINGER DOUBLER CNDAIRCL600 CL6002B19 1900309EA BS 484 CORRODED E ASOAK NONE O OTHER ININSP/MAINT 1 WP19839AS 7284 DURING A C-CHECK IN MCN, THE FINGER DOUBLERS AT FS 484, LBL 44 AND RBL 44 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO BOMBARDIER FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. (M) 2L72 4F RTA21EA 20050927000292005092700029SO 2005 9 27 SIMA200522703 120050814A2760 WARNING LIGHT EMB 145 EMB145LR 3260212SO SPOILERS ILLUMINATED A SIMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW21649PP 145234 SPOILER FAIL MESSAGE ON EICAS DURING TAKEOFF ROLL. FOLLOWED FIM TASK 27-63-00-810-802 SYSTEM OPS CHECK GOOD AS PER AMM 27-63-01. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20050927000302005092700030NM 2005 9 27 C7WA200500115 120050820A2697 WIRE BOEING727 7272M7 138407SNM FIRE LOOP SHORTED A C7WAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 SO17742RW 21952 AIR TURNBACK, NR 3 ENGINE FIRE DETECTOR INOPERATIVE LIGHT ILLUMINATED AND NR 3 ENGINE FIRE WARNING LIGHT AND BELL WENT OFF REPEATEDLY 7 TIMES. FOUND NR 3 ENGINE B-LOOP WIRE SHORTED. REPAIRED WIRE PER B727 MM 20-00-00. OPS CHECKS GOOD PER 26-11-01. (M) 2L73 4F A3WE 20050927000312005092700031SO 2005 9 27 SIMA200524102 120050826A3244302K622 TIRE EMB 145 EMB145LR 3260212SO MLG FAILED A SIMAA UNSCHED LANDING A FLAME/FIRE CLCLIMB 1 SW21690AE 14500858 BLOWN TIRE ON TAKEOFF. RETURN TO ORD DID NOT LAND OVERWEIGHT. REPLACED NR 2 MAIN LANDING GEAR WHEEL ASSEMBLY. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20050927000332005092700033SO 2005 9 27 SIMA200525201 120050828A534713500439007 SEAT TRACK EMB 135 EMB135KL 3260302SO CABIN CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21817AE 145554 SAW - DURING CPCP INSPECTION, FOUND LEFT FORWARD SEAT TRACK CORRODED AROUND SCREW HOLES. REPLACED SEAT TRACK IAW EMB AMM 53-01-06-400-801-A. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050927000362005092700036SO 2005 9 27 SIMA200525202 120050828A534714532606017 SEAT TRACK EMB 135 EMB135KL 3260302SO CABIN CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21817AE 145554 SAW - DURING CPCP INSPECTION, FOUND LEFT UPPER 5TH FROM FRONT SEAT TRACK CORRODED. REPLACED SEAT TRACK IAW AMM 53-01-06-400-801A. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050927000412005092700041EU 2005 9 27 KBM2005F00246 120050822A6220117775P BALL JOINT SNIAS 350 AS350BA 8680817EU STARFLEX WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P 2347 UNITS ARE WORN. REMOVED AND REPLACED BALL JOINT. (M) 1G71 3U NCH9EU 20050927000422005092700042EU 2005 9 27 KBM2005F00250 120050818A2121050143 MOTOR SNIAS 350 AS350B1 8680811EU BLOWER INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19215LA 2143 A/C NOT BLOWING COLD AIR, MOTOR INOPERATIVE. REMOVED AND REPLACED MOTOR. (M) 1G71 3U H9EU 20050927000432005092700043EU 2005 9 27 KBM2005F00251 120050815A7931704A37642043 TRANSMITTER SNIAS 350 AS350B1 8680811EU OIL PRESSURE INOPERATIVE E KBMAO OTHER P NO WARNING INDICATION NRNOT REPORTED 1 WP1953SH 2009 UNIT SHOWS NO INDICATION OF PRESSURE. REMOVED AND REPLACED ENG OIL TRANSMITTER. (M) 1G71 3U H9EU 20050927000462005092700046EA 2005 9 27 ASOA05730 120050830A5320 SILL CNDAIRCL600 CL6002B19 1900309EA BS 529 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11834AS 7254 DURING A C-CHECK IN MCN, THE LEFT SIDE PRESSURE FLOOR SILL STRUCTURE AT FS 529 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO BOMBARDIER FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. (M) 2L72 4F RTA21EA 20050927000482005092700048SO 2005 9 27 SIMA200525204 120050828A534714532605017 SEAT TRACK EMB 135 EMB135KL 3260302SO CABIN CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21817AE 145554 SAW - DURING CPCP INSPECTION, FOUND RIGHT UPPER 4TH FROM FRONT SEAT TRACK CORRODED. REPLACED SEAT TRACK IAW EMB AMM 53-01-06-400-801-A. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050927000502005092700050SO 2005 9 27 SIMA200523506 120050816A532014521721009 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21711PH11821 145235 THE GALLEY FORWARD DIGITAL WAS FOUND TO BE CORRODED. REMOVED THE CORROSION BY MAKING A CUTOUT. FABRICATED A FILLER AND DOUBLER. REPAIR DONE IAW EMB REPAIR STATEMENT IC2005-145/4287 DATED AUGUST 11,2005. (M) 2L72 4F RTT00011AT 20050927000522005092700052EA 2005 9 27 ASOA05718 120050810A5712 RIB CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11853AS 7374 DURING A C-CHECK IN HOT, THE LEFT BATT RIB ASSY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LEFT BATT RIB ASSY AT WS 53.60 IAW ASA EO 600-57-039A. (M) 2L72 4F RTA21EA 20050927000532005092700053EA 2005 9 27 ASOA05715 120050823A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN MALFUNCTIONED A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11673BR 7599 DURING AN A-CHECK IN BTR, THE CENTER IN BTR, THE CENTER SECTION OF EMERGENCY FLOOR TRACK LIGHTING WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERFORMED A FUNCTIONAL TEST ON THE EMERGENCY FLOOR TRACK LIGHTING WITH NO DEFECTS FOUND. OPS CHECK GOOD. (M) 2L72 4F RTA21EA 20050927000572005092700057EA 2005 9 27 ASOA05736 120050831A7830 THRUST REVERSER CNDAIRCL600 CL6002B19 1900309EA LEFT MALFUNCTIONED A ASOAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO11853AS 7474 FLT 4802 - DURING CRUISE FROM CVG-IAH, AT APPROXIMATELY 24,000 FEET, THE CREW RECEIVED A L REV UNLOCKED AMBER MESSAGE ALONG WITH AN ASSOCIATED REV AMBER ICON ON THE L N1 GAUGE AND THE LEFT EMER STOW SWITCH LIGHT ILLUMINATED. THE LEFT THRUST REVERSER HAD AUTOMATICALLY RETARDED AND THE CREW REDUCED THE RIGHT ENGINE TO IDLE IN COMPLIANCE WITH THE QRH FOR THE REMAINDER OF THE FLIGHT. AN EMERGENCY WAS DECLARED. WHEN DESCENDING AT APPROXIMATELY 8,000 FEET ALL ELECTRONIC INDICATIONS EXTINGUISHED. THE AIRCRAFT LANDED SAFELY IN IAH. MAINTENANCE PERFORMED GROUND POWER RUN-UPS WITH THE CREW WITH NO DEFECTS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050927000582005092700058EA 2005 9 27 ASOA05739 120050904A3697 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA ENGINE LOOSE A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11879AS 7600 DURING CLIMB-OUT FROM ATL-PHF, THE CREW RECEIVED A LT 14TH STAGE DUCT OVERHEAT WARNING MESSAGE. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED TO ATL AND LANDED SAFELY. MAINTENANCE FOUND A LOOSE CONNECTION ON THE LEFT 14TH STAGE BLEED AIR DUCT LOOP AND TIGHTENED THE LOOSE TERMINAL. MAINTENANCE RAN THE ENGINE AT MAX POWER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050927000602005092700060SO 2005 9 27 SIMA200521606 120050724A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO FS 27 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21813AE 145539 THE LEFT OMEGA BEAM AT FRAME 27 WAS FOUND CORRODED. PERFORMED A CUTOUT OF THE OMEGA BEAM TO REMOVED THE CORROSION. FABRICATED AN EXTERNAL, DOUBLER, AND FILLER AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB145/1142 REV 29, CHAPTER 53-00-10, FIG 202. (M) 2L72 4F RTT00011AT 20050927000622005092700062EA 2005 9 27 ASOA05702 120050821A5210601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11867AS 7463 FLT 4741 - DURING A GROUND INSPECTION IN ABE, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR IAW CRJ200 AMM 52-11-04. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050927000642005092700064EA 2005 9 27 ASOA05704 120050822A5210 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11827AS 7212 DURING AN A-CHECK IN BTR, THE TOP STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE TOP STEP ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20050927000652005092700065SO 2005 9 27 SIMA200521615 120050803A5330 SKIN EMB 135 EMB135KL 3260302SO FR 11 DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21856AE 145748 THE FUSELAGE SKIN JUST AFT OF FRAME 11 AND BETWEEN STRINGERS 20L AND 21L WAS FOUND TO BE DENTED. REMOVED THE DAMAGED SKIN BY MAKING A CUT OUT. FABRICATED A REPAIR DOUBLER AND FILLER. REPAIR DONE IAW EMB SRM, SRM 145 1142 REV 30, CHAPTERS 53-10-01. (M) 2L72 4F RTT00011AT 20050927000662005092700066SO 2005 9 27 SIMA200522005 120050801A532014000491017 GUSSET EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21816AE 145552 DURING IMBV INSPECTION, FOUND CENTER HAT BEAM GUSSET CORRODED ON TOP. REMOVED AND INSTALLED NEW HAT BEAM GUSSET IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050927000682005092700068 2005 9 27 SIMA200522007 420050804A2210 WIRE EMB 145 EMB145 3260210SO AUTOPILOT FAILED A SIMAO OTHER F FLT CONT AFFECTED LDLANDING 1 SW21612AE 145079 AMA - FLT 3779 - ON LANDING, CREW RECEIVED DUAL PITCH TRIM FAILURE 50 FT ABOVE GROUND. FOUND NR 2 AUTOPILOT DISCONNECT TRIM SWITCH WIRING CAUSED SWITCH TO BIND. REPOSITIONED WIRES AND SWITCH OPERATES CORRECTLY. ALL OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050927000712005092700071SO 2005 9 27 SIMA200521602 120050727A532014522178005 SILL EMB 135 EMB135KL 3260302SO SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21813AE 145539 THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. BLENDED THE SERVICE DOOR SILL TO REMOVE THE CORROSION. FABRICATED A DOUBLER. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 29, CHAPTER 53-21-02 FIG 201 AND 203. (M) 2L72 4F RTT00011AT 20050927000772005092700077CE 2005 9 27 GUU2005F00045 120050811A2797MS53476W2039SW CONNECTOR BEECH 1900 1900D 1154162CE ELEVATOR TRIM LOOSE A GUUAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SO29231YV UE231 FLT - 9292 - JAX/TPA - AFTER TAKEOFF, WHILE ADJUSTING THE ELEVATOR TRIM FROM CLIMB TO LEVEL FLIGHT, THE YOKE WAS PULLED AWAY FROM THE FIRST OFFICERS HANDS. IT WAS IF THE TRIMMING CABLE SNAPPED INTO A NEW POSITION. DETERMINED BACK SHELL WIRE BUNDLE CLAMP EAR FOR THE GPWS ELECTRICAL CONNECTOR J726/P371, BELOW TCAS INDICATOR, WAS MOMENTARILY CAUGHT INSIDE THE CONTROL COLUMN ASSEMBLY VERTICAL TUBE. SECURED CONNECTOR J726/P371 OUT OF THE WAY. VERIFIED SUFFICIENT CLEARANCE OF CONTROL COLUMN THROUGH OUT FULL TRAVEL SWEEPS. (M) 2L72 4T RTA24CE 20050927000792005092700079SO 2005 9 27 SIMA2005232403 120050816A532014521721009 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO FR 14 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21715AE 145262 SAW - FOUND DURING CPCP INSPECTION, DIGITAL CORRODED AT FRAME 14 COCKPIT ENTRY. REMOVED CORROSION AND FOUND DIGITAL TO BE CRACKED. REPLACED DIGITAL IAW SRM 51-21-10. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050927000802005092700080SO 2005 9 27 SIMA200523503 120050812A532014525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO FS 25 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21710TB11880 145224 THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 25. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED A DOUBLER, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 30, CHAPTER 53-00-10. (M) 2L72 4F RTT00011AT 20050927000812005092700081SO 2005 9 27 SIMA200523405 120050816A55401209421249 ROD EMB 135 EMB135LR 3260305SO RUDDER DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21715AE 145262 FOUND DURING MBV, FORWARD END OF LOWER NR 2 RUDDER ROD HAS PLAY WHERE FORWARD FITTING SCREWS INTO ROD. REPLACED LOWER NR 2 RUDDER ROD IAW EMB AMM 27-21-08. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050927000822005092700082EA 2005 9 27 ASOA05698 120050818A5210 DOOR FRAME CNDAIRCL600 CL6002B19 1900309EA BS 320-338 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11839AS 7284 DURING A C-CHECK IN MCN, THE PASSENGER DOOR AFT OUTBOARD FRAME MEMBER LOWER END AT FS 320.10 AND FS 338 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE PASSENGER DOOR AFT OUTBOARD FRAME MEMBER LOWER END AT FS 320.10 AND FS 338 IAW BOMBARDIER REO NR 601R-52-11-402. (M) 2L72 4F RTA21EA 20050927000862005092700086SO 2005 9 27 SIMA200521607 120050721A532014525380003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO FS 27 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21813AE8307 145539 ABI - THE CENTER OMEGA BEAM AT FRAME 27 WAS FOUND CORRODED. PERFORMED A CUT OUT OF BEAM TO REMOVE THE CORROSION. FABRICATED AN EXTERNAL DOUBLER, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB145/1142 REV 29, CHAPTER 53-00-10, FIG 203. (M) 2L72 4F RTT00011AT 20050927000872005092700087SO 2005 9 27 SIMA200524110 120050823A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO FS 25 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21858AE 145754 THE CENTER OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE CENTER OMEGA BEAM TO REMOVED THE DAMAGE. FABRICATED A FILLER, EXTERNAL, ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 30, CHAPTER 53-00-10 FIG 203. (M) 2L72 4F RTT00011AT 20050927000902005092700090SO 2005 9 27 SIMA200525212 120050829A532014521700007 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO FR 20 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21817AE 145554 SAW - DURING CPCP INSPECTION, FOUND LEFT OMEGA BEAM CORRODED AT FRAME 20. INSTALLED DOUBLER IAW SRM 53-00-10. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050927000912005092700091SO 2005 9 27 SIMA200525216 120050829A321314521680003 HOUSING EMB 135 EMB135KL 3260302SO NLG CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21817AE 145554 DURING MBV INSPECTION, FOUND NOSE LANDING GEAR LEFT MAIN STRUT BEARING HOUSING SHOWS SIGNS OF PITTING. REWORKED BEARING HOUSING TO WITHIN LIMITS IAW SRM 53-11-08 PAGE 101. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050927000962005092700096SO 2005 9 27 SIMA200525217 120050829A321014524475001 CAP EMB 135 EMB135KL 3260302SO BEARING CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21817AE 145554 DURING MBV INSPECTION, FOUND NOSE LANDING GEAR RIGHT DRAG BRACE BEARING CAP HAS SIGNS OF PITTING. REMOVED NEGLIGIBLE PITTING FROM BEARING CAP FOUND TO BE IN LIMITS IAW SRM 53-11-08 PAGE 101. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050927000972005092700097SW 2005 9 27 KBM2005F00236 120050814A28407G547 SWITCH BELL 206 206B 1181511SW FUEL SYSTEM INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19188TV 2704 SWITCH INOPERATIVE, DOES NOT ACTIVATE WARNING LIGHT. REMOVED AND REPLACED SWITCH. (M) 1G71 3U H2SW 20050927000992005092700099EA 2005 9 27 A6WA200540301 120050905A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA BS 621-625.3 CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31424AW 7656 LT FS 621-625.3 INTERCOSTAL AT STRINGER 14L IS CRACKED NEAR RADIUS APPROX 1 INCH LONG. (M) 2L72 4F RTA21EA 20050927001002005092700100SO 2005 9 27 SIMA200523510 120050822A33102LA00626500 LIGHT EMB 145 EMB145LR 3260212SO COCKPIT MAP BURNED A SIMAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW21682AE 14500826 CAPTAINS MAP LIGHT SMOKES AFTER A FEW MINUTES OF OPERATION AT FULL INTENSITY. REPLACED MAP LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. A/C RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20050927001012005092700101EU 2005 9 27 KBM2005F00237 120050813A21500500521 MOTOR SNIAS 350 AS350B2 8680813EU EVAPORATOR INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH 2957 EVAP MOTOR INOPERATIVE. REMOVED AND REPLACED EVAP MOTOR. (M) 1G71 3U H9EU 20050927001022005092700102EU 2005 9 27 KBM2005F00239 120050902A2110060018 BELT SNIAS 350 AS350B2 8680813EU COMPRESSOR BROKEN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH 2884 AC BELT BROKEN DUE TO FAULTY PSI SWITCH, REPLACED WITH NEW. (M) 1G71 3U H9EU 20050927001082005092700108SO 2005 9 27 SIMA200521604 120050724A531112010732001 FRAME EMB 135 EMB135KL 3260302SO FS 81 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21813AE8307 145539 ABI - FRAME 81 WAS FOUND GOUGED AT THE 6 O`CLOCK POSITION. 2L72 4F RTT00011AT 20050927001112005092700111EA 2005 9 27 ASOA05667 120050815A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A ASOAO OTHER J WARNING INDICATION APAPPROACH 1 SO11855AS 7395 FLT 4386 - DURING APPROACH INTO CVG FROM MHT, THE CREW RECEIVED A FLAPS FAIL MESSAGE WITH THE FLAPS SELECTED TO EIGHT DEGREES. EMERGENCY VEHICLES WERE REQUESTED TO BE ON STANDBY AS A PRECAUTION. THE AIRCRAFT LANDED SAFELY IN CVG. MAINTENANCE REMOVED AND REPLACED THE LEFT BRAKE POSITION SENSOR UNIT (BPSU) AND THE FLAPS POWER DRIVE UNIT (PDU). OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050927001142005092700114EA 2005 9 27 ASOA05672 120050819A33974871907191 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT LOOSE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11876AS 7576 DURING OVERNIGHT MAINTENANCE IN SHV, THE FORWARD EMERGENCY FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE RESEATED THE CONNECTORS TO THE FORWARD EMERGENCY FLOOR LIGHTS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050927001192005092700119EA 2005 9 27 ASOA05674 120050819A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11839AS 7284 DURING A C-CHECK IN MCN, THE FS 280 FRAME AT LBL 10 AND RBL 10 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FS 280 FRAME AT LBL 10 AND RBL 10 IAW ASA EO 600-53-0309. (M) 2L72 4F RTA21EA 20050927001222005092700122EA 2005 9 27 ASOA05670 120050817A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11839AS 7284 DURING A C-CHECK IN MCN, THE ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW ASA EO 600-53-0072B. (M) 2L72 4F RTA21EA 20050927001252005092700125EA 2005 9 27 ASOA05716 120050823A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO113350 7503 FLT 4155 - DURING A GROUND INSPECTION IN ATL, THE CABIN FLOOR WAS FOUND WATER SOAKED WITH OVER HALF OF THE EMERGENCY FLOOR LIGHTING FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FIRST FOUR EMERGENCY FLOOR LIGHT STRIPS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050927001272005092700127EU 2005 9 27 ASOA05710 120050729A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU FR 36-39 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11636AS 375 DURING A C-CHECK IN YUL, THE SEAT TRACKS BETWEEN FRAME 36 TO FRAME 39 LEFT/RIGHT WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS BETWEEN FRAME 36 TO FRAME 39 LEFT/RIGHT IAW ATR72 SRM 51-21-42 AND 51-25-04. (M) 2H72 4T RTA53EU 20050927001292005092700129EA 2005 9 27 ASOA05665 120050815A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11916EV 7757 FLT 4152 - DURING A GROUND INSPECTION IN ATL, THE RIGHT MIDDLE EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE RIGHT MIDDLE EXTERIOR EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050927001302005092700130EU 2005 9 27 ASOA05709 120050728A5320 FLOOR SUPPORT AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11636AS 375 DURING A C-CHECK IN YUL, THE Z-FLOOR SUPPORTS AT FRAME 39, STRINGER 14 LEFT AND FRAME 39 TO FRAME 41 RIGHT WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE Z-FLOOR SUPPORTS AT FRAME 39, STRINGER 14 LEFT AND FRAME 39 TO FRAME 41 RIGHT IAW ATR-72 SRM 51-21-42, 51-25-01 AND 51-25-03. (M) 2H72 4T RTA53EU 20050928000032005092800003SO 2005 9 28 SIMA200525704 120050913A28202770138101 VALVE EMB 145 EMB145LR 3260212SO RT WING FLAPPER BROKEN A SIMAB EMER. DESCENT KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW21618AE 145097 FUEL STREAMING FROM RIGHT WING. REPLACED RIGHT FUEL TANK OUTBOARD FLAPPER VALVE IAW 28-11-04. PERFORMED A FUNCTIONAL CHECK FLIGHT WITH NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20050928000042005092800004SO 2005 9 28 SIMA200525504 120050906A335082321 SIGN EMB 145 EMB145LR 3260212SO EMERGENCY EXIT FAILED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21655AE 145452 MSN - FLT 4242 - OVERWING EMERGENCY EXIT LOCATION SIGN FAILS TO ILLUMINATE. REPLACED THE CEILING EMERGENCY EXIT LOCATION SIGN IAW EMB 145 AMM 33-5-15. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20050922000732005092200073NM 2005 9 22 USAA051102 120050920A5311 FRAME BOEING737 737401 1384701NM BS 312 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19418US 23985 FOUND CRACK AFT E/E FRAME 312. FABRICATED AND INSTALLED NEW STRAPS IAW SRM 53-10-51, DEFECT SIZE: 1" LONG CRACKS. 2L72 4F RTA16WE 20050922000832005092200083EA 2005 9 22 MASA200500688 120050831A2410 IDG CNDAIRCL600 CL6002B19 1900309EA NR 2 MALFUNCTIONED A MASAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SW07154SF 7154 ASH 2730 BGM. ABORTED TAKEOFF. NR 2 IDG FAILED ON TAKEOFF ROLL. OPS CHECKED GOOD. 2L72 4F RTA21EA 20050922000922005092200092EU 2005 9 22 AWXA200501069 120050904A5315D53472094000 FLOORBEAM AIRBUS320 A320231 3930325EU CABIN CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28634AW 091 DURING C4 CHECK, DISCOVERED EXFOLIATION CORROSION LOCATED ON FLOORBEAM FROM FR 64 TO FR 70, Y512. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-14. REMOVED FLOORBEAM FROM FR 64 TO FR 70, Y512 IAW AIRBUS 320 SRM 51-72-11. INSTALLED NEW FLOORBEAM FROM FR 64 TO FR 70, Y512 IAW AIRBUS 320 SRM 51-72-11. 2L72 4F RTA28NM 20050922000982005092200098CE 2005 9 22 09122005D 120050910A2810 FUEL TANK BEECH 1900 1900D 1154162CE LEAKING A NSVAO OTHER K FLUID LOSS TXTAXI/GRND HDL 1 EA27220CJ UE20 FUEL LEAKING FROM LT WHEEL WELL. WAITING FOR FUEL REPAIR SPECIALIST AND TOOLS. 2L72 4T RTA24CE 20050922000992005092200099NE 2005 9 22 09122005G 220050911A7200 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LEFT OVERTEMP A NSVAC ABORTED TAKEOFF MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 EA27301CE 191 LT ENGINE EXCEEDED ITT ON TAKEOFF (931 FOR 30 SECS. PERFORMED CAPPED AND UNCAPPED RUNS. ENGINE PERFORMANCE WITHIN LIMITS PER GE MANUAL. 2L72 4T4 TRTA52EU E8NE 20050922001032005092200103EU 2005 9 22 09162005A 120050915A8011M832481210 O-RING SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE STARTER LEAKING A NSVAD RETURN TO BLOCK KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA27301CE 191 LEFT ENG SMOKING FROM NACELLE. REMOVED AND REPLACED STARTER SHAFT O-RING. NO LEAKS NOTED. 2L72 4T4 TRTA52EU E8NE 20050922001092005092200109SO 2005 9 22 RAIA00509027 120050917A3397 CONNECTOR EMB 145 EMB145 3260210SO EMERGENCY LIGHT LOOSE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03802HK 145066 FLT 3546 - RIC - CEILING OVERWING EMERGENCY LIGHT OUT. MAINTENANCE RECONNECTED LOOSE CONNECTOR ON CEILING OVERWING EMERGENCY LIGHT. 2L72 4F RTT00011AT 20050922001202005092200120NM 2005 9 22 SWAA052867 120050920A53306545890 SKIN BOEING737 7373L9 1384470NM BS 344 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 344, STR 18L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050922001212005092200121NM 2005 9 22 05FDEA02989 120050918A5744 ATTACH FITTING DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 LT WING, O/B FLAP I/B HINGE (WING SIDE), LWR ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. REPAIR CARRIED OUT AS PER CMM 57-44-08 AND FOUND WITHIN LIMIT AS PER DAC DWG ARC 0502. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2L73 4F RTA22WE 20050923000082005092300008EU 2005 9 23 AWXA200501078 120050904A5320D5348004320 SILL AIRBUS320 A320231 3930325EU CABIN CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28634AW 091 DURING C04 CHECK DISCOVERED CORROSION AROUND NUT PLATE HOLES ON LOWER SILL BEAM AT FR 68 AND Y1732. MAINTENANCE REMOVED CORROSION ON LOWER SILL BEAM AND FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-41-14 FIG 101. REMOVED DAMAGED SILL BEAM AT FR 68, Y1732 IAW AIRBUS 320 SRM 53-11-14 FIG 201. FABRICATED REPLACEMENT ANGLE IAW AIRBUS 320 SRM 53-41-14 FIG 201. INSTALLED FABRICATED REPAIR PARTS IAW AIRBUS SRM 53-42-11. 2L72 4F RTA28NM 20050923000152005092300015EU 2005 9 23 AWXA200501085 120050903A5347D53371112000 SEAT TRACK AIRBUS320 A320231 3930325EU FR 36-41 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28634AW 091 DURING C4 CHECK DISCOVERED EXFOLIATION CORROSION ON RT OUTBOARD SEAT TRACK AT FS 40+15", Y-1292. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 101. MAINTENANCE REMOVED SEAT TRACK FROM FS 36 TO FS 41, Y-1292 IAW AIRBUS 320 SRM 51-42-11. RECEIVED NEW SEAT TRACK AND INSTALLED FROM FS 36 TO FS 41 Y-1292 IAW AIRBUS 320 SRM 51-42-11 AND 51-72-11. 2L72 4F RTA28NM 20050923000162005092300016 2005 9 23 UPS05245464 420050918A2565D31075101 SLIDE BOEING727 72731C 1384011NM L1 DOOR INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 INSPECTION TYPE:N/A L-1 DOOR SLIDE INOP. REMOVED AND REPLACED SLIDE ASSY PER 25-60-14, THIS CLEARS M310071. 2L73 4F A3WE 20050923000182005092300018NM 2005 9 23 UPS05245466 120050830A5754 RIB BOEING727 72731C 1384011NM NR 8 SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01922UP 19231 INSPECTION TYPE:C-CRACK ON NR 8 SLAT O/B RIB AT I/B TRACK ATTACHMENT AREA. SLAT STOP DRILLED IAW AAAE EO 2005-081-004 REV 1 (UPS ENG FILE NR 727- 57-20133). 2L73 4F A3WE 20050923000262005092300026WP 2005 9 23 UPS05845476 120050909A5330561386215N1 SKIN DOUG DC8 DC871F 302199DWP FS 21.92-70 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 INSPECTION TYPE:SP REMOVE AND REPLACE LOWER FWD SKIN STA -21.92 TO STA 70 L31L- L31R. REMOVED AND REPLACED LWR FWD SKIN STA -21.92 TO STA 70 L31L-L31R IAW EO DC8-5330-8942-D. 2L74 4F RT4A25 20050923000442005092300044EU 2005 9 23 09212005A 120050919A2622BA51015GR3 FIRE BOTTLE SAAB SF340 340B 7860101EU COCKPIT LOW A NSVAO OTHER O OTHER TXTAXI/GRND HDL 1 EA27344CJ 344 COCKPIT FIRE EXTINGUISHER PRESSURE IS INDICATING LOW. REMOVED AND REPLACED COCKPIT FIRE EXTINGUISHER. 2L72 4T RTA52EU 20050923000472005092300047NE 2005 9 23 09212005F 220050920A7320 HMU SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LT ENGINE MALFUNCTIONED A NSVAO OTHER O OTHER TXTAXI/GRND HDL 1 EA27321CJ 321 LEFT ENGINE WILL NOT SHUT DOWN, HAD TO PULL T-HANDLE TO SHUT DOWN. RIGGED CONDITION LEVER INPUT TO HMU GEAR BOX AND THE PCU. 2L72 4T4 TRTA52EU E8NE 20050923000482005092300048CE 2005 9 23 09212005C 120050919A7500E305WDM SWITCH BEECH 1900 1900D 1154162CE BLEED AIR FAILED A NSVAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA2760MJ UE60 DUAL ENVIROMENTAL FAIL. T/O ABORTED AT 50 KNOTS. PERFORMED OPS CHECK OF RIGHT TEST VALVE OPS CHECKED GOOD. CLEANED LEFT PNEUMATIC BLEED TEST SWITCH E305WDM, OPS CHECK GOOD. 2L72 4T RTA24CE 20050923000632005092300063NM 2005 9 23 PIDA20050108 120050913A5320 INTERCOSTAL BOEING737 7373G7 1384595NM BS 790 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05370WL 24011 CORROSION ON TRIANGLE STRAP ON STR 25 LT INTERCOSTAL AT BS 790. REPLACED STRAP AT STR 25 LT AT BS 790 PER SRM 51-10-2. 2L72 4F RTA16WE 20050923000882005092300088NM 2005 9 23 05FDEA03011 120050920A5315 FLOORBEAM BOEING727 727233 138408ANM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25286FE 22623 FLOORBEAM STA 344 HAS CORROSION AT LBL10-RBL16 (PREVIOUS SPLICE AT LBL10). REMOVED DAMAGED AREA PER FE SR27-53-007 FIG 11. FABRICATED AND INSTALLED NEW UPPER CAP BEAM REPAIR IAW FX SR27-53-007 FIG 11. ALLODINED AND PRIMED IAW FX B727 SRM 51-10-02. 2L73 4F RTA3WE 20050923000902005092300090NM 2005 9 23 05FDEA03012 120050920A5315 FLOORBEAM BOEING727 727233 138408ANM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25286FE 22623 FLOORBEAM STA 322 CORRODED AT BL0TO LBL45. REMOVED DAMAGED AREA, FABRICATED REPAIR AND INSTALLED IAW FXB727 SRM 53-10-8 FIG 9. ALODINED AND PRIMED PARTS IAW FX B727 SRM 51-10-2. 2L73 4F RTA3WE 20050923000922005092300092EA 2005 9 23 COMA0560508 120050918A2750865D1007 PDU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAULTY A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01814CA27087 7387 FLIGHT 5638 - DURING JFK APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE AT 40 DEGREE FLAP POSITION SETTING. REPLACED THE POWER DRIVE UNIT. 2L72 4F RTA21EA 20050923000982005092300098NM 2005 9 23 05FDEA03025 120050921A5753 FITTING DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 LEFT WING, OUTBOARD FLAP INBOARD AFT HINGE FITTING FORWARD MOUNT OUTBOARD AFT HOLE (FLAP SIDE) CORRODED. REMOVED AND REPLACED AS PER AMM 27- 50-30-4. ADJUSTMENT AND OPERATION TEST CARRIED OUT FOUND SATISFACTORY AS PER AMM 27-50-00. 2L73 4F RTA22WE 20050923001002005092300100NM 2005 9 23 05FDEA03027 120050921A5311 FRAME BOEING727 727232 1384082NM BS 1070 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 FRAME DENTED AT BS 1070, JUST BELOW STR 25R. REPAIRED FRAME AT B.S. 1070, STR 25R PER SRM 51-40-3. 2L73 4F A3WE 20050923001022005092300102NM 2005 9 23 05FDEA03029 120050921A5311 FRAME BOEING727 727232 1384082NM BS 1130 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 FRAME DENTED AT BS 1130, STR 26L. REPAIRED FRAME AT BS 1130 STR. 26L PER SRM 51-40-3. 2L73 4F A3WE 20050923001042005092300104NM 2005 9 23 05FDEA03031 120050921A5311 FRAME BOEING727 727232 1384082NM BS 1050 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 FRAME DENTED AT BS 1050, BELOW STR 26R. REPAIRED FRAME AT B.S. 1050 BELOW STR 26R PER SRM 51-40-3. 2L73 4F A3WE 20050923001062005092300106NM 2005 9 23 05FDEA03033 120050921A5311 FRAME BOEING737 737232 1384475NM BS 990 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 FRAME DENTED AT BS 990, BELOW STR 25L. REPAIRED FRAM AT BS 990 STR 25L PER SRM 51-40-3. 2L72 4F RTA16WE 20050923001082005092300108NM 2005 9 23 05FDEA03036 120050921A5314 KEELBEAM BOEING727 727232 1384082NM BS 740 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 LT AC BAY, BS 740 TO 800 KEELBEAM LWR WEB, 4 LIGHTNING HOLES HAVE OUT OF ROUND HOLES AND ARE MISSING STRESS BEVELS. REPAIRED LOWER KEELBEAM WEB PER SRM 51-40-2. 2L73 4F A3WE 20050923001092005092300109CE 2005 9 23 DJFA2005140 120050918A324140955 TRANSDUCER CESSNA500 560CESSNA 2076750CE IAE V2524 V2524A5 NE ANTI SKID SYS INTERMITTENT E DJFAO OTHER SJ AFFECT SYSTEMS WARNING INDICATION TXTAXI/GRND HDL 1 EA23501CW12900 5600050 THE CREW REPORTED THAT THE AIRCRAFT BRAKING FAILED UPON EXITING THE RUNWAY AFTER LANDING. WHEN THE ANTI-SKID SYSTEM WAS TURNED OFF, NORMAL BRAKING POWER WAS RESTORED. MAINTENANCE REPLACED BOTH ANTI-SKID WIRING HARNESSES, AND DISCOVERED BOTH MAIN LANDING GEAR WHEEL SPEED TRANSDUCERS TO BE INTERMITTENT. BOTH WHEEL SPEED TRANSDUCERS WERE REPLACED. A GROUND OPERATIONAL CHECK OF THE ANTI-SKID SYSTEM WAS SATISFACTORY. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA22CE E40NE 20050923001102005092300110NM 2005 9 23 PIDA20050115 120050919A532069539711 BRACKET BOEING737 737228 13844AGNM BS 787 CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 SUPPORT CHANNEL FOR AFT CARGO DOOR HOLD-OPEN BRACKET AT BS 787 + 9 IS CRACKED. REPLACED BRACKET PER SRM 51-10-1. 2L72 4F RTA16WE 20050923001112005092300111NM 2005 9 23 PIDA20050116 120050919A5340 ATTACH ANGLE BOEING737 737228 13844AGNM BS 1016 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 AFT FLOOR PAN ATTACH ANGLES COMMON TO BS 1016 PRESSURE WEB HAVE CORROSION. REPLACED INTERCOSTALS PER SRM 51-10-1. 2L72 4F RTA16WE 20050923001122005092300112NM 2005 9 23 PIDA20050117 120050906A52106517688165 ANGLE BOEING737 737228 13844AGNM L1 DOOR CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 L1 DOOR Z-ANGLE HAS CORROSION AT NUT PLATE HOLES. REPLACED Z-ANGLE PER SRM 51-10-1. 2L72 4F RTA16WE 20050923001132005092300113NM 2005 9 23 PIDA20050112 120050921A5347 SEAT TRACK BOEING737 737228 13844AGNM BS 344 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 CORROSION AT FORWARD END OF LT O/B SEAT TRACK AT BS 344. REPLACED SEAT TRACK PER SRM 53-10-5. 2L72 4F RTA16WE 20050923001142005092300114NM 2005 9 23 PIDA20050113 120050907A5320 ANGLE BOEING737 737228 13844AGNM BS 500A-520 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 RIGHT Z-ANGLE IN FWD CARGO BIN CORRODED FROM BS 500A TO BS 520. REPLACED Z-ANGLE PER SRM 53-10-13. 2L72 4F RTA16WE 20050923001152005092300115NM 2005 9 23 PIDA20050137 120050920A5320 INTERCOSTAL BOEING737 737228 13844AGNM BS 492-500A CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 INTERCOSTAL IN FWD CARGO BIN AT RBL 23 CORRODED AT NUT PLATES FROM BS 492 TO BS 500A. REPLACED INTERCOSTAL PER DWG 65-20726 AND SRM 51-10-6. 2L72 4F RTA16WE 20050923001162005092300116NM 2005 9 23 PIDA20050121 120050920A5320694580731 ANGLE BOEING737 737228 13844AGNM BS 277 CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 ANGLE BELOW STR12RT JUST FWD OF R1 DOOR AT BS 277 + 10 IS CRACKED. REPLACED ANGLE PER DWG 69-45807. 2L72 4F RTA16WE 20050923001182005092300118NM 2005 9 23 PIDA20050124 120050912A5320 INTERCOSTAL BOEING737 737228 13844AGNM BS 298 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 INTERCOSTAL AT BS 298 FROM RBL 32 TO RBL 45 HAS LITE SCRATCHES ON UPPER SURFACE AND CORROSION ON LOWER SURFACE AT CLIP NUT HOLES. REPLACED INTERCOSTAL PER SRM 51-10-1. 2L72 4F RTA16WE 20050923001212005092300121NM 2005 9 23 05FDEA03037 120050921A5320 BEAM BOEING727 727232 1384082NM BS 760-848 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION ON TOP LONGITUDINAL BEAM BS 760 TO 848.95 LBL 25 WL 208. REPAIRED PER SRM 53-10-1, 53-10-2. 2L73 4F A3WE 20050923001232005092300123NM 2005 9 23 05FDEA03039 120050921A5322 SHEAR TIE BOEING727 727232 1384082NM BS 950B CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 AFT CARGO BAY, SHEAR TIE IS CORRODED AT BS 950B, RBL9, WL138. REPAIRED AFT CARGO BAY, SHEAR TIE AT BS 950B, RBL 9 WL 138 IAW SRM 51-10-2, 53-10-4. 2L73 4F A3WE 20050923001252005092300125EU 2005 9 23 AWXA200501087 120050921A335032145410 POWER SUPPLY AIRBUS320 A320232 3930326EU EMERGENCY LIGHT INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28652AW2644826437 953 ATL - EEL - DURING 8 DAY CHECK DISCOVERED THE FORWARD GALLEY EMERGENCY POWER SUPPLY WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD GALLEY EMERGENCY POWER SUPPLY IAW AIRBUS 320 AMM 33-51-38-000-001. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA28NM 20050923001272005092300127NM 2005 9 23 AWXA200501089 120050921A2560P4010021 BATTERY BOEING737 7373B7 1384580NM FLASHLIGHT INOPERATIVE A AWXAO OTHER O OTHER TXTAXI/GRND HDL 1 WP28328AW 23377 PHX - EEL - CREW REPORTED TO MAINTENANCE THE FORWARD GALLEY FLASH LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD GALLEY EMERGENCY FLASHLIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20050923001292005092300129EU 2005 9 23 AWXA200501091 120050921A2910 O-RING AIRBUS320 A320231 3930325EU HYD SYSTEM LEAKING A AWXAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP28620AW 052 PHX - EMERGENCY LANDING - FLT 506 - DURING CRUISE, EN ROUTE TO PHX, CREW RECEIVED ECAM MSG HYD Y RSVR LO LVL. CREW MADE PRECAUTIONARY EMERGENCY LANDING IN PHX. LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED UNION O-RINGS ON THE HYDRAULIC POWER TRANSFER UNIT MANIFOLD. LEAK CHECKS WERE GOOD. 2L72 4F RTA28NM 20050926000082005092600008SO 2005 9 26 RAIA00509033 120050920A2611 SMOKE DETECTOR EMB 145 EMB145LR 3260212SO LAVATORY MALFUNCTIONED A RAIAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 CE03847HK 14500857 FLT 7936 - STL - LAVATORY SMOKE LIGHT. MAINTENANCE INSPECTED LAVATORY SMOKE DETECTOR AND FOUND NO FAULTS. 2L72 4T RTT00011AT 20050926000112005092600011SO 2005 9 26 RAIA00509037 120050919A3397 CONNECTOR EMB 145 EMB145EP 3260221SO BATTERY PACK LOOSE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03826HK 145016 FLT 5493 - STL - FLOOR EMERGENCY LIGHTS INOP AT SEAT 12A. MAINTENANCE RESEATED CONNECTION TO THE BATTERY PACK AT 12A. 2L72 4F RTT00011AT 20050926000172005092600017NM 2005 9 26 PIDA20050135 120050923A5347 SEAT TRACK BOEING737 737228 13844AGNM BS 986-1016 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 SEAT TRACK AT RBL18 HAS CORROSION ON FLANGES FROM BS 986 TO BS 1016. REPLACED TRACK PER SRM 53-10-2 AND SRM 51-30-2. 2L72 4F RTA16WE 20050926000182005092600018NM 2005 9 26 PIDA20050138 120050922A5320 INTERCOSTAL BOEING737 737228 13844AGNM BS 987-1006 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 INTERCOSTAL AT BL0 FROM BS 987 TO BS 1006 HAS CORROSION ON UPPER SURFACE. REPLACED INTERCOSTAL PER SRM 51-10-1. 2L72 4F RTA16WE 20050926000202005092600020NM 2005 9 26 USAA051138 120050921A5340 STRINGER CLIP BOEING737 7374B7 1384702NM BS 500F CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19443US 24842 FOUND TIE CLIP CRACKED, BS 500F S-8R. REPLACED WITH IDENTICAL PART, REMOVED AND REPLACED STRINGER TIE CLIP IAW SRM 51-40-02, DEFECT SIZE: .250". 2L72 4F RTA16WE 20050926000282005092600028EU 2005 9 26 USAA200509004 120050920A5320D5347217220500 FLOOR SUPPORT AIRBUS320 A320214 3930316EU FS 68-67 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19115US 1171 TWO EACH 1" BY 1" CORRODED AREAS AT RT -Y1292 FLOOR SUPPORT AT FS 68 AND 10" FWD OF FS 67. REPLACED FLOOR SUPPORT PER SRM 51-72-11. 2L72 4F RTA28NM 20050926000312005092600031EA 2005 9 26 SWIA200515560 120050402A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 621 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07917SW 7641 FS 621 FLOORBEAM ANGLE LBL 42 CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED ANGLE IAW CRJ REO 601R-53-61-117 REV "B". 2L72 4F RTA21EA 20050926000442005092600044EA 2005 9 26 SWIA200515573 120050917A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLT SPOILERS MALFUNCTIONED A SWIAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 NM07443SW 7638 ON DEPARTURE THROUGH 2000' RT FLIGHT SPOILER DEPLOYED MSG WAS DISPLAYED, FOLLOWED BY A SPOILER FAULT MESSAGE. REPLACED RT OB FLIGHT SPOILER PCU IAW MM 27-62-01, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050926000552005092600055NM 2005 9 26 USAA051141 120050922A53206545834551 INTERCOSTAL BOEING737 7374B7 1384702NM BS 328-344 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19443US 24842 INTERCOSTAL CRACKED, LBL 45 BETWEEN STA 328 AND 344. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-40-02, DEFECT SIZE: .375" CRACK. 2L72 4F RTA16WE 20050926000732005092600073NM 2005 9 26 QXEA200501254 120050921A2910 B-NUT BOMBDRDHC8 DHC8402 1390042NM HYD LINE LOOSE A QXEAD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 NM09400QX 4030 GEG FLIGHT NR 2365: ON PUSHBACK, HYDRAULIC FLUID WAS NOTED LEAKING FROM NOSE GEAR. AIRCRAFT WAS PULLED BACK TO GATE. MAINTENANCE TIGHTENED LOOSE B-NUT AT NLG DOWN ACTUATOR LINE. PRESSURIZED ALL HYDRAULIS SYSTEMS. NO LEAKS FOUND. CYCLED NOSE WHEEL STEERING. HYDRAULIC SYSTEMS OPERATED NORMALLY. HYDRAULIC FLUID QUANTITIES ALL GOOD. NO PARTS REPLACE. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050926000752005092600075NM 2005 9 26 SB05118 120050921A5497FRF0E2822P03 CONNECTOR BOEING737 7374B7 1384702NM NR 2 PYLON BURNED A USAAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 EA19430US 24552 BOS - FLT822 - ON FINAL APPROACH TO BOS, THE TR2 AND TR3 CIRCUIT BREAKERS POPPED. CREW INITIATED A GO-AROUND THE FIELD AND POWERED UP THE APU. EVERYTHING WAS NORMAL FOR LANDING. UPON SECOND FINAL APPROACH, THE SAME THING HAPPENED AS WITH THE FIRST APPROACH. CAPTAIN DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. AIRCRAFT TAXIED TO THE GATE ON ITS OWN POWER. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE PYLON CONNECTOR D3024 AND MATING FIREWALL CONNECTOR D410 PLUS GENERATOR FEEDER PINS AND SOCKETS. ALSO, REMOVED AND REPLACED NR 3 TRANSFORMER RECTIFIER UNIT AS PRECAUTIONARY. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050926000802005092600080EA 2005 9 26 COMA0560505 120050916A2752852D10019 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA FLAP FAULTY A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01956CA6270 7105 FLIGHT 5786 - DURING CLIMBOUT OF JFK RECEIVED A FLAP FAIL CAUTION MESSAGE AT 20 DEGREE FLAP SETTING. REPLACED FLAP ACTUATOR. 2L72 4F RTA21EA 20050926000832005092600083NM 2005 9 26 QXEA200501251 120050921A335061047811 BATTERY PACK DHAV DHC8 DHC8202 2809007NM EMERGENCY LIGHT INOPERATIVE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09352PH1188251 494 PDX - OVERHEAD EMERGENCY LIGHTS CABIN, INOPERABLE AT NR 1 AND NR 4 POSITIONS. REMOVED AND REPLACED BATTERY PACK AT PS 2 STATION OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050926000852005092600085NM 2005 9 26 QXEA200501253 120050919A3220 STRUT BOMBDRDHC8 DHC8402 1390042NM NLG DISCHARGED A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09415QX 4081 PDX FLIGHT NR 2311: WITH AIRCRAFT LOADED, AFTER PUSH BACK, NOSE STRUT APPEARS FLAT. MAINTENANCE SERVICED NOSE LANDING GEAR STRUT WITH NITROGEN PER SERVICE PLACARD USING A CALIBRATED GAUGE. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050926000882005092600088NE 2005 9 26 QXEA200501242 220050919A7310 MANIFOLD CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE NR 2 ENG FUEL LEAKING A QXEAO OTHER K FLUID LOSS NRNOT REPORTED 1 NM09600QX 10005 PDX - NR 2 ENGINE FUEL LEAK. REPLACED THE VG SLAVE ACTUATOR WITH NO HELP. REPLACED THE HEAD-END MANIFOLD. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050926000922005092600092 2005 9 26 SWAA052868 420050921A2565D31354 SLIDE BOEING737 7373Q8 1384670NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29317WN 24068 R2 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20050926000942005092600094NM 2005 9 26 SWAA052870 120050920A53306545774 SKIN BOEING737 7373H4 1384600NM BS 773-787 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 773 & BS 787, STR 18L TO STR 19L. REPAIRED SKIN PER SRM & SWA EA. 2L72 4F RTA16WE 20050926000962005092600096 2005 9 26 SWAA052872 420050921A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29603SW 27954 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20050926000982005092600098NM 2005 9 26 SWAA052874 120050921A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 665 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 665, STR 10R. REMOVED AND REPLACED STR CLIP PER SRM. 2L72 4F RTA16WE 20050926001002005092600100NM 2005 9 26 SWAA052876 120050921A53106547978 CREASE BEAM BOEING737 7373H4 1384600NM BS 817 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29618WN 28034 DURING SCHEDULED D-CHECK, FOUND FUSELAGE LT CREASE BEAM CORRODED AT BS 817. REPAIRED CREASE BEAM PER SRM. 2L72 4F RTA16WE 20050926001042005092600104NE 2005 9 26 QXEA200501247 220050920A73204120T02P02 ACTUATOR CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 30049NE ZONE 400 LEAKING A QXEAO OTHER K FLUID LOSS NRNOT REPORTED 1 NM09613QX 10045 PDX - FUEL LEAKING FROM NR 2 ENGINE. MAINTENANCE REPLACED THE MASTER VG ACTUATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E00063EN 20050926001382005092600138NM 2005 9 26 UPS05645480 120050923A2420 GENERATOR BOEING767 767300 1385204NM RIGHT LEAKING A IPXABA EMER. DESCENT UNSCHED LANDING KHJFLUID LOSS ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 SO01315UP 27743 ATB - RT GENERATOR FAILED, EMERGENCY DECLARED. SERVICE RT IDGE WITH 2 QTS OIL GWL 0558164/REMOVED NR 2 ENG IDG IAW MM 24-11-01 DW 0558595\ TRANSFERRED FITTINGS WITH NEW O-RINGS TW 1229598 REF MM 24-11-01 INSTALLED NEW IDGE ON NR 2 ENG OPS AND LEAK CK GOOD. 2L72 4F RTA1NM 20050926001512005092600151NM 2005 9 26 SWAA052886 120050922A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29403WN 29815 EEPLS TRACK LOOSE AT FWD END. SECURED EEPLS PER MM. 2L72 4F RTA16WE 20050926001922005092600192EA 2005 9 26 A1Z2005F00000 220050811A74144370 MAGNETO PIPER PA28 PA28R180 7102809SO LYC O360 IO360B1E 41514EA HARTZLHCC2Y HCC2YK1 GL RIGHT FAILED E A1ZAO OTHER O OTHER NRNOT REPORTED 1 SO337565J512 28R30943 L1899751A CH7906 MAGNETO EXIBITED EXCESSIVE DROP AT RUN-UP. INSPECTION REVEALED THAT THE ROTATING MAGNET SHAFT HAD DISINTEGRATED BETWEEN THE FWD BEARING AND THE ROTATING MAGNET THE 2 WERE SEPARATED COMPLETELY. THE FAILURE DID NOT APPEAR TO BE CAUSED BY STRESS. IT EXIBITED EVIDENCE OF A METALURGICAL FLAW. A PROP STRIKE DID NOT OCCUR. (K) 1L71 3O3 O 2A13 1E10 5 CP920 20050926001962005092600196NM 2005 9 26 S2YA05051 120050827A2420ALT3524 GENERATOR DORNERDO32 DO328300 NM PWA 306 PW306B NE AC SYSTEM INOPERATIVE A S2YAC ABORTED TAKEOFF J WARNING INDICATION TXTAXI/GRND HDL 1 GL13360SK100113074 3136 BEFORE TAKEOFF, THE CREW REPORTED A RT ALTERNATOR FAIL AND ABORTED THE TAKEOFF. MAINTENANCE REPLACED THE RT AC GENERATOR, WITH OPS CHECKS GOOD, THE AC WAS RETURNED TO SERVICE. (K) 2H72 4T4 FRTA55NM E35NE 20050926002012005092600201EA 2005 9 26 ASOA05678 120050819A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FS 559-605 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27839AS 7284 DURING A C-CHECK, THE RT FLOOR SUPPORT WEB AT FS 559.112 TO FS 605 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE WILL DETERMNE THE APPROPRIATE REPAIR UPON FURTHER INSPECTION ON THE RT FLOOR SUPPORT WEB AT FS 559.112 TO FS 605. THIS MRR WILL REMAIN OPEN PENDING THE APPROPRIATE CORRECTIVE ACTION. (K) 2L72 4F4 FRTA21EA E15NE 20050927000152005092700015EU 2005 9 27 KBM2005F00241 120050828A6520350A33215001 BALL END SNIAS 350 AS350B2 8680813EU TAIL ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV 3296 BALL END HAS EXCESSIVE PLAY. REPLACED WITH O/H UNIT. (M) 1G71 3U H9EU 20050927000172005092700017SO 2005 9 27 SIMA200522004 120050801A532014522459003 SUPPORT EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21816AE 145552 SAW - DURING IMBV INSPECTION, FOUND CENTER HAT BEAM RAMP CORRODED. REMOVED AND INSTALLED NEW HAT BEAM RAMP IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050927000222005092700022EU 2005 9 27 SIMA200522008 120050804A53477253742409 SEAT TRACK SAAB SF340 340B 7860101EU CABIN CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21324AE 340B324 THE SEAT TRACK AT BL 36R WAS FOUND CORRODED. REMOVED EXISTING SEAT TRACK AT BL 36R. CLEANED AND TREATED NEW SEAT TRACK. REPAIR DONE IAW SAAB 340B SRM, SRM 72LKS 3079, CHAPTERS 51-40-21, 51-40-22, 51-40-25 AND 51-40-40. (M) 2L72 4T RTA52EU 20050927000252005092700025EU 2005 9 27 USAA050933 120050729A5315 FLOORBEAM AIRBUSA319 A319112 3930323EU CARGO BAY CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19723UW 1109 PIT - FOUND BEAM CORRODED 1 SQUARE INCH, FLOOR SUPPORT AT C-20 Y-254. INSTALLED REPAIR ANGLE PER SRM 53-00-14, PAGE 223/224 FIG 204. (M) 2L72 4F RTA28NM 20050927000382005092700038NM 2005 9 27 USAA051007 120050815A5320 SPLICE BOEING737 7374B7 1384702NM BS 360 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19449US 24893 CLT - FOUND SPLICE CHANNEL 1 INCH, BS 360 S15L STRINGER. REMOVED DAMAGED SPLICE AND INSTALLED NEW SPLICE P/N 65-61777-5 IAW SRM 51-40-02. (M) 2L72 4F RTA16WE 20050927000402005092700040SO 2005 9 27 SIMA200523507 120050814A532014525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO FS 20 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21711PH 145235 A PREVIOUS REPAIR ON THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. REMOVED THE CORRODED PREVIOUS REPAIR. FABRICATED A DOUBLER, (EPNEM53EP54701) AND FILLER (EPNNEM53EP54703). FABRICATED A PLATE AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 30, CHAPTERS 51-40-02 AND 53-00-10. (M) 2L72 4F RTT00011AT 20050927000702005092700070EA 2005 9 27 SIMA200522006 120050805A335020131A BATTERY PACK CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT DISCHARGED A SIMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW21503AE 10021 ORD - EMERGENCY LIGHTS SWITCH ON THE F/A STATION WERE LEFT ON AND DRAINED EMERGENCY LIGHT BATTERIES. REPLACED ALL 4 EMERGENCY LIGHT BATTERY PACKS. ALL FOUR PART NUMBERS OFF ARE P/N 2013-1A AND NR 1 BATTERY PACK S/N 62620, NR 2 IS S/N 83873, NR 3 IS S/N 78392, AND NR 4 IS S/N 67593. (M) 2L72 4F RTA21EA 20050927000732005092700073SO 2005 9 27 SIMA200523508 120050813A532014525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21710TB 145224 A PREVIOUS REPAIR ON THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED A PLATE, FILLER, AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 30, CHAPTER 53-00-10. (M) 2L72 4F RTT00011AT 20050927000742005092700074SO 2005 9 27 SIMA200522001 120050729A532014532637401 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO FR 24-25 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21816AE 145552 SAW - DURING IMBV INSPECTION, FOUND RIGHT OMEGA BEAM CORRODED BETWEEN FRAMES 24 AND 25 BY CROSS BEAM ATTACHMENTS POINTS. REPAIRED RIGHT OMEGA BEAM WITH DOUBLER IAW SRM 53-22-10 FIGURE 202. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050927000832005092700083EU 2005 9 27 KBM2005F00243 120050820A6410355A09103601 BEARING SNIAS 350 AS350BA 8680817EU TAIL ROTOR CRACKED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P 2347 UNIT HAS MULTIPLE CRACKS. REMOVED AND REPLACED UNIT. (M) 1G71 3U NCH9EU 20050927000842005092700084SO 2005 9 27 SIMA200523404 120050812A554212051385007 SKIN EMB 135 EMB135LR 3260305SO RUDDER CRACKED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21715AE 145262 FOUND DURING MBV, RUDDER NR 2 SKIN CRACKED ON RIGHT LOWER TRAILING EDGE. REPAIRED DAMAGED SKIN ON RUDDER NR 2 IAW IC2005-145/4198A. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050927000932005092700093SO 2005 9 27 SIMA200525207 120050828A321014571035411 CAP EMB 135 EMB135KL 3260302SO RT MLG CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21817AE 145554 SAW - DURING MBV INSPECTION, FOUND RIGHT MLG AFT BEARING CAP CORRODED. REMOVED AND REPLACED RIGHT MLG AFT BEARING CAP IAW EMB 140 WORK CARD 57-200-84. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050927001042005092700104EU 2005 9 27 KBM2005F00238 120050901A6520 BUSHING SNIAS 350 AS350B2 8680813EU T/R GEARBOX DEBONDED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19966SH MA04703 3787 TAIL ROTOR GEAR BOX LEVER BUSHING HAD DEBONDED. REPLACED TRGB CONTROL LEVER WITH NEW. (M) 1G71 3U H9EU 20050927001072005092700107EA 2005 9 27 ASOA05669 120050817A5210601R3198087 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11889AS 7538 DURING HANGAR MAINTENANCE IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20050927001162005092700116SO 2005 9 27 SIMA200523402 120050810A5320 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO FR 22 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21715AE 145262 FOUND DURING CPCP INSPECTION, GALLEY FLOOR SUPPORT CORRODED AT FRAME 22. INSTALLED NEW GALLEY FLOOR SUPPORT AT FRAME 22 IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050927001172005092700117SO 2005 9 27 SIMA200524109 120050825A531314533888001 STRINGER EMB 135 EMB135KL 3260302SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21824AE 145584 STRINGER 19R WAS FOUND TO BE CHAFED AT THE AFT BELLY PANEL. BLENDED THE CHAFED AREA AND FABRICATED AND ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 30 CHAPTER 53-24-02. (M) 2L72 4F RTT00011AT 20050927001212005092700121EA 2005 9 27 ASOA05676 120050819A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA BS 280 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11839AS 7284 DURING A C-CHECK IN MCN, THE FORWARD AND AFT FLOOR SUPPORT ANGLES AT FS 280 BETWEEN LBL 9 AND RBL 9 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FORWARD AND AFT FLOOR SUPPORT ANGLES AT FS 280 BETWEEN LBL 9 AND RBL 9 IAW ASA EO 600-53-0309. (M) 2L72 4F RTA21EA 20050927001262005092700126EA 2005 9 27 ASOA05717 120050810A5310 DOOR FRAME CNDAIRCL600 CL6002B19 1900309EA BS 338.9 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11853AS 7374 DURING A C-CHECK IN HOT, THE PASSENGER DOOR FRAME AND INNER SKIN AT FS 338.90, DOOR DATUM 1 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE PASSENGER DOOR FRAME AND INNER SKIN AT FS 338.90, DOOR DATUM 1 IAW ASA EO 600-52-0130. (M) 2L72 4F RTA21EA 20050927001282005092700128EU 2005 9 27 ASOA05714 120050801A5740 BRACKET AEROSPATR72 ATR72 EU WING CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11636AS 375 DURING A C-CHECK IN YUL, FOUR OMEGA BRACKETS ON THE LEFT WING AT THE NR 4 FLAP HINGE, RIB 8 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED FOUR OMEGA BRACKETS ON THE LEFT WING AT THE NR 4 FLAP HINGE, RIB 8 IAW ATR 72 SRM 51-25-01. (M) 2H72 4T RT 20050928000052005092800005SO 2005 9 28 SIMA200525225 120050908A335020131A BATTERY EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT DISCHARGED A SIMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW21700LE 145156 CLT - FLT 4892 - DURING PREFLIGHT, EMERGENCY LIGHT FROM ROW 7 FORWARD FAILED TO ILLUMINATE. REMOVED AND REPLACED NR 2 EMERGENCY LIGHT BATTERY IAW EMB AMM 33-50-04. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050928000072005092800007SO 2005 9 28 SIMA200525505 120050906A335010049 BATTERY PACK EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCHARGED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21655AE 145452 MAINTENANCE DISCOVERED RIGHT OVERWING EMERGENCY HATCH LIGHT INOPERATIVE. REPLACED NUMBER THREE EMERGENCY BATTERY POWER SUPPLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20050928000082005092800008SO 2005 9 28 SIMA200525502 120050909A261147359713 SMOKE DETECTOR EMB 135 EMB135LR 3260305SO CARGO BAY WILL NOT TEST A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21728AE 145328 AFT BAGGAGE SMOKE DETECTOR WILL NOT TEST. REPLACED SMOKE DETECTOR NR 1 IAW EMB 135 AMM 26-15-01. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050928000092005092800009SO 2005 9 28 SIMA200525224 120050907A33207287503517 LIGHT EMB 135 EMB135LR 3260305SO ROW 6A BURNED A SIMAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW21735TS 145386 SMOKE COMING FROM FLOURESCENT LAMP FIXTURE OVER ROW 6A. REPLACED LIGHT FIXTURE AT SEAT 6A IAW EMB WM SP CH 20-21. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050928000102005092800010SO 2005 9 28 SIMA200525222 120050904A571014569009408 FITTING EMB 135 EMB135KL 3260302SO RT WING AILERON DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21821AE 145577 ABI - THE RIGHT AILERON PCA FITTING INBOARD BUSHING HOLE WAS FOUND DAMAGED. REMOVED AND THE EXISTING PCA FITTING. INSTALLED NEW PCA FITTING IAW EMB 145 SRM, SRM EMB-145/1142 REV 30, CHAPTERS 51-40-02 AND EMB REPAIR STATEMENT IC2005-145/4844 DATED SEPT 2, 2002 PARA 1. (M) 2L72 4F RTT00011AT 20050928000112005092800011SO 2005 9 28 SIMA200525701 120050910A21214611028900 FAN EMB 135 EMB135KL 3260302SO CABIN SEIZED A SIMAG O2 MASK DEPLOYED B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21813AE 145539 SJC - FLT 3158 - CREW REPORTED PLASTIC BURNING SMELL IN ENTIRE AIRCRAFT HAD TO DON OXYGEN MASKS. REPLACED NR 1 RECIRCULATION FAN. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050928000122005092800012SO 2005 9 28 SIMA200525219 120050902A532014522178005 SILL EMB 135 EMB135KL 3260302SO SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21821AE 145577 ABI - THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED THE SERVICE DOOR SILL AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM, SRM EMB145/1142 REV 30, CHAPTERS 51-40-02 AND 51-20-01. (M) 2L72 4F RTT00011AT 20050928000132005092800013SO 2005 9 28 SIMA200525223 120050901A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO FS 20 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21818AE 145561 ON THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. REMOVED THE PREVIOUS REPAIR AND CLEANED THE AREA. FABRICATED A REPAIR PLATE AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB-145/1142 REV 30, CHAPTER 53-00-10 FIG 201. (M) 2L72 4F RTT00011AT 20050928000142005092800014SO 2005 9 28 SIMA200525702 120050912A28102810051102 VALVE EMB 145 EMB145LR 3260212SO RT WING LEAKING A SIMAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW21618AE 145097 DFW - FLT 3807 - FUEL STREAMING FROM THE RIGHT WING. CREW DECLARED AN EMERGENCY AND LANDED SAFELY. REPLACED RIGHT FUEL VENT VALVE AND OUTBOARD FUEL FLOAT VALVE PER AMM 05-50-02. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. FLOAT VALVE P/N 2930015101. (M) 2L72 4T RTT00011AT 20050928000152005092800015EU 2005 9 28 ASOA05712 120050729A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU FR 39-41 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11636AS 375 DURING A C-CHECK IN YUL, THE SEAT TRACK BETWEEN FRAME 39 TO FRAME 41 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK BETWEEN FRAME 39 TO FRAME 41 IAW ATR 72 SRM 51-25-04. (M) 2H72 4T RTA53EU 20050928000172005092800017NE 2005 9 28 KBM2005F00255 220050815A72609560115450 MAGNETIC SEAL SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE ENGINE LEAKING E KBMAO OTHER K FLUID LOSS NRNOT REPORTED 1 WP19115SH 3141 UNIT LEAKS. REMOVED AND REPLACED MAG SEAL. (M) 1G71 3U3 U H9EU E19EU 20050928000182005092800018SO 2005 9 28 SIMA200524106 120050824A531314533888001 STRINGER EMB 135 EMB135LR 3260305SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21719AE 145276 A PREVIOUS REPAIR OF STRINGER 19R WAS FOUND TO BE CHAFED. REMOVED THE EXISTING REPAIR AND CLEANED THE AREA. FABRICATED A REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 30, CHAPTERS 53-24-02 AND EMB IC2005-145/4506 DATED AUGUST 19, 2005. (M) 2L72 4F RTT00011AT 20050928000192005092800019EU 2005 9 28 KBM2005F00247 120050820A21210500547 MOTOR SNIAS 350 AS350BA 8680817EU BLOWER OSCILLATES E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P 2347 RPM OSCILLATES. REMOVED AND REPLACED BLOWER MOTOR. (M) 1G71 3U NCH9EU 20050928000202005092800020NE 2005 9 28 KBM2005F00245 220050820A749718466 IGNITION LEAD SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE RT ENGINE DETERIORATED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P 2347 RIGHT ENGINE INGNITER CABLE DETERORATED AND WEAK SPARKS. REMOVED AND REPLACED IGNITER CABLE. (M) 1G71 3U3 UNCH9EU E19EU 20050928000212005092800021EU 2005 9 28 KBM2005F00244 120050820A6520 BUSHING SNIAS 350 AS350BA 8680817EU CONTROL LEVER DEBONDED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P MA05254 2347 TRGB LEVER CONTROL ARM BUSHING IS DEBONDED, REMOVED AND REPLACED. (M) 1G71 3U NCH9EU 20050928000222005092800022EA 2005 9 28 ASOA05729 120050830A5320 SILL CNDAIRCL600 CL6002B19 1900309EA BS 499-513 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11834AS 7254 DURING A C-CHECK IN MCN, THE RIVETS ON THE LEFT SIDE PRESSURE FLOOR SILL STRUCTURE AT FS 499 TO FS 513 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO BOMBARDIER OR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. (M) 2L72 4F RTA21EA 20050928000242005092800024NM 2005 9 28 USAA051052 120050824A5754 SKIN BOEING737 7373B7 1384580NM NR 6 SLAT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19511AU 23594 CLT - FOUND SKIN CRACKED 1 INCH, OUTBOARD LOWER SKIN OF NR 6 SLAT. INSTALLED DOUBLER IAW SRM 57-43-01. (M) 2L72 4F RTA16WE 20050928000252005092800025NM 2005 9 28 USAA050997 120050810A532065C336557 INTERCOSTAL BOEING737 7374B7 1384702NM BS 380-400 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19449US41152 24893 CLT - FOUND CHORD CRACKED .4 INCHES, UPPER CHORD ON INTERCOSTAL BETWEEN BS 380 AND 400, RBL 11. FABRICATED AND INSTALLED NEW CHORD IAW BOEING DRAWING 65C33655 AND SRM 51-40-02. (M) 2L72 4F RTA16WE 20050928000262005092800026NM 2005 9 28 USAA050998 120050810A5320 INTERCOSTAL BOEING737 7374B7 1384702NM BS 380-400 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19449US41152 24893 CLT - FOUND CHORD CRACKED .3 INCH, UPPER CHORD ON INTERCOSTAL BETWEEN BS 380 AND BS 400 AT BL 0. FABRICATED AND INSTALLED NEW CHORD IAW BOEING DRAWING 69-35365 AND SRM 51-40-02. (M) 2L72 4F RTA16WE 20050928000272005092800027NM 2005 9 28 USAA050996 120050809A5330 SKIN BOEING737 7373B7 1384580NM FS 727 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19391US55571 23313 CLT - FOUND SKIN CRACKED 1.75 INCH, FS 727, STRINGER 20L. INSTALLED DOUBLER AND TRIPLER AND FILLERS IAW SRM 53-00-01 FIG 201. (M) 2L72 4F RTA16WE 20050928000302005092800030NM 2005 9 28 USAA050994 120050809A5330 SKIN BOEING737 7373B7 1384580NM BS 328 DENTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19530AU 24412 CLT - FOUND SKIN DENTED 5 INCHES LONG, .0200 INCHES WIDE AND .002 INCHES DEEP, FUSELAGE STATION 328 BETWEEN STRINGERS 20 AND 21 LEFT. INSTALLED DOUBLER AND TRIPLER IAW SRM 53-00-01 FIG 201. (M) 2L72 4F RTA16WE 20050928000312005092800031NM 2005 9 28 USAA051003 120050815A5753 WEDGE BOEING737 7374B7 1384702NM TE FLAP DELAMINATED A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19449US 24893 CLT - FOUND WEDGE SKIN AND CORE DELAMINATED 2 INCHES BY 3 INCHES, RT L/B T/E FLAP WEDGE AT LB END. REMOVED AND REPLACED SKIN AND CORE AS REQUIRED IAW SRM 51-70-10. (M) 2L72 4F RTA16WE 20050928000322005092800032EA 2005 9 28 ASOA05734 120050830A5321 PRESSURE PANEL CNDAIRCL600 CL6002B19 1900309EA CABIN FLOOR CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11834AS 7254 DURING A C-CHECK IN MCN, THE RIGHT SIDE PRESSURE FLOOR SKIN AT FS 499 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO BOMBARDIER FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. AFTER MAINTENANCE BLENDED THE RIGHT SIDE PRESSURE FLOOR SKIN AT FS 499, IAW ASA EO 600-53-0319, IT WAS FOUND TO BE WITHIN ACCEPATABLE LIMITS. (M) 2L72 4F RTA21EA 20050928000332005092800033EA 2005 9 28 ASOA05728 120050830A5321 PRESSURE PANEL CNDAIRCL600 CL6002B19 1900309EA CABIN FLOOR CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11834AS 7254 DURING A C-CHECK IN MCN, THE RIGHT SIDE PRESSURE FLOOR SILL STRUCTURE AT FS 461 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE 2L72 4F RTA21EA 20050928000352005092800035EA 2005 9 28 ASOA05731 120050830A5320 SILL CNDAIRCL600 CL6002B19 1900309EA BS 541 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11834AS 7254 DURING A C-CHECK IN MCN, THE LEFT SIDE PRESSURE FLOOR SILL STRUCTURE AT FS 541 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO BOMBARDIER FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. (M) 2L72 4F RTA21EA 20050928000362005092800036EA 2005 9 28 ASOA05733 120050830A5320 SILL CNDAIRCL600 CL6002B19 1900309EA BS 484 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11834AS 7254 DURING A C-CHECK IN MCN, THE RIGHT SIDE PRESSURE FLOOR SILL AT FS 484 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO BOMBARDIER FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. MAINTENANCE REPAIRED THE RT SIDE PRESSURE FLOOR SILL AT FS 484 IN ACCORDANCE WITH ASA EO 600-53-0319 CLOSED (M) 2L72 4F RTA21EA 20050928000372005092800037EA 2005 9 28 ASOA05727 120050830A5321 PRESSURE PANEL CNDAIRCL600 CL6002B19 1900309EA CABIN FLOOR CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11834AS 7254 DURING A C-CHECK IN MCN, THE LEFT SIDE PRESSURE FLOOR SKIN PLANK AT FS 461 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO BOMBARDIER FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. (M) 2L72 4F RTA21EA 20050928000382005092800038EU 2005 9 28 KBM2005F00253 120050810A6420350A33215300 BEARING SNIAS 350 AS350B2 8680813EU TAIL ROTOR BULGED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19751H 3403 UNIT HAS CUTS AND BULGING. REMOVED AND REPLACED LAMINATED BEARING. (M) 1G71 3U H9EU 20050928000402005092800040EA 2005 9 28 ASOA05693 120050820A5330 FINGER DOUBLER CNDAIRCL600 CL6002B19 1900309EA BS 499-510 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11839AS 7284 DURING A C-CHECK IN MCN, THE FINGER DOUBLER AT FS 499 TO FS 510, RBL 44 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO BOMBARDIER FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. S/D - MAINTENANCE REMOVED THE CORROSION FROM THE FINGER DOUBLER AT FS 499 TO FS 510, RBL 44 COMPLYING WITH ASA EO 600-53-0313. (M) 2L72 4F RTA21EA 20050928000422005092800042EU 2005 9 28 USAA050936 120050729A5310 BEAM AIRBUSA319 A319112 3930323EU FR 66-68 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19723UW 1109 PIT - FOUND BEAM CORRODED 1 INCH BY 1 INCH, .5 INCH BY .5 INCH, .5 INCH BY .5 INCH , .5 INCH BY .5 INCH, BETWEEN FRAME 68 AND 66, APPROX Y48. REMOVED AND REPLACED BEAM PER SRM 51-72-11. (M) 2L72 4F RTA28NM 20050928000432005092800043EA 2005 9 28 ASOA05694 120050820A5330 FINGER DOUBLER CNDAIRCL600 CL6002B19 1900309EA BS 510-517 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11839AS 7284 DURING A C-CHECK IN MCN, THE FINGER DOUBLER AT FS 510 TO FS 517, RBL 34-44 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO BOMBARDIER FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. S/D - MAINTENANCE REMOVED THE CORROSION FROM THE FINGER DOUBLER AT FS 51- TO FS 517, RBL 34-44 BY COMPLYING WITH ASA EO 600-53-0313. (M) 2L72 4F RTA21EA 20050928000462005092800046EA 2005 9 28 ASOA05721 120050825A3220 LANDING GEAR CNDAIRCL600 CL6002B19 1900309EA NOSE VIBRATION A ASOAO OTHER E VIBRATION/BUFFET TOTAKEOFF 1 SO11901EV 7616 FLT 4300 - DURING THE TAKEOFF ROLL FROM ATW-ATL, AT APPROXIMATELY 130 KTS THE AIRCRAFT EXPERIENCED A LOUD SHIMMY FROM THE NOSE WHEEL AREA. THE CREW NOTIFIED THE ATW TOWER AFTER TAKEOFF AND REQUESTED A RUNWAY SWEEP. PIECES OF TIRE WERE FOUND AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT CONTINUED TO ATL AND LANDED SAFELY. MAINTENANCE INSPECTED THE NOSE GEAR, DOOR, FUSELAGE AND AXLES WITH NO DAMAGES NOTED. MAINTENANCE REMOVED AND REPACED BOTH NOSE TIRE WHEEL ASSEMBLIES. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050928000482005092800048EA 2005 9 28 ASOA05677 120050819A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 584 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11839AS 7284 DURING A C-CHECK IN MCN, THE FLOORBEAM AT FS 584, LBL 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FLOORBEAM AT S 584, LBL 9 IAW CRJ200 SRM 53-00-43. (M) 2L72 4F RTA21EA 20050928000512005092800051EA 2005 9 28 A6WA200540295 120050830A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA RT WING CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31467AW 7900 RIGHT WING LOWER WING FUEL TANK ACCESS DOOR CUTOUT FOR 650 OUTBOARD HAS PITTING CORROSION LESS THAN .003. MAINTENANCE REMOVED CORROSION, PERFORMED NDT, ROTO-PEENED AND APPLIED SURFACE TREATMENT IAW REO 601R-57-27-030 REV D. (M) 2L72 4F RTA21EA 20050928000532005092800053EA 2005 9 28 ASOA05662 120050913A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11917EV 7769 DURING A GROUND INSPECTION IN ATL, THE RIGHT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE RIGHT OVERWING EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050928000542005092800054NM 2005 9 28 USAA051002 120050815A5313 STRINGER BOEING737 7373B7 1384580NM FS 500A CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US 23933 CLT - FOUND STRINGER .5 INCH CRACK, FUSELAGE STATION 500A STRINGER 8L. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-00-03 FIG 203. (M) 2L72 4F RTA16WE 20050928000552005092800055EA 2005 9 28 A6WA200540294 120050830A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA LAVATORY MALFUNCTIONED A A6WAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL31402AW 7281 SMOKE TOILET MESSAGE ON GROUND WITH AURAL WARNING WHILE WAITING FOR GATE. NO SIGN OF FIRE OR SMOKE. RAN PACK AT FULL HOT, TESTED LAV SMOKE/TOILET DETECTION, OPS CHECK OK. COULD NOT DUPLICATE. OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050928000562005092800056EU 2005 9 28 SIMA200524105 120050810A53477253742407 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21324AE 340B324 THE LEFT UPPER SEAT TRACK WAS FOUND TO BE CORRODED. REMOVED THE CORRODED LEFT UPPER SEAT TRACK. INSTALLED NEW SEAT TRACK. REPAIR DONE IAW SAAB 340 SRM, SRM 72LKS3079 REV 45, CHAPTERS 51-40-21, 51-40-22 AND 51-40-40. (M) 2L72 4T RTA52EU 20050928000572005092800057EU 2005 9 28 SIMA200524104 120050817A53477253799383 SEAT TRACK SAAB SF340 340B 7860101EU BS 297-329 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21324AE21469 340B324 SEAT TRACK AT BL 18.3 BETWEEN STATION 297 AND STATION 329 WAS FOUND TO BE CORRODED. CUT OUT SECTION OF EXISTING SEAT TRACK. PREPARED A 32.5 REPAIR SECTION FROM NEW SEAT TRACK. PREPARED A 15 INCH REPAIR U BEAM. REPAIR DONE IAW SAAB 340 SRM, SRM 72LKS3079 REV 45, CHAPTER 53-70-60. (M) 2L72 4T RTA52EU 20050928000602005092800060NM 2005 9 28 UIEA200500129 120050906A541465B941002 SKIN BOEING747 7472D7B 1384803NM STA 248 CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15524MC 21784 DURING D-CHECK, FOUND NR 3 PYLON, CRACKED DAMAGE WAS FOUND IN THE SKIN ASSEMBLY AND THE ADJACENT NR 3 STIFFENER, AT PRECOOLER EXHAUST CUTOUT LOWER EDGE NEAR THE AFT CORNER AT STATION 248. THE NR 3 STIFFENER LOWER FLANGE WAS TRIMMED TO REMOVE CRACKS. THE CRACK IN THE SKIN ASSEMBLY WAS CONTAINED WITH 1 INCH DIAMETER HOLE AT THE CRACK TIP. THE NR 3 STIFFENER WAS REINFORCED WITH A NEW STEEL LOWER REPAIR ANGLE FROM NS 235-254. THE RIB INSTALLATION AT NS 248 WAS MODIFIED TO ACCOMMODATE THE NEW STEEL LOWER REPAIR ANGLE INSTALLATION ON THE NR 3 STIFFENER. (M) 2L74 4F RTA20WE 20050928000622005092800062SO 2005 9 28 SIMA200524502 120050901A2120 SMOKE EMB 135 EMB135LR 3260305SO CABIN DETECTED A SIMAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW21718AE 145275 BOS - FLT 4596 - DURING TAXI CREW REPORTED SMOKE IN COCKPIT BUT NOT IN CABIN. AIRCRAFT WAS RETURNED TO THE GATE. MAINTENANCE COULD NOT DUPLCIATE DISCREPANCY. A GOUND ENGINE RUN WITH BOTH ENGINES AND BOTH PACKS OPERATING WAS SATISFACTORY WITH NO SMOKE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050928000632005092800063EA 2005 9 28 ASOA05700 120050821A33501961002 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN FAILED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11839AS 7284 DURING A C-CHECK IN MCN, THE EMERGENCY EXIT BETA LIGHT ON THE PASSENGER DOOR HANDLE FAILED THE TEST. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT BETA LIGHT ON THE PASSENGER DOOR HANDLE. OPERATIONAL CHECKS GOOD. (M) 2L72 4F RTA21EA 20050928000642005092800064EA 2005 9 28 ASOA05697 120050820A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA BS 453 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11839AS 7284 DURING A C-CHECK IN MCN, THE FUSELAGE SKIN AT FS 453, LBL 45 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO BOMBARDIER FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. S/D - MAINTENANCE REMOVED THE CORROSION FROM THE FUSELAGE SKIN AT FS 453, LBL 45 BY COMPLYING WITH ASA EO 600-53-0314. (M) 2L72 4F RTA21EA 20050928000652005092800065NM 2005 9 28 UIEA200500128 120050906A5414 SKIN BOEING747 7472D7B 1384803NM NR 2 PYLON DAMAGED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15524MC 21784 DURING D-CHECK FOUND NR 2 PYLON HAS CRACK DAMAGE IN THE SKIN ASSEMBLY AND THE ADJACENT NR 3 STIFFENER, AT PRE-COOLER EXHAUST CUTOUT LOWER EDGE NEAR THE AFT CORNER AT STATION 248. THE NR 3 STIFFENER LOWER FLANGE WAS TRIMMED TO REMOVED CRACKS. THE CRACK IN THE SKIN ASSEMBLY WAS CONTAINED WITH 1 INCH DIAMETER OLE AT THE CRACK TIP. THE NR 3 STIFFENER WAS REINFORCED WITH A NEW STEEL LOWER REPAIR ANGLE FROM NS 235-254. THE RIB INSTALLATION AT NC 248 WAS MODIFIED TO ACCOMMODATE THE NEW STEEL LOWER REPAIR ANGLE INSTALLATION ON THE NR 3 STIFFENER. (M) 2L74 4F RTA20WE 20050928000672005092800067NM 2005 9 28 SB05122 120050924A21337133991 SEAL BOEING737 7374B7 1384702NM OUTFLOW VALVE MISSING A USAAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 EA19433US 24555 CLT - FLT 1169 DURING CRUISE, AT FL240, THE AIRCRAFT BEGAN LOSING CABIN PRESSURIZATION WHILE OPERATING ON ONE PACK. CABIN PRESSURE COULD NOT BE STABILIZED. FLIGHT DESCENDED TO 10,000 FEET WHERE CABIN PRESSURE DROPPED TO 7,000 FEET. FLIGHT CONTINUED ONTO CLT AT 10,000 FEET AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE BLADE SEAL FOR THE AFT OUTFLOW VALVE MISSING. INSTALLED NEW SEAL. ALSO, TIGHTENED LOOSE APU DUCT CLAMP AT BULKHEAD THRU FITTING AND REMOVED AND REPLACED TWENTY FUSELAGE BELLY DRAINS. ACCOMPLISHED CABIN PRESSURE LEAK TEST PER MM 05-51-91. LEAK TEST GOOD. 2L72 4F RTA16WE 20050928000692005092800069NM 2005 9 28 05FDEA03054 120050922A5311 FRAME BOEING727 727232 1384082NM BS 680 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 FORWARD CARGO BAY, FRAME IS DENTED ON IB FLANGE AT BS 680 STRINGER 25 RT. REPAIRED FRAME AT BS 680 STR 25R PER SRM 51-40-3. 2L73 4F A3WE 20050928000702005092800070NM 2005 9 28 05FDEA03055 120050922A5311 FRAME BOEING727 727232 1384082NM BS 660 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 DENT IN FRAME AT BS 660 STR 24L. REPAIRED DENT IN FRAME AT B.S. 660 STR 24L PER SRM 51-40-3. 2L73 4F A3WE 20050923001172005092300117NM 2005 9 23 PIDA20050123 120050907A5315 FLOORBEAM BOEING737 737228 13844AGNM BS 312 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 FLOORBEAM AT BS 312 HAS CORROSION ON UPPER SURFACE FROM BL 0 TO RBL 8. REPLACED TEE CAP FROM RBL 23 TO LBL 18 PER SRM 53-10-9. 2L72 4F RTA16WE 20050923001192005092300119NM 2005 9 23 PIDA20050125 120050830A5320 INTERCOSTAL BOEING737 737228 13844AGNM BS 294-312 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 INTERCOSTAL AT LBL 11 FROM BS 294 TO BS 312 HAS CORROSION AT CLIP NUT HOLES. REPLACED INTERCOSTAL PER SRM 51-10-1. 2L72 4F RTA16WE 20050923001202005092300120NM 2005 9 23 PIDA20050126 120050831A5320 CHANNEL BOEING737 737228 13844AGNM BS 307 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 HAT SECTION EXTRUSION AT BS 307 FROM LBL 11 TO LBL 39 HAS CORROSION AT CLIP NUT HOLES. REPLACED HAT CHANNEL PER SRM 51-10-1. 2L72 4F RTA16WE 20050923001222005092300122NM 2005 9 23 05FDEA03038 120050921A5315 FLOORBEAM BOEING727 727232 1384082NM BS 1148 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 UPON REMOVAL OF BL "0" TENSION STRAP ON FEDEX CARD, FOUND CORROSION ON LOWER FLANGE OF FLOORBEAM AT BS 1148, WL200, BL'0'. REPAIRED FLOORBEAM AT B.S. 1148, BLO, WL 200 PER SRM 53-10-8. 2L73 4F A3WE 20050923001242005092300124NM 2005 9 23 05FDEA03040 120050921A5512 PANEL BOEING727 727227 1384078NM HORIZONTAL STAB GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 RT HORIZONTAL STABILIZER UPPER T/E PANEL INNER SIDE IS GOUGED JUST 3 INCHES I/B OF NR 7 RIB. REPAIRED PER E.A. 7-5510-91362. 2L73 4F A3WE 20050923001262005092300126EU 2005 9 23 AWXA200501088 120050921A335032145410 POWER SUPPLY AIRBUS320 A320232 3930326EU EMERGENCY LIGHT INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28652AW2526025250 953 ATL - EEL - DURING 8 DAY CHECK DISCOVERED THE AFT GALLEY EMERGENCY POWER SUPPLY WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT GALLEY EMERGENCY POWER SUPPLY IAW AIRBUS 320 AMM 33-51-38-000-001. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA28NM 20050923001282005092300128NM 2005 9 23 AWXA200501090 120050921A335020121 CHARGER BOEING737 7373G7 1384595NM EMERGENCY LIGHT INOPERATIVE A AWXAO OTHER O OTHER TXTAXI/GRND HDL 1 WP28160AW 23782 SAN - EEL - ON GROUND DISCOVERED EMERGENCY LIGHTS AT SEATS 18-23L INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY CHARGER IN THE LEFT GALLEY OVERHEAD PANEL. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20050923001302005092300130NE 2005 9 23 AWXA200501092 220050919A7320550MK1 FMU AIRBUSA319 A319132 3930340NM IAE V2500 V2500A1 NE NR 2 ENGINE MALFUNCTIONED A AWXAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 WP28819AW1790517905 1395 CREW REPORTED THAT DURING TAKE OFF, NR 2 ENGINE SPOOLED MUCH SLOWER THAN NR 1. ABORTED TAKEOFF AT 30 KNOTS & RETURNED TO GATE WITHOUT FURTHER INCIDENT. MX R & R LP/HP FUEL PUMP IAW AMWEST TASK CARD R5M73304. ALSO R & R FUEL FLOW METERING UNIT IAW AWA TASK CARD R5M73308. OPS TESTS GOOD. RECIEVED FUEL PUMP ASSY FOR REPAIR/OVERHAUL. REMOVAL NOT CONFIRMED. VENDOR DID REPLACED ERODED SEAL, PN 5910350. REPAIRED/OVERHAULED & INSPECTED UNIT IAW CMM 73-18-41. DID NOT CONFIRM FAULT FOR FMU REPLACED. FOUND NO FAULTS WITH UNIT. UNIT FULLY DIASSEMBLED, CLEANED, INSPECTED & ALL SEALS, GASKETS ETC REPLACED UPON REASSEMBLY. ALL WORK PERFORMED IAW CMM 73-28-08. 2L72 4F4 FRTA28NM E311NE 20050923001322005092300132NM 2005 9 23 05FDEA03041 120050922A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 UPPER CARGO, SEAT TRACK LBL 8 CORRODED AT STA 1551. SEAT TRACK REPAIRED AS PER SRM 53-70-00 VOLUME I FIGURE 1. CLASSIFIED AS MAJOR REPAIR PER GMM 6-2-100. 2L73 4F RTA22WE 20050923001342005092300134NM 2005 9 23 05FDEA03043 120050922A5313 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 CENTER CARGO, LONGERON CORROSION FOUND AT STA 1701 R50. REMOVED AS PER SRM 51-21-01 VOLUME II. 2L73 4F RTA22WE 20050923001362005092300136NM 2005 9 23 PIDA20050127 120050919A5320 INTERCOSTAL BOEING737 737228 13844AGNM BS 320 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 INTERCOSTAL AT BS 320 FROM RBL 11 TO RBL 30 HAS CORROSION ON LOWER SIDE AT CLIP NUT HOLES. REPLACED DAMAGED SECTION OF INTERCOSTAL PER SRM 51-10-1. 2L72 4F RTA16WE 20050923001382005092300138NM 2005 9 23 PIDA20050129 120050907A53206545834260 INTERCOSTAL BOEING737 737228 13844AGNM BS 312-328 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 INTERCOSTAL AT LBL 11 FROM BS 312 TO BS 328 HAS CORROSION AT CLIP NUT HOLES. REPLACED INTERCOSTAL PER SRM 51-10-1. 2L72 4F RTA16WE 20050923001402005092300140NM 2005 9 23 PIDA20050132 120050902A53206546812169 INTERCOSTAL BOEING737 737228 13844AGNM BS 947-967 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 INTERCOSTAL AT LBL 18 FROM BS 947 TO BS 967 HAS CORROSION. REPLACED INTERCOSTAL PER SRM 51-10-1. 2L72 4F RTA16WE 20050923001422005092300142NM 2005 9 23 PIDA20050120 120050920A5311 FRAME BOEING737 737228 13844AGNM BS 360 CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 FRAME CRACKED AT BS 360 ABOVE STR 9 RT AT RAIL ATTACHMENT. REPAIRED PER SRM 53-10-4. 2L72 4F RTA16WE 20050923001442005092300144NM 2005 9 23 PIDA20050119 120050919A5315 FLOORBEAM BOEING737 737228 13844AGNM BS 344 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 CORROSION AT SEVERAL CLIP-NUT HOLES ON UPPER SURFACE OF BS 344 FLOORBEAM. REPAIRED SECTION OF FLOORBEAM PER SRM 53-10-9. 2L72 4F RTA16WE 20050923001462005092300146NM 2005 9 23 PIDA20050122 120050919A53156546568610 FLOORBEAM BOEING737 737228 13844AGNM BS 1016 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 FLOORBEAM AT BS 1016 HAS CORROSION AT FLOORBOARD ATTACH HOLES FROM LBL 5 TO LBL 35. FLOORBEAM PREVIOUSLY REPAIRED WITH A ONE PIECE REPLACEMENT TEE CAP FROM FRAME TO FRAME. REPLACED DAMAGED SECTION OF FLOORBEAM T-CAP PER EA 53-246. 2L72 4F RTA16WE 20050928000712005092800071NM 2005 9 28 05FDEA03056 120050922A5311 FRAME BOEING727 727232 1384082NM BS 660 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 DENT IN FRAME BETWEEN STR 24R-25R BS 660. REPAIRED DENT IN FRAME AT B.S. 660, STR 24R-25R PER SRM 51-40-3. 2L73 4F A3WE 20050928000722005092800072NM 2005 9 28 05FDEA03057 120050922A5311 FRAME BOEING727 727232 1384082NM BS 520 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 FWD CARGO BAY, FRAME IS DENTED ON IB FLANGE AT BS 520 BETWEEN STR 22 LT AND 25 LT. REPAIRED PER SRM 53-10-1, 51-30-2, 51-40-3 FIG 1 MAJOR REPAIR. 2L73 4F A3WE 20050928000742005092800074NM 2005 9 28 05FDEA03059 120050922A5311 FRAME BOEING727 727232 1384082NM BS 560 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 FORWARD CARGO BAY, FRAME IS DENTED ON IB FLANGE AT BS 560 BETWEEN STRINGER 24 LT AND 25 LT. REPAIRED FWD CARGO BAY FRAME AT BS 560 BETWEEN STR 24LT & 25LT PER SRM 51-40-3. 2L73 4F A3WE 20050928000752005092800075NM 2005 9 28 05FDEA03060 120050922A5311 FRAME BOEING727 727232 1384082NM BS 660 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION, FWD CARGO BAY (C53-111-01(2)) ON FRAME BS 660 BETWEEN BL 0 AND STRINGER 38RT (ON FWD SIDE OF FRAME). REPAIRED FRAME AT BS 660 BETWEEN BL0 AND STR 28RT IAW SRM 51-40-2. 2L73 4F A3WE 20050928000772005092800077NM 2005 9 28 05FDEA03062 120050922A5330 SKIN BOEING727 727225 1384077NM ZONE 100 MISREPAIRED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25464FE 21288 EXTERNAL SKIN DOUBLER AT STA 715-720A AND STRINGER 28R REQUIRES EVALUATION. DOUBLER FOUND TO NOT CONFORM TO SRM STANDARDS. REMOVED, FABRICATED, ALODINED, PRIMED AND INSTALLED NEW DOUBLER AT STA 715 TO 720A BEWEEN STRINGERS 27R AND 28R ALL C/W IAW FX B727 SRM 53-30-3,51-30-2 AND 51-10-2. 2L73 4F A3WE 20050928000782005092800078NM 2005 9 28 05FDEA03063 120050922A5347 SEAT TRACK BOEING727 727225 1384077NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25465FE 21289 SEAT TRACK INBOARD FLANGE HAS CORROSION BS 700 TO BS 740 LBL 24. 2L73 4F A3WE 20050928000802005092800080EA 2005 9 28 VNAA0509012 120050920A2710 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE AILERONS FALSE ACTIVATIONA VNAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL05229PS 7898 DURING TAKEOFF ROLL CONFIG AILERON WARNING MESSAGES ILLUMINATED AND SOUNDED. A REJECTED TAKEOFF WAS PERFORMED. THE CREW RESET THE CONTROLS AND REPORTED THE TAKEOFF CONFIG SYSTEM OPERATIONALLY CHECKED GOOD. AFTER THE BRAKES COOLED, THE CREW CONTINUED THE FLIGHT WITH NO FURTHER PROBLEMS. 2L72 4F4 FRTA21EA E15NE 20050928000812005092800081NE 2005 9 28 QXEA200501261 220050925A7310 FITTING CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE FUEL LINE LEAKING A QXEAO OTHER K FLUID LOSS NRNOT REPORTED 1 NM09609QX 10031 DEN - NR 2 ENGINE FUEL LEAK. MAINTENANCE TIGHTENED THE LINE FITTING AT THE VG SLAVE ACTUATOR. OPERATIONAL CHECKS GOOD, NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050928000822005092800082NM 2005 9 28 SCNA05005 120050922A3242 WARNING LIGHT BOEING737 7378Q8 13844BXNM BRAKE DISARM ILLUMINATED A SCNAO OTHER J WARNING INDICATION CRCRUISE 1 GL15801SY 30332 PILOT DISCOVERED AUTO BRAKE DISARM LIGHT ILLUMINATED. MAINTENANCE PLACED ON MEL 32-7 AND PERFORMED FIM TASK 32-42 TASK 828. DETERMINED FAULT TO BE INTERMITTENT. REMOVED MEL 32-7. 2L72 4F RTA16WE 20050928000842005092800084EU 2005 9 28 UPS05145481 120050912A5420A5451506320400 ANGLE AIRBUSA300 A300F4622R 3930360EU NR 2 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01125UP 0809 NR 2 PYLON LOWER AFT DOUBLER ANGLE CRACKED. REMOVED AND REPLACED LOWER AFT DOUBLER ANGLE ON NR 2 PYLON IAW A300 SRM 51-40-00. 2L72 4F RTA35EU 20050928000872005092800087EA 2005 9 28 VTZA200500190 120050923A5320 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA BS 640 CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27943BR 7363 ENGINE SUPPORT BEAM IS CRACKED .250" IN LENGTH AT FS 640 AND LBL 8.5. 2L72 4F RTA21EA 20050928000882005092800088NE 2005 9 28 ARWA20050910 220050918A7200 ENGINE DOUG DC10 DC1030 3023501WP GE CF6 CF650C2 30018NE NR 1 MALFUNCTIONED A ARWAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SO19526MD 46998 ON TAKEOFF, NR 1 ENGINE ADVANCED TO 40 PERCENT N1 AND WOULD NOT GO BEYOND, ALL OTHER PARAMETERS NORMAL. ENTERED ON DMI NR19537 AS PER MEL 77-11-1 CAT "B" REFER TO DDG 77-1 C/W. PERFORMED NR 1 ENGINE RUN-UP IN ACCORDANCE WITH M/M 71-00-00. FOUND N1 INDICATION OPERATING WITHIN LIMITS IN ACCORDANCE WITH M/M 77-11-01. COULD NOT DUPLICATE FAILURE. ALL OTHER PARAMETERS NORMAL. CLEARED DMI 19535 - LOG PAGE 115870. 2L73 4F4 F A22WE E23EA 20050928000892005092800089SO 2005 9 28 C2XA05SH114 120050920A533014520554001 SKIN EMB 145 EMB145LR 3260212SO FR 19A-20 DENTED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713992 145284 SHV - DURING C-CHECK, EXTERNAL FUSELAGE HAS A DENT BETWEEN FR 8-19A, STRINGER 11L-12L. MAINTENANCE REPAIRED EXTERNAL FUSELAGE DENT BETWEEN FS 18-19A, STRINGER 11L-12L IAW EC5330-01503. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050928000912005092800091WP 2005 9 28 ARWA20050911 120050920A77979015M71PD3 WIRE HARNESS DOUG DC10 DC1010 3022110WP EGT LEAD DAMAGED A ARWAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO1968041 46900 NR 2 EGT FAILED IN FLIGHT. REMOVED AND REPLACED EGT LEAD JUNCTION IN ACCORDANCE WITH M/M 77-21-02. SYSTEM TESTED IN ACCORDANCE WITH M/M 77-21-01 AND 77-21-00; FOUND NORMAL. 2L73 4F A22WE 20050928000922005092800092NM 2005 9 28 05FDEA03065 120050922A5320 INTERCOSTAL BOEING727 727225 1384077NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 AFT PIT INTERCOSTAL AT STA 950B STRINGER 28R IS CRACKED. REMOVED AND REPLACED INTERCOSTAL AT FS 950B, STRINGER 28R, IAW B727 SRM 51-30-2, IAW B727 MM 51-20-013-7. 2L73 4F A3WE 20050928000952005092800095EA 2005 9 28 QXEA200501262 120050901A2840 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA FUEL SYSTEM ILLUMINATED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09602QX 10010 DEN - ON FLIGHT 4327, CLIMBING AT 8,000 FEET RECEIVED A FUEL CHANNEL 1 AND 2 FAIL CAUTION MESSAGE. RETURNED TO FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE CLEARED THE FAULT PER THE FIM TASK 28-40-00-810-804-A01. NO FURTHER DEFECTS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2L72 4F RTA21EA 20050928000962005092800096NM 2005 9 28 SWAA052909 120050924A53116546558 FRAME BOEING737 7373H4 1384600NM BS 907 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29618WN 28034 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L TO STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050928001012005092800101NM 2005 9 28 SWAA052899 120050924A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 947 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CORRODED AT BS 947, STR 26L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050928001022005092800102NM 2005 9 28 SWAA052900 120050923A27316545166 ROD END BOEING737 7373H4 1384600NM RT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED C2 CHECK, RT ELEVATOR TAB FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB ROD ENDS PER MM. 2L72 4F RTA16WE 20050928001042005092800104NM 2005 9 28 SWAA052902 120050922A53306545776 SKIN BOEING737 7373H4 1384600NM BS 967 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29335SW 23939 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 967, STR 21L. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050928001052005092800105NM 2005 9 28 SWAA052903 120050923A53306545774 SKIN BOEING737 7373H4 1384600NM 727E CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 19R. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050928001072005092800107NM 2005 9 28 SWAA052905 120050924A3350207377 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29436WN 32456 DURING SCHEDULED MV2 CHECK, FOUND EEPLS TRACK LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20050928001082005092800108NM 2005 9 28 SWAA052906 120050924A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29462WN 32466 EEPLS TRACK COVER WORN AT FWD END. REMOVED AND REPLACED COVER PER MM. 2L72 4F RTA16WE 20050928001092005092800109NM 2005 9 28 SWAA052907 120050925A53306545776 SKIN BOEING737 7375H4 138449DNM BS 944 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29522SW 26564 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 944, STR 24L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050928001102005092800110NM 2005 9 28 SWAA052908 120050924A53116545808 FRAME BOEING737 7373H4 1384600NM BS 294.5 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29618WN 28034 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 294.5, L1 DOOR UPPER CUTOUT. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20050928001112005092800111GL 2005 9 28 CHQA200500168 220050917A7200AE3007A1P ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 2 UNSERVICEABLE A CHQAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL11579RP9625 14500871 CAE312008 FLIGHT 6234 - CMH-FLL - LAVATORY SMOKE INDICATION DURING GEAR RETRACTION. PERFORMED QRH CHECKLIST AND RETURNED TO FIELD. REMOVED AND REPLACED NR 2 ENGINE IAW JC CE720001. OPS CHECK GOOD. NO LEAKS NOTED. 2L72 4T4 FRTT00011ATTE6CH 20050928001122005092800112NM 2005 9 28 SWAA052910 120050924A53116546550 FRAME BOEING737 7373H4 1384600NM BS 787 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29618WN 28034 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R TO STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050928001132005092800113NM 2005 9 28 SWAA052911 120050924A55516551524 FITTING BOEING737 7373H4 1384600NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29618WN 28034 DURING SCHEDULED D-CHECK, FOUND LT & RT HORIZONTAL STAB FITTING LUG FACES CORRODED. REPAIRED LUG FACES PER SRM. 2L72 4F RTA16WE 20050928001152005092800115NM 2005 9 28 SWAA052913 120050924A53116546550 FRAME BOEING737 7373H4 1384600NM BS 787 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29618WN 28034 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L TO STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050928001172005092800117NM 2005 9 28 SWAA052915 120050924A53116520723 FRAME BOEING737 7373H4 1384600NM CARGO DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29618WN 28034 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR AFT FRAME, BOTTOM DOOR STOP CUTOUT. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20050928001222005092800122NM 2005 9 28 SWAA052920 120050923A53306545776 SKIN BOEING737 7373Q8 1384670NM BS 907 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 907, STR 25L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050928001232005092800123NM 2005 9 28 SWAA052921 120050923A3350D71702001 BATTERY PACK BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29710SW 27844 DURING SCHEDULED RON CHECK, FOUND FWD GALLEY EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050928001242005092800124 2005 9 28 SWAA052922 420050919A256565C16820 HOOK BOEING737 7377H4 1384404NM L1 DOOR GIRT BARLOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29742SW 29278 DURING SCHEDULED RON CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED HOOK PER MM. 2L72 4F RTA16WE 20050928001252005092800125NM 2005 9 28 SWAA052923 120050924A3350D71701100 BATTERY PACK BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29749SW 29801 DURING SCHEDULED RON CHECK, FOUND LT FWD EMERGENCY EXIT BULLNOSE LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050928001262005092800126WP 2005 9 28 IXXA05RNG053S 120050907A5350 TAIL CONE DOUG DC8 DC872 302199BWP FUSELAGE DENTED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX 46013 DURING INSPECTION CHECK, FOUND SOME DENTS ON LT FUSELAGE TAIL CONE STA`S 1746, 1745 AND 1754. SKIN DENTS WILL BE REPAIRED IAW EWO ATI-53-013 AND FAA FORM 8110-3 MUST BE ISSUED APPROVING THIS REPAIR. 2L74 4F RT4A25 20050928001282005092800128WP 2005 9 28 IXXA05RNG057S 120050906A5730 SKIN DOUG DC8 DC872 302199BWP LT WING CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX 46013 DURING INSPECTION CHECK, FOUND A CRACK ON TOP PANEL PLATING AT CENTER SPAR AND STA XRS 74.869 LT. DAMAGE WILL BE REPAIRED IAW EWO ATI 57-040 AND SRM 57-2-1 FIG 17. 2L74 4F RT4A25 20050928001342005092800134EA 2005 9 28 COMA0570103 120050916A4900WE388007703 APU CNDAIRCL600 CL6002C10 1390015EA EMPENNAGE FAULTY A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01367CA4684 10069 FLIGHT 4989 - RECEIVED A FORWARD LAVATORY SMOKE WARNING MESSAGE DURING TAKEOFF ROLL, FLIGHT RETURNED TO GATE. REPLACED THE APU. 2L72 4F RTA21EA 20050928001352005092800135EA 2005 9 28 COMA0560514 120050921A2150 ACM CNDAIRCL600 CL6002B19 1900309EA LEFT MALFUNCTIONED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01912EV 7728 FLIGHT 5263 - LEFT PACK HIGH PRESSURE CAUTION. CND, FOUND NO DEFECT WITH THE LT AC SYSTEM. 2L72 4F RTA21EA 20050928001372005092800137EA 2005 9 28 COMA0560516 120050921A5312601R32026 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA RT WHEEL WELL CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01934CA27377 7042 WHILE PERFORMING TASK INS-2-2-27L0005 ITEM NR 6, CLEANING OF THE RIGHT REAR AILERON QUADRANT LOCATED ON THE AFT WALL OF THE MLG WHEEL WELL, DISCOVERED A CRACK ON THE SEMI-PRESSURE BULKHEAD FS 559.00, RBL 23L-23R. PERFORMED REO 601R-53-41-344. 2L72 4F RTA21EA 20050928001382005092800138SO 2005 9 28 CHQA200500166 120050921A2611FDS765A2 SMOKE DETECTOR EMB 145 EMB145LR 3260212SO LAVATORY FALSE INDICATIONA CHQAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL11574RP 14500845 FLIGHT 6378 - CMH-RSW - LAVATORY SMOKE WARNING PRESENTED ON EICAS (AND ASSOCIATED MASTER WARNING) AT 400 FEET AGL ON TAKEOFF. FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN AND CONFIRMED THE LAVATORY SMOKE DETECTOR WAS GOING OFF. DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. AFTER APPROXIMATELY 3 MINUTES, THE "LAV SMOKE" EICAS WARNING WENT AWAY. THE FLIGHT ATTENDANT REPORTED THAT THE SMOKE IN THE CABIN WAS BEGINNING TO DISSIPATE SLOWLY. NO EVACUATION WAS REQUIRED. MAINTENANCE REMOVED AND REPLACED THE LAVATORY SMOKE DETECTOR AND PERFORMED A GROUND RUN AND TEST FLIGHT. ALL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20050928001402005092800140EA 2005 9 28 QXEA200501258 120050923A2150 A/C PACK CNDAIRCL600 CL6002C10 1390015EA RIGHT MALFUNCTIONED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09610QX 10033 DEN - ON TAXI OUT FOR FLIGHT 4177, RECEIVED A RIGHT AIR CONDITIONING PACK FAULT. RETURNED TO THE GATE. MAINTENANCE PLACED ON MEL. MEL CLEARED IN GEG BY PERFORMING FIM TASK 21-51-20-810-802-A01. OPERATIONAL CHECKS GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20050928001412005092800141SO 2005 9 28 FFKA2005105 120050921A3220452334 ROD END PIPER PIPER PA34 PA34200T 7103406SO DOWNLOCK LINK BROKEN B FFKAO OTHER O OTHER TXTAXI/GRND HDL 1 SO058076N9692 60 347970487 DURING COMPLIANCE WITH AD 2005-13-16 THE DOWN LOCK LINK ASSEMBLY WAS INSPECTED AND FOUND TO BE AIRWORTHY AT THAT TIME AND WAS REINSTALLED INTO THE AIRCRAFT (THIS PART IS NOT PART OF AD2005-13-16 INSPECTION). AFTER 60 HRS OF OPERATION THE PART IN QUESTION FAILED, DUE TO UNKNOWN REASONS. 1L72 3O A7SO 20050928001442005092800144CE 2005 9 28 DXTA200500984 120050925A3240 BRAKE CESSNA500 560CESSNA 2076750CE MLG MALFUNCTIONED E DXTAO OTHER O OTHER NRNOT REPORTED 1 GL07331QS 5600331 BRAKING PRESSURE ERRACTIC , BRAKES SEEM TO CATCH AND RELEASE, PRESSURE INCREASE AND DECREASE, FELT IN PEDALS. 2L72 4F RTA22CE 20050928001472005092800147NE 2005 9 28 QXEA200501260 220050924A72304114T15P02 FAN BLADE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE NR 1 ENGINE VIBRATION A QXEAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 NM09602QX8202 526 10010 GEE965305 DEN - ON FLIGHT 4177, DURING CLIMB, NR 1 ENGINE FAN VIBRATIONS WERE IN THE YELLOW ARC, WITH POWER REDUCTION, THE READING WAS 2.1. AIRCRAFT RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE REPLACED THE N1 FAN BLADES. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050928001482005092800148NM 2005 9 28 05FDEA03103 120050925A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 HORIZ STAB LT BARREL NUT BORE NR 34 FOUND WITH CORROSION. REWORK/ REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 18. MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20050928001502005092800150NM 2005 9 28 P5CA0501401 120050922A5720 SUPPORT BEAM BOEING747 747283B 1384867NM LT WING CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 EA15921FT 21575 LEFT WING TRAILING EDGE SUPPORT BEAM UPPER CHORD CRACKED (APPROX 2 INCHES) AT WS 528.20, WBL 235.20. 2L74 4F A20WE 20050928001512005092800151NM 2005 9 28 P5CA0501402 120050922A575565B0225041 PANEL BOEING747 747283B 1384867NM SPOILER CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 EA15921FT 21575 LEFT WING NR 3 O/B SPOILER HAS A CRACK AT UPPER SURFACE (NEAR HINGE FITTING SUPPORT). REMOVED AND REPLACED NR 3 SPOILER PER MM 27-61-02. 2L74 4F A20WE 20050928001522005092800152NM 2005 9 28 PIDA20050140 120050923A534365C25636517518 FITTING BOEING737 7373Y0 1384671NM NLG TRUNNION CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05373PA 23749 CORROSION FOUND IN THE BEARING CUP OF THE NLG TRUNNION FITTING ASSEMBLY BORES AT THE LEFT AND RIGHT SIDES. REPAIRED FITTING ASSEMBLIES PER EA 53-259A. 2L72 4F RTA16WE 20050928001552005092800155NM 2005 9 28 SWAA052925 120050923A53306545765 SKIN BOEING737 7373H4 1384600NM BS 514.50 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 514.50, STR 15L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050928001562005092800156NM 2005 9 28 SWAA052926 120050925A335065C53829 CHARGER BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29341SW 24091 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM. 2L72 4F RTA16WE 20050928001582005092800158NM 2005 9 28 SWAA052928 120050926A3350207377 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29444WN 29839 LT OVERWING LOWER EMERGENCY EXIT LIGHT LENS COVER MISSING. INSTALLED LENS COVER PER MM. 2L72 4F RTA16WE 20050928001602005092800160NM 2005 9 28 SWAA052930 120050923A53306545775 SKIN BOEING737 7375H4 138449DNM BS 865 WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN WORN AT BS 865, UNDER DORSAL FIN BLADE SEAL. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050928001612005092800161NM 2005 9 28 SWAA052931 120050926A534065C27314 STRINGER CLIP BOEING737 7375H4 138449DNM BS 348 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29506SW 24183 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 348, STR 16L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20050928001632005092800163NM 2005 9 28 SWAA052933 120050926A55516551524 FITTING BOEING737 7373H4 1384600NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 DURING SCHEDULED D CHECK, FOUND LT AND RT HORIZONTAL STAB ATTACH FITTING LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER. 2L72 4F RTA16WE 20050928001642005092800164NM 2005 9 28 SWAA052934 120050926A53116546526 FRAME BOEING737 7373H4 1384600NM BS 400 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29618WN 28034 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L TO STR 9L AND STR 8R TO STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050928001662005092800166EA 2005 9 28 QXEA200501259 120050924A2760 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA SPOILERS FALSE ACTIVATIONA QXEAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 NM09607QX 10024 TUL- ON TAXI OUT FOR FLIGHT 4202, AFTER PLACING PITOT HEAT TO ON, RECEIVED A SPOILER STAB FAULT AND A RUDDER LIMIT FAULT. RETURNED TO THE GATE. MAINTENANCE PERFORMED A SSCU SELF TEST WITH NO FAULTS. CHECKED THE PITOT PROBES AND STATIC PORTS AND MOISTURE TRAPS. NO FAULTS FOUND. BITE CHECKED COMPUTERS NO DEFECTS NOTED. OPERATIONAL CHECKS GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20050928001712005092800171WP 2005 9 28 IXXA05RNG051S 120050907A5330 SKIN DOUG DC8 DC872 302199BWP BS 460 MISREPAIRED B IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW11721CX 46013 DURING INSPECTION CHECK, FOUND A IMPROPER REPAIR ON SKIN STA 460 LONGERON 28-29 RT. PERMANENT REPAIR WILL BE MADE IAW SRM 53-2-1 FIGURE 7 AND EWO ATI-53-012. THIS REPAIR CONSTITUTES A MAJOR REPAIR. 2L74 4F RT4A25 20050928001722005092800172WP 2005 9 28 IXXA05RNG062S 120050912A5330 SKIN DOUG DC8 DC872 302199BWP BS 1160-1180 CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX 46013 DURING INSPECTION CHECK, FOUND A CORROSION ON INTERNAL SKIN OF PASSENGER WINDOW STA 1160-1180, LT. DAMAGE WILL BE REPAIRED IAW EWO ATI-53-020 AND SRM 53-2-0 FIGURE 22A, TR-53-170. 2L74 4F RT4A25 20050928001732005092800173WP 2005 9 28 IXAA05RNG058S 120050908A5744 FITTING DOUG DC8 DC872 302199BWP RT WING CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX 46013 DURING MAINTENANCE CHECK, FOUND RT OUTBOARD FLAP, INBOARD FLAP HINGE FITTING STA XF 219.459 CRACKED. DAMAGE WILL BE REPAIRED IAW EWO ATI-57-041 AND FAA FORM 8110-3 MUST BE ISSUED APPROVING THIS REPAIR. 2L74 4F RT4A25 20050928001742005092800174WP 2005 9 28 IXXA05RNG054S 120050907A5730 SKIN DOUG DC8 DC872 302199BWP RT WING CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX 46013 DURING INSPECTION CHECK, FOUND A CRACK (1.5 INCHES) ON TOP PANEL PLATING OUTBOARD OF STA XCW 69.5 AND STRINGER 1 RT. DAMAGE WILL BE REPAIRED IAW EWO ATI 57-039 AND SRM 57-2-1 FIG 18A. 2L74 4F RT4A25 20050928001762005092800176WP 2005 9 28 IXXA05RNG056S 120050904A5340 FITTING DOUG DC8 DC872 302199BWP BS 857.125 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX 46013 DURING INSPECTION CHECK, FOUND A CRACKED FITTING LONGERON 24 STA 857.125 BATH TUB RT. REPAIR WILL BE MADE IAW EWO ATI 53-015 AND SRM 53-2-2 FIGURE 5, TEMPORARY REVISION 53-123. 2L74 4F RT4A25 20050928001772005092800177EA 2005 9 28 QXEA200501248 120050915A2820 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA FUEL SYSTEM ILLUMINATED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09615QX 10065 PDX - ON FLIGHT 2507, DURING TAXI OUT, RECEIVED A AUTO CROSSFLOW INHIBIT CAUTION MESSAGE. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE RESET PER THE SERVICE LETTER 28-007C. OPERATIONAL CHECKS GOOD AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2L72 4F RTA21EA 20050928001782005092800178NM 2005 9 28 SWAA052936 120050926A531165C25228 FRAME BOEING737 7373H4 1384600NM BS 727D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29618WN 28034 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R TO STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050928001802005092800180CE 2005 9 28 DXTA200500972 120050916A215073838433 ACM CESSNA750 750 2076810CE UNSERVICEABLE E DXTAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL07919QS2030 7500224 UNABLE TO CONTROL TEMP RISE FOR CABIN PACK. SMOKE ENTERED CABIN ON LEFT SIDE OF CABIN AND TAIL CONE AREA SMELLED LIKE SOMETHING HAD BEEN BURNING. ACM WOULD NOT TURN. REMOVED AND INSTALLED AN OVERHAULED ACM. OPS AND LEAK CHECKS GOOD AT THIS TIME ALL WORK DONE IAW CESSNA 750 MM CHAPTER 21-51-00. 2L72 4J RTT00007WI 20050928001812005092800181CE 2005 9 28 DXTA200500976 120050919A3240 BRAKE CESSNA500 560CESSNA 2076750CE MLG MALFUNCTIONED E DXTAO OTHER O OTHER LDLANDING 1 GL07395QS 5600496 UPON LANDING, EXPERIENCED "HARD PEDALS" AND NO BRAKES FOR ABOUT 6 SECONDS. JUST BEFORE USING EMER BRAKING THE BRAKES SUDDENLY GRABBED VIOLENTLY. AFTER THAT THEY WORKED NORMALLY. GAINED ACCESS TO ANTI-SKID FAULT INDICATORS IN NOSE BAGGAGE AREA. FOUND NO FAULT INDICATIONS. INSPECTED BRAKE ASSEMBLIES FOR ANY DEFECTS, NONE NOTED. PERFORMED SEVERAL BUILT-IN BITE TESTS. ALL TESTS SATISFACTORY. PERFORMED TAXI CHECK AND OPERATIONAL CHECK OF BRAKE AND ANTI-SKID CONT SYSTEM. NO DEFECTS NOTED. ALL WORK PERFORMED IAE CE560 MM CH 32-42-00. 2L72 4F RTA22CE 20050928001842005092800184NM 2005 9 28 SWAA052938 120050921A5320BAC15171489 STRUCTURE BOEING737 7373H4 1384600NM COCKPIT FLOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29635SW 27708 DURING SCHEDULED C3 CHECK, FOUND COCKPIT FLOOR Z-CHORD CORRODED AT BS 270, BETWEEN LBL 54 TO RBL 54. MX FERRY TO DALLAS. REMOVED AND REPLACED Z-CHORD PER SRM. 2L72 4F RTA16WE 20050928001872005092800187 2005 9 28 SWAA052941 420050926A256563550101 SLIDE BOEING737 7377H4 1384404NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29724SW 27856 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20050928001882005092800188EA 2005 9 28 COMA0560521 120050923A2750860D10018ABCD CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01466CA278891442 7627 FLIGHT 5463- FLAPS FAIL CAUTION. REPLACED THE FECU. 2L72 4F RTA21EA 20050928001912005092800191SO 2005 9 28 C2XA05IA105 120050912A2730 ELEVATOR EMB 145 EMB145LR 3260212SO OUT OF RIG A C2XAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 SW2713949 145057 IAH - FLIGHT 2703, THE CREW REPORTED THAT THEY HAD INSUFFICENT TRAVEL ON THE ELEVATOR FOR ROTATION. THE CREW ABORTED THE TAKEOFF WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND ELEVATOR RIGGING WITH NO DEFECTS BEING NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050928001932005092800193NE 2005 9 28 ABXA050235 220050922A7200 ENGINE DOUG DC9 DC941 302207NWP PWA JT8 JT8D17 52049NE NR 1 DEFECTIVE A ABXAB EMER. DESCENT O OTHER DEDESCENT 1 GL23960AX1 47762 676190 LEFT ENGINE WOULD NOT SPOOL UP DURING APPROACH. WHEN THROTTLE WAS ADVANCED, ENGINE WOULD NOT START, COMPRESSOR STALLED. EMERGENCY DECLARED. LANDED WITH ENGINE AT IDLE POWER. SERVICED FUEL CONTROL UNIT WITH 6 ML OF SILICON OIL IAW P&W JT8D-11 MM 73-21-01. LUBRICATED PRBC IAW JT8D MM 75-30-00. RAN ENGINE AND BLEED, SCHEDULING CHECKED NORMAL. NR 1 ENGINE ACCELERATION MATCHED NR 2 ENGINE. NOTE: PROBLEM REPEATED ON SYSTEM OPS DATE OF 9-23-05. ON L/P 32844-82/1&2, DELAY REPORT 14782, REPLACED NR 1 ENGINE. 2L72 4F4 F A6WE E2EA 20050928001942005092800194NM 2005 9 28 2005UALA00994 120050917A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE BS 600 DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29549UA 25397 SKIN DENT STA 600, RBL 8. REMOVED SKIN DAMAGE, INSTALLED DOUBLER AND TRIPLER REPAIR PER TIMCO REO-G10977B AND EVA- 50640 WITH FAA APPROVAL VIA 8100-9. 2L72 4F4 FRTA2NM E17NE 20050928001952005092800195NM 2005 9 28 2005UALA00995 120050916A2910 HYDRAULIC SYSTEM BOEING757 757222 1384956NM PWA 2037 PW2037 NE MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29516UA 24860 RETURNED TO FIELD DUE TO HYDRAULIC PROBLEMS. FOUND HYDRAULIC PRESSURE LINE WITH STREAMING LEAK. REPLACED HOSE, REPLACED RETURN AND CASE DRAIN FILTERS, AND SERVICED SYSTEM TO FULL. LEAK CHECKED SAME. PRESSURE WASHED FUSELAGE BELLY AS REQUIRED. RETURNED AIRCRAFT TO SERVICE. 2L72 4F4 FRTA2NM E17NE 20050928001962005092800196NM 2005 9 28 2005UALA00996 120050916A2780 SLAT SYSTEM BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29676UA 30028 RETURNED TO HNL DUE TO A SLAT ASYMMETRY MESSAGE. 2L72 4F4 FRTA1NM E24NE 20050928001982005092800198NM 2005 9 28 2005UALA00998 120050916A335058781 LIGHT BOEING737 737322 1384676NM ROW 16 INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29330UA 24191 EEL LIGHTS INOP FROM ROW 16 AFT TO AND INCLUDING EEL STRIP IN FRONT OF AFT GALLEY CART STOWAGE COMPARTMENT. REPLACED FEEDER CABLE, PCN 560-0809, AND REPLACED EEL STRIP IN FRONT OF AFT GALLEY CART STOWAGE COMP, PCN 560-0857. 2L72 4F RTA16WE 20050928001992005092800199NM 2005 9 28 2005UALA00999 120050918A335020131A POWER SUPPLY BOEING737 737322 1384676NM ROW 12 INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29336UA 24240 EMERGENCY EXIT LIGHTS AFT OF SEAT ROW 12 ARE INOP. REPLACED BATTERY PACK 2L72 4F RTA16WE 20050928002002005092800200EU 2005 9 28 2005UALA01000 120050920A5313 STRINGER AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FR 54-55 CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29421UA 500 STRINGER 43L HAS CORROSION BETWEEN FS 54 AND FS 55. 2L72 4F4 FRTA28NM E40NE 20050928002012005092800201NM 2005 9 28 2005UALA01001 120050920A3350321454 BATTERY PACK AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29825UA 980 CABIN EMERGENCY LIGHT TEST FAILS: EPSU INT LOADS AFT L AND EPSU BATTERY R. REPLACED AFT EPSU 13WL PER MM 33-51-38 AND BATTERY PACK FOR RIGHT MID POWER SUPPLY. 2L72 4F4 FRTA28NM E40NE 20050929000032005092900003EU 2005 9 29 USAA200509008 120050924A5315 FLOORBEAM AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19115US 1171 FLOORBEAM CORRODED .5 X 7 INCH AT Y1292 BETWEEN FR 64 & FR 66. NO CORROSION LEVEL OR TASK. REMOVED CORRODED SECTION AND SPLICED IN A NEW BEAM SECTION PER SRM 51-72-11. 2L72 4F RTA28NM 20050929000052005092900005EU 2005 9 29 USAA200509006 120050923A5315 FLOORBEAM AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19115US 1171 FLOORBEAM AND R2 DOOR SILL CORRODED .20 X .5 X .60 INCH AT FR 67, STR 18. NO CORROSION LEVEL OR TASK. BLENDED AND TREATED CORROSION; FABRICATED AND INSTALLED REPAIR BATH TUB FITTING PER EA 96921. 2L72 4F RTA28NM 20050929000062005092900006NM 2005 9 29 05FDEA03081 120050924A5330 SKIN BOEING727 727200 138407ENM BS 227.8-237 MISREPAIRED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25483FE 21465 EXTERNAL REPAIR. 9.2 INCHES X 3 INCHES AT BS 227.8 - 237, STR. 26L REQUIRES EVALUATION. DETERMINE IF THE REPAIR IS MAJOR OR MINOR AND IF THE REPAIR IS IN ACCORDANCE WITH FAA APPROVED DATA. REMOVED & REPAIRED EXTERNAL REPAIR AT BS 227-8-37 STR 6L PER FED EX EA 7-5330-91366 PREVIOUS REPAIR NOT ACCOMPLISHED PER SRM, FOUND TO BE A MAJOR REPAIR. 2L73 4F RTA3WE 20050929000072005092900007NM 2005 9 29 05FDEA03083 120050924A5320 STRAP BOEING727 727200 138407ENM BS 229 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 N01609 WHILE WORKING FOUND INNER AND OUTER STRAPS CRACKED AT B.S 229 STR 26L. REPAIRED INNER & OUTER STRAPS AT BS 229 STR 26L IAW FED EX EA 7-5330-91366 FOUND TO BE A MAJOR REPAIR. 2L73 4F RTA3WE 20050929000082005092900008NM 2005 9 29 05FDEA03049 120050922A5330 SKIN BOEING727 727200 138407ENM BS 385-396 MISREPAIRED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25499FE 21018 EXISTING REPAIR BS 385 TO 396 STR 26L TO 27L 11"L X 7.5W. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPLACED REPAIR AT BS 385 TO 396, STR 26L-27L PER SRM 53-30-3. 2L73 4F RTA3WE 20050929000092005092900009NM 2005 9 29 05FDEA03084 120050924A5320 STRAP BOEING727 727200 138407ENM BS 229 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 WHILE WORKING FOUND INNER AND OUTER STRAPS CRACKED AT B.S 229 STR 26R. REPAIRED INNER AND OUTER STRAPS AT BS 229 STR 26R IAW FED EX EA 7-5330-91366 FOUND TO BE A MAJOR REPAIR. 2L73 4F RTA3WE 20050929000102005092900010NM 2005 9 29 BB05083 120050923A5610141T480013 WINDSHIELD BOEING757 757225 1384959NM COCKPIT CRACKED A USAAH DEACTIVATE SYST/CIRCUITS A FLAME/FIRE CRCRUISE 1 EA19601AU 22193 PHL FLT 30 EN-ROUTE LAS TO PHL - DURING THE FLIGHT, THE FORWARD LEFT WINDOW BEGAN TO CRACK AS FOUR SMALL AREAS OF ARCING BECAME APPARENT IN THE BOTTOM CENTER OF THE WINDOW. THE CREW SELECTED THE WINDOW HEAT OFF AND CONTINUED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT SIDE WINDSHIELD. OPERATIONALLY CHECKS OK. 2L72 4F RTA2NM 20050929000122005092900012NM 2005 9 29 AWXA200501105 120050925A2450941D3352 CIRCUIT BREAKER BOEING737 737301 1384611NM GENERATOR DAMAGED A AWXAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CLCLIMB 1 WP28326AW361611246 23258 CREW REPORTED "ON CLIMB OUT LEFT GENERATOR CAME OFF LINE FOLLOWED BY RIGHT GENERATOR. AC POWER LOST MOMENTARY. CYCLED BOTH GENERATORS. BOTH CAME BACK ON." CREW ELECTED TO RETURN TO PHX. LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. REMOVED AND REPLACED THE NR 1 ENGINE GENERATOR BREAKER, C801, AND THE NR 2 ENGINE GENERATOR BREAKER, C802, IAW AMWEST TASKCARD A8M24002. OPS CHECKS GOOD. VENDOR CONFIRMED FAILURE ON BOTH BUS TIE BREAKERS THAT WERE REPLACED. 2L72 4F RTA16WE 20050929000222005092900022 2005 9 29 WRNA200500021 420050916A2210 INDICATOR AIRBUS300 A300B4203 3930306EU ADI FAILED A WRNAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO05820SC 154 FLIGHT DIRECTOR FAIL FLAG IN VIEW ON CAPT ADI WHEN FLT DIR 1 OR FLT DIR 2 SELECTED. FLT DIR CMD BARS BIAS OUT OF VIEW. F/O ADI GYRO FAILED, UNABLE TO TRANSFER ATTITUDE INFO WITH INSTRUMENT SWITCHING. GYRO FLAG IN VIEW. BOTH LOGIC COMPUTER TRI-FOILS IN VIEW CODE 52. LANDING NORMAL. FLIGHT DIR FAIL FLAG ASSIGNED MEL 22-10-01 DMI NR 2464, PLACARD INSTALLED. F/O ADI R&R'D IAW 34-25-23, OP'S CHECK SATISFACTORY. R&R'D LOGIC COMPUTER NR 1 AND RESET LOGIC COMPUTER NR 2 IAW 22-13-34 OP'S CHECK SATISFACTORY. R&R'D ATTITUDE SWITCHING UNIT, OP'S CHECK SATISFACTORY IAW 34-25-35. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA35EU 20050930000012005093000001CE 2005 9 30 DJFA2005138 120050911A21505861109 COOLING TURBINE BEECH MU300 400A 1155402CE ACM DRAGGING E DJFAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 EA23740TA RK123 10 MINS AFTER T/O, SMOKY ELECTRICAL ODOR NOTICED. ODOR COMING FROM RT COCKPIT. NO SMOKE OR FIRE SEEN. DONNED O2 MASKS. RETURNED W/O INCIDENT. AFTER LANDING ODOR DISSIPATED. MX INSP CONNECTOR & WIRING. NO SIGNS OF HEAT OR ARCING. A/C POWERED FOR 5 HRS, NO SMOKE OR OVERHEATING. RETURNED TO SERVICE. 12 SEPT 2005, BURNING ODOR FROM WINDOW VENT. O2 MASKS DONNED & A/C RETURNED. ODOR LIKE BURNED RUBBER, ABSENT ON TOUCHDOWN. TROUBLESHOT ENVIRON SYS IAW MM. COOLING TURBINE REPLACED. DUCTING INSP. NO DAMAGE FOUND. SIDEWALL PANEL BOTTOM FOUND UNGLUED & BLOCKING HEATED AIR. PANEL TRIMMED. ENG RUNS, ENVIRON & BLEED AIR WATER SEPARATOR TEMP CHKS COMPLETED. NO LEAKS OR ODORS NOTED. A/C RETURNED TO SERVICE. 2H72 4F RTA16SW 20050930000022005093000002NM 2005 9 30 PIDA20050142 120050923A5320 ANGLE BOEING737 737228 13844AGNM R1 DOOR CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 CORROSION AT THE CLIP NUT HOLES ON THE UPPER AND LOWER SURFACES OF THE ZEE ANGLE AT THE R1 DOOR. REPLACED Z ANGLE PER SRM 51-10-1. 2L72 4F RTA16WE 20050930000032005093000003NM 2005 9 30 PIDA20050143 120050926A532069374024 ANGLE BOEING737 737228 13844AGNM R1 DOOR CUTOUT CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 ATTACH ANGLE FOR THE RIGHT FORWARD ZEE ANGLE JUST FORWARD OF THE R1 DOOR CUTOUT IS CRACKED. REPLACED ANGLE PER SRM 51-10-1. 2L72 4F RTA16WE 20050930000052005093000005NM 2005 9 30 PIDA20050145 120050926A5313BAC1498156 STRINGER BOEING737 737228 13844AGNM BS 1006-1016 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 STR 26 RT HAS CORROSION FROM BS 1006 TO BS 1016. REPLACED STRINGER SECTION PER SRM 51-10-1. 2L72 4F RTA16WE 20050930000072005093000007NM 2005 9 30 MZZA0500006 120050925A3350D71702030 CHARGER BOEING737 737824 13844BZNM ROW 5 & 11 DEF INOPERATIVE A MZZAK NONE O OTHER ININSP/MAINT 1 WP1335236 28801 THE FORWARD EMERGENCY LIGHTS WOULD NOT TEST. THE BATTERY PACK AND CHARGER AND BATTERY PACKS AT SEAT 5DEF AND 11DEF WERE REMOVED AND REPLACED IAW MM 33-51-06. 2L72 4F RTA16WE 20050930000082005093000008NM 2005 9 30 MZZA0500007 120050925A2560P4010021 BATTERY BOEING737 737824 13844BZNM FLASHLIGHT INOPERATIVE A MZZAK NONE O OTHER ININSP/MAINT 1 WP1314228 28792 THE EMERGENCY FLASHLIGHT INDICATOR DID NOT TEST DURING PREDEPARTURE TEST. THE FORWARD RT EMERGENCY FLASHLIGHT BATTERY WAS REMOVED AND REPLACED IAW MM 25-60-00. 2L72 4F RTA16WE 20050930000092005093000009NM 2005 9 30 MZZA0500008 120050928A3350D71701100 BATTERY BOEING737 737824 13844BZNM EMERGENCY LIGHT INOPERATIVE A MZZAK NONE O OTHER ININSP/MAINT 1 WP1313227 28788 SEVERAL EMERGENCY LIGHTS WERE FOUND INOPERATIVE DURING AN "S" CHECK. TROUBLESHOOTING FOUND TWO EACH BARE WIRES IN SIDEWALL FLOOR AREA AT SEAT 5ABC AND TWO EACH LIGHT BULBS BURNED OUT AT SEAT 9ABC. THE WIRING WAS REPAIRED AND LIGHT BULBS WERE REPLACED. BATTERY PACKS WERE ALSO REPLACED AT L-I CEILING, 5DEF, 12ABC, 12DEF, 20DEF, AND AFT GALLEY CEILING LT SIDE. OPERATIONAL CHECKS WERE GOOD IAW MM 33-51-06. 2L72 4F RTA16WE 20050930000102005093000010NM 2005 9 30 DHL2005748506 120050815A5330 SKIN BOEING727 727225 1384077NM BS 1144 DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 FUSELAGE HAS A DENT FWD BS 1144 ABOVE STR 24R. CUT OUT DAMAGED AREA DIMS 2" BY 1 1/2" AND FABRICATED REPAIR DOUBLER FROM MATERIAL USE 2024T3 .080 PO NR 900-2255 DIMS 11" BY 8" IAW B727 SRM 53-30-3 FIG 1 TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED NEW DOUBLER IAW B727 SRM 53-30-3 FIG 1. THIS REPAIR A CAT A. 2L73 4F A3WE 20050930000152005093000015WP 2005 9 30 AALA20050620 120050922A3260 SENSOR DOUG DC9 DC982 3022082WP NLG INOPERATIVE A AALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW217509 49803 DFW INFLIGHT T1001/22SEPT - ON CLIMB-OUT, RED NOSE GEAR LIGHT ILLUMINATED INTERMITTENTLY. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR POSITION SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050930000162005093000016NM 2005 9 30 AALA20050624 120050926A3244 TIRE BOEING777 777223 1385213NM MLG DEFLATED A AALAA UNSCHED LANDING O OTHER CLCLIMB 1 SW21782AN 30003 LHR INFLIGHT T104/26SEPT - ON CLIMB-OUT, TIRE PRESSURE ADVISORY ILLUMINATED. RIGHT NOSE WHEEL INDICATED ONE PSI. LEFT NOSE WHEEL INDICATED 219 PSI. RETURNED TO LHR AND LANDED WITHOUT INCIDENT. FOUND RIGHT HAND NOSE TIRE DEFLATED. CHANGED RIGHT AND LEFT NOSE TIRES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20050930000172005093000017NM 2005 9 30 AALA20050626 120050922A3350D71701100 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21923AN 29524 TUL - EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20050930000182005093000018NE 2005 9 30 AALA20050622 220050926A7261 OIL SYSTEM BOEING737 737823 13844BZNM GE CFM56 CFM56* 13802NE LT ENGINE CONTAMINATED A AALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW21926AN 29527 876180 JFK INFLIGHT T1558/26 SEPT - LEFT ENGINE OIL FILTER CLOG LIGHT ILLUMINATED. PERFORMED REQUIRED SHUTDOWN AND DIVERTED TO JFK. FOUND METAL IN OIL FILTER AND CHIP DETECTORS. CHANGED NUMBER ONE ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA16WE E2GL 20050930000192005093000019EU 2005 9 30 AALA20050621 120050926A2910 LINE AIRBUS300 A300B4605R 3930308EU HYDRAULIC SYSTEMFAILED A AALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW2170074 517 JFK - INFLIGHT T9646/26 SEPT - GREEN HYDRAULIC SYSTEM QUANTITY DECREASED TO AMBER AND PRESSURE WAS DECREASED BELOW LIMITS. MANUALLY EXTENDED LANDING GEAR. LANDED JFK WITHOUT INCIDENT. REPLACED GREEN SYSTEM HYDRAULIC RESERVOIR AND SUPPLY TUBE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20050930000222005093000022NE 2005 9 30 AT0500034 220050919A7200BR700715AI30 ENGINE BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE NR 1 UNSERVICEABLE A ZZDAEA ENGINE SHUTDOWN UNSCHED LANDING REJPARTIAL RPM/PWR LOSS VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 SO15930AT 55072 AT CRUISE, A GROWLING NOISE HEARD ALONG WITH ENGINE SURGE FOLLOWED BY TWO LOUD POPPING NOISES ACCOMPANIED BY A BRIEF SMELL OF SMOKE. SHUT ENGINE DOWN AND DIVERTED. REMOVED AND REPLACED NR 1 ENGINE. 2L72 4F4 FTRA6WE E00061EN 20050930000232005093000023NM 2005 9 30 DHL2005748514 120050816A5753 TRUNNION BOEING727 727225 1384077NM KRUGER FLAP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 NR 6 K FLAP ACTUATOR TRUNNION BRACKETS SUPPORT 2EA BOTH L/R ARE CRACKED. NOT CONFIRMED. FAB LEFT AND RIGHT NR 6 K FLAP ACTUATOR TRUNNION BRACKET SUPPORT FROM 7075 T6 .063 PO 9001920 DIM FOR RIGHT SIDE 8" BY 3 1/2" DIM FOR LEFT SIDE 8" BY 3 1/2" IAW B727 SRM 57-10-2 FIG 3. TREATED AND PRIMED MAT IAW B727 SRM 51-10-2. INSTALLED NR 6 K FLAP ACTUATOR TRUNNION BRACKETS SUPPORT LT AND RT IAW B727 SRM IAW B727 SRM 51-30-2. 2L73 4F A3WE 20051003000022005100300002NM 2005 10 3 DHL2005748529 120050817A5230 SKIN BOEING727 727225 1384077NM C2 DOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 AFT CARGO (C2) DOOR LWR AFT CORNER IS CRACKED AND DENTED STA 990 STR 26R. REMOVED AND REPLACED AFT LWR DOOR CORNER ON AFT CARGO DOOR IAW B727 SRM 51-30-07. REMOVED AND REPLACED LEVELING COMPOUND IAW B727 MM 20-60-01 PN 65-59948-502 PO 5314173. 2L73 4F A3WE 20051003000042005100300004NM 2005 10 3 DHL2005748532 120050818A5754 SUPPORT ANGLE BOEING727 727225 1384077NM NR 2 K FLAP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 NR 2 K FLAP LWR O/B ACTUATOR MOUNTING SUPPORT ANGLE CRACKED IN L/WING L/E. REMOVED O/B ACTUATOR MOUNTING SUPPORT ANGLE IAW B727 SRM 51-30-2 FAB NEW SUPPORT ANGLE FROM 7075 T6 .063 PO 9001417 8" X8" IAW B727 SRM 57-10-2 FIG 3. TREATED AND PRIMED NEW PARTS IAW B727 SRM 51-10-2. INSTALLED NEW SUPPORT ANGLE IAW B727 SRM 51-30-2. 2L73 4F A3WE 20051003000072005100300007NM 2005 10 3 05FDEA03106 120050925A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 CRACK INDICATION FOUND AT STRINGER END OF STRINGER 14 (UPPER STRINGER), APPROXIMATE LENGTH 7 INCHES, RIGHT SIDE WING TANK. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I . 2L73 4F RTA22WE 20051003000102005100300010NM 2005 10 3 05FDEA03109 120050925A5730 ACCESS PANEL DOUG MD11 MD11 3023602NM ZONE 500 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 LEFT WING, UPPER FUEL TANK ACCESS PANEL 534BT CUTOUT FASTENER HOLE FOUND ELONGATED. REPAIRED AS PER FEDEX E.A. 1-5710-90037. 2L73 4F RTA22WE 20051003000112005100300011NM 2005 10 3 05FDEA03110 120050925A5730 ACCESS PANEL DOUG MD11 MD11 3023602NM ZONE 600 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 RIGHT WING, LOWER FUEL TANK PANEL 638CB CUTOUT FASTENER HOLE FOUND ELONGATED. REPAIRED AS PER FEDEX EA 1-5710-90029. 2L73 4F RTA22WE 20051003000122005100300012NM 2005 10 3 05FDEA03125 120050926A5330 SKIN DOUG MD11 MD11 3023602NM BS 1019 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 LOWER FX, DENT ON FX EXTERIOR SKIN AREA ALONG STA 1019, BETWEEN L-49L AND L-50L. REPAIR CARRIED OUT PER SRM 53-20-00 FIG.6 VOL I, EO 1-5100-7-5001. 2L73 4F RTA22WE 20051012000412005101200041NM 2005 10 12 AWXA200501205 120050927A5347BAC1520792 SEAT TRACK BOEING737 7373S3 1384711NM BS 903 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 MCN - MAJOR REPAIR - DURING C18 CHECK DISCOVERED EXFOLIATION CORROSION ON SEAT TRACK AT BS 903 AND BL 45L. CORROSION WAS REMOVED AND FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-00-52-1A-1 FIG 101. DAMAGED SEAT TRACK WAS REMOVED IAW BOEING 737-300 SRM 51-40-02-0G FIG 8. FABRICATED REPAIR SPLICE PLATE AND SEAT TRACK IAW BOEING 737-300SRM 51-40-05-0G FIG 2 AND SRM 53-60-52-01 FIG 1. INSTALLED REPAIR PARTS AT BS 903 AND BL 45L IAW BOEING 737-300 SRM 53-00-52-2R3 FIG 201. 2L72 4F RTA16WE 20051012000422005101200042NM 2005 10 12 AWXA200501206 120050927A5347BAC1520792 SEAT TRACK BOEING737 7373S3 1384711NM BS 903 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 MCN - MAJOR REPAIR - DURING C18 CHECK DISCOVERED EXFOLIATION CORROSION ON SEAT TRACK AT BS 903 AND BL 45R. CORROSION WAS REMOVED AND FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-00-52-1A-1 FIG 101. DAMAGED SEAT TRACK WAS REMOVED IAW BOEING 737-300 SRM 51-40-02-0G FIG 8. FABRICATED REPAIR SPLICE PLATE AND SEAT TRACK IAW BOEING 737-300 SRM 51-40-05-0G FIG 2 AND SRM 53-60-52-01 FIG 1. INSTALLED REPAIR PARTS AT BS 903 AND BL 45R IAW BOEING 737-300 SRM 53-00-52-2R3 FIG 201. 2L72 4F RTA16WE 20051003000182005100300018EU 2005 10 3 05FDEA03116 120050926A5532 PANEL AIRBUS310 A310203 3930313EU VERTICAL STAB DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25425FE 264 VERTICAL STAB PNL 325DL DELAMINATED AT LOWER END SCREW HOLE. 2L72 4F RTA35EU 20051003000192005100300019EU 2005 10 3 05FDEA03117 120050926A5321 FLOOR PANEL AIRBUS310 A310203 3930313EU CARGO BAY CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25425FE 264 MCD FLOOR PNL 232AH CRACKED ON BACK. 2L72 4F RTA35EU 20051003000212005100300021EU 2005 10 3 05FDEA03119 120050926A5350 RADOME AIRBUS310 A310203 3930313EU FUSELAGE DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25425FE 264 RADOME HAS DAMAGE AREA AT 1 O`CLOCK POSITION, DELAM AREA. 2L72 4F RTA35EU 20051003000222005100300022NM 2005 10 3 SWAA052960 120050927A33507003661 BALLAST BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29213WN 34217 DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING SIDEWALL EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK BALLAST PER MM. 2L72 4F RTA16WE 20051003000232005100300023NM 2005 10 3 SWAA052961 120050928A53106547978 CREASE BEAM BOEING737 7373H4 1384600NM BS 578.5 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D CHECK, FOUND FUSELAGE CREASE BEAM WEB CRACKED AT BS 578.5, RBL 66. REPAIRED CREASE BEAM WEB PER SRM. 2L72 4F RTA16WE 20051003000242005100300024NM 2005 10 3 SWAA052962 120050928A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM BS 867 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 867, STR 26R. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20051003000262005100300026NM 2005 10 3 SWAA052964 120050928A3350BR2013 LIGHT BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29357SW 26594 EEPLS STRIP LOOSE AT FWD END. REMOVED AND REPLACED EEPLS PER MM. 2L72 4F RTA16WE 20051003000272005100300027 2005 10 3 SWAA052965 420050928A2565D31354 SLIDE BOEING737 7375H4 138449DNM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29507SW 24184 DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051003000282005100300028NM 2005 10 3 SWAA052966 120050928A531165C25229 FRAME BOEING737 7373H4 1384600NM BS 727D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051003000292005100300029NM 2005 10 3 SWAA052967 120050928A53116546548 FRAME BOEING737 7373H4 1384600NM BS 747 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051003000302005100300030NM 2005 10 3 SWAA052968 120050928A53116546552 FRAME BOEING737 7373H4 1384600NM BS 827 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051003000332005100300033NM 2005 10 3 SWAA052971 120050928A53116546539 FRAME BOEING737 7373H4 1384600NM BS 616 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29618WN 28034 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, BELOW LT CREASE BEAM WEB. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20060421000442006042100044EA 2006 4 21 MASA200501027 120051210A2720601R5122623 TRIM SYSTEM CNDAIRCL600 CL6002B19 1900309EA RUDDER INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW071735812899 7358 ASH 6022 FAT - RUDDER TRIM SYSTEM INOP. MAINTENANCE REMOVED AND REPLACED RUDDER TRIM CONTROL PANEL. 2L72 4F RTA21EA 20060421000612006042100061EA 2006 4 21 MASA200500941 120051121A3150 CAUTION MESSAGE CNDAIRCL600 CL6002B19 1900309EA ILLUMINATED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW0775984 7489 ASH 7311 MSN - LEFT FLIGHT SPOILER EICAS MESSAGE. CONTRACT MAINTENANCE RESET THE SYSTEM. 2L72 4F RTA21EA 20060421000622006042100062EA 2006 4 21 MASA200500385 120050523A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA MAIN PAX LACK OF LUBE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07591ML 7388 ASH 2631 PHL TO ATL - THE CREW FOUND THE MAIN PASSENGER DOOR DIFFICULT TO OPEN. MAINTENANCE APPLIED LUBRICATION. 2L72 4F RTA21EA 20060424000172006042400017EA 2006 4 24 MASA200500577 120050722A27604916405 ECU CNDAIRCL600 CL6002B19 1900309EA SPOILERS FAILED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07773029812 7302 ASH 7640 SBA - CONFIGURATION SPOILERS WARNING MESSAGE. FERRIED A/C TO PHX WHERE MX REPLACED THE SSCU. 2L72 4F RTA21EA 20060424000202006042400020EA 2006 4 24 MASA200501013 120051205A2410755469D IDG CNDAIRCL600 CL6002B19 1900309EA NR 2 DISCONNECTED A MASAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW07715SF18920 7115 ASH 2972 CLT - NR 2 IDG DISCONNECTED ON TAXI OUT. MAINTENANCE REMOVED AND REPLACED IDG. 2L72 4F RTA21EA 20060424000732006042400073EA 2006 4 24 MASA200500499 120050628A7830 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER OUT OF RIG A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW0775996 7357 ASH 2218 YUL - CAPTAIN ABORTED TAKEOFF AND RETURNED AIRCRAFT TO GATE WHEN AIRCRAFT EXPERIENCED A RT THRUST REVERSER UNLOCK MESSAGE. THE AIRCRAFT IS CURRENTLY FERRYING TO PHL WHERE MAINTENANCE RIGGED ACTUATOR. 2L72 4F RTA21EA 20060424000842006042400084EA 2006 4 24 MASA200500747 120050924A5200 ACCESS PANEL CNDAIRCL600 CL6002B19 1900309EA OXY ACCESS UNSECURE A MASAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 SW0775992 7401 ASH 7102 BNA - CREW O2 ACCESS PANEL OPENED IN FLIGHT. MX INSPECTED PANEL FOUND NO DAMAGE AND RESECURED IT. 2L72 4F RTA21EA 20060424002362006042400236SO 2006 4 24 SIMA200610407 120050412A2611FAU751A4 SMOKE DETECTOR EMB 145 EMB145LR 3260212SO LAVITORY DEFECTIVE A SIMAK NONE B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW21694AE 14500869 LAVITORY SMOKE IN FLIGHT. REPLACED LAVITORY SMOKE DETECTOR WITH OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED. (K) 2L72 4T RTT00011AT 20060425000912006042500091EA 2006 4 25 SIMA200610406 120050610A335020131A BATTERY CNDAIRCL600 CL6002C10 1390015EA CABIN DISCHARGED A SIMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW21524AE 10154 OVERHEAD EXIT SIGN INOPERATIVE. REPLACED NR 2 BATTERY PACK WITH OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (K) 2L72 4F RTA21EA 20060425000962006042500096SO 2006 4 25 SIMA200534709 120051212A532014521700007 BEAM EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21723AE 145288 DURING IMBV INSPECTION FOUND LT OMEGA BEAM IS CORRODED AT CARBON FIBER SUPPORT AT FRAME 33. REPAIRED LT OMEGA BEAM AT FRAME 33 BY INSTALLING A DOUBLER IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4F RTT00011AT 20060425000972006042500097SO 2006 4 25 SIMA200535502 120051218A532014525381003 BEAM EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21725AE11842 145312 THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 38. REMOVED THE CORROSION BY MAKING A CUT OUT. PREPARED A DOUBLER, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (K) 2L72 4F RTT00011AT 20060425001212006042500121NM 2006 4 25 MASA200500967 120051127A21311305221 SELECTOR DHAV DHC8 DHC8202 2809007NM CABIN PRESSURE MALFUNCTIONED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07987HA4092 425 ASH 6322 PHX. AIRCRAFT DIVERTED TO DRO WHEN THE CABIN WOULD NOT PRESSURIZE IN AUTO. MAINTENANCE REPLACED PRESSURE CONTROLLER, CONTROL PANEL AND STATIC SOURCE SELECTOR. 2H72 4T RTA13NM 20060425001272006042500127SO 2006 4 25 SIMA200535504 120051218A531514521721009 FLOORBEAM EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21725AE11842 145312 THE GALLEY FORWARD DIGITAL WAS FOUND TO BE CORRODED. BLENDED THE FORWARD DIGITAL TO REMOVED THE CORROSION. FABRICATED THE REPAIR DOUBLER, MARKED AND DRILLED FASTENER HOLES. REPAIR DONE IAW EMB. (K) 2L72 4F RTT00011AT 20060425001482006042500148SO 2006 4 25 SIMA200534711 120051212A532014521725613 SILL EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21723AE 145288 DURING IMBV INSPECTION FOUND LT FWD SERVICE DOOR SILL IS CORRODED. REPAIRED FWD SERVICE DOOR SILL IAW SRM BY INSTALLING AN EXTERNAL DOUBLER. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4F RTT00011AT 20060426000012006042600001NM 2006 4 26 MASA200501077 120051224A27202379003001 REGULATOR DHAV DHC8 DHC8202 2809007NM RUDDER MALFUNCTIONED A MASAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW07448YV11160 448 ASH 7053 DEN, THE CREW RETURNED THE AIRCRAFT TO THE FIELD DUE TO LITTLE TO NO RIGHT RUDDER DEFLECTION IN FLIGHT. THE CREW REPORTED THE RUDDER FUNCTIONING NORMALLY ON THE GROUND. MX REMOVED AND REPLACED THE RUDDER DUAL PRESSURE REGULATOR. 2H72 4T RTA13NM 20060426000022006042600002SW 2006 4 26 LNX2006F000AA 120050516A5100 UNKNOWN SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP UNKNOWN UNKNOWN A LNXAO OTHER O OTHER CRCRUISE 1 SO29438MA AC7218 P44080C DURING ENROUTE CRUISE FLIGHT, THE LT ENGINE CHIP DETECTOR LIGHT ILLUMINATED. THE CREW MONITORED AND FOUND NO ADDITIONAL DISCREPANCY. THE FLIGHT CONTINUED TO ITS DESTINATION WITHOUT INCIDENT. UPON INVESTIGATION. THE MAINTENANCE CREW FOUND METAL PARTICLES IN THE OIL. OIL FILTER AND OIL SYSTEM. THE ENGINE HAS BEEN REMOVED FOR TEARDOWN AND FURTHER INVESTIGATION. INFORMATION TO BE SUPPLIED WHEN AVAILABLE. (K) 2L72 4T4 TRTA8SW E4WE 20060426000032006042600003GL 2006 4 26 MASA200500955 120051128A571185710064 SPAR DHAV DH82 DH82 2801000GL RT WING CRACKED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07456YV20379 456YV "MAJOR REPAIR TO RT WING LEADING EDGE SPAR OUTBOARD OF STN. YW423.0 PER REPAIR ORDER DHC82-57-1054." INSPECTION OF REMAINING SPAR FOR CRACKS AND SPLICING C/W. REMOVED AND REPLACED DAMAGED SPAR SECTION - OUTB’D OF APPROXIMATELY YW41 1. 1Q71 3I EXPA1Q71 20060426000062006042600006EA 2006 4 26 SIM2006F00003 120051205A2133GG670950035 CONTROL VALVE CNDAIRCL600 CL6002C10 1390015EA FLOW CONTROL INOPERATIVE A SIMAA UNSCHED LANDING O OTHER CRCRUISE 1 SW21519A 10131 LT PACK CYCLES ON AND OFF IN AUTO MODE. WORKS NORMAL IN MANUAL MODE. PRESSURIZATION SPIKES WHEN PACK CYCLES OFF AND ON UP TO 1000 FT PER MIN. CHANGED EXISTING REFERENCE FOR MEL ORIGINALLY ISSUED FOR RT AUTO PRESS CONTROL TO MEL TO ADDRESS BOTH PRESS CONTROLLERS INOP IN AUTO MODE. AUTHORIZATION NR AND DUE DATE REMAIN THE SAME IAW THE ORIGINAL MEL. R&I L/H FLOW CONTROL VALVE IAW AMM. OPS CHECKED GOOD. (K) 2L72 4F RTA21EA 20060426000112006042600011SO 2006 4 26 SIMA200533903 120051204A335082321 LIGHT EMB 135 EMB135KL 3260302SO CABIN` INOPERATIVE A SIMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW21853AE 145742 OVERHEAD EMERGENCY EXIT ROW LIGHT AT ROW 1C WILL NOT ILLUMINATE. REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (K) 2L72 4F RTT00011AT 20060426000122006042600012EA 2006 4 26 SIM2006F00004 120051210A284073811812 COMPUTER CNDAIRCL600 CL6002C10 1390015EA FUEL SYS FAILED A SIMAA UNSCHED LANDING O OTHER CRCRUISE 1 SW21514AE 10119 NOTIFIED BY DISPATCH, AIRCRAFT DIVERSION, DUE TO FUEL CHANNEL 1 FAIL EICAS MESSAGE. CREW FOLLOWED AOM PROCEDURES AND LANDED. RAI FQGC OPS CHECK GOOD. (K) 2L72 4F RTA21EA 20060424000282006042400028NE 2006 4 24 MASA200500365 220050517A7261 OIL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 2 ENGINE MALFUNCTIONED A MASAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 SW0717275 7275 ASH FLT 6145 PHX TO SBA - THE PILOT RETURNED TO FIELD WITH THE NR 2 ENGINE OIL PRESSURE AT 35 PSI AND THE NR 2 OIL TEMP AT 157 DEGREES. MAINTENANCE DRAINED AND RESERVICED THE NR 2 ENGINE OIL. 2L72 4F4 FRTA21EA E15NE 20060424001392006042400139EA 2006 4 24 MASA200500734 120050918A3230601R751451 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA MLG MALFUNCTIONED A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07759942235 11 7367 ASH 7179 IAD - RETURNED TO FIELD DUE TO THE GEAR DISAGREE. FERRIED THE AIRCRAFT TO CLT WHERE MX CHANGED THE MAIN LANDING GEAR SELECTOR VALVE. 2L72 4F RTA21EA 20060424001612006042400161EA 2006 4 24 MASA200500996 120051205A5210 CAUTION MESSAGE CNDAIRCL600 CL6002D24 1390016EA PAX DOOR FALSE ACTIVATIONA MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW07910FJ 15010 ASH 6017 PHX - PAX DOOR CAUTION MESSAGE. OPS CHECKED GOOD. 2L72 4F RTA21EA 20060424001622006042400162EA 2006 4 24 MASA200501033 120051213A5230 DOOR CNDAIRCL600 CL6002D24 1390016EA CARGO BAY UNSECURE A MASAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW07909FJ 15009 ASH 2652 DFW - AIRCRAFT WAS NOT PRESSURIZING IN FLIGHT. MAINTENANCE INSPECTED AND FOUND THE AFT CARGO DOOR NOT PROPERLY SEATED. MAINTENANCE OPENED THE DOOR AND CLOSED PROPERLY AND PERFORM PRESSURIZATION CHECKS WHICH OPS CHECKED GOOD. 2L72 4F RTA21EA 20060425001132006042500113EA 2006 4 25 SIMA200536103 120051225A2780766389K CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA WING INOPERATIVE A SIMAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 SW21507AE 10059 CREW RECEIVED SLAT FAIL CAUTION, COMPLIED WITH AOM PROCEDURES. DECLARED EMERGENCY LANDING UNEVENTFUL. REPLACED SLAT ELECTRONIC CONTROL UNIT IAW AMM. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (K) 2L72 4F RTA21EA 20060425001172006042500117SO 2006 4 25 SIMA200535503 120051217A532014522178005 SILL EMB 135 EMB135LR 3260305SO SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21725AE11842 145312 SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. BLENDED THE CORRODED AREA. CLEANED AND TREATED THE BLENDED AREA. APPLIED EPOXY PRIMER AND TOP COAT OF PAINT. FILLED THE BLENDED AREA WITH EPOXY RESIN HYSOL EA934NA, SANDED THE RESIN TO MAKE IT FLAT AND APPLIED EPOXY PRIMER. FABRICATED 2 REPAIR DOUBLERS. REPAIR DONE IAW SRM. (K) 2L72 4F RTT00011AT 20060425001282006042500128SO 2006 4 25 SIMA200534707 120051211A531513500469403 FLOORBEAM EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21723AE 145288 DURING IMBV INSPECTION FOUND GALLEY 2 FLOOR SUPPORT BEAM AT FRAME 22 IS CORRODED. REPLACED FLOOR SUPPORT IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4F RTT00011AT 20060425001342006042500134SO 2006 4 25 SIMA200534713 120051212A532014521713003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21723AE 145288 DURING IMBV INSPECTION FOUND CENTER OMEGA BEAM CORRODED AT CARBON FLOOR SUPPORT AT FRAME 24. REPAIRED AREA IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4F RTT00011AT 20060425001372006042500137SO 2006 4 25 SIMA200533904 120051204A335010049 BATTERY PACK EMB 135 EMB135LR 3260305SO CABIN DISCHARGED A SIMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW21716AE 145264 EMERGENCY FLOOR LIGHTING STRIP INOPERATIVE FROM ROW 9 TO 13. REPLACED BATTERY POWER SUPPLY AT LOCATION NR 4. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (K) 2L72 4F RTT00011AT 20060425001382006042500138SO 2006 4 25 SIMA200534710 120051212A534714532605001 SEAT TRACK EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21723AE 145288 DURING IMBV INSPECTION FOUND LT IB SEAT TRACK CORRODED AROUND FRAME 23. REPLACED SEAT TRACK IAW AMM. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4F RTT00011AT 20060426000752006042600075EA 2006 4 26 SWIA200516554 120051117A5312 PRESSURE PANEL CNDAIRCL600 CL6002B19 1900309EA BS 621 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07411SW 7067 CARGO COMPARTMENT AFT PRESSURE WEB FS 621 LBL 27.5 WL 130 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. WEB REPAIR CARRIED OUT REF RII 53-401 & M-337. 2L72 4F RTA21EA 20060426000762006042600076EA 2006 4 26 SWIA200516555 120051117A5312 PRESSURE PANEL CNDAIRCL600 CL6002B19 1900309EA BS 621 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07411SW 7067 CARGO COMPARTMENT AFT PRESSURE WEB FS 621 LINTEL INSTALLATION CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED WEB IAW CRJ REO 601R-53-61-1230 REV C. 2L72 4F RTA21EA 20060426000772006042600077EA 2006 4 26 SWIA200516556 120051117A5210 FRAME CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07411SW 7067 SUB FRAME CRACKED AT FS 323.6 ON PAX DOOR UPPER END. ITEM FOUND AT C-CHECK INSPECTION. PAX DOOR SUB-FRAME AT STA 323.6 REPLACED IAW CRJ SRM 51-40-11, 51-25-06, 51-23-00, 51-21-16, 51-42-06, 51-42-10 FIG 4, 51-42-13, 51-42-21. 2L72 4F RTA21EA 20060426000782006042600078EA 2006 4 26 SWIA200516557 120051117A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA BS 449 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07411SW 7076 INTERCOSTAL FLANGE CHAFED ON LT SIDE FUSELAGE AT FS 449.85 BETWEEN STRINGER 8 AND 9. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED REF REO 601R-53-41-375. 2L72 4F RTA21EA 20060426000792006042600079EA 2006 4 26 SWIA200516558 120051117A5210 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07411SW 7067 PAX DOOR, TOP STEP, AFT SIDE WEB, CRACKED ON INBOARD RETURN FLANGE, FS 340.0. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-52-11-702 REV NC. 2L72 4F RTA21EA 20060426000802006042600080EA 2006 4 26 SWIA200516559 120051117A5310 VERTICAL BEAM CNDAIRCL600 CL6002B19 1900309EA BS 559 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07411SW 7067 FUSELAGE; VERTICAL BEAM; LOWER I/B + O/B FLANGES ARE CRACKED FS 559.00; LBL 9.0. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW REO 601R-53-41-377 AND 601R-53-41-057. 2L72 4F RTA21EA 20060425000952006042500095SO 2006 4 25 SIMA200534708 120051211A532014522461 DOUBLER EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21723AE 145288 DURING IMBV INSPECTION, FOUND GUSSET ABOVE RT OMEGA BEAM AT FRAME 20 IS CORRODED. REPLACED DOUBLER ABOVE RT OMEGA BEAM IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4F RTT00011AT 20060425000982006042500098SO 2006 4 25 SIMA200610408 120050405A783083990168 SWITCH EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL LT ENGINE FAILED A SIMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW21653AE7217 145433 E-1 REVERSER DISAGREE WARNING ON TAKEOFF. TROUBLESHOT IAW EMB. REPLACED UPPER OB STOW SWITCH IAW EMB AMM. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVIC. (K) 2L72 4T4 FRTT00011ATTE6CH 20060425001012006042500101SO 2006 4 25 SIMA200610409 120050403A2121 INSULATION EMB 135 EMB135LR 3260305SO FWD ELECT COMP INGESTED A SIMAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21711PH 145235 BURNING PLASTIC SMELL REPORTED BY F/A IN CABIN DURING FLIGHT. NO SMOKE NOTED.. REMOVED THERMOCOUPLE INSULATION OUT OF BOTH FWD ELECTRONIC COMPARTMENT INTERNAL RECIRCULATION FANS. FUNCTIONAL CHECK FLIGHT PASSED. AIRCRAFT RETURNED TO SERVICE. (K) 2L72 4F RTT00011AT 20060425001242006042500124NM 2006 4 25 MASA200500998 120051205A323154C546349 SEQUENCE VALVE DHAV DHC8 DHC8202 2809007NM MLG DOORS MALFUNCTIONED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07456YV10681 456 ASH 7066 DEN. MLG DOORS WILL NOT RETRACT AFTER TAKE-OFF. MAINTENANCE REMOVED AND REPLACED SEQUENCING VALVE. 2H72 4T RTA13NM 20060425001352006042500135SO 2006 4 25 SIMA200534714 120051212A532014521700007 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21723AE 145288 DURING IMBV INSPECTION FOUND LT OMEGA BEAM CORRODED AT CARBON FLOOR SUPPORT AT FRAME 20. REPAIRED AREA IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4F RTT00011AT 20060425001362006042500136SO 2006 4 25 SIMA200534712 120051212A532014521713003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21723AE 145288 DURING IMBV INSPECTION FOUND CENTER OMEGA BEAM CORRODED AT CARBON FLOOR SUPPORT AT FRAME 33. REPAIRED AREA IAW SRM BY INSTALLING AN EXTERNAL DOUBLER. AIRCRAFT WAS RETURNED SERVICE. (K) 2L72 4F RTT00011AT 20060427002582006042700258NM 2006 4 27 ASAA0540603 120051108A5311656055211 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND BS 380 FRAME MEMBER CRACK AT BIN RAIL ATTACHMENT. REPAIRED PER B737-400 SRM 53-00-07. (M) 2L72 4F RTA16WE 20060427002512006042700251NM 2006 4 27 ASAA0540736 120051125A53306546558 SKIN BOEING737 7374Q8 138447QNM FUSELAGE DAMAGED A ASAAK NONE O OTHER TXTAXI/GRND HDL 1 NM02763AS 25100 KTN - FOUND BAGGAGE CART IMPACTED FUSELAGE SKIN. REPAIRED FRAME AT BS 907, STRINGERS 22 RT, BS 897, STRINGER 23RT, BS 847-907, STRINGER 24 RT, BS 847-907 AND FUSELAGE SKIN AT S22-24RT AND BS 887-927. ALL WORK PERFORMED IAW B737-400 SRM 53-00-03 REPAIR 1. (M) 2L72 4F RTA16WE 20050926000072005092600007 2005 9 26 RAIA00509031 420050921A34207011672112 SYMBOL GENERATOR JETAIRJETSTMJETSTM4101 1500501EU EADI/EHSI FAILED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03557HK135931309 41074 FLT 3615 - RIC - FO'S EADI AND EHSI ARE IN REVERSE SCREENS. MAINTENANCE REMOVED AND REPLACED THE FO'S SYMBOL GENERATOR. 2L72 4T RTA41NM 20050926000092005092600009SO 2005 9 26 RAIA00509035 120050920A325012302323403 TILLER EMB 145 EMB145LR 3260212SO NLG STEERING DAMAGED A RAIAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 CE03812HK1161811618 145373 FLT 3574 - PIT - STEERING DISENGAGED UNCOMMANDED. MAINTENANCE REMOVED AND REPLACED THE STEERING TILLER HANDLE. 2L72 4T RTT00011AT 20050926000102005092600010SO 2005 9 26 RAIA00509034 120050920A2150 A/C PACK EMB 145 EMB145 3260210SO NR 2 SMOKE A RAIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CE03806HK 145112 FLT 3542 - ST L- COCKPIT AND CABIN FILLED WITH SMOKE WHILE RUNNING PACKS AT THE GATE. MAINTENANCE DETERMINED THAT THE SMOKE WAS COMING FROM THE NR 2 PACK. SERVICED/CLEANED THE WATERSOCK AND DEFERRED THE NR 2 PACK. 2L72 4F RTT00011AT 20050926000142005092600014SO 2005 9 26 RAIA00509036 120050919A3350 LIGHT EMB 145 EMB145EP 3260221SO CABIN MALFUNCTIONED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03826HK 145016 FLT 5563 - STL - EMERGENCY LIGHTS OUT AT ENTRANCE TO THE FLIGHT DECK. MAINTENANCE CYCLED POWER TO THE EMERGENCY LIGHTS. SYSTEM CHECKED GOOD. 2L72 4F RTT00011AT 20050926000152005092600015NM 2005 9 26 BB05082 120050921A3230098C00210 SEQUENCE VALVE BOEING757 7572B7 1384964NM MLG MALFUNCTIONED A USAAO OTHER J WARNING INDICATION CLCLIMB 1 EA19633AU35227 27811 FLL FLT 365 EN-ROUTE CLT TO FLL - AFTER TAKE-OFF, AND UPON GEAR RETRACTION, RECEIVED EICAS MESSAGE "GEAR DOOR" WITH THE GEAR HANDLE UP. ALSO, THE LEFT GEAR DOOR LIGHT ILLUMINATED. HOWEVER, THE GEAR AMBER LIGHT AND ALL GREEN LIGHTS WERE EXTINGUISHED. THE CREW CYCLED THE GEAR, AND ALL INDICATIONS RETURNED TO NORMAL. FLIGHT CONTINUED TO FLL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT MAIN GEAR UPLOCK OPERATED SEQUENCING VALVE. OPERATIONALLY AND LEAK CHECKED OK. 2L72 4F RTA2NM 20050926000162005092600016NM 2005 9 26 PIDA20050139 120050922A5330 SKIN BOEING737 737228 13844AGNM BS 951 CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 FUSELAGE SKIN CRACKED AT R2 DOOR LOWER FORWARD CORNER CUT-OUT. REPAIRED PER EA 53-247 DUE TO CLOSE PROXIMITY TO AN EXISTING REPAIR AT BS 951 AT STR 19RT. 2L72 4F RTA16WE 20050926000192005092600019NM 2005 9 26 USAA051139 120050921A5340 STRINGER CLIP BOEING737 7374B7 1384702NM STA 787 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19443US 24842 TIE CLIP CRACKED, STA 787L STRINGER 4L. REPLACED WITH IDENTICAL PART, REMOVED AND REPLACED STRINGER TIE CLIP IAW SRM 51-40-02, DEFECT SIZE: .025. 2L72 4F RTA16WE 20050926000232005092600023NM 2005 9 26 USAA051135 120050921A5315 FLOORBEAM BOEING737 7374B7 1384702NM BS 312 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19443US 24842 FOUND FLOORBEAM T-CAP CORRODED STATION 312 LBL 10 TO RBL 36. T-CAP REPLACED IAW SRM 53-10-51-2R-5, DEFECT SIZE: 2" X 6". 2L72 4F RTA16WE 20050926000302005092600030EA 2005 9 26 SWIA200515559 120050402A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA BS 625 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07917SW 7641 FS 625 LT INTERCOSTAL ANGLE STR 14L CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06. 2L72 4F RTA21EA 20050926000402005092600040EA 2005 9 26 SWIA200515569 120050916A5210 LATCH CNDAIRCL600 CL6002B19 1900309EA PAX DOOR LACK OF LUBE A SWIAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 NM07903SW 7425 UNABLE TO TURN ON MCD TO OPEN IT. LUBED CABIN DOOR LATCH PINS AS NEEDED. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050926000422005092600042EA 2005 9 26 SWIA200515571 120050916A27805912999 SENSOR CNDAIRCL600 CL6002C10 1390015EA SLATS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07760SK 10223 SLATS HALFSPEED MESSAGE POSTED. REPLACED LEFT BRAKE POSITION SENSE UNIT IAW CRJ 700 AMM 27-50-00. OPERATIONAL CHECK GOOD PN ON 5912999 SNOFF 0521. 2L72 4F RTA21EA 20050926000432005092600043EA 2005 9 26 SWIA200515572 120050916A2740 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA COCKPIT STICKING A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07433SW 7550 FO'S TRIM SWITCH STICKING. REPLACED FO'S TRIM SWITCH. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050926000462005092600046NE 2005 9 26 EM05012 220050920A7200 ENGINE EMB ERJ170ERJ170100 EU GE CF34 CF348E5 30015NE NR 2 SHUTDOWN A USAAO OTHER YJ ENGINE STOPPAGE WARNING INDICATION DEDESCENT 1 EA19802MD 000013 GEE193126 ON APPROACH, NR 2 ENGINE AUTO SHUTDOWN. CREW DECLARED AN EMERGENCY & LANDED WITHOUT FURTHER INCIDENT. AS ACFT TAXIED TO GATE, NR 2 ENGINE HAD AN AUTO RESTART. MX BORESCOPED NR 2 ENGINE HPT, NO FAULTS FOUND. DOWNLOADED NR 2 ENGINE FADEC INFO FORWARDED TO GE. PER GE REQUEST, REPLACED NR 2 ENGINE FADEC, NR 2 ENGINE FMU, & BLEED VALVE. PERFORMED GVI OF NR 2 ENGINE FMU FUEL FILTER. NO FAULTS FOUND. PERFORMED GROUND POWER RUNS. NO DEFECTS NOTED. PERFORMED PRECAUTIONARY FUEL TANK SUMP. NO CONTAMINATION FOUND. R & R NR 2 ENGINE MAIN FUEL FILTER. NO CONTAMINANTS NOTED. PERFORMED A BORESCOPE OF NR 2 ENGINE COMPRESSOR SECTION. NO FAULTS FOUND. REPLACED NR 2 ENGINE LOW STAGE BLEED CHECK VALVE. 2L74 4F4 FRTA56NM E00063EN 20050926000472005092600047SO 2005 9 26 SWIA200515575 120050921A3397 WIRE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07296SW 120325 EMERGENCY EXIT SIGN ON OVERHEAD BIN AT SEATS 9B/9C DOES NOT LIGHT UP. REPAIRED BROKEN WIRE AT EMERGENCY SIGN OF SEAT 9BC, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050926000492005092600049SO 2005 9 26 SWIA200515577 120050919A275012064207615 SELECTOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07268UE5842 5842 120207 CREW REPORTED AN INTERMITTENT FLAP CONTROL FAULT. REPLACED FLAP CONTROL HANDLE ASSY. OPERATIONAL CHECK GOOD IAW 27-50-00. 2L72 4T RTA31SO 20050926000512005092600051EA 2005 9 26 SWIA200515579 120050913A274170609 TRIM SYSTEM CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION DEDESCENT 1 NM07927SW3183 3183 7693 DURING DESCENT INTO DEN "AP STAB TRIM CAUTION MSG ILLUMINATED. REPLACED HSTCU REF AMM 27-41-01 AS REQUIRED. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050926000542005092600054NM 2005 9 26 USAA051142 120050922A5311 FRAME BOEING737 7374B7 1384702NM BS 380 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 FRAME CRACKED BS 380 JUST BELOW STR 8L. CUT OUT CRACKED AREA, INSTALLED REPAIR PER T/R 53-10-20B, DEFECT SIZE: APPROX 1 INCH CRACK. 2L72 4F RTA16WE 20050926000572005092600057NM 2005 9 26 USAA051143 120050923A5730 SKIN BOEING737 7374B7 1384702NM LT WING CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 FOUND LT WING SKIN CRACKED, FWD OF FRONT SPAR O/B SIDE OF PYLON. REMOVED DAMAGED SKIN, FABRICATED AND INSTALLED REPAIR PIECES IAW TR 57-41-023. 2L72 4F RTA16WE 20050926000592005092600059EU 2005 9 26 USAA050932 120050729A5315 FLOORBEAM AIRBUSA319 A319112 3930323EU FR 66 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19723UW 1109 PIT - FOUND BEAM CORRODED .75 INCH BY .75 INCH, ON FLOORBEAM FRAME 66 - Y 53 INCH. CORROSION LEVEL 1, TASK JA-260-53500. REPLACED BEAM PER SRM 53-41-00. (M) 2L72 4F RTA28NM 20050926000672005092600067NM 2005 9 26 QXEA200501252 120050919A3060 WARNING LIGHT BOMBDRDHC8 DHC8402 1390042NM PROP DE ICE ILLUMINATED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09416QX 4083 GEG FLIGHT NR 2357: AFTER PUSHBACK, ENGINE START, PROP DE-ICE CAUTION LIGHT ILLUMINATED. MAINTENANCE COMPLIED WITH PROCEDURE IAW DH8-SL-31-001R14 PER MTX CONTROL. CAUTION LIGHT EXTINGUISHED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050926000682005092600068EA 2005 9 26 COMA0560498 120050913A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAK NONE J WARNING INDICATION ININSP/MAINT 1 SO01506CA 7793 FLIGHT 5781- RECEIVED A FLAP FAIL CAUTION MESSAGE DURING PREFLIGHT CHECK. COMPLIED WITH AD 98-20-01 FLAP FAIL CAUTION MESSAGE FIRST EVENT MAINTENANCE ACTION PARAGRAPH (B) 1, 2, 3 (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2L72 4F RTA21EA 20050926000702005092600070EA 2005 9 26 COMA0560500 120050914A3230601R751461 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01924CA1801613774 7026 FLIGHT 5029 - GEAR DISAGREE WARNING. REPLACED THE NLG SELECTOR VALVE. 2L72 4F RTA21EA 20050926000742005092600074EA 2005 9 26 COMA0560503 120050915A2752852D10019 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA NR 2 FLAP UNRELIABLE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01956CA6270 7105 FLIGHT 5262 - FLAPS FAIL CAUTION. CND, REPLACED 2 FLAP ACTUATORS AND 1 FLEX DRIVE CABLE. RE-RIGGED SYSTEM. 2L72 4F RTA21EA 20050926001062005092600106NM 2005 9 26 ASMF200509008 120050917A792042D110 PRESSURE SWITCH DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE LT ENGINE OIL INOPERATIVE W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23831LF 53050 AIRCRAFT RETURNED TO PLATFORM, LT ENGINE OIL PRESSURE WAS 38 PSI NEAR YELLOW RANGE. THE PARAMETERS IN FLIGHT CABIN WAS CHECKED AND OIL PRESSURE ADJUST WAS PERFORMED IAW MM 79-20-03. AFTER, TO ACCELERATE THE ENGINE, THE ENGINE PRESSURE WAS INCREASED TO 90 PSI. AIRCRAFT WAS SENT TO THE HANGAR, THE LT ENGINE OIL PRESSURE WAS ADJUSTED AND THE LOW PRESSURE SWITCH WAS REPLACED IAW 79-20-03, THE ENGINE RUNNING WAS PERFORMED IAW MM 71-00-00, TESTED CORRECT. 2L72 4F4 FRT E9NE 20050926001072005092600107EA 2005 9 26 QXEA200501241 120050918A7500 SEAL CNDAIRCL600 CL6002C10 1390015EA RT BLEED SYS LEAKING A QXEAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 NM09613QX 10045 PDX - RIGHT BLEED DUCT WARNING/CAUTION ILLUMINATED. RETURNED TO PDX AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE FOUND A LEAK AT THE CROSSOVER PIPE AT THE RIGHT CONNECTION. REPLACED THE SEALS AND THE CLAMPS AT THE CROSSOVER PIPE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20050926001082005092600108EA 2005 9 26 QXEA200501244 120050920A273070744 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA HORIZONTAL STAB MALFUNCTIONED A QXEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM09604QX9542 10019 PDX - ON FLIGHT 2510 IN CRUISE, RECEIVED A STAB TRIM MESSAGE, AND A MACH TRIM MESSAGE. RETURNED TO PDX AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT (MCU). OPERATIONAL CHECK FLIGHT TESTS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20050926001102005092600110NM 2005 9 26 SWAA052880 120050921A53206551698 SPLICE BOEING737 7373L9 1384470NM BS 359 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED 1/2D CHECK, FOUND STR SPLICE CRACKED AT BS 359, STR 14L. REMOVED AND REPLACED STR SPLICE PER SRM. 2L72 4F RTA16WE 20050926001122005092600112NM 2005 9 26 SWAA052881 120050921A53306545767 SKIN BOEING737 7373H4 1384600NM BS 500D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29371SW 26598 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 15R. REPAIRED SKIN PER SRM & SWA EA. 2L72 4F RTA16WE 20050926001142005092600114NM 2005 9 26 05FDEA02994 120050919A5314 KEELBEAM BOEING727 727232 1384082NM BS 873 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CRACK IN KEEL BEAM UPPER FLANGE AT FASTENER LOCATION ON STA 873 LBL 6. REPAIRED KEEL BEAM PER EA 7-5310-91372. 2L73 4F A3WE 20050926001172005092600117EU 2005 9 26 05FDEA02997 120050919A5511 FRAME AIRBUS310 A310203 3930313EU HORIZONTAL STAB CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25425FE 264 LT HORIZ STAB T/E FORMER/WEB CORRODED AROUND NUTPLATES AND WEB FROM REAR SPAR TO 10" AFT OF REAR SPAR AND 54" FROM FUSELAGE. REMOVED CORROSION FOUND OUT OF LIMITS IAW SRM 55-10-00 FIG 101. REMOVED FORMER WEB RIB IAW SRM 51-40-21. RIB FABRICATED ON PCT NR T5/546620 LOCATED AND DRILLING IAW SRM 51-40. INSTALLED NEW RIB IAW SRM 51-40-21 PG 27. 2L72 4F RTA35EU 20050926001202005092600120EU 2005 9 26 05FDEA03000 120050920A5310 ADAPTER AIRBUS300 A300F4605R 3930327EU FR 42-44 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25681FE 799 MDCC CLAS ADAPTER AT FR 42 AND FR 44 BETWEEN S/T L4 AND L5 HAVE DAMAGE IN SCALLOP AREAS. REMOVED AND REPLACED 2 CROSSBEAMS IAW A300-600 SRM 51-72-10. 2L72 4F RTA35EU 20050926001272005092600127NM 2005 9 26 ASMF200509012 120050921A27205914387515 ACTUATOR DOUG MD80 MD83 3023681NM RUDDER FAILED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23881LF 53051 CAPTAIN REPORTED THAT AFTER LANDING RUDDER TRAVEL UNRESTRICTED LIGHT TURNED ON. AIRCRAFT WAS SENT TO THE HANGAR; THE RUDDER THROW LIMITER AND PUSHROD NR 5 WERE REPLACED AND SYSTEM WAS ADJUSTED IAW MM 27-20-06, PAGE 201, TESTED CORRECT. 2L72 4F RT 20050926001392005092600139WP 2005 9 26 UPS05845484 120050923A3510 REGULATOR DOUG DC8 DC871F 302199DWP OXYGEN INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01715UP 45915 CREW OXYGEN REGULATOR INOP. REPLACED CAPTAIN'S 02 REGULATOR PER 35-10-07. OPS CHECK NORMAL. 2L74 4F RT4A25 20050926001442005092600144NM 2005 9 26 ASMF200509013 120050922A492097980611 VALVE BOEING757 7572Q8 1384972NM APU MALFUNCTIONED W ASMFD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SW23804AM 26271 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING ENGINES START, APU SHUT DOWN, FAULT LIGHT TURNED ON AND EICAS MESSAGE APU FAULT WAS DISPLAYED. THE FIM 49-11-00 PROCEDURES WAS PERFORMED. THE ENGINES START WAS PERFORMED WITH GROUND EQUIPMENT, ALL CORRECT. DURING OVERNIGHT CHECK SURGE VALVE AND GEARBOX VALVE WERE REPLACED IAW MM 49-53-01 AND MM 49-27-11, RESPECTIVELY. TESTS WERE PERFORMED AND BOTH ENGINE WERE MOTORIZED AT 30 PERCENT OF N2 IAW MM 49-00-00, OPERATING CORRECTLY THE APU. 2L72 4F RTA2NM 20050926001482005092600148NM 2005 9 26 72400004 120050920A5210 STRUCTURE BOEING727 727225 1384077NM PAX DOOR CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23724CK 20383 CORROSION ON DOOR OPENING REINFORCEMENT. 2L73 4F A3WE 20050926001502005092600150NM 2005 9 26 SWAA052885 120050921A335010107451 SIGN BOEING737 7373H4 1384600NM LT OVERWING LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29387SW 26602 LT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM. 2L72 4F RTA16WE 20050926001522005092600152NM 2005 9 26 SWAA052887 120050921A53116516301 FRAME BOEING737 7375H4 138449DNM BS 188 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29505SW 24182 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STUB FRAMES CRACKED AT BS 188, LT & RT SIDE, WL 208. REPAIRED STUB FRAMES PER SRM. 2L72 4F RTA16WE 20050926001662005092600166EA 2005 9 26 VNAA0509011 120050918A34110851HF PITOT HEAD CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE STANDBY PITOT SYDAMAGED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL05221PS3771 7889 AS THE JETWAY WAS BEING PULLED BACK, THE AUTO LEVELER CONTACTED AND DAMAGED THE STANDBY PITOT PROBE. THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE REMOVED & REPLACED THE STANDBY PITOT PROBE IAW CRJ200 AMM 34-11-02-000(400)-801. OPERATIONAL AND LEAK CHECKS WERE GOOD IAW CRJ200 AMM 34-11-00-790-803. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050926001892005092600189CE 2005 9 26 S2YA05038 120050617A7400 PRESSURE SWITCH BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA ENGINE MALFUNCTIONED A S2YAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL13841SK UE84 ON CLIMB OUT, THE CREW REPORTED TO MAINTENANCE THE LT AUTO IGNITION REMAINS ILLUMINATED IN FLIGHT. MAINTENANCE REQUEST THE AC RETURN TO DEPARTURE. THE CREW PERFORMED AN AIR-TURN-BACK TO DEPARTURE. MAINTENANCE REPLACED THE LT HIGH PRESSURE SWITCH AND RETURNED THE AC TO SERVICE. (K) 2L72 4T3 TRTA24CE E2NE 20050927000022005092700002SO 2005 9 27 SIMA200525206 120050828A532014522461017 DOUBLER EMB 135 EMB135KL 3260302SO FR 22 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21817AE 145554 SAW - DURING CPCP INSPECTION, FOUND DOUBLER PLATE WHERE RIGHT HAT BEAM AND FLOORBEAM AT FRAME 22 MEET IS CORRODED. REPLACED DOUBLER IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050927000062005092700006SO 2005 9 27 SIMA200525214 120050829A532012004149002 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO FR 24-25 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21817AE 145554 SAW - FOUND DURING CPCP INSPECTION, LEFT OMEGA BEAM CORRODED BETWEEN FRAMES 24-25. REPLACED DAMAGED AREA IAW SRM 53-00-01 FIG 202 AND IC2005-145/4572. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050927000072005092700007SO 2005 9 27 SIMA200525213 120050829A532014521725015 SILL EMB 135 EMB135KL 3260302SO SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21817AE 145554 SAW - DURING CPCP INSPECTION, FOUND SERVICE DOOR AFT SILL HAS CORROSION. INSTALLED NEW AFT SILL PLATE IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050927000082005092700008 2005 9 27 KBM2005F00242 420050821A2312064105430 RADIO SNIAS 350 AS350B2 8680813EU VHF MALFUNCTIONED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19351WM 2167 RADIO EXHIBITED BLEED OVER ON CERTAIN FREQUENCIES. REMOVED AND REPLACED WITH SERVICEABLE UNIT. (M) 1G71 3U H9EU 20050927000092005092700009EA 2005 9 27 ASOA05699 120050820A5340 NUT PLATE CNDAIRCL600 CL6002B19 1900309EA BS 530 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11839AS 7284 DURING A C-CHECK IN MCN, THE NUT PLATE AT FS 530, RBL 44 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO BOMBARDIER FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. S/D - MAINTENANCE REMOVED THE CORROSION FROM THE NUT PLATE AT FS 530, RBL 44 BY COMPLYING WITH ASA EO 600-53-0313. (M) 2L72 4F RTA21EA 20050927000112005092700011EA 2005 9 27 ASOA05690 120050820A5330 FINGER DOUBLER CNDAIRCL600 CL6002B19 1900309EA BS 459 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11839AS 7284 DURING A C-CHECK, THE FINGER DOUBLER AT FS 459, LBL 44 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO BOMBARDIER FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. S/D - MAINTENANCE REMOVED THE CORROSION FROM THE FINGER DOUBLER AT FS 459, LBL 44 BY COMPLYING WITH ASA EO 600-53-0314. (M) 2L72 4F RTA21EA 20050927000212005092700021SO 2005 9 27 SIMA200522002 120050729A532014532636401 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO FR 24-25 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21816AE 145552 SAW - DURING IMBV INSPECTION, FOUND LEFT OMEGA BEAM CORRODED BETWEEN FRAMES 24 AND 25 AT CROSSBEAM ATTACH POINT. REPAIRED LEFT OMEGA BEAM WITH DOUBLER IAW SRM 53-00-10 FIGURE 202. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050927000242005092700024SO 2005 9 27 SIMA200525203 120050828A534714532605015 SEAT TRACK EMB 135 EMB135KL 3260302SO CABIN CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21817AE 145554 SAW - DURING CPCP INSPECTION, FOUND RIGHT UPPER 3RD FROM FRONT SEAT TRACK CORRODED AROUND SCREW HOLES. REPLACED SEAT TRACK IAW EMB AMM 53-01-06-400-801A. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050927000272005092700027EA 2005 9 27 ASOA05691 120050820A5330 FINGER DOUBLER CNDAIRCL600 CL6002B19 1900309EA BS 461 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11839AS 7284 DURING A C-CHECK IN MCN, THE FINGER DOUBLER AT FS 461, RBL 44 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO BOMBARDIER FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. S/D - MAINTENANCE REMOVED THE CORROSION FROM THE FINGER DOUBLER AT FS 461, RBL 44, BY COMPLYING WITH ASA EO 600-53-0313. (M) 2L72 4F RTA21EA 20050927000342005092700034SO 2005 9 27 SIMA200525205 120050828A534714532606015 SEAT TRACK EMB 135 EMB135KL 3260302SO CABIN CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21817AE 145554 SAW - DURING CPCP INSPECTION, FOUND LEFT UPPER 4TH SEAT TRACK FROM FRONT IS CORRODED AROUND SCREW HOLES. REPLACED SEAT TRACK IAW EMB AMM 53-01-06-400-801A. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050927000352005092700035EA 2005 9 27 ASOA05722 120050825A5240 FITTING CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11839AS 7284 DURING A C-CHECK IN MCN, THE FORWARD ANCHOR FITTING ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE FORWARD ANCHOR FITTING ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20050927000392005092700039EU 2005 9 27 ASOA05724 120050828A3230 BRACE AEROSPATR72 ATR72212 8680945EU LT MLG DAMAGED A ASOAO OTHER J WARNING INDICATION APAPPROACH 1 SO11641AS 387 FLT 4089 - DURING APPROACH INTO ATL FROM AGS, UPON SELECTING GEAR DOWN, THE LEFT MAIN LANDING GEAR INDICATED UNSAFE ON BOTH LANDING GEAR PANELS. THE AIRCRAFT PERFORMED A GO AROUND TO COMPLY WITH THE QRH. AN EMERGENCY WAS DECLARED AND EMERGENCY VEHICLES WERE REQUESTED. THE AIRCRAFT LANDED SAFELY IN AT. MAINTENANCE REMOVED AND REPLACED THE UPPER ARM ASSEMBLY ON THE SECONDARY BRACE OF THE LEFT MLG IAW ASA EO 72-32-0020A, PART C. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20050927000442005092700044EU 2005 9 27 KBM2005F00252 120050816A2931MA12401 PRESSURE SWITCH SNIAS 350 AS350B2 8680813EU HYD SYSTEM FAILED E KBMAO OTHER N FALSE WARNING NRNOT REPORTED 1 WP19884SH 2884 HYDRAULIC PRESSURE LIGHT STAYED ILLUMINATED AFTER RUN UP CHECK OF HYDRAULIC ACTUATORS. (M) 1G71 3U H9EU 20050927000492005092700049NM 2005 9 27 USAAA051049 120050824A5320 FLOOR SUPPORT BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19449US 24893 CLT - FOUND FLOOR SUPPORT STRINGER CORRODED, RBL 13.80 BETWEEN STATION 794 AND 847. CORROSION LEVEL 1. FABRICATED NEW FLOOR SUPPORT STRINGER AND INSTALLED PER TR 53-10-08 AND 51-10-02. (M) 2L72 4F RTA16WE 20050927000512005092700051NM 2005 9 27 USAA051053 120050824A575365C26602218 WEDGE BOEING737 7373B7 1384580NM TE FLAPS DENTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US 23933 CLT - FOUND WEDGE WITH DENT 4 INCH BY 5 INCH, BOTTOM OF THE WEDGE AT THE OUTBOARD TRAILING EDGE. REMOVED DAMAGE, INSTALLED A NEW CORE AND DOUBLER IAW EA 96745. (M) 2L72 4F RTA16WE 20050927000562005092700056EA 2005 9 27 ASOA05723 120050828A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11920EV 7810 DURING A GROUND INSPECTION IN CAE, THE LEFT MOST AFT EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE LEFT MOST AFT EXTERIOR EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050927000612005092700061EU 2005 9 27 ASOA05705 120050727A5340 ATTACH FITTING AEROSPATR72 ATR72212 8680945EU FR 27 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11636AS 375 DURING A C-CHECK IN YUL, THE FUSELAGE TO WEB ATTACH FITTING BRACKET AT FRAME 27, STRINGER 14 RIGHT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FUSELAGE TO WEB ATTACH FITTING BRACKET AT FRAME 27, STRINGER 14 RT IAW ATR-72 SRM 51-25-01 AND 51-25-04. (M) 2H72 4T RTA53EU 20050927000692005092700069SO 2005 9 27 SIMA200523504 120050811A532014522178005 SILL EMB 135 EMB135LR 3260305SO SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21710TB11880 145224 THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED CENTER SILL. INSTALLED A NEW SILL IAW EMB SRM, SRM 145/1142 REV 30, CHAPTERS 51-40-02, 51-20-03, 51-40-06. (M) 2L72 4F RTT00011AT 20050927000722005092700072SO 2005 9 27 SIMA200522003 120050729A532014527614001 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO FR 27 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21816AE 145552 SAW - DURING IMBV INSPECTION, FOUND RIGHT OMEGA BEAM CORRODED AT FRAME 27 AT CROSSBEAM ATTACH POINT. REPAIRED RIGHT OMEGA BEAM WITH DOUBLER IAW SRM 53-22-10 FIGURE 201 SHEET 1. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050927000752005092700075NM 2005 9 27 USAA051054 120050824A573065C26603138A SKIN BOEING737 7373B7 1384580NM WING CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US50585 23933 CLT - FOUND SKIN CRACKED 12 INCHES, IMMEDIATELY AFT OF SLAT ACTUATOR. REMOVED DAMAGE AND INSTALLED SPACER AND DOUBLER IAW SRM 57-43-01. (M) 2L72 4F RTA16WE 20050927000782005092700078NM 2005 9 27 C7WA200500116 120050824A326031886301001034 INDICATOR BOEING727 7272M7 138407SNM MLG INOPERATIVE A C7WAO OTHER P NO WARNING INDICATION NRNOT REPORTED 1 SO17742RW 21952 NOSE LANDING GEAR DOWN AND LOCKED INDICATOR LIGHT FAILED TO ILLUMINATE UPON GEAR EXTENSION. FOLLOWED ABNORMAL PROCEDURES, LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NOSE LANDING GEAR GREEN LIGHT ASSEMBLY PER MM 33-10-51. OPS CHECKS GOOD. (M) 2L73 4F A3WE 20050927000852005092700085SO 2005 9 27 SIMA200523505 120050816A532014521713005 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21711PH 145235 THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED THE CORROSION BY MAKING TWO CUT OUTS. FABRICATED A REPAIR CHANNEL TO COVER BOTH CUTOUTS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2005-145/4307 DATED AUGUST 12, 2005. (M) 2L72 4F RTT00011AT 20050927000882005092700088SO 2005 9 27 SIMA200524103 120050824A5320 SILL EMB 135 EMB135KL 3260302SO SERVICE DOOR DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21858AE 145754 THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. BLENDED THE SILL TO REMOVED THE DAMAGE. APPLIED ALODINE, EPOXY PRIMER AND POLYURETHANE PAINT TO BLENDED AREA. FILLED THE BLENDED AREA WITH HYSOL 9394 RESIN AND CURED. FABRICATED TWO DOUBLERS. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 30, CHAPTER 53-21-02 PARA 2. (M) 2L72 4F RTT00011AT 20050927000942005092700094SO 2005 9 27 SIMA200525210 120050828A532014522459003 INTERCOSTAL EMB 135 EMB135KL 3260302SO FR 20 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21817AE 145554 SAW - DURING CPCP INSPECTION, FOUND RIGHT INTERCOSTAL FOR AISLE RAMP AT FRAME 20 IS CORRODED. INSTALLED NEW INTERCOSTAL IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050927000952005092700095SO 2005 9 27 SIMA200525215 120050829A321314521680003 HOUSING EMB 135 EMB135KL 3260302SO NLG CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21817AE 145554 SAW - DURING MBV INSPECTION, FOUND NOSE LANDING GEAR LEFT STRUT DRAG BRACE BEARING HOUSING SHOWS SIGNS OF PITTING. REWORKED BEARING HOUSING TO WITHIN LIMITS IAW SRM 53-11-08 PAGE 101. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050927000982005092700098EA 2005 9 27 A6WA200540297 120050906A3350 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31418AW 7618 TRACK LIGHTING IS INOPERATIVE AT FORWARD CABIN. REMOVED AND REPLACED POWER SUPPLY CABLE, FLOOR TRACK LIGHT AND CONNECTOR IAW CRJ AMM 33-51-01-400 AND CRJ200 WM 20-17-10. OPERATIONAL CHECK GOOD AT THIS TIME. (M) 2L72 4F RTA21EA 20050927001032005092700103EU 2005 9 27 KBM2005F00240 120050801A2435150SG122Q STARTER GEN SNIAS 350 AS350B2 8680813EU ENGINE NOISY E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19351WM 2167 STARTER GEN MAKING GRINDING NOISE. REMOVED AND REPLACED STARTER GEN. (M) 1G71 3U H9EU 20050927001062005092700106SO 2005 9 27 SIMA200524107 120050823A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO FS 20 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21824AE 145584 A PREVIOUS REPAIR, REF FAA FOR 337 DATED DEC 9, 2004, OF THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. REMOVED THE EXISTING REPAIR AND CLEANED THE AREA. FABRICATED A REPAIR PLATE AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, EMB145/1142 REV 30, CHAPTERS 53-00-10 FIG 201. (M) 2L72 4F RTT00011AT 20050927001092005092700109SO 2005 9 27 SIMA2300523511 120050822A2750363500001001 FLAP SYSTEM EMB 145 EMB145LR 3260212SO RT WING FAILED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21641AE 145191 DFW - FLT 3719 - FLAP FAIL AT 9 DEGREES, WOULD NOT MOVE IN EITHER DIRECTION. REPLACED RIGHT FLAP BRAKE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20050927001122005092700112SO 2005 9 27 SIMA20054108 120050824A5320145425381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO FS 25 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21824AE 145584 ABI - THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 25. REMOVED THE CORROSION BY MAKING A CUTOUT. FABRICATED A FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 30, CHAPTER 53-00-10. (M) 2L72 4F RTT00011AT 20050927001132005092700113EA 2005 9 27 ASOA05675 120050819A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11839AS 7284 DURING A C-CHECK IN MCN, THE FLOOR SUPPORT ANGLE AT FS 280, LBL 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FLOOR SUPPORT ANGLE AT FS 280, LBL 9 IAW ASA EO 600-53-0309. (M) 2L72 4F RTA21EA 20050927001152005092700115EA 2005 9 27 ASOA05668 120050816A5210601R3170767 STEP CNDAIRCL600 CL6002C10 1390015EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11730EV 10141 DURING A C-CHECK IN MCN, THE BOTTOM STEP ON PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE BOTTOM STEP ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20050927001232005092700123SO 2005 9 27 SIMA200517107 120050818A335078241 INVERTER EMB 135 EMB135KL 3260302SO EMERGENCY LIGHT INOPERATIVE A SIMAO OTHER O OTHER TXTAXI/GRND HDL 1 SW21804AE 145487 EMERGENCY EXIT SIGN FOR OVERWING EXIT INOPERATIVE. REPLACED INVERTER NR 6 IAW EMB MM 33-50-11. OPERATIONAL CHECK GOOD. REMOVED AND REPLACED BATTERY POWER SUPPLY NR 4 (BT 8503) IAW EMB MM 33-50-04. OPERATIONAL CHECK GOOD, P/N 20131A S/N 63075. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050928000062005092800006SO 2005 9 28 SIMA200524501 120050830A33502013BR BATTERY PACK EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21684JW 14500835 CREW REPORTED AFTER NORMAL SHUTDOWN EMERGENCY LIGHTS AT ROWS 8 THROUGH 12. MAINTENANCE REMOVED AND REPLACED THE NR 3 BATTERY PACK IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20050928000162005092800016EU 2005 9 28 ASOA05711 120050729A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU FR 39-40 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11636AS 375 DURING A C-CHECK IN YUL, THE SEAT TRACK BETWEEN FRAME 39 TO FRAME 40 RIGHT WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK BETWEEN FRAME 39 TO FRAME 40 RIGHT IAW ATR 72 SRM 51-25-04. (M) 2H72 4T RTA53EU 20050928000232005092800023EA 2005 9 28 ASOA05726 120050829A5330 DOUBLER CNDAIRCL600 CL6002B19 1900309EA BS 718 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11834AS 7254 DURING A C-CHECK IN MCN, THE DOUBLER AT FS 718, STRINGER 11 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE DOUBLER AT FS 718, STRINGER 11 IAW ASA EO 600-53-0067A. (M) 2L72 4F RTA21EA 20050928000282005092800028NM 2005 9 28 USAA050999 120050810A5340 ANGLE BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19449US41152 24893 CLT - FOUND ZEE ANGLE CORRODED 3.5 INCHES, SCREW HOLES ON THE SURFACE OF THE LEFT SUPPORT ZEE ANGLE AT LBL 20.20. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW 53-40-01. (M) 2L72 4F RTA16WE 20050928000292005092800029EU 2005 9 28 USAA050931 120050802A5347D5311278220201 SEAT TRACK AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19723UW17735 1109 PIT - FOUND SEAT TRACK CORRODED 1 INCH DIAMETER, Y-765, ABOVE C-20. DEFECTIVE PART REPLACED WITH IDENTICAL PART. (M) 2L72 4F RTA28NM 20050928000392005092800039EA 2005 9 28 ASOA05735 120050830A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11834AS 7254 DURING A C-CHECK IN MCN, THE FS 280 FRAME, RBL 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FS 280 FRAME, RBL 9 IAW ASA EO 600-53-0318. (M) 2L72 4F RTA21EA 20050928000442005092800044SO 2005 9 28 SIMA200521610 120050728A532014522178005 SILL EMB 135 EMB135KL 3260302SO SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21815AE 145545 ABI - THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED CENTER SILL. INSTALLED SERVICEABLE SILL IAW EMB SRM, SRM 145/1142 REV 30, CHAPTER 51-40-02. (M) 2L72 4F RTT00011AT 20050928000452005092800045NM 2005 9 28 USAA051011 120050817A5314 KEELBEAM BOEING737 7373B7 1384580NM BS 664-727 WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US 23933 CLT - FOUND CHORD WITH 60 INCHES OF WEAR, KEEL BEAM LEFT OUTBOARD FLANGE STATION 664-727. REMOVED DAMAGED AREAS, FABRICATED AND INSTALLED FILLER PLUGS IAW EA 96777. 2L72 4F RTA16WE 20050928000472005092800047EA 2005 9 28 ASOA05720 120050824A5210601R319805 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11820AS 7188 FLT 4368 - DURING A GROUND INSPECTION IN ATL, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050928000492005092800049EA 2005 9 28 A6WA200540296 120050830A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA LT WING CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31467AW 7900 LEFT WING LOWER WING FUEL TANK ACCESS DOOR CUTOUT FOR 510AB HAS CORROSION LESS THAN .004 INC DEEP IN SEVERAL AREAS. MAINTENANCE REMOVED CORROSION, PERFORMED NDT ROTO-PEENED AND APPLIED SURFACE TREATMENT IAW REO 601R-57-21-030 REV D. (M) 2L72 4F RTA21EA 20050928000522005092800052NM 2005 9 28 USAA051001 120050815A53226940710511 SHEAR TIE BOEING737 7373B7 1384580NM BS 727A-727B CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US 23933 CLT - FOUND SHEAR TIE CORRODED .5 INCH BY 2 INCH, RBL 3, BETWEEN BS 727A AND 727B FRAMES AFT CARGO AREA. CORROSION LEVEL 1. DEFECTIVE PART REPLACED WITH IDENTICAL PART, IAW BOEING DWG 69-40710 AND SRM 51-10-02. (M) 2L72 4F RTA16WE 20050928000682005092800068NM 2005 9 28 SB05121 120050924A335020131A BATTERY PACK BOEING737 7374B7 1384702NM EMERGENCY LIGHT DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19440US 24811 CLT - DURING EMERGENCY LIGHT OPERATIONAL TEST, MAINTENANCE REPORTED THE LEFT AFT OVERWING EXIT LIGHT ON THE SIDEWALL EXTINGUISHED AND WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK FOR CHARGER ASSEMBLY M1435 PER MM 33-51-51. OPERATIONAL TEST GOOD. 2L72 4F RTA16WE 20050928000732005092800073NM 2005 9 28 05FDEA03058 120050922A5311 FRAME BOEING727 727232 1384082NM BS 520 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 FORWARD CARGO BAY, FRAME IS DENTED ON IB FLANGE AT BS 520 BETWEEN STRINGER 24 RT AND 26RT. REPAIRED FRAME AT B.S. 520 STR 24R & 26R PER SRM 51-40-3. 2L73 4F A3WE 20050928000762005092800076NM 2005 9 28 05FDEA03061 120050922A5310 STRINGER BOEING727 727200 138407ENM ZONE 200 MISREPAIRED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25464FE 21288 IMPROPER STRINGER SPLICE AT STR 23R BETWEEN STA 680 TO 720. REMOVED, FABRICATED, ALODINED, PRIMED AND INSTALLED STRINGER REPAIR AT STA 680 TO 720 ON STRINGER 23R ALL IAW FX B727 SRM 53-10-3, 51-30-2 AND 51-10-2. 2L73 4F RTA3WE 20050928000792005092800079NM 2005 9 28 05FDEA03064 120050922A5330 SKIN BOEING727 727225 1384077NM ZONE 100 MISREPAIRED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25464FE 21288 EXTERNAL SKIN DOUBLER AT STA 950B STRINGER 28R REQUIRES EVALUATION. REMOVED IMPROPERLY INSTALLED DOUBLER, FABRICATED AND INSTALLED NEW DOUBLER IAW B727 SRM 53-30-3, 51-10-2, 51-30-2, 53-30-2. 2L73 4F A3WE 20050928000862005092800086EU 2005 9 28 UPS05145483 120050907A5753A57960000007 SKIN AIRBUSA300 A300F4622R 3930360EU RT WING TE FLAP CHAFED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01125UP 0809 RT INBD FLAP TOP MID FWD CHAFING. REPAIRED FLAP IAW A300 SRM 57-50-00 FIG 205 AND 51-25-00. 2L72 4F RTA35EU 20050928000932005092800093EA 2005 9 28 REXA200500124 120050924A2750855D10011 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A REXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25827AY 8027 FLAPS FAIL AT ZERO ON CLIMBOUT. 2L72 4F RTA21EA 20050928000942005092800094EA 2005 9 28 REXA200500125 120050924A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A REXAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO258505Q 7505 FLAP FAIL ON TAXI OUT. RESET AND PLACED ON 72 HOUR WATCH PER AD98-20-01. 2L72 4F RTA21EA 20050928001002005092800100NM 2005 9 28 SWAA052898 120050924A53226546529 SHEAR TIE BOEING737 7373H4 1384600NM BS 500 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500, RBL 12. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050928001032005092800103NM 2005 9 28 SWAA052901 120050924A53306545768 SKIN BOEING737 7373H4 1384600NM BS 370 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29327SW 23691 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 370, STR 15R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050928001142005092800114NM 2005 9 28 SWAA052912 120050924A53116546555 FRAME BOEING737 7373H4 1384600NM BS 867 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29618WN 28034 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R TO STR 9. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050928001162005092800116NM 2005 9 28 SWAA052914 120050924A53116546548 FRAME BOEING737 7373H4 1384600NM BS 747 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29618WN 28034 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L TO STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050928001182005092800118NM 2005 9 28 SWAA052916 120050924A53116546554 FRAME BOEING737 7373H4 1384600NM BS 847 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29618WN 28034 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 847, RBL 21. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050928001192005092800119 2005 9 28 SWAA052917 420050924A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29645SW 28330 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050928001202005092800120 2005 9 28 SWAA052918 420050923A25656557463 FITTING BOEING737 7373H4 1384600NM GIRT BAR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29652SW 27722 R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET OUT OF ADJUST. ADJUSTED BRACKET PER MM. 2L72 4F RTA16WE 20050928001212005092800121NM 2005 9 28 SWAA052919 120050923A53306545774 SKIN BOEING737 7373Q8 1384670NM BS 767 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 19L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050928001272005092800127WP 2005 9 28 IXXA05RNG055S 120050903A5340 FITTING DOUG DC8 DC872 302199BWP STA 902 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX 46013 DURING INSPECTION CHECK, FOUND A CRACKED FITTING, LONGERON 24 STA 902 LT. REPAIR WILL BE MADE IAW EWO ATI 53-014 AND SRM 53-2-2 FIG 5 TEMPORARY REVISION 53-123. 2L74 4F RT4A25 20050928001302005092800130NM 2005 9 28 05FDEA03067 120050923A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 CRACK INDICATION FOUND AT STRINGER END OF STRINGER 10 (UPPER STRINGER), APPROXIMATE LENGTH 11.5 INCHES, LEFT SIDE WING TANK. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. 2L73 4F RTA22WE 20050928001312005092800131EA 2005 9 28 COMA0560515 120050921A5312601R32026 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA RT WHEEL WELL CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01949CA25733 7080 WHILE PERFORMING TASK CRJ-2-162014, DETAILED INSPECTION OF THE PRESSURE BULKHEAD WEBS AND VERTICAL BEAMS AT FS 559.0, TWO CRACKS WERE DISCOVERED IN THE BULKHEAD WEB RADIATING FROM THE HOLES FOR THE ATTACH BOLTS OF THE RIGHT AILERON CONTROL CABLE REAR QUADRANT MOUNT BRACKET AT RBL 23. REPAIRED BULKHEAD WEB PER REO 601R-53-41-260 REV A. 2L72 4F RTA21EA 20050928001332005092800133EA 2005 9 28 COMA0560513 120050920A215078279015 ACM CNDAIRCL600 CL6002B19 1900309EA LEFT LEAKING A COMAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SO01865AS11013 7507 FLIGHT 5792 - SMOKE TOILET CAUTION. REPLACED THE LT ACM. 2L72 4F RTA21EA 20050928001432005092800143EU 2005 9 28 DXTA200500980 120050923A282131B370201 FUEL FILTER ISRAELGALAXYGALAXY 4500307EU PWA 306 PW306B NE LT ENGINE CLOGGED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07700QS 052 PCECCO142 LEFT FUEL PRESS, LOW CAS MESSAGE ILLUMINATED ON TAKEOFF ROLL. ABORTED TAKEOFF AT 75 KNOTS. REPLACED FUEL FILTERS (BOTH ENGINES) AND LEAK CHECKED, NO LEAKS NOTED. OP'S CHECKED FUEL SYS FOR PRESS LOW CAS MESSAGE. SYS OP'S CHECKS GOOD, REF PW MAINT MAN 73-00-00. 2L72 4F4 FRTA53NM E35NE 20050928001452005092800145CE 2005 9 28 DXTA200500982 120050925A3240 BRAKE CESSNA500 560CESSNA 2076750CE MLG MALFUNCTIONED E DXTAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07377QS 5600377 AFTER LANDING, BRAKE PEDALS LOST PRESSURE AND THE AIRCRAFT LOST BRAKING EFFECTIVENESS AT 50KIAS, REGAINED AGAIN AT A LOWER SPEED, THEN LOST AGAIN DURING TAXI. 2L72 4F RTA22CE 20050928001462005092800146NM 2005 9 28 05FDEA03079 120050923A3220 BUSHING DOUG MD11 MD11 3023602NM ZONE 700 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 NOSE LANDING GEAR, GROUND SENSING CRANK ASSY, FOUND WITH PLAY. CARRIED OUT BUSHING REPAIR AS PER FEDEX EA 1-3220-90020. 2L73 4F RTA22WE 20050928001492005092800149NM 2005 9 28 P5CA0501400 120050922A5740 FITTING BOEING747 747283B 1384867NM LT WING CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 EA15921FT 21575 LEFT WING AT UPPER CHORD OF SPLICE FITTING OF WING REAR SPAR HAS CORROSION BETWEEN WS 553 AND WS 558. CORROSION BLENDED OUT IAW SRM 57-30-01. HFEC & ULTRASONIC INSPECTION OF AREA CONFIRMED REMOVAL OF CORROSION IAW NDT 06-7170 PT 6, 51-00-00 FIG 23, 12. D6-7170 PT4. 2L74 4F A20WE 20050928001532005092800153NM 2005 9 28 PIDA20050141 120050923A5280 SKIN BOEING737 7373Y0 1384671NM MLG DOOR DELAMINATED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05373PA BN271 23749 DELAMINATION IN INNER AND OUTER SKIN OF RIGHT CENTER MLG DOOR. REPAIRED DOOR PER EA 52-250. 2L72 4F RTA16WE 20050928001622005092800162NM 2005 9 28 SWAA052932 120050926A53306545776 SKIN BOEING737 7375H4 138449DNM BS 944 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29522SW 26564 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 944, STR 24L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050928001652005092800165NM 2005 9 28 SWAA052935 120050926A53116546558 FRAME BOEING737 7373H4 1384600NM BS 907 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29618WN 28034 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R TO STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050928001682005092800168WP 2005 9 28 IXXA05RNG064S 120050913A5330 SKIN DOUG DC8 DC872 302199BWP BS 1500-1530 MISREPAIRED B IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW11721CX 46013 DURING INSPECTION CHECK, FOUND A IMPROPER REPAIR ON FUSELAGE SKIN STA 1500-1530, LONG 17-21, LT. DAMAGE WILL BE REPAIRED IAW EWO ATI-53-017 AND FAA FORM 8110-3 MUST BE ISSUED. 2L74 4F RT4A25 20050928001692005092800169WP 2005 9 28 IXXA05RNG060S 120050912A5330 SKIN DOUG DC8 DC872 302199BWP BS 640-660 CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX 46013 DURING INSPECTION CHECK, FOUND A CORROSION ON INTERNAL SKIN OF PASSENGER WINDOW STA 640-660, RT. DAMAGE WILL BE REPAIRED IAW EWO ATI-53-018 AND SRM 53-2-0 FIGURE 22A TR-53-170. 2L74 4F RT4A25 20050928001792005092800179EA 2005 9 28 COMA0560524 120050926A2750860D10018ABCD CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01814CA6238 235 7387 FLIGHT 5301- FLAPS FAIL CAUTION. CND, REPLACED THE FECU. 2L72 4F RTA21EA 20050928001822005092800182EA 2005 9 28 COMA0560522 120050925A3610 SHUTOFF VALVE CNDAIRCL600 CL6002B19 1900309EA LT BLEED SYSTEM INOPERATIVE A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01473CA 7668 FLIGHT 5528 - LEFT BLEED AIR WILL NOT OPEN. CND, OPERATIONAL CHECK NORMAL. 2L72 4F RTA21EA 20050928001892005092800189SO 2005 9 28 C2XA05TY054 120050918A531114524061008 FRAME EMB 145 EMB145 3260210SO FR 18 CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2727962 145110 TYS - DURING A SCHEDULED INSPECTION, A CRACK INDICATION WAS FOUND ON THE OUTBOARD UPPER DOOR STOP HOLE AT FRAME 18, STRINGER 14L, CRACK IS AT 9 O'CLOCK HOLE POSITION AND GREATER THAN 50 PERCENT OF STANDARD DEFLECTION. MAINTENANCE REAMED THE DOOR STOP HOLE IAW EA5310-01054 AND EC5310-01351 AND CRACK INDICATION WAS REMOVED. 2L72 4F RTT00011AT 20050928001902005092800190SO 2005 9 28 C2XA05SH113 120050920A532014532638401 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO FR 28 CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713992 145284 SHV - DURING C-CHECK, THE LEFT OMEGA BEAM CRACKED AT SUPPORT ANGLE FRAME 28. MAINTENANCE REPAIRED LEFT OMEGA BEAM AT SUPPORT ANGLE FRAME 18 IAW EC5320-01261. THE AIRCRAFT WAS APPROVE FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050928001922005092800192SO 2005 9 28 C2XA05CL084 120050922A28102810051104 VALVE EMB 145 EMB145XR 3260214SO FUEL VENT LEAKING A C2XAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW27241035053 145645 CLE FLIGHT NR 2693, THE CREW REPORTED A FLUID LEAK FROM THE NR 1 WING. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 WING FUEL VENT VALVE. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RT 20050928001972005092800197NM 2005 9 28 2005UALA00997 120050917A33501317 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29187UA 26877 UPPER DECK FLT DECK CEILING EMERGENCY LIGHT INOP. REPLACED LAMP. 2L74 4F4 FRTA20WE E24NE 20050929000022005092900002NM 2005 9 29 05FDEA03066 120050922A5330 DOUBLER BOEING727 727225 1384077NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 CORROSION FWD PIT BETWEEN STA 720E AND STA 720F INTERIOR SKIN BETWEEN STRINGER 29R AND STRINGER 28R. REMOVED CORROSION FOUND OUT OF LIMITS ORIG MAT .100 MAT. REMAINING .038, REMOVED DAMAGE, FABBED REPAIR DBLR. LOCATED AND DRILLED, ALODINED, PRIMED, INSTALLED DOUBLER IAW B727 SRM 53-30-1, SRM 51-10-6, SRM 53-30-3 FIG 1, SRM 53-30-2, SRM 53-30-2. 2L73 4F A3WE 20050929000112005092900011NM 2005 9 29 BB05084 120050925A335020131A BATTERY PACK BOEING757 757225 1384959NM EMERGENCY LIGHT DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19606AU 22202 BDL - THE FORWARD CABIN EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE FORWARD EMERGENCY LIGHT BATTERY PACK. OPERATIONALLY CHECKS OK. 2L72 4F RTA2NM 20050929000132005092900013NM 2005 9 29 AWXA200501116 120050924A2910 LINE BOEING737 7373G7 1384595NM HY SYSTEM RUPTURED A AWXAL ABORTED APPROACH KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 WP28156AW 23778 CREW REPORTED SYS "A" HYD FAILURE ON FINAL WHEN LOWERING GEAR. LT GEAR INTRANSIT INDICATION ILLUMINATED. MANUALLY EXTENDED GEAR AND RECEIVED THREE GREEN GEAR DOWN AND LOCKED INDICATION. TOWER VERIFIED ALL THREE GEARS WERE DOWN. A/C LANDED WITH NO NLG STEERING. A/C TOWED TO GATE. MX R&R A RUPTURED PRESSURE FLEX LINE FOR LT MLG UPLOCK ACTUATOR. FLEX LINE RUPTURED AGAIN DURING OPS TESTS. MX R&R LT MLG UPLOCK ACTUATOR, PRESSURE FLEX LINE, & LT MLG MODULE. OPS TESTS GOOD. CONFIRMED FAILURE. VENDOR FOUND UNIT TO FAIL INCOMING TEST. UPON DISSASEMBLY UNIT WAS FOUND TO HAVE PACKING WORN. UNIT WAS OVERHAULED & A NEW SET OF PACKING WERE INSTALLED. PASSED FUNCTIONAL TESTS. WORK PERFORMED IAW CMM 65-44691-5. 2L72 4F RTA16WE 20050929000142005092900014NM 2005 9 29 AWXA200501117 120050924A2910 PTU AIRBUSA319 A319132 3930340NM HYD SYSTEM NOISY A AWXAO OTHER J WARNING INDICATION DEDESCENT 1 WP28821AW 1406 EMERGENCY LANDING - FLT 113 - DURING DESCENT, CREW NOTICED NOISE COMING FROM PTU. DESELECTED PTU AND RECEIVED HYD Y ENG PUMP LO PR MSG. MADE EMERGENCY LANDING IN LAX, LANDED WITHOUT FURTHER EVENT. TAXIED TO THE GATE. MX TROUBLESHOT AND TESTED THE YELLOW ENGINE DRIVEN PUMP, NR 2 ENGINE, IAW AIRBUS 319/320 TSM 29-13-00-710-002. ALSO, TROUBLESHOOT AND TESTED YELLOW HYD PSI SWITCH IAW AIRBUS 319/320 TSM 27-97-00-810-828A. COULD NOT DUPLICATED DISCREPANCY AND NO FAULTS WERE FOUND. 2L72 4F RTA28NM 20050929000182005092900018NM 2005 9 29 DHL2005748505 120050815A5330 SKIN BOEING727 727225 1384077NM BS 460 DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 REFERENCE FLIGHTSTAR AIRCRAFT SERVICES NR 109558, FUSE HAS A DENT BS 460 ABOVE STR 26R. CUT OUT DAMAGED AREA DIMS 3" BY 3 1/2 AND FABRICATED REPAIR DOUBLER FROM MATERIAL USE 2024T3 .080 PO NR 900-2255 AND FILLER FROM MATERIAL USE 2024T3 .080 PO NR 900-22-55 DIMS 10" BY 5" IAW B727 SRM 53-30-3 FIG NR 14 TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED NEW DOUBLER AND FILLER IAW B727 SRM 53-30-3 FIG 14, REPAIR IS A CAT B. 2L73 4F A3WE 20050929000212005092900021NM 2005 9 29 XN0A1268 120050925A2782 ACTUATOR BOEING727 727173C 1384059NM NR 3 SLAT LEAKING A XN0AO OTHER K FLUID LOSS NRNOT REPORTED 1 GL23704A 19504 LOSS OF HYDRAULIC SYSTEM "A" QUANTITY TO ZERO. REMOVED AND REPLACED LT NR 3 STAT ACTUATOR LEAK AND OPS CHECK GOOD IAW MM 27-81-32. 2L73 4F A3WE 20050930000112005093000011NM 2005 9 30 DHL2005748511 120050814A5322 SHEAR TIE BOEING727 727225 1384077NM BS 950F CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 AFT CARGO COMPARTMENTS CORROSION AT SHEAR TIE STA 950F BETWEEN STR 30 29L (MARKED). CUT OUT DAMAGED AREA 6 1/8 BY 1" IAW B727 SRM 53-10-4 FIG 13. FAB DOUBLER 6 1/2 BY 3 AND FILLERS (2" BY 1") (4 BY 1/2) AND (1" BY 4") MAT ID 7075T6 .071 PO5096275 IAW B727 SRM 53-10-4 FIG 13 TREATED PRIMED IAW B727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B727 SRM 51-30-2 AND 53-10-4 FIG 13. 2L73 4F A3WE 20050930000142005093000014NM 2005 9 30 DHL2005748508 120050815A5753 SKIN BOEING727 727225 1384077NM FORE FLAP DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 L/WING I/B FORE FLAP I/B END DELAM. CUT OUT DELAMINATED AREA OF UPPER I/B END OF L/WING I/B FOREFLAP APPROX 3 1/2" BY 14" AFTER RUBSTEP REMOVAL CUT OUT DAMAGED CORE APPROX 8 1/2" BY 2 3/4" FABBED SEPTUM APPROX 8 1/2" BY 2 3/4" REPAIR SKIN APPROX 3 1/2" BY 14" AND EXTERNAL DOUBLER APPROX 5 1/4" BY 15" FROM 2024T3 .016 PO NR 9002273 AND REPAIR CORE APPROX 8 1/2" BY 2 3/4" FROM 5052-4.4-3/16-N-0.750 PO9911139 CLEANED PREPPED APPLIED ADHESIVE PRIMER AND ADHESIVE MIX TO REPAIR PARTS AND SURFACES VACUUM BAGGED FOR BONDING. BONDED CLEANED TREATED PRIMED AND SEALED REPAIR FABBED REPLACEMENT RUBSTEP APPROX 3" BY 14" FROM 301 1/2 HD .016 PO9002619 AND BONDED IAW B727 MM 51-51-11 B727 SRM 51-40-23 AND 57-50-2 FIG 3. 2L73 4F A3WE 20050930000202005093000020NE 2005 9 30 AALA20050623 220050926A7200 ENGINE AIRBUS300 A300B4605R 3930308EU GE CF6 CF680C2A5 NE NR 2 BIRD INGESTION A AALAA UNSCHED LANDING C F.O.D. CLCLIMB 1 SW217076A 610 695195 MIA INFLIGHT T903/26SEPT - NR 2 ENGINE INGESTED A BIRD DURING CLIMB. EXPERIENCED SOME VIBRATION WITHIN LIMITS. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. PERFORMED BIRD STRIKE INSPECTION AND BOROSCOPE. REPLACED THREE FAN BLADES AND RIGHT TRANSCOWL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA35EU E13NE 20050930000212005093000021NM 2005 9 30 AALA20050625 120050926A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21947AN 29536 TUL - EMERGENCY LIGHTS AT FIRST CLASS SEATS INOPERATIVE. REPLACED BATTERY PACKS FOR EMERGENCY LIGHTS AT FIRST CLASS SEATS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20051003000012005100300001EU 2005 10 3 05FDEA03104 120050925A7931VT0304S TRANSMITTER AIRBUS310 A310222 3930315EU OIL PRESSURE MALFUNCTIONED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25417FE 333 NR 1 ENG HI OIL PRESS, DURING CLIMB POWER, ECAM SELECTED NR 1 OIL PRESS 100 PSI AMBER. NO CAUTION LIGHT ALL OTHER ENG NORMAL. THEN AT FL 280 GOT INTERMITTENT HI PRESS CAUTION LIGHT. THROTTLE RETARDED TO IDLE IN DESCENT THEN OIL PRESS TO 38 PSI, NR 1 AND GOT ENG ADV FOR LOW OIL PRESS. ENG OIL PRESS INDICATOR THEN GREEN 38-48 PSI IN DESCENT. R & R NR 1 ENGINE OIL PRESSURE TRANSMITTER AS PER MM 79-33-11-4-03. RAN NR 1 ENGINE AS PER A310 JRH. ALL INDICATION NORMAL. OPS CHECK "SATIS". 2L72 4F RTA35EU 20051003000052005100300005NM 2005 10 3 DHL2005748523 120050816A5753 ANGLE BOEING727 727225 1384077NM RT WING TE FLAP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 ANGLE CRACKED AT T/E OF RT WING INBD MID FLAP 36" FROM INBD END. CUT OUT CRACKED SECTION OF ANGLE 8 1/2" AND FAB DOUBLER FROM AND 10133-1401, 7075 T6 .063 EXTRUSION 17 3/8" PO501952 FILLER FROM BAC 1509-10861 .050 8 1/2" PO 5079108 IAW B727 SRM 57-50-2 FIG 5 AND SRM 51-40-4 FIG 1. TREATED AND PRIMED FILLER DOUBLER AND REPAIR AREA IAW B727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B727 SRM 51-40-4 FIG 1. 2L73 4F A3WE 20051003000062005100300006NM 2005 10 3 05FDEA03105 120050925A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 CRACK INDICATION FOUND AT STRINGER END OF STRINGER 12 (UPPER STRINGER), APPROXIMATE LENGTH 7 INCHES, RIGHT SIDE WING TANK. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. 2L73 4F RTA22WE 20051003000132005100300013NM 2005 10 3 05FDEA03142 120050927A5315 FLOORBEAM BOEING727 727232 1384082NM BS 1148 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 REMOVAL OF BL 0 TENSION STRAP ON FED EX CARD, FOUND CORROSION ON LWR FLANGE OF FLOORBEAM AT B/S 1148, WL 200 BL 0. REPAIRED FLOORBEAM AT B.S. 1148, BL0, WL 200 PER SRM 53-10-8. 2L73 4F A3WE 20050926001132005092600113NM 2005 9 26 SWAA052882 120050921A53306545766 SKIN BOEING737 7373H4 1384600NM BS 500D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29371SW 26598 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 12R. REPAIRED SKIN PER SRM & SWA EA. 2L72 4F RTA16WE 20050926001192005092600119NM 2005 9 26 05FDEA02998 120050919A575365192509 FLAP TRACK BOEING727 7272S2F 1384O81NM NR 7 FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25211FE 22933 RT WING O/B FLAP I/B TRACK NR 7 HAS SURFACE CORROSION AND SMALL CHAFINGS ON FACES AND ROLLERS SLIDING TRACKS. REMOVED AND REPLACED FLAP TRACK IAW MM 27-51-032-4. 2L73 4F A3WE 20050926001212005092600121EU 2005 9 26 05FDEA03001 120050920A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25681FE 799 SEAT TRACK L2 AT FS 54.2 - 54.3 HAS DAMAGE IN SCALLOP AREA. FABRICATED SEAT TRACK SECTION AND INSTALLED WITH SPLICES (2EA) IAW A300-600 SRM 53-10-16. ALODINED, PRIMED, AND TOPCOATED IAW A300-600 SRM 51-25-10. 2L72 4F RTA35EU 20050926001422005092600142WP 2005 9 26 0501441243 120050915A3213AYG71517 CYLINDER DOUG DC10 DC1030 3023501WP GE CF6 CF650* 30018NE MLG FRACTURED A NWAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL01243NW6546919655 48315 DURING PUSHBACK FOR DEPARTURE A LOUD BANG WAS HEARD AND THE CENTER GEAR STARTED TO RETRACT. THE TOP PORTION OF THE CLG OUTER CYLINDER FRACTURED AND LIBERATED FROM THE MAIN BODY OF THE OUTER CYLINDER. THE LIBERATED PORTION OF THE OUTER CYLINDER WAS FORCED UPWARD DUE TO THE INTERNAL PRESSURE IN THE CYLINDER CAUSING IT TO CONTRACT AND FRACTURE THE UPPER LOCK LINK. REASON FOR FRACTURE FAILURE OF THE OUTER CYLINDER IS AWAITING FURTHER ANALYSIS OF THE FAILED PARTS. 2L73 4F4 F A22WE E23EA 20050926001692005092600169EA 2005 9 26 VNAA0509009 120050912A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS FALSE INDICATIONA VNAAO OTHER N FALSE WARNING APAPPROACH 1 GL05254PS 7935 THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED WITH FLAPS SELECTED TO 20 DEGREES AND INDICATING 8 DEGREES. THE CREW FOLLOWED THE QRH AND LANDED SAFELY. MAINTENANCE PERFORMED FAULT ISOLATION AND RESET PROCEDURES IAW CRJ200 FIM 27-50-00. THE SYSTEM RESET AND NO FURTHER DEFECTS WERE NOTED. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050926001722005092600172NM 2005 9 26 S2Y2005F00001 120050831A32972342530000 WIRE HARNESS DORNERDO32 DO328300 NM PWA 306 PW306B NE NLG STEERING FAILED A S2YAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL13358SK13165 3188 DURING FLIGHT, THE CREW REPORTED A CAS MESSAGE INDICATING THE NOSE WHEEL STEERING (NWS) PROXY FAILED. THE CREW PERFORMED AN AIR-TURN-BACK. MAINTENANCE REPLACED NWS CONTROL VALVE, WIRING HARNESS AND NWS ELECTRICAL CONTROL UNIT (ECU). WITH OPS CHECKS GOOD THE AC WAS RETURNED TO SERVICE. (K) 2H72 4T4 FRTA55NM E35NE 20050926001732005092600173NE 2005 9 26 KNK2005F00002 220050829A73130292208230 INJECTOR SNIAS 350 AS350* EU TMECA ARRIELARRIEL1D1 NE FUEL MANIFOLD COKED E KNKAO OTHER O OTHER NRNOT REPORTED 1 WP13112AK4459 3254 9672 FUEL MANIFOLD INJECTOR COKED UP, UNABLE TO TURN ENGINE. REPLACED FUEL MANIFOLD INJECTOR. (K) 1G71 3U3 U H9EU E19EU 20050926001782005092600178CE 2005 9 26 GAJ2005F00001 120050815A7602565580015 CONTROL CABLE CESSNA206 TU206G 2073357CE CONT O520 TSIO520M 17040SO MIXTURE FROZEN E GAJAO OTHER O OTHER NRNOT REPORTED 1 NM117537N636 U20603665 520247 3/25/04, HOBBS 3218.1, TTAF 9745.1, REMOVED AND REINSTALLED ENGINE, THROTTLE, MISTURE AND PROP CONTROLS. 7/22/04, HOBBS 3417.7, TTAF 9944.0, VERNIER CONTROL RELEASE BUTTON FROZE IN PUSHED POSITION, REMOVED MIXTURE CONTROL CABLE AND REPLACED WITH NEW. 8/12/05, HOBBS, 4054.2 TTAF 10580.5, VERNIER CONTROL RELEASE BUTTON FROZE IN PUSHED IN POSITION, REMOVED MIXTURE CONTROL CABLE AND REPLACED WITH NEW. (K) 1H71 3O3 O A4CE E8CE 20050926001792005092600179NM 2005 9 26 S2Y2005F00002 120050831A3250231800002 ECU DORNERDO32 DO328300 NM PWA 306 PW306B NE NLG STEERING FAILED A S2YAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL13358SK10412 3188 DURING FLIGHT, THE CREW REPORTED A CAS MESSAGE INDICATING THE NOSE WHEEL STEERING (NWS) PROXY FAILED. THE CREW PERFORMED AN AIR-TURN-BACK. MAINTENANCE REPLACED NWS CONTROL VALVE, WIRING HARNESS, AND NWS ELECTRICAL CONTROL UNIT (ECU). WITH OPS CHECKS GOOD, AC WAS RETURNED TO SERVICE. (K) 2H72 4T4 FRTA55NM E35NE 20050926001812005092600181EA 2005 9 26 ASOA05686 120050820A5330 DOUBLER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FS499-516 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27839AS 7284 DURING A C-CHECK, THE DOUBLERS AT FS 499 TO FS 516, LBL 44 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO MFG FOR ISSUANCE OF AN REO TO DETERMNE THE APPROPRIATE CORRECTIVE ACTION. (K) 2L72 4F4 FRTA21EA E15NE 20050926001842005092600184CE 2005 9 26 S2YA05050 120050827A21211143800289 BLOWER BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA CABIN SMOKE A S2YAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL1381SK 1165 UE81 SHORTLY AFTER TAKEOFF, THE CREW REPORTED AN ELECTRICAL BURNING SMELL. AFTER CONSULTING WITH DISPATCH AND MAINTENANCE, THE CREW PERFORMED AN AIR-TURN-BACK. MAINTENANCE INSPECTED THE AC AND FOUND THE FORWARD CABIN BLOWER INOPERATIVE AND SMELLED OF BURNED. MAINTENANCE REPLACED THE BLOWER AND WITH NO FURTHER DEFECTS RETURNED THE AC TO SERVICE. (K) 2L72 4T3 TRTA24CE E2NE 20050926001852005092600185CE 2005 9 26 S2YA05052 120050830A561010138402523 WINDSHIELD BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE COCKPIT CRACKED A S2YAO OTHER O OTHER CRCRUISE 1 GL13831SK4338 UE83 DURING FLIGHT, THE CREW REPORTED THE CAPTAINS WINDSHIELD HAD CRACKED IN SEVERAL PLACES. THE FLIGHT CONTINUED WITH NO OTHER DISCREPANCIES. MAINTENANCE REPLACED THE LT WINDSHIELD. WITH NO FURTHER DEFECTS RETURNED THE AC TO SERVICE. (K) 2L72 4T4 TRTA24CE E26NE 20050926001952005092600195 2005 9 26 S2YA05049 420050826A3416066030620008 ALTIMETER BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA COCKPIT INOPERATIVE A S2YAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 GL1381SK 230718917 UE81 SHORTLY AFTER TAKEOFF, THE CREW REPORTED THE FLAPS WILL NOT RETRACT AND THE CAPTAINS ALTIMETER FAILED. MAINTENANCE CLEANED AND ADJUSTED THE LT SPLIT FLAP SWITCH AND SUCCESSFULLY OPS CHECKED THE FLAPS. MAINTENANCE REPLACED THE PILOTS ALTIMETER AND OPS CHECKED GOOD WITH NO FURTHER DEFECTS RETURNED AC TO SERVICE. NEXT DAY, SHORTLY AFTER TAKEOFF, THE CREW REPORTED THE FLAPS WILL NOT RETRACT. AFTER CONSULTING WITH DISPATCH AND MAINTENANCE, THE CREW PERFORMED AND AIR-TURN-BACK. MAINTENANCE REPLACED THE RT SAFETY SWITCH LINK AND CAM, OPS CHECKED THE SYSTEM AND WITH NO FURTHER DEFECTS RETURNED AC TO SERVICE. (K) 2L72 4T3 TRTA24CE E2NE 20050926001972005092600197CE 2005 9 26 DYV2005F00000 120050806A2121903840311 BLOWER BEECH 90 C90A 1152911CE PWA PT6 PT6* 52043EA E/E BAY SEIZED E DYVAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM0713GZ 1306 LJ1590 PILOT NOTICED A BURNING SMELL AND SUBSEQUENT SMOKE ACCUMULATION IN THE COCKPIT. AFTER BEING UNABLE TO BE CERTAIN OF THE CAUSE, HE TURNED OFF ALL ELECTRICAL POWER AND LANDED AT OUR MAINTENANCE BASE. THE CABIN ENVIRONMENTAL VENTALATION BLOWER MOTOR WAS FOUND SEIZED AND VERY HOT. THE CIRCUIT IS PROTECTED BY A 30 AMP LIMITER IN THE LT DC POWER PANEL. FURTHER INVESTIGATION IS BEING CONDUCTED TO DETERMINE IF 30 AMPS MAY OR MAY HAVE BEEN EXCEEDED. THE VENT BLOWER MOTOR WAS REPLACED WITH A SERVICEABLE PART AND THE SYSTEM TESTED TO ASSURE NORMAL OPERATIONS. THE AC WAS TEST FLOWN AND RETURNED TO SERVICE WITH NO FURTHER PROBLEMS. (K) 1L72 3T3 TRT3A20 E2NE 20050926001992005092600199SW 2005 9 26 ALG2005F00063 120050819A6320206040004115 TRANSMISSION BELL 206 206L4 1182110SW ALLSN 250C 250C30P 03013GL MAIN ROTOR FAILED E ALGAA UNSCHED LANDING J WARNING INDICATION HOHOVERING 1 SW03175AL 52117 TRANSMISSION CHIP LIGHT ILLUMINATED IN HOVER. MAINTENANCE REMOVED TRANSMISSION, MAST, AND OIL COOLER. A SERVICEABLE TRANSMISSION, MAST AND OIL COOLER WERE INSTALLED. FLUSHED TRANSMISSION OIL SYSTEM. IAW MM. GROUND AND LEAK CHECK, OK. (K) 1G71 3U3 UNCH2SW E1GL 20050927000032005092700003EU 2005 9 27 ASOA05706 120050728A5320 INTERCOSTAL AEROSPATR72 ATR72212 8680945EU FR 36-38 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11636AS 375 DURING A C-CHECK IN YUL, THE INTERCOSTAL BETWEEN FRAME 36 AND FRAME 38 LEFT WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTAL BETWEEN FRAME 36 AND 38 LEFT IAW ATR-72 SRM 51-25-01. (M) 2H72 4T RTA53EU 20050927000052005092700005SO 2005 9 27 SIMA200525209 120050828A531014521725001 SILL EMB 135 EMB135KL 3260302SO FR 22 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21817AE 145554 DURING CPCP INSPECTION, FOUND LEFT CREASE BEAM CORRODED AT FRAME 22. INSTALLED NEW CREASE BEAM IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050927000102005092700010EA 2005 9 27 ASOA05696 120050820A5330 FINGER DOUBLER CNDAIRCL600 CL6002B19 1900309EA BS 523-559 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11839AS 7284 DURING A C-CHECK IN MCN, THE FINGER DOUBLER AT FS 523 TO FS 559, LBL 44 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO BOMBARDIER FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. S/D - MAINTENANCE REMOVED THE CORROSION FROM THE FINGER DOUBLER AT FS 523 TO FS 559, LBL 44 BY COMPLYING WITH ASA EO 600-53-0314. (M) 2L72 4F RTA21EA 20050927000132005092700013EA 2005 9 27 ASOA05695 120050820A5330 FINGER DOUBLER CNDAIRCL600 CL6002B19 1900309EA BS 540-544 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11839AS 7284 DURING A C-CHECK IN MCN, THE FINGER DOUBLER AT FS 540 TO FS 544, RBL 44 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO BOMBARDIER FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. S/D - MAINTENANCE REMOVED THE CORROSION FROM THE FINGER DOUBLER AT FS 540 TO FS 544, RBL 44 BY COMPLYING WITH ASA EO 600-53-0313. (M) 2L72 4F RTA21EA 20050927000162005092700016SO 2005 9 27 SIMA200521616 120050802A532014522178005 SILL EMB 135 EMB135KL 3260302SO SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21856AE4824 145748 ABI - THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. BLENDED THE SERVICE DOOR TO REMOVE CORROSION. FABRICATED TWO DOUBLERS FOR REPAIR. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 30, CHAPTERS 53-21-02. (M) 2L72 4F RTT00011AT 20050927000182005092700018SO 2005 9 27 SIMA200523501 120050812A532014521721009 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21710TB 145224 THE GALLEY FORWARD DIGITAL WAS FOUND TO BE CORRODED. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED A DOUBLER. REPAIR DONE IAW EMB REPAIR IC2005-145/4212 DATED AUGUST 10, 2005. (M) 2L72 4F RTT00011AT 20050927000192005092700019EA 2005 9 27 SIMA200524901 120050903A335020131A POWER SUPPLY CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT DISCHARGED A SIMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW21509AE 10078 FLT 3639 - DFW - CABIN LEFT WING EMERGENCY EXIT LOWER LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA21EA 20050927000232005092700023SO 2005 9 27 SIMA200522702 120050815A2612 FIRE WARNING EMB 135 EMB135KL 3260302SO CARGO BAY FALSE INDICATIONA SIMAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SW21813AE 145539 THE BAGGAGE COMPARTMENT EXTINGUISHER LIGHT ILLUMINATED. THE CAPTAIN DISCHARGED THE BAGGAGE COMPARTMENT FIRE BOTTLES AS A PRECAUTIONARY. THE FIRE DEPT INSPECTED THE CARGO AREA AND FOUND NO EVIDENCE OF SMOKE OR FIRE. RAI HIGH RATE BOTTLE AS PER EMB 140 AMM 26-23-01 AND METERING BOTTLE P/N 34600731, S/N 17924F1. ALL SYSTEMS OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050927000282005092700028EA 2005 9 27 ASOA05719 120050813A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11853AS 7374 DURING A C-CHECK IN HOT, THE LEFT OUTBOARD FS 280 ANGLE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT OUTBOARD FS 280 ANGLE IAW CRJ200 SRM 51-42-21 AND 51-42-02. (M) 2L72 4F RTA21EA 20050927000322005092700032SO 2005 9 27 SIMA200523502 120050812A532014521713005 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO FS 25 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21710TB11880 145224 A PREVIOUS REPAIR ON THE CENTER OMEGA BEAM AT FRAME 25 WAS FOUND TO BE CORRODED. ADDITIONAL CORROSION WAS FOUND ON THE CENTER OMEGA BEAM AT THE GRAPHITE CROSSBEAM. REMOVED THE PREVIOUS REPAIR AND ENLARGED THE CUT OUT. FABRICATED A DOUBLER, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 30 CHAPTERS 53-00-10. (M) 2L72 4F RTT00011AT 20050927000372005092700037EA 2005 9 27 ASOA05737 120050831A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA BS 640 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11841AS 7300 DURING HANGAR MAINTENANCE IN BTR, THE LEFT FS 640, STRINGER 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT FS 640 FRAME IAW THE CRJ SRM AND DEVIATION BOMBARDIER REO 601R-54-51-011. (M) 2L72 4F RTA21EA 20050927000452005092700045EA 2005 9 27 ASOA05663 120050813A2997 WIRE CNDAIRCL600 CL6002B19 1900309EA CONTROL PANEL LOOSE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11829AS 7232 FLT 4403 - DURING APPROACH INTO HSV FROM ATL, THE CREW RECEIVED A NOSE GEAR DISAGREE MESSAGE. THE AIRCRAFT PERFORMED A GO AROUND TO COMPLY WITH THE QRH. AN EMERGENCY WAS DECLARED AS A PRECAUTION AND THE AIRCRAFT LANDED SAFELY IN HSV. MAINTENANCE FOUND A LOOSE GROUND WIRE TO THE 3B TOGGLE SWITCH ON THE ELECTRIC PUMP CONTROL PANEL ASSEMBLY AND RESECURED THE WIRE. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050927000472005092700047EA 2005 9 27 ASOA05725 120050829A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA BS 718 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11834AS 7254 DURING A C-CHECK IN MCN, THE FUSELAGE FRAMES FS 718, STRINGER 10 LEFT AND THE FORWARD SIDE OF FS 718, STRINGER 10 AND 11 RIGHT WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FUSELAGE FRAMES FS 718, STRINGER 10 LEFT AND 11 RT IAW ASA EO600-53-0067A. (M) 2L72 4F RTA21EA 20050927000542005092700054SO 2005 9 27 SIMA200524101 120050822A5330 SKIN EMB 135 EMB135LR 3260305SO FUSELAGE BIRD STRIKE A SIMAO OTHER O OTHER CRCRUISE 1 SW21724AE 145301 JFK - FLT 4613 - AIRCRAFT EXPERIENCED BIRDSTRIKE ON LEFT CORNER OF WINDSHIELD. COMPLETED BIRDSTRIKE INSPECTION AND FERRIED AIRCRAFT TO SAW FOR FUSELAGE STRUCTURAL REPAIR BETWEEN FRAME 1 AND FRAME 5, FORWARD OF CAPTAINS WINDSHIELD. MAINTENANCE INSTALLED NEW FUSELAGE SKIN P/N 12041320065, UPPER LEFT FRAME 2 P/N 12001897001, AND REPAIRED STRINGER P/N 12041320043 4L IAW EMB SRM 51-40-02, 53-00-00 FIG 201. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050927000552005092700055NE 2005 9 27 ASOA05738 220050903A7200 ENGINE AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE LEFT FAILED A ASOAA UNSCHED LANDING A FLAME/FIRE DEDESCENT 1 SO11634AS 370 DURING DESCENT FROM PFN-ATL, AT APPROXIMATELY 13,000 FEET THE LEFT ENGINE FEATHERED UNCOMMANDED WITH AN INITIAL RISE UP TO APPROXIMATELY 120 PERCENT THEN POWER WAS LOST AND THE PROPELLER FEATHERED. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT DIVERTED TO SG AND LANDED SAFELY. MAINTENANCE WILL BE REMOVING AND REPLACING THE LEFT ENGINE. 2H72 4T4 TRTA53EU E20NE 20050927000592005092700059EU 2005 9 27 KBM2005F00248 120050820A2810355A5330017501 LINE SNIAS 350 AS350BA 8680817EU FUEL SYSTEM CRACKED E KBMAO OTHER K FLUID LOSS NRNOT REPORTED 1 WP191188P 2347 FUEL LINE FROM THE BOOST PUMP TO THE ALT FUEL FILTER IS CRACKED. REMOVED AND REPLACED HOSE. (M) 1G71 3U NCH9EU 20050927000632005092700063EA 2005 9 27 ASOA05701 120050821A5210601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11840AS 7290 FLT 4482 - DURING A GROUND INSPECTION IN ATL, THE BOTTOM STEP BRACKET ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ASSEMBLY ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050927000672005092700067NE 2005 9 27 SIMA200522009 220050804A7230 COMPRESSOR SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RT ENGINE STALLED A CKSAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SW21390AE 340B390 GEE785656 DURING TAKEOFF, RIGHT ENGINE BEGAN TO GO INTO COMPRESSOR STALLS. ENGINE OVERTEMPED BETWEEN 1013 AND 1025. REMOVED AND REPLACED RIGHT ENGINE IAW W/C 4903. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T4 TRTA52EU E8NE 20050927000762005092700076NM 2005 9 27 USAA051000 120050815A5320 CHANNEL BOEING737 7373B7 1384580NM FS 500-500A CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US 23933 CLT - FOUND HAT SECTION CHANNEL CORRODED 6 INCH AREA, STATION 500-500A, BL 0. REMOVED DAMAGED HAT SECTION, REMOVED LIGHT SURFACE CORROSION INSTALLED NEW HAT SECTION CHANNEL. (M) 2L72 4F RTA16WE 20050927000892005092700089SO 2005 9 27 SIMA200525211 120050829A532014521713005 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO FR 18-19 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21817AE 145554 SAW - DURING CPCP INSPECTION, FOUND RIGHT HAT BEAM IS CORRODED BETWEEN FRAMES 18-19. REPLACED HAT BEAM IAW EMB IC2005-145/4638. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050927000922005092700092SO 2005 9 27 SIMA200525208 120050828A321014571035412 CAP EMB 135 EMB135KL 3260302SO RT MLG CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21817AE 145554 SAW - DURING MBV INSPECTION, FOUND RIGHT MAIN LANDING GEAR FORWARD BEARING CAP CORRODED. REPLACED BEARING CAP IAW EMB 140 WORK CARD 57-200-84. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050927001052005092700105EA 2005 9 27 ASOA05740 120050904A291673011 RESERVOIR CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM MALFUNCTIONED A ASOAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO11900EV 7608 FLT 4292 - DURING CRUISE FROM ATL-SAT, AT APPROXIMATELY 30,000 FEET, THE CREW RECEIVED A HYD HI TEMP NR 1 CAUTION MESSAGE. THE QRH WAS COMPLED WITH, AN EMERGENCY WAS DECLARED AND THE CREW SHUTDOWN THE LEFT ENGINE. THE AIRCRAFT DIVERTED TO IAH AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE HYDRAULIC RESERVOIR AND HEAT EXCHANGER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050927001102005092700110EU 2005 9 27 ASOA05671 120050818A3350 LIGHT AEROSPATR72 ATR72 EU CABIN INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11640AS 405 DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20050927001182005092700118SO 2005 9 27 SIMA200523401 120050810A532014522459003 SUPPORT EMB 135 EMB135LR 3260305SO FR 20 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21715AE 145262 SAW - FOUND DURING CPCP INSPECTION, INBOARD RAMP AT FRAME 20 CORRODED. REPLACED INBOARD RAMP AT FRAME 20 IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050927001202005092700120NE 2005 9 27 ASOA05673 220050819A7261 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RIGHT MALFUNCTIONED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11851AS 7360 FLT 4534 - DURING CRUISE FROM ATL-SBN, THE CREW RECEIVED A LOW OIL PRESSURE WARNING ON THE RIGHT ENGINE. THE QRH WAS COMPLIED WITH AND THE RIGHT ENGINE WAS REDUCED TO IDLE FOR THE REMAINDER OF THE FLIGHT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO CVG. THE AIRCRAFT LANDED SAFELY IN CVG. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE. THE MRR WILL REMAIN OPEN PENDING AN ENGINE TEAR DOWN REPORT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F4 FRTA21EA E15NE 20050927001242005092700124NM 2005 9 27 UIEA200500131 120050906A3232 ACTUATOR BOEING747 7472F6B 1384807NM RT MLG DOOR ACTIVATED A UIEAO OTHER J WARNING INDICATION TOTAKEOFF 1 EA15534MC 21832 FLT 8867 - WRI-JFK- AFTER TAKEOFF, GEAR RETRACTED WITH NO PROBLEM. THEN DURING CLIMB TO 5,000 FEET THE RED DOOR LIGHT ILLUMINATED WITH PRIMARY AND SECONDARY LIGHT ON ENGINEERS PANEL. USED FHB SECTION 3 TO BRING GEAR UP, RIGHT WING GEAR. VIBRATION WAS ALSO EVIDENT UNTIL GEAR WAS RETRACTED. REMOVED AND REPLACED RIGHT WING GEAR DOOR ACTUATOR PER 32-12-00. OPS AND LEAK CHECK OK S/N OFF 4079. (M) 2L74 4F A20WE 20050927001312005092700131EA 2005 9 27 ASOA05664 120050814A5210601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11882AS 7503 DURING HANGAR MAINTENANCE IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED AT THE STAY ROD LOWER ATTACH POINT. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20050927001322005092700132EU 2005 9 27 ASOA05707 120050728A5330S53672408228 DOUBLER AEROSPATR72 ATR72212 8680945EU FR 39 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11636AS 375 DURING A C-CHECK IN YUL, THE DOUBLER AT FRAME 39, STRINGER 14 RIGHT WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE DOUBLER AT FRAME 39, STRINGER 14 RIGHT IAW ATR-72 SRM 51-21-42 AND 51-25-01. (M) 2H72 4T RTA53EU 20050928000012005092800001SO 2005 9 28 SIMA200525221 120050902A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO FS 25 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21818AE 145561 THE CENTER OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE OMEGA BEAM TO REMOVE THE CORROSION. FABRICATED A DOUBLER, FILLER AND SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 30 CHAPTER 53-00-10 FIGURE 203. (M) 2L72 4F RTT00011AT 20050928000022005092800002SO 2005 9 28 SIMA200525220 120050905A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO FS 25 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21818AE 145561 THE LEFT OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE LEFT OMEGA BEAM TO REMOVE CORROSION. FABRICATED A FILLER AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 30, CHAPTER 53-00-10 FIGURE 201. (M) 2L72 4F RTT00011AT 20050928000342005092800034EA 2005 9 28 ASOA05732 120050830A5320 SILL CNDAIRCL600 CL6002B19 1900309EA BS 544 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11834AS 7254 DURING A C-CHECK IN MCN, THE LT AND RT SIDE PRESSURE FLOOR SILL STRUCTURES AT FS 544 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO BOMBARDIER FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. (M) 2L72 4F RTA21EA 20050928000412005092800041SO 2005 9 28 SIMA200521611 120050728A531314533888001 STRINGER EMB 135 EMB135KL 3260302SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21815AE 145545 ABI - FOUND STRINGER 19L WAS FOUND TO BE CHAFED AT THE AFT BELLY PANEL CUTOUT. BLENDED THE CHAFED AREA. FABRICATED A REPAIR ANGLE AND SHIMS. REPAIR DONE IAW EMB SRM, 145/1142 REV 29 CHAPTER 53-24-02. (M) 2L72 4F RTT00011AT 20050928000502005092800050NM 2005 9 28 HALA0500914 120050907A2910 LINE BOEING767 767* NM HYD SYSTEM LEAKING A HALAO OTHER KA FLUID LOSS FLAME/FIRE NRNOT REPORTED 1 WP13584HA 24258 CENTER HYD QTY DROPPED TO .24 AND MAY HAVE LEAKED FROM RIGHT MAIN AREA. GROUND CONTROL REPORTED FIRE FROM 45 MAIN AREA WHICH WAS PUT OUT BY FIRE TRUCKS. FOUND PIN HOLE LEAK ON HYD LINE. REPLACED BOTH HYD FLEX LINES TO RIGHT MLG POSITIONER ACT. ACCOMP HEAT DMG INSPECTION AMM 05-51-14-212-111. CHECK OK. OPS AND LEAK CHECK RIGHT MLG. SERVICED CENTER SYSTEM, ACT LK CHECK GOOD. REMOVED AND REPLACED BOTH BRAKE LINES NR 7 AND NR 8. OPS LEAK CHECK GOOD. OK FOR SERVICE. CHECK DELTS P`S ALL GOOD PER AMM 32-32-18. NO EVIDENCE OF FIRE OF DAMAGE. AS PRECAUTIONARY CHANGED 7/8 BRAKES AND TIRES. (M) 2L72 4F RTA1NM 20050928000582005092800058EU 2005 9 28 SIMA200524111 120050818A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21324AE 340B324 THE SEAT TRACK AT BL 0 WAS FOUND CORRODED. REMOVED THE EXISTING SEAT TRACK AND CLEANED THE AREA. INSTALLED NEW SEAT TRACK. REPAIR DONE IAW SAAB 340 SRM, SRM 72LKS3079 REV 45, CHAPTER 53-70-60 PARA 8. (M) 2L72 4T RTA52EU 20050928000592005092800059NM 2005 9 28 UIEA200500127 120050906A5414 SKIN BOEING747 7472D7B 1384803NM STA 248 CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15524MC 21784 DURING D-CHECK, NR 1 PYLON HAD CRACK DAMAGE IN THE SKIN ASSEMBLY AND THE ADJACENT NR 3 STIFFENER, AT PRECOOLER EXHAUST CUTOUT LOWER EDGE NEAR THE AFT CORNER AT STATION 248. THE NR 3 STIFFENER LOWER FLANGE WAS TRIMMED TO REMOVE CRACKS. THE CRACK IN THE SKIN ASSEMBLY WAS CONTAINED WITH 1 INCH DIAMETER HOLE AT THE CRACK TIP. THE NR 3 STIFFENER WAS REINFORCED WITH A NEW STEEL LOWER REPAIR ANGLE FROM NAC STATION 235 TO 254. THE RIB INSTALLATION AT NACELLE STATION 248 WAS MODIFIED TO ACCOMMODATE THE NEW STEEL LOWER REPAIR ANGLE INSTALLATION ON THE NR 3 STIFFENER. (M) 2L74 4F RTA20WE 20050928000612005092800061EU 2005 9 28 USAA050935 120050729A5347 SEAT TRACK AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19723UW17735 1109 PIT - FOUND DUMMY RAIL CORRODED 1 INCH EACH THREE AREAS, C-16 Y510. CORROSION LEVEL 1, TASK JA-220-53500. INSTALLED/REPLACED DUMMY RAIL PER SRM 53-00-14 FIG 201. (M) 2L72 4F RTA28NM 20050928000662005092800066NM 2005 9 28 UIEA200500130 120050906A5414 SKIN BOEING747 7472D7B 1384803NM NR 4 PYLON DAMAGED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15524MC 21784 DURING D-CHECK, NR 4 PYLON HAD CRACK DAMAGE IN THE SKIN ASSEMBLY AND THE ADJACENT NR 3 STIFFENER, AT PRECOOLER EXHAUST CUTOUT LOWER EDGE NEAR THE AFT CORNER AT STATION 248. THE NR 3 STIFFENER LOWER FLANGE WAS TRIMMED TO REMOVE CRACKS. THE CRACK IN THE SKIN ASSEMBLY WAS CONTAINED WITH 1 INCH DIAMETER HOLE AT THE CRACK TIP. THE NR 3 STIFFENER WAS REINFORCED WITH A NEW STEEL LOWER REPAIR ANGLE FROM NACELLE STATION 235 TO STATION 254. THE RIB INSTALLATION AT NACELLE STATION 248 WAS MODIFIED TO ACCOMMODATE THE NEW STEEL LOWER REPAIR ANGLE INSTALLATION ON THE NR 3 STIFFENER. (M) 2L74 4F RTA20WE 20050928000832005092800083 2005 9 28 SCNA05006 420050922A2230 ENGINE BOEING737 7378Q8 13844BXNM NR 2 MALFUNCTIONED A SCNAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 GL15805SY 30032 PILOT WROTE, ON TAKEOFF, BOTH ENGINES STABLE AT 40 PERCENT. GOT NO ACCELERATION ON ENGINE NR 2 A/T RESPONDS NORMALLY TO MANUAL INPUT. MAINTENANCE PLACED ON MEL 22-4. PERFORMED A/T BITE PROCEDURE 22-31 TASK 801 AND A/T TO/GA SWITCH OPERATION. NO DISCREPANCIES OR CURRENT FAULTS. CLEARS MEL 22-4. 2L72 4F RTA16WE 20050928000852005092800085EU 2005 9 28 UPS05145482 120050912A5420A5451506320400 ANGLE AIRBUSA300 A300F4622R 3930360EU NR 1 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01125UP 0809 NR 1 PYLON LOWER AFT DOUBLER ANGLE CRACKED INBD SIDE. REMOVED AND REPLACED LOWER AFT DOUBLER ANGLE ON THE NR 1 PYLON IAW A300 SRM 51-40-00. 2L72 4F RTA35EU 20050928000902005092800090SO 2005 9 28 C2XA05CL085 120050924A3230355022002 CONTROL MODULE EMB 145 EMB145LR 3260212SO MLG INOPERATIVE A C2XAO OTHER J WARNING INDICATION DEDESCENT 1 SW27175607707 145605 CLE FLIGHT NR 3247, THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE WHEN THE GEAR WAS SELECTED DOWN. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20050928000972005092800097NM 2005 9 28 SWAA052895 120050923A53306545767 SKIN BOEING737 7373H4 1384600NM BS 412.375 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 412.375, STR 16L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050928000982005092800098NM 2005 9 28 SWAA052896 120050923A53306545765 SKIN BOEING737 7373H4 1384600NM BS 500A CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500A, STR 16L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050928000992005092800099NM 2005 9 28 SWAA052897 120050924A53116546552 FRAME BOEING737 7373H4 1384600NM BS 827 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 20L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050928001062005092800106NM 2005 9 28 SWAA052904 120050923A335007912 COVER BOEING737 7373H4 1384600NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29362SW 26573 EEPLS TRACK COVER MISSING AT ROW 17 ABC. INSTALLED COVER PER MM. 2L72 4F RTA16WE 20050928001292005092800129WP 2005 9 28 IXXA05RNG059S 120050908A5753 FITTING DOUG DC8 DC872 302199BWP TE FLAPS CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX 46013 DURING INSPECTION CHECK WAS FOUND RT OUTBOARD FLAP, INBOARD FLAP HINGE FITTING AT STA XF339.7332 CRACKED. DAMAGE WILL BE REPAIRED IAW EWO ATI-57-042 AND FAA FORM 8110-3 MUST BE ISSUED APPROVING THIS REPAIR. 2L74 4F RT4A25 20050928001322005092800132EA 2005 9 28 COMA0560512 120050919A2750860D10018 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01910EV11377 7727 FLIGHT 5023 - FLAPS FAIL CAUTION. REPLACED THE FECU. 2L72 4F RTA21EA 20050928001362005092800136EA 2005 9 28 COMA0570104 120050921A29136619002 PUMP CNDAIRCL600 CL6002C10 1390015EA LT HYD SYSTEM DEFECTIVE A COMAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO01390CA 10106 FLIGHT 5296 - HYDRAULIC SYSTEM 1 LOW PRESSURE WARNING. QUANTITY INDICATES EMPTY. REPLACED THE NR 1 EDP. 2L72 4F RTA21EA 20050928001392005092800139 2005 9 28 QXEA200501257 420050925A235052611 CONTROL PANEL DHAV DHC8 DHC8202 2809007NM CABIN MALFUNCTIONED A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09352PH14773872 494 SEA FLIGHT NR 2210, FIRST OFFICER TO FLIGHT ATTENDANT INTERPHONE CUTTING OUT FIRST OFFICER AUDIO CONTROL SELECT KNOB WIGGLED, FLIGHT ATTENDANT HAND MIC INTERMITTENT WHEN MIC WAS TAPPED ON. MAINTENANCE REPLACED FIRST OFFICER AUDIO CONTROL PANEL, FLIGHT ATTENDANT HAND MIC P/N 5260-1-1 SN 511 TSN 12408.7 CSN 17972 TSR 957.8) AND AMPLIFIER (P/N 5082-1-2 S/N 469, TSN 99755.4 CSN 42662). OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050928001422005092800142SO 2005 9 28 FFKA2005104 120050921A3220452334 ROD END PIPER PIPER PA34 PA34200T 7103406SO DOWNLOCK LINK BROKEN B FFKAO OTHER O OTHER TXTAXI/GRND HDL 1 SO058076N9692 60 347970487 DURING COMPLIANCE WITH AD 2005-13-16, THE DOWN LOCK LINK ASSEMBLY WAS INSPECTED AND FOUND TO BE AIRWORTHY AT THAT TIME AND WAS REINSTALLED INTO THE AIRCRAFT (THIS PART IS NOT PART OF AD2005-13-16 INSPECTION). AFTER 60HRS OF OPERATION THE PART IN QUESTION FAILED, DUE TO UNKNOWN REASONS. 1L72 3O A7SO 20050928001542005092800154NM 2005 9 28 SWAA052924 120050926A3350207377 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29212WN 32485 EEPLS TRACK LENS LOOSE AT FWD END. SECURED LENS PER MM. 2L72 4F RTA16WE 20050928001572005092800157NM 2005 9 28 SWAA052927 120050926A2121215201 GASPER FAN BOEING737 7373H4 1384600NM CABIN FAULTY A SWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW29392SW 27379 STRONG SMOKE SMELL IN AFT CABIN AND COCKPIT. REMOVED AND REPLACED GASPER FAN PER MM. 2L72 4F RTA16WE 20050928001592005092800159NM 2005 9 28 SWAA052929 120050926A3350MS155721 BULB BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29451WN 32495 LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20050928001672005092800167WP 2005 9 28 IXXA05RNG063S 120050915A5330 SKIN DOUG DC8 DC872 302199BWP BS 340-360 MISREPAIRED B IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW11721CX 46013 DURING INSPECTION CHECK, FOUND A IMPROPER REPAIR ON FUSELAGE SKIN LOWER DOOR JAMB STA 340-360, LT. DAMAGE WILL BE REPAIRED IAW EWO ATI-53-016 AND FAA FORM 8110-3 MUST BE ISSUED. 2L74 4F RT4A25 20050928001702005092800170WP 2005 9 28 IXXA05RNG061S 120050912A5330 SKIN DOUG DC8 DC872 302199BWP BS 560-580 CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX 46013 DURING INSPECTION CHECK, FOUND A CORROSION ON INTERNAL SKIN OF PASSENGER WINDOW STA 560-580, LT. DAMAGE WILL BE REPAIRED IAW EWO ATI-53-019 AND SRM 53-2-0 FIGURE 22A TR 53-170. 2L74 4F RT4A25 20050928001752005092800175WP 2005 9 28 IXXA05RNG052S 120050904A5730 SKIN DOUG DC8 DC872 302199BWP RT WING CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX 46013 DURING INSPECTION CHECK, FOUND STRESS CORROSION CRACK ON RT WING UPPER EXTERIOR SURFACE STA XRS74 STRINGERS 9 TO 15. DAMAGE WILL BE REPAIRED IAW EWO ATI 57-038 AND FAA FORM 8110-3 MUST BE ISSUED APPROVING THIS REPAIR. 2L74 4F RT4A25 20050928001832005092800183NM 2005 9 28 SWAA052937 120050926A53156546811 FLOORBEAM BOEING737 7373H4 1384600NM BS 986 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29618WN 28034 DURING SCHEDULED D CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 986, BETWEEN LBL 65 TO RBL 65, WL 208. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20050928001852005092800185NM 2005 9 28 SWAA052939 120050926A33506128251 CHARGER BOEING737 737317 138447PNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 DURING SCHEDULED RON CHECK, FOUND FWD CABIN SIDEWALL EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM. 2L72 4F RTA16WE 20050928001862005092800186NM 2005 9 28 SWAA052940 120050925A33506104781 BATTERY PACK BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29723SW 27855 DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050928002022005092800202NM 2005 9 28 2005UALA01002 120050921A2120 SOLENOID BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN BURNED A UALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP29128UA 30023 RUBBER BURNING SMELL IN CABIN/FLIGHT DECK. SMOKE IN FLIGHT DECK RESULT OF STRIKE SOLENOID OVERHEATING. DOOR MAY HAVE BEEN SLIGHTLY SPRUNG OR "PRELOADED" IN THE FULLY CLOSED POSITION WHICH CAUSED THE STRIKE SOLENOID TO BIND AND PREVENT FULL EXTENSION OF THE LOCK PIN. THIS IN TURN CAUSED IN THE SOLENOID TO CONTINUALLY DRIVE AND OVERHEAT. THIS SOLENOID HAS BEEN REVISED BY THE MANUFACTURER TO INCORPORATE THERMAL PROTECTION. NEW SOLENOIDS ARE REQUIRED TO BE INSTALLED EVERY 4 YEARS PER EC 82-5251-002AD-A. NEW STRIKE SOLENOIDS WILL SUPERSEDE OLD STRIKE SOLENOIDS IN THE UAL SYSTEM VIA SCR. 2L74 4F4 FRTA20WE E24NE 20050929000042005092900004EU 2005 9 29 USAA200509007 120050924A5320D534800432401 SPLICE AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19115US 1171 LEFT AFT ENTRY DOOR THRESHOLD CORRODED .75 X 3 X .070 INCH DEEP AT UPPER SPLICE ANGLE STATION FR 67. NO CORROSION LEVEL OR TASK. REMOVED UPPER SPLICE ANGLE, FABRICATED AND INSTALLED REPAIR ANGLES PER SRM 53-41-14, REPAIR PRINCIPAL 2. 2L72 4F RTA28NM 20050929000152005092900015NM 2005 9 29 C8GA20050021 120050924A2780H1010271 SWITCH BOEING727 727223 1384074NM NR 5 SLAT MALFUNCTIONED A C8GAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO29898AA57059 22014 FLT 1737 FROM MTY TO TOL, AFTER TAKEOFF FROM MTY, NR 5 LEADING EDGE SLAT EXTEND LIGHT REMAINED ILLUMINATED AT FLAPS 2 POSITION. AIRCRAFT RETURNED TO MTY AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 5 LEADING EDGE SLAT POSITION INDICATION SWITCH. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L73 4F A3WE 20050929000192005092900019NM 2005 9 29 DHL2005748512 120050814A5330 SKIN BOEING727 727225 1384077NM BS 990 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 AFT CARGO BILGE SKIN AREA HAS CORROSION AT STA 990 BETWEEN STR 28R AND 29R WCT 1312. CUT OUT DAMAGED AREA (3' BY 2 1/2") AT BS 970 AND REMOVED PREVIOUS DOUBLER AT BS 990 STR 29R -28R WITH PREVIOUS CUT OUT 5 1/2" BY 4" FABRICATED DOUBLER 2024T3 .125 PO 9002678 35" BY 34" AND 2 FILLER 8" BY 5" AND NR " BY 2 1/2" 2024-T3 .100 PO 9002507 IAW B727 SRM 53-30-3 FIG 3. TREATED AND PRIMED AREA AND REPAIR PARTS IAW B727 SRM 51-10-2. INSTALLED DOUBLER IAW B727 SRM 53-30-3 FIG 3 REPAIR IS A CAT B. 2L73 4F A3WE 20050929000202005092900020 2005 9 29 AT0500035 420050921A2565D29982225 SLIDE BOEING717 717200 1383700NM R-1 DOOR MALFUNCTIONED A ZZDAK NONE L NO TEST ININSP/MAINT 1 SO15977AT 55036 SLIDE DID NOT FULLY DEPLOY ON TEST. REMOVED AND REPLACED SLIDE ASSY. 2L72 4F TRA6WE 20050929000232005092900023NM 2005 9 29 SB05120 120050923A21337110033 OUTFLOW VALVE BOEING737 7373B7 1384580NM CABIN PRESSURE FAILED A USAAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 EA19533AU5403654036 24515 EN ROUTE AT CRUISE, CREW NOTICED PRESSURIZATION CHANGE AS CABIN CLIMBED AT 2,000 FPM. NO LIGHTS, NO WARNING AND NO OBVIOUS REASON FOR PROBLEM. PACKS OPERATING NORMALLY & HIGH MODE HAD NO EFFECT. CREW INITIATED DESCENT & CABIN REACHED A MAX OF ABOUT 8,000 FT. STANDBY MODE SELECTED WITH NO EFFECT. OUTFLOW VALVE INDICATED FULLY CLOSED ENTIRE TIME. FLT LANDED AT ILM W/O FURTHER INCIDENT. MX R & R AFT OUTFLOW VALVE DUE TO A FAILED AC MOTOR PER MM. OPS CHK NORM. DURING CHK OUT OF AFT OUTFLOW VALVE, FOUND FWD OUTFLOW VALVE FAILED IN CLOSED POSITION. REPLACED FORWARD OUTFLOW VALVE. ACCOMPLISHED PRESSURIZATION CONTROL SYS OPS TEST PER MM & PRESSURIZATION CONFIDENCE CHK PER JOB CARD. ALL CHECKS NORMAL. 2L72 4F RTA16WE 20050930000042005093000004NM 2005 9 30 PIDA20050144 120050926A5311 FRAME BOEING737 737228 13844AGNM BS 294.5 CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 RIGHT FORWARD DOOR FRAME (FUSELAGE FRAME) CRACKED AT FLOOR LEVEL BEHIND THE ZEE ANGLE. REPAIRED DAMAGE PER SRM 51-40-3 AND SRM 51-10-1. 2L72 4F RTA16WE 20050930000062005093000006NM 2005 9 30 200514 120050918A26113023112 SMOKE DETECTOR DHAV DHC8 DHC8103 1386005NM CARGO BAY INTERMITTENT A KPVAK NONE L NO TEST ININSP/MAINT 1 WP13805WP 353 (MX) SMOKE AND MASTER WARNING LIGHTS INTERMITTENT DURING TEST OF NR 2 BAGGAGE SMOKE DETECTOR. REMOVED AND REPLACED NR 2 BAGGAGE SMOKE DETECTOR. INSTALLED CONNECTOR AND SECURED WITH 4 MOUNTING SCREWS. OPS CHECK GOOD IAW DHC-8 MM 26-12-00, PG 201. 2H72 4T RTA13NM 20050930000122005093000012 2005 9 30 0501479955 420050926A256513621228 SLIDE DOUG DC9 DC931 3022065WP TAIL CONE DEPLOYED A NWAAO OTHER O OTHER NRNOT REPORTED 1 GL01922RW 47182 DURING OVERNIGHT MAINTENANCE ACTIVITIES AT IND, THE TAIL CONE WAS INADVERTENTLY JETTISONED. WHEN THE TAIL CONE SEPARATED FROM THE FUSELAGE THE EMERGENCY EVACUATION SLIDE DID NOT DEPLOY. NO OBVIOUS REASON FOR FAILURE TO DEPLOY WAS NOTED DURING A VISUAL CHECK BY MAINTENANCE AT IND. THE AIRCRAFT WAS FERRIED TO MSP WHERE THE EVACUATION SLIDE AND THE TAIL CONE WERE REPLACED. THE AIRCRAFT HAS RETURNED TO SERVICE. 2L72 4F A6WE 20050930000132005093000013 2005 9 30 0501466718 420050924A346066346390002 CONTROL PANEL BOEING747 747251F 1384898NM COCKPIT FAILED A NWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL01618US 21122 DURING CRUISE THE PMS (PERFORMANCE MANAGEMENT SYSTEM) WENT BLANK. SMELLED ELECTRICAL SMOKE, AND SMOKE WAS VISIBLE FROM PEDESTAL AROUND PMS BASE. FLIGHT CREW PUT ON O2 MASKS AND GOGGLES, REFERRED TO RED CHECK LIST AND COM PROCEDURE. FOUND PMS CDU C/B POPPED, AND PULLED OTHER PMS C/B'S AND SMOKE DISSIPATED. AIRCRAFT DIVERTED TO FAI (FAIRBANKS, ALASKA) AND LANDED WITHOUT INCIDENT. PMS WAS MEL'D IN FAI. THEN AIRCRAFT CONTINUED ON. 2L74 4F A20WE 20051003000032005100300003NM 2005 10 3 DHL2005748530 120050817A5230 DEPRESSOR BOEING727 727225 1384077NM C1 DOOR SEAL DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 C1 DOOR AFT LWR BS 610 SEAL DEPRESSOR GAUGE. REMOVED AND REPLACED SEAL DEPRESSOR P/N 65-57146-3 PO 5314122 IAW B727 SRM 51-30-2 LEAK CK GOOD IAW B727 MM 5-51-101. 2L73 4F A3WE 20051003000082005100300008NM 2005 10 3 05FDEA03107 120050925A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 CRACK INDICATION FOUND AT STRINGER END OF STRINGER 13, UPPER STRINGER, LEFT SIDE WING TANK. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. 2L73 4F RTA22WE 20051003000092005100300009NM 2005 10 3 05FDEA03108 120050925A5320 FLOOR SUPPORT DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 AFT CARGO, 02 CORROSION FOUND AT RIGHT CEILING FLOOR STRUCTURE AT STA 1921 TO STA 1941 X= -40. 2L73 4F RTA22WE 20051003000142005100300014NM 2005 10 3 05FDEA03111 120050925A5730 SKIN DOUG MD11 MD11 3023602NM ZONE 600 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 RIGHT WING UPPER SURFACE AFT OF NR 7 SLAT, 2 EACH LOCKBOLT HEAD FOUND FUEL LEAK, SKIN PLANK FOUND TO HAVE AN ELONGATED BORE. CARRIED OUT REPAIR AS PER FEDEX EA 1-5710-90018. 2L73 4F RTA22WE 20051003000152005100300015NM 2005 10 3 05FDEA03112 120050925A5310 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 UPPER CARGO RIGHT SIDEWALL, FRAME AT STA 1561 INNER CHORD FOUND DENT AT LONGERON 12R TO LONGERON 13R. CARRIED OUT REPAIR AS PER SRM 53-30-00 FIGURE 1 VOLUME I DUE TO CAT B REPAIR. REFER TO FEDEX EA 1-5330-90040. 2L73 4F RTA22WE 20051003000162005100300016EU 2005 10 3 05FDEA03114 120050926A5321 FLOOR PANEL AIRBUS310 A310203 3930313EU CARGO BAY CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25425FE 264 MCD FLOOR PNL 231XG CRACKED AND DELAMINATED ON BACK SIDE. 2L72 4F RTA35EU 20051003000172005100300017EU 2005 10 3 05FDEA03115 120050926A5512 PANEL AIRBUS310 A310203 3930313EU HORIZONTAL STAB CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25425FE 264 LT IB HORIZONTAL STAB L/E HAS MULTIPLE CRACKS WHERE RIBS ATTACH TO SKIN. 2L72 4F RTA35EU 20051003000202005100300020 2005 10 3 05FDEA03118 420050926A2565NSA93203002 LIMIT SWITCH AIRBUS300 A300F4605R 3930327EU ZONE 800 MALFUNCTIONED A FDEAK NONE L NO TEST ININSP/MAINT 1 SO25655FE 742 L1 DOOR ESCAPE SLIDE WARNING LIGHT (13WN) DOES NOT ILLUMINATE DURING TEST. REPLACED SWITCH NSA932030-02 2L72 4F RTA35EU 20051003000252005100300025NM 2005 10 3 SWAA052963 120050927A3350101331 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29353SW 24889 DURING SCHEDULED C2 CHECK, FOUND OVERWING EXIT SIGN LENS LOOSE. SECURED LENS PER MM. 2L72 4F RTA16WE 20051003000312005100300031NM 2005 10 3 SWAA052969 120050928A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 787 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CORRODED AT BS 787, STR 26R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051003000322005100300032NM 2005 10 3 SWAA052970 120050928A53116517684 FRAME BOEING737 7373H4 1384600NM BS 303 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29618WN 28034 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303, L1 DOOR LOWER FWD STOP FITTING CUTOUT. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20051003000342005100300034NM 2005 10 3 SWAA052972 120050928A3350D71702001 BATTERY PACK BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED SERVICE CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20051003000352005100300035NM 2005 10 3 DHL2005748520 120050816A5322 SHEAR TIE BOEING727 727225 1384077NM BS 990 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 AFT CARGO COMP HAS CORROSION AT SHEAR TIE STA 990 STR 29R. CUT DAMAGED AREA 6" BY 1" FAB REPAIR DOUBLER AND FILLER 7075T6 .071 PO 5096275 IAW B727 SRM 53-10-4 FIG 13 (DOUBLER DIM 6 1/2 BY 3 1/8") (FILLERS 3 1/2 BY 1 1/2) (2" BY 1") & (4" BY 1"). TREATED AND PRIMED REPAIR PART IAW B727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B727 SRM 51-10-4 FIG 11. 2L73 4F A3WE 20051003000372005100300037NM 2005 10 3 DHL2005748510 120050815A2782 ACTUATOR BOEING727 727225 1384077NM NR 1 SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 NR 1 SLAT ACT TO SLAT ATTACH POINT CRACKED AT I/B RIB. OPENED ACCESS PANELS TO FACILITATE MAINT IAW B727 SRM 51-30-2. REMOVED DAMAGED RIB IAW B727 SRM 51-30-2. LOCATED & DRILLED NEW RIB P/N 65-17327-3 PO NR 531452 IAW B727 SRM 51-30-5 TREATED & PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED NEW RIB IAW B727 SRM 51-30-2 2L73 4F A3WE 20051003000392005100300039NM 2005 10 3 RYNA200500029 120050916A2910271N61191 LINE BOEING757 75728A 1384976NM HYDRAULIC SYS LEAKING A RYNAB EMER. DESCENT KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 CE07753NA 24544 EICAS MESSAGE LEFT HYDRAULIC QUANTITY AND PRESSURE LOST. QUANTITY LEVEL 0.10 LT. REMOVED AND REPLACED RIGHT DOWNLOCK ACTUATOR RETURN LINE. LEAK CHECK GOOD, ALSO FOUND NR 1 ENGINE DRIVEN HYDRAULIC PUMP LEAKING. REMOVED AND REPLACED ENGINE DRIVE PUMP AND PRESSURE DRAIN FILTER. SYSTEM LEAKED AND OPERATIONALLY CHECKED GOOD. 2L72 4F RTA2NM 20051003000402005100300040NM 2005 10 3 UPS05245507 120050913A5330 SKIN BOEING727 72725C 138400HNM BS 521 DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01932UP 19856 INDICATION OF MATERIAL LOSS AT BS 521 S1L-2L. REPAIR CARRIED OUT IAW SRM 51-30-2, 53-30-3, MM 25-21-33 AND AAAE EO 200 5-087-007. UPS ENGINEERING FILE NR B727-5330-22937. 2L73 4F A3WE 20051003000412005100300041NM 2005 10 3 UPS05245508 120050909A7160 INTAKE DUCT BOEING727 72725C 138400HNM NR 2 ENGINE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01932UP 19856 NR 2 ENG S-DUCT HAS A CRACKED ON INNER SKIN AT 3 O`CLOCK POS. ON RIB NR 5 REPAIR CARRIED OUT IAW AAAE EO 2005-087-002. UPS ENGINEERING FILE NR 727-54-20024. 2L73 4F A3WE 20051003000422005100300042 2005 10 3 UPS05245509 420050914A2565 RING BOEING727 72725C 138400HNM DOOR SLIDE DISCONNECTED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01932UP 19856 CHAIN DISCONNECTED FROM LATCH ON ESCAPE SLIDE BOX ON FWD ENTRY DOOR. NEW RING FITTED TO LATCH CHAIN IAW MM 25-60-00. 2L73 4F A3WE 20051003000432005100300043NM 2005 10 3 UPS05245510 120050911A5315 FLOORBEAM BOEING727 72725C 138400HNM BS 340 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01932UP 19856 CORROSION ON FLOORBEAM TOP ANGLE AT BS 340 RBL 24. REPAIR CARRIED OUT IAW SRM 51-30-2, 53-10-8 AND 53-10-1. 2L73 4F A3WE 20051003000462005100300046WP 2005 10 3 UPS05845487 120050903A5712 RIB DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 LEFT WING LE LOWER RIB IS CRACKED AT XFS 616.250. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-3-0 FIG 2. 2L74 4F RT4A25 20051003000482005100300048WP 2005 10 3 UPS05845489 120050910A57403645611U FITTING DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 LT WING XW 408 STRINGER NR 58 UNDER THE BOOST PUMP FITTING CRACKED. REMOVED AND REPLACED BOOST PUMP FITTING IAW SRM51-1-20D AND 51-1-21. 2L74 4F RT4A25 20051003000522005100300052NM 2005 10 3 AWXA200501120 120050927A3350BR964411 LIGHT BOEING757 7572S7 1384962NM CABIN INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28905AW 23567 PHX - EEL - DURING A9 CHECK DISCOVERED SEAT MOUNTED EMERGENCY EXIT LIGHT AT ROW 29 LEFT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EXIT LIGHT ASSEMBLY AT ROW 29 LEFT. OPS CHECKS WERE GOOD. 2L72 4F RTA2NM 20051003000552005100300055EU 2005 10 3 AWXA200501123 120050927A5320D53112785200 WEB AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28634AW 091 DURING C4 CHECK DISCOVERED EXFOLIATION CORROSION ON WEB LOCATED AT Y1379.5, FLOOR STRUCTURE AREA AT FS 16. MAINTENANCE REMOVED CORROSION FROM WEB IAW AIRBUS 320 SRM 51-74-00. REWORK FOUND TO BE OUT OF THE SRM SCOPE. CUTOUT DAMAGED AREA OF WEB IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NO. 26-5311-05269-SS4. FABRICATED REPAIR ANGLE AND SHIM IAW AWA ER 26-5311-05269-SS4. INSTALLED FABRICATED REPAIR PARTS AT Y1379.5, FLOOR STRUCTURE AREA AT FS 16 IAW AWA ER 26-5311-05269-SS4. 2L72 4F RTA28NM 20051003000572005100300057NM 2005 10 3 DHL2005748518 120050816A5753 SKIN BOEING727 727225 1384077NM FOREFLAP WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 RT WING OTBD FORE FLAP WORN AT L/E 12" FROM INBD END. REMOVED EXISTING REPAIR ON RT WING O/B FORE FLAP L/E IAW B727 SRM 51-30-2 FAB NEW DOUBLER FROM 2024T3 .050 4" BY 5 1/2" PO9002507 IAW B727 SRM 57-50-4 FIG 1. TREATED AND PRIMED DOUBLER IAW B727 SRM 51-10-2. INSTALLED NEW DOUBLER IAW B727 SRM 51-30-2 AND 57-50-04 FIG 1. 2L73 4F A3WE 20051003000592005100300059NM 2005 10 3 DHL2005748515 120050816A5754 SKIN BOEING727 727225 1384077NM NR 8 SLAT DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 NR 8 SLAT LE LWR SKIN CREASE AND DENTED TO O/B END WS760. CUT OUT DAMAGED AREA OF SKIN 6" BY 4" AND FAB FILLER 6.0" BY 4.0 .050 2024 T3 PO 9002435 IAW B727 SRM 57-50-3 FIG 1 FAB SPLICE STRAPS 5 BY 2.2 2EACH 3.3 BY 2.2 2EACH 2.4 BY 3.5 1EACH .080 2024 T3 PO 50962 IAW B727 SRM 57-50-3 FIG 1. TREATED AND PRIMED ALL REPAIR PARTS IAW B727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B727 SRM 57-50-3 FIG 1. 2L73 4F A3WE 20051003000602005100300060NM 2005 10 3 DHL2005748521 120050816A5330 SKIN BOEING727 727225 1384077NM BS 950F CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 FOUND CORROSION AFT CARGO COMP STA 950F+6 BETWEEN STR 28R AND 27R. CUT OUT 1.875" BY 6.875" SECTION OF FUSE SKIN AT STR 28R AND STA 950F+6 MAT LOSS .038 REMAINING THICKNESS OF .106 BEYOND LIMITS IAW B727 SRM 53-30-2 AND 53-30-30 FIG 3. FAB DOUBLER FROM 2024T3 .080 10 3/4" BY 20 1/2" AND TRIPLER FROM 2024T3 .080 8 3/4" AND 17 5/8" PO 9002255 AND FILLER FROM 2024T3 .160 1 7/8" BY 6 7/8" PO 900844 IAW ERO-ASTY-007RO-1. TREATED AND PRIMED REPAIR PARTS IAW B727 SRM 51-10-2 HFEC INSP CUT OUT VERIFIED DAMAGED REMOVED IAW B727 NDT MAN PT6 51-00-00 FIG 23. INSTALLED REPAIR PARTS IAW EMTE ERO-ASTR-007RO-1. 2L73 4F A3WE 20051003000622005100300062NM 2005 10 3 05FDEA03086 120050924A5320BAC1510335X2830 CHANNEL BOEING727 7272S2F 1384O81NM BS 1130-1148 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25211FE 22933 MCD FLOOR SUPPORT SEVERAL NUT PLATES CORRODED BETWEEN STA 1130 TO STA 1148, RBL 27 TO RBL 62. REMOVED CORRODED FLOOR SUPPORT IAW SRM 51-30-2-1, FOUND OUT OF LIMITS IAW SRM 52-10-1 FIG 1. RECEIVED NEW FLOOR SUPPORT ON TRAV NR T5/547544, MAT ID 60357/7075-T6511, BATCH NR 98R000924004. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-30-2. INSTALLED NEW NUT PLATES IAW SRM 51-30-2. (MINOR REPAIR) 2L73 4F A3WE 20051003000672005100300067NM 2005 10 3 05FDEA03091 120050925A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 HORIZ STAB LT BARREL NUT BORE NR 18 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 - EA 1-5510-87628 ATTACHMENT 14. CLASSIFIED AS MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20051003000682005100300068NM 2005 10 3 05FDEA03092 120050925A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 HORIZ STAB LT BARREL NUT BORE NR 22 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 15. MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20051003000692005100300069NM 2005 10 3 SPAA0500075 120050914A3350900835A BATTERY PACK BOEING737 7372T4 1384492NM EMERGENCY LIGHT INOPERATIVE A SPAAK NONE O OTHER ININSP/MAINT 1 WP28703S 22529 AFT CEILING EMERGENCY EXIT SIGN DOESN'T ILLUMINATE WHEN SWITCHED ON. REPLACED BATTERY PACK PER MM 33-51-81, OPS CHECK NORMAL. 2L72 4F A16WE 20051003000702005100300070NM 2005 10 3 05FDEA03093 120050925A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 HORIZ STAB LT BARREL NUT BORE NR 24 FOUND WITH CORROSION. REWORK/ REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 16. MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20051003000712005100300071NM 2005 10 3 05FDEA03094 120050925A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 HORIZ STAB LT BARREL NUT BORE NR 30 FOUND WITH CORROSION. DUPLICATE CARD. REFER TO SNRM N2662 WITH SDR TRACKING NO.05-3102 FOR REPAIR DETAILS. 2L73 4F RTA22WE 20051003000732005100300073NM 2005 10 3 05FDEA03096 120050925A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 HORIZ STAB RT BARREL NUT BORE NR 29 FOUND WITH CORROSION. SNRM N2607: DUPLICATE CARD. REFER TO SNRM N2659 WITH SDR TRACKING NO.05-3099 FOR REPAIR DETAILS. 2L73 4F RTA22WE 20051003000752005100300075NM 2005 10 3 05FDEA03098 120050925A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 HORIZ STAB RT BARREL NUT BORE NR 27 FOUND WITH CORROSION. REWORK/ REPAIR AD 2003-22-08 EA1-5510-87628, ATTACHMENT 19. MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20051003000842005100300084NM 2005 10 3 AWXA200501112 120050906A5312651758243 BULKHEAD BOEING737 7373G7 1384595NM BS 178 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - DURING C18 CHECK DISCOVERED VERTICAL CHORD CRACKED IN WEB AT BS 178, WL 230, BL 17.1R. MAINTENANCE CUTOUT DAMAGED SECTION OF WEB AT BULKHEAD 178 IAW BOEING 737-300 SRM 53-10-08-2R. FABRICATED WEB IAW BOEING 737-300 SRM 53-10-08-2R. INSTALLED FABRICATED REPAIR PARTS AT BS 178, WL 230, BL 17.1R IAW BOEING 737-300 SRM 53-10-08-2R. 2L72 4F RTA16WE 20051003000852005100300085NM 2005 10 3 AWXA200501113 120050903A5330655582171 SKIN BOEING737 7373G7 1384595NM BS 944.5 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 DISCOVERED DURING C18 CHECK THE FUSELAGE SKIN CRACKED .5 INCHES IN LENGTH AT BS 944.5, STR 24L. MAINTENANCE REMOVED DAMAGED AREA OF SKIN IAW BOEING 737-300 SRM 53-00-01-2R. FABRICATED DOUBLER, TRIPLER AND FILLER IAW BOEING 737-300 SRM 53-00-01-2R. INSTALLED FABRICATED REPAIR PARTS AT BS 944.5, STR 24L IAW BOEING 737-300 SRM 51-40-02-0G. 2L72 4F RTA16WE 20051003000872005100300087NM 2005 10 3 SPAA0500076 120050924A3350900542 POWER SUPPLY BOEING737 7372T4 1384492NM EMERGENCY LIGHT INOPERATIVE A SPAAK NONE L NO TEST ININSP/MAINT 1 WP28703S 22529 PREFLIGHT CHECK, AFT OVERHEAD AISLE EMERGENCY EXIT SIGN DOES NOT LIGHT. REPLACED BATTERY POWER SUPPLY IAW 33-51-81. OPERATIONAL CHECK NORMAL. 2L72 4F A16WE 20051003000882005100300088SO 2005 10 3 CHQA200500170 120050927A3350100865 BATTERY PACK EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11846RP4537 4537 145600 RIGHT FUSELAGE FORWARD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE NR 2 FORWARD EMERGENCY LIGHT BATTERY PACK AS PER THE EMB 135 MM 33-50-04. OPS CHECK IS GOOD. 2L72 4F RTT00011AT 20051003000892005100300089SO 2005 10 3 CHQA200500169 120050923A3350 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11286SK 145443 SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BULB IAW EMB 145 MM 30-50-09. OPS CHECK GOOD. ALSO, FOUND PIN 5 OF P8641 CONNECTOR LOOSE FOR THE FORWARD AISLE OVERHEAD EMERGENCY LIGHT. REPINNED WIRE AND OPS CHECK GOOD IAW EMB 145 WM 20-50-00. 2L72 4T RTT00011AT 20051003000902005100300090SO 2005 10 3 CHQA200500167 120050928A335066367 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11257JQ 14500812 TWO FLOOR EMERGENCY LIGHT STRIPS BETWEEN ROWS 7 AND 13 ARE INOPERATIVE. REMOVED AND REPLACED LIGHT STRIP 7A ROW IAW EMB 145 MM 33-50-12-4. OPS CHECK GOOD. 2L72 4T RTT00011AT 20051003000912005100300091NM 2005 10 3 05FDEA02498 120050817A5754 RIB BOEING727 727227 1384078NM NR 5 SLAT CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 RIGHT WING, NR 5 SLAT, LEADING EDGE RIB CRACKED OUTBOARD OF OUTBOARD MAIN TRACK. REMOVED AND REPLACED RIB IAW SRM 51-30-5, 51-30-2. 2L73 4F A3WE 20051003000932005100300093SO 2005 10 3 1454092305 120050923A2432100020101 BATTERY GULSTMG1159 GIV 3980115SO EMERGENCY INOPERATIVE E N93AA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO13454QS3640 1454 NR 1 EMERGENCY BATTERY FAILED AFTER DEPARTURE FROM SAV. 2L72 4F RTA12EA 20051003000942005100300094EA 2005 10 3 QXEA200501265 220050920A7397312240105 WIRE HARNESS BOMBDRDHC8 DHC8402 1390042NM PWC 150 PW150A EA NR 1 FCU INOPERATIVE A QXEAK NONE J WARNING INDICATION ININSP/MAINT 1 NM09408QX 4050 SMF - POWERPLANT MESSAGE ON ED FOLLOWED BY NR 1 ENGINE FADEC FAIL MASTER WARNING. ENGINE SHUTDOWN PER CHECKLIST. FOUND FAULT CODES 935, 936, AND 360. BOTH A & B CHANNELS FAILED. REMOVED AND REPLACED FUEL CONTROL ELECTRICAL HARNESS. CLEARED FAULT CODES. GROUND RAN FOR HARNESS REPLACEMENT. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E00062EN 20051003000952005100300095NM 2005 10 3 QXEA200501266 120050924A5210 STOP BOMBDRDHC8 DHC8402 1390042NM PAX DOOR OUT OF ADJUST A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09412QX 4059 PDX - ON FLIGHT 2362, MAIN CABIN DOOR HARD TO OPEN. ADJUSTED DOOR LIMIT STOP AND UP LIMIT STOPS. PERFORMED OPERATIONAL TEST. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051003000962005100300096NM 2005 10 3 C8GA20050020 120050924A2780 CONNECTOR BOEING727 727223 1384074NM SLATS DIRTY A C8GAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 SO29898AA 22014 FLT 1737 FROM MTY TO TOL, AFTER TAKEOFF FROM MTY, NR 5 LEADING EDGE DEVICES RED EXTENDED AT FLAPS 2 POSITION. AIRCRAFT RETURNED TO MTY AND LANDED WITHOUT INCIDENT. CLEANED NR 5 SLAT TRACK POSITION SENSOR CONNECTOR. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L73 4F A3WE 20051003000982005100300098EU 2005 10 3 05FDEA03070 120050923A5511 SPAR CAP AIRBUS310 A310203 3930313EU HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25425FE 264 LEFT HORIZONTAL STAB FWD UPPER SPAR CAP IS CORRODED AT NR 10 NUTPLATE COUNTING IB-OUT. 2L72 4F RTA35EU 20051003001032005100300103NM 2005 10 3 DHL2005748502 120050807A5330 SKIN BOEING727 727225 1384077NM BS 950-1010 BULGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 LOWER FUSELAGE AT APPROX STA 950E BELOW AFT CARGO DOOR HAS RIVET HEAD CORRODED OFF AND BULGE IN SKIN. REMOVED STR 29R KEEL BEAM CHORD FROM BS 950 TO BS 1010 REMOVED CORR AND CLEANED AREA BELOW STR 29R FROM SKIN MAT LOSS .007 AT BS 950E ORIGINAL THICKNESS .135 AND IS WITHIN LIMITS ALLOWED IAW B727 SRM 53-30-1 FIG 1 AND S/B 727-53-129 FIG 12 DRILLED AND LOCATED NEW STR 29R KEEL BEAM CHORD P/N 65-56441-8 PO NR 53141 IAW S/B 727-53-129 FIG 12. TREATED AND PRIMED STRINGER AND SKIN IAW B727 SRM 51-10-2. INSTALLED STR 29R KEEL BEAM CHORD AND TORQUED BOLTS AS REQUIRED TO LIMITS IAW S/B 727-53-129 FIG 12 AND SRM 51-30-4 FIG 2. 2L73 4F A3WE 20051003001042005100300104NE 2005 10 3 DJFA2005143 220050926A7261CF343A2 ENGINE CNDAIRCL600 CL6002B16 1900305EA GE CF34 CF343A 30015NE RIGHT OVERSERVICED E DJFAA UNSCHED LANDING WMJINADEQUATE Q C OVER TEMP WARNING INDICATION CLCLIMB 1 EA23699CW6985 793 5009 350488 KAPA - KSMO - WHILE CLIMBING THROUGH 15,000 FEET, THE NR 2 ENGINE OIL TEMPERATURE BEGAN TO RISE INTO THE AMBER BAND. WHEN POWER WAS REDUCED THE OIL TEMPERATURE CONTINUED TO RISE INTO THE RED BAND. ENGINE POWER WAS REDUCED TO IDLE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT WAS RETURNED TO KAPA. MAINTENANCE DRAINED APPROXIMATELY TWO GALLONS OF OIL FROM THE NR 2 ENGINE GEAR BOX SUMP DUE TO THE ENGINE BEING OVER SERVICED. THE ENGINE WAS GROUND RUN FOR FIVE MINUTES AT POWER WITH NO NOTED DEFECTS. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20051003001072005100300107NM 2005 10 3 TSAA0549042 120050923A492038007021 APU BOEING737 73776N 13844CHNM APU BAY SHUTDOWN A TSAAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 WP13742AL19864 30830 FLT 484 OGG-SNA - APU AUTO SHUT DOWN WITH OVER SPEED INDICATION. CREW DIVERTED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED APU INSPECTION AND AUTO SHUTDOWN INSPECTION PER AIRCRAFT FIM 49-30-00-810-802 AND OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA16WE 20051003001092005100300109NM 2005 10 3 TSAA0523044 120050923A5330 SKIN BOEING737 737209 13844AENM FUSELAGE LIGHTNING STRIKEA TSAAA UNSCHED LANDING O OTHER CRCRUISE 1 WP13827AL 23913 FLIGHT 270 (HNL-KOA) LIGHTNING STRIKE DURING CLIMB-OUT AT 10,000’. NO MALFUNCTIONS. MTX ACTION COMPLIED WITH M-118 LIGHTNING STRIKE INSPECTION. REMOVED AND REPLACED DAMAGED RIVETS ON STATION 188R AND STATIC WICK. 2L72 4F RTA16WE 20051003000362005100300036NM 2005 10 3 DHL2005748519 120050816A5344 HINGE BOEING727 727225 1384077NM CARGO DOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 MAIN CARGO DOOR AFT HINGE SEGMENT CRACKED. REMOVED AFT SECTION OF AFT HINGE IAW AEI CHAPTER 52 FIG 5201A CUT NEW HINGE SECTION FROM NS20001-16-7200 PO9002527 18" DRILLED COUNTERSINK TREATED AND PRIMED NEW HINGE SECTION IAW AEI CHAPTER 52 FIG 5201A. INSTALLED NEW AFT SECTION OF AFT HINGE IAW AEI CHAPTER 52 FIG 5201A. 2L73 4F A3WE 20051003000382005100300038EA 2005 10 3 SWIA200515593 120050921A2750860D10018 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07930SW6961 6961 7713 FLAPS FAIL CAUTION MESSAGE. REPLACED FECU. OPERATIONAL CHECK GOOD IAW CRJ MM 27-51-05. 2L72 4F RTA21EA 20051003000452005100300045WP 2005 10 3 UPS05845486 120050904A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 RT WING LE LOWER RIB IS CRACKED AT XFR 791.250. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 2, 51-1-21 AND 51-1-20D. 2L74 4F RT4A25 20051003000492005100300049WP 2005 10 3 UPS05845490 120050910A574036456124 FITTING DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 RT WING FUEL TANK NR 4 ALTERNATE STA XW 408 LWR STR NR 58 END FITTING CRACKED 2" LONG. REMOVED AND REPLACED BATHTUB FITTING IAW SRM 51-1-20D. 2L74 4F RT4A25 20051003000502005100300050WP 2005 10 3 UPS05845491 120050912A5313 LONGERON DOUG DC8 DC873F 302199FWP BS 1756 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 FOUND CRACKED LONGERON AT STA 1756 L14L. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-3-0, 53-2-2 FIG 11 AND 51-1-20D. 2L74 4F RT4A25 20051003000512005100300051NM 2005 10 3 AWXA200501118 120050925A532065C2181814 CHANNEL BOEING737 7373G7 1384595NM BS 597 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 CHANNEL JUST AFT OF BS 597 CRACKED, .85 INCHES IN LENGTH, AT BL 70R, WL 204. MAINTENANCE REMOVED CHANNEL AT BL 70R, WL 204 JUST AFT OF BS 597 IAW BOEING 737-300 SRM 51-40-02-0G. FABRICATED NEW CHANNEL IAW BOEING DWG 65C21818. INSTALLED FABRICATED REPAIR AT BL 70R, WL 204 JUST AFT OF BS 597 PARTS IAW BOEING 737-300 SRM 51-40-02-0G FIGS 3, 4, 6, 8, AND 12. 2L72 4F RTA16WE 20051003000532005100300053NM 2005 10 3 AWXA200501121 120050927A5330654577572 SKIN BOEING737 7373G7 1384595NM BS 727D CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - MAJOR REPAIR - DURING C18 CHECK, DISCOVERED FUSELAGE SKIN CRACKED AT STATION 727D, STR 23R. MAINTENANCE CUT OUT DAMAGED SKIN AT STATION 727D, STR 23R IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NO. 03-5361-05267-ES4. FABRICATED REPAIR DOUBLER, TRIPLER, TEAR STRAP INTERNAL DOUBLERS, TAPERED FILLER AND FILLER IAW AWA ER 03-5361-05267-ES4. INSTALLED FABRICATED REPAIR PARTS AT STATION 727D, STR 23R IAW AWA ER 03-5361-05267-ES4. 2L72 4F RTA16WE 20051003000562005100300056EU 2005 10 3 SF20050923 120050923A2721 TRIM SYSTEM SAAB SF340 SF340A 7850100EU AILERONS MALFUNCTIONED A UHLAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL17123 123XS FLIGHT 7578, IAD-ABE, PILOT CALLED ON THE RADIO SHORTLY AFTER TAKEOFF REPORTING AN AUTO TRIM LIGHT WARNING WITH YAW DAMPER ENGAGED. PILOT REPORTED YAW TRIM WAS 4 UNITS TO THE RIGHT AND 1/2 UNIT AILERON TRIM. AIRCRAFT RETURNED TO FIELD. 2L72 4T RTA52EU 20051003000582005100300058NM 2005 10 3 DHL2005748513 120050927A3350BR964411 LIGHT BOEING757 7572S7 1384962NM CABIN INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28905AW 23567 PHX - EEL - DURING A9 CHECK DISCOVERED SEAT MOUNTED EMERGENCY EXIT LIGHT AT ROW 29 LEFT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EXIT LIGHT ASSEMBLY AT ROW 29 LEFT. OPS CHECKS WERE GOOD. 2L72 4F RTA2NM 20051003000612005100300061NM 2005 10 3 05FDEA03080 120050924A57536521631261 SKIN BOEING727 727225 1384077NM ZONE 500 TORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 LEFT WING OUTBORD FORE FLAP UPPER SKIN SECTION MISSING (HONEYCOMB EXPOSED) REFERENCE FEDEX NSRM N00007. ORDERED AND RECEIVED LEFT OUTBORD FORE FLAP. INSTALLATION, ADJUSTMENT AND OPERATIONAL CHECK WAS ACCOMPLISHED ON FEDEX NSRM N00079 IAW B727-200 MM 27-51-011-4. 2L73 4F A3WE 20051003000632005100300063EU 2005 10 3 05FDEA03087 120050924A5320 FILLER AIRBUS310 A310203 3930313EU FS 3 MISSING A FDEAK NONE O OTHER ININSP/MAINT 1 SO25425FE 264 EXTERNAL DOUBLER AT FWD RT LOWER FUSELAGE NOSE SECTION AT FS 3 IS MISSING FILLER. REMOVED FLOOR ACCOMPLISHED REPAIR WITH MINOR DEVIATION BY EA 6-5330-92339. INSTALLED FLOOR AND PAINTED. 2L72 4F RTA35EU 20051003000652005100300065EU 2005 10 3 05FDEA03089 120050924A5347 SEAT TRACK AIRBUS310 A310203 3930313EU BS 543 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25445FE 297 SEAT TRACK LOBES ARE GOUGED. REPLACED, PRIMED AND PAINTED IAW SRM 51-40-21, 51-21-10, 53-10-16 AND MM 51-75-10-8. 2L72 4F RTA35EU 20051003000662005100300066NM 2005 10 3 05FDEA03090 120050925A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 HORIZ STAB LT BARREL NUT BORE NR 2 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 13. MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20051003000722005100300072NM 2005 10 3 05FDEA03095 120050925A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 HORIZ STAB LT BARREL NUT BORE NR 34 FOUND WITH CORROSION. SNRM N2606: DUPLICATE CARD. REFER TO SNRM N2663 WITH SDR TRACKING NO.05-3103 FOR REPAIR DETAILS. 2L73 4F RTA22WE 20051003000742005100300074NM 2005 10 3 05FDEA03097 120050925A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 HORIZ STAB RT BARREL NUT BORE NR 33 FOUND WITH CORROSION. SNRM N2609: DUPLICATE CARD. REFER TO SNRM N2661 WITH SDR TRACKING NO.05-3101 FOR REPAIR DETAILS. 2L73 4F RTA22WE 20051003000762005100300076NM 2005 10 3 05FDEA03099 120050925A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 HORIZ STAB RT BARREL NUT BORE NR 29 FOUND WITH CORROSION. REWORK/ REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 20. MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20051003000772005100300077NM 2005 10 3 05FDEA03100 120050925A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 HORIZ STAB RT BARREL NUT BORE NR 31 FOUND WITH CORROSION. REWORK/ REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 21. MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20051003000782005100300078NM 2005 10 3 05FDEA03101 120050925A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 HORIZ STAB RT BARREL NUT BORE NR 33 FOUND WITH CORROSION. REWORK/ REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 22. MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20051003000792005100300079NM 2005 10 3 05FDEA03102 120050925A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 HORIZ STAB LT BARREL NUT BORE NR 30 FOUND WITH CORROSION. REWORK/ REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 17. MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20051003000802005100300080EU 2005 10 3 AWXA200501108 120050904A5320D5311278900301 WEB AIRBUS320 A320231 3930325EU CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28634AW 091 SAL - DURING C4 CHECK DISCOVERED CORROSION ON WEB AT FS 20, Y-1584. REWORK WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 51-40-04. MAINTENANCE REMOVED WEB FROM FS 20 TO FS 24, Y-1584 TO Y-1784 IAW AIRBUS 320 SRM 51-72-11. NEW WEB INSTALLED FROM FS 20 TO FS 24, Y-1584 TO Y-1784 IAW AIRBUS 320 SRM 51-72-11. 2L72 4F RTA28NM 20051003000832005100300083NM 2005 10 3 AWXA200501111 120050903A5311654653754 FRAME BOEING737 7373G7 1384595NM BS 578 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - DURING C18 CHECK DISCOVERED RT OUTBOARD ATTACH ANGLE SIDE FRAME WEB CRACKED, .5 INCHES IN LENGTH, AT BS 578, WL 204, BL 68L. MAINTENANCE REMOVED THE SIDE FRAME WEB FROM BS 578 IAW BOEING 737-300 SRM 51-40-02-0G. FABRICATED NEW SIDE FRAME WEB IAW BOEING 737-300 DWG 65-46537 AND SRM 51-30-01-0G. INSTALLED FABRICATED REPAIR PART IAW BOEING 737-300 SRM 51-40-02-0G. 2L72 4F RTA16WE 20051003000862005100300086EU 2005 10 3 AWXA200501114 120050923A2150D2157160000000 BELLOWS AIRBUS320 A320232 3930326EU NR 1 A/C PACK INOPERATIVE A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28639AW 471 LAS - AIR TURNBACK - FLT 372 - DURING CLIMB CREW REPORTED THAT THE AIRCRAFT WOULD NOT HOLD CABIN CLIMB THRU 23000. CABIN AT 9900 AND CLIMBING, ECAM ACTION FOLLOWED. AIRCRAFT RETURNED TO LAS, DECLARED EMERGENCY, AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 PACK AIR COOLING BELLOWS IAW AIRBUS MM 51-52-00-200. PRESSURIZATION AND LEAK CHECKS WERE GOOD. 2L72 4F RTA28NM 20051003000922005100300092NM 2005 10 3 DHL2005748503 120050807A5313 STRINGER BOEING727 727225 1384077NM BS 970-990 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 AFT CARGO COMPT LOWER FUSELAGE STR 29L IS CORRODED BETWEEN STA 970 AND STA 990. REMOVED STR 29L KEEL BEAM CHORD FROM BS 950-1010 DRILLED AND LOCATED NEW KEEL BEAM CHORD P/N 65-56441-7 PO NR 53143 IAW S/B 727-53-179 FIG 12 TREATED AND PRIMED AREA AND CHORD IAW B727 SRM 51-10-2 INSTALLED AND TORQUED BOLTS AT BS 950A STR 29L - BS 1010 (TORQUED AS REQUIRED) IAW S/B 727-53-179 DATED JULY 13, 1989 FIG 12 AND SRM 51-30-4 FIG 2. 2L73 4F A3WE 20051003000992005100300099NM 2005 10 3 05FDEA03074 120050923A5314 KEELBEAM BOEING727 727232 1384082NM BS 805 CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25499FE 21018 FOUND CRACK IN THE DELTA KEELBEAM LWR FLANGE AT B/S 805 RBL 6 WL 148. REPAIRED DELTA KEELBEAM, BS 805, RBL6, WL 148 PER FED-EX EA 7-5310-91384. 2L73 4F A3WE 20051003001002005100300100NM 2005 10 3 2005UALA01003 120050918A335058781 LIGHT BOEING737 737322 1384676NM ROWS 12C-21C DIRTY A UALAK NONE O OTHER ININSP/MAINT 1 WP29364UA 24533 EEL LIGHTS INOP FROM ROW 12C TO 21C. CLEANED AND DRIED EEL LIGHTS BY SEAT 19A. 2L72 4F RTA16WE 20051003001012005100300101EU 2005 10 3 2005UALA01004 120050921A5313 STRINGER AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FS 53-54 CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29415UA 475 AFT PIT STR 42L HAS CORROSION BETWEEN FS 53 AND FS 54. 2L72 4F4 FRTA28NM E40NE 20051003001052005100300105NM 2005 10 3 DHL2055748504 120050813A5330 SKIN BOEING727 727225 1384077NM BS 1010 BULGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 FUSELAGE HAS A BULGE AT BS 1010 BETWEEN STR 29R AND STR 30. REMOVED FASTENERS AT DAMAGED AREA BS 1010 STR 30 IAW B727-SRM 51-30-2 EVALUATED SKIN AND EXFOLIATED BEYOND LIMITS PER SRM 53-30-1 FIG 1 B727. CUT OUT DAMAGED AREA 3 1/2" BY 2 1/2" IAW B727 SRM 53-30-3 FIG 1. FABRICATED DOUBLER MAT ID 2024T3 .090 PO NR 9002435 DIM.S 9" BY 16" AND FILLER MAT ID 2024T3 .080 PO NR 9002435 DIMS., 6" BY 7" IAW B727 SRM 53-30-3 FIG 3A. TREATED AND PRIMED AREA IAW B727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B727 SRM 51-30-2 AND 53-30-3 FIG 1. THIS REPAIR IS CATEGORY "B". 2L73 4F A3WE 20051003001062005100300106NM 2005 10 3 05FDEA03068 120050923A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 CRACK INDICATION FOUND AT STRINGER END OF STRINGER 16 (UPPER STRINGER), APPROXIMATE LENGTH 17 INCHES, RIGHT SIDE WING TANK. CRACK PROPAGATES TOWARDS INBOARD TO THE NEAREST WEB. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I AND CLIP REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. CLIP. 2L73 4F RTA22WE 20051003001142005100300114CE 2005 10 3 DXTA200500979 120050922A2120 SMOKE CESSNA750 750 2076810CE COCKPIT DETECTED E DXTAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL07904QS 7500210 AFTER ENGINES WERE STARTED, THE COCKPIT FILLED UP W/ SMOKE. SHUTDOWN ENGINES AND APU AND EVACUATED AIRCRAFT, NO PAX ONBOARD. 2L72 4J RTT00007WI 20051003001162005100300116EU 2005 10 3 2005UALA01006 120050921A3350 SWITCH AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE EMERGENCY LIGHT MALFUNCTIONED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29455UA 1105 ALL CABIN EMERGENCY EXIT SIGNS ILLUMINATED WITH SWITCHES SELECTED OFF. AMIS ITEM 8612012, CONTINUATION OF AMIS ITEM 8612010: CYCLED NO SMOKING SWITCH. 2L72 4F4 FRTA28NM E40NE 20051003001172005100300117NM 2005 10 3 2005UALA01007 120050819A4990 ODOR BOEING737 737322 1384676NM COCKPIT DETECTED A UALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP29347UA 24251 ELECTRICAL SMELL OCCURRED IN COCKPIT AND CABIN AFTER 1ST ATTEMPT TO CONNECT GROUND POWER. REMOVED SPEED SENSOR ACC PNL FOUND APU INLET OIL SOAKED, RAN APU UNABLE TO FIND SOURCE 22SEP SFO: PER AMM 49-00-00-0101 PG 180M FIG 140 LK 21. REPLACE SPEED SENSOR PACKINGS PER AMM 49-61 -41 AS PRECAUTION. 24SEP DEN: REPLACED SPEED SENSOR PROBE PACKINGS. FOUND HYD LEAK IN TAIL ENTERING APU INLET. LEAK FIXED. PERFORMED PACK BURN. APU OPERATIONAL. PACKS USEABLE. 2L72 4F RTA16WE 20051003001182005100300118NM 2005 10 3 2005UALA01008 120050913A2751 CONNECTOR BOEING737 737322 1384676NM FLAP TRANSMITTERCORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29303UA 23644 FOUND RIGHT FLAP POSITION TRANSMITTER CONNECTOR D229 HAD CORROSION DAMAGE. PIN 9 OF FLAP TRANSMITTER CONNECTOR WAS CORRODED. CAPTAIN'S STALL WARNING SYSTEM WOULD NOT TEST DUE TO A CORRODED WIRE DISCONNECT PLUG (D229). THE SUBJECT DISCONNECT PLUG WAS REPLACED AND ALL ASSOCIATED WIRING DISCREPANCIES WERE CORRECTED. STALL WARNING TEST WAS ACCOMPLISHED PER MM 27-32-00 AND ALL CHECKED NORMAL. THIS IS CONSIDERED AN ISOLATED INCIDENT. ON-CONDITION, THERE IS NO HISTORY OF SIMILAR PREVIOUS FAILURES AT THIS LOCATION 2L72 4F RTA16WE 20051003001202005100300120NM 2005 10 3 2005UALA01010 120050922A3350362624 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE SEAT 8H INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29128UA 30023 SEAT 8H AFT EMERGENCY LIGHT INOP. REPLACED EEL LAMP. 2L74 4F4 FRTA20WE E24NE 20051003001212005100300121NM 2005 10 3 2005UALA01011 120050922A3397794640 WIRE BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29128UA 30023 AFT MID GALLEY FWD CROSS AISLE WALL MOUNTED EMERGENCY LIGHT INOP. REPAIRED FEEDER CABLE. 2L74 4F4 FRTA20WE E24NE 20051003001242005100300124NM 2005 10 3 2005UALA01014 120050923A33977945243 CONNECTOR BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT UNSECURE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29193UA 26890 EEL 41H INOP. SECURED CONNECTOR. 2L74 4F4 FRTA20WE E24NE 20051003001252005100300125EU 2005 10 3 2005UALA01015 120050922A5313 STRINGER AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FS 57-58 CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29421UA 500 CORROSION ON STR 43L BETWEEN FS 57 AND FS 58. BUSINESS DECISION TO REPLACE STRINGER RATHER THAN REPAIR. 2L72 4F4 FRTA28NM E40NE 20051003001262005100300126NM 2005 10 3 2005UALA01016 120050922A2780 WARNING LIGHT BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE SLAT ASYMMETRY ILLUMINATED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29676UA 30028 RETURNED TO SFO DUE TO LEADING EDGE SLAT ASYMMETRY PROBLEM. 2L72 4F4 FRTA1NM E24NE 20051003001282005100300128CE 2005 10 3 G41A200500001 120050802A3241393091 ANTI-SKID SYS LEAR 55 55LEAR 5170702CE MLG MALFUNCTIONED E G41AO OTHER O OTHER LDLANDING 1 SW01277AL 104 AFTER LANDING, MIDLAND TX, APPROX 13:49 PM TO DROP OFF PAX`S, SCHEDULED TO PROCEED TO DALLAS TO DROP OFF REMAINING PAX`S, THE PILOT EXPERIENCED A VIBRATION DURING TAXI. INSPECTION OF A/C REVEALED RT OUTBOARD MAIN TIRE HAD A BLOW OUT DUE TO A POSSIBLE LOCKUP OF THE WHEEL. A SERVICEABLE WHEEL AND TIRE WAS INSTALLED ON THE A/C AND A/C WAS FLOWN TO EL PASO. ANOTHER A/C WAS DISPATCHED TO MIDLAND TO TRANSPORT PAX`S TO FINAL DESTINATION TO ADDISON AIRPORT IN DALLAS TX. UPON ARRIVAL AT ELP, A/C WAS PLACED ON JACKS AND RT WHEEL ANTI-SKID SYSTEM WAS NOT FUNCTIONING PROPERLY. A BROKEN WIRE WAS DISCOVERED ON ANTI-SKID WIRING HARNESS LOCATED IN THE WHEEL WELL. THE WIRE WAS REPAIRED AND SYSTEM CHECKED OK. 2L72 4F A10CE 20051003001312005100300131NM 2005 10 3 2005UALA01019 120050922A5330 SKIN BOEING737 737522 138449FNM BS 1064 DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29918UA 25385 AFT LOWER FUSELAGE APPROX STA 1064 BETWEEN STR 27L AND 28L HAS DENT. REMOVED DAMAGE, FABRICATED & INSTALLED DOUBLER. REF SRM 53-80-01 FIG 201 2L72 4F RTA16WE 20051003001322005100300132NM 2005 10 3 2005UALA01020 120050922A5311 FRAME BOEING737 737522 138449FNM BS 867 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29918UA 25385 AFT CABIN FRAME IS CRACKED AT STA 867 NEAR STR 8R, AROUND FASTENER HOLE. REMOVED DAMAGED AREA ON FRAME. VERIFIED CRACK WAS REMOVED BY HFEC INSPECTION. FABRICAT ED AND INSTALLED REPAIR ANGLES. ANGLES FORMED FROM 7075-0 MAT ERIAL AND HEAT TREATED TO 7075 T6. FABRICATED NEW AC DUCT BRA CKET AND INSTALLED ON FRAME. REF MM 53-10-84. 2L72 4F RTA16WE 20051003001332005100300133NM 2005 10 3 2005UALA01021 120050923A7500 BLEED AIR SYS BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU NR 1 MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29203UA 24718 FLIGHT DIVERTED DUE TO NR 1 BLEED WILL NOT SHUT OFF. NR 1 ENGINE BLEED AIR REGULATOR FAILED. REPLACED BLEED AIR REGULATOR PER MM 36-11-16 AND PERFORMED OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA16WE E21EU 20051003001352005100300135NM 2005 10 3 DL73S050563 120050921A215020405011 ACM BOEING737 737247 138448DNM RIGHT UNSERVICEABLE A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27237WA 23185 A/C WOULD NOT MAINTAIN CABIN PRESSURE. REPLACED RT ACM AND FWD LAV FILL LINE CHECK VLV. 2L72 4F A16WE 20051003001402005100300140EA 2005 10 3 COMA0560517 120050922A5312601R32026 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA BS 559 CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01926CA28934 7027 WHILE PERFORMING TASK INS-2-2-27L0005 ITEM NR 6, CLEANING OF THE RIGHT REAR AILERON QUADRANT LOCATED ON THE AFT WALL OF THE MLG WHEEL WELL, DISCOVERED A CRACK ON THE SEMI-PRESSURE BULKHEAD FS 559.00, BL 23L-23R. PERFORMED REO 601R-53-41-350. 2L72 4F RTA21EA 20051003001412005100300141WP 2005 10 3 UPS05845492 120050825A5730 DOUBLER DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 RT WING LWR SURFACE DOUBLER CORRODED AND POSSIBLE CRACK AT XW 408.343 AFT SIDE AROUND FASTENER HOLE. NDT DETECTED A 1/2" CRACK EXTENDING FROM FASTENER HOLE TO EDGE OF PART. CUT OUT DAMAGE, TREAT, AND PRIMED IAW SAA SK 801-804073. 2L74 4F RT4A25 20051003001422005100300142WP 2005 10 3 UPS05845493 120050825A5310 DOOR FRAME DOUG DC8 DC873F 302199FWP CARGO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE: C3, D-PIT DOOR FWD UPPER CORNER CRACKED 1/2" LONG. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0 FIG 21. 2L74 4F RT4A25 20051003001442005100300144WP 2005 10 3 UPS05845498 120050831A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE:C3 LT UPPER WING NR 2 MAIN TANK ACCESS PANEL 505F UNDER LANDING HAS 1" LONG POSSIBLE CRACK. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1 FIG 36. 2L74 4F RT4A25 20051003001462005100300146WP 2005 10 3 UPS05845500 120050831A53404640162502N FITTING DOUG DC8 DC873F 302199FWP BS 1040 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE:C3 MAIN CABIN BELT FRAME END FITTING CORRDED AT STA 1040 L21R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-0. 2L74 4F RT4A25 20051003001482005100300148WP 2005 10 3 UPS05845503 120050902A5313 LONGERON DOUG DC8 DC873F 302199FWP BS 25 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE:C3 A/C COMPARTMENT STA 25 LONGERON 31R, LONGERON HAS HEAVY CORROSION. REMOVED LONGERON, FABRICATED, AND INSTALLED REPLACEMENT LONGERON IAW DC-8 SRM 51-1-20D AND 51-1-21. 2L74 4F RT4A25 20051003001492005100300149WP 2005 10 3 UPS05845504 120050902A534047731561N FITTING DOUG DC8 DC873F 302199FWP BS 1688 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE:C3 L26L END FITTING APPEARS CRACKED AT STA 1688. REMOVED AND REPLACED LONGERON END FITTING IAW DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20051003001502005100300150WP 2005 10 3 UPS05845505 120050903A5340 FITTING DOUG DC8 DC873F 302199FWP BS 1180 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE:C3 C PIT STA 1180 LONG 35R BATH TUB FITTING IS CRACKED. REMOVED AND REPLACED BATH TUB FITTING IAW DC-8 SRM 53-2-0 FIG 2D. 2L74 4F RT4A25 20051003001512005100300151WP 2005 10 3 UPS05845511 120050903A5712 RIB DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE:C3 LT WING LE LOWER RIB PREVIOUS REPAIR IS CRACKED AT XFS 385.250. REMOVED REPAIR ANGLE, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 51 -1-20D, 57-3-3 FIG 5, 57-2-0 FIG 2 AND 51-1-15. 2L74 4F RT4A25 20051003001522005100300152WP 2005 10 3 UPS05845512 120050903A5712 RIB DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE:C3 LT WING LE LOWER RIB PREVIOUS REPAIR IS CRACKED AT XFS 360.250. REMOVED REPAIR ANGLE, FABRICATED AND INSTALLED REPAIR ANGLE.IAW SRM 5 1-1-20D,57-3-3 FIG 5,57-2-0 FIG 2 AND 51-1-15. 2L74 4F RT4A25 20051003001532005100300153NE 2005 10 3 WRNA200500022 220050914A7230 COMPRESSOR AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE NR 1 ENGINE STALLED A WRNAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SO05821SC 211 517410 NR 1 ENGINE COMPRESSOR STALLED 4 TIMES CLIMBING THROUGH 15,500 FT. AFTER COMPRESSOR STALL, WITH SAME THROTTLE ANGLE, NR 1 ENG N1 WAS 98.4 PERCENT WHILE NR 2 WAS 104 PERCENT. ALL OTHER PRIMARY ENGINE PARAMETERS WERE FLUCTUATING. WHEN THE NR 1 THRUST LEVER WAS RETARDED TO FLT IDLE THE COMPRESSOR STALL CEASED AND NORMAL FLIGHT IDLE PARAMETERS WERE NOTED. AIRCRAFT LANDED WITHOUT INCIDENT. 2L72 4F4 FRTA35EU E23EA 20051003001542005100300154NM 2005 10 3 BB05085 120050926A335020131A BATTERY PACK BOEING757 757225 1384959NM EMERGENCY LIGHT DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19606AU 22202 BOS - THE LEFT FORWARD EMERGENCY LIGHTS SOURCE INOP. MAINTENANCE REPLACED THE LEFT FORWARD EMERGENCY LIGHTS BATTERY PACK. OPERATIONALLY CHECKS OK. 2L72 4F RTA2NM 20051003001562005100300156EU 2005 10 3 EMB05013 120050924A3350340022 BATTERY PACK EMB ERJ170ERJ170100 EU EMERGENCY LIGHT DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19814MD1412 000033 PHL - AN EMERGENCY LIGHT BATTERY FAULT ILLUMINATED. MAINTENANCE REPLACED THE RIGHT SIDE EMERGENCY LIGHT BATTERY PACK. OK FOR SERVICE. 2L74 4F RTA56NM 20051003001612005100300161NM 2005 10 3 SWAA052953 120050927A55536546874 FITTING BOEING737 7373H4 1384600NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29618WN 28034 DURING SCHEDULED D CHECK, FOUND LT AND RT VERTICAL STAB ATTACH FITTINGS CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER. 2L72 4F RTA16WE 20051003001642005100300164NM 2005 10 3 SWAA052956 120050927A53306545766 SKIN BOEING737 7373A4 1384585NM BS 452 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 452, STR 16L. REPAIRED SKIN PER SWA EA AND SRM. 2L72 4F RTA16WE 20051003001662005100300166NM 2005 10 3 SWAA052942 120050927A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 616 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 616, STR 5R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051003001672005100300167NM 2005 10 3 SWAA052943 120050927A53226546529 SHEAR TIE BOEING737 7373H4 1384600NM BS 500A CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500A, LBL 18. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051003001682005100300168NM 2005 10 3 SWAA052944 120050927A53226546529 SHEAR TIE BOEING737 7373H4 1384600NM BS 500 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500, RBL 12. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051003001692005100300169 2005 10 3 SWAA052945 420050927A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051003001702005100300170NM 2005 10 3 DHL2005748524 120050816A5753 SKIN BOEING727 727225 1384077NM FORE FLAP DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 RT WING INBD FORE FLAP DELAMINATED ON UPPER SURFACE 70" FROM OTBD END. CUT OUT DELAMINATED AREA RT I/B FORE FLAP UPPER SURFACE 70" FROM O/B END APPROX 4" DIA FAB FILLER APPROX 4" DIA AND DOUBLER APPROX 7" DIA FROM 2024 T3 .016 PO 9002273, CLEANED PREPPED APPLIED ADHESIVE PRIMER BONDED CLEANED TREATED PRIMED AND SEALED EDGES IAW B727 SRM 57-50-1 FIG 3 57-50-2 FIG 3 AND 51-40-20-FIG 1. 2L73 4F A3WE 20051003001752005100300175NM 2005 10 3 C1HA200568004 120050927A5311 FRAME BOEING727 7272S7 138407ZNM BS 990 CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15686CA 22021 UPPER FRAME CHORD CORRODED ON LWR SURFACE IN AFT PIT BS 990 OVER STR 27R JUST BEHIND AFT DOOR CUTOUT. CUT OUT DAMAGED AREA FABBED AND INSTALLED FILLER 2" BY 1" AND DOUBLER ANGLE 8 3/4" BY 3 1/4" FROM 10134-3001 7075 T6 PO NR 9001253 IAW 727 SRM 51-40-4 FIG 1. 2L73 4F A3WE 20051003001772005100300177WP 2005 10 3 UPS05845513 120050903A5712 RIB DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE:C3 LT WING LE LOWER RIB IS CRACKED AT XFS 622.500. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-3-0 FIG 1 AND 51-1-21. 2L74 4F RT4A25 20051003001782005100300178WP 2005 10 3 UPS05845514 120050909A5330 SKIN DOUG DC8 DC873F 302199FWP 1746 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE: C3, CRACK ON FUSEAGE SKIN STA 1746 L15R. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER, FILLER AND FINGER DOUBLER IAW SRM 53-02-01, 53-05-03, 51-1-26, 51-1-20D AND 51-1-21. 2L74 4F RT4A25 20051003001792005100300179WP 2005 10 3 UPS05845515 120050910A53204772397U1 FITTING DOUG DC8 DC873F 302199FWP BS 1766 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE:C3 INSIDE 60 HOLE, LONGERON END FITTING CRACKED 2" LONG AT STA 1766 L10R. REMOVED AND REPLACED END FITTING IAW SRM 51-3-0, 51-1-21 AND 51-1-20D. 2L74 4F RT4A25 20051003001802005100300180WP 2005 10 3 UPS05845516 120050911A5320 INTERCOSTAL DOUG DC8 DC873F 302199FWP BS 1079 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE:C3 HEAVY CORROSION ON INTERCOSTAL AT STA 1079 L35L. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW 51-1-20D AND DWG 9758 507. 2L74 4F RT4A25 20051003001822005100300182NM 2005 10 3 UPS05M45521 120050815A5510 STRUCTURE DOUG MD11 MD11F 3023600NM HORIZONTAL STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01256UP 48405 RT HORIZ STAB BARREL NUT BORE NR 22R FOUND WITH CORROSION. CORROSION REMOVED PER SRM 51-21-01.V2R37, B/N HOLE 22R REAMED TO 1.067" AND REMAINING BLEND OUT 0.020" DEEP, FOUND OUT OF LIMIT. REWORKED B/N HOLE 22R BORE RADIUS SMOOTHENED AND PROTECTED PER SRM 51-21-01V2.R37. FAB SLEEVE REPAIR BUSHING PER EO MD11-5510-19409-J.FIG.5. APPLIED SEALANT PR1422 B1/2 AT 22R BORE AND INSTALLED S/BUSHING PER SRM51-21-01V2.R37, SATIS. 2L73 4F RTA22WE 20051003001832005100300183NM 2005 10 3 05FDEA03048 120050922A3297 CONNECTOR BOEING727 727233 138408ANM HYD SYSTEM DETERIORATED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25265FE 21671 ON T/O FROM MSN, PLACED GEAR HANDLE TO UP, GEAR RETRACTED AND ALL LIGHTS EXTINGUSIHED NORMALLY, HOWEVER WHEN THE GEAR HANDLE WAS PLACED TO OFF, THE RED DOOR LIGHT ON FWD PANEL AND RT MAIN GEAR DOOR LIGHT ON S/O PANEL ILLUMINATED. REMOVED THE CANON PLUG FROM THE RT LANDING GEAR DOOR SWITCH AND FOUND THE PLUG DETERIORATED AND SATURATED WITH HYDRAULIC FLUID. REMOVED THE CANON PLUG AND CLEANED THE CONTACTS WITH CONTACT CLEANER INSTALLED THE NEW PLUG IAW THE B727-200 WDM 32-60-04-PLUG(D752). 2L73 4F RTA3WE 20051003001842005100300184NM 2005 10 3 05FDEA03050 120050922A2197 WIRE BOEING727 727233 138408ANM ZONE 100 MELTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25267FE 21673 WIRE BUNDLE MELTED TO LEFT AFT AIR CONDITIONING HEAT EXCHANGER AFT SIDE. REMOVED MELTED PLASTIC FROM HARNESS IAW BOEING SWPM 20-10-11. NO DAMAGE TO WIRING WAS FOUND. REPOSITIONED HARNESS AND INSTALLED PROTECTIVE SLEEVING IAW BOEING SWPM 20-10-11. 2L73 4F RTA3WE 20051003001862005100300186NM 2005 10 3 SWAA052947 120050927A3350D71702001 BATTERY PACK BOEING737 7373H4 1384600NM EMERGENCY LIGHT FAULTY A SWAAK NONE O OTHER ININSP/MAINT 1 SW29385SW 26600 DURING SCHEDULED RON CHECK, L2 DOOR EMERGENCY EXIT LIGHT REMAINED ILLUMINATED. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20051003001872005100300187NM 2005 10 3 SWAA052948 120050927A53306545775 SKIN BOEING737 7375H4 138449DNM BS 817 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29508SW 24185 DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 817, STR 25L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051003001902005100300190EA 2005 10 3 COMAO560518 120050922A5312601R32026 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA BS 559 CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01931CA27852 7037 WHILE PERFORMING TASK INS-2-2-27L0005 ITEM NR 6, CLEANING OF THE RIGHT REAR AILERON QUADRANT LOCATED ON THE AFT WALL OF THE MLG WHEEL WELL, DISCOVERED A CRACK ON THE SEMI-PRESSURE BULKHEAD FS 559.00, BL 23L-23R. PERFORMED TEMPORARY REPAIR PER REO 601R-53-41-353. 2L72 4F RTA21EA 20051004000542005100400054NM 2005 10 4 CALA0500322 120050929A5315BAC1505100246 FLOORBEAM BOEING737 7373T0 1384582NM STA 344 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769333 23571 INSPECTION FOUND MAIN DECK FLOORBEAM CORRODED AT STA 344, LBL 16 TO RBL 9. THE SECTION OF FLOORBEAM WAS REPLACED IAW SRM 53-10-51. 2L72 4F RTA16WE 20051004000562005100400056NM 2005 10 4 CALA0500324 120051003A3397 WIRE BOEING737 7373T0 1384582NM EMERGENCY LIGHT SHORTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769348 23586 THE FIRST CLASS EMERGENCY ESCAPE AISLE PATH LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE FOUND SHORTED WIRING TO TRANSFORMER. THE WIRING WAS REPAIRED AND OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20051004000572005100400057 2005 10 4 CALA0500325 420051002A2330RDAV980301 MONITOR BOEING757 757224 1384958NM ROW 17ABC INOPERATIVE A CALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW272612336609 28966 A STRONG ELECTRICAL SMELL WAS NOTICED IN THE CABIN AND THEN THE LCD VIDEO SCREEN AT ROW 17 ABC BLANKED OUT WHILE EN ROUTE TO LAX. THE POWER TO THE ENTERTAINMENT SYSTEM WAS REMOVED AND THE SMELL DISSIPATED. THE FLIGHT WAS CONTINUED TO LAX WHERE IT LANDED WITHOUT FURTHER PROBLEMS. THE LCD VIDEO MONITOR WAS FOUND AT FAULT. THE MONITOR WAS REMOVED AND REPLACED AND OPERATIONAL CHECKS WERE GOOD IAW MM 23-32-08, PAGE 401. IN ADDITION, THE ASSOCIATED WIRING WAS INSPECTED IAW MM 20-60-04, PAGE 201 AND NO DEFECTS WERE NOTED. 2L72 4F RTA2NM 20051004000592005100400059NM 2005 10 4 PIDA20050146 120050927A5340654580711 ATTACH ANGLE BOEING737 737228 13844AGNM BS 294 CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 CRACK IN THE WEB AND ATTACH ANGLE JUST FORWARD OF THE R1 DOOR AT BS 294 ABOVE STR 12RT. REPLACED WEB AND ANGLE PER DWG 65-45807 AND SRM 51-10-1. 2L72 4F RTA16WE 20051004000662005100400066NM 2005 10 4 PIDA20050149 120050930A5313 STRINGER BOEING737 737228 13844AGNM BS 986 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 STR 25 LT HAS CORROSION UNDER FRAME AT BS 986. REPLACED DAMAGED SECTION OF STRINGER FROM BS 967 TO BS 1016 PER SRM 53-10-03 AND SRM 51-30-00. 2L72 4F RTA16WE 20051004000682005100400068NM 2005 10 4 PIDA20050148 120050930A5313 STRINGER BOEING737 737228 13844AGNM BS 967-1016 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 FOUND STR 27 LT HAS CORROSION FROM BS 967 TO BS 1016. REPLACED DAMAGED SECTION OF STRINGER PER SRM 53-10-03 AND SRM 51-30-00. 2L72 4F RTA16WE 20051004000692005100400069SO 2005 10 4 SWIA200515582 120050923A27513471001001 ANNUNCIATOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07212SW686 686 120276 CREW REPORTS FLAP CONTROL FAULTS DURING FLAP MOVEMENT. REPLACED FLAP ANNUNCIATOR ASSY. OPERATIONAL CHECK GOOD IAW EMB MM 27-50-05. 2L72 4T RTA31SO 20051004000702005100400070 2005 10 4 SWIA200515583 420050923A22166225734002 SERVO EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07224SW1460514605 120294 GRINDING NOISE HEARD WITH YAW ENGAGED INFLIGHT, VIBRATION FELT THOUGHT PEDALS. REPLACED RUDDER AUTOPILOT SERVO IAW MM 22-10-05. OPERATIONAL CHECK GOOD IAW MM 22-10-00. 2L72 4T RTA31SO 20051004000712005100400071SO 2005 10 4 SWIA200515584 120050921A27513471001001 ANNUNCIATOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER N FALSE WARNING APAPPROACH 1 NM07293SW8923 4689 120320 ON FINAL FLAPS 15 SELECTED FLAP CONTROL FAULT, AND SINGLE CHIME SOUNDED. REPLACED FLAP ANNUNCIATOR UNIT IAW 27-50-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20051004000722005100400072EA 2005 10 4 SWIA200515585 120050920A335020131A BATTERY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCHARGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07961SW4941 4941 7857 EMERG LIGHT STRIP (FLOOR) ON RIGHT SIDE IS BURNED OUT. REPLACED NR 2 EMERGENCY BATTERY PACK NR 2 IAW CRJ MM 33-51-04. OPERATIONAL CHECK GOOD, PN ON 2013-1A SN ON 36254 OFF 83055. 2L72 4F RTA21EA 20051004000762005100400076SO 2005 10 4 SWIA200515590 120050922A27203081401003 ACTUATOR EMB 120 EMB120ER 3260203SO RUDDER INOPERATIVE A SWIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM07236SW4977 4977 120312 ON TAKEOFF, RUDDER JAMMED. REPLACED RUDDER BLUE SYSTEM ACTUATOR IAW MM 27-22-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20051004000792005100400079NM 2005 10 4 CALA0500319 120050924A5310 CROSSBEAM BOEING737 737724 13844BYNM BS 344 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716701 28762 INSPECTION FOUND TOP OF CROSSBEAM CORRODED AT STA 344, LBL 17 TO RBL 7. REPAIRED IAW ECRA 5321-01294. 2L72 4F RTA16WE 20051004000812005100400081NM 2005 10 4 CALA0500321 120050926A32322745711 ACTUATOR BOEING757 757324 1384930NM LT MLG DOOR INOPERATIVE A CALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW27748561079 32815 CREW RECEIVED EICAS MSG "GEAR DOORS" WITH DOORS LIGHT AND GEAR DISAGREE WITH GEAR LIGHT AFTER GEAR RETRACTION DEPARTING SEA. THERE WAS ALSO ASSOCIATED BUFFETING. THE GEAR DOORS LIGHT WENT OUT DURING CLIMB AND AT ALTITUDE THE GEAR DISAGREE LIGHT WENT OUT. THE AIRCRAFT WAS RETURNED TO SEA WHERE IT LANDED WITHOUT INCIDENT. PROX BOX FAULT CODES INDICATED THE LEFT MAIN GEAR WAS NOT UP AND LOCKED AND THE DOOR WAS NOT CLOSED. THE LT MLG DOOR ACTUATOR WAS REMOVED AND REPLACED IAW MM 32-32-12. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA2NM 20051004000832005100400083EU 2005 10 4 UPS05145532 120050928A3350 LAMP AIRBUSA300 A300F4622R 3930360EU EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01154UP 0840 WALL MOUNTED EMERGENCY LIGHT ABOVE MIRROR INOP, IN LAVATORY. RELAMPED WITH SERVICEABLE LAMP IAW A-300-600 AMM 33-51-21-4. OPS CHECK NORMAL. 2L72 4F RTA35EU 20051004000842005100400084NM 2005 10 4 UPS05245523 120050913A5311 FRAME BOEING727 72725C 138400HNM BS 680 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01932UP 19856 CORROSION FOUND AROUND ANCHOR NUT ON FRAME UPPER CHORD LWR SIDE AT BS 680 RBL 25. REPAIR CARRIED OUT IAW SRM 51-10-01, 51-10-2 AND 51-40-3. 2L73 4F A3WE 20051004000852005100400085NM 2005 10 4 UPS05245524 120050912A5330 LAP JOINT BOEING727 72725C 138400HNM BS 590 SKIN CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01932UP 19856 SUSPECT CORROSION AT LAP JOINT DUE TO 2 POPPED FASTENER HEADS AT BS 590, S10R. CORROSION ON UPPER SKIN FOUND TO BE OUTSIDE LIMITS. REPAIR CARRIED OUT IAW SRM 51-30-02, 51-10-06, 53-30-1 & 53-30-3. 2L73 4F A3WE 20051004000862005100400086NM 2005 10 4 UPS05245525 120050909A5751 CASTING BOEING727 72725C 138400HNM LT AILERON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01932UP 19856 CRACK FOUND ON LT OUTBOARD AILERON LOCKOUT SUPPORT CASTING. LEFT O/B AILERON LOCKOUT SUPPORT CASTING REPLACED IAW MM 27-10-64, 27-1 0-60, 20-10-20, 27-10-00 & SRM 51-30-2. 2L73 4F A3WE 20051004000872005100400087NM 2005 10 4 UPS05245526 120050817A2820 FITTING BOEING727 72731C 1384011NM FUEL SYSTEM LEAKING A IPXAK NONE K FLUID LOSS ININSP/MAINT 1 SO01922UP 19231 INSPECTION TYPE: C+SI, FUEL LEAK FROM UNDERNEATH LT LANDING GEAR FWD TRUNNION SUPPORT SITTING SEEMS TO BE COMING FROM LWR LARGE BOLTS. LWR I/B FASTENERS (X2) REMOVED IAW TRUNNION REMOVED AND CORROSION FOUND SRM 51-30-02 AND BOTH HOLES REAMED TO 1ST OVERSIZE DUE TO CORROSION. CORROSION STILL EVIDENT. FITTING REMOVED IAW AAAE EO 2005-081-001 AND REWORKED. TRUNNION RESEALED IAW MM28-11-00. UPS FILE NUMBER = B727-5 330-22949. 2L73 4F A3WE 20051004000902005100400090NE 2005 10 4 UPS05545535 220050928A7200 ENGINE BOEING757 75724APF 1384969NM RROYCERB211 RB211535E4 54555NE LEFT FLAMED OUT A IPXAE ENGINE SHUTDOWN XJ ENGINE FLAMEOUT WARNING INDICATION LDLANDING 1 SO01445UP 27390 L ENG EEC EICAS MESSAGE. LT ENG LIMITER EICAS MESSAGE. LT ENG STALLED, FLAMED OUT, SHUTDOWN AFTER LANDING. BOROSCOPED NR 1 ENG PER MM 72-00-00-6. NO DEFECTS NOTED. 2L72 4F4 FRTA2NM E12EU 20051004000912005100400091EA 2005 10 4 COMA0560520 120050922A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION DEDESCENT 1 SO01819CA 7415 FLIGHT 5265 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2L72 4F RTA21EA 20051004000932005100400093NM 2005 10 4 MASA200500671 120050824A612378249050 CONTROL UNIT DHAV DHC8 DHC8202 2809007NM NR 2 ENGINE MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07455YV18864 455 ASH 7047 DEN, NR 2 ENG FEATHERS ABOVE IDLE. MX REMOVED AND REPLACED NR 2 PCU. 2H72 4T RTA13NM 20051004000952005100400095EA 2005 10 4 COMA0560519 120050922A322016736 SERVO VALVE CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A COMAO OTHER J WARNING INDICATION LDLANDING 1 SO01962CA2420 7123 FLIGHT 5757- NWS CAUTION. REPLACED THE ELECTRO HYD SERVO VALVE. 2L72 4F RTA21EA 20051004000962005100400096NM 2005 10 4 SWAA052973 120050928A335010107451 SIGN BOEING737 7373A4 1384585NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29669SW 23752 L1 DOOR EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM. 2L72 4F RTA16WE 20051004000982005100400098NM 2005 10 4 SWAA052975 120050928A53306545777 SKIN BOEING737 7373Q8 1384670NM BS 960 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 960, STR 21L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051004000992005100400099NM 2005 10 4 SWAA052976 120050928A53116546529 BELTFRAME BOEING737 737317 138447PNM BS 500A CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE BELTFRAME CORRODED AT BS 500A, RBL 1. REPAIRED BELTFRAME PER SRM. 2L72 4F RTA16WE 20051004001002005100400100NM 2005 10 4 SWAA052977 120050927A33506104781 BATTERY PACK BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29735SA 27867 DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20051004001022005100400102 2005 10 4 SWAA052979 420050926A256563550 SLIDE BOEING737 7377AD 1384502NM R2 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29798SW 28436 R2 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20051004001032005100400103NM 2005 10 4 DHL2005748525 120050817A5344 HINGE BOEING727 727225 1384077NM L1 DOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 L1 DOOR LWR HINGE CUT OUT CRACKED (HFEC CONFIRMED). REMOVED DOOR TRIM FWD SIDE AND FASTENERS AS NEEDED IAW B727 SRM 51-30-2, CUT OUT DAMAGED SKIN AND DOUBLER AT L1 DOOR LOWER HINGE CUT OUT IAW S/B 727-53A0198 FIG 3 REV 2 1 3/8" BY 2 5/8" CRACK WAS 1.75 LONG FAB FILLER AND DOUBLER FROM FILLER 2024T3 .125 1 3/8" BY 2 5/8" PO 9912445 DOUBLER CRES 301- 1/2 HD .063" (6 1/4" X 17 1/2") PO 9001442 IAW S/B 72753A0198 FIG 4 DETAIL IV SHEETS 1 THRU REV 2 TREATED AND PRIMED FILLER DOUBLER AND WORK AREA IAW S/B 727-53A0198 FIG 4 SHEETS 5, 6. INSTALLED FILLER DOUBLER AT LI DOOR LWR HINGE CUT OUT IAW B727 53A0198 FIG 4 SHEETS 5 AND 6 REV 2. 2L73 4F A3WE 20051004001042005100400104NM 2005 10 4 DHL2005748526 120050817A5210 SKIN BOEING727 727225 1384077NM L1 DOOR BENT A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 A/C L1 DOOR UPPER HINGE AREA DOOR SKIN BENT. EVAL BENT AREA FOUND CRACK AND STOP DRILLED CRACK DIA 250 IAW B727 SRM 51-10-1. FAB DOUBLER REPAIR 2024T3 .063 8" BY 7 1/4" PO 9001634 IAW B727 SRM 52-00-3 FIG 3 SHEETS 1-4. TREATED AND PRIMED DOUBLER AND AREA IAW B727 SRM 51-10-2. INSTALLED REPAIR IAW B727 SRM 52-003 FIG 3. NOTE NDT NO CRACKS NOTED PER NDT MAN PART 6, 51-00-00 FID 23. 2L73 4F A3WE 20051004001052005100400105NM 2005 10 4 05FDEA03122 120050926A5330 SKIN DOUG MD11 MD11 3023602NM BS 695 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 LOWER FX: DENT ON FX EXTERIOR SKIN AREA ALONG STA 695, ALONG L-50L. REPAIRED PER SRM 53-20-00 FIG.6 VOL I, EO 1-5100-7-5001. 2L73 4F RTA22WE 20051004001062005100400106NM 2005 10 4 05FDEA03123 120050926A5330 SKIN DOUG MD11 MD11 3023602NM BS 700-702 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 DENT ON FX EXTERIOR SKIN AREA BETWEEN STA 700 AND STA 702, ALONG L-50L. REPAIRED PER SRM 53-20-00 FIG.6 VOL.I, EO 1-5100-7-5001. 2L73 4F RTA22WE 20051004001092005100400109 2005 10 4 05FDEA03072 420050923A3441 COMPUTER DOUG DC10 DC1030F 3023504WP ROLL AXIS MALFUNCTIONED A FDEAO OTHER G MULTIPLE FAILURE CRCRUISE 1 SO25313FE 48311 PDIS - WHILE IN CRUISE FLIGHT AT FL330, LOST NR 1 INU WITH LOSS OF ADI AND HSI, WENT TO ATT REF POS, NO HELP AND THEN WENT TO OFF AND THEN TO ATT REF POS AND GOT ADI AND HSI BACK. DIVERTED TO ATL. REMOVED AND REPLACED NR 2 ROLL AXIS COMPUTER AND NR 1 INU, LOADED DATA BASE. 2L73 4F RTA22WE 20051004001102005100400110NM 2005 10 4 05FDEA03073 120050923A5315 FLOORBEAM BOEING727 727232 1384082NM BS 560 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION ON TOP FLOORBEAM BS 560 BL 0 TO RBL 50 AROUND NUT PLATES HOLES. REPAIRED FLOORBEAM IAW SRM 53-10-1. 2L73 4F A3WE 20051004001172005100400117NM 2005 10 4 05FDEA03139 120050927A5730 PANEL BOEING727 727233 138408ANM LT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25267FE 21673 LEFT WING LOWER PANEL NR 6249 REQUIRES FABRICATION FOR REPLACEMENT ON FED, EX NON-ROUTINE N00517. FABRICATED NEW PANEL IAW BAC DRAWING 65-21675-5, ALODINED, PRIMED AND PAINTED IAW B727 SRM 51-10-2. 2L73 4F RTA3WE 20051004001182005100400118EU 2005 10 4 05FDEA03141 120050927A5330 SKIN AIRBUS310 A310222 3930315EU FS 37-38 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25448FE 260 ACCOMPLISH MAINTENANCE "C" CHECK NR 004, FWD CARGO COMPARTMENT, FUSELAGE SKIN SURFACE PANEL FOUND WITH CORROSION AT INTERNAL PART OF COMPARTMENT BETWEEN FS 37 AND FS 38 BETWEEN STR 53 LT AND STR 53 RT. REPAIRED ACCOMPLISH PER FEDEX EA 6-5330-93193 (FOR DETAILS SEE JOB PROGRESS FORM). REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR. 2L72 4F RTA35EU 20051004001192005100400119NM 2005 10 4 DHL2005748531 120050817A5230 SKIN BOEING727 727225 1384077NM CARGO DOOR DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 AFT CARGO COMP C2 DOOR LWR FWD CORNER IS DENTED STA 950E. REMOVED AND REPLACED AFT CARGO C2 DOOR LWR FWD CORNER RETAINER P/N 65-59947-501 PO 531498 IAW B727 SRM 51-30-2. 2L73 4F A3WE 20051013000202005101300020NM 2005 10 13 SWAA053117 120051010A53106552271 CREASE BEAM BOEING737 7373H4 1384600NM BS 500A-500B CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED D CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 500A TO BS 500B. REPAIRED CREASE BEAM WEB PER SRM. 2L72 4F RTA16WE 20051013000232005101300023NM 2005 10 13 05FDEA03383 120051011A5340 STRINGER CLIP BOEING727 72722 1384002NM BS 380 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 MAIN CARGO COMPARTMENT STRINGER CLIP GOUGED BS 380 STR 5R. REMOVED AND REPLACED MAIN CARGO COMPARTMENT CLIP BS 380 STR 5R IAW SRM 51-30-2. 2L73 4F A3WE 20051004001202005100400120EU 2005 10 4 05FDEA03133 120050927A5410 ANGLE AIRBUS310 A310203 3930313EU NR 1 PYLON CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25445FE 297 NR 1 PYLON AFT AREA INSIDE PNL 474DR L ANGLE SUPPORT IS CRACKED. 2L72 4F RTA35EU 20051004001212005100400121EU 2005 10 4 05FDEA03134 120050927A5410 ANGLE AIRBUS310 A310203 3930313EU NR 2 PYLON CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25445FE 297 NR 2 PYLON AFT AREA INSIDE PNL 474DR L ANGLE SUPPORT IS CRACKED. 2L72 4F RTA35EU 20051004001222005100400122NM 2005 10 4 DHL2005748533 120050819A5753 SKIN BOEING727 727225 1384077NM FORE FLAP DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 LT WING I/B FOREFLAP UPPER SURFACE DELAMINATED APPROX 16" O/B OF I/B END. CUT OUT DELAMINATED UPPER SKIN APPROX 6 1/2" BY 5". CUT OUT DAMAGED CORE APPROX 6 1/2" BY 5". FABED SEPTUM APPROX 6 1/2 BY 5 AND REPAIR CORE APPROX 6 1/2 BY 5 FROM DUR-5052-4.4-3/16 --0.750 PO 9911139. FAB EXTERNAL DOUBLER APPROX 8" BY 9 1/2 FROM 2024 T3 .016 PO 9002273 CLEANED PREPPED APPLIED ADHESIVE PRIMER AND ADHESIVE MIX TO REPAIR SURFACES AND VACUUM BAGGED FOR BONDING BONDED SEPTUM AND REPAIR CORE CLEANED PREPPED APPLIED ADHESIVE PRIMER AND ADHESIVE TO EXTERNAL DOUBLER AND REPAIR SURFACES VACUUM BAGGED FOR BONDING BONDED CLEANED TREATED PRIMED AND SEALED REPAIR IAW B727 SRM 51-40-23 AND 57-50-2 FIG 3. 2L73 4F A3WE 20051004001242005100400124NM 2005 10 4 DHL2005765003 120050915A3350 LIGHT BOEING727 727264 138408MNM CABIN INOPERATIVE A DHLAK NONE O OTHER ININSP/MAINT 1 SO01765AT 23014 EMERGENCY EXIT LIGHT OVER COCKPIT DOOR INOP. REMOVE AND INSTALL NEW LIGHT ASSY, OPS CKS GOOD IAW B727 MM 33-50-101. 2L73 4F A3WE 20051003000442005100300044NM 2005 10 3 UPS05245518 120050913A5754 SLAT TRACK BOEING727 72731C 1384011NM NR 6 SLAT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01922UP 19231 ON REMOVAL OF NR 6 SLAT I/B TRACK SKIN SUPPORT BRACKET, CORROSION ON TEE TRACK FOUND BENEATH BRACKET. NR 6 SLAT TRACK REPLACED IAW MM 27-81-11. 2L73 4F A3WE 20051003000472005100300047WP 2005 10 3 UPS05845488 120050910A57403645612U FITTING DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 LT WING XW 408 STRINGER NR 59 UNDER THE BOOST PUMP FITTING CRACKED. REMOVED AND REPLACED BOOST PUMP FITTING IAW SRM 51-1-20D AND 51-1-21. 2L74 4F RT4A25 20051003000542005100300054EU 2005 10 3 AWXA200501122 120050905A5320D53475765200 SILL AIRBUS320 A320231 3930325EU BS 60-62 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28634AW 091 SAL - MAJOR REPAIR - DURING C4 CHECK DISCOVERED GALVANIC CORROSION AROUND NUT PLATE LOCATED ON BULK CARGO DOOR SEAL FROM FS 60 TO FS 62 AT STRINGER 38R. RE-WORK OF DAMAGED AREA WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-41-49 PG 103, FIG 101. MAINTENANCE CUT OUT DAMAGED AREA FROM FS 60 TO FS 62 AT STRINGER 38R IAW AIRBUS 320 SRM 51-41-49 PAGE 203. FABRICATED DOUBLER AND FILLER IAW AIRBUS 320 SRM 53-41-49. INSTALLED FABRICATED REPAIR PARTS FROM FS 60 TO FS 62 AT STRINGER 38R IAW AIRBUS 320 SRM 51-42-11 AND 53-41-49 FIG 203. 2L72 4F RTA28NM 20051003000642005100300064EU 2005 10 3 05FDEA03088 120050924A5730 SKIN AIRBUS310 A310203 3930313EU RT WING DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25445FE 297 RT WING L/E HAS DENT ABOVE NR 3 FLAP TRACK. REMOVED DAMAGE, FABED REPAIR PARTS, TREATED AND PRIMED, INSTALLED REPAIR PARTS IAW SRM 57-53-12, 51-21-10, AND 51-40-2. 2L72 4F RTA35EU 20051003000812005100300081EU 2005 10 3 AWXA200501109 120050905A5320D53470485002 PLATE AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28634AW 091 DURING C4 CHECK DISCOVERED CORROSION ON WEB LOCATED IN THE AFT CARGO COMPARTMENT FROM FS 54 TO FS 57, Y-700. MAINTENANCE REMOVED WEB FROM FS 54 TO FS 57, Y-700 IAW AIRBUS 320 SRM 51-72-11. NEW WEB INSTALLED FROM FS 54 TO FS 57, Y-700 IAW AIRBUS 320 SRM 51-72-11. 2L72 4F RTA28NM 20051003000822005100300082NM 2005 10 3 AWXA200501110 120050908A5312651758243 BULKHEAD BOEING737 7373G7 1384595NM BS 178 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - DURING C18 CHECK DISCOVERED VERTICAL BEAM WEB CRACKED, .780 INCHES IN LENGTH, AT BS178, WL 230, BL 17.1L. MAINTENANCE REMOVED DAMAGED PART OF WEB IAW BOEING 737-300 SRM 53-10-08-2R. FABRICATED REPAIR WEB IAW BOEING 737-300 SRM 53-10-08-2R. INSTALLED FABRICATED REPAIR PARTS AT BS178, WL 230, BL 17.1L IAW BOEING 737-300 SRM 53-10-08-2R. 2L72 4F RTA16WE 20051003000972005100300097WP 2005 10 3 05FDEA03069 120050923A5311 FRAME DOUG DC10 DC1010 3022110WP ZONE 100 PUNCTURED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25389FE 46623 LOWER FUSELAGE STATION 808 FRAME HAS PUNCTURE DAMAGE FROM SKIN SIDE OF J-ANGLE AT LONGERON 51L. REMOVED DAMAGE, FABRICATED NEW ANGLE SECTION AND INSTALLED REPAIR SPLICE AND FILLER IAW DC10 SRM 53-30-00 FIG 5 VOL I. 2L73 4F A22WE 20051003001022005100300102NE 2005 10 3 0820200501 220050828A7200 ENGINE BOEING747 747341 13848AMNM GE CF6 CF650E2 30018NE NR 3 LEAKING A OZYAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO29354MC 23394 455294 ABOUT (1) HR AFTER DEPARTURE FROM (ORD), AT CRUISE FLT, NR 3 ENGINE LOSS OIL QTY AND OIL PRESSURE (TO ZERO) ACCOMPANIED BY ENGINE OIL PRESSURE NR 3 LIGHT. ACCOMPLISHED AOM PROCEDURE AND ENGINE FAILURE/SHUTDOWN CKLIST. AIRCRAFT RETURNED TO (ORD) WITHOUT FURTHER INCIDENT. REMOVE AND REPLACED THE NR 3 ENGINE IAW MM 71-00-02 AND COMPANY WORKFORMS. RUN-UP AND FUNCTIONAL TEST OK, AIRCRAFT RETURNED TO SERVICE. 2L74 4F4 FRTA20WE E23EA 20051003001082005100300108NM 2005 10 3 TSAA0549043 120050923A49304419214 FUEL CONTROL BOEING737 73776N 13844CHNM APU FAILED A TSAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13742AL 30830 ETOPS FLT 944 HNL-SNA - APU AUTO SHUT DOWN WITH OVER SPEED INDICATION. CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND FCU CANNON PLUG PIN 1 TO 10 RESISTANCE MORE THAN 100K OHMS AND PIN 10 TO 12 UNDER 30 OHMS. REPLACED APU FUEL CONTROL UNIT PER AMM 49-31-11-000-801. FOUND OPS AND LEAK CHECK OKAY. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA16WE 20051003001102005100300110 2005 10 3 AWXA200501106 420050924A2565 BOTTLE AIRCRUISERS BOEING757 757225 1384959NM L1 DOOR SLIDE LOW A AWXAK NONE O OTHER ININSP/MAINT 1 WP28907AW 0276 22691 DURING 4 DAY CHECK DISCOVERED THE L1 SLIDE DOOR BOTTLE PRESSURE LOW. MAINTENANCE REMOVED AND REPLACED THE L1 DOOR SLIDE IAW AMERICA WEST AIRLINES TASK CARD R1C25602. UNIT WAS OVERHAULED AT VENDOR. UNIT PASSED ALL TESTS. WORK WAS PERFORMED IAW CMM 25-66-01 REV. 8. 2L72 4F RTA2NM 20051003001112005100300111NM 2005 10 3 AWXA200501107 120050924A2560P4010021000 BATTERY AIRBUSA319 A319132 3930340NM FLASHLIGHT DISCHARGED A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28809AW 1111 PHX - EEL - CREW REPORTED THAT AN EMERGENCY FLASHLIGHT BATTERY WAS LOW. MAINTENANCE REMOVED AND REPLACED THE FLASHLIGHT AND BATTERY. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA28NM 20051003001192005100300119NM 2005 10 3 2005UALA01009 120050921A339758781 WIRE BOEING737 737522 138449FNM ROW 15 AFT DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29942UA 26679 EEL LIGHTS FROM ROW 15 AFT ARE INOP. REPLACED FEEDER CABLE IN EEL TRACK DUE TO CONNECTORS WERE SWAMPED WITH GALLEY GOO. 2L72 4F RTA16WE 20051003001292005100300129SO 2005 10 3 CHQA200500165 120050912A323114571121403 ROD EMB 145 EMB145LR 3260212SO MLG DOOR BROKEN A CHQAO OTHER E VIBRATION/BUFFET CRCRUISE 1 GL11275SK 145345 FLIGHT 3441 - LGA-IND - IN FLIGHT, A LOUD "WHIRRING" NOISE WAS COMING FROM AROUND ROW 15 ON THE LEFT SIDE OF THE AIRCRAFT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE LEFT MAIN LANDING GEAR DOOR RODS BROKEN. MAINTENANCE REMOVED THE LEFT MAIN LANDING GEAR DOOR AND CDL'D. 2L72 4T RTT00011AT 20051003001382005100300138NM 2005 10 3 DL777050568 120050926A2611 SMOKE DETECTOR BOEING777 777232 1385232NM LAVATORY MALADJUSTMENT A DALAO OTHER N FALSE WARNING CRCRUISE 1 SO27867DA 29743 LAV 204 SMOKE DETECTOR CHIRPS, REPLACED BATTERY. 2L72 4F RTT00001SE 20051003001432005100300143WP 2005 10 3 UPS05845497 120050829A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE: C3, RT UPPER WING SKIN CRACKED AT XCW 69.500 REAR SPAR SKIN, (4 INCHES LONG CRACK). REMOVED DAMAGED SECTION OF SKIN, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1 FIG 20. 2L74 4F RT4A25 20051003001452005100300145WP 2005 10 3 UPS05845499 120050831A5313 LONGERON DOUG DC8 DC873F 302199FWP BS 1749 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE:C3, L15R CRACKED AT STA 1749. REMOVED CRACKED SECTION OF LONGERON, FABRICATED, AND INSTALLED REPLACEMENT SECTION OF LONGERON IAW DC-8 SRM 53-2-2 FIG 10. 2L74 4F RT4A25 20051003001472005100300147WP 2005 10 3 UPS05845502 120050831A53404772397U1 FITTING DOUG DC8 DC873F 302199FWP BS 1760 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE: C3, LONG END FITTING CRACKED AT STA 1760 L17R. REMOVED AND REPLACED LONGERON END FITTING IAW DC-8 SRM 51-1-21. 2L74 4F RT4A25 20051003001582005100300158NM 2005 10 3 SWAA052950 120050927A53156545812 FLOORBEAM BOEING737 7373H4 1384600NM BS 328 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED D CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 328, BETWEEN RBL 45 TO RBL 52, WL 208. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20051003001592005100300159NM 2005 10 3 SWAA052951 120050927A53156545808 FLOORBEAM BOEING737 7373H4 1384600NM BS 294 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED D CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 294, RBL 25, WL 208. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20051003001602005100300160NM 2005 10 3 SWAA052952 120050927A53106547980 CREASE BEAM BOEING737 7373H4 1384600NM BS 988 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29618WN 28034 DURING SCHEDULED D CHECK, FOUND FUSELAGE CREASE BEAM WEB CORRODED AT BS 988, RBL 48. REPAIRED CREASE BEAM WEB PER SRM. 2L72 4F RTA16WE 20051003001652005100300165NM 2005 10 3 SWAA052957 120050926A3350612825 BATTERY PACK BOEING737 7373T5 1384608NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 DURING SCHEDULED C2 CHECK, FOUND RT CABIN AISLE BULLNOSE EMERGENCY LIGHT INOP AT ROW 19 AND ROW 20. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20051003001812005100300181WP 2005 10 3 UPS05845517 120050911A534037540231 FITTING DOUG DC8 DC873F 302199FWP BS 315 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE:C3 DEEP CORROSION PIT OR DRILL START IN BATHTUB FITTING TA STA 315 BETWEEN L33R AND L34R. REMOVED AND REPLACED BATHTUB FITTING IAW SRM 51-1-20D, 51-3-0 AND 51- 1-21. 2L74 4F RT4A25 20051003001882005100300188NM 2005 10 3 SWAA052958 120050926A57536546431 SKIN BOEING737 7373T5 1384608NM LT WING FOREFLAPDELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 DURING SCHEDULED C2 CHECK, FOUND LT WING OTBD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM. 2L72 4F RTA16WE 20051003001892005100300189NM 2005 10 3 SWAA052959 120050926A53306545768 SKIN BOEING737 7373T5 1384608NM BS 365 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 365, STR 19R. REPAIRED SKIN PER SWA EA AND SRM. 2L72 4F RTA16WE 20051003001912005100300191SO 2005 10 3 Z4TA20050002 220050919A8530537296 HOUSING BEECH 58 58 1152740CE CONT O550 IO550B SO RT ENGINE CRACKED E Z4TAK NONE K FLUID LOSS ININSP/MAINT 1 SO0595KM 1401 1401 TH1315 810485R PILOT REPORTED ABNORMAL OIL LOSS FOR RIGHT ENGINE. ALSO, OIL TRAIL ON LOWER RT WING. UPON INSPECTION, FOUND NR 6 CYLINDER FORWARD PUSH ROD HOUSING CRACKED, ALLOWING OIL TO DRAIN INTO LOWER COWL. REPLACED PART. 1L72 3O3 O 3A16 E3SO 20051004000532005100400053EA 2005 10 4 COMA0570106 120050928A531267053110521 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA FS 280 CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01367CA7872 10069 THE LT AND RT LOWER BULKHEAD WEBS AT FS 280 ARE CORRODED FROM LBL 36 TO RBL 36. REMOVED THE CORRODED WEBS AND INSTALLED NEW WEBS IAW REO 670-53-11-052 REV A. 2L72 4F RTA21EA 20051004000622005100400062NM 2005 10 4 PIDA20050153 120050929A5320 PANEL BOEING737 737228 13844AGNM BS 1016 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 CLOSE-OUT PANEL AT BS 1016 HAS CORROSION ON UPPER SURFACE AT RBL4. REPAIRED CLOSE-OUT PANEL PER SRM 51-40-1. 2L72 4F RTA16WE 20051004000632005100400063NM 2005 10 4 PIDA20050151 120050930A5320 INTERCOSTAL BOEING737 737228 13844AGNM BS 500B-520 CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 TOP FLANGE OF INTERCOSTAL BETWEEN BS 500B AND BS 520 AT BL 0 IS CRACKED. REPLACED INTERCOSTAL PER DWG 69-41680 AND SRM 51-10-1 AND SRM 51-30-0. 2L72 4F RTA16WE 20051004000672005100400067NM 2005 10 4 PIDA20050150 120050928A5311 FRAME BOEING737 737228 13844AGNM BS 616 CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 CRACK AT I/B CHORD LOWER FASTENER HOLE IN BS 616 FRAME LEFT. REPAIRED FRAME PER SB 737-53-1182. 2L72 4F RTA16WE 20051004000732005100400073 2005 10 4 SWIA200515586 420050922A2220607300001 TRANSDUCER CNDAIRCL600 CL6002B19 1900309EA NR 2 MACH MALFUNCTIONED A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07465SW 7845 STALL FAIL CAUTION MSG AND YAW NR 2 STATUS MSG. REPLACED NR 2 MACH TRANSDUCER IAW MM 27-35-25. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051004000742005100400074EA 2005 10 4 SWIA200515588 120050923A274183963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07720SW9500 9146 7297 STAB TRIM CH 1 INOP. REPLACED HSTA AND MCU IAW 27-42-01 AND 27-42-05. OPERATIONAL CHECK GOOD, PN 7062-3 SN/OFF 795. 2L72 4F RTA21EA 20051004000782005100400078EA 2005 10 4 SWIA200515592 120050921A274170744 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA STAB TRIM MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07705SK 10145 STAB TRIM CH 2 WILL NOT ENGAGE. REPLACED MCU IAW MM 27-42-00. OPERATIONAL CHECK GOOD, PN 7074-5. 2L72 4F RTA21EA 20051004000922005100400092 2005 10 4 QXEA200501263 420050927A31606229810204 DISPLAY CNDAIRCL600 CL6002C10 1390015EA COCKPIT OVERHEATED A QXEAO OTHER MB OVER TEMP SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM09600QX6133 5392 10005 DEN - ARRIVING AT THE AIRCRAFT IN THE MORNING FOR FLIGHT 2457, NOTICED A STRONG ELECTRICAL BURNING SMELL IN THE COCKPIT, AND THE DISPLAY TEMP WARNING WAS DISPLAYED. AIRCRAFT HAD ELECTRICAL POWER APPLIED ALL NIGHT, AND THE DISPLAY FAN HAD BEEN TURNED TO STANDBY. MAINTENANCE TURNED THE DISPLAYS TO DIM POSITION AND COOLED THE DISPLAYS WITH FANS. THE NR 1 MULTI-FUNCTION DISPLAY REMAINED BLANK. REMOVED AND REPLACED NR 1 MULTI-FUNCTION DISPLAY. OPERATIONAL CHECKS GOOD. ODOR CLEARED FROM AIRCRAFT BY OPENING EMERGENCY EXITS AND WITH CONDITIONED AND RECIRC AIR. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20051004000942005100400094NE 2005 10 4 IXXA0500106O 220050912A7200 ENGINE DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE NR 4 FLAMED OUT A IXXAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION DEDESCENT 1 SW11823BX881392111 46064 693379 DURING DESCENT FROM BIKF TO KNGU, NR 4 ENGINE EXPERIENCED VIBRATION AND A FLAME OUT. CREW LANDED AIRCRAFT IN KNGU WITHOUT INCIDENT. MAINTENANCE COMPLIED WITH FAULT 53, FAN VIBRATION AND NO DEFECTS WERE NOTED. FAULT 51 COMPLIED WITH AND MAINTENANCE SUMPED WATER CONTAMINATION FROM THE NR 4 MAIN. A POWER ASSURANCE WAS PERFORMED PER ATI ERH 91.1 AND AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F4 FRT4A25 E2GL 20051004001012005100400101NM 2005 10 4 SWAA052978 120050927A3350MS155721 BULB BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29752SW 29804 DURING SCHEDULED HC2 CHECK, FOUND EMERGENCY BULLNOSE LIGHT INOP AT ROW 6 ABC. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20051004001132005100400113NM 2005 10 4 C8GA20050019 120050908A5754651724021 BRACKET BOEING727 727223 1384074NM LT WING SLAT CRACKED A C8GAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO29713AA56172 22469 FLT 718 FROM STL TO ELP, DURING CLIMB-OUT, THE NR 2 SLAT WILL NOT RETRACT. AIRCRAFT RETURNED TO STL AND LANDED WITHOUT INCIDENT. INSPECTED SLAT ACTUATOR AND LUBED SLAT TRACKS. NO OTHER DEFECTS NOTED. OPERATIONAL AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. IN ELP, PERFORMED FOLLOW-UP INSPECTION. FOUND NR 2 SLAT ACTUATOR ATTACH BRACKET CRACKED. REPLACED BRACKET. AIRCRAFT RETURNED TO SERVICE. 2L73 4F A3WE 20051004001252005100400125NM 2005 10 4 AALA20050628 120050929A3350D71702001 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21755AN 30263 LHR - EMERGENCY LIGHTS IN FIRST CLASS GALLEY INOPERATIVE. REPLACED BATTERY PACK AT DOOR LEFT ONE FOR EMERGENCY LIGHTS IN FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20051004001272005100400127WP 2005 10 4 AALA20050631 120050928A3243 VALVE DOUG DC9 DC982 3022082WP BRAKE INOPERATIVE A AALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW21955U 49427 ORD - INFLIGHT T730/28SEPT, DURING TAKEOFF ROLL WHEEL NOT TURNING LIGHT ILLUMINATED. ABORTED TAKEOFF. SPEED LESS THAN 10 KNOTS. FOUND NO ELECTRICAL OUTPUT FROM NUMBER 3 TRANSDUCER. REPLACED NR 3 TRANSDUCER AND REPLACED ANTI-SKID CONTROL BOX AS PRECAUTION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051004001282005100400128NM 2005 10 4 AALA20050627 120050828A3350 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21658AA 24616 DFW - EMERGENCY LIGHTS IN AFT LEFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN AFT LEFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20051004001312005100400131NM 2005 10 4 05FDEA03143 120050927A5315 FLOORBEAM BOEING727 727232 1384082NM BS 950 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION AT FLOORBEAM BS 950 RBL 48-54 WL 208 AT NUT PLATE HOLES. REPAIRED FLOORBEAM PER FED EX EA 7-5310-91395. 2L73 4F A3WE 20051004001322005100400132NM 2005 10 4 05FDEA03146 120050927A5315 FLOORBEAM BOEING727 727225 1384077NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25465FE 21289 CORRODED FLOORBEAM FS 620 FROM LBL 24 - LBL 45 THREE HEAVY AREAS. REMOVED, FABRICATED, ALODINED, PRIMED, HEAT TREATED, CAD PLATED AND INSTALLED FLOORBEAM REPAIR AT STA 620 FROM LBL24-45 ALL IAW FX DWG SR27-53-034E REPAIR NR 4 B727SRM 51-10-2,BAC5619H AND AMSPP-8-416. 2L73 4F A3WE 20051004001332005100400133WP 2005 10 4 05FDEA03150 120050928A5347 SEAT TRACK DOUG DC10 DC1010 3022110WP ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25389FE 46623 MAIN CABIN, SEAT TRACK AT RBL 27.5 IS CRACKED AT FS 1272. MANUFACTURED AND INSTALLED NEW SEAT TRACK SECTION AND SPLICE IAW DOUGLAS DWG NEA6022 SH2 REV AM AND DC10 SRM 53-70-00 VOL I. SEE FEDEX NONROUTINE N00323 OF WORK ORDER 00029899. 2L73 4F A22WE 20051004001352005100400135NM 2005 10 4 USAA051150 120050926A5414 SKIN BOEING737 7374B7 1384702NM NR 1 PYLON CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 NR 1 ENG PYLON, ACCESS PNL OPENING NR 5727L. REPAIR DOUBLER INSTALLED IAW TYP REP 54-30-07, DEFECT SIZE: .400". 2L72 4F RTA16WE 20051004001372005100400137NM 2005 10 4 USAA051148 120050926A575365C263101A SKIN BOEING737 7374B7 1384702NM TE FLAP CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 FOUND SKIN CRACKED IL I/B MID FLAP 39" FROM O/B END. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW SRM 57-53-01, DEFECT SIZE: .25". 2L72 4F RTA16WE 20051004001402005100400140NE 2005 10 4 AWXA200501119 220050926A732079830018052 EEC AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE NR 2 ENGINE MALFUNCTIONED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28621AW2635724896 053 V0075 DURING CLIMB CREW REPORTED "COMPRESSOR STALL ON THE NR 2 ENG ON CLIMB-OUT OF KCLE-RETURN TO KCLE ENG RAN FINE DURING DESCENT." ACFT LANDED IN CLE WITHOUT FURTHER INCIDENT. MX PERFORMED BOROSCOPE OF NR 2 ENG & VISIUAL INSP WITH NO DEFECTS BEING NOTED. R&R NR 2 ENG EEC IAW AMWEST TASKCARD R5M73302. HIGH POWER RUNS WERE ACCOMPLISHED & OPS TESTS WERE GOOD. VENDOR TEAR DOWN REPORT CONFIRMS REASON FOR REMOVAL. EEC WAS FOUND TO HAVE A BENT PIN, NO. 26, ON THE J1007 CONNECTOR. CONNECTOR WAS REPLACED AND UNIT PASSED OPERATIONAL TESTS. UNIT REPAIRED AND TESTED IAW CMM 73-22-34 REV. 2. 2L72 4F4 FRTA28NM E311NE 20051004001422005100400142NM 2005 10 4 AWXA200501125 120050903A5315654581292 FLOORBEAM BOEING737 7373G7 1384595NM BS 328 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - DURING C18 CHECK DISCOVERED .9 INCH LONG CRACK ON FLOORBEAM AT BS 328, RBL 19, AND WL 208. MAINTENANCE CUT OUT DAMAGED AREA OF FLOORBEAM IAW BOEING 737-300 SRM 53-10-51-2R. FABRICATED REPAIR FILLER AND REPAIR ANGLES IAW BOEING 737-300 SRM 53-10-51-2R 6 FIG 201. INSTALLED FABRICATED REPAIR PARTS AT BS 328, RBL19, AND WL208 IAW BOEING 737-300 SRM 53-10-51-2R6 FIG 201. 2L72 4F RTA16WE 20051004001442005100400144NM 2005 10 4 AWXA200501127 120050903A575465C267943 SKIN BOEING737 7373G7 1384595NM ZONE 500 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - DURING C18 CHECK, DISCOVERED SEVERAL CRACKS ON THE BOTTOM OF THE NR 2 SLAT SKIN INBOARD OF THE TELESCOPING ANTI-ICE TUBE FROM SS 210L TO SS 230L. MAINTENANCE CUT OUT DAMAGED SKIN ON NR 2 SLAT IAW BOEING 737-300 SRM 57-43-02-2R. FABRICATED REPAIR FILLER AND REPAIR SPLICE PLATE IAW BOEING 737-300 SRM 57-43-01-2 FIG 201. INSTALLED FABRICATED REPAIR PARTS AT NR 2 SLAT FROM SS 210L TO SS 230L IAW BOEING 737-300 SRM 57-43-01-2R6 FIG 201. 2L72 4F RTA16WE 20051004001462005100400146NM 2005 10 4 AWXA200501129 120050903A53306552988519 SKIN BOEING737 7373G7 1384595NM BS 977 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - DURING C18 CHECK DISCOVERED .5-INCH CRACK ON FUSELAGE SKIN AT BS 977, STRINGER 21L. MAINTENANCE REMOVED DAMAGED SKIN IAW BOEING 737-300 SRM 53-00-01-2R-31 FIG 201. FABRICATED DOUBLER, TRIPLER, FILLER AND STRUCTURAL FILLER IAW BOEING 737-300 SRM 53-00-01-2R-31 FIG 201. INSTALLED FABRICATED REPAIR PARTS AT BS 977 AND STR 21L IAW BOEING 737-300 SRM 53-00-01-21-2R-31 FIG 201. 2L72 4F RTA16WE 20051004001482005100400148NM 2005 10 4 05FDEA03144 120050927A5315 FLOORBEAM BOEING727 727232 1384082NM BS 950 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION AT BS 950 LBL 48-53 WL 207 AT UNDERSIDE OF FLOORBEAM . ALL WORK ACCOMPLISHED IAW FED EX EA 7-5310-91391. 2L73 4F A3WE 20051004001502005100400150NM 2005 10 4 BMAC050012 120050828A21317638101 CONTROLLER BOEING727 727222 1384073NM CABIN PRESSURE MALFUNCTIONED A B16AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO35342PA 21893 UNABLE TO MAINTAIN AND CONTROL CABIN ALTITUDE IN AUTO, STBY OR MANUAL. OUTFLOW VALVE SHOWS FULLY CLOSED, HOWEVER, CABIN ALTITUDE CONTINUED TO CLIMB. REMOVED AND REPLACED PRESSURE CONTROLLER AND SAFETY VALVE. 2L73 4F A3WE 20051004001532005100400153NM 2005 10 4 USAA051145 120050926A575365C2632011A SKIN BOEING737 7374B7 1384702NM TE FLAP WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19443US 24842 WORN AREA OB FLAP LEADING EDGE AT IB END. REMOVED DAMAGE AND INSTALLED FABRICATED REPAIR PARTS IAW SRM 57-53-01 REPAIR 8 PG 204, DEFECT SIZE: 1". 2L72 4F RTA16WE 20051004001542005100400154NM 2005 10 4 USAA051144 120050926A5313 STRINGER BOEING737 7374B7 1384702NM BS 303.9 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 STRINGER CRACKED STA 303.9, S10L. REMOVED DAMAGE, FABRICATED REPAIR DOUBLER AND INSTALLED PER EA 96914, DEFECT SIZE: .25". 2L72 4F RTA16WE 20051004001562005100400156NM 2005 10 4 USAA051152 120050928A5340 ANGLE BOEING737 7374B7 1384702NM BS 360 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19443US 24842 ANGLE CRACKED STA 360 AND STR 9L. FABRICATED NEW ATTACH ANGLE AND INSTALLED IAW DWG 69-48985, SRM 1-10-02, DEFECT SIZE: .50". 2L72 4F RTA16WE 20051004001592005100400159SO 2005 10 4 SWIA200515596 120050926A3350 SIGN EMB 120 EMB120ER 3260203SO ROW 9C BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07223SW 120291 LOWER EXIT SIGN AT ROW 9C BROKEN. REPLACED LOWER EXIT SIGN. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20051004001602005100400160EA 2005 10 4 SWIA200515597 120050919A2741 SWITCH CNDAIRCL600 CL6002B19 1900309EA TRIM SYSTEM STICKING A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07983SW 7961 FO'S TRIM SWITCH STICKS. REPLACED FO'S TRIM SWITCH IAW 27-41-05-400-801. OPERATIONAL CHECK GOOD IAW 27-40-00-710-801. 2L72 4F RTA21EA 20051004001612005100400161EA 2005 10 4 SWIA200515598 120050924A274183963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07915SW5252 5252 7615 STAB TRIM CH 2 INOP STATUS MSG. REPLACED HSTA, MCU IAW AMM 27-42-01 AND 27-42-05. OPERATIONAL CHECK GOOD IAW AMM 27-40-00, 27-41-00. 2L72 4F RTA21EA 20051004001622005100400162EA 2005 10 4 SWIA200515599 120050912A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07408SW 7055 MAIN FUSELAGE, FS 280.00, LBL 9.0, UPPER FLANGE CRACKED ON FLOORBEAM, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED MAIN FUSELAGE FS 280.00, LBL 9.0 UPPER ANGLE ON TRANSVERSE BEAM IAW CRJ REO 601R-53-11-138 REV "NC". 2L72 4F RTA21EA 20051004001632005100400163EA 2005 10 4 SWIA200515600 120050912A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07408SW 7055 MAIN FUSELAGE, FS 280 RBL 9.0, O/B AND I/B CLIP CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIPS IAW CRJ SRM 51-40-11, 51-42-13, 51-23-00. 2L72 4F RTA21EA 20051004001642005100400164EA 2005 10 4 SWIA200515601 120050912A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07408SW 7055 MAIN FUSELAGE, FS 280 LBL 9.0, O/B AND I/B CLIP CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLES IAW CRJ SRM 51-40-11, 51-42-6, 51-42-13, 51-23-00 (REF REO 601R-53-11-171 REV B DUE TO REPAIR IN SAME AREA). 2L72 4F RTA21EA 20051004001652005100400165EA 2005 10 4 SWIA200515602 120050912A5310 DOOR FRAME CNDAIRCL600 CL6002B19 1900309EA BS 320 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07408SW 7055 PAX DOOR, DOOR FRAME IS CRACKED ON UPPER END, FS 320.10, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED FRAME IAW CRJ REO 601R-52-11-402 REV E. 2L72 4F RTA21EA 20051004001662005100400166EA 2005 10 4 SWIA200515603 120050912A5210 FRAME CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07408SW 7055 PAX DOOR, SUB FRAME IS CRACKED AT UPPER END, FS 335.70, ITEM FOUND AT C-CHECK INSPECTION. REPLACED SUB-FRAME. 2L72 4F RTA21EA 20051004001672005100400167EA 2005 10 4 SWIA200515604 120050912A5210 FRAME CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07408SW 7055 PAX DOOR, DOOR FRAME IS CRACKED ON UPPER END, FS 338.90, ITEM FOUND AT C-CHECK INSPECTION. FRAME REPAIRED IAW REO 601R-52-11-402 REPAIR 2. 2L72 4F RTA21EA 20051004001682005100400168EA 2005 10 4 SWIA200515605 120050912A5210 FITTING CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07408SW 7055 PAX DOOR, LOWER CORNER FITTINGS ARE CORRODED, FS 312.00 AND FS 346.00, ITEM FOUND AT C-CHECK INSPECTION. REPLACED FITTINGS (FWD & AFT). 2L72 4F RTA21EA 20051004001692005100400169SO 2005 10 4 N93A1316 120050915A2910NAS16124A O-RING GULSTMG1159 GIV 3980115SO HYD SYSTEM LEAKING E N93AA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO13416QS7662 1316 LOSS OF HYDRAULIC FLUID ON THE FLIGHT SIDE HYDRAULIC SYSTEM. FOUND PRESSURE TRANSMITTER O-RING AT FAULT. 2L72 4F RTA12EA 20051004001702005100400170WP 2005 10 4 IXXA0500107O 120050915A3210 BOLT DOUG DC8 DC871F 302199DWP MLG OUT OF ADJUST A IXXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW11822BX90078187 45813284 DURING TAKEOFF FROM KTOL, GEAR UPLATCH CHECK UNSATISFACTORY DOORS LIGHT AND LANDING GEAR UNSAFE LIGHT CAME ON IN UPLATCH POSITION. CYCLED GEAR DOWN AND UP, SAME RESULTS CREW RETURNED AIRCRAFT TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND STRUT TO UNIVERSAL BOLT SAFETY BOLT CONTACTING SIDE BRACE LINK, REPOSITIONED BOLT, NO DEFECTS NOTED. FOUND BOTH ACTUATING CYLINDERS NOT BOTTOMED OUT IN CYLINDER, ADJUSTED. PERFORMED EXTENSION RETRACTION SYSTEM AND A SYSTEMS CHECK WAS GOOD PER ALL APPLICABLE MANUALS AND AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20051004001712005100400171WP 2005 10 4 0501459928 120050919A27504925842503 LEVER DOUG DC9 DC931 3022065WP TE FLAPS WORN A NWAAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL018921E 45836 ON FINAL APPROACH, THE TRAILING EDGE FLAPS BEGAN AN UNCOMMANDED RETRACTION. THE AURAL WARNING SOUNDED AT THAT TIME, THE FLIGHT CREW RESET THE FLAPS TO 40 DEGREES, AND LANDED WITHOUT INCIDENT. DURING THE LANDING ROLLOUT THE FLAPS AGAIN RETRACTED TO 25 DEGREES UNCOMMANDED. MAINTENANCE FOUND THE FLAP HANDLE LATCH AND SPRING WORN ALLOWING THE FLAP HANDLE TO "FLOAT" AND NOT LOCK INTO THE 40 DEGREE POSITION. THE HANDLE LATCH AND SPRING WERE REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F A6WE 20051004001732005100400173EA 2005 10 4 SWIA200515607 120050912A5210 CHANNEL CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07408SW 7055 PAX DOOR, LWR CENTER CHANNEL HAS CORROSION ON INSIDE UNDER WATER DAM, ITEM FOUND AT C-CHECK INSPECTION. REPLACED CHANNEL. 2L72 4F RTA21EA 20051004001752005100400175EA 2005 10 4 SWIA200515609 120050912A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA BS 484 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07408SW 7055 FUSELAGE, PULLEY INTERCOSTAL IS CRACKED ON O/B FLANGE, FS 484.00 - LBL 36.0, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED PULLEY INTERCOSTAL. REF. CRJ REO 601R-53-41-059 REV A, AMM 20-24-00, SRM 51-41-02. 2L72 4F RTA21EA 20051004001772005100400177EA 2005 10 4 SWIA200515611 120050912A5320 POST CNDAIRCL600 CL6002B19 1900309EA BS 559 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07408SW 7055 FUSELAGE, VERT POST IS CRACKED AT LOWER RIVET LOCATION, FS 559.00 - RBL 9.0, I/B AND O/B SIDES, ITEM FOUND AT C-CHECK INSPECTION. VERTICAL POST AT FS 559.00; RBL 9.0 REPLACED IAW CRJ REO 601R-53-41-260 REV "A". 2L72 4F RTA21EA 20051004001792005100400179EA 2005 10 4 SWIA200515613 120050912A5320 POST CNDAIRCL600 CL6002B19 1900309EA BS 409 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07408SW 7055 FUSELAGE, VERTICAL POST IS CRACKED AT LOWER RIVET LOCATION, FS409.0+128 - RBL27.0, I/B SIDE, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-41-056 REV C . 2L72 4F RTA21EA 20051004001812005100400181EA 2005 10 4 SWIA200515615 120050912A5220 DOOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY EXIT CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07408SW 7055 LT EMERG EXIT, LOWER CORNERS HAVE CORROSION ON INNER STRUCTURE ITEM FOUND AT C-CHECK INSPECTION. REMOVED CORROSION IAW CRJ SRM 52-00-00, FIG 102, 51-21-06, 51-45-00. .002 MAT LOSS WITHIN LIMITS IAW CRJ SRM 52-00-00, FIG. 102. 2L72 4F RTA21EA 20051004001832005100400183EA 2005 10 4 SWIA200515617 120050912A5340 ATTACH FITTING CNDAIRCL600 CL6002B19 1900309EA BS 625 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07408SW 7055 AFT EQUIP COMP, 6 INTERCOSTAL TO STRINGER ATTACH CLIP ARE CRACKED FS 625.00, STR 11 RT, ITEM FOUND AT C-CHECK INSPECTION. REMOVED & REPLACED CLIPS IAW CRJ SRM 51-42-06, 51-40-11, 51-42-21, 51-23-00, 51-25-16. 2L72 4F RTA21EA 20051004001852005100400185NM 2005 10 4 DHL2005748507 120050815A5753 SKIN BOEING727 727225 1384077NM TE FLAP DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 L/WING O/B AFT FLAP DENTED ON L/E I/B END. CUT OUT DAMAGED AREA DIM 1" BY 2 1/4" FABRICATED NEW PART PO NR 9001938 2024T3 .050 IAW SRM 57-50-4 FIG 9 5" BY 3 1/2" TREATED AND PRIMED NEW PART IAW B727 SRM 51-10-2. INSTALLED NEW PART IAW SRM 57-50-4. 2L73 4F A3WE 20051004001872005100400187WP 2005 10 4 ABXA050239 120050912A532099581773 INTERCOSTAL DOUG DC9 DC933F 302207AWP BS 718-699 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23930AX 47363 INTERCOSTAL AT LONGERON 11 LEFT, FS 718 - 699 CRACKED ON ONE END. REPAIRED AREA IAW DC-9 SRM 53-01. 2L72 4F A6WE 20051004001922005100400192EA 2005 10 4 SWIA200515620 120050912A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA BS 605 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07408SW 7055 CARGO COMP, FRAME FLANGE IS CRACKED, FS 605.00 - STRL 9L, LOWER SIDE ITEM FOUND AT C-CHECK INSPECTION. REPAIRED DAMAGE FRAME FLANGE FS 605.00; STR 9L IAW CRJ REO 601R-53-61-1529 2L72 4F RTA21EA 20051004001942005100400194NM 2005 10 4 C1HA200592004 120050919A5343 TRUNNION BOEING727 727212 138407GNM MLG CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15292AS 21458 NOSE LANDING GEAR TRUNNION CAPS CORRODED, LEFT AND RIGHT. REMOVED CORROSION ON LT TRUNNION FITTING TO A FINAL BORE DIAMETER OF 2.602" AND RT 2.727" AND WITHIN LIMITS IN ACCORDANCE WITH 727 SRM 53-40-01, FIGURE 2. REWORKED AREAS TREATED AND PRIMED IN ACCORDANCE WITH 727 SRM 51-10-2. NEW BEARINGS MACHINED IN ACCORDANCE WITH SRM 53-40-1, FIGURE 2. RII ACCOMPLISHED. 2L73 4F A3WE 20051004001962005100400196NE 2005 10 4 XN0A1265 220050916A7320 SOLENOID AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE NR 2 ENGINE MALFUNCTIONED A XN0AC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL23372PC 196 517463 NR 2 ENGINE WOULD NOT ACCELERATE ON TAKEOFF. TROUBLESHOOT GROUND IDLE SOLENOID AND TRANFERRED TO DMI NR 5726 IAW MEL 73-30-02 CAT-C. CLEARED AND RESEATED NR 2 ENG FTL IDLE SOLENOID C/P, OPS CHECK NORMAL IAW A300 MM 73-21-00. DMI NR 5726 CLEARED (STATUS:ORIG/CLOSED). 2L72 4F4 FRTA35EU E23EA 20051004001972005100400197WP 2005 10 4 UPS05845528 120050904A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 C3 - RT WING LE UPPER RIB IS CRACKED AT XFS 347.750. STOP DRILLED CRACK, FABRICATED AND INSTALLED 2 EA. REPAIR ANGLES IAW SRM 57-2-0 FIG 2 AND 57-3-3 FIG 5. 2L74 4F RT4A25 20051004001982005100400198WP 2005 10 4 UPS05845529 120050904A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 C3 - RT WING LE UPPER RIB CRACKED AT XS 484.895. STOP DRILLED CRACK, FABRICATED AND INSTALLED 2 EA. REPAIR ANGLES IAW SRM 57-2-0 FIG 2, 53-3-3 FIG 5. 2L74 4F RT4A25 20051004001992005100400199WP 2005 10 4 UPS05845530 120050912A52303614122501 FITTING DOUG DC8 DC873F 302199FWP CARGO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 C3 - D-PIT DOOR INTERIOR FWD UPPER ANGLE CRACKED JUST BELOW UPPER STOP. REMOVED AND REPLACED DOOR UPPER ANGLE SUPPORT FITTING IAW SRM 51-1-2 AND 51-3-0. 2L74 4F RT4A25 20051004002002005100400200WP 2005 10 4 UPS05845531 120050912A5313S1616757 LONGERON DOUG DC8 DC873F 302199FWP BS 1720-1776 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 C3 - CRACKED LONGERON AT STA 1736 L15R. CUT OUT DAMAGED LONGERON, FABRICATED AND INSTALLED REPLACEMENT LONGERON IAW SRM 51-1-21, 51-1-20D, 53-2-2 FIG 10 AND DWG 5894025. 2L74 4F RT4A25 20051004002012005100400201NM 2005 10 4 SWAA052989 120050928A575465C266022 SKIN BOEING737 7373Q8 1384670NM RT WING SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 DURING SCHEDULED C2 CHECK, FOUND RT WING NR 5 L/E SLAT T/E WEDGE OTBD UPPER CORNER DELAMINATED. REMOVED AND REPLACED SLAT PER MM. 2L72 4F RTA16WE 20051004002022005100400202NM 2005 10 4 SWAA052990 120050928A53306545776 SKIN BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051004002032005100400203NM 2005 10 4 SWAA052991 120050928A53306545768 SKIN BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR CUTOUT, LOWER AFT CORNER. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051004002042005100400204NM 2005 10 4 SWAA052992 120050928A575265C26485 SKIN BOEING737 737317 138447PNM LT AILERON TAB DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED 1/4D CHECK, FOUND LT WING AILERON TAB T/E DELAMINATED. REMOVED AND REPLACED TAB PER MM. 2L72 4F RTA16WE 20051004002052005100400205NM 2005 10 4 SWAA052993 120050929A335065C53829 CHARGER BOEING737 7373A4 1384585NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED SPECIAL VISIT, FOUND SEVERAL RT AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM. 2L72 4F RTA16WE 20051004002062005100400206NM 2005 10 4 SWAA052980 120050929A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM BS 787 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, LBL 16. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051004002082005100400208NM 2005 10 4 SWAA052982 120050929A3350101114 COVER BOEING737 7373H4 1384600NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29396SW 27690 R1 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED COVER PER MM. 2L72 4F RTA16WE 20051004002092005100400209NM 2005 10 4 SWAA052983 120050929A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM BS 767 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29618WN 28034 DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 767, BETWEEN RBL 4 TO RBL 9. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051004002112005100400211NM 2005 10 4 SWAA052985 120050929A53116520722 FRAME BOEING737 7373H4 1384600NM BS 440 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29618WN 28034 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L TO STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051004002132005100400213NM 2005 10 4 SWAA052987 120050928A53306545775 SKIN BOEING737 737317 138447PNM BS 806 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 806, STR 20L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051004002152005100400215EU 2005 10 4 05FDEA03044 120050922A3230D221270005 DAMPER AIRBUS310 A310222 3930315EU MLG MALFUNCTIONED A FDEAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 SO25428FE10056822 248 LDG GEAR HANDLE WON'T GO PAST NEUTRAL ON RETRACT IN SYS2. WORKED SYS1. ACN RELEASED MEL: 32-61-04 CAT: C XP: 30SEP05 "LDG GEAR POS DET SYS2 INOP." PERFORMED BITE TEST ON PROX . ALL TESTS OK. MEMORY RECALL ,FC 04 ON THE PROX UNIT. SHAKE TEST OF ALL 4 LDG GEAR HARNESSES OM PROX DET UNIT. BOGIE SENSORS, C/P 929VC,1930VC, 25VC,1926VC TO BOGIE SENSORS NO SHORTS/OPENS NOTED. INSP BOGIE SENSOR/TARGET NO DEFECTS. CLEANED AND INSP BOTH C/P AT MID-POINT OF EA GEAR, ALL PINS CLEAN/SECURE, NO EROSION/DAMAGE. R/R RMLG BOGIE PITCH DAMPER FOR LOW FLUID/N2 SERVICE. REMOVED AND REPLACED 8GA/12GA PROX SENSORS, RMLG/BOGIE DET SYS. GEAR RETRACT CK GOOD SYS 1/2. 2L72 4F RTA35EU 20051005000012005100500001SO 2005 10 5 SWIA200515621 120050929A273152991 ACTUATOR EMB 120 EMB120ER 3260203SO ELEVATOR TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07291SW1848 1848 120318 ELEVATOR TRIM FEELS LIKE IT IS BINDING A BIT WHEN TRIMMING NOSE UP. REPLACED LT ELEVATOR TRIM TAB ACTUATOR IAW EMB MM 27-32-02. 2L72 4T RTA31SO 20051005000022005100500002EA 2005 10 5 SWIA200515622 120050929A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLT SPOILERS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07939SW5364 5364 7742 SPOILERON FAULT ON TAXI OUT. REPLACED LT OUTBOARD SPOILERON PCU PER CRJ 200 MM 27-62-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051005000042005100500004EA 2005 10 5 SWIA200515624 120050928A274170609 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07932SW1362 1362 7714 MACH TRIM DISENGAGED WHILE PARKED AT THE GATE. REPLACED HSTCU. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051005000062005100500006EA 2005 10 5 SWIA200515626 120050926A3397 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT LOOSE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07906SW 7510 GALLEY/BOARDING AREA "EXIT" LIGHT DOES NOT ILLUMINATE, BULKHEAD FLOOR EXIT LIGHT. RESEATED AND RESECURED LIGHT PLUG. OPERATIONAL CHECK NORMAL IAW MM 20-00-00. 2L72 4F RTA21EA 20051005000072005100500007EA 2005 10 5 SWIA200515627 120050926A2750855D10011 POSITION SENSOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07960SW1710 1710 7853 FLAPS FAIL MESSAGE DISPLAYED WHILE ON RAMP. REPLACED RT BPSU IAW MM 27-50-00. REPLACED SKEW DETECTION UNIT PER 27-51-15-400-801. OPERATIONAL CHECK GOOD IAW MM 27-51-10-830-801, P/N: 601R59014-1 S/N OFF: A325. 2L72 4F RTA21EA 20051005000082005100500008NM 2005 10 5 05FDEA03166 120050930A5730 PANEL BOEING727 727233 138408ANM ZONE 600 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25267FE 21673 RIGHT WING LEADING EDGE FIBERGLASS PANEL NR 6212, BADLY WORN AROUND EDGE. FABRICATED NEW PANEL IAW BAC DRAWING 65-21674. ALODINED, PRIMED AND PAINTED IAW B727 SRM 51-10-2. 2L73 4F RTA3WE 20051005000092005100500009SO 2005 10 5 CHQA200500171 120051001A2120 ODOR EMB 145 EMB145LR 3260212SO COCKPIT DETECTED A CHQAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 GL11276SK 145348 FLIGHT 6320 - FLL-MCO - ON FINAL APPROACH, NOTICED SMOKE AND AN ODOR OF SMOKE. THE ELECTRIC PAGE INDICATED GEN 3 AMP 105. PERFORMED GENERAL VISUAL INSPECTION OF COMPONENTS IN THE FORWARD AVIONICS BAY. NO BURNS OR ODOR OF SMOKE. RAN BOTH ENGINES FOR 20 MINUTES, AND NO SMOKE OR ODOR APPEARED IN THE COCKPIT OR CABIN. GEN NR 3 STABLE AT 50 AMPS. OPS CHECK GOOD IAW EMB 145 SMP. 2L72 4T RTT00011AT 20051005000102005100500010SO 2005 10 5 CHQA200500172 120051002A3350 SIGN EMB 145 EMB145 3260210SO EMERGENCY EXIT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11264SK 145221 FORWARD EMERGENCY EXIT LOCATOR SIGN IN CEILING INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LOCATOR SIGN IAW EMB MM 33-50-15. OPS CHECK GOOD. 2L72 4F RTT00011AT 20051005000122005100500012NM 2005 10 5 QXEA200501267 120050927A2530 RECEPTACLE DHAV DHC8 DHC8202 2809007NM COFFEEMAKER MALFUNCTIONED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM09346PH 477 SEA FLIGHT NR 2137, BURNING ODOR FROM GALLEY, NO ODOR NOTED AFTER HOT JUGS TURNED OFF. MAINTENANCE REPLACED NR 2 HOT JUG ELECTRICAL RECEPTICLE. ALLOWED JUGS TO REMAIN ON FOR 15 MINUTES. NO BURNING ODOR NOTED. BOTH JUGS WORK AND CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051005000292005100500029NM 2005 10 5 DHL2005748539 120050902A5311 FRAME BOEING727 727225 1384077NM BS 520 DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 REFERENCE FLIGHTSTAR AIRCRAFT SERVICES NR 110155, DENT ON FRAME ABOVE STR 17R AT BS 520. CUT OUT DAMAGED AREA OF FRAME 1.6 BY 1.2 FAB REPAIR CHANNEL /050 7075 T6 PO NR 9001777 IAW B727 SRM 53-10-4 FIG 1. TREATED AND PRIMED ALL BARE SURFACES IAW B727 SRM 51-10-2. INSTALLED REPAIR CHANNEL IAW B727 SRM 53-10-4 FIG 1 REPAIR PART DIM 8.5 BY 4.0 IAW B727 SRM 53-10-4 FIG 1. 2L73 4F A3WE 20051005000302005100500030NM 2005 10 5 DHL2005748540 120050902A5311 FRAME BOEING727 727225 1384077NM BS 500 DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 REFERENCE FLIGHTSTAR AIRCRAFT SERVICES NR 110156, DENT ON FRAME ABOVE STR 17R AT BS 500. CUT OUT DAMAGED AREA OF FRAME 1.3 BY 1.2 FAB REPAIR CHANNEL .050 7075 T6 PO NR 9001777 IAW B727 SRM 53-10-4 FIG1. TREATED AND PRIMED ALL BARE SURFACES IAW B727 SRM 51-10-2. INSTALLED REPAIR CHANNEL IAW B727 SRM 53-10-4 FIG 1 REPAIR PART DIM 8.5 BY 4.0 IAW B727 SRM 53-10-4 FIG 1. 2L73 4F A3WE 20051005000322005100500032NM 2005 10 5 DHL2005748534 120050824A5740 ANGLE BOEING727 727225 1384077NM NR 1 SLAT ACT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 INNER WEB FWD OF NR 1 SLAT ACTUATOR ROD END IS CRACKED. CUT OUT SECTION OF WEB TO GAIN ACCESS DIM 7.75 BY 1.50 IAW B727 SRM 51-40-2. CUT CRACKED SECTION OF ANGLE IAW B727 SRM 51-40-3 FIG 1. FAB REPAIR ANGLE PO NR 9081237 .040 2024T3 2" BY 10" IAW B727 SRM 51-40-3 AND 57-50-2 FIG 2. FAB WEB REPAIR PO NR 9081237 .040 2024T3 2" X 12" IAW B727 SRM 51-40-2 & 57-50-2 FIG2 TREATED AND PRIMED REPAIR PARTS IAW B727 SRM BY 51-10-2. INSTALLED REPAIR PARTS IAW B727 5-40-2 AND 51-40-3 2L73 4F A3WE 20051005000332005100500033NM 2005 10 5 DHL2005748535 120050824A5740 CHANNEL BOEING727 727225 1384077NM NR 1 SLAT ACT BROKEN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 NR 1 SLAT ACTUATOR ROD END CHANNEL BRACKET IS BROKEN. REMOVED BROKEN ROD END CHANNEL AND BUSHINGS IAW B727 SRM 51-30-2 LOCATED AND DRILLED NEW CHANNEL P/N 65-17327-7 PO NR 5314113 IAW B727 SRM 51-40-5. TREATED AND PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED NEW CHANNEL IAW B727 SRM 51-30-2 AND BUSHINGS P/N NAS 538B11P016 PO NR 5314147 IAW B727 OHM 20-50-03. 2L73 4F A3WE 20051005000342005100500034NM 2005 10 5 DHL2005478537 120050831A5313 STRINGER BOEING727 727225 1384077NM BS 950A CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 AFT CARGO STR 30 AT BS 950A IS CRACKED. CUT OUT DAMAGED SECTION OF STR 30 DIM 15 1/2" IAW B727 53-10-3 FIG 1. FAB REPAIR PARTS AND REPLACED STR SECTIONS IAW B727 SRM 53-10-3 FIG 1 AND COTNEY AERO INC DWG NR AA00-53-R01 REV IR. TREATED AND PRIMED REPAIR PARTS IAW B727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW COTNEY AERO INC DWG NR AA00-53-0R01 REV IR. 2L73 4F A3WE 20051005000352005100500035 2005 10 5 BB05104 420050930A2565D30664105 SLIDE AIRBUSA319 A319112 3930323EU SERVICE DOOR FAULTY A USAAK NONE J WARNING INDICATION ININSP/MAINT 1 EA19733UW200154248 1205 PIT - A FORWARD SERVICE DOOR SLIDE ECAM WARNING INDICATED INTERMITTENTLY. MAINTENANCE REPLACED THE FORWARD SERVICE DOOR ESCAPE SLIDE. OK FOR SERVICE. 2L72 4F RTA28NM 20051005000372005100500037NM 2005 10 5 SB05124 120051001A335020121 POWER SUPPLY BOEING737 7374B7 1384702NM EMERGENCY LIGHT FAULTY A USAAO OTHER O OTHER CRCRUISE 1 EA19780AU 24997 CLT - FLT892 - EN ROUTE FROM BNA TO CLT, THE FLIGHT ATTENDANT REPORTED THE FORWARD CABIN EMERGENCY LIGHTS BEGAN FLICKERING OFF AND ON. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20051005000392005100500039NM 2005 10 5 DHL2005748536 120050825A5330 SKIN BOEING727 727225 1384077NM BS 950F CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 AFT CARGO AT BS 950F + 6, STR 28R IS CORRODED. CUT OUT DAMAGED AREA OF STR 28R AT BS950F +6 DIM 39". REPLACED WITH FILLER P/N BAC 1509-100204 PO NR 5314211 7075T6 39" AND 2EA SPLICES 7075T6 PO NR 5314245 PART FLT 092205 21 1/2" IAW B727 SRM 51-10-3 FIG1 AND COTNEY AERO INC DWG NR AA00-53-R01, REV IR. TREATED AND PRIMED REPAIR PARTS IAW B727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW COTNEY AERO INC DWG NR AA00-53-R01, REV IR 2L73 4F A3WE 20051005000492005100500049NM 2005 10 5 DHL2005748544 120050902A5311 FRAME BOEING727 727225 1384077NM BS 600 BENT A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 BENT FRAME ABOVE STR 17R AT BS 600. CUT OUT DAMAGED AREA OF FRAME 2.3 BY 1.7 FAB REPAIR CHANNEL 10 BY 4 .050 7075 T6 PO 9001777 IAW B727 SRM 53-10-4 FIG 1. TREATED AND PRIMED ALL BARE SURFACES IAW B727 SRM 51-10-2. INSTALLED REPAIR CHANNEL IAW B727 SRM 53-10-4 FIG 1. 2L73 4F A3WE 20051005000502005100500050NM 2005 10 5 DHL2005748545 120050902A5311 FRAME BOEING727 727225 1384077NM BS 640 BENT A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 BENT FRAME ABOVE STR 17R AT BS 640. CUT OUT DAMAGED AREA OF FRAME 1.3 BY 1.2 FAB REPAIR CHANNEL 8 1/2 BY 2 1/2 7075 T6 PO NR 9001777 IAW B727 SRM 53-10-4 FIG 1. TREATED AND PRIMED ALL BARE SURFACES IAW B727 51-10-2. INSTALLED NEW CHANNEL FRAME REPAIR IAW B727 SRM 53-10-4 FIG 1. 2L73 4F A3WE 20051005000512005100500051 2005 10 5 SWAA053005 420051002A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29628SW 27703 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051005000522005100500052NM 2005 10 5 SWAA053006 120050929A575465C26602 SKIN BOEING737 7373H4 1384600NM RT WING SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29631SW 27706 DURING SCHEDULED C4 CHECK, FOUND RT WING NR 5 L/E SLAT DELAMINATED. REMOVED AND REPLACED SLAT PER MM. 2L72 4F RTA16WE 20051006000012005100600001NM 2005 10 6 USAA051155 120050930A5753 SKIN BOEING737 7374B7 1384702NM TE FLAP DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 INBD END OF FLAP DELAMINATED. REMOVED DAMAGE AND REPAIRED IAW SRM 51-70-10, DEFECT SIZE: 6" BY 2". 2L72 4F RTA16WE 20051006000022005100600002NM 2005 10 6 USAA051156 120050930A5320 ANGLE BOEING737 7374B7 1384702NM BS 727E - 835 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 LEFT TRANSITION ANGLE BS 727 - 835 FOUND CORRODED. REPLACED ANGLE IAW SRM 53-60-53, DEFECT SIZE: CORROSION IN AREA'S FROM BS 727E TO 835. 2L72 4F RTA16WE 20051006000032005100600003NM 2005 10 6 USAA051157 120050930A575365C263208 SKIN BOEING737 7374B7 1384702NM FLAP WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19443US 24842 FOUND FLAP SKIN WORN OUTBOARD MID FLAP LEADING EDGE SKIN AT WING STATION 196.8461. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-53-1, REPAIR 8 DEFECT SIZE: 3.5X.75". 2L72 4F RTA16WE 20051003001122005100300112NM 2005 10 3 AWXA200501115 120050926A335020131A BATTERY BOEING737 7373Y0 1384671NM EMERGENCY LIGHT DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 DFW - EEL - DURING 8 DAY CHECK DISCOVERED EMERGENCY EXIT LIGHT INOPERATIVE AT OVERHEAD BINS 2L AND 4R. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY PACK AS REQUIRED IAW BOEING 737-300 AMM 33-51-51-2. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20051003001132005100300113CE 2005 10 3 DXTA200500978 120050919A3241 ANTI-SKID SYS CESSNA500 560CESSNA 2076750CE BRAKES MALFUNCTIONED E DXTAO OTHER O OTHER LDLANDING 1 GL07395QS 5600496 UPON LANDING, EXPERIENCED "HARD PEDALS" AND NO BRAKES FOR ABOUT 6 SECONDS. JUST BEFORE USING EMER BRAKING THE BRAKES SUDDENLY GRABBED VIOLENTLY. AFTER THAT THEY WORKED NORMALLY. GAINED ACCESS TO ANTI-SKID FAULT INDICATORS IN NOSE BAGGAGE AREA. FOUND NO FAULT INDICATIONS. INSPECTED BRAKE ASSEMBLIES FOR ANY DEFECTS, NONE NOTED. PERFORMED SEVERAL BUILT-IN BITE TESTS. ALL TESTS SATISFACTORY. PERFORMED TAXI CHECK AND OPERATIONAL CHECK OF BRAKE AND ANTI-SKID CONT SYSTEM. NO DEFECTS NOTED. ALL WORK PERFORMED IAW CE560 MM CH 32-42-00. 2L72 4F RTA22CE 20051003001222005100300122NM 2005 10 3 2005UALA01012 120050921A2150 A/C PACK AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE NR 1 INOPERATIVE A UALAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 WP29840UA 1522 WHILE AT FL310, A/C EXPERIENCED SLOW DEPRESSURIZATION. NR 1 PACK WAS INOP. NR 2 PACK WAS ON HIGH. EMERGENCY DESCENT TO FL160. CHECKED CABIN PRESSURE CONTROLLER AND BLEED MONITORING COMPUTER, CHECKED OK. PERFORMED PRESSURE CHECK OF LEFT AND RIGHT PACKS AND FOUND BOTH OPERATED NORMALLY FROM ANY SOURCE. FOUND BOTH FWD AND AFT CARGO DOOR SEAL LEAKING BADLY. REPLACED FWD CARGO DOOR SEAL PER AMM 52-31-18. REPLACE AFT CARGO DOOR SEAL PER AMM 52-32-18. FWD/AFT CARGO DOOR SEALS, P/N D5237106020200, PCN 110-4753. 2L72 4F4 FRTA28NM E40NE 20051003001302005100300130NM 2005 10 3 2005UALA01018 120050922A254010C10E SWITCH BOEING757 757222 1384956NM PWA 2037 PW2037 NE LAVATORY DOOR SHORTED A UALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP29536UA 25156 ELECTRICAL SMOKE SMELLED, WHITE SMOKE SEEN BRIEFLY IN AFT LAV. REPLACED DOOR LOCK SWITCH. 2L72 4F4 FRTA2NM E17NE 20051003001372005100300137NE 2005 10 3 DL73S050566 220050926A7200JT8D15AHK ENGINE BOEING737 737247 138448DNM PWA JT8 JT8D15A 52051NE NR 2 MALFUNCTIONED A DALAC ABORTED TAKEOFF C F.O.D. TOTAKEOFF 1 SO27244WA45346 23518 717141 MOMENTS AFTER ADDING T/O POWER HEARD A LOUD BOOM FROM RT SIDE OF A/C. ABORTED T/O APPROX 20 KTS. PAX REPORTED ORANGE FLAME FROM NR 2 ENG EXHAUST. SHUTDOWN NR 2 ENG AFTER CLEAR OF RUNWAY. NO ABNORMAL ENG INDICATIONS, NO FIRE INDICATION. INSP NR 2 INTAKE AND EXHAUST ON GATE ARRIVAL FOUND PIECES OF PLASTIC SHIPPING WRAP ON STATOR BLADES AND IN EXHAUST. PERFORMED BOROSCOPE INSP PER M/M CHAP 71. NO DEFECTS NOTED. RAN ENGINE TO T/O POWER PER PFHB ALL INDICATIONS AND OP CKS NORMAL. ACFT RTS. 2L72 4F4 F A16WE E2EA 20051003001572005100300157NM 2005 10 3 SWAA052949 120050927A53116546550 FRAME BOEING737 7373H4 1384600NM BS 787 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051003001712005100300171NM 2005 10 3 C1HA200568005 120050927A53206518636378 STIFFENER BOEING727 7272S7 138407ZNM KEELBEAM CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15686CA 22021 RT WHEEL WELL BS 870 AND KEEL BEAM VERTICAL STIFFENER CRACKED NOT CONFIRMED. REMOVED AND REPLACED DAMAGED ANGLE PN 65-18636-378 PO NR 535322 IAW 727 SRM 51-30-2, LEAK CHECK PERFORMED ON POST CHECK RUN SHEET M-054. 2L73 4F A3WE 20051003001722005100300172NM 2005 10 3 C1HA200586002 120050927A5311 FRAME BOEING727 7272S7 138407ZNM BS 700 CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15686CA 22021 FRAME LEG CORRODED IN FWD PIT AT FRAME 700 BETWEEN STRINGERS 28L AND 29L. CUT OUT DAMAGED AREA FABBED AND INST REPAIR DOUBLER AND ANGLE MADE FROM 7075 T6 .050 PO NR 9002126 DIM DOUBLER 6" BY 4 1/2" AND ANGLE 7" BY 2" IAW B727 SRM 53-10-4 FIG 11. OPENED WTB PANEL NR 3337 FOR ACCESS IAW 727 SRM 51-30-2. 2L73 4F A3WE 20051003001732005100300173NM 2005 10 3 C1HA200586001 120050927A5340691798820 SUPPORT BRACKET BOEING727 7272S7 138407ZNM NLG LOCK CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15686CA 22021 RT NLG LOCK ACTUATOR SUPPORT BRACKET HAS NUMEROUS GOUGES CORROSION IN ONE OF THE BOLT HOLES AND WORN BUSHING. REMOVED AND REPLACED RT AND LT NLG LOCK ACTUATOR SUPPORT BRACKETS IAW B727 MM 32-33-11. 2L73 4F A3WE 20051003001742005100300174NM 2005 10 3 C1HA200568003 120050927A534069191222 CHANNEL BOEING727 7272S7 138407ZNM NLG WW CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15686CA 22021 NLG LOCK ACTUATOR SUPPORT CHANNEL IS CRACKED BY LWR INB SUCTION VISUAL AND HFEC CONFIRMED. REMOVED AND REPLACED NLG LOCK ACTUATOR SUPPORT CHANNEL PN 69-19122-2 PO NR 535313 IAW 727 SRM 51-30-2. REMOVED DAMAGED FITTING CHANNEL IAW 727 SRM 51-30-2. 2L73 4F A3WE 20051003001852005100300185 2005 10 3 SWAA052946 420050927A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051003001922005100300192SO 2005 10 3 SWIA200515581 120050901A3350 LAMP EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07232SW 120306 ROW 9 OVERHEAD LIGHT INOP. REPLACED EXIT LAMP ASSY IAW33-60-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20051004000612005100400061NM 2005 10 4 PIDA20050155 120050928A5320654580727 ANGLE BOEING737 737228 13844AGNM BS 294.5 CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 ANGLE FORWARD OF R1 DOOR JUST BELOW STR 12RT IS CRACKED. REPLACED CRACKED ANGLE PER DWG 65-45807 AND SRM 51-10-1. 2L72 4F RTA16WE 20051004000642005100400064NM 2005 10 4 PIDA20050152 120050929A5320 STRAP BOEING737 737228 13844AGNM BS 1006-1016 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 STRAP IN AFT LAVATORY AREA HAS CORROSION FROM BS 1006 TO BS 1016+12. REPLACED STRAP PER DWG 65-46812 AND SRM 51-10-1. 2L72 4F RTA16WE 20051004000772005100400077EA 2005 10 4 SWIA200515591 120050922A3350 CHARGER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07963SW 7865 CENTER CABIN EMERGENCY EXIT CEILING SIGN WILL NOT ILLUMINATE. REPLACED BASE CHARGER IAW MM 33-51-00. OPERATIONAL CHECK GOOD, PN 11-0049 SN/OFF C03132. 2L72 4F RTA21EA 20051004000802005100400080NM 2005 10 4 CALA0500320 120050926A5315BAC1505100849 FLOORBEAM BOEING737 737724 13844BYNM BS 986.5 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716701 28762 INSPECTION FOUND FLOORBEAM AROUND FLOORBOARD HOLES AT STA 986.5, LBL 38.5 TO RBL 24. THE UPPER CHORD FLOORBEAM WAS REMOVED AND REPLACED IAW ECRA 5321-01293. 2L72 4F RTA16WE 20051004000892005100400089NM 2005 10 4 UPS05245534 120050913A3210 TRUNNION BOEING727 72725C 138400HNM LT MLG CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01932UP 19856 INSPECTION TYPE:C ON INSPECTION OF LT TRUNNION 2 SUSPECT CRACKS DETECTED ON HOLE C ON BOTH I/B SIDES. REPAIR CARRIED OUT IAW AAAE EO'S 2005-087-004, 2005-087-005, UPS EO B7 27-5740-20666 APPX F. UPS ENGINEERING FILE NO'S B727-5740-22955-A AND B727-5740-22975. 2L73 4F A3WE 20051004001122005100400112NM 2005 10 4 05FDEA03078 120050923A5330 DOUBLER BOEING727 727225 1384077NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 CORRSION FWD PIT BETWEEN STA 720D AND STA 720E INTERIOR SKIN BETWEEN STR 29L AND STR 29R. REMOVED CORROSION ORIG MAT .100 MAT REM .053 FAB PARTS, LOCATED AND DRILL ALODINE AND PRIME PARTS IAW B727 SRM 53-30-1, 51-10-6, 53-30-3, 53-30-2, 51-10-2, 51-20-1, FIG 2. 2L73 4F A3WE 20051004001142005100400114NM 2005 10 4 05FDEA03121 120050926A5230 SKIN BOEING727 727232 1384082NM CARGO DOOR MISSING A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 MAIN CARGO DOOR LOWER AFT CORNER HAS A PIECE OF EXTERIOR SKIN MISSING. REPAIRED MAIN CARGO DOOR SKIN PER FED EX EA 7-5230-93692A 2L73 4F A3WE 20051004001152005100400115EU 2005 10 4 05FDEA03137 120050927A5330 SKIN AIRBUS310 A310203 3930313EU FR 60 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25425FE 264 EXTERNAL FUSELAGE SKIN BULGING AT FR 60 S52 LT AND HAS SEVERAL SHEARED RIVETS. 2L72 4F RTA35EU 20051004001162005100400116EU 2005 10 4 05FDEA03138 120050927A7830 ATTACH BRACKET AIRBUS310 A310203 3930313EU THRUST REVERSER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25445FE 297 NR 2 ENG LT T/R FWD UPPER COMPRESSOR PAD ATTACHED BRACKET CRACKED AROUND MOUNTING HOLE. 2L72 4F RTA35EU 20051004001232005100400123NM 2005 10 4 DHL2005748516 120050816A5754 SKIN BOEING727 727225 1384077NM NR 8 SLAT DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 8 SLAT LE LWR SKIN SHOW DENT WS 716 (MARKED). CUT OUT DAMAGED AREA OF SKIN 2.5" BY 1.7" AND FAB DOUBLER 3.3" BY 5.7" .040 2024T3 PO 9051237 IAW B727 IAW B727 SRM 57-50-3. FAB FILLER 2.5 BY 1.6 .040 2024T3 PO 9051237 IAW B727 SRM 57-50-3. TREATED AND PRIMED ALL REPAIR PARTS IAW B727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B727 SRM 57-50-3 FIG 1. 2L73 4F A3WE 20051004001262005100400126NM 2005 10 4 AALA20050630 120050914A3350BPS73 BATTERY PACK BOEING767 767223 1385123NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21320AA 22321 AFW - EMERGENCY ESCAPE PATH LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK AT SEAT 25HJ FOR EMERGENCY ESCAPE PATH LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20051004001552005100400155NM 2005 10 4 USAA051153 120050928A5340 CLIP BOEING737 7374B7 1384702NM BS 772 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 CLIP CRACKED BS 772, RBL 20, AFT CARGO COMPARTMENT. REPLACED CLIP WITH NEW PART IAW SRM 51-10-02, DEFECT SIZE: .5". 2L72 4F RTA16WE 20051004001582005100400158SO 2005 10 4 SWIA200515595 120050924A3397 WIRE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07284YV 120284 ONE RED FLOOR EMERGENCY LIGHT AT OVERWING EXITS INOP. REPAIRED WIRES TO RED FLOOR EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20051005000382005100500038 2005 10 5 BB05087 420050930A2565 LANYARD BOEING757 7572B7 1384964NM ESCAPE SLIDE OUT OF ADJUST A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19627AU 27805 TPA - FOUND ESCAPE SLIDE D-RING LANYARDS NOT VISIBLE ON L1, L2, R1, R2, AND R4 DOORS. ALSO, FOUND R2 DOOR D-RING TANGLED ON GIRT BAR. MAINTENANCE REMOVED SLIDE COVERS AND CORRECTED ROUTING OF LANYARDS ON L1, L2, R1, R2, AND R4 DOORS. 2L72 4F RTA2NM 20051005000482005100500048NM 2005 10 5 DHL2005748542 120050902A5311 FRAME BOEING727 727225 1384077NM BS 650 BENT A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 BENT FRAME ABOVE STR 17R AT BS 560. CUT OUT DAMAGED AREA OF FRAME 1.3 BY 1.2 FAB REPAIR CHANNEL 10" BY 4" .050 7075 T6 PO NR 9001777 IAW B727 SRM 53-10-4 FIG 1. TREATED AND PRIMED ALL BARE SURFACES IAW B727 SRM 51-10-2. INSTALLED REPAIR CHANNEL IAW B727 SRM 53-10-4 FIG 1. 2L73 4F A3WE 20051006000052005100600005NM 2005 10 6 USAA051159 120050930A53116545771174 FLANGE BOEING737 7374B7 1384702NM BS 559 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 FOUND FUSELAGE CRACKED STATION 559 STRINGER 13L. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR ANGLE IAW EA 96912, DEFECT SIZE: .7". 2L72 4F RTA16WE 20051006000062005100600006NM 2005 10 6 USAA051160 120050930A53201137986 STRAP BOEING737 7374B7 1384702NM BS 767-858 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 FOUND STRAP CORRODED, STA 767-STA 858, RBL 20. REMOVED DAMAGED PART, REINSTALL NEW PART W/FILLER IAW SRM 51-10-02, DEFECT SIZE: 1.0". 2L72 4F RTA16WE 20051006000102005100600010NM 2005 10 6 USAA051162 120051003A531365617777 STRINGER SPLICE BOEING737 7374B7 1384702NM BS 360 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19443US 24842 FOUND BS 360, STRINGER SPLICE 15L, CRACKED. DEFECTIVE PART REPLACED WITH IDENTICAL PART, REMOVED AND REPLACED STRINGER SPLICE IAW SRM 51-40-02, DEFECT SIZE: .250". 2L72 4F RTA16WE 20051006000132005100600013NM 2005 10 6 SWAA053009 120050930A53306545774 SKIN BOEING737 7373A4 1384585NM BS 727E CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 24R. REPAIRED SKIN PER BFG ER. 2L72 4F RTA16WE 20051006000142005100600014NM 2005 10 6 SWAA053010 120050930A53306545765 SKIN BOEING737 7373A4 1384585NM BS 500D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 12L. REPAIRED SKIN PER BFG ER. 2L72 4F RTA16WE 20051006000162005100600016NM 2005 10 6 SWAA053012 120050930A53306545774 SKIN BOEING737 7373A4 1384585NM BS 762 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 762, BETWEEN STR 22R TO STR 23R. REPAIRED SKIN PER BFG ER. 2L72 4F RTA16WE 20051006000182005100600018NM 2005 10 6 SWAA053014 120050929A53226546546 SHEAR TIE BOEING737 737317 138447PNM BS 787 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, LBL 3. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051006000192005100600019NM 2005 10 6 SWAA053015 120050929A53156545410 FLOORBEAM BOEING737 737317 138447PNM BS 663 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 663, BL 0, WL 208. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20051006000212005100600021NM 2005 10 6 SWAA053017 120050930A2560PH22300L GLOWSTRIP BOEING737 7377H4 1384404NM ROW 8-10 LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29767SW 29807 PHOTOLUMINESCENT STRIP LOOSE AT ROW 8 TO ROW 10. SECURED STRIP PER MM. 2L72 4F RTA16WE 20051006000232005100600023NM 2005 10 6 AWXA200501140 120050906A531365617777 STRINGER SPLICE BOEING737 7373G7 1384595NM BS 359 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - MAJOR REPAIR - DURING C18 CHECK DISCOVERED STRINGER SPLICE CHANNEL CRACKED, .5 INCHES, AT BS 359 AND STR 15L. MAINTENANCE REMOVED CHANNEL IAW BOEING 737-300 SRM 51-40-02-0G FIG 8. RECEIVED REPLACEMENT CHANNEL AND PREPPED FOR INSTALLATION IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NO. 03-5311-05271-ES1. INSTALLED REPAIR PARTS AT BS 359 AND STR 15L IAW AWA ER 03-5311-05271-ES1. 2L72 4F RTA16WE 20051006000242005100600024NM 2005 10 6 AWXA200501141 120050906A53206517684643 ANGLE BOEING737 7373G7 1384595NM BS 294 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - DURING C18 CHECK DISCOVERED WEB ANGLE CRACKED, .5 INCHES IN LENGTH, AT STR 7L, BS 294. REMOVED ANGLE IAW BOEING 737-300 SRM 51-40-02-0G FIG 8. FABRICATED REPLACEMENT ANGLE IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5311-05271-ES1. INSTALLED FABRICATED REPAIR PARTS AT STR 7L, BS 294 IAW AWA ER 03-5311-05271-ES1. 2L72 4F RTA16WE 20051006000262005100600026NM 2005 10 6 AWXA200501143 120050906A534069265552 STRINGER CLIP BOEING737 7373G7 1384595NM BS 348 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - DURING C18 CHECK DISCOVERED .5 INCH LONG CRACK LOCATED AT STRINGER 16L, BS 348. REMOVED CRACKED CLIP IAW BOEING 737-300 SRM 51-40-02-06 FIG 8. FORMED AND INSTALLED CLIP AT BS 348, STRINGER 16L IAW AMERICA WEST AIRLINES ENGINEERING REQUEST NR 03-5311-05271-ES1. 2L72 4F RTA16WE 20051006000282005100600028NM 2005 10 6 AWXA200501145 120050904A5330654580026 SKIN BOEING737 7373G7 1384595NM BS 360 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 DURING C18 CHECK DISCOVERED 2 CRACKS, .250 INCHES IN LENGTH, ON FUSELAGE SKIN FROM FASTENER HOLE AT L1 CUTOUT LOWER AFT CORNER BS 360 AND STR 17L. MAINTENANCE TRIMMED OUT CRACKS IAW BOEING 737-300 SRM 55-00-01-2R FIG 201. FABRICATED DOUBLER, TRIPLER AND FILLER IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5300-05273-ES2. INSTALLED FABRICATED REPAIR PARTS AT L1 CUTOUT LOWER AFT CORNER BS 360 AND STR 17L IAW AWA ER NR 03-5300-05273-ES2. 2L72 4F RTA16WE 20051006000292005100600029NM 2005 10 6 AWXA200501146 120050906A53226948204505 ANGLE BOEING737 7373G7 1384595NM BS 360 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - DURING C18 CHECK, DISCOVERED FUSELAGE SKIN ATTACH ANGLE CRACKED .5 INCHES IN LENGTH AT BS 360 AND STR 13L. MAINTENANCE REMOVED ATTACH ANGLE IAW BOEING 737-300 SRM 51-40-02-0G FIG 8. FABRICATED REPLACEMENT FUSELAGE SKIN ATTACH ANGLE IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5311-05271-ES1. INSTALLED FABRICATED REPAIR PARTS AT BS 360 AND STR 13L IAW AWA ER NR 03-5311-05271-ES1. 2L72 4F RTA16WE 20051006000312005100600031NM 2005 10 6 AWXA200501148 120050911A5320654795711 SILL BOEING737 7373G7 1384595NM BS 794.3-847 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 MCN - DURING C15 CHECK DISCOVERED LEVEL 2 EXFOLIATION CORROSION AT AFT CARGO DOOR CUTOUT SILL STRAP BS 794.3 - 847, STRINGER 25R. CORROSION DETERMINED TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 58-60-15-1A1 FIG 101. REMOVED AND REPLACED WITH NEW STRAP IAW BOEING 737-300 SRM 51-40-02-0G FIG. 4 AND 8. 2L72 4F RTA16WE 20051006000322005100600032NM 2005 10 6 AWXA200501149 120050929A3040 CONTROLLER BOEING737 7373G7 1384595NM WINDSHILED HEAT FAILED A AWXAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP28158AW274674827 23780 DURING CRUISE, CREW REPORTED THAT F/O'S WINDOW ARCING & BEGAN TO CRACK. DIVERTED & LANDED WITHOUT FURTHER INCIDENT. MX R & R F/O'S NR 1 WINDOW IAW AMWEST TASK CARD R1B56001. ALSO, R & R FORWARD WINDOW HEAT CONTROL, FOR PRECAUTIONARY PURPOSES, IAW BOEING 737-300 MM 30-41-11-4. OPS TESTS GOOD. UPON TEARDOWN ON WINDOW HEAT CONTROLLER, FOUND COLD SOLDER JOINT ON SCR DRIVER CIRCUIT CAUSING INTERMITTENT OPERATION. VENDOR REWORKED PC BOARD. VENDOR REPAIRED UNIT IAW KOITO CMM 30-40-03 REV. 6. WINDOW WAS SCRAPPED AT VENDOR. 2L72 4F RTA16WE 20051006000352005100600035EU 2005 10 6 RAIA00509043 120050928A3350 LIGHT JETAIRJETSTMJETSTM4101 1500501EU ROW 8-9 INOPERATIVE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03559HK 41075 POST FLIGHT INSPECTION, EMERGENCY LIGHTS OUT AT ROW 8 AND 9. MAINTENANCE RESECURED LIGHTS. 2L72 4T RTA41NM 20051006000372005100600037SO 2005 10 6 RAIA00509045 120050929A3350 LIGHT EMB 145 EMB145 3260210SO CABIN INOPERATIVE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03801HK 145053 POST FLIGHT INSPECTION, EXIT ROW OVERHEAD EMERGENCY LIGHTS INOP. MAINTENANCE PERFORMED OPS CHECK OF EMERGENCY LIGHTING SYSTEM. 2L72 4F RTT00011AT 20051006000382005100600038SO 2005 10 6 RAIA00509048 120050929A2460 SMOKE EMB 145 EMB145 3260210SO COCKPIT DETECTED A RAIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CE03821HK 145068 FLT 5550 - LIT - PRIOR TO BOARDING, CREW NOTICED SMOKE COMING FROM UNDER FLOOR ON CAPTAINS SIDE. MAINTENANCE PERFORMED OPS CHECK OF THE AVIONICS SYSTEM WITH NO DEFECTS NOTED. 2L72 4F RTT00011AT 20051006000402005100600040EU 2005 10 6 RAIA00509050 120050930A33506047051 POWER SUPPLY JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT INOPERATIVE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03561HK19031570 41077 POST FLIGHT INSPECTION, OVERHEAD EMERGENCY LIGHT OUT AT 6A. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY. 2L72 4T RTA41NM 20051006000412005100600041SO 2005 10 6 RAIA00509046 120050929A3350 WARNING LIGHT EMB 145 EMB145ER 3260211SO EMERGENCY LIGHTSFALSE ACTIVATIONA RAIAO OTHER N FALSE WARNING CRCRUISE 1 CE03808HK 145157 FLT 3504 - PIT - EMERGENCY LIGHT NOT ARMED MESSAGE ON EICAS. MAINTENANCE OPS CHECKED THE EMERGENCY LIGHTING SYSTEM. NO FAULTS FOUND. 2L72 4F RTT00011AT 20051006000422005100600042SO 2005 10 6 RAIA00509047 120050925A5210 HANDLE EMB 145 EMB145LR 3260212SO PAX DOOR INOPERATIVE A RAIAO OTHER O OTHER TXTAXI/GRND HDL 1 CE03835HK 145670 FLT 8043 - MHT - MAIN DOOR DOES NOT OPEN. MAINTENANCE REMOVED AND REPLACED THE SIDE HINGED DOOR EXTERNAL ACTUATING HANDLE. 2L72 4T RTT00011AT 20051006000432005100600043NM 2005 10 6 QXEA200501276 120050930A27303170801A GENERATOR DHAV DHC8 DHC8202 2809007NM A/C SYSTEM MALFUNCTIONED A QXEAO OTHER HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 NM09357PH139744080 504 PDX FLIGHT NR 2298 ON ROTATION, RIGHT STALL WARNING ILLUMINATED THEN WENT DARK, A TRU LIGHT ILLUMINATED THEN WENT DARK, AND FINALLY NR 2 AC GENERATOR LIGHT ILLUMINATED AND STAYED ON. WHEN RUNNING NR 2 AC GENERATOR CHECKLIST, THE SAME SEQUENCE OF LIGHTS CAME ON AND OFF WITH FINAL RESULT ONCE AGAIN LEAVING NR 2 AC GENERATOR LIGHT ILLUMINATED. MX INSPECTED RIGHT AC CONTACTOR BOX. FOUND NO DISCREPANCIES. INSPECTED RIGHT BRUSH ASSEMBLY SLIP RINGS CLEANED RINGS, GROUND RAN AIRCRAFT NR 2 AC GENERATOR ONLY MAKING .08 VOLTS THEN CYCLING OFF. REMOVED AND REPLACED NR 2 AC GENERATOR PER AMM 24-21-00, PAGE 401-407. COMPLIED WITH FUNCTIONAL TEST PER AMM 24-21-00, PAGES 501/503. CHECKS GOOD. AIRCRAFT RETURNED TO SERVIC2H72 4T RTA13NM 20051006000462005100600046CE 2005 10 6 DXTA200500995 120050929A3210 LANDING GEAR CESSNA750 750 2076810CE VIBRATION E DXTAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL07977QS 7500077 LANDING GEAR BUMP OCCURS REPEATEDLY DURING CLIMB. PERFORMED GEAR BUMP TROUBLESHOOTING CHECKLIST IAW 750 MM 32-30-00. ALL CHECKS GOOD. PERFORMED NUMEROUS GEAR SWINGS, FAST AND SLOW. COULD NOT DUPLICATE DISCREPANCY. NO PREVIOUS HISTORY OF SQUAWK. OPS CHECK GOOD. 2L72 4J RTT00007WI 20051006000472005100600047CE 2005 10 6 DXTA200500997 120051002A3260 INDICATOR CESSNA560 560XL 2076702CE NLG NO INDICATION E DXTAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL07641QS 5605295 ON LANDING GEAR EXTENSION GREEN L/R MAIN WITH NO NOSE GEAR GREEN AND RED UNLOCK LIGHT. RECYCLED GEAR UP AND THEN DOWN WITH NO GREEN OR RED INDICATION. NO ANOMALIES ON LANDING ROLL OUT. JACKED AIRCRAFT, PERFORMED SEVERAL GEAR RETRACTIONS WITH NO DEFECTS NOTED PER CE560XL MM 32-30-00 AND 32-61-00. 2L72 4F RTA22CE 20051006000482005100600048NM 2005 10 6 QXEA200501277 120051001A2751 WARNING LIGHT BOMBDRDHC8 DHC8402 1390042NM TE FLAPS ILLUMINATED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09410QX 4053 SJC FLIGHT NR 2403: FLAP CAUTION POWER LIGHT ILLUMINATED AT TAKEOFF FLAP RETRACTION. C/W ABNORMAL CHECKLIST. FLAP POWER CAUTION LIGHT EXTINGUISHED. NO FURTHER PROBLEMS NOTED. MAINTENANCE CONTROL WAS NOTIFIED. OK FOR SERVICE PER DH8-400-SL-27-002A. NO PARTS REPLACED. AIRCRAFT OK FOR CONTINUED SERVICE. 2H72 4T RTA13NM 20051006000502005100600050NM 2005 10 6 AWXA200501153 120050912A534069353521 STRINGER CLIP BOEING737 7373G7 1384595NM BS 727D CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 MCN - DURING C15 CHECK, DISCOVERED .5 INCH CRACK IN AFT CARGO COMPARTMENT STRINGER TIE AT BS 727D STRINGER 23L. REMOVED STRINGER TIE IN AFT CARGO COMPT BS 727D STRINGER 23L IAW BOEING 737-300 SRM 51-40-02-0G FIG 8. FORMED NEW STRINGER TIE CLIP IAW BOEING DRAWING 69-35-352 AND BOEING 737-300 SRM 51-40-05-0G FIG 3. INSTALLED STRINGER TIE AT BS 727D STR 23L IAW BOEING 737-300 SRM 51-40-02-0G FIG 7 AND FIG 12. 2L72 4F RTA16WE 20051006000512005100600051NM 2005 10 6 AWXA200501154 120050910A532065C3267723 SHEAR WEB BOEING737 7373G7 1384595NM BS 986-1016 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 MCN - DURING C15 CHECK DISCOVERED LEVEL 2 CORROSION ON SHEAR WEB AT BS 986 TO 1016, WATERLINE 208, RBL 34 TO 43. DETERMINED CORROSION TO BE OUT OF LIMITS PER BOEING 737-300 SRM 53-60-51-1A1 FIG 101. FABRICATED NEW SHEAR WEB IAW BOEING DRAWING 65C32677 AND BOEING 737-300 SRM 51-30-01-0G FIG 2. INSTALLED SHEAR WEB AT BS 986 TO 1016, WATERLINE 208, RBL 34 TO 43 IAW BOEING 737-300 SRM 51-40-02-0G FIG 3, 4, 6, 7, AND 12. 2L72 4F RTA16WE 20051006000522005100600052NM 2005 10 6 AWXA200501155 120050909A57536546486155 WEDGE BOEING737 73733A 1384673NM TE FLAPS DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW 23634 GYR - DURING C20 CHECK DISCOVERED THE LT WING INBOARD FLAP, MID FLAP PANEL 7220, DELAMINATED AT UPPER SKIN. MAINTENANCE REMOVED DAMAGED SKIN AND CLEANED AREA IAW BOEING 737-300 SRM 51-70-10-2R. FABRICATED DOUBLER AND FILLER AND BONDED TO SKIN AT THE LT WING INBOARD FLAP, MID FLAP PANEL 7220 IAW BOEING 737-300 SRM 51-70-10-24. 2L72 4F RTA16WE 20051006000532005100600053NM 2005 10 6 AWXA200501156 120050912A5753 SKIN BOEING737 73733A 1384673NM ZONE 500 DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW BN949 23634 GYR - DURING C20 CHECK, DISCOVERED THE LT OUTBOARD AFT FLAP LOWER AND UPPER EDGE AREA DEBONDED, FROM WBL 224.40 TO WBL 231.4. MAINTENANCE REMOVED DAMAGED ARE ON THE AFT FLAP LOWER AND UPPER SURFACE IAW BOEING 737-300 SRM 51-70-10-2R. FABRICATED CORE AND DOUBLER IAW BOEING 737-300 SRM 51-70-10-2R. BONDED REPAIR PARTS TO THE LT OUTBOARD AFT FLAP IAW BOEING 737-300 SRM 51-70-10-2R. 2L72 4F RTA16WE 20051006000542005100600054NM 2005 10 6 AWXA200501157 120050910A532065C334191 SHEAR WEB BOEING737 7373G7 1384595NM BS 1016-1031 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 MCN - DURING C15 CHECK DISCOVERED LEVEL 2 GALVANIC CORROSION ON THE LEFT HAND AFT LAV SUB-FLOOR (MAIN DECK) SHEAR WEB AT BS 1016 - 1031, LBL 2 - 36, WL 208. DETERMINED CORROSION OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-51-1A-1 FIG 101. REMOVED SHEAR WEB IAW BOEING 737-300 SRM 51-40-02-0G FIG 8. INSTALLED NEW SHEAR WEB IAW BOEING 737-300 SRM 51-40-02-0G PAR 4 FIG 3, 4, 6, 7, AND 8 AT BS 1016 - 1031, LBL 2 - 36 WL 208. 2L72 4F RTA16WE 20051006000562005100600056NM 2005 10 6 AWXA200501159 120050911A534065465951 STRINGER CLIP BOEING737 7373G7 1384595NM BS 727A CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 MCN - DURING C15 CHECK, DISCOVERED STRINGER TIE CRACKED AT BS 727A, STR 25L IN THE AFT CARGO COMPARTMENT. MAINTENANCE REMOVED CRACKED STRINGER TIE IAW BOEING 737-300 SRM 51-40-02-0G. RECEIVED NEW STRINGER TIE AND INSTALLED AT BS 727A, STR 25L IN THE AFT CARGO COMPARTMENT IAW BOEING 737-300 SRM 51-40-02-0G FIGS 3 AND 8. 2L72 4F RTA16WE 20051006000572005100600057NM 2005 10 6 AWXA200501160 120050912A532269389722 SHEAR TIE BOEING737 7373G7 1384595NM BS 312 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 MCN - DURING C15 CHECK, DISCOVERED SHEAR TIE CLIP CRACKED .450 INCHES IN LENGTH IN THE E AND E COMPARTMENT BILGE AT BS 312 AND STRINGER 28L. MAINTENANCE REMOVED CRACKED SHEAR TIE IAW BOEING 737-300 SRM 51-40-02. FABRICATED SHEAR TIE IAW BOEING 737-300 BAC DRAWING 69-38972. INSTALLED FABRICATED REPAIR PARTS AT BS 312 AND STRINGER 28L IAW BOEING 737-300 SRM 51-40-02-0G. 2L72 4F RTA16WE 20051006000612005100600061EA 2005 10 6 QXEA200501269 120050927A2760 WARNING SYSTEM CNDAIRCL600 CL6002C10 1390015EA COCKPIT FALSE ACTIVATIONA QXEAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 NM09612QX 10042 PDX- ON TAXI OUT FOR FLIGHT 2509, RECEIVED A SPOILER STAB AND RUDDER LIMIT FAULT MESSAGE. FLIGHT RETURNED TO THE GATE. MAINTENANCE DETERMINED MESSAGE WAS DUE TO A ISI AND ADI MISMATCH. PURGED THE PITOT STATIC SYSTEM. NO FAULTS OR MOISTURE FOUND. OPERATIONAL CHECKS GOOD. NO PARTS REPLACED. 2L72 4F RTA21EA 20051006000652005100600065NM 2005 10 6 2005UALA01025 120050923A5230 SKIN BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE CARGO DOOR DENTED A UALAO OTHER O OTHER NRNOT REPORTED 1 WP29918UA 25385 AFT PIT DOOR EXTERIOR SKIN HAS DENTS. DAMAGE REMOVED, MANUFACTURED AND INSTALLED REPAIR PER SRM. 2L72 4F4 FRTA16WE E2GL 20051006000662005100600066NM 2005 10 6 2005UALA01026 120050923A5310 CREASE BEAM BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE BS 962-1006 CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29918UA 25385 AFT CABIN FLOOR STA 962 TO STA 1006 WL 208 RBL 54 RT CREASE BEAM CORRODED. REMOVED DAMAGE CREASE BEAM INNER CORD. MATCH DRILLED AND INSTALLED NEW CORD REF SRM 51-40-0 2. 2L72 4F4 FRTA16WE E2GL 20051006000672005100600067NM 2005 10 6 2005UALA01027 120050923A5313 STRINGER SPLICE BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE BS 907 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29918UA 25385 AFT CABIN CROWN STRINGER SPLICE IS CRACKED AT STA 907 STR 4R. REMOVED DAMAGED STRINGER SPLICE. ACCOMP HFEC INSPECTION ON EXISTING STRINGER SECTIONS. NO CRACKS FOUND. DRILLED UP NEW STRINGER SPLICE CHANNEL PN 65-51698-2 AND INSTALLED. REF SRM 51-40-02. 2L72 4F4 FRTA16WE E2GL 20051006000682005100600068NM 2005 10 6 2005UALA01028 120050923A5311 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE BS 907 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29918UA 25385 AFT CABIN FRAME IS CRACKED AT STA 907 NEAR STR 8L. FABRICATED AND INSTALLED REPAIR PARTS WITH REF TO MM 53-10-84. FABRICATED NEW RAIL SUPPORT BRACKET. 2L72 4F4 FRTA16WE E2GL 20051006000692005100600069NM 2005 10 6 2005UALA01029 120050923A5311 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE BS 787 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29918UA 25385 AFT CABIN FRAME IS CRACKED AT STA 787 NEAR STR 8L MARKED. FABRICATED ANGLE,FILLER & SUPPORT BRACKET PER MM 53-10-84 AND INSTALLED. 2L72 4F4 FRTA16WE E2GL 20051006000702005100600070NM 2005 10 6 2005UALA01030 120050923A5311 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE BS 867 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29918UA 25385 AFT CABIN STA 867 FRAME IS CRACKED NEAR STR 8L. FABRICATED AND INSTALLED REPAIR PARTS WITH REF. TO MM CHAPT 53-10-84. FABRICATED NEW RAIL SUPPORT BRACKET. 2L72 4F4 FRTA16WE E2GL 20051006000712005100600071NM 2005 10 6 2005UALA01031 120050923A5311 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE STA 827 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29918UA 25385 AFT CABIN FRAME IS CRACKED AT STA 827 NEAR STR 8L MARKED. FABRICATED AND INSTALLED ANGLE, FILLER AND SUPPORT PER MM 53-10-84 2L72 4F4 FRTA16WE E2GL 20051006000802005100600080NM 2005 10 6 2005UALA01032 120050924A5311 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE BS 727B CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29918UA 25385 MID CABIN FRAME IS CRACKED AT FASTENER HOLE AT STA 727B NEAR STR 8L. ACCOMPLISHED A REPAIR PER MM 53-10-84, FABRICATED ANGLE, FILLER AND SUPPORT AND INSTALLED PER MM. 2L72 4F4 FRTA16WE E2GL 20051006000812005100600081NM 2005 10 6 2005UALA01033 120050924A3350362624 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE SEAT 3A INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29121UA 29167 EEL INOP AT SEAT 3A AFT AND 44ABC. REPLACED LAMP. 2L74 4F4 FRTA20WE E24NE 20051006000822005100600082NM 2005 10 6 2005UALA01034 120050924A33501317 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE ROW 13 BURNED OUT A UALAK NONE L NO TEST ININSP/MAINT 1 WP29121UA 29167 EMERG LTS INOP AT CEILING ROW 13 AND 14. REPLACED LAMPS. 2L74 4F4 FRTA20WE E24NE 20051006000842005100600084NM 2005 10 6 2005UALA01036 120050925A5200213T31011 DOOR BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE RAM AIR SEPARATED A UALAA UNSCHED LANDING DE INFLIGHT SEPARATION VIBRATION/BUFFET CLCLIMB 1 WP29649UA58394 25286 DIVERTED TO YQX DUE TO AIRFRAME VIBRATION. RAM AIR INLET DOOR ASSY WAS FOUND WITH FORWARD INLET DOOR ASSY P/N 213T3010-1 MISSING. AFT HINGE ASSY P/N 213T3108-4 ATTACHING THE FORWARD AND AFT INLET DOOR ASSY WAS ALSO MISSING. FORWARD HINGE ASSY P/N 213T3109-4 WAS FOUND ATTACHED TO THE AIRCRAFT. THE FIVE FASTENERS ATTACHING FORWARD HINGE ASSY TO THE FORWARD INLET DOOR WERE SHEARED. AFT INLET DOOR ASSY P/N 213T3009-1 WAS FOUND WITH NO VISIBLE STRUCTURAL DAMAGE. THE EIGHT FASTENERS INCLUDING THE COLLARS, ATTACHING THE AFT INLET DOOR ASSY TO AFT HINGE ASSY P/N 213T3108-4 WERE MISSING. BLOCKS AND ATTACHING HARDWARE WERE STILL INSTALLED ON THE AFT INLET DOOR. ACTUATOR WAS REPORTED TO HAD BEEN REPLACED. 2L72 4F4 FRTA1NM E24NE 20051006000852005100600085NE 2005 10 6 2005UALA01037 220050922A7200 WARNING LIGHT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 2 ENGINE ILLUMINATED A UALAO OTHER J WARNING INDICATION CLCLIMB 1 WP29454UA 1104 V10614 UPPER ECAM NR 2 ENGINE STALL DISPLAYED ON TAKEOFF. ECM DATA SHOW STALL OCCURRED IN FLIGHT PHASE 6. MAINTENANCE FOUND MUSCLE LINE LOOSE ON TENTH STAGE HPC BLEED SOLENOID. LEAKING MUSCLE AIR COULD OF LEAD TO SLOW OR FAULTY OPERATION OF TENTH STAGE HPC STABILITY BLEED RESULTING IN A STALL. NO FURTHER EVENTS CONFIRMS THIS HYPOTHESIS. 2L72 4F4 FRTA28NM E40NE 20051006000872005100600087NM 2005 10 6 2005UALA01039 120050924A2751 WARNING SYSTEM BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FLAPS ACTIVATED A UALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP29642UA 25092 ABORTED TAKE OFF DUE TO FLAP CONFIGURATION MESSAGE. 2L72 4F4 FRTA1NM E24NE 20051006000892005100600089NM 2005 10 6 2005UALA01041 120050923A335060253 LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE GALLEY G2B CUT A UALAK NONE O OTHER ININSP/MAINT 1 WP29512UA 24809 EEL INOP AT GALLEY G2A AND G2B. SUPPLEMENTAL DATA UPDATE, G2B EEL FOUND CUT, REPLACED EEL LIGHT. 2L72 4F4 FRTA2NM E17NE 20051006000912005100600091NM 2005 10 6 2005UALA01043 120050926A2130 CABIN PRESSURE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE MALFUNCTIONED A UALAO OTHER J WARNING INDICATION NRNOT REPORTED 1 WP29399UA 24674 UNABLE TO HOLD PRESSURIZATION. REPLACED OVERHEAD CABIN PRESSURE SELECTOR REF MM21-31-25 AND CABIN PRESSURE CONTROLLER REF MM21-31-21 AND ACCOMPLISHED SYSTEM OPS TEST PER MM21-31-00 ALL CK OK. ALSO PRESSURIZED A-C MANUALLY UP TO 3.5 DIFFERENTIAL ALL CK OK. 2L72 4F4 FRTA16WE E2GL 20051006000922005100600092NM 2005 10 6 2005UALA01044 120050926A2120 ODOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN DETECTED A UALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 WP29572UA 26682 AFTER APU START AT DEPARTURE WITH PACKS ON FOR SEVERAL MINUTES FLT CREW NOTED ELECTRICAL ODOR THROUGHOUT CABIN AND FLIGHT DECK. MAINTENANCE RAN PACKS USING APU PNEUMATICS FOR 20 MINS IN ACCORDANCE WITH MM21-00-01 WITH NO FURTHER SMELL NOTED. RETURNED AIRCRAFT TO SERVICE. 2L72 4F4 FRTA2NM E17NE 20051006000932005100600093NE 2005 10 6 SWAA053018 220051003A7200CFM563 ENGINE BOEING737 7373H4 1384600NM GE CFM56 CFM563B1 13802NE NR 2 OVERTEMP A SWAAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SW29315SW 23337 857573 AIR TURNBACK, NR 2 ENGINE OVERTEMP AT 990 DEGREES FOR 15 SECONDS. RED OVERTEMP LIGHT ILLUMINATED FOR MORE THAN 1 MINUTE. MX FERRY TO PHX. REMOVED AND REPLACED NR 2 ENGINE PER MM. 2L72 4F4 FRTA16WE E2GL 20051006000942005100600094NM 2005 10 6 SWAA053019 120051003A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM BS 312 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D CHECK, FOUND FUSELAGE FLOORBEAM UPPER CHORD CORRODED AT BS 312, BETWEEN LBL 12 TO RBL 12. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20051006000952005100600095NM 2005 10 6 SWAA053020 120051002A2560PH22300L GLOWSTRIP BOEING737 7373H4 1384600NM ROW 8-12 WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED C1 CHECK, FOUND PHOTOLUMINESCENT STRIP WORN BETWEEN ROW 8 TO ROW 12. REMOVED AND REPLACED STRIP PER MM. 2L72 4F RTA16WE 20051006000962005100600096NM 2005 10 6 SWAA053021 120051002A53116517684 FRAME BOEING737 7373H4 1384600NM R1 DOORWAY CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE FRAME CRACKED AT R1 DOOR UPPER HINGE CUTOUT. REPAIRED FRAME PER SWA EA. 2L72 4F RTA16WE 20051006000972005100600097NM 2005 10 6 SWAA053022 120051002A2560PH22300L GLOWSTRIP BOEING737 7373H4 1384600NM ROW 8-10 WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29364SW 26575 DURING SCHEDULED C1 CHECK, FOUND PHOTOLUMINESCENT STRIP WORN FROM ROW 8 TO ROW 10. REMOVED AND REPLACED STRIP PER MM. 2L72 4F RTA16WE 20051006000982005100600098NM 2005 10 6 SWAA053023 120051002A53306545769 SKIN BOEING737 7377H4 1384404NM BS 510A CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29408WN 27895 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 510A, NR 2 DME ANTENNA MOUNT HOLES. REPAIRED SKIN PER SWA EA AND SRM. 2L72 4F RTA16WE 20051006000992005100600099NM 2005 10 6 SWAA053024 120051003A53116520722 FRAME BOEING737 7375H4 138449DNM CARGOWAY CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29506SW 24183 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, FWD BOTTOM DOOR STOP FITTING. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20051006001032005100600103 2005 10 6 2005UALA01046 420050927A2565 HOSE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE DOOR SLIDE BROKEN A UALAK NONE O OTHER ININSP/MAINT 1 WP29430UA 568 FOUND BROKEN HOSE. 2L72 4F4 FRTA28NM E40NE 20051006001072005100600107 2005 10 6 2005UALA01050 420050929A2565 MOUNT BRACKET AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE L1 DOOR SLIDE BROKEN A UALAK NONE O OTHER ININSP/MAINT 1 WP29826UA 989 DOOR 1L SLIDE AFT LWR MOUNT BRACKET BROKEN. THE STEP BRACKETS OF SLIDE (LH & RH) ARE THE TWO BOTTOM ATTACHMENT POINTS THAT HOLD THE SLIDE ASSEMBLY ONTO THE AIRCRAFT DOOR. THESE PARTS ARE STICKING OUT OF THE WHOLE ASSEMBLY AND ARE LIABLE TO DAMAGE ESPECIALLY DURING TRANSPORTATION AND HANDLING. WHEN THE ASSEMBLY IS DROPPED ACCIDENTALLY THE BRACKETS ARE THE IMPACT POINTS. BRACKETS ARE ROUTINELY REPLACED WHEN FOUND BROKEN IN THE SHOP. 2L72 4F4 FRTA28NM E40NE 20051006001082005100600108NM 2005 10 6 2005UALA01051 120050929A335020131A BATTERY PACK BOEING757 757222 1384956NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29529UA 25019 EMERGENCY EXIT LIGHT ABOVE ROW 16 LT INOP. REPLACED BATTERY PACK AT POWER SUPPLY LOC, M10699 (ROW 23DEF). 2L72 4F4 FRTA2NM E17NE 20051006001102005100600110NM 2005 10 6 2005UALA01053 120050930A335020131A POWER SUPPLY BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29175UA 24382 EMERGENCY EXIT CEILING LIGHT IN FLIGHT DECK INOP. REPLACED POWER SUPPLY. 2L74 4F4 FRTA20WE E24NE 20051006001112005100600111NM 2005 10 6 2005UALA01054 120050930A3397794640 WIRE BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT DAMAGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29175UA 24382 CENTER LAV CROSS AISLE WALL MOUNTED EMERGENCY EEL LIGHT INOP. REPAIRED FEEDER CABLE. 2L74 4F4 FRTA20WE E24NE 20051006001122005100600112NM 2005 10 6 2005UALA01055 120050930A3350BACC45FT1610 CONNECTOR BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT DAMAGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29175UA 24382 EMERGENCY EXIT SIGN BELOW VIDEO MONITOR AT DOOR 3 LEFT INOP. REPAIRED CONNECTOR. 2L74 4F4 FRTA20WE E24NE 20051006001142005100600114NM 2005 10 6 SWAA053028 120051003A531165C22908 FRAME BOEING737 737317 138447PNM BS 500B CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SWA EA. 2L72 4F RTA16WE 20051006001182005100600118NM 2005 10 6 DHL2005748543 120050902A5311 FRAME BOEING727 727225 1384077NM BS 580 BENT A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 BENT FRAME ABOVE STR 17R AT BS 580. CUT OUT DAMAGED AREA OF FRAME 1.8 BY 1.7 FAB REPAIR CHANNEL 10 BY 4 .050 7075 T6 PO NR 9001777 IAW B727 SRM 53-10-4 FIG 1. TREATED AND PRIMED ALL BARE SURFACES IAW B727 SRM 51-10-2. INSTALLED REPAIR CHANNEL IAW B727 SRM 53-10-4 FIG 1. 2L73 4F A3WE 20051006001242005100600124NM 2005 10 6 SWAA052999 120050930A53116520723 FRAME BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29506SW 24183 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, AFT BOTTOM DOOR STOP FITTING. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20051006001252005100600125NM 2005 10 6 SWAA053000 120050930A3350MS155721 BULB BOEING737 7375H4 138449DNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29523SW 26565 DURING SCHEDULED SERVICE CHECK, FOUND LT AFT LOWER EXTERNAL EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20051006001262005100600126NM 2005 10 6 SWAA053001 120050930A3397W115001120 WIRE BOEING737 7375H4 138449DNM EMERGENCY LIGHT SHORTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29523SW 26565 DURING SCHEDULED SERVICE CHECK, FOUND FWD GALLEY EMERGENCY EXIT LIGHTS INOP. REPAIRED WIRE NR W1150-011-20 PER WDM. 2L72 4F RTA16WE 20051006001282005100600128NM 2005 10 6 SWAA053003 120050930A53116546555 FRAME BOEING737 7373H4 1384600NM BS 867 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051006001302005100600130NM 2005 10 6 DHL2005748541 120050902A5311 FRAME BOEING727 727225 1384077NM BS 540 DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 DENT ON FRAME ABOVE STR 17R AT BS 540. CUT OUT DAMAGED AREA OF FRAME 1.5 BY 1.2 FAB REPAIR CHANNEL .050 7075 T6 PO NR 9001777 IAW B727 SRM 53-10-4 FIG 1. TREATED AND PRIMED ALL BARE SURFACES IAW B7272 SRM 51-10-2. INSTALLED REPAIR CHANNEL IAW B727 SRM 53-10-4 FIG 1 REPAIR PART DIM 8.5 X 4.0 IAW B727 SRM 53-10-4 FIG1 2L73 4F A3WE 20051006001322005100600132NM 2005 10 6 USAA051166 120051003A5320 ANGLE BOEING737 7374B7 1384702NM BS 727C-767 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 FOUND AFT CARGO COMPARTMENT RT TRANSITION ANGLE AT BS 727C TO 767 CORRODED. FABRICATED AND INSTALLED A NEW TRANSITION ANGLE IAW SRM 53-60-53, DEFECT SIZE: 1" BY 28". 2L72 4F RTA16WE 20051006001332005100600133NM 2005 10 6 USAA051168 120051003A5315 FLOORBEAM BOEING737 7374B7 1384702NM BS 294 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19443US 24842 FOUND FLOORBEAM UPPER T-CAP AT CLIPNUT HOLE AT BL 0 AND STA 294 CORRODED. INSTALLED REPAIR T CAP IAW SRM 53-10-51 FIG 201, SHEETS 1-4, DEFECT SIZE: 1". 2L72 4F RTA16WE 20051006001342005100600134NM 2005 10 6 USAA051170 120051003A5330 SKIN BOEING737 7373B7 1384580NM BS 727 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19395US 23317 FOUND FUSELAGE STATION 727, STRINGER 22L CRACKED. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-00-01 DETAIL X DEFECT SIZE: 1.5". 2L72 4F RTA16WE 20051006001352005100600135NM 2005 10 6 USAA051171 120051003A5340 STRINGER CLIP BOEING737 7374B7 1384702NM BS 344 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19443US 24842 FOUND STRINGER 11R AND STA 344, CRACKED. REMOVED AND REPLACED CLIP IAW SRM 51-40-02, DEFECT SIZE: .4". 2L72 4F RTA16WE 20051006001382005100600138NM 2005 10 6 USAA051174 120051003A575465C26602 WEDGE BOEING737 7374B7 1384702NM NR 5 SLAT DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 FOUND NUMBER 5 SLAT WEDGE TOP SURFACE 10 INCHES FROM OUTBOARD END DAMAGED. REMOVED DAMAGE, FABRICATED AND INSTALLED CORE, FABRICATED AND INSTALLED DOUBLER IAW 57-42-02, DEFECT SIZE: 6". 2L72 4F RTA16WE 20051006001422005100600142NM 2005 10 6 USAA051177 120051004A5314 KEELBEAM BOEING737 7374B7 1384702NM BS 500G CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19443US 24842 FOUND LEFT KEEL BEAM AFT SIDE OF STA 500G, CRACKED. FABRICATED AND INSTALLED NEW ATTACH ANGLE IAW SRM 51-10-02 AND BOEING DWG 69-73527, DEFECT SIZE: 1" CRACK. 2L72 4F RTA16WE 20051006001452005100600145EU 2005 10 6 USAA051180 120051004A5347D5347218820400 SEAT TRACK AIRBUSA319 A319112 3930323EU FR 68 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19733UW 1205 FOUND CORROSION LEVEL 1; TASK JA-260-53500; LEFT OTBD SEAT TRACK FLOORBEAM AT FS 68. REMOVED AND REPLACED PART WITH NEW PER SRM 51-72-11, DEFECT SIZE: 1" BY 3" AREA. 2L72 4F RTA28NM 20051006001462005100600146EU 2005 10 6 USAA051181 120051004A5310D5342707500100 BEAM AIRBUSA319 A319112 3930323EU SERVICE DOORWAY CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19733UW 1205 FOUND CORROSION TASK JA-260-53500; LEVEL 1; AFT SVD DOOR SILL BEAM AT FS 66. REMOVED AND REPLACED BEAM PER SRM 51-42-00, DEFECT SIZE: 4" BY 6". 2L72 4F RTA28NM 20051006001472005100600147EU 2005 10 6 USAA051182 120051004A5347D5347209000300 SEAT TRACK AIRBUSA319 A319112 3930323EU FS 64 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19733UW 1205 FOUND CORROSION, LEVEL 1; TASK JA-260-53500; 8" AFT OF FS 64 ON RT SIDE INBD SEAT TRACK. REMOVED AND REPLACED WITH NEW PART PER SRM 51-72-11, DEFECT SIZE: 2" BY 4". 2L72 4F RTA28NM 20051006001482005100600148NM 2005 10 6 DHL2005748546 120050902A5311 FRAME BOEING727 727225 1384077NM BS 660 BENT A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 BENT FRAME ABOVE STR 17R AT BS 660. CUT OUT DAMAGED AREA OF FRAME 1.2 BY 1.7 FAB REPAIR CHANNEL 8 1/2 BY 2 1/2 7075 T6 PO NR 9001777 IAW B727 SRM 53-10-4 FIG 1. TREATED AND PRIMED ALL BARE SURFACES IAW B727 51-10-2. INSTALLED NEW CHANNEL FRAME REPAIR IAW B727 SRM 53-10-4 FIG 1. 2L73 4F A3WE 20051006001492005100600149NM 2005 10 6 DHL2005748547 120050902A5311 FRAME BOEING727 727225 1384077NM BS 680 DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 DENT ON FRAME ABOVE STR 17R AT BS 680. CUT OUT DAMAGED AREA OF FRAME 1 BY 1.5 FAB REPAIR CHANNEL 8 1/2 BY 2 1/2 7075 T6 PO 9001777 IAW B727 SRM 53-10-4 FIG1. TREATED AND PRIMED ALL BARE SURFACES IAW B727 51-10-2. INSTALLED NEW FRAME REPAIR B727 SRM 53-10-4 FIG 1. 2L73 4F A3WE 20051006001522005100600152NM 2005 10 6 QXEA200501268 120050928A5210 BOLT DHAV DHC8 DHC8202 2809007NM HAND RAIL LOOSE A QXEAK NONE O OTHER TXTAXI/GRND HDL 1 NM09351PH 490 SEA - MAIN CABIN DOOR WILL NOT OPEN. MAINTENANCE INSPECTED AND FOUND LOOSE BOLT AT AFT HANDRAIL PIVOT POINT. TIGHTENED BOLT. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051006001532005100600153 2005 10 6 QXEA200501249 420050723A3418C12851AA03 COMPUTER CNDAIRCL600 CL6002C10 1390015EA STALL PROTECTIONMALFUNCTIONED A QXEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM09609QX2441 10031 DEN - ON FLIGHT 4165 (DEN-SJC) DURING CLIMB, THE RIGHT STALL CAUTION ILLUMINATED. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE REPLACED THE STALL PROTECTION COMPUTER. OPERATIONAL CHECKS GOOD AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20051006001552005100600155NM 2005 10 6 05FDEA03168 120050930A5730 PANEL BOEING727 727233 138408ANM ZONE 600 ERODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25267FE 21673 RIGHT WING LEADING EDGE PANEL NR 6541 ERRODED. FABRICATED NEW PANEL IAW BAC DRAWING 65-21675. ALODINED, PRIMED AND PAINTED IAW B727 SRM 51-10-2. 2L73 4F RTA3WE 20051006001572005100600157WP 2005 10 6 05FDEA03172 120050930A5313 LONGERON DOUG DC10 DC1010 3022110WP BS 1961 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25389FE 46623 CORROSION ON LONGERON L49L AT FS 1961 INBD VERTICAL LEG. REMOVED CORROSION ORIGINAL THICKNESS .068, REMAINING .051, REMOVED .071 FOUND TO BE OUT OF LIMITS IAW SRM 51-10-0. REMOVED DAMAGED LONGERON IAW DC10 SRM 51-33-01 VOL 11. MACHINED NEW LONGERON SECTION AND SPLICE IAW DWG AGA3104 AND DC10 SRM 53-10-00 VOL II. ALODINED AND PRIMED IAW DC10 SRM 51-21-01 VOL II. INSTALLED IAW DC10 SRM 51-33-01 VOLII. 2L73 4F A22WE 20051006001582005100600158EA 2005 10 6 COMA0560527 120050929A275011045D100 COUPLING CNDAIRCL600 CL6002B19 1900309EA TE FLAPS WORN A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01910EV 7727 FLIGHT 5228 - FLAPS FAIL CAUTION. REPLACED 5 FLEX DRIVE CABLES ON LT WING AND 3 FLEX DRIVE CABLES ON RT WING. 2L72 4F RTA21EA 20051006001592005100600159EA 2005 10 6 COMA0560528 120050930A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01926CA 7027 FLIGHT 5033 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2L72 4F RTA21EA 20051006001602005100600160EA 2005 10 6 COMA0560529 120050930A2752854D10020 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA RT WING TE FLAPSUNRELIABLE A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01814CA8402 7387 FLIGHT 5858 - FLAPS FAIL CAUTION. REPLACED THE RT WING FLAP ACTUATORS. 2L72 4F RTA21EA 20051006001632005100600163SO 2005 10 6 RAIA00509041 120050925A2150 CLAMP EMB 145 EMB145 3260210SO CABIN COOLING LOOSE A RAIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CE03801HK 145053 FLT 3504 - PIT - SMOKE IN CABIN WHILE AT GATE. MAINTENANCE PERFORMED OPS CHECK OF COOLING SYSTEM AND SECURED LOOSE CLAMP. NO SMOKE FOUND. 2L72 4F RTT00011AT 20051006001662005100600166WP 2005 10 6 05FDEA03159 120050929A5347 SEAT TRACK DOUG DC10 DC1010 3022110WP ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25389FE 46623 10" CRACK INSIDE SEAT TRACK FS 1830 TO FS 1840 7.5 RBL. FABRICATED TRACK AND SPLICE AND INSTALLED IAW DC10- SRM 53-70-00-VOL1 FIG 1, SRM 51-31-01 VOL 2 SEE NR N00980 OF WORK ORDER 00029899. 2L73 4F A22WE 20051006001672005100600167NM 2005 10 6 05FDEA03160 120050929A278040174 SWITCH BOEING727 7272S2F 1384O81NM LE FLAPS FAILED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25203FE 22925 GOT AMBER LE FLAP LT ON FLAP RETRACTION AT FLAP 2 DEGREE SETTING. LE FLAP ANNUNCIATOR ON S/O PANEL SHOWED NR 6 IN TRANSIT. FOLLOWED QRH PROCEDURES, NO HELP RETURNED TO DEPARTURE AIRPORT. REMOVED AND REPLACED NR 6 L/E FLAP SWITCH PER MM 27-82-001-4. DURING SWITCH REPLACEMENT FOUND LINKAGE INSTALLED INCORRECTLY PER FIG 401. OPS CHECKED L/E FLAPS AND SLATS PER MM 27-82-001-4. ACFT OK FOR SERVICE. 2L73 4F A3WE 20051006001682005100600168NM 2005 10 6 05FDEA03162 120050929A5320 WEB DOUG MD11 MD11 3023602NM BS 879 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 FWD CARGO COMPT, ALONG STA 879 BETWEEN L52R AND L50L, FRAME ATTACHED CHORD WEB CORRODED. REPAIRED AS PER SRM 53-00-01 FIG.9 VOL.I. MAJOR REPAIR PER GMM 6-2-100. 2L73 4F RTA22WE 20051006001702005100600170EU 2005 10 6 05FDEA03164 120050930A5420 WEB AIRBUS310 A310222 3930315EU NR 2 PYLON CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25445FE 297 NR 2 ENG LWR LT SIDE WEB 28" FROM NOSE COWL. 2L72 4F RTA35EU 20051006001752005100600175SO 2005 10 6 LR7A05113 120050920A53203675841 GUSSET LKHEED382 382G 526414USO FS 921.5 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03406LC 272 4676 DURING SCHEDULED "A" CHECK PER JOB CARD HA1200, FOUND LT FS 921.5 GUSSET CRACKED AT LBL 61.5, , WL 270. REPLACED GUSSET IAW SRM SMP 583 51-10 AND 51-70, LP 17758, ITEM M4. 2H74 4T A1SO 20051006001782005100600178EU 2005 10 6 05FDEA03156 120050928A3297 WIRE HARNESS AIRBUS310 A310203 3930313EU MLG UNKNOWN A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25428FE 248 NR 1 GEAR SYSTEM WOULD NOT RETRACT GEAR AFTER T/O. NR 2 BROUGHT GEAR UP BUT LOST NUMEROUS SYSTEMS AFTERWARDS, SUCH AS A/C PRESSURIZATION, A/C PITOT/HEAT SYSTEM, TRANSPONDER, ETC. REPEAT TROUBLE SHOT PER TSM 32-61-00 SENSORS 55GB FOUND TO BE BAD. NIS IN MEM ORDER SAME. INSP HARNESS TO SENS OR FOUND PLUG AT JUNCTION BOX TO BE LOOSE. REMOVED AND REPLACED HARNESS AS A PRECAUTIONARY ON SYSTEM NR 1. ALSO, AS A PRECAUTIONARY REPLACED RELAY 20GB. OPERATED GEAR, GEAR OPERATED NORMALLY IN BOTH SYSTEMS, A310 MM 32-21-44-4. 2L72 4F RTA35EU 20051006001832005100600183NM 2005 10 6 DL76G050550 120050915A2760 WARNING SYSTEM BOEING767 767332 1382001NM SPOILERS ACTIVATED A DALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO2716065 30199 SPOILER CONFIG WARNING ACTIVATED DURING TAKEOFF. SUBSEQUENT TAKEOFF CONFIG TEST CONFIRMED SAME PREFLT T/O TEST WAS NORMAL. ONLY SHOWED FLAPS, RESET M620 CARD T/O WARN SYS IN CARD FILE P51. OP CHKS NORMAL, ACTUAL DATE OF FLT 17 IS 091605. 2L72 4F RTA1NM 20051006001842005100600184NM 2005 10 6 DL767050551 120050915A5697 WIRE BOEING767 767232 1385132NM COCKPIT WINDOW SHORTED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO27110DL 22222 NOTICED ELECTRICAL PLASTIC ODOR NEAR CAPTAINS GLARESHIELD LIGHT CONTROL PANEL, NEAR LOWER LEFT CORNER OF WINDSCREEN. FOUND L1 WINDOW SENSOR CONNECTION BAD AND SHORTED. REMOVED AND REPLACED L1 WINDOW ASSY PER AMM. 2L72 4F RTA1NM 20051006001852005100600185NM 2005 10 6 DL757050552 120050916A4900 APU BOEING757 757232 1384965NM APU BAY SMOKE A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27683DA33600 27103 LIGHT SMOKE VISABLE IN COCKPIT DURING TAXI IN. SEEMED TO APPEAR AFTER BLEED SOURCE SWITCHED TO APU. UNABLE TO DUPLICATE OR LOCATE FAULT. 2L72 4F RTA2NM 20051006001872005100600187NE 2005 10 6 DL76L050556 220050919A753280217010 BLEED VALVE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE RT ENGINE MALFUNCTIONED A DALAD RETURN TO BLOCK RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SO27189DN 25990 RIGHT ENG BLEED VALVE WILL NOT OPEN. HPSOV DEACT IN CLOSED POSITION. REACTIVATED VALVE BACK TO NORMAL. ENG GRD RUN OK. A/C OK FOR SERVICE. 2L72 4F4 FRTA1NM E24NE 20051003001232005100300123NM 2005 10 3 2005UALA01013 120050923A3350362624 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29193UA 26890 EEL AT 34C AND 4H INOP. REPLACED EEL LAMP. 2L74 4F4 FRTA20WE E24NE 20051003001272005100300127NM 2005 10 3 2005UALA01017 120050922A2120 ODOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE COCKPIT DETECTED A UALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP29523UA 24932 LIGHT SMOKE AND BURNING ODOR IN COCKPIT WITH RIGHT PACK OPERATING OFF APU. ACCOMPLISHED AIR CONDITIONING SYSTEM OIL CONTAMINATION MAINTENANCE PRACTICES PER MM21-00-01. NO SMELLS NOTED. RETURNED AIRCRAFT TO SERVICE. 2L72 4F4 FRTA2NM E17NE 20051003001342005100300134GL 2005 10 3 DL764050562 220050921A7200 ENGINE BOEING767 767432ER 1385134NM GE CF6 CF680C2* GL NR 1 FIRE A DALAE ENGINE SHUTDOWN FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SO27836MH15101 706162 29709 706162 ON CLIMB-OUT OGG AT 3000 FT, NR 1 ENG EGT WENT 997 - N2 OVERSPEED THE A/C SHUTTERED EXCESSIVELY DID NOT HAVE FIRE WARNING BUT C/W ENGINE FIRE OR SEVERE DAMAGE OR SEPARATION CHECKLIST AND FIRED ONE BOTTLE. FLT ATTENDANT REPORTS FLAMES OUT TAIL PIPE, DID SHUT DOWN THE ENG, UNABLE TO DUPLICATE OR FIND FAULT. REPLACED ENGINE. 2L72 4F4 FRTA1NM E23EA 20051003001362005100300136 2005 10 3 DL76L050564 420050922A34164039892904 ALTIMETER BOEING767 767332 1382001NM COCKPIT INOPERATIVE A DALAA UNSCHED LANDING O OTHER CLCLIMB 1 SO27183DN 27110 RTB, DUE CAPT ALT INDICATOR FLAG IN VIEW. AFTER POWER RESET FLAG RETRACTED AND IND OK. AFTER TAKEOFF BRU, CAPT ALTIMETER FLAG IN VIEW FLT DIV TO FRA FOR REPAIRS. FRA MTC REPLACED THE CAPT ALTIMETER. 2L72 4F RTA1NM 20051003001392005100300139NM 2005 10 3 DLM88050569 120050927A2741279001350 MOTOR DOUG MD88 MD88 3023688NM TRIM SYS FAILED A DALAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO27924DL 49711 ACFT PRIMARY TRIM INOP NOSE DOWN AFTER TAKEOFF. REPLACED TRIM MOTOR. 2L72 4F RTA6WE 20051003001552005100300155 2005 10 3 BB05086 420050926A2565140N276217 GIRT BAR BOEING757 757225 1384959NM L1 DOOR DISENGAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19608AU 22204 CLT - THE L1 DOOR ESCAPE SLIDE GIRT BAR WAS FOUND DISENGAGED FROM THE SLIDE BAR. MAINTENANCE INSTALLED THE GIRT BAR. OK FOR SERVICE. 2L72 4F RTA2NM 20051003001622005100300162NM 2005 10 3 SWAA052954 120050927A53156545812 FLOORBEAM BOEING737 7373H4 1384600NM BS 328 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29618WN 28034 DURING SCHEDULED D CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 328, LBL 27, WL 208. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20051003001632005100300163NM 2005 10 3 SWAA052955 120050927A57546573714 SKIN BOEING737 7373L9 1384470NM LT WING SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED 1/2D CHECK, FOUND LT WING NR 3 L/E SLAT T/E LOWER SKIN CRACKED. REMOVED AND REPLACED NR 3 SLAT PER MM. 2L72 4F RTA16WE 20051003001762005100300176EU 2005 10 3 F3LA200500042 120050917A30301663214301 COMPUTER AIRBUSA318 A318111 3940019EU PROBE HEAT FAILED A F3LAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 NM03801FR 4440 1939 FLIGHT CREW REPORTED A BURNING ELECTRICAL ODOR 20 MIN OUT FROM DEN FL390. APPROXIMATELY 20 SEC AFTER ODOR BEGAN, ECAM ANTI-ICE CAPT L & R STAT ILLUMINATED. REPLACED PROBE HEAT COMPUTER PER MM 30-31-34, PB 401. COMPLIED WITH MM 24-00-00-810-823 AND 30-31-20-710-001 AND CHECKED OKAY. 2L72 4F RT 20051004000552005100400055NM 2005 10 4 CALA0500323 120050928A5315BAC1505100246 FLOORBEAM BOEING737 7373T0 1384582NM STA 328 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769333 23571 INSPECTION FOUND MAIN DECK FLOORBEAM CORRODED AT STA 328, RBL 42 TO LBL 35. THE FLOORBEAM SECTION WAS REMOVED AND REPLACED IAW SRM 51-10-02 AND 51-40-02. 2L72 4F RTA16WE 20051004000582005100400058WP 2005 10 4 05FDEA02489 120050816A5711ARB0007502 SPAR CAP DOUG MD10 MD1010F 3022112WP ZONE 600 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25396FE 46630 A TEMPORARY REPAIR (PER S/B DC10-57A137) INSTALLED BY A PREVIOUS OPERATOR ON THE RT REAR SPAR LOWER CAP AT STATION XORS 417.00 REQUIRES REPLACEMENT. E.A. 8-5710-86514 PROVIDES INSTRUCTIONS FOR THE REPLACEMENT OF THE TEMPORARY WITH A PERMANENT REPAIR. THE PERMANENT REPAIR SPLICES IN A NEW SECTION OF LOWER SPAR CAP PER DRAWING SR10570019-7007. LAX (FEDEX) HEAVY MAINTENANCE IS ACCOMPLISHING EA (CLASSIFIED AS MAJOR REPAIR. COMPLIED WITH FEDEX W/C 57X1205 ALI-PT . 2, PT. 4, AND PT. 6. ACCOMPLISHED PERMANENT REPAIR AS PER EA 8-5710-86514 (SEQ #773). 2L73 4F RTA22WE 20051004000602005100400060NM 2005 10 4 PIDA20050147 120050928A532065457835 CHANNEL BOEING737 737228 13844AGNM BS 506 CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 CRACK IN VHF ANTENNA MOUNT BRACKET AND HAT CHANNEL AT BS 506 AND BL 0. REPLACED MOUNT BRACKET AND HAT CHANNEL PER DWG 65-45783 AND SRM 51-10-1. 2L72 4F RTA16WE 20051004000652005100400065NM 2005 10 4 PIDA20050154 120050930A5320 SUPPORT CHANNEL BOEING737 737228 13844AGNM BS 986-1006 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 LOWER SUPPORT CHANNEL FOR AFT DRAIN MAST BETWEEN BS 986 AND BS 1006 BETWEEN STR 24 LT AND STR 25 LT HAS CORROSION. REPLACED HAT CHANNEL PER SRM 51-10-1 AND SRM 51-30-2. 2L72 4F RTA16WE 20051004000752005100400075EA 2005 10 4 SWIA200515589 120050922A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07412SW 7101 EMERGENCY LIGHT BY ENTRY DOOR BURNED OUT. INSTALLED NEW LIGHT ASSY. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051004000822005100400082NM 2005 10 4 DHL2005748522 120050816A5730 SKIN BOEING727 727225 1384077NM RT WING DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 DENT ON LWR SURFACE OF RT WING INBD AFT FLAP 70" FROM OTBD END. REMOVED EXISTING REPAIR AND CUT OUT DAMAGED AREA 8.0 BY 2.25 AND FAB DOUBLER .050 7075 T6 PO 9002507 5.25 BY 11.25 IAW B727 SRM 57-50-4 FIG 5. TREATED AND PRIMED REPAIR PART AND AREA IAW B727 SRM 51-10-2. INSTALLED DOUBLER IAW B727 SRM 57-50-4 FIG 5. 2L73 4F A3WE 20051004000882005100400088NM 2005 10 4 UPS05245533 120050913A3210 TRUNNION BOEING727 72725C 138400HNM RT MLG CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01932UP 19856 INSPECTION TYPE:C ON INSP OF RT TRUNNION, 2 SUSPECT CRACKS DETECTED ON HOLE C I/B FLANGE O/B FACE AND O/B FLANGE I/B FACE. REPAIR CARRIED OUT IAW AAAE EO'S 2005-087-001, 2005-087-006 AND UPS EO 2 B727-5740-20666 APPX F. UPS ENGINEERING FILE NO'S B727-5740-22955-A AND B727-5740-22974-A. 2L73 4F A3WE 20051004000972005100400097NM 2005 10 4 SWAA052974 120050927A3350MS155721 BULB BOEING737 7373T0 1384582NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29684WN 23941 DURING SCHEDULED A2 CHECK, FOUND LT AFT GALLEY EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20051004001072005100400107NM 2005 10 4 05FDEA03124 120050926A5330 SKIN DOUG MD11 MD11 3023602NM BS 635 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 DENT ON FX EXTERIOR SKIN AREA ALONG STA 635, ALONG L-49L. REPAIRED PER SRM 53-20-00 FIG.6 VOL I, EO 1-5100-7-5001. 2L73 4F RTA22WE 20051004001082005100400108EU 2005 10 4 05FDEA03071 120050923A5511 SPAR CAP AIRBUS310 A310203 3930313EU HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25425FE 264 LEFT HORIZONTAL STAB UPPER SPAR CAP IS CORRODED AT NR 23 NUTPLATE COUNTING IB-OUT. 2L72 4F RTA35EU 20051004001112005100400111NM 2005 10 4 05FDEA03077 120050923A5330 DOUBLER BOEING727 727225 1384077NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 CORRSION FWD PIT BETWEEN STA 720D AND STA720E INTERIOR SKIN BETWEEN STR 29L AND STR 29R. REMOVED CORROSION ORIG MAT .100 MAT REM .053 FAB PARTS, LOCATED AND DRILL ALODINE AND PRIME PARTS IAW B727 SRM 53-30-1, 51-10-6, 53-30-3, 53-30-2, 51-10-2, 51-20-1, FIG 2. 2L73 4F A3WE 20051012000242005101200024EA 2005 10 12 COMA0560538 120051009A30402315M1082 WINDSHIELD WIPER CNDAIRCL600 CL6002B19 1900309EA RIGHT BROKEN A COMAA UNSCHED LANDING D INFLIGHT SEPARATION CLCLIMB 1 SO01963CA 7127 FLIGHT 5314 - RIGHT WINDSHIELD WIPER BROKE IN HALF. REPLACED WIPER BLADE ASSEMBLY. 2L72 4F RTA21EA 20051004001722005100400172EA 2005 10 4 SWIA200515606 120050912A5321 STRUCTURE CNDAIRCL600 CL6002B19 1900309EA PRESSURE FLOOR CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07408SW 7055 PRESSURE FLOOR SIDE BOX STRUCTURE, CORROSION ON UPPER DOUBLER, RT SIDE, FS 473.00, ITEM FOUND AT C-CHECK INSPECTION. CORROSION ON UPPER DOUBLER; R/H SIDE; FS 478.00 REMOVED IAW CRJ SRM 53-41-45. BLENDED AREA REPROTECTED IAW CRJ SRM 51-21-16 (CODE A023). MATERIAL REMOVED 0.005; MATERIAL REMAINING 0.075" AND FOUND TO BE WITHIN ALLOWABLE LIMITS IAW CRJ SRM 53-41-45. 2L72 4F RTA21EA 20051004001742005100400174EA 2005 10 4 SWIA200515608 120050912A5312 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA BS 559 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07408SW 7055 RT MLG WHEEL BAY, PRESSURE BULKHEAD WEB IS CRACKED BEHIND AILERON QUADRANT, FS 559.00 - RBL 17.0, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-41-260 REV A & CRJ REO 601R-53-41-251 REV "A" & CRJ REO 601R-53-41-348. 2L72 4F RTA21EA 20051004001762005100400176EA 2005 10 4 SWIA200515610 120050912A5320 POST CNDAIRCL600 CL6002B19 1900309EA BS 559 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07408SW 7055 FUSELAGE, VERT POST IS CRACKED AT LOWER RIVET LOCATION, FS 559.00 - LBL 9.0, I/B AND O/B SIDES, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-41-057 REV NC. 2L72 4F RTA21EA 20051004001782005100400178EA 2005 10 4 SWIA200515612 120050912A5320 POST CNDAIRCL600 CL6002B19 1900309EA BS 409 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07408SW 7055 FUSELAGE, VERTICAL POST IS CRACKED AT LOWER RIVET LOCATION, FS409.0+128 - LBL27.0 - I/B SIDE, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-41-056 REV C . 2L72 4F RTA21EA 20051004001802005100400180EA 2005 10 4 SWIA200515614 120050912A5320 POST CNDAIRCL600 CL6002B19 1900309EA BS 409 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07408SW 7055 FUSELAGE, VERTICAL POST IS CRACKED AT LOWER RIVET LOCATION, FS409.0+128 - LBL36.0 - I/B SIDE, ITEM FOUND AT C-CHECK INSPECTION. DAMAGE REPAIRED IAW CRJ REO 601R-53-41-189 REV NC 2L72 4F RTA21EA 20051004001822005100400182EA 2005 10 4 SWIA200515616 120050912A5411 RIB CNDAIRCL600 CL6002B19 1900309EA RT PYLON CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07408SW 7055 RT PYLON, RIB CRACKED ON LOWER FLANGE AT FS605, ITEM FOUND AT C-CHECK INSPECTION. RIB REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00 . 2L72 4F RTA21EA 20051004001842005100400184EA 2005 10 4 SWIA200515618 120050912A5312 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07408SW 7055 REAR PRESSURE BULKHEAD, AFT SIDE RBL - 36.0 - WL 73.50, CRACKED ON VERTICAL BEAM, FWD RADIUS, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO CRJ REO 601R-53-61-1532. 2L72 4F RTA21EA 20051004001862005100400186WP 2005 10 4 NACA20050021 120050921A7931 WARNING LIGHT DOUG DC6 DC6 3021702WP OIL PRESSURE FALSE INDICATIONA NACAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 AL032907F 533265 LOW OIL PRESSURE LIGHT ON DURING TAKEOFF ROLL. PERFORMED TAKEOFF POWER CHECK PER NAC DC-6 OP MANUAL SECTION 9.20 PT. 5 ON ENGINES 1, 2, 3, AND 4. NO DEFECTS NOTED. DURING TAKEOFF POWER CHECKS OIL PRESSURES WITHIN LIMITS, NO LOW OIL PRESSURE WARN LIGHT ON. FOUND TO BE OK FOR SERVICE. 2L74 4R A781 20051004001882005100400188WP 2005 10 4 ABXA050236 120050907A53205956026255 CHANNEL DOUG DC9 DC933F 302207AWP BS 313 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23930AX 47363 RIGHT FLOOR CHANNEL CORRODED ON UPPER AND LOWER SURFACE, FORWARD OF FRAME FS 313. CORRODED AREAS BEYOND LIMITS. REMOVED BAD SECTION FROM APPROXIMATELY STR 308 - 360. FABRICATED REPLACEMENT SECTION AS NEEDED AND RE-INSTALLED. 2L72 4F A6WE 20051004001892005100400189WP 2005 10 4 ABXA050237 120050907A53119923409501 FRAME DOUG DC9 DC933F 302207AWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23930AX 47363 LEFT FORWARD MAIN FRAME CRACKED AT FORWARD AND AFT FLANGE POINTS G & J. MAIN FRAME REQUIRES REPLACEMENT PER NEA53400100-002-30 AND ES00914. REMOVED AND REPLACED LEFT FORWARD MAIN FRAME IAW EA 53400321-001-3. 2L72 4F A6WE 20051004001902005100400190WP 2005 10 4 ABXA050238 120050909A533059114015 SKIN DOUG DC9 DC933F 302207AWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23930AX 47363 FORWARD FUSELAGE SKIN AFT OF LEFT NOSE WHEEL WELL CRACKED IN SEVERAL PLACES. FABRICATED DOUBLER/INSTALLED IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 20051004001912005100400191EA 2005 10 4 SWIA200515619 120050912A5230 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA CARGO DOOR CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07408SW 7055 CARGO DOOR, INTERCOSTAL IS CRACKED, LOWER AFT CORNER, ITEM FOUND AT C-CHECK INSPECTION. REPLACE INTERCOSTAL IAW CRJ SRM 51-40-11, 51-42-06, 51-23-00, 51-42-21, 51-25-16, 51-42-13. 2L72 4F RTA21EA 20051004001932005100400193CE 2005 10 4 DJFA2005139 120050914A21611173T0635 THERMOSWITCH CESSNA500 560CESSNA 2076750CE CABIN TEMP FAILED E DJFAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA23525CW 5600225 KMDW - KMDW - DURING CLIMB WHILE PASSING 13,000 FT, THE EMERGENCY PRESSURIZATION SYSTEM ENGAGED. THE CREW DONNED THEIR OXYGEN MASKS AND RETURNED THE AIRCRAFT TO KMDW. THE CABIN AIR WAS REPORTED TO BE VERY WARM PRIOR TO THE EMERGENCY PRESSURIZATION SYSTEM ENGAGING. MAINTENANCE REPLACED THE 410 DEGREE SWITCH. BOTH OPERATIONAL AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA22CE 20051004001952005100400195NM 2005 10 4 BMAC050011 120050820A2782651785216 ACTUATOR BOEING727 727222 1384073NM ZONE 500 LEAKING A B16AA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO35349PA 21898 AFTER TAKEOFF, NR 1 SLAT WOULD NOT RETRACT. SYSTEM "A" HYDRAULIC QUANTITY DECREASED TO 0.3 GALLONS. MAINTENANCE REMOVED AND REPLACED NR 1 L/E SLAT ACTUATOR, LEAK AND OPS CHECK GOOD. 2L73 4F A3WE 20051004002072005100400207NM 2005 10 4 SWAA052981 120050929A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 597 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIPS CRACKED AT BS 597, BETWEEN STR 7R TO STR 9R. REMOVED AND REPLACED CLIPS PER SRM. 2L72 4F RTA16WE 20051004002102005100400210NM 2005 10 4 SWAA052984 120050929A53226546554 FRAME BOEING737 7373H4 1384600NM BS 847 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29618WN 28034 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 847, RBL 21. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051004002122005100400212NM 2005 10 4 SWAA052986 120050928A575465C26686 SKIN BOEING737 7373L9 1384470NM RT WING SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED 1/2D CHECK, FOUND RT WING NR 4 L/E SLAT T/E INBD LOWER SKIN CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051004002142005100400214NM 2005 10 4 SWAA052988 120050928A53306545774 SKIN BOEING737 737317 138447PNM BS 767 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 22L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051004002162005100400216NM 2005 10 4 05FDEA03158 120050929A5315 FLOORBEAM BOEING727 727233 138408ANM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25267FE 21673 FLOORBEAM AT STATION 344 BL.0 CORRODED. RERAIRED FLOORBEAM IAW FED EX DWG SR 27-53-007. 2L73 4F RTA3WE 20051005000032005100500003EA 2005 10 5 SWIA200515623 120050929A2797 WIRE CNDAIRCL600 CL6002B19 1900309EA FLT CONTROLS BROKEN A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07913SW 7597 "CPLT ROLL CMD" ADVISORY MESSAGE. CAPTAIN'S AILERONS WORK NORMAL, NO JAM. REPAIRED WIRE CN619A22 AND CN620A22 IAW WDM 20-11-00. OPERATIONAL CHECK GOOD IAW 27-61-20. 2L72 4F RTA21EA 20051005000052005100500005EA 2005 10 5 SWIA200515625 120050924A271010231007 DAMPER CNDAIRCL600 CL6002B19 1900309EA AILERONS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07964SW4784 4784 7868 FLUTTER DAMPER STATUS MSG. INFLIGHT LEFT AILERON. REPLACED LT AILERON FLUTTER DAMPER REF AMM 27-15-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051005000112005100500011NE 2005 10 5 QXEA200501264 220050928A73145008269H PUMP DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE FUEL SYS MALFUNCTIONED A QXEAD RETURN TO BLOCK RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TXTAXI/GRND HDL 1 NM09351PH15556104 490 SEA FLIGHT NR 2176 - AFTER PUSHBACK, POWER LEVERS MOVED TO FLIGHT IDLE, PROP LEVERS MOVED TO MAX TORQUE ON NR 2 ENGINE INDICATED 62 PERCENT AND WARNING HORN SOUNDED. THE TORQUE INDICAITON OCCURED AS THE PROPS WERE COMING OUT OF FEATHER. SECONDS LATER, TORQUE WAS NORMAL. MAINTENANCE REPLACED NR 2 FUEL PUMP AND FUEL CONTROL P/N 3244853-18, S/N C31264T, 11821 TSN 17005 CSN 104.3 TSR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20051005000532005100500053NM 2005 10 5 SWAA053007 120050929A57536546430 SKIN BOEING737 7373H4 1384600NM FOREFLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29631SW 27706 DURING SCHEDULED C4 CHECK, FOUND LT WING INBD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM. 2L72 4F RTA16WE 20051006000072005100600007NM 2005 10 6 USAA051161 120050930A5311 FRAME BOEING737 7374B7 1384702NM BS 887 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 FOUND FRAME CRACKED AT STATION 887 BETWEEN STRINGERS 8R AND 9R. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER IAW SRM 53-10-20B, DEFECT SIZE: .6". 2L72 4F RTA16WE 20051006000082005100600008NM 2005 10 6 USAA051154 120050930A5315 FLOORBEAM BOEING737 7374B7 1384702NM BS 967 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19443US 24842 FOUND FLOORBEAM CORRODED, STA 967 RBL 31. REMOVED DAMAGE AND INSTALLED NEW SPLICE DOUBLER AND CAP ON FLOORBEAM IAW TYPICAL REPAIR 53-10-05B, DEFECT SIZE: 1" BY 6". 2L72 4F RTA16WE 20051006000112005100600011NM 2005 10 6 USAA051163 120051003A53116545771174 FLANGE BOEING737 7374B7 1384702NM BS 559 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 FOUND FUSELAGE STATION 559, STRINGER 13L CRACKED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR ANGLE IAW EA 96912, DEFECT SIZE: .7". 2L72 4F RTA16WE 20051006000122005100600012NM 2005 10 6 SWAA053008 120050930A53306545774 SKIN BOEING737 737301 1384611NM BS 727D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 19L. REPAIRED SKIN PER SWA EA AND SRM. 2L72 4F RTA16WE 20051006000202005100600020NM 2005 10 6 SWAA053016 120051002A3350D71701100 BATTERY PACK BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29747SA 29799 DURING SCHEDULED RON CHECK, FOUND AFT GALLEY EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20051006000272005100600027NM 2005 10 6 AWXA200501144 120050831A53306545766 SKIN BOEING737 7373G7 1384595NM BS 518 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - DURING C18 CHECK DISCOVERED FUSELAGE SKIN CRACKED, 1.5 INCHES IN LENGTH, AT STA 518, STR 12L. TRIMMED OUT DAMAGED SKIN AT BS 518 AND STR 12L IAW AMERICA WEST AIRLINES ER 03-5331-05272-RC1. FABRICATED FILLER, DOUBLER, AND TRIPLER IAW AWA ER NR 03-5331-05272-RC1. INSTALLED FABRICATED REPAIR PARTS IAW AWA ER NR 03-5331-05272-RC1. 2L72 4F RTA16WE 20051006000302005100600030NM 2005 10 6 AWXA200501147 120050906A534069482042 ATTACH ANGLE BOEING737 7373G7 1384595NM BS 360 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - DURING C18 CHECK, DISCOVERED ATTACH ANGLE CRACKED .05 INCHES IN LENGTH AT BS 360, FROM STRINGER 14L TO STRINGER 15L. MAINTENANCE REMOVED ATTACH ANGLE IAW BOEING 737-300 SRM 51-40-02-0G FIG 8. FORMED REPLACEMENT ATTACH ANGLE IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5311-05271-ES1. INSTALLED REPAIR PARTS AT BS 360 FROM STRINGER 14L TO STRINGER 15L IAW AWA ER NR 03-5311-05271-ES1. 2L72 4F RTA16WE 20051006000392005100600039SO 2005 10 6 RAIA00509049 120050929A2797 WIRE EMB 145 EMB145 3260210SO CIRCUIT BREAKER UNSECURE A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03807HK 145119 FLT 3518-PIT-MAIN PITCH TRIM INOP. MAINTENANCE RESECURED WIRE ON PITCH TRIM CIRCUIT BREAKER. 2L72 4F RTT00011AT 20051006000442005100600044NM 2005 10 6 QXEA200501275 120051003A2130 CABIN PRESSURE BOMBDRDHC8 DHC8402 1390042NM MALFUNCTIONED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09408QX 4050 YEG FLIGHT NR 2315, PRESSURIZATION NEVER OCCURRED ABOVE 0.5 PSI DIFFERNTIAL. BLEED AIR OK, MANUAL PRESS WOULD NOT PRESSURIZE EITHER. MTX PERFORMED OPERATIONAL CHECK OF AUTO PRESSURIZATION CONTROL FAULT INDICATION IAW AMM TASK 21-31-00-710-802. OPS CHECKS OK. PERFORMED FUNCTIONAL TEST OF PRESSURIZATION SYSTEM IAW AMM TASK 21-31-00-720-801. OPS CHECK OK. UNABLE TO DUPLICATE FAULT. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051006000452005100600045GL 2005 10 6 DXTA200500994 220050929A75326809125 BLEED VALVE CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL RT ENGINE FAILED E DXTAE ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TXTAXI/GRND HDL 1 GL07918QS 7500223 CAE330466 ON INITIAL POWER UP FOR TAXI, RIGHT ENGINE MADE A LARGE THUMP AND SHUT ITSELF DOWN. REMOVED UPPER, LOWER BLEED AIR VALVES & ACCELERATION BLEED VALVE. INSTALLED NEW VALVES. OPS CKED GOOD. WORK DONE IAW ROLLS ROYCE AE3007C MM CH 75-31-10 & 75-31-15. 2L72 4J4 FRTT00007WITE6CH 20051006000492005100600049NM 2005 10 6 AWXA200501152 120051001A2560P4010021 BATTERY BOEING737 7373G7 1384595NM FLASHLIGHT DISCHARGED A AWXAO OTHER O OTHER TXTAXI/GRND HDL 1 WP28157AW 23779 OAK - EEL - CREW REPORTED ON GROUND FORWARD CABIN EMERGENCY FLASHLIGHT INOP. FORWARD CABIN FLASHLIGHT WAS DEFERRED. WHEN AIRCRAFT ARRIVED IN PHX THE FORWARD FLASHLIGHT BATTERY WAS REPLACED. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20051006000582005100600058EA 2005 10 6 QXEA200501270 120050928A2150 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA NR 2 A/C PACK ILLUMINATED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09610QX 10033 DEN - ON TAXI OUT FOR FLIGHT 4014, RECEIVED A RIGHT PACK CAUTION MESSAGE. RETURNED TO THE GATE. MAINTENANCE FOUND A CONTROL VALVE 2 POSITION DISAGREE. CYCLED NR 2 PACK. NO FAULTS FOUND. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2L72 4F RTA21EA 20051006000632005100600063EU 2005 10 6 2005UALA01023 120050924A3240 B-NUT MESSIER AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE PARKING BREAKS LEAKING A UALAA UNSCHED LANDING KJJFLUID LOSS WARNING INDICATION WARNING INDICATION CRCRUISE 1 WP29409UA 462 YELLOW HYDRAULIC SYSTEM PROBLEM IAD MM FOUND FLUID LEAKING AT BRAKE SHUTOFF VALVE 2579GM LOWER B-NUT FITTING. IAD MM REPLACED PARKING BRAKE SHUTOFF VALVE FIN 2579GM PER MM 32-45-14. NO LEAKS NOTED. SERVICED YELLOW HYD SYSTEM TO FULL. 2L72 4F4 FRTA28NM E40NE 20051006000642005100600064NM 2005 10 6 2005UALA01024 120050924A5753 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE LT WING FOREFLAPWORN A UALAK NONE O OTHER ININSP/MAINT 1 WP29512UA 24809 LT WING INBD FOREFLAP HAS WORN AREA AT UPPER OTBD END. SUPPLEMENTAL DATA UPDATE REMOVED EXISTING DOUBLER, NDT FOR DELAM, INSTALLED BOND REPAIR PER REO-G10990-B AND APPROVED PER 8100-9 DATED 9-23-05. 2L72 4F4 FRTA2NM E17NE 20051006000832005100600083NM 2005 10 6 2005UALA01035 120050924A33501317 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE LT OVERWING BURNED OUT A UALAK NONE L NO TEST ININSP/MAINT 1 WP29121UA 29167 EMERG LT INOP AT LT OVERWING 2ND AFT ASSY. REPLACED LAMP. 2L74 4F4 FRTA20WE E24NE 20051006001042005100600104 2005 10 6 2005UALA01047 420050902A2565D31038201 SLIDE BOEING757 757222 1384956NM PWA 2037 PW2037 NE R1 DOOR RUPTURED A UALAK NONE O OTHER ININSP/MAINT 1 WP29536UA 25156 TUBE RUPTURED DURING OVERPRESSURE (PROOF) TEST. TEST PRESSURE WAS AT 3.41 PSI FOR FIVE MINUTES. INFLATABLE FAILED OVERPRESSURE TEST DUE TO SEAM FAILURE. INFLATABLE WAS BEYOND REPAIR PER CMM. SLIDE WAS SENT TO OEM FOR INFLATABLE REPLACEMENT. 2L72 4F4 FRTA2NM E17NE 20051006001052005100600105NM 2005 10 6 2005UALA01048 120050929A5241 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE GALLEY DOOR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29918UA 25385 FWD SIDE OF DOOR LOWER END FRAME CRACKED AT FASTENER HOLE FWD GALLEY DOOR. ACCOMPLISHED A REPAIR PER MM 51-40-02, FABRICATED AND INSTALLED FRAME SPLICES REF BOEING DRW 69-69430, 2L72 4F4 FRTA16WE E2GL 20051006001062005100600106NM 2005 10 6 2005UALA01049 120050929A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE BS 258 DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29545UA 25323 FUSELAGE EXTERIOR AT BS 258 AND STR 28L HAS 1 DENT. REMOVED DAMAGE AND ACP HFEC NO CRACK INDICATION FABRICATED DOUBLER RPR IAW MM 53-30-95. 2L72 4F4 FRTA2NM E17NE 20051006001132005100600113NM 2005 10 6 2005UALA01056 120050930A3350362624 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29175UA 24382 EMERGENCY EXIT LIGHT AT SEAT 32 HJK INOP. REPLACED LAMP. 2L74 4F4 FRTA20WE E24NE 20051006001162005100600116NM 2005 10 6 DHL2005748750 120050908A5753 SKIN BOEING727 727225 1384077NM LT WING FLAPS DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 L/WING I/B AFT FLAP HAS DENT ON UPPER SURFACE I/B END. CUT OUT DENTED AREA ON LT IMB AFT FLAP APPROX 2" DIA FAB FILLER APPROX 2" DIA AND DOUBLER APPROX 5" DIA FROM .012 2024 T3 PO NR 900534 BONDED FILLER AND DOUBLER CURED CLEANED PRIMED AND EALED IAW B727 SRM 51-40-20-FIG 1. 2L73 4F A3WE 20051006001292005100600129NM 2005 10 6 SWAA053004 120050930A53116520723 FRAME BOEING737 7373H4 1384600NM FWD CARGO CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29618WN 28034 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, AFT BOTTOM DOOR STOP FITTING. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20051006001432005100600143NM 2005 10 6 USAA051178 120051004A575465C26602257A WEDGE BOEING737 7374B7 1384702NM NR 2 SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19433US 24555 FOUND NR 2 SLAT T/E WEDGE O/B END DELAMINATED. REMOVED DAMAGE, INSTALLED REPAIR PIECES IAW SRM 51-70-10, DEFECT SIZE: 3" X 6" DELAMINATION. 2L72 4F RTA16WE 20051006001442005100600144NM 2005 10 6 USAA051179 120051004A575465C26602257A WEDGE BOEING737 7374B7 1384702NM NR 2 SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19433US 24555 FOUND NR 2 SLAT T/E WEDGE INBD END DELAMINATED. REMOVED DAMAGE, INSTALLED REPAIR PIECES IAW SRM 51-70-10, DEFECT SIZE: 3" BY 5" DELAMINATION. 2L72 4F RTA16WE 20051006001512005100600151NM 2005 10 6 DHL2005748752 120050916A5754 CHANNEL BOEING727 727225 1384077NM NR 1 SLAT LOOSE A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 NR 1 SLAT HAS PLAY AT ACTUATOR TO SLAT ATTACH POINT. REMOVED CHANNEL AND BUSHINGS IAW B727 SRM 51-30-2. LOCATED AND DRILLED NEW CHANNEL P/N 65-17327-7 PO NR 5070637 IAW B727 SRM 51-40-5. TREATED AND PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED NEW CHANNEL IAW B727 SRM 51-30-2 AND BUSHINS P/N NAS 538B11P16 PO NR 4175375 IAW B727 OHM 20-50-03. 2L73 4F A3WE 20051006001562005100600156NM 2005 10 6 05FDEA03169 120050930A5730 PANEL BOEING727 727233 138408ANM ZONE 600 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25267FE 21673 RIGHT WING LOWER LEADING EDGE PANEL NR 6212 REQUIRES FABRICATION FOR REPLACEMENT ON-N00505. FABRICATED NEW PANEL IAW BAC DRAWING 65-21661. ALODINED, PRIMED AND PAINTED NEW PANEL IAW FED-EX SRDM SR-57-005B. 2L73 4F RTA3WE 20051006001612005100600161NM 2005 10 6 DHL2005748517 120050816A5730 SKIN BOEING727 727225 1384077NM RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 RT WING UPPER TE PANEL CRACK NOTED FWD OF NR 11 SPOILER HINGE CUT OUT WS 464 AND REAR SPAR. STOP DRILLED CRACK .250 DIA IAW B727 SRM 51-10-1 FAB FROM 7075 T6 .071 6 3/4" BY 4" PO 900989 IAW B727 SRM 57-30-04 FIG10 DETAIL III. TREATED AND PRIMED DOUBLER IAW B727 SRM 51-10-2 AND MM 51-20-0. INSTALLED DOUBLER IAW B727 SRM 57-30-04 FIG 10. 2L73 4F A3WE 20051006001642005100600164NE 2005 10 6 COMA0560525 220050927A72615018T49P01 CARBON SEAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE RT ENGINE LEAKING A COMAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO01938CA 7046 FLIGHT 5809 - RIGHT ENGINE OIL PRESSURE WARNING. REPLACED THE ACCESSORY DRIVE OIL SEALS. 2L72 4F4 FRTA21EA E15NE 20051006001712005100600171EU 2005 10 6 05FDEA03165 120050930A5420 FLANGE AIRBUS310 A310222 3930315EU NR 1 PYLON CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25445FE 297 NR 1 PYLON FLANGE CRACKED BELOW COLD AIR DUCT. 2L72 4F RTA35EU 20051006001792005100600179NM 2005 10 6 DL76G050545 120050914A28227G1018 PRESSURE SWITCH BOEING767 7673P6 1385105NM BOOST PUMP FAILED A DALAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO27152DL 24984 RIGHT CENTER FUEL PUMP PRESSURE LIGHT INOP. REPLACED RIGHT OVERRIDE BOOST PUMP PRESSURE SWITCH. 2L72 4F RTA1NM 20051006001812005100600181NM 2005 10 6 DLM88050547 120050914A3350 FUSE DOUG MD88 MD88 3023688NM EMERGENCY LIGHT BLOWN A DALAK NONE L NO TEST ININSP/MAINT 1 SO27909DL 49540 IRREG/LAST 6 SEATS EMERGENCY LIGHTS INOP. FOUND BAD FUSE IN AFT POWER SUPPLY, REPLACED SAME, OPS NML. 2L72 4F RTA6WE 20051006001882005100600188NM 2005 10 6 DLM88050558 120050919A2140 HEATER DOUG MD88 MD88 3023688NM CARGO OVERHEATED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO27974DL 53242 ON DESCENT INTO ATL AT FL240, F/A REPORTED A STRONG SULFUR ODOR AND A LIGHT HAZE. TURNED OFF GALLEY POWER AND RADIO RACK SWITCH TO VENTURI. THE HAZE AND ODOR DISSIPATED WITHIN 2 MINUTES. REPLACED FWD CARGO HEATER. 2L72 4F RTA6WE 20051006001892005100600189NM 2005 10 6 DL777050560 120050919A3350 FUSE BOEING777 777232 1385232NM EMERGENCY LIGHT BLOWN A DALAK NONE O OTHER ININSP/MAINT 1 SO27862DA 29734 EMERG LIGHTS IN FORWARD TOURIST CLASS SEATS INOP. REPLACED FUSE IN PWR SUPPLY, CKS GOOD. 2L72 4F RTT00001SE 20051006001912005100600191CE 2005 10 6 DXTA200500989 120050928A215073838433 ACM CESSNA750 750 2076810CE LEFT FAULTY E DXTAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL07932QS108 7500032 AFTER LANDING AT TEB, CABIN FILLED WITH SMOKE. OVERHEAD GASPERS ON RIGHT SIDE, TOO HOT TO TOUCH. TAILCONE COMPARTMENT SHOWED FORWARD PAC OIL BOWL BLACK WITH FOAM INSULATION WAS LOOSE ON LEFT SIDE. HEAT FROM OVERHEAD TOILET AREA EXTREMLY HOT. REMOVED AND REPLACED FAULTY ACM WITH AN OVERHAULED UNIT SAME P/N. OPS CHECK AND LEAK CHECK GOOD. WORK PERFORM IAW CE-750 MM CHAP 21-50-00. 2L72 4J RTT00007WI 20051006001942005100600194CE 2005 10 6 DXTA200500987 120050928A3220 LANDING GEAR CESSNA560 560XL 2076702CE NOSE COLLAPSED E DXTAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07699QS 5605199 NOSE GEAR RETRACTED WHILE TAXIING, AIRCRAFT SUSTAINED DAMAGE TO THE NOSE STRUCTURE AREA. DAMAGE TO AIRCRAFT IS BEING TEMPORARILY REPAIRED FOR A ONE TIME FERRY FLIGHT TO ICT. 2L72 4F RTA22CE 20051006001982005100600198CE 2005 10 6 DXTA200500983 120050924A3220 LIMIT SWITCH CESSNA750 750 2076810CE NLG OUT OF ADJUST E DXTAO OTHER E VIBRATION/BUFFET CRCRUISE 1 GL07903QS 7500162 NOSE GEAR MAKES CLUNKING SOUND DURING CRUISE FLIGHT. APPROXIMATELY EVERY 15 MINUTES IT SOUNDS LIKE NOSE GEAR IS BEING RETRACTED. ADJUSTED NOSE GEAR UPLOCK CABLE IAW 750 MM 32-30-06. ADJUSTED NOSE GEAR UPLOCK SWITCH IAW 750 MM 32-30-05, NOSE GEAR OPS CK GOOD. 2L72 4J RTT00007WI 20051006002002005100600200NM 2005 10 6 DXTA200500998 120051003A3230 LANDING GEAR GULSTM200 200 4500308NM RIGHT FAILED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07725QS 105 RIGHT MAIN LANDING GEAR WILL NOT RETRACT. CYCLED GEAR IAW G200 QRH, BUT RT MAIN WOULD NOT COME UP. 2L72 4F RTA53NM 20051006002022005100600202EU 2005 10 6 XN0A1269 120050928A7722 INDICATOR AIRBUS300 A300B4203 3930306EU NR 2 EGT ERRATIC A XN0AD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL23370PC 134 NR 2 EGT ANALOG POINTER AND DIGITAL READOUT ERRATIC. CLEANED AND RESEATED NR 2 EGT INDICATOR PERFORMED ENGINE RUN-UP, OPS CHECKS NORMAL PER MM 77-21-11. 2L72 4F RTA35EU 20051006002032005100600203NM 2005 10 6 AWXA200501132 120050929A2560P2070001101 FLASHLIGHT BOEING757 7572S7 1384962NM CABIN INOPERATIVE A AWXAO OTHER O OTHER TXTAXI/GRND HDL 1 WP28905AW 23567 PHX - EEL - DISCOVERED EMERGENCY FLASHLIGHT AT FLIGHT ATTENDANT STATION 4 NOT DISPLAYING THE RED CHARGING LIGHT AND FORWARD FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BOTH FLASHLIGHT. OPERATIONAL CHECKS GOOD. 2L72 4F RTA2NM 20051006002042005100600204EU 2005 10 6 AWXA200501134 120050904A5347D53472090010 SEAT TRACK AIRBUS320 A320231 3930325EU FR 66 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28634AW 091 SAL - DURING C4 CHECK, DISCOVERED CORROSION ON SEAT RAIL BEAM ASSY AT FR 66, Y1292. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-14 FIG 102. RECEIVED NEW FLOORBEAM AND PREPPED FOR INSTALLATION IAW AIRBUS 320 SRM 51-44-11. INSTALLED FLOORBEAM FROM FR 64 TO FR 66 AND Y1292 IAW AIRBUS A320 SRM 51-42-11. 2L72 4F RTA28NM 20051006002052005100600205 2005 10 6 AWXA200501135 420050905A2565D521155900140 SUPPORT FITTING AIRBUS320 A320231 3930325EU R2 DOOR SLIDE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28634AW 091 SAL - DURING C4 CHECK, DISCOVERED CORROSION ON SLIDE SUPPORT FITTING AT AFT R2 DOOR, BEAM 2 TO BEAM 3. NO ALLOWABLE DAMAGE LIMITS FOUND IN THE AIRBUS 320 SRM. MAINTENANCE REMOVED FITTING IAW AIRBUS 320 SRM 51-72-11. INSTALLED NEW FITTING AT AFT R2 DOOR BETWEEN BEAM 2 AND BEAM 3, IAW AIRBUS 320 SRM 51-42-11. 2L72 4F RTA28NM 20051006002072005100600207NM 2005 10 6 AWXA200501137 120050911A532065479573 SILL BOEING737 7373G7 1384595NM CARGO BAY CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 MCN - DURING C15 CHECK, DISCOVERED CORROSION ON THE AFT CARGO COMPARTMENT DOOR CUTOUT SILL WEB FROM BS 794.5 TO BS 847, STR 25. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-15-1A FIG 101. MAINTENANCE REMOVED AFT CARGO COMPARTMENT DOOR SILL WEB IAW BOEING 737-300 SRM 51-40-02-0G FIG 10. INSTALLED NEW WEB AT AFT CARGO COMPARTMENT CUT OUT SILL FROM BS 794.5 TO BS 847, STR 25L IAW BOEING 737-300 SRM 51-40-02-0G FIG 9 AND FIG 10. 2L72 4F RTA16WE 20051006002082005100600208NM 2005 10 6 AWXA200501138 120050914A532069432332 ATTACH ANGLE BOEING737 7373G7 1384595NM CARGO SILL CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 MCN - DURING C16 CHECK, DISCOVERED CORROSION ON AFT CARGO DOOR SILL WEB ATTACH ANGLE AT BS 847, STR 25R. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-15-1A FIG 101. REMOVED ATTACH ANGLE AT BS 847, STR 25R IAW BOEING 737-300 SRM 51-40-02-0G FIG 10. INSTALLED NEW ATTACH ANGLE AT CARGO DOOR SILL WEB BS 847, STR 25R IAW BOEING 737-300 SRM 51-40-02-0 FIG 12. 2L72 4F RTA16WE 20051006002112005100600211NE 2005 10 6 AALA20050611 220050921A7230 COMPRESSOR DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE LT ENGINE STALLED A AALAA UNSCHED LANDING RY PARTIAL RPM/PWR LOSS ENGINE STOPPAGE CLCLIMB 1 SW21969TW 53619 709796 DFW INFLIGHT DURING CLIMBOUT LEFT HAND ENGINE COMPRESSOR STALLED. ENGINE PRESSURE RATIO WENT BACK TO 1.73. ALL INDICATIONS NORMAL AFTER BRINGING FLIGHT TO IDLE. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND METAL IN TAILPIPE. REPLACED LEFT HAND ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA6WE E9NE 20051006002132005100600213NM 2005 10 6 AALA20050612 120050925A3350 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21658AA 24616 DFW - OVERHEAD EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20051006002162005100600216NM 2005 10 6 AALA20050615 120050925A3350 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21643AA 24601 MIA - EMERGENCY LIGHTS AT SEAT ROWS 25 TO 36 INOPERATIVE. REPLACED BATTERY PACKS FOR EMERGENCY LIGHTS AT ROWS 25 TO 36. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20051006002172005100600217NM 2005 10 6 AALA20050619 120050926A2611033638 BLOWER BOEING757 757223 1384957NM SMOKE DETECTOR INOPERATIVE A AALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW21172AJ 32400 BOS - INFLIGHT CARGO DETECTION AIR STATUS MESSAGE DISPLAYED AFTER TAKEOFF. RETURNED TO BOS AND LANDED WITHOUT INCIDENT. REPLACED PLENUM PRESSURE SWITCH FOR NUMBER 4 SMOKE DETECTION BLOWER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20051006002182005100600218EA 2005 10 6 VTZA200500193 120050924A5315S6830 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 325.5-334-5 CORRODED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27623BR 7192 LBL 27 FLOORBEAM HAS CORROSION AT FS 325.5 THROUGH 334.5. 2L72 4F RTA21EA 20051006002192005100600219EA 2005 10 6 VTZA200500194 120050924A5320S6830 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA BS 325-392 CORRODED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27623BR 7192 RBL 9 FLOOR SUPPORT HAS CORROSION AT FS 325 TO 392. 2L72 4F RTA21EA 20051006002202005100600220EA 2005 10 6 VTZA200500191 120050924A5712601R102328 RIB CNDAIRCL600 CL6002B19 1900309EA RT WING CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27623BR 7192 RIGHT BATT RIB IS CRACKED .750 INCH BETWEEN ATTACHING FASTENERS. 2L72 4F RTA21EA 20051006002212005100600221EA 2005 10 6 VTZA200500192 120050924A5320S6830 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA BS 325-379 CORRODED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27623BR 7192 LBL 9 FLOOR SUPPORT HAS CORROSION AT FS 325 TO 379. 2L72 4F RTA21EA 20051006002222005100600222EA 2005 10 6 VTZA200500195 120050924A5315S6830 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 337 CORRODED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27623BR 7192 RBL 27 FLOORBEAM HAS CORROSION AT FS 337. 2L72 4F RTA21EA 20051006002232005100600223EA 2005 10 6 VTZA200500197 120050924A5315601R35031239 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 621 CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27643BR 7363 LEFT FS 621 FLOOR SUPPORT IS CRACKED 1 INCH IN ANGLE. 2L72 4F RTA21EA 20051006002242005100600224EA 2005 10 6 VTZA200500198 120050924A5712601R107091 RIB CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27643BR 7363 LEFT BATT RIB IS CRACKED 1.5 INCH. 2L72 4F RTA21EA 20051006002272005100600227 2005 10 6 DL76G050561 420050920A3421 INDICATOR BOEING767 767332 1382001NM ATTITUDE MALFUNCTIONED A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO271605 30198 STANDBY ATTITUDE GYRO FLAG IN VIEW. REPLACED STANDBY ATTITUDE INDICATOR. 2L72 4F RTA1NM 20051006002282005100600228 2005 10 6 SB05119 420050923A34174061100901 ADC BOEING737 7373B7 1384580NM COCKPIT FAILED A USAAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 EA19383US3633836338 22956 CLT FLT448 ON TAKEOFF ROLL, WITH FIRST OFFICER FLYING, THE FIRST OFFICER LOST AIRSPEED INDICATOR, ALTIMETER AND VERTICAL SPEED. AFTER TRANSFER OF CONTROLS TO CAPTAIN, THE FLIGHT RETURNED TO FIELD AT CLT. FLIGHT LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE NR 2 DIGITAL AIR DATA COMPUTER. FUNCTIONAL CHECK GOOD. 2L72 4F RTA16WE 20051012000052005101200005NM 2005 10 12 05FDEA03113 120050926A5280 SKIN BOEING727 727233 138408ANM NLG DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25268FE 21674 LT FWD NOSE GEAR DOOR INNER SKIN IS CRACKED 8 INCHES FROM FRONT EDGE, LBL 1 WHEN DOOR IS CLOSED. REPAIRED CRACK IN LH FWD NOSE GEAR DOOR INNER SKIN IAW SRM 51-40-2, AND SRM 52-00-2. 2L73 4F RTA3WE 20051012000072005101200007NM 2005 10 12 05FDEA03258 120051006A5230 STOP FITTING BOEING727 727200 138407ENM CARGO DOOR GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 N00460 FWD CARGO BAY DOOR, FWD 2ND UP FROM BOTTOM STOP FITTING IS GOUGED. INSTALLED NEW FWD CARGO DOOR, FWD 2ND UP FROM THE BOTTOM DOOR STOP FITTING PER SRM 51-30-2. 2L73 4F RTA3WE 20051012000092005101200009NM 2005 10 12 05FDEA03260 120051006A5230 STOP FITTING BOEING727 727200 138407ENM CARGO DOOR GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 FWD CARGO BAY DOOR, FWD LOWER DOOR STOP FITTING IS GOUGED. INSTALLED NEW FWD CARGO DOOR FWD LWR DOOR STOP FITTING PER SRM 51-30-2. 2L73 4F RTA3WE 20051012000112005101200011EU 2005 10 12 05FDEA03047 120050922A5714 SKIN AIRBUS310 A310222 3930315EU CENTER WING CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25448FE 260 CORROSION AT CENTRAL WING UPPER SKIN SURFACE FR 46 Y- 2126. REMOVED/INSTALLED ELEMENTS PER SRM 51-40-21 & 51-40-44. REMOVED CORROSION PER SRM 51-74-10 & 51-29-00 PG. 201. PERFORMED EDDY CURRENTS FOUND "OK". PAINTED PER SRM 51-75-10-08. 2L72 4F RTA35EU 20051012000122005101200012NM 2005 10 12 05FDEA03161 120050929A3610577957 LINE BOEING727 727200 138407ENM FUEL HEAT CRACKED A FDEAO OTHER J WARNING INDICATION CLCLIMB 1 SO25288FE 21850 AT 800' AGL AND 180 KIAS NR 2 FIRE LIGHT ILLUMINATED PERFORMED PHASE 1 AND CHECKLIST LANDED UNEVENTFULLY. 2L73 4F RTA3WE 20051012000132005101200013NM 2005 10 12 05FDEA03331 120051010A5753 RIB BOEING727 727232 1384082NM TE FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 R/W I/B MID FLAP TE RIB IS CRACKED AT IB AFT FLAP PUSHROD CUT OUT. REMOVED CRACKED SECTION & INSTALLED NEW SECTION IAW SRM 51-40-4. 2L73 4F A3WE 20051012000172005101200017NM 2005 10 12 05FDEA03148 120050928A3230859803 PSEU DOUG MD11 MD11 3023602NM COCKPIT MALFUNCTIONED A FDEAO OTHER J WARNING INDICATION CLCLIMB 1 SO25592FE 48550 ALL FOUR LANDING GEAR INDICATED UNSAFE UP UPON GEAR RETRACTION AFTER TAKE OFF BOTH PRIMARY AND SECONDARY INDICATORS. COMPLIED WITH JRH AND CYCLED LANDING GEAR. BOTH PRIMARY AND SECONDARY INDICATORS SHOWED AND LOCKED. CONTINUED TO DESTINATION. R & R PSEU PER MM 31-71-01-2.OPS CHECK NORMAL. AS PER MOCC AND FIM, PSEU INOP. TESTED PSEU, TEST PASSED. PSEU LOGGED MANY FAULTS FROM THE PREVIOUS LEG (FAULTS LOGGED 21, 20, 19, 13, 11, 12) PSEU NOT IN STOCK AT HNL, PARTS ON ORDER FROM LAX. 2L73 4F RTA22WE 20051012000182005101200018NM 2005 10 12 05FDEA03194 120051003A5280 ATTACH BRACKET DOUG MD11 MD11 3023602NM NLG DOOR BROKEN A FDEAA UNSCHED LANDING O OTHER CLCLIMB 1 SO25601FE 48401 DURING CLIMB PASSING 1200FT ACCELLERATING THROUGH 270KTS.LOUD BANG FOLLOWED BY SEVERE VIBRATION. NO ALERTS IN COCKPIT. ON POST FLT, FOUND NLG LEFT DOOR ACTUATION RODS DETACHED FROM DOOR FRAME AND NOSE GEAR CASE. R & R FWD LT NOSE GEAR DOOR AND FWD DOOR DRIVE LINK PER MM 32-23-03-4. R & R AFT LT NOSE GEAR DOOR AND NOSE GEAR SIDE BRACE ATTACH BRACKET PER MM 32-23-05-4. JACKED A/C NOSE PER MM 07-11-00-2 AND PERF.NOSE GEAR OPS CHK. ALL ADJUSTMENTS AND MEASURES ARE WITHIN MM LIMITS. R & R NOSE GEAR WHEEL WELL INSULATION BLANKET PER SRM. 2L73 4F RTA22WE 20051012000192005101200019CE 2005 10 12 DJFA2005141 120050922A2997MS3116F84S CONNECTOR BEECH MU300 400A 1155402CE HYD SYSTEM DEFECTIVE E DJFAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 EA23709TA RK180 CREW REPORTED DURING CRUISE FLT, HYDRAULIC PRESSURE INDICATED 2,000 PSI AND ON RED LINE. WHEN PRESSURE RELIEF SWITCH MOVED, HYDRAULIC PRESSURE INDICATED 100 PSI. DUE TO A LONGER RUNWAY LENGTH AIRCRAFT DIVERTED TO KLGB AND AN EMERGENCY DECLARED. A MANUAL GEAR EXTENSION PERFORMED AND AN UNEVENTFUL NO FLAPS LANDING MADE. EMERGENCY BRAKES WERE USED TO STOP ACFT. MX DISCOVERED SEVERAL AREAS OF NICKED WIRING FOR HYDRAULIC PRESSURE INDICATION. AREAS OF NICKED WIRE REPLACED. A CONNECTOR FOUND TO BE DEFECTIVE AND REPLACED. AIR REMOVED FROM EMERGENCY BRAKING SYS, AND SEVERAL LANDING GEAR EXTENSION AND RETRACTION CYCLES WERE COMPLETED. ALL OPERATIONAL CHECKS WERE NORMAL. THE AIRCRAFT RETURNED TO SERVICE. 2H72 4F RTA16SW 20051012000202005101200020CE 2005 10 12 DJFA2005145 120050930A275045A6103511 CONTROL CABLE BEECH MU300 400A 1155402CE RT TE FLAPS BROKEN E DJFAK NONE O OTHER ININSP/MAINT 1 EA23746TA6787 RK146 DURING A ROUTINE MAINTENANCE VISIT WHILE PERFORMING "A" LEVEL INSPECTION, CORROSION WAS FOUND ON THE RT WING MAIN INBOARD FLAP FOLLOW UP CABLE AT THE END SWEDGE FITTING. WHILE CHECKING THE INTEGRITY IF THE CABLE IN THE FITTING, THE CABLE COMPLETELY SEPERATED FROM THE FITTING. THE RIGHT WING FLAP CABLE WAS REPLACED AND RIGGED. FLAP SYSTEM OPERATIONAL CHECKS WERE GOOD, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4F RTA16SW 20051012000212005101200021EU 2005 10 12 AWXA200501133 120050904A5320 STRUCTURE AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28634AW 091 DURING C4 CHECK DISCOVERED CORROSION ON AFT CORNER SEALING LOCATED IN AFT CARGO COMPARTMENT AT FR 55+19", Y-695 TO Y-900. NO ALLOWABLE DAMAGE FOUND IN THE AIRBUS 320 SRM. MAINTENANCE REMOVED AFT CORNER AT FR 55+19", AND Y-695 TO Y-900 IAW AIRBUS 320 SRM 51-42-11. INSTALLED NEW AFT CORNER IN THE AFT CARGO COMPARTMENT FR 55+19", Y-695 TO Y-900 IAW AIRBUS SRM 51-42-11. CORROSION WAS ALSO FOUND ON THE FWD CORNER SEALING IN THE AFT CARGO COMPARTMENT AT FR 52+12", Y-730. SAME CORRECTIVE ACTION AS WITH THE AFT CORNER SEALING. 2L72 4F RTA28NM 20051012000262005101200026WP 2005 10 12 DHL2005806511 120050822A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP BS 1240 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH87034 46002 AFT CARGO COMPT FLOORBEAM LWR FLANGE CORRODED, STA 1240.000 RBL 30" (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 51-2-1 FIG 1 SHEET 9, TR 51-130. REMOVED FASTENERS IAW SRM 51-1-20D. REMOVED CORROSION FROM FLOORBEAM LWR FLANGE, STA 1240.000 RBL 30" IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. CUT OUT CORRODED SECTION IAW SRM 51-2-1 FIG 1 SHEET 9, TR 51-130. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED REPAIR ANGLE (EXTRUSION 7075T6511 0.125") AND FILLER (AL7075T6511 0.125") IAW SRM 51-2-1 FIG 1 SHEET 9-12, TR 51-130. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS. 2L74 4F RT4A25 20051012000272005101200027NM 2005 10 12 DHL2005788017 120051006A3260 WARNING LIGHT BOEING727 727214 138407RNM MLG ILLUMINATED A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01788AT 21958 GEAR DOOR WARNING LIGHT ILLUMINATED AFTER TAKEOFF WITH GEAR LEVER UP. PERFORMED ABNORMAL AND AFTER CYCLING GEAR RESULTED IN DOORS LIGHT AND LT AND RT GEAR RED DOOR LIGHTS ILLUMINATED. 2L73 4F A3WE 20051012000282005101200028NM 2005 10 12 DHL2005788016 120051004A3231 DOOR BOEING727 727214 138407RNM NLG DOOR OUT OF ADJUST A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01788AT 21958 DURING CLIMBOUT AFTER COMPLETION OF AFTER LANDING CHECKLIST, NOSE GEAR DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT SLOWED BELOW 280 KIAS AND LIGHT WENT OUT. TRANSFER LANDING GEAR DOOR WARNING SYSTEM TO DMI LOG IAW MEL 32-1 CAT C ITEM DMI NR 22691 PLACARD INSTALLED. REF DMI NR 22691-DURING CLIMBOUT AFTER COMPLETION OF AFTER LANDING CHECKLIST, NOSE GEAR DOOR WARNING LIGHT ILLUMINATED. A/C SLOWED TO 280 KIAS LIGHT WENT OUT. ADJUSTED SYNCHRONIZING ROD A - REF MM 32-22-1. ADJUSTED NOSE GEAR DOOR SW IAW MM 32-62-11. NO OTHER DEFECTS NOTED. OK FOR SERVICE. DMI NR 22691 CLEARED. 2L73 4F A3WE 20051012000292005101200029NM 2005 10 12 DHL2005781004 120051003A2740 STABILIZER BOEING727 727227 1384078NM PWA JT8 JT8D17 52049NE HORIZONTAL STAB OUT OF ADJUST A DHLAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO01781DH 21996 AIRCRAFT ROTATES 15 KTS BEFORE VR AND THEN REQUIRES 1.0 UNIT DOWN TRIM TO MAINTAIN V2 +10 ON CLIMBOUT. 2L73 4F4 F A3WE E2EA 20051012000302005101200030NM 2005 10 12 DHL2005788015 120051001A3231 DOOR BOEING727 727214 138407RNM NLG OUT OF RIG A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01788AT 21958 RED NOSE GEAR DOOR LIGHT ON FRONT PANEL & AMBER NOSE GEAR DOOR LIGHT ON SO PANEL ILLUMINATED FLASHED DURING CLIMB. ABNORMAL PROCEDURE COMPLETED CONDITION NORMAL LIGHT EXTINGUISHED W/ GEAR HANDLE UP. DOOR WARNING SYS DEFFERRED IAW MEL 32-1 DMI 22651 CAT C PLACARDS INSTALLED. REF DMI 22651; RED NOSE GEAR DOOR LIGHT ON FRONT PNL AND AMBER NOSE GEAR DOOR LIGHT ON SO PNL ILLUMINATED/ FLASHED DURING CLIMB. LIGHTS EXTINGUISHED W/ GEAR HANDLE UP. FOUND ROD ASSY -G- IN HARD CONTACT WITH WELL STRUCTURE. RIGGED NOSE DOOR SYSTEM IAW BMM 32-22-1. OPS NORMAL. THIS CLEARS DMI 22651, PLACARDS REMOVED. 2L73 4F A3WE 20051012000312005101200031EA 2005 10 12 COMA0560523 120050925A5240 DOOR CNDAIRCL600 CL6002B19 1900309EA SERVICE DOOR OPEN A COMAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 SO01496CA 7791 FLIGHT 5222 - CREW O2 SERVICE DOOR CAME OPEN IN FLIGHT. INSPECTED DOOR AND FOUND SERVICEABLE, CLOSED DOOR. 2L72 4F RTA21EA 20051012000322005101200032EA 2005 10 12 COMA0560543 120051009A2750860D10018ABCD CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01818CA15622190 7408 FLIGHT 5682 - FLAPS FAIL CAUTION. REPLACED THE FECU. 2L72 4F RTA21EA 20051012000332005101200033NM 2005 10 12 AWXA200501197 120050924A575465C266023 SKIN BOEING737 7373S3 1384711NM ZONE 600 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 MCN - MAJOR REPAIR - DURING C18 CHECK DISCOVERED THE NR 5 SLAT LOWER SKIN CRACKED, .750 INCHES IN LENGTH, APPROXIMATELY 39 INCHES FROM INBOARD SIDE, UNDER THE CENTER AUXILIARY TRACK AT SS 163.53. MAINTENANCE REMOVED DAMAGED PART OF SKIN ON THE NR 5 SLAT IAW BOEING 737-300 SRM 57-43-01-02R6 FIG 201. FABRICATED FILLER AND SPLICE PLATE IAW BOEING 737-300 SRM 57-43-01-02R6 FIG 201. INSTALLED FABRICATED REPAIR PARTS ONTO THE NR 5 SLAT LOWER SKIN IAW BOEING 737-300 SRM 57-43-01-02R6 FIG 201. 2L72 4F RTA16WE 20051012000342005101200034NM 2005 10 12 AWXA200501198 120050928A53226545833108 SHEAR TIE BOEING737 7373S3 1384711NM BS 195 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 MCN - MAJOR REPAIR - DURING C18 CHECK DISCOVERED SHEAR TIE CRACKED, 1.1 INCHES IN LENGTH, AT BS 195, WL 207 AND BL 33L. MAINTENANCE REMOVED SHEAR TIE IAW BOEING 737-300 SRM 51-40-02-0G FIG 8. FABRICATED NEW SHEAR TIE IAW BOEING 737-300 SRM 51-40-02-0G FIG 1. INSTALLED SHEAR TIE AT BS 195, WL 207, AND BL 33L IAW BOEING 737-300 SRM 51-40-02-0G FIG 12. 2L72 4F RTA16WE 20051012000352005101200035NM 2005 10 12 AWXA200501199 120050923A53206545834551 CHANNEL BOEING737 7373S3 1384711NM BS 313-327 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 MCN - MAJOR REPAIR - DURING C18 CHECK DISCOVERED CHANNEL CRACKED IN 2 PLACES AT WL 207, BL 47L BS 313 AND BS 327. MAINTENANCE REMOVED DAMAGE CHANNEL AT BS 313 AND BS 327 IAW BOEING 737-300 SRM 51-40-02-0G FIG 8. PREPPED NEW CHANNEL FOR INSTALLATION IAW BOEING 737-300 SRM 51-40-05-0G FIG 4 AND FIG 7. INSTALLED FABRICATED REPAIR PARTS AT WL 207, BL 47L BS 313 AND BS 327 IAW BOEING 737-300 SRM 51-40-02-0G. 2L72 4F RTA16WE 20051012000362005101200036NM 2005 10 12 AWXA200501200 120050921A531165C80735183 FRAME BOEING737 7373S3 1384711NM BS 445 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 MCN - MAJOR REPAIR - DURING C18 CHECK DISCOVERED FORWARD CARGO COMPARTMENT DOOR FRAME CRACKED, 1.5 INCHES IN LENGTH, AT THE UPLOCK AT BS 445 AND STR 24R. MAINTENANCE REMOVED THE CRACKED FRAME IAW BOEING 737-300 SRM 51-40-02-0G FIG 8 AND FIG 11. INSTALLED NEW FRAME ASSEMBLY AT BS 445 AND STR 24R IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 3, 9 AND 12. 2L72 4F RTA16WE 20051012000372005101200037NM 2005 10 12 AWXA200501201 120050923A5313654576722 STRINGER BOEING737 7373S3 1384711NM BS 500C CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 MCN - MAJOR REPAIR - DURING C18 CHECK DISCOVERED STRINGER 16L CRACKED AT BS 500C. MAINTENANCE REMOVED CRACKED END OF STRINGER IAW AMERICA WEST AIRLINES (AWA) ENGINEERING REQUEST (ER) 03-5312-01094-001 FIG 6. FABRICATED FILLER, CHANNEL AND RADIUS FILLER IAW AWA ER 03-5312-01094-001. INSTALLED FABRICATED REPAIR PARTS AT BS 500C STRINGER 16L IAW AWA ER 03-5312-01094-001. 2L72 4F RTA16WE 20051012000382005101200038NM 2005 10 12 AWXA200501202 120050923A53156545812147 FLOORBEAM BOEING737 7373S3 1384711NM BS 328 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 MCN - MAJOR REPAIR - DURING C18 CHECK DISCOVERED GALVANIC CORROSION ON THE TOP OF BEAM AT BS 328, WL 208 AND FROM BL 27R TO BL 33R. CORROSION WAS REMOVED AND FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-10-51-1A1 FIG 101. CUT OUT DAMAGED AREA OF BEAM IAW BOEING 737-300 SRM 53-10-51-2R 5 FIG 201. FABRICATED REPAIR CHORD, ANGLES AND SHIM IAW BOEING 737-300 SRM 53-10-51-2R 5 FIG 201. INSTALLED FABRICATED REPAIR PARTS AT BS 328, WL 208 AND FROM BL 27R TO BL 33R IAW BOEING 737-300 SRM 53-10-51-2R 5 FIG 201. 2L72 4F RTA16WE 20051012000392005101200039NM 2005 10 12 AWXA200501203 120050922A5755654645165 SKIN BOEING737 7373S3 1384711NM ZONE 500 DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 MCN - MAJOR REPAIR - DURING C18 CHECK DISCOVERED DISBOND AREA ON THE LOWER SURFACE OF THE NR 1 SPOILER, APPROXIMATELY 6 INCHES FROM INBOARD EDGE, FROM WBL 398.50L TO WBL 408.50L. MAINTENANCE REMOVED DISBOND AREA AND CORE FROM NR 1 SPOILER LOWER SURFACE IAW BOEING 737-300 SRM 51-70-10-2R3 FIG 201. FABRICATED REPAIR CORE, SEPTUM AND DOUBLER IAW BOEING 737-300 SRM 51-70-10-2R3 FIG 201. BONDED REPAIR PARTS TO THE NR 1 SPOILER LOWER SURFACE FROM WBL 398.50L TO WBL 408.50L IAW BOEING 737-300 SRM 51-70-10-2R3 REPAIR 3 FIG 201. 2L72 4F RTA16WE 20051012000402005101200040NM 2005 10 12 AWXA200501204 120050927A521065512769 STOP FITTING BOEING737 7373S3 1384711NM L1 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 MCN - MAJOR REPAIR - DURING C18 CHECK DISCOVERED L1 DOOR UPPER AFT STOP FITTING ON DOOR CRACKED, 1.0 INCHES IN LENGTH, AT BS 344 AND STR 8L. MAINTENANCE REMOVED CRACKED UPPER AFT STOP FITTING IAW BOEING 737-300 SRM 51-40-02-0G. INSTALLED NEW UPPER AFT STOP FITTING ON THE L1 DOOR AT BS 344 AND STRINGER 8L IAW BOEING 737-300 SRM 51-40-05-0G FIG 2 AND SRM 51-40-02-0G FIGS 8, 9, AND 10. 2L72 4F RTA16WE 20051004001292005100400129EU 2005 10 4 AALA20050629 120050927A3232 ACTUATOR AIRBUS300 A300B4605R 3930308EU NLG DOOR INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2150051 459 JFK INFLIGHT T1683/27SEPTEMBER, NOSE GEAR UNSAFE LIGHTS ILLUMINATED. RETURNED TO JFK AND LANDED WITHOUT INCIDENT. REPLACED RIGHT HAND NOSE LANDING GEAR UPLOCK ACTUATOR AND DOOR CYLINDER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20051004001302005100400130NE 2005 10 4 ARWA20050909 220050910A7532563883 BLEED VALVE DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE NR 2 ENGINE FAILED A ARWAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO19661AV 45969 678976 DURING TAKEOFF AT MAX POWER 1.87 GPR BETWEEN 60 AND 80 KNOTS, HAD A LOUD BANG ON NR 2 ENGINE COMPRESSOR N2 INDICATOR SWUNG VIOLENTLY. ABORTED TAKEOFF AND SECURED NR 2 ENGINE WITH APPROPRIATE CHECKLIST. REMOVED AND REPLACED NR 2 SURGE BLEED VALVE ON ENGINE NR 2 IN ACCORDANCE WITH DC-8 M/M 75-30-3; OPERATIONAL CHECK PERFORMED BY CREW WITNESS, OPERATIONAL CHECK ENGINE RUN ALL PARAMETERS FOUND WITHIN LIMITS IN ACCORDANCE WITH M/M 71-00. 2L74 4F4 F 4A25 1E8 20051004001342005100400134NM 2005 10 4 USAA051151 120050926A5310 SKATE ANGLE BOEING737 7374B7 1384702NM BS 1016 WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 RIGHT SIDE BS 1016 L/E STATION 0.0. FABRICATED AND INSTALLED A NEW SKATE ANGLE IAW TYP REP 53-20-05A, DEFECT SIZE: .5" X 1.3". 2L72 4F RTA16WE 20051004001362005100400136NM 2005 10 4 USAA051149 120050926A5730 SKIN BOEING737 7374B7 1384702NM LT WING CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 LT WING SKIN FWD OF FRONT SPAR O/B SIDE OF PYLON. REMOVED DAMAGED SKIN, FABRICATED AND INSTALLED REPAIR PIECES, DEFECT SIZE: 1". 2L72 4F RTA16WE 20051004001382005100400138NM 2005 10 4 USAA051147 120050926A5320 SILL BOEING737 7374B7 1384702NM BS 967-986 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19443US 24842 ZEE ANGLE AT AFT ENTRANCE DOOR SILL AROUND NUTPLATES BETWEEN STA 967 AND 986. REMOVED DAMAGE AND REINSTALLED FABRICATED REPAIR PARTS IAW SRM 51-70-11, DEFECT SIZE: 20". 2L72 4F RTA16WE 20051004001392005100400139EA 2005 10 4 COMA0570105 120050928A5310CC670341757 CROSSBEAM CNDAIRCL600 CL6002C10 1390015EA FS 280 CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01367CA7872 10069 THE TRANSVERSE BEAM AT FS 280 IS CORRODED FROM LBL 36 TO RBL 36. THE CORRODED TRANSVERSE BEAM WAS REMOVED. A NEW TRANSVERSE BEAM WILL BE INSTALLED IAW REO 670-53-11-047 REV C. 2L72 4F RTA21EA 20051004001412005100400141NM 2005 10 4 AWXA200501124 120050926A3241 WARNING SYSTEM BOEING737 7373Y0 1384671NM AUTO BRAKE ACTIVATED A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28331AW 23747 LAS - ABORTED TAKEOFF - FLT 421 - AIRCRAFT ABORTED TAKEOFF FOR POSSIBLE AUTO BRAKE PROBLEM. SAFETY EVENT REPORT REVEALS THAT TAKE OFF WAS ABORTED, UNDER 60 KNOTS, DUE TO TAKE OFF CONFIGURATION WARNING. CREW NOTICED SPEED BRAKE LEVER NOT FULLY IN DETENT AFTER TAXIING OFF RUNWAY. RE-SET SPEED BRAKE AND ATTEMPTED TAKE OFF AGAIN WITHOUT FURTHER EVENTS. 2L72 4F RTA16WE 20051004001432005100400143NM 2005 10 4 AWXA200501126 120050914A5320654587547 CUSP WEB BOEING737 7373G7 1384595NM BS 310 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - DURING C18 CHECK DISCOVERED 1.1 INCH LONG CRACK ON CUSP WEB AT FASTENER HOLE LOCATED AT BS 310, WL 208 AND BL 60R. MAINTENANCE REMOVED CUSP WEB IAW BOEING 737-300 SRM 51-40-02-0G FIG 8. FABRICATED NEW CUSP WEB IAW BOEING 737-300 SRM 51-40-05-0G FIG 1 AND BAC DWG 65-45875. INSTALLED FABRICATED REPAIR PARTS AT BS 310, WL 208 AND BL 60R IAW BOEING 737-300 SRM 51-40-02-0G FIG 12. 2L72 4F RTA16WE 20051004001452005100400145NM 2005 10 4 AWXA200501128 120050903A53306545409232 SKIN BOEING737 7373G7 1384595NM BS 663 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - DURING C18 CHECK DISCOVERED CRACKED SKIN AT BS 663 JUST FORWARD OF AILERON BELL CRANK AT WL 203, BL 30L. MAINTENANCE CUT OUT AND REMOVED DAMAGED SECTION OF WEB IAW BOEING 737-300 SRM 53-60-51-2R 4. FABRICATED DOUBLER, FILLERS, AND STIFFENER IAW BOEING 737-300 SRM 53-60-51-2R 4. INSTALLED FABRICATED REPAIR PARTS IAW BOEING 737-300 SRM 51-40-02-0G FIG 12 AND FIG 3. 2L72 4F RTA16WE 20051004001472005100400147EA 2005 10 4 COMA0560526 120050928A275011045D100501 COUPLING CNDAIRCL600 CL6002B19 1900309EA TE FLAPS WORN A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01814CA 7387 FLIGHT 5184 - FLAPS FAIL CAUTION. REPLACED NR 1 AND NR 5 FLEX DRIVES ON LT FLAPS. 2L72 4F RTA21EA 20051004001492005100400149EU 2005 10 4 05FDEA03145 120050927A5330 SKIN AIRBUS310 A310203 3930313EU FS 66 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25425FE 264 FS 66 BL 0 HAS SURFACE CORROSION ON SKIN AND FRAME. REMOVED DAMAGED SKIN AND STRINGER FABED NEW PARTS INSTALLED PARTS IAW SRM 53-10-12, 53-10-14, 53- 17-14, AND MM 51-75-10-8. 2L72 4F RTA35EU 20051004001512005100400151CE 2005 10 4 090605N342CS1 120050906A3297 WIRE CESSNA500 550 2076604CE MLG INDICATOR BROKEN E Z5FAL ABORTED APPROACH N FALSE WARNING LDLANDING 1 NE03342CS 5501101 LANDING GEAR WOULD NOT INDICATE DOWN AND LOCKED. PERFORMED IN FLIGHT DIVERSION TO SWF, FACTORY SERVICE CENTER. RECYCLED GEAR WITH NO CHANGE SO COMPLIED WITH CHECKLIST PROCEDURE TO EMERGENCY EXTEND GEAR. STILL NO DOWN INDICATION SO EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED WITHOUT A PROBLEM. MAINTENANCE CORRECTED PROBLEM BY REPAIRING A BROKEN WIRE IN THE WHEEL WELL. 1L72 4F A22CE 20051004001522005100400152NM 2005 10 4 USAA051146 120050926A5340 ATTACH ANGLE BOEING737 7374B7 1384702NM BS 967 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19443US 24842 FOUND ANGLE CRACKED, STA 967 ABOVE AFT ENTRY DOOR. REMOVED DAMAGE AND INSTALLED FABRICATED REPAIR PARTS IAW SRM 53-00-07, DEFECT SIZE: .250". 2L72 4F RTA16WE 20051004001572005100400157EA 2005 10 4 SWIA200515594 120050925A215078279015 ACM CNDAIRCL600 CL6002B19 1900309EA LEFT ODOR A SWIAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM07913SW9272 9272 7597 BURNING SMELL IN COCKPIT AND CABIN. REPLACED LEFT AIR CYCLE MACHINE IAW 21-51-10. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051005000362005100500036 2005 10 5 SA05104 420050930A2565D30664105 SLIDE AIRBUSA319 A319112 3930323EU SERVICE DOOR FAULTY A USAAK NONE J WARNING INDICATION ININSP/MAINT 1 EA19733UW200154248 1205 PIT - A FORWARD SERVICE DOOR SLIDE ECAM WARNING INDICATED INTERMITTENTLY. MAINTENANCE REPLACED THE FORWARD SERVICE DOOR ESCAPE SLIDE. OK FOR SERVICE. 2L72 4F RTA28NM 20051006000042005100600004NM 2005 10 6 USAA051158 120050930A53206545834610 STIFFENER BOEING737 7374B7 1384702NM BS 336 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19443US 24842 FOUND STIFFENER CORRODED FUSELAGE STATION 336 RBL 51 TO 59. REMOVED AND REPLACED STIFFENER IAW SRM 51-40-0, DEFECT SIZE: .75 BY 5". 2L72 4F RTA16WE 20051006000222005100600022NM 2005 10 6 AWXA200501139 120050906A534069489852 CLIP BOEING737 7373G7 1384595NM BS 360 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - DISCOVERED DURING C18 CHECK CLIP CRACKED, .05 INCHES IN LENGTH, AT BS 360, STR 8L ON LOWER SIDE. REMOVED CRACKED CLIP IAW BOEING 737-300 SRM 51-40-02-06 FIG 8. FABRICATED NEW CLIP IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5311-05271-ES1. INSTALLED FABRICATED REPAIR PARTS AT BS 360, STR 8L IAW AWA ER 03-5311-05271-ES1. 2L72 4F RTA16WE 20051006000252005100600025NM 2005 10 6 AWXA200501142 120050906A534065165096 CLIP BOEING737 7373G7 1384595NM BS 351.2 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - DURING C18 CHECK DISCOVERED CLIP CRACKED, .5 INCHES, AT BS 351.20 AND STR 16L. MAINTENANCE REMOVED CRACKED CLIP AT BS 351.20 AND STR 16L IAW BOEING 737-300 SRM 51-40-02-06 FIG 8. FABRICATED AND INSTALLED REPLACEMENT CLIP AT BS 351.20 AND STR 16L IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5311-05271-ES1. 2L72 4F RTA16WE 20051006000592005100600059EA 2005 10 6 QXEA200501273 120050930A2120GG43120223 SPRAYER CNDAIRCL600 CL6002C10 1390015EA RAM AIR MALFUNCTIONED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09605QX 10022 DEN - NOTICEABLE SMELL IN THE CABIN AND COCKPIT WITH THE AIR CONDITIONING PACKS ON. INCREASED IN INTENSITY AT IDLE DESCENT AND WITH THE APU ON. MAINTENANCE REMOVED AND REPLACED THE RAM AIR WATER SPRAYERS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED SERVICE. 2L72 4F RTA21EA 20051006000602005100600060 2005 10 6 QXEA200501278 420051001A2310CDU3933AE04 DISPLAY BOMBDRDHC8 DHC8402 1390042NM COCKPIT INOPERATIVE A QXEAO OTHER O OTHER LDLANDING 1 NM09413QX8782 4060 LAX FLIGHT NR 2389, ON LANDING NR 1 ARCDU SHORTED OUT WITH ELECTRICAL SMOKE. NO DISPLAY ON DU. EMERGENCY VOLUME ON RADIO. MAINTENANCE REMOVED AND REPLACED PILOT'S ARCDU IAW MTC 6238101 WITH SERVICEABLE UNIT. CAT LLL FUNCTIONAL CHECK GOOD. AIRCRAFT REMAIN CAT LLL. PLACARD SHOWS CAT LLL. MTX CONTROL INFORMED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051006000622005100600062NE 2005 10 6 2005UALA01022 220050923A7261 ENGINE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 1 LEAKING A UALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP29434UA 592 V10078 FLIGHT DIVERTED WITH NR 1 ENGINE OIL QUANTITY PROBLEM. DURING FLIGHT, LEFT ENGINE OIL QTY DECREASED TO 1.5 QTS. THE PILOTS DID NOT SHUT DOWN THE ENGINE & KEPT THE ENGINE RUNNING AT IDLE THRUST 62% N1, WITH OIL PRS 120, OIL TEMP 115. NONE OF THE ENGINE PARAMETER EXCEEDED DURING FLIGHT DIVERSION. AFTER LANDING, LINE MECHANICS FOUND EVIDENCE OF OIL LINE & ADEL CLAMP BROKEN. REPLACED OIL LINE 5A9356 & ASSOCIATED "O-RINGS". THE OIL LINE HAD CRACKED AT THE WEAR PAD. VISUAL INDICATION SHOWED THAT THE CLAMP MOVED FROM ITS ORIGINAL LOCATION CAUSING THE WEAR ON THE TUBE. THIS IS AN UNUSUAL EVENT. 2L72 4F4 FRTA28NM E40NE 20051006000862005100600086NM 2005 10 6 2005UALA01038 120050924A335060253 LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE AFT GALLEY TORN A UALAK NONE L NO TEST ININSP/MAINT 1 WP29365UA 24534 EMERGENCY EXIT LIGHTING STRIP TORN NEAR AFT GALLEY. SUPPLEMENTAL DATA UPDATE, REPLACED LIGHT STRIP. 2L72 4F4 FRTA16WE E2GL 20051006000882005100600088NM 2005 10 6 2005UALA01040 120050924A2612 FIRE WARNING BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE APU BAY WILL NOT TEST A UALAK NONE L NO TEST ININSP/MAINT 1 WP29399UA 24674 DURING PREFLT TEST, FIRE BELL DOES NOT RING ON ENG APU TEST OR CARGO TEST. 2L72 4F4 FRTA16WE E2GL 20051006000902005100600090NM 2005 10 6 2005UALA01042 120050927A5330 SKIN BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE BS 1263 DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29664UA 29236 SHARP DENT AND GOUGES IN BELLY SKIN 1 INCH AFT OF STA 1263 FRAME, BETWEEN 39L AND 39R STRINGERS. FUSELAGE DAMAGE AT STA 1264 LOWER CENTERLINE BEYOND LIMITS DEEP DENT AND SEVERAL GOUGES ACROSS SKIN AND FASTENERS. CONTACT DAMAGE TO LOWER AFT BELLY SKIN. REPAIRED PER BOEING SRM. REINSPECTION PER SRM LOADED INTO AMIS PER CF9031. 2L72 4F4 FRTA1NM E24NE 20051006001002005100600100NM 2005 10 6 SWAA053025 120051003A534065C27314 STRINGER CLIP BOEING737 7375H4 138449DNM BS 348 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29506SW 24183 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 348, STR 16L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051006001012005100600101NM 2005 10 6 SWAA053026 120051003A53116546558 FRAME BOEING737 7373H4 1384600NM BS 907 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051006001092005100600109NM 2005 10 6 2005UALA01052 120050930A33501317 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29175UA 24382 EMERGENCY EXIT LIGHT ABOVE DOOR 3 RIGHT INOP. REPLACED LAMP. 2L74 4F4 FRTA20WE E24NE 20051006001152005100600115NM 2005 10 6 USAA051164 120051003A53206545833435 WEB BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 FOUND NLG DOWNLOCK VIEWER FRAME, LT FWD EDGE CRACKED. REMOVED DAMAGED PART, INSTALL NEW PART IAW SRM 51-10-02, DEFECT SIZE: 1.00". 2L72 4F RTA16WE 20051006001272005100600127NM 2005 10 6 SWAA053002 120050930A33506104781 BATTERY PACK BOEING737 7375H4 138449DNM EMERGENCY LIGHT FAULTY A SWAAK NONE O OTHER ININSP/MAINT 1 SW29523SW 26565 DURING SCHEDULED SERVICE CHECK, FOUND BLOWN FUSES IN LT FWD CABIN EMERGENCY LIGHTS BATTERY PACK. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20051006001312005100600131NM 2005 10 6 USAA051165 120051003A5320 ANGLE BOEING737 7374B7 1384702NM BS 747-767 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 FOUND AFT CARGO COMPARTMENT RT TRANSITION ANGLE AT BS 747 TO 767 CORRODED. FABRICATED AND INSTALLED A NEW TRANSITION ANGLE IAW SRM 53-60-53, DEFECT SIZE: 1 BY 12". 2L72 4F RTA16WE 20051006001652005100600165SO 2005 10 6 RAIA00509042 120050927A3350 LIGHT EMB 145 EMB145LR 3260212SO SERVICE DOOR INOPERATIVE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03830HK 145313 PREFLIGHT INSPECTION, EMERGENCY LIGHT OUT AT SERVICE DOOR. MAINTENANCE REPLACED THE EMERGENCY LIGHT. 2L72 4T RTT00011AT 20051006001692005100600169EU 2005 10 6 05FDEA03163 120050930A5420 WEB AIRBUS310 A310222 3930315EU NR 2 PYLON CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25445FE 297 NR 2 PYLON LWR RT SIDEWEB CRACKED 28" FROM NOSE COWL. 2L72 4F RTA35EU 20051006001732005100600173NM 2005 10 6 AWXA200501131 120050929A2560P2070001214 FLASHLIGHT AIRBUSA319 A319132 3930340NM CABIN DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28822AW 1410 PHX - EEL - DURING 4 DAY CHECK, DISCOVERED THE AFT FLIGHT ATTENDANT INBOARD FLASHLIGHT DIM. MAINTENANCE REMOVED AND REPLACED THE AFT FLIGHT ATTENDANT INBOARD EMERGENCY FLASHLIGHT. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA28NM 20051006001742005100600174CE 2005 10 6 DJFA2005142 120050924A3397 TERMINAL BEECH MU300 400A 1155402CE HEATER SWITCH LOOSE E DJFAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA23799TA RK209 KBNA - THE CREW REPORTED THAT SMOKE WAS COMING FROM THE WINDSHIELD HEATER SWITCHES DURING CLIMB-OUT. THE SWITCHES WERE TURNED OFF. AN EMERGENCY WAS DECLARED AND THE CREW DONNED OXYGEN MASKS. THE AIRCRAFT WAS RETURNED TO KBNA AND AN UNEVENTFUL LANDING WAS MADE. MAINTENANCE FOUND A LOOSE TERMINAL SCREW ON THE WING INSPECTION LIGHT SWITCH/CIRCUIT BREAKER. THE SWITCH WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4F RTA16SW 20051006001762005100600176EU 2005 10 6 05FDEA03152 120050928A2910 SOCKET AIRBUS300 A300F4605R 3930327EU HYD SOLENOID CONLEAKING A FDEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO25651FE 728 EN ROUTE AT FL330 RECEIVED ECAM FOR GREEN SYSTEM HYDRAULIC RESV LO. COMPLIED WITH ECAM AND DESELECTED GREEN PUMPS. AFTER NR 1 GREEN PUMP DESELECTED, ENGINE NR 1 GREEN PUMP C/B POPPED AND WOULD NOT ALLOW NR 1 GREEN PUMP TO BE DESELECTED. REFERENCE A300-600 AMM 29-00-00-3 GREEN HYDRAULIC QUANTITY WAS 4 GALS IN WHEEL WELL AT RESERVOIR. PERFORMED INSPECTION OF GREEN SYSTEM. PERFORMED TEST IAW A300-600 AMM 29-11-32, P. BLOCK 401. FOUND NR 1 ENGINE DEPRESS SOLENOID CONNECTOR SOCKET LOOSE ON SOLENOID ASSY. REMOVED AND REPLACED DEPRESSURIZING VALVE IAW MM SUP 29-11-32-4. OP'S CHECKS NORMAL AT THIS TIME. NO LEAKS NOTED, SEE 29-10/9080. 2L72 4F RTA35EU 20051006001772005100600177EU 2005 10 6 05FDEA03155 120050928A7830 CONNECTOR AIRBUS300 A300B4622R 3930312EU THRUST REVERSER DIRTY A FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25720FD 417 ENGINE 2 REV UNLK LT COMES ON ABOVE APPROX 35 N1. ABORTED TO AND RETURNED TO RAMP. REMOVED ELECTRICAL CONNECTORS ON RT AND LT CENTER ACTR SEC LOCK SW AND LT AND RT CENTER ACTUATOR STOW AND DEPLOY SWITCHES. CLEANED AND REINSTALLED ELECTRICAL CONNECTORS. RAN ENGINE TO 47 N1, SYSTEM OPS CHECKS NORMAL PER MM 78-30-00-2. 2L72 4F RTA35EU 20051006001802005100600180NM 2005 10 6 DL73G050546 120050914A3411106145818 PROBE BOEING737 7373L9 1384470NM PITOT SYSTEM OVERHEATED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27231DN 23717 ATB DUE TO FO PITOT TUBE OVERHEATING AND CAUSING INSULATION IN COCKPIT SIDEWALL TO SMOLDER. REPLACED PROBE. 2L72 4F RTA16WE 20051006001862005100600186NM 2005 10 6 DL76K050553 120050917A2721658D1003 ACTUATOR BOEING767 767332 1382001NM RUDDER TRIM INOPERATIVE A DALAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 SO27173DZ 551A 29692 RUDDER TRIM INOP. REPLACED RUDDER TRIM ACTUATOR. 2L72 4F RTA1NM 20051006001902005100600190CE 2005 10 6 DXTA200500991 120050929A3260327 BULB BEECH MU300 400A 1155402CE MLG INDICATOR BURNED E DXTAO OTHER O OTHER APAPPROACH 1 GL07108QS RK382 WITH GEAR DOWN, R MAIN GREEN LIGHT DID NOT ILLUMINATE. BULB TEST CHECKED GOOD. PERFORMED ALTERNATE GEAR EXTENSION. NO RED LIGHT TO INDICATE UNSAFE GEAR ONCE ALTERNATE GEAR EXTENSION CHECKLIST COMPLETED. RESET GEAR EMERGENCY EXTENSION SYSTEM PER HAWKER 400 XP MM 32-30-00. FOUND THREE BULBS IN INDICATION ANNUNCIATOR AND ONE IN GEAR HANDLE FAULTY AND REPLACED ALL FOUR WITH P/N 327 PER HAWKER 400 XP MM 33-10-00. LIGHTS OPS CK GOOD. PERFORMED EXTENSION AND RETRACTION OF GEAR PER HAWKER 400XP MM 32-30-00 WITH NO DEFECTS NOTED. 2H72 4F RTA16SW 20051006001932005100600193CE 2005 10 6 DXTA200500988 120050928A261172P11211102 SMOKE DETECTOR CESSNA650 650 2076802CE FAULTY E DXTAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL07795QS 6507095 DURING THE TAKEOFF ROLL, THE RED "SMOKE DETECT" LIGHT CAME ON TRIGGING THE MASTER WARNING, DURING THE TAXI BACK TO THE FBO THE LIGHT AND MASTER WARNING KEPT ON ILLUMINATING AND FLASHING. TROUBLESHOT SYSTEM AND FOUND SMOKE DETECTOR BOX FAULTY. REMOVED DEFECTIVE SMOKE DETECTOR BOX AND INSTALL NEW CUSTOMER SUPPLIED UNIT IAW CE 650 MM CH 26-12-04. PERFORMED OPERATIONAL CHECK WITH APU AND ENGINES RUNNING AND NO FURTHER DEFECTS WERE NOTED AT THIS TIME. 2L72 4F A9NM 20051006001972005100600197CE 2005 10 6 DXTA200500990 120050929A3240 BRAKE CESSNA500 560CESSNA 2076750CE MLG MALFUNCTIONED E DXTAD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07324QS 5600423 BRAKES VERY SPONGY, ACCUMULATOR GAUGE READS IN YELLOW. BLED BRAKES IAW CE560 M/M 32-42-00 SERVICE ACCUMULATOR. 2L72 4F RTA22CE 20051006002012005100600201CE 2005 10 6 DXTA200500996 120051002A2120 SMOKE RAYTHNDH125 HAWKER800XP 7150012CE CABIN DETECTED E DXTAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL07852QS 258452 WITH APU RUNNING SMOKE WAS COMING FROM THE NR 2 AIR DUCT DUCT TEMP WAS 104 DEG C, ALSO WOULD NOT COOL OFF. RAN ONLY NR 2 ENGINE WITH SAME RESULTS AIRPLANE FILLED WITH SMOKE. ACM INOP. 2L72 4F RTA3EU 20051006002092005100600209NM 2005 10 6 SB05123 120050926A335020131A BATTERY PACK BOEING737 737301 1384611NM EMERGENCY LIGHT DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US 23555 PHL - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT ABOVE THE L2 DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK PER MM 33-51-51. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20051006002122005100600212WP 2005 10 6 AALA20050616 120050926A3350P4010049 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21434AA 49452 LGA - SEAT MOUNTED ESCAPE PATH EMERGENCY LIGHTS AT ROWS 20 TO 32 INOPERATIVE. REPLACED BATTERY PACK IN AFT POSITION AT ROW 20 FOR SEAT MOUNTED ESCAPE PATH EMERGENCY LIGHTS AT ROWS 20 TO 32. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20051012000012005101200001EU 2005 10 12 UPS05145522 120050928A2820 ACTUATOR AIRBUSA300 A300F4622R 3930360EU ISOLATION VALVE INOPERATIVE A IPXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01139UP 0822 FUEL IMBALANCE BETWEEN LT AND RT INNER TANKS. EMERGENCY DECLARED. R & R LT ISOLATION VALVE ACTUATOR IAW AMM 28-22-52-4. R&R'D LEFT ISOLATION VALVE PB SW. SYSTEM CKS GOOD. 2L72 4F RTA35EU 20051012000022005101200002NM 2005 10 12 UPS05M45537 120050929A5610 WINDSHIELD DOUG MD11 MD11F 3023600NM COCKPIT CRACKED A IPXAO OTHER O OTHER NRNOT REPORTED 1 SO01254UP 48406 F/O FRONT WINDOW HAS A CRACK. R & R R1 WINDOW IAW MM 56-11-01-4. 2L73 4F RTA22WE 20051012000032005101200003WP 2005 10 12 UPS05845520 120050927A3411 INDICATOR DOUG DC8 DC871F 302199DWP COCKPIT INOPERATIVE A IPXAA UNSCHED LANDING G MULTIPLE FAILURE CLCLIMB 1 SO01703UP 45939 ALL 3 (CAPT'S, FO'S & ALTERANTE) AIRSPEED INDICATIONS ARE UNRELIABLE. AIR TURN BACK - EMERGENCY DECLARED. REPLACED STANDBY ALT/AIRSPEED INDICATOR PER MM 34-11-02-4. R&R AUXILIARY PITOT STATIC DRAIN. SYSTEM OPS CKS NORMAL IAW AMM 34-12-00-5. 2L74 4F RT4A25 20051012000042005101200004NM 2005 10 12 UPS05645552 120051005A3040141T480150 WINDOW BOEING767 767300 1385204NM COCKPIT SMOKE A IPXABA EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO01324UP 27750 STRONG ODOR & SMOKE IN COCKPIT. CREW DECLARED AN EMERGENCY. T/S - FOUND SMOKE COMING FROM F/O FRONT WINDOW ELECT. CONNECTOR ON AFT LWR CORNER OF WINDOW. F/O FRONT WINDOW REPLACED IAW MM 56-11-01 WINDOW HEATING SYS TEST PERFORMED IAW 30-41-00-5. ALL OPS OK NO EICAS OR INOP IND'S SHOWN ALSO NO MORE SMOKE PRESENT. NOTE: WINDOW HEAT CONTROL UNIT REPLACED. REF LP 372441 ITEM 1. ALSO REPLACED WIRE & CONNECTOR ASSY REFER WDM 30-41-12 SH. 2. 2L72 4F RTA1NM 20051012000152005101200015NM 2005 10 12 05FDEA03135 120050927A5311 FRAME BOEING727 727200 138407ENM BS 1166 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION, STA 1166 RBL 20 TO LBL 20 CORROSION ON BULK CARGO FRAME UPPER FLANGE. REPAIRED FRAME AT BS 1166 RBL 20 TO LBL 20 PER SRM 51-40-3 2L73 4F RTA3WE 20051012000162005101200016NM 2005 10 12 05FDEA03136 120050927A5311 FRAME BOEING727 727200 138407ENM BS 950F DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 MAIN CARGO BAY, MECHANICAL DAMAGE TO FRAME BS 950F BETWEEN STRINGER 4 LT AND 5 LT. REPAIRED FRAME AT BS 950F BETWEEN STR 4L & 5L PER SRM 53-10-4 2L73 4F RTA3WE 20051012000432005101200043NM 2005 10 12 AWXA200501207 120051010A2150 A/C PACK BOEING757 7572S7 1384962NM LEFT TRIPPED A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28902AW 23322 PHX - ABORTED TAKEOFF - FLT 662 - AFTER ADVANCING THROTTLES FOR TAKEOFF THE LEFT PACK AND BLEED TRIPPED OFF. AIRCRAFT TAXIED OFF RUNWAY AND RESET THE LEFT PACK SYSTEM PER MOC. SYSTEMS RETURNED TO NORMAL, AIRCRAFT ATTEMPTED SECOND TAKEOFF WITHOUT FURTHER INCIDENT. 2L72 4F RTA2NM 20051012000452005101200045WP 2005 10 12 AALA20050648 120050929A2597 WIRE DOUG DC9 DC982 3022082WP POWER PORT SHORTED A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21498AA 49736 BNA - INFLIGHT ELECTRICAL SHORT IN POWER PORT SYSTEM AT SEAT 10B. LANDED BNA WITHOUT INCIDENT. REPLACED POWERPORT POWER SUPPLY SEAT TO SEAT CABLE BETWEEN SEAT ROW 10AB AND SEAT ROW 11AB. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051012000472005101200047NM 2005 10 12 AALA20050651 120051004A2150 A/C PACK BOEING757 757223 1384957NM SMOKE A AALAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 SW21665AA 25299 CCS - INFLIGHT AIRCRAFT ARRIVED WITH ACRID SMELL IN COCKPIT AND NUMBER ONE FLIGHT ATTENDANT REPORTED A HAZY SMOKE IN FIRST CLASS CABIN. INSPECTED MAIN CABIN AND FIRST CLASS CABIN AND NO EVIDENCE OF ACRID SMELL. ACCOMPLISHED PACK BURN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20051012000492005101200049EA 2005 10 12 SWIA200515660 120051003A2741 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07913SW 7597 CAPT'S TRIM SWITCH STICKS. REPLACED CAPT'S TRIM SWITCH. OPERATIONAL CHECK GOOD IAW MM 27-40-00. 2L72 4F RTA21EA 20051012000512005101200051EA 2005 10 12 SWIA200515662 120051006A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07439SW7714 7714 7578 SPOILERON FAULT MSG. REPLACED LEFT INBOARD SPOILERON PCU IAW 27-61-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051012000532005101200053EA 2005 10 12 SWIA200515664 120051004A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07453SW 7743 SPOILERONS FAULT. REPLACED RT INBOARD SPOILERON IAW AMM 27-62-01 AND NR 1 SECU IAW AMM 27-61-05. OPERATIONAL CHECK GOOD. P/N 49-164-06, S/N OFF 1205. 2L72 4F RTA21EA 20051012000552005101200055EA 2005 10 12 SWIA200515666 120051002A2760C13045BA04 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA SPOILERS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07705SK307 307 10145 STAB TRIM CHANNEL 2 WOULD NOT ENGAGE. REPLACED SSCU NR 2. OPERATIONAL CHECK GOOD IAW 23-60-00. 2L72 4F RTA21EA 20051012000562005101200056EA 2005 10 12 COMA0560540 120051009A5610NP1393215 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT FAILED A COMAA UNSCHED LANDING O OTHER CLCLIMB 1 SO01984CA145035073 7171 FLIGHT 5196 - PILOT'S WINDSHIELD SHATTERED. REPLACED WINDSHIELD. 2L72 4F RTA21EA 20051012000572005101200057EA 2005 10 12 COMA0560541 120051009A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01805CA 7354 FLIGHT 5093 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2L72 4F RTA21EA 20051012000582005101200058EA 2005 10 12 COMA0560546 120051010A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01818CA185569770 7408 FLIGHT 5505 - FLAPS FAIL CAUTION. REPLACED THE RIGHT BPSU. 2L72 4F RTA21EA 20051012000612005101200061NM 2005 10 12 DHL2005751005 120050928A3240 BRAKE ASSY BOEING727 727264 138408MNM LEFT MALFUNCTIONED A DHLAD RETURN TO BLOCK E VIBRATION/BUFFET TXTAXI/GRND HDL 1 SO01751DH 22982 WHEN LEFT BRAKE APPLIED A/C SHAKES. BLEED NR 1 AND NR 2 BRAKE IAW AMM 32-41. OPS CHECK NORMAL AT THIS TIME. 2L73 4F A3WE 20051012000632005101200063EA 2005 10 12 COMA0560544 120051010A335020131A BATTERY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCHARGED A COMAO OTHER O OTHER NRNOT REPORTED 1 SO01949CA1193029 7080 FLIGHT 5903 - EMERGENCY FLOOR LIGHTNING INOPERABLE ROWS 9 TO 13. REPLACED THE EMERGENCY BATTERY. 2L72 4F RTA21EA 20051012000652005101200065CE 2005 10 12 DXTA200500999 120051004A2720666061312 ACTUATOR CESSNA560 560XL 2076702CE RUDDER INOPERATIVE E DXTAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 GL07624QS2914 5605302 AFTER SETTING T/O POWER ON DEPARTURE ROLL RUDDER PEDALS BECOME VERY STIFF (FEELS LIKE YAW-DAMP IS ON). ABORTED TAKEOFF AT STP AFTER REACHING 60 KIAS. A/C TAXI'S NORMAL AND RUDDER BIAS TEST WAS NORMAL. REMOVED AND INSTALLED A NEW RUDDER BIAS ACTUATOR, OPS CHECK GOOD IAW CE560XL M/M 27020-05. 2L72 4F RTA22CE 20051012000662005101200066NM 2005 10 12 DXTA200501005 120051005A3231 LATCH GULSTM200 200 4500308NM NLG DOOR OUT OF RIG E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07725QS 105 UPON TAKEOFF RIGHT MAIN LANDING GEAR DID NOT RETRACT. SUSPECT GEAR DOOR. ONLY NOT CLOSING FULLY. CYCLED GEAR PER G-200 QRH, GEAR DOOR DID NOT CLOSE FULLY EACH TIME. INSPECTION REVEALED RIGHT FWD MAIN GEAR DOOR LATCH TO BE OUT OF RIG. ALSO FOUND RIGHT GEAR DOOR LINKAGE TO BE MIS-RIGGED. RE-RIGGED FWD LATCH & DOOR LINKS IAW GULFSTREAM G-200 SB 200-36-226 (PREVIOUSLY INSTALLED). OPS CHECKED GOOD. 2L72 4F RTA53NM 20051012000672005101200067 2005 10 12 DXTA200501000 420051004A3414 STATIC PORT CESSNA500 560CESSNA 2076750CE CONTAMINATED E DXTAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL07837QS 5600685 DURING TAKEOFF ROLL THE RIGHT AIRSPEED TAPE ADVANCED PRIOR TO THE LEFT, AFTER LEFT TAPE BEGAN TO ADVANCE IAW ANNUNCIATOR APPEARED ON BOTH PFD'S. TAKEOFF ABORTED AT 65 KNOTS. COULD NOT DUPLICATE DISCREPANCY. FOUND BOTH ALTIMETERS WERE IN AGREEMENT. RAN BOTH AIRSPEEDS UP AND DOWN, BOTH APPEARED IN AGREEMENT. TESTED ALL STATIC PORTS FOR RESTRICTION. NO RESTRICTIONS FOUND. SUSPECT MOISTURE THAT HAS SINCE BEEN DRAINED OUT. WORK PERFORMED PER CESSNA 560MM CHAPTERS 34-11-10 AND 34-11-25. 2L72 4F RTA22CE 20051012000682005101200068CE 2005 10 12 DXTA200501001 120051004A2910S3128E023533E HOSE CESSNA750 750 2076810CE HYD SYSTEM CHAFED E DXTAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL07937QS 7500137 AFTER TAKEOFF, LOST ALL HYDRAULIC FLUID ON THE -B- SYSTEM WITH ASSOCIATED HYD PRESS LOW -B- AND HYD FLUID LOW -B- AMBER CAS MESSAGES. AFTER LANDING, COULD SEE FLUID DRIPPING DOWN FROM THE TAIL. REMOVED LEFT ELEVATOR OUTBOARD PCU HOSE ASSEMBLY DUE TO BEING CHAFED THROUGH. INSTALLED NEW HOSE ASSEMBLY. CHECKED RIGHT ENGINE HYDRAULIC SYSTEM CASE DRAIN FILTER, NO DEFECTS NOTED. PERFORMED SATISFACTORY OPERATIONAL CHECK AND LEAK CHECK. CLEANED AREA AS NEEDED. WORK IAW 20-10-01 AND 29-10-08 OF C750 MAINT MANUAL. 2L72 4J RTT00007WI 20051012000692005101200069CE 2005 10 12 DXTA200501002 120051005A3260 UPLOCK SWITCH BEECH MU300 400A 1155402CE MLG OUT OF ADJUST E DXTAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL07108QS RK382 AFTER GEAR RETRACTION, RED GEAR UNSAFE LIGHT HANDLE STAYS ILLUMINATED, CYCLED GEAR THREE TIMES, SAME RESULT. ADJUSTED LEFT AND RIGHT MAIN LANDING GEAR DOOR UPLOCK SWITCHES IAW BEECHJET 400XP M/M CHAP 32-60-00, PERFORMED LANDING GEAR RETRACTIONS, OPERATIONAL CHECKED SATISFACTORY. SERVICED HYDRAULIC RESERVOIR. 2H72 4F RTA16SW 20051012000702005101200070CE 2005 10 12 DXTA200501003 120051005A3240 ACCUMULATOR CESSNA500 560CESSNA 2076750CE BRAKE SYSTEM LOW E DXTAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 GL07342QS 5600324 WHILE HOLDING SHORT OF THE RUNWAY THE BRAKE PEDALS WENT TO THE FLOOR FOLLOWED BY THE ANTISKID INOP & POWER BRAKE PRESSURE LOW ANNUNCIATORS ILLUMINATING. AFTER ABOUT 60 SECONDS THE ANNUNCIATORS EXTINGUISHED & BOTH CAPTAINS & COPILOTS BRAKES WORKED. SERVICED BRAKE ACCUMULATOR TO PROPER PRECHARGE IAW CE560 MM 12-13-02. LEAK CHECKS GOOD. BRAKE OPS CHECKS GOOD, OK TO CONTINUE. 2L72 4F RTA22CE 20051012000712005101200071CE 2005 10 12 DXTA200501004 120051005A2910 LINE CESSNA560 560XL 2076702CE HYDRAULIC SYS LEAKING E DXTAD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 GL07677QS 5605367 RIGHT BRAKE PEDAL LOOSES PRESSURE DURING BRAKING. BLED LT & RT BRAKE SYSTEM & PERFORMED SYSTEM PRESSURE CHECKS IAW CHAPT 32-43-00 CESSNA 560XL MM. ALL CHECKS GOOD. OPERATED SYSTEM NUMEROUS TIMES AND DID NOT EXPERIENCE PRESSURE LOSS. SERVICE LEVELS GOOD. 2L72 4F RTA22CE 20051012000732005101200073SO 2005 10 12 SWIA200515642 120051003A3350 BULB EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07226SW 120296 WHITE EMERGENCY (FLOOR) LIGHT AT ROW 9 IS INOP. REPLACED BULB AT ROW 9 EMERGENCY LIGHT, OPERATIONAL CHECK OK. 2L72 4T RTA31SO 20051012000742005101200074SO 2005 10 12 SWIA200515643 120051001A27513069001017 ANNUNCIATOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER N FALSE WARNING LDLANDING 1 NM07268UE4696 1861 120207 NUMEROUS FLAP MALFUNCTIONS -DISAGREEMENT ON LANDING APPROACH, CONTROL FAULT ON TAXI. REPLACED FLAP ANNUNCIATOR, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20051012000752005101200075SO 2005 10 12 SWIA200515644 120051001A275012064207615 SELECTOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07220SW6913 6913 120288 DURING CRUISE FLIGHT AT FL220 FLAP CONTROL FAULT O/B FLAP SECOND LIGHT SEGMENT FLASHING. REPLACED FCU AND FLAP CONTROL HANDLE ASSY, OPERATIONAL CHECK GOOD. P/N: 347200-1001, S/N: OFF 0217. 2L72 4T RTA31SO 20051012000762005101200076EA 2005 10 12 SWIA200515645 120050219A5312 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07912SW 7595 CRACK 280 BULKHEAD RBL 9 INBOARD CLIP. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED ANGLE BRACKET PER CRJ200 SRM 51-42-06 AND 51-42-21. 2L72 4F RTA21EA 20051012000772005101200077NM 2005 10 12 UPS05545561 120051003A2910 LINE BOEING757 75724APF 1384969NM LT MAIN GEAR LEAKING A IPXAO OTHER K FLUID LOSS APAPPROACH 1 SO01459UP 25480 INSPECTION TYPE:N/A ON FINAL APPROACH LEFT HYD QTY EICAS MSG APPEARED WITH GEAR DOWN & FLAPS 20. LANDED NORMAL WITH FLAPS 20. CLEARED RUNWAY & UNABLE TO STEER ACFT. STOPPED FOR TOW. REMOVED AND REPLACED LEFT MAIN GEAR DOWNLOCK PRESS LINE AND CARRIED OUT LEFT HYD SYS INSP AND TEST PER MM 29-11-00-2 CONDITION NUMBER 1 ALL CHECKS NORMAL. REPLENISHED LEFT HYD SYS PER MM 12-12-01. ACCORDING TO THE PILOT EVENT REPORT JUST AFTER THE GEAR HIT THE DOWN & LOCKED POS THE LT HYD SYS LET GO COMPLETELY. 2L72 4F RTA2NM 20051012000782005101200078WP 2005 10 12 UPS05845553 120050911A534037540231N FITTING DOUG DC8 DC873F 302199FWP FS 320 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE:C3 CORROSION ON BACK UP FITTING AT STA 320 BETWEEN L33R-L34R. REMOVED BACK UP FITTING AND INSTALLED REPLACEMENT FITTING AND CLIPS IAW SRM 51-1-20D AND 51-3-0. 2L74 4F RT4A25 20051012000792005101200079WP 2005 10 12 UPS05845554 120051005A3350 BATTERY PACK DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT WEAK A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 EMERGENCY EXIT LIGHTS DIM. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK IAW MM 33-50-01. 2L74 4F RT4A25 20051012000802005101200080WP 2005 10 12 UPS05845557 120051006A2560 ESCAPE ROPE DOUG DC8 DC871F 302199DWP COVER DEPLOYED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 CAPT SIDE ESCAPE ROPE DEPLOYED, COVER WON'T STAY ON. STOWED ESCAPE ROPE AND PROPERLY INSTALLED COVER ASSY. OK FOR SERVICE. 2L74 4F RT4A25 20051012000812005101200081CE 2005 10 12 DXTA200501007 120051007A2916 RESERVOIR CESSNA560 560XL 2076702CE HYD SYSTEM LOW E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07668QS 5605268 LANDING GEAR WOULD NOT UPLOCK, UNLOCK LIGHT REMAINED ILLUMINATED FOLLOWED BY HYD PRESS LIGHT. FOUND HYD RESERVOIR LOW. SERVICED RESERVOIR TO FULL. PERFORMED LANDING GEAR FUNCTIONAL CHECK 10 TIMES. ALL OPERATIONS WERE NORMAL. NO FURTHER DEFECTS NOTED. ALL WORK PERFORMED IAW CE 560XL AMM 7-10-00/12-12-00/32-30-00. 2L72 4F RTA22CE 20051012000822005101200082CE 2005 10 12 DXTA200501006 120051007A3260 WARNING LIGHT CESSNA560 560XL 2076702CE NLG ILLUMINATED E DXTAO OTHER J WARNING INDICATION CLCLIMB 1 GL07601QS 5605301 AFTER GEAR RETRACTION NOSE WHEEL INDICATOR LIGHT REMAINED ON. ALL INDICATIONS WERE THAT NOSE GEAR WAS RETRACTED. NORMAL EXTENSION FOLLOWED BY PRECAUTIONARY BLOW DOWN. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20051012000832005101200083CE 2005 10 12 DXTA200501012 120051009A4900 APU RAYTHNDH125 HAWKER800XP 7150012CE APU BAY ODOR E DXTAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL07893QS 258393 TEN SECONDS AFTER STARTING THE APU ON SHORT FINAL, RECEIVED A MASTER WARNING AND SMELLED A HOT ELECTRICAL ODOR AND THE APU DID NOT AUTO SHUTDOWN. SHUTDOWN THE APU MANUALLY, THE ODOR WENT AWAY. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA3EU 20051012000842005101200084WP 2005 10 12 UPS05845558 120051006A3350 BATTERY PACK DOUG DC8 DC871F 302199DWP EMERGENCY LIGHT WEAK A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 EMERGENCY EXIT LIGHTS DIM. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD PER AMM 33-50-01-2. 2L74 4F RT4A25 20051012000852005101200085WP 2005 10 12 UPS05845559 120051007A2697 GROUND WIRE DOUG DC8 DC871F 302199DWP SMOKE DETECTOR SHORTED A IPXAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO01750UP 45950 CARGO SMOKE LIGHT ILLUMINATED - ALL POSITIONS. T/S SYS FOUND & REPAIRED BAD GROUND WIRE 8M OHMS ON SMOKE DETECTOR UNIT NR 1. FOUND & REPAIRED BAD GND WIRE ON SDU NR 3. FOUND AND REPAIRED BAD GNU D WIRE ON SDU NR 5. ALL OTHER SDU GND WIRES CKD GOOD PER WDM 26-11-01 PG 1. SYS OPS OK PER MM 26-10-07-2 2L74 4F RT4A25 20051012000862005101200086EA 2005 10 12 AE0R2005CKXT8 120051007A492038421322 TURBINE HONEYWELL 36150RJ CNDAIRCL600 CL6002B19 1900309EA APU FRACTURED B SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO03947SW3924 1307 P1006 7786 TURBINE ROTOR FRACTURED INTO TWO LARGE PIECES. OPERATOR REPORTED THAT ONE PORTION OF THE TURBINE ROTOR EXITED THE TAILPIPE. VISUAL AND SEM ANALYSIS INDICATES A CASTING FLAW CONTAINING HAFNIUM AND MAGNESIUM (REF SAL ENGINE REPORT ER-400-01-05). 2L72 4F RTA21EA 20051012000872005101200087EA 2005 10 12 SWIA200515646 120050219A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA BS 625 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07912SW 7595 LEFT INTERCOSTAL CLIP CRACKED AT FRAME STA 625; STR 14. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW CLIP PER SRM 51-42-21 PG 17. 2L72 4F RTA21EA 20051012000882005101200088EA 2005 10 12 SWIA200515647 120050219A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA BS 625 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07912SW 7595 RIGHT INTERCOSTAL CLIP CRACKED AT FRAME STA 625. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW INTERCOSTAL CLIP IAW SRM 51-42-21 PG 17. 2L72 4F RTA21EA 20051012000892005101200089EA 2005 10 12 SWIA200515648 120050219A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07912SW 7595 CRACKED CLIP AT FS 280 LBL 9 OUTBOARD. ITEM FOUND AT C-CHECK INSPECTION. CLIP REPLACED IAW SRM 51-42-21. 2L72 4F RTA21EA 20051012000902005101200090EA 2005 10 12 SWIA200515649 120050219A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA ENGINE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07912SW 7595 CRACKED WEB ON ENGINE SUPPORT BEAM LOWER SIDE RIGHT BY CORNER OF ACCESS. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW REO 601R-53-61-358 AND SRM 51-42-06 AND 51-42-20. 2L72 4F RTA21EA 20051012000912005101200091EA 2005 10 12 SWIA200515650 120050219A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA ENGINE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07912SW 7595 CRACKED WEB ON ENGINE SUPPORT BEAM LOWER SIDE LEFT BY CORNER OF ACCESS PNL. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW REO 601R-53-61-358 AND SRM 51-62-06-51-42-20. 2L72 4F RTA21EA 20051012000922005101200092EA 2005 10 12 SWIA200515651 120050219A5312 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07912SW 7595 CRACK 280 BULKHEAD LBL 9 INBOARD CLIP. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE BRACKET PER CRJ200 SRM 51-40-11, CRJ200 SRM 51-42-21 AND 51-42-06. 2L72 4F RTA21EA 20051012000932005101200093EA 2005 10 12 SWIA200515652 120050303A5210 DRAG ANGLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07417SW 7400 PAX DOOR AFT DRAG ANGLE IS CRACKED ABOVE DOOR ASSIST PULLEY. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED DRAG ANGLE AND SPLICES IAW REO 601R-52-11-513. 2L72 4F RTA21EA 20051012000942005101200094EA 2005 10 12 SWIA200515653 120050303A5712 RIB CNDAIRCL600 CL6002B19 1900309EA RT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07417SW 7400 RIGHT BATTERY RIB IN MLG BAY CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW REO 601R-57-51-046. 2L72 4F RTA21EA 20051012000952005101200095EA 2005 10 12 SWIA200515654 120050303A5712 RIB CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07417SW 7400 LEFT BATTERY RIB IN MLG BAY CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW 601R-57-51-046. 2L72 4F RTA21EA 20051012000962005101200096EA 2005 10 12 SWIA200515655 120050303A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07417SW 7400 FLOORBEAM AT FS 280 IS CRACKED AT O/B OF RBL 9.0 AND LBL 9.0. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR ANGLE IAW REO 601R 53-11-136. 2L72 4F RTA21EA 20051012000972005101200097EA 2005 10 12 SWIA200515656 120050303A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07417SW 7400 FLOORBEAM AT FS 280 IS CRACKED AT O/B OF RBL 9.0 AND LBL 9.0. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR ANGLE IAW REO 601R 53-11-136. 2L72 4F RTA21EA 20051012000982005101200098EA 2005 10 12 SWIA200515657 120050303A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07417SW 7400 TRANSVERSE FLOORBEAM AT FS 280 IS CRACKED O/B OF RBL 9.0 AND LBL 9.0. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW 51-42-06 PG 1-20 AND 51-42-21 PG 1-4 AND REO 601R-53-11-171. 2L72 4F RTA21EA 20051012000992005101200099EA 2005 10 12 SWIA200515658 120050424A5712 RIB CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07594SW 7285 LEFT WING WHEEL BIN AREA; FORWARD BATTERY ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW REO 601-57-51-046. 2L72 4F RTA21EA 20051012001002005101200100EA 2005 10 12 SWIA200515659 120050424A5712 RIB CNDAIRCL600 CL6002B19 1900309EA RT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07594SW 7285 RIGHT WING WHEEL BIN AREA; FORWARD BATTERY ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW REO 601R-57-51-046. 2L72 4F RTA21EA 20051012001012005101200101EA 2005 10 12 COMA0560532 120051002A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01958CA 7111 FLIGHT 5093 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2L72 4F RTA21EA 20051012001022005101200102EA 2005 10 12 COMA0570108 120051002A2780 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA SLATS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01331CA 10061 FLIGHT 5316 - SLAT FAIL CAUTION. CLEARED FAULTS FROM COMPUTER. SYSTEM TEST NORMAL. 2L72 4F RTA21EA 20051012001032005101200103EA 2005 10 12 COMA0560533 120051004A7830 THRUST REVERSER CNDAIRCL600 CL6002B19 1900309EA LT ENGINE UNLOCKED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01811CA 7380 FLIGHT 4943 - LEFT ENGINE REVERSER UNLOCK CAUTION. DEFERRED MAINTENANCE ON T/R PER MEL. 2L72 4F RTA21EA 20051012001042005101200104EA 2005 10 12 COMA0560534 120051004A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION CRCRUISE 1 SO01814CA 7387 FLIGHT 5096 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2L72 4F RTA21EA 20051012001052005101200105EA 2005 10 12 COMA0560531 120051002A2410755469E IDG CNDAIRCL600 CL6002B19 1900309EA NR 1 FAILED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01937CA7363 26 7044 FLIGHT 5118 - NR 1 IDG CAUTION. REPLACED THE IDG. 2L72 4F RTA21EA 20051012001062005101200106EA 2005 10 12 COMA0570107 120050926A5347SH670322493 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 374-485 CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01367CA 10069 FLOOR SEAT TRACK RAIL AT LBL 9 FS 374 TO 485 HAS CORROSION. DEPTH IS .025 INCH AROUND BOLT HOLE. INSTALLED NEW SEAT RAIL IAW BRAS EO 601R-53-4713 AND IAW CRJ700 AMM TASK 53-00-49-400-801-A03. 2L72 4F RTA21EA 20051012001072005101200107NM 2005 10 12 CALA0500335 120051007A532065C807351 ANGLE BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2732626 27530 R2 Z-ANGLE CORRODED. REPLACED Z-ANGLE PER SRM 51-40-02. 2L72 4F RTA16WE 20051012001082005101200108NM 2005 10 12 CALA0500336 120051007A53306545774 SKIN BOEING737 7373T0 1384582NM BS 727E CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714325 23455 CRACK IN FUSELAGE SKIN AT STA 727E, STRINGER 18, 2.5 IN. REPAIRED CRACK PER SRM 53-00-01, FIG 201. 2L72 4F RTA16WE 20051012001092005101200109NM 2005 10 12 CALA0500337 120051007A53206552457502 WEB BOEING737 7373T0 1384582NM RT LAVATORY CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769333 23571 AFT RIGHT LAV PAN CORRODED. REPLACED LAV PAN PER SRM 51-40-01. 2L72 4F RTA16WE 20051012001102005101200110NM 2005 10 12 CALA0500338 120051007A53206552457501 WEB BOEING737 7373T0 1384582NM LT LAVATORY CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769333 23571 AFT LEFT LAV PAN CORRODED. REPLACED LAV PAN PER SRM 51-40-01. 2L72 4F RTA16WE 20051012001112005101200111NM 2005 10 12 CALA0500339 120051007A531465C385021 KEELBEAM BOEING737 7373T0 1384582NM BS 500D CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769333 23571 LEFT KEELBEAM CORRODED FWD OF STA 500D. INSTALLED NEW SECTION OF KEEL BEAM PER SRM 53-60-12. 2L72 4F RTA16WE 20051012001132005101200113WP 2005 10 12 ABXA050240 120051005A5330 SKIN DOUG DC9 DC931 3022065WP BS 887-917 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23944AX 47550 DURING ROUTINE LINE MAINTENANCE AT ILN, CRACKS AND BULGING SKIN WAS DISCOVERED NEAR THE LOWER AFT CARGO DOOR CUTOUT. THE INTERIOR OF THE -17 SKIN AND INTERNAL DOUBLERS WERE FOUND TO BE CORRODED AT FS 887 - 917 BETWEEN LONGERONS 26 RIGHT - 29 RIGHT. FABRICATED REPAIR SKIN AND INTERNAL DOUBLERS IAW DC-9 SRM 53-04. 2L72 4F A6WE 20051012001152005101200115NM 2005 10 12 CALA0500342 120051009A531165C352436 FRAME BOEING737 7373T0 1384582NM BS 847 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769333 23571 AFT BAG BIN FLOOR FRAME STA 847 CORRODED AT SHEAR CLIPS. REPLACE FRAME SECTION PER SRM 51-10-02. 2L72 4F RTA16WE 20051012001162005101200116NM 2005 10 12 CALA0500343 120051009A52306547952 SKIN BOEING737 7373T0 1384582NM CARGO DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769333 23571 AFT BAG BIN CARGO DOOR SKIN CRACKED AROUND HANDLE. INSTALLED DOUBLER PER SRM 52-00-01, 51-40-02, 51-20-05, 51-20-01. 2L72 4F RTA16WE 20051012001172005101200117NM 2005 10 12 CALA0500344 120051007A5320 INTERCOSTAL BOEING737 737524 1384721NM BS 340-360 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716648 28909 TOP OF INTERCOSTAL AT STA 340-360, LBL 11 IS CRACKED. INSTALLED ANGLE PER SRM 51-10-02 AND ECRA 5310-03585. 2L72 4F RTA16WE 20051012001192005101200119 2005 10 12 CALA0500346 420051010A256560B1000075 BEARING BOEING757 757224 1384958NM GIRT BAR RODEND BROKEN A CALAK NONE O OTHER ININSP/MAINT 1 SW2717126 27566 L4 DOOR, RIGHT AND LEFT GIRT BAR CRANK PUSHRODS BROKEN. REPLACED PUSHROD RODENDS PER AMM 52-11-25. 2L72 4F RTA2NM 20051012001212005101200121NM 2005 10 12 CALA050341 120050930A531265H6568524 BULKHEAD BOEING737 7373T0 1384582NM BS 1016 DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769333 23571 RIVET HOLE ELONGATED AT AFT PRESSURE BULKHEAD WEB, STA 1016, BL 0. INSTALLED SKIN PER DRAWING 65C28106. 2L72 4F RTA16WE 20051012001232005101200123WP 2005 10 12 UPS05845585 120050920A5330569028U DOUBLER DOUG DC8 DC871F 302199DWP A/C BAY CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE:SP A/C DOUBLER BETWEEN L26R - L31R FS 30 TO 65 INTERNAL DOUBLER IS EXFOLIATED AT FS 55 TO FS 35. REMOVED AND INSTALLED INTERNAL DOUBLER IAW SRM 51-1-21 & 51-3-0. 2L74 4F RT4A25 20051012001252005101200125WP 2005 10 12 UPS05845588 120050930A53404610355 FITTING DOUG DC8 DC871F 302199DWP FS 70 L35L CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE:SP FS 70 L35L END FITTING IS CRACKED BETWEEN ATTACH FASTENER HOLES. REMOVED AND REPLACED END FITTING IAW SRM 51-3-2 AND 51-1-21. 2L74 4F RT4A25 20051012001332005101200133NE 2005 10 12 CALA0500331 220051005A7200 ENGINE BOEING737 737824 13844BZNM CFMINTCFM56 CFM567B26US NE NR 2 MAKING METAL A CALAEA ENGINE SHUTDOWN UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 SW2714230 28794 874285 THE NR 2 ENGINE GAVE OFF A LOUD BOOM AND THE AIRCRAFT SHUDDERED AND YAWED DURING CLIMBOUT OF ORD AT 8,000 FEET. THE NR 2 ENGINE INDICATIONS WERE FROZEN. QRH WAS FOLLOWED AND THE CREW SHUTDOWN THE ENGINE. THE AIRCRAFT WAS RETURNED TO ORD WHERE IT LANDED WITHOUT INCIDENT. INITIAL INSPECTION BY MAINTENANCE FOUND METAL IN THE ENGINE TAILPIPE. THE NR 2 ENGINE WILL BE REMOVED AND REPLACED. THE SDR WILL REMAIN OPEN FOR PART INFORMATION PENDING ENGINEERING INVESTIGATION. ENGINEERING INVESTIGATION CONCLUDED THAT THE PRIMARY CAUSE OF ENGINE FAILURE WAS FAILURE OF THE LPT DUE TO A HOT START ON PREVIOUS ENGINE START. 2L72 4F4 FRTA16WE E00055EN 20051012001342005101200134WP 2005 10 12 DHL2005806512 120050828A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP BS 1320 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH87034 46002 AFT CARGO COMPT FLOORBEAM UPPER FLANGE CORRODED STA 1320.000 RBL 40 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 51-2-1 FIG 1 SHEET 9-12, TR 51-130. REMOVED FASTENERS IAW SRM 51-1-20D. REMOVED CORROSION ON FLOORBEAM UPPER FLANGE STA 1320 RBL 40 IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. CUT OUT CORRODED SECTION IAW SRM 51-2-1 FIG 1 SHEET 9, TR 51-130. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED REPAIR ANGLE AND FILLER IAW SRM 51-2-1. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW SRM 51-2-1 FIG 1 SHEET 9-12, TR 51-130, SRM 51-1-20D, SRM 51-3-1. 2L74 4F RT4A25 20051012001362005101200136NM 2005 10 12 CALA0500326 120051003A5315BAC15181211 FLOORBEAM BOEING737 737724 13844BYNM STA 986.5 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716703 28764 INSPECTION FOUND SEVERAL NUT CLIP HOLES ON FLOORBEAM CORRODED AT STA 986.5, LBL 43-LBL 45. REPAIRED IAW ECRA 5321-01297. 2L72 4F RTA16WE 20051013000022005101300002EU 2005 10 13 10102005A 120051007A24216043T28P05 STATOR SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE ALTERNATOR FAULTY A NSVAC ABORTED TAKEOFF O OTHER TXTAXI/GRND HDL 1 EA27303CE 194 GEE785253 BOTTOM GOVERNOR WILL NOT ENGAGE AND TORQUE REMAINS AT 0 PERCENT WITH POWER LEVER MOVEMENT. PRPM SEEMS TO OPERATE NORMALLY. REMOVED AND REPLACED NR 1 ENG ALT STATOR P/N 6043T28P05, S/N GJA45098, ROTOR P/N 4068T18P02. S/N OFF GJAJ4130, IAW AMM 77-11-10-2. ALSO REMOVED AND REPLACED NR 1 ENGINE TORQUE SENSOR INDICATOR P/N 5066T52G05, IAW AMM 77-13-10-2 & PERFORMED ENGINE RUNS IAW AMM 71-00-00-5, OPS CHECK GOOD ON GROUND. 2L72 4T4 TRTA52EU E8NE 20051013000032005101300003NM 2005 10 13 AWXA200501179 120050919A53476546592 CARGO TRACK BOEING737 7373G7 1384595NM GE CFM56 CFM56* 13802NE BS 945 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 DURING C18 CHECK, DISCOVERED CORROSION ON THE AFT CARGO COMPARTMENT RT TIE DOWN TRACK AT BS 945, BL 13.8R AND WL 158. MAINTENANCE TRIMMED OUT CORROSION ON TIE DOWN TRACK IAW (EO) NR 03-5300-05277-SS2. FABRICATED REPAIR ANGLES AND FILLERS IAW EO 03-5300-05277-SS2. INSTALLED FABRICATED REPAIR PARTS IAW EO 03-5300-05277-SS2. 2L72 4F4 FRTA16WE E2GL 20051013000042005101300004NM 2005 10 13 QXEA200501290 120050925A5320 SILL BOMBDRDHC8 DHC8402 1390042NM CARGO BAY CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09401QX 4031 MCD ENTRYWAY APERTURE LOWER SILL HAS 4 AREAS CORRODED AROUND NUTPLATES, TOP SIDE OF SILL AND UNDERSIDE OF SILL. MAINTENANCE REMOVED MCD THRESHOLD BY DRILLING OUT RIVETS HOLDING THRESHOLD TO LOWER SILL. INSTALLED NEW THRESHOLD FROM STOCK. REF Q400 SRM 51-42-05 FOR RIVET INSTALLATION. 2H72 4T RTA13NM 20051013000052005101300005NM 2005 10 13 CALA0500333 120051006A5220 HANDLE BOEING767 767424ER 1385270NM GE CF6 CF680C2* GL L-3 EMERG EXIT OUT OF ADJUST A CALAK NONE O OTHER ININSP/MAINT 1 SW2766051 29446 THE L-3 EMERGENCY EXIT DOOR INTERIOR HANDLE DOES NOT BACK AGAINST THE DOOR LINING ONCE DURING OPERATIONAL CHECK. THIS WOULD HAVE PREVENTED THE EMERGENCY ESCAPE SLIDE FROM DEPLOYING. PERFORMED TORSION SPRING ADJUSTMENT ON THE TORQUE TUBE IAW MM 52-22-01, PAGE 511. OPERATIONAL CHECKS OF THE EMERGENCY DOOR WERE GOOD. 2L72 4F4 FRTA1NM E23EA 20051013000062005101300006NM 2005 10 13 CALA0500334 120051006A5220 HANDLE BOEING767 767424ER 1385270NM GE CF6 CF680C2* GL R-3 DOOR OUT OF ADJUST A CALAK NONE O OTHER ININSP/MAINT 1 SW2766051 29446 THE R-3 EMERGENCY EXIT DOOR INTERIOR HANDLE DOES NOT BACK AGAINST THE DOOR LINING AT ONCE DURING OPERATIONAL CHECK. THIS WOULD HAVE PREVENTED THE EMERGENCY ESCAPE SLIDE FROM DEPLOYING. PERFORMED TORSION SPRING ADJUSTMENT ON THE TORQUE TUBE IAW MM 52-22-01. PAGE 511. OPERATIONAL CHECKS OF THE EMERGENCY DOOR WERE GOOD. 2L72 4F4 FRTA1NM E23EA 20051013000072005101300007SO 2005 10 13 62310032005 120051003A55111159CSM52025007 RIB GULSTMGV GULFSTREAMGV3980116SO STABILIZER DAMAGED E N93AO OTHER O OTHER NRNOT REPORTED 1 SO13506QS 623 ON POST FLIGHT DAMAGE NOTED TO FAIRING ON OUTSIDE PORTION OF RIGHT STABILIZER LOWER SURFACE. 2L72 4F RTA12EA 20051013000092005101300009NM 2005 10 13 AWXA200501181 120051005A3240C24703003 VALVE AIRBUSA319 A319132 3930340NM PARKING BRAKE MALFUNCTIONED A AWXAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP28822AW 1410 PDURING TAXI OUT, PARKING BRAKE WOULD NOT RELEASE BRAKE PRESSURE. CREW CYCLED CIRCUIT BREAKERS PER MOC WITH NO HELP. MAINTENANCE WENT OUT TO THE AIRCRAFT AND MANUALLY BLED OFF BRAKE PRESSURE. AIRCRAFT TOWED TO GATE WITHOUT FURTHER EVENT. MAINTENANCE PREFORMED BITE CHECK OF THE BSCU'S AND TROUBLESHOT THE BRAKING SYSTEM PER AIRBUS TSM 32-45-00-810-806 FINDING NO FAULTS. MAINTENANCE REMOVED AND REPLACED THE PARKING BRAKE CONTROL VALVE FOR PRECAUTIONARY PURPOSES. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA28NM 20051013000102005101300010NM 2005 10 13 MZZA0500009 120051007A3350D71701100 BATTERY PACK BOEING737 737824 13844BZNM EMERGENCY LIGHT INOPERATIVE A MZZAK NONE O OTHER ININSP/MAINT 1 WP1314228 28792 INSPECTION FOUND EMERGENCY LIGHTS IN RT SIDE Y-CLASS SECTION INOPERATIVE. A TOTAL OF FIVE BATTERY PACKS WERE REPLACED. THE LOCATIONS WERE R-1 OVERHEAD, 5DEF,11DEF, 20DEF, AND R-5 DOOR. OPERATIONAL CHECKS WERE GOOD IAW MM 33-51-00. 2L72 4F RTA16WE 20051013000112005101300011 2005 10 13 HNAA0500087 420051006A2210 CONTROLLER DHAV DHC8 DHC8102 2809003NM ROLL CONTROL JAMMED A HNAAO OTHER F FLT CONT AFFECTED APAPPROACH 1 EA07935HA 142 ROLL CONTROL JAMMED 10 MILES OUT ON APPROACH, CREW SPLIT YOKES IAW CHECK LIST AND CAPTAINS SIDE FREED. FIRST OFFICER STAYED JAMMED UNTIL JUST BEFORE TOUCH DOWN. CAPTAIN CONTROLLED AIRCRAFT WITH SPOILERS. INSPECTED ROLL CONTROL FOR JAMMING AND BINDING OPS NORMAL AND FREE. NO DEFECTS. DISCUSSED PROBLEM WITH CREW AGAIN AND MOST LIKELY RELATED TO AUTO PILOT NOT DISENGAGING. ISSUED MEL 22-1 AUTOPILOT. MORE TO FOLLOW. 2H72 4T RTA13NM 20051013000142005101300014NM 2005 10 13 05FDEA03389 120051011A5320 FLOOR SUPPORT BOEING727 727233 138408ANM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25267FE 21673 FLOOR SUPPORT AT BS 1179 RBL 6 HAS CORROSION. COMPLIED WITH FED EX E7-5320-92564. FUSELAGE FLOOR SUPPORT AT 1176.9 HAS CORROSION. REPAIRED. MAJOR REPAIR 2L73 4F RTA3WE 20051013000162005101300016NM 2005 10 13 SWAA053113 120051010A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM BS 737 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 767, STR 25L. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20051013000172005101300017NM 2005 10 13 SWAA053114 120051010A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051006000092005100600009NM 2005 10 6 USAA051169 120051003A5320 ANGLE BOEING737 7374B7 1384702NM BS 294 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19443US 24842 FOUND SILL Z ANGLE AT STA 294 RIGHT SIDE CORRODED. REPLACED Z ANGLE IAW SRM 51-40-05, DEFECT SIZE: 2" BY 8". 2L72 4F RTA16WE 20051006000152005100600015NM 2005 10 6 SWAA053011 120050930A53306545774 SKIN BOEING737 7373A4 1384585NM BS 765 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 765, STR 22R. REPAIRED SKIN PER BFG ER. 2L72 4F RTA16WE 20051006000172005100600017NM 2005 10 6 SWAA053013 120050930A53306545774 SKIN BOEING737 7373A4 1384585NM BS 764 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 764, STR 4R. REPAIRED SKIN PER BFG ER. 2L72 4F RTA16WE 20051006000332005100600033EU 2005 10 6 AWXA200501150 120050929A3260350F51000 CIRCUIT BOARD AIRBUS320 A320231 3930325EU ANNUNCIATOR FALSE INDICATIONA AWXAO OTHER N FALSE WARNING DEDESCENT 1 WP28645AW 238 LAS - EMERGENCY LANDING - FLT 176 - DURING GEAR EXTENSION RECEIVED NOSE LANDING GEAR LIGHT ON UPPER PANEL, ALL OTHER INDICATIONS WERE NORMAL. CREW PERFORMED FLY BY TO VERIFY GEAR STATUS. AIRCRAFT LANDED IN LAS WITHOUT FURTHER INCIDENT AND TAXIED TO THE GATE. MAINTENANCE REMOVED AND REPLACED CIRCUIT BOARD 9LP IAW AIRBUS MM 33-14-33-04. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA28NM 20051006000342005100600034EU 2005 10 6 AWXA200501151 120051001A3350321431 BATTERY AIRBUS320 A320232 3930326EU EMERGENCY LIGHT MALFUNCTIONED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28648AW 770 PHX - EEL - DURING E-05 CHECK DISCOVERED THE AFT LEFT ESPU FAULTING. MAINTENANCE REMOVED AND REPLACED THE AFT LEFT ESPU BATTERY IAW AIRBUS MM 33-51-38-04. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA28NM 20051006000362005100600036SO 2005 10 6 RAIA00509044 120050929A3397 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT UNSECURE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03817HK 145058 PREFLIGHT INSPECTION, EMERGENCY LIGHT OUT ABOVE LEFT OVERWING EXIT. MAINTENANCE RESEATED CONNECTOR TO LIGHT ASSEMBLY. 2L72 4T RTT00011AT 20051006000552005100600055NM 2005 10 6 AWXA200501158 120050913A552069702514 BOLT BOEING737 7373G7 1384595NM VERTICAL STAB CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 MCN - DURING C15 CHECK, DISCOVERED CORROSION ON LEFT OUTBOARD VERTICAL STABILIZER ATTACH BOLT. NO CORROSION LIMITS ARE AVAILABLE FOR BOLT. MAINTENANCE REMOVED AND REPLACED THE LT OUTBOARD VERTICAL STABILZER ATTACH BOLT IAW BOEING 737-300 AMM 55-30-00-4. 2L72 4F RTA16WE 20051006001022005100600102NM 2005 10 6 SWAA053027 120051002A2750654510751 CONTROL CABLE BOEING737 737317 138447PNM LT WING TE FLAP BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 LT WING INBD T/E FLAP BOOM CABLE BROKEN. REMOVED AND REPLACED BOOM CABLES BC-3 AND BC-4 PER MM. 2L72 4F RTA16WE 20051006001172005100600117NM 2005 10 6 DHL2005748751 120050910A5315 FLOORBEAM BOEING727 727225 1384077NM BS 1166 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 FLOORBEAM AT BS 1166 RBL 36 HAS HEAVY EXFOLIATION ON UPPER FLANGE. CUT OUT DAMAGED AREA OF TOP AFT FLANGE OF FLOORBEAM 4.6 BY 1.0 AT STA 1166 RBL 36 IAW B727 SRM 53-10-8 FIG 8. FAB REPAIR SUPPORT ANGLES FROM 7075T6 PO NR 9001487 22.0 BY 6.0 AND 15.2 BY 6.0 IAW B727 SRM 53-10-8 FIG 8. FAB REPAIR STRIP 7075T6 .125 PO NR 9002067 15.0 BY 2.0 IAW B727 SRM 53-10-8 FIG 8. TREATED AND PRIMED REPAIR PARTS IAW B727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B727 SRM 53-10-8 FIG 8. 2L73 4F A3WE 20051006001192005100600119NM 2005 10 6 SWAA052994 120051002A53306545766 SKIN BOEING737 7373H4 1384600NM BS 450 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING WALKAROUND INSP, FOUND FUSELAGE SKIN CRACKED AT BS 450, STR 17L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051006001202005100600120NM 2005 10 6 SWAA052995 120051002A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 706 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051006001212005100600121NM 2005 10 6 SWAA052996 120051002A55516551524 FITTING BOEING737 7373H4 1384600NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D CHECK, FOUND LT AND RT HORIZONTAL STAB FITTING LUG FACES CORRODED. REPAIRED LUG FACES PER SRM. 2L72 4F RTA16WE 20051006001222005100600122 2005 10 6 SWAA052997 420051001A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29386SW 26601 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20051006001232005100600123NM 2005 10 6 SWAA052998 120051001A3350MS155721 BULB BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29489WN 33855 DURING SCHEDULED MV3 CHECK, FOUND LT AFT LOWER EXTERNAL EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20051006001362005100600136NM 2005 10 6 USAA051172 120051003A5320 ANGLE BOEING737 7374B7 1384702NM BS 290-344 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19443US 24842 FOUND FUSELAGE STA 290-344, CORRODED. DEFECTIVE PART REPLACED WITH IDENTICAL PART, REPLACED Z ANGLE IAW SRM 51-40-05, DEFECT SIZE: 54 BY 2". 2L72 4F RTA16WE 20051006001372005100600137NM 2005 10 6 USAA051173 120051003A5340 CLIP BOEING737 7374B7 1384702NM BS 277 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19443US 24842 FOUND CLIP CRACKED, STA 277 AND STR 15R. MAJOR REPAIR IAW SRM 51-10-02, DEFECT SIZE: .75". 2L72 4F RTA16WE 20051006001392005100600139NM 2005 10 6 USAA051167 120051003A53201128323 WEB BOEING737 7374B7 1384702NM BS 793-847 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 FOUND FUSELAGE STA 793-STA 847 RBL 20, CORRODED. REMOVED AND REPLACED WITH NEW PART IAW SRM 51-10-02, DEFECT SIZE: 1.0". 2L72 4F RTA16WE 20051006001402005100600140EU 2005 10 6 USAA051183 120051004A5347 SEAT TRACK AIRBUSA319 A319112 3930323EU FR 66-68 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19733UW 1205 FOUND CORROSION TASK JA-260-53500; LEVEL 1; RT OTBD SEAT TRACK AT FS 66-68 FLOORBEAM. REMOVED OLD PART AND REPLACED WITH NEW PER SRM 51-72-11, DEFECT SIZE: 2" BY 8". 2L72 4F RTA28NM 20051006001412005100600141NM 2005 10 6 USAA051175 120051004A5314 KEELBEAM BOEING737 7374B7 1384702NM BS 500G CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19443US 24842 FOUND RT KEELBEAM AT AFT SIDE OF STA 500G, CRACKED. FABRICATED ANGLE AND INSTALLED IAW SRM 51-10-02 AND BOEING DWG 69-73527, DEFECT SIZE: 1" CRACK. 2L72 4F RTA16WE 20051006001502005100600150NM 2005 10 6 DHL2005748748 120050902A5311 FRAME BOEING727 727225 1384077NM BS 700 DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 BENT FRAME ABOVE STR 17R AT BS 0. CUT OUT DAMAGED AREA OF FRAME 1 BY 1.5 FAB REPAIR CHANNEL 8 1/2 X 2 1/2 7075 T6 PO 9001777 IAW B727 SRM 53-10-4 FIG 1. TREATED AND PRIMED ALL BARE SURFACES IAW B727 51-10-2. INSTALLED NEW CHANNEL FRAME REPAIR B727 SRM 53-10-4 FIG 1. 2L73 4F A3WE 20051006001542005100600154NM 2005 10 6 05FDEA03167 120050930A5730 PANEL BOEING727 727233 138408ANM ZONE 600 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25267FE 21673 RIGHT WING LOWER LEADING EDGE PANEL NR 6539 REQUIRES FABRICATION FOR REPLACEMENT ON N00158. FABRICATED NEW PANEL IAW BAC DRAWING 65-21674. ALODINED, PRIMED, AND PAINTED IAW B727 SRM 51-10-2. 2L73 4F RTA3WE 20051006001622005100600162NE 2005 10 6 RAIA00509040 220050923A7210310430211 GEARBOX JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114GR 01514NE NR 1 ENGINE SEIZED A RAIAB EMER. DESCENT YJ ENGINE STOPPAGE WARNING INDICATION DEDESCENT 1 CE03567HK17861717 41085 75108 FLT 5436 - SPI - NR 1 ENGINE SHUTDOWN IN FLIGHT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE DUE TO INTERMEDIATE GEAR BOX FAILURE. 2L72 4T4 TRTA41NM E18NE 20051006001722005100600172NM 2005 10 6 AWXA200501130 120050928A3397BR963180 WIRE HARNESS BOEING737 7373Y0 1384671NM EMERGENCY LIGHT INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 PHX - EEL - DURING 8 DAY CHECK, DISCOVERED ROW 16, EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY WIRE HARNESS AT ROW 16. OPERATIONAL TESTS WERE GOOD. 2L72 4F RTA16WE 20051006001822005100600182NM 2005 10 6 DL76G050548 120050915A5754114T41457 BOLT BOEING767 767332 1382001NM NR 5 SLAT BROKEN A DALAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SO271605 30198 LE SLAT ASYM EICAS MSG ON APPROACH. FOUND NR 5 SLAT IB S286 TARGET BOLT BROKEN. REPLACED SAME. 2L72 4F RTA1NM 20051006001922005100600192CE 2005 10 6 DXTA200500992 120050929A212099145232 CONVERTER CESSNA560 560XL 2076702CE OZONE MALFUNCTIONED E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL07650QS 5605150 SHORTLY AFTER TAKEOFF, AN ODOR PERMEATED THE AIRPLANE. SMELLED ELECTRICAL, BUT NO SMOKE OR VISIBLE INDICATIONS. SIC'S EYES WERE BURNING, PIC HAD SLIGHT HEADACHE AFTER LANDING. RAN A/C. INSTANTLY ON START-UP OBSERVED A SOAP OR CRAYON LIKE ODOR. RAN A/C FOR 30 MIN. ODOR GRADUALLY WENT AWAY. NO BURNING EYES OR HEADACHES. OPERATED COCKPIT & CABIN TEMP CONTROL TO FULL HOT & COLD SEVERAL TIMES. ODOR NOT NOTICEABLE AT END OF RUN-UP. NO DEFECTS NOTED IAW 560 XL MM 71-00-04. REMOVED AND REPLACED LEFT AND RT OZONE CONVERTERS PERFORMED FULL POWER RUN LEAK CHECK GOOD. NO ODOR IN COCKPIT OR CABIN NOTED WORK PERFORMED PER CESSNA 560XL CH 27-71-00. 2L72 4F RTA22CE 20051006001962005100600196CE 2005 10 6 DXTA200500985 120050926A21201173T0635 THERMAL SWITCH CESSNA560 560XL 2076702CE CABIN AIR INOPERATIVE E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07675QS2982 5605275 RIGHT AT V1, EMER PRESS CAME ON FOLLOWED BY ACM OVERHEAT, AIR DUCT OVERHEAT ALSO AND SMOKE STARTED TO FILL THE CABIN. - GAINED ACCESS TO THE ACM, VISUALLY INSPECTED INLET DUCTS FOR DEBRIS NONE FOUND, TROUBLE SHOT AND FOUND AIR CONDITIONING TEMP SWITCH INOP. REMOVED AND REPLACED TEMP SWITCH (ST020) WITH A NEW SWITCH, OPS LEAK CHECKS GOOD IAW CE-560XL MM CH 36-11-00. 2L72 4F RTA22CE 20051006001992005100600199CE 2005 10 6 DXTA200500993 120050929A323099146371 MANIFOLD CESSNA750 750 2076810CE MLG FAULTY E DXTAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 GL07930QS4479 7500130 WHILE IN FLIGHT AT 43000 FT, THERE WAS A BANG OR NOISE WITH VIBRATIONS FELT THROUGH THE FLOOR. IT APPEARED TO BE FROM THE NOSE COMPARTMENT, POSSIBLY THE NOSE GEAR. REMOVED AND REPLACED GEAR MANIFOLD IAW CE750 M/M CHAPTER 32-30-02. SYSTEM OPS CHECK GOOD. 2L72 4J RTT00007WI 20051006002142005100600214WP 2005 10 6 AALA20050613 120050924A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21406A 49317 SFO - OVERWING EMERGENCY LIGHTS AT FORWARD HATCH LEFT AND RIGHT HAND INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING EMERGENCY LIGHTS AT FORWARD HATCH LEFT AND RIGHT HAND. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051006002262005100600226EA 2005 10 6 VTZA200500196 120050924A5315601R35031239 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 621 CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27643BR 7363 RIGHT FS 621 FLOOR SUPPORT IS CRACKED AT 1 INCH IN ANGLE. 2L72 4F RTA21EA 20051012000062005101200006NM 2005 10 12 05FDEA03254 120051006A5230 FRAME BOEING727 727200 138407ENM CARGO DOOR DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 FWD CARGO BAY DOOR LOWER CHORD IS DENTED AND CHAFED FROM CENTER TO AFT CORNER. REMOVED AND REPLACED LOWER CENTER CHORD IAW SRM 51-30-2. 2L73 4F RTA3WE 20051012000082005101200008NM 2005 10 12 05FDEA03259 120051006A5230 STOP FITTING BOEING727 727200 138407ENM CARGO DOOR GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 FWD CARGO BAY DOOR, AFT LOWER DOOR STOP FITTING IS GOUGED. INSTALLED NEW FWD CARGO DOOR, AFT LWR DOOR STOP FITTING PER SRM 51-30-2. 2L73 4F RTA3WE 20051012000142005101200014NM 2005 10 12 05FDEA03253 120051006A5320 INTERCOSTAL BOEING727 727200 138407ENM LT MLG WW CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 WHILE PERFORMING BUYBACK OF UPLOCK OF THE LT MLG WW, FOUND INTERCOSTAL CORRODED ON THE UPPER SURFACE, BS 900 TO BS 905, LBL 68, 12 BELOW CEILING. REPLACED INTERCOSTAL IN LT MLG WW, BS 900-905, LBL 68 PER SRM 51-.30-2. 2L73 4F RTA3WE 20051012000232005101200023EA 2005 10 12 COMA0560537 120051008A3260172825 TARGET CNDAIRCL600 CL6002B19 1900309EA RT MLG LOOSE A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01978CA 7158 FLIGHT 5847 - GEAR DISAGREE WARNING. TIGHTENED LOOSE PROXIMITY SWITCH TARGET ON RIGHT MLG UPLOCK. 2L72 4F RTA21EA 20051012000252005101200025EA 2005 10 12 COMA0560536 120051008A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01969CA 7141 FLIGHT 5605 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2L72 4F RTA21EA 20051013000082005101300008GL 2005 10 13 AWXA200501180 220051004A7200 ENGINE BOEING737 7373G7 1384595NM CFMINTCFM56 CFM563B1US GL NR 1 FAILED A AWXAA UNSCHED LANDING EA VIBRATION/BUFFET FLAME/FIRE CLCLIMB 1 WP28305AW4947543220 24012 720864 AFTER TAKEOFF CREW HEARD LOUD BANG AND FELT VIBRATION COMING FROM THE NR 1 ENGINE. AIRCRAFT RETURNED TO PHX, DECLARED EMERGENCY AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE BORESCOPED THE NR 1 ENGINE LPC AND HPC, FINDING DAMAGE TO THE HPC STAGES 7, 8 AND 9. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE IAW AMERICA WEST AIRLINES TASK CARDS R5M71001 AND F8M71001. OPERATIONAL CHECKS WERE GOOD. 2L72 4F4 FRTA16WE E2GL 20051013000222005101300022NM 2005 10 13 05FDEA03382 120051011A5311 FRAME BOEING727 72722 1384002NM BS 826 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 STA 826 LBL 47 FRAME WEB SUPPORT CRACKED. REMOVED CRACKED FRAME WEB SUPPORT BS 826, LBL 47, INSTALLED NEW SUPPORT IAW SRM 51-30-2, 51-30-5, AND 51-10-2. 2L73 4F A3WE 20051013000252005101300025EU 2005 10 13 05FDEA03385 120051011A2611 SMOKE DETECTOR AIRBUS310 A310222 3930315EU E/E BAY MALFUNCTIONED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25448FE 260 JUST AFTER T/O HAD AVIONICS SMOKE WARNING ON ECAM AND OVERHEAD. NO ODOR OR SIGN OF SMOKE. DECLARED EMERGENCY. RETURNED TO KABQ LANDING WT APPROX 209,000 NR, BELOW MAX LANDING WEIGHT. CHECKED AVIONICS COMPT FOR EVIDENCE OF SMOKE. DUE TO NO EVIDENCE OF SMOKE IN COCKPIT OR AVIONICS COMPT SUSPECT INTERMITTENT DETECTOR 11WA. REPLACED 11WA , NOT TESTING AND 12WA PRECAUTIONARY. 2L72 4F RTA35EU 20051013000272005101300027NM 2005 10 13 ABXA050241 120050913A5712114T222415 RIB BOEING767 767281 1385109NM LT WING CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23774AX 22789 LT WING LEADING EDGE RIB AT STA. WA 920 (APPROXIMATELY) HAD EXFOLIATED CORROSION AT FORWARD END AND LOWER FLANGE LOWER SURFACE. REMOVED AND REPLACED RIB IAW B767 SRM 51-40-01. 2L72 4F RTA1NM 20051013000292005101300029WP 2005 10 13 P9RA200500101 120050928A7933162BL709C INDICATOR DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE ENGINE OIL TEMP INOPERATIVE A P9RAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO11135NJ 49440 ON CLIMBOUT, AT APPROX. 20,000 FT., RT ENGINE OIL TEMPERATURE PEGGED OUT AT TOP OF GUAGE. TURNED BACK, DESCENDED AND DECLARED AN EMERGENCY. PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN. LANDING WAS UNEVENTFUL.7 CREW. 88 PAX. 1 ACM ON BOARD. FOUND THE RT ENGINE OIL TEMPERATURE GUAGE TO BE PEGGED. REMOVED AND REPLACED INDICATOR IAW M/M. OPERATIONAL CHECKED GOOD AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 20051013000342005101300034EA 2005 10 13 ACE101005 220051010A73141143890425 PUMP BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA ENGINE FUEL LEAKING E YADAK NONE K FLUID LOSS ININSP/MAINT 1 AL03114AX 3606 UC36 NR 2 ENGINE LEAKING FUEL FROM NACELLE. MAINTENANCE REPLACED LOW PSI FUEL PUMP DUE EXTRUDED VALVE BODY GASKET. FUEL WAS NOT DUMPED OVERBOARD AS THE VALVE BODY WAS LEAKING EXTERNALLY. 2L72 4T4 TRTA24CE E4EA 20051013000352005101300035NM 2005 10 13 HNAA0500088 120051006A323382910016009 ACTUATOR DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE MLG BYPASSING A HNAAO OTHER J WARNING INDICATION APAPPROACH 1 EA07982HA2960129601 380 NOSE GEAR DID NOT EXTEND WHEN GEAR HANDLE SELECTED DOWN, GEAR DID EXTEND WHEN ALT. EXTENSION PROCEDURE WAS FOLLOWED. REMOVED AND REPLACED NOSE DOOR ACTUATOR. 2H72 4T4 TRTA13NM E20NE 20051013000402005101300040WP 2005 10 13 DHL2005806523 120050902A53403755822U515 FITTING DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE BS 300 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH87034 46002 FWD CARGO COMPT ZEE FITTING CRACKED 0.500 IN STA 300.000 L-27L. REMOVED CRACKED ZEE FITTING IAW SRM 53-1-0 PG. 1, SRM 51-1-20D. FABRICATED 2EA REPAIR ANGLES IAW SRM 53-2-0 FIG 2D SHEET 1,2, SRM 51-1-4 PG. 1 (FORMING). CUT NEW ZEE FITTING IN HALF USING TRIM DIMENSIONS NOTED IN THE SRM CHAPTER 53-2-0 FIG. 2D SHEET 2. HEAT TREATED REPAIR ANGLES IAW SRM 51-1-1 PG. 1,13,17. CLEANED, TREATED AND PRIMED AREA AND REPAIR ANGLES IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG. 9. INSTALLED NEW ZEE FITTING AND REPAIR ANGLES IAW SRM 53-2-0 FIG. 2D SHEET 1,2, SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2L74 4F4 FRT4A25 E2GL 20051013000422005101300042NM 2005 10 13 CALA0500329 120051004A533065C35794 SKIN BOEING737 7373T0 1384582NM GE CFM56 CFM563B1 13802NE BS 767 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769333 23571 INSPECTION FOUND A 1 INCH CRACK IN FUSELAGE SKIN BONDED DOUBLER LINE STA 767 BETWEEN S21R AND S22R. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-00-01, FIGURE 201. 2L72 4F4 FRTA16WE E2GL 20051013000452005101300045WP 2005 10 13 05FDEA03289 120051007A5712 RIB DOUG DC10 DC1010 3022110WP RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE RT WING FIXED L/E COMPT AT STA XORS 949 ZONE 627 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 5 AND 6 VOL I. 2L73 4F A22WE 20051013000462005101300046WP 2005 10 13 05FDEA03290 120051007A5712 RIB DOUG DC10 DC1010 3022110WP RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE RT WING FIXED L/E COMPT AT STA XORS 610 ZONE 619 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 1, 4 AND 6 VOL I. 2L73 4F A22WE 20051013000472005101300047WP 2005 10 13 05FDEA03291 120051007A5712 RIB DOUG DC10 DC1010 3022110WP RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE RT WING FIXED L/E COMPT AT STA XORS 873 ZONE 625 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 4 AND 6 VOL I. 2L73 4F A22WE 20051013000482005101300048NM 2005 10 13 SWAA053119 120051009A53306545765 SKIN BOEING737 7373A4 1384585NM BS 500D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29669SW 23752 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 10R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051013000532005101300053NM 2005 10 13 05FDEA03178 120050930A5347 SEAT TRACK BOEING727 727225 1384077NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25465FE 21289 SEAT TRACK LBL 24 HAS 2 SPLICES AND CORROSION STA 380 - STA 480. REMOVED CORROSION, MATERIAL LOSS FOUND OUT OF LIMITS, ORIGINAL THICKNESS .085 MATERIAL REMOVED .029 RAMAINING .056, REMOVED SEAT TRACK. FABRICATED, DRILLED TO FIT, ALODINED, PRIMED AND INSTALLED NEW SEAT TRACK IAW B727 SRM 51-10-1, FIG 6, SRM 51-10-2 AND DWG 65-23-637. 2L73 4F A3WE 20051013000542005101300054WP 2005 10 13 05FDEA03180 120050928A7830 WARNING LIGHT DOUG DC10 DC1010 3022110WP THRUST REVERSER ILLUMINATED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO2568058 46705 WHILE IN FLIGHT CLIMBING-OUT OF 15000 FT, THE NR 2 THRUST REVERSER UNLOCK LIGHT WAS FLICKERING ON AND OFF. THRUST REV CHECKLIST WAS COMPLETED AND RETURN AND LANDED ACN RELEASED FOR SERVICE PER MEL/CDL: 78-01-01-B 2L73 4F A22WE 20051013000572005101300057NM 2005 10 13 DHL2005748501 120050815A5310 VERTICAL BEAM BOEING727 727225 1384077NM PWA JT8 JT8D15 52051NE BS 1183 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 VERTICAL BEAM AT BS1183 RBL 36.WL 240, APPROX, SHOWS CRACK AT CHORD ANGLE. STOP DRILLED CRACK IAW SRM 51-10-1,LOCATED,DRILLED AND INSTALLED REPAIR KIT P/N 65C34406-15,PO NR 531481 IAW S/B 727-53-0192 REV 1,MAY 30,1991. 2L73 4F4 F A3WE E2EA 20051013000582005101300058NM 2005 10 13 DHL2005748599 120050815A5310 VERTICAL BEAM BOEING727 727225 1384077NM PWA JT8 JT8D15 52051NE BS 1183 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 VERTICAL BEAM AT BS.1183, RBL 36, WL 240, APPROX, SHOWS CRACK AT CHORD ANGLE. STOP DRILLED CRACK IAW SRM 51-10-1,LOCATED,DRILLED AND INSTALLED REPAIR KIT P/N 65C34406-15,PO NR 531481 IAW S/B 727-53-0192 REV 1,MAY 30,1991 2L73 4F4 F A3WE E2EA 20051013000612005101300061WP 2005 10 13 UPS05845541 120050912A534037558401 FITTING DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE FS 1153 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 INSPECTION TYPE: C3, DEEP CORROSION PITTING AROUND LOWER FASTENER THRU BATHTUB FITTING AT STA. 1153 ABOVE L33R. REMOVED BATHTUB FITTING, FABRICATED SPLICE ANGLES, INSTALLED FITTING AND SPLICE ANGLES IAW SRM 53-02-00 FIG 2D, 51-1-20D. 2L74 4F4 FRT4A25 E2GL 20051013000622005101300062WP 2005 10 13 UPS05845542 120050825A5730 SKIN DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE: C3, LT WING UPPER SURFACE CRACKED AT XRS 22.750. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW SAA SK 801-804078 A. 2L74 4F4 FRT4A25 E2GL 20051013000642005101300064NM 2005 10 13 DHL2005743002 120051005A5260 SWITCH BOEING727 727225 1384077NM PWA JT8 JT8D15 52051NE AIRSTAIR OUT OF ADJUST A DHLAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01743DH 22438 AFT AIRSTAIR AMBER LIGHT ON S/O PANEL ILLUMINATES INTERMITTENTLY. ADJUSTED AFT AIRSTAIR UP SWITCH, OPS CHECK GOOD IAW M/M 52-62-01. 2L73 4F4 F A3WE E2EA 20051013000672005101300067WP 2005 10 13 DHL2005806532 120050904A53403759222IN FITTING DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE BS 1260-1280 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH87034 46002 ITEM REF NR 041339: AFT CARGO COMPT. SPLICE FITTING CORRODED (STA 1260.000-1280.000, L-36) MAJOR REPAIR, PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG. 1. REMOVED CORROSION FROM SPLICE FITTING (STA 1260.000-1280.000 L-36) IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG. 2P. REMOVED CORRODED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1 PG. 2A (TORQUE) 2L74 4F4 FRT4A25 E2GL 20051013000702005101300070EA 2005 10 13 QXEA200501282 120051003A2150 A/C PACK CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE LEFT MALFUNCTIONED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09612QX 10042 ON TAXI OUT FOR FLIGHT 4310, RECEIVED A LT AIR CONDITIONING PACK FAULT. FLIGHT RETURNED TO THE GATE. MAINTENANCE PLACED ON MEL 21-51-1(A) RSI NR 352561. CLEARED LATER IN THE DAY BY CYCLING THE LT PACK SWITCH. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2L72 4F4 FRTA21EA EOOO63EN 20051013000712005101300071 2005 10 13 QXEA200501281 420051004A3418C12851AA03 COMPUTER CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE STALL WARNING MALFUNCTIONED A QXEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM09611QX8904 10041 DURING CLIMB OUT, RECEIVED A STALL FAIL CAUTION MESSAGE ALONG WITH BOTH LT AND RT FADEC FAULT MESSAGES. AIRCRAFT RETURNED TO FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE REPLACED THE STALL PROTECTION COMPUTER. OPS CHECKS GOOD, AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20051013000742005101300074WP 2005 10 13 UPS05845594 120050906A575356423421 FITTING DOUG DC8 DC873F 302199FWP TE FLAP TRACK CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE:C3 STA 3 LT FLAP TRACK ATTACH POINT IS CRACKED. REMOVED AND REPLACED STA 3 LT FLAP TRACK ATTACH POINT FITTING IAW DC-8 SRM 51-3-0, 51-1-21, AND 51-1-20D. 2L74 4F RT4A25 20051013000782005101300078WP 2005 10 13 ABXA050242 120051004A335041B004AD07G3 BATTERY DOUG DC9 DC932 3022066WP PWA JT8 JT8D7A 52053NE EMERGENCY LIGHT INOPERATIVE A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 OVERHEAD COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERIES IAW AMM 33-53-00-8. 2L72 4F4 F A6WE E2EA 20051013000792005101300079EA 2005 10 13 QXEA200501314 120050917A5730 SKIN CNDAIRCL600 CL6002C10 1390015EA RT WING CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09617QX 10130 YYC - RIGHT WING LEADING EDGE SKIN AT WING STATION 108 CHAFED. REMOVED DAMAGE IAW CRJ-700 SRM 51-12-00-001-001-A01, MATERIAL REMOVED .004". RESTORED FINISH. 2L72 4F RTA21EA 20051013000802005101300080EA 2005 10 13 QXEA200501315 120050917A5753 PANEL CNDAIRCL600 CL6002C10 1390015EA TE FLAP WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09617QX 10130 YYC - LEFT WING INBOARD FLAP, INBOARD PANEL 584ET WORN IN LEADING EDGE. REMOVED DAMAGE IAW CRJ-700 SRM 51-12-00-001-001-A01. RESTORED FINISH. 2L72 4F RTA21EA 20051013000812005101300081EA 2005 10 13 QXEA200501318 120050917A5320CC670341577 CROSSBEAM CNDAIRCL600 CL6002C10 1390015EA BS 280 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09617QX 10130 YYC - FUSELAGE STATION 280 CROSSBEAM HAS CORROSION AND IS CRACKED ALONG THE TOP FLANGE. MEASURED AND INSTALLED NEW CROSSBEAM IAW REO 670-53-11-047 REV "C". 2L72 4F RTA21EA 20051013000822005101300082EU 2005 10 13 TRBA2005057 120050904A610011S76180650008 SWITCH AEROSPATR72 ATR72212 8680945EU POWER CONTROL DEFECTIVE A TRBAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO29420AT 420 AUTOMATIC TAKE-OFF POWER CONTROL SYSTEM (ATPCS) DID NOT ARM DURING TAKE-OFF POWER. REPLACED DEFECTIVE SWITCH. (K) 2H72 4T RTA53EU 20051013000832005101300083NM 2005 10 13 MWEA050108 120051001A3810 VALVE BOEING717 717200 1383700NM POTABLE WATER OUT OF POSITION A MWEAA UNSCHED LANDING O OTHER CLCLIMB 1 GL31907ME 55171 NO WATER FROM ANY FAUCETS. FOUND VENT AND FILL VALVE IN HALF INCH POSITION ON SERVICE PANEL, MOVED VALVE TO OFF POSITION. SERVICED WATER AND VERIFIED PRESSURE. 2L72 4F TRA6WE 20051013000842005101300084NM 2005 10 13 XNOA1271 120051006A2133 OUTFLOW VALVE BOEING727 727227 1384078NM PWA JT8 JT8D9A 52048NE CABIN PRESSURE MALFUNCTIONED A XN0AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23793A 20774 AIRCRAFT FAILED TO PRESSURIZE MORE THAN 2 PSI DIFFERENTIAL. R & R THE RT FLOW CONTROL VALVE IAW MM 36-12-61, SYSTEMS OPS CHECK GOOD. (STATUS:ORIG/CLOSED) 2L73 4F4 F A3WE E2EA 20051013000852005101300085EA 2005 10 13 QXEA200501310 120050917A5753 FAIRING CNDAIRCL600 CL6002C10 1390015EA RT WING CHAFED A QXEAO OTHER O OTHER ININSP/MAINT 1 NM09617QX 10130 YYC - RIGHT WING LOWER SURFACE HAS CHAFED DAMAGE FROM THE FLAP HINGE FAIRING AT WS 128. BLENDED CHAFFED AREA IAW CRJ-700 SRM 51-12-00-001-001-A01. MATERIAL LOSS .002". RESTORED FINISH. 2L72 4F RTA21EA 20051013000862005101300086NM 2005 10 13 SWAA053065 120051006A53306545774 SKIN BOEING737 7373H4 1384600NM BS 727D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 19L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051013000872005101300087NM 2005 10 13 SWAA053066 120051006A53306518420 SKIN BOEING737 7373H4 1384600NM BS 259.5 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 259.5, WL 210, LT SIDE. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051013000902005101300090NM 2005 10 13 SWAA053069 120051005A3350MS155721 BULB BOEING737 7377H4 1384404NM L1 DOOR INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29490WN 32476 DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20051013000922005101300092NM 2005 10 13 SWAA053071 120051006A53226546529 SHEAR TIE BOEING737 7373H4 1384600NM BS 500C CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500C, BETWEEN LBL 2 AND RBL 9. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051013000952005101300095NM 2005 10 13 SWAA053074 120051005A5753 SKIN BOEING737 7373A4 1384585NM TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29677AA 23289 DURING SCHEDULED C4 CHECK, FOUND LT WING OTBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM. 2L72 4F RTA16WE 20051013000962005101300096 2005 10 13 SWAA053075 420051006A2565D31354 SLIDE BOEING737 7373A4 1384585NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29680AA 23505 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051013000972005101300097NM 2005 10 13 SWAA053076 120051006A33506104781 BATTERY PACK BOEING737 7373Y0 1384671NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED A2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20051013000982005101300098NM 2005 10 13 SWAA053077 120051005A2560PH22300L GLOWSTRIP BOEING737 7373T0 1384582NM RO 1 AND 6 WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29684WN 23941 DURING SCHEDULED C1 CHECK, FOUND PHOTOLUMINESCENT STRIP WORN BETWEEN ROW 1 AND ROW 6. REMOVED AND REPLACED STRIP PER MM. 2L72 4F RTA16WE 20051013001032005101300103EU 2005 10 13 TRBA2005058 120050906A3260 PROXIMITY SWITCH AEROSPATR72 ATR72212 8680945EU MLG OUT OF ADJUST A TRBAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO29408AT 408 AFTER SELECTED GEARS UP, BOTH INDICATOR PANELS SHOWED 3 UNSAFE AND 3 GREEN LIGHTS, SIMULTANEOUSLY. ADJUSTED PROXIMITY SWITCH AT LT MAIN LANDING GEAR. (K) 2H72 4T RTA53EU 20051013001042005101300104EU 2005 10 13 TRBA2005055 120050825A2612 FIRE DETECTOR AEROSPATR72 ATR72212A 8680902EU NR 1 ENGINE MALFUNCTIONED A TRBAEF ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING TXTAXI/GRND HDL 1 SO29529AM 529 ON GROUND, NR 1 ENGINE FIRE WARNING CAME ON. HEAVY TAIL WINDS WERE PRESENT CREATING A FALSE INDICATION. CAPTAIN DISCHARGED FIRE BOTTLE. REPLACED FIRE BOTTLE. NO INDICATION OF FIRE NOTED. (K) 2H72 4T RTA53EU 20051013001052005101300105NM 2005 10 13 05FDEA03266 120051006A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 FOUND CRACK INDICATION ON LEFT HAND TANK AT END OF STRINGER 11 (UPPER STRINGER). REPAIR CARRIED OUT AS PER SRM 57-20-00. 2L73 4F RTA22WE 20051013001072005101300107EU 2005 10 13 05FDEA03268 120051007A3411 PITOT TUBE AIRBUS300 A300F4605R 3930327EU PITOT STATIC CONTAMINATED A FDEAC ABORTED TAKEOFF C F.O.D. TOTAKEOFF 1 SO25669FE 774 ON TAKEOFF ROLL FROM KMSP F/O`S PFD AIRSPEED FROZEN. REJECTED TAKEOFF, RETURNED TO RAMP. FOUND A BUGS NEST OF DIRT AND DEBRIS IN THE PITOT TUBE, CLEANED OUT PITOT TUBE AND PERFORMED AIRSPEED TEST WITH PITOT STATIC TEST BOX PER M/M 34-10-00-5, ALL SYSTEMS CK GOOD. 2L72 4F RTA35EU 20051013001082005101300108NM 2005 10 13 05FDEA03269 120051007A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 CRACK FOUND APPROXIMATELY 6 INCHES AT STRINGER END OF STRINGER 15 OF LEFT HAND SIDE WING TANK. REPAIR CARRIED OUT AS PER SRM 57-20-00. 2L73 4F RTA22WE 20051013001122005101300112WP 2005 10 13 05FDEA03273 120051007A5712 RIB DOUG DC10 DC1010 3022110WP LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE LT WING FIXED L/E COMPT AT STA XORS 735 ZONE 518 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 4 AND 6 VOL I. 2L73 4F A22WE 20051013001132005101300113WP 2005 10 13 05FDEA03274 120051007A5712 RIB DOUG DC10 DC1010 3022110WP LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE LT WING FIXED L/E COMPT AT STA XORS 662 ZONE 525 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 4 AND 6 VOL I, INSTALL REPAIR ANGLE -35. 2L73 4F A22WE 20051013001142005101300114WP 2005 10 13 05FDEA03275 120051007A5712 RIB DOUG DC10 DC1010 3022110WP LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE LT WING FIXED L/E COMPT AT STA XORS 512 ZONE 519 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET3 AND 4 VOL I, INSTALL REPAIR ANGLE -35. 2L73 4F A22WE 20051013001162005101300116NM 2005 10 13 AT0500036 120050930A2612473465MOD01 CONTROL UNIT BOEING717 717200 1383700NM FIRE DETECTION SHORTED A ZZDAF ACTIVATE FIRE EXT. N FALSE WARNING CRCRUISE 1 SO15944AT 55007 (ENG L FIRE) LEVEL 3 INDICATION IN CRUISE FLIGHT. RAN QRH, PULLED T-HANDLE, EXPENDED FIRE BOTTLE 1 AND 2. REMOVED AND REPLACED NR 1 ENGINE FIRE DETECTOR CONTROL UNIT, REF 26-11, RAN ENGINE, PERFORMED FIRE TEST AND FAULT TEST, CHECKS GOOD, SEE 749178-3 AND 749178-2. 2L72 4F TRA6WE 20051013001182005101300118WP 2005 10 13 05FDEA03277 120051007A5712 RIB DOUG DC10 DC1010 3022110WP LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE LT WING FIXED L/E COMPT AT STA XORS 114 ZONE 515 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 4 AND 2 VOL I, INSTALL REPAIR ANGLE -43. 2L73 4F A22WE 20051013001202005101300120WP 2005 10 13 05FDEA03279 120051007A5712 RIB DOUG DC10 DC1010 3022110WP LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE LT WING FIXED L/E COMPT AT STA XORS 6737 ZONE 525 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 4 AND 6 VOL I. 2L73 4F A22WE 20051013001222005101300122WP 2005 10 13 05FDEA03281 120051007A5712 RIB DOUG DC10 DC1010 3022110WP LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE LT WING FIXED L/E COMPT AT STA XORS 644 ZONE 519 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 3 AND 4 VOL I , INSTALL REPAIR ANGLE -37. 2L73 4F A22WE 20051013001262005101300126NM 2005 10 13 05FDEA03299 120051007A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 CRACK INDICATION ON RIGHT SIDE WING TANK AT END OF STRINGER 13, UPPER STRINGER. SLOTTED OUT AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CARRIED OUT AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051013001282005101300128NM 2005 10 13 05FDEA03301 120051007A5311 FRAME BOEING727 72722 1384002NM BS 760 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 WHILE WORKING FEDEX WORK CARD 7-5310-7-3367 B4 PT1 FOUND LT 760 FRAME CORRODED LBL 65 WL 205. REMOVED AND REPLACED L/H 760 FRAME IAW SRM 51-30-2, 51-30-5, 51-10-2. 2L73 4F A3WE 20051013001292005101300129WP 2005 10 13 05FDEA03302 120051007A5330 SKIN DOUG DC10 DC1010 3022110WP BS 879-899 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LWR FUSELAGE RT SIDE ON SKIN FOUND DENT (1.2" BY 0.106") BETWEEN Y=899 AND Y=879 LONGERON 37-38. INSTALLED FINGER DOUBLER IAW SRM 53-20-00 VOL I. 2L73 4F A22WE 20051013001322005101300132WP 2005 10 13 MWEA050107 120050928A2913AS66411LS666 PUMP DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE RT ENG HYD SYS INOPERATIVE A MWEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31810ME 48072 RT ENGINE HYDRAULIC PUMP INOPERATIVE. REMOVED AND REPLACED RT ENGINE HYDRAULIC PUMP. 2L72 4F4 F A6WE E2EA 20051013001342005101300134SO 2005 10 13 C2XA05CL082 120050912A3350SG9632 LIGHT EMB 145 EMB145XR 3260214SO CABIN MISSING A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711113 145662 CLE FLIGHT NR 2468, THE CREW REPORTED THE EMERGENCY AISLE PATH LIGHT STRIP WAS MISSING AT GALLEY. MAINTENANCE INSPECTED AND REPLACED THE LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RT 20051013001362005101300136SO 2005 10 13 C2XA05CL083 120050915A3350110049 POWER SUPPLY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714991 145278 DURING ROUTINE MAINTENANCE, THE LEFT EMERGENCY DOOR EXIT SIGN WAS INOPERATIVE. MAINTENANCE REPLACED THE NR 3 BATTERY POWER SUPPLY. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20051013001382005101300138SO 2005 10 13 C2XA05IA106 120050913A335078241 INVERTER EMB 145 EMB145 3260210SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715973 145159 STL - DURING MAINTENANCE INSPECTION, THE OVERWING EMERGENCY EXIT LOCATOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER SIX EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20051013001402005101300140SO 2005 10 13 C2XA05IA107 120050930A335078241 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713978 145180 MCI - DURING MAINTENANCE INSPECTION, THE EMERGENCY EXIT MARKER AT ROW 12BC WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT INVERTER FOR THE AFFECTED LIGHT, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20051013001412005101300141NM 2005 10 13 UPS05M45539 120051002A3350 BULB DOUG MD11 MD11F 3023600NM PWA 4460 PW4460 NE EMERGENCY LIGHT BURNED OUT A IPXAK NONE O OTHER ININSP/MAINT 1 SO01279UP 48573 R1 DOOR EMERGENCY EXIT SIGN, HALF OF THE BULBS ARE BURNED OUT. RELAMPED, OPS CKS NORMAL IAW MM CH 33-50-00. 2L73 4F4 FRTA22WE E24NE 20051013001422005101300142NM 2005 10 13 PIDA20050158 120051004A532065528941 INTERCOSTAL BOEING737 737228 13844AGNM BS 540 CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 INTERCOSTAL AT BS 540 IS CRACKED AT BL0. REPLACED INTERCOSTAL PER DWG 65-46891 AND SRM 51-10-1. 2L72 4F RTA16WE 20051013001432005101300143NM 2005 10 13 PIDA20050162 120051003A532065528944 INTERCOSTAL BOEING737 737228 13844AGNM BS 540 CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 INTERCOSTAL AT BS 540 IS CRACKED AT THE AFT I/B EDGE AT RBL47. REPLACED INTERCOSTAL PER DWG 65-46891. 2L72 4F RTA16WE 20051013001442005101300144NM 2005 10 13 PIDA20050164 120051005A33506104789 BATTERY PACK BOEING737 7372K5 138448XNM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05250TR 22597 EMERGENCY EXIT LIGHTS AT REAR EXIT DOORS AND AT FORWARD EXIT DOORS ARE NOT ILLUMINATING. REPLACED BATTERY PACK FOR REAR DOOR LIGHTS AND FORWARD DOOR LIGHTS AND OPS CHECKED PER MM 33-51-71. 2L72 4F RTA16WE 20051013001452005101300145NM 2005 10 13 PIDA20050161 120051004A5320 INTERCOSTAL BOEING737 737228 13844AGNM R1 DOOR FRAME CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 INTERCOSTAL BEHIND THE UPPER AFT STOP FITTING ON THE AFT SIDE OF THE R1 DOOR FRAME IS CRACKED UNDER THE RIVET HEADS. REPLACED INTERCOSTAL PER 737 SB 53A1108. 2L72 4F RTA16WE 20051013001462005101300146NM 2005 10 13 PIDA20050159 120051004A532065C105926 INTERCOSTAL BOEING737 737228 13844AGNM BS 947 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 INTERCOSTAL AT BS 947 + 9 HAS CORROSION FROM LBL 8 TO LBL 18. REPLACED INTERCOSTAL PER DWG 65C10592. 2L72 4F RTA16WE 20051013001472005101300147 2005 10 13 PIDA20050163 420051005A2210 CONTROL PANEL BOEING737 737306 13844BGNM AUTOPILOT MALFUNCTIONED A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05371PA 23543 "B" AUTO PILOT CMD WILL NOT ENGAGE WITHOUT PAUSING IN CWS AND "A" AUTO PILOT WILL NOT ENGAGE (INTERMITTENT). REPLACED MODE CONTROL PANEL PER MM 22-11-34. BITE TEST ACCOMPLISHED SATISFACTORY. 2L72 4F RTA16NE 20051013001482005101300148NM 2005 10 13 PIDA20050156 120050930A5315 FLOORBEAM BOEING737 737228 13844AGNM BS 520 CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 FLOORBEAM AT BS 520 IS CRACKED AT LBL24. REPAIRED FLOORBEAM PER 737 SB 53-1120. 2L72 4F RTA16WE 20051013001492005101300149NM 2005 10 13 PIDA20050157 120051004A532065528942 INTERCOSTAL BOEING737 737228 13844AGNM BS 540 CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 INTERCOSTAL SHIM AT BS 540 IS CRACKED AT RBL1. REPLACED INTERCOSTAL PER DWG 65-46891 AND SRM 51-10-1. 2L72 4F RTA16WE 20051013001502005101300150NM 2005 10 13 PIDA20050160 120051004A532065C1059210 INTERCOSTAL BOEING737 737228 13844AGNM BS 947 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 INTERCOSTAL AT BS 947 + 9 HAS CORROSION FROM LBL 18 TO LBL 42. REPLACED INTERCOSTAL SRM 51-10-1. 2L72 4F RTA16WE 20051013001512005101300151WP 2005 10 13 05FDEA03283 120051007A5712 RIB DOUG DC10 DC1010 3022110WP LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE LT WING FIXED L/E COMPT AT STA XORS 789 ZONE 526 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 4 AND 6 VOL I. 2L73 4F A22WE 20051013001532005101300153WP 2005 10 13 05FDEA03284 120051007A5712 RIB DOUG DC10 DC1010 3022110WP RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE RT WING FIXED L/E COMPT AT STA XORS 542 ZONE 619 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 4 AND 6 VOL I. 2L73 4F A22WE 20051013001552005101300155WP 2005 10 13 05FDEA03286 120051007A5712 RIB DOUG DC10 DC1010 3022110WP RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE RT WING FIXED L/E COMPT AT STA XORS 510 ZONE 619 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 1, 3 AND 4 VOL I, INSTALL REPAIR ANGLE -36. 2L73 4F A22WE 20051013001572005101300157NM 2005 10 13 SB05126 120051007A2133322684003 OUTFLOW VALVE BOEING737 737301 1384611NM CABIN PRESSURE FAULTY A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19591US6217962179 23936 CLT - FLT568 - EN ROUTE FROM PIT TO RSW, AT FL310, AIRCRAFT WOULD NOT MAINTAIN CABIN PRESSURIZATION. CREW DESCENDED FLIGHT TO FL260 AND WAS ABLE TO GAIN CONTROL OF CABIN PRESSURE WITH PACKS IN HIGH FLOW MODE ONLY. MAINTENANCE ADVISED CREW TO DIVERT TO CLT WHERE THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE FORWARD OUTFLOW VALVE AND FLEX DUCT. OPERATIONAL CHECK GOOD. ACCOMPLISHED SATISFACTORY DECAY RATE TEST PER MM 21-43-11 AND PRESSURIZATION CONFIDENCE CHECK PER JOB CARD J321-00-01. 2L72 4F RTA16WE 20051013001592005101300159NM 2005 10 13 PIDA20050166 120051005A5320 INTERCOSTAL BOEING737 737228 13844AGNM BS 344-360 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 CORROSION AT CLIP NUT HOLES ON INTERCOSTAL AT RBL12 BETWEEN BS 344 AND BS 360. REPLACED INTERCOSTAL PER SRM 51-10-1. 2L72 4F RTA16WE 20051013001612005101300161NM 2005 10 13 PIDA20050168 120051004A5315 FLOORBEAM BOEING737 737228 13844AGNM BS 520 CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 CRACK IN RADIUS OF RBL 45.50 FLOORBEAM AT BS 520. REPAIRED PER SB 737-53-1120. 2L72 4F RTA16WE 20051013001622005101300162NM 2005 10 13 PIDA20050169 120051004A5315 FLOORBEAM BOEING737 737228 13844AGNM BS 520 CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 CRACK IN RADIUS OF RBL 24 FLOORBEAM AT BS 520. REPAIRED PER SB 737-53-1120. 2L72 4F RTA16WE 20051013001632005101300163NM 2005 10 13 05FDEA03364 120051011A5712ARB77748 RIB DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 RT WING LOWER WINGLET RIB FOUND CRACKED AT LEADING EDGE AREA. REMOVED AS PER SRM 51-31-01 VOLUME II. NEW RIB FABRICATED AS PER DRAWING ARB7774 AND INSTALLED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051013001642005101300164WP 2005 10 13 05FDEA03368 120051011A5311 FRAME DOUG DC10 DC1010 3022110WP BS 469 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 AV COMPT FOUND NR 1 CRACK (1" LONG ) ON FRAME AT STA Y= 469 X= 75. INSTALLED FRAME REPAIR IAW SRM 53-30-00 FIG 5 VOL 1. 2L73 4F A22WE 20051013001652005101300165WP 2005 10 13 0501519623 120051002A2150 DUCT DOUG DC9 DC941 302207NWP PWA JT8 JT8D9 52048NE ACM OUTLET BLOWN A NWAAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 GL01623NW 47591 DURING CRUISE, CREW HAD TROUBLE REGULATING THE CABIN TEMPERATURE. THE CABIN STARTED TO CLIMB AT 1600 FPM AND THE RED (CABIN PRESS) WARNING LIGHT ILLUMINATED. CREW INITIATED A RAPID DESCENT AND COMPLIED WITH COM PROCEDURES BUT WAS NOT ABLE TO REGAIN CABIN PRESSURE CONTROL AND THE FIGHT CONTINUED TO DESTINATION AT 12,000 FEET. THE MASKS DID NOT DEPLOY AND THE LANDING WAS UNEVENTFUL. MAINTENANCE REPLACED SOME AIR CYCLE MACHINE DUCTS AND BOTH WATER SEPARATORS. FUNCTION CHECKS GOOD, NO MENTION OF BITE, AND THE AIRCRAFT HAS RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 20051013001662005101300166WP 2005 10 13 ARWA20050912 120050928A521010MQ0026246 CABLE DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL DOOR MECHANISM DAMAGED A ARWAK NONE O OTHER ININSP/MAINT 1 SO1968041 46900 MAIN CABIN L1 DOOR WITH DOOR OPEN, NO WARNING LIGHT. UPON INSPECTION OF DOOR MECHANISM FOUND DAMAGED CABLES AT AFT SECTION OF L1 DOOR. REMOVED DAMAGED SECTIONS IAW M/M 52-10-02; INSTALLED PASSENGER DOOR DRIVE CABLE IAW M/M 52-10-02. OPERATIONAL CHECK OK. 2L73 4F4 F A22WE E23EA 20051013001672005101300167GL 2005 10 13 2005F00098 120050914A3246 BOLT AMTR LARK LARKJK1 GL CONT C75 C75* 17005SO MLG WHEEL LOOSE B O OTHER O OTHER NRNOT REPORTED 1 SO25650 2308 263 149 WHEEL ASSEMBLY RETURNED FOR LOOSE BOLTS, OF 18 BOLTS INSTALLED 10 WERE FOUND TO HAVE LOOSENED. MFG HAS NOW RELEASED SERVICE LETTER F6137-32-843 TO RESOLVE. 1M71 3O3 O EXPA1M71E233 20051013001702005101300170EU 2005 10 13 05FDEA03310 120051007A5753 SKIN AIRBUS300 A300F4605R 3930327EU ZONE 500 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25659FE 757 LT WING CENTER FLAP UPPER SKIN HAD 4 SMALL CHAFED AREAS. INSTALLED REPAIR DOUBLER PER EA NR 6-5750-92547. 2L72 4F RTA35EU 20051013001712005101300171EU 2005 10 13 SF20051003 120051003A5270 WARNING LIGHT SAAB SF340 SF340A 7850100EU GE CT7TS CT71 30030NE CARGO DOOR FALSE ACTIVATIONA UHLAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL1719XS 340A019 PIT CARGO DOOR LIGHT ON IN FLIGHT. A/C RETURNED TO FIELD. C/A CLEANED CARGO DOOR SWITCH IAW MFG MM 52-70-15-4, CYCLED CARGO DOOR SEVERAL TIMES IAW MFG MM 52-30-00-2, COULD NOT DUPILCATE WRITE-UP, OPS CHECK GOOD. 2L72 4T4 URTA52EU E8NE 20051013001722005101300172EU 2005 10 13 NACA20050022 120050929A2910USP1514J4S SWIVEL FITTING AEROSPATR42 ATR42300 8680920EU PWA 120 PW120 NE HYD SYSTEM BROKEN A NACAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 AL0342NC 067 HYDRAULIC BLUE LOW LEVEL LIGHT ON. RT OB SWIVEL FITTING FOUND BROKEN. REMOVED AND REPLACED WITH NEW FITTING. REF JIC 32-11-00-RAI-10020 TASK 1-3. BLED ALL MAIN LANDING GEAR BRAKES IAW ATR42 JIC 32-42-00-BLD-10010. SYSTEM OPS LEAK CHECKED GOOD. 2H72 4T4 TRTA53EU E20NE 20051013001742005101300174 2005 10 13 SWAA053078 420051006A256563550 SLIDE BOEING737 7377H4 1384404NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29707SA 27841 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051013001752005101300175 2005 10 13 SWAA053079 420051006A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29753SW 29848 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051013001772005101300177NM 2005 10 13 SWAA053081 120051006A5210692914 GATE BOEING737 7375H4 138449DNM PAX DOOR LEAKING A SWAAA UNSCHED LANDING O OTHER CLCLIMB 1 SW29503SW 24180 AIR TURNBACK, AUTO FAIL LIGHT ILLUMINATED, SELECTED STANDBY, NO HELP. REMOVED AND REPLACED EXTERNAL GROUND AIR CONDITIONING FLAPPER DOOR PER MM. 2L72 4F RTA16WE 20051013001782005101300178NM 2005 10 13 QXEA200501322 120050925A5730 PANEL BOMBDRDHC8 DHC8402 1390042NM WING CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09401QX 4031 PDX: LEADING EDGE PANEL 512AL HAS CHAFE ON INBOARD WEB. MAINTENANCE BLENDED CHAFE MARK ON WEB IAW Q400 SRM 51-14-00 TO REMOVE DAMAGE. HFEC INSPECTED BLENDED AREA FOR CRACKS IAW Q400 PART 6, 51-00-01. NO CRACKS NOTED. COMPLIED WITH STEPS 4-6 OF EA 6-57-378. 2H72 4T RTA13NM 20051013001792005101300179NM 2005 10 13 QXEA200501323 120050930A5740 NUT PLATE BOMBDRDHC8 DHC8402 1390042NM RT WING PANEL DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09401QX 4031 PDX: NUT PLATES FOR RT WING PANEL 613DR HAS INSERT MISSING, 2ND NUTPLATE FROM OUTBOARD EDGE. MAINTENANCE DRILLED OFF BROKEN NUT PLATE AND RIVETED IN NEW NUT PLATE IAW Q400 SRM 51-42-05, TASK 51-42-05-330-801. 2H72 4T RTA13NM 20051013001802005101300180NM 2005 10 13 QXEA200501326 120050928A5714 BRACKET BOMBDRDHC8 DHC8402 1390042NM WING BOX LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09401QX 4031 PDX: LT TRAILING WING BOX BRACKET IS LOOSE YW 52. MAINTENANCE REMOVED AFT 2 CHERRY MAX RIVETS IAW Q400 SRM 51-42-45-330-801. DRILLED HOLES TO AN ALTERNATE FASTENER SIZE REF RD8/4-57-257. HFEC AROUND HOLES IAW 1-84-78A, PT-6, 51-00-06. NO CRACKS NOTED. INSTALLED AFT 2 CHERRY MAX RIVETS REF RD 8/4-57-257 IAW Q400 SRM 51-42-45-330-801 PAR 6E,F, G. COMPLETED STEPS OF RD 8/4-57-257. 2H72 4T RTA13NM 20051013001822005101300182EA 2005 10 13 QXEA200501306 120050917A5753 SKIN CNDAIRCL600 CL6002C10 1390015EA LT TE FLAP DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09617QX 10130 YYC- LEFT INBOARD FLAP LOWER EXTERIOR SURFACE HAS GRAVEL DAMAGE. BLENDED OUT DAMAGE, REMOVED .008" MATERIAL IAW CRJ-700 SRM 57-52-01-101-001-A01. RESTORED FINISH. 2L72 4F RTA21EA 20051013001842005101300184EA 2005 10 13 QXEA200501297 120050917A5310 DOOR FRAME CNDAIRCL600 CL6002C10 1390015EA CARGO DOOR DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09617QX 10130 YYC - AFT BAGGAGE BAY DOOR TRACKS STRUCTURE HAS SCRATCHES ON FORWARD AND AFT FRAMES. REPAIRED IAW EA R-53-297 AND REO 670-53-61-199. TOUCHED UP REWORK AREA. 2L72 4F RTA21EA 20051013001862005101300186 2005 10 13 200510031 420050928A25654A40302 SLIDE EMB ERJ170ERJ170100 EU CABIN DEPLOYED A UHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL17859RW 17000082 EVACUATION SLIDE DEPLOYED A THE GATE. AIRCRAFT WAS FERRIED, WHERE THE SLIDE WAS REPLACED. 2L74 4F RTA56NM 20051013001872005101300187 2005 10 13 PCSA09280501 420050928A3442 RADAR BOEING727 7272D3 138407NNM PWA JT8 JT8D217C 52053NE WX SYSTEM INTERMITTENT A PCSAA UNSCHED LANDING O OTHER CLCLIMB 1 SO29804AJ 21021 CREW REPORTED WEATHER RADAR INOPERATIVE UPON LANDING. MAINTENANCE REMOVED AND REPLACED THE RECEIVER/TRANSMITTER AND THE WAVEGUIDE ASSY. IAW MFG MM 34-43-0, AND 34-41-11, SYSTEM OPERATIONALLY CHECKED NORMAL IAW MM 34-40-0 AND 34-41-0. AIRCRAFT WAS RETURNED TO SERVICE. AIRCRAFT DEPARTED, CREW REPORTED THE WEATHER RADAR FAILED AFTER TAKE-OFF. AIRCRAFT RETURNED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RADAR ANTENNA AND THE RADAR INDICATOR IAW MM 34-41-12 AND 34-41-0. OPERATIONALLY CHECKED NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. 2L73 4F4 F A3WE E9NE 20051006001952005100600195CE 2005 10 6 DXTA200500986 120050926A2711991444015 PCU CESSNA750 750 2076810CE AILERON TRIM BINDING E DXTAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 GL07947QS6451 7500047 DURING ALL PHASES OF FLIGHT, AIRCRAFT HAD EXTREME RIGHT ROLL REQUIRED ABNORMAL LEFT AILERON TRIM WITH AUTO PILOT ENGAGED RETRIM L WING DOWN CAS MESSAGE ILLUMINATED WHICH REQURED MORE LEFT AILERON TRIM TO EXTINGUISH MESSAGE. TESTED AND FOUND TRIM SYSTEM BINDING. GAINED ACCESS TO AILERON PCU AND FOUND TO BE BINDING. REMOVED AILERON PCU P/N 9914440-15 S/N 0038 AND INSTALLED EXCHANGE PCU P/N 9914440-15 S/N 0400. WORK DONE IAW CITATION 750 MM 27-11-05. 2L72 4J RTT00007WI 20051006002062005100600206NM 2005 10 6 AWXA200501136 120050903A53306545767130 SKIN BOEING737 7373G7 1384595NM BS 380 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - DURING C18 CHECK, DISCOVERED .4 INCH LONG CRACK LOCATED ON FUSELAGE SKIN AT FASTENER HOLE AT BS 380, JUST BELOW STR 14L. MAINTENANCE CUT OUT DAMAGED SKIN AT BS 380, STR 14L IAW BOEING 737-300 SRM 53-00-01-ER FIG 201. FABRICATED FILLER, STRUCTURAL FILLERS, DOUBLER AND TRIPLER IAW BOEING 737-300 SRM 53-00-01-2R 31 FIG 201. INSTALLED FABRICATED REPAIR PARTS AT BS 380, JUST BELOW STR 14L IAW BOEING 737-300 SRM 53-00-01-2R 31 FIG 201. 2L72 4F RTA16WE 20051006002102005100600210EU 2005 10 6 SA05103 120050924A2120 ODOR AIRBUSA319 A319112 3930323EU CABIN DETECTED A USAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA19732US 1203 CLT FLT 1109 EN-ROUTE LGA TO CLT - A HOT ODOR WAS NOTED IN CABIN IN BOTH TAKEOFF AND DESCENT. THE ODOR WAS NOTED TO BE PARTICULARLY PRESENT DESCENT AT IDLE. FLIGHT COMPLETED WITHOUT FURTHER INCIDENT. MAINTENANCE RAN BOTH ENGINES AND BLEED SYSTEMS. NO ODORS NOTED. 2L72 4F RTA28NM 20051006002152005100600215WP 2005 10 6 AALA20050614 120050926A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21296AA 49308 LGA - OVERHEAD EMERGENCY LIGHTS IN FIRST CLASS ROWS 3 TO 6 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS IN FIRST CLASS ROWS 3 TO 6. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051006002252005100600225EA 2005 10 6 VTZA200500199 120050924A53116013600130 DOUBLER CNDAIRCL600 CL6002B19 1900309EA FRAME CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27643BR 7363 RIGHT FRAME DOUBLER IS CRACKED IN RADIUS AT 1 INCH IN LENGTH. 2L72 4F RTA21EA 20051012000102005101200010EU 2005 10 12 05FDEA03045 120050922A5210A52111134600096 ARM AIRBUS310 A310222 3930315EU PAX DOOR CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25448FE 260 RT FWD DOOR, LOWER ARM ASSY FOUND CORRODED. REPLACED BY A NEW ONE IAW AMM 52-11-21-4. FUNCTIONAL CHECK IAW AMM 52-10-11-501. 2L72 4F RTA35EU 20051012000222005101200022NM 2005 10 12 05FDEA03208 120051004A5753ARC4125502 FITTING DOUG MD11 MD11 3023602NM TE FLAPS CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 RT WING O/B FLAP MOUNTED L/E UP-STOP FITTING SUSPECTED CRACKED. RT WING O/B FLAP MOUNTED L/E UP-STOP FITTING CRACKED REMOVED AND REPLACED AS PER SRM 51-35-01 AND SRM 51-33-01 VOL.II. THIS REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051012001122005101200112EA 2005 10 12 COMA0560530 120051001A2752 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS LACK OF LUBE A COMAO OTHER WJ INADEQUATE Q C WARNING INDICATION APAPPROACH 1 SO01910EV 7727 FLIGHT 5711 - FLAPS FAIL CAUTION. LUBRICATED THE RIGHT WING FLAP ACTUATORS. 2L72 4F RTA21EA 20051012001142005101200114NM 2005 10 12 CALA0500340 120051007A5312 BULKHEAD BOEING737 7373T0 1384582NM BS 1016 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769333 23571 CORROSION AT STA 1016, BL 0, FWD LWR PRESSURE BULKHEAD. REPAIRED PER DRAWING 65C28106. 2L72 4F RTA16WE 20051012001182005101200118NM 2005 10 12 CALA0500345 120051010A532065C80735353 INTERCOSTAL BOEING737 737524 1384721NM BS 344-360 BROKEN A CALAK NONE O OTHER ININSP/MAINT 1 SW2716648 28909 INTERCOSTAL AT STA 344-360, LBL 0 IS BROKEN. REPLACED INTERCOSTAL PER SRM 51-10-02. 2L72 4F RTA16WE 20051012001202005101200120NM 2005 10 12 CALA0500347 120051007A253072067002 OVEN BOEING757 757224 1384958NM GALLEY SMOKE A CALAO OTHER O OTHER TXTAXI/GRND HDL 1 SW2767134 29283 SMOKE IN AFT CABIN GALLEY AREA. REPLACED OVEN PER AMM 25-32-75. 2L72 4F RTA2NM 20051012001222005101200122WP 2005 10 12 UPS05845584 120050922A5310 STRUCTURE DOUG DC8 DC871F 302199DWP FS 70 L28R-L33L CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE:SP, STA 70 LOWER AFT CHORD HAS EXFOLIATION CORROSION AT APPROX L28R-L33L. CUT OUT CORRODED CHORD, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-1-21, 51-1-20D, 53-2-5 FIG 8C. 2L74 4F RT4A25 20051012001242005101200124WP 2005 10 12 UPS05845587 120050930A53404610355 FITTING DOUG DC8 DC871F 302199DWP FS 70 L35R CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE:SP, STA 70 L35R END FITTING HAS EXFOLIATION CORROSION AFT CHORD SIDE. REMOVED AND REPLACED END FITTING IAW SRM 51-1-20D AND 51-1-21. 2L74 4F RT4A25 20051012001262005101200126NM 2005 10 12 UPS05M45578 120051008A3510MC1025104 OXYGEN MASK DOUG MD11 MD11F 3023600NM COCKPIT INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01253UP 48439 INSPECTION TYPE:PS4, F/O'S OXYGEN MASK REGULATOR FAILS PRESS TO TEST. REMOVED AND REPLACED F/O'S OXYGEN MASK PER MM 35-13-01-4. 2L73 4F RTA22WE 20051012001282005101200128EA 2005 10 12 COMA0560535 120051005A3260 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA MLG ILLUMINATED A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01409CA 7441 FLIGHT 5355 - NWS INOP CAUTION DURING GEAR EXTENSION. CND, PERFORMED OPERATIONAL CHECK OF NWS SYSTEM, FOUND NO FAULTS. 2L72 4F RTA21EA 20051012001302005101200130NM 2005 10 12 UPS05M45590 120051009A2560 SMOKE GOGGLES DOUG MD11 MD11F 3023600NM COCKPIT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01253UP 48439 INSPECTION TYPE:N/A CAPTS SMOKE GOGGLE LENS CRACKED. REPLACED SMOKE GOGGLES. 2L73 4F RTA22WE 20051012001322005101200132NM 2005 10 12 UPS05M45592 120051009A2560 SMOKE GOGGLES DOUG MD11 MD11F 3023600NM COCKPIT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01253UP 48439 COURIER SEAT LT SMOKE GOGGLE LENS CRACKED. REPLACED SMOKE GOGGLES. 2L73 4F RTA22WE 20051012001352005101200135NM 2005 10 12 SWAA053111 120051008A5754114A5040 SKIN BOEING737 7377H4 1384404NM RN 5 SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29200WN 32482 RIGHT WING NR 5 L/E SLAT CRACKED. REMOVED AND REPLACED SLAT PER MM. 2L72 4F RTA16WE 20051012001372005101200137NM 2005 10 12 CALA0500327 120051003A53206517688U175 ANGLE BOEING737 737524 1384721NM STA 312-380 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2732626 27530 INSPECTION FOUND LIGHT TO MODERATE SURFACE CORROSION ALONG L-1 DOOR Z-ANGLE AT STA 312-380, LBL 33. A NEW Z-ANGLE WAS INSTALLED IAW SRM 51-40-02. 2L72 4F RTA16WE 20051013000132005101300013EA 2005 10 13 ASOA05752 120050911A5210 ANCHOR FITTING CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11922EV 7822 DURING HANGAR MAINTENANCE, THE REAR ANCHOR FITTING ON THE PASSENGER DOOR WAS FOUND TO BE CRACKED. UPON INSPECTION, MAINTENANCE DETERMINED THE CRACKED REAR ANCHOR FITTING TO BE WITHIN LIMITS. A REPEAT INSPECTION OF THE ANCHOR FITTING IS TO BE PERFORMED AT EVERY SUBSEQUENT SERVICE CHECK FOR PROPAGATION OF THE CRACK IAW MFG REO 601R-11-272. MAINTENANCE REMOVED AND REPLACED THE ASD AFT ANCHOR FITTING IAW AMM. (CLOSED) 2L72 4F RTA21EA 20051013000152005101300015NM 2005 10 13 SWAA053112 120051010A53156545410 FLOORBEAM BOEING737 7373H4 1384600NM BS 662 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CRACKED AT BS 662, RBL 24.75. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20051013000262005101300026WP 2005 10 13 05FDEA03367 120051011A5330 SKIN DOUG DC10 DC1010 3022110WP BS 1721-1741 SCRATCHED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 UPPER FUSELAGE LT SIDE FOUND 1 SCRATCH (6" LONG ) ON SKIN BTWN AT STA Y= 1721 AND Y=1741 CLOSE OUT LONGERON 5. INSTALLED FINGER DOUBLER IAW SRM 53-20-00 FIG 13 SHEET 7 VOL 1. 2L73 4F A22WE 20051013000282005101300028EA 2005 10 13 ASOA05749 120050828A5322 SHEAR TIE CNDAIRCL600 CL6002B19 1900309EA BS 718 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11839AS 7284 DURING A C-CHECK IN MCN, THE AFT FUSELAGE FS 718 SHEAR CLIPS ABOVE AND BELOW STRINGER 10 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE AFT FUSELAGE FS 718 SHEAR CLIPS ABOVE AND BELOW STRINGER 10 IAW ASA EO 600-53-0067A. (M) 2L72 4F RTA21EA 20051013000312005101300031NM 2005 10 13 SWAA053118 120051009A551265C25727 SKIN BOEING737 7373H4 1384600NM HORIZONTAL STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 DURING SCHEDULED C2 CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED AT INBD AFT SPAR, STAB STA 110. REPAIRED HORIZONTAL STAB PER SRM. 2L72 4F RTA16WE 20051013000372005101300037WP 2005 10 13 DHL2005806534 120050904A53404772359 FITTING DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE FLOORBEAM CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH87034 46002 ITEM REF NR 040974: FWD CARGO COMPARTMENT, FLOORBEAM FITTING CRACKED 0.250 IN, STA 280.000 BL 0 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG. 9. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-0, SRM 51-3-1 (TORQUE). 2L74 4F4 FRT4A25 E2GL 20051013000442005101300044WP 2005 10 13 05FDEA03288 120051007A5712 RIB DOUG DC10 DC1010 3022110WP RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE RT WING FIXED L/E COMPT AT STA XORS 632 ZONE 619 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 1, 3 AND 4 VOL I, INSTALL REPAIR ANGLE -36. 2L73 4F A22WE 20051013000552005101300055WP 2005 10 13 DHL2005806541 120050916A2730 BRACKET DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE ELEVATOR CONTROLCORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH87034 46002 ITEM REF NR 041572: RT ELEVATOR SYSTEM 1EA BRACKET CORRODED STA -141.000. REMOVED AND REPLACED RT ELEVATOR SYSTEM BRACKET STA -141.000. TIGHTENED BOLT IAW MM 20-16-0 PG. 201. ADJUSTED ELEVATOR CONTROL CABLES IAW MM 27-30-0 PG. 512-513. REFER TO NR 041920 FOR OPS CHECK. 2L74 4F4 FRT4A25 E2GL 20051013000722005101300072WP 2005 10 13 UPS05845577 120050922A5340461265OU FITTING DOUG DC8 DC871F 302199DWP BS 12 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE:SP L33R END FITTING CRACKED AT STA 12. REMOVED AND REPLACED END FITTING AT STA 12 L33R IAW SRM 51-3-0 AND SRM 51-1-20D. 2L74 4F RT4A25 20051013000762005101300076WP 2005 10 13 UPS05845596 120050922A5230 SKIN DOUG DC8 DC873F 302199FWP CARGO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE:C3 MCD NR 3 LATCH INTERNAL DOUBLER CUTOUT HOLE HAS TORN AND CRACKED SKIN A T 6 O`CLOCK POS. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW SAA SK 801-805297. 2L74 4F RT4A25 20051013000882005101300088NM 2005 10 13 SWAA053067 120051006A53116546558 FRAME BOEING737 7373H4 1384600NM BS 907 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 1. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051013000992005101300099WP 2005 10 13 05FDEA03262 120051006A5320 SPLICE DOUG DC10 DC1010 3022110WP ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25389FE 46623 CTR PIT STA 1704-1715, OUTBOARD SECTION OF L48R SPLICE, CRACKED (FITTING). REMOVED CRACKED SPLICE IAW DC10 SRM 51-31-01 VOL II. FABBED SPLICE FITTING IAW DAC DWG AFA 3113. REMOVED INTERCOSTAL FOR ACCESS IAW DC10-SRM 51-35-01 VOL II AND 51-33-01 VOL II, INSTALLED SPLICE FITTING IAW DC10- SRM 51-33-01 VOL II. REINSTALLED INTERCOSTAL IAW DC10-SRM 51-33-01 VOL II AND DC10 SRM 51-35-01 VOL II; MAJOR REPAIR, N/R 00887. 2L73 4F A22WE 20051013001012005101300101NM 2005 10 13 05FDEA03264 120051006A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 FOUND CRACK INDICATION ON LEFT HAND TANK AT END OF STRINGER 9 (UPPER STRINGER). 2L73 4F RTA22WE 20051013001092005101300109NM 2005 10 13 05FDEA03270 120051007A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 FOUND CRACK INDICATION ON RIGHT WING TANK AT END OF STRINGER 9. CRACK AT RIGHT HAND WING TANK END OF STRINGER 9 SLOTTED OUT AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR ON SLOTTED OUT AREA CARRIED OUT AS PER SRM 57- 20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051013001102005101300110NM 2005 10 13 05FDEA03271 120051007A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 FOUND CRACK INDICATION ON RIGHT HAND WING TANK AT END OF STRINGER 11. SLOTTED OUT AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR ANGLE FABRICATED AND INSTALLED AS PER SRM 57-20- 00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051013001192005101300119WP 2005 10 13 05FDEA03278 120051007A5712 RIB DOUG DC10 DC1010 3022110WP LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE LT WING FIXED L/E COMPT AT STA XORS 921 ZONE 527 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET5 AND 6 VOL I. 2L73 4F A22WE 20051013001232005101300123WP 2005 10 13 05FDEA03282 120051007A5712 RIB DOUG DC10 DC1010 3022110WP LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE LT WING FIXED L/E COMPT AT STA XORS 719 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 4 AND 6 VOL I. 2L73 4F A22WE 20051013001302005101300130WP 2005 10 13 05FDEA03304 120051007A5330 PANEL DOUG DC10 DC1010 3022110WP BS 939-959 CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25556FE 46710 FWD CARGO COMPT FOUND ONE SUMP PANEL BETWEEN Y=939 AND Y=959 LT SIDE WITH CRACK 2 INCH LONG. INSTALLED REPAIR DOUBLER IAW SRM 53-00-01 FIG 4. 2L73 4F A22WE 20051013001312005101300131WP 2005 10 13 05FDEA03306 120051007A5313 LONGERON DOUG DC10 DC1010 3022110WP BS 1781-1561 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 CNTR CARGO COMPT TUNNEL AREA LT SIDE FROM STA 1781 TO 1561 LONGERON 38 LT FOUND CORROSION. INSTALLED REPAIR LONGERON IAW SRM 53-10-00 FIG 2A SHEET 1, 2 VOL I. 2L73 4F A22WE 20051013001332005101300133NM 2005 10 13 QXEA200501285 120050929A5753 SKIN BOMBDRDHC8 DHC8402 1390042NM TE FLAP WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 PDX: LT OUTBOARD FLAP INBOARD EDGE NEXT TO NACELLE HAS A WORN SPOT 1/4" DIAMETER. MX CHAFE DAMAGE IS 4" LX, 35" W AND IS .014" MAX DEPT.MAPPED FOR ENGINEERING. HFEC INSP OF CHAFED AREA FOR CRACKS IAW Q400 NDTM PART 6, 51-00-02. NO CRACKS NOTED. PERFORMED DISBOND CHECK IAW 1-84-7Q, PT-1, 51-00-05. NO DISBOND NOTED. VERIFIED THAT CHAFE AREA IS BLENDED IAW EA 6-57-351 AND RD 8/4-57-559. HFEC INSP BLEND IAW 1-84-7A, PT-6, 51-00-02. NO CRACKS NOTED. UT THICKNESS CHECK IAW 1-84-7A PT-6, 51-00-02. NO CRACKS NOTED. UT THICKNESS CHECK IAW 1-84-7A, 51-00-04-ME .032, NIM .022. ALODINED, PRIMED AND PAINTED IAW EA 6-57-351 AND RD-8/4-57-559. REINSTALLED POLYURETHANE/ACRYLIC TAPE TO INBOARD LT FLAP AND EDGE SEALED WITH POLYU2H72 4T RTA13NM 20051013001352005101300135SO 2005 10 13 C2XA05IA104 120050910A3350 LIGHT EMB 135 EMB135LR 3260305SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715527 145413 LRD - FLIGHT 2359, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT BOTH SIDE PANEL EXIT LIGHTS AT THE OVERWING EXITS WERE INOPERATIVE. THE CREW RESET THE EMERGENCY LIGHT SYSTEM, OPERATIONALLY CHECK WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20051013001372005101300137SO 2005 10 13 C2XA05BT069 120050914A33501317 BULB EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT BURNED OUT A C2XAK NONE O OTHER ININSP/MAINT 1 SW2734110 145658 DURING SERVICE AND ROUTINE CHECK, MAINTENANCE FOUND THE ROW NR 3 OVERHEAD EMERGENCY EXIT LIGHT NOT WORKING. REMOVED AND REPLACED BULB AT ROW NR 3 EMERGENCY EXIT LIGHT IAW EMB145 AMM NR 33-50-08. OPS CHECK GOOD. 2L72 4F RT 20051013001392005101300139SO 2005 10 13 C2XA05SD027 120051003A3350110049 CHARGER EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713123 145688 SDF - OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED NR 4 BATTERY CHARGER IAW EMB 145XR AMM 33-50-04. OPS CHECK GOOD. 2L72 4F RT 20051013001522005101300152NM 2005 10 13 ASMF200510001 120051001A213339271411 OUTFLOW VALVE DOUG MD80 MD83 3023681NM PWA JT8 JT8D1 52044NE CABIN PRESSURE FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23861LF17281 49826 CAPTAIN REPORTED THE PRESSURIZATION VERY UNSTABLE, NOT POSSIBLE TO PRESSURIZE AIR CONDITIONING PACKAGES. THE CABIN PRESSURE CONTROL WAS RESEATED IAW MM 21-32-04. LATER, AIRCRAFT RETURNED TO PLATFORM, PNEUMATIC LEAK ON RT AIR CONDITIONING. THE RUBBER HOSE BETWEEN HEAT EXCHANGER AND REFRIGERATION UNIT CLAMP WERE REPLACED IAW MM 21-20-00, TESTED CORRECT. DURING RT ENGINE START, THE IGNITION WAS OUT OF SERVICE. THE EXCITER IGNITION BOX WAS REPLACED IAW MM 74-1001, TESTED CORRECT. DURING OVERNIGHT CHECK, BOTH A/C REGULATION VALVES, LT A/C PILOT PRESS REGULATOR AND DUAL ACCELEROMETER WERE REPLACED IAW MM 21-31-01, MM 21-31-00 AND MM 22-219-02 RESPECTIVELY, TESTED CORRECT. 2L72 4F4 FRT E2EA 20051013001542005101300154WP 2005 10 13 05FDEA03285 120051007A5712 RIB DOUG DC10 DC1010 3022110WP RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE RT WING FIXED L/E COMPT AT STA XORS 644 ZONE 619 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 1, 3 AND 4 VOL I, INSTALL REPAIR ANGLE -36. 2L73 4F A22WE 20051013001562005101300156WP 2005 10 13 05FDEA03287 120051007A5712 RIB DOUG DC10 DC1010 3022110WP RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE RT WING FIXED L/E COMPT AT STA XORS 626 ZONE 619 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 1, 3 AND 4 VOL I, INSTALL REPAIR ANGLE -36. 2L73 4F A22WE 20051013001582005101300158NM 2005 10 13 PIDA20050165 120051005A5321 PAN BOEING737 737228 13844AGNM LAVATORY FLOOR CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 AFT LAVATORY PAN HAS CORROSION ON LOWER SURFACE FROM BS 986+8 TO BS 1016 AT LBL 38. REPLACED PAN PER DWG 65-46812 AND SRM 51-10-1. 2L72 4F RTA16WE 20051013001602005101300160NM 2005 10 13 PIDA20050167 120051004A5315 FLOORBEAM BOEING737 737228 13844AGNM BS 520 CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 CRACK IN RADIUS OF LBL 45.50 FLOORBEAM AT BS 520. REPAIRED PER SB 737-53-1120. 2L72 4F RTA16WE 20051013001892005101300189SW 2005 10 13 ALGA105863 120050820A6320206040032105 BEARING BELL 206 206L4 1182110SW ALLSN 250C 250C30P 03013GL TRANSMISSION FAILED B ALGAK NONE O OTHER ININSP/MAINT 1 SW03175AL 52117 TRANSMISSION ASSY MAKING METAL, DISASSEMBLED AND FOUND DUPLEX BEARING BREAKING DOWN. REMOVED AND REPLACED DUPLEX BEARING. 1G71 3U3 UNCH2SW E1GL 20051013001912005101300191NM 2005 10 13 QXEA200501324 120050928A5347 SEAT TRACK BOMBDRDHC8 DHC8402 1390042NM BS 780 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09401QX 4031 PDX: AFT CARGO BAY LT IB SEAT TRACK NR 9 HAS PITTING CORROSION INSIDE LUG AREA AT APPROX FS X780.00. MAINTENANCE BLENDED PIT CORROSION FROM SEAT TRACK PER Q400 RD 8/4-53-884, PG 6, STEP 1. HFEC BLENDED AREA IAW 4-84-7A, PT-6, 51-00-02. NO CRACKS NOTED. COMPLETED REPAIR OF BLEND BY ALODINE, PRIME AND PAINT APPLICATION PER Q400 RD 8/4-53-884, PG 6, STEPS 3-8. NO DEFECTS NOTED. 2H72 4T RTA13NM 20051013001922005101300192SW 2005 10 13 YTRR105929 120050906A6300406310405101 BEARING BELL 407 407 1182206SW ALLSN 250C 250C47B GL MAIN ROTOR WORN B YTRRK NONE O OTHER ININSP/MAINT 1 SW03595RL1408 53595 ON ROUTINE INSPECTION FOUND PITCH CHANGE LINK BEARING WORN BEYOND LIMITS IN BOTH THE AXIAL AND RADIAL DIRECTIONS. 1G71 3U3 UO H2SW E1GL 20051013001932005101300193EA 2005 10 13 QXEA200501296 120050917A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA BS 1000-1047 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09617QX 10130 YYC - FUSELAGE EXTERIOR HAS SCRATCHES AND NICKS AT THE FORWARD AND TOP EXTERNAL SKIN AROUND THE AFT BAGGAGE DOOE CUTOUT FS 1000 TO 1047. REPAIRED DOOR SURROUND SKIN IAW EA R-53-296 AND REO 670-53-61-197. PRIMED AND REPAINTED AREA. 2L72 4F RTA21EA 20051013001942005101300194EA 2005 10 13 QXEA200501300 120050917A5751 SKIN CNDAIRCL600 CL6002C10 1390015EA LT AILERON CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09617QX 10130 YYC - LEFT AILERON UPPER LEADING EDGE SKIN HAS CHAFED MARKS. REMOVED CHAFFED DAMAGE IAW CRJ-700 SRM 51-12-00-001-001-A01. 2L72 4F RTA21EA 20051013001952005101300195EA 2005 10 13 QXEA200501308 120050917A5730 SKIN CNDAIRCL600 CL6002C10 1390015EA RT WING DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09617QX 10130 YYC - RIGHT WING UPPER SKIN TRAILING EDGE INBOARD OF MULTI FUNCTION SPOILERS HAS A LOOSE FASTENER. INSTALLED RIVETS IAW CRJ-700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20051013001962005101300196EA 2005 10 13 QXEA200501311 120050917A7830 THRUST REVERSER CNDAIRCL600 CL6002C10 1390015EA LT ENGINE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09617QX 10130 YYC - LEFT ENGINE AFT FLANGE OF UPPER AND LOWER COWLING AND LEADING EDGE OF EXHAUST FAIRING ARE CHAFED. BLENDED OUT DAMAGED AREA IAW REO 670-54-13-451 AND EA R-54-83. NO CRACKS FOUND. RESTORED FINISH 2L72 4F RTA21EA 20051013001972005101300197EA 2005 10 13 QXEA200501316 120050917A5315CC670341441 FLOORBEAM CNDAIRCL600 CL6002C10 1390015EA BS 280 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09617QX 10130 YYC- FUSELAGE FLOORBEAM STRUCTURE AT FS 280 AND BL 9.04 BRACKETS ARE CRACKED. REPLACED BRACKETS IAW CRJ-700 SRM 51-42-00-001-001-A01 AND 51-42-21-001-001-A01 (RIGHT SIDE). LEFT SIDE NEW BRACKET FABRICATED AND REPLACED IAW CRJ-700 SRM 53-11-10-991-802-39 AND 51-42-06-001-001-A01, AND 51-42-21-001-001-A01. 2L72 4F RTA21EA 20051013001992005101300199NM 2005 10 13 QXEA200501325 120050928A5720 BRACKET BOMBDRDHC8 DHC8402 1390042NM LT WING LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09401QX 4031 PDX: LT TRAILING WING BOX BRACKET IS LOOSE YW 60. MAINTENANCE REMOVED 2 CHERRY MAX RIVETS IAW Q400 SRM 51-42-45-330-801, PAR 1-6A AND C. DRILLED HOLES TO AN ALTERNATE FASTENER SIZE REF RD 8/4-57-257. HFEC AROUND HOLES IAW 1-84-7A, PT-6, 51-00-02. NO CRACKS NOTED. PRIMERED AND SEALED REF RD 8/4-57-257. INSTALLED AFT 2 CHERRY MAX RIVETS IAW Q400 SRM 51-42-45-330-801, PAR E-G. COMPLETED RD 8/4-57-257 BY PAINTING. 2H72 4T RTA13NM 20051013002002005101300200 2005 10 13 ASMF200509014 420050924A34212587794 VALVE DOUG MD80 MD83 3023681NM PWA JT8 JT8D1 52044NE COCKPIT FAILED W ASMFK NONE J WARNING INDICATION ININSP/MAINT 1 SW23831LF1448112567 53050 CAPTAIN REPORTED, DURING FLIGHT, THE F/O RMI CHANGED HEADING, BEING NECESSARY TO ADJUST CONTINUOUSLY. DURING REVISION, DETECTED A DIFFERENCE OF 20 GRADES BETWEEN COURSES. THE LT FLUX VALVE NR 1 WAS REPLACED IAW MM, SYNCHRONY TEST WAS PERFORMED IAW MM, BEING SATISFACTORY. DURING TOWING, THE LT EHSI INFORMATION GOT LOST, RMI FLAG TURNED ON. AC WAS SENT TO HANGAR, COMPASS SYS NR 1 WAS VERIFIED, DETECTING THAT FLUX TOOK TOO MUCH TIME TO COMPENSATE, REPLACED IAW MM 34-21-06, OPERATING CORRECTLY. COMPASS RACK NR 1 WAS REPLACED IAW MM 34-21-09, 360 GRADES OF AC MOVEMENT TEST WAS PERFORMED IAW MM 34-21-00, BEING CORRECT. DURING OVERNIGHT CHECK, THE COMPASS ROSE SWING TESTS WERE PERFORMED IAW MM 34-21-06, ALL CORRECT. 2L72 4F4 FRT E2EA 20051013002012005101300201NM 2005 10 13 SWAA053051 120051005A53306545765 SKIN BOEING737 7373H4 1384600NM BS 500A CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500A, STR 16L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051013002022005101300202NM 2005 10 13 SWAA053052 120051005A53306545767 SKIN BOEING737 7373H4 1384600NM BS 426.25 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 426.25, STR 16L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051013002032005101300203NM 2005 10 13 SWAA053053 120051005A3350101114 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED 1/4D CHECK, FOUND CENTER CABIN EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20051013002042005101300204NM 2005 10 13 SWAA053054 120051005A53116546541 FRAME BOEING737 7373H4 1384600NM BS 663 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 2L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051013002052005101300205NM 2005 10 13 SWAA053055 120051005A53226546536 SHEAR TIE BOEING737 7373H4 1384600NM BS 616 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 616, BETWEEN STR 7R TO STR 8R. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051013002062005101300206NM 2005 10 13 SWAA053056 120051005A53226546529 SHEAR TIE BOEING737 7373H4 1384600NM BS 500 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500, LBL 18. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051013002072005101300207NM 2005 10 13 SWAA053057 120051005A53116545812 FRAME BOEING737 7373H4 1384600NM BS 328 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 328, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051013002082005101300208NM 2005 10 13 SWAA053058 120051005A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM BS 827 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 827, LBL 17. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051013002092005101300209NM 2005 10 13 SWAA053059 120051004A3350311500 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29380SW 26587 DURING SCHEDULED C4 CHECK, FOUND FWD CABIN BULLNOSE EMERGENCY EXIT LENS LOOSE. SECURED LENS PER MM. 2L72 4F RTA16WE 20051013002102005101300210NM 2005 10 13 SWAA053060 120051004A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29470WN 33860 DURING SCHEDULED HC2 CHECK, FOUND EEPLS STRIP WORN AT FWD END. REMOVED AND REPLACED EEPLS STRIP PER MM. 2L72 4F RTA16WE 20051013002112005101300211NM 2005 10 13 SWAA053061 120051005A53116546539 FRAME BOEING737 7373H4 1384600NM BS 616 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, LBL 65, WL 203. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20051013002122005101300212NM 2005 10 13 SWAA053062 120051005A53116517684 FRAME BOEING737 7373H4 1384600NM BS 303 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303, STR 16L. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20051013002132005101300213NM 2005 10 13 SWAA053063 120051005A55536547450 FITTING BOEING737 7373H4 1384600NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 DURING SCHEDULED D CHECK, FOUND LT AND RT VERTICAL STAB ATTACH FITTINGS CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER. 2L72 4F RTA16WE 20051013002142005101300214NM 2005 10 13 DXTA200501008 120051007A27524AS5120213006 ACTUATOR GULSTM200 200 4500308NM NR 3 FLAP INOPERATIVE E DXTAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 GL07720QS895 085 AFTER TAKEOFF FROM SUX, SLATS AND FLAPS WOULD NOT RETRACT. SLAT/FLAP MAINTEN ICAS MESSAGE CAME ON. TRIED TO RECYCLE SEVERAL TIMES BUT THE PROBLEM WOULD NOT CLEAR. REPLACED NR 3 RT FLAP (OUTBD) ACTUATOR. IAW A/C MM CHAPTER 27 AND CMP 275215 COMPLETED FLAP/SLAT CONTROL AND DRIVE SYSTEM - FUNCTIONAL TEST IAW CMP 275101 NO DEFECTS NOTED. FLAP CONTROL SURFACES CHECK WITH CLINOMETER ALL DEG WITHIN LIMITS, 12 DEGREES, 20 DEGREES, 40 DEGREES NO DEFECTS. 2L72 4F RTA53NM 20051013002152005101300215CE 2005 10 13 DXTA200501009 120051008A7332 WARNING LIGHT CESSNA500 560CESSNA 2076750CE BOOST PUMP ILLUMINATED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07333QS 5600333 WHEN BRAKES SET & POWER AT 96.3 PERCENT N1, BEGAN TAKEOFF ROLL; BEFORE REACHING 40 KTS THE RT FUEL BOOST PUMP ON LIGHT ILLUMINATED. TAKEOFF WAS ABORTED. INSPECTED RT FUEL FILTER NO DEBRIS FOUND C/W GROUND RUNS RT GEN CAME ONLINE NORMAL DURING START. C/W POWER OF DAY RUN NO LIGHTS ILLUMINATED ON ANNUNCIATOR PANEL FOR BOOST PUMP OR RT GEN OFF HIGH & NORMAL IDLE CHECKS GOOD ALL READINGS ON RT ENGINE CLOSELY MATCH LT SIDE UNABLE TO DUPLICATE, ALL WORK IAW CE560 MM 73-30 & 24-50. 2L72 4F RTA22CE 20051013002162005101300216 2005 10 13 DXTA200501010 420051008A34178220374412 ADC AMD FALC50FALCON2000 2730170NM NR 1 INOPERATIVE E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07275QS2416 75 ON TAKEOFF ROLL. EXPERIENCED AN ADC FAILURE. TAKEOFF WAS ABORTED. REMOVED AND REPLACED NR 1 ADC, SYSTEM OPERATIONALLY CHECKS NORMAL IN ACCORDANCE WITH FALCON 2000 MAINTENANCE MANUAL CHAPTER 34-100 AND 34-104. ALL WORK PERFORMED BY DUNCAN AVIONICS TEB. 2K73 4F RTA50NM 20051013002172005101300217CE 2005 10 13 DXTA200501011 120051008A3210 LANDING GEAR CESSNA750 750 2076810CE NOISY E DXTAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 GL07941QS 7500141 BANG CAN BE FELT AND HEARD FROM NOSE AREA DURING FLIGHT ABOUT EVERY 10 MINS IN CLIMB & DESCENT EVERY 15-20 IN CRUISE. REQUIRING TEST FLIGHT OCF FOR FURTHER EVALUATION. PERFORMED GEAR SWING MULTIPLE TIMES AND COULD NOT DUPLICATE PROBELM. CONFIRMED THE GEAR BUMP CHECKLIST HAD BEEN PERFORMED WHEN AT CESSNA WITH SAMES DISCREPANCY PRIOR TO CMH ARRIVAL. INSPECTED ALL GEAR ROLLERS FOR FREEDOM OF MOVEMENT AND HOOK / ROLLER INTERFACE. 2L72 4J RTT00007WI 20051013002182005101300218EA 2005 10 13 QXEA200501291 120050917A5230 SEAL CNDAIRCL600 CL6002C10 1390015EA CARGO DOOR TORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09617QX 10130 YYC - FORWARD BAGGAGE BAY DOOR EXTERNAL SEAL IS TORN OPEN AT THE FORWARD END AND BUCKLED, NOT SEALING. REPLACED SEAL. OPERATIONAL CHECKS GOOD IAW CMM 52-35-00-300-804-A01. 2L72 4F RTA21EA 20051013002192005101300219EA 2005 10 13 QXEA200501293 120050917A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA BS 969 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09617QX 10130 YYC - FUSELAGE EXTERIOR HAS A NICK AT FS 969 STRINGER 18R. BLENDED THE DAMAGE SMOOTH IAW CRJ-700 SRM 53-51-01-101-001-A01. REPROTECTED AND PAINTED AREA. 2L72 4F RTA21EA 20051013002212005101300221EA 2005 10 13 QXEA200501302 120050917A5260 SKIN CNDAIRCL600 CL6002C10 1390015EA AIRSTAIR DOOR CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09617QX 10130 YYC - PASSENGER AIRSTAIR DOOR AFT SKIN IS CRACKED UNDER HANDRAIL STOWAGE SPRING BRACKET. REPAIRED IAW REO 670-52-11-104. 2L72 4F RTA21EA 20051013002232005101300223EA 2005 10 13 QXEA200501304 120050917A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA BS 981 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09617QX 10130 YYC - CENTER FUSELAGE SKIN DAMAGED AT FS 981 STR 27 LOWER SKIN AT 2 LOCATIONS. REPAIRED IAW REO 670-53-00-014. BLENDED DAMAGED AREA MATERIAL LOSS OF .015". FINISH RESTORED. 2L72 4F RTA21EA 20051014000012005101400001NE 2005 10 14 0501529941 220051010A7320654233 VALVE DOUG DC9 DC932 3022066WP PWA JT8 JT8D17 52049NE ENGINE LEAKING A NWAAE ENGINE SHUTDOWN KRJFLUID LOSS PARTIAL RPM/PWR LOSS WARNING INDICATION APAPPROACH 1 GL013324L4430812406 47103 707907 DURING FINAL APPROACH ENGINE NR 2 ROLLED BACK TO 30 PERCENT N2 AND WOULD NOT RESPOND TO THROTTLE INPUT. ENGINE NR 2 WAS SHUTDOWN AND FLIGHT CREW PERFORMED AN UNEVENTFUL LANDING. MAINTENANCE FOUND A FUEL LEAK AT P&D VALVE COUPLING. MAINTENANCE REPLACED ENGINE NR 2 P&D VALVE. 2L72 4F4 F A6WE E2EA 20051014000032005101400003NM 2005 10 14 SWAA053125 120051011A53126546568 BULKHEAD BOEING737 7373H4 1384600NM BS 1016 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED 1/4D CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT DOME CAP, 1 O'CLOCK POSITION. REPAIRED WEB PER SWA EA. 2L72 4F RTA16WE 20051014000112005101400011NM 2005 10 14 SWAA053133 120051010A5753 SKIN BOEING737 7373H4 1384600NM RT WING FOREFLAPDELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29606SW 1882 27926 DURING SCHEDULED C3 CHECK, FOUND RT WING INBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM. 2L72 4F RTA16WE 20051014000132005101400013NM 2005 10 14 CALA0500348 120051011A5330147A3400Y4 SKIN BOEING737 737824 13844BZNM BS 887-970 DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2773251 30582 FUSELAGE LOWER SKIN AT STA 887 TO 970 AND BETWEEN STR 23 LT TO STR 26 LT HEAVILY DAMAGED. REPLACED SKIN AT STA 886-1016 & STR 23L-23R PER ECRA 5331-01198. 2L72 4F RTA16WE 20051014000142005101400014NM 2005 10 14 CALA0500349 120051011A5330147A31103 SKIN BOEING737 737824 13844BZNM BS 887-947 DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2773251 30582 FUSELAGE UPPER SKIN AT STA 887-947 AND BETWEEN STR 14 LT TO STR 23 LT HEAVILY DAMAGED. REPLACED UPPER SKIN AT STA 886-1016, STR 14L-23L PER ECRA 5331-01198. 2L72 4F RTA16WE 20051014000152005101400015NM 2005 10 14 CALA0500350 120051011A5330147A321Y46 STRINGER BOEING737 737824 13844BZNM BS 887-1016 UNKNOWN A CALAK NONE O OTHER ININSP/MAINT 1 SW2773251 30582 STRINGER 20L STA 887-1016 REPLACED PER ECRA 5331-01198. 2L72 4F RTA16WE 20051014000172005101400017NM 2005 10 14 CALA0500352 120051011A53131473211Y41 STRINGER BOEING737 737824 13844BZNM BS 887-1016 UNKNOWN A CALAK NONE O OTHER ININSP/MAINT 1 SW2773251 30582 STRINGER 22L, AT STA 887-1016 REPLACED PER ECRA 5331-01198. 2L72 4F RTA16WE 20051014000192005101400019NM 2005 10 14 CALA0500355 120051011A531514T5107 FLOORBEAM BOEING767 767424ER 1385270NM BS 303 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2766051 29446 CABIN FLOORBEAM CORRODED AT BS 303 LBL 18 TO 35. REPAIRED FLOORBEAM PER SRM 53-00-51, FIG 201. 2L72 4F RTA1NM 20051014000202005101400020NM 2005 10 14 CALA0500356 120051011A5315141T5108 FLOORBEAM BOEING767 767424ER 1385270NM BS 325 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2766051 29446 CABIN FLOORBEAM CORRODED AT BS 325 LBL 26 TO 52. REPAIRED FLOORBEAM PER SRM 51-10-02 AND 51-20-01. 2L72 4F RTA1NM 20051014000212005101400021NM 2005 10 14 CALA0500358 120051011A3350ADD71701100 BATTERY PACK BOEING737 737824 13844BZNM EMERGENCY LIGHT INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2724202 30429 LEFT SEATS 11-14 AND OVERWING HATCH EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK PER AMM 33-51-06. 2L72 4F RTA16WE 20051014000222005101400022NM 2005 10 14 CALA050357 120051011A3350ADD71701100 BATTERY PACK BOEING737 737824 13844BZNM EMERGENCY LIGHT INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2724202 30429 L2 DOOR EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK PER AMM 33-51-06. 2L72 4F RTA16WE 20051014000232005101400023NM 2005 10 14 CALA05354 120051011A5315141T5108 FLOORBEAM BOEING767 767424ER 1385270NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2766051 29446 CABIN FLOORBEAM CORRODED AT BS 325 LBL 33 - LBL 55. REPAIRED FLOORBEAM PER SRM 53-00-51. 2L72 4F RTA1NM 20051014000242005101400024NM 2005 10 14 PIDA20050177 120050930A5315 FLOORBEAM BOEING737 737228 13844AGNM BS 967 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 BS 967 FLOORBEAM HAS CORROSION FROM LBL 42 TO LBL 48. REPLACED DAMAGED SECTION OF FLOORBEAM PER EA 53-268. 2L72 4F RTA16WE 20051014000252005101400025NM 2005 10 14 PIDA20050176 120051010A5315 FLOORBEAM BOEING737 737228 13844AGNM BS 986 CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 BS 986 FLOORBEAM HAS CORROSION AT FLOORBOARD ATTACH LOCATIONS LBL 48 TO RBL 48. REPLACED DAMAGED SECTION OF FLOORBEAM PER EA 53-301. 2L72 4F RTA16WE 20051014000262005101400026EU 2005 10 14 DHL2005366004 120050918A2610 WARNING LIGHT AIRBUS300 A300B4203 3930306EU FALSE INDICATIONA DHLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01366DH 249 ABORTED T/O AT 100 KTS DUE TO SMOKE LIGHT ON MWP OAT 24 DEG CELSIUS MAX BRAKE TEMP 320. REMOVED AND REPLACED DISTRIBUTION BOX PRECAUTIONARY IAW MMS 26-11-00. DEFER 4R SMOKE DET IAW MEL 26-17-01 PLACARD INSTALLED CAT B DMI 22481. RTO WITHIN LIMITS IAW AOM CH 5.4. REF DMI 22481 SMOKE LIT ON MASTER WARNING PANEL ON TAKEOFF. REMOVED AND REPLACED MASTER WARNING CONT AS PRECAUTIONERY IAW 33-15-00 OPS CHECK OK DMI 22481. STILL OPEN. 2L72 4F RTA35EU 20051014000272005101400027NM 2005 10 14 SWAA053135 120051011A5753 SKIN BOEING737 7373H4 1384600NM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 2502 27697 DURING SCHEDULED RON CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM. 2L72 4F RTA16WE 20051014000282005101400028NM 2005 10 14 SWAA053136 120051011A53226546529 SHEAR TIE BOEING737 7373H4 1384600NM BS 500C CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500C, RBL 17. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051014000302005101400030NM 2005 10 14 SWAA053138 120051011A53226546547 SHEAR TIE BOEING737 7373H4 1384600NM BS 907 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 907, BETWEEN STR 19L TO STR 20L. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051017000022005101700002EA 2005 10 17 QXEA200501341 120051007A3040 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE WINDSHIELD HEAT ILLUMINATED A QXEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM09603QX 10011 RT WINDSHIELD CAUTION MESSAGE. CYCLED IAW THE CHECKLIST AND MESSAGE WENT AWAY FOR 2 MINUTES THEN RE-APPEARED. MAINTENANCE CHECKED MDC FOR FAULTS, NO FAULTS FOUND. CYCLED POWER TO THE RT WINDSHIELD HEAT SYSTEM AND PERFORMED OPERATIONAL CHECK IAW TASK 30-46-06-710-801-A01. SYSTEM CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2L72 4F4 FRTA21EA EOOO63EN 20051017000042005101700004WP 2005 10 17 DJFA2005148 220051006A7261 LINE CESSNA650 650 2076802CE GARRTTTPE731TFE7313C WP RT ENGINE LEAKING E DJFAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA23397CW100822167 6500107 P87328C CREW REPORTED THAT RT ENGINE OIL LOW PRESSURE ANNUNCIATOR HAD ILLUMINATED WHILE IN CRUISE FLIGHT APPROX AN HOUR AND A HALF AFTER TAKE OFF. RT ENGINE OIL PRESSURE INDICATED BETWEEN 38 - 25 PSI. POWER TO RT ENGINE WAS REDUCED TO FLIGHT IDLE, AND AN EMERGENCY WAS DECLARED. AC LANDED WITHOUT FURTHER INCIDENT. MAINT DISCOVERED A LOOSE BOLT AT NR 6 ENGINE BEARING OIL RETURN LINE. THE OIL LINE WAS REMOVED AND REINSTALLED WITH A NEW GASKET. THE NR 6 BEARING OIL PRESSURE LINE AND N1 TRANSDUCER COVER PLATE WERE RESEALED. THE ENGINE OIL WAS SERVICED AND A SATISFACTORY OPERATIONAL AND LEAK CHECK WAS PERFORMED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 F A9NM E6WE 20051017000052005101700005EU 2005 10 17 09232005A 120050922A3246 TIRE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE MLG FLAT A NSVAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 EA27305CE 202 DURING TAKEOFF, EXPERIENCED STRONG YAW TO RT AT +80 KIAS. ABORTED TAKEOFF AND EXITED RUNWAY. SHUTDOWN AND NOTICED NR3 AND NR4 TIRES BLOWN DUE TO MISSING TREAD. FOUND NR1 AND NR2 TIRES FLAT. REMOVED AND REPLACED NR1 TIRE IAW CHAPTER 32-41-05-4 OF THE AMM P/N OFF 5010488-R7-1 S/N OFF MAR92-0297 S/N ON JUN97-2212. NR2 TIRE PN OFF 5010488-1 PN ON 5010488-2 SN OFF UNREADABLE SN ON DEC94-1302/OCT00-3318. NR3 TIRE PN OFF 5010488-1 PN ON 5010488 SN OFF UNREADABLE SN ON FEB95-1348. NR4 TIRE PN OFF 5010488 PN ON 5010488-2 SN OFF MAR95-1375 SN ON MAY96-1833. 2L72 4T4 TRTA52EU E8NE 20051017000062005101700006NE 2005 10 17 C8GA20050022 220051011A7261 LINE BOEING727 727223 1384074NM PWA JT8 JT8D17 52049NE NR 2 ENGINE GBOXLEAKING A C8GAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO29713AA 22469 666201 WHILE IN CRUISE AIRCRAFT EXPERIENCED A LOSS OF NR 2 ENGINE OIL QTY DOWN TO TWO GALLONS. ENGINE WAS SHUTDOWN AS A PRECAUTIONARY. EMERGENCY WAS DECLARED, AIRCRAFT WAS DIVERTED AND LANDED WITHOUT INCIDENT. FOUND LOOSE OIL LINE ON NR 2 ENGINE GEARBOX, SECURED LINE AND PERFORMED LEAK CHECK, NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 20051017000072005101700007EA 2005 10 17 A6WA200540306 120050920A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE BS 621 CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31425AW 7663 LT FS 621 FLOOR SUPPORT ANGLE CRACKED. MAINTENANCE LT FS 621.00, FLOOR SUPPORT ANGLE IAW REO. (M) 2L72 4F4 FRTA21EA E15NE 20051017000082005101700008EA 2005 10 17 A6WA200540303 120050915A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FS 625-640 DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31456ZW 7849 AIRCRAFT DAMAGED BY IMPACT FROM BELT LOADER, LT LOWER SKIN AFT OF CARGO DOOR. REPAIRED FUSELAGE SKIN BY CUTTING OUT DAMAGE AND FABRICATING AND INSTALLING SHIM FILLERS AND EXTERNAL DOUBLER IAW EO. (M) 2L72 4F4 FRTA21EA E15NE 20051017000102005101700010NE 2005 10 17 BA0520 220051012A75326764B040000 BLEED VALVE AIRBUS330 A330323 3930335EU PWA 4168 PW4168A NE NR 2 ENGINE MALFUNCTIONED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19673UW 0337 FLIGHT 1470, PHL-SJU - ON DEPARTURE FROM PHL, RECEIVED ECAM MESSAGES AIR ENG 2 BLEED FAULT, ENG 1 COOL VALVE FAULT, ELEC IDG 2 OIL SYS FAULT. ELECTED TO RETURN TO PHL RATHER THAN PLACE ON MEL. REPLACED THE NR 2 PRESSURE REGULATING VALVE AND DRAINED IDG 2 OIL TO PROPER LEVEL. ENGINE 1 COOL VALVE MEL WAS ALREADY APPLIED TO THIS AIRCRAFT. 2L72 4F4 FRTA46NM 20051017000152005101700015NM 2005 10 17 TSAA0549046 120051009A49204419215 FCU BOEING737 73773A 1384606NM GE CFM56 CFM567B24 NE APU DEFECTIVE A TSAAK NONE J WARNING INDICATION ININSP/MAINT 1 WP13739AL 28500 DURING PREFLIGHT CHECK, APU AUTO SHUTDOWN ON RAMP, SENSING LOW OIL PRESSURE. T/S IAW FIM 49-90/802-803 TROUBLESHOT IAW FIM. REPLACED APU LUBE MODULE TASK 49-91-11-4/PG. 1- REPLACED FCU IAW 49-31-11-4/SEC 4 199286 ITEM 2/3. LEAK AND OPS CHECK GOOD. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA16WE E00055EN 20051017000162005101700016NM 2005 10 17 TSAA0549045 120051008A499038762552 SWITCH BOEING737 73773A 1384606NM GE CFM56 CFM567B24 NE APU DEFECTIVE A TSAAO OTHER J WARNING INDICATION NRNOT REPORTED 1 WP13739AL 28500 AUTO SHUTDOWN LOW OIL PRESSURE OCCURRED ON RAMP. TROUBLESHOT IAW FIM 49-90-00-810-803 FOUND APU LOP INOP. REPLACED APU LOP, OPS CHECK OK. LEAK CHECK OK. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA16WE E00055EN 20051017000172005101700017WP 2005 10 17 DHL2005806535 120050909A5330 SKIN DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE BS 1265 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH87034 46002 LWR FUSELAGE EXTERIOR SKIN CORRODED, BS 1265.000 L-36 (MAJOR REPAIR). PERFORMED MAJOR REPAIR, DWG U80-R28 REV. IR DATED 08-08-05. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-3-0. REMOVED CORROSION IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG. 2P. CUT OUT CORRODED SECTION IAW DWG U80-R28. PERFORMED NDT INSP IAW NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER, TRIPLER, INTERNAL FINGER DOUBLER AND FILLER IAW DWG U80-R28. CLEANED, TREATED AND PRIMED AREA, REPAIR PARTS IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG. 9. INSTALLED REPAIR PARTS IAW DWG U80-R28, SRM (TORQUE). 2L74 4F4 FRT4A25 E2GL 20051017000202005101700020WP 2005 10 17 DHL2005806519 120050828A5310 DOOR DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE PAX MISREPAIRED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01806DH87034 46002 AFT PASSENGER DOOR REPAIR ON AFT UPPER JAMB CORNER IS NOT IAW SR08530021 STA 1660.000 L-18L TO L-12L. PERFORMED MAJOR REPAIR IAW AD200-20-08, DWG NR SR08530021, 5750776 (S/B 53-075). REMOVED EXISTING REPAIR IAW SRM 51-1-21, SRM 51-1-20D. PERFORMED DETAIL VISUAL INSP. NO CRACK NEITHER CORROSION FOUND. FABRICATED REPAIR DOUBLER AND REPAIR TRIPLER IAW DWG SR08530021, SRM 51-1-4 PG. 1. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG. 9. INSTALLED REPAIR PARTS IAW MFG DWG NR SR08530021, SRM 51-1-21, SRM 51-1-20D, SRM 51-3-0, SRM 51-3-1. 2L74 4F4 FRT4A25 E2GL 20051017000222005101700022NM 2005 10 17 05FDEA03396 120051012A3210 CYLINDER DOUG MD11 MD11 3023602NM ZONE 700 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 CENTER LANDING GEAR UNLOCK CYLINDER RIGHT HAND SUPPORT BRACKET FOUND CHAFED. REMOVED AS PER AMM 32-38-02. CHAFFING MARK SMOOTHENED OUT AND FOUND WITHIN LIMIT AS PER DRAWING AEA0661-2. SUPPORT BRACKET RE-INSTALLED AS PER AMM 32-38-02. REPAIR IS CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051017000232005101700023EU 2005 10 17 05FDEA03397 120051012A5710 RETAINER AIRBUS300 A300F4605R 3930327EU STATIC WICK LOOSE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25681FE 799 STATIC DISCHARGER RETAINER AT RT WING MOST OUTBOARD IS BAD/LOOSE. COMPLIED WITH EA6-5720-92943 REF N00232. 2L72 4F RTA35EU 20051017000262005101700026EU 2005 10 17 05FDEA03401 120051012A5730 SKIN AIRBUS300 A300B4605R 3930308EU LT WING CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25681FE 799 LEFT WING O/B UPPER SURFACE HAS 4 EA CHAFE MARKS. COMPLIED WITH EA 6-5750-93355 REF N00076. 2L72 4F RTA35EU 20051017000272005101700027EU 2005 10 17 05FDEA03402 120051012A5755 SKIN AIRBUS300 A300B4605R 3930308EU LT WING SPOILER CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25681FE 799 LEFT WING SPOILER NR 2 O/B FWD EDGE 2 EA AREAS THAT ARE CHAFED. COMPLIED WITH EA 6-5750-92961 N00044. 2L72 4F RTA35EU 20051017000282005101700028NM 2005 10 17 05FDEA03404 120051012A5315 FLOORBEAM BOEING727 727100 1384036NM BS 328 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 CORROSION BS 328 FLOORBEAM AT FASTENER HOLES. CORROSION ON FLOORBEAM AT B.S. 328 LBL 22 WAS OUT OF LIMITS REPAIRED FLOORBEAM PER FED EX EA 7-5310-91401. 2L73 4F RTA3WE 20051017000302005101700030NM 2005 10 17 05FDEA03406 120051012A5320 WEB BOEING727 727100 1384036NM BS 640 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 HAYES MOD WEB GOUGED AT BS 640L AT STR 12L AND 14L. 2L73 4F RTA3WE 20051017000312005101700031NM 2005 10 17 05FDEA03407 120051012A5320 WEB BOEING727 727100 1384036NM BS 620 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 HAYES MOD WEB GOUGED AT 9 PLACES BETWEEN STR 5L AND STR 13L BS 620. REPAIRED GOUGES STR 5L AND 13L, BS 620 HAYES MOD WEB PER SRM 53-10-2, 51-40-2, 51-30- 2. 2L73 4F RTA3WE 20051017000332005101700033WP 2005 10 17 05FDEA03414 120051012A5420 BOLT DOUG MD10 MD1010F 3022112WP ZONE 400 SHEARED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25390FE 46624 NR 1 PYLON, UPPER PLUG LOCKING BOLT HEAD SHEARED OFF DURING REMOVAL. REF BOLT P/N AUB7227-1. INSTALLED NR 1 PYLON UPPER PLUG LOCKING BOLT. REF M/M 54-00-01-4 2L73 4F RTA22WE 20051017000342005101700034NM 2005 10 17 05FDEA03415 120051013A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 HORIZONTAL STAB LT BARREL NUT BORE NR 4 FOUND WITH CORROSION. HORIZONTAL STAB BARREL NUT BORE NR 4 LT REPAIRED IAW STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK/ REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 43. MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20051017000362005101700036NM 2005 10 17 05FDEA03417 120051013A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 HORIZONTAL STAB RT BARREL NUT BORE NR 35 FOUND WITH CORROSION. HOR. STAB. BARREL NUT BORE 35 RT REPAIRED IAW STABILIZERS-HORIZONTAL STABILIZER- BARREL NUT BORE REWORK/ REPAIR AD 2003-22-08 EA1-5510-87628, ATTACHMENT 45. MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20051017000372005101700037NM 2005 10 17 SB05131 120051013A335020121 POWER SUPPLY BOEING737 737301 1384611NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US 23555 MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT SEAT ROWS 12 THROUGH 16 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20051017000392005101700039NM 2005 10 17 SWAA053140 120051011A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 380 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051017000402005101700040NM 2005 10 17 SWAA053141 120051011A53306545776 SKIN BOEING737 7373A4 1384585NM BS 947 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29679AA 23291 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 21L. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20051017000412005101700041NM 2005 10 17 SWAA053142 120051010A324226123021 BRAKE ASSY BOEING737 7377H4 1384404NM MLG W/W SEIZED A SWAAO OTHER O OTHER TXTAXI/GRND HDL 1 SW29716SW 27850 AIRCRAFT DIFFICULT TO PUSH BACK, AFTER TUG DISCONNECT- AIRCRAFT WOULD NOT MOVE WITH NORMAL BREAKAWAY THRUST. FOUND NR 4 MAIN BRAKE SEIZED & DAMAGED. REMOVED AND REPLACED NR 4 MAIN BRAKE ASSY AND NR 4 MAIN TIRE/WHEEL ASSY PER MM. 2L72 4F RTA16WE 20051017000422005101700042NM 2005 10 17 SWAA053122 120051011A53306545777 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051017000442005101700044WP 2005 10 17 AALA20050663 120051011A3350P4010051111 MODULE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21452AA 49553 LGA - EMERGENCY EGRESS LIGHTS AT ROWS 21 TO AFT OF AIRCRAFT INOPERATIVE. REPLACED CHARGER AND BATTERY PACK AT MID POSITION ABOVE ROW 20DEF FOR EMERGENCY EGRESS LIGHTS AT ROWS 21 TO AFT OF AIRCRAFT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051017000472005101700047WP 2005 10 17 AALA20050657 120051007A335050030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW219302B 49528 ORD - CABIN AND COCKPIT EMERGENCY LIGHTS INOPERATIVE. RECHARGED BATTERIES AND REPLACED BATTERY PACK AT B5 23. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20051017000502005101700050NM 2005 10 17 AALA20050662 120051010A3397 CONNECTOR DOUG MD80 MD83 3023681NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW219414W 53189 SFO - EMERGENCY LIGHT CONNECTOR AT SEAT 15D IN PINNED. REPAIRED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 15D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RT 20051017000512005101700051NM 2005 10 17 AALA20050666 120051012A3350 BATTERY PACK DOUG MD80 MD83 3023681NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW219413T 53188 IAH - COCKPIT AND GALLEY EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR COCKPIT AND GALLEY EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RT 20051017000542005101700054NM 2005 10 17 AALA20050656 120051005A3397 WIRE BOEING757 757231 1384950NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21717TW 28485 DFW - EMERGENCY ESCAPE PATH LIGHT IN AFT CABIN INOPERATIVE. REPLACED AFT FLOOR LIGHT POWER STRIP FOR EMERGENCY ESCAPE PATH LIGHT IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20051017000552005101700055NM 2005 10 17 AALA20050661 120051011A3350P4010049 BATTERY PACK BOEING757 757223 1384957NM EMEGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21660AM 25294 SFO - SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 16 TO 25 INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 16 TO 25. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20051017000592005101700059NM 2005 10 17 SWAA053145 120051012A53306545767 SKIN BOEING737 7373H4 1384600NM BS 390 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 390, STR 17R. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20051017000622005101700062NM 2005 10 17 SWAA053148 120051012A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 706 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 706, STR 2L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051017000652005101700065NM 2005 10 17 SWAA053151 120051012A3350BR2013 LIGHT BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29368SW 26579 EEPLS STRIP LOOSE AT FWD END. REMOVED AND REPLACED STRIP PER MM. 2L72 4F RTA16WE 20051017000662005101700066NM 2005 10 17 SWAA053152 120051012A53116520723 FRAME BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29506SW 24183 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, AFT BOTTOM DOOR STOP FITTING. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20051017000682005101700068NM 2005 10 17 SWAA053154 120051012A55536547450 FITTING BOEING737 7373H4 1384600NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED D-CHECK, FOUND LT & RT VERTICAL STAB ATTACH FITTINGS CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER. 2L72 4F RTA16WE 20051012000442005101200044EA 2005 10 12 COMA0560542 120051009A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01814CA 7387 FLIGHT 5707 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2L72 4F RTA21EA 20051012000462005101200046EU 2005 10 12 AALA20050649 120050928A2530 COFFEEMAKER AIRBUS300 A300B4605R 3930308EU GALLEY SMOKE A AALAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SW217083A 645 SDQ - INFLIGHT SMOKE STARTED COMING OUT OF THE BACK OF COFFEEMAKER NR 1. FOUND E-58 LABEL TAG BURNING. EXTINGUISHED LABEL TAG AND PLACARD COFFEEMAKER NUMBER 1. REPLACED COFFEEMAKER NUMBER 1. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20051012000482005101200048NM 2005 10 12 AALA20050650 120051004A3231 SEQUENCE VALVE BOEING757 757223 1384957NM NLG DOOR INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21698AN 26980 MIA - INFLIGHT GEAR DOORS LIGHT ILLUMINATED AFTER GEAR RETRACTION. REPLACED RETRACT LINE HYDRAULIC FUSE AND NOSE LANDING GEAR DOOR SEQUENCE VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20051012000502005101200050EA 2005 10 12 SWIA200515661 120051007A274170609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07963SW 7865 MACH TRIM AND STAB TRIM MASTER CAUTION MSGS. REPLACED HSTCU IAW MM 27-41-00, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051012000522005101200052EA 2005 10 12 SWIA200515663 120051006A274170623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07459SW919 919 7782 NR 2 STAB CHANNEL WILL NOT ENGAGE. REPLACED HSTA AND MOTOR CONTROL IAW AMM 27-40-00, 27-42-01, 27-42-05. OPERATIONAL CHECK GOOD. P/N 8396-3, S/N OFF 969. 2L72 4F RTA21EA 20051012000542005101200054EA 2005 10 12 SWIA200515665 120051007A5610 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAO OTHER O OTHER CRCRUISE 1 NM07709BR 7850 F/O SIDE WINDOW CRACKED. REPLACED F/O SIDE WINDOW IAW MM 56-00-00 AND 56-11-01 AND 56-12-01. P/N NP139322-3, S/N OFF 03161H6059. 2L72 4F RTA21EA 20051012000592005101200059 2005 10 12 DHL2005365006 420050922A34189654020007 SENSOR AIRBUS300 A300B4203 3930306EU AOA MALFUNCTIONED A DHLABA EMER. DESCENT UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01365DH 149 STALL WARNING AT TAKEOFF WITH CONTINUOUS STICK SHAKER FROM TAKEOFF TO LANDING. REMOVED AND REPLACED AOA PROBE. OPS CHECKS OK IAW MM 27-36-15. 2L72 4F RTA35EU 20051012000602005101200060NM 2005 10 12 DHL2005788013 120050927A3260 SWITCH BOEING727 727214 138407RNM NLG DOOR OUT OF ADJUST A DHLAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01788AT 21958 AT 340 KIAS RED LANDING GEAR DOORS LIGHT ON FWD PANEL ILLUMINATED & AMBER NOSE GEAR DOOR WARNING LIGHT ON S/O PANEL ILLUMINATED. FOUND NOSE GEAR DOOR SWITCH OUT OF ADJ. ADJ SWITCH IAW MM 32-62-11, OPS CHECK GOOD. 2L73 4F A3WE 20051012000622005101200062NM 2005 10 12 DHL2005749000 120050929A335037067001 BATTERY BOEING727 7272J0 138407ENM EMERGENCY LIGHT WEAK A DHLAO OTHER J WARNING INDICATION CRCRUISE 1 SO01749DH 22013 EMERGENCY EXIT LIGHT OVER MAIN CABIN DOOR ILLUMINATED IN FLIGHT. FOUND BATTERIES WEAK. REPLACED BOTH EMERGENCY EXIT LIGHT BATTERIES AND RESEATED UNIT. OPS CHECKS NORMAL IAW B727 M/M CH 33-50-71. TWO EA P/N 37067-001. 2L73 4F RTA3WE 20051012000642005101200064EA 2005 10 12 COMA0560545 120051010A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01962CA 7123 FLIGHT 5400 - FLAPS FAIL CAUTION. CND, INSPECTED FLAPS SYSTEM AND FOUND NO FAULTS. 2L72 4F RTA21EA 20051012000722005101200072EA 2005 10 12 SWIA200515641 120051004A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07957SW 7829 ROW 10 CEILING EMERGENCY LIGHT INOP. RELAMPED ROW 10 EMERGENCY LIGHT, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051012001272005101200127EA 2005 10 12 COMA0560539 120051009A3230601R751461 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01967CA23873 7134 FLIGHT 5062 - GEAR DISAGREE WARNING. REPLACED THE NLG SELECTOR VALVE. 2L72 4F RTA21EA 20051012001292005101200129NM 2005 10 12 UPS05M45582 120050720A5313AEA75332 LONGERON DOUG MD11 MD11F 3023600NM BS 1239-1256 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01256UP 48405 INSPECTION TYPE:C, CABIN ANGLE FITTING BETWEEN STA 1239-1256 LONGERON 27 RT FOUND CORRODED. CORROSION REMOVED AT CABIN AREA STA 1239 TO 1256, FOUND OUT OF LIMIT. ORIG THK 0.238" & MAT REMOVED IS 0.090" PER SRM 53-00-01 F3.V1 R.37. ANGLE FITTING BRACKET REMOVED & FAB LONGERON AEA7533-2 PER EN1419-05 & DOUGLAS DWG AEA7533. NEW FAB LONGERON PICK UP HOLE PER SRM 51-31-01V.2.R37. INSTALLATION NEW FAB LONGERON CUTOUT PER 51-33-01.V2.R37-SATIS. 2L73 4F RTA22WE 20051012001312005101200131NM 2005 10 12 UPS05M45591 120051009A2560 SMOKE GOGGLES DOUG MD11 MD11F 3023600NM COCKPIT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01253UP 48439 SECOND OBS POSITION SMOKE GOGGLE LENS CRACKED. REPLACED SMOKE GOGGLES. 2L73 4F RTA22WE 20051013000012005101300001EU 2005 10 13 10072005A 120051001A2910GPP125012 PRESSURE SWITCH SAAB SF340 340B 7860101EU HYD SYSTEM MALFUNCTIONED A NSVAB EMER. DESCENT J WARNING INDICATION DEDESCENT 1 EA27339CJ 339 DURING DESCENT HYD LIGHT ILLUMINATED (NO PRESSURE IN MAIN RESERVOIR) DID CHECKLIST, COULD NOT BRING IT BACK TO GREEN. ALSO, DID CHECKLIST FOR MANUAL EXTENSION OF GEAR AND FLAPS, IT DID MAINTAIN HYDRAULIC PRESSURE WITH HAND PUMP. AFTER LANDING, OVERRIDE SWITCH DID WORK AND MAINTAINED PRESSURE. PRESSURE BLEEDS TO ZERO WHEN IN AUTO MODE. REMOVED AND REPLACED HYD PRESSURE SWITCH 9ML IAW SAAB 340 M/M CHAPTER 29-10-45, OPS CHECK GOOD. 2L72 4T RTA52EU 20051013000122005101300012SO 2005 10 13 62309302005 120050903A55111159CSM52025007 RIB GULSTMGV GV 3980116SO RROYCEBR700 BR700710A110 NE STABILIZER DAMAGED E N93AO OTHER O OTHER NRNOT REPORTED 1 SO13506QS 623 ON POST FLIGHT DAMAGE NOTED TO FAIRING ON OUTSIDE PORTION OF RT STABILIZER LOWER SURFACE. 2L72 4F4 FRTA12EA E00057EN 20051013000192005101300019NM 2005 10 13 SWAA053116 120051010A5320BAC15171489 FLOOR SUPPORT BOEING737 7373H4 1384600NM BS 270 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED D CHECK, FOUND COCKPIT FLOOR SUPPORT CORRODED AT BS 270, BETWEEN LBL 11 TO RBL 11, WL 208. REPAIRED FLOOR SUPPORT PER SRM. 2L72 4F RTA16WE 20051013000212005101300021WP 2005 10 13 05FDEA03380 120051011A5744 HINGE FITTING DOUG DC10 DC1010 3022110WP TE FLAP GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 FLAP I/B FITTING HINGE OUTBOARD FOUND DEEP NICK ON INSIDE HOLES ACTUATOR AND LIGHT COROSION ON SURFACE AROUND OF THE HOLE. INSTALLED OVERSIZED BUSHING IAW CMM 57-52-01. 2L73 4F A22WE 20051013000302005101300030NM 2005 10 13 HNAA0500086 120051003A326082400033033 SENSOR DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE MLG FAILED A HNAAA UNSCHED LANDING N FALSE WARNING DEDESCENT 1 EA07931HA4425011250 132 AFTER SELECTING GEAR UP BOTH MAIN GEAR DOOR AMBER LIGHTS, NOSE GEAR RED IN TRANSIT LIGHT AND GEAR SELECTOR HANDLE AMBER LIGHTS REMAINED ON. CYCLED GEAR NO FIX. REMOVED AND REPLACED THE DRAG STRUT SENSOR. 2H72 4T4 TRTA13NM E20NE 20051013000362005101300036WP 2005 10 13 DHL2005806517 120050901A5310 DOUBLER DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE HEAT EXCHANGER CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH87034 46002 PRIMARY HEAT EXCHANGER AFT LWR CORNER ACS STRUCTURAL MODIFICATION DOUBLER CRACKED 0.75 IN STA -12.000 L-27L (MAJOR REPAIR). REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGE SECTION IAW DWG NR U80-R19. PERFORMED DETAIL VISUAL INSP OF REWORKED AREA. NO CRACK OR CORROSION FOUND. FABRICATED REPAIR DOUBLER (AL2024T3 0.050 IN) REPAIR TRIPLER (AL2024T3 0.063 IN) AND FILLER (AL2024T3 0.100 IN) IAW DWG NR U80-R19. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG. 9. INSTALLED REPAIR PARTS IAW DWG3U80-R19, SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1 (TORQUE) 2L74 4F4 FRT4A25 E2GL 20051013000382005101300038WP 2005 10 13 DHL2005806514 120050901A5310 DOUBLER DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE BS -12 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH87034 46002 ITEM REF. NR. 040957: PRIMARY HEAT EXCHANGER AFT LWR CORNER ACS STRUCTURAL MODIFICATION DOUBLER CRACKED 0.750 IN STA -12.000 L-27R. DWG U80-R18 REV. IR DATED 08-08-05. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED SECTION IAW DWG U80-R18. PERFORMED DETAIL VISUAL INSP OF WORKED AREA. NO CRACK NEITHER CORROSION FOUND. FABRICATED REPAIR DOUBLER (AL2024T3 0.050 IN) REPAIR TRIPLER (AL2024T3 0.063 IN) AND FILLER (AL2024T3 0.100 IN) IAW DWG U80-R18. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG. 9. INSTALLED REPAIR PARTS IAW DWG U80-R18, SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1 (TORQUE) 2L74 4F4 FRT4A25 E2GL 20051013000412005101300041NM 2005 10 13 CALA0500328 120051004A533065C35794 SKIN BOEING737 7373T0 1384582NM GE CFM56 CFM563B1 13802NE BS 767 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769333 23571 INSPECTION FOUND A 1.5 INCH CRACK IN FUSELAGE SKIN ON BONDED DOUBLER LINE STA 767 BETWEEN S22R AND S23R. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-00-01, FIGURE 201. 2L72 4F4 FRTA16WE E2GL 20051013000432005101300043NM 2005 10 13 CALA0500330 120050820A5347BAC1508240 SEAT TRACK BOEING757 757224 1384958NM RROYCERB211 RB211535E4B3 NE STA 725-745 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718112 27302 THE RT IB SEAT TRACK HAD CORROSION ON IB FLANGE AT STA 725-745, BL 0. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F4 FRTA2NM E12EU 20051013000492005101300049 2005 10 13 SWAA053120 420051007A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29755SA 27871 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051013000602005101300060NM 2005 10 13 UPS05645551 120051004A21503987505 A/C PACK BOEING767 767300 1385204NM GE CF6 CF680 30025NE RIGHT MALFUNCTIONED A IPXAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO01324UP 27750 INSPECTION TYPE: ETOP IN FLT FL350 M80 AFTER AND DURING TRANSMITTING NOTICE ACRID ODOR IN COCKPIT, NO OTHER INDICATIONS NOTED. COULD NOT ISOLATE OR IDENTIFY SOURCE OF ODOR 1 PACK OPS, PRIOR TO COAST OUT HF COULD NOT BE OPERATED FOR 45 MINS EVENTUALLY TO WORK, SUSPECTED FUMES. RT PACK TEMP RUNS CONTINOUS. DEFER RT PACK IAW MEL 21-51-1-0-1. M311331 REMOVED AND REPLACED RT PACK TEMP CONTROL VALVE IAW AMM 21-51-12-4. THIS CLEARS DMI M311331. 2L72 4F4 FRTA1NM E13NE 20051013000662005101300066WP 2005 10 13 DHL2005806531 120050902A5751 SKIN DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE LT AILERONS CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH87034 46002 LT OB AILERON UPPER PLATING INTERNAL SKIN CORRODED (STA XA 724.000-756.000) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 57-8-1 FIG. 4 PG. 9, DACO DWG NR 5763133. REMOVED CORROSION ON INTERNAL SKIN OF LT OB AIL UPPER PLATING IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG. 16. REMOVED CORRODED PANEL PLATING IAW SRM 57-1-0 PG. 1, SRM 51-1-21. FABRICATED NEW PLATING (AL2024T3 0.020 IN) AND DOUBLER (2024T3 0.046 IN) IAW SRM 57-8-1 FIG. 4 PG. 9 ITEM (F)(G), DWG 5763133. BONDED BOTH PARTS WITH HYSOL IAW SRM 51-1-9. CLEANED TREATED AND PRIMED AREA AND NEW PLATING INNER FACE IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG. 9. INSTALLED NEW PANEL PLATING IAW SRM 51-1-21. 2L74 4F4 FRT4A25 E2GL 20051013000732005101300073WP 2005 10 13 UPS05845593 120050830A5510 STRUCTURE DOUG DC8 DC873F 302199FWP HORIZONTAL STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE:C3 EXFOLIATION TYPE CORROSION AROUND FASTENER HOLES FOR THE RT HORIZONTAL L/E TOP SURFACE FROM STA XFS 78.750 TO XFS 266.250. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SAA SK 801-804773. 2L74 4F RT4A25 20051013000752005101300075WP 2005 10 13 UPS05845595 120050912A534036471172N FITTING DOUG DC8 DC873F 302199FWP BS 960 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE:C3 BATHTUB FITTING CRACKED AT LT L24L WW STA 960. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-3-0, 51-1-20D, AND DWG 56 43117. 2L74 4F RT4A25 20051013000932005101300093NM 2005 10 13 SWAA053072 120051005A5753 SKIN BOEING737 7373A4 1384585NM TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29677AA 23289 DURING SCHEDULED C4 CHECK, FOUND RT WING OTBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM. 2L72 4F RTA16WE 20051013001022005101300102NM 2005 10 13 05FDEA03265 120051006A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 FOUND CRACK INDICATION ON LEFT HAND TANK AT END OF STRINGER 10 (UPPER STRINGER). REPAIR CARRIED OUT AS PER SRM 57-20-00. 2L73 4F RTA22WE 20051013001112005101300111WP 2005 10 13 05FDEA03272 120051007A5712 RIB DOUG DC10 DC1010 3022110WP ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE LT WING FIXED L/E COMPT AT STA XORS 347 ZONE 518 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET3 AND 4 VOL I , INSTALL REPAIR ANGLE -35. 2L73 4F A22WE 20051013001242005101300124WP 2005 10 13 05FDEA03297 120051007A5712 RIB DOUG DC10 DC1010 3022110WP RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE RT WING FIXED L/E COMPT AT STA XORS 762 ZONE 625 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 3 AND 4 VOL I, INSTALL REPAIR ANGLE -35. 2L73 4F A22WE 20051013001252005101300125NM 2005 10 13 05FDEA03298 120051007A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 CRACK INDICATION ON RIGHT WING TANK AT END OF STRINGER 42, LOWER STRINGER. SLOTTED OUT AS PER SRM 57-20-00 FIGURE 10 VOLUME I. NEW SPLICE ANGLE MACHINED AS PER DRAWING ARB 2570 AND INSTALLED AS PER SRM 51-34-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS GMM 6-2-100. 2L73 4F RTA22WE 20051013001682005101300168WP 2005 10 13 05FDEA03307 120051007A5340 FITTING DOUG DC10 DC1010 3022110WP BS 1159 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 CAC FOUND ONE FITTING AT STA 1159 BETWEEN L=38 AND L=39 RT SIDE ONE CRACK 3 INCH LONG. REPAIR IAW SRM 53-40-00 FIG 8. 2L73 4F A22WE 20051013001692005101300169WP 2005 10 13 05FDEA03309 120051007A5330 SKIN DOUG DC10 DC1010 3022110WP BS 295-285 BUCKLED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LWR FUSELAGE NOSE AREA LT SIDE FROM STA 295 TO 285 FOUND BUCKLING SKIN WITH NR 3 DENT (0.286"X1"), (0.176"X1"), (0.080"X1 1/4). INSTALLED REPAIR DOUBLER IAW SRM 53-00-01 FIG 4. 2L73 4F A22WE 20051013001762005101300176NM 2005 10 13 SWAA053080 120051006A335007912 COVER BOEING737 7377H4 1384404NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29774SW 27882 EEPLS TRACK COVER LOOSE AT FWD END. SECURED COVER PER MM. 2L72 4F RTA16WE 20051013001812005101300181NM 2005 10 13 QXEA200501327 120050926A5710 PLATE BOMBDRDHC8 DHC8402 1390042NM RT WING CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09401QX 4031 PDX: RT WING STRESS PANEL LADDER PLATE AFT ROW HAS A SCREW HOLE WITH PITTING CORROSION THAT HAS BEEN BLENDED BEYOND LIMITS. LOCATED AT YW 157.825, APPROX DEPTH IS .017". MAINTENANCE HFEC INSPECTED BLENDED AREA FOR CRACKS IAW Q400 NDTM PART 6, TASK 51-00-02-250-801. NO CRACKS NOTED. REPAIRED IAW EA 6-57-377, PG 6, STEPS 1-7. SANDED FASTWELD DOWN SMOOTH. 2H72 4T RTA13NM 20051013001832005101300183EA 2005 10 13 QXEA200501307 120050917A5751 SKIN CNDAIRCL600 CL6002C10 1390015EA RT AILERON CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09617QX 10130 YYC - RIGHT AILERON UPPER NAD LOWER LEADING EDGE SKIN HAS CHAFED MARKS. REMOVED CHAFFING IAW CRJ-700 SRM 51-12-00-001-001-A01. FINISH RESTORED. 2L72 4F RTA21EA 20051013001852005101300185EA 2005 10 13 QXEA200501292 120050917A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA BS 724 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09617QX 10130 YYC - FUSELAGE EXTERIOR HAS SCRATCH IN THE PAINT 3" LONG AT FUSELAGE STATION 724 STRINGER 8 LEFT HAND. REPAIRED IAW CRJ-700 SRM 51-12-00-001-801-A01. AREA REPROTECTED AND PAINTED. 2L72 4F RTA21EA 20051013001882005101300188NE 2005 10 13 B65A105845 220050814A73149A2045 PUMP UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE FUEL SYSTEM UNSERVICEABLE B B65AO OTHER J WARNING INDICATION CRCRUISE 1 GL13135CR 0164 PART FAILED IN FLIGHT, REPLACED PART. 1G72 3U3 U H88EU E34NE 20051013001902005101300190SW 2005 10 13 ALGA105864 120050826A6220204011116001 NUT BELL 212 212 1181420SW ALLSN 250C 250C30 03013GL MAIN ROTOR CRACKED B ALGAK NONE O OTHER ININSP/MAINT 1 SW03XATRP 30869 CRACK INDICATION, REPLACED AS REQUIRED. 1G71 4U3 U H4SW E1GL 20051014000062005101400006NM 2005 10 14 SWAA053128 120051011A53226546538 SHEAR TIE BOEING737 7373H4 1384600NM BS 639 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 639, BETWEEN STR 7L TO STR 8L. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051014000072005101400007NM 2005 10 14 SWAA053129 120051011A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 685 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 685, STR 4L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051014000082005101400008NM 2005 10 14 SWAA053130 120051011A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 706 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 706, STR 10R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051014000102005101400010NM 2005 10 14 SWAA053132 120051009A53306545775 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29505SW 24182 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT AFT CARGO DOOR CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051014000182005101400018NM 2005 10 14 CALA0500353 120051011A5313147A3215U1 STRINGER BOEING737 737824 13844BZNM BS 887-1016 UNKNOWN A CALAK NONE O OTHER ININSP/MAINT 1 SW2773251 30582 STRINGER 23L AT STA 887-1016 REPLACED PER ECRA 5331-01198. 2L72 4F RTA16WE 20051017000032005101700003EU 2005 10 17 SB05129 220051011A72009325M85G04 ENGINE BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU ZONE 500 FAILED A USAAEA ENGINE SHUTDOWN UNSCHED LANDING JBYWARNING INDICATION SMOKE/FUMES/ODORS/SPARKS ENGINE STOPPAGE CLCLIMB 1 EA19778AU4133141331 24980 724408 PIT - FLT 391 - ON CLIMBOUT FROM PIT, AT FL140, CREW REPORTED A LOUD BANG FROM THE NR 1 ENGINE. SIMULTANEOUSLY, SMOKE FILLED THE COCKPIT, THE NR 1 ENGINE OVERTEMP LIGHT ILLUMINATED AND THE AIRCRAFT YAWED. ENGINE CAME TO AN ABRUPT STOP. CREW SECURED THE ENGINE IN THE OFF POSITION AND DECLARED AN EMERGENCY. FLIGHT RETURNED TO FIELD AT PIT WITHOUT FURTHER INCIDENT. TOTAL SINGLE ENGINE TIME WAS APPROXIMATELY 15 MINUTES. MAINTENANCE REPORTED THE ENGINE FAILURE WAS CONTAINED WITH SOME METAL FOUND IN THE TAILPIPE. REMOVED AND REPLACED THE NR 1 ENGINE ASSEMBLY PER JOB CARD JK71-00-01. OPERATIONAL CHECK AND LEAK CHECK GOOD. 2L72 4F4 FRTA16WE E21EU 20051017000092005101700009EA 2005 10 17 A6WA200540304 120050919A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FS 621-625.3 CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31425AW 7663 FOUND RT SIDE FS 621 TO 625.3 INTERCOSTAL AT STRINGER 142 IS CRACKED NEAR RADIUS APPROX .80 INCH LONG. MAINTENANCE REMOVED CRACKED INTERCOSTAL AND INSTALLED NEW INTERCOSTAL IAW SRM. (M) 2L72 4F4 FRTA21EA E15NE 20051017000112005101700011SW 2005 10 17 2005FA0001404 120051011A5310206031200001 BEAM BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL STA 120 CRACKED B MHNAK NONE O OTHER ININSP/MAINT 1 SO212763N11284 2744 AN INSPECTION WAS CONDUCTED ON THE UPPER BOX BEAM OF THE CABIN. UPON REMOVAL OF THE INSULATION BLANKET, MULTIPLE CRACKS TO THE BOX BEAM ASSY WAS DISCOVERED. THE AC HAS BEEN INVOLVED IN 2 INCIDENTS. 1G71 3U3 U H2SW E4CE 20051017000252005101700025EU 2005 10 17 05FDEA03400 120051012A5753 SKIN AIRBUS300 A300F4605R 3930327EU TE FLAP CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25681FE 799 LEFT WING TRAILING EDGE SUBSTRUCTURE LOWER SURFACE 7 EA RIVET HEADS CHAFING INTO UPPER SURFACE, INTO THE O/B FLAP (LOCATED BETWEEN SPOILER 3 AND 4) DAMAGE ON SUBSTRUCTURE AND ON FLAP. COMPLIED WITH EA 6-5750-93356 REF N00077. 2L72 4F RTA35EU 20051017000292005101700029NM 2005 10 17 05FDEA03405 120051012A5313 STRINGER BOEING727 727100 1384036NM BS 782 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 UPPER LOBE INTERIOR SIDE OF STRINGER IS DAMAGED BS 782 STR 4L. REPAIRED STRINGER AT B.S. 782 STR 4L PER SRM 53-10-1. 2L73 4F RTA3WE 20051017000462005101700046NM 2005 10 17 AALA20050665 120051012A3350 MODULE BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21625AA 24583 MIA - SEAT MOUNTED EMERGENCY ESCAPE LIGHTS FROM SEAT 25 TO AFT GALLEY INOPERATIVE. REPLACED AFT BATTERY CHARGER AND BATTERY FOR SEAT MOUNTED EMERGENCY LIGHTS FROM SEATS 25 TO AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20051017000482005101700048WP 2005 10 17 AALA20050658 120051007A33506011779 TERMINAL DOUG DC9 DC983 3022083WP BATTERY INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21593AA 53256 SFO - EMERGENCY EXIT LIGHTS AT AFT OVERWING INOPERATIVE. CLEANED AFT OVERWING BATTERY PACK TERMINALS FOR EMERGENCY EXIT LIGHTS AT AFT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20051017000572005101700057NM 2005 10 17 SWAA053143 120051012A53306545774 SKIN BOEING737 7373H4 1384600NM BS 700 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 700, STR 10L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051017000632005101700063NM 2005 10 17 SWAA053149 120051012A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM BS 294.5 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FLOORBEAM UPPER CHORD CORRODED AT BS 294.5, BETWEEN LBL 12 TO RBL 12. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20051017000692005101700069NM 2005 10 17 SWAA053155 120051012A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM BS 727E CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 727E, RBL 8. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051017000702005101700070EA 2005 10 17 A6WA200540307 120050920A5340 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE BS 484 CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31425AW 7663 RIGHT FS 484 AT RBL 36 ANGLE CRACKED. MAINTENANCE REPAIRED CRACKED ANGLE BY REMOVING CRACKS FLANGE AND INSTALLING A REPAIR FLANGE BRAS AND REO. (M) 2L72 4F4 FRTA21EA E15NE 20051017000712005101700071EA 2005 10 17 A6WA200540308 120050920A5340 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE BS 484 CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31425AW 7663 FOUND LT FS 484 AT LBL 36 ANGLE CRACKED. MAINTENANCE REPAIRED CRACKED ANGLE BY REMOVEING CRACKED FLANGE AND INSTALLING REPAIRED FLANGE IAW SRM AND REO. (M) 2L72 4F4 FRTA21EA E15NE 20051017000722005101700072EA 2005 10 17 VTZA200500200 120051013A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA RT WING CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27621BR 7186 RIGHT WING PLANK AT WS 148.019 IS CRACKED. 2L72 4F RTA21EA 20051017000742005101700074EA 2005 10 17 VTZA2005202 120051010A5311601R5211680 FRAME CNDAIRCL600 CL6002B19 1900309EA BS 338 CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27621BR 7186 PAX DOOR FRAME TOP RADIUS CRACKED AT 1 INCH IN LENGTH FORWARD OF DATUM 1 AT FS 338.90. 2L72 4F RTA21EA 20051017000772005101700077EA 2005 10 17 VTZA200500205 120051010A53116013600129 FRAME CNDAIRCL600 CL6002B19 1900309EA BS 640 CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27621BR 7186 LEFT FS 640 FRAME DOUBLER IS CRACKED IN RADIUS AT 1 INCH IN LENGTH. 2L72 4F RTA21EA 20051017000792005101700079EA 2005 10 17 VTZA200500207 120051010A5315S6830 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 325-392 CORRODED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27621BR 7186 RBL 9 FLOORBEAM HAS CORROSION AT FS 325 TO 392. 2L72 4F RTA21EA 20051017000812005101700081NM 2005 10 17 QXEA200501337 120050923A5310 GUIDE BOMBDRDHC8 DHC8402 1390042NM PAX DOOR FRAME DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09401QX 4031 PDX - AFT PASSENGER DOOR SURROUND UPPER FWD ROLLER GUIDE IS NOTCHED IN THE INBOARD FACE OF THE LOWER CHANNEL. MAINTENANCE BLENDED DAMAGED AREA IAW EA 6-52-405 TO REMOVE SHARP EDGES. MAPPED ROLLER GUIDE FOR ENGINEERING. HFEC INSP OF BLENDED AREA FOR CRACKS IAW NDTM PART 6, 51-00-02. NO CRACKS NOTED. 2H72 4T RTA13NM 20051017000832005101700083NM 2005 10 17 BB05089 120051010A29133508806 PUMP BOEING757 757225 1384959NM HYD SYSTEM MALFUNCTIONED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19606AU 22202 AFTER TAKEOFF PHL, MOMENTARY GEAR DISAGREE LIGHT & GEAR DOOR LIGHT. EICAS STATUS MESSAGE RT HYD SYS MAINT. DIVERTED TO CLT. LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED FIM PROCEDURE 29-11-00/101 FIG 116. PERFORMED MAIN GEAR EXTENSION AND RETRACTION CHECKS. NO FAULTS NOTED. PROGRAMMED RT ENGINE HYD PUMP FOR REPLACEMENT DUE TO PRODUCING PRESSURE AT THE LOWER LIMIT OF SPECIFIED OUTPUT. PUMP REPLACED 10/12/05. 2L72 4F RTA2NM 20051017000852005101700085NM 2005 10 17 AALA20050652 120051004A3241 TRANSDUCER BOEING757 757223 1384957NM ANTI-SKID SYS INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21668AA 25333 MIA - INFLIGHT AFTER TAKEOFF UPPER EICAS ANTI-SKID MESSAGE AND LIGHT CAME ON ANNUNCIATOR PANEL. AFTER GEAR DOWN, LIGHT AND MESSAGE STAYED ON THROUGH ROLL OUT. BOTH ARE INTERMITTENT. REPLACED NUMBER 7 TRANSDUCER FOR ANTI-SKID AUTOBRAKE CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20051017000872005101700087NM 2005 10 17 AWXA200501209 120050912A53206545819112 ANGLE BOEING737 73733A 1384673NM BS 274-294 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW 23634 GYR - MAJOR REPAIR - DURING C20 CHECK DISCOVERED ANGLE, AT BL 16 AND FROM BS 274 TO BS 294, CORRODED BEYOND SRM LIMITS. MAINTENANCE REMOVED CORRODED ANGLE AND INSTALLED NEW ANGLE AT BL 16 AND FROM BS 274 TO BS 294 IAW BOEING 737-300 SRM 51-40-02. 2L72 4F RTA16WE 20051017000882005101700088EU 2005 10 17 AWXA200501210 120050930A5347D5337111200500 SEAT TRACK AIRBUS320 A320231 3930325EU FR 40-41 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28626AW 65 SAL - MAJOR REPAIR - DURING C5 CHECK DISCOVERED THE RIGHT OUTBOARD SEAT TRACK LOCATED AT FR 40+16" AND Y-1292 CORRODED BEYOND SRM LIMITS. MAINTENANCE REMOVED CORRODED SEAT TRACK FROM FR 36 TO FR 41 AND INSTALLED NEW SEAT TRACK AT Y-192 AND FROM FR 36 TO FR 41 IAW AIRBUS 320 SRM 51-72-11. 2L72 4F RTA28NM 20051017000892005101700089EA 2005 10 17 COMA0560547 120051011A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS UNRELIABLE A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01818CA23210 7408 FLIGHT 5074 - FLAPS FAIL CAUTION. REPLACED THE RIGHT BPSU. 2L72 4F RTA21EA 20051017000922005101700092 2005 10 17 BB05090 420051012A2330233N320925 CONTROL PANEL BOEING757 757225 1384959NM ENTERTAIN SYS SMOKE A USAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA19611AU 27123 FLIGHT 791, SJU-CLT - UTILITY BUSS OFF AFTER TAKEOFF. FLIGHT ATTENDANTS REPORTED SMOKE WHEN INFLIGHT VIDEO WAS TURNED ON. RETURNED TO SJU. RELEASED A/C PER MEL 24-5101. MAINTENANCE LATER REPLACED THE P5 OVERHEAD PANEL TO CLEAR MEL. 2L72 4F RTA2NM 20051017000932005101700093NM 2005 10 17 SWAA053156 120051012A53116546549 FRAME BOEING737 7373H4 1384600NM BS 767 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 767, RBL 7, WL 150. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051017000952005101700095NE 2005 10 17 REXA200500130 220051005A72616087T04P06 SCAVENGE PUMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT ENGINE FAILED A REXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO258907A4076 7907 GEE950030 EN ROUTE TO DTW FROM GSP THE RT ENGINE MASTER WARNING ILLUMINATED FOLLOWED BY THE FLUCTUATION OF THE OIL PRESSURE GAUGE. THE FLIGHT CREW EXECUTED THE QRH AND SHUT DOWN THE ENGINE. DECLARED AN EMERGENCY. ATC CLEARED THEM DIRECT TO AVL WHERE AN OTHERWISE UNEVENTFUL APPROACH AND LANDING WERE MADE. MAINTENANCE FOUND THAT THE ENGINE LUBE AND SCAVENGE PUMP WAS DEFECTIVE. THE PUMP WAS REPLACED AND GROUND RUNS SUCCESSFULLY COMPLETED. THE AIRCRAFT WAS RELEASED FOR FLIGHT. 2L72 4F4 FRTA21EA E15NE 20051017001002005101700100NM 2005 10 17 SWAA053160 120051012A534065C27314 STRINGER CLIP BOEING737 7375H4 138449DNM BS 351 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29505SW 24182 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 351, STR 18L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051017001012005101700101EA 2005 10 17 COMA0560549 120051012A5210LC063MW SPRING CNDAIRCL600 CL6002B19 1900309EA DOOR HANDLE UNRELIABLE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01915CA 7013 FLIGHT 5065 - CABIN DOOR WARNING. REPLACED INNER DOOR HANDLE SPRING. 2L72 4F RTA21EA 20051017001022005101700102EA 2005 10 17 COMA0560550 120051012A3230601R751461 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01967CA2072412551 7134 FLIGHT 5575 - GEAR DISAGREE WARNING. CLUNKING NOISE FROM NLG. REPLACED THE NLG DOOR SELECTOR VALVE. 2L72 4F RTA21EA 20051017001062005101700106EA 2005 10 17 SWIA200515667 120051011A2752852D10019 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED LDLANDING 1 NM07930SW 7713 FLAPS FAILED AT 30 DEGREES ON FINAL FOR LANDING. REPLACED RT NR 1 AND NR 2 FLAP ACTUATORS IAW MM 27-53-05. OPERATIONAL CHECK GOOD, PN 852D100-19 SN/OFF 4194, PN 852D100-19 SN/OFF 4272. 2L72 4F RTA21EA 20051017001082005101700108EA 2005 10 17 SWIA200515669 120051010A274070623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07915SW4651 4651 7615 STAB CH 2 WOULD NOT ENGAGE AFTER POWER UP. REPLACED MOTOR CONTROL UNIT IAW AMM 27-42-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051017001092005101700109EA 2005 10 17 SWIA200515670 120051008A7603FE284000005 THROTTLE CONTROL CNDAIRCL600 CL6002C10 1390015EA MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07728SK8 8 10192 INBOARD GROUND SPOILER FAULT STATUS MESSAGE. REPLACED THROTTLE QUADRANT IAW CRJ 700 AMM 76-11-01. OPERATIONAL CHECKS GOOD. 2L72 4F RTA21EA 20051017001102005101700110EA 2005 10 17 SWIA200515671 120051008A274070744 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07706SK 10149 "STAB CHAN 1" CAUTION MSG. REPLACED HORIZ STAB MOTOR CONTROL UNIT IAW AMM 27-42-07. OPERATIONAL CHECK GOOD IAW 27-40-00-710-801. 2L72 4F RTA21EA 20051017001122005101700112EA 2005 10 17 SWIA200515673 120051007A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07908SW 7540 AFT OVERHEAD EMERGENCY FLOODLIGHT INOP. RELAMPED LIGHT. OPERATIONAL CHECK GOOD IAW AMM 33-51-00. 2L72 4F RTA21EA 20051017001132005101700113EA 2005 10 17 SWIA200515674 120051010A274070623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07427SW1180811808 7497 STAB TRIM INOP MSG. REPLACED HSTA AND MOTOR CONTROL UNIT IAW MM 27-42-01 AND 27-42-05, HSTA PN: 839603, SN:OFF 868. 2L72 4F RTA21EA 20051017001142005101700114SO 2005 10 17 SWIA200515675 120051005A3397 WIRE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07567SW 120342 EXIT SIGN OVER ROW 9 ON OVERHEAD BIN INOP. REPAIRED BROKEN WIRE FOR "EXIT" LIGHT ON ROW 9 OVERHEAD BIN. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20051017001182005101700118EU 2005 10 17 DHL2005366006 120050921A2611FSD200500 SMOKE DETECTOR AIRBUS300 A300B4203 3930306EU MALFUNCTIONED A DHLAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01366DH 249 AT APPROX 120 KIAS ON TAKEOFF ROLL RED SMOKE LIGHT ON MWP ILLUMINATED, CONTINUOUS REPETITIVE CHIME SOUNDED SMOKE DETECTOR LIGHT ON 2ND OFFICERS PANEL 2R ILLUMINATED. REJECTED TAKEOFF AT 120 KIAS MODERATE BRAKING AND REVERSER USED 342000 LBS 840 FT PA BRAKED DID NOT GET ABNORMALLY HOT. COMPLETED CHECKLIST AND RETURNED TO BLOCKS. FOUND A/C DUCT CLAMPS LOOSE (AIR BLOWING ON NR 4 SMOKE DETECTOR WITH A/CAT TAKEOFF POWER SECURED DUCTS IAW MM 21-22-00 AND LEAK CHECKED DUCTS OK. PERFORMED CONTINUITY CHECK OF SMOKE DETECTOR SYSTEM OK IAW SWDM 26-11-14. REMOVED & REPLACED NR 4R AND NR 3L SMOKE DETECTOR. OPS CHECKED SYSTEM OK. OPS CHECKED SMOKE ISOLATION VALVE CONTROL OK. CLEARED AND PLACARD REMOVED. 2L72 4F RTA35EU 20051017001212005101700121NM 2005 10 17 QXEA200501338 120050924A5753 SKIN BOMBDRDHC8 DHC8402 1390042NM TE FLAP DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09401QX 4031 PDX - RT OUTBOARD FLAP HAS TRAILING EDGE DAMAGE AT APPROX WING STATION YW 273.0. DAMAGE AREA IS APPROX 2.75 INCH IN LENGTH BY APPROX .75 INCH WIDE IN CENTER OF DAMAGED AREA. MAINTENANCE CUT AWAY DAMAGE IN UPPER PLANK AND TRAILING EDGE CHANNEL IAW STEP 2 OF SECT II OF RED 8/4-57-556. REMOVED PLANK FROM AIRCRAFT. COMPLETED STEPS 3-7 OF RD 8/4-57-556. CONTINUED WITH SECT III STEPS 1-4. C/W SECT III STEPS 5-6 OF RD 8/4-57-556. C/W SECT II STEP 7 OF WA 6-57-381. INSPECTED FLAP TRAILING EDGE AND PLANK FOR CLEANLINESS AND DEBRIS. NO DISCREPANCIES NOTED. OK TO INSTALL PLANK. C/W STEP 7-10 OF EA 6-57-381. PAINTED RT OUTBOARD FLAP TRAILING EDGE IAW EA 6-57-381, PG 4 STEP 11. 2H72 4T RTA13NM 20051017001232005101700123EA 2005 10 17 QXEA200501340 120051006A5610 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA COCKPIT WINDOW FALSE INDICATIONA QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09603QX 10011 PDX - RIGHT WINDOW HEAT CAUTION LIGHT CAME ON AFTER TAKEOFF. CYCLING THE WINDOW HEAT SWITCH PER THE CHECKLIST CAUSED THE MESSAGE TO CLEAR. MAINTENANCE INVESTIGATED AND FOUND NO CURRENT WINDOW HEAT FAULTS RECORDED IN MDC MEMORY. PERFORMED OPERATIONAL CHECK PER FIM 30-41-00-810-803, CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2L72 4F RTA21EA 20051017001242005101700124EA 2005 10 17 QXEA200501342 120051009A3040165911 CONTROLLER CNDAIRCL600 CL6002C10 1390015EA WINDOW HEAT MALFUNCTIONED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09603QX6917 10011 RT WINDOW HEAT CAUTION MESSAGE. CYCLED PER CHECKLIST, CAUTION WENT OFF. AFTER 10 MIN MESSAGE CAME BACK. F/O WINDOW FEELS COLD. MX PLACED ON MEL 30-41-1(A), RSI 352674. C/W STEP 1 OF EA R-56-17 BY CHANGING ELEMENT TO SPARE. PERFORMED OPS CHECK OF WINDOW, STILL COLD, MEL CONTINUED. PERFORMED RESISTANCE CHECK OF ALL 3 SENSING ELEMENTS AND HEATER ON RT WINDSHIELD. NO DEFECTS NOTED. PERFORMED RESISTANCE AND MEGGER CHECKS OF RT WINDSHIELD WIRES, NO DEFECTS NOTED. REPLACED RT WINDSHIELD TEMPERATURE CONTROLLER IAW TASK 30-41-06-000-801-A01 & 30-41-06-400-801-A01 AS A PRECAUTION. OPERATIONAL CHECKS GOOD. MEL CLEARED AND WIRES RECONNECTED TO PRIMARY ELEMENT. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20051017001332005101700133EA 2005 10 17 QXEA200501343 120051011A2780 SLAT SYSTEM CNDAIRCL600 CL6002C10 1390015EA MALFUNCTIONED A QXEAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 NM09613QX 10045 SEA - SLATS FAIL MESSAGE UPON SLAP/FLAP SELECTION ON APPROACH. FLAPS WORKED FINE, NO CHANGE AFTER PERFORMANCE OF APPLICABLE CHECKLIST. MAINTENANCE FOUND A SLAT ACTUATOR FAILED MECHANICAL JAM MESSAGE IN THE MDC. INSPECTED THE SLATS AND FLAPS FOR FOD DAMAGE. NO DAMAGE NOTED. PERFORMED FAULT ISOLATION PROCEDURES IAW CRJ-700 FIM TASK 27-81-09-810-802-A01. FAULT CLEARED. EXTENDED AND RETRACTED FLAPS SEVERAL TIMES WITH NO FAULT MESSAGES. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2L72 4F RTA21EA 20051017001352005101700135WP 2005 10 17 IXXA05RNG050S 120050906A5330 DOUBLER DOUG DC8 DC872 302199BWP BS 235 MISREPAIRED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX 46013 DURING INSPECTION CHECK WAS FOUND A TEMPORAL REPAIR ON SKIN STA 235 LONGERON 24-25-LT. DAMAGE WILL BE REPAIRED IAW EWO ATI-53-011 AND SRM 53-2-1 FIGURE 7. THIS REPAIR CONSTITUTES A MAJOR REPAIR. 2L74 4F RT4A25 20051017001362005101700136EA 2005 10 17 REXA200500128 120051005A2120 ODOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE COCKPIT DETECTED A REXAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO258758D 7758 TURNED BATTERY MASTER (AC) ON AND AFTER 40 SEC, SMELLED A STRONG ELECT, BURN SMELL AND A LITTLE SMOKE BY THE TILLER. RAN AIRCRAFT AC SYSTEM ON GROUND, COULD NOT DUPLICATE PROBLEM. PULLED OUT TILLER AND INSP, NO DEFECTS NOTED. OPS CHECKS NORMAL AT THIS TIME IN IAW AMM. A/C OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20051017001372005101700137NM 2005 10 17 05FDEA03391 120051011A5315 FLOORBEAM BOEING727 727100 1384036NM BS 1110 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 CORROSION AFT CARGO BAY FLOORBEAM LWR CHORD BS 1110 RBL 4 - 24 WL 200. CUT OUT DAMAGE ON LWR FLANGE OF BS 1110 FLOORBEAM RBL 2-RBL 26. FABRICATED AND INSTALLED REPAIR IAW FEDEX SR DRAWING SR 27-53-034E. 2L73 4F RTA3WE 20051017001392005101700139NM 2005 10 17 05FDEA03393 120051011A5322 SHEAR TIE BOEING727 727100 1384036NM BS 1110 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 AFT CARGO COMP SHEAR TIE IS CORRODED BS 1110 RBL 8 WL 150. 2L73 4F RTA3WE 20051017001402005101700140NM 2005 10 17 05FDEA03394 120051011A3260 WARNING LIGHT BOEING727 727200 138407ENM RT MLG ILLUMINATED A FDEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO25268FE 21674 RT MAIN GEAR DOOR LIGHTS ILLUMINATED AFTER CYCLING GEAR HANDLE FROM UP TO OFF POSITION. ADJUSTED RT MLG DOOR LIGHT SWITCH I.A.W FED-EX MM 32-62-011-4 STEP 2BJ. PERFORMED FUNCTIONAL CHECK, FUNTIONAL CHECKS GOOD. 2L73 4F RTA3WE 20051017001422005101700142NM 2005 10 17 USAA051196 120051011A5240 STOP FITTING BOEING737 7374B7 1384702NM SERVICE DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 RIGHT FWD SERVICE DOOR, AFT FRAME AT NR 4 STOP FITTING CUTOUT CRACKED. FABRICATED AND INSTALLED REPAIR DOUBLER IAW TYPICAL REPAIR 52-10-11, DEFECT SIZE: 0.625 INCH CRACK. 2L72 4F RTA16WE 20051017001432005101700143NM 2005 10 17 USAA051199 120051012A5312 BULKHEAD BOEING737 737301 1384611NM BS 1016 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19300AU 23228 AFT PRESSURE BULKHEAD CRACKED. REPAIRED AS REQUIRED, DOUBLER INSTALLED EA 96994, DEFECT SIZE 1 INCH. 2L72 4F RTA16WE 20051017001442005101700144NM 2005 10 17 USAA051198 120051012A57536546435274MCIR WEDGE BOEING737 7374B7 1384702NM RT WING TE FLAP DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19443US 24842 RIGHT WING O/B AFT FLAP BEHIND NR 8 FLAP TRACK DELAMINATED. INJECTED WEDGE SPLIT WITH TWO PART ADHESIVE IN DISBOND. NO FURTHER ACTION REQUIRED IAW SRM 57-53-01, DEFECT SIZE 3 X 5 INCHES. 2L72 4F RTA16WE 20051017001452005101700145NM 2005 10 17 USAA051197 120051012A5320 INTERCOSTAL BOEING737 7374B7 1384702NM BS 344 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19443US 24842 STRINGER 16L AND STA 344 CRACKED. FABRICATED NEW INTERCOSTAL/WEB AND ANGLES, INSTALLED REF DWG 65-17685-47 AND SRM 53-10-04. DEFECT SIZE 1 INCH. 2L72 4F RTA16WE 20051017001462005101700146NM 2005 10 17 USAA051208 120051013A5751 SKIN BOEING757 7572B7 1384964NM RT AILERON ERODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19627AU 27805 RIGHT AILERON UPPER SURFACE I/B EDGE ERRODED. REPAIRED AILERON (COMPOSITE) TIME LIMITED REPAIR PER EA 96922, SRM 51-60-01, 51-70-03. DEFECT SIZE NOT DOCUMENTED. 2L72 4F RTA2NM 20051017001492005101700149EU 2005 10 17 USAA051205 120051013A5315D5347209001100 FLOORBEAM AIRBUSA319 A319112 3930323EU FR 66 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19737US 1245 FLOORBEAM AT Y1292 FR 66; CORROSION LEVEL 1; TASK JA-260-53500. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-24-00, 51-42-11, 53-41-04. DEFECT SIZE 1 INCH DIA AREA. 2L72 4F RTA28NM 20051017001512005101700151EU 2005 10 17 USAA051203 120051013A5320D5347117220400 FLOOR SUPPORT AIRBUSA319 A319112 3930323EU FR 66-68 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19737US 1245 FLOOR SUPPORT AT Y1162.5 FR 66 AND FR 68; CORRODED LEVEL 1; TASK JA-260-53500. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 53-41-14, 51-72-11, DEFECT SIZE .75 INCH DIA IN 2 AREAS. 2L72 4F RTA28NM 20051017001532005101700153EU 2005 10 17 USAA051201 120051013A5320 SILL AIRBUSA319 A319112 3930323EU FR 66 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19737US 1245 FR 66 FWD SIDE OF LT DOOR SILL; CORROSION LEVEL 1; TAK JA-260-53500. REMOVED CORROSION, INSTALLED MANUFACTURED BATH TUB FITTING PER SRM 53-41-14. DEFECT SIZE 1 X 1 INCH AREA. 2L72 4F RTA28NM 20051017001542005101700154EU 2005 10 17 USAA051200 120051013A5347D53112827202 DUMMY RAIL AIRBUSA319 A319112 3930323EU DUMMY RAIL CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19737US 1245 DUMMY RAIL 503.2 LEVEL 1; TASK 2L6-230-96165. DEFECTIVE PART REPLACED WITH IDENT PART PER EA 96165A. DEFECT SIZE 1 INCH X 36 INCHES. 2L72 4F RTA28NM 20051017001552005101700155NM 2005 10 17 QXEA200501346 120051012A3250 WARNING LIGHT DHAV DHC8 DHC8202 2809007NM NLG STEERING ILLUMINATED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09365PH 526 NOSE STEERING CAUTION LIGHT AFTER ENGAGING NOSE STEERING SWITCH. MAINTENANCE CLOSED AND GUARDED THE L/G DOWN SELECT INHIBIT SWITCH AFTER RETURNING THE SELECT SWITCH TO THE NORMAL POSITION AND RETURNING POWER TO THE LANDING GEAR SYSTEM, NOSE WHEEL STEERING WORKS GOOD WITH NO FAULTS. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051017001582005101700158WP 2005 10 17 ABXA050247 120050929A32135920602501 STRUT DOUG DC9 DC941 302207NWP NLG CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23955AX 47619 NOSE LANDING GEAR STRUT BARREL HAD PITTING IN FIRST BEVEL OF BARREL HOUSING. REMOVED AND REPLACED STRUT BARREL IAW DC-9 SRM. 2L72 4F A6WE 20051017001592005101700159WP 2005 10 17 ABXA050248 120050929A5311591359677 FRAME DOUG DC9 DC941 302207NWP BS 1152 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23955AX 47619 FRAME 1152 CRACKED LONGERON 2 RIGHT. REPLACED CRACKED FRAME SECTION FS 1152 IAW DC-9 SRM 53-03. 2L72 4F A6WE 20051017001602005101700160NM 2005 10 17 AWXA200501208 120051011A3397BMS13311122 WIRE BOEING737 7373G7 1384595NM EMERGENCY LIGHT SHORTED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 SNA - EEL - DURING INSPECTION FOUND ROWS 7, 8, 9, 10, AND 11 SEAT MOUNTED EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE FOUND SHORTED WIRE AT SEAT 10, LT SIDE. REPAIRED WIRE AND OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20051017001622005101700162EU 2005 10 17 AWXA200501212 120050930A5347D5337111200400 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28626AW 65 DURING C5 CHECK DISCOVERED CORROSION LOCATED ON SEAT TRACK AT FR 42+17" AND Y1292. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 101. REMOVED SEAT TRACK AND INSTALLED NEW SEAT TRACK FROM FR 41 TO FR 47 AND Y1292 IAW AIRBUS 320 SRM 51-42-11. 2L72 4F RTA28NM 20051017001642005101700164EU 2005 10 17 AWXA200501214 120050930A5347D3371110001 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28626AW 65 SAL - DURING C5 CHECK DISCOVERED CORROSION LOCATED ON SEAT TRACK AT FR 42 + 17"AND Y-765. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 101. REMOVED SEAT TRACK AND INSTALLED NEW SEAT TRACK FROM FS 41 TO FS 47 AND Y-765 IAW AIRBUS 320 SRM 51-42-11. 2L72 4F RTA28NM 20051017001652005101700165EU 2005 10 17 AWXA200501215 120050930A5347D5337111001 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28626AW 65 SAL - DURING C5 CHECK DISCOVERED CORROSION LOCATED ON SEAT TRACK AT FS 42 AND Y765. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 101. REMOVED SEAT TRACK AND INSTALLED NEW SEAT TRACK FROM FS 41 TO FS 47 AND Y765 IAW AIRBUS 320 SRM 51-42-11. 2L72 4F RTA28NM 20051017001662005101700166EU 2005 10 17 AWXA200501216 120050930A5347D5713014720302 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28626AW 65 SAL - DURING C5 CHECK DISCOVERED CORROSION LOCATED ON SEAT TRACK AT FR 44 + 17" AND Y-1292. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 101. REMOVED SEAT TRACK AND INSTALLED NEW SEAT TRACK FROM FS 41 TO FS 47 AND Y-1292 IAW AIRBUS 320 SRM 51-42-11. 2L72 4F RTA28NM 20051017001672005101700167EU 2005 10 17 AWXA200501217 120050930A5347D57130147200 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28626AW 65 SAL - DURING C5 CHECK DISCOVERED CORROSION LOCATED ON LT INBOARD SEAT TRACK AT FS 38 + 13" AND Y765. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 101. REMOVED SEAT TRACK AND INSTALLED NEW SEAT TRACK FROM FR 36 TO FR 41 AND Y765 IAW AIRBUS 320 SRM 51-42-11. 2L72 4F RTA28NM 20051017001682005101700168EU 2005 10 17 AWXA200501218 120051001A5320D53230465200 FLOOR SUPPORT AIRBUS320 A320231 3930325EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28626AW 65 SAL - DURING C20 CHECK DISCOVERED CRACK, 3.025 INCHES LONG, LOCATED ON FLOORBEAM AT Y254 BETWEEN FS 28 AND FS 29. MAINTENANCE CUT OUT DAMAGED ARE IAW AIRBUS 320 SRM 53-00-14. FABRICATED FILLER AND ANGLE IAW AIRBUS 320 SRM 53-00-14 FIG 204. INSTALLED FABRICATED REPAIR PARTS ON FLOORBEAM AT Y254 BETWEEN FS 28 AND FS 29 IAW AIRBUS 320 SRM 51-42-11. 2L72 4F RTA28NM 20051017001692005101700169NM 2005 10 17 AWXA200501219 120050927A5347BAC1520792 SEAT TRACK BOEING737 7373S3 1384711NM BS 807-907 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 MCN - DURING C 18 CHECK DISCOVERED CORROSION ON SEAT TRACK LOCATED AT BS 903 AND BL 25R. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-00-52-1A FIG 101. CUT OUT DAMAGED SECTION OF SEAT TRACK FROM STA 887 TO STA 907 IAW BOEING 737-300 SRM 53-00-52. RECEIVED NEW SEAT TRACK AND FABRICATED SPLICE PLATE IAW BOEING G737-300 SRM 53-00-52 FIG 201. INSTALLED REPAIR PARTS IAW BOEING 737-300 SRM 53-00-52-2R 3 FIG 201. 2L72 4F RTA16WE 20051017001722005101700172NM 2005 10 17 DHL2005749002 120050928A335038931002 BATTERY BOEING727 727200 138407ENM EMERGENCY LIGHT ACTIVATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01749DH 22013 EMERGENCY EXIT LIGHT IN ENTRYWAY INOP. INSTALLED NEW BATTERIES IN LIGHT IAW B727 M/M 33-50-00. OP CHECK GOOD, P/N 38931-002. 2L73 4F RTA3WE 20051017001732005101700173NM 2005 10 17 DHL2005783005 120050928A335038931002 BATTERY BOEING727 727227 1384078NM EMERGENCY LIGHT INOPERATIVE A DHLAK NONE O OTHER ININSP/MAINT 1 SO01783DH 21999 EMERGENCY EXIT LIGHT OVER COCKPIT DOOR DOES NOT ILLUMINATE DURING STBY POWER CHECK. INSTALLED NEW BATTERIES IN EMERGENCY EXIT LIGHT P/N 38931-002. LIGHT OP CHECKS GOOD IAW B727 M/M 33-50-00. 2L73 4F A3WE 20051017001752005101700175WP 2005 10 17 DHL2005806507 120050818A5710 STRAP DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH87034 46002 RIGHT WING CTR L/E INTERNAL SPLICE STRAP CRACKED 12 INCHES XW 257.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-3-3 FIG 3 SHEET 3. REMOVED SPLICE STRAP DAMAGED IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. FABRICATED NEW SPLICE STRAP (AL7075Y6 0.100") IAW SRM 57-3-3 FIG 3 SHEET 3 ITEM V, SRM 51-1-4 PG 1. CLEANED, TREATED AND PRIMED AREA AND SPLICE STRAP IAW SRM 51-1-8B. INSTALLED NEW SPLICE STRAP IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1, SRM 51-1-20D PG 9. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20051017001762005101700176WP 2005 10 17 DHL2005802009 120050920A2612472450 FIRE DETECTOR DOUG DC8 DC873 302199CWP NR 2 ENGINE MALFUNCTIONED A DHLAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO01802DH 46076 AT FL 320 NR 2 ENGINE HAD INTERMITTENT FIRE WARNING. COMPLETED PHASE 1 OF ENGINE FIRE CHECKLIST, NO INDICATION OF FIRE, COMPLETED CHECKLIST. CHECKED BOTH LOOP A AND B. FIRE BOTTLE WAS NOT DISCHARGED. PLACED FIRE DETECTION LOOP A ON NR 2 ENGINE ON MEL 26-2-3, DMI 22502 CAT C, PLACARDS INSTALLED. LOOP-B OK. REF DMI 22544, NR 2 ENGINE INDICATED FIRE. A/C ENGINE NOT BURNING, LOOP-A. REMOVED AND REPLACED LT CORE FIRE LOOP ASSY AS PER MM 26-10-1. PERFORMED OPS CHECK AS PER MM 26-10-0. OPS CHECKED OK. THIS CLEARS DMI 22544. PLACARD REMOVED. 2L74 4F RT4A25 20051017001812005101700181EA 2005 10 17 QXEA200501299 120050917A5230 SKIN CNDAIRCL600 CL6002C10 1390015EA CARGO DOOR DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09617QX 10130 YYC - AFT BAGGAGE DOOR HAS DAMAGED RIVET ON THE AFT LOWER OUTER SKIN. REPLACED RIVET IAW CRJ-700 SRM 51-42-000-001-001-A01. 2L72 4F RTA21EA 20051017001822005101700182WP 2005 10 17 05FDEA03312 120051007A7600D107300102 TUBE DOUG MD10 MD1010F 3022112WP GE CF6 CF66D 30020GL NR 2 ENGINE LOOSE A FDEAE ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION DEDESCENT 1 SO25391FE 46625 451109 DURING DESCENT THRU FL200, NOTICED NR 2 ENGINE WOULD NOT SPOOL UP FOR LEVEL OFF. N1 REMAINED AT LESS THAN 35 N1, N2 60 PERCENT. NR 2 THROTTLE HAD A VERY LIGHT TRAVEL FORCE AND FELT DISCONNECTED. ACCOMPLISHED RED TABS AND SHUT DOWN ENGINE DUE TO ENGINE BEING UNRESPONSIVE TO THROTTLE COMMANDS. T/S AND FOUND CDP LINE LOOSE AT MEC RETORQUED AND SAFETY LINE IAW SMP RAN NR 2 ENGINE AT HIGH POWER IAW JRH 4-5, NO DEFECTS NOTED. OK FOR SERVICE. 2L73 4F4 FRTA22WE E23EA 20051017001842005101700184WP 2005 10 17 AALA20050640 120051004A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21552AA 53034 SAT - FORWARD OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051017001872005101700187NM 2005 10 17 AALA20050637 120051002A335002019242005 LIGHT BOEING767 767223 1385123NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21322AA 22323 JFK - EMERGENCY LIGHT AT MID GALLEY RIGHT IS BROKEN. REPLACED EMERGENCY LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT MID GALLEY RIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20051017001882005101700188NM 2005 10 17 AALA20050633 120051002A3350 LIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21791AN 30254 DFW - EMERGENCY LIGHT ON FORWARD LEFT GALLEY NEXT TO CLOSET INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT ON FORWARD LEFT HAND GALLEY NEXT TO CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20051017001902005101700190WP 2005 10 17 AALA20050635 120051001A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21480AA 49655 SFO - EMERGENCY LIGHT FROM SEAT 21DEF TO 30DEF INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEATS 21DEF TO 30DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051017001912005101700191WP 2005 10 17 AALA20050636 120051003A33506011779 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21593AA 53256 SFO - EMERGENCY LIGHTS AT EMERGENCY OVERWING DOOR LEFT AND RIGHT INOPERATIVE. SPUN BATTERIES IN PACK FOR EMERGENCY LIGHTS AT EMERGENCY OVERWING DOOR LEFT AND RIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20051017001922005101700192EU 2005 10 17 AALA20050643 120051005A3350BR964814 LIGHT AIRBUS300 A300B4605R 3930308EU SEAT 35G INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2177080 626 BOS - EMERGENCY LIGHT MISSING ON SEAT 35G. INSTALLD NEW EMERGENCY LIGHT ON SEAT 35G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20051017001942005101700194NM 2005 10 17 AALA20050647 120051005A33500201922001 LIGHT BOEING777 777223 1385213NM SEAT 4D INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21774AN 29581 EZE - EMERGENCY LIGHT AT SEAT 4D FORWARD INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHTS AT SEAT 4D FORWARD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20051017001952005101700195WP 2005 10 17 AALA20050644 120051005A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2190511 49805 LGA - EMERGENCY LIGHT IN COCKPIT AND ABOVE L1 AND R1 DOOR INOPERATIVE. REPLACED BATTERY PACK AT B523 FOR EMERGENCY LIGHT IN COCKPIT AND ABOVE L1 AND R1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051017001972005101700197EA 2005 10 17 QXEA200501317 120050917A3213521011 CYLINDER CNDAIRCL600 CL6002C10 1390015EA NLG CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09617QX 10130 YYC - NOSE GEAR OUR CYLINDER HAS AREAS OF CORROSION. REPAIRED CORROSION IAW EA R-32-194 AND REO 670-32-21-070 AND SCR 0008-4 STEPS 1-8. NO CRACKS NOTED. LOCALLY BRUSH CADMIUM PLATED REWORKED AREAS OF CYLINDER PER MIL-STD 865 USING LOW HYDROGEN EMBRITTLEMENT SOLUTION. SOLUTION SELECTION LITE CODE 5070 IAW EAR-32-194 AND SCR 0008-04 REV C PARAGRAPH 11. RESTORED FINISH. 2L72 4F RTA21EA 20051017001982005101700198EA 2005 10 17 QXEA200501320 120050917A531267053110522 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA BS 280 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09617QX 10130 YYC - FUSELAGE STATION 280 BULKHEAD HAS CORROSION AT RBL 11 TO RBL 15 AND WL 72. REMOVED CORROSION IAW REO 670-53-11-052 REV "A" REPAIR NR 1. REPLACED RT LOWER BULKHEAD WEB IAW REO 670-53-11-052 REV "A" REPAIR NR 2. AREA REMOVED WAS .029". 2L72 4F RTA21EA 20051017001992005101700199SO 2005 10 17 139810042005 120051004A2910 HYDRAULIC SYSTEM GULSTMG1159 GIV 3980115SO FAILED E N93AO OTHER O OTHER LDLANDING 1 SO13498QS5181 1398 LOST FLIGHT SIDE HYDRAULIC FLUID AFTER LANDING. 2L72 4F RTA12EA 20051017002002005101700200EA 2005 10 17 QXEA200501298 120050917A5230 SKIN CNDAIRCL600 CL6002C10 1390015EA CARGO DOOR SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09617QX 10130 YYC - AFT BAGGAGE DOOR OUTER SKIN HAS SCRATCHES ON THE FORWARD LOWER EDGE. REMOVED THE DAMAGE IAW CRJ-700 SRM 52-00-01 PAGE 109. RESTORED FINISH. 2L72 4F RTA21EA 20051013000182005101300018NM 2005 10 13 SWAA053115 120051010A53306545767 SKIN BOEING737 7373H4 1384600NM BS 433 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 433, STR 16L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051013000242005101300024WP 2005 10 13 05FDEA03384 120051011A5313 LONGERON DOUG DC10 DC1010 3022110WP BS 1958-1998 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25389FE 46623 AFT PIT STA 1958 LONG 50L SPLICE IS CORRODED ALL THE WAY TO STA 1998. REMOVED LONG SECTION AND SPLICE IAW DC10 SRM 53-10-00 VOL, 51-35-01 VOL11. MACHINED LONG SECTION AGA7742-19 IAW DAG AGA7742 DALF E7946A. MACHINED LONG SECTION AGA 3104-1 IAW DAC DAG AGA3104 CAL NR E7946A. LOCATED AND DRILLED 2EA, LONG AND 6 SPLICE SECTIONS IAW DAC DAG NR AGA7742. ALODINE AND PRIMED LONGERONS AND SPLICES IAW DC10 SRM 51-21-01 VOL 11. INSTALLED 2 LONG AND 6EA SPLICES IAW SRM 51-33-01 VOL 11. 2L73 4F A22WE 20051013000392005101300039EU 2005 10 13 DHL2005364003 120051002A3231 SELECTOR VALVE AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE MLG INOPERATIVE A DHLAO OTHER E VIBRATION/BUFFET LDLANDING 1 SO01364DH 141 ON THE GROUND DURING TAXI WHEN MAKING LARGE TURN REQUIRING MORE THAN 10 DEG TILLER. TILLER IS VERY DIFFICULT TO TURN; REQUIRES TWO HANDS. ALSO DURING THIS TIME, WHEN PRESSING THE RUDDER PEDALS, CAN FEEL A HIGH FREQUENCY VIBRATION IN RUDDER PEDALS. DURING LANDING GEAR EXTENSION, GEAR FAILED TO EXTEND. PERFORMED ABNORMAL PROCEDURE FOLLOWING CHANGE OF ELECTRO VALVE AND RESTORATION OF LDG GEAR ACTUATING SYSTEM AND RESETTING GREEN HYD SYSTEM, PERFORMED OPS CHECK OF NOSE WHEEL STEERING SYS. OPS CHECK GOOD IAW AMM 32-51-00 AND 32-30-00 (RESTORATION) REMOVED AND REPLACED LANDING GEAR SELECTOR ELECTRO VALVE IAW MM 32-31-12. OPS CK GOOD. 2L72 4F4 FRTA35EU E23EA 20051013000502005101300050 2005 10 13 SWAA053121 420051007A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29769SW 30588 DURING SCHEDULED RON CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051013000562005101300056WP 2005 10 13 DHL2005806540 120050916A2730 BRACKET DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE ELEVATOR CONTROLCORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH87034 46002 ITEM REF NR 041577: RT ELEVATOR SYSTEM, 1EA BRACKET CORRODED, STA -90.000. REMOVED AND REPLACED RT ELEVATOR SYS BRACKET AT STA -90.000. TIGHTENED BOLT IAW MM 20-16-0 PG. 201. ADJUSTED CONTROL CABLES IAW MM 27-30-0 PG. 512-513. OPS CHECKED SEE NR 041920 2L74 4F4 FRT4A25 E2GL 20051013000632005101300063EU 2005 10 13 DHL2005365007 120051004A5250 LATCH AIRBUS300 A300B4203 3930306EU GE CF6 CF650* 30018NE COCKPIT DOOR LACK OF LUBE A DHLAK NONE O OTHER ININSP/MAINT 1 SO01365DH 149 COCKPIT DOOR LATCH IS FAULTY AND DIFFICULT TO LOCK. LUBED CREW ENTRY DOOR TO COCKPIT SYS OPS CHECKED GOOD ON GROUND IAW A300 M/M 52-00-00. 2L72 4F4 FRTA35EU E23EA 20051013000652005101300065WP 2005 10 13 DHL2005807004 120050917A5270H2024B SWITCH DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE CARGO DOOR INOPERATIVE A DHLAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01807DH 45990 BEGINNING OF TAKEOFF ROLL MASTER WARNING AND BELLY DOOR OPEN LIGHT ILLUMINATED RTO AT NO IND AIRSPEED. FOUND B PIT BELLY DOOR SWITH STUK, DISCONNECTED SWITCH, DEFERRED BY MEL 52-6 IN DMI NR 22471. TLATEMPA 999017. RE DMI 22471 BEGINNING OF TAKEOFF ROLL, MASTER WARNING AND BELLY DOOR OPEN LIGHT ILLUMINATED RTO AT NO INDICATION AIRSPEED. REMOVED AND REPLACED (B) CARGO COMPARTMENT WARNING SWITCH P/N:H20-24B IAW MM,CHECKED OPERATION OK. DMI 22471 CLEARED . . 2L74 4F4 FRT4A25 E2GL 20051013000682005101300068CE 2005 10 13 DJFA2005146 120051004A2120 SMOKE BEECH MU300 400A 1155402CE PWA JT15 JT15D5 52112NE CABIN DETECTED E DJFAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA23457CW RK57 DURING CRUISE FLIGHT, LT GENERATOR FAIL ANNUNCIATOR ILLUMINATED. AFTER APPROX 1-2 MIN, LIGHT SMOKE WAS VISIBLE IN THE LT SIDE OF COCKPIT. AN IMMEDIATE DESCENT WAS INITIATED, ANTI-ICING SYS FOR WINGS, HORIZ STAB, ENGINES WERE TURNED ON. AFTER ANTI-ICE WAS TURNED ON, BLEED AIR DUCT FAIL ANNUNCIATOR ILLUMINATED FOR APPROX 1 MINUTE, THEN EXTINGUISHED. AT 10,000 FT ALTITUDE, SMOKE HAD CLEARED AND GENERATOR WAS ABLE TO BE RESET. AC WAS DIVERTED, LANDED WITHOUT FURTHER INCIDENCE. MAINT RAN AC ON GROUND, LT GENERATOR WAS CYCLED ON AND OFF AND WAS RESET. GENERATOR OPERATIONALLY CHECKED GOOD. BLEED AIR DUCT FAILURE INDICATION, AND INCIDENT OF SMOKE IN COCKPIT COULD NOT BE DUPLICATED. AC WAS RETURNED TO SERVICE.2H72 4F4 FRTA16SW E25EA 20051013000892005101300089 2005 10 13 SWAA053068 420050925A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29462WN 32466 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20051013000912005101300091NM 2005 10 13 SWAA053070 120051005A5754 SKIN BOEING737 7375H4 138449DNM NR 2 SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29513SW 24190 DURING SCHEDULED C4 CHECK, FOUND NR 2 L/E SLAT UPPER T/E WEDGE DELAMINATED AT INBD AND OTBD ENDS. REPAIRED SLAT PER SRM. 2L72 4F RTA16WE 20051013000942005101300094NM 2005 10 13 SWAA053073 120051005A53306545777 SKIN BOEING737 7373A4 1384585NM BS 960 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29677AA 23289 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 960, STR 21L. REPAIRED SKIN PER SWA EA AND SRM. 2L72 4F RTA16WE 20051013001002005101300100NM 2005 10 13 05FDEA03263 120051006A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 CABIN SEAT TRACK LOWER FLANGE ADJACENT TO STATION 755, X=-8.5 FOUND CRACK. REPAIR CARRIED OUT AS PER SRM 53-70-00. 2L73 4F RTA22WE 20051013001062005101300106NM 2005 10 13 05FDEA03267 120051006A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 FOUND CRACK INDICATION ON LEFT HAND WING TANK AT END OF STRINGER 14 (UPPER STRINGER). REPAIR CARRIED OUT AS PER SRM 57-20-00. 2L73 4F RTA22WE 20051013001152005101300115WP 2005 10 13 05FDEA03276 120051007A5712 RIB DOUG DC10 DC1010 3022110WP LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE LT WING FIXED L/E COMPT AT STA XORS 755 ZONE 525 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 4 AND 6 VOL I. 2L73 4F A22WE 20051013001212005101300121WP 2005 10 13 05FDEA03280 120051007A5712 RIB DOUG DC10 DC1010 3022110WP LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE L WING FIXED L/E COMPT AT STA XORS 917 ZONE 527 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 5 AND 6 VOL I. 2L73 4F A22WE 20051013001272005101300127NM 2005 10 13 05FDEA03300 120051007A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 CRACK INDICATION ON RIGHT HAND SIDE WING TANK AT END OF STRINGER 14 , UPPER STRINGER. CRACK AT RIGHT HAND WING TANK END OF STRINGER 14 SLOTTED OUT AS PER SRM 57-20-00 FIGURE 10 VOLUME I. NEW REPAIR ANGLE FABRICATED AND INSTALLED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051014000052005101400005NM 2005 10 14 SWAA053127 120051011A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 663 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIPS CRACKED AT BS 663, STR 10L & STR 10R. REMOVED AND REPLACED CLIPS PER SRM. 2L72 4F RTA16WE 20051014000162005101400016NM 2005 10 14 CALA0500351 120051011A5313147A3215U23 STRINGER BOEING737 737824 13844BZNM BS 887-1016 UNKNOWN A CALAK NONE O OTHER ININSP/MAINT 1 SW2773251 30582 STRINGER 25L, STA 887-1016 REPLACED PER ECRA 5331-01198. 2L72 4F RTA16WE 20051017000382005101700038NM 2005 10 17 SWAA053139 120051011A53116546546 SHEAR TIE BOEING737 7373H4 1384600NM BS 787 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, BETWEEN LBL 8 TO RBL 8. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051017000492005101700049NE 2005 10 17 AALA20050659 220051008A7200 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE NR 2 DAMAGED A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21498AA 49736 718520 MCI - INFLIGHT CLIMBING THROUGH FL20, FLIGHT CREW HEARD A BANG AND SAW NR 2 ENGINE EXHAUST GAS TEMPERATURE DOUBLED AND LOSS OF N1 AND N2. AIR RETURNED TO MCI AND LANDED WITHOUT INCIDENT. FOUND SEVERAL MISSING FAN BLADES. REPLACED RIGHT HAND ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 F A6WE E9NE 20051017000522005101700052NM 2005 10 17 AALA20050653 120051005A28205006151A VALVE BOEING767 767323 1385205NM FUEL SYSTEM INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21354AA 24035 ORD - INFLIGHT DURING CLIMB RECEIVED FUEL INBALANCE EICAS MESSAGE. FUEL WAS 2500 POUNDS HEAVIER IN RIGHT HAND MAIN TANK. FUEL WAS THEN BALANCED. ON LANDING RIGHT HAND MAIN TANK SHOWED 1500 POUNDS LESS THAN LEFT HAND MAIN TANK. REPLACED RIGHT HAND MAIN TANK DISCHARGE CHECK VALVE, MOTIVE FLOW VALVE, AND SCREEN VALVE. ALSO REPLACED RIGHT HAND AFT BOOST PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20051017000612005101700061NM 2005 10 17 SWAA053147 120051011A575465C266011 STRUCTURE BOEING737 7373Y0 1384671NM LT WING SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29308SA 23498 DURING SCHEDULED C3 CHECK, FOUND LT WING NR1 L/E SLAT CRACKED. REPAIRED SLAT PER SWA EA. 2L72 4F RTA16WE 20051017000642005101700064NM 2005 10 17 SWAA053150 120051012A335090083 BATTERY PACK BOEING737 7373H4 1384600NM EMERGENCY LIGHTSINOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED RON CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20051017000672005101700067NM 2005 10 17 SWAA053153 120051012A534065C27314 STRINGER CLIP BOEING737 7375H4 138449DNM BS 927 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 927, STR 25R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051017000782005101700078EA 2005 10 17 VTZA200500206 120051010A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27621BR 7186 LEFT WING PLANK AT FS 148.019 IS CRACKED AT 1 INCH IN LENGTH. 2L72 4F RTA21EA 20051017000802005101700080EA 2005 10 17 VTZA200500208 120051010A5315S6830 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 337 CORRODED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27621BR 7186 RBL 27 FLOORBEAM HAS CORROSION AT FS 337. 2L72 4F RTA21EA 20051017000822005101700082NM 2005 10 17 AALA20050655 120051005A3350 BATTERY PACK BOEING757 757231 1384950NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21717TW 28485 DFW - AISLE EMERGENCY LIGHT ON RIGHT HAND SIDE SECOND FROM AFT INOPERATIVE. REPLACED LIGHT ASSEMBLY AND BATTERY PACK FOR AISLE EMERGENCY LIGHT ON RIGHT HAND SIDE SECOND FROM AFT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20051017000972005101700097NM 2005 10 17 SWAA053157 120051012A3350 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29644SW 28329 L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20051017001032005101700103EA 2005 10 17 COMA0560551 120051012A2750860D10018ABCD CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01975CA2141520096 7150 FLIGHT 5033 - FLAPS FAIL CAUTION. REPLACED THE FECU. 2L72 4F RTA21EA 20051017001052005101700105 2005 10 17 BSYA200500014 420051007A3100MS250382 TACH GENERATOR BEECH 58 58 1152740CE RT ENGINE INOPERATIVE E BSYAA UNSCHED LANDING O OTHER CLCLIMB 1 GL079044V TH216 RIGHT ENGINE TACHOMETER QUIT AFTER TAKEOFF OUT OF MKE. AIRCRAFT RETURNED TO MKE. REMOVED AND REPLACED TACH GENERATOR, OPS CHECKS GOOD. 1L72 3O 3A16 20051017001072005101700107EA 2005 10 17 SWIA200515668 120051011A2760 BOLT CNDAIRCL600 CL6002B19 1900309EA SPOILER LOOSE A SWIAC ABORTED TAKEOFF FJ FLT CONT AFFECTED WARNING INDICATION TOTAKEOFF 1 NM07592SW 7279 ABORTED T/O DUE TO "CONFIG SPOILERS" WARNING MSG. REPLACED BOLT AND BUSHINGS AT ROD END ATTACH POINT RIGHT FLIGHT SPOILER OB PCU AND ADJUSTED PCU IAW MM 27-62-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051017001152005101700115 2005 10 17 SWIA200515676 420051007A34206229336400 COMPUTER CNDAIRCL600 CL6002B19 1900309EA AHRS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07929SW 7703 YD1 DISENGAGES DURING FLIGHT AND WILL NOT REENGAGE. REPLACED NR 1 AHRS. OPERATIONAL CHECK GOOD IAW MM 34-21-00 AND 22-10-00. 2L72 4F RTA21EA 20051017001172005101700117EA 2005 10 17 QXEA200501347 120051013A2710 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA AILERONS ILLUMINATED A QXEAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM09605QX 10022 EN ROUTE TO SEA ON FLIGHT 2478 (FAT-SEA), OVER SMF, RECEIVED A FLT CONTROL AILERON MALFUNCTION MESSAGE. FLIGHT DIVERTED TO SMF AND ACCOMPLISHED A UNEVENTFUL LANDING. MTX IN SMF PERFORMED A DETAILED INSPECTION OF THE AILERON CONTROL SYSTEM AND A RIGGING CHECK OF THE SYSTEM WITH NO DEFECTS NOTED. REPLACED THE AILERON SERVO MOUNT/CLUTCH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20051017001192005101700119CE 2005 10 17 DXTA200501021 120051014A3240 BRAKE ASSY CESSNA500 560CESSNA 2076750CE MLG WEAK E DXTAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL07325QS 5600425 COPILOT'S BRAKE PEDALS ARE SOFT. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20051017001222005101700122EA 2005 10 17 QXEA200501339 120051011A5610NP1393216 WINDSHIELD CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CRACKED A QXEAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM09603QX10574 10011 PDX - FIRST OFFICERS WINDSHIELD WAS SMOKING EVEN WITH WINDSHIELD HEAT SELECTED OFF. MAINTENANCE PULLED CIRCUIT BREAKERS FOR SYSTEM. WINDSHIELD WAS REPLACED DUE TO A PREVIOUS DISCREPANCY FOR CRACKING. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20051017001412005101700141NM 2005 10 17 05FDEA03395 120051012A5311 FRAME DOUG MD11 MD11 3023602NM BS 6-50 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 FWD CARGO COMPT ALONG STA 6-50 BETWEEN L51L AND L51R, FRAME CHORD CORRODED. CORROSION REMOVED, FOUND OUT OF LIMITS IAW SRM 53-00-01 AND REPAIRED IAW SRM 53-00-01. MAJOR REPAIR PER GMM 6-2-100. 2L73 4F RTA22WE 20051017001522005101700152EU 2005 10 17 USAA051202 120051013A5315D5347218820400 FLOORBEAM AIRBUSA319 A319112 3930323EU FR 69 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19737US 1245 FLOORBEAM AT Y1162.5 FR. 69; CORROSION LEVEL 1; TASK JA-260-53500. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 53-41-14 51-72-11, DEFECT SIZE .75 INCH DIA AREA. 2L72 4F RTA28NM 20051017001562005101700156NM 2005 10 17 QXEA200501344 120051012A3040SLYZ50970 CONTROLLER DHAV DHC8 DHC8202 2809007NM WINDSHIELD HEAT MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09360PH295217981 515 PDX FLIGHT 2289 RIGHT WINDSHIELD HOT CAUTION LIGHT ON TOP OF DESCENT. WINDSHIELD FELT HOT, OAT WAS +1 DEGREE CELCIUS. RAN CHECKLIST AND THEN LIGHT WENT OUT. MAINTENANCE REPLACED RIGHT WINDSHIELD HEAT CONTROLLER IAW ANN TASK 30-41-00-710-801. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051017001702005101700170WP 2005 10 17 DHL2005806521 120050831A5310 DOOR FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH87034 46002 D-BELLY DOOR FRAME UPPER AFT CORNER CRACKED 1.000. PERFORMED STOP HOLE IAW SRM 52-2-0 PG 1. FABRICATED DOUBLER IAW SRM 52-4-1 FIG 4, SRM 51-1-4 PG 1. HEAT TREATED FROM 2024T3 TO 2024T4 IAW SRM 51-1-1 PG 1, 13, 17. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20051017001742005101700174WP 2005 10 17 DHL2005806506 120050819A5320 ANGLE DOUG DC8 DC873F 302199FWP LT MLG WW CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH87034 46002 LEFT MLG W/W REINFORCING ANGLE CRACKED 1 INCH (STA 946.000 - XCW 69.500). REMOVED CRACKED REINFORCING ANGLE IAW SRM 51-1-21, SRM 51-3-0, SRM 57-1-0. FABRICATED NEW REINFORCING ANGLE (AL2024T3 0.040") IAW SRM 57-2-0 PG 1, SRM 51-1-4 PG 1. CLEANED, TREATED AND PRIMED AREA AND REINFORCING ANGLE IAW SRM 51-1-8B. INSTALLED NEW REINFORCING ANGLE IAW SRM 51-1-21, SRM 51-3-0. TORQUED IAW SRM 51-3-1 TABLE III. 2L74 4F RT4A25 20051017001792005101700179EA 2005 10 17 QXEA200501294 120050917A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA BS 310 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09617QX 10130 YYC - FUSELAGE EXTERIOR HAS SCRATCHES AT FORWARD AIRSTAIR DOOR CUTOUT FS 310 STR 15L. REMOVED DAMAGE IAW CRJ-700 SRM 53-21-01-101-801-A01. RE-PROTECTED AND PAINTED AREA. 2L72 4F RTA21EA 20051017001802005101700180EA 2005 10 17 QXEA200501295 120050917A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA BS 295 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09617QX 10130 YYC - FUSELAGE EXTERIOR HAS SCRATCHES AND NICKS AROUND THE LEFT PITOT HEAT PROBE DOUBLER AT FS 295. BLENDED DAMAGE OUT IAW EA R-53-298 AND REO 670-53-21-128. PRIMED AND REPAINTED AREA. 2L72 4F RTA21EA 20051017001862005101700186WP 2005 10 17 AALA20050632 120051002A3350 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21228AA 49178 SAT - AFT OVERWING AND OVERHEAD EMERGENCY LIGHTS AT ROWS 24 - 28 INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK FOR AFT OVERWING AND OVERHEAD EMERGENCY LIGHTS FOR ROWS 24 - 28. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051017001932005101700193NM 2005 10 17 AALA20050646 120051005A3397 CONNECTOR BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21799AN 30258 LHR - EMERGENCY PATH LIGHTING IN REAR SECTION OF CABIN INOPERATIVE. FOUND PLUG D3204J DISCONNECTED AT SEAT 33C. REFITTED PLUG FOR EMERGENCY PATH LIGHTING IN REAR SECTION OF CABIN AT SEAT 33C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20051017001962005101700196NM 2005 10 17 AWXA200501182 120050909A53306545766 SKIN BOEING737 7373G7 1384595NM BS 518 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 MCN - DURING C18 CHECK DISCOVERED FUSELAGE SKIN CRACKED, .60 INCHES IN LENGTH, AT BS 518 AND STRINGER 12L. MAINTENANCE TRIMMED OUT DAMAGED SKIN IAW AMERICA WEST AIRLINES (AWA) ENGINEERING REPAIR (ER) NR 03-5300-05278-ES1. FABRICATED FILLER, DOUBLER, TRIPLER IAW AWA ER 03-5300-05278-ES1. INSTALLED FABRICATED REPAIR PARTS AT BS 518 AND STRINGER 12L IAW AWA ER 03-5300-05278-ES1. 2L72 4F RTA16WE 20051017002022005101700202EA 2005 10 17 QXEA200501319 120050917A5315CC6703329213 FLOORBEAM CNDAIRCL600 CL6002C10 1390015EA BS 280 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09617QX 10130 YYC - FLIGHT DECK FLOOR SUPPORT ANGLES AT FS 280 LBL 11 TO RBL 11 ARE CORRODED. REPLACED ANGLES IAW CRJ-700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20051017002042005101700204EA 2005 10 17 QXEA200501312 120050917A7830 STRUCTURE CNDAIRCL600 CL6002C10 1390015EA THRUST REVERSER GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09617QX 10130 YYC - LEFT ENGINE UPPER COWLING STRUCTURE ABOVE 6TH LATCH FROM THE FRONT IS GOUGED. BELNDED DAMAGE IAW EA R-71-117 AND REL 670-78-34-450 STEPS 1, 2 AND 3. RESTORED FINISH. 2L72 4F RTA21EA 20051017002062005101700206NM 2005 10 17 CALA0500360 120051013A531565C3394825 FLOORBEAM BOEING737 737524 1384721NM BS 947.5 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2732626 27530 HEAVY CORROSION IN AFT CABIN STA 947.5 FROM LBL 10 TO RBL 15. REPAIRED CHORD PER ECRA 5311-01242. 2L72 4F RTA16WE 20051017002072005101700207NM 2005 10 17 CALA050361 120051014A531565C339502 FLOORBEAM BOEING737 737524 1384721NM BS 986.5 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2732626 27530 AFT CABIN FLOORBEAM CHORD HEAVILY CORRODED AT STA 986.5. REPAIRED CHORD PER ECRA 5311-01241. 2L72 4F RTA16WE 20051017002082005101700208NM 2005 10 17 05FDEA03409 120051012A5320 WEB BOEING727 727100 1384036NM BS 344 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 WHILE WORKING N01046 FOUND WEB AT BS 344 LBL 32 CRACKED. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-40-02 ON WEB AT BS 344 LBL 32. 2L73 4F RTA3WE 20051017002092005101700209NM 2005 10 17 05FDEA03410 120051012A5315 FLOORBEAM BOEING727 727100 1384036NM BS 344 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 CORROSION BS 344 FLOORBEAM LBL 55 TO RBL 10. REPAIRED BS 344 FLOORBEAM LBL 55 TO RBL 10 PER FED-EX DWG SR 27-53-007. 2L73 4F RTA3WE 20051017002112005101700211NM 2005 10 17 05FDEA03412 120051012A5320 CHANNEL BOEING727 727200 138407ENM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25265FE 21671 LEFT AFT SERVICE DOOR ZEE CHANNEL HAS BARE METAL AND CORROSION AT STRINGER 17L FROM STA 1045 TO 1060. REMOVED AND REPLACED CHORD ANGLE IAW BOEING DRAWING 65-56148 AND FX SRM B727 53-10-8 AND 51-30-2. 2L73 4F RTA3WE 20051017002142005101700214 2005 10 17 QXEA200501279 420051003A34207003360941 AHRS DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE COCPIT FAILED A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09354PH13448705 498 SEA FLIGHT NR 2297 CAPTAINS AHRS FAILED. MAINTENANCE REPLACED AHRS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20051017002162005101700216EU 2005 10 17 YENA200569 120050923A27804917011 COMPUTER AIRBUS320 A320232 3930326EU IAE V2524 V2524A5 NE SLATS INOPERATIVE A YENAO OTHER J WARNING INDICATION DEDESCENT 1 EA15624JB173 2520 F/CTL SLATS LOCKED, WING TIP BRK ON. HAPPENED ON DECENT ABOUT 2 HRS INTO FLIGHT. AFTER EXTENSIVE TROUBLESHOOTING REPLACED NR 2 SFCC. AIRCRAFT HAS BEEN OPERATED ON AN EVALUTION FLIGHT, NO ECAM SYSTEM WARNINGS, CAUTIONS OR FLAP INDICATION ANOMALIES NOTED. SFCC SYSTEM 1 AND 2 HAVE BEEN BITE CHECKED IAW AMM 27-51-00-740-002 AND 27-81-00-740-002, NO DEFECTS NOTED AIRCRAFT IS RETURNED TO SERVICE. 2L72 4F4 FRTA28NM E40NE 20051017002172005101700217 2005 10 17 PIDA20050170 420051008A22104051601932 CONTROL PANEL BOEING737 7373G7 1384595NM AUTOPILOT MALFUNCTIONED A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05390WL 23219 MCP COURSE DISPLAY SKIPS NUMBERS. REPLACED MODE CONTROL PANEL PER MM 22-01-00. GROUND OPS CHECKS GOOD. 2L72 4F RTA16WE 20051017002202005101700220EU 2005 10 17 B65A106130 120050921A7712G55567 METER BOLKMS105 BO105LSA1 5626021EU ALLSN 250C 250C28 03013GL TORQUE UNSERVICEABLE B B65AO OTHER N FALSE WARNING CRCRUISE 1 GL13202LF 2014 CAE280089 TORQUE KEEPS FLUCTUATING. 1G72 3U3 U H3AU E1GL 20051017002232005101700223NM 2005 10 17 SWAA053082 120051009A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM BS 409 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 409, STR 17R. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20051017002242005101700224NM 2005 10 17 SWAA053083 120051009A53116517685 FRAME BOEING737 7373H4 1384600NM BS 348 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 348.2, STR 17L. REPAIRED FRAME WEB PER SRM. 2L72 4F RTA16WE 20051017002252005101700225NM 2005 10 17 SWAA053084 120051009A3350311500 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED 1/4D CHECK, FOUND BULLNOSE EMERGENCY LIGHT LENS LOOSE AT ROW 10 ABC. REMOVED AND REPLACED LENS PER MM. 2L72 4F RTA16WE 20051017002262005101700226NM 2005 10 17 SWAA053085 120051009A53306545777 SKIN BOEING737 7373H4 1384600NM BS 950 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 950, STR 10R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051017002292005101700229NM 2005 10 17 SWAA053088 120051009A53306545765 SKIN BOEING737 7373H4 1384600NM BS 500D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 12L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051017002352005101700235NM 2005 10 17 SWAA053103 120051009A2560P2070001 FLASHLIGHT BOEING737 737317 138447PNM AFT GALLEY ACTIVATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 AFT GALLEY INBD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2L72 4F RTA16WE 20051017002372005101700237NM 2005 10 17 05FDEA03316 120051009A5710651926012 HINGE BOEING727 727227 1384078NM AILERON CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25484FE 21466 RT OB AILERON 2ND FROM I/B HINGE ASSY FLANGE SECTION MISSING. REMOVED AND REPLACED HINGE ASSY IAW SRM 51-30-2. 2L73 4F A3WE 20051017002382005101700238NM 2005 10 17 05FDEA03317 120051009A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 HORIZ STAB RT BARREL NUT BORE NR 4 FOUND WITH CORROSION. REWORK/ REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 23. MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20051017002392005101700239NM 2005 10 17 05FDEA03318 120051009A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 LEFT HORIZ STAB BARREL NUT BORE NR 17 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 34. MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20051017002412005101700241NM 2005 10 17 05FDEA03320 120051009A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 LEFT HORIZ STAB BARREL NUT BORE NR 3 FOUND WITH CORROSION. REWORK/ REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 38. MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20051017002432005101700243NM 2005 10 17 05FDEA03322 120051009A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 RT HORIZ STAB BARREL NUT BORE NR 18 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 35. MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20051017002442005101700244 2005 10 17 BB05088 420051009A2210 MODULE BOEING767 767201 1385125NM RUDDER MALFUNCTIONED A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19648US 23900 FLIGHT 43, AMS-PHL - ON CLIMB-OUT FROM AMS, AILERON LOCKOUT AND RUDDER RATIO EICAS MESSAGES DISPLAYED. DIVERTED TO LGW. RESET LEFT AND RIGHT SAM MODULES AND LEFT RUDDER RATIO CHANGER MODULE. NO FURTHER FAULTS NOTED. 2L72 4F RTA1NM 20051017002452005101700245NM 2005 10 17 PIDA20050171 120051006A3350 BATTERY PACK BOEING737 7372K5 138448XNM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05250TR 22597 RIGHT SIDE EMERGENCY LIGHT FOR OVERWING EXIT NOT ILLUMINATING. REPLACED RIGHT SIDE OVERWING EXIT LIGHT BATTERY PACK. LIGHT OPS CHECKS GOOD. 2L72 4F RTA16WE 20051017002472005101700247 2005 10 17 PIDA20050172 420051007A2230244202389 TRANSFORMER BOEING737 7372K5 138448XNM ELECTRICAL FAILED A PIDAK NONE O OTHER NRNOT REPORTED 1 SO05250TR 22597 AUTO THROTTLES WON'T ENGAGE. LOSS OF VALID AIR DATA SPEED SIGNAL PREVENTED AUTO THROTTLE ENGAGEMENT. REPLACED T98 TRANSFORMER IN J4 BOX PER WDM SPM CHAPTER 20 DUE TO SHORT. AUTO THROTTLES OPS CHECK GOOD PER MM 22-31-01. 2L72 4F RTA16WE 20051017002482005101700248NM 2005 10 17 SB05128 120051008A2710R15048 ACTUATOR BOEING737 7373B7 1384580NM AILERONS FAULTY A USAAO OTHER F FLT CONT AFFECTED APAPPROACH 1 EA19522AU3574535745 23857 PHL - FLT1243 - ON APPROACH TO PHL, WHEN AUTO PILOT WAS MANUALLY DISCONNECTED AT 1,000 FT AGL, THE AIRCRAFT ROLLED TO THE LEFT. AILERON TRIM SYSTEM WAS FOUND TO BE INTERMITTENT. BOTH THE CAPTAIN AND FIRST OFFICER WERE REQUIRED TO REGAIN LEVEL FLIGHT. CREW NOTED THAT THE FUEL WAS IN-BALANCE AND USED ABOUT 1 UNIT OF RIGHT AILERON TRIM. AFTER LANDING, AILERONS POSITIONED 3 UNITS OF TRIM TO LT. AILERON TRIM SWITCHES ARE INTERMITTENT AS OCCASIONALLY THE AILERONS MOVE AFTER TRIM SWITCHES ARE RELEASED. FLT TAXIED TO THE GATE. MX R/R`D THE AILERON TRIM ACTUATOR PER MM 27-11-54. OPS CHECK GOOD. ALSO, R/R`D THE AILERON/RUDDER TRIM CONTROL MODULE P8-43, AS PRECAUTIONARY, PER MM 27-11-94. OPS CHECK GOOD. 2L72 4F RTA16WE 20051017002492005101700249NM 2005 10 17 AMTA200500711 120050920A2612 FIRE LOOP BOEING757 75723N 1384973NM RROYCERB211 RB211* 54555NE RT ENGINE MALFUNCTIONED A AMTAO OTHER N FALSE WARNING CLCLIMB 1 GL21519AT 27975 RT ENGINE FIRE LP 2 DISPLAYED. PERFORMED FIM 26-11-00, FIG 103 BITE PROCEDURE. NO FAULTS FOUND COULD NOT DUPLICATE. INSPECTED ENG LOOPS FOR DEFECTS. NONE FOUND. OK FOR SERVICE. (K) 2L72 4F4 FRTA2NM A12EU 20051018000012005101800001NM 2005 10 18 C1HA200594003 120051014A5330 SKIN BOEING727 727290 138408WNM FUSELAGE CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15294AS 22146 L1 DOOR LOWER HINGE CUTOUT ON FUSE SKIN IS CRACKED. CUT OUT DAMAGED AREA, FABBED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SB 727-53A0198 REV 2 FIG 3 & 5. 2L73 4F A3WE 20051018000052005101800005NM 2005 10 18 C1HA200594007 120051017A5311 FRAME BOEING727 727290 138408WNM BS 950F DENTED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15294AS 22146 AFT CARGO COMPT FRAME AT STA 950F IS DENTED BETWEEN STR 25L - 026L. FOUND DENT OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 1. CUT OUT DAMAGE AREA IAW B727 SRM 51-10-1. FABRICATED ANGLE REPAIR IAW B727 SRM 53-10-2 FIG 3 AND 51-20-1. TREATED AND PRIMED PORT AND AREA IAW B727 SRM 51-10-2. INSTALLED REPAIR IAW B727 SRM 51-30-2. 2L73 4F A3WE 20051018000062005101800006NM 2005 10 18 C1HA200594008 120051017A5322 SHEAR TIE BOEING727 727290 138408WNM BS 312 CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15294AS 22146 RT SIDE OF THE NOSE WHEEL WELL DOGHOUSE FRAME AT STA 312 IS CRACKED. CUT OUT DAMAGED FRAME TO SKIN ATTACHMENT ANGLE FABBED & INSTALLED REPAIR SHEAR TIE IAW 727 SRM 53-10-4 FIG 15. 2L73 4F A3WE 20051018000082005101800008NM 2005 10 18 C1HA200594010 120051017A5740 SUPPORT BOEING727 727290 138408WNM SPOILER ACTUATORBROKEN A C1HAK NONE O OTHER ININSP/MAINT 1 GL15294AS 22146 NR 12 SPOILER ACTUATOR OUTBOARD SUPPORT IS BROKEN WS 510. REMOVED AND REPLACED NR 12 SPOILER ACTUATOR O/B SUPPORT IAW B727 MM 27-61-0 AND SRM 51-30-2 NR 12 SPOILER ACTUATOR, OP CHECK GOOD IAW B727 MM 27-61-0. 2L73 4F A3WE 20051018000092005101800009WP 2005 10 18 DHL2005806538 120050906A5313 LONGERON DOUG DC8 DC873F 302199FWP BS 1260-1280 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH87034 46002 AFT CARGO COMPT L-34L CRACKED 1.5 INCH BETWEEN STA 1260 & STA 1280. PERFORMED MAJOR REPAIR. REMOVED FASTENERS, CUT OUT CRACKED LONGERON SEGMENT, PERFORMED NDT INSP OF WORK AREA, NO CRACK NEITHER CORROSION FOUND. FABRICATED NEW LONGERON SEGMENT. PERFORMED NDT INSP OF NEW LONGERON SEGMENT. FABRICATED SPLICE & DOUBLER. CLEANED, TREATED AND PRIMED AREA & REPAIR PARTS. APPLIED SEALANT (PRC) TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW SRM 53-2-2 FIG 13, TR 53-191, SRM 51-1-20D, SRM 51-3-1. 2L74 4F RT4A25 20051018000102005101800010WP 2005 10 18 DHL2005806536 120050906A5313 LONGERON DOUG DC8 DC873F 302199FWP BS 1260-1280 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH87034 46002 AFT CARGO COMPT L-34R CRACKED 7.5 INCH BETWEEN STA 1260 & 1280. PERFORMED MAJOR REPAIR. REMOVED FASTENERS, CUT OUT CRACKED LONGERON SEGMENT, PERFORMED NDT INSPECTION OF WORK AREA. NO CRACK NEITHER CORROSION FOUND. FABRICATED NEW LONGERON SEGMENT. PERFORMED NDT INSPECTION OF NEW LONGERON SEGMENT. FABRICATED SPLICE & DOUBLER IAW SRM 53-2-2 FIG 13. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW SRM 53-2-2 FIG 13. 2L74 4F RT4A25 20051018000112005101800011WP 2005 10 18 DHL2005806537 120050906A5313 LONGERON DOUG DC8 DC873F 302199FWP BS 1270-1280 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH87034 46002 AFT CARGO COMPT L-36 CRACKED 7 INCHES BETWEEN STA 1270 & 1280. PERFORMED MAJOR REPAIR. REMOVED FASTENERS, CUT OUT CRACKED LONGERON SEGMENT, PERFORMED NDT INSP OF WORK AREA IAW DC8 NDT SPM PART 06-10-01-001. NO CRACK NEITHER CORROSION FOUND. FABRICATED NEW LONGERON SEGMENT. PERFORMED NDT INSPECTION OF THE NEW LONGERON SEGMENT. FABRICATED SPLICE AND DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW SRM 53-2-2 FIG 13, TR 53-191, SRM 51-1-20D, SRM 51-3-1. 2L74 4F RT4A25 20051018000122005101800012WP 2005 10 18 DHL2005806520 120050828A5330 SKIN DOUG DC8 DC873F 302199FWP BS 1868 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH87034 46002 EXTERIOR AFT FUSELAGE DOUBLER REPAIR FASTENERS SHEARED, STA 1868 BETWEEN L-36 & L-32L AND CORROSION ON ADJACENT SKIN TO DOUBLER REPAIR. PERFORMED MAJOR REPAIR. REMOVED EXISTING REPAIR DOUBLER. REMOVED CORROSION FROM ADJACENT SKIN. FOUND OUT OF LIMITS. CUT OUT DAMAGED AREA IAW SRM 53-2-1 FIG 7 SHEET 1-5. PERFORMED DETAIL VISUAL INSP OF AREA, NO CRACK NEITHER CORROSION FOUND. FABRICATED REPAIR DOUBLER, 2 EA INTERNAL FINGER DOUBLERS AND FILLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS IAW SRM 53-2-1 FIG 7 SHEET 1-5, SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1 PG 2A. 2L74 4F RT4A25 20051018000152005101800015WP 2005 10 18 DHL2005806513 120050826A5540 WEB DOUG DC8 DC873F 302199FWP RUDDER CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH87034 46002 RUDDER WEB LWR PART CRACKED .5 INCH STA ZR. 61.156. PERFORMED MAJOR REPAIR. REMOVED CRACKED RIB WEB IAW SRM 51-1-21 PG 1. FABRICATED NEW RIB WEB, 2EA DOUBLERS AND 2EA COVERS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS IAW BOEING MSGS 1-113628973-3, 1-113628973-2, ROD SKETCH 05-08-12-002 (SRM 55-2-3 FIG. 5), SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1. REBALANCED RUDDER IAW SRM 51-4-6 PG 1-6. INSTALLED 1EA COUNTERWEIGHT P/N 3702567505 AT STA 161.000. FOUND WITHIN TOLERANCE (MOMENT 24637 IN-LB). 2L74 4F RT4A25 20051018000182005101800018CE 2005 10 18 DXTA200501028 120051016A3246 YAW DAMPER CESSNA750 750 2076810CE MLG MALFUNCTIONED E DXTAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 GL07942QS 7500024 ABORTED T/O IN TEB DUE TO EXCESSIVE VIBRATION DURING T/O AND YAW DAMPER OFF LOWER CAS MESSAGE. ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20051018000192005101800019CE 2005 10 18 DXTA200501027 120051016A3260 WARNING LIGHT CESSNA500 560CESSNA 2076750CE MLG ILLUMINATED E DXTAO OTHER J WARNING INDICATION APAPPROACH 1 GL07837QS 5600685 UPON GEAR EXTENSION GOING INTO SUN, THE GEAR LIGHTS INDICATED 2 GREEN 1 RED. THE LT MAIN WAS NOT INDICATING GREEN. TURNED OUT OF THE VALLEY TO RUN THE EMERGENCY CHECKLIST ABOUT ONE MINUTE AFTER THE INITIAL GEAR EXTENSION THE LEFT MAIN INDICATED GREEN. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20051018000202005101800020CE 2005 10 18 DXTA200501022 120051014A2120 ODOR CESSNA750 750 2076810CE COCKPIT DETECTED E DXTAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 GL07951QS 7500151 REMOTE CB TRIPPED CYAN CAS MESSAGE CAME ON DURING DESCENT. BURNING ODOR WAS NOTICED FOR ABOUT 30 -45 SEC. ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20051018000232005101800023NM 2005 10 18 SB05132 120051016A3397 CONNECTOR BOEING737 7373B7 1384580NM EMERGENCY LIGHTSDAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19395US 23317 CLT - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHTS AT THE FORWARD ENTRY AND SERVICE DOORS AND SEAT ROWS 1 THROUGH 4 WERE INOPERATIVE. MAINTENANCE FOUND 2 PINS BACKED OUT OF CONNECTOR D9021J. REMOVED AND REPLACED CONNECTOR. ALSO, FOUND FORWARD ENTRY DOOR IDENTIFIER LIGHT ASSEMBLY SHORTED. REMOVED AND REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECK OF EMERGENCY LIGHTS GOOD. 2L72 4F RTA16WE 20051018000252005101800025 2005 10 18 DXTA200501023 420051014A3414HG1153CA02 AIR DATA MODULE CESSNA680 680CE 2076811CE COCKPIT FAILED E DXTAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 GL07338QS835 6800011 AIR SPEED RT PFD FAILED, NO AIRSPEED INDICATION ON TAKEOFF ROLL. LEAK CHECKED COPILOT PITOT STATIC SYSTEM WITH NO DEFECTS NOTED. SYSTEM OPERATED NORMALLY. SWAPPED NR 1 AND NR 2 AIR DATA MODULES FOR FURTHER TROUBLESHOOTING IAW CE680 M/M CH 34-12-00, 34-11-00. PERFORMED STATIC LEAK CHECK IAW FAR 91.411. LEAK AND OPERATIONAL CHECKS GOOD. 2L72 4F RCT00012WI 20051018000262005101800026WP 2005 10 18 DHL2005806522 120050831A5313S25972423 LONGERON DOUG DC8 DC873F 302199FWP BS 8-35 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH87034 46002 FWD ACCY COMPT LONGERON 28R CRACKED 1 INCH STA 8.000-35.000 MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 53-3-3 FIG 2 SHEET 1, SRM 51-2-0 FIG 52 SHEET 1. REMOVED DAMAGED LONGERON IAW SRM 53-1-0 PG 1, SRM 51-1-21. FABRICATED NEW LONGERON IAW SRM 53-3-3 FIG 2 SHEET 1 ITEM R, SRM 51-2-0 FIG 52 SHEET 1. PERFORMED NDT INSP IAW DC8 NDT SPM PART 08-00-02 TO 07. HEAT TREATED NEW LONGERON IAW SRM 51-1-1 PG 1, 13, 17. CLEANED, TREATED AND PRIMED AREA AND NEW LONGERON IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW LONGERON IAW SRM 51-1-21. 2L74 4F RT4A25 20051018000272005101800027WP 2005 10 18 DHL2005806509 120050823A5751 SKIN DOUG DC8 DC873F 302199FWP LT WING AILERON DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH87034 46002 LT WING O/B AILERON LWR SKIN RIVETS SHEARED, XA 722 - XA 752 (PLATING DAMAGED). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-8-1 FIG 4, DOUGLAS DWG 5763133. REMOVED DAMAGED PANEL PLATING IAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICATED NEW PANEL AND BONDED FINGER DOUBLER IAW SRM 57-8-1 FIG 4. BONDED REPAIR PARTS IAW SRM 51-1-9. CLEANED, TREATED AND PRIMED NEW PANEL PLATING INNER FACE IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11. INSTALLED NEW PANEL PLATING IAW SRM 51-1-21. PERFORMED LT OUTBOARD AILERON BALANCING IAW SRM 51-4-3 PG 1-3. FOUND WITHIN LIMITS. 2L74 4F RT4A25 20051018000282005101800028WP 2005 10 18 DHL2005806533 120050822A5751 ACCESS DOOR DOUG DC8 DC873F 302199FWP AILERON CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH87034 46002 RT OUTBOARD AILERON COUNTERWEIGHTS ACCESS DOOR INTERIOR CORRODED STA XA 615.000 - 630.000. REMOVED CORROSION FROM ACCESS DOOR IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. REMOVED ACCESS DOOR IAW SRM 57-1-0, 51-3-0. FABRICATED NEW ACCESS DOOR IAW SRM 57-8-1 FIG 4, SRM 51-1-4. CLEANED, TREATED AND PRIMED NEW ACCESS DOOR AND AREA IAW SRM 51-1-8B. INSTALLED NEW ACCESS DOOR IAW SRM 51-3-0, SRM 51-3-1. PERFORMED RT OUTBOARD AILERON BALANCING IAW SRM 51-4-3 PG 1-3. FOUND WITHIN ALLOWABLE LIMITS. 2L74 4F RT4A25 20051018000292005101800029NE 2005 10 18 QXEA200501349 220051016A7200 WARNING LIGHT DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE ENGINE ILLUMINATED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09348PH 484 PCEAE0009 SEA - FLIGHT 2060, ENGINE MANUAL CAUTION LIGHT. COMPLIED WITH RESET AND TEST PROCEDURES PER MCN 27631-01. TEST GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20051018000332005101800033NM 2005 10 18 QXEA200501348 120051016A241023088002B GENERATOR DHAV DHC8 DHC8202 2809007NM DC SYSTEM MALFUNCTIONED A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09367PH7511 984 511 SEA - FLIGHT 2085, NR 2 DC GENERATOR INOP. MAINTENANCE REPLACED NR 2 DC GENERATOR IAW AMM 8-10-11. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051018000342005101800034EA 2005 10 18 VTZA200500212 120051014A274170609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB TRIM FAILED A VTZAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 EA27662BR 3255 7526 DUAL STAB TRIM AND MACH TRIM FAILURE. REPLACED HORIZONTAL STABILIZER TRIM CONTROL UNIT. 2L72 4F RTA21EA 20051018000382005101800038WP 2005 10 18 UPS05845606 120051003A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP BS 940 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE:C2 FLOORBEAM HEAVY CORROSION STA 940 LBL 60 UNDER THE SEAT TRACK. CUT OUT DAMAGED AREA OF FLOORBEAM IAW SRM 53-2-0 AND TEMP REV 53-152, FABRICATED AND INSTALLED REPAIR ANGLE AT STA 940 LBL 60 IAW SRM 53-2-0 TEMP REV 53-152, AND SRM 51-1-20D. 2L74 4F RT4A25 20051018000392005101800039WP 2005 10 18 UPS05845611 120050829A5312 PRESSURE PANEL DOUG DC8 DC873F 302199FWP BS 902 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE:C3 CORROSION UNDER STIFFENER ON RIGHT W/W CEILING STA 902 RBL 50-55. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW UPS EO DC8-5310- 23036-A AND SAA SK 801-804599. 2L74 4F RT4A25 20051018000422005101800042EA 2005 10 18 COMA0560552 120051012A335020131A BATTERY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCHARGED A COMAO OTHER O OTHER NRNOT REPORTED 1 SO01810CA 7370 FLIGHT 5605 - FLOOR LEVEL EMERGENCY LIGHTS AT CABIN AND SERVICE DOOR ARE INOPERABLE. REPLACED EMERGENCY BATTERY. 2L72 4F RTA21EA 20051018000442005101800044EA 2005 10 18 COMA0560554 120051014A2741 MOTOR CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01457CA 7612 FLIGHT 5569 - STAB AND MACH TRIM CAUTION. CND, OPERATIONAL CHECK WAS NORMAL. 2L72 4F RTA21EA 20051018000452005101800045EA 2005 10 18 COMA0560555 120051015A2750865D1007 PDU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01446CA10913 7546 FLIGHT 5876 - FLAPS FAIL. REPLACED THE PDU. 2L72 4F RTA21EA 20051018000482005101800048NM 2005 10 18 UPS05M45607 120050831A5347S4929147 SEAT TRACK DOUG MD11 MD11F 3023600NM BS 855-875 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01280UP 48634 INSPECTION TYPE:C, MAIN DECK MID-ENTRY AREA, SEAT TRACK ALONG LBL 8.5, CORROSION FOUND ON BASE, BETWEEN STA 855 AND STA 875. M/D MID ENTRY AREA CORROSION REMOVED FROM STA 855 TO STA 875. SEAT TRACK FASTENERS REMOVED & SPLICE CUT AT STA 832 TO STA 949, SRM 53-70-00 FIG 1 VOL 1 REV 37. HFEC CARRIED OUT & FOUND NO CRACK EVIDENT. REPAIR SPLICE FAB AS PER SRM 51-31-01 VOL II REV 37, REWORKED AREA REPROTECTED AND PAINTED. NEW SEAT TRACK EXT INSTALLED PER SRM 51-31-01 VOL II, 53-70-00 VOL I REV 37. 2L73 4F RTA22WE 20051018000492005101800049NM 2005 10 18 UPS05M45614 120051016A2150 A/C PACK DOUG MD11 MD11F 3023600NM ODOR A IPXAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO01275UP 48774 INSPECTION TYPE:N/A, STRONG ODOR - SMELLS LIKE BURNING PLASTIC. A/C DUCTS OPERATING AT NORMAL TEMPS. MULITPLE REPEAT GRIPES. REMOVED AND REPLACED PACKS 1, 2 AND 3 COALESCER BAGS PER MM 21-54-05-2. 2L73 4F RTA22WE 20051018000522005101800052EU 2005 10 18 TRBA2005063 120050913A612330048000018 AUTOFEATHER SYS AEROSPATR72 ATR72212 8680945EU INOPERATIVE A TRBAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO29448AM 448 AUTOMATIC TAKEOFF POWER CONTROL SYSTEM (ATPCS) DID NOT ARM DURING TAKEOFF POWER. REPLACED AUTO FEATHERING UNIT. (K) 2H72 4T RTA53EU 20051018000532005101800053EA 2005 10 18 A6WA200540309 120050921A5210 DRAG ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31425AW 7663 PASSENGER DOOR DRAG ANGLE IS CRACKED 1.0 INCH IN RADIUS ABOVE POWER ASSIST CABLE SUPPORT PULLEY BRACKET. MAINTENANCE REPAIRED PAX DOOR ANGLE IAW MDG REO. (K) 2L72 4F4 FRTA21EA E15NE 20051018000542005101800054EA 2005 10 18 SWIA200515678 120051009A335020131A BATTERY CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT DISCHARGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07750SK7877 7877 10207 OVERHEAD EMERGENCY LIGHTS WILL NOT COME ON WHEN TESTED. REPLACED BATTERY PACK NR 1 AND BATTERY POWER SUPPLY NR 1 REF CRJ MM 33-51-17. OPERATIONAL CHECK GOOD, PN 11-0049, SN OFF 20881. 2L72 4F RTA21EA 20051018000592005101800059WP 2005 10 18 UPS05845600 120051003A534046401621N FITTING DOUG DC8 DC873F 302199FWP BS 1500 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE:C2 STA 1500 L21R FUSELAGE FRAME TO CUSP FITTING HEAVY CORROSION. REMOVED FRAME FITTING TO CUSP AT FS 1500 L21R IAW 51-1-8 AND SRM 53-02-0 FIG 1F. REPLACED FUSELAGE FRAME TO CUSP FITTING IAW SRM 51-3-2, AND SRM 51-1-20D. 2L74 4F RT4A25 20051018000602005101800060WP 2005 10 18 UPS05845601 120051004A534037739061 FITTING DOUG DC8 DC873F 302199FWP BS 822.5 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE:C2 FS 822.500 RBL 24 FWD FITTING CRACKED. REMOVED AND REPLACED FITTING AT FS 822.500 RBL 24 IAW SRM 51-1-20D, 51-3-2 AND SRM 51-3-0. 2L74 4F RT4A25 20051018000612005101800061WP 2005 10 18 UPS05845602 120051003A5340 FITTING DOUG DC8 DC873F 302199FWP BS 70 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE:C2 CORROSION ON END FITTING AT L35L BS 70 A/C COMPT. REMOVED AND REPLACED END FITTING IAW SRM 51-1-21, 51-1-8 SRM 53-2-0 AND 51-1-20D. 2L74 4F RT4A25 20051018000642005101800064NM 2005 10 18 SWAA053162 120051013A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM BS 787-807 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CORRODED BETWEEN BS 787 TO BS 807, STR 26R. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20051018000652005101800065 2005 10 18 SWAA053163 420051012A25656949956 CABLE BOEING737 7373H4 1384600NM R2 DOOR SLIDE MISROUTED A SWAAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW29324SW 23414 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE LATCH CABLE ASSY MISROUTED. REROUTED CABLE ASSY PER MM. 2L72 4F RTA16WE 20051018000672005101800067NM 2005 10 18 SWAA053165 120051012A3350MS155721 BULB BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT ROW 13. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20051018000692005101800069NM 2005 10 18 SWAA053167 120051013A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29451WN 32495 EEPLS TRACK LIGHT INOP AT FWD END. REMOVED AND REPLACED EEPLS TRACK PER MM. 2L72 4F RTA16WE 20051018000712005101800071NM 2005 10 18 SWAA053169 120051013A57126545445 RIB BOEING737 7375H4 138449DNM LT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED 1/2D CHECK, FOUND LT WING RIB LOWER CHORD CRACKED AT WBL 135.5, STR 2. REPAIRED RIB PER SWA EA. 2L72 4F RTA16WE 20051018000722005101800072NM 2005 10 18 SWAA053170 120051013A53306545768 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR CUTOUT, LOWER AFT CORNER. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051018000742005101800074NM 2005 10 18 SWAA053172 120051013A53126546568 BULKHEAD BOEING737 7375H4 138449DNM BS 1016 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED 1/2D CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT STR 23R, 5 O'CLOCK POSITION. REPAIRED WEB PER SWA EA. 2L72 4F RTA16WE 20051018000762005101800076NM 2005 10 18 05FDEA03332 120051010A5311 FRAME BOEING727 72722 1384002NM BS 804 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 UPPER LOBE INTERIOR FRAME IS CRACKED BS 804 RBL 68, WL 210.5. REMOVED AND REPLACED FRAME PER SRM 51-30-02. 2L73 4F A3WE 20051018000772005101800077NM 2005 10 18 05FDEA03333 120051010A5322 SHEAR TIE BOEING727 72722 1384002NM BS 990 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 FOUND CORROSION ON SHEAR TIE BS 990 LBL 10 WL 148. REPAIRED SHEAR TIE AT BS 990, LBL 10 PER SRM 53-10-4. 2L73 4F A3WE 20051018000782005101800078NM 2005 10 18 05FDEA03334 120051010A5320 SPLICE BOEING727 72722 1384002NM BS 680 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 STR 15L END SPLICE/CLIP IS CRACKED AT AFT FASTENER BS 680. REMOVED DAMAGED CLIP AT STR 5L, BS 680 AND INSTALLED IAW SRM 51-30-2. 2L73 4F A3WE 20051018000792005101800079NM 2005 10 18 05FDEA03335 120051010A5313 STRINGER BOEING727 72722 1384002NM BS 503-509 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 UPPER LOCE INTERIOR STRINGER IS CRACKED AT 6 EA FASTENER LOCATIONS BS 503-509 STR 16R. REMOVED AND REPLACED CRACKED STR. IAW SRM 51-30-2 AND SRM 53-10-2. 2L73 4F A3WE 20051018000802005101800080NM 2005 10 18 05FDEA03336 120051010A5322 SHEAR TIE BOEING727 72722 1384002NM BS 1030 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 CORROSION ON SHEAR TIE BS 1030 RBL 10 WL 148. REMOVED CORROSION ON SHEAR TIE FOUND TO BE OUT OF LIMITS. INSTALLED NEW SHEAR TIE, ALL WORK DONE IAW SRM 53-10-1, 53-10-4 & 51-30-2. 2L73 4F A3WE 20051018000812005101800081NM 2005 10 18 05FDEA03337 120051010A5322 SHEAR TIE BOEING727 72722 1384002NM BS 1030 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 CORROSION ON SHEAR TIE BS 1030 LBL 10. 2L73 4F A3WE 20051018000842005101800084NM 2005 10 18 05FDEA03181 120050930A5315 FLOORBEAM BOEING727 727225 1384077NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25465FE 21289 CORROSION ON FLOORBEAM AT STA. 344 FROM BL 12 L TO BL 12 R. REMOVED CORROSION FROM FLOOORBEAM UPPER CAP IAW FED-EX SRM 53-10- 1. REMOVED, FABRICATED AND INSTALLED SPLICES AND FLOORBEAM IAW SRDM SR27-53-007, B727 SRM 51-10-2,51-30-2. 2L73 4F A3WE 20051018000852005101800085NM 2005 10 18 05FDEA03182 120051001A5315 FLOORBEAM BOEING727 727225 1384077NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25462FE 22550 UPPER CHORD FLOORBEAM AT FS 344 LBL 22.5 TO RBL 22.5 CORRODED. REMOVED, FABRICATED AND INSTALLED CHORD AND HAT-CHANNEL IAW FED-EX DRAWING SR-27-53-007 AND B727 SRM 51-30-2. 2L73 4F A3WE 20051018000862005101800086NM 2005 10 18 05FDEA03183 120051001A5315 FLOORBEAM BOEING727 727225 1384077NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25462FE 22550 CORROSION ON FLOORBEAM UPPER SURFACE STA 560 LBL 24-62. REMOVED, FABRICATED, AND REPLACED T-CAP, WEB AND STIFFENER IAW B727 SRM 53-10-8 FIG 3, 51-10-2 AND 51-30-2. 2L73 4F A3WE 20051018000872005101800087EU 2005 10 18 05FDEA03184 120051001A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25659FE15605 757 MAIN DECK FLOOR ARTICULATED SEAT TRACK NR 6 RT ATTACH BOLT IS WORN BEYOND SERVICABLE LIMITS AT FRAME 54 MAX ALLOWABLE WEAR IS .039 ACTUAL MEASUREMENT .039. REMOVED SEAT TRACK IAW A300-600 SRM 51-40-21, RECEIVED NEW SEAT TRACK PO NR 499975.1. INSTALLED NEW SEAT TRACK IAW A300-600 SRM 51-40-21. 2L72 4F RTA35EU 20051018000892005101800089EU 2005 10 18 05FDEA03186 120051002A5330 FILLER AIRBUS310 A310203 3930313EU FUSELAGE SKIN MISSING A FDEAK NONE O OTHER ININSP/MAINT 1 SO25425FE 264 EXTERNAL DOUBLER AT FWD LOWER FUSELAGE NOSE SECTION AT FS 4 MISSING FILLER. 2L72 4F RTA35EU 20051018000902005101800090WP 2005 10 18 05FDEA03187 120051002A3243 CABLE DOUG DC10 DC1010 3022110WP BRAKE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25389FE 46623 BRAKE CABLE NR 144 RUSTY AT PULLEY BEND UNDER MAIN CARGO COMPARTMENT FLOOR STA 1450 RBL 37. REMOVED, REPLACED, ADJUSTED LEFT HAND BRAKE CONTROL SYSTEM, OPS CHECK GOOD IAW DC10-10 M/M 32-44-00-2 . 2L73 4F A22WE 20051018000912005101800091WP 2005 10 18 05FDEA03188 120051002A3243 CABLE DOUG DC10 DC1010 3022110WP BRAKE DAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25389FE 46623 BRAKE CABLE NR 148 AT PULLEY BEND UNDER MAIN CARGO CARGO FLOOR STA 1450 RBL 37. REMOVED, REPLACED, AND ADJUSTED LT BRAKE CONTROL SYSTEM. OPS CHECK GOOD . 2L73 4F A22WE 20051018000922005101800092NM 2005 10 18 05FDEA03323 120051009A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 RT HORIZ STAB BARREL NUT BORE NR 20 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 37. MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20051018000942005101800094NM 2005 10 18 05FDEA03325 120051009A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 RT HORIZ STAB BARREL NUT BORE NR 30 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 41. MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20051018000952005101800095NM 2005 10 18 05FDEA03326 120051009A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 RT HORIZ STAB BARREL NUT BORE NR 32 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 42. MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20051018000972005101800097NM 2005 10 18 SWAA053173 120051013A291065C26839 HOSE BOEING737 7375H4 138449DNM HYD SYSTEM LEAKING A SWAAA UNSCHED LANDING K FLUID LOSS NRNOT REPORTED 1 SW29521SW 25320 DECLARED EMERGENCY HYDRAULIC B-SYSTEM QUANTITY WENT TO ZERO. ENGINE & ELECTRIC B-PUMP LOW PRESSURE LIGHTS ILLUMINATED. REMOVED AND REPLACED HYDRAULIC B-SYSTEM FLEX HOSE AT HYDRAULIC ACCOUSTIC FILTER PER MM. 2L72 4F RTA16WE 20051018000982005101800098NM 2005 10 18 05FDEA03328 120051010A5320 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 FORWARD CARGO, LONGERON SPLICE ADJACENT TO STATION 765 LONGERON 45 LEFT HAND FOUND CRACK. REMOVED AND REPLACED WITH FABRICATED LONGERON SPLICE AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051018000992005101800099WP 2005 10 18 05FDEA03329 120051010A5712 RIB DOUG DC10 DC1010 3022110WP RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE RIGHT WING FIXED LEADING EDGE AT STA XORS 672 ZONE 625 FOUND RIB CRACK. REPAIRED FORMER INSTALLED REPAIR CLIP ARB1291-38 AND SRM 57-20-00 FIG.1 SHEET 4, 6 VOL 1. 2L73 4F A22WE 20051018001002005101800100NM 2005 10 18 UPS05445538 120051002A21507192389 ACM BOEING747 747121 1384871NM PWA JT9 JT9D7A 52054NE NR 1 INOPERATIVE A IPXAJA DUMP FUEL UNSCHED LANDING EB VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO01682UP 20349 NR 1 PACK ELEC SMOKE, VIBRATION AFTER TAKEOFF. VIBRATION STOPPED WITH NR 1 PACK OFF. REMOVED AND REPLACED NR 1 PACK AIR CYCLE MACHINE IAW AMM 21-51-04, RAN PACK ON GROUND FOR 2 HOURS, ALL OPERATIONS NORMAL. 2L74 4F4 F A20WE E20EA 20051018001022005101800102SO 2005 10 18 RAIA00510015 120051011A3350 POWER SUPPLY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03818HK 145059 PREFLIGHT INSPECTION, OVERHEAD EMERGENCY LIGHT INOP AT ROW 3. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY. 2L72 4T RTT00011AT 20051018001042005101800104NM 2005 10 18 AALA20050669 120051012A3397 CONNECTOR BOEING777 777223 1385213NM EMERGENCY LIGHTSLOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21790AN 30251 JFK - EMERGENCY LIGHTS FROM SEAT 39 TO 44 INOPERATIVE. FOUND LOOSE PLUG AT ROW 38. RECONNECTED AND SECURED PLUG FOR EMERGENCY LIGHTS FROM SEAT 39 TO 44. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20051018001052005101800105WP 2005 10 18 AALA20050670 120051009A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2114551 53033 SFO - EMERGENCY CEILING LIGHTS AT ROWS 3 TO 6 AND 23 TO 26 INOPERATIVE. REPLACED BATTERY PACKS AT ROWS 6 AND 25 FOR EMERGENCY CEILING LIGHTS AT ROWS 3 TO 6 AND 23 TO 26. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051013002202005101300220EA 2005 10 13 QXEA200501301 120050917A5730 SKIN CNDAIRCL600 CL6002C10 1390015EA LT WING DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09617QX 10130 YYC - LEFT WING UPPER SKIN TRAILING EDGE JUST INBOARD OF THE MULTI-FUNCTION SPOILERS HAS LOOSE FASTENERS. REPLACED RIVETS IAW CRJ-700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20051013002222005101300222EA 2005 10 13 QXEA200501303 120050917A5241 SKIN CNDAIRCL600 CL6002C10 1390015EA GALLEY DOOR NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09617QX 10130 YYC - FORWARD GALLEY SERVICE CART DOOR OUTER DOOR SKIN HAS NICKS ON THE AFT LOWER CORNER. REMOVED DAMAGE IAW CRJ-700 SRM 52-41-01-001-A01 PAGE 101 AND SRM 53-00-01-101-001-A01. RESTORED FINISH. 2L72 4F RTA21EA 20051013002242005101300224EA 2005 10 13 QXEA200501305 120050917A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA BS 975 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09617QX 10130 YYC - CENTER FUSELAGE LOWER SKIN DAMAGED AT FS 975 STR 27. BLENDED OUT CHAFING DAMAGE IAW REO 670-53-00-014. MATERIAL LOSS .026". RESTORED FINISH. 2L72 4F RTA21EA 20051014000022005101400002NM 2005 10 14 SWAA053124 120051011A53306545765 SKIN BOEING737 7373H4 1384600NM BS 500D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 12R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051014000042005101400004NM 2005 10 14 SWAA053126 120051011A57536546435 SKIN BOEING737 7373H4 1384600NM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED C1 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM. 2L72 4F RTA16WE 20051014000092005101400009NM 2005 10 14 SWAA053131 120051011A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM BS 438 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 438, STR 27L. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20051014000122005101400012 2005 10 14 SWAA053134 420051010A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29606SW 27926 DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051014000292005101400029NM 2005 10 14 SWAA053137 120051011A53156545805 FLOORBEAM BOEING737 7373H4 1384600NM BS 259 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 259, BETWEEN LBL 11 TO RBL 11. REPAIRED FLOORBEAM PER BFG ER. 2L72 4F RTA16WE 20051017000182005101700018WP 2005 10 17 DHL2005806539 120050828A5240 DOUBLER DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE SERVICE DOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH87034 46002 AFT SVC DOOR UPPER AFT CORNER INTERNAL DOUBLER CRACKED 1IN (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW AD2000-20-08, S/B 53-075, DWG NR SR08530021, 5750776. CUT OUT DAMAGED SECTION IAW DWG SR08530021. PERFORMED NDT INSP IAW NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER, TRIPLER AND FILLER IAW DOUGLAS DWG NR SR08530021, SRM 51-1-4 PG. 1. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG. 9. INSTALLED REPAIR PARTS IAW MFG DWG NR SR08530021, SRM 51-1-21, SRM 51-3-0, SRM 51-1-20D, SRM 51-1-20B, SRM 51-3-1. 2L74 4F4 FRT4A25 E2GL 20051017000192005101700019WP 2005 10 17 DHL2005806505 120050822A5754 SPLICE DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE LT WING SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH87034 46002 LT INNER WING OB EXTENDED L/E SLOT SPLICE CRACKED 10 IN STA XFS 207.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG. 1, SRM 57-3-3 FIG. 3 SHEET 1. REMOVED CRACKED SPLICE IAW SRM 57-1-0 PG. 1, SRM 51-1-21, SRM 51-1-20D. FABRICATED NEW SPLICE IAW SRM 57-3-3 FIG 3 SHEET 1 ITEM G, SRM 51-1-4 PG. 1. CLEANED, TREATED AND PRIMED AREA AND NEW SPLICE IAW SRM 51-1-8B. INSTALLED NEW SPLICE IAW SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1. 2L74 4F4 FRT4A25 E2GL 20051017000242005101700024EU 2005 10 17 05FDEA03398 120051012A5310 DOOR FRAME AIRBUS300 A300F4605R 3930327EU CARGO BAY GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25681FE 799 FWD CARGO DOOR FRAME 20A SKIN IS GOUGE AND SCRATCH LWR FWD CORNER OF CARGO DOOR. COMPLIED WITH EA 6-533092960 REF N00212. 2L72 4F RTA35EU 20051017000322005101700032NM 2005 10 17 05FDEA03413 120051012A5311 FRAME DOUG MD11 MD11 3023602NM ZONE 200 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 FORWARD CABIN - LEFT HAND STATION 535 FRAME LOCATED AT SUPPORT YOKE FOUND GOUGE, 2 PLACES. DAMAGED AREA AT FORWARD CABIN - LEFT HAND STATION 535 FRAME SUPPORT YOKE TRIM OUT AS PER DRAWING SRZ 53-503. REPAIR ANGLE, REPAIR STRAP, AND REPAIR FILLER FABRICATED AND INSTALLED AS PER DRAWING SRZ 53-503. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2- 100. 2L73 4F RTA22WE 20051017000352005101700035NM 2005 10 17 05FDEA03416 120051013A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 HORIZONTAL STAB LT BARREL NUT BORE NR 35 FOUND WITH CORROSION. REWORK/ REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 39. MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20051017000432005101700043NM 2005 10 17 SWAA053123 120051011A53116546546 SHEAR TIE BOEING737 7373H4 1384600NM BS 767 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 767, BETWEEN LBL 7 TO LBL 13. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051017000452005101700045WP 2005 10 17 AALA20050664 120051011A3350P4010049 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21452AA 49553 LGA - AFT EMERGENCY LIGHT ABOVE AFT GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR AFT EMERGENCY LIGHT ABOVE AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051017000532005101700053NE 2005 10 17 AALA20050654 220051005A7397 WIRE BOEING777 777223 1385213NM RROYCERB211 RB211TRENT89 NE ZONE 100 CHAFED A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21790AN 30251 51443 JFK - INFLIGHT RIGHT ENGINE FUEL FILTER LIGHT CAME ON TWICE DURING FLIGHT. REPLACED RIGHT ENGINE FUEL FILTER AND FUEL PRESSURE SWITCH. FOUND WIRE W08182001R20 CHAFED UNDER CONNECTOR D573001 BACK SHELL. ACCOMPLISHED INTERIM REPAIR TO WIRE PER MAINTENANCE MANUAL 20-10-13. RE-INSPECT AT EACH B-CHECK AND PERMANENT REPAIR AT NEXT MAIN BASE VISIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTT00001SEE00050EN 20051017000562005101700056NM 2005 10 17 AALA20050667 120051004A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21950AN 30087 TUL - EMERGENCY LIGHTS IN COACH INOPERATIVE. REPLACED BATTERY PACK AT STATION 967 FOR EMERGENCY LIGHTS IN COACH. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20051017000582005101700058NM 2005 10 17 SWAA053144 120051012A53306545767 SKIN BOEING737 7373H4 1384600NM BS 404 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 404, STR 17R. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20051017000602005101700060NM 2005 10 17 SWAA053146 120051012A53116520723 FRAME BOEING737 7373H4 1384600NM BS 500C CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, BETWEEN STR 19R TO STR 20R. REPAIRED FRAME PER SWA EA. 2L72 4F RTA16WE 20051017000732005101700073EA 2005 10 17 VTZA2005201 120051010A5311601R5211680 FRAME CNDAIRCL600 CL6002B19 1900309EA BS 320 CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27621BR 7186 PAX DOOR FRAME TOP RADIUS CRACKED AT 1 INCH IN LENGTH FORWARD OF DATUM 1 AT FS 320.90. 2L72 4F RTA21EA 20051017000752005101700075EA 2005 10 17 VTZA2005203 120051010A5315S6830 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 325-379 CORRODED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27621BR 7186 LBL 9 FLOORBEAM HAS CORROSION AT FS 325 TO 379. 2L72 4F RTA21EA 20051017000912005101700091NM 2005 10 17 SWAA052184 120050726A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 727A CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIPS CRACKED AT BS 727A, STR 25L & STR 25R. REMOVED AND REPLACED CLIPS PER SRM. 2L72 4F RTA16WE 20051017000962005101700096NM 2005 10 17 QXEA200501334 120051011A2121 WARNING LIGHT BOMBDRDHC8 DHC8402 1390042NM E/E BAY ILLUMINATED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09404QX 4046 AVIONICS CAUTION LIGHT CAME ON AFTER START. MAINTENANCE CYCLED POWER AFTER CDS SHOWED AVIONICS FAN MESSAGE. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051017000992005101700099NM 2005 10 17 SWAA053159 120051012A534065C27314 STRINGER CLIP BOEING737 7375H4 138449DNM BS 348 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29505SW 24182 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 348, STR 18L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051017001042005101700104NM 2005 10 17 ANCF200400055 120051009A3260 WARNING LIGHT BOEING757 757236 1384971NM RROYCERB211 RB211535E4 54555NE MLG DOOR ILLUMINATED W ANCFO OTHER J WARNING INDICATION CLCLIMB 1 SO23506NA 24771 EICAS MSG GEAR DOORS DISPLAYED WITH GEAR HANDLE UP. DOOR AMBER LGT ILLUM. GEAR AMBER LGT AND ALL GREEN DN LGTS EXTIN IAW FIM 32-30-00 PAG. 129. AIRCRAFT WAS RAISED ON JACKS TO PERFOM MLG OPERATIONAL TEST AMM 07-11-01 AMM 29-11-00 TEST SASTIFACTORY. 2L72 4F4 FRTA2NM E12EU 20051017001202005101700120CE 2005 10 17 DXTA200501020 120051012A3230 WARNING LIGHT CESSNA750 750 2076810CE MLG ILLUMINATED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07913QS 7500113 AFTER TAKEOFF, GREEN NOSE WHEEL DOWN INDICATOR LIGHT REMAINING ON. NO RED UNLOCK INDICATOR, AND NO AUDIBLE GEAR OR GEAR DOOR NOISE. GEAR EXTENDED NORMALLY, NORMAL LANDING. ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20051017001262005101700126SO 2005 10 17 CHQA200500174 120051006A335078241 STATIC INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11563RP 145509 LEFT OVERWING EMERGENCY EXIT MARKER LIGHT INOPERATIVE. REMOVED AND REPLACED NR 4 STATIC INVERTER IAW EMB 145 MM 33-50-11. OPS CHECK GOOD. 2L72 4T RTT00011AT 20051017001382005101700138NM 2005 10 17 05FDEA03392 120051011A5315 FLOORBEAM BOEING727 727100 1384036NM BS 360 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 CORROSION BS 360 FLOORBEAM BL 0. REJECTED BECAUSE CORROSION AND BARE METAL STILL PRESENT ON BOTTOM SIDE OF UPPER CHORD AND BL 0. REPAIRED PER SRM 53-10-8. 2L73 4F RTA3WE 20051017001472005101700147NM 2005 10 17 USAA051207 120051013A5320 INTERCOSTAL BOEING757 7572B7 1384964NM BS 310-324 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19627AU 27805 MAIN CABIN, BS 310-324, RBL 45 CORRODED. REPLACED CHANNEL INTERCOSTAL WITH NEW FABRICATED ASSY PER SRM 53-00-51, 51-40-02. DEFECT SIZE, 11 INCHES LONG X 5 INCHES WIDE X .025 INCH DEEP. 2L72 4F RTA2NM 20051017001502005101700150EU 2005 10 17 USAA051204 120051013A5315D5347209001000 FLOORBEAM AIRBUSA319 A319112 3930323EU FR 66 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19737US 1245 FLOORBEAM AT LAV MOUNT HOLE AT Y1292, FR 66. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 53-41-14, 51-72-11. DEFECT SIZE 1 INCH DIA AREA. 2L72 4F RTA28NM 20051017001572005101700157WP 2005 10 17 ABXA050246 120050927A5330591143267 SKIN DOUG DC9 DC941 302207NWP BS 1135 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23955AX 47619 FUSELAGE CRACKED AT STA 1135 LONGERON 4 LEFT. REPAIRED AREA IAW DC-9 SRM. 2L72 4F A6WE 20051017001892005101700189NM 2005 10 17 AALA20050634 120051001A3350 LIGHT BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21393AN 29430 DFW - EMERGENCY PATH LIGHT AT SEAT 28B INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 28B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20051017002032005101700203NM 2005 10 17 ASMF200510005 120051006A5754 STRUCTURE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE SLATS DAMAGED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23158PL 49761 CAPTAIN REPORTED THAT DURING SLATS EXTENSION, AIRPLANE TURNED TO LT 5 AND LT WING DOWN CONDITION, IT ENDS ONCE TAKEOFF LIGHT ILLUMINATED, AFTER SLATS EXTENSION PROCESS. AIRPLANE WAS SENT TO HANGAR AND SLATS / FLAPS SEQUENCE MECHANISM AND BUS CABLE CONDITION WERE CHECKED, TESTED CORRECT. IN NEXT FLIGHT CAPTAIN REPORTED SAME CONDITION, SO DURING OVERNIGHT CHECK EXCESSIVE WEAR WAS DETECTED IN SLAT ZERO OF RT WING. INTERCONNECTION PINS OF SLATS 0 AND 1 WERE REPLACED IAW MM 27-80-01. ADJUSTMENTS OF FLAP FIXED VANE BOTH SIDES, FLAP/SLAT SEQUENCE MECHANISM WERE VERIFIED. FLAPS CONTROL SYSTEM OF BOTH SIDES WAS TESTED IAW MM 27-51-03, 27-50-00 AND 27-81-02, ALL CORRECT. 2L72 4F4 FRTA6WE E9NE 20051017002182005101700218NM 2005 10 17 AWXA200500901 120050730A571265C26707 RIB BOEING737 737375 13844BNNM ZONE 500 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 PHX - DISCOVERED SERVERAL CRACKS ON THE LT LEADING EDGE BETWEEN STATION 208-219. REMOVED CRACKS ON LT LEADING EDGE IAW AMERICA WEST AIRLINES ENGINEERING REPAIR 03-5741-05214-RC2. FABRICATED FILLER IAW AWA ER 03-5741-05214-RC2. INSTALLED FABRICATED REPAIR PARTS IAW AWA ER 03-5751-05214-RC2. REPAIRS PERFORMED ON THE FIXED LEADING EDGE ARE NOT CONSIDERED MAJOR REPAIRS. SDR NOT REQUIRED. 2L72 4F RTA16WE 20051017002212005101700221SW 2005 10 17 ALGA106077 120050911A6220406310405101 PITCH LINK BELL 407 407 1182206SW ALLSN 250C 250C47B GL MAIN ROTOR BINDING B ALGAK NONE O OTHER ININSP/MAINT 1 SW03409AL692 53494 EXCESSIVE BINDING AND EXCESSIVE AXIAL PLAY. REPLACED WITH NEW BY FIELD MAINTENANCE. 1G71 3U3 UO H2SW E1GL 20051017002272005101700227NM 2005 10 17 SWAA053086 120051009A53306545775 SKIN BOEING737 7373H4 1384600NM BS 773 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 773, STR 14L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051017002312005101700231NM 2005 10 17 SWAA053090 120051009A5320BAC1509 FLOOR SUPPORT BOEING737 7373H4 1384600NM BS 859-867 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOOR SUPPORT CORRODED BETWEEN BS 859 TO BS 867, LBL 8.0. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20051017002342005101700234NM 2005 10 17 SWAA053102 120051007A53116546529 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR FWD FRAME, NR 5 STOP FITTING CUTOUT. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20051017002402005101700240NM 2005 10 17 05FDEA03319 120051009A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 LEFT HORIZ STAB BARREL NUT BORE NR 19 FOUND WITH CORROSION. REWORK/ REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 36. MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20051017002422005101700242NM 2005 10 17 05FDEA03321 120051009A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 RT HORIZ STAB BARREL NUT BORE NR 2 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 33. MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20051018000022005101800002NM 2005 10 18 C1HA200594005 120051017A534069191222 CHANNEL BOEING727 727290 138408WNM NLG ACTUATOR CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15294AS 22146 NLG LOCK ACTUATOR SUPPORT CHANNEL HAS CRACK INDICATION AT UPPER OUTBOARD HOLE. REMOVED & REPLACED NLG LOCK ACTUATOR SUPPORT CHANNEL IAW B727 SRM 51-30-2, P/N 69-19122-2. 2L73 4F A3WE 20051018000032005101800003NM 2005 10 18 C1HA200594004 120051017A5242 SKIN BOEING727 727290 138408WNM E/E BAY DOOR PUNCTURED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15294AS 22146 E&E BAY COMPARTMENT HATCH INTERIOR SKIN HAS SEVERAL GOUGES & A LARGE PUNCTURE HOLE. CUT OUT DAMAGED AREA, FABBED AND INSTALLED REPAIR FILLER & DOUBLER (7075 T6 .050 PO 9002126, DIM 5.375 X 5.125 INCHES IAW SRM 51-40-2 FIG 1. 2L73 4F A3WE 20051018000212005101800021CE 2005 10 18 DXTA200501025 120051015A2930 WARNING LIGHT CESSNA560 560XL 2076702CE HYD SYSTEM ILLUMINATED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07681QS 5605181 ON TAKEOFF WHEN GEAR WAS RETRACTED GEAR UNLOCK LIGHT & HYD PUMP ANNUNCIATOR LIGHT REMAINED ILLUMINATED. GEAR WAS CYCLED DOWN WITH LOCK INDICATION HYD PUMP EXTINGUISHED. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20051018000222005101800022CE 2005 10 18 DXTA200501029 120051016A2750 WARNING LIGHT CESSNA750 750 2076810CE TE FLAPS ILLUMINATED E DXTAA UNSCHED LANDING JF WARNING INDICATION FLT CONT AFFECTED DEDESCENT 1 GL07944QS 7500144 WHILE DESCENDING TO LAND, WITH NO FLAPS OR SLATS EXTENDED, RECEIVED AN AMBER FLAP FAIL MESSAGE ALONG WITH THE FLAPS INDICATING FLAPS 15 DEGREES WHEN UP. FOLLOWED EMERGENCY CHECKLIST. LANDED WITH SLATS EXTENDED ONLY. COULDN'T RETRACT AFTER LANDING. ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20051018000322005101800032NM 2005 10 18 QXEA200501352 120051013A5751 SHROUD DHAV DHC8 DHC8202 2809007NM AILERON DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09354PH 498 PDX - DENT IN LOWER AILERON SHROUD, RIGHT HAND WING. REPAIRED IAW HORIZON AIR EA 2-57-322A. 2H72 4T RTA13NM 20051018000352005101800035EA 2005 10 18 VTZA200500210 120051013A325116735109 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA NLG STEERING FAILED A VTZAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 EA27686BR6705 7715 NOSE WHEEL STEERING WENT LEFT THEN RIGHT ON TAKEOFF ROLL. REPLACED LEFT RVDT, CHECKED NOSE WHEEL STEERING RIGGING; HIGH SPEED TAXI TEST CHECK GOOD. 2L72 4F RTA21EA 20051018000462005101800046WP 2005 10 18 05FDEA03420 120051013A5315 FLOORBEAM DOUG DC10 DC1010 3022110WP BS 1256 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 MAIN CABIN INTERNAL FUSELAGE FOUND NR 1 CRACK LONG 2" ON FLOORBEAM AT STA Y= 1256 X= 107. REPAIRED WITH NEW SECTION OF FLOORBEAM AND SPLICE IAW SRM 53-00-01 FIG 9 VOL 1. 2L73 4F A22WE 20051018000472005101800047WP 2005 10 18 UPS05845615 120051014A5610 WINDSHIELD DOUG DC8 DC873F 302199FWP COCKPIT CRACKED A IPXAO OTHER O OTHER CRCRUISE 1 SO01851UP 46051 INSPECTION TYPE:N/A, F/O'S WINDSHIELD TOP EDGE GLOWING. WINDSHIELD CRACKED AT 17K FT. REMOVED AND REPLACED F/O WINDSHIELD W/REF TO MM 56-10-02-2. 2L74 4F RT4A25 20051018000622005101800062WP 2005 10 18 UPS05845603 120051003A5310 FINGER DOUBLER DOUG DC8 DC873F 302199FWP BS 880 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE:C2 STA 880 RBL 65 SUBFLOOR FINGER DOUBLER HAS HEAVY CORROSION. REMOVED FINGER DOUBLER AT STA 880 RBL 65 IAW SRM 51-1-21, AND 51-3-0, FABRICATED AND INSTALLED FINGER DOUBLER AT FS 880 RBL 65 IAW SRM 53-7-3 FIG4, 51-9-0 FIG 68A, AND SRM 51-1-21. 2L74 4F RT4A25 20051018000662005101800066NM 2005 10 18 SWAA053164 120051012A53306518420 SKIN BOEING737 7373H4 1384600NM BS 259 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29324SW 23414 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 259, BETWEEN STR 22L TO STR 25L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051018000682005101800068NM 2005 10 18 SWAA053166 120051012A55236959227 BUSHING BOEING737 7373H4 1384600NM ELEVATOR TAB WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29399WN 27693 DURING SCHEDULED C1 CHECK, LT & RT ELEVATOR TABS FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TABS NR 1 HINGE BUSHINGS & HARDWARE PER MM. 2L72 4F RTA16WE 20051018000732005101800073NM 2005 10 18 SWAA053171 120051013A53126546568 BULKHEAD BOEING737 7375H4 138449DNM BS 1016 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED 1/2D CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT STR 7R, 2 O'CLOCK POSITION. REPAIRED WEB PER SWA EA. 2L72 4F RTA16WE 20051018000822005101800082NM 2005 10 18 05FDEA03176 120050930A5220 FITTING BOEING727 727232 1384082NM DOOR HANDLE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 LEFT FWD EMERGENCY ESCAPE DOOR, ACCESS HANDLE CLOSURE FRAME CORRODED. REPLACED LT FWD EMERGENCY ESCAPE DOOR ACCESS HANDLE CLOSURE FITTING PER SRM 51-30-2. 2L73 4F A3WE 20051018000832005101800083NM 2005 10 18 05FDEA03177 120050930A5340 STRINGER CLIP BOEING727 727232 1384082NM BS 1110 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 STA 1110 STR 28R STRINGER CLIP CRACKED. REPLACED STRINGER CLIP AT B.S. 1110 STR 28R PER SRM 51-30-2. 2L73 4F A3WE 20051018000882005101800088NM 2005 10 18 05FDEA03185 120051001A5347 SEAT TRACK BOEING727 727225 1384077NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25462FE 22550 CORROSION ON SEAT TRACK FLANGE BETWEEN STA 560 AND 600 AT LBL 24. REMOVED AND REPLACED SEAT TRACK FROM STA 480 TO 630 AT LBL, 24 IAW FX B727 SRM 53-10-5 FIG 1, 51-10-2 AND 51-30-2. 2L73 4F A3WE 20051018001032005101800103WP 2005 10 18 AALA20050668 120051012A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21259AA 49289 LGA - AFT OVERWING EMERGENCY LIGHT EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 20DEF FOR AFT OVERWING EMERGENCY LIGHT EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051018001082005101800108NM 2005 10 18 AALA20050676 120051013A2150 A/C PACK BOEING757 7572Q8 1384972NM RIGHT SMOKE A AALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21704X 28163 MCO - INFLIGHT SHORTLY AFTER TAKEOFF HAD A STRONG OIL SMELL WITH VERY LITE SMOKE IN THE CABIN. SHUT OFF THE RIGHT PACK AND THE SMELL CLEARED. ACCOMPLISHED PACK BURN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20051018001102005101800110WP 2005 10 18 AALA20050672 120051010A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21490AA 49683 SFO - CEILING EMERGENCY LIGHTS AT ROWS 13 TO 15 INOPERATIVE. REPLACED BATTERY PACK AT ROW 13 FOR CEILING EMERGENCY LIGHTS FROM ROWS 13 TO 15. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051018001112005101800111NM 2005 10 18 AALA20050674 120051013A3397 CONNECTOR BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21633AA 24591 LGA - EMERGENCY LIGHT AT ROW 26 RIGHT SIDE INOPERATIVE. SECURED PLUG FOR EMERGENCY LIGHTS AT ROW 26 RIGHT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20051018001122005101800112NE 2005 10 18 AWXA200501221 220050912A7200 ENGINE BOEING757 7572S7 1384962NM RROYCERB211 RB211535E4 54555NE NR 2 MALFUNCTIONED A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28902AW 23322 SAN - ABORTED TAKEOFF - FLT 542 - CREW REPORTED THAT ON TAKEOFF THE NR 2 ENGINE EGT EXCEEDED AND ENGINE ROLLED DOWN PAST IDLE. AIRCRAFT TAXIED OFF RUNWAY AND CONTINUED BACK TO THE GATE WITHOUT FURTHER INCIDENT. AIRCRAFT IS STILL IN WORK. THE NR. 2 ENGINE WAS REMOVED AND REPLACED IAW AMERICA WEST AIRLINES TASK CARD R5M71601. OPERATIONAL CHECKS WERE GOOD. 2L72 4F4 FRTA2NM E12EU 20051018001132005101800113NM 2005 10 18 AWXA200501222 120051011A3234 HANDLE BOEING737 737375 13844BNNM MLG MALFUNCTIONED A AWXAA UNSCHED LANDING O OTHER CLCLIMB 1 WP28336AW 23707 AFTER T/O AND UPON RETRACTION OF GEAR, GEAR HANDLE WOULD NOT PHYSICALLY MOVE PAST CENTER FOR GEAR RETRACTION. A/C RETURNED TO STL AND LANDED W/O FURTHER INCIDENT. MX TROUBLESHOT AND REPLACED THE LOCKING SOLENOID IN THE GEAR HANDLE. ACFT THEN WENT ON MX FERRY TO RETURN TO PHX FOR EXPIRED 4 DAY. PROBLEM REPEATED AND A/C TURNED BACK TO STL AGAIN. LANDED W/O FURTHER INCIDENT. A/C IS STILL OUT OF SERVICE. ONLY OTHER HISTORY ON GEAR RETRACTION SYSTEM WAS ON 29AUG FOR ALL THREE RED AND GREEN GEAR LIGHTS RECEIVED UPON EXTENSION ALONG WITH AURAL "TOO LOW GEAR". MX CLEANED SENSOR'S ON THAT PARTICULAR INCIDENT. 2L72 4F RTA16WE 20051018001152005101800115SO 2005 10 18 2005F00103 120050914A3246C20211170 WHEEL LKHEEDP38 P38L 5260206SO ALLSN V1710 V1710* GL TIE BOLTS LOOSE B K NONE O OTHER ININSP/MAINT 1 WP01718 2602 82 8187 WHEEL ASSEMBLY RETURNED FOR LOOSE TIE BOLTS, OF 18 TIE BOLTS INSTALLED 2 ARE MISSING 11 ARE LOOSE. MFG HAS NOW ISSUED SERVICE LETTER F6137-32-843 IN HOPES THIS WILL RESOLVE. 2M72 4V4 V LTC10 EXPE4V 20051018001192005101800119WP 2005 10 18 05FDEA03189 120051002A3243 CABLE DOUG DC10 DC1010 3022110WP BRAKE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25389FE 46623 BRAKE CABLE NR 143 RUSTY AT PULLEY BEND UNDER MAIN CARGO COMPT FLOOR STA 1445 RBL37. REMOVED REPLACED AND ADJUSTED LT BRAKE CONTROL SYSTEM. OPS CHECK GOOD. 2L73 4F A22WE 20051018001202005101800120NM 2005 10 18 QXEA200501329 120051007A33506104781 BATTERY PACK DHAV DHC8 DHC8202 2809007NM EMERGENCY LIGHT MALFUNCTIONED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09349PH* 41 486 PDX - EMERGENCY LIGHT INOP AT CABIN AFT OVERHEAD AND OUTSIDE RIGHT AFT, AND CABIN CENTER EMERGENCY OVERHEAD. MAINTENANCE REPLACED NR 4 EMERGENCY BATTERY PACK AND PERFORMED OPERATIONAL TEST OF THE EMERGENCY LIGHTS SYSTEM, IAW DASH 9 AMM 33-51-01-710-801, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051018001212005101800121 2005 10 18 SB05127 420051007A3441HG1050AE09 IRU BOEING737 737401 1384701NM COCKPIT MISALIGNED A USAAC ABORTED TAKEOFF GJ MULTIPLE FAILURE WARNING INDICATION TOTAKEOFF 1 EA19406US 23876 DURING TAKEOFF ROLL, CREW RECEIVED A DUAL IRS FAILURE WITH ALL RED FLAGS APPEARING. BOTH THE CAPTAIN'S AND FIRST OFFICER'S SCRATCH PAD SHOWED "IRS NAV MOTION FAULT". CREW DECLARED AN EMERGENCY, CIRCLED THE FIELD AND THEN RETURNED TO THE FIELD AT MHT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REALIGNED AND TESTED BOTH IRU'S PER MM 34-28-31. AIRCRAFT OK FOR SERVICE. 2L72 4F RTA16WE 20051018001232005101800123NM 2005 10 18 05FDEA03200 120051004A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 HORIZ STAB RT BARREL NUT BORE NR 16 FOUND WITH CORROSION. REWORK/ REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 28. MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20051018001262005101800126NM 2005 10 18 05FDEA03203 120051004A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 HORIZ STAB LT BARREL NUT BORE NR 7 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 27. MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20051018001272005101800127NM 2005 10 18 05FDEA03204 120051004A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 HORIZ STAB LT BARREL NUT BORE NR 3 FOUND WITH CORROSION. REWORK/ REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 26. MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20051018001292005101800129 2005 10 18 SWAA053175 420051012A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29605SW 27956 DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051018001302005101800130NM 2005 10 18 SWAA053176 120051013A53116546581 FRAME BOEING737 7373H4 1384600NM BS 992 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 992, RBL 55, WL 209. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051018001312005101800131NM 2005 10 18 SWAA053177 120051013A53116517684 FRAME BOEING737 7373H4 1384600NM BS 303 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303, STR 16L. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20051018001322005101800132NM 2005 10 18 SWAA053178 120051013A53116546526 FRAME BOEING737 7373H4 1384600NM BS 400 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051018001332005101800133NM 2005 10 18 SWAA053179 120051013A213340631997201AB OUTFLOW VALVE BOEING737 7373H4 1384600NM CABIN PRESSURE FAULTY A SWAAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 SW29639SW 27712 DIVERSION/DECLARED EMERGENCY CABIN ALTITUDE WARNING HORN SOUNDED. ALTERNATE & MANUAL POSITIONS INOP. REMOVED AND REPLACED AFT OUTFLOW VALVE PER MM. 2L72 4F RTA16WE 20051018001342005101800134WP 2005 10 18 05FDEA03190 120051002A3243 CABLE DOUG DC10 DC1010 3022110WP BRAKE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25389FE 46623 BRAKE CABLE NR 147 RUSTY AT PULLEY BEND BELOW MAIN CARGO COMPT FLOOR STA 1450 RBL37. REMOVED REPLACED ADJUSTED LT BRAKE CONTROL SYSTEM IAW DC10 M/M 32-44-00-2. OPS CHECK GOOD IAW DC10 M/M 32-44-00-2 . 2L73 4F A22WE 20051018001352005101800135WP 2005 10 18 05FDEA03191 120051002A3243 CABLE DOUG DC10 DC1010 3022110WP BRAKE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25389FE 46623 BRAKE CABLE NR 143 RUSTY AT PULLEY BEND UNDER MAIN CARGO COMPT FLOOR STA 1445 N RBL 37. REMOVED, REPLACED AND ADJUSTED LT BRAKE CONTROL SYSTEM IAW DC10 M/M 32-44-00-2 . OPS CHECK GOOD IAW DC10 M/M 32-44-00-2 . 2L73 4F A22WE 20051018001392005101800139NM 2005 10 18 05FDEA03197 120051004A5310 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 HORIZ STAB RT BARREL NUT BORE NR 14 FOUND WITH CORROSION. REMOVED AND NEW FITTING INSTALLED IAW SRM 51-32-01 VOL.II, SRM 51-38-01 VOL.II, SRM 51-33-01 VOL.II AND E1-5510-7-5000 D1 PT1. MINOR REPAIR I.A.W FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20051018001402005101800140NM 2005 10 18 05FDEA03198 120051004A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 HORIZ STAB RT BARREL NUT BORE NR 24 FOUND WITH CORROSION. REWORK/ REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 30. MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20051018001412005101800141EU 2005 10 18 AWXA200501183 120051007A335030320228VCC RELAY AIRBUS320 A320232 3930326EU EMERGENCY LIGHTSINTERMITTENT A AWXAK NONE O OTHER ININSP/MAINT 1 WP28661AW 1284 PHX - EEL - ON GROUND CREW REPORTED THAT THE AIRCRAFT OVERWING LEFT AND CEILING EMERGENCY EXITS LIGHTS FLICKER. MAINTENANCE REMOVED AND REPLACED RELAY 8WL IAW AIRBUS TSM 33-51-00-810-819. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA28NM 20051018001422005101800142NM 2005 10 18 AWXA200501184 120051008A2560P4010021000 BATTERY AIRBUSA319 A319132 3930340NM FLASHLIGHT INOPERATIVE A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28827AW 1547 PHX - EEL - ON THE GROUND REPORTED THAT THE AFT FLIGHT ATTENDANT RT EMERGENCY FLASHLIGHT DOES NOT BLINK. MAINTENANCE REMOVED AND REPLACED THE RT FLIGHT ATTENDANT EMERGENCY FLASHLIGHT BATTERY. OPERATIONAL CHECKS GOOD. 2L72 4F RTA28NM 20051018001432005101800143EU 2005 10 18 AWXA200501185 120051009A3350321430 BATTERY AIRBUS320 A320232 3930326EU EMERGENCY LIGHTSFAILED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28648AW 770 PHX - EEL - DURING OVERNIGHT INSPECTION, FOUND THAT THE EMERGENCY PATH LIGHTS FAILED THE CIDS TEST FAULTING "COM AFT L". MAINTENANCE REMOVED AND REPLACED THE EPSU POWER SUPPLY IN THE AFT GALLEY. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA28NM 20051018001452005101800145NM 2005 10 18 AWXA200501187 120051009A2560P4010021 BATTERY BOEING737 7373G7 1384595NM FLASHLIGHT INOPERATIVE A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28305AW 24012 PHX - EEL - ON GROUND CREW REPORTED FLIGHT ATTENDANTS EMERGENCY FLASHLIGHT STOPPED BLINKING. MAINTENANCE REMOVED AND REPLACED THE FLASHLIGHT BATTERY IN THE FORWARD EMERGENCY FLASHLIGHT. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20051018001462005101800146NM 2005 10 18 AWXA200501188 120051007A53306545776 SKIN BOEING737 7373B7 1384580NM BS 727D-996 CRACKED A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28332AW 23384 PHX - FLT 289 - ON GROUND IN PHX, REPORTED POSSIBLE TAIL STRIKE. MAINTENANCE DISCOVERED FUSELAGE CRACK 1 INCH LONG AT STATION 727D STRINGER S-23L AND AFT GALLEY DRAIN MAST DAMAGED. MAINTENANCE REMOVED DAMAGED AREA AT BS 727D AND BS 996 IAW BOEING 737-300 SRM 53-00-01 AND AMERICA WEST AIRLINES ENGINEERING REQUEST 03-5361-05280-HF1. FABRICATED DOUBLERS, TRIPLERS, FILLERS, BRACKET CLIPS FOR DRAIN MAST AND TEAR STRAPS FOR CRACKED SKIN IAW AWA ER 03-5361-05280-HF1. INSTALLED FABRICATED REPAIR PARTS AT BS 727D, STR 23L AND BS 996 IAW BOEING 737-300 SRM 53-00-01 AND AWA ER 03-5361-05280-HF1. 2L72 4F RTA16WE 20051018001482005101800148NM 2005 10 18 AWXA200501190 120050917A532065479573 WEB BOEING737 73733A 1384673NM BS 800-845 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW 23634 GYR - DURING C20 CHECK DISCOVERED GALVANIC CORROSION LOCATED ON THE AFT BAG PIT THRESHOLD FROM BS 800 TO BS 845, WL 154, STR 25R, AND FROM BL 16R TO BL 18R. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-53. MAINTENANCE REMOVED AFT CARGO THRESHOLD WEB IAW BOEING 737-300 SRM 51-40-02. RECEIVED NEW WEB AND INSTALLED WEB FROM BS 800 TO BS 845, WL 154, STR 25R, AND FROM BL 16R TO BL 18R IAW BOEING 737-300 SRM 51-40-05 AND 51-40-08. 2L72 4F RTA16WE 20051018001492005101800149NM 2005 10 18 AWXA200501191 120050923A534069468314 STRINGER CLIP BOEING737 7373S3 1384711NM BS 360 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 MCN - DURING C18 CHECK DISCOVERED STRINGER TIE CLIP CRACKED .375 INCHES IN LENGTH LOCATED AT BS 360 AND STR 4L. MAINTENANCE REMOVED STRINGER TIE CLIP AND FABRICATED NEW CLIP IAW BOEING 737-300 SRM 51-40-05-0G FIG 3 AND FIG 7. INSTALLED FABRICATED REPAIR PARTS AT BS 360 AND STR 4L IAW BOEING 737-300 SRM 51-40-02-0G FIG 3 AND 12. 2L72 4F RTA16WE 20051018001502005101800150NM 2005 10 18 AWXA200501192 120050923A534069353502 STRINGER CLIP BOEING737 7373S3 1384711NM BS 500A CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 MCN - DURING C18 CHECK DISCOVERED STRINGER TIE CLIP CRACKED .4 INCHES IN LENGTH LOCATED AT BS 500A AND STR 16R. MAINTENANCE REMOVED STRINGER TIE CLIP AND FABRICATED NEW CLIP IAW BOEING 737-300 SRM 51-40-05-0G FIG 3 AND FIG 7. INSTALLED FABRICATED REPAIR PARTS AT BS 500A AND STR 16R IAW BOEING 737-300 SRM 51-40-02-0G FIG 3 AND 12. 2L72 4F RTA16WE 20051018001512005101800151NM 2005 10 18 AWXA200501193 120050921A57536546486130 WEDGE BOEING737 7373S3 1384711NM ZONE 600 DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 MCN - DURING C18 CHECK DISCOVERED DISBOND AREA AT THE OUTBOARD END OF THE RT INBOARD MID FLAP TRAILING EDGE WEDGE, LOWER SURFACE FROM WS 176.5 TO WS 183.0. MAINTENANCE REMOVED DISBONDED SKIN AND PREPPED REPAIR AREA IAW BOEING 737-300 SRM 51-70-10-2R4 FIG 202. FABRICATED DOUBLER AND FILLER IAW BOEING 737-300 SRM 51-70-10-2R4. BONDED REPAIR PARTS TO THE OUTBOARD END OF THE RT INBOARD MID FLAP TRAILING EDGE WEDGE, LOWER SURFACE FROM WS 176.5 TO WS 183.0 IAW BOEING 737-300 SRM 51-70-10-2R4 FIG 202. 2L72 4F RTA16WE 20051018001522005101800152NM 2005 10 18 AWXA200501194 120050921A57536546435277 SKIN BOEING737 7373S3 1384711NM TE FLAP DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 MCN - DURING C18 CHECK DISCOVERED DISBOND AREA ON THE LOWER SURFACE OF THE LT OUTBOARD AFT FLAP, 25" FROM INBOARD END FROM WS 254.68 TO WS 256.68. MAINTENANCE REMOVED DISBONDED SKIN AND PREPPED REPAIR AREA IAW BOEING 737-300 SRM 51-70-10-2R4 FIG 202. FABRICATED DOUBLER AND FILLER IAW BOEING 737-300 SRM 51-70-10-2R4. BONDED REPAIR PARTS TO THE LOWER SURFACE OF THE LT OUTBOARD AFT FLAP, 25" FROM INBOARD END FROM WS 254.68 TO WS 256.68 IAW BOEING 737-300 SRM 51-70-10-2R4 FIG 202. 2L72 4F RTA16WE 20051018001532005101800153NM 2005 10 18 USAA051186 120051005A5340 STRINGER CLIP BOEING737 7374B7 1384702NM BS 907 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19443US 24842 FOUND STRINGER CLIP CRACKED, STA 907 AND STR 4R. REMOVED DAMAGED CLIP, REPLACED WITH FABRICATED PART IAW SRM 53-00-03, DEFECT SIZE: 1". 2L72 4F RTA16WE 20051018001552005101800155NM 2005 10 18 USAA051184 120051005A5311 FRAME BOEING737 7374B7 1384702NM BS 847 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19443US 24842 FOUND FRAME BOX CORRODED AT STA 847 AND STR 25. REMOVED, FABRICATED AND INSTALLED NEW BOX PANEL IAW SRM 53-60-15, DEFECT SIZE: 3" BY 5". 2L72 4F RTA16WE 20051018001572005101800157NM 2005 10 18 USAA051194 120051006A5310 DOOR FRAME BOEING737 7374B7 1384702NM FWD SERVICE DOORCRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19443US 24842 FOUND FWD SERVICE DOOR FWD CUTOUT FRAME CRACKED. REMOVED OLD DOOR WEB FRAME UPPER FRAME WEB AND NEW ANGLE AND SHIMS IAW SRM 51-10-02, DEFECT SIZE: 1/2" CRACK. 2L72 4F RTA16WE 20051018001582005101800158NM 2005 10 18 USAA051193 120051006A5311 FRAME BOEING737 7374B7 1384702NM BS 380 DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19443US 24842 LEFT HAND SIDE AT STA 380, STR 5 DEFECT. FABRICATED FRAME REPAIR DOUBLER & INSTALLED IAW REPAIR DOCUMENT TYP. REPAIR 53-10-14 DEFECT SIZE: 1 X 1 INCH RUB AREA AT STA 380 STR 5 LT SIDE. 2L72 4F RTA16WE 20051018001612005101800161NM 2005 10 18 USAA051190 120051006A5314 KEELBEAM BOEING737 7374B7 1384702NM BS 500G CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19443US 24842 FOUND CRACKED RT KEEL BEAM AT AFT SIDE OF STA 500G. FAB`D ANGLE AND INSTALLED. REMOVED AND REPLACED DAMAGED CLIP IAW SRM 51-10-02 AND BOEING DWG 69-73527, DEFECT SIZE: 1" CRACK. 2L72 4F RTA16WE 20051018001622005101800162NM 2005 10 18 USAA051189 120051006A575465C26602257A SKIN BOEING737 7374B7 1384702NM NR 2 SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19443US 24842 NR 2 SLAT T/E WEDGE INBOARD END DELAMINATED. REMOVED DAMAGE, INSTALLED REPAIR PIECES IAW SRM 51-70-10, DEFECT SIZE: 3" BY 5" DELAMINATION. 2L72 4F RTA16WE 20051018001642005101800164NM 2005 10 18 USAA051187 120051006A575365C263101 WEDGE BOEING737 7374B7 1384702NM TE FLAP WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19443US 24842 FOUND LEFT HAND INBOARD MID FLAP INBOARD END WORN. REMOVED DAMAGED FLAP WEDGE AND REINSTALLED NEW WEDGE IAW BOEING DWG 65-46486U155, FLAP WEDGE WORN DUE TO CONTACT WITH THE CONTROL ROD. DAMAGE MEASURES .5" BY 2.75". 2L72 4F RTA16WE 20051018001652005101800165EU 2005 10 18 SA05106 120051008A2432350L5100508 CHARGER AIRBUSA319 A319112 3930323EU AVIONICS BAY FAILED A USAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA19737US15967 1245 LGA - FLT 802 - EN-ROUTE PIT TO LGA - DURING THE FLIGHT, NR 1 BATTERY VOLTS OCCASIONALLY DROP TO 25V. THE CHARGE WOULD GO UP TO 5A, THEN RETURN TO 28 VOLTS AND 0 AMPS. A LIGHT ELECTRICAL ODOR WAS PRESENT, BUT NO SMOKE WAS EVIDENT. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 BATTERY CHARGE LIMITER. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20051018001662005101800166EU 2005 10 18 SA05107 120051008A4990 CONTROL VALVE AIRBUSA319 A319112 3930323EU APU CONTAMINATED A USAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA19746UW 1297 AFTER TAKEOFF, THERE WAS A STRONG ODOR THROUGHOUT THE AIRCRAFT. THE ODOR DISSIPATED AFTER REACHING 15,000 FT. ON DESCENT, THE ODOR RETURNED AROUND 12,000 FT AND GOT STRONGER UNTIL THE AIRCRAFT LANDED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND OIL IN THE APU LOAD CONTROL VALVE. PLACED THE APU PNEUMATICS ON MEL. REPLACED THE RIGHT AND LEFT RECIRCULATION FILTERS AND THE RIGHT OZONE FILTER. FOUND THE APU PNEUMATICS SYSTEM INGESTING OIL FROM AN APU STARTER LEAK. REPLACED THE APU STARTER ASSEMBLY. REPLACED THE RIGHT SIDE PRIMARY AND SECONDARY HEAT EXCHANGERS DUE TO OIL CONTAMINATION. RAN THE ENGINES AND AIR CONDITIONING PACKS. OPERATIONALLY CHECKS OK. REMOVED THE APU PNEUMATICS MEL. 2L72 4F RTA28NM 20051018001702005101800170EU 2005 10 18 KBM2005F00288 120050919A2121050031 BRUSHES SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1D NE CONDENSER BLOWERINOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19215LA 2143 LT CONDENSER BLOWER INOPERATIVE, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051018001722005101800172NM 2005 10 18 QXEA200501353 120051014A2750 WARNING LIGHT BOMBDRDHC8 DHC8402 1390042NM TE FLAPS ILLUMINATED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09417QX 4086 SEA - FLIGHT 2390 FLAP POWER CAUTION LIGHT ILLUMINATED. MAINTENANCE COMPLIED WITH FIM TASK 27-50-00-810-802. RESET CONTINUOUS BIT FAULT, CYCLED FLAP C/B. COMPLIED WITH Q400 AMM TASK 27-50-00-710-801. OPERATIONAL TEST OF WING FLAPS. NO FURTHER FAULTS OR CAUTIONS OCCURRED. OPS CHECK GOOD. NO PARTS REPLACED. AIRCRAFT OK FOR CONTINUED SERVICE. 2H72 4T RTA13NM 20051018001732005101800173SO 2005 10 18 CHQA200500179 120051017A335078241 INVERTER EMB 145 EMB145 3260210SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11263SK 145199 DURING A-CHECK, FOUND AFT OVERWING EXIT LOCATOR SIGN INOP. REMOVED AND REPLACED NR 4 EMERGENCY LIGHT POWER INVERTER IAW EMB 145 AMM 33-50-11. OPS CHECK GOOD. 2L72 4F RTT00011AT 20051018001742005101800174SO 2005 10 18 CHQA200500177 120051015A3350 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSLOOSE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11281SK 145391 DARNING INSPECTION, OVERHEAD AND OVERWING EMERGENCY LIGHTS ARE INOP. RECONNECTED LOOSE FORWARD LOCATOR LIGHT WIRING CONNECTOR IAW EMB 145 AMM 33-50-07. OPS CHECK GOOD AT THIS TIME 2L72 4T RTT00011AT 20051018001752005101800175SO 2005 10 18 CHQA200500178 120051016A335078241 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11284SK 145427 EMERGENCY EXIT LOCATOR ON AFT GALLEY WALL IS INOP. REMOVED AND REPLACED EMERGENCY LIGHT INVERTER IAW EMB145 AMM 30-50-11. OPS CHECK GOOD. 2L72 4T RTT00011AT 20051018001802005101800180 2005 10 18 KBM2005F00283 420050922A3422103002301 GYRO SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE DIRECTIONAL INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P456 2347 DIRECTIONAL GYRO INOPERATIVE, REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20051018001812005101800181 2005 10 18 SWAA053104 420051009A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29739GB 29275 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051018001872005101800187WP 2005 10 18 UPS05845548 120050907A5310 DOOR FRAME DOUG DC8 DC873F 302199FWP BS 520-560 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE:C3 "B" PIT DOOR TORQUE JAMB FROM FS 520-560 HAS CORROSION AROUND NUT PLATES. REMOVED CORROSION AROUND NUT PLATES AND FOUND IN LIMITS. FOUND CORROSION ON FRAME AT FS 540 L36. CORROSION FOUND OUT OF LIMITS, CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DWG DC8-53A-011. 2L74 4F RT4A25 20051018001882005101800188WP 2005 10 18 UPS05845549 120050909A534010824101 FITTING DOUG DC8 DC873F 302199FWP BS 880 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 LEFT FWD LOWER TRAP FITTING IS CRACKED. REMOVED AND REPLACED TRAP FITTING IAW DC-8 SRM 51-3-0 AND 51-2-20D. 2L74 4F RT4A25 20051018001892005101800189WP 2005 10 18 UPS05845550 120050909A5340 TEE FITTING DOUG DC8 DC873F 302199FWP BS 860 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 C3 TEE CHORD CRACKED STA 860 RBL 40 UPPER AFT END OF CENTER TANK LOOKING FROM INSIDE MAIN CABIN. AFTER FURTHER EVALUATION CRACK FOUND TO BE CAUSED BY INTERGRANULAR CORROSION, CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 53-2-5 FIG 12 AND DWG 5644011. 2L74 4F RT4A25 20051018001922005101800192NM 2005 10 18 05FDEA03353 120051011A5754 SKIN DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 LEFT WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT XORS 635. REPAIR CARRIED OUT AS PER SRM 57-10-00. 2L73 4F RTA22WE 20051109002802005110900280NM 2005 11 9 05FDEA03355 120051011A5730ARB39548 DOUBLER DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 SNRM N0605 : RIGHT HAND WING FIXED LEADING EDGE INTERNAL RIB DOUBLER FOUND CRACKED AT XORS 680. CORRECTIVE ACTION: SNRM N0605 : CRACKED INTERNAL RIB DOUBLER AT RIGHT HAND WING FIXED LEADING EDGE XORS 680 REMOVED AS PER SRM 51-31-01 VOLUME II. NEW RIB DOUBLER FABRICATED AS PER DRAWING ARB3954 AND INSTALLED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR AS PER GMM6-2-100. 2L73 4F RTA22WE 20051018001942005101800194NM 2005 10 18 05FDEA03356 120051011A5754 SKIN DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 RIGHT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT XORS 590. TRIMMED OUT AS PER FEDEX EA 1-5710-89998. REPAIR DOUBLER AND ANGLE FABRICATED AND INSTALLED AS PER FEDEX EA 1-5710-89998. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051018001952005101800195WP 2005 10 18 05FDEA03357 120051011A5330 SKIN DOUG DC10 DC1010 3022110WP BS 447 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LOWER FUSELAGE NOSE LT SIDE FOUND NR 1 DENT (1.5" X 0.080") ON SKIN AT STA Y= 447. INSTALLED TITANIUM FINGER DOUBLER IAW SRM 53-20-00 FIG 13 SHEET 5 VOL 1. 2L73 4F A22WE 20051018001962005101800196NM 2005 10 18 05FDEA03358 120051011A5754 SKIN DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 RIGHT WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT XORS 536. FASTENERS AT CRACKED INTERNAL BEADED DOUBLER AT RIGHT HAND WING FIXED LEADING EDGE XORS 536 REMOVED AS PER SRM 51-31-01 VOLUME II. REPAIR DOUBLER FABRICATED AS PER SRM 57-10-00 FIGURE 25 VOLUME I AND INSTALLED AS PER SRM 51-35-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051018001992005101800199WP 2005 10 18 05FDEA03361 120051011A5330 SKIN DOUG DC10 DC1010 3022110WP BS 735-755 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LOWER FUSELAGE NOSE LT SIDE FOUND NR 1 DENT (1.18" BY 0.067") ON SKIN AT BETWEEN STA Y=735 AND STA Y= 755 CLOSE OUT LONGERON 38. INSTALLED TITANIUM FINGER DOUBLER IAW SRM 53-20-00 FIG 13 SHEET 7 VOL 1. 2L73 4F A22WE 20051018002002005101800200NM 2005 10 18 05FDEA03362 120051011A5754 SKIN DOUG MD11 MD11 3023602NM NR 8 SLAT CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 LT WING NR 8 SLAT INNER SURFACE FOUND CRACKED AT SLAT TRACK NR 18 AREA. CARRIED OUT REPAIRED AS PER SRM 57-10-00 FIG 10, VOL I. REPAIR CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20051018002012005101800201NM 2005 10 18 05FDEA03363 120051011A5712ARB77747 RIB DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 LT WING LOWER WINGLET RIB FOUND CRACKED AT LEADING EDGE AREA. REMOVED AS PER SRM 51-31-01 VOLUME II. NEW RIB FABRICATED AS PER DRAWING ARB7774 AND INSTALLED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051018002042005101800204NM 2005 10 18 SWAA053106 120051006A5540 SKIN BOEING737 7377H4 1384404NM RUDDER CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29771SA 27879 DURING SCHEDULED HC1 CHECK, FOUND RUDDER L/E CRACKED AT BOTTOM RT SIDE. REPAIRED RUDDER PER SRM. 2L72 4F RTA16WE 20051018002052005101800205NM 2005 10 18 SWAA053107 120051006A3350MS155721 BULB BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29771SA 27879 DURING SCHEDULED HC1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20051018002062005101800206NM 2005 10 18 SWAA053108 120051008A2560PH22300L GLOWSTRIP BOEING737 7377H4 1384404NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29781WN 30601 PHOTOLUMINESCENT FLOOR TRACK COVER MISSING. REMOVED AND REPLACED PHOTLUMINESCENT FLOOR TRACK SECTION PER MM. 2L72 4F RTA16WE 20051018002072005101800207NM 2005 10 18 SWAA053109 120051008A5315BAC1509 FLOORBEAM BOEING737 7377H4 1384404NM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29788SA 30603 DURING SCHEDULED 5Y CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 775, LBL 3. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20051018002132005101800213NM 2005 10 18 SWAA053097 120051007A335007912 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29433LV 33716 EEPLS TRACK LENS COVER LOOSE. SECURED COVER PER MM. 2L72 4F RTA16WE 20051018002142005101800214NM 2005 10 18 SWAA053098 120051007A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29444WN 29839 EEPLS TRACK COVER MISSING AT ROW 1. INSTALLED COVER PER MM. 2L72 4F RTA16WE 20051018002152005101800215CE 2005 10 18 DXTA200501013 120051009A3260 WARNING LIGHT CESSNA560 560XL 2076702CE MLG MALFUNCTIONED E DXTAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL07601QS 5605301 AFTER GEAR RETRACTION NOSE WHEEL INDICATOR LITE REMAINED ON. ALL INDICATIONS WERE THAT NOSE GEAR WAS RETRACTED. NORMAL EXTENTION FOLLOWED BY PRECAUTIONARY BLOW DOWN. - COULD NOT DUPLICATE DISCREPANCY. CYCLED GEAR 20 TIMES PERFORMED TIME CYCLE TEST. NOTE: LANDING GEAR BREAKS LOOSE LAST DURING RETRACTION CYCLE. ALL INDUCTIONS ARE NORMAL PER CE 560 XL M/M CHAPTER 32-01-00. 2L72 4F RTA22CE 20051018002162005101800216CE 2005 10 18 DXTA200501014 120051010A3260 INDICATOR BEECH MU300 400A 1155402CE MLG INOPERATIVE E DXTAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL07102QS RK380 LEFT GREEN LANDING GEAR DOWN INDICATOR LIGHT WOULD NOT ILLUMINATE WITH GEAR SELECTED . CYCLED GEAR 2 TIMES NO CHANGE, DID EMERGENCY GEAR RETRACTION (PNEUMATIC) AND LEFT LIGHT STILL DIDN'T ILLUMINATE . TURNED ON ALL INDICATOR LIGHTS AND LEFT GEAR WOULD NOT ILLUMINATE. - REPLACED LANDING GEAR INDICATOR LIGHT ASSEMBLY IAW HAWKER 400XP M/M, CHAPTER 32-60-00, OPS CHECK GOOD. POWERED LDG. GEAR HDYRAULIC SYSTEM AND SERVICED HYDRAULIC RESERVIOR I.A.W. 400XP M/M CHAPTER 32-30-00, OPS CHECK GOOD. 2H72 4F RTA16SW 20051018002172005101800217CE 2005 10 18 DXTA200501017 120051011A3241991228113 FILTER CESSNA500 560CESSNA 2076750CE ANTI-SKID SYS FAILED E DXTAD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07377QS 5600377 ON TAXI OUT A/C WAS UNRESPONSIVE ON BRAKE CHECK CAPT. SIDE: FULL PRESSURE WITH NO BRAKING AVALIBLE. F/O SIDE: PEDALS COMPLETLY FLOORED WITH NO PRESSURE. - REMOVED & REPLACED ANTI-SKID CONTROL FILTER & BLEED BRAKE SYSTEM IAW CE 560 MLM 32-42-00. COMPLIED WITH TAXI CHECK OF BRAKE OPERATIONAL TEST. OPERATIONAL CHECK GOOD. 2L72 4F RTA22CE 20051018002182005101800218NM 2005 10 18 DXTA200501015 120051010A3260803682 POSITION SWITCH AMD FALC50FALCON2000 2730170NM MLG INOPERATIVE E DXTAO OTHER N FALSE WARNING APAPPROACH 1 GL07224QS 124 ON FINAL APPROACH AT 170K THE GEAR HANDLE WAS PUT DOWN, BUT JUST THE 3 RED LTS CAME ON AFTER 20 SEC THE GEAR HANDLE STARTED TO FLASH. THE GEAR WAS EXTENDED USING THE EMER GEAR PULL HANDLE. 3 GREEN CAME ON. - REMOVED L/H MLG DOOR PROX SWITCH, P/N 803682, S/N 0790. NEW PROX SWITCH P/N 803682, S/N 1256. REMOVED RT MLG DOOR PROX SWITCH, P/N 803682, 0956, & INSTALLED NEW SWITCH, P/N 803682, S/N 1225. PERFORMED FUNCTIONAL EXTENSION / RETRACTION TEST OF LANDING GEARS + DOORS, FUCTIONAL CHECK GOOD WITH NO DEFECTS NOTED. DONE IAW F-200 MM CHAP 07-100, 52-300 & 32-311. DETAILS REF FAS05-102. 2K73 4F RTA50NM 20051018002192005101800219CE 2005 10 18 DXTA200501018 120051011A31104026206974 CONTROL PANEL CESSNA650 650 2076802CE COCKPIT HOT E DXTAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL07787QS 6507087 BURNT WIRING SMELL WAS NOTICED AFTER ENGINE SHUTDOWN. HEADING AD SELECTION CONTROL PANEL WAS EXTREMELY HOT SO COMPLETE SHUTDOWN WAS INITIATED. - TROUBLESHOT TO BAD REMOTE INSTRUMENT CONTROLLER, REPLACED BAD R.I.C. IAJ CE 650MM CH 34-21-00 + OPS CHECK GOOD. 2L72 4F A9NM 20051018002202005101800220NM 2005 10 18 SB05130 120051012A2910 FITTING BOEING737 737401 1384701NM MLG WHEELWELL LEAKING A USAAA UNSCHED LANDING KBJFLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 EA19424US 23991 ON CLIMBOUT, CREW REPORTED A LIGHT HAZE/SMOKE APPEARING IN CABIN & COCKPIT. HAZE/SMOKE BURNED THE NOSE, THROAT & EYES. FLIGHT RETURNED TO FIELD & LANDED WITHOUT INCIDENT. NO EMERGENCY DECLARED. MX FOUND HYD PRESSURE LINE FITTING AT -A- AUTOPILOT AILERON ACTUATOR LEAKING. TIGHTENED SAME. LEAK & OPS CHECK GOOD. RAN BOTH ENGINES & PACKS TO CLEAR OUT ACFT ODOR. UNFORTUNATELY, ACFT RETURNED TO GATE FOR SAME PROBLEM. FERRIED TO CLT FOR REPAIR, WHEREAS, MX FOUND RESERVOIR PRESSURE MODULE LEAKING INTO CROSSBLEED MANIFOLD. REPLACED MODULE PER MM 29-09-11. LEAK CHECK GOOD. RAN ENGINES, APU & PACKS. NO HAZE OR SMOKE NOTED IN CABIN. 2L72 4F RTA16WE 20051018002212005101800221NM 2005 10 18 05FDEA03390 120051011A5410 STRUCTURE BOEING727 727200 138407ENM NACELLE CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 NR 2 ENGINE BS 1342, MATING SURFACE FOR RT FWD COWL CHAFED, WORN TO KNIFE EDGE AT 5:30 TO 6:00 O'CLOCK POSITION. REPLACED 1342 CHORD PER SRM 51-30-2. 2L73 4F RTA3WE 20051018002222005101800222EU 2005 10 18 EMB05014 120051010A215010007004 ACM EMB ERJ170ERJ170100 EU NR 2 ODOR A USAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA19819MD971 000040 THE CREW REPORTED THE SMELL OF SMOKE AND FUMES IN THE CABIN AND FLIGHT DECK AT CRUISE ALT OF 340. THERE WERE NO WARNINGS IN THE COCKPIT, THE CAPTAIN REQUESTED TO DIVERT TO PIT AS A PRECAUTIONARY. THE NR 2 PACK FAILED PRIOR TO LANDING. MAINTENANCE VISUALLY INSPECTED NR 2 PACK, FOUND ACM FROZE UP, DAMAGED. A/C RELEASED ON MEL 1003C20, CONTROL 21-8100A. 10/12/05 - REMOVED AND REPLACED ACM. OPERATIONAL CHECK IS GOOD, THIS REMOVES MEL. 2L74 4F RTA56NM 20051018002242005101800224NM 2005 10 18 05FDEA03247 120051005A5347ADA83891 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 MAIN DECK CARGO COMPARTMENT: LEFT HAND SEAT TRACK MOUNTING EDGE FOUND GOUGE AT STATION 939, X=47.5. MAIN DECK CARGO COMPARTMENT: LEFT HAND SEAT TRACK AT STATION 939, X=47.5 REPAIR CARRIED OUT AS PER SRM 53-70-00 VOL I FIG 1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051018002262005101800226NM 2005 10 18 05FDEA03209 120051004A5510ALC8107Y2 FITTING DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 HOR STAB RT BARREL NUT BORE NR 26 FOUND WITH CORROSION. SPLICE FITTING AT BARREL NUT BORE NR 26R REMOVED AND NEW FITTING INSTALLED IAW SRM 51-32-01 VOL.II, SRM 51-38-01 VOL.II, SRM 51-33-01 VOL.II AND E1-5510-7-5000 D1 PT1. MINOR REPAIR I.A.W FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20051018002282005101800228NM 2005 10 18 2005UALA01061 120051002A33501317 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29173UA 24380 EMERG LT INOP AT DR 1R AND 3R CEILING. REPLACED LAMP 2L74 4F4 FRTA20WE E24NE 20051018002372005101800237NM 2005 10 18 2005UALA01074 120051003A335059193 WIRE BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29179UA 25158 INOPERATIVE EMERGENCY EXIT LIGHTS AT DOOR 1L. REPLACED CABLE BEHIND FLT ATTENDANT SEAT DOOR 1L. 2L74 4F4 FRTA20WE E24NE 20051018002382005101800238EU 2005 10 18 2005UALA01077 120051004A3350AD321430 BATTERY AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE EMERGENCY LIGHT FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29455UA 1105 EMERGENCY LIGHT BATTERY RT FAILED 3SVC TEST. REPLACED EMERGENCY LIGHT BATTERY. 2L72 4F4 FRTA28NM E40NE 20051018002392005101800239NM 2005 10 18 2005UALA01078 120051005A33501317 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29182UA 25279 EMERGENCY CEILING LIGHT NEAR SEAT ROW 44 ABC IS INOP. REPLACED LAMP 2L74 4F4 FRTA20WE E24NE 20051017000762005101700076EA 2005 10 17 VTZA200500204 120051010A5315S6830 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 325-334 CORRODED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27621BR 7186 LBL 27 FLOORBEAM HAS CORROSION AT FS 325.5 THROUGH 334.5. 2L72 4F RTA21EA 20051017000842005101700084SO 2005 10 17 138910092005 120051009A324160064211 ANTI-SKID SYS GULSTMG1159 GIV 3980115SO MLG MALFUNCTIONED E N93AO OTHER O OTHER LDLANDING 1 SO13489QS 1389 NR 1 TIRE BLEW ON LANDING. 2L72 4F RTA12EA 20051017000862005101700086WP 2005 10 17 AALA20050660 120051009A2610 ELECTRONIC UNIT DOUG DC9 DC983 3022083WP CARGO BAY INOPERATIVE A AALAO OTHER N FALSE WARNING DEDESCENT 1 SW219618A 53565 PSP - INFLIGHT DURING DESCENT WARNING SOUNDED INDICATING FIRE IN AFT CARGO. BOTTLES DISCHARGED. LANDED PSP WITHOUT INCIDENT. NO FIRE. FOUND CARGO ELECTRONIC UNIT IN AFT CARGO COMPARTMENT CAUSING FIRE WARNING. REPLACED CARGO ELECTRONIC UNIT AND REPLACED CARGO SUPPRESSION SYSTEM FIRE BOTTLES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20051017000902005101700090EA 2005 10 17 COMA0560548 120051011A3232 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA NLG DOOR FROZEN A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01929CA 7035 FLIGHT 5227 - NLG DOOR OPEN WARNING. LUBRICATED AND FREED UP FROZEN ROLLER IN NLG DOORS OPERATING MECHANISM. 2L72 4F RTA21EA 20051017000942005101700094EA 2005 10 17 REXA200500129 120051005A7603A33721 BRACKET CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE THRUST LEVER UNSECURE A REXAE ENGINE SHUTDOWN F FLT CONT AFFECTED CLCLIMB 1 SO25812A 1822 8012 GEE950294 ON CLIMBOUT, ATTEMPTED TO REDUCE CLIMB POWER FL250. CAPTAIN CONFIRMED THE THRUST LEVER WAS JAMMED. COMPLIED WITH THE QRH CHECKLIST, AND DECLARED AN EMERGENCY. THE FLIGHT WAS CLEARED DIRECT TO MEMPHIS (MEM). AT THIRTY MILES OUT AND ON THE ILS TO RUNWAY 18C, THE FLIGHT CREW SHUTDOWN THE ENGINE USING THE FIRE SWITCH. AN OTHERWISE UNEVENTFUL APPROACH AND LANDING WAS MADE. THE AIRCRAFT WAS ABLE TO TAXI TO THE GATE AND NO EVACUATION OF THE PASSENGERS WAS NECESSARY. MAINTENANCE FOUND THAT THE UPPER CORE COWL DOOR STAY BRACE STRUT HAD NOT BEEN PROPERLY STOWED AND THAT IT HAD JAMMED THE THROTTLE CONTROL GEARBOX. THE STAY BRACE STRUT WAS PROPERLY SECURED AND THE AIRCRAFT RELEASED FOR FLIGHT. 2L72 4F4 FRTA21EA E15NE 20051017000982005101700098 2005 10 17 SWAA053158 420051011A256563550 SLIDE BOEING737 7377H4 1384404NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29715SW 27849 DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051017001112005101700111EA 2005 10 17 SWIA200515672 120051008A2740 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION DEDESCENT 1 NM07927SW 7693 AP PITCH TRIM CAUTION MSG INFLIGHT DURING DESCENT. REPLACED 1 H/RF CARD AND HORIZONTAL STAB CONTROL UNIT. OPERATIONAL CHECK GOOD IAW 22-11-00, 22-12-00 AND 27-41-00, PN: 7060-9 SN: OFF 1218. 2L72 4F RTA21EA 20051017001162005101700116SO 2005 10 17 CHQA200500176 120051013A33507287560505 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11571RP 14500827 FORWARD EMERGENCY LIGHT PROXIMITY STRIP FAILED TO ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT PROXIMITY STRIP IAW EMB 145 MM 35-50-00. OPS CHECK GOOD. 2L72 4T RTT00011AT 20051017001272005101700127SO 2005 10 17 CHQA200500173 120051005A2120 ODOR EMB 145 EMB145LR 3260212SO COCKPIT DETECTED A CHQAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL11562RP 145451 FLIGHT 6370 - RDU-MCO - INTERMITTENT ODOR IN COCKPIT DURING FLIGHT. SMELL RESEMBLES BURNING SULFUR, AND ALMOST HAS AN ELECTRICAL BURNING SMELL. VERY STRONG FOR APPROXIMATELY 30-60 SECONDS, THEN GOES AWAY. NO ACTUAL SMOKE WAS PRESENT. BOTH TIMES, STARTED WHEN ENTERING PRECIPITATION. INSPECTED UNDER FLOOR BOARD OF AFT CABIN FORWARD OF LAVATORY. INSPECTED UNDER FLOOR BOARD OF CARGO COMPARTMENT. ALL ACCESS DOORS OPENED AND INSPECTED. NO DISCREPANCY NOTICED. COULD NOT DUPLICATE SMELL. ALL WORK DONE IAW EMB 145 MM 36-00-00 AND 70-00-00 ENGINE RUNS. 2L72 4T RTT00011AT 20051017001342005101700134WP 2005 10 17 IXXA05SMN160S 120050809A5753 SKIN DOUG DC8 DC873F 302199FWP NR 3 FLAP VANE DELAMINATED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL948072897 46003 DURING ROUTINE C CHECK INSPECTION, RT WING, NR 3 VANE FLAP LWR. SKIN DELAMINATED. REMOVED AND REPLACED NR 3 FLAP VANE ON RT WING (REPAIRED CONDITION) IAW DC8 MM 27-51-14 PAGES 201-202. 2L74 4F RT4A25 20051017001482005101700148NM 2005 10 17 USAA051206 120051013A5310 CREASE BEAM BOEING757 7572B7 1384964NM BS 310-324 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19627AU 27805 MAIN CABIN BS 310 - 324, RBL 62, R1 DOOR AREA; NO LEVEL OR TASK. REPLACED CREASE BEAM WITH NEW FABRICATED BEAM ASSY PER SRM 53-00-51, FIG 101, 53-30-13. DEFECT SIZE 6 INCHES LONG X 1.5 INCH WIDE X .040 INCH DEEP. 2L72 4F RTA2NM 20051017001612005101700161NM 2005 10 17 AWXA200501211 120050921A532079434562 FILLER BOEING737 73733A 1384673NM THRESHOLD CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW 23634 DURING C20 CHECK DISCOVERED CORROSION ON THE AFT BAG PIT THRESHOLD INBOARD SUPPORT FILLER, LOWER SURFACE AT BS 802, BL 16R. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-15-1A FIG 101. REMOVED FILLER AND INSTALLED NEW SUPPORT FILLER AT BS 802 AND BL 16R IAW BOEING 737-300 SRM 51-40-02. 2L72 4F RTA16WE 20051017001632005101700163EU 2005 10 17 AWXA200501213 120050930A5347D5713014720000 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28626AW 65 DURING C5 CHECK DISCOVERED CORROSION LOCATED ON SEAT TRACK AT FR 36 + 15" AND Y-765. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 101. REMOVED SEAT TRACK AND INSTALLED NEW SEAT TRACK FROM FS 36 TO FS 41 AND Y-765 IAW AIRBUS 320 SRM 51-42-11. 2L72 4F RTA28NM 20051017001712005101700171NM 2005 10 17 DHL2005788014 120050927A3260 WARNING LIGHT BOEING727 727214 138407RNM NLG FALSE ACTIVATIONA DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01788AT 21958 RED NOSE GEAR DOOR AND AMBER NOSE GEAR DOOR ON S/O PANEL CAME ON DURING CLIMB. ABNORMAL PROCEDURE COMPLETED. CONDITION RETURNED TO NORMAL WITH GEAR HANDLE UP. INSP NOSE GEAR DOOR'S IAW 727 MM CH 32-22-1, NO DEFECTS FOUND AT THIS TIME. INDICATION PLACED ON DMI IAW MEL 32-1 CAT-C CONTROL 22587. REF DMI 22587 RED NOSE GEAR DOOR AND AMBER NOSE GEAR DOOR ON S/O PANEL CAME ON DURING CLIMB. ABNORMAL POR COMPLETED CONDITION RETURNED TO NORMAL WITH GEAR HANDEL UP. JACKED NOSE & PERFORMED NOSE GEAR RETRACTION TO VERIFY NOSE GEAR DOOR RIGGING AND OPERATION. NO DEFECTS NOTED. OPS CHECK GOOD IAW 727 MM 32-22-0. THIS CLEARS DMI 22587. 2L73 4F A3WE 20051017001772005101700177EU 2005 10 17 DHL2005366005 120050920A2611RCG90900 SMOKE DETECTOR AIRBUS300 A300B4203 3930306EU UNKNOWN MALFUNCTIONED A DHLABA EMER. DESCENT UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01366DH 249 SMOKE LIGHT ILLUMINATED IN FLIGHT ON MWP. REMOVED AND REPLACED SMOKE DETECTOR FAULT UNIT. OPS CHECK GOOD IAW 26-16-11. 2L72 4F RTA35EU 20051017001782005101700178NM 2005 10 17 05FDEA03408 120051012A5321 FLOOR PANEL BOEING727 727100 1384036NM BS 1150 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 CORROSION ON MAIN CARGO DECK FLOOR PANEL WEB AT BS 1150, RBL 60, WL 208. CUT OUT DAMAGE FLOOR WEB AT BS 1150, RBL 60, WL 208 AND INSTALLED REPAIR DOUBLER PER SRM 51-40-2. 2L73 4F RTA3WE 20051017001832005101700183EU 2005 10 17 YENA200568 120050921A5343 SUPPORT BRACKET AIRBUS320 A320232 3930326EU IAE V2524 V2524A5 NE NLG DAMAGED A YENAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA15536JB14228 1784 AFTER TAKEOFF, THE NOSE LANDING GEAR (NLG) DID NOT RETRACT AND WHEELS WERE OFFSET AT A 90 DEGREE ANGLE. THE AIRCRAFT WAS DIVERTED, WHERE IT LANDED WITH THE NLG AT ABNORMAL STEERING ANGLE. PRILIMINARY BORESCOPE INSPECTION FINDINGS INDICATE NLG UPPER SUPPORT ASSY (P/N D59831) TANGS HAVE FAILED. 2L72 4F4 FRTA28NM E40NE 20051017001852005101700185WP 2005 10 17 AALA20050638 120051003A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21416AA 49327 SAT- OVERHEAD EMERGENCY LIGHTS AT ROWS 5 TO 9 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT ROWS 5 TO 9. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051017002052005101700205EA 2005 10 17 QXEA200501313 120050917A5754 SKIN CNDAIRCL600 CL6002C10 1390015EA LE SLAT CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09617QX 10130 YYC - RIGHT WING SLAT PANEL NR 622CB CHAFED. BLENDED OUT DAMAGE IAW EA R-57-108 AND REO 670-57-42-069. NO CRACKS FOUND. RESTORED FINISH. 2L72 4F RTA21EA 20051017002192005101700219NE 2005 10 17 MASA200500764 220051001A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LEFT OVERTEMP A MASAC ABORTED TAKEOFF MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 SW077730215410 7302 872491 ASH 6110 PHX. RED FLASHING ITT ON LT ENGINE DURING TAKE OFF ROLL. TEMPERATURE EXCEEDED 900 DEGREES. MX R2 ENGINE. 2L72 4F4 FRTA21EA E15NE 20051017002332005101700233NM 2005 10 17 SWAA053092 120051009A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM BS 767 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 767, RBL 6. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051018000042005101800004NM 2005 10 18 C1HA200594006 120051017A533065198618 SKIN BOEING727 727290 138408WNM BS 350 BULGED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15294AS 22146 RT FUSE SKIN BULGED AT NOSE WHEEL WELL LWR CHORD BS 350. REMOVED AND REPLACED DAMAGED NOSE WHEEL WELL RT LWR CHORD P/N 65-19861-8, IAW 727 SRM 51-30-2. 2L73 4F A3WE 20051018000132005101800013EA 2005 10 18 VTZA200500209 120051007A2751855D1009 POSITION SENSOR CNDAIRCL600 CL6002B19 1900309EA LT TE FLAPS FAILED A VTZAO OTHER J WARNING INDICATION APAPPROACH 1 EA27641BR7751 60 7349 FLAPS FAILED AT 0 DEGREES ON APPROACH. 2L72 4F RTA21EA 20051018000162005101800016NM 2005 10 18 SB05133 120051016A335020131A BATTERY PACK BOEING737 7373B7 1384580NM EMERGENCY LIGHTSDISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19395US 23317 CLT - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT POWER SOURCE BATTERY WAS WEAK IN THE FORWARD CABIN. MAINTENANCE REMOVED AND REPLACED THE FORWARD CABIN BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20051018000372005101800037WP 2005 10 18 UPS05845605 120051012A5322 SHEAR TIE DOUG DC8 DC873F 302199FWP BS 1395 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE:C2 CRACKED SHEAR TIE AT STA 1395 BETWEEN L35 AND L36 RT. REMOVED SHEAR TIE IAW SRM 53-2-0 FIG 2B, FABRICATED AND INSTALLED SHEAR TIE AND SPLICE REPAIR IAW SRM 53-2-0 FIG 2D AND SRM 51-1-20D. 2L74 4F RT4A25 20051018000512005101800051EA 2005 10 18 SWIA200515677 120051009A2751855D10011 POSITION SENSOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07917SW7458 7458 7641 FLAPS DEGRADED MSG ON EICAS. REMOVED AND REPLACED RT BPSU IAW MM 27-50 AND SKEW DETECTION UNIT PER CRJ MM 27-51-15. OPERATIONAL CHECK GOOD, PN 601R59014-1; SN OFF A580. 2L72 4F RTA21EA 20051018000552005101800055NM 2005 10 18 UPS05245130 120050713A5330 SKIN BOEING727 72722C 138400FNM BS 290 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01941UP 19196 LIGHT SURFACE CORROSION FOUND ON FUSELAGE SKIN BS 290 STR 6L TO 7L. SURFACE CORROSION BLENDED AND FOUND O/S LIMITS. SKIN CUT AND EXTENSIVE CORROSION FOUND ON INNER SURFACE AND DISBOND BETWEEN SKIN AND DOUBLER. FABRICATED NEW SKIN IAW SRM 51-20-01 FOR BS 277-360 S4L AND S10L. RE AIR CARRIED OUT IAW UPS EO B727-5330-22625. 2L73 4F A3WE 20051018000582005101800058WP 2005 10 18 UPS05845599 120051005A53203750257U1 SPLICE DOUG DC8 DC873F 302199FWP BS 440-460 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE:C2 A PIT L31L SPLICE FITTING CRACKED BETWEEN STA 440 AND 460. REMOVED AND REPLACED SPLICE FITTING AT STA 440-460 L31L IAW SRM 51-1-20D, 51-3-2. 2L74 4F RT4A25 20051018000632005101800063NM 2005 10 18 SWAA053161 120051013A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 787 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 787, STR 13L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051018000932005101800093NM 2005 10 18 05FDEA03324 120051009A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 RT HORIZ STAB BARREL NUT BORE NR 28 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 40. MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20051018001072005101800107 2005 10 18 AALA20050675 420051010A2565 SLIDE AIRBUS300 A300B4605R 3930308EU L3 DOOR DEPLOYED A AALAO OTHER O OTHER TXTAXI/GRND HDL 1 SW2114056 463 JFK - L3 DOOR SLIDE INADVERTANTLY DEPLOYED UNSUCCESSFULLY. REPLACED L3 DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20051018001092005101800109WP 2005 10 18 AALA20050671 120051010A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21490AA 49683 SFO - BOTH FORWARD OVERWING EMERGENCY ESCAPE HATCHES EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT ROW 20 FOR BOTH FORWARD OVERWING EMERGENCY ESCAPE HATCHES EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051018001142005101800114SO 2005 10 18 2005F00102 120050914A3246C20211170 WHEEL LKHEEDP38 P38L 5260206SO ALLSN V1710 V1710* GL LOOSE LOOSE B K NONE O OTHER ININSP/MAINT 1 WP01718 2602 82 8187 WHEEL ASSEMBLY RETURNED FOR LOOSE TIE BOLTS, OF 18 TIE BOLTS INSTALLED 2 ARE MISSING 11 ARE LOOSE. MFG HAS NOW ISSUED SERVICE LETTER F6137-32-843 IN HOPES THIS WILL RESOLVE. 2M72 4V4 V LTC10 EXPE4V 20051018001162005101800116CE 2005 10 18 2005F00104 120050914A3246C2021170 WHEEL CESSNA337 T337G 2075726CE CONT O360 TSIO360* 17025SO MLG LOOSE B K NONE O OTHER ININSP/MAINT 1 WP01435 566 137 P3370261 WHEEL ASSEMBLY RETURNED FOR LOOSE TIE BOLTS OF 18 INSTALLED 14 WERE FOUND LOOSE 2 MISSING. MFG HAS NOW RELEASE SERVICE LETTER F6137-32--843 IN HOPES THIS WILL RESOLVE. 1H72 3O3 O A6CE E9CE 20051018001172005101800117NM 2005 10 18 05FDEA03338 120051010A5322 SHEAR TIE BOEING727 72722 1384002NM BS 1030 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 CORROSION ON SHEAR TIE BS 1030 RBL 3 WL 148. REMOVED CORROSION ON SHEAR TIE FOUND TO BE OUT OF LIMTIS. INSTALLED NEW SHEAR TIE, ALL WORK DONE IAW SRM 53-10-1, 53-10-4, 51-30-2. 2L73 4F A3WE 20051018001222005101800122NM 2005 10 18 05FDEA03199 120051004A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 HORIZ STAB RT BARREL NUT BORE NR 22 FOUND WITH CORROSION. REWORK/ REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 29. MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20051018001252005101800125NM 2005 10 18 05FDEA03202 120051004A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 HORIZ STAB LT BARREL NUT BORE NR 15 FOUND WITH CORROSION. REWORK/ REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 31. MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20051018001362005101800136WP 2005 10 18 05FDEA03192 120051002A3243 CABLE DOUG DC10 DC1010 3022110WP BRAKE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25389FE 46623 BRAKE CABLE NR 148 RUSTY AT PULLEY BEND UNDER MAIN CARGO COMPT FLOOR STA 1450 RBL37. REMOVED, REPLACED AND ADJUSTED LT BRAKE CONTROL SYSTEM IAW DC10 M/M 32-44-00. OPS CHECK GOOD IAW DC10 M/M 32-44-00-2 . 2L73 4F A22WE 20051018001382005101800138NM 2005 10 18 05FDEA03196 120051004A5310 STRUCTURE DOUG MD11 MD11 3023602NM BS 535-547 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 LOWER FUSELAGE, AIRCON COMP 1 AT STA 535 TO 547 LONG 32-33 FOUND EDGE CRACK. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL.II. MAJOR REPAIR PER GMM 6-2-100. 2L73 4F RTA22WE 20051018001472005101800147NM 2005 10 18 AWXA200501189 120050916A3210654611321 TRUNNION BOEING737 7373G7 1384595NM RT MLG CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 MCN - DURING C16 CHECK DISCOVERED CORROSION ON THE RT MLG TRUNNION PIN AND NUT ASSEMBLY. NO CORROSION REMOVAL LIMITS ARE AVAILABLE FOR PIN OR NUT. MAINTENANCE REMOVED AND REPLACED THE RT MLG TRUNNION PIN AND NUT IAW AMERICA WEST AIRLINES TASK CARD E4R32002. 2L72 4F RTA16WE 20051018001562005101800156NM 2005 10 18 USAA051195 120051006A534050826110 STRINGER CLIP BOEING737 7374B7 1384702NM BS 303.9 DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19443US 24842 FOUND ATTACH CLIP BLENDED, STATION 303.9 AT STRINGER 4L. ATTACH CLIP INSTALLED PER SRM 51-40-02, DEFECT SIZE: 1" DIA. 2L72 4F RTA16WE 20051018001632005101800163NM 2005 10 18 USAA051188 120051006A575465C26602257A SKIN BOEING737 7374B7 1384702NM NR 2 SLAT WEDGE DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19443US 24842 FOUND NR 2 SLAT T/E WEDGE O/B END DELAMINATED. REMOVED DAMAGE INSTALLED REPAIR PIECES IAW SRM 51-70-10, DEFECT SIZE: 3" X 6" DELAMINATION. 2L72 4F RTA16WE 20051018001862005101800186WP 2005 10 18 UPS05845547 120050902A534037549301N FITTING DOUG DC8 DC873F 302199FWP CARGO DOORWAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 C3 C PIT DOOR JAMB FITTING CRACKED I/B OF NR 2 TEE BOLT FITTING AT FWD SIDE. REMOVED AND REPLACED FITTING IAW DC-8 SRM 53-2-0 FIG 2D AND 51-1-20D. 2L74 4F RT4A25 20051018001932005101800193NM 2005 10 18 05FDEA03354 120051011A5754 SKIN DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 RIGHT WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT XORS 680. TRIMMED OUT AS PER FEDEX EA 1-5710-89997. REPAIR DOUBLER AND ANGLE FABRICATED AND INSTALLED AS PER FEDEX EA 1-5710-89997. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2- 100. 2L73 4F RTA22WE 20051018001972005101800197NM 2005 10 18 05FDEA03359 120051011A5712ARB39544 RIB DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 RT WING FIXED LEADING EDGE INTERNAL RIB DOUBLER FOUND CRACKED AT XORS 559. CRACKED INTERNAL RIB DOUBLER AT RIGHT HAND WING FIXED LEADING EDGE XORS 559 REMOVED AS PER SRM 51-31-01 VOLUME II. NEW RIB DOUBLER FABRICATED AS PER DRAWING ARB3954 AND INSTALLED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051018002112005101800211 2005 10 18 SWAA053095 420051009A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29355SW 25250 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051018002122005101800212NM 2005 10 18 SWAA053096 120051006A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29406WN 27894 EEPLS TRACK LENS COVER LOOSE AT FWD END. SECURED COVER PER MM. 2L72 4F RTA16WE 20051018002232005101800223WP 2005 10 18 DHLA102005AA 120051017A57305612385 SKIN DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH 46033 LEFT WING SKIN CRACKED AT STRINGER 64 LT. APPROX XRS 450 AT FASTENER HOLE FOUND WHILE ACCOMPLISHING S/B 57-100 INSPECTION 2L74 4F RT4A25 20051018002402005101800240NM 2005 10 18 2005UALA01079 120051005A3350362624 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29182UA 25279 SEAT EMERGENCY LIGHT 58 HJK IS INOP. REPLACED EEL LIGHT. 2L74 4F4 FRTA20WE E24NE 20051018002412005101800241NM 2005 10 18 2005UALA01080 120051005A335080541 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29182UA 25279 MID LAV FLOOR TO WALL CROSS AISLE EMERGENCY LIGHT IS INOP. REPLACED EEL LAMP. 2L74 4F4 FRTA20WE E24NE 20051019000032005101900003SO 2005 10 19 64710152005 120051015A2530 COFFEEMAKER GULSTMGV GULFSTREAMGV3980116SO GALLEY ODOR E N93AH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO13511QS 647 ELECTRICAL BURNING SMELL IN CABIN. NO SMOKE. 2L72 4F RTA12EA 20051019000052005101900005NM 2005 10 19 2005UALA01124 120051010A2530 SMOKE BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE CABIN DETECTED A UALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP29785UA 26954 ELECTRICAL ODOR (HEAT) APPARENT AROUND DOOR 2R. OPENED CLOSET AT 2R AND SMOKE WAS SEEN TO EXIT. GALLEY POWER TURNED OFF AND ODOR DISSIPATED. REPLACED TRANSFORMER 10/11/05. SYSTEM HAS BEEN FUNCTIONING NORMALLY AS OF 11/10/05. PROBLEM APPEARS TO HAVE BEEN A ONE TIME FAILURE OF THE TRANSFORMER. 2L72 4F4 FRTT0001SE E46NE 20051019000072005101900007NM 2005 10 19 2005UALA01126 120051012A5610 WINDSHIELD BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE COCKPIT CRACKED A UALAA UNSCHED LANDING O OTHER CLCLIMB 1 WP29655UA 25393 CAPTAINS WINDSHIELD CRACKED. FLIGHT DIVERTED TO LHR. 2L72 4F4 FRTA1NM E24NE 20051019000082005101900008EU 2005 10 19 2005UALA01127 120051012A335032145410 EPSU AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE EMERGENCY LIGHTSWILL NOT TEST A UALAK NONE L NO TEST ININSP/MAINT 1 WP29447UA 836 EMERGENCY LIGHT TEST FAILED EPSU INT LOAD FWD L. REPLACED THE FWD LEFT EPSU. 2L72 4F4 FRTA28NM E40NE 20051019000092005101900009NM 2005 10 19 2005UALA01128 120051012A5241 DOOR FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE GALLEY DOOR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29919UA 25386 FORWARD GALLEY DOOR, FORWARD SIDE LOWER END FRAME IS CRACKED AT FASTENER HOLE. REMOVED DAMAGE. FABRICATED FRAME & FRAME SPLICE PARTS PER UAL SM-90-52-40-14-JD. INSTALLED REPAIR PER SM-90-52-40-14-JD. 2L72 4F4 FRTA16WE E2GL 20051019000102005101900010NM 2005 10 19 2005UALA01129 120051012A5210 DOOR FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE PAX DOOR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29919UA 25386 FORWARD ENTRY DOOR AFT SIDE LOWER END FRAME IS CRACKED AT FASTENER HOLE. REMOVED DAMAGE. INSTALLED REPAIR KIT, INNER SKIN & AFT LOWER STOP PER SM-90-52-40-14-JD. 2L72 4F4 FRTA16WE E2GL 20051019000122005101900012NM 2005 10 19 2005UALA01131 120051012A5522 SKIN BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE LT ELEVATOR DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29919UA 25386 LT ELEVATOR UPPER SURFACE HAS A ONE SQUARE INCH AREA OF CORE DAMAGE AT 88 INCHES OUTBOARD OF INBD EDGE. REMOVED DAMAGE. ACP. LAYUP AND COOK PER SRM 51-70-05 & SRM 55-20-01. 2L72 4F4 FRTA16WE E2GL 20051019000132005101900013NM 2005 10 19 2005UALA01132 120051013A3244H4919022 TIRE BOEING747 747422 1384935NM PWA 4056 PW4056 NE MLG FAILED A UALAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 WP29181UA 25278 TWO LEFT MAIN TIRES BLEW. TWO LEFT REAR BODY GEAR TIRES BLOWN DURING TAKEOFF ROLL. DAMAGE TO BODY GEAR STEERING AND FAIRING. REPLACED BOTH TIRE ASSEMBLIES AND REPAIRED DAMAGE. 2L74 4F4 FRTA20WE E24NE 20051019000142005101900014NM 2005 10 19 2005UALA01133 120051012A335020131A BATTERY BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE EMERGENCY LIGHTSDISCHARGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29643UA 25093 DOOR 1LH AND 1RH EMERGENCY EXIT LIGHTS INOP REPLACED POWER SUPPLY. REPLACED POWER SUPPLY. 2L72 4F4 FRTA1NM E24NE 20051019000172005101900017NM 2005 10 19 2005UALA01136 120051013A2120 ODOR BOEING777 777222 1385219NM PWA PW4077PW4077 NE CABIN DETECTED A UALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP29779UA 26941 ELECTRICAL BURNING SMELL AND HUMMING NOISE FROM DOOR 2 AFT CHILLER. MANUFACTURER REPORTS COMPRESSOR CRUSH WASHERS RELIEVED, ALLOWING RELEASE OF REFRIGERANT AND OIL. NO CAUSE FOR OVERPRESSURE FOUND. MANUFACTURER REPORTS PERIOD OF QUALITY DEPARTURE DESCRIBED AS INCORRECT USE OF INSTALLATION TOOL. THIS UNIT WAS MANUFACTURED DURING THAT PERIOD AND BELIEVED TO BE SUBJECT TO THE REPORTED FAILURE AS A RESULT. 2L72 4F4 FRTT0001SE E46NE 20051019000192005101900019NM 2005 10 19 2005UALA01138 120051013A2750 FLAP SYSTEM BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE MALFUNCTIONED A UALAO OTHER J WARNING INDICATION LDLANDING 1 WP29642UA 25092 LANDED ORD UNDER AMBER ALERT DUE TO TRAILING EDGE FLAP INDICATION PROBLEM. 2L72 4F4 FRTA1NM E24NE 20051102000022005110200002WP 2005 11 2 ARWA20051003 120051011A30809788403 VALVE DOUG DC10 DC1030 3023501WP PACK ANTI-ICE FAILED A ARWAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO19524MD 46999 APPROACHING TOP OF CLIMB (TOC) OUT OF TJSJ; DENSE WHITE SMOKE ENTERING THE COCKPIT AREA WHILE PERFORMING SMOKE SOURCE 10 CHECKLIST, SMOKE STOPPED; FLIGHT CONTINUED OK. PERFORMED T/S DC-10 M/M TAFI 21-50-00; FOUND NR 3 PACK EXHAUST DOOR STAYING CLOSED; DEFERRED NR 3 PACK, TRANSFERRED TO DMI 19590 IN ACCORDANCE WITH MEL 21-1 CAT "C" REF MEL DDG, SECURED CLOSED THE PACK CONTROL VALVE AS PER MEL/DDG. AS PER TAFI M/M 21-50-00 FOUND NR 3 PACK ANTI-ICE VALVE STOCK OPEN. REMOVED AND REPLACED VALVE SEPARATOR COACESCER BAG IN ACCORDANCE WITH M/M 21-50-03. OPERATIONAL CHECK SYSTEM INDICATOR IN ACCORDANCE WITH M/M 21-00-00. CLEARED DMI NR 19590. 2L73 4F A22WE 20051019000222005101900022NM 2005 10 19 SWAA053181 120051015A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 294 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIPS CRACKED AT BS 294.5, BETWEEN STR 11L & STR 12L. REMOVED AND REPLACED CLIPS PER SRM. 2L72 4F RTA16WE 20051019000242005101900024NM 2005 10 19 SWAA053183 120051014A53306545774 SKIN BOEING737 7373H4 1384600NM BS 739 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 739, STR 19R. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20051019000252005101900025NM 2005 10 19 SWAA053184 120051014A53306545765 SKIN BOEING737 7373H4 1384600NM BS 520 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 12R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051019000262005101900026NM 2005 10 19 SWAA053185 120051014A53306545766 SKIN BOEING737 7373H4 1384600NM BS 473-474 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 473 TO BS 474, STR 16R. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20051019000272005101900027NM 2005 10 19 SWAA053186 120051015A53306545777 SKIN BOEING737 7373H4 1384600NM BS 953 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 953, STR 24R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051019000292005101900029NM 2005 10 19 SWAA053188 120051013A53306545765 SKIN BOEING737 7373H4 1384600NM BS 500D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29341SW 24091 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 16L. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20051019000342005101900034NM 2005 10 19 AT0500037 120051006A2910 HYDRAULIC SYSTEM BOEING717 717200 1383700NM RIGHT LOW A ZZDAO OTHER J WARNING INDICATION APAPPROACH 1 SO15972AT 55033 RIGHT HYD QTY LOW PERFORMED MANUAL GEAR EXTENSION PRIOR TO LANDING. CLEANED W/W & INSPECTED FOR LEAKS. NO LEAKS NOTED REF M/M 32-20. R&R RIGHT AND LEFT NOSE STEERING CYLINDER AND SERVICED RIGHT AND LEFT HYDRAULIC SYSTEM. 2L72 4F TRA6WE 20051019000352005101900035WP 2005 10 19 ARWA20051002 120051008A29105773964206 LINE DOUG DC8 DC863F 302198FWP HYD SYSTEM LEAKING A ARWAO OTHER KJ FLUID LOSS WARNING INDICATION LDLANDING 1 SO19441J 45988 LOST HYD FLUID FROM MAIN HYD RESERVOIR AFTER LANDING. UPON INSPECTION; FOUND FLEX LINE LEAKING ON RT MAIN GEAR TRUCK O/B HYD MANIFOLD NEXT TO BOGGIE TRIM ACTUATOR. REMOVED & REPLACED LINE WITH E EACH FLEX LINE FROM FAK. REPLACED DAMAGE LINE IN HYD SYSTEM ON A TEMPORARY BASIS UNTIL PERMANENT REPAIR CAN BE ACCOMPLISHED IN ACCORDANCE WITH DC-8 M/M 20-00 AND ARROW GMM 6-6-1; AND TRANSFERRED TO MASTER CARRY-OVER CONTROL 07093. REMOVED AND REPLACED FLEX-LINE WITH CORRECT PART NUMBER LINE, P/N 57739-6-4206 IN ACCORDANCE WITH M/M 20-12-0. PRESURIZED HYD SYS, OPS CHECK NORMAL. NO LEAKS NOTED; CLEARED CARRY-OVER 7093. 2L74 4F 4A25 20051019000362005101900036NE 2005 10 19 PCSA10120501 220051012A7200 ENGINE BOEING727 7272F9 138407DNM PWA JT8 JT8D17 52049NE NR 3 OVERHEATED A PCSAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO29199AJ 21426 AFTER DEPARTURE ENGINE NR 3 OIL TEMPERTURE INCREASED TO 160, PERFORMED ALTERNATE PROCEDURE, NO HELP. SHUT DOWN ENGINE, DUMPED FUEL TO LAND. MX INSPECTED INLET & EXHAUST OF NR 3 ENGINE; INLET OK, EXHAUST SHOWS EVIDENCE OF OIL LEAK, SUSPECT NR 6 BEARING SEAL. PERFORMED T/S, OIL LEVEL OK. INSPECTED MAIN OIL SCREEN FOR CONTAMINATION, NORMAL CARBON DEPOSIT FOUND, FUEL DEICING CHECKS OK, NR 4 & NR 5 BEARING TEMP IND WERE DARK. INSTALLED NR 4 & NR 5 BEARING OIL LINE TEMP INDICATORS AS REQUIRED. REMOVED & REPLACED NR 6 OIL PUMP. LEAK CHECK NORMAL. INSTALLED NR 3 THRUST REVERSER IAW BOEING MM 78-30-0 AND MIXER IAW DUGAN MM 78-30-22. THRUST REVERSER OPS CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 FRTA3WE E2EA 20051019000372005101900037 2005 10 19 ARWA20051001 420051006A3400 UNKNOWN DOUG DC10 DC1030F 3023504WP UNKNOWN UNKNOWN A ARWAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 SO19478CT 47819 AT TOP OF CLIMB; AIR TRAFFIC CONTROL (ATC) REPORTED AIRCRAFT OFF COURSE. COULD NOT CORRECT AND REQUESTED VECTORS BACK TO SJU. RESET POWER IN A/C, REPROGRAMMED I.N.S. 1-2-3, ALL CHECKED NORMAL. NO FAULTS FOUND IN ACCORDANCE WITH M/M 34-43-0. 2L73 4F RTA22WE 20051019000382005101900038NM 2005 10 19 AT0500038 120051016A33508039251 POWER SUPPLY BOEING717 717200 1383700NM EMERGENCY LIGHT INOPERATIVE A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15910AT 55086 LOWER EMERGENCY LIGHTS FROM 1-10 DID NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY SUPPLY ASSY IAW 717 MM 33-51, OPS CHECK GOOD. 2L72 4F TRA6WE 20051019000392005101900039NM 2005 10 19 2005UALA01121 120051010A5311 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE BS 482 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29919UA 25386 FORWARD CARGO PIT STA 482A BETWEEN STR 28 LEFT AND STR 28 RIGHT FRAME HAS SEVERAL CRACKS. REMOVED DAMAGED AREAS PER MM53-11-87. NDT FOR CRACKS. NONE FOUND. FABRICATED & INSTALLED FILLER & DOUBLER PER MM 53-11-87 FIG. 801. 2L72 4F4 FRTA16WE E2GL 20051019000412005101900041NM 2005 10 19 P5CA0501403 120050801A5310 BEAM BOEING747 747249F 1384849NM BS 300-320 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 EA15920FT 22237 FWD CARGO, FOUND CRACKS PROPAGATED FROM BLANKET HOLE AT STA 300 AND 320 AND LT NOSE WHEEL WELL VERTICAL BEAM WEB AT WL 160. REPAIR CARRIED OUT IAW LO-BY714-072 INTERIM WEB REPAIR. CONTINUE INSPECTION PER SB 747-53A2293. 2L74 4F A20WE 20051019000422005101900042CE 2005 10 19 DJFA2005147 120051006A32524510041 SHIMMY DAMPENER BEECH MU300 400A 1155402CE NLG WORN E DJFAO OTHER E VIBRATION/BUFFET LDLANDING 1 EA23783TA RK234 UPON ARRIVAL AFTER APPROACH AND NORMAL LANDING WITH NORMAL DECELERATION USING THRUST REVERSERS, AND AFTER ACHIEVING TAXI SPEED OF A FAST PACED WALK, THE AIRCRAFT EXPERIENCED A SEVERE NOSEWHEEL VIBRATION. NORMAL BRAKING APPEARED TO BE LOST, AND EMERGENCY BRAKING WAS USED TO STOP THE AIRCRAFT. MAINTENANCE REPLACED THE NOSE LANDING GEAR SHIMMY DAMPER, BLED THE BRAKING SYSTEM AND SERVICED THE EMERGENCY BRAKE NITROGEN BOTTLE. OPERATIONAL CHECKS OF THE BRAKES AND SHIMMY DAMPER WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4F RTA16SW 20051019000432005101900043NM 2005 10 19 P5CA0501405 120051013A5730 SKIN BOEING747 747249F 1384849NM LT WING CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 EA15920FT 22237 LEFT WING LOWER SKIN CORROSION ON OUTBOARD JACK PAD AREA AT FSS 1295. REPAIR CARRIED OUT IAW BOEING FAA FORM 8100-9. SUPPLEMENTARY JOB CARDS AFM 0147 AND AFM 1068 FOR DETAILS. 2L74 4F A20WE 20051019000442005101900044NE 2005 10 19 ALG2005F00072 120050930A3230 LINK SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL LANDING GEAR INOPERATIVE E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03717AL 760221 AFTER TAKEOFF, LANDING GEAR WAS RETRACTED AND ALL GEAR LIGHTS EXTINGUISHED. FLIGHT CREW RECEIVED A RADIO CALL THAT THE MAIN LANDING WAS NOT FULLY RETRACTED. AIRCRAFT RETURNED AND MAINTENANCE WAS NOTIFIED. MAINTENANCE PERFORMED A GEAR RETRACTION TEST. THE EXPLOSIVE LINK WAS ADJUSTED AND THE LANDING OPERATED NORMALLY IAW MM. (K) 1G72 3U3 U H1NE E1GL 20051019000452005101900045NE 2005 10 19 ALG2005F00071 120051005A2821 FUEL FILTER SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL NR 1 FAILED E ALGAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW03519AL 760058 AFTER TAKEOFF, FUEL PRESSURE DROPPED TO 4 PSI. RETURNED TO BASE AND NOTIFIED MAINTENANCE. MAINTENANCE REPLACED NR 1 FUEL FILTER. GROUND RUN AND OPS CHECK GOOD IAW MM. (K) 1G72 3U3 U H1NE E1GL 20051019000462005101900046NM 2005 10 19 CALA0500366 120051017A5315 FLOORBEAM BOEING737 737724 13844BYNM BS 986 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714704 28765 SEVERAL CLIP HOLES CORRODED AT BS 986.5, FROM RBL 51- LBL51. REPAIRED PER ECRA 5321-01300. 2L72 4F RTA16WE 20051019000472005101900047NM 2005 10 19 CALA0500367 120051017A5320147A8540U8 THRESHOLD BOEING737 737724 13844BYNM BS 947-1086 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714704 28765 THRESHOLD CHORD CORRODED FROM STA 947.5R TO 1086R, INBOARD EDGE OF R2 DOOR. INSTALLED R2 CHORD PER DRAWING 147A5710. 2L72 4F RTA16WE 20051019000492005101900049SO 2005 10 19 RAIA00510016 120051013A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03819HK 145062 PRE-FLIGHT INSPECTION - RIC - ROW 13 EMERGENCY LIGHTS INOP. MAINTENANCE DEFERRED THE EMERGENCY LIGHT STRIP BY SEAT 13. 2L72 4T RTT00011AT 20051019000502005101900050NM 2005 10 19 CALA0500362 120051014A5314656212526 KEELBEAM BOEING737 737524 1384721NM BS 700-727 DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2732626 27530 RT KEEL BEAM CORRODED AND ELONGATED HOLES, STA 700-727. REPAIRED BEAM PER ECRA 5311-01243. 2L72 4F RTA16WE 20051019000512005101900051NM 2005 10 19 CALA0500363 120051014A533065C3579238 SKIN BOEING737 737524 1384721NM BS 887-915 WORN A CALAK NONE O OTHER ININSP/MAINT 1 SW2732626 27530 UPPER FUSELAGE SKIN WORN LIGHTLY BELOW DORSAL FIN FROM STA 887-915. INSTALLED DOUBLER PER ECRA 5331-01206 2L72 4F RTA16WE 20051019000582005101900058SO 2005 10 19 RAIA00510010 120051006A3350 LIGHT EMB 145 EMB145EP 3260221SO CABIN INOPERATIVE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03826HK 145016 POSTFLIGHT INSPECTION -STL - EMERGENCY LIGHTS INOP AT 12A AND 12C. MAINTENANCE INSPECTED EMERGENCY LIGHTS WITH NO DEFECTS NOTED. 2L72 4F RTT00011AT 20051019000592005101900059NM 2005 10 19 SWAA053189 120051015A3350612825 BATTERY PACK BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29372SW 26599 CABIN AFT OVERHEAD BULLNOSE EMERGENCY EXIT LIGHTS INOP. RECHARGED BATTERY PACKS PER MM. 2L72 4F RTA16WE 20051019000602005101900060NM 2005 10 19 SWAA053029 120051004A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 706 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 706. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051019000622005101900062NM 2005 10 19 SWAA053191 120051016A53116546526 FRAME BOEING737 7375H4 138449DNM BS 400 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29505SW 24182 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 24R. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20051019000632005101900063NM 2005 10 19 SWAA053192 120051016A53116520722 FRAME BOEING737 7375H4 138449DNM BS 455 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29505SW 24182 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT BS 455, STR 24R. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20051019000642005101900064NM 2005 10 19 SWAA053193 120051016A5210507945 FRAME BOEING737 7375H4 138449DNM L1 DOOR CHAFED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED 1/2D CHECK, FOUND L1 DOOR UPPER AFT FRAME CHAFED AT TOP EDGE. REPAIRED FRAME PER SWA EA. 2L72 4F RTA16WE 20051019000652005101900065NM 2005 10 19 SWAA053194 120051016A5315BAC1503 FLOORBEAM BOEING737 7375H4 138449DNM BS 312 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FLOORBEAM T-CHORD CORRODED AT BS 312, BETWEEN LBL 54 TO RBL 54. REMOVED AND REPLACED T-CHORD PER SRM. 2L72 4F RTA16WE 20051019000672005101900067NM 2005 10 19 SWAA053196 120051016A5313BAC1498 STRINGER BOEING737 7375H4 138449DNM BS 663 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 663, STR 14R. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20051019000682005101900068NM 2005 10 19 SWAA053197 120051016A534065C27314 STRINGER CLIP BOEING737 7375H4 138449DNM BS 663 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051019000702005101900070NM 2005 10 19 SWAA053208 120051015A53116546539 FRAME BOEING737 7373H4 1384600NM BS 616 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME INNER CHORD CRACKED AT BS 616, BETWEEN LBL 65 TO RBL 65, WL 202. REPAIRED FRAME INNER CHORD PER BFG ER. 2L72 4F RTA16WE 20051019000712005101900071NM 2005 10 19 SWAA053209 120051013A335010107451 LIGHT BOEING737 7373H4 1384600NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29645SW 28330 AFT GALLEY EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20051019000722005101900072EA 2005 10 19 REXA200500126 120050928A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A REXAO OTHER J WARNING INDICATION DEDESCENT 1 SO25812AY 9012 FLAPS FAILED AT 20 DEGREES ON APPROACH. SYSTEM RESET AND PLACED UNDER 72 HOUR WATCH PER AD 98-20-01. 2L72 4F RTA21EA 20051019000732005101900073SO 2005 10 19 SWIA200515628 120051001A3350 BULB EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07585SW 120353 ONE RED FLOOR PROXIMITY EMERGENCY ESCAPE PATH MARKING SYSTEM LIGHT INOP. REPLACED BULB. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20051019000752005101900075EA 2005 10 19 SWIA200515630 120051001A2741 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CLCLIMB 1 NM07927SW 7693 RECEIVED "STAB TRIM" AND "MACH TRIM" CAUTION MSG'S SHORTLY AFTER ROTATION. REPLACED PILOT'S PITCH TRIM DISC SWITCH. OPERATIONAL CHECK GOOD IAW CRJ 200 MM 27-41-30. 2L72 4F RTA21EA 20051019000792005101900079EA 2005 10 19 SWIA200515634 120050930A3350 SWITCH CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INTERMITTENT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07961SW 7857 2ND AND 3RD ROWS OF EMERGENCY EXIT LIGHTS INTERMITTENT. REPLACED FA STATION TOGGLE SWITCH. OPERATIONAL CHECK GOOD IAW MM 33-51-01 AND 33-51-00. 2L72 4F RTA21EA 20051019000802005101900080EA 2005 10 19 SWIA200515635 120050930A3350 SIGN CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSINOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07591SW 7079 FWD GALLEY EMERGENCY LIGHT INOP. REPLACED FWD EMERGENCY SIGN. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051019000822005101900082SO 2005 10 19 SWIA200515637 120050930A3350 FUSE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07586SW 120354 ALL EMERGENCY LIGHTS AFT OF ROW 9 INOP. REPLACED LAMP FUSE, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20051019000832005101900083SO 2005 10 19 SWIA200515638 120051003A3350 SIGN EMB 120 EMB120ER 3260203SO EMERGENCY EXIT BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07223SW 120291 EMERGENCY EXIT SIGN, FLOOR LEVEL AT 6A IS BROKEN. REPAIRED E-EXIT SIGN AT 6A. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20051019000842005101900084EU 2005 10 19 YENA200572 120051002A25304110001137 COFFEEMAKER AIRBUS320 A320232 3930326EU GALLEY BURNED A YENAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15623JB586 586 2504 NR 1 FLIGHT ATTENDANT REPORTED ODOR OF BURNING PLASTIC IN AFT GALLEY NEAR COFFEE POTS. PULLED COFFEE C/B'S STILL REPORTED ODOR FROM A/C LEFT BEHIND GALLEY CARTS. FOUND COFFEEMAKER 508 TO BE AT FAULT. FOUND STRONG ELECTRICAL ODOR COMING FROM COFFEEMAKER. REMOVED & REPLACED COFFEEMAKER 508 PER AMM 25-35-15. OPS CHECK GOOD. ALSO CHECK FOR DAMAGE AT AFT GALLEY COFFEEMAKERS TERM BLOCKS PER AMM TASK 24-00-00. 2L72 4F RTA28NM 20051019000852005101900085NM 2005 10 19 SWAA053030 120051004A53106547979 CREASE BEAM BOEING737 7373H4 1384600NM BS 787 - 807 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 787 TO BS 807, WL 208. REPAIRED CREASE BEAM PER SRM. 2L72 4F RTA16WE 20051019000862005101900086NM 2005 10 19 SWAA053031 120051004A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM BS 447 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 447, STR 26L. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20051019000882005101900088NM 2005 10 19 SWAA053033 120051004A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 727A CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727A, STR 6L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051019000902005101900090NM 2005 10 19 SWAA053035 120051004A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 597 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 597. REMOVED AND REPLACED CLIPS PER SRM. 2L72 4F RTA16WE 20051019000932005101900093NM 2005 10 19 SWAA053038 120051004A53116546555 FRAME BOEING737 7373H4 1384600NM BS 867 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051019000942005101900094NM 2005 10 19 SWAA053039 120051004A55516551524 FITTING BOEING737 7373H4 1384600NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED D CHECK, FOUND LT AND RT HORIZONTAL STAB ATTACH FITTING LUG FACES CORRODED. REPAIRED LUG FACES PER SRM. 2L72 4F RTA16WE 20051019000952005101900095NM 2005 10 19 SWAA053040 120051004A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM BS 747 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 747, RBL 8. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051019000962005101900096NM 2005 10 19 SWAA053041 120051004A53226546529 SHEAR TIE BOEING737 7373H4 1384600NM BS 500A CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500A, RBL 2. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051019000972005101900097NM 2005 10 19 SWAA053042 120051004A53116546529 SHEAR TIE BOEING737 7373H4 1384600NM BS 500C CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500C, BETWEEN LBL 9 TO RBL 2. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051019000982005101900098NM 2005 10 19 SWAA053043 120051004A53106545834 CREASE BEAM BOEING737 7373H4 1384600NM BS 300 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED D CHECK, FOUND RT CREASE BEAM WEB CORRODED AT BS 300, WL 208. REPAIRED CREASE BEAM WEB PER SRM. 2L72 4F RTA16WE 20051019000992005101900099NM 2005 10 19 SCNA05007 120051010A5753 BOLT BOEING737 7378Q8 13844BXNM TE FLAP SHEARED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15806SY 28215 ON POST FLIGHT WALKAROUND, MAINTENANCE FOUND LT INBOARD AFT FLAP DROOPING WITH FLAPS RETRACTED. AFT FLAP ASSY BOLTS WERE SHEARED. MAINTENANCE REPLACED LT INBOARD AFT FLAP LINKAGE MOUNT BOLTS WITH BOLTS, WASHERS & NUTS. 2L72 4F RTA16WE 20051019001002005101900100NM 2005 10 19 SWAA053210 120051014A53306545774 SKIN BOEING737 7373Q8 1384670NM BS 727E CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 24L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051019001022005101900102NM 2005 10 19 SWAA053212 120051014A53306545775 SKIN BOEING737 7373Q8 1384670NM BS 787 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STR 21R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051019001042005101900104 2005 10 19 SWAA053100 420051005A25656557450 COVER BOEING737 7377H4 1384404NM R2 DOOR SLIDE LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29496WN 32478 R2 DOOR EMERGENCY EVAC SLIDE COVER LOOSE. SECURED COVER PER MM. 2L72 4F RTA16WE 20051019001052005101900105 2005 10 19 SWAA053213 420051014A2565D31354 SLIDE BOEING737 7373Q8 1384670NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051019001062005101900106NM 2005 10 19 SWAA053214 120051016A3350D71702001 BATTERY PACK BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29748SW 29800 DURING SCHEDULED MV2 CHECK, FOUND FWD GALLEY EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20051019001072005101900107NM 2005 10 19 SWAA053215 120051016A53306518420 SKIN BOEING737 7377AD 1384502NM BS 235 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29798SW 28436 FUSELAGE SKIN CRACKED AT BS 235.8, EXTERNAL GROUND POWER DOOR CUTOUT. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051019001082005101900108NM 2005 10 19 SWAA053198 120051016A534065C27314 STRINGER CLIP BOEING737 7375H4 138449DNM BS 663 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051019001092005101900109NM 2005 10 19 SWAA053199 120051016A53106547978 CREASE BEAM BOEING737 7375H4 138449DNM BS 616-639 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED 1/2D CHECK, FOUND RT CREASE BEAM CORRODED BETWEEN BS 616 TO BS 639. REPAIRED CREASE BEAM PER SRM. 2L72 4F RTA16WE 20051019001102005101900110NM 2005 10 19 SWAA053200 120051016A5754 SKIN BOEING737 7375H4 138449DNM LT WING SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED 1/2D CHECK, FOUND LT WING NR 2 L/E SLAT OUTBOARD UPPER CORNER DELAMINATED. REPAIRED SLAT PER SRM. 2L72 4F RTA16WE 20051019001122005101900112NM 2005 10 19 2005UALA00817 120050813A2100806002 SWITCH BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN PRESSURE FAILED A UALAA UNSCHED LANDING JG WARNING INDICATION MULTIPLE FAILURE CLCLIMB 1 WP29374UA 24639 AIRCRAFT PRESSURIZATION PROBLEM. AFTER T/O, CREW REPORTED LOSS OF LNAV, VNAV, AUTOTHROTTLE, TCAS AND ENGINE LOW IDLE LIGHT WAS ON. THROUGH 25,000 FT, ALTITUDE WARNING HORN SOUNDED AND THE CABIN ALTITUDE MAXED OUT AT 11,000 FT. AFTER T/O, CREW REPORTED LOST LNAV, VNAV, AUTOTHROTTLE, TCAS AND THE ENGINE LOW IDLE LIGHT WAS ON. THROUGH 25,000 FT, THE ALTITUDE WARNING HORN SOUNDED AND THE CABIN ALTITUDE MAXED OUT AT 11,000 FT. THE AIRCRAFT RETURNED TO FIELD WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE PROBLEM TO A FAULTY LANDING GEAR SAFETY SWITCH S105 AND THE GRD SENSING SQUAT SWITCH M990. BOTH COMPONENTS WERE REPLACED. 2L72 4F4 FRTA16WE E2GL 20051019001132005101900113EA 2005 10 19 COMA0570109 120051016A29169604501 RESERVOIR CNDAIRCL600 CL6002C10 1390015EA NR 3 HYD SYSTEM OVERTEMP A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01625CA6108 10113 FLIGHT 5416 - HYDRAULIC SYSTEM 3 OVERTEMP. REPLACED THE SYSTEM 3 HYDRAULIC RESERVOIR. 2L72 4F RTA21EA 20051019001142005101900114WP 2005 10 19 05FDEA03242 120051005A5313 STRINGER DOUG DC10 DC1010 3022110WP BS 1510 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25389FE 46623 CENTER GEAR WHEEL WELL BILGE AREA AT STRINGER 52 STA 1510 IS CORRODED. REMOVED CORROSION IAW DC10 SRM 51-21-01 VOL 11. FOUND TO BE OUT OF LIMITS IAW DC10 SRM 53-00-01 VOL 1. REPAIRED LONGERON IAW DC10 SRM 53-00-01 FIG 9 VOL 1. ALODINED AND PRIMED IAW DC10 SRM 51-21-01 VOL 11. INSTALLED LONG IAW DC10 SRM 51-33-01 VOL11. MACHINED LONG IAW DAC DWG AYB7013 REV C. 2L73 4F A22WE 20051019001172005101900117NM 2005 10 19 AWXA200501170 120050910A532065C3267714 STRAP BOEING737 7373G7 1384595NM BS 1009-1029 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 MCN - DURING C16 CHECK, DISCOVERED EXFOLIATION CORROSION, LEVEL TWO, ON THE UPPER FLOOR STRAP FROM BS 1009 TO BS 1029, BL 3L AND WL 208. FOUND CORROSION TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 51-10-02-0G FIG 1. REMOVED UPPER FLOOR STRAP FROM BS 1009 TO BS 1029, BL 3L AND WL 208 IAW BOEING 737-300 SRM 51-40-02-0G FIG 8. FABRICATED STRAP IAW BOEING 737-300 SRM 51-40-02-0G FIG 1. INSTALLED FABRICATED REPAIR PARTS AT BS 1009 TO BS 1029, BL 3L AND WL 208 IAW BOEING 737-300 SRM 51-40-02-0G FIG 3. 2L72 4F RTA16WE 20051019001192005101900119NM 2005 10 19 USAA200510001 120051004A5330 SKIN BOEING737 7374B7 1384702NM BS 757F CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19441US 24812 FOUND 2.25" CRACK FOUND AT BS 727F S-25L. INSTALLED DOUBLER PER SRM 53-00-01 FIG 201. 2L72 4F RTA16WE 20051019001202005101900120NM 2005 10 19 QXEA200501283 120051005A33506519024BG LIGHT DHAV DHC8 DHC8202 2809007NM CABIN INOPERATIVE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09369QX 513 SEA - FORWARD 4" SECTION OF FLOOR PROXIMITY EMERGENCY ESCAPE PATH MARKINGS INOPERABLE. REMOVED AND REPLACED EMERGENCY FLOOR PROXIMITY STRIP. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051019001222005101900122NM 2005 10 19 QXEA200501354 120051014A2840 BULB BOMBDRDHC8 DHC8402 1390042NM INDICATOR BURNED OUT A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09415QX 4081 NR 2 TANK AUX PUMP LIGHT BURNED OUT. SPOILER OUTBD CAUTION LIGHT COMES ON AT 185-190 KTS. MAINTENANCE REMOVED AND REPLACED FCECU AND PERFORMED APPLICABLE OPS TESTS AND FUNCTIONAL TESTS. NO DEFECTS NOTED. REMOVED AND REPLACED NR 2 SPOILER UNLOAD VALVE. PERFORMED APPLICABLE OPS CHECKS. NO DEFECTS NOTED FOR THE NR 2 TANK AUX PUMP LIGHT, MAINTENANCE REPLACED NR 2 TANK AUX PUMP SWITCH LIGHT. NO HELP. REMOVED AND REPLACED ADVISORY CONTROL UNIT IAW Q400 TASK 31-51-06-000-801 AND 31-51-06-400-801. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051019001232005101900123WP 2005 10 19 05FDEA03228 120051005A5712 RIB DOUG DC10 DC1010 3022110WP RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE RT WING FIXED L/E COMPT AT STA XORS 518 ZONE 619 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 1.3 AND 4 VOL I. INSTALL REPAIR ANGLE -38. 2L73 4F A22WE 20051019001242005101900124WP 2005 10 19 05FDEA03229 120051005A5511 RIB DOUG DC10 DC1010 3022110WP ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LT HORIZ STAB TIP INTERNAL SIDE FOUND CRACK 1 INCH LONG ON RIB FROM THE EDGE. STOPPED DRILL CRACK AND INSTALLED REPAIR ANGLE IAW SRM 55-00-01 FIG 2 VOL I. 2L73 4F A22WE 20051019001252005101900125WP 2005 10 19 05FDEA03230 120051005A5512 SKIN DOUG DC10 DC1010 3022110WP ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LT HORIZ STAB LEADING EDGE INBOARD FOUND CRACK 2 INCH LONG ON OUTBOARD EDGE LWR SIDE. STOPPED DRILL CRACK AND INSTALLED REPAIR ANGLE IAW SRM 55-00-01 FIG 2 VOL III. 2L73 4F A22WE 20051019001262005101900126WP 2005 10 19 05FDEA03231 120051005A5730 ACCESS PANEL DOUG DC10 DC1010 3022110WP ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 ACCESS PANEL LT WING 516ET FOUND 2 CRACK ON ANGLE INTERNAL SKIN. REMOVED EXISTING REPAIR AND REPAIR STIFFENERS IAW SRM 51-35-01 PAG 1-13 AND 51-33- 01 PAGE 34-47 AND SRM 57-10-00 FIG 23 VOL I. 2L73 4F A22WE 20051019001272005101900127WP 2005 10 19 05FDEA03232 120051005A5330 SKIN DOUG DC10 DC1010 3022110WP ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 FWD CARGO COMPT FOUND ON STRUCTURE AT STA 1102 X= -57 RT SIDE QTY 1 CRACK LONG HALF INCH. SMOOTH AND BLENDED OUT CRACK IAW SRM 53-00-01 FIG 1A VOL 1. INSTALLED CHANNEL REPAIR IAW SRM 53-00-01 FIG 2 SHEET 2 VOL I. 2L73 4F A22WE 20051019001312005101900131WP 2005 10 19 05FDEA03236 120051005A29102700179 CONTROL VALVE DOUG DC10 DC1010 3022110WP HYD SYSTEM LEAKING A FDEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SO25389FE 46623 RT O/B SLAT CONTROL VALVE LEAKING AT SPLINE SHAFT. REMOVED AND REPLACED RT O/B SLATE CONTROL VALVE IAW DC 10 M/M 27-82-02-2. LEAK CHECK GOOD IAW DC10 M/M 27-82-02-2. 2L73 4F A22WE 20051019001342005101900134NE 2005 10 19 AWXA200501196 220051009A72302607MK2 ACTUATOR AIRBUSA319 A319132 3930340NM IAE V2524 V2524A5 NE NR 1 ENGINE VSV FAULTY A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28813AW113386916 1223 DURING TAKEOFF, AT 70 KNOTS, RECEIVED NR 1 ENG COMPRESSOR VANE FAULT. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE VSV ACTUATOR IAW AMERICA WEST AIRLINES TASK CARD F5M71312. OPERATIONAL CHECKS WERE GOOD. VENDOR CONFIRMED FAILURE. INCOMING TEST REVEALED THE LVDT CONNECTOR SHELL TO MOUNT FLANGE RESISTANCE OUT OF TOLERANCE. ALSO FOUND THE PISTON VELOCITIES, INTERNAL LEAKAGE AND PISTON STROKE TO BE OUT OF CMM LIMITS. THE UNIT WAS REPAIRED AND TESTED IAW CMM 75-32-61 REV.1. 2L72 4F4 FRTA28NM E40NE 20051017002012005101700201EA 2005 10 17 QXEA200501309 120050917A5753 SKIN CNDAIRCL600 CL6002C10 1390015EA TE FLAP CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09617QX 10130 YYC - RIGHT INBOARD FLAP LOWER EXTERIOR SURFACE HAS CHAFED MARKS UNDER THE INBOARD AND OUTBOARD HINGE FAIRINGS. BLENDED OUT DAMAGE IAW CRJ-700 SRM 57-52-101-101-001-A01. MATERIAL LOSS .009" RESTORED FINISH. 2L72 4F RTA21EA 20051017002102005101700210WP 2005 10 17 05FDEA03411 120051012A2460 CSD DOUG DC10 DC1010 3022110WP NR 2 GENERATOR FAILED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25389FE 46623 NR 2 ENGINE GENERATOR WILL NOT COME ON LINE, HAS 0 VOLTS AND 0 FREQUENCES. REMOVED AND REPLACED NR 2 ENGINE CSD IAW DC10 M/M 24-11-09-2. SERVICED NR 2 CSD IAW DC10 M/M 24-10-00. OPS CHECK GOOD IAW DC10 M/M 24-11-09 . 2L73 4F A22WE 20051017002222005101700222EU 2005 10 17 SA05105 120051007A3350321430 BATTERY AIRBUSA321 A321211 3930370EU EMERGENCY LIGHT FAULTY A USAAK NONE L NO TEST ININSP/MAINT 1 EA19172US 1472 TPA - THE L2 DOOR SLIDE EMERGENCY ESCAPE LIGHTS INDICATE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY IN EMERGENCY POWER SUPPLY UNIT 15WL. 2L72 4F RTA28NM 20051017002282005101700228NM 2005 10 17 SWAA053087 120051009A53126546568 BULKHEAD BOEING737 7373H4 1384600NM BS 1016 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED 1/4D CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT DOME CAP, 2 O'CLOCK AND 4 O'CLOCK POSITIONS. REPAIRED WEB PER SWA EA. 2L72 4F RTA16WE 20051017002302005101700230NM 2005 10 17 SWAA053089 120051009A5320BAC1509 FLOOR SUPPORT BOEING737 7373H4 1384600NM BS 859-867 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOOR SUPPORT CORRODED BETWEEN BS 859 TO BS 867, LBL 3.0. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20051017002322005101700232NM 2005 10 17 SWAA053091 120051009A5320BAC1509 FLOOR SUPPORT BOEING737 7373H4 1384600NM BS 859-867 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOOR SUPPORT CORRODED BETWEEN BS 859 TO BS 867, LBL 12.0. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20051017002362005101700236NM 2005 10 17 05FDEA03313 120051008A5260 UPLOCK SWITCH BOEING727 7272D4 138407UNM AIR STAIR MALFUNCTIONED A FDEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO25288FE 21850 AMBER AIRSTAIR LIGHT ON S/O PANEL CAME ON IN FLIGHT. CHECKED A/C ON ARRIVAL, FOUND DOOR UP AND LOCKED. RAN DOOR SEVERAL TIMES. LIGHT STAYED ON ON FIRST TRY. ADJUSTED UPLOCK SWITCH ON LEFT AND RIGHT SIDE UPLOCK SWITCHES, PER AMM 52-62-001-5. OPS CHECK NORMAL. RII:193167 2L73 4F A3WE 20051017002462005101700246 2005 10 17 PIDA20050173 420051009A2210 YAW DAMPER BOEING737 7372K5 138448XNM FAILED A PIDAK NONE O OTHER NRNOT REPORTED 1 SO05250TR 22597 YAW DAMPER WILL NOT ENGAGE. PLACED YAW DAMPER ON MEL 22-3-18. 2L72 4F RTA16WE 20051017002502005101700250EU 2005 10 17 TRBA2005059 120050909A6123 AUTOFEATHER SYS AEROSPATR72 ATR72212A 8680902EU MALFUNCTIONED A TRBAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO29541AT 541 AUTOMATIC TAKEOFF POWER CONTROL SYSTEM (ATPCS) DID NOT ARM DURING TAKEOFF POWER. REPLACED AUTO-FEATHERING UNIT. (K) 2H72 4T RTA53EU 20051018000072005101800007NM 2005 10 18 C1HA200594009 120051017A5320 STIFFENER BOEING727 727290 138408WNM BS 870 CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15294AS 22146 RIGHT MLG WHEEL WELL 870 BULKHEAD VERTICAL STIFFENER CRACKED AT KEELBEAM APU CUTOUT. REMOVED AND REPLACED VERTICAL STIFFENER BS 870 RIGHT WHEEL WELL P/N 65-18636-378 IAW 727 SRM 51-30-2. PERFORMED AT KEELBEAM AREA PNEUMATIC LEAK CHECK, NO LEAKS NOTED IAW B727 MM 36-00. 2L73 4F A3WE 20051018000142005101800014WP 2005 10 18 DHL2005806525 120050901A5710 CAP DOUG DC8 DC873F 302199FWP RT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH87034 46002 RT SLANT PANEL UPPER CAP CORRODED, STA XFS 95. PERFORMED MAJOR REPAIR. REMOVED FASTENERS, REMOVED CORROSION FROM RT SLANT PANEL UPPER CAP STA XFS 95 IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG 37. PERFORMED DETAIL VISUAL INSP OF REWORKED AREA. NO CRACK NEITHER CORROSION FOUND. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FILLED REMAINING VOIDS ON REWORKED AREAS OF SLANT PANEL CAP WITH FILLER AND BONDED FILLER TO CAP WITH SEALANT IAW DWG U80-R21. FABRICATED EXTERNAL REPAIR DOUBLER IAW DWG U80-R21. CLEANED, TREATED AND PRIMED EXTERNAL REPAIR DOUBLER INNER FACE. APPLIED SEALANT TO FAYING SURFACES. INSTALLED EXTERNAL REPAIR DOUBLER. 2L74 4F RT4A25 20051018000172005101800017CE 2005 10 18 DXTA200501024 120051015A3240GPP125073 PRESSURE SWITCH CESSNA560 560XL 2076702CE BRAKES INOPERATIVE E DXTAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07631QS 5605131 WHILE ON THE TAXIWAY WITH THE PARKING BRAKE SET THE MASTER CAUTION ILLUMINATED WITH THE LOW BRAKE PRESS AND ANTI-SKID INOP ANNUNCIATORS ILLUMINATED. THE BRAKES FAILED AND HAD TO USE THE EMERGENCY PNEUMATIC BRAKE TO STOP ROLLING. ACCOMPLISHED SEVERAL OPERATIONAL CHECKS OF BRAKE SYSTEM. FOUND BRAKE PACK TO OPERATE AT 1200 PSI AND TURN OFF AT 1500 PSI. REPLACED PRESSURE SWITCH S/N 011 AS A PRECAUTION. REMOVED SWITCH. INSTALLED A REPAIRED SWITCH. LEAK AND OPS CHECK WAS FOUND TO BE SATISFACTORY. ACCOMPLISHED IAW CE560XL MM 32-42-06. ACCOMPLISHED BLEEDING OF ANTI-SKID BRAKE SYSTEM IAW CE560XL MM 32-40-00. SERVICED EMERGENCY GEAR AND PNEUMATIC BRAKE BOTTLE IAW CE560XL MM 12-13-01. 2L72 4F RTA22CE 20051018000242005101800024NM 2005 10 18 SB05134 120051016A335020131A BATTERY PACK BOEING737 7374B7 1384702NM AFT CABIN DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19426US 24548 CLT - DURING OPERATIONAL TEST OF EMERGENCY LIGHT SYSTEM, MAINTENANCE REPORTED THE AFT ENTRY DOOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT ENTRY DOOR EMERGENCY EXIT LIGHT BATTERY PACK PER MM 33-51-51. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20051018000302005101800030NM 2005 10 18 QXEA200501350 120051014A33506104781 BATTERY PACK DHAV DHC8 DHC8202 2809007NM EMERGENCY LIGHTSMALFUNCTIONED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09355PH* 87 500 PDX - EMERGENCY LIGHTS AT CABIN CENTER OVERHEAD, AFT OVERHEAD AND OUTSIDE RIGHTHAND AFT ARE INOP. REPLACED NR 4 EMERGENCY BATTERY PACK AND PERFORMED OPERATIONAL TEST OF THE EMERGENCY LIGHTS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051018000312005101800031NM 2005 10 18 QXEA200501351 120051017A33506104781 BATTERY PACK DHAV DHC8 DHC8202 2809007NM EMERGENCY LIGHTSMALFUNCTIONED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09361PH* 75 520 PSC - EMERGENCY LIGHT AT MAIN CABIN EXIT THRESHOLD AND LEFT FORWARD EGRESS ARE INOP. REPLACED EMERGENCY BATTERY PACK AT 3351-PS1 AND COMPLIED WITH TEST OF EMERGENCY LIGHT IAW MM TASK 33-51-01-710-801. OPERATION TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051018000362005101800036EA 2005 10 18 VTZA200500211 120051013A274170609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB TRIM FAILED A VTZAO OTHER F FLT CONT AFFECTED CRCRUISE 1 EA27697BR5536 7787 MACH/STAB TRIM FAILED SHORTLY AFTER TAKEOFF. REPLACED HORIZONTAL STABILIZER TRIM CONTROL UNIT. 2L72 4F RTA21EA 20051018000402005101800040WP 2005 10 18 UPS05845612 120050830A53135750198501 LONGERON DOUG DC8 DC873F 302199FWP BS 863-871 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE:C3 LONGERON 24L CRACKED IN BATHTUB STA 863-871. REMOVED AND REPLACED LONGERON 24L IAW UPS EO DC8-5310-22823-A AND SAA SK 801-804705. 2L74 4F RT4A25 20051018000412005101800041WP 2005 10 18 UPS05845613 120050830A5512 SKIN DOUG DC8 DC873F 302199FWP HORIZONTAL STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 INSPECTION TYPE:C3 EXFOLIATING CORROSION AROUND FASTENER HOLE ON THE LT HORIZONTAL L/E AS MARKED ON TOP SURFACE. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW SAA SK 801-804772 . 2L74 4F RT4A25 20051018000432005101800043EA 2005 10 18 COMA0560553 120051013A2760 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01451CA 7562 FLIGHT 5045- FLIGHT SPOILER FAULT. DEFERRED MAINTENANCE PER MEL. 2L72 4F RTA21EA 20051018000502005101800050EU 2005 10 18 TRBA2005060 120050910A2612 FIRE WARNING AEROSPATR72 ATR72212 8680945EU NR 1 ENGINE FALSE INDICATIONA TRBAF ACTIVATE FIRE EXT. N FALSE WARNING TXTAXI/GRND HDL 1 SO294AE 244 WHILE ON GROUND, NR 1 ENGINE FIRE INDICATION CAME ON. ENGINE SHUT-DOWN AND FIRE EXTINGUISHER DISCHARGED. VISUAL INSPECTION, NO EVIDENCE OF FIRE NOTED. REPLACED FIRE EXTINGUISHER BOTTLE. (K) 2H72 4T RTA53EU 20051018000562005101800056WP 2005 10 18 UPS05845597 120051005A5320 ANGLE DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE:C2 ANGLE CRACKED ON FWD SIDE OF APB AT L6L. REMOVED ANGLE AT FWD SIDE OF AFT PRESS BULKHEAD IAW SRM 51-1-21. FABRICATED AND INSTALLED ANGLE ON FWD SIDE OF APB AT L6L IAW DWG 5773844 AND SRM 51-1-20D. 2L74 4F RT4A25 20051018000572005101800057WP 2005 10 18 UPS05845598 120051006A534037558452N FITTING DOUG DC8 DC873F 302199FWP BS 1180 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE:C2 C PIT INTERGRANULAR CORROSION ON BATH TUB FITTING AT STA 1180 L35L . REMOVED BATHTUB FITTING AT STA 1180 L35L IAW SRM 51-1-20D AND 51-1-21. REPLACED BATH TUB FITTING AT STA 1180 L35L IAW SRM 53-2-0 FIG 2D AND SRM 51-1-8. 2L74 4F RT4A25 20051018000702005101800070NM 2005 10 18 SWAA053168 120051011A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29471WN 32471 EEPLS TRACK LOOSE AT ROW 1. REMOVED AND REPLACED EEPLS PER MM. 2L72 4F RTA16WE 20051018000752005101800075WP 2005 10 18 05FDEA03330 120051010A5712 RIB DOUG DC10 DC1010 3022110WP RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE RIGHT WING FIXED LEADING EDGE AT STA XORS 655 ZONE 625 FOUND RIB CRACK. REPAIRED FORMER INSTALLED REPAIR ANGLE -36 AND SRM 57-20-00 FIG 1 SHEET 1, 3, 4 VOL 1. 2L73 4F A22WE 20051018000962005101800096NM 2005 10 18 05FDEA03327 120051009A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 RT HORIZ STAB BARREL NUT BORE NR 34 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 44. MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20051018001012005101800101SO 2005 10 18 RAIA00510014 120051011A3397 CONNECTOR EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT LOOSE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03808HK 145157 POST FLIGHT INSPECTION, EXIT ROW EMERGENCY LIGHT OUT. MAINTENANCE RESECURED A LOOSE CONNECTOR. 2L72 4F RTT00011AT 20051018001242005101800124NM 2005 10 18 05FDEA03201 120051004A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 HORIZ STAB LT BARREL NUT BORE NR 27 FOUND WITH CORROSION. REWORK/ REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 32. MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20051018001372005101800137EU 2005 10 18 05FDEA03193 120051003A5712 RIB AIRBUS300 A300F4605R 3930327EU LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25655FE16915 742 LT NR 5 SPOILER, LT CENTER HINGE, HINGE PIN HEAD HAS ROTATED AND CRACKED THE FLANGE OF THE SUPPORT RIB ABOVE IT. VIEW FROM TOP OF WING THROUGH ACCESS PANEL BETWEEN CENTER HINGES. FABBED AND INSTALLED ANGLE AND STOP BLOCKS IAW EA NR 6-5710-91294. 2L72 4F RTA35EU 20051018001672005101800167EU 2005 10 18 SA05108 120051009A2120 ODOR AIRBUSA319 A319112 3930323EU CABIN DETECTED A USAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA19746UW 1297 CLT - FLT 9163 - EN ROUTE FLL TO CLT, DURING THE FERRY FLIGHT TO CLT, AN OIL ODOR BECAME PRESENT IN THE CABIN. FLIGHT CONTINUED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE APU PNEUMATICS SYSTEM INGESTING OIL FROM AN APU STARTER LEAK. REPLACED THE APU STARTER ASSEMBLY. REPLACED THE RIGHT SIDE PRIMARY AND SECONDARY HEAT EXCHANGERS DUE TO OIL CONTAMINATION. RAN THE ENGINES AND AIR CONDITIONING PACKS. OPERATIONALLY CHECKS OK. REMOVED THE APU PNEUMATICS MEL. 2L72 4F RTA28NM 20051018001712005101800171EU 2005 10 18 YENA200571 120051002A2133VFT300B00 OUTFLOW VALVE AIRBUS320 A320232 3930326EU CABIN PRESSURE FAILED A YENAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA15509JB12150330 1270 VENT SKIN VALVE FAULT ON T/O ROLL, ABOUT 60 KTS. REMOVED AND REPLACED SKIN AIR OUTLET VALVE IAW AMM 21-26-53. OPS OK. 2L72 4F RTA28NM 20051018001762005101800176SO 2005 10 18 CHQA200500180 120051016A2120 SMOKE EMB 135 EMB135LR 3260305SO CABIN DETECTED A CHQAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 GL11832RP 145676 FLIGHT 6241 FLL-GSO - CREW REPORTS SMOKE IN CABIN WITH PACK HEAT ON ALONG WITH BITS OF INSULATION COMING OUT OF DUCTS. ON SITE CONTRACT MAINTENANCE REPORTS, WITH JUST THE NR 1 PACK HEAT ON, CABIN HAS SMOKE AND SMELLS LIKE BURNED RUBBER WITH BITS OF INSULATION BEING BLOWN INTO CABIN. AIRCRAFT IS TO BE FERRIED TO IAD WITH OUTFLOW VALVES SECURED OPENED. 2L72 4F RTT00011AT 20051018001832005101800183EA 2005 10 18 A6WA200540305 120050920A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE BS 621 CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31425AW 7663 RIGHT FS 621 FLOORBEAM ANGLE CRACKED. REPAIRED RT FS 621.00 FLOOR SUPPORT ANGLE IAW REO. (M) 2L72 4F4 FRTA21EA E15NE 20051018001842005101800184WP 2005 10 18 UPS05845545 120050829A5312 BULKHEAD DOUG DC8 DC873F 302199FWP BS 980 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 HEAVY CORROSION ON AFT 980 BULKHEAD LT WW OB CORNER ABOVE LONG 24 LT. REMOVED CORROSION, FABRICATED, AND INSTALLED SHIM IAW SAA SK 801-80457 2. 2L74 4F RT4A25 20051018001982005101800198NM 2005 10 18 05FDEA03360 120051011A5712ARB293114 RIB DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 RT WING FIXED LEADING EDGE INTERNAL RIB ANGLE FOUND CRACKED AT XORS 482. REMOVED AS PER SRM 51-31-01 VOLUME II. NEW RIB ANGLE FABRICATED AS PER DRAWING ARB2931 AND INSTALLED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051018002092005101800209NM 2005 10 18 SWAA053093 120051007A53116546556 FRAME BOEING737 7373H4 1384600NM BS 882 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 882, STR 19L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051018002102005101800210NM 2005 10 18 SWAA053094 120051007A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM BS 827 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 827, BETWEEN LBL 4 TO RBL 4. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051018002252005101800225NM 2005 10 18 05FDEA03248 120051005A5347ADA83901 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 MAIN DECK CARGO COMPARTMENT: LEFT HAND SEAT TRACK FOUND CRACKED AT STATION 939, X=28.5. MAIN DECK CARGO COMPARTMENT: LEFT HAND SEAT TRACK AT STATION 939, X=28.5 REPAIR CARRIED OUT AS PER SRM 53-70-00 VOL I FIG 1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051018002292005101800229NM 2005 10 18 2005UALA01062 120051002A335020131A BATTERY BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29173UA 24380 EMERG EXIT LT INOP AT UPPER DK LT DOOR SIGN. REPLACED BATTERY 2L74 4F4 FRTA20WE E24NE 20051018002312005101800231NM 2005 10 18 2005UALA01064 120051002A335020131A BATTERY BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29173UA 24380 EMERG LTS INOP AT UPPER DK LT DOOR SLIDE ILLUM. REPLACED BATTERY. 2L74 4F4 FRTA20WE E24NE 20051018002332005101800233NM 2005 10 18 2005UALA01066 120051003A33501317 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29180UA 25224 DR 1R REAR EMER DOOR SILL LIGHT INOP. REPLACED LAMP. 2L74 4F4 FRTA20WE E24NE 20051018002352005101800235NM 2005 10 18 2005UALA01068 120051003A3350362624 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE SEAT 4A INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29180UA 25224 EEL LIGHT AT SEAT 4A FWD INOP. REPLACED EEL LIGHT. 2L74 4F4 FRTA20WE E24NE 20051018002422005101800242NM 2005 10 18 2005UALA01088 120051006A3350362624 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29122UA 29168 EMERGENCY LIGHT INOP AT SEAT 47 HJK, SEAT 5F AFT, SEAT 5J AFT, SEAT 23AB AFT, SEAT 24AB AND SEAT 58ABC. REPLACED EEL LAMP. 2L74 4F4 FRTA20WE E24NE 20051019000022005101900002NM 2005 10 19 2005UALA01122 120051010A5315 FLOORBEAM BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE BS 294 CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29919UA 25386 CABIN FLOORBEAM AT STA 294 RBL 38 TO RBL 39 AT WL 208 CORRODED AT BOLT HOLES. REMOVED CORROSION & FOUND BLEND OUT OF LIMITS. FABRICATED & INSTALLED REPAIR STRAP PER SRM 53-00-51 REPAIR NR 3. 2L72 4F4 FRTA16WE E2GL 20051019000042005101900004NM 2005 10 19 2005UALA01123 120051010A5311 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE BS 400 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29919UA 25386 CABIN FRAME CRACKED AT STA 400 BETWEEN STRINGER 8L AND 9L AT STOW BIN RAIL ATTACH. REMOVED DAMAGE PER MM 53-10-84. NDT TO VERIFY NO CRACKS. FABRICATED & INSTALLED NESTED ANGLE REPAIRS & FILLER PER MM 53-10-84. 2L72 4F4 FRTA16WE E2GL 20051019000152005101900015NM 2005 10 19 2005UALA01134 120051012A5311 FRAME BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29646UA 25283 FOUND SMALL AREA OF ELECTRICAL ARCH DAMAGE TO VERTICAL FRAME RT FLANGE APPROX 1.5 INCHES ABOVE BASE. 2L72 4F4 FRTA1NM E24NE 20051019000312005101900031 2005 10 19 PCSA10070501 420051007A3442 RADAR BOEING727 7272D3 138407NNM WX SYSTEM FAILED A PCSAA UNSCHED LANDING O OTHER CRCRUISE 1 SO29804AJ 21021 FLIGHT 0741 DEPARTED MIA & CLIMBED TO CRUISE, CREW REPORTED WEATHER RADAR FLASHED BRIGHT ON THE INDICATOR THEN WENT INOPERATIVE. AIRCRAFT RETURNED BACK TO MIA WITH NO FURTHER INCIDENT & LANDED. MAINTENANCE CHECKED ALL WX RADAR WIRING, ALL WIRING FOUND GOOD, THE WEATHER RADAR RECEIVER TRANSMITTER WAS REMOVED AND REPLACED IAW BOEING 727 MM CH 34-41-00 AND THE WEATHER RADAR INDICATOR WAS REMOVED & REPLACED IAW BOEING 727 MM CH 34-41-01. THE WEATHER RADAR SYSTEM WAS FUNCTIONALLY TESTED IAW BOEING 727 MM CH 34-41-0 AND FUNCTIONALLY CHECKED GOOD. AIRCRAFT WAS RETURNED BACK TO SERVICE. 2L73 4F A3WE 20051019000332005101900033NM 2005 10 19 WRLA2005144 120051011A5101 UNKNOWN DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE UNKNOWN UNKNOWN A WRLAO OTHER G MULTIPLE FAILURE APAPPROACH 1 SO11274 48633 UPON GEAR DOWN HAD A VIOLENT SHUDDER LIKE ACFT HIT SOMETHING & LOUD NOISE, THEN COULD NOT GET RT MLG DOWN ON PRIMARY OR SECONDARY SYS. LOST NR 1 TRANSPONDER, INTERMITTENT LOSS OF OTHER SYS: AUTO FLT, CAC, ETC. MLG HELD AT LANDING BUT STILL HAVE RED MLG LIGHTS AND ANTISKID FAIL. REMOVED & REPLACED RT MLG RETRACT CYLINDER AND RH MLG DOWN-LOCK CYLINDER PER MM PROCEDURES. ALSO REMOVED & REPLACED BOTH PRIMARY AND SECONDARY SENSORS AND ACCOMPLISHED GEAR SWING IAW MM PROCEDURES. ACCOMPLISHED ERA 05-32-075 NDT INSPECTION ON THE AFFECTED AREA BEFORE DEPARTURE, NO DEFECTS FOUND. 2L73 4F4 FRTA22WE E24NE 20051019000572005101900057EU 2005 10 19 RAIA00510008 120051004A3397 WIRE AEROSPATR42 ATR42300 8680920EU EMERGENCY LIGHT LOOSE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03426TE 228 PREFLIGHT INSPECTION - STL - EMERGENCY LIGHTING INOP AT SEAT 10-13. MAINTENANCE RESECURED LOOSE CONNECTION AT FLOOR STRIP LIGHT ASSY. 2H72 4T RTA53EU 20051019000662005101900066NM 2005 10 19 SWAA053195 120051016A53156545812 FLOORBEAM BOEING737 7375H4 138449DNM BS 328 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 328, RBL 21, RBL 28 & RBL 36. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20051019000782005101900078SO 2005 10 19 SWIA200515633 120050929A2731 TRIM SWITCH EMB 120 EMB120ER 3260203SO ELEVATORS INOPERATIVE A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07581SW 120349 "TRIM FAIL" WARNING WHEN USING CAPTIANS TRIM SWITCH. REPLACED CAPTIANS TRIM SWITCH. OPERATIONAL CHECK GOOD IAW MM 22-10-00. 2L72 4T RTA31SO 20051019000912005101900091 2005 10 19 SWAA053036 420051003A256565C16820 HOOK BOEING737 7373H4 1384600NM R2 DOOR SLIDE OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29355SW 25250 R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOKS OUT OF ADJUST. ADJUSTED GIRT BAR HOOKS PER MM. 2L72 4F RTA16WE 20051019000922005101900092NM 2005 10 19 SWAA053037 120051003A3350207377 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29402WN 29814 EEPLS LENS MISSING AT FWD END. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20051019001032005101900103NM 2005 10 19 05FDEA03244 120051005A5347 SEAT TRACK BOEING727 727225 1384077NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25465FE 21289 SEAT TRACK AT LBL 45 STA 690-740 IS CORRODED. REMOVED, FABRICATED, ALODINED, PRIMED AND INSTALLED NEW SEAT TRACK FROM STA 680-740 AT LBL45 ALL IAW FX B727-200 SRM 53-10-5,53-10-1 FIG 3, 51-30-2 AND 51-10-2. 2L73 4F A3WE 20051019001152005101900115WP 2005 10 19 05FDEA03243 120051005A5330 SKIN DOUG DC10 DC1010 3022110WP BS 1480-1521 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25389FE 46623 CENTER GEAR WELL BILGE AREA LIGHT CORROSION ON SKIN AND DETERIORATED PAINT FS 1480 TO FS 1521. REPAIRED AREA IAW FEDEX EA 8-5330-91291, N/R N00316. 2L73 4F A22WE 20051019001182005101900118NM 2005 10 19 AWXA200501171 120050910A5330654577885 SKIN BOEING737 7373G7 1384595NM BS 944 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 MCN - DURING C16 CHECK DISCOVERED FUSELAGE SKIN CRACKED .5 INCHES AT BS 944.5, STRINGER 24R. MAINTENANCE TRIMMED OUT CRACKED SECTION OF FUSELAGE SKIN IAW BOEING 737-300 SRM 53-00-01-2A FIG 201. FABRICATED DOUBLER, TRIPLER AND STRUCTURAL FILLERS IAW BOEING 737-300 SRM 53-00-01-2R. INSTALLED FABRICATED REPAIR PARTS AT BS 944.5 AND STRINGER 24R IAW BOEING 737-300 SRM 53-00-01-2R FIG 201. 2L72 4F RTA16WE 20051019001282005101900128WP 2005 10 19 05FDEA03233 120051005A5320 WEB DOUG DC10 DC1010 3022110WP ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 COCKPIT FOUND 1 CRACK 2" LONG ON WEB AT STA 304 X=-27 Z= -2.925 AND MODERATE CORRSION AT STA 313 X=-39 Z=-2.925. REMOVED CORROSION IAW SRM 51-21-01 AND PROTECT AREA IAW SRM 51-21-01. CUT DAMAGED PORTION OF WEB AND REPAIRED IAW SRM 53-00-01 FIG 4 SHEET 2. 2L73 4F A22WE 20051019001302005101900130WP 2005 10 19 05FDEA03235 120051005A5330 SKIN DOUG DC10 DC1010 3022110WP ZONE 100 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 NOSE AREA RT SIDE BETW Y=285 AND Y=295 UNDER LONGERON 27 FOUND 1 DENT 0.512"X0.043") ON SKIN. REPAIRED DENT IAW SRM 51-10-00 VOL II. PERFORMED NDI INSPECTION: FOUND OK AND INST DOUBLER IAW SRM 53-20-00 VOL 1 FIG 13 SHEET 5. 2L73 4F A22WE 20051019001322005101900132WP 2005 10 19 05FDEA03237 120051005A29102700179 CONTROL VALVE DOUG DC10 DC1010 3022110WP HYD SYSTEM LEAKING A FDEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SO25389FE 46623 EVIDENCE OF HYDRAULIC LEAK AT I/B SLAT CONTROL VALVE IN CAC COMPARTMENT. REMOVED AND REPLACED I/B SLATE CONTROL VALVE IAW DC10 M/M 27-82-02-2. LEAK CHECK GOOD IAW DC10 M/M 27-82-02-2. 2L73 4F A22WE 20051019001332005101900133NM 2005 10 19 AWXA200501195 120050921A5753 SKIN BOEING737 7373S3 1384711NM ZONE 600 - RIGHTDEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 DURING C18 CHECK DISCOVERED DISBOND AREA ON THE UPPER AND LOWER SURFACE OF THE RT INBOARD AFT FLAP, FROM WS 230.68 TO WS 236.68. MAINTENANCE REMOVED DISBONDED SKIN AND PREPPED REPAIR AREA IAW BOEING 737-300 SRM 51-70-10-2R4 FIG 202. FABRICATED DOUBLER AND FILLER IAW BOEING 737-300 SRM 51-70-10-2R4. BONDED REPAIR PARTS TO THE UPPER AND LOWER SURFACE OF THE RT INBOARD AFT FLAP, FROM WS 230.68 TO WS 236.68 IAW BOEING 737-300 SRM 51-70-10-2R4 FIG 202. 2L72 4F RTA16WE 20051019001352005101900135NM 2005 10 19 SWAA053201 120051016A53306545776 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051020000012005102000001EA 2005 10 20 MASA200500438 120050603A2711 TRIM SYSTEM CNDAIRCL600 CL6002D24 1390016EA MALFUNCTIONED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07934FJ 15034 THE CREW ABORTED TAKEOFF ROLL DUE TO A TRIM MISCONFIGURATION FAULT. AS THE SPEED DECREASED THE CREW REPORTED THE FAULT CLEARED. MX PERFORMED OPERATIONAL CHECKS OF THE TRIM SYSTEMS AND FOUND THE SYSTEMS TO BE FUNCTIONING NORMALLY. 2L72 4F RTA21EA 20051020000062005102000006NM 2005 10 20 72400009 120050929A5313 STRINGER BOEING727 727225 1384077NM FUSELAGE CRACKED A K11AK NONE O OTHER ININSP/MAINT 1 GL23724CK 20383 CRACKS ON STRINGER RIB FLANGE. 2L73 4F A3WE 20051020000082005102000008NM 2005 10 20 724000011 120050929A5311 FRAME BOEING727 727225 1384077NM FUSELAGE CRACKED A K11AK NONE O OTHER ININSP/MAINT 1 GL23724CK 20383 CRACK IN FUSELAGE FRAME SUPPORT. 2L73 4F A3WE 20051020000092005102000009NM 2005 10 20 724000012 120050929A5311 FRAME BOEING727 727225 1384077NM FUSELAGE DENTED A K11AK NONE O OTHER ININSP/MAINT 1 GL23724CK 20383 DENT ON FUSELAGE FRAME FLANGE. 2L73 4F A3WE 20051020000112005102000011NM 2005 10 20 724000014 120051005A5330 DOUBLER BOEING727 727225 1384077NM FUSELAGE NICKED A K11AK NONE O OTHER ININSP/MAINT 1 GL23724CK 20383 NICK IN DOUBLER. 2L73 4F A3WE 20051020000132005102000013NM 2005 10 20 724000016 120051005A5310 STRUCTURE BOEING727 727225 1384077NM FUSELAGE CRACKED A K11AK NONE O OTHER ININSP/MAINT 1 GL23724CK 20383 CRACK IN LOWER CHORD. 2L73 4F A3WE 20051020000142005102000014EA 2005 10 20 MASA200500263 120050331A2700 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA INTERMITTENT A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07503MJ 10058 ASH 7289 DSM-DEN. THE AIRCRAFT ABORTED TAKEOFF AND RETURNED TO THE GATE WITH GLD UNSAFE MSG. MAINTENANCE WAS CALLED AND THE PROBLEM SEEMED TO BE INTERMITTENT. SECURED THE SYSTEM IN THE OFF MODE AND FERRIED THE AIRCRAFT TO TUS FOR REPAIR. 2L72 4F RTA21EA 20051020000152005102000015EA 2005 10 20 MASA200500655 120050819A3350316 LIGHT CNDAIRCL600 CL6002C10 1390015EA CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07507MJ 10077 ASH 7118 IAD. DURING PREFLIGHT CREW FOUND ONE CEILING EMERGENCY FLOOD LIGHT INOP. REPLACED LIGHT. 2L72 4F RTA21EA 20051020000182005102000018NM 2005 10 20 SWAA053216 120051017A26126554499 MODULE BOEING737 7373Y0 1384671NM FIRE WARNING ERRATIC A SWAAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW29308SA 23498 FIRE WARNING BELL SOUNDED & AMBER MASTER CAUTION LIGHT ILLUMINATED. REMOVED AND REPLACED AURAL WARNING MODULE PER MM. 2L72 4F RTA16WE 20051020000222005102000022NM 2005 10 20 SWAA053220 120051017A53116546555 FRAME BOEING737 7373H4 1384600NM BS 867 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051020000242005102000024NM 2005 10 20 SWAA053222 120051017A53116546551 FRAME BOEING737 7373H4 1384600NM BS 807 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051020000252005102000025NM 2005 10 20 SWAA053223 120051017A53116546550 FRAME BOEING737 7373H4 1384600NM BS 787 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051020000282005102000028NM 2005 10 20 SWAA053226 120051017A53116546526 FRAME BOEING737 7373H4 1384600NM BS 400 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051020000302005102000030EA 2005 10 20 MASA200500262 120050330A2741 TRIM SYSTEM CNDAIRCL600 CL6002D24 1390016EA STAB FAILED A MASAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 SW07906FJ 15006 ASH 6532 ONT - LAS. THE AIRCRAFT HAD A TOTAL STAB/MACH TRIM FAILURE IN FLIGHT. MAINTENANCE RESET THE SYSTEM AND DID A COMPLETE OPS CHECK OF WHICH CHECKED NORMAL. 2L72 4F RTA21EA 20051020000322005102000032EA 2005 10 20 MASA200500712 120050907A2711AL00102 ACTUATOR CNDAIRCL600 CL6002C10 1390015EA AILERON TRIM MALFUNCTIONED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07508MJ18 18 10087 ASH 7129 PWM. ABORTED T/O FOR REPEAT AILERON CONFIG WARNING MESSAGE. MAINTENANCE REMOVED AND REPLACED THE AILERON TRIM ACTUATOR. 2L72 4F RTA21EA 20051020000342005102000034EA 2005 10 20 MASA200500773 120051005A2711AL00102 ACTUATOR CNDAIRCL600 CL6002C10 1390015EA AILERON TRIM MALFUNCTIONED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07508MJ170 170 10087 ASH 7134 MCI. CONFIG TRIM MSG. AIRCRAFT FERRIED TO CLT WHERE MAINTENANCE REMOVED AND REPLACED THE TRIM ACTUATOR. 2L72 4F RTA21EA 20051020000352005102000035EA 2005 10 20 MASA200500794 120051011A2711601A516703 CIRCUIT BOARD CNDAIRCL600 CL6002C10 1390015EA AILERON TRIM SYSFAILED A MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW07508MJ 10087 ASH 7036 ORD. AILERON TAKEOFF CONFIG WARNING. R2 POWER SUPPLY & BOARD ASSY. 2L72 4F RTA21EA 20051020000362005102000036EA 2005 10 20 MASA200500811 120051016A2711 DCU CNDAIRCL600 CL6002C10 1390015EA AILERON TRIM SYSMALFUNCTIONED A MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW07508MJ 10087 ASH 7134 MCI. AILERON TRIM WARNING MESSAGE. R2 NR 1 DCU. 2L72 4F RTA21EA 20051020000382005102000038EA 2005 10 20 MASA2005465 120050613A335020131A BATTERY PACK CNDAIRCL600 CL6002D24 1390016EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07906FJ4231 15006 ASH 6340 PHX - CAPTAIN REPORTED EMERGENCY EXIT LIGHTS AT ROW 15, BOTTOM SIDEWALL INOP. MX TROUBLESHOT TO BAD EMERG BATTERY PACK. REPLACED THE BATTERY PACK LOCATED AT ROW 17 AND IT OPS CHECKED GOOD. 2L72 4F RTA21EA 20051020000392005102000039NM 2005 10 20 SWAA053228 120051017A3297655825029 CIRCUIT CARD BOEING737 7373H4 1384600NM MLG FAULTY A SWAAO OTHER J WARNING INDICATION CLCLIMB 1 SW29330SW 23694 RED UNSAFE LT MLG LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. RECYCLED GEAR HANDLE AND RED UNSAFE LIGHT EXTINGUISHED. REMOVED AND REPLACED MLG RED LIGHT SWITCH PC CARD M986 PER MM. 2L72 4F RTA16WE 20051020000402005102000040SO 2005 10 20 C2XA05IA109 120051004A26117013348948 DAU EMB 145 EMB145XR 3260214SO NR 2 INOPERATIVE A C2XAO OTHER J WARNING INDICATION CRCRUISE 1 SW27161831097 1097 14500914 IAH - FLIGHT 3097, THE CREW REPORTED A BAGGAGE SMOKE INDICATION IN FLIGHT WITH NO ASSOCIATED SMOKE NOTICED IN THE BAGGAGE COMPARTMENT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NR 2 DAU, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20051020000412005102000041WP 2005 10 20 AALA20050677 120051017A3350 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21598AA 53288 SFO - EMERGENCY LIGHTS FROM FLIGHT ATTENDANT STATION NR 1 INOPERATIVE. RECONNECTED BATTERY PACK B549 FOR EMERGENCY LIGHTS FROM FLIGHT ATTENDANT STATION NR 1. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20051020000432005102000043WP 2005 10 20 AALA20050683 120051014A30002028TP DUCT DOUG DC9 DC982 3022082WP ANTI-ICE SYSTEM LOOSE A AALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW2116545 53027 LAX - INFLIGHT DURING CLIMBOUT AT 4000 MEAN SEA LEVEL, LEFT ENGINE FIRE WARNING LIGHT ILLUMINATED. QUICK REFERENCE HANDBOOK PROCEDURES COMPLETED. SHUT DOWN ENGINE. NO BOTTLE FIRED. RETURNED TO LAX AND LANDED SINGLE ENGINE LANDING WITHOUT INCIDENT. FOUND DUCT SECTION LOOSE IN LEFT HAND COWL. REPLACED ANTI ICE DUCT ON LEFT HAND ENGINE UPPER COWL. 2L72 4F A6WE 20051020000442005102000044NM 2005 10 20 AALA20050679 120051015A3350P4010051112 MODULE BOEING767 767223 1385123NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21324AA 22325 LAX - SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 31 TO 40AB INOPERATIVE. REPLACED POWER SUPPLY AND BATTERY PACK MODULE FOR SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 31 TO 40AB. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20051020000452005102000045EU 2005 10 20 AALA20050681 120051014A3232 ACTUATOR AIRBUS300 A300B4605R 3930308EU MLG INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2150051 459 INFLIGHT UPON RETRACTION OF GEAR ON TAKEOFF GOT ECAM LANDING GEAR SYSTEM FAULT. EXCESSIVE NOISE, ELECTED TO PUT GEAR DOWN AND GOT THREE GREEN. NO DOOR LIGHTS. ELECTED TO ONCE AGAIN RETRACT GEAR RESULTING IN GEAR UP NO FAULT OR DOOR LIGHTS UNTIL GEAR HANDLE WAS PLACED IN NEUTRAL OR MID POSITION. AT THAT TIME NOISE RETURNED WITH NO AMBER LIGHTS. FOUND LEFT NOSE GEAR DOOR ACTUATOR LOCK TAB BROKEN. THE ACTUATOR ROD END LENGTHENED DUE TO THE SHAFT ROTATION. DOOR WOULD NOT CLOSE PROPERLY. REPLACED LEFT HAND NOSE GEAR DOOR ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20051020000462005102000046NM 2005 10 20 AALA20050684 120051012A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21914AN 29515 TUL - BATTERY PACKS IN FIRST CLASS SEATS, AFT GALLEY, AND RIGHT HAND FORWARD COACH INOPERATIVE. REPLACED BATTERY PACKS IN FIRST CLASS SEATS, AFT GALLEY, AND RIGHT HAND FOWARD COACH. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20051020000472005102000047NM 2005 10 20 AALA20050685 120050928A5414 SKIN BOEING767 767223 1385123NM LT PYLON DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21323AA 22324 AFW - LEFT HAND PYLON STRUT SKIN ON INBOARD AND OUTBOARD SIDE HAD GOUGE CAUSED BY THRUST REVERSER SEAL RETAINER BETWEEN STATION 244 TO 250 AND WATER LINE 195. DAMAGED AREA WAS 5 INCH BY 7 INCH AND 0.053 INCH DEEP. BLENDED DAMAGE AND PERFORMED HIGH FREQUENCY EDDY CURRENT OF REWORKED AREA. VERIFIED USING NDT METHODS. ENSURE THICKNESS WITHIN LIMITS. REMOVED SOURCE OF WEAR FROM THRUST REVERSER BY PERFORMING A RIG AND SHIM OF THE THRUST REVERSER. 2L72 4F RTA1NM 20051020000482005102000048NM 2005 10 20 AALA20050686 120051007A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21949AN 29537 TUL - BATTERY PACKS FOR EMERGENCY LIGHTS FOR COACH AND FIRST CLASS SEATS INOPERATIVE. REPLACED BATTERY PACK AT STATIONS 727, 559, 947.5, AND 328 FOR EMERGENCY LIGHTS IN COACH AND FIRST CLASS SEATS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20051020000492005102000049WP 2005 10 20 AALA20050678 120051018A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21290AA 49302 ORD - OVERWING FORWARD RIGHT AND LEFT HAND EMERGENCY EXIT UPPER EXIT SIGNS INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING FORWARD RIGHT AND LEFT HAND EMERGENCY EXIT UPPER EXIT SIGNS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051020000502005102000050NM 2005 10 20 AALA20050680 120051016A3350 WIRE BOEING757 757223 1384957NM EMERGENCY LIGHT PINCHED A AALAO OTHER O OTHER CRCRUISE 1 SW21613AA 24489 LAX - INFLIGHT NUMBER 4 RIGHT AND LEFT EMERGENCY LIGHT INTERMITTENT DURING FLIGHT. FOUND 4L FORWARD EXIT LIGHT ASSEMBLY WITH PINCHED WIRING. REPAIRED WIRING AND REPLACED 4L FORWARD EXIT ASSEMBLY FOR 4 RIGHT AND LEFT EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20051020000522005102000052NM 2005 10 20 AWXA200501228 120050923A53156545410129 FLOORBEAM BOEING737 7373S3 1384711NM BS 727B CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 DURING C18 CHECK DISCOVERED 2 CRACKS, .75 INCHES IN LENGTH, ON FLOORBEAM UPPER CHORD AT BS 727B AND BL 45L. MAINTENANCE TRIMMED OUT CRACK AT BS 727B AND BL 24L IAW AMERICA WEST AIRLINES ENGINEERING REQUEST NR 03-4702-05280-DF1. FABRICATED FILLER, REPAIR STRAPS AND SHIMS IAW AWA ER NR 03-5702-05280-DF1. INSTALLED FABRICATED REPAIR PARTS AT BS 727B AND BL 45L IAW AWA ER NR 03-5702-05280-DF1. 2L72 4F RTA16WE 20051020000552005102000055NM 2005 10 20 AWXA200501231 120050921A53136546877143 STRINGER BOEING737 7373S3 1384711NM BS 727 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 DURING C18 CHECK DISCOVERED CRACK, 1.7 INCHES IN LENGTH, AT STRINGER 18A ON WEB JUST FORWARD OF BS 727. MAINTENANCE TRIMMED OUT CRACK AT BS 727 AND STR 18A IAW AMERICA WEST AIRLINES ENGINEERING REQUEST NR 03-5361-05285-ES1. FABRICATED FILLER AND RADIUS FILLER IAW AWA ER NR 03-5361-05285-ES1. INSTALLED FABRICATED REPAIR PARTS ON WEB AT BS 727 AND STR 18A IAW AWA ER NO. 03-5361-05285-ES1. 2L72 4F RTA16WE 20051020000562005102000056NM 2005 10 20 AWXA200501232 120050924A534069353501 STRINGER CLIP BOEING737 7373S3 1384711NM BS 727D CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 DURING C18 CHECK DISCOVERED EXFOLIATION CORROSION LOCATED AT AFT CARGO COMPARTMENT ON A STRINGER TIE AT BS 727D AND STR 26L. MAINTENANCE REMOVED STRINGER TIE IAW BOEING 737-300 SRM 51-40-02-0G. INSTALLED NEW STRINGER TIE AT BS 727D AND STR 27L IAW BOEING 737-300 SRM 51-40-02-0G. 2L72 4F RTA16WE 20051020000582005102000058NM 2005 10 20 AWXA200501234 120050922A532065617771 CHANNEL BOEING737 7373S3 1384711NM BS 360 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 DURING C18 CHECK DISCOVERED CHANNEL CRACKED, .5 INCHES IN LENGTH, AT STR 15L AND BS 360. MAINTENANCE REMOVED CRACKED CHANNEL IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5310-05285-ES4. FABRICATED NEW CHANNEL IAW DWG 65-61777 AND AWA ER NR 03-5310-05285-ES4. INSTALLED FABRICATED REPAIR PARTS AT STR 15L AND BS 360 IAW AWA ER NR 03-5310-05285-ES4. 2L72 4F RTA16WE 20051020000592005102000059NM 2005 10 20 AWXA200501235 120050928A5322654583312 SHEAR TIE BOEING737 7373S3 1384711NM BS 195 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 DURING C18 CHECK DISCOVERED SHEAR TIE CRACKED, .5 INCHES, AT BS 195, WL 2076 AND BL 33R. MAINTENANCE REMOVED SHEAR TIE AT BS 195, WL 207 AND BL 33R IAW BOEING 737-300 SRM 51-40-02-0G. FABRICATED NEW SHEAR TIE AND INSTALLED AT BS 1295, WL 207 AND BL 33R IAW BOEING 737-300 SRM 51-40-0G FIGS 7, 8 AND 12. 2L72 4F RTA16WE 20051020000612005102000061NM 2005 10 20 AWXA200501237 120050923A531165465269 FRAME BOEING737 7373S3 1384711NM BS 400 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 DURING C18 CHECK DISCOVERED FRAME ANGLE CRACKED, .5 INCHES IN LENGTH, AT BS 400 AND STR 14L. MAINTENANCE TRIMMED OUT CRACK ON FRAME IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5332-05284-HF1. FABRICATED REPAIR ANGLE, SPLICE ANGLE AND FILLER IAW AWA ER NR 03-5332-05284-HF1. INSTALLED FABRICATED REPAIR PARTS AT BS 400 AND STR 14L IAW AWA ER NR 03-5332-05284-HF1. 2L72 4F RTA16WE 20051020000622005102000062NM 2005 10 20 AWXA200501238 120050923A53406546816 ATTACH ANGLE BOEING737 7373S3 1384711NM BS 927-947 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 DURING C18 CHECK DISCOVERED ATTACH ANGLE CRACKED, .375 INCHES IN LENGTH, FROM BS 927 TO BS 947, WL 207 AND BL 0. MAINTENANCE REMOVED CRACKED ATTACH ANGLE IAW BOEING 737-300 SRM 51-40-02-0G. FORMED NEW ATTACH ANGLE IAW BOEING 737-300 SRM 51-30-01-0G. INSTALLED FABRICATED REPAIR PARTS AT BS 927 TO BS 947, WL 207 AND BL 0 IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 8 AND 12. 2L72 4F RTA16WE 20051020000642005102000064NM 2005 10 20 SWAA053229 120051017A53306545765 SKIN BOEING737 7373H4 1384600NM BS 500D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29359SW 26596 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 10L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051020000652005102000065NM 2005 10 20 SWAA053230 120051012A2120214A30013 CHECK VALVE BOEING737 7377H4 1384404NM A/C BAY FAULTY A SWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SW29405WN 27893 WITH THROTTLES IN IDLE POSITION, STRONG ODOR IN COCKPIT. REMOVED AND REPLACED LT & RT FILTER CHECK VALVES PER MM. 2L72 4F RTA16WE 20051020000662005102000066 2005 10 20 SWAA053231 420051017A256565C16820 HOOK BOEING737 7377H4 1384404NM R1 DOOR GIRT BARLOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29424WN 29828 R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR STOW HOOK LOOSE. SECURED HOOK PER MM. 2L72 4F RTA16WE 20051020000672005102000067NM 2005 10 20 SWAA053232 120051016A53306545775 SKIN BOEING737 7375H4 138449DNM BS 807 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29507SW 24184 DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 807, STR 24L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051020000702005102000070NM 2005 10 20 SWAA053235 120051016A3350101114 COVER BOEING737 7373H4 1384600NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29636WN 27709 DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT COVER CRACKED. REMOVED AND REPLACED COVER PER MM. 2L72 4F RTA16WE 20051020000712005102000071NM 2005 10 20 SWAA053236 120051014A53306545765 SKIN BOEING737 7373Q8 1384670NM BS 500D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 12R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051020000742005102000074NM 2005 10 20 SWAA053239 120051015A53306545774 SKIN BOEING737 7373Q8 1384670NM BS 730 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 730, STR 18R. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20051020000802005102000080EA 2005 10 20 MASA200500235 120050319A2120 SMOKE CNDAIRCL600 CL6002D24 1390016EA CABIN DETECTED A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW07902FJ 15002 ASH 6424 PHX-DSM. CAPT REPORTED SMOKE IN CABIN ON GROUND. MX RAN PACKS AND FOUND NO DEFECTS. MX RETURNED THE A/C TO SERVICE. 2L72 4F RTA21EA 20051020000812005102000081EA 2005 10 20 MASA200500246 120050322A2120 ODOR CNDAIRCL600 CL6002D24 1390016EA CABIN DETECTED A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW07910FJ 15010 THE PILOT REPORTED AN ODOR OF SMOKE IN THE CABIN BUT NO VISUAL. MAINTENANCE PERFORMED AN EXTENSIVE VISUAL INSPECTION AND HIGH POWER ENGINE RUNS AND COULD NOT FIND ANY DEFECTS IN THE SYSTEM. AIRCRAFT CONTINUED REVENUE SERVICE. 2L72 4F RTA21EA 20051020000822005102000082EA 2005 10 20 MASA200500257 120050326A3297 CIRCUIT CARD CNDAIRCL600 CL6002D24 1390016EA MLG MALFUNCTIONED A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07907FJ 15007 CAPTAIN RETURNED TO THE FIELD WHEN AIRCRAFT EXPERIENCED A NOSE LANDING GEAR DISAGREE MASTER WARNING FOLLOWING ATTEMPTED GEAR RETRACTION. MAINTENANCE REMOVED AND REPLACED THE IOC CARD. 2L72 4F RTA21EA 20051020000852005102000085SO 2005 10 20 C2XA05SH119 120051014A5751 SKIN EMB 145 EMB145LR 3260212SO AILERON DELAMINATED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713997 327 145298 SHV - DURING C-CHECK THE LT AILERON HAS TWO AREAS OF DELAMINATION AND CRACKS ON LOWER INNER SKIN AT HINGE POINT. MAINTENANCE REPAIRED THE TWO AREAS OF DELAMINATION AND CRACK ON LOWER INNER SKIN AT HINGE POINT IN THE LT AILERON IAW EC5750-01260. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2L72 4T RTT00011AT 20051020000872005102000087CE 2005 10 20 4513410162005 120051016A32324532103050001 GIMBAL JOINT LEAR 45 45LEAR 5170805CE MLG ACTUATOR SHEARED E J7SAO OTHER K FLUID LOSS APAPPROACH 1 SW05423FX4207 134 ON APPROACH, SELECTED FLAPS 8 THEN 20, FLAPS OPS NORM TO DETENTS. SELECTED MLG DOWN, 3 GREEN DOWN & LOCK, LT MLG DOOR UNSAFE LIGHT ILLUM. SELECTED FLAPS 40. CYCLED MLG, DID NOTHING. DID A GO AROUND & SELECTED FLAPS 8. ON SELECTING FLAPS 8 AN AMBER FLAPS FAULT CAS ILLUM & FLAPS DID NOT MOVE. A FEW SECONDS LATER AN AMBER HYD PRESS CAS ILLUM. SELECTED HYD SYNOPSIS PAGE & LT & RT EDP AMBER & MAIN HYD PRESS SHOWED 40 PSI & AMBER BOXED. DECLARED EMERG & LANDED. LANDING UNEVENTFUL, USED NORMAL BRAKING. NO T/R'S OR SPOILERS AVAILABLE. LT MLG DOOR ACT SEVERED OFF GIMBAL ASSY & SEVERED ACTUATION LINE FROM UPLOCK ACT. SB 45-32-20 ISSUED ADDRESSING PROBLEM. A/C SCHEDULED BUT HAD NOT BEEN COMPLETED. 2L72 4F RTT00008WI 20051020000882005102000088GL 2005 10 20 3002003610120 120051012A3411 PITOT TUBE BOMBDRBD700 BD7001A10 1390006GL PITOT STATIC OBSTRUCTED E J7SAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 SW05516FX 20036 CREW REJECTED THE TAKEOFF ROLL WHEN THE PILOTS AIRSPEED INDICATOR WOULD NOT REGISTER ABOVE 40 KNOTS. MAINTENANCE FOUND PITOT PROBE PARTIALLY OBSTRUCTED. CLEANED OUT PROBE AND PERFORMED PITOT STATIC CHECK. NO FURTHER DEFECTS NOTED. 2L72 4F RTT00003NY 20051020000902005102000090NM 2005 10 20 AWXA200501240 120050924A534069265552 STRINGER CLIP BOEING737 7373S3 1384711NM BS 348 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 DURING C18 CHECK DISCOVERED CLIP CRACKED, .05 INCHES, AT STR 16L AND BS 348. REMOVED CLIP AT STR 16L AND BS 348.1 IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5310-5285-ES5. FABRICATED NEW CLIP AND INSTALLED AT BS 348 AND STR 16L IAW AWA ER NR 03-5310-5285-ES5. 2L72 4F RTA16WE 20051020000952005102000095NM 2005 10 20 05FDEA03430 120051013A5753 HINGE FITTING DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 LEFT WING OUTBOARD FLAP INBOARD HINGE FITTING INBOARD NR 2 BOLT HOLE FROM FORWARD FOUND CORROSION. REPAIR ACCOMPLISHED PER EA 1-5750-93247. 2L73 4F RTA22WE 20051020000972005102000097NM 2005 10 20 05FDEA03432 120051014A5330 SKIN BOEING727 72722 1384002NM BS 465 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 FOUND BS 465 STR 19L HAS A DENT. REPAIRED STR 19L AT BS 465 PER SRM 51-30-2 AND 53-10-3. 2L73 4F A3WE 20051020000982005102000098NM 2005 10 20 05FDEA03433 120051014A5330 SKIN BOEING727 72722 1384002NM BS 368 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 FOUND GOUGE IN SKIN AT STR 20L BS 368. REPAIRED GOUGE IN SKIN AT STR 20L BS 368 PER SRM 53-30-3 FIG 3. 2L73 4F A3WE 20051020000992005102000099NM 2005 10 20 05FDEA03435 120051016A5311 FRAME DOUG MD11 MD11 3023602NM BS 6-30 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 FWD CARGO COMPT AT STA 6-30 RT LOWER FRAME ASSY BETWEEN LONGERON 42 TO LONGERON 43 FOUND CORRODED DURING REMOVAL. FRAME REMOVED AS PER SRM 51-35-01 VOL.II. NEW FRAME FABRICATED AS PER DWG ACA 7049 AND NEW FRAME INSTALLED AS PER SRM 51-35-01 VOL.II. MINOR REPAIR PER GMM 6-2-100. 2L73 4F RTA22WE 20051020001012005102000101EA 2005 10 20 MASA200500174 120050304A274170744 CONTROL UNIT CNDAIRCL600 CL6002D24 1390016EA TRIM SYSTEM FAILED A MASAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW07914FJ 15014 ASH 6092 TUS - DECLARED AN EMERGENCY AND DIVERTED INTO TUS HEADED FOR PHX DUE TO STAB TRIM INOP. MAINTENANCE NOTIFIED TO PULL CVR, FDR CB'S NTSB NOTIFIED AND ACFT WAS RELEASED. MX WILL DOWNLOAD FDR AND REPLACE CVR, MCU AND MACH/STAB TRIM PANEL. WAITING PART INFO, REPLACED MCU. 2L72 4F RTA21EA 20051020001032005102000103NM 2005 10 20 05FDEA03423 120051013A5340 STRINGER CLIP BOEING727 72722 1384002NM BS 440 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 FOUND MAIN CARGO DECK STRINGER CLIP IS DAMAGED AT BS 440, STR 8L. REMOVED AND REPLACED MAIN CARGO DECK STRINGER CLIP BS 440 STR 8L IAW SRM 51-30-2. 2L73 4F A3WE 20051020001052005102000105NM 2005 10 20 05FDEA03425 120051013A5322 SHEAR TIE BOEING727 72722 1384002NM BS 620 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 FOUND BS 620 STR 25 LT DAMAGE AROUND FASTENER ON SHEAR TIE THROUGH SKIN. REMOVED AND REPLACED SHEAR TIE AT BS 620 STR 25 LH IAW SRM 51-10-2, 51-20, AND SRM 51-30-2. 2L73 4F A3WE 20051020001072005102000107EA 2005 10 20 MASA200500444 120050605A2710 WARNING SYSTEM CNDAIRCL600 CL6002D24 1390016EA CONFIGURATION ACTIVATED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07934FJ 15034 ASH 6445 - PHX - AIRCRAFT RTG WITH CONFIG WARNING MESSAGE ON TAKEOFF ROLL. MX TROUBLESHOT AND COULD NOT DUPLICATE THE PROBLEM. 2L72 4F RTA21EA 20051109002782005110900278NM 2005 11 9 AWXA200501242 120051015A7120LM321118V ISOLATOR BOEING737 7373G7 1384595NM ENGINE MOUNT COLLAPSED A AWXAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 WP28158AW1050410504 23780 LAX - AIR TURN BACK - FLT 425 - CREW REPORTED AFTER TAKEOFF VERY PRONOUNCED VIBRATION SHOOK THE AIRCRAFT FROM JUST AFTER ROTATION UNTIL POWER PULLED TO IDLE FOR FINAL DESCENT. AS AIRSPEED INCREASED, VIBRATION INCREASED. IN INTENSITY. CYCLED GEAR WITH NO NOTICABLE EFFECT. ALL ENGINE PARAMITERS WERE NORMAL. VIB INPS NEVER ROSE ABOVE 1.0. NO FLIGHT CONTROL ABNORMALITIES NOTICED. AIRCRAFT PERFORMED NORMALLY EXCEPT FOR VIBRATION. AIRCRAFT RETURNED TO LAX AND LANDED WITHOUT FURTHER EVENT. **SUPP** AIRCRAFT WAS EXTENSIVELY TROUBLESHOT DUE TO PREVIOUS HISTORY. DURING TROUBLESHOOTING DISCOVERED ISOLATOR MOUNT COLLAPSED ON THE NR 1 ENGINE. ALSO DISCOVERED THE AFT MOUNT CONE BOLT ON THE NR 2 ENGINE TURNED TO ONE SIDE2L72 4F RTA16WE 20051020001082005102000108EA 2005 10 20 MASA200500545 120050713A2760 WARNING LIGHT CNDAIRCL600 CL6002D24 1390016EA SPOILERS ILLUMINATED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07907FJ 15007 ASH 6307 PHX - AIRCRAFT EXPERIENCED AN OUTBD SPOILERON AND OUTBD FLIGHT SPOILER CAUTION MESSAGE. MAINTENANCE DISPATCHED TO AIRCRAFT AND CAUTION HAD ALREADY CLEARED. INTERROGATED MDC AND NO FAULTS FOUND. PERFORMED SYSTEM RESET AND SPOST 1 AND 2, SYSTEM OPS CHECKED GOOD. 2L72 4F RTA21EA 20051020001102005102000110NM 2005 10 20 724000017 120051005A5320 ANGLE BOEING727 727225 1384077NM FUSELAGE CRACKED A K11AK NONE O OTHER ININSP/MAINT 1 GL23724CK 20383 CRACK IN ANGLE. 2L73 4F A3WE 20051020001112005102000111NM 2005 10 20 724000018 120051006A5313 STRINGER BOEING727 727225 1384077NM FUSELAGE CRACKED A K11AK NONE O OTHER ININSP/MAINT 1 GL23724CK 20383 CRACK IN STRINGER SPLICE. 2L73 4F A3WE 20051020001132005102000113EA 2005 10 20 MASA200500506 120050630A521012028455001 SEAL CNDAIRCL600 CL6002D24 1390016EA PAX DOOR DAMAGED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07902FJ 15002 ASH 6579 PHX - MAIN PASSENGER DOOR SEAM/SEAL DAMAGED. MAINTENANCE REMOVED AND REPLACED THE SEAL/RETAINER. 2L72 4F RTA21EA 20051020001162005102000116CE 2005 10 20 4511209142005 120050914A7603 MONOPOLE LEAR 45 45LEAR 5170805CE ALIDSGTPE331TPE331201A 0517 WP ENGINE FAILED E J7SAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SW05415FX 112 P116216C ENGINE ROLLS BACK 10 PERCENT AND THE GREEN IGN. LIGHT ILLUMINATES WHEN THE POWER LEVER IS ADVANCED INTO MCT. LT ENGINE ROLLS BACK 10 PERCENT N1 IN MCT OR MCR. THE AUTO IGN ALSO INDICATED DURING ROLL BACKS W/AIRCRAFT YAW TO THE LEFT. ALL INDICATIONS NORMAL AT OTHER POWER SETTINGS. MX FOUND THE N1 MONOPOLE SHIMMED AT .038. SHOULD HAVE BEEN SHIMMED .012 TO .015. MONOPOLE RESHIMMED TO PROPER DIMENSION AND ENGINE PERFORMANCE RUN MADE SATISFACTORILY. COULD NOT FIND IN RECORDS WHERE N1 MONOPOLE HAD BEEN RECENTLY DISTURBED. N2 MONOPOLE HAD BEEN REPLACED ONE WEEK PREVIOUS WITH SATISFACTORY FLIGHTS MADE BETWEEN INCIDENTS. 2L72 4F3 TRTT00008WIAEXJ STC 20051020001172005102000117CE 2005 10 20 4508909252005 120050925A3010 RELAY LEAR 45 45LEAR 5170805CE ANTI ICE SYS FAILED E J7SAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SW05406FX 089 RED CAS STAB OVERHEAT, BURNING SMELL IN CABIN. CREW ADVISED THE RED (STAB OVHT) CAS MESSAGE ILLUMINATED WITH CWP AND TRIPLE CHIME DURING CLIMB THROUGH FL 30.0. THE THRUST LEVERS WERE JUST BELOW MCR, 82% N1 AND -29 TEMP. CREW SELECTED ANTIICE *OFF* AND PULLED POWER BACK. THE CAS MESSAGE EXTINGUISHED. CREW SELECTED ANTI-ICE BACK *ON* 2 MINUTES LATER AND CAS MESSAGE DID NOT RETURN. PER FSR RECOMMENDATIONS AND T/S, REPLACED THE P-40 RELAY PANEL. OPS CHECKS PERFORMED, NO DEFECTS NOTED. 2L72 4F RTT00008WI 20051020001182005102000118EA 2005 10 20 MASA200500301 120050416A2120 SMOKE CNDAIRCL600 CL6002C10 1390015EA CABIN DETECTED A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW07509MJ 10094 ASH 7220 BNA TO DEN. RETURN TO GATE DUE TO LEFT AND RIGHT PACKS AUTO FAIL WITH VISIBLE SMOKE IN THE CABIN. OPERATED BOTH ENGINES, BOTH PACKS AND THE APU FOR APPROXIMATELY 20 MINUTES WITH NO DEFECTS NOTED. 2L72 4F RTA21EA 20051020001202005102000120EA 2005 10 20 MASA200500616 120050805A2612 FIRE LOOP CNDAIRCL600 CL6002C10 1390015EA FALSE ACTIVATIONA MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW07510MJ 10101 ASH 7241 DEN. FIRE SYSTEM FAULT STATUS MESSAGE. MX PERFORMED OPERATIONAL TESTS AND COULD NOT DUPLICATE THE FAULT. 2L72 4F RTA21EA 20051020001222005102000122NM 2005 10 20 05FDEA03437 120051017A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 HORIZ STAB RT BARREL NUT BORE NR 8 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 24. MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20051020001242005102000124EU 2005 10 20 05FDEA03439 120051016A2611 SMOKE DETECTOR AIRBUS300 A300F4605R 3930327EU N/A MALFUNCTIONED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25680FE 794 ON TAXI OUT, NR 1 AFT SMOKE FAULT LIGHT ILLUMINATED. TURNED OFF PER PROCEDURE. ON TAKEOFF, AFT SMOKE LIGHT ILLUMINATED. NR 2 MID SMOKE LIGHT ILLUMINATED ON LANDING ROLL. CONFIMED BOTH MID 2 AND AFT ON MX PANEL AND CONTROL UNITS ARE HARD FAULTS. REMOVED AND REPLACED 5 DETECTORS, AND BOTH COALESCER BAGS. SYSTEM CHECKS GOOD. 2L72 4F RTA35EU 20051020001262005102000126EA 2005 10 20 MASA200500674 120050825A2611 SMOKE DETECTOR CNDAIRCL600 CL6002D24 1390016EA LAVATORY WILL NOT TEST A MASAO OTHER L NO TEST NRNOT REPORTED 1 SW07923FJ 15023 ASH 6254 DRO - ON PRE-FLIGHT CREW WAS UNABLE TO GET BOTH LAV FIRE DETECTORS TO TEST. MAINTENANCE ARRIVED AND PERFORMED OPERATIONAL CHECK AND FOUND NO DEFECTS, SYSTEM CHECKED GOOD. 2L72 4F RTA21EA 20051020001282005102000128EA 2005 10 20 MASA200500693 120050903A261147388904 CONTROL UNIT CNDAIRCL600 CL6002D24 1390016EA SMOKE DETECTOR MALFUNCTIONED A MASAO OTHER L NO TEST NRNOT REPORTED 1 SW07920FJ5307 15020 ASH 6932 SAN - FWD AND AFT LAVATORY SMOKE DETECTOR WARNING MESSAGES IN FLT. MX REMOVED AND REPLACED FIDEX CONTROL UNIT. 2L72 4F RTA21EA 20051020001302005102000130NM 2005 10 20 MWEA050116 120051019A575359359002 FLAP TRACK DOUG MD88 MD88 3023688NM RIGHT WING CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 RIGHT HAND WING MOST INBOARD FLAP TRACK HAS PITTING ON UPPER AND LOWER SURFACE WHERE ROLLERS RIDE. REMOVED AND REPLACED FLAP TRACK. 2L72 4F RTA6WE 20051020001322005102000132EA 2005 10 20 MASA200500583 120050722A5210 DOOR CNDAIRCL600 CL6002D24 1390016EA MAIN PAX STUCK A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07908FJ 15008 ASH 6457 LAS - FLIGHT ATTENDENT COULDN'T OPEN PAX DOOR FROM INSIDE UPON ARRIVAL TO LAS. MX INSPECTED AND NO FAULTS FOUND, OPS CHECKED GOOD. 2L72 4F RTA21EA 20051020001342005102000134EA 2005 10 20 MASA200500598 120050727A31504120T00P29 FADEC CNDAIRCL600 CL6002D24 1390016EA COCKPIT MALFUNCTIONED A MASAO OTHER N FALSE WARNING CLCLIMB 1 SW07934FJ1856 15034 ASH 6451 PHX - ABORTED T/O FOR CONFIG AILERON MSG. MX REPLACED NR 2 FADEC. 2L72 4F RTA21EA 20051020001362005102000136EA 2005 10 20 MASA200500536 120050710A5220 COVER CNDAIRCL600 CL6002D24 1390016EA EMERGENCY DOOR UNSECURE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07906FJ 15006 ASH 6115 MFR - EMERGENCY EXIT HANDLE COVER AT ROW 1 LEFT WILL NOT STAY ATTACHED TO DOOR. MAINTENANCE REMOVED AND REPLACED THE VELCRO. OPS CK GOOD. 2L72 4F RTA21EA 20051018001062005101800106NM 2005 10 18 AALA20050673 120051013A3350 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21685AA 25342 DFW - EMERGENCY R1 DOOR SLIDE LIGHT INOPERATIVE. REPLACED BATTERY PACK M730 FOR EMERGENCY R1 DOOR SLIDE LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20051018001182005101800118NE 2005 10 18 QXEA200501328 220051009A7320 WARNING LIGHT DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE NR 1 ENGINE ILLUMINATED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09366PH 510 PCEAG0104 SEA FLIGHT NR 2062, NR 1 ENGINE MANUAL CAUTION LIGHT ILLUMINATED, CHECKLIST PROCEDURE COMPLIED WITH. MAINTENANCE COMPLIED WITH MCN 2763-01, OPERATIONAL CHECK OF BETA BACKUP SYSTEM. CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20051018001282005101800128 2005 10 18 SWAA053174 420051012A256565C16820 HOOK BOEING737 7373H4 1384600NM L2 DOOR SLIDE LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29605SW 27956 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED GIRT BAR HOOK PER MM. 2L72 4F RTA16WE 20051018001442005101800144NM 2005 10 18 AWXA200501186 120051009A2560P4010021 BATTERY BOEING737 7373G7 1384595NM FLASHLIGHT INOPERATIVE A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28154AW 23776 LAS - EEL - ON GROUND IN LAS CREW REPROTED THAT THE FORWARD FLIGHT ATTENDANTS EMERGENCY FLASHLIGHT STOPPED BLINKING. MAINTENANCE REMOVED AND REPLACED THE FLASHLIGHT BATTERY IN THE FORWARD EMERGENCY FLASHLIGHT. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20051018001542005101800154NM 2005 10 18 USAA051185 120051005A5320 ANGLE BOEING737 7374B7 1384702NM BS 767-787 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19443US 24842 FOUND ZEE ANGLE CORRODED BETWEEN STA 767 AND 787 RT SIDE. REMOVED AND REPLACED ZEE ANGLE IAW SRM 53-60-53, DEFECT SIZE: 3" BY 1". 2L72 4F RTA16WE 20051018001592005101800159NM 2005 10 18 USAA051192 120051006A5340 STRINGER CLIP BOEING737 7374B7 1384702NM BS 907 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19443US 24842 FOUND STRINGER CRACKED, STA 907 AND STR 4R. REMOVED DAMAGED CLIP, REPLACED WITH FABRICATED PART IAW SRM 53-00-03, DEFECT SIZE: 1 INCH CRACK. 2L72 4F RTA16WE 20051018001602005101800160NM 2005 10 18 USAA051191 120051006A5314 KEELBEAM BOEING737 7374B7 1384702NM BS 500G CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19443US 24842 FOUND LEFT KEEL BEAM AFT SIDE OF STA 500G. FABRICATED AND INSTALLED NEW ATTACH ANGLE. REMOVED AND REPLACED CLIP IAW SRM 51-10-02 AND BOEING DWG 69-73527, DEFECT SIZE: 1" CRACK. 2L72 4F RTA16WE 20051018001692005101800169WP 2005 10 18 UPS05845544 120050828A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CHAFED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 RT WING LE LOWER RIB IS CHAFFED AT XFS 416.500. CHAF FOUND OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2-0 FIG. 2. 2L74 4F RT4A25 20051018001772005101800177EA 2005 10 18 ASOA05692 120050820A5330 FINGER DOUBLER CNDAIRCL600 CL6002B19 1900309EA BS 484 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11839AS 7284 DURING A C-CHECK IN MCN, THE FINGER DOUBLERS AT FS 484, LBL 44 AND RBL 44 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT. S/D - MAINTENANCE REMOVED THE CORROSION FROM THE FINGER DOUBLERS AT FS 484, LBL 44 AND RBL 44 BY COMPLYING WITH ASA EO 600-53-0314. (M) 2L72 4F RTA21EA 20051018001792005101800179EU 2005 10 18 10042005A 120050929A2612472326 FIRE LOOP SAAB SF340 340B 7860101EU LT ENGINE MALFUNCTIONED A NSVAO OTHER N FALSE WARNING LDLANDING 1 EA27347CJ 347 LT ENG FIRE DETECTION FAIL ANNUNCIATOR ILLUMINATED AFTER LANDING. REMOVED AND REPLACED AFT FIRE LOOP. 2L72 4T RTA52EU 20051018001822005101800182NM 2005 10 18 AMTA200500706 120050917A2530 OVEN BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE GALLEY SMOKE A AMTAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL11518AT 27974 OVEN SMOKING, GALLEY G1B. CLEANED SPILLS IN OVEN. RAN AT 450 DEGREES FOR 20 MINUTES, NO SMOKE NOTED. (M) 2L72 4F4 FRTA2NM E12EU 20051018001852005101800185WP 2005 10 18 UPS05845546 120050829A531256434332 BULKHEAD DOUG DC8 DC873F 302199FWP BS 857 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 HEAVY CORROSION ON VERTICAL STIFFENER ON FWD BULKHEAD RT W/W STA 857, RBL 45, 12" BELOW CEILING. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DWG 5643433 AND SRM TR 51-2-1 FIG 1. 2L74 4F RT4A25 20051018002022005101800202SO 2005 10 18 CHQA200500175 120051009A2560P2070005120 FLASHLIGHT EMB 145 EMB145MP 3260216SO CABIN BURNED A CHQAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL11976RP 145322 AT 28,000 FT, TURBULENCE WAS ENCOUNTERED AND A STRONG ELECTRICAL BURNING SMELL FLOODED FLT DECK WITH NO VISUAL SMOKE. THREE PAX`S SAW BLACK SMOKE FROM ROW 3 THAT LASTED NO MORE THAN 10 SECONDS. RAN QRH. DIVERTED FLT TO ORF. FLT CREW TOOK MASKS OFF BELOW 10,000 FT. NO SMOKE WAS DETECTED. LANDED IN ORF W/O INCIDENT. PERFORMED INSPECTION OF FWD ELECTRONIC BAY COOLING FANS; ALL OPERATING NORMALLY. RAN BOTH ENGINES AND BOTH PACKS AT VARIOUS POWER SETTINGS. COULD NOT DUPLICATE. FERRIED TO CMH. TEST FLT REQUIRED DUE TO BURNING SMELL AND SMOKE IN CABIN. FOUND FWD F/A FLASHLIGHT HOLDER GETTING HOT. R/R`D FWD F/A FLASHLIGHT IAW EMB 145 MM 33-50-16. TEST FLIGHT COMPLETED, NO MALFUNCTIONS OR ABNORMAL EVENTS NOTED. 2L72 4F RTT00011AT 20051018002032005101800203NM 2005 10 18 SWAA053105 120051008A3350D71701100 BATTERY PACK BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29760SW 27874 DURING SCHEDULED RON CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20051018002082005101800208NM 2005 10 18 SWAA053110 120051008A5315BAC1509 FLOORBEAM BOEING737 7377H4 1384404NM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29788SA 30603 DURING SCHEDULED 5Y CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 775, LBL 8. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20051018002272005101800227NM 2005 10 18 2005UALA01060 120051003A335020131A BATTERY BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29119UA 28812 CABIN EMERGENCY LIGHTS ON AND OFF INTERMITTENT AT ROW 56 AND AFT. REPLACED EMERGENCY LIGHT BATTERY. 2L74 4F4 FRTA20WE E24NE 20051018002302005101800230NM 2005 10 18 2005UALA01063 120051002A335020131A BATTERY BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29173UA 24380 EMERGENCY EXIT LT INOP, UPPER DK CROSS AISLE AT DOORS AFT FACING SIGN. REPLACED BATTERY. 2L74 4F4 FRTA20WE E24NE 20051018002322005101800232NM 2005 10 18 2005UALA01065 120051002A33501317 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29173UA 24380 EMERG LT INOP AT RT OVERWING 2ND AFT ASSY FWD BULB. REPLACED LAMP 2L74 4F4 FRTA20WE E24NE 20051018002342005101800234NM 2005 10 18 2005UALA01067 120051003A3350276005 FUSE BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29180UA 25224 LT BODY FAIRING OVRWING EMER LT, 2 AFT ASSY'S INOP. REPLACED FUSE AT PWR SUPPLY. 2L74 4F4 FRTA20WE E24NE 20051018002362005101800236NM 2005 10 18 2005UALA01069 120051003A3350 SIGN BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29180UA 25224 DR 2L EEL THRESHOLD AND EXIT SIGN INOP. AFTER CHARGING ALL WORKED NORMAL. 2L74 4F4 FRTA20WE E24NE 20051019000062005101900006EU 2005 10 19 2005UALA01125 120051010A2840 COMPUTER AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUEL QTY MALFUNCTIONED A UALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP29468UA 1363 RETURN TO FIELD DUE TO A FUEL QUANTITY ISSUE. OPERATED BOTH ENGINES TO OBSERVE ENGINE FUEL BURN AND THE POSSIBILITY OF FUEL LEAKS. VISUALLY CHECKED MFLI (MAGNETIC FUEL LEVEL INDICATORS) FOR VERIFICATION OF FUEL QUANTITY INDICATIONS. ALSO, FQIC (FUEL QUANTITY INDICATING COMPUTER) WAS REPLACED AND OPERATIONAL TEST OF FUEL TRANSFER SYSTEM WAS PERFORMED. NO SIGNS OF EXTERNAL LEAKS AND MFLI'S MATCHED FUEL QUANTITY INDICATIONS. FUEL TRANSFER SYSTEM OPERATIONAL CHECK WAS NORMAL. ENGINEERING WILL CONTINUE TO MONITOR BUT NO ISSUES NOTED SINCE INCIDENT. 2L72 4F4 FRTA28NM E40NE 20051019000162005101900016NM 2005 10 19 2005UALA01135 120051013A3350 LIGHT AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE CABIN MISSING A UALAK NONE O OTHER ININSP/MAINT 1 WP29809UA 825 RED EEL LIGHT ASSY MISSING AT FWD CLOSET. REPLACED RED LIGHT ASSY. 2L72 4F4 FRTA28NM E40NE 20051019000202005101900020 2005 10 19 PIDA20050178 420051017A2210158000104 ACTUATOR BOEING737 737228 13844AGNM AUTOPILOT LEAKING A PIDAK NONE K FLUID LOSS ININSP/MAINT 1 SO05251TR 23792 HYDRAULIC FLUID ON LINES AT AUTO PILOT ACTUATOR -B- IN LEFT WHEEL WELL. REPLACED -B- SYSTEM AUTO PILOT ACTUATOR PER MM 22-11-251. 2L72 4F RTA16WE 20051019000212005101900021NM 2005 10 19 SWAA053180 120051015A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM BS 787 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, RBL 7. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051019000302005101900030CE 2005 10 19 DJFA2005144 120051001A2731258CT29115A JACKSCREW RAYTHNDH125 HAWKER800XP 7150012CE ELEVATOR ICED E DJFAO OTHER F FLT CONT AFFECTED APAPPROACH 1 EA23893CW2519 258603 WHILE ON A COUPLED ILS APPROACH AUTOPILOT TRIM FAIL ANNUNCIATOR ILLUMINATED EACH TIME FLAPS WERE SELECTED TO A LOWER SETTING. WHEN AUTOPILOT DISCONNECTED ACFT PITCHED DOWN. REGAINED CONTROL USING YOKE BACK PRESSURE & MANUAL TRIM WHEEL MOVEMENT. MX ISSUED MEL 22-10-1, ACFT RETURNED TO SERVICE. SEPT 30, 2005 ELECTRIC PITCH TRIM BINDING, ELEVATOR TRIM FROZE. DURING DESCENT, TRIM WHEEL WAS ABLE TO BE MOVED MORE FREELY, A SLIGHT GRINDING FEELING WHEN MOVED. AN UNEVENTFUL LANDING WAS MADE IN KOAK. MX DISCOVERED WATER IN BOTH ELEVATOR TRIM JACK BOXES. THE WATER WAS CLEARED BY LUBRICATION OF THE JACK BOXES, SPROCKET AND DRIVE CHAIN. OPERATIONAL CHECKS WERE GOOD, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA3EU 20051019000402005101900040NM 2005 10 19 P5CA0501404 120050921A575565B0225041 PANEL BOEING747 747283B 1384867NM SPOILER CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 EA15921FT 21575 LT WING NR 3 O/B SPOILER HAS A CRACK AT UPPER SURFACE (NEAR HINGE FITTING SUPPORT). REPLACED NR 3 SPOILER ASSEMBLY IAW AMM 27-61-02. 2L74 4F A20WE 20051019000482005101900048CE 2005 10 19 DJFA2005149 120051017A3260 BULB CESSNA525 525 2076601CE MLG INDICATOR INOPERATIVE E DJFAO OTHER P NO WARNING INDICATION APAPPROACH 1 EA23291CW 5250301 THE CREW REPORTED THAT WHEN THE GEAR WAS SELECTED DOWN FOR LANDING, RECEIVED THE NOSE AND LEFT MAIN GEAR ANNUNCIATORS. THERE WAS NO INDICATION OF A DOWN AND LOCKED RIGHT MAIN GEAR, BUT THE RED UNLOCK LIGHT WAS EXTINGUISHED. THE LANDING GEAR WAS MANUALLY BLOWN DOWN AND AN UNEVENTFUL LANDING WAS MADE IN KMEM. MAINTENANCE REPLACED BOTH LEFT AND RIGHT MAIN LANDING GEAR INDICATION LAMPS AND SERVICED THE BLOW DOWN BOTTLE. EXTENSION AND RETRACTION TESTS OF THE LANDING GEAR SYSTEM WERE PERFORMED WITH NO NOTED DEFECTS. THE AIRCRAFT WAS RETURNED TO SERVICE. 1L72 4F RTA1WI 20051019000532005101900053NM 2005 10 19 CALA0500365 120051016A5320 WEB BOEING737 737724 13844BYNM BS 986-996 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714704 28765 RT SIDE FLOOR WEB AT R2 DOOR CORRODED FROM 986.5-996.5. REPLACED FLOOR WEB AND DOUBLER PER SRM 51-40-02. 2L72 4F RTA16WE 20051019000612005101900061NE 2005 10 19 SWAA053190 220051013A7230P332P02 BLADE BOEING737 7377H4 1384404NM CFMINTCFM567CFM567B22 13802NE NR 1 ENGINE TORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29467WN 33830 874194 DURING SCHEDULED HC2 CHECK, NR 1 ENGINE FAILED BOROSCOPE INSP 2ND STAGE COMPRESSOR HAD TWO BLADES TORN AND SEVERAL BLADES HAD MATERIAL MISSING ON LEADING EDGES. REMOVED AND REPLACED NR 1 ENGINE PER MM. 2L72 4F4 FRTA16WE E00055EN 20051019000762005101900076EA 2005 10 19 SWIA200515631 120051003A2741 TRIM SWITCH CNDAIRCL600 CL6002C10 1390015EA STAB STICKING A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07709SK 10159 FO'S STAB TRIM SWITCH IS STICKY. REPLACED FO'S STAB TRIM SWITCH IAW MM 27-41-05. OPERATIONAL CHECK GOOD IAW MM 27-40-00. 2L72 4F RTA21EA 20051019000812005101900081EA 2005 10 19 SWIA200515636 120051001A5610 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT FAILED A SWIAO OTHER O OTHER CRCRUISE 1 NM07912SW 7595 FO SIDE WINDOW SHATTERED AT FL350. REPLACED RT SIDE WINDOW IAW CRJ 200 MM 56-12-01. OPERATIONAL CHECK GOOD, PN OFF NP139322-6, SN OFF 02058H9575. 2L72 4F RTA21EA 20051019000872005101900087NM 2005 10 19 SWAA053032 120051004A53156545829 FLOORBEAM BOEING737 7373H4 1384600NM BS 328 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 328, LBL 39. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20051019001012005101900101NM 2005 10 19 SWAA053211 120051014A53306545775 SKIN BOEING737 7373Q8 1384670NM BS 767 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 21R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051019001292005101900129WP 2005 10 19 05FDEA03234 120051005A5751 SKIN DOUG DC10 DC1010 3022110WP ZONE 500 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LEFT WING LWR SURFACE INBOARD AILERON FOUND QTY 1 DENT AT STA XW 373. INSTALLED EXT DOUBLER IAW SRM 57-00-01 FIG 4 SHEET 2. 2L73 4F A22WE 20051020000022005102000002NM 2005 10 20 72400005 120050921A5311 FRAME BOEING727 727225 1384077NM FUSELAGE CRACKED A K11AK NONE O OTHER ININSP/MAINT 1 GL23724CK 20383 A 1 INCH CRACK ON FUSELAGE FRAME. 2L73 4F A3WE 20051020000042005102000004NM 2005 10 20 72400007 120051017A5340 TEE FITTING BOEING727 727225 1384077NM FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23724CK 20383 SEVERAL AREAS OF CORROSION ON NOSE T-CHORD. 2L73 4F A3WE 20051020000052005102000005NM 2005 10 20 72400008 120050929A5313 STRINGER BOEING727 727225 1384077NM FUSELAGE CRACKED A K11AK NONE O OTHER ININSP/MAINT 1 GL23724CK 20383 CRACKS ON STRINGER RIB ATTACHMENT. 2L73 4F A3WE 20051020000072005102000007NM 2005 10 20 724000010 120050929A5313 STRINGER BOEING727 727225 1384077NM FUSELAGE CRACKED A K11AK NONE O OTHER ININSP/MAINT 1 GL23724CK 20383 CRACKS ON STRINGER RIB ATTACHMENT. 2L73 4F A3WE 20051020000232005102000023NM 2005 10 20 SWAA053221 120051017A53116546552 FRAME BOEING737 7373H4 1384600NM BS 827 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051020000262005102000026NM 2005 10 20 SWAA053224 120051017A531165C25230 FRAME BOEING737 7373H4 1384600NM BS 727E CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727E, STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051020000272005102000027NM 2005 10 20 SWAA053225 120051017A53116558280 FRAME BOEING737 7373H4 1384600NM BS 360 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051020000312005102000031SO 2005 10 20 C2XA05SH120 120051016A532014521700007 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO FR 20 CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2726545 145558 SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 20. MAINTENANCE PERFORMED REPAIR AT LT OMEGA BEAM AT FR 20 IAW EMB 145 SRM 53-00-10 FIGURE 201 SHEET 1. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20051020000332005102000033EA 2005 10 20 MASA200500735 120050919A2711 TRIM SYSTEM CNDAIRCL600 CL6002C10 1390015EA AILERONS MALFUNCTIONED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07508MJ 10087 ASH 7273 IAD. AILERON TRIM MISCONFIG WARNING ON TAKEOFF. MAINTENANCE RESET. 2L72 4F RTA21EA 20051020000512005102000051 2005 10 20 MASA200500215 420050314A3497 CONNECTOR CNDAIRCL600 CL6002D24 1390016EA RADIO ALTIMETER LOOSE A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07905J 15005 ASH 6555 DEN-PHX. ABORTED TAKEOFF FOR GLD UNSAFE MASTER CAUTION MESSAGE. MAINTENANCE INTERROGATED THE MDC AND IT FLAGGED THE NR 1 RADIO ALTIMETER. MAINTENANCE PLACED THE RADIO ALTIMETER ON MEL AND NO FURTHER DEFECTS WERE NOTED. MAINTENANCE RESECURED LOOSE RAD ALT PLUG AND OPS CHECKED GOOD. 2L72 4F RTA21EA 20051020000602005102000060NM 2005 10 20 AWXA200501236 120050922A53206517684638 INTERCOSTAL BOEING737 7373S3 1384711NM BS 294.5 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 DURING C18 CHECK DISCOVERED INTERCOSTAL CRACKED, .375 INCHES IN LENGTH, AT STR 12L AND BS 294.5. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT BS 294.5 IAW AMERICA WEST AIRLINES ENGINEERING REQUEST NR 03-5310-5285-ES4. FABRICATED NEW INTERCOSTAL AND INSTALLED AT STRINGER 12L AND BS 294.5 IAW AWA ER NR 03-5310-5285-ES4. 2L72 4F RTA16WE 20051020000762005102000076EA 2005 10 20 MASA200500095 120050209A3260533407 SELECTOR VALVE CNDAIRCL600 CL6002D24 1390016EA MLG FAILED A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07905J 718 15005 ASH 6398 PHX-MEM. RETURNED TO THE FIELD DUE TO A GEAR DISAGREE MESSAGE AFTER TAKEOFF. MAINTENANCE REPLACED GEAR SELECTOR VALVE. A/C RETURNED TO SERVICE. 2L72 4F RTA21EA 20051020000772005102000077EA 2005 10 20 MASA200500122 120050216A3242 BRAKE ASSY CNDAIRCL600 CL6002D24 1390016EA MLG OVERHEATED A MASAO OTHER MBJOVER TEMP SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NRNOT REPORTED 1 SW07923FJ 15023 ASH 6185 PHX. NR 4 MLG BRAKE SMOKING AND EICAS READOUT READS 9. MAINTENANCE COOLED THE BRAKE AND PERFORMED OPERATIONAL CHECKS AND NO DEFECTS WERE NOTED. 2L72 4F RTA21EA 20051020000842005102000084SO 2005 10 20 C2XA05IA110 120051004A261147359713 SMOKE DETECTOR EMB 145 EMB145XR 3260214SO CARGO BAY INOPERATIVE A C2XAO OTHER JB WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW27161838010 13 14500914 IAH - FLIGHT 3097, THE CREW REPORTED A BAGGAGE SMOKE INDICATION IN FLIGHT WITH NO ASSOCIATED SMOKE IN THE BAGGAGE COMPARTMENT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE AFT BAGGAGE COMPARTMENT SMOKE DETECTOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20051020000862005102000086SO 2005 10 20 C2XA05SH121 120051016A532014532637401 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO FR 23 CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713997 145298 SHV - DURING C-CHECK RT OMEGA BEAM CORRODED AROUND NUT PLATE AT FR 23. MAINTENANCE REPAIRED RT OMEGA BEAM NUT PLATE AREA AT FR 23 BY INSTALLING DOUBLER IAW EMB 145 SRM 53-21-10 FIG 205 & EC 5320-01137. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20051020000892005102000089SO 2005 10 20 C2XA05SH118 120051013A323122250100003 SOLENOID VALVE EMB 145 EMB145EP 3260221SO NLG DOOR FAILED A C2XAO OTHER J WARNING INDICATION CLCLIMB 1 SW2715926 145005 SHV - PILOT REPORT AFTER TAKEOFF, NOSE GEAR DID NOT NORMALLY RETRACT PERFORMANCE QRH, CYCLE GEAR NOSE GEAR RETACTED NORMALLY. MAINTENANCE REMOVED AND REPLACED NLG DOOR SOLENOID VALVE IAW EMB 145 AMM 32-33-02 OPS AND LEAK CHECK GOOD. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2L72 4F RTT00011AT 20051020000922005102000092NM 2005 10 20 05FDEA03427 120051013A7500 CLAMP BOEING727 727233 138408ANM BLEED AIR LOOSE A FDEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO25219FE 21102 CRUISE POWER SETTING , NR 1 ENG STRUT OVERHEAT LIGHT ILLUMINATED. RAN QRH AND LIGHT WENT OUT GOOD SYST TEST, RETURNED TO KMIA. INSPECTED ALL DUCTS, CLAMPS AND SENSE LINES. FOUND NUMEROUS CLAMPS LOOSE AT NR 1 PRECOOLER AND NR 1 BLEED VALVE. TIGHTEN CLAMPS IAW MM 36-00-001-2. RAN ENG AT IDLE PER JRH NO LEAKS NOTED. FOUND CLAMPS ON NR 1 ENG BLEED VALVE WORN REPLACED SAME, RAN A/C TO HIGH POWER, NO MORE LEAKS NOTED, A/C OK FOR SERVICE. FOUND NR 1 ENG BLEED VALVE CLAMPS WORN REPLACED SAME, RAN A/C AT HIGH POWER NO LEAKS FOUND. CLOSED ALL PANELS ON NR 1 ENG STUB WING. 2L73 4F RTA3WE 20051020000942005102000094NM 2005 10 20 05FDEA03429 120051013A5753 HINGE FITTING DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 LEFT WING OUTBOARD FLAP INBOARD HINGE FITTING OUTBOARD NR 3 BOLT HOLE FROM FORWARD FOUND CORROSION. REPAIR ACCOMPLISHED PER EA 1-5750-93247. 2L73 4F RTA22WE 20051020001062005102000106NM 2005 10 20 05FDEA03426 120051013A7500 DUCT BOEING727 727227 1384078NM BLEED SYSTEM LOOSE A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25489FE 21492 ENG 3 STRUT OVERHEAT LIGHT ILLUMINATED, COMPLETED QRH PROC AND ISOLATED ENG NR 3 BLEED AIR. LIGHT EXTINGUISHED WHEN NR 3 BLEED AIR SW AND NR 2 PACK SW TURNED OFF AND NR 3 THROTTLE RETURNED TO IDLE. LIGHT REMAINED OFF THROUGH REST OF FLIGHT. 13 OCT 05 REMOVED AND REPLACED GROUND PNEU DUCT AND GASKETS AND CLAMP PER MM 36-00-001-2, LEAKS CKS GOOD ON APU. SEE TSI 26-13/8048 FOR FURTHER ACTIONS REQUIRED PER MOCC. 14 OCT 05 AS PER MOCC REQUEST AND AS A PRECAUTIONARY MEASURE REMOVED AND REPLACED THE OVERHEAT DETECTOR OF THE NR 3 ENGINE. PERFORMED HIGH PWR RUN AS PER JRH. ALL ENG INDICATIONS NORMAL. OVERHEAT LIGHT NEVER ILLUMINATED. A/C OK FOR SERVICE. 2L73 4F A3WE 20051109002792005110900279NM 2005 11 9 AWXA200501241 120051015A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE DAMAGED A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28332AW 23384 FLT 391 - CREW DISCOVERED DAMAGE TO TAIL SECTION DURING POST FLT INSPECTION. DAMAGE IS BELIEVED TO BE DUE TO TAIL STRIKE ON PREVIOUS TAKE OFF. MX R & R AFT BELLY SKIN FROM BS 908-1016 AND FROM STR 25L-25R IAW BOEING 737-300 SMR 51-40-02. REMOVED, FABED & INSTALLED SHEAR TIE AT BS 947 AND BL 0. REMOVED, FABBED REPAIR DOUBLER & INSTALLED REPAIR PARTS ON FRAME CHORD AT BS 1006 & STR 27L IAW BOEING 737-300 SRM 51-70-01-0G. R & I NEW STRINGER AT 27L FROM BS 908-1016 IAW BOEING 737-300 SRM 51-40-02. DFDR DOWN LOAD SHOWS THAT DAMAGE WAS CAUSED BY PILOT ERROR AND WAS NOT AIRCRAFT PROBLEM. SDR SUBMITTED FOR PRECAUTIONARY PURPOSES. 2L72 4F RTA16WE 20051020001382005102000138EA 2005 10 20 MASA200500570 120050719A5220 SEAL CNDAIRCL600 CL6002D24 1390016EA EMERGENCY DOOR DIRTY A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07906FJ 15006 ASH 6263 PHX - EMERGENCY EXIT DOOR AT SEAT 15 A/C MAKES A SQUEALING NOISE. MX CLEANED THE DOOR SEAL AND HAD NO FURTHER DEFECTS NOTED. 2L72 4F RTA21EA 20051020001402005102000140EA 2005 10 20 MASA200500639 120050813A7830TY214810A CONTROL VALVE CNDAIRCL600 CL6002D24 1390016EA THRUST REVERSER FAILED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07915FJ4365 15015 ASH 6588 SAN - RIGHT THRUST REVERSER UNSAFE CAUTION MESSAGE. MX REMOVED AND REPLACED ICV, OPS CHECKED GOOD. 2L72 4F RTA21EA 20051020001412005102000141EA 2005 10 20 MASA200500661 120050820A2611PV90421R3 SMOKE DETECTOR CNDAIRCL600 CL6002D24 1390016EA LAVATORY MALFUNCTIONED A MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW07920FJ9332 15020 ASH 6528 SFO - FWD LAV SMOKE DETECTOR GOES OFF ERRONEOUSLY. REPEAT. MX REMOVED AND REPLACED THE SMOKE DETECTOR. 2L72 4F RTA21EA 20051020001422005102000142EA 2005 10 20 MASA200500662 120050821A33501317 BULB CNDAIRCL600 CL6002D24 1390016EA PAX DOOR INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07925FJ 15025 ASH 6634 SMF - PAX DOOR FLOOR EMERGENCY LIGHTING SIGN HAS 2 MISSING BULBS IN DIFFERENT LOCATIONS INOP. MX RELAMPED. 2L72 4F RTA21EA 20051020001432005102000143EA 2005 10 20 MASA200500670 120050824A2697 CONNECTOR CNDAIRCL600 CL6002D24 1390016EA SMOKE DETECTOR LOOSE A MASAO OTHER P NO WARNING INDICATION NRNOT REPORTED 1 SW07920FJ 15020 ASH 6586 OAK - SMOKE IN THE FWD LAV. MAINTENANCE RESECURED CONNECTOR ON SMOKE DETECTOR. 2L72 4F RTA21EA 20051020001442005102000144EA 2005 10 20 VNAA0510002 120051002A329717300233 WIRE HARNESS CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NLG STEERING FAILED A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL05209PS3942 7874 THE STEERING INOP CAUTION MESSAGE ILLUMINATED AFTER DEPARTURE. THE NWS SWITCH WAS CYCLED BUT THE SYSTEM WOULD NOT RESET. THE CREW FOLLOWED THE QRH AND RETURNED TO PIT AND LANDED SAFELY. THE AIRCRAFT WAS FERRIED TO CAK WHERE AFTER TROUBLESHOOTING, MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR HARNESS ASSEMBLY IAW CRJ200 AMM 32-61-25-000(400)-801. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20051020001462005102000146EA 2005 10 20 MASA200500505 120050630A2760 FLT CONTROLS CNDAIRCL600 CL6002C10 1390015EA SPOILERS MALFUNCTIONED A MASAO OTHER J WARNING INDICATION CLCLIMB 1 SW07501MJ 10047 ASH 7201 IAD. ABORTED TAKEOFF AND RETURNED TO THE GATE DUE TO INBOARD FLIGHT SPOILERS AND INBOARD SPOILERONS CAUTION MESSAGE. MAINTENANCE RESET SYSTEM AND PERFORMED T/O CONFIGURATION CHECK. NO FURTHER DEFECTS NOTED. 2L72 4F RTA21EA 20051020001472005102000147EA 2005 10 20 MASA200500544 120050713A261224403615 FIRE DETECTOR CNDAIRCL600 CL6002C10 1390015EA MLG MALFUNCTIONED A MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW07509MJ 10094 ASH 7131 PWM. A MLG OVERHEAT MESSAGE WARNING IN FLIGHT. R2 LOOP OPS CHECK GOOD. 2L72 4F RTA21EA 20051020001482005102000148EA 2005 10 20 MASA200500595 120050726A27605120011 PCU CNDAIRCL600 CL6002C10 1390015EA FLT CONTROLS MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07501MJ6439 10047 ASH 7125 IAD. ABORTED T/O DUE TO INBOARD FLIGHT SPOILERS AND INBOARD SPOILERONS CAUTION MESSAGE. R2 PCU. 2L72 4F RTA21EA 20051020001492005102000149EA 2005 10 20 MASA200500604 120050730A2611 SMOKE DETECTOR CNDAIRCL600 CL6002D24 1390016EA LAVATORY MALFUNCTIONED A MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW07920FJ 15020 ASH 6158 SAT - AFT LAV SMOKE DETECTION WARNING MESSAGE IN FLIGHT. THE PILOT FOLLOWED HIS CFM AND MESSAGE CLEARED. SAT - MX MET THE ACFT AND INVESTIGATED, INSPECTED AND TESTED THE SYSTEM AND NO DEFECTS WERE NOTED. 2L72 4F RTA21EA 20051020001512005102000151NM 2005 10 20 MWEA050118 120051019A575499375846 DOUBLER DOUG MD88 MD88 3023688NM SLAT CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 RIB CRACKED BY LEADING EDGE SLATE CABLE PULLEY BRACKET, DO TO SLAT MAKING CONTACT WITH WORK STAND. FABRICATED AND INSTALLED DOUBLER. 2L72 4F RTA6WE 20051020001522005102000152EA 2005 10 20 MASA2005582 120050722A2613 WARNING LIGHT CNDAIRCL600 CL6002D24 1390016EA CARGO OVERHEAT FALSE ACTIVATIONA MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW07902FJ 15002 ASH 6644 PHX - AIRCRAFT INDICATED AN AFT CARGO OVERHEAT MESSAGE. MX INSPECTED THE BAY FOR OVERHEAT CONDITIONS, NONE WERE FOUND, RESET SYSTEM WITH NO FURTHER MSG NOTED. 2L72 4F RTA21EA 20051020001542005102000154EA 2005 10 20 MASA200500236 120050319A2150 A/C PACK CNDAIRCL600 CL6002C10 1390015EA RIGHT MALFUNCTIONED A MASAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW07509MJ 10094 ASH 7209 AUS TO IAD. RETURNED TO THE GATE DUE TO RT PACK AUTO FAIL AND RT PACK TEMP MASTER CAUTION ALONG WITH ERONIOUS LAV SMOKE CAUTION WHICH EXTINGUISHED ONCE PACK FELL OFF LINE. CREW C/W MEL PROCEDURES AND THE AIRCRAFT WAS RETURNED TO SERVICE. 3/20/05 MAINTENANCE PERFORMED OPS CHECK AND OPS CHECKED GOOD. 2L72 4F RTA21EA 20051020001562005102000156EA 2005 10 20 MASA200500591 120050725A33501317 LAMP CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07502MJ 10050 ASH 7083 ORD. THE CREW REPORTED THE SERVICE DOOR FLOOR EMERGENCY EXIT SIGN HAD 1 BULB INOPERATIVE, AND THE LEFT OVERWING EMERGENCY EXIT SIGN HAD 2 BULBS INOPERATIVE. MX RELAMPED. 2L72 4F RTA21EA 20051020001572005102000157EA 2005 10 20 MASA200500358 120050514A2797 CONNECTOR CNDAIRCL600 CL6002C10 1390015EA TRIM SYSTEM LOOSE A MASAO OTHER N FALSE WARNING CLCLIMB 1 SW07507MJ 10077 ASH 7041 RDU TO ORD. THE CREW ABORTED THE TAKEOFF DUE TO THE RUDDER AND AILERON CONFIG TRIM MESSAGE. MAINTENANCE FOUND THE CONNECTOR ON THE AILERON ACTUATOR LOOSE. MAINTENANCE TIGHTENED THE CONNECTOR, SYSTEM AND OPS CHECKED GOOD. 2L72 4F RTA21EA 20051020001582005102000158 2005 10 20 MASA200500362 420050516A2210 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA STAB TRIM MALFUNCTIONED A MASAO OTHER J WARNING INDICATION CRCRUISE 1 SW07515MJ 10117 ASH 7220 CID TO DEN. THE CREW HAD A MACH TRIM, STAB TRIM AND AUTO PILOT FAIL CAUTION MESSAGES IN FLIGHT. MAINTENANCE RESET THE SSCU'S PER ALL OPERATORS MEMO NR 275. NO FAULTS OR MESSAGES WERE PRESENT AFTER RESET. 2L72 4F RTA21EA 20051020001592005102000159EA 2005 10 20 MASA200500392 120050524A7830TY214810A CONTROL VALVE CNDAIRCL600 CL6002C10 1390015EA THRUST REVERSER MALFUNCTIONED A MASAO OTHER J WARNING INDICATION CLCLIMB 1 SW07501MJ6025 10047 ASH 7228 DEN TO MEM. THE CREW APORTED TAKEOFF DUE TO THE RIGHT REVERSER UNSAFE CAUTION MESSAGE. MAINTENANCE REMOVED AND REPLACED THE ICV AND OPERATIONS WERE NORMAL. 2L72 4F RTA21EA 20051020001602005102000160WP 2005 10 20 ASMF200510006 120051012A2410696233B CSD DOUG DC9 DC987 3022087WP NR 2 FAILED W ASMFD RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TXTAXI/GRND HDL 1 SW23204AM3604 3604 49404 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE THAT BEFORE TAKEOFF THE RIGHT GENERATOR FREQUENCY AND AHRS-2 WERE OUT OF SERVICE. THE REPORT WAS DEFERRED IAW MEL 24-1-B. DURING OVERNIGHT CHECK, THE RIGHT CSD AND OIL HEAT EXCHANGER WERE REPLACED IAW MM 24-10-01/-03, RESPECTIVELY AND THE AHRS-2 WAS TESTED IAW MM 34-21-10, BEING CORRECT. DEFERRED REPORT WAS CLOSED. 2L72 4F RTA6WE 20051020001622005102000162EA 2005 10 20 MASA200500607 120050731A2720 WARNING LIGHT CNDAIRCL600 CL6002D24 1390016EA ELEVATOR FALSE ACTIVATIONA MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW07920FJ 15020 ASH 6484 PHX - ELEVATOR SPILT CAUTION MESSAGE. MX RESET THE SYSTEM WITH THE HELP OF BOMBA REP AND ALL OPS CHECKS WERE GOOD. 2L72 4F RTA21EA 20051020001712005102000171EA 2005 10 20 MASA200500660 120050820A2611 SMOKE DETECTOR CNDAIRCL600 CL6002D24 1390016EA LAVATORY MALFUNCTIONED A MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW07920FJ 15020 ASH 6528 SFO - THE CREW REPORTED THE FORWARD LAVATORY SMOKE DETECTOR ON CONTINUOUSLY. CONTRACT MAINTENANCE RESET THE SYSTEM AND THE SYSTEM FUNCTIONED NORMALLY. 2L72 4F RTA21EA 20051020001732005102000173EA 2005 10 20 MASA200500710 120050906A2150 A/C PACK CNDAIRCL600 CL6002D24 1390016EA LEFT SMOKE A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW07920FJ 15020 ASH 6340 SAN - LEFT PACK TEMP SPIKES AND SMOKE IN FLT DECK WHEN CHANGING BLEED SOURCES. MAINTENANCE COULD NOT DUPLICATE. 2L72 4F RTA21EA 20051020001752005102000175EA 2005 10 20 MASA200500737 120050920A4990WE38007703 APU CNDAIRCL600 CL6002D24 1390016EA APU BAY LEAKING A MASAO OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW07920FJ6241 6241 15020 ASH 6351 PHX - MX FOUND INTERNAL APU OIL LEAK CAUSING SMOKE IN THE AIR DUCTS AND SETTING OFF THE LAV SMOKE DETECTOR. MX REMOVED AND REPLACED APU OPS CHECKED GOOD. 2L72 4F RTA21EA 20051020001772005102000177NM 2005 10 20 05FDEA03157 120050929A5312 BEAM BOEING727 727233 138408ANM BULKHEAD DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25267FE 21673 AFT LOWER CARGO BS 1183 BULKHEAD VERTICAL BEAM AT LBL 20 HAS FASTENERS INSTALLED WITH SHORT PITCH, (SIDE BY SIDE). COMPLIED WITH FED EX EA E7-5310-91297-FUSELAGE, BS 1183 AFT PRESSURE BULKHEAD SHORT ON CENTER FASTENER SPACING REPAIR. MAJOR REPAIR. 2L73 4F RTA3WE 20051020001792005102000179EA 2005 10 20 MASA200500772 120051005A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0737178 7178 ASH 6373 PHX - AFT OVERHEAD EMERGENCY LIGHT INOP. MX RELAMPED. 2L72 4F RTA21EA 20051020001822005102000182EA 2005 10 20 MASA200500809 120051015A33501317 LAMP CNDAIRCL600 CL6002D24 1390016EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07931LR 15031 ASH 6121 OMA - OVERHEAD EMERGENCY LIGHT AT ROW 7 INOP. MAINTENANCE RELAMPED THE LIGHT. 2L72 4F RTA21EA 20051020001872005102000187EA 2005 10 20 MASA200500780 120051008A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN DISCHARGED A MASAO OTHER L NO TEST NRNOT REPORTED 1 SW0777181 7181 ASH 2910 AVP - EMERGENCY LIGHTS ARE INOPERATIVE. CONTRACT MX CHARGED THE LIGHTS AND THEY OPS CHECKED. 2L72 4F RTA21EA 20051020001892005102000189EA 2005 10 20 MASA200500782 120051008A3010 DUCT CNDAIRCL600 CL6002B19 1900309EA ANTI ICE SYSTEM DAMAGED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07154SF 7154 ASH 2893 ALB - A-ICE DUCT WARNING. MX REMOVED AND REPLACED DUCT ASSY, OPS CHECKED GOOD. 2L72 4F RTA21EA 20051020001902005102000190EA 2005 10 20 MASA200500787 120051005A32304622 CHECK VALVE CNDAIRCL600 CL6002B19 1900309EA NLG PRIORITY MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0747202171538072 7202 ASH 2746 PIT - LANDING GEAR DISAGREE WARNING MESSAGE. REPLACED NOSE GEAR PRIORTY CHECK VALVE. 2L72 4F RTA21EA 20051020001912005102000191EA 2005 10 20 MASA200500801 120051013A3411 PITOT LINE CNDAIRCL600 CL6002B19 1900309EA PITOT STATIC CONTAMINATED A MASAO OTHER P NO WARNING INDICATION NRNOT REPORTED 1 SW0717217 7217 ASH 7154 SAV - STANDBY AIRSPEED INDICATOR INDICATES 0 KNOTS AT 80 KNOTS. MX DRAINED WATER AND LEAK CHECKED STANDBY PITOT SYSTEM. 2L72 4F RTA21EA 20051021000012005102100001CE 2005 10 21 AMWA73619 120051019A3210 LANDING GEAR BEECH 1900 1900D 1154162CE MALFUNCTIONED A AMWAD RETURN TO BLOCK O OTHER TOTAKEOFF 1 CE07127ZV UE127 AFTER TAKEOFF, CREW UNABLE TO RETRACT LANDING GEAR. RETURNED TO FIELD WITH NO FURTHER INCIDENT. MORE INFORMATION WILL BE AVAILABLE AT A LATER DATE. 2L72 4T RTA24CE 20051021000022005102100002NM 2005 10 21 DL76L050571 120050928A3244 TIRE BOEING767 767332 1382001NM MLG DEFLATED A DALAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO27180DN 25985 DURING PUSHBACK NR 6 MAINWHEEL DEFLATED AND 2 RIM BOLTS SHEARED OFF. REMOVED AND REPLACED MAINWHEEL NR 6 AS PER MM. 2L72 4F RTA1NM 20051021000032005102100003NM 2005 10 21 DL75K050573 120050929A5532175N20012 SKIN BOEING757 757232 1384965NM VERTICAL STAB PUNCTURED A DALAK NONE O OTHER ININSP/MAINT 1 SO27655DL 24395 GROUND DAMAGE OCCURRED TO VERTICAL STABILIZER, FWD TORQUE BOX, RIGHT, LOWER SKIN, JUST FWD OF THE STAB FRONT SPAR. DAMAGE CONSISTS OF PUNCTURE TO THE OUTER SKIN, CORE, AND INNER SKIN. REPAIRED PER DELTA ERA 450853-14. 2L72 4F RTA2NM 20051021000052005102100005NM 2005 10 21 DL76K050575 120050930A2120 ODOR BOEING767 767332 1382001NM CABIN AFT DETECTED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27171DZ 29690 PASSENGERS AND FLIGHT ATTENDANTS SMELLED SMOKE IN CABIN NEAR ROW 46, RAN PACKS AND THOROUGHLY INSPECTED AIRCRAFT. 2L72 4F RTA1NM 20051021000082005102100008NM 2005 10 21 DL757050579 120051001A3350 BULB BOEING757 757232 1384965NM LT OVERWING INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27672DL 25977 AFT LT EXTERIOR OVERWING EMERGENCY LIGHT INOP. RELAMPED, CK OK. 2L72 4F RTA2NM 20051021000092005102100009NM 2005 10 21 DLM88050581 120051002A2612 FIRE LOOP DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 1 ENGINE FAILED A DALAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO27987DL39903 53338 725530 IN FLIGHT NR 1 ENGINE LOOP A FAIL LIGHT ILLUMINATED, CREW SAID SELECTED THE A LOOP AND THE FIRE WARNING ILLUMINATED, SECURED THE ENGINE AND DIVERTED TO MCN. UNABLE TO DUPLICATE, REPLACED A LOOP. 2L72 4F4 FRTA6WE E9NE 20051021000102005102100010NM 2005 10 21 DL76L050584 120051002A33500201804001 LENS BOEING767 767332 1382001NM SEATS 3F & 6B MISSING A DALAK NONE O OTHER ININSP/MAINT 1 SO27184DN 27111 SEAT MOUNTED ESCAPE PATH LIGHTING AT 3F AND 6B MISSING 1 WHITE LENS AND BOTH BULBS. RELAMPED AND REPLACED WHITE LENS AT SEATS 3F AND 6B. OPS CKS OK. 2L72 4F RTA1NM 20051021000122005102100012NM 2005 10 21 DL76L050587 120051003A3244B767ERM TIRE BOEING767 767332 1382001NM NR 3 CUT A DALAO OTHER C F.O.D. TXTAXI/GRND HDL 1 SO27185DN 27961 NR 3 MAIN TIRE HAS DEEP CUTS /3 EA/ 2 THRU SECOND CHORD PLY AND 1 WITH TINY PIECE OF WHITE GLASS. FOUND ON ARRIVAL. REMOVED AND REPLACED NR 3 MAIN WHEEL ASSY. INSP RT MAIN GEAR, NO OTHER DAMAGE NOTED. 2L72 4F RTA1NM 20051024000012005102400001NE 2005 10 24 HNAA0500093 220051009A7200 ENGINE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE NR 2 MALFUNCTIONED A HNAAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 EA07837EX 217 190900 NR 2 TORQUE DROPPED FOM 90 PERCENT TO 61 PERCENT WHEN ECU SELECTED TO NORMAL AFTER TAKEOFF WITH NO ILLUMINATION OF NR 2 MANUAL LIGHT. CYCLED BETA LOCKOUT CIRCUIT BREAKER. 2H72 4T4 TRTA13NM E20NE 20051024000022005102400002NM 2005 10 24 BB05093 120051019A493038760355 TRANSDUCER BOEING757 757225 1384959NM APU FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19605AU 22201 FLIGHT 2, FLL-PHL: APU FAILED IN FLIGHT, WHILE THE RIGHT GENERATOR SYSTEM WAS ALREADY ON MEL. DIVERTED TO CLT. NO OTHER DIFFICULTIES. MAINTENANCE REPLACED THE APU INLET PRESSURE TRANSDUCER AND THE RIGHT IDG, CLEARING BOTH THE APU AND GENERATOR SYSTEMS. 2L72 4F RTA2NM 20051024000032005102400003SO 2005 10 24 GUU2005F00053 120050930A3240 BRAKE ASSY EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE RIGHT MALFUNCTIONED A GUUAO OTHER O OTHER TXTAXI/GRND HDL 1 SO17282AS 120226 DURING TAXI, AIRCRAFT PULLS TO THE LEFT. RT BRAKE SPONGY, POOR BRAKING ACTION ON RT SIDE. VISUALLY INSPECTED BRAKE SYSTEM. NO LEAKS NOTED. PERFORMED HIGH SPEED TAXI, NO DEFECTS NOTED. (K) 2L72 4T4 TRTA31SO E20NE 20051024000052005102400005NM 2005 10 24 SWAA053255 120051019A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 294.5 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 294.5, STR 13L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051024000072005102400007NM 2005 10 24 SWAA053257 120051019A52306547952 DOOR FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29347SW 24374 DURING SCHEDULED SPECIAL VISIT, FOUND AFT CARGO DOOR AFT FRAME CRACKED AT NR 5 STOP FITTING CUTOUT. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20051024000102005102400010 2005 10 24 SWAA053260 420051019A25655A33075 SLIDE BOEING737 7377H4 1384404NM L1 DOOR DEPLOYED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29441WN 29837 L1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY DEPLOYED. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20051024000122005102400012NM 2005 10 24 SWAA053262 120051019A53116546532 FRAME BOEING737 7373H4 1384600NM BS 480 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051024000132005102400013NM 2005 10 24 SWAA053263 120051019A53116546525 FRAME BOEING737 7373H4 1384600NM BS 380 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051024000152005102400015NM 2005 10 24 SWAA053265 120051019A53116546550 FRAME BOEING737 7373H4 1384600NM BS 787 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051024000172005102400017NM 2005 10 24 SWAA053267 120051019A53116546558 FRAME BOEING737 7373H4 1384600NM BS 907 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051024000192005102400019NM 2005 10 24 CALA0500368 120051016A3520889251 LATCH BOEING767 767424ER 1385270NM PAX O2 INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2766051 29446 FOUND SEAT 38C PAX OXYGEN MODULE DOOR INOP. REPLACE LATCH PER AMM 35-21-00. 2L72 4F RTA1NM 20051024000232005102400023EU 2005 10 24 RAIA00510021 120051018A3350 CONTACT JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT DIRTY A RAIAK NONE O OTHER ININSP/MAINT 1 CE03561HK 41077 POST FLIGHT INSPECTION -STL - EMERGENCY LIGHT OUT AT 9A. MAINTENANCE REPAIRED CONTACT ON EMERGENCY LIGHT. 2L72 4T RTA41NM 20051024000242005102400024NM 2005 10 24 BB05092 120051017A3260 SENSOR BOEING757 757225 1384959NM MLG DOOR MALFUNCTIONED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19623AU 27244 FLIGHT 742, CLT-BOS: AFTER TAKEOFF, GEAR DISAGREE & GEAR DOOR MESSAGE ON EICAS. PLACED GEAR HANDLE TO -DOWN- POSITION. ALL INDICATIONS NORMAL. RETURNED TO CLT. MAINTENANCE REPLACED THE RIGHT MLG DOOR SENSOR. 2L72 4F RTA2NM 20051024000262005102400026EU 2005 10 24 B65A106299 120051012A6200105627794 SHIELD BOLKMS105 BO105LSA1 5626021EU ALLSN 250C 250C28 03013GL MAIN ROTOR BROKEN B B65AO OTHER O OTHER NRNOT REPORTED 1 GL13202LF 2014 SHIELD, BROKEN AND REPLACED. 1G72 3U3 U H3AU E1GL 20051024000272005102400027EU 2005 10 24 B65A106300 120051012A6200105627794 SHIELD BOLKMS105 BO105LSA1 5626021EU ALLSN 250C 250C28 03013GL MAIN ROTOR BROKEN B B65AO OTHER O OTHER NRNOT REPORTED 1 GL13202LF 2014 SHIELD, BROKEN AND REPLACED. 1G72 3U3 U H3AU E1GL 20051024000302005102400030EA 2005 10 24 VNAA0510003 120051006A3250 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NLG STEERING FALSE ACTIVATIONA VNAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL05228PS 7897 THE STEERING INOP CAUTION MESSAGE ILLUMINATED AFTER TAKEOFF FROM DCA. THE CREW FOLLOWED THE QRH, DIVERTED TO BTV, AND MADE AN UNEVENTFUL LANDING. THE STEERING SYSTEM OPERATED NORMAL ON LANDING. MAINTENANCE PERFORMED AN OPERATIONAL TEST OF THE NOSE WHEEL STEERING SYSTEM IAW CRJ200 AMM 32-51-00-710-802. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20051024000312005102400031EA 2005 10 24 VNAA0510008 120051012A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PILOT ERROR FALSE ACTIVATIONA VNAAO OTHER N FALSE WARNING APAPPROACH 1 GL05209PS 7874 THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED DURING LANDING APPROACH. THE CREW FOLLOWED THE QRH AND MADE AN UNEVENTFUL LANDING. THE CREW REPORTED THAT THE FLAP SELECTOR WAS NOT IN THE DETENT. MAINTENANCE RESET AND OPERATIONALLY CHECKED THE FLAP SYSTEM IAW CRJ200 SL-00-001. OPS CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20051024000332005102400033SO 2005 10 24 CHQA200500186 120051017A3350100865 BATTERY EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11844RP131834994 145620 AFT EMERGENCY LIGHTS COME ON, DIM, AND THEN GO OUT WITHIN A FEW SECONDS. REPLACED NR 3 AND NR 4 EMERGENCY POWER SUPPLY ASSEMBLY IAW MM. OPS CHECK GOOD. 2L72 4F4 FRTT00011ATTE6CH 20051024000342005102400034SO 2005 10 24 CHQA200500181 120051018A3240 BRAKE ASSY EMB 145 EMB145MP 3260216SO ALLSN AE300 AE3007A GL MLG MALFUNCTIONED A CHQAO OTHER E VIBRATION/BUFFET LDLANDING 1 GL11976RP 145322 VIOLENT SHUDDER OF BRAKES COUPLED WITH LOSS OF BRAKING EFFECTIVENESS DECELERATING FROM 80 KNOTS THROUGH 40 KNOTS ON LANDING ROLL OUT. INSPECTED ALL 4 WHEEL SPEED TRANSDUCERS AND CHECKED BRAKES FOR DRAGGING. ALL OPS CHECKS GOOD IAW MM 32-41-00. 2L72 4F4 FRTT00011ATTE6CH 20051024000352005102400035 2005 10 24 AWXA200501244 420051018A34426225130021 RADAR AIRBUSA319 A319132 3930340NM IAE V2524 V2524A5 NE WX SYSTEM FAILED A AWXAA UNSCHED LANDING O OTHER CRCRUISE 1 WP28836AW52 52 2570 DURING CRUISE, ENROUTE, THE WEATHER RADAR FAILED. THERE WERE THUNDERSTORMS, AIRCRAFT DIVERTED AND LANDED WITHOUT FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED THE WEATHER RADAR TRANSCEIVER UNIT AND THE WEATHER RADAR CONTROL UNIT IAW AMM 34-41-12 AND 34-41-33. OPERATIONAL CHECKS WERE GOOD. VENDOR TEAR DOWN REPORT CONFIRMS REASON FOR REMOVAL OF THE WEATHER RADAR TRANSCEIVER. TRANSCEIVER WOULD NOT TRANSMIT DURING INCOMING TESTS. REPLACED A2F1, A4CR201, A4Q201 AND A4VR10. UNIT WAS TESTED AND REPAIRED IAW CMM 34-45-47 REV 5 TEMP REV 48. WEATHER RADAR CONTROL UNIT PASSED INCOMING TESTS AND INSPECTION; NO FAULTS WERE FOUND WITH THE UNIT. UNIT TESTED IAW CMM 34-45-24 REV 7 TEMP REV 27. 2L72 4F4 FRTA28NM E40NE 20051024000392005102400039NM 2005 10 24 AWXA200501254 120051009A57536546434301 WEDGE BOEING737 7373G7 1384595NM TE FLAPS DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - MAJOR REPAIR - DURING C16 DISCOVERED AREA OF DEBOND ON UPPER AND LOWER SURFACES OF THE LT INBOARD AFT FLAP, 37 INCHES FROM INBOARD END FROM WBL 110.00 TO WBL 114.00. MAINTENANCE REMOVED DAMAGED SKIN AND CORE IAW BOEING 737-300 SRM 51-700-10-2R4. FABRICATED REPLACEMENT CORE AND REPAIR DOUBLER IAW BOEING 737-300 SRM 51-70-10-2R4. BONDED REPAIR PARTS TO THE LT INBOARD AFT FLAP FROM WBL 110.00 TO WBL 114.00 IAW BOEING 737-300 SRM 51-70-10-2R4. 2L72 4F RTA16WE 20051024000402005102400040NM 2005 10 24 AWXA200501255 120050917A53206520726 SILL BOEING737 73733A 1384673NM BS 400-450 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW 23634 GYR - MAJOR REPAIR - DURING C20 FOUND INTERGRANULAR CORROSION ON FORWARD BAG PIT THRESHOLD SILL WEB FROM BS 400 TO BS 450 AND FROM BL 28R TO BL 48R. MAINTENANCE REMOVED WEB AND FABRICATED NEW WEB IAW BOEING 737-300 SRM 51-30-01. INSTALLED WEB IN THE FORWARD BAG PIT FROM BS 400 TO BS 450 AND FROM BL 28R TO BL 48R IAW BOEING 737-300 SRM 51-20-01. 2L72 4F RTA16WE 20051024000422005102400042NM 2005 10 24 AWXA200501257 120051004A5753654643099 SKIN BOEING737 7373S3 1384711NM FOREFLAP DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 MCN - MAJOR REPAIR - DURING C18 CHECK DISCOVERED DISBOND AREA, UPPER SURFACE OF LT INBOARD FORE FLAP, 34: FROM INBOARD END. MAINTENANCE REMOVED DISBOND AREA ON THE UPPER SURFACE OF THE LT INBOARD FORE FLAP IAW BOEING 737-300 SRM 51-20-10-2R. FABRICATED AND BONDED DOUBLER AND REPAIR FILLER ONTO THE UPPER SURFACE OF THE LT INBOARD FORE FLAP 34 INCHES FROM THE INBOARD END IAW BOEING 737-300 SRM 51-70-10-2R, REPAIR 4 FIG 203. 2L72 4F RTA16WE 20051024000432005102400043NM 2005 10 24 AWXA200501258 120051004A57536546435277 WEDGE BOEING737 7373S3 1384711NM TE FLAP DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 MCN - MAJOR REPAIR - DURING C18 CHECK DISCOVERED DISBOND AREA, ON THE LEFT OUTBOARD AFT FLAP FROM WBL 230.68L TO WBL 232.68L. MAINTENANCE REMOVED DISBOND AREA FROM THE LT OUTBOARD AFT FLAP IAW BOEING 737-300 SRM 51-70-10-2R. FABRICATED AND BONDED REPAIR FILLER AND DOUBLER TO THE LEFT OUTBOARD AFT FLAP FROM WBL 230.68L TO WBL 232.68L. 2L72 4F RTA16WE 20051024000442005102400044NM 2005 10 24 QXEA200501356 120051018A2430 WARNING LIGHT DHAV DHC8 DHC8202 2809007NM NR 1 DC GENER FALSE ACTIVATIONA QXEAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 NM09347PH 480 SEA FLIGHT NR 2278, NR 1 DC GENERATOR LIGHT WOULD NOT EXTINGUISH AFTER ENGINE START. MAINTENANCE PERFORMED OPERATIONAL CHECK OF DC GENERATORS PER D-8 MM CH 24-31-00, PAGES 501-504. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051024000472005102400047SW 2005 10 24 690100305DG 120050930A7810610632503 RESTRAINT GULSTM690TP 690A 0141722SW GARRTTTPE331TPE331* 01514WP NR 2 ENGINE BROKEN B JBZAE ENGINE SHUTDOWN J WARNING INDICATION ININSP/MAINT 1 WP27677WA 11243 SCHEDULED MX, BOTH ENG`S STARTED FOR A ROUTINE OPS CHK. ABOUT 4 MINS INTO RUN-UP, WITH PROP BLADES LT IN FLAT PITCH, NR 2 ENG FIRE WARN LIGHT ILLUMINATED. PILOT PERFORMED A CAUTIONARY SHUTDOWN OF BOTH ENG`S. AN INITIAL INSPECT OF NR 2 ENG FOR CAUSE OF FIRE WARN LIGHT ILLUMINATION RESULTED IN NO NOTED DEFECTS. ALL FOUR SENSORS REPLACED & FIRE SENSOR SYS THOROUGHLY INSPECTED. NR 2 ENG ONCE AGAIN STARTED RESULTING IN ANOTHER FIRE WARN ILLUMINATION WITHIN A 5 MIN PERIOD. WITH THIS RUN-UP, NOTED WHEN PROP TAKEN OFF FLAT PITCH LOCKS, WARN LIGHT EXTINGUISHED. FURTHER INVEST, EXHAUST STACK SLIP JOINT REVEALED THAT 2 OF STACK ATTACH RESTRAINTS BROKEN, ALLOWING EXCESSIVE MOVEMENT AT JOINT. 1H72 3T3 T 2A4 E2WE 20051024000492005102400049NM 2005 10 24 USAA200510002 120051017A5330 SKIN BOEING737 7373B7 1384580NM BS 727E CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19505AU 23380 A 1.375 INCH CRACK FOUND AT STA 727E AT STRINGER 21 LEFT. INSTALLED REPAIR DOUBLER PER SRM 53-00-01 FIG 201. 2L72 4F RTA16WE 20051024000502005102400050NM 2005 10 24 USAA051210 120051014A5330 SKIN BOEING737 737301 1384611NM BS 727E CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19334US 23231 BS 727E -10 S-18R CRACKED. INSTALLED DOUBLER IAW SRM 53-00-01 FIG 201, REPAIR 31 DEFECT SIZE: 3.25 INCH. 2L72 4F RTA16WE 20051024000512005102400051NM 2005 10 24 USAA051211 120051014A5330 SKIN BOEING737 737301 1384611NM BS727 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19334US 23231 BS 727 S19R CRACKED. INSTALLED DOUBLER IAW 53-00-01 FIG 201, DEFECT SIZE: 1.35 INCH. 2L72 4F RTA16WE 20051024000522005102400052NM 2005 10 24 USAA051209 120051014A5311 FRAME BOEING737 7374B7 1384702NM BS 380 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19443US 24842 STA 380 BETWEEN S19L TO S22L CRACKED. REPAIRED IAW EA 96971, DEFECT SIZE: .25 INCH. 2L72 4F RTA16WE 20051024000542005102400054SO 2005 10 24 SWIA200515690 120051016A27203081401003 ACTUATOR EMB 120 EMB120ER 3260203SO RUDDER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CLCLIMB 1 NM07393SW9689 7713 120330 RIGHT RUDDER JAMS AFTER ROTATION. REPLACED BLUE SYSTEM RUDDER ACTUATOR IAW EMB MM 27-22-00 AND 27-22-02. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20051024000582005102400058EA 2005 10 24 SWIA200515694 120051015A27604916405 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07435SW1200312003 7555 SPOILERS FAULT. REPLACED NR 1 SECU IAW AMM 27-61-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051024000622005102400062EA 2005 10 24 SWIA200515698 120051015A3350 SWITCH CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHTSMALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07754SK 10215 EMERGENCY LIGHTS COME ON WHEN COCKPIT SWITCH IS ARMED AND F/A SWITCH IS OFF. RESET BREAKER. OPERATIONAL CHECK GOOD OF EMERGENCY LIGHTS IAW CRJ AMM CHAP 33-51-00. 2L72 4F RTA21EA 20051024000632005102400063EA 2005 10 24 SWIA200515699 120051014A2751 DETECTOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07954SW 7815 RECEIVED A -FLAPS DEGRADED MESSAGE-. REPLACED SKEW DETECTOR UNIT AND NR 3 AND NR 4 FLAP ACTUATOR SKEW DETECTOR SENSORS ON LT AND RT. REF CRJ 200 MM 27-51-15. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051024000652005102400065 2005 10 24 YENA200573 420051011A3414HG2030AD11 ADIRU AIRBUS320 A320232 3930326EU NR 1 MALFUNCTIONED A YENAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 EA15624JB15042220 2520 REJECTED T/O AT APPROX 90-100 KTS. NO AIRSPEED INDICATION ON CAPT SIDE. ACCOMPLISHED FLUSHING OF PITOT PROBE NR 1 IAW MM 34-10-00. NO FOD FOUND IN LINES. REF POST FLIGHT REPORT APR NR 1 FAULT. REMOVED AND REPLACED ADIRU NR 1 IAW MM 34-12-34. OPS CK GOOD PER MX CNTRL ACCOMPLISH TSM TASK 34-13-00 810-998. ACCOMPLISH LEAK TEST OF PRINCIPAL STATIC AND TOTAL AIR DATA SYSTEM AS PER AMM 34-13-00-790-002 OPS TEST NORMAL. CREW PERFORMED HIGH SPEED TAXI UP TO 105 KTS, NO DEFECTS WERE NOTED, OPS CHECK NORMAL. 2L72 4F RTA28NM 20051024000662005102400066EA 2005 10 24 VNAA0510007 120051010A5210840534 PROXIMITY SWITCH CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR INTERMITTENT A VNAAO OTHER O OTHER NRNOT REPORTED 1 GL05254PS7935 7935 THE PAX DOOR OUT HANDLE CAUTION MESSAGE ILLUMINATED SEVERAL TIMES DURING THE FLIGHT. THE AIRCRAFT WAS FERRIED TO CLT WHERE MAINTENANCE REMOVED & REPLACED THE PAX DOOR OUTER HANDLE PROXIMITY SWITCH IAW CRJ200 AMM 52-70-04-000(400)-803. AN OPERATIONAL CHECK FLIGHT WAS PERFORMED WITH NO DISCREPANCIES NOTED. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20051024000672005102400067NM 2005 10 24 ANCF200400058 120051016A5220 SEAL DOUG MD80 MD83 3023681NM PWA JT8 JT8D* NE EMERGENCY DOOR DAMAGED W ANCFA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO23583AN 53183 AFTER TAKEOFF, CABIN ALT WARNING LIGHT COME ON. PACKS AUTO NORMAL PRESSURE, FLOW LIGHT ON, OUTFLOW VALVE CLOSE IAW AMM 52-21-02 PAG 201 OVERWING EMERGENCY DOOR SEAL WAS REPLACED. 2L72 4F4 FRT E2EA 20051024000702005102400070NM 2005 10 24 SWAA053247 120051018A3350MS155721 BULB BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29468WN 33858 DURING SCHEDULED SERVICE CHECK, FOUND RT EXTERNAL EMERGENCY LIGHT INOP FWD OF AFT CARGO BIN. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20051024000722005102400072NM 2005 10 24 SWAA053249 120051018A3350311500 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29607SW 27927 BULLNOSE EMERGENCY LIGHT LENS LOOSE AT ROW 6. SECURED LENS PER MM. 2L72 4F RTA16WE 20051024000752005102400075NM 2005 10 24 SWAA053252 120051018A53306545776 SKIN BOEING737 7373A4 1384585NM BS 939.75 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 939.75, STR 21L. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20051024000762005102400076NM 2005 10 24 SWAA053253 120051014A3350S417N5101007 LIGHT BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29736SA 27868 FWD CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20051024000772005102400077SO 2005 10 24 SWIA200515701 120051013A2913 PUMP EMB 120 EMB120ER 3260203SO HYD SYSTEM LEAKING A SWIAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 NM07576SW 120345 ON DESCENT, GREEN SYSTEM MAIN PUMP LOW PRESSURE LIGHT ILLUMINATED AND ELECTRIC PUMP CYCLED ON AND OFF. HYDRAULIC QUANTITY WENT TO -0- AND FREE FALL ACCOMPLISHED. REPAIRED LEFT ENGINE HYD PUMP PRESSURE LINE, LEAK CHECK GOOD. 2L72 4T RTA31SO 20051024000782005102400078CE 2005 10 24 DJFA2005152 120051019A3260327 BULB BEECH MU300 400A 1155402CE EMERGENCY LIGHT BURNED OUT E DJFAA UNSCHED LANDING O OTHER LDLANDING 1 EA23480LX RK398 UPON LANDING AT KHEZ, THE CREW DID NOT RECEIVE A DOWN AND LOCKED INDICATION FOR THE LEFT MAIN GEAR. THE GEAR INDICATION BULB WOULD NOT ILLUMINATE WHEN TESTED. THE AIRCRAFT WAS DIVERTED TO KHOU FOR MAINTENANCE. FIRE/RESCUE RESPONSE WAS GIVEN AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT MAIN GEAR INDICATION BULB. OPERATIONAL CHECKS WERE GOOD, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4F RTA16SW 20051024000792005102400079NM 2005 10 24 TAMF20050007O 120051017A5330 SKIN BOEING767 767200 1385120NM GE CF6 CF680C2B2 30025NE BS 172.5 DENTED W TAMFK NONE O OTHER ININSP/MAINT 1 SO23768QT 23803 DURING INSPECTION CHECK, FOUND THE AIRPLANE HIT AT FUSELAGE SKIN, STA 172.5 STRINGER 21 RT BY A CARGO LOADING EQUIPMENT.REPAIR DOUBLER AS TEMPORARY REPAIR WAS INSTALLED IAW EWO 767-53-002, MFG SERVICE REQUEST NR 1-134757238 AND SRM 53-00-01 FIGURE 201. PERMANENT REPAIR WILL BE PERFORMED IN NEXT (C) MAINTENANCE CHECK. (MAY, 2006). 2L72 4F4 FRTA1NM E13NE 20051019000112005101900011NM 2005 10 19 2005UALA01130 120051012A5310 CREASE BEAM BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE AFT GALLEY DOOR CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29919UA 25386 AFT GALLEY DOOR CUTOUT AREA LOWER THRESHOLD CREASE BEAM CORRODED STA 913 TO 1016. REMOVED & REPLACED CREASE BEAM IN ACCORDANCE WITH SRM 51-40-02. 2L72 4F4 FRTA16WE E2GL 20051019000182005101900018NM 2005 10 19 2005UALA01137 120051014A3210 LANDING GEAR BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE MAINS MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29379UA 24654 UNABLE TO RAISE GEAR AFTER DEPARTURE. SAFETY SENSORS (AIR & GROUND) FOUND OUT OF ADJUSTMENT . (SENSORS STUCK IN GROUND MODE). REPLACED S106 SENSOR AND ADJUSTED THE CLEARANCE PER MM 32-09-01 AND PERFORMED OPS CHECK GOOD. 2L72 4F4 FRTA16WE E2GL 20051019000232005101900023NM 2005 10 19 SWAA053182 120051015A53116546540 FRAME BOEING737 7373H4 1384600NM BS 639 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D-HECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, STR 7R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051019000282005101900028NM 2005 10 19 SWAA053187 120051015A53306545776 SKIN BOEING737 7373H4 1384600NM BS 927 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 24R. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20051019000322005101900032NM 2005 10 19 SCNA05008 120051012A3242 PSEU BOEING737 7378Q8 13844BXNM BRAKES MALFUNCTIONED A SCNAO OTHER O OTHER LDLANDING 1 GL15809SY 30683 AFTER TOUCHDOWN IN SEA, SPEEDBRAKE DO NOT ARM LIGHT ILLUMINATED AND SPEEDBRAKE DID NOT AUTOMATICALLY EXTEND. PSEU LIGHT ILLUMINATED WITH MASTER CAUTION & OVERHEAD LIGHTS. MAINTENANCE PERFORMED PSEU BITE PER TASK 32-09-00-810-801. FOUND FAULT 32-62002 PSEU. MAINTENANCE MANUAL TASK 32-09-00-810-86A PER MAINTENANCE MANUAL TASK. FAULT WAS INTERMITTENT. FAULTS RESET, OK FOR SERVICE. 2L72 4F RTA16WE 20051019000522005101900052NM 2005 10 19 CALA0500364 120051016A5315147A57101 FLOORBEAM BOEING737 737724 13844BYNM BS 986 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714704 28765 RT GALLEY FLOORBEAM ANGLE CORRODED AFT OF STA 986.5, RBL 50. REPLACED FLOOR SUPPORT ANGLE PER SRM 51-40-02. 2L72 4F RTA16WE 20051019000542005101900054NM 2005 10 19 SWAA053099 120051008A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29471WN 32471 EEPLS TRACK LIGHT MISSING AT FWD END. REMOVED AND REPLACED EEPLS PER MM. 2L72 4F RTA16WE 20051019000552005101900055 2005 10 19 PIDA20050174 420051005A2210AR6460M2 ACTUATOR BOEING737 737306 13844BGNM AUTOPILOT TRIM MALFUNCTIONED A PIDAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 SO05371PA 23543 ALTITUDE OCCASIONALLY CLIMBS 300 FEET WITH STAB OUT OF TRIM LIGHT (LEAVES FLIGHT DIRECTOR). REPLACED AUTO PILOT STAB TRIM ACTUATOR PER MM 22-11-81. OPS CHECKS GOOD PER MM 22-11-81. 2L72 4F RTA16NE 20051019000562005101900056EU 2005 10 19 RAIA00510009 120051005A3397 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT LOOSE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03558HK 41071 POST-FLIGHT INSPECTION - RIC - FLOOR STRIP EMERGENCY LIGHTS INOP. MAINTENANCE RESECURED LIGHT STRIP CONNECTOR AND PERFORMED FUNCTIONAL CHECK. 2L72 4T RTA41NM 20051019000692005101900069NM 2005 10 19 SWAA053207 120051015A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM BS 807 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 807, BETWEEN RBL 4 TO LBL 4. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051019000742005101900074EA 2005 10 19 SWIA200515629 120051003A335020131A BATTERY CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT DISCHARGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07724SK4761 4761 10189 AFT EMERGENCY LIGHT IN CABIN INOP. REPLACED EMERGENCY BATTERY. OPERATIONAL CHECK GOOD, REF 33-51-17. 2L72 4F RTA21EA 20051019000772005101900077SO 2005 10 19 SWIA200515632 120050930A27213081401003 ACTUATOR EMB 120 EMB120ER 3260203SO RUDDER TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED DEDESCENT 1 NM07189SW9922 9922 120048 RUDDER TRIM INEFFECTIVE IN DESCENT. REPLACED UPPER RUDDER ACTUATOR IAW 27-22-02. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20051019000892005101900089NM 2005 10 19 SWAA053034 120051004A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM BS 747 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 747, LBL 9. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051019001112005101900111NM 2005 10 19 PCSA10100501 120051010A2131 CONTROLLER BOEING727 7272F9 138407DNM CABIN PRESSURE MALFUNCTIONED A PCSAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO29199AJ 21426 FLIGHT 751 MIA TO MEX CREW REPORTED, PRESSURIZATION WOULD NOT LEVEL OFF ON CLIMBOUT, JETTISONED FUEL BELOW LANDING WEIGHT. AIRCRAFT RETURNED TO MIA AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND FLOW CONTROL VALVE NOT OPERATING PROPERLY. REMOVED AND REPLACED LT & RT FLOW CONTROL, SHUT-OFF VALVES, RT HP REGULATOR & NR 1 8TH STAGE CHECK VALVE. OPERATIONAL NORMAL IN ACCORDANCE WITH MM 36-10-21 & MM 71-00. AIRCRAFT RETURNED TO SERVICE. 2L73 4F RTA3WE 20051019001162005101900116NM 2005 10 19 AWXA200501169 120051004A3350BR964411 LIGHT BOEING737 7373G7 1384595NM CABIN INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28322AW 25400 PHX - EEL - DURING INSPECTION DISCOVERED SEAT ROW 5 EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY AT ROW 5. OPERATIONAL CHECKS GOOD. 2L72 4F RTA16WE 20051019001212005101900121EA 2005 10 19 QXEA200501284 220050929A7200312162701 ENGINE BOMBDRDHC8 DHC8402 1390042NM PWC 150 PW150A EA NR 2 DAMAGED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09414QX5545 4061 PCEFA0174 PDX: BORESCOPE INSPECTION OF THE NR 2 ENGINE S/N FCEFA0174 CIS REVEALED MISSING MATERIAL AT APPROXIMATELY 10 O'CLOCK POSITION REQUIRING ENGINE REMOVAL IAW EO 6-72-136B FIGURE 12 (SHEET 2). MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE PER MTC #6710003 AND 6710004. ALL OPS CHECKS ARE GOOD. LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E00062EN 20051020000172005102000017EA 2005 10 20 MASA200500774 120051006A2560MXP21000 SMOKE GOGGLES CNDAIRCL600 CL6002C10 1390015EA COCKPIT CRACKED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07503MJ 10058 ASH 7275 CLT. BOTH COCKPIT SMOKE GOGGLES CRACKED. MX R2 GOGGLES. 2L72 4F RTA21EA 20051020000192005102000019NM 2005 10 20 SWAA053217 120051017A53116546537 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 578, BETWEEN STR 13L TO STR 14L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051020000202005102000020 2005 10 20 SWAA053218 420051017A25656557463 FITTING BOEING737 7373H4 1384600NM GIRT BAR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D-CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FLOOR FITTING CORRODED. REMOVED AND REPLACED FLOOR FITTING PER SRM. 2L72 4F RTA16WE 20051020000292005102000029NM 2005 10 20 SWAA053227 120051017A53116546532 FRAME BOEING737 7373H4 1384600NM BS 480 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, BETWEEN STR 8L TO STR 9L & BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051020000422005102000042NE 2005 10 20 AALA20050682 220051015A7200 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE RIGHT MAKING METAL A AALAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 SW21456AA 49561 725505 BOS - INFLIGHT JUST AFTER ROTATION A STRANGE RUBBING NOISE WAS HEARD FROM THE COCKPIT FOLLOWED BY A THUMP. A STRONG VIBRATION WAS FELT IN THE REAR OF THE AIRCRAFT. RETURNED TO BOS AND LANDED WITHOUT INCIDENT. FOUND METAL IN OIL FILTER. REPLACED RIGHT ENGINE. FLIGHT DATA RECORDER DOWNLOAD REQUESTED FROM ENGINEERING. 2L72 4F4 F A6WE E9NE 20051020000542005102000054NM 2005 10 20 AWXA200501230 120050928A5311654588340 FRAME BOEING737 7373S3 1384711NM BS 188 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 DURING C18 CHECK DISCOVERED CRACK, 2.0 INCHES IN LENGTH, ON FRAME IN RADIUS AT BS 188, WL 209 AND BL 33R. MAINTENANCE TRIMMED OUT CRACK AT BS 188, WL 209 AND BL 33R IAW AMERICA WEST AIRLINES ENGINEERING REQUEST NR 03-5300-05286-RC1. FABRICATED FILLERS AND ANGLES IAW AWA ER NR 03-5300-05286-RC1. INSTALLED FABRICATED REPAIR PARTS AT BS 188, WL 209 AND BL 33R IAW AWA ER NR 03-5300-05286-RC1. 2L72 4F RTA16WE 20051020000792005102000079EA 2005 10 20 MASA200500225 120050316A2120 SMOKE CNDAIRCL600 CL6002D24 1390016EA CABIN DETECTED A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW07902FJ 15002 CAPTAIN REPORTED SMOKE IN CABIN ON GROUND WITH FORWARD AND AFT LAV SMOKE MASTER WARNING. CONTRACT MX INSPECTED AFT EQUIPMENT BAY EQUIPMENT AND DUCTING FOR INTEGRITY AND FOUND NO DEFECTS, INSPECTED AND OPS CHECKED BOTH FORWARD AND AFT LAV SMOKE DETECTORS AND OPS CHECKED NORMAL. PERFORMED APU NORMAL START AND LT & RT PACK OPERATION WITH NO REPEAT OF CABIN SMOKE. ACCOMPLISHED TWICE WITH NO REPEAT, NO FAULTS FOUND RETURNED TO SERVICE. 2L72 4F RTA21EA 20051020000962005102000096NM 2005 10 20 05FDEA03431 120051013A5753 HINGE FITTING DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 LEFT WING OUTBOARD FLAP OUTBOARD HINGE FITTING OUTBOARD NR 3 BOLT HOLE FROM FORWARD FOUND CORROSION. REPAIR ACCOMPLISHED PER EA 1-5750-93248. 2L73 4F RTA22WE 20051020001002005102000100NM 2005 10 20 05FDEA03436 120051016A5320 INTERCOSTAL DOUG MD11 MD11 3023602NM BS 6-30 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 FWD CARGO COMPT AT STA 6-30 LT LOWER INTERCOSTAL ASSY BETWEEN LONGERON 42 TO LONGERON 43 FOUND CORRODED DURING REMOVAL. 2L73 4F RTA22WE 20051020001152005102000115NE 2005 10 20 NACA20050023 220051003A7397 WIRE BOEING727 72722C 138400FNM PWA JT8 JT8D7B 52053NE FUEL INDICATOR DAMAGED A NACAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 AL03792A 19195 654678 ENGINE NR 1, NR 2 & 3 FUEL FLOW INDICATORS READ ZERO AT TAKEOFF. REMOVED CONNECTOR FROM PREVIOUSLY DEFERRED NR 3 ENGINE FUEL FLOW TRANSMITTER AND NR 1 & NR 2 ENGINE FUEL INDICATIONS OP CHECKED GOOD ON GROUND RUN. THE FUEL FLOW POWER SUPPLY WAS REPLACED WITH NEGATIVE RESULTS. ADDITIONAL TROUBLESHOOTING LEAD TO THE REPAIR OF WIRING. OP CHECK GOOD BY FLIGHT CREW. 2L73 4F4 F A3WE E2EA 20051020001192005102000119EA 2005 10 20 MASA200500326 120050502A3234533443 LEVER CNDAIRCL600 CL6002C10 1390015EA MLG FAILED A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07502MJ6333 6333 10050 ASH 7275 CLT TO DEN. THE CREW RETURNED TO THE FIELD DUE TO THE NLG GEAR UP DISAGREE MESSAGE AFTER TAKEOFF. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL HANDLE PSEU. 2L72 4F RTA21EA 20051020001212005102000121EA 2005 10 20 MASA200500623 120050805A3150 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA PITCH FEEL ILLUMINATED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07502MJ 10050 ASH 7241 DEN. PILOT AIR INC'D WITH A PITCH FEEL CAUTION IN CRUISE. CONTINUED TO BNA PER CFM. DECLARED EMERGENCY DURING LANDING. MX RESET, OPS CHECKED GOOD. 2L72 4F RTA21EA 20051020001232005102000123NM 2005 10 20 05FDEA03438 120051017A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 HORIZ STAB RT BARREL NUT BORE NR 10 FOUND WITH CORROSION. REWORK/REPAIR AD 2003-22-08 EA 1-5510-87628, ATTACHMENT 25. MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20051020001252005102000125EA 2005 10 20 MASA200500672 120050824A5270 SENSOR CNDAIRCL600 CL6002D24 1390016EA EMERGENCY DOOR OUT OF ADJUST A MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW07935LR 15035 ASH 6092 PHX - RT FWD EMERGENCY DOOR CAUTION MESSAGE. MX INSPECTED AND FOUND DOOR TO BE SECURE BUT EXPERIENCED AN INDICATION PROBLEM. MX ADJUSTED DOOR SENSOR. 2L72 4F RTA21EA 20051020001272005102000127EA 2005 10 20 MASA200500680 120050828A2611 SMOKE DETECTOR CNDAIRCL600 CL6002D24 1390016EA LAVATORY WILL NOT TEST A MASAO OTHER L NO TEST NRNOT REPORTED 1 SW07911FJ 15011 ASH 6093 PHX - FWD LAV SMOKE DETECTOR WILL NOT TEST. MX TESTED AND FOUND NO DEFECTS. 2L72 4F RTA21EA 20051020001292005102000129EA 2005 10 20 MASA200500694 120050904A2611 SMOKE DETECTOR CNDAIRCL600 CL6002D24 1390016EA LAVATORY MALFUNCTIONED A MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW07920FJ 15020 ASH 6587 PVR - FWD AND AFT LAVATORY SMOKE DETECTOR WARNING MESSAGES IN FLT. MX RESET SYSTEM AND OPS CHECK NORMAL. 2L72 4F RTA21EA 20051020001312005102000131NM 2005 10 20 MWEA050117 120051019A554459553913 HINGE BRACKET DOUG MD88 MD88 3023688NM RUDDER CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 VERTICAL STABILIZER RUDDER HINGE BRACKET HAVE CORROSION AROUND BOLT HOLES TO ATTACH THE BEARING ASSEMBLY AND CORROSION IN THE FIN ATTACHMENT BOLT HOLES. REMOVED AND REPLACED RUDDER HINGE BRACKET. 2L72 4F RTA6WE 20051020001332005102000133EA 2005 10 20 MASA200500584 120050723A5270 WARNING LIGHT CNDAIRCL600 CL6002D24 1390016EA PAX DOOR HANDLE FALSE ACTIVATIONA MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW07902FJ 15002 ASH 6141 PHX - PAX DOOR OUTER HANDLE CAUTION MESSAGE. OPS CHECKED GOOD. 2L72 4F RTA21EA 20051020001352005102000135EA 2005 10 20 MASA200500600 120050728A5220 COVER CNDAIRCL600 CL6002D24 1390016EA EMERGENCY DOOR UNSECURE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07906FJ 15006 ASH 6104 PHX - EMERGENCY DOOR HANDLE COVER AT SEAT 15 A WAS FALLING OFF. MX RESECURED THE HANDLE COVER. 2L72 4F RTA21EA 20051020001372005102000137EA 2005 10 20 MASA200500559 120050712A5330BA690352082 SKIN CNDAIRCL600 CL6002D24 1390016EA BS 1031-1069 DAMAGED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07913FJ 15013 DAMAGE TO AFT FUSELAGE FORWARD OF VENTRAL FIN AT FS 1031 TO 1069, STR21R-22R, REPLACED. 2L72 4F RTA21EA 20051020001392005102000139EA 2005 10 20 MASA200500629 120050810A3350316 LIGHT CNDAIRCL600 CL6002D24 1390016EA CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07904FJ 15004 ASH 6584 OAK - DURING PRE-FLT, CREW FOUND CEILING EMER FLOODLIGHT INOP. MX RELAMPED. 2L72 4F RTA21EA 20051020001612005102000161EA 2005 10 20 MASA200500606 120050731A32445013640 TIRE CNDAIRCL600 CL6002D24 1390016EA NLG FAILED A MASAO OTHER D INFLIGHT SEPARATION NRNOT REPORTED 1 SW07907FJ 15007 ASH 6531 COS - GEAR WOULD NOT RETRACT AND RIGHT NOSE TIRE TREAD DEPARTED ON ROTATION. MX REPLACED THE TIRES. 2L72 4F RTA21EA 20051020001642005102000164NE 2005 10 20 HNAA0500091 220051016A7200 ENGINE DHAV DHC8 DHC8201 2809001NM PWA PW120 PW123 NE NR 2 MALFUNCTIONED A HNAAA UNSCHED LANDING Y ENGINE STOPPAGE CLCLIMB 1 EA07966HA 452 AE0090 APPROXIMATELY 200 FT AGL, NR 2 ENGINE TORQUE AND NH FLUCTUATED +/- 50 PERCENT SHUT DOWN ENGINE IN FLIGHT. REMOVED AND REPLACED NR 2 ENGINE. 2H72 4T4 TRTA13NM E20NE 20051020001652005102000165EA 2005 10 20 MASA200500168 120050301A2611 SMOKE WARNING CNDAIRCL600 CL6002C10 1390015EA CARGO BAY FALSE ACTIVATIONA MASAFD ACTIVATE FIRE EXT. RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SW07509MJ4288 10094 ASH 7041 ORD. THE CREW REPORTED A CARGO SMOKE WARNING DURING TAXI AND THE BOTTLES WERE DISCHARGED. THE AIRCRAFT RETURNED TO THE GATE WHERE ON CALL MAINTENANCE INSPECTED THE AREA FOR ANY EVIDENCE OF FIRE OR SMOKE AND NONE WAS FOUND. THE DETECTORS WERE PLACED ON DEFERRAL AND THE AIRCRAFT CONTINUED SERVICE. 3/1 MX REPLACED BOTH FIREX BOTTLES, P/N 473919-1, S/N 50777EL AND P/N 473920-1, S/N 51122EL. 2L72 4F RTA21EA 20051020001662005102000166EA 2005 10 20 MASA200500130 120050218A2120 ODOR CNDAIRCL600 CL6002C10 1390015EA CABIN DETECTED A MASAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SW07508MJ 10087 ASH 7248 CLT. THE CREW REPORTED A LAV SMOKE WARNING DURING TAKEOFF WITH AN ASSOCIATED SMELL OF SMOKE THAT CLEARED PRIOR TO LANDING. THE AIRCRAFT RETURNED TO THE FIELD WHERE MAINTENANCE RAN BOTH ENGINES AND THE APU TO ATTEMPT TO DUPLICATE THE PROBLEM. THE OPERATIONAL CHECKS WERE OK AND THE AIRCRAFT CONTINUED REVENUE SERVICE. 2L72 4F RTA21EA 20051020001672005102000167NM 2005 10 20 HNAA0500092 120051011A2400 INVERTER DHAV DHC8 DHC8102 2809003NM AUX WARNING LIGHT A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07846EX 326 CLIMBING THROUGH 4000 FEET ON CLIMB-OUT L26AC, R26AC, PRIMARY, SECONDARY AND AUX INVERTER CAUTION LIGHTS WITH TERRAIN INOP AND GPWS CAUTION LIGHTS ILLUMINATED. DURING CHECKLIST UPON SWITCHING AUX INVERTER TO RIGHT AFTER 45 SECONDS ALL LIGHTS EXTINGUISHED. REMOVED AND REPLACED SECONDARY INVERTER. 2H72 4T RTA13NM 20051020001702005102000170EA 2005 10 20 MASA200500643 120050815A2760 WARNING LIGHT CNDAIRCL600 CL6002D24 1390016EA SPOILERS ILLUMINATED A MASAO OTHER J WARNING INDICATION CRCRUISE 1 SW07923FJ 15023 ASH 6158 LAX - PHX - SBA, CAPTAIN DIVERTED TO LAX WHEN AIRCRAFT INDICATED AN O/B SPOILERON AND O/B FLIGHT SPOILER CAUTION MESSAGE. MX RESET SYSTEM, PERFORMED SPOST PER SERVICE LETTER AND IT OPS CHECKED GOOD WITH NO FURTHER FAULTS FOUND. 2L72 4F RTA21EA 20051020001722005102000172EA 2005 10 20 MASA200500698 120050905A5230CC670387303 SEAL CNDAIRCL600 CL6002D24 1390016EA CARGO DOOR DAMAGED A MASAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW07922FJ 15022 ASH 6611 LAS - DIVERTED TO PHX DUE TO THE CREW BEING UNABLE TO CONTROL PRESSURIZATION. MX REPLACED THE AFT CARGO DOOR PRESSURIZATION SEAL. 2L72 4F RTA21EA 20051020001742005102000174EA 2005 10 20 MASA200500730 120050915A2611 SMOKE DETECTOR CNDAIRCL600 CL6002D24 1390016EA LAVATORY FALSE ACTIVATIONA MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW07928LR 15028 ASH 6104 PHX - PILOT REPORTED SMOKE IN THE AFT LAV WARNING MESSAGE IN FLIGHT. MX INSPECTED AND FOUND NO DEFECTS. 2L72 4F RTA21EA 20051020001762005102000176NM 2005 10 20 NACA20050024 120051018A2781H1010262 POSITION SWITCH BOEING727 72722C 138400FNM LE SLATS MALFUNCTIONED A NACAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 AL03727YK 19806 OUT OF 19,000 FEET NR 4 LEADING EDGE LIGHT CAME ON. AT 11,000 FEET THE LIGHT WENT OUT. REMOVED & REPLACED FLAP POSITION SWITCH. OP CHECKED GOOD IAW UAL 727 AMM 27-81-0 PG 512. NR 4 K-FLAP RT LEADING EDGE. 2L73 4F A3WE 20051020001782005102000178EA 2005 10 20 MASA200500745 120050923A2760 PCU CNDAIRCL600 CL6002D24 1390016EA SPOILERS MALFUNCTIONED A MASAD RETURN TO BLOCK J WARNING INDICATION NRNOT REPORTED 1 SW07904FJ6230 15004 ASH 6090 PHX - PILOT RETURNED TO GATE DUE TO A INBOARD SPOILERS AND INBOARD SPOILERONS FAULT. MX R2 PCU. 2L72 4F RTA21EA 20051020001802005102000180EA 2005 10 20 MASA200500756 120050927A2560266 BATTERY CNDAIRCL600 CL6002D24 1390016EA MEGA PHONE INOPERATIVE A MASAO OTHER L NO TEST NRNOT REPORTED 1 SW07917FJ 15017 ASH 6531 COS - DURING PRE-FLIGHT, THE MEGA PHONE WAS INOPERATIVE. MX REPLACED THE BATTERY. 2L72 4F RTA21EA 20051020001812005102000181NE 2005 10 20 MASA200500755 220050925A7200 PLUG CNDAIRCL600 CL6002D24 1390016EA GE CF34 CF34* NE ENGINE MISSING A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07921FJ 15021 194247 ASH 6085 MEM - E1 ROLL BACK TO IDLE DURING FLIGHT. ENGINE RECOVERED ITSELF AFTER A FEW MINUTES AND CONTINUED TO PHX NORMALLY. FOUND BOROSCOPE PLUG MISSING INSTALLED AND PERFORMED POWER RUNS OPS CHK GOOD. 2L72 4F4 FRTA21EA E15NE 20051020001832005102000183EA 2005 10 20 MASA200500149 120050223A2741CC670511151 TRIM PANEL CNDAIRCL600 CL6002C10 1390015EA STAB WARNING LIGHT A MASAO OTHER FG FLT CONT AFFECTED MULTIPLE FAILURE CLCLIMB 1 SW07509MJ3666 10094 ASH 7219 - BNA-DEN - DURING CLIMB-OUT, THE MACH TRIM AND STAB TRIM BOTH FAILED AND WOULD NOT RE-ENGAGE. THE FLIGHT CONTINUED TO DEN. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE STAB TRIM CONTROL PANEL AND THE MCU. OPS WERE NORMAL. WAITING PART INFO MOTOR CONTROL UNIT P/N 7074-4 S/N 267 (SFIM) 2L72 4F RTA21EA 20051020001852005102000185EA 2005 10 20 MASA200500726 120050913A2120 ODOR CNDAIRCL600 CL6002D24 1390016EA CABIN DETECTED A MASAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SW07920FJ 15020 ASH 6005 LAX - THE CREW REPORTED THE FORWARD LAVATORY SMOKE DETECTOR ON DURING CLIMB-OUT FOR APPROXIMATLY ONE MINUTE WITH AN ODOR OF BURNING OIL. MAINTENANCE PERFORMED AN OPS CHECK OF THE SMOKE DETECTOR AND RAN RIGHT AND LEFT PACKS WITH NO DEFECTS NOTED. 2L72 4F RTA21EA 20051020001862005102000186EA 2005 10 20 MASA200500754 120050926A2750855D1009 SENSOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW073717811958 7178 ASH 6428 PHX - DECLARED AN EMERGENCY DUE TO THE FLAPS FAILED AT ZERO. A & B FLAPS FAIL INSPECTION AND REPLACED LEFT BPSU. 2L72 4F RTA21EA 20051020001882005102000188EA 2005 10 20 MASA200500781 120051008A3010 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA ANTI ICE SYSTEM FALSE ACTIVATIONA MASAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW07154SF 7154 ASH 2893 ALB - LEFT WING ANTI-ICE WARNING MESSAGE. CONTRACT MAINTENANCE PERFORMED A TEST OF THE SYSTEM BUT WERE UNABLE TO DUPLICATE THE DISCREPANCY. 2L72 4F RTA21EA 20051021000072005102100007NM 2005 10 21 DL764050578 120051001A21508252092 ACM BOEING767 767432ER 1385134NM LEFT FAILED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27831MH 20000333 29702 AT FL330, 5 MINS INTO CRUISE, CABIN FILLED WITH SMOKE. A/C DIVERTED INTO OAK AND LANDED WITHOUT INCIDENT. FOUND LEFT ACM FAILED. FWD TO MCO AND PLACARD PER MEL 21-51-01. 2L72 4F RTA1NM 20051021000112005102100011NM 2005 10 21 DLM88050585 120051003A3244329001470 TIRE DOUG MD88 MD88 3023688NM NR 3 FAILED A DALAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SO27988DL 53339 F/A REPORTED BURNING RUBBER SMELL IN CABIN AFTER T/O, RT ENGINE STALLED DURING CLIMB. FOUND NR 3 TIRE TREAD SEPARATED AND MISSING. REPLACED TIRE AND REPAIRED FLAP DAMAGE. 2L72 4F RTA6WE 20051024000042005102400004 2005 10 24 SWAA053254 420051019A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29218WN 32489 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051024000812005102400081WP 2005 10 24 IXXA05SMN163S 120050809A5730 ACCESS DOOR DOUG DC8 DC873F 302199FWP LT WING CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL948072897 46003 DURING ROUTINE C CHECK INSPECTION, LT WING, SLOT ACCESS DOOR CRACKED 1, XILD 7095 XS 250.089. REMOVED AND REPLACED INBD SLOT UPPER DOOR ON LT WING IAW DC-8 MM 27-80-02 PAGES 201-204. 2L74 4F RT4A25 20051024000832005102400083WP 2005 10 24 IXXA05SMN162S 120050809A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CRACKED B IXXAO OTHER O OTHER ININSP/MAINT 1 SW11603AL948072897 46003 DURING C CHECK INSPECTION, LT WING, UPPER SKIN HAS 03 CRACKS, XRS 74.000 S-9 S-10. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-2-1 FIG 17, EO SEMAN NR 20051135 DATE 08-10-05. REMOVED FASTENERS IAW DC-8 SRM 51-1-20D PAGE 21. REMOVED DAMAGED AREA IAW DC-8 SR, 57-2-1 FIG 17. PERFORMED NDT INSPECTION IAW DC-8 NDT SPM, PART 06-10-01-001. FAB`D REPAIR DOUBLER (7075T6 AL 0.160) + (03EA) FILLERS PLUG (AL 7075T6 0.175) IAW DC8 SRM 57-2-1FIG 17, DC8 SRM 57-3-3 FIG 12 ITEM A. MAKE TAPER DOUBLER FROM 0.160 TO 0.080 IAW DC8 SRM 51-10-0 FIG 1 (SHEET 20). CLEANED, TREATED AND PRIMED AREA + REPAIR PARTS IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11 PAGE 9. INSTALLED REPAIR PARTS IAW DC8 SRM 572L74 4F RT4A25 20051024000842005102400084WP 2005 10 24 IXXA05SMN161S 120050809A5753 SKIN DOUG DC8 DC873F 302199FWP ZONE 500 DELAMINATED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL948072897 46003 DURING ROUTINE C CHECK INSPECTION, LT WING NR 4 VANE FLAP LWR SKIN DELAMINATED. REMOVED AND REPLACED NR 4 FLAP VANE (LT WING) IN REPAIRED CONDITION IAW DC8 MM 27-51-14 PAGE 201-202. 2L74 4F RT4A25 20051024000852005102400085NM 2005 10 24 AWXA200501246 120050924A534069265553 STRINGER CLIP BOEING737 7373S3 1384711NM BS 348 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 MCN - MAJOR REPAIR - DURING C18 CHECK DISCOVERED STRINGER 16L CLIP CRACKED, .35 INCHES, BETWEEN BS 348.2 AND BS 351.2. MAINTENANCE REMOVED STR 16L CLIP AND REPLACED WITH NEW FABRICATED PART BETWEEN BS 348.2 AND BS 351.2 IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NO. 03-5310-05285-ES5. 2L72 4F RTA16WE 20051024000932005102400093WP 2005 10 24 IXXA05SMN167S 120050810A5340 FITTING DOUG DC8 DC873F 302199FWP BS 300 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL948072897 46003 DURING ROUTINE C CHECK INSPECTION, FWD CARGO COMPT FITTING CRACKED .500 INCHES, STA 300.000 , L-32R L-33R. REMOVED CRACKED FITTING IAW DC-8 SRM 51-1-21 PAGE 1. CLEANED, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8B. INSTALLED NEW FITTING WITH FASTENERS (HILOKS) IAW DC-8 SRM 51-1-20D PAGE 9. TORQUED IAW DC-8 SRM 51-3-1. 2L74 4F RT4A25 20051024000942005102400094WP 2005 10 24 IXXA05SMN179S 120050811A5340 FITTING DOUG DC8 DC873F 302199FWP BS 1690 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL948072897 46003 DURING ROUTINE C CHECK INSPECTION, AFT ACCY CMPT BATHTUB FITTING CRACKED 1, STA 1690.000, L-28R. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D PG 9 AND DC8 SRM 51-3-1 (TORQUE). 2L74 4F RT4A25 20051024000952005102400095WP 2005 10 24 IXXA05SMN170S 120050811A5330 SKIN DOUG DC8 DC873F 302199FWP BS 195 DAMAGED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL948072897 46003 DURING C-CHECK INSPECT, RT FWD FUSELAGE BELOW FWD STATIC PORT, DOUBLER THICKNESS RATIO EXCEEDED MAX ALLOWED, ALUMINUM RIVETS USED IN LONGERONS. REWORK REPAIR IAW TO BRING INTO CONFORMANCE, STA FS 195, L-35R. PERFORMED MAJOR REPAIR IAW FAA 8110-3 NR 05367 DATED 08-19-05, SEMAN DWG ED 4045 DATED 08-12-05 AND EO SEMAN NR 20051122 DATED 08-19-05. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PAGE 21. TRIMMED OUT DAMAGED AREA IAW SEMAN DWG ED 4045. PERFORMED NDT INSPECT IAW DC-8 NDT SPM, PART 06-10-01-001. FAB`D REPAIR DOUBLER, INTERNAL FINGER DOUBLER & FILLER IAW SEMAN DWG ED 4045, DC8 SRM 51-1-4 PAGE 1. INSTALLED REPAIR PARTS IAW SEMAN DWG ED 4045, DC-8 SRM 51-1-20D PG 9, DC8 2L74 4F RT4A25 20051024000992005102400099NM 2005 10 24 BB05091 120051017A2760 ROLLER BOEING757 757225 1384959NM SPOILERS OUT OF ADJUST A USAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA19614AU 27145 FLIGHT 412, PHL-BOS: DURING TAKEOFF, -SPOILERS- LIGHT ILLUMINATED. EICAS MESSAGE -SPOILERS- DISPLAYED WITH SPOILERS SELECTED DOWN. AIRCRAFT WAS ON THE GROUND. REJECTED TAKEOFF. MAINTENANCE ADJUSTED THE CAM ROLLER CONTROL ROD. SPEEDBRAKES REMAIN ON MEL 27-6201, CONTROL NUMBER 1320C23. 2L72 4F RTA2NM 20051024001042005102400104NM 2005 10 24 DLM88050591 120051004A213121184904 CONTROLLER DOUG MD88 MD88 3023688NM CABIN PRESSURE MALFUNCTIONED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27944DL 49817 DURING CLIMB FLOW LIGHT ILLUMINATED PASSING 10000 FT AUTO 1 LIGHT ON. DURING RETURN TO ATL CABIN ALTITUDE REACHED 5500 FT VERY LITTLE AIRFLOW WAS PRODUCED BY THE RIGHT PACK. SECURED LOOSE DUCTING AND REPLACED NR 1 PRESSURE CONTROLLER. 2L72 4F RTA6WE 20051024001072005102400107NM 2005 10 24 DL78K050594 120050926A5312148A22816 BULKHEAD BOEING737 737832 13844CFNM BS 1016 CANNING A DALAK NONE O OTHER ININSP/MAINT 1 SO273737C 30799 OIL CANNING FOUND IN THE BS 1016 AFT PRESSURE BULKHEAD AT APPROX RBL 10 & WL 290. DAMAGE CUT OUT AND REPAIR DOUBLER INSTALLED. 2L72 4F RTA16WE 20051024001102005102400110NM 2005 10 24 DL75K050597 120051006A2560 BATTERY BOEING757 757232 1384965NM FLASHLIGHT DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO276700 30337 EMERGENCY FLASHLIGHT BATTERY AT L4 DOOR INOP. REPLACED BATTERY, FLASHLIGHT CHECK OK. 2L72 4F RTA2NM 20051024001132005102400113EA 2005 10 24 MASA200500807 120051015A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA LAVATORY WILL NOT TEST A MASAO OTHER L NO TEST NRNOT REPORTED 1 SW07570ML 7206 ASH 7209 IAD - LAVATORY SMOKE DETECTOR WILL NOT TEST. MX REPLACED SMOKE DETECTOR. 2L72 4F RTA21EA 20051024001162005102400116EA 2005 10 24 MASA200500790 120051010A2730 WARNING LIGHT CNDAIRCL600 CL6002D24 1390016EA ELEVATOR FALSE ACTIVATIONA MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW07930LR 15030 ASH 6041 PHX - ELEVATOR SPLIT CAUTION MESSAGE. MX RESET SYSTEM, CHECKED RIGGING OF ELEVATOR POSITION TRANSMITTER, FOUND TO BE WITHIN LIMITS. TEST FLOWN TO BE GOOD. 2L72 4F RTA21EA 20051024001172005102400117EA 2005 10 24 MASA200500800 120051013A33501317 BULB CNDAIRCL600 CL6002D24 1390016EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07916FJ 15016 ASH 6104 PHX - RT AFT EXTERIOR EMERGENCY EXIT LIGHT INOP. MX RELAMPED. 2L72 4F RTA21EA 20051024001182005102400118EA 2005 10 24 MASA200500810 120051015A5220 WARNING LIGHT CNDAIRCL600 CL6002D24 1390016EA EMERGENCY EXIT FALSE ACTIVATIONA MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW07903FJ 15003 ASH 6680 LAS - LT AFT OVERWING EMERGENCY EXIT DOOR CAUTION MESSAGE. MX REMOVED AND REINSTALLED EXIT DOOR, NO FURTHER DEFECTS NOTED. 2L72 4F RTA21EA 20051024001202005102400120EA 2005 10 24 MASA200500753 120050925A3260 WARNING SYSTEM CNDAIRCL600 CL6002D24 1390016EA MLG FALSE ACTIVATIONA MASAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW07938LR 15038 ASH 6143 LGB - GEAR DISAGREE WARNING MESSAGE AND GEAR WOULD NOT RETRACT. CREW DECLARED EMERGENCY AND LANDED UNEVENTFULLY. MX PERFORMED GEAR SWING OPS CHECK NORMAL. 2L72 4F RTA21EA 20051024001222005102400122WP 2005 10 24 0501531224 120051013A2120 SMOKE DOUG DC10 DC1030 3023501WP COCKPIT DETECTED A NWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL01224NW 46581 DURING CRUISE SMELLED ELECTRICAL FUMES IN COCKPIT AND OBSERVED SMOKE AROUND FLOOR BEHIND F/O SEAT. FOLLOWED COM LIST TO "RECIRC FANS OFF" AND SMOKE DISSIPATED. DID NOT RE-OCCUR FOR REMAINDER OF FLIGHT WITH CIRC FANS OFF. FLIGHT CONTINUED TO MEM AND LANDED WITHOUT INCIDENT. CHECKED RECIRC FANS WITH FULL LOAD FOR 3 HRS. CHECKED WIRING UNDER F/O SEAT. NO ABNORMALITIES FOUND. A/C OK FOR SERVICE. 2L73 4F A22WE 20051024001232005102400123NM 2005 10 24 DL76L050599 120051007A2720285T0014104 MODULE BOEING767 767332 1382001NM RUDDER MALFUNCTIONED A DALAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO27172DN 24775 ON TAXI OUT, RUDDER RATIO LIGHT ILLUMINATED, RTB. FOUND LEFT RUDDER RATIO CHANGER MODULE IN TEST MODE. RESET SAME. 2L72 4F RTA1NM 20051024001242005102400124NE 2005 10 24 DL757050602 220051009A7230 COMPRESSOR BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 1 ENGINE STALLED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27681DA15949 26957 728768 NR 1 ENGINE COMPRESSOR STALL ON CLIMBOUT AT FL140. PULLED PWR BACK AND ENGINE INDS NORMAL. VISUALLY SAW SPARKS FROM TAILPIPE. DID NOT SHUT ENG DOWN. REPLACED ENGINE DUE TO INTERNAL DAMAGE. 2L72 4F4 FRTA2NM E17NE 20051024001302005102400130NM 2005 10 24 DL75K050610 120050923A5330143N31512 SKIN PANEL BOEING757 757232 1384965NM BS 520 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27610DL 22817 LIGHTNING STRIKE DAMAGE TO THE FUSELAGE SKIN AT FS 520 ABOVE STR 10R. INSTALLED REPAIR DOUBLER PER ER/A 450613-14. 2L72 4F RTA2NM 20051024001362005102400136WP 2005 10 24 UPS05845620 120051012A53403619434U1 FITTING DOUG DC8 DC873F 302199FWP BS 1490 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 FOUND CRACKED LONGERON END FITTING AT STA 1490 L33R. REMOVED LONGERON AND END FITTING IAW SRM 51-1-20D. INSTALLED LONG TRAVERSE SKIN SPLICE FITTING IAW SRM 51-1-20D AT STA 1490 L33R. 2L74 4F RT4A25 20051024001402005102400140WP 2005 10 24 UPS05845625 120051019A2150 CONTROL VALVE DOUG DC8 DC873F 302199FWP LEFT PACK BYPASSING A IPXAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO01814UP 46090 FLT CREW REPORTED SMOKE IN COCKPIT AND PERFORMED AN EMERGENCY EVACUATION VIA ESCAPE SLIDE. SLIDE DEPLOYED NORMALLY. CREW REPORTED LEFT PACK TRIP PRIOR TO SMOKE IN C/P. LEFT PACK TRIP LIGHT ILLUMINATED. FOUND LEFT PACK S/O AND FLOW CNTRL VLV BYPASSING WHEN SELECTED CLOSED. REMOVED AND REPLACED VALVE IAW DC8 MM 21-55-05-4. PERFORMED 4 ENG TO DUPLICATE FLT. CREW CONDITIONS. NO ABNORMAL CONDITIONS NOTED. LEFT AND RIGHT A/C PACKS OPERATING NORMALLY. NO SMOKE/SMELLS NOTED. 2L74 4F RT4A25 20051024001412005102400141NM 2005 10 24 UPS05M45623 120051017A5753 WEB DOUG MD11 MD11F 3023600NM INBD LT FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 FOUND 6 INCH CRACK OF INBD LT FLAP OUTBD CLOSURE WEB. IAW EO MD11-5750-23071-A CUT OUT DAMAGE AREA. ACCOMPLISHED EFEC, NO CRACKS FOUND. INSTALLED REPAIR DOUBLER PER EO MD11-5350-23071-A CONSIDERED PERMANENT REPAIR PER EO REPEAT INSP REQ'D EVERY C CK. EVERY C CHECK. REF D312135. 2L73 4F RTA22WE 20051024001472005102400147WP 2005 10 24 IXXA05SMN168S 120050810A5330 SKIN DOUG DC8 DC873F 302199FWP BS 80 CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL948072897 46003 DURING ROUTINE C CHECK INSPECTION, FWD CARGO COMPT INTERNAL SKIN CORRODED, STA 80.000, L-31R. DURING ROUTINE C CHECK INSPECTION, FWD CARGO COMPT INTERNAL SKIN CORRODED, STA 80.000 , L-31R. REMOVED SKIN IAW DC-8 SRM 51-1-21 PAGE 1. REMOVED LEVEL I CORROSION IAW DC-8 SRM 51-1-8 PAGES 17-18. MEASURED: BLEND OUT 0,002. MATERIAL MUCKINESS 0,063" REMAINING MATERIAL 0,061". FOUND WITHIN ALLOWABLE LIMITS IAW DC-8 SRM 53-2-0 FIG 1F. CLEANED, TREATED AND PRIMED IAW DC-8 SRM 51-1-8B. 2L74 4F RT4A25 20051024001542005102400154NM 2005 10 24 SWAA053205 120051015A53156546811 FLOORBEAM BOEING737 7373H4 1384600NM BS 986 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 986, BETWEEN LBL 45 TO RBL 45. REPAIRED FLOORBEAM PER BFG ER. 2L72 4F RTA16WE 20051024001562005102400156EA 2005 10 24 COMA0560556 120051015A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT OUT OF ADJUST A COMAO OTHER O OTHER NRNOT REPORTED 1 SO01920CA 7022 FLIGHT 5714 - FWD SECTION OF EMERGENCY FLOOR LIGHTING IS INOPERABLE. ADJUSTED LIGHT STRIP. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051024001602005102400160NM 2005 10 24 AWXA200501220 120051013A3350321431 BATTERY AIRBUSA319 A319132 3930340NM EMERGENCY LIGHT INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28816AW 1350 LAS - EEL - DURING OVERNIGHT INSPECTION DISCOVERED THE AFT EMERGENCY FLASH LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY IN THE AFT EMERGENCY FLASHLIGHT. OPERATIONAL CHECKS WERE NORMAL. 2L72 4F RTA28NM 20051024001612005102400161NM 2005 10 24 AWXA200501223 120051013A2913 PUMP AIRBUSA319 A319132 3930340NM HYD SYSTEM FAILED A AWXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP28813AW 1223 STL - DIVERSION - DURING CRUISE, EN ROUTE TO PHL FROM PHX, CREW REPORTED THE NR 1 ENGINE GREEN YD PUMP FAULT. AIRCRAFT DIVERTED INTO STL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE RAN ENGINE AND PERFORMED OPERATIONAL TESTS WITH NO DEFECTS OR LEAKS BEING NOTED. AIRCRAFT CONTINUED TO PHL. 2L72 4F RTA28NM 20051024001632005102400163NM 2005 10 24 AWXA200501225 120051014A3397BMS13311122 WIRE BOEING737 7373G7 1384595NM EMERGENCY LIGHT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 PHX - EEL - DURING OVERNIGHT INSPECTION DISCOVERED THE EMERGENCY EXIT PATH LIGHT AT ROW 12 WAS INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE UNDER ROW 12. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20051024001672005102400167NM 2005 10 24 ASMF200510008 120051014A325159142965507 VALVE DOUG MD88 MD88 3023688NM NLG STEERING FAILED W ASMFD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SW23158PL26824 49761 CAPTAIN REPORTED THAT IT WAS DIFFICULT TO TURN THE NOSE GEAR STEERING WHEEL TO THE RIGHT, NOT REACHING 74 DGS OF TURN. AIRCRAFT WAS SENT TO THE HANGAR AND THE NOSE WHEEL STEERING HYDRAULIC CONTROL VALVE WAS ADJUSTED IAW MM 32-52-01 AND THE STEERING WHEELS WERE CHECKED IAW MM 32-50-00. DURING OVERNIGHT CHECK, THE NOSE WHEEL STEERING HYDRAULIC CONTROL VALVE WAS REPLACED AND TRIMMED. DUE TO FAILURE CONTINUED, THE SEQUENCE GEAR VALVE, STEERING ACTUATORS AND BYPASS VALVE WERE REPLACED. THE STEERING AND NOSE LANDING GEAR EXTENSION/RETRACTION TESTS WERE PERFORMED IAW MM 32-50-00 AND MM 32-30-00 RESPECTIVELY, BEING CORRECT. 2L72 4F RTA6WE 20051024001692005102400169NM 2005 10 24 ASMF200510011 120051016A80127755386 START VALVE BOEING757 7572Q8 1384972NM LEFT SIDE MALFUNCTIONED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23804AM156937387 26271 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING LEFT ENGINE START, THE STARTER VALVE LIGHT TURNED ON AND EICAS MESSAGES, L ENG STARTED. DISPLAYED WITH START SELECTOR IN GND, ENGINE FAILED TO ROTATE. THE BREAKERS WERE RESEATED AND THE LEFT ENGINE WAS STARTED IN MANUAL MODE, BEING CORRECT. THE REPORT WAS DEFERRED IAW MEL 80-00-2. DURING OVERNIGHT CHECK, THE LEFT START VALVE WAS REPLACED IAW MM 80-11-02, TESTED CORRECT. DEFERRED REPORT WAS CLOSED. 2L72 4F RTA2NM 20051024001712005102400171EA 2005 10 24 SWIA200515679 120051014A5610 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAO OTHER O OTHER CRCRUISE 1 NM07409SW 7056 CAPTAIN'S SIDE WINDOW CRACKED. CAPT'S SIDE WINDOW INSTALLED IAW MM 56-11-00, 56-12-01, PN/OFF NP-139322-5 SN/OFF 01144H8545. 2L72 4F RTA21EA 20051024001762005102400176EA 2005 10 24 SWIA200515684 120051010A27604916406 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07426SW9072 9072 7468 FLIGHT SPOILER FAULT STATUS MESSAGE DURING FLIGHT. REPLACED NR 2 SECU IAW MM 27-61-05, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051024001772005102400177EA 2005 10 24 SWIA200515685 120051013A2741 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA ELEVATOR MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07965SW 7871 CAPTAINS ELEVATOR TRIM SWITCH DOES NOT PITCH NOSE DOWN. REPLACED CAPT TRIM SWITCH REF, CRJ MM 27-41-05, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051024001792005102400179EA 2005 10 24 SWIA200515687 120051009A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07597SW 7293 EMERGENCY OVERHEAD LIGHT INOP 2ND BACK FROM FRONT. REPLACED LAMP. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051024001822005102400182NM 2005 10 24 QXEA200501330 120051007A5230 STOP FITTING DHAV DHC8 DHC8202 2809007NM CARGO DOOR CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09362PH 518 PDX - BOTH UPPER BAG DOOR STOP FITTINGS CHAFED. INSTALLED NEW UPPER STOP FITTINGS IAW RD 8/53/7447, PAGE 3, STEP 5. 2H72 4T RTA13NM 20051024001832005102400183NM 2005 10 24 DL73S050614 120051013A53156545410513 FLOORBEAM BOEING737 737232 1384475NM BS 660 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27329DL 23101 THE LBL 24 LONGITUDINAL OVERWING FLOORBEAM WAS MODIFIED USING A PREVIOUSLY ACCEPTALBE C-CHANNEL THAT IS NOT ACCEPTABLE PER AD 2001-17-18. CRACKS WERE FOUND IN THE BEAM AFT WEB AND WEB DOUBLER. C-CHANNEL WAS REPLACED. WEB REPAIR DOUBLER WAS INSTALLED, AND CRACKS WERE REMOVED PER ER/A 451073-14AD. 2L72 4F RTA16WE 20051024001852005102400185NM 2005 10 24 DL73S050616 120051014A24300802032501 TRANSFORMER BOEING737 737232 1384475NM NR 1 FAILED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27334DL 23105 EN ROUTE TO DFW FROM CVG, FLT ATTENDANTS REPORTED ELECTRICAL SMOKE SMELL IN CABIN. FLT DIVERTED TO LIT WITHOUT FURTHER INCIDENT. NOTED ON POST FLT INSP, NR 1 TRANSFORMER RECTIFIER CIRCUIT BREAKER POPPED. FOUND NR 1 TRANSFORMER RECTIFIER AS SOURCE OF ELECTRICAL SMOKE SMELL. REPLACED SAME, OPS CHECKS OK. ELECTRICAL SMELL DISSIPATED. 2L72 4F RTA16WE 20051024001872005102400187GL 2005 10 24 DL764050618 220051009A7200CF680C2B8F ENGINE BOEING767 767432ER 1385134NM GE CF6 CF680C2* GL NR 1 FAILED A DALAD RETURN TO BLOCK RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SO27841MH15980 706203 29714 706203 LEFT ENGINE EGT STAYING AROUND 687 DEG CELSIUS AND N2 IS AT 75.5 ENG WILL NOT ACCEL. METAL SIZE OF BB-S CAN BE SEEN IN THE AFT TURBINE SECTION. BOROSCOPE REVEALED HPC DAMAGED. THE T/E OF THE HPT SHOWED EVIDENCE OF FOD DAMAGE. REPLACED ENGINE. 2L72 4F4 FRTA1NM E23EA 20051024001882005102400188NM 2005 10 24 DLM88050620 120051015A2910AE7055381 LINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE HYD SYSTEM CRACKED A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO27947DL 49878 726021 LEFT HYD SYS PRESSURE AND QUANTITY DROPPED TO ZERO IN FLIGHT. REPLACED HYD SUPPLY LINE TO NUMBER 1 ENGINE HYD PUMP. 2L72 4F4 FRTA6WE E9NE 20051024001892005102400189NM 2005 10 24 DLM90050622 120051016A3213 STRUT DOUG MD90 MD9030 3023690NM NLG DISCHARGED A DALAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 SO27906DA 53386 FELT JOLT/SHUTTER JUST AFTER TAKEOFF RAISING GEAR HANDLE. THOUGHT PROBLEM MIGHT BE WITH NOSE GEAR, HOWEVER JOLT/SHUT FELT FROM COCKPIT TO AFT FLT ATTENDANT STA. ALL COCKPIT IND NORMAL THROUGHOUT FLT. RETURNED TO SLC. SERVICED NOSE GEAR PER MM 31-21-01. CYCLED NOSE GEAR SEVERAL TIMES, OPERATION AND IND CHECKED NORMAL. RAISED AND LOWERED FLAP AND CYCLED ALL MOVEABLE FLT CONTROLS. ALL CHECKED NORMAL. 2L72 4F RTA6WE 20051024001922005102400192 2005 10 24 HNAA0500089 420051007A3442 RADAR DHAV DHC8 DHC8102 2809003NM WX SYSTEM INOPERATIVE A HNAAA UNSCHED LANDING O OTHER CRCRUISE 1 EA07942HA 163 WEATHER RADAR SPOKING, WILL NOT RETURN KNOWN WEATHER. REPLACED RADAR R/T ANTENNA. MORE TO FOLLOW (P/N'S AND S/N'S) 2H72 4T RTA13NM 20051024001932005102400193NE 2005 10 24 HNAA0500090 320051008A6111021200249891 TAPE DHAV DHC8 DHC8102 2809003NM HAMSTD14SF 14SF7 NE ZONE 400 PEELING A HNAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA07975HA9404 9404 176 910731 RETURN TO FIELD DUE TO NOISE FROM LEFT PROP. FOUND EROSION TAPE PEELING OFF BLADE. 2H72 4T RTA13NM 6 CP7NE 20051024001962005102400196SO 2005 10 24 RAIA00510011 120051009A2497 WIRE EMB 145 EMB145LR 3260212SO ELECTRICAL BURNED A RAIAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 CE03823HK 145475 FLT 7977 - RIC - PILOT REPORTED STRONG ELECTRICAL BURNING SMELL FROM FRONT OF AIRCRAFT JUST AFTER DEPARTURE. MAINTENANCE INSPECTED THE FORWARD SECTION OF THE AIRCRAFT FOR SIGNS OF HEAT/BURNING WIRES AND RAN ALL ELECTRICAL SYSTEMS. NO DEFECTS NOTED. 2L72 4T RTT00011AT 20051024001972005102400197SO 2005 10 24 RAIA00510013 120051008A3350 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03837HK 145255 PREFLIGHT - STL - CEILING EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE LIGHT BULB. 2L72 4T RTT00011AT 20051024001982005102400198SO 2005 10 24 RAIA00510012 120051008A3397 CONNECTOR EMB 145 EMB145 3260210SO EMERGENCY LIGHT LOOSE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03802HK 145066 PRE-FLIGHT INSPECTION - STL - EMERGENCY LIGHT OUT AT ROW 12. MAINTENANCE RESEATED CONNECTOR ON LIGHT ASSY. 2L72 4F RTT00011AT 20051024002002005102400200NM 2005 10 24 DHL2005742501 120050916A5753 SKIN BOEING727 727225 1384077NM TE FLAPS DAMAGED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15742DH 21290 LEFT O/B FLAP I/B END LEADING EDGE GROOVED AND CHAFED. FABRICATED EXTERNAL REPAIR 4 X 4 INCHES FROM 2024-T3 .050. LOCATED, DRILLED, DEBURRED IAW B727 SRM 57-50-4, ALODINED AND PRIMED REPAIR IAW B727 SRM 51-10-2, INSTALLED DOUBLER REPAIR IAW B727 SRM 51-30-2 AND 57-50-4 ON LEFT O/B FLAP I/B END LEADING EDGE. 2L73 4F A3WE 20051024002082005102400208NM 2005 10 24 DHL2005742511 120050913A5330 SKIN BOEING727 727225 1384077NM BS 947 DENTED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15742DH 21290 RIGHT FWD LOWER HALF OF FUSELAGE EXTERIOR SKIN HAS DENT STA 947 BELOW STRINGER 27R. FOUND A=1.100 Y + .028 = 39 NOT IN LIMITS IAW B727 SRM 53-30-1. REMOVED WEB, CUT OUT DENT, FABRICATED AND INSTALLED REPAIR DOUBLER 9.5 X 7.5 INCHES FROM 20240-T3 .050 IAW B727 FRM 53-30-3 FIG 1, AND 51-30-2. 2L73 4F A3WE 20051025000032005102500003SO 2005 10 25 SWIA200515710 120051012A3397 WIRE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT ARCED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM07289YV 120289 FA REPORTS BURNING ODOR NEAR FA SEAT. FOUND LOOSE WIRE ON RED FLOOR EMERGENCY LIGHT ARCING. REPLACED HARDWARE NO DEFECTS NOTED. 2L72 4T RTA31SO 20051025000052005102500005EA 2005 10 25 SWIA200515712 120051014A2760 PRESSURE SWITCH CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION LDLANDING 1 NM07426SW 7468 LEFT FLIGHT SPOILER CAUTION ON TOUCHDOWN AT SLC. REPLACED HYDRAULIC PRESSURE SWITCHES IAW MM 29-34-1. REPLACED LT IB PCU IAW MM 27-62-01. REPLACED NR 1 AND NR 2 SECU'S. OPERATIONAL CHECK GOOD IAW 27-61-05, PN 27000-7 SN/OFF 4704, PN 49-164-05, SN/OFF 00156, PN 49-164-05, SN/OFF 1137. 2L72 4F RTA21EA 20051025000062005102500006WP 2005 10 25 ABXA050254 120051007A53119919619505 FRAME DOUG DC9 DC941 302207NWP CABIN CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23967AX 47509 ADDITIONAL CRACK FOUND IN LEFT AFT MAIN FRAME FORWARD FLANGE. FRAME IS OUT OF REPAIR LIMITS IAW ES00916 DUE TO CRACKS IN BOTH FLANGES. REPLACED MAIN FRAME ON EA 53400325-001-5. 2L72 4F A6WE 20051025000072005102500007WP 2005 10 25 ABXA050251 120051006A57555910055515 FITTING DOUG DC9 DC941 302207NWP SPOILER CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23967AX 47509 LEFT INBOARD SPOILER HAD AN APPROXIMATE .1562 INCH CRACK IN THE CENTER DOUBLER ABOVE THE CENTER DRIVE FITTING. BLENDED CRACK IAW REA D957-52510. 2L72 4F A6WE 20051025000092005102500009WP 2005 10 25 ABXA050253 120051006A53405913093501 SUPPORT FITTING DOUG DC9 DC941 302207NWP BS 1219 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23967AX 47509 LEFT SUPPORT FITTING CRACKED CANTED BULKHEAD 1219, LT OF RUDDER TORQUE TUBE MECHANISM. REMOVED AND REPLACED FITTING IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 20051025000272005102500027NM 2005 10 25 SWAA053281 120051020A53116520722 FRAME BOEING737 7373H4 1384600NM BS 440 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051025000312005102500031WP 2005 10 25 AALA20050691 120051019A3350 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW21228AA 49178 SFO - DURING OVERNIGHT MAINTENANCE FOUND EMERGENCY CEILING LIGHTS ROWS 23-26 INOPERATIVE. REPAIRED BROKEN WIRE AT EMERGENCY POWER SUPPLY AT ROW 26 RIGHT HAND SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051025000342005102500034NM 2005 10 25 TSAA0527048 120051019A276065449617 ACTUATOR BOEING737 7372T4 1384492NM PWA JT8 JT8D9A 52048NE NR 1 SPOILER LEAKING A TSAAO OTHER O OTHER CRCRUISE 1 WP13808AL 23445 CREW HAD INDICATION OF HYDRAULIC SYSTEM A, DROP IN PRESSURE. CREW DECLARED AN EMERGENCY AND WERE ABLE TO DEPLOY THE LANDING GEAR. LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 SPOILER ACTUATOR AND INSPECTED AND REPLACED BOTH ENGINE CASE DRAINS, SYSTEM A MODULE AND RETURN FILTERS AND RETURNED THE AIRCRAFT TO SERVICE. 2L72 4F4 F A16WE E2EA 20051025000362005102500036NM 2005 10 25 TSAA0532049 120051018A324065449201 BRAKE BOEING737 7372M6C 1384708NM PWA JT8 JT8D15 52051NE MLG PARKING INOPERATIVE A TSAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13805AL 21809 PILOTS OBSERVED BOTH ANTI-SKID LIGHTS CAME ON IN FLIGHT ONLY WHEN THE LANDING GEAR IS IN THE (OFF) POSITION; LANDED WITH NO DIFFICULTIES. REMOVED AND REPLACED PARKING BRAKE SHUTOFF VALVE ASSEMBLY. MAINTENANCE ALSO FOUND A BAD NR 4 TRANSDUCER AND CURRENTLY WAITING FOR AN ANTI-SKID CONTROL UNIT TO BE REPLACED. 2L72 4F4 FRTA16WE E2EA 20051025000372005102500037WP 2005 10 25 IXXA05SMN177S 120050811A5730 ACCESS DOOR DOUG DC8 DC873F 302199FWP RT WING CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL948072897 46003 DURING ROUTINE C-CHECK INSPECTION, RIGHT WING SLOT DOOR CRACKED 1, STA XILD 7095 XS 250.089. REMOVED AND REPLACED INBOARD SLOT UPPER DOOR (NEW CONDITION) ON RIGHT WING IAW DC-8 MM 27-80-02 PAGES 201-204. 2L74 4F RT4A25 20051025000382005102500038WP 2005 10 25 IXXA05SMN178S 120050811A5340 FITTING DOUG DC8 DC873F 302199FWP BS 1260-1280 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL948072897 46003 DURING ROUTINE C-CHECK INSPECTION, AFT CARGO COMPT SPLICE FITTING CRACKED 6, STA 1260.000 STA 1280.000 L-34L. REMOVED CRACKED SPLICE FITTING IAW DC8 SRM 51.1.20D PAGE 21. CLEANED, TRETAED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW SPLICE FITTING IAW DC8 SRM 51-1-20D PAGE 9 DC8 SRM 51-3-1. 2L74 4F RT4A25 20051025000392005102500039WP 2005 10 25 IXXA05SMN180S 120050812A5311 FRAME DOUG DC8 DC873F 302199FWP BS 55 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL948072897 46003 DURING ROUTINE C-CHECK INSPECTION, FWD ACCY CMPT- FRAME CRACKED, STA 55, L-24R. PERFORMED MAJOR REPAIR. REMOVED FASTENERS. TRIMMED OUT DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK CORROSION FOUND AROUND TRIMMED AREA. FABRICATED NEW SEGMENT FRAME (EXTRUSION P/N S2641520) 7075.0.0.071. (02EA) ANGLES (AL 7075.0.0.071) IAW DC8 SRM 53-2-0 FIG 2 (SHEET 5) TR 53-125, DC8 SRM 53-2-0 FIG 2 (SHEET 6), DC8 SRM 53-2-0 FIG 2 (SHEET 7, 8) TR 53-110, DC8 SRM 51-1-4 PAGE 1. PERFORMED HEAT TREATMENT FROM 7075.0 TO 7075 T6 (FRAME SEGMENT, ANGLES) IAW DC8 SRM 51-1-1 PAGES 1, 13, 17. CLEANED, TREATED AND PRIMED AREA, REPAIR PARTS IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS. 2L74 4F RT4A25 20051025000522005102500052WP 2005 10 25 UPS05845639 120051011A53404641326U FITTING DOUG DC8 DC873F 302199FWP BS 1880 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 FS 1880 L36 END FITTING IS CRACKED AT FASTENER HOLE. REMOVED AND REPLACED LONGERON END FITTING IAW SRM 51-1-20D AND SRM 51-1-21. 2L74 4F RT4A25 20051025000542005102500054WP 2005 10 25 UPS05845642 120051020A2750 FLAP SYSTEM DOUG DC8 DC873F 302199FWP WINGS SPLIT A IPXAO OTHER J WARNING INDICATION APAPPROACH 1 SO01874UP 46074 RIGHT HAND INBD FLAP OUTBD HINGE BRACKET COVER FWD PANEL CRACKED. INSTALLED INTERIM AIRWORTHY PANEL IAW EO DC8-5720-23117-A. DEFERRAL D312507 PER EO. REPLACED PANEL IAW MM 57-30. THIS CLEARS D312507. 2L74 4F RT4A25 20051025000562005102500056NM 2005 10 25 UPS05M45637 120050831A5347S4929147 SEAT TRACK DOUG MD11 MD11F 3023600NM BS 855-890 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01280UP 48634 MAIN DECK MID ENTRY AREA, SEAT TRACK ALONG 8.5 RBL, BETWEEN STA 855 AND STA 890, CORROSION FOUND ON BASE. SEAT TRACK BET STA 855 AND 890 CORROSION ON BASE. REMOVED 53-70-00, SEAT TRACK FASTENERS REMOVED, SPLICE CUT AT STA 832 TO 949. REPAIR SPLICE AND SPLICE PLATE FAB 53-70-00. HFEC INSP SATISFACTORY. REPAIR SEAT TRACK REWORKED, HOLE TRANSFERRED TO REPAIR PART, REPROTECTED AND PAINTED. SEAT TRACK EXT REPAIR SPLICE HATS AND SPLICE INSTALLED BET STA 832 TO 949, SRM 51-31-01, 53-70-00. 2L73 4F RTA22WE 20051025000572005102500057NM 2005 10 25 SWAA053291 120051020A3230806002 LOGIC CARD BOEING737 7373H4 1384600NM MLG SYSTEM FAULTY A SWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW29611SW 27697 AIR TURNBACK, UNSAFE LANDING GEAR INDICATION AFTER GEAR RETRACTION. WARNING HORN ALSO SOUNDED. REMOVED AND REPLACED LANDING GEAR M990 LOGIC CARD PER MM. 2L72 4F RTA16WE 20051025000582005102500058NM 2005 10 25 05FDEA03457 120051020A5315 FLOORBEAM BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE BS 344 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25223FE 20935 MAIN CARGO COMP FLOORBEAM CORRODED, STA 344 FROM LBL36 TO RBL18. REMOVED, FABRICATED, ALODINED, PRIMED, PAINTED AND INSTALLED FLOORBEAM REPAIR AT STA 344 FROM LBL36 TO RBL18 ALL IAW SRM 51-30-2, 51-10-2, 51-20-031-7 AND SRZ SR27-53-007.**S/D COMING** 2L73 4F4 FRTA3WE E2EA 20051025000592005102500059NM 2005 10 25 QXEA200501361 120051020A2611 SMOKE WARNING DHAV DHC8 DHC8202 2809007NM INTERMITTENT A QXEAO OTHER N FALSE WARNING CRCRUISE 1 NM09352PH 494 YVR - FLIGHT 2174 INTERMITTENT SMOKE WARNING. MAINTENANCE COMPLIED WITH OPERATIONAL CHECK IAW DHC8-200 AMM TASK 26-15-00-710-801. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051025000602005102500060SO 2005 10 25 1398-10142005 120051014A7830GH12AR1G0122C HOSE GULSTMG1159 GIV 3980115SO RROYCETAY TAY6118 EU HYD SYSTEM LEAKING E N93AD RETURN TO BLOCK K FLUID LOSS TXTAXI/GRND HDL 1 SO13498QS5182 1398 LOSS OF FLIGHT SYSTEM HYDRAULIC FLUID AFTER LANDING. FOUND RT THRUST REVERSER DEPLOY LINE LEAKING. 2L72 4F4 FRTA12EA E25NE 20051025000612005102500061CE 2005 10 25 DJFA2005153 120051022A3231 DOOR BEECH MU300 400A 1155402CE MLG MALFUNCTIONED E DJFAL ABORTED APPROACH J WARNING INDICATION LDLANDING 1 EA23792TA RK264 KTUL - KSBN WHILE MAKING A VISUAL APPROACH TO LANDING IN KSBN, THE GEAR WAS SELECTED DOWN AND THE CREW RECEIVED 3 GREEN INDICATIONS, HOWEVER, THE MAIN GEAR DOORS WOULD NOT RETRACT. A MISSED APPROACH WAS EXECUTED. THE SAME INDICATION WAS RECEIVED WHEN THE LANDING GEAR WAS CYCLED. WITH THE LANDING GEAR EXTENDED, A FLY-BY PAST THE TOWER CONFIRMED THAT THE GEAR DOORS WERE NOT RETRACTED. THE CREW THEN PERFORMED AN ALTERNATE GEAR DOOR RETRACTION WHICH SUCCESSFULLY EXTINGUISHED THE GEAR DOOR INDICATION. A FLY-BY PAST THE TOWER CONFIRMED THAT THE GEAR DOORS WERE RETRACTED, AND A LANDING WAS MADE IN KSBN WITHOUT FURTHER INCIDENT. 2H72 4F RTA16SW 20051025000622005102500062SO 2005 10 25 CHQA200500182 120051020A33501317 BULB EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11265SK 145226 MAIN ENTRANCE EMERGENCY COURTESY STAIR LIGHT INOPERATIVE. RELAMPED IAW MM 33-50-6-4. OPS CHECK GOOD. 2L72 4F4 FRTT00011ATTE6CH 20051025000632005102500063SO 2005 10 25 CHQA200500183 120051020A3350 WIRE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL EXIT SIGN LOOSE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11281SK 145391 LT OVERWING EXIT LOCATOR SIGN INOPERATIVE. FOUND LOOSE WIRING AT SP.RE 9126. RECONNECTED IAW MM 33-50-50. OPS CHECK GOOD. 2L72 4T4 FRTT00011ATTE6CH 20051025000642005102500064SO 2005 10 25 CHQA200500185 120051020A3397 WIRE EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT BROKEN A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11834RP 145696 RT EMERGENCY LIGHT ON FAIRING INOPERATIVE. FOUND BROKEN WIRE. REPLACED WIRE IAW WM STANDARD PRACTICES. OPS CHECK GOOD. 2L72 4F4 FRTT00011ATTE6CH 20051025000652005102500065SO 2005 10 25 CHQA200500184 120051018A3397 WIRE EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT BROKEN A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11382SK 145624 EMERGENCY CRAWL STRIP WIRE BROKEN NEAR LAVATORY. REPAIRED BROKEN WIRE, ISNTALLED NEW END IAW WM 145-1520-20-21-00-2. 2L72 4F4 FRTT00011ATTE6CH 20051025000662005102500066WP 2005 10 25 IXXA05SMN175S 120050811A5310 BEAM DOUG DC8 DC873F 302199FWP BS 50 CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL948072897 46003 DURING ROUTINE C-CHECK INSPECTION, FWD ACCY CMPT BEAM CORRODED AT STA 50, RBL 4. PERFORMED MAJOR REPAIR. REMOVED FASTENERS. REMOVED CORROSION, FOUND OUT OF LIMITS. REMOVED CORRODED AREA. PERFORMED NDT INSPECTION IAW DC-8 NDT SPM, PART 06-10-01-001. NO CRACK CORROSION FOUND. FABRICATED REPAIR ANGLE, FILLER (EXTRUSION PN S132S214/7075T6511) IAW DC8 SRM 51-2-1 FIG 1 (SHEET 7, 12), DC8 SRM 53-7-3 FIG 6 SHEET 1, ITEM S DC8 SRM 51-2-0 FIG 50 (SHEET 73). CLEANED, TREATED AND PRIMED AREA, REPAIR PARTS IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11 PAGE 9. INSTALLED REPAIR PARTS IAW DC-8 SRM 51-1-20D PG 9, DC8 SRM 51-1-21 PAGE 1. TORQUED IAW DC8 SRM 51-3-1, DC8 SRM 51-2-1. 2L74 4F RT4A25 20051025000672005102500067WP 2005 10 25 IXXA05SMN176S 120050811A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL948072897 46003 DURING ROUTINE C-CHECK INSPECTION, RIGHT WING UPPER SKIN CRACKED 1, STA XW 74 STR 9. PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW DC-8 SRM 51-1-20D PAGE 21. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION IAW DC-8 NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER & FILLER PLUG. MADE TAPE DOUBLER. OVER 4 INCHES LENGTH TYPICAL CHANFER BOTH ENDS. INSTALLED REPAIR PARTS IAW DC-8 SRM 57-2-1 FIG 10 , DC-8 SRM 51-1-20D PAGE 9 , TORQUED IAW DC-8 SRM 51-3-1. 2L74 4F RT4A25 20051025000682005102500068WP 2005 10 25 IXXA05SMN181S 120050812A5311 FRAME DOUG DC8 DC873F 302199FWP BS 80 CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL948072897 46003 DURING ROUTINE C-CHECK INSPECTION, FWD CARGO CMPT FRAME CORRODED, STA 80.000, L-26L. PERFORMED MAJOR REPAIR. REMOVED FASTENERS. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FRAME SEGMENT (CORRODED). PERFORMED NDT INSPECTION. NO CRACK, CORROSION FOUND AROUND TRIMMED AREA. FABRICATED NEW SEGMENT FRAME. ANGLE SPLICE. PERFORMED HEAT TREATMENT TO FRAME SEGMENT, ANGLE & SPLICE. PERFORMED NDT INSPECTION REPORT TO NEW FRAME SEGMENT. INSTALLED REPAIR PARTS. 2L74 4F RT4A25 20051025000702005102500070NM 2005 10 25 USAA051227 120051021A5320BAC15063384 FLOOR SUPPORT BOEING757 7572B7 1384964NM BS 345-365 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19619AU 27198 FOUND FLOOR SUPPORT STA 345 AND 365.25 BL 0; CORROSION LEVEL 1; TASK C53-322-03. INSTALLED NEW BEAM PER BOEING DWG 141N5191, SRM 51-30-05, 51-40-02 AND 51-30-05, DEFECT SIZE: 1.5" BY 1" BY 0.012" AREA. 2L72 4F RTA2NM 20051020000032005102000003NM 2005 10 20 72400006 120051012A5320 WEB BOEING727 727225 1384077NM FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23724CK 20383 A 2 X 10 INCH AREA OF CORROSION ON WEB. 2L73 4F A3WE 20051020000102005102000010NM 2005 10 20 724000013 120051005A5320 BRACE BOEING727 727225 1384077NM FUSLEAGE CRACKED A K11AK NONE O OTHER ININSP/MAINT 1 GL23724CK 20383 CRACK IN BRACE. 2L73 4F A3WE 20051020000122005102000012NM 2005 10 20 724000015 120051005A5330 DOUBLER BOEING727 727225 1384077NM FUSELAGE NICKED A K11AK NONE O OTHER ININSP/MAINT 1 GL23724CK 20383 NICK IN DOUBLER. 2L73 4F A3WE 20051020000162005102000016EA 2005 10 20 MASA200500711 120050907A2710 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA AILERONS ILLUMINATED A MASACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 SW07508MJ 10087 ASH 7110 IAD. RETURNED TO THE GATE DUE TO AILERON CONFIG MESSAGE ON TAKEOFF ROLL. MAINTENANCE RESET SYSTEM, OPS TEST GOOD. 2L72 4F RTA21EA 20051020000212005102000021NM 2005 10 20 SWAA053219 120051017A53116546557 FRAME BOEING737 7373H4 1384600NM BS 887 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051020000372005102000037EA 2005 10 20 MASA200500721 120050910A2711CC670511143 CONTROL PANEL CNDAIRCL600 CL6002C10 1390015EA TRIM SYSTEM MALFUNCTIONED A MASAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SW07508MJ1934 1934 10087 ASH 7134 MCI. THE CREW ABORTED TAKEOFF DUE TO A CONFIGURE AILERON WARNING MESSAGE UPON INITIATING TAKEOFF ROLL. MX REMOVED AND REPLACED AILERON/RUDDER CONTROL PANEL. 2L72 4F RTA21EA 20051020000532005102000053NM 2005 10 20 AWXA200501229 120051003A531565468046 FLOORBEAM BOEING737 7373S3 1384711NM BS 727B CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 DURING C18 CHECK DISCOVERED CRACK, .25 INCHES IN LENGTH, ON FLOORBEAM AT BS 727B AND BL 45L. MAINTENANCE TRIMMED OUT CRACK AT BS 727B AND BL 45L IAW AMERICA WEST AIRLINES ENGINEERING REQUEST NR 03-5702-05284-SS2. FABRICATED FILLER, REPAIR STRAPS AND SHIMS IAW AWA ER NR 03-5702-05284-SS2. INSTALLED FABRICATED REPAIR PARTS AT BS 727B AND BL 45L IAW AWA ER NR 03-5702-05284-SS2. 2L72 4F RTA16WE 20051020000572005102000057NM 2005 10 20 AWXA200501233 120051004A5312651630088 BULKHEAD BOEING737 7373S3 1384711NM BS 178 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 DURING C18 CHECK DISCOVERED WEB CRACKED, 1.5 INCHES IN LENGTH, AT BS 178 FROM BL 17.5L TO BL 29.5L AND FROM WL 184.5 TO WL 240. MAINTENANCE REMOVED CRACKED WEB FROM BS 178 IAW BOEING 737-300 SRM 51-40-02-0G. FABRICATED NEW WEB IAW BOEING 737-300 SRM 51-30-01-0G AND DWG 65-16300. INSTALLED FABRICATED REPAIR PARTS AT BS 178 FROM BL 17.5L TO BL 29.5L AND FROM WL 184.5 TO WL 240 IAW BOEING 737-300 SRM 51-40-02-0G. 2L72 4F RTA16WE 20051020000632005102000063NM 2005 10 20 AWXA200501239 120050923A53206916970501 ANGLE BOEING737 7373S3 1384711NM BS 348 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 DURING C18 CHECK DISCOVERED ANGLE CRACKED, .05 INCHES IN LENGTH, AT BS 348 AND STR 15L. MAINTENANCE REMOVED CRACKED ANGLE IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5310-05285-ES4. FORMED NEW ANGLE IAW AWA ER NO. 03-5310-05285-ES4. INSTALLED FABRICATED REPAIR PARTS AT BS 348 AND STR 15L IAW AWA ER NR 03-5310-5285-ES4. 2L72 4F RTA16WE 20051020000682005102000068NM 2005 10 20 SWAA053233 120051017A53306545775 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT CARGO DOOR CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051020000692005102000069NM 2005 10 20 SWAA053234 120051016A2560PH22300L GLOWSTRIP BOEING737 7373H4 1384600NM ROW 7 WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29629SW 27704 DURING SCHEDULED C4 CHECK, FOUND PHOTOLUMINESCENT STRIP WORN AT ROW 7. REMOVED AND REPLACED STRIP PER MM. 2L72 4F RTA16WE 20051020000722005102000072NM 2005 10 20 SWAA053237 120051014A53306545765 SKIN BOEING737 7373Q8 1384670NM BS 514 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 514, STR 10R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051020000732005102000073NM 2005 10 20 SWAA053238 120051014A53306545774 SKIN BOEING737 7373Q8 1384670NM BS 741 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 741, STR 19R. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20051020000752005102000075NM 2005 10 20 SWAA053240 120051015A53306545774 SKIN BOEING737 7373Q8 1384670NM BS 740 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 740, STR 18R. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20051020000782005102000078EA 2005 10 20 MASA200500173 120050303A2741 WARNING LIGHT CNDAIRCL600 CL6002D24 1390016EA STAB TRIM ILLUMINATED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07914FJ 15014 ASH 6043 PDX TO LAS. DECLARED EMERGENCY DUE TO STAB AND MACH TRIM CAUTION MESSAGE. MAINTENANCE COMPLIED WITH THE SPOST AND NO FURTHER FAULTS NOTED. 2L72 4F RTA21EA 20051020000832005102000083EA 2005 10 20 MASA200500309 120050421A27505913164 SENSOR CNDAIRCL600 CL6002D24 1390016EA TE FLAPS MALFUNCTIONED A MASAO OTHER J WARNING INDICATION CRCRUISE 1 SW07904FJ 15004 ASH 6588 SAN TO PVR. THE CREW REPORTED FLAPS FAIL IN FLIGHT. MX R2 RIGHT OUTBOARD FLAP OUTBOARD SKEW SENSOR. 2L72 4F RTA21EA 20051020000912005102000091EA 2005 10 20 MASA200500494 120050627A3244 TIRE CNDAIRCL600 CL6002D24 1390016EA NLG FAILED A MASAO OTHER E VIBRATION/BUFFET TOTAKEOFF 1 SW07918FJ899 15018 ASH 6152 MEM - DURING TAKEOFF, THE PILOT HARD A LOUD SOUND FROM THE A/C NOSE AREA. ONCE THE A/C ARRIVED IN PHX, MX FOUND THAT THE NOSE TIRE WAS BLOWN AND THE NOSE LANDING GEAR WAS DAMAGE BY THE RUBBER. MX REPLACED THE TIRE. 2L72 4F RTA21EA 20051020000932005102000093NM 2005 10 20 05FDEA03428 120051013A5753 HINGE FITTING DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 LT WING OUTBOARD FLAP INBOARD HINGE FITTING OUTBOARD NR 1 BOLT HOLE FROM FORWARD FOUND CORROSION. REPAIR ACCOMPLISHED PER EA 1-5750-93247. 2L73 4F RTA22WE 20051020001022005102000102NM 2005 10 20 05FDEA03422 120051013A5340 STRINGER CLIP BOEING727 72722 1384002NM BS 380 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 FOUND MAIN CARGO COMPARTMENT STRINGER CLIP GOUGED BS 380 STR 6R. REMOVED AND REPLACED MAIN CARGO COMPARTMENT STRINGER CLIP BS 380, STR 6R IAW SRM 51-30-2. 2L73 4F A3WE 20051020001042005102000104NM 2005 10 20 05FDEA03424 120051013A5313 STRINGER BOEING727 72722 1384002NM BS 480 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 FOUND UPPER LOBE INTERIOR STRINGER IS CRACKED BS 480 STR 16R. REMOVED AND REPLACED WITH NEW STR. SECTION IAW SRM 53-30-2 AND SRM 53-10-4. 2L73 4F A3WE 20051020001122005102000112EA 2005 10 20 MASA200500512 120050702A5220 HANDLE CNDAIRCL600 CL6002D24 1390016EA EMERGENCY DOOR LOOSE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07909FJ 15009 ASH 6040 PHX - EMERGENCY DOOR HANDLE COVER WAS FALLING OFF. MAINTENANCE RESECURED THE HANDLE COVER. 2L72 4F RTA21EA 20051024000082005102400008NM 2005 10 24 SWAA053258 120051019A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29374SW 26582 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051024000092005102400009NM 2005 10 24 SWAA053259 120051019A5310573149 WINDOW POST BOEING737 7373H4 1384600NM COCKPIT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29374SW 26582 DURING SCHEDULED 1/4D CHECK, FOUND R1 COCKPIT WINDOW UPPER POST CRACKED. REPAIRED WINDOW POST PER SRM. 2L72 4F RTA16WE 20051024000162005102400016NM 2005 10 24 SWAA053266 120051019A53116546552 FRAME BOEING737 7373H4 1384600NM BS 827 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 6L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051024000182005102400018NM 2005 10 24 05FDEA03441 120051017A5330 SKIN BOEING727 72722 1384002NM BS 235-245 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 FOUND EXTERNAL SKIN CRACKED AT F/O'S NR 5 WINDOW CUT OUT AT UPPER AFT FASTENER HOLE. INSTALLED REPAIR DOUBLER F/O'S NR 5 WINDOW CUT OUT UPPER AFT CORNER IAW SRM 53-30-3. 2L73 4F A3WE 20051024000252005102400025EU 2005 10 24 B65A106298 120051012A6200105627794 SHIELD BOLKMS105 BO105LSA1 5626021EU ALLSN 250C 250C28 03013GL MAIN ROTOR BROKEN E B65AO OTHER O OTHER NRNOT REPORTED 1 GL13202LF 2014 SHIELD, BROKEN AND REPLACED. 1G72 3U3 U H3AU E1GL 20051024000372005102400037NM 2005 10 24 AWXA200501252 120051019A33501012721 LIGHT BOEING737 7373G7 1384595NM CABIN BROKEN A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28156AW 23778 DFW - EEL - ON GROUND CREW REPORTED THAT THE EMERGENCY EXIT LIGHT AT 5C WAS BROKEN. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AT SEAT 5C. OPERATIONAL TESTS WERE GOOD. 2L72 4F RTA16WE 20051024000382005102400038NM 2005 10 24 AWXA200501253 120051019A3397 CONNECTOR BOEING737 7373G7 1384595NM EMERGNECY LIGHT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28311AW 24712 PHX - EEL - DURING OVERNIGHT INSPECTION FOUND SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE AT ROW 3C. MAINTENANCE REPAIRED BROKEN CONNECTOR UNDER SEAT AT ROW 3C. 2L72 4F RTA16WE 20051024000532005102400053CE 2005 10 24 ACE100305 120051003A2997MS24171D1 RELAY BEECH 1900 1900C 1154161CE HYD SYSTEM CONTAMINATED E YADAO OTHER S AFFECT SYSTEMS APAPPROACH 1 AL03112AX74 UC45 PIREP - HAD TO EXTEND LANDING GEAR MANUALLY. MAINTENANCE REPLACED "WATER LOGGED" HYDRAULIC POWER PACK RELAY. 2L72 4T RTA24CE 20051024000612005102400061EA 2005 10 24 SWIA200515697 120051012A2760C13045BA04 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA SPOILER MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07740SK525 525 10196 RECEIVED A -SPLR/STAB FAULT- STATUS MSG. REPLACED SSCU 2 IAW CRJ MM27-61-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051024000642005102400064EA 2005 10 24 SWIA200515700 120051016A274070623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07923SW6438 6438 7664 RECEIVED A -STAB CH 1 INOP- STATUS MSG. REPLACED MOTOR CONTROL UNIT. OPERATIONAL CHECK GOOD REF 27-41-00. 2L72 4F RTA21EA 20051024000682005102400068NM 2005 10 24 SWAA053245 120051018A53116546569 SHEAR TIE BOEING737 7373H4 1384600NM BS 967 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 967, BETWEEN STR 6L TO STR 7L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051024000692005102400069NM 2005 10 24 SWAA053246 120051018A53126546568 BULKHEAD BOEING737 7373H4 1384600NM BS 1016 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D-CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT AFT SIDE, LBL 40, WL 209. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20051024000712005102400071NM 2005 10 24 SWAA053248 120051018A534065C27314 STRINGER CLIP BOEING737 7375H4 138449DNM BS 277 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051024000732005102400073NM 2005 10 24 SWAA053250 120051018A5530BAC15061880 BEAM BOEING737 7373H4 1384600NM VERTICAL STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED D-CHECK, FOUND VERTICAL STABILIZER LEFT T/E BEAM CRACKED AT NR 2 RUDDER HINGE ATTACHMENT. REMOVED AND REPLACED BEAM PER SRM. 2L72 4F RTA16WE 20051024000742005102400074NM 2005 10 24 SWAA053251 120051018A53116520722 FRAME BOEING737 7373H4 1384600NM BS 440 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051024000982005102400098WP 2005 10 24 DJFA2005150 220051016A7261TFE7315BR ENGINE RAYTHNDH125 HAWKER800XP 7150012CE GARRTTTFE731TFE7315BR WP LEFT LEAKING E DJFAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA23733TA5897 3835 258337 P107214 UPON CLIMB-OUT FROM KTEB, LT ENGINE OIL PRESS GAUGE FLUCTUATED BETWEEN 30 AND 40 PSI, AND RT OIL PRESS GAUGE REMAINED STEADY AT 37 PSI. APPROX 30 TO 40 MINS INTO TRIP LT ENG OIL PRESS WAS INDICATING BETWEEN 26 TO 35 PSI. A/C WAS THEN BEING DIVERTED TO KIND, AND A MASTER WARNING ANNUNCIATOR ILLUMINATED WITH NO ASSOCIATED LIGHT TO TRIP MASTER WARNING INDICATION. AT INITIAL DESCENT, THE LT OIL PRESS LOW LIGHT FLICKERED, ALONG WITH THE MASTER WARNING ANNUNCIATOR. DURING DESCENT, OIL PRESS ROSE TO 30-35 PSI AND MAINTAINED THAT PRESS THROUGHOUT FLT. A LANDING WAS MADE IN KIND W/O FURTHER INCIDENT. CREW OPENED THE LT AND RT ENG COWLINGS AND DISCOVERED BOTH ENG OIL CAPS TO BE LAYING IN LOWER COWLING. 2L72 4F4 FRTA3EU E6WE 20051024001022005102400102NM 2005 10 24 DL73S050589 120051003A291065468581103 LINE BOEING737 737232 1384475NM PWA JT8 JT8D15A 52051NE NR 2 ENGINE LEAKING A DALAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 SO27305DL 23077 695239 LOSS OF A SYSTEM HYD, ALT GEAR EXTENSION. REPLACED LEAKING PRESSURE LINE IN RIGHT PYLON. 2L72 4F4 FRTA16WE E2EA 20051024001212005102400121EA 2005 10 24 MASA200500761 120050928A2560MXP21000 SMOKE GOGGLES CNDAIRCL600 CL6002D24 1390016EA COCKPIT CRACKED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07904FJ 15004 ASH 6475 LAX - FO'S SMOKE GOGGLES CRACKED. MX REPLACED SMOKE GOGGLES. 2L72 4F RTA21EA 20051024001252005102400125 2005 10 24 DL76L050603 420051010A2565 GIRT BAR BOEING767 767332 1382001NM R1 DOOR STICKING A DALAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO27178DN 25143 1R ENTRY DOOR SLIDE WILL NOT ARM. LUBRICATED GIRT BAR ARM HANDLE. 2L72 4F RTA1NM 20051024001292005102400129NM 2005 10 24 DL73S050609 120050924A5315 FLOORBEAM BOEING737 737247 138448DNM BS 678 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27375DL 23602 FUSELAGE/OVERWING LONGITUDINAL FLOORBEAMS, CRACK REPAIR DURING ACCOMPLISHMENT OF INSPECTIONS OF THE LT/RT BL 24.8 OVERWING LONGITUDINAL FLOORBEAMS PER SI 3-056673-12AD, FATIGUE CRACKS WERE DETECTED IN THE WEB DOUBLERS AND BS 678 VERTICAL STIFFENER. CRACKED DOUBLERS AND STIFFENERS REPLACED AND INSTALLS 3-056673-3AD MODIFICATION PER ER/A 450791-14AD. 2L72 4F A16WE 20051024001322005102400132NM 2005 10 24 UPS05545626 120051007A2120 UNKNOWN BOEING757 75724APF 1384969NM COCKPIT FUMES A IPXAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO01405UP 23727 FUMES IN COCKPIT DURING PREFLIGHT. COCKPIT CLEARED OF FUMES (CAUSE WAS OTHER DEPARTING FLTS AND CROSS WINDS) POS 3 SPOT 14. 2L72 4F RTA2NM 20051024001782005102400178EA 2005 10 24 SWIA200515686 120051010A3350 INVERTER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSINOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07961SW 7857 FLOOR EXIT SIGN BY SEAT 8A IS INOP. REPLACED NR 2 INVERTER IAW AMM CH 33-51-00. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051024001812005102400181 2005 10 24 SWIA200515689 420051008A22166225027101 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA ELEVATORS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07465SW 7845 CREW REPORTS AUTOPILOT DISCONNECTS IN CRUISE. REPLACED ELEVATOR SERVO IAW 22-11-24. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051025000082005102500008WP 2005 10 25 ABXA050252 120051006A53475418203 SEAT TRACK DOUG DC9 DC941 302207NWP COCKPIT CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23967AX 47509 SEAT TRACK WAS CRACKED 2 PLACES BETWEEN FS 160 AND 200 AT LEFT BUTT LINE 41.5. REPAIRED DAMAGED AREAS (2 EA) IAW DC-9 SSRM DWG K05159. 2L72 4F A6WE 20051025000102005102500010WP 2005 10 25 ABXA050250 120051004A533099234349 SKIN DOUG DC9 DC941 302207NWP BS 626 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23967AX 47509 AREA OF BULGING AND DISHED RIVETS - FS 626 AT LONGERON 26 LEFT. EXFOLIATED DOUBLER ON THE INSIDE, ABOVE HAT CHANNEL. REPAIRED AREA IAW REA D953-52507. 2L72 4F A6WE 20051025000122005102500012NM 2005 10 25 SWAA053272 120051020A53306552988 SKIN BOEING737 7375H4 138449DNM BS 944 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29513SW 24190 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 944, STR 23R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051025000152005102500015NM 2005 10 25 SWAA053275 120051020A55536547450 ATTACH FITTING BOEING737 7373H4 1384600NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D CHECK, FOUND VERTICAL STAB ATTACH FITTING LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER. 2L72 4F RTA16WE 20051025000172005102500017NM 2005 10 25 SWAA053277 120051020A53306545772 SKIN BOEING737 7373H4 1384600NM BS 882-887 WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29347SW 24374 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN WORN AT BS 882 TO BS 887, STR 1R TO STR 2R. REPAIRED SKIN PER BFG ER. 2L72 4F RTA16WE 20051025000192005102500019NM 2005 10 25 SWAA053279 120051020A53116546554 FRAME BOEING737 7373H4 1384600NM BS 847 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29347SW 24374 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT AFT CARGO DOOR CUT OUT BS 847, NR 5 STOP FITTING. REPAIRED FRAME BFG ER. 2L72 4F RTA16WE 20051025000212005102500021NM 2005 10 25 UPS05245632 120051004A5743 FITTING BOEING727 727180C 138406GNM LT MLG TRUNNION CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 INSPECTION TYPE: C, SEVERAL CRACKS ON LT MLG TRUNNION FITTING. REPLACED MLG TRUNNION FITTING IAW AAAE EO = 2005-091-001 AND UPS FILE APPROVAL B727-5740-23096. 2L73 4F A3WE 20051025000232005102500023NM 2005 10 25 UPS05445604 120051014A2897 WIRE BOEING747 747123F NM BS 960 BURNED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 WHILE T/S D311541 FOUND WIRE SPLICES BURNED REF WD W1210-014 BYR, W121 0-001 BYR, W1210-014BYR, W1210-024 BYR, W206-022 BYR, AND W1210-024 BYR. NOTE BYR IS BLUE, YELLOW, AND RED WIRE RUNS, SPLICE LOC IS STA 960 LT. REPLACED DAMAGED WIRES AND SPLICES WITH NEW MATERIAL AND OPS CHECK EAC SYSTEM. 2L74 4F A20WE 20051025000402005102500040NM 2005 10 25 05FDEA03451 120051019A5330 SKIN BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE BS 495 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25265FE 21671 EXTERNAL FUSELAGE SKIN IS DENTED AT RT STA 495 AND STRINGER 20R. REMOVED, FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR ON FUSELAGE EXTERNAL SKIN FROM STA 480 TO 540 FROM STRINGER 20R TO 23R ALL IAW SRM 53-30-1,53-30-2 FIG 2,53-30-3 FIG 3,51-30-2 AND 51-10-2. 2L73 4F4 FRTA3WE E2EA 20051025000412005102500041NM 2005 10 25 SWAA053282 120051020A53116546555 FRAME BOEING737 7373H4 1384600NM BS 867 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051025000422005102500042NM 2005 10 25 SWAA053283 120051020A53116546557 FRAME BOEING737 7373H4 1384600NM BS 907 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051025000432005102500043NM 2005 10 25 SWAA053284 120051020A53156546804 FLOORBEAM BOEING737 7375H4 138449DNM BS 986 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM UPPER CAP CORRODED AT BS 986. REMOVED AND REPLACED FLOORBEAM UPPER CAP PER SWA EA. 2L72 4F RTA16WE 20051025000442005102500044NM 2005 10 25 SWAA053285 120051020A53156546804 FLOORBEAM BOEING737 7375H4 138449DNM BS 360 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 360, BETWEEN RBL 51 TO RBL 61. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20051025000452005102500045NM 2005 10 25 SWAA053286 120051020A53306545766 SKIN BOEING737 7373H4 1384600NM BS 515D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29374SW 26582 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 515D, STR 10R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051025000462005102500046NM 2005 10 25 SWAA053287 120051020A53306545774 SKIN BOEING737 7373T5 1384608NM BS 863 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29694SW 23061 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 863, STR 23R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051025000472005102500047NM 2005 10 25 SWAA053288 120051020A53306545774 SKIN BOEING737 7373T5 1384608NM BS 780 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29694SW 23061 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 780, STR 18R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051025000482005102500048NM 2005 10 25 SWAA053289 120051020A53306545774 SKIN BOEING737 7373T5 1384608NM BS 780 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29694SW 23061 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 780, STR 23L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051025000492005102500049NM 2005 10 25 SWAA053290 120051020A53226546549 SHEAR TIE BOEING737 7373H4 1384600NM BS 867 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29374SW 26582 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPT FUSELAGE SHEAR TIE CORRODED AT BS 867, LBL4 TO RBL 5. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051025000512005102500051WP 2005 10 25 UPS05845636 120051011A5340 FITTING DOUG DC8 DC873F 302199FWP BS 1890 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 C2 BS 1890 L32L END FITTING HAS CORROSION AND ELONGATED HOLES. REMOVED AND REPLACED END FITTING AT FS 1890 L32L IAW SRM 51-1-20D, AND SRM 51-3-2. 2L74 4F RT4A25 20051025000692005102500069NM 2005 10 25 USAA051237 120051021A5315 FLOORBEAM BOEING757 7572B7 1384964NM BS 1640 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19619AU 27198 STA 1640 RBL 56 AND LBL 56 MAIN CABIN FLOORBEAM CORRODED. REPLACED NEW UPPER CHORD AND SPLICE PER TYP REP 53-15-01 AND SRM 51-40-02, DEFECT SIZE: 10" L BY 1.5" W BY .97"D. 2L72 4F RTA2NM 20051025000712005102500071NM 2005 10 25 USAA051228 120051021A5340 MOUNT BOEING757 7572B7 1384964NM BS 1687 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19619AU 27198 AFT GALLEY MOUNT AT BS 1687 LBL 7; CORROSION LEVEL 1; TASK C53-251-03. REMOVED AND REPLACED GALLEY MOUNT PAD PER SRM 51-40-02, DEFECT SIZE: 1 SQ IN. 2L72 4F RTA2NM 20051025000732005102500073EA 2005 10 25 COMA0560561 120051018A2752852D10011 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT WING TE FLAPFAILED A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01818CA14446 7408 FLAPS FAIL. CND REPLACED 4 FLAP ACTUATORS ON LT WING. 2L72 4F4 FRTA21EA E15NE 20051025000742005102500074NM 2005 10 25 CALA0500370 120051020A324026123121 BRAKE BOEING737 737824 13844BZNM NR 1 LEAKING A CALAA UNSCHED LANDING KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW2737263 31583 CLIMBING THROUGH 10,000, FUMES IN COCKPIT. REPLACED LEAKING NR 1 BRAKE PER AMM 32-41-41-400-801. 2L72 4F RTA16WE 20051025000752005102500075NM 2005 10 25 05FDEA02754 120050905A5753 SKIN DOUG MD11 MD11 3023602NM IB FLAP ASSY DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 EXISTING REPAIR DOUBLER FOUND AT RT WING IB FLAP, IB T/E SECTION UPPER SKIN, BETWEEN XIFH 165.300 AND XIFH 171.300. REPAIRED IAW SRM 57-10-00 FIG.34 VOL.I. THIS REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. 2L73 4F RTA22WE 20051025000762005102500076NM 2005 10 25 05FDEA02755 120050905A5753NRC6055508 SKIN DOUG MD11 MD11 3023602NM IB FLAP ASSY DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 EXISTNG REPAIR DOUBLER FOUND AT RT WING IB FLAP IB T/E SECTION UPPER SKIN BETWEEN XIFH 195.300 AND XIFH 201.300. EXISTING REPAIR DOUBLER AT RT WING IB FLAP IB T/E SECTION UPPER SKIN BETWEEN XIFH 195.300 AND XIFH 201.300 REPAIRED IAW SRM 57-10-00 FIG.34 VOL.I. THIS REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. 2L73 4F RTA22WE 20051025000772005102500077NM 2005 10 25 05FDEA03458 120051020A5315 FLOORBEAM BOEING727 727200 138407ENM PWA JT8 JT8D17A 52049NE BS 1166 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25213FE 22935 FLOORBEAM HAS SEVERAL CORRODED FASTENERS NUT PLATES AND SURFACE UNDER NUT PLATES. BS 1166 FROM RBL 27 TO OB END. REMOVED CORRODED NUT PLATES IAW SRM 51-31-2 REMOVED CORROSION IAW SRM51-10-6,CHECKED LIMITS . ORIGINAL MATERIAL: .125 AFTER REWORK: .118 WITH IN LIMITS IAW SRM 53-10--1 PG 1. TREATED AND PRIMED IAW SRM 51-10-2, INSTALLED NUT PLATES IAW SRM 51-30-2. 2L73 4F4 FRTA3WE E2EA 20051025000782005102500078NM 2005 10 25 05FDEA03459 120051020A5200 ACCESS DOOR BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE BULKHEAD OUT OF POSITION A FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25466FE 21292 A/C TOOK OFF AND RETURNED TO GATE. FLT CREW SAID THE A/C WOULD NOT PRESSURIZE. MAIN ENTRY DOOR WAS CLOSED DOOR WAS JAMMED WOULDN'T OPEN. REMOVED DOOR SLIDE DOOR TRIM FOUND THE AFT ROLLERS WERE NOT IN THE ROLLER GUIDES OR IN THE CAMS. FOUND SOLID BULKHEAD ACCESS DOOR INTERFERING WITH ENTRY DOOR WHEN CLOSING. REPOSITIONED BULKHEAD ACCESS DOOR IN ITS TRACK. OPERATED MAIN ENTRY DOOR SEVERAL TIMES OPERATES NORMAL, ROLLERS ENGAGE CAMS AT ALL 4 POSITIONS AND HANDLE GOES OVER CENTER INDICATION NORMAL. 2L73 4F4 FRTA3WE E2EA 20051025000792005102500079NM 2005 10 25 USAA051230 120051021A5340146N8712 SUPPORT ANGLE BOEING757 7572B7 1384964NM STA 1650-1675 RBCORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19619AU 27198 FOUND SUPPORT ANGLES CORRODED STA 1650-1675 RBL 62 WL 208.10 (R-4 DOOR) THRESHOLD; CORROSION LEVEL 1; TASK C53. FABRICATED AND INSTALLED NEW SUPPORT ANGLES PER SRM 51-20-02, 51-40-02, BOEING DWG 146N8712 AND 146N8769 DEFECT SIZE: 0.5" BY 0.37" BY 0.013" AND 0.5" BY 0.37" BY 0. 2L72 4F RTA2NM 20051025000802005102500080NM 2005 10 25 USAA051231 120051021A5340415N40026 MOUNT BOEING757 7572B7 1384964NM BS 1687 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19619AU 27198 FOUND GALLEY MOUNT PAD CORRODED STA 1687 RBL 7; LEVEL 1; TASK C53-252-03. REMOVED AND REPLACED WITH NEW MOUNT PAD PER SRM 51-40-02 DEFECT SIZE: 1 SQ IN. 2L72 4F RTA2NM 20051025000812005102500081NM 2005 10 25 USAA051232 120051021A5315141N517045LF FLOORBEAM BOEING757 7572B7 1384964NM BS 397 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19619AU 27198 FOUND CORROSION STA 397 RBL 51, WL 208.10; CORROSION LEVEL 1; TASK C53-222-03. FABRICATED AND INSTALLED FLOOR SUPPORT PER SRM 53-00-51, 51-40-02, DWG 141N5170, DEFECT SIZE: 4" BY 3" BY .030". 2L72 4F RTA2NM 20051025000822005102500082NM 2005 10 25 USAA051233 120051021A5320146N52421 FLOOR SUPPORT BOEING757 7572B7 1384964NM BS 1640-1661 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19619AU 27198 FOUND FLOOR SUPPORT CORRODED STA 1640-1661 BL 0; CORROSION LEVEL 1; TSK C53-251-03. INSTALLED FABRICATED FLOOR SUPPORT PER SRM 51-10-02, 51-40-02, 51-40-05, DEFECT SIZE: 2" BY 3" AREA. 2L72 4F RTA2NM 20051025000832005102500083NM 2005 10 25 USAA051234 120051021A5320146N52465LF PLATE BOEING757 7572B7 1384964NM BS 1640-1681 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19619AU 27198 FOUND PLATE SUPPORTS CORRODED STA 1640-1681 LBL 57 WL 208.10; CORROSION LEVEL 1; TASK C53-251-03. REMOVED, FABRICATED AND INSTALLED SUPPORTS PER SRM 51-40-02, 53-60-51 FIG 101 AND 51-20-02, DEFECT SIZE: 1" BY 1" AND 1.5" BY 2". 2L72 4F RTA2NM 20051025000842005102500084NM 2005 10 25 USAA051235 120051021A5320146N524681F SUPPORT BOEING757 7572B7 1384964NM BS 1640-1681 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19619AU 27198 FOUND SUPPORT CORRODED STA 1640 AND 1681 RBL 57; CORROSION LEVEL 1; TASK C53-252-03. REMOVED, FABRICATED AND INSTALLED SUPPORTS PER SRM 51-40-02, 53-00-51, DEFECT SIZE: 1 BY 2 BY .065 AND 2 BY 2.5 BY .070. 2L72 4F RTA2NM 20051025000852005102500085NM 2005 10 25 USAA051236 120051021A5320US146N5191391F INTERCOSTAL BOEING757 7572B7 1384964NM BS 1661-1681 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19619AU 27198 FOUND INTERCOSTAL CORRODED CABIN FLOOR STA 1661-1681 RBL10; LEVEL 1;CORROSION LEVEL 1; TASK C53-252-03. FABRICATED NEW INTERCOSTAL AND INSTALLED PER SRM 51-30-01, DEFECT SIZE: 2" SQ. 2L72 4F RTA2NM 20051025000862005102500086EA 2005 10 25 SWIA200515702 120050406A5340 STRINGER CLIP CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07903SW 7425 STATION 280 LBL 9.00' INBOARD CLIP CRACKED AT TOP RADIUS; RBL 9.00' INBOARD AND OUTBOARD CLIP CRACKED AT TOP RADIUS, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW CLIPS AT STA 280 RBL 9.0 INBD SIDE AND AT STA 280 RBL 9.0 INBD AND OTBD IAW CRJ200 SRM 51-10-06 PG 3 51-42-06 PG 15 AND 51-42-20 PG 1. 2L72 4F RTA21EA 20051025000872005102500087EA 2005 10 25 SWIA200515703 120050406A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA BS 625 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07903SW LT AND RT SUPPORT CLIPS ON AFT SIDE OF REAR PRESSURE BULKHEAD AT FS 625.00 ARE CRACKED, ITEM FOUND AT C-CHECK INSPECTION. NEW CLIPS INSTALLED IAW CRJ 200 SRM 51-42-06; 51-42-21 AND REO601R-53-61-985. 2L72 4F RTA21EA 20051025000882005102500088EA 2005 10 25 SWIA200515704 120050326A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07916SW 7634 FS280; CLIPS AT LBL9.0 AND RBL9.0 ARE CRACKED, ITEM FOUND AT C-CHECK INSPECTION. CLIP AT LBL 9.0 INBOARD AND CLIP AT RBL 9.0 INBOARD REPLACED AS REQUIRED IAW SRM 51-42-06 AND 51-42-21. 2L72 4F RTA21EA 20051025000892005102500089EA 2005 10 25 SWIA200515705 120050326A5210 DRAG ANGLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07916SW 7634 PAX DOOR AFT DRAG ANGLE IS CRACKED BY DOOR ASSIST PULLEY BRACKET, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR ANGLE SECTION AND SPLICE ANGLES IAW REO 601R-52-11-513 CRJ200 SRM 51-42-06 PG 1-15. 2L72 4F RTA21EA 20051025000902005102500090EA 2005 10 25 SWIA200515706 120050326A5340 BRACKET CNDAIRCL600 CL6002B19 1900309EA BS 621 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07916SW 7634 STA 621 LT LOWER ANGLE BRACKET (AFT BULKHEAD) CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED LT FLOOR SUPPORT IN ACCORDANCE WITH REO NR 601R-53-61-117 2L72 4F RTA21EA 20051025000912005102500091EA 2005 10 25 SWIA200515707 120051019A27604916406 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07465SW6431 6431 7845 "SPOILERON FAULT" STATUS MESSAGE ON TAXI OUT. REPLACED NR 1 SECU REF 27-61-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051025000922005102500092EA 2005 10 25 SWIA200515708 120051017A2760 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION LDLANDING 1 NM07465SW 7845 "OB GND SPOILER" CAUTION UPON LANDING WITH RIGHT SIDE OUTBOARD GROUND SPOILER NOT DEPLOYING. REPLACED PROXIMITY SENSOR PS21GA FOR RT OB GROUND SPOILER AND ADJUSTED IAW MM 27-60-00. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051025000932005102500093NM 2005 10 25 USAA051223 120051019A5315141N516139 FLOORBEAM BOEING757 7572B7 1384964NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19619AU 27198 FOUND FLOORBEAM WEB CORRODED STA 331 RBL 1, FLOORBEAM WEB; LEVEL 1;TASK C53-222-03. REMOVED AND REPLACED FLOORBEAM; LEVEL 1; TASK C53-222-03, DEFECT SIZE: 1.9"L BY 1.6"W BY .080"D. 2L72 4F RTA2NM 20051025000942005102500094WP 2005 10 25 05FDEA03465 120051021A5330 SKIN DOUG DC10 DC1010 3022110WP GE CF6 CF66K 30020NE BS 1009 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LWR FUS RT SIDE ON SKIN: BTW LONG 37 AND LONG 38 FOUND AT STA 1009 NR 1EA DENT (LENGTH 1,063 INCH X DEPTH 0,082 INCH) AND AT STA 1006 FOUND 1EA DENT (DEPTH 0,161 INCH X LENGTH 2 INCH) BTW LONG38 AND LONG 39 AT STA Y=1007 FOUND NR1 DENT (LENGTH 1.57 INCH X DEPTH 0,102 INCH). REPAIRED SKIN IAW SRM 53-20-00 FIG 6 SHEET 3/4 VOL1. 2L73 4F4 F A22WE E23EA 20051025000952005102500095WP 2005 10 25 05FDEA03475 120051021A5511ALC70491 RIB DOUG DC10 DC1010 3022110WP GE CF6 CF66K 30020NE HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LT HORIZ STAB LEADING EDGE OB FOUND CORROSION BETWEEN SKIN AND RIB. REMOVED CORROSION AND REPAIRED WITH NR 2EA DOUBLER IAW SRM 55-13-01 FIG 1 VOL3. 2L73 4F4 F A22WE E23EA 20051025000962005102500096CE 2005 10 25 1050921026 120051020A5311 FRAME BEECH 1900 1900D 1154162CE FUSELAGE CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07146ZV UE146 CRACKED INNER SKIN AND FRAME. MAINTENANCE REPAIRED IAW SRM 51-70-00 AND 51-70-15. MORE INFORMATION WILL BE AVAILABLE AT A LATER TIME. 2L72 4T RTA24CE 20051025000972005102500097NM 2005 10 25 SWAA053292 120051021A3350079123 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29433LV 33716 FWD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED EXIT LIGHT LENS PER MM. 2L72 4F RTA16WE 20051025000982005102500098NM 2005 10 25 SWAA053293 120051021A335065C27095 BATTERY PACK BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29734SA 27866 DURING SCHEDULED RON, FOUND EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 3 AND 5 DEF. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20051025000992005102500099 2005 10 25 SWAA053294 420051023A2565D31591478 SLIDE BOEING737 7373H4 1384600NM L1 DOOR DEPLOYED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 L1 DOOR EVACUATION SLIDE INADVERTANTLY DEPLOYED. REMOVED AND REPLACED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20051025001002005102500100NM 2005 10 25 SWAA053295 120051020A53306545767 SKIN BOEING737 7373H4 1384600NM BS 515A CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 505A AND BS 515A, STR 15L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051025001012005102500101NM 2005 10 25 SWAA053296 120051020A53306545767 SKIN BOEING737 7373H4 1384600NM BS 504-513 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 504B AND BS 513B, STR 16L AND STR 17L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051025001022005102500102NM 2005 10 25 SWAA053297 120051020A53306545769 SKIN BOEING737 7373H4 1384600NM BS 444 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29322SW 23343 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 444, STR 26L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051025001032005102500103NM 2005 10 25 SWAA053298 120051021A53306565552 SKIN BOEING737 7373A4 1384585NM BS 315 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRAKCED AT BS 315, STR 17R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051025001042005102500104NM 2005 10 25 CALA0500371 120051020A53302024T3050 SKIN BOEING737 7373T0 1384582NM BS 727E-747 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714308 23359 INSPECTION FOUND A 1 INCH CRACK IN FUSELAGE SKIN BETWEEN STA 727E - 747 JUST BELOW S24R. THE SKIN WAS REPAIRED IAW SRM 53-00-01, REPAIR 31, FIGURE 201, DETAIL XI. 2L72 4F RTA16WE 20051025001052005102500105NM 2005 10 25 CALA0500372 120051023A2530HFE9520D01 COFFEEMAKER BOEING767 767224 1385170NM GALLEY INOPERATIVE A CALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW277615111213 30430 THE FORWARD ESPRESSO COFFEEMAKER BEGAN TO SMOKE AND GAVE OFF A BURNED ELECTRICAL ODOR WHILE EN ROUTE FROM EWR TO FCO. THE CIRCUIT BREAKER WAS PULLED AND THE SMOKE CEASED. THE FLIGHT WAS CONTINUED TO FCO WHERE IT LANDED WITHOUT FURTHER INCIDENT. THE ESPRESSO COFFEEMAKER 209 IN THE FIRST CLASS GALLEY WAS REMOVED AND REPLACED. THE AREA WAS INSPECTED FOR BURNED WIRING AND NONE WAS FOUND. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA1NM 20051025001062005102500106NM 2005 10 25 CALA0500373 120051022A253072067002 OVEN BOEING737 737524 1384721NM FWD GALLEY INOPERATIVE A CALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW273761527833 27328 SMOKE AND A BURNING METALLIC ODOR CAME FROM THE FORWARD GALLEY 205 OVEN. THE GALLEY POWER WAS TURNED OFF AND THE SMOKE CEASED. THE FLIGHT ATTENDANT REPORTED THAT THE OVEN WAS EMPTY AT THE TIME OF THE OCCURRENCE. THE FORWARD GALLEY OVEN WAS REMOVED AND REPLACED AND OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20051025001072005102500107NM 2005 10 25 CALA0500374 120051009A24976130802503 WIRE HARNESS BOEING737 7373T0 1384582NM LT WING ROOT BURNED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716339 23577 MAINTENANCE DISCOVERED THE W802 WIRE BUNDLE AT LT WING ROOT UNDER I/B FLAP FAIRING BURNT. THERE WAS EVIDENCE OF CHAFING AND ARCING. THE WIRING BUNDLE WAS REPAIRED IAW ECRA 2821-01011. 2L72 4F RTA16WE 20051025001082005102500108NM 2005 10 25 SWAA053299 120051021A53306565567 SKIN BOEING737 7373A4 1384585NM BS 480 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRAKCED AT BS 480, STR 16R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051025001092005102500109NM 2005 10 25 SWAA053300 120051021A53306565574 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 737, STR 18R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051025001102005102500110 2005 10 25 SWAA053301 420051020A2565D31354 SLIDE BOEING737 7377H4 1384404NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29736SA 27868 L1 DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20051025001112005102500111NM 2005 10 25 SWAA053302 120051023A5753 SKIN BOEING737 7373H4 1384600NM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29604SW 27955 DURING SCHEDULED RON, FOUND RT INBD T/E AFT FLAP DELAMINATED. REPAIRED FLAP PER SWA EA. 2L72 4F RTA16WE 20051025001122005102500112NM 2005 10 25 SWAA053303 120051023A53116546550 FRAME BOEING737 7373H4 1384600NM BS 787 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 787, LBL 22, WL 156. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051025001132005102500113NM 2005 10 25 SWAA053304 120051023A53116546533 FRAME BOEING737 7373H4 1384600NM BS 500A CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051025001142005102500114NM 2005 10 25 SWAA053305 120051023A53116546548 FRAME BOEING737 7373H4 1384600NM BS 747 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051025001152005102500115NM 2005 10 25 SWAA053306 120051023A53116546550 FRAME BOEING737 7373H4 1384600NM BS 787 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051025001162005102500116NM 2005 10 25 SWAA053307 120051023A53116546552 FRAME BOEING737 7373H4 1384600NM BS 827 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051025001172005102500117NM 2005 10 25 SWAA053308 120051023A53116546555 FRAME BOEING737 7373H4 1384600NM BS 867 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051025001182005102500118NM 2005 10 25 SWAA053309 120051023A5320BAC1505 FLOOR SUPPORT BOEING737 7373H4 1384600NM BS 706 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D CHECK, FOUND LONGITUDINAL FLOOR SUPPORT CRACKED AT BS 706, RBL 25, WL 203. REPAIRED FLOOR SUPPORT PER BFG ER. 2L72 4F RTA16WE 20051025001192005102500119 2005 10 25 SWAA053310 420051020A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29651SW 27721 DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20051025001222005102500122NM 2005 10 25 0501576718 120050916A5311 FRAME BOEING747 747251F 1384898NM PWA JT9 JT9D7F 52054NE BS 1146 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01618US 21122 DURING L-CHECK FOUND CORROSION AND CRACK ON FRAME IN LT BLG WHEEL WELL AT BS 1146. REPAIRED IAW EA 67-165244. 2L74 4F4 F A20WE E20EA 20051025001232005102500123EU 2005 10 25 BAQA106369 120051014A7714645383081 TACHOMETER AEROSPSA365 SA365N 8680669EU TMECA ARRIELARRIEL1 60030NE ENGINE FLUCTUATES E BAQAK NONE O OTHER ININSP/MAINT 1 EA0363CF 6068 NG GAUGE WOULD FLUCTUATE THROUGH ENTIRE ENGINE RANGE. 1G72 3U3 U H10EU E19EU 20051025001242005102500124EA 2005 10 25 ASOA05795 120050923A5320 DUCT CNDAIRCL600 CL6002B19 1900309EA BS 559 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27835AS 7258 DURING A C-CHECK IN MCN, FOUND CORROSION AROUND THE INLET DUCT AT FS 559 PLUS 96 RT. AFTER MAINTENANCE BLENDED, ALODINED, AND PRIMED THE INLET DUCT AT FS 559 PLUS 96 RT, IAW REO 601R-53-41-037, IT WAS FOUND TO BE WITHIN LIMITS. (M) 2L72 4F RTA21EA 20051025001262005102500126EA 2005 10 25 ASOA05794 120050923A5347 CARGO TRACK CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CARGO BAY CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27835AS 7258 DURING A C-CHECK IN MCN, CORROSION WAS FOUND ON THE TIE DOWN FITTINGS AND TIE DOWN TRACKS. AFTER MAINTENANCE REMOVED CORROSION ON THE TIE DOWN FITTINGS AND THE TIE DOWN TRACKS, THEY WERE FOUND TO BE WITHIN LIMITS. (M) 2L72 4F4 FRTA21EA E15NE 20051025001272005102500127EA 2005 10 25 ASOA05788 120050922A5280 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NLG DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27835AS 7258 DURING A C-CHECK IN MCN, THE RADIUS OF FUSELAGE SKIN FORWARD OF THE NOSE LANDING GEAR DOOR WAS SUSPECTED OF BEING CRACKED BEYOND LIMITS. S/D - MAINTENANCE REPAIRED THE FUSELAGE SKIN RADIUS RH AND LHS, AT FS 235, IAW ASA EO 600-53-0122. (M) 2L72 4F4 FRTA21EA E15NE 20051025001332005102500133EA 2005 10 25 ASOA05758 120050914A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27692BR 7759 DURING AN OVERNIGHT INSPECTION IN VPS, AN EMERGENCY CEILING LIGHT AT ROW 4 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY LIGHT ASSEMBLY. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F4 FRTA21EA E15NE 20051025001342005102500134EA 2005 10 25 ASOA05757 120050914A5210H341433 HANDLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR BINDING A ASOAK NONE O OTHER ININSP/MAINT 1 SO27837AS 7271 DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WOULD NOT OPEN FROM THE OUTSIDE. MAINTENANCE REMOVED AND REPLACED THE ROLLER ON THE INNER DOOR HANDLE OF THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F4 FRTA21EA E15NE 20051025001362005102500136EA 2005 10 25 ASOA05760 120050819A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA ENGINE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27839AS 7284 DURING A C-CHECK IN MCN, THE CENTER ENGINE SUPPORT BEAM WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACE THE CENTER ENGINE SUPPORT BEAM IAW EO`S 600-53-0078 AND 600-54-0009. (M) 2L72 4F RTA21EA 20051025001382005102500138CE 2005 10 25 100705N549CS1 120051007A291099126254 VALVE CESSNA560 560XL 2076702CE HYD SYSTEM MALFUNCTIONED E Z5FAAH UNSCHED LANDING DEACTIVATE SYST/CIRCUITS FGJFLT CONT AFFECTED MULTIPLE FAILURE WARNING INDICATION CRCRUISE 1 NE03549CS485 5605546 DURING CLIMB OUT FROM AOO TO PWK THE CREW NOTICED A STAB MISCOMPARE LIGHT. COMPLIED WITH CHECKLIST PROCEDURES AND DISCOVERED THAT HYDRAULIC CONTROL C/B WAS POPPED DISABLING ALL HYDRAULIC SYSTEMS. DECIDED TO DIVERT TO TOL FOR CORRECTIVE ACTION. LANDED WITH NO FLAPS AND THRUST REVERSERS AFTER BLOWING DOWN THE LANDING GEAR. LANDING WAS UNEVENTFUL. MAINTENANCE DETERMINED THAT HYDRAULIC LOADING VALVE HAD FAILED. VALVE REPLACED AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA22CE 20051025001402005102500140NM 2005 10 25 AALA20050687 120051017A3241S274T12010 SHUTTLE VALVE BOEING757 757223 1384957NM ANTI SKID SYSTEMINOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW21685AA 25342 JFK - AUA - DURING CRUISE CREW REPORTED UNCOMMANDED RIGHT HYDRAULIC SYSTEM TRANSFERRING TO LEFT HYDRAULIC SYSTEM. REMOVED AND REPLACED THE LEFT AND RIGHT ANIT-SKID SHUTTLE VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20051025001422005102500142NM 2005 10 25 AALA20050689 120051019A3397 CONNECTOR BOEING767 767323 1385205NM EMERGENCY LIGHT DISCONNECTED A AALAK NONE O OTHER ININSP/MAINT 1 SW21391AA 27451 SFO - DURING OVERNIGHT MAINTENANCE FOUND EMERGENCY LIGHTS AT ROWS 2H THROUGH 6H INOPERATIVE. SECURED CONNECTOR AT ROW 2H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20051025001452005102500145NM 2005 10 25 05FDEA03347 120051011A5730 SKIN DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 LEFT WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT XORS 598. TRIMMED OUT AS PER FEDEX EA 1-5710-89996, FABRICATED AND INSTALLED AS PER FEDEX EA 1-5710-89996. 2L73 4F RTA22WE 20051025001482005102500148NM 2005 10 25 DL76G050626 120051017A2131211738813 CONTROLLER BOEING767 767332 1382001NM CABIN PRESSURE FAILED A DALAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO271603 29695 AFTER ENGINE START ACFT BEGAN TO PRESSURIZE THE CABIN TO 1000 FT MSL. AUTO INOP LIGHT CAME ON CABIN AUTO INOP EICAS MSG DISPLAYED AND CABIN AUTO 1 AND CABIN AUTO 2 STATUS MSG. BOTH CABIN PRESS CONTROLLERS FAULTED CONTROLLERS. REPLACED NR 1 CONTROLLER CKS OK. FWD TO MCO/PLAC MEL 21-31-01A THE NR 2 CABIN PRESS CONTROLLER. 2L72 4F RTA1NM 20051025001512005102500151NE 2005 10 25 DLM88050627 220051017A7200JT8D219 ENGINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 FAILED A DALAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SO27910DL41647 49541 725403 NR 2 ENG FAILED DURING CLIMB-OUT AT 19,800 FT MSL, LOUD BANG, MODERATE VIBRATION FOLLOWED. REPLACED ENGINE. 2L72 4F4 FRTA6WE E9NE 20051025001532005102500153NM 2005 10 25 DL73G050629 120051018A21216454052 FAN BOEING737 73735B 13844BMNM CABIN SEIZED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27224DA 24269 AFTER T/O THROUGH 5000 AND 7000 FEET, AN UNUSUAL SMELL THROUGH CABIN. REPLACED CABIN RECIRC FAN. 2L72 4F RTA16WE 20051025001552005102500155NE 2005 10 25 DL76G050632 220051018A7200CF680C2B6 ENGINE BOEING767 7673P6 1385105NM GE CF6 CF680C2B6 30025NE NR 1 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27155DL347498356 25269 695476 DAMAGED BRACKETS, VSV LEVER ARMS, AND HEAT SHIELDS ON NR 1 ENGINE. REPLACED ENGINE. 2L72 4F4 FRTA1NM E13NE 20051025001572005102500157NM 2005 10 25 SWAA053045 120051004A335020131 BATTERY PACK BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 FWD GALLEY EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20051025001592005102500159NM 2005 10 25 SWAA053047 120051004A278065C30462 LINK BOEING737 7373TO 138447GNM RT WING LE FLAP BROKEN A SWAAO OTHER O OTHER NRNOT REPORTED 1 SW29697SW 23838 NR 3 L/E FLAP TRANSIT INDICATOR LIGHT ILLUMINATED. FOUND BROKEN ATTACH LINK ASSY. REMOVED AND REPLACED NR 3 L/E FLAP ATTACH LINK ASSY PER MM. 2L72 4F RTA16WE 20051025001612005102500161NM 2005 10 25 SWAA053049 120051004A5313BAC1498 STRINGER BOEING737 737317 138447PNM BS 360 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 360, STR 14L. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20051025001632005102500163EA 2005 10 25 MASA200500373 120050520A2720 TRIM SYSTEM CNDAIRCL600 CL6002C10 1390015EA MALFUNCTIONED A MASAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW07507MJ 10077 ASH 7165. THE CREW RETURNED TO THE GATE DUE TO AN AILERON TRIM AND RUDDER TRIM RUN AWAY. MAINTENANCE TROUBLESHOT AND RESET THE SYSTEM. 2L72 4F RTA21EA 20051025001652005102500165EA 2005 10 25 MASA200500424 120050601A3230533407 SELECTOR VALVE CNDAIRCL600 CL6002C10 1390015EA MLG FAILED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07512MJ3260 10109 ASH 7256 RDU. CREW REPORTED A DISAGREE WARNING AND GEAR WOULD NOT EXTEND. CREW HAD TO MANUAL EXTEND GEAR AND DECLARED EMERGENCY. AIRCRAFT LANDED UNEVENTFULLY AND MAINTENANCE R2 GEAR CONTROL VALVE. 2L72 4F RTA21EA 20051025001672005102500167EA 2005 10 25 MASA200500451 120050608A2720 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA FLT CONTROLS ILLUMINATED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07511MJ 10104 ASH 7201 IAD. DIVERTED TO RIC DUE TO A RUDDER TRAVEL LIMITER CAUTION MESSAGE. THE MAINTENANCE DATA COMPUTER WAS INTERROGATED, THE SYSTEM WAS RESET PER THE FIM AND THE FAULT CLEARED. THE FLIGHT CONTROLS WERE ACTUATED MULTIPLE TIMES WITH NO FAULTS AND THE AIRCRAFT WAS RELEASED. 2L72 4F RTA21EA 20051025001702005102500170EU 2005 10 25 RAIA00510018 120051017A3350 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT LOOSE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03561HK 41077 FLIGHT INSPECTION - STL - EMERGENCY LIGHTS INOP AT ROWS 1-6. MAINTENANCE RESECURED LOOSE CONNECTOR. 2L72 4T RTA41NM 20051025001722005102500172NM 2005 10 25 SWAA053268 120051019A53116517685 FRAME BOEING737 7373H4 1384600NM BS 348 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 348, STR 16L. REPAIRED FRAME WEB PER SRM. 2L72 4F RTA16WE 20051020001452005102000145EA 2005 10 20 MASA200500259 120050329A27505912952 PDU CNDAIRCL600 CL6002C10 1390015EA TE FLAPS FAILED A MASAO OTHER J WARNING INDICATION CRCRUISE 1 SW07505MJ5681 10070 ASH 7209 RDU - IAD CREW REPORTED A FLAP FAIL DURING FLIGHT. MAINTENANCE ARE IN THE PROCESS OF TROUBLESHOOTING. 3/29/05 MAINTENANCE REPLACED NR 1 PDU MOTOR AND RT BPSU. BPSU P/N 5913000, S/N OFF A0401, TT; 504, TC;333. 2L72 4F RTA21EA 20051020001502005102000150EA 2005 10 20 VNAA0510006 120051009A2150 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT PACK FALSE ACTIVATIONA VNAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL05245PS 7919 CLIMBING THRU 5000 FT WITH THE LT PACK DEFERRED, THE RT PACK HI PRESS CAUTION MESSAGE ILLUMINATED. DUCT PRESSURE WAS REPORTED >80 PSI. THE FLIGHT RETURNED TO CLT AND LANDED. MAINTENANCE COMPLIED WITH AN OPERATIONAL CHECK OF THE RT AIR CONDITIONING SYSTEM AND FOUND NO DISCREPANCIES. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20051020001532005102000153EA 2005 10 20 VNAA0510001 120051002A3250 STEERING SYS CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NLG WARNING LIGHT A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL05209PS 7874 THE STEERING INOP CAUTION MESSAGE ILLUMINATED AFTER DEPARTURE. THE NWS SWITCH WAS CYCLED BUT THE SYSTEM WOULD NOT RESET. THE CREW FOLLOWED THE QRH AND MADE A PRECAUTIONARY LANDING WITH EQUIPMENT AT DESTINATION. MAINTENANCE PERFORMED AN OPERATIONAL TEST OF THE NOSE WHEEL STEERING SYSTEM IAW CRJ200 AMM 32-51-00-710-802. OPS CHECKS WERE GOOD. NO FAULTS WERE FOUND. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20051020001552005102000155EA 2005 10 20 MASA200500571 120050719A3350316 LAMP CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07509MJ 10094 ASH 7195 IAD. EMERGENCY LIGHTS ARE OUT IN FORWARD GALLEY. MX RELAMPED THE LIGHT ASSEMBLY. 2L72 4F RTA21EA 20051020001842005102000184EA 2005 10 20 MASA200500700 120050903A2720 WARNING LIGHT CNDAIRCL600 CL6002D24 1390016EA ELEVATOR FALSE ACTIVATIONA MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW07930LR 15030 ASH - 6613 LAS, THE CREW REPORTED AN ELEVATOR SPLIT CAUTION MESSAGE UPON LANDING. THE FAULT CLEARED WHILE AWAITING MAINTENANCE. MAINTENANCE PERFORMED A SYSTEM RESET AND OPERATIONAL CHECK WITH NO FAULTS NOTED. 2L72 4F RTA21EA 20051021000042005102100004NE 2005 10 21 DL73S050574 220050929A7220JT8D15AHK ENGINE BOEING737 737232 1384475NM PWA JT8 JT8D15A 52051NE NR 1 BIRD INGESTION A DALAA UNSCHED LANDING CJ F.O.D. WARNING INDICATION CLCLIMB 1 SO27311DL42341 717148 23083 717148 ON T/O AT 1000 FT, HEARD LOUD BANG AND AIRCRAFT YAWED MOMENTARLLY LT AND RT. PASSENGER REPORTED BLUE FLAME FROM FWD OF LT ENGINE. FOWL SMELL IN CABIN. ENGINE PARAMETERS NORMAL. RETURNED TO CVG. FOUND EVIDENCE OF BIRD INGESTION IN NR 1 ENGINE. INSPECTED SAME. OK FOR SERVICE. 2L72 4F4 FRTA16WE E2EA 20051021000062005102100006NM 2005 10 21 DL76P050576 120050930A3610 CLAMP BOEING767 767332 1382001NM BLEED VALVE LOOSE A DALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO27143DA 25991 ON TAKEOFF HAD RT DUCT BLEED CAUTION LIGHT AND EICAS MSG . RTO AT 70 KTS. MTC FOUND THE UPSTREAM CLAMP ON THE RT BLEED ISLN VALVE LOOSE. SECURED SAME. 2L72 4F RTA1NM 20051021000132005102100013EU 2005 10 21 0501543239 120051018A213190221570210 CONTROLLER AIRBUS320 A320212 3930322EU CABIN PRESSURE MALFUNCTIONED A NWAAB EMER. DESCENT J WARNING INDICATION CLCLIMB 1 GL01339NW181579315 367 DURING CLIMB-OUT OF MSP PACKS 1 AND 2 FAULTED. CABIN ALTITUDE CLIMBED TO 14,300 FEET. AN EMERGENCY DESCENT WAS MADE TO FL 10,000. CAPTAIN MANUALLY DROPPED THE MASKS AND BEGAN AN ATB TO MSP. THE A/C MADE AN UNEVENTFUL LANDING. 2L72 4F RTA28NM 20051025001742005102500174WP 2005 10 25 05FDEA03213 120051005A5712 RIB DOUG DC10 DC1010 3022110WP ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE LT WING FIXED L/E COMPT AT STA XORS 600 ZONE 519 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET3 AND 4 VOL I. INSTALL REPAIR ANGLE -35. 2L73 4F A22WE 20051025001762005102500176WP 2005 10 25 05FDEA03215 120051005A5712 RIB DOUG DC10 DC1010 3022110WP ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE LT WING FIXED L/E COMPT AT STA XORS 731 ZONE 525 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET4 AND 6 VOL I. 2L73 4F A22WE 20051025001802005102500180WP 2005 10 25 ABXA050243 120051007A3510 FITTING DOUG DC9 DC941 302207NWP OXYGEN SYS LEAKING A ABXAO OTHER O OTHER CRCRUISE 1 GL23964AX 47781 AT FLIGHT LEVEL 350, NOTICED CREW 02 BOTTLE WAS LOSING PRESSURE. DESCENDED TO LOWER ALTITUDE (170). REMAINDER OF FLIGHT, PRESSURE REMAINED AT 1000 PSI. SERVICED CREW 02 BOTTLE TO 1800 (WAS 1000) PSI. FOUND LINE FROM BOTTLE TO VALVE FITTING ON BULKHEAD LEAKING. REMOVED LINE, CLEANED FITTING. REINSTALLED LINE, NO LEAK NOTED. LEAK CHECKED SYS AT BACK OF ALL 3 02 REGULATORS. REMOVED SIDE PANEL ON F/O'S LOWER SIDEWALL & LEAK CHECKED FITTING BELTING PANEL. REINSTALLED PANEL & ALL 3 REGULATORS, LEAK CHECKED. ALL LINES LEAK CHECKED GOOD. ALL 3 MASKS AND REGULATRORS GOOD. PRESSURE HELD STEADY FOR 2.5 HRS AFTER MASK CHECKS & FIXING LEAK IN LINE 02 PRESSURE WAS 1750 PSI AT 16:15 GMT 10-08-05. 2L72 4F A6WE 20051025001812005102500181CE 2005 10 25 DXTA200501016 120051011A3240 BRAKE ASSY CESSNA500 560CESSNA 2076750CE MLG WEAK E DXTAD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07366QS 5600466 ON TAXI OUT BRAKES FELT SOFT. BLED BRAKES PER CESSNA 560 ULTRA MM 32-42-00. BRAKES FUNCTION NORMALLY AT THIS TIME. 2L72 4F RTA22CE 20051025001822005102500182NM 2005 10 25 2005UALA01057 120050930A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE BS 750 DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29545UA 25323 SKIN DENT AT STA 750, STR 16L. TRIMMED OUT DAMAGE, INSURE CUT, INSTALLED FILLERS, DOUBLER, AND TRIPLER REPAIR PER REO-G11 002-C AND EVA-50676 2L72 4F4 FRTA2NM E17NE 20051025001832005102500183EU 2005 10 25 2005UALA01059 120050929A5320 FLOOR SUPPORT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE AFT GALLEY CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29459UA 1192 AFT GALLEY CORROSION. FLOORBEAM AND SPLICE ANGLE REPLACED. 2L72 4F4 FRTA28NM E40NE 20051025001842005102500184NM 2005 10 25 SWAA053269 120051018A2560P4010021 BATTERY PACK BOEING737 7373Q8 1384670NM FLASHLIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 DURING SCHEDULED SERVICE CHECK, FOUND LT AFT CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20051025001852005102500185 2005 10 25 SWAA053270 420051018A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29742SW 29278 DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051025001872005102500187WP 2005 10 25 05FDEA03219 120051005A5712 RIB DOUG DC10 DC1010 3022110WP LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE LT WING FIXED L/E COMPT AT STA XORS 815 ZONE 526 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 4 AND 6 VOL I. 2L73 4F A22WE 20051025001882005102500188NE 2005 10 25 ABXA050244 220051003A7261JT8D7B ENGINE DOUG DC9 DC932 3022066WP PWA JT8 JT8D7B 52053NE LEFT DEFECTIVE A ABXAEA ENGINE SHUTDOWN UNSCHED LANDING KMJFLUID LOSS OVER TEMP WARNING INDICATION CRCRUISE 1 GL23986AX844 47543 657055 NR 1 ENGINE HIGH OIL TEMP. LEFT ENGINE SHUTDOWN AT FLT LEVEL 310 DUE TO OIL TEMP IN THE RED ZONE. INITIALLY TEMP WAS AT TOP OF YELLOW BAND, THEN WENT TO RED, THEN PEGGED ON SHUTDOWN. REMOVED AND REPLACED LEFT ENGINE IAW ABX JOB CARD 90900010. 2L72 4F4 F A6WE E2EA 20051025001892005102500189WP 2005 10 25 ABXA050245 120051007A3220 PUSHROD DOUG DC9 DC941 302207NWP NLG DAMAGED A ABXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23969AX 47464 UNABLE TO RAISE GEAR HANDLE PAST UPLATCH POSITION. NOSEWHEEL STEERING STILL ENGAGED AFTER TAKEOFF. FOUND GROUND SHIFT LOWER SECTOR PUSH ROD BOLT WITH MISSING HARDWARE. REMOVED AND REPLACED GROUND SHIFT LOWER SECTOR PUSH ROD BOLT AND HARDWARE IAW DC9 MM 20-16-00. INSPECTED GROUND SHIFT CABLES, LINKAGE AND GROUND SENSING MECHANISM. NO DEFECTS NOTED. PERFORMED POSITION AND WARNING TEST IAW DC9 MM 32-60-00-2. NO DEFECTS NOTED. 2L72 4F A6WE 20051025001902005102500190WP 2005 10 25 05FDEA03220 120051005A5712 RIB DOUG DC10 DC1010 3022110WP LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE LT WING FIXED L/E COMPT AT STA XORS 911 ZONE 527 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET3 AND 4 VOL I, INSTALL REPAIR ANGLE -35. 2L73 4F A22WE 20051025001922005102500192WP 2005 10 25 05FDEA03222 120051005A5315 FLOORBEAM DOUG DC10 DC1010 3022110WP ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 FWD CARGO COMPT FOUND ON FLOORBEAM AT STA 979 X=-97 RT SIDE CRACK LONG 1/2 INCH. CUT DAMAGED PORTION BEAM. REPLACED SECTION IAW SRM 51-35-01 PAGE 1-13 VOL II. REPLACED BRACKET ADA0144-27 AND REPAIRED IAW 53-00-01 FIG 9 SHEET 8. 2L73 4F A22WE 20051025001942005102500194WP 2005 10 25 05FDEA03224 120051005A5712 RIB DOUG DC10 DC1010 3022110WP ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE RT WING FIXED L/E COMPT AT STA XORS 684 ZONE 625 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 1, 3 AND 4 VOL I, INSTALL REPAIR ANGLE -36. 2L73 4F A22WE 20051025001962005102500196WP 2005 10 25 05FDEA03226 120051005A5712 RIB DOUG DC10 DC1010 3022110WP RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE RT WING FIXED L/E COMPT AT STA XORS 638 ZONE 619 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 1, 3 AND 4 VOL I. INSTALL REPAIR ANGLE -38. 2L73 4F A22WE 20051025001992005102500199WP 2005 10 25 05FDEA03238 120051004A5313 LONGERON DOUG DC10 DC1010 3022110WP BS 791 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25389FE 46623 FWD LOWER PIT STA 791 L52 LONGERON END CAP CORRODED. REMOVED DAMAGED END CAP IAW DC10 SRM 51-35-01 VOL 11. MAT ID FOR NEW END CAP FOUND TO BE 7075-0 .063" PO 495488.1 IAW DAC DWG ADA3064 AND FED-EX EA8-5310-92565. FORMED END CAP FITTING IAW DAC DWG3064. HEAT TREATED END CAP. ALODINE AND PRIME IAW DC10 SRM 51-21-01 VOL 11. PAINTED IAW DC10 SRM 51-21-02 VOL 11. INSTALLED END CAP FITTING IAW DC10 SRM 51-33-01 VOL 11. 2L73 4F A22WE 20051025002002005102500200NM 2005 10 25 QXEA200501335 120051002A5414 COWLING BOMBDRDHC8 DHC8402 1390042NM LEFT CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09401QX 4031 PDX - LEFT LOWER COWL, 412AR, HAS CHAFE MARK ON UPPER DECK, LEFT SIDE OF INTAKE. MAINTENANCE BLENDED AREA OF CHAFE TO REMOVE DAMAGE AND MAPPED AREA FOR ENGINEERING. HFEC INSP BLENDED AREA FOR CRACKS IAW Q400 NDTM PART 6, 51-00-02. NO CRACKS NOTED. 2H72 4T RTA13NM 20051025002012005102500201NM 2005 10 25 QXEA200501336 120050923A5210 GUIDE BOMBDRDHC8 DHC8402 1390042NM PAX DOOR DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09401QX 4031 PDX - AFT PASSENGER DOOR SURROUND UPPER AFT ROLLER GUIDE IS NOTCHED IN THE OUTBOARD FACE OF THE LOWER CHANNEL. MAINTENANCE BLENDED OUT THE CHAFED AREA AND MAPPED FOR ENGINEERING. HFEC INSP BLENDED AREA FOR CRACKS IAW NDTM PART 6, 51-00-02. NO CRACKS NOTED. 2H72 4T RTA13NM 20051026000032005102600003EA 2005 10 26 ASOA05742 120050907A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27688BR 7723 FLT 4692 - DURING A GROUND INSPECTION IN ATL, THE RIGHT WING AFT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE RIGHT WING AFT EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051026000052005102600005EA 2005 10 26 ASOA05756 120050831A5712 RIB CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27834AS 7254 DURING A C-CHECK IN MCN, THE LEFT MAIN WHEEL WELL BATTERY RIB ASSEMBLY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LEFT MAIN WHEEL WELL BATT RIB ASSY IAW ASA EO 600-57-039A. (M) 2L72 4F RTA21EA 20051026000102005102600010EA 2005 10 26 ASOA05755 120050912A3350 LIGHT CNDAIRCL600 CL6002C10 1390015EA CABIN MALFUNCTIONED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27709EV 10068 DURING A GROUND INSPECTION IN SLC, THE EMERGENCY LIGHTS WOULD NOT TEST. MAINTENANCE CYCLED CIRCUIT BREAKERS. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051026000122005102600012EA 2005 10 26 ASOA05753 120050911A5610 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT FAILED A ASOAO OTHER J WARNING INDICATION CRCRUISE 1 SO27903EV 7621 FLT 4463 - DURING CRUISE FROM ATL-MDT, AT APPROXIMATELY 27,000 FEET THE FIRST OFFICERS WINDSHIELD SHATTERED FOLLOWED BY A SMALL GLOW AT THE BASE OF THE RIGHT WINDSHIELD. THE CREW THEN RECEIVED A R WSHLD HEAT CAUTION MESSAGE. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED SAFELY IN MDT. MAINTENANCE REMOVED AND REPLACED THE NR 3 WINDSHIELD. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051026000152005102600015NM 2005 10 26 DHL2005742518 120051004A5315 FLOORBEAM BOEING727 727225 1384077NM BS 1120 CORRODED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15742DH 21290 AFT PIT CEILING, CABIN FLOORBEAM BS 1120 UPPER SURFACE HAS CORROSION AT RBL 44. REMOVED CORROSION IAW B727 SRM 51-10-6, UT INSPECTED. CUT OUT CORROSION, FABRICATED AND INSTALLED FLOORBEAM REPAIR 9-3/4" BY 2.9" BY .300" FROM 7075-T6 .050 AND 8.0" BY 2.0" BY 1" BY .300 FROM 7075-T6 .063 AND FILLER 1-1/2" BY 1-1/8" FROM 7075-T6 .156 IAW B727 SRM 53-10-8 FIG 10 AND 51-30-2. 2L73 4F A3WE 20051026000162005102600016NM 2005 10 26 DHL2005742519 120051012A5315 FLOORBEAM BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE BS 1010 CORRODED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15742DH 21290 CABIN FLOORBEAM CORRODED ON FLOWER FLANGE LOWER SURFACE BS 1010 LBL 24. CUT OUT CORRODED PORTION OF LOWER LEG OF FLOORBEAM AT BS 1010 LBL 24. FABRICATED AND INSTALLED FLOOR BEAM REPAIRS 18.0 INCH X 1.95 INCH FROM BAC1505-10097, 29.50 INCH X 1.95 INCH FROM 7075-T6 .100 AND 2 EACH 28.0 INCH X 1.85 INCH FROM BAC1490-2734 IAW SRM 51-10-01, 53-10-8 FIG. 2 AND 51-30-2. 2L73 4F4 F A3WE E2EA 20051026000172005102600017NM 2005 10 26 USAA200510003 120051023A5340 BRACKET BOEING767 7672B7 1385107NM BS 287 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19656US 26847 3 INCH CRACK FOUND AT BS 287-S8L FRAME TO LATCH TORQUE TUBE HOUSING BRACKET. FABRICATED AND INSTALLED A NEW BRACKET PER BOEING DWG 141T6605. 2L72 4F RTA1NM 20051026000182005102600018NM 2005 10 26 DL733050637 120051019A5330 SKIN BOEING737 737347 1384647NM BS 727E CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27309WA 23442 FUSELAGE SKIN CRACK WAS FOUND AT CHEM MILL LINE AT BS 727E, STR 24R. CRACK IS 3 INCHES LONG. DOULBER INSTALLED PER ER/A 451199-14AD, AD 2004-18-06, AND SRM 53-00-01. 2L72 4F RTA16WE 20051026000222005102600022 2005 10 26 DL76G050644 420051022A344220412170416 TRANSCEIVER BOEING767 7673P6 1385105NM WX RADAR SYS FAILED A DALAA UNSCHED LANDING O OTHER CRCRUISE 1 SO27156DL 25354 RADAR DISPLAY SHOWING NOTHING BUT GREEN AND YELLOW ON SCREEN REGARDLESS OF TILT. REMOVED AND REPLACED R/T IAW MM, ALL OPS CHECK OK. 2L72 4F RTA1NM 20051026000272005102600027EA 2005 10 26 ASOA05748 120050902A2913848847 PUMP CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM MALFUNCTIONED A ASOAA UNSCHED LANDING J WARNING INDICATION DEDESCENT 1 SO27882AS14458 7503 DURING DESCENT INTO CRW FROM ATL, AT APPROXIMATELY 20,000 FEET THE CREW RECEIVED A 3A HYD LOW PRESS CAUTION MESSAGE. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT DIVERTED TO TRI AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE 3A HYDRAULIC PUMP. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051026000292005102600029EU 2005 10 26 ASOA05741 120050907A2752FE231003 ACTUATOR AEROSPATR72 ATR72212 8680945EU TE FLAPS MALFUNCTIONED A ASOAO OTHER J WARNING INDICATION APAPPROACH 1 SO27635AS18588 372 FLT 4092 - DURING FINAL APPROACH INTO ATL FROM AVL, THE CREW RECEIVED A FLAP UNLOCK MESSAGE AND EXECUTED A MISSED APPROACH TO COMPLY WITH THE QRH. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT PERFORMED A REDUCED FLAP LANDING SAFELY INTO ATL. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT INBOARD AND OUTBOARD FLAP ACTUATORS. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20051026000302005102600030EA 2005 10 26 ASOA05747 120050909A2910 TRANSDUCER CNDAIRCL600 CL6002B19 1900309EA NR 1 HYD SYSTEM FAILED A ASOAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27900EV 7608 FLT 4620 - DURING CRUISE FROM ABE-ATL, AT APPROX 28,000 FEET THE CREW RECEIVED A HYD NR 1 HI TEMP MESSAGE. THE QRH WAS COMPLIED WITH AND THE CREW SHUTDOWN THE LEFT ENGINE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO GSP, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE NR 1 HYDRAULIC SYSTEM TRANSDUCER AND CONNECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051026000322005102600032EA 2005 10 26 ASOA05785 120050921A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27835AS 7258 DURING A C-CHECK IN MCN, THE FS 280 LBL 9 AND RBL 9 OUTBOARD CLIPS WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FS 280, LBL 9 AND RBL 9 OUTBOARD CLIPS IAW BOMBARDIER REO 601R-53-11-638. (M) 2L72 4F RTA21EA 20051026000332005102600033EA 2005 10 26 ASOA05784 120050921A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27835AS 7258 DURING A C-CHECK IN MCN, THE FS 280, LBL 9 AND RBL 9 INBOARD CLIPS WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACED THE FS 280, LBL 9 AND RBL 9 INBOARD CLIPS IAW REO 601R-53-11-638. (M) 2L72 4F RTA21EA 20051026000362005102600036EA 2005 10 26 ASOA05780 120050921A5330 DOUBLER CNDAIRCL600 CL6002B19 1900309EA BS 640 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27903EV 7621 DURING AN A C-CHECK IN BTR, THE LEFT FS 640 DOUBLER, AT STRINGER 9L, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT FS 640 DOUBLER, AT STRINGER 9L. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051026000372005102600037EA 2005 10 26 ASOA05768 120050917A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27873AS 7549 FLT 4539 - DURING A GROUND INSPECTION IN SHV, THE EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. (M) 2L72 4F RTA21EA 20051026000392005102600039EA 2005 10 26 ASOA05765 120050917A5312 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA BS 202 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27841AS 7300 DURING A C-CHECK IN MCN, THE PRESSURE BULKHEAD AT FS 202.75 WAS FOUND CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED PRESSURE BULKHEAD AT FS 202.75 IAW BOMBARDIER REO 601R-53-11-583. (M) 2L72 4F RTA21EA 20051026000402005102600040EU 2005 10 26 ASOA05766 120050917A3350 LAMP AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27635AS 372 DURING A GROUND INSPECTION IN MGM, THE FLIGHT COMPARTMENT OVERHEAD PANEL EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE OVERHEAD PANEL EMERGENCY EXIT LIGHT. OPERATIONAL CHECKS GOOD. (M) 2H72 4T RTA53EU 20051026000412005102600041EA 2005 10 26 ASOA05782 120050921A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN CONTAMINATED A ASOAK NONE O OTHER ININSP/MAINT 1 SO273350 7284 DURING A GROUND INSPECTION IN ATL, THE FORWARD SECTION OF EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND MOISTURE IN THE FORWARD SECTION OF THE EMERGENCY LIGHTS. THE EMERGENCY LIGHTS WERE CLEANED AND DRIED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051026000422005102600042EA 2005 10 26 ASOA05781 120050921A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27844AS 7317 DURING AN OVERNIGHT CHECK IN VPS, THE EMERGENCY CEILING LIGHT AT ROW 4 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY CEILING LIGHT AT ROW 4. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051026000432005102600043CE 2005 10 26 HSY2005F00004 120051011A53433643030201 SUPPORT CESSNA208 208B 2073701CE PWA PT6 PT6* 52043EA NLG DRAG LINK DAMAGED E HSYAO OTHER O OTHER NRNOT REPORTED 1 NM05748FX 208B0503 DAMAGE TO NOSE GEAR SUPPORT. (K) 1H71 3T3 T A37CE E2NE 20051026000452005102600045EA 2005 10 26 ASOA05776 120050920A3350OL3071BPEGPL LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27928EV 8006 DURING A GROUND INSPECTION IN CAE, THE LEFT FORWARD EMERGENCY FLOODLIGHT WAS FOUND TO INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE LEFT FORWARD EMERGENCY FLOODLIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051026000462005102600046EU 2005 10 26 ASOA05746 120050908A3350701210 LAMP AEROSPATR72 ATR72 EU EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27643AS 413 DURING AN A-CHECK IN MCN, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY LIGHT ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20051026000472005102600047EA 2005 10 26 ASOA05790 120050923A5320 SILL CNDAIRCL600 CL6002B19 1900309EA BS 559-621 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27835AS 7258 DURING A C-CHECK IN MCN, SEVERAL NUT PLATES AND THE SILL AREA FLOOR LEVEL UNDER THE LAVATORY POTABLE WATER TANK BETWEEN FS 559.64-621 RT WERE FOUND TO BE CORRODED. S/D - MAINTENANCE REPAIRED THE RHS FLOOR SILL, AT FS 559.64-621, IAW BOMBARDIER REO 601R-53-51-036. (M) 2L72 4F RTA21EA 20051026000492005102600049NM 2005 10 26 05FDEA03483 120051024A5315 FLOORBEAM BOEING727 7272S2F 1384O81NM BS 312 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25213FE 22935 MDCC - FLOORBEAM CORRODED BS 312 LBL-42. REMOVED CORROSION IAW SRM 53-10- 1 MATERIAL LOSS OF 0.007 ORIGINAL THICKNESS 0.080 , FOUND TO BE WITHIN LIMITS PER SRM 53-10-1 FIG 5. TREATED AND PRIMED AREA IAW SRM 51-10-2. 2L73 4F A3WE 20051026000522005102600052EA 2005 10 26 ASOA05797 120050923A3350BR9279232 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27925EV 7831 FLT 4287 - DURING A GROUND INSPECTION IN ATL, THE EMERGENCY EXIT LIGHT COVER AT THE PASSENGER DOOR WAS FOUND BROKEN OFF. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY AT THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051026000552005102600055EU 2005 10 26 05FDEA03477 120051021A5312 VERTICAL BEAM AIRBUS310 A310203 3930313EU BULKHEAD DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25445FE 297 COMPLY WITH EA 6-5310-92347 FUSELAGE - FR 54 BULKHEAD VERTICAL STIFFENER REPAIR. COMPLIED WITH EA 6-5310-92347 FUSELAGE FR 54 BULKHEAD VERTICAL STIFFENER REPAIR. 2L72 4F RTA35EU 20051026000572005102600057NM 2005 10 26 05FDEA03480 120051024A5322 SHEAR TIE BOEING727 727100 1384036NM BS 1130 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 AFT CARGO COMP SHEAR TIE IS CORRODED BS 1130 RBL 8 WL 152. REPAIRED PER SRM 53-10-4. 2L73 4F RTA3WE 20051026000612005102600061 2005 10 26 SWAA053312 420051023A25656557463 FITTING BOEING737 7375H4 138449DNM L1 DOOR SLIDE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED 1/2D CHECK, FOUND L1 DOOR EVACUATION SLIDE GIRT BAR AFT FLOOR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM. 2L72 4F RTA16WE 20051026000642005102600064EA 2005 10 26 ASOA05792 120050923A5320 SILL CNDAIRCL600 CL6002B19 1900309EA BS 559 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27835AS 7258 DURING A C-CHECK IN MCN, THE RIGHT SILL PLATE AT FS 559 PLUS 48 FLOOR LEVEL WAS FOUND TO BE CORRODED. S/D - MAINTENANCE REPAIRED THE RHS SILL PLATE, AT FS 559 PLUS 48, IAW BOMBARDIER REO 601R-53-51-036. (M) 2L72 4F RTA21EA 20051026000672005102600067EA 2005 10 26 ASOA05787 120050922A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA BS 280 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27835AS 7258 DURING A C-CHECK, THE FORWARD AND AFT FLOOR SUPPORT ANGLES, AT FS 280 BETWEEN LBL 9 AND RBL 9, WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE WILL REMOVED AND REPAIR THE FORWARD AND AFT FLOOR SUPPORT ANGLES, AT FS 280 BETWEEN LBL 9 AND RBL 9, IAW REO 601R-53-11-638. (M) 2L72 4F RTA21EA 20051026000682005102600068NM 2005 10 26 SWAA053313 120051023A53226558280 SHEAR TIE BOEING737 7375H4 138449DNM BS 360 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME SHEAR TIE CRACKED AT BS 360, BETWEEN STR 15R AND STR 16R. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051026000692005102600069SO 2005 10 26 RAIA00510022 120051019A5230 SEAL EMB 145 EMB145LR 3260212SO CARGO DOOR LEAKING A RAIAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 CE03830HK 145313 FLT 5561 - STL - CABIN DEPRESSURIZED AT 28,000 FEET DEPLOYING DROP DOWN MASK. MAINTENANCE REMOVED AND REPLACED LOWER BAGGAGE DOOR SEAL. 2L72 4T RTT00011AT 20051026000732005102600073EA 2005 10 26 COMA0570112 120051023A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA BS 364-394 CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01368CA7849 10075 CORROSION FWD EDGE OF AVIONICS BAY DOOR CUTOUT. REMOVED CORROSION IAW BRAS EO 601R-53-7495. 2L72 4F RTA21EA 20051026000742005102600074EA 2005 10 26 ASOA05775 120050919A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA MAIN PAX STICKING A ASOAK NONE O OTHER ININSP/MAINT 1 SO27860AS 7433 DURING AN OVERNIGHT INSPECTION, THE MAIN CABIN DOOR WOULD NOT OPEN FROM THE INSIDE OR OUTSIDE. MAINTENANCE REMOVED EXCESS GREASE FROM THE MAIN CABIN DOOR HANDLE. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051026000762005102600076 2005 10 26 PIDA20050179 420051021A2210 YAW DAMPER BOEING737 7372K5 138448XNM MALFUNCTIONED A PIDAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO05250TR 22597 YAW DAMPER TRIPS OFF ON GROUND ONLY WHEN WIDE TURNS ARE MADE WITH TILLER OR RUDDER. PLACED ON MEL 22-3-1B. 2L72 4F RTA16WE 20051026000782005102600078NM 2005 10 26 SWAA053315 120051023A53306545877 SKIN BOEING737 7373H4 1384600NM BS 303 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29374SW 26582 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED R1 DOOR FWD LOWER CUT OUT, BS 303, STR 18R. REPAIRED SKIN. 2L72 4F RTA16WE 20051026000792005102600079NM 2005 10 26 SWAA053316 120051023A53116545810 FRAME BOEING737 7373H4 1384600NM BS 303 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29374SW 26582 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303 AND L1 DOOR CUT OUT LOWER STOP FITTING. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051026000832005102600083NM 2005 10 26 DL76S050650 120051024A5330146T35523 SKIN BOEING767 767332 1382001NM BS 1219 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27138DL 25409 FUSELAGE/SKIN/STA 1197+132 - STA 1219 BELOW S-36R CORRODED. CORROSION DAMAGE CUT OUT FROM SKIN AT LAP SLICE AND AN EXTERNAL ALUMINUM DOUBLER AND FILLER INSTALLED WITH HI-LOKS. 2L72 4F RTA1NM 20051026000842005102600084NE 2005 10 26 DL76G050651 220051024A7200 ENGINE BOEING767 767332 1382001NM GE CF6 CF680 30025NE NR 1 SMOKE A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO271611B25662 30595 704805 CREW REPORTS SMOKE OIL SMELL HAZE IN CRUISE. DONNED MASK AND MADE AN EMERGENCY LANDING. SMOKE DETECTORS IN CABIN WENT OFF. ENGINE USED 5 PINTS OF OIL. ENGINE CHANGED. 2L72 4F4 FRTA1NM E13NE 20051026000852005102600085NM 2005 10 26 DHL2005742514 120050916A5753 SKIN BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE FORE FLAP GOUGED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15742DH 21290 RT OB FORE FLAP LEADING EDGE HAS 2 EACH GOUGES ABOUT 12 INCHES OB OF IB EDGE. FABRICATED AND INSTALLED REPAIR DOUBLER 8 INCHES X 3 INCHES FROM 024-T3 .050 FOR RT OB FORE FLAP LEADING EDGE IAW 57-50-4, 51-30-2 AND 51-10-2. 2L73 4F4 F A3WE E2EA 20051026000862005102600086NM 2005 10 26 DHL2005742517 120051003A5315 FLOORBEAM BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE BS 1070 CORRODED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15742DH 21290 AFT PIT CEILING, CABIN FLOORBEAM BS 1070 LOWER SURFACE HAS CORROSION AT LBL 14. REMOVED CORROSION IAW SRM 53-10-8. CORROSION REMOVAL INTO TANGENT OF RADIUS. FABRICATED AND INSTALLED REPAIR STRAP 13.3 INCHES FROM 7075-T6 .100 AND TEE FILLER FROM BAC1505-100797 IAW SRM 51-10-2 AND 53-10-08 FIG. 2. 2L73 4F4 F A3WE E2EA 20051026000902005102600090NM 2005 10 26 DHL2005742513 120050917A5322 SHEAR TIE BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE BS 720 CORRODED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15742DH 21290 S/O 284002 N/R 037490 FWD PIT FUSELAGE FRAME AT BS 720 BETWEEN STR 28L AND STR 28R HAS AN (L) ANGLE WHICH ATTACHES TO THE FUSELAGE SKIN CORRODED IN MULTIPLE AREAS. REMOVED CORROSION BETWEEN STR 28L AND 28R BS 720. FOUND SHEAR TIE TO BE OUT OF LIMITS IAW SRM 53-10-1. CUT OUT SECTION OF SHEAR TIE IAW SRM 53-10-4. FABRICATED AND INSTALLED REPAIR SHEAR TIE 10 INCHES FROM 7075-T6 .040 IAW SRM 53-10-4 FIG. 15. 2L73 4F4 F A3WE E2EA 20051026000922005102600092NM 2005 10 26 2005UALA01140 120051015A5310 FRAME BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU FWD GALLEY DOOR CRACKED A UALAO OTHER O OTHER LDLANDING 1 WP29919UA 25386 FWD GALLEY DOOR, AFT SIDE FRAME IS CRACKED AT 3RD AND 4TH STOP FITTING CUTOUTS FROM BOTTOM OF DOOR. REMOVE DAMAGE AREA & INSTALL REPAIR DOUBLER REF SRM 51-70-11 PER JD 90-52-40-14 PG 24 FIG 10 2L72 4F4 FRTA16WE E21EU 20051026000942005102600094EU 2005 10 26 2005UALA01142 120051015A3350 LIGHT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE SEAT 13ABC INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29404UA 450 SEAT MOUNTED EEL LIGHT INOP AT SEAT 13ABC. REPLACED CABLE ASSY. 2L72 4F4 FRTA28NM E40NE 20051026000972005102600097CE 2005 10 26 2005F00105 120050914A3246C2021170 WHEEL CESSNA337 T337G 2075726CE MLG LOOSE B TDMRO OTHER O OTHER NRNOT REPORTED 1 SO25435 566 137 P3370261 WHEEL ASSEMBLY RETURNED FOR LOOSE TIE BOLTS OF 18 INSTALLED 14 WERE FOUND LOOSE 2 MISSING. MESSIER HAS NOW RELEASE SERVICE LETTER F6137-32--843 IN HOPES THIS WILL RESOLVE. 1H72 3O A6CE 20051026000982005102600098NM 2005 10 26 2005UALA01144 120051016A7500 HOUSING BOEING777 777222 1385219NM PWA PW4077PW4077 NE INLET DEFFUSER DAMAGED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29768UA 26919 LOSS OF LEFT BLEED AIR. MAINTENANCE FOUND A 5 INCH DIAMETER HOLE IN FAN INLET DIFFUSER HOUSING (FIDH) DUE TO BROKEN FLANGE ATTACHING THE FIDH TO THE HEAT EXCHANGER. REPLACE FAILED FIDH 2L72 4F4 FRTT0001SE E46NE 20051026000992005102600099NM 2005 10 26 2005UALA01145 120051014A3350 LIGHT BOEING777 777222 1385219NM PWA PW4077PW4077 NE CABIN INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29769UA 26921 EEL LIGHT AT 18G AND 39G INOP. REPLACED EEL LIGHT. 2L72 4F4 FRTT0001SE E46NE 20051026001022005102600102NM 2005 10 26 2005UALA01148 120051015A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE GALLEY INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29195UA 26899 FWD GALLEY FWD RIGHT WALL MOUNTED EEL LIGHT INOP. 2L74 4F4 FRTA20WE E24NE 20051026001032005102600103NM 2005 10 26 2005UALA01149 120051015A5250 SWITCH BOEING747 747422 1384935NM PWA 4056 PW4056 NE COCKPIT DOOR FAILED A UALAO OTHER O OTHER NRNOT REPORTED 1 WP29122UA 29168 COCKPIT DOOR ELECTRIC SWITCH FAILED. BURNT ELEC SMELL IN CABIN & COCKPIT. 2L74 4F4 FRTA20WE E24NE 20051026001072005102600107NM 2005 10 26 2005UALA01153 120051016A3350 LIGHT BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29919UA 25386 BOTH LT & RT EMERGENCY EXIT LIGHTS INOP NEAR INBOARD FLAPS. CHARGED BATTERY. THIS ITEM IS NOT A SAFETY SIGNIFICANT ITEM. PER AOP 06-01-02 PARA 3.4.2, THIS ITEM IS NOT REPORTABLE AS AN SDR. 2L72 4F4 FRTA16WE E21EU 20051026001092005102600109 2005 10 26 2005UALA01155 420051014A25657A147914 ASPIRATOR BOEING747 747422 1384935NM PWA 4056 PW4056 NE ESCAPE SLIDE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29175UA 24382 THERE WAS A LARGE HOLE FOUND ON THE UNDERSIDE OF THE ASPIRATOR DURING THE ASPIRATOR INSPECTION. ASPIRATOR DAMAGED BEYOND REPAIR. DAMAGE CAUSED BY IMPROPER PACKING. REPLACED ASPIRATOR. 2L74 4F4 FRTA20WE E24NE 20051026001102005102600110CE 2005 10 26 2005F00107 120050914A3246C2021170 WHEEL CESSNA337 T337G 2075726CE MLG LOOSE B TDMRO OTHER O OTHER NRNOT REPORTED 1 SO25435 566 137 P3370261 WHEEL ASSEMBLY RETURNED FOR LOOSE TIE BOLTS OF 18 INSTALLED 14 WERE FOUND LOOSE 2 MISSING. MESSIER HAS NOW RELEASE SERVICE LETTER F6137-32--843 IN HOPES THIS WILL RESOLVE. 1H72 3O A6CE 20051026001122005102600112NM 2005 10 26 2005UALA01157 120051017A5320 INTERCOSTAL BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE BS 852 CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29643UA 25093 CORROSION ON UPPER SURFACE OF INTERCOSTAL AT STA 852 AND LBL 54. 2L72 4F4 FRTA1NM E24NE 20051026001142005102600114NM 2005 10 26 2005UALA01159 120051016A5754 SKIN BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU NR 6 SLAT DELAMINATED A UALAO OTHER O OTHER NRNOT REPORTED 1 WP29311UA 23672 NR 6 SLAT LEADING EDGE HAS DELAMINATION ON UPPER SURFACE. HONEYCOMB EXPOSED. REINSTALLED NEW SLAT. 2L72 4F4 FRTA16WE E21EU 20051026001152005102600115NM 2005 10 26 2005UALA01160 120051017A5754 WEDGE BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE NR 9 SLAT DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29220UA 30223 NR 9 LEADING EDGE SLAT HAS INTERIM REPAIR INSTALLED INBOARD T/E WEDGE ON LWR SKIN. LOCALIZED DELAMINATION ON THE LOWER SKIN AT THE ENDS OF THE TRAILING EDGE WEDGE OR JUCT AFT OF THE ACTUATOR ATTACH POINTS IS COMMONPLACE FOR THE 777 SLATS. THE 777 AMM 57-43-99 WAS ISSUED TO ALLOW FOR A STRUCTURAL ADHESIVE INJECTION INTERIM REPAIR FOR SMALL DELAMINATED AREAS. IN THIS CASE, AN AREA OF DELAMINATION THAT WAS WITHIN THE LIMITS OF THE AMM WAS REPAIRED. FOLLOW-UP INSPECTIONS ARE REQUIRED AT 50 AND EVERY 500 CYCLES THEREAFTER UNTIL A PERMANENT REPAIR IS INSTALLED AT THE NEXT HMV. THE LONG TERM SOLUTION FOR THIS SYSTEMIC PROBLEM IS TO INSTALL A NEWLY DESIGNED TE WEDGE ON THESE SLATS. BOEING IS CURRENTLY WORKING 2L72 4F4 FRTT0001SE E46NE 20051026001162005102600116NM 2005 10 26 2005UALA01161 120051018A5311 FRAME BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE BS 1562 CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29643UA 25093 AFT CARGO COMPARTMENT, LOWER LOBE DRAIN HOLE IN FRAME AT BS 1562, BL 0, IS CORRODED. 2L72 4F4 FRTA1NM E24NE 20051026001192005102600119NM 2005 10 26 05FDEA03456 120051020A5315 FLOORBEAM BOEING727 727200 138407ENM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25223FE 20935 FLOORBEAM 380 HAS CORROSION AT RBL 53 TO RBL 56. REMOVED, FABRICATED, HEAT TREATED, CAD PLATED, ALODINED, PRIMED, PAINTED AND INSTALLED FLOORBEAM REPAIR AT STA 380 FROM RBL 53 TO RBL 56 ALL IAW FX SRZ SR27-53-034E REPAIR 5, BAC5619, AMS-QQ-P-416, B727 SRM'S 51-10-2, 51-20-031-7, 51-30-1, 51-30-2 AND 53-10-1 FIG 4A. 2L73 4F RTA3WE 20051026001202005102600120WP 2005 10 26 05FDEA03463 120051021A5330 SKIN DOUG DC10 DC1010 3022110WP BS 1921-2007 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LOWER FUSELAGE RIGHT SIDE ON SKIN BETWEEN LONGERON 48 RIGHT AND LONGERON 48 LEFT FROM STA Y= 1921 AT STA Y= 2007 FOUND NR 1 NEW SKIN PANEL WITH 200 SCREW AND ONE SPLICE REPAIR DOUBLER. CHECKED MATERIAL AND THK. THE REPAIR IS IN COMPLIANCE WITH SRM 53-20-00 FIG 17 SHEET 1 VOL 1. 2L73 4F A22WE 20051026001212005102600121SW 2005 10 26 U0GA106181 120050927A3213AB205050403031 CROSSOVER TUBE BELL 212 212 1181420SW PWA PT6T PT6T3 52045EA LANDING GEAR BROKEN E U0GAO OTHER O OTHER TXTAXI/GRND HDL 1 SW03507EH1793 30950 DURING NORMAL SHUTDOWN PROCEDURES, THE FORWARD CROSS TUBE BROKE IN HALF CAUSING THE NOSE OF THE AIRCRAFT TO LOWER. NO HARD LANDING WAS REPORTED PRIOR TO THIS FAILURE. INITIAL EXAMINATION OF THE TUBE REVEALS THAT THE TUBE BREAK WAS NOT FRESH. THE ATTACHMENT SADDLE MOUNTED TO THE CROSS TUBE APPEARS TO HAVE HIDDEN THE CRACK FROM BEING DETECTED DURING THE NORMAL SCHEDULED INSPECTIONS AT THE 25/375/1000/3000 HOUR INTERVALS. TUBE IS AN ON CONDITION PART AND THIS IS THE FIRST FAILURE RECORDED OF A FORWARD TUBE AS FAR AS OUR RECORDS SEARCH REVEALED. 1G71 4U4 U H4SW E22EA 20051026001242005102600124 2005 10 26 Z1RA106191 420050923A34526221270001 TRANSPONDER SKRSKYS76 S76C 8143008NE ATC INOPERATIVE E Z1RAO OTHER O OTHER NRNOT REPORTED 1 SW11760AF3006 760523 ATC UNABLE TO TRACK AIRCRAFT TRANSPONDER INFLIGHT. 1G72 3U NCH1NE 20051026001272005102600127EU 2005 10 26 B65A106213 120050921A6700105980624 CONTROL UNIT BOLKMS105 BO105LSA1 5626021EU ALLSN 250C 250C28 03013GL FLT CONTROLS UNSERVICEABLE E B65AO OTHER F FLT CONT AFFECTED CRCRUISE 1 GL13202LF 2014 CONTROL UNIT IS CAUSING AN UNCONTROLLABLE LATERAL INPUT. 1G72 3U3 U H3AU E1GL 20051026001292005102600129NM 2005 10 26 C8GA20050023 120051018A327065579277 DRAG LINK BOEING727 727223 1384074NM DOOR DAMAGED A C8GAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO29715AA57777 22470 FLT 5201FROM MIA TO CCS. AFTER TAKEOFF, AND UPON GEAR RETRACTION, TAIL SKID LIGHT REMAINED ON. CYCLED GEAR NO AFFECT. CREW DUMPED FUEL, RETURNED TO MIA, AND LANDED WITHOUT INCIDENT. FOUND TAIL SKID HEEL MISSING AND BOLTS SHEARED. REPLACED DRAG LINK DOOR ASSEMBLY AND TAIL SKID ENERGY ABSORBER CARTRIDGE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L73 4F A3WE 20051026001312005102600131EU 2005 10 26 PNSA050906 120050926A2130522783 INDICATOR SAAB SF340 340B 7860101EU CABIN PRESSURE FAULTY A PNSAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 AL03676PA 316 WHILE ON CLIMBOUT AIRCRAFT CABIN PRESSURIZATION STARTED MAKING FULL SCALE FLUCTUATIONS OR HAD NO INDICATION AT ALL. PILOT REPORTED , ALSO THAT IT SEEMED TO HAVE NO POWER. CREW ELECTED TO RETURN TO DEPARTURE AIRPORT AND A UNEVENTFUL LANDING WAS ACCOMPLISHED. MX DISCOVERED A FAULTY CABIN PRESSURE INDICATOR, PART WAS REPLACED AND OPS CHECKED NORMAL. 2L72 4T RTA52EU 20051026001322005102600132CE 2005 10 26 ESUA08142005 120050814A2131660021115 THERMOSWITCH LEAR 35 35A 5170602CE GARRTTTFE731TFE731* 01518WP CABIN PRESSURE FAILED E ESUAO OTHER O OTHER NRNOT REPORTED 1 CE03351AS 146 THE AIRCRAFT EXPERIENCED A CABIN DEPRESSURIZATION AT FL390. THE CREW WAS ABLE TO MAINTAIN THE CABIN ALTITUDE AT BELOW FL100 (10,000 FEET) WITH THE EMERGENCY AIR AND WINDSHIELD HEAT VALVES. THE CREW ELECTED TO DON THEIR O2 MASK AND ASK FOR A EMERGENCY DESCENT. THE AIRCRAFT LANDED UNEVENTFULLY AT FINAL DESTINATION. 2L72 4F4 F A10CE E6WE 20051026001332005102600133NM 2005 10 26 C1HA200581018 120051017A2131 CONTROLLER BOEING727 7272S7 138407ZNM CABIN PRESSURE MALFUNCTIONED A C1HAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15681CA 22020 CLIMBING THROUGH FL290, NOTICED CABIN ALTITUDE RAPIDLY CLIMBING, ALTITUDE HORN THEN CAME ON, COULDN'T CONTROL CABIN, PERFORMED COM PROCEDURE 2.21.5 & THEN PERFORMED COM PROCEDURE 2.21.3. MAINTENANCE IS CURRENTLY TROUBLESHOOTING SYSTEM. 2L73 4F A3WE 20051026001342005102600134NM 2005 10 26 AWXA200501261 120051020A5330 SKIN BOEING737 73733A 1384673NM BS 927 DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 PHX - MAJOR REPAIR - DURING OVERNIGHT INSPECTION DISCOVERED 3.5 INCH CRACK IN FUSELAGE LOCATED AT STA 927 AND STR 25R. MAINTENANCE REMOVED DAMAGED SKIN IAW BOEING 737-300 SRM 53-00-01. FABRICATED DOUBLER, TRIPLER AND FILLER IAW BOEING 737-300 SRM 53-00-01 FIG 201. INSTALLED FABRICATED REPAIR PARTS AT STA 927 AND STR 25R IAW BOEING 737-300 SRM 53-00-01 FIG 201. [OPEN] 2L72 4F RTA16WE 20051026001352005102600135EU 2005 10 26 DHL2005365500 120051015A5753A57960050002000 RIB AIRBUS300 A300B4203 3930306EU NR 7 TE FLAP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01365DH46846 149 DURING ACCOMPLISHMENT OF EA57530001-001-A WHILE AT AVBORNE HEAVY MAINTENANCE INC LEFT INBOARD FLAP RIB NR 7 (FITTING} OUTBOARD SIDE FOUND CRACKED. REMOVED AND REPLACED NR 7 RIB IAW S/B A300-57-0242 REF ASTAR NON ROUTINE 034345. 2L72 4F RTA35EU 20051026001372005102600137WP 2005 10 26 ABXA050256 120051010A53305910228135 SKIN DOUG DC9 DC941 302207NWP BS 1087 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23962AX 47768 FUSELAGE CRACK AT STA. 1087, LONGERON 2 LEFT. REPAIRED AREA IAW DC-9 SRM 53-01. 2L72 4F A6WE 20051026001392005102600139WP 2005 10 26 ABXA050258 120051012A53475922358543 CARGO TRACK DOUG DC9 DC941 302207NWP BS 218-237 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23962AX 47768 FORWARD LOWER CARGO LEFT TRACK HAD EXFOLIATED CORROSION AT TWO ATTACH FASTENERS BETWEEN STA 218 AND 237. REPLACED BAD SECTION OF TRACK IAW DC-9 SSRM K05159 DRAWING. 2L72 4F A6WE 20051026001422005102600142NM 2005 10 26 2005UALA01163 120051018A2130 RELIEF VALVE BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN PRESSURE OPEN A UALAA UNSCHED LANDING W INADEQUATE Q C CRCRUISE 1 WP29556UA 26650 LOSS OF CABIN PRESSURE. LOWER POSITIVE PRESSURE RELIEF VALVE FOUND OPEN. REPLACED VALVE, OPS CHECKED OK. RETURNED AIRCRAFT TO SERVICE. 2L72 4F4 FRTA2NM E17NE 20051026001432005102600143NM 2005 10 26 2005UALA01164 120051019A3297 WARNING SYSTEM BOEING757 757222 1384956NM PWA 2037 PW2037 NE MLG ACTIVATED A UALAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 WP29523UA 24932 ANTI-SKID EICAS AND VIBRATION DURING TAKEOFF ROLL AND GEAR RETRACTION. REPLACED WIRING FR0M D2040 TO TB211, FOUND OPEN ON WIRE W4904-2501R-20. RE-SECURED SHIELDING PINS AT TB211 (LA4 AND LE4) ALL PER WD32-42-11. OPS CHK NORMAL. 2L72 4F4 FRTA2NM E17NE 20051026001452005102600145NM 2005 10 26 2005UALA01166 120051019A5330 SKIN BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU BS 363-365 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29336UA 24240 EXTERNAL FUSELAGE SKIN STA 363 TO 365 ABOVE STR 4R AT CHEM MILL STEP HAS A CRACK INDICATION. MAJOR REPAIR ACP'D - DOUBLER-TRIPLER REPAIR INSTALLED PER SRM 53-00-01 REPAIR 31 FIG 210 2L72 4F4 FRTA16WE E21EU 20051026001472005102600147NM 2005 10 26 2005UALA01168 120051019A2120 SMOKE BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU CABIN DETECTED A UALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP29928UA 26651 RETURNED TO FIELD DUE TO SMOKE IN CABIN. NO FINDINGS OF GALLEY EQUIPMENT FAILURE. FA REPORTS SMELL IN FWD AND AFT CABIN, INCLUDING SEAT 4D. SUSPECT OTHER SOURCE OF SMELL. DENVER ALSO RAN PACKS WITH APU AND ENGINE BLEEDS NOTED NO ELECTRICAL ODOR ON AIRCRAFT. NOTED AFT LAV SMELLED AS IF NOT SERVICED FOR DAYS AND STRONG ODOR FROM LAV. A FT LAV SERVICED, OPERATED AFT GALLEY EQUIP. NO ODOR NOTED. 2L72 4F4 FRTA16WE E21EU 20051026001482005102600148NM 2005 10 26 2005UALA01169 120051020A5330 SKIN BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29782UA 26948 FOUND DENT 3 FT FWD OF DOOR 4L, AND 1 FT BELOW DOOR THRESHOLD. SKIN DENT REPAIRED PER SRM. 2L72 4F4 FRTT0001SE E46NE 20051026001492005102600149NM 2005 10 26 2005UALA01170 120051020A5311 FRAME BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU BS 616 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29336UA 24240 MID CABIN LT FRAME IS CRACKED AT STUB BEAM AT STA 616 LOWER FASTENER HOLE. REPAIRED LT FRAME STA 616 REF MM 53-11-89 ,INSTALLED FILLER AND ANGLE DOUBLER. 2L72 4F4 FRTA16WE E21EU 20051026001522005102600152NM 2005 10 26 2005UALA01171 120051020A5311 FRAME BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU BS 616 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29336UA 24240 MID CABIN RT FRAME IS CRACKED AT STUB BEAM AT STA. 616 LOWER FASTENER HOLE. ACCOMPLISHED A REPAIR REF MM53-11-89, INSTALLED A FILLER AND DOUBLER ANGLE. 2L72 4F4 FRTA16WE E21EU 20051026001532005102600153NM 2005 10 26 2005UALA01172 120051020A5321 FLOOR PANEL BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU BS 280-348 CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29336UA 24240 FWD CABIN FLOOR RT INNER CORD UNDER FLOOR PANEL IS CORRODED, FROM BS 280 TO 348 WL 208.1 RBL 54. REMOVED AND REPLACED CREASE BEAM AND DRAIN PAN REF SRM 51-40-02. 2L72 4F4 FRTA16WE E21EU 20051026001552005102600155EU 2005 10 26 2005UALA01174 120051021A3350 POWER SUPPLY AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29419UA 487 FWD LEFT POWER SUPPLY UNIT AND BATTERY FOR EMERGENCY LIGHT INOP. REPLACED FWD LEFT POWER SUPPLY UNIT WITH BATTERY. 2L72 4F4 FRTA28NM E40NE 20051026001572005102600157NM 2005 10 26 2005UALA01176 120051014A3350 LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE ROW 29-32 INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29548UA 25396 EMERGENCY AISLE LIGHTS FROM ROW 29 TO 32 ARE INOP. REMOVED AND REPLACED BATTERY. 2L72 4F4 FRTA2NM E17NE 20051026001592005102600159 2005 10 26 QXEA200501365 420051024A2330 HANDSET DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE PA/INTERPHONE INOPERATIVE A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09353PH 496 FLIGHT ATTENDANTS PA AND INTERPHONE INOPERATIVE. MAINTENANCE REPLACED HANDSET. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20051026001602005102600160NM 2005 10 26 QXEA200501360 120051023A26113023143 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE CARGO BAY MALFUNCTIONED A QXEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM09357PH3152111998 504 MASTER WARNING (SMOKE) LIGHT IN FLIGHT. MAINTENANCE INSPECTED CARGO COMPARTMENT, NO EVIDENCE OF SMOKE OR SMOKE DAMAGE NOTED. REPLACED NR 1 AND NR 2 SMOKE DETECTORS, P/N 473054, S/N 1764, TSN 1681.4, CSN 12543. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20051026001612005102600161NM 2005 10 26 QXEA200501366 120051024A2430 WARNING LIGHT DHAV DHC8 DHC8202 2809007NM NR 2 GENERATOR FALSE ACTIVATIONA QXEAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 NM09367PH 511 SEA FLIGHT NR 2127, NR 2 DC GENERATOR STAYED ILLUMINATED AFTER START-UP. RECYCLED NR 2 DC GENERATOR OFF AND ON PER EMERGENCY CHECKLIST. LIGHT WENT OUT. OPERATED NORMAL FOR REMAINDER OF FLIGHT. MAINTENANCE COMPLIED WITH FUNCTIONAL TEST OF THE DC GENERATORS IAW -8 AMM 24-31-00, PAGE 501-504. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051026001622005102600162EA 2005 10 26 COMA0570114 120051020A2741 MOTOR CNDAIRCL600 CL6002C10 1390015EA STAB TRIM MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01653CA 10129 FLIGHT 5764 - STAB TRIM AND MACH TRIM CAUTION. CND RESET SYSTEM, OPERATIONAL CHECK WAS NORMAL. 2L72 4F RTA21EA 20051026001632005102600163EA 2005 10 26 COMA0560562 120051020A2750865D1007 PDU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION DEDESCENT 1 SO01818CA17855229 7408 FLIGHT 5582 - FLAPS FAIL CAUTION. CND REPLACED THE PDU FOR TROUBLESHOOTING. 2L72 4F RTA21EA 20051026001652005102600165NM 2005 10 26 SWAA053319 120051022A32606546141 SENSOR BOEING737 7373H4 1384600NM RT MLG OUT OF ADJUST A SWAAO OTHER N FALSE WARNING APAPPROACH 1 SW29611SW 27697 RT MLG UNSAFE LIGHT INDICATION, CYCLED THE GEARS AND OPERATED NORMAL. ADJUSTED RT MLG UPLOCK SENSOR PER MM. 2L72 4F RTA16WE 20051026001662005102600166NM 2005 10 26 SWAA053320 120051023A53306545774 SKIN BOEING737 7375H4 138449DNM BS 747-767 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29509SW 24186 FOUND FUSELAGE SKIN CRACKED AT BS 747 TO BS 767, BETWEEN STR 18L TO STR 19L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051026001712005102600171NM 2005 10 26 SWAA053325 120051023A53306545774 SKIN BOEING737 737301 1384611NM BS 884 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 884, STR 25R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051026001722005102600172NM 2005 10 26 SWAA053326 120051023A3350300432 LIGHT BOEING737 737301 1384611NM LT WING INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED A1 CHECK, FOUND EXTERNAL EMERGENCY EXIT LIGHT INOP AFT OF LT WING. RELAMPED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20051026001752005102600175NM 2005 10 26 SWAA053329 120051024A2913 PUMP BOEING737 7377H4 1384404NM NR 1 ENGINE MAKING METAL A SWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW29778SW 27883 AIR TURBACK, LANDING GEAR LEVER WOULD NOT MOVE TO THE UP POSITION AFTER T/O. FOUND METAL DEBRIS AT HYD A-SYS NR 1 ENG HYD PUMP CASE DRAIN FILTER. REMOVED AND REPLACED BOTH NR 1 ENG HYD PUMP CASE DRAIN FILTERS. REMOVED AND REPLACED HYD RESTRICTOR CHECK VALVE. REMOVED AND REPLACED LANDING GEAR BYPASS VALVE PER MM. OPS CK GOOD. 2L72 4F RTA16WE 20051026001762005102600176NM 2005 10 26 SWAA053330 120051024A52306545871 DOOR FRAME BOEING737 7373TO 138447GNM CARGO DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29697SW 23838 DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR LOWER FRAME CRACKED AT STOP FITTING CUT OUT. REMOVED AND REPLACED AFT CARGO DOOR PER MM. 2L72 4F RTA16WE 20051026001782005102600178EA 2005 10 26 COMA0570110 120051005A5315CC670341757 FLOORBEAM CNDAIRCL600 CL6002C10 1390015EA BS 280 CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01367CA7872 10069 FS 280 TRANSVERSE BEAM CORRODED BETWEEN LBL 36 TO RBL 36. REPAIRED IAW BOMBARDIER REO 670-53-11-047 REV C. 2L72 4F RTA21EA 20051026001792005102600179NM 2005 10 26 QXEA200501364 120051023A3010697079003 BRUSH BLOCK BOMBDRDHC8 DHC8402 1390042NM PROP DE ICE DAMAGED A QXEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM09409QX8009 4051 SEA FLIGHT NR 2345, PROP DE-ICE CAUTION LIGHT ILLUMINATED. RAN ONE (1) CYCLE IN FLIGHT PER CHECKLIST. RT PROP DEICE ADVISORY LIGHT ONLY CAME ON. NO ELEC LOADS NOTED ON ANY PHASE A/C. MAINTENANCE TROUBLE SHOT. FOUND NR 1 ENGINE BRUSE BLOCK GAP DISTANCE TO BE OUT OF LIMITS AND BRUSHES WORN ON ONE SIDE. REPLACED NR 1 ENGINE PROP BRUSH BLOCK PER AMM 30-61-14, PAGE 401-407. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051026001842005102600184NE 2005 10 26 MWEA050115 220051012A7200 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE NR 2 MALFUNCTIONED A MWEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31810ME 48072 NUMBER TWO ENGINE PRESSURE RATIO DECREASED AT 0.2 AND ENGINE PRESSURE RATIO AND 10 PERCENT N1 BOTH PACKS ALSO SHUTDOWN. SERVICED FUEL CONTROL BELLOWS. INSPECTED PT2 MOISTURE TRAP AND PT7 MOISTURE TRAP, PS4 STRAINER, CHECKED PT2 AND PT7 LINE AND FITTING AND B-NUT ON ENGINE AND PLYON SECURITY. 2L72 4F4 F A6WE E2EA 20051026001852005102600185 2005 10 26 ANCF200400054 420050927A34426225135202 ANTENNA BOEING757 75728A 1384976NM RROYCERB211 RB211535E4 54555NE WX RADAR SYS INOPERATIVE W ANCFO OTHER O OTHER CLCLIMB 1 SO23517NA22423220 24260 (WXR FAIL DISPLAYED ON HSI. WXR TEST INOP) IAW AMM 34-43-05/401 AND 34-3-00/401 WXR ANTENNA AND TRANSCEIVER WERE REPLACED. ANTENNA P/N 622-5135-202 S/N ON 1959 OFF 2967 TRANSCEIVER P/N 622-5132-101S/N ON 4604 OFF:6335 2L72 4F4 FRTA2NM E12EU 20051026001862005102600186CE 2005 10 26 BSYA200500013 120051006A5250 LATCH BEECH 58 58 1152740CE COCKPIT DOOR LACK OF LUBE E BSYAA UNSCHED LANDING O OTHER CLCLIMB 1 GL07297AT TH1349 COCKPIT DOOR CAME OPEN AFTER TAKEOFF. RETURNED TO TEB. MAINTENANCE LUBED DOOR LATCHES AND CABLE OPS CHECKS GOOD. 1L72 3O 3A16 20051026001872005102600187WP 2005 10 26 UPS05845563 120050922A5322 SHEAR TIE DOUG DC8 DC871F 302199DWP BS 55 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE:SP SHEAR TIE AT STA 55 L34R TO L34L HAS EXFOLIATION CORROSION. REMOVED SHEAR TIE AT STA 55 L34R - L34L IAW SRM 51-1-21 FABRICATED AND INSTALLED SHEAR TIE AT STA 55 L34R -L34L IAW DWG 5613836, SRM 51-1-21 AND SRM 51-1-20D. 2L74 4F RT4A25 20051026001882005102600188WP 2005 10 26 UPS05845564 120050930A5330 FINGER DOUBLER DOUG DC8 DC871F 302199DWP BS 70-190 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE: SP, FS 70 - FS 190 FINGER DOUBLER BETWEEN L30R - L32R IS CRACKED AND HAS EXFOLIATION CORROSION. REMOVED FINGER DOUBLER AT FS 70 - FS 190 L30R - L32R IAW SRM 51-1-21. FABRICATED AND INSTALLED FINGER DOUBLER AT FS 70 - FS 190 L30R - L32R IAW 53-04-01 AND SRM 51-1-21. 2L74 4F RT4A25 20051026001922005102600192WP 2005 10 26 UPS05845568 120050920A5330 FINGER DOUBLER DOUG DC8 DC871F 302199DWP BS 8-70 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE:SP FINGER DOUBLER AT FS 8 TO FS 70 L31R HAS EXFOLIATION CORROSION. REMOVED FINGER DOUBLER AT FS 8 - FS 70 L31R IAW SRM 51-1-20D FABRICATED AND INSTALLED FINGER DOUBLER AT FS 8 TO FS 70 IAW DWG 5649028 AND SRM 51-1-21. 2L74 4F RT4A25 20051026001982005102600198EU 2005 10 26 05FDEA03239 120051004A3230 LANDING GEAR AIRBUS300 A300F4605R 3930327EU RIGHT MALFUNCTIONED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25655FE 742 RIGHT MAIN LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. 2L72 4F RTA35EU 20051026002002005102600200NM 2005 10 26 AWXA200501161 120050919A53116546558 FRAME BOEING737 7373G7 1384595NM BS 907 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28322AW 25400 MCN - DURING 8 DAY CHECK, FOUND FRAME CRACKED AT FASTENER HOLE AT BS 907 BETWEEN STRINGERS 10R AND 11R. MAINTENANCE TRIMMED OUT DAMAGE TO FRAME AT BS 907 IAW BOEING 737-300 SRM 51-20-02-06. FABRICATED REPAIR CHANNELS AND FILLER IAW BOEING 737-300 SRM 53-60-07-01 FIG 1. INSTALLED FABRICATED REPAIR PARTS IAW BOEING 737-300 SRM 53-00-07-2R1 FIG 201. 2L72 4F RTA16WE 20051026002032005102600203NM 2005 10 26 AWXA200501164 120050910A5315654681143 FLOORBEAM BOEING737 7373G7 1384595NM BS 986 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 MCN - DURING C15 CHECK DISCOVERED CORROSION ON UPPER CAP OF FLOORBEAM, PREVIOUS BLEND OUT, AT BS 986 AND FROM BL 17R TO BL 44R. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-51-1A FIG 101. MAINTENANCE REMOVED FLOORBEAM UPPER CAP IAW BOEING 737-300 SRM 51-40-02-0G. FABRICATED REPAIR SECTION, SUPPORT ANGLE AND STRAPS IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5310-05258-ES1. INSTALLED FABRICATED REPAIR PARTS IAW AWA ER NR 03-5310-0528-ES1 AND BOEING 737-300 SRM 53-00-51-2R FIG 201. 2L72 4F RTA16WE 20051026002042005102600204NM 2005 10 26 AWXA200501165 120050910A532065C334192 SHEAR WEB BOEING737 7373G7 1384595NM BS 1016-1028 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 MCN - DURING C15 CHECK DISCOVERED LEVEL 2 GALVANIC CORROSION ON THE RT AFT LAV SUB-FLOOR (MAIN DECK) SHEAR WEB FROM BS 1016 TO BS 1028, BL 1R TO BL 36R, WL 208. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-51-1A-1 FIG 101. REMOVED SHEAR WEB IAW BOEING 737-300 SRM 51-40-02-0G FIG 8. INSTALLED NEW SHEAR WEB FROM BS 1016 TO BS 1028, BL 1R TO BL 36R, WL 208 IAW BOEING 737-300 SRM 51-40-02-0G FIG 3, 4, 6, 7, AND 8. 2L72 4F RTA16WE 20051026002072005102600207NM 2005 10 26 AWXA200501167 120050909A575465C26799 SKIN BOEING737 7373G7 1384595NM ZONE 500 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 MCN - DURING C15 CHECK DISCOVERED 4 CRACKS, .5 INCHES IN LENGTH, ON THE NR 1 SLAT SKIN BELOW THE OUTBOARD MAIN TRACK. MAINTENANCE TRIMMED OUT DAMAGED SKIN ON THE NR 1 SLAT IAW BOEING 737-300 SRM 57-43-01-2R FIG 201. FABRICATED FILLER AND SPLICE PATE IAW BOEING 737-300 SRM 57-43-01-2R FIG 201. INSTALLED REPAIR PARTS ON THE NR 1 SLAT SKIN BELOW OUTBOARD MAIN TRACK IAW BOEING 737-300 SRM 57-43-01-2R FIG 201. 2L72 4F RTA16WE 20051026002102005102600210NM 2005 10 26 05FDEA03205 120051004A5311 FAILSAFE BOEING727 727200 138407ENM BS 1148 FRAME CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 STA 1148 LBL 12 CORROSION ON BULK CARGO FRAME FAILSAFE CHORD. REPLACED STIFFENER AT BS 1148 LBL 12 PER 51-40-4. 2L73 4F RTA3WE 20051026002112005102600211EA 2005 10 26 SWIA200515639 120051002A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY MALFUNCTIONED A SWIAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 NM07943SW 7762 SMOKE CARGO MSG. WHILE AT GATE ONLY ON FOR 1 SEC. NO SMOKE OBSERVED IN CARGO BAY. REPLACED AFT SMOKE DETECTOR IAW CMM 26-10-73. OPERATIONAL CHECK GOOD, PN 473597-19, SN OFF 2271. 2L72 4F RTA21EA 20051026002132005102600213NM 2005 10 26 2005UALA01071 120051003A5313 STRINGER BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE BS 907 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29919UA 25386 AFT CABIN STA 907 STR 4L IS CRACKED AT 2 EA FASTENER HOLES. REPLACED STRINGER SPLICE. REF SRM 51-40-02. 2L72 4F4 FRTA16WE E2GL 20051026002152005102600215NM 2005 10 26 2005UALA01075 120050921A5754144N300334 WEDGE BOEING BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 6 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29524UA 24977 SLAT HAS DAMAGED DELAMINATED T/E WEDGE. WEDGE REPLACED. 2L72 4F4 FRTA2NM E17NE 20051026002162005102600216NM 2005 10 26 2005UALA01076 120051002A2430 TRANSFORMER BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE NR 1 OVERHEATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29378UA 24653 NR 1 TRANSFORMER, RECTIFIER WAS FOUND TO HAVE OVERHEAT DAMAGE. FOUND GRND PWR CB-S BURNT. COVER OVER ALL THREE TRANSFORMER-RECTIFIER UNITS WAS BURNED, DUE TO SUSPECTED OVERHEAT IN ONE OR MORE TRS. ALL THREE TRS REPLACED, AS WAS THE BATTERY, BATTERY CHARGER, TR1 CIRCUIT BREAKER C806, AND GROUND SERVICE CIRCUIT BREAKER C813. ALL UNITS REPLACED PRECAUTIONARY. AS OF 10/25 NO SHOP FINDINGS AVAILABLE FOR ANY OF THE REMOVED UNITS. 2L72 4F4 FRTA16WE E2GL 20051026002172005102600217NM 2005 10 26 2005UALA01081 120051004A3350 LIGHT BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE CABIN INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29938UA 26671 EMERGENCY EXIT PATH LIGHTING IN REAR THIRD OF AIRCRAFT NOT WORKING. REPLACED POWER STRIP. 2L72 4F4 FRTA16WE E2GL 20051026002202005102600220SO 2005 10 26 1341092905 120050929A3213 STRUT GULSTMG1159 GIV 3980115SO RIGHT COLLAPSED E N93AO OTHER O OTHER TXTAXI/GRND HDL 1 SO13441QS 1341 RIGHT MLG STRUT COLLAPSED WHILE WAITING TO DEPART. 2L72 4F RTA12EA 20051026002232005102600223NM 2005 10 26 05FDEA03443 120051018A5312 BULKHEAD DOUG MD11 MD11 3023602NM BS 2007 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 AFT CABIN STA 2007 RBL 103 TO 107, Z=-18, AFT PRESSURE BULKHEAD T-CHORD FOUND REPAIR PATCH . SNRM N0845: WORK ACCOMPLISHED AS PER EA#1-5310-87647 TITLE: FUSELAGE- MAIN FRAME- PRESSURE BULKHEAD BODY STA. Y = 2007.000, TEE CHORD REPAIR. CLASSIFIED MAJOR REPAIR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20060222000802006022200080NM 2006 2 22 05FDEA04163 120051206A5310 DOOR FRAME DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 SNRM N1259: AFT CARGO COMPARTMENT: UPON REMOVAL OF LOOSE SEALANT AFT DOOR JAMB STA 1935 ADJACENT TO FWD LATCH FOUND CORRODED.**S/D COMING** 2L73 4F RTA22WE 20060222001062006022200106NM 2006 2 22 05FDEA04341 120051215A5700 REPAIR BOEING727 727200 138407ENM UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25274FE 22039 FOUND PREVIOUS REPAIR ON LOWER SURFACE OF RIGHT INBOARD AFT FLAP WAS ACCOMPLISHED IAW SRM 57-50-4 FIG 5, PAGE 12, BASED ON AN EXTERNAL EVALUATION CONSISTED OF LOCATION, SIZE, SHAPE, FASTENER SPACING AND NUMBERS, MATERIAL THICKNESS AND GENERAL WORKMANSHIP, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2L73 4F RTA3WE 20060222001082006022200108NM 2006 2 22 05FDEA04296 120051214A5313AFA77761 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 CENTER CARGO COMPARTMENT STATION 1561 TO STA 1581 LONGERON 48 LEFT HAND FOUND CORRODED. CTR CARGO COMPARTMENT STATION 1561 TO STA 1581 LONGERON 48 LT REPAIR CARRIED OUT AS PER SRM 53-10-00 FIG 2 VOL I . REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20060223000062006022300006 2006 2 23 STN121305 420051213A2565101651303 SLIDE BOEING767 767238 1385114NM PWA JT9 JT9D* NE L1 DOOR DETACHED A L43AK NONE O OTHER ININSP/MAINT 1 EA27770WD537805231 23306 L1 DOOR SLIDE DETACHED FROM DOOR. 2L72 4F4 FRTA1NM E20EA 20060223000102006022300010 2006 2 23 200519 420051214A3417 COMPUTER DHAV DHC8 DHC8103 1386005NM AHRS MALFUNCTIONED A KPVAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 WP13806WP 357 (PIREP) DADC DATA INVALID DISPLAYED ON ADVISORY DISPLAY ON TAKEOFF ROLL. (MX) PERFORMED AHRS SELF TEST IAW DHC-8 MM 34-20-14 PG 202-203 PAR 2B. NO FAULTS FOUND OK FOR SERVICE. 2H72 4T RTA13NM 20060223000152006022300015EU 2006 2 23 05FDEA04313 120051213A324635242100 COMPENSATOR AIRBUS310 A310222 3930315EU BRAKE TEMP MALFUNCTIONED A FDEAO OTHER J WARNING INDICATION TOTAKEOFF 1 SO25419FE 345 DURING L/G RETRACTION AT FLL, ALL 4 RT SIDE BRAKE TEMP INDICATORS SHOWED 700*ITH CORRESPONDING CAUTION. LOWERED GEAR FOR COOLING AFTER APPROX 1 MIN CAUTION WENT AWAY AND BRAKES TEMP INDICATED FROM 125 TO 150 (LEFT MAIN TEMPS 50- 65). ALL OTHER INDICATIONS NORMAL. ON TOUCHDOWN RT WHEEL TEMP INDICATIONS SHOWED 700 THEN RETURNED TO NORMAL INDICATIONS. DURING T/S FOUND 4GW TO BE BAD. 4GW NEEDS TO BE REPLACED PER A310- 200 AMM ATA 32-47-13-4. REMOVED AND REPLACED RT BRAKE TEMP COMPENSATOR IAW A310 AMM 32-47-13-4. OPS CHECK GOOD AT THIS TIME. OFF MFG 35-242-100 POS 2SRL 242002046 TAG 7A2184ON MFG 35-242-100SRL BB0091 TAG 152A69S. 2L72 4F RTA35EU 20060223000162006022300016NM 2006 2 23 05FDEA04298 120051214A5101AFA774014 REPAIR DOUG MD11 MD11 3023602NM ZONE 200 NONE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 SEAT TRACK MISMATCH RIGHT OUTBOARD CURVED TRACK FS1879. SNRM N2649: PREVIOUS REPAIR AT RIGHT HAND OUTBOARD CURVED SEAT TRACK AT FUSELAGE STATION 1879 MISMATCH EVALUATED AND FOUND REPAIR PREVIOUSLY ACCOMPLISHED IN ACCORDANCE WITH DELTA AIRLINES ENGINEERING REPAIR/AUTHORIZATION 333185-14, TITLE: FUSELAGE/CABIN/SEAT TRACK MISMATCH/RT OUTBOARD CURVED TRACK/FS1879. REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100. 2L73 4F RTA22WE 20060223000182006022300018NM 2006 2 23 05FDEA04345 120051215A3210 TRIM CYLINDER DOUG MD11 MD11 3023602NM MLG UNKNOWN A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25596FE 48554 ON GEAR RETRACTION RIGHT MAIN GEAR ILLUMINATED RED ON BOTH PRIMARY AND SECONDARY DISPLAYS. FOLLOWED QRH, CYCLED LANDING GEAR. AS SOON AS GEAR HANDLE DOWN, RIGHT MAIN SHOWED GREEN ON BOTH DISPLAYS (IE, NEVER IN TRANSIT). RETURNED TO HKG, DID NOT DECLARED EMERGENCY AND NO FUEL DUMP. REMOVED AND REPLACED RT MAIN LANDING GEAR TRIM CYLINDER PER MM 32-37-01-4. PERFORMED LANDING GEAR RETRACTION AND EXTENSION, ALTERNATION EXTENSION, FREE FALL OPERATION CHECK. ALL WORK OK AND INDICATION NORMAL PER MM 32-30-00. A/C OK FOR SERVICE. 2L73 4F RTA22WE 20060223000372006022300037WP 2006 2 23 05FDEA04310 120051214A5310 DOUBLER DOUG DC10 DC1030 3023501WP GE CF6 CF650C2 30018NE BS 595 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 PERFORMED INSPECTION IAW EO 8-5100-7-5001-P1 FOUND DOUBLER DIM 15 INCHES BY 14 INCHES LT EXT FUS STA 595 LONG 46 TO LONG 48. PERFORMED A GVI OF REPAIR IAW SRM 53-20-00 FIG 2 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001-1D E3. 2L73 4F4 F A22WE E23EA 20060223000532006022300053NE 2006 2 23 VTZA200500222 220051217A7261 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RIGHT MALFUNCTIONED A VTZAE ENGINE SHUTDOWN JK WARNING INDICATION FLUID LOSS DEDESCENT 1 EA27650BR 7418 RIGHT ENGINE LOW OIL PRESSURE ON DESCENT 25PSI, ENGINE SHUTDOWN. 2L72 4F4 FRTA21EA E15NE 20060223000692006022300069EU 2006 2 23 200512251 120051225A3244 TIRE EMB ERJ170ERJ170100 EU MLG FAILED A UHLAO OTHER J WARNING INDICATION APAPPROACH 1 GL17648RW 17000068 CREW REPORTED, DID NOT HAVE A DOWN AND LOCKED GEAR INDICATION. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. FOUND NR 3 TIRE BLOWN WHICH CAUSED DAMAGE TO WEIGHT ON WHEELS HARNESS. 2L74 4F RTA56NM 20060223001052006022300105SW 2006 2 23 HEEA107309 120051129A7700212075037101 INDICATOR BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE NR 2 ENGINE UNKNOWN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893N 33010 EN ROUTE TO VHPW, ENGINE OUT LIGHT CAME ON FOR NUMBER 2 ENGINE. PARTICLE SEPARATOR FOR NR 2 CAME ON AND N1 GAUGE FOR NR 2 WENT TO ZERO. ITT AND N2 WAS NORMAL. RETURNED TO EZF AND CONTACTED MAINTENANCE. 1G72 4U4 U H4SW E22EA 20060223001142006022300114NE 2006 2 23 HEEA107308 120051115A32607655200904046 DOWNLOCK SKRSKYS76 S76A 8143006NE MLG FALSE INDICATIONB HEEAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW03761PH 760224 TEN MINUTES OUT, AN AIRCRAFT REPORTED THAT ONE MAIN LANDING GEAR WAS DOWN OR PARTIALLY DOWN. SLOWED TO 130 KTS AND FLEW BY TOWER AND THEY CONFIRMED THE LT MAIN GEAR WAS DOWN. COCKPIT INDICATIONS SHOWED GEAR UP AND LOCKED. LOWERED LANDING GEAR AND GOT INDICATION OF ALL GEAR DOWN AND LOCKED. MAINTENANCE REPLACED THE LT MAIN GEAR DOWN LOCK SENSOR AND INSPECTED AIRCRAFT IAW LETTER DATED 11-16-05 FROM MFG. 1G72 3U H1NE 20060223001172006022300117NE 2006 2 23 HEEA107319 120051210A7997 WIRE SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL OIL TEMP IND BROKEN E HEEAO OTHER N FALSE WARNING CRCRUISE 1 SW03763P 760166 IN CRUISE FLIGHT, NR 2 ENGINE OIL TEMPERATURE SUDDENLY DROPPED TO ZERO. LANDED WITHOUT INCIDENT. MAINTENANCE REPAIRED BROKEN WIRE TO TEMP BULB IN THE ENGINE INTAKE AREA. 1G72 3U3 U H1NE E1GL 20060223001242006022300124SW 2006 2 23 HEEA107327 120050908A6340212075036101 INDICATOR BELL 412 412 1182202SW MAIN ROTOR FLUCTUATES B HEEAO OTHER J WARNING INDICATION CRCRUISE 1 SW033893P 33012 WHILE PERFORMING CRUISE CHECKLIST, NOTED C-BOX OIL PRESSURE LOW AND FLUCTUATING. MAINTENANCE REPLACED INDICATOR. 1G72 4U H4SW 20060223001262006022300126SW 2006 2 23 HEEA107332 120050624A2913AN6289D4 NUT BELL 214 214ST 1182106SW HYD PUMP SPLIT B HEEAO OTHER J WARNING INDICATION CLCLIMB 1 SW035748M 28102 SHORTLY AFTER TAKEOFF, THE NR 2 HYDRAULIC LIGHT ILLUMINATED. RETURNED TO MORGAN CITY. MAINTENANCE FOUND A JAM NUT ON A FITTING ON THE HYDRAULIC MANIFOLD SPLIT ALLOWING THE PACKING TO UNSEAT UNDER PRESSURE CAUSING THE LOSS OF HYDRAULIC FLUID. REPLACED THE NUT AND PACKING. ALSO REPLACED THE HYDRAULIC PUMP AS A PRECAUTION DUE TO IT RUNNING DRY. 2G72 4U H10SW 20060223001312006022300131NE 2006 2 23 HEEA107340 120050110A32977655200904045 WIRE HARNESS SKRSKYS76 S76A 8143006NE LT MLG UNKNOWN B HEEAO OTHER P NO WARNING INDICATION CLCLIMB 1 SW031546K 760082 AFTER TAKEOFF, WHEN LANDING GEAR WAS RETRACTED, LEFT MAIN GEAR WARNING LIGHT DID NOT EXTINGUISH. REPLACED HARNESS. 1G72 3U H1NE 20060223001392006022300139NE 2006 2 23 HEEA107352 120050721A79210401272820 DUCT SKRSKYS76 S76A 8143006NE OIL COOLER COLLAPSED B HEEAO OTHER J WARNING INDICATION CLCLIMB 1 SW0389H 760406 AFTER DEPARTURE, NR 2 ENGINE OIL TEMP GAUGE SHOWED TEMPERATURE ABOVE RED LINE. EMERGENCY PROCEDURE PERFORMED. FOUND OIL COOLER DUCT COLLAPSED INSIDE. REPLACED DUCT. 1G72 3U H1NE 20060223001902006022300190NE 2006 2 23 HEEA107420 120051213A31107610708004119 ISOLATION MOUNT SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL COCKPIT UNKNOWN E HEEAO OTHER O OTHER CRCRUISE 1 SW03792P 760193 IN CRUISE FLIGHT THE AIRFRAME DEVELOPED A LATERAL VIBRATION WHICH INCREASED IN DIRECT PROPORTION TO THE INCREASE OF AIRSPEED. MAINTENANCE REPLACED TWO BIFILAR BUMPERS AND THE MOUNTING CLAMPS (PN 700006-2) AND (PN 6438B-103) ON ONE ALTITUDE INDICATOR AND ONE HSI. 1G72 3U3 U H1NE E1GL 20060223002012006022300201EU 2006 2 23 05FDEA04107 120051203A5101 REPAIR AIRBUS310 A310203 3930313EU HORIZ STAB MISINSTALLED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25424FE 241 COMPLY WITH AGING 9-AGING-INSP, PREVIOUS REPAIR INSTALLED AT LEFT HAND HORIZONTAL STABILIZER (LEADING EDGE ROOT SECTION) AT WS 95 TO WS 105. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR NEW REPAIR ACCOMPLISHED PER SRM 55-12-12 FIG 203 AND 55-12-19 FIG 201 REPAIR EVALUATED OPER GMM 6-2-100 AND CLASSIFIED AS MAJOR. 2L72 4F RTA35EU 20060223002022006022300202EU 2006 2 23 05FDEA04108 120051203A5101 REPAIR AIRBUS310 A310203 3930313EU RUDDER MISREPAIRED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25424FE 241 COMPLY WITH AGING 9-AGING-INSP, PREVIOUS MAJOR REPAIR INSTALLED ON RUDDER FRONT SPAR PER FEDEX EA 6-5540-89212 IS NOT IN ACCORDANCE REPAIR DATA SRM 51-77-12 REFERENCED IN EA INJECTION HOLES ARE NOT COMPLETELY FILLED LEAVING AVOID. REPAIRED PER SRM 51-77-12 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR. 2L72 4F RTA35EU 20060223002322006022300232EU 2006 2 23 YENA200591 120051229A3297 CONNECTOR EMB ERJ170ERJ170100 EU BRAKES DIRTY A YENAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA15179JB 19000006 ON TAKEOFF BELOW 40 KTS RECEIVED AURAL NO TAKEOFF BRAKE WARNING. NO EICAS MESSAGES, BRAKE HANDLE WAS OFF, PARKING BRAKE LIGHT WAS OFF. OP CHECKED PRESSURE SWITCHES IAW 32-44-09 CHECKED INTEGRITY OF SWITCHES WITH BRAKE ON AND OFF BY USING OHM METER. SWITCHES CHECKED GOOD IN BOTH POSITIONS. CLEANED CONNECTORS AND CHECKED SWITCHES FOR BENT OR DEFORMED PINS. ALSO NO LEAKAGE FOUND AT SWITCHES. OP CHECKED PARKING BRAKE IAW 32-44-09 OPS NORMAL. 2L74 4F RTA56NM 20060223002412006022300241NM 2006 2 23 SPAA0500077 120051215A2560P4010021 BATTERY BOEING737 7372Y5 1384554NM PWA JT8 JT8D15A 52051NE FLASHLIGHT DISCHARGED A SPAAK NONE L NO TEST ININSP/MAINT 1 WP28712S 23038 EMERGENCY FLASHLIGHT BATTERY DEAD AT AFT FLIGHT ATTENDANT STATION. REPLACED EMERGENCY FLASHLIGHT BATTERY IAW MM 25-69-0 AND 20-50-11, OPS CHECK NORMAL. 2L72 4U4 FRTA16WE E2EA 20060223002482006022300248NM 2006 2 23 SPAA0500049 120051214A5330 SKIN BOEING737 7372T4 1384492NM FUSELAGE CRACKED A SPAAK NONE O OTHER ININSP/MAINT 1 WP28703S 22529 CRACK IN FUSELAGE SKIN AT FWD LWR L-2 DOOR CUTOUT, BS 947.5 STR 14 LT. REPAIRED CRACK IAW SRM 53-30-3. 2L72 4F A16WE 20060223002492006022300249NM 2006 2 23 SPAA0500079 120051214A5330 SKIN BOEING737 7372T4 1384492NM FUSELAGE CRACKED A SPAAK NONE O OTHER ININSP/MAINT 1 WP28703S 22529 CRACK IN FUSELAGE SKIN AT FWD LWR L-2 DOOR CUTOUT, BS 947.5 STR 14 LT. REPAIRED CRACK IAW BOEING SRM 53-30-3. 2L72 4F A16WE 20060223002932006022300293NM 2006 2 23 DHL2006752500 120051229A5230 HINGE BOEING727 727223 1384074NM MAIN CARGO DECK CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01752DH 22466 DISCREPANCY FOUND NR 110541; EXT FUSE BS 510 MCD FWD HINGE SECT HAS FWD LOBE CRACKED. REMOVED FWD SECTION OF MCD HINGE AT BS 510-530 AND REPLACED WITH NEW SECTION PO NR 9002527 P/N MS20001-16-7200 IAW B727 AEI M/M CHAPTER 52 FIG 5201B, REV F DATE 01-22-01 2L73 4F A3WE 20060223002942006022300294NM 2006 2 23 DHL2006752502 120051229A5754 SKIN BOEING727 727223 1384074NM L/E SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01752DH 22466 DISCREPANCY FOUND NR 110620; CRACK INDICATION ON NR 2 SLAT SKIN UPPER SURFACE 6 INCHES O/B OF ACTUATOR MARKED. CUT OUT DAMAGED AREA DIMENSION 4" X 2" AND FABBED NEW DOUBLER FROM MATERIAL USE 2024 T3 0.80 PO 9002459 IAW B727 SRM 57-50-3 FIG 1 TREATED AND PRIMED IAW B727 SRM 51-10-2 INSTALLED NEW DOUBLER IAW B727 SRM 57-50-3 FIG 1 DOUBLER DIM 7 3/4" X 5 1/2" 2L73 4F A3WE 20060223003022006022300302NM 2006 2 23 05FDEA04162 120051206A5280ARC28272 DOOR DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE RT MLG CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RT MLG FLIPPER DOOR FORWARD HINGE AREA SUSPECTED WITH A HAIR LINE CRACK. REPAIR CARRIED OUT AT RT MLG FLIPPER DOOR FORWARD HINGE. CRACKED AREA IAW SRM 52-10-00 FIGURE 18 VOLUME I. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. 2L73 4F4 FRTA22WE E24NE 20060223003052006022300305NM 2006 2 23 05FDEA04414 120051227A5330 SKIN BOEING727 727100 1384036NM FUSELAGE LIGHTNING STRIKEA FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 N00280 LIGHTNING STRIKE IN EXTERNAL FUSELAGE SKIN AT BS 1167, STR 13R. DETERMINED LIGHTNING STRIKE DAMAGE IN SKIN AT BS 1167, STR 13R TO BE OUT OF LIMITS, REPAIRED IAW SRM 53-30-3 FIG 13A. 2L73 4F RTA3WE 20060223003082006022300308NM 2006 2 23 05FDEA04412 120051227A5320 STRAP BOEING727 727100 1384036NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 N00310 CORROSION ON REINFORCEMENT STRAP AT UPPER FLANGE OF FLOORBEAM AT BS 1130 RBL 63, WL 208. REMOVED AND REPLACED REINFORCEMENT STRAP AT UPPER FLANGE OF FLOORBEAM AT BS 1130, RBL 63, WL 208, PER SRM 51-30-2. 2L73 4F RTA3WE 20060223003092006022300309NM 2006 2 23 05FDEA04394 120051221A5210 STOP FITTING BOEING727 727200 138407ENM ENTRY DOOR GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 N00757 FORWARD ENTRY DOOR AFT LOWER STOP PIN FITTING GOUGED. COMPLIED WITH FED EX EA 7-5210-91434. 2L73 4F RTA3WE 20060224000262006022400026EU 2006 2 24 05FDEA04099 120051203A5101 REPAIR AIRBUS310 A310 EU FUSELAGE NONE A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25424FE 241 PREVIOUS REPAIR INSTALLED AT RIGHT HAND INBOARD FLAP (METAL CENTER SECTION), AT WS 192 TO WS 222. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 57-52-12 FIG.205 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR 2L72 4F RTA35EU 20060223000012006022300001NM 2006 2 23 PCSA12140501 120051214A5242 DOOR BOEING727 727231 1384079NM E/E BAY OPEN A PCSAJA DUMP FUEL UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 SO29905AJ 21989 FLIGHT 8313 DEPARTED AND DURING CLIMB OUT CREW REPORTED AIRCRAFT WOULD NOT PRESSURIZE, CREW DUMPED FUEL AND RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE LOWER 43 ELECTRONICS COMPARTMENT DOOR OPEN, ALSO THE COCKPIT DOOR WARNING INDICATION LIGHT WAS TROUBLESHOT AND A BROKEN WIRE WAS FOUND AT THE LOWER 43 ELECTRONICS COMPARTMENT DOOR. THE LOWER 43 ELECTRONICS COMPARTMENT DOOR SWITCH BROKEN WIRE WAS REPAIRED IAW MM CH 20-10-13 AND OPERATIONALLY CHECKED NORMAL IAW MM CH 52-70-01. A PRESSURIZATION CHECK WAS ACCOMPLISHED IAW WORK CARD 7-29, PRESSURIZATION SYSTEM OPERATIONALLY CHECKED NORMAL, AND AIRCRAFT WAS RETURNED TO SERVICE. 2L73 4F A3WE 20060223000022006022300002SO 2006 2 23 LR7A05207 120051211A5340342593L SUPPORT BRACKET LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FS 858 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03406LC 82 4676 DURING A-CHECK IAW HA1200 FOUND LT LWR SLOPING LONGERON SUPPORT BRACKET CRACKED AT FS858, WL187, LBL63. REPLACED FITTING IAW SMP583 CH 51-10 AND 51-70. LP NR 21479 ITEM M2. 2H74 4T4 T A1SO E282 20060223000382006022300038WP 2006 2 23 05FDEA04359 120051216A5753 SKIN DOUG DC10 DC1010 3022110WP ZONE 600 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25359FE 46635 RIGHT WING FLAP LOWER SKIN DENT AT XFS 674, 22" FROM TRAILING EDGE IS OUT OF LIMITS. REPAIRED SKIN IAW DC-10 SRM 57-10-00 FIG 85 VOL I. SEE FEDEX NONROUTINE NR N00599 OF WORK ORDER 00031297. 2L73 4F A22WE 20060223000442006022300044CE 2006 2 23 DJFA2005176 120051215A783022500231 SWITCH BEECH MU300 400A 1155402CE PWA JT15 JT15D5 52112NE THRUST REVERSER FAULTY E DJFAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA23783TA RK234 THE CREW REPORTED THAT SHORTLY AFTER LIFT OFF, THE RT THRUST REVERSER ARM LIGHT BEGAN TO FLICKER, AND THEN REMAINED ILLUMINATED. AFTER THE LANDING GEAR AND FLAPS WERE RETRACTED, THE EMERGENCY STOW SWITCH WAS DEPRESSED. THE AIRCRAFT WAS DIVERTED WHERE IT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED A FAULTY STOW SWITCH FOR THE RT THRUST REVERSER. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4F4 FRTA16SW E25EA 20060223000462006022300046EU 2006 2 23 R61A200500001 120051128A3350340022 BATTERY PACK EMB ERJ170ERJ170100 EU EMERGENCY LIGHTSINOPERATIVE A R61AO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL11827M 516 17000047 EMERGENCY LIGHT ON FAULT MESSAGE ON EICAS. REPLACED FAULTY BATTERY PACK. 2L74 4F RTA56NM 20060223000482006022300048NM 2006 2 23 05FDEA04378 120051220A7711 INDICATOR BOEING727 727225 1384077NM NR 3 EPR INOPERATIVE A FDEAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 SO25463FE 22551 NR 3 EPR GAUGE DID NOT MOVE WHEN THROTTLES ADVANCED FOR TAKEOFF. RELEASED FOR SERVICE PER MEL/CDL: 77-01-01 CATEGORY: A EXPIRATION: 23DEC05 "MEL 77-01-01: NR 3 ENGINE EPR INDICATOR INOP." 2L73 4F A3WE 20060223000542006022300054EA 2006 2 23 REXA200500158 120051216A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A REXAO OTHER J WARNING INDICATION APAPPROACH 1 SO258903A 7903 FLAPS FAILED ON APPROACH. FOLLOWED QRH UNEVENTFUL LANDING. FLAPS RESET AND PLACED ON 72 HOUR WATCH PER AD 98-20-01. 2L72 4F RTA21EA 20060223000592006022300059NM 2006 2 23 05FDEA04366 120051216A2611105080037525 FIRE LOOP BOEING727 727227 1384078NM NR 2 ENGINE FALSE ACTIVATIONA FDEAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO25491FE 21529 MASTER FIRE WARNING LIGHT ILLUMINATED IN FLIGHT INTERMITTENTLY. NO OTHER FIRE INDICATIONS. NR 2 ENGINE LOOP WILL NOT TEST REF AMM 26-11-000-1. REMOVED AND REPLACED ENG NR 2 SENSING ELEMENT IAW MM 26-11-012-4. OPS TEST NR 2 FIRE LOOP PER MM 26-11-000-5. OPS TEST NORMAL ON GROUND PER JRH RAN NR 2 ENG ALL INDICATION WERE NORMAL. OK TO CONTINUE. 2L73 4F A3WE 20060223000612006022300061NM 2006 2 23 05FDEA04395 120051221A5310 STRUCTURE BOEING727 72722 1384002NM BS 297 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 BS 297 CORROSION ON LT LOWER NOSE CHORD. 2L73 4F A3WE 20060223000632006022300063NM 2006 2 23 05FDEA04398 120051221A5753 FLAP TRACK BOEING727 727227 1384078NM NR 2 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 NR 2 FLAP TRACK HAS CORROSION AT BOLT HOLES. REPLACED NR 2 FLAP TRACK ON CUSTOMER CARD 27X5706-03. 2L73 4F A3WE 20060223000642006022300064EU 2006 2 23 05FDEA04399 120051222A2721359301001 INDICATOR AIRBUS310 A310203 3930313EU RUDDER TRIM SMOKE A FDEAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO25411FE3618 3618 359 N CRUISE BURNING SMELL IN COCKPIT, DIVERTED AND LANDED. STRONGEST SMELL FROM THROTTLE QUADRANT AREA, FIRE CREW TEMP DETECTOR SHOWED HIGHEST HEAT IN THAT LOCATION. NEVER ANY VISIBLE SPARKS OR FLAMES, SOME SMOKE. INSPECTED THROTTLE QUADRANT AREA AND FOUND THE RUDDER TRIM INDICATOR BURNED UP. NO OTHER DAMAGE FOUND IN THE AREA. REMOVED AND REPLACED THE RUDDER TRIM INDICATOR. OP CHECK NORMAL PER MM 27-22-22-4G 27-12-00, 27-27-00. PREMATURE REMOVAL/INSTALLATION OFF MFG 35-930-1001. 2L72 4F RTA35EU 20060223000932006022300093NE 2006 2 23 Z1RA107283 120051206A30977630407900111 HEATER SKRSKYS76 S76C 8143008NE NR 1 NACELLE INOPERATIVE B Z1RAK NONE J WARNING INDICATION ININSP/MAINT 1 SW11760AF3233 760523 NR 1 ENGINE HEATED FIREWALL INOP, WILL NOT HEAT. TEMP SENSOR BAD. 1G72 3U NCH1NE 20060223001152006022300115SW 2006 2 23 HEEA107314 120051109A2910MS2877806 PACKING BELL 212 212 1181420SW PWA PT6T PT6T3 52045EA NR 1 HYD SYSTEM INOPERATIVE E HEEAO OTHER K FLUID LOSS CLCLIMB 1 SW035736J 31140 ON CLIMB-OUT HEARD A LOUD WHINNING NOISE, HYDRAULIC CAUTION LIGHT CAME ON AND NR 1 HYDRAULIC PRESSURE WENT TO ZERO. STARTED EMERGENCY CHECK LIST AND NOISE STOPPED AND PRESSURE CAME BACK UP. MOMENTS LATER NOISE RETURNED AND PRESSURE DROPPED TO ZERO. MAINTENANCE REPLACED THE PACKING AND RETAINER MS28773-06 ON THE HYDRAULIC PUMP DISCHARGE FITTING. 1G71 4U4 U H4SW E22EA 20060223001202006022300120 2006 2 23 HEEA107322 420051102A3197E284C24 WIRE BELL 214 214ST 1182106SW WARNING LIGHT BROKEN B HEEAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW038045T 28101 IN FLIGHT, NR 2 FUEL VALVE CAUTION LIGHT ILLUMINATED. DEVIATED TO HOUMA AND NOTIFIED MAINTENANCE. MAINTENANCE FOUND BROKEN WIRE BEHIND INSTRUMENT PANEL APPROXIMATELY 8. 2G72 4U H10SW 20060223001302006022300130SW 2006 2 23 HEEA107339 120050209A6340214040806003 PRESSURE SWITCH BELL 214 214ST 1182106SW MAIN ROTOR MALFUNCTIONED B HEEAO OTHER J WARNING INDICATION CRCRUISE 1 SW0359806 28140 DURING CRUISE FLIGHT TRANSMISSION CAUTION LIGHT ILLUMINATED. MAINTENANCE REPLACED THE PRESSURE SWITCH AND THERMO SWITCH 214-040-805-001. 2G72 4U H10SW 20060223001342006022300134GL 2006 2 23 HEEA107346 220050419A720023063392 ENGINE BELL 407 407 1182206SW ALLSN 250C 250C47B GL NOISY B HEEAO OTHER E VIBRATION/BUFFET DEDESCENT 1 SW03510PH4504 53209 UPON DESCENT, CREW NOTICED UNUSUAL NOISES COMING FROM THE ENGINE COMPARTMENT. ENTERED A POWER-ON AUTO ROTATIONAL PROFILE AND LANDED IN A NEARBY FIELD. MAINTENANCE REPORTS, ENGINE HAS A NOISE AT FULL THROTTLE, FLAT PITCH, THAT WILL INCREASE IN INTENSITY WHEN TORQUE IS APPLIED AND LOUDEST JUST AFT OF THE EXHAUST COLLECTOR. THE NOISE WAS DESCRIBED AS A HIGH PITCH GROWL TYPE SOUND THAT OSCILLATES. THE CREW IN THE AFT CABIN HAD FIRST THOUGHT THE WHELAN SIREN WAS ON. REPLACED ENGINE. 1G71 3U3 UO H2SW E1GL 20060223001372006022300137NE 2006 2 23 HEEA107350 120050404A29107665103003053 TUBE SKRSKYS76 S76A 8143006NE HYD SYSTEM LEAKING B HEEAO OTHER K FLUID LOSS CLCLIMB 1 SW031545K 760047 AFTER TAKEOFF, THE ODOR OF HYDRAULIC OIL WAS NOTED IN THE COCKPIT, THE AIRCRAFT WAS TURNED AROUND AND LANDED. AFTER LANDING, THE NR 2 HYDRAULIC PRESSURE FLUCTUATED AND STARTED TO GO DOWN, THE AICRAFT WAS SHUTDOWN, AND MAINTENANCE FOUND PIN HOLE IN THE TUBE CAUSING LEAK. REPLACED TUBE ASSY. 1G72 3U H1NE 20060223001572006022300157 2006 2 23 PCSA12070502 420051207A3417HG480B100 ADC BOEING727 727212 138407GNM NR 1 FAILED A PCSACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 SO29598AJ 21947 FLIGHT 8216 DURING TAKEOFF FROM CUR CREW REPORTED CAPTAIN'S AIRSPEED INDICATION SHOWED NO AIRSPEED INDICATION, THE F/O'S AIRSPEED INDICATOR WAS SHOWING 80 KNOTS, CREW ABORTED THE TAKEOFF AND RETURNED TO THE BLOCK WITHOUT ANY FURTHER INCIDENT. MAINTENANCE TROUBLESHOT CAPTAIN'S AIRSPEED INDICATION SYSTEM AND FOUND THE NR 1 ADC AT FAULT, THE NR 1 AIR DATA COMPUTER WAS REMOVED AND REPLACED IAW BOEING 727 MM CH 34-12-11, SYSTEM WAS OPERATIONALLY CHECKED IAW AMERIJET WORK CARD 816 AND 817, OPERATIONALLY CHECKED NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L73 4F A3WE 20060223001812006022300181NM 2006 2 23 05FDEA04416 120051227A5531 STRINGER BOEING727 727227 1384078NM VERTICAL FIN CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 VERTICAL FIN TUNNEL STR 8RT CRACKED AT RIB 8. REPAIRED STRINGER PER SRM 55-30-4 FIG 1. 2L73 4F A3WE 20060223001842006022300184NM 2006 2 23 200520 120051224A26113023143 SMOKE DETECTOR DHAV DHC8 DHC8103 1386005NM AFT CARGO MALFUNCTIONED A KPVAO OTHER N FALSE WARNING CLCLIMB 1 WP13811WP 366 (PIREP) SMOKE WARNING ILLUMINATED 3 TIMES AFTER TAKEOFF. RETURN TO MKK. REMOVE AND REPLACED NR 1 SMOKE DETECTOR IAW DHC -8MM, 26-12-00 PG 201. PERFORMED OPS CHECK OF SMOKE DETECTOR SYSTEM. NO DEFECTS NOTED. ALSO, FOUND PASSENGER BAG WITH CELL PHONE ON IN BAGGAGE. 2H72 4T RTA13NM 20060223001882006022300188NM 2006 2 23 05FDEA04164 120051206A5310 DOOR FRAME DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 UPON REMOVAL OF LOOSE SEALANT AFT DOOR JAMB FORWARD CORNER FOUND CORRODED, SNRM N1260: AFT CARGO COMPARTMENT: AFT DOOR JAMB FORWARD CORNER, CORRODED AREA FOUND CRACKED. CARRIED OUT REPAIR AS PER FEDEX EA NR 1-5350-90711, TITLE: "FUSELAGE - AFT CARGO DOOR JAMB LOWER BEAM CORROSION AND CRACK, REPAIR". 2L73 4F RTA22WE 20060223001922006022300192SW 2006 2 23 HEEA107321 120051101A79313019630 TUBE BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE CHAFED B HEEAK NONE O OTHER NRNOT REPORTED 1 SW032148K 36001 NR 2 ENGINE OIL PRESSURE BEGAN TO FLUCTUATE AND SLOWLY DECREASED. WHEN GAUGE READING APPROACHED THE LOWER LIMIT THE MASTER CAUTION LIGHT BEGAN TO FLICKER. ENGINE WAS SHUTDOWN AND AIRCRAFT RETURNED TO BASE. MAINTENANCE FOUND A HOLE CHAFED IN THE OIL TO FUEL HEATER TUBE BY THE FUEL PUMP SEAL DRAIN TUBE. 1G72 4U4 U H4SW E22EA 20060223001932006022300193EU 2006 2 23 05FDEA04104 120051203A5101 REPAIR AIRBUS310 A310203 3930313EU T/E FLAP UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25424FE 241 COMPLY WITH AGING 9-AGING-INSP, PREVIOUS REPAIR INSTALLED AT LEFT HAND INBOARD FLAP (TRAILING EDGE WEDGE SECTION - COMPOSITE) AT WS 40 TO WS 50. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIRED IAW SRM 57-52-12 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR. 2L72 4F RTA35EU 20060223001942006022300194NE 2006 2 23 HEEA107361 120050317A3210EWS22741 BOLT SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL MLG FROZEN E HEEAO OTHER O OTHER CLCLIMB 1 SW03776P 760275 AFTER TAKEOFF, RETRACTED LANDING GEAR IAW CHECKLIST. GEAR RETRACTION NORMAL. ON DOWNWIND LEG HEARD A LOUD POP FROM AFT LT SIDE OF AIRCRAFT AND THEN RED UNLOCK LIGHT CAME ON. SLOWED AIRCRAFT TO BELOW 80 KIAS AND RECYCLED GEAR LEVER. GEAR CAME DOWN NORMAL WITH THREE GREEN LIGHTS. RETURNED TO DEPARTURE, LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND MAIN LANDING GEAR TIEDOWN RING ATTACHEMENT BOLT FROZEN, CAUSING TIEDOWN RING TO NOT BE FREE TO SPRING AND LAY AGAINST LANDING GEAR STRUT, CAUSING INTERFERENCE WITH LANDING GEAR DOOR DURING RETRACTION. REPLACED BOLT. 1G72 3U3 U H1NE E1GL 20060223001972006022300197SW 2006 2 23 HEEA107418 120051214A28249A1746 PUMP BELL 214 214ST 1182106SW GE CT7TS CT72A 30030NE NR 2 TRANSFER POPPED E HEEAO OTHER J WARNING INDICATION CRCRUISE 1 SW033897N 28106 DURING CRUISE FLIGHT, THE NR 2 TRANSFER LIGHT ILLUMINATED AND CIRCUIT BREAKER POPPED. FOLLOWED EMERGENCY PROCEDURE AND LANDED. MAINTENANCE REPLACED NR 2 TRANSFER PUMP. 2G72 4U4 U H10SW E8NE 20060223002422006022300242NM 2006 2 23 SPAA0500078 120051216A3350900835A BATTERY PACK BOEING737 7372Y5 1384554NM PWA JT8 JT8D15 52051NE CABIN DISCHARGED A SPAAK NONE L NO TEST ININSP/MAINT 1 WP28712S 23038 SCHEDULED MAINTENANCE VISIT, FWD DOOR AREA CEILING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK IAW B737MM 33-51-02. OPERATIONAL CHECK NORMAL. 2L72 4U4 FRTA16WE E2EA 20060223003102006022300310NM 2006 2 23 05FDEA04409 120051227A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 N01499 WHILE PREPPING FOR CLOSE FOUND INTERNAL FUSELAGE SKIN CORRODED AT BS 684 STR 26R. REPAIRED INTERNAL FUSELAGE SKIN AT BS 684 STR 26R IAW SRM 53-30-3. 2L73 4F RTA3WE 20060224000012006022400001CE 2006 2 24 DJFA2005183 120051228A32315EN16 SWITCH BEECH MU300 400A 1155402CE ZONE 700 FALSE INDICATIONE DJFAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA23408CW RK108 AFTER MLG RETRACTION, RED UNLOCK LIGHT REMAINED ILLUMINATED. PERFORMED A FLY-BY OF TOWER & ADVISED RT MLG DOOR DOWN. A/C LANDED W/O INCIDENT. RT MLG DOOR REMAINED DOWN. MX REPLACED RT MLG DOOR. DOOR & UPLOCK MECHANISM ADJUSTED. MLG EXTENSION & RETRACTION CHKS NORMAL & A/C RTS. RECEIVED A MLG UNSAFE LIGHT AFTER EXTENDING MLG. MLG CYCLED & RECEIVED SAME INDICATION. A/C DIVERTED & AN EMERG MLG DOOR RETRACTION PERFORMED. A NORMAL LANDING MADE & ON TOUCHDOWN MLG HANDLE LIGHT WENT OUT. MX REPLACED LT & RT MLG UPLOCK SWITCHES. RT DOOR ACT RIGGED, & A BENCH CHK PERFORMED ON PCB A-162, K-1 RELAY & SHUTTLE VALVE. DIODES OF HYD PACK WIRING CHKED. MLG OPS CHKS GOOD, & A SATIS CHK FLT PERFORMED. ACFT RTS. 2H72 4F RTA16SW 20060224000042006022400004EU 2006 2 24 HE17107526 120051230A6410C642A0300103 BLADE UROCOPEC120 EC120B 8680987EU TAIL ROTOR CHIPPED B HEEAK NONE O OTHER ININSP/MAINT 1 SW03524MW486 1371 TAIL ROTOR BLADE FAILED INSP. PER AMM 64-21-00,6-9 ZONE I 1G72 3U NCR0001RD 20060224000272006022400027EU 2006 2 24 05FDEA04100 120051203A5754 REPAIR AIRBUS310 A310 EU TE FLAP MISINSTALLED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25424FE 241 PREVIOUS REPAIR INSTALLED AT RIGHT HAND INBOARD FLAP (TRAILING EDGE WEDGE SECTION - LOWER SIDE - COMPOSITE) AT WS 67 TO WS 207. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. TRAILING EDGE WAS REPLACED IAW FEDEX E.A. 6-5710-94665 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR 2L72 4F RTA35EU 20060224000282006022400028EU 2006 2 24 05FDEA04101 120051203A5753 REPAIR AIRBUS310 A310 EU TE FLAP MISINSTALLED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25424FE 241 PREVIOUS REPAIR INSTALLED AT RIGHT HAND INBOARD FLAP (TRAILING EDGE WEDGE SECTION - LOWER SIDE - COMPOSITE) AT WS 40 TO WS 50. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. TRAILING EDGE WAS REPLACED PER FEDEX E.A. 6-5710-94665 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR 2L72 4F RTA35EU 20060224000292006022400029EU 2006 2 24 05FDEA04102 120051203A5753 REPAIR AIRBUS310 A310 EU TE FLAP MISINSTALLED A FDEAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 SO25424FE 241 PREVIOUS REPAIR INSTALLED AT RIGHT HAND INBOARD FLAP (TRAILING EDGE WEDGE SECTION - TOP SIDE - COMPOSITE) AT WS 60 TO WS 110. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. TRAILING EDGE WAS REPLACED IAW FEDEX E.A. 6-5710-94665 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR 2L72 4F RTA35EU 20060224001572006022400157WP 2006 2 24 IXXA05SMN281S 120051216A5330 SKIN DOUG DC8 DC872 302199BWP FUSELAGE DENTED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11722CX71621 46130 DURING ROUTINE C CHECK INSPECTION, EXTERNAL FUS.- LWR EXTERNAL SKIN DENTED, L-22L STA 364.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05582 DATE 12-23-05, SEMAN DWG NR ED 4116 DATE 12-20-05, EO SEMAN 20051439 DATE 12-23-05. REMOVED EXISTING REPAIR DOUBLER IAW DC-8 SRM 51-1-21, PERFORMED NDT INSPECTION IAW DC-8 NDT IAW DC-8 NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER (ALCLAD 7075 T6 0.080”) + (03 EA) INTERNAL FINGER DOUBLER (ALCLAD 7075 T6 0.032”) IAW SEMAN DWG # ED 4116. CLEANED, TREATED AND PRIMED AREA + REPAIR PARTS IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11. INSTALLED REPAIR PARTS IAW SEMAN DWG ED 4116, DC-8 SRM 51-1-12, DC-8 SRM 51-1-20D, DC-8 SRM 51-3-1.2L74 4F RT4A25 20060223001222006022300122EU 2006 2 23 HEEA107324 120050823A2120 SMOKE AEROSPAS355 AS355* EU COCKPIT DETECTED B HEEAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW03956AE 3352 PILOT REPORTED SMOKE IN COCKPIT AND BURNED ODOR. MADE PRECAUTIONARY LANDING AT WILEY FIRE STATION. 1G72 3U H11EU 20060223001272006022300127NE 2006 2 23 HEEA107333 220050614A7320292858560 HMU SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL1S1 60030NE ENGINE MALFUNCTIONED B HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03276X 760405 MASTER CAUTION 5-PACK ILLUMINATED. CHECKED CAUTION PANEL AND NR 2 LOW FUEL PRESSURE SEGMENT WAS DIMLY ILLUMINATED. MASTER CAUTION WOULD NOT RESET. SUSEQUENTLY NR 2 DECU DEGRADE LIGHT ILLUMINATED. CHECKED DDR FAULT. P3 DRIFT WAS THE DEGRADE. THEN FUEL PRESSURE GAUGE, N1 AND TORQUE BEGAN OSCILLATING MODERATELY. TRIED MANUAL TRAINING START SWITCH TO ISOLATE OSCILLATING ENGINE. NO EFFECT. WHEN PNF BEGAN RETARDING NR 2 ENGINE LEVER FROM THE FLY GATE, ENGINE FLAMED OUT. REPLACED HMU. 1G72 3U3 UNCH1NE E19EU 20060223001332006022300133SW 2006 2 23 HEEA107345 120050423A2910MS28775212 O-RING BELL 412 412 1182202SW NR 2 HYD SYSTEM LEAKING B HEEAO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 SW03412SM 33197 DURING PATIENT TRANSFER LOW HYDRAULIC PRESSURE WARNING LIGHT ILLUMINATED, SECURED NR 2 HYDRAULIC SWITCH AND LANDED AT NEAREST AIRPORT WITHOUT INCIDENT. MAINTENANCE FOUND ACCUMULATOR O-RING LEAKING. REPLACED O-RING. 1G72 4U H4SW 20060223001562006022300156EA 2006 2 23 REXA200500159 120051228A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA WING MALFUNCTIONED A REXAK NONE J WARNING INDICATION TXTAXI/GRND HDL 1 SO258914A 7914 FLAP FAILURE AT EIGHT DEGREES ON TAXI. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD 98-20-01. 2L72 4F RTA21EA 20060223001822006022300182NM 2006 2 23 05FDEA04417 120051227A5740 FITTING BOEING727 727227 1384078NM LT WING GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 AFTER REMOVAL OF L/W 870 TERMINAL PIN, DISCOVERED A GOUGE INSIDE THE TERMINAL PIN FITTING BORE, AT APPROXIMATELY THE ONE O'CLOCK POSITION NEXT TO THE TERMINAL PIN RETAINING NUT. REPAIRED L/W TERMINAL PIN FITTING BORE AT 87 PER FED EX EA 7-5310-91432. 2L73 4F A3WE 20060223001832006022300183EU 2006 2 23 NACA20050034 120051231A274148635018011 INDICATOR AEROSPATR42 ATR42300 8680920EU TRIM INTERMITTENT A NACAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 AL0342NC 067 TAKEOFF ABORTED DUE TO FLICKERING TAKEOFF CONFIGURATION AT 1 DEGREE DOWN TRIM. REPLACED TRIM POSITION INDICATOR. OP CHECKED GOOD. REF: JIC 27-15-81-RAI-10000. 2H72 4T RTA53EU 20060223001872006022300187NM 2006 2 23 05FDEA04350 120051216A5311 FRAME DOUG MD11 MD11 3023602NM BS 1305 CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25575FE 48500 DURING AIRPLANE'S CONVERSION FROM P TO F: A CRACK 2.2" LONG HAS BEEN FOUND ON FRAME AT THE STA Y=1305 LT BETWEEN L=11 AND L=12. PERFORMED REPAIR IN ACCORDANCE WITH FEDEX EA N 1-5310-93785. 2L73 4F RTA22WE 20060223001892006022300189NM 2006 2 23 05FDEA04165 120051207A5313AFA77761 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 CENTER CARGO COMPARTMENT STATION 1571 LONGERON 48 RIGHT HAND FOUND CORRODED AROUND FASTENER AREA. CORROSION REMOVED AT CENTER CARGO COMPARTMENT STATION 1571 LONGERON 48 RIGHT FOUND EXCEEDED LIMIT AS PER SRM 53-00-01 FIGURE 3 VOLUME I. ORIGINAL THICKNESS=0.100", REMAINING THICKNESS=0.062", MATERIAL REMOVED=0.038". REFER TO SNRM N1269 FOR LONGERON 48R REPLACEMENT FROM STATION 5-123 TO STATION 1588. 2L73 4F RTA22WE 20060223002512006022300251NM 2006 2 23 SPAA0500080 120051215A523065479531 DOOR FRAME BOEING737 7372T4 1384492NM CARGO DOOR CRACKED A SPAAK NONE O OTHER ININSP/MAINT 1 WP28703S 22529 AFT LOWER CARGO DOOR HAS CRACKS ON THE FWD AND AFT CORNER FRAMES & THE LOWER BEAM FWD END. REPAIRED CRACKS ON AFT CARGO DOOR FWD AND AFT CORNERS AND LWR BEAM FORWARD END IAW BOEING SERVICE BULLETIN 737-52A-1079. 2L72 4F A16WE 20060223003072006022300307NM 2006 2 23 05FDEA04410 120051227A5320 STRAP BOEING727 727100 1384036NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 N00312 CORROSION ON REINFORCEMENT STRAP AT UPPER FLANGE OF FLOORBEAM BS 1130 LBL. 63, WL 208. REMOVED AND REPLACED REINFORCEMENT STRAP AT UPPER FLANGE OF FLOORBEAM BS 1130, LBL 63, WL 208, IAW SRM 51-30-5, 51-30-2. 2L73 4F RTA3WE 20060224000032006022400003NE 2006 2 24 DJFA2005168 220051128A7200JT15D5 ENGINE BEECH MU300 400A 1155402CE PWA JT15 JT15D5 52112NE RIGHT POWER LOSS E DJFAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION DEDESCENT 1 EA23691TA4015 1719 RK317 PCEJA0407 EN ROUTE, SHORTLY AFTER POWER WAS REDUCED TO BEGIN DESCENT FROM CRUISE ALTITUDE, BOTH ENGINES EXPERIENCED A SUSTAINED POWER LOSS. UNABLE TO RESTART EITHER ENGINE IN FLT. EMERGENCY DECLARED & ACFT DIVERTED. UNDER NTSB INVESTIGATION. MX REPLACED AIRFRAME & ENGINE FUEL FILTERS. CHECKS PERFORMED ON IGNITION ANTI-ICE, FUEL TEMP, AIRFRAME FUEL FILTER BY-PASS INDICATION SYS, NO DISCREPANCIES. LT & RT ENG P-3 BOSSES INSP FOR WORN GASKETS. NO LEAK OR DAMAGE. ENG OIL SOAP SAMPLES & FUEL SAMPLES TAKEN. RT ENG REPLACED, 5 PT ENG RUNS PERFORMED ON LT & RT POWERPLANTS. REMOVED ENG WILL BE TORN DOWN BY MANUF AS PART OF NTSB INVESTIGATION. THREE GROUND POWER RUNS WERE COMPLETED, NO NOTED PROBLEMS. 2H72 4F4 FRTA16SW E25EA 20060224001772006022400177WP 2006 2 24 IXXA05SMN296S 120051229A5753 VANE DOUG DC8 DC872 302199BWP TE FLAP DAMAGED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11722CX71621 46130 C-CHECK INSPECTION, LT WING INBD FLAP VANE HOLES ELONGATED, XILD 42. PERFORMED MAJOR REPAIR. REMOVED FASTENERS, REMOVED DAMAGED SECTION. PERFORMED NDT INSPECTION. FABRICATED REPAIR DOUBLER (AL7075T60.070) & FILLER (AL7075T60.063) & INTERNAL DOUBLER (AL7075T60.063). CLEANED, TREATED; PRIMED AREA & REPAIR PARTS INNER SIDE. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW SEMAN DWG ED-4120, DC8 SRM 51-1-20D, DC8 SRM 51-3-0, DC8 SRM 51-3-1 (TORQUE). 2L74 4F RT4A25 20060224002182006022400218WP 2006 2 24 IXXA05SMN285S 120051229A5753 REPAIR DOUG DC8 DC872 302199BWP T/E FLAP IMPROPER B IXXAK NONE O OTHER ININSP/MAINT 1 SW11722CX71621 46130 DURING INSP, RT INBD FLAP FWD UPPER SURFACE HAS NO STANDARD REPAIR (STA XW 37.000-48.000). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05580 DATE 12-21-05, SEMAN DWG NR ED 4129 DATE 12-20-05, EO SEMAN 20051444 DATE 12-21-05. REMOVED REPAIR IAW DC-8 SRM 51-1-21, DC-8 SRM 51-1-20D. TRIMMED OUT DAMAGED AREA IAW SEMN DWG ED-4129. PERFORMED NDT INSP IAW DC-8 NDT IAW DC-8 NDT SPM PART 06-10-01-001. FAB PLATING SEGMENT (02 EA) INTERNAL SPLICE (02 EA) INTERNAL SHIMS & REPAIR DOUBLERS (04 EA) IAW SEMAN DWG ED 4129. CLEANED, TREATED AND PRIMED AREA & REPAIR PARTS IAW DC-8 SRM 51-1-8B. SEALED FAYING SURFACES IAW DC-8 SRM 51-1-11. INSTALLED REPAIR PARTS IAW SEMAN DWG ED 4129, DC-8 SRM 51-1-12, DC-8 SRM 51-1-20D, D2L74 4F RT4A25 20060224002272006022400227SO 2006 2 24 F05002 120050916A2530 ODOR EMB 145 EMB145LR 3260212SO GALLEY DETECTED A FDKAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW07825MJ 145179 THE CREW REPORTED A SMOKE LIKE SMELL IN GALLEY DURING FLIGHT. MAINTENANCE PERFORMED A GVI TO GALLEY AREA AND WIRING. MAINTENANCE CHANGED TRASH OUT AND CLEANED COFFEE POTS. NO SMOKE SMELL DETECTED. 2L72 4T RTT00011AT 20060224002302006022400230SO 2006 2 24 F05006 120050920A2622466090 SEAL EMB 145 EMB145LR 3260212SO FIRE BOTTLE MISSING A FDKAK NONE O OTHER NRNOT REPORTED 1 SW07825MJ9755 145179 THE CREW REPORTED FWD CABIN FIRE EXTINGUISHER SEAL MISSING. MAINTENANCE REPLACED THE FIRE EXTINGUISHER. 2L72 4T RTT00011AT 20060224002312006022400231SO 2006 2 24 F05007 120051023A7830 WARNING SYSTEM EMB 145 EMB145LR 3260212SO COCKPIT MALFUNCTIONED A FDKAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SW07826MJ 145214 CREW ABORTED, THE TAKEOFF AND RETURNED TO THE GATE. CREW REPORTED AN E1 REVERSER DISAGREE MESSAGE. CONTRACT MAINTENANCE INSPECTED THE REVERSER AND PERFORMED OPERATIONAL CHECKS WITH THE CREW. NO DEFECTS NOTED. 2L72 4T RTT00011AT 20060224002322006022400232SO 2006 2 24 F05010 120051109A783083990168 SWITCH EMB 145 EMB145LR 3260212SO THRUST REVERSER FAULTY A FDKAO OTHER N FALSE WARNING TOTAKEOFF 1 SW07826MJ 145214 THE CREW ABORTED TAKEOFF DUE TO A NR 1 ENGINE THRUST REVERSER DISAGREE. CONTRACT MAINTENANCE REMOVED AND REPLACED THE LOWER LT TRANSIT SWITCH. 2L72 4T RTT00011AT 20060224002332006022400233SO 2006 2 24 F05011 120051112A4920 APU EMB 145 EMB145LR 3260212SO APU BAY CONTAMINATED A FDKAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW07829MJ 145228 THE CREW NOTED SMOKE IN THE CABIN AFTER APU START UP ON THE GROUND DURING PREFLIGHT INSPECTION. MAINTENANCE INSPECTED THE PLANE AND DETERMINED THAT THE APU WAS NOT RUNNING DURING DE-ICING AND INGESTED THE STRAY FLUID CAUSING THE SMOKE AND ODOR. 2L72 4T RTT00011AT 20060224002342006022400234SO 2006 2 24 F05014 120051218A2120C1431236 DUAL VALVE EMB 145 EMB145LR 3260212SO A/C BAY FAILED A FDKAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW07829MJ605 145228 THE CREW NOTED SMOKE IN CABIN COMING FROM THE NR 2 PACK. MAINTENANCE REMOVED AND REPLACED THE DUAL VALVE. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20060227000552006022700055WP 2006 2 27 IXXA060078S 120051003A5320 WEB DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE ZONE 200 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND EXTERNAL FUSELAGE FORWARD BULKHEAD UPPER WEB CRACKED AT STATION -165 BETWEEN +X17 AND +Z23. REMOVED DAMAGED AREA. FABRICATED DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED DOUBLER, AND FASTENERS AT STATION -165 FROM +X17 TO +Z23. IAW SRM 53-2-0, 51-1-21, 51-1-5, AND 51-1-8. 2L74 4F4 FRT4A25 E2GL 20060227000562006022700056WP 2006 2 27 IXXA05SMN272S 120051215A5753 SKIN DOUG DC8 DC872 302199BWP LT TE FLAP DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11722CX71621 46130 DURING INSPECT, LT OB FLAP UPPER SURFACE HAS NO STANDARD REPAIR, STA XF 347.000. PERFORMED MAJOR REPAIR, DWG NR ED 4118 DATE 12-20-05, EO 20051446 DATE 12-21-05. REMOVED NON STANDARD REPAIR IAW SRM 51-1-21. REMOVED DAMAGED SEGMENT IAW DWG ED-4118. PERFORMED NDT INSPECT IAW NDT IAW NDT SPM PART 06-10-01-001. FABD NEW REPAIR PLATING SEGMENT (ALCLAD 2024 T3 0.063) + INTERNAL SPLICE (ALCLAD 2024 T3 0.071”) + (02 EA) REPAIR DOUBLERS (ALCLAD 2024 T3 0.071”) IAW DWG ED 4118. CLEANED, TREATED AND PRIMED AREA + REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PAGE 9. INSTALLED REPAIR PARTS IAW DWG ED 4118, SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2L74 4F RT4A25 20060227000712006022700071NM 2006 2 27 PCSA12150501 120051215A2131 OUTFLOW VALVE BOEING727 727233 138408ANM PWA JT8 JT8D15 52051NE RT A/C PACK STUCK A PCSAJA DUMP FUEL UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO29495AJ 20937 FLIGHT 731 AFTER DEPARTURE, DURING CLIMB THRU 6000 FT. CREW REPORTED CABIN PRESSURIZATION STARTED CLIMBING AT AN EXCESSIVE RATE AND COULD NOT MAINTAIN CABIN PRESSURIZATION. THE CREW REPORTED THE OUTFLOW VALVE WAS FULLY CLOSED, IT APPEARED THAT THE RT PACK WAS CLOSED. THE CREW DUMPED FUEL AND RETURNED TO DEPARTURE WITHOUT ANY FURTHER INCIDENT. MAINTENANCE FOUND THE RT PACK VALVE CLOSED AND NOT OPENING, THE RT PACK VALVE WAS REMOVED AND REPLACED IAW MM CH 21-55-71, THE SYSTEM WAS OPERATIONALLY CHECKED AND FOUND NORMAL AND A DECAY CHECK WAS FOUND NORMAL IAW MM CH 5-51-101. 2L73 4F4 FRTA3WE E2EA 20060223002342006022300234CE 2006 2 23 DJFA2006190 120051221A783022500231 SWITCH BEECH MU300 400A 1155402CE THRUST REVERSER WORN E DJFAA UNSCHED LANDING N FALSE WARNING DEDESCENT 1 EA23445CW RK45 ON DESCENT, NR 1 THRUST REVERSER UNLOCK LIGHT ILLUMINATED. THRUST REVERSER EMERGENCY STOW BUTTON WAS PUSHED, DIVERTED. ACFT WANTED TO ROLL LEFT. UNSURE IF ROLL WAS RELATED TO THRUST REVERSER ISSUE, DECLARED AN EMERGENCY. YAW DAMPER WAS THEN DISENGAGED. DURING APPROACH ROLL TENDENCY DISAPPEARED. MX PERFORMED AUTO-PILOT & FLT MANAGEMENT SYS BITE TESTS, WITH NO NOTED DISCREPANCIES. NR 1 & 2 FLT CONTROL COMPUTER CARD POSITIONS SWAPPED. OPS CHECK OF AUTO-PILOT SYS PERFORMED. PRINTED C/B A185 REPLACED AFTER BEING SWAPPED FROM POSITION A186 WHILE T/S THRUST REVERSER SYS. INBOARD THRUST REVERSER STOW LIMIT SWITCH REPLACED AFTER FAILED TEST. NO DEFECTS NOTED IN THRUST REVERSER SYS AFTER OPS CHK PERFORMED. 2H72 4F RTA16SW 20060223002522006022300252NM 2006 2 23 RYNA200500031 120051231A2781697437015 TARGET BOEING737 7374Y0 1384705NM NR 1 SLAT OUT OF POSITION A RYNAB EMER. DESCENT N FALSE WARNING LDLANDING 1 CE07251RY 25180 DURING LANDING, NR 1 SLAT INDICATED NOT FULLY EXTENDED. FOUND SLAT NR 1 PROXIMITY SWITCH TARGET OUT OF POSITION. ADJUSTED PROXIMITY SWITCH/TARGET CLEARANCE. OPERATIONAL CHECK NORMAL. 2L72 4F RTA16WE 20060223002752006022300275EA 2006 2 23 COMA0660155 120050217A2752857SD100101 DRIVE SHAFT CNDAIRCL600 CL6002B19 1900309EA T/E FLAP WORN A COMAK NONE J WARNING INDICATION APAPPROACH 1 SO01967CA 7134 FLIGHT 5373- DURING JFK APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE AT 42 DEGREES. REPLACED THE LEFT WING NR 1 FLEX DRIVE SHAFT. 2L72 4F RTA21EA 20060223003112006022300311NM 2006 2 23 05FDEA04411 120051227A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 N00235 GRAVEL DAMAGE BS 620-720 STR 25L -20R. REMOVED GRAVEL DAMAGE BS 620-720 STR 25L-20R COMMON TO SKIN WITHIN LIMITS PER SRM 53-30-1 DETAIL 1 AND FIG 2. 2L73 4F RTA3WE 20060224000252006022400025EU 2006 2 24 05FDEA04097 120051203A5101 REPAIR AIRBUS310 A310 EU FUSELAGE NONE A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25424FE 241 PREVIOUS REPAIR INSTALLED AT FUSELAGE LEFT HAND SIDE, BELOW REGISTRATION NR N424FE AT STA 4181 TO STA 4241, FR77 TO FR78, STR 23 LT TO STR 24 LT. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND TO CONFORM SRM 53-10-12 FIG.224 SHEET 1 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR 2L72 4F RTA35EU 20060224001662006022400166WP 2006 2 24 IXXA05SMN298S 120051229A5730 SKIN DOUG DC8 DC872 302199BWP LT WING CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11722CX71621 46130 DURING INSPECT, LT WING CTR L/E EXT LWR SKIN CORRODED, XFS 304.000. PERFORMED REPAIR IAW FAA FORM 8110-3 NR 05586 DATE 12-28-05, SEMAN DWG NR ED 4123 DATE 12-27-05 AND EO SEMAN NR 20051454 DATE 12-28-05. REMOVED FASTENERS IAW DC-8 SRM 51-1-21 AND DC-8 SRM 51-3-0. REMOVED CORROSION IAW DC-8 RM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW DC-8 SRM 57-2-1 FIG. 2G. REMOVED CORRODED AREA IAW SEMAN DWG ED-4123. PERFORMED NDT INSPECT IAW DC-8 NDT IAW DC-8 NDT SPM PART 06-10-01-001. FAB`D REPAIR DOUBLER (ALCLAD 7075 T6 0.071”) + FILLER (ALCLAD 7075 T6 0.063) IAW SEMAN DWG # ED 4123. CLEANED, TREATED AND PRIMED AREA & REPAIR PARTS INTERNAL PART IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-12L74 4F RT4A25 20060224002202006022400220WP 2006 2 24 IXXA05SMN302S 120051229A5730 SKIN DOUG DC8 DC872 302199BWP LT WING CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11722CX71621 46130 DURING INSPECT, LT WING CTR L/E CORRODED, XFS 422.750. PERFORMED REPAIR IAW FAA FORM 8110-3 # 05587 DATE 12-29-05, SEMAN DWG # ED 4127 DATE 12-28-05 AND EO SEMAN # 20051458 DATE 12-29-05. REMOVED FASTENERS IAW DC-8 SRM 51-1-21. REMOVED CORROSION IAW DC-8 SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW DC-8 SRM 57-2-1 FIG. 2G. REMOVED CORRODED AREA IAW SEMAN DWG ED 4127. PERFORMED NDT INSPECTION IAW DC-8 NDT IAW DC-8 NDT SPM PART 06-10-01-001. FAB`D REPAIR DOUBLER AND FILLER IAW SEMAN DWG # ED 4127. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS INTERNAL PART IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11. INSTALLED REPAIR PARTS IAW SEMAN DWG ED 4127, DC-8 SRM 51-1-21, DC-8 SRM2L74 4F RT4A25 20060227002372006022700237NM 2006 2 27 UPS06M46268 120051215A5754 SKIN DOUG MD11 MD11F 3023600NM L/E SLAT DENTED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01282UP 48452 INSPECTION TYPE:C LEFT WING INBOARD NR 1 SLAT HAS DENT AS MARKED. LEFT WING INBOARD NR 1 SLAT DENT (QTY/01/EA) EVALUATED FOUND EXCEEDED PER SRM LIMIT. HFEC CUTOUT FOUND NO EVIDENT OF CRACK. DENT AREA FASTENERS REMOVED AS PER SRM 51-35-01V.2.R.38. DENT AREA SKIN TRIMMED PER SRM 57-10-00.F33. V.1.R.38. REPAIR ANGLE FAB USING MAT 7075-0-0.050 PER SRM 57-10-00 FIG 33 SHT 2. REPAIR ACCOMPLISHED AT NR 1 SLAT LEFT WING PER EN1041-06, FOUND SATISFACTORY. 2L73 4F RTA22WE 20060227002382006022700238NM 2006 2 27 UPS06M46269 120051221A5514 STRUCTURE DOUG MD11 MD11F 3023600NM HORIZ STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01282UP 48452 INSPECTION TYPE:C EMPENNAGE - BARREL NUT HOLE NR 08 LT FOUND BEARING WITH SURFACE CORROSION ON SIDE & BOTTOM AREA. CORROSION REMOVAL CUTOUT & FOUND BLENDED OUT BEYOND ALLOWABLE LIMIT. B/N BORE & BOTTOM REWORKED PER EN 1643-05. FAB SLEEVE BUSHING PER EO MD 11-5510-19409-K, FIG 5. APPLIED SEALANT PR1422B 1/2 BLEND OUT AREA & S/BUSHING PER EO MD11-5510-19409-K. REPAIR ACCOMPLISHED AT B/N HOLE NR 08 LT PER EO MD11-5510-19409-K & EN 1643-05, FOUND SATISFACTORY. 2L73 4F RTA22WE 20060224000302006022400030EU 2006 2 24 05FDEA04103 120051203A5753 REPAIR AIRBUS310 A310 EU TE FLAP MISINSTALLED A FDEAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 SO25424FE 241 PREVIOUS REPAIR INSTALLED AT RIGHT HAND INBOARD FLAP (TRAILING EDGE WEDGE SECTION - TOP SIDE - COMPOSITE) AT WS 115 TO WS 200. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. TRAILING EDGE WAS REPLACED IAW FEDEX E.A. 6-5710-94665 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR 2L72 4F RTA35EU 20060224001682006022400168WP 2006 2 24 IXXA05SMN300S 120051229A5730 SKIN DOUG DC8 DC872 302199BWP LT WING CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11722CX71621 46130 DURING INSPECT, LT WING CTR L/E LWR PART SKIN CORRODED, XFS 341.000. PERFORMED REPAIR IAW FAA FORM 8110-3 NR 05586 DATE 12-28-05, SEMAN DWG NR ED 4124 DATE 12-22-05, EO SEMAN NR 20051455 DATE 12-28-05. REMOVED FASTENERS IAW DC-8 SRM 51-1-21, DC-8 SRM 51-3-0. REMOVED CORROSION IAW DC-8 SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW DC-8 SRM 57-2-1 FIG 2G. REMOVED CORRODED AREA IAW SEMAN DWG ED 4124. PERFORMED NDT INSPECT IAW DC-8 NDT IAW DC-8 NDT SPM PART 06-10-01-001. FAB`D REPAIR DOUBLER (ALCLAD 7075 T6 0.071”) + FILLER (ALCLAD 7075 T6 0.063) IAW SEMAN DWG NR ED 4124. CLEANED, TREATED AND PRIMED AREA + REPAIR PARTS INTERNAL PART IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11. I2L74 4F RT4A25 20060224001752006022400175WP 2006 2 24 IXXA05SMN282S 120051216A5330 SKIN DOUG DC8 DC872 302199BWP BS 403 DENTED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11722CX71621 46130 C-CHECK INSPECTION, EXTERNAL FUS LWR EXTERNAL SKIN DENTED BETWEEN L-23 & L-24L STA 403. PERFORMED MAJOR REPAIR. REMOVED FASTENERS, DAMAGED FRAME SEGMENT. FABRICATED NEW FRAME SEGMENT, (02 EA) ANGLES. HEAT TREATED FRAME SEGMENT & ANGLES. CLEANED, TREATED AND PRIMED AREA & REPAIR PARTS IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11 PAGE 9. INSTALLED REPAIR PARTS IAW DC-8 SRM 53-2-0 FIG 2 (SHEET 5, 6), DC-8 SRM 51-1-20D, DC-8 SRM 51-3-1 (TORQUE). 2L74 4F RT4A25 20060224002192006022400219WP 2006 2 24 IXXA05SMN301S 120051229A5730 SKIN DOUG DC8 DC872 302199BWP LT WING CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11722CX71621 46130 DURING INSPECT, LT WING OTBD L/E HAS NON STANDARD REPAIR, XW 485.000. PERFORMED REPAIR IAW FAA FORM 8110-3 # 05582 DATE 12-23-05, SEMAN DWG # ED 4125 DATE 12-22-05 AND EO SEMAN # 20051456 DATE 12-23-05. REMOVED NON STANDARD REPAIR IAW DC-8 SRM 51-1-21, DC-8 SRM 51-3-0. REMOVED DAMAGED AREA IAW SEMAN DWG ED-4125. PERFORMED NDT INSPECT IAW DC-8 NDT IAW DC-8 NDT SPM PART 06-10-01-001. FAB`D REPAIR DOUBLER AND FILLER IAW SEMAN DWG # ED 4125. CLEANED, TREATED AND PRIMED AREA + REPAIR PARTS INTERNAL PART IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11. INSTALLED REPAIR PARTS IAW SEMAN DWG ED 4125, DC-8 SRM 51-1-21, DC-8 SRM 51-3-0, DC-8 SRM 51-1-20D AND DC-8 SRM 51-3-1. 2L74 4F RT4A25 20060227001122006022700112NM 2006 2 27 USAA05001 120050418A5330 SKIN BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19448US 24892 A 1.5 INCH CRACK AT LBS 727D + 2 INCHES; S23L (BELOW EMERGENCY EGRESS LIGHT). INSTALLED DOUBLER PER SRM 53-00-01 FIG 231. 2L72 4F RTA16WE 20060227002032006022700203WP 2006 2 27 FRISBY06001 120050826A292041022021 HOUSING DOUG DC9 DC982 3022082WP DRAIN PORT CRACKED B UFHRO OTHER J WARNING INDICATION LDLANDING 1 SO05 7330 1372 B28037 DURING LANDING, PILOT REPORTED L/R THRUST REVERSER ACCUMULATOR "LOW" LIGHT CAME ON, THRUST REVERSER DEPLOYMENT, AND BOTH HYD PRESS INDICATED "0", WHILE HYD QTY WAS NORMAL AT L 15 AND R 17. PILOT PROCEEDED TO ACCOMP QRH HYD PRESS LOW PROCEDURE BY TURNING TRANSFER PUMP SWITCH "OFF", AND HYD SYS PRESS`S RETURNED TO NORMAL. A/C THEN PROCEEDED TO TAXI TO GATE. INSPECTION BY MX REVEALED PTU, P/N 4100310-6, S/N 1372 WAS LEAKING SO IT WAS REPLACED. AFTER REMOVAL, MX PERSONNEL FOUND DRAIN PORT HOUSING, P/N 4102202-1, INSTALLED ON SUBJECT PTU, HAD CRACKED COMPLETELY AROUND CIRCUMFERENCE. PTU WAS REPORTED TO HAVE 7,330 TSN AND 10,082 CSN, AND IT WAS RETURNED REPAIR STATION FOR INVESTIGATION. 2L72 4F A6WE 20060227002592006022700259NM 2006 2 27 05FDEA04419 120051227A5315 FLOORBEAM BOEING727 727227 1384078NM BS 1130 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 FOUND CORROSION IB FLOORBEAM LOWER FLANGE BS 1130 LBL 44-RBL 44 WL 201. REPAIRED FLOORBEAM LOWER CHORD BS 12130 RBL 44 TO LBL 44 IAW SRM 51-10-2. 2L73 4F A3WE 20060224001762006022400176WP 2006 2 24 IXXA05SMN287S 120051229A5330 SKIN DOUG DC8 DC872 302199BWP BS 480 CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11722CX 46130 C-CHECK INSPECTION, EXTERNAL FUS LWR EXTERNAL SKIN CORRODED BETWEEN L33 AND L35R, STA 480.000 STATION 500. PERFORMED MAJOR REPAIR. REMOVED FASTENERS, REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SECTION. PERFORMED NDT INSPECTION. FABRICATED REPAIR DOUBLER (ALCLAD 7075 T6 0.071) & REPAIR TRIPLER (ALCLAD 7075 T6 0.090) & FILLER SKIN (ALCLAD 7075 T6 0.063) & FILLER INTERNAL DOUBLER (ALCLAD 7075 T6 0.071). CLEANED, TREATED AND PRIMED AREA & REPAIR PARTS IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11. INSTALLED REPAIR PARTS IAW SEMAN DWG ED 4117, DC-8 SRM 51-1-20D, DC-8 SRM 51-3-1 (TORQUE). 2L74 4F RT4A25 20060224002112006022400211NM 2006 2 24 05FDEA04418 120051227A5531 STRINGER BOEING727 727227 1384078NM VERTICAL STAB CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 VERTICAL FIN TUNNEL STR 8 RT CRACKED AT RIB 7. REPAIRED VERTICAL FIN TUNNEL STR 8 RT AT RIB 7 IAW SRM 55-30-4 FIG 1. 2L73 4F A3WE 20060224002172006022400217WP 2006 2 24 IXXA05SMN295S 120051229A5753 VANE DOUG DC8 DC872 302199BWP T/E FLAP DAMAGED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11722CX71621 46130 DURING INSPECT, LT WING OUTBD VANE FWD HOLES ELONGATED, XOLDO 66.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05586 DATE 12-28-05, SEMAN DWG NR ED 4121 DATE 12-23-05 AND EO SEMAN NR 20051452 DATE 12-28-05. REMOVED FASTENERS IAW DC-8 SRM 51-1-21. REMOVED AREA IAW SEMAN DWG ED-4121. PERFORMED NDT INSPECT IAW DC-8 NDT IAW DC-8 NDT SPM PART 06-10-01-001. FAB`D REPAIR DOUBLER (ALCLAD 7075 T6 0.071) + FILLER (ALCLAD 7075 T6 0.063”) + INTERNAL DOUBLER (ALCLAD 7075 T6 0.063”) IAW SEMAN DWG NR ED 4121. CLEANED, TREATED AND PRIMED AREA + REPAIR PARTS INTERNAL PART IAW DC-8 SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SEMAN DWG ED 4121, DC-8 SRM 51-1-21, DC-8 SRM 51-3-0, DC-8 SRM 51-1-20D AND DC-8 SRM 51-3-1 (TQ). 2L74 4F RT4A25 20060224002282006022400228SO 2006 2 24 F05004 120050919A2560 ESCAPE ROPE EMB 145 EMB145LR 3260212SO COCKPIT UNSECURE A FDKAK NONE O OTHER NRNOT REPORTED 1 SW07825MJ 145179 THE CREW HAD A F/O EMERGENCY ESCAPE ROPE THAT WAS NOT SECURE IN ITS CONTAINER. MAINTENANCE SECURED ESCAPE ROPE. 2L72 4T RTT00011AT 20060224002292006022400229SO 2006 2 24 F05005 120050919A49304951545 PUMP EMB 145 EMB145LR 3260212SO APU LEAKING A FDKAO OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW07825MJ512 145179 THE CREW NOTED A STRONG ODOR OF FUEL IN THE CABIN. MAINTENANCE HAS TROUBLESHOT FAULT TO LEAKING PACKINGS AT THE APU ACCELERATION UNIT. MAINTENANCE REMOVED AND REPLACED APU FUEL PUMP. 2L72 4T RTT00011AT 20060227000802006022700080EU 2006 2 27 HEEA107879 120051121A6210355A11003000 BLADE AEROSPAS355 AS355* EU MAIN ROTOR DEBONDED B HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03975AE1452 2777 UNBONDED ABOVE TRIM TAB AREA IN TWO PLACES. 1G72 3U H11EU 20060227000872006022700087SW 2006 2 27 ALGA107653 120050917A6320206040032105 BEARING BELL 206 206L1 1182107SW TRANSMISSION SPALLED B ALGAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW033188P BMC00497 45778 TRANSMISSION ASSY HAD METAL IN OIL, DISASSEMBLED AND FOUND DUPLEX BEARING BREAKING DOWN. REMOVED AND REPLACED DUPLEX BEARING PN:206-040-032-105. 1G71 3U H2SW 20060227000892006022700089SW 2006 2 27 HEEA107687 120051227A5630205032669233 WINDOW BELL 412 412 1182202SW CARGO DOOR DEPARTED B HEEAO OTHER D INFLIGHT SEPARATION DEDESCENT 1 SW03800Y 33134 DURING DESCENT, THE FORWARD WINDOW IN THE RIGHT HAND CARGO DOOR DEPARTED THE AIRCRAFT. NO DAMAGE TO THE AIRCRAFT. MAINTENANCE REPLACED THE WINDOW. 1G72 4U H4SW 20060227000902006022700090EU 2006 2 27 HEEA107688 120051222A2400EO535W5100UJ RESISTOR SNIAS 350 AS350B3 8680954EU UNKNOWN BURNED B HEEAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW03351LG 3722 DURING FLIGHT, AN ELECTRICAL BURNING SMELL WAS NOTED IN THE COCKPIT AND THE CABIN. MAINTENANCE REPLACED RESISTOR. 1G71 3U H9EU 20060227000922006022700092EU 2006 2 27 ALGA107785 120051114A6200 UNKNOWN UROCOPEC120 EC120B 8680987EU MAIN ROTOR WORN B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03516AL470 1157 WORN BEYOND LIMITS IN DROOP AREA. REPLACED UNIT WITH NEW SERVICEABLE PART. 1G72 3U NCR0001RD 20060228001052006022800105WP 2006 2 28 IXXA05SMN280S 120051216A5330 SKIN DOUG DC8 DC872 302199BWP BS 356 DENTED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11722CX71621 46130 DURING ROUTINE C-CHECK INSPECTION, EXTERNAL FUS LWR EXTERNAL SKIN DENTED L-232, STA 356.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 05582 DATE 12-23-05, SEMAN DWG ED 4116 DATE 12-20-05, EO SEMAN 20051439 DATE 12-23-05. FABRICATED REPAIR DOUBLER & (03 EA) INTERNAL FINGER DOUBLER IAW SEMAN DWG ED 4116 ORIGINAL DOCUMENT CERT. 2L74 4F RT4A25 20060228001062006022800106WP 2006 2 28 IXXA05SMN290S 120051229A5340 FITTING DOUG DC8 DC872 302199BWP BS 270 CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11722CX71621 46130 DURING ROUTINE C-CHECK INSPECTION, FWD ACCY COMPT INTERNAL PART FITTING CORRODED AT STA 270.000, L-34 (RT). REMOVED CORROSION FROM FITTING IAW DC-8 SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW DC-8 SRM 53-2-0 PAGE 2P. REMOVED CRACKED FITTING IAW DC-8 SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8B. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-21, DC-8 SRM 51-1-20D, DC-8 SRM 51-3-1 (TORQUE). 2L74 4F RT4A25 20060228001072006022800107WP 2006 2 28 IXXA05SMN310S 120051229A7830 FITTING DOUG DC8 DC872 302199BWP ZONE 600 CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11722CX71621 46130 DURING ROUTINE C-CHECK INSPECTION, NR 4 ENGINE RIGHT T/R RAIL FITTING CORRODED AT 12 O`CLOCK POSITION (THRUST REVERSER). REMOVED LEVEL I CORROSION FROM RAIL FITTING IAW DC-8 SRM 51-1-8 PAGES 17-18 (MATERIAL THICKNESS: 0.133, BLEND OUT: 0.003, REMAINING THICKNESS: 0.130) FOUND WITHIN ALLOWABLE LIMITS IAW CFM MM 78-31-20 PAGES 609-610. CLEANED, TREATED AND PRIMED IAW DC-8 SRM 51-1-8B. 2L74 4F RT4A25 20060228001082006022800108WP 2006 2 28 IXXA05SMN311S 120051229A7830 FITTING DOUG DC8 DC872 302199BWP ZONE 600 CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11722CX71621 46130 DURING ROUTINE C-CHECK INSPECTION, NR 4 ENGINE - LEFT T/R RAIL FITTING CORRODED AT 12 O`CLOCK POSITION (THRUST REVERSER). REMOVED LEVEL I CORROSION FROM RAIL FITTING IAW DC-8 SRM 51-1-8 PAGES 17-18 (MATERIAL THICKNESS: 0.133, BLEND OUT: 0.003, REMAINING THICKNESS: 0.130) FOUND WITHIN ALLOWABLE LIMITS IAW CFM MM 78-31-20 PAGES 609-610. CLEANED, TREATED AND PRIMED IAW DC-8 SRM 51-1-8B. 2L74 4F RT4A25 20060228001092006022800109WP 2006 2 28 IXXA05SMN312S 120051229A5730 REPAIR DOUG DC8 DC872 302199BWP WS 304 MISINSTALLED B IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW11722CX71621 46130 DURING ROUTINE C-CHECK, RT WING - CTR L/E LWR PART HAS NON STANDARD REPAIR, XFS 304.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 06006 DATED 01-05-06, SEMAN DWG ED-4134 DATED 01-04-06, ED SEMAN 2005 1471 DATED 01-05-06. REMOVED NON STANDARD REPAIR IAW DC8 SRM 51-1-21. STOP DRILLER CRACK END IAW SEMAN DWG ED-4134. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01-001, FABRICATED REPAIR DOUBLER (AL 7075 T6 0.071) IAW SEMAN DWG ED-4134. CLEANED TREATED; PRIMED AREA & REPAIR DOUBLER IAW DC8 SRM 51-1-8B, APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11. INSTALLED REPAIR PARTS IAW SEMAN DWG ED-4134, DC8 SRM 51-1-21, DC8 SRM 51-1-20D, DC-8 SRM 51-3-0, DC8 SRM 51-3-1 (TORQUE). 2L74 4F RT4A25 20060228001102006022800110WP 2006 2 28 IXXA05SMN313S 120051229A5730 REPAIR DOUG DC8 DC872 302199BWP WS 63.75 MISINSTALLED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11722CX71621 46130 DURING ROUTINE C-CHECK INSPECTION, RIGHT WING - INBOARD L/E LWR PART HAS NON STANDARD REPAIR, XFS 63.750. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 06006 DATED 01-05-06, SEMAN DWG ED-4133 DATED 02-06-06, ED SEMAN 2005 1470 DATED 01-05-06. REMOVED EXISTING NON STANDARD REPAIR IAW DC8 SRM 51-1-21. FABRICATED REPAIR DOUBLER (AL 7075 T6 0.071) IAW SEMAN DWG ED-4133. CLEANED, TREATED; PRIMED AREA & REPAIR DOUBLER IAW DC8 SRM 51-1-8B, APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11, INSTALLED REPAIR DOUBLER IAW SEMAN DWG ED-4133, DC8 SRM 51-1-21, DC8 SRM 51-1-20D, DC8 SRM 51-3-1 (TORQUE). 2L74 4F RT4A25 20060228001112006022800111WP 2006 2 28 IXXA05SMN315S 120051229A5754 REPAIR DOUG DC8 DC872 302199BWP RT WING MISINSTALLED B IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW11722CX71621 46130 DURING C-CHECK, RT WING - L/E SLOT VANE HAS NON STANDARD REPAIR, XOLDO 66. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 05586 DATED 12-28-05, SEMAN DWG ED-4136 DATED 12-23-05, ED SEMAN 2005 1473 DATED 12-28-05. REMOVED NON STANDARD REPAIR. REMOVED DAMAGED SECTION, PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01-001, FABRICATED REPAIR DOUBLER (AL 7075 T6 0.071) & FILLER, INTERNAL DOUBLER (ALCLAD 7075 T6 0.063) IAW SEMAN DWG ED-4136. CLEANED, TREATED; PRIMED AREA & INNER FACE OF REPAIR PARTS IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11, INSTALLED REPAIR PARTS IAW SEMAN DWG ED-4136, DC8 SRM 51-1-21, DC8 SRM 51-1-20D, DC-8 SRM 51-3-0, DC8 SRM 51-3-1 (TORQUE). 2L74 4F RT4A25 20051024000062005102400006NM 2005 10 24 SWAA053256 120051019A53106935367 CREASE BEAM BOEING737 7373H4 1384600NM BS 309-349 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D CHECK, FOUND FUSELAGE CREASE BEAM WEB CORRODED BETWEEN BS 309 TO BS 349, LBL 55 TO LBL 61, WL. 208. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20051024000112005102400011NM 2005 10 24 SWAA053261 120051019A53116546526 FRAME BOEING737 7373H4 1384600NM BS 400 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051024000142005102400014NM 2005 10 24 SWAA053264 120051019A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 664 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 664, STR 10R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051024000202005102400020NM 2005 10 24 CALA0500369 120051019A33501010428 LIGHT BOEING737 737824 13844BZNM CABIN INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2724202 30429 FOUND EMERGENCY LIGHTS ON OVERHEAD BIN, ROWS 17-20 INOP. REPLACED LIGHT ASSY PER AMM 33-51-06. 2L72 4F RTA16WE 20051024000212005102400021SO 2005 10 24 RAIA00510019 120051017A3350 BULB EMB 145 EMB145LR 3260212SO EMERGNCY LIGHT INOPERATIVE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03838HK 145321 PREFLIGHT INSPECTION - ORD - CABIN EMERGENCY LIGHT INOP BETWEEN ROWS 7 AND 8. MAINTENANCE RELAMPED THE BULB. 2L72 4T RTT00011AT 20051024000222005102400022SO 2005 10 24 RAIA00510020 120051018A3350 POWER SUPPLY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03845HK 14500842 PREFLIGHT INSPECTION -SYR - EMERGENCY EXIT LIGHT IN SIGN AT ROW 12 NOT FUNCTIONING PROPERLY. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY POWER SUPPLY NR 4. 2L72 4T RTT00011AT 20051024000282005102400028 2005 10 24 VNAA0510004 420051007A3400 COMPUTER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE MALFUNCTIONED A VNAAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 GL05213PS 7879 THE CREW ABORTED TAKEOFF WHEN THE EFIS COMP MON CAUTION MESSAGE ILLUMINATED AND BOTH HEADING INDICATORS RED FLAGGED. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE CYCLED THE AHARS SYSTEM POWER. THE SYSTEM OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20051024000292005102400029EA 2005 10 24 VNAA0510005 120051008A5200 DOOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE OPEN A VNAAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 GL05260JS 7957 SHORTLY AFTER TAKEOFF THE CREW REPORTED A LOUD POPPING NOISE NEAR THE NOSE OF THE AIRCRAFT. THE FLIGHT RETURNED TO CLT AND LANDED SAFELY. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE EXTERNAL SERVICES PANEL DOOR OPEN AND A HEADSET PLUG ADAPTOR PLUGGED INTO THE AUDIO JACKS. THE ADAPTOR WAS REMOVED. NO DAMAGE WAS FOUND ON THE EXTERNAL SERVICES PANEL OR DOOR. PAINT WAS FOUND SCRATCHED ON AN 8 X 4 AREA OF SKIN AFT OF THE PANEL. THE PAINT DAMAGE WAS WITHIN LIMITS AND TRANSFERRED TO THE DAI LIST. THE DOOR WAS SECURED CLOSED AND THE AIRCRAFT RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20051024000322005102400032EA 2005 10 24 COMA0560559 120051017A2750 DRIVE ASSY CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FLAP SYSTEM DIRTY A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01818CA 7408 FLAPS FAIL CAUTION. CND, FOUND NO DEFECTS IN FLAP SYSTEM, CLEANED AND GREASED FLEX DRIVE CABLES. 2L72 4F4 FRTA21EA E15NE 20051024000362005102400036NM 2005 10 24 AWXA200501245 120051018A2560P4010021 FLASHLIGHT BOEING737 7373G7 1384595NM CABIN MALFUNCTIONED A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28311AW 24712 LAS - EEL - ON GROUND CREW REPORTED THAT THE AFT FLIGHT ATTENDANT EMERGENCY FLASHLIGHT LED WAS NOT FLASHING. MAINTENANCE REMOVED AND REPLACED THE AFT GALLEY FLASHLIGHT. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20051024000412005102400041NM 2005 10 24 AWXA200501256 120050918A5322654655216 SHEAR TIE BOEING737 73733A 1384673NM BS 827 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW 23634 GYR - MAJOR REPAIR - DURING C18 CHECK DISCOVERED CORROSION ON AFT CARGO COMPARTMENT BILGE ON SHEAR TIE AT BS 827, WL 250 AND FROM STR 28R TO STR 27R. MAINTENANCE CUT OUT DAMAGED SECTION OF SHEAR TIE IAW BOEING 737-300 SRM 53-00-07-2R. FABRICATED REPAIR SHEAR TIE AND INSTALLED FROM STR 28R TO STR 27R, WL 205 AND BS 827 IAW BOEING 737-300 SRM 53-30-07-2R4. 2L72 4F RTA16WE 20051024000452005102400045CE 2005 10 24 DJFA2005151 120051016A2910 HYDRAULIC SYSTEM RAYTHNDH125 HAWKER800XP 7150012CE MAIN MALFUNCTIONED E DJFAA UNSCHED LANDING GJ MULTIPLE FAILURE WARNING INDICATION APAPPROACH 1 EA23848CW 258648 THE CREW REPORTED, EXPERIENCED A MAIN HYDRAULIC SYSTEM FAILURE DURING LANDING GEAR AND FLAP EXTENSION WHILE ON A VISUAL APPROACH INTO KCKV. A GO-AROUND WAS EXECUTED AND A SUBSEQUENT DIVERSION WAS MADE TO KBNA. THE LANDING GEAR WAS EXTENDED AND FLAPS WERE AT 15 DEGREES WHEN THE FAILURE OCCURRED. THE AUXILIARY HYDRAULIC SYSTEM WAS USED TO COMPLETE FLAP EXTENSION. AN EMERGENCY WAS DECLARED BY THE CREW AND THE AIRCRAFT WAS LANDED IN KBNA WITHOUT FURTHER INCIDENT. 2L72 4F RTA3EU 20051024000462005102400046SO 2005 10 24 BSYA200500015 120051018A3260 SWITCH PIPER PA31 PA31P350 7103111SO MLG DIRTY E BSYAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL073587P 8052120 AIRCRAFT FLYING FROM BUF TO ALB GOT A GEAR UNSAFE LIGHT. PILOT ELECTED TO LAND AT ROC. AIRCRAFT MAINTENANCE JACKED AIRCRAFT, CLEANED AND LUBED SWITCH. OPS CHECKED GOOD OK FOR SERVICE. 1L72 3O RTA8EA 20051024000482005102400048 2005 10 24 SWAA053244 420051018A25656557463 FITTING BOEING737 7373H4 1384600NM GIRT BAR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D-CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FLOOR FITTING CORRODED. REMOVED AND REPLACED FLOOR FITTING PER SRM. 2L72 4F RTA16WE 20051024000552005102400055EA 2005 10 24 SWIA200515691 120051017A2750855D10011 SENSOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 NM07960SW4465 4465 7853 RECEIVED A -FLAP FAIL CAUTION MSG- WHEN FLAPS WERE SELECTED TO 30 DEG ON APPROACH. REPLACED RT BPSU IAW AMM 27-51-10. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051024000562005102400056 2005 10 24 SWIA200515692 420051013A34256226190204 COMPUTER EMB 120 EMB120ER 3260203SO E/E BAY MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07565SW1255312553 120340 AUTOPILOT PITCH IS JERKY AND NOT SMOOTH IN ALL MODES OF FLIGHT. REPLACED PITCH SERVO AND NR 1 AHRS IAW MM 34-21-01. OPERATIONAL TEST GOOD IAW MM 22-10-00. P/N: 622-5734-002, S/N: OFF 3767. 2L72 4T RTA31SO 20051024000572005102400057EA 2005 10 24 SWIA200515693 120051016A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 NM07962SW1288812888 7859 SPOILERON FAULT MESSGAE DISPLAYED ON APPROACH TO SLC. REPLACED RT INBOARD AND OUTBOARD SPOILERON PCU IAW AMM 27-62-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051024000592005102400059EA 2005 10 24 SWIA200515695 120051015A273010231007 DAMPER CNDAIRCL600 CL6002B19 1900309EA ELEVATOR MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07951SW6421 6421 7795 RECEIVED A -FLUTTER DAMPER STATUS MSG- INFLIGHT. REPLACED RT ELEVATOR INBOARD FLUTTER DAMPER IAW CRJ MM 27-34-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051024000602005102400060EA 2005 10 24 SWIA200515696 120051015A27604916405 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07941SW9135 9135 7750 SPOILERONS FAULT ON THE GROUND. REPLACED LT SECU IAW 27-61-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051024000802005102400080CE 2005 10 24 DELA200500009 120050926A29105417005L095 LINE LEAR 55 55LEAR 5170702CE HYD SYSTEM CHAFED E DELAK NONE K FLUID LOSS ININSP/MAINT 1 CE03522WK8473 088 HYDRAULIC FLUID LOSS WAS NOTED BY FLIGHT CREW DURING POST FLIGHT INSPECTION. INSPECTION BY MAINTENANCE NOTED THAT THE LEFT HAND CASE DRAIN LINE AND PRESSURE LINE WERE CHAFFED. THE CASE DRAIN LINE WAS LEAKING DUE TO A CHAFFED HOLE. BOTH LINES WERE REPLACED. 2L72 4F A10CE 20051024000822005102400082WP 2005 10 24 IXXA05SMN165S 120050810A5330 SKIN DOUG DC8 DC873F 302199FWP BS 10 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL948072897 46003 DURING ROUTINE C CHECK INSPECTION, EXTERNAL FUSELAGE AFT HEAT EXCHANGER RT LWR CORNER CRACKED 1, STA 10.000, L-27L. PERFORMED MAJOR REPAIR IAW FAA 8110.3 NR 05367 DATED 08-19-05, SEMAN DWG ED 4055 DATED 08-14-03 AND EO SEMAN NR 20051140 DATED 08-19-05. REMOVED FASTENERS IAW DC8 SRM 51-1-21 PAGE 1, DC8 SRM 51-1-20D PAGE 21. REMOVED DAMAGED AREA IAW SEMAN DWG ED 4055. PERFORMED NDT INSPECTION IAW DC-8 NDT SPM, PART 06-10-01-001. FAB`D REPAIR DOUBLER (AL 2024T3 0.050) + REPAIR TRIPLER (AL 2024T3 0.063) + FILLER (AL 2024T3 0.100) IAW SEMAN DWG ED 4055, DC8 SRM 51-1-4 PAGE 1 (FORMING). CLEANED, TREATED AND PRIMED REPAIR PARTS IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11 PAGE 9.2L74 4F RT4A25 20051024000882005102400088NM 2005 10 24 AWXA200501247 120050924A534069165096 STRINGER CLIP BOEING737 7373S3 1384711NM BS 348 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 MCN - MAJOR REPAIR - DURING C18 CHECK DISCOVERED STR 16L CLIP CRACKED, .3 INCHES, BETWEEN BS 348. MAINTENANCE REMOVED STR 16L CLIP AND REPLACED WITH NEW FABRICATED PART AT BS 348 IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NO. 03-5310-05285-ES5. 2L72 4F RTA16WE 20051024000902005102400090NM 2005 10 24 AWXA200501249 120051011A532065917001156 INTERCOSTAL BOEING737 7373G7 1384595NM BS 640 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED INTERCOSTAL ANGLE CRACKED, 1.1 INCHES, AT BS 640 AND STR 15L. MAINTENANCE REMOVED ATTACH ANGLE AND FABRICATED ATTACH ANGLE IAW BOEING 737-300 SRM 51-40-02-0G AND DWG 65-91700. INSTALLED FABRICATED REPAIR PARTS AT BS 640 AND STR 15L IAW BOEING 737-300 SRM 51-40-02-0G FIGURE 8. 2L72 4F RTA16WE 20051024000912005102400091NM 2005 10 24 AWXA200501250 120051012A5340653535214 STRINGER CLIP BOEING737 7373G7 1384595NM BS 639 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED STRINGER TIE CLIP CRACKED, .75 INCHES, AT BS 639 AND STR 3R. MAINTENANCE REMOVED AND INSTALLED NEW STRINGER TIE CLIP AT BS 639 AND STR 34 IAW BOEING G737-300 SRM 51-40-02-0G FIGS 3, 8, AND 12. 2L72 4F RTA16WE 20051024000962005102400096EA 2005 10 24 VNAA0510009 120051012A35103801950110 HOSE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE OXYGEN SYSTEM RUPTURED A VNAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL05220PS3809 7887 CLIMBING THRU FL120, THE CREW HEARD A HISSING SOUND AND REPORTED THAT THE CREW OXYGEN QUANTITY WAS DEPLETED. THE QRH WAS FOLLOWED AND THE FLIGHT DIVERTED TO PIT. MAINTENANCE FOUND THE OXYGEN HOSE UNDER THE FIRST OFFICER'S MASK STOWAGE BOX RUPTURED. THE HOSE WAS REMOVED AND REPLACED IAW CRJ200 AMM 35-11-15-000(400)-801. THE CREW OXYGEN BOTTLE WAS ALSO REMOVED AND REPLACED IAW CRJ200 AMM 35-11-03-000(400)-801. THE OXYGEN SYSTEM WAS SERVICED AND LEAK CHECKED GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20051024001002005102400100WP 2005 10 24 IXXA05SMN172S 120050811A5330 SKIN DOUG DC8 DC873F 302199FWP ZONE- 800 OUT OF LIMITS B IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL948072897 46003 DURING C-CHECK INSPECT, DOUBLER BEHIND D-PIT DOOR OPENING ON SKIN SPLICE, SIDES 2 AND 3 EXCEED MAX RIVET SPACING, ALUMINUM & JO-BOLTS IN LONGERONS. ADD ADDITIONAL RIVETS TO BRING UNDER MAX SPACING OF 1.400, STA FS 1520 L-29R. PERFORMED REPAIR IAW FAA FORM 8110-3 NR 05366, SEMAN DWG ED-4052 DATED 08-11-05 AND EO SEMAN NR 20051130 DATED 8-19-05. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21 PG 1 AND DC8 SRM 51-1-20D PG 21. PERFORMED DETAILED VISUAL INSPECT. NO CRACK OR CORROSION FOUND. FABRICATED REPAIR DOUBLER INTERNAL FINGER DOUBLERS IAW SEMAN DWG ED-4050 AND DC8 SRM 51-1-4 PG 1. INSTALLED REPAIR PARTS IAW SEMAN DWG ED-4052, DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 9, AND DC8 SRM 51-3-1. 2L74 4F RT4A25 20051024001062005102400106NM 2005 10 24 DL73S050593 120050905A3244B737MAIN TIRE BOEING737 737232 1384475NM MLG DAMAGED A DALAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO27304DL 23076 ON WALK AROUND, FOUND NR 3 MAIN TIRE FAILURE CAUSING DAMAGE TO RT INBD FLAP AND RT GEAR INBD TRAILING EDGE FORE FLAP. CLOSE OUT PANEL. REPLACED TIRE AND REPAIRED DAMAGE. 2L72 4F RTA16WE 20051024001082005102400108NM 2005 10 24 DL75K050595 120050923A5330143N31211 SKIN BOEING757 757232 1384965NM BS 878 LIGHTNING STRIKEA DALAK NONE O OTHER ININSP/MAINT 1 SO27610DL 22817 LIGHTNING STRIKE DAMAGE TO THE FUSELAGE SKIN AT FS 878, ABOVE STRINGER 4R. DAMAGE TO OUTER SKIN ONLY AT A PRODUCTION FASTENER LOCATION. REPAIR DOUBLER INSTALLED TO REPAIR THE DAMAGE CUTOUT. 2L72 4F RTA2NM 20051024001092005102400109NM 2005 10 24 DL76G050596 120051006A2131UKN CONTROLLER BOEING767 767332 1382001NM CABIN PRESSURE MALFUNCTIONED A DALAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO271609 30574 AFTER STARTING RT ENGINE PRIOR TO TAKEOFF THE CABIN ALT DESCENDED RAPIDLY APPROX 1000 FPM. AUTO INOP LIGHT ILLUM SHORTLY THEREAFTER. T/S PER FIM. BIT CHECKED CABIN AUTO CONTROLLERS. CABIN AUTO 1 FAULTED SELECTOR PANEL AND AUTO 2 FAULTED ITSELF. PER FIM REPLACED NR 2 CABIN AUTO CONTROLLER AND CABIN ALT CONT PANEL PER MM. CABIN AUTO CONTROLLER 1 AND 2 BITE CHECK OK. NO FAULT. EICAS MSG CLEARED. 2L72 4F RTA1NM 20051024001112005102400111 2005 10 24 SA05109 420051018A256561639103 BOTTLE AIRBUSA321 A321211 3930370EU ESCAPE SLIDE FAULTY A USAAK NONE J WARNING INDICATION ININSP/MAINT 1 EA19164UW159056984 1425 BOS - A SLIDE BOTTLE PRESSURE CAUTION LIGHT CAME ON THE CABIN INTERCOMMUNICATION DATA SYSTEM PANEL DURING DOOR CLOSURE. MAINTENANCE RELEASED THE AIRCRAFT ON MEL. REPLACED THE L3 DOOR SLIDE BOTTLE. OK FOR SERVICE. 2L72 4F RTA28NM 20051024001122005102400112NM 2005 10 24 DLM88050598 120051007A3230 LEVER DOUG MD88 MD88 3023688NM LANDING GEAR BYPASSING A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27963DL 49982 ON CLIMBOUT LANDING GEAR DID NOT RETRACT, 3 RED LIGHTS INITIALLY THEN THREE GREEN UPON EXTENSION. STOWED LANDING GEAR BYPASS LEVER. 2L72 4F RTA6WE 20051024001142005102400114EA 2005 10 24 MASA200500813 120051017A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA LAVATORY WILL NOT TEST A MASAO OTHER L NO TEST NRNOT REPORTED 1 SW07154SF 7154 ASH 6150 PHX - LAV SMOKE DETECTOR WILL NOT TEST. OPS CHECKED GOOD. 2L72 4F RTA21EA 20051024001262005102400126NM 2005 10 24 DLM88050604 120051009A2432203BC1021 CHARGER DOUG MD88 MD88 3023688NM MASTER BATTERY BURNED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27966DL 53115 AFTER T/O, SMELLED ODOR OF BURNT TOAST. ODOR DISSIPATED BY LEVEL OFF. FOUND BATTERY CHARGER WITH BURN SPOT ON IT. REPLACED BATTERY CHARGER BATTERYS AND BATTERY CHARGER C/B. 2L72 4F RTA6WE 20051024001342005102400134WP 2005 10 24 UPS05845618 120051011A5330 DOUBLER DOUG DC8 DC873F 302199FWP FUSLEAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 AT 60 HOLE INTERNAL SUPPORT DOUBLER HAS CORROSION OUT OF LIMITS AND DOUBLE DRILLED HOLES. REMOVED INTERNAL SUPPORT DOUBLER AT THE 60 HOLE IAW SRM 51-3-0. FABRICATED AND INSTALLED INTERNAL SUPPORT DOUBLER AT THE 60 HOLE IAW DWG 5649329. 2L74 4F RT4A25 20051024001372005102400137WP 2005 10 24 UPS05845621 120051012A5330 FINGER DOUBLER DOUG DC8 DC873F 302199FWP BS 1350-1490 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 FINGER DOUBLER CRACKED AND CORRODED AT STA 1350-1490 L31L. REMOVED FINGER DOUBLER AT STA 1350-1490 L31L IAW SRM 51-1-21. FABRICATED AND INSTALLED FINGER DOUBLER AT STA 1350-1490 L31L IAW SRM 51-3-2, AND SRM 51-1-8, AND 51-1-21. 2L74 4F RT4A25 20051024001382005102400138WP 2005 10 24 UPS05845622 120050912A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP BS 902 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 POSSIBLE CRACK AT FLOORBEAM LOWER AREA STA 902 RBL 50-55. NDT VERIFIED TWO CRACKS. CUT OUT DAMAGED SECTION OF FLOORBEAM, FABRICATED REPLACEMENT SECTION OF FLOORBEAM AND REPAIR PARTS IAW SAA SK 801-805214. 2L74 4F RT4A25 20051024001392005102400139WP 2005 10 24 UPS05845624 120051017A5414 SKIN DOUG DC8 DC871F 302199DWP NR 4 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 NR 4 PYLON O/B SKIN CRACKED APPROX 1 INCH LONG OB SIDE APPROX 6 INCHES AFT OF FWD BOX BULKHEAD. ACCOMPLISHED INTERIM REPAIR PER EO DC8-5430-23086A. PERMANENT REPAIR WITHIN 10 FLT CYCLIES, D312151 ASSIGNED. ACCOMPLISHED PERMANENT REPAIR PER EO DC8-5430-23086B. THIS CLEARS D312151. 2L74 4F RT4A25 20051024001452005102400145WP 2005 10 24 IXXA05SMN164S 120050810A5720 VANE DOUG DC8 DC873F 302199FWP LT WING DAMAGED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL948072897 46003 DURING C-CHECK INSPECT, LT WING, VANE SLOT L/E HAS INTERIM REPAIR, XOLDI 6.225. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05368 DATED 08-19-05, DWG SEMAN ED-4054 DATED 08-15-05 AND EO SEMAN NR 20051136 DATED 08-19-05. REMOVED NON STANDARD REPAIR IAW DC8 SRM 51-1-21 PG 1 AND DC8 SRM 51-1-20D PG 21. REMOVED DAMAGED AREA IAW DWG ED-4054. PERFORMED NDT INSPECTION DC8 NDT SPM PART 06-10-01-001. FABRICATED EXTERNAL REPAIR DOUBLER, FILLER IAW SEMAN DWG ED-4054 AND DC8 SRM 51-1-4 PG 1. INSTALLED REPAIR PARTS IAW SEMAN DWG ED-4054, DC8 SRM 51-1-21 PG 1 AND DC8 SRM 51-3-0 PG 1, DC8 SRM 51-1-20D PG 9, AND DC8 SRM 51-3-1. 2L74 4F RT4A25 20051024001462005102400146WP 2005 10 24 IXXA05SMN166S 120050810A5340 FITTING DOUG DC8 DC873F 302199FWP BS 340 CRACKED B IXXAO OTHER O OTHER ININSP/MAINT 1 SW11603AL948072897 46003 DURING ROUTINE C CHECK INSPECTION, FWD CARGO COMPT FITTING CRACKED .5 INCHES STA 340.000 , L-32R L-33R. REMOVED AND REPLACED CRACKED FITTING ON FWD CARGO CMPT, STA 340.000, L32R-L33R IAW DC8 SRM 51.1.20D PAGES 9, 21. TORQUED IAW DC8 SRM 51-3-1. 2L74 4F RT4A25 20051024001482005102400148WP 2005 10 24 IXXA05SMN169S 120050811A5330 SKIN DOUG DC8 DC873F 302199FWP BS 255 DAMAGED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL948072897 46003 DURING C-CHECK INSPECT, RT FWD FUSELAGE JUST FWD OF A-PIT DOOR OPENING DOUBLER THICKNESS RATIO EXCEEDED MAX ALLOWED. DOUBLER THICKNESS 0.135", SKIN 0.071". REWORK REPAIR TO BRING INTO SRM LIMITATIONS WITH LOCK FASTENERS IN LONGERONS, STA FS 255 L-36. PERFORMED REPAIR IAW FAA 8110.3 05367 DATED 08-19-05, SEMAN DWG ED 4046 DATED 08-15-05 AND EO SEMAN NR 20051123 DATED 08-19-05. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-20D PAGE 21, DC8 SRM 51-1-21 PG 1. REMOVED DAMAGED AREA IAW SEMAN DWG ED 4046. PERFORMED NDT INSPECT IAW DC-8 NDT SPM, PART 06-10-01-001. FABRICATED REPAIR DOUBLER, REPAIR TRIPLER, FILLER & FILLER IAW SEMAN DWG ED 4046, DC8 SRM. INSTALLED REPAIR PARTS IAW SEMAN DWG ED 4046, DC-8 SRM. 2L74 4F RT4A25 20051024001492005102400149NM 2005 10 24 SWAA053241 120051018A53226546529 SHEAR TIE BOEING737 7373H4 1384600NM BS 500D CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051024001502005102400150NM 2005 10 24 SWAA053242 120051018A53116546538 FRAME BOEING737 7373H4 1384600NM BS 597 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, BETWEEN STR 13L TO STR 14L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051024001512005102400151NM 2005 10 24 SWAA053202 120051016A57546573714 SKIN BOEING737 7375H4 138449DNM RT WING SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED 1/2D CHECK, FOUND RT WING NR 5 L/E SLAT DELAMINATED & DISBONDED. REPAIRED SLAT PER SRM. 2L72 4F RTA16WE 20051024001522005102400152NM 2005 10 24 SWAA053203 120051015A53116546529 FRAME BOEING737 7373H4 1384600NM BS 440 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, RBL 39. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20051024001532005102400153NM 2005 10 24 SWAA053204 120051015A53116520723 FRAME BOEING737 7373H4 1384600NM BS 492 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 492.4, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20051024001552005102400155NM 2005 10 24 SWAA053206 120051015A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM BS 787 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, LBL 17. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051024001572005102400157EA 2005 10 24 COMA0560557 120051016A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO01818CA 7408 FLIGHT 5711- FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2L72 4F RTA21EA 20051024001592005102400159NM 2005 10 24 SWAA053243 120051018A5315BAC15171489 FLOORBEAM BOEING737 7373H4 1384600NM COCKPIT FLOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D-CHECK, FOUND COCKPIT FLOOR Z-CHORD CORRODED AT BS 270, BETWEEN LBL 11 TO RBL 11. REPAIRED Z-CHORD PER SRM. 2L72 4F RTA16WE 20051024001642005102400164NM 2005 10 24 AWXA200501226 120051015A5230 SEAL BOEING737 7373G7 1384595NM CARGO DOOR FAILED A AWXABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP28308AW 24710 GYM - DIVERSION - DURING CRUISE, EN ROUTE TO SJD FROM PHX, AIRCRAFT BEGAN TO DEPRESSURIZE AT FL330. CREW PERFORMED EMERGENCY DESCENT, PASSENGER O2 WAS DEPLOYED AND USED. AIRCRAFT DIVERTED INTO GYM WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND SEVERAL FEET OF AFT CARGO DOOR SEALING DISPLACED. RE-INSTALLED SEALING AS REQUIRED. PRESSURIZATION CHECKS WERE GOOD AND AIRCRAFT MAINTENANCE FERRIED BACK TO PHX FOR REPLACEMENT OF USED O2 GENERATORS. 2L72 4F RTA16WE 20051024001662005102400166NM 2005 10 24 ASMF200510007 120051014A7711LG80E1 INDICATOR DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE LEFT EPR FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23158PL6702 49761 725604 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF LEFT ENGINE EPR’S INDICATOR REMAINED ON 1.00 WHEN APPLYING TAKEOFF POWER. THE EPR INDICATOR WAS REPLACED IAW MM 77-11-02, TESTED CORRECT. DURING OVERNIGHT CHECK, THE LEFT ENGINE TRIM WAS PERFORMED IAW MM 71-00-00, ALL CORRECT. 2L72 4F4 FRTA6WE E9NE 20051024001682005102400168NE 2005 10 24 ASMF200510010 220051016A742147649 IGNITER BOX BOEING757 75729J NM PWA 2037 PW2037 NE RT ENGINE FAILED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23703AM7481 27203 726730 CAPTAIN REPORTED THAT DURING RIGHT ENGINE START WITH IGNITION SELECTOR IN POSITION ONE, THE RIGHT ENGINE EGT DID NOT INCREASE. AIRCRAFT WAS SENT TO THE HANGAR AND DURING MAINTENANCE REVISION WAS DETECTED THE CABLE OF THE SYSTEM TWO DAMAGED. THE EXCITER IGNITION BOX AND IGNITION SYSTEM ONE AND TWO CABLES WERE REPLACED IAW MM 74-11-01 AND MM 74-21-01 RESPECTIVELY, CONTINUING THE FAILURE IN SYSTEM ONE. THE REPORT WAS DEFERRED IAW MEL 74-00-1 CAT C, SYSTEM TWO OPERATED CORRECTLY. DURING OVERNIGHT CHECK, THE IGNITION PLUG NUMBER ONE WAS REPLACED IAW MM 74-21-02 AND OPERATIONAL TEST WAS PERFORMED, BEING CORRECT. DEFERRED REPORT WAS CLOSED. 2L72 4F4 FRTA2NM E17NE 20051024001722005102400172EA 2005 10 24 SWIA200515680 120051012A27604916420 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07435SW2781 2781 7555 "FLIGHT SPOILER FAULT" MESSAGE ON EICAS. REPLACED SECU AS REQUIRED. OPERATIONAL CHECK GOOD IAW 27-61-05. 2L72 4F RTA21EA 20051024001732005102400173 2005 10 24 SWIA200515681 420051012A22106229815704 COMPUTER CNDAIRCL600 CL6002B19 1900309EA FLIGHT CONTROL MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07929SW 7703 YAW DAMP 1 INOP STATIS MSG. REPLACED NR 1 AND NR 2 FCC CARDS IAW CRJ 200 MM 22-12-14, OPERATIONAL CHECK GOOD, PN OFF 622-9815-704, SN1 OFF: 10BMP, SN2 OFF: 09RW 2L72 4F RTA21EA 20051024001742005102400174EA 2005 10 24 SWIA200515682 120051008A2750860D10018 FCU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07416SW1286912869 7089 FLAPS FAIL CAUTION MESSAGE WITH OVERSPEED CLACKER FLAPS WERE IN THE 0 DEGREE DETENT POSITION. REPLACED FECU IAW MM 27-51-05, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051024001752005102400175SO 2005 10 24 SWIA200515683 120051013A3350 LIGHT EMB 120 EMB120ER 3260203SO CABIN BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07186SW 120034 RT OVERWING EMERGENCY LIGHT BROKEN. REPLACED RIGHT WING EMERGENCY EXIT LIGHT ASSY, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20051024001802005102400180EA 2005 10 24 SWIA200515688 120051007A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07975SW 7951 AFT OVERWING EXIT EMERGENCY LIGHT BURNED OUT. REPLACED BULB. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051024001842005102400184NM 2005 10 24 DL73S050615 120051013A53156545410224 FLOORBEAM BOEING737 737232 1384475NM BS 660 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27329DL 23101 THE RBL 24 LONGITUDINAL OVERWING FLOORBEAM HAS BEEN PREVIOUSLY MODIFIED PER 3-056673-3AD. THE C-CHANNEL INSTALLED PER THIS EO DOES NOT MEET EXISTING AD REQUIREMENTS. CRACKS WERE FOUND IN THE UPPER CHORD, BEAM AFT WEB, AND WEB DOUBLERS. THE C-CHANNEL WAS REPLACED, WEB DOUBLER WAS REPLACED, WEB WAS REPAIRED AND UPPER CHORD WAS REPAIRED PER ER/A 451091-14AD. 2L72 4F RTA16WE 20051024001862005102400186NE 2005 10 24 DL76G050617 220051006A7200CF680C2B6F ENGINE BOEING767 767332 1382001NM GE CF6 CF680C2B6F 30025NE NR 1 FAILED A DALAK NONE O OTHER ININSP/MAINT 1 SO271606529282 704883 30199 704883 NR 1 ENGINE, S/N 704883 FAILED OPN 5155 BOROSCOPE INSP DUE TO 1 EA 1ST STAGE NGV HAVING BURN THRU AREA BEYOND M/M LIMITS. ENGINE REMOVAL REQUIRED. ENGINE S/N 704883, REMOVED AND REPLACED PER TRANS 1T160. 2L72 4F4 FRTA1NM E13NE 20051024001912005102400191NM 2005 10 24 DL73S050625 120050919A5315654541039 FLOORBEAM BOEING737 737247 138448DNM BS 660 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27373DL 23520 DURING INSPECTION PER SI 3-56673-12, AN EXISTING REPAIR/MODIFICATION WAS FOUND TO BE CRACKED IN THE UPPER FORWARD HOLE OF THE WEB DOUBLER, WEB, UPPER CHORD, AND MOD CHANNEL AT RBL 24.8 AND LBL 24.8. CRACKS WERE REMOVED, WEB DOUBLERS, CHORDS, AND MOD CHANNELS WERE REPLACED AND THE WEB WAS REPAIRED WITH A DOUBLER PER ER/A'S 450662-12AD AND 450663-14AD. 2L72 4F A16WE 20051024001942005102400194EA 2005 10 24 REXA200500131 120051007A2752 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA TE FLAP FAILED A REXAO OTHER J WARNING INDICATION APAPPROACH 1 SO25826AY 8026 FLAPS FAIL ON APPROACH WHEN SELECTED TO 30. FOLLOWED QRH, LANDED WITHOUT INCIDENT. REMOVED AND REPLACED LEFT INBOARD FLAP ACTUATORS POSITION 1 AND 2 P/N 852D100-19. 2L72 4F RTA21EA 20051024001952005102400195EA 2005 10 24 REXA200500132 120051009A2120 SMOKE CNDAIRCL600 CL6002B19 1900309EA COCKPIT DETECTED A REXAC ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SO258721B 7721 ABORTED TAKEOFF FOR COCKPIT SMOKE. NO WARNING INDICATIONS, SMOKE VISIBLE. FOLLOWED QRH AND CHECKLIST, NOTIFIED DISPATCH AND MAINTENANCE CONTROL ALONG WITH LOCAL OPERATIONS, RETURN TO GATE. AIRCRAFT SWAP. GVI OF LEFT ENGINE COMPLETED AND HIGH POWER RUNS PERFORMED WITH NO DEFECTS NOTED. 2L72 4F RTA21EA 20051024001992005102400199EA 2005 10 24 ASOA05688 120050820A5330 FINGER DOUBLER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE BS 439 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27839AS 7284 DURING C-CHECK, THE FINGER DOUBLERS AT FS439, LBL44, RBL44 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO MFG FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. (K) S/D - MAINTENANCE REMOVED THE CORROSION FROM THE FINGER DOUBLERS AT FS 439, LBL 44 AND RBL 44 BY COMPLYING WITH ASA EO 600-53-0314. (M) 2L72 4F4 FRTA21EA E15NE 20051024002012005102400201NM 2005 10 24 DHL2005742503 120050918A5347 SEAT TRACK BOEING727 727225 1384077NM BS 950E GOUGED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15742DH 21290 SEAT TRACK GOUGED AT BS 950E+5 LBL 45 (O/B TRACK). REMOVED SEAT TRACK, FABRICATED AND INSTALLED SEAT TRACK 130 -.875 INCH FROM 7178-T6511 IAW B727 SRM 51-30-2. 2L73 4F A3WE 20051024002022005102400202NM 2005 10 24 DHL2005742504 120050918A5347 SEAT TRACK BOEING727 727225 1384077NM BS 804 GOUGED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15742DH 21290 SEAT TRACK GOUGED AT BS 804 LBL 45 (O/B TRACK). REMOVED SEAT TRACK, FABRICATED AND INSTALLED SEAT TRACK 130 - .5 INCH FABRICATED FROM 7178-T6511 IAW B727 SRM 51-30-2. 2L73 4F A3WE 20051024002032005102400203NM 2005 10 24 DHL2005742505 120050918A5347 SEAT TRACK BOEING727 727225 1384077NM BS 720B GOUGED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15742DH 21290 SEAT TRACK GOUGED AT BS 720B + 15 LBL 45. REMOVED SEAT TRACK, FABRICATED AND INSTALLED SEAT TRACK 130 - .5 INCH FABRICATED FROM 7178-T6511 IAW B727 SRM 51-30-2. 2L73 4F A3WE 20051024002042005102400204NM 2005 10 24 DHL2005742507 120050917A5320 WEB BOEING727 727225 1384077NM BS 720 CRACKED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15742DH 21290 RT BL 65 WEB CRACKED BEHIND GILL LINER BS 720D + 10. REMOVED GILL LINER SUPPORT ANGLE, FABRICATED AND INSTALLED 2 EACH REPAIR ANGLES 32 INCHES AND 33 INCHES AND 1 EACH DOUBLER 36 - .5 X 16 INCHES FROM 2024-T3 .025 IAW B727 SRM 51-40-2 AND 51-30-2. 2L73 4F A3WE 20051024002052005102400205NM 2005 10 24 DHL2005742508 120050930A5320 SUPPORT ANGLE BOEING727 727225 1384077NM BS 1163 CORRODED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15742DH 21290 AFT PIT BS 1163 WL 25 LBL 25 TO RBL 25 FRAME HAS EXFOLIATED CORROSION. SUPPORT ANGLE FOUND BEYOND LIMITS IAW B727 SRM 53-10-1 FIG 1, 100 PERCENT MATERIAL LOSS. REMOVED SUPPORT ANGLE, FABRICATED AND INSTALLED SUPPORT ANGLE 81 - .375 INCH FROM AND10133-1401 IAW B727 SRM 51-10-2 AND 51-30-2 AND DWG 6567250. 2L73 4F A3WE 20051025000022005102500002WP 2005 10 25 UPS05845633 120051011A5313 LONGERON DOUG DC8 DC873F 302199FWP BS 1880 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE:C2 LONGERON L32L CORRODED AND HAS ELONGATED HOLES AT FS 1880. REMOVED LONGERON 32L AT FS 1880 IAW SRM 51-3-0. FABRICATED AND INSTALLED LONGERON AND SPLICE FITTING AT FS 1880 L32L IAW SRM 53-02-02 AND SRM 51-1-20D. 2L74 4F RT4A25 20051025000042005102500004SO 2005 10 25 SWIA200515711 120051015A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT DISCHARGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07221SW1128411284 120290 ON FFOD CHECKS, MULTIPLE EMERGENCY LTS WILL NOT WORK ON FLOOR STRIP, AND AT EXITS. REPLACED BATTERY PACK AT ROW 5. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20051025000142005102500014NM 2005 10 25 SWAA053274 120051020A3350BR2013 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29451WN 32495 EEPLS FWD END COVER OUT OF POSITION. SECURED EEPLS COVER PER MM. 2L72 4F RTA16WE 20051025000162005102500016 2005 10 25 SWAA053276 420051020A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EVACUATION SLIDE OUT OF ADJUST. REINSTALLED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20051025000182005102500018NM 2005 10 25 SWAA053278 120051020A53306545774 SKIN BOEING737 7373H4 1384600NM BS 791 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29347SW 24374 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 791, STR 17L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051025000202005102500020NM 2005 10 25 SWAA053280 120051020A53116546533 FRAME BOEING737 7373H4 1384600NM BS 495 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29347SW 24374 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUT OUT BS 495, NR 1 STOP FITTING. REPAIRED FRAME BFG ER. 2L72 4F RTA16WE 20051025000222005102500022NM 2005 10 25 UPS05245641 120051021A3350 BATTERY BOEING727 727185C 138406NNM EMERGENCY EXIT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 EXIT LIGHT OVER COCKPIT DOOR INOP. REMOVED AND REPLACED LIGHT ASSY AND BATTERIES. OPS CK GOOD PER AMM 33-50-01-5. 2L73 4F A3WE 20051025000332005102500033WP 2005 10 25 AALA20050693 120051020A3350 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW21561AA 53091 LGA - DURING OVERNIGHT MAINTENANCE FOUND TAIL CONE EMERGENCY LIGHTS INOPERATIVE. REPAIRED A BROKEN WIRE TO THE TAIL CONE EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051025000352005102500035NM 2005 10 25 TSAA0532050 120051020A3241 ANTI-SKID SYS BOEING737 737282 13844ATNM PWA JT8 JT8D9A 52048NE MLG DEACTIVATED A TSAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13824AL 23045 ON CLIMB OUT, PILOT OBSERVED THE LT ANTI-SKID LIGHT ON AND STAYED AND RETURNED BACK TO DEPARTURE. THE ANTI-SKID SYSTEM WAS MEL’D WAITING FOR AN ANTI-SKID CONTROL BOX. THE ANTI-SKID SYSTEM AND ANTI-SKID BRAKES WERE DEACTIVATED. 2L72 4F4 FRTA16WE E2EA 20051025000502005102500050WP 2005 10 25 UPS05845635 120051005A5310 DOOR FRAME DOUG DC8 DC873F 302199FWP BS 280 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 A-PIT DOOR JAMB FWD LWR CORNER O/B OF L33R STA 280 ANGLE IS CRACKED APPROX 1". REMOVED AND REPLACED DOOR FRAME JAMB FITTING IAW SRM 51-1-20D AND SRM 51-1-8. 2L74 4F RT4A25 20051025001202005102500120 2005 10 25 SWAA053311 420051020A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29651SW 27721 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20051025001212005102500121NM 2005 10 25 0501566718 120050915A5311 FRAME BOEING747 747251F 1384898NM PWA JT9 JT9D7F 52054NE BS 380 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01618US 21122 DURING L-CHECK FOUND CRACK IN FRAME AT BS 380 S27R AND S28R. REPAIRED IAW EA 67-165241. 2L74 4F4 F A20WE E20EA 20051025001252005102500125EA 2005 10 25 ASOA05789 120050923A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE BS 559-621 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27835AS 7258 DURING A C-CHECK IN MCN, THE FLOORBEAM CAP AT FS 559 PLUS 112 THRU 621.00, LBL 27 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FLOOREAM CAP AT FS 559 PLUS 112 THROUGH 621.00, LBL 27. (M) 2L72 4F4 FRTA21EA E15NE 20051025001292005102500129EA 2005 10 25 ASOA05779 120050921A5712 RIB CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT WING CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27835AS 7258 DURING A C-CHECK IN MCN, THE RIGHT BATT RIB ASSEMBLY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REPAIR THE RIGHT BATTERY RIB ASSEMBLY AT WS 53.60 IAW ASA EO 600-57-0039B. (M) 2L72 4F4 FRTA21EA E15NE 20051025001312005102500131EA 2005 10 25 COMA0560558 120051017A2752854D10020 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF341A NE TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01804CA8054 7352 FLIGHT 5814 - FLAPS FAIL. REPLACED THE RT OB FLAP ACTUATOR. 2L72 4F4 FRTA21EA E15NE 20051025001322005102500132EA 2005 10 25 ASOA05759 120050820A5242H34455 HANDLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE E/E BAY DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27839AS 7284 DURING A C-CHECK IN MCN, THE AVIONICS BAY DOOR HANDLE WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AVIONICS BAY DOOR HANDLE. OPS CHECKS GOOD. (M) 2L72 4F4 FRTA21EA E15NE 20051025001352005102500135EA 2005 10 25 ASOA05764 120050917A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27841AS 7300 DURING A C-CHECK IN MCN, THE RIGHT INBOARD AND OUTBOARD FS 280 CLIP WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT INBOARD AND OUTBOARD FS 280 CLIPS IAW CRJ200 SRM 51-42-20. (M) 2L72 4F RTA21EA 20051025001372005102500137EA 2005 10 25 ASOA05763 120050917A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA BS 718 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27841AS 7300 DURING A C-CHECK IN MCN, THE RIGHT FRAME AT FS 718, STRINGER 11 AND 12, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RIGHT SIDE FRAME AT FS 718, STRINGER 11 AND 12, IAW ASA EO 600-53-0066. (M) 2L72 4F RTA21EA 20051025001392005102500139EA 2005 10 25 COMA0560560 120051018A2752854D10020 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01804CA8047 7352 FLIGHT 5814 - FLAPS FAIL. REPLACED THE RIGHT OUTBOARD FLAPS ACTUATOR. 2L72 4F RTA21EA 20051025001412005102500141WP 2005 10 25 AALA20050688 120051018A3350P4010049 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT DISCHARGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21495AA 49733 SFO - DURING OVERNIGHT MAINTENANCE FOUND OVERHEAD EMERGENCY LIGHTS INOPERATIVE FROM SEATS 3B TO 6B AND 22B TO 27B. REPLACED THE EMERGENCY LIGHTS POWER SUPPLY AT ROW 6 AND ROW 25 PER MAINTENANCE MANUAL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051025001442005102500144NM 2005 10 25 F3LA200500044 120051013A3244315311 TIRE AIRBUSA319 A319111 3930336NM MLG FAILED A F3LAO OTHER O OTHER LDLANDING 1 NM03918FR 1943 UPON LANDING IN DEN, BOTH NOSE WHEEL TIRES CAME APART. REPLACED BOTH NOSE TIRES PER MM 32-41-12, PG 401. COMPLIED WITH INSPECTION AFTER TIRE BURST PER MP 05510-7. 2L72 4F RTA28NM 20051025001462005102500146NM 2005 10 25 05FDEA03342 120051010A3350 SWITCH BOEING727 72722 1384002NM EMERGENCY LIGHT INOPERATIVE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25268FE 21674 FLIGHT TEST, EMERGENCY EXIT LIGHTS WOULD NOT COME ON WITH ESSENTIAL POWER IN STBY. RESEATED EMERGENCY EXIT LIGHTS AND PERFORMED EMERGENCY LIGHTING OPERATIONAL TEST PER FED-EX MM 33-50-001-5, AND ALSO PLACED ESSENTIAL POWER SELECT SWITCH TO STBY, FOUND SYSTEM TO CHECK GOOD. 2L73 4F A3WE 20051025001472005102500147NM 2005 10 25 05FDEA03344 120051011A5730 DOUBLER DOUG MD11 MD11 3023602NM LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 LEFT WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT XORS 538. RIMMED OUT AS PER FEDEX EA 1-5710-89995. REPAIR DOUBLER AND ANGLE FABRICATED AND INSTALLED AS PER FEDEX EA 1-5710-89995 REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100. 2L73 4F RTA22WE 20051025001492005102500149 2005 10 25 SWAA053044 420051004A25656557463 BRACKET BOEING737 7373H4 1384600NM R2 DOOR SLIDE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED D CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD FLOOR BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER MM. 2L72 4F RTA16WE 20051025001522005102500152NM 2005 10 25 DLM88050628 120051018A3310 SWITCH DOUG MD88 MD88 3023688NM COCKPIT FAILED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 SO27905DL 49536 UPON LANDING HEARD POP AND SAW SMALL AMOUNT OF SMOKE UNDER GLARESHIELD BENEATH NOSE LTS SWITCH. SMOKE/VAPOR DISSIPATE WITHIN SECONDS. ODOR ASSOCIATED. FOUND WIRES FOR BACKGROUND LIGHTING ON LANDING. PANEL CONNECTOR LOOSE AND ARCING. INSTALLED NEW LOCKWASHERS AND SECURED TERMINALS, ALL CHECKS GOOD. 2L72 4F RTA6WE 20051025001542005102500154NM 2005 10 25 DL75K050631 120051017A5330143N31212 SKIN BOEING757 757232 1384965NM BS 686 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27649DL 24389 THE FUSELAGE SKIN AT BS 686, STR 2R HAS A LIGHTNING STRIKE NEXT TO FASTENER. SKIN DAMAGE WAS REMOVED STRINGER WAS REINFORCED, AND A DOUBLER WAS INSTALLED ON THE SKIN PER ER/A 451161-14. 2L72 4F RTA2NM 20051025001562005102500156NM 2005 10 25 DL76L050635 120051019A2432BA0601 BATTERY BOEING767 767332 1382001NM MASTER INOPERATIVE A DALAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CRCRUISE 1 SO27172DN 87874 24775 MAIN BATTERY CHARGER STATUS MESSAGE REMAINED ON IN FLIGHT. REPLACED MAIN BATTERY CHARGER AND MAIN BATTERY PER M/M, OPS NORMAL MSG CLEARED. 2L72 4F RTA1NM 20051025001582005102500158NM 2005 10 25 SWAA053046 120051003A53306545774 SKIN BOEING737 7373Q8 1384670NM BS 727D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 14R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051025001602005102500160NM 2005 10 25 SWAA053048 120051004A53306545777 SKIN BOEING737 737317 138447PNM BS 992 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 992, MAST DRAIN CUTOUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051025001622005102500162NM 2005 10 25 SWAA053050 120051004A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29772SW 27880 EEPLS STRIP MISSING COVER AT ROW 2 TO ROW 3. INSTALLED COVER PER MM. 2L72 4F RTA16WE 20051025001642005102500164EA 2005 10 25 MASA200500411 120050528A5270840534 PROXIMITY SENSOR CNDAIRCL600 CL6002C10 1390015EA PAX DOOR MALFUNCTIONED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07503MJ 10058 ASH 7222 DEN. PAX DOOR HANDLE MESSAGE. R2 PX107 DOOR PROX SWITCH. 2L72 4F RTA21EA 20051025001662005102500166EA 2005 10 25 MASA200500431 120050601A3350316 LAMP CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07509MJ 10094 ASH 7253 TUS. SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. MX RELAMPED. 2L72 4F RTA21EA 20051025001692005102500169SO 2005 10 25 RAIA00510017 120051014A27203603001001 PCU EMB 145 EMB145 3260210SO RUDDER MALFUNCTIONED A RAIAO OTHER F FLT CONT AFFECTED LDLANDING 1 CE03801HK1776317763 145053 FLT 3545 - RIC - RUDDER SYSTEM 1/2 INOP MESSAGE ON EICAS. RUDDER WAS STILL POWERED. MAINTENANCE REMOVED AND REPLACED RUDDER PCU. 2L72 4F RTT00011AT 20051025001712005102500171NM 2005 10 25 05FDEA03207 120051004A57534125501 FITTING DOUG MD11 MD11 3023602NM LT WING TE FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 LTW O/B FLAP MOUNTED L/E UP, STOP FITTING SUSPECTED CRACKED. LT WING O/B FLAP MOUNTED L/E UPSTOP FITTING CRACKED. REMOVED AND NEW FITTING, REPLACED AS PER SRM 51-31-01 VOL II. THIS REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051025001732005102500173WP 2005 10 25 05FDEA03212 120051005A5712 RIB DOUG DC10 DC1010 3022110WP ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE LT WING FIXED L/E COMPT AT STA XORS 559 ZONE 519 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET4 AND 6 VOL I. 2L73 4F A22WE 20051025001752005102500175WP 2005 10 25 05FDEA03214 120051005A5712 RIB DOUG DC10 DC1010 3022110WP ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE LT WING FIXED L/E COMPT AT STA XORS 688 ZONE 525 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 3 AND 4 VOL I. INSTALL REPAIR ANGLE -35. 2L73 4F A22WE 20051025001792005102500179WP 2005 10 25 05FDEA03218 120051005A5712 RIB DOUG DC10 DC1010 3022110WP LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE LT WING FIXED L/E COMPT AT STA XORS 795 ZONE 526 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET4 AND 6 VOL I. 2L73 4F A22WE 20051026000022005102600002EU 2005 10 26 ASOA05761 120050916A3350 LAMP AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27633AS 344 DURING AN A-CHECK IN MCN, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY LIGHT ASSEMBLY ON THE PAX DOOR. OPERATIONAL CHECKS GOOD. (M) 2H72 4T RTA53EU 20051026000042005102600004EA 2005 10 26 ASOA05750 120050829A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA BS 718 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27834AS 7254 DURING A C-CHECK IN MCN, THE FORWARD SIDE OF FUSELAGE FRAME FS 718, STRINGER 10-11 RT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FORWARD SIDE OF FUSELAGE FRAME FS 718, STRINGER 10-11 RT IAW ASA EO 600-53-0066. (M) 2L72 4F RTA21EA 20051026000062005102600006NM 2005 10 26 P5CA0501406 120051020A2120 ODOR BOEING747 74746NF 13848BTNM COCKPIT DETECTED A P5CAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 EA15450PA 30808 ON PREFLIGHT, NOTED ODOR IN COCKPIT. PERFORMED VISUAL INSPECTION IN E/E COMPARTMENT AND COCKPIT PER MM 45-00-00. NO DEFECTS NOTED. 2L74 4F RTA20WE 20051026000072005102600007EA 2005 10 26 ASOA05783 120050921A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA BS 718 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27835AS 7258 DURING A C-CHECK IN MCN, THE LEFT FS 718 FRAME REPAIR WAS FOUND TO POSSIBLY BE CRACKED. S/D - MAINTENANCE INSTALLED A NEW 718 DOUBLER AND A NEW REPAIR DOUBLER IAW BOMBARDIER REO601R-53-61-243. (M) 2L72 4F RTA21EA 20051026000082005102600008EA 2005 10 26 ASOA05745 120050907A335020131A BATTERY PACK CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHTSDISCHARGED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27753EV2743 10169 FLT 4871 - DURING A GROUND INSPECTION IN ATL, THE EMERGENCY LIGHTS BATTERY PACK IN THE AVIONICS COMPARTMENT WAS FOUND DEAD. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK IN THE AVIONICS COMPARTMENT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051026000092005102600009EU 2005 10 26 WRNA20050024 120051023A28217581187 FILTER AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE NR 1 ENGINE FUELDIRTY A WRNAJA DUMP FUEL UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO05502TA 075 517190 NR 1 ENGINE FUEL CLOG LIGHT ILLUMINATED. FUEL DUMPED, AIRCRAFT RETURNED TO BASE. LANDING NORMAL. FUEL FILTER DIRTY, REMOVED AND REPLACED FUEL FILTER, CLEANED FUEL STRAINER IAW 73-12-03. FUNCTIONAL CHECK SATISFACTORY, AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA35EU E23EA 20051026000112005102600011EA 2005 10 26 ASOA05754 120050911A5210601R380741 ANCHOR FITTING CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27674BR 7601 DURING AN A-CHECK IN MCN, THE AFT ANCHOR FITTING ON THE PASSENGER DOOR WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFT ANCHOR FITTING ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. (M) 2L72 4F RTA21EA 20051026000132005102600013NM 2005 10 26 DHL2005742520 120050914A5310 WINDOW FRAME BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE COCKPIT CRACKED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15742DH 21290 PILOT'S NR 2 WINDOW AFT LOWER INTERNAL CORNER ANGLE CRACKED AND CORRODED. REMOVED FITTING P/N 69-367305, FABRICATED SHIMS IAW EA NR AA15-53-1 REV. IR, DRILLED UP FITTING IAW SRM 51-30-2. INSTALLED FITTING IAW SRM 51-30-2, HEAT CHECK IAW MM 56-12-11 STEP. 2L73 4F4 F A3WE E2EA 20051026000142005102600014NM 2005 10 26 DHL2005742521 120051004A5315 FLOORBEAM BOEING727 727225 1384077NM BS 1130 CORRODED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15742DH 21290 AFT PIT CEILING, CABIN FLOORBEAM STA 1130 UPPER SURFACE HAS CORROSION AT LBL 60. REMOVED FLOOR PANEL AT BS 1130. CUT OUT CORRODED AREA ON FLOORBEAM UPPER STA 1130 LBL 60. FABRICATED AND INSTALLED REPAIR 10.0" BY 2.0" BY 1.0" BY .30" FROM 7075-T6 .050, AND STRAP 13.0" BY 2.90" BY 1" BY .30" FROM 7075-T6 .063 AND FILLER 2.55" BY 1.2" FROM 7075-T6 .156 IAW B727 SRM 53-10-8 FIG 10 AND 51-30-2. 2L73 4F A3WE 20051026000242005102600024 2005 10 26 DL76L050646 420051023A34174040800911 COMPUTER BOEING767 767332 1382001NM ADC FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27196DN 28453 AT LEVEL OFF FL330 ALT DISAGREE EICAS LIGHT CAME ON. CAPT ALT READ 300 FEET DIFF FROM F/O ALT. AFTER DESCENT TO FL280 CAPT ALT READ 28010, F/O ALT READ 27760 STDBY READ 28350. PER FIM REPLACED F/O`S ADC AND CHECKS NORMAL. OPS OK PER M/M. ALSO REPLACED F/O`S ALT IND AS PRECAUTIONARY. 2L72 4F RTA1NM 20051026000262005102600026NM 2005 10 26 DL76L050648 120051023A3397 CONNECTOR BOEING767 767332 1382001NM EMERGENCY LGHT LOOSE A DALAK NONE O OTHER ININSP/MAINT 1 SO27189DN 25990 SEAT 38B EMERGENCY SEAT LIGHT INOP. RESEATED CONNECTOR AT SIDEWALL, OPS CHECK OK. 2L72 4F RTA1NM 20051026000282005102600028EA 2005 10 26 ASOA05744 120050907A335020131A BATTERY PACK CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT DISCHARGED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27753EV 10169 DURING A GROUND INSPECTION IN ATL, THE NR 2, 3 AND 4 EMERGENCY LIGHT BATTERY PACKS WERE FOUND DEAD. MAINTENANCE REMOVED AND REPLACED THE NR 2, 3 AND 4 EMERGENCY LIGHT BATTERY PACKS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051026000342005102600034EA 2005 10 26 ASOA05778 120050922A5310 BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27835AS 7258 DURING A C-CHECK IN MCN, THE CENTER BOX BEAM WAS SUSPECTED OF BEING CRACKED UNDER THE CLIP. MAINTENANCE WILL REPAIR THE CENTER BOX BEAM IAW ASA EO 600-53-0072B. (M) 2L72 4F RTA21EA 20051026000352005102600035EA 2005 10 26 ASOA05777 120050920A335020131A BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCHARGED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27825AS11516 7207 DURING A GROUND INSPECTION IN ATL, THE LEFT AND RIGHT EMERGENCY LIGHTS FORWARD OF THE CENTER EMERGENCY EXITS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 BATTERY PACK ASSEMBLY. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051026000442005102600044WP 2005 10 26 05FDEA03476 120051021A2750 FLAP SYSTEM DOUG DC10 DC1030 3023501WP TE FLAPS MALFUNCTIONED A FDEAO OTHER DF INFLIGHT SEPARATION FLT CONT AFFECTED DEDESCENT 1 SO25326FE 47813 UPON CONFIG, A/C ROLLED LEFT REQ 3/4 DEFLECTION TO RIGHT TO HOLD A/C LEVEL. A/C WAS CONTROLLABLE TO TOUCHDOWN. ON POST FLIGHT WALK AROUND, DISCOVERED THAT THE MIDDLE OF THE LEFT OUTBD FLAP VANE HAD DEPARTED THE A/C. REMOVED RT INBD FLAP SPRING CARTRIGDE. REMOVED AND REPLACED LT OB FLAP ASSY AND PERFORMED ADJUSTMENT/TEST IAW UAL DC10-30 MM 27-50-02. INSTALLED INBOARD AND OUTBOARD FLAP VANES ON LT OUTER FLAP, REF UAL M/M 27-50-03. INSTALLED LT OUTBOARD FLAP VANE CARTRIDGE, REF UAL M/M 27-51-04. REMOVED AND REPLACED NR 5 SPOILER PER UAL M/M27-60-01. REMOVED AND REPLACED NR 4 SPOILER PANEL PER M/M 27-60-01. 2L73 4F A22WE 20051026000482005102600048NM 2005 10 26 05FDEA03482 120051024A5315 FLOORBEAM BOEING727 7272S2F 1384O81NM BS 560 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25213FE 22935 MDCC - FLOORBEAM BS 560 LBL21 HAS CORROSION. REMOVED CORROSION IAW SRM 53-10-1MAT LOSS OF .001 ORIGINAL THICKNESS OF 0.230 FOUND TO BE WITHIN LIMITS IAW SRM 51-10-6 TREATED AND PRIMED IAW SRM 51-10-2. 2L73 4F A3WE 20051026000542005102600054NM 2005 10 26 05FDEA03478 120051021A5730 SKIN DOUG MD11 MD11 3023602NM RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 RT WING DROOP L/E UPPER SKIN FOUND WITH CRACK. RT WING DROOP L/E UPPER SKIN CRACK CARRIED OUT REPAIR AS PER SRM 57- 10-00 FIG.26 VOL.I. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051026000562005102600056NM 2005 10 26 05FDEA03479 120051022A5270 WARNING LIGHT BOEING727 727200 138407ENM AIRSTAIR DOOR FALSE ACTIVATIONA FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25203FE 22925 CLIMBING THROUGH 11,000 ON DEPARTURE, AFT AIRSTAIR ANNUNCIATOR ILLUMINATED ON ENGINEER'S PANEL. ACFT FLYING STABLE WITHOUT ANY INCREASED DRAG. AN EMERGENCY DECLARED DUE TO POSSIBILITY OF AIRSTAIRS STRIKING RUNWAY DURING TOUCHDOWN. AFT AIRSTAIR ILLUMINATED INFLT CHKLIST RUN & DIRECTED A LANDING AT NEAREST SUITABLE AIRPORT. DURING ROLLOUT LIGHT EXTINGUISHED & THEN FLICKERED JUST BEFORE COMING TO A STOP AT THE GATE. RELEASED FOR SERVICE PER MEL/CDL. 01NOV05 AMBER AFT AIRSTAIR DOOR WARNING LIGHT INOP. 2L73 4F RTA3WE 20051026000592005102600059EA 2005 10 26 VTZA200500213 120051019A27419960013 SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB TRIM FAULTY A VTZAO OTHER F FLT CONT AFFECTED CRCRUISE 1 EA27684BR 7708 STABILIZER TRIM/MACH TRIM CAUTION MESSAGE. FOUND PILOT STAB DISCONNECT SWITCH FAULTED. REMOVED AND REPLACED SWITCH. 2L72 4F RTA21EA 20051026000602005102600060EA 2005 10 26 VTZA200500214 120051022A2741 TRIM SYSTEM CNDAIRCL600 CL6002B19 1900309EA STABILIZER MALFUNCTIONED A VTZAO OTHER F FLT CONT AFFECTED CLCLIMB 1 EA27627BR 7233 STAB TRIM CAUTION AT 500 FT AGL ON ED1 WITH NO ELEVATOR TRIM UNTIL 15,000 FT. 2L72 4F RTA21EA 20051026000622005102600062NE 2005 10 26 SF20051023 220051023A7200 ENGINE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE LEFT SURGES A UHLAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 GL1714XS 340A014 FLIGHT 7591 IAD-PIT ABORTED TAKEOFF AT 100 KNOTS DUE TO LT ENGINE SURGING. DEFERRED CTOT, CONT OPS PER MEL 76-10-1, CONTROL 3150, CAT C, DDD 11/02/05. RTO INSPECTION DUE FOR ABORTED T/O AT 100 KNOTS. C/W RTO INSPECTION IAW M/M 05-50-00-6 PROCEDURE NR 3, NO DEFECTS NOTED AT THIS TIME. 2L72 4T4 TRTA52EU E8NE6 20051026000712005102600071EA 2005 10 26 A6WA200540311 120050928A2410 IDG CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 1 LACK OF LUBE A A6WAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL31427ZW 7685 IDG NR 1 CAUTION MESSAGE AT TAKEOFF THRUST ABORTED TAKEOFF BELOW 40 KNOTS BTMS INDICATES 3, 3, 4, 4 LIGHT BRAKING. NO HIGH ENERGY STOP INSPECTION REQUIRED IAW 05-51-27 P601. COMPLIED WITH (M) ACTION FOR MEL 24-11-01-01 PLACARDED. SERVICED IDG NR 1 WITH OIL IAW CRJ AMM, LEAK AND OPS CHECK GOOD. REMOVED FROM MEL. (K) 2L72 4F4 FRTA21EA E15NE 20051026000722005102600072EA 2005 10 26 COMA0570111 120051023A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA BS 364-394 CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01368CA7849 10075 SEVERAL MINOR NICKS AROUND THE CIRCUMFERENCE OF AVIONICS BAY DOOR CUTOUT. REPAIRED AVIONICS BAY DOOR CUTOUT IAW BRAS EO 601R-53-7495. 2L72 4F RTA21EA 20051026000752005102600075EA 2005 10 26 ASOA05774 120050919A5242H34455 HANDLE CNDAIRCL600 CL6002B19 1900309EA E/E BAY DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27841AS4428 7300 DURING A C-CHECK, THE AVIONICS BAY DOOR HANDLE WAS FOUND TO BE CRACKED. MAINTENANCE WILL REMOVE AND REPLACE THE AVIONICS BAY DOOR HANDLE. (M) 2L72 4F RTA21EA 20051026000772005102600077NM 2005 10 26 SWAA053314 120051023A53306545766 SKIN BOEING737 7373H4 1384600NM BS 518D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29374SW 26582 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 518D, STR 12R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051026000802005102600080NM 2005 10 26 SWAA053317 120051023A53206551698 SPLICE BOEING737 7373H4 1384600NM BS 359 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29374SW 26582 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STR SPLICE CRACKED AT BS 359, STR 14L. REPAIRED STR SPLICE PER SRM. 2L72 4F RTA16WE 20051026000812005102600081NM 2005 10 26 SWAA053318 120051023A575465C26686 SKIN BOEING737 7373H4 1384600NM NR 2 SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29639SW 27712 DURING SCHEDULED SPECIAL VISIT, FOUND NR 2 L/E SLAT LOWER SKIN CRACKED AT OUTBD END. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051026000872005102600087NM 2005 10 26 DHL2005742515 120050918A5347 SEAT TRACK BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE BS 878 GOUGED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15742DH 21290 S/O 284002 N/R 037550 SEAT TRACK GOUGED AT BS 878 LBL 45. REMOVED FLOOR PANELS AT BS 870 - 950 LBL 24 - 60 IAW SRM 51-30-2. REMOVED GOUGED SEAT TRACK. FABRICATED AND INSTALLED NEW SEAT TRACK 91.00 INCHES X 1.80 INCH FROM 7178-T6511 IAW SRM 53-10-1 FIG. 3 AND 51-30-2. 2L73 4F4 F A3WE E2EA 20051026000892005102600089NM 2005 10 26 DHL2005742512 120050916A5340 NUT PLATE BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE BS 1070-1130 MISINSTALLED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15742DH 21290 NUT PLATES IMPROPERLY INSTALLED ON FLOOR SUPPORT BETWEEN BS 1070 - BS 1130 STR. 30 (ABOVE) REMOVED DAMAGED FLOOR SUPPORT BETWEEN BS 1070 - 1130. CUT AND FABRICATED NEW SUPPORT 13INCHES FROM BAC1490-2583 AND SPLICES 12 INCHES X 1INCH X 1INCH FROM AND10133-0702 AND 89.5 INCHES X 1INCH X .8750 INCH FROM BAC1509-100146. DRILLED, TREATED AND PRIMED AND INSTALLED IAW SRM 53-10-5 FIG. 4 AND SRM 51-30-2. 2L73 4F4 F A3WE E2EA 20051026000912005102600091NM 2005 10 26 2005UALA01139 120051014A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE BS 700 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP297UA 25368 BS 700 CABIN FLOORBEAM UPPER CAP HAS DAMAGE. BS 700 LBL 25 FLOORBEAM UPPER CHORD SPLICE REPAIR ACP'D PER MM 53 00 98 825 DUE TO CRACK IN RADIUS. 2L72 4F4 FRTA2NM E17NE 20051026000932005102600093NM 2005 10 26 2005UALA01141 120051016A5310 FRAME BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU FWD GALLEY DOOR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29336UA 24240 FWD GALLEY DOOR AFT SIDE CLOSURE FRAME IS CRACKED AT 1EA FASTENER HOLE AT LOWER CORNER. REPAIR ACP'D TO CRACKED FRAME WITH SPLICE IN NEW FRAME SECTION PER SRM 51-40-02. 2L72 4F4 FRTA16WE E21EU 20051026000962005102600096 2005 10 26 XN0A1272 420051017A2312 RADIO AIRBUS300 A300B4203 3930306EU VHF SYSTEM INTERMITTENT A XN0AO OTHER O OTHER NRNOT REPORTED 1 GL23474AS 219 NR 1 & 2 VHF COMM INTERMITTENT. INSPECTED NR 1 VHF TRANSCEIVER & VHF COMM TRANSMITTER, FOUND NO DEFECTS. PERFORMED MANY RADIO CHECKS ON GROUND. SYSTEM OPS CHECK GOOD IAW A300 MM REF 23-00-00. DURING FURTHER TROUBLESHOOTING FOUND RADIO AMPLIFIER TO BE WORKING INTERMITTENTLY. REMOVED AND REPLACED AMPLIFIER AS REQUIRED. REMOVED AND REPLACED NR 2 VHF COMM TRANSCEIVER AS REQUIRED IAW A300 MM REF 23-00-00. OPS CHECK GOOD. REMOVED AND REPLACED RADIO AMPLIFIER AS REQUIRED IAW A300 MM REF 23-51-19. ALL VHF RADIOS, OPS CHECK GOOD ON GROUND. ALL VHF RADIOS, VHF NR 1, VHF NR 2 OPS CHECK GOOD ON GROUND IAW A300 MM REF 23-51-19. NO FURTHER DEFECTS AT THIS TIME. 2L72 4F RTA35EU 20051026001062005102600106NM 2005 10 26 2005UALA01152 120051015A2120 ODOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN DETECTED A UALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP29572UA 26682 ACRID ODOR AND SLIGHT AMOUNT OF SMOKE IN CABIN. SOURCE OF SMELL DETERMINED TO BE RIGHT AIR CONDITIONING PACK. RAN RIGHT PACK FOR 20 MINS PER MM 21-00-01. NO SMELL NOTED. RETURNED AIRCRAFT TO SERVICE. 2L72 4F4 FRTA2NM E17NE 20051026001082005102600108NM 2005 10 26 2005UALA01154 120051015A2150213N100115 LINE BOEING757 757222 1384956NM PWA 2037 PW2037 NE WATER SEPARATOR CRACKED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29522UA 24931 FLIGHT DIVERTED DUE TO CABIN ALTITUDE WARNING AND INABILITY TO MAINTAIN CABIN PRESSURE. ORD FOUND RIGHT AIR CONDITIONING PACK WATER SEPARATOR DRAIN LINES CRACKED. REPLACED PART NUMBERS 213N1001-16 AND 213N1001-15. RETURNED AIRCRAFT TO SERVICE. NOTE: THIS SAME PROBLEM OCCURRED ON 10/16/2005 (NEXT DAY) AND DETAILS ARE ON SDR 2005UALA01150. 2L72 4F4 FRTA2NM E17NE 20051024000862005102400086 2005 10 24 YENA200575 420051008A2565D5211053100000 GIRT BAR AIRBUS320 A320232 3930326EU ESCAPE SLIDE INOPERATIVE A YENAK NONE O OTHER ININSP/MAINT 1 EA15527JB 1557 DURING C-4 CHECK WHILE PERFORMING INSPECTION, FOUND L1 MED GIRT BAR SLIDE INOPERABLE. REPLACED GIRT BAR ASSY PER JETBLUE AND AIRBUS AMM. 2L72 4F RTA28NM 20051024000872005102400087 2005 10 24 YENA200574 420051008A2565D5211053100100 GIRT BAR AIRBUS320 A320232 3930326EU ESCAPE SLIDE DEFECTIVE A YENAK NONE O OTHER ININSP/MAINT 1 EA15527JB 1557 DURING C-4 CHECK WHILE PERFORMING INSPECTION, FOUND R2 MED GIRT BAR SLIDE INOPERABLE. REPLACED R2 GIRT BAR ASSY PER JETBLUE AND AIRBUS AMM. 2L72 4F RTA28NM 20051024000892005102400089NM 2005 10 24 AWXA200501248 120051011A532065468097 INTERCOSTAL BOEING737 7373S3 1384711NM BS 927 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 MCN - MAJOR REPAIR - DURING C18 CHECK DISCOVERED INTERCOSTAL ANGLE CRACKED, .75 INCHES, AT BS 927, BL 0 AND WL 208. MAINTENANCE REMOVED ATTACH ANGLE AND FABRICATED ATTACH ANGLE IAW BOEING 737-300 SRM 51-40-02-0G AND DWG 65-46809. INSTALLED FABRICATED REPAIR PARTS AT BS 927, WL 208 AND BL 0 IAW BOEING 737-300 SRM 51-40-02-0G FIGS 3, 4, 6, 7, AND 8. 2L72 4F RTA16WE 20051024000922005102400092NM 2005 10 24 AWXA200501251 120051009A57536546431279 SKIN BOEING737 7373G7 1384595NM FOREFLAP DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - DURING C16 CHECK DISCOVERED DISBOND AREA AT AFT EDGE OF LT OUTBOARD FORE FLAP, 72-76 INCHES FROM INBOARD END. MAINTENANCE REMOVED DISBOND AREA ON THE LT OUTBOARD FOREFLAP IAW BOEING 737-300 SRM 51-70-10-2R. FABRICATED FILLER AND DOUBLER IAW BOEING 737-300 SRM 51-70-10-2R. INSTALLED FABRICATED REPAIR PARTS ON THE LT OUTBOARD FORE FLAP IAW BOEING 737-300 SRM 51-70-10-2R FIG 8. 2L72 4F RTA16WE 20051024001012005102400101NM 2005 10 24 QXEA200501355 120051016A3260401020101 PROXIMITY SENSOR BOMBDRDHC8 DHC8402 1390042NM LT MLG MALFUNCTIONED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09411QX 4055 GEG FLIGHT NR 2393: MAIN GEAR DOORS AND GEAR IN TRANSIT CAME ON A FEW SECONDS THEN WENT OUT. DID THIS SEVERAL TIMES. MAINTENANCE PERFORMED INSP OF THE A/C AND ENGINES AS REQUIRED BY PARA C OF THE FERRY FLIGHT PERMIT AND DETERMINED THAT THE A/C IS SAFE FOR FLIGHT FROM GEG TO PDX. IN PDX , MAINTENANCE REPLACED THE LT MLG DOOR CLOSED PROX SENSOR. PERFORMED OPERATIONAL CHECK OF PRIMARY GEAR EXTENSION RETRACTION SYSTEM IAW AMM TASK 32-31-00-710-801. OPS CHECK GOOD. A/C RETURNED TO SERVICE 2H72 4T RTA13NM 20051024001032005102400103NE 2005 10 24 DL76L050590 220051003A7261PW40603 ENGINE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 1 LEAKING A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO27194DN32564 28451 727650 LEFT ENGINE LOSING OIL AT THE RATE OF 1 - 2 QTS/HOUR. CURRENTLY AT 4 QTS GOT DOWN TO 0 - 1 QTS AND ELECTED TO DIVERT TO LGW. REPLACED ENGINE. 2L72 4F4 FRTA1NM E24NE 20051024001052005102400105NM 2005 10 24 DLM90050592 120051004A2910000AE9080200 HOSE DOUG MD90 MD9030 3023690NM HYD SYSTEM LEAKING A DALAL ABORTED APPROACH KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SO27909DA 53389 ON APPROACH LOST ALL RIGHT SIDE HYDRAULIC QUANTITY. REPLACED LEAKING RT ENGINE PUMP PRESSURE LINE. 2L72 4F RTA6WE 20051024001152005102400115EA 2005 10 24 MASA200500777 120051007A5270 PROXIMITY SENSOR CNDAIRCL600 CL6002D24 1390016EA E/E BAY DOOR DIRTY A MASAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SW07905J 15005 ASH 6438 PHX - AVIONICS BAY DOOR OPEN INDICATION ON TAKEOFF. CLEANED PROX SENSORS. 2L72 4F RTA21EA 20051024001192005102400119EA 2005 10 24 MASA200500750 120050925A2150GG670950093 ACM CNDAIRCL600 CL6002D24 1390016EA LEFT SMOKE A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW07907FJ132 132 15007 ASH 6029 LAS - LT PACK AUTO FAIL CREATED SMOKE AND FUMES IN CABIN. MAINTENANCE REPLACED ACM. 2L72 4F RTA21EA 20051024001272005102400127NM 2005 10 24 DL73S050607 120051011A53126546568571 BULKHEAD BOEING737 737247 138448DNM BS 1016 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27245WA 23519 WHILE ACCOMPLISHING BOEING RECOMMENDED REWORK TO AN AFT PRESSURE BULKHEAD REDIAL STIFFENER REPAIR INSTALLED PER ER/A 089941-14AD, SEVERAL ELONGATED AND OVERSIZED HOLES WERE FOUND IN THE WEB AND STIFFENER. DAMAGE ALSO OCCURRED TO THE PAN DURING REWORK. INSTALLED DOUBLER REPAIR PER ER/A 450872-14AD. 2L72 4F A16WE 20051024001282005102400128NM 2005 10 24 DL73S050608 120051005A53306545767103 SKIN BOEING737 737247 138448DNM BS 525 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27376DL 23603 A CRACK WAS FOUND IN THE FUSELAGE SKIN AS A RESULT OF INSPECTION PER DAL OPN 57546. THE CRACK IS APPROX 1.5 INCH LONG AT BS 525 ABOVE STRINGER 16L. INSTALLED DOUBLER REPAIR PER B737-200 SRM 53-30-3, FIG 48, DETAIL XI AND ER/A 450994-14AD. 2L72 4F A16WE 20051024001332005102400133WP 2005 10 24 UPS05845616 120051018A33505708458503 BATTERY PACK DOUG DC8 DC871F 302199DWP EMERGENCY LIGHT DISCHARGED A IPXAO OTHER L NO TEST NRNOT REPORTED 1 SO01752UP 45952 EMERGENCY BATTERY INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK. OPS CK GOOD IAW MM 33-10. 2L74 4F RT4A25 20051024001352005102400135WP 2005 10 24 UPS05845619 120051005A5340 FITTING DOUG DC8 DC873F 302199FWP BS 210 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 A-BAG BIN, L28L SPLICE FITTING CRACKED STA 210. REMOVED CRACKED SPLICE FITTING AT STA 210 L28L IAW SRM 51-1-20D. FABRICATED AND INSTALLED LONGERON SPLICE FITTING AT STA 210 L28L IAW DWG 4653726 ANG SRM 51-3-2, AND SRM 51-1-20D. 2L74 4F RT4A25 20051024001422005102400142WP 2005 10 24 ASMF200510009 120051016A322239567851 LINK DOUG DC9 DC983 3022083WP NLG DOOR FAILED W ASMFA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SW23838AM2166820384 49397 AIRCRAFT RETURNED OF FLIGHT AS A CONSEQUENCE OF STRONG VIBRATION IN THE NOSE LANDING GEAR. AIRCRAFT WAS SENT TO THE HANGAR AND DURING MAINTENANCE REVISION, IT WAS DETECTED THAT THE NOSE LANDING GEAR DOOR DID NOT RISE. THE NOSE LANDING GEAR DOOR LINKS WERE REPLACED IAW MM 32-22-01 AND NOSE LANDING GEAR DOOR TRIM WAS PERFORMED IAW MM 32-22-01, TESTED CORRECT. THE OVERWEIGHT LANDING INSPECTION WAS PERFORMED IAW MM 05-50-00. DURING OVERNIGHT CHECK, THE NOSE LANDING GEAR WAS TESTED IAW MM 32-22-00, BEING CORRECT. 2L72 4F RTA6WE 20051024001432005102400143EA 2005 10 24 VNAA0509014 120050928A2750 FCU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A VNAAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL05254PS 7935 THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED ON APPROACH WITH THE FLAPS AT 20 DEGREES. THE CREW FOLLOWED THE QRH AND LANDED SAFELY. MAINTENANCE CLEARED CODES FROM THE FECU AND RESET THE SYSTEM IAW CRJ200 FIM 27-50-00. THE FLAP SYSTEM OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20051024001442005102400144CE 2005 10 24 ACE091905 120050919A28221333890311 DIAPHRAGM ROMEC RG37060AM BEECH 1900 1900C 1154161CE NR 1 FUEL PUMP RUPTURED E YADAD RETURN TO BLOCK K FLUID LOSS TXTAXI/GRND HDL 1 AL03114AX 672 B1012 UC36 PIREP - FUEL OBSERVED DRIPPING FROM NR 1 ENGINE DRAIN MAST. VERIFIED LOW PSI FUEL PUMP DIAPHRAGM RUPTURE, THIS UNIT WAS IN COMPLIANCE WITH THE LATEST SB FOR DIAPHRAGM DESIGN. 2L72 4T RTA24CE 20051024001622005102400162NM 2005 10 24 AWXA200501224 120051014A3397BMS13311122 WIRE BOEING737 7373G7 1384595NM EMERGENCY LIGHT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 PHX - EEL - DURING OVERNIGHT INSPECTION DISCOVERED THE EMERGENCY EXIT PATH LIGHT AT ROW 10 LEFT WAS INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRES UNDER ROW 10 LEFT. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20051024001652005102400165EU 2005 10 24 AWXA200501227 120051015A3397E0261CF20 WIRE AIRBUS320 A320232 3930326EU EMERGENCY LIGHT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28649AW 803 PHX - EEL - DURING OVERNIGHT INSPECTION DISCOVERED EMERGENCY EXIT LIGHT AT ROW 7 LEFT INOPERATIVE. MAINTENANCE FOUND WIRES BROKEN UNDER ROW 7 LEFT. SPLICED WIRES TOGETHER, OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA28NM 20051024001902005102400190 2005 10 24 DL76G050623 420051016A34144039891906 INDICATOR BOEING767 767332 1382001NM AIRSPEED FAILED A DALAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 SO271605 30198 ABORTED TAKEOFF AT 100 KTS, DUE TO CAPTS AIRSPEED IND SHOWING 0 AND RED INOP FLAG A/SPD IND STARTED TO WORK AS SOON AS ABORT INITIATED. WORKED OK DURING DECEL ON RUNWAY. REMOVED AND REPLACED CAPT AIRSPEED IND, TESTS OPS NORMAL. 2L72 4F RTA1NM 20051024002062005102400206NM 2005 10 24 DHL2005742509 120051003A5315 FLOORBEAM BOEING727 727225 1384077NM BS 1070 CORRODED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15742DH 21290 AFT PIT CEILING, CABIN FLOORBEAM BS 1070 LOWER SURFACE HAS CORROSION AT RBL 16. REMOVED CORRODED FLOORBEAM STA 1070 RBL 16 IAW B727 SRM 53-10-8. FABRICATED 2 EACH ANGLES 18 X .9 X .8 INCHES AND 12 X .8 X 1.2 INCHES FROM BAC 1490-2888 AND 1 EACH FILLER FROM 7075-T6 .125 IW B727 SRM 53-10-8 AND 51-30-2. 2L73 4F A3WE 20051024002072005102400207NM 2005 10 24 DHL2005742510 120051004A5320 WEB BOEING727 727225 1384077NM BS 354 CORRODED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15742DH 21290 CLOSE OUT WEB LEFT AT STA 354 S-15 - 17L HAS ELONGATED HOLES, GOUGES AND EXFOLIATED CORROSION. REMOVED WEB, FABRICATED AND INSTALLED SHEAR WEB 15 X 4.2 INCHES FROM 7075-T6 .040 SRM 51-40-2, 51-20-1 AND 51-10-2. 2L73 4F A3WE 20051025000012005102500001EA 2005 10 25 SWIA200515709 120051018A274170609 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07418SW5108 5108 7446 STAB CH1 INOP STATUS MSG. ON ED2 CAME UP TWICE DURING CRUISE FLIGHT. REPLACED HSTCU, NR 1 SLATS ENGAGE SWITCH AND STAB TRIM CONTROL PANEL REF AMM 27-41-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051025000112005102500011 2005 10 25 SWAA053271 420051020A2565416A2100 COVER BOEING737 7377H4 1384404NM L2 DOOR SLIDE LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29745SW 29491 L2 DOOR EVACUATION SLIDE CONTAINER ATTACH FASTENER LOOSE. SECURED FASTENER PER MM. 2L72 4F RTA16WE 20051025000132005102500013NM 2005 10 25 SWAA053273 120051020A3350BR2013 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29436WN 32456 EEPLS COVER LOOSE AT ROW 1. REPAIRED COVER PER MM. 2L72 4F RTA16WE 20051025000242005102500024NE 2005 10 25 UPS05545634 220051019A7200 ENGINE BOEING757 75724APF 1384969NM RROYCERB211 RB211535E4 54555NE NR 2 MALFUNCTIONED A IPXAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SO01445UP 27390 AFTER T/O RT ENG EGT STARTED TO RISE RAPIDLY. ENG EXCEEDANCES RT EGT 879, N2 101, N3 99. RT ENG EEC AND LIMITER EICAS MSGS. APPROACHING FINAL TO LAND AT IDLE THRUST NI A RT TURN. RT ENG FLAMED OUT. EGT 879 FOR 21 SEC N2 101.4 21 SEC N3 99.7 FOR 21 SEC DM 0557649 0558594 ENTERED IN ERROR. REMOVED AND REPLACED RT ENG EEC PER MM 73-21-07-4. EEC BT CK PER 73-21-00-L CK NORM, NO FAULTS. REMOVED AND REPLACED GEN ROTOR AND STATOR IAW MM 73-21-08-4. C/W TEST 2-13 MM 71-00-00-5, CKS NORM AND BUCU BTS NORM. REMOVED AND REPLACED RT BLEED VALVE CONTROL UNIT PER MM. COMPLIED WITH BUCU BT AFTER ENG RUN PER MM 75-32-00-2, CKS NORM. REMOVED AND REPLACED UPPER/LWR DGC PER MM. C/W TEST 3 IN MM. NO FAULTS. 2L72 4F4 FRTA2NM E12EU 20051025000252005102500025WP 2005 10 25 UPS05845631 120051005A53403755854502N FITTING DOUG DC8 DC873F 302199FWP BS 1180 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 C-PIT STA 1180 L26L BANANA FITTING CRACKED. REMOVED AND INSTALLED NEW BANANA FITTING AT STA 1180 L26L IAW SRM 51-3-2 AND SRM 51-1-20D. 2L74 4F RT4A25 20051025000282005102500028SO 2005 10 25 LR7A05114 120051020A534034258111 FITTING LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FS 858 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03405LC 595 5025 DURING PREFLIGHT CHECK FOUND LT SIDE STRUCTURE STRUT BRACE AT FS 858 LOWER ATTACH BRACKET CRACKED. REPLACED ATTACH BRACKET IAW SRM SMP 583 51-10 PG. 3(G) AND 51-70. LP 16393, ITEM M1. 2H74 4T4 T A1SO E282 20051025000292005102500029EU 2005 10 25 YENA200576 120051020A3350321431 BATTERY PACK AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE EMERGENCY LIGHT DISCHARGED A YENAK NONE L NO TEST ININSP/MAINT 1 EA15503JB317 317 1123 DURING EMERGENCY LIGHT SYSTEM TEST. EPSU EMER. L DISPLAYED. REMOVED AND REPLACED EPSU (11WL) BATTERY PACK IAW AMM 33-51-38. SYSTEM OPS CHECK GOOD. 2L72 4F4 FRTA28NM E40NE 20051025000302005102500030SO 2005 10 25 AALA20050694 120051010A3350 LIGHT LUSCOM8 8A 8190104SO EXTERIOR INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2128485 1352 DFW - DURING OVERNIGHT MAINTENANCE FOUND L3 DOOR EMERGENCY ESCAPE EXTERIOR LIGHT INOPERATIVE. REPLACED L3 DOOR EXTERIOR EMERGENCY SPOT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 1H71 3O A694 20051025000322005102500032WP 2005 10 25 AALA20050692 120051019A2150 MANIFOLD DOUG DC9 DC982 3022082WP A/C PACK DEFECTIVE A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW2177421 49333 JAX - AFTER TAKEOFF SMOKE IN CABIN. TURNED OFF PACK DURING APPROACH AND SMOKE DISSIPATED. LANDED JAX NO INCIDENT. REPLACED ELEVATOR POWER MANIFOLD AND COALESCER BAGS. CONDUCTED PACK BURN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051025000532005102500053WP 2005 10 25 UPS05845640 120051011A5340 ANGLE DOUG DC8 DC873F 302199FWP BS 1190 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 C-PIT AT STA 1190 RBL 39 L-ANGLE HAS INTERGRANULAR CORROSION. REMOVED ANGLE IAW SRM 51-1-20D, FABRICATED AND INSTALLED ANGLE AT STA 1190 RBL 39 IAW DWG 5711283, SAA SK 866-833103, UPS EO FILE NUMBER DC8-53-20512, AND BOEING MESSAGE NR 1-134429123-2 DATED 10-18-2005. 2L74 4F RT4A25 20051025000552005102500055NM 2005 10 25 UPS05M45629 120050831A5347S4929147 SEAT TRACK DOUG MD11 MD11F 3023600NM BS 865-887 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01280UP 48634 MAIN DECK MID-ENTRY AREA, SEAT TRACK ALONG RBL 27.5, CORROSION FOUND ON CROWN, BETWEEN STA 865 AND STA 887. MID ENTRY SEAT TRACK BET STA 865 AND 887 CROWN REMOVED SRM5 3-70-00 FIG 3 VOL I REV 37, MAT THK 0.145 INCH AND MAT REMOVED 0.035" EXCEED LIMIT 53-70-00. SEAT TRACK FASTENERS REMOVED AND SPLICE CUT BET STA 832 AND 909. HFEC INSP SATISFACTORY. REPAIR SPLICE PLATE FAB SRM 53-70-00, HOLES PICK-UP, REPROTECTED AND PAINTED. SEAT TRACK EXTRUSION INSTALLED BETWEEN STA 832 TO 909, SRM 51-31-01. 2L73 4F RTA22WE 20051025001282005102500128EA 2005 10 25 ASOA05786 120051021A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE BS 280 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27835AS 7258 DURING A C-CHECK IN MCN, THE FS 280 INTERCOSTAL, AT RBL 9, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACE THE FS 280 INTERCOSTAL, AT RBL 9, IAW REO 601R-53-11-638. (M) 2L72 4F4 FRTA21EA E15NE 20051025001302005102500130EA 2005 10 25 ASOA05751 120050831A5712 RIB CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT WING CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27834AS 7254 DURING A C-CHECK IN MCN, THE RIGHT WHEEL WELL BATT RIB ASSY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RIGHT WHEEL WELL BATT RIB ASSY AT WS 53.60 IAW ASA EO 600-57-039A. (M) 2L72 4F4 FRTA21EA E15NE 20051025001432005102500143EU 2005 10 25 F3LA200500043 120051003A3244315311 TIRE AIRBUSA319 A319112 3930323EU MLG FAILED A F3LAO OTHER O OTHER LDLANDING 1 NM03901FR 1488 ON LANDING, BOTH NOSE TIRES BLEW. STOPPED ACFT ON RUNWAY. PERFORMED INSPECTION AFTER TIRE BURST. NO DAMAGE NOTED. REPLACED LT NOSE WHEEL & TIRE ASSEMBLY, P/N 3-1531-1, S/N 4964, TSI 690.80 &CSI 285 SINCE REPAIR, RT NOSE WHEEL & TIRE ASSEMBLY, P/N 3-1531-1, S/N 7017, TSI 690.8 & CSI 285 SINCE OVERHAUL, MOVED AIRCRAFT FROM RUNWAY. PERFORMED INSPECTION OF AXLE SLEEVES, NO DAMAGE NOTED. REPLACED LOWER TORSION LINK, P/N GA65227. DUE TO DAMAGE SUSTAINED FROM JACKING NOSE GEAR, PERFORMED INSPECTION AND OPERATIONAL CHECK OF NLG. NLG SLIDING TUBE LUG FOUND TO BE DAMAGED. REPLACED NLG SHOCK ABSORBER ASSY, P/N D23592020-1, S/N L1665, PERFORMED A HEAVY CHECK. PERFORMED GEAR SWING, ALL INDICATIONS NORMAL. 2L72 4F RTA28NM 20051025001772005102500177WP 2005 10 25 05FDEA03216 120051005A5712 RIB DOUG DC10 DC1010 3022110WP ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE LT WING FIXED L/E COMPT AT STA XORS 761 ZONE 525 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 4 AND 6 VOL I. 2L73 4F A22WE 20051025001862005102500186EU 2005 10 25 0501483274 120051001A21332079003AC OUTFLOW VALVE AIRBUS320 A320212 3930322EU CABIN PRESSURE MALFUNCTIONED A NWAAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 GL01374NW 1646 AT CRUISE ALTITUDE OF 37,000 FEET RECEIVED A CAB PR SYS 1 FAULT. MOMENTS LATER RECEIVED CAB PR 1 & 2 FAULT. REQUESTED IMMEDIATE DESCENT WITH ATC. CABIN PRESSURE WAS HOLDING STEADY AT 7,000 FEET. REPORTED TO ATC THAT CABIN PRESSURE WAS HOLDING AND RECEIVED CLEARANCE TO LEVEL AT 19,000 FEET. NO EMERGENCY WAS DECLARED, CABIN O2 MASKS DID NOT DEPLOY. UNEVENTFUL LANDING. REMOVED AND REPLACED OUTFLOW VALVE 32-2130-9-0009, S/N OFF 91680. 2L72 4F RTA28NM 20051025001912005102500191WP 2005 10 25 05FDEA03221 120051005A5712 RIB DOUG DC10 DC1010 3022110WP ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE LT WING FIXED L/E COMPT AT STA XORS 933 ZONE 527 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET3 AND 4 VOL I. 2L73 4F A22WE 20051025001932005102500193WP 2005 10 25 05FDEA03223 120051005A5712 RIB DOUG DC10 DC1010 3022110WP RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE RT WING FIXED L/E COMPT AT STA XORS 690 ZONE 625 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 1, 3 AND 4 VOL I, INSTALL REPAIR ANGLE -36. 2L73 4F A22WE 20051025001952005102500195WP 2005 10 25 05FDEA03225 120051005A5712 RIB DOUG DC10 DC1010 3022110WP RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE RT WING FIXED L/E COMPT AT STA XORS 917 ZONE 627 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 1, 3 AND 5 VOL I. INSTALL REPAIR ANGLE -36. 2L73 4F A22WE 20051025001972005102500197WP 2005 10 25 05FDEA03227 120051005A5712 RIB DOUG DC10 DC1010 3022110WP ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 THE RIGHT WING FIXED L/E COMPT AT STA XORS 514 ZONE 619 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 3 AND 4 VOL I, INSTALL REPAIR ANGLE -36. 2L73 4F A22WE 20051025001982005102500198WP 2005 10 25 0501501237 120051002A3397 WIRE DOUG DC10 DC1030 3023501WP EMERGENCY LIGHT BROKEN A NWAAK NONE O OTHER ININSP/MAINT 1 GL01237NW 47844 DURING LINE CHECK MAINTENANCE FOUND SEAT EMERGENCY LIGHTS INOP 10AB - 20AB. FOUND BROKEN WIRE UNDER SEAT 20AB. REPAIRED WIRE AND OPERATION CHECKS GOOD. 2L73 4F A22WE 20051026000012005102600001EA 2005 10 26 ASOA05762 120050917A5712 RIB CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27841AS 7300 DURING A C-CHECK IN MCN, THE LEFT BATT RIB ASSEMBLY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LEFT BATT RIB ASSEMBLY AT WS 53.60 IAW ASA EO 600-57-0039B. (M) 2L72 4F RTA21EA 20051026000202005102600020 2005 10 26 DL76G050641 420051020A344220414440401 ANTENNA BOEING767 7673P6 1385105NM WX RADAR SYS FAILED A DALAA UNSCHED LANDING O OTHER CRCRUISE 1 SO27156DL 4176 25354 WXR RADAR INOP ANTENNA FAULT MESSAGE RIGHT HALF DISPLAY BLANK WITH NO WXR. REMOVED AND REPLACED WXR ANTENNA ASY IAW M/M OPS CHECKS GOOD. 2L72 4F RTA1NM 20051026000212005102600021NM 2005 10 26 DL757050642 120051022A2120 ODOR BOEING757 757232 1384965NM CABIN DETECTED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27674DL 25979 BRIEF ELECTRICAL BURNING SMELL NOTED BY FLT ATTENDANT AND PASSENGERS APPROX ROWS 28-32. DURING FLIGHT SMELL DISSIPATED THEN RETURNED ON DESCENT. MTC IN SJO OPENED AND CHECKED ALL PSU FROM ROW 20-39, FOUND NORMAL CONDITIONS. OPERATED BOTH A/C PACKS AND RECIRCULATION FANS WITH DOORS CLOSED FOR ONE HOUR, NO SMELL DETECTED. RAN BOTH ENGINES AND OPERATED ALL CABIN ELECTRICAL SYSTEMS COULD NOT DUPLICATE SMELL. 2L72 4F RTA2NM 20051026000232005102600023NM 2005 10 26 DL738050645 120051022A3350D71701100 BATTERY PACK BOEING737 737800* NM BS 322 INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27383DN 30346 FOUND F/C EMERGENCY LIGHTS DO NOT ILLUMINATE. T/S SYSTEM AND REPLACED BATTERY PACK M1674, OPS CHECK GOOD. 2L72 4F RTA16WE 20051026000252005102600025 2005 10 26 DL76G050647 420051023A2565H2052K3833 LATCH BOEING767 7673P6 1385105NM LT OFFWING SLIDEFAILED A DALAK NONE O OTHER ININSP/MAINT 1 SO27153DL 24985 DURING LEFT WING SLIDE REPLACEMENT FOUND DOOR LATCH NR 3 BROKEN. REMOVED AND REPLACED LEFT OFFWING SLIDE COMPARTMENT DOOR LATCH NR 3 PER AMM. 2L72 4F RTA1NM 20051026000632005102600063EA 2005 10 26 ASOA05796 120050923A5340 NUT PLATE CNDAIRCL600 CL6002B19 1900309EA BS 559 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27835AS 7258 DURING A C-CHECK IN MCN, CORROSION WAS FOUND ON THE CARGO SILL NUT PLATE AFT OF THE LAVATORY AT FS 559 +80 RT. MAINTENANCE REMOVED AND REPLACED CORRODED NUT PLATES ON CARGO SILL RT SIDE AFT OF LAV 559+80 IAW SRM 51-00-00 (CLOSED) 2L72 4F RTA21EA 20051026000652005102600065EA 2005 10 26 ASOA05793 120050923A5340 STRINGER CLIP CNDAIRCL600 CL6002B19 1900309EA BS 339 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27835AS 7258 DURING A C-CHECK IN MCN, A POSSIBLE CRACK IN THE CLIP AT FS 339, STRINGER 15 RIGHT JUST ABOVE THE SEAT TRACK WAS FOUND. MAINTENANCE PERFORMED AN EDDY CURRENT INSPECTION OF CLIP AT FS 339.00, STRINGER 15 RT. NO DEFECTS WERE NOTED. (M) 2L72 4F RTA21EA 20051026000822005102600082NM 2005 10 26 DL738050649 120051022A5330 SKIN BOEING737 737800* NM BS 365-382 PUNCTURED A DALAK NONE O OTHER ININSP/MAINT 1 SO27381DA 30350 THE FUSELAGE SKIN WAS STRUCK BY GROUND EQUIPMENT BETWEEN FS 365 & 382, JUST ABOVE STRINGER 24R. THE DAMAGE TO THE SKIN WAS REMOVED WITH A 20 X 6 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 451256-14, REV A. 2L72 4F RTA16WE 20051026000882005102600088NM 2005 10 26 DHL2005742516 120050917A5311 FRAME BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE BS 1070 CORRODED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15742DH 21290 BS 1070 LBL 65 WL 255 FRAME JUST AFT OF L-2 DOOR HAS A CORROSION BULGE. CUT OUT CORROSION ON FORMED WEB ANGLE ATTACHED TO FRAME AT BS 1070 LBL 65 AFT DOOR CUT OUT AT L-2 DOOR IAW SRM 51-40-3 FIG. 1. REMOVED (T) ANGLE, FABRICATED AND INSTALLED NEW ANGLE 2.75 INCHES X 3 INCHES X 2 INCHES X 1.6 INCHES FROM 7075-T6 .125 EXTRUSION AND FORMED SECTION 12.5 INCHES X 1.5INCHES FROM 7075-T6 .090 IAW AND 51-40-3 FIG. 1, 51-30-2 AND 51-30-5. 2L73 4F4 F A3WE E2EA 20051026000952005102600095EU 2005 10 26 2005UALA01143 120051015A3350 LIGHT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE ROW 20 ABC INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29405UA 452 EMERGENCY LIGHT AT SEAT ROW 20 ABC INOPERATIVE. REPLACED HARNESS. 2L72 4F4 FRTA28NM E40NE 20051026001002005102600100NM 2005 10 26 2005UALA01146 120051015A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29177UA 24384 EEL AT 5A AFT AND 2A AFT INOP. 2L74 4F4 FRTA20WE E24NE 20051026001112005102600111NM 2005 10 26 2005UALA01156 120051017A5230 ATTACH ANGLE BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FWD CARGO DOOR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29643UA 25093 FWD CARGO DOOR SILL ATTACHING ANGLE HAS A CRACK AT BS 610. 2L72 4F4 FRTA1NM E24NE 20051026001132005102600113NM 2005 10 26 2005UALA01158 120051017A5347 SEAT TRACK BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE GALLEY CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29643UA 25093 CABIN SEAT TRACK AT GALLEY 4A FWD ATTACH POINT IS CRACKED, OUTBOARD SEAT TRACK. 2L72 4F4 FRTA1NM E24NE 20051026001172005102600117EA 2005 10 26 REXA200500133 120051017A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A REXAO OTHER J WARNING INDICATION APAPPROACH 1 SO258936A 7936 FLAPS FAILED ON APPROACH, FOLLOWED QRH WITH UNEVENTFUL LANDING. SYSTEM RESET AND PLACED ON 72 HOUR MONITOR PER AD 98-20-01. 2L72 4F RTA21EA 20051026001182005102600118NM 2005 10 26 05FDEA03452 120051019A5330 SKIN BOEING727 727200 138407ENM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25265FE 21671 FORWARD PIT SKIN CORRODED AT BS 720D BETWEEN STRINGERS 26L AND 27L. REMOVED, FABRICATED, ALODINED, PRIMED, PAINTED AND INSTALLED REPAIR TO FUSELAGE SKIN AT STA 720D BETWEEN STRINGERS 26L AND 27L ALL IAW FX B727 SRM 53-30-3, 53-20-2 FIG 2, 51-30-2, 51-33-2, 51-20-13-7, 51-10-2 AND 51-10-1. 2L73 4F RTA3WE 20051026001222005102600122 2005 10 26 Z1RA106192 420050926A22107690001821103 TRANSDUCER SKRSKYS76 S76C 8143008NE TMECA ARRIUSARRIUS2B1 NE AUTOPILOT INTERMITTENT E Z1RAK NONE O OTHER ININSP/MAINT 1 SW11761AF2867 760524 DURING FLIGHT AL-300 DISPLAYS 1E30 CODE INTERMITTENTLY. 1G72 3U3 UNCH1NE E34NE 20051026002252005102600225NM 2005 10 26 05FDEA03445 120051018A5315 FLOORBEAM DOUG MD11 MD11 3023602NM BS 1801 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 AFT INTERMEDIATE FUSELAGE, FLOORBEAM LOWER CAP FOUND CRACK AT STA 1801 LBL 8 TO RBL 8. REPAIRED AS PER EA 1-5310-87655. CLASSIFIED MAJOR REPAIR PER GMM 6-2-100. 2L73 4F RTA22WE 20051026002262005102600226NE 2005 10 26 05FDEA03446 220051013A7261 ENGINE AIRBUS310 A310203 3930313EU GE CF6 CF680A3 30025NE NR 2 LEAKING A FDEAEBA ENGINE SHUTDOWN EMER. DESCENT UNSCHED LANDING KRJFLUID LOSS PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 SO25431FE29071 316 DURING CRUISE, NR 2 ENGINE TRIM LIGHT/ECAM ILLUMINATED NR 2 ENGINE, NOTICED N1 AND N2 INOP, OIL QUANTITY ZERO, OIL PRESSURE IN YELLOW, 14 PSI. ECAM ALERT FOR ENGINE SHUTDOWN, OIL PRESSURE ZERO. FLIGHT TIME ON ONE ENGINE -2 5 MINUTES. HYD LOW PRESS LIGHTS AND SPOILER FAULT LIGHTS DID NOT ILLUMINATE, ALTHOUGH ENGINE SYSTEM PAGE ON ECAM SHOWED ZERO OIL PRESSURE. REMOVED AND REPLACED NR 2 ENG PER ENG CHANGE WORK CARDS. 2L72 4F4 FRTA35EU E13NE 20051026002272005102600227NM 2005 10 26 05FDEA03447 120051018A5310 BEAM BOEING727 7272S2F 1384O81NM BS 500 DAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25211FE 22933 COMPLY WITH EA 7-5230-92344, DOORS, MAIN CARGO DOOR LOWER BEAM REPAIR AT BS 500.0. COMPLIED WITH EA 7-5230-92344 DOORS, MAIN CARGO DOOR LOWER BEAM REPAIR AT BS 500. 2L73 4F A3WE 20051026002282005102600228NM 2005 10 26 2005UALA01084 120051006A5210 BEAM BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29120UA 29166 NR 5R MAIN ENTRY DOOR UPPER GATE CLOSURE BEAM CRACKED AT ATTACH HOLE. NR 5R MAIN ENTRY DOOR UPPER GATE CLOSURE BEAM WAS FOUND CRACKED AT ATTACH HOLE. CRACK WAS PROBABLY CAUSED BY FATIGUE. ANGLE REPAIR WAS INSTALLED REFERENCING SM-80-52-10-08-JD AND SRM 51-70-11. 2L74 4F4 FRTA20WE E24NE 20051026002302005102600230NM 2005 10 26 2005UALA01086 120051006A5210 BEAM BOEING747 747422 1384935NM PWA 4056 PW4056 NE PAX DOOR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29120UA 29166 NR 5L MAIN ENTRY DOOR UPPER GATE CLOSURE BEAM CRACKED AT ATTACH HOLE. NR 5L MAIN ENTRY DOOR UPPER GATE CLOSURE BEAM CRACKED AT ATTACH HOLE. CRACK WAS PROBABLY CAUSED BY FATIGUE. ANGLE REPAIR WAS INSTALLED REFERENCING SM-80-52-10-08-JD AND SRM 51-70-11. 2L74 4F4 FRTA20WE E24NE 20051027000022005102700002CE 2005 10 27 ACE102505 120051025A3397 WIRE BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA EMERGENCY LIGHTSOVERHEATED E YADAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 AL03112AX UC45 TAIL FLOOD WHEN TURNED ON, CAN SMELL ELECTICAL SMOKE. THEN SWITCH (FLOOD LIGHTS) FLIPS OFF. INSPECTED WIRING AT FLOOD LIGHT SWITCH AND FOUND OVERHEATED WIRE AT LOOSE TERMINAL ON CIRCUIT BREAKER SWITCH. 2L72 4T4 TRTA24CE E4EA 20051027000072005102700007NM 2005 10 27 SWAA053340 120051025A3350PL2230LH00 LIGHT BOEING737 7377H4 1384404NM CFMINTCFM567CFM567B22 13802NE ROW 12 ABC CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29429WN 33658 DURING SCHEDULED HC1 CHECK, FOUND EEPLS STRIP CRACKED BETWEEN ROW 12 ABC AND ROW 21 ABC. REMOVED AND REPLACED STRIP SECTION IAW MM. 2L72 4F4 FRTA16WE E00055EN 20051027000122005102700012EA 2005 10 27 COMA0560566 120051025A2797 WIRE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE FLAP SYSTEM BROKEN A COMAO OTHER J WARNING INDICATION CRCRUISE 1 SO01952CA 7092 FLAPS FAIL CAUTION. REPAIRED BROKEN WIRE AT THE LT BPSU. 2L72 4F4 FRTA21EA E15NE 20051027000162005102700016EA 2005 10 27 COMA0560565 120051024A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE MAIN PAX OUT OF POSITION A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01917CA 7017 CABIN DOOR WARNING. AC LOST PRESSURIZATION. CND SUSPECT DOOR NOT CLOSED PROPERLY. NO DEFECTS NOTED WITH DOOR OR PRESSURIZATION SYSTEM. 2L72 4F4 FRTA21EA E15NE 20051027000172005102700017EA 2005 10 27 COMA0560568 120051025A2752852D10011 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT WING UNRELIABLE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01818CA14484 7408 FLAPS FAIL CAUTION. CND REPLACED THE RT WING FLAP ACTUATORS. 2L72 4F4 FRTA21EA E15NE 20051027000232005102700023EU 2005 10 27 AWXA200501263 120051024A3350321431 BATTERY PACK AIRBUS320 A320231 3930325EU EMERGENCY LIGHT INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28632AW 81 PHX - EEL - DURING OVERNIGHT INSPECTION MAINTENANCE REPORTED SEVERAL CABIN EMERGENCY LIGHTS INOPERATIVE IN THE AFT CABIN AND GALLEY. MAINTENANCE REMOVED AND REPLACED THE AFT BATTERY PACK IAW AIRBUS MM 33-51-38. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA28NM 20051027000292005102700029NM 2005 10 27 AWXA200501269 120050914A57536546150100 SKIN BOEING737 73733A 1384673NM ZONE 600 DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW 23634 GYR - MAJOR REPAIR - DURING C20 CHECK, DISCOVERED DISBOND ARE ON THE LOWER SURFACE OF THE RT INBOARD FORE FLAP LOWER SKIN, OUTBOARD END AT WING STA 190 AND WBL 128. MAINTENANCE REMOVED DISBONDED SKIN IAW BOEING 737-300 SRM 51-70-10-2. FABRICATED REPAIR FILLER AND DOUBLER IAW BOEING 737-300 SRM 51-70-10-2. BONDED REPAIR PARTS TO THE RT INBOARD FORE FLAP LOWER SKIN AT WS 190 AND WBL 128 IAW BOEING 737-300 SRM 51-70-10. 2L72 4F RTA16WE 20051027000302005102700030NM 2005 10 27 AWXA200501270 120050923A53156545808179 FLOORBEAM BOEING737 7373S3 1384711NM BS 294 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 MCN - MAJOR REPAIR - DURING C18 CHECK DISCOVERED CORROSION ON THE TOP OF UPPER CHORD FROM BL 32R TO BL 38R, WL 208 AND BS 294. CORROSION WAS REMOVED AND FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-10-51-1A1 FIG 101. MAINTENANCE FABRICATED REPAIR CHORD AND ANGLES IAW BOEING 737-300 SRM 53-10-51-2R5 FIG 201. INSTALLED FABRICATED REPAIR PARTS FROM BL 32R TO BL 38R, WL 208 AND BS 294 IAW BOEING 737-300 SRM 53-10-51-2R5 FIG 201. 2L72 4F RTA16WE 20051027000322005102700032NM 2005 10 27 AWXA200501272 120050921A5320 SUPPORT ANGLE BOEING737 7373S3 1384711NM BS 800 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 MCN - DURING C18 CHECK DISCOVERED TWO CRACKS, .890 INCHES EACH, LOCATED AT THE AFT PIT DOOR INNER CHORD AND SUPPORT ANGLE AT BS 800 AND STR 20R. MAINTENANCE REMOVED SUPPORT ANGLE AND CHORD IAW BOEING 737-300 SRM 51-70-13-0G FIG 1. FABRICATED REPAIR DOUBLER AND REPAIR ANGLE IAW BOEING 737-300SRM 51-70-13-0G. INSTALLED FABRICATED REPAIR PARTS IAW BOEING 737-300 SRM 51-70-13-0G. 2L72 4F RTA16WE 20051027000332005102700033EU 2005 10 27 U30A200500009 120050914A5330 SKIN AIRBUS320 A320214 3930316EU FUSELAGE DENTED A U30AK NONE O OTHER ININSP/MAINT 1 EA17260AV1206512065 1564 GROUND HANDLING EQUIPMENT CAME IN CONTACT WITH LT FWD SIDE OF AIRCRAFT. DAMAGE INSPECTION PER SRM & WITHIN ALLOWABLES FOR 3000 FC. PERMANENT MAJOR REPAIR ACCOMPLISHED TO LT SIDE OF FUSELAGE, DENT NEAR STRINGER 24 & FRAME 9. REPAIRED UNDER USA 3000 AIRLINES EO 04-53-008R01, WHICH INCORPORATES PERMANENT REPAIR DEFINITION PER AIRBUS SRM 53-00-11, PAR 4A, FIG 204. REMOVED DAMAGED SKIN, FABRICATED EXTERNAL DOUBLER & FILLER ALUMINUM. APPLIED PROTECTIVE TREATMENTS PER SRM 51-23-00 & APPLIED SEALANTS PER SRM 51-76-11. FAA FORM 337 ACCOMPLISHED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA28NM 20051027000342005102700034NM 2005 10 27 QXEA200501367 120051022A6120 AUTOFEATHER SYS BOMBDRDHC8 DHC8402 1390042NM MALFUNCTIONED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09409QX 4051 SEA FLIGHT NR 2392, AUTOFEATHER ARM LIGHT FAILED TO ILLUMINATE ON TAKEOFF. MAINTENANCE INTERROGATED CDS. FOUND FAULT CODE 64 CH A. CLEARED FAULTS. PERFORMED OPS TEST, AUTOFEATHER SYSTEM IAW 61-20-00-710-805. NO DEFECTS NOTED. PERFORMED GROUND RUN AT T/O POWER. A/F SYSTEM ARMED OK. NO FURTHER FAULTS FOUND. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051027000352005102700035CE 2005 10 27 DXTA200501030 120051018A3260MS243311 POSITION SWITCH BEECH MU300 400A 1155402CE MLG MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 GL07108QS RK382 ON APPROACH RT MAIN GEAR LIGHT WOULD NOT ILLUMINATE WHEN GEAR SELECTED DOWN. GEAR CYCLED TWICE AND LIGHT CAME ON, 3 GREEN. REPLACED FAULTY RT GEAR DOWNLOCK SWITCH WITH NEW. OPS CHECK GOOD IAW 400XP MM 32-31-02. 2H72 4F RTA16SW 20051027000422005102700042NM 2005 10 27 QXEA200501368 120051020A5340 CLIP DHAV DHC8 DHC8202 2809007NM BS 424 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09345PH 476 PDX - THERE IS A CLIP CORRODED AT THE AFT SIDE OF FRAME 424.124, STRINGER 24, RIGHT SIDE. REPAIRED IAW SRM 51-40-11, HORIZON AIR EA 2-53-638. 2H72 4T RTA13NM 20051027000492005102700049NM 2005 10 27 P5CA0501407 120051019A5730 SKIN BOEING747 747283B 1384867NM RT WING CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 EA15921FT 21575 CORROSION ON RT UPPER SKIN AFT OF REAR SPAR WS 560 TO 575. REMOVED CORROSION & REPAIRED IAW BOEING REPAIR PROCEDURE 1-129539127-5 AND 8100-9. 2L74 4F A20WE 20051027000502005102700050SO 2005 10 27 CHQA200500187 120051022A335078241 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11266SK 145241 AFT EMERGENCY AISLE LIGHTING INOPERATIVE IN CABIN. REMOVED AND REPLACED NR 8 INVERTER IAW EMB 145 MM 33-50-11. OPS CHECK GOOD. 2L72 4T RTT00011AT 20051027000542005102700054EA 2005 10 27 SWIA200515714 120051021A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07964SW 7868 THE 3RD CEILING EMERGENCY FLOOD INOP. RELAMPED FLOOD LIGHT AS NECESSARY IAW AMM 33-20-00. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051027000552005102700055EA 2005 10 27 SWIA200515715 120051022A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLT SPOILERSL MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07935SW 7725 A -FLIGHT SPOILERS FAULT- STATUS MESSAGE. REPLACED NR 1 SECU AND NR 2 PCU-SPOILERON IAW MM 27-61-05 AND 27-61-05, OPERATIONAL CHECK GOOD. P/N 49-164-05, S/N OFF 01607. 2L72 4F RTA21EA 20051027000562005102700056SO 2005 10 27 SWIA200515716 120051022A2611 BATTERY EMB 120 EMB120ER 3260203SO SMOKE DETECTOR DISCHARGED A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07291SW 120318 SMOKE DETECTOR IN LAV SOUNDS FOR NO REASON. REPLACED SMOKE DETECTOR BATTERY IN THE LAV AS REQUIRED, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20051027000572005102700057EA 2005 10 27 SWIA200515717 120051023A274170623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07941SW 7750 CREW REPORTS STAB CHAN 2 WILL NOT ENGAGE. REPLACED MOTOR CONTROL UNIT. OPERATIONAL CHECK GOOD REF CRJ AMM 27-42-05. 2L72 4F RTA21EA 20051027000592005102700059EA 2005 10 27 SWIA200515719 120051021A274170623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM07418SW1368813688 7446 STAB TRIM CH 1 INOP MESSAGE ON TAXI OUT. REPLACED THE HSTA IAW MM 27-12-01 AND MCU IAW MM 27-42-05. OPERATIONAL CHECK GOOD. P/N 8396-3; S/N OFF 643. 2L72 4F RTA21EA 20051027000652005102700065EA 2005 10 27 VNAA0510014 120051017A27306225027101 SERVO CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE ELEVATOR FAILED A VNAAO OTHER O OTHER NRNOT REPORTED 1 GL05259PS2875 7945 THE CREW REPORTED STAB TRIM MOVEMENT WITHOUT PILOT INPUT IN FLIGHT. THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE FOUND A FAILED AUTOPILOT ELEVATOR SERVO. THE SERVO WAS REMOVED & REPLACED IAW CRJ200 AMM 22-11-24-000(400)-801. OPERATIONAL TESTS OF AUTOPILOT & STAB TRIM SYSTEMS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20051027000662005102700066 2005 10 27 2005UALA01089 420051001A2565 SLIDE BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE OVERWING EXIT MALFUNCTIONED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29672UA 30027 BOTH SPOILER AND SLIDE SQUIBS DO NOT TEST ON BOTH LEFT AND RIGHT OVERWING EXITS. REPLACED BOTH OFF-WING SLIDE BATTERIES. TEST OK AFTER CHANGE OUT. 2L72 4F4 FRTA1NM E24NE 20051027001192005102700119NM 2005 10 27 AWXA200501274 120051011A5754 SKIN BOEING737 7373G7 1384595NM ZONE 500 DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - MAJOR REPAIR - DURING C16 CHECK, DISCOVERED THE UPPER AND LOWER SURFACE OF THE NR 3 SLAT WEDGE DISBONDED FROM SS 12.25L TO SS 18.25L. MAINTENANCE REMOVED DAMAGED AREA FROM THE NR 3 SLAT WEDGE IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED REPAIR CORE AND REPAIR DOUBLER IAW BOEING 737-300 SRM 51-70-10-2R4. BONDED FABRICATED REPAIR PARTS TO THE UPPER AND LOWER SURFACES OF THE NR 3 SLAT WEDGE FROM SS 12.25L TO SS 18.25L IAW BOEING 737-300 SRM 51-70-10-2R4. 2L72 4F RTA16WE 20051027001222005102700122NM 2005 10 27 AWXA200501277 120051019A575369388487 TRACK BOEING737 7373G7 1384595NM ZONE 500 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - MAJOR REPAIR - DURING C16 DISCOVERED CORROSION ON THE LT INBOARD FLAP, OUTBOARD CAM TRACK AT WBL 185L. NO CORROSION REMOVAL LIMITS ARE AVAILABLE FOR CAM TRACK. MAINTENANCE REMOVED CAM TRACK AND INSTALLED NEW CAM TRACK ON THE LT INBOARD FLAP, OUTBOARD TRACK AT WBL 185 IAW BOEING 737-300 CMM 57-53-22. 2L72 4F RTA16WE 20051027001242005102700124NM 2005 10 27 AWXA200501279 120051019A575369388487 TRACK BOEING737 7373G7 1384595NM TE FLAPS CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - MAJOR REPAIR - DURING C16 DISCOVERED CORROSION ON THE RT INBOARD FLAP, OUTBOARD CAM TRACK AT WBL 185.00R. NO CORROSION REMOVAL LIMITS ARE AVAILABLE FOR CAM TRACK. MAINTENANCE REMOVED CAM TRACK AND INSTALLED NEW CAM TRACK ON THE RT INBOARD FLAP, OUTBOARD TRACK AT WBL 185.00L IAW BOEING 737-300 CMM 57-53-22. 2L72 4F RTA16WE 20051027001252005102700125NM 2005 10 27 AWXA200501280 120051019A575369388485 TRACK BOEING737 7373G7 1384595NM TE FLAPS CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - MAJOR REPAIR - DURING C16, DISCOVERED CORROSION ON THE RT INBOARD FLAP, INBOARD CAM TRACK AT WBL 71.00R. NO CORROSION REMOVAL LIMITS ARE AVAILABLE FOR CAM TRACK. MAINTENANCE REMOVED CAM TRACK AND INSTALLED NEW CAM TRACK ON THE RT INBOARD FLAP, INBOARD TRACK AT WBL 71.00L IAW BOEING 737-300 CMM 57-53-22. 2L72 4F RTA16WE 20051027001262005102700126NM 2005 10 27 AWXA200501281 120051011A575465C2660310157 SKIN BOEING737 7373G7 1384595NM NR 3 SLAT DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - MAJOR REPAIR - DURING C16 CHECK, DISCOVERED THE UPPER AND LOWER SURFACE OF THE NR 3 SLAT DELAMINATED FROM SS 116.27L TO SS 124.27L. MAINTENANCE REMOVED DAMAGED AREA FROM THE UPPER AND LOWER SURFACE OF THE NR 3 SLAT IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED REPAIR CORE AND REPAIR DOUBLER IAW BOEING 737-300 SRM 51-70-10-2R4. BONDED FABRICATED REPAIR PARTS TO THE UPPER AND LOWER SURFACES OF THE NR 3 SLAT FROM SS 116.27L TO SS 124.27L IAW BOEING 737-300 SRM 51-70-10-2R4 FIGS 201 AND 202. 2L72 4F RTA16WE 20051027001282005102700128NM 2005 10 27 AWXA200501283 120051011A575465C2679913 SKIN BOEING737 7373G7 1384595NM NR 1 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED 4 CRACKS, 1.0 INCHES IN LENGTH, ON THE NR 1 LOWER SLAT SKIN BELOW THE CENTER AUXILIARY TRACK FROM SS 298L TO SS 302L. MAINTENANCE CUT OUT DAMAGED AREA ON THE NR 1 LOWER SLAT SKIN IAW BOEING 737-300 SRM 57-43-01-2R6 FIG 201. FABRICATED FILLER AND SPLICE PLATE IAW BOEING 737-300 SRM 57-43-01-2R6 FIG 201. INSTALLED FABRICATED REPAIR PARTS ON THE NR 1 LOWER SLAT SKIN FROM SS 298L TO SS 302L IAW BOEING 737-300 SRM 51-43-01-2R6. 2L72 4F RTA16WE 20051027001302005102700130NM 2005 10 27 AALA20050641 120051005A3350 SOCKET BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21631AA 24589 JFK - EMERGENCY PATH LIGHT AT 17D INOPERATIVE. REPLACED EMERGENCY PATH LIGHT SOCKET AT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20051027001322005102700132NM 2005 10 27 05FDEA03252 120051006A5314 KEELBEAM BOEING727 727200 138407ENM BS 905E CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 STA 950E 2 STR 29R CORROSION ON STR FLANGE. REPAIRED STRINGER AT BS 950E 2, 29R PER FED EX EA 7-5310-91393 2L73 4F RTA3WE 20051027001332005102700133NM 2005 10 27 05FDEA03257 120051006A3230 BEARING DOUG MD11 MD11 3023602NM MLG PUSH ROD WORN A FDEAO OTHER J WARNING INDICATION APAPPROACH 1 SO25598FE 48597 UPON GEAR EXTENSION DURING APPROACH ALL FOUR GEARS INDICATED UNSAFE AND NO EXTENSION. GEAR HANDLE RECYCLED UP AND DOWN AGAIN WITH GEAR EXTENSION BEING ABOUT ONE FOURTH THE SPEED OF NORMAL GEAR EXTENSION. SEQUENCE OF DOWN AND LOCKED INDICATIONS WERE NOSE, CENTER, LEFT, THEN RIGHT. REMOVED AND REPLACED RT MAIN GEAR DOOR POSITION FOLLOW UP PUSH ROD BEARING PER REF TO MD-11 MM CHAPTER 25 SMP. CYCLED GEAR SEVERAL TIMES PER REF TO MD-11 MM CHAPTER 32-31-00-5. ALL INDICATIONS NORMAL. REFERENCE PREVIOUS SHORT SIGN OCT 5 2005 AT 0012Z. FOR REMOVAL AND REPLACEMENT OF LT AND RT MAIN LANDING GEAR FOLLOW LINKS. 2L73 4F RTA22WE 20051027001352005102700135EU 2005 10 27 131110052005 220051005A7532321474031 BLEED VALVE GULSTMG1159 GIV 3980115SO RROYCETAY TAY6118 EU ENGINE FAILED E N93AA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO13411QS 1311 LEFT BLEED AIR READS 1 PSI ON TAXI, RIGHT READS 10 PSI. LEFT BLEED AIR AT ALL ALTITUDES READS 10 PSI AND RIGHT READS 21 TO 24 PSI. ON TAKEOFF RIGHT BLEED PRESSURE HI ILLUMINATED RIGHT BLEED READ 78 PSI. SWITCHED OFF RIGHT BLEED AND LIGHT WENT OUT TURNED RIGHT BLEED BACK ON AT 17000 FT WORKED NORMAL DISPLAYING 21 PSI ON RIGHT AND 10 PSI ON LEFT. CABIN RATE OF CLIMB PEGGED FULL RATE UP AND THEN ALTERNATING FULL RATE DOWN AT NORMAL CRUISE FLIGHT LEVER 410. THIS CONTINUED UNTIL OUTFLOW VALVE WAS FULL OPEN, TRIED MANUAL AND ADC 1&2. 2L72 4F4 FRTA12EA E25NE 20051027001372005102700137WP 2005 10 27 MWEA050109 120051006A57545936284501 DOUBLER DOUG DC9 DC981 3022081WP LT WING SLAT DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31812ME 48006 SLAT HORN ON THE LEFT WING HAS A DENT. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20051027001392005102700139WP 2005 10 27 MWEA050111 120051006A5751995757111 RUB STRIP DOUG DC9 DC981 3022081WP LEFT AILERON CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31812ME 48006 LEFT AILERON INBOARD HINGE RUBSTRIP IS CRACKED. FABRICATED AND INSTALLED FILLER. 2L72 4F A6WE 20051027001412005102700141WP 2005 10 27 MWEA050113 120051006A5320J0602283 SILL DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31812ME 48006 FORWARD CARGO DOOR SILL HAS MODERATE CORROSION. BLENDED CORROSION. 2L72 4F A6WE 20051027001432005102700143NM 2005 10 27 AWXA200501259 120051007A575465C26603100SP WEDGE BOEING737 7373S3 1384711NM ZONE 600 DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 MCN - MAJOR REPAIR - DURING C18 CHECK DISCOVERED DISBOND AREA ON OUTBOARD END OF THE RIGHT WING NR 4 SLAT WEDGE. MAINTENANCE REMOVED DISBOND AREA FROM THE NR 4 SLAT WEDGE IAW BOEING 737-300 SRM 51-70-10-2R. FABRICATED AND BONDED REPAIR FILLER AND DOUBLER TO OUTBOARD END OF THE RIGHT WING 4 SLAT WEDGE FROM WBL 230.68L TO WBL 232.68L IAW BOEING 737-300 SRM 51-70-10-2R4 REPAIR 4 FIGURE 203. 2L72 4F RTA16WE 20051027001442005102700144EA 2005 10 27 SWIA200515723 120051019A274170623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07976SW7094 7094 7952 STAB TRIM NR 2 C/B POPS WHEN STAB TRIM NR 2 IS ENGAGED. REPLACED HORIZONTAL STAB MOTOR CONTROL UNIT REF AMM 27-41-01. OPERATIONAL CHECK GOOD, REF AMM 27-41-00. 2L72 4F RTA21EA 20051027001452005102700145EA 2005 10 27 SWIA200515724 120051022A274183963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07446SW9002 9002 7666 A -STAB CH 1 INOP MESSAGE- WHEN TRIMMING STAB TRIM NOSE UP. REPLACED STAB ACTUATOR AND MOTOR CONTROL UNIT IAW AMM 27-42-01 AND AMM 27-42-05. OPERATIONAL CHECK GOOD IAW AMM 27-41-00. P/N 7062-3, SN/OFF 255. 2L72 4F RTA21EA 20051027001462005102700146EA 2005 10 27 SWIA200515725 120051020A5610 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07958SW 7833 LEFT SIDE WINDOW OUTER PANE CRACKED. REPLACED LEFT SIDE WINDOW IAW CRJ 200 MM CHAPTER 56-12-01. 2L72 4F RTA21EA 20051027001482005102700148EA 2005 10 27 SWIA200515727 120051016A2750601R590141 DETECTOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07969SW 7876 RECEIVED FLAPS FAIL CAUTION MESSAGE ON TAXI OUT. REPLACED RIGHT FLAP PDU BRAKE MOTOR IAW AMM 27-52-00, OPERATIONAL CHECK GOOD. P/N ON 601R59014-1, S/N OFF A568. 2L72 4F RTA21EA 20051027001492005102700149EA 2005 10 27 SWIA200515728 120050414A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA BS 625 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07905SW 7437 LEFT SIDE FS 625 CLIP CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALL CLIP IAW CRJ200 SRM 51-42-06. 2L72 4F RTA21EA 20051027001502005102700150EA 2005 10 27 SWIA200515729 120050414A5712 RIB CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07905SW 7437 LEFT MLG WHEEL WELL BATTERY RIB CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED DOUBLER IAW CRJ200 REO 601R-57-51-046 TYPE 1 REPAIR. 2L72 4F RTA21EA 20051027001512005102700151EA 2005 10 27 SWIA200515730 120050414A5712 RIB CNDAIRCL600 CL6002B19 1900309EA RT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07905SW 7437 RIGHT MLG WHEEL WELL BATTERY RIB CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR PARTS PER REO 601R-57-51-046. 2L72 4F RTA21EA 20051027001522005102700152EA 2005 10 27 SWIA200515731 120050414A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07905SW 7437 FRAME 280 AND BL-9 LT SIDE CLIP CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIP IAW CRJ200 SRM 51-10-06 PG 3, PARAGRAPH D. 2L72 4F RTA21EA 20051027001532005102700153WP 2005 10 27 AALA20050690 120051018A2841 INDICATOR DOUG DC9 DC982 3022082WP FUEL QTY MALFUNCTIONED A AALAA UNSCHED LANDING S AFFECT SYSTEMS CRCRUISE 1 SW21251AA 49270 BDL - ORD - DURING CRUISE HAD FUEL QUANTITY INDICATION FAULT. DIVERTED AND LANDED SAFELY AT GRR. INSPECTED ENGINES. NO DISCREPANCIES NOTED. TANKS CHECKED, DRAINED AND RE-FUELED. VERIFIED LOAD BY STICKING TANKS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051027001552005102700155EA 2005 10 27 REXA200500127 120051001A2750860D10018 FCU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS INOPERATIVE A REXAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO258721B 8021 FLAPS FAILED ON APPROACH AT 0 WHEN SELECTED TO 20. 2L72 4F RTA21EA 20051027001562005102700156NM 2005 10 27 2005UALA01109 120051009A5311 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE BS 867 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29919UA 25386 AFT CABIN STA 867 FRAME IS CRACKED BETWEEN STR 8R AND 9R. REMOVED CRACK, FABRICATED REPAIR ANGELS AND INSTALLED PER MM 53-10-84. 2L72 4F4 FRTA16WE E2GL 20051027001572005102700157NM 2005 10 27 2005UALA01110 120051009A5311 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE BS 440 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29919UA 25386 CABIN STA 440 BTWN STR 8R AND 9R FUSELAGE FRAME CRACKED. REMOVED CRACKED,INSTALLED REPAIR ANGELS PER MM 53-10-84. 2L72 4F4 FRTA16WE E2GL 20051027001602005102700160NM 2005 10 27 2005UALA01113 120051008A3350362624 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE SEATS 1J & 4F INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29107UA 26900 EMERGENCY EEL LIGHT AT SEAT 1J AND 4F IS INOPERATIVE. REPLACED EEL LIGHT. REPLACED EEL LIGHT. 2L74 4F4 FRTA20WE E24NE 20051027001622005102700162NM 2005 10 27 2005UALA01115 120051009A3350582233 POWER SUPPLY BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29119UA 28812 ALL EEL INOP LT A ZONE IB AND OB. REPLACED POWER SUPPLY. 2L74 4F4 FRTA20WE E24NE 20051027001632005102700163NM 2005 10 27 2005UALA01116 120051009A33501317 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHTSINOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29119UA 28812 EMERGENCY LIGHT INOPERATIVE CEILING ROW 6 RT. REPLACED LAMP. 2L74 4F4 FRTA20WE E24NE 20051027001692005102700169WP 2005 10 27 05FDEA03293 120051007A5712 RIB DOUG DC10 DC1010 3022110WP RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE RT WING FIXED L/E COMPT AT STA XORS 650 ZONE 625 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 4 AND 6 VOL I. 2L73 4F A22WE 20051027001712005102700171WP 2005 10 27 05FDEA03295 120051007A5712 RIB DOUG DC10 DC1010 3022110WP RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE RT WING FIXED L/E COMPT AT STA XORS 530 ZONE 619 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 4 AND 6 VOL I. 2L73 4F A22WE 20051027001732005102700173NM 2005 10 27 AWXA200501260 120051004A57536546435278 SKIN BOEING737 7373S3 1384711NM TE FLAP DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 MCN - MAJOR REPAIR - DURING C18 CHECK DISCOVERED DISBOND AREA ON LOWER SURFACE OF THE RT OUTBOARD AFT FLAP AT THE INBOARD AFT CORNER. MAINTENANCE REMOVED DISBOND AREA FROM THE OUTBOARD AFT FLAP IAW BOEING 737-300 SRM 51-70-10-2R. FABRICATED AND BONDED REPAIR FILLER AND DOUBLER TO OUTBOARD END OF THE RT OUTBOARD AFT FLAP IAW BOEING 737-300 SRM 51-70-10-2R4 REPAIR 4 FIGURE 203. 2L72 4F RTA16WE 20051027001792005102700179EU 2005 10 27 YENA200570 120050928A3350321430 BATTERY AIRBUS320 A320232 3930326EU EMERGENCY LIGHT INOPERATIVE A YENAK NONE O OTHER ININSP/MAINT 1 EA15528JB16442 1591 FOUND ON CIDS CHECK - EPSU BATTERY FWD L MESSAGE. T/S IAW 33-51-00-810-802. REMOVED AND REPLACED BATTERY IAW AMMM 33-51-38. CHECKS OK AT THIS TIME. 2L72 4F RTA28NM 20051027001812005102700181NM 2005 10 27 AWXA200501177 120050909A53306545766 SKIN BOEING737 7373G7 1384595NM BS 500D CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 MCN - DURING C18 CHECK DISCOVERED FUSELAGE SKIN CRACKED, .75 INCHES IN LENGTH, AT BS 500D-2 AND STRINGER 12R. MAINTENANCE TRIMMED OUT DAMAGED SKIN IAW AMERICA WEST AIRLINES (AWA) ENGINEERING REPAIR (ER) NR 03-5331-05273-ES1. FABRICATED FILLERS, DOUBLER, TRIPLER AND TEAR STRAP DOUBLER IAW AWA ER 03-5331-05273-ES1. INSTALLED FABRICATED REPAIR PARTS AT BS 500D-2 AND STRINGER 12R IAW AWA ER 03-5331-05273-ES1. 2L72 4F RTA16WE 20051027001842005102700184EA 2005 10 27 ASOA05802 120050924A5340 ANGLE CNDAIRCL600 CL6002B19 1900309EA BS 559 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27835AS 7258 DURING A C-CHECK IN MCN, THE FLOORBEAM SUPPORT ANGLE, AT FS 559 PLUS 112, LBL 9 WAS SUSPECTED OF BEING CRACKED BEYOND LIMITS. S/D - MAINTENANCE PERFORMED AN INSPECTION ON THE FLOORBEAM SUPPORT ANGLE, AT FS 559 PLUS 112, LBL 9 WITH NO DEFECTS FOUND. (M) 2L72 4F RTA21EA 20051027001862005102700186NM 2005 10 27 PIDA20050181 120051017A5312 PRESSURE PANEL BOEING737 737306 13844BGNM GE CFM56 CFM563B1 13802NE BS 663 CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05371PA 23543 EVIDENCE OF CRACK AT PRESSURE WEB AT BS663 AT LBL33. REPAIRED PRESSURE WEB IAW SRM 53-60-51. 2L72 4F4 FRTA16NE E2GL 20051027001892005102700189EU 2005 10 27 AWXA200501284 220051023A7200 ENGINE BOEING737 7373Y0 1384671NM CFMINTCFM56 CFM562AFR 13802EU NR 2 MALFUNCTIONED A AWXAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 WP28334AW 23747 SMF - AIR TURNBACK - FLT 544 - AFTER TAKEOFF, DURING CLIMB EN ROUTE TO PHX FROM SMF, CREW HEARD LOUD NOISE FROM THE NR 1 ENGINE AND NOTICED NR 2 ENGINE OIL QUANTITY GAUGE DROP BELOW ONE. AIRCRAFT RETURNED TO SMF AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND SERVICED THE NR 2 ENGINE IAW BOEING 737-300 AMM 71-00-44-01. NO DEFECTS WERE NOTED AT THE TIME. ALSO RAN ENGINES AND PREFORMED AMERICA WEST AIRLINES TASK CARD F2A77001, AVM INTERROGATION, ON THE NR 1 ENGINE, WHICH ENGINE WAS WITHIN OPERATING RANGE. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA16WE E21EU 20051028000032005102800003NM 2005 10 28 05FDEA03489 120051025A5320 INTERCOSTAL BOEING727 727100 1384036NM PWA JT8 JT8D7B 52053NE BS 660 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 N01148 CRACK BS 660 STR 2L UPPER INTERCOSTAL EXTENSION. [OPEN] 2L73 4F4 FRTA3WE E2EA 20051028000062005102800006 2005 10 28 05FDEA03492 420051025A3416 INDICATOR AIRBUS300 A300F4605R 3930327EU PWA 4158 PW4158 NE NR 2 AIRSPEED INACCURATE A FDEAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 SO25718FD 365 DURING TAKEOFF ROLL, NR 2 PRIMARY AIRSPEED INDICATOR CONTINUED TO INDICATE 30 KIAS WHILE NR 1 INDICATED 80 KIAS. TAKEOFF ABORTED AT 90 KIAS. ENT BY: 275418 RPT BY: 056042 FACT 25OCT05 06:18 ONT R AS PRECAUTIONARY USING DRY NITROGEN BLEW OUT NR 2 PITOT AND NO OBSTRUCTIONS WERE NOTED. REPLACED NR 2 ADC OPS NORMAL REF MM 34-11-34-4. 2L72 4F4 FRTA35EU E24NE 20051028000092005102800009SO 2005 10 28 C2XA05TY056 120051019A532014521713005 FLOOR SUPPORT EMB 145 EMB145 3260210SO GALLEY CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713964 145123 DURING A SCHEDULED INSPECTION THE CENTER OMEGA BEAM IN THE GALLEY WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE CENTER OMEGA BEAM. IAW SRM-51-40-02. 2L72 4F RTT00011AT 20051028000102005102800010NM 2005 10 28 QXEA200501377 120051026A2930570347 PUMP DHAV DHC8 DHC8202 2809007NM HYDRAULIC SYS MALFUNCTIONED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09375PH133686675 529 SEA FLIGHT 2108, AFTER DEPARTING HAD A NR 2 HYDRAULIC PRESSURE CAUTION. RAN CHECKLIST WENT BACK TO SEA. MAINTENANCE REPLACED NR 2 HYDRAULIC PUMP. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051028000142005102800014WP 2005 10 28 UPS05845646 120051026A7100 ENGINE DOUG DC8 DC871F 302199DWP CFMINTCFM56 CFM562AFR 13802EU NR 4 FLAMED OUT A IPXAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 SO01706UP 46056 NR 4 ENGINE FLAMED OUT IN CRUISE FLIGHT. T/S PER MM 71-00-00-1 FIG 139 SHT 1&2. REPLACED FUEL FILTER ELEMENT, RAN ENG WITH FEED & BOOST PUMP OFF, FUEL PRESS WITHIN LIMITS. ENG OPS NORMAL. 2L74 4F4 FRT4A25 E21EU 20051028000152005102800015NM 2005 10 28 SWAA053333 120051025A335065C27093 LENS BOEING737 7377AD 1384502NM EXIT SIGN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29798SW 28436 DURING SCHEDULED RON, FOUND CABIN CEILING NR 3 EMERGENCY EXIT SIGN FWD LENS MISSING. REMOVED AND REPLACED EMERGENCY EXIT SIGN PER MM. 2L72 4F RTA16WE 20051028000192005102800019NM 2005 10 28 SWAA053337 120051025A5754 SKIN BOEING737 7373H4 1384600NM LT WING SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29332SW 23696 DURING SCHEDULED C2 CHECK, FOUND NR 1 L/E SLAT SKIN CRACKED NEAR INBOARD END. REPAIRED SLAT PER SRM. 2L72 4F RTA16WE 20051028000212005102800021NM 2005 10 28 SWAA053339 120051025A5753 SKIN BOEING737 7373H4 1384600NM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29375SW 2320 26583 DURING SCHEDULED SERVICE CHECK, FOUND RIGHT WING T/E OUTBOARD AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP ASSY PER MM. 2L72 4F RTA16WE 20051028000242005102800024NM 2005 10 28 05FDEA03504 120051026A5311 FRAME BOEING727 727100 1384036NM BS 890 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 UPPER LOBE INTERIOR FRAME HAS MACH DAMAGE AND OPEN HOLES BS 890 STR 9L. [OPEN] 2L73 4F RTA3WE 20051028000252005102800025EU 2005 10 28 05FDEA03505 120051026A5230 DOOR AIRBUS310 A310 EU CARGO BAY MALFUNCTIONED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25412FE 360 SOON AFTER T/O GOT ECAM ALERT FOR AFT CARGO NOT CLOSED AFT CARGO SW FAULT AND AN AMBER DOOR LIGHT FO R AFT CARGO ON RT ECAM. ACN RELEASED FOR SERVICE PER MEL/CDL: 52-71-01 CATEGORY: C EXPIRATION: 05NOV05 MEL 52-71-01: AFT DOOR CLOSED AND LOCKED INDICATION ON ECAM DOOR PAGE - INOP. AFT DOOR VISUALLY CHECKED CLOSED AND LOCKED. NOTE: NO CABIN PRESS PROBLEMS NOTED. 2L72 4F RTA35EU 20051028000262005102800026NM 2005 10 28 05FDEA03495 120051025A5330 DOUBLER BOEING727 727200 138407ENM BS 740 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25484FE 21466 COMPLY WITH EA 7-5310-92343 FUSELAGE SKIN-STA 740 BKHD SUPPORT DOUBLER CORROSION. [OPEN] 2L73 4F RTA3WE 20051028000302005102800030NM 2005 10 28 SWAA053342 120051025A53116546554 FRAME BOEING737 7373H4 1384600NM BS 847 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847 AND AFT CARGO DOOR CUT OUT NR 5 STOP FITTING. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20051028000312005102800031NM 2005 10 28 SWAA053343 120051025A53116546529 FRAME BOEING737 7373H4 1384600NM BS 440 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 23R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051025001782005102500178WP 2005 10 25 05FDEA03217 120051005A5712 RIB DOUG DC10 DC1010 3022110WP ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE LT WING FIXED L/E COMPT AT STA XORS 767 ZONE 526 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET4 AND 6 VOL I. 2L73 4F A22WE 20051026000192005102600019NE 2005 10 26 DL757050638 220051019A7397 CONNECTOR BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 2 ENGINE LOOSE A DALAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION TXTAXI/GRND HDL 1 SO27635DL 23762 716433 DURING MAIN ENGINE START AFTER PUSHBACK NUMBER 2 ENGINE SPAR VALVE LIGHT REMAINED ILLUMINATED AND ENGINE FLAMED OUT. RESEATED CONNECTOR ON SPAR VALVE, ENGINE STARTS NORMALLY. 2L72 4F4 FRTA2NM E17NE 20051026000312005102600031EU 2005 10 26 ASOA05743 120050907A3350 LAMP AEROSPATR72 ATR72 EU EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27642AS 395 DURING AN A-CHECK IN MCN, THE EMERGENCY EXIT LIGHT BY THE PASSENGER DOOR ON THE AFT WALL WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMPS IN THE EMERGENCY EXIT LIGHT BY THE PASSENGER DOOR ON THE AFT WALL. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20051026000382005102600038EA 2005 10 26 ASOA05767 120050917A3350OL3071BPEGPL LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27836AS 7263 DURING A GROUND INSPECTION IN SHV, EMERGENCY FLOODLIGHT AND THE EMERGENCY EXIT LIGHT, NEAR THE SERVICE DOOR, WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMPS IN THE EMERGENCY FLOOD LIGHT AND THE EMERGENCY EXIT LIGHT NEAR THE SERVICE DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051026000502005102600050NM 2005 10 26 05FDEA03484 120051024A5315 FLOORBEAM BOEING727 7272S2F 1384O81NM BS 344 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25213FE 22935 MDCC - FLOORBEAM BS 344 LBL-14-40 HAS SURFACE CORROSION. REMOVED CORROSION IAW SRM 51-10-6, BEFORE REMOVED MATERIAL 0.110 AFTER 0.104 WITHIN LIMITS IAW SRM 51-10-1. TREATED AND PRIMED IAW SRM 51-10-2. 2L73 4F A3WE 20051026000512005102600051WP 2005 10 26 05FDEA03486 120051025A21501879009 HEAT EXCHANGER DOUG DC10 DC1010 3022110WP ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25372FE 46610 AIR CONDITIONING, NR 1 AC PACK HEAT EXCHANGE FLANGE REPAIR. COMPLIED WITH EA 8-2150-92346. WELD REPAIR OF HEAT EXCHANGER FLANGE AREA. 2L73 4F A22WE 20051026000532005102600053 2005 10 26 CALA0500375 420050922A256561620468 SLIDE BOEING737 7373T0 1384582NM R-1 DOOR TWISTED A CALAK NONE O OTHER ININSP/MAINT 1 SW271432028262 23371 R-1 DOOR EVACUATION SLIDE FAILED TO DEPLOY PROPERLY DURING DEPLOYMENT TEST. SLIDE INFLATED EARLY CAUSING SLIDE TO INFLATE BETWEEN DOOR & DOOR OPENING NOT ALLOWING DOOR TO COMPLETELY OPEN. SLIDE DEPLOYED SIDEWAYS INSTEAD OF FLAT. SLIDE INFLATED COMPLETELY WITHIN 10 SEC. SLIDE WAS REMOVED & REPLACED. BOEING HAS SEEN PROBLEM WITH OTHER OPERATORS (SIDEWAYS OR TWISTED SLIDE DEPLOYMENT) DESCRIBED IN THEIR "FLEET TEAM DIGEST 737-FTD-25-02007". BOEING ATTRIBUTES SLIDE'S SIDEWAYS DEPLOYMENT TO ALIGNMENT(IE. POSITIONING) OF SLIDE WITHIN SLIDE COMPARTMENT ASSEMBLY (50% SLIDE FAULT AND 50% COMPARTMENT FAULT). BOEING PLANS TO INCORPORATE SEVERAL DESIGN IMPROVEMENTS TO ESCAPE SLIDE COMPARTMENT WITH RELEASE OF S/B. 2L72 4F RTA16WE 20051026000582005102600058NM 2005 10 26 05FDEA03481 120051024A5311 FRAME BOEING727 727100 1384036NM BS 1030 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 AFT CARGO BAY FRAME BS 1030 BETWEEN STR 26 LT AND 27 LT DENTED. FABRICATED DOUBLER CAP AT BS 1030 BTWN STR 26 AND 27 L/H USING 7075T6 .071 M590750 PER SRM 51-40-3. INSTALLED DOUBLER CAP AT BS 1030 BETWEEN STR 26 AND STR 27 LT PER SRM 51-30-2. 2L73 4F RTA3WE 20051026000662005102600066EA 2005 10 26 ASOA05791 120050923A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27835AS 7258 DURING A C-CHECK, THE INNER BELLY SKIN AFT OF THE LAVATORY FAN BELOW RBL 27 WAS FOUND TO BE CORRODED. S/D - MAINTENANCE REPAIRED THE INNER BELLY SKIN, AFT OF THE LAVATORY, BELOW RBL 27, IAW BOMARDIER REO 601R-53-41-037. (M) 2L72 4F RTA21EA 20051026000702005102600070SO 2005 10 26 RAIA00510023 120051023A3260 UPLOCK EMB 145 EMB145LR 3260212SO RT MLG MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03816HK 145055 FLT 5584 - RIC - ON TAKEOFF DURING GEAR RETRACTION, PILOT GOT LG/LEVER DISAGREE MESSAGE ON THE EICAS AND RIGHT MAIN GEAR RED UNSAFE INDICATION. MAINTENANCE REMOVED AND REPLACED THE RIGHT MLG UPLOCK. 2L72 4T RTT00011AT 20051026001012005102600101NM 2005 10 26 2005UALA01147 120051015A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29195UA 26899 SEAT 4B LEFT HAND EEL LIGHT INOP. 2L74 4F4 FRTA20WE E24NE 20051026001042005102600104NM 2005 10 26 2005UALA01150 120051016A2130STBC10GG234 CLAMP BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN PRESSURE LOOSE A UALAB EMER. DESCENT J WARNING INDICATION CLCLIMB 1 WP29522UA 24931 EMERGENCY DESCENT DUE TO LOSS OF CABIN PRESSURE CONTROL. FOUND CLAMPS TO LEFT AND RIGHT CABIN AIR SUPPLY CHECK VALVES LOOSE. SECURED CLAMPS. LEAK AND OPS CHECKED OK PER MM21-31-00. RETURNED AIRCRAFT TO SERVICE. 2L72 4F4 FRTA2NM E17NE 20051026001052005102600105NM 2005 10 26 2005UALA01151 120051015A3150 WARNING LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE GENERATOR/APU ILLUMINATED A UALAO OTHER O OTHER LDLANDING 1 WP29514UA 24839 LANDED UNDER AMBER ALERT DUE TO INOP GENERATOR & APU OIL QTY STATUS MESSAGE. APU REMOVED. DIAGNOSTIC TEST FOUND NO HOC/ OIL LEAKS. APU DISSASSEMBLED FOR LIFE LIMITED PART. APU OIL QTY MESSAGE DISPLAYED ON EICAS. - NO HOC IN AMIS (ENGOIL) EXCEPT ONE AMBER HIT, & DECLINING! MECH NAME THAT DID WRITE UP IS: FESTA, M F/N118437 SFOMM SEQ 5002004 ON 10/17/05. DIAG TEST GOOD. NO OIL CONSUMPTION, NO HIDING OIL. SECOND STAGE TURBINE DISK CLOSE TO CYCLE LIMITED LIFE EXPIRATION (412 CYCLES REMAIN). REPLACED. REMOVED TURBINE PARTS SHOW NO SIGNS OF DISTRESS OR REASON FOR A NO START OR HOC CONDITION. NO CAUSE FOUND FOR APU REMOVAL AND REPORTED AS MAINTENANCE ERROR. 2L72 4F4 FRTA2NM E17NE 20051028000332005102800033NM 2005 10 28 SWAA053345 120051025A53216545409 FLOOR PANEL BOEING737 7373H4 1384600NM COCKPIT CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED D CHECK, FOUND COCKPIT FLOOR WEB CORRODED AT BS 259 TO BS 270, LBL 11 AND RBL 11. WL 208. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20051028000342005102800034NM 2005 10 28 SWAA053346 120051025A335065C34691 LIGHT BOEING737 737317 138447PNM MAIN CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29686SW 23175 DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT LOOSE AT ROW 16 DEF. SECURED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20051028000352005102800035NM 2005 10 28 SWAA053347 120051025A53306545774 SKIN BOEING737 7375H4 138449DNM BS 890 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29501SW 24178 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 890, STR 17L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051028000362005102800036NM 2005 10 28 SWAA053348 120051026A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29212WN 32485 EEPLS TRACK LOOSE AT ROW 1. SECURED TRACK PER MM. 2L72 4F RTA16WE 20051028000412005102800041NM 2005 10 28 SWAA053353 120051025A53306545776 SKIN BOEING737 7373H4 1384600NM BS 927 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29333SW 23697 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 24L. REPAIRED SKIN PER SWA EA AND SRM. 2L72 4F RTA16WE 20051028000442005102800044NM 2005 10 28 SWAA053362 120051026A53116546581 FRAME BOEING737 7373H4 1384600NM BS 992 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 992, RT SIDE, WL 208. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051028000502005102800050SO 2005 10 28 C2XA05TY057 120051024A3097 CONNECTOR EMB 135 EMB135ER 3260203SO ANTI ICE SYSTEM LOOSE A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2725504 145186 TYS - ON CLIMB THE CREW GOT A ICAS MESSAGE THAT THE WING ANTI-ICE FAIL, CREW RETURN TO BLOCK AND MAINTENANCE FOUND A PUSH PIN ON A CONNECTOR LOOSE. MAINTENANCE REINSERTED THE PIN AND OPS CHECKS WERE GOOD. AIRCRAFT WAS RELEASED TO SERVICE. 2L72 4F RTT00011AT 20051028000532005102800053NM 2005 10 28 DL75K050654 120051023A7120 BRACE BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 1 ENGINE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27640DL 23994 716564 NR 1 ENGINE UPPER DIAGONAL BRACE FUSE PIN INNER BORE CORRODED. REPAIRED SAME. 2L72 4F4 FRTA2NM E17NE 20051028000552005102800055NM 2005 10 28 DL73S050657 120051025A5330 SKIN BOEING737 737232 1384475NM BS 765 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27301DL 23073 A CRACK WAS FOUND IN THE FUSELAGE SKIN APPROX 2 INCHES LONG AT BS 765, S-19R. DOUBLER INSTALLED PER ER/A 451283-14, REF AD 2004-18-06 & 2005-13-30. 2L72 4F RTA16WE 20051028000562005102800056NM 2005 10 28 DL76S050658 120050728A5311145T10018 FRAME BOEING767 767332 1382001NM BS 903.5 CRACKED A DALAO OTHER O OTHER ININSP/MAINT 1 SO27116DL 23275 THE INNER CHORD OF THE RIGHT STA 903.5 FRAME WAS FOUND WITH A 0.25 INCH CRACK. CHORD WAS REPAIRED WITH AN ANGLE PER ACTS PP B767-53-20585, REF ER/A 099690-14AD. 2L72 4F RTA1NM 20051028000572005102800057NM 2005 10 28 DL733050659 120051020A5330 SKIN BOEING737 737347 1384647NM BS 727D CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27309WA 23442 A CRACK WAS FOUND IN THE FUSELAGE SKIN. CRACK IS APPROX 2 INCHES LONG AFT OF BS 727D, JUST BELOW STR 23L. REPAIRED WITH DOUBLER PER ER/A 451209-14AD, REF AD 2004-18-06. 2L72 4F RTA16WE 20051028000582005102800058NM 2005 10 28 DL76L050660 120051026A3244321002928 TIRE BOEING767 767332 1382001NM LT MLG DAMAGED A DALAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 SO271201P 28458 A/C REJECTED T/O AT 100 KTS DUE SWERVED RIGHT AND POPPING NOISE HEARD ON LEFT. PERFORMED HIGH ENERGY STOP INSPECTION NR 1 AND NR 2 TIRES HAD MINOR CHUNKING DAMAGE. REPLACED SAME AND REPLACED NR 2 BRAKE AS PRECAUTION. 2L72 4F RTA1NM 20051028000592005102800059EU 2005 10 28 05FDEA03493 120051025A2611 SMOKE DETECTOR AIRBUS300 A300F4605R 3930327EU E/E BAY MALFUNCTIONED A FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25679FE 793 INTERMITTENT AVIONICS SMOKE WARNING. DID NOT SMELL ANY SMOKE. REMOVED AND REPLACED AVIONICS SMOKE DETECTOR 11WA IAW A 300 MM 26-15-12-4. OPS CHECKS GOOD. SERVICEABLE PART CANNED FROM ACFT 653 MFG CG7GO-11. S/N ON AB1058 S/N OFF 1021. SERVICEABLE TAG B55383. OK FOR SERVICE. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION OFF MFG CG7G0-11. 2L72 4F RTA35EU 20051028000602005102800060NM 2005 10 28 05FDEA03506 120051026A5330 SKIN BOEING727 727225 1384077NM BS 330 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 FOUND SIX INCH DENT IN SKIN AT BS 330 STR 20R. REMOVED DAMAGE ON SKIN BS 330 BETWEEN STR 20R & 21R FABRICATED REPAIR DOUBLER AND FILLER. ALODINE, PRIME INSTALLED AND PAINTED AT BS 330 BETWEEN STR 20R & 21 R IAW SRM 53-30-3 FIG 1. 2L73 4F A3WE 20051028000672005102800067EA 2005 10 28 ASOA05772 120050919A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27907EV 7648 DURING AN OVERNIGHT INSPECTION IN VPS, THE OVERHEAD EMERGENCY LIGHT AT ROW 4 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE OVERHEAD EMERGENCY LIGHT AT ROW 4. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051028000722005102800072SO 2005 10 28 C2XA05IA121 120051020A3260852701 PROXIMITY SWITCH EMB 145 EMB145XR 3260214SO NLG INOPERATIVE A C2XAO OTHER N FALSE WARNING DEDESCENT 1 SW27161127961 7961 145660 ON DESCENT, A LARGE RUMBLING FELT AND HEARD AS POWER WAS REDUCED CONTINUING UNTIL GEAR WAS FULLY EXTENDED. PERFORMED A FLY-BY OF THE TOWER, AND LANDED WITHOUT INCIDENT. MX INSPECTED AIRCRAFT AND FOUND A LOOSE BONDING JUMPER, AND AIRCRAFT WAS APPROVED FOR A TEST FLIGHT. TEST FLIGHT WAS UNSATISFACTORY, AND ANOTHER FLY-BY OF THE TOWER CONFIRMED, NOSE LANDING GEAR DOORS REMAINED OPEN. THE AIRCRAFT LANDED AT RSW WITHOUT INCIDENT, WHERE THE AIRCRAFT WAS INSPECTED AND APPROVED FOR A FERRY FLIGHT TO IAH. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NLG DOOR SEQUENCING PROX SWITCH, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20051028000732005102800073SO 2005 10 28 C2XA05CL090 120051025A21508152916 SWITCH EMB 145 EMB145LR 3260212SO NR 2 A/C PACK FAULTY A C2XAB EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SW2715912 145439 CLE FLIGHT 2991 THE CREW REPORTED A STRONG ODOR/HOT AIR SMELL DURING ICING CONDITIONS. MAINTENANCE INSPECTED AND REPLACED THE NR 2 PACK DUCT OVERTEMP SWITCH. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20051028000742005102800074EA 2005 10 28 ASOA05771 120050918A2750860D10018ABCD FCU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A ASOAO OTHER F FLT CONT AFFECTED CRCRUISE 1 SO27872AS 7542 DURING CRUISE, THE CREW RECEIVED A FLAPS FAIL INDICATION. AFTER COMPLYING WIT THE QRH THE FLIGHT CONTINUED. AN EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE ELECTRONIC FLAP CONTROL UNIT (FECU). OPS CHECK OF THE FLAP SYSTEM IAW 27-51-05 WAS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051028000752005102800075EA 2005 10 28 ASOA05773 120050919A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27841AS 7300 DURING A C-CHECK, THE LT OB FS 280 CLIP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LT OB FS 280 CLIP IAW SRM 51-00-00. (M) 2L72 4F RTA21EA 20051028000762005102800076EA 2005 10 28 ASOA05798 120050924A5210 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27848AS 7339 DURING HANGAR MAINTENANCE, THE PASSENGER DOOR LOWER STEP WAS FOUND CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR LOWER STEP. (M) 2L72 4F RTA21EA 20051028000772005102800077 2005 10 28 USAABB05094 420051027A3441HG1050AD04 IRU BOEING767 767200 1385120NM GE CF6 CF680C2B2 30025NE FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19652US 24765 FLIGHT 948, PHL-BCN: AFTER TAKEOFF, CREW RECEIVED CENTER IRS FAULT LIGHT WITH ASSOCIATED EICAS MESSAGE, DIVERTED. REPLACED THE CENTER IRS. NO FURTHER DIFFICULTIES. 2L72 4F4 FRTA1NM E13NE 20051028000792005102800079EA 2005 10 28 QXEA200501382 120051024A801113739002 SWITCH CNDAIRCL600 CL6002C10 1390015EA NR 2 ENG STARTERMALFUNCTIONED A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09618QX 10205 PDX - DURING PUSHBACK FOR FLIGHT 2471, NR 2 ENGINE WILL NOT START. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE PLACED ON MEL 80-11-3 RSI 346266. MAINTENANCE REPLACED THE STARTER CONTROL VALVE ON 10/24 WITH NO HELP. MEL CONTINUED. ON 10/25 THE K32 RELAY ON THE PCB4 WAS REPLACED WITH NO HELP. REPLACED THE NR 2 ENGINE FADEC WITH NO HELP. REPLACED THE STOP SWITCH ON THE START CONTROL PANEL IN THE COCKPIT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. MEL CLEARED. 2L72 4F RTA21EA 20051028000842005102800084NM 2005 10 28 AALA20050708 120051019A3350BPS73 BATTERY PACK BOEING767 767223 1385123NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21321AA 22322 AFW BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS ON RIGHT HAND SIDE FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS ON RIGHT HAND SIDE FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20051028000872005102800087NM 2005 10 28 AALA20050701 120051023A3350 CONNECTOR BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21631AA 24589 SFO - EMERGENCY LIGHTS AT SEAT 20D INOPERATIVE. REPAIRED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT SEAT 20D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20051028000882005102800088NM 2005 10 28 AALA20050703 120051026A3350 BATTERY PACK BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21392AN 29429 JFK - LAST THREE LEFT AFT EMERGENCY OUTSIDE LIGHTS INOPERATIVE. RESET BATTERY PACK M738 FOR LAST THREE LEFT AFT EMERGENCY OUTSIDE LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20051028000922005102800092WP 2005 10 28 AALA20050705 120051026A3350 BATTERY DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21570AA 49352 DFW - EMERGENCY EXIT LIGHT IN OVERHEAD TAILCONE INOPERATIVE. REPLACED BATTERIES AND BULBS FOR EMERGENCY EXIT LIGHT IN OVERHEAD TAILCONE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20051028000932005102800093NM 2005 10 28 AALA20050702 120051024A3350233T32101033 CONTROL PANEL BOEING767 767323 1385205NM COCKPIT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21354AA 24035 LAX EMERGENCY LIGHT UNARMED LIGHT DOES NOT ILLUMINATE WITH LIGHT DECK EMERGENCY LIGHT SWITCH IN OFF POSITION. REPLACED PILOTS EMERGENCY LIGHT CONTROL PANEL FOR INOPERATIVE EMERGENCY LIGHT UNARMED LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20051028000972005102800097EA 2005 10 28 VNAA0510012 120051016A7810NAS6303U4U9 BOLT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EXHAUST NOZZLE FAILED A VNAAO OTHER O OTHER NRNOT REPORTED 1 GL05244PS3440 7912 AFTER POST FLIGHT INSPECTION THE CREW REPORTED THE LEFT ENGINE EXHAUST NOZZLE AND FAIRING WERE MISSING. MAINTENANCE INSPECTED THE AIRCRAFT AND DETERMINED ALL 31 ATTACH BOLTS HAD FAILED AND WERE ALSO MISSING. ALL MISSING AND DAMAGED PARTS WERE REPLACED WITH SERVICEABLE PARTS IAW BOMBARDIER AND GENERAL ELECTRIC MAINTENANCE MANUALS. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20051028000992005102800099WP 2005 10 28 05FDEA03499 120051026A5313 LONGERON DOUG DC10 DC1010 3022110WP BS 2122-2163 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 UPPER INTERNAL FUSELAGE AFT BODY FOUND NR1 LONGERON REPAIRED BETWEEN STA 2122 TO STA 2163 AT LONG 51 RT SIDE. REPAIRED IAW EA 8-5310-90131. 2L73 4F A22WE 20051028001082005102800108NM 2005 10 28 SWAA053357 120051026A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29429WN 33658 EEPLS TRACK COVER CRACKED AT FWD END. REMOVED AND REPLACED COVER PER MM. 2L72 4F RTA16WE 20051028001102005102800110NM 2005 10 28 SWAA053359 120051026A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM BS 787 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051028001112005102800111NM 2005 10 28 SWAA053360 120051026A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM BS 787 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051028001122005102800112SO 2005 10 28 C2XA05SD028 120051007A3350 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714977 145175 SDF - RIGHT AFT WING EMERGENCY LIGHT INOP. REMOVED AND REPLACED RIGHT AFT WING EMERGENCY LIGHT BULB, OPS CHECK GOOD IAW EMB 145 AMM 33-50-07, 33-50-00. 2L72 4T RTT00011AT 20051028001132005102800113SO 2005 10 28 C2XA05CL086 120051010A335066903 LIGHT EMB 145 EMB145 3260210SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712957 145080 CLE - FLIGHT 2917 THE CREW REPORTED THE 1ST ROW OF THE AISLE PATH EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE LIGHT PATH STRIP. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20051028001152005102800115SO 2005 10 28 C2XA05IA111 120051009A335078241 INVERTER EMB 145 EMB145 3260210SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714959 145091 IAH - DURING MAINTENANCE INSPECTION, THE AFT CEILING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20051028001162005102800116SO 2005 10 28 C2XA05IA112 120051010A3350B6245 LIGHT EMB 145 EMB145EP 3260221SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714938 145029 IAH - DURING MAINTENANCE INSPECTION, THE SERVICE DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20051028001202005102800120NM 2005 10 28 QXEA200501385 120051018A5730 ACCESS PANEL DHAV DHC8 DHC8202 2809007NM LT WING DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09345PH 476 PDX - THE LEFT WING LADDER PLATE FOR ACCESS PANEL 522AT HAS A CHIP IN THE EDGE OF THE SIXTH SCREW HOLE IN THE AFT ROW, COUNTING FROM THE INBOARD AFT EDGE. REPAIRED IAW RD 8-57-1471 AND HORIZON AIR EA 2-57-333. 2H72 4T RTA13NM 20051028001222005102800122EA 2005 10 28 QXEA200501380 120051026A2150 A/C PACK CNDAIRCL600 CL6002C10 1390015EA RIGHT MALFUNCTIONED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09612QX 10042 SJC - ON FLIGHT 2528 RETURNED TO THE GATE FOR A RIGHT AIR CONDITIONING PACK CAUTION MESSAGE. MAINTENANCE PLACED THE RIGHT PACK ON MEL 21-51-1 B- RSI NUMBER 353012. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20051028001312005102800131EA 2005 10 28 SWIA200515736 120050514A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07918SW 7645 L-BRACKET (CLIP) AT OUTBOARD LEFT HAND 9' LBL ATTACHMENT TO 280 FS BEAM IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED CLIP LEFT HAND INBOARD STA 280.00 LBL 9 IAW CRJ200 SRM 51-42-06 PG 1-4. 2L72 4F RTA21EA 20051031000012005103100001EA 2005 10 31 SWIA200515737 120050514A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07918SW 7645 L-BRACKET CLIP AT INBOARD RIGHT HAND 9' LBL ATTACHMENT TO 280 FS FLOORBEAM IS CRACKED AT TOP RADIUS. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED CLIP STA 280 INBOARD RBL 9 IAW CRJ200 SRM 51-42-06 PG 1-17. 2L72 4F RTA21EA 20051031000042005103100004SO 2005 10 31 SWIA200515740 120051023A3320 SOCKET EMB 120 EMB120ER 3260203SO SEAT LIGHT SMOKE A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM07584SW 120352 SIDEWALL LIGHT ABOVE SEAT 6A EMITS SMOKE, STRONG ELECTRICAL ODOR AND BURN MARK IN CEILING PANEL. REPLACED LIGHT FIXTURE IN CEILING ABOVE SEAT 6A. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20051031000052005103100005EA 2005 10 31 SWIA200515741 120051023A2750855D10011 POSITION SENSOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07953SW6663 6663 7813 FLAPS FAIL CAUTION MSG. INSTALLED SERVICEABLE BPSU IAW 27-56-00. ALSO ADJUSTED FECU POTS, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051031000062005103100006EA 2005 10 31 SWIA200515742 120051024A2741 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07963SW 7865 STAB CH1 KICKED OFF. REPLACED CAPTAINS TRIM SWITCH. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051031000092005103100009EA 2005 10 31 SWIA200515745 120051018A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA FLOORBEAM CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07924SW 7681 FUSELAGE; FLOORBEAM ATTACH CLIPS ARE CRACKED I/B AND O/B FS 280.00 RBL 9.0. ITEM FOUND AT C-CHECK INSPECTION. 2L72 4F RTA21EA 20051031000112005103100011EA 2005 10 31 SWIA200515747 120051018A5320 WEB CNDAIRCL600 CL6002B19 1900309EA BS 628.5 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07924SW 7681 AFT EQUIP BAY; ESB LOWER WEB IS CRACKED ON RIGHT SIDE AT PANEL CUTOUT; FS 628.50; RBL 38.40. ITEM FOUND AT C-CHECK INSPECTION. 2L72 4F RTA21EA 20051031000122005103100012EA 2005 10 31 SWIA200515748 120051018A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 621 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07924SW 7681 CARGO COMPT; FLOORBEAM ANGLE IS CRACKED; FS 621.0 - LBL 40.0. ITEM FOUND AT C-CHECK INSPECTION. 2L72 4F RTA21EA 20051031000142005103100014NE 2005 10 31 HALA0500873 220050819A7321 EEC BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE RT ENGINE FAILED A HALAO OTHER O OTHER NRNOT REPORTED 1 WP13484HA 55129 ENGINE RT SYSTEM FAIL MESSAGE ILLUMINATED. REMOVED AND REPLACED EEC, OPS CHECK OK. AIRCRAFT RELEASED FOR SERVICE. (K) 2L72 4F4 FTRA6WE E00061EN 20051031000172005103100017NM 2005 10 31 USAA051027 120050817A52106555478502 GATE BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU AFT PAX DOOR CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19444US40668 24862 BFM - Q2 - DOOR GATE SKIN, 29 INCH L X .250 INCH W, CORROSION; LEVEL 2; TASK C53-100-01, AFT ENTRY DOOR BOTTOM GATE LOWER EDGE OF SKIN. REMOVED AND REPLACED AFT ENTRY DOOR BOTTOM GATE IAW MM, SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051031000242005103100024CE 2005 10 31 S2YA05042 120050714A3297420000202 CIRCUIT BREAKER BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA MLG INTERMITTENT A S2YAO OTHER J WARNING INDICATION APAPPROACH 1 GL13881SK UE88 DURING APPROACH OF FLIGHT, THE CREW REPORTED THE GEAR WAS NOT EXTENDING NORMALLY BUT IS THEY JIGGLED THE HANDLE IT WOULD OPERATE. THE CREW PUMPED THE GEAR DOWN AND ACHIEVED THREE GREEN. MAINTENANCE FOUND INTERMITTENT HIGH OHMS READING THROUGH LANDING GEAR CIRCUIT BREAKER. INSPECTED LANDING GEAR CONTROL WIRING, CIRCUIT BREAKERS AND CONNECTORS NO OTHER DEFECTS WERE NOTED. MAINTENANCE REPLACED THE CIRCUIT BREAKER AND OPS CHECKED THE SYSTEM WITH NO FURTHER DEFECTS NOTED. 2L72 4T3 TRTA24CE E2NE 20051031000332005103100033EU 2005 10 31 COE2005F00003 120051010A5320 SILL AEROSPATR42 ATR42320 8680930EU PWA PW121 PW121 52124NE HAMSTD14SF 14SF5 NE FWD CARGO DOOR LOOSE A COEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM13902FX 175 120623 891122 CARTGO DOOR WARNING LIGHT ILLUMINATED AFTER TAKEOFF. PILOT ELECTED TO RETURN TO DEPARTURE. NO EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. PILOT INSPECTED CARGO DOOR AND FOUND THAT IT WAS CLOSED PROPERLY, HOWEVER THE DOOR SILL GUARD WAS PRESSING AGAINST THE CARGO DOOR, PREVENTING COMPLETE CLOSURE. THE PILOT STOWED THE SILL GUARD TO THE IB POSITION AND THE UNLOCK LIGHT EXTINGUISHED. THE CARGO STC HOLDER HAS A SB TO CORRECT THIS PROBLEM, AND THE PARTS ARE SCHEDULED TO BE AVAILABLE IN NOVEMBER. (K) 2H72 4T4 TRTA53EU E20NE 6 CP7NE 20051031000342005103100034CE 2005 10 31 JDW2005F00000 120051005A323062411132 PIN CESSNA650 650 2076802CE GARRTTTFE731TFE731* 01518WP MLG LOOSE E JDWAO OTHER O OTHER NRNOT REPORTED 1 CE09650DA7929 6500114 RT MAIN GEAR OLEO STRUT WOULD NOT COMPRESS AFTER LANDING, MORE THAN 50 PERCENT OF NORMAL. AC WAS JACKED, SERVICE OF THE STRUT WAS CHECKED NORMALLY. NEX LANDING, STRUT WOULD AGAIN NOT COMPRESS. OLEO WAS REMOVED FROM AC AND DISASSEMBLED. METERING PIN INSIDE STRUT WAS LOOSE AND MOVING AROUND INSIDE THE STRUT. FUTURE EXAMINATION OF METERING PIN REVEALED THAT NYLON THREAD LOCKING DEVICE SHOWED NO EVIDENCE OF EVER CONCTIGN THE THREADS INSIDE THE UPPER BARREL. THE LOCKING DEVVICE WAS TOO DEEP IN CRCESS PROVIDED IN METERING PIN. THIS CONDITION DID NOT PROVIDE SELF-LOCKING FEATURE THUS ALLOWED PIN TO ROTATE AND COME LOOSE. DAMAGE TO UPPER BARREL OF OLEO WAS EXTENSIVE AND HAD TO BE REPLACED. 2L72 4F4 F A9NM E6WE 20051031000482005103100048NE 2005 10 31 DAT2005F00013 220050914A7230PT6A67R COMPRESSOR STBROSSD3 SD360 8100606EU PWA PT6 PT6A67R 52043NE LT ENGINE SURGES E DATAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 GL13136LR SH3752 PCE106089 AS POWER WAS BROUGHT TO TAKEOFF SETTINGS, THE RT TORQUE INSTANTLY INCREASED FROM 1400 LBS. THE RISE IN TORQUE OF THE LT ENGINE WAS FOLLOWED BY 2 COMPRESSOR STALLS, AT WHICH POINT THE TAKEOFF WAS ABORTED. AFTER A RUNUP WAS PERFORMED BY MAINTENANCE, IT WAS FOUND THE RTOP WAS SET INCORRECTLY. THE RTOP WAS MEL`D ON THE LT AND RT ENGINES. THE AIRCCRAFT WAS RETURNED TO MAINTENANCE FOR REPAIR. MAINTENANCE RIGGED THE RTOP SWITCHES IAW MM. OPS CHECK GOOD AND THE AC WAS RETURNED TO SERVICE. 2H72 4T4 T A41EU E26NE 20051031000582005103100058NE 2005 10 31 Y2PA05014 220050901A7200 ENGINE AMD FALC20FALCOND 2720304EU GE CF700 CF7002D 30010NE BIRD STRIKE E Y2PAA UNSCHED LANDING CJ F.O.D. WARNING INDICATION CLCLIMB 1 GL23821AA 203 DURING TAKEOFF, JUST AFTER ROTATION, AIRCRAFT ENCOUNTERED A FLOCK OF BIRDS, RESULTING IN FOD TO BOTH ENGINES AND SUBSEQUENT SHUTDOWN OF BOTH ENGINES. AIRCRAFT HEAVILY DAMAGED. INVESTIGATION UNDER WAY. NTSB AND FAA NOTIFIED. (K) 2L72 4F4 F A7EU E7EA 20051031000612005103100061EU 2005 10 31 KBM2005F00295 120050925A21000500521 MOTOR SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE EVAPORATOR INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19966SH2177 3787 FORWARD EVAPORATOR MOTOR, INOPERATIVE, REPLACED WITH NEW UNIT. (K) 1G71 3U3 U H9EU E19EU 20051031000632005103100063NM 2005 10 31 UIEA200500122 120050830A5321 PRESSURE PANEL BOEING747 7472D7B 1384803NM GE CF6 CF650E2 30018NE BS 1241 CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15524MC 21784 D-CHECK, FUSELAGE STA 1241 SLOPING PRESSURE DECK WEB WAS FOUND WITH CRACK AT DUCT CUTOUT. THE CRACKED AREA REPAIRED BY CUTTING EXISTING WEB SECTIONS BETWEEN UPPER EDGE OF THE SLOPING DECK AND REAR SPAR AND FROM BL 0 TO TRIM LINE. HFEC INSPECTED THE EDGE OF THE WEB TRIM. A NEW REPAIR WEB SECTION WAS INSTALLED. (K) 2L74 4F4 FRTA20WE E23EA 20051031000672005103100067GL 2005 10 31 ALG2005F00075 220050824A720023004545 ENGINE BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL VIBRATION E ALGAO OTHER EJ VIBRATION/BUFFET WARNING INDICATION NRNOT REPORTED 1 SW03187AL 51135 CAE895516 ON REPOSITION TO THE FLY AWAY, A LOUD BANG WAS HEARD FOLLOWED BY A NOTICEABLE CHANGE AND A VIBRATION IN THE AIRCRAFT. AC FELT UNSTABLE AND WAS SET DOWN. DURING COAST DOWN/ SHUTDOWN AC CONTINUED TO HAVE ODD VIBRATION/ OSCILLATION. MAINTENANCE NOTIFIED. REMOVED AND REPLACED ENGINE ASSY IAW MM AND THE APPLICABLE STC. WORK ACCOMPLISHED 8/28/2005. COMP, GRIND NOISE, OIL PUMP. (K) 1G71 3U3 U H2SW E1GL 20051031000682005103100068SW 2005 10 31 ALG2005F00076 120050917A6320206040004111 TRANSMISSION BELL 206 206L1 1182107SW ALLSN 250C 250C28B 03013GL MAIN ROTOR MAKING METAL E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW033188P 45778 DURING CRUISE FLIGHT, TRANSMISSION CHIP LIGHT ILLUMINATED. PILOT LANDED ASAP AND PERFORMED CHIP PLUG CHECK IAW THE OPS MANUAL PROCEDURE, WHILE IN COMMUNICATION WITH MAINTENANCE. UPON COMPLETION OF 30 MINUTE PENALITY RUN AND LEAK CHECK, AC WAS FLOWN. MAINTENANCE INSPECTED CHIP PLUGS AND FILTER.. METAL FOUND DURING THIS INSPECTION GROUND AC FOR TRANSMISSION CHANGE MM. (K) 1G71 3U3 U H2SW E1GL 20051031000782005103100078 2005 10 31 KBM2005F00292 420050925A3422505031904 GYRO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE DIRECTIONAL SPINNING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19351WM 2167 DIRECTIONAL GYRO WAS SPINNING, REPLACED WITH OVERHAULED UNIT. (K) 1G71 3U3 U H9EU E19EU 20051031000792005103100079GL 2005 10 31 I5HA0558005 220050903A72006874100 ENGINE CVAC 340 340CVAC 242270AWP ALLSN 501D 501D13 03004GL LEFT FAILED A I5HAO OTHER O OTHER NRNOT REPORTED 1 GL23584E 7083 24 500963 WHILE ENROUTE, THE PILOT NOTICED A SIGNIFICANT DROP IN HORSEPOWER ON THE LT ENGINE. THE PILOT PERFORMED EMERGENCY SHUTDOWN OF THE LT ENGINE USING THE (E) HANDLE. AC LANDED UNEVENTFULLY AND TAXIED TO FACILITY. INSP OF LT ENGINE REVEALED A CATASTROPHIC FAILURE OF THE LT TURBINE. A 10 INCH X 2 INCH HOLE WAS FOUND IN THE SIDE OF THE TURBINE CASE. THE COWLING BENEATH THE TURBINE WAS DAMAGED AND THE NR 1 TIRE WAS PUNCTURED BY TURBINE DEBRIS. ENTIRE ENGINE QEC WAS REMOVED AS PRECAUTIONARY MEASURE. AS AC HAS BEEN INDUCTED INTO A HEAVY, REPORT WILL REMAIN OPEN UNTIL AC IS RETURNED TO SERVICE. (K) 2L72 4R4 T 6A6 E282 20051031000852005103100085NE 2005 10 31 KCB2005F00000 220050929A7200CF7002D ENGINE AMD FALCONFALCON20 2730103EU GE CF700 CF7002D 30010NE RIGHT FLAMED OUT E KCBAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION NRNOT REPORTED 1 GL23998CK12747 98 304428 RT ENGINE FLAMED OUT DUE TO TURBULANCE. ENGINE WAS RESTARTED AND CONTINUED TO ORIGINAL DESTINATION. CAPTAIN CONTACTED MAINTENANCE DEPARTMENT. ENGINE WAS INSPECTED IAW OPS MANUAL WITH NO DEFECTS NOTED. THE FLIGHT WAS CONTINUED WITH NO OTHER ABNORMAL ENGINE OPERATION. (K) 2L72 4F4 FRTA7EU E7EA 20051031000982005103100098 2005 10 31 KBM2005F00298 420051010A34225050031904 GYRO SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE DIRECTIONAL INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P88 2347 DIRECTIONAL GYRO, UNIT FLAG WILL NOT RETRACT, SPINS, REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20051031001022005103100102NM 2005 10 31 AMTA200500883 120051012A2612 FIRE LOOP BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE LT ENGINE MALFUNCTIONED A AMTAO OTHER N FALSE WARNING CRCRUISE 1 GL11552TZ 32586 EICAS STATUS MESSAGE: L ENGINE FIRE LOOP 1. ACCOMPLISHED TEST IAW FIM 26-11-00. OPS OK. (K) 2L72 4F4 FRTA2NM E12EU 20051031001082005103100108CE 2005 10 31 AJC2005F00012 120050826A3260MS243311 SQUAT SWITCH BEECH MU300 400A 1155402CE PWA JT15 JT15D1 52060NE LT WHEEL ASSY DEFECTIVE A AJCAO OTHER J WARNING INDICATION CLCLIMB 1 EA25400HS1998 RK314 DEPARTED, ENROUTE, AFTER TAKEOFF THE CREW REPORTED THAT THE LANDING GEAR HANDLE WAS LOCKED IN THE DOWN POSITION AND THEY COULD NOT RETRACT THE GEAR. THE LANDING GEAR DOWN LOCK OVER RIDE WAS ENGAGED AND THE GEAR RETRACTED NORMALLY. ON DESCENT, THE CREW REPORTED THAT THEY EXTENDED THE GEAR AND GOT A GREEN NOSE AND LT MAIN LIGHT ONLY. THEY CYCLED THE GEAR TWICE AND GOT 3 GREEN, DOWN AND LOCKED INDICATION ON THE SECOND TRY. THEY CONTINUED ON AND LANDED SAFELY WITHOUT INCIDENT. THE CREW DID NOT DECLARE AN EMERGENCY. RT DOWNLOCK SWITCH, PN 41HE1-6, DEFECTIVE, RT MLG ASSEMBLY. (K) 2H72 4F4 FRTA16SW E1NE 20051031001112005103100111EA 2005 10 31 A6WA200540302 120050905A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE BS 621-625.3 CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31424AW 7656 RT FS621-625.3 INTERCOSTAL AT STR 14R IS CRACKED NEAR RADIUS APPROX 1.2 INCHES LONG. REMOVED CRACKED INTERCOSTAL AND INSTALLED NEW INTERCOSTAL IAW SRM. (K) 2L72 4F4 FRTA21EA E15NE 20051031001172005103100117NE 2005 10 31 ILD2005F00001 220050901A7310 MANIFOLD SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE ENGINE FUEL LEAKING E ILDAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 WP13451H 8857 2876 3231 9643 ON THE FIRST FLIGHT OF THE DAY PILOT COULD NOT START THE AIRCRAFT DUE TO FUEL COKING AT GAS GENERATOR INJECTION MANIFOLD. REMOVED ENGINE ASSY AND INSTALLED SAME TYPE. CLEAR GROUND RUN AND LEAK CHECKED, OPS FLIGHT CHECK. (K) 1G71 3U3 U H9EU E19EU 20051031001192005103100119 2005 10 31 KBM2005F00278 420050912A34215040017901 GYRO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE ATTITUDE INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19351WM 2167 H.GYRO, UNIT INOPERATIVE. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051031001372005103100137NM 2005 10 31 GAIA05024OP 120050912A5210507945152 SKIN BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE L1 DOOR CRACKED A GAIAO OTHER O OTHER NRNOT REPORTED 1 SW07180AX 20041 NO FLIGHT; DURING INSPECTION A SMALL CRACK WAS FOUND ON THE L1 DOOR UPPER AFT BEARING WHICH CAUSED THE DOOR FRAME TO CRACK. REMOVED AND REPLACED L1 DOOR. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L73 4F4 F A3WE E2EA 20051031001392005103100139EA 2005 10 31 A6WA200540314 120051017A2150 A/C PACK CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LEFT CONTAMINATED A A6WAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 GL31430AW 7719 UPON CLEANING OIL RESIDUE FROM APU, FOUND LT PACK SMOKING SLIGHTLY FROM EXHAUST. FOUND OIL CAME FROM APU OIL COOLER RESIDUE. OPERATED LT PACK IAW AMM, NO FUMES OR SMOKE NOTED FROM AIR CONDITIONING SYSTEM OR EXHAUST. (K) 2L72 4F4 FRTA21EA E15NE 20051031001402005103100140EU 2005 10 31 RMX2005F00000 120051011A6220109011205105 DAMPER AGUSTAA109 A119 0261102EU PWA PT6 PT6* 52043EA MAIN ROTOR HEAD LEAKING D RMXAO OTHER O OTHER NRNOT REPORTED 1 WP07820NA664 14011 DAMPER HYDRAULIC FLUID COMPLETELY LEAKED OUT OF END SEAL IN A 0.1 HOUR FLIGHT. (K) 1G72 3U3 T H7EU E2NE 20051031001432005103100143CE 2005 10 31 SFO2005F00002 120050525A7120AN737AM BOLT BEECH 58 58 1152740CE CONT O550 IO550C SO RT ENGINE MOUNT LOOSE E SFOAO OTHER O OTHER NRNOT REPORTED 1 EA23917SF300 TH2037 685354 WHILE PERFORMING A SCHEDULED INSPECTION, 3 OF THE 4 ENGINE MOUNT (CUSHION) BOLTS WERE FOUND LOOSE. 2 REQUIRED 1 FULL TURN TO TIGHTEN, AND THE 3RD TOOK ALMOST 2 TURNS TO TIGHTEN. THE SELF LOCKING FEATURE OF THE NUTS WAS CHECKED AND APPEARED TO BE OK. IT CAN ONLY BE ASSUMED THAT THE BOLTS WERE NOT PROPERLY TORQUED BY THE MFG AT ENGINE INSTALLATION. THE BOLTS WERE TORQUED IAW SRM AND THE OPPOSITE ENGINE MOUNT BOLTS WERE CHECKED AND FOUND TO BE PROPERLY TORQUED. (K) 1L72 3O3 O 3A16 E3SO 20051031001442005103100144EU 2005 10 31 USAA051013 120050817A5340 CLIP AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19110UW13254 1112 PIT - S2 - CLIP, 2 INCH X 1 INCH CORROSION; LEVEL 1; TASK JA-220-53500, FRAME C-20 AND AFT CORNER OF FWD SERVICE DOORWAY. REPAIRED WITH MANUFACTURED PART IAW SRM. (K) 2L72 4F4 FRTA28NM E38NE 20051031001452005103100145EU 2005 10 31 USAA051016 120050817A5315D5347217220400 FLOORBEAM AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FR 68-69 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19742US15033 1275 PIT - S1 - FLOORBEAM, 1 INCH X 1 INCH CORROSION; LEVEL 2; TASK JA260-53500, FRAME 68-69, Y120MM. REMOVED AND REPLACED FLOORBEAM WITH SAME PN. (K) 2L72 4F4 FRTA28NM E37NE 20051031001502005103100150EU 2005 10 31 KBM2005F00280 120050917A5210350A25153202 LOCK SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE SLIDING DOOR CYLBROKEN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH5577 2884 CENTER CYLINDER LOCK ON SLIDING DOOR WAS BROKEN. REPLACED HANDLE AND LOCK WITH NEW. (K) 1G71 3U3 U H9EU E19EU 20051031001522005103100152EU 2005 10 31 USAA051017 120050817A5315D5347218820400 FLOORBEAM AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FR 67 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19742US15033 1275 PIT - S1 - FLOORBEAM, .5 INCH X .7500 INCH X 1 INCH SQ. CORROSION; LEVEL; TASK JA-260-53500, FRAME 67 Y117MM. REMOVED AND REPLACED WITH SAME PN. (K) 2L72 4F4 FRTA28NM E37NE 20051031001602005103100160 2005 10 31 GAIA05026 420051014A2565101660105 SLIDE BOEING737 7373Y0 1384671NM CFMINTCFM56 CFM563C1 13802EU R1 DOOR DEPLOYED A GAIAO OTHER O OTHER TXTAXI/GRND HDL 1 SW07106KH 24916 POST ARRIVAL AND PARKING, GROUND CREW WAS OPENING R1 DOOR, SLIDE WAS STILL ARMED, EXIT SLIDE DEPLOYED. NO DAMAGE OR INJURY OCCURRED. REMOVED AND REPLACED R1 DOOR SLIDE AS REQUIRED. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4F4 FRTA16WE E21EU 20051031001622005103100162NE 2005 10 31 DAT2005F00014 220050915A7230PT6A67R GAS GENERATOR STBROSSD3 SD360 8100606EU PWA PT6 PT6A67R 52043NE LT ENGINE SURGES E DATAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 GL13136LR SH3752 PCE106089 ABORTED THE TAKEOFF DUE TO THE LT RTOP INDICATOR DID NOT ILLUMINATE ON THE TAKEOFF. AC WAS RETURNED TO MAINTENANCE HANGAR. CHIEF INSPECTOR TESTED THE RTOP SYSTEM ON THE GROUND. OPS CHECK GOOD IAW MM. AC WAS RETURNED TO SERVICE. (K) 2H72 4T4 T A41EU E26NE 20051031001642005103100164NE 2005 10 31 KBM2005F00301 220050926A7200 BEARING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE ENGINE WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH485 2884 HALF SHELL BEARING, UNIT WORN, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051031001682005103100168NM 2005 10 31 UIEA200500120 120050829A3230 TRUNNION BOEING747 7472D7B 1384803NM GE CF6 CF650E2 30018NE MLG CHAFED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15524MC 21784 D-CHECK, RECESSED MARK ON RT BODY GEAR IB TRUNNION SUPPORT FITTING. THE RECESSED MARK WAS BLENDED OUT WITH A MINIMUM 63 RHR SURFACE FINISH. 10X VISUALLY AND HFEC INSPECTED TO ENSURE CRACK AND CORROSION FREE CONDITION. ALODINED AND REINSTATED THE FINISH. FILLED THE VOID WITH SEALANT. (K) 2L74 4F4 FRTA20WE E23EA 20051031001722005103100172NM 2005 10 31 USAA051029 120050817A5320US65516989LF SPLICE BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU BS 907 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19444US40668 24862 BFM - Q2 - STRINGER SPLICE, .250 INCH, STA 907, STR; CRACK ON FASTENER HEAD, STA 907, STRINGER CRACK ON FASTENER HEAD. INSTALLED REPAIR/ FAB SPLICE ON STRINGER IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051031001732005103100173NM 2005 10 31 USAA051009 120050816A5314 KEELBEAM BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU BS 673-678 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US 23933 CLT - Q6 - ANGLE, ON KEELBEAM COMPOSITE SKIN ATTACH ANGLE HAS FRETTING WORN INTO IT, 5 INCHES X 1 INCH. CORROSION, STA 673, STA 678, LBL 8. REMOVED CORROSION, BLENDED, AND TREATED IAW SRM, DWG. (K) 2L72 4F4 FRTA16WE E21EU 20051031001832005103100183EU 2005 10 31 DAT2005F00012 120050714A324493GA112 TIRE STBROSSD3 SD330 8100602EU PWA PT6 PT6A45R 52043EA LT MLG DEFLATED E DATAO OTHER O OTHER TXTAXI/GRND HDL 1 GL13334AC 223 SH3029 THE LT MAIN WHEEL ASSY DEFLATED DURING TAXI AFTER LANDING. A MECHANIC WAS DISPATCHED AND REMOVED THE DEFLATED LT MAIN WHEEL AND REPLACED WITH A SERVICEABLE MAIN WHEEL ASSY IAW MM. THE AIRCRAFT WAS RETURNED TO SERVICE. (K) 2H72 4T4 T A41EU E4EA 20051031001872005103100187EU 2005 10 31 ASOA05741D 120050907A2750S2901200000060 FLAP SYSTEM AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE TE FLAPS MALFUNCTIONED A ASOAO OTHER O OTHER NRNOT REPORTED 1 SO27635AS2711427114 372 FLAP CONTROL ASSEMBLY, MALFUNCTIONED. (K) 2H72 4T4 TRTA53EU E20NE 20051031001902005103100190CE 2005 10 31 V2J2005F00000 120050915A27503903814010011 FLAP SYSTEM RAYTHN390 390 7150030CE TE FLAPS FAILED E V2JAO OTHER O OTHER NRNOT REPORTED 1 EA25311SL276 RB120 THE FLAP/SPOILER SYSTEM ON THIS AIRCRAFT IS PLAGUED WITH FAILURES, THERE ARE MORE OF THESE REPORTS TO FOLLOW. (EA25200510358) (K) 17 2 3F RTA00010WI 20051031001962005103100196EU 2005 10 31 KBM2005F00256 120050908A7712305731365 GAUGE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE TORQUE INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19115SH 3141 TORQUE GAUGE INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. (K) 1G71 3U3 U H9EU E19EU 20051031002032005103100203NM 2005 10 31 UIEA200500166 120051018A5270602ENG01 SWITCH BOEING747 7472D3B 1384805NM GE CF6 CF650E2 30018NE AFT CARGO DOOR DEFECTIVE A UIEAB EMER. DESCENT N FALSE WARNING CLCLIMB 1 EA15506MC 21252 AT APPROX FL 280, AFT CARGO LIGHT ON FE`S PANEL AND CARGO DOOR LIGHT ON PILOTS PANEL BEGAN FLICKERING, SHORTLY IT CAME ON STEADY. DESCENDED AC TO FL250 AND ACCOMPLISHED FHB PROCEDURES FOR DOOR OPEN LIGHT. AT NO TIME EXPERIENCED PRESSURIZATION PROBLEMS PRIOR TO DEPRESSURIZING AIRCRAFT. FOUND AFT CARGO WARNING SWITCH INOPERATIVE. REMOVED AND REPLACED AFT CARGO WARNING SWITCH IAW MM. OPS CHECK NORMAL. (K) 2L74 4F4 FRTA20WE E23EA 20051031002072005103100207EU 2005 10 31 COE2005F00002 120051003A242215188E INVERTER FOKKERF27 F27MK600 4990706EU RROYCEDART DART5327R 54509NE LT AC INOPERATIVE A COEAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM13741FE37 10387 17546 DEPARTURE, ENROUTE, NR 1 INVERTER WENT OFF LINE AND WOULD NOT COME BACK ON. CREW REPORTED A STRONG BURNING ODOR BUT NO SMOKE. AIRCRAFT DIVERTED. THE NR 1 INVERTER CB WAS POPPED. THE NR 1 INVERTER WAS REMOVED AND REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE. (K) 2H72 4T4 T A817 E297 20051031002182005103100218 2005 10 31 KBM2005F00270 420050916A2312064105430 RADIO SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1D NE VHF FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1937SH 166 2300 VHF RADIO, DISPLAY BLANK OFF AND CAN`T TRANSMITT OR RECEIVE. REMOVED AND REPLACED VHF RADIO. (K) 1G71 3U3 UNCH9EU E19EU 20051031002192005103100219EU 2005 10 31 KBM2005F00275 120050904A6220350A332150001 BALL END SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE MAIN ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH478 2884 BALL END, UNIT HAS EXCESSIVE PLAY, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051031002312005103100231SO 2005 10 31 GUU2005F00047 120050828A2121EVAC2322C2 FAN EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE CABIN SHORTED A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO17266AS 120188 AFTER TAXING TO 8R, RT PACK FAIL ANNUNCIATOR ILLUMINATED AND SMOKE NOTICED IN CABIN. RETURNED TO GATE. REPLACED RT GROUND FAN. (K) 2L72 4T4 TRTA31SO E20NE 20051101000022005110100002WP 2005 11 1 05FDEA03577 120051028A5311 FRAME DOUG DC10 DC1030 3023501WP GE CF6 CF66D 30020GL BS 919 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 IN THE FWD CARGO COMPT SUMP AREA AT STA 919 FOUND SEVERE CORROSION WITH EXFOLIATION ON THE FRAME'S CAP BETWEEN L 51 LH TO L 50 RH. TRIMMED OUT FRAME CAP CORRODED REMOVED REMAINING CORROSION IAW SRM 51-21-01 PAR 34 VOL2 ORIGINAL MATERIAL THK IS .071 INCHES MATERIAL REMOVED .019 INCHES. REMAIN MATERIAL THK .052 INCHES MATERIAL REMOVED 26.25 PERCENT REMAIN 73.25 PERCENT IAW SRM53-30-00 FIG8 (NOTE2)FAB PARTS IAW DETAIL PARTS TRAVELER F160441-3 FILLER, F160441-5 CHANNEL, F160441-9 SHEAR CLIP AND F160441-7 SPLICE IAW SRM 53-30-00 FIG 10 AND FIG 8, SRM 53-13- 01 FIG 17 VOL 3 INSTALLED PARTS IAW SRM 53-30-00 FIG 8-10 INSTALLED 3EA HILOCKS .250 INCHES DIA IAW SRM 51-33-01 PAR 6-10 VOL 2. 2L73 4F4 F A22WE E23EA 20051101000032005110100003WP 2005 11 1 05FDEA03568 120051028A5730 SKIN DOUG DC10 DC1030 3023501WP LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 LT WING L/E NR 517 CT FOUND 1 CRACK 3'' LONG ON SKIN. REPAIRED PANEL IAW SRM 57-10-00 FIG 10-A VOL 1 AND SRM 51-35-01 PAGE 1-13 VOL 2. 2L73 4F A22WE 20051101000042005110100004WP 2005 11 1 05FDEA03571 120051028A5730 SKIN DOUG DC10 DC1030 3023501WP RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 RT WING L/E CRACK ON CHORD FIXED PANEL AT STA XORS 498. FAB AND INSTALLED REPAIR DOUBLER PER SRM 57-10-00 FIG 49 AND SRM 51-35-01 PAG 1-13. FAB PART IAW DETAIL PART TRAVELER F160742/N00742 PER SRM 57-10-00 FIG 49. 2L73 4F A22WE 20051101000072005110100007WP 2005 11 1 05FDEA03574 120051028A5730 SKIN DOUG DC10 DC1030 3023501WP RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 RT WING OUTBD FLAP CRACK LONG 1 INCH ON UPPER SKIN AT STA XOF787. CUTE DAMAGED AREA AND REPAIRED PER SRM 57-10-00 VOL 1 FIG 85 FAB PART IAW DETAIL PART TRAVELER F160347/N00347 PER SRM57-10-00 VOL 1 SHT 4. 2L73 4F A22WE 20051101000122005110100012WP 2005 11 1 05FDEA03576 120051028A5311 FRAME DOUG DC10 DC1030 3023501WP BS 1505 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 LT MLG WHEEL WELL FOUND SEVERE CORROSION ON FRAME AND ANGLE AT STA Y1505 X62. REMOVED CORROSION IAW SRM 51-21-01 PAR 34 VOL 2 ORIGINAL THK OF FRAME IS .090''. MATERIAL REMOVED IS .045',' REMAIN MATERIAL THK .045''. MATERIAL REMOVED 50 PERCENT IS OUT LIMIT IAW SRM 51-21-01 FIG 1B; TRIMMED OUT DAMAGED FRAME, FAB PARTS IAW DETAIL PARTS TRAVELER F161114-3 FILLER AND F161114-5. REPAIR ANGLE IAW SRM53-00-01 FIG 8. INSTALLED PARTS IAW SRM 53-00-01 FIG 8 SHT 1. 2L73 4F A22WE 20051101000132005110100013WP 2005 11 1 05FDEA03578 120051028A5730 SKIN DOUG DC10 DC1030 3023501WP GE CF6 CF66D 30020GL LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 LT WING L/E WING TIP FOUND 1 EA CRACK .50 INCH LONG ON EXISTING REPAIR ON LOWER SKIN AT STA XW99. TRIMED OUT CRACKED PORTION SKIN REPAIR IAW SRM 57-00-01 FIG 4 VOL 2 FAB PART IAW DETAIL PART TRAVELER N00550/F160550. 2L73 4F4 F A22WE E23EA 20051101000152005110100015EA 2005 11 1 COMA0560575 120051027A5610NP1393216 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A COMAO OTHER O OTHER CRCRUISE 1 SO01729CA132905628 7265 FLIGHT 4993 - CO-PILOT WINDSHIELD CRACKED. REPLACED WINDSHIELD. 2L72 4F RTA21EA 20051101000162005110100016NM 2005 11 1 SWAA053401 120051028A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29496WN 32478 DURING SCHEDULED RON CHECK, FOUND AFT CABIN EEPLS TRACK INOP. REMOVED AND REPLACED EEPLS SECTION PER MM. 2L72 4F RTA16WE 20051101000172005110100017EU 2005 11 1 RAIA00510024 120051026A3397 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHTSLOOSE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03574HK 41093 POST - FLIGHT INSPECTION - STL - EMERGENCY FLOOR LIGHTS OUT AT SEATS 1-3. MAINTENANCE RESET CONNECTOR AT FLOOR STRIP. 2L72 4T RTA41NM 20051101000192005110100019EA 2005 11 1 COMA0560572 120051026A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01484CA 7702 FLIGHT 5640 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2L72 4F RTA21EA 20060501000862006050100086EA 2006 5 1 A6WA200540368 120051230A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA RT WING CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31432AW 7257 RT WING LOWER PLANK HOLE NR 5 WS 76.161 HAS CORROSION AT IB FORWARD SIDE 4 INCHES L X .002 INCH D. NOT IN CRITICAL AREA. MAINTENANCE REPAIRED RT WING LOWER WING PLANK ACCESS HOLE NR 5 IAW REO. (K) 2L72 4F RTA21EA 20060501000872006050100087EA 2006 5 1 A6WA200540370 120051230A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA RT WING CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31432AW 7257 RT WING LOWER PLANK HOLE NR 16, WS 303.861 HAS CORROSION AT IB SIDE 1 INCH L X .005 INCH D. NOT CRITICAL. MAINTENANCE REPAIRED RT LWR WING PLANK ACCESS HOLE NR 16 IAW REO. (K) 2L72 4F RTA21EA 20051026001232005102600123NE 2005 10 26 Z1RA106190 120050921A21217650007901103 MOTOR SKRSKYS76 S76C 8143008NE BLOWER INOPERATIVE E Z1RAO OTHER O OTHER NRNOT REPORTED 1 SW11760AF 760523 VENT BLOWER INOPERATIVE. 1G72 3U NCH1NE 20051026001252005102600125NE 2005 10 26 Z1RA106189 120050921A2121ES731032 MOTOR SKRSKYS76 S76C 8143008NE BLOWER INOPERATIVE B Z1RAO OTHER O OTHER NRNOT REPORTED 1 SW11760AF2991 760523 AIRCONDITIONING EVAP BLOWER INOPERATIVE. 1G72 3U NCH1NE 20051026001262005102600126NE 2005 10 26 Z1RA106188 120050904A24977655203104041 WIRE HARNESS SKRSKYS76 S76C 8143008NE ELECTRICAL INTERMITTENT B Z1RAK NONE O OTHER ININSP/MAINT 1 SW11760AF2952 760523 MULTIPLE T5 SIGNAL FAULTS DURING STARTING. NO AUTOSTART AVAILABLE. HARNESS LOSES CONTINUITY AT PLUG P528 AT DECU ASSY. 1G72 3U NCH1NE 20051026001282005102600128EU 2005 10 26 B65A106278 120050929A2910105450121 HYDRAULIC SYSTEM BOLKMS105 BO105LSA1 5626021EU ALLSN 250C 250C28 03013GL LEAKING E B65AO OTHER K FLUID LOSS NRNOT REPORTED 1 GL13202LF 2014 LEAKING HYDRAULIC UNIT. 1G72 3U3 U H3AU E1GL 20051026001302005102600130NM 2005 10 26 2005UALA01162 120051018A5322 SHEAR TIE BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE BS 1562 CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29643UA 25093 CORROSION ON AFT SIDE OF FRAME BS 1562 FROM BL 0 TO RBL 10 ON SHEAR TIE. 2L72 4F4 FRTA1NM E24NE 20051026001362005102600136EA 2005 10 26 QXEA200501359 120051018A52102R5206B MOTOR CNDAIRCL600 CL6002C10 1390015EA PAX DOOR MALFUNCTIONED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09608QX 10026 DEN - MAIN CABIN DOOR HARD TO CLOSE AND OPEN. MAINTENANCE FOUND THE POWER ASSIST CABLE OFF THE ROLLER AND THE CABLE DAMAGED. REPLACED THE POWER ASSIST MOTOR AND CABLE ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20051026001382005102600138WP 2005 10 26 ABXA050257 120051011A5320991224697 INTERCOSTAL DOUG DC9 DC941 302207NWP BS 1114-1133 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23962AX 47768 AFT ASSY COMPARTMENT INTERCOSTAL BETWEEN FS 1114 AND FS 1133, LONGERON 17 RIGHT AND LONGERON 16 RIGHT HAD A CRACK ON BOTTOM FORWARD SIDE. FABRICATED AND INSTALLED REPAIR ANGLE AS REQUIRED IAW DC-9 SRM K05159 DRAWING. 2L72 4F A6WE 20051026001402005102600140NE 2005 10 26 NACA20050026 220051021A8530356993 CYLINDER DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE NR 2 CRACKED A NACAEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 AL0399330956 956 43576 P34218 NR 2 ENGINE SHUT DOWN ON CLIMB OUT DUE TO DOUBLE SHORTED SECONDARY NR 2 CYLINDER. FOUND NR 2 CYLINDER CRACKED. REPLACED NR 2 CYLINDER. LEAK AND OP CHECKED GOOD IAW NAC DC-6MM SECTION V PG 16 & 16A. 2L74 4R4 R 6A3 5E8 20051026001412005102600141NE 2005 10 26 QXEA200501358 220051018A7230 COMPRESSOR CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE NR 2 ENGINE VIBRATION A QXEAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 NM09610QX 10033 GEE965304 PDX - ON FLIGHT 2455 (PDX-SBA) 30 MINUTES OUT OF PORTLAND NR 2 ENGINE N1 FAN VIBRATIONS. FLIGHT RETURNED TO PDX AND ACCOMPLISHED A UNEVENTFUL LANDING. NO EMERGENCY DECLARED. 2L72 4F4 FRTA21EA EOOO63EN 20051026001442005102600144NM 2005 10 26 2005UALA01165 120051019A5330 SKIN BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29371UA 24540 FUSELAGE HAS THREE INCH CRACK BEHIND LT WING EMERGENCY EXIT LIGHT AREA. ACCOMPLISHED CATEGORY B REPAIR REF. SRM 53-00-01. CRITICAL FASTNER ROW WILL NEED INSPECTION AT 60,000 CYCLES AFTERINSTALLATION OF REPAIR. ** MF5633 CREATED TO MONITOR ** 2L72 4F4 FRTA16WE E21EU 20051026001462005102600146NM 2005 10 26 2005UALA01167 120051018A2130 WARNING FLAG AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE CABIN PRESSURE ILLUMINATED A UALAO OTHER J WARNING INDICATION NRNOT REPORTED 1 WP29841UA 1545 EXCESS CABIN ALT DISPLAYED ON UPPER ECAM SCREEN. CABIN ALTITUDE CLIMBED TO 10400 MSL. AIRCRAFT DESCENDED AND CABIN ALTITUDE CONTROLLER RETURNED TO NORMAL. NO FAULTS ON PFR. ACCOMPLISHED PRESSURE MONITOR AND CONTROL TEST PER MM 21-31-00, OP CHECK GOOD. FOUND FWD CARGO DOOR SEALS DAMAGED. REMOVED AND REINSTALLED SEAL ON FWD CARGO DOOR PER MM 52-31-18. ALSO CHECKED CONDITION OF AFT SEALS PER MM 52-32-18. ACCCOMPLISHED PRESSURIZATION CHECK PER JRH 2-40-80. CABIN PRESSURE CHECKS AND LEAK CHECK OF CARGO DOOR NORMAL. 2L72 4F4 FRTA28NM E40NE 20051026001502005102600150EA 2005 10 26 QXEA200501362 120051022A26119847101502 CHIMNEY CNDAIRCL600 CL6002C10 1390015EA SMOKE DETECTOR DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09606QX 10023 PDX - FORWARD CARGO BAY CHIMNEY DAMAGED. MAINTENANCE REPLACED THE CARGO BAY CHIMNEY. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20051026001512005102600151EA 2005 10 26 QXEA200501363 120051021A2150 WARNING SYSTEM CNDAIRCL600 CL6002C10 1390015EA RT A/C PACK ACTIVATED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09612QX 10042 PDX - ON TAXI OUT FOR FLIGHT 2456 RECEIVED A RIGHT PACK CAUTION MESSAGE. FLIGHT RETURNED TO THE GATE. MAINTENANCE PLACED THE RIGHT AIR CONDITIONING PACK ON MEL. MEL CLEARED ON 10/23 BY PERFORMING TROUBLESHOOTING IAW FIM 21-53-14, WITH NO DEFECTS NOTED. PERFORMED OPERATIONAL CHECK IAW AMM 21-51-00, NO DEFECTS NOTED. COULD NOT DUPLICATE DISCREPANCY. MEL CLEARED AND AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2L72 4F RTA21EA 20051026001542005102600154NM 2005 10 26 2005UALA01173 120051020A5310 DOOR FRAME BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29336UA 24240 FWD SIDE GALLEY DOOR FRAME LOWER END IS CRACKED AT TWO EACH FASTENER LOCATION. REMOVED THE CRACKS, INSTALLED FRAME REPAIR AND INNER SKIN REF JD SM90-52-40-14JD AND BOEING DRAWING 69-69430. 2L72 4F4 FRTA16WE E21EU 20051026001562005102600156EU 2005 10 26 2005UALA01175 120051019A3350 LIGHT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CABIN FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29420UA 489 CABIN EMERGENCY LIGHT TEST FAILED, INDICATES ON MESSAGE, FWD BATTERY LOW ON THE FIRST TEST. FOLLOWED BY INT LOADS FWD L MESSAGE AFTER FEW MORE TEST. REPLACED EMERGENCY POWER SUPPLY AND BATTERY 2L72 4F4 FRTA28NM E40NE 20051026001582005102600158NM 2005 10 26 MZZA0500010 120051003A5330146A32318 SKIN BOEING737 737824 13844BZNM GE CFM56 CFM56* 13802NE BS 727J CORRODED A MZZAK NONE O OTHER ININSP/MAINT 1 WP1327246 28956 INSPECTION FOUND CORROSION TO THE EXTERIOR OF THE FUSELAGE SKIN ADJACENT TO THE DRAIN HOLE AT STA 727J, BL 0. THE SKIN WAS REPAIRED IAW ECRA 5330-03490. 2L72 4F4 FRTA16WE E2GL 20051026001642005102600164EA 2005 10 26 COMA0570113 120051020A3210CC67010520951 DOOR CNDAIRCL600 CL6002C10 1390015EA LT MLG MISSING A COMAO OTHER D INFLIGHT SEPARATION NRNOT REPORTED 1 SO01354CA8100 10064 FLIGHT 5855 - LT MLG DOOR IS MISSING. REPAIRED COLLATERAL DAMAGE FROM IN FLIGHT SEPARATION AND DEFERRED GEAR DOOR PER CDL. 2L72 4F RTA21EA 20051026001672005102600167NM 2005 10 26 SWAA053321 120051023A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 663 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D CHECK, FOUND STR CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED STR CLIP PER SRM. 2L72 4F RTA16WE 20051026001682005102600168NM 2005 10 26 SWAA053322 120051023A53226546550 SHEAR TIE BOEING737 7373H4 1384600NM BS 787 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, BETWEEN STR 26L AND 27L. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051026001692005102600169NM 2005 10 26 SWAA053323 120051023A53306545768 SKIN BOEING737 7373H4 1384600NM BS 515 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 515, STR 16L. REPAIRED SKIN PER BFG ER. 2L72 4F RTA16WE 20051026001702005102600170NM 2005 10 26 SWAA053324 120051023A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM BS 515 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D CHECK, FOUND FUSELAGE STR CORRODED AT BS 515, STR 26L. REPAIRED STR PER SRM. 2L72 4F RTA16WE 20051026001732005102600173NM 2005 10 26 SWAA053327 120051024A53226546525 SHEAR TIE BOEING737 7373A4 1384585NM BS 380 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29678AA 23290 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 380, ABOVE STR 15L. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051026001742005102600174NM 2005 10 26 SWAA053328 120051024A53306560552 SKIN BOEING737 7373A4 1384585NM BS 376 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29678AA 23290 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 376, BETWEEN STR 14L AND STR 15L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051026001772005102600177CE 2005 10 26 01100405 120051005A322126430621 DRAG LINK CESSNA208 208B 2073701CE ZONE 700 BROKEN G HSYAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM05885FE 208B0185 ON RUN-UP BEFORE TAKEOFF, THE PILOT HEARD A POPPING NOISE AND RETURNED TO THE BLOCKS TO HAVE MAINTENANCE INSPECT THE NOSE LANDING GEAR. MAINTENANCE DISCOVERED THAT THE NOSE GEAR SPRING HAD BROKEN COMPLETELY AWAY AT THE REAR ATTACHMENT POINT (BEARING CAP/SUPPORT). THE APPARENT CAUSE OF PROBLEM, FAILURE OF NOSE GEAR SPRING (REAR DRAG LINK). MAINTENANCE IS REMOVING AND REPLACING THE NOSE GEAR SPRING. THE DEFECTIVE SECTION WILL BE SENT OUT FOR METALLURGICAL ANALYSIS TO DETERMINE IF A FLEETWIDE INSPECTION IS WARRANTED. THE AIRCRAFT IS EXPECTED TO RETURN TO SERVICE ON 10/6/05. 1H71 3T A37CE 20051026001802005102600180EU 2005 10 26 WRNA200500023 120050902A3230A2519903 VALVE AIRBUS300 A300B4203 3930306EU MLG UNSERVICEABLE A WRNAO OTHER J WARNING INDICATION APAPPROACH 1 SO05821SC 211 UNABLE TO LOWER GEAR, LANDING GEAR EXT C/B POPPED, PERFORMED ALTERNATE GEAR EXTENSION. LANDING NORMAL. REMOVED AND REPLACED LANDING GEAR ELECTRO VALVE IAW 32-31-12. OP'S CHECK AND LEAK CHECK SATISFACTORY IAW 32-30-00. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA35EU 20051026001812005102600181NM 2005 10 26 TSAA0527047 120051012A2782654465116 ACTUATOR BOEING737 7372T4 1384492NM NR 5 SLAT FAILED A TSAAA UNSCHED LANDING GJ MULTIPLE FAILURE WARNING INDICATION CLCLIMB 1 WP13808AL 23445 COOPESA TO BROWNSVILLE TX FERRY FLIGHT 808. NR 5 SLAT DID NOT RETRACT. LEFT WING TO BODY OVERHEAT INDICATION. THE CREW RETURNED TO COOPESA WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 5 SLAT ACTUATOR AND PNEUMATIC DUCT AND CLAMP. OPS AND LEAK CHECKS OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A16WE 20051026001822005102600182EU 2005 10 26 SF20050930 120050930A2731 TRIM SYSTEM SAAB SF340 SF340A 7850100EU ELEVATORS MALFUNCTIONED A UHLAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 GL1714XS 340A014 FLIGHT 7557 IAD-SCE, PILOT REPORTED, DURING THE CLIMBOUT UNABLE TO TRIM AIRCRAFT WITH EITHER LEFT OR RIGHT YOKE PITCH TRIM SWITCHES. STANDBY TRIM FUNCTIONED NORMALLY. AIRCRAFT RETURNED SAFELY TO IAD. 2L72 4T RTA52EU 20051026001832005102600183NE 2005 10 26 MWEA050114 220051011A7200 ENGINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D* NE RIGHT OUT OF LIMITS A MWEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31701ME 49760 RIGHT ENGINE AT/NEAR ALL PARAMETER LIMITS. PERFORMED RIGHT ENGINE PT7 LEAK CHECK, NO LEAKS. PERFORMED PT7 AND PT2 LEAK DOWN CHECKS TEST PASSED. RAN BOTH ENGINES AND FOUND NO ABNORMAL GAUGE READINGS AT TAKEOFF POWER SETTINGS. STICK SPILT WAS WITHIN LIMITS, OK FOR SERVICE. 2L72 4F4 FRTA6WE E2EA 20051026001892005102600189WP 2005 10 26 UPS05845565 120050920A53303648666 LONGERON DOUG DC8 DC871F 302199DWP BS 70-8.0 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE:SP L27R FS 70 TO FS 8.0 LONGERON 27R HAS EXFOLIATION CORROSION. REMOVED AND REPLACED LONGERON 27R AT FS 70 TO FS 8.0 IAW SRM 51-1-21 AND SRM 51-1-20D. 2L74 4F RT4A25 20051026001902005102600190WP 2005 10 26 UPS05845566 120050930A53404611067N FITTING DOUG DC8 DC871F 302199DWP BS 70 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE:SP FS 70 L30R END FITTING HAS EXFOLIATION CORROSION AFT CHORD SIDE. REMOVED AND REPLACED END FITTING IAW SRM 51-1-20D AND SRM 51-1-21. 2L74 4F RT4A25 20051026001912005102600191WP 2005 10 26 UPS05845567 120050922A5322 SHEAR TIE DOUG DC8 DC871F 302199DWP FS 35 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE: SP, SHEAR TIE AT FS 35 L34R TO L34L HAS EXFOLIATION CORROSION. REMOVED SHEAR TIE AT FS 35 L34R - L34L IAW SRM 53-2-0 FIG 1F FABRICATED AND INSTALLED SHEAR TIE AT FS 35 L34R - L34L IAW DWG 5613836, AND SRM 51-1-21, 51-1-20D. 2L74 4F RT4A25 20051026001932005102600193WP 2005 10 26 UPS05845569 120050920A5330 DOUBLER DOUG DC8 DC871F 302199DWP BS8-70 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE:SP INTERNAL DOUBLER HAS EXFOLIATION CORROSION AT FS 8 - FS 70 L29R L31R. REMOVED DOUBLER AT FS 8 TO FS 70 L29R TO 31R IAW SRM 51-1-21. FABRICATED AND INSTALLED INTERNAL DOUBLER IAW DWG 5649028 AND SRM 51-1-21. 2L74 4F RT4A25 20051026001942005102600194WP 2005 10 26 UPS05845570 120050922A5330 LONGERON DOUG DC8 DC871F 302199DWP FS 8-70 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE:SP L33R FS 70 TO FS 8.0 HAS EXFOLIATION CORROSION. REMOVED AND REPLACED LONGERON 33R IAW DWG 3642838 AND SRM 51-1-20D. 2L74 4F RT4A25 20051026001952005102600195WP 2005 10 26 UPS05845571 120050920A53303648667 LONGERON DOUG DC8 DC871F 302199DWP BS 8-70 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE:SP L30R FS 70 TO FS 8, LONGERON 30R HAS EXFOLIATION CORROSION. REMOVED AND REPLACED LONGERON 30R AT FS 70 - FS 8 IAW SRM 51-1-20 AND 51-20D. 2L74 4F RT4A25 20051026001962005102600196WP 2005 10 26 UPS05845572 120050930A5313 LONGERON DOUG DC8 DC871F 302199DWP BS 100-190 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE:SP LONGERON 36 FS 100 TO FS 190 HAS EXFOLIATION CORROSION. REMOVED AND REPLACED LONGERON 36 IAW DWG 5779925 AND SRM 51-1-20D. 2L74 4F RT4A25 20051026001972005102600197WP 2005 10 26 UPS05845573 120050914A5330561386215N1 SKIN DOUG DC8 DC871F 302199DWP BS 21-70 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE:SP TRANSFERRED FROM LOG PAGE 442150, REF DMI LOG D-309966 SKIN CORRODED AT STA 25 - 74 LONG 28R - 31L. REMOVED AND REPLACED BELLY SKIN AT STA -21.92 TO 70 LONG 31R TO L31L IAW EO DC8-5330-8942-D. 2L74 4F RT4A25 20051026001992005102600199WP 2005 10 26 05FDEA03240 120051005A5320 SPLICE DOUG DC10 DC1010 3022110WP BS 775 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25389FE 46623 FWD LOWER PIT STA 775 L52 LONGERON SPLICE CORRODED AFT END. REMOVED FASTENERS AT LONGERON SPLICE STA 755 L52. NO CORROSION FOUND. ALODINE AND PRIMED LONG SPLICE IAW DC10 SRM 51-21-01 VOL 1. PAINTED LONG SPLICE IAW DC10 SRM 51-21-02 VOL 11. FABRICATED LONG END CAP IAW DC10 DWG 3064. INSTALLED LONG END CAP IAW DC10 SRM 51-33-01 VOL 11. 2L73 4F A22WE 20051026002012005102600201NM 2005 10 26 AWXA200501162 120050913A5322654583311 SHEAR TIE BOEING737 7373G7 1384595NM BS 196 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 MCN - DURING C15 CHECK DISCOVERED TWO FLOOR WEBS CRACKED, .85 INCHES EACH, AT BS 196, WL 207, AND BL 29L. MAINTENANCE REMOVED FLOOR WEBS AT BS 196 BL 29L, AND WL 207 IAW BOEING 737-300 SRM 51-40-02-0G FIG 8. FABRICATED REPLACEMENT FLOOR WEBS IAW BOEING DWG NR 65-45833. INSTALLED FABRICATED REPAIR PARTS AT BS 196, WL 207 AND BL 29L IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 9 AND 10. 2L72 4F RTA16WE 20051026002022005102600202NM 2005 10 26 AWXA200501163 120050907A57536546486130 WEDGE BOEING737 7373G7 1384595NM ZONE 600 DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 MCN - DURING C15 CHECK, DISCOVERED DISBOND AREA ON LOWER SURFACE OF THE RT INBOARD MID-FLAP TRAILING EDGE WEDGE, 35" FROM OUTBOARD END. MAINTENANCE REMOVED DISBOND SKIN ON LOWER SURFACE OF RT INBOARD MID FLAP TRAILING EDGE WEDGE IAW BOEING 737-300 SRM 51-70-10-2R. FABRICATED REPAIR FILLER AND DOUBLER IAW BOEING 737-300 SRM 51-70-10-2R FIG 203. BONDED AND SEALED REPAIR PARTS TO IAW BOEING 737-300 SRM 51-70-10-2R FIG 203. 2L72 4F RTA16WE 20051026002062005102600206NM 2005 10 26 AWXA200501166 120050909A575465C2679413 SKIN BOEING737 7373G7 1384595NM ZONE 500 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 MCN - DURING C15 CHECK, DISCOVERED 4 CRACKS, .5 INCHES IN LENGTH, AT BOTTOM OF THE NR 2 SLAT SKIN AT OUTBOARD MAIN TRACK. MAINTENANCE TRIMMED OUT DAMAGED SKIN ON THE NR 2 SLAT IAW BOEING 737-300 SRM 57-43-01-2R FIG 201. FABRICATED FILLER AND SPLICE PATE IAW BOEING 737-300 SRM 57-43-01-2R FIG 201. INSTALLED REPAIR PARTS IAW BOEING 737-300 SRM 57-43-01-2R FIG 201. 2L72 4F RTA16WE 20051026002082005102600208NM 2005 10 26 AWXA200501168 120050907A5753 SKIN BOEING737 73733A 1384673NM TE FLAP DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW 23634 GYR - DURING C20 CHECK DISCOVERED,THE RT AFT FLAP, RT WING, ON THE INBOARD END DELAMINATED. MAINTENANCE REMOVED DAMAGED SKIN AND CORE ON THE RT AFT FLAP IAW BOEING 737-300 SRM 51-70-10-2R. FABRICATED DOUBLER AND FILLER IAW BOEING 737-300 SRM 51-70-10-2R. BONDED AND SEALED REPAIR PARTS TO THE RT AFT FLAP, RT WING, ON THE INBOARD END IAW BOEING 737-300 SRM 51-70-10-2R. 2L72 4F RTA16WE 20051026002122005102600212NM 2005 10 26 2005UALA01070 120051001A3320 LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE GALLEY BURNED A UALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP29577UA 26693 SMOKE COMING FROM LIGHT FIXTURE IN FORWARD GALLEY. ACCOMPLISHED VISUAL INSPECTION. FOUND NO BURNT WIRES NO CHAFFING, BALLASTS OK , NO ARCING, 0-2 GEN OK. OP CHECK LIGHTS FOR 20 MINUTES NO SMELL OR SMOKE. NO FURTHER INCIDENTS SINCE. 2L72 4F4 FRTA2NM E17NE 20051026002142005102600214NM 2005 10 26 2005UALA01072 120051002A5610 WINDOW BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU COCKPIT CRACKED A UALAO OTHER O OTHER NRNOT REPORTED 1 WP29202UA 24717 CAPT WINDSCREEN CRACKED AT 11000 FT. EXTERIOR PANE ONLY. WINDOW REPLACED WITH MM 56-11-21. 2L72 4F4 FRTA16WE E21EU 20051026002182005102600218WP 2005 10 26 0501491236 120050922A3350 POWER SUPPLY DOUG DC10 DC1030 3023501WP EMERGENCY LIGHT INOPERATIVE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01236NW 46934 DURING LINE CHECK MAINTENANCE FOUND LT AND RT EMERGENCY LIGHTS INOP ROWS 10 TO 20 ZONE B. REPLACED POWER SUPPLY AND OPERATION CHECKS GOOD. 2L73 4F A22WE 20051026002212005102600221NM 2005 10 26 XN0A1270 120051001A3510 TRANSMITTER BOEING727 727227 1384078NM OXYGEN SYSTEM MALFUNCTIONED A XN0AD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL2373751 21247 CREW O2 TO 0 PSI IN TAXI OUT SWF, BACK TO THE RAMP. RESET PRESS TRANSMITTER ON CREW BOTTLE, CHECK GOOD IAW 35-11-00. 2L73 4F A3WE 20051026002222005102600222SO 2005 10 26 1262-101805 120051018A325051507 MANIFOLD GULSTMG1159 GIV 3980115SO NLG STEERING MALFUNCTIONED E N93AO OTHER O OTHER TXTAXI/GRND HDL 1 SO13462QS3704 1262 NOSE STEERING PULLS TO LEFT DURING TAXI. 2L72 4F RTA12EA 20051026002242005102600224NM 2005 10 26 05FDEA03444 120051018A5311 FRAME DOUG MD11 MD11 3023602NM BS 1841 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 CENTER CARGO COMPT STA 1841 RT LOWER FRAME ASSY CORNER FOUND CRACK DURING REMOVAL. REPAIRED PER SRM 53-00-00 FIG.3 VOL.I. NEW ANGLE P/N FX AGA 7171-20 FABRICATED PER DRAWING AGA 7171. MAJOR REPAIR PER GMM 6-2-100. 2L73 4F RTA22WE 20051026002292005102600229NM 2005 10 26 2005UALA01085 120051006A5210 BEAM BOEING747 747422 1384935NM PWA 4056 PW4056 NE PAX DOOR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29120UA 29166 NR 2R MAIN ENTRY DOOR UPPER GATE CLOSURE BEAM CRACKED AT ATTACH HOLE. NR 2R MAIN ENTRY DOOR UPPER GATE CLOSURE BEAM WAS FOUND CRACKED AT ATTACH HOLE. CRACK WAS PROBABLY CAUSED BY FATIGUE. ANGLE REPAIR WAS INSTALLED REFERENCING SM 80-52-10-05-JD AND SRM 57-70-11. 2L74 4F4 FRTA20WE E24NE 20051027000012005102700001EA 2005 10 27 ASOA05769 120050918A2611 SMOKE WARNING CNDAIRCL600 CL6002C10 1390015EA LAVATORY FALSE ACTIVATIONA ASOAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27702EV 10035 FLT 4416 - DURING CLIMB-OUT FROM SLC-ABQ, AN AFT LAV SMOKE WARNING APPEARED. THE QRH WAS COMPLIED WITH AND THE SMOKE WARNING SUBSEQUENTLY CLEARED BEFORE THE CHECKLIST WAS COMPLETED. THE CREW PULLED THE CIRCUIT BREAKERS AND THE FLIGHT CONTINUED TO ABQ AND LANDED SAFELY. MAINTENANCE RAN THE RIGHT ENGINE AND PACK WITH NO SMOKE NOTED, AND RESET THE CIRCUIT BREAKERS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051027000032005102700003EA 2005 10 27 VNAA0510010 120051014A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A VNAAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL05249PS 7926 THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED ON APPROACH WITH FLAPS 20 DEGREES. THE CREW FOLLOWED THE QRH AND LANDED SAFELY. MAINTENANCE INSPECTED THE FLAP SYSTEM AND RESET THE FECU IAW CRJ200 FIM 27-50-00. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20051027000052005102700005CE 2005 10 27 DJFA2005154 120051023A3260 INDICATION SYS CESSNA500 560CESSNA 2076750CE MLG MALFUNCTIONED E DJFAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 EA23583CW 5600123 ON APPROACH INTO KBED, ATTEMPTED TO EXTEND THE LANDING GEAR AND DID NOT RECEIVE GEAR DOWN INDICATION. RED GEAR UNSAFE LIGHT WAS ILLUMINATED. LANDING GEAR WAS THEN CYCLED AGAIN WITH THE SAME RESULT AND THE APPROACH WAS MISSED. WHEN IT WAS DISCOVERED THAT THE LANDING GEAR CONTROL CIRCUIT BREAKER WAS POPPED OUT, THE CREW RESET THE CIRCUIT BREAKER AND ATTEMPTED TO LOWER THE LANDING GEAR WITHOUT SUCCESS, AND THE CIRCUIT BREAKER POPPED AGAIN. AN EMERGENCY WAS DECLARED AND THE CREW PERFORMED AN EMERGENCY LANDING GEAR EXTENSION. THREE GREEN GEAR DOWN AND LOCK INDICATIONS WERE RECEIVED. THE TOWER CONFIRMED THAT ALL THREE LANDING GEAR APPEARED TO BE DOWN. THE AIRCRAFT WAS LANDED IN KBED WITHOUT FURTHER INCIDENT. 2L72 4F RTA22CE 20051027000062005102700006EA 2005 10 27 VTZA200500215 120051022A5610NP1393225 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A VTZAB EMER. DESCENT O OTHER CRCRUISE 1 EA27647BR13326 7399 CAPTS SIDE WINDOW SHATTERED IN FLIGHT. REMOVED AND REPLACED RIGHT SIDE WINDOW. 2L72 4F RTA21EA 20051027000082005102700008NM 2005 10 27 CALA0500377 120051025A531465621258 KEELBEAM BOEING737 7373T0 1384582NM CFMINTCFM567CFM567B22 13802NE BS 540 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770352 23590 INSPECTION FOUND RT LOWER CHORD OF KEELBEAM CORRODED AT STA 540, RT A/C BAY COMPARTMENT. THE CORROSION WAS REMOVED IAW ECRA 5310-04491. 2L72 4F4 FRTA16WE E00055EN 20051027000102005102700010 2005 10 27 SWAA053341 420051025A2565416A200 SLIDE BOEING737 7377H4 1384404NM CFMINTCFM567CFM567B22 13802NE L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29429WN 33658 DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EVACUATION SLIDE OUT OF ADJUST. REINSTALLED SLIDE ASSY IAW MM. 2L72 4F4 FRTA16WE E00055EN 20051027000142005102700014EA 2005 10 27 COMA0560564 120051022A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE TE FLAPS FAILED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01932CA2221 855 7038 FLAPS FAIL CAUTION. CND REPLACED THE RT BPSU. 2L72 4F4 FRTA21EA E15NE 20051027000152005102700015EA 2005 10 27 COMA0570115 120051023A2760 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE RUDDER/SPOILERS MALFUNCTIONED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01398CA 10112 SPOILER, STAB AND RUDDER LIMITER FAULT. RESET THE SSCU. NO DEFECTS NOTED. 2L72 4F4 FRTA21EA EOOO63EN 20051027000222005102700022NM 2005 10 27 AWXA200501262 120051023A339713311122 WIRE BOEING757 7572S7 1384962NM EMERGENCY LIGHT SHORTED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28902AW 23322 PHX - EEL - DURING OVERNIGHT MAINTENANCE DISCOVERED ROWS 27 THROUGH 35 EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPAIRED WIRE UN SEAT 29 IAW BOEING SWPM 20-30. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA2NM 20051027000242005102700024NM 2005 10 27 AWXA200501264 120051010A5320654587512 ANGLE BOEING737 7373S3 1384711NM BS 304-325 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 DURING C18 CHECK DISCOVERED CORROSION ON THE R1 INNER CHORD, UPPER ANGLE FROM BS 304 TO BS 325, RBL 61, AND WL 209. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-10-13-1A1 FIG 101. MAINTENANCE REMOVED R1 INNER CHORD UPPER ANGLE AND INSTALLED NEW ANGLE FROM BS 304 TO BS 325, BL 61R AND WL 209 IAW BOEING 737-300 SRM 51-40-02-0G FIGS 8 AND 12. 2L72 4F RTA16WE 20051027000252005102700025NM 2005 10 27 AWXA200501265 120051012A532065528941 CHANNEL BOEING737 7373S3 1384711NM BS 540 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 DURING C18 CHECK DISCOVERED CABIN FLOOR CHANNEL ASSEMBLY CRACKED IN RADIUS, .65 INCHES IN LENGTH, AT BS 540, WL 208.1 AND BL 0. MAINTENANCE REMOVED CABIN FLOOR SUPPORT IAW BOEING 737-300 SRM 51-40-02-0G AND INSTALLED NEW CABIN FLOOR CHANNEL ASSEMBLY AT BS 540, WL 208.1 AND BL 0 IAW BOEING 737-300 SRM 51-40-02-0G FIG 15. 2L72 4F RTA16WE 20051027000262005102700026NM 2005 10 27 AWXA200501266 120051020A575369388487 TRACK BOEING737 7373S3 1384711NM ZONE 500 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 DURING C18 DISCOVERED CORROSION ON THE LT INBOARD MIDFLAP, OUTBOARD CARRIAGE, INBOARD FORE FLAP SEQUENCE CAM TRACK AT WBL 185. NO CORROSION REMOVAL LIMITS ARE AVAILABLE FOR CAM TRACK. MAINTENANCE REMOVED CAM TRACK AND INSTALLED NEW CAM TRACK ON THE LT INBOARD MIDFLAP, OUTBOARD CARRIAGE, INBOARD FORE FLAP AT WBL 185 IAW BOEING 737-300 SRM 20-50-11-2 FIG 202. 2L72 4F RTA16WE 20051027000272005102700027NM 2005 10 27 AWXA200501267 120051020A575369388485 TRACK BOEING737 7373S3 1384711NM TE FLAPS CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 MCN - DURING C18 DISCOVERED CORROSION ON THE LT AND RT INBOARD MIDFLAP, INBOARD AND OUTBOARD CARRIAGE, INBOARD FORE FLAP SEQUENCE CAM TRACK AT WBL 71L AND 71R. NO CORROSION REMOVAL LIMITS ARE AVAILABLE FOR CAM TRACK. MAINTENANCE REMOVED CAM TRACKS AND INSTALLED NEW CAM TRACKS ON THE LT AND RT INBOARD MIDFLAP, INBOARD AND OUTBOARD CARRIAGE, INBOARD FORE FLAP AT WBL 71L AND 71R IAW BOEING 737-300 SRM 20-50-11-2 FIG 202 2L72 4F RTA16WE 20051027000312005102700031NM 2005 10 27 AWXA200501271 120050923A531169730571 FRAME BOEING737 7373S3 1384711NM BS 500D CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 MCN - DURING C18 CHECK DISCOVERED FRAME ANGLE CRACKED, .375 INCHES IN LENGTH, AT BS 500D AND STR 13L. MAINTENANCE REMOVED FRAME ANGLE FROM STR 11L TO STR 13L AND BS 500D IAW BOEING 737-300 SRM 51-40-02-0G. FABRICATED REPLACEMENT FRAME ANGLE IAW BOEING DRAWING 69-73057. INSTALLED FRAME ANGLE FROM STR 11L TO STR 13L AND BS 500D IAW BOEING 737-300 SRM 51-40-02-0G. 2L72 4F RTA16WE 20051027000362005102700036CE 2005 10 27 DXTA200501032 120051020A323399125374 ACTUATOR CESSNA560 560XL 2076702CE RT MLG FAILED E DXTAO OTHER J WARNING INDICATION CLCLIMB 1 GL07663QS3361 5605263 LANDING GEAR RETRACTION DURING TAKEOFF, RT MAIN GREEN DOWN LIGHT REMAINED ILLUMINATED (UNLOCK LIGHT NOT ILLUMINATED) PERFORMED LANDING GEAR WILL NOT EXTEND CHECKLIST AND BLEW GEAR DOWN WITH NITROGEN SYSTEM. REMOVED RT MAIN GEAR ACTUATOR DUE TO HIGH RESISTANCE IN DOWNLOCK SWITCH. INSTALLED RENTAL ACTUATOR IAW CE560XL M/M CH 32-30-04, OPS CHECKED GOOD IAW CE560XL M/M CH 32-01-00. DURING GEAR SWING AND BLOW DOWN ACTUATOR (RENTAL) WAS INSPECTED AND RETURNED TO SERVICE BY CESSNA AIRCRAFT CO CRS CN1R918C. 2L72 4F RTA22CE 20051027000382005102700038NM 2005 10 27 DXTA200501033 120051020A3411 PITOT HEAD AMD FALC50FALCON2000 2730170NM PITOT STATIC SYSOBSTRUCTED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07218QS 118 ON TAKEOFF ROLL AFTER 50 KTS & BEFORE 80 KTS PILOTS AIRSPEED FAILED CO-PILOTS PFD INDICATED YELLOW IAS MISCOMPAIR FLAG, NR 2 EIED DISPLAYED FLA ADC MN RANGE SOFT FAULT, FIB ADC MN RANGE SOFT FAULT, FZA ADC MN RANGE SOFT FAULT F2B MN RANGE SOFT FAULT. ABORTED TAKEOFF. INSPECTED & FOUND PILOTS PITOT LINE TO BE CLOGGED WITH DIRT. DISCONNECT PITOT STATIC LINES FROM NR 1 ADC & BACK BLEW LINE TO CLEAN DEBRIS. RECONNECTED LINES. COMPLETED PITOT STATIC LEAK CHECK OF NR 1 PITOT STATIC SYSTEM PER F2000 MM 34-100 & FAR 91.411 ON 10/20/05. LEAK CHECK GOOD. 2K73 4F RTA50NM 20051027000392005102700039CE 2005 10 27 DXTA200501034 120051021A215073838433 ACM CESSNA750 750 2076810CE CABIN COOLING FAILED E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07956QS62 7500156 STRONG ODOR LIKE OIL BURNING COMING FROM PACKS IRRITATING EYES AND SHORTNESS OF BREATHING. REMOVED COCKPIT ACM/COMP TURBO. CLEANED SECONDARY HEAT EXCHANGER. INSTALLED ACM/COMP. TURBO OVERHAULED BY HAMILTON SUNDSTRAND CRS SI3R842L IAW CESSNA 750 M/M CHAP 21-51-00. LEAK AND OPERATIONAL CHECK NORMAL. 2L72 4J RTT00007WI 20051027000412005102700041NM 2005 10 27 QXEA200501369 120051019A5712 RIB DHAV DHC8 DHC8202 2809007NM RT WING GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09345PH 476 PDX - RIGHT WING, RIB AT YW261, HAS MINOR GOUGE IN RADIUS AT AFT, OUTBOARD, LOWER, CORNER. REPAIRED IAW HORIZON AIR EA 2-57-332 AND RD 8-57-3197. 2H72 4T RTA13NM 20051027000462005102700046NM 2005 10 27 QXEA200501373 120051022A5230 BRACKET BOMBDRDHC8 DHC8402 1390042NM CARGO DOOR LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09401QX 4031 PDX: AFT CARGO DOOR LOWER FORWARD STOP BRACKET, LOWER FORWARD BOLT (ON INSIDE SURFACE) SPIN IN NUTPLATE WHEN TORQUED. MAINTENANCE REPAIRED IAW Q400 SRM 51-42-05, SRM 51-42-15, Q400 AMM 52-31-24-420-041 AND HORIZON EA 6-52-408. 2H72 4T RTA13NM 20051027000472005102700047CE 2005 10 27 HYIA051006 120051006A322251411022 AXLE CESSNA402 402C 207590RCE NLG CRACKED G HYIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NE011376 ON ROLLOUT AFTER LANDING CREW ENCOUNTERED WHAT WAS THOUGHT TO BE A FLAT TIRE. MAINTENANCE PERSONNEL FOUND THAT THE RIGHT MAIN LANDING GEAR AXLE WAS CRACKED AT THE INNER BEARING AREA. 1L72 3O A7CE 20051027000482005102700048NM 2005 10 27 CALA0500376 120050921A2497UNK WIRE HARNESS BOEING737 7373T0 1384582NM RH AFT W/W BURNED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769333 23571 FUEL SHUT-OFF VALVE WIRES & O/B LANDING LIGHT WIRES FOUND BURNED IN JUNCTION BOX NEAR D5164J (LANDING LIGHT DISCONNECT) AT RT SIDE AFT WHEEL WELL. SMOKE & COKING RESIDUE ON INSIDE SURFACE OF JUNCTION BOX COVER PLATE. ALL 3 LANDING LIGHT WIRES APPEARED TO HAVE INSULATION BURNED AS DID 2 FUEL SHUT-OFF VALVE WIRES. THIS WIRING IS I/B OF SPLICE THAT IS SPLICED TO W804 WIRE BUNDLE & NOT IN W804 WIRE BUNDLE. WIRES WERE REMOVED & REPLACED WITH NEW WIRING IAW WDM 28-21-08 AND 33-42-01. IN ADDITION, NR 2 ENGINE FUEL SHUT-OFF VALVE AND P5-2 PANEL WERE FOUND FAULTY. THE VALVE AND PANEL WERE REMOVED AND REPLACED IAW MM 28-22-11 AND 28-22-43. OPERATIONAL CHECKS OF THE VALVE, PANEL, AND LANDING LIGHT WERE GOOD. 2L72 4F RTA16WE 20051027000532005102700053EA 2005 10 27 SWIA200515713 120051018A2751601R590141 DETECTOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07969SW 7876 FLAPS DEGRADED MESSAGE. REPLACED SKEW DET UNIT IAW RJ MM 27-51-15. OPERATIONAL CHECK GOOD. P/N ON 601R59014-1 OFF A1011. 2L72 4F RTA21EA 20051027000582005102700058EA 2005 10 27 SWIA200515718 120051021A27518004301 DETECTOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CLCLIMB 1 NM07919SW560 560 7657 FLAP FAIL CAUTION MESSAGE, AFTER T/O. REPLACED SKEW DETECTOR UNIT, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051027000602005102700060EA 2005 10 27 SWIA200515720 120051023A274170609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07963SW5571 5571 7865 A -STAB CH 1 INOP- STATUS MESSAGE. REPLACED HSTCU IAW CRJ MM 27-40-00, 27-41-01, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051027000622005102700062EA 2005 10 27 SWIA200515722 120051017A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA FLOOD LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07906SW 7510 ONE CEILING FLOODLIGHT INOP. RELAMPED CEILING EMERGENCY FLOOD LIGHT AND OPERATIONAL CHECK GOOD. REF AMM 33-51-16. 2L72 4F RTA21EA 20051027000672005102700067EU 2005 10 27 2005UALA01091 120051005A2130 WARNING LIGHT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CABIN PRESSURE ILLUMINATED A UALAO OTHER J WARNING INDICATION DEDESCENT 1 WP29442UA 780 LANDED UNDER AMBER ALERT DUE TO FLUCTUATING CABIN PRESSURE. CABIN PRESSURE EXCESS CABIN ALTITUDE ON DESCENT. AFTER RAPID DESCENT, THEN GOT CABIN PRESSURE LOW DIFFERENTIAL PRESSURE AND SAFETY VALVE OPEN ECAM MESSAGES. CABIN PRESSURE CHANGES FELT BY CREW & PASSENGERS. HEARD AIR VENTING NOISE NEAR COCKPIT WINDOWS. NO BLEED OR PACK PROBLEMS NOTICED. SUPPLEMENTAL DATA UPDATE FLUCTUATING CABIN PRESSURE. EXCESS CABIN ALTITUDE ON DESCENT. AFTER DESCENT, CREW GOT CABIN PRESSURE LOW DIFFERENTIAL PRESSURE AND SAFETY VALVE OPEN ECAMS. CREW HEARD AIR VENTING NOISE NEAR FLIGHT DECK WINDOW. NO BLEED OR PACK PROBLEMS NOTICED. REPLACED N1 CABIN PRESSURE CONTROLLER PER MM 21-31-34. OP CHECKS GOOD. PRESSURIZED AIRCRAFT 2L72 4F4 FRTA28NM E40NE 20051027000682005102700068EU 2005 10 27 2005UALA01092 120051006A2150 A/C PACK AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 2 MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29438UA 678 FLIGHT DIVERTED WITH THE NR 1 PACK TRIPPING AND NR 2 PACK ALREADY DEFERRED. AIRCRAFT LOST NR 1 PACK APPROXIMATELY 20 MINUTES AFTER TAKEOFF. NR 2 PACK PREVIOUSLY DEFERRED. CIRCUIT BREAKERS CYCLED AND PROVIDED NO HELP. REPLACED NR 1 RAI ACTUATOR (MR21603-11 WITH MR21603-67), NO HELP. REMOVED AND REPLACED NR 1 ENGINE BLEED REGULATED PRESSURE TRANSDUCER (644-1251), 8HA1 PER MM 36-11-16-401. RAN ENGINES AND OP CHECKS AND LEAK CHECKS GOOD. 2L72 4F4 FRTA28NM E40NE 20051027000692005102700069NM 2005 10 27 2005UALA01094 120051006A2560 FLASHLIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29180UA 25224 EMERGENCY FLASHLIGHT 4R OUTBOARD INOP. 2L74 4F4 FRTA20WE E24NE 20051027000702005102700070NM 2005 10 27 2005UALA01095 120051006A3350 LIGHT BOEING777 777222 1385219NM PWA PW4077PW4077 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29781UA 26945 AFT EEL LIGHT 2E INOP. REPLACED EEL LIGHT. 2L72 4F4 FRTT0001SE E46NE 20051027000712005102700071NE 2005 10 27 ASMF200509015 220050929A732076960615 FCU DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE RT ENGINE FAILED W ASMFD RETURN TO BLOCK RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SW23204AM5721 49404 718260 AIRCRAFT RETURNED TO PLATFORM AFTER RT ENGINE START, THE RPMS IN IDLE WERE NOT REACHED, STAYING N2 ON 45 PERCENT AND AFTER A/A AND HYD WERE SHUTDOWN THE ENGINE WAS STABILIZED IN MANUAL MODE. WHEN A/A AND HYD WERE ACTIVATED AGAIN, N2 COME DOWN TO 40 PERCENT. THROTTLE PUMP PROCEDURE WAS PERFORMED AND THE FCU WAS ADJUSTED IAW MM, REACHING 56 PERCENT, BUT AFTER N2 COME DOWN TO 54 PERCENT. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT CHECK, THE RT PYD VALVE AND FCU WERE REPLACED IAW MM 73-13-05 AND MM 73-20-01 RESPECTIVELY. THE TRIM AND OPERATIONAL TESTS WERE PERFORMED IAW MM 71-00-00, BEING CORRECT. 2L72 4F4 FRTA6WE E9NE 20051027000722005102700072NM 2005 10 27 MWEA050119 120051025A523059101419 DOUBLER DOUG MD88 MD88 3023688NM CARGO DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 CRACK ON MID CARGO DOOR, BOTTOM INNER SURFACE. FABRICATED AND INSTALLED DOUBLER. 2L72 4F RTA6WE 20051027000732005102700073NM 2005 10 27 QXEA200501357 120051023A3233465507 ACTUATOR BOMBDRDHC8 DHC8402 1390042NM MLG MALFUNCTIONED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09403QX2116 4037 AFTER TAKEOFF AND SELECTING GEAR UP, NR 2 GEAR DID NOT PROPERLY RETRACT. RED "RIGHT", UNSAFE LIGHT, AMBER "R DOOR" AND AMBER GEAR SELECTOR HANDLE LIGHTS REMAINED ILLUMINATED. RAN CHECKLIST. CONFIGURATIONS WERE OK. CYCLED GEAR SOLVED PROBLEM. FA REPORTED LOUD NOISE FROM RIGHT SIDE PRIOR TO 2ND CYCLING OF THE GEAR. MAINTENANCE OPERATED GEAR USING GROUND CART. FOUND NR 2 GEAR RETRACT ACTUATOR LEAKING FROM PISTON SHAFT AND ACTUATOR SLOW TO STOW GEAR INTO UPLOCK. REPLACED NR 2 GEAR RETRACT ACTUATOR IAW Q400 TASK 32-31-11-000-801 AND 32-31-11-400-801. LEAK CHECK, BLEED NR 2 HYD SYSTEM AND FUNCTIONAL CHECK OF LANDING GEAR PRIMARY RETRACTION AND EXTENSION SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051027000742005102700074 2005 10 27 ASMF200510004 420051004A34426225132101 TRANSCEIVER DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE WX RADAR SYS FAILED W ASMFA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW23861LF14490 49826 AC PERFORMED AN UNSCHEDULED LANDING BECAUSE WEATHER RADAR LEVELED AT 340 FT DOES NOT DEPICT ECHO’S AND FLOW LIGHT TURNED ON DURING FLIGHT. THE RECEIVER / TRANSMITTER AND INDICATOR WEATHER RADAR WERE REPLACED IAW MM 34-41-04 AND MM 34-41-02 PAGE 202, TESTED CORRECT. ADDITIONALLY, THE VERTICAL GYRO NR 2 AND CADC NR 1 WERE REPLACED AND ADC NR 2 CONNECTORS WERE SERVICED IAW MM 34-16-01, TESTED CORRECT. IAW AUTOMATIC PILOT OUT OF SERVICE REPORT, AILERON SERVO, RUDDER AND NEUTRAL RUDDER WERE ADJUSTED IAW MM 22-11-01 AND 27-20-00 RESPECTIVELY. TESTS WERE PERFORMED TO RADAR, DFGC, SENSORS AND STP, BEING ALL CORRECT. 2L72 4F4 FRT E9NE 20051027000752005102700075NE 2005 10 27 ASMF200510003 220051003A72301A9031001 BLADE BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE 1ST STAGE DAMAGED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23804AM 26271 727137 DURING TRANSIT CHECK, DETECTED A BLADE DAMAGED, LT ENGINE LPC 1ST STAGE. THE BLADE WAS OUT OF LIMITS WITH A DAMAGE OF 4 X 0.750 AT LEADING EDGE. DURING OVERNIGHT CHECK, THE TWO BLADES SET OF LPC 1 ST STAGE WAS REPLACED IAW MM 72-31-02, VIBRATION TEST NR 8 WAS PERFORMED BEING OUT OF LIMITS, SO THE LT ENGINE WAS REPLACED IAW MM 71-00-00 AND OPERATIONAL CHECK WAS PERFORMED IAW MPCM 71-00-01, BEING CORRECT. 2L72 4F4 FRTA2NM E17NE 20051027000762005102700076SO 2005 10 27 RAIA00510003 120051001A521014540131001 SPRING EMB 145 EMB145LR 3260212SO PAX DOOR FAILED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03812HK 145373 PREFLIGHT INSPECTION, ERI MAIN CABIN STAIRS WON'T FOLD DOWN WHEN DOOR OPENS. MAINTENANCE REMOVED AND REPLACED THE MAIN DOOR STEP SPRING AND ADJUSTED METAL TRIM. 2L72 4T RTT00011AT 20051027000772005102700077SO 2005 10 27 RAIA005100001 120051001A3610 DUCT EMB 145 EMB145 3260210SO CABIN AIR BLOWN A RAIAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE03801HK 145053 FLT 3553 - LGA - SMOKE IN CABIN DURING CRUISE. INSPECTED AND FOUND BLOWN DUCT. SYSTEM DEFERRED. 2L72 4F RTT00011AT 20051027000782005102700078EU 2005 10 27 RAIA00510002 120051001A3397 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE331* 01514WP EMERGENCY LIGHT UNSECURE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03558HK 41071 POST FLIGHT, EMERGENCY LIGHTS AT 6A AND 8A ON FLOOR INOPERATIVE. MAINTENANCE SECURED ELECTRICAL CONNECTOR WITHIN FLOOR STRIP. 2L72 4T3 TRTA41NM E2WE 20051027000792005102700079SO 2005 10 27 RAIA00510004 120051003A5210 DOOR EMB 145 EMB145EP 3260221SO MAIN PAX STIFF A RAIAK NONE O OTHER ININSP/MAINT 1 CE03827HK 145021 POST FLIGHT - STL - FLIGHT ATTENDANT REPORTS MAIN DOOR IS VERY DIFFICULT TO OPEN. MAINTENANCE PERFORMED, OPS CHECK WITH NO DEFECTS NOTED. 2L72 4F RTT00011AT 20051027000802005102700080SO 2005 10 27 RAIA00510005 120051004A3350 LIGHT EMB 145 EMB145 3260210SO CABIN INTERMITTENT A RAIAK NONE O OTHER ININSP/MAINT 1 CE03801HK 145053 PREFLIGHT - PIT - EMERGENCY LIGHT INOP AT BULKHEAD AND OVER 24DF. MAINTENANCE OPS CHECKED SEVERAL TIMES WITH NO DEFECTS. 2L72 4F RTT00011AT 20051027000812005102700081SO 2005 10 27 RAIA00510006 120051004A3397 WIRE EMB 145 EMB145 3260210SO EMERGENCY LIGHT LOOSE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03801HK 145053 PREFLIGHT - PIT - EMERGENCY LIGHTS OUT. MAINTENANCE RESECURED LOOSE WIRING. 2L72 4F RTT00011AT 20051027000822005102700082SO 2005 10 27 RAIA00510007 120051004A3397 WIRE EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT LOOSE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03808HK 145157 PREFLIGHT - PIT - VARIOUS EMERGENCY LIGHTS IN CABIN INOP. MAINTENANCE RESECURED WIRE ON FLOOR PROXIMITY STRIP. 2L72 4F RTT00011AT 20051027000832005102700083SO 2005 10 27 C2XA05IA108 120051003A261147359713 SMOKE DETECTOR EMB 145 EMB145XR 3260214SO CARGO BAY INOPERATIVE A C2XAFA ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 SW2716183300 300 14500914 IAH - FLIGHT 2086, THE CREW REPORTED A BAGGAGE SMOKE INDICATION IN FLIGHT. THE CREW DISCHARGED THE CARGO FIRE BOTTLES AS A PRECAUTION, AND RETURNED TO IAH WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND REPLACED THE FORWARD BAGGAGE SMOKE DETECTOR, AND BOTH CARGO FIRE BOTTLES. OPERATIONAL CHECKS WERE PERFORMED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20051027000842005102700084SO 2005 10 27 C2XA05SH116 120051005A491014526850401 FIREWALL EMB 145 EMB145LR 3260212SO APU BAY CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713538 145527 SHV - DURING C-CHECK, APU FIREWALL HAS NUMEROUS CRACK ON RT SIDE. MAINTENENCE REPAIRED APU FIREWALL CRACK ON RT SIDE IAW EC5330-01483. THE AIRCRAFT WAS APPROVE FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20051027000852005102700085SO 2005 10 27 C2XA05SH117 120051005A532014530642401 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO FS 24-25 CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713538 145527 SHV - DURING C-CHECK, THE LT OMEGA BEAM HAS CORROSION BETWEEN FS 24-25. MAINTENANCE PERFORMED REPAIRED AT LT OMEGA BEAM BETWEEN FS 24-25 IAW EMB 145 SRM 53-00-10 FIGURE 202 SHEET 2. THE AIRCRAFT WAS APPROVE FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20051027000862005102700086NM 2005 10 27 DU4R2005191 120051006A5330 SKIN BOEING757 757232 1384965NM BS 395 CRACKED B DALAK NONE O OTHER ININSP/MAINT 1 SO15671DN 25332 FOUND STA 395-17 BETWEEN STR 16R AND 17R SKIN DENTED. SKIN DENTED OUT OF LIMITS AND STRINGER 16R CRACKED. CUT OUT DENTED SKIN AND CRACKED SECTION OF STRINGER. FABRICATED SKIN AND STRINGER REPAIR IAW B757 SRM 53-00-01 FIG 101 AND B757 SRM 53-00-03 FIG 201. SKIN REPAIR IS CLASS B AND HAS REINSPECT THRESHOLD AS REQUIRED IN B757 SRM 53-00-01 FIG 203 DETAIL II. 2L72 4F RTA2NM 20051027000872005102700087 2005 10 27 SWIA200515640 420050930A22166225734002 SERVO EMB 120 EMB120ER 3260203SO ELEVATOR MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07564SW1291712917 120339 BINDING AND FRICTION FELT IN ELEVATOR MOVEMENT. REPLACED ELEVATOR SERVO IAW EMB 120 MM 22-10-05. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20051027000892005102700089NM 2005 10 27 SWAA053064 120051005A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM BS 767 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 767, LBL 17. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051027000902005102700090NM 2005 10 27 2005UALA01096 120051006A3350 LIGHT BOEING777 777222 1385219NM PWA PW4077PW4077 NE CABIN LOOSE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29781UA 26945 AFT EEL LIGHT 1F RIPPED FROM POS. REPLACED EEL LIGHT. 2L72 4F4 FRTT0001SE E46NE 20051027000912005102700091 2005 10 27 SWAA053331 420051024A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 R1 DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. ADJUSTED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20051027000922005102700092NM 2005 10 27 SWAA053332 120051024A2761 SHAFT BOEING737 7373K2 13844BANM ACTUATOR SHEARED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29340LV 4714 23738 NR 4 GRND SPOILER INBD HYD ACTUATOR SHAFT SHEARED. REMOVED AND REPLACED NR 4 GROUND SPOILER INBD ACTUATOR PER MM. 2L72 4F RTA16WE 20051027000932005102700093NM 2005 10 27 QXEA200501286 120050923A7110 DIAPHRAGM BOMBDRDHC8 DHC8402 1390042NM LT NACELLE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09401QX 4031 LT NACELLE DIAPHRAM CRACKED. MAINTENANCE INSTALLED NEW DIAPHRAM IAW Q400 SRM 51-10-10 FOR HI LITES AND 51-42-05 FOR SOLID RIVETS. 2H72 4T RTA13NM 20051027000942005102700094NM 2005 10 27 QXEA200501288 120050924A5347 SEAT TRACK BOMBDRDHC8 DHC8402 1390042NM CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09401QX 4031 PDX: RT I/B SEAT TRACK IS CORRODED AT APPROX STA X527. MAINTENANCE REMOVED NR 13 SEAT TRACK. REF Q400 SRM 51-40-07. INSTALLED SEAT TRACK. INSTALLED FWD SPLICE AND WEB RIVETS AND DRIP TRAYS. REF Q400 SRM 51-40-15 FOR LOCK BOLTS IN SPLICE AND 51-42-05 FOR RIVETS IN WEBS AND DRIP TRAYS. 2H72 4T RTA13NM 20051027000952005102700095EA 2005 10 27 MASA200500556 120050716A2610GG670801053 ELEMENT CNDAIRCL600 CL6002C10 1390015EA LOOP-A MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07505MJ 10070 ASH 7265 IAD. EN ROUTE TO ATL HAD A RT BLEED CAUTION MESSAGE. THIS TURNED INTO A WARNING DURING TAXI WITH BLEEDS OFF. CREW REPORTED SMELL OF OIL ODOR, ALTHOUGH BLEEDS WERE OFF. AIRCRAFT FERRIED TO CLT WHERE MAINTENANCE REMOVED AND REPLACED SENSOR IN LOOP-A. 2L72 4F RTA21EA 20051027000962005102700096NM 2005 10 27 2005UALA01097 120051007A5340 STRINGER CLIP BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE BS 907 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29919UA 25386 FOUND STA 907 STR 8L CLIP IS CRACKED AT IB FASTENER. REMOVED AND REPLACED STR. CLIP PER SRM 51-40-02. 2L72 4F4 FRTA16WE E2GL 20051027000972005102700097NM 2005 10 27 2005UALA01098 120051007A5311 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE BS 440 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29919UA 25386 FOUND STA 440 BET STR 8L AND 9L FRAME CRACKED WHERE STOW BIN RAIL ATTACHES TO THE FRAME. REMOVED CRACKED AND ACCOMPLISHED A DOUBLER AND FILLER REPAIR PER MM 53-10-84, 2L72 4F4 FRTA16WE E2GL 20051027000982005102700098NM 2005 10 27 2005UALA01099 120051007A5311 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE BS 827 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29919UA 25386 AFT CABIN STA 827 FRAME IS CRACKED BETWEEN STR 8R AND 9R. REMOVED CRACK, ACCOMPLISHED A DOUBLER AND FILLER REPAIR PER MM 53-10-84. 2L72 4F4 FRTA16WE E2GL 20051027000992005102700099NM 2005 10 27 QXEA200501287 120050923A7110 DIAPHRAGM BOMBDRDHC8 DHC8402 1390042NM RT NACELLE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09401QX 4031 PDX: RT NACELLE DIAPHRAM CRACKED. MAINTENANCE INSTALLED NEW DIAPHRAM IAW Q400 SRM 51-40-10 AND 51-42-05. 2H72 4T RTA13NM 20051027001002005102700100NM 2005 10 27 CALA0500332 120051005A21401168175 HEATER BOEING757 757224 1384958NM R-4 DOOR INOPERATIVE A CALAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION APAPPROACH 1 SW2714118 27560 THE CREW REPORTED THAT THE AFT RIGHT LAV (LAV M) SMOKE DETECTOR WENT OFF WHILE ON APPROACH TO EWR. THERE WAS VISIBLE SMOKE WITH AN ELECTRICAL SMELL IN THE AFT LAV AREA. THE AFT LAVS WERE OPENED AND THE TRASH CONTAINERS WERE INSPECTED WITH NO EVIDENCE OF FIRE IN EITHER OF THE AFT LAVS. THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. AN INITIAL INSPECTION OF THE LIGHTS AND CEILING AREA FOUND NO EVIDENCE OF BURNED WIRES. MAINTENANCE FOUND THE R-4 DOOR HEATER BAD. THE DOOR HEATER WAS REPLACED IAW MM 21-45-06, PAGE 401. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA2NM 20051027001012005102700101NM 2005 10 27 05FDEA03245 120051005A5347 SEAT TRACK BOEING727 727200 138407ENM ZONE 200 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25465FE 21289 SEAT TRACK STA 480-620 LBL 24 FLANGE HAS CORROSION. REMOVED, FABRICATED, ALODINED, PRIMED AND INSTALLED NEW SEAT TRACK AT STA 480-690 ON LBL 24 ALL IAW FX B727 SRM 53-10-5, 53-10-2, 51-30-2 AND 51-10-2. 2L73 4F RTA3WE 20051027001022005102700102NM 2005 10 27 05FDEA03246 120051005A5347 SEAT TRACK BOEING727 727200 138407ENM ZONE 200 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25465FE 21289 SEAT TRACK STA 600-620 AT LBL 45 IS CORRODED. REMOVED, FABRICATED, ALODINED, PRIMED AND INSTALLED SEAT TRACK REPAIR AT STA 590-690 ON LBL45 ALL IAW FX B727-200 SRM 53-10-5, 51-3-2 AND 51-10-2. 2L73 4F RTA3WE 20051027001032005102700103NM 2005 10 27 05FDEA03249 120051005A5753651920812 FLAP TRACK BOEING727 727200 138407ENM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25484FE 21466 LEFT WING FLAP TRACK NR 1 FWD ATTACH POINT INSIDE HAS CORROSION. REMOVED AND REPLACED NR 1 FLAP TRACK IAW MM 27-51-031-4. 2L73 4F RTA3WE 20051027001042005102700104WP 2005 10 27 05FDEA03250 120051006A5320 SPLICE DOUG DC10 DC1010 3022110WP BS 1711-1721 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25389FE 46623 CTR LOWER CARGO COMPT STA 1711 TO STA 1721 L48R CORRODED AT INBOARD SIDE AROUND FASTENER. REMOVED CORRODED SPLICE IAW DC10 SRM 51-33-01 VOL 11. FABBED SPLICE IAW DAC DWG AFA 3113. ALODINED AND PRIMED IAW DC10 SRM 51-21-01 VOL 11. INSTALLED SPLICE IAW DC10 SRM 51-33-01 VOL 11. MAJOR REPAIR. 2L73 4F A22WE 20051027001052005102700105NM 2005 10 27 05FDEA03251 120051006A5320 STIFFENER BOEING727 727200 138407ENM BS 870 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION, C53-100-01, FOUND HORIZONTAL STIFFENER CORRODED AT CLAMP STANDOFF, BS 870, WL 198 LBL 8. REPLACED STIFFENER AT BS 870, LBL 6 WL 198 PER SRM 51-30-2. 2L73 4F RTA3WE 20051027001062005102700106WP 2005 10 27 ABXA050249 120051017A335041B004AD07G3 BATTERY DOUG DC9 DC941 302207NWP EMERGENCY LIGHT DEFECTIVE A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING PRE-DEPARTURE CHECK FOUND EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 AMM 33-53-00. 2L72 4F A6WE 20051027001072005102700107NM 2005 10 27 QXEA200501333 120051010A3150 LAMP BOMBDRDHC8 DHC8402 1390042NM INDICATOR INOPERATIVE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 SEA - FLIGHT 2411: VENT INLET LIGHT FAILS TO ILLUMINATE DURING AFT BAGGAGE SMOKE WARNING TEST. MAINTENANCE RELAMPED VENT INLET CLOSED LIGHT. OPS CHECK GOOD. NO COMPONENTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051027001082005102700108NM 2005 10 27 2005UALA01100 120051007A5311 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE BS 867 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29919UA 25386 CABIN FRAME CRACKED AT FASTENER HOLE STA 867 BETWEEN STR 7 AND 8 LEFT. REMOVED CRACK ACCOMPLISHED A DOUBLER AND FILLER REPAIR PER MM 53-10-84. 2L72 4F4 FRTA16WE E2GL 20051027001092005102700109NM 2005 10 27 2005UALA01101 120051008A5311 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE BS 927 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29919UA 25386 AFT CABIN STA 927 FRAME IS CRACKED BETWEEN STR 8L AND 9L. REMOVED CRACKED AREA, ACCOMPLISHED A DOUBLER AND FILLER REPAIR PER SRM 53-00-07 FIG.201 REPAIR 2. 2L72 4F4 FRTA16WE E2GL 20051027001102005102700110 2005 10 27 PIDA20050175 420051011A22104051601932 CONTROL PANEL BOEING737 737306 13844BGNM COCKPIT MALFUNCTIONED A PIDAK NONE O OTHER NRNOT REPORTED 1 SO05371PA 23543 AIRSPEED IN THE IAS/MACH WINDOW IS FROZEN IN PLACE AND CANNOT BE MANUALLY SET. REPLACED MODE CONTROL PANEL PER MM 22-11-01. 2L72 4F RTA16NE 20051027001112005102700111NM 2005 10 27 2005UALA01102 120051008A5311 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE BS 747 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29919UA 25386 AFT CABIN STA 747 FRAME CRACKED BETWEEN STR 8L AND 9L. REMOVED CRACK, INSTALLED REPAIR ANGLES AND FILLER PER MM 53-10-84 REPAIR III. 2L72 4F4 FRTA16WE E2GL 20051027001122005102700112NM 2005 10 27 2005UALA01103 120051008A5311 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE BS 727B CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29919UA 25386 AFT CABIN STA 727B FRAME IS CRACKED BETWEEN STR 8L AND 9L. REMOVED CRACK, INSTALLED ANGLE AND FILLER REPAIR PER MM 53-10-84. 2L72 4F4 FRTA16WE E2GL 20051027001132005102700113NM 2005 10 27 2005UALA01104 120051009A5311 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE BS 787 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29919UA 25386 AFT CABIN STA 787 FRAME CRACKED BETWEEN STR 8L AND 9L. REMOVED CRACK AND INSTALLED ANGEL REPAIR AND FILLER PER MM 53-10-84. 2L72 4F4 FRTA16WE E2GL 20051027001142005102700114NM 2005 10 27 AALA20050645 120051005A3350P4010049 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21669AA 25334 LGA - EMERGENCY SEAT PATH LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK AT FIRST CLASS OVERHEAD PANEL FOR EMERGENCY SEAT PATH LIGHTS IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20051027001152005102700115NM 2005 10 27 2005UALA01105 120051009A5311 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE BS 400 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29919UA 25386 STA 400 STR 8R AND 9R FUSELAGE FRAME CRACKED. REMOVED CRACK, INSTALLED REPAIR ANGLE AND FILLER PER MM 53-10-84. 2L72 4F4 FRTA16WE E2GL 20051027001162005102700116NM 2005 10 27 2005UALA01106 120051009A5311 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE BS 827 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29919UA 25386 AFT CABIN STA 827 FRAME IS CRACKED BETWEEN STR 8L & 9L. REMOVED CRACK, INSTALLED REPAIR ANGELS PER MM 53-10-84 REPAIR III. 2L72 4F4 FRTA16WE E2GL 20051027001172005102700117NM 2005 10 27 2005UALA01107 120051009A5311 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE BS 907 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29919UA 25386 AFT CABIN STA 907 FRAME IS CRACKED BETWEEN STR 8L AND 9L. REMOVED CRACK, INSTALLED REPAIR ANGLES PER MM 53-10-84 REPAIR III. 2L72 4F4 FRTA16WE E2GL 20051027001182005102700118NM 2005 10 27 AWXA200501273 120051009A5753 SKIN BOEING737 7373G7 1384595NM ZONE 600 DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED DISBOND ARE ON THE UPPER SURFACE OF THE RT OUTBOARD FORE FLAP, 92" FROM INBOARD END AT WBL 293.69L TO WBL 299.69L. MAINTENANCE CUT OUT AND REMOVED DAMAGE AREA IAW BOEING 737-300 SRM 51-70-10-2R3. FABRICATED REPAIR CORE, SEPTUM AND DOUBLER IAW BOEING 737-300 SRM 51-70-10-2R3. BONDED REPAIR PARTS TO IAW BOEING 737-300 SRM 51-70-10-2R3 AND 2R4. 2L72 4F RTA16WE 20051027001212005102700121NM 2005 10 27 AWXA200501276 120051015A5312651758243 BULKHEAD BOEING737 7373G7 1384595NM BS 180 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - MAJOR REPAIR - DURING C16 CHECK, DISCOVERED VERTICAL WEB CRACKED, .5 INCHES IN LENGTH, AT BS 180, WL 229 AND BL 17.1R. MAINTENANCE REMOVED DAMAGED AREA FROM VERTICAL WEB IAW BOEING 737-300 SRM 53-10-08-2R 12. FABRICATED REPAIR WEB AND TAPERED SHIMS IAW BOEING 737-300 SRM 53-10-08-2R 12,. INSTALLED FABRICATED REPAIR PARTS AT BS 180, WL 229 AND BL 17.1R IAW BOEING 737-300 SRM 53-10-08-2R12 FIG 201. 2L72 4F RTA16WE 20051027001232005102700123NM 2005 10 27 AWXA200501278 120051019A575369388485 TRACK BOEING737 7373G7 1384595NM ZONE 500 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - MAJOR REPAIR - DURING C16, DISCOVERED CORROSION ON THE LT INBOARD FLAP, INBOARD CAM TRACK AT WBL 71.00L. NO CORROSION REMOVAL LIMITS ARE AVAILABLE FOR CAM TRACK. MAINTENANCE REMOVED CAM TRACK AND INSTALLED NEW CAM TRACK ON THE LT INBOARD FLAP, INBOARD TRACK AT WBL 71.00L IAW BOEING 737-300 CMM 57-53-22. 2L72 4F RTA16WE 20051027001362005102700136NM 2005 10 27 ASMF200510002 120051003A2410729825L IDG BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE LT SIDE FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23804AM146807866 26271 AIRCRAFT RETURNED TO PLATFORM DURING TAXING. THE LT GENERATOR SHUTDOWN AND EICAS MESSAGES (RUDDER PCU, R ELEV PCU, L ELEV PCU, EQPT CLG TEST) WERE SHOWN. THE LT IDG REPORT WAS DEFERRED AND MAINTENANCE PROCEDURE WAS PERFORMED IAW MEL 24-00-1. THE LT IDG WAS REPLACED IAW MM 24-11-01, TESTED CORRECT. 2L72 4F4 FRTA2NM E17NE 20051027001382005102700138WP 2005 10 27 MWEA050110 120051006A5753 SKIN DOUG DC9 DC981 3022081WP FLAP CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31812ME 48006 LEFT OUTBOARD FLAP AT STATION 262, UPPER SKIN IS CRACKED. FABRICATED AND INSTALLED DOULBER. 2L72 4F A6WE 20051027001402005102700140WP 2005 10 27 MWEA050112 120051006A3411591041279 STATIC WICK DOUG DC9 DC981 3022081WP HORIZONTAL STAB LIGHTNING STRIKEA MWEAK NONE O OTHER ININSP/MAINT 1 GL31812ME 48006 RIGHT HORIZONTAL OUTBAORD TRAILING EDGE STATIC WICK MOUNTING BASE HAS LIGHTNING STRIKE DAMAGE. REMOVED AND REPLACED STATIC WICK. 2L72 4F A6WE 20051027001592005102700159NM 2005 10 27 2005UALA01112 120051009A2730 ELEVATOR BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE MALFUNCTIONED A UALAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 WP29313UA 23674 ABORTED TAKE OFF AT 140 KNOTS DUE TO NO ELEVATOR MOVEMENT. UNSECURED ELEVATOR BALANCE WEIGHT BECAME LODGED BETWEEN LOWER SURFACE OF BALANCE BAY & ANGLE USED TO SUPPORT ACCESS PANEL AT STABILIZER BS 94.07. SUBJECT BALANCE WEIGHT BECAME DISLODGED FROM BALANCE STRUCTURE DUE TO MISSING ATTACH FASTENERS. STRUCTURE INSPECTED (BOTH VISUAL AND HFEC) FOR DAMAGE & ADDITIONAL MISSING FASTENERS & ALL REQUIRED CORRECTIVE ACTION TAKEN PER SRM. NO ADDITIONAL MISSING FASTENERS IDENTIFIED. NEW BALANCE WEIGHTS ATTACHED & ELEVATOR BALANCED. ELEVATOR SYS OPS CHECKED & ALL CHECKED OK. ELEVATORS & TABS ARE REMOVED & OVERHAULED DURING HMVS. ENGINEERING CONSIDERS THIS TO BE AN ISOLATED EVENT. 2L72 4F4 FRTA16WE E2GL 20051027001612005102700161NM 2005 10 27 2005UALA01114 120051008A33501317 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE ROW 8R INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29107UA 26900 EMERGENCY CEILING LIGHT ABOVE ROW 8 RIGHT INOP. REPLACED LAMP. 2L74 4F4 FRTA20WE E24NE 20051027001642005102700164NM 2005 10 27 2005UALA01117 120051009A3350362624 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE SEAT 58 ABC INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29119UA 28812 EEL INOPERATIVE AT SEAT 58 ABC. REPLACED EEL LIGHT. 2L74 4F4 FRTA20WE E24NE 20051027000042005102700004EA 2005 10 27 ASOA05805 120050920A1100S157416 PLACARD CNDAIRCL600 CL6002B19 1900309EA CABIN PEELING A ASOAK NONE O OTHER ININSP/MAINT 1 SO27835AS 7258 DURING A C-CHECK IN MCN, THE EMERGENCY EXIT PLACARD NEAR THE FLIGHT ATTENDANTS SEAT WAS FOUND TO BE PEELING. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT PLACARD NEAR THE FLIGHT ATTENDANTS SEAT. (M) 2L72 4F RTA21EA 20051027000092005102700009EA 2005 10 27 COMA0560567 120051025A2133 OUTFLOW VALVE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE CABIN PRESSURE OUT OF POSITION A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01982CA 7168 OVERBOARD COOL SYSTEM WAS ALREADY ON DEFERRED MAINTENANCE LIST. SECURED VALVES IN PROPER POSITION. 2L72 4F4 FRTA21EA E15NE 20051027000112005102700011CE 2005 10 27 BSYA200500016 120051026A5250 DOOR BEECH 58 58 1152740CE CONT O520 IO520CB 17032SO COCKPIT UNSECURE E BSYAA UNSCHED LANDING O OTHER CLCLIMB 1 GL07297AT TH1349 COCKPIT DOOR POPPED OPEN AFTER TAKEOFF, RETURNED AND LANDED PROPERLY, SECURED DOOR AND CONTINUED WITH FLIGHT. 1L72 3O3 O 3A16 E5CE 20051027000132005102700013EA 2005 10 27 COMA0560563 120051022A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE EMERGENCY LIGHT BROKEN A COMAK NONE O OTHER ININSP/MAINT 1 SO01926CA 7027 OVERHEAD EMERGENCY LIGHT, BACK OF CABIN IS INOPERATIVE. REPAIRED BROKEN WIRE AT LIGHT. 2L72 4F4 FRTA21EA E15NE 20051027000192005102700019NM 2005 10 27 QXEA200501374 120051022A5753 FAILSAFE BOMBDRDHC8 DHC8402 1390042NM TE FLAPS WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09401QX 4031 PDX: LT INBOARD FLAP AFT FAIL SAFE CATCHER FOR THE OUTBOARD AFT ROLLER HAS HEAVY WEAR, REF AMM 27-54-01 PG 427, ITEM 26. MAINTENANCE REPAIRED IAW HORIZON EA 6-27-177 AND MOD SUM IS4Q-2700001 STEPS 4-9. 2H72 4T RTA13NM 20051027000282005102700028NM 2005 10 27 AWXA200501268 120050914A531465621258 KEELBEAM BOEING737 73733A 1384673NM BS 527 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW 23634 GYR - MAJOR REPAIR - DURING C20 CHECK DISCOVERED LEVEL 2 EXFOLIATION CORROSION ON KEEL BEAM AT BS 527, STR 28R AND WL 149.0. MAINTENANCE CUT OUT DAMAGED AREA IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5369-05278-ES2. FABRICATED OUTBOARD REPAIR ANGLE, STRUCTURAL FILLERS, BLANK SHEAR TIE, BLANK CLIP, FILLER AND REPAIR ANGLE IAW AWA ER NR 03-5369-05278-ES2. INSTALLED FABRICATED REPAIR PARTS ON KEEL BEAM AT BS 527, STR 28R AND WL 149.0 IAW AWA ER NR 03-5369-05278-ES2. 2L72 4F RTA16WE 20051027000372005102700037CE 2005 10 27 DXTA200501035 120051023A3260NPN POSITION SWITCH CESSNA750 750 2076810CE MLG OUT OF ADJUST E DXTAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL07921QS 7500241 NOSE GEAR RELEASED FROM LOCK IN FLIGHT CLIMBING THROUGH FL 280 AND FL 320 AND DESCENDING THROUGH FL 230. GEAR DID NOT EXTEND, NOR DID NOT OBSERVE THE GEAR UNLOCK LIGHT. PERFORMED GEAR BUMP TROUBLESHOOTING IAW CESSNA 750 MM 32-30-00. FOUND NOSE GEAR UPLOCK SWITCH OUT OF ADJUSTMENT. ADJUSTED NOSE GEAR UPLOCK SWITCH IAW CESSNA 750 MM 32-30-05. PERFORMED MULTIPLE GEAR SWINGS AFTER SWITCH ADJUSTMENT SYSTEM, CHECKS GOOD AT THIS TIME. 2L72 4J RTT00007WI 20051027000402005102700040CE 2005 10 27 DXTA200501031 120051019A3213 STRUT CESSNA500 560CESSNA 2076750CE MLG DISCHARGED E DXTAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL07806QS 5600614 LOUD BANG HEARD AT ROTATION ON THE AIRCRAFT. JACKED AIRCRAFT AND SERVICED MAIN STRUTS WITH FLUID AND NITROGEN IAW 560 MM 12-14-01. PERFORMED GEAR SWING SEVERAL TIMES WITH NO DISCREPANCES NOTED. SERVICED RESERVOIR IAW 560 MM 12-12-01. 2L72 4F RTA22CE 20051027000432005102700043NM 2005 10 27 QXEA200501370 120051020A5340 CLIP DHAV DHC8 DHC8202 2809007NM BS 387 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09345PH 476 PDX - THERE IS A CLIP CORRODED AT THE AFT SIDE OF FRAME X387.350, STRINGER 24, RIGHT SIDE. REPAIRED IAW HORIZON AIR EA 2-53-638 AND SRM 51-40-11. 2H72 4T RTA13NM 20051027000442005102700044NM 2005 10 27 QXEA200501371 120051020A5340 CLIP DHAV DHC8 DHC8202 2809007NM BS 424 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09345PH 476 PDX - THERE IS A CLIP CORRODED AT THE FORWARD SIDE OF FRAME 424-124, STRINGER 24, RIGHT SIDE. REPAIRED IAW HORIZON AIR EA 2-53-638 AND SRM 51-20-46, 51-20-36. 2H72 4T RTA13NM 20051027000452005102700045NM 2005 10 27 QXEA200501372 120051013A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM BS 375 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09345PH 476 PDX - RIGHT OUTBOARD CABIN SEAT TRACK HAS CORROSION INSIDE CHANNEL AND TOPSURFACE AT FS X375. REPAIRED IAW RD 8-53-1342 AND DHC-8-200 SRM 51-40-00. 2H72 4T RTA13NM 20051027000512005102700051EU 2005 10 27 YENA200577 120051021A2611PPA110100 SMOKE DETECTOR AIRBUS320 A320232 3930326EU CARGO BAY FAILED A YENAO OTHER N FALSE WARNING CRCRUISE 1 EA15561JB6869 6817 1927 RECEIVED ECAM SMOKE LAV & CRG DET FAULT. FOUND FWD CARGO DET 1WH FAULTY. REPLACED PER AMM 26-16-15-000-001. MSG NO LONGER PRESENT. ALL LAV/CGO SMOKE DET SELF TEST NORMAL. 2L72 4F RTA28NM 20051027000522005102700052EU 2005 10 27 YENA200578 120051021A2120 ODOR AIRBUS320 A320232 3930326EU CABIN DETECTED A YENAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15597JB 2307 LIVE TV SYSTEM INTERMITTENT THEN ELECTRICAL SMELL FROM SEAT ROWS 4 & 5. LIVE TV SYSTEM TURNED OFF EN ROUTE. PERFORMED TSM 24-00-00-810-823, INFO NOTICE 2002-T023TR & INSPECTED CEILING, SIDEWALL LIGHTS, SEAT TO SEAT CABLES, VDU'S, CONNECTORS AND NO DISCREPANCIES NOTED. PASSENGER DID NOT REPORT OR SECOND CREW MEMBER DID NOT CONFIRM ANY ODOR. THERE WAS A INTERMITTENT LOSS OF LTV AT SEVERAL OTHER SEATS NOT ADJACENT TO REPORTED SEATS. 2L72 4F RTA28NM 20051027000612005102700061EA 2005 10 27 SWIA200515721 120051023A274170609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CLCLIMB 1 NM07463SW 7820 A -STAB CH 1 STATUS MESSAGE-, AFTER TAKEOFF. REPLACED HSTCU. OPERATIONAL CHECK GOOD IAW MM 27-41-01. 2L72 4F RTA21EA 20051027000632005102700063WP 2005 10 27 IXXA05RNG072S 120050913A5753 SKIN DOUG DC8 DC872 302199BWP TE FLAP CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX46013 46013 DURING INSPECTION CHECK WAS FOUND A CORROSION ON RT INBOARD FLAP EXTERIOR SURFACE, BETWEEN STA XW3-XW92 (VIEW LOOKING UP). RT WING INBOARD FLAP SKIN WAS REMOVED AND REPLACED IAW DOUGLAS DRAWING 5642960. RIVETS WERE INSTALLED IAW DC8 SRM 51-1-21 PAGE 1 TO 7. 2L74 4F RT4A25 20051027000642005102700064WP 2005 10 27 IXXA05RNG073S 120050909A5730 SKIN DOUG DC8 DC872 302199BWP RT WING MISREPAIRED A IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW11721CX46013 46013 DURING INSPECTION CHECK WAS FOUND A IMPROPER REPAIR ON WING LEADING EDGE, STA XW 257.50, RT. PERMANENT REPAIR WAS PERFORMED IAW EWO ATI 57-044 AND EO ATI-090905. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR. 2L74 4F RT4A25 20051027001202005102700120NM 2005 10 27 AWXA200501275 120051015A5312651758245 BULKHEAD BOEING737 7373G7 1384595NM BS 178 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - MAJOR REPAIR - DURING C16 CHECK, DISCOVERED VERTICAL WEB CRACKED, .05 INCHES IN LENGTH, AT BS 178, WL 193 AND BL 17.1L. MAINTENANCE REMOVED VERTICAL WEB IAW BOEING 737-300 SRM 51-40-02-0G. FABRICATED VERTICAL WEB IAW BOEING 737-300 SRM 51-40-02-0G. INSTALLED VERTICAL WEB AT BS 178, WL 193 AND BL 17.1L IAW BOEING 737-300 SRM 51-40-05-0G FIGS 2 AND 3. 2L72 4F RTA16WE 20051027001272005102700127NM 2005 10 27 AWXA200501282 120051011A575465C2679913 SKIN BOEING737 7373G7 1384595NM ZONE 500 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - MAJOR REPAIR - DURING C16 CHECK,DISCOVERED 4 CRACKS, 1.0 INCHES IN LENGTH, ON THE NO. 1 LOWER SLAT SKIN BELOW THE INBOARD AUXILIARY TRACK FROM SS 274L TO SS 278L. MAINTENANCE CUT OUT DAMAGED AREA ON THE NO. 1 LOWER SLAT SKIN IAW BOEING 737-300 SRM 57-43-01-2R6 FIG 201. FABRICATED FILLER AND SPLICE PLATE IAW BOEING 737-300 SRM 57-43-01-2R6 FIG 201. INSTALLED FABRICATED REPAIR PARTS ON THE NO. 1 LOWER SLAT SKIN FROM SS 274L TO SS 278L IAW BOEING 737-300 SRM 51-43-01-2R6. 2L72 4F RTA16WE 20051027001292005102700129WP 2005 10 27 AALA20050639 120051004A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21569AA 49351 SFO - OVERHEAD EMERGENCY LIGHTS FOR ROWS 8, 9, AND 11 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT ROWS 8, 9, AND 11. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20051027001312005102700131NM 2005 10 27 AALA20050642 120051006A3350191411 BALLAST BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21392AN 29429 SFO - RIGHT AFT EMERGENCY EXIT SIDEWALL LIGHT INOPERATIVE. REPLACED BALLAST FOR RIGHT AFT EMERGENCY EXIT SIDEWALL LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20051027001422005102700142NM 2005 10 27 2005UALA01108 120051009A5340 STRINGER CLIP BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE BS 887 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29919UA 25386 AFT CABIN STA 887 STR 4R IS CRACKED AT STRINGER CLIP. REMOVED CRACK, INSTALLED REPAIR ANGLES AND CLIP PER SRM 53-00-03. 2L72 4F4 FRTA16WE E2GL 20051027001472005102700147EA 2005 10 27 SWIA200515726 120051019A2760C13045BA04 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA SPOILERS MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07713SK435 435 10174 SPLR/STAB FAULT STATUS ON EICAS. REPLACED NR 1 SSCU IAW MM 27-61-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051027001542005102700154EU 2005 10 27 SF200510201 120051020A2120 ODOR SAAB SF340 SF340A 7850100EU COCKPIT DETECTED A UHLAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL17118SD 118 FLT 9003 FWA-DAY FOUL ODOR IN COCKPIT & FWD GALLEY AREA. 2L72 4T RTA52EU 20051027001582005102700158 2005 10 27 2005UALA01111 420051009A3160 DISPLAY AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE COCKPIT INOPERATIVE A UALAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 WP29415UA 475 ABORTED TAKEOFF AT 142 KNOTS DUE TO CAPTAIN'S PFD BLANKED OUT. HOT BRAKES ECAM WITH ONE BRAKE OVER 600 DEGREES. 2L72 4F4 FRTA28NM E40NE 20051027001652005102700165NM 2005 10 27 2005UALA01118 120051009A339758784 CABLE BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE EMERGENCY LIGHTSINOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29643UA 25093 RT SIDE A-ZONE EEL INOPERATIVE. REPAIRED DAMAGED EEL FEEDER CABLE. 2L72 4F4 FRTA1NM E24NE 20051027001662005102700166NM 2005 10 27 2005UALA01119 120051009A335058784 CABLE BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE EMERGENCY LIGHTSINOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29643UA 25093 LT FWD LAV EEL LIGHT BAR INOPERATIVE. FOUND LIGHT CABLE BROKEN AND REPAIRED. 2L72 4F4 FRTA1NM E24NE 20051027001672005102700167NM 2005 10 27 2005UALA01120 120051010A5315 FLOORBEAM BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE BS 986 CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29919UA 25386 CABIN FLOORBEAM CORRODED ON UPPER CAP STA 986.5, RBL 25-45 AT WL 208. MAJOR REPAIR ACP'D PER MM 53-10-95, APPROX 50" SECTION OF UPPER "T" CAP SPLICE TYPE REPAIR SCHEME. 2L72 4F4 FRTA16WE E2GL 20051027001682005102700168WP 2005 10 27 05FDEA03292 120051007A5712 RIB DOUG DC10 DC1010 3022110WP RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE RT WING FIXED L/E COMPT AT STA XORS 660 ZONE 625 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 4 AND 6 VOL I. 2L73 4F A22WE 20051027001702005102700170WP 2005 10 27 05FDEA03294 120051007A5712 RIB DOUG DC10 DC1010 3022110WP RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE RT WING FIXED L/E COMPT AT STA XORS 522 ZONE 619 FOUND RIB CRACK. REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 4 AND 6 VOL I. 2L73 4F A22WE 20051027001722005102700172WP 2005 10 27 05FDEA03296 120051007A5712 RIB DOUG DC10 DC1010 3022110WP RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE RT WING FIXED L/E COMPT AT STA XORS 340 ZONE 618 FOUND RIB CRACK (4" LONG). REPAIR FORMER IAW SRM 57-20-00 FIG 1 SHEET 2 AND 3 VOL I. 2L73 4F A22WE 20051027001742005102700174NM 2005 10 27 QXEA200501289 120050924A5347 SEAT TRACK BOMBDRDHC8 DHC8402 1390042NM BS 674 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09401QX 4031 PDX: RT I/B SEAT TRACK IS CORRODED AT APPROX ATA X674. MAINTENANCE REMOVED SEAT TRACK. INSTALLED SEAT TRACK AT LOCATION IAW Q400 SRM 51-40-15 AND 51-42-05. ALSO INSTALLED MOUNT BOLTS AT FRAMES. 2H72 4T RTA13NM 20051027001752005102700175NM 2005 10 27 AWXA200501172 120051005A256020131A BATTERY BOEING737 737301 1384611NM FLASHLIGHT INOPERATIVE A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28325AW 23260 PHX - EEL - CREW REPORTED "FWD F/A EMERGENCY FLASHLIGHT INOP". MAINTENANCE REMOVED AND REPLACED THE FORWARD F/A EMERGENCY FLASHLIGHT BATTERY. OPERATIONAL CHECKS GOOD. 2L72 4F RTA16WE 20051027001762005102700176NM 2005 10 27 AWXA200501173 120050912A5753654647579 STIFFENER BOEING737 7373G7 1384595NM ZONE 500 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 MCN - DURING C18 CHECK DISCOVERED STIFFENER ASSY CRACKED, .75" IN LENGTH, INSIDE THE LT OUTBOARD MID FLAP, 100" FROM INBOARD END OF FLAP. MAINTENANCE WAS UNABLE TO REPAIR DUE TO THE LOCATION OF THE DAMAGE. MAINTENANCE REMOVED AND REPLACED THE LT OUTBOARD MID FLAP ASSEMBLY IAW AMERICA WEST AIRLINES TASK CARD C3L27002. 2L72 4F RTA16WE 20051027001772005102700177NM 2005 10 27 AWXA200501174 120050913A5312651630089 BULKHEAD BOEING737 7373G7 1384595NM BS 178 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 MCN - DURING C18 CHECK DISCOVERED VERTICAL BEAM WEB CRACKED, 1.0" IN LENGTH, AT BS 178, WL 230 AND BL 17.1L. MAINTENANCE CUT OUT DAMAGED SECTION OF WEB IAW BOEING 737-300 SRM 53-10-082R FIG 201. FABRICATED REPAIR WEB AND SHIM IAW BOEING 737-300 SRM 53-10-08-01. INSTALLED FABRICATED REPAIR PARTS, AT BS 178, WL 230 AND BL 17.1L, IAW BOEING 737-300 SRM 53-10-08-3R12 FIG 201. 2L72 4F RTA16WE 20051027001782005102700178NM 2005 10 27 AWXA200501175 120050909A575465C2679413 SKIN BOEING737 7373G7 1384595NM NR 2 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 MCN - DURING C18 CHECK DISCOVERED 5 CRACKS ON THE BOTTOM OF THE NR 2 SLAT SKIN AT THE INBOARD AUXILIARY TRACK, SS 175.00L. MAINTENANCE CUT OUT AND REMOVED DAMAGE PART OF SKIN IAW BOEING 737-300 SRM 57-43-01-2R FIG 201. FABRICATED FILLER AND SPLICE PLATE IAW BOEING 737-300 SRM 57-43-01-2R FIG 201. INSTALLED FABRICATED REPAIR PARTS IAW BOEING 737-300 SRM 57-43-01-2R FIG 201. 2L72 4F RTA16WE 20051027001802005102700180NM 2005 10 27 AWXA200501176 120050909A53206546877144 WEB BOEING737 7373G7 1384595NM BS 727 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 MCN - DURING C18 CHECK DISCOVERED WEB, LOCATED AT STRINGER 18A, CRACKED JUST FORWARD OF BULKHEAD 727. MAINTENANCE TRIMMED OUT CRACK IAW AMERICA WEST AIRLINES (AWA) ENGINEERING REPAIR (ER) NR 03-5361-05272-ES1. FABRICATED FILLER, GUSSET AND RADIUS FILLER IAW AWA ER NR 03-5361-05272-ES1. INSTALLED FABRICATED REPAIR PARTS JUST FORWARD OF BULKHEAD 727 IAW AWA ER NR 03-5361-05272-ES1. 2L72 4F RTA16WE 20051027001822005102700182NM 2005 10 27 AWXA200501178 120050912A5320 INTERCOSTAL BOEING737 73733A 1384673NM BS 294 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW 23634 GYR - DISCOVERED, DURING C20 CHECK, INTERCOSTAL AT STA 294.5, STR 16L, FORWARD END, CRACKED 1.0 INCHES IN LENGTH. MAINTENANCE REMOVED DAMAGED INTERCOSTAL IAW BOEING 737-300 SRM 51-40-02-0G. FABRICATED NEW INTERCOSTAL IAW BOEING 737-300 DWG 65-17684 AND SRM 51-30-01. INSTALLED FABRICATED REPAIR PARTS AT STA 294.5, STR 16L IAW BOEING 737-300 SRM 51-40-02-0G. 2L72 4F RTA16WE 20051027001832005102700183 2005 10 27 DJFA2005155 420051024A2210 AUTOPILOT SYS BRAERODH125 BAE125800A 1500285EU GARRTTTFE731TFE7315R 01518WP MALFUNCTIONED E DJFAO OTHER F FLT CONT AFFECTED DEDESCENT 1 EA23861CW 258061 WHEN CREW SELECTED VERTICAL SPEED ON MODE CONTROL PANEL TO BEGIN DESCENT, AC BEGAN STEEP CLIMB, AIRSPEED INDICATOR WAS NEAR BARBER POLE. CONTROL COLUMN YOKE WAS PUSHED FWD TO REDUCE CLIMB. AC FOUGHT CREW BY TRIMMING AC FURTHER NOSE UP. CLIMB WAS REPORTED TO HAVE STEEPENED, AC WAS CLOSING IN TO BASE OF RVSM AIRSPACE. AC WAS THEN ROLLED BY CREW TO APPROX 100 DEGREES BANK IN ORDER TO VECTOR LIFT DOWNWARD AND MAINTAIN A POSITIVE LOAD ON WINGS. FOLLOWING MANEUVER, AC STOPPED CLIMB. NML LANDING WAS MADE W/O FURTHER INCIDENT. MAINT HAS ISSUED MEL FOR AUTO-PILOT SYS AND MEL DUE TO VERT SPEED IND ON CAPTAINS SIDE JUMPING ERRATICALLY + / - 100 TO 300 FT. AIRSPEED INDICATION HAD SPLIT BETWEEN LT, RT INDICATORS.2L72 4F4 FRTA3EU E6WE 20051027001852005102700185SO 2005 10 27 1403102605 120051026A3244217K221 TIRE GULSTMG1159 GIV 3980115SO RROYCETAY TAY6118 EU ZONE 700 FAILED E N93AO OTHER O OTHER TXTAXI/GRND HDL 1 SO13403QS410 1403 LT NOSE TIRE FAILED ON LANDING. 2L72 4F4 FRTA12EA E25NE 20051027001872005102700187NM 2005 10 27 USAA051243 120051025A5311 FRAME BOEING737 7374B7 1384702NM BS 787 DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19779AU 24996 FOUND DAMAGE ON FUSELAGE FRAME STA 787, BETWEEN S-8R AND S-9R. CUT OUT DAMAGE, FABRICATED FRAME DOUBLER, INSTALLED DOUBLER IAW SRM 53-10-14, DEFECT SIZE: .5 INCH CRACK IN THE FUSELAGE FRAME. 2L72 4F RTA16WE 20051027001882005102700188NM 2005 10 27 USAA051249 120051025A5310 CREASE BEAM BOEING737 7373B7 1384580NM BS 727B-727C CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND CORROSION TOP SURFACE OF S-17L CREASE BEAM WEB; BETWEEN BS 727B AND 727C. REMOVED FASTENERS IN AREA, REMOVED SURF CORROSION, TREATED AND PRIMED, INSTALLED FASTENERS IAW SRM 53-60-13, DEFECT SIZE: 2" BY 1" BY 0.002" CORRODED AREA. 2L72 4F RTA16WE 20051027001902005102700190NM 2005 10 27 USAA051250 120051025A5320141T66015 BRACKET BOEING767 7672B7 1385107NM BS 287 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19656US 26847 FOUND CRACK, BS 287-S8L FRAME TO LATCH TORQUE TUBE HOUSING BRACKET. FABRICATED AND INSTALLED A NEW BRACKET IAW BOEING DRAWING NR 141T6605, DEFECT SIZE: 3 INCH CRACK. 2L72 4F RTA1NM 20051027001912005102700191EU 2005 10 27 USAA051257 120051026A5310D5347218820400 BEAM AIRBUSA319 A319112 3930323EU FUSLEAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19740UW 1265 FOUND CORROSION Y1162 FS 68, DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 53-41-04, DEFECT SIZE: 2" BY 21". 2L72 4F RTA28NM 20051027001922005102700192EU 2005 10 27 USAA051251 120051026A5311D53112830202 FRAME AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19740UW 1265 FOUND FRAME CORRODED, A FRAME C-16 -Y50. CORROSION LEVEL 1; TASK JA-220-53500. REPLACED BEAM PER SRM 51-72-11, DEFECT SIZE: 2" BY 2" AND 2" BY 2" CORROSION. 2L72 4F RTA28NM 20051027001932005102700193EU 2005 10 27 USAA051252 120051026A5315D5311282600201 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19740UW 1265 FOUND CORROSION UPPER SURF FLOORBEAM Y503.2 STA 14 - 16; CORROSION LEVEL 1; TASK JA-220-53500. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 53-11-14, DEFECT SIZE: 1/2" BY 4" AREA. 2L72 4F RTA28NM 20051027001942005102700194EU 2005 10 27 USAA051253 120051026A5320D5347219020200 FLOOR SUPPORT AIRBUSA319 A319112 3930323EU FR 64-66 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19740UW 1265 FOUND CORROSION BETWEEN FRAME 64 AND 66 AT 765. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-12-11, DEFECT SIZE: 2" BY 36" BY .100" 2L72 4F RTA28NM 20051027001952005102700195EU 2005 10 27 USAA051254 120051026A3213 STRUT AIRBUSA319 A319112 3930323EU NLG CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19740UW 1265 FOUND CORROSION UPPER HINGE OF NOSE LANDING GEAR TORQUE LINK, HINGE BORE. MESSIER DOWTY CMM 32-27-20 PG 609, DEFECT SIZE: 1-1/4" BY .008" DEEP; CORROSION LEVEL 1; TASK JA-74-32500. 2L72 4F RTA28NM 20051027001962005102700196EU 2005 10 27 USAA051255 120051026A5310D5347217220400 BEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19740UW 1265 FOUND BEAM CORRODED Y1162 - 1292 FS 66-68, DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 53-41-04, DEFECT SIZE: 2' BY 10". 2L72 4F RTA28NM 20051027001972005102700197EU 2005 10 27 USAA051256 120051026A5310D534720900100 BEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19740UW 1265 FOUND Y1292 FS 66, DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 53-41-04, DEFECT SIZE: 2" BY 30". 2L72 4F RTA28NM 20051027001982005102700198EA 2005 10 27 VNAA0510013 120051017A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A VNAAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL05213PS 7879 ON APPROACH WITH FLAPS AT 20 DEGREES, THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED WHEN SELECTING FLAPS 30 DEGREES. THE CREW FOLLOWED THE QRH AND LANDED SAFELY. MAINTENANCE RESET AND OPERATIONALLY CHECKED THE FLAP SYSTEM IAW CRJ200 AMM 27-54-00-710-801. OPS CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20051027001992005102700199WP 2005 10 27 ABXA050259 120051025A3260 ROLLER DOUG DC9 DC931 3022065WP PWA JT8 JT8D7B 52053NE MLG OUT OF ADJUST A ABXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL23928AX 47392 ON TAKEOFF, RT GEAR UNSAFE LIGHT REMAINED ILLUMINATED WHEN GEAR HANDLE PLACED IN UP POSITION. GREEN SAFE LIGHT WAS NOT ILLUMINATED. AC FELT LIKE GEAR WAS UP. RECYCLED GEAR DOWN (SHOWED NORMAL INDICATION) THEN BACK UP AND GEAR UNSAFE LIGHT WENT OUT. DEFERRED IAW FERRY PERMIT NR 022-05 AND GMM 07-04 FOR TRACKING AND GMM 04-04 CODE 05. CLEARING ACTION: FOUND RT MLG DOOR FAILED (GO) GAUGE CHECK. ADJUSTED RT MLG DOOR LATCH ROLLER IAW MM32-31-04-2-0101 STEP 4.A (5) (A) OPS CHECKED GOOD. PERFORMED TEST OF LANDING GEAR POSITION AND WARNING IAW 32-60-00-2-0101 STEP 2.A. 2L72 4F4 F A6WE E2EA 20051027002002005102700200NM 2005 10 27 05FDEA03487 120051025A5311 FRAME BOEING727 727100 1384036NM PWA JT8 JT8D1 52044NE BS 990 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 N00737 FRAME BS 990 BTWN STR 22 LT- 24 LT DAMAGED. [OPEN] 2L73 4F4 FRTA3WE E2EA 20051027002012005102700201EU 2005 10 27 05FDEA03488 120051025A2612 SMOKE DETECTOR AIRBUS300 A300F4605R 3930327EU GE CF6 CF680C2A5 NE E/E BAY MALFUNCTIONED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25679FE 793 INTERMITTENT AVIONICS SMOKE WARNING. DID NOT SMELL ANY SMOKE. REMOVED AND REPLACED AVIONICS SMOKE DETECTOR 11WA IAW A 300 MM 26-15-12-4. OPS CHECKS GOOD. SERVICEABLE PART CANNED FROM ACFT 653 MFG CG7GO-11. SN ON AB1058 SN OFF 1021. SERVICEABLE TAG B55383. OK FOR SERVICE. 2L72 4F4 FRTA35EU E13NE 20051028000012005102800001 2005 10 28 SWAA053365 420051025A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 & L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29634SW 27937 DURING SCHEDULED C4 CHECK, FOUND L1AND L2 DOORS EMERGENCY EVAC SLIDES OUT OF ADJUST. ADJUSTED SLIDES PER MM. 2L72 4F RTA16WE 20051028000022005102800002 2005 10 28 SWAA053366 420051025A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 & R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29634SW 27937 DURING SCHEDULED C4 CHECK, FOUND R1 AND R2 DOORS EMERGENCY EVAC SLIDES OUT OF ADJUST. ADJUSTED SLIDES PER MM. 2L72 4F RTA16WE 20051028000042005102800004NM 2005 10 28 05FDEA03490 120051025A5315 FLOORBEAM BOEING727 727100 1384036NM PWA JT8 JT8D7B 52053NE BS 480 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 BS 480 FLOORBEAM UPPER CHORD CORRODED AT RBL 48, WL 208. [OPEN] 2L73 4F4 FRTA3WE E2EA 20051028000052005102800005NM 2005 10 28 05FDEA03491 120051025A5330 SKIN BOEING727 727100 1384036NM PWA JT8 JT8D7B 52053NE BS 591 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 CRACK IN FUSELAGE OUTER SKIN STA 591 STR 15R FWD UPPER CORNER OF WING L/E ILLUMINATION LIGHT CUT OUT. REPAIRED PER FED EX EA 7-5330-95384. 2L73 4F4 FRTA3WE E2EA 20051028000072005102800007NM 2005 10 28 SB05137 120051026A335020121 CHARGER BOEING737 7374B7 1384702NM EMERGENCY LIGHTSINOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19777AU 24979 MCO - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHTS INOPERATIVE AT SEAT ROWS 23 AND 24ABC AND AT THE AFT SERVICE DOOR EXTERIOR. MAINTENANCE REMOVED AND REPLACED THE AFT RIGHT-HAND EMERGENCY LIGHT BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20051028000082005102800008GL 2005 10 28 C2XA05CL087 220051013A7297M24308213F CONNECTOR EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL ENGINE SHORTED A C2XAK NONE O OTHER CLCLIMB 1 SW2713988 145265 THE CREW REPORTED THE AIRCRAFT WOULD NOT ACCEPT CLIMB MODE UNTIL APPROX 7000FT, NORMAL AFTER THAT. ON APPROACH AT 3000 FT. SELECTED T/O MODE AND AIRCRAFT STUCK IN T/O RESERVE UNTIL LANDING. MAINTENANCE INSPECTED AND REPLACED CONNECTOR 10584 FOR NR 2 ENGINE RESISTOR MODULE. OPERATIONAL CHECKS WERE GOOD. 2L72 4T4 FRTT00011ATTE6CH 20051028000112005102800011NM 2005 10 28 QXEA200501378 120051026A3060 RELAY DHAV DHC8 DHC8202 2809007NM PROPELLER HEAT FAILED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09358PH 506 SEA FLIGHT 2297, TAXIING OUT TO THE RUNDWAY THE PROP HEAT LIGHT WAS ON AND PROP DEICE WAS NOT SELECTED. TRIED TO RECYCLE THE SYSTEM WITH NO SUCCESS. THE LEFT B-PHASE IS SHOWING 28 VOLTS AND OTHER PHASES WERE AT 14 VOLTS, THE PROP HEAT WILL NOT CYCLE. MAINTENANCE REPLACED THE K3 RELAY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051028000122005102800012NM 2005 10 28 QXEA200501375 120051022A5753 FAILSAFE BOMBDRDHC8 DHC8402 1390042NM TE FLAP DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09401QX 4031 LT INBOARD FLAP AFT FAIL SAFE CATCHER FOR THE INBOARD AFT ROLLER HAS CRACKED AND JAMMED AGAINST THE ROLLER. MAINTENANCE REPAIRED IAW HORIZON EA 6-27-117 AND MOD SUM IS4Q-2700001, STEPS 4-9. 2H72 4T RTA13NM 20051028000132005102800013EA 2005 10 28 ASOA05809 120050925A5220 HANDLE CNDAIRCL600 CL6002B19 1900309EA ESCAPE HATCH CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27835AS 7258 DURING A C-CHECK IN MCN, THE CREW EMERGENCY ESCAPE HATCH HANDLE WAS FOUND TO POSSIBLY BE CRACKED. S/D - MAINTENANCE INSPECTED THE CREW EMERGENCY ESCAPE HATCH HANDLE. NO DEFECTS NOTED. (M) 2L72 4F RTA21EA 20051028000162005102800016NE 2005 10 28 SWAA053334 220051024A7261 SEAL BOEING737 7373H4 1384600NM GE CFM56 CFM56* 13802NE NR 2 ENG OIL SYSLEAKING A SWAAO OTHER KBJFLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SW29315SW 23337 722405 ELECTRICAL ODOR IN CABIN FOR APROX 5 MINUTES DURING CLIMB. FOUND NR 2 ENGINE OIL LEAK AT NR 3 OIL BEARING SEAL. MX FERRY TO MDW AND REMOVED AND REPLACED NR 2 ENGINE PER MM. 2L72 4F4 FRTA16WE E2GL 20051028000172005102800017NM 2005 10 28 SWAA053335 120051025A53126546568 BULKHEAD BOEING737 7373H4 1384600NM BS 1016 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D-CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT STR 7L. REPAIRED WEB PER BFG ER & SRM. 2L72 4F RTA16WE 20051028000182005102800018NM 2005 10 28 SWAA053336 120051025A57126545445 RIB BOEING737 7373H4 1384600NM RT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D-CHECK, FOUND RIGHT WING RIB LOWER CHORD CRACKED AT WBL 135.5, BETWEEN STR 2 & STR 3. REPAIRED RIB PER BFG ER. 2L72 4F RTA16WE 20051028000202005102800020NM 2005 10 28 SWAA053338 120051025A53306552988 SKIN BOEING737 7373H4 1384600NM BS 947 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29332SW 23696 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, BETWEEN STR 23L & STR 24L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051028000222005102800022NM 2005 10 28 QXEA200501376 120051022A5230 BRACKET BOMBDRDHC8 DHC8402 1390042NM CARGO DOOR DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09401QX 4031 PDX - AFT CARGO DOOR LOWER FORWARD STOP BRACKET LOWER FORWARD BOLT SPINS IN NUT PLATE WHEN TORQUED. MAINTENANCE CHECKED ADJUSTMENT OF AFT BAGGAGE DOOR IAW Q400 TASK 52-31-00-820-801. NO ADJUSTMENTS WERE NECESSARY. 2H72 4T RTA13NM 20051028000232005102800023NM 2005 10 28 2005UALA01093 120051007A5330 SKIN BOEING747 747422 1384935NM PWA 4056 PW4056 NE BS 1740-2180 DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29196UA 28715 AFT FUSELAGE DAMAGED FROM CONTACT WITH GROUND WHILE STATIONARY. DAMAGE IS FROM STA 1740 TO 2180, STR 46L TO 46R. BODY SECTION 46 STRUCTURE COMPLETELY REPAIRED BY BOEING AOG STRUCTURES TEAM. STATION 1480 BULKHEAD BEING REPAIRED INDEPENDENTLY BY REPLACEMENT OR SRM. NEW GEARSET BEING INSTALLED. 2L74 4F4 FRTA20WE E24NE 20051028000272005102800027NE 2005 10 28 05FDEA03496 220051025A7210786269 CASE BOEING727 727200 138407ENM PWA JT8 JT8D9A 52048NE NR 1 ENGINE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25484FE 21466 NR 1 ENGINE IGV CASE CRACKED 3 PLACES ALONG FWD. AND AFT SIDE WELD BEAD. REMOVED NR 1 ENGINE IGV CASE ON WK CARD 7200-2002,N/R00937. REMOVED AND REINSTALLED ENGINE NOSE COWL ,NOSE DOME FOR ACCESS IAW MM 71-10-021-4, MM71-10- 041-4 LEAK AND OPS. CHECKED GOOD IAW 71-10-021. 2L73 4F4 FRTA3WE E2EA 20051028000282005102800028WP 2005 10 28 05FDEA03497 120051026A5730ARC0292503 SKIN DOUG DC10 DC1010 3022110WP LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE LT WING REAR SPAR AT STA XORS 308 FOUND EXFOLIATION CORROSION IN THE UPPER SKIN PANEL SUPPORT. REMOVED CORROSION IAW SRM 51-21-01 PAR 34 FOUND OUT OF LIMITS. REPAIRED IAW SRM 57-00-01 FIG 3 SHEET 2. 2L73 4F A22WE 20051028000322005102800032NM 2005 10 28 SWAA053344 120051025A55516551524 FITTING BOEING737 7373H4 1384600NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED D CHECK, FOUND HORIZ STAB ATTACH FITTING LUG FACES CORRODED. REPAIRED LUG FACES PER SRM. 2L72 4F RTA16WE 20051028000372005102800037NM 2005 10 28 SWAA053349 120051025A3350BR2013 LIGHT BOEING737 7373H4 1384600NM CABIN WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED A2 CHECK, FOUND EEPLS STRIP WORN BETWEEN ROW 5 TO ROW 7. REMOVED AND REPLACED STRIP PER MM. 2L72 4F RTA16WE 20051028000382005102800038NM 2005 10 28 SWAA053350 120051024A53116520722 FRAME BOEING737 7373H4 1384600NM BS 492 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 492, FWD CARGO DOOR CUTOUT. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051028000392005102800039NM 2005 10 28 SWAA053351 120051026A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 867 BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP BROKEN AT BS 867, STR 23R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051028000402005102800040NM 2005 10 28 SWAA053352 120051025A335065C34691 LIGHT BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29333SW 23697 DURING SCHEDULED SERVICE CHECK, FOUND BULLNOSE EMERGENCY LIGHT INOP AT ROW 4 DEF. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20051028000432005102800043NM 2005 10 28 SWAA053361 120051026A53116546546 SHEAR TIE BOEING737 7373H4 1384600NM BS 787 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, STR 25L TO STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051028000452005102800045NM 2005 10 28 SWAA053363 120051026A53216545834 FLOOR PANEL BOEING737 7373H4 1384600NM COCKPIT FLOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED D CHECK, FOUND COCKPIT FLOOR WEB CORRODED AT BS 267, RBL 12. REPAIRED FLOOR WEB PER SRM. 2L72 4F RTA16WE 20051028000462005102800046 2005 10 28 SWAA053364 420051025A256565C16820 HOOK BOEING737 7373H4 1384600NM L1 DOOR GIRT BARLOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29634SW 27937 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT HOOK LOOSE. SECURED HOOK PER SRM. 2L72 4F RTA16WE 20051028000492005102800049SO 2005 10 28 C2XA05SH122 120051023A533014520554003 SKIN EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713978 145180 SHV - RON AIRCRAFT GOUGE IN SKIN FWD OF FRAME 20 AFT OF FRAME 19 BETWEEN STRINGERS 11L AND 12L. MAINTENANCE REPAIRED GOUGES IN SKIN FWD OF FRAME 20 AFT OF FRAME 19 BETWEEN STRINGERS 11L AND 12L IAW EMB 145 SRM 53-21-01 & IC 2005-145/4770. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20051028000522005102800052NM 2005 10 28 DL76S050652 120051024A2741 MODULE BOEING767 767332 1382001NM TRIM CONTROL FAILED A DALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO27138DL 25409 UNSHEDULED STAB TRIM EICAS MESSAGE. ABORTED T/O AT 100 KTS. REPLACED LEFT STAB TRIM CONTROL MODULE BRAKE PRESSURE SWITCH. 2L72 4F RTA1NM 20051028000542005102800054NE 2005 10 28 DL76G050656 220051026A7261791701589 SCAVENGE PUMP BOEING767 767332 1382001NM GE CF6 CF680C2B6F 30025NE LT ENGINE FAILED A DALAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 SO271611B 30595 704805 FL 390 DURING CABIN WALK NOTICED SMELL IN MID CABIN AREA. MID CABIN SMOKE DETECTOR SOUNDED, NO SMOKE NOTICED. NO SMELL OR SMOKE IN COCKPIT. REPLACED LUBE SCAVENGE PUMP IN LEFT ENGINE. 2L72 4F4 FRTA1NM E13NE 20051028000612005102800061EU 2005 10 28 05FDEA03507 120051026A2133 OUTFLOW VALVE AIRBUS310 A310203 3930313EU CABIN PRESSURE MALFUNCTIONED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25413FE 397 PASSING 11,000 FT ON CLIMB-OUT, GOT EXCESSIVE CABIN ALTITUDE ECAM WARNING. CABIN ALT WAS 10170. FOLLOWED ECAM AND QRH. NO FAULT LIGHTS COULD GET OUTFLOW VALVES TO CLOSE IN AUTO OR MANUAL. AIR TURN BACK TO KME. 2L72 4F RTA35EU 20051028000622005102800062SO 2005 10 28 ENHA2005PA310 120051014A2822 PUMP PIPER PA31 PA31350 7103110SO LYC O540 LTIO540J2BD 41533EA FUEL BOOST MALFUNCTIONED E ENHAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 AL0378GA 318352030 L158068A IN FLIGHT RT ENG SHUTDOWN. PILOT ATTEMPT AIR RESTART, UNABLE TO AIR START, SECURED ENG, LANDED, 1 ENG OPERATING. OBSERVED FUEL STREAMING OFF OF RT WING, OBSERVED FUEL IND (QTY) DROPPING FASTER THAN LT IND, R ENG SPUTTERED, SHUTDOWN. NO EVIDENCE OF FUEL LEAKAGE, RESIDUE. MAINT INSP RT ENG, FUEL SYS OPS NML. PERFORMED NML GROUND START OF RT ENG AND OPS RUN UP, ENG RUN UP NML. SUMPED RT OB FUEL TANK LESS THAN 1 GAL FUEL REMAINING. R IB EST .1250 REMAINING, L IB EST .3750 REMAINING, L OB FULL JUST BELOW FILLER. FUEL SYS FILTERS FREE OF CONT. L FUEL LOW BOOST PUMP INOP MEL EXISTED AT TIME OF INCIDENT 28-1C (M) PROCEDURE. NO NONROUTINE MAINT PERFORMED. AC RELEASED FOR TEST FLIGHT, SYS CK NORMAL. 1L72 3O3 O A20SO E14EA 20051028000682005102800068NM 2005 10 28 SWAA053367 120051025A323365448105 ACTUATOR BOEING737 737317 138447PNM RT MLG W/W FAULTY A SWAAO OTHER O OTHER CLCLIMB 1 SW29693SW 23174 RT MLG EXTENDED WITH GEAR HANDLE IN "OFF" POSITION. RECYCLED GEAR HANDLE-GEAR RETRACTED. REMOVED AND REPLACED RT MLG UPLOCK ACTUATOR PER MM. 2L72 4F RTA16WE 20051028000692005102800069SO 2005 10 28 C2XA05BT074 120051021A32201170C000004 LEG ASSY EMB 145 EMB145LR 3260212SO NLG FAULTY A C2XAO OTHER J WARNING INDICATION CLCLIMB 1 SW27139941241112411 145291 CREW REPORTED, LANDING GEAR AIR/GROUND FAILURE, GEAR WOULD NOT RETRACT. RETRACTED GEAR WITH DOWNLOCK RLS. MAINTENANCE REMOVED AND REPLACED THE NOSE GEAR LEG IAW EMB145 AMM 32-20-01. PERFORMED GEAR RETRACTION, OPS.CHECKED GOOD. NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20051028000702005102800070SO 2005 10 28 C2XA05IA119 120051021A3260852701 SWITCH EMB 145 EMB145LR 3260212SO NLG INOPERATIVE A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2716919 145393 IAH - FLIGHT 2989, THE CREW REPORTED THAT THE NLG DOORS WOULD NOT CLOSE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NLG DOOR SEQUENCE PROXIMITY SWITCH, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20051028000712005102800071SO 2005 10 28 C2XA05IA120 120051020A323122250100003 VALVE EMB 145 EMB145XR 3260214SO FUSELAGE INOPERATIVE A C2XAO OTHER J WARNING INDICATION DEDESCENT 1 SW27161127961 7961 145660 ON DESCENT, A LARGE RUMBLING TO BE FELT AND HEARD AS POWER WAS REDUCED CONTINUING UNTIL GEAR WAS FULLY EXTENDED. PERFORMED A FLY-BY OF TOWER, AND LANDED WITHOUT INCIDENT. MX INSPECTED AIRCRAFT AND FOUND A LOOSE BONDING JUMPER, AND AIRCRAFT WAS APPROVED FOR A TEST FLIGHT. THE TEST FLIGHT WAS UNSATISFACTORY, AND ANOTHER FLY-BY OF THE TOWER CONFIRMED THE NOSE LANDING GEAR DOORS REMAINED OPEN. THE AIRCRAFT LANDED AT RSW WITHOUT INCIDENT, WHERE THE AIRCRAFT WAS INSPECTED AND APPROVED FOR A FERRY FLIGHT TO IAH. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NLG DOOR SOLENOID VALVE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20051028000782005102800078NM 2005 10 28 SWAA053354 120051025A53306545776 SKIN BOEING737 7373H4 1384600NM BS 947 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29333SW 23697 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 24R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051028000812005102800081NM 2005 10 28 AALA20050706 120051020A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM BS 328 INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21951AA 29538 TUL- BATTERY PACKS AT BS 328 FOR EMERGENCY LIGHTS IN FIRST CLASS SEATS FAILED OPERATIONAL CHECK. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN FIRST CLASS SEATS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20051028000822005102800082NM 2005 10 28 AALA20050696 120050829A5315 FLOORBEAM BOEING767 767323 1385205NM BS 347 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21389AA 27449 FLOORBEAM AT STATION 347 HAS CORROSION REMOVED ON UPPER AND LOWER SURFACE BEYOND SRM LIMITS. AREA IS 1.0 BY .027 INCH AT RT BUTTLINE 26, 1.2 BY .033 INCH AT RIGHT BUTTLINE 33, 1.1 BY .036 INCH AT RIGHT BUTTLINE 36 AND 1.0 BY .048 INCH AT RIGHT BUTTLINE 37. DEPTH IS .048. REMOVED AND VERIFIED CORROSION REMOVED. FABRICATED REPAIR STRAP FROM 301 AND A HALF HARD STAINLES STEEL .063 THICK. ALODINED ALL BARE ALUMINUM SURFACES. FINISHED BLEND AND REPAIR PARTS WITH TWO COATS OF BMS 10-11 PRIMER. FILLED BLENDS WITH BMS592. INSTALLED REPAIR STRAP WITH BMS595 SEALANT USING BACB30NWG FASTENERS FOR NEW LOCATIONS AND SAME TYPE AS EXISTING FASTENERS AT EXISTING LOCATIONS. INSTALL WITH 4 6D SPACING. 2L72 4F RTA1NM 20051028000832005102800083NM 2005 10 28 AALA20050707 120051020A3350D71701100 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21951AA 29538 TUL - BATTERY PACK AT STATION 589 FOR EMERGENCY LIGHTS AT RIGHT SIDE EMERGENCY DOORS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT RIGHT SIDE EMERGENCY DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20051028000852005102800085NM 2005 10 28 AALA20050697 120050829A5315 FLOORBEAM BOEING767 767323 1385205NM BS 325 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21389AA 27449 AFW FLOORBEAM AT STATION 325 HAS CORROSION REMOVED ON UPPER AND LOWER SURFACE BEYOND SRM LIMITS. AREA IS 1.0 INCH BY .021 INCH AT RT BUTTLINE 16, 1.1 BY .040 AT RT BUTTLINE 19.5, 1.2 BY .045 INCH AT RT BUTTLINE 25.5 AND 2.0 BY .021 INCH AT RT BUTTLINE 54 WITH A DEPTH OF .045. REMOVED AND VERIFIED CORROSION REMOVED. FABRICATED REPAIR STRAP FROM 301 AND A HALF HARD STAINLES STEEL .063 THICK. ALODINED ALL BARE ALUMINUM SURFACES. FINISHED BLEND AND REPAIR PARTS WITH TWO COATS OF BMS 10-11 PRIMER. FILLED BLENDS WITH BMS592. INSTALLED REPAIR STRAP WITH BMS595 SEALANT USING BACB30NWG FASTENERS FOR NEW LOCATIONS AND SAME TYPE AS EXISTING FASTENERS AT EXISTING LOCATIONS. INSTALL WITH 4 6D SPACING. 2L72 4F RTA1NM 20051028000862005102800086NE 2005 10 28 AALA20050698 220051023A7200 ENGINE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE RIGHT MAKING METAL A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21984TW 53634 709779 BUF INFLIGHT T305/23OCT - RIGHT ENGINE WAS SHUT DOWN BY CREW DUE TO OIL FILTER CLOG LIGHT ILLUMINATING. FOUND METAL IN SCREEN AND FILTER AND OIL TANK. REPLACED ENGINE. FLIGHT DATA RECORDER DOWNLOAD REQUESTED BY ENGINEERING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA6WE E9NE 20051028000892005102800089WP 2005 10 28 AALA20050699 120051022A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217519A 49896 SFO - LEFT AND RIGHT NUMBER ONE DOOR EMERGENCY LIGHTS ON CEILING INOPERATIVE. REPLACED FORWARD BATTERY PACK FOR LEFT AND RIGHT NUMBER ONE DOOR EMERGENCY LIGHTS ON CEILING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051028000902005102800090NM 2005 10 28 AALA20050700 120051023A3350P2010031303 LIGHT BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21197AN 32391 JFK - EMERGENCY LIGHTS FROM ROW 26 AFT TO LEFT AND RIGHT NUMBER 4 DOOR INOPERATIVE. FOUND LEFT NUMBER 4 DOOR FORWARD EXIT LIGHT L759 SHORTED. REPLACED LEFT NUMBER 4 EXIT LIGHT ASSEMBLY FOR EMERGENCY LIGHTS FROM ROW 26 AFT TO LEFT AND RIGHT NUMBER 4 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20051028000912005102800091WP 2005 10 28 AALA20050704 120051026A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21570AA 49352 DFW - OVERHEAD EMERGENCY EXIT LIGHT IN AFT CABIN BETWEEN LAVATORIES INOPERATIVE. REPLACED BATTERY PACK AND CHARGER FOR OVERHEAD EMERGENCY EXIT LIGHT IN AFT CABIN BETWEEN LAVATORIES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20051028000942005102800094 2005 10 28 SWAA053368 420051026A2565D31354 SLIDE BOEING737 7373T5 1384608NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29694SW 23061 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051028000952005102800095NM 2005 10 28 SWAA053369 120051026A3350311500 LENS BOEING737 7377H4 1384404NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29733SA 27865 BULLNOSE EMERGENCY LIGHT LENS LOOSE AT ROW 10. SECURED LENS PER MM. 2L72 4F RTA16WE 20051028000962005102800096NM 2005 10 28 SWAA053370 120051025A3350PH22300L STRIP BOEING737 7377H4 1384404NM CABIN DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29743SW 29279 DURING SCHEDULED MV2 CHECK, FOUND PHOTOLUMINESCENT STRIP DAMAGED AT FWD END. REMOVED AND REPLACED STRIP PER MM. 2L72 4F RTA16WE 20051028000982005102800098WP 2005 10 28 05FDEA03498 120051026A5730 SKIN DOUG DC10 DC1010 3022110WP LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE LT WING REAR SPAR AT STA XORS 338 FOUND CORROSION EXFOLIATION ON UPPER SKIN PANEL SUPPORT. REPAIRED IAW SRM 57-00-01 FIG 3 SHEET 2 VOL 1. 2L73 4F A22WE 20051028001002005102800100NM 2005 10 28 QXEA200501384 120051025A3010 DEICE SYSTEM BOMBDRDHC8 DHC8402 1390042NM MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM09401QX 4031 SEA FLIGHT 2434, DEICE PRESSURE CAUTION ILLUMINATED INFLIGHT. CHECKLIST WAS RUN. CAUTION LIGHT STAYED ILLUMINATED UNTIL DESCENDING THROUGH 10,000 FEET. MAINTENANCE INTEROGATED CDS WITH NO RELATED FAULT CODES FOUND. PERFORMED FUNCTIONAL TEST OF THE AIRFRAME PNEUMATIC DEICING SYSTEM IAW Q400 AMM TASK 30-11-00-720-801. NO DISCREPANCIES NOTED AND NO REOCCURANCE OF CAUTION LIGHT. ALL INDICATIONS NORMAL. OPS/FUNCTIONAL TEST IS GOOD. SUSPECT MOISTURE PREVIOUSLY PRESENT IN SYSTEM. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051028001022005102800102NM 2005 10 28 DLM88050663 120051026A3397 WIRE HARNESS DOUG MD88 MD88 3023688NM SEAT 2CD DAMAGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27911DL 49542 ON INSPECTION, FOUND EMERGENCY TRACK LIGHT OUT SEAL 2CD. REPLACED LIGHT HARNESS. 2L72 4F RTA6WE 20051028001032005102800103 2005 10 28 DL757050664 420051026A2565D30656132 SLIDE BOEING757 757232 1384965NM LT CABIN DOOR UNSERVICEABLE A DALAK NONE O OTHER ININSP/MAINT 1 SO27667DN 25035 ON INSPECTION, FOUND AFT LT CABIN DOOR SLIDE PRESSURE IND OUT OF GREEN BAND. REPLACED SLIDE. 2L72 4F RTA2NM 20051028001042005102800104NM 2005 10 28 DL757050665 120051006A5330146N313128 SKIN BOEING757 757232 1384965NM BS 1253 DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27656DL 24396 FUSELAGE SKIN DENTED AT STA 1253 BETWEEN S-4L & S-5L. THE DENT IS CUT OUT AND EXTERNAL ALUMINUM DOUBLER AND STRUCTURAL FILLER ARE INSTALLED WITH ALUMINUM RIVETS. 2L72 4F RTA2NM 20051028001052005102800105NM 2005 10 28 DL777050666 120051027A492038005501 APU BOEING777 777232 1385232NM APU BAY FIRE A DALAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27864DA 29736 APU TAILPIPE FIRE ON PUSHBACK. NO DAMGE TO AIRCRAFT. REPLACED APU. 2L72 4F RTT00001SE 20051028001062005102800106NM 2005 10 28 SWAA053355 120051025A53306545774 SKIN BOEING737 7373H4 1384600NM BS 767 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29355SW 25250 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 23L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051028001072005102800107NM 2005 10 28 SWAA053356 120051026A57536546434 SKIN BOEING737 7373H4 1384600NM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29382SW 26588 DURING SCHEDULED C4 CHECK, FOUND RT WING INBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM. 2L72 4F RTA16WE 20051028001092005102800109NM 2005 10 28 SWAA053358 120051026A53106545834 CREASE BEAM BOEING737 7373H4 1384600NM BS 270-344 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED D CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 270 TO BS 344, WL 208. REPAIRED CREASE BEAM PER SRM. 2L72 4F RTA16WE 20051028001142005102800114SO 2005 10 28 C2XA05BT071 120051007A3350375921 SIGN EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT FAULTY A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712996 145296 DURING SERVICE ROUTINE CHECK ON OVERNIGHT, MAINTENANCE FOUND ROW 12 OVERHEAD EMERGENCY EXIT SIGN NOT WORKING. REMOVED AND REPLACED ROW 12 OVERHEAD EMERGENCY EXIT SIGN IAW EMB145 AMM 33-50-15, OPS CHECKED GOOD. 2L72 4T RTT00011AT 20051028001172005102800117SO 2005 10 28 C2XA05BT072 120051015A33501317 LAMP EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT FAULTY A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715985 145248 DURING 5A/3A INSPECTION AND SERVICE AND ROUTINE CHECK MAINTENANCE FOUND THE PASSENGER AND SERVICE DOOR EMERGENCY LIGHTS NOT WORKING. REMOVED AND REPLACED LAMPS IN SERVICE DOOR EMERGENCY LIGHT ASSEMBLY AND RECONNECTED WIRE SPLICE FOR PASSENGER DOOR EMERGENCY LIGHTS IAW EMB145 33-50-00, OPS CHECKED SYSTEM GOOD. 2L72 4T RTT00011AT 20051028001182005102800118SO 2005 10 28 C2XA05BT073 120051017A3350110049 CHARGER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT FAULTY A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712967 145133 CREW REPORTED, THE EMERGENCY LIGHT ON THE LEFTHAND SIDE WING/FUSELAGE FAIRING IS NOT OPERATING AND EMERGENCY LIGHT IN CABIN NOT ILLUMINATING. MAINTENANCE REMOVED AND REPLACED NR 1 EMERGENCY LIGHT BATTERY CHARGER IAW EMB145AMM 33-50-04, OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20051028001192005102800119SO 2005 10 28 C2XA05IA114 120051014A3350 LIGHT EMB 145 EMB145 3260210SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714974 145161 STL - FLIGHT 3221, DURING PREFLIGHT INSPECTION, THE AISLE PATH LIGHTING STRIP BETWEEN SEATS 6A AND 7A WAS FOUND TO BE INOPERATIVE. MAINTENANCE PLACED THE AIRCRAFT ON MEL 33-50-00/2 CAT C CONTROL NUMBER 061034, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20051028001212005102800121EA 2005 10 28 QXEA200501381 120051026A3350E520005705A CIRCUIT BOARD CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT MALFUNCTIONED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09600QX 10005 SEA - EMERGENCY LIGHTS IN THE CABIN AS WELL AS THE EMERGENCY LT ON STATUS MESSAGE KEEPS CYCLING ON AND OFF. MAINTENANCE REPLACED THE PCB-5 IN JB11. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20051028001232005102800123 2005 10 28 PIDA20050182 420051024A2230 POWER LEVER BOEING737 7373G7 1384595NM LT ENGINE OUT OF ADJUST A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05380WL 23218 LEFT POWER LEVER DID NOT GO TO FLIGHT IDLE WITH LEVEL CHANGE SELECTED, THUS RESULTING IN ASYMMETRICAL THRUST. PERFORMED CABLE LUB PER MM 12-26-00. 2L72 4F RTA16WE 20051028001242005102800124EA 2005 10 28 QXEA200501383 120051021A2820M259882230 O-RING CNDAIRCL600 CL6002C10 1390015EA FUEL SYSTEM LEAKING A QXEAK NONE K FLUID LOSS ININSP/MAINT 1 NM09601QX 10009 DEN - MAINTENANCE FOUND POSSIBLE FUEL LEAK AT BOTTOM OF AIRCRAFT FUSELAGE. REPLACED 2 O-RINGS AT THE REFUEL/DEFUEL HOUSING ADAPTER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20051028001252005102800125EA 2005 10 28 SWIA200515732 120050506A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07445SW 7651 FS 280 RBL 9 (2 EA) CLIPS CRACKED I/B & O/B. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED RIGHT O/B CLIP PER CRJ200 SRM 51-42-06 & 51-40-20. INSTALLED RIGHT I/B CLIP PER CRJ200 SRM 51-42-06. 2L72 4F RTA21EA 20051028001262005102800126EA 2005 10 28 SWIA200515733 120050506A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07445SW 7651 FS 280 LBL 9, 2 EA CLIPS CRACKED I/B & O/B. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED CLIPS IAW ENG DWG 601R31113 AND CRJ200 SRM CG 51-42-06 & 51-42-20. 2L72 4F RTA21EA 20051028001272005102800127EA 2005 10 28 SWIA200515734 120050506A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 621 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07445SW 7651 LEFT FLOORBEAM ANGLE AT FS 621 BETWEEN LBL 27 AND LBL 45. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR PARTS PER REO 601R-53-61-117 AND CRJ200 SRM 51-42-06 AND 51-42-21. 2L72 4F RTA21EA 20051028001282005102800128SO 2005 10 28 CHQA200500188 120051026A335066903 BULB EMB 135 EMB135KL 3260302SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11382SK 145624 EMERGENCY PROXIMITY STRIP IN FROM OF REAR LAVATORY HAS FRAYED AND BROKEN WIRES. REPAIRED WIRE SPLICE IAW EMB 140 WM 20-21-00. OPS CHECK GOOD AT THIS TIME. 2L72 4F RTT00011AT 20051028001292005102800129NM 2005 10 28 DL76S050661 120051014A5311145T10017 FRAME BOEING767 767332 1382001NM BS 903.5 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27138DL 25409 THE INNER CHORD OF THE LT STA 903.5 FRAME WAS FOUND WITH A 0.60 INCH LONG CRACK. REPAIR ANGLE INSTALLED PER ACTS PP B767-53-21657, REF ER/A 450982-14AD, AD 2003-18-10. 2L72 4F RTA1NM 20051028001302005102800130EA 2005 10 28 SWIA200515735 120050506A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 621 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07445SW 7651 RIGHT FLOORBEAM ANGLE AT FS 621.00 BETWEEN RBL 27 AND RBL 45. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR PARTS PER REO 601R-53-61-117 AND CRJ200 SRM 51-42-06 AND SRM 51-42-21. 2L72 4F RTA21EA 20051028001332005102800133EU 2005 10 28 KBM2005F00303 120050920A3210 BEARING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE CROSSBEAM SPINNING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19351WM 2167 CROSSBEAM, LAMINATED BEARING, SPINNING, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051031000022005103100002EA 2005 10 31 SWIA200515738 120050514A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA BS 621 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07918SW 7651 CRACKED SUPPORT ANGLE FS 621; LBL 45; WL 73.5. ITEM FOUND AT C-CHECK INSPECTION. REPAIR PARTS INSTALLED AS REQUIRED AND ALL WORK DONE IAW REO 601R-53-61-004 SRM 51-42-06 AND 51-42-21. 2L72 4F RTA21EA 20051031000032005103100003EA 2005 10 31 SWIA200515739 120050514A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 461 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07918SW 7645 MAIN CABIN OVER PRESSURE FLOOR AT STA 461.00 BL 9 FLOORBEAM ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. FLOORBEAM INSTALLED AS REQUIRED IAW EO 600-31068 AND SRM 51-42-06; 51-42-21. 2L72 4F RTA21EA 20051031000072005103100007EA 2005 10 31 SWIA200515743 120051018A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07924SW 7681 FUSELAGE; UPPER TRANSVERSE BEAM ANGLE CRACKED; FS 280.00 LBL 12.0. ITEM FOUND AT C-CHECK INSPECTION. 2L72 4F RTA21EA 20051031000082005103100008EA 2005 10 31 SWIA200515744 120051018A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA FLOORBEAM CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07924SW 7681 FUSELAGE; FLOORBEAM ATTACH CLIPS ARE CRACKED; I/B AND O/B - FS 280.00; LBL 9.0. ITEM FOUND AT C-CHECK INSPECTION. 2L72 4F RTA21EA 20051031000102005103100010EA 2005 10 31 SWIA200515746 120051018A5320 WEB CNDAIRCL600 CL6002B19 1900309EA BS 628.5 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07924SW 7681 AFT EQUIP BAY; ESB LOWER WEB IS CRACKED ON LT SIDE AT PANEL CUTOUT; FS 628.50; LBL 38.40. ITEM FOUND AT C-CHECK INSPECTION. 2L72 4F RTA21EA 20051031000132005103100013NE 2005 10 31 N9W2005F00000 120051014A32301945E55 SWIVEL SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL1 60030NE RT MLG SHEARED E N9WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA11986AH 760438 HELICOPTER TAKING OFF, WENT TO RETRACT LANDING GEAR AND HAD A RED GEAR UNLOCKED LIGHT. PILOTS FOLLOWED PROCEDURE, FLEW AIRCRAFT BACK TO DEPARTURE. AIRCRAFT LANDED UNEVENTFULLY, AFTER AIRCRAFT WAS SHUTDOWN MAINTENANCE FOUND RT GEAR DOOR RETRACTION/EXTENSION LINK SWIVEL ON MAIN GEAR ASSY SHEARED. PART POSSIBLY HAD A SMALL UNDETECTABLE CRACK FOR SOMETIME WHICH EVENTFULLY LDE TO A SHEARED CONDITION. RECOMMENDATION MIGHT BE AN ANNUAL DYE PENETRANT INSPECTION AROUND BASE OF SWIVEL FITTING. (EA25200604717) (K) 1G72 3U3 UNCH1NE E19EU 20051031000152005103100015NE 2005 10 31 HALA0500905 220050827A7321114E6112G120 EEC BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE NR 2 MALFUNCTIONED A HALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13481HA 55126 WHILE CLIMBING OUT AT 5000 FT, WE GO A RT ENGINE FADEC SELECT LIGHT ABNORMAL WAS PERFORMED BUT SOON AFTER EXPERIENCED A MOMENTARY RT ENGINE SHUTDOWN. ENGINE CAME BACK TO NORMAL, RETURNED TO AIRPORT. FOUND FAULT 732167 FOR EEC, 2 REPLACED, NR 2 EEC PERFORMED RTS, CHECK OK IAW MM. OK FOR SERVICE. (K) 2L72 4F4 FTRA6WE E00061EN 20051031000212005103100021CE 2005 10 31 KC82005F00007 120050907A29101116 HOSE LEAR 35 36A 5170603CE GARRTTTFE731TFE731* 01518WP HYDRAULIC SYS LEAKING E KC8AO OTHER K FLUID LOSS NRNOT REPORTED 1 GL2371CK 035 CREW NOTICED A LOSS OF HYDRAULIC PRESSURE. PERFORMED EMERGENCY GEAR EXTENSION AND LANDED WITHOUT INCIDENT. AUX HYDRAULIC PUMP SUPPLIED PRESSURE FOR FLAPS AND BRAKES UPON LANDING. FOUND NOSE GEAR ACTUATOR RETRACT HOSE LEAKING AT BULKHEAD FITTING IN THE NOSE AVIONICS BAY. REPLACED HOSE ASSY WITH NEW HOSE. NOTHING NOTICEABLE FOUND IN HYDRAULIC FILTERS. SERVICED HYDRAULIC SYSTEM. PERFORMED PURGING OF NITROGEN FROM LANDING GEAR HYDRAULIC SYSTEM. PERFORMED GEAR RETRACTION CHECKS AND LEAKAGE CHECKS. PERFORMED ENGINE DRIVEN HYDRAULIC PUMP OPERATIONAL CHECKS. ALL WORK PERFORMED IAW MM. (K) 2L72 4F4 F A10CE E6WE 20051031000312005103100031NM 2005 10 31 S2YA05039 120050630A2421ALT3524 GENERATOR DORNERDO32 DO328300 NM PWA 306 PW306B NE LT AC INOPERATIVE A S2YAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL13360SK12188 3136 SHORTLY AFTER DEPARTURE OF FLIGHT, THE LT ALTERNATOR FAILED. MAINTENANCE REQUEST THE AC RETURNED TO DEPARTURE AIRPORT. THE CREW PERFORMED AN AIR-TURN-BACK. MAINTENANCE REPLACED THE LT AC GENERATOR (ALTERNATOR) AND WITH OPERATIONAL CHECK GOOD THE AC WAS RETURNED TO SERVICE. (K) 2H72 4T4 FRTA55NM E35NE 20051031000372005103100037NE 2005 10 31 AMTA200500854 220051011A7200 LINE BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE TEMP SENSOR LOOSE A AMTAO OTHER J WARNING INDICATION CRCRUISE 1 GL11552TZ 32586 EICAS MSG LT ENG OVHT DISPLAYED WITH ENG OVHT ILLUMINATED. LGT EXTIN AFTER THRUST REDUCTION. FOUND NR 1 ENG TEMP SENSOR SENSE LINE LOOSE ON FAN AIR MODULATING VALVE, SECURED IN PLACE, RAN ENGINE, OPS CHECK NORMAL. (K) 2L72 4F4 FRTA2NM E12EU 20051031000382005103100038EU 2005 10 31 KBM2005F00300 120050929A2121 BLADES SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE EVAP BLOWER BROKEN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19751H 116 3403 FAN BLADES, ALL BROKEN ON AFT EVAPORATOR BLOWER. REMOVED ASSY AND REPLACED WITH REBUILT UNIT. (K) 1G71 3U3 U H9EU E19EU 20051031000412005103100041NM 2005 10 31 AMTA200500900 120051016A3350233T3210300 CONTROL PANEL BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE EMERGENCY LIGHT UNSERVICEABLE A AMTAK NONE O OTHER ININSP/MAINT 1 GL11519AT 27975 EGRESS LIGHTING ONLY TURNS OFF IN ARMED POSITION. RR PILOTS EMERGENCY LIGHT PANEL IAW MM. OPS CHECK GOOD. (K) 2L72 4F4 FRTA2NM E12EU 20051031000462005103100046NM 2005 10 31 AMTA200500909 120051019A3397 WIRE BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE EMERGENCY LIGHT DISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11522AT 29330 ROW 30 EMERGENCY FLOOR PAX LIGHT INOPERATIVE. RECONNECTED WIRES AT ROW 30. OPS CHECK GOOD. (K) 2L72 4F4 FRTA2NM E12EU 20051031000542005103100054NM 2005 10 31 USAA051032 120050819A5320 PAN BOEING737 737301 1384611NM CFMINTCFM56 CFM563B2 13802EU BS 1000 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19356US 23559 CLT - C4 - PAN AND SERVICE DOOR, .25 INCH CRACK, BS 1000, STRINGER S26R. INSTALLED DOUBLER IAW EA. (K) 2L72 4F4 FRTA16WE E21EU 20051031000732005103100073EU 2005 10 31 KBM2005F00287 120050919A6520350A33215300 BEARING SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1D NE TAIL ROTOR TORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19215LA 2143 LAMINATED BEARING, UNIT RUBBER TORN, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051031000742005103100074 2005 10 31 KBM2005F00293 420050922A3452 LAMP SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE TRANSPONDER INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH 22228 2884 TRANSPONDER, LAMPS INOPERATIVE, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051031000752005103100075EU 2005 10 31 KBM2005F00289 120050919A80120174078030 DRAIN VALVE SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1D NE START DRAIN LEAKING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19215LA1223 2143 7158 ENGINE FUEL START DRAIN VALVE LEAKING IN THE WEEPING HOLE, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051031000882005103100088NE 2005 10 31 SFO2005F00003 220050621A720031079041 HEAT SHIELD CESSNA500 500CESSNA 2076602CE PWA JT15 JT15D1 52060NE LT ENGINE FAILED E SFOAO OTHER O OTHER NRNOT REPORTED 1 EA2327SF 4053 5000064 685354 INSP, A LOUD SCRAPING NOISE WAS HEARD WHEN FAN WAS TURNED. BORESCOPE OF TURBINE SEC., AFTER EXHAUST DUCT WAS REMOVED, NR 4 BRG HSG HEAT SHIELD WAS FOUND BROKEN, TWISTED, IN 3 SEPARATE PIECES, WAS RUBBING ON AFT FACE OF NR 3 LOW PRESSURE TURBINE DISC. DISC WAS GOUGED, HAD TO BE REPLACED ALONG WITH 10 BLADES. MINOR DAMAGE TO EXHAUST DUCT AT GAP BETWEEN DUCT, NR 3 LPT WHERE PIECES OF HEAT SHIELD HAD EXITED, A CRACK WAS NOTED ON 1 OF THE SUPPORT STRUTS. NR 4 BRG HAD PITTING ON ROLLERS, BUT COULD NOT BE CONFIRMED THAT IT WAS DUE TO LOSS OF HEAT SHIELD. ALL HEAT SHIELD MNTG HARDWARE WAS INTACT AND TIGHT. PART TT AND/OR UNRECOGNISED FATIGUE CRACK WERE CONTRIBUTING FACTORS TO THIS FAILURE. 1L72 4F4 F A22CE E1NE 20051031001142005103100114CE 2005 10 31 S2YA05047 120050803A3060HCE4A31 BOOT BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA RT PROP DEICE SHORTED A S2YAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 GL1392SK 144603829 UE92 DURING FLIGHT, THE CREW REPORTED A GLOW COMING FROM THE RT PROPELLER. AFTER CONSULTING WITH DISPATCH AND MAINTENANCE, THE CREW PERFORMED AN AIR-TURN-BACK. MAINTENANCE INSPECTED THE RT PROP AND FOUND THE DEICE BOOT HAD SHORTED AND BURNED. MAINTENANCE REPLACED THE RT PROP AND RETURNE THE AC TO SERVICE. (K) 2L72 4T3 TRTA24CE E2NE 20051031001202005103100120CE 2005 10 31 GUU2005F00044 120050817A55201016200111 BRACKET BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA RT ELEVATOR CORRODED A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO298755218547 UE216 AT SCHEDULED ROUTINE MAINTENANCE, RT ELEVATOR OB HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RT ELEVATOR OB HINGE BRACKET. (K) 2L72 4T3 TRTA24CE E2NE 20051031001212005103100121CE 2005 10 31 GUU2005F00050 120050929A2697W80A22 WIRE BEECH 1900 1900D 1154162CE PWA PT6 PT6A6 52043EA FIRE EXTING CHAFED A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO1787555 UE234 RT ENGINE FIRE EXTINGUISHER DISCHARGE ANNUNCIATOR ILLUMINATED IN FLIGHT. REPAIRED CHAFED WIRE BENEATH FORWARD FLOORBOARD 131AT. (K) 2L72 4T3 TRTA24CE E4EA 20051031001232005103100123EA 2005 10 31 UG82005F00008 120050821A34110856KV10 PROBE CNDAIRCL604 CL604 1900301EA GE CF34 CF34* NE PITOT/STATIC SYSDENTED E UG8AO OTHER O OTHER NRNOT REPORTED 1 GL23599DA 5498 5498 (REF CNTRL NR: PA 05-004) ALTITUDE SPLIT BETWEEN NR 1 AND NR 2 ALTIMETERS OF 250 FT AT 17000 FT. THE RT PITOT/STATIC PROBE HAS IMPACT DAMAGE. REPLACED THE RT PITPT/STATIC PROBE. COMPLETED ALTITUDE AND LEAK CHECKS IAW MM. RETURNED AIRCRAFT TO SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20051031001292005103100129SO 2005 10 31 UG82005F00011 120050922A2760HTL452 FASTENER GULSTM GULSTMGV GULFSTREAMGV3980116SO SWITCH BRACKET LOOSE A UG8AO OTHER O OTHER NRNOT REPORTED 1 GL235101 4445 AC551 550 (REF: GM05009) GROUND SPOILER CHECK IS INTERMITTENT. IT WAS DISCOVERED THAT THE AFT OF 2 HI-LOK FASTENERS SECURING THE LT GROUND SPOILER STOW SWITCH MOUNTING BRACKET TO THE WING HAD ITS NUR MISSING AND PIN BACKED OUT. ON THE RT WING BRACKET THE NUT AND PIN WERE MISSNG. THIS CONDITION ALLOWED THE BRACKETS TO MOVE, INTERMITTENTLY CAUSING THE SWITCHES NOT TO ACTUATE. CONDITION WAS CORRECTED WITH INSTALLATION OF NEW FASTENERS. OPERATIONAL TEST OF GROUND SPOILER SYSTEM WAS NORMAL. (K) 2L72 4F RTA12EA 20051202000032005120200003EU 2005 12 2 USAA051429 120051130A5315D5311281820401 FLOORBEAM AIRBUSA321 A321211 3930370EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19164UW 1425 FLOORBEAM Y254 AT FR 21, DEFECTIVE PART REPLACED WITH IDENTICAL PART IAW SRM 51-72-11, DEFECT SIZE: 1 INCH DIA. 2L72 4F RTA28NM 20051031001782005103100178NE 2005 10 31 HALA0501023 220051013A7200 BEARING BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE ENGINE FAILED A HALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13477HA5242 55122 13242 ON CLIMBOUT AT 16,00 FEET GOT (ENG R SURGE) LIGHT. FOLLOWED BY SOME SMOKE IN CABIN. FOLLOWED BY (ENG R SYS FAIL) LIGHT AND (R OIL FILTER) LIGHT. REDUCED POWER ON RT ENGINE RETURNED FOR LANDING. RT ENGINE INDICATIONS WERE NORMAL AFTER POWER REDUCTION. HOWEVER AFTER LANDING SOME VIBRATIONS. ENGINE SHUTDOWN AFTER LANDING. FOUND METAL IN GEAR BOX SUMP SUSPECT BEARING FAILURE ENGINE REPLACED. TEARDOWN REPORT TO FOLLOW. (K) 2L72 4F4 FTRA6WE E00061EN 20051031001842005103100184NM 2005 10 31 AMTA200500798 120051005A3350MS25308302 SWITCH BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE EMERGENCY LIGHT UNSERVICEABLE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11518AT 27974 EXTERIOR EMERGENCY LIGHTS DO NOT TEST AT L4 AND R4 DOORS FROM P-62 PANEL. (NOSE GEAR). REMOVED AND REPLACED EXT EMERGENCY LIGHT SWITCH ON P-62 PANEL, EMERG LT SYS OPS AND TEST NORMAL. (K) 2L72 4F4 FRTA2NM E12EU 20051101000092005110100009NM 2005 11 1 QXEA200501388 120051028A24203170801A GENERATOR DHAV DHC8 DHC8202 2809007NM AC SYSTEM MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09353PH6508 702 496 PDX FLIGHT NR 2094 RECEIVED NR 1 AC GENERATOR CAUTION LIGHT IN CRUISE, TRIED A RESET PER CHECKLIST, CAUTION LIGHT REMAINED ON. MAINTENANCE REPLACED NR 1 AC GENERATOR IAW DHC-200 AMM TASK 24-21-00-400-801. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051101000102005110100010NM 2005 11 1 QXEA200501387 120051028A2797 WIRE DHAV DHC8 DHC8202 2809007NM SPOILER CLUTCH SHORTED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09346PH 477 PDX FLIGHT NR 2133 PFCS - PUSH OFF SPOILER NR 2 LIGHT ILLUMINATED, COMPLIED WITH CHECKLIST. MAINTENANCE TROUBLESHOT, INSPECTED AND FOUND LEFT WING OUTBOARD SPOILER CLUTCH SWITCH WIRES AT 27-15-01. 19G22 AND 23C22N SHORTED TOGETHER FROM CORROSION IN ENVIROMENTAL SPLICING. REMOVED CORRODED SPLICE AND RE-SPLICED WIRING IAW MM TASK 20-45-07-300-802, SUBTASK 20-45-07-910-003, PARAGRAPH C(1) (Q)-J. PERFORMED OPERATIONAL TEST OF THE ROLL SPOILER CLUTCH SWITCHES IAW MM TASK 27-14-36-710-801. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051101000182005110100018SO 2005 11 1 RAIA00510025 120051029A3350 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03823HK 145475 PRE-FLIGHT INSPECTION - IAD - EMERGENCY LIGHT IN CABIN NOT WORKING. MAINTENANCE RELAMPED THE BULB. 2L72 4T RTT00011AT 20051101000212005110100021EA 2005 11 1 COMA0560574 120051027A27419960013 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA CO-PILOT YOKE MALFUNCTIONED A COMAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION DEDESCENT 1 SO01710CA 7241 FLIGHT 5116 - STAB TRIM 1 AND 2 DISCONNECT AND MACH TRIM INOPERABLE. REPLACED THE CO-PILOT TRIM DISCONNECT SWITCH. 2L72 4F RTA21EA 20051101000222005110100022NM 2005 11 1 SB05140 120051028A3397 WIRE BOEING737 7373B7 1384580NM EMERGENCY LIGHT BROKEN A USAAK NONE O OTHER ININSP/MAINT 1 EA19527AU 23862 CLT - PILOT REPORTED THE LOW LEVEL EMERGENCY LIGHTS AT SEAT ROWS 5, 9 AND 11 INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AND REMOVED AND REPLACED LOW LEVEL LAMP AT SEAT ROW 5, LEFT SIDE. OPERATIONAL CHECK OF LIGHTS GOOD. 2L72 4F RTA16WE 20051101000242005110100024NM 2005 11 1 SWAA053388 120051029A335020131 BATTERY PACK BOEING737 7373H4 1384600NM EMERGENCY LIGHTSINOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED SERVICE CHECK, FOUND FWD CABIN EMERGENCY LIGHTS INOP AT FWD END. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20051101000262005110100026NM 2005 11 1 SWAA053390 120051027A3350MS155721 BULB BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 DURING SCHEDULED SERVICE CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 2. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20051101000272005110100027NM 2005 11 1 SWAA053391 120051028A3350D71702001 BATTERY PACK BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20051101000292005110100029NM 2005 11 1 SWAA053393 120051028A3350604222 CHARGER BOEING737 7373K2 13844BANM L1 & R1 DOOR INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29340LV 23738 DURING SCHEDULED C1 CHECK, FOUND L1 AND R1 DOORS LOWER EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM. 2L72 4F RTA16WE 20051101000312005110100031NM 2005 11 1 SWAA053395 120051028A521065C36231 SKIN BOEING737 7373K2 13844BANM L1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29340LV 23738 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR SKIN CRACKED AT LOWER FWD CORNER. REPAIRED L1 DOOR SKIN PER SRM. 2L72 4F RTA16WE 20051101000322005110100032NM 2005 11 1 SWAA053396 120051028A2560P2070001 FLASHLIGHT BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29356SW 25251 AFT CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2L72 4F RTA16WE 20051101000352005110100035NM 2005 11 1 SWAA053399 120051028A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29402WN 29814 EEPLS COVER MISSING AT ROW 1 ABC. INSTALLED COVER PER MM. 2L72 4F RTA16WE 20051101000362005110100036 2005 11 1 SWAA053400 420051030A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29483WN 32472 L1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATING LOW. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20051101000372005110100037WP 2005 11 1 IXXA05SMN243S 120051013A5753 VANE DOUG DC8 DC871F 302199DWP TE FLAPS ELONGATED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING ROUTINE C CHECK INSPECTION, RT WING CTR L/E SLOT VANE HAS ELONGATED HOLES AT STA XILD 7095. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05461 DATED 10-10-05, SEMAN DWG NR ED-4081 DATED 10-08-05, EO SEMAN NR 20051290 DATED 10-10-05. REMOVED FASTENERS IAW DC8 SRM 51-1-21, DC8 SRM 51-3-0. REMOVED DAMAGED SECTION IAW SEMAN DWG NR ED-4081. NDT INSPECTED IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D EXTERNAL REPAIR DOUBLER, FILLER & INTERNAL DOUBLER IAW SEMAN DWG NR ED-4081. CLEANED, TREATED, INSTALLED REPAIR PARTS IAW SEMAN DWG NR ED-4081, DC8 SRM 51-1-21, DC8 SRM 51-3-0, DC8 SRM 51-1-20D, DC8 SRM 51-3-1 (TQ). 2L74 4F RT4A25 20051101000432005110100043NM 2005 11 1 SWAA053406 120051030A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD CARGO DOOR AFT FRAME CUTOUT, NR 5 STOP FITTING. REPAIRED SKIN PER BFG ER. 2L72 4F RTA16WE 20051101000452005110100045NM 2005 11 1 SWAA053408 120051030A53116546532 FRAME BOEING737 7373H4 1384600NM BS 490 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 490, FWD CARGO DOOR CUTOUT. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20051101000472005110100047NM 2005 11 1 SWAA053410 120051029A3350101331 LENS BOEING737 7373A4 1384585NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29669SW 23752 EMERGENCY EXIT LIGHT LENS MISSING AT RT OVERWING EXIT. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20051101000482005110100048NM 2005 11 1 SWAA053411 120051027A53306545775 SKIN BOEING737 7373A4 1384585NM BS 790 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29678AA 23290 DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 790, STR 18L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051101000532005110100053WP 2005 11 1 ABXA050261 120051011A53125917579507 BULKHEAD DOUG DC9 DC941 302207NWP PWA JT8 JT8D1 52044NE FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23962AX 47768 AFT PRESSURE BULKHEAD DOOR UPPER LT CORNER 13 DOUBLER HAD RADIAL CRACK EXTENDING FROM STOP DRILL. CRACK EXCEEDED APPLICABILITY AND CRACK REPAIR LIMITS FOR PREVIOUS J060088-1 ANGLE REPAIR. STOP DRILLED CRACKS AND REPAIRED IAW SRM. 2L72 4F4 F A6WE E2EA 20051101000542005110100054NE 2005 11 1 SB05139 220051029A73209334M96P02 SENSOR BOEING737 7374B7 1384702NM GE CFM56 CFM56* 13802NE LEFT ENGINE FAULTY A USAAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 EA19440US4971620635 24811 720976 DURING CRUISE, EN ROUTE FROM ROC TO CLT AT FL340, THE NR 1 ENGINE EXPERIENCED MULTIPLE COMPRESSOR STALLS WHICH LASTED APPROXIMATELY 30 SECONDS EACH. PER QUICK REFERENCE HANDBOOK, CREW REDUCED THRUST AND OPERATED AT THAT POWER THE REMAINDER OF FLIGHT. EGT REMAINED NORMAL. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE COMPLETED A BOROSCOPE INSPECTION OF THE NR 1 ENGINE. REMOVED AND REPLACED THE NR 1 ENGINE CIT SENSOR, VBV GEAR MOTOR AND THE 5TH STAGE BLEED AIR CHECK VALVE. PERFORMED TESTS OF VBV'S AND VSV'S WITH NO FAULTS NOTED. PERFORMED TRIM AND TAKEOFF POWER RUNS WITH NO PROBLEMS NOTED. 2L72 4F4 FRTA16WE E2GL 20051101000552005110100055NM 2005 11 1 SWAA053412 120051027A53306545775 SKIN BOEING737 7373A4 1384585NM BS 795 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29678AA 23290 DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 795, STR 18L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051101000562005110100056NM 2005 11 1 SWAA053413 120051028A33506104781 BATTERY PACK BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29710SW 27844 DURING SCHEDULED RON CHECK, FOUND CABIN EMERGENCY EXIT LIGHTS INOP AT RT OVERWING EXIT. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20051101000572005110100057NM 2005 11 1 SWAA053414 120051027A3040 CONTROLLER BOEING737 7377H4 1384404NM WINSHIELD HEAT FAILED A SWAAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW29775SW 30590 L2 COCKPIT WINDOW ARCED. REMOVED AND REPLACED L2 WINDOW AND HEAT CONTROLLER PER MM. 2L72 4F RTA16WE 20051101000582005110100058NM 2005 11 1 SWAA053415 120051028A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29796SW 27889 EEPLS TRACK LOOSE AT FWD END. REMOVED AND REPLACED EEPLS SECTION PER MM. 2L72 4F RTA16WE 20051101000592005110100059EA 2005 11 1 COMA0560576 120051027A2110 SENSOR CNDAIRCL600 CL6002B19 1900309EA COCKPIT CONTAMINATED A COMAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO01739CA 7273 CREW SMELLED STRONG BURNED RUBBER ODOR. CLEANED DUST CLOGS FROM COCKPIT TEMP SENSOR FAN. 2L72 4F RTA21EA 20051101000602005110100060NM 2005 11 1 05FDEA03512 120051026A5753651920612 FLAP TRACK BOEING727 7272S2F 1384O81NM NR 6 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25213FE 22935 NR 6 FLAP TRACK HAS CORROSION ON AFT MOUNT PAD. REPLACED FLAP TRACK WITH SERVICEABLE FLAP TRACK IAW MM 27-51-031-4. 2L73 4F A3WE 20051101000622005110100062NM 2005 11 1 05FDEA03508 120051026A2130 WARNING HORN BOEING727 727233 138408ANM CABIN PRESSURE ACTIVATED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25219FE 21102 PASSING THRU FL250 CABIN ALTITUDE WARNING HORN CAME ON AND CABIN WAS AT 10,000FT. BOTH PACKS ON, ENGINE BLEED NR 1 AND NR 3 OPEN. NO OTHER ABNORMAL INDICATIONS (OUTFLOW VALVE CLOSED AND ALL DOES CLOSED). EMERGENY DECLARED AND NO FUEL DUMP REQUIRED. 2L73 4F RTA3WE 20051101000642005110100064WP 2005 11 1 05FDEA03567 120051028A5310 STRUCTURE DOUG DC10 DC1030 3023501WP BS 1561-1581 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 IN THE CENTRAL CARGO COMPT BILGE UNDERFLOOR SPACE BETWEEN STA 1561 TO 1581 L 45 RT SIDE FOUND LIGHT CORROSION ON INTERNAL OF LONGERON AROUND FASTENERS. REMOVED FASTENERS IAW SRM 51-33-01 PAR 6-10 VOL 2. REMOVED CORROSION IAW SRM 51-21-01 PAR 34 VOL 2; AT THE END OF LONGERON ORIGINAL THK IS .060'' AFTER REMOVED, CORROSION MATERIAL AT 2.50 INCHES OF THE END FOUND THK .040'' MATERIAL REMOVED IS OUT OF LIMITS IAW SRM 53-00-01 FIG 1 B VOL 1. FAB PART IAW DETAIL PART TRAVELER F160211- 3 REPAIR CHANNEL IAW SRM 53-10-00 FIG2A. TREATED REWORKED AREA IAW SRM 51-21-01, PAR 31-24. INSTALLED REPAIR CHANNEL IAW SRM 53-10-00 FIG2A. 2L73 4F A22WE 20051101000652005110100065CE 2005 11 1 DXTA200501036 120051023A321367410133 LINK CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL MLG CRACKED E DXTAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL07934QS7243 7500034 DURING REMOVAL OF MLG ASSY, EXCESS MOISTURE CAME OUT OF RT OB AXLE WHEN REMOVING HUBCAP ASSY. TRAILING LINK ASSY HAS VISIBLE CRACK APPROX 10 INCHES IN LENGTH, ON TOP SIDE OF TRAILING LINK, CTRD BETWEEN MLG RETRACT ACTUATOR ATTACH LUGS. BORESCOPE INSP FOUND COROSSION ON INSIDE OF TRAILING LINK, CRACK 12 O'CLOCK POSITION INSIDE BARREL. REMOVED LWR TRAILING LINK. FOUND PIVOT PIN, ATTACH HARDWARE TO BE CORRODED AND WORN. FINISHED INSTALL ON LINK, BLED BRAKES LEAK CHECKED GOOD FIT CHECK GOOD. INSTALLED IB, OB WHEEL ASSY, SWUNG GEAR. OPS CHECK GOOD. DISASSEBLED TRAILING LINK, CUT OPEN TRAILING LINK BORE, PERFORMED BORESCOPE INSP, FOUND (CRATERS) ON INNER SURFACE OF APEX OF TRAILING LINK BELOW OLEO ATTACH POINT. 2L72 4J4 FRTT00007WITE6CH 20051101000662005110100066CE 2005 11 1 DXTA200501037 120051027A326065430087 POSITION SWITCH CESSNA560 560XL 2076702CE PWA 545 PW545A NE MLG INOPERATIVE E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07668QS 5605268 HYDRAULIC PRESS & UNLOCK LIGHT REMAIN ILLUMINATED ON GEAR RETRACTION. RECYCLED HYD CONTROL PER CK LIST. RECYCLED GEAR & PROBLEM REPEATED ITSELF (SUSPECT NOSE GEAR). - REMOVED AND REPLACED NOSE GEAR UPLOCK SWITCH WITH NEW IAW THE CESSNA 560XL M/M CHAPTER 32-30-05, OPERATIONAL CHECK NORMAL. 2L72 4F4 FRTA22CE E00059EN 20051101000672005110100067CE 2005 11 1 DXTA200501026 120051015A281099145051 FLOAT VALVE CESSNA750 750 2076810CE FUEL TANK LEAKING E DXTAH DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL07930QS4544 7500130 WING TANK OVERFILL "R" CAS MESSAGE ILLUMINATED INFLIGHT AND VENTED ABOUT 300LBS. OF FUEL IN ABOUT A MINUTE. THE RIGHT TANK CONTINUED TO VENT FUEL INTERMITTENTLY DURING DESCENT AND STILL VENTED FUEL WITH 2900LBS. - TROUBLESHOT SYSTEM, DEFUELED A/C AND FOUND (1) TWISTED O-RING IN CENTER WING FLOAT VALVE LINE. REPLACED ALL O-RINGS ON LINE WITH NEW P/N MS29513-214. REMOVED AND REPLACED CENTER WING FLOAT VALVE WITH NEW. OPS CHECKS AND LEAK CHECKS GOOD. WORK DONE PER CE750 M/M 28-10-04. 2L72 4J RTT00007WI 20051101000742005110100074NM 2005 11 1 05FDEA03552 120051027A5311 FAILSAFE BOEING727 727100 1384036NM BS 990 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 BS 990 FRAME IS CRACKED AT STRINGER 25 RIGHT. REPAIRED PER SRM 51-40-3 2L73 4F RTA3WE 20051101000752005110100075NM 2005 11 1 05FDEA03553 120051027A5311 FAILSAFE BOEING727 727100 1384036NM BS 1010 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 BS 1010 FRAME IS CRACKED AT STRINGER 25 LEFT. REPAIRED PER SRM 51-40-3 2L73 4F RTA3WE 20051101000762005110100076NM 2005 11 1 05FDEA03562 120051027A5330 SKIN BOEING727 727100 1384036NM BS 1352 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 BS 1352 RT SKIN CRACK AT RAIN GUTTER LOCATION. REPAIRED PER SRM 54-30-2 2L73 4F RTA3WE 20051101000772005110100077NM 2005 11 1 05FDEA03175 120050930A5220 HANDLE BOEING727 727200 138407ENM ESCAPE DOOR CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 RT FWD EMERGENCY ESCAPE DOOR, ACCESS HANDLE CLOSURE FRAME IS CORRODED. REPLACED RT FORWARD EMERGENCY ESCAPE DOOR ACCESS HANDLE CLOSURE FITTING PER SRM 51-30-2. 2L73 4F RTA3WE 20051101000782005110100078NM 2005 11 1 05FDEA03442 120051017A5310 SHEAR WEB BOEING727 727100 1384036NM BS 805-825 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 WHILE WORKING CARD N00368 FOUND SHEAR WEB 8-5-825, RBL 65-70, WL 208 TO BE CRACKED. SHEAR WEB BS 805-825 RBL 65-70 W/L 208 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REMOVED AND REPLACED IAW SRM 51-30-2. SRM 51-30-5, SRM 51-10-2. 2L73 4F RTA3WE 20051101000792005110100079NM 2005 11 1 05FDEA03453 120051019A323369141001 ACTUATOR BOEING727 727200 138407ENM MLG FAILED A FDEAO OTHER J WARNING INDICATION APAPPROACH 1 SO25205FE 22927 UPON GEAR EXTENSION, WHEN LANDING GEAR HANDLE WAS LOWERED, THE NOSE GEAR REMAINED UP. THE NOSE GEAR DOOR LT ON THE ENGINEERS PANEL NEVER ILLUMINATED, THE RED NOSE GEAR LT REMAINED ON ON THE FORWARD PANEL, THE GREEN NOSE GEAR LT REMAINED OUT, AND NO AURAL CLUES WERE HEARD THAT WOULD INDICATE GEAR EXTENSION. NORMAL HYDRAULIC QTY AND PRESSURE. AFTER APPROXIMATELY 3 MINUTES, WITH NO CREW ACTION, THE NOSE GEAR CAME DOWN NORMALLY, WITH GOOD INDICATIONS. 2L73 4F RTA3WE 20051102000012005110200001NE 2005 11 2 ARWA20051004 220051022A7230 COMPRESSOR DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE NR 2 ENGINE STALLED A ARWAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SO19661AV 45969 LOG PAGE NR 117333, DURING TAKEOFF, NR 2 ENGINE COMPRESSOR STALLED. PERFORM NR 2 ENGINE INLET AND EXHAUST SECTION INSPECTION FOR DAMAGE IAW M/M 71-00 AND PERFORMED OPERATIONAL RUN IAW M/M 71-00; FOUND ALL PARAMETERS IN LIMITS, COULD NOT DUPLICATE FAILURE. NOTE: BRAKE TEMP CHECK IAW AOM. 2L74 4F4 F 4A25 1E8 20051102000062005110200006NM 2005 11 2 05FDEA03352 120051011A5712ARB39547 RIB DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 LT WING FIXED LEADING EDGE INTERNAL RIB DOUBLER FOUND CRACKED AT XORS 686. CRACKED INTERNAL RIB DOUBLER AT LT WING FIXED LEADING EDGE XORS 686 REMOVED AS PER SRM 51-31-01 VOLUME II. NEW RIB DOUBLER FABRICATED AS PER DRAWING ARB3954 AND INSTALLED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051102000072005110200007NM 2005 11 2 05FDEA03341 120051010A5340 STRINGER CLIP BOEING727 727100 1384036NM BS 600 MISSING A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 STRINGER CLIP MISSING AT BS 600 STR 4R. INSTALLED STRINGER CLP AT BS 600 STR 4R PER SRM 51-30-2. 2L73 4F RTA3WE 20051102000092005110200009NM 2005 11 2 05FDEA03340 120051010A5340 STRINGER CLIP BOEING727 72722 1384002NM BS 700 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 STRINGER CLIP HAS MECHANICAL DAMAGE BS 700 STR 4L. REPLACED STRINGER CLIP AT BS 700, STR 4L PER SRM 51-30-2. 2L73 4F A3WE 20051102000102005110200010NM 2005 11 2 SB05125 120051007A335003600570010 FUSE BOEING737 7374B7 1384702NM EMERGENCY LIGHTSBLOWN A USAAK NONE O OTHER ININSP/MAINT 1 EA19780AU 24997 CLT - MAINTENANCE REPORTED THE EMERGENCY LIGHT AT SEAT ROW 2C OVERHEAD, AT STA 346, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FUSE IN POWER SUPPLY. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20051102000122005110200012NM 2005 11 2 2005UALA01083 120051004A335060253 LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE SEAT 25 CUT A UALAK NONE O OTHER ININSP/MAINT 1 WP29513UA 24810 ROW 23 THROUGH 24 EEL LIGHTS INOP. REPAIRED CUT IN STRIP. REPLACED STRIP AT SEAT 25. 2L72 4F4 FRTA2NM E17NE 20051102000142005110200014EU 2005 11 2 USAA051218 120051019A5310D5347112420100 SHEAR WEB AIRBUSA319 A319112 3930323EU FR 69-70 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19738US 1254 LT SIDE SHEAR WEB BETWEEN FR 69 & 70; CORROSION LEVEL 1; TASK JA-260-53500. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-42-00, DEFECT SIZE: .75 INCH DIA AREA. 2L72 4F RTA28NM 20051102000152005110200015NM 2005 11 2 USAA051212 120051019A575465C26602218 SKIN BOEING737 7373B7 1384580NM LE SLAT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 IN LOWER SKIN OF NR 5 SLAT AT RIVET, ADJACENT TO SLAT ACTUATOR CRACKED. INSTALLED A 30.25 X 3.75 INCH REPAIR DOUBLER ON LOWER SKIN AT CENTER OF SLAT, IAW 57-43-01, DEFECT SIZE: .250 INCH. 2L72 4F RTA16WE 20051102000162005110200016EU 2005 11 2 USAA051213 120051019A5315D5311282600200 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19738US 1254 Y505, FRAME C-12 TO C-16; CORROSION LEVEL 1; TASK JA-220-53500. REMOVED & REPLACED FLOORBEAM PER SRM 53-11-14, DEFECT SIZE: 1 X 4 INCH. 2L72 4F RTA28NM 20051102000172005110200017EU 2005 11 2 USAA051214 120051019A5315D5347209001100 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19738US 1254 Y1162 BEAM AT SPLICE FR 68 & 69; CORROSION LEVEL 2; TASK JA-260-53500. REMOVED & REPLACED PER SRM 51-72-11 & IPC 53-41-04, DEFECT SIZE: 3 X 3 X .030 INCH DEEP. 2L72 4F RTA28NM 20051102000252005110200025NM 2005 11 2 USAA051224 120051019A5320 PLATE BOEING757 7572B7 1384964NM BS 1680 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19619AU 27198 STA 1680, LBL 12, LBL 32; CORROSION LEVEL 1; TSK C53-252-03. BLEND OUT PLUS DOUBLER & CUTOUT PLUS DOUBLER PER SRM 51-10-02, 53-00-51, DEFECT SIZE: 1.2"L X 2"W X .043"D, 1.3"L X 1.4"W X .019". 2L72 4F RTA2NM 20051102000272005110200027EU 2005 11 2 USAA051216 120051019A5311 FRAME AIRBUSA319 A319112 3930323EU FR 66 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19738US 1254 AROUND CLIP NUT HOLE ON AFT SERVICE DOOR (RT) SILL BEAM AT FR 66 CORRODED. INSTALLED REPAIR ANGLES & FILLED PER SRM 53-41-14; CORROSION, LEVEL 2; TASK JA-260-53500, DEFECT SIZE: 0.500" X 0.500". 2L72 4F RTA28NM 20051102000312005110200031EU 2005 11 2 EMB05015 120051020A32349037B000103 CONTROL LEVER EMB ERJ170ERJ170100 EU MLG INOPERATIVE A USAAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 EA19813MA2628 000031 EN ROUTE DFW TO DCA - DURING CLIMB-OUT, THE LANDING GEAR WOULD NOT RETRACT. THE FLIGHT RETURNED TO FIELD IN DFW AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT SYSTEM, REMOVED AND REPLACED LANDING GEAR CONTROL LEVER. LANDING GEAR OPERATIONAL CHECKS DURING GEAR SWINGS ARE GOOD. 2L74 4F RTA56NM 20051103000022005110300002NM 2005 11 3 05FDEA03563 120051028A5313AFA71271 LONGERON DOUG MD11 MD11 3023602NM BS 1641-1661 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 FOUND CENTER CARGO COMP AFTER REMOVAL OF CRACKED LONGERON SPLICE AT STA 1641 TO 1661 LONGERON 44R FOR REPLACEMENT, LONGERON 44R FOUND CRACK AT STA 1646 TO 1651. REPAIRED AS PER SRM 53-10-00. 2L73 4F RTA22WE 20051103000042005110300004EA 2005 11 3 N6WA00510001 120051031A3350 LIGHT CNDAIRCL600 CL6002C10 1390015EA CABIN INOPERATIVE A N6WAK NONE L NO TEST ININSP/MAINT 1 CE03153GJ 10219 7891 - DEN - FOUND EMERGENCY LIGHT OVER ROW 4 OUT. RESECURED LIGHT IAW CRJ700 M/M 33-51-00. OPS CHECK GOOD. 2L72 4F RTA21EA 20051103000052005110300005NE 2005 11 3 AT0500039 220051028A7230 COMPRESSOR BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE LT ENGINE STALLED A ZZDAE ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 SO15985AT 55090 13162 INDICATIONS OF COMPRESSOR STALL FOLLOWED BY RED BOXED OIL PRESS LOW ON LEFT ENGINE. COMPLIED W/QRT AND SHUT DOWN LEFT ENGINE. REMOVED AND REPLACED LEFT ENGINE PER TASK CARD 603. 2L72 4F4 FTRA6WE E00061EN 20051103000062005110300006NE 2005 11 3 AT0500040 220051028A7200 ENGINE BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE RIGHT INOPERATIVE A ZZDAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SO15933AT 55071 13258 RT ENG COMP STALL ON CLIMB-OUT, ENG SHUT DOWN, HIGH TGT. REMOVED AND REPLACED RT ENG ASSY. LEAK AND OPS CK NORMAL. OK FOR SVC. 2L72 4F4 FTRA6WE E00061EN 20051103000082005110300008EU 2005 11 3 WRNA200500025 120051031A2597 WIRE HARNESS AIRBUS300 A300B4203 3930306EU CABIN SPARKS A WRNAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO05821SC 211 FLIGHT ENGINEER SEAT HAD SPARKS COMING OUT OF ELECT CONNECTOR ON RIGHT SIDE OF SEAT, THEN C/B POPPED. FOUND WIRES FUSED TOGETHER AT SEAT CANNON PLUG. SEAT DEACTIVATED AND PLACED ON MEL 25-11-01. 2L72 4F RTA35EU 20051103000092005110300009NE 2005 11 3 BB05096 220051029A7532C8E3812 CONTROLLER BOEING757 757225 1384959NM RROYCERB211 RB211* 54555NE LT BLEED VALVE FAILED A USAAO OTHER E VIBRATION/BUFFET DEDESCENT 1 EA19614AU 27145 031377 ON DESCENT, VIBRATIONS WERE FELT FROM THE LEFT ENGINE. MAINTENANCE REPLACED THE NR 1 BLEED VALVE CONTROLLER. 2L72 4F4 FRTA2NM A12EU 20051103000102005110300010NM 2005 11 3 USAA200511001 120051031A5330 SKIN BOEING737 7373B7 1384580NM BS 867 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19396US 23318 1.5 INCH CRACK FOUND STA 867 AT STRINGER S23R. REPAIR: INSTALLED REPAIR DOUBLER IAW SRM 53-00-01 FIG. 201. 2L72 4F RTA16WE 20051103000122005110300012NM 2005 11 3 USAA051325 120051102A5310 DOOR FRAME BOEING737 7374B7 1384702NM GE CFM56 CFM56* 13802NE AFT DOOR CUTOUT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19779AU 24996 LOCATION: AFT DOOR CUTOUT AFT FRAME AT S25R. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-70-13. DEFECT SIZE: 1 INCH 2L72 4F4 FRTA16WE E2GL 20051103000142005110300014NM 2005 11 3 USAA051323 120051102A5315 FLOORBEAM BOEING737 7374B7 1384702NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19779AU 24996 FLOORBEAM AT RT SERVICE DOOR ENTRY WAY. INSTALLED NEW REPAIR PART IAW SRM 51-40-02 DEFECT SIZE: 2 INCHES X 5 INCHES. 2L72 4F4 FRTA16WE E2GL 20051103000172005110300017NM 2005 11 3 SB05138 120051028A21337110033 OUTFLOW VALVE BOEING737 7373B7 1384580NM AFT FUSELAGE FAULTY A USAAGA O2 MASK DEPLOYED UNSCHED LANDING O OTHER CRCRUISE 1 EA19517AU5084750847 23703 BWI - FLT1243 - DURING CRUISE, CREW REPORTED A LOUD BUZZING NOISE COMING FROM CABIN AND ALMOST INSTANTLY FELT PRESSURE IN THEIR EARS. CREW FOUND CABIN PRESSURE CLIMBING 3,000 TO 4,000 FT PER MINUTE. OUTFLOW VALVE WAS CLOSED PER PROCEDURES WITH NO AFFECT ON PRESSURE LOSS. CABIN PRESSURE REACHED CLOSE TO 14,000 FT, BUT CREW WAS ABLE TO DESCEND FLT BEFORE MASKS DEPLOYED IN CABIN. CREW DONNED THEIR OXYGEN MASKS AND DIVERTED FLT TO BWI FOR MX. FLT LANDED W/O FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MX FOUND AFT OUTFLOW VALVE NOT OPERATING CORRECTLY. REMOVED AND REPLACED AFT OUTFLOW VLV PER MM 21-31-11. OPS CHECK GOOD. ALSO, REPAIRED LEAK FROM AFT CARGO DOOR SILL AREA. PERFORMED SATISFACTORY PRESS CONFIDENCE 2L72 4F RTA16WE 20051103000182005110300018NM 2005 11 3 USAA051321 120051102A5313 STRINGER BOEING737 7373B7 1384580NM GE CFM56 CFM56* 13802NE BS 1138 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 S-5AR B.S. 1138 ACTION: INTERIM REPAIR WAS PREVIOUSLY INSTALLED IAW EA 73450B IAW EA 73450B. LENGTH UNKNOWN. 2L72 4F4 FRTA16WE E2GL 20051103000192005110300019NM 2005 11 3 USAA051319 120051102A5210507945264 BRACKET BOEING737 7373B7 1384580NM GE CFM56 CFM56* 13802NE PAX DOOR SEAL CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 LOWER FWD CORNER OF MAIN ENTRY DOOR. FABRICATED AND INSTALLED NEW BRACKET IAW SRM 51-10-02. DEFECT SIZE: .50 INCH. 2L72 4F4 FRTA16WE E2GL 20051103000202005110300020NM 2005 11 3 USAA051318 120051102A5340 STRINGER CLIP BOEING737 7374B7 1384702NM GE CFM56 CFM56* 13802NE BS360 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19779AU 24996 LOCATION: BS360 AND S4R. DEFECTIVE PART REPLACED WITH IDENTICAL PART, IAW SRM 51-10-02 DEFECT SIZE: .50 IN. 2L72 4F4 FRTA16WE E2GL 20051103000212005110300021NM 2005 11 3 USAA051317 120051102A554265C2584151 SKIN BOEING737 7374B7 1384702NM GE CFM56 CFM56* 13802NE RUDDER DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19779AU 24996 RUDDER SKIN LT SISE STATION 233.9. DOUBLER INSTALLED ON LT UPPER SIDE OF RUDDER IAW SRM 51-60-05, DEFECT SIZE: 7 INCHES X 1INCH. 2L72 4F4 FRTA16WE E2GL 20051103000222005110300022NM 2005 11 3 USAA051263 120051031A5347 SEAT TRACK BOEING737 7373B7 1384580NM BS 500A CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND SEAT TRACK CORRODED, LBL 45 BS 500A + 12. BLENDED AREA, WITHIN LIMITS IAW SRM 53-00-52, DEFECT SIZE: 1" BY 2". 2L72 4F RTA16WE 20051103000232005110300023EU 2005 11 3 USAA051309 120051101A5315D5347217220400 FLOORBEAM AIRBUSA319 A319112 3930323EU FR 66-68 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19741UW 1269 FOUND CORROSION ON FLOORBEAM Y1292 BETWEEN FS 66 AND 68; CORROSION LEVEL 1; TASK JA-260-53500. REMOVED AND REPLACED PER SRM 51-72-11, DEFECT SIZE: 2' X 3". 2L72 4F RTA28NM 20051103000242005110300024EU 2005 11 3 USAA051308 120051101A5315D5311282600101 FLOORBEAM AIRBUSA319 A319112 3930323EU FR 14-16 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19741UW 1269 FOUND BEAM CORRODED BETWEEN FRAME 14 AND 16; CORROSION LEVEL 1; TASK JA-220-53500. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-72-11, DEFECT SIZE: 2" BY 40". 2L72 4F RTA28NM 20051103000252005110300025EU 2005 11 3 USAA051307 120051101A5315D5311281820401 FLOORBEAM AIRBUSA319 A319112 3930323EU FR 24 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19741UW 1269 FOUND FRAME CORRODED 16 Y254 TO FRAME 24; CORROSION LEVEL 1; TASK JA-220-53500. REMOVED AND REPLACED BEAM PER SRM 51-72-11, DEFECT SIZE: 2" BY 2". 2L72 4F RTA28NM 20051103000262005110300026EU 2005 11 3 USAA051306 120051101A5315D5347218820400 FLOORBEAM AIRBUSA319 A319112 3930323EU FR 68 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19741UW 1269 FOUND FLOORBEAM CORRODED Y1292 AT FRAME 68, CORROSION LEVEL 1; TASK #JA-260-53500. REMOVED AND REPLACED PER SRM 51-72-11, DEFECT SIZE: 2" BY 2". 2L72 4F RTA28NM 20051103000272005110300027EU 2005 11 3 USAA051305 120051101A5315D5311281520200 FLOORBEAM AIRBUSA319 A319112 3930323EU FR16 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19741UW 1269 FOUND TOP OF BEAM CORRODED, FRAME 16 AND Y765; CORROSION LEVEL 1; TASK JA-220-53500. REMOVED AND REPLACED PER SRM 51-72-11, DEFECT SIZE: 2" BY 2". 2L72 4F RTA28NM 20051103000282005110300028NM 2005 11 3 USAA051304 120051101A5320141N8422 SILL BOEING757 7572B7 1384964NM R1 DOOR CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19626AU 27303 FOUND DOOR SILL SUPPORT CORRODED AT R1 DOOR. REMOVED AND REPLACED CORRODED SUPPORT (BY FAB) PER SRM 53-00-51, 51-40-02, DEFECT SIZE: 2.5 BY 1.0 BY .020". 2L72 4F RTA2NM 20051103000302005110300030NM 2005 11 3 USAA051302 120051101A5315US22477LF FLOORBEAM BOEING757 7572B7 1384964NM BS 324 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19626AU 27303 FOUND FLOORBEAM CORRODED STA 324 RBL 58 UPPER CAP. FAB FLOORBEAM UPPER CAP AND SPLICE ANGLES PER SRM 53-00-51, 51-40-02, 51-20-01, 51-70-12, EA 96967, DEFECT SIZE: 4"L BY 3"W BY 0.025"D. 2L72 4F RTA2NM 20051103000312005110300031NM 2005 11 3 USAA051287 120051101A5315 FLOORBEAM BOEING737 7373B7 1384580NM BS 986 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND FLOORBEAM SHIM FAULTY AT STA 986. CLEANED AREA, REMOVED CORRODED SHIMS AND RETREATED AREA IAW SRM 53-60-51, DEFECT SIZE: APPROX .250" DAMAGE. 2L72 4F RTA16WE 20051103000322005110300032NM 2005 11 3 USAA051300 120051101A5320US141N517C30LF FLOOR SUPPORT BOEING757 7572B7 1384964NM STA 324-342 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19626AU 27303 FOUND STA 324 AND 342 FLOOR SUPPORT CORRODED. FAB'D NEW FLOOR SUPPORT PER MAE TRAVELER T5/551168, SRM 51-010-00 AND SRM 53-00-51, DEFECT SIZE: 3"W BY 2"W BY .025"D. 2L72 4F RTA2NM 20051103000332005110300033NM 2005 11 3 USAA051299 120051101A5320141N516139 FLOOR SUPPORT BOEING757 7572B7 1384964NM BS 324-345 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19626AU 27303 FOUND FLOOR SUPPORT CORRODED (FITTING) STA 324-345 RBL 3. REMOVED AND REPLACED WITH NEW SUPPORT PER SRM 53-10-13 AND 51-40-02, DEFECT SIZE: 3"L BY 2"W BY .040"D. 2L72 4F RTA2NM 20051103000342005110300034NM 2005 11 3 USAA051298 120051101A5340415N400217 MOUNT BOEING757 7572B7 1384964NM STA 327 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19626AU 27303 FOUND GALLEY MOUNT CORRODED STA 327 RBL 45. REMOVED AND REPLACED WITH NEW MOUNT PER SRM 53-00-51, DEFECT SIZE: 1"W BY 2"L BY .025"D. 2L72 4F RTA2NM 20051103000352005110300035NM 2005 11 3 USAA051297 120051101A5320 SUPPORT BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND CRACK VERTICAL STANCHION SUPPORT AT FWD E1 RT SHELF. FABRICATED AND INSTALLED DOUBLER IAW SRM 51-70-11, DEFECT SIZE: 1" CRACK. 2L72 4F RTA16WE 20051103000362005110300036NM 2005 11 3 USAA051296 120051101A5310 CREASE BEAM BOEING737 7373B7 1384580NM BS 500B CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 AROUND RIVET HEADS AT CREASE BEAM BS 500B+8 S17L. REMOVED CORROSION AND TREATED AREA IAW SRM 51-20-01, DEFECT SIZE: APPROXIMATE 1/16" DIA SPOTS OF CORROSION. 2L72 4F RTA16WE 20051103000372005110300037NM 2005 11 3 USAA051295 120051101A575465C26602214A SKIN BOEING737 7373B7 1384580NM SLAT DEBONDED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND SLAT DISBOND, T/E WEDGE O/B END. REMOVED DAMAGE, FAB AND INSTALLED REPAIR PARTS IAW TR 57-42-04, DEFECT SIZE: 3" X 5" DISBOND. 2L72 4F RTA16WE 20051103000382005110300038NM 2005 11 3 USAA051294 120051101A575465C26602257A SKIN BOEING737 7373B7 1384580NM NR 2 SLAT DEBONDED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND DISBOND O/B END OF T/E WEDGE. REMOVED DAMAGE, FAB AND INSTALLED REPAIR PARTS IAW TR 51-30-03, DEFECT SIZE: 2" BY 5" DISBOND. 2L72 4F RTA16WE 20051103000392005110300039NM 2005 11 3 USAA051293 120051101A5340 ANGLE BOEING737 7373B7 1384580NM BS 986 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND Z-ANGLE CORRODED, FLOOR STRUCTURE AT L2 DOOR, STA 986 AND LBL 53. REMOVED CORRODED PART AND INSTALLED NEW PART IAW SRM 51-10-02, DEFECT SIZE: 1" BY 3" AREA OF CORROSION. 2L72 4F RTA16WE 20051103000402005110300040NM 2005 11 3 USAA051292 120051101A5320 ANGLE BOEING737 7373B7 1384580NM BS 955-990 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND CORROSION STA 955 TO 990, LBL 53. REMOVED DAMAGED PARTS AND INSTALLED NEW PARTS IAW SRM 51-10-02, DEFECT SIZE: NUMEROUS AREAS OF CORROSION THROUGHOUT THE PART/TYPICAL 1/2" DIA OF CORROSION. 2L72 4F RTA16WE 20051103000412005110300041NM 2005 11 3 USAA051291 120051101A5315 FLOORBEAM BOEING737 7373B7 1384580NM BS 986.5 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND FLOORBEAM CORRODED STA 986.5 AT LT DOOR SILL AREA. REPLACED ENTIRE T-CAP IAW TR 53-10-05B, DEFECT SIZE: .500" AREA OF CORROSION AROUND SEVERAL SCREW HOLES. 2L72 4F RTA16WE 20051103000422005110300042NM 2005 11 3 USAA051290 120051101A5315 FLOORBEAM BOEING737 7374B7 1384702NM BS 328 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19779AU 24996 FOUND FLOORBEAM CORRODED AT 328, CORROSION AROUND CLIP NUT HOLES RBL 10 TO Z-ANGLE AT FWD SER. CLEANED CORROSION ALODINED AND PRIMED EXCEPT RBL 21 (OUT OF SRM LIMITS) IAW SRM 51-10-51, TR53-15-01B, DEFECT SIZE: .500 DIA CORRODED AREAS. 2L72 4F RTA16WE 20051103000432005110300043NM 2005 11 3 USAA051289 120051101A5320 ANGLE BOEING737 7373B7 1384580NM BS 955-990 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND Z-ANGLE CORRODED, STA 955 TO 990 . REMOVED CORRODED PART AND INSTALLED NEW PART AND REPAIR PARTS IAW SRM 53-60-15, DEFECT SIZE: CORROSION ON "Z" ANGLE 1 INCH BY 1 INCH. 2L72 4F RTA16WE 20051103000452005110300045NM 2005 11 3 USAA051303 120051101A5320141N5160 SILL BOEING757 7572B7 1384964NM R1 DOOR CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19626AU 27303 FOUND CORROSION DOOR SILL SUPPORT AT R1. REPLACED CORRODED SILL SUPPORT (BY FAB) PER SRM 53-00-51, 51-40-02, 51-20-01, DEFECT SIZE: 36 BY 4 BY .015. 2L72 4F RTA2NM 20051103000462005110300046 2005 11 3 USAA051262 420051031A2565 FITTING BOEING737 7373B7 1384580NM GIRT BAR CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND FITTING CORRODED GIRT BAR ATTACH FITTING AT BS344 RBL 58. REMOVED AND REPLACED ANGLE IAW BOEING DWG 65C16121, DEFECT SIZE: 1". 2L72 4F RTA16WE 20051103000502005110300050NM 2005 11 3 USAA051285 120051101A5315 FLOORBEAM BOEING737 7373B7 1384580NM BS 986.5 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND FLOORBEAM CORRODED STA 986.5. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW SRM 53-60-51, DEFECT SIZE: 1/4" AREA'S OF CORROSION. 2L72 4F RTA16WE 20051103000522005110300052EU 2005 11 3 USAA051315 120051101A5320D534720900030000BEAM AIRBUSA319 A319112 3930323EU FR 66 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19741UW 1269 FOUND BEAM CORRODED FRAME 66, BEAM -Y765; CORRODED LEVEL 1; TASK JA-260-53500. REMOVED AND REPLACED PER SRM 51-72-11, DEFECT SIZE: 2" BY 2". 2L72 4F RTA28NM 20051103000542005110300054EU 2005 11 3 USAA051313 120051101A5315D53472189204 FLOORBEAM AIRBUSA319 A319112 3930323EU FR 68 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19741UW 1269 FOUND FLOORBEAM CORRODED -Y1292 AT FS 68; CORRODED LEVEL 1; TASK JA-260-53500. REMOVED AND REPLACED BEAM PER SRM 51-72-11, DEFECT SIZE: .080"D BY 2" BY 2". 2L72 4F RTA28NM 20051103000552005110300055EU 2005 11 3 USAA051312 120051101A5315D53472172205 FLOORBEAM AIRBUSA319 A319112 3930323EU -Y1292 BETWEEN FCORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19741UW 1269 FOUND FLOORBEAM CORRODED -Y1292 BETWEEN FS 66 AND 68; CORRODED LEVEL 1; TASK JA-260-53500. REMOVED AND REPLACED BEAM PER SRM 51-72-11, DEFECT SIZE: .040"D BY 1" BY 4". 2L72 4F RTA28NM 20051103000572005110300057EU 2005 11 3 USAA051310 120051101A5315D5347209001000 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19741UW 1269 FOUND FLOORBEAM CORRODED Y1292 PT FRAME 66; CORROSION LEVEL 1; TASK JA-260-53500. REMOVED AND REPLACED PER SRM 51-72-1, DEFECT SIZE: 2" BY 2". 2L72 4F RTA28NM 20051103000592005110300059NM 2005 11 3 USAA051259 120051028A5320 INTERCOSTAL BOEING737 7373B7 1384580NM BS 328-344 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND INTERCOSTAL CORRODED, BS 328-344 RBL 12. REMOVED CORROSION AND TREATED IAW SRM 53-10-51-1A-1, DEFECT SIZE: .25". 2L72 4F RTA16WE 20051103000612005110300061NM 2005 11 3 USAA051258 120051028A5320 STRAP BOEING737 7373B7 1384580NM BS 344 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND STABILIZER AT BS 344 AND RBL 47. INSTALLED DOUBLER IAW SRM 53-10-51, DEFECT SIZE: .50". 2L72 4F RTA16WE 20051103000632005110300063NM 2005 11 3 USAA051284 120051031A5343 SUPPORT BOEING737 7373B7 1384580NM LT MLG CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND LT MLG SUPPORT FITTING BOTTOM SURFACE CORRODED. BLENDED AREAS AS REQUIRED IAW TR 57-53-53A, DEFECT SIZE: .25". 2L72 4F RTA16WE 20051103000652005110300065NM 2005 11 3 USAA051282 120051031A5340 MOUNT BOEING737 7373B7 1384580NM RT AFT LAV/ FWD CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND LAV MOUNTS CORRODED, RT AFT LAV/FWD MOUNTS. REMOVED CORRODED PARTS AND INSTALLED REPAIR PARTS IAW SRM 53-60-51, DEFECT SIZE: 2". 2L72 4F RTA16WE 20051103000672005110300067NM 2005 11 3 USAA051280 120051031A5315 FLOORBEAM BOEING737 7374B7 138449CNM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19779AU 24996 FOUND FLOORBEAM CORRODED, STA 986.7. REMOVED MINOR SURFACE CORROSION, ALODINED, PRIMED AND PAINTED IAW SRM 53-60-51, DEFECT SIZE: 1" BY 3". 2L72 4F RTA16WE 20051103000692005110300069NM 2005 11 3 USAA051278 120051031A5320 SPLICE BOEING737 7373B7 1384580NM STA 360 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND SPLICE CHANNEL CRACKED, STA 360 S14L. REPLACED SPLICE PART IAW SRM 51-10-02, DEFECT SIZE: .500". 2L72 4F RTA16WE 20051103000702005110300070NM 2005 11 3 USAA051277 120051031A5320 WEB BOEING737 7373B7 1384580NM BS 294.5 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND WEB CRACKED, STA 294.5, S12L. REMOVED DAMAGED PART, REPLACED W/FABRICATED REPLACEMENT WEB/INTERCOSTAL, DEFECT SIZE: .500". 2L72 4F RTA16WE 20051104000032005110400003NM 2005 11 4 USAA051276 120051031A5311 FRAME BOEING737 7373B7 1384580NM BS 480 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND FRAME CRACKED BETWEEN STRINGERS S-8R AND S-9R STA 480. CUT OUT DAMAGE, INSTALL FRAME DOUBLERS P/N 1133533 AND 1133534 PER TR 53-10-20, DEFECT SIZE: .5". 2L72 4F RTA16WE 20051104000042005110400004NM 2005 11 4 USAA051275 120051031A5340 CLIP BOEING737 7373B7 1384580NM STA 685 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND CLIP CRACKED, STA 685 S4L. REPLACED CLIP IAW SRM 51-10-02, 51-40-03, DEFECT SIZE: 2.00". 2L72 4F RTA16WE 20051104000062005110400006NM 2005 11 4 USAA051272 120051031A5320 ANGLE BOEING737 7374B7 1384702NM Z ANGLE AT L/H ECORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19779AU 24996 FOUND Z ANGLE CORRODED AT LT ENTRY DOOR. REMOVED OLD Z ANGLE AND REPLACED WITH NEW PART IAW SRM 51-20-05, DEFECT SIZE: .75" BY 8". 2L72 4F RTA16WE 20051104000082005110400008NM 2005 11 4 USAA051269 120051031A5315 SHIM BOEING737 7373B7 1384580NM FLOORBEAM AT ST CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND FLOORBEAM SHIM CORRODED AT STA 986. CLEANED AREA, REMOVED CORRODED SHIMS AND RETREATED AREA IAW SRM 53-60-51, DEFECT SIZE: .250". 2L72 4F RTA16WE 20051104000092005110400009NM 2005 11 4 USAA051268 120051031A5313 STRINGER BOEING737 7373B7 1384580NM S26R, STA 1016 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND STRINGER CORRODED, S26R, STA 1016. REPLACED STRINGER SECTION AND BLKHD FITTING IAW SRM 51-10-02, DEFECT SIZE: .75" BY 3". 2L72 4F RTA16WE 20051104000102005110400010NM 2005 11 4 USAA051267 120051031A534369827626 LUG BOEING737 7373B7 1384580NM OB FWD FACE OF LGOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND LUG GOUGE OB FWD FACE OF LT MLG BEAM. BLEND OUT DAMAGE IAW TYP REP 57-40-05 BOEING DWG 65-82763, DEFECT SIZE: .750 BY .008. 2L72 4F RTA16WE 20051031000192005103100019WP 2005 10 31 QOF2005F00003 120051020A6210RHCC1581 BLADES ROBSINR44 R44RAVENII 7640122WP LYC O540 IO540* 41532EA MAIN ROTOR OUT OF BALANCE E QOFAO OTHER O OTHER NRNOT REPORTED 1 AL01944AK 10634 BLADES CAME OUT OF BALANCE SITTING STATIC OVER A PERIOD OF 4 DAYS, FOR REASON OR REASONS UNKNOWN. (K) 1G71 3O3 O H11NM 1E4 20051031000232005103100023NM 2005 10 31 UIEA200500123 120050830A541465B940521 SKIN BOEING747 7472D7B 1384803NM GE CF6 CF650E2 30018NE NR 2 PYLON CHAFED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15524MC 21784 D-CHECK, DURING MAINTENANCE INSPECTION, THE NR 2 STRUT RT SIDE SKIN ASSEMBLY INTERNAL BONDED DOUBLER WAS FOUND CHAFED AT THE 463AR ACCESS PANEL CUTOUT. THE INTERNAL DOUBLER AND SKIN WERE TRIMMED BACK PAST THE EXISTING CUTOUT IN THE OUTER SKIN. THE REPAIR AREA WAS HFEC INSPECTED FOR CRACKS OR OTHER DAMAGE. REPAIR DOUBLERS WERE FABRICATED TO COVER THE ENTIRE ACCESS CUTOUT AND TO REPLICATE THE ACCESS DOOR LAND ATTACHMENT DETAILS. THE REPAIR DOUBLERS WERE INSTALLED BY BONDING TOGETHER WITH HI-LOCK FASTENERS. EO TO ACCOMPLISH REPEAT DETAIL VISUAL INSPECTION OF THE REPAIR AREA EVERY C-CHECK OR 18 MONTHS, WHICHEVER OCCURS EARLIER FOR CRACKS AND LOOSE OR MISSING FASTENERS. (K) 2L74 4F4 FRTA20WE E23EA 20051031000252005103100025CE 2005 10 31 S2YA05046 120050722A32601293640455 PCB BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA MLG SHORTED A S2YAO OTHER JB WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 GL13891SK2851 UE89 DURING APPROACH OF FLIGHT, THE CREW DID NOT RECEIVE THE DOWN AND LOCK INDICATION FOR THE NOSE LANDING GEAR. THE CREW ALSO NOTED A SMOKE ODOR IN THE COCKPIT. THE CREW MADE A SAFE LANDING. MAINTENANCE INSPECTED THE SYSTEM AND FOUND BOTH THE ANNUNCIATOR FAULT DETECT PCB AND THE ANNUNCIATOR CONTROL PCB HAD SHORTS. MAINTENANCE REPLACED BOTH PCB AND OPS CHECKED THE SYSTEM WITH NO FURTHER DEFECTS NOTED. (K) 2L72 4T3 TRTA24CE E2NE 20051031000302005103100030NM 2005 10 31 USAA051006 120050815A5512 SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU HORIZONTAL STAB CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US50585 23933 CLT - Q6 - SKIN, 1.50 INCH CRACK. 1.25 INCH FWD OF REAR SPAR, SPAR STA 124 TO 55-123.6. HORIZONTAL STABILIZER. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER IAW EA. (K) 2L72 4F4 FRTA16WE E21EU 20051031000322005103100032EU 2005 10 31 A6WA200540310 120050927A5730 ACCESS DOOR AIRBUS320 A320231 3930325EU GE CF34 CF343B1 NE RT WING CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31625AW 064 RT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT PANEL 650 GB WING STA 274.319 HAS MINOR CORROSION .006 INCH DEEP AND 2 INCH LONG. MAINTENANCE REMOVED MINOR CORROSION IAW REO. MATERIAL REMOVED WAS LESS THAN .010 INCH IAW REINSPECT IS DUE OF HOLE NR 14 AT 38602 FLIGHT CYCLES. 2L72 4F4 FRTA28NM E15NE 20051031000352005103100035CE 2005 10 31 GUU2005F00043 120050817A55201016200131 BRACKET BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA RT ELEVATOR CORRODED A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO298755218547 UE216 AT SCHEDULED ROUTINE MAINTENANCE, RT ELEVATOR CENTER HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RT ELEVATOR CENTER HINGE BRACKET. (K) 2L72 4T3 TRTA24CE E2NE 20051031000622005103100062 2005 10 31 KBM2005F00294 420050921A340024138900 ANTENNA SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE TRANSPONDER DEFECTIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19966SH2159 3787 TRANSPONDER INOPERATIVE, ANTENNA DEFECTIVE, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051031000722005103100072EU 2005 10 31 KBM2005F00296 120050925A3150KW9 WARNING HORN SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE COCKPIT INTERMITTENT E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19966SH2177 3787 WARNING HORN, INTERMITTENT ON GROUND. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051031000822005103100082 2005 10 31 KBM2005F00304 420050928A2312064105430 RADIO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE VHF SYSTEM FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19351WM 2167 VHF RADIO, UNIT FREQ IS TOO DIM TO READ, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051031001222005103100122SO 2005 10 31 GUU2005F00052 120050924A3397 WIRE EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE EMERGENCY LIGHT BROKEN A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO17268AS 120202 FLOOR EMERGENCY LIGHTING BETWEEN ROW 3A AND ROW 5A INOPERATIVE. REPAIRED BROKEN WIRE AT EMERGENCY LIGHTING STRIP. (K) 2L72 4T4 TRTA31SO E20NE 20051031001282005103100128WP 2005 10 31 I5HA0558007 120050927A324634479 BEARING CVAC 580 580 2422806WP ALLSN 501D 501D13 03004GL NR 4 MLG WHEEL SEIZED A I5HAC ABORTED TAKEOFF D INFLIGHT SEPARATION TOTAKEOFF 1 GL23587XP 361 DURING TAKEOFF, ENROUTE, CREW NOTIFIED THAT LANDING GEAR WHEEL AND TIRE WAS SEEN DEPARTING AIRCRAFT. CREW ELECTED TO CONTINUE FOR MAINTENANCE. MAINT CREW DISCOVERED NR 4 WHEEL BROKEN WITH PART OF THE WHEEL MISSING. TIRE WAS MISSING. FOUND THE FAILURE OF THE OUTER WHEEL BEARING EVIDENCED BY BURN MARKS AND SEIZED ROLLERS. NR 4 TIRE AND WHEEL ASSY WERE REMOVED AND AXLE WAS INSPECTED BOTH VISUALLY AND WITH DYE PENETRANT. THERE WAS NO DAMAGE TO AXLE. SERVICEABLE TIRE AND WHEEL ASSY WAS INSTALLED AND AC RETURNED TO SERVICE. (K) 2L72 4T4 TRT E282 20051031001472005103100147EU 2005 10 31 USAA051021 120050817A5310D5347217220390 BEAM AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FR 67-68 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19742US15033 1275 PIT - S1 - BEAM, 1 INCH X 1 INCH, CORROSION; LEVEL 1; TASK JA-260-53500 BETWEEN FR 67 AND FR 68 AT Y115MM. REPLACED BEAM IAW TYPE REP. (K) 2L72 4F4 FRTA28NM E37NE 20051031001532005103100153EU 2005 10 31 USAA051019 120050817A5321D5361067500000 FLOOR PANEL AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FR 16-20 DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19742US15033 1275 PIT - S1 - FLOOR PANEL, 3 INCH X 3 INCH AREA, DELAMINATION. FLOORBOARD TORN AND DELAMINATED, FR 16 TO 20, Z222 (222EF). DEFECTIVE PART REPLACED WITH IDENTICAL PART. (K) 2L72 4F4 FRTA28NM E37NE 20051031001562005103100156GL 2005 10 31 DAT2005F00011 320050823A6110 FLANGE STBROSSD3 SD330 8100602EU PWA PT6 PT6A45R 52043EA HARTZLHCB5M HCB5MP3 GL PROPELLER FAILED E DATAO OTHER O OTHER NRNOT REPORTED 1 GL13936MA4464 1069 SH3036 PCE84005 EVA2186 DURING THE COMPLIANCE OF AD, SB, FRO THE RT SIDE PROPELLER, THE (8) PROP ATTACH BOLTS, FAILED THE DESCRIBED TORQUE CHECK AS DESCRIBED IN AD (SB). THE PROPELLER WAS REMOVED IAW MM. AFTER THE PROP WAS REMOVED, THE INSPECTION FOUND FRETTING ON THE PROP FLANGE, HOWEVER, THERE WAS NO DAMAGE TO THE ENGINE FLANGE. A SERVICEABLE PROP WAS INSTALLED IAW MM. AD AND SB HAS BEEN COMPLIED WITH ONTHE INSTALLED PROPELLER AND IS NEXT DUE AT 25868.2 TAT WITH NO DEFECTS FOUND. OPS CHECKED GOOD. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE. (K) 2H72 4T4 T A41EU E4EA 6 CP44GL 20051031001662005103100166NE 2005 10 31 KBM2005F00299 220051001A7250 BLADE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE TURBINE DAMAGED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19345SH5131 3345 POWER FREE TURBINE ON ENGINE, FOUND TO BE DAMAGED ON INSPECTION. FOUND 1 EACH BLADE WITH CHUNK MISSING ON TOP .3333 OF TRAILING EDGE. NO OTHER FOD WAS FOUND IN COMPRESSOR OR GAS PRODUCER SECTIONS. REMOVED ENGINE ASSY AND REPLACED WITH SERVICEABLE ASSY. (K) 1G71 3U3 U H9EU E19EU 20051031001712005103100171NM 2005 10 31 USAA051026 120050817A5322US65458053LF SHEAR TIE BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU BS 277 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19444US40668 24862 BFM - Q2 - SHEAR TIE CLIP, .250 INCH CRACK, STA 277, SHEAR TIE CLIP, STR 9L TO 10L. INSTALLED SHEAR CLIP ON STR STA 277 IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051031001762005103100176EU 2005 10 31 ASOA05741B 120050907A2752FE231003 ACTUATOR AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE RT WING TE FLAPSMALFUNCTIONED A ASOAO OTHER O OTHER NRNOT REPORTED 1 SO27635AS2711427114 372 RT OB ACTUATOR, MALFUNCTIONED, RT WING. (K) 2H72 4T4 TRTA53EU E20NE 20051031001912005103100191CE 2005 10 31 V2J2005F00001 120050910A27503903814010013 FLAP SYSTEM RAYTHN390 390 7150030CE TE FLAPS INOPERATIVE E V2JAO OTHER O OTHER NRNOT REPORTED 1 EA25311SL298 RB120 THE FLAP/ SPOILER SYSTEM ON THIS AIRCRAFT IS PLAGUED WITH FAILURES. THERE ARE MORE OF THESE REPORTS TO FOLLOW. (EA25200510359) (K) 17 2 3F RTA00010WI 20051031002002005103100200NM 2005 10 31 UIEA200500167 120051019A5330HZ7075001606T SKIN BOEING747 74747UF 1384812NM GE CF6 CF680C2* GL BS 2577 DAMAGED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15493MC 29254 DURING TRANSIT CHECK, FOUND AIRCRAFT DAMAGE AT AFT FUSELAGE NEAR STA 2577.75. REPAIR SCHEME FROM SRM 53-00-01 REPAIR 1 AND 2 , H/F EDDY CURRENT INSPECTION, SIGNED ON WORK PERFORMANCE STATEMENT. REPAIR TO CAT B STANDARD, TO BE INSPECTED EVERY 1500 HOURS. REPAIR ACCOMPLISHED UNDER XEO 53-101705. NON MEL RAISED. (K) 2L74 4F4 FRTA20WE E23EA 20051031002062005103100206CE 2005 10 31 CNQ2005F00000 120051004A2910AE5435E0235332 LINE CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL HYDRAULIC SYS CHAFED B CNQ3O OTHER O OTHER NRNOT REPORTED 1 GL13937QS4666 7500137 FLEXIBLE HYDRAULIC HOSE CHAFED THROUGH ALLOWING HYDRAULIC FLUID TO BE LOST IN THE (B-SYSTEM). HOSE WAS CONTACTING LT ELEVATOR POWER CONTROL UNIT. REPLACED HOSE AND VERIFIED ROUTING UNIT. REPLACED HOSE AND VERIFIED ROUTING TO PREVENT CHAFING. MFG IS ISSUING A SL ADDRESSING THE INSPECTION OF THE HYDRAULIC HOSES IN THIS AREA FOR CHAFING. (K) 2L72 4J4 FRTT00007WITE6CH 20051031002082005103100208SO 2005 10 31 GUU2005F00054 120051005A3240 BRAKE ASSY EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE RIGHT WEAK A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO17282AS 120226 AFTER LANDING, RT BRAKE WEAK, AIRCRAFT PULLS EXCESSIVELY TO THE LT WHEN BRAKES APPLIED. INSPECTED, BLED BRAKES AND OPERATIONAL CHECKED BRAKES. (K) 2L72 4T4 TRTA31SO E20NE 20051031002172005103100217EU 2005 10 31 KBM2005F00269 120050917A79215055PFA2 BLOWER MOTOR SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE OIL COOLER READS HIGH E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19351WM665 2167 OIL TEMP RUNNING EXTREMELY HIGH. TROUBLESHOT REPLACED OIL COOLER BLOWER MOTOR WITH O/H UNIT. (K) 1G71 3U3 U H9EU E19EU 20051101000052005110100005WP 2005 11 1 05FDEA03572 120051028A5320 WEB DOUG DC10 DC1030 3023501WP COCKPIT CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 INTERNAL LOWER COCKPIT AREA FOUND CORROSION INTERGRANULAR ON MEMBRANE BETWEEN STA 330 TO STA 313 X42 LT SIDE. REPAIRED MEMBRANE IAW SRM 53-00-01 VOL 1 FIG 10 SHT 4 AND SRM 51-35-01 PAG 1-13 FAB PARTS IAW DETAIL PARTS TRAVELER F160481/N00481 PER SRM 53-00-01 FIG 10 SHT 4 2L73 4F A22WE 20051101000202005110100020EA 2005 11 1 COMA0560573 120051027A3260864808 PSEU CNDAIRCL600 CL6002B19 1900309EA MLG MALFUNCTIONED A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01958CA161199578 7111 FLIGHT 5684- PROX SYSTEM FAULT. REPLACED THE PSEU. 2L72 4F RTA21EA 20051101000252005110100025NM 2005 11 1 SWAA053389 120051028A551265C25727 SKIN BOEING737 7373H4 1384600NM HORIZONTAL STAB DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D CHECK, FOUND RT HORIZONTAL STAB OTBD T/E UPPER SKIN DELAMINATED. REPAIRED STAB PER SRM. 2L72 4F RTA16WE 20051101000392005110100039NM 2005 11 1 SWAA053402 120051028A53126516300 BULKHEAD BOEING737 7375H4 138449DNM BS 178 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29507SW 24184 DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BLKHD WEB CRACKED AT RBL 17.1 & LBL 17.1, WL 227. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20051101000402005110100040NM 2005 11 1 SWAA053403 120051028A3350MS155721 BULB BOEING737 7375H4 138449DNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29524SW 26566 DURING SCHEDULED SERVICE CHECK, FOUND CABIN EMERGENCY LIGHT INOP AT ROW 20 DEF. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20051101000412005110100041NM 2005 11 1 SWAA053404 120051030A53116546554 FRAME BOEING737 7373H4 1384600NM BS 847 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 847, BETWEEN STR 25R TO STR 26R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051101000462005110100046NM 2005 11 1 SWAA053409 120051028A3350MS155721 BULB BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29623SW 27933 DURING SCHEDULED A2 CHECK, FOUND CABIN EMERGENCY LIGHT INOP AT ROW 12 DEF. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20051101000502005110100050WP 2005 11 1 05FDEA03540 120051027A5321 FLOOR PANEL DOUG DC10 DC1030 3023501WP COCKPIT CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 INTERNAL COCKPIT FLOOR AREA FOUND 1 EA CRACK 2 INCHES LONG ON TEE ANGLE AT STA 275 X -45, RT. PERFORMED INSPECTION IAW NDT SPM 06, NO CRACK FOUND ON FLOOR AREA TEE ANGLE STA 275 X-45 ONLY PENCILE MARK. 2L73 4F A22WE 20051101000512005110100051WP 2005 11 1 05FDEA03541 120051027A5311 FRAME DOUG DC10 DC1030 3023501WP BS 440 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 AVIONICS COMPT FOUND CORROSION WITH EXFOLIATION ON FRAME STA 440 X-49 RT SIDE. TRIMMED OUT DAMAGE FLANGE FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 53-30-00 FIG 4 AND SRM 51-33-01 PAGE 34-47. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F161176/N01176 IAW SRM 53-30-00 FIG 4. 2L73 4F A22WE 20051101000802005110100080NM 2005 11 1 05FDEA03348 120051011A5730ARB28931 DOUBLER DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 LEFT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT XORS 663. FASTENERS ON CRACKED INTERNAL BEADED DOUBLER AT XORS 663 OF LEFT HAND WING FIXED LEADING EDGE REMOVED AS PER SRM 51-31-01 VOLUME II. REPAIR DOUBLER FABRICATED AS PER SRM 57-10-00 FIGURE 24 VOLUME I AND INSTALLED AS PER SRM 51-35-01 VOLUME II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051101000812005110100081NM 2005 11 1 05FDEA03350 120051011A5730ARB28931 DOUBLER DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 LEFT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT XORS 653. FASTENERS ON CRACKED INTERNAL BEADED DOUBLER AT XORS 653 OF LEFT HAND WING FIXED LEADING EDGE REMOVED AS PER SRM 51-31-01 VOLUME II. REPAIR DOUBLER FABRICATED AS PER SRM 57-10-00 FIGURE 24 VOLUME I AND INSTALLED AS PER SRM 51-35-01 VOLUME II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051102000032005110200003NM 2005 11 2 05FDEA03255 120051006A5311 FRAME BOEING727 727100 1384036NM BS 460 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 E & E BAY CORROSION ON FRAME SPLICE ANGLE AFT SIDE BS 460 STR 26L. REMOVED CORROSION ON FRAME SPLICE FOUND TO BE OUT OF LIMITS. FABRICATED NEW SPLICE ANGLE & INSTALLED ALL WORK DONE IAW SRM 53-10-1, 51-40-04, 51-30-2. 2L73 4F RTA3WE 20051102000182005110200018EU 2005 11 2 USAA051215 120051019A5315D53472217220500 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19738US 1254 Y1292 BEAM AT SPLICE AT FR 66; CORROSION LEVEL 2; TASK JA-260-53500. REMOVED & REPLACED PER SRM 51-72-11, IPC 53-41-04, DEFECT SIZE: 2 X 4 X .030 INCH DEEP. 2L72 4F RTA28NM 20051102000202005110200020NM 2005 11 2 USAA051226 120051019A5320141N5170311F FLOOR SUPPORT BOEING757 7572B7 1384964NM BS 310.5-324 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19619AU 27198 STA 310.5-324 LBL 18.75 & WL 208.10; CORROSION LEVEL 1; TSK C53-221-003. FABRICATED & INSTALLED NEW FLOOR SUPPORT PEER SRM 53-00-00, 51-40-02 & DWG 141N5170, DEFECT SIZE: 3.0 X 2.75 X 0.050 INCH AREA. 2L72 4F RTA2NM 20051102000222005110200022NM 2005 11 2 USAA051220 120051019A5210507945264 SKIN BOEING737 737301 1384611NM PAX DOOR DEBONDED A USAAK NONE O OTHER ININSP/MAINT 1 EA19592US 23937 FWD ENTRY DOOR INNER WALL AT LWR SKIN DISBONDED. FABRICATED REPAIR DOUBLER, FILLER PER TR 52-10-16, DEFECT SIZE: 0.250 INCH. 2L72 4F RTA16WE 20051103000012005110300001NM 2005 11 3 05FDEA03560 120051027A5315 FLOORBEAM BOEING727 72722 1384002NM PWA JT8 JT8D1 52044NE BS 1130 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 FOUND CORROSION (C53-224-01) ON MAIN CARGO DECK FLOORBEAM UPPER AND LOWER FLANGE AT BS 1130 BETWEEN RBL 25 AND RBL 45, WL 208. REPAIRED MAIN DECK FLOORBEAM UPPER FLANGE AT BS 1130, RBL 45, WL 208 REF SRM 53-10- 8 FIG 10. 2L73 4F4 F A3WE E2EA 20051103000072005110300007EU 2005 11 3 XN0A1273 120051026A7400 IGNITER AIRBUS300 A300B4203 3930306EU GE CF6 CF650* 30018NE ENGINE FAILED A XN0AD RETURN TO BLOCK P NO WARNING INDICATION TXTAXI/GRND HDL 1 GL23372PC 196 ENG NR 1 NO LIGHT OFF DURING START ON A-IGNITORS. STARTS ON B-IGNITORS. TRANSFERRED TO DMI NR 5833 IAW ENA MEL 74-00-01 CAT (C). PLACARDS INSTALLED. (ORIG/OPEN) 2L72 4F4 FRTA35EU E23EA 20051103000112005110300011NM 2005 11 3 USAA200511002 120051031A5330 SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU BS 727E CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19396US 23318 2.5 INCH CRACK FOUND AT STA 727E AT STRINGER 23L. REPAIR: INSTALLED REPAIR DOUBLER IAW SRM 53-00-01 FIG. 201. 2L72 4F4 FRTA16WE E21EU 20051103000132005110300013NM 2005 11 3 USAA051324 120051102A5753 CLIP BOEING737 7374B7 1384702NM GE CFM56 CFM56* 13802NE NR 3 FLAP TRACK CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19779AU 24996 NR 3 FLAP TRACK STRUCTURE IB SIDE, AFT END. FABRICATED AND INSTALLED NEW ANGLE IAW SRM 51-10-02 DEFECT SIZE: 1 INCH. 2L72 4F4 FRTA16WE E2GL 20051103000152005110300015EU 2005 11 3 SA05111 120051028A335032145410 EPSU AIRBUS320 A320214 3930316EU EMERGENCY LIGHTSFAULTY A USAAK NONE L NO TEST ININSP/MAINT 1 EA19102UW122646530 844 LAX - THE PASSENGER LEFT HAND EMERGENCY LIGHTING SYSTEM IN ROWS 14, 16, 19, AND 23 WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20051103000562005110300056 2005 11 3 USAA051311 420051101A2565D5348015800500 GIRT BAR AIRBUSA319 A319112 3930323EU AFT DOOR CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19741UW 1269 FOUND RT AFT DOOR GIRT BAR FLOOR FITTINGS CORRODED; CORROSION LEVEL 1; TASK JA-260-53500. REMOVED AND REPLACED FITTINGS (2 EA) PER SRM 51-72-11, DEFECT SIZE: 1" BY 3" (2 AREAS). 2L72 4F RTA28NM 20051103000582005110300058NM 2005 11 3 BB05095 120051029A4900 IDG BOEING757 757225 1384959NM APU FAILED A USAAO OTHER H ELECT. POWER LOSS-50 PC CRCRUISE 1 EA19633AU 27811 APU SHUTDOWN IN FLIGHT WHILE THE LEFT IDG WAS ALREADY ON MEL. MAINTENANCE PLACED THE APU ON MEL AND CLEARED THE LEFT IDG MEL BY REPLACING THE IDG. 2L72 4F RTA2NM 20051103000602005110300060NM 2005 11 3 USAA051260 120051028A5320 STIFFENER BOEING737 7373B7 1384580NM BS 328-344 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND STIFFENER CORRODED, BS 328-344 LBL 12. REMOVED CORROSION AND TREATED IAW SRM 51-10-02, DEFECT SIZE: .25". 2L72 4F RTA16WE 20051103000622005110300062NM 2005 11 3 USAA051271 120051031A53201122424 SPLICE BOEING737 7373B7 1384580NM STA 907 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND STRINGER SPLICE CRACKED, STA 907 S4L. REMOVED AND REPLACED W/NEW PART IAW 51-10-02, DEFECT SIZE: .250". 2L72 4F RTA16WE 20051103000642005110300064NM 2005 11 3 USAA051283 120051031A5340 MOUNT BOEING737 7373B7 1384580NM STA. 986.5 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND LAV MOUNTS CORRODED, STA. 986.5 AND 1016. REMOVED CORRODED PARTS AND INSTALLED REPAIR PIECES IAW SRM 51-10-02, DEFECT SIZE: 1" BY 3". 2L72 4F RTA16WE 20051103000662005110300066NM 2005 11 3 USAA051281 120051031A5340 STRINGER CLIP BOEING737 7373B7 1384580NM STA68, S10R CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND TIE CLIP CRACKED, STA68, S10R. REPLACED WITH NEW CLIP IAW SRM 51-10-02, 51-40-03, DEFECT SIZE: .250". 2L72 4F RTA16WE 20051103000682005110300068NM 2005 11 3 USAA051279 120051031A5315 FLOORBEAM BOEING737 7374B7 1384702NM STA 947 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19779AU 24996 FOUND FLOORBEAM CORRODED, STA 947, RTB 6 TO LBL 2. REMOVED MINOR SURFACE CORROSION, PRIMED AND PAINTED IAW SRM 53060-51, DEFECT SIZE: .25". 2L72 4F RTA16WE 20051104000012005110400001 2005 11 4 YENA200580 420051101A2300C12848CA01 RADIO AIRBUS320 A320232 3930326EU IAE V2500 V2500A1 NE CAPT RMP 1 INOPERATIVE A YENAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15516JB1899 8 1302 CAPT' RMP (DIGIT WINDOW) BLANK/SLIGHT ODOR OF SMOKE/BURNING TURNED IT OFF. PERFORMED TSM 24-00-00-810-823 FOR ELECTRICAL BURNING SMELL IN COCKPIT. PERFORMED INTERNAL SURVEY (REPORT OF COCKPIT CABIN ODOR). TRACED SMELL TO RMP 1 WHICH IS INOP WITH BLANK DISPLAY. REMOVED AND REPLACED RMP 1 OPS AND BITE TESTED IAW AMM 23-13-13 AND 23-13-00. ALL NORMAL. 2L72 4F4 FRTA28NM E311NE 20051104000022005110400002EU 2005 11 4 YENA200579 120051031A34110851HL PITOT TUBE AIRBUS320 A320232 3930326EU F/O BLOCKED A YENAA UNSCHED LANDING O OTHER CLCLIMB 1 EA15536JB1456814568 1784 AIRSPEED INDICATION ON F/O SIDE QUIT WORKING AT 90 KTS APPROX AIR RETURN TO JFK. REMOVED AND REPLACED F/O'S ADM IAW 34-11-17. ALL OPS CHECK GOOD. LEAK CHECK OF F/O'S PITOT FOUND OK. REMOVED AND REPLACED F/O'S PITOT PROBE IAW AMM 34-11-15. ALL OPS CHECK GOOD. PITOT LEAK CHECK OK. REMOVED AND REPLACED PRECAUTIONARY NR 2 ADR IAW AMM 37-12-34. ALL OPS CHECK GOOD. 2L72 4F RTA28NM 20051104000112005110400011NM 2005 11 4 USAA051265 120051031A5320 WEB BOEING737 7373B7 1384580NM WEB @ STR 16 STACRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND WEB CRACKED AT STR 16 STA 294.5. FABRICATED WEB AND INSTALLED IAW SRM 53-10-15 AND 51-10-02, DEFECT SIZE: .50". 2L72 4F RTA16WE 20051104000142005110400014NE 2005 11 4 2005UALA01177 220051022A72006A5942 BLADE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CLAPPER WORN A UALAO OTHER J WARNING INDICATION CLCLIMB 1 WP29441UA12458 751 V10350 ENGINE 2 STALL DISPLAYED ON UPPER ECAM SCREEN DURING CLIMB OR CRUISE ACCELERATION. ENGINE NOT SHUTDOWN. STALL DISPLAYED ON UPPER ECAM SCREEN AFTER POWER REDUCTION FROM T/O POWER. ENGINE NOT SHUT DOWN. TROUBLESHOOTING BORESCOPE INSPECTION REVEALED OUT-OF-LIMITS WEAR ON HPC R3 BLADE CLAPPERS. ENGINE WAS REMOVED. 2L72 4F4 FRTA28NM E40NE 20051104000182005110400018NM 2005 11 4 2005UALA01181 120050811A2750 FLAP SYSTEM BOEING757 757222 1384956NM PWA 2037 PW2037 NE TE FLAPS MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29507UA 24743 DIVERTED TO SFO DUE TO FLAP RETRACTION PROBLEM. 2L72 4F4 FRTA2NM E17NE 20051104000192005110400019EU 2005 11 4 2005UALA01182 120051022A5210 SKIN AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE DOOR 1L DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29403UA 442 DOOR 1L HAS SKIN DAMAGE. MAJOR REPAIR OF DOOR SKIN PER SRM 52-10-00 FIGURE 203 WITH INCLUSION OF CORNER PRINCIPLE FROM FIGURE 205. 2L72 4F4 FRTA28NM E40NE 20051104000202005110400020EU 2005 11 4 2005UALA01183 120051025A2120 ODOR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE COCKPIT DETECTED A UALAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 WP29444UA 824 WHILE DESCENDING THRU 7000 FT, HAD BURNING RUBBER SMELL AND ACRID FUMES IN THE FWD CABIN AREA AND THE COCKPIT. INITIALLY SUSPECTED THERAPUETIC O2 CYCLINDER TO BE REASON FOR BURNING RUBBER SMELL. THERAPUETIC O2 BOTTLE WAS REMOVED. THE PSUS, SIDEWALL PANELS, O2 GENERATORS, UNDERSEATS. NO DEFECTS FOUND. OPERATED CABIN LIGHTS, VIDEO, GALLEY EQUIPMENT, RAN BOTH ENGINES AND OPERATED PACKS. NO DEFECTS FOUND. ACCOMPLISHED CIDS TEST ON PTP - NO DEFECTS FOUND. WHEN AN O2 BOTTLE IS FIRED IT BECOMES COLD. COULD NOT DUPLICATE BURNING RUBBER ODOR. 2L72 4F4 FRTA28NM E40NE 20051104000212005110400021EU 2005 11 4 2005UALA01184 120051025A3350 LIGHT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE DOOR 1L SLIDE NO TEST A UALAK NONE L NO TEST ININSP/MAINT 1 WP29428UA 523 WHILE TESTING EMERGENCY LIGHTS FAULTED EXT LOADS FWD L HAD RED FAULT LIGHT EXT LOADS. WHILE PERFORMING THE AIRCRAFT EMERGENCY LIGHT TEST, SYSTEM MESSAGE POINTING TO FAULT IN FWD DOOR SLIDE ASSY. THE SLIDE WAS REPLACED SERVICEABLE ONE AND THE AIRCRAFT SYSTEM BECAME NORMAL. THE AIRBUS SLIDES HAVE LIGHT SYSTEM THAT CAN ONLY BE MAINTAINED IN THE SHOP. COMMON SLIDE LIGHT SYSTEM DEFECT IS BUSTED BULB OR BROKEN HARNESS. AS REQUIRED BY THE UALCMM FOR THE SLIDE, A SDR IS INITIATED BY THE OSV SHOP EVERYTIME A DEFECT IS FOUND DURING THE MAINTENANCE OF SLIDES. 2L72 4F4 FRTA28NM E40NE 20051104000232005110400023EU 2005 11 4 2005UALA01186 120051024A3350 LIGHT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE DOOR LEFT AFT MALFUNCTIONED A UALAO OTHER L NO TEST ININSP/MAINT 1 WP29407UA 456 LEFT AFT EMERGENCY EXIT DISPLAYED ON UPPER ECAM SCREEN, DOOR. REPLACED EMERGENCY BATTERY AT LEFT OVERWING POSITION AND LEFT AFT POSITION. 2L72 4F4 FRTA28NM E40NE 20051104000262005110400026NM 2005 11 4 2005UALA01189 120051025A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29193UA 26890 MAIN STAIRS UPPER DECK EMERGENCY LIGHT INOP. 2L74 4F4 FRTA20WE E24NE 20051104000272005110400027NM 2005 11 4 2005UALA01191 120051026A3350 SLIDE BOEING747 747422 1384935NM PWA 4056 PW4056 NE R3 DOOR INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29116UA 26908 EEL AT DOOR 3R SLIDE INOP. 2L74 4F4 FRTA20WE E24NE 20051104000292005110400029NM 2005 11 4 2005UALA01193 120051026A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE RT OVERWING INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29116UA 26908 EEL AT RT OVERWING 2 FWD ASSY'S INOP. 2L74 4F4 FRTA20WE E24NE 20051104000302005110400030NM 2005 11 4 2005UALA01194 120051026A5330 SKIN BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU RT FUSELAGE APPRDENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29336UA 24240 SMALL SHARP DENT IN RIGHT FUSELAGE APPROXIMATELY 15 INCHES AFT OF AND 6 INCHES BELOW DOOR 1R CUTOUT. REMOVED DAMAGE REF SRM 53-00-01, MANUFACTURED A DOUBLER AND TRIPLER PER SRM 53-00-01 REPAIR 31. 2L72 4F4 FRTA16WE E21EU 20051104000322005110400032NM 2005 11 4 2005UALA01196 120051026A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE 6 O'CLOCK POSITIDAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29514UA 24839 FOUND DENT AT 6 O'CLOCK POSITION STA 1600. FOUND DENT WITHIN LIMITS IAW SRM 53-00-01. BURNISHED AND SMOOTHED OUT DENT. 2L72 4F4 FRTA2NM E17NE 20051104000342005110400034EU 2005 11 4 2005UALA01198 120051026A3350 BATTERY AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FWD LT EPSU FAILED A UALAK NONE O OTHER ININSP/MAINT 1 WP29459UA 1192 EPSU BATTERY FWD LT FAILED EMERGENCY LIGHT TEST. REPLACED EPSU BATTERY. 2L72 4F4 FRTA28NM E40NE 20051104000352005110400035NM 2005 11 4 2005UALA01199 120051027A3350 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT LOOSE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29199UA 28717 LOWER WALL EMERGENCY LIGHT, FWD OF AFT LAV NEAR DOOR 5 LT IS INOP. SECURED CONNECTOR TO LAMP. 2L74 4F4 FRTA20WE E24NE 20051104000362005110400036NM 2005 11 4 2005UALA01200 120051027A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE SEAT 1A INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29199UA 28717 SEAT 1A FWD EMERGENCY LIGHT IS INOPERATIVE. REPLACED LAMP. 2L74 4F4 FRTA20WE E24NE 20051104000372005110400037NM 2005 11 4 2005UALA01201 120051022A5414 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR2 ENG PYLON IBDAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29514UA 24839 NR 2 ENGINE PYLON IB SIDE FWD ACCESS HOLE, DAMAGED. MAJOR REPAIR ACP ON NR 2 ENGINE PYLON INBD SIDE FWD ACCESS HOLE REF DOCK W.U.G2788H. 2L72 4F4 FRTA2NM E17NE 20051104000382005110400038NM 2005 11 4 2005UALA01202 120051026A3350 LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE SLIDE INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29514UA 24839 EXTERIOR EMERGENCY SLIDE LIGHT L41 AT DOOR 2RT IS INOPERATIVE. RE-SECURED TERMINAL LUGS. 2L72 4F4 FRTA2NM E17NE 20051104000402005110400040NM 2005 11 4 2005UALA01204 120051027A3350 LIGHT BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU ROW 13 INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29315UA 23947 EEL FLOOR LIGHTS INOPERATIVE FROM ROW 13 AFT. REPLACED INVERTER AT ROW 19. 2L72 4F4 FRTA16WE E21EU 20051104000422005110400042EA 2005 11 4 SWIA200515769 120051028A2750860D10018 FCU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAD RETURN TO BLOCK FJ FLT CONT AFFECTED WARNING INDICATION TOTAKEOFF 1 NM07453SW 7743 FLAPS FAIL MESSAGE, AFTER TAKEOFF. RETURNED TO SLC. REPLACED FECU IAW MM 27-51-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051104000442005110400044 2005 11 4 SWIA200515749 420051027A22166225734002 SERVO EMB 120 EMB120ER 3260203SO RUDDER BINDING A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07217SW1298012980 120286 CAPTAINS RUDDER PEDALS BINDING. REPLACED RUDDER SERVO. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20051104000452005110400045EA 2005 11 4 SWIA200515750 120051021A274070623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA MOTOR MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07927SW8171 8171 7693 DURING CRUISE AND DESCENT AP PITCH TRIM CAUTION MSG ILLUMINATED FOLLOWED BY STAB TRIM CH 1 STATUS MSG. REPLACED STAB MCU IAW CRJ 200 MM 27-43-05 AND 27-41-00. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051104000472005110400047EA 2005 11 4 SWIA200515752 120051027A2741 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07937SW 7735 FO'S TRIM SWITCH STICKS. REPLACED SWITCH IAW 27-42-00. 2L72 4F RTA21EA 20051104000492005110400049EA 2005 11 4 SWIA200515754 120051025A2751855D1009 POSITION SENSOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07416SW5882 5882 7089 FLAPS FAIL CAUTION MESSAGE EN ROUTE. REPLACED LT WING FLAP BPSU IAW MM 27-51-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051104000502005110400050EA 2005 11 4 SWIA200515767 120051029A2741 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CLCLIMB 1 NM07963SW 7865 STAB CHANNEL 1 KICK OFF LINE ON CLIMBOUT. REPLACED CAPTAINS STAB TRIM SWITCH AS REQUIRED IAW 27-40-00. 2L72 4F RTA21EA 20051104000512005110400051EA 2005 11 4 SWIA200515755 120051031A274070623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA MOTOR MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07446SW996 996 7666 STAB CH2 INOP, WILL NOT ENGAGE. REPLACED MCU IAW MM 27-42-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051104000532005110400053SO 2005 11 4 SWIA200515757 120051028A2611 SMOKE DETECTOR EMB 120 EMB120ER 3260203SO LAVATORY ACTIVATED A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07213SW 120277 LAV SMOKE DETECTOR GOES OFF. REPLACED LAV SMOKE DETECTOR. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20051104000552005110400055EA 2005 11 4 SWIA200515759 120051029A27604916405 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER INTERMITTENT A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07916SW1464710042 7634 AFTER PUSHBACK RECEIVED FLT SPOILERON FAULT CAUTION MESSAGE. REPLACED NR 1 SECU IAW AMM 27-61-05. OPERATIONAL CHECK GOOD IAW AMM 27-61-05-720-801AND 27-64-00-710-810. 2L72 4F RTA21EA 20051104000562005110400056EA 2005 11 4 SWIA200515760 120051027A5610 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07925SW 7682 RIGHT WINDOW CRACKED UP. REPLACED F/O'S SIDE WINDOW IAW MM 56-21-01. PN/OFF 601R33033-12, SN/OFF 02053H9219. 2L72 4F RTA21EA 20051104000582005110400058SO 2005 11 4 SWIA200515762 120051025A3350 LIGHT EMB 120 EMB120ER 3260203SO CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07268UE 120207 EMERGENCY LIGHT 1ST FRONT ONE ON GROUND STRIP OUT. REPLACED 1ST FRONT EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20051104000592005110400059EA 2005 11 4 SWIA200515763 120051028A5210 LATCH CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BINDING A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07411SW 7067 MAIN CABIN DOOR IS VERY DIFFICULT TO LATCH CLOSED OR OPEN USING THE INTERIOR HANDLE. LUBRICATED MAIN CABIN DOOR LATCH PINS, OPERATIONAL CHECKS GOOD. 2L72 4F RTA21EA 20051104000602005110400060EA 2005 11 4 SWIA200515764 120051027A2750865D1007 PDU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07954SW 7815 FLAP DEGRADED MESSAGE, ON TAXI OUT. REPLACED FLAP PDU IAW MM 27-52-01, OPERATIONAL CHECK GOOD. P/N 865D100-7, S/N ON 0792, S/N OFF 1093. 2L72 4F RTA21EA 20051104000612005110400061EA 2005 11 4 SWIA200515765 120051028A5210 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BINDING A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07454SW 7749 MAIN CABIN DOOR WON'T OPEN FROM OUTSIDE. LUBED INNER DOOR ASSY AND OUTER DOOR HANDLE ASSY. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051104000622005110400062EA 2005 11 4 SWIA200515766 120051028A274170609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07979SW952 952 7954 MACH TRIM/STAB TRIM FAILED INFLIGHT. REPLACED HSTCU. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051104000642005110400064NM 2005 11 4 SWAA053371 120051027A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 277, STR 15R. REMOVED AND REPLACED CLIP IAW SRM. 2L72 4F RTA16WE 20051104000652005110400065NM 2005 11 4 SWAA053386 120051026A53306545765 SKIN BOEING737 7373H4 1384600NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 12R. REPAIRED SKIN IAW EA. 2L72 4F4 FRTA16WE E2GL 20051104000662005110400066NM 2005 11 4 SWAA053416 120051031A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051104000672005110400067NM 2005 11 4 SWAA053417 120051031A55516551524 FITTING BOEING737 7373H4 1384600NM TAIL CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D CHECK, FOUND LT AND RT HORIZONTAL STAB FITTING LUG FACES CORRODED. REPAIRED LUG FACES PER SRM. 2L72 4F RTA16WE 20051104000682005110400068NM 2005 11 4 SWAA053418 120051031A3350PH22300L STRIP BOEING737 7373H4 1384600NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29364SW 26575 DURING SCHEDULED C1 CHECK, FOUND PHOTOLUMINESCENT STRIP CRACKED. REMOVED AND REPLACED STRIP PER MM. 2L72 4F RTA16WE 20051104000692005110400069NM 2005 11 4 SWAA053419 120051023A3350PH22300L STRIP BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29368SW 26579 PHOTOLUMINESCENT STRIP LOOSE AT ROW 8 DEF. SECURED STRIP PER MM. 2L72 4F RTA16WE 20051104000702005110400070NM 2005 11 4 SWAA053420 120051031A3350207377 LENS BOEING737 7377H4 1384404NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29402WN 29814 EEPLS TRACK LENS MISSING AT FWD END. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20051104000712005110400071 2005 11 4 SWAA053421 420051031A2565D31354 SLIDE BOEING737 7373A4 1384585NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051104000722005110400072NM 2005 11 4 SWAA053422 120051030A3350MS155721 BULB BOEING737 7377H4 1384404NM FUSELAGE INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29774SW 27882 DURING SCHEDULED RON CHECK, FOUND L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20051104000732005110400073NM 2005 11 4 SWAA053372 120051026A53306545774 SKIN BOEING737 7373H4 1384600NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 19R. REPAIRED SKIN IAW EA. 2L72 4F4 FRTA16WE E2GL 20051104000742005110400074NM 2005 11 4 SWAA053373 120051026A53306545774 SKIN BOEING737 7373H4 1384600NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 18L. REPAIRED SKIN IAW SRM. 2L72 4F4 FRTA16WE E2GL 20051104000762005110400076NM 2005 11 4 SWAA053375 120051024A56105893543130 WINDOW BOEING737 7373H4 1384600NM GE CFM56 CFM56* 13802NE COCKPIT ARCED A SWAAO OTHER O OTHER NRNOT REPORTED 1 SW29352SW 24888 R1 COCKPIT WINDOW ARCED AND CRACKED. REMOVED AND REPLACED R1 WINDOW AND HEAT CONTROLLER IAW MM. 2L72 4F4 FRTA16WE E2GL 20051104000782005110400078NM 2005 11 4 SWAA053377 120051027A335007912 COVER BOEING737 7377H4 1384404NM GE CFM56 CFM56* 13802NE CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29454WN 29851 EEPLS TRACK COVER LOOSE AT FWD END. SECURED COVER IAW MM. 2L72 4F4 FRTA16WE E2GL 20051104000802005110400080NM 2005 11 4 SWAA053379 120051027A53116545808 FRAME BOEING737 7373H4 1384600NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 304, STR 16L. REPAIRED FRAME IAW MFG ER. 2L72 4F4 FRTA16WE E2GL 20051104000822005110400082NM 2005 11 4 SWAA053381 120051027A53116545834 CREASE BEAM BOEING737 7373H4 1384600NM GE CFM56 CFM56* 13802NE CABIN FLOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED D CHECK, FOUND LT CREASE BEAM CORRODED BETWEEN BS 294.5 TO BS 360, WL 208. REPAIRED CREASE BEAM IAW SRM. 2L72 4F4 FRTA16WE E2GL 20051104000842005110400084 2005 11 4 SWAA053383 420051026A25656949956 CABLE ASSY BOEING737 7373Y0 1384671NM GE CFM56 CFM56* 13802NE L2 DOOR MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED C1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE LATCH CABLE ASSY MISROUTED. REROUTED CABLE ASSY IAW MM. 2L72 4F4 FRTA16WE E2GL 20051104000862005110400086NM 2005 11 4 SWAA053385 120051026A53306545776 SKIN BOEING737 7373H4 1384600NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 910, STR 4L. REPAIRED SKIN IAW EA. 2L72 4F4 FRTA16WE E2GL 20051104000892005110400089NM 2005 11 4 SWAA053438 120051101A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 700, STR 10R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051104000912005110400091NM 2005 11 4 SWAA053440 120051102A53116519603 CREASE BEAM BOEING737 7373H4 1384600NM CABIN FLOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D-CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 360 TO BS 380, WL 208. REPAIRED CREASE BEAM PER SRM. 2L72 4F RTA16WE 20051104000932005110400093NM 2005 11 4 SWAA053442 120051102A53146545866 KEELBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D-CHECK, FOUND LT KEEL BEAM CORRODED BETWEEN BS 500D TO BS 727. REMOVED AND REPLACED KEEL BEAM PER SRM. 2L72 4F RTA16WE 20051104000952005110400095NM 2005 11 4 SWAA053444 120051102A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM AFT CARGO CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 927, STR 20L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051104001102005110400110 2005 11 4 QXEA200501379 420051026A34207003360941 COMPUTER DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE AHRS MALFUNCTIONED A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09357PH166141098 504 FLIGHT NR 2147, WHEN TAXIING TO THE RUNWAY, THE FIRST OFFICERS ADI WENT UP TO 8 DEGREES AND BANKED THEN DIPPED DOWN TO -3 PITCH. MAINTENANCE REPLACED THE NR 2 AHRS COMPUTER IAW MTC 9340019. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20051104001132005110400113NM 2005 11 4 MZZA0500011 120051102A3350D71702030 CHARGER BOEING737 737824 13844BZNM EMERGENCY LIGHT INOPERATIVE A MZZAK NONE O OTHER ININSP/MAINT 1 WP1314249 28809 INSPECTION FOUND THE LT FAIRING EMERGENCY LIGHT INOPERATIVE. THE M1670 CHARGER WAS REPLACED IAW MM 33-51-00. 2L72 4F RTA16WE 20051104001152005110400115NM 2005 11 4 MZZA0500013 120051102A3350D71701100 BATTERY PACK BOEING737 737824 13844BZNM RT OVERWING INOPERATIVE A MZZAK NONE O OTHER ININSP/MAINT 1 WP1314249 28809 INSPECTION FOUND RT OVERWING INTERIOR EMERGENCY LIGHT INOPERATIVE. THE M1965 BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51-06. 2L72 4F RTA16WE 20051104001182005110400118NM 2005 11 4 MASA200500804 120051014A2910731840 POWER UNIT DHAV DHC8 DHC8202 2809007NM HYD SYSTEM MALFUNCTIONED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07449YV3470 3470 449 NR 2 ENGINE HYD CAUTION. MAINTENANCE REMOVED AND REPLACED SPU AND SERVICED HYDRAULIC SYSTEM. 2H72 4T RTA13NM 20051104001202005110400120SO 2005 11 4 MASA200500342 120050509A3230355022002 CONTROL UNIT EMB 145 EMB145LR 3260212SO MLG MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07846MJ718 718 145507 THE CREW DIVERTED TO IAD DUE TO THE LANDING GEAR WOULD NOT RETRACT AND AN ASSOCIATED LG AIR/GROUND DISAGREE MESSAGE. THE AIRCRAFT FERRIED TO CLT WHERE MAINTENANCE REMOVED AND REPLACED THE LEFT GEN L/O AND T/R SYSTEM. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20051104001222005110400122SO 2005 11 4 MASA200500477 120050618A261014522285401 DUCT EMB 145 EMB145LR 3260212SO CABIN AIR UNKNOWN A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07829MJ 145228 THE CREW HAD SMOKE IN THE CABIN WHILE THE AIR START CART WAS USED TO RUN THE PACKS. MX REMOVED AND REPLACED DUCTING AND TEMP SWITCH. 2L72 4T RTT00011AT 20051104001232005110400123SO 2005 11 4 MASA200500509 120050630A2710 CONTROL CABLE EMB 145 EMB145LR 3260212SO AILERONS OBSTRUCTED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07846MJ 145507 AILERONS MOMENTARILY -JAMMED- THE CAPTAIN WAS ABLE TO REGAIN TOTAL CONTROL AND LAND WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE GPWS. MX FOUND ROOT CAUSE TO BE A DISLODGED DISTRIBUTION DUCT THAT BLEW COLD AIR INTO THE INSULATION BLANKET WHICH CAUGHT THE CABLES RESULTING IN INTERMITTENT BINDING. 2L72 4T RTT00011AT 20051104001242005110400124SO 2005 11 4 MASA200500554 120050715A272015793101 PRESSURE SWITCH EMB 145 EMB145LR 3260212SO RUDDER FAILED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07834MJ10955 145340 A RUDDER SYS 1-2 INOP EICAS MESSAGE. MX REPLACED NR 1 AND NR 2 RUDDER PRESSURE SWITCHES. NO FURTHER DEFECTS NOTED. 2L72 4T RTT00011AT 20051104001252005110400125SO 2005 11 4 MASA200500324 120050429A3230355022002 CONTROL UNIT EMB 145 EMB145LR 3260212SO MLG FAILED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07842MJ9093 9093 145457 THE AIRCRAFT RETURNED TO THE FIELD FOR A LANDING GEAR AIR/GROUND FAIL MESSAGE ON THE EICAS. MAINTENANCE REPLACED THE LANDING GEAR ECU AND THE NOSE DOOR PROX SWITCH. 2L72 4T RTT00011AT 20051104001262005110400126SO 2005 11 4 MASA200500331 120050504A7897601R579005 WIRE HARNESS EMB 145 EMB145LR 3260212SO THRUST REVERSER UNKNOWN A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07833MJ 145327 THE CREW ABORTED TAKEOFF DUE TO AN E2 REVERSER DISAGREE MESSAGE DURING TAKEOFF ROLL. MAINTENANCE REPAIRED RED ELECTRICAL HARNESS. 2L72 4T RTT00011AT 20051104001272005110400127SO 2005 11 4 MASA200500366 120050509A8011 CARBON SEAL EMB 145 EMB145LR 3260212SO STARTER FAILED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07853MJ7041 1425 145464 NR 1 ATS CARBON SEAL FAILED 400HR CHECK (N857MJ) WITH A LOSS OF 45CC OF OIL. EMB145-80-0003 FOR A FLY ON FOR 50FH WAS GENERATED. NO PHYSICAL DAMAGE NOTICED ON PART, ONLY OIL LOSS. 2L72 4T RTT00011AT 20051104001282005110400128SO 2005 11 4 MASA200500374 120050519A32608005701 PROXIMITY SENSOR EMB 145 EMB145LR 3260212SO NLG FAILED A MASAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 SW07842MJ 145457 THE CREW RETURNED TO THE FIELD DUE TO A L/G AIR GROUND FAIL EICAS MESSAGE AND LANDING GEAR WOULD NOT RETRACT. MAINTENANCE REPLACED THE LT MAIN LANDING GEAR WOW PROXIMITY SENSOR AND SERVICED THE NOSE LANDING GEAR STRUT. 2L72 4T RTT00011AT 20051104001302005110400130 2005 11 4 KBM2005F00307 420051018A34215040017901 GYRO SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1 60030NE ATTITUDE FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19215LA161491124 2143 UNIT WILL NOT HOLD CAGE. REMOVED AND REPLACE. (K) 1G71 3U3 U H9EU E19EU 20051104001322005110400132WP 2005 11 4 IXXA05SMN246S 120051013A5740 FITTING DOUG DC8 DC871F 302199DWP FS 74.000S.51 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING ROUTINE C CHECK INSPECTION, LT WING NR 2 MAIN TANK FITTING CRACKED, FS 74.000 S.51 (FWD EXTERNAL PART). REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D. CLEANED AND APPLIED POLYURETHANE TOP COATING YELLOW IAW DC8 SRM 51-1-12 PAGES 7-25. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D. TORQUED IAW DC8 SRM 51-3-1. FOR LEAK CHECK SEE JC 99116. 2L74 4F RT4A25 20051104001342005110400134WP 2005 11 4 IXXA05SMN202S 120050927A5340 FITTING DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE BS 834.5 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING ROUTINE C CHECK INSPECTION, MAIN CARGO COMPT. AFT FITTING CRACKED 3, STA 834.5 L-14RREMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9, SRM 51-3-1 (TORQUE). 2L74 4F4 FRT4A25 E2GL 20051104001362005110400136WP 2005 11 4 IXXA05SMN221S 120050929A5730 SKIN DOUG DC8 DC871F 302199DWP XRS172.000 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING C CHECK INSPECT, LT WING LWR SKIN CRACK AT STA XRS 172.000 BETWEEN S-56 AND S-57. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-1 FIG 1, EO SEMAN # 20051287 DATED 09-29-05. REMOVED FASTENERS IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D. STOP DRILLED CRACK END IAW DC8 SRM 57-2-1A FIG. 1 PAR. 7. NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D EXTERNAL REPAIR DOUBLER (AL7075T6 0.080”) IAW DC8 SRM 57-2-1A FIG 1, DC8 SRM 51-3-1 FIG 26 ITEM “A”. CLEANED, TREATED, PRIMED AREA, INNER SIDE OF EXTERNAL REPAIR DOUBLER IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED EXTERNAL REPAIR DOUBLER IAW DC8 SRM 57-2-1A FIG 1, DC8 SRM 2L74 4F RT4A25 20051104001382005110400138WP 2005 11 4 IXXA05SMN223S 120051013A5330 RIVET DOUG DC8 DC871F 302199DWP FS 104 IMPROPER B IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW11829BX896722998 45994 DURING C CHECK INSPECT, FWD LWR FUSELAGE BELLY, FS 104 L-35.75L, UPGRADE EXTERNAL DOUBLER TO INCORPORATE A MIN OF 3 ROWS OF RIVETS. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-1 FIG 7, EO SEMAN NR 20051192 DATED 09-20-05. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D. REMOVED DAMAGED SECTION IAW DC8 SRM 53-2-1 FIG 7 (SHEET 1, 3). NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D REPAIR DOUBLER (AL7075T6 O.O63”), (02 EA) INTERNAL FINGER DOUBLERS (AL7075T6 0.032”) IAW DC8 SRM 53-2-1 FIG 7 (SHEET 1-3), DC8 SRM 53-4-1 FIG 1 ITEM “C”, DC8 SRM 51-9-8 FIG 68ª, DC8 SRM 51-1-4 (FORMING). CLEANED, TREATED, PRIMED AREA, REPAIR PARTS IAW DC8 SRM2L74 4F RT4A25 20051104001392005110400139WP 2005 11 4 IXXA05SMN233S 120051013A5754 SKIN DOUG DC8 DC871F 302199DWP XW 435.000 IMPROPER B IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW11829BX896722998 45994 DURING C CHECK INSPECTION, LT OTBD FLAP UPPER SKIN HAS NON STANDARD REPAIR, XW 435.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-5 FIG 1, EO SEMAN # 20051210 DATED 09-21-05. REMOVED FASTENERS IAW DC8 SRM 51-1-21, DC8 SRM 51-3-0. REMOVED DAMAGED SECTION IAW DC8 SRM 57-2-5 FIG 1. PERFORMED DETAIL VISUAL INSP OF REWORKED AREA. NEITHER CRACK NOR CORROSION FOUND. FAB`D NEW PLATING SEGMENT (AL2024T3 0.050”), SPLICE (AL2024T3 0.063”), FILLER (AL2024T3 0.020”) IAW DC8 SRM 57-2-5 FIG 1 (SHEET 1-2), DC8 SRM 57-7-1 FIG 4, TR#57-94 ITEMS “Q”, “V”. CLEANED, TREATED, PRIMED AREA, REPAIR PARTS IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW DC8 SRM 57-2-5 FIG2L74 4F RT4A25 20051104001402005110400140WP 2005 11 4 IXXA05SMN234S 120051013A5754 SKIN DOUG DC8 DC871F 302199DWP ZONE 600 IMPROPER B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING C CHECK INSPECTION, RT WING INBD FLAP UPPER SKIN HAS NON STANDARD REPAIR. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-7-1 FIG 1, EO SEMAN NR 20051279 DATED 09-26-05. REMOVED DAMAGED PLATING IAW DC8 SRM 57-1-0 PG 1, DC8 SRM 51-1-21. FABRICATED NEW PLATING (AL2024T3 0.050”) IAW DC8 SRM 57-7-1 FIG 1 ITEM “F”, DC8 SRM 51-1-4 (FORMING). CLEANED, TREATED, PRIMED AREA, NEW PLATING INNER FACE IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACE IAW DC8 SRM 51-1-11 PG 9. INSTALLED NEW PLATING IAW DC8 SRM 51-1-21. 2L74 4F RT4A25 20051104001412005110400141WP 2005 11 4 IXXA05SMN235S 120051013A5754 SKIN DOUG DC8 DC871F 302199DWP XF 230.000 IMPROPER B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING C CHECK INSPECTION, RT OTBD FLAP UPPER SKIN HAS NON STANDARD REPAIR, STA XF 230.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 # 05447 DATED 10-05-05, SEMAN DWG # ED 4072 DATED 10-01-05, EO SEMAN # 20051298 DATED 10-05-05. REMOVED EXISTING NON STANDARD REPAIR IAW DC8 SRM 51-1-21. REMOVED DAMAGED SECTION IAW SEMAN DWG # ED-4072. NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D NEW PLATING SEGMENT (AL2024T3 0.071”), INTERNAL SPLICE (AL2024T3 0.080”, (02EA) EXTERNAL DOUBLERS (AL2024T3 0.080”) IAW SEMAN DWG NR ED-4072, DC8 SRM 51-1-4 PG 1 (FORMING). CLEANED, TREATED, PRIMED AREA, REPAIR PARTS IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES2L74 4F RT4A25 20051104001422005110400142WP 2005 11 4 IXXA05SMN248S 120051013A5330 RIVET DOUG DC8 DC871F 302199DWP FS 10 L-22 OUT OF TOLERANCEB IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING C CHECK INSPECT, LT FUSELAGE NOSE SECTION PLATING DOUBLER REPAIR EXCEED MAX RIVETS SPACING STA FS 10 L-22 LT. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 # 05448 DATED 10-05-05, SEMAN DWG # ED 4076 DATED 10-03-05, EO SEMAN # 20051294 DATED 10-05-05. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21 PG 1, DC8 SRM51-1-20D. REMOVED DAMAGED SECTION IAW SEMAN DWG # ED-4076. NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NO CRACK NOR CORROSION FOUND. FABRICATED REPAIR DOUBLER (AL7075T6 0.071”, FINGER DOUBLER (AL7075T6 0.032”) IAW SEMAN DWG # ED-4076. CLEANED, TREATED, PRIMED AREA, REPAIR PARTS IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED R2L74 4F RT4A25 20051104001442005110400144WP 2005 11 4 IXXA05SMN199S 120050923A5730 SKIN DOUG DC8 DC871F 302199DWP XFS710. - 716. CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING C CHECK INSPECTION, RT WING OTBD L/E LOWER SKIN CRACKED 1” APPROX, BETWEEN STA XFS 710.000 AND XFS 716.250. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 # 05461 DATED 10-05-05, SEMAN DWG # ED-4071 DATED 10-06-05, EO SEMAN # 20051277 DATED 10-05-05. REMOVED FASTENERS IAW DC8 SRM 51-1-21, DC8 SRM 51-3-0. REMOVED CORROSION FROM RT WING OUTBD L/E LWR SKIN (STA XFS 710.000-716.000) IAW DC8 SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW DC8 SRM 57-2-1 FIG 2G. CUT OUT DAMAGED SECTION IAW SEMAN DWG # ED-4071. NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D REPAIR DOUBLER (AL7075T6 0.063”), FILLER (AL7075T6 0.050”) IAW SEMAN DWG # ED-4071. CLEANED, TREAT2L74 4F RT4A25 20051031000292005103100029NM 2005 10 31 AMTA200500851 120051011A335020131A BATTERY PACK BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE EMERGENCY LIGHT UNSERVICEABLE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11517AT 27973 EMERGENCY EXIT LIGHTS INOPERATIVE AT L2 DOOR AND AFT. REPLACED L2 EMERGENCY BATTERY PACK. ALL EMERGENCY LIGHTS. OPS CHECK GOOD. (K) 2L72 4F4 FRTA2NM E12EU 20051031000362005103100036NE 2005 10 31 AMTA200500884 220051012A7321356A7065G181 EEC BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE RT ENGINE UNSERVICEABLE A AMTAH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CRCRUISE 1 GL11554TZ1400514005 32588 RT ENGINE LIMITER INOP LIGHT ILLUM. EICAS MSG AND R ENG LIMITER DISPLAYED. PERFORMED FIM 73-21-00, FIG 103A, FAULT CODE (BF) FOUND ON EEC, ONLY FAULT FOUND, IAW FIM REMOVED AND REPLACED RT ENGINE EEC IAW 73-21-07-4, ENGINE RUN-UP AND TAXI. OPS CHECK NORMAL. (K) 2L72 4F4 FRTA2NM E12EU 20051031000392005103100039EU 2005 10 31 KBM2005F00302 120051004A80120174078030 DRAIN VALVE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE START DRAIN LEAKING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19966SH2227 3787 START DRAIN VALVE, UNIT LEAKING EXTERNALLY, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051031000402005103100040EA 2005 10 31 A6WA200540313 120051013A4930 B-NUT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE APU FUEL SYS LOOSE A A6WAE ENGINE SHUTDOWN KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL31439AW 7753 WHILE APU RUNNING HEARD LOUD BANG NOISE FROM REAR OF AIRCRAFT. APU RPM DROPPED BY 10 PERCENT. FLIGHT ATTENDANT NOTICED SMELL OF FUEL IN REAR OF AIRCRAFT. NO INDICATION OF FIRE. SHUTDOWN APU. INSPECTED APU, FOUND LOOSE B-NUT ON FUEL SOLENOID. RETORQUED B-NUT. NO FURTHER FUEL LEAKS NOTED. ATTEMPTED TO START APU. HAGS AT 49 PERCENT, PLACED ON MEL. (K) 2L72 4F4 FRTA21EA E15NE 20051031000442005103100044NM 2005 10 31 UIEA200500121 120050830A541065B94141110 ANGLE BOEING747 7472D7B 1384803NM GE CF6 CF650E2 30018NE NR 4 PYLON OUT OF LIMITS A UIEAK NONE O OTHER ININSP/MAINT 1 EA15524MC 21784 D-CHECK, NR 4 PYLON SIDE COWL HINGE SUPPORT ANGLE BRACE, ONE HOLE EXCEEDING LIMITS. THE HOLE WAS OVERSIZED TO 0.484 INCHES DIAMETER INCLUDING A .0312 DIAMETER INSURANCE CUT. THE HOLE WAS NDT INSPECTED TO ENSURE A CRACK AND DAMAGE FREE CONDITION. A REPAIR STEEL STRAP WAS INSTALLED ONT HE AFT SIDE OF THE ANGLE. A FREEZE PLUG WAS INSTALLED AND A .3750 INCHE DIAMETER FASTENER WAS INSTALLED THRU THE FREEZE PLUG, TO INSTALL A NEW ANGLE WITHIN 18 MONTHS. (K) 2L74 4F4 FRTA20WE E23EA 20051031000452005103100045NM 2005 10 31 AMTA200500902 120051014A3397 LIGHT BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE ROW 28 DISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11522AT 29330 FLOOR PATH EXIT MARKER, ROW 28, INOPERATIVE. RECONNECTED LIGHT ASSY. OPS CHECK GOOD. (K) 2L72 4F4 FRTA2NM E12EU 20051031000522005103100052EA 2005 10 31 A6WA200540291 120050822A2611 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE SMOKE DETECTOR LOOSE A A6WAK NONE N FALSE WARNING ININSP/MAINT 1 GL31402AW 09000 7281 (SMOKE TOILET) MESSAGE WITH AUDIBLE ALARM. NO SMOKE NOTED. LASTED FOR 2 MINUTES. COMPLIED WITH QRH. RESECURED CONNECTOR PLUG TO SMOKE DETECTOR (THAT WAS FOUND LOOSE), OPS CHECK GOOD IAW AMM. (K) 2L72 4F4 FRTA21EA E15NE 20051031000532005103100053NM 2005 10 31 USAA051024 120050817A5315 FLOORBEAM BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU BS 986 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19444US40668 24862 BFM - Q2 - FLOORBEAM UPPER CHORD, 50 INCH CORROSION; NO LEVEL OR TASK; FS 986.5, LBL 0 TO LBL 50 INCH. FABED PART FLOORBEAM UPPER CHORD, INSTALLED IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051031000592005103100059EU 2005 10 31 KBM2005F00290 120050922A3310704A46814049 POTENTIOMETER SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1B 6OO30NE CABIN LIGHTS INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH 2337 LIGHT WILL NOT DIM, DIMMER BOX REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051031000602005103100060EU 2005 10 31 KBM2005F00291 120050926A6520350A33215001 BALL END SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE T/ROTOR SPIDER WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19351WM 2167 SPIDER BALL END WORN BEYOND LIMITS. REPLACED WITH OVERHAULED UNIT. (K) 1G71 3U3 U H9EU E19EU 20051031000662005103100066NM 2005 10 31 AMTA200500853 120051011A2612 FIRE LOOP BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE LT ENGINE LOOSE A AMTAO OTHER N FALSE WARNING CRCRUISE 1 GL11552TZ 32586 EICAS STATUS MSG L ENG FIRE LOOP 1, DISPLAYED. SECURED TEMP SENSE LINE, RAN ENGINE. OPS CHECK NORMAL. NO EICAS MSG. (K) 2L72 4F4 FRTA2NM E12EU 20051031000762005103100076EU 2005 10 31 KBM2005F00284 120050923A7931704A37642043 TRANSMITTER SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE ENG OIL PRESSUR INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P43 2347 OIL PRESSURE GAUGE READS -0-, REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20051031000772005103100077 2005 10 31 KBM2005F00285 420050924A34215040111920 GYRO SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE ATTITUDE INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P442 2347 ATTITUDE INDICATOR FLAG WOULD NOT RETRACT. REPLACED WITH SERVICEABLE UNIT. (K) 1G71 3U3 UNCH9EU E19EU 20051031000892005103100089NM 2005 10 31 S2YA05043 120050720A30105E2546 BOOT DORNERDO32 DO328300 NM PWA 306 PW306B NE RT ELEVATOR INOPERATIVE A S2YAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL13355SK 3124 DURING FLIGHT, THE CREW REPORTED ELEVATOR HEAT MESSAGE. SINCE WEATHER WAS ENROUTE, THE CREW PERFORMED AN AIR-TURN-BACK. MAINTENANCE REPLACED THE RT ELEVATOR HORN ASSEMBLY IN ORDER TO REPAIR THE HEAT WITH OPERATIONAL CHECKS GOOD THE AC WAS RETURNED TO SERVICE. (K) 2H72 4T4 FRTA55NM E35NE 20051031000902005103100090CE 2005 10 31 S2YA05044 120050720A7931PT6A67D PRESSURE SYSTEM BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE RT ENGINE OIL FLUCTUATES A S2YAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL13891SK215474736 UE89 SHORTLY AFTER TAKEOFF, THE CREW REPORTED THE OIL PRESSURE DROPPED TO ABOUT 40 PSI ACCOMPANIED BY A TEMPERATURE INCREASE TO 800 DEGREES AND TORQUE FLUCTUATIONS. THE CREW PERFORMED AN AIR-TURN-BACK. MAINTENANCE INSPECTED THE AC AND REPLACED THE RT ENGINE. WITH ALL OPS CHECKS GOOD, THE AC WAS RETURNED TO SERVICE. (K) 2L72 4T4 TRTA24CE E26NE 20051031000932005103100093CE 2005 10 31 GUU2005F00042 120050820A2697 WIRE BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA EXTINGUISHER LOOSE A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO2969549 UE194 DURING FLIGHT, RT ENGINE FIRE EXTINGUISHER DISCHARGE LIGHT ILLUMINATED. SECURED FIRE EXTINGUISHER SQUIB WIRES IN RT WHEEL WELL. (SO29200508218) (K) 2L72 4T3 TRTA24CE E2NE 20051031000962005103100096EU 2005 10 31 KBM2005F00297 120051005A5340 MOUNT SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE BLOWER MOTOR BROKEN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19115SH951 99023 3141 7 INCH BLOWER MOTOR, UNIT HAS A BROKEN MOTOR MOUNT, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051031001012005103100101NM 2005 10 31 AMTA200500882 120051012A2612 FIRE LOOP BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE LT ENGINE MALFUNCTIONED A AMTAO OTHER N FALSE WARNING CRCRUISE 1 GL11552TZ 32586 EICAS STATUS MESSAGE INFLIGHT LT ENGINE FIRE LOOP 1. REMOVED AND REPLACED CONNECTOR IAW RRECMM. PERFORMED AMM 26-10-00 FIRE/OVERHEAT LOGIC SYSTEM TEST. CHECKED GOOD. (K) 2L72 4F4 FRTA2NM E12EU 20051031001152005103100115NM 2005 10 31 UIEA200500117 120050824A324026056623 BRAKE BOEING747 747271C 1384869NM GE CF6 CF650E2 30018NE LT MLG LEAKING A UIEAH DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 EA15537MC 22403 AFTER TAKEOFF, NR 4 HYD LOW QUANTITY LIGHT CAME ON. NR 4 SYSTEM WAS 1.5 GAL. SYSTEM WAS SHUTDOWN AND USED ONLY FOR LANDING. FOUND NR 8 BRAKE ASSY BLANKING PLATE MISSING AND LEAKING BAD. REMOVED AND REPLACED NR 8 BRAKE ASSY IAW MM. LEAK CHECK, OK. REPLACED NR 8 WHEEL ASSY DUE CONTAMINATED WITH HYD FLUID. (K) 2L74 4F4 F A20WE E23EA 20051031001242005103100124SW 2005 10 31 KBM2005F00271 120050915A291070061H00A180A LINE BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL HYD SYSTEM LEAKING E KBMAO OTHER K FLUID LOSS NRNOT REPORTED 1 WP1973DP 2513 IN-FLIGHT HYDRAULIC BOOST, INOPERATIVE. REPLACED LEAKING HYDRAULIC SUPPLY LINE FROM PUMP TO FILTER. (K) 1G71 3U3 U H2SW E4CE 20051031001252005103100125EU 2005 10 31 KBM2005F00273 120050911A21500500846 CONDENSER SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE AIR CON SYS INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19751H 975 3403 AC CONDENSOR WAS INOPERATIVE. REMOVED AND REPLACED WITH SERVICEABLE UNIT. (K) 1G71 3U3 U H9EU E19EU 20051031001262005103100126EA 2005 10 31 ASOA05678S 120050819A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE BS 559-605 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27839AS 7284 DURING C-CHECK, THE RT FLOOR SUPPORT WEB AT FS 559.112 TO FS 605 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED THE CORROSION ON THE RT FLOOR SUPPORT WEB AT FS 559.112 TO FS 605 BY COMPLYING WITH EO. (K) 2L72 4F4 FRTA21EA E15NE 20051031001342005103100134SW 2005 10 31 ALG2005F00065 120050824A7714407375002103 INDICATOR BELL 407 407 1182206SW ALLSN 250C 250C47B GL ENGINE FAILED E ALGAA UNSCHED LANDING P NO WARNING INDICATION TOTAKEOFF 1 SW03577AL 53247 ON TAKEOFF, NG INDICATOR PEGGED OUT. RETURNED TO BASE AND NOTIFIED MAINTENANCE. REMOVED AND REPLACED INDICATOR WITH SERVICEABLE UNIT. FUNCTIONAL CHECK OK. IAW MM. (K) 1G71 3U3 UO H2SW E1GL 20051031001462005103100146EU 2005 10 31 SFO2005F00001 120050727A29134005303 PUMP AMD FALC10FALCON10 2730101EU GARRTTTFE731TFE731* 01518WP NR 2 HYD SYS FAILED E SFOAO OTHER O OTHER NRNOT REPORTED 1 EA2377SF 58 141 AFTER LANDING, THE NR 2 HYDRAULIC LIGHT CAME ON AND THE NR 2 HYDRAULIC PRESSURE WENT TO -0- PSI. INVESTIGATION REVEALED THE NR 2 HYDRAULIC PUMP HAD FAILED. THE PUMP AND REQUIRED FILTERS WERE REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. THIS FAILED, OVERHAULED PUMP WAS A RECENT WARRANTY REPLACEMENT FOR PREVIOUS OVERHAULED PUMP THAT HAD FAILED WITH LOW (220 HRS) TSO. BOTH PUMPS WERE O/H BY SAME REPAIR STATION. THIS OPERATOR HAS NEVER SEEN THIS BRAND OF PUMP GO TO THE REQUIRED O/H INTERVAL (3,000 HRS). THESE PUMPS GENERALLY SEEM TO FAIL AROUND 700-900 HRS OFOPERATING TIME AS DERIVED FROM PREVIOUS AC RECORDS. (K) 2L72 4F4 F A33EU E6WE 20051031001492005103100149EU 2005 10 31 USAA051020 120050817A5310D5347209001100 BEAM AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FR 66 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19742US15033 1275 PIT - S1 - BEAM, .5 INCH X .5 INCH CORROSION; LEEL 1; TASK JA260-53500, FR 66 AT Y132MM. INSTALLED NEW BEAM IAW TYP REP. (K) 2L72 4F4 FRTA28NM E37NE 20051031001512005103100151 2005 10 31 KBM2005F00281 420050910A2312064105430 RADIO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE VHF SYSTEM MALFUNCTIONED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19966SH2114 3787 VHF RADIO HAS STATIC INFLIGHT. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051031001542005103100154SW 2005 10 31 HA42005F00000 120050828A5210269A475511 HINGE HUGHES269 269C1 8059504SW LYC O360 HIO360* 41514EA PAX DOOR BROKEN A HA4RO OTHER O OTHER NRNOT REPORTED 1 SO151565B292 0202 THE DOOR PIN PORTION OF THE HINGE, WHICH IS RESPONSIBLE RETAINING THE DOOR, BROKE. THIS LEAVES THE DOOR CONNECTED AT ONLY 1 POINT AND AN IN-FLIGHT FAILURE COULD POTENTIALLY ALLOW THE DOOR SEPARATE FROM THE AIRCRAFT. (K) 1G71 3O3 OO 4H12 1E10 20051031001572005103100157EU 2005 10 31 USAA051018 120050817A5315D5311281400200 FLOORBEAM AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19742US 1275 PIT - S1 - BEAM CORROSION; LEVEL 1; TASK JA-220-53500, C20-Y1292. REPLACED BEAM IAW SRM. (K) 2L72 4F4 FRTA28NM E37NE 20051031001612005103100161NM 2005 10 31 S2YA05045 120050721A24301030200 HED DORNERDO32 DO328300 NM PWA 306 PW306B NE LEFT FAILED A S2YAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL13359SK 3202 DURING FLIGHT, THE CREW REPORTED LT DC GEN AND FLAP CONTROL FAIL. FLAPS STUCK EXTENDED TO 3 DEGREES. THE CREW PERFORMED AN AIR-TURN-BACK. BRAKES USED HEAVILY ON LANDING AND BRAKE TEMP HIGH MESSAGE RESULTED. MAINTENANCE INSPECTED THE AC. THE LT DC GEN COULD NOT DUPLICATE THE PROBLEM. THE FLAP SYTEM AFTER RESETTING THE FLAP CONTROL UNIT COULD NOT DUPLICATE THE PROBLEM. WHILE INSPECTING THE BRAKES IT WAS DETERMINED THAT THE NR 1 BRAKE WAS WORN TO LIMITS. DURING A FLIGHT THE LT DC GEN FAILED AFTER CYCLING THE GEN THE GENERATOR OPS CHECKED GOOD. MAINTENANCE LATER ON, MAINTENANCE REPLACED THE LT HALL EFFECT DEVICE (HED) FOR TROUBLESHOOTING. (K) 2H72 4T4 FRTA55NM E35NE 20051031001632005103100163EU 2005 10 31 KBM2005F00305 120051006A2435150S6122Q STARTER GEN SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE ENGINE FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19351WM179 2167 INTERNAL FAILURE- ARMATURE, REPLACED STARTER GEN WITH OFF UNIT. (K) 1G71 3U3 U H9EU E19EU 20051031001692005103100169NM 2005 10 31 USAA051010 120050816A5343 SUPPORT BEAM BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU LT MLG CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US 23933 CLT - Q6 - LT MLG SUPPORT BEAM OB LUG FACE AND HEAVY WEAR/ MATERIAL LOSS ON IB LUG FACE 2 INCH X 2 INCH TYPICAL. LT MLG SUPPORT BEAM; STABILIZER BEAM FITTING ASSY. CLEANED AND TREATED CORROSION, INSTALLED BUSHINGS IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051031001702005103100170NM 2005 10 31 USAA051023 120050817A5320 INTERCOSTAL BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU BS 328-344 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19444US 24862 BFM - Q2 - FLOORBEAM INTERCOSTAL, .250 INCH CRACK, BET STA 328, 344 CABIN FLOORBEAM. INSTALLED REPAIR DOUBLER, TREATED AND PRIMED IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051031001802005103100180NM 2005 10 31 AMTA200500715 120050922A335020121 BATTERY BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE EMERGENCY LIGHT UNSERVICEABLE A AMTAK NONE O OTHER ININSP/MAINT 1 GL11514AT 27971 INTERIOR EMERGENCY FLOOR LIGHTING BETWEEN SEAT ROW 12 THROUGH 22 ARE DIM. REMOVED AND REPLACED BATTERY CHARGER AT L-2 DOOR IAW MM 33-51-07. OPS CHECKS GOOD. (K) 2L72 4F4 FRTA2NM E12EU 20051031001822005103100182NM 2005 10 31 AMTA200500824 120051010A2612 FIRE WARNING BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE FALSE INDICATIONA AMTAK NONE N FALSE WARNING ININSP/MAINT 1 GL11519AT 27975 FIRE PROTECTION SYSTEM FAIL LGT ILLUM EICAS MSG: FIRE/OVHT SYS DISPLAYED. EICAS STATUS MSG R TURB OH DET 1 AND 2 DISPLAYED. T/S ENG NR 2 OVERHEAT DETECTION SYSTEM IAW FIM. CHECK WIRING FROM FIRE DET CARD FILE TO OVERHEAT DETECTOR NR 1 AND NR 2. VISUALLY INSP WIRING, NO DEFECT FOUND. REMOVED AND REPLACED ENG OVHT DETECTOR SWITCH IAW WDM. (K) 2L72 4F4 FRTA2NM E12EU 20051031001852005103100185 2005 10 31 L7C2005F00000 420050718A2562AK450 ELT PIPER PA18 PA18150 7101828SO LYC O360 O360A1D 41514EA CABIN INOPERATIVE E L7CCO OTHER O OTHER NRNOT REPORTED 1 AL034144E873 187809084 ELT REMOTE WOULD NOT ACTIVATE. ELT LIGHT WOULD COME ON BUT DID NOT TRANSMIT. INSTALLED IN AC FOR LESS THAN 4 YEARS. (K) 1H71 3O3 O 1A2 E286 20051031001862005103100186NE 2005 10 31 ALG2005F00074 120050908A2435 SHAFT SKRSKYS76 S76 8143010NE TMECA ARRIUSARRIU2F NE STARTER GEN SHEARED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03702AL 1946 760243 DURING CRUISE FLIGHT, GENERATOR CAUTION ILLUMINATED AND WOULD NOT RESET. LANDED ON EI-120 AND NOTIFIED MAINTENANCE. STARTED/GENERATOR SHAFT FOUND SHEARED. REMOVED AND REPLACED STARTER/GENERATOR WITH SERVICEABLE UNIT IAW MM. (K) 1G72 3U3 U H1NE E34NE 20051031001952005103100195CE 2005 10 31 AKG2005F00000 120050906A324613685XL BEARING BEECH 200 B200 1152922CE PWA PT6 PT6* 52043EA LT MLG WHEEL FAILED E AKGAO OTHER O OTHER NRNOT REPORTED 1 CE0589WA 317 BB1540 BEARING ON WHEEL FAILED. THE BEARING WAS LOCATED ON THE LT MAIN LANDING GEAR ON THE IB WHEEL. THIS BEARING FAILURE SUBSEQUENTLY CAUSED THE WHEEL TO DEPART THE AIRFRAME. IT IS SUSPECTED THAT THE EVENT OCCURED ON LANDING. (K) 1L72 4T3 T A24CE E2NE 20051031002022005103100202CE 2005 10 31 AHD2005F00000 120050922A2120 BLOWER MOTOR CESSNA414 414A 2075907CE CONT O520 TSIO520NB 17040SO MCAULY3AF32C3AF32C* GL EVAPORATOR SMOKE E AHDAO OTHER O OTHER NRNOT REPORTED 1 EA13414AK5087 414A0321 521059 991467 AFTER A FLIGHT SEPT 22, 2005, ABOUT 1905 HRS, SMOKE WAS NOTED IN THE COCKPIT WHILE TAXING TO THE RAMP. FIRETRUCKS WERE REQUESTED BY THE PILOTS, THE AC WAS SHUTDOWN ON THE TAXI WAY AND PASSENGERS AND CREW WERE OFF-LOADED. THE FIRE CREW FOUND NO SIGNS OF HEAT AND THE AC WAS TOWED TO THE RAMP. UPON INSPECTION BY MAINTENANCE TECH, IT WAS DETERMINED THAT THE SMOKE HAD COME FROM THE RT EVAPORATOR BLOWER MOTOR. THE SYSTEM WAS DISABLED IAW THE AC MEL AND GROUND RUN REVEALED NO MORE SMOKE WAS BEING EMITTED. (EA09200505819) (K) 1L72 3O3 O A7CE E8CE 5 CP22EA 20051031002112005103100211SO 2005 10 31 B7T2005F00000 220050706A8530AEC631397 CYLINDER CESSNA207 207 2073602CE CONT O520 IO520F 17032SO HARTZLHCC3Y HCC3YF1 GL NR 5 CRACKED E B7TAO OTHER O OTHER NRNOT REPORTED 1 AL0391002 596 20700003 564011 EE2069A CYLINDER CRACKED UNDER UPPER SPARK PLUG HOLE ACROSS ENTIRE WIDTH OF CYLINDER AREA UNDER SPARK PLUG, LEAKING AIR. (K) 1H71 3O3 O A16CE E5CE 5 CP25EA 20051031002162005103100216EU 2005 10 31 KBM2005F00279 120050916A33404572 BULB SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE LANDING LIGHT INOPERATIVE B KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH 2884 LANDING LIGHT WAS INOPERATIVE. REPLACED WITH NEW BULB. (K) 1G71 3U3 U H9EU E19EU 20051031002222005103100222SO 2005 10 31 WWQ2005F00000 120051013A29101158P41718013P12LINE GULSTMG1159 GIV 3980115SO RROYCETAY TAY6118 EU HYDRAULIC SYS LEAKING E WWQAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP07823GA8190 1005 AFTER TAKEOFF, CREW WAS ALERTED THAT THE FLIGHT HYDRAULIC SYSTEM PRESSURE HAD FALLEN BELOW LIMITS, SOON AFTER THE CREW NOTICED THAT THE QUANTITY WAS NEAR EMPTY. CREW CALL MAINTENANCE FROM AC TO DISCUS THE PROBLEM AND THEY ALL AGREED TO LAND ENROUTE FOR MAINTENANCE. MAINT INSPECTED AC, AFTER AN OPERATIONAL CHECK, FOUND RT OR FLIGHT SIDE HYDRAULIC PUMP PRESSURE LINE WAS LEAKING. AFTER FURTHER INSPECTION OF THE PRESSURE LINE, FOUND THAT THE PERMASWAGE FITTING ON THE LINE WAS THE PROBLEM. A NEW LINE AND FITTING WERE ORDERED AND INSTALLED. FLIGHT HYDRAULIC SYSTEM WAS SERVICED AND A LEAK CHECK COMPLIED WITH. NO FURTHER LEAKS OR PROBLEMS NOTED. 2L72 4F4 FRTA12EA E25NE 20051031002302005103100230SO 2005 10 31 GUU2005F00046 120050830A3350 SOCKET EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE EMERGENCY LIGHT INOPERATIVE A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO17280AS 120231 ON POST FLIGHT, EMERGENCY FLOOR TRACK LIGHT AT TROW 9A WAS INOPERATIVE. REPOSITIONED BULB IN SOCKET. (K) 2L72 4T4 TRTA31SO E20NE 20051101000062005110100006WP 2005 11 1 05FDEA03573 120051028A5712 RIB DOUG DC10 DC1030 3023501WP LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 LEFT WING L/E INTERNAL STRUCTURE FOUND 1EA CRACK 0.25'' LONG ON RIB AT STA XORS 873. REPAIRED L/E FORMER PER SRM 57-20-00 FIG 1 SHT 6 VOL 1 AND SRM 51-35-01 PAG1-13 AND SRM 51-33-01 PAGE 34-47. 2L73 4F A22WE 20051101000082005110100008EA 2005 11 1 COMA0560569 120051026A2170P1096 COALESCER BAG CNDAIRCL600 CL6002B19 1900309EA ACM DIRTY A COMAGA O2 MASK DEPLOYED UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO01995CA 7229 STRONG OILY SMELL FUMES IN COCKPIT AND CABIN. REPLACED THE COALESCER SOCKS. NO FURTHER SMELL. 2L72 4F RTA21EA 20051101000112005110100011WP 2005 11 1 05FDEA03575 120051028A5310 DOOR FRAME DOUG DC10 DC1030 3023501WP L3 DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 IN CARGO COMPT JAMB L3 DOOR AT STA 1256 X 92 AND Z 61 FOUND PLATE IN THE UPPER SECTION OF JAMB WITH 1 CRACK 0.5"LONG. REPAIRED CRACK IAW SRM 53-50-00 FIG 19 VOL 1. FAB PART IAW DETAIL PART TRAVELER N01158. 2L73 4F A22WE 20051101000142005110100014EA 2005 11 1 COMA0560570 120051026A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS UNRELIABLE A COMAO OTHER J WARNING INDICATION LDLANDING 1 SO01735CA5529 2468 7267 FLIGHT 5267 - FLAPS FAIL CAUTION. REPLACED THE RT BPSU. 2L72 4F RTA21EA 20051101000232005110100023NM 2005 11 1 QXEA200501390 120051028A29105114904 PTU BOMBDRDHC8 DHC8402 1390042NM HYD SYSTEM MALFUNCTIONED A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09401QX25 4031 BOI FLIGHT NR 2391 - LOUD BUZZING SOUND COMING FROM THE CABIN. BUZZING STOPPED WHEN POWER TRANSFER UNIT WAS TURNED OFF. MAINTENANCE REMOVED AND REPLACED PTU IAW AMM 29-11-61, PG 401-407, 501-503. BLED AND SERVICED NR 1 AND NR 2 HYD SYSTEM. GROUND CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE 2H72 4T RTA13NM 20051101000282005110100028NM 2005 11 1 SWAA053392 120051028A3350101073 LENS BOEING737 7373K2 13844BANM L1 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29340LV 23738 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM. 2L72 4F RTA16WE 20051101000302005110100030NM 2005 11 1 SWAA053394 120051028A53306545768 SKIN BOEING737 7373K2 13844BANM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29340LV 23738 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT, AFT LOWER CORNER. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051101000332005110100033 2005 11 1 SWAA053397 420051028A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29384SW 26590 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051101000342005110100034NM 2005 11 1 SWAA053398 120051028A5753 SKIN BOEING737 7373H4 1384600NM LT WING FOREFLAPDELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29384SW 26590 DURING SCHEDULED C4 CHECK, FOUND LT WING INBD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM. 2L72 4F RTA16WE 20051101000382005110100038WP 2005 11 1 IXXA05SMN251S 120051013A5330 SKIN PANEL DOUG DC8 DC871F 302199DWP BS 70 BROKEN B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING C CHECK INSPECTION, LT FUSELAGE NOSE SECTION LWR PLATING UPPER AFT CORNER BROKEN OFF AT BS 70 L-33. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-2 FIG 8C-2, TR NR 53-176, EO SEMAN NR 20051299 DATED 09-29-05. PERFORMED DETAIL VISUAL INSPECT. NEITHER CRACK NOR CORROSION FOUND. FABRICATED REPAIR DOUBLER IAW DC8 SRM 53-2-5 FIG 8C-2, DC8 SRM 53-2-5 FIG 8B-2, DC8 SRM 53-3-1 FIG 1 ITEM A, DC 8 SRM 53-4-1 FIG 1 ITEM C, DC8 SRM 51-9-0 FIG 68A. INSTALLED REPAIR DOUBLER IAW DC8 SRM 53-2-5 FIG 8C-2, DC8 SRM 51-1-20D, DC8 SRM 51-3-1. 2L74 4F RT4A25 20051101000422005110100042NM 2005 11 1 SWAA053405 120051030A53306545890 BEAR STRAP BOEING737 7373H4 1384600NM L2 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED D CHECK, FOUND FUSELAGE BEAR STRAP CRACKED AT L2 DOOR CUTOUT, LOWER FWD CORNER. REPAIRED BEAR STRAP PER SRM. 2L72 4F RTA16WE 20051101000442005110100044NM 2005 11 1 SWAA053407 120051030A53116546529 FRAME BOEING737 7373H4 1384600NM BS 440 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 440, FWD CARGO DOOR CUTOUT. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20051101000492005110100049WP 2005 11 1 05FDEA03539 120051027A5730 SKIN DOUG DC10 DC1030 3023501WP RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 RT WING EXT L/E, CRACK LONG 0,5'' ON EXT SKIN AT STA XORS 804. REPAIRED CRACK PER SRM 57-00-01 FIG 4 SHT 2 VOL 1 AND SRM 51-33-01 PAGE 34-47 FABRICATED PART IAW DETAIL PART TRAVELER F161055/N01055 PER SRM 57-00-01 FIG 4 SHT 2 VOL 1. 2L73 4F A22WE 20051101000522005110100052WP 2005 11 1 ABXA050260 120051010A533099234343 SKIN DOUG DC9 DC941 302207NWP PWA JT8 JT8D1 52044NE BS 579 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23962AX 47768 FUSELAGE SKIN BULGED AT STA 579, LONERON 30, EVIDENCE OF CORROSION INTERNAL. REMOVED INTERNAL CORRODED DOUBLER / INSTALLED NEW DOUBLER IAW SRM. 2L72 4F4 F A6WE E2EA 20051101000612005110100061NM 2005 11 1 05FDEA03513 120051026A5753651920612 FLAP TRACK BOEING727 7272S2F 1384O81NM NR 6 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25213FE 22935 NR 6 FLAP TRACK HAS CORROSION ON AFT MOUNT PAD. REPLACED FLAP TRACK WITH SERVICEABLE FLAP TRACK IAW MM 27-51-031-4. 2L73 4F A3WE 20051101000632005110100063NM 2005 11 1 05FDEA03509 120051026A5230 DOOR BOEING727 72725C 138400HNM CARGO BAY OPEN A FDEAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 SO25136FE 19855 AFTER DEPARTURE, AIRCRAFT WOULD NOT PRESSURIZE. RAN QRH AND NO SUCCESS. APPLIED SYSTEMS KNOWLEDGE AND COULD NOT SOLVE PROBLEM. RETURNED TO MEMPHIS. AFTER BLOCK-IN TO MEMPHIS, AND A VISUAL INSPECTION, FOUND AFT CARGO DOOR OPEN, AND FAIRING DOOR CLOSED. SUSPECT NO INDICATION IN COCKPIT DUE TO AFT CARGO DOOR WARNING SWITCH STUCK CLOSED. CLEANED SWITCH PER 727 M/M REF SMP'S AND CYCLED DOOR SEVERAL TIMES. ALL INDICATIONS NORMAL. OK TO CONTINUE. 2L73 4F A3WE 20051101000682005110100068CE 2005 11 1 DXTA200501038 120051027A281099145053 FLOAT VALVE CESSNA750 750 2076810CE ALLSN AE300 AE3007A GL FUEL CELL FAILED E DXTAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL07956QS572 7500156 IN FLIGHT ,WING TANK OFULL R AMBER CAS MESSAGE ILLUMINATED AT FL290 SHORTLY AFTER LEVELING OFF. THE APPROPIATE CHECKLIST WAS COMPLETED FUEL VENTED OUT OF R WING FOR 3 MINUTES (LOST 150 LBS).THEN MESSAGE WENT OUT 2 MINUTES LATER (TOTAL FUEL 4900 LBS/L TANK 2350/CTR TANK 0/R TANK 2550/REPEAT WRITE UP. - REMOVED AND REPLACED OUTBOARD VENT FLOAT VALVE AND REMOVED AND REPLACED INBOARD VENT VALVE. I.A.W. 750 M/M 28-10-04 OPERATIONAL AND LEAK CHECK GOOD. 2L72 4J4 FRTT00007WITE6CH 20051101000692005110100069NM 2005 11 1 05FDEA03548 120051027A5322 SHEAR TIE BOEING727 727100 1384036NM BS 990 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 CORROSION ON SHEAR TIE BS 990 LBL 3 WL 148. REPAIRED PER SRM 53-10-2 2L73 4F RTA3WE 20051101000702005110100070NM 2005 11 1 05FDEA03549 120051027A5320 SUPPORT BOEING727 727100 1384036NM BS 1107 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 CORROSION AFT CARGO BAY CEILING SUPPORT BS 1107 RBL 6 WL 200. REPAIRED PER SRM 53-10-1 2L73 4F RTA3WE 20051101000712005110100071NM 2005 11 1 05FDEA03551 120051027A5311 FAILSAFE BOEING727 727100 1384036NM BS 990 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 N01348 BS 990 FRAME IS CRACKED TWO PLACES AT STRINGER 25 LT. REPAIRED PER SRM 51-40-3 2L73 4F RTA3WE 20051101000722005110100072NM 2005 11 1 05FDEA03448 120051018A5315 FLOORBEAM BOEING727 727100 1384036NM BS 295 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 N00474 E&E BAY FLOORBEAM WEB BS 295 LBL 30 WL 200 CRACK EXTENDING UP FROM STOP DRILL. STOP DRILLED CRACK AND REPAIRED WEB AT CRACK IN E&E BAY FLOORBEAM WEB BS 295 LBL 30 WL 200 IAW SRM 51-10-1 AND SRM 51-40-2 2L73 4F RTA3WE 20051101000732005110100073NM 2005 11 1 05FDEA03450 120051018A2611774001 SMOKE DETECTOR BOEING727 727200 138407ENM CARGO BAY FAILED A FDEAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO25208FE 22930 ON CLIMB OUT GOT NR 6 MAIN CARGO SMOKE LIGHT AND FIRE BELL. PERFORMED EMERGENCY PROCEDURES PER QRH. AT 500 AGL THE LIGHT WENT OUT AND THE SYSTEM TESTED OK. R & R NR 6 DETECTOR AND MAIN CARGO SMOKE DETECTOR MODULE PER 727-200 MM 26-16-011-4 AND 26-16-000-5. 2L73 4F RTA3WE 20051102000042005110200004NM 2005 11 2 05FDEA03349 120051011A5712ARB293113 RIB DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 LEFT HAND WING FIXED LEADING EDGE INTERNAL RIB ANGLE FOUND CRACKED AT XORS 482. CRACKED INTERNAL RIB ANGLE AT LEFT HAND WING FIXED LEADING EDGE XORS 482 REMOVED AS PER SRM 51-31-01 VOLUME II. NEW RIB ANGLE FABRICATED AS PER DRAWING ARB2931 AND INSTALLED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051102000052005110200005NM 2005 11 2 05FDEA03351 120051011A57306AL4V0020 DOUBLER DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 LT WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT XORS 628. FASTENERS AT LT WING FIXED LEADING EDGE CRACKED INTERNAL BEADED DOUBLER AT XORS 628 REMOVED AS PER SRM 51-31-01 VOLUME II. REPAIR DOUBLER FABRICATED AS PER SRM 57-10-00 FIGURE 25 VOLUME I AND INSTALLED AS PER SRM 51-35-01 VOLUME II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051102000082005110200008NM 2005 11 2 05FDEA03345 120051011A5712ARB39547 RIB DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 LT WING FIXED LEADING EDGE INTERNAL RIB DOUBLER FOUND CRACKED AT XORS 562. CRACKED INTERNAL RIB DOUBLER AT LT WING FIXED LEADING EDGE XORS 562 REMOVED AS PER SRM 51-31-01 VOLUME II. NEW RIB DOUBLER FABRICATED AS PER DRAWING ARB 3954 AND INSTALLED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051102000112005110200011NM 2005 11 2 2005UALA01082 120051004A339759193 WIRE BOEING757 757222 1384956NM PWA 2037 PW2037 NE ROWS 9-12 DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29519UA 24872 EEL FLOOR STRIP BETWEEN SEAT ROWS 9 AND 12 IS INOP. REPAIRED EEL JUMPER CABLE. 2L72 4F4 FRTA2NM E17NE 20051102000132005110200013NM 2005 11 2 2005UALA01087 120051005A5320 SILL BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29643UA 25093 FWD PIT LWR DOOR SILL AT APPROX RBL 40 IS CORRODED. STRAP WAS REPLACED. 2L72 4F4 FRTA1NM E24NE 20051102000192005110200019EU 2005 11 2 USAA051217 120051019A5315D534720900100 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19738US 1254 AT SPLICE PLATE Y1292 FR 66 TO 68 FLOORBEAM; CORROSION LEVEL 1; TASK JA-260-53500. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-72-11, DEFECT SIZE: .030 TO .060 INCH DEEP. 2L72 4F RTA28NM 20051102000212005110200021EU 2005 11 2 USAA051219 120051019A5315 FLOORBEAM AIRBUSA319 A319112 3930323EU FR 66 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19738US 1254 LEFT AFT ENTRY SILL BEAM (FR 66 & Y1492) HAS CORROSION. DOUBLERS INSTALLED PER SRM 53-41-14, DEFECT SIZE: 1.5 X 1 INCH AREA. 2L72 4F RTA28NM 20051102000232005110200023NM 2005 11 2 USAA051221 120051019A5320US69412267LF ANGLE BOEING737 737301 1384611NM BS 907-1006 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19592US 23937 STA 907 TO 1006; NO TASK OF LEVEL, CORROSION. FABRICATED PART PER TR 549929, DWG 6941226, SRM 51-40-02, 53-60-15, DEFECT SIZE: 2L X 0.5W X .049 INCH DEEP. 2L72 4F RTA16WE 20051102000242005110200024NM 2005 11 2 USAA051222 120051019A5320141N51612 WEB BOEING757 7572B7 1384964NM BS 397-418 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19619AU 27198 STA 397-418 RBL 63 WL 208.10; LEVEL 1 CORROSION; TASK C53-222-03. REMOVED & INSTALLED NEW FLOOR WEB PER SRM 53-00-51, 51-40-02, DEFECT SIZE: 4.6 X 1.5 X 0.044 INCH. 2L72 4F RTA2NM 20051102000262005110200026NM 2005 11 2 USAA051225 120051019A5320146N871227LF SUPPORT BOEING757 7572B7 1384964NM BS 1675 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19619AU 27198 STA 1675 UNDER DOOR 4L THRESHOLD LBL 62; LEVEL 1 CORROSION; TASK C53-251-03. REMOVED & REPLACE SUPPORT, FABRICATED PART PER SRM 53-60-15, 51-10-02, 51-40-02, DWG 146N8712, DEFECT SIZE: .5" W X 2.0"L X .063"D. 2L72 4F RTA2NM 20051102000282005110200028NM 2005 11 2 SB05135 120051020A3397 WIRE BOEING737 7373B7 1384580NM EMERGENCY LIGHT DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19512AU 23595 MAINTENANCE REPORTED THE SEAT MOUNTED EMERGENCY LIGHT AT SEAT 14ABC INOPERATIVE. MAINTENANCE REPAIRED THE WIRING AT SEAT 14ABC. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20051102000292005110200029NM 2005 11 2 SB05136 120051021A21307110025 SELECTOR PANEL BOEING737 7373B7 1384580NM CABIN PRESSURE STICKS A USAAG O2 MASK DEPLOYED O OTHER CRCRUISE 1 EA19512AU9241192411 23595 DURING CRUISE, AT FL350, NOTICED CABIN ALT STARTED TO CLIMB. CREW DONNED OXYGEN MASKS & STARTED DESCENT. PAX O2 MASKS DROPPED AT FL140. STANDBY PRESSURIZATION DID NOT WORK, F/O SWITCHED TO MANUAL. AFTER CABIN ALT RESTORED, F/O SWITCHED BACK TO STANDBY & IT WORKED. SINCE STANDBY & MANUAL METHODS NOW BOTH WORKED, CREW AGREED TO CONTINUE ONTO PHL. FLT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY DECLARED. MX FOUND CABIN PRESSURE SELECTOR PANEL OUTFLOW VALVE OPEN/CLOSE SWITCH STICKS INTERMITTENTLY. REPLACED PANEL PER MM 21-31-00. 2L72 4F RTA16WE 20051102000302005110200030EU 2005 11 2 SA05110 120051020A335032145510 EPSU AIRBUSA321 A321211 3930370EU EMERGENCY LIGHT FAULTY A USAAK NONE L NO TEST ININSP/MAINT 1 EA19172US16169 1472 DCA - THE EMERGENCY POWER SUPPLY UNIT AT THE MID LEFT POSITION FAILED THE SYSTEM TEST. MAINTENANCE REPLACED THE MID LEFT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY TESTED OK. 2L72 4F RTA28NM 20051102000322005110200032NM 2005 11 2 UPS05445664 120051026A7110 COWLING BOEING747 747123 1384873NM PWA JT9 JT9D3 52050NE NR 4 OPEN A IPXAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO01676UP 20101 N/A RTO BTB NR 4 ENG OB CORE COWL OPEN ON TAKE-OFF ROLL. REPLACED OB NR 4 ENG CORE COWLS PER MM 71-10-00. 2L74 4F4 F A20WE E20EA 20051103000032005110300003NM 2005 11 3 05FDEA03564 120051028A5313AFA71271 LONGERON DOUG MD11 MD11 3023602NM BS 1641-1661 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 FOUND CENTER CARGO COMP, AFTER REMOVAL OF CRACKED LONGERON SPLICE AT STA 1641 TO 1661 LONGERON 44R FOR REPLACEMENT, LONGERON 44R FOUND CRACK AT STA 1652 TO 1658. REPAIRED AS PER SRM 53-10-01. 2L73 4F RTA22WE 20051103000162005110300016NM 2005 11 3 SB05141 120051030A3350110049 CHARGER BOEING737 7373B7 1384580NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19395US 23317 CLT - MAINTENANCE REPORTED THE AFT CABIN SEAT/AISLE EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT BATTERY CHARGER AND BATTERY. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20051103000292005110300029NM 2005 11 3 USAA051286 120051101A5313 STRINGER BOEING737 7373B7 1384580NM BS 907 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND STRINGER SPLICE CORRODED, STA 907, S4L. REMOVED AND REPLACE WITH NEW PART IAW SRM 51-10-02, DEFECT SIZE: .250" CRACKS AT TWO RIVET HOLES. 2L72 4F RTA16WE 20051103000442005110300044EU 2005 11 3 USAA051316 120051101A5320D5348004320501 SILL AIRBUSA319 A319112 3930323EU FR 66 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19741UW 1269 FOUND CORROSION, RT AFT DOOR SILL AT FR 66; CORROSION LEVEL 2; TASK JA-260-53500. REMOVED AND REPLACED SILL PER SRM 51-40-00, DEFECT SIZE: 0.500" BY 0.500" BY 0.060" DEEP. 2L72 4F RTA28NM 20051103000472005110300047NM 2005 11 3 USAA051261 120051031A5320 INTERCOSTAL BOEING737 7373B7 1384580NM BS 312-328 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND INTERCOSTAL AT BS 312-328 LBL 12. REPLACED STIFFENER IAW BOEING DWG 65-45834, DEFECT SIZE: 2" BY 2". 2L72 4F RTA16WE 20051103000482005110300048NM 2005 11 3 USAA051273 120051031A5311 FRAME BOEING737 7374B7 1384702NM BS 867 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19779AU 24996 FOUND FRAME CORRODED AT STATION 867 BETWEEN S27L AND S27R. REMOVED MINOR CORROSION AND THREE FASTENERS IN THE AREA. INSTALLED NEW FASTNERS IAW SRM 53-00-07, DEFECT SIZE: .4" BY .2". 2L72 4F RTA16WE 20051103000492005110300049NM 2005 11 3 USAA051288 120051101A5313 STRINGER BOEING737 7373B7 1384580NM BS 1016 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND STRINGER CORRODED, S26R, STA 1016. REPLACED STRINGER SECTION AND BULKHEAD FITTING IAW SRM 51-10-02, DEFECT SIZE: .75" BY 3" STRINGER HAS A CORRODED AREA. 2L72 4F RTA16WE 20051103000512005110300051NM 2005 11 3 USAA051301 120051101A5320US141N516046LF FLOOR SUPPORT BOEING757 7572B7 1384964NM BS 312-324 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19626AU 27303 FOUND FLOOR SUPPORT CORRODED, STA 312-324 RBL 43. FAB PART PER MAE TRAVELER T5/551155 AND SRM 51-40-02, 53-00-51, 51-40-05, 51-20-02, DEFECT SIZE: 1"L BY 1" W BY 0.032"D. 2L72 4F RTA2NM 20051103000532005110300053EU 2005 11 3 USAA051314 120051101A5315D5347209005 FLOORBEAM AIRBUSA319 A319112 3930323EU FR 66 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19741UW 1269 FOUND FRAME CORRODED, -Y292 AND FRAME 66; CORROSION LEVEL 1; TASK JA-160-53500. REMOVED AND REPLACED BEAM PER SRM 51-72-11, DEFECT SIZE: .060" D BY 1" BY 3". 2L72 4F RTA28NM 20051104000052005110400005NM 2005 11 4 USAA051274 120051031A5315 FLOORBEAM BOEING737 7374B7 1384702NM STATION 1016 RIGCORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19779AU 24996 FOUND FLOORBEAM CORRODED, STATION 1016 RIGHT. REMOVED MINOR CORROSION TREATED AND PRIMED IAW SRM 53-60-01, DEFECT SIZE: 1" BY 4". 2L72 4F RTA16WE 20051104000072005110400007NM 2005 11 4 USAA051270 120051031A5310 STRUCTURE BOEING737 7374B7 1384702NM BETWEEN BS 380 ACRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19779AU 24996 UPPER CHORD CORRODED BETWEEN BS 380 AND BS400 AT BL0. REMOVED AND REPLACED UPPER CHORD IAW SRM 51-10-02 BOEING DWG 69-35365, DEFECT SIZE: 1.5". 2L72 4F RTA16WE 20051104000132005110400013EU 2005 11 4 SF200510261 120051026A2780 SLAT SYSTEM EMB ERJ170ERJ170100LR EU GE CF34 CF34* NE LE SLATS MALFUNCTIONED A UHLAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 GL17640RW 17000058 RECEIVED SLAT FAIL MESSAGE ON EICAS DECLARED EMERGENCY AND PERFORMED EMERGENCY LANDING. FOLLOWED QRH AND SLATS DID NOT MOVE AND FLAPS WENT TO 2 DEG. REMOVED AND REPLACED NR 2 S/F ACE IAW MM 27-53-02. PERFORMED OPS CHECK IAW MM 27-50-00 AND 27-80-00. OPS CHECK GOOD. NO FAULTS NOTED AT THIS TIME. OK FOR SERVICE. 2L74 4F4 FRTA56NM E15NE 20051104000152005110400015NM 2005 11 4 2005UALA01178 120051022A5330 SKIN AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE SKIN & STR AFT ODAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29843UA 1573 LEFT EXTERNAL FUSELAGE SKIN & STRINGER AFT OF STA 897 FRAME 23 BETWEEN STR 22L & 23L IS DAMAGED. MAJOR REPAIR ACP ON LH EXTERNAL FUSELAGE SKIN AFT OF STA 897 FR 23 BETWEEN STR 22L AND 23LH PER SRM 53-00-11 FIG 220. 2L72 4F4 FRTA28NM E40NE 20051104000162005110400016NM 2005 11 4 2005UALA01179 120051021A5270 TARGET BOEING777 777222 1385219NM PWA PW4077PW4077 NE CARGO DOOR OUT OF ALIGNMENTA UALAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 WP29778UA 26940 EICAS MSG FOR FORWARD CARGO DOOR OPEN. INSPECTED DOOR WHEN AIRCRAFT ARRIVED AND FOUND TARGETS NOT ALIGNED. DOORS WERE CYCLED: DOOR LATCHES AND TARGETS ARE ALIGNED. MESSAGE IN MAT IS NOT ACTIVE. NO LOSS OF PRESSURE. 2L72 4F4 FRTT0001SE E46NE 20051104000172005110400017NM 2005 11 4 2005UALA01180 120051023A2120 SMOKE BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN DETECTED A UALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP29175UA 24382 ELECTRICAL SMOKE IN CABIN. 2L74 4F4 FRTA20WE E24NE 20051104000222005110400022EU 2005 11 4 2005UALA01185 120051024A3350 LIGHT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE DOOR LEFT FWD MALFUNCTIONED A UALAO OTHER L NO TEST ININSP/MAINT 1 WP29407UA 456 LEFT FWD EMERGENCY EXIT DISPLAYED ON UPPER ECAM SCREEN, DOOR. REPLACED FWD EMER BATTERY. 2L72 4F4 FRTA28NM E40NE 20051104000242005110400024NM 2005 11 4 2005UALA01187 120051025A3350 LIGHT BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29315UA 23947 EMERGENCY FLOOR PATH EXIT LIGHTING INOP AT ROW 15 AFT. REPLACED EEL POWER STRIP AND MOST AFT LIGHT ASSY. 2L72 4F4 FRTA16WE E21EU 20051104000252005110400025NM 2005 11 4 2005UALA01188 120051025A3350 LIGHT BOEING777 777222 1385219NM PWA PW4077PW4077 NE CABIN DISLODGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29780UA 26944 EEL LIGHT AT 1F HAS FALLEN OFF. REPLACED FOWARD EEL LIGHT AT 1F. 2L72 4F4 FRTT0001SE E46NE 20051104000752005110400075NM 2005 11 4 SWAA053374 120051026A53306545774 SKIN BOEING737 7373H4 1384600NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 760, STR 18L. REPAIRED SKIN IAW SRM. 2L72 4F4 FRTA16WE E2GL 20051104000772005110400077 2005 11 4 SWAA053376 420051027A256563550 SLIDE BOEING737 7377H4 1384404NM GE CFM56 CFM56* 13802NE R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29434WN 32454 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE IAW MM. 2L72 4F4 FRTA16WE E2GL 20051104000792005110400079NM 2005 11 4 SWAA053378 120051027A5313BAC1498 STRINGER BOEING737 7375H4 138449DNM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29502SW 24179 DURING SCHEDULED MAINTENANCE, FOUND FUSELAGE STRINGER DAMAGED AT BS 482, STR 3R. REPAIRED STRINGER IAW SRM. 2L72 4F4 FRTA16WE E2GL 20051104000812005110400081NM 2005 11 4 SWAA053380 120051027A5315BAC15171489 FLOORBEAM BOEING737 7373H4 1384600NM GE CFM56 CFM56* 13802NE COCKPIT FLOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED D CHECK, FOUND COCKPIT FLOOR Z-CHORD CORRODED AT BS 270, BETWEEN RBL 11 TO LBL 11, WL 208. REMOVED AND REPLACED Z-CHORD IAW SRM. 2L72 4F4 FRTA16WE E2GL 20051104000832005110400083NM 2005 11 4 SWAA053382 120051026A2710KP23BSNJC BEARING BOEING737 7373H4 1384600NM GE CFM56 CFM56* 13802NE CENTER BOX BINDING A SWAAO OTHER O OTHER TXTAXI/GRND HDL 1 SW29635SW 27708 SHUDDERING AND BINDING FELT IN AILERONS DURING FLIGHT CONTROL CHECK. REMOVED AND REPLACED AILERON CENTERING MECHANISM ROLLER BEARING IAW MM. 2L72 4F4 FRTA16WE E2GL 20051104000852005110400085NM 2005 11 4 SWAA053384 120051027A53306518420 SKIN BOEING737 7377H4 1384404NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29709SW 27843 FUSELAGE SKIN CRACKED AT BS 235.8, EXTERNAL GROUND POWER DOOR CUTOUT. REPAIRED SKIN IAW EA. 2L72 4F4 FRTA16WE E2GL 20051104000882005110400088NM 2005 11 4 SWAA053437 120051101A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500, STR 16R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051104000902005110400090NM 2005 11 4 SWAA053439 120051102A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM CABIN FLOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FLOORBEAM UPPER CHORD CORRODED AT BS 312, BETWEEN LBL 10 TO RBL 32, WL 208. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20051104000922005110400092NM 2005 11 4 SWAA053441 120051102A53226545805 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 277, STR 11L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051104000942005110400094NM 2005 11 4 SWAA053443 120051102A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM AFT CARGO CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 986, STR 20L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051104000962005110400096NM 2005 11 4 SWAA053445 120051102A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM AFT CARGO CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 927, STR 21L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051104000982005110400098NM 2005 11 4 SWAA053424 120051101A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 704, STR 11R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051104001002005110400100NM 2005 11 4 SWAA053426 120051101A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM AFT CARGO CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 927, STR 25R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051104001022005110400102NM 2005 11 4 SWAA053428 120051101A5754 SKIN BOEING737 7373H4 1384600NM LT WING SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29375SW 26583 DURING SCHEDULED 1/4D CHECK, FOUND NR 1 L/E SLAT LOWER T/E SKIN CRACKED. REPAIRED SLAT PER SRM. 2L72 4F RTA16WE 20051104001042005110400104NM 2005 11 4 SWAA053430 120051101A53206582671 WEB BOEING737 7373H4 1384600NM LT MLG W/W CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED D-CHECK, FOUND LT MLG W/W WEB CRACKED AT BS 663.75, RBL 16, WL 180. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20051104001062005110400106NM 2005 11 4 SWAA053432 120051030A5313BAC1498 STRINGER BOEING737 737317 138447PNM E & E COMPART CORRODED A SWAAO OTHER O OTHER NRNOT REPORTED 1 SW29686SW 23175 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 360, STR 26R. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20051104001082005110400108NM 2005 11 4 SWAA053434 120051031A53306545777 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29687SW 23388 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 954, STR 21L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051104001162005110400116WP 2005 11 4 MWEA050120 120051029A3260833605 PSEU DOUG DC9 DC981 3022081WP LANDING GEAR INOPERATIVE A MWEAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 GL31805ME 48031 GEAR EXTENDED UPON SELECTING FLAPS BEYOND 28 DEGREES, THE GEAR WARNING CAME ON AND STAYED ON. COULD NOT DUPLICATE DISCREPANCY, PERFORMED A FULL FUNCTION CHECK OF LANDING GEAR POSITION WARNING SYSTEM. REMOVED AND REPLACED PROXIMITY SENSING ELECTRONICS UNIT FOR PRECAUTIONARY PURPOSES. 2L72 4F A6WE 20051104001192005110400119SO 2005 11 4 MASA200500488 120050624A2710701700082430 CONTROL CABLE EMB 145 EMB145LR 3260212SO AILERONS LOCKED A MASAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 SW07846MJ2304 145507 ABORTED TAKEOFF AT 40 KTS. AILERON CONTROLS LOCKED, PILOT'S COULD NOT MOVE BOTH CONTROL COLUMNS. MAINTENANCE REPLACED IC600 AND AILERON CABLE FAINLADS. 2L72 4T RTT00011AT 20051104001212005110400121SO 2005 11 4 MASA200500443 120050604A2720 BUSHING EMB 145 EMB145LR 3260212SO RUDDER MISSING A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07855MJ7786 7786 145614 REPORTED AN AIRFRAME VIBRATION INBOUND FROM CHA. MX FOUND THE RUDDER MOUNT BUSHINGS MISSING AND THE MOUNT BADLY WORN. AOG FOR PARTS COMING FROM FLL DUE TO ARRIVE AT APPROX 1828L. MX R2 RUDDER ON 6/6. 2L72 4T RTT00011AT 20051104001292005110400129NM 2005 11 4 200515 120051026A7712SEDL002S INDICATOR DHAV DHC8 DHC8103 1386005NM PWA PW121 PW121 52124NE TORQUE FLUCTUATES A KPVAO OTHER J WARNING INDICATION CRCRUISE 1 WP13809WP 032 ROUGH NR 2 ENG, TQ FLUCTUATION +/-2 PERCENT NON-STOP, CONTINUOUS. REMOVED AND REPLACED NR 2 ENGINE TORQUE GAUGE IAW MM CHAP. 77-10-00 PG. 201-202. NOTE: SUBSEQUENT TEST FLIGHT GOOD. 2H72 4T4 TRTA13NM E20NE 20051104001312005110400131WP 2005 11 4 IXXA05SMN241S 120051013A5730 DOUBLER DOUG DC8 DC871F 302199DWP XFS 250.000 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING ROUTINE C CHECK INSPECTION, RT INNER WING CTR L/E INTERNAL DOUBLER CRACK 3 AT STA XFS 250.000. REMOVED CRACKED INTERNAL DOUBLER IAW DC8 SRM 51-1-21. FABRICATED NEW INTERNAL DOUBLER (AL7075T6 0.063”) IAW DC8 SRM 57-3-1 FIG 3. CLEANED, TREATED, PRIMED AREA, DOUBLER IAW DC8 SRM 51-1-8B. INSTALLED NEW INTERNAL DOUBLER IAW DC8 SRM 51-1-21. 2L74 4F RT4A25 20051104001332005110400133WP 2005 11 4 IXXA05SMN190S 120050922A5330 RIVET DOUG DC8 DC871F 302199DWP FS 55.000 IMPROPER B IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW11829BX896722998 45994 DURING C CHECK INSPECTION, FWD LWR FUSELAGE BELLY, STA FS 545.000 L-35.75R, UPGRADE REPAIR DOUBLER TO INCORPORATE A MIN OF 3 ROWS OF RIVETS. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 # 05447 DATED 10-05-05, SEMAN DWG # ED-4061 DATED 09-27-05, EO SEMAN # 20051196 DATED 10-05-05. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D, DC8 SRM 51-3-0. REMOVED DAMAGED SECTION IAW SEMAN DWG # ED-4061. NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D REPAIR DOUBLER (AL7075T6 0.100”), INTERNAL FINGER DOUBLER (AL7075T6 0.032”) IAW SEMAN DWG # ED-4061, DC8 SRM 51-1-4 PG 1 (FORMING). CLEANED, TREATED, PRIMED AREA, REPAIR PARTS IAW DC8 SRM 51-1-82L74 4F RT4A25 20051104001352005110400135WP 2005 11 4 IXXA05SMN203S 120050927A5340 FITTING DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE 857.000 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING ROUTINE C CHECK INSPECTION, MAIN CARGO COMPT. AFT FITTING CRACKED 1, STA 857.000 L-19LREMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1. (TORQUE) 2L74 4F4 FRT4A25 E2GL 20051104001372005110400137WP 2005 11 4 IXXA05SMN222S 120050929A5730 SKIN DOUG DC8 DC871F 302199DWP XW255.000 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING C CHECK INSPECTION, NR 3 RT STUB WING LWR SKIN CRACK 2 AT STA XW 255.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-1 FIG 37, EO SEMAN NR 20051284 DATED 09-27-05. REMOVED FASTENERS IAW DC8 SRM 51-1-20D. REMOVED CORROSION IAW DC8 SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW DC8 SRM 57-2-1 FIG 2G. FAB`D REPAIR DOUBLER (AL7075T6 0.125”) IAW DC8 SRM 57-2-1 FIG 37. TAPERED DOUBLER FROM 0.125” TO 0.050” IAW DC8 SRM 57-2-1 FIG 37 NOTE 7. CLEANED, TREATED AND PRIMED AREA, REPAIR DOUBLER IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACE IAW DC8 SRM 51-1-11 PG 9. INSTALLED REPAIR DOUBLER IAW DC8 SRM 57-2-1 FIG 37, DC8 SRM 51-1-20D, DC8 SRM 51-3-1. 2L74 4F RT4A25 20051104000122005110400012NM 2005 11 4 USAA051264 120051031A5347 SEAT TRACK BOEING737 7373B7 1384580NM LBL 45 BS 494 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND SEAT TRACK CORRODED, LBL 45 BS 494. BLENDED WITHIN LIMITS IAW SRM 53-00-52, DEFECT SIZE: 1" BY 2". 2L72 4F RTA16WE 20051104000282005110400028NM 2005 11 4 2005UALA01192 120051026A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE EEL,48RT, 5E AFTINOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29116UA 26908 EEL LIGHT AT 48 RT AND 5E AFT INOPERATIVE. 2L74 4F4 FRTA20WE E24NE 20051104000312005110400031NM 2005 11 4 2005UALA01195 120051026A5330 SKIN BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU STA 807, STR 18 GOUGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29336UA 24240 FUSELAGE SKIN APPROXIMATE STA 807 AND STR 18R ABOVE AFT CARGO DOOR HAS A DEEP GOUGE APPROX .025 INCH LONG. BLENDED GOUGE, REPAIRED SKIN PER SRM 53-00-01 REPAIR 32 BY INSTALLING DOUBLER AND TRIPLER. 2L72 4F4 FRTA16WE E21EU 20051104000332005110400033NM 2005 11 4 2005UALA01197 120051026A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE STA 618 TO 620 SDENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29514UA 24839 LT FUSELAGE APPROX STA 618 TO 620, S-15 TO S-16 HAS A DENT. REMOVED DAMAGED ACP NDT INSP, NO CRACKS NOTED. FABRICATED REPAIR AND INSTALLED IAW SRM 53-00-01. 2L72 4F4 FRTA2NM E17NE 20051104000392005110400039 2005 11 4 2005UALA01203 420051026A256560322103 ASPIRATOR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE SLIDE UNSERVICEABLE A UALAK NONE O OTHER ININSP/MAINT 1 WP29406UA 454 TWO (2) DAMAGED ASPIRATORS. 2L72 4F4 FRTA28NM E40NE 20051104000412005110400041EA 2005 11 4 SWIA200515768 120051022A2760 SECU CNDAIRCL600 CL6002B19 1900309EA NR 1 MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07465SW 7845 OUTBOARD GROUND SPOILER FAULT. REPLACED OUTBOARD GROUND SPOILER MANIFOLD IAW 27-63-05, NR 1 SECU IAW 27-61-05 AND RIGHT OUTBOARD SPOILER GROUND PROX SENSOR IAW 23-60-00. OPERATIONAL TEST GOOD. 2L72 4F RTA21EA 20051104000432005110400043EA 2005 11 4 SWIA200515770 120051025A2760C13045BA04 SECU CNDAIRCL600 CL6002C10 1390015EA SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07758SK 10222 AT GATE, RECEIVED STAB FAULT & PITCH FEEL FAULT. REPLACED SSCU NR 1 REF CRJ MM 27-61-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051104000462005110400046SO 2005 11 4 SWIA200515751 120051025A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT DISCHARGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07568SW1029010290 120343 AFT EMERGENCY LIGHTS DO NOT ILLUMINATE. REPLACED AFT EMERGENCY BATTERY PACK, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20051104000482005110400048EA 2005 11 4 SWIA200515753 120051023A27515913163 DETECTOR CNDAIRCL600 CL6002C10 1390015EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07710SK2628 2628 10170 FLAP HALFSPEED MSG AT FL360. REPLACED RT INBOARD FLAP SKEW DETECTOR IAW CRJ 700 AMM 27-52-45. OPERATIONAL CHECKS OK. 2L72 4F RTA21EA 20051104000522005110400052EA 2005 11 4 SWIA200515756 120051029A274170609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07446SW3049 3049 7666 STAB CH2 STATUS MSG. REPLACED HSTCU IAW 27-40-00. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051104000542005110400054SO 2005 11 4 SWIA200515758 120051024A3350 SIGN EMB 120 EMB120ER 3260203SO CABIN MISSING A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07212SW 120276 EXIT SIGN AT 6C MISSING. REPLACED EXIT SIGN AT 6C AS REQUIRED. 2L72 4T RTA31SO 20051104000572005110400057SO 2005 11 4 SWIA200515761 120051027A2611 SMOKE DETECTOR EMB 120 EMB120ER 3260203SO UNKNOWN ACTIVATED A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07291SW 120318 SMOKE DETECTOR ALARM GOES OFF FOR NO REASON. REPLACED MOUNT FLANGE AND SMOKE DETECTOR. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20051104000632005110400063NM 2005 11 4 SWAA053387 120051027A249791252ZC7C4001 RELAY BOEING737 7373H4 1384600NM GE CFM56 CFM56* 13802NE COCKPIT FAULTY A SWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW29604SW 27955 AIR TURNBACK, SMOKE AND BURNING ELECTRICAL SMELL IN COCKPIT AND CABIN. REMOVED AND REPLACED R3 RELAY IAW MM. 2L72 4F4 FRTA16WE E2GL 20051104000872005110400087NM 2005 11 4 SWAA053436 120051101A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 446, STR 26L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051104000972005110400097NE 2005 11 4 SWAA053423 220051029A7200CFM567B ENGINE BOEING737 7377H4 1384404NM CFMINTCFM567CFM567B22 13802NE RIGHT POWER LOSS A SWAAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SW29200WN 32482 876502 NR 2 ENGINE WOULD NOT SPOOL UP. REMOVED AND REPLACED NR 2 ENGINE HMU, FUEL PUMP, EEC, T25 SENSOR & FUEL NOZZLE FILTER, NO HELP. REMOVED AND REPLACED NR 2 ENGINE PER MM. 2L72 4F4 FRTA16WE E00055EN 20051104000992005110400099NM 2005 11 4 SWAA053425 120051101A53156545410 FLOORBEAM BOEING737 7373H4 1384600NM CABIN FLOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED BETWEEN BS 540 TO BS 727, RBL 25. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20051104001012005110400101NM 2005 11 4 SWAA053427 120051031A53306545777 SKIN BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 986.5, BL 0. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051104001032005110400103NM 2005 11 4 SWAA053429 120051101A53116545804 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 259.5, BETWEEN RBL 11 TO LBL 11, WL 208. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20051104001052005110400105NM 2005 11 4 SWAA053431 120051030A56105893543130 WINDOW BOEING737 737317 138447PNM COCKPIT ARCED A SWAAO OTHER O OTHER NRNOT REPORTED 1 SW29686SW 23175 R1 COCKPIT WINDOW ARCED & CRACKED. REMOVED AND REPLACED R1 WINDOW PER MM. 2L72 4F RTA16WE 20051104001072005110400107NM 2005 11 4 SWAA053433 120051030A53306545768 SKIN BOEING737 737317 138447PNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29686SW 23175 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 360, STR 25R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051104001092005110400109NM 2005 11 4 SWAA053435 120051031A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29704SW 27838 EEPLS STRIP DELAMINATED AT ROW 8 DEF. REMOVED AND REPLACED STRIP PER MM. 2L72 4F RTA16WE 20051104001112005110400111EU 2005 11 4 0501583234 120051009A2120 SMOKE AIRBUS320 A320212 3930322EU COCKPIT DETECTED A NWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL01334NW 339 SMOKE IN COCKPIT WITH ASSOCIATED PRINTER FAIL ANNUNCIATION. CREW PULLED C/B J-21 PRINTER SUPPLY. SMOKE SUBSIDED. MAINTENANCE REMOVED AND REPLACED PRINTER. 2L72 4F RTA28NM 20051104001122005110400112WP 2005 11 4 0501559869 120051018A5411 RIB DOUG DC9 DC951 3022051WP LT PYLON CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01778NC 48100 DURING INSPECTION, FOUND CRACK IN LOWER SURFACE OF LT PYLON CLOSING RIB AND ANGLE BEHIND THE AFT ENGINE MOUNT. REPAIRED PER EA 98-205378. 2L72 4F RTA6WE 20051104001142005110400114NM 2005 11 4 MZZA0500012 120051102A3350D71701100 BATTERY PACK BOEING737 737824 13844BZNM ROWS 5-10 INOPERATIVE A MZZAK NONE O OTHER ININSP/MAINT 1 WP1314249 28809 INSPECTION FOUND SEAT EMERGENCY LIGHTS INOPERATIVE AT ROWS 5, 6, 7, 8, 9 AND 10. THE M1676 BATTERY PACK WAS REPLACED IAW MM 33-51-00. 2L72 4F RTA16WE 20051104001172005110400117SO 2005 11 4 MASA200500284 120050405A5210 HANDLE EMB 145 EMB145LR 3260212SO PAX DOOR UNSECURE A MASAO OTHER O OTHER TXTAXI/GRND HDL 1 SW07850MJ 145568 PAX DOOR THAT WOULD NOT OPEN FROM THE INSIDE OF THE AIRCRAFT. THE AIRCRAFT WAS FERRIED TO CLT FOR FURTHER TROUBLESHOOTING. MAINTENANCE RESECURED THE INNER HANDLE. 2L72 4T RTT00011AT 20051104001432005110400143WP 2005 11 4 IXXA05SMN197S 120050923A5730 SKIN DOUG DC8 DC871F 302199DWP XFS 566.250 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING C CHECK INSPECTION, RT WING OTBD L/E LOWER SKIN CRACKED 1” APPROX, BETWEEN STA XFS 566.250 AND XFS 572.500. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 # 05446 DATED 10-05-05, SEMAN DWG # ED-4068 DATED 09-27-05, EO SEMAN # 20051231 DATED 10-05-05. REMOVED FASTENERS IAW DC8 SRM 51-1-21, DC8 SRM 51-3-0. REMOVED DAMAGED SECTION IAW SEMAN DWG # ED-4068. NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D REPAIR DOUBLER (AL7075T6 0.063”), FILLER (AL7075T6 0.050”) IAW SEMAN DWG # ED-4068. CLEANED, TREATED, PRIMED FILLER, REPAIR DOUBLER INNER FACE IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW2L74 4F RT4A25 20051104001452005110400145WP 2005 11 4 IXXA05RNG065S 120050916A5730 SKIN DOUG DC8 DC872 302199BWP STA XW408 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX* 46013 DURING INSPECTION CHECK WAS FOUND A CORROSION ON UPPER SKIN AT LEADING EDGE STA XW 408 TO 454, LT.CORROSION ON UPPER SKIN AT LEADING EDGE STA XW 408 TO 454-LT WAS REPAIRED IAW SRM 57-2-1 FIGURE 38 AND EWO ATI 57-043. 2L74 4F RT4A25 20051104001472005110400147WP 2005 11 4 IXXA05SMN227S 120051013A5330 RIVET DOUG DC8 DC871F 302199DWP FS 1693. IMPROPER B IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW11829BX896722998 45994 DURING C CHECK INSPECT, AFT LWR FUSELAGE BELLY, STA FS 1693 L-30.75R. UPGRADE REPAIR DOUBLER TO INCORPORATE A MIN OF 3 ROWS OF RIVETS (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-1 FIG 7, EO SEMAN # 20051202 DATED 09-20-05. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21. REMOVED DAMAGED SECTION IAW DC8 SRM 53-2-1 FIG 7 (SHEET 1, 5). NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D REPAIR DOUBLER (AL7075T6 0.063”), INTERNAL FINGER DOUBLER (AL7075T6 0.032”), FILLER (AL7075T6 0.050”) IAW DC8 SRM 53-2-1 FIG 7 (SHEET 1, 5), DC8 SRM 53-5-1 ITEM “E” FIG 1, DC8 SRM 51-1-4 PG 1 (FORMING). CLEANED, TREATED, PRIMED AREA, REPAIR PARTS IAW DC8 SRM 512L74 4F RT4A25 20051104001492005110400149WP 2005 11 4 IXXA05SMN229S 120051013A5330 RIVET DOUG DC8 DC871F 302199DWP FS 1544.000 IMPROPER B IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW11829BX896722998 45994 DURING C CHECK INSPECT, AFT LWR FUSELAGE BELLY, STA FS 1544.000 L-35.5L, UPGRADE REPAIR DOUBLER TO INCORPORATE A MIN OF 3 ROWS OF RIVETS (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-1 FIG 7, EO SEMAN # 20051200 DATED 09-20-05. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D. REMOVED DAMAGED SECTION IAW DC8 SRM 53-2-1 FIG 7 (SHEET 1, 3). NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D REPAIR DOUBLER (AL7075T6 0.080”) + (02 EA) INTERNAL FINGER DOUBLERS (AL7075T6 0.050”) IAW DC8 SRM 53-2-1 FIG 7 (SHEET 1, 3), DC8 SRM 53-4-1 FIG 16 (SHEET 2) ITEM “B”, DC8 SRM 51-9-0 FIG 68A, DC8 SRM 51-1-4 PG 1 (FORMING). CLEANED, TREATED,2L74 4F RT4A25 20051104001512005110400151WP 2005 11 4 IXXA05SMN231S 120051013A5730 SKIN DOUG DC8 DC871F 302199DWP XW 91.000 IMPROPER B IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW11829BX896722998 45994 DURING C CHECK INSPECT, LT INBD FLAP L/E UPPER SKIN HAS NON STANDARD REPAIR, XW 91.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 # 05446 DATED 10-05-05, SEMAN DWG # ED 4065 DATED 09-27-05, EO SEMAN # 20051208 DATED 10-05-05. REMOVED NON STANDARD REPAIR IAW DC8 SRM 51-1-21, DC8 SRM 51-3-0, DC8 SRM 51-1-20D. REMOVED DAMAGED SECTION IAW SEMAN DWG # ED-4065. PERFORMED NDT INSP OF REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D NEW PLATING SEGMENT (AL2024T3 0.040”), INTERNAL SPLICE (AL2024T3 0.050”), (02EA) EXTERNAL DOUBLERS (AL2024T3 0.050”) IAW SEMAN DWG # ED-4065, DC8 SRM 51-1-4 (FORMING). CLEANED, TREATED, PRIMED AREA, REPAIR PARTS IAW DC8 SRM 51-1-8B. APPLIED 2L74 4F RT4A25 20051104001522005110400152WP 2005 11 4 IXXA05SMN184S 120050920A5330 DOOR DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE STA -54.000 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING ROUTINE C CHECK INSP, EXTERNAL FUS. FREON SYS EXHAUST DOOR AFT UPPER CORNER CRACKED .5, STA 54.000 L-2/8L L29L. PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 13 (SHEET 1, 5), TR NR 53-169, EO SEMAN NR 20051190 DATED 09-20-05. REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-3-0. REMOVED DAMAGED SECTION IAW SRM (SHEET 1). NDT INSPECTED REWORKED AREA IAW NDT SRM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FABRICATED REPAIR DOUBLER (AL2024T3 0.071) FILLER (AL2024T3 0.050”) IAW SRM 53-2-0 FIG 13 (SHEET 1, 5), SRM 53-2-0 FIG 13, TR NR53-169. CLEANED, TREATED, PRIMED AREA + REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW SRM. (TORQUE). 2L74 4F4 FRT4A25 E2GL 20051104001532005110400153WP 2005 11 4 IXXA05SMN198S 120050923A5730 SKIN DOUG DC8 DC871F 302199DWP XFS335.250-340. CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING C CHECK INSPECT, RT WING CTR L/E LOWER SKIN CRACKED 1” APPROX, BETWEEN STA XFS 335.250 AND XFS 340.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05463 DATED 10-11-05, SEMAN DWG NR ED-4067 DATED 10-11-05, EO SEMAN NR 20051227 DATED 10-11-05. REMOVED FASTENERS IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D, DC8 SRM 51-3-0. REMOVED DAMAGED SECTION IAW SEMAN DWG NR ED-4067. NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D EXTERNAL REPAIR DOUBLER (AL7075T6 0.071) + (02EA) FILLER (AL7075T6 0.063) IAW SEMAN DWG # ED-4067. CLEANED, TREATED, PRIMED AREA, FILLER, REPAIR DOUBLER INNER SIDE IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 52L74 4F RT4A25 20051104001552005110400155WP 2005 11 4 IXXA05SMN214S 120050927A5751 SKIN DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE XA 470.000 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING ROUTINE C CHECK INSPECTION, RT IB AIL L/E UPPER PLATING CRACK .2500 AT STA XA 470.000. PERFORMED MAJOR REPAIR IAW SRM 57-8-1 FIG 1, EO SEMAN NR 20051280 DATED 09-26-05. REMOVED DAMAGED PLATING IAW SRM 51-1-21. FABRICATED NEW PLATING (AL2024T3 0.040) IAW SRM 57-8-1 FIG 1 ITEM E, SRM 51-1-4 PG 1 (FORMING). CLEANED,TREATED, PRIMED AREA + INNER FACE OF NEW PLATING IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACE IAW SRM 51-1-11 PG 9. INSTALLED NEW PLATING IAW SRM 51-1-21. 2L74 4F4 FRT4A25 E2GL 20051104001572005110400157WP 2005 11 4 IXXA05SMN216S 120050927A5313 LONGERON DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE 1786.000 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING ROUTINE C CHECK INSPECTION, AFT FUSELAGE LONGERON 17R CRACKED 1, STA 1786.000. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, EO SEMAN NR 20051286 DATED 09-27-05. REMOVED CRACKED LONGERON IAW SRM 53-5-1 FIG 7 (SHEET 1) ITEM B SRM 51-2-0 FIG 5 (SHEET 37). CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACE IAW SRM 51-1-11 PG 9. INSTALLED NEW LONGERON IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE), SRM 51-1-21. 2L74 4F4 FRT4A25 E2GL 20051104001592005110400159WP 2005 11 4 IXXA05SMN185S 120050922A5330 RIVET DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE FS 76.000 INCORRECT B IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW11829BX896722998 45994 DURING ROUTINE C CHECK INSP, FUSELAGE BELLY, STA FS 76.000 L-35. 75R. UPGRADE REPAIR DOUBLER TO INCORP A MINIMUM OF 3 ROWS OF RIVETS. PERFORMED REPAIR IAW NR 05446 DATED 10-05-05, DWG NR ED-4058 DATED 09-27-05, EO NR 20051191 DATED 10-05-05. REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-1-21. REMOVED DAMAGED SECTION IAW DWG NR ED-4058. NDT INSPECTED REWORKED AREA IAW NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FABRICATED REPAIR DOUBLER (AL7075T6 0.063) + INTERNAL FINGER DOUBLER (AL7075T6 0.032) IAW DWG NR ED-4058, SRM 51-1-4 PG 1 (FORMING). CLEANED, TREATED, PRIMED AREA + REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM. INSTALLED REPAIR PARTS IAW SRM. (TORQUE) 2L74 4F4 FRT4A25 E2GL 20051104001612005110400161WP 2005 11 4 IXXA05SMN219S 120050929A5344 FITTING DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE 60.-70.000 CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING ROUTINE C CHECK INSPECTION, FWD ACCY COMPT, FITTING CORRODED, STA 60.000, 70.000 L-34R. PERFORMED MAJOR REPAIR IAW MSG NR 1-126059161-2 DATED 09-26-05, SRM 52-1-0 PG 1. REMOVED DAMAGED SKIN IAW SRM 51-1-21. FABRICATED NEW SKIN (AL7075T6 0.050) IAW MSG NR 1-126059161-2, SRM 52-4-1 FIG 1 ITEM Q. CLEANED, TREATED AND PRIMED AREA + NEW SKIN IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW SKIN IAW SRM 51-1-21, SRM 51-3-0, SRM 51-3-1 (TORQUE). 2L74 4F4 FRT4A25 E2GL 20051104001632005110400163WP 2005 11 4 IXXA05SMN186S 120050922A5330 RIVET DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE FS 173.000 IMPROPER B IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW11829BX896722998 45994 DURING ROUTINE C CHECK INSPECTION, FWD LOWER FUSELAGE BELLY, STA FS 173.000 L-35.5R. UPGRADE EXTERNAL REPAIR DOUBLER TO INCORPORATE A MINIMUM OF 3 ROWS OF RIVETS. PERFORMED MAJOR REPAIR, REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-1-21. REMOVED DAMAGED SECTION IAW DWG NR ED-4059. NDT INSPECTED REWORKED AREA IAW NDT SPM. NEITHER CRACK NOR CORROSION FOUND. FABRICATED REPAIR DOUBLER (AL7075T6 0.063) INTERNAL FINGER DOUBLER (AL7075T6 0.032) IAW DWG NR ED-4059, SRM 51-1-4 PG 1 (FORMING). CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM. INSTALLED REPAIR PARTS IAW SRM. 2L74 4F4 FRT4A25 E2GL 20051104001652005110400165WP 2005 11 4 IXXA05SMN188S 120050922A5330 RIVET DOUG DC8 DC871F 302199DWP FS 1143 IMPROPER B IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW11829BX896722998 45994 DURING C CHECK INSPECT, AFT LWR FUSELAGE BELLY, STA FS 1143 L-35.5L, UPGRADE REPAIR DOUBLER TO INCORPORATE A MIN OF 3 ROWS OF RIVETS. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05463 DATED 10-11-05, SEMAN DWG NR ED-4062 DATED 10-10-05, EO SEMAN NR 20051197 DATED 10-11-05. REMOVED EXISTING REPAIR DOUBLERS IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D, DC8 SRM 51-3-0. REMOVED DAMAGED SECTION IAW SEMAN DWG NR ED-4062. NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D REPAIR DOUBLER (AL7075T6 0.080”) + REPAIR TRIPLER (AL7075T6 0.090) + (04EA) FINGER DOUBLERS (AL7075T6 0.050”) IAW SEMAN DWG NR ED-4062. CLEANED, TREATED, PRIMED AREA, REPAIR PARTS IAW DC8 SRM 51-1-82L74 4F RT4A25 20051104001672005110400167WP 2005 11 4 IXXA05SMN200S 120050927A5730 VANE DOUG DC8 DC871F 302199DWP XS 520.168 ELONGATED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING C CHECK INSPECT, LT WING OTBD SLOT VANE HOLES ELONGATED, STA XS 520.168. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05447 DATED 10-05-05, SEMAN DWG # ED-4064 DATED 09-30-05, EO SEMAN # 20051206. REMOVED FASTENERS IAW DC8 SRM 51-1-21, DC8 SRM 51-3-0. REMOVED DAMAGED SECTION IAW SEMAN DWG # ED-4064. NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D REPAIR DOUBLER (AL7075T6 0.071), INTERNAL DOUBLER, FILLER (AL7075T6 0.063) IAW SEMAN DWG NR ED-4064, DC8 SRM 51-1-4 PG 1 (FORMING). CLEANED, TREATED, PRIMED AREA, INNER SIDE OF REPAIR PARTS IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW 2L74 4F RT4A25 20051104001682005110400168WP 2005 11 4 IXXA05SMN201S 120050927A5340 FITTING DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE 781.000 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING ROUTINE C CHECK INSPECTION, MAIN CARGO COMPT FWD FITTING CRACKED 2, STA 781.000 L-19L. REMOVED CRACKED FITTING IAW SRM 51-1-20D. FABRICATED NEW FITTING (AL7075T651) IAW MFG DWG NR 3779978, EA NR 20051313. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02 TO 07. CLEANED, TREATED AND PRIMED AREA AND NEW FITTING IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2L74 4F4 FRT4A25 E2GL 20051104001702005110400170WP 2005 11 4 IXXA05SMN206S 120050927A5730 SKIN DOUG DC8 DC871F 302199DWP XFS 304-310.000 CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING C CHECK INSPECT, LT WING CTR UPPER L/E CORRODED, STA XFS 304 310.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-1 FIG 44, EO SEMAN # 20051213 DATED 09-22-05. REMOVED FASTENERS IAW DC8 SRM 51-1-21. REMOVED CORROSION IAW DC8 SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW DC8 SRM 57-2-1 FIG 26. REMOVED CORRODED SECTION IAW DC8 SRM 57-2-1 FIG 44 (SHEET 2, 5) TR #57-102. PERFORMED NDT INSP OF REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D REPAIR DOUBLER (AL7075T6 0.063”) IAW DC8 SRM 57-2-1 FIG 44 (SHEET 2, 5, 6, 8) TR # 57-102, DC8 SRM 57-3-1 FIG 4 SHEET 1 ITEM “A”. CLEANED, TREATED, PRIMED INTERNAL FACE OF REPAIR DOUBLER IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO 2L74 4F RT4A25 20051104001712005110400171WP 2005 11 4 IXXA05SMN209S 120050927A5730 SKIN DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE XFS 597.500 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING ROUTINE C CHECK INSPECTION, RT OUTER WING IB L/E LOWER SKIN, .2500 IN CRACK, STA XFS 597.500. PERFORMED MAJOR REPAIR DATED 10-07-05, DWG NR ED-4069 DATED 10-06-05, EO NR 20051275 DATED 10-07-05. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-3-0. PERFORMED STOP DRILL OF 0.250 AT CRACK END IAW DWG NR ED-4069. NDT INSPECTED REWORKED AREA IAW NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FABRICATED REPAIR DOUBLER (AL7075T6 0.063) IAW DWG NR ED-4069. CLEANED, TREATED, PRIMED AREA, REPAIR DOUBLER INNER SIDE IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED REPAIR DOUBLER IAW DWG NR ED-4069, SRM 51-1-21, SRM 51-1-20D, SRM 51-3-0, SRM 51-3-1 (TORQUE). 2L74 4F4 FRT4A25 E2GL 20051104001722005110400172WP 2005 11 4 IXXA05SMN210S 120050927A5730 SKIN DOUG DC8 DC871F 302199DWP XFS 710.000 CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING C CHECK INSPECTION, RT OUTER WING INBD L/E UPPER SKIN CORRODED, STA XFS 710.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05461 DATED 10-10-05, SEMAN DWG # ED-4070 DATED 10-07-05, EO SEMAN # 20051276 DATED 10-10-05. REMOVED FASTENERS IAW DC8 SRM 51-1-21, DC8 SRM 51-3-0. REMOVED CORROSION ON RH OUTER WING I/B L/E UPPER SKIN, STA XFS 710.000 IAW DC8 SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW DC8 SRM 57-2-1 FIG 2G. REMOVED DAMAGED SECTION IAW SEMAN DWG # ED-4070. NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D REPAIR DOUBLER (AL7075T6 0.063”) + FILLER (AL7075T6 0.050) IAW SEMAN DWG # ED-4070. CLEANED, TREATED, PRIMED AREA + FILLER + INNE2L74 4F RT4A25 20051104001742005110400174WP 2005 11 4 IXXA05SMN212S 120050927A5340 FITTING DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE 445.000 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING ROUTINE C CHECK INSPECTION, FWD LOWER FUSELAGE. SPLICE FITTING CRACKED 2 , STA 445.000, STA 455.000 L-31R. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D AND TORQUED IAW SRM 51-3-1. 2L74 4F4 FRT4A25 E2GL 20051104001762005110400176WP 2005 11 4 IXXA05SMN204S 120050927A5340 FITTING DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE 902.000 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING ROUTINE C CHECK INSPECTION, MAIN CARGO COMPT FITTING CRACKED 1.5, STA 902.000 L-19L. REMOVED CRACKED FITTING IAW SRM 51-1-20D. FABRICATED NEW FITTING (AL7075T651) IAW MFG DWG NR 3779498, EA NR 20051314. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02 TO 07. CLEANED, TREATED AND PRIMED AREA, NEW FITTING IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2L74 4F4 FRT4A25 E2GL 20051104001782005110400178WP 2005 11 4 IXXA05SMN237S 120051013A5730 DOUBLER DOUG DC8 DC871F 302199DWP XFS 341.500 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING C CHECK INSPECTION, LT WING CTR L/E LWR PART INTERNAL DOUBLER CRACKED 7, XFS 341.500. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05463 DATED 10-11-05, SEMAN DWG # ED-4083 DATED 10-10-05, EO SEMAN # 20051312 DATED 10-11-05. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D, DC8 SRM 51-3-0. REMOVED DAMAGED SECTION IAW SEMAN DWG # ED-4083. NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D EXTERNAL REPAIR DOUBLER (AL7075T6 0.071) + NEW INTERNAL DOUBLER SEGMENT (AL7075T6 0.080) + (02EA) INTERNAL STRAPS (AL7075T6 0.050) IAW SEMAN DWG # ED-4083. CLEANED, TREATED, PRIMED AREA + REPAIR PARTS IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FA2L74 4F RT4A25 20051104001802005110400180WP 2005 11 4 IXXA05SMN240S 120051013A5720 PAN DOUG DC8 DC871F 302199DWP XS 250.089 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING ROUTINE C CHECK INSPECTION, RT INNER WING OUTBD L/E ZEE PAN CRACK 2” AT STA XS 250.089. REMOVED CRACKED SPLICE PAN IAW DC8 SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW SPLICE PAN IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D. 2L74 4F RT4A25 20051104001812005110400181WP 2005 11 4 IXXA05SMN191S 120050922A5542 SKIN DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE ZONE 300 DELAMINATED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING ROUTINE C CHECK INSPECTION, VERT STAB DELAMINATED SKIN ON RUDDER TAB. REMOVED DAMAGED SECTION PLUS FABRICATED DOUBLER (AL2024T3 0.012) IAW SRM 55-2-2 PARA 2. BONDED CORE PLUS DOUBLER WITH HYSOL IAW SRM 51-1-9. REFER TO NR 2801 FOR WEIGHT. 2L74 4F4 FRT4A25 E2GL 20051104001822005110400182WP 2005 11 4 IXXA05SMN192S 120050922A5710 DOOR DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE ZONE 500 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING ROUTINE C CHECK INSPECTION, LT WING NR 2 ALT TANK 506B ACCESS DOOR CRACKED. REMOVED AND REPLACED CRACKED ACCESS DOOR NR 506 B (NR 2 ALT TANK) IAW SRM 51-3-0, SRM 51-3-1 (TORQUE) REFER TO JC 99116 FOR LEAK CHECK. 2L74 4F4 FRT4A25 E2GL 20051104001832005110400183WP 2005 11 4 IXXA05SMN193S 120050922A5710 SKIN DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE XRS 72.000 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING ROUTINE C CHECK INSPECTION, LT WING. UPPER SKIN AROUND HILOK CRACKED, XRS 72.000 S.9PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 17, EO SEMAN NR 20051211 DATED 09-21-05. REMOVED FASTENERS IAW SRM . REMOVED DAMAGED SECTION IAW SRM 57-2-1 FIG 17. PERFORMED NDT INSP. OF REWORK AREA IAW NDT SPM PART. NEITHER CRACK NOR CORROSION FOUND. FABRICATED REPAIR DOUBLER (AL7075T6 0.160) + FILLER PLUG (AL7075T6 0.175”) IAW SRM 57-2-1 FIG. 17, SRM 57-3-1 FIG 10. TAPERED DOUBLER FROM 0.160 TO 0.080 IAW SRM 57-2-1 FIG 17, SRM 51-10-0 PG 8 FIG 1 (SHEET 6). CLEANED, TREATED, PRIMED AREA + REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM. INSTALLED REPAIR PARTS IAW SRM. (TORQUE) 2L74 4F4 FRT4A25 E2GL 20051104001842005110400184WP 2005 11 4 IXXA05SMN194S 120050922A5310 CAP DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE STA 680.000 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING ROUTINE C CHECK INSPECTION, MID ACCY CMPT. CAP CRACKED 1, STA 680.000 BETWEEN L 27 AND L 28LPERFORMED MAJOR REPAIR IAW SRM 53-2-5 FIG 14, EO SEMAN NR 20051313 DATED 09-30-05. REMOVED FASTENERS IAW SRM 51-1-20D PG 1. STOP DRILLED ON CRACK END IAW SRM 53-2-5 FIG 14 (SHEET 1). PERFORMED NDT INSPECTION IAW NDT DPM PART 06-10-01-001. NO CRACK NOR CORROSION FOUND. FABRICATED REPAIR ANGLE (7075 O AL-0.100) IAW SRM 53-2-5 FIG 14 (SHEET 1 AND 3), AND SRM 51-1-4 PG 1 AND DPS 3-69-4 (FORMING). PERFORMED HEAT TREATMENT IAW SRM 51-1-1 PG 1, 13 AND D.P.S 7.00-1 REV BK. CLEANED, TREATED, PRIMED AREA + REPAIR ANGLE IAW SRM 53-2-5 FIG 14 (SHEET 1 AND 3), SRM 51-1-20D PG 9 AND SRM 51-3-1 (TORQUE). 2L74 4F4 FRT4A25 E2GL 20051104001862005110400186WP 2005 11 4 IXXA05SMN217S 120050927A5313 LONGERON DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE 1786.000 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING ROUTINE C-CHECK INSPECTION, AFT FUSELAGE LONGERON 17L CRACKED 1, STA 1786.000PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, EO SEMAN NR 20051285 DATED 09-27-05. REMOVED CRACKED LONGERON IAW SRM 51-1-20D. FABRICATED NEW LONGERON (EXTRUSION P/N S1616757) IAW SRM 53-5-1 FIG 7 (SHEET 1) ITEM B, SRM 51-0 FIG 50 (SHEET 37). CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACE IAW SRM 51-1-11 PG 9. INSTALLED NEW LONGERON IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE), SRM 51-1-21. 2L74 4F4 FRT4A25 E2GL 20051104001882005110400188NM 2005 11 4 UPS05445651 120051023A541065B903604 LINK BOEING747 747121 1384871NM PWA JT9 JT9D3 52050NE NR 2 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 AD NR 2 PYLON REAR ENGINE MOUNT THRUST LINK ULTRASONIC INSP FOUND CRACK INDICATION EXCEEDED LIMIT AT BOTH FWD AND AFT LUG. NR 2 PYLON REAR UPPER ENGINE MOUNT AFT THRUST LINK ASSY CHANGED AND INSTALLED IAW MM 71-21-03. 2L74 4F4 F A20WE E20EA 20051104001902005110400190NM 2005 11 4 UPS05445653 120051025A541065B903604 LINK BOEING747 747121 1384871NM PWA JT9 JT9D3 52050NE NR 4 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 AD NR 4 PYLON REAR MOUNT THRUST LINK AFT IND LUG FOUND CRACK INDICATION EXCEED LIMIT. NR 4 PYLON REAR UPPER MOUNT THRUST LINK ASSY CHANGED AND INSTALLED MM 71-21-03. 2L74 4F4 F A20WE E20EA 20051104001942005110400194WP 2005 11 4 UPS05845654 120051005A53403755854U1 FITTING DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE FS1200 L26L CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 C2 C-PIT STA 1200 L26L BANANA FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED BANANA FITTING AT STA 1200 L26L IAW SRM 53-2-0, AND 51=1-20D,AND SRM 51-3-2. 2L74 4F4 FRT4A25 E2GL 20051104001962005110400196WP 2005 11 4 UPS05845656 120051013A5310 STIFFENER DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE FS283 APIT DOOR CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 C2 A-PIT STA 283 AT LWR FWD DOOR CUTOUT, EXTRUDED STIFFNER IS CORRODED OUT OF LIMITS. REMOVED A-PIT LWR FWD DOOR CUTOUT STIFFNER IAW SRM 51-1-24 FABRICATED AND HEAT TREATED STIFFNER IAW DWG 5733892 AND INSTALLED STIFFNER AT STA 283 LWR FWD DOOR CUTOUT IAW DWG 5733892 AND SRM 51-1-20D. 2L74 4F4 FRT4A25 E2GL 20051104001982005110400198EU 2005 11 4 UPS05145666 120051021A5320A5341076522200 BRACKET AIRBUSA300 A300F4622R 3930360EU FR 54, BL 0 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01135UP 0818 AFT CARGO FS 54 BL 0 SIDEWALL BRACE CRACKED. REMOVED AND REPLACED SIDEWALL BRACE IAW SRM 51-40-21. 2L72 4F RTA35EU 20051104002002005110400200EU 2005 11 4 UPS05145668 120051021A5320A5341076521900 BRACKET AIRBUSA300 A300F4622R 3930360EU FR54 BL 30 R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01135UP 0818 INSPECTION TYPE:2C AFT CARGO FS 54 BL 30 R SIDEWALL BRACE CRACKED. REMOVED AND REPLACED SIDEWALL BRACE IAW SRM 51-40-21. 2L72 4F RTA35EU 20051104002022005110400202NM 2005 11 4 UPS05545670 120051007A5320146N544016 ANCHOR BOEING757 75724APF 1384969NM BULK CARGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01406UP 23728 INSPECTION TYPE:C-4 BULK CARGO RT MBA TIE DOWN FITTING HAS CORROSION, STA 1460 AND STA 1480. REPLACED FITTING PER SRM 51-40-05-OG. 2L72 4F RTA2NM 20051104002032005110400203NM 2005 11 4 UPS05545671 120051010A5310 BEAM BOEING757 75724APF 1384969NM SECT 44 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01406UP 23728 INSPECTION TYPE:C-4 MAIN CARGO LONGITUDINAL BEAM HAS CORROSION AT STA 974 LBL 24. REPAIRED PER ER 05-4559. 2L72 4F RTA2NM 20051104002042005110400204NM 2005 11 4 UPS05545672 120051010A5315 FLOORBEAM BOEING757 75724APF 1384969NM SECT 44 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01406UP 23728 INSPECTION TYPE:C4 CORROSION ON TOP OF FLOORBEAM FWD FLANGE AROUND FASTENER HOLES AT SEVERAL LOCATIONS AT BS 1200 BETWEEN BL-O AND LBL 65 REPAIRED PER ER 05-4596. 2L72 4F RTA2NM 20051104002052005110400205NM 2005 11 4 UPS05545673 120051008A5321 FLOOR PANEL BOEING757 75724APF 1384969NM SECT 41 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01406UP 23728 INSPECTION TYPE:C4 CONTROL CABIN FLOOR SURFACE CORRODED BS282 LBL 28 WL 200. REPAIRED PER SRM 51-70-13-00. 2L72 4F RTA2NM 20051104002062005110400206NM 2005 11 4 UPS05545674 120051010A5347 SEAT TRACK BOEING757 75724APF 1384969NM SECT 46 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01406UP 23728 INSPECTION TYPE: C4- SEAT TRACK CORRODED BETWEEN BS 1180 AND 1200 RBL 46 TO BE REPAIRED ON CUST CARD NR 561511. BLENDED CORROSION ON SEAT TRACK FLANGE AT BS 1190 RBL 46 REMOVED .20" ON A 1X 1.2" AREA ORIGINAL THICKNESS OF .085 WHICH IS OUT OF LIMITS PER SRM 53-00-52-1A1 FIG 101. DETAIL VII. SEAT TRACK WILL BE REPAIRED ON CUST CARD 561511 (INTERIOR 05138). 2L72 4F RTA2NM 20051104002072005110400207NM 2005 11 4 UPS05545675 120051010A5310 BEAM BOEING757 75724APF 1384969NM SECT 44 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01406UP 23728 INSPECTION TYPE:C4 LONGITUDINAL BEAM CORRODED AT STA 1063 LBL 26, LONGITUDINAL BEAM IS BEING REPLACED FROM BS 1040-BS1080, LBL26 WL 208 0N CUST CARD#561467. 2L72 4F RTA2NM 20051104002082005110400208NM 2005 11 4 UPS05545676 120051010A5320 FLOOR SUPPORT BOEING757 75724APF 1384969NM SECT. 44 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01406UP 23728 INSPECTION TYPE:C4 MAIN CARGO FLOOR SUPPORT CORRODED AT STA 1056 RBL 5-23. REMOVED AND REPLACED PER SRM 51-40-02 AND SRM 51-30-01 2L72 4F RTA2NM 20051104002102005110400210WP 2005 11 4 UPS05845689 120051003A5320 CUSP WEB DOUG DC8 DC873F 302199FWP FS1140-1170 L21LCRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 FOUND CUSP CRACKED STA 1140 L21L. REMOVED CRACK CUSP AT FS 1140 L21L IAW SRM 53-2-5 FIG 15. FABRICATED AND INSTALLED -3 ANGLES, -7 DOUBLERS AND CUSP AT FS 1140 TO 1170 IAW SRM 53-2-5 FIG 15 AND 53-1-2 FIG 1. 2L74 4F RT4A25 20051104002122005110400212WP 2005 11 4 UPS05845691 120051004A5340 FITTING DOUG DC8 DC873F 302199FWP FS 1775 L17L CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 FOUND L17L CRACKED AT END FITTING IN 60 COMPT, STA 1775. REMOVED END FITTING AT FS 1775 L17L IAW SRM 51-1-21. FABRICATED AND INSTALLED LONGERON AND END FITTING IAW SRM53-5-1 FIG 7 AND SRM 51-1-20D. 2L74 4F RT4A25 20051104002142005110400214WP 2005 11 4 UPS05845693 120050929A5330564932975N2 SKIN DOUG DC8 DC873F 302199FWP STA.1690 L28R- LCORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 FOUND FUSELAGE SKIN HAS HEAVY CORROSION AND SEVERAL CRACKS AT AFT MANUFACTURING SPLICE AREA STA 1690 L32L TO L32R. REMOVED AND REPLACED SKIN FROM STA 1690 TO 1890 L28R TO L28L IAW SRM 51-1-21, 51-3-2, 51-20-00, 51-3-0 AND 51-1-20D. 2L74 4F RT4A25 20051104002162005110400216WP 2005 11 4 UPS05845698 120051017A5313 LONGERON DOUG DC8 DC873F 302199FWP STA 1716 L18L CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 FOUND STA 1716 L18L IS CRACKED AT INTERSECTION OF CANTED FRAME UPPER ATTACH FASTENER. CUT OUT DAMAGED SECTION OF LONGERON, FABRICATED, AND INSTALLED REPLACEMENT SECTION OF LONGERON IAW DC-8 SRM 53-2-2 FIG 10. 2L74 4F RT4A25 20051104002182005110400218WP 2005 11 4 UPS05845700 120051017A53404772397U1 FITTING DOUG DC8 DC873F 302199FWP FS 1760 L17R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 FOUND RT AFT FUSELAGE INTERIOR FS 1760 L17R END FITTING HAS POSSIBLE CRACK AT UPPER FLANGE. NDT VERIFIED 1.5" CRACK. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51- 1-20D. 2L74 4F RT4A25 20051104002202005110400220WP 2005 11 4 UPS05845702 120051018A53404758514511 FITTING DOUG DC8 DC873F 302199FWP STA 1280 L33R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 FOUND FITTING CRACKED 1" LONG AT STA 1280 L33R. REMOVED, FABRICATED, AND INSTALLED FITTING IAW DWG 4758514 AND DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20051104002222005110400222NM 2005 11 4 UPS05545678 120051010A5310 BEAM BOEING757 75724APF 1384969NM SECT 44 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01406UP 23728 INSPECTION TYPE:C4 MAIN CARGO LONGITUDINAL BEAM HAS CORROSION STA 997, RBL 44. REPAIRED PER ER 05-4558. 2L72 4F RTA2NM 20051104002242005110400224NM 2005 11 4 UPS05545680 120051010A5310 BEAM BOEING757 75724APF 1384969NM SECT 44 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01406UP 23728 INSPECTION TYPE:C4 MAIN CARGO LONGITUDINAL BEAM HAS CORROSION STA 1007 RBL44. REPAIRED PER ER 05-4558. 2L72 4F RTA2NM 20051104002262005110400226NM 2005 11 4 UPS05545682 120051016A5310 BEAM BOEING757 75724APF 1384969NM MAIN CARGO BAY CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01406UP 23728 INSPECTION TYPE:C4 MAIN CARGO LONITUDINAL BEAM HAS CORROSION AT STA 1058, RBL 44. CORROSION FOUND OUT OF LIMITS, REMOVED AND REPLACED LONGITUDINAL BEAM BS 1040 TO BS 1080, RBL 44, WL 208 IAW SRM 53-00-57-1A, SRM 51-40-02 2L72 4F RTA2NM 20051104002282005110400228NM 2005 11 4 UPS05545684 120051017A5340146N544020 FITTING BOEING757 75724APF 1384969NM BULK CARGO BAY CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01406UP 23728 INSPECTION TYPE:C4 BULK CARGO RT MBA TIE DOWN FITTING HAS CORROSION STA 1580,1600, AND 1620. REMOVED CORROSION FROM FITTINGS AT BS 1580, FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED FITTING AT BS 1580 IAW SRM 53-00-53-1A AND SRM 51-40-02. REMOVED CORROSION FROM FITTINGS AT BS 1600 AND 1620 FOUND IN LIMITS ARE RESTORED FINISH IAW SRM 53-00-53-1A. 2L72 4F RTA2NM 20051104002302005110400230NM 2005 11 4 UPS05545686 120051016A5347BAC25202472 SEAT TRACK BOEING757 75724APF 1384969NM MAIN CARGO BAY CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01406UP 23728 INSPECTION TYPE:C4 MAIN CARGO SEAT TRACK CORRODED AT STA 1173, LBL 44.5. REMOVED AND REPLACED SEAT TRACK BS 1070 TO BS 1180 IAW SRM 53-00-52 AND SRM 51-40-02. 2L72 4F RTA2NM 20051104002312005110400231NM 2005 11 4 UPS05545696 120051031A5610 WINDSHIELD BOEING757 75724APF 1384969NM COCKPIT DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01459UP 25480 CAPT W/S CRACKED/DELAM'D AND OUT OF MM LIMITS. R/R'D L1 WINDOW UP TO & INCLUDING STEP 3, FIG 10 & PERFORMED INITIAL TORQUE COMPLIED AT 0615L. CONNECTED ELEC WIRES TO PWR TERMINIALS REF MM 56-11-01-4. ALL TORQUES COMPLIED WITH. DUE TO INCLEMENT WEATHER COULD NOT SEAL CAPT #1 WINDOW. PLACARD INSTALLED. THIS CLEARS D313149 2L72 4F RTA2NM 20051104002332005110400233WP 2005 11 4 UPS05845703 120051018A53403754916501N FITTING DOUG DC8 DC873F 302199FWP STA 1230 L31R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 FOUND "C" PIT LONGERON END FITTING CRACKED STA 1230 L31R. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20051104002342005110400234WP 2005 11 4 UPS05845658 120051011A5322 SHEAR TIE DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE FS710 L35L CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE: C2 SHEAR TIE AT STA 710 L35L IS CRACKED. REMOVED SHEAR TIE AT STA 710 L35L IAW SRM 51-1-20D, FABRICATED AND INSTALLED SHEAR TIE AT STA 710 L35L IAW DWG 5750365, AND SRM 51-1-21D. 2L74 4F4 FRT4A25 E2GL 20051104002352005110400235WP 2005 11 4 UPS05845661 120051007A5330 SKIN DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE MCD LWR AFT CRNRCRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE: C2 FUSELAGE SKIN HAS A .5 INCH CRACK AT MCD LWR AFT CORNER, UNDER REMOVED SCUFF PLATE, AT PREVIOUS CUT OUT. TRIMMED OUT CRACK AT MCD LWR AFT CORNER IAW DWG SR 08530027, FABRICATED AND INSTALLED -11 FILLERS, -4 DOUBLER AND -7 DOUBLER IAW DWG SRO8530027. 2L74 4F4 FRT4A25 E2GL 20051104002362005110400236WP 2005 11 4 UPS05845662 120051003A5320 CUSP WEB DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE FS1080 L21L CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE: C2 C CUSP CRACKED 3 INCH LONG STA 1080 L21L. REMOVED DAMAGED AREA IAW SRM 53-02-05-0 AT FS 1080 L21L FABRICATED AND INSTALLED CUSP SPLICE,-7 DOUBLER, -3 AND -5 ANGLES AND -9 CUSP IAW 51-1-21, AND SRM 53-2-5 FIG 1. 2L74 4F4 FRT4A25 E2GL 20051104002372005110400237WP 2005 11 4 UPS05845704 120051018A534038877991 FITTING DOUG DC8 DC873F 302199FWP STA 450 L14L CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 FOUND STA 450 L14L SPLICE FITTING IS CRACKED. REMOVED, FABRICATED, AND INSTALLED FITTING IAW DWG 3887799 AND DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20051104002382005110400238WP 2005 11 4 UPS05845705 120051017A53403779659U501 FITTING DOUG DC8 DC873F 302199FWP STA 860 L7R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 FOUND MAIN CARGO COMPARTMENT L7R FITTING CRACKED STA 860. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20051104002402005110400240WP 2005 11 4 UPS05845707 120051019A5322 SHEAR TIE DOUG DC8 DC873F 302199FWP 60COMP'T L3L-L3RCRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 FOUND LARGE SHEAR TIE CRACKED AT BOTH ENDS AROUND FASTENERS IN 60 COMP'T CEILING BETWEEN L3L AND L3R. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SHEAR TIE AND REPAIR PARTS IAW DWG 5612148 AND DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20051104002422005110400242WP 2005 11 4 UPS05845709 120051026A5512 RIB DOUG DC8 DC873F 302199FWP STAB LH XFS 47.5CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 FOUND LT HORIZONTAL STAB IB L/E STA XFS 47.5 RIB HAS 1/2" CRACK ON LOWER FLANGE ANGLE. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 55-2- 0 FIG 2 AND 3. 2L74 4F RT4A25 20051104002442005110400244WP 2005 11 4 UPS05845711 120051022A5330 DOUBLER DOUG DC8 DC873F 302199FWP STA -55 RBL 24 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 FOUND COCKPIT SUBFLOOR FINGER DOUBLER HAS SEVERAL SHEARED HEAD FASTENERS AT STA -55 RBL 24. REMOVED FINGER DOUBLER, FOUND CORROSION OUT OF LIMITS, FABBED, AND INSTALLED REPLACEMENT DOUBLER IAW DC-8 SRM 53-3-1 AND 51-1-21. 2L74 4F RT4A25 20051104002452005110400245 2005 11 4 HNAA0500094 420051022A3442066308601 INDICATOR DHAV DHC8 DHC8102 2809003NM WX RADAR SYS LOCKED A HNAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA07837EX3511135111 217 WEATHER RADAR LOCKED UP AND DISPLAY IS DISTORTED. REMOVED AND REPLACED THE WEATHER RADAR INDICATOR. 2H72 4T RTA13NM 20051104002462005110400246NM 2005 11 4 HNAA0500095 120051028A5610 WINDSHIELD DHAV DHC8 DHC8102 2809003NM COCKPIT CRACKED A HNAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA07937HA 148 SPARKS AND SMOKE COMING FROM NR 2 WINDSHIELD HEAT, FOLLOWED BY FO'S WINDSHIELD CRACKING. REMOVED AND REPLACED FO'S WINDSHIELD. 2H72 4T RTA13NM 20051104002482005110400248NM 2005 11 4 HNAA0500097 120051029A52108SC0156 STRUT DHAV DHC8 DHC8103 1386005NM PAX DOOR LEAKING A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07941HA4294442944 161 PAX DOOR WARNING LIGHT ILLUMINATED AT 8000FT. REMOVED AND REPLACED GAS STRUT (SHORT). 2H72 4T RTA13NM 20051104002492005110400249WP 2005 11 4 05FDEA03586 120051028A5321 FLOOR PANEL DOUG DC10 DC1010 3022110WP COCKPIT CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 FOUND COCKPIT FLOOR SECTION STA 304 BY 13 CRACK ON MEMBRANE 2'' LONG RIF SRM 53-11-01 ITEM 1. REPAIRED CRACK ON MEMBRANE RIF SRM 53-11-01 ITEM 1 STA 304 BY 13. 2L73 4F A22WE 20051104002502005110400250NM 2005 11 4 05FDEA03587 120051028A5340 STRINGER CLIP BOEING727 727225 1384077NM BS 560 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 FOUND CORROSION ON STRINGER CLIP IN FWD CARGO BAY AT BS 560, STR 26L. REPLACED STRINGER CLIP AT BS 560 STR 26L PER SRM 51-20-1. 2L73 4F A3WE 20051104002512005110400251WP 2005 11 4 05FDEA03588 120051028A5310 PANEL DOUG DC10 DC1010 3022110WP MLG WW CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25367FE 46605 NOSE LANDING GEAR WHEEL WELL RT SIDE WEB UPPER FWD CORNER APPROX 2' FROM FWD PRESSURE BULKHEAD HAS 6" DIAGONAL CRACK. CUT OUT DAMAGED SECTION OF RT UPPER WEB IN NOSE WHEEL WELL LANDING GEAR. INSTALLED REPAIR DOUBLER REF: SRM 53-00-01. SNRM N00025 EMP. 356511 2L73 4F A22WE 20051104002522005110400252NM 2005 11 4 05FDEA03589 120051028A3610 CLAMP BOEING727 727233 138408ANM PRECOOLER OUT OF POSITION A FDEAJA DUMP FUEL UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25220FE 20934 DURING CLIMB-OUT ENG NR 1 STRUT OVHT LIGHT ILLUMINATED ACCOMPLISHED ABNORMAL CHK LIST AFTER BLEED AND PACK SW'S CLOSED AND THRUST LEVER TO IDLE LIGHT OUT. INSPECT ALL THE CLAMPS ON THE NR 1 STRUT. PRESSURIZING THE DUCTS USING APU AIR FOUND CLAMP ADJACENT TO PRECOOLER LEAKING AND BLOWING HOT AIR ONTO OVHT SENSOR. REPOSTION CLAMP AND TIGHTENED, NO LEAK NOTED. STILL NEEDS HIGH POWER RUN FOR PROPER LEAK CHK. AFTER REPOSITIONING CLAMP DECIDED TO REMOVED AND REPLACED SAME CLAMP AS PRECAUTIONARY. RAN ENGINE AT TAKEOFF POWER SETTING FOR APPROX 5 MIN AS PER JRH. NO LEAKS NOTED A/C OK FOR SERVICE. 2L73 4F RTA3WE 20051104002542005110400254NM 2005 11 4 05FDEA03591 120051030A5740 FITTING BOEING727 727232 1384082NM LT WING BROKEN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 LEFT MLG LOWER TRAILING EDGE PANEL ATTACH BRACKET COMMON TO THE NR 7 SPOILER ACTUATOR FITTING IS BROKEN. REPAIRED L/H T/E CHORD PER FED-EX E.A. 7-5710-91398. 2L73 4F A3WE 20051104002562005110400256NM 2005 11 4 05FDEA03593 120051031A5311 FRAME BOEING727 727233 138408ANM FUSELAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25266FE 21672 AFT CARGO COMPARTMENT FRAME HAS CORROSION STA 1030 RBL 18 IN. REMOVED CORROSION FROM SURFACE IAW SRM 51-10-6. ID MAT BEFORE 0.063 AFTER 0.060 FOUND TO BE WITHIN LIMITS IAW SRM 53-10-10 FIG 1. TREATED AND PRIMED SRM 51-10-2. 2L73 4F RTA3WE 20051104002802005110400280WP 2005 11 4 05FDEA03542 120051027A5340 ATTACH FITTING DOUG DC10 DC1030F 3023504WP BS 595 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 FWD CARGO FOUND STA 595 LT SIDE X-95 CORROSION ON POTABLE WATER SYSTEM ATTACHMENT. ACCURATELY POLISHED AREA ON SUPPORT AND BULKHEAD IAW MM 12-22-01-7 PERFORMED VISUAL INSPECTION ON AREA FOUND LIGHT CORROSION ON SUPPORT CLAMP REMOVED CORROSION IAW SRM 51-21-01 PAR 34 VOL 2. ORIGINAL THK MATERIAL IS .100'' REMAIN MATERIAL THK IS .081''. MATERIAL REMOVED IS WITHIN LIMITS IAW SRM 53-00-01 FIG 1B VOL 1. PROTECTED REWORKED AREA IAW SRM 51-21-01 PAR 31-24 VOL 2. 2L73 4F RTA22WE 20051104002822005110400282WP 2005 11 4 05FDEA03544 120051027A5312 RIB DOUG DC10 DC1030F 3023504WP LTWING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 LEFT WING L/E ON INTERNAL STRUCTURE FOUND 1 CRACK 0.50'' LONG ON RIB AT STA XORS 427. PERFORMED INSPECTION IAW NDT SRM 06, NO CRACK FOUND ON RIB AT STA XORS427 LT WING L/E ONLY PENCIL MARK. 2L73 4F RTA22WE 20051104002912005110400291WP 2005 11 4 05FDEA03520 120051027A5753 SKIN DOUG DC10 DC1030F 3023504WP LT WING TE FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 LEFT WING OUTBD FLAP UPPER SURFACE FOUND 1 CRACK 1" LONG ON SKIN AT STA XOF 575. TRIMMED OUT DAMAGED SKIN INSTALLED FILLER AND DOUBLER IAW SRM 57-10-00 FIG 85 AND COLD BOND SRM 51-71-00 PAR 16C VOL2 AND SRM 51-35-02 PAGE 3-9. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F160231/N00231 IAW SRM 57-10-00 FIG 85. 2L73 4F RTA22WE 20051104002922005110400292WP 2005 11 4 05FDEA03521 120051027A5712 RIB DOUG DC10 DC1030F 3023504WP LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 LT WING L/E INTERNAL STRUCTURE FOUND 1 CRACK 0.50" LONG ON RIB AT STA XORS 490. REPAIRED RIB IAW SRM 57-20-00 FIG1 SHT 6 VOL 2 AND SRM 51-33-01 PAGE 34-37. 2L73 4F RTA22WE 20051104002932005110400293WP 2005 11 4 05FDEA03522 120051027A5730 PANEL DOUG DC10 DC1030F 3023504WP RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 FOUND RT WING L/E, CRACK ON CHORD FIXED PANEL AT STA XORS 442. INSTALLED REPAIR DOUBLER PER SRM 57-10-00 FIG 49 AND SRM 51-33-01 PAGE 34-47. FABRICATED PARTS IAW DETAIL PART TRAVELER F160798/N00798 PER SRM 57-10-00 FIG 49. 2L73 4F RTA22WE 20051104002942005110400294WP 2005 11 4 05FDEA03523 120051027A5712 RIB DOUG DC10 DC1030F 3023504WP LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 LT WING L/E INT STRUCTURE FOUND 1 CRACK 0.25" LONG ON RIB AT STA XORS 770. REPAIRED FORMER PER SRM 57-20-00 FIG 1 SHT 6 VOL 1 AND SRM 51-35-01 PAGE 1 3 AND SRM 51-33-01 PAGE 34-47. 2L73 4F RTA22WE 20051104002952005110400295WP 2005 11 4 05FDEA03524 120051027A5730 DOUBLER DOUG DC10 DC1030F 3023504WP LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 LT WING L/E INT STRUCTURE FOUND 1 CRACK 5" LONG ON UPPER DOUBLER AT STA XORS 660. REPAIRED BEADED DOUBLER PER SRM 57-10-00 FIG 71 VOL1 AND SRM 51-35-01 PAGE 1-13 AND SRM 51-33-01 PAGE 34-47. FABRICATED PARTS IAW DETAIL PART TRAVELER F160729/N00729 PER SRM 57-10-00 FIG 71 VOL 1. 2L73 4F RTA22WE 20051104002972005110400297NM 2005 11 4 05FDEA03555 120051027A5330 SKIN BOEING727 72722 1384002NM PWA JT8 JT8D1 52044NE BS 1081 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 FOUND MATERIAL LOSS EXCEEDS 10 PERCENT AT BS 1081 STR 10L. REPAIRED PER E.O. 7-5330-7-2313F PT 5 2L73 4F4 F A3WE E2EA 20051104002982005110400298NM 2005 11 4 05FDEA03556 120051027A5330 SKIN BOEING727 72722 1384002NM PWA JT8 JT8D1 52044NE BS 361 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 FOUND MATERIAL LOSS EXCEEDS 10 PERCENT AT BS 361 STR 19. REPAIRED PER E.O. 7-5330-7-2319 PT 5 2L73 4F4 F A3WE E2EA 20051104002992005110400299NM 2005 11 4 05FDEA03557 120051027A5330 SKIN BOEING727 72722 1384002NM PWA JT8 JT8D1 52044NE BS 261 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 FOUND MATERIAL LOSS EXCEEDS 10 PERCENT AT BS 261 STR 14R. REPAIRED PER E.O. 7-5330-7-2319 PT 5 2L73 4F4 F A3WE E2EA 20051104003002005110400300NM 2005 11 4 05FDEA03558 120051027A5330 SKIN BOEING727 72722 1384002NM PWA JT8 JT8D1 52044NE BS 361 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 FOUND MATERIAL LOSS EXCEEDS 10 PERCENT AT BS 361 STR 10R. REPAIRED PER E.O. 7-5330-7-2319 PT 5 2L73 4F4 F A3WE E2EA 20051104003022005110400302EU 2005 11 4 05FDEA03561 120051027A5310 WINDOW FRAME AIRBUS300 A300B4622R 3930312EU COCKPIT CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25723FD 543 RT WINDSHIELD FRAME LOWER SECTION BETWEEN FRAMES 4 AND 2 HOLE WITH FASTENER REMOVED HAS CRACK INDICATION REF N00029. COMPLIED WITH EA 6-5310-93391. 2L72 4F RTA35EU 20051104003042005110400304WP 2005 11 4 05FDEA03566 120051028A5330 DOUBLER DOUG DC10 DC1030F 3023504WP BS 885 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 FOUND DOUBLER LENGTH 8.5 INCH WIDTH 6 INCHES ON RT EXTERNAL FUSELAGE AT STA 885 FROM L 31 TO L32. REMOVED AND REPLACED REPAIR IAW SRM 53-50-00 FIG 8 AND FEDEX EA NR 8-5350-88889 FAB PARTS IAW DETAIL PARTS TRAVELER F160357-1 AND F160357-2 IAW SRM 53-50-00 FIG 8 VOL 1. 2L73 4F RTA22WE 20051104003062005110400306CE 2005 11 4 DXTA200501045 120051031A3240 BRAKE CESSNA500 560CESSNA 2076750CE MLG MALFUNCTIONED E DXTAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07325QS 5600425 PILOTS LEFT BRAKE ALMOST GOES TO THE FLOOR. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20051104003082005110400308CE 2005 11 4 DXTA200501043 120051028A3220 LANDING GEAR CESSNA750 750 2076810CE NOSE MALFUNCTIONED E DXTAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL07961QS 7500061 DURING CLIMB THROUGH FL 250-350 NOSE GEAR THUMPS, NO UNLOCK LIGHT NOTICED. ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20051104003102005110400310CE 2005 11 4 DXTA200501040 120051028A3411 PITOT HEAD CESSNA500 560CESSNA 2076750CE DIRTY E DXTAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 GL07309QS 5600509 DURING THE T/O ROLL AT APPROX 40 TO 60 KNOTS CAPT A/S INDICATOR REMAINED BLANK AND A/S COMPARISON MONITOR ILLUMINATED. T/O WAS ABORTED. VERIFIED DISCREPANCY. NOTED DIRT DEBRIS IN LT PITOT. PURGED PITOT LINE & TUBE WITH AIR. LEAK TEST CHECKS GOOD. AIRSPEED OPERATIONAL CHECKS GOOD. MAINTENANCE DONE IAW 560 MAINTENANCE MANUAL CH 34-11-05. 2L72 4F RTA22CE 20051104003122005110400312CE 2005 11 4 DXTA200501039 120051026A3230 LANDING GEAR CESSNA500 560CESSNA 2076750CE LEFT MALFUNCTIONED E DXTAO OTHER J WARNING INDICATION APAPPROACH 1 GL07801QS 5600601 WENT TO LOWER THE GEAR AND THE LEFT MAIN GREEN LIGHT NEVER ILLUMINATED. ALSO HAD A RED GEAR UNSAFE LIGHT, A WARNING HORN AND THE HYD PRESS ANNUNCIATOR STAYED ILLUMINATED. APPROX 2 TO 3 MIN LATER THE LEFT MAIN CAME DOWN BY ITSELF AND ALL OTHER INDICATIONS WERE NORMAL. JACKED A/C FOR GEAR SYSTEM TROUBLESHOOTING. READ OUT RESISTANCE OF LEFT DOWN AND LOCKED SWITCH AND FREEZE SWITCH. RESISTANCE ACROSS SWITCH CONTACT -0 OHMS-. CHECKED GEAR CONTROL AND GEAR MONITOR ECB FOR VISUAL DEFECTS AND SEATING IN SOCKET, NO FAULTS FOUND. CYCLED GEAR REPEATEDLY AND PERFORMED OPERATIONAL CHECKS. ALL INDICATIONS NORMAL, NO FAULTS. ALL WORK PERFORMED IAW CE 560 M/M 32-01011-712 AND CE 560 M/M 32-30-0101. 2L72 4F RTA22CE 20051104003142005110400314NM 2005 11 4 DHL2005742522 120050916A5753 SKIN BOEING727 727225 1384077NM LT WING TE FLAP CHAFED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15742DH 21290 LT O/B MID FLAP I/B END L/E CUT AND CHAFED. REMOVED DOUBLER IAW B727 SRM 51-10-1 AND 51-30-2. FABRICATED AND INSTALLED DOUBLER REPAIR 7" BY 6.0" BY 3.2" FROM 2024-T3 .040 IAW B727 SRM 51-10-2, 57-50-4. 2L73 4F A3WE 20051104003162005110400316NM 2005 11 4 DHL2005742524 120050916A5753 SKIN BOEING727 727225 1384077NM FLAP DEBONDED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15742DH 21290 LT I/B AFT FLAP HAS AREA OF DISBOND NEAR I/B END. FABRICATED AND INSTALLED DOUBLER REPAIRS 8.2" BY 7.5" AND 5.2" BY 4.5" FROM 2024-T3 .016 AND 5.1" BY 4.4" FROM BMS 4.4 HONEYCOMB IAW B727 SRM 51-40-20, 51-40-23 AND 57-50-2 NOTE G. 2L73 4F A3WE 20051104003182005110400318NM 2005 11 4 DHL2005742526 120050916A5753 SKIN BOEING727 727225 1384077NM FLAP CHAFED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15742DH 21290 RT WING O/B MID FLAP CHAFFED EXISTING REPAIR I/B TOP. REMOVED EXISTING REPAIR. FABRICATED AND INSTALLED FORMED ANGLE REPAIR 7" BY 2.30" BY .75" FROM 2024-T3 .063 IAW B727 SRM 57-20-2 FIG 5, 51-20-1 PARA 7, 51-30-6 FIG 3 51-10-2, 51-40-3 FIG 1 AND 51-30-2 PARA B. 2L73 4F A3WE 20051104003202005110400320NM 2005 11 4 DHL2005742528 120050923A5751 HINGE BOEING727 727225 1384077NM AILERON NICKED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15742DH 21290 RT AILERON O/B HINGE FITTING O/B SIDE (ON WING) FITTING NICKED AND GOUGED AROUND BUSHING. BLENDED GOUGE FOUND OUT OF LIMITS IAW BOEING DRAWING 65-19259-8. DRILLED, DEBURRED AND INSTALLED NEW FITTING, P/N 65-19259-6 IAW B727 SRM 51-30-2. 2L73 4F A3WE 20051104003222005110400322NM 2005 11 4 DU4R2005221 120051101A5340 STRINGER CLIP BOEING757 757232 1384965NM BS 1620 CORRODED B DALAK NONE O OTHER ININSP/MAINT 1 SO15693DL 29725 FOUND CORROSION ON CLIP AT STR-30 BL 0 BS 1620. REMOVED STRINGER CLIP. FABRICATED AND INSTALLED NEW REPAIR STRINGER CLIP 6" BY 1" FROM 7075-T6 .050 IAW B757 SRM 51-40-02, 51-70-11, 53-00-03, 51-20-02 AND 51-40-02. 2L72 4F RTA2NM 20051104003232005110400323NM 2005 11 4 DL738050667 120051028A3320 SOCKET BOEING737 737832 13844CFNM PSU LOOSE A DALAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27392DA 30561 DURING PUSHBACK AFT FLT ATTENDANT REPORTED THE AFT GALLEY (PORT SIDE) NO SMOKE/SEAT BELT SIGN HANGING OUT OF SOCKET. WHEN PUTTING SIGN BACK IN THE WIRING STARTED SPARKING, WITH SMELL OF SPARKING. DROPPED ALL ELEC OFF LINE, RETURN TO GATE AREA. FOUND C/B POPPED. AFT GALLEY LEFT FASTEN SEAT BELT TERMINAL INTERFERING WITH FRAME OF GALLEY OPENING. REPOSITIONED TERMINAL. RELAMPED, ALL LIGHTS CHECK GOOD. 2L72 4F RTA16WE 20051104003242005110400324NM 2005 11 4 DLM90050668 120051028A5210 GUIDE ARM DOUG MD90 MD9030 3023690NM PAX DOOR OUT OF ALIGNMENTA DALAO OTHER O OTHER CLCLIMB 1 SO27913DN 53393 FLOW LIGHT ILLUMINATED ON CLIMBOUT. GOOD FLOW ON BOTH PACKS FLT ATTENDANT REPORTED LOUD NOISE AT 2 LEFT DOOR. MAX CABIN ALT 9000. CABIN PRESSURE 2 PSID. FOUND DOOR GUIDE ARM ON WRONG SIDE OF ROLLER MECHANISM AND GUIDE ROLLERS NOT SEATED IN GUIDES. LUBRICATED DOOR GUIDE MECHANISM AS PRECAUTIONARY, EXERCISED DOOR SEVERAL TIMES. CHECKS GOOD. PRESSURIZES A/C TO 4.0 PSI. NO LEAKS NOTED. 2L72 4F RTA6WE 20051104003262005110400326NM 2005 11 4 DL767050670 120051028A2910S256T00610 SHUTOFF VALVE BOEING767 767232 1385132NM HYD SYSTEM LEAKING A DALAO OTHER KJ FLUID LOSS WARNING INDICATION LDLANDING 1 SO27114DL 22226 EICAS MESSAGE -L/E SLAT DISAGREE- ILLUMINATED WHEN THE FLAP LEVER WAS PLACED AT 1 DEGREE POSITION. FOLLOWED QRH PROC AND SLATS EXTENDED ELECTRICALLY AND FLAPS EXTENDED HYDRAULICALLY. L/E SLAT DISAGREE MSG WAS NOT ILLUMINATED DURING MTC CHECK. PERFORMED BITE CHECK ON BOTH FSEU AND PSEU WITH NO FAULTS. PUT ALTN FLAP AND L/E SWITCH BACK TO NORMAL AND RAN FLAP/SLAT SEVERAL TIMES WITH NO FAULTS. DURING FURTHER CHECK FOUND FLAP/SLAT HYD SHUTOFF VALVE LEAKING HYD FLUID. REPLACED SAME. 2L72 4F RTA1NM 20051104003272005110400327NM 2005 11 4 DL764050671 120051029A2720 RUDDER PEDAL BOEING767 767432ER 1385134NM RUDDER CONTROL OUT OF ADJUST A DALAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 SO27834MH 29707 RETURNED TO BLOCKS DUE TO ON TAXI OUT DURING FLT CONTROL CHECK OF LT RUDDER INPUT HEARD A LOUD BANGING SOUND. FOUND RUDDER PEDAL ADJ ALL THE WAY AFT WITH LT RUDDER INPUT OR RT RUDDER INPUT ON EITHER SIDE PEDAL HITS METAL COVER. ADJUSTED FULL FORWARD AND FULL AFT, OPS CHECK GOOD PER FIM 27-21-00 PG 113. NO TROUBLE FOUND, OPERATION NORMAL. 2L72 4F RTA1NM 20051104003282005110400328NM 2005 11 4 DL76S050672 120051030A3230 DRAG BRACE BOEING767 767332 1382001NM LT MLG LOOSE A DALAO OTHER O OTHER LDLANDING 1 SO27138DL 25409 LANDING GEAR UNSAFE AURAL WARNING AND GEAR DOOR LIGHT ILLUMINATED ON LANDING TOUCHDOWN. REPLACED LEFT MLG UPPER DRAG BRACE SPINDLE. INSPECTED GEAR AS PER ERA 01-0451457-14. 2L72 4F RTA1NM 20051104003292005110400329NM 2005 11 4 DL76L050673 120051030A2121732591B FAN BOEING767 767332 1382001NM FWD CARGO FAILED A DALAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27171DN 24759 AFTER PUSHBACK AND ENGINE START SMOKE ODOR NOTICED IN CABIN. EICAS MESSAGE FORWARD EQ SUP FAN. REPLACED FAN. 2L72 4F RTA1NM 20051104003302005110400330NM 2005 11 4 DL76G050675 120051102A2750285T004963 FSEU BOEING767 767332 1382001NM TE FLAPS FAILED A DALAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SO271604R 30180 ON APPROACH T/E FLAP DISAGREE WHEN FLAPS 25 SELECTED RIGHT SIDE STAYED AT 20 LEFT WENT TO 25. LANDED WITH T/E FLAPS 20. REPLACED FSEU AND POSITION INDICATOR. 2L72 4F RTA1NM 20051104003312005110400331NM 2005 11 4 DL76L050676 120051102A335020121 CHARGER BOEING767 767332 1382001NM CABIN UNKNOWN A DALAK NONE L NO TEST ININSP/MAINT 1 SO27181DN 25986 MID CABIN SEAT EMERGENCY LIGHTS FROM SEAT ROW 6-20 FG. REPLACED POWER SUPPLY. 2L72 4F RTA1NM 20051104003322005110400332NM 2005 11 4 DLM88050677 120051102A2170 COALESCER BAG DOUG MD88 MD88 3023688NM CABIN DIRTY A DALAC ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SO27958DL 49977 ODOR IN COCKPIT AND CABIN. AIR TURNBACK. REPLACED COALESCER BAGS, PERFORMED DUCT BURN OUT AND HIGH PWR RUN. 2L72 4F RTA6WE 20051104003332005110400333NE 2005 11 4 DL76S050662 220051026A7250CF680A2 ENGINE BOEING767 767332 1382001NM GE CF680 CF680A2 NE NR 2 MAKING METAL A DALAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 SO27127DL57230 24077 580164 IN CRUISE, THE RT ENG HAD VIBRATION TO 5.0. DURING T/S IN FLT, THE ENG ANALYST AT HOME GOT A SMART SIGNAL THAT SHOWED A SHIFT IN F/F GET AND LOW N-2 ROTOR SPEED OCCURRED. CALLED THE MTC COORDINATOR WHILE ON THE RADIO PATCH AND ADVISED WHAT OBSERVED. ADVISED THE CREW TO RETURN TO ATL, METAL WAS FOUND IN THE TAIL PIPE AND ENGINE WAS REPLACED. 2L72 4F4 FRTA1NM E13NE 20051104003342005110400334NM 2005 11 4 USAA051266 120051031A5311 FRAME BOEING737 7373B7 1384580NM STA480 S-9L ON FCRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND FRAME CRACKED, STA 480 S-9L ON FRAME AT PSU RAIL. CUT OUT DAMAGE. INSTALL REPAIR DOUBLERS IAW TR 53-10-20, DEFECT SIZE: .25". 2L72 4F RTA16WE 20051104003372005110400337 2005 11 4 WRLA2005145 420051102A2565 SLIDE DOUG MD11 MD11F 3023600NM PWA 4460 PW4460 NE L1 DOOR DEPLOYED A WRLAK NONE O OTHER TXTAXI/GRND HDL 1 SO11381 48523 L1 DOOR SLIDE WAS INADVERTANTLY DEPLOYED; SLIDE DID NOT INFLATE BECAUSE THE BOARDING STAND WAS IN PLACE AND PREVENTED IT FROM DROPPING FAR ENOUGH TO ACTIVATE. REPACKED AND REPLACED SLIDE ON L1 DOOR PER AIRCRAFT MAINTENANCE MANUAL PRACTICES. 2L73 4F4 FRTA22WE E24NE 20051104003382005110400338NM 2005 11 4 USAA051322 120051102A575465C26601197 SKIN BOEING737 7374B7 1384702NM NR 1 SLAT DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19779AU 24996 NR 1 SLAT WITH FLUSH PATCH. MAJOR REPAIR IAW SRM 57-43-01, DEFECT SIZE: 5.5" BY 3.5". 2L72 4F RTA16WE 20051107000012005110700001NM 2005 11 7 SB05142 120051101A33501012721 LIGHT BOEING737 737401 1384701NM SEAT 12C INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19419US 23986 PHL - PILOT REPORTED THE EMERGENCY EXIT LIGHT AT SEAT 12C INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT AT SEAT 12C. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20051107000032005110700003NM 2005 11 7 SB05143 120051103A2120AB0470044 FILTER BOEING737 7374B7 1384702NM AIR CON BAY DIRTY A USAAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 EA19430US 24552 ON SHORT FINAL, THE FLIGHT ATTENDANTS REPORTED FUMES IN THE CABIN. WITH PACKS ON HIGH, FUMES DECREASED. WITH PACKS ON AUTO, FUMES INCREASED. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND TAXIED TO THE GATE. MAINTENANCE INSPECTED LEFT AND RIGHT PACK BAY AREAS FOR DEFECTS. NO DEFECTS FOUND. REMOVED AND REPLACED LEFT AND RIGHT RECIRCULATION FAN FILTERS PER MM 21-21-23. GROUND RAN LEFT AND RIGHT PACKS WHILE SUPPLYING AIR WITH APU AND LEFT AND RIGHT ENGINES. NO FUMES NOTED. 2L72 4F RTA16WE 20051107000042005110700004EU 2005 11 7 2005102901 120051029A2130 CABIN PRESSURE EMB ERJ170ERJ170100 EU MALFUNCTIONED A UHLABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL17856RW 17000078 FLIGHT 6438 JFK-AUS AUTO PRESSURIZATION MALFUNCTION, PASSENGER OXYGEN MASKS DEPLOYED. AIRCRAFT MADE A EMERGENCY DESCENT & DIVERTED TO SHV. 2L74 4F RTA56NM 20051107000052005110700005NM 2005 11 7 TSAA0529051 120051023A29106590737329 HOSE BOEING737 7372T4 1384492NM HYD SYSTEM LEAKING A TSAAO OTHER KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP13807AL 23443 NON-ETOPS FLIGHT 88 LIH-HNL - AFTER GEAR UP, HYD PRESSURE INDICATOR SHOWED ZERO. LEFT MAIN LANDING GEAR INDICATOR LIGHTS SHOWED BOTH RED AND GREEN (UNSAFE). WHEN EXTENDING FLAPS AND GEAR, HYD SYSTEM A PRESSURE FLUCTUATED AND A SYSTEM LOW PRESSURE CAUTION LIGHT ILLUMINATED. PRESSURE RETURNED TO NORMAL AFTER GEAR AND FLAPS WERE EXTENDED. CREW LANDED IN HNL WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED A LEAKING HYDRAULIC LINE BETWEEN THE LEFT HAND MAIN LANDING GEAR AND TRANSFER TUBE. LEAK CHECKED OK AND PERFORMED ENGINE RUN AND FUNCTION CHECK OF FLIGHT CONTROLS. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A16WE 20051107000062005110700006NM 2005 11 7 TSAA0529052 120051023A2910 FILTER BOEING737 7372T4 1384492NM HYD SYSTEM CONTAMINATED A TSAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13807AL 23443 NON-ETOPS FLIGHT 278 HNL - KOA, AFTER TAKEOFF, NR 1 ENGINE HYDRAULIC SYSTEM A LOW PRESSURE LIGHT ILLUMINATED. CREW DISENGAGED ENGINE DRIVEN HYDRAULIC PUMP AND RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND CHANGED HYDRAULIC SYSTEM A CASE DRAIN FILTERS, PRESSURE MODULE FILTERS AND RETURN FILTER. LEAK CHECK OK. NO FLUID CONTAMINATION NOTED. MAINTENANCE CONDUCTED A GEAR SWING CHECK WITH NO DEFECTS FOUND. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F A16WE 20051107000072005110700007NM 2005 11 7 TSAA0529053 120051101A29136507506 PUMP BOEING737 737230 1384401NM HYDRAULIC SYS MALFUNCTIONED A TSAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13820AL 22138 NON-ETOPS FLT 266 HNL-OGG, AFTER TAKEOFF, HYD SYS QUANTITY INDICATION DROPPED TO 1.5 GAL. AND SYSTEM A LOW PRESSURE LIGHT ILLUMINATED. CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE SERVICED HYDRAULIC RESERVOIR TO FULL, PERFORMED ENGINE RUN, OPERATED HYDRAULIC SYSTEM AND CONDUCTED A VISUAL INSPECTION NR 1 ENGINE CASE DRAIN FILTER. NO HYDRAULIC SYSTEM LEAKS NOTED. FOUND NR 2 ENGINE HYDRAULIC SYSTEM A PUMP LOW PRESSURE LIGHT INTERMITTENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP, IN ACCORDANCE WITH AMM 29-11-31. ENGINE RUN AND LEAK CHECK VERIFIED OK. 2L72 4F RTA16WE 20051107000082005110700008EA 2005 11 7 SWIA200515771 120050613A5311 CLIP CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07970SW 7881 FWD AVIONICS COMPARTMENT STA 280 LBL 9 INBD FRAME CLIP CRACKED, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW FRAME CLIP IAW CRJ200 SRM 51-42-06 AND 51-42-21. 2L72 4F RTA21EA 20051104001462005110400146WP 2005 11 4 IXXA05SMN226S 120051013A5330 RIVET DOUG DC8 DC871F 302199DWP FS 1384. L-34-75IMPROPER B IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW11829BX896722998 45994 DURING C CHECK INSPECT, AFT LWR FUSELAGE BELLY, STA FS 1384.000 L-35-75R, UPGRADE REPAIR DOUBLER TO INCORPORATE A MIN OF 3 ROWS OF RIVETS (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-1 FIG 7, EO SEMAN # 20051199 DATED 09-20-05. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D. REMOVED DAMAGED SECTION IAW DC8 SRM 53-2-1 FIG 7 (SHEET 1-3). PERFORMED NDT INSP OF REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D REPAIR DOUBLER (AL7075T6 0.080”), (02 EA) INTERNAL FINGER DOUBLERS (AL7075T6 0.050”) IAW DC8 SRM 53-2-1 FIG 7 (SHEET 1-3), DC8 SRM 53-4-1 FIG 16 (SHEET 2) ITEM “B”, DC8 SRM 51-9-0 FIG 68. CLEANED, TREATED, PRIMED AREA, REPAIR PARTS2L74 4F RT4A25 20051104001482005110400148WP 2005 11 4 IXXA05SMN228S 120051013A5330 RIVET DOUG DC8 DC871F 302199DWP FS 1693 IMPROPER B IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW11829BX896722998 45994 DURING C CHECK INSPECT, AFT LWR FUSELAGE BELLY, STA FS 1693.000 L-30.75L. UPGRADE REPAIR DOUBLER TO INCORPORATE A MIN OF 3 ROWS OF RIVETS (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-1 FIG 7, EO SEMAN # 20051203 DATED 09-20-05. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21. REMOVED DAMAGED SECTION IAW DC8 SRM 53-2-1 FIG 7 (SHEET 1, 5). NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D REPAIR DOUBLER (AL7075T6 0.063”), INTERNAL FINGER DOUBLER (AL7075T6 0.032”), FILLER (AL7075T6 0.050”) IAW DC8 SRM 53-2-1 FIG 7 (SHEET 1, 5), DC8 SRM 53-5-1 ITEM “E” FIG 1, DC8 SRM 51-1-4 PG 1 (FORMING). CLEANED, TREATED, PRIMED AREA + REPAIR PARTS IAW DC8 S2L74 4F RT4A25 20051104001502005110400150WP 2005 11 4 IXXA05SMN230S 120051013A5730 SKIN DOUG DC8 DC871F 302199DWP XW 77.000 DENTED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX* 2998 45994 DURING C CHECK INSPECT, LT INBD FLAP UPPER SKIN DENTED, XW 77.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-5 FIG 1, EO SEMAN #20051207 DATED 09-21-05. REMOVED FASTENERS IAW DC8 SRM 51-1-21, DC8 SRM 51-1-21, DC8 SRM 51-3-0. REMOVED DAMAGED SECTION IAW DC8 SRM 57-2-5 FIG 1. PERFORMED DETAIL VISUAL INSP OF REWORK AREA. NEITHER CRACK NOR CORROSION FOUND. FAB`D NEW PLATING SEGMENT (AL2024T3 0.050”), (02EA) INTERNAL SPLICES (AL2024T3 0.063”), FILLER (AL2024T3 0.020”) IAW DC8 SRM 57-2-5 FIG 1 (SHEET 1-2), DC8 SRM 57-7-1 FIG 1 ITEM “A”. CLEANED, TREATED, PRIMED AREA, REPAIR PARTS IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-21, DC8 SRM 51-3-0, DC8 SRM 51-3-1. 2L74 4F RT4A25 20051104001542005110400154WP 2005 11 4 IXXA05SMN213S 120050927A5340 FITTING DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE 445.000 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING ROUTINE C CHECK INSPECTION, FWD LOWER FUSELAGE SPLICE FITTING CRACKED 8, STA 445, STA 455.000 L-31L. REMOVED CRACKED FITTING IAW SRM 51-1-20D, SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-0 PAGE 1. TORQUED IAW SRM 51-3-1 PAGE 2A. 2L74 4F4 FRT4A25 E2GL 20051104001562005110400156WP 2005 11 4 IXXA05SMN215S 120050927A5340 FITTING DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE 1770.00 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING ROUTINE C CHECK INSPECTION, AFT FUSELAGE SPLICE FITTING CRACKED 2, STA 1770.000 RT, L-17R. REMOVED CRACKED FITTING IAW SRM 51-3-0, SRM 51-21-1. FABRICATED NEW FITTING (AL7075T651) IAW ATI REPAIR SPECIFICATION NR 2003-05, EA SEMAN NR 20051318. HEAT TREATED FROM AL7075T651 TO AL7075T6 IAW SRM 51-1-1 PG 1, 13, 17. (ENCLOSED SMN FORM NR 075) + PERFORMED NDT INSPECTION OF NEW FITTING IAW NDT SPM PART 08-00-02 TO 07. CLEANED, TREATED AND PRIMED AREA + NEW FITTING IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-21, SRM 51-3-0, SRM 51-3-1 (TORQUE). 2L74 4F4 FRT4A25 E2GL 20051104001582005110400158WP 2005 11 4 IXXA05SMN183S 120050920A5330 SKIN DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE 12.000 L27R CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING ROUTINE C CHECK INSPECTION, NOSE SECTION. RT PRIMARY HEAT EXCHANGER AFT LWR CORNER HAS STRUCTURAL MODIFICATION CRACKED .7500 ON DOUBLER STA 12.000 L-27R. PERFORMED MAJOR REPAIR IAW MM 53-30-09, EO SEMAN NR 20051205 DATED 09-21-05. REMOVED FASTENERS IAW SRM 51-1-21. REMOVED DAMAGED SECTION IAW SRM 53-30-09 PG 207. PERFORMED NDT INSP OF REWORKED AREA IAW NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FABRICATED REPAIR DOUBLER (AL7075T6 0.100) + FILLER (AL7075T6 0.100) IAW MM. CLEANED, TREATED, PRIMED AREA + REPAIR PARTS IAW SRM. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW MM 53-30-09 PG 201-202, 208-209, SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2L74 4F4 FRT4A25 E2GL 20051104001602005110400160WP 2005 11 4 IXXA05SMN207S 120050927A5340 FITTING DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE 1215.000 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING ROUTINE C CHECK INSPECTION, AFT LWR CARGO BILGE INTERIOR, FITTING CRACKED 2, STA 1215.000 L-29R. REMOVED CRACKED FITTING IAW SRM 51-3-0 PG 1. CLEANED, TREATED, PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-3-0, SRM 51-1-20D, SRM 51-3-1. 2L74 4F4 FRT4A25 E2GL 20051104001622005110400162WP 2005 11 4 IXXA05SMN220S 120050929A5730 SKIN DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE ZONE 800 SCRATCHED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING ROUTINE C CHECK INSPECTION, EXTERNAL FUS. (C) BELLY PIT DOOR SKIN SCRATCHES OUT OF LIMITS. PERFORMED MAJOR REPAIR, REMOVED FASTENERS IAW SRM 51-1-20D. REMOVED DAMAGED SECTION IAW DWG NR ED-4075. NDT INSPECTED IAW NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FABRICATED REPAIR DOUBLER (AL7075T6 0.190”) + FILLER PLUG (AL7075T6 0.250”) IAW DWG NR ED-4075. TAPERED REPAIR DOUBLER FROM 0.190 TO 0.08 IAW DWG ED-4075. CLEANED, TREATED, PRIMED AREA + REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW DWG NR ED-4075, SRM 51-1-20D, SRM 51-3-0, SRM 51-3-1 (TORQUE) FOR FUEL LEAK CK. 2L74 4F4 FRT4A25 E2GL 20051104001642005110400164WP 2005 11 4 IXXA05SMN187S 120050922A5330 RIVET DOUG DC8 DC871F 302199DWP FS 399.000 IMPROPER B IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW11829BX896722998 45994 DURING C CHECK INSPECT, FWD LWR FUSELAGE BELLY, STA FS 399.000 L-35.75R UPGRADE REPAIR DOUBLER TO INCORPORATE A MINIMUM OF 3 ROWS OF RIVETS. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05448 DATED 10-05-05, SEMAN DWG NR ED-4060 DATED 10-03-05, EO SEMAN NR 20051193 DATED 10-05-05. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21. REMOVED DAMAGED AREA IAW SEMAN DWG NR ED-4060. PERFORMED NDT INSPECTION. NO CORROSION, CRACK FOUND IAW NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D REPAIR DOUBLER (AL7075T6 0.080) + (06EA) INTERNAL FINGER DOUBLERS (AL7075T6 0.032) IAW SEMAN DWG NR ED-4060. CLEANED, TREATED, PRIMED AREA, REPAIR PARTS IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURF2L74 4F RT4A25 20051104001662005110400166WP 2005 11 4 IXXA05SMN189S 120050922A5330 RIVET DOUG DC8 DC871F 302199DWP FS 1683.000 IMPROPER B IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW11829BX896722998 45994 DURING C CHECK INSPECT, AFT LWR FUSELAGE BELLY, STA FS 1683.000 L-35.5R, UPGRADE REPAIR DOUBLER TO INCORPORATE A MIN OF 3 ROWS OF RIVETS. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05448 DATED 10-05-05, SEMAN DWG NR ED-4063 DATED 10-03-05, EO SEMAN NR 20051201 DATED 10-05-05. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D. REMOVED DAMAGED SECTION IAW SEMAN DWG NR ED-4063. NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D REPAIR DOUBLER (AL7075T6 0.080”) + FILLER INTERNAL DOUBLER (AL7075T6 0.090”) + FILLER (AL7075T6 0.071”) IAW SEMAN DWG NR ED-4063. CLEANED, TREATED, PRIMED AREA, REPAIR PARTS IAW DC8 SRM 51-1-8B. APPLIED SEA2L74 4F RT4A25 20051104001692005110400169WP 2005 11 4 IXXA05SMN205S 120050927A5730 SKIN DOUG DC8 DC871F 302199DWP XFS 285.250 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING C CHECK INSPECT, LT WING CTR L/E SKIN CRACKED ½, STA XFS 285.250. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 # 05451 DATED 10-07-05, SEMAN DWG # ED-4066 DATED 10-03-05, EO SEMAN # 20051212 DATED 10-07-05. REMOVED FASTENERS IAW DC8 SRM 51-1-21, DC8 SRM 51-3-0. REMOVED DAMAGED SECTION IAW SEMAN DWG # ED-4066. NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FABRICATED REPAIR DOUBLER (AL7075T6 0.071) + FILLER (AL7075T6 0.063) IAW SEMAN DWG NR ED-4066, DC8 SRM 51-1-4 PG 1 (FORMING). CLEANED, TREATED, PRIMED AREA, REPAIR PARTS IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW SEMAN DWG # ED-4062L74 4F RT4A25 20051104001732005110400173WP 2005 11 4 IXXA05SMN211S 120050927A5340 FITTING DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE 445.000 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING ROUTINE C CHECK INSPECTION, FWD CARGO COMPT RT TUNNEL SPLICE FITTING CRACKED 2, STA 445.000 L-27R REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-20D PAGE 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW SPLICE FITTING IAW SRM 51-1-20D AND TORQUED NUT IAW SRM 51-3-1 PAGE 2A. 2L74 4F4 FRT4A25 E2GL 20051104001752005110400175WP 2005 11 4 IXXA05SMN182S 120050920A5210 DOOR DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE 130.000 L-21L CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING ROUTINE C CHECK INSP, FWD ENTRANCE DOOR.- JAMB FWD LWR CORNER CRACKED, STA 130.000 L-21L.PERFORMED MAJOR REPAIR IAW AD 2000-20-08, S/B 53-075, SRM 53-2-0 FIG 15 SHEET 2, SRM 53-2-0, TR NR 53-196, MFG DWG NR SRD8530021, EO NR 20051204 DATED 09-21-05, DWG NR 5750776. REMOVED FASTENERS IAW SRM 51-1-21. REMOVED DAMAGED SECTION IAW SRM. NDT INSPECTED REWORKED AREA IAW NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FABRICATED REPAIR DOUBLER, REPAIR TRIPLER, FILLER, IAW SRM (SHEET 2), TR NR 53-196, DWG NR SRD85330021, SRM (FORMING). CLEANED, TREATED, PRIMED AREA REPAIR PARTS IAW SRM. APPLIED SEALANT TO FAYING SURFACES IAW SRM. INSTALLED REPAIR PARTS IAW SRM. (TORQUE). 2L74 4F4 FRT4A25 E2GL 20051104001772005110400177WP 2005 11 4 IXXA05SMN236S 120051013A5700 SKIN DOUG DC8 DC871F 302199DWP XF 210.000 IMPROPER B IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW11829BX896722998 45994 DURING C CHECK INSPECTION, RT OTBD FLAP UPPER SKIN HAS NON STANDARD REPAIR, STA XF 210.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 57-7-1 FIG 4, TR#57-94, EO SEMAN # 20051288 DATED 09-28-05. REMOVED DAMAGED PLATING IAW DC8 SRM 57-1-0, DC8 SRM 51-1-21. FABRICATED NEW PLATING (AL2024T3 0.040”) IAW DC8 SRM 57-7-1 FIG 4, TR#57-94 ITEM “C”, DC8 SRM 51-1-4 PG 1 (FORMING). CLEANED, TREATED, PRIMED AREA + NEW PLATING INNER FACE IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACE IAW DC8 SRM 51-1-11 PG 9. INSTALLED NEW PLATING IAW DC8 SRM 51-1-21. 2L74 4F RT4A25 20051104001792005110400179WP 2005 11 4 IXXA05SMN239S 120051013A5512 SKIN DOUG DC8 DC871F 302199DWP XFS 78.750-85.00DENTED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING ROUTINE C CHECK INSPECTION, LT HORIZONTAL STABILIZER L/E UPPER SKIN DENTED, XFS 78.750 XFS 85.00. PERFORMED MAJOR REPAIR IAW DC8 SRM 55-2-1 FIG 4, EO SEMAN # 20051292 DATED 09-27-05. REMOVED EXISTING REPAIR DOUBLER NEXT DENT IAW DC8 SRM 51-1-21. REMOVED DAMAGED AREA IAW DC8 SRM 55-2-1 FIG 4. PERFORMED NDT INSPECTION TO INDICATED AREA, NO CRACK, CORROSION FOUND IAW NDT SPM PART 06-10-01-001. FAB`D REPAIR DOUBLER, FILLER (AL7075T6 O.O50”) IAW DC8 SRM 55-2-1 FIG 4, DC8 SRM 55-3-1 FIG 1 ITEM “A”. CLEANED, TREATED, PRIMED AREA + REPAIR DOUBLER INTERNAL PART IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED REPAIR DOUBLER IAW DC8 SRM 55-2-1- FIG 4, DC8 SRM 51-1-22L74 4F RT4A25 20051104001852005110400185WP 2005 11 4 IXXA05SMN195S 120050922A5751 SKIN DOUG DC8 DC8* WP GE CFM56 CFM56* 13802NE XA 502.000 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING ROUTINE C CHECK INSPECTION, LT WING IB AILERON UPPER PLATING CRACKED 1, XA 502.000 PERFORMED MAJOR REPAIR IAW SRM 57-7-0 FIG 1, SRM 57-8-1 FIG 1, EO SEMAN NR 20051336. REMOVED DAMAGED PLATING IAW SRM 51-1-21. FABRICATED NEW PLATING (AL7075T6 0.040) IAW SRM 57-8-1 FIG 1 ITEM R. CLEANED, TREATED, PRIMED AREA + NEW PLATING INTERNAL PART IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACE IAW SRM 51-1-11 PG 9. INSTALLED NEW PLATING IAW SRM 51-1-21, SRM 51-3-0, SRM 51-3-1. FOR WEIGHT AND BALANCE SEE N/R 2815. 2L74 4J4 FF 4A25 E2GL 20051104001872005110400187WP 2005 11 4 IXXA05SMN218S 120050929A5340 FITTING DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE 60.070.000 CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING ROUTINE C CHECK INSPECTION, FWD ACCY COMPT FITTING CORRODED, STA 60.000, 70.000 L-34R. REMOVED CORROSION FROM FITTING IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED FITTING IAW SRM 51-1-21, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-1-21 AND TORQUED NUTS IAW SRM 51-3-1 PG 2A. 2L74 4F4 FRT4A25 E2GL 20051104001892005110400189NM 2005 11 4 UPS05445652 120051023A541065B903604 LINK BOEING747 747121 1384871NM PWA JT9 JT9D3 52050NE NR 4 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 AD NR 4 PYLON REAR ENGINE MOUNT THRUST LINK FWD END LUG FOUND CRACK INDICATION EXCEEDED LIMIT. NR 4 PYLON REAR UPPER ENGINE MOUNT AFT THRUST LINK ASSY CHANGED AND INSTALLED IAW MM 71-21-03. 2L74 4F4 F A20WE E20EA 20051104001912005110400191 2005 11 4 UPS05445665 420051027A3442 COMPUTER BOEING747 747121 1384871NM PWA JT9 JT9D3 52050NE NR 2 FAILED A IPXAA UNSCHED LANDING S AFFECT SYSTEMS CRCRUISE 1 SO01681UP 19661 N/A DIVERSION - NR 2 AND NR 3 INS SYSTEMS FAILED. SAI FAIL FLAG INTERMITTENT. RERACKED NR 2 INS CMPUTER IAW MM 34-41-03 REALIGNED INS, NO FAULT NOTED, OPS CHECK NORMAL. 2L74 4F4 F A20WE E20EA 20051104001922005110400192WP 2005 11 4 UPS05845648 120051019A534047723861A FITTING DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE FS216 L21L CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 NA FRAME SUPPORT ATTACH FITTING BELOW L21L AT FS 216 IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D, AND SRM 51-3-2 AT FS 216 L21L. 2L74 4F4 FRT4A25 E2GL 20051104001932005110400193WP 2005 11 4 UPS05845649 120051005A534037558262N FITTING DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE FS280 L32L CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 C2 A- PIT BAG BIN, INTERGRANULAR CORROSION ON BATH TUB FITTING AT STA 280 L32L. REMOVED AND REPLACED BATH TUB FITTING AT STA 280, L32L IAW SRM 53-02-00 FIG 002D AND SRM 51-1-21. 2L74 4F4 FRT4A25 E2GL 20051104001952005110400195WP 2005 11 4 UPS05845655 120051011A5313 LONGERON DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE FS17901880L36 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE:C2 FS 1790 TO FS 1880 L36 IS CRACKED AND HAS ELONGATED HOLES. REMOVED LONGERON 26 AT FS 1790 TO 1880 IAW SRM 51-1-20D FABRICATED AND INSTALLED LONGERON 36 AND SPLICE REPAIR IAW S1415997 AND SRM 51-1-20D, AND 51-1-20. 2L74 4F4 FRT4A25 E2GL 20051104001972005110400197WP 2005 11 4 UPS05845657 120051001A5312 PRESSURE PANEL DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE FS960 LBL57-62 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 C2 CORROSION UNDER DOUBLER ON LT W/W CEILING STA 960 LBL 57-62, CORROSION AT SAME LOCATION IN MAIN CABIN UNDER FLOORBEAM. REMOVED MLG LT WHEEL WELL HORIZ. PRESSURE PANEL WEB AT FS 960 LBL 57-62 IAW SAA SK 866-832452, AND UPS EO FABRICATED AND INSTALLED PRESSURE PANEL, REPAIR DOUBLERS, FINGER DOUBLERS AND SPLICE REPAIRS IAW EO, AND SAA SK 866-832452. 2L74 4F4 FRT4A25 E2GL 20051104001992005110400199EU 2005 11 4 UPS05145667 120051021A5320A5341076522300 BRACKET AIRBUS300 A300B4622R 3930312EU FR 54 BL 60 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01135UP 0818 INSPECTION TYPE:2C AFT CARGO FS 54 BL 60 L SIDEWALL BRACE CRACKED. REMOVED AND REPLACED SIDEWALL BRACE IAW SRM 51-40-21. 2L72 4F RTA35EU 20051104002012005110400201EU 2005 11 4 UPS05145669 120051021A5320A5341076521700 BRACKET AIRBUSA300 A300F4622R 3930360EU FR 54 BL 60 R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01135UP 0818 INSPECTION TYPE:2C AFT CARGO FS 54 BL 60 R SIDEWALL BRACE CRACKED. REMOVED AND REPLACED SIDEWALL BRACE IAW SRM 51-40-21. 2L72 4F RTA35EU 20051104002092005110400209 2005 11 4 UPS05145697 420051009A2565UNK PIN AIRBUSA300 A300F4622R 3930360EU ESCAPE SLIDE DEACTIVATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01125UP 0809 DURING INSTALLATION OF ENTRY DOOR ESCA PE SLIDE LOCKOUT PIN FOUND DEACTIVATION PIN INSTALLED. REMOVED INSTALLED PIN AND ROUTED TO QC SDF. 2L72 4F RTA35EU 20051104002112005110400211WP 2005 11 4 UPS05845690 120051003A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP FS940 RBL60 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 FOUND FLOORBEAM CRACKED 2" LONG AT FS 940 RBL 60 UPPER FLANGE AREA. CUT OUT DAMAGED AREA OF FLOORBEAM AT STA 940, RBL 60 IAW SRM TR# 53-152, FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER IAW SRM TR# 51-1-21 FIG 1AND SRM 51-1-20D AT STA 940 RBL60. 2L74 4F RT4A25 20051104002132005110400213WP 2005 11 4 UPS05845692 120051001A5313 LONGERON DOUG DC8 DC873F 302199FWP FS690-710 L31L CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 FOUND L31L CORRODED BEYOND LIMITS IN LT BELLY STRESS PNL STA 690-710. REMOVED LONGERN 31L FS 690-710 IAW SRM 53-02--02-0. FABRICATED AND INSTALLED LONGERON 31L AND -37. REPAIR SPLICES IAW DWG 3750575 AND SRM 53-02-02-0 AND SRM 51-1-20D. 2L74 4F RT4A25 20051104002152005110400215WP 2005 11 4 UPS05845695 120051013A5313SAA36440462 STRINGER DOUG DC8 DC873F 302199FWP #4 ALT STR.64 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 NR 4 ALT HAS CRACK ON STRINGER 64 NEAR FRONT SPAR. REMOVED, FAB`D AND INSTALLED STRINGER SPLICE IAW SRM 51-1-21, 51-1-20D. 2L74 4F RT4A25 20051104002172005110400217WP 2005 11 4 UPS05845699 120051017A53404641324U501 FITTING DOUG DC8 DC873F 302199FWP STA 1690 L3L CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 FOUND STA 1690 L3L AFT PROD SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20051104002192005110400219WP 2005 11 4 UPS05845701 120051017A5313 LONGERON DOUG DC8 DC873F 302199FWP FS 1756 L14R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 RT AFT INTERIOR FS 1756 L14R CRACKED AT UPPER CANTED FRAME INTERSECTION. CUT OUT DAMAGED SECTION OF LONGERON, FABRICATED, AND INSTALLED REPLACEMENT SECTION OF LONGERON IAW DC-8 SRM 53-2-2 FIG 10. 2L74 4F RT4A25 20051104002212005110400221NM 2005 11 4 UPS05545677 120051025A5347 SEAT TRACK BOEING757 75724APF 1384969NM SECT. 46 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01406UP 23728 INSPECTION TYPE:C4 MAIN CARGO SEAT TRACK CORRODED STA 1542 RBL 47 REPAIRED PER ER 05-4597. 2L72 4F RTA2NM 20051104002232005110400223NM 2005 11 4 UPS05545679 120051025A5347 SEAT TRACK BOEING757 75724APF 1384969NM SECT 46 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01406UP 23728 INSPECTION TYPE:C4 MAIN CARGO SEAT TRACK CORRODED AT STA 1318, LBL 24. REPAIRED PER ER 05-4597. 2L72 4F RTA2NM 20051104002252005110400225NM 2005 11 4 UPS05545681 120051009A5310 BEAM BOEING757 75724APF 1384969NM SECT 44 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01406UP 23728 INSPECTION TYPE:C4 CORRISION OUT OF LIMITS ON LONGITUDINAL BEAM AT BS 1040 TO BS 1080 LBL 25 WL 208. REPLACED LONGITUDINAL BEAM. 2L72 4F RTA2NM 20051104002272005110400227NM 2005 11 4 UPS05545683 120051025A5310BAC15202474 STRUCTURE BOEING757 75724APF 1384969NM MAIN CARGO BAY CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01406UP 23728 INSPECTION TYPE:C4 CORROSION ON TOP OF SEAT TRACK AT BS 1184 RBL 1. REMOVED AND REPLACED SEAT TRACK BS 1180 TO BS 1209 IAW UPS ER 05-4598. 2L72 4F RTA2NM 20051104002292005110400229NM 2005 11 4 UPS05545685 120051010A5347 SEAT TRACK BOEING757 75724APF 1384969NM MAIN DECK CARGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01406UP 23728 INSPECTION TYPE:C4 MAIN CARGO LONGITUDINAL BEAM HAS CORROSION AT STA 1084. REPLACED SEAT TRACK IAW 51-40-02. 2L72 4F RTA2NM 20051104002322005110400232WP 2005 11 4 UPS05845687 120051027A5300 UNKNOWN DOUG DC8 DC873F 302199FWP MLG WW CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 FOUND CORROSION IN LT W/W. AIRCRAFT BEING FERRIED NR 9157 TO SAA FOR REPAIR. CUT OUT CORROSION FROM EXTERNAL SKIN, AND FAB'D AND INSTALLED REPAIR PARTS FOR SKIN REPAIR. ALL WORK PERFORMED IAW SAA SK 840-727258 & UPS EO DC8-53-20523. 2L74 4F RT4A25 20051104002392005110400239WP 2005 11 4 UPS05845706 120051017A534047505211 FITTING DOUG DC8 DC873F 302199FWP STA 900 L1 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 FOUND MAIN CARGO COMPARTMENT L1 AFT OF STA 900 FITTING CRACKED. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D AND 51-3-0. 2L74 4F RT4A25 20051104002412005110400241WP 2005 11 4 UPS05845708 120051019A5340 FITTING DOUG DC8 DC873F 302199FWP FS 1140 L35L CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 FOUND C-PIT INTERCOSTAL END FITTING AT FS 1140 AT LONGERON 35L CRACKED AT UP PER FASTENER ATTACH POINT. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FITTING IAW DWG 3758496 9 AND DC-8 SRM 51-1-21. 2L74 4F RT4A25 20051104002432005110400243WP 2005 11 4 UPS05845710 120051026A5511 RIB DOUG DC8 DC873F 302199FWP LH STAB LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 FOUND LT HORIZ STAB I/B L/E STA 141.250 RIB HAS CRACK ON LWR FLANGE ANGLE. STOP DRILLED CRACK, FABBED, AND INSTALLED REPAIR IAW DC-8 SRM 55-2-0 FIG 2 AND 3. 2L74 4F RT4A25 20051104002472005110400247NE 2005 11 4 HNAA0500096 220051026A7200 ENGINE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE NR 2 SMOKE A HNAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA07982HA401041192 380 120586 IN FLIGHT SMOKE IN CABIN AND COCKPIT. USED COCKPIT 02 MASKS. TURNED 13 BLEED OFF AND OPENED OUTFLOW VALVE ON DESCENT TO CLEAR SMOKE AND FLY UNPRESSURIZED, THEN TURNED OFF NR 2 BLEED DIVERTED AND DECLARED EMERGENCY. REMOVED AND REPLACED NR 2 ENGINE. 2H72 4T4 TRTA13NM E20NE 20051104002532005110400253EU 2005 11 4 05FDEA03590 120051030A5730 PANEL AIRBUS300 A300B4622R 3930312EU RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25720FD 417 RT WING BOTTOM PNL 675 DB CUT-OUT HAS CRACK. 2L72 4F RTA35EU 20051104002552005110400255NM 2005 11 4 05FDEA03592 120051031A5310 DOOR FRAME BOEING727 727225 1384077NM EMERGENCY EXIT GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 AFT FRAME IS GOUGED NEXT TO THE CRANK ARM FITTING OF THE LEFT AFT EMERGENCY ESCAPE DOOR. REPAIRED FRAME AT LEFT AFT EMERGENCY ESCAPE DOOR PER SRM 51-40-3. 2L73 4F A3WE 20051104002572005110400257NM 2005 11 4 05FDEA03594 120051101A5410 FITTING DOUG MD11 MD11 3023602NM NACELLE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 CRACK FOUND ON RT AFT CTR FASTENER HOLE AT BANJO NR 4 FTG FAYING SURFACE. VIEW LOOKING I/B AT 2 O'CLOCK DIRECTION. CRACK LENGTH FROM THE EDGE OF THE BANJO NR 4 FTG APPROX 1/8 INCH LONG. CORRECTIVE ACTION: SNRM N1614: BANJO FTG R/H NO.4 AFT CENTER FASTENER CRACK HOLE REPAIRED AS PER SRM 55-20-00 FIG. 3 VOL.I. CLASSIFIED MAJOR REPAIR PER GMM 6-2-100. 2L73 4F RTA22WE 20051104002582005110400258WP 2005 11 4 05FDEA03579 120051028A5320 INTERCOSTAL DOUG DC10 DC1030 3023501WP GE CF6 CF66D 30020GL RT MLG WW CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 RT MAIN LANDING GEAR WHEEL WELL INT CRACK LONG 1.5 INCH ON HORIZONTAL INTERCOSTAL AT STA 1475 Z-103 OB SIDE. FAB PART IAW DETAIL PART TRAVELER F 161131-3 IAW SRM 53-50-00 FIG 2. INSTALLED STRAP DOUBLER F161131-3 IAW SRM 53-50-00 FIG 2 VOL 1. 2L73 4F4 F A22WE E23EA 20051104002592005110400259WP 2005 11 4 05FDEA03580 120051028A5347 SEAT TRACK DOUG DC10 DC1030 3023501WP GE CF6 CF66D 30020GL BS 1029 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 MAIN CABIN AT STA 1029 LT SIDE AT X27.500 ON SEAT TRACK FOUND 1EA CRACK 10 INCHES LONG. CUT OUT CRACKED SECTION OF SEAT TRACK, REPLACED NEW SECTION IAW SRM 53-70-00, FIG 1 SHT1-2, VOL1. FAB PARTS IAW DETAIL PARTS TRAVELER F161689/N01689. 2L73 4F4 F A22WE E23EA 20051104002602005110400260WP 2005 11 4 05FDEA03581 120051028A5310 DOOR FRAME DOUG DC10 DC1030 3023501WP GE CF6 CF66D 30020GL CARGO DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 MAIN CARGO COMPARTMENT JAMB DOOR R3 STA 1256 X92 AND Z61 FOUND PLATE IN THE UPPER SECTION OF JAMB CRACK FOR 0.5 INCH LONG. REPAIRED CRACK IAW SRM 53-50-00 FIG 19 VOL1 FAB PART IAW DETAIL PART TRAVELER N01159. 2L73 4F4 F A22WE E23EA 20051104002612005110400261WP 2005 11 4 05FDEA03582 120051028A5321 FLOOR PANEL DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL COCKPIT CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 COCKPIT FLOOR SECTION STA 313 CRACK ON MEMBRANE 1 INCH LONG RIF SRM 53-11-01, ITEM 1. REPAIRED MEMBRANE AT STA 313 RIF SRM53-11-01 FIG 4 SHT 2 VOL 1. 2L73 4F4 F A22WE E23EA 20051104002622005110400262WP 2005 11 4 05FDEA03584 120051028A5321 FLOOR PANEL DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL COCKPIT CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 COCKPIT FLOOR STRUCTURE FOUND 1 EA CRACK 2 INCHES LONG ON MEMBRANE STA 304 X-12 RT SIDE. REPAIRED CRACK ON MEMBRANE STA 304 X-12 RT SIDE RIF SRM53-11-01, ITEM 1. 2L73 4F4 F A22WE E23EA 20051104002632005110400263WP 2005 11 4 05FDEA03585 120051028A5321 FLOOR PANEL DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL COCKPIT CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 COCKPIT FLOOR STRUCTURE FOUND 1 EA CRACK 2 INCHES LONG ON MEMBRANE STA 304 X-27 RT SIDE. REPAIRED CRACK ON MEMBRANE RIF 53-11-01 STA 304 X-27 RT SIDE. 2L73 4F4 F A22WE E23EA 20051104002642005110400264WP 2005 11 4 05FDEA03511 120051026A5340ARB71581 FITTING DOUG DC10 DC1030F 3023504WP KEELBEAM CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25319 47820 DURING ACCOMPLISHMENT OF B- CHECK MX, IND MX FOUND THE UPPER SECTION OF BOTH THE ARB7158-1 AND ARB7158-2 KEEL FITTING WERE CRACKED, EA 8-5740-79133P4 ISSUED TO COMPLY WITH REPAIR. 2L73 4F RTA22WE 20051104002652005110400265WP 2005 11 4 05FDEA03525 120051027A5720 INTERCOSTAL DOUG DC10 DC1030 3023501WP RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 RT WING INT L/E CRACK LONG 1,5" ON INTERCOSTAL AT STA XORS 980. REPAIRED CRACK INSTALLED 2 ANGLE PER SRM 57-00-01 FIG 3 SHT 2 VOL 1 AND SRM 51-35-01 PAGE 1-13 AND 51-33-01 PAG 34-47. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F160838-N00838 PER SRM 57-00-01 FIG 3 SHT 2 VOL 1. 2L73 4F A22WE 20051104002662005110400266WP 2005 11 4 05FDEA03526 120051027A5730 SKIN DOUG DC10 DC1030F 3023504WP RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 RT WIND INT L/E, CRACK LONG 1, 5" ON RIB AT STA XOS 450. REPAIRED CRACK PER SRM 57-20-00 FIG 1 SHT 3 VOL 1 AND SRM 51-35-01 PAGE 1-13 AND 51-33-01 PAGE 34-47. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F160840/N00840 PER SRM 57- 20-00 FIG 1 SHT VOL 1. 2L73 4F RTA22WE 20051104002672005110400267WP 2005 11 4 05FDEA03527 120051027A5730 DOUBLER DOUG DC10 DC1030F 3023504WP LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 LT WING L/E INT STRUCTURE FOUND 1 EA CRACK 0,5" ON UPPER DOUBLER AT STA XORS 683. REPAIRED BEADED DOUBLER PER SRM 57-10-00 FIG 71 VOL 1 AND SRM 51-35-01 PAGE 1-13 AND 51-33-01 PAGE 34-47. FABRICATED PARTS IAW DETAIL PART TRAVELER F160726/N00726 PER SRM 57-10-00 FIG 71 VOL 1. 2L73 4F RTA22WE 20051104002682005110400268WP 2005 11 4 05FDEA03538 120051027A5310 STRUCTURE DOUG DC10 DC1030F 3023504WP BILGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 IN THE CENTER CARGO COMPT BILGE SUMP AREA AT STA 1781 BETWEEN L 51 RT TO L 51 LT. FOUND MODERATE CORROSION ON THE FRAME'S CAP. REMOVED CORROSION IAW SRM 51-21-01 PAR 34 VOL 2. ORIGINAL THK MATERIAL IS .071'', AFTER REMOVED MATERIAL FOUND THK .042''. MATERIAL REMOVED IS OUT LIMITS IAW SRM 53-30-00 FIG 8 SHT 1 VOL 1. FABRICATED PARTS IAW DETAIL PART TRAVELER F160215-1 IAW SRM 53-30-00 FIG 8 SHT 1 VOL 1. INSTALLED REPAIR CHANNEL IAW SRM 53-30-00 FIG 8 VOL 1. 2L73 4F RTA22WE 20051104002692005110400269WP 2005 11 4 05FDEA03528 120051027A5712 RIB DOUG DC10 DC1030F 3023504WP LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 FOUND LT WING L/E INT STRUCTURE FOUND 1 EA CRACK 0.50" LONG ON RIB AT STA XORS 523. REPAIRED RIB PER SRM 57-20-00 FIG 1 SHT 6 VOL 1 AND SRM 51-33-01 PAGE 34-47. 2L73 4F RTA22WE 20051104002702005110400270WP 2005 11 4 05FDEA03529 120051027A5730 DOUBLER DOUG DC10 DC1030F 3023504WP RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 RT WING INT L/E, 3EA CRACKS ON DOUBLER AT STA XORS 685.REPAIRED BEADED DOUBLER PER SRM 57-10-00 FIG 71 VOL 1 AND SRM 51-35-01 PAGE 1-13 AND 51-33-01 PAGE 34-47. FABRICATED PART IAW DETAIL PART TRAVELER F160836/N00836 PER SRM 57-10-00 FIG 71 VOL 1. 2L73 4F RTA22WE 20051104002712005110400271WP 2005 11 4 05FDEA03530 120051027A5712 RIB DOUG DC10 DC1030F 3023504WP LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 LEFT WING L/E INT STRUCTURE FOUND 1 CRACK 0.25" LONG ON RIB AT STA XORS 516. REPAIRED L/E FORMER PER SRM 51-20-00 FIG 1 SHT 6 VOL 3 AND SRM 51-33-01 PAGE 34-47. 2L73 4F RTA22WE 20051104002722005110400272WP 2005 11 4 05FDEA03531 120051027A5730 PANEL DOUG DC10 DC1030F 3023504WP RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 RT WING INT L/E, CRACK ON CHORD FIXED PANEL AT STA XORS 803. REPAIRED STRINGER DOUBLER PER SRM 57-10-00-00 FIG 49 VOL 1 AND SRM 51-33-01 PAGE 34-47. FABRICATED PART IAW DETAIL PART TRAVELER F161054/N01054 PER SRM 57-10-00 FIG 49 VOL 1. 2L73 4F RTA22WE 20051104002732005110400273WP 2005 11 4 05FDEA03532 120051027A5730 DOUBLER DOUG DC10 DC1030F 3023504WP RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 RT WING INT L/E, CRACK LONG 0,5" ON INTERNAL DOUBLER AT STA XORS 540. REPAIRED BEADED DOUBLER PER SRM 57-10-00 FIG 71 VOL 1 AND SRM 51-35-01 PAGE 1-13 AND SRM 51-33-01 PAGE 34-47. FABRICATED PART IAW DETAIL PART TRAVELER F160799/N00799 PER SRM 57-10-00 FIG 71 VOL 1. 2L73 4F RTA22WE 20051104002742005110400274WP 2005 11 4 05FDEA03533 120051027A5753 SKIN DOUG DC10 DC1030F 3023504WP LT WING TE FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 LEFT WING OUTBD FLAP UPPER SURFACE FOUND 1 EA CRACK 3" LONG ON SKIN AT STA XOF 557. TRIMMED OUT DAMAGE SKIN INSTALLED FILLER DOUBLER PER SRM 57-10-00 FIG 85 AND SRM 51-35-01 PAGE 1-13 COLD BOND PER SRM 51-71-00 PAR 16C VOL 2. FABRICATED PART IAW DETAIL PART TRAVELER F160229/N00229 SRM 57-10-00 FIG 85. 2L73 4F RTA22WE 20051104002752005110400275WP 2005 11 4 05FDEA03534 120051027A5712 RIB DOUG DC10 DC1030F 3023504WP LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 LEFT WING L/E INT STRUCTURE FOUND 1 EA CRACK 1" LONG ON RIB AT STA XORS 676. REPAIRED L/E FORMER PER SRM 57-20-00 FIG 1 SHT 3 VOL 1. INSTALLED REPAIR ANGLE-31 PER SRM 51-35-01 PAGE 1-13 AND SRM-51-33-01 PAGE 34-47. FABRICATED PART IAW DETAIL PART TRAVELER F160727/N00727 PER SRM 57-20-00 FIG 1 SHT 3 VOL 1. 2L73 4F RTA22WE 20051104002762005110400276WP 2005 11 4 05FDEA03535 120051027A5753 SKIN DOUG DC10 DC1030F 3023504WP LT WING TE FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 LEFT WING OUTBD FLAP UPPER SURFACE FOUND 1 EA CRACK 0.50" LONG ON SKIN AT STA XOF 563. TRIMMED OUT DAMAGE SKIN FABRICATED FILLER DOUBLER AND INSTALLED PER SRM 57-10-00 FIG 85 COLD BOND PER SRM 51-71-00 PAR 16C VOL 2. FABRICATED PART IAW DETAIL PART TRAVELER F160230/N00230 PER SRM 57-10-00 FIG 85. 2L73 4F RTA22WE 20051104002772005110400277WP 2005 11 4 05FDEA03536 120051027A5753 SKIN DOUG DC10 DC1030F 3023504WP LT WING TE FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 LEFT WING OUTBD FLAP UPPER SURFACE FOUND 2 EA CRACKS 0.25" LONG ON SKIN AT STA XOF 787. TRIMMED OUT DAMAGE SKIN INSTALLED DOUBLER AND FILLER IAW SRM 57-10-00 FIG 85 COLD BOND IAW SRM 51-71-00 PAR 16C VOL 2 AND SRM 51-35-02 PAGE 3/9. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F160228/N00228 PER SRM 57-10-00 FIG 85. 2L73 4F RTA22WE 20051104002782005110400278WP 2005 11 4 05FDEA03537 120051027A5311 FRAME DOUG DC10 DC1030F 3023504WP BS 959 DAMAGED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25302FE 46801 MAIN CABIN AT STA 959 LT AT L6 DURING REM/INST STAND OFF PER J/C SP10240303-7003-17F FOUND ON FRAME EXISTING HOLE OVALIZED (1/4 INCHES DIA). CUT OUT DAMAGED AREA OF FRAME FABRICATED PARTS IAW DETAIL PART TRAVELER F161528-1 REPAIR ANGLE IAW SRM 53-30-00 FIG 13 AND DWG ADA 0049 INSTALLED REPAIR ANGLE PER SRM 53-30-00 FIG 4 VOL 1. 2L73 4F RTA22WE 20051104002792005110400279EU 2005 11 4 05FDEA03510 120051026A2131 CONTROLLER AIRBUS310 A310203 3930313EU CABIN PRESSURE MALFUNCTIONED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25413FE 397 PASSING 11,000 FT ON CLIMB-OUT, GOT EXCESSIVE CABIN ALTITUDE ECAM WARNING. CABIN ALT WAS 10170. FOLLOWED ECAM AND QRH. NO FAULT LIGHTS COULD GET OUTFLOW VALVES TO CLOSE IN AUTO OR MANUAL. AIR TURN BACK TO KMEM NO DEFECTS NOTED. AS PRECAUTIONARY SUGGEST CHANGING BOTH CABIN PRESSURE CONTROLLERS. REMOVED AND REPLACED NR 1 AND NR 2 CABIN PRESSURE CONTROLLERS IN REFERENCE TO A310-200 M/M 21-31-11-4. TESTED IN REFERENCE TO A310-200 M/M 21-31-00-5-01 NO DEFECTS NOTED. 2L72 4F RTA35EU 20051104002812005110400281WP 2005 11 4 05FDEA03543 120051027A5311 FRAME DOUG DC10 DC1030F 3023504WP BS 959 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 FWD CARGO COMPT UNDERFLOOR SUMP AREA AT STA 959 FOUND SEVERE CORROSION WITH EXFOLIATION ON THE FRAME'S CAP BETWEEN L51 RT TO L51 LT. CUT AND REMOVED SECTION OF FRAME CAP IAW SRM 51-35-01 PAGE 1-13. FAB PART IAW DETAIL PART TRAVELER F160315-3 REPAIR SPLICE AND F160315-5 FRAME CAP IAW SRM 53-30- 00 FIG 5-8 AND SRM 53-13-01 FIG 17 VOL 3, INSTALLED REPAIR CAP AND SPLICE IAW SRM 53-30-00 FIG 5-8. 2L73 4F RTA22WE 20051104002832005110400283EU 2005 11 4 05FDEA03546 120051027A5270 WARNING LIGHT AIRBUS310 A310203 3930313EU CARGO DOOR FALSE ACTIVATIONA FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25412FE 360 SOON AFTER T/O GOT ECAM ALERT FOR AFT CARGO NOT CLOSED AFT CRAGO SW FAULT AND AN AMBER DOOR LIGHT FOR AFT CARGO ON RT ECAM. ACN RELEASED FOR SERVICE PER MEL/CDL: 52-71-01 CATEGORY: C EXPIRATION: 05NOV05 "MEL 52-71-01: (IDENTIFY) AFT DOOR CLOSED AND LOCKED INDICATION ON ECAM DOOR PAGE INOP. AFT DOOR VISUALLY CHECKED CLOSED AND LOCKED. 2L72 4F RTA35EU 20051104002842005110400284EU 2005 11 4 05FDEA03547 120051027A5270 WARNING LIGHT AIRBUS310 A310203 3930313EU GE CF6 CF66D 30020GL CARGO DOOR FALSE ACTIVATIONA FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25412FE 360 SOON AFTER T/O GOT ECAM ALERT FOR AFT CARGO DOOR NOT CLOSED. AFT CARGO SW FAULT AND AN AMBER DOOR LIGHT FOR AFT CARGO ON RT ECAM. ACN RELEASED FOR SERVICE IAW MEL/CDL: 52-71-01 CATEGORY: C EXPIRATION: 05NOV05 MEL 52-71-01: AFT DOOR CLOSED AND LOCKED INDICATION ON ECAM DOOR PAGE, INOP. AFT DOOR VISUALLY CHECKED CLOSED AND LOCKED. 2L72 4F4 FRTA35EU E23EA 20051104002852005110400285NM 2005 11 4 05FDEA03514 120051026A5753651920612 FLAP TRACK BOEING727 7272S2F 1384O81NM NR 3 FLAP CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25213FE 22935 NR 3 FLAP TRACK AFT MOUNT PAD HAS HEAVY CORROSION. REPLACED FLAP TRACK WITH SERVICEABLE FLAP TRACK IAW MM 27-51-031-4. 2L73 4F A3WE 20051104002862005110400286WP 2005 11 4 05FDEA03515 120051027A5313 LONGERON DOUG DC10 DC1030F 3023504WP BS 485 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 FOUND IN THE AIR CONDITIONING COMPARTMENT LT SIDE AT STA 485 ON THE SKIN SPLICE LONGERON 36 MODERATE CORROSION AND N35 SELF ALIGNMENT NUTS RUST. REPLACED NUTS IAW SRM 51-31-01 PAR 6 VOL 2. REMOVED CORROSION IAW SRM 51-21-01 PAGE 28 ORIGINAL MATERIAL IS .094 FOR TEE AND FOR DOUBLER .071 THK REMAINING IS .083 FOR TEE AND .063 FOR DOUBLER MTL. REMOVED IS WITHIN LIMITS IAW SRM 53-00-01 FIG 1B TREATED AREA IAW SRM 51-21-01 PAR 31-34 VOL 2. 2L73 4F RTA22WE 20051104002872005110400287WP 2005 11 4 05FDEA03516 120051027A5311 FRAME DOUG DC10 DC1030F 3023504WP BS 485 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 IN THE AIR CONDITIONING COMPARTMENT LT SIDE AT STA 485 AND Z=-84 THERE IS DEEP WORN ON THE FRAME. TRIMMED OUT DAMAGE TO FRAME AND INSTALLED REPAIR CHANNEL IAW SRM 53-30-00 FIG 4 AND SRM 51-33-01 PAGE 34-4. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F160563/N00563 IAW SRM 53-30-00 FIG 4. 2L73 4F RTA22WE 20051104002882005110400288WP 2005 11 4 05FDEA03517 120051027A5321 FLOOR PANEL DOUG DC10 DC1030F 3023504WP COCKPIT CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 INTERNAL LWR COCKPIT AREA FOUND 2 CRACKS ON SAME MEMBRANE 1ST .50" LONG; 2ND IS 2" LONG; BETWEEN STA 304 TO STA 318; AND BETWEEN X12 TO X13 LT SIDE. REPAIRED MEMBRANE IAW SRM 53-00-01 VOL 1 FIG 10 SHT 4 AND SRM 51-35-01. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F160482/N00482 AND IAW SRM 53-00-01 VOL 1 FIG 10 SHT 4 AND SRM 51-35-01. 2L73 4F RTA22WE 20051104002892005110400289WP 2005 11 4 05FDEA03518 120051027A5753 SKIN DOUG DC10 DC1030F 3023504WP TE FLAP NICKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 LT WING OUTBD FLAP UPPER SURFACE FOUND DEEP DENT AND NICK ON SKIN AT STA XOF 467. TRIMMED OUT DAMAGE SKIN INSTALLED REPAIR DOUBLER PER SRM 57-10-00 FIG 85 SHT 1 AND SRM 51-35-02 PAGE 3/9 VOL 2. COLD BOND PER SRM 51-71-00 PAR 16C VOL 2 FABRICATED PARTS IAW DETAIL PARTS TRAVELER F160232/N00232 PER SRM 57-10-00 FIG 85. 2L73 4F RTA22WE 20051104002902005110400290WP 2005 11 4 05FDEA03519 120051027A5751 SKIN DOUG DC10 DC1030F 3023504WP LT WING AILERON CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 FOUND LT WING OUTBD AILERON WITH ONE CRACK 2" LONG WITH A STOP HOLE ON SKIN LOWER SURFACE AT STA XOA 824. TRIMMED BLEND OUT DAMAGE SKIN INSTALLED DOUBLER IAW SRM 57-10-00 FIG 85 AND SRM 51-71-00 PAR 16C VOL 2 AND SRM 51-35-02 PAGE 3-9. FABRICATED PART IAW DETAIL PART TRAVELER F160226/N00226 IAW SRM 57-10-00 FIG 85. 2L73 4F RTA22WE 20051104002962005110400296NM 2005 11 4 05FDEA03554 120051027A5230 SKIN BOEING727 72722 1384002NM PWA JT8 JT8D1 52044NE CARGO DOOR DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 FOUND FORWARD CARGO DOOR HAS MULTIPLE SCRATCHES ON EXTERIOR SKIN IN THE UNPAINTED AREA. REPAIRED PER E.A. 7-5230-91411. 2L73 4F4 F A3WE E2EA 20051104003012005110400301NM 2005 11 4 05FDEA03559 120051027A5330 SKIN BOEING727 72722 1384002NM PWA JT8 JT8D1 52044NE BS 361 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 FOUND MATERIAL LOSS EXCEEDS 10 PERCENT AT BS 361 STR 10L. REPAIRED PER E.O. 7-5330-7-2319 PT 5 2L73 4F4 F A3WE E2EA 20051104003032005110400303WP 2005 11 4 05FDEA03565 120051028A5712 RIB DOUG DC10 DC1030 3023501WP LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 LEFT WING L/E INT STRUCTURE FOUND 1CRACK 0.50'' ON RIB AT STA XORS 974. REPAIRED L/E FORMER IAW SRM 57-20-00 FIG 1 SHT 6 VOL 1. 2L73 4F A22WE 20051104003052005110400305NM 2005 11 4 05FDEA03550 120051027A5330 SKIN BOEING727 72722 1384002NM BS 1081 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 FOUND MATERIAL LOSS EXCEEDS 10 PERCENT BS 1081 STR 10R. REPAIRED PER E.O. 7-5330-7-2313 PT 5 2L73 4F A3WE 20051104003072005110400307CE 2005 11 4 DXTA200501042 120051028A3230 FORK CESSNA560 560XL 2076702CE MLG MALADJUSTMENT E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07662QS 5605262 A -GEAR UNLOCK- LIGHT REMAINED ON AFTER TAKEOFF WITH THE GEAR IN THE -UP POSITION-, THE -HYD PRESS- LIGHT REMAINED ON AS WELL. REMOVED NLG STRUT PISTON ASSY. FOUND MEASUREMENT BETWEEN FORK AND BEARING ORIFICE ASSY TO BE AT 16 .0 IN. RETORQUED BEARING AND ORIFICE ASSY TO ACHIEVE A MEASUREMENT OF 15.94 IN. (15.9375) BETWEEN FORK AND BEARING ORIFICE. REINSTALLED NLG STRUT PISTON ASSY. GEAR SWING GOOD. NO FAULTS FOUND. 2L72 4F RTA22CE 20051104003092005110400309CE 2005 11 4 DXTA200501044 120051028A3150 WARNING SYSTEM CESSNA750 750 2076810CE COCKPIT FALSE ACTIVATIONE DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07979QS 7500079 DURING TAKEOFF ROLL AT APPROXIMATLEY 50 KNOTS, RECEIVED AMBER CAS MESSAGE HP DUCT OVERPRESSURE. TAKEOFF WAS ABORTED. CAS MESSAGE WENT AWAY WHEN POWER WAS REDUCED ON ABORT. RAN ENGS TO MAX POWER N2 OF THE DAY (86 PERCENT) FOR 10 MIN W/ NO DEFECTS. PULLED POWER BACK TO -TO/MC- AND ALLOWED ENG TO RUN FOR 10 MIN W/ NO DEFECTS. PULLED POWER BACK TO CLIMB AND ALLOWED ENG TO RUN FOR 20 MIN W/ NO DEFECTS. PULLED POWER BACK TO CRUISE AND ALLOWED ENG TO RUN FOR 15 MIN W/ NO DEFECTS NOTED AT THIS TIME. ALL WORK PERFORMED IAW CITATION 750 MM CH 36-11-00 AND 71-00-04. 2L72 4J RTT00007WI 20051104003112005110400311CE 2005 11 4 DXTA200501041 120051028A324140955 TRANSDUCER CESSNA500 560CESSNA 2076750CE ANTI SKID SYS MALFUNCTIONED E DXTAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07325QS7298 5600425 CAPT LEFT BRAKE PEDAL INTERMITTENTLY LOSES PRESSURE IN TURNS. REMOVED AND REPLACED LT ANTI SKID TRANSDUCER IAW CE 560 MM 32-42-07. 2L72 4F RTA22CE 20051104003132005110400313CE 2005 11 4 DJFA2005156 120051030A3240 BRAKE BEECH MU300 400A 1155402CE MLG MALFUNCTIONED E DJFAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 EA23744TA RK245 KSJC - THE CREW REPORTED THAT WHILE THEY WERE TAXIING THE AIRCRAFT IN KSJC, THE LEFT BRAKE DEGRADED FROM POOR TO NIL. BRAKING ON THE RIGHT SIDE WAS NORMAL. MAINTENANCE BLED AIR FROM BOTH BRAKING SYSTEMS, AND PERFORMED AN OPERATIONAL CHECK. NO DEFECTS WERE NOTED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4F RTA16SW 20051104003152005110400315NM 2005 11 4 DHL2005742523 120050916A5753 SKIN BOEING727 727225 1384077NM FLAP DENTED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15742DH 21290 LT I/B FORE FLAP L/E NEAR CENTER HAS DENTS IN SKIN. REMOVED DENTED SKIN. FABRICATED AND INSTALLED REPAIR SKIN 8" BY 8" FROM 2024-T3 .040 IAW B727 SRM 51-10-1 AND 51-30-2. 2L73 4F A3WE 20051104003172005110400317NM 2005 11 4 DHL2005742525 120050916A5322 SHEAR TIE BOEING727 727225 1384077NM BS 1130 CORRODED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15742DH 21290 CORROSION ON BS 1130 BETWEEN STR. 27L - STR. 26R. FABRICATED AND INSTALLED SHEAR TIE 5-1/2" BY 3" FROM 7075-T6 .080 IAW B727 SRM 51-10-2, AND 51-30-2. 2L73 4F A3WE 20051104003192005110400319NM 2005 11 4 DHL2005742527 120050918A5347 SEAT TRACK BOEING727 727225 1384077NM BS 1018 GOUGED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15742DH 21290 SEAT TRACK GOUGED AT BS 1018 LBL 45 (OUTBD TRACK). REMOVED GOUGED SECTION OF TRACK, FABRICATED AND INSTALLED SEAT TRACK 80" FROM 7178T6511 IAW B727 SRM 51-10-6, 51-10-01, 51-30-2, 53-10-5 FIG 1 DRAWING 66-1573. 2L73 4F A3WE 20051104003212005110400321NM 2005 11 4 DU4R2005220 120051101A5330 SKIN BOEING757 757232 1384965NM FUSELAGE DENTED B DALAK NONE O OTHER ININSP/MAINT 1 SO15693DL 29725 FUSELAGE HAS 2 ADJACENT SHARP CREASED DENTS LOCATED AFT OF THE AFT CARGO DOOR CUT OUT AT OR BETWEEN BS 1480 TO 1500 AND BETWEEN S-23R AND S-24R. CUT OUT DENTS. FABRICATED AND INSTALLED REPAIRS 7-1/2" BY 7-1/2" AND 1-1/2" BY 2" FROM 2024-T3 .050 IAW B757 SRM 53-00-01, FIG 101 DETAIL III, 53-00-01 FIG 206 AND INSTALLED ID TAG PER DELTA B757 STANDARD 900-S-0 NR 04. 2L72 4F RTA2NM 20051104003252005110400325NM 2005 11 4 DL767050669 120051028A2121 FAN BOEING767 767232 1385132NM CABIN SEIZED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27101DA 22213 FUMES REPORTED IN MID CABIN OVERHEAD AREA, DIVERSION RDU. FOUND GASPER FAN AT FAULT. REPLACED SAME. 2L72 4F RTA1NM 20051104003352005110400335CE 2005 11 4 110205N541CS1 120051102A3260GE387 BULB CESSNA560 560XL 2076702CE MLG INDICATOR BURNED OUT E Z5FAL ABORTED APPROACH P NO WARNING INDICATION LDLANDING 1 NE03541CS 5605521 GOING INTO TEB THERE WAS A NOSE GEAR DOWN LIGHT MISSING AFTER GEAR EXTENSION. PILOT VERIFIED GEAR DOWN BY PERFORMING EMERGENCY GEAR BLOWDOWN CHECKLIST AND NOTING NOSE GREEN LIGHT FAILED LAMP TEST. AIRCRAFT LANDED WITH NO PROBLEMS. MAINTENANCE DISCOVERED BULB WAS INOP, REPLACED BULB AND SERVICED GEAR SYSTEM. ALL REQUIRED CHECKS PERFORMED WITH NO DEFECTS NOTED. 2L72 4F RTA22CE 20051104003362005110400336NE 2005 11 4 XN0A1274 220051028A7200 ENGINE BOEING727 727227 1384078NM PWA JT8 JT8D9 52048NE NR 1 FAILED A XN0AC ABORTED TAKEOFF XJ ENGINE FLAMEOUT WARNING INDICATION TOTAKEOFF 1 GL2379754 21363 665812 NR 1 ENGINE FAULT ON T/O ROLL AT STEWART, LOUD BAND HEARD FOLLOWED BY EPR REDUCTIVE TOWARDS 0. ALL OTHER ENGINE INDICATIONS NORMAL DURING T/O ROLL. 2L73 4F4 F A3WE E2EA 20051107000022005110700002NM 2005 11 7 USAA051320 120051102A5530 ANGLE BOEING737 7373B7 1384580NM VERTICAL STAB DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND VERT STAB TRANSITION ANGLE LEFT SIDE AFT OF REAR ATTACH POINT. FABRICATED AND INSTALLED NEW ANGLE IAW TR 53-20-05A, DEFECT SIZE: 12". 2L72 4F RTA16WE 20051107000092005110700009EA 2005 11 7 SWIA200515772 120050613A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07970SW 7881 FWD AVIONICS COMPARTMENT STA 280 LBL 9 OTBD FRAME CLIP CRACKED ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW FRAME CLIP IAW CRJ200 SRM 51-40-11. 2L72 4F RTA21EA 20051107000102005110700010EA 2005 11 7 SWIA200515773 120050613A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07970SW 7881 FWD AVIONICS COMPARTMENT STA 280 RBL 9 INBD FRAME CLIP CRACKED, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW FRAME CLIP AT STA280 RBL 9 INBD IAW CRJ200 SRM 51-42-06 AND 51-42-16. 2L72 4F RTA21EA 20051107000112005110700011EA 2005 11 7 SWIA200515774 120050613A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07970SW FWD AVIONICS COMPARTMENT STA 280 RT BL 9 OTBD FRAME CLIP CRACKED, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW FRAME CLIP AT STA 280 RBL 9 OTBD IAW CRJ200 SRM 51-42-06 AND 51-42-16. 2L72 4F RTA21EA 20051107000132005110700013EA 2005 11 7 SWIA200515776 120050523A5712 RIB CNDAIRCL600 CL6002B19 1900309EA RT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07409SW RIGHT BAT RIB CRACKED ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR OF RIGHT BAT RIB IAW REO 601R-57-51-046 AND REO 601R-57-51-217. 2L72 4F RTA21EA 20051107000142005110700014EA 2005 11 7 SWIA200515777 120050523A5712 RIB CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07409SW LEFT BAT RIB CRACKED, ITEM FOUND AT C-CHECK INSPECTION. RIB INSTALLED IAW CRJ200 SRM 51-42-21 AND 51-25-16. 2L72 4F RTA21EA 20051107000152005110700015EA 2005 11 7 SWIA200515778 120050523A5712 RIB CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07409SW 7056 LEFT BAT RIB CRACKED, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR OF LEFT BAT RIB IAW REO 601R-57-51-046. 2L72 4F RTA21EA 20051107000162005110700016EA 2005 11 7 SWIA200515779 120050523A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA BS 484 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07409SW 7056 FOUND CRACKED ANGLE FS 484 LBL27, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW PART CLIP IAW 51-23-00; 51-42-06 AND 51-42-21 CRJ200 SRM AT FS 484 LBL 27. 2L72 4F RTA21EA 20051107000182005110700018EA 2005 11 7 SWIA200515781 120051030A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA BS 484 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07926SW 7687 FUSELAGE; PULLEY INTERCOSTAL HAS A CRACKED I/B REMOTE ANGLE; FS 484.00; LBL 27.0, ITEM FOUND AT C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-42-21 & 51-23-16. 2L72 4F RTA21EA 20051107000222005110700022EA 2005 11 7 SWIA200515786 120051030A5320 WEB CNDAIRCL600 CL6002B19 1900309EA CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07926SW 7687 AFT EQUIPMENT COMP; ESB LOWER WEB IS CRACKED; RBL 38.0 EXTENDING FROM PANEL CUTOUT; FWD I/B CORNER, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-61-366 REV E. 2L72 4F RTA21EA 20051107000232005110700023EA 2005 11 7 SWIA200515787 120051030A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA BS 625 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07926SW 7687 AFT EQUIPMENT COMP; INTERCOSTAL CLIP IS CRACKED; FS 625.00 - STR 14L, ITEM FOUND AT C-CHECK INSPECTION. CLIP REPLACED IAW CRJ REO 601R-53-61-100 REV 'NC" & CRJ REO 601R-53-61-422 REV "NC". 2L72 4F RTA21EA 20051107000242005110700024EA 2005 11 7 SWIA200515788 120051030A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA BS 621 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07926SW 7687 CARGO COMP; FLOOR SUPPORT STRUCTURE IS CRACKED ; FS 621.00 LBL 38.0, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-61-117 REV C . 2L72 4F RTA21EA 20051107000252005110700025EA 2005 11 7 SWIA200515789 120051030A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA BS 621 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07926SW 7687 CARGO COMP; FLOOR SUPPORT STRUCTURE IS CRACKED; RBL 38.0 - FS 621.00, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-61-117 REV C. 2L72 4F RTA21EA 20051107000262005110700026EA 2005 11 7 SWIA200515790 120050604A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA DAMAGED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07919SW 7657 FUSELAGE SKIN AT PASSENGER DOOR CUTOUT STR 18 LT LOWER FORWARD CORNER SKIN DENTED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED DAMAGE IAW REO 601R-53-00-030 REV "D". 2L72 4F RTA21EA 20051107000272005110700027EA 2005 11 7 SWIA200515791 120050604A5210 DRAG ANGLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07919SW 7657 PAX DOOR; AIRSTAIR AFT DRAG ANGLE IS CRACKED BESIDE DOOR ASSIST PULLEY BRACKET; FS 357.00, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED DRAG ANGLE IAW CRJ REO 601R-52-11-513. 2L72 4F RTA21EA 20051107000292005110700029EA 2005 11 7 SWIA200515587 120050924A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA EMERGENCY EXT INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07709BR 7850 LOWER LEFT EMERGENCY EXIT SIGN AND AISLE LIGHTS INOP. REPLACED FLOOR POWER STRIP. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051107000322005110700032NM 2005 11 7 SWAA053452 120051102A53306545777 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29335SW 23939 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 967, STR 21L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051107000362005110700036NE 2005 11 7 SWAA053456 220051102A73148283004 PUMP BOEING737 7377H4 1384404NM CFMINTCFM567CFM567B22 13802NE NR 1 ENGINE FUELLEAKING A SWAAD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SW29763SW 27877 NR 1 ENGINE FUEL PUMP LEAKING. REMOVED AND REPLACED FUEL PUMP PER MM. 2L72 4F4 FRTA16WE E00055EN 20051107000392005110700039NM 2005 11 7 SWAA053448 120051102A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 1006, STR 24L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051107000422005110700042EA 2005 11 7 QXEA200501393 120051029A335020131A BATTERY PACK CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT DISCHARGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX6608 3132 10033 PDX - NUMEROUS EMERGENCY LIGHTS ARE OUT IN THE CABIN. MAINTENANCE REPLACED THE EMERGENCY BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20051107000432005110700043EA 2005 11 7 QXEA200501394 120051029A2611 SMOKE DETECTOR CNDAIRCL600 CL6002C10 1390015EA LAVATORY MALFUNCTIONED A QXEAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 NM09604QX 10019 FAT- ON TAKEOFF FOR FLIGHT 4299, THE LAVATORY SMOKE DETECTOR WENT OFF. ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE FOUND NO EVIDENCE OF SMOKE OR FIRE. SMOKE DETECTOR OPERATIONAL CHECKS GOOD. PLACED APU ON MEL 49-10-1B, RSI 353032 FOR BLEED AIR CONTAMINATION. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2L72 4F RTA21EA 20051107000442005110700044EA 2005 11 7 QXEA200501391 120051028A2710 FLT CONTROLS CNDAIRCL600 CL6002C10 1390015EA COCKPIT STIFF A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09609QX 10031 DEN - FLIGHT CONTROLS FEEL STIFF ON PITCH AND ROLL ON YOKE. MAINTENANCE INSPECTED BOTH CONTROL YOKES FOR STIFFNESS AND FOUND NO OBSTRUCTIONS. OPERATE NORMALLY. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2L72 4F RTA21EA 20051107000452005110700045EA 2005 11 7 QXEA200501392 120051027A3020 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA RT WING ANTIICE FALSE ACTIVATIONA QXEAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM09615QX 10065 PDX - RIGHT WING ANTI-ICE CAUTION CAME ON AFTER THE SYSTEM HAD BEEN ON 5 MINUTES. WENT OFF AFTER THE WING A/I CROSSBLEED WAS SELECTED "LEFT" AS PER THE CHECKLIST. MAINTENANCE FOUND A VALVE DISAGREE MESSAGE IN THE MDC. PERFORMED A OPERATIONAL TEST OF THE SYSTEM WITH NO DEFECTS. NO FAULTS REOCCURRED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2L72 4F RTA21EA 20051107000462005110700046NM 2005 11 7 QXEA200501499 120051030A5347 SEAT TRACK BOMBDRDHC8 DHC8402 1390042NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX: LT INBD SEAT TRACK SHOWS SIGNS OF CORROSION ALONG PREVIOUS REPAIR FROM APPROX STA X481-X490. MAINTENANCE REPAIRED IAW Q400 RD 8/4-53-884 AND NDTM PART 6, 51-00-02. 2H72 4T RTA13NM 20051107000502005110700050EA 2005 11 7 QXEA200501400 120051019A7830 FRAME CNDAIRCL600 CL6002C10 1390015EA THRUST REVERSER DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09615QX 10065 PDX: RIGHT ENGINE UPPER FAN COWL HAS FRETTING DAMAGE ON THRUST REVERSE FIXED FRAME JUST AFT OF CENTER LATCH APPROX NACELLE STA STA 155.00. MAINTENANCE REPAIRED IAW REO 670-78-34-460 AND QX EA R-78-68. 2L72 4F RTA21EA 20051107000512005110700051EA 2005 11 7 QXEA200501395 120051030A274084898001 SENSOR CNDAIRCL600 CL6002C10 1390015EA PITCH FEEL MALFUNCTIONED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09605QX9588 10022 FAT- ON FLIGHT 4299, PITCH FEEL FAULT STATUS MESSAGE ILLUMINATED. AIRCRAFT RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE REPLACED THE HTSA SENSOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20051107000522005110700052NM 2005 11 7 QXEA200501497 120051030A5347 SEAT TRACK BOMBDRDHC8 DHC8402 1390042NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX: LT INBD SEAT TRACK SHOWS SIGNS OF CORROSION ALONG PREVIOUS REPAIR FROM APPROX STA X376-X382. MAINTENANCE REPAIRED IAW Q400 RD 8/4-53-884 AND Q400 NDTM PART 6, 51-00-02. 2H72 4T RTA13NM 20051107000532005110700053NM 2005 11 7 QXEA200501496 120051101A30104100S00505 VALVE BOMBDRDHC8 DHC8402 1390042NM DEICE SYSTEM MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION APAPPROACH 1 NM09410QX3480 4053 SEA FLIGHT NR 2327: WHILE DESCENDING ON APPROACH AND OAT-2 DEG C, THE DE-ICE PRESSURE CAUTION LIGHT ILLUMINATED. AFTER SELECTING AIRFRAME MODE TO SLOW, THE NR 1 BOOT PAIR LIGHT ON FO'S SIDE WASN'T ILLUMINATED. RAN THE CHECKLIST AND THE DEICE LIGHT DIDN'T GO OUT BUT PRESSURES WERE NORMAL. MAINTENANCE REMOVED AND REPLACED NR 2 DUAL DISTRIBUTION VALVE AND INSTALLED LEADING EDGE 613AR. ALL CHECKS GOOD. NO DEFECTS NOTED. MTX CONTROL WAS NOTIFIED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051107000542005110700054NM 2005 11 7 QXEA200501492 120051023A5753 BEAM DHAV DHC8 DHC8202 2809007NM NR 4 FLAP CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09345PH 476 PDX - LEFT NR 4 FLAP BEAM HAS TWO PITS THROUGH PLATING ON SURFACE OUTBOARD, AT O POSITION AND 4" AFT OF O. REPAIRED IAW RD 8/57-988. 2H72 4T RTA13NM 20051107000552005110700055NM 2005 11 7 QXEA200501493 120051023A5753 BEAM DHAV DHC8 DHC8202 2809007NM NR 4 FLAP CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09345PH 476 PDX - LEFT NR 4 FLAP BEAM HAS TWO PITS THROUGH PITTING IN SURFACE C OUTBOARD, AT O POSITION AND 4" AFT OF O. REPAIRED IAW RD 8-57-988. 2H72 4T RTA13NM 20051107000562005110700056NM 2005 11 7 QXEA200501494 120051023A5753 BEAM DHAV DHC8 DHC8202 2809007NM NR 4 FLAP CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09345PH 476 PDX - LEFT NR 4 FLAP BEAM HAS SURFACE RUST AND LIGHT PITS OVER ENTIRE LENGTH OF OUTBOARD SURFACE "E". REPAIRED IAW RD 8/57/988. 2H72 4T RTA13NM 20051107000572005110700057NM 2005 11 7 QXEA200501495 120051023A5753 BEAM DHAV DHC8 DHC8202 2809007NM NR 4 FLAP CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09345PH 476 PDX - LEFT NR 4 FLAP BEAM HAS SURFACE RUST AND LIGHT PITTING OVER ENTIRE LENGTH OF INBOARD SURFACE "E". REPAIRED IAW RD 8/57/988. 2H72 4T RTA13NM 20051107000582005110700058NM 2005 11 7 QXEA200501396 120051101A2760H188C INDICATOR DHAV DHC8 DHC8202 2809007NM PFCS MALFUNCTIONED A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09347PH272804755 480 MFR FLIGHT NR 2066, BEFORE TAKEOFF CONTROL CHECK, PFCS OUTBOARD SPOILER INDICATOR STUCK IN FULLY RETRACTED POSITION. MAINTENANCE REPLACED PFCS INDICATOR. OPERATIONAL TEST OF PFCS INDICATOR IAW DASH-8-200 AMM TASK 27-05-00-000-802, 27-05-00-400-801, 27-05-00-710-801. 2H72 4T RTA13NM 20051107000622005110700062NE 2005 11 7 PCSA11030501 220051103A7200JT8D17 ENGINE BOEING727 727212 138407GNM PWA JT8 JT8D17 52049NE NR 1 VIBRATION A PCSAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 SO17598AJ418134803 21947 WHILE IN CRUISE, CREW REPORTED VIBRATION ON THE CENTER CONSOLE, WHEN NR 1 ENGINE THROTTLE WAS PULLED BACK VIBRATION SEEMS TO DIMINISH. AIRCRAFT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED ALL 3 ENGINES, INTAKES, AND EXHAUST, NO DAMAGE FOUND. ENGINE RUNS WERE ACCOMPLISHED AT TAKEOFF POWER NO VIBRATION FELT, OPERATION CHECK NORMAL IAW MM. AN ADDITIONAL AIRFRAME VIBRATION INSPECTION WAS ACCOMPLISHED, ENGINE ACCESSORIES INSPECTED FOR SECURITY AND LOOSENESS IAW MM NO DEFECTS NOTED, AN ENGINE AVM CHECK WAS ACCOMPLISHED IAW MM AND WAS FOUND TO BE WITHIN LIMITS, THE AIRCRAFT WAS RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 20051107000632005110700063NM 2005 11 7 P5CA0501410 120051030A2720 RUDDER BOEING747 747230B 1384889NM OUT OF POSITION A P5CAK NONE O OTHER ININSP/MAINT 1 EA15508MC 21644 CREW REPORTED LOWER RUDDER OFF TO LEFT 3 DEGREES WITH UPPER RUDDER NEUTRAL. CLEANED PLUG ON SURFACE POSITION INDICATOR, CYCLED RUDDER, ALL OPS AND INDICATIONS NORMAL IAW MM. 2L74 4F A20WE 20051107000652005110700065EA 2005 11 7 MASA200500824 120051023A2730 CONTROL UNIT CNDAIRCL600 CL6002D24 1390016EA ELEVATORS MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07930LR 15030 ASH 6213 TUS - EICAS ELEVATOR SPLIT CAUTION MESSAGES. UPON ARRIVING AT THE GATE THE FAULT HAD CLEARED. MX CHECKED THE MDC AND FOUND BOTH SSCUS FAULTED. THE SSCUS WERE RESET AND SELF TESTED WITH NO FAULTS NOTED. AN OPERATIONAL TEST WAS PERFORMED WITH NO FAULTS NOTED. 2L72 4F RTA21EA 20051107000682005110700068EA 2005 11 7 MASA200500817 120051020A2750860D10018ABCD CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0747239 7239 ASH 7100 ORD, FLAPS FAILED AT 20 DEG. MX R2 FLAP CONTROL UNIT. 2L72 4F RTA21EA 20051107000692005110700069EA 2005 11 7 MASA200500821 120051022A5210 LATCH CNDAIRCL600 CL6002B19 1900309EA PAX DOOR OVERSERVICED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0737218 7218 ASH 6251 PHX - CABIN DOOR THAT WOULD NOT OPEN FROM THE INSIDE THE A/C. MX REMOVED EXCESS GREASE FROM THE DOOR LATCHING ASSEMBLY AND FOUND NO FURTHER FAULTS. 2L72 4F RTA21EA 20051107000702005110700070EA 2005 11 7 MASA200500822 120051022A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA MAIN PAX MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0737218 7218 ASH 6251 PHX - RON HAD A CABIN DOOR THAT WOULD NOT OPEN FROM INSIDE THE CABIN. MX PRESSURIZED AIRCRAFT AND COULD NOT DUPLICATE. 2L72 4F RTA21EA 20051107000742005110700074EA 2005 11 7 MASA200500768 120051004A2150GG670950093 ACM CNDAIRCL600 CL6002D24 1390016EA RIGHT SMOKE A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW07905J 2922 2922 15005 ASH 6185 MEM - EVACUATED THE AIRCRAFT DUE TO SMOKE IN THE CABIN WITH A RT PACK OVERHEAT. MAINTENANCE REMOVED AND REPLACED RT ACM OPS CHECKED GOOD. 2L72 4F RTA21EA 20051107000752005110700075EA 2005 11 7 MASA200500816 120051020A5240 SENSOR CNDAIRCL600 CL6002D24 1390016EA SERVICE DOOR OUT OF RIG A MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW07918FJ 15018 ASH 6431 PHX - FWD SERVICE DOOR HANDLE CAUTION. MX RIGGED SENSOR, OPS CHECKED GOOD. 2L72 4F RTA21EA 20051107000772005110700077EA 2005 11 7 MASA200500829 120051024A3213 STRUT CNDAIRCL600 CL6002D24 1390016EA NLG UNDERSERVICED A MASAC ABORTED TAKEOFF WE INADEQUATE Q C VIBRATION/BUFFET TOTAKEOFF 1 SW07905J 15005 ASH 6330 PHX - ABORTED TAKEOFF DUE TO EXCESSIVE NOSE WHEEL SHIMMY. HIGH ENERGY STOP WITHIN LIMITS AND MX RE-SERVICED THE NLG STRUT. 2L72 4F RTA21EA 20051107000812005110700081NM 2005 11 7 72400022 120051030A5340 STRINGER CLIP BOEING727 727225 1384077NM CRACKED A K11AK NONE O OTHER ININSP/MAINT 1 GL23724CK 20383 A .5 INCH CRACK IN STRINGER CLIP. 2L73 4F A3WE 20051107000822005110700082NM 2005 11 7 72400023 120051030A5340 FITTING BOEING727 727225 1384077NM CRACKED A K11AK NONE O OTHER ININSP/MAINT 1 GL23724CK 20383 A .5 INCH CRACK IN FITTING. 2L73 4F A3WE 20051107000832005110700083NM 2005 11 7 72400024 120051030A5320 WEB BOEING727 727225 1384077NM CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23724CK 20383 A 3 X 1 INCH AREA OF CORROSION ON WEB. 2L73 4F A3WE 20051107000842005110700084NM 2005 11 7 72400025 120051030A5340 ATTACH ANGLE BOEING727 727225 1384077NM CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23724CK 20383 A .5 X .5 INCH AREA OF CORROSION ON ATTACH ANGLE. 2L73 4F A3WE 20051107000852005110700085NM 2005 11 7 72400026 120051030A5330 SKIN BOEING727 727225 1384077NM CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23724CK 20383 THREE 2 INCH DIAMETER AREAS OF CORROSION ON INNER SKIN. 2L73 4F A3WE 20051107000892005110700089NM 2005 11 7 UPS05445716 120051031A541065B903604 LINK BOEING747 747212B 1384886NM NR 3 PYLON MOUNTCRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 NR 3 ENG REAR ENG MOUNT THRUST LINK AFT LUG UPPER AND LOWER OF BORE FOUND SUSPECTED CRACK INDICATIONS WHICH WERE GREATER THAN 40 PERCENT FSH, EXCEEDED LIMIT. REFER TO EO NR B747-7120-22596-A FOR THRUST LINK REPLACEMENT. ENGINE REMOVED AND REINSTALLED ON TASK CARD NR 5000. 2L74 4F A20WE 20051107000122005110700012EA 2005 11 7 SWIA200515775 120050523A5712 RIB CNDAIRCL600 CL6002B19 1900309EA RT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07409SW 7056 RIGHT BAT RIB CRACKED, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW RIB AT RIGHT BAT IAW SRM 51-42-21. 2L72 4F RTA21EA 20051107000172005110700017EA 2005 11 7 SWIA200515780 120051030A5210 DRAG ANGLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07926SW 7687 FOUND PAX DOOR; AFT STAIR DRAG ANGLE CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED REPAIR ANGLE SECTION IAW CRJ REO 601R-52-11-513 REV A. 2L72 4F RTA21EA 20051107000192005110700019EA 2005 11 7 SWIA200515782 120051030A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA BS 484 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07926SW 7687 FUSELAGE; PULLEY INTERCOSTAL HAS A CRACKED I/B REMOTE ANGLE AND O/B ATTACHED ANGLE CRACKED; FS 484.00; RBL 27.0 AND 36.0, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-41-059 REV A. 2L72 4F RTA21EA 20051107000202005110700020EA 2005 11 7 SWIA200515784 120051030A5310 BEAM CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07926SW 7687 FUSELAGE; TRANSVERSE BEAM CRACKED ON LOWER FLANGE; RBL 11.0 - FS 280.00, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-11-171 REV "C" 2L72 4F RTA21EA 20051107000212005110700021EA 2005 11 7 SWIA200515785 120051030A5320 WEB CNDAIRCL600 CL6002B19 1900309EA CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07926SW 7687 AFT EQUIPMENT COMP; ESB LOWER WEB CRACKED; LBL 38.0 EXTENDING FROM PANEL CUTOUT; FWD I/B CORNER, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-61-366 REV E. 2L72 4F RTA21EA 20051107000282005110700028EA 2005 11 7 SWIA200515792 120051102A5610 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT FAILED A SWIAO OTHER O OTHER CRCRUISE 1 NM07923SW 7664 RT SIDE WINDOW SHATTERED IN FLIGHT. REPLACED FO'S RIGHT SIDE WINDOW IAW CRJ MM 56-12-00, PN/OFF NP-139322-6, SN/OFF 02057H9529. 2L72 4F RTA21EA 20051107000302005110700030EA 2005 11 7 SWIA200515783 120051030A5310 BEAM CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07926SW 7687 FUSELAGE; TRANSVERSAL BEAM CRACKED ON LOWER FLANGE; LBL 11.0 - FS 280.0, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-11-171 REV "C". 2L72 4F RTA21EA 20051107000312005110700031NM 2005 11 7 SWAA053451 120051102A53116546529 BELTFRAME BOEING737 7373H4 1384600NM FWD CARGO CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29335SW 23939 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE BELTFRAME CRACKED AT BS 500B, ABOVE RT GENERATOR FEEDER CABLES ACCESS HOLE. REPAIRED BELTFRAME PER SWA EA. 2L72 4F RTA16WE 20051107000332005110700033 2005 11 7 SWAA053453 420051102A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29423WN 29827 R1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATING LOW. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20051107000342005110700034NM 2005 11 7 SWAA053454 120051101A335007912 COVER BOEING737 7377H4 1384404NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29446WN 29842 DURING SCHEDULED HC1 CHECK, FOUND EEPLS TRACK COVER CRACKED AT FWD END. REMOVED AND REPLACED COVER PER MM. 2L72 4F RTA16WE 20051107000352005110700035 2005 11 7 SWAA053455 420051102A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29483WN 32472 L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR WOULD NOT ENGAGE IN FLOOR FITTINGS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20051107000372005110700037NM 2005 11 7 SWAA053446 120051102A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM AFT CARGO CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 927, STR 23L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051107000382005110700038NM 2005 11 7 SWAA053447 120051102A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM AFT CARGO CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 927, STR 24L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051107000402005110700040NM 2005 11 7 SWAA053449 120051102A53126546568 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D-CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT STR 5R. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20051107000412005110700041 2005 11 7 SWAA053450 420051102A256565C168211 MOUNT BOEING737 7373H4 1384600NM R2 DOOR SLIDE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29335SW 23939 DURING SCHEDULED 1/4D CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD ATTACH MOUNT CRACKED. REMOVED AND REPLACED FWD MOUNT PER MM. 2L72 4F RTA16WE 20051107000472005110700047NM 2005 11 7 QXEA200501498 120051030A5347 SEAT TRACK BOMBDRDHC8 DHC8402 1390042NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX: LT INBD SEAT TRACK SHOWS SIGNS OF CORROSION ALONG PREVIOUS REPAIR FROM APPROX STA X416-X422. MAINTENANCE REPAIRED IAW Q400 RD 8/4-53-884 AND NDTM PART 6, 51-00-02. 2H72 4T RTA13NM 20051107000482005110700048NM 2005 11 7 QXEA200501500 120051030A5347 SEAT TRACK BOMBDRDHC8 DHC8402 1390042NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX: LT INBD SEAT TRACK SHOWS SIGNS OF CORROSION ALONG PREVIOUS REPAIR FROM APPROX STA X609-X621. MAINTENANCE REPAIRED IAW Q400 RD 8/4-53-884 AND Q400 NDTM PART 6, 51-00-02. 2H72 4T RTA13NM 20051107000492005110700049EA 2005 11 7 QXEA200501397 120051014A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 645-661 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09615QX 10065 YYC: FUSELAGE INT, LEFT OUTBOARD SEATRAIL AT FS 645 TO FS 661 HAS PITTING CORROSION ON INBOARD FACING SURFACE. MAINTENANCE REPAIRED IAW REO 670-53-00-013. 2L72 4F RTA21EA 20051107000592005110700059 2005 11 7 PIDA20050185 420051031A22104038891916 COMPUTER BOEING737 7372K5 138448XNM MALFUNCTIONED A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05249TR 22598 AUTO PILOT "A" CHANNEL DISENGAGES. REPLACED "A" SYSTEM FCC. OPERATION NORMAL PER MM 22-11-00. 2L72 4F RTA16WE 20051107000602005110700060 2005 11 7 PIDA20050183 420051102A22104038890948 CONTROL PANEL BOEING737 7372K5 138448XNM MALFUNCTIONED A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05250TR 22597 MODE CONTROL PANEL INOP. REPLACED MODE CONTROL PANEL PER MM 22-11-01. 2L72 4F RTA16WE 20051107000612005110700061 2005 11 7 PIDA20050184 420051021A3130 RECORDER BOEING737 7372K5 138448XNM MALFUNCTIONED A PIDAO OTHER L NO TEST NRNOT REPORTED 1 SO05249TR 22598 AERO INSTRUMENTS & AVIONICS READOUT OF THE FDR INDICATE THAT THE LEADING EDGE SLAT DISCRETES NEVER CHANGE STATE DURING FLIGHT. ACCOMPLISHED EMTEQ ENGINEERING MOD PAA1-001M-1 DATED 9-6-05. 2L72 4F RTA16WE 20051107000642005110700064NM 2005 11 7 P5CA0501409 120051031A801174017912 STARTER BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE NR 3 ENGINE FAILED A P5CAK NONE O OTHER ININSP/MAINT 1 EA15920FT 22237 AFTER PUSH BACK, CREW REPORTED NR 3 ENGINE WOULD NOT START. PARAMETERS INDICATE NORMAL, NR N1 OR N2 INDICATION. REPLACED STARTER IAW MM 80-10-00. OPS NORMAL. 2L74 4F4 F A20WE E3NE 20051107000662005110700066EA 2005 11 7 MASA200500834 120051026A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0777195 7195 ASH 7216 ORD - CEILING EMERGENCY LIGHTS ABOVE SEAT ROWS 5 AND 14 ARE INOPERATIVE. MAINTENANCE REPLACED THE LIGHTS. 2L72 4F RTA21EA 20051107000672005110700067EA 2005 11 7 MASA200500838 120051028A5210 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA PAX DOOR FALSE ACTIVATIONA MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW0727173 7173 ASH 7173 IAD - PASSENGER DOOR WARNING MESSAGE IN FLIGHT. OPS CHECKED COULD NOT DUPLICATE. 2L72 4F RTA21EA 20051107000712005110700071EA 2005 11 7 MASA200500826 120051023A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA EMERGENCY EXIT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0737218 7218 ASH 6338 PHX - EMERGENCY EXIT ORANGE LIGHT INOPERATIVE. MX SECURED CONNECTION AT LIGHTING STRIP. 2L72 4F RTA21EA 20051107000722005110700072EA 2005 11 7 MASA200500827 120051023A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0737228 7228 ASH 6428 PHX - NR 1 FLOOR TRACK EMERG LIGHT INOP. MX REPLACED THE LAMP. 2L72 4F RTA21EA 20051107000732005110700073EA 2005 11 7 MASA200500842 120051029A5270 PROXIMITY SWITCH CNDAIRCL600 CL6002B19 1900309EA PAX DOOR OUT OF ADJUST A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0727173 7173 ASH 7203 IAD - PASSENGER DOOR WARNING IN FLIGHT. MAINTENANCE ADJUSTED MAIN ENTRY DOOR UPPER CAM, CAM LATCH AND PROX SWITCH. 2L72 4F RTA21EA 20051107000762005110700076EA 2005 11 7 MASA200500831 120051024A5210 PIN CNDAIRCL600 CL6002B19 1900309EA PAX DOOR HANDLE TANGLED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0777195 7195 ASH 7101 IAD - PAX DOOR THAT WOULD NOT OPEN. MX FOUND THAT THE PAX DOOR HAND RAIL PIN WAS TANGLED IN THE HAND RAIL. MX PROPERLY STOWED HAND RAIL PIN AND FOUND NO FURTHER FAULTS WITH DOOR. 2L72 4F RTA21EA 20051107000782005110700078NM 2005 11 7 72400019 120051030A5340 STRINGER CLIP BOEING727 727225 1384077NM CRACKED A K11AK NONE O OTHER ININSP/MAINT 1 GL23724CK 20383 A 1 INCH CRACK IN STRINGER CLIP. 2L73 4F A3WE 20051107000792005110700079NM 2005 11 7 72400020 120051030A5320 STOP FITTING BOEING727 727225 1384077NM PAX DOOR CRACKED A K11AK NONE O OTHER ININSP/MAINT 1 GL23724CK 20383 A 5 INCH CRACK IN DOOR STOP FITTING. 2L73 4F A3WE 20051107000802005110700080NM 2005 11 7 72400021 120051030A5320 STOP FITTING BOEING727 727225 1384077NM CRACKED A K11AK NONE O OTHER ININSP/MAINT 1 GL23724CK 20383 A 5 INCH CRACK IN DOOR STOP FITTING. 2L73 4F A3WE 20051107000862005110700086NM 2005 11 7 UPS05445713 120051028A541065B903604 LINK BOEING747 747212B 1384886NM NR 1 PYLON MOUNTCRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 NR 1 ENG MOUNT THRUST LINK SUSPECTED CRACK INDICATION REVEALED AT BOTH FWD AND AFT END LUG, BOTH INDICATION GREATER THAN 40 PERCENT FSH (EXCEEDED LIMIT). REFER TO EO NR B747-7120-22596-A FOR THRUST LINK REPLACEMENT. ENGINE REMOVED AND REINSTALLED ON TASK CARD NR 5000. 2L74 4F A20WE 20051107000872005110700087NM 2005 11 7 UPS05445714 120051028A541065B903604 LINK BOEING747 747212B 1384886NM NR 2 PYLON MOUNTCRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 NR 2 ENG MOUNT THRUST LINK SUSPECTED CRACK INDICATION REVEALED AT BOTH FWD AND AFT END LUG, BOTH INDICATION GREATER THAN 40 PERCENT FSH (EXCEEDED LIMIT). REFER TO EO NR B747-7120-22596-A FOR THRUST LINK REPLACEMENT. ENGINE REMOVED AND REINSTALLED ON TASK CARD NR 5000. 2L74 4F A20WE 20051107000882005110700088NM 2005 11 7 UPS05445715 120051028A541065B903604 LINK BOEING747 747212B 1384886NM NR 3 PYLON MOUNTCRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 NR 3 ENG MOUNT THRUST LINK SUSPECTED CRACK INDICATION REVEALED AT FWD LUG UPPER SIDE, THE INDICATION GREATER THAN 40 PERCENT FSH, EXCEEDED LIMIT. REFER TO EO NR B747-7120-22596-A FOR THRUST LINK REPLACEMENT. ENGINE REMOVED AND REINSTALLED ON TASK CARD NR 5000. 2L74 4F A20WE 20051107000962005110700096EA 2005 11 7 COMA0560577 120051028A2750 FLEX COUPLING CNDAIRCL600 CL6002B19 1900309EA TE FLAPS LACK OF LUBE A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01735CA 7267 FLIGHT 4997 - FLAPS FAIL CAUTION. CLEANED AND LUBRICATED RT WING FLEX DRIVE CABLES. 2L72 4F RTA21EA 20051107000982005110700098EA 2005 11 7 COMA0570116 120051029A3230 COMPUTER CNDAIRCL600 CL6002C10 1390015EA MLG MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01656CA 10143 FLIGHT 5476 - GEAR DISAGREE WARNING. GEAR SWINGS WERE NORMAL. NO FAULT CODES IN MDC. 2L72 4F RTA21EA 20051107001002005110700100EA 2005 11 7 COMA0560578 120051030A2750865D1007 PDU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01735CA18011 7267 FLIGHT 5013 - FLAPS FAIL CAUTION. REPLACED THE FLAP PDU. 2L72 4F RTA21EA 20051107001012005110700101SO 2005 11 7 CHQA200500190 120051101A2611 SMOKE DETECTOR EMB 145 EMB145LR 3260212SO LAVATORY ACTIVATED A CHQAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 GL11269SK 145293 FLIGHT 7796 - IAD-BUF - LAVATORY SMOKE WENT OFF. WHILE INSPECTING THE LAVATORY, SMOKE WAS SEEN COMING FROM CEILING AREA. PERFORMED VISUAL INSPECTION OF AIRCRAFT AND FOUND NO TRACES OF BURNED WIRES OR ANY SIGNS OF BURNING. AIRCRAFT OK TO CONTINUE SERVICE. 2L72 4T RTT00011AT 20051107001022005110700102SO 2005 11 7 CHQA200500189 120051030A21332099L011100 OUTFLOW VALVE EMB 145 EMB145 3260210SO TORN A CHQAB EMER. DESCENT J WARNING INDICATION CLCLIMB 1 GL11263SK1430814308 145199 FLT 3155 - BOS-SAV - CLIMBING THRU 10,000 FT, "ICE DET 2 FAIL" APPEARED ONE EICAS. RAN QRH PROCEDURES AND CONTINUED CLIMB. CLIMBING THRU FL180 AT APPROX 0950L IN ICING CONDITIONS WITH THE ANTI-ICING 'ON', CABIN PRESS WAS LOST. DECLARED EMERG. AT 10,000 FT, L/G RETRACTED AND EICAS THEN DISPLAYED "LG AIR/GND FAIL." RAN QRH AND APPLIED APPROPRIATE PROCEDURES AFTER EXITING ICING CONDITIONS. DUE TO AMOUNT OF FUEL O/B AND AN O/W LANDING ISSUE, DETERMINED THERE WOULD BE NO DANGER OF DELAYING LANDING ABOUT 25 MINS FOR FUEL TO BURN OFF. LOWERED L/G AND SELECTED FLAPS 22 TO AID IN BURN OFF. LANDED ON RUNWAY 04R AT BOS WITH NO FURTHER DIFFICULTIES AND TAXIED TO GATE. FOUND PNEUMATIC OUTFLOW VLV DIAPHRAGM DRY ROTTE2L72 4F RTT00011AT 20051107001032005110700103NM 2005 11 7 CALA0500378 120051028A3233651781914 ACTUATOR BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE NLG INOPERATIVE A CALAO OTHER J WARNING INDICATION APAPPROACH 1 SW271432555781 23455 WHEN THE GEAR HANDLE WAS PLACED DOWN ON FINAL APPROACH, THE NLG DID NOT EXTEND. THE CHECKLIST WAS RUN AND THE GEAR WAS EXTENDED MANUALLY WITH THREE GREEN LIGHTS RECEIVED. THE AIRCRAFT LANDED NORMALLY. MAINTENANCE REMOVED AND REPLACED THE NLG LOCK ACTUATOR IAW MM 32-33-21. IN ADDITION, THE NLG HYDRAULIC MODULE WAS REPLACED AS A PRECAUTIONARY MEASURE IAW MM 32-33-31. LEAK AND OPERATIONAL CHECKS WERE GOOD. 2L72 4F4 FRTA16WE E2GL 20051107001042005110700104NM 2005 11 7 CALA0500382 120051102A3350S283T0143 BATTERY PACK BOEING737 737824 13844BZNM EMERGENCY LIGHT INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2726226 28935 SOME EMERGENCY EXIT LIGHTS UNDER THE OVERHEAD BINS WERE FOUND INOPERATIVE. THE M1671 AND M1673 BATTERY PACKS AND CHARGERS WERE REMOVED AND REPLACED IAW MM 33-51-14 AND 33-51-06-960-805. 2L72 4F RTA16WE 20051107001052005110700105NM 2005 11 7 CALA0500380 120051030A5320141T5107 FLOOR SUPPORT BOEING767 767424ER 1385270NM BS 303-325 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2759053 29448 INSPECTION FOUND FLOORBEAM CORRODED AT STA 303-325, LBL 22-34. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, FIGURE 201, REPAIR 1. 2L72 4F RTA1NM 20051107001062005110700106NM 2005 11 7 CALA0500381 120051030A5315141T5108 FLOORBEAM BOEING767 767424ER 1385270NM STA 325 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2759053 29448 INSPECTION FOUND FLOORBEAM CORRODED AT STA 325, LBL 48 - RBL 45. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, FIGURE 201. 2L72 4F RTA1NM 20051107001072005110700107NM 2005 11 7 CALA0500383 120051103A57121137T1539 RIB BOEING767 767424ER 1385270NM GE CF6 CF680 30025NE WS 467.8 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2759053 29448 INSPECTION FOUND A 0.025 INCH CRACK IN RT WING IB AILERON IB HINGE RIB SUPPORT AT AFT HI-LOK AREA, WS 467.8. THE CRACKED AREA WAS TRIMMED OUT AND A REPAIR WAS INSTALLED IAW ECRA 5740-02094. 2L72 4F4 FRTA1NM E13NE 20051107001082005110700108NM 2005 11 7 CALA0500379 120051029A5315147A5506 FLOORBEAM BOEING737 737724 13844BYNM STA 986.5 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2723707 28768 INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, LBL 43 TO RBL 43. THE FLOORBEAM WAS REPAIRED IAW ECRA 5321-01306. 2L72 4F RTA16WE 20051107001102005110700110SO 2005 11 7 C2XA05SH123 120051028A532014521713005 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714543 145553 SHV - DURING C-CHECK THE CENTER OMEGA BEAM CORRODED AT FR 20. MAINTENANCE REMOVED AND REPLACED CENTER OMEGA BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2L72 4T RTT00011AT 20051107001112005110700111SO 2005 11 7 C2XA05SH124 120051101A532014521700007 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711551 145411 SHV - DURING C-CHECK MAINTENANCE FOUND LT OMEGA BEAM CORRODED AT FRAME 20. MAINTENANCE REPAIRED LT OMEGA BEAM AT FRAME 20 IAW EMB 145 SRM 51-40-02 & EC 5320-01140. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20051107001122005110700112SO 2005 11 7 C2XA05TY058 120051031A555314504980602 FITTING EMB 135 EMB135LR 3260305SO VERTICAL STAB WORN A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714505 145192 TYS, DURING A SCHEDULE INSPECTION THE RIGHT HAND VERTICAL BEARING WAS FOUND WITH EXCESSIVE PLAY. MAINTENANCE REMOVED THE BEARING REAMED THE HOLE, INSTALLED BUSHING AND REPLACED THE BEARING IAW EC5510-01128. 2L72 4F RTT00011AT 20051107001142005110700114SO 2005 11 7 C2XA05SH126 120051101A491014526850401 FIREWALL EMB 145 EMB145LR 3260212SO APU BAY CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711551 145411 SHV - DURING C-CHECK MAINTENANCE FOUND APU FIREWALL CRACKED ON RT SIDE 3 O'CLOCK POSITION AT END OF STIFFENER. MAINTENANCE REPAIRED APU FIREWALL RT SIDE AT 3 O'CLOCK POSITION IAW EMB 145 SRM 53-32-13 SEC 5 FIG 204. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20051107001152005110700115SO 2005 11 7 C2XA05SH127 120051101A491014526850401 FIREWALL EMB 145 EMB145LR 3260212SO APU BAY CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711551 145411 SHV - DURING C-CHECK MAINTENANCE FOUND APU FIREWALL CRACKED AT RIVET ADJACENT TO RT SIDE OF COWLING ALIGNMENT PIN. MAINTENANCE REPAIRED APU FIREWALL AT RT SIDE OF COWLING ALIGNMENT PIN IAW EMB 145 SRM 53-32-13. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20051107001162005110700116SO 2005 11 7 C2XA05SH128 120051101A491014526850401 FIREWALL EMB 145 EMB145LR 3260212SO APU BAY CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711551 145411 SHV - DURING CHECK MAINTENANCE FOUND APU FIREWALL CRACKED AT FASTENER AT STR 16R. MAINTENANCE REPAIRED APU FIREWALL IAW EMB 145 SRM 53-32-13. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20051107001172005110700117NM 2005 11 7 AWXA200501300 120051009A5523 SKIN BOEING737 7373G7 1384595NM ELEVATOR DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - DURING C16 CHECK DISCOVERED LT ELEVATOR, INBOARD TRAILING EDGE, TIP DELAMINATED FROM ELEVATOR STATIONS 24.9 TO 25.9. MAINTENANCE REMOVED DELAMINATED PLIES IAW BOEING 737-300 SRM 51-70-04-06 REPAIR 11 FIGURE 17. BONDED GRAPHITE REPAIR TO THE LT ELEVATOR, INBOARD TRAILING EDGE, TIP DELAMINATED FROM ELEVATOR STATIONS 24.9 TO 25.9 IAW BOEING 737-300 SRM 51-70-04-0G REPAIR 11 FIG 17. 2L72 4F RTA16WE 20051107001202005110700120NM 2005 11 7 AWXA200501303 120051015A53126516300239 BULKHEAD BOEING737 7373G7 1384595NM BS 178 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - DURING C16 CHECK DISCOVERED WEB CRACKED, 1.1 INCHES IN LENGTH, AT BL 5.7L, WL 180 AND BS 178. MAINTENANCE CUT OUT DAMAGED PART OF WEB AT BL 5.7L, WL 180 AND BS 178 IAW BOEING 737-300 SRM 53-10-08-2R 12 FIG 201. FABRICATED REPAIR WEB IAW BOEING 737-300 SRM 53-10-08-2R12. INSTALLED FABRICATED REPAIR PARTS AT BL 5.7L, WL 180 AND BS 178 IAW BOEING 737-300 SRM 53-10-08-2R 12 FIG 201. 2L72 4F RTA16WE 20051107001212005110700121NM 2005 11 7 AWXA200501304 120051013A5321654583311 FLOOR PANEL BOEING737 7373G7 1384595NM BS 195 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - DURING C16 CHECK DISCOVERED FLOOR WEB CRACKED, 1.1 INCHES IN LENGTH, AT BS 195 BL 31L AND WL 207. MAINTENANCE REMOVED FLOOR WEB AT BS 195, BL 31L AND WL 207 IAW BOEING 737-300 SRM 51-40-02-0G FIG 8. FABRICATED REPAIR WEB IAW BOEING 737-300 SRM 53-10-51-2R 8 FIG 201. INSTALLED FABRICATED REPAIR WEB AT BS 195 BL 31L AND WL 207 IAW BOEING 737-300 SRM 53-10-51-2R 8 FIG 201. 2L72 4F RTA16WE 20051107001222005110700122NM 2005 11 7 AWXA200501305 120051013A53216545833 FLOOR PANEL BOEING737 7373G7 1384595NM 195 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - DURING C16 CHECK DISCOVERED FLOOR WEB CRACKED AT BS 195 BL 31R AND WL 207. MAINTENANCE REMOVED FLOOR WEB AT BS 195, BL 31R AND WL 207 IAW BOEING 737-300 SRM 51-40-02-0G FIG 8. FABRICATED REPAIR WEB IAW BOEING 737-300 SRM 53-10-51-2R 8 FIG 201. INSTALLED FABRICATED REPAIR WEB AT BS 195 BL 31R AND WL 207 IAW BOEING 737-300 SRM 53-10-51-2R 8 FIG 201. 2L72 4F RTA16WE 20051107001242005110700124NM 2005 11 7 AWXA200501307 120051101A3397BMS13311122 WIRE BOEING757 7572S7 1384962NM EMERGENCY LIGHT DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW 23323 PHX - EEL - DURING OVERNIGHT INSPECTION DISCOVERED EMERGENCY LIGHT ON SEAT 34L INOPERATIVE. MAINTENANCE REPAIRED WIRING AT SEAT 34L IAW BOEING 757 SPM 20-10-11. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA2NM 20051107001262005110700126NM 2005 11 7 AWXA200501309 120051101A3397BMS13311122 WIRE BOEING757 7572S7 1384962NM EMERGENCY LIGHT OPEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW 23323 PHX - EEL - DURING OVERNIGHT MAINTENANCE DISCOVERED EMERGENCY EXIT LIGHT ON SEAT 22L INOPERATIVE. MAINTENANCE REPAIRED WIRING AT SEAT 22L IAW BOEING 757 SPM 20-10-11. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA2NM 20051107001282005110700128EU 2005 11 7 AWXA200501311 120051030A5320D53670098206 STIFFENER AIRBUS320 A320232 3930326EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28640AW 448 SAL - DURING C1 CHECK DISCOVERED CRACK, 5 INCHES IN LENGTH, LOCATED ON STIFFENING SECTION AT FS 41+19" AND Y1292. MAINTENANCE REMOVED CRACKED STIFFENING SECTION AND INSTALLED NEW STIFFENING SECTION AT FS 41+19" AND Y1292 IAW AIRBUS SRM 51-72-11. 2L72 4F RTA28NM 20051107001292005110700129NM 2005 11 7 AWXA200501312 120051017A5347BAC1520792 SEAT TRACK BOEING737 7373S3 1384711NM BS 887-947 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 MCN - DURING C18 CHECK DISCOVERED CORROSION ON SEAT TRACK AT BS 899 AND BL 25R. CORROSION WAS REMOVED AND WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-00-52-1A 1 FIG 101. REMOVED SECTION OF SEAT TRACK FROM BS 887 TO BS 947 IAW BOEING 737-300 SRM 53-00-52-2R3. FABRICATED NEW SEAT TRACK IAW BOEING 737-300 SRM 53-00-52-2R3. INSTALLED FABRICATED REPAIR PARTS FROM BS 887 TO BS 947 AND BL 25R IAW BOEING 737-300 SRM 53-00-52-2R3 FIG 201. 2L72 4F RTA16WE 20051107001302005110700130NM 2005 11 7 AWXA200501313 120051017A5347BAC1520792 SEAT TRACK BOEING737 7373S3 1384711NM BS 887-947 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 MCN - DURING C18 CHECK DISCOVERED CORROSION ON SEAT TRACK AT BS 899 AND BL 45L. CORROSION WAS REMOVED AND WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-00-52-1A 1 FIG 101. REMOVED SECTION OF SEAT TRACK FROM BS 887 TO BS 947 IAW BOEING 737-300 SRM 53-00-52-2R3. FABRICATED NEW SEAT TRACK IAW BOEING 737-300 SRM 53-00-52-2R3. INSTALLED FABRICATED REPAIR PARTS FROM BS 887 TO BS 947 AND BL 45L IAW BOEING 737-300 SRM 53-00-52-2R3 FIG 201. 2L72 4F RTA16WE 20051107001312005110700131NM 2005 11 7 AWXA200501314 120051017A5347BAC1520762 SEAT TRACK BOEING737 7373S3 1384711NM BS 887-947 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 MCN - DURING C18 CHECK DISCOVERED CORROSION ON SEAT TRACK AT BS 899 AND BL 45R. CORROSION WAS REMOVED AND WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-00-52-1A 1 FIG 101. REMOVED SECTION OF SEAT TRACK FROM BS 887 TO BS 947 IAW BOEING 737-300 SRM 53-00-52-2R3. FABRICATED NEW SEAT TRACK IAW BOEING 737-300 SRM 53-00-52-2R3. INSTALLED FABRICATED REPAIR PARTS FROM BS 887 TO BS 947 AND BL 45R IAW BOEING 737-300 SRM 53-00-52-2R3 FIG 201. 2L72 4F RTA16WE 20051107001332005110700133NM 2005 11 7 AWXA200501316 120051010A53406916970501 CLIP BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 MCN - DURING C18 CHECK DISCOVERED CLIP ANGLE CRACKED, .6 INCHES IN LENGTH, AT STR 15L AT BS 348. MAINTENANCE REMOVED CLIP IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5310-5292-ES2. FABRICATED NEW CLIP ANGLE IAW BOEING AWA ER NR 03-5310-052925-ES2. INSTALLED FABRICATED REPAIR PARTS AT STR 15L AND BS 348 IAW AWA ER NR 03-5310-052925-ES2. 2L72 4F RTA16WE 20051107001342005110700134NM 2005 11 7 AWXA200501317 120051009A534769165096 CLIP BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 MCN - DURING C18 CHECK DISCOVERED CLIP ANGLE CRACKED, .7 INCHES IN LENGTH, AT STR 16L BETWEEN BS 348-351. MAINTENANCE REMOVED CLIP IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5310-5292-ES2. FABRICATED NEW CLIP ANGLE IAW BOEING AWA ER NR 03-5310-052925-ES2. INSTALLED FABRICATED REPAIR PARTS AT STR 16L BETWEEN BS 348 AND BS 351 IAW AWA ER NR 03-5310-052925-ES2. 2L72 4F RTA16WE 20051107001352005110700135NM 2005 11 7 AWXA200501318 120051010A534069265652 CLIP BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 MCN - DURING C18 CHECK DISCOVERED CLIP ANGLE CRACKED, .7 INCHES IN LENGTH, AT STR 16L BETWEEN BS 348-351. MAINTENANCE REMOVED CLIP IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NO. 03-5310-5292-ES2. FABRICATED NEW CLIP ANGLE IAW BOEING AWA ER NR 03-5310-052925-ES2. INSTALLED FABRICATED REPAIR PARTS AT STR 16L BETWEEN BS 348 AND BS 351 IAW AWA ER NR 03-5310-052925-ES2. 2L72 4F RTA16WE 20051107001372005110700137EU 2005 11 7 AWXA200501286 120051027A2530 OVEN AIRBUS320 A320232 3930326EU GALLEY ODOR A AWXAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP28651AW 866 CREW REPORTED FORWARD OVENS EMIT NOXIOUS FUMES WHEN USED. MAINTENANCE REMOVED AND REPLACED FORWARD GALLEY NR 1 OVEN. OPERATIONAL CHECKS GOOD. VENDOR TEAR DOWN REPORT CONFIRMS REASON FOR REMOVAL. UNIT WAS RECEIVED WITH TEMPERATURES OUT OF RANGE. TEMPERATURE PROBE WAS ADJUSTED AND REPAIRED IAW CMM 25-35-53 REV 2. OPERATIONAL TESTS WERE GOOD IAW CMM 25-35-53 REV 2. 2L72 4F RTA28NM 20051107001382005110700138EU 2005 11 7 AWXA200501288 120051025A5347D57130147200 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28640AW 448 SAL - DURING C1 CHECK DISCOVERED CORROSION ON LT INBOARD SEAT TRACK AT Y765 AND FS 36+16". MAINTENANCE REMOVED SEAT TRACK FROM FS 36 TO FS 41 IAW AIRBUS 320 SRM 53-31-15. INSTALLED NEW SEAT TRACK FROM FS 36 TO FS 41 AT Y765 IAW AIRBUS 320 SRM 53-31-15 AND 51-72-11. 2L72 4F RTA28NM 20051107001402005110700140EU 2005 11 7 AWXA200501290 120051020A5347D5713014720200 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28640AW 448 SAL - DURING C1 CHECK DISCOVERED CORROSION ON RT INBOARD SEAT TRACK AT Y-765 AND FR 40+15". MAINTENANCE REMOVED SEAT TRACK FROM FS 36 TO FS 41 IAW AIRBUS 320 SRM 53-31-15. INSTALLED NEW SEAT TRACK FROM FS 36 TO FS 42 AT Y-765 IAW AIRBUS 320 SRM 51-42-11 AND DRAWING NR D53371110. 2L72 4F RTA28NM 20051107001422005110700142NM 2005 11 7 AWXA200501292 120051027A53306545769 SKIN BOEING737 7373G7 1384595NM BS 380 CRACKED A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28303AW 24010 PHX - DISCOVERED BELLY SECTION AT E/E EXHAUST AREA, BS 380 FROM STR 28L TO STR 28R, CRACKED .50 INCHES IN LENGTH. MAINTENANCE REMOVED CRACKED SKIN IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5331-05300-HF1. FABRICATED INTERNAL DOUBLER AND EXTERNAL DOUBLER IAW AWA ER NR 03-5331-05300-HF1. INSTALLED FABRICATED REPAIR PARTS AT BS 380 FROM STR 28L TO STR 28R IAW AWA ER NR 03-5331-05300-HF1. 2L72 4F RTA16WE 20051107001432005110700143NM 2005 11 7 AWXA200501328 120051101A2530 COFFEEMAKER AIRBUSA319 A319132 3930340NM GALLEY SMOKE A AWXAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP28819AW 1395 SJC - SMOKE - FLIGHT ATTENDANT REPORTED A BURNING SMELL IN AFT GALLEY, FOLLOWED BY SMOKE. GALLEY C/B'S WERE PULLED AND WHEN THE 3RD COFFEEMAKER C/B WAS PULLED, SMOKE CEASED. 3RD COFFEE MAKER IS CURRENTLY ON MEL. MAINTENANCE REPLACED THE AFT NR 3 COFEEMAKER. OPS TESTS GOOD. CONFIRMED FAILURE. COLD WATER TUBE WAS SPRAYING WATER ON ELECTRICAL CONNECTION. UNIT WAS REPAIRED AND TESTED IAW B/E AEROSPACE CMM 25-30-09. 2L72 4F RTA28NM 20051107001442005110700144NM 2005 11 7 AWXA200501329 120051102A3350321431 BATTERY AIRBUSA319 A319132 3930340NM EMERGENCY LIGHT FAILED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28806AW 1056 LAX - EEL - DURING OVERNIGHT INSPECTION OPERATIONAL TEST OF EMERGENCY LIGHTS FAILING TEST. MAINTENANCE REMOVED AND REPLACED THE L1 POWER SUPPLY BATTERY PACK. OPERATIONAL TESTS WERE GOOD. 2L72 4F RTA28NM 20051107001522005110700152NM 2005 11 7 AWXA200501323 120051007A53126516300512 BULKHEAD BOEING737 7373S3 1384711NM BS 178 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 MCN - DURING C18 CHECK DISCOVERED WEB CRACKED AT FASTENER HOLE AT BS 178, WL254, BL 9R. MAINTENANCE CUT OUT AND REMOVED DAMAGED AREA OF WEB IAW BOEING 737-300 SRM 53-10-08-2R4 FIG 201. FABRICATED DOUBLER AND FILLER IAW BOEING 737-300 SRM 53-10-08-2R4 FIG 201. INSTALLED FABRICATED REPAIR PARTS AT BS 178, WL254, BL 9R IAW BOEING 737-300 SRM 53-10-08-2R4. 2L72 4F RTA16WE 20051107001532005110700153NM 2005 11 7 AWXA200501324 120051006A572065C2670127 ANGLE BOEING737 7373S3 1384711NM ZONE 500 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 MCN - DURING C18 CHECK DISCOVERED ANGLE CRACKED AT LOWER LEFT WING, INSIDE TOP LT PYLON PANEL NR 57720L, AT FSS 237. MAINTENANCE REMOVED DAMAGED ZEE ANGLE IAW BOEING 737-300 SRM 51-40-02-0R. FORMED NEW ZEE ANGLE IAW BOEING DWG 65C26701 SHEET 1 REV D. INSTALLED FORMED REPAIR PARTS AT FSS 237 AND LT PYLON PANEL 57720L IAW BOEING 737-300 SRM 51-40-02. 2L72 4F RTA16WE 20051107001542005110700154NM 2005 11 7 AWXA200501325 120051009A5340652981818 ATTACH BRACKET BOEING737 7373S3 1384711NM BS 323 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 MCN - DURING C18 CHECK DISCOVERED LOWER L1 SILL ATTACH BRACKET CRACKED, .5 INCHES IN LENGTH, AT BS 323, WL 207 AND BL 66L. MAINTENANCE REMOVED CRACKED BRACKET AND INSTALLED NEW BRACKET AT BS 323, WL 207 AND BL 66L IAW BOEING 737-300 SRM 51-40-02-00. 2L72 4F RTA16WE 20051107001562005110700156NM 2005 11 7 AWXA200501327 120051101A323365448105 ACTUATOR BOEING737 7373S3 1384711NM RT MLG MALFUNCTIONED A AWXAA UNSCHED LANDING O OTHER CLCLIMB 1 WP28313AW26911476 23712 AFTER TAKEOFF, DURING CLIMB, THE RT MLG WOULD NOT STOW PROPERLY. DECLARED EMERGENCY, RETURNED TO ELP & LANDED WITHOUT FURTHER INCIDENT. ACFT FERRIED BACK TO PHX WITH MLG DOWN. MX TROUBLESHOT & FOUND UPLOCK ACTUATOR NOT ENGAGING. REPLACED THE RT MLG UPLOCK ACTUATOR IAW AMWEST TASK CARD R4M32010. LEAK CHECK & OPS CHECKS GOOD. VENDOR TEAR DOWN REPORT SHOWS THAT THE UNIT DID NOT HAVE ANY INCOMING TESTS PERFORMED ON IT. VENDOR FOUND WORN HARDWARE, SCRAPER, SEALS, BACK UP RINGS, AND PACKINGS. UNIT WAS OVERHAULED IAW BOEING OHM 32-30-21 REV. 13. 2L72 4F RTA16WE 20051107001572005110700157NM 2005 11 7 AWXA200501287 120051029A521080330035 RESERVOIR BOEING757 7572G7 1384963NM PAX DOOR ASSIST LOW A AWXAK NONE O OTHER ININSP/MAINT 1 WP28908AW 24233 PHX - EES - DURING OVERNIGHT INSPECTION DISCOVERED THE L2 DOOR ASSIST BOTTLE BELOW LIMITS. MAINTENANCE REMOVED AND REPLACED THE L2 DOOR ASSIST BOTTLE IAW BOEING 757 AMM 51-11-30. 2L72 4F RTA2NM 20051107001592005110700159NM 2005 11 7 AWXA200501294 120051029A3150 WARNING SYSTEM BOEING737 73733A 1384673NM CONFIGURATION FALSE ACTIVATIONA AWXAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 WP28166AW 23627 PHX - ABORTED TAKEOFF - FLT 788 - CREW RECEIVED TAKEOFF WARNING WITH AIRCRAFT IN POWER CONFIGURATION FOR TAKEOFF. AIRCRAFT TAXIED BACK TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED TAKEOFF CONFIGURATION WARNING TASK IAW AMERICA WEST AIRLINES TASK CARD A1B31009. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20051107001622005110700162NM 2005 11 7 AWXA200501297 120051011A575465C2679413 SKIN BOEING737 7373G7 1384595NM ZONE 500 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED 4 CRACKS ON THE BOTTOM OF THE NR 2 SLAT SKIN, INBOARD OF ACTUATOR FROM SS178 TO SS182. MAINTENANCE CUT OUT DAMAGED SKIN IAW BOEING 737-300 SRM 57-43-01-2R6 FIG 201. FABRICATED FILLER AND SPLICE PLATE IAW BOEING 737-300 SRM 57-43-01-2R6 FIG 201. INSTALLED FABRICATED REPAIR PARTS ON THE BOTTOM OF THE NR 2 SLAT SKIN, INBOARD OF ACTUATOR FROM SS178 TO SS182 IAW BOEING 737-300 SRM 57-43-01-2R6 FIG 201. 2L72 4F RTA16WE 20051107002262005110700226EA 2005 11 7 QXEA200501401 120051015A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA BS 1070-1088 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09615QX 10065 YYC - FUSELAGE INT SKIN, BETWEEN FS 1070-FS 1088 AND STR 9R-10R IS SCRATCHED. MAINTENANCE REPAIRED IAW CRJ700/900 SRM 51-12-00-001-001-A01, QX EA R-53-382 AND REO 670-53-61-203. 2L72 4F RTA21EA 20051107002272005110700227EA 2005 11 7 QXEA200501403 120051018A5530AV67021421976 INTERCOSTAL CNDAIRCL600 CL6002C10 1390015EA VERTICAL STAB BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09615QX 10065 YYC - VERTICAL STAB TAIL CONE ASSY HAS A BROKEN INTERCOSTAL. MAINTENANCE REPLACED INTERCOSTAL IAW CRJ-700 SRM 51-42-27-001-001-A01. 2L72 4F RTA21EA 20051107002282005110700228CE 2005 11 7 DXTA200501048 120051102A7714 INDICATOR CESSNA560 560XL 2076702CE PWA 545 PW545A NE N1 MALFUNCTIONED E DXTAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 GL07684QS 5605084 LT N1 GAGE INDICATED 0 JUST AFTER POWER UP AT T/O. NO TAPE OR DIGITS. RAN LT ENGINE TO T/O POWER . N1 TAPE HAD NO DEFECTS. REMOVED UPPER AND LOWER LT ENGINE COWLS TO GAIN ACCESS TO N1 SENSOR. RANG OUT SENSOR IAW PWA MM CH. 77-10-01. NO DEFECTS NOTED. COULD NOT DUPLICATE SQUAWK. 2L72 4F4 FRTA22CE E00059EN 20051107002302005110700230NM 2005 11 7 AWXA200501333 120051021A5320654795711 STRAP BOEING737 7373G7 1384595NM BS 787-847 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - DURING C18 CHECK DISCOVERED CORROSION ON AFT CARGO BAY DOOR CUTOUT TORQUE BOX STRAP, IN SEVERAL AREAS AROUND FASTENER HOLES FROM BS 787 TO BS 847, WL 158 AND BL 22R. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-00-15-1A FIG 101. INSTALLED TORQUE BOX STRAP FROM BS 787 TO BS 847, WL 158 AND BL 22R IAW BOEING 737-300 SRM 51-40-02-0G FIGS 3 AND 8. 2L72 4F RTA16WE 20051107002312005110700231NM 2005 11 7 AWXA200501334 120051011A53116546541504 FRAME BOEING737 7373G7 1384595NM BS 663 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - DURING C16 CHECK DISCOVERED FRAME CRACKED AT BS 663 FROM STR 1L TO STR 3L. MAINTENANCE REMOVED STRINGER SPLICE AND STRINGER SPLICE STRAPS IN ADDITION TO STOP DRILLING CRACKS IAW BOEING 737-300 SRM 53-00-07-2R9 FIG 201. FABRICATED ANGLE, FILLERS AND STRINGER SPLICES IAW BOEING 737-300 SRM 53-00-07-2R 9. INSTALLED FABRICATED REPAIR PARTS AT BS 663 FROM STR 1L TO STR 3L IAW BOEING 737-300 SRM 53-00-07-2R 9. 2L72 4F RTA16WE 20051107002352005110700235NM 2005 11 7 WRNA200050026 120051105A7830 COWLING BOEING747 747200 1384847NM PWA JT9 JT9D7J 52054NE THRUST REVERSER MISSING A WRNAO OTHER O OTHER NRNOT REPORTED 1 SO05524UP 21446 702000 UPON LANDING AT SKBO, POST FLIGHT REVEALED THAT NR 1 ENGINE REVERSER COWLING MISSING. 2L74 4F4 FRTA20WE E20EA 20051107002372005110700237EU 2005 11 7 05FDEA03610 120051103A5320 PAN AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 RT OB MOST FLOOR PAN BETWEEN FS 33 AND 34 HAS 3 AREAS OF CORROSION, REF N00550. REMOVED AND REPLACED THRUST PLATE IAW SRM 51-72-10. 2L72 4F RTA35EU 20051107002392005110700239EU 2005 11 7 05FDEA03612 120051103A5320 ROLLER TRAY AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 CENTER ROLLER TRAY FS 33 TO FS 20 RT SIDE FLOOR PANEL ATTACH HOLES HAVE MINOR CORROSION AND MISSING PROTECTIVE COATING, REF N00523. REMOVED AND REPLACED ROLLER TRAY IAW AMM 25-52-21-4. 2L72 4F RTA35EU 20051107002402005110700240WP 2005 11 7 05FDEA03613 120051103A5753 SKIN DOUG DC10 DC1030F 3023504WP ZONE 600 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25310FE 48299 RIGHT WING INBOARD FLAP HAS SPEED TAPE (LINE REPAIR) AFT OF NR 7 TIRE. REMOVED TEMP REPAIR AND REPAIRED SKIN IAW DC10 SRM 57-10-00 VOL I AND FEDEX EA 8-5750-91110 PART 3. P3 MOD TYPE T MOD REV NO A PS P3. EA IS ATTACHED TO WORK CARD 57501429, WORK ORDER 00030375, WRI 57501429. SEE NONROUTINE N00149 OF WORK ORDER 00030375. 2L73 4F RTA22WE 20051107002412005110700241NM 2005 11 7 05FDEA03614 120051103A5311 FRAME BOEING727 72722 1384002NM BS 520 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 FUSELAGE, MAIN FRAME FORWARD CARGO DOOR FORWARD FRAME REPLACEMENT AD'S 90-06-09 AND 98-11-03 R1 (LOG BOOK ENTRY REQUIRED). REPAIRED PER E.A. 7-5310-93709 2L73 4F A3WE 20051107002422005110700242NM 2005 11 7 05FDEA03615 120051103A5313 STRINGER BOEING727 72722 1384002NM BS 384-396 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 STR 25R REQUIRES ENGINEERING DISPOSITION PER EO 7-5100-7-5000 PT1. COMPLIED WITH E.A. 7-5330-91409 2L73 4F A3WE 20051107002462005110700246NM 2005 11 7 05FDEA03619 120051104A5713 STRINGER DOUG MD11 MD11F 3023600NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 DURING HFEC INSPECTION, FOUND CRACK INDICATION AT RIGHT WING, END OF STRINGER 9. 2L73 4F RTA22WE 20051107002472005110700247WP 2005 11 7 05FDEA03595 120051101A2611 SMOKE DETECTOR DOUG MD10 MD1010F 3022112WP CARGO BAY FALSE ACTIVATIONA FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25359FE 46635 AIR TURN BACK, GOT A RED LEVEL 3 CARGO SMOKE WARNING AT 18,000. RAN QRH PROCEDURE AND WARNING QUIT, WARNING RETURNED ON SHORT FINAL TO TPA, MEL: ACN RELEASED FOR SERVICE PER MEL/CDL: 26-17-01-03-A CATEGORY: C EXPIRATION: NR 4 MAIN DECK CENTERLINE SMOKE DETECTORS INOP. FOUND NR 4 MAIN DECK SMOKE DETECTOR INTERMITTENT. CAP AND STOW ELECTRICAL CONNECTOR. AS PER MEL. REMOVED AND REPLACED NR 4 MAIN CARGO DECK CENTERLINE SMOKE DETECTOR PER MD10-10 M/M REF 26-15-01-4. OPS CHECK GOOD. 2L73 4F RTA22WE 20051107002492005110700249SO 2005 11 7 658-110405 120051104A56101159SCB51021 WINDSHIELD GULSTMGV GULFSTREAMGV3980116SO COCKPIT BROKEN E N93AA UNSCHED LANDING O OTHER CRCRUISE 1 SO13516QS3407 658 LEFT WINDSHIELD SHATTERED DURING FLIGHT. 2L72 4F RTA12EA 20051107002512005110700251EU 2005 11 7 05FDEA03599 120051101A5330 SKIN AIRBUS310 A310222 3930315EU FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25450FE 162 SMALL DENT LT SIDE OF FUSELAGE ABOVE CAPT FIXED WINDOW 1" FWD OF FS 9 DENT .8" LONG AND APPROX 0.150" DEEP REF N00052. CUTOUT DAMAGED AREA AND REPAIRED IAW A310 SRM 53-11-12 AND 53-27-00. REPROTECTED REPAIRED AREA IAW A310 SRM 51-21-00 AND 51-23-00. 2L72 4F RTA35EU 20051107002522005110700252EU 2005 11 7 05FDEA03600 120051101A5330 SKIN AIRBUS310 A310222 3930315EU FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25450FE 162 DEEP GOUGE W/DENT TOP OF CROWN SKIN AT FS 14 Y = 12 RT APPROX 3.5" LONG AND 2 INCH WIDE AND 0.25 DEEP REF N00055. REMOVED DAMAGE FABBED DOUBLER ALODINE PRIME AND PAINTED AND INSTALLED DOUBLER IAW A310 SRM 53-12-12 NDT FOR CRACKS IAW NTM 51-10-08, NONE NOTED. 2L72 4F RTA35EU 20051107002542005110700254WP 2005 11 7 05FDEA03602 120051102A5330 SKIN DOUG DC10 DC1010 3022110WP BS 383-374 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 NOSE RT SIDE ON SKIN FROM STA 383 TO STA 374 UPPER LONG 36 FOUND 1EA DENT (LENGTH 1.65 INCH DEPTH 0.075 INCH) AND 1EA DENT (LENGTH 0.315'' DEPTH 0.028''). PERFORMED NDI INSPECTION NO CRACK FOUND. REFORMED DENT IAW SRM 51-10-00 AND FABRICATED DOUBLER IAW DETAIL PART TRAVELER F148061-3/N000061. INSTALLED INTERNAL DOUBLER IAW SRM 53-20-00 FIG 13 DET H. 2L73 4F A22WE 20051107002552005110700255WP 2005 11 7 05FDEA03603 120051102A5330 SKIN DOUG DC10 DC1010 3022110WP BS 295-304 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 LWR FUSELAGE EXT STRUCTURE FOUND DEEP DENT ON SKIN (2'' BY 1'' DEEP 0.07'') BTWN STA 295 AND STA 304 BY 15 LT SIDE. REFORMED DENT AS PER SRM 53-20-00 FIG 13 SHT 14 VOL 1. INSTALLED FINGER DOUBLER AS PER SRM 53-20-00 FIG 13 SHT 14 VOL 1. 2L73 4F A22WE 20051107002572005110700257NM 2005 11 7 05FDEA03605 120051102A5260 WARNING LIGHT BOEING727 727227 1384078NM AIRSTAIR ILLUMINATED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25481FE 21463 ON DEPARTURE AFT AIRSTAIR LIGHT ILLUMINATED ON S/O PANEL, RETURNED TO MEM, LIGHT EXTINGUISHED ON TOUCHDOWN. ACN RELEASED FOR SERVICE PER MEL/CDL: 52-06-B CATEGORY: C EXPIRATION: 2L73 4F A3WE 20051107002612005110700261EU 2005 11 7 05FDEA03609 120051103A5320 FLOOR SUPPORT AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 FLOORBOARD SUPPORT BEAM FS 23 LT SIDE BETWEEN MIDDLE LT AND OB MOST ROLLER TRAY HAS CORROSION AROUND HOLE AS MARKED REF N00529. REMOVED AND REPLACED SUPPORT BEAM IAW SRM 51-72-10. 2L72 4F RTA35EU 20051107002622005110700262EA 2005 11 7 QXEA200501407 120051015A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 811 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09615QX 10065 YYC - FUSELAGE INT, LEFT O/B SEAT RAIL AT FS 811 HAS PITTING CORROSION ON I/B FACING SURFACE. MAINTENANCE REPAIRED IAW REO 670-53-00-013 REV A. 2L72 4F RTA21EA 20051107002632005110700263EU 2005 11 7 05FDEA03597 120051101A5330 SKIN AIRBUS310 A310222 3930315EU FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25450FE 162 FOUND ACCESS DOOR 134AR HAS 2 EA GOUGES IN SKIN REF N00122. REPAIRED IAW SRM 51-71-30. HFEC PER NTM 51-10-08. DAMAGE REMOVED, NO FURTHER DAMAGE NOTED RESTORED PROTECTIVE COATING IAW SRM 51-23-20 REF N00122. 2L72 4F RTA35EU 20051107002642005110700264EU 2005 11 7 05FDEA03598 120051101A5730 PANEL AIRBUS310 A310222 3930315EU RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25450FE 162 RT WING UPPER LE PANEL 6-7830-7-5007-402 HAS 1 EA CRACK APPROX 3.5" LONG ON IB LE REF N00123. REPAIRED APPROX 3.5 CRACK ON RT WING UPPER LE PNL 6-7830-7-5007-402 USING EPOXY RESIN AND GLASS OVERLAY IAW A310 SRM 51-77-11 PAR 4D. 2L72 4F RTA35EU 20051107002672005110700267EA 2005 11 7 QXEA200501405 120051015A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 796 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09615QX 10065 YYC - FUSELAGE INT, LEFT O/B SEAT RAIL AT FS 796 HAS PITTING CORROSION ON INSIDE EDGES. MAINTENANCE REPAIRED IAW REO 670-53-00-013 REV A. 2L72 4F RTA21EA 20051107002702005110700270NM 2005 11 7 SWAA053459 120051103A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 277 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 277, STR 10L. REMOVED AND REPLADED CLIP PER SRM. 2L72 4F RTA16WE 20051107002712005110700271NM 2005 11 7 SWAA053460 120051103A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM BS 295 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D CHECK, FOUND CABIN FLOORBEAM CORRODED AT BS 295, BETWEEN LBL 20 TO RBL 59, WL 208. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20051107002732005110700273NM 2005 11 7 SWAA053462 120051103A53306545775 SKIN BOEING737 7373H4 1384600NM BS 789 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29336SW 23940 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 789, STR 20L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051107002762005110700276NM 2005 11 7 SWAA053465 120051103A53116517684 FRAME BOEING737 7373H4 1384600NM BS 303 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29375SW 26583 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303.9, STR 16L. REPAIRED FRAME PER SWA EA. 2L72 4F RTA16WE 20051107000902005110700090NM 2005 11 7 UPS05445717 120051031A541065B903604 LINK BOEING747 747212B 1384886NM NR 3 PYLON MOUNTCRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 NR 3 ENG REAR ENGINE MOUNT THRUST LINK FWD LUG LOWER OF BORE FOUND SUSPECTED CRACK INDICATION WHICH WAS GREATER THAN 40 PERCENT FSH, EXCEEDED LIMIT. REFER TO EO NR B747-7120-22596-A FOR THRUST LINK REPLACEMENT. ENGINE REMOVED AND REINSTALLED ON TASK CARD NR 5000. 2L74 4F A20WE 20051107000912005110700091WP 2005 11 7 UPS05845718 120051003A57145597830502 SPAR CAP DOUG DC8 DC873F 302199FWP CENTER WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 FOUND CRACK ON CENTER WING REAR SPAR LWR CAP, INSIDE KEEL BEAM BOX RT SIDE. STOP DRILLED CRACK AT REAR SPAR IAW SK SAA 866-832589, NDT VERIFIED CRACK TERMINATES AT STOP DRILL IAW NDT SPM 06-10-01.001 REPAIRED RT WING, REAR SPAR, LWR CAP CENTER LINE AT XCW-0 IAW UPS DC8-57-20144-A, BOEING MESSAGE 1-131953277-2 DATED 10/12/05, FAA FORM 8100-9 DATED 10/12/05, AND SAA SK 866-832589-A. 2L74 4F RT4A25 20051107000932005110700093 2005 11 7 UPS05M45473 420050920A256560289117 SLIDE DOUG MD11 MD11F 3023600NM L1 ENTRY DOOR MALFUNCTIONED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP 48774 DURING C1 HEAVY MAINTENANCE CHECK, THE L1 DOOR SLIDE ON N275UP WAS INADVERTENTLY DEPLOYED BY MAINTENANCE PERSONNEL, BUT THE SLIDE DID NOT FULLY DEPLOY. REMOVED L-1 FWD ENTRY DOOR SLIDE PER MM 25-61-04 CMM 25-61-11. OK TO INSTALL SLIDE ON L-1 DOOR. INSTALLED SLIDE ON L-1 DOOR IAW MM 25-61-01. NEED TO SERVICE PNEUMATIC BOTTLE FOR L-1 DOOR. SERVICED PNEUMATIC BOTTLE FOR L-1 DOOR IAW MM 12-25-04. 2L73 4F RTA22WE 20051107000972005110700097EA 2005 11 7 COMA0560579 120051031A5240 DOOR CNDAIRCL600 CL6002B19 1900309EA O2 SERVICE OPEN A COMAA UNSCHED LANDING JW WARNING INDICATION INADEQUATE Q C CLCLIMB 1 SO01863AS 7487 FLIGHT 5487 - STALL FAIL MESSAGE AFTER TAKEOFF. FOUND O2 SERVICE DOOR AND GALLEY WATER SERVICE DOOR OPEN. INSPECTED AND FOUND LATCHES WORK PROPERLY. CLOSED DOORS. 2L72 4F RTA21EA 20051107000992005110700099EA 2005 11 7 COMA0560580 120051031A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FALSE ACTIVATIONA COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01915CA 7013 FLIGHT 5582- FLAPS FAIL CAUTION. INSPECTED FLAPS PER AD 98-20-01. NO DEFECTS NOTED. 2L72 4F RTA21EA 20051107001092005110700109SO 2005 11 7 C2XA05BT070 120051006A32608005701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212SO LANDING GEAR FAULTY A C2XAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW27139942588 2588 145291 DURING TAKEOFF, A LANDING GEAR AIR/GROUND FAIL MESSAGE SHORTLY AFTER TAKEOFF & LANDING GEAR LEVER WOULD NOT MOVE TO UP/LOCK POSITION. AIRCRAFT RETURNED AND LANDED UNEVENTFULLY. AIRCRAFT INSPECTED & LANDING GEAR DOWN AND PINNED. MX FERRIED TO BTV. T/S SYSTEM, REMOVED AND REPLACED LEFT MAIN LANDING GEAR NR 1 & 2 PROXIMITY SWITCHES IAW EMB AMM 32-63-01 P/N.80-057-01, S/N'S 3280 AND 3273 AND NOSE GEAR WOW PROXIMITY SWITCH IAW EMB145 AMM 32-63-02, OPS CHECKED SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE. NOTE: MAIN LANDING GEAR PROXIMITY SWITCHES P/N 80-057-01, S/N 3273 TSN/TSO 9392 HRS AND 7335 CYCLES//PROXIMITY SWITCH P/N 80-057-01, S/N 3280 TSN/TSO 7325 HRS AND 5897 CYCLES. 2L72 4T RTT00011AT 20051107001322005110700132NM 2005 11 7 AWXA200501315 120051009A534069265553 CLIP BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 MCN - DURING C18 CHECK DISCOVERED CLIP ANGLE CRACKED, .7 INCHES IN LENGTH, AT STR 16L BETWEEN BS 348-351. MAINTENANCE REMOVED CLIP IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5310-5292-ES2. FABRICATED NEW CLIP ANGLE IAW BOEING AWA ER NR 03-5310-052925-ES2. INSTALLED FABRICATED REPAIR PARTS AT STR 16L BETWEEN BS 348 AND BS 351 IAW AWA ER NR 03-5310-052925-ES2. 2L72 4F RTA16WE 20051107001392005110700139EU 2005 11 7 AWXA200501289 120051020A5347D533711101000 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28640AW 448 SAL - DURING C1 CHECK DISCOVERED CORROSION ON RT INBOARD SEAT TRACK AT Y-765 AND FS 42+18". MAINTENANCE REMOVED SEAT TRACK FROM FS 41 TO FS 47 IAW AIRBUS 320 SRM 51-42-11. INSTALLED NEW SEAT TRACK FROM FS 41 TO FS 47 AT Y-765 IAW AIRBUS 320 SRM 51-42-11 AND DRAWING D53371110. 2L72 4F RTA28NM 20051107001412005110700141NM 2005 11 7 AWXA200501291 120050909A5330 BEAR STRAP BOEING737 73733A 1384673NM BS 349 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW 23634 GYR - DURING C20 CHECK DISCOVERED LEVEL 2 EXFOLIATION CORROSION ON THE INTERNAL DOOR CUTOUT STRUCTURE AT BS 349, STR 19L AND WL 188, AFT CORNER OF AIR STAIR DOOR CUTOUT. MAINTENANCE REMOVED DAMAGED ARE AT THE LOWER AFT CORNER OF AIR STAIR CUT OUT IAW BOEING 737-300 SRM 53-00-01. FABRICATED FILLER, DOUBLER AND TRIPLER IAW AMERICA WEST AIRLINES ENGINEERING REPAIR 03-5310-05279-ES2A. INSTALLED FABRICATED REPAIR PARTS AT BS 349, STR 19L AND WL 188, AFT CORNER OF AIR STAIR DOOR CUTOUT IAW AWA ER NR 03-5310-05279-ES2A. 2L72 4F RTA16WE 20051107001452005110700145NM 2005 11 7 AWXA200501330 120051102A3397BMS13311122 WIRE BOEING757 7572G7 1384963NM EMERGENCY LIGHT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28908AW 24233 SEA - EEL - DURING OVERNIGHT INSPECTION FOUND ROW 8 FORWARD EMERGENCY PATHWAY LIGHT INOPERATIVE. MAINTENANCE FOUND WIRE BROKEN AT SPLICE. INSTALLED NEW SPLICE AT ROW 8 AND OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA2NM 20051107001472005110700147NM 2005 11 7 AWXA200501332 120051013A532069372742 FILLER BOEING737 7373G7 1384595NM BS 645 DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - DURING C16 CHECK DISCOVERED DELAMINATED BONDED DOUBLER AT BS 645 AND STR 9R. MAINTENANCE REMOVED FASTENERS AROUND DISBONDED AREA AND INJECTED SEALANT BETWEEN SKIN AND TAPERED FILLER, FILLING VOID AREA. INSTALLED NEW FASTENERS AND TWO ADDITIONAL FASTENERS AT BS 645 AND STR 9R. SEALED EDGES OF REPAIR IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5361-05301-ES4. ALL WORK WAS PERFORMED IAW AWA ER NR 03-5361-05301-ES4. 2L72 4F RTA16WE 20051107001482005110700148NM 2005 11 7 AWXA200501319 120051007A53206561277503 CHANNEL BOEING737 7373S3 1384711NM BS 360 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 MCN - DURING C18 CHECK DISCOVERED STRINGER SPLICE CHANNEL CRACKED, 1.2 INCHES IN LENGTH, AT STR 14L AND BS 360. MAINTENANCE REMOVED STRINGER SPLICE CHANNEL AT STR 14L, BS 360 AND INSTALLED NEW STRINGER SPLICE CHANNEL AT STR 14L AND BS 360 IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5310-5292-ES2. 2L72 4F RTA16WE 20051107001492005110700149NM 2005 11 7 AWXA200501320 120051008A5312651758243 BULKHEAD BOEING737 7373S3 1384711NM BS 178 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 MCN - DURING C18 CHECK DISCOVERED VERTICAL BEAM WEB CRACKED, 1.1 INCHES IN LENGTH, AT BS 178, WL 182 AND BL 17.1R. MAINTENANCE REMOVED DAMAGED AREA OF WEB IAW BOEING 737-300 SRM 53-10-08-2R 12 FIG 201. FABRICATED WEB AND SHIMS FOR VERTICAL BEAM IAW BOEING 737-300 SRM 53-10-08-2R12. INSTALLED FABRICATED REPAIR PARTS AT BS 178, WL 182 AND BL 17.1R IAW BOEING 737-300 SRM 51-40-02-0G FIG 12. 2L72 4F RTA16WE 20051107001502005110700150NM 2005 11 7 AWXA200501321 120051008A5312651758335 BULKHEAD BOEING737 7373S3 1384711NM BS 178 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 MCN - DURING C18 CHECK DISCOVERED VERTICAL BEAM WEB CRACKED, 1.3 INCHES IN LENGTH, AT BS 178, WL 183 AND BL 5.7R. MAINTENANCE REMOVED DAMAGED AREA OF WEB IAW BOEING 737-300 SRM 53-10-08-2R 12 FIG 201. FABRICATED WEB AND SHIMS FOR VERTICAL BEAM IAW BOEING 737-300 SRM 53-10-08-2R12. INSTALLED FABRICATED REPAIR PARTS AT BS 178, WL 183 AND BL 5.7R IAW BOEING 737-300 SRM 51-40-02-0G FIG 12. 2L72 4F RTA16WE 20051107001512005110700151NM 2005 11 7 AWXA200501322 120051008A5312651758243 VERTICAL BEAM BOEING737 7373S3 1384711NM BS 178 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 MCN - DURING C18 CHECK DISCOVERED VERTICAL BEAM WEB CRACKED, .95 INCHES IN LENGTH, AT BS 178, WL 184 AND BL 17.1L. MAINTENANCE REMOVED DAMAGED AREA OF WEB IAW BOEING 737-300 SRM 53-10-08-2R 12 FIG 201. FABRICATED WEB AND SHIMS FOR VERTICAL BEAM IAW BOEING 737-300 SRM 53-10-08-2R12. INSTALLED FABRICATED REPAIR PARTS AT BS 178, WL 184 AND BL 17.1L IAW BOEING 737-300 SRM 51-40-02-0G FIG 12. 2L72 4F RTA16WE 20051107001582005110700158EU 2005 11 7 AWXA200501293 120051031A3350321454 POWER SUPPLY AIRBUS320 A320232 3930326EU EMERGENCY LIGHT INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28658AW 1110 ORD - EEL - DURING 4 DAY CHECK DISCOVERED EVERY OTHER EMERGENCY EXIT LIGHT ILLUMINATED IN FWD CABIN DURING EMERGENCY LIGHTS TEST. MAINTENANCE REMOVED AND REPLACED THE LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL). OPERATIONAL TESTS WERE GOOD. 2L72 4F RTA28NM 20051107001602005110700160NM 2005 11 7 AWXA200501295 120051030A27512061141 INDICATOR BOEING737 7373G7 1384595NM TE FLAPS INOPERATIVE A AWXAO OTHER N FALSE WARNING APAPPROACH 1 WP28155AW9348 5340 23777 PHX - EMERGENCY LANDING - FLT 541 - ON APPROACH INTO PHX, COMING FROM DFW, CREW REPORTED FLAPS WOULD NOT EXTEND PAST 1 DEGREE IN NORMAL POSITION. IN ALTERNATE POSITION, FLAPS EXTENDED TO 15 DEGREES. CREW DECLARED EMERGENCY FOR PRECAUTIONARY PURPOSES AND LANDED IN PHX WITHOUT FURTHER INCIDENT. PASSENGERS WERE NOT BRACED. MAINTENANCE REMOVED AND REPLACED THE FLAP POSITION INDICATOR IAW TASK CARD R1B27001. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20051107001612005110700161NM 2005 11 7 AWXA200501296 120051011A533065C8576816 SKIN BOEING737 7373G7 1384595NM BS 727E CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED FUSELAGE SKIN CRACK, 1.0 INCHES IN LENGTH, AT BS 727E+3" AND STR 24R. MAINTENANCE CUT OUT DAMAGED SKIN AT BS 727E+3" AND STR 24R IAW BOEING 737-300 SRM 53-00-01-2R-31. FABRICATED DOUBLER, TRIPLER AND FILLER IAW BOEING 737-300 SRM 53-00-01-2R-31. INSTALLED FABRICATED REPAIR PARTS AT BS 727E+3" AND STR 24R IAW BOEING 737-300 SRM 53-00-01-2R-31. 2L72 4F RTA16WE 20051107001642005110700164NM 2005 11 7 AWXA200501299 120051011A5542 SKIN BOEING737 7373G7 1384595NM RUDDER CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 0306 24633 MCN - DURING C16 DISCOVERED RT SIDE OF RUDDER CRACKED, 1.5 INCHES IN LENGTH, FROM RUDDER STA 928 TO RUDDER STA 930. MAINTENANCE REMOVED CRACKED SKIN FROM RT SIDE OF RUDDER IAW BOEING 737-300 SRM 51-70-17-0G REPAIR 1 FIG 11. BONDED REPAIR PLIES TO RT SIDE OF RUDDER FROM RUDDER STA 928 TO RUDDER STA 930 IAW BOEING 737-300 SRM 51-70-17-0G REPAIR 1 FIG 11. 2L72 4F RTA16WE 20051107001662005110700166WP 2005 11 7 ARWA20051005 120051020A324226014122 BRAKE ASSY DOUG DC8 DC863F 302198FWP PWA JT3D JT3D3 52039NE NR 2 DAMAGED A ARWAO OTHER O OTHER TXTAXI/GRND HDL 1 SO19661AV 45969 LOG PAGE NR 117327. NR 2 MAIN WHEEL TIRE BLOWN; NR 2 BRAKE DAMAGED. REMOVED AND REPLACED NR 2 MAIN WHEEL IAW M/M 32-40-1; REMOVED AND REPLACED NR 2 BRAKE ASSEMBLY IAW MM 32-42-1, NO LEAKS NOTICE. 2L74 4F4 F 4A25 1E8 20051107002322005110700232NM 2005 11 7 AWXA200501335 120051013A5311651630160 FRAME BOEING737 7373G7 1384595NM BS 188 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - DURING C16 CHECK DISCOVERED CHORD CRACKED, 1.1 INCHES IN LENGTH, IN OUTBOARD RADIUS AT BS 188, WL 207 AND BL 31L. MAINTENANCE CUT OUT DAMAGED AREA ON CHORD FLANGE IAW BOEING 737-300 SRM 53-00-07-2R11 FIG 201. FABRICATED ANGLE, FILLERS, TAPERED FILLER AND REPAIR ANGLE IAW BOEING 737-300 SRM 53-00-07-2R 11. INSTALLED FABRICATED REPAIR PARTS IAW BOEING 737-300 SRM 53-00-07-2R 11. 2L72 4F RTA16WE 20051107002452005110700245NM 2005 11 7 05FDEA03618 120051104A5347 SEAT TRACK DOUG MD11 MD11F 3023600NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 MAIN DECK COMPARTMENT, SEAT TRACK FOUND CORROSION AT STATION 5/0- 5/73, X=8.5. REPAIR CARRIED OUT IAW SRM 53-70-00 VOL. I FIG. 1 AND SRM 51-33-01 VOL. II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051107002582005110700258EU 2005 11 7 05FDEA03606 120051103A5347 SEAT TRACK AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 MAIN DECK CARGO NR 2 L SEAT TRACK AT FRAME 64 HAS MILD CORROSION REF N00440. REMOVED CORROSION CHECK LIMITS IAW SRM 51-74-10 AND 53-10-16 FIG 101. FOUND TO BE WITHIN LIMITS RESTORED FINISH IAW SRM 51-75-10. 2L72 4F RTA35EU 20051107002652005110700265EA 2005 11 7 QXEA200501406 120051015A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 785 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09615QX 10065 YYC - FUSELAGE INT, LEFT O/B SEAT RAIL AT FS 785 HAS PITTING CORROSION AND A TOOL MARK ON I/B FACING SURFACE. MAINTENANCE REPAIRED IAW REO 670-53-00-013 REV A. 2L72 4F RTA21EA 20051107002782005110700278NM 2005 11 7 SWAA053467 120051103A33501010427 COVER BOEING737 7373H4 1384600NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29390SW 26593 BULLNOSE EMERGENCY LIGHT COVER MISSING AT ROW 8. INSTALLED COVER PER MM. 2L72 4F RTA16WE 20051107002802005110700280NM 2005 11 7 DHL2005742529 120051015A5320 WEB BOEING727 727225 1384077NM BS 1166-1170 CORRODED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15742DH 21290 CORROSION ON SUBDECK FLOOR UPPER SURFACE AT LBL 16 STA 1166 - 1170 AT AFT ENTRY DOORWAY. CUT OUT CORROSION ON SUBDECK FLOOR UPPER SURFACE AT LBL 1166 - 1170 AT AFT ENTRY DOORWAY. FABRICATED AND INSTALLED REPAIR DOUBLER 12.25 X 14.5 INCHES FROM 2024-T3 .050 IAW B727 SRM 51-40-2 FIG 1, 51-10-2, B727 MM 51-20-31 PG 701 & 705, B727 SRM 51-40-2 FIG 1 AND 51-30-2. FABRICATED AND INSTALLED REPAIR CENTER SUB FLOOR WEB 38.75 X 30 X 35 X 19 INCHES FROM 2024-T3 .040 IAW B727 SRM 51-10-1, 51-30-6 PG 1, 51-30-8 PG 1, 51-10-2, B727 MM 51-20-31 PG 101 AND 51-30-2 PARA B. 2L73 4F A3WE 20051107002822005110700282NM 2005 11 7 DHL2005742531 120051026A5313 STRINGER BOEING727 727225 1384077NM BS 1148 UNKNOWN B DHLAK NONE O OTHER ININSP/MAINT 1 SO15742DH 21290 AFT CARGO COMPT AT STR 28R BETWEEN STA1166 THRU STA 1148 NEED REMOVED FOR FRAME REPAIR. CUT AND REMOVED STR 28R STA 1166 TO 1148 TO FOM S/M REPAIR. FABRICATED STRINGER SPLICE 10.0 INCHES FROM BAC1498-131 TREATED, PRIMED AND TOPCOATED REPAIR PARTS AND INSTALLED STRINGER SPLICE IAW B727 SRM 53-10-3, 51-10-2 AND B727 MM 51-20-11. 2L73 4F A3WE 20051107002832005110700283NM 2005 11 7 DHL2005742532 120051027A5322 SHEAR TIE BOEING727 727225 1384077NM BS 1170 CORRODED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15742DH 21290 AFT PIT STA 1170 SHEAR TIE BETWEEN STR 28R AND 29R HAS EXFOLIATED CORROSION. REMOVED SHEAR TIE ANGLE. FABRICATED AND INSTALLED SHEAR TIE ANGLE 12 X 2.75 X 2.5 INCHES FROM 60-12480 - 7075-T6 6511 IAW SRM 51-30-2, 51-20-01, 51-10-2 AND B727 MM 51-20-11, 21-32-0 AND 21-32-11. 2L73 4F A3WE 20051107002842005110700284NM 2005 11 7 USAA051332 120051103A5752654645521C TRIM TAB BOEING737 7373B7 1384580NM AILERON DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 OUTBOARD T/E CORNER DELAMINATED. ROUTED TO COMPOSITE FOR REPAIR IAW SRM 51-70-06 REPAIR NR 6 DEFECT SIZE: 3 INCHES DELAM. 2L72 4F RTA16WE 20051107002862005110700286NM 2005 11 7 USAA051330 120051103A52106545849169 NUT PLATE BOEING737 7374B7 1384702NM ENTRY DOOR FLOORCORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19779AU 24996 ENTRY DOOR FLOOR LEVEL CORROSION. FABRICATED AND INSTALLED NEW NUT PLATE HOLDER PLATE IAW SRM 53-00-50. DEFECT SIZE: 2 X 6 INCH CORROSION. 2L72 4F RTA16WE 20051107002942005110700294EA 2005 11 7 QXEA200501411 120051015A5300 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 398 CORRODED A QXEAO OTHER O OTHER ININSP/MAINT 1 NM09615QX 10065 YYC - FUSELAGE INT, LEFT O/B SEAT RAIL AT FS 398 HAS PITTING CORROSION ON I/B FACING SURFACE. MAINTENANCE REPAIRED IAW REO 670-53-00-013 REV A. 2L72 4F RTA21EA 20051107002962005110700296EA 2005 11 7 QXEA200501414 120051014A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 796 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09615QX 10065 YYC - FUSELAGE INT, RIGHT O/B SEAT RAIL AT FS 796 HAS PITTING CORROSION ON I/B FACING SURFACE. MAINTENANCE REPAIRED IAW REO 670-53-00-013 REV A. 2L72 4F RTA21EA 20051107002972005110700297EA 2005 11 7 QXEA200501410 120051015A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 585 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09615QX 10065 YYC - FUSELAGE INT, LEFT O/B SEAT RAIL AT FS 585 HAS PITTING CORROSION ON I/B FACING SURFACE. MAINTENANCE REPAIRED IAW REO 670-53-00-013 REV A. 2L72 4F RTA21EA 20051107002992005110700299NM 2005 11 7 AALA20050710 120051027A3350BPS73 BATTERY PACK BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21357AA 24038 LAX - EMERGENCY LIGHTS FROM 20AB TO 24AB SEATS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FORM 20AB TO 24AB SEATS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20051107003022005110700302NM 2005 11 7 05FDEA02668 120050826A5754NRB6719501 SKIN DOUG MD11 MD11 3023602NM NR 2 SLAT CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 LHW L/E UPPER SURFACE AFT OF NR 1 AND NR 2 SLAT AREA AT APPROX XORS 150 FOUND WITH EXISTING DOUBLER REPAIR. LT WING L/E UPPER SURFACE AFT OF NR 1 AND NR 2 SLAT AREA AT APPROX XORS 150. CARRIED OUT REPAIR AS PER SRM 57-10-00 FIG 24 VOL I. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051107003032005110700303NM 2005 11 7 05FDEA02670 120050826A5330NDA6313501 SKIN DOUG MD11 MD11 3023602NM BS 899 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 EXISTING REPAIR DOUBLER FOUND AT FWD CARGO DOOR JAMB FWD EDGE AT STA 899 L-37R. FWD CARGO JAMB FWD EDGE STA 899 L-37R SKIN REPAIRED AS PER SRM 53-50-00 FIG 16 VOL I. MAJOR REPAIR PER GMM 6-2-100. 2L73 4F RTA22WE 20051107003042005110700304NM 2005 11 7 05FDEA02671 120050826A5330NDA6313501 SKIN DOUG MD11 MD11 3023602NM BS 999 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 EXISTING REPAIR DOUBLER FOUND AT FWD CARGO DOOR JAMB AFT EDGE AT STA 999 L-41R. FWD CARGO DOOR JAMB AFT EDGE STA 999 L-41R SKIN REPAIRED AS PER SRM 53-50-00 FIG 16 VOL I. MAJOR REPAIR PER GMM 6-2-100. 2L73 4F RTA22WE 20051107003062005110700306NM 2005 11 7 SWAA053493 120051106A21307207375 RELIEF VALVE BOEING737 7373H4 1384600NM CABIN PRESSURE FAULTY A SWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW29334SW 23938 AIR TURNBACK, CABIN PRESSURE AUTO FAIL LIGHT ILLUMINATED. REMOVED AND REPLACED LT CABIN PRESSURE SAFETY RELIEF VALVE PER MM. 2L72 4F RTA16WE 20051107003072005110700307NM 2005 11 7 CALA0500386 120051105A3230 SWITCH BOEING737 737824 13844BZNM MLG W/W OUT OF RIG A CALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2712216 28776 THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM EWR. THE GEAR HANDLE WAS VERY STIFF AND HARD TO MOVE. QRH PROCEDURES WERE FOLLOWED AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE MANUAL EXTENSION SYSTEM ACCESS DOOR SWITCH OUT OF RIG. THE SWITCH WAS ADJUSTED IAW MM 32-34-00-820-802. A GEAR RETRACTION TEST WAS PERFORMED AND OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20051107003082005110700308NM 2005 11 7 CALA0500385 120051104A253045300015 WARMER BOEING737 737824 13844BZNM AFT GALLEY OVERHEATED A CALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2778285 33452 AN ELECTRICAL ODOR ACCOMPANIED BY MOMENTARY SMOKE CAME FROM THE AFT GALLEY WHILE EN ROUTE TO EWR. THE OVEN AND COFFEEMAKER CIRCUIT BREAKERS WERE PULLED AND THE SMOKE AND ODOR CEASED. THE FLIGHT CONTINUED TO EWR WHERE IT LANDED WITHOUT FURTHER PROBLEMS. MAINTENANCE FOUND COFFEE WARMERS AT POSITION 417 AND 418 OVERHEATING. THE COFFEE WARMERS WERE REMOVED AND REPLACED. ALL THREE AFT GALLEY OVENS WERE REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE. ALSO THE AFT GALLEY COFFEE WARMER CIRCUIT BREAKERS WERE REMOVED AND REPLACED. 2L72 4F RTA16WE 20051107003122005110700312NM 2005 11 7 USAA051334 120051104A5311 FRAME BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 BETWEEN STRINGERS S-8R AND S-9R STA 480. CUT OUT DAMAGE, INSTALL FRAME DOUBLERS IAW TR 53-10-20. DEFECT SIZE: .5 INCH. 2L72 4F RTA16WE 20051107003172005110700317NM 2005 11 7 USAA051328 120051103A575365C263208 SKIN BOEING737 7374B7 1384702NM T/E FLAP WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19779AU 24996 INBOARD LEADING EDGE. FABRICATED DOUBLER AND INSTALLED IAW SRM 57-53-01. DEFECT SIZE: 1 X 8 INCH DEEP WEAR AREA ON LEADING EDGE. 2L72 4F RTA16WE 20051107003202005110700320NM 2005 11 7 DXTA200501049 120051102A26127101771050 FIRE LOOP GULSTM200 200 4500308NM LT ENGINE FAILED E DXTAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL07720QS583 085 DURING CLIMB THRU RECEIVED LT ENG FIRE DETECT MSG ON EICAS. RETURNED WITH NO PROBLEM. ACCESS EXTERNAL AND INTERNAL BYPASS DUCT ON LT ENGINE VISUALLY INSPECTED INTERNAL ZONE 2 FIRE DETECTOR ALSO EXTERNAL ZONE 1 FIRE DETECTOR. NO DEFECTS FOUND. REMOVED LOWER PYLON PANELS FOR ACCESS TO CONNECTOR TROUBLESHOT SYSTEM AND FOUND ZONE 2 OVERHEAT LOOP TO BE BAD. REPLACED ZONE 2 FIRE LOOP, OPS CHECKS GOOD. ALL WORK DONE IAW MM 21-10-10. 2L72 4F RTA53NM 20051107003222005110700322NM 2005 11 7 USAA200511003 120051102A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19396US 23318 A 2.5 INCH CRACK FOUND IN FUSELAGE SKIN. INSTALLED EXT SKIN DOUBLER PER SRM 53-00-01 FIG 2. 2L72 4F RTA16WE 20051107003232005110700323SO 2005 11 7 RAIA00510026 120051004A323023092900001 UPLOCK EMB 145 EMB145 3260210SO NLG FAULTY A RAIAA UNSCHED LANDING O OTHER CLCLIMB 1 CE03804HK1579815798 145082 FLT 3520- PIT - NOSE WHEEL FAILED TO RETRACT AFTER TAKEOFF. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR UPLOCK BOX. 2L72 4F RTT00011AT 20051107003242005110700324EA 2005 11 7 QXEA200501402 120051022A3222 CYLINDER CNDAIRCL600 CL6002C10 1390015EA NLG STRUT CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09615QX 10065 YYC - NLG OUTER CYLINDER HAS AREAS OF CORROSION. MAINTENANCE REPAIRED IAW QX EA R-32-197, REO 670-32-21-073, ASTM 1444-01 AND SCR 0008-04 REV C. 2L72 4F RTA21EA 20051107003252005110700325NM 2005 11 7 SWAA053486 120051102A53306545774 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29694SW 23061 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 19R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051107003292005110700329NM 2005 11 7 SWAA053482 120051102A53306545775 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29694SW 23061 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 773, STR 21L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051107003302005110700330NM 2005 11 7 SWAA053481 120051102A53306545775 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29694SW 23061 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 762, STR 21L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051107003322005110700332NM 2005 11 7 SWAA053479 120051102A53306545774 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29694SW 23061 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 25L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051107003332005110700333NM 2005 11 7 SWAA053478 120051102A53306545775 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29694SW 23061 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 22L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051107003362005110700336 2005 11 7 SWAA053475 420051103A2565D31354 SLIDE BOEING737 7373Q8 1384670NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29687SW 23388 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051107003382005110700338NM 2005 11 7 SWAA053473 120051103A53116546554 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT AFT CARGO DOOR CUTOUT, LOWER FRAME NR 5 DOOR STOP FITTING. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20051107003392005110700339NM 2005 11 7 SWAA053472 120051103A55516551524 FITTING BOEING737 7373H4 1384600NM HORIZ STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED D CHECK, FOUND LT AND RT HORIZONTAL STAB ATTACH FITTINGS LUG FACES CORRODED. REPAIRED LUG FACES PER SRM. 2L72 4F RTA16WE 20051107003402005110700340NM 2005 11 7 SWAA053471 120051103A534065C27314 STRINGER CLIP BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29507SW 24184 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051107003412005110700341NM 2005 11 7 SWAA053470 120051103A3350MS155721 LIGHT BOEING737 7377H4 1384404NM EXTERIOR INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29442WN 32459 DURING SCHEDULED MV2 CHECK, FOUND RT AFT EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20051107003422005110700342NM 2005 11 7 SWAA053469 120051103A3350D71702001 BATTERY PACK BOEING737 7377H4 1384404NM CABIN FAILED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29410WN 27897 DURING SCHEDULED HC2 CHECK, CABIN EMERGENCY LIGHTS BATTERY PACKS FAILED TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2L72 4F RTA16WE 20051107003482005110700348NM 2005 11 7 SWAA053498 120051106A25606557463 BRACKET BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29360SW 26571 DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FLOOR BRACKET LOOSE. SECURED BRACKET PER MM. 2L72 4F RTA16WE 20051107003492005110700349NM 2005 11 7 SWAA053499 120051104A3350207377 LENS BOEING737 7373H4 1384600NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29365SW 26576 RIGHT OVERWING LOWER EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM. 2L72 4F RTA16WE 20051107003512005110700351NM 2005 11 7 SWAA053501 120051105A30402315 CONTROLLER BOEING737 7377H4 1384404NM COCKPIT MALFUNCTIONED A SWAAK NONE O OTHER UKUNKNOWN 1 SW29452WN 29846 L2 COCKPIT WINDOW ARCED. REMOVED AND REPLACED L2 WINDOW HEAT CONTROLLER PER MM. 2L72 4F RTA16WE 20051107003532005110700353NM 2005 11 7 SWAA053503 120051104A53306545776 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29519SW 25318 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 932, STR 24L. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20051107003542005110700354NM 2005 11 7 SWAA053504 120051104A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 706, STR 13L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051107003552005110700355NM 2005 11 7 SWAA053505 120051104A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 706, STR 13R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051107003572005110700357NM 2005 11 7 SWAA053508 120051104A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 685, STR 13L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051107003582005110700358NM 2005 11 7 SWAA053509 120051104A53116558280 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051107003592005110700359NM 2005 11 7 SWAA053510 120051105A335020131 BATTERY PACK BOEING737 7373H4 1384600NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29640SW 27713 DURING SCHEDULED SERVICE CHECK, FOUND RT AFT CABIN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20051107003602005110700360NM 2005 11 7 SWAA053487 120051104A53116546532 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051107003622005110700362NM 2005 11 7 SWAA053489 120051104A53116546551 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 8L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051107003632005110700363NM 2005 11 7 SWAA053490 120051104A53116546541 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 2R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051107003692005110700369EA 2005 11 7 SWIA200515794 120050619A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07920SW 7660 FS 280 AT LBL 9 I/B ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. ANGLE REPAIRED IAW REO 601R-53-11-136 AND SRM 51-42-06 AND 51-42-21. 2L72 4F RTA21EA 20051107003712005110700371EA 2005 11 7 SWIA200515796 120050619A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07920SW 7660 AT FS 484 AND RBL 36 JUST UNDER FLOOR LEVEL INTERCOSTAL CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW REO 601R-53-41-059 AND SRM 51-42-06. 2L72 4F RTA21EA 20051107003732005110700373EA 2005 11 7 SWIA200515798 120050704A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07923SW 7664 FWD AVIONICS BAY FS 280 LT FRAME CRACKED BL-+8 AND +11 INBOARD OUTBOARD. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED TWO NEW BRACKETS IAW REO 601R-53-11-136. 2L72 4F RTA21EA 20051107003752005110700375EA 2005 11 7 SWIA200515800 120050704A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07923SW 7664 MAIN CABIN FS 484.00 BC 28RT WL 72 ANGLE CLIP CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW SUPPORT ANGLE IAW REO 601R-53-41-059. 2L72 4F RTA21EA 20051107003762005110700376EA 2005 11 7 SWIA200515801 120050704A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07923SW 7664 AFT CARGO FS 621 LT SIDE ANGLE CRACKED. REPAIR ANGLE IAW REI 601R 53-61-117. 2L72 4F RTA21EA 20051107003782005110700378EA 2005 11 7 SWIA200515803 120051103A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07913SW 7597 FURTHEST AFT CEILING LEVEL EMERGENCY FLOOD LIGHT INOP. RELAMPED EMERGENCY FLOODLIGHT. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051107003792005110700379SO 2005 11 7 SWIA200515804 120051102A3350 LIGHT EMB 120 EMB120ER 3260203SO CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07227SW 120304 FLOOR EMERGENCY LIGHTS 2A INOP. INSTALLED NEW EMERGENCY LIGHT ASSY IAW WM 20-20-00. OPERATIONAL CHECK GOOD IAW 33-50-00. 2L72 4T RTA31SO 20051107003802005110700380EA 2005 11 7 SWIA200515805 120051029A2751 CONNECTOR CNDAIRCL600 CL6002C10 1390015EA T/E FLAP CORRODED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07710SK 10170 FLAPS HALFSPEED STATUS MESSAGE. REPAIRED CONNECTOR AT WS 54.55 SKEW DETECTOR RT/IND FLAP. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051108000012005110800001WP 2005 11 8 IXXA05SMN238S 120051013A5730 DOUBLER DOUG DC8 DC871F 302199DWP XFS 342.500 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING ROUTINE C-CHECK INSPECTION, LEFT WING CTR L/E LWR INTERNAL DOUBLER CRACK 2 AT STA XFS 342.500. REMOVED CRACKED INTERNAL DOUBLER IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D. FABRICATED NEW INTERNAL DOUBLER (AL7075T6 0.090”) IAW DC8 SRM 57-3-1 FIG 4. CLEANED, TREATED, PRIMED AREA + INTERNAL DOUBLER IAW DC8 SRM 51-1-8B. INSTALLED INTERNAL DOUBLER IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D, DC8 SRM 51-3-1. 2L74 4F RT4A25 20051108000022005110800002WP 2005 11 8 IXXA05SMN245S 120051013A5340 FITTING DOUG DC8 DC871F 302199DWP BS 897.375 IMPROPER B IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW11829BX896722998 45994 DURING ROUTINE C-CHECK INSPECTION, RIGHT MLG W/W - L-24R FITTING HAS NO STANDARD REPAIR AT STA 879.375. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-0 FIG 8. REMOVED NON STANDARD REPAIR IAW DC8 SRM 51-1-20D. FABIRCATED (4) REPAIR FITTING (P/N 5802677-4) FROM AL7075T7351 IAW DC8 SRM 53-2-0 FIG 8 (SHEET 1, 3, 6). CLEANED, TREATED, PRIMED AREA + REPAIR FITTING IAW DC8 SRM 51-1-8B. INSTALLED REPAIR FITTING IAW DC8 SRM 53-2-0 FIG 8 (SHEET 1, 3, 6) DC8 SRM 51-1-20D, DC8 SRM 51-3-1 (TORQUE). 2L74 4F RT4A25 20051108000032005110800003EA 2005 11 8 QXEA200501398 120051016A5753 GUIDE CNDAIRCL600 CL6002C10 1390015EA TE FLAPS CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09615QX 10065 YYC - LEFT WING AFT SHROUD AREA AT STA 169, ON O/B FLAP ROLLER GUIDE FITTING CHAFED BY FLAP ROLLER FITTING. MAINTENANCE REPAIRED IAW REO 670-57-51-036, CRJ-700 NDTM PT 1, 51-20-006, SRM TASK 51-24-11-001-001-A01 AND FIELD P.S.18.0, CRJ 700/900 SRM 51-21-16, AND CRJ 700/900 SRM 51-42-21-001-001-A01. 2L72 4F RTA21EA 20051108000122005110800012CE 2005 11 8 DELA200500010 120051021A7500 WARNING LIGHT LEAR 45 45LEAR 5170805CE LT BLEED SYS FALSE ACTIVATIONE DELAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03545EC 199 DURING INITIAL CLIMB, THE LEFT BLEED LEAK WARN LIGHT ILLUMINATED. CHECK LIST PROCEDURES FOLLOWED BUT LIGHT FAILED TO EXTINGUISH. PRECAUTIONARY LANDING WAS MADE. MAINTENANCE TECH INSPECTED WARN SYSTEM. NO DEFECTS NOTED. GROUND RUN AND SUBSEQUENT FLIGHT SHOWED NO DUPLICATION. 2L72 4F RTT00008WI 20051108000152005110800015WP 2005 11 8 IXXA05SMN232S 120051013A5730 DOUBLER DOUG DC8 DC871F 302199DWP XW 105.000 IMPROPER B IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW11829BX896722998 45994 DURING ROUTINE C-CHECK INSPECTION, LEFT INBOARD FLAP L/E UPPER SKIN HAS NON STANDARD REPAIR, XW 105.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 57-7-1, EO SEMAN 20051209. REMOVED DAMAGED PANEL PLATING IAW DC8 SRM 57-1-0 PG 1, DC8 SRM 51-1-21. FABRICATED NEW PANEL PLATING (AL2024T3 0.025) + BONDED FINGER DOUBLER (AL2024T3 0.020) IAW DC8 SRM 57-7-1 FIG 1. BONDED PARTS WITH HYSOL IAW DC8 SRM 51-1-9, DC8 SRM 51-1-9A, DACO DPS 1.950. CLEANED, TREATED, PRIMED NEW PANEL PLATING INNER FACE IAW DC8 SRM 51-1-8B. APPLIED (PRC) SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED NEW PANEL PLATING IAW DC8 SRM 51-1-21. 2L74 4F RT4A25 20051108000232005110800023EU 2005 11 8 SA05112 120051105A335032145410 EPSU AIRBUS320 A320214 3930316EU EMERGENCY LIGHTSFAULTY A USAAK NONE L NO TEST ININSP/MAINT 1 EA19102UW1488277 844 DCA - THE EMERGENCY LIGHTS FAILED THE OPERATIONAL TEST. MAINTENANCE REPLACED THE LEFT HAND, MID CABIN EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20051108000352005110800035NM 2005 11 8 UPS05445720 120051104A541065B903604 LINK BOEING747 747123 1384873NM NR 1 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:AD NR 1 NACELLE REAR ENGINE MOUNT THRUST LINK, CRACK INDICATION REVEALED AT AFT END LUG EXCEEDED LIMIT. NR 1 ENG REAR MOUNT THRUST LINK REPLACED AS PER EO B747-7120-22596-A ON APPENDIX-F. ENG REMOVED AND REINSTALLED AS PER UPS TASK CARD TC 5000. 2L74 4F A20WE 20051108000362005110800036WP 2005 11 8 UPS05845721 120051017A53405641008501 FITTING DOUG DC8 DC873F 302199FWP BS 798 L19L CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE:C1 MAIN CARGO COMPARTMENT LEFT STA 798 LONGERON 19L BOOT FITTING CRACKED IN RADIUS 4 INCHES LONG. REMOVED AND REPLACED BOOT FITTING IAW DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20051108000372005110800037WP 2005 11 8 UPS05845722 120051017A534037798742 FITTING DOUG DC8 DC873F 302199FWP BS 840 L12R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE:C1 MAIN CARGO COMPARTMENT RT STA 840 L12R INTERCOSTAL FITTING CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FITTING IAW DWG 3779874 AND DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20051108000382005110800038WP 2005 11 8 UPS05845723 120051017A534038877991 FITTING DOUG DC8 DC873F 302199FWP BS440-460 L14R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE:C1 MAIN CARGO COMPARTMENT RIGHT BETWEEN STA 440-460 SPLICE FITTING CRACKED L14R. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW DWG 3887799 AND DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20051108000422005110800042WP 2005 11 8 UPS05845727 120051020A534047516391 FITTING DOUG DC8 DC873F 302199FWP BS 798 L19L CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE:C1 MAIN CABIN FITTING CRACKED AT STA 798 L19L. REMOVED, FABRICATED, AND INSTALLED FITTING IAW DWG 4751639 AND DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20051108000462005110800046WP 2005 11 8 IXXA05RNG067S 120050916A5330 SKIN DOUG DC8 DC872 302199BWP BS 1120-1140 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK WAS FOUND CORROSION ON INTERNAL SKIN OF PASSENGER WINDOW STA 1120-1140, LEFT. CORRODED AREA WAS REMOVED AND REPAIR DOUBLER WAS INSTALLED IAW EWO ATI-53-021 AND SRM 53-2-0 FIGURE 22A, TR 53-170. 2L74 4F RT4A25 20051108000472005110800047NM 2005 11 8 EVAS094003 120050930A2840 INDICATION SYS DOUG MD11 MD11F 3023600NM FUEL SYSTEM MALFUNCTIONED W QOCFA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP0316113 48790 DURING AIRCRAFT CLIMBING , CAPTAIN FOUND THE FUEL INDICATION UNRELIABLE (FUEL INDICATION SHOW 800KG AND INDICATION STUCK UNTIL AIRCRAFT TOUCHDOWN). AFTER AIRCRAFT LANDING, FUEL INDICATION BACK TO NORMAL. REPLACED SEM, SYSTEM TEST OK AND CONFIRMED FUEL QUALITY BY FUEL STICK. 2L73 4F RTA22WE 20051108000482005110800048NM 2005 11 8 EVAS094001 120050127A2130 SHUTOFF VALVE BOEING767 767200 1385120NM LT A/C PACK FAILED W QOCFA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP0316623 27194 WHEN AIRCRAFT FLEW TO 31,000 FT , CAPTAIN FOUND BOTH PACK TRIP OFF. AIRCRAFT DESCENT TO 10,000 FT, THEN LEFT PACK RECOVERED. FOR SAFETY REASON, AIRCRAFT DIVERTED TO MNL. ON GROUND CHECK, FOUND LEFT PRSOV (PRESSURE REGULATING SHUT OFF VALVE) MODULATING FUNCTION NO GOOD AND RIGHT FCV (FLOW CONTROL VALVE) TORQUE MOTOR ELECTRICAL CONNECTOR WAS NO GOOD. REPLACED BOTH COMPONENTS, AIRCRAFT CONDITION BACK TO NORMAL. 2L72 4F RTA1NM 20051108000542005110800054SO 2005 11 8 C2XA05IA115 120051018A21308166041 CONTROL VALVE EMB 145 EMB145XR 3260214SO FUSELAGE INOPERATIVE A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SW2712145 145745 IAH - FLIGHT 2955, CREW REPORTED A OILY BURNING ODOR IN THE COCKPIT AND FORWARD CABIN DURING DESCENT WITH A PAX OVERLOAD INDICATION IN AUTO. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE PLACED THE PAX SYSTEM ON MEL 21-30-00/1 CAT C CONTORL NUMBER 060980, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 10/20/05 THE AIRCRAFT RON'D AT MCI WHERE MAINTENANCE REMOVED AND REPLACED THE LEFT HAND PACK CONTROL VALVE, OPERATIONALLY CHECKED WITH NO DEFECTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20051108000552005110800055NM 2005 11 8 P5CA0501411 120051026A3244 TIRE BOEING747 747123 1384873NM MLG FAILED A P5CAK NONE M OVER TEMP ININSP/MAINT 1 EA15858FT 20109 ON TAXI INTO BLOCKS NR 10 AND 12 THERMALED. REPLACED NR 9, 10, 11 AND 12 TIRES IAW MM 32-45-01. 2L74 4F A20WE 20051107000922005110700092WP 2005 11 7 UPS05845719 120051019A5330 FINGER DOUBLER DOUG DC8 DC873F 302199FWP BS 207 L21L CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 FOUND FINGER DOUBLER AT FS 207 HAS TWO CRACKS 3" AND 2" BELOW L21L. REMOVED FINGER DOUBLER AT FS 207 L21L IAW SRM 51-1-20D. FABRICATED AND INSTALLED FINGER DOUBLER AT FS 207 L21L IAW SRM 53-4-1 FIG 4, AND SRM 51-1-21. 2L74 4F RT4A25 20051107001132005110700113SO 2005 11 7 C2XA05SH125 120051101A532014521713005 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711551 145411 SHV - DURING C-CHECK MAINTENANCE FOUND CENTER OMEGA BEAM AT FRAME 20 WITH CORROSION BETWEEN RAMP ANGLE AND BUTTSTRAP. MAINTENANCE REPAIRED CENTER OMEGA BEAM AT FRAME 20 IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20051107001182005110700118NM 2005 11 7 AWXA200501301 120051010A5755654645170SP SPOILER BOEING737 7373G7 1384595NM NR 8 DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - DURING C16 CHECK DISCOVERED DISBOND AREA ON THE NR 8 SPOILER UPPER AND LOWER SURFACE, 15.5" FROM OUTBOARD END AND 6" FROM THE AFT EDGE, FROM WL 430.97 TO WBL 432.97. MAINTENANCE CUT OUT AND REMOVED DAMAGED SKIN AND CORE FROM THE NR 8 SPOILER IAW BOEING 737-300 SRM 51-70-10-2R4 REPAIR 4 FIG 201. FABRICATED DOUBLER AND REPAIR CORE FOR UPPER AND LOWER SURFACE OF THE NR 8 SPOILER IAW BOEING 73-300 SRM 51-70-10-2R4. BONDED REPAIR PARTS TO THE NR 8 SPOILER UPPER AND LOWER SURFACE, 15.5" FROM OUTBOARD END AND 6" FROM THE AFT EDGE, FROM WBL 430.97 TO WBL 432.97 IAW BOEING 737-300 SRM 51-70-10-2R4 REPAIR 4 FIG 201. 2L72 4F RTA16WE 20051107001192005110700119NM 2005 11 7 AWXA200501302 120051010A53136546877 STRINGER BOEING737 7373G7 1384595NM BS 727 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - DURING C16 CHECK DISCOVERED STRINGER 18A CRACKED, 2.0 INCHES IN LENGTH, AT BS 727 AND FROM WL 212 TO WL 213. MAINTENANCE TRIMMED OUT CRACK ON STRINGER IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5361-05298-SS1. FABRICATED WEB FILLER, RADIUS FILLER, STIFFENER AND GUSSET IAW AWA ER NO 03-5361-05298-SS1. INSTALLED FABRICATED REPAIR PARTS ON STRINGER 18A AT BS 727 AND FROM WL 212 TO WL 213 IAW AWA ER NR 03-5361-05298-SS1. 2L72 4F RTA16WE 20051107001232005110700123NM 2005 11 7 AWXA200501306 120051023A534069429494 ATTACH ANGLE BOEING737 7373G7 1384595NM BS 807 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - DURING C16 CHECK DISCOVERED AFT CARGO BAY DOOR CUTOUT TORQUE BOX LOWER FRAME TO WEB ATTACH ANGLE CRACK, .3 INCHES IN LENGTH, AT BS 807 AND BL 22R. MAINTENANCE REMOVED CRACKED ANGLE AND INSTALLED NEW ATTACH ANGLE AT BS 807, BL 22R IAW BOEING 737-300 SRM 51-40-02-0G FIG 8. 2L72 4F RTA16WE 20051107001252005110700125NM 2005 11 7 AWXA200501308 120051101A3350252005 FUSE BOEING757 7572S7 1384962NM ESCAPE SLIDE OPEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW 23323 PHX - EEL - DURING OVERNIGHT MAINTENANCE DISCOVERED EMERGENCY ESCAPE SLIDE LIGHT NEXT TO L1 DOOR INOPERATIVE. MAINTENANCE REPLACED FUSE IN POWER SUPPLY M731. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA2NM 20051107001272005110700127EU 2005 11 7 AWXA200501310 120051020A5347D57130147202 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28640AW 448 SAL - MAJOR REPAIR - DURING C1 CHECK DISCOVERED CORROSION ON LT OUTBOARD SET TRACK AT FR37 AND Y1292. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 101. REMOVED SEAT TRACK FROM FS 36 TO FS 41 AT Y1292 IAW AIRBUS 320 SRM 51-42-11 AND INSTALLED NEW SEAT TRACK FROM FS 36 TO FS 41 AT Y1292 IAW AIRBUS 320 SRM 51-72-11. 2L72 4F RTA28NM 20051107001362005110700136NM 2005 11 7 AWXA200501285 120051026A53306545775 SKIN BOEING737 7373G7 1384595NM BS 727D CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 PHX - DURING OVERNIGHT INSPECTION DISCOVERED RT SIDE OF FUSELAGE SKIN CRACK 2 INCHES IN LENGTH LOCATED AT BS 727 D AND FROM STR 22R TO STR 23R. MAINTENANCE REMOVED DAMAGED SKIN IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5361-05300-RC1. FABRICATED DOUBLER AND TRIPLER IAW AWA ER NR 03-5361-05300-RC1. INSTALLED FABRICATED REPAIR PARTS AT BS 727D AND FROM STR 22R TO STR 23R IAW AWA ER NR 03-5361-05300-RC1. 2L72 4F RTA16WE 20051107001462005110700146NM 2005 11 7 AWXA200501331 120051013A532069372741 FILLER BOEING737 7373G7 1384595NM BS 612 DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - DURING C16 CHECK DISCOVERED DELAMINATED BONDED DOUBLER AT BS 612 AND STR 9L. MAINTENANCE REMOVED FASTENERS AROUND DISBONDED AREA AND INJECTED SEALANT BETWEEN SKIN AND TAPERED FILLER, FILLING VOID AREA. INSTALLED NEW FASTENERS AND TWO ADDITIONAL FASTENERS AT BS 612 AND STR 9L. SEALED EDGES OF REPAIR IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5361-05302-ES1. ALL WORK WAS PERFORMED IAW AWA ER NR 03-5361-05302-ES1. 2L72 4F RTA16WE 20051107001552005110700155NM 2005 11 7 AWXA200501326 120051020A575369388488 CAM BOEING737 7373S3 1384711NM ZONE 600 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 MCN - DURING C18 CHECK DISCOVERED CORROSION ON THE RT INBOARD MID FLAP, OUTBOARD CARRIAGE, INBOARD FORE FLAP SEQUENCE CAM TRACK. MAINTENANCE REMOVED AND REPLACED THE RT INBOARD MID FLAP, OUTBOARD CARRIAGE, INBOARD FORE FLAP SEQUENCE CAM TRACK IAW BOEING SOPM 20-50-01 PAGES 1 THROUGH 9. 2L72 4F RTA16WE 20051107001632005110700163NM 2005 11 7 AWXA200501298 120051011A575465C2679413 SKIN BOEING737 7373G7 1384595NM LE SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - DURING C16 CHECK DISCOVERED 4 CRACKS ON THE BOTTOM OF THE NR 2 SLAT SKIN, OUTBOARD OF ACTUATOR FROM SS221 TO SS225. MAINTENANCE CUT OUT DAMAGED SKIN IAW BOEING 737-300 SRM 57-43-01-2R6 FIG 201. FABRICATED FILLER AND SPLICE PLATE IAW BOEING 737-300 SRM 57-43-01-2R6 FIG 201. INSTALLED FABRICATED REPAIR PARTS ON THE BOTTOM OF THE NR 2 SLAT SKIN, OUTBOARD OF ACTUATOR FROM SS221 TO SS225 IAW BOEING 737-300 SRM 57-43-01-2R6 FIG 201. 2L72 4F RTA16WE 20051107001652005110700165EA 2005 11 7 ASOA05868 120051013A5210601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27885AS 7521 DURING A GROUND INSPECTION IN ATL, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN AT THE RETRACTING LEVER. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051107001672005110700167WP 2005 11 7 ABXA050262 120051101A335060030451 POWER SUPPLY DOUG DC9 DC931 3022065WP EMERGENCY LIGHTSWEAK A ABXAO OTHER L NO TEST NRNOT REPORTED 1 GL23944AX 691 47550 ON PREFLIGHT, THE EMERGENCY EXIT PEANUT LIGHTS WERE INOP. REMOVED & REPLACED EMERGENCY BATTERIES PER DC9 AMM 33-53 OPS CHECKED GOOD. ON SUBSEQUENT MAINTENANCE, THE BATTERY EMERGENCY POWER SUPPLY WAS REPLACED. 2L72 4F A6WE 20051107002292005110700229EA 2005 11 7 QXEA200501404 120051015A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 739 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09615QX 10065 YYC: FUSELAGE INT, LEFT O/B SEAT RAIL AT FS 739 HAS PITTING CORROSION ON INSIDE AND I/B FACING SURFACES. MAINTENANCE REPAIRED IAW REO 670-53-00-013 REV A. 2L72 4F RTA21EA 20051107002332005110700233NM 2005 11 7 AWXA200501336 120051019A532065479573 WEB BOEING737 7373G7 1384595NM BS 800-840 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - DURING C16 CHECK DISCOVERED CORROSION AROUND FASTENER HOLES ON AFT CARGO THRESHOLD WEB. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-15-1A1. REMOVED AND REPLACED THE AFT CARGO THRESHOLD WEB FROM BS 800 TO BS 840 AND STR 25R IAW BOEING 737-300 SRM 51-40-02-0G FIG 9 AND FIG 10. 2L72 4F RTA16WE 20051107002342005110700234NM 2005 11 7 AWXA200501337 120051009A5322654583311 SHEAR TIE BOEING737 7373S3 1384711NM BS 188 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 MCN - DURING C18 CHECK DISCOVERED FLOOR SHEAR TIE CRACKED AT WL 207 BETWEEN BS 188 AND 196.5, BL 30R. MAINTENANCE REMOVED FLOOR WEB IAW BOEING 737-300 SRM 57-40-02-0G. FABRICATED NEW WEB IAW BOEING 737-300 51-40-05-0G FIG 3 AND DWG 65-45383. INSTALLED FABRICATED REPAIR PARTS AT WL 207 BETWEEN BS 188 AND 196.5, BL 30R IAW BOEING 737-300 SRM 51-40-02-0G. 2L72 4F RTA16WE 20051107002362005110700236NM 2005 11 7 MZZA0500014 120051102A5320146A75018 FLOOR SUPPORT BOEING737 737824 13844BZNM CFMINTCFM56 CFM567B26US NE BS 727G CRACKED A MZZAK NONE O OTHER ININSP/MAINT 1 SW2714240 28952 INSPECTION FOUND A .5 INCH CRACK IN AFT CARGO FLOOR PANEL SUPPORT AT STA 727G, RBL 13.84. AN INTERIM REPAIR WAS ACCOMPLISHED IAW ECRA 5320-01816. A DIP WAS ISSUED TO REINSPECT THE REPAIR EVERY 6 MONTHS AND TO PERFORM A PERMANENT REPAIR WITHIN 2 YEARS. 2L72 4F4 FRTA16WE E00055EN 20051107002382005110700238EU 2005 11 7 05FDEA03611 120051103A5320 TRACK AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 LT CENTER ROLLER TRACK FS 33 TO FS 20 FLOOR BOARD ATTACH HOLES HAVE MINOR CORROSION AND MISSING PROTECTIVE COATING REF N00524. REMOVED AND REPLACED ROLLER TRACK IAW AMM 25-52-21-4. 2L72 4F RTA35EU 20051107002432005110700243NM 2005 11 7 05FDEA03616 120051104A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 MAIN DECK COMPARTMENT, SEAT TRACK EDGE FOUND WORN AT STATION 755, X=-8.5. CARRIED OUT REPAIR IAW SRM 53-70-00 FIG. 1 VOL. I AND SRM 51-33-01 VOL.II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051107002442005110700244NM 2005 11 7 05FDEA03617 120051104A5330 SKIN BOEING727 7272S2F 1384O81NM BS 1050 DENTED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25213FE 22935 EXTERNAL FUSELAGE SKIN DENTED BS 1050 S-17R. CHECKED LIMITS MEASURED DENT .900 WIDE .750 LONG AND .055 DEEP A/Y =13.6 OUT OF LIMITS IAW SRM 53-10-1 FIG 1 SHEET 3 DETAIL II. NDT PERFORMED NO CRACK NOTED, FABRICATED DOUBLER AND CUT OUT DAMAGE. INSTALLED DOUBLER IAW SRM 53-30-2, PAINTED IAW SRM 51-20-151-7, CLASSIFIED AS MAJOR REPAIR. 2L73 4F A3WE 20051107002482005110700248EU 2005 11 7 05FDEA03596 120051101A5754 SKIN AIRBUS310 A310 EU NR 2 SLAT GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25450FE 162 RT WING NR 2 SLAT IB TE HAS DENT AND GOUGE APPROX 4.7" LONG UPPER END (HURRICANE RITA NR 31) REF N00081. COMPLIED WITH EA 6-5750-93420 2L72 4F RTA35EU 20051107002502005110700250SO 2005 11 7 140811052005 120051105A56101159SCB310213 WINDSHIELD GULSTMG1159 GIV 3980115SO COCKPIT CRACKED E N93AO OTHER O OTHER NRNOT REPORTED 1 SO13401QS5181 1408 LEFT WINDSHIELD HAS 3 SMALL CRACKS IN OUTER PANE. 2L72 4F RTA12EA 20051107002532005110700253EU 2005 11 7 05FDEA03601 120051101A5330 SKIN AIRBUS310 A310222 3930315EU FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25450FE 162 UPPER FUSELAGE EXTERIOR SKIN BETWEEN FS 55-56 RT STGR 5 HAS MULTIPLE MINOR SCRATCHED REF N00099. COMPLIED WITH EA 6-5330-94440. 2L72 4F RTA35EU 20051107002562005110700256WP 2005 11 7 05FDEA03604 120051102A5330 SKIN DOUG DC10 DC1010 3022110WP BS 295 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 LWR FUSELAGE EXT STRUCTURE FOUND DEEP DENT ON SKIN (2.25'' BY 1'' DEEP 0.11'') AT STA 295 BY 4 LT SIDE. REFORMED DENT AS PER SRM 53-20-00 FIG 13 VOL 1. INSTALLED FINGER DOUBLER AS PER SRM 53-20-00 FIG 13 VOL 1. 2L73 4F A22WE 20051107002592005110700259EU 2005 11 7 05FDEA03607 120051103A5320 TRACK AIRBUS310 A310203 3930313EU CARGO BAY CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 RT CENTER ROLLER TRACK FROM FS 38.1 TO FS 33 OB SIDE HAS 11 EA HOLES WITH CORROSION ON OR AND AROUND REF N00464. REMOVED AND REPLACED ROLLER TRACK IAW AMM 25-52-21-4. 2L72 4F RTA35EU 20051107002602005110700260EU 2005 11 7 05FDEA03608 120051103A5320 TRACK AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 RT SIDE ROLLER TRACK OB OF CENTER AT FS 37 IB SIDE HAS CORROSION ON AND AROUND FASTENERS REF N00467. REMOVED AND REPLACED ROLLER TRACK IAW SRM 51-40-21. 2L72 4F RTA35EU 20051107002662005110700266EA 2005 11 7 QXEA200501408 120051013A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 707 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09615QX 10065 YYC - FUSELAGE INT, LEFT O/B SEAT RAIL AT FS 707 HAS PITTING CORROSION ON INSIDE SURFACE AND TWO RUSTY SCREWS. MAINTENANCE REPAIRED IAW SRM 51-41-02 AND REO 670-53-00-013 REV A. 2L72 4F RTA21EA 20051107002682005110700268NM 2005 11 7 SWAA053457 120051103A5311BAC14902785 FRAME BOEING737 7373H4 1384600NM BS 328 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME TO SKIN ATTACH ANGLE CRACKED AT BS 328, LBL 45, WL 206. REPAIRED ATTACH ANGLE PER SRM. 2L72 4F RTA16WE 20051107002692005110700269NM 2005 11 7 SWAA053458 120051103A53116546561 FRAME BOEING737 7373H4 1384600NM BS 947.5 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 947.5, BETWEEN STR 10R TO STR 13R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051107002722005110700272NM 2005 11 7 SWAA053461 120051103A53306545776 SKIN BOEING737 7373H4 1384600NM BS 930 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29336SW 23940 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STR 25R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051107002742005110700274NM 2005 11 7 SWAA053463 120051103A53306545775 SKIN BOEING737 7373H4 1384600NM BS 783 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29336SW 23940 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 783, STR 19L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051107002752005110700275NM 2005 11 7 SWAA053464 120051102A2560PH22300L GLOWSTRIP BOEING737 7373H4 1384600NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29356SW 25251 PHOTOLUMINESCENT STRIP COVER MISSING BETWEEN ROW 5 TO ROW 7. REMOVED AND REPLACED STRIP PER MM. 2L72 4F RTA16WE 20051107002772005110700277NM 2005 11 7 SWAA053466 120051103A531165C277091 FRAME BOEING737 7373H4 1384600NM BS 727 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29375SW 26583 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE BLKHD OTBD LOWER CHORD CORRODED AT BS 727, RBL 4.375. REPAIRED CHORD PER SWA EA AND SRM. 2L72 4F RTA16WE 20051107002792005110700279EA 2005 11 7 QXEA200501409 120051015A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 616 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09615QX 10065 YYC - FUSELAGE INT, LEFT O/B SEAT RAIL AT FS 616 HAS PITTING CORROSION ON I/B FACING SURFACE. MAINTENANCE REPAIRED IAW REO 670-53-00-013 REV A. 2L72 4F RTA21EA 20051107002812005110700281NM 2005 11 7 DHL2005742530 120051015A5714 STRUCTURE BOEING727 727225 1384077NM WING BOX CORRODED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15742DH 21290 CORROSION ON CENTER WING BOX APPROX 830 AT RBL 10.0. MECHANICALLY REMOVED CORROSION ON CENTER WING BOX STA 830 RBL 10 IAW B727 SRM 51-10-6. ULTRASONIC INSPECTION OF BLEND AREA IAW ASTM E797-95, HIGH READING .209" LOW READING .128" MATERIAL LOSS .082" FOUND OUT OF LIMITS IAW B727 SRM 57-30-1 FIG 4. CUT OUT AREA OF SKIN FOR REPAIR IAW B727 SRM 57-30-3. FABRICATED REPAIR DOUBLER AND FILLER FROM 7075-T6 .250, 12 X 12 INCHES, ALODINED, PRIMED IAW B727 SRM 57-30-3 FIG 1, INSTALLED REPAIR IAW B727 SRM 57-30-3 FIG 1, 51-10-1 PART 6, AND 51-30-2. 2L73 4F A3WE 20051107002852005110700285NM 2005 11 7 USAA051331 120051103A5754 SKIN BOEING737 7373B7 1384580NM SLAT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 LOWER SKIN T/E CRACKED. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-43-01 FIG 201, DEFECT SIZE: 6 INCH CRACK. 2L72 4F RTA16WE 20051107002952005110700295EA 2005 11 7 QXEA200501413 120051014A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 811 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09615QX 10065 YYC - FUSELAGE INT, RIGHT O/B SEAT RAIL AT FS 811 HAS PITTING CORROSION ON I/B FACING SURFACE. MAINTENANCE REPAIRED IAW REO 670-53-11-013 REV A. 2L72 4F RTA21EA 20051107002982005110700298NM 2005 11 7 AALA20050709 120051028A7160 GUIDE VANE BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE ENGINE LEAKING A AALAA UNSCHED LANDING KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21704X 28163 727197 DFW INFLIGHT T450/28OCT - AFTER TAKEOFF, RIGHT ENGINE OIL TEMPERATURE INDICATED 184 DEGREES FOLLOWED BY HEAVY SMOKE IN COCKPIT AND CABIN. SOURCE CLEARED WHILE ON APPROACH AND OIL TEMPERATURE RETURNED TO NORMAL. FOUND OIL LEAKING FROM VARIABLE GUIDE VANES ON NUMBER TWO ENGINE. REPLACED NUMBER 2 ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA2NM E17NE 20051107003092005110700309NM 2005 11 7 CALA0500384 120051106A5320147A5660041 INTERCOSTAL BOEING737 737724 13844BYNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2723708 28769 INSPECTION FOUND L-2 DOOR INTERCOSTAL CORRODED AT STA 947.5-967, LBL 62. 2L72 4F RTA16WE 20051107003102005110700310NM 2005 11 7 SB05144 120051106A332081781 BALLAST BOEING737 7373B7 1384580NM AFT LT LAVATORY OVERHEATED A USAAFA ACTIVATE FIRE EXT. UNSCHED LANDING BP SMOKE/FUMES/ODORS/SPARKS NO WARNING INDICATION CRCRUISE 1 EA19384US 22957 JAX FLT1067 DURING CRUISE, EN ROUTE FROM CLT TO MIA AT FL340, FLIGHT ATTENDANTS NOTICED SMOKE COMING FROM THE AFT LEFT LAVATORY. FLIGHT ATTENDANT EMPTIED PORTABLE HALON FIRE EXTINGUISHER INTO THE AREA. NO SMOKE ALARM SOUNDED. CREW DECLARED AN EMERGENCY AND DIVERTED TO JAX. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE LIGHT BALLAST FOR THE AFT LEFT LAVATORY MIRROR OVERHEATED AND MELTED. REMOVED AND REPLACED BALLAST ASSEMBLY M148 AND LIGHT ASSEMBLY L261 IN AFT LEFT LAVATORY. OPERATIONAL CHECK GOOD. ALSO, REMOVED AND REPLACED AFT LEFT SMOKE DETECTOR PER MM 26-14-01 AND PORTABLE HALON BOTTLE. 2L72 4F RTA16WE 20051107003132005110700313NM 2005 11 7 USAA051335 120051104A5534 BEAM BOEING737 7374B7 1384702NM VERTICAL FIN CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19779AU 24996 VERTICAL FIN RIGHT AFT LOWER T/E AREA, THE I/B FLANGE OF THE TRAILING EDGE. REPLACED CRACKED BEAM, IAW SRM 51-40-02. DEFECT SIZE: 6 INCHES. 2L72 4F RTA16WE 20051107003142005110700314NM 2005 11 7 USAA051336 120051104A5320 ANGLE BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19779AU 24996 JUST INBOARD OF FWD SERVICE DOOR THRESHOLD. REPLACED WITH IDENTICAL PART, REMOVED DAMAGED Z-ANGLE IAW SRM 51-40-02. DEFECT SIZE: 3 X 7.3 INCH. 2L72 4F RTA16WE 20051107003152005110700315NM 2005 11 7 USAA051326 120051103A575465C26602218 SKIN BOEING737 7373B7 1384580NM L/E SLAT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 IN LOWER SKIN OF NR 5 SLAT AT RIVET, ADJACENT TO SLAT ACTUATOR ATTACH. A 30.25 X 3.75 INCH REPAIR DOUBLER ON LOWER SKIN AT CTR OF SLAT ADJ TO ACTUATOR ATTACH IAW SRM 57-43-01. DEFECT SIZE: .250 INCH LONG CRACK AT RIVET. 2L72 4F RTA16WE 20051107003162005110700316NM 2005 11 7 USAA051327 120051103A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FLOOR SKIN, STA 665, LBL 30. REMOVED DAMAGE, INSTALL FILLER DOUBLER & STIFFENER IAW TYPE REPAIR 53-60-04. DEFECT SIZE: .500 INCH CRACK. 2L72 4F RTA16WE 20051107003212005110700321CE 2005 11 7 DXTA200501047 120051019A3222 STRUT CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL NLG DIRTY E DXTAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 GL07982QS 7500182 DURING FLIGHT GEAR RETRACTS HEARD AND FELT BUMP IN THE NIGHT FOUR (4) TIMES DURING FLIGHT. MEASURED EXTENSION OF NOSE STRUT, MEASURED 9.80 INCHES DISASSEMBLED AND CLEANED LOWER BARREL ASSEMBLY. RESEALED AND REASSEMBLED. MEASUREMENT NOW 9.75 INCHES IAW MM. SERVICED STRUT. DOWNJACKED AND GOOD. WORK C/W IAW MM CH 32-20-02, C/W GEAR CHECKLIST, NO FURTHER DEFECTS NOTED. 2L72 4J4 FRTT00007WITE6CH 20051107003262005110700326NM 2005 11 7 SWAA053485 120051102A53306545774 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29694SW 23061 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 18R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051107003432005110700343NM 2005 11 7 SWAA053507 120051104A55536546874 ANGLE BOEING737 7373H4 1384600NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED D-CHECK, FOUND VERTICAL STAB FITTING RIGHT AFT DRAG ANGLE CORRODED. REMOVED AND REPLACED DRAG ANGLE PER SRM. 2L72 4F RTA16WE 20051107003442005110700344NM 2005 11 7 SWAA053494 120051106A53206551698 STRINGER SPLICE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29335SW 23939 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER SPLICE CHANNEL CRACKED AT BS 359, STR 15L. REMOVED AND REPLACED SPLICE CHANNEL PER SRM. 2L72 4F RTA16WE 20051107003502005110700350NM 2005 11 7 SWAA053500 120051103A335007912 COVER BOEING737 7377H4 1384404NM CABIN OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29452WN 29846 EEPLS TRACK COVER OUT OF POSITION AT FWD END. SECURED COVER PER MM. 2L72 4F RTA16WE 20051107003522005110700352NM 2005 11 7 SWAA053502 120051104A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29474WN 33861 EEPLS TRACK LOOSE AT FWD END. SECURED EEPLS PER MM. 2L72 4F RTA16WE 20051107003562005110700356NM 2005 11 7 SWAA053506 120051104A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051107003612005110700361NM 2005 11 7 SWAA053488 120051104A53116546532 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051107003642005110700364NM 2005 11 7 SWAA053491 120051104A278065C268692 CONTROL VALVE BOEING737 7373H4 1384600NM L/E SLAT FAILED A SWAAD RETURN TO BLOCK JF WARNING INDICATION FLT CONT AFFECTED TOTAKEOFF 1 SW29319SW 23340 AIR TURNBACK, L/E DEVICES DID NOT RETRACT AND L/E FLAPS TRANSIT LIGHT REMAINED ILLUMINATED. REMOVED AND REPLACED AUTO SLAT CONTROL VALVE PER MM. 2L72 4F RTA16WE 20051107003662005110700366NM 2005 11 7 SWAA053511 120051106A5311963820 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29644SW 28329 DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD SIDE CHORDS CRACKED AT WL 207. REMOVED AND REPLACED SIDE CHORDS PER SWA ACO. 2L72 4F RTA16WE 20051107003672005110700367 2005 11 7 SWAA053512 420051103A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29716SW 27850 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051108000142005110800014NM 2005 11 8 EVAS094004 120051019A5330 ACCESS PANEL BOEING747 747400 NM FUSELAGE MISSING W QOCFA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 WP0316465 26062 DURING AIRCRAFT CLIMBING, CAPTAIN FELT AIRFRAME VIBRATION. CAPTAIN DECIDED TO AIR TURNBACK. ON GROUND CHECK , FOUND NR 3 PACK ACCESS PANEL MISSING (192AR). REPLACED 192AR/191AL/191BL PANEL, THEN AIRCRAFT CONDITION BACK TO NORMAL. 2L74 4F RTA20WE 20051108000212005110800021NM 2005 11 8 05FDEA03620 120051104A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 DURING HFEC INSPECTION, FOUND CRACK INDICATION AT LEFT HAND WING, END OF STRINGER 41. REPAIR CARRIED OUT IAW SRM 57-20- 00 FIG. 10 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051108000242005110800024NM 2005 11 8 200516 120051104A2910AS3209153 O-RING DHAV DHC8 DHC8103 1386005NM HYD SYSTEM LEAKING A KPVAL ABORTED APPROACH KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 WP13808WP 026 LOSS OF NR 1 HYD FLUID ON APPROACH. MX FOUND BAD O-RING ON SPU NR 1 OUTLET UNION. REPLACED O-RING IAW DHC -8 MM CH 29-00-00 PG 401. LEAK CHECK GOOD IAW DHC -8 MM CH 29-00-00 PG 501. 2H72 4T RTA13NM 20051108000432005110800043NE 2005 11 8 REXA200500134 220051102A72306040T92P02 GUIDE VANE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE COMPRESSOR CASE BROKEN A REXAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 SO258751D6622 7751 GEE873650 THE AIRCRAFT DEPARTED, ON A FERRY FLIGHT TO THE MAINTENANCE BASE, DUE TO A MISSING RT THRUST REVERSER BLOCKER DOOR. AT FL230 AND 80 MILES OUT, THE RT ENGINE FLAMED OUT. THE FLIGHT CREW EXECUTED THE SINGLE ENGINE OPERATION PORTION OF THE QRH AND DECLARED AN EMERGENCY. AN OTHERWISE UNEVENTFUL APPROACH AND LANDING WAS MADE. MAINTENANCE INSPECTED THE ENGINE AND FOUND SEVERAL COMPRESSOR STAGE 2 VANES FAILED. BORESCOPE INSPECTION REVEALED FURTHER INTERNAL ENGINE DAMAGE. THE ENGINE WAS REPLACED AND THE AIRCRAFT RELEASED FOR FLIGHT. 2L72 4F4 FRTA21EA E15NE 20051108000442005110800044NM 2005 11 8 QXEA200501508 120051105A5270 PROXIMITY SENSOR BOMBDRDHC8 DHC8402 1390042NM SERVICE DOOR CONTAMINATED A QXEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM09414QX 4061 GTF FLIGHT 2321: AFT SERVICE DOOR WARNING LIGHT INTERMITTENT AFTER DEPARTURE. MAINTENANCE CLEANED ICE AND DEBRIS FROM DOOR PROX SENSOR. CYCLED DOOR SEVERAL TIMES. OPS CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051108000452005110800045EA 2005 11 8 REXA200500135 120051105A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A REXAO OTHER J WARNING INDICATION APAPPROACH 1 SO258969A 7969 FLAPS FAILED AT ZERO ON APPROACH. QRH FOLLOWED ZERO FLAP LANDING WITHOUT INCIDENT. FLAPS RESET PER AD 98-20-01 PLACED ON 72 HOUR WATCH. 2L72 4F RTA21EA 20051108000642005110800064WP 2005 11 8 IXXA05SMN247S 120051013A5740 FITTING DOUG DC8 DC871F 302199DWP FS 74.000 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING ROUTINE C-CHECK INSPECTION, LEFT WING NR 2 MAIN TANK FITTING CRACKED, FS 74.000 S.51 (FWD INTERNAL PART). REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D. CLEANED AND APPLIED POLYURETHANE TOP COATING YELLOW IAW DC8 SRM 51-1-12 PAGES 7-25. INSTALLED NEW FITTING WITH FASTENERS (HI-LOKS) AND TORQUED NUTS IAW DC8 SRM 51-1-20D, DC8 SRM 51-3-1. 2L74 4F RT4A25 20051108000652005110800065NM 2005 11 8 QXEA200501509 120051104A2730 ELEVATOR BOMBDRDHC8 DHC8402 1390042NM MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM09408QX 4050 PDX FLIGHT 2362: PUSHER SYSTEM FAIL CAUTION LIGHT ILLUMINATES AFTER LANDING. AFTER CONDUCTING AN ABNORMAL CHECKLIST, CAUTION LIGHT REMAINS ILLUMINATED. MAINTENANCE PERFORMED OPS CHECK IAW AMM TASK 27-33-00-720-801. OPS TEST GOOD. REF FIM FAULT CONFIRMATION IAW TASK 27-33-00-810-829. NO FAULT FOUND. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051108000762005110800076NE 2005 11 8 WRLA2005146 220051104A7200 ENGINE DOUG DC10 DC1030F 3023504WP GE CF6 CF650C2 30018NE NR 1 OVERHEATED A WRLAEA ENGINE SHUTDOWN UNSCHED LANDING MJ OVER TEMP WARNING INDICATION DEDESCENT 1 SO11303 46917 BRU-DAY DIVERSION TO YYZ BECAUSE OF NR 1 ENGINE HIGH EGT AND HIGH FUEL FLOW. BEGINNING/DURING DESCENT INTO YYZ THE ENGINE FIRE WARNING BEGIN FLICKERING LIGHT AND ENGINE WAS SHUTDOWN PER ENGINE FIRE/FAILURE CHECKLIST. FLICKERING LIGHT WAS IN FIRE HANDLE AND START LEVER NR 1. ABOVE 92 PERCENT N1 THE EGT WAS HIGH AND THE FUEL FLOW WOULD INCREASE IN CRUISE FLIGHT. FOUND 14TH STAGE BLEED AIR MANIFOLD DAMAGED, R/R SAME AND R/R LEFT & RIGHT THRUST REVERSERS PER DC10 MM 71-10 OPS CHECK ALL NORMAL. 2L73 4F4 FRTA22WE E23EA 20051108000852005110800085EA 2005 11 8 QXEA200501399 120051019A7830 FRAME CNDAIRCL600 CL6002C10 1390015EA THRUST REVERSER DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09615QX 10065 YYC - RIGHT ENGINE LOWER FAN COWL HAS FRETTING DAMAGE ON FRAME JUST AFT OF CENTER LATCH APPROX NACELLE STA ESTA 155.00. MAINTENANCE REPAIRED IAW QX EA R-78-68, REO 370-78-34-460 STEPS 4 AND 5. 2L72 4F RTA21EA 20051108000872005110800087NE 2005 11 8 05134 220051102A72306040T92P02 GUIDE VANE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE ENGINE BROKEN A REXAO OTHER X ENGINE FLAMEOUT CRCRUISE 1 SO258751D6622 UNK 7751 GEE873650 FLIGHT LEFT SBN ON A FERRY FLIGHT TO THE TYS MAINTENANCE BASE DUE TO A MISSING RIGHT HAND ENGINE THRUST REVERSER BLOCKER DOOR. AT FL230 AND 80 MILES OUT OF KNOXVILLE, THE RIGHT HAND ENGINE FLAMED OUT. THE FLIGHT CREW EXECUTED THE SINGLE ENGINE OPERATION QRH AND DECLARED AN EMERGENCY WITH ATC. AN OTHERWISE UNEVENTFUL APPROACH AND LANDING WAS MADE AT KTYS. 2L72 4F4 FRTA21EA E15NE 20051108000882005110800088WP 2005 11 8 GTIA050231 120050724A5320 PAN DOUG DC9 DC983 3022083WP CARGO DOORWAY CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FORWARD LOWER CARGO COMPARTMENT, LOWER DOOR JAMB PAN HAVE CORROSION. REMOVED CORROSION. REMOVED CORROSION AT FORWARD LOWER CARGO COMPARTMENT LOWER DOOR JAMB PAN. FOUND OUT OF LIMITS. CUT OUT LOWER DOOR JAMB PAN. FABRICATED REPAIR ANGLES. TREATED, PRIMED AND INSTALLED REPAIR ANGLES. (M) 2L72 4F RTA6WE 20051108000892005110800089WP 2005 11 8 GTIA050230 120050724A5330 SKIN DOUG DC9 DC983 3022083WP BS 540 GOUGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FOUND MID PIT, SKIN GOUGED/DENTED AT STATION 540 BETWEEN LONGERONS 26L AND 27L. DAMAGED AREA FOUND, OUT OF LIMITS AT STATION 540 BETWEEN 26L AND 27L. CUT OUT DAMAGED AREA. FABRICATED FINGER DOUBLER, TREATED, PRIMED AND INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20051108000902005110800090EA 2005 11 8 ASOA05857 120051010A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FS 718 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27836AS 7263 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT FS 718 FRAME, AT STRINGER 10-12, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REPAIR THE LEFT AND RIGHT FS 718 FRAME, AT STRINGER 10-12, IAW ASA EO 600-53-0067A. (M) 2L72 4F RTA21EA 20051108000912005110800091EA 2005 11 8 ASOA05810 120050925A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA BS 640 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27838AS 7276 DURING AN A-CHECK IN BTR, THE RIGHT SIDE 640 FRAME DOUBLER WAS FOUND TO POSSIBLY BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT SIDE FS 640 FRAME DOUBLER IAW CRJ200 SRM 51-40-00. (M) 2L72 4F RTA21EA 20051108000922005110800092EA 2005 11 8 ASOA05883 120051018A2420755469E IDG CNDAIRCL600 CL6002B19 1900309EA NR 2 MALFUNCTIONED A ASOAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27876AS 7576 FLT 4568 - DURING CRUISE FROM YOW-ATL, THE CREW RECEIVED A NR 2 IDG CAUTION MESSAGE, ACCOMPANIED BY AN AMBER IDG BOX ON THE ELECTRIC SYNOPTIC PAGE. THE CREW COMPLIED WITH THE QRH AND THE NR 2 IDG DISCONNECT FAILED TO FUNCTION. AN APU OIL TEMP LIGHT ILLUMINATED, THE QRH WAS COMPLIED WITH AND APU OPERATION WAS CONSIDERED ESSENTIAL BECAUSE NR 2 IDG WAS ALREADY OFFLINE. THE AIRCRAFT DIVERTED TO ROA, WHERE IT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE NR 2 IDG AND THE APU OIL COOLER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051108000952005110800095EA 2005 11 8 ASOA05770 120050918A33500L3071BPEGPL LAMP CNDAIRCL600 CL6002B19 1900309EA GALLEY INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27673BR 7599 DURING A GROUND INSPECTION IN SHV, THE EMERGENCY EXIT LIGHT NEAR THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMPS IN THE EMERGENCY EXIT LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051108000962005110800096NE 2005 11 8 ASOA05804 220050915A7200 ENGINE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE VIBRATION A ASOAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 SO11719EV 10099 FLT 4469 - DURING CRUISE FROM SLC-SJC, AT APPROXIMATELY 32,000 FEET, THE VIBRATION METER WENT INTO THE YELLOW AT 1.9. THE QRH WAS COMPLIED WITH AND THE ENGINE WAS BROUGHT BACK INTO THE GREEN. THE TOWER DECLARED AN EMERGENCY, AND THE AIRCRAFT RETURNED TO SLC, LANDING SAFELY. MAINTENANCE PERFORMED ENGINE RUNS THROUGH ALL POWER SETTINGS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F4 FRTA21EA EOOO63EN 20051108000972005110800097EA 2005 11 8 ASOA05806 120050925A1100S1859 PLACARD CNDAIRCL600 CL6002B19 1900309EA CABIN WORN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27835AS 7258 DURING A C-CHECK IN MCN, THE EMERGENCY ESCAPE PLACARD ON THE PILOT`S ESCAPE HATCH WAS FOUND TO BE WORN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PLACARD ON THE PILOT`S ESCAPE HATCH. (M) 2L72 4F RTA21EA 20051108000982005110800098EU 2005 11 8 ASOA05808 120050925A33503011052 COVER AEROSPATR72 ATR72 EU EMERGENCY LIGHT BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11641AS 387 FLT 4121 - DURING HANGAR MAINTENANCE IN ATL, THE LEFT EXIT LIGHT COVER WAS FOUND TO BE BROKEN. MAINTENANCE REPLACED THE LEFT EXIT LIGHT COVER. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20051108001012005110800101EA 2005 11 8 ASOA05891 120051021A33974871907191 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27672BR 7594 DURING A GROUND INSPECTION IN ROA, THE CABIN FLOOR EMERGENCY LIGHTS, AT ROWS 7 AND 8, WERE FOUND TO BE INOPERATIVE. MAINTENANCE RESECURED THE FLOOR EMERGENCY LIGHT CONNECTORS, AT ROWS 7 AND 8. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051108001022005110800102EA 2005 11 8 ASOA05867 120051013A5210601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27868AS 7474 DURING A GROUND INSPECTION IN CVG, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND TO BE BROKEN AT THE ATTACH POINT. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051108001052005110800105WP 2005 11 8 GTIA050221 120050718A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP BS 522-1178 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 RIGHT CABIN FLOOR WEB RBL 44 TO RBL 45 HAS CORROSION AT STATION 522 THROUGH 617, STATION 636 THROUGH 646, STATION 674 THROUGH 680, STATION 1068 THROUGH 1076, STATION 1105 THRU 1110 AND STATION 1178 THRU 1135. FLOOR WEB AT STATION RIGHT 560-579 AND FLOOR WEB STATION 598-617 WERE FOUND OUT OF LIMITS. FABRICATED DOUBLERS AND FILLERS FOR STATION 560-579, STATION 1068-1076 AND STATION 636-680. TREATED, PRIMED AND INSTALLED REPAIRED PARTS. REMOVED CORROSION AT RBL 44-54, STATION 1105-1110, STATION 1178-1185 AND 1068-1076 AND FOUND WERE OUT OF LIMITS. FABRICATED REPAIR DOUBLERS AND FILLERS ON DAMAGED AREAS. TREATED, PRIMED AND INSTALLED REPAIRED PARTS. (M) 2L72 4F RTA6WE 20051108001062005110800106EA 2005 11 8 ASOA05853 120050904A5210601R3170767 STEP CNDAIRCL600 CL6002C10 1390015EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27717EV 10088 FLT 4116 - DURING A HANGAR INSPECTION IN MCN, THE PASSENGER DOOR LOWER STEP, AT THE ATTACHED STAY ROD BRACKET, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR LOWER STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051108001072005110800107 2005 11 8 C7WA200500117 420050809A34526222224001 TRANSPONDER BOEING727 7272M7 138407SNM E/E BAY INOPERATIVE A C7WAO OTHER O OTHER NRNOT REPORTED 1 SO17721RW 21200 FLIGHT RETURN, NR 2 TRANSPONDER FAILED DURING FLIGHT. RETURNED TO KDAY PER ATC REQUEST. REMOVED AND REPLACED TRANSPONDER OPERATIONAL CHECKS GOOD PER B727 MM 34-43-10. (M) 2L73 4F A3WE 20051108001082005110800108WP 2005 11 8 GTIA050200 120050603A5310 STRUCTURE DOUG DC9 DC982 3022082WP LAVATORY CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23830NK 49932 FOUND FORWARD LAV MODULE INBOARD BOTTOM STRUCTURE CORRODED. REMOVED FORWARD LAV INBOARD BOTTOM STRUCTURE FOUND TO BE OUT OF LIMITS. FABRICATED NEW RT BOTTOM STRUCTURE MEMBER. PERFORMED DYE PENETRANT INSPECTION, TREATED, PRIMED AND INSTALLED BOTTOM STRUCTURE. (M) 2L72 4F A6WE 20051108001102005110800110WP 2005 11 8 GTIA050242 120050826A5511 SPAR DOUG DC9 DC983 3022083WP HORIZONTAL STAB DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23834NK 49847 LEFT HORIZ STAB AFT SPAR CHANNEL DAMAGED STATION XHS 85. REMOVED CHANNEL ON LEFT HORIZONTAL STAB ON AFT SPAR. FABRICATED CHANNEL. TREATED, PRIMED AND INSTALLED REPAIR CHANNEL. (M) 2L72 4F RTA6WE 20051108001112005110800111WP 2005 11 8 GTIA050240 120050813A5320 FLOOR SUPPORT DOUG DC9 DC983 3022083WP BS 1095-1113 CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 MAIN CABIN FLOOR SUPPORT BETWEEN STATION 1095 AND 1113 CRACKED. ACCESSIBLE FROM AFT CARGO COMPT CEILING SECTION. REMOVED AND REPLACED FLOOR SUPPORT BETWEEN STATION 1095 AND 1113. (M) 2L72 4F RTA6WE 20051108001122005110800112EU 2005 11 8 ASOA05880 120051017A3350 LIGHT AEROSPATR72 ATR72 EU CABIN UNKNOWN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27634AS 370 FLT 4103 - DURING A GROUND INSPECTION IN ATL, THE ARMED SWITCH HAD TO BE TURNED ON 3 TIMES FOR THE EMERGENCY LIGHTS TO REMAIN OFF. MAINTENANCE INSPECTED THE EMERGENCY LIGHT SYSTEM WITH NO DEFECTS FOUND. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20051108001132005110800113EU 2005 11 8 ASOA05826 120050830A5313 STRINGER AEROSPATR72 ATR72 EU FR 38-39 CORRODED A ASOAO OTHER O OTHER NRNOT REPORTED 1 SO27637AS 383 DURING A C-CHECK IN YUL, THE STRINGER 21L BETWEEN FRAME 38-39 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE STRINGER 21L BETWEEN FRAME 38-39 IAW ASA EO 72-53-0166A. (M) 2H72 4T RT 20051108001142005110800114EU 2005 11 8 ASOA05822 120050830A5311 FRAME AEROSPATR72 ATR72212 8680945EU FR 37 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11637AS 383 DURING A C-CHECK IN YUL, THE FS 37 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED FS 37 AT STRINGER 14R IAW ASA EO 72-53-0166A. (M) 2H72 4T RTA53EU 20051108001152005110800115EA 2005 11 8 ASOA05818 120050926A5347 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA BS 364 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27835AS 7258 DURING A C-CHECK IN MCN, THE RIGHT INBOARD SEAT TRACK, AT FS 364, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACE THE RIGHT INBOARD SEAT TRACK, AT FS 364. (M) 2L72 4F RTA21EA 20051108001162005110800116EA 2005 11 8 ASOA05817 120050926A5347 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA BS 559 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11835AS 7258 DURING A C-CHECK IN MCN, THE LEFT UPPER SEAT TRACK, AT FS 559 PLUS 64, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACED THE LEFT UPPER SEAT TRACK, AT FS 559 PLUS 64. (M) 2L72 4F RTA21EA 20051108001172005110800117NE 2005 11 8 GTIA050222 220050731A7200 ENGINE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE NR 2 FAILED A GTIAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 GL23802NK 53168 1500 FT ON CLIMB-OUT LOUD BANG, NR 2 ENGINE FAILURE, ROLLBACK. ENGINE FAILURE CHECKLIST COMPLETED, OVERWEIGHT LANDING PERFORMED. REMOVED AND REPLACED NR 2 ENGINE, OPS AND LEAK CHECK GOOD. (M) 2L72 4F4 FRTA6WE E9NE 20051108001182005110800118WP 2005 11 8 GTIA050199 120050603A5310 DOOR FRAME DOUG DC9 DC982 3022082WP CARGO DOORWAY CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23830NK 49932 FTW - FOUND AFT CARGO DOOR FUSELAGE JAMB BEAM STATION 1155-1211, L25R CORRODED. REMOVED PANELS TO FOM. AFT CARGO DOOR JAMB BEAM IS OUT OF LIMITS. FABRICATED DOUBLER AND SPACERS. TREATED AND PRIMED AND INSTALLED REPAIRED DOUBLERS. (M) 2L72 4F A6WE 20051108001202005110800120SO 2005 11 8 SIMA200526904 120050923A532014525480003 SILL EMB 135 EMB135KL 3260302SO CARGO DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21820AE 145576 THE CARGO DOOR CUTOUT LOWER SILL WAS FOUND CORRODED. REMOVED EXISTING LOWER SILL AND INSTALLED SERVICEABLE SILL. REPAIR DONE IAW EMB 145 SRM, SRM EMB-145/1142 REV 30) CHAPTERS 51-40-2, 51-20-03 AND 51-40-06. (M) 2L72 4F RTT00011AT 20051108001242005110800124EA 2005 11 8 ASOA05812 120050926A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11904EV 7628 DURING A GROUND INSPECTION IN MGM, THE EMERGENCY CEILING LIGHT, NEAR THE LAVATORY DOOR, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY CEILING LIGHT NEAR THE LAVATORY DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051108001252005110800125EU 2005 11 8 ASOA05890 120051021A5311 FRAME AEROSPATR72 ATR72 EU FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27642AS 395 DURING HANGAR MAINTENANCE IN MCN, THE RIGHT CENTER HALF FRAME, INSIDE THE WHEEL WELL, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT CENTER HALF FRAME, INSIDE THE WHEEL WELL, IAW SRM 51-24-01. (M) 2H72 4T RT 20051108001282005110800128NM 2005 11 8 C7WA200500118 120050916A52702314143 SWITCH BOEING727 727281 138408NNM MLG DOOR OUT OF ADJUST A C7WAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 SO17902PG 20725 AIR RETURN, RIGHT MAIN LANDING GEAR DOOR ANNUNCIATOR LIGHT CAME ON WHEN GEAR HANDLE IS PUT IN OFF POSITION. ADJUSTED RIGHT MAIN LANDING GEAR DOOR SWITCH. OPERATIONAL CHECKS GOOD PER B727 MM 32-62-11. (M) 2L73 4F A3WE 20051108001292005110800129CE 2005 11 8 GUU2005F00048 120050912A55231016200111 BRACKET BEECH 1900 1900D 1154162CE LT ELEVATOR CORRODED A GUUAK NONE O OTHER ININSP/MAINT 1 SO2981556 UE239 AT SCHEDULED MAINTENANCE, THE LEFT ELEVATOR, OUTBOARD HINGE BRACKET WAS DETERMINED TO HAVE EXFOLIATION CORROSION. REPLACED THE LEFT ELEVATOR OUTBOARD HINGE BRACKET. (M) 2L72 4T RTA24CE 20051108001302005110800130EA 2005 11 8 ASOA05852 120050903A5210601R3170767 STEP CNDAIRCL600 CL6002C10 1390015EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27750EV 10161 DURING A HANGAR INSPECTION IN MCN, THE PASSENGER DOOR LOWER STEP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR LOWER STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051108001312005110800131WP 2005 11 8 GTIA050213 120050713A5220 RELEASE CABLE DOUG DC9 DC983 3022083WP TAILCONE FAILED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 AFT TAIL CONE RELEASE SYSTEM CHECK FAILED TO RELEASE WHEN AFT EMERGENCY HANDLE OPERATED TO OPEN POSITION. REMOVED TAIL CONE EVAC SLIDE TO FOM AND INSTALLED TAIL CONE IAW MD80 MM 53-53-00. (M) 2L72 4F RTA6WE 20051108001322005110800132WP 2005 11 8 GTIA050211 120050630A5347 SEAT TRACK DOUG DC9 DC983 3022083WP BS 1117-1174 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23815NK 49415 FOUND CABIN SEAT TRACK CORRODED, LBL 24 FROM STATION 1117-1174. SEAT TRACK FOUND TO BE OUT OF LIMITS. CUT OUT SEAT TRACKS FOR REPAIR. TREATED AND PRIMED, SEAT TRACKS INSTALLED. (M) 2L72 4F RTA6WE 20051108001392005110800139WP 2005 11 8 GTIA050205 120050628A5330 SKIN DOUG DC9 DC983 3022083WP BS 1291 DAMAGED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23815NK 49415 FOUND FUSELAGE STATION 1291 LONGERON 20R-21R, FLUSH REPAIR, SIZE 5 INCH BY 4 INCH NOT PER SRM. REMOVED PANELS FOR ACCESS TO FOM, CUT OUT 12.75 BY 10.75 AROUND OLD REPAIR. FABRICATED REPAIR DOUBLER, FILLER TREATED, PRIMED AND INSTALLED REPAIRED PARTS. INSTALLED ACCESS PANEL. (M) 2L72 4F RTA6WE 20051108001412005110800141NM 2005 11 8 C7WA200500110 120050723A261369266652 OVERHEAT LOOP BOEING727 727222 1384073NM ENGINE FIREWALL GROUNDED A C7WAO OTHER O OTHER NRNOT REPORTED 1 SO177640U 19913 LOWER AFT BODY OVERHEAT LIGHT ON. COMPLETED EMERGENCY PROCEDURE, FOUND IT TO BE NR 2 ENGINE. INSPECTED NUMBER 2 ENGINE FOUND LOOP TOUCHING BLEED AIR DUCT. REPOSITIONED LOOP OPERATIONAL CHECKS GOOD PER MM 26-14-0. (M) 2L73 4F A3WE 20051107003002005110700300EA 2005 11 7 QXEA200501412 120051014A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 843 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09615QX 10065 YYC - FUSELAGE INT, RIGHT O/B SEAT RAIL AT FS 843 HAS PITTING CORROSION ON I/B FACING SURFACE. MAINTENANCE REPAIRED IAW REO 670-53-00-013 REV A. 2L72 4F RTA21EA 20051107003012005110700301NM 2005 11 7 SWAA053468 120051103A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHTSCRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29410WN 27897 DURING SCHEDULED HC2 CHECK, FOUND EEPLS TRACK COVER CRACKED AT ROW 12 ABC. REMOVED AND REPLACED COVER PER MM. 2L72 4F RTA16WE 20051107003112005110700311NM 2005 11 7 USAA051333 120051104A5320 TIE CLIP BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FUSELAGE STATION 277 STRINGER 10R. REMOVED AND REPLACED STRINGER TIE CLIP IAW SRM 51-10-02. DEFECT SIZE: .075 INCH. 2L72 4F RTA16WE 20051107003182005110700318NM 2005 11 7 USAA051329 120051103A532069353521 TIE CLIP BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19779AU 24996 TIE CLIP S25L STA 400 CRACKED. REPLACED WITH IDENTICAL PART, REMOVED & REPLACED TIE CLIP IAW SRM 51-40. DEFECT SIZE: .1875 INCH CRACK. 2L72 4F RTA16WE 20051107003192005110700319SO 2005 11 7 138611032005 120051103A56101159SCB310214 WINDSHIELD GULSTMG1159 GIV 3980115SO COCKPIT CRACKED E N93AK NONE O OTHER UKUNKNOWN 1 SO13486QS5527 1386 RIGHT FORWARD WINDSHIELD HAS SPYDER WEB CRACKS IN OUTER PLY. 2L72 4F RTA12EA 20051107003272005110700327NM 2005 11 7 SWAA053484 120051102A53306545774 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29694SW 23061 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 24R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051107003282005110700328NM 2005 11 7 SWAA053483 120051102A53306545775 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29694SW 23061 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 835, STR 23L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051107003312005110700331NM 2005 11 7 SWAA053480 120051102A53306545774 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29694SW 23061 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 23L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051107003342005110700334NM 2005 11 7 SWAA053477 120051102A53306545774 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29694SW 23061 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 21L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051107003352005110700335NM 2005 11 7 SWAA053476 120051102A53306545774 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29694SW 23061 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 19L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051107003372005110700337NM 2005 11 7 SWAA053474 120051103A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 578, STR 12R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051107003452005110700345NM 2005 11 7 SWAA053495 120051106A575465C26686 SKIN BOEING737 7373H4 1384600NM L/E SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29335SW 23939 DURING SCHEDULED 1/4D CHECK, FOUND NR 6 L/E SLAT SKIN CRACKED AT ACTUATOR INBOARD STOP FITTING. REPAIRED SLAT PER SRM. 2L72 4F RTA16WE 20051107003462005110700346NM 2005 11 7 SWAA053496 120051106A575465C26686 SKIN BOEING737 7373H4 1384600NM L/E SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29335SW 23939 DURING SCHEDULED 1/4D CHECK, FOUND NR 5 L/E SLAT SKIN CRACKED INBOARD OF ACTUATOR. REPAIRED SLAT PER SRM. 2L72 4F RTA16WE 20051107003472005110700347 2005 11 7 SWAA053497 420051103A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29336SW 23940 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051107003652005110700365NM 2005 11 7 SWAA053492 120051105A79331122514 BULB BOEING737 7373H4 1384600NM NR 2 ENGINE FAULTY A SWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW29322SW 23343 DIVERSION/DECLARED EMERGENCY. NR 2 ENGINE OIL TEMP EXCEEDED RED LINE. REMOVED AND REPLACED NR 2 ENGINE OIL TEMP BULB PER MM. 2L72 4F RTA16WE 20051107003682005110700368EA 2005 11 7 SWIA200515793 120050619A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07920SW 7660 FLOOR SUPPORT AT FS 621 REAR CARGO BAY LEFT FOUND TO BE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW REO 601R-53-61-114. 2L72 4F RTA21EA 20051107003702005110700370EA 2005 11 7 SWIA200515795 120050619A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07920SW 7660 FS 280 AT RBL 9 I/B AND O/B ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. ANGLES REPAIRED IAW REO 601R-53-11-136 AND SRM 51-42-06 AND 51-42-21. 2L72 4F RTA21EA 20051107003722005110700372EA 2005 11 7 SWIA200515797 120050704A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07923SW 7664 FWD AVIONICS BAY FS 280 RT FRAME CRACKED BL- +8 AND +11 INBOARD OUTBOARD. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED TWO NEW BRACKETS IAW REO 601R 53-11-136. 2L72 4F RTA21EA 20051107003742005110700374EA 2005 11 7 SWIA200515799 120050704A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07923SW 7664 MAIN CABIN FS 484.00 BL36R WL 72 ANGLE CLIP CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR ANGLE IAW RO 601R 53-41-059. 2L72 4F RTA21EA 20051107003772005110700377EA 2005 11 7 SWIA200515802 120051031A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA CABIN DAMAGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07457SW 7773 CABIN DOOR EMERGENY EXIT SIGN WILL NOT ILLUMINATE. REPAIRED WIRES AT SIGN. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051108000392005110800039WP 2005 11 8 UPS05845724 120051020A53403779658502 FITTING DOUG DC8 DC873F 302199FWP BS 860 L10R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE:C1 LONGERON END FITTING CRACKED STA 860 L10R. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20051108000402005110800040WP 2005 11 8 UPS05845725 120051019A5313 LONGERON DOUG DC8 DC873F 302199FWP BS 8-25 L19R CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE:C1 STA 8-25 LONGERON 19R IS CORRODED (EXFOLIATING). REMOVED LONGERON END FITTING, REMOVED CORROSION, AND REINSTALLED LONG END FITTING IAW SAA SK 813-822730. 2L74 4F RT4A25 20051108000412005110800041WP 2005 11 8 UPS05845726 120051019A5310 FINGER DOUBLER DOUG DC8 DC873F 302199FWP BS 960-940 RBL65CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE:C1 MAIN CABIN SUB FLOOR FINGER DOUBLER CORRODED AND HAS SHEARED HEAD FASTENERS AT STA 960 TO 940 RBL 65. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FINGER DOUBLER IAW DC-8 SRM 53-07-03 FIG 4 AND 51-1-21. 2L74 4F RT4A25 20051108000932005110800093EA 2005 11 8 ASOA05856 120051010A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27836AS 7263 DURING A C-CHECK IN MCN, THE FS 280 AND LBL 9 FLOOR SUPPORT BEAM, ON THE INBOARD RIVET OF FLOOR SUPPORT LEG, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REPAIR THE FS 280 AND LBL 9 FLOOR SUPPORT BEAM, ON THE INBOARD RIVET OF THE FLOOR SUPPORT LEG, IAW BOMBARDIER REO 601R-53-11-926. (M) 2L72 4F RTA21EA 20051108001002005110800100WP 2005 11 8 GTIA050201 120051024A5321 FLOOR PANEL DOUG DC9 DC982 3022082WP BS 450-200 CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23830NK 49932 FTW - FOUND FORWARD ENTRY AREA FLOOR WEB STATION 450-200, LBL 12 INCHES IS CORRODED. REMOVED FORWARD AIRSTAIR SHROUD TO FOM. REMOVED CORROSION AND FOUND MATERIAL IS OUT OF LIMITS. CUT OUT DAMAGE AREA (2 INCHES BY 2 INCHES). FABRICATED REPAIR DOUBLER. TREATED AND PRIMED. INSTALLED REPAIR DOUBLER AND REINSTALLED AIRSTAIR SHROUD. (M) 2L72 4F A6WE 20051108001192005110800119WP 2005 11 8 GTIA050220 120050727A5320 WEB DOUG DC9 DC983 3022083WP BS 408-427 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FOUND MAIN CABIN, RIGHT SIDE STATION 408 TO STATION 427 WEB MEMBRANE HAVE CORROSION ON SURFACE. REMOVED CORROSION FOUND ITS OUT OF LIMITS. CUT OUT CORRODED AREA BETWEEN STATION 389R-427R AT WEB MEMBRANE. FABRICATED TWO REPAIR DOUBLERS. TREATED, PRIMED AND INSTALLED REPAIR DOUBLERS. (M) 2L72 4F RTA6WE 20051108001212005110800121WP 2005 11 8 GTIA050236 120050811A5311 FRAME DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FTW - AFT ACCY 3RD FROM AFT MAIN CANT FRAME WEB CRACKED AND ATTACHED ANGLE INSIDE CRACKED. CUT OUT DAMAGED AREA. FABRICATED REPAIR DOUBLER AND FILLER. TREATED, PRIMED AND INSTALLED REPAIR DOUBLER AND FILLER. (M) 2L72 4F RTA6WE 20051108001272005110800127SO 2005 11 8 SIMA200526205 120050909A532014525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21718AE11981 145275 A PREVIOUS REPAIR ON THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED. REMOVED THE CORRODED PREVIOUS REPAIR. FABRICATED A PLATE AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 30, CHAPTERS 53-00-10 FIG 201 SHEET AND 51-40-02. (M) 2L72 4F RTT00011AT 20051108001332005110800133EU 2005 11 8 ASOA05820 120050830A5210S52176204206 PAN AEROSPATR72 ATR72212 8680945EU PAX DOOR CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27637AS 383 DURING A C-CHECK IN YUL, THE TOP AND BOTTOM PASSENGER DOOR PAN DRESSING AROUND BEAM 8 AND FS 39 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE TOP AND BOTTOM PASSENGER DOOR PAN DRESSING AROUND BEAM 8 AND FS 39 IAW ASA EO 72-52-0087. (M) 2H72 4T RTA53EU 20051108001342005110800134EA 2005 11 8 ASOA05819 120050928A5330 DOUBLER CNDAIRCL600 CL6002B19 1900309EA BS 640 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27838AS 7276 DURING AN A-CHECK IN BTR, THE RIGHT FS 640 BONDED SKIN DOUBLER, AT STRINGER 8-13, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REPAIR THE RIGHT FS 640 BONDED SKIN DOUBLER, AT STRINGER 8-13, IAW ASA EO 600-53-0107. (M) 2L72 4F RTA21EA 20051108001362005110800136SO 2005 11 8 SIMA200526204 120050910A532014525381 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO FS 24-25 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21718AE 145275 THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB IC2005-145/4951 DATED SEPT 8, 2005. (M) 2L72 4F RTT00011AT 20051108001422005110800142WP 2005 11 8 GTIA050204 120050625A2170 COALESCER BAG DOUG DC9 DC982 3022082WP CABIN CONTAMINATED A GTIAO OTHER O OTHER TXTAXI/GRND HDL 1 GL23829NK 49931 DTW - UPON TAXI WATER BEGAN POURING FROM AFT CEILING, AIRCRAFT TAIL SWAP WITH 822. REMOVED AND REPLACED BOTH WATER SEPARATOR COALESCER BAGS, OPS CHECK GOOD. (M) 2L72 4F A6WE 20051108001442005110800144EA 2005 11 8 ASOA05839 120051003A5210601R5170767 STEP CNDAIRCL600 CL6002C10 1390015EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27738EV 10146 DURING A C-CHECK IN MCN, THE PASSENGER DOOR LOWER STEP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACE THE PASSENGER DOOR LOWER STEP. (M) 2L72 4F RTA21EA 20051108001452005110800145EA 2005 11 8 ASOA05877 120051016A3350OL3071BPEGPL LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27908EV 7654 DURING A MAINTENANCE CHECK IN MCN, THE EMERGENCY LIGHT, NEAR THE SERVICE DOOR, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY LIGHT, NEAR THE SERVICE DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051108001462005110800146SO 2005 11 8 SIMA20052602 120050909A532014522178003 SILL EMB 135 EMB135LR 3260305SO SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21718AE 145275 THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED SERVICE DOOR CENTER SILL AND INSTALLED SERVICEABLE SILL IAW EMB SRM, SRM 145/1142 REV 30, CHAPTERS 51-40-02, 51-20-03, 51-20-01, 41, 51-40-06 AND 51-40-09. (M) 2L72 4F RTT00011AT 20051108001522005110800152WP 2005 11 8 GTIA050226 120050808A4910 DOOR DOUG DC9 DC983 3022083WP APU BAY CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 APU INLET DOOR ASSY IS CRACKED ON FORWARD LEFT SIDE. REMOVED APU INLET DOOR PANEL. STOPPED DRILLED CRACK. FABRICATED REPAIR DOUBLER. TREATED, PRIMED AND INSTALLED REPAIRED DOUBLER. (M) 2L72 4F RTA6WE 20051108001562005110800156EU 2005 11 8 ASOA05821 120050830A5330S5367240826001 SKIN AEROSPATR72 ATR72212 8680945EU FR-39 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27637AS 383 DURING A C-CHECK IN YUL, THE FS 39 BETWEEN STRINGER 21R-20L WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FS 39 LOWER SEGMENT IAW ASA EO 72-53-0166A. (M) 2H72 4T RTA53EU 20051108001582005110800158EU 2005 11 8 ASOA05911 120051010A5300 RETAINER AEROSPATR72 ATR72212 8680945EU SEAL CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27641AS 387 DURING A C-CHECK IN YUL, THE SEAL RETAINERS, AT FS 45 AND FS 46, WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SEAL RETAINERS, AT FS 45 AND FS 48, IAW SRM 51-21-42 AND AMM 20-21-12. (M) 2H72 4T RTA53EU 20051108001602005110800160SO 2005 11 8 SIMA200526206 120050912A532014521713005 CHANNEL EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21718AE 145275 THE RIGHT HAT BEAM IN THE GALLEY WAS FOUND TO BE CORRODED. REMOVED THE CORRODED HAT BEAM. INSTALLED NEW SERVICEABLE HAT BEAM IAW EMB SRM, SRM 145/1142 REV 30 CHAPTERS 51-20-03, 51-40-02 AND EMB CPM, CPM-145/1132 REV 12, CHAPTERS 51-21-04. (M) 2L72 4F RTT00011AT 20051108001612005110800161SO 2005 11 8 SIMA200526403 120050917A5330AL2024T3 SKIN EMB 145 EMB145LR 3260212SO FS 16-17 DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21656AE4875 145740 A DENT WITH A SCRATCH WAS DISCOVERED ON THE SKIN PANEL BETWEEN FRAMES 16 AND 17 AD BETWEEN STRINGERS 18L AND 19L. PERFORMED A CUTOUT OF THE SKIN PANEL TO REMOVE THE DAMAGE. FABRICATED A FILLER AND REPAIR DOUBLER. REPAIR DONE IAW EMB REPAIR STATEMENT IC2005-145/5137 PARA 3 DATED SEPT 15, 2003. (M) 2L72 4T RTT00011AT 20051108001622005110800162EA 2005 11 8 ASOA05871 120051014A2916 RESERVOIR CNDAIRCL600 CL6002B19 1900309EA NR 1 HYD SYSTEM OVERHEATED A ASOAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CRCRUISE 1 SO27900EV 7608 DURING CRUISE FROM ATL-YUL, AT APPROXIMATELY 33,000 FEET, THE CREW RECEIVED A NR 1 HYD TEMP HIGH EICAS MESSAGE. THE QRH WAS COMPLIED WITH AND UPON CHECKING THE NR 1 HYD TEMP THE CREW OBSERVED IT HOVERING APPROXIMATELY 110 DEGREES CELSIUS, BUT THEN ROSE TO 150 DEGREES C AND QUICKLY TO 191 DEGREES CELSIUS. THE CREW THEN SHUTDOWN THE LEFT ENGINE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO SYR, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE NR 1 HYDRAULIC RESERVOIR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051108001642005110800164EA 2005 11 8 ASOA05850 120051009A3350BR9279106 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27836AS 7263 DURING A C-CHECK IN MCN, THE EMERGENCY EXIT LIGHT, NEAR THE SERVICE DOOR, WAS FOUND TO HAVE A CRACKED LENS COVER. MAINTENANCE WILL REMOVE AND REPLACE THE EMERGENCY EXIT LIGHT ASSEMBLY. (M) 2L72 4F RTA21EA 20051108001662005110800166NM 2005 11 8 GTIA050260 120050910A3210 CONTROL UNIT AIRBUSA319 A319132 3930340NM MLG MALFUNCTIONED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23503NK 2470 FLT 516 - AFTER STARTING 2ND ENGINE RECEIVED ECAM `ALTN BRAKING` INOPERATIVE, RETURNED TO THE GATE, AIRCRAFT TAIL SWAP WITH N822NK. REMOVED AND REPLACED ABCU. ALL SYSTEMS OPS CHECK GOOD. (M) 2L72 4F RTA28NM 20051108001672005110800167EA 2005 11 8 ASOA05829 120050927A25602618 FLASHLIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27870AS 7530 DURING A GROUND INSPECTION SHV, THE FIRST OFFICERS FLASHLIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FIRST OFICERS FLASHLIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051108001712005110800171WP 2005 11 8 GTIA050259 120050914A5415 ATTACH ANGLE DOUG DC9 DC983 3022083WP LT PYLON CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23808NK 49504 LEFT PYLON T/E ATTACH ANGLE IS CRACKED APPROX 16 INCHES FROM THE T/E ROOT. REMOVED DAMAGED SECTION. FABRICATED REPAIR ANGLE AND FILLER. TREATED, PRIMED AND INSTALLED REPAIR ANGLE AND FILLER. (M) 2L72 4F RTA6WE 20051108001722005110800172SO 2005 11 8 SIMA200527709 120050926A532013500469403 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO FR 22 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21716AE 145264 SAW - FOUND FLOOR SUPPORT PROFILE AT FRAME 22 RIGHT IS CORRODED. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20051108001732005110800173SO 2005 11 8 SIMA200527710 120050926A533014522461011 DOUBLER EMB 135 EMB135LR 3260305SO FR 22 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21716AE 145264 FOUND RIGHT SIDE DOUBLER PLATE CORRODED AT FRAME 22. INSTALLED NEW DOUBLER PLATE IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20051108001772005110800177SO 2005 11 8 SIMA200526401 120050912A5300 SILL EMB 135 EMB135KL 3260302SO FR 20-22 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21857AE 145752 SAW - DURING CPCP INSPECTION, FOUND SERVICE DOOR SILL IS CORRODED BETWEEN FRAMES 20 AND 22. MAINTENANCE INSTALLED A NEW SERVICE DOOR SILL IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20051108001792005110800179EU 2005 11 8 ASOA05864 120051012A33503011210 LIGHT AEROSPATR72 ATR72212 8680945EU CABIN INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27634AS 370 DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. (M) 2H72 4T RTA53EU 20051108001822005110800182EA 2005 11 8 ASOA05842 120051003A335060206 SIGN CNDAIRCL600 CL6002B19 1900309EA EMERGENCY EXIT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27835AS 7258 DURING A C-CHECK IN MCN, THE PASSENGER DOOR EMERGENCY EXIT SIGN, ON THE LOWER FORWARD CLOSET, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY EXIT SIGN, LOCATED ON THE LOWER FORWARD CLOSET. OPS CHECKS GOOD. (M) 2L72 4F RTA21EA 20051108001832005110800183WP 2005 11 8 GTIA050214 120050713A3610 SENSOR DOUG DC9 DC983 3022083WP VENTURI CLOGGED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23802NK 53168 UPON CLIMB-OUT, "TAIL COMPT TEMP HI" LIGHT ILLUMINATED, AIR RETURN BACK TO ACY. ENGINE GROUND POWER RUN PERFORMED, LEFT AND RIGHT PACKS OPERATED. NO DUCT LEAKS FOUND, RAN PACKS OFF OF AP. NO LEAKS FOUND. FOUND VENTURI SENSOR CLOGGED WITH DEBRIS, OIL SUBSTANCE, CLEANED VENTURI AND PROBE SENSORS. SYSTEM CHECKED NORMAL. (M) 2L72 4F RTA6WE 20051108001842005110800184EA 2005 11 8 ASOA05811 120050926A3350BC50393106 LENS CNDAIRCL600 CL6002B19 1900309EA CABIN MISSING A ASOAK NONE O OTHER ININSP/MAINT 1 SO11827AS 7212 FLT 4084 - DURING A GROUND INSPECTION IN ATL, THE FLOOR LEVEL EMERGENCY EXIT SIGN ON THE FORWARD BULKHEAD WAS FOUND TO BE MISSING A COVER. MAINTENANCE REPLACED THE FLOOR LEVEL EMERGENCY EXIT SIGN MISSING COVER ON THE FORWARD BULKHEAD. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051108001862005110800186SO 2005 11 8 SIMA200526201 120050917A3350 BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSDISCHARGED A SIMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21650AE 145417 THE EMERGENCY LIGHTS ILLUMINATED IN THE COCKPIT AND CABIN. SHORTLY AFTERWARDS THE EMERGENCY LIGHTS NOT ARMED MESSAGE APPEARED ON THE EICAS. REPLACED EMERGENCY BATTERIES NR 1 AND NR 3 IAW EMB 145 MM 33-50-04. BOTH BATTERIES HAD LOW VOLTAGE. PERFORMED EMERGENCY LIGHTING TEST IAW EMB-145 MM 33-50-00. NO DEFECTS NOTED. A/C RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20051108001922005110800192WP 2005 11 8 GTIA050257 120050921A5330 SKIN DOUG DC9 DC983 3022083WP BS 474-480 DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23808NK 49504 FOUND DENT STATION 474-480, 18L X=0.028 D=1.0. CUT OUT DAMAGED AREA. FABRICATED REPAIR DOUBLERS. TREATED, PRIMED AND INSTALLED REPAIR DOUBLERS. (M) 2L72 4F RTA6WE 20051108001932005110800193WP 2005 11 8 GTIA050255 120050907A5320 SUPPORT DOUG DC9 DC983 3022083WP BS 351-370 WORN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23808NK 49504 MAIN CABIN STATION 351-370 AT L4L HAS WORN SUPPORT. BLENDED WORN OUT SUPPORT STRUCTURES AND FOUND OUT OF LIMITS. FABRICATED SUPPORT STRUCTURE AT MAIN CABIN STATION 351-370. TREATED, PRIMED AND INSTALLED SUPPORT STRUCTURE. (M) 2L72 4F RTA6WE 20051108001972005110800197WP 2005 11 8 GTIA050232 120050726A5330 SKIN DOUG DC9 DC983 3022083WP BS 212 DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FOUND DENT AT FS 212, X=0.038, D=0.5 AND D/X=17.2. REMOVED FLOORBOARDS, COVER GRILL, AND CUT OUT WEB TO FOM FOR SKIN REPAIR. FABRICATED INTERNAL REPAIR DOUBLER. TREATED, PRIMED AND INSTALLED INTERNAL REPAIR DOUBLER. FABRICATED WEB REPAIR DOUBLER. TREATED, PRIMED AND INSTALLED REPAIRED WEB DOUBLER. RE-INSTALLED DUCTS, GRILLS AND FLOORBOARDS FOR ACCESS. (M) 2L72 4F RTA6WE 20051108001992005110800199SO 2005 11 8 SIMA200527705 120050929A532014521725013 SILL EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21820AE 145576 THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED THE DAMAGED SILL AND CLEANED THE AREA. INSTALLED SERVICEABLE SILL IAW EMB REPAIR STATEMENT IC2005-145/5419 DATED SEPT 27, 2005. (M) 2L72 4F RTT00011AT 20051108002002005110800200WP 2005 11 8 GTIA050239 120050826A5320 CUSP WEB DOUG DC9 DC983 3022083WP BS 598 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23834NK 49847 FOUND CORROSION INSIDE CABIN AT CUSP LINE, WEB STATION 598, L18L. REMOVED CORROSION AT WEB STATION 598. FOUND ITS OUT OF LIMITS. CUT OUT DEFECTIVE AREA. FABRICATED REPAIR DOUBLER AND FILLER. TREATED, PRIMED AND INSTALLED DOUBLER AND FILLER. (M) 2L72 4F RTA6WE 20051108002042005110800204SO 2005 11 8 SIMA200527702 120050928A531014522460013 BEAM EMB 135 EMB135KL 3260302SO FRAME 24 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21820AE 145576 THE CENTER BEAM AT FRAME 24 WAS FOUND CORRODED. PERFORMED A CUT OUT TO REMOVE THE CORROSION. FABRICATED A FILLER, DOUBLER AND SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC 2005-145/5255 DATED SEPT 21, 2005 AND EMB 145 SRM, SRM EMB 145/1142 REV 30, CHAPTER 53-00-10 FIG 203. (M) 2L72 4F RTT00011AT 20051108002062005110800206WP 2005 11 8 GTIA050237 120050724A5730 VANE DOUG DC9 DC983 3022083WP LT WING FLAP GOUGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FOUND LEFT WING, FIXED FLAP VANE, 4TH FROM INBOARD, L/E IS GOUGED. FIXED T-CAP VANE, FOUND OUT OF LIMITS. FABRICATED DOUBLERS AND REPAIRED LEFT FIXED VANE. (M) 2L72 4F RTA6WE 20051108002082005110800208SO 2005 11 8 SIMA200527706 120050929A5311 FRAME EMB 135 EMB135KL 3260302SO FUSELAGE CRACKED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21820AE 145576 FOUND FRAME 68 WAS FOUND CRACKED AT THE BAGGAGE DOOR STAY ROD HOLDER CUP BRACKET. PERFORMED CUT OUT OF FRAME 68 TO REMOVE THE DAMAGE. FABRICATED AN ANGLE SPLICE AFT AND ONE FOR FORWARD. FABRICATED A CUP SUPPORT. REPAIR DONE IAW EMB REPAIR STATEMENT IC2005-145/5216A, DATED SEPT 21, 2005. (M) 2L72 4F RTT00011AT 20051108002102005110800210SO 2005 11 8 SIMA200526203 120050910A532014525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21718AE 145275 THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 23 AND 25. REMOVED THE CORROSION BY MAKING A CUTOUT. FABRICATED A DOUBLER, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB IC2005-145/4951 DATED SEPT 8, 2005. (M) 2L72 4F RTT00011AT 20051108002112005110800211EA 2005 11 8 ASOA05844 120051005A5210601R3198055 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27901EV 7616 FLT 4460 - DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR LOWER STEP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LOWER STEP. OPERATIONAL CHECKS GOOD. (M) 2L72 4F RTA21EA 20051108002122005110800212WP 2005 11 8 GTIA050229 120050723A4910 DOOR DOUG DC9 DC983 3022083WP APU BAY CHAFED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FTW - FOUND LEFT APU COMPARTMENT DOOR, LOWER EDGE IS CHAFFED ALONG WITH MATING SURFACE. BLEND OUT CHAFED AREA FOUND OUT OF LIMITS. CUT OUT DAMAGED AREA. FABRICATED REPAIR DOUBLER AD FILLER. TREATED, PRIMED AND INSTALLED REPAIRED DOUBLER AND FILLER. (M) 2L72 4F RTA6WE 20051108002142005110800214WP 2005 11 8 GTIA050254 120050911A5320 CUSP WEB DOUG DC9 DC983 3022083WP BS 389-408 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23808NK 49504 FTW - MAIN CABIN, LEFT SIDE STATION 389 TO STATION 408 CUSP WEB SURFACE HAVE CORROSION. REMOVED CORROSION FOUND WEB TO BE OUT OF LIMITS. FABRICATED REPAIR DOUBLER AND FILLER. TREATED, PRIMED AND INSTALLED REPAIR DOUBLER AND FILLER. (M) 2L72 4F RTA6WE 20051108002152005110800215WP 2005 11 8 GTIA050252 120050914A5312 BULKHEAD DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23808NK 49504 FTW - FOUND MID CARGO AFT PRESSURE BULKHEAD PANEL (5318C) HAS A PULLED RIVET AND LIGHT SURFACE CORROSION, MISSING CAMLOCKS. CORROSION REMOVED, FOUND CRACK AND OUT OF LIMITS. FABRICATED REPAIR DOUBLER AND FILLER. TREATED, PRIMED AND INSTALLED REPAIR DOUBLER AND FILLER. (M) 2L72 4F RTA6WE 20051108002162005110800216NE 2005 11 8 GTIA050217 220050722A7200 ENGINE DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE NR 1 OVERHEATED A GTIAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 GL23828NK 49823 718190 SJU - LEFT ENGINE OIL GREATER THAN 170 ON CLIMB-OUT. SHUT ENGINE DOWN PER QRH AND RETURNED TO SJU. REMOVED AND REPLACED NR 1 ENGINE IAW MM 71-00-00 AND W/C 00191. (M) 2L72 4F4 FRT E9NE 20051108002172005110800217 2005 11 8 GTIA050216 420050720A2565D30664309 SLIDE AIRBUSA321 A321211 3930370EU PAX DOOR DEPLOYED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23585NK 1438 FLT 507 - FLL - FOUND FORWARD SLIDE ACCIDENTALLY DEPLOYED AT THE GATE, SLIDE PACK DID NOT FULLY INFLATE DUE TO A RUPTURED LINE ON THE CHARGE BOTTLE. (M) 2L72 4F RTA28NM 20051108002202005110800220SO 2005 11 8 SIMA200525218 120050907A5210 SKIN EMB 145 EMB145LR 3260212SO PAX DOOR GOUGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21633AE 145148 SAW - DURING PHASE 5A INSPECTION, FOUND GOUGE ON EXTERNAL SKIN ON PASSENGER DOOR AFT LOWER EDGE. REPAIRED PAX DOOR BY INSTALLING EXTERNAL DOUBLER IAW SRM 52-10-01 FIGURE 204 AND IC 2005-145/4892. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20051108002212005110800221EA 2005 11 8 ASOA05843 120051024A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27823AS 7196 FLT 4552 - DURING A GROUND INSPECTION IN CVG, THE EMERGENCY LIGHTS WOULD NOT TURN OFF WHILE IN THE ARMED POSITION. MAINTENANCE CYCLED THE CIRCUIT BREAKERS, AND VERIFIED PROPER OPERATION OF THE EMERGENCY LIGHTS. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051108002222005110800222WP 2005 11 8 GTIA050248 120050831A5754 SKIN DOUG DC9 DC983 3022083WP NR 1 SLAT DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23834NK 49847 LT WING NR 1 SLAT DENTED STATION XTS 128.000, DENT DIAMETER = 2.0 DEPTH = .048. LEFT WING, NR 1 SLAT DENT FOUND OUT OF LIMIT. REPAIRED DENT AREA. (M) 2L72 4F RTA6WE 20051108002232005110800223WP 2005 11 8 GTIA050247 120050817A5315 FLOORBEAM DOUG DC9 DC983 3022083WP COCKPIT CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 LEFT COCKPIT ENTRY WAY FLOORBEAM HAS AREAS OF CORROSION. AREAS OF CORROSION FOUND OUT OF LIMITS. FABRICATED ENTRY WAY FLOORBEAM. TREATED, PRIMED AND INSTALLED FABRICATED FLOORBEAM. (M) 2L72 4F RTA6WE 20051108002262005110800226WP 2005 11 8 GTIA050250 120050829A5511 RIB DOUG DC9 DC983 3022083WP HORIZONTAL STAB CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23834NK 49847 FOUND RIGHT HORIZONTAL STABILIZER L/E, OUTBOARD L/E RIB CRACKED AT UPPER EDGE. STOPPED DRILLED CRACKED AREA. FABRICATED REPAIR PART. TREATED, PRIMED AND INSTALLED REPAIR PART. (M) 2L72 4F RTA6WE 20051108002282005110800228WP 2005 11 8 GTIA050249 120050819A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP BS 180 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 FOUND FLOOR WEB AT APPROX STATION 180 BETWEEN L1 AND R1 DOOR HAS SEVERAL AREAS OF CORROSION. REMOVED CORRODED MEMBRANE AND SUPPORT. FABRICATED NEW MEMBRANE. TREATED, PRIMED AND INSTALLED REPAIR MEMBRANE. (M) 2L72 4F RTA6WE 20051108002292005110800229NM 2005 11 8 AMTA200500700 120050909A3350 LIGHT BOEING757 75723N 1384973NM CABIN INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11522AT 29330 EMERGENCY LIGHT STRIP NUMEROUS LIGHTS INOPERATIVE FROM SEAT ROW 2FED TO 9FED. REPAIRED EGRESS EMERGENCY LIGHT SYSTEM FROM SEAT ROW 2 DEF TO 9 DEF PER AMM 33-51-11-403-049, OPS CHECK GOOD. (M) 2L72 4F RTA2NM 20051108002302005110800230NM 2005 11 8 AMTA200500694 120050910A3350 LIGHT BOEING757 75723N 1384973NM CABIN INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11514AT 27971 FOUND 9 FLOOR PATH EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY AT ROW 9, OPS CHECK GOOD. (M) 2L72 4F RTA2NM 20051108002322005110800232WP 2005 11 8 GTIA050208 120050628A5210 HOOK DOUG DC9 DC983 3022083WP L1 DOOR CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23815NK 49415 FOUND L-1 DOOR HOLD OPEN HOOK CUT OUT CRACKED STATION 200. REMOVED COVERS TO FOM. STOPPED DRILLED L1 DOOR CUTOUT. FABRICATED DOUBLER, TREATED, PRIMED AND INSTALLED DOUBLER. INSTALLED COVERS. (M) 2L72 4F RTA6WE 20051108002342005110800234WP 2005 11 8 GTIA050210 120050712A5753 VANE DOUG DC9 DC983 3022083WP LT WING TE FLAP DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23815NK 49415 FOUND LEFT WING OUTBOARD FLAP, OUTBOARD VANE, HOLE IN LEADING EDGE. REPAIRED OUTBOARD VANE IAW MD80 SRM 57-03 PAR 8A. TREATED AND PRIMED AREA. (M) 2L72 4F RTA6WE 20051108002372005110800237WP 2005 11 8 GTIA050245 120050811A5315 FLOORBEAM DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 FOUND LEFT FLOORBEAM IN FRONT OF L1 DOOR CORRODED. MEASURED CORRODED AREAS, FOUND OUT OF LIMITS. MANUFACTURED FLOORBEAM. TREATED, PRIMED AND INSTALLED FLOORBEAM. (M) 2L72 4F RTA6WE 20051108002382005110800238EU 2005 11 8 ASOA05909 120051006A5311 FRAME AEROSPATR72 ATR72212 8680945EU FS 39 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27641AS 387 DURING A C-CHECK IN YUL, THE FS 39, AND STRINGER 14R, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FS 39, AT STRINGER 14R, IAW ASA EO 72-53-0185. 2H72 4T RTA53EU 20051108002412005110800241NE 2005 11 8 ASOA05851 220051009A72616087T04P06 SCAVENGE PUMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE RT ENGINE MALFUNCTIONED A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27687BR 7720 FLT 4179 - DURING CLIMB-OUT FROM ATL-ISP, THE RIGHT ENGINE OIL PRESSURE FLUCTUATED AND GRADUALLY DECREASED THROUGH OUT CLIMB BETWEEN 25-45 PSI FOLLOWED BY THE OIL TEMPERATURE READING 146 DEGREES CENTRIGRADE. THE CREW REDUCED POWER, AND ALL INDICATIONS RETURNED TO NORMAL. AIRCRAFT RETURNED TO ATL, WITH CREW REQUESTING EMERGENCY VEHICLES TO BE ON STANDBY AS A PRECAUTION. AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE LUBE AND SCAVENGE PUMP. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F4 FRTA21EA E15NE 20051108002422005110800242WP 2005 11 8 GTIA050256 120050907A5330 SKIN DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23808NK 49504 FOUND CRACK AT NLG RIGHT HINGE CUT OUT STATION 101. REMOVE AFT RIGHT NOSE GEAR DOOR. FABRICATED REPAIR DOUBLER. TREATED, PRIMED AND INSTALLED AFT RIGHT NOSE GEAR DOOR. (M) 2L72 4F RTA6WE 20051108002432005110800243EA 2005 11 8 ASOA05863 120051012A5321 FLOOR PANEL CNDAIRCL600 CL6002B19 1900309EA BS 473 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27836AS 7263 DURING A C-CHECK IN MCN, THE PRESSURE FLOOR SKIN AT FS 473.15, LBL 36 WAS FOUND TO BE CORRODED BEYOND LIMITS. (M) 2L72 4F RTA21EA 20051108002452005110800245EA 2005 11 8 ASOA05858 120051010A33506100928 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27909EV 7658 FLT 4500 - DURING A GROUND INSPECTION IN SHV, THE FLOOR LEVEL EMERGENCY LIGHT, NEAR THE PASSENGER DOOR, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE FLOOR LEVEL EMERGENCY LIGHT, NEAR THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051108002462005110800246EA 2005 11 8 ASOA05845 120051005A3320BC10059003 LIGHT CNDAIRCL600 CL6002B19 1900309EA GALLEY MALFUNCTIONED A ASOAB EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27868AS 7474 FLT 4916 - DURING CRUISE FROM ATL-BUF, THE CAPTAIN NOTICED AN ELECTRICAL BURNING SMELL IN THE COCKPIT. SHORTLY AFTER, THE FLIGHT ATTENDANT REPORTED AN ELECTRICAL BURNING SMELL IN THE CABIN. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO TYS, WHERE IT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE GALLEY FLOOR LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051108002502005110800250EA 2005 11 8 ASOA05816 120050926A5347 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA BS 473 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27835AS 7258 DURING A C-CHECK IN MCN, THE LEFT UPPER SEAT TRACK, AT FS 473.15, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACE THE LEFT UPPER SEAT TRACK, AT FS 473.15. (M) 2L72 4F RTA21EA 20051108002512005110800251EA 2005 11 8 ASOA05841 120051003A33502013BR BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27835AS 7258 DURING A C-CHECK IN MCN, THE SERVICE DOOR EMERGENCY LIGHT, MOUNTED ON THE GALLEY, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY PACK. OPS CHECKS GOOD. (M) 2L72 4F RTA21EA 20051108002522005110800252EA 2005 11 8 ASOA05801 120050924A5321 DOUBLER CNDAIRCL600 CL6002B19 1900309EA BS 449-559 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27835AS 7258 DURING A C-CHECK IN MCN, THE RIGHT SIDE DOUBLERS, FROM 449-559, ON THE PRESSURE FLOOR WERE FOUND TO BE CORRODED. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO BOMBARDIER TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. AFTER MAINTENANCE BLENDED, ALODINED, AND PRIMED THE RIGHT SIDE DOUBLERS, FROM FS 449-559, IAW REO 601R-53-41-359, FOUND TO BE WITHIN LIMITS. (M) 2L72 4F RTA21EA 20051108002542005110800254EA 2005 11 8 ASOA05813 120050926A5347 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27835AS 7258 DURING A C-CHECK IN MCN, THE RIGHT SIDE SEAT RAIL, FROM THE FRONT TO THE REAR, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACE THE RIGHT SIDE SEAT RAIL, FROM THE FRONT TO REAR. (M) 2L72 4F RTA21EA 20051108002562005110800256EA 2005 11 8 ASOA05840 120051003A5270 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA APU DOOR ILLUMINATED A ASOAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 SO27923EV 7826 FLT 4541 - DURING CRUISE FROM ATL-SHV, AFTER SHUTTING DOWN THE APU, THE CREW RECEIVED AN `APU DOOR INHIBIT/OPEN` MESSAGE WITH A FUEL SMELL COMING FROM THE PACKS. THE AIRCRAFT LANDED SAFELY IN SHV. MAINTENANCE RESET THE APU DOOR TO THE NORMAL POSITION. THE APU STARTED NORMALLY WITH NO ODOR OF ANY KIND DETECTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051108002572005110800257EA 2005 11 8 ASOA05878 120051016A3350100865 POWER SUPPLY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27921EV 7819 FLT 4164 - DURING A MAINTENANCE CHECK IN MCN, THE RIGHT FORWARD EXTERNAL OVERWING EMERGENCY LIGHT AND THE CENTER AISLE EMERGENCY LIGHT AT ROW 9 WERE FOUND TO BE INOPERATIVE. MAINTENANCE WILL REMOVE AND REPLACE THE NR 2 POWER SUPPLY (BATTERY PACK), AND THE RIGHT FORWARD EXTERNAL OVERWING EMERGENCY LIGHT ASSEMBLY. (M) 2L72 4F RTA21EA 20051108002582005110800258EU 2005 11 8 ASOA05869 120051013A33503011210 LIGHT AEROSPATR72 ATR72212 8680945EU PAX DOOR INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27633AS 344 DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY ON THE PASSENGER DOOR. OPERATIONAL CHECK GOOD. (M) 2H72 4T RTA53EU 20051108002592005110800259EU 2005 11 8 ASOA05866 120051013A33507012210 LAMP AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27636AS 375 FLT 4223 - DURING A GROUND INSPECTION IN MGM, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY LIGHT ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20051108002612005110800261NE 2005 11 8 ASOA05803 220050915A72615016T32POL CARBON SEAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT ENGINE WORN A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27665BR 7534 FLT 4514 - DURING CLIMB-OUT FROM ATL, AT APPROXIMATELY 2000 FEET, A `RIGHT ENGINE OIL PRESSURE` WARNING WAS RECEIVED. THE WARNING WENT OUT AND RETURNED APPROXIMATELY 5 SECONDS LATER WITH OIL PRESSURE READING 20 PSI. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED TO ATL WHERE IT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE CARBON SEALS IAW CRJ AMM 72-60-00. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F4 FRTA21EA E15NE 20051108002622005110800262EA 2005 11 8 ASOA05881 120051017A5210601R319805 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27828AS 7213 DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR BOTTOM STEP WAS FOUND TO BE BROKEN. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051108002632005110800263EA 2005 11 8 ASOA05859 120051010A5210601R319805 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27825AS 7207 FLT 4460 - DURING A HANGAR INSPECTION IN MCN, THE PASSENGER DOOR LOWER STEP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR LOWER STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051108002672005110800267EA 2005 11 8 ASOA05837 120051001A3350OL3071BPEGPL LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27874AS 7551 FLT 4794 - DURING A GROUND INSPECTION IN ATL, THE EMERGENCY EXIT SIGN, NEAR THE PASSENGER DOOR, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT SIGN, NEAR THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051108002682005110800268EA 2005 11 8 ASOA05838 120051001A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FS 640 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27838AS 7276 DURING AN A-CHECK IN BTR, THE RIGHT FS 640, AT STRINGER 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT FS 640, AT STRINGER 9. OPERATIONAL CHECKS GOOD. (M) 2L72 4F RTA21EA 20051108002702005110800270EA 2005 11 8 ASOA05887 120051019A5260601R3198057 STEP CNDAIRCL600 CL6002B19 1900309EA AIRSTAIR DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27902EV 7620 DURING A HANGAR INSPECTION IN MCN, THE AIRSTAIR DOOR BOTTOM STEP WAS FOUND TO BE CRACKED AT THE ATTACHED BRACKET STAY ROD. MAINTENANCE REMOVED AND REPLACED THE AIR STAIR DOOR BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051108002712005110800271EA 2005 11 8 ASOA05835 120050930A5347 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA BS 513 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27835AS 7258 DURING A C-CHECK IN MCN, THE UPPER LEFT SEAT TRACK, AT FS 513, AS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE UPPER LEFT SEAT TRACK AT FS 513. (M) 2L72 4F RTA21EA 20051108002722005110800272EA 2005 11 8 ASOA05834 120050928A5210 LINKAGE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR HANDLE OUT OF ADJUST A ASOAK NONE O OTHER ININSP/MAINT 1 SO27836AS 7263 FLT 4307 - DURING A GROUND INSPECTION IN ATL, THE FLIGHT ATTENDANT NEEDED ASSISTANCE TO LOCK PASSENGER DOOR. MAINTENANCE ADJUSTED THE PASSENGER DOOR HANDLE LINKAGE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051108002732005110800273EA 2005 11 8 ASOA05833 120050928A5210HSP115B094900 SHEAR PIN CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27833AS 7404 DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WOULD NOT CLOSE AND LOCK. MAINTENANCE REMOVED AND REPLACED A BROKEN SHEAR PIN IN THE DOOR HANDLE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051108002742005110800274EA 2005 11 8 ASOA05830 120050919A1100S1859 PLACARD CNDAIRCL600 CL6002B19 1900309EA CABIN MISSING A ASOAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO27841AS 7300 DURING A C-CHECK IN MCN, THE EMERGENCY ESCAPE PLACARDS ON THE CREW ESCAPE HATCH WERE FOUND TO BE MISSING. MAINTENANCE INSTALLED EMERGENCY ESCAPE PLACARDS ON THE CREW ESCAPE HATCH IAW CRJ AMM 11-20-01. (M) 2L72 4F RTA21EA 20051108002752005110800275EU 2005 11 8 ASOA05831 120050928A33507012210 LAMP AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27633AS 344 DURING A GROUND INSPECTION IN ATL, THE EMERGENCY TRACK LIGHTS, NEAR SEATS 6A AND 6B WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY TRACK LIGHT LAMP, NEAR 6A AND 6B. OPERATIONAL CHECKS GOOD. (M) 2H72 4T RTA53EU 20051108002762005110800276EU 2005 11 8 KBM2005F00254 120050810A5101355909103601 CASE SNIAS 350 AS350B2 8680813EU UNKNOWN TORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19751H 3403 UNITS ARE TORN AND WORN. REMOVED AND REPLACED CASE. (M) 1G71 3U H9EU 20051108002862005110800286EU 2005 11 8 ASOA05741A 120050907A2752FE231003 ACTUATOR AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE TE FLAPS MALFUNCTIONED A ASOAO OTHER O OTHER NRNOT REPORTED 1 SO27635AS267502995 372 LT IB ACTUATOR, MALFUNCTIONED. LT WING. 2H72 4T4 TRTA53EU E20NE 20051108002932005110800293EU 2005 11 8 KBM2005F00257 120050916A7931704A37642043 TRANSMITTER SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE ENG OIL PRESSUREMALFUNCTIONED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P 2347 UPON ENGINE START, ENGINE OIL PRESSURE WENT TO ZERO. REMOVED AND REPLACED TRANSMITTER. (K) 1G71 3U3 UNCH9EU E19EU 20051108002942005110800294EU 2005 11 8 KBM2005F00264 120050830A6420350A33214501 LINK SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE T/R PITCH CONTROWORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV2667 3296 T/R P/C LINK, WORN BEYOND LIMITS. REPLACED WITH SERVICEABLE UNIT. (K) 1G71 3U3 U H9EU E19EU 20051108002962005110800296SO 2005 11 8 GUU2005F00055 120051005A3350AGC1 FUSE EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE EMERGENCY LIGHT OPEN A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO17261AS 120141 EXTERIOR EMERGENCY LIGHT AFT OF WING INOPERATIVE. REPLACED FUSE FOR AFT EMERGENCY LIGHT. (K) 2L72 4T4 TRTA31SO E20NE 20051108002992005110800299NM 2005 11 8 AMTA200500823 120051005A3350 LAMP BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE EMERGENCY LIGHT INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11518AT 27974 L-3 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. CLEANED SOCKET AND RESEATED LAMP. OPS CHECK GOOD IAW AMM. (K) 2L72 4F4 FRTA2NM E12EU 20051108003002005110800300EU 2005 11 8 KBM2005F00306 120050925A311056337078013 INDICATOR SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE COCKPIT INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV2368 3296 BACK LIGHTING INOPERATIVE ON NG GAUGE, REMOVED AND REPLACED WITH REPAIRED UNIT. (K) 1G71 3U3 U H9EU E19EU 20051108003072005110800307NE 2005 11 8 TRB2005F00006 220050913A7230PW127 COMPRESSOR AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE ENGINE FOD A TRBAC ABORTED TAKEOFF C F.O.D. TOTAKEOFF 1 SO29451AT16677 451 127111 ( REF NR: SDR2005065 ) DURING TAKEOFF ROLL, SPARKS WERE COMING OUT THE RT ENGINE. TAKEOFF ABORTED. FOUND FOD DAMAGE IN THE COMPRESSOR BLADES. ENGINE REPLACED. (K) 2H72 4T4 TRTA53EU E20NE 20051108003192005110800319SO 2005 11 8 B7T2005F00001 220050706A8530AEC631397 CYLINDER HEAD CESSNA207 207 2073602CE CONT O520 IO520F 17032SO HARTZLHCC3Y HCC3YF1 GL NR 1 CRACKED E B7TAO OTHER O OTHER NRNOT REPORTED 1 AL0391002 596 20700003 564011 EE2069A CYLINDER CRACKED UNDER SPARK PLUG HOLE RT LOWER CONNER AT SECOND FIN LEAKING AIR. (K) 1H71 3O3 O A16CE E5CE 5 CP25EA 20051108003202005110800320SO 2005 11 8 B7T2005F00002 220050706A8530AEC631397 CYLINDER HEAD CESSNA207 207 2073602CE CONT O520 IO520F 17032SO HARTZLHCC3Y HCC3YF1 GL NR 1 CRACKED E B7TAO OTHER O OTHER NRNOT REPORTED 1 AL0391002 596 20700003 564011 EE2069A CYLINDER CRACKED UNDER SPARK PLUG HOLE RT LOWER CONNER AT SECOND FIN LEAKING AIR. (K) 1H71 3O3 O A16CE E5CE 5 CP25EA 20051108003262005110800326CE 2005 11 8 S2YA05054 120050905A5753 MOUNT BEECH 1900 1900D 1154162CE PWA 306 PW306B NE TE FLAPS LOOSE A S2YAA UNSCHED LANDING O OTHER CLCLIMB 1 GL1381SK UE81 PREVIOUS SDR, SHORTLY AFTER TAKEOFF OF FLIGHT, CREW REPORTED FLAPS WILL NOT RETRACT. AFTER CONSULTING WITH DISPATCH AND MAINT CREW PERFORMED AND AIR-TURN-BACK. MAINT REPLACED RT SAFELY SWITCH LINK AND CAM, OPS CHECKED SYSTEM AND WITH NO FURTHER DEFECTS RETURNED THE AC TO SERVICE. SHORTLY AFTER TAKEOFF OF FLIGHT, THE CREW REPORTED THE FLAPS WILL NOT RETRACT. AFTER CONSULTING WITH DISPATCH AND MAINTENANCE. CREW PERFORMED AN AIR-TURN-BACK. MAINT USED THE FLAP OVERRIDE SWITCH RETURNED THE FLAPS TO ZERO DEGREES AND MELED THE SYS. INSPECTED SYS AND FOUND RT SAFETY SWITCH MOUNT TO BE LOOSE. MAINT TIGHTENED THE MOUNT, OPS CHECKED SYSTEM, NO FURTHER DEFECTS. RETURNED AC TO SERVICE. (K) 2L72 4T4 FRTA24CE E35NE 20051108003272005110800327NM 2005 11 8 S2YA05057A 120050913A282131B370201 FUEL FILTER DORNERDO32 DO328300 NM PWA 306 PW306B NE LEFT INOPERATIVE A S2YAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL13359SK8485 1639 3202 DURING CLIMBOUT, THE CREW REPORTED A FUEL FILTER CAS MESSAGE. THE CREW PERFORMED AN AIR-TURN-BACK. MAINTENANCE REPLACED BOTH THE LT FUEL FILTER AND FUEL FILTER PRESSURE SWITCH. OPS CHECKS GOOD THE AC WAS RETURNED TO SERVICE. (K) 2H72 4T4 FRTA55NM E35NE 20051108000942005110800094SO 2005 11 8 SIMA200527712 120050927A532014521700007 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO FR 20 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21716AE 145264 FOUND REPAIR DOUBLER ON LEFT OMEGA BEAM AT FRAME 20 IS CORRODED. REPLACED REPAIR DOUBLER IAW EMB SRM 53-00-10 FIGURE 201. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20051108001222005110800122EA 2005 11 8 ASOA05888 120051020A3350362624 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27882AS 7503 DURING A GROUND INSPECTION IN ATL, THE FLOOR EMERGENCY LIGHT STRIP FROM ROW 5 FORWARD, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FLOOR EMERGENCY LIGHT STRIP, FROM ROW 5 FORWARD. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051108001232005110800123EA 2005 11 8 ASOA05885 120051019A5315 FLOORBEAM CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11712EV 10074 DURING HANGAR MAINTENANCE IN MCN, THE FLOORBOARD SUPPORT BEAM, JUST INBOARD OF THE AIRSTAIR DOOR SILL, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACE THE FLOORBOARD SUPPORT BEAM, INBOARD OF THE AIRSTAIR DOOR SILL. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051108001352005110800135EA 2005 11 8 ASOA05814 120050926A5347 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA BS 364 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27835AS 7258 DURING A C-CHECK IN MCN, THE LEFT INBOARD SEAT TRACK, AT FS 364, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACE THE LEFT INBOARD SEAT TRACK, AT FS 364. (M) 2L72 4F RTA21EA 20051108001382005110800138WP 2005 11 8 GTIA050207 120050618A5320 CUSP WEB DOUG DC9 DC983 3022083WP BS 516 CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23815NK 49415 FOUND CABIN L18R CUSP WEB CORRODED/CRACKED STATION 516. REMOVED CORROSION AND FOUND OUT OF LIMITS. CUTOUT AND CRACKED WEB. FABRICATED REPAIR DOUBLER AND FILLER. TREATED, PRIMED AND INSTALLED REPAIR DOUBLER AND FILLER. (M) 2L72 4F RTA6WE 20051108001402005110800140EA 2005 11 8 ASOA05815 120050926A5347 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA BS 559 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27835AS 7258 DURING A C-CHECK IN MCN, THE AFT CARGO COMPARTMENT SEAT TRACK, AT FS 559 PLUS 112, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACED THE AFT CARGO COMPARTMENT SEAT TRACK, FROM FS 559 PLUS 112. (M) 2L72 4F RTA21EA 20051108001482005110800148EA 2005 11 8 ASOA05879 120051015A3350BC50393106 COVER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT MISSING A ASOAK NONE O OTHER ININSP/MAINT 1 SO27909EV 7658 DURING A GROUND INSPECTION IN ATL, THE EXIT SIGN, NEAR THE GALLEY, WAS FOUND TO HAVE A MISSING COVER. MAINTENANCE REPLACED THE EXIT SIGN COVER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051108001492005110800149EU 2005 11 8 ASOA05824 120050830A5320 FLOOR SUPPORT AEROSPATR72 ATR72212 8680945EU FS 36-38 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27637AS 383 DURING A C-CHECK IN YUL, THE LT/RT FLOOR SUPPORTS BETWEEN FS 36-38 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LT/RT FLOOR SUPPORTS BETWEEN FS 36-38 IAW ATR-72 SRM 51-25-01. (M) 2H72 4T RTA53EU 20051108001512005110800151EA 2005 11 8 ASOA05875 120051015A3350 COVER CNDAIRCL600 CL6002B19 1900309EA FLOODLIGHT LOOSE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27827AS 7212 DURING A GROUND INSPECTION IN ATL, THE EMERGENCY FLOOD LIGHT COVER, NEAR THE PASSENGER DOOR, WAS FOUND TO BE UNSECURED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOODLIGHT, NEAR THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051108001632005110800163EA 2005 11 8 ASOA05873 120051015A3397 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENC LIGHTS DIRTY A ASOAK NONE O OTHER ININSP/MAINT 1 SO27828AS 7213 DURING A GROUND INSPECTION IN TPA, THE EMERGENCY LIGHTS REMAINED ON WITH THE SWITCH IN THE ARMED POSITION. MAINTENANCE CLEANED THE CONNECTOR ON JUNCTION BOX 6 PANEL. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051108001702005110800170WP 2005 11 8 GTIA050261 120050930A2120 ODOR DOUG DC9 DC983 3022083WP UNKNOWN DETECTED A GTIAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL23802NK 53168 F/A REPORTED SMELL OF RUBBER BURNING, BETWEEN ROWS 7-11, BUT NO SMOKE NOTED, PRECAUTIONARY DIVERSION INTO SDF. INSPECTED BALLAST BETWEEN ROW 7-11, INSPECTED OXYGEN GENERATORS, INSPECTED EMERGENCY POWER SUPPLIES, INSPECTED PSU PANELS. NO DEFECTS NOTED. (M) 2L72 4F RTA6WE 20051108001742005110800174SO 2005 11 8 SIMA200527711 120050926A532013500224001 DOUBLER EMB 135 EMB135LR 3260305SO FR 22 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21716AE 145264 FOUND TRIANGULAR DOUBLER PLATE THAT ATTACHES FLOOR SUPPORT AT FRAME 22 CORRODED. FABRICATED AND INSTALLED NEW DOUBLER IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20051108001802005110800180EA 2005 11 8 ASOA05861 120051012A5220H341933 HANDLE CNDAIRCL600 CL6002B19 1900309EA ESCAPE HATCH CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27836AS 7263 DURING A C-CHECK IN MCN, THE CREW ESCAPE HATCH HANDLE WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CREW ESCAPE HATCH HANDLE IAW CRJ200 MM 52-22-03. (M) 2L72 4F RTA21EA 20051108001812005110800181EU 2005 11 8 ASOA05860 120051011A33503011210 LIGHT AEROSPATR72 ATR72212 8680945EU PAX DOOR INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27631AS6283 362 DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ON THE PASSENGER DOOR OPERATIONAL CHECKS GOOD. (M) 2H72 4T RTA53EU 20051108001852005110800185EU 2005 11 8 ASOA05910 120051012A5320 ANGLE AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27641AS 387 DURING A C-CHECK IN YUL, THE ANGLE BETWEEN THE TAIL BUMPER BOX AND FS 39 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE ANGLE BETWEEN THE TAIL BUMPER BOX AND FS 39 IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20051108001892005110800189SO 2005 11 8 SIMA200527701 120050928A5320 SILL EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21832AE 145627 THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED THE EXISTING SILL AND INSTALLED SERVICEABLE SILL. REPAIR DONE IAW EMB 135 SRM, SRM EMB-145/1142 REV 30, CHAPTERS 51-40-02 AND 51-20-03. (M) 2L72 4F RTT00011AT 20051108001902005110800190WP 2005 11 8 GTIA050258 120050921A5415 ATTACH ANGLE DOUG DC9 DC983 3022083WP RT PYLON CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23808NK 49504 FTW - RIGHT PYLON T/E ATTACHED ANGLE IS CRACKED APPROX 16 INCHES FROM T/E ROOT. REMOVED DAMAGE AREA. FABRICATED REPAIR. TREATED, PRIMED AND INSTALLED REPAIR ANGLE. (M) 2L72 4F RTA6WE 20051108001912005110800191WP 2005 11 8 GTIA050241 120050826A5320 CUSP WEB DOUG DC9 DC983 3022083WP BS 622 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23834NK 49847 FTW - FOUND CORROSION INSIDE CABIN AT CUSP LINE, WEB STATION 622, L18L. REMOVED CORROSION INSIDE CABIN AT WEB STATION 622, L18L. FABRICATED REPAIR DOUBLER AND FILLER. TREATED, PRIMED AND INSTALLED REPAIR DOUBLER AND FILLER. (M) 2L72 4F RTA6WE 20051108001952005110800195WP 2005 11 8 GTIA050225 120050714A5320 INTERCOSTAL DOUG DC9 DC983 3022083WP BS 1497 BENT A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 FTW - AFT ACCESSORY COMPARTMENT BETWEEN STATION 1497 CANT TO STATION 1510 CANT ABOUT 4 O`CLOCK POSITION INTERCOSTAL BENT. FURTHER INSPECTION, INTERCOSTAL WAS FOUND TO HAVE A CRACK IN THE RADIUS MATERIAL. TRIMMED OUT CRACKED AREA. FABRICATED REPAIR ANGLE AND FILLER. TREAT, PRIMED AND INSTALLED REPAIRED ANGLE AND FILLER. (M) 2L72 4F RTA6WE 20051108001962005110800196WP 2005 11 8 GTIA050224 120050726A5260 SKIN DOUG DC9 DC983 3022083WP AIRSTAIR DOOR DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 DENT AT AFT AIRSTAIR DOOR 74 INCHES FROM FORWARD EDGE. STRIPPED PAIN AND MEASURED DENT AREA. FOUND IS OUT OF LIMITS. CUT OUT 2 INCHES AT DAMAGED AREA. FABRICATED REPAIR DOUBLER AND FILLER. TREATED, PRIMED AND INSTALLED REPAIRED PARTS. (M) 2L72 4F RTA6WE 20051108002012005110800201SO 2005 11 8 SIMA200527704 120050928A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO FS 20 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21820AE 145576 THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. PERFORMED A CUT OUT TO REMOVE THE CORROSION. PREPARED DOUBLER, FILLER AND SHIMS FOR THE REPAIR. REPAIR DONE IAW EMB 145 SRM, SRM EMB-145/1142 REV 30, CHAPTER 53-00-10 FIG 201. (M) 2L72 4F RTT00011AT 20051108002032005110800203WP 2005 11 8 GTIA050233 120050723A4910 DOOR DOUG DC9 DC983 3022083WP APU BAY CHAFED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23831NK 49617 RIGHT APU COMPARTMENT DOOR, LOWER EDGE IS CHAFED ALONG WITH MATING SURFACES. BLENDED APU LOWER RIGHT DOOR EDGE AND FOUND IS OUT OF LIMITS. FABRICATED REPAIR DOUBLER. TREATED, PRIMED AND INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20051108002052005110800205WP 2005 11 8 GTIA050238 120050826A2150 ACM DOUG DC9 DC982 3022082WP LEFT LEAKING A GTIAK NONE K FLUID LOSS ININSP/MAINT 1 GL23804NK 49104 DTW - SMOKE DETECTOR AFT LEFT ON, SOME HOT ELECT CHEMICAL SMELL AFT END OF AIRCRAFT, SMELL CAME BACK AFTER LANDING, AIR RETURN BACK TO DTW, AIRCRAFT TAIL SWAP WITH N810NK. REMOVED AND REPLACED AFT LEFT LAV SMOKE DETECTOR WITH UPDATED P/N FOR PRECAUTION. REMOVED BOTH WATER SEPARATORS AND INSTALLED NEW COALESCER BAGS. FOUND NO CONTAMINATION. REMOVED AND INSPECTED INLET AND OUTLET DUCTS ON BOTH ACM`S. NO CONTAMINATED NOTED. LEFT ACM LEAKING WATER. FOUND FLANGE RETAINING BOLTS LOOSE, SECURED. RIGHT ACM INLET HAS TORN HOSE. REMOVED AND REPLACED CONNECTOR, LEAK CHECKS GOOD. (M) 2L72 4F A6WE 20051108002252005110800225EU 2005 11 8 ASOA05827 120050830A5315 FLOORBEAM AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27637AS 383 DURING A C-CHECK IN YUL, THE FLOORBEAMS AT FRAME 36, FRAME 38, FRAME 39, FRAME 40 AND FRAME 41 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAMS AT FRAME 36, FRAME 38, FRAME 39, FRAME 40 AND FRAME 41 IAW ASA EO 72-53-0166A. (M) 2H72 4T RTA53EU 20051108002272005110800227WP 2005 11 8 GTIA050251 120050912A5315 FLOORBEAM DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 FOUND FLOORBEAM JUST INSIDE R-1 DOOR CORRODED, INSIDE CHANNEL. REMOVED AND REPLACED FLOORBEAM INSIDE R-1 DOOR. (M) 2L72 4F RTA6WE 20051108002442005110800244EA 2005 11 8 ASOA05862 120051012A5347601R3877949 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA BS 559 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27836AS 7263 DURING A C-CHECK IN MCN, THE CARGO COMPARTMENT FORWARD BULKHEAD SEAT TRACK AT FS 559 PLUS 112, RBL 9 AND RBL 27 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CARGO COMPARTMENT FORWARD BULKHEAD SEAT TRACK AT FS 559 PLUS 112, RBL 9 AND RBL 27 IAW CRJ200 AMM 53-00-11. (M) 2L72 4F RTA21EA 20051108002482005110800248EA 2005 11 8 ASOA05884 120051018A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 785-797 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27712EV 10074 DURING A C-CHECK IN MCN, THE LEFT SEAT TRACK, AT S 785 TO FS 797, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACED THE LEFT SEAT TRACK, AT FS 785 TO 797. (M) 2L72 4F RTA21EA 20051108002532005110800253EA 2005 11 8 ASOA05848 120051007A32347179015 HANDLE CNDAIRCL600 CL6002B19 1900309EA MLG INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27852AS 7369 DURING CLIMB-OUT FROM ATL-BHM, THE CREW RECEIVED A NOSE GEAR DISAGREE MESSAGE ON THE EICAS. THE NOSE DOOR WAS OPEN AND THE NOSE GEAR REMAINED IN THE LOCKED POSITION. THE AIRCRAFT RETURNED TO ATL AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE GEAR HANDLE BOX. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051108002642005110800264EA 2005 11 8 ASOA05807 120050925A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27871AS 7537 FLT 4861 - DURING HANGAR MAINTENANCE IN BTR, THE FORWARD EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE FORWARD EMERGENCY CEILING LIGHT. OPERATIONAL CHECKS GOOD. (M) 2L72 4F RTA21EA 20051108002692005110800269EA 2005 11 8 ASOA05889 120051020A335020131A BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27882AS 7503 DURING A GROUND INSPECTION IN ATL, THE NR 1 BATTERY PACK FOR THE FORWARD EMERGENCY LIGHTS WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 BATTERY PACK FOR THE FORWARD EMERGENCY LIGHTS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051108002772005110800277EA 2005 11 8 SIMA200526903 120050923A2720DL2428M9 ACTUATOR CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE RUDDER FAILED A SIMAO OTHER F FLT CONT AFFECTED CRCRUISE 1 SW21502AE 10018 RUDDER LIMITER MESSAGE DURING FLIGHT. REPLACED THE LT TRAVEL LIMITER ACTUATOR IAW AMM. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (K) 2L72 4F4 FRTA21EA EOOO63EN 20051108002782005110800278SO 2005 11 8 SIMA200529312 120051016A57413631001013 CONTROL UNIT EMB 135 EMB135LR 3260305SO ALLSN AE3007AE3007C GL AVIONICS BAY INOPERATIVE A SIMAO OTHER O OTHER NRNOT REPORTED 1 SW21701MH 145162 DURING GEAR EXTENTION OBSERVED MOMENTARY EICAS MESSAGE MAIN PITCH TRIM FAIL AND BACKUP PITCH TRIM FAIL. WARNING WENT OUT AFTER GEAR EXTENDED. TROUBLESHOT SYSTEM REPLACED HORIZONTAL STABILIZER UNIT. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (K) 2L72 4F4 FRTT00011ATTE6CH 20051108002842005110800284 2005 11 8 S2YA05058 420050916A34226226136002 GYRO BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE LT DIRECTIONAL INOPERATIVE A S2YAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL1381SK 24198988 UE81 DURING FLIGHT, THE CREW REPORTED THE (D) DISCHARGE LIGHT ON THE RT PUSH TO DISCHARGE FIRE EXTINGUISHER BUTTON WAS INTERMITTENTLY ILLUMINATING. ALSO THE CREW REPORTED CAPTAIN`S DIRECTIONAL GYRO (DG) WAS INOP IN ALL MODES. THE CREW PERFORMED AN AIR-TURN-BACK. MAINTENANCE FOUND A BROKEN TERMINAL END AT THE RT SQUIB. MAINTENANCE REPLACED THE TERMINAL END. MAINTENANCE REPLACED THE CAPTAIN`S DG AND WITH NO FURTHER DEFECTS RETURNED THE AC TO SERVICE. (K) 2L72 4T4 TRTA24CE E26NE 20051108002952005110800295EU 2005 11 8 KBM2005F00265 120050908A3320704A46814049 POTENTIOMETER SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE CABIN LIGHTS INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV 3296 DIMMER BOX, LIGHT WORKS, NR 1 DOESN`T DIM, NR 2 DOES DIM. (K) 1G71 3U3 U H9EU E19EU 20051108003292005110800329NM 2005 11 8 USAA051345 120051107A5320 INTERCOSTAL BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19779AU 24996 NUMEROUS CLIP NUT HOLES BETWEEN 294.5 AND 312 RBL 10. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-40-02. DEFECT SIZE: .250 INCH. 2L72 4F RTA16WE 20051108003302005110800330WP 2005 11 8 I5HA0558008 120051001A32303408500010101 ARM CVAC 340 34031 2422704WP ALLSN 501D 501D13 03004GL MLG BROKEN A A6WAO OTHER O OTHER NRNOT REPORTED 1 GL31581P 29 ENROUTE, CREW OBSERVED A (LANDING GEAR UNSAFE UP) INDICATION ON THE ANNUNCIATOR PANEL. THE LANDING GEAR WAS PLACED DOWN WITH ALL 3 LANDING GEAR INDICATING DOWN AND LOCKED. AC LANDED SAFELY. INSP OF RT LANDING GEAR BY THE OB MECHANIC REVEALED A BROKEN MLG ARM ASSY. ACTUATOR AND ARM ASSY WERE REMOVED AND THE HYDRAULIC LINES SECURED. AC FERRIED BACK WITH LANDING GEAR DOWN AND PINNED. MLG ACTUATOR AND MLG ARM WERE REPLACED WITH SERVICEABLE UNITS AND AC WAS RETURNED TO SERVICE. (K) 2L72 4R4 T 6A6 E282 20051108003312005110800331EU 2005 11 8 KBM2005F00258 120050916A3110704A47270101 GAUGE SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE CLUSTER INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P 2347 CLUSTER GAUGE, UNIT INOPERATIVE, REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20051108003332005110800333NM 2005 11 8 USAA051343 120051107A5320 BEAM BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19779AU 24996 BEAM 312 LEVEL 1 CORROSION. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS, IAW SRM 53-10-51 REPAIR 5. DEFECT SIZE: 5 INCHES. 2L72 4F RTA16WE 20051108003362005110800336NM 2005 11 8 USAA051341 120051107A5753 SKIN BOEING737 7373B7 1384580NM T/E FLAP GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 WEDGE SKIN 13.5 INCH FROM THE OUTBOARD END GOUGED. REMOVED SKIN AND DAMAGED CORE, INSTALLED CORE, FILLER AND DOUBLER IAW SRM 57-50-15 REV A. DEFECT SIZE: 4.3 X .5 INCH. 2L72 4F RTA16WE 20051108003382005110800338GL 2005 11 8 ALG2005F00078 220051006A732123078032 HMU BELL 407 407 1182206SW ALLSN 250C 250C47B GL ENGINE FAILED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03796RV 53037 DURING HOVER, RESTART LIGHT CAME ON, FOLLOWED BY THE DEGRADE LIGHT. REMOVED AND REPLACED HMU WITH SERVICEABLE UNIT. IAW MM. (K) 1G71 3U3 UO H2SW E1GL 20051108003392005110800339SO 2005 11 8 SIMA200528001 120050926A532014590071401 SILL EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL CABIN CORRODED A SIMAO OTHER O OTHER NRNOT REPORTED 1 SW21716AE 145264 FOUND SERVICE DOOR AFT SILL CORRODED AT FRAME 22. REPAIRED AFT SILL WITH DOUBLER REPAIR IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200600332) (K) 2L72 4F4 FRTT00011ATTE6CH 20051108003402005110800340NM 2005 11 8 USAA051340 120051107A554265C2584151 SKIN BOEING737 7373B7 1384580NM RUDDER DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 LEFT RUDDER SKIN 99 INCHES FROM THE BASE AND 19 INCHES IN FROM THE TRAILING EDGE DELAMINATED. REMOVED DAMAGE, LAID UP AND INSTALLED REPAIR IAW SRM 55-40-01. DEFECT SIZE: 6 INCHES. 2L72 4F RTA16WE 20051108003412005110800341SO 2005 11 8 B7T2005F00003 220050706A8530AEC631397 CYLINDER HEAD CESSNA207 207 2073602CE CONT O520 IO520F 17032SO HARTZLHCC3Y HCC3YF1 GL NR 5 CRACKED E B7TAO OTHER O OTHER NRNOT REPORTED 1 AL0391002 596 20700003 564011 EE2069A CYLINDER CRACKED UNDER UPPER SPARK PLUG HOLE ACROSS ENTIRE WIDTH OF CYLINDER AREA UNDER SPARK PLUG. LEAKING AIR. (K) 1H71 3O3 O A16CE E5CE 5 CP25EA 20051108003482005110800348NM 2005 11 8 USAA051337 120051107A5320 ANGLE BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19779AU 24996 AFT CARGO FLOOR LT ZEE ANGLE FUSELAGE STATION 727D TO 747 LEVEL 1 CORROSION. REMOVED DAMAGED ANGLE AND INSTALLED A NEW ANGLE IAW SRM 51-10-02. DEFECT SIZE: 18 X .75 INCHES. 2L72 4F RTA16WE 20051108003512005110800351NM 2005 11 8 AWXA200501340 120051018A5755654645170 SKIN BOEING737 7373G7 1384595NM NR 6 SPOILER CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED THE NR 6 SPOILER ON UPPER SURFACE BULGING WITH CRACK, .5 INCHES LONG, WS 228R. MAINTENANCE REMOVED SPOILER AND REMOVED DAMAGE IAW BOEING 737-300 SRM 57-70-01-2R4 FIG 201. FABRICATED AND INSTALLED DOUBLER ON THE NR 6 SPOILER UPPER SURFACE IAW BOEING 737-300 SRM 57-70-01-2R4 FIG 201. RE-INSTALLED SPOILER IAW BOEING 737-300 SRM 57-70-01-2R4 FIG 201. 2L72 4F RTA16WE 20051108003522005110800352NM 2005 11 8 AWXA200501341 120050907A57536546435277 SKIN BOEING737 73733A 1384673NM T/E FLAP DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW 23634 GYR - MAJOR REPAIR - DURING C20 CHECK DISCOVERED DELAMINATED AREA ON THE LT OUTBOARD AFT FLAP, UPPER SKIN AT WBL 244.40. MAINTENANCE REMOVED DAMAGED SKIN AND CORE FROM LT OUTBOARD AFT FLAP IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED CORE AND DOUBLER IAW BOEING 737-300 SRM 51-70-10-2R. BONDED REPAIR PARTS TO THE UPPER SURFACE OF THE LT OUTBOARD AFT FLAP IAW BOEING 737-300 SRM 51-70-10-2R4. 2L72 4F RTA16WE 20051108003532005110800353SO 2005 11 8 RAIA00511006 120051105A33501317 LIGHT EMB 145 EMB145LR 3260212SO CABIN BURNED OUT A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03825HK 145510 MX - STL - ONE EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED BULB. 2L72 4T RTT00011AT 20051108003592005110800359EU 2005 11 8 2005UALA01205 120051029A3350321430 BATTERY PACK AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CABIN FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29424UA 506 EMERGENCY LIGHT TEST FAILS RT EPSU. REPLACED BATTERY PACK AT 12WL. 2L72 4F4 FRTA28NM E40NE 20051108003612005110800361NM 2005 11 8 2005UALA01207 120051029A33501317 LIGHT BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU CABIN BURNED OUT A UALAK NONE L NO TEST ININSP/MAINT 1 WP29318UA 23950 EMERGENCY AISLE LIGHT INOP AT ROW 21. RELAMPED WITH NR 1317 LAMP. 2L72 4F4 FRTA16WE E21EU 20051108003622005110800362NM 2005 11 8 2005UALA01208 120051028A335078941 LIGHT BOEING777 777222 1385219NM PWA PW4077PW4077 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29768UA 26919 SEAT 1E EMERGENCY PROX LIGHT INOP. REPLACED FOWARD EEL LIGHT AT 1E. 2L72 4F4 FRTT0001SE E46NE 20051108003632005110800363NM 2005 11 8 2005UALA01209 120051030A2421 GENERATOR BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU NR 2 MALFUNCTIONED A UALAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC NRNOT REPORTED 1 WP29374UA 24639 LOST NR 2 GENERATOR AND THEN RECEIVED A NR 2 ENGINE OVERHEAT MESSAGE. LOSS OF GENERATOR CAUSED BY APPARENT CSD FAILURE. GENERATOR, CSD, AND CSD OIL COOLER WERE REPLACED. GENERATOR RECEIVED ROUTINE SHOP MAINTENANCE, BUT HAD NOT FAILED. CSD AND CSD OILER COOLER HAVE NOT BEEN WORKED BY THE SHOP AS OF 11/21/05, THUS NO FINDINGS AVAILABLE AT THIS TIME. THE AIRCRAFT HAS HAD NO REPEAT INCIDENTS. 2L72 4F4 FRTA16WE E21EU 20051108003642005110800364NM 2005 11 8 2005UALA01210 120051101A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29198UA 28716 EMERGENCY EEL LIGHT INOP AT SEAT 61 RIGHT AISLE. SECURED UNDERSEAT CONNECTOR. 2L74 4F4 FRTA20WE E24NE 20051108003652005110800365NM 2005 11 8 2005UALA01211 120051101A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29198UA 28716 EMERGENCY EEL LIGHT INOP AT AFT GALLEY RIGHT SIDE WALL. REPLACED FEEDER CABLE. 2L74 4F4 FRTA20WE E24NE 20051108003692005110800369NM 2005 11 8 2005UALA01214 120051021A5754114N300334 WEDGE BOEING 114N3002120ABOEING757 757222 1384956NM PWA 2037 PW2037 NE L/E SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29572UA A20593 26682 T/E WEDGE DELAMINATED. WEDGE REPLACED. 2L72 4F4 FRTA2NM E17NE 20051108003702005110800370NM 2005 11 8 2005UALA01215 120051028A335020131A POWER SUPPLY BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN ACTIVATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29520UA 24890 THE FOLLOWING EMERGENCY LIGHTS ARE INOP: EXTERIOR, LEFT FWD OVERWING, DOOR 4L. INTERIOR, EXIT SIGN OVER DOOR 4L, EXIT MARKERS AT DOORS 4L & 4R, OVERHEAD EXIT SIGN IN AFT GALLEY, AISLE LIGHTS AT ROWS 29 & 32. LEFT AFT HATCH ILLUMINATION LIGHTS, AFT LIGHT IN RIGHT FWD HATCH ILLUMINATION. REPLACED M10818 POWER SUPPLY. 2L72 4F4 FRTA2NM E17NE 20051108003732005110800373NM 2005 11 8 2005UALA01218 120051031A3897 WIRE BOEING757 757222 1384956NM PWA 2037 PW2037 NE WATER SYSTEM BURNED A UALAK NONE O OTHER ININSP/MAINT 1 WP29540UA 25252 FOUND C/B'S FOR WATER HEATERS & DRAIN MAST POPPED. FOUND BURNED WIRES. WIRES BURNED THRU AT STA 1681 , WL 208 DUE TO CHAFE THRU BY HOSE BAND CLAMP FROM IMPROPERLY ROUTED WIRES AND VENT HOSES WHICH LED TO ARCING AND BURN-THRU OF WIRES. BOEING NOTIFIED, AND NO PREVIOUS OCCURANCES WERE NOTED. STRICTLY DUE TO IMPROPER ROUTING OF VENT HOSES AND WIRING BUNDLE WITH IMPROPER STAND-OFFS, AS VERIFIED IN IPC 38-31-56-004, FIG G. 3 OTHER AIRCRAFT INSPECTED FOR PROPER ROUTING, AND WERE IN ACCORDANCE WITH IPC. 2L72 4F4 FRTA2NM E17NE 20051108003742005110800374EU 2005 11 8 2005UALA01219 120051102A2421 GENERATOR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 2 MALFUNCTIONED A UALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP29411UA 464 F/A REPORTS INTERMITTENT BURNING SMELL AT ROW 15, SMELLS LIKE BURNT RUBBER. CREW SHUT DOWN & SECURED GEN 2. NR 2 ENG IDG PYLON CONNECTOR FOUND WITH EVIDENCE OF FRETTING, ARCING AND BLACK SOCKETS WITH SOME PITTING. NR 2 ENG IDG HARNESS REPLACED. 2L72 4F4 FRTA28NM E40NE 20051108003752005110800375NM 2005 11 8 2005UALA01220 120051103A3510MF20003 OXYGEN MASK BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE COCKPIT LEAKING A UALAA UNSCHED LANDING O OTHER CLCLIMB 1 WP29228UA14662 30556 CREW OXYGEN WAS LEAKING. REPLACED SECOND OBSERVER'S FULL FACE MASK. THIS MASK WAS ORIGINALLY INSTALLED IN THE CAPT'S POSITION AND THEN SWAPPED. OXYGEN LEAK FOLLOWED AFTER SWAP. NO NEW WRITE UPS FOR OXYGEN AFTER THE MASK WAS REPLACED. 2L72 4F4 FRTT0001SE E46NE 20051108003782005110800378NM 2005 11 8 2005UALA01223 120051103A5754 SKIN BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE L/E SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29787UA 26939 NR 2 SLAT LWR SURFACE DELAMINATED AT INBOARD END 3 INCHES FROM THE TRAILING EDGE. INTERIM REPAIR PER 777 AMM 57-43-99. ACP AN INITIAL INSP AT 50 CYCLE AND EVERY 500 FLT CYCLE UNTIL PERMANENT REPAIR ACPL AT NEXT HMV (5JUNE06). OK TO CF PER AMM AND SFOIQ WALSH. 2L72 4F4 FRTT0001SE E46NE 20051108003802005110800380NM 2005 11 8 2005UALA01225 120051104A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29171UA 24322 EMERGENCY LIGHTS OUT IN ROWS 55, 56, 57 & 58 SEATS ABC. REPAIRED FEEDER CABLE. 2L74 4F4 FRTA20WE E24NE 20051108003822005110800382EU 2005 11 8 2005UALA01227 120051103A3350 LIGHT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CABIN BURNED OUT A UALAK NONE L NO TEST ININSP/MAINT 1 WP29421UA 500 ONE LIGHT OF THE EMERGENCY LIGHTING PATH IS BURNED OUT ROW 15. 2L72 4F4 FRTA28NM E40NE 20051108003832005110800383NE 2005 11 8 EIA2005152 220050823A7530 CONTROLLER BOEING747 747212B 1384886NM PWA JT9 JT9D7J 52054NE NR 3 ENGINE MALFUNCTIONED A EIAAE ENGINE SHUTDOWN O OTHER DEDESCENT 1 NM09486EV 20888 662551 NR 3 ENGINE ON DESCENT FL 350 WOULD NOT RESPOND TO PUSH-UP. RESTART REQUIRED ALL PAREMETERS WERE NORMAL RESTART OK. NR 3 EVC REPLACED AND TRIMMED PER MMS 71-00-00 AND 75-31-01 RESPONCE NORMAL. 2L74 4F4 F A20WE E20EA 20051108003842005110800384NM 2005 11 8 EIA2005153 120050719A3350276005 FUSE MARATHON BOEING747 747100 1384825NM BATTERY PACK BLOWN A EIAAK NONE L NO TEST ININSP/MAINT 1 NM09478EV 21033 DOOR EMERGENCY EXIT LIGHT BY THE UPPER DECK ESCAPE SLIDE INOP. REPLACED FUSE IN BATTERY PACK. 2L74 4F RTA20WE 20051108003852005110800385NM 2005 11 8 EIA2005160 120050925A5755 HINGE FITTING BOEING747 747212B 1384886NM NR 7 SPOILER FAILED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 NR 7 SPOILER HINGE FITTING FAILED CAUSED DAMAGE TO NR 7 SPOILER AND LEADING EDGE OF INBOARD FORE FLAP. ACCOMPLISHED ECRA 486-57-046-1 BEFORE FLIGHT. REPLACED NR 7 SPOILER PANEL, REWORKED HINGE AND REPAIRED FLAP AS PER INSTRUCTIONS OF ECRA PART 1. 2L74 4F A20WE 20051108003862005110800386NM 2005 11 8 EIA2005161 120050929A3300 BATTERY BOEING747 747273C 1384896NM CABIN DISCHARGED A EIAAK NONE L NO TEST ININSP/MAINT 1 NM09470EV 20653 M/D RIGHT STA 2180 1EA EMERGENCY LIGHT INOP. RECHARGED LIGHT BATTERY AND OPS CHECKED GOOD PER B747 MM 33-51-00. 2L74 4F A20WE 20051108003872005110800387NM 2005 11 8 EIA2005162 120050930A3350 COVER BOEING747 747273C 1384896NM CABIN MISSING A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 R5 DOOR SILL EMERGENCY LIGHT 2 EA COVERS MISSING. REPLACED 2 EA COVERS AND OPS CHECKED GOOD PER B747 MM 33-51-00. 2L74 4F A20WE 20051108003892005110800389NM 2005 11 8 EIA2005164 120050927A3300 BATTERY BOEING747 747273C 1384896NM CABIN DISCHARGED A EIAAK NONE L NO TEST ININSP/MAINT 1 NM09470EV 20653 R5 DOOR EMERGENCY LIGHT INOP. RECHARGED BATTERY AND OPS CHECKED PER B747 MM 33-51-50. 2L74 4F A20WE 20051108003902005110800390NM 2005 11 8 EIA2005165 120050928A3350 LIGHT BOEING747 747273C 1384896NM CABIN INOPERATIVE A EIAAK NONE L NO TEST ININSP/MAINT 1 NM09470EV 20653 L5 DOOR SILL EMERGENCY LIGHT INOP. REPLACED BULB AND OPS CHECKED GOOD PER B747 MM 33-51-50. 2L74 4F A20WE 20051108003912005110800391NM 2005 11 8 EIA2005166 120051010A5414 SKIN BOEING747 747212B 1384886NM NR 4 PYLON CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 NUMBER 4 PYLON SKIN CRACKED AT ACCESS PANEL 483CL CUTOUT HINGE ATTACH FASTENER HOLE. NUMBER 4 PYLON 483CL ACCESS PANEL CUTOUT SKIN REPAIR CARRIED OUT IAW SRM 54-30-03 FIG 17B. 2L74 4F A20WE 20051108003932005110800393NM 2005 11 8 EIA2005168 120051010A5414 SKIN BOEING747 747212B 1384886NM NR 2 PYLON CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 NR 2 PYLON 463EL ACCESS PANEL CUTOUT SKIN CRACKED ON THE STRIKER PAD TWO FASTENER HOLES. NR 2 PYLON 463EL ACCESS PANEL CUT OUT SKIN REPAIR CARRIED OUT IAW SRM 54-30-03 FIG 7B. 2L74 4F A20WE 20051108003952005110800395NM 2005 11 8 EIA2005170 120051011A5315 FLOORBEAM BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 BS 380 FLOORBEAM UPPER CHORD HORIZONTAL AFT FLANGE LBL 55 FLOOR PANEL ATT HOLE CRACKED RUNNING FWD APPROX .125 INCH AND AFT APPROX .0625 INCH LONG. DEFECTIVE FLOORBEAM UPPER CHORD REPAIRED AS PER SB 747-53A2431 FIG 9 (HORIZONTAL AFT FLANGE LBL 55). 2L74 4F A20WE 20051108003962005110800396EU 2005 11 8 2005UALA01228 120051104A3350 BATTERY AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CABIN MALFUNCTIONED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29421UA 500 EPSU COMM FWD LT MESSAGE DURING EMERGENCY BATTERY SYS TEST. REPLACED BATTERY PACK AT DOOR 1 LEFT, 2L72 4F4 FRTA28NM E40NE 20051108003972005110800397NM 2005 11 8 EIA2005171 120051011A5315 FLOORBEAM BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 BS 360 FLOORBEAM UPPER CHORD HORIZONAL AFT FLANGE LBL 45 FLOOR PANEL AFT HOLE CRACKED RUNNING FWD APPROX .125 INCH AND AFT APPROX .125 INCH LONG. DEFECTIVE FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 53-10-07 FIG 9 (HORIZONTAL AFT FLANGE LBL 43). 2L74 4F A20WE 20051109000032005110900003NE 2005 11 9 KBM2005F00331 220051031A72109560137520 MAGNETIC SEAL SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1B 6OO30NE LEAKING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH1145 2337 MAGNETIC SEAL, UNIT HAS LEAKS, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051109000042005110900004 2005 11 9 KBM2005F00325 420051027A2562 G SWITCH SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE ELT INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19115SH 62328 3141 G-SWITCH WILL NOT ACTIVATE, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051109000122005110900012CE 2005 11 9 OEJ2005F00000 120051025A3210 LANDING GEAR CESSNA421 421B 2076014CE CONT O520 GTSIO520* 17032SO LT MLG FAILED E OEJAO OTHER O OTHER TXTAXI/GRND HDL 1 SW15968J 5611 421B0012 21049872H AFTER LANDING, DURING ROLL OUT THE LT MLG FOLDED UP. BEFORE LANDING, ON FINAL APPROACH. THE GEAR WAS VERIFIED BY BOTH PILOTS THAT THE GEAR WAS DOWN AND LOCK WITH ALL GREEN LIGHTS AND ALL SYSTEMS NORMAL. AT THIS TIME NO VERIFICATION ON WHY THIS INCIDENT OCCURED. THIS WAS PART91 FLIGHT WITH ONLY 2 PILOTS ON BOARD. (SW15200606368) (K) 1L72 3O3 O A7CE E7CE 20051109000132005110900013SO 2005 11 9 N382005F00005 120051012A32311EN616 UPLOCK SWITCH GULSTMG1159 G1159 3953505SO RROYCESPEY SPEY511* 54523EU LT MLG DOOR DISCONNECTED E N38AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA05510SR 070 ON TAKEOFF WITH GEAR UP, THE GEAR HANDLE LIGHT WAS ON. PRELIMINARY TROUBLESHOOTING DETERMINED THAT THE LT MAIN GEAR DOOR UP SWITCH WAS AT FAULT. WHEN REPLACING SWITCH, FOUND A LOOSE WIRE AT A BUTT SPLICE. (K) 2L72 4F4 FRTA12EA E2EU 20051109000142005110900014CE 2005 11 9 O2G2005F00012 120051021A3260 SQUAT SWITCH CESSNA500 560CESSNA 2076750CE PWA 530 PW535A NE MLG FAILED E O2GAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NE0323YZ 5600638 AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT TO UP POSITION. AIRCRAFT DIVERTED. CHANGED RT MAIN GEAR SQUAT SWITCH. (K) (NE03200604804) 2L72 4F4 FRTA22CE E00053EN 20051109000152005110900015NE 2005 11 9 GAIA05023 220050908A7200 ENGINE BOEING727 727223 1384074NM PWA JT8 JT8D9 52048NE NR 2 FAILED A GAIAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 SW076827 590183405 20180 DURING CRUISE, NR 2 ENGINE LOW OIL PRESSURE LIGHT CAME ON BRIGHT, NOTICED NR 2 OIL PRESSURE DROPPED RAPIDLY TO ZERO. OIL TEMPS AND QUANTITY REMAINED NORMAL. ENGINE FAILURE CHECKLIST WAS PERFORMED. N1S WIND MILLED FOR APPROXIMATELY 25 MINUTES. EMERGENCY WAS DECLARED. FLIGHT DIVERTED, WHERE LANDING WAS MADE WITHOUT INCIDENT. ENGINE REMOVED AND REPLACED. (K) 2L73 4F4 F A3WE E2EA 20051109000162005110900016NM 2005 11 9 S2YA05060 120050925A2810 PROBE DORNERDO32 DO328300 NM PWA 306 PW306B NE FUEL TANK UNCALIBRATED A S2YAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL13357SK 3164 DURING FLIGHT, THE CREW REPORTED LT FEEDER TANK LOW ANNUCIATOR. MAINT REQUESTED THE AIRCRAFT TO PERFORM AN AIR-TURN-BACK. THE AC WAS INSPECTED AND THE FEEDER TANK PROBE WAS RECALIBRATED. WITH OPERATIONAL CHECKS GOOD THE AC WAS RETURNED TO SERVICE. (K) 2H72 4T4 FRTA55NM E35NE 20051109000172005110900017NM 2005 11 9 S2YA05059 120050922A24348160121 GENERATOR DORNERDO32 DO328300 NM PWA 306 PW306B NE LT DC GENERATOR INOPERATIVE A S2YAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL13356SK6609 598 3163 SHORTLY AFTER DEPARTURE OF FLIGHT, THE LT GENERATOR FAILED. SEVERAL ATTEMPTS TO RESET THE GENERATOR WHERE UNSUCCESSFUL. THE CREW PERFORMED AN AIR-TURN-BACK. MAINTENANCE REPLACED THE LT DC GENERATOR AND WITH OPERATIONAL CHECK GOOD THE AC WAS RETURNED TO SERVICE. (K) 2H72 4T4 FRTA55NM E35NE 20051109000232005110900023NE 2005 11 9 ALG2005F00077 120051005A771423007981A PICKUP SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL N2 DUAL COIL RPMFAILED E ALGAA UNSCHED LANDING P NO WARNING INDICATION CRCRUISE 1 SW031547N 760088 DURING CRUISE FLIGHT, N2 INDICATOR WENT FROM 100 PERCENT TO ZERO. REMOVED AND REPLACED N2 PICKUP, NR 2 ENGINE WITH SERVICEABLE UNIT IAW MM. GROUND RUN AND OPS CHECK GOOD. (K) 1G72 3U3 U H1NE E1GL 20051109000272005110900027NM 2005 11 9 S2YA05055 120050905A31107014300902 DISPLAY DORNERDO32 DO328300 NM PWA 306 PW306B NE NR 2 INOPERATIVE A S2YAA UNSCHED LANDING O OTHER CRCRUISE 1 GL13355SK13133 3124 DURING FLIGHT, THE CREW REPORTED THE NR 2 DISPLAY UNIT WENT BLANK. AFTER SEVERAL ATTEMPTS AT CYCLING THE CIRCUIT BREAKER, THE CREW PERFORMED AND AIR-TURN-BACK. MAINTENANCE REPLACED NR 2 DU. OPS CHECKS GOOD THE AC WAS RETURNED TO SERVICE. (K) 2H72 4T4 FRTA55NM E35NE 20051109000282005110900028EU 2005 11 9 KBM2005F00262 120050916A6520350A33215300 BEARING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1B 6OO30NE TAIL ROTOR CUT E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH464 2337 LAMINATED BEARING, UNIT HAS CUTS AROUND THE RUBBER, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051109000292005110900029NE 2005 11 9 KBM2005F00263 220050906A74219550175400 IGNITER SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE ENGINE ERODED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19250SH 3874 RT IGNITER SEMI-CONDUCTOR ON TIP IS SEVERELY ERODED AND CENTER ELECTRODE TIP IS UNEVEN POINTED WEAR. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051109000312005110900031EU 2005 11 9 KBM2005F00259 120050910A2435150SG122Q STARTER GEN SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1 60030NE ENGINE INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19215LA1227 2143 STARTER GEN - UNIT WILL NOT COME ON LINE, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051109000322005110900032EU 2005 11 9 KBM2005F00266 120050912A28406475100302 PROBE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE FUEL SYSTEM READS LOW E KBMAO OTHER N FALSE WARNING NRNOT REPORTED 1 WP19351WM155 2167 FUEL PROBE, UNIT READING LOW (13 PERCENT), REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051109000332005110900033 2005 11 9 KBM2005F00268 420050914A3452066106200 TRANSPONDER SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE ATC INOPERATIVE E KBMAO OTHER N FALSE WARNING NRNOT REPORTED 1 WP19351WM5 2167 TRANSPONDER, ATC REPORTED NO MODE C AND AN INCORRECT CODE IN THE TRANSPONDER., REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051109000342005110900034EU 2005 11 9 KBM2005F00272 120050909A2121420800001 BLOWER SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19751H 3403 BLOWER ASSY, INOPERATIVE, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051109000352005110900035NM 2005 11 9 AMTA200500719 120050922A2697644501 CIRCUIT CARD BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE RT FIRE LOOP UNSERVICEABLE A AMTAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL11519AT 27975 (R ENG FIRE LP 2) DISPLAYED. CAME ON 1 HR AFTER ALL 4 LOOP CHANGES. AS PER FIM 26-11-00, FIGURE 103, SHEET 5, BLOCK 113, RERACKED AFOLTS NR 2 CARD, M10274. MESSAGE WENT AWAY. REMOVED AND REPLACED M684 R ENG FIRE LOOP 2 AFOLTS CARD IAW MM 26-10-01-4. OPERATIONAL CHECK NORMAL. (K) 2L72 4F4 FRTA2NM E12EU 20051109000382005110900038EA 2005 11 9 ASOA05679S 120050819A5340 WEB CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT FLOOR ATTACH CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27839AS 7284 DURING A C-CHECK, THE LT FLOOR ATTACH WEB AT FS 559.80 TO FS 574 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED THE CORROSION ON THE LT FLOOR ATTACH WEB AT FS 559.80 TO FS 574 BY COMPLYING WITH EO. (K) 2L72 4F4 FRTA21EA E15NE 20051109000422005110900042 2005 11 9 SIMA200529003 420051014A34256227713004 DPU SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE AVIONICS RACK INOPERATIVE A SIMAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW21329AE 340B329 CREW REPORTED AN ELECTRICAL BURNING SMELL IN THE COCKPIT. REPLACED NR 2 DPU IAW AMM. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200600453) (K) 2L72 4T4 TRTA52EU E8NE 20051109000432005110900043EA 2005 11 9 SIMA200526902 120050922A5610601R3303317 WINDSHIELD CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE COCKPIT CRACKED A SIMAA UNSCHED LANDING O OTHER CRCRUISE 1 SW21513AE 10114 DURING CRUISE NR 1 WINDSHIELD CRACKED. REPLACED NR 1 WINDSHIELD IAW AMM. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (K) 2L72 4F4 FRTA21EA EOOO63EN 20051109000442005110900044EU 2005 11 9 KBM2005F00274 120050915A6520350A33215001 BALL END SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE TAIL ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19751H 1178 3403 T/R BALL END WORN BEYOND LIMITS. REMOVED AND REPLACED WITH OVERHAULED UNIT. (K) 1G71 3U3 U H9EU E19EU 20051109000492005110900049EA 2005 11 9 UG82005F00010 120050815A3260 INDICATOR CNDAIRCL600 CL6002B16 1900305EA GE CF34 CF343A 30015NE MLG DEFECTIVE E UG8AO OTHER P NO WARNING INDICATION NRNOT REPORTED 1 GL23241FB4972 5102 ( REF: PA 05-003) THERE WAS NO GREEN DOWN AND LOCKED INDICATION ON THE NOSE GEAR. THERE WAS ALSO NO RED UNSAFE INDICATION. THE CREW WENT THROUGH THE REQUIRED CHECKLIST AND DECLARED AN EMERGENCY TO KDAL TOWER. THERE WERE MULTIPLE FAILURES IN THE GEAR INDICATION SYSTEM. THE LANDING GEAR CONTROL UNIT, PN 717001-7, SN 316, WAS FOUND DEFECTIVE AND WAS REPLACED WITH A REPAIRED UNIT. THE RT MAIN GEAR NR 2 DOWNLOCK PROXIMITY SWITCH, PN 8-40534, SN F52129 WAS ALSO FOUND TO BE FAULTY AND WAS REPLACED WITH A NEW UNIT. SYSTEM CHECKS WERE CARRIED OUT IAW THE MM AND THE AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20051109000512005110900051NM 2005 11 9 AMTA200500716 120050922A3350 LIGHT BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE CABIN INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11514AT 27971 TWO BULLNOSE LIGHTS INOPERATIVE AT SEATS 16 ABC AND 20 ABC OF EMERGENCY LIGHT SYSTEM. REPLACED LIGHT ASSY AT ROB 20 ABC. OPS CHECKS GOOD. (K) 2L72 4F4 FRTA2NM E12EU 20051109000522005110900052SO 2005 11 9 SIMA200528307 120051007A2611 SMOKE WARNING EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL LAVATORY FALSE ACTIVATIONA SIMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW21699AE 14500883 CREW RECEIVED LAV SMOKE DETECTION INDICATION ON EICAS. PERFORMED OPERATIONAL CHECKS OF THE LAVATORY SMOKE DETECTION SYSTEM WITH NO DISCREPANCIES NOTED. AC RETURNED TO SERVICE. (K) 2L72 4T4 FRTT00011ATTE6CH 20051109000572005110900057EU 2005 11 9 KBM2005F00329 120051024A6520350A33215001 BALL END SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE TAIL ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19115SH3871 3141 BALL END WORN. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051109000612005110900061SO 2005 11 9 SIMA200528315 120051004A21214611028900 FAN EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL CABIN BURNED A SIMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21824AE 145584 AFTER TAKEOFF CREW GOT VISIBLE SMOKE IN CABIN AND LAV SMOKE EICAS MESSAGE. REPLACED RECIRCULATION FAN. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200600536) (K) 2L72 4F4 FRTT00011ATTE6CH 20051109000642005110900064CE 2005 11 9 MCC2005F00000 120050923A2612 FIRE WARNING MTSBSIMU2 MU2B36 5780412CE GARRTTTPE331TPE3316251M 01514WP RT ENGINE INTERMITTENT E MCCAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 SW11103RC 673 RT ENGINE FINE WARNING FLICKERED ONE TIME IN FLIGHT. PILOT SECURED ENGINE AND FEATHERED PROP. UNEVENTFUL LANDING MADE AT MAINTENANCE INSPECTED ENGINE AND FOUND NO EVIDENCE OF FIRE OR FIRE DAMAGE. GROUND RUN ENGINE COULD NOT DUPLICATE PROBLEM. (K) 1H72 3T4 TRTA10SW E2WE 20051109000652005110900065SW 2005 11 9 ALG2005F00085 120051025A7712407375003107 INDICATOR BELL 407 407 1182206SW ALLSN 250C 250C47B GL TORQUE FAILED E ALGAO OTHER P NO WARNING INDICATION CRCRUISE 1 SW03597AL 53091 IN FLIGHT, TORQUE INDICATOR FAILED. RETURNED TO DEPARTURE AND NOTIFIED MAINTENANCE. REMOVED AND REPLACED TORQUE INDICATOR WITH SERVICEABLE UNIT IAW MM. (K) 1G71 3U3 UO H2SW E1GL 20051109000662005110900066EU 2005 11 9 ALG2005F00086 120051013A6220C622A1011201 PLATE UROCOPEC120 EC120B 8680987EU TMECA ARRIUSARRIU2F NE MAIN ROTOR HEAD DEBONDED E ALGAK NONE O OTHER ININSP/MAINT 1 SW03523AL 1262 DURING POST FLIGHT, THE PILOT SUSPECTED THAT M/R DROOP STOP PLATE IS DEBONDED, NOTIFIED MAINTENANCE. THE MECHANIC REMOVED M/R HUB AND BLADE TO GAIN ACCESS TO THE WEAR PLATES AND FOUND BOTH UPPER AND LOWER WEAR PLATED WERE DEBONDED, REMOVED AND REPLACED BOTH WEAR PLATES AND AC WAS RETURNED TO SERVICE. (K) 1G72 3U3 UNCR0001RD E34NE 20051109000672005110900067GL 2005 11 9 ALG2005F00088 220051011A7321 HMU BELL 407 407 1182206SW ALLSN 250C 250C47B GL ENGINE FAILED E ALGAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 SW03617AL 53265 DURING LEVEL FLIGHT RESTART FAULT LIGHT ILLUMINATED. RETURNED TO DEPARTURE AND NOTIFIED MAINTENANCE. REMOVED AND REPLACED HMU WITH SERVICEABLE UNIT IAW MM. OPS CHECK GOOD. (K) 1G71 3U3 UO H2SW E1GL 20051109000702005110900070 2005 11 9 KBM2005F00324 420051012A3422200DCL GYRO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE DIRECTIONAL SPINNING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19966SH416 3787 DG, UNIT SPINS, REMOVED AND REPLACED. 1G71 3U3 U H9EU E19EU 20051109000712005110900071SW 2005 11 9 ALG2005F00082 120051019A6330209033505101 BEAM BELL 206 206L1 1182107SW ALLSN 250C 250C28B 03013GL RT MOUNT ARM ELONGATED E ALGAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 SW033186P 45776 IN CRUISE FLIGHT, PILOT HEARD A NOISE IN THE AIRFRAME. UPON LANDING NOTIFIED MAINTENANCE. INSPECTION OF AIRCRAFT BY MAINTENANCE FOUND THE RT NOODLE BEAM ARM ASSY HOLES ELONGATED AT WEIGHT BOLTS. REMOVED AND REPLACED ARM ASSY WITH SERVICEABLE UNIT IAW MM. (K) 1G71 3U3 U H2SW E1GL 20051109000722005110900072EU 2005 11 9 KBM2005F00322 120051022A2844642792002 TRANSMITTER SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE FUEL PRESSURE INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH 2884 NO FUEL PRESSURE INDICATION, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051109000832005110900083 2005 11 9 KBM2005F00309 420050930A3422200DC GYRO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1B 6OO30NE DIRECTIONAL INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH156 2337 DIRECTIONAL GYRO INOPERATIVE, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051109000852005110900085EU 2005 11 9 KBM2005F00314 120051015A6230704A33699008 BOOT SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE M/R SWASHPLATE WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19351WM 2167 MAIN ROTOR SWASHPLATE RUBBER BOOT WAS WORN. REPLACED WITH NEW UNIT. (K) 1G71 3U3 U H9EU E19EU 20051109000892005110900089 2005 11 9 KBM2005F00317 420051021A34215040017901 GYRO SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1D NE ATTITUDE INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1953SH 2009 AG, UNIT INOPERATIVE. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051109000912005110900091NM 2005 11 9 S2YA05057 120050913A28447014300902 PRESSURE SWITCH DORNERDO32 DO328300 NM PWA 306 PW306B NE FUEL SYSTEM INOPERATIVE A S2YAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL13359SK8485 1639 3202 DURING CLIMBOUT, THE CREW REPORTED A FUEL FILTER CAS MESSAGE. THE CREW PERFORMED AN AIR-TURN-BACK. MAINTENANCE REPLACED BOTH THE LT FUEL FILTER AND THE FUEL FILTER PRESSURE SWITCH. OPS CHECK GOOD, AC WAS RETURNED TO SERVICE. (K) 2H72 4T4 FRTA55NM E35NE 20051109000932005110900093NE 2005 11 9 KBM2005F00313 220051013A72610235237600 CHIP DETECTOR SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE ENGINE INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP13351WM 2167 CHIP DETECTOR, UNIT INOPERATIVE. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051109000972005110900097 2005 11 9 KBM2005F00312 420050930A34225050010902 GYRO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE DIRECTIONAL SPINNING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19351WM36 2167 DIRECTIONAL GYRO, UNIT SPINS IN FLIGHT, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051109000982005110900098EU 2005 11 9 KBM2005F00316 120051002A624039951213 GAUGE SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE FLUCTUATES E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1937SH 2300 NR GAUGE, UNIT FLUCTUATION FROM 250-350 RPM STUCK AT 350. REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20051109001012005110900101SO 2005 11 9 SIMA200529008 120051013A532014525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO ALLSN AE3007AE3007C GL FR 25 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21722AE11727 145287 A PREVIOUS REPAIR ON THE LT OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. REMOVED THE EXISTING REPAIR AND CLEANED THE AREA. PREPARED A DOUBLER, FILLER AND SHIMS. REPAIR DONE IAW SRM. (SW21200500542) (K) 2L72 4F4 FRTT00011ATTE6CH 20051109001022005110900102SO 2005 11 9 SIMA200529304 120051012A532014525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO ALLSN AE3007AE3007C GL GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21722AE 145287 A PREVIOUS REPAIR ON THE CENTER OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. FABRICATED REPAIR DOUBLER, FILLER AND SHIMS. REPAIR DOEN IAW SRM. (SW21200600542) (K) 2L72 4F4 FRTT00011ATTE6CH 20051109001032005110900103GL 2005 11 9 SIMA200528313 220051005A7261 CARBON SEAL EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL NR 1 ENGINE LEAKING A SIMAA UNSCHED LANDING KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21824AE113835839 145584 CAE34442 AFTER TAKEOFF CREW GOT VISIBLE SMOKE IN CABIN AND A LAV SMOKE EICAS MESSAGE. REPLACED NR 1 ENGINE DUE TO CARBON SEAL LEAKING. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200600331) (K) 2L72 4F4 FRTT00011ATTE6CH 20051109001052005110900105SO 2005 11 9 SIMA200529305 120051014A532014525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO ALLSN AE3007AE3007C GL FR 20 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21722AE 145287 A PREVIOUS REPAIR ON THE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. REMOVED THE EXISTING REPAIR AND CLEANED THE AREA. PREPARED A DOUBLER, FILLER, REPAIR ANGLE AND 2 SHIMS. REPAIR DONE IAW SRM. (SW21200500542) (K) 2L72 4F4 FRTT00011ATTE6CH 20051109001072005110900107SO 2005 11 9 SIMA200529007 120051012A5320 SILL EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAO OTHER O OTHER NRNOT REPORTED 1 SW21717AE 145272 DURING CPCP INSPECTION FOUND FLOORBEAM AT FRAME 22 ABOVE SERVICE DOOR AFT SILL IS CORRODED. REPLACED (Z) PROFILE AT FRAME 22 ABOVE SERVICE DOOR AFT SILL IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200600538) (K) 2L72 4F4 FRTT00011ATTE6CH 20051109001082005110900108SO 2005 11 9 SIMA200529302 120051013A532014522178005 SILL EMB 135 EMB135LR 3260305SO ALLSN AE3007AE3007C GL SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21722AE11727 145287 THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. BLENDED THE CORRODED AREAS ON THE SILL TO REMOVED THE CORROSION. FABRICATED 3 REPAIR DOUBLER. REPAIR DONE IAW SRM. (SW2120060542) (K) 2L72 4F4 FRTT00011ATTE6CH 20051109001102005110900110 2005 11 9 KBM2005F00318 420051023A2340AA83001 ICS BOX SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1D NE INTERCOM INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1953SH 864 2009 ICS BOX, UNIT INOPERATIVE. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051109001122005110900112SW 2005 11 9 ALG2005F00080 120050805A2914206076030111 HAND PUMP BELL 206 206L1 1182107SW ALLSN 250C 250C28B 03013GL HYD SYS DAMAGED E ALGAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SW0341GH 45502 DURING TAKEOFF, THE PILOT NOTICED THE CYCLIC AND COLLECTIVE ARE STIFF WITH NO FRICTION APPLIED. THE PILOT FOLLOWED EMERGENCY CHECK LIST AND LANDED. THE SUBSEQUENT INSPECTION BY MECHANIC REVEALED THAT THE HYD PUMP SHAFT SPLINES WERE STRIPPED. REMOVED AND REPLACED HYD PUMP, HYD FILTER AND HYD LINES AND THE AC WAS RETURNED TO SERVICE UPON COMPLETION OF ALL FUNCTION CHECKS IAW MM. (K) 1G71 3U3 U H2SW E1GL 20051109001142005110900114EU 2005 11 9 SIMA200528311 120051008A3350330151 POWER SUPPLY SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE EMERGENCY LIGHT DISCHARGED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21383AE 340B383 EMERGENCY LIGHT OVERHEAD SIGN AT ROW 8, INOPERATIVE. REPLACED EMERGENCY POWER SUPPLY 201N. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200600359) (K) 2L72 4T4 TRTA52EU E8NE 20051108000862005110800086WP 2005 11 8 ABXA050263 120051104A2130 CABIN PRESSURE DOUG DC8 DC863 302198AWP UNKNOWN A ABXAG O2 MASK DEPLOYED J WARNING INDICATION CLCLIMB 1 GL23825AX 46115 DURING CLIMB AT FL310, CABIN RATE OF CLIMB WENT FROM 500 FPM TO 6,000 FPM. COULD NOT STOP THE CABIN FROM CLIMBING USING AUTO OR MANUAL LEVER. CABIN WENT TO 11,000 FT. DONNED OXYGEN AND STARTED DESCENT. AT ABOUT FL290, REGAINED CONTROL OF BOTH AUTO AND MANUAL PRESSURIZATION. LUBRICATED PRESSURIZATION OUTFLOW VALVE AND SCOOP AS REQUIRED. INSPECTED CABIN PRESSURE SAFETY VALVES AND NO DEFECTS NOTED. PRESSURIZED AIRCRAFT IAW DC8 MM. OPS CHECKED GOOD. 2L74 4F 4A25 20051108000992005110800099SO 2005 11 8 SIMA200523509 120050820A532014529101003 STRAP EMB 135 EMB135LR 3260305SO FUSELAGE DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21734EK 145371 WHILE SITTING ON RAMP AT EWR, A/C WAS HIT IN FORWARD RIGHT FUSELAGE SECTION BY VEHICLE. COMPLETED REPAIR TO SKIN BETWEEN FRAMES 10-13 AND STRINGER 13R TO 18R BY REPLACING DAMAGED PORTION OF SKIN (P/N 14527606007) AND INSTALLING AN EXTERNAL DOUBLER IAW EO EB-53MR-326R1 AND SRM 51-40-02, SPLICING IN A NEW SECTION OF FRAME (P/N 14521667001) 12 BETWEEN STRINGERS 15R AND 17R IAW EMB SRM 53-00-04 FIGURE 201 AND RECONTOURING SKIN BETWEEN FRAMES 13 AND 14 STRINGERS 15R AND 17R AND REPLACING INNER STRAP IAW SRM 53-00-01 FIGURE 203 AND I/C2005-145/4309. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20051108001032005110800103EA 2005 11 8 ASOA05832 120050928A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27903EV 7621 FLT 4260 - DURING A GROUND INSPECTION IN VPS, THE EMERGENCY CEILING LIGHT, AT ROW 4, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY CEILING LIGHT AT ROW 4. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051108001042005110800104SO 2005 11 8 GUU2005F00049 120050907A3397AGC1 FUSE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT FAILED A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO29268AS 120202 FLT 9230 - FLL-NAS - EMERGENCY TRACK LIGHTS INOPERATIVE IN CABIN. REPLACED CABIN EMERGENCY LIGHT FUSELAGE. (M) 2L72 4T RTA31SO 20051108001092005110800109SO 2005 11 8 SIMA200527713 120051001A322014521680004 BEARING EMB 135 EMB135LR 3260305SO NLG CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21716AE 145264 FOUND NOSE LANDING GEAR BRACE STRUT FITTINGS HAVE MINOR CORROSION. REMOVED CORROSION ON MAIN BRACE HALF BEARINGS IAW SRM 53-11-08. FOUND TO BE ACCEPTABLE AS PER FACSIMILE REF IC2005-145/5445D. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20051108001372005110800137EA 2005 11 8 ASOA05836 120051001A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27842AS 7304 DURING A GROUND INSPECTION IN MGM, THE AFT EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE AFT EMERGENCY CEILING LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051108001472005110800147WP 2005 11 8 GTIA050219 120050718A5320 WEB DOUG DC9 DC983 3022083WP BS 620-675 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 FOUND LEFT CABIN FLOOR WEB LBL 44 TO LBL 54 HAS CORROSION AT STATION 675 AND STATION 620-630. FOUND WEB STATION 640 LT - 678 LT ARE OUT OF LIMITS. REMOVED DAMAGED AREAS, FABRICATED DOUBLERS. TREATED, PRIMED AND INSTALLED DOUBLERS. (M) 2L72 4F RTA6WE 20051108001502005110800150EU 2005 11 8 ASOA05823 120050830A5310 CREASE BEAM AEROSPATR72 ATR72212 8680945EU FR 35-40 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27637AS 383 DURING A C-CHECK IN YUL, THE LEFT CREASE BEAMS BETWEEN FS 35-36 AND FS 39-40 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LT CREASE BEAMS BETWEEN FS 35-26 AND FS 39-40 IAW ATR-72 SRM 51-25-01. (M) 2H72 4T RTA53EU 20051108001552005110800155EA 2005 11 8 ASOA05854 120051010A5312 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA BS 202 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27836AS 7263 DURING A C-CHECK IN MCN, THE FORWARD PRESSURE BULKHEAD, FS 202.75, AT BL 23.71, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REPAIR THE FORWARD PRESSURE BULKHEAD FS 202.75, AT BL 23.71, IAW ASA EO 600-53-0217. (M) 2L72 4F RTA21EA 20051108001572005110800157EU 2005 11 8 ASOA05912 120051013A5330 DOUBLER AEROSPATR72 ATR72212 8680945EU FS 48 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27641AS 387 DURING A C-CHECK IN YUL, THE UPPER AND LOWER STATIC BASE DOUBLERS, AT FS 48 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE UPPER AND LOWER STATIC BASE DOUBLERS AT FS 48, IAW AMM 20-21-12. (M) 2H72 4T RTA53EU 20051108001682005110800168EA 2005 11 8 ASOA05870 120051014A3350 LIGHT CNDAIRCL600 CL6002C10 1390015EA CABIN INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11760EV 10212 DURING A GROUND INSPECTION IN ATL, ALL OF THE EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE EMERGENCY EXIT LIGHTS AND NO DEFECTS WERE NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051108001692005110800169EA 2005 11 8 ASOA05849 120051009A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27871AS 7537 FLT 4186 - DURING A GROUND INSPECTION IN CAE, THE RIGHT SIDE OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE RIGHT SIDE OVERWING EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051108001872005110800187EU 2005 11 8 ASOA05828 120050901A5320 FLOOR SUPPORT AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27637AS 383 DURING A C-CHECK IN YUL, THE LEFT FLOOR SUPPORT BETWEEN FRAME 39-40 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT FLOOR SUPPORT BETWEEN FRAME 39-40 IAW ATR 72 SRM 51-25-01. (M) 2H72 4T RTA53EU 20051108002182005110800218EA 2005 11 8 ASOA05876 120051014A33508F50357901 LENS CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27836AS 7263 DURING A C-CHECK IN MCN, THE EXIT LIGHT LENS, ABOVE THE SERVICE DOOR, WAS FOUND TO BE CRACKED. MAINTENANCE WILL REMOVE AND REPLACE THE EXIT LIGHT LENS, ABOVE THE SERVICE DOOR. (M) 2L72 4F RTA21EA 20051108002332005110800233WP 2005 11 8 GTIA050206 120050628A5260 STRUCTURE DOUG DC9 DC983 3022083WP AIRSTAIR DOOR DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23815NK 49415 FOUND DENT AT STATION 1465 ON VENTRAL AIRSTAIR DOOR. FOUND DENTS OUT OF LIMITS. CUTOUT 2 INCH DIAMETER. FABRICATED DOUBLER AND FILLER. TREATED, PRIMED AND INSTALLED FILLER AND DOUBLER. (M) 2L72 4F RTA6WE 20051108002402005110800240WP 2005 11 8 GTIA050244 120050827A5310 DOOR FRAME DOUG DC9 DC983 3022083WP LT MLG CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23834NK 49847 FOUND LT MLG, AFT DOOR JAMB IS CRACKED AT CORNER T-CAP. STOPPED DRILLED CRACK AT AFT DOOR JAMB. FABRICATED REPAIR DOUBLER. TREATED, PRIMED AND INSTALLED DOUBLER. (M) 2L72 4F RTA6WE 20051108002492005110800249EU 2005 11 8 ASOA05825 120050830A5310S53678008216 STRUCTURE AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27637AS 383 DURING A C-CHECK IN YUL, THE Z-FLOORS BETWEEN FS 39-40 LEFT AND FS 39 AND 41 RIGHT WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE Z-FLOORS BETWEEN FS 39-40 LT AND FS 39 AND 41 RT IAW ASA EO 72-53-0166A. (M) 2H72 4T RTA53EU 20051108002552005110800255EA 2005 11 8 ASOA05846 120051027A33506100976 LAMP CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT BURNED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27712EV 10074 FLT 4192 - DURING HANGAR MAINTENANCE IN BTR, THE AFT EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE AFT EMERGENCY CEILING LIGHT. OPERATIONAL CHECKS GOOD. (M) 2L72 4F RTA21EA 20051108002662005110800266EA 2005 11 8 ASOA05799 120050924A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA BS 484 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27835AS 7258 DURING A C-CHECK IN MCN, THE LEFT OUTBOARD FS 484 CLIP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT OUTBOARD FS 484 CLIP IAW BOMBARDIER REO 601R-53-41-059. (M) 2L72 4F RTA21EA 20051108002802005110800280EU 2005 11 8 SIMA200526406 120050913A53477253799379 SEAT TRACK SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE STA 339-363 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21329AE21268 340B329 SEAT TRACK BL0 WAS FOUND TO BE CORRODED BETWEEN STA 339 AND 363. BLENDED THE SEAT TRACKS TO REMOVE THE CORROSION. CUT A SECTION FROM U-BEAM FOR REPAIR. CLEANED TREATED AND INSTALLED U-BEAM IN SEAT TRACK. REPAIR DONE IAW SRM. (K) 2L72 4T4 TRTA52EU E8NE 20051108002832005110800283NM 2005 11 8 S2YA05062 120050925A3231001A322A150000 ROD DORNERDO32 DO328300 NM PWA 306 PW306B NE LT NLG DOOR SHEARED A S2YAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL13351SK 3108 SHORTLY AFTER DEPARTURE OF FLIGHT, THE CREW REPORTED A STRONG VIBRATION UPON RETRACTING THE GEAR. THE CREW PERFORMED AN AIR-TURN-BACK. MAINTENANCE FOUND THE LT FORWARD NOSE WHEEL GEAR DOOR SHEER ROD BROKEN. MAINTENANCE REPLACED THE ROD AND RETURNED THE AC TO SERVICE. (K) 2H72 4T4 FRTA55NM E35NE 20051108003132005110800313EA 2005 11 8 COMA0570117 120051031A2120 SMOKE CNDAIRCL600 CL6002C10 1390015EA COCKPIT DETECTED A COMAK NONE B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO01398CA 10112 FLIGHT 5803 - FUMES IN COCKPIT. TURNED OFF LEFT BLEED AIR AND FUMES DISSIPATED. NO FUMES OR SMELL DURING GROUND RUNS. 2L72 4F RTA21EA 20051108003142005110800314EU 2005 11 8 USAA051348 120051107A5315D5347209001000 FLOORBEAM AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19111US 1114 FLOORBEAM Y1292 FR 64-68 CLIP NUT HOLES; CORROSION LEVEL 1; TASK JA-260-53500. REPLACED FLOORBEAM WITH NEW IDENTICAL PARTS PER DWG D53472780. DEFECT SIZE: .5 X .5 INCH AREA EACH HOLE. 2L72 4F RTA28NM 20051108003152005110800315EU 2005 11 8 USAA051347 120051107A5320D534800480 PLATE AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19111US 1114 LEFT AFT DOOR SILL BETWEEN FR 66-68; CORROSION LEVEL 1; TASK JA-260-53500. REMOVED & REPLACED SHAPE PER SRM 51-72-11. DEFECT SIZE: .25 X 10 INCH AND .25 X 5 INCH. 2L72 4F RTA28NM 20051108003162005110800316NM 2005 11 8 USAA051346 120051107A5320 ATTACH ANGLE BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19779AU 24996 STA 500C LT FUSELAGE FRAME AND ATTACH ANGLE CRACKED. REMOVED CRACK, FABRICATED AND INSTALLED REPAIR STRAPS IAW EA 97079. DEFECT SIZE: .50 INCH. 2L72 4F RTA16WE 20051108003252005110800325CE 2005 11 8 S2YA05061 120050925A3297G1122 WIRE BEECH 1900 1900D 1154162CE PWA 306 PW306B NE MLG DAMAGED A S2YAO OTHER J WARNING INDICATION APAPPROACH 1 GL1391SK UE91 DURING APPROACH, THE CREW REPORTED THEY WERE UNABLE TO EXTEND THE GEAR AND FOUND THE CIRCUIT BREAKER (CB) POPPED. THE CREW RESET THE CB ONLY TO HAVE IT POP WHEN SELECTING GEAR DOWN. THE CREW MANUALLY EXTENDED THE GEAR, ACHIEVED 3 GREEN AND PROCEEDED TO LAND WITHOUT INCIDENT. THE AC WAS INSPECTED AND MAINTENANCE FOUND A WIRE (G1122) INSIDE THE AC WALL TO BE SHORTED. MAINTENANCE REPAIRED THE WIRE AND WITH NO FURTHER DISCREPANCIES, RETURNED AC TO SERVICE. (K) 2L72 4T4 FRTA24CE E35NE 20051108003442005110800344EA 2005 11 8 SIMA200527201 120050927A335020131A BATTERY PACK CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE EMERGENCY LIGHT DISCHARGED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21509AE 10078 LT SIDEWALL EMERGENCY LIGHT FAILS TO TEST. REPLACED EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200600354) (K) 2L72 4F4 FRTA21EA EOOO63EN 20051108003492005110800349CE 2005 11 8 DXTA200501046 120051101A3240 LINE CESSNA560 560XL 2076702CE BRAKE SYSTEM CONTAMINATED E DXTAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07677QS 5605367 ON CAPTAIN`S SIDE, RIGHT BRAKE FADES WHEN PRESSURE APPLIED DURING TAXI OR TURNING. BLED BRAKE SYSTEM PER CE560XL MM 32-42-00. TAXI CHECK WAS GOOD. 2L72 4F RTA22CE 20051108003552005110800355 2005 11 8 RAIA00511002 420051103A34180020BN4 COMPUTER EMB 145 EMB145LR 3260212SO STALL WARNING MALFUNCTIONED A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03840HK11175 145341 FLT 8018 - STL - STALL PROTECTION SYSTEM MESSAGE DURING FLIGHT. MAINTENANCE REMOVED AND REPLACED SPS COMPUTER. 2L72 4T RTT00011AT 20051108003582005110800358SO 2005 11 8 RAIA00511005 120051105A33507287580505 LIGHT EMB 145 EMB145 3260210SO CABIN DAMAGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03807HK 145119 MX - PIT- FWD MOST FLOOR LIGHT STRIP INOP. MAINTENANCE REMOVED AND REPLACED LIGHT STRIP ASSEMBLY. 2L72 4F RTT00011AT 20051108003712005110800371NM 2005 11 8 2005UALA01216 120051031A2913 PUMP BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE HYDRAULIC SYS OVERHEATED A UALAH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION DEDESCENT 1 WP29646UA 25283 CANCELLED DUE TO INBOUND HYDRAULIC PUMP OVERHEAT AND LOSS OF HYDRAULIC SYSTEM PRESSURE. MAINTENANCE REPLACED RIGHT ENGINE HYDRAULIC DRIVEN PUMP AND CASE DRAIN AND PRESSURE FILTERS. PERFORMED ENGINE RUN AND REQUIRED OP CK. ALL OK. 2L72 4F4 FRTA1NM E24NE 20051108003722005110800372NM 2005 11 8 2005UALA01217 120051102A5315 FLOORBEAM BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29173UA 24380 M-D STA 1660 GALLEY AREA FLOORBEAM UPPER CHORD HAS CORROSION (AT SCREW HOLE AREA) LBL 30. LOCAL DAMAGE REPAIRED PER SRM AS PERMANENT. 2L74 4F4 FRTA20WE E24NE 20051108003772005110800377NM 2005 11 8 2005UALA01222 120051103A5754 SKIN BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE L/E SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29787UA 26939 NR 3 SLAT LWR SURFACE DELAMINATED AT OUTBOARD END 4 INCHES FROM TRAILING EDGE. INTERIM REPAIR PER 777 AMM 57-43-99. ACP AN INITIAL INSP AT 50 CYCLE AND EVERY 500 FLT CYCLE UNTIL PERMANENT REPAIR ACPL AT NEXT HMV (5JUNE06). OK TO CF PER AMM AND SFOIQ WALSH. 2L72 4F4 FRTT0001SE E46NE 20051108003922005110800392NM 2005 11 8 EIA2005167 120051010A5330 SKIN BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 FX SKIN BS 2598 BETWEEN S-42R AND S-46R JUST BELOW TAIL JACK SKIN CRACKED. FX SKIN BS 2588-2589 BETWEEN S-42R AND S-46R SKIN REPAIR CARRIED OUT IAW SRM 53-30-03 FIG 1A. 2L74 4F A20WE 20051108003942005110800394NE 2005 11 8 EIA2005169 220051020A7261 SEAL BOEING747 747121 1384871NM PWA JT9 JT9D7A 52054NE NR 1 ENGINE LEAKING A EIAAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 NM09480EV 20348 685897 NR 1 ENG OIL PRESSURE FLUCTUATED IN CRUISE WITH DECREASING OIL QUANTITY FOLLOWED BY OIL PRESSURE LIGHT ON AT 35 PSI. OIL QTY DECREASED TO 2 GALS. SHUTDOWN ENGINE IAW EV PROCEDURES OIL PRESSURE REMAINED AT APPROX 20 PSI DURING WINDMILLING. FOUND OIL LEAK EDP DRAIN. REPLACED HYD PUMP DRIVE SEAL ON SHAFT AND CARBON SEAL RING PER MM 72-61-09. REPLACED O-RING SEAL ON CARBON SEAL AND RETAINER ASSY. PERFORMED WINDMILLING INSP (ENG WINDMILLED FOR 55 MIN AT 20 PSI) ENGINE RUN OIL PRESSURE STEADY AT 50 PSI QTY REMAINED FULL SYSTEM O/B NORMAL. REMOVED AND INSTALLED NR 1 ENG HYD PUMP PER MM 29-11-05, NO LEAKS NOTED AFTER RUN. 2L74 4F4 F A20WE E20EA 20051109000022005110900002CE 2005 11 9 AJC2005F00013 120050923A243566085122 STARTER GEN LEAR 60 60LEAR 5170707CE PWA 306 PW306B NE LT ENGINE FAILED E AJCAO OTHER E VIBRATION/BUFFET CLCLIMB 1 EA2543NR 1007 7 043 PASSING THROUGH FL 250, CREW EXPERIENCED AN IRREGULAR AIRFRAME VIBRATION AND A YAW MOTION LT TO RT. AFTER INCREASING AND DECREASING THE POWER, THE CREW FELT THE SAME IRREGULAR YAW. AFTER LANDING, CREW ISOLATED THE VIBRATION TO THE LT ENGINE. MAINTENANCE BORESCOPED THE LT ENGINE FIRST STAGE COMPRESSOR, FOUND NO DISCREPANCIES. SWAPPED STARTER GENERATOR FOR TROUBLESHOOTING AND FOUND THE LT STARTER/GENERATOR AT FAULT. REPLACED SAME WITH A SERVICEABLE UNIT IAW MM. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4F4 FRTA10CE E35NE 20051109000462005110900046 2005 11 9 KBM2005F00260 420050911A2312064105430 RADIO SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1 60030NE VHF INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19215LA17118 2143 VHF RADIO KNOB WILL NOT ADJUST ITS NUMBERS, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051109000472005110900047SW 2005 11 9 ALG2005F00084 120051021A2436VR1010241A VOLT REGULATOR BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL DC SYSTEM FAILED E ALGAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 SW03116AL 2389 IN CRUISE FLIGHT, BATTERY TEMP LIGHT ILLUMINATED. BATTERY SWITCH WAS TURNED OFF IAW EMERGENCY PROCEDURES. BATTERY HOT LIGHT ILLUMINATED A SHORT TIME AFTERWARDS. AIRCRAFT WAS LANDED A SHORT TIME AFTERWARDS AND MAINTENANCE NOTIFIED. REMOVED AND REPLACED AIRCRAFT BATTERY, REMOVED AND REPLACED BATTERY TEMP SENSOR, REMOVED AND REPLACED VOLTAGE REGULATOR. ALL PARTS INSTALLED WERE SERVICEABLE PARTS AND ALL WORK WAS IAW MM. (K) 1G71 3U3 U H2SW E4CE 20051109000482005110900048NE 2005 11 9 ALG2005F00087 220051010A7323 CONTROL ROD UROCOPEC120 EC120B 8680987EU TMECA ARRIUSARRIU2F NE ENG GOVERNOR OUT OF ADJUST E ALGAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION HOHOVERING 1 SW03516AL 1157 DURING HOVER, ROTOR RPM WAS LOW, LANDED AND NOTIFIED MAINTENANCE. FUEL CONTROL WAS REPLACED THE NIGHT BEFORE. ADJUSTED GOVERNOR CONTROL ROD IAW MM AND RFM. GROUND RUN AND OPS. CHECK GOOD. (K) 1G72 3U3 UNCR0001RD E34NE 20051109000592005110900059EU 2005 11 9 KBM2005F00327 120051027A6730AC67244 SERVO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE M/ROTOR CONTROL LEAKING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19115SH1339 3141 UNIT LEAKING EXCESSIVELY HYDRAULIC FLUID ON WEEPLE HOLE. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051109000782005110900078EA 2005 11 9 JTK2005F00000 220051006A8500 THRUST WASHER SKRSKYS58 S58D 8141808NE WRIGHTR1820 989C9HE2 67020EA ENGINE FAILED G JTKLO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL0358NS 581453 W523278 ENGINE BREATHER STARTED EMITTING SMOKE AS ENGINE CHIP LIGHT CAME ON. AIRCRAFT LANDED UNDER POWER WITHOUT FURTHER INCIDENT INITIAL INSPECTION INDICATED POSSIBLE MASTER BEARING THRUST WASHER FAILURE. (K) 2G71 4R4 R 1H11 E259 20051109000872005110900087 2005 11 9 KBM2005F00310 420051017A3457066011480102 GPS SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE COCKPIT INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV4911 3296 GPS DISPLAY INOPERATIVE. AIRCRAFT MEL`D UNITL 10/24/05. (K) 1G71 3U3 U H9EU E19EU 20051109000962005110900096SO 2005 11 9 SIMA200529301 120051016A5210AL2024T3 SKIN EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL MAIN DOOR SCRATCHED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21851AE5897 145734 DISC STRATCH ON THE MAIN ENTRANCE DOOR SKIN. PERFORMED A CUT OUT OF THE MAIN ENTRANCE DOOR SKIN. FABRICATED A REPAIR DOUBLER AND FILLER. REPAIR DONE IAW SRM AND EO. (SW21200600537) (K) 2L72 4F4 FRTT00011ATTE6CH 20051109001002005110900100SO 2005 11 9 SIMA200529303 120051014A532014524131007 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO ALLSN AE3007AE3007C GL FR 20 DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21722AE11727 145287 DAMAGED FASTENER HOLE WAS DISCOVERED ON THE LT OMEGA BEAM FLOOR SUPPORT TOWER AT FRAME 20. PERFORMED A CUT OUT OF THE SUPPORT TOWER TO REMOVE THE DAMAGE. FABRICATED A FILLER AND REPAIR ANGLE. REPAIR DONE IAW SRM. (K) 2L72 4F4 FRTT00011ATTE6CH 20051109001062005110900106SO 2005 11 9 SIMA200529006 120051012A531014522460009 BEAM EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FR 18-22 CORRODED A SIMAO OTHER O OTHER NRNOT REPORTED 1 SW21717AE 145272 DURING CPCP INSPECTION, FOUND PROFILE ON CENTER HAT BEAM BETWEEN FRAMES 18-22 CORRODED. REPLACED CENTER HAT BEAM PROFILE IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200600538) (K) 2L72 4F4 FRTT00011ATTE6CH 20051109001202005110900120NM 2005 11 9 05FDEA03664 120051107A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 CRACK INDICATION FOUND AT END OF STRINGER -42 (LOWER STRINGER). DURING HFEC INSPECTION AT RT WING TANK. REPAIRED AS PER SRM 57-20-00. 2L73 4F RTA22WE 20051109001232005110900123WP 2005 11 9 05FDEA03668 120051107A5754 DOUBLER DOUG DC10 DC1010 3022110WP NR 1 SLAT UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 LEFT WING NR 1 SLAT L/E UPPER SURFACE FOUND A FLUSH DOUBLER REPAIR BETWEEN WING STATION XIS152 AND XIS157. PERFORMED A GVI OF EXISTING DOUBLER IAW EO8-5100-7-5001 CRITERIA REQUEST FOUND IN COMPLIANCE WITH SRM 57-10-00 FIG 11. 2L73 4F A22WE 20051109001242005110900124WP 2005 11 9 05FDEA03669 120051107A5754 DOUBLER DOUG DC10 DC1010 3022110WP NR 1 SLAT UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 FOUND EXTERNAL DOUBLER REPAIR AT LEFT WING NR 1 SLAT UPPER SURFACE L/E AREA BETWEEN WING STATIONS XIS129 TO XIS133. PERFORMED A GVI OF EXISTING REPAIR IAW SRM 57-10-00 FIG 84 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO8-5100-7-5001. 2L73 4F A22WE 20051109001262005110900126WP 2005 11 9 05FDEA03671 120051107A5751 DOUBLER DOUG DC10 DC1010 3022110WP AILERON UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 RIGHT WING LOWER SURFACE INBOARD AILERON FOUND AN EXTERNAL DOUBLER REPAIR BETWEEN WING STATIONS XIA316 TO XIA321. PERFORMED A GVI OF EXISTING DOUBLER IAW EO8-5100-7-5001 CRITERIA REQUEST AND FOUND IN COMPLIANCE WITH SRM 57-00-01 FIG 4. 2L73 4F A22WE 20051109001302005110900130NM 2005 11 9 SWAA053516 120051107A575265C26485 TAB BOEING737 7373H4 1384600NM RT WING AILERON DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29335SW 23939 DURING SCHEDULED 1/4D CHECK, FOUND RT WING AILERON TAB DELAMINATED. REMOVED AND REPLACED TAB PER MM. 2L72 4F RTA16WE 20051109001322005110900132NM 2005 11 9 SWAA053518 120051107A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 685 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 685, STR 13R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051109001332005110900133NM 2005 11 9 SWAA053519 120051107A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 706 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051109001342005110900134NM 2005 11 9 SWAA053520 120051107A53306545774 SKIN BOEING737 7373Y0 1384671NM BS 749 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29664WN 23495 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 749, STR 18R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051109001362005110900136NM 2005 11 9 SWAA053522 120051107A3350311500 LENS BOEING737 7373A4 1384585NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 BULLNOSE EMERGENCY LIGHT LENS MISSING AT ROW 12. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20051109001382005110900138NM 2005 11 9 SWAA053524 120051106A5315BAC1509 FLOORBEAM BOEING737 7377H4 1384404NM BS 773 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29792SW 27887 DURING SCHEDULED 5Y CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 773, LBL 3. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20051109001392005110900139NM 2005 11 9 SWAA053525 120051106A5315BAC1509 FLOORBEAM BOEING737 7377H4 1384404NM BS 773 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29792SW 27887 DURING SCHEDULED 5Y CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 773, LBL 12. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20051109001432005110900143NM 2005 11 9 QXEA200501506 120051104A2160 HEATER DHAV DHC8 DHC8202 2809007NM INADEQUATE A QXEAK NONE O OTHER NRNOT REPORTED 1 NM09369PH 513 PDX FLIGHT NR 2207 - FLIGHT COMPARTMENT DOES NOT PROVIDE ADEQUATE HEAT IN BOTH AUTO AND MANUAL MODES. CABIN WORK NORMAL. PERFORMED DELATCHING PROCEDURE IAW DHC-8 EMERGENCY AND ABNORMAL CHECKLIST AND ADJUSTMENT TEST 21-60-00, PAGE 501-502. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051109001442005110900144NM 2005 11 9 QXEA200501502 120051104A5200 LATCH DHAV DHC8 DHC8202 2809007NM BREAKER DOOR INOPERATIVE A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09351PH 490 PDX FLIGHT NR 2208 - GALLEY BREAKER PANEL DOOR INOP. MAINTENANCE RELATCHED GALLEY BREAKER DOOR AS REQUIRED. NO PARTS REPLACED. OPERATIONAL CHECK GOOD. 2H72 4T RTA13NM 20051109001452005110900145NM 2005 11 9 QXEA200501503 120051105A2913570347 PUMP DHAV DHC8 DHC8202 2809007NM NR 2 HYD SYSTEM MALFUNCTIONED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09368PH16794 512 SEA FLIGHT NR 2180 - NR 2 HYDRAULIC PUMP CAUTION. MAINTENANCE REPLACED NR 2 EDP. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051109001462005110900146NM 2005 11 9 QXEA200501505 120051105A33506104781 BATTERY PACK DHAV DHC8 DHC8202 2809007NM EMERENCY LIGHT MALFUNCTIONED A QXEAK NONE O OTHER TXTAXI/GRND HDL 1 NM09375PH* 581 529 SEA - FLIGHT ATTENDANT REPORTS EMERGENCY LIGHTS NEAR 1E OUT. MAINTENANCE REPLACED EMERGENCY BATTERY PACKS. AERIAL NUMBERS 9706303, H056, H092 AND 0049. ALL UNITS HAD 581.8 HOURS SINCE REPAIR. OPERATIONAL TEST OF ALL EMERGENCY LIGHTS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051109001532005110900153NM 2005 11 9 SWAA053527 120051106A5315BAC1509 FLOORBEAM BOEING737 7377H4 1384404NM BS 773 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29792SW 27887 DURING SCHEDULED 5Y CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 773, RBL 8. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20051109001612005110900161WP 2005 11 9 05FDEA03689 120051107A5330 DOUBLER DOUG DC10 DC1010 3022110WP FUSELAGE UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 FOUND TRIPLE DOUBLER BOTTOM OF FUSELAGE BETWEEN STA 1019 AND 1059, AND STRINGERS 51 LT TO 51 RT ADF LOOP ANTENNA LOCATION. PERFORMED A GVI OF EXISTING DOUBLER IAW EO8-5100-7-5001 CRITERIA FOUND DOUBLER IN COMPLIANCE WITH SRM 53-20-00 FIG 7 PG 85. 2L73 4F A22WE 20051109001722005110900172NM 2005 11 9 EIA2005173 120051008A5315 FLOORBEAM BOEING747 747212B 1384886NM BS 360 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 BS 360 RBL 3 FLOORBEAM SCREW HOLE AREA FOUND CRACKED. DEFECTIVE FLOORBEAM UPPER CHORD REPAIRED PER SB 747 53A2452 FIG 13 (HORIZONTAL AFT FLANGE RBL 3). 2L74 4F A20WE 20051109001732005110900173NM 2005 11 9 EIA2005174 120051007A5347 CARGO TRACK BOEING747 747212B 1384886NM BS 1950-1970 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 BS 1950-1970 RBL 96 TIE DOWN TRACK O/B FLANGE FOUND CRACKED. DEFECTIVE TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG A AT BS 1930-BS 1970 RBL 96. 2L74 4F A20WE 20051109001742005110900174NM 2005 11 9 EIA2005175 120051007A5320 CHANNEL BOEING747 747212B 1384886NM BS 520-820 CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 BS 520 TO BS 840 RBL 40 HAT SECTION FOUND CORRODED. DEFECTIVE HAT SECTION REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20051109001752005110900175NM 2005 11 9 EIA2005176 120051011A5315 FLOORBEAM BOEING747 747212B 1384886NM BS 340 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 BS 340 FLOORBEAM UPPER CHORD HORIZONTAL AFT FLANGE RBL 34 FLOOR PANEL HOLE CRACKED RUNNING FWD 0.060 INCH AND AFT 0.040 INCH LONG. DEFECTIVE FLOORBEAM UPPER CHORD REPAIRED AS PER SB 747-53A2431 FIG 9 (HORIZONTAL AFT FLANGE RBL 34). 2L74 4F A20WE 20051109001802005110900180NM 2005 11 9 05FDEA03621 120051104A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 DURING HFEC INSPECTION, FOUND CRACK INDICATION AT RIGHT WING, END OF STRINGER 10. REPAIR CARRIED OUT IAW SRM 57-20 -00 FIG. 10 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051109001812005110900181NM 2005 11 9 05FDEA03622 120051104A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 DURING HFEC INSPECTION, FOUND CRACK INDICATION AT RIGHT WING, END OF STRINGER 11. REPAIR CARRIED OUT IAW SRM 57-20 -00 FIG. 10 VOL I. CLIP FABRICATED AS PER FEDEX EA 1-5720-90051. 2L73 4F RTA22WE 20051109001822005110900182NM 2005 11 9 05FDEA03623 120051104A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 DURING HFEC INSPECTION, FOUND CRACK AT RIGHT WING, END OF STRINGER 12 APPROXIMATELY 13.25 INCHES. REPAIR CARRIED OUT IAW SRM 57-20-00 FIG. 10 VOL I. CLIP FABRICATED AS PER FEDEX EA 1-5720-90052. 2L73 4F RTA22WE 20051109001842005110900184NM 2005 11 9 05FDEA03625 120051104A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 DURING HFEC INSPECTION, FOUND CRACK INDICATION AT LEFT WING, END OF STRINGER 10. 2L73 4F RTA22WE 20051109001852005110900185NM 2005 11 9 05FDEA03626 120051104A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 DURING HFEC INSPECTION FOUND CRACK AT RIGHT WING, END OF STRINGER 14 APPROXIMATELY 14 INCHES. REPAIR CARRIED OUT IAW SRM 57-20 -00 FIG. 10 VOL I. CLIP FABRICATED AS PER FEDEX EA 1-5720-90053 2L73 4F RTA22WE 20051109001862005110900186NM 2005 11 9 05FDEA03630 120051104A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 DURING HFEC INSPECTION, FOUND CRACK AT LEFT WING, END OF STRINGER 14 APPROXIMATELY 13 INCHES. REPAIRED AS PER SRM 57-20-00 FIG. 10 VOL. I. CLIP FABRICATION CARRIED OUT AS PER FEDEX E.A. 1-5720-90050 (TITLE: WINGS - STRINGER 14L REPAIR PER SRM VOL. I 57-20-00 FIG. 10 -FX ARB2689-502 CLIP FABRICATION). REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051109001942005110900194NM 2005 11 9 05FDEA03627 120051104A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 DURING HFEC INSPECTION, FOUND CRACK INDICATION AT LEFT WING, END OF STRINGER 11. 2L73 4F RTA22WE 20051109001952005110900195NM 2005 11 9 05FDEA03628 120051104A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 DURING HFEC INSPECTION, FOUND CRACK AT RIGHT WING, END OF STRINGER 44 APPROXIMATELY 2 INCHES. 2L73 4F RTA22WE 20051109001982005110900198EU 2005 11 9 05FDEA03640 120051104A5315 FLOORBEAM AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 LT FLOOR SUPPORT BEAM AT FS 23 BETWEEN CENTER AND LT MIDDLE ROLLER TRAY HAS CORROSION AROUND HOLES AS MARKED, REF N00530. REMOVED AND REPLACED FLOOR SUPPORT BEAM IAW SRM 51-72-10. 2L72 4F RTA35EU 20051109001992005110900199NM 2005 11 9 05FDEA03641 120051104A5311 FRAME BOEING727 727225 1384077NM BS 613 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 FOUND CRACK IN STUB FRAME UPPER FLANGE IN FWD CARGO BAY BILGE AT BS 613, STR 26R. REPLACED STUB FRAME AT BS 613 STR 26R PER SRM 51-30-2. 2L73 4F A3WE 20051109002062005110900206NM 2005 11 9 EIA2005236 120051008A5414 SKIN BOEING747 747212B 1384886NM NR 1 PYLON CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 LHW LE NOSE SKIN WEB FOUND CRACKED AT LBS 1116 IB OF NR 1 PYLON. REPLACED DEFECTIVE CRACKED RIB PER SRM 51-10-01, PG 9. 2L74 4F A20WE 20051109002102005110900210NM 2005 11 9 EIA2005240 120051006A5330 SKIN BOEING747 747212B 1384886NM BS 1820 DEFECTIVE A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 NEW ROTARY ACTUATOR AT BS 1820 WITH PILOT HOLE NOT ALIGNED WITH EXISTING FASTENER PATTERN AT SKIN. DEFECTIVE SKIN TRIMMED OFF AND REPAIRED PER RS R53-4-35387. 2L74 4F A20WE 20051109002122005110900212NM 2005 11 9 EIA2005242 120050830A5312 BULKHEAD BOEING747 747132 1384882NM BS 260 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09479EV 19898 FWD CARGO STA 260 S-34L TO S-40L CANTED PRESSURE BULKHEAD WEB FOUND CRACKED. REPAIRED PER EA-53-0997. 2L74 4F A20WE 20051109002142005110900214NM 2005 11 9 EIA2005244 120050830A5315 FLOORBEAM BOEING747 747132 1384882NM BS 420 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09479EV 19898 FOUND BS 420 UPPER DECK FLOORBEAM UPPER CHORD FASTENER HOLE CRACKED AT RBL 86 AND RBL 90. FLOORBEAM UPPER CHORD REPAIRED PER EA-53-0993. 2L74 4F A20WE 20051109002162005110900216NM 2005 11 9 05FDEA03650 120051107A5713 STRINGER DOUG MD11 MD11F 3023600NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 FOUND CRACK INDICATION AT END OF STRINGER -9 (UPPER STRINGER) WAS FOUND DURING HFEC INSPECTION AT LT WING TANK. REPAIR CARRIED OUT AS PER SRM 57-20-00. 2L73 4F RTA22WE 20051109002172005110900217NM 2005 11 9 05FDEA03651 120051107A5713 STRINGER DOUG MD11 MD11F 3023600NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 FOUND CRACK INDICATION AT END OF STRINGER -10 (UPPER STRINGER) WAS FOUND DURING HFEC INSPECTION AT LT WING TANK. CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-20-00. 2L73 4F RTA22WE 20051109002182005110900218NM 2005 11 9 05FDEA03652 120051107A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 FOUND CRACK INDICATION AT END OF STRINGER -12 (UPPER STRINGER) WAS FOUND DURING HFEC INSPECTION AT LT WING TANK. CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-20-00. 2L73 4F RTA22WE 20051109002202005110900220NM 2005 11 9 05FDEA03654 120051107A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 FOUND CRACK INDICATION AT END OF STRINGER -40 (UPPER STRINGER). DURING HFEC INSPECTION AT LT WING TANK. REPAIR CARRIED OUT AS PER SRM 57-20-00. 2L73 4F RTA22WE 20051109002232005110900223NM 2005 11 9 EIA2005210 120051010A5310 PLATE BOEING747 747212B 1384886NM BS 400 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 NWW LT AFT CORNER AT BS 400 INTERNAL SPLICE PLATE FOUND CRACK RUNNING FROM FWD EDGE GOING UNDER B/H CHORD. REPLACED DEFECTIVE INTERNAL SPLICE PLATE PER SRM 51-10-01, PG 9. 2L74 4F A20WE 20051109002242005110900224NM 2005 11 9 EIA2005211 120051010A5310 PLATE BOEING747 747212B 1384886NM BS 400 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 NWW RT AFT CORNER AT BS 400 INTERNAL SPLICE PLATE FOUND CRACK RUNNING FROM FWD EDGE GOING UNDER B/H CHORD. REPLACED DEFECTIVE SPLICE PLATE PER SRM 51-10-01, PG 9. 2L74 4F A20WE 20051109002252005110900225NM 2005 11 9 EIA2005212 120051009A5210 INTERCOSTAL BOEING747 747212B 1384886NM L4 DOOR CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 FOUND L4 DOOR INTERCOSTAL WEB FOUND CORRODED. REPAIRED DEFECTIVE INTERCOSTAL WEB PER SRM 51-40-03, FIG 1. 2L74 4F A20WE 20051109002282005110900228NM 2005 11 9 EIA2005215 120051006A5320 SUPPORT BRACKET BOEING747 747212B 1384886NM BS 1308 CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 KEEL BEAM PANEL SUPPORT FLOAT NUT BASE FOUND CORRODED AT STA 1308, LBL 15 TO RBL 15. REPLACED DEFECTIVE SUPPORT PER SRM 51-1--01, PG 9. 2L74 4F A20WE 20051109002302005110900230NM 2005 11 9 EIA2005217 120051009A5310 DOOR FRAME BOEING747 747212B 1384886NM LT DOOR CHIPPED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 LT DOOR FWD CUTOUT MIDDLE REVEAL FRAME EDGE CHIPPED. DEFECTIVE CHIPPED REVEAL REPLACED PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20051109002322005110900232NM 2005 11 9 EIA2005219 120051007A5311 FRAME BOEING747 747212B 1384886NM BS 434 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 LT SIDE BS 434 FRAME AT STR 26L FOUND FOUR EACH FASTENER HOLES CRACKED AT FRAME WEB. REFER TO ATTACHED SKETCH FOR DETAILS. REPAIRED DEFECTIVE FRAME WEB PER SRM 53-10-04, FIG 99 BS 434 FROM STR 23L TO 30L. 2L74 4F A20WE 20051109002372005110900237NM 2005 11 9 EIA2005155 120050830A5330 SKIN BOEING747 747132 1384882NM BS 2000 BULGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09479EV 19898 FOUND BS 2000 STR 45R FUSELAGE SKIN BULGE UP. BS 2000 STR 45R FUSELAGE SKIN REPAIRED PER EA-53-0991. 2L74 4F A20WE 20051109002382005110900238NM 2005 11 9 EIA2005199 120051008A5340 CLIP BOEING747 747212B 1384886NM BS 1940 DEFORMED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 FOUND BS 1940 STR 14R FRAME ATT TIE CLIP FOUND DEFORMED. REPLACED DEFECTIVE TIE CLIP PER SRM 51-10-01, PG 9. 2L74 4F A20WE 20051109002392005110900239NM 2005 11 9 EIA2005200 120051014A5315 FLOORBEAM BOEING747 747212B 1384886NM BS 380 DAMAGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 BS 380 UPPER DECK FLOORBEAM UPPER CHORD FWD FLANGE FLOOR PANEL ATT HOLE FOUND SHORT OF E/D AT LBL 44" AND 56". REPAIRED FLOORBEAM UPPER CHORD LBL 40 THRU 49, AND 51 THRU 61, PER SB747-53A2431 FIG 8. 2L74 4F A20WE 20051109002412005110900241NM 2005 11 9 EIA2005202 120051007A5340 CLIP BOEING747 747212B 1384886NM BS 1640 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 FOUND BS 1640 STR 14L, FRAME ATT TIE CLIP FOUND CRACKED. REPLACED DEFECTIVE TIE CLIP PER SRM 51-10-01, PG 9. 2L74 4F A20WE 20051109002422005110900242NM 2005 11 9 EIA2005203 120051014A5315 FLOORBEAM BOEING747 747212B 1384886NM BS 380 DAMAGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 BS 380 FLOORBEAM UPPER CHORD FWD FLANGE FLOOR PANEL AT HOLE FOUND SHORT OF E/D AT LBL 36", 30", 21", 16", RBL 9.5', 16.5", 20", AND 25". REPAIRED DEFECTIVE FLOORBEAMS UPPER CHORD PER SB 747-53A2452 FIG 7. 2L74 4F A20WE 20051109002452005110900245NM 2005 11 9 EIA2005206 120051008A5315 FLOORBEAM BOEING747 747212B 1384886NM BS 340 DAMAGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 FOUND LT BS 340 FLOORBEAM UPPER CHORD 1 EACH HOLE COMMON TO FRAME INNER CHORD FOUND CRACKED AT FLOORBEAM UPPER CHORD, RUNNING UP AND DOWN. REPAIRED DEFECTIVE FLOORBEAM UPPER CHORD PER SRM 53-10-07, FIG 23. 2L74 4F A20WE 20051109002472005110900247NM 2005 11 9 EIA2005208 120051007A5322 SHEAR TIE BOEING747 747212B 1384886NM BS 1520 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 FOUND BS 1520 STR 20R-22R SHEAR TIE FOUND CRACKED. REPLACED DEFECTIVE SHEAR TIE PER SRM 51-10-01, PG 9. 2L74 4F A20WE 20051109002482005110900248NM 2005 11 9 EIA2005209 120051007A5322 SHEAR TIE BOEING747 747212B 1384886NM BS 1500 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 FOUND BS 1500 STR 20-22L FRAME SHEAR TIE CRACKED. REPLACED DEFECTIVE SHEAR TIE PER SRM 51-10-01, PG 9. 2L74 4F A20WE 20051109002492005110900249NM 2005 11 9 EIA2005223 120051006A5320 SUPPORT BRACKET BOEING747 747212B 1384886NM BS 1333 CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 KEEL BEAM SUPPORT SPLICE BRACKET CORRODED AT BS 1333, RBL 16. REPLACED DEFECTIVE SUPPORT BRACKET PER SRM 51-10-01, PG 9. 2L74 4F A20WE 20051109002502005110900250NM 2005 11 9 EIA2005224 120051006A5320 SUPPORT BRACKET BOEING747 747212B 1384886NM BS 1330 CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 KEEL BEAM PANEL SUPPORT FLOAT NUT BASE, FOUND CORROSION AT STA 1330 LBL 15 TO RBL 15. REPLACED DEFECTIVE SUPPORT PER SRM 51-10-01, PG 9. 2L74 4F A20WE 20051109002512005110900251NM 2005 11 9 EIA2005225 120051006A5320 SUPPORT BRACKET BOEING747 747212B 1384886NM BS 1308 CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 KEEL BEAM PANEL SUPPORT FLOAT NUT BASE FOUND CORRODED AT STA 1308, LBL 15 TO RBL 15. REPLACED DEFECTIVE SUPPORT PER SRM 51-10-01, PG 9. 2L74 4F A20WE 20051109002552005110900255NM 2005 11 9 EIA2005229 120051007A5720 SUPPORT BRACKET BOEING747 747212B 1384886NM CANOE FAIRING CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 LHW NR 2 FLAP TRACK CANOE FAIRING AFT SUPPORT FRAME CRACKED. REPAIRED DEFECTIVE CRACKED FRAME PER SRM 51-40-04, FIG 2. 2L74 4F A20WE 20051109002562005110900256NM 2005 11 9 EIA2005230 120051008A5711 SPAR BOEING747 747212B 1384886NM RT WING CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 RHW NR 3 MAIN TANK MID SPAR WEB UPPER FASTENER HOLES (2 EA) CRACKED BETWEEN WS 614 AND WS 642. REPAIRED DEFECTIVE CRACKED WEB PER SRM 57-1-06, FIG 5. 2L74 4F A20WE 20051109002572005110900257NM 2005 11 9 EIA2005231 120051007A5330 LAP JOINT BOEING747 747212B 1384886NM BS 370 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 FX BS 370 ST 6L SKIN LAP JOINT (1EA) FASTENER HOLE CRACKED AT TOP ROW. FOUND BS 365-378 BETWEEN STR 5L AND STR 6L SKIN LAP JOINT REPAIRED PER SRM 53-30-03. 2L74 4F A20WE 20051109002582005110900258NM 2005 11 9 EIA2005232 120051007A5347 CARGO TRACK BOEING747 747212B 1384886NM BS 2100-2120 CHIPPED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 FOUND BS 2100-2120 LBL 11 TIE DOWN TRACK CROWN FOUND CHIPPED. REPAIRED DEFECTIVE TIE DOWN TRACK PER SRM 53-19-05, FIG 14. 2L74 4F A20WE 20051109002592005110900259NM 2005 11 9 EIA2005233 120051007A5311 FRAME BOEING747 747212B 1384886NM BS 2230 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 FOUND RT SIDEWALL FRAME BS 2230 STR 16R TO STR 17R AROUND LIGHTENING HOLE CUTOUT CRACKED. REPAIRED PER 53-10-04, FIG 91. 2L74 4F A20WE 20051109002622005110900262NM 2005 11 9 05FDEA03632 120051104A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 DURING HFEC INSPECTION, FOUND CRACK AT LEFT WING, END OF STRINGER 43. REPAIR CARRIED OUT IAW SRM 57-20- 00 FIG. 10 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051109002652005110900265EU 2005 11 9 05FDEA03635 120051104A5347 SEAT TRACK AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 FOUND MAIN CABIN SEAT TRACK 1 BETWEEN FR 74 TO 79 HAS 6 EA AREAS OF CORR REF N00520. REPAIRED SEAT TRACK IAW SRM 53-10-16. 2L72 4F RTA35EU 20051109002682005110900268NM 2005 11 9 05FDEA03661 120051107A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 FOUND CRACK INDICATION FOUND AT END OF STRINGER -12 (UPPER STRINGER) DURING HFEC INSPECTION AT RT WING TANK. REPAIRED AS PER SRM 57-20-00. 2L73 4F RTA22WE 20051109002692005110900269NM 2005 11 9 05FDEA03642 120051104A5315 REPAIR BOEING727 727225 1384077NM BS 1110 IMPROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 FOUND EXISTING FLOORBEAM REPAIR AT BS 1110, RBL 16 - LBL 35, WL 208. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. INSTALLED FLOORBEAM REPAIR AT B.S. 1110 RBL 16-LBL 35 WL 208 PER SRM 53-10-8. 2L73 4F A3WE 20051109002712005110900271EU 2005 11 9 KBM2005F00332 120051030A6520350A33215300 BEARING SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE TAIL ROTOR CUT E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1937SH 897 2300 LAMINATED BEARING, UNIT HAS MULTIPLE CUTS, REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20051109002722005110900272NM 2005 11 9 05FDEA03643 120051104A5313 STRINGER BOEING727 727225 1384077NM BS 915 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 FOUND LT W/W, 18A SHELF IS CRACKED, STA 915, LBL 63, WL 189. REMOVED AND REPLACED LEFT MLG W/W 18A SHELF STA 870-940 LBL 63 WL 189 PER SRM 51- 30-2 2L73 4F A3WE 20051109002732005110900273NM 2005 11 9 05FDEA03644 120051104A5315 FLOORBEAM BOEING727 7272S2F 1384O81NM BS 1090-1110 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25213FE 22935 LATERAL / LONGITUDINAL FLOORBEAM HAS SEVERAL CORRODED NUT PLATES AND SURFACE UNDER NUT PLATES ,FROM STA. 1090 TO 1110 BL 0 TO RBL 15., REMOVED CORROSION ON LWR. CHORD .090 BEFORE REWORK .040AFTER REWORK OUT OF LIMITS. IAW SRM 53-10-1. REMOVED CORRODED NUT PLATES AND CORROSION ON LWR SURFACE OF BL 0 CHORD .090 BEFORE REWORK.050 AFTER REWORK OUT OF LIMITS IAW SRM 53-10-.REMOVED FLOORBEAM IAW SRM 51-30-2 STA 1080-1166. REMOVED SPLICE IAW SRM 51-30-2 REMOVED ANGLE& STIFFENER STA. 1070 IAW SRM 51-30-2. REMOVED CEILING SUPPORT IAW SRM 51-30- 2.REMOVED SPLICE PLATE STA.1160 IAM SRM 51-30-2. LOCATED & DRILLED NEW LWR. CHORD 51-10-5.INSTALLED ANGLE, STIFFENER LWR. CHORD & SPLICES IAW SRM 51-30- 2 2L73 4F A3WE 20051109002742005110900274NM 2005 11 9 05FDEA03645 120051106A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 FOUND MAIN DECK COMPARTMENT, SEAT TRACK FOUND CORROSION AT STA 5/0 - 5/73, X=8.5. REPAIR CARRIED OUT IAW SRM 53-70-00 VOL. I FIG. 1 AND SRM 51-33-01 VOL. II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051109002762005110900276NM 2005 11 9 05FDEA03647 120051106A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 FOUND MAIN DECK COMPARTMENT, SEAT TRACK FOUND EDGE DAMAGED AT STA 5/23, X= -47.5. REPAIR CARRIED OUT AS PER SRM 53-70-00 VOL. I FIG. 1 AND SRM 51-33-01 VOL. II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051108001432005110800143SO 2005 11 8 SIMA200526404 120050915A5320 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO FR 20 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21656AE 145740 THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. PERFORMED A CUT OUT OF LEFT OMEGA BEAM TO REMOVE CORROSION. PREPARED DOUBLER, FILLER, REPAIR PLATE AND TWO SHIMS. REPAIR DONE IAW EMB145 SRM, SRM 145/1142 REV 30 CHAPTER 53-00-10 FIG 201. (M) 2L72 4T RTT00011AT 20051108001532005110800153EU 2005 11 8 GTIA050223 120050802A5270 PROXIMITY SWITCH AIRBUSA321 A321211 3930370EU R1 DOOR OUT OF ADJUST A GTIAO OTHER P NO WARNING INDICATION CLCLIMB 1 GL23587NK 2476 R1 DOOR NOT SHOWING CLOSED INFLIGHT ON ECAM. RECYCLED EMERGENCY LIGHT TEST SWITCH ON FAP AND DOOR LIGHTS WORKED NORMALLY. PERFORMED ADJUSTMENT OF R1 DOOR PROX SWITCH PER AMM. SYSTEM OPS CHECK GOOD, LP NR 179708-3. (M) 2L72 4F RTA28NM 20051108001542005110800154EA 2005 11 8 ASOA05874 120051015A25602618 FLASHLIGHT CNDAIRCL600 CL6002B19 1900309EA COCKPIT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11922EV 7822 FLT 4290 - DURING A GROUND INSPECTION IN ATL, THE FIRST OFFICERS FLASHLIGHT WAS FOUND TO BE DIFFICULT TO OPERATE. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS FLASHLIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051108001592005110800159EU 2005 11 8 ASOA05872 120051014A3350 LAMP AEROSPATR72 ATR72 EU EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27642AS 395 FLT 4293 - DURING A GROUND INSPECTION IN ATL, THE FLIGHT ATTENDANT REPORTED LAMPS BURNED OUT IN THE EMERGENCY TRACK LIGHTING. MAINTENANCE DID AN OPERATIONAL CHECK OF THE EMERGENCY TRACK LIGHTING WITH NO DEFECTS FOUND. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20051108001652005110800165SO 2005 11 8 SIMA200525703 120050914A335077812 POWER SUPPLY EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT DISCHARGED A SIMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW21717AE 145272 BOS - FLT 4592 - EMERGENCY LIGHT STRIP AT ROW 7 AND 8 INOPERATIVE. REPLACED NR 3 EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20051108001752005110800175WP 2005 11 8 GTIA050235 120050818A7700 DISPLAY DOUG DC9 DC983 3022083WP ENGINE MALFUNCTIONED A GTIAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL23836NK 53045 DTW - ABORTED TAKEOFF, LEFT ENGINE EPR STUCK AT 1.71 DURING TAKEOFF, CAPTAIN CALLED FOR SET FLEX POWER, F/O PUSHED THROTTLES UP EPR STAYED AT 1.71, N2 FLASHING AT 010 OR 001 ABORTED TAKEOFF AT 70 KNOTS, AIRCRAFT TAIL SWAP WITH N811NK. REMOVED AND REPLACED ENGINE DISPLAY PANEL, OPS CHECK GOOD. (M) 2L72 4F RTA6WE 20051108001762005110800176 2005 11 8 GTIA050218 420050722A2340 BUTTON DOUG DC9 DC982 3022082WP PA SYSTEM SPARKS A GTIAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL23803NK 48087 F/A "A" CALL C/P TO INFORM OF "SMOKE SMELL" BEWEEN ROWS 28 PLUS 31. SEEMED TO ORGINATE FROM F/A STATION NR 2 PILOT INFORMED F/A TO PULL ALL C/B`S IN AREA, COFFEE POT (1 & 2). ONE AND HALF MINUTE AFTER PULLING C/B`S, SMELL WENT AWAY. MONITORED AREA FOR ANY TRACK OF SMOKE/FIRE FOR DURATION OF FLIGHT (1HR). AT SOME POINT F/A NOTICED A SPARK NEAR F/A STATIO NR 2 HANDSET AREA, PAX COMPLAINED OF SMOKE BRIEFLY. REST OF FLIGHT NORMAL. REMOVED AND REPLACED MID F/A P/A BUTTON. (M) 2L72 4F A6WE 20051108001782005110800178EA 2005 11 8 ASOA05865 120051013A3350OL3071BPEGPL LAMP CNDAIRCL600 CL6002B19 1900309EA GALLEY BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27870AS 7530 DURING A GROUND INSPECTION IN SHV, THE EMERGENCY EXIT LIGHT AT THE FORWARD SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT AT THE FORWARD SERVICE DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051108001882005110800188SO 2005 11 8 SIMA200526901 120050923A3350 BATTERY EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT UNKNOWN A SIMAK NONE L NO TEST TXTAXI/GRND HDL 1 SW21725AE 145312 EMERGENCY EXIT LIGHT FLOOR STRIP AT OVERWING EXIT DOES NOT ILLUMINATE ON TEST. REPLACED NR 3 BATTERY POWER SUPPLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20051108001942005110800194WP 2005 11 8 GTIA050228 120050728A5320 CHANNEL DOUG DC9 DC983 3022083WP BS 484 CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FOUND MAIN CABIN, LEFT SIDE STATION 484 WEB MEMBRANE PANEL HAT CHANNEL CRACKED. FABRICATED REPAIR DOUBLER. TREATED, PRIMED AND INSTALLED REPAIR DOUBLERS. (M) 2L72 4F RTA6WE 20051108001982005110800198SO 2005 11 8 SIMA200527703 120050929A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO FS 24 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21820AE 145576 THE LEFT OMEGA BEAM AFT OF FRAME 24 WAS FOUND CORRODED. PERFORMED A CUT OUT TO REMOVE THE CORROSION. PREPARED A DOUBLER, FILLER AND SHIMS FOR REPAIR. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 30, CHAPTER 53-00-10 FIG 202. (M) 2L72 4F RTT00011AT 20051108002022005110800202WP 2005 11 8 GTIA050234 120050806A7900 STRAINER DOUG DC9 DC981 3022081WP RT ENGINE CLOGGED A GTIAO OTHER O OTHER TXTAXI/GRND HDL 1 GL23810NK 48015 RIGHT ENGINE OIL STRAINER CLOGGING LIGHT CAME ON DURING TAXI, RIGHT ENGINE WAS SHUTDOWN AND AIRCRAFT RETURNED TO GATE. REMOVED NR 2 OIL FILTER AND INSPECTED, INSPECTION SHOWED NO CONTAMINATION, INSTALLED NEW OIL FILTER, LEAKS CHECK GOOD AND OPS CHECK GOOD. (M) 2L72 4F A6WE 20051108002072005110800207EA 2005 11 8 ASOA05882 120051016A3350100865 POWER SUPPLY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27836AS 7263 DURING A C-CHECK IN MCN, THE NR 2 POWER SUPPLY WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 POWER SUPPLY. OPERATIONAL CHECKS GOOD. (M) 2L72 4F RTA21EA 20051108002092005110800209SO 2005 11 8 SIMA200526405 120050918A532014525380003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO FS 24-25 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21713AE 145249 THE CENTER OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE OMEGA BEAM TO REMOVE THE CORROSION. FABRICATED A DOUBLER, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2005-145/4777 PARA 7 DATED 15, 2005. (M) 2L72 4F RTT00011AT 20051108002132005110800213SO 2005 11 8 SIMA200526402 120050918A532014525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO FS 25 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21713AE 145249 THE LEFT OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE OMEGA BEAM TO REMOVE THE CORROSION. FABRICATED A DOUBLER, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2005-145/4777 PARA 8 DATED SEPT 15, 2005. (M) 2L72 4F RTT00011AT 20051108002192005110800219WP 2005 11 8 GTIA050246 120050811A5315 FLOORBEAM DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 FTW - FOUND FLOORBEAM LEFT OF DOT 204 HAS SEVERAL AREAS OF CORROSION. FLOORBEAM CORROSION FOUND OUT OF LIMITS. MANUFACTURED FLOORBEAM. TREATED, PRIMED AND INSTALLED FLOORBEAM. (M) 2L72 4F RTA6WE 20051108002242005110800224WP 2005 11 8 GTIA050253 120050912A5320 WEB DOUG DC9 DC983 3022083WP BS 212 CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23808NK 49504 FOUND WEB CRACKED STATION 212 L15L. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLR AND FILLER. TREATED, PRIMED AND INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20051108002312005110800231WP 2005 11 8 GTIA050215 120050720A2613 OVERHEAT SENSOR DOUG DC9 DC983 3022083WP TAILCONE MALFUNCTIONED A GTIAO OTHER N FALSE WARNING CLCLIMB 1 GL23802NK 53168 CLIMBING THROUGH 27000 FEET WITH ENGINE AND AIRFOIL ICE ON TAIL COMPARTMENT TEMP HI LIGHT ILLUMINATED, PERFORMED MEMORY ITEMS REQUESTED LOWER ALTITUDE AND VECTOR TO MCO, LIGHT EVENTUALLY WENT OUT FOLLOWED BY FLOW LIGHT ON AUTO PRESSURE CONTROLLER, DIVERTED INTO MCO. LEAK CHECK LT/RT PACKS, WING AND TAIL ANTI-ICE DUCTS AND ASSOCIATED DUCTS FOR LEAKS VIA THE APU AND ENGINE BLEED AIR. NO LEAKS NOTED. REMOVED AND REPLACED LT/RT TAIL COMPARTMENT OVERHEAT SENSORS, SYSTEM OPS CHECK GOOD. (M) 2L72 4F RTA6WE 20051108002352005110800235WP 2005 11 8 GTIA050209 120050628A5330 SKIN DOUG DC9 DC983 3022083WP BS 97 CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23815NK 49415 RIGHT NOSE GEAR CUTOUT CRACKED AT STATION 97.99. REMOVED RIGHT AFT NLG DOOR. STOPPED DRILLED CRACK. FABRICATED DOUBLER. REINSTALLED RIGHT AFT NLG DOOR. TREATED, PRIMED AND INSTALLED DOUBLER. (M) 2L72 4F RTA6WE 20051108002362005110800236WP 2005 11 8 GTIA050203 120050626A2120 DUCT DOUG DC9 DC982 3022082WP A/C PACK RUPTURED A GTIAO OTHER J WARNING INDICATION CLCLIMB 1 GL23817NK 49141 FLL - LEFT PACK OVER TEMP WITH LEFT PACK ON AND CABIN WOULD NOT HOLD PRESSURE WITH ONE PACK, AIRCRAFT SWAP WITH 821. FOUND LEFT PACK DUCT RUPTURE FROM LEFT WATER SEPARATOR TO CHECK VALVE. REMOVED AND REPLACED DUCT, LEAK CHECKED AND OPS CHECK, SYSTEM OK. (M) 2L72 4F A6WE 20051108002392005110800239WP 2005 11 8 GTIA050243 120050826A5730 SKIN DOUG DC9 DC983 3022083WP LT WING CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23834NK 49847 FTW - FOUND RIGHT WING REFUELING STATION DOOR CUTOUT INBOARD CORNER DOUBLER CRACKED. REMOVED CRACKED SECTION AND FABRICATED REPAIR DOUBLER. TREATED, PRIMED AND INSTALLED DOUBLER. (M) 2L72 4F RTA6WE 20051108002472005110800247EA 2005 11 8 ASOA05855 120051010A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 280 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27836AS 7263 DURING A C-CHECK IN MCN, THE FS 280 FLOOR SUPPORT BEAM ANGLE, BETWEEN LBL 9 AND RBL 9, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE WILL REPAIR THE FS 280 FLOOR SUPPORT BEAM ANGLE, BETWEEN LBL 9 AND RBL 9, IAW BOMBARDIER REO 601R-53-11-926. (M) 2L72 4F RTA21EA 20051108002602005110800260EA 2005 11 8 ASOA05847 120050921A5310 DOOR FRAME CNDAIRCL600 CL6002B19 1900309EA BS 338 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27855AS 7395 DURING A C-CHECK IN HTO, THE FS 338 PASSENGER DOOR FRAME WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FS 338 PASSENGER DOOR FRAME IAW BOMBARDIER REO 601R-52-11-402. (M) 2L72 4F RTA21EA 20051108002652005110800265EA 2005 11 8 ASOA05800 120050924A5330 DOUBLER CNDAIRCL600 CL6002B19 1900309EA BS 449-529 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27835AS 7258 DURING A C-CHECK IN MCN, THE LEFT SIDE DOUBLERS, FROM 449-529, BL 45 ON THE PRESSURE FLOOR WERE FOUND TO BE CORRODED. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO BOMBARDIER TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. AFTER MAINTENANCE BLENDED, ALODINED, AND PRIMED THE LEFT SIDE DOUBLERS, FROM 449-529, BL 45, IAW REO 601R-53-41-359, FOUND TO BE WITHIN LIMITS. (M) 2L72 4F RTA21EA 20051108002792005110800279SW 2005 11 8 ALG2005F00083 120051006A6410 BLADE BELL 206 206L4 1182110SW ALLSN 250C 250C30P 03013GL TAIL ROTOR DAMAGED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03275AL 52285 DURING THE DAILY MAINTENANCE INSPECTION, IT WAS DETERMINED THE TAIL ROTOR BLADE TIP WAS DAMAGED BY STRIKING AN UNDETERMINED OBJECT. COMPLIED WITH THE CONDITIONAL INSPECTION, 5-28 SUDDEN STOPPAGE/ACCELERATION-TAIL ROTOR. (K) 1G71 3U3 UNCH2SW E1GL 20051108002822005110800282EU 2005 11 8 TRB2005F00007 120051007A3297D23197000 WIRE HARNESS AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE LT MLG INTERMITTENT A TRBAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO29377AT 377 (REF NR: SDR2005066) AFTER TAKEOFF, THE LANDING GEAR DID NOT RETRACT AND THE IDLE GATE DID NOT MOVE INTO THE FLIGHT POSITION. AIRCRAFT RETURNED TO AIRPORT. REPLACED MAIN LANDING GEAR HARNESS. (K) 2H72 4T4 TRTA53EU E20NE 20051108003222005110800322EU 2005 11 8 TRB2005F00008 120050914A2497S7618065000800 SWITCH AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE CENTER PEDESTAL INTERMITTENT A TRBAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO29448AM 448 ( REF NR: SDR2005064) ON TAKEOFF ROLL, THE ATPCS DID NOT ARM. TAKEOFF ABORTED. REPLACED MICROSWITCH BOX UNIT. (K) 2H72 4T4 TRTA53EU E20NE 20051108003432005110800343NM 2005 11 8 USAA051339 120051107A5542 SKIN BOEING737 7373B7 1384580NM RUDDER DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 LEFT RUDDER SKIN 96 INCHES FROM THE BASE AND 11 INCHES FROM THE TRAILING EDGE DAMAGED. REMOVED DAMAGED, LAID UP AND INSTALLED REPAIR IAW SRM 55-40-01. DEFECT SIZE: 1.5 INCH. 2L72 4F RTA16WE 20051108003502005110800350NM 2005 11 8 USAA200511004 120051106A5330 SKIN BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19427US 24549 A 1.5 INCH CRACK FOUND AT BS 944 S-24L. INSTALLED DOUBLER PER EA 97050. 2L72 4F RTA16WE 20051108003562005110800356 2005 11 8 RAIA00511003 420051105A31607011672112 SYMBOL GENERATOR JETAIRJETSTMJETSTM4101 1500501EU NR 2 INOPERATIVE A RAIAA UNSCHED LANDING O OTHER CRCRUISE 1 CE03571HK183152048 41090 FLT - 5445 - STL - NAV NR 2 WENT BLANK. MAINTENANCE REMOVED AND REPLACED NR 2 SYMBOL GENERATOR. 2L72 4T RTA41NM 20051108003572005110800357EU 2005 11 8 RAIA00511004 120051105A2910141910013 HOSE JETAIRJETSTMJETSTM4101 1500501EU HYDRAULIC SYS CHAFED A RAIAA UNSCHED LANDING J WARNING INDICATION DEDESCENT 1 CE03572HK 41091 FLT- 3603- SYR - RT AND LT HYD SYSTEM FAIL. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE HYD PUMP PRESSURE AND SUCTION HOSES. 2L72 4T RTA41NM 20051108003662005110800366NM 2005 11 8 2005UALA01212 120051101A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29198UA 28716 EMERGENCY EEL LIGHT INOP AT SEAT 26 AB FWD. REPLACED EEL LAMP. 2L74 4F4 FRTA20WE E24NE 20051108003762005110800376NM 2005 11 8 2005UALA01221 120051103A5754 SKIN BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE L/E SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29787UA 26939 NR 5 SLAT LWR SURFACE DELAMINATED AT INBOARD END NEAR TRAILING EDGE. INTERIM REPAIR PER 777 AMM 57-43-99. ACP AN INITIAL INSP AT 50 CYCLE AND EVERY 500 FLT CYCLE UNTIL PERMANENT REPAIR ACPL AT NEXT HMV (5JUNE06). OK TO CF PER AMM AND SFOIQ WALSH. 2L72 4F4 FRTT0001SE E46NE 20051109000092005110900009CE 2005 11 9 GUU2005F00051 120050923A55241016200131 BRACKET BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA RT ELEVATOR CORRODED A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO171654020366 UE172 AT SCHEDULED MAINTENANCE, RT ELEVATOR, CENTER HINGE BRACKET SHOWS SIGN OF EXFOLIATION. REPLACED RT ELEVATOR CENTER HINGE BRACKET. (K) 2L72 4T3 TRTA24CE E2NE 20051109000112005110900011 2005 11 9 KBM2005F00323 420051012A3421A321EHM GYRO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE HORIZON SPINNING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19966SH2257 3787 GYRO HORIZON, UNIT SPINS INFLIGHT. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051109000262005110900026EU 2005 11 9 KBM2005F00277 120050904A6520350A33215300 BEARING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE TAIL ROTOR CUT E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH 2884 T/R HUB HINGE LAMINATED BEARING HAS MULTIPLE CUTS, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051109000302005110900030EU 2005 11 9 KBM2005F00261 120050906A2432RG355 BATTERY SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1B 6OO30NE MASTER ODOR E KBMAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP19230SH145 2337 BATTERY, REMOVED DUE TO SULFUR SMELL, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051109000372005110900037EA 2005 11 9 A6WA200540312 120050930A2410820465 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE COCKPIT INOPERATIVE A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31455AW4664 4097 7848 ADG INADVERDENTLY DEPLOYED DURING CLIMBOUT, PERFORMED QRH AMBER CAS MESSAGE FOR L WINDOW HEAT, L AOA HEAT, PITOT BASE HEAT ILLUMINATED. ADG POWERED AC ESS BUS. EMERGENCY LIGHTS ILLUMINATED BEFORE ADG DEPLOYMENT. REMOVED AND REPLACED AUTO DEPLOY CONTROL PANEL IAW MM 24-23-15 STOWED ADG IAW MM 24-23-01. PERFORMED INSPECTION OF ADG IAW 05-51-19. OPS CHECK GOOD. (K) 2L72 4F4 FRTA21EA E15NE 20051109000562005110900056NE 2005 11 9 KBM2005F00328 220051027A75329550164960 BLEED VALVE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE ENGINE MALFUNCTIONED A KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19115SH 3141 9666 FOUND ENGINE PNEUMATIC BLEED VALVE IS NOT FUNCTIONING OR WOULD NOT CLOSE TO DESIRE. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051109000692005110900069 2005 11 9 KBM2005F00321 420051023A3452066106200 TRANSPONDER SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE ATC FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19751H 3403 UNIT FAILED TRANSPONDER CHECK. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051109000762005110900076SO 2005 11 9 SIMA200528303 120051003A531514521721009 FLOORBEAM EMB 135 EMB135KL 3260302SO IAE V2524 V2524A5 NE GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21823AE8173 145582 THE GALLEY FORWARD DIGITAL WAS FOUND TO BE CORRODED. PERFORMED A CUT OUT OF THE FORWARD DIGITAL TO REMOVE THE CORROSION. FABRICATED A FILLER AND DOUBLER. REPAIR DONE IAW SRM. (SW21200600333) (K) 2L72 4F4 FRTT00011ATE40NE 20051109000792005110900079 2005 11 9 BSY2005F00000 420051017A3417702490031304 ADC LEAR 35 35A 5170602CE GARRTTTFE731TFE731* 01518WP LT AVIONICS BAY DEFECTIVE E BSYAO OTHER O OTHER NRNOT REPORTED 1 GL0727TT 0122 THE PILOTS ALTIMETER BLANKED OUT AND ALTITUDE ALERTER DIED. THE ADC WAS FOUND TO BE DEFECTIVE AND REPLACED. THE SYSTEM WAS TESTED AND INSPECTED AND FOUND TO COMPLY WITH FAR 91 AND TO REMAIN RVSM COMPLAINT. THERE HAVE BEEN NO PRIOR REPORTS OF PROBLEMS WITH THIS SYSTEM. (GL07200602750) (K) 2L72 4F4 F A10CE E6WE 20051109000822005110900082SO 2005 11 9 SIMA200528304 120051004A532014525480003 SILL EMB 135 EMB135KL 3260302SO IAE V2524 V2524A5 NE BAGGAGE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21823AE8173 145582 THE BAGGAGE DOOR CUT OUT LOWER SILL WAS FOUND CORRODED. REMOVED THE EXISTING LOWER SILL AND CLEANED THE AREA. INSTALLED SERVICEABLE SILL IAW SRM. (SW21200600333) (K) 2L72 4F4 FRTT00011ATE40NE 20051109000882005110900088 2005 11 9 KBM2005F00311 420050930A2312064105430 RADIO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE VHF SYSTEM FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19351WM10 2167 VHF RADIO, UNIT DISPLAY BLANKS OFF AND UNREADABLE. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051109000942005110900094SW 2005 11 9 ALG2005F00079 120051015A6321206340301103 CALIPER BELL 206 206L4 1182110SW ALLSN 250C 250C30P 03013GL ROTOR BRAKE LOOSE E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03265AL 52280 DURING DAILY INSPECTION THE MECHANIC FOUND ROTOR BRAKE BOLTS LOOSE AND A PAD WAS MISSING, REMOVED AND REPLACED BOTH CALIPERS WITH SERVICEABLE SET AND THE AC WAS RETURNED TO SERVICE. (K) 1G71 3U3 UNCH2SW E1GL 20051109000952005110900095SO 2005 11 9 SIMA200528601 120051010A2150 A/C PACK EMB 135 EMB135KL 3260302SO IAE V2524 V2524A5 NE BOTH CONTAMINATED A SIMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21824AE 145584 ON CLIMB OUT FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN. RECEIVED LAV SMOKE INDICATION ON EICAS. RAN BOTH ENGINES WITH BOTH PACKS ON TO BURN OUT RESIDUAL OIL FROM BLEED DUCTS. RESIDUAL OIL IN DUCTS WAS FROM THE ENGINE THAT WAS PREVIOUSLY MOUNTED ON THE LT SIDE. AC RETURNED TO SERVICE. (K) 2L72 4F4 FRTT00011ATE40NE 20051109001192005110900119NM 2005 11 9 05FDEA03663 120051107A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 CRACK INDICATION FOUND AT END OF STRINGER -14 (UPPER STRINGER). DURING HFEC INSPECTION AT RIGHT WING TANK. REPAIRED AS PER SRM 57-20-00. 2L73 4F RTA22WE 20051109001222005110900122WP 2005 11 9 05FDEA03667 120051107A5754 SKIN DOUG DC10 DC1010 3022110WP NR 1 SLAT DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 FOUND A SPLICE DOUBLER REPAIR AT RIGHT WING NR 1 SLAT LOWER SURFACE ON SLAT SKIN WING STATION XIS247 AT NR 3 SLAT TRACK AREA. PERFORMED A GVI OF EXISTING REPAIR IAW EO8-5100-7-5001 CRITERIA REQUEST AND FOUND IN COMPLIANCE WITH SRM 57-10-00 FIG 29. 2L73 4F A22WE 20051109001352005110900135NM 2005 11 9 SWAA053521 120051107A53306545765 SKIN BOEING737 7373Y0 1384671NM BS 500D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29664WN 23495 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 16L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051109001372005110900137 2005 11 9 SWAA053523 420051107A256563550 SLIDE BOEING737 7377H4 1384404NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29718SW 27852 DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051109001762005110900176NM 2005 11 9 EIA2005177 120051011A5315 FLOORBEAM BOEING747 747212B 1384886NM BS 340 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 BS 340 FLOORBEAM UPPER CHORD HORIZONTAL AFT FLANGE RBL 45 FLOOR PANEL AFT HOLE CRACKED RUNNING FWD APPROX 0.040 INCH LONG. DEFECTIVE FLOORBEAM UPPER CHORD REPAIRED AS PER SB 747-53A2431 FIG 9 (HORIZONTAL AFT FLANGE RBL45). 2L74 4F A20WE 20051109001792005110900179EU 2005 11 9 05FDEA03637 120051104A2550 ROLLER TRAY AIRBUS310 A310203 3930313EU CARGO BAY CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 LT CENTER ROLLER TRAY OB LEG HAS 8 EA AREAS OF CORROSION AS MARKED FS 38.1 TO FS 33 REF N00465. REMOVED AND REPLACED ROLLER TRAY IAW AMM 25-52-21-4. 2L72 4F RTA35EU 20051109002132005110900213NM 2005 11 9 EIA2005243 120050830A5312 BULKHEAD BOEING747 747132 1384882NM BS 260 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09479EV 19898 FWD CARGO STA 260 S-34R TO S-40R CANTED PRESSURE BULKHEAD WEB FOUND CRACKED. REPAIRED PER EA-53-0997. 2L74 4F A20WE 20051109002212005110900221NM 2005 11 9 05FDEA03655 120051107A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 FOUND CRACK INDICATION AT END OF STRINGER -50 (LOWER STRINGER). DURING HFEC INSPECTION AT LHS WING TANK. CRACK AT END OF STRINGER 50 TRIMMED OUT AND REPAIRED AS PER SRM 57-10-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2L73 4F RTA22WE 20051109002402005110900240NM 2005 11 9 EIA2005201 120051007A5322 SHEAR TIE BOEING747 747212B 1384886NM BS 1520 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 FOUND BS 1520 STR 20-22L, FRAME SHEAR TIE FOUND CRACKED. REPLACED DEFECTIVE SHEAR TIE PER SRM 51-10-01, PG 9. 2L74 4F A20WE 20051109002522005110900252NM 2005 11 9 EIA2005226 120051006A5320 SUPPORT BRACKET BOEING747 747212B 1384886NM BS 1384 CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 KEEL BEAM PANEL SUPPORT ATTACH ANGLE, FOUND SURFACE CORROSION AT STA 1384, LBL 16 TO RBL 16. REPLACED DEFECTIVE SUPPORT PER SRM 51-10-01, PG 9. 2L74 4F A20WE 20051109002532005110900253NM 2005 11 9 EIA2005227 120051007A5311 FRAME BOEING747 747212B 1384886NM BS 2230 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 RT SIDEWALL FRAME BS 2230, STR 16R TO STR 17R, FOUND CRACKED AROUND LIGHTENING HOLE CUTOUT. REPAIRED DEFECTIVE CRACKED REVEAL PER SRM 53-10-04 FIG 91. 2L74 4F A20WE 20051109002642005110900264EU 2005 11 9 05FDEA03634 120051104A5347 SEAT TRACK AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 FOUND MAIN CABIN SEAT TRACK 4R AT FS 76 TO 77 HAS MILD CORR IN 2 AREAS REF N00518. REPAIRED SEAT TRACK IAW SRM 53-10-16. 2L72 4F RTA35EU 20051109002662005110900266WP 2005 11 9 05DEA01860 120050708A5330 DOUBLER DOUG DC10 DC1010 3022110WP BS 959 UNKNOWN A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25571FE 47830 DURING AIRPLANE'S CONVERSION FROM P TO F FOUND EXISTING REPAIR AT FUSELAGE STA 959, STR 41-38 RT. REPAIR IS CONFORM TO SRM 53-50-00 FIG 8 SH 14. 2L73 4F A22WE 20051109002672005110900267WP 2005 11 9 05FDEA03660 120051107A5312 PRESSURE PANEL DOUG DC10 DC1030F 3023504WP RT MLG WW CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 RT MLG WHEEL WELL 2EA CRACKS ON VERTICAL WEB AT STA 1485 X-95 OUTBOARD SIDE. REPAIRED IAW SRM 53-50-00 FIG 2A. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F161133-29 REPAIR WEB, F161133-3 FILLER (QTY 2), F161133-31 STRAP, F161133-31A STRAP AND F161133-31B STRAP IAW SRM 53-50-00 FIG 2A. 2L73 4F RTA22WE 20051109002932005110900293WP 2005 11 9 05FDEA03680 120051107A5315 DOUBLER DOUG DC10 DC1010 3022110WP FLOORBEAM UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 AFT CARGO COMPT BILGE AREA, FLOOR SUPPORT BEAM FOUND A SPLICE DOUBLER REPAIR LBL 36 STA 1841. PERFORMED A GVI OF EXISTING SPLICE IAW EO8-5100-7-5001 CRITERIA, FOUND SPLICE DOUBLER REPAIR IN COMPLIANCE WITH SRM 53-60-01 PAGE 7. 2L73 4F A22WE 20051109002942005110900294WP 2005 11 9 05FDEA03683 120051107A5315 DOUBLER DOUG DC10 DC1010 3022110WP FLOORBEAM UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 CENTER CARGO COMPT, FLOOR SUPPORT BEAM FOUND A SPLICE DOUBLE REPAIR AT FUSELAGE STA 1701 BETWEEN X24 AND X48. PERFORMED A GVI OF EXISTING SPLICE IAW EO8-5100-7-5001 CRITERIA, FOUND SPLICE DOUBLER IN COMPLIANCE WITH SRM 53-60-01 PAGE 7. 2L73 4F A22WE 20051109002952005110900295WP 2005 11 9 05FDEA03684 120051107A5347 PLUG DOUG DC10 DC1010 3022110WP SEAT TRACK UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 SEAT TRACK PLUG REPAIR LOCATED AT STATION 1511 X75. PERFORMED A GVI OF EXISTING REPAIR IAW EO8-5100-7-5001 CRITERIA FOUND REPAIR IN COMPLIANCE WITH SRM 53-70-00 PAGE 11 FIG 62A VOL 1. 2L73 4F A22WE 20051109002962005110900296WP 2005 11 9 05FDEA03685 120051107A5347 PLUG DOUG DC10 DC1010 3022110WP SEAT TRACK UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 SEAT TRACK PLUG REPAIR AT STA 969 X47. PERFORMED A GVI OF EXISTING REPAIR IAW EO8-5100-7-5001 CRITERIA FOUND REPAIR IN COMPLIANCE WITH SRM 53-70-00 PAGE 11 FIG 62A VOL 1. 2L73 4F A22WE 20051109002972005110900297WP 2005 11 9 05FDEA03686 120051107A5347 REPAIR DOUG DC10 DC1010 3022110WP SEAT TRACK UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 MAIN CABIN STA 635 X27 FOUND STANDARD SEAT TRACK REPAIR. PERFORMED A GVI OF EXISTING REPAIR IAW EO8-5100-7-5001 CRITERIA FOUND REPAIR IN COMPLIANCE WITH SRM 53-70-00 FIG 2 SHT 1-2 VOL 1. 2L73 4F A22WE 20051109002982005110900298WP 2005 11 9 05FDEA03687 120051107A5315 REPAIR DOUG DC10 DC1010 3022110WP FLOORBEAM UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 CENTER CARGO COMPT FLOORBEAM SPLICE REPAIR AT STA 1701 RBL 36. PERFORMED A GVI OF EXISTING SPLICE IAW EO8-5100-7-5001 CRITERIA FOUND SPLICE DOUBLER IN COMPLIANCE WITH SRM 53-60-01 PAGE 7. 2L73 4F A22WE 20051109002992005110900299WP 2005 11 9 05FDEA03688 120051107A5310 DOUBLER DOUG DC10 DC1010 3022110WP DOOR FRAME UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 MAIN CABIN L-3 DOOR AT FUSELAGE STA 1305 FOUND DOUBLER REPAIR AT AFT DOOR JAMB. PERFORMED A GVI ON EXISTING REPAIR IAW SRM 53-50-00 FIG 19. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO8-5100-7-5001. 2L73 4F A22WE 20051109003002005110900300WP 2005 11 9 05FDEA03672 120051107A5754 DOUBLER DOUG DC10 DC1010 3022110WP SLAT TRACK UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 LT WING FOUND AN EXTERNAL DOUBLER REPAIR AT FIXED L/E LOWER SURFACE AT CUT OUT FOR SLAT TRACK LEFT SIDE STATION XOS 775. PERFORMED A GVI OF EXISTING DOUBLER IAW EO8-5100-7-5001 CRITERIA REQUEST FOUND IN COMPLIANCE WITH SRM 57-10-00 PAGE 215. 2L73 4F A22WE 20051109003012005110900301NM 2005 11 9 05FDEA02667 120050826A5754NRB6719502 DOUBLER DOUG MD11 MD11 3023602NM NR 2 SLAT DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 RIGHT L/E UPPER SURFACE AFT OF NR 1 AND NR 2 SLAT AREA AT APPROX XORS 150 FOUND WITH EXISTING DOUBLER REPAIR. RIGHT WING L/E UPPER SURFACE AFT OF NR 1 AND NR 2 SLAT AREA AT APPROX XORS 150. CARRIED OUT REPAIR AS PER SRM 57-00-01 FIG 24 VOL I. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051109003062005110900306EU 2005 11 9 ASOA05905 120051008A5310 STANCHION AEROSPATR72 ATR72212 8680945EU FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27641AS 387 DURING A C-CHECK IN YUL, THE LEFT STANCHION, AT FLOORBEAM 39, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT STANCHION, AT FS 39, IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20051109003072005110900307EU 2005 11 9 ASOA05901 120051006A5320 INTERCOSTAL AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27641AS 387 DURING A C-CHECK IN YUL, THE INTERCOSTAL BETWEEN FS 36-38, LBL 35 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTAL, BETWEEN FS 36-38 LBL 35, IAW ASA EO 72-53-0187. (M) 2H72 4T RTA53EU 20051109003082005110900308EU 2005 11 9 ASOA05902 120051006A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27641AS 387 DURING A C-CHECK IN YUL, THE SEAT TRACK, BETWEEN FS 41-42, RBL 18 OUTBOARD, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED IAW ASA EO 72-53-0193. (M) 2H72 4T RTA53EU 20051109003092005110900309EU 2005 11 9 ASOA05900 120051006A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27641AS 387 DURING A C-CHECK IN YUL, THE SEAT TRACKS, BETWEEN FRAME 36-41, AT LBL 4, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK, BETWEEN FRAME 36-39 IAW ASA EO 72-53-0186 AND REMOVED AND REPLACED THE SEAT TRACKS BETWEEN FS 39-41 IAW ASA EO 72-53-0191. (M) 2H72 4T RTA53EU 20051109003102005110900310EA 2005 11 9 ASOA05897 120051024A3397VS643 RELAY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSMALFUNCTIONED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27907EV 7648 DURING A GROUND INSPECTION IN RDU, THE EMERGENCY LIGHTS REMAINED ON WITH AN ESS AC BUSS CAUTION MESSAGE. MAINTENANCE REMOVED AND REPLACED THE K1XD RELAY. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051109003112005110900311EA 2005 11 9 ASOA05898 120051024A25602618 FLASHLIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27921EV 7819 DURING A GROUND INSPECTION IN ATL, THE FLIGHT ATTENDANTS FLASHLIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FLIGHT ATTENDANTS FLASHLIGHT. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051109003122005110900312EU 2005 11 9 ASOA05899 120051006A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27641AS 387 DURING A C-CHECK IN YUL, THE SEAT TRACKS, BETWEEN FRAME 36-40, AT RBL 8, WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS, BETWEEN FS 36-39, IAW ASA EO 72-53-0190, AND REPLACED THE SEAT TRACKS BETWEEN FS 36-39 IAW ASA EO 72-53-0192. (M) 2H72 4T RTA53EU 20051109003132005110900313EU 2005 11 9 ASOA05908 120051006A5315 FLOORBEAM AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27641AS 387 DURING A C-CHECK IN YUL, FLOORBEAM AT FS 41, BETWEEN BL 0 TO RBL 26, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM AT FS 41, BETWEEN BL 0 TO RBL 26, IAW ASA EO 72-53-0184. (M) 2H72 4T RTA53EU 20051109003142005110900314EU 2005 11 9 ASOA05904 120051006A5315 FLOORBEAM AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27641AS 387 DURING A C-CHECK IN YUL, THE FLOORBEAM AT FS 38, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM AT FS 38 IAW ASA EO 72-53-0171. (M) 2H72 4T RTA53EU 20051109003152005110900315EU 2005 11 9 ASOA05903 120051006A5315 FLOORBEAM AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27641AS 387 DURING A C-CHECK IN YUL, THE FLOORBEAM AT FS 36, BETWEEN LBL 30 TO RBL 30, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM AT FS 36, BETWEEN LBL 30 TO RBL 36 IAW ASA EO 72-53-0170. (M) 2H72 4T RTA53EU 20051109003162005110900316EU 2005 11 9 ASOA05907 120051006A5315 FLOORBEAM AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27641AS 387 DURING A C-CHECK IN YUL, THE FLOORBEAM, AT FS 40, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM AT FS 40, IAW ASA EO 72-53-0173. (M) 2H72 4T RTA53EU 20051109003172005110900317EU 2005 11 9 ASOA05906 120051006A5315 FLOORBEAM AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27641AS 387 DURING A C-CHECK IN YUL, THE FLOORBEAM, AT FS 39, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM, AT FS 39, IAW ASA EO 72-53-0172. (M) 2H72 4T RTA53EU 20051109003182005110900318NM 2005 11 9 05FDEA03657 120051107A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 FOUND CRACK INDICATION AT END OF STRINGER -9 (UPPER STRINGER), DURING HFEC INSPECTION AT RT WING TANK. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. CLIP FABRICATED AND REPLACED AS PER FEDEX EA 1-5720-94574. 2L73 4F RTA22WE 20051109003192005110900319NM 2005 11 9 05FDEA03658 120051107A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 FOUND CRACK INDICATION AT END OF STRINGER -10 (UPPER STRINGER), DURING HFEC INSPECTION AT RT WING TANK. REPAIRED AS PER SRM 57-20-00. 2L73 4F RTA22WE 20051109003202005110900320NM 2005 11 9 EIA2005246 120050830A5315 FLOORBEAM BOEING747 747132 1384882NM BS 600 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09479EV 19898 FWD CARGO COMPARTMENT STA 600 CARGO FLOORBEAM CRACKED. STA 600 FLOORBEAM UPPER CHORD RT OB SECTION REPLACED PER SRM 51-10-01. 2L74 4F A20WE 20051109003212005110900321NM 2005 11 9 EIA2005247 120050814A5347 SEAT TRACK BOEING747 747132 1384882NM BS 160-175 CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09479EV 19898 CABIN BS 160-175 RBL 10" SEAT TRACK FLANGE FOUND CORROSION. SEAT TRACK REPLACED FROM BS 140-185 RBL 10" AND INSTALLED PER SRM 51-1-01 AND 51-30-02. 2L74 4F A20WE 20051109003222005110900322NM 2005 11 9 EIA2005248 120050830A5321 PRESSURE PANEL BOEING747 747132 1384882NM BS 1480 FLOOR CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09479EV 19898 BS 1480 LBL 4" MD PRESSURE DECK WEB FOUND CORRODED. REPAIRED PER EA-53-0995. 2L74 4F A20WE 20051109003232005110900323NM 2005 11 9 EIA2005249 120050830A5320 SILL BOEING747 747132 1384882NM BS 560 CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09479EV 19898 FWD CARGO DOOR FWD LWR CUT-OUT CORNER AT BS 560 FOUND CORRODED. FWD LWR DOOR SILL REPAIRED PER EA-53-0996. 2L74 4F A20WE 20051109003242005110900324NM 2005 11 9 EIA2005250 120050830A5510 FRAME BOEING747 747132 1384882NM BS 2460 CHAFED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09479EV 19898 HORIZONTAL STABILIZER JACK SCREW COMPARTMENT BS 2460 LBL 25" FRAME INNER CHORD FOUND CHAFFED. REPAIRED PER EA-53-0990. 2L74 4F A20WE 20051109003252005110900325NM 2005 11 9 EIA2005251 120051103A3350 COVER BOEING747 747273C 1384896NM EMERGENCY LIGHT MISSING A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 CEILING EMERGENCY LIGHT AT L5 DOOR MISSING LIGHT COVER. REPLACED LENS COVER IAW MM 33-51-07, OPS CHECKED GOOD. 2L74 4F A20WE 20051109003262005110900326NM 2005 11 9 EIA2005252 120051103A3350 LIGHT BOEING747 747273C 1384896NM R5 DOOR INOPERATIVE A EIAAK NONE L NO TEST ININSP/MAINT 1 NM09470EV 20653 R5 DOOR FWD SILL EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT AASY AT DOOR R5 IAW 33-51-07, OPS CHECKED GOOD. 2L74 4F A20WE 20051109003272005110900327NM 2005 11 9 EIA2005253 120051103A3350 LIGHT BOEING747 747273C 1384896NM R5 DOOR INOPERATIVE A EIAAK NONE L NO TEST ININSP/MAINT 1 NM09470EV 20653 R5 FLOOD LIGHT INOP OVER DOOR EMERGENCY LIGHT. REPLACED EMERGENCY LIGHT ASSY IAE MM 33-51-07, OPS CHECKED GOOD. 2L74 4F A20WE 20051109003282005110900328NM 2005 11 9 EIA2005254 120051103A3350 LIGHT BOEING747 747273C 1384896NM CABIN INOPERATIVE A EIAAK NONE L NO TEST ININSP/MAINT 1 NM09470EV 20653 EMERGENCY LIGHT AT TOP OF STAIRS INOP. REPLACED EMERGENCY LIGHT AT TOP OF STAIRS IAW MM 33-51-07, OPS CHECKED GOOD. 2L74 4F A20WE 20051109003292005110900329NM 2005 11 9 EIA20005156 120050830A5300 SKIN BOEING747 747132 1384882NM BS 2460-2484 CORRODED A EIAAO OTHER O OTHER ININSP/MAINT 1 NM09479EV 19898 BS 2460-2484 STR 23L FUS SKIN EXT SURFACE CORROSION. REPAIR FUSE SKIN BS 2460-2484 PER EA-52-0992. 2L74 4F A20WE 20051109003302005110900330NM 2005 11 9 EIA2005157 120050813A5347 SEAT TRACK BOEING747 747132 1384882NM BS 515-520 CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09479EV 19898 CABIN BS 515-520 LBL 33 SEAT TRACK FOUND CORROSION. SEAT TRACK REPLACED FROM BS 510-590, INSTALLED PER SRM 51-10-01 AND 51-30-02. 2L74 4F A20WE 20051109003312005110900331NM 2005 11 9 EIA2005158 120050830A5321 PRESSURE PANEL BOEING747 747132 1384882NM BS 1480 FLOOR CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09479EV 19898 BS 1480 LBL4" M/D PRESSURE DECK WEB FOUND CORRODED. BS 1480 LBL4" M/D PRESSURE DECK WEB REPAIRED PER EA-53-0995. 2L74 4F A20WE 20051109003322005110900332NM 2005 11 9 EIA2005159 120050830A5320 SILL BOEING747 747132 1384882NM BS 560 CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09479EV 19898 FWD CARGO DOOR FORWARD LOWER CUT-OUT CORNER AT BS 560 FOUND CORROSION. REPAIRED FWD CARGO DOOR CUT-OUT AT FORWARD LOWER DOOR SILL PER EA-53-0996. 2L74 4F A20WE 20051109003332005110900333NM 2005 11 9 EIA2005179 120051011A5315 FLOORBEAM BOEING747 747212B 1384886NM BS 340 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 U/D BS 340 FLOORBEAM UPPER CHORD HORIZONTAL AFT FLANGE RBL 52" FLOOR PANEL ATTACH HOLE CRACKED RUNNING FWD APPROX .040" LONG. DEFECTIVE FLOORBEAM UPPER CHORD REPAIRED PER SB747-53A2431 FIG 10 HORIZONTAL AFT FLANGE RBL 52. 2L74 4F A20WE 20051109003342005110900334NM 2005 11 9 EIA2005180 120051011A5315 FLOORBEAM BOEING747 747212B 1384886NM BS 340 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 U/D BS 340 FLOORBEAM UPPER CHORD HORIZONTAL FWD FLANGE LBL 13" FLOOR PANEL A77, HOLE CRACKED RUNNING FWD APPROX .060" LONG. REPAIRED PER SB747-53A2431 FIG 9. 2L74 4F A20WE 20051109003352005110900335NM 2005 11 9 EIA2005181 120051011A5315 FLOORBEAM BOEING747 747212B 1384886NM BS 360 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 U/D BS 360 FLOORBEAM UPPER CHORD HORIZONTAL FWD FLANGE RBL 29" FLOOR PANEL ATT HOLE CRACKED RUNNING FWD APPROX .040" LONG. REPAIRED PER SB747-53A2431 FIG 9. 2L74 4F A20WE 20051109003362005110900336NM 2005 11 9 EIA2005182 120051011A5315 FLOORBEAM BOEING747 747212B 1384886NM BS 360 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 U/D BS 360 FLOORBEAM UPPER CHORD HORIZONTAL FWD FLANGE RBL 41 FLOOR PANEL ATT HOLE CRACKED RUNNING AFT APPROX .040" LONG. REPAIRED PER SB747-53A2431 FIG 10. 2L74 4F A20WE 20051109003372005110900337NM 2005 11 9 EIA20005183 120051011A5315 FLOORBEAM BOEING747 747212B 1384886NM BS 380 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 U/D BS 380 FLOORBEAM UPPER CHORD HORIZONTAL FWD FLANGE RBL 53 FLOOR PANEL ATT HOLE CRACKED RUNNING FWD APPROX .040 AND AFT APPROX .060 LONG. REPAIRED PER SB747-53A2431 FIG 10. 2L74 4F A20WE 20051109003382005110900338NM 2005 11 9 EIA2005184 120051011A5315 FLOORBEAM BOEING747 747212B 1384886NM BS 360 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 U/D BS 360 FLOORBEAM UPPER CHORD HORIZONTAL FWD FLANGE RBL 55 FLOOR PANEL ATT HOLE CRACKED RUNNING AFT APPROX .040" LONG. REPAIRED PER SB747-53A2431 FIG 10. 2L74 4F A20WE 20051109003392005110900339NM 2005 11 9 EIA2005185 120051011A5315 FLOORBEAM BOEING747 747212B 1384886NM BS 380 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 U/D BS 380 FLOORBEAM UPPER CHORD HORIZONTAL AFT FLANGE RBL 24" FLOOR PANEL ATT HOLE CRACKED RUNNING AFT APPROX. .040" LONG. REPAIRED PER SB747-53A2431 FIG 9. 2L74 4F A20WE 20051109003402005110900340NM 2005 11 9 EIA2005186 120051011A5315 FLOORBEAM BOEING747 747212B 1384886NM BS 360 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 U/D BS 360 FLOOR BEAM UPPER CHORD HORIZONTAL AFT FLANGE RBL 34 FLOOR PANEL ATT HOLE CRACKED RUNNING FWD APPROX. .060" LONG. REPAIRED PER SB747-53A2431 FIG 9. 2L74 4F A20WE 20051109003412005110900341NM 2005 11 9 EIA2005187 120051011A5315 FLOORBEAM BOEING747 747212B 1384886NM BS 360 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 U/D BS 360 FLOORBEAM UPPER CHORD HORIZONTAL AFT FLANGE RBL 44" FLOOR PANEL ATT HOLE CRACKED RUNNING AFT APPROX. .040" LONG. REPAIRED PER SB747-53A2431 FIG 9. 2L74 4F A20WE 20051109003422005110900342NM 2005 11 9 EIA2005188 120051011A5315 FLOORBEAM BOEING747 747212B 1384886NM BS 380 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 U/D BS 380 FLOORBEAM UPPER CHORD HORIZONTAL FWD FLANGE LBL 26" FLOOR PANEL ATT HOLE CRACKED RUNNING FWD APPROX .040" LONG. REPAIRED PER SB747-53A2452 FIG 9. 2L74 4F A20WE 20051109003432005110900343EA 2005 11 9 SWIA200515816 120051102A27505911330 LEVER CNDAIRCL600 CL6002C10 1390015EA MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07708SK 10156 FLAPS WILL NOT MOVE TO THE 20 DEGREE DETENT. REPLACED FLAP HANDLE ASSY IAW CRJ MM 27-50-00. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051109003442005110900344EU 2005 11 9 AALA20050719 120051101A3350 BATTERY PACK AIRBUS300 A300B4605R 3930308EU GE CF6 CF680 30025NE CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW2111060 470 MIA - EMERGENCY EXIT LIGHTING AT LEFT FIRST CLASS SEAT INOPERATIVE. REPLACED BATTERY PACK AT 110WL1 FOR EMERGENCY EXIT LIGHTING AT LEFT FIRST CLASS SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA35EU E13NE 20051109003452005110900345NM 2005 11 9 CALA0500387 120051106A531565C33948 FLOORBEAM BOEING737 737524 1384721NM GE CFM56 CFM56* 13802NE STA 947 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717620 27333 INSPECTION FOUND FLOORBEAM CORRODED AT STA 947, RBL 4 TO LBL 15. THE CORRODED AREAS WERE TRIMMED OUT AND FILLERS AND DOUBLERS WERE INSTALLED IAW SRM 53-60-51, FIGURE 201. 2L72 4F4 FRTA16WE E2GL 20051109003462005110900346NM 2005 11 9 CALA0500388 120051107A531165458075 FRAME BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE STA 294.5 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2759338 23576 INSPECTION FOUND A .5 INCH CRACK JUST BELOW UPPER HINGE, LOWER GUIDE PLATE AREA IN R-1 DOOR FUSELAGE CUTOUT FRAME, STA 294.5, S11 R TO S14R. THE DOOR FUSELAGE CUTOUT FRAME WAS REMOVED AND REPLACED IAW SRM 51-10-02 AND 51-40-02. 2L72 4F4 FRTA16WE E2GL 20051110000032005111000003 2005 11 10 CALA0500391 420051107A2565D31591475 SLIDE BOEING737 737524 1384721NM R-1 DOOR LOW A CALAK NONE O OTHER ININSP/MAINT 1 SW271963849349 28899 THE R-1 DOOR EMERGENCY ESCAPE SLIDE WAS FOUND TO HAVE LOW PRESSURE. THE R-1 DOOR SLIDE WAS REMOVED AND REPLACED IAW MM 25-61-35. 2L72 4F RTA16WE 20051110000042005111000004EU 2005 11 10 AWXA200501338 120051104A2560P401002100 BATTERY AIRBUS320 A320232 3930326EU FLASHLIGHT INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28668AW 1764 PHX - EEL - DURING CHECK DISCOVERED THE EMERGENCY EXIT FLASHLIGHT AT THE L1 DOOR, RT SIDE, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY IN THE L1 DOOR RT SIDE EMERGENCY FLASHLIGHT, OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA28NM 20051110000052005111000005EU 2005 11 10 AWXA200501339 120051105A2560P4010021000 BATTERY AIRBUS320 A320231 3930325EU FLASHLIGHT INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28626AW 65 PHX - EEL - DURING OVERNIGHT INSPECTION DISCOVERED, THE FORWARD FLIGHT ATTENDANT STATION EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA28NM 20051110000082005111000008NM 2005 11 10 AALA20050718 120051031A3350 BATTERY PACK BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21798AN 30797 MIA - EMERGENCY LIGHTS MOUNTED ON FORWARD GALLEY CLOSET MODULES INOPERATIVE. REPLACED BATTERY PACK M33093 FOR EMERGENCY LIGHTS MOUNTED ON FORWARD GALLEY CLOSET MODULES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20051110000092005111000009NM 2005 11 10 AALA20050723 120051106A3397 CONNECTOR BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21376AN 25445 DFW - EMERGENCY LIGHT AT SEAT 40AB INOPERATIVE. RESEATED CONNECTOR AT INSIDE WALL CONNECTION FOR EMERGENCY LIGHT AT SEAT 40AB. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20051110000122005111000012EA 2005 11 10 SWIA200515808 120051107A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07935SW 7725 CREW REPORTS FLOOR LIGHTING INOP. CLEANED FLOOR TRACK POWER STRIP ROW 2 TO 6 CONNECTION AND REINSTALLED POWER STRIP AND LIGHT STRIPS. OPERATIONAL CHECK GOOD IAW CRJ 200 MM 33-51-00-710-801. 2L72 4F RTA21EA 20051110000152005111000015EA 2005 11 10 SWIA200515811 120051103A3350 BULB CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT MISSING A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07701SK 10133 FLOOR LEVEL EMERGENCY FLOOD LIGHT BY SERVICE DOOR MISSING PANEL AND TWO BULBS. REPLACED FLOODLIGHT COVER AND BULB IAW CRJ AMM CHAP 33-50-00. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051110000162005111000016SO 2005 11 10 SWIA200515812 120051104A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT DISCHARGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07251YV9379 9379 120251 ALL EXIT SIGNS AT ROW 6 DO NOT ILLUMINATE. REPLACED MIDDLE ELBP. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20051110000192005111000019SO 2005 11 10 SWIA200515815 120051102A3350 LAMP EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07188SW 120039 EMERGENCY LIGHTS AT ROW 6 ON RIGHT SIDE INOP. RELAMPED EMERGENCY LIGHT AT ROW 6 ON RIGHT SIDE. OPERATIONAL CHECK GOOD IAW EMB MM 33-51-02. 2L72 4T RTA31SO 20051110000222005111000022NM 2005 11 10 EIA2005191 120051011A5315 FLOORBEAM BOEING747 747212B 1384886NM BS 420 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 U/D BS 420 FLOORBEAM UPPER CHORD HORIZONTAL AFT FLANGE LBL 33 FLOOR PANEL ATT HOLE CRACKED RUNNING AFT APPROX .060" LONG. REPAIRED PER SB747-53A2452 FIG 9. 2L74 4F A20WE 20051110000232005111000023NM 2005 11 10 EIA2005192 120051011A5315 FLOORBEAM BOEING747 747212B 1384886NM BS 520 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 U/D BS 520 FLOORBEAM UPPER CHORD HORIZONTAL AFT FLANGE LBL 42" FLOOR PANEL ATT HOLE CRACKED RUNNING FWD APPROX .060" LONG. REPAIRED PER SB747-53A2452 FIG 9. 2L74 4F A20WE 20051110000242005111000024NM 2005 11 10 EIA2005193 120051014A5315 FLOORBEAM BOEING747 747212B 1384886NM BS 600 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 U/D BS 600 FLOORBEAM UPPER CHORD HORIZONTAL AFT FLANGE RBL 25 FLOOR PANEL ATT HOLE CRACKED RUNNING FWD AND AFT APPROX .125" LONG. REPAIRED PER SB 747-53A2452 FIG 13. 2L74 4F A20WE 20051110000252005111000025NM 2005 11 10 EIA2005194 120051007A5320 INTERCOSTAL BOEING747 747212B 1384886NM BS 1220 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 M/D WING CENTER SECTION STA 1220 LBL 114 BELOW FLOOR INTERCOSTAL WEB CRACKED AT 2 LOCATION (FWD UPPER AND AFT LOWER). REPAIRED DEFECTIVE WEB PER SRM 51-40-02. 2L74 4F A20WE 20051110000262005111000026NM 2005 11 10 EIA2005195 120051007A5322 SHEAR TIE BOEING747 747212B 1384886NM BS 1500 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 M/D BS 1500 STR 20-22R FRAME SHEAR TIE FOUND CRACKED. DEFECTIVE SHEAR TIE REPLACED PER SRM 51-10-01, PG 9. 2L74 4F A20WE 20051110000272005111000027NM 2005 11 10 EIA2005196 120051014A5315 FLOORBEAM BOEING747 747212B 1384886NM BS 520 DAMAGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 U/D BS 520 FLOORBEAM UPPER CHORD FWD FLANGE FLOOR PANEL ATT HOLE FOUND SHORT OF E/D AT LBL 73", 77", 80", 84", & 91". REPAIRED PER SB747-53A2452 FIG 9. 2L74 4F A20WE 20051108003322005110800332NM 2005 11 8 USAA051344 120051107A5320 STRINGER SPLICE BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19779AU 24996 STA 907 AND STR 4R CRACKED. REMOVED DAMAGE AND INSTALLED STRINGER SPLICE. DEFECT SIZE: 1 INCH. 2L72 4F RTA16WE 20051108003342005110800334NM 2005 11 8 USAA051342 120051107A5315 FLOORBEAM BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 BS 312, WL 208, LBL 16 TO RBL 16 LEVEL 1 CORROSION. SPLICED IN REPLACEMENT EXTRUSION IAW SRM 53-10-51 FIG 201. DEFECT SIZE: .50 X .50 INCH. 2L72 4F RTA16WE 20051108003452005110800345NM 2005 11 8 USAA051338 120051107A5330 SKIN BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19779AU 24996 CARGO DOOR CUTOUT FWD FRAME INNER SKIN AT LWR END 2ND RIVET UP FROM S26R CRACKED. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 51-70-13 BOEING DWG 69-15224. DEFECT SIZE: .5 INCH. 2L72 4F RTA16WE 20051108003472005110800347 2005 11 8 KBM2005F00282 420050821A8300350A35105901 COUPLING SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE GEARBOX CRACKED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P 2347 COUPLING CRACKED AT MAIN GB TO ENGINE SHORT SHAFT FWD COUPLING. REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20051108003542005110800354SO 2005 11 8 RAIA00511001 120051103A33501317 LIGHT EMB 145 EMB145LR 3260212SO CABIN BURNED OUT A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03817HK 145058 MX - FOUND OVERHEAD MID CABIN EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED LIGHT BULB. 2L72 4T RTT00011AT 20051108003602005110800360EU 2005 11 8 2005UALA01206 120051030A5330 SKIN AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE GOUGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29435UA 613 THREE EACH GOUGES FOUND IN RVSM AREA ON RIGHT SIDE OF AIRCRAFT. DAMAGE IS APPROXIMATELY SIX INCHES FORWARD OF FORWARD CARGO DOOR. BLENDED DAMAGES TO REPAIR, REF. SRM53-11-11 AND SRM 53-00-11. 2L72 4F4 FRTA28NM E40NE 20051108003672005110800367NM 2005 11 8 2005UALA01213 120051101A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29198UA 28716 EMERGENCY EEL LIGHT INOP AT LAV 112 RIGHT HAND FWD WALL. RECONNECTED EEL LIGHT CONNECTOR. 2L74 4F4 FRTA20WE E24NE 20051108003682005110800368CE 2005 11 8 DJFA2005157 120051104A2131645471305305 CONTROLLER RAYTHNDH125 HAWKER800XP 7150012CE CABIN PRESSURE MALFUNCTIONED E DJFAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA23848CW2328 258648 THE CREW REPORTED THAT DURING CLIMBOUT AT FL 210 THE CABIN ALTITUDE COULD NOT BE CONTROLLED. THE ALTITUDE HORN SOUNDED AND THE CREW DECLARED AN EMERGENCY. DURING DESCENT, CABIN ALTITUDE COULD NOT BE CONTROLLED USING THE CABIN RATE CONTROL KNOB OR MANUAL RATE CONTROL KNOB. THE AIRCRAFT CABIN ALTITUDE NEVER EXCEEDED 9,500 FT. WHEN RETURNING TO KLAS THE AIRCRAFT WAS LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE OUTFLOW / SAFETY VALVE CONTROLLER. OPERATIONAL CHECKS WERE GOOD, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA3EU 20051108003792005110800379NM 2005 11 8 2005UALA01224 120051104A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN BROKEN A UALAK NONE O OTHER ININSP/MAINT 1 WP29117UA 28810 SEAT 2J SIDE FWD EMERGENCY LIGHT BROKEN. REPLACED LIGHT ASSY. 2L74 4F4 FRTA20WE E24NE 20051108003812005110800381EU 2005 11 8 2005UALA01226 120051103A3350 LIGHT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29460UA 1248 EELS INOPERATIVE. 2L72 4F4 FRTA28NM E40NE 20051108003882005110800388NM 2005 11 8 EIA2005163 120050930A3350 COVER BOEING747 747273C 1384896NM CABIN MISSING A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 M/D STA 380 & 680 & R5 EMERGENCY LIGHT COVER MISSING. REPLACED COVERS PER B747 33-51-07. 2L74 4F A20WE 20051109000252005110900025EU 2005 11 9 KBM2005F00326 120051027A6520350A33215300 BEARING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE TAIL ROTOR CUT E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19115SH945 3141 LAMINATED BEARING, UNIT HAS MULTIPLE CUTS. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051109000402005110900040NM 2005 11 9 GAIA05025 120051005A33501000679 LIGHT BOEING727 727251 138408HNM PWA JT8 JT8D9 52048NE COCKPIT INOPERATIVE A GAIAK NONE L NO TEST ININSP/MAINT 1 SW07278US 21157 DURING POST FLIGHT, FOUND COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED COCKPIT EMERGENCY LIGHT ASSY, CHECKS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L73 4F4 F A3WE E2EA 20051109000412005110900041EU 2005 11 9 KBM2005F00330 120051101A2432RG355 BATTERY SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1B 6OO30NE MASTER WEAK E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH210 2337 BATTERY, UNIT IS WEAK. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051109000452005110900045EU 2005 11 9 KBM2005F00276 120050904A771456337078012 TACHOMETER SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE COCKPIT MALFUNCTIONED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH 2884 TACHOMETER INDICATOR, BLEED VALVE FLAG DOES NOT RETRACT, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051109000532005110900053SO 2005 11 9 SIMA200528306 120051006A33207281000501 MODULE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL CABIN LIGHTS OVERHEATED A SIMAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW21641AE 145191 BURNING SMELL IN GALLEY AFTER LANDING. REPLACED CABIN LIGHTING CONTROL MODULE IAW AMM. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (K) 2L72 4T4 FRTT00011ATTE6CH 20051109000622005110900062SO 2005 11 9 SIMA200528302 120051002A534414525175001 CLIP EMB 135 EMB135KL 3260302SO IAE V2524 V2524A5 NE BAGGAGE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21823AE8173 145582 THE BAGGAGE DOOR FWD LATERIAL (SHEAR CLIP) LOWER SECTION AT FRAME 65 WAS FOUND CORRODED. REMOVED A SECTION OF THE SHEAR CLIP TO REMOVE THE CORROSION. PREPARED A SHEAR CLIP. FABRICATED A SHEAR CLIP SPLICE DOUBLER. REPAIR DONE IAW SRM. (SW21200600333) (K) 2L72 4F4 FRTT00011ATE40NE 20051109000682005110900068EU 2005 11 9 KBM2005F00320 120050930A2120050085 BLOWER SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE AFT EVAPORATOR FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19751H 5 3403 AFT EVAPORATOR BLOWER, UNIT NOT WORKING. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051109000812005110900081SW 2005 11 9 ALG2005F00081 120051019A3340A402W LENS BELL 206 206L1 1182107SW ALLSN 250C 250C28B 03013GL STROBE MISSING E ALGAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 SW033190P 45779 IN CRUISE FLIGHT, FELT BUMP IN T/R PEDALS, UPON LANDING, NOTIFIED MAINTENANCE. INSPECTION OF AIRCRAFT BY MAINTENANCE FOUND THE UPPER WHITE STROBE LENS MISSING AND DAMAGE TO ONE TAIL ROTOR BLADE. INSTALLED NEW WHITE LENS AND REPLACED THE T/R ASSY WITH A SERVICEABLE UNIT IAW MM. (K) 1G71 3U3 U H2SW E1GL 20051109000842005110900084 2005 11 9 KBM2005F00308 420051018A3422200DC GYRO SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1 60030NE DIRECTIONAL FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19215LA15871 2143 DIRECTIONAL GYRO WILL NOT HOLD CAGE. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051109000862005110900086EU 2005 11 9 KBM2005F00315 120051016A6520350A33215300 BEARING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE TAIL ROTOR FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19351WM891 2167 T/R HINGE LAMINATED BEARING HAD MULTIPLE CUTS IN RUBBER. REPLACED WITH NEW. (K) 1G71 3U3 U H9EU E19EU 20051109000992005110900099SO 2005 11 9 SIMA200529005 120051012A532014521700007 DOUBLER EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FLOOR SUPPORT CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21717AE 145272 DURIN CPCP INSPECTION FOUND LT OMEGA BEAM DOUBLER AT FRAME 20 IS CORRODED. REPLACED LT OMEGA BEAM DOUBLER AT FRAME 20 IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4F4 FRTT00011ATTE6CH 20051109001182005110900118NM 2005 11 9 05FDEA03662 120051107A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 CRACK INDICATION FOUND AT END OF STRINGER -13 (UPPER STRINGER). DURING HFEC INSPECTION AT RT WING TANK. REPAIRED AS PER SRM 57-20-00. 2L73 4F RTA22WE 20051109001282005110900128NM 2005 11 9 SWAA053514 120051107A575465C26686 SKIN BOEING737 7373H4 1384600NM RT WING SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29335SW 23939 DURING SCHEDULED 1/4D CHECK, FOUND NR 4 L/E SLAT SKIN CRACKED AT ACTUATOR OUTBOARD STOP FITTING. REPAIRED SLAT PER SRM. 2L72 4F RTA16WE 20051109001292005110900129NM 2005 11 9 SWAA053515 120051107A5712BAC1518 STIFFENER BOEING737 7373H4 1384600NM BULKHEAD CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29335SW 23939 DURING SCHEDULED 1/4D CHECK, FOUND LEFT MLG W/W VERTICAL STIFFENER CRACKED AT BS 663 BULKHEAD, LBL 6.15. REPAIRED STIFFENER PER SWA EA. 2L72 4F RTA16WE 20051109001412005110900141NM 2005 11 9 QXEA200501504 120051106A30104D205401 TIMER DHAV DHC8 DHC8202 2809007NM DEICE SYSTEM MALFUNCTIONED A QXEAA UNSCHED LANDING O OTHER CRCRUISE 1 NM09357PH108332259 504 SEA FLIGHT NR 2177, AIRFRAME AUTO DEICE DOES NOT OPERATE IN SLOW OR FAST MODE. AIRFRAME MANUAL WORKS NORMAL. MAINTENANCE REPLACED AIRFRAME DEICE TIMER. FUNCTIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051109001422005110900142NM 2005 11 9 QXEA200501501 120051104A2910 HYDRAULIC SYSTEM DHAV DHC8 DHC8202 2809007NM NR 2 CONTAMINATED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09361PH 516 PDX FLIGHT NR 2126 - NOSE DOOR ADVISORY LIGHT REMAINED ILLUMINATED AND NR 2 HYDRAULIC PRESSURE DROPPED TO ZERO WITH NR 2 ENGINE HYDRAULIC PUMP CAUTION LIGHT ILLUMINATED. AFTER CHECKLIST PRESSURE READING TO NORMAL AGAIN. ACCOMPLISHED ALTERNATE GEAR EXTENSION AND LANDING NORMAL. MAINTENANCE FOUND AIR IN NR 2 HYDRAULIC SYSTEM. SYSTEM BLED AND SPECIAL INSPECTION COMPLIED WITH. SYSTEM CHECKS GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051109001972005110900197EU 2005 11 9 05FDEA03639 120051104A5347 SEAT TRACK AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 MAIN CABIN BETWEEN FS 17 AND FS 19 SEAT TRACK 1R RIGHT SIDE HAS 2 SQ INCHES OF CORROSION REF N00665. REMOVED AND REPLACED SEAT TRACK 1R IAW SRM 51-72-10. 2L72 4F RTA35EU 20051109002002005110900200NM 2005 11 9 05FDEA03629 120051104A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 DURING HFEC INSPECTION, FOUND CRACK AT LEFT WING, END OF STRINGER 12. REPAIR CARRIED OUT IAW SRM 57-20- 00 FIG. 10 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051109002072005110900207NM 2005 11 9 EIA2005237 120051009A5310 DOOR FRAME BOEING747 747212B 1384886NM BS 400 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 NR 1 L DOOR FWD FRAME LWR CORNER AREA CRACKED BS 400, WL 210. REPAIRED DEFECTIVE FWD FRAME PER SRM 52-10-02, FIG 10. 2L74 4F A20WE 20051109002092005110900209NM 2005 11 9 EIA2005239 120051008A4910 SKIN BOEING747 747212B 1384886NM APU INLET DETERIORATED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 APU INLET DUCT ADJ ACTR FIBERGLASS HONEYCOMB FOUND DETERIORIATED AROUND THE PROTECTIVE SHROUD CUTOUT ON THE OUTER SKIN. TEMPORARY REPAIR PER SRM 51-40-12, HAECO REPAIR SCHEME R-49-15-35395, ECRA 486-49-052-1. REPEAT INSPECTION TO REPAIRED AREA WITHIN 10 DAYS AND EVERY "A" CHECK. 2L74 4F A20WE 20051109002152005110900215NM 2005 11 9 EIA2005245 120050830A5321 PRESSURE PANEL BOEING747 747132 1384882NM BS 1480 FLOOR CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09479EV 19898 MAIN DECK BS 1480 LBL 21-26 FLOOR PRESSURE WEB CORRODED. REPAIRED PER EA-53-0995. 2L74 4F A20WE 20051109002192005110900219NM 2005 11 9 05FDEA03653 120051107A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 FOUND CRACK INDICATION AT END OF STRINGER -13 (UPPER STRINGER) WAS FOUND DURING HFEC INSPECTION AT LHS WING TANK. REPAIR CARRIED OUT AS PER SRM 57-20-00. 2L73 4F RTA22WE 20051109002222005110900222NM 2005 11 9 05FDEA03656 120051107A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 FOUND CRACK INDICATION AT END OF STRINGER -7 (UPPER STRINGER). DURING HFEC INSPECTION AT RT WING TANK. REPAIRED AS PER SRM 57-20-00. 2L73 4F RTA22WE 20051109002262005110900226NM 2005 11 9 EIA2005213 120051007A5320 SUPPORT BRACKET BOEING747 747212B 1384886NM BS 1333 CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 KEEL BEAM SUPPORT SPLICE BRACKET CORRODED AT BS 1333, RBL 16". REPLACED DEFECTIVE SUPPPORT BRACKET PER SRM 51-10-01, PG 9. 2L74 4F A20WE 20051109002272005110900227NM 2005 11 9 EIA2005214 120051006A5320 SUPPORT BRACKET BOEING747 747212B 1384886NM BS 1330 CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 KEEL BEAM PANEL SUPPORT FLOAT NUT BASE CORROSION FOUND AT STA 1330, LBL 15 TO RBL 15. REPLACED DEFECTIVE SUPPORT PER SRM 51-10-01, PG 9. 2L74 4F A20WE 20051109002312005110900231NM 2005 11 9 EIA2005218 120051007A5310 FRAME BOEING747 747212B 1384886NM BS 434 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 RT SIDE BS 434 FRAME AT STR 26R ONE EACH, FASTENER HOLE CRACKED AT FRAME WEB. REPAIRED DEFECTIVE CRACKED FRAME WEB PER SRM 53-10-04 FIG 9. 2L74 4F A20WE 20051109002332005110900233NM 2005 11 9 EIA2005220 120051010A5310 PLATE BOEING747 747212B 1384886NM BS 400 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 NWW LT AFT CORNER AT BS 400 INTERNAL SPLICE PLATE FOUND CRACK RUNNING FROM FWD EDGE GOING UNDER B/H CHORD. REPLACED DEFECTIVE INTERNAL SPLICE PLATE PER SRM 51-10-01, PG 9. 2L74 4F A20WE 20051109002342005110900234NM 2005 11 9 EIA2005221 120051010A5310 PLATE BOEING747 747212B 1384886NM BS 400 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 NWW RT AFT CORNER AT BS 400 INTERNAL SPLICE PLATE FOUND CRACK RUNNING FROM FWD EDGE GOING UNDER B/H CHORD. PLACED DEFECTIVE SPLICE PLATE PER SRM 51-10-01, PG 9. 2L74 4F A20WE 20051109002352005110900235NM 2005 11 9 EIA2005222 120051009A5210 INTERCOSTAL BOEING747 747212B 1384886NM L4 DOOR CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 L4 DOOR INTERCOSTAL WEB FOUND CORRODED. REPAIRED DEFECTIVE INTERCOSTAL WEB PER SRM 51-40-03, FIG 1. 2L74 4F A20WE 20051109002442005110900244NM 2005 11 9 EIA2005205 120051009A5320 INTERCOSTAL BOEING747 747212B 1384886NM BS 2220-2240 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 BULK CARGO AREA AFT OF STA 2220 - 2240, RT SR 40 ATT INTERCOSTAL CRACKED. REPLACED DEFECTIVE INTERCOSTAL PER SRM 51-10-01, PG 9. 2L74 4F A20WE 20051109002602005110900260NM 2005 11 9 EIA2005234 120051006A5753 TIE ROD BOEING747 747212B 1384886NM FLAP TRACK CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 LHW NR 4 FLAP TRACK TIE ROD UPPER MOUNT FTG FLANGE CRACKED. REPAIRED DEFECTIVE CHORD PER SRM 51-40-04, FIG 3. 2L74 4F A20WE 20051109002752005110900275NM 2005 11 9 05FDEA03646 120051106A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 FOUND MAIN DECK COMPARTMENT, SEAT TRACK FOUND CORROSION AT STA 1521, X=8.5. REPAIR CARRIED OUT IAW SRM 53-70-00 FIG. 3 VOL. I AND SRM 51-33-01 VOL. II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051109002772005110900277NM 2005 11 9 05FDEA03648 120051106A5730 SKIN DOUG MD11 MD11 3023602NM RT WING BULGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 FOUND RHW IN SPAR UPPER SKIN AT APPROX XORS 280 STRINGER 13 FOUND WITH SKIN BULGE. CARRIED OUT REPAIR AS PER EA 1-5720-87644. 2L73 4F RTA22WE 20051109002812005110900281WP 2005 11 9 05FDEA03665 120051107A5510 DOUBLER DOUG DC10 DC1010 3022110WP HORIZONTAL STAB UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 TRAILING EDGE LT HAND HORIZONTAL STABILIZER UPPER SURFACE ON SKIN THERE'S AN EXTERNAL DOUBLER REPAIR BETWEEN STAB STATIONS XE67 AND XE82. PERFORMED A GVI OF EXISTING DOUBLER IAW FEDEX EA8-5510-49668 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO8-5100-7-5001. 2L73 4F A22WE 20051109002832005110900283WP 2005 11 9 05FDEA03666 120051107A5510 DOUBLER DOUG DC10 DC1010 3022110WP HORIZONTAL STAB UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 LEFT HAND HORIZONTAL STABILIZER UPPER SURFACE ON SKIN TRAILING EDGE, FOUND AN EXTERNAL DOUBLER REPAIR BETWEEN STATIONS XE84 AND XE109. PERFORMED A GVI OF EXISTING DOUBLER IAW EO8-5100-7-5001 CRITERIA REQUEST AND FOUND IN COMPLIANCE WITH FEDEX EA8-5510-49668. 2L73 4F A22WE 20051109002852005110900285WP 2005 11 9 05FDEA03682 120051107A5330 TRIPLER DOUG DC10 DC1010 3022110WP FUSELAGE UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 FOUND TRIPLE REPAIR AT STA 575 LONGERON 48 RT SIDE AT RAM AIR DUCT CORNER. PERFORMED A GVI ON EXISTING REPAIR DOUBLER IAW SRM 53-20-00 FIG 2. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO8-5100-7-5001. 2L73 4F A22WE 20051109002872005110900287WP 2005 11 9 05FDEA03674 120051107A5520 DOUBLER DOUG DC10 DC1010 3022110WP ELEVATOR UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 LEFT HORIZONTAL STABILIZER INBOARD ELEVATOR LOWER SURFACE ON SKIN, FOUND AN INTERNAL DOUBLER REPAIR BETWEEN STAB STATIONS XE130 AND XE146. PERFORMED A GVI OF EXISTING REPAIR IAW EO8-5100-7-5001 CRITERIA REQUEST, FOUND DOUBLER IN COMPLIANCE WITH SRM 55-00-01 PG 9. 2L73 4F A22WE 20051109002892005110900289WP 2005 11 9 05FDEA03676 120051107A5510 DOUBLER DOUG DC10 DC1010 3022110WP HORIZONTAL STAB UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 RT HAND HORIZONTAL STABILIZER LOWER SURFACE FOUND AN EXTERNAL DOUBLER REPAIR ON SKIN, BETWEEN HORIZONTAL STAB STATIONS XE75 AND XE86. PERFORMED A GVI OF EXISTING DOUBLER IAW EO8-5100-7-5001 CRITERIA REQUEST FOUND DOUBLER IN COMPLIANCE WITH SERVICE BULLETIN 55-16 FIG 22. 2L73 4F A22WE 20051109002912005110900291WP 2005 11 9 05FDEA03678 120051107A5510 DOUBLER DOUG DC10 DC1010 3022110WP HORIZONTAL STAB UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 EXTERNAL DOUBLER REPAIR FOUND ON RT HORIZONTAL STABILIZER UPPER SURFACE BETWEEN STA XE79 AND XE86. PERFORMED A GVI OF EXISTING DOUBLER IAW EO8-5100-7-5001 CRITERIA REQUEST FOUND DOUBLER IN COMPLIANCE WITH SERVICE BULLETIN 55-16 FIG 17. 2L73 4F A22WE 20051109003472005110900347NM 2005 11 9 CALA0500389 120051108A5315147A55053 FLOORBEAM BOEING737 737724 13844BYNM GE CFM56 CFM56* 13802NE STA 967 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2723708 28769 INSPECTION FOUND FLOORBEAM CORRODED AT STA 967, RBL 0 TO RBL 51. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51. 2L72 4F4 FRTA16WE E2GL 20051110000062005111000006NM 2005 11 10 AWXA200501342 120051107A3397BMS13311122 WIRE BOEING737 7373G7 1384595NM EMERGENCY LIGHT DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 PHX - EEL - DURING OVERNIGHT INSPECTION DISCOVERED ROW 9 AISLE EMERGENCY EXIT LIGHT NOT ILLUMINATING. MAINTENANCE REPAIRED WIRING AT ROW 9 IAW SWPM CHAPTER 20. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20051110000102005111000010SO 2005 11 10 SWIA200515806 120051103A3350 SIGN EMB 120 EMB120ER 3260203SO EMERGENCY EXIT BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07567SW 120342 6A LOWER EMERG EXIT SIGN BROKEN. REPLACED 6A EXIT SIGN ASSY. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20051110000132005111000013 2005 11 10 SWIA200515809 420051106A22166225734002 SERVO EMB 120 EMB120ER 3260203SO ELEVATOR MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07233SW1054610546 120307 SLIGHT RESISTANCE AND RUBBING SOUND FROM CAPT SIDE WHEN YOKE IS EXERCISED FWD AND AFT. REPLACED ELEVATOR SERVO IAW MM 22-10-05. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20051110000212005111000021NM 2005 11 10 EIA2005190 120051011A5315 FLOORBEAM BOEING747 747212B 1384886NM BS 400 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 U/D BS 400 FLOORBEAM UPPER CHORD HORIZONTAL FWD FLANGE LBL 55 FLOOR PANEL ATT HOLE CRACKED RUNNING FWD APPROX .060" LONG. REPAIRED PER SB 747-53A2452 FIG 9. 2L74 4F A20WE 20051110000282005111000028NM 2005 11 10 EIA2005197 120051009A5320 FLOOR SUPPORT BOEING747 747212B 1384886NM BS 1700-1720 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 M/D BS 1700-1720 RBL 78 LONGITUDINAL FLOOR SUPPORT WEB FOUND CRACKED. REPLACED DEFECTIVE FLOOR SUPPORT WEB PER SRM 51-10-01, PG 9. 2L74 4F A20WE 20051110000422005111000042SO 2005 11 10 SWIA200515818 120051104A3397 FUSE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07289YV 120289 BOTH AFT EXTERNAL EMERGENCY LIGHTS DO NOT WORK. REPOSITIONED WIRE BUNDLE IN OVERHEAD AT ROW 7 AND REPLACED FUSE. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20051110000432005111000043EA 2005 11 10 SWIA200515819 120051101A27604916406 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07916SW5334 5334 7634 OB GROUND SPOILER FAULT STATUS MSG ON EICAS. REPLACED NR 2 SECU IAW CRJ 200 MM 27-61-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051110000462005111000046SO 2005 11 10 SWIA200515822 120051031A3350 LIGHT EMB 120 EMB120ER 3260203SO CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07292UX 120292 RED EMERGENCY LIGHT BY THE MAIN CABIN DOOR INOP. REPLACED RED EMERGENCY LIGHT BY MAIN CABIN DOOR. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20051110000472005111000047WP 2005 11 10 ABXA050264 120051019A5340991224339 ATTACH BRACKET DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23952AX 47615 ATTACH BRACKET ON AFT SIDE OF PYLON BULKHEAD AT LONGERON 17 RIGHT WAS CRACKED. REMOVED AND REPLACED BRACKET IAW DC9 SRM 51-30-2. 2L72 4F A6WE 20051110000482005111000048WP 2005 11 10 ABXA050265 120051019A532299577399 SHEAR TIE DOUG DC9 DC941 302207NWP BS 1021 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23952AX 47615 SHEAR TIE CRACKED AT STA 1021 BETWEEN LONGERON 15 RIGHT AND LONGERON 16 RIGHT. REMOVED AND REPLACED SHEAR TIE IAW DC-9 SRM 51-30-5 AND 51-30-2. 2L72 4F A6WE 20051110000492005111000049WP 2005 11 10 ABXA050267 120051020A53403924028501 FITTING DOUG DC9 DC941 302207NWP BS 649 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23952AX 47615 END FITTING CORRODED LONGERON 29 LEFT APPROXIMATELY STA FS 649, LOWER WING CENTER SECTION IN KEEL BEAM AREA. REMOVED AND REPLACED LONGERON END FITTING IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20051110000502005111000050WP 2005 11 10 ABXA050268 120051020A5314 KEELBEAM DOUG DC9 DC941 302207NWP CENTER WING SECTCRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23952AX 47615 END FITTING SIDE SUPPORT CRACKED ON LEFT SIDE OF KEEL BEAM CENTER SUPPORT LONGERON 30, FS 646 APPROXIMATELY. REMOVED AND REPLACED END FITTING AT STA 646, LONGERON 30 IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20051110000522005111000052WP 2005 11 10 ABXA050266 120051020A534039240271 FITTING DOUG DC9 DC941 302207NWP CENTER WING SECTCORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23952AX 47615 END FITTING CORRODED JUST INBOARD OF LONGERON 29 RIGHT IN KEEL BEAM AREA LOWER WING CENTER SECTION FS 649. REMOVED AND REPLACED END FITTING IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20051110000542005111000054NE 2005 11 10 NACA20050025 220051021A7261 SHAFT PWA DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE SCAVENGE PUMP SHEARED A NACAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 AL03438721570 1570 138 533294 P28443 NR 3 ENGINE SHUTDOWN ON GROUND UPON TAXI-IN DUE TO EXCESSIVE OIL LEAK. CAUSE OF EXCESSIVE OIL LEAKAGE WAS DUE TO A SHEARED LOWER SHAFT SECTION OF THE NOSE CASE OIL SCAVENGE PUMP. THE UPPER PORTION WAS STILL INTACT DISPLAYING GOOD PRESSURE AND GOOD BMEP. THE ENGINE WAS REPLACED DUE TO FRONT CAM FAILURE FOUND DURING INSPECTION. 2L74 4R4 R A781 5E8 20051110000602005111000060 2005 11 10 SCNA05009 420051105A2565 SLIDE BOEING737 7378Q8 13844BXNM GE CFM56 CFM56* 13802NE R1 DOOR DISLODGED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15801SY 30332 R1 DOOR SLIDE FELL OUT OF SLIDE CASE, DOOR WAS DISARMED. INSTALLED R1 DOOR ESCAPE SLIDE PACK AND COVER TASK 25-66-01-400-801 RII ACCOMPLISHED 2083126. 2L72 4F4 FRTA16WE E2GL 20051110000612005111000061CE 2005 11 10 FFKA2005106 120051019A2430646655A1 HUB BEECH 58 58 1152740CE CONT O520 IO520* 17032SO ZONE 400 SHEARED B FFKAAE UNSCHED LANDING ENGINE SHUTDOWN YFPENGINE STOPPAGE FLT CONT AFFECTED NO WARNING INDICATION CLCLIMB 1 SO0511HW 511 E070221 TH271 823813R ALTERNATOR HUB ASSEMBLY SHEARED (DESIGNED TO DO THIS) AND/OR BECAME OBLONG AND THEN SHEARED THE SHAFT OF THE ALTERNATOR ALLOWING IT TO COME IN CONTACT WITH THE CRANKSHAFT AND CONTAMINATING THE OIL WITH METAL. 1L72 3O3 O 3A16 E5CE 20051110000632005111000063 2005 11 10 QXEA200501507 420051107A2310 SWITCH DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE CONTROL PANEL MALFUNCTIONED A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09362PH167254127 228088 520 RADIO PROBLEMS WHEN FIRST OFFICERS WAFER SWITCH ON RADIO PANEL IS MOVED. THERE IS A STUCK MIC ON WHICHEVER RADIO IS SELECTED. THE FIRST OFFICER HAS A HOT MIC AT ALL TIMES (REGARDLESS OF HOT MIC SELECTOR SWITCH POSITION). CAPTAIN CANNOT TRANSMIT ON EITHER RADIO (USING EITHER YOKE OR TILLER PTT). SUSPECT DRIPPING WATER ON FIRST OFFICER INPH/XMIT SIDE PANEL SWITCH (WINDOW IS LEAKING). REPLACED FIRST OFFICERS PTT/STBY ELEVATOR CONTROL PANEL PERFORMED AN OPERATION TEST FOR CIRCUIT BREAKER LIGHT SWITCH, CO-PILOTS FLIGHT PANEL LIGHTS, INPH/PTT SWITCH AND STANDBY ELEVATOR SWITCH IAW DASH 8 AMM TASK 27-36-11-710-801. CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20051110000642005111000064NM 2005 11 10 AALA20050715 120051029A3350P4010049 BATTERY PACK BOEING757 757223 1384957NM RROYCERB211 RB211* 54555NE CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21602AN 27053 SFO EMERGENCY LIGHTS AFT OF SEAT 28 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AFT OF SEAT 28. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F4 FRTA2NM A12EU 20051110000652005111000065NM 2005 11 10 AALA20050717 120051101A335060030451 BATTERY PACK BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21668AA 25333 SFO CEILING EMERGENCY LIGHTS FROM ROWS 28 TO 32 INOPERATIVE. REPLACED BATTERY PACK B5 107 FOR CEILING EMERGENCY LIGHTS FROM ROWS 28 TO 32. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA2NM 20051110000662005111000066EU 2005 11 10 AALA20050711 120051027A2150 DUCT AIRBUS300 A300B4605R 3930308EU GE CF6 CF680C2A5 NE A/C PACK CONTAMINATED A AALAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SW2170079 619 AFTER LANDING GEAR EXTENSION THERE WAS A SLIGHT ODOR OF PLASTIC AND SMOKE DETECTORS 2R AND 4R WERE ALARMING. LANDED WITHOUT INCIDENT. REPLACED GREEN, BLUE, AND YELLOW HYD PRES CHECK VALVES AT RESERVOIRS, APU PRESSURIZATION LINE ISOLATION CHECK VALVE, ENGINE PRES LINE ISOLATION CHECK VALVE, AND HYD RESERVOIR PRESSURIZATION FILTER ELEMENT DUE TO POSSIBLE HYDRAULIC FLUID CONTAMINATION. FOUND APU LEAKING OIL AND ENTERING APU AIR INLET. APU BLEED DUCTS CONTAMINATED WITH OIL. REPLACED APU AND ACCOMPLISHED NUMEROUS PACK BURNS. REPLACED WATER SEPARATOR BAGS AFTER LAST PACK BURN. BOROSCOPED LT AND RT ENGINES FOR OIL CONTAMINATION ON COMPRESSOR BLADES WITH NO FINDINGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F4 FRTA35EU E13NE 20051110000712005111000071SO 2005 11 10 RAIA00511007 120051105A3397 CONNECTOR EMB 145 EMB145EP 3260221SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT LOOSE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03826HK 145016 EMERGENCY LIGHTS OUT AT FWD CABIN DECK AND AT ROWS 8-12. MAINTENANCE RE-SET CONNECTOR AT LIGHT INVERTER. 2L72 4F4 FRTT00011ATTE6CH 20051110000732005111000073NM 2005 11 10 SWAA053529 120051108A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 360 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051110000742005111000074NM 2005 11 10 SWAA053530 120051108A53226546540 SHEAR TIE BOEING737 7373H4 1384600NM BS 639 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 639, BETWEEN STR 7R TO STR 8R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051110000752005111000075NM 2005 11 10 SWAA053538 120051108A53106552271 CREASE BEAM BOEING737 7373H4 1384600NM BS 500B-500C CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED D CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 500B TO BS 500C, WL 208. REPAIRED CREASE BEAM WEB PER SRM. 2L72 4F RTA16WE 20051110000762005111000076NM 2005 11 10 SWAA053539 120051108A53116546526 FRAME BOEING737 7373H4 1384600NM BS 400 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051110000772005111000077NM 2005 11 10 SWAA053540 120051108A531165C22909 FRAME BOEING737 7373H4 1384600NM BS 500C CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051110000782005111000078NM 2005 11 10 SWAA053541 120051108A53116546525 FRAME BOEING737 7373H4 1384600NM BS 380 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051110000792005111000079NM 2005 11 10 SWAA053542 120051108A53116546552 FRAME BOEING737 7373H4 1384600NM BS 827 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051110000802005111000080NM 2005 11 10 SWAA053543 120051108A53116546558 FRAME BOEING737 7373H4 1384600NM BS 907 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051110000812005111000081 2005 11 10 SWAA053528 420051108A256569633931 SPACER BOEING737 7373H4 1384600NM L2 DOOR SLIDE WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE CONTAINER FWD BRACKET GUIDE SPACER WORN. REMOVED AND REPLACED SPACER PER MM. 2L72 4F RTA16WE 20051110000822005111000082NM 2005 11 10 SWAA053531 120051108A53116546558 FRAME BOEING737 7373H4 1384600NM BS 907 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051110000832005111000083NM 2005 11 10 SWAA053532 120051108A53116546555 FRAME BOEING737 7373H4 1384600NM BS 867 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051110000872005111000087NM 2005 11 10 SWAA053536 120051108A53226546569 SHEAR TIE BOEING737 7373H4 1384600NM BS 967 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 967, BETWEEN BL 0 TO BL 3, LT SIDE. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051110000882005111000088NM 2005 11 10 SWAA053537 120051107A3350BR2013 LIGHT BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29330SW 23694 DURING SCHEDULED C2 CHECK, FOUND EEPLS STRIP LOOSE BETWEEN ROW 8 TO ROW 10. REMOVED AND REPLACED STRIP PER MM. 2L72 4F RTA16WE 20051110000912005111000091NM 2005 11 10 AALA20050724 120051027A3350BPS73 BATTERY PACK BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21357AA 24038 ORD - LEFT OVERWING SLIDE SQUIB DOES NOT TEST IN COCKPIT. REPLACED M961 AND M962 BATTERY PACKS FOR LEFT OVERWING SLIDE SQUIB IN COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20051110000962005111000096WP 2005 11 10 IXXA05SMN259S 120051013A5240 DOOR DOUG DC8 DC871F 302199DWP FS 54.000 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING C CHECK INSPECT, LT FUSE NOSE SECTION PLATING FREON SYS EXHAUST DOOR UPPER AFT JAMB CORNER CRACK DAMAGE AT STA FS 54.000, L-28L TO L-29L. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-0 FIG 13. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-3-0. REMOVED DAMAGED SECTION IAW DC8 SRM 53-2-0 FIG 13. NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D REPAIR DOUBLER (AL2024T3 0.071) + FILLER (AL2024T3 0.050) IAW DC8 SRM 53-2-0 FIG 13. CLEANED, TREATED, PRIMED AREA + REPAIR PARTS IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-0 FIG 13. 2L74 4F RT4A25 20051110000972005111000097WP 2005 11 10 IXXA05SMN262S 120051013A5330 SKIN DOUG DC8 DC871F 302199DWP FS 360.000 IMPROPER B IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW11829BX896722998 45994 DURING ROUTINE C CHECK INSPECTION, FWD FUSELAGE CTR LWR PLATING AFT OF FWD BASKET DOOR EXISTING REPAIR ALL SIDES EXCEED MAXIMUM RIVETS SPACING AT STA FS 360.000 L-36. INSTALLED HILOKS IAW FAA FORM 8110-3 # 05448 DATE 10-05-05, SEMAN DWG ED 4080 DATE 10-03-05 EO SEMAN 20051310 DATE 10-05-05 DC8 SRM 51-1-20D, DC8 SRM 51-3-1. THE HILOKS WERE INSTALLED ON CTR LWR PLATING ALT OF FWD BASKET DOOR REPAIR. 2L74 4F RT4A25 20051110000982005111000098WP 2005 11 10 IXXA05SMN263S 120051013A5330 SKIN PANEL DOUG DC8 DC871F 302199DWP STA 8.000-17.000MISREPAIRED B IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW11829BX896722998 45994 DURING C CHECK INSPECTION, EXT FS NON STANDARD REPAIR, STA 8.000 STA 17.000 BTWN L-15 AND L-16L. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05447 DATED 10-05-05, SEMAN DWG # ED-4077 DATED 10-01-05 AND EO SEMAN # 20051295 DATED 10-05-05. REMOVED EXISTING DOUBLER IAW DC8 SRM 51-1-21, DC8 SRM 51-3-0. REMOVED DAMAGED AREA IAW SEMAN DWG # ED-4097. PERFORMED NDT INSPECT ON AFFECTED AREA IAW DC8 NDT SPM PART 06-10-01-001. NO CORROSION NEITHER CRACK FOUND. FAB`D REPAIR DOUBLER (AL7075T6 0.071), 02 INTERNAL FINGER DOUBLERS (AL7075T6 0.032), FILLER (AL7075T6 0.050) IAW SEMAN DWG NR ED-4077. CLEANED, TREATED, PRIMED AREA + REPAIR PARTS IAW DC8 SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-2L74 4F RT4A25 20051110001002005111000100WP 2005 11 10 IXXA05SMN264S 120051020A5542 SKIN DOUG DC8 DC871F 302199DWP ZRT 98 UNBONDED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING ROUTINE C CHECK INSPECTION, LT RUDDER TAB SKIN UNBONDED 2 AT STA ZRT 98. REMOVED DAMAGED SKIN, CORE SECTION IAW DC8 SRM 55-2-2 PART 2 PAGE 1. FAB`D REPAIR CORE PLUG (AL. HONEY COMB CORE), REPAIR DOUBLER (ALCLAD 2024 T3 0.012) IAW DC8 SRM 55-2-2 PAR 2 PAGE 1. BONDED REPAIR CORE PLUG, REPAIR DOUBLER WITH HUSOL IAW DC8 SRM 55-2-2 PAGE 2, DC8 SRM 51-1-9 PAR 4. REFER TO N/R 2801 FOR WEIGHT AND BALANCE. 2L74 4F RT4A25 20051110001032005111000103WP 2005 11 10 IXXA05SMN253S 120051013A5330 DOUBLER DOUG DC8 DC871F 302199DWP FS 279.000 IMPROPER B IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW11829BX896722998 45994 DURING C CHECK INSPECT, LT FUS FWD CTR SECTION LWR PLATING BASKET DOOR FWD JAMB EXISTING REPAIR DBLR NOT ACCOMP 3 ROWS FASTENERS PAST CUT OUT STA FS 279.000 L-35.5L. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05461. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D. PERFORMED DETAIL VISUAL INSP. NEITHER CRACK NOR CORROSION FOUND. FAB`D REPAIR DOUBLER AND FILLER IAW SEMAN DWG # ED-4079. CLEANED, TREATED, PRIMED AREA, REPAIR PARTS IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW SEMAN DWG # ED-4079, DC8 SRM 51-1-20D, DC8 SRM 51-1-21, DC8 SRM 51-3-1. 2L74 4F RT4A25 20051110001042005111000104WP 2005 11 10 AALA20050722 120051104A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21411AA 49322 LGA - INTERIOR OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR INTERIOR OVERWING EXIT EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051110001082005111000108GL 2005 11 10 ALG2005F00089 220051030A7200 ENGINE BELL 206 206L4 1182110SW ALLSN 250C 250C30P 03013GL MAKING METAL E ALGAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 SW03272AL 52288 IN FLIGHT, ENGINE CHIP LIGHT ILLUMINATED. AFTER LANDING, NOTIFIED MAINTENANCE. THE ENGINE CHIP PLUG WAS FOUND TO HAVE METAL FLAKES. REMOVED AND REPLACED ENGINE WITH SERVICEABLE UNIT, IAW MM. (K) 1G71 3U3 UNCH2SW E1GL 20051114000012005111400001NM 2005 11 14 05FDEA03723 120051109A5311AGA71703 FRAME DOUG MD11 MD11 3023602NM BS 1841 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 CENTER CARGO BAY, STA 1841 LOWER FRAME SKIN FOUND DAMAGED. CENTER CARGO COMPT STA 1841 LOWER FRAME DAMAGE WEB REMOVED AND NEW WEB INSTALLED AS PER DRAWING AGA 7170, SRM 51-33-01 VOL II AND SRM 51-35-01, VOL II. NEW WEB P/N FX AGA 7170-3 LT AND FX AGA 7170-4 RT FABRICATED PER DRAWING AGA 7170. CLASSIFIED MAJOR REPAIR PER GMM 6-2-100. 2L73 4F RTA22WE 20051114000022005111400002NM 2005 11 14 05FDEA03691 120051107A5311 FRAME BOEING727 727200 138407ENM BS 680 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 EXISTING FRAME REPAIR IN FWD CARGO BAY AT BS680, S28R RBL 6, WL 154 (6" X 3"). REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED EXISTING FRAME REPAIR AT BS 680 RBL 6 AND FABRICATED NEW REPAIR FROM 7075T6 .071 LOT 586672. ALODINE, PRIMED AND INSTALLED NEW REPAIR IAW SRM 51-40-3, FIG 1. THIS WAS FOUND TO BE A MAJOR REPAIR 2L73 4F RTA3WE 20051114000032005111400003NM 2005 11 14 05FDEA03692 120051107A5311 FRAME BOEING727 727200 138407ENM BS 321 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 STA 321 STR 22L, FRAME CRACKED AT PREVIOUS REPAIR. REMOVED PREVIOUS REPAIR DOUBLER, FABRICATED, DRILLED, ALODINED, PRIMED REPAIR DOUBLER CAP, AND INSTALLED BS 321 STR 22L PER SRM 51-40-3. 2L73 4F RTA3WE 20051114000042005111400004NM 2005 11 14 05FDEA03693 120051107A5315 FLOORBEAM BOEING727 727200 138407ENM BS 1030 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 EXISTING UPPER FLOOR BEAM REPAIR AT BS 1030 LBL 10 WL 208, REPAIR REQUIRED EVALUATION FOR MAJ OR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USIING FAA APPROVED DATA. EVALUATED EXISTING REPAIR TO BS 1030 UPPER FLOORBEAM LBL 10 WL 208, TO BE A MAJOR REPAIR ACCOMPLISHED IAW SRM 53-10-2 FIG 7 AND SRM 53-10-8 FIG 3. REPAIR EVALUATION BASED ON A VISUAL INSPECTION WITH REPAIR INSTALLED. MAJOR REPAIR DETERMINATION BASED ON GMM 6-2-100 CRITERIA. 2L73 4F RTA3WE 20051114000052005111400005NM 2005 11 14 05FDEA03694 120051107A5311 FRAME BOEING727 727200 138407ENM BS 312 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 STA 312 STR 22L, FRAME CRACKED AT PREVIOUS REPAIR. REMOVED AND REPLACED FRAME WEB BS 312 STR 21-23L PER SRM 51-30-2 2L73 4F RTA3WE 20051114000092005111400009NM 2005 11 14 05FDEA03716 120051108A5313 STRINGER BOEING727 727200 138407ENM BS 480-530 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 EXISTING STRINGER REPAIR IN FWD CARGO BAY BS 480-530 S28R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED AND REPLACED AFT SPLICE PER SRM 53-10-3. 2L73 4F RTA3WE 20051114000172005111400017EU 2005 11 14 05FDEA03711 120051108A5320 FLOOR SUPPORT AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 MAIN CABIN LEFT SIDE FLOOR LEVEL FRAME 11 TO 14 FLOORBOARD SUPPORT ANGLE HAS SEVERAL AREAS OF EXFOLIATION REF N00670. REMOVED AND REPLACED FLOOR SUPPORT ANGLE IAW SRM 51-72-10. 2L72 4F RTA35EU 20051114000262005111400026NM 2005 11 14 AWXA200501351 120051011A534069387903 STRINGER CLIP BOEING737 7373G7 1384595NM BS 578 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 DURING C16 CHECK DISCOVERED STRINGER TIE CRACKED, .7 INCHES, AT BS 578 AND STR 10L. MAINTENANCE REMOVED INTERCOSTAL AT BS 578 AND STR 10L IAW BOEING 737-300 SRM 51-40-2-0G FIG 8. RECEIVED NEW INTERCOSTAL AND INSTALLED AT BS 578 AND STR 10L IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 3, 8 AND 12. 2L72 4F RTA16WE 20051114000282005111400028NM 2005 11 14 AWXA200501353 120051010A533065457767 SKIN PANEL BOEING737 7373S3 1384711NM BS 727E CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 DURING C18 CHECK DISCOVERED SKIN CRACKED, 2.1 INCHES, AT BS 727E+8 AND STR 24L. MAINTENANCE DAMAGED AREA IN SKIN IAW BOEING 737-300 SRM 53-00-01-2R FIG 201. FABRICATED DOUBLER AND TRIPLER IAW BOEING 737-300 SRM 53-00-01-2R FIG 201. INSTALLED FABRICATED REPAIR PARTS AT BS 727E+8 AND STR 24L IAW BOEING 737-300 SRM 53-00-01-2R FIG 201. 2L72 4F RTA16WE 20051114000302005111400030NM 2005 11 14 AWXA200501355 120051009A5340654583311 SHEAR TIE BOEING737 7373S3 1384711NM BS 188-196.5 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 DURING C18 CHECK DISCOVERED SHEAR TIE CRACKED, .5 INCHES, BETWEEN BS 188 AND BS 196.5, WL 207 AND BL 30L. MAINTENANCE REMOVED CRACKED SHEAR TIE FROM BS 188 TO BS 196.5 IAW BOEING 737-300 SRM 51-40-02-0G FIG 8. FABRICATED SHEAR TIE IAW BOEING 737-300 SRM 51-40-05-0G FIG 2 AND BOEING DWG 65-45833. INSTALLED FABRICATED REPAIR PARTS FROM BS 188 TO BS 196.5, WL 207 AND BL 30L IAW BOEING 737-300 SRM 51-40-02-0G FIG 8 AND FIG 12. 2L72 4F RTA16WE 20051114000322005111400032NM 2005 11 14 05FDEA03739 120051109A5754 SKIN BOEING727 727225 1384077NM LE K-FLAPS UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 EXISTING EXTERNAL REPAIRS ON NR 5 K-FLAP INNER TAI SKIN, 14 EACH 2" ROUND REPAIRS. REPAIRS REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIRS WERE ACCOMPLISHED USING FAA APPROVED DATA. REMOVED FASTENERS, INSTALLED WASHERS AND INSTALLED FASTENERS PER SRM 57-50-3. 2L73 4F A3WE 20051114000332005111400033NM 2005 11 14 05FDEA03740 120051109A5330 SKIN BOEING727 7272S2F 1384O81NM BS 1080 UNDAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25213FE 22935 FOUND REPAIR AFT CARGO COMPARTMENT STA 1080, LBL3. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT STA 1080 LBL 3 WAS DETERMINED TO BE IAW SRM 53-10-5 FIG 4 BASED ON AN EXTERNAL VISUAL EVALUATION WITH REPAIR INSTALLED. 2L73 4F A3WE 20051114000352005111400035NM 2005 11 14 05FDEA03743 120051109A5330 SKIN BOEING727 7272S2F 1384O81NM BS 1135 UNDAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25213FE 22935 FOUND REPAIR AFT CARGO COMPARTMENT STA 1135 RBL 8, REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT STA 1135 RBL 8 WAS DETERMINED TO BE IAW SRM 53-10-5 FIG 4 SHT 1 SHT 5 BASED ON AN EXTERNAL VISUAL EVALUATION WITH REPAIR INSTALLED. 2L73 4F A3WE 20051114000372005111400037NM 2005 11 14 05FDEA03745 120051109A5330 SKIN BOEING727 7272S2F 1384O81NM BS 560-620 UNDAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25213FE 22935 FOUND REPAIR FORWARD CARGO COMPARTMENT, STA. 560- STA 620 RBL 20. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT STA 560 STA 620 RBL 20 WAS DETERMINED TO BE IAW SRM 51-40-4 FIG 1 SHT 8 ZEE SECTION, BASED ON EXTERNAL VISUAL EVALUATION WITH REPAIR INSTALLED. 2L73 4F A3WE 20051114000392005111400039NM 2005 11 14 05FDEA03747 120051109A5330 REPAIR BOEING727 727233 138408ANM BS 1090 UNDAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25266FE 21672 FOUND REPAIR AT STA 1090 FWD EDGE OF LOWER AFT CARGO DOOR CUT-OUT. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR AT STA 1090 FWD EDGE OF LOWER AFT. CARGO DOOR CUT-OUT WAS ACCOMPLISHED ON FED-EX CARD N00292 DATED 11/01/05. INSTALLED REPAIR WAS DETERMINED TO BE IAW SRM 53-30-3 FIG 3. REPAIR CLASSIFIED AS MAJOR. 2L73 4F RTA3WE 20051114000412005111400041NM 2005 11 14 AWXA200501358 120051007A53116545815233 FRAME BOEING737 7373S3 1384711NM BS 344 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 DURING C18 CHECK DISCOVERED MAIN CABIN FRAME CRACKED, .3 INCHES, AT BS 344 AND STR 6L ABOVE THE L1 DOOR CUTOUT. MAINTENANCE REMOVED DAMAGE IAW BOEING 737-300 SRM 53-00-07-2R1 FIG 201. FABRICATED REPAIR SPLICE IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5310-05305-SS1. INSTALLED FABRICATED REPAIR PARTS AT BS 344 AND STR 6L ABOVE THE L1 DOOR CUTOUT IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5310-05305-SS1. 2L72 4F RTA16WE 20051114000432005111400043NM 2005 11 14 AWXA200501360 120051109A3150 WARNING LIGHT BOEING737 7373S3 1384711NM CONFIGURATION FALSE ACTIVATIONA AWXAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 WP28316AW 23713 FLT 876 - DURING TAKEOFF CREW ABORTED TAKEOFF. NO REASON WAS SPECIFIED. SAFETY EVENT PERSONNEL SPOKE WITH CAPTAIN AND RECEIVED VERBAL CONFORMATION OF EVENT. CAPTAIN REPORTED THAT THE CONFIG WARNING WENT OFF, TAKE OFF POWER WAS NOT SET AND THAT THE SPEED BRAKE WAS IN THE CORRECT POSITION. WIGGLED SPEED BRAKE HANDLE, SYSTEM FUNCTIONED NORMALLY AFTERWARDS. 2L72 4F RTA16WE 20051114000452005111400045NM 2005 11 14 05FDEA03699 120051107A5510 NONE DOUG MD11 MD11 3023602NM ZONE 300 NONE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 EMPENNAGE: BARREL NUT RT NR 26 BORE, FOUND WITH EXISTING 2-STEP. BORE EVALUATED AND FOUND WITHIN LIMIT AS PER FEDEX EO 1-5510-7-5000 D1 PT1. BUSHING FABRICATED AND INSTALLED AS PER FEDEX EO 1-5510-7-5000 D1 PT1. N/R, NO M OR D. 2L73 4F RTA22WE 20051114000472005111400047WP 2005 11 14 05FDEA03701 120051108A5320 WEB DOUG DC10 DC1010 3022110WP BS 350 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 COCKPIT AREA FOUND SEVERE CORROSION WITH EXFOLIATION ON WEB AT STA 350 X47 Z - 10.925. REMOVED CORROSION IAW SRM 53-00-01 VOL 1 FIG 1B, MATERIAL REMOVED IS OUT OF LIMIT CUT DAMAGED SECTION OF WEB IAW 53-00-01 FIG 10 SHT 4. 2L73 4F A22WE 20051114000492005111400049WP 2005 11 14 05FDEA03703 120051108A5312 REPAIR DOUG DC10 DC1010 3022110WP BULKHEAD UNDAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 FOUND FLUSH DOUBLER REPAIR AT AFT PRESSURE BULKHEAD LOWER SECTION STA 2007 FROM X25 TO X-25 LONGERON 48L TO 48R. PERFORMED A GVI OF EXISTING REPAIR IAW EO 8-5100-7-5001 CRITERIA FOUND IN COMPLIANCE WITH SRM 53-40-00 PAG 9A. 2L73 4F A22WE 20051114000512005111400051WP 2005 11 14 05FDEA03705 120051108A5347 REPAIR DOUG DC10 DC1010 3022110WP BS 625 UNDAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 FOUND SEAT TRACK PLUG REPAIR AT STA 625 X 27. PERFORMED A GVI OF EXISTING REPAIR IAW EO 8-5100-7-5001 CRITERIA FOUND REPAIR IN COMPLIANCE WITH SRM 53-70-00 FIG 2 PAG 9. 2L73 4F A22WE 20051114000532005111400053WP 2005 11 14 05FDEA03707 120051108A5245 REPAIR DOUG DC10 DC1010 3022110WP BS 595 UNDAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 AFT AIR CONDITIONING ACCESS DOOR, AFT TOP CORNER FOUND AN EXTERNAL TRIPLE DOUBLER REPAIR AT STA 595 LT SIDE. PERFORMED A GVI OF EXISTING REPAIR IAW EO 8-5100-7-5001 CRITERIA FOUND IN COMPLIANCE WITH SRM 53-50-00 PAG 19. 2L73 4F A22WE 20051114000552005111400055WP 2005 11 14 IXXA05SMN267S 120051026A5414 SKIN DOUG DC8 DC871F 302199DWP YN 254 S ELONGATED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING C CHECK INSPECTION, NR 4 PYLON UPPER PLATING HAS ELONGATED HOLES AT STA YN 254 S. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05471 DATED 10-18-05, SEMAN DWG # ED-4084 DATED 10-11-05 AND EO SEMAN # 20051341 DATED 10-18-05. REMOVED FASTENERS IAW DC8 SRM 51-1-21, DC8 SRM 51-3-0. REMOVED DAMAGED SECTION IAW SEMAN DWG # ED-4084. NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D (02EA) EXTERNAL REPAIR DOUBLERS (AL7075T6 0.100) + (02EA) FILLERS (AL7075T6 0.100) + FILLER (AL7075T6 0.032) IAW SEMAN DWG # ED-4084. CLEANED, TREATED, PRIMED FILLERS + INNER SIDE OF REPAIR DOUBLERS IAW DC8 SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW DC8 SRM 512L74 4F RT4A25 20051114000572005111400057WP 2005 11 14 IXXA05RNG074S 120050924A5330 SKIN DOUG DC8 DC872 302199BWP STA 360-380 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK, FOUND CORROSION ON INTERNAL SKIN OF PASSENGER WINDOW STA 360 AND 380 LH. CORRODED AREA WAS REMOVED AND REPAIR DOUBLER WAS INSTALLED IAW EWO ATI 53-024, SRM 53-2-0 FIGURE 22A AND BOEING SERVICE REQUEST 1-129925991. 2L74 4F RT4A25 20051109001252005110900125WP 2005 11 9 05FDEA03670 120051107A5753 DOUBLER DOUG DC10 DC1010 3022110WP TE FLAPS UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 FOUND EXTERNAL DOUBLER REPAIR AT LEFT WING INBOARD FLAP, INBOARD TRAILING EDGE AREA BETWEEN WING STATION XIF187 AND XIF189. PERFORMED A GVI OF EXISTING DOUBLER IAW EO8-5100-7-5001 CRITERIA REQUEST FOUND IN COMPLIANCE WITH SRM 57-00-01 FIG 4 SHT 2 VOL 1. 2L73 4F A22WE 20051109001272005110900127NM 2005 11 9 SWAA053513 120051106A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29219WN 32490 DURING SCHEDULED MV2 CHECK, FOUND EEPLS TRACK COVER MISSING AT ROW 8 ABC. INSTALLED COVER PER MM. 2L72 4F RTA16WE 20051109001312005110900131 2005 11 9 SWAA053517 420051107A256569451433 WINDOW BOEING737 7375H4 138449DNM R2 DOOR SLIDE LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29522SW 26564 R2 DOOR EMERGENCY EVAC SLIDE CONTAINER VIEWING WINDOW LOOSE. SECURED WINDOW PER MM. 2L72 4F RTA16WE 20051109001402005110900140NM 2005 11 9 SWAA053526 120051106A5315BAC1509 FLOORBEAM BOEING737 7377H4 1384404NM BS 773 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29792SW 27887 DURING SCHEDULED 5Y CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 773, RBL 3. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20051109001622005110900162WP 2005 11 9 05FDEA03690 120051107A5330 DOUBLER DOUG DC10 DC1010 3022110WP FUSELAGE UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 AT FUSELAGE STA 392 RT SIDE FOUND INTERNAL DOUBLER REPAIR AT Z53 BEHIND CO-PILOT WINDOW. PERFORMED A GVI OF EXISTING DOUBLER IAW EO8-5100-7-5001 CRITERIA, FOUND DOUBLER IN COMPLIANCE WITH SRM 53-20-00 FIG 13 SHT 14. 2L73 4F A22WE 20051109001712005110900171NM 2005 11 9 EIA2005172 120051011A5315 FLOORBEAM BOEING747 747212B 1384886NM BS 360 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 BS 360 FLOORBEAM UPPER CHORD HORIZONTAL FWD FLANGE LBL 55 FLOOR PANEL AFT HOLE CRACKED RUNNING FWD APPROX 0.060 INCH LONG. DEFECTIVE FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-10-07 FIG 9 (HORIZONTAL FWD FLANGE LBL 55). 2L74 4F A20WE 20051109001772005110900177NM 2005 11 9 EIA2005178 120051011A5315 FLOORBEAM BOEING747 747212B 1384886NM BS 340 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 BS 340 FLOORBEAM UPPER CHORD HORIZONTAL AFT FLANGE RBL 52 FLOOR PANEL ATTACH HOLE CRACKED RUNNING FWD APPROX 0.040 INCH. DEFECTIVE FLOORBEAM UPPER CHORD REPAIRED AS PER S/B 747-53A2431 FIG 10 (HORIZONTAL AFT FLANGE RBL 52). 2L74 4F A20WE 20051109001782005110900178EU 2005 11 9 05FDEA03636 120051104A5347 SEAT TRACK AIRBUS310 A310203 3930313EU FR 74-79 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 MAIN CABIN SEAT TRACK 3L AT FS 74 TO FS 79 HAS 4 EA AREAS OF CORROSION REF N00522. REPAIRED SEAT TRACK IAW SRM 53-10-16. 2L72 4F RTA35EU 20051109001832005110900183NM 2005 11 9 05FDEA03624 120051104A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 DURING HFEC INSPECTION, FOUND CRACK INDICATION AT LEFT WING, END OF STRINGER 9. 2L73 4F RTA22WE 20051109001872005110900187NM 2005 11 9 05FDEA03631 120051104A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 DURING HFEC INSPECTION, FOUND CRACK AT LEFT WING, END OF STRINGER 44 APPROXIMATELY 1/2 INCH. REPAIR CARRIED OUT IAW SRM 57-20- 00 FIG. 10 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051109001962005110900196EU 2005 11 9 05FDEA03638 120051104A5347 SEAT TRACK AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 NR 3 SEAT TRACK HAS 3 AREAS OF CORROSION BETWEEN FS 47 AND FS 51, REF N00618. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-72-10. 2L72 4F RTA35EU 20051109002082005110900208NM 2005 11 9 EIA2005238 120051006A5712 RIB BOEING747 747212B 1384886NM WING CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 LE CAVITY SUPPORT RIB CRACKED AT NR 4 V/C FLAP OB LINKAGE IB AND OB HOLE FLANGE AREA. REPAIRED DEFECTIVE SUPPORT RIB PER RS R57-51-35370. 2L74 4F A20WE 20051109002112005110900211NM 2005 11 9 EIA2005241 120051027A5754 SKIN BOEING747 747212B 1384886NM FLAP BULLNOSE REPAIRED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 PER CUSTOMER REQUEST CHECK, NR 3 L/E FLAP BULLNOSE FAIRING FOUND PREVIOUSLY REPAIRED. DEFECTIVE BULLNOSE FAIRING SKIN REPAIRED PER SRM 57-50-03, FIG 3. 2L74 4F A20WE 20051109002292005110900229NM 2005 11 9 EIA2005216 120051006A5320 SUPPORT BRACKET BOEING747 747212B 1384886NM BS 1394 CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 KEEL BEAM PANEL SUPPORT ATTACH ANGLE SURFACE CORRODED AT STA 1394 LBL 16 TO RBL 16. REPLACED DEFECTIVE SUPPORT PER SRM 51-10-01, PG 9. 2L74 4F A20WE 20051109002362005110900236NM 2005 11 9 EIA2005154 120050830A5330 SKIN BOEING747 747132 1384882NM BS 2020 BULGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09479EV 19898 FOUND BS 2020 STR 45R FUSELAGE SKIN HAS BULGE UP. SUBJECT AREA FUSELAGE SKIN REPAIRED IAW EA-53-0991. 2L74 4F A20WE 20051109002432005110900243NM 2005 11 9 EIA2005204 120051011A5315 FLOORBEAM BOEING747 747212B 1384886NM BS 340 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 FOUND BS 340 FLOORBEAM UPPER CHORD HORIZONTAL FWD FLANGE LBL 45 FLOOR PANEL ATT HOLE CRACKED RUNNING FWD APPROX .125". REPAIRED PER SRM 53-10-07, FIG 23. 2L74 4F A20WE 20051109002462005110900246NM 2005 11 9 EIA2005207 120051007A5321 FLOOR PANEL BOEING747 747212B 1384886NM BS 2198 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 FOUND BS 2198 LBL 99 FLOOR WEB CRACKED. REPAIRED FLOOR WEB PER SRM 51-40-02, FIG 1. 2L74 4F A20WE 20051109002542005110900254NM 2005 11 9 EIA2005228 120051006A5753 TIE ROD BOEING747 747212B 1384886NM FLAP TRACK CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 LHW NR 4 FLAP TRACK TIE ROD UPPER MOUNT FTG FLANGE CRACKED. REPAIRED DEFECTIVE CHORD PER SRM 51-40-04, FIG 3. 2L74 4F A20WE 20051109002612005110900261NM 2005 11 9 EIA2005235 120051004A5712 RIB BOEING747 747212B 1384886NM LT WING CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 LHW LE CAVITY SUPPORT RIB CRACKED AT NR 5 VC FLAP IB LINKAGE OB D HOLE FLANGE AREA. REPAIRED DEFECTIVE SUPPORT RIB PER R.R. NO. R57-51-35370. 2L74 4F A20WE 20051109002632005110900263EU 2005 11 9 05FDEA03633 120051104A5347 SEAT TRACK AIRBUS310 A310203 3930313EU FR 45-50 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 FOUND MAIN DECK FS 45 TO 50 SEAT TRACK 4 LEFT HAS 4 EA AREAS OF EXFOIATION REF N00610. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-72-10. 2L72 4F RTA35EU 20051109002702005110900270EU 2005 11 9 KBM2005F00333 120051102A2432RG355 BATTERY SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE MASTER DISCHARGED E KBMAO OTHER O OTHER TXTAXI/GRND HDL 1 WP19351WM1120 2167 BATTERY, REMOVED DUE TO SLOW START. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051110000012005111000001NM 2005 11 10 MWEA050121 120051109A5522993780413 SKIN DOUG MD88 MD88 3023688NM LT ELEVATOR TEMPORARY A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 LEFT ELEVATOR HAS A TEMPORARY SKIN INSTALLED AT STATION XE182 TO TIP WATCH ITEM NUMBER W000403. REMOVED AND REPLACED NEW SKIN SECTION. 2L72 4F RTA6WE 20051110000022005111000002 2005 11 10 MWEA050122 420051108A2210 AUTOPILOT SYS BOEING717 717200 1383700NM COCKPIT WARNING LIGHT A MWEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31923ME 55185 AUTO PILOT BOX CONTINUOUSLY FLASHED AMBER THEN WHITE, AUTO PILOT WOULD NOT ENGAGE AND BOTH MULTIFUNCTION CONTROL DISPLAY UNIT WOULD NOT RESPOND. COMPLIED WITH FIM TASK AND RETURN TO SERVICE OF AUTO PILOT SYSTEM ON BOTH NR 1 AND NR 2 FLIGHT CONTROL COMPUTER, NO OTHER FAULTS NOTED. OK FOR SERVICE. 2L72 4F TRA6WE 20051110000072005111000007NM 2005 11 10 AALA20050725 120051107A3350 LIGHT BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21377AN 25446 DFW - EMERGENCY LIGHT AT MID GALLEY BULKHEAD ON LEFT SIDE INOPERATIVE. REPLACED LIGHT ASSEMBLY AT MID GALLEY BULKHEAD ON LEFT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20051110000142005111000014EA 2005 11 10 SWIA200515810 120051104A2760278003 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION LDLANDING 1 NM07465SW 7845 OB GROUND SPOILER CAUTION ON LANDING. REPLACED LT WING OUTBOARD GROUND SPOILER ACTUATOR IAW CRJ MM 27-60-00. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051110000172005111000017EA 2005 11 10 SWIA200515813 120051104A2710 CONTROL CABLE CNDAIRCL600 CL6002B19 1900309EA AILERONS OUT OF RIG A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07431SW 7536 AILERONS HAVE A CATCH/CLICK FEEL AFTER NEAR NEUTRAL POSITION WHEN YOKE IS TURNED LEFT AND RIGHT. CHECKED CABLE CIRCUITS. RERIGGED RIGHT AILERON FUSELAGE WING CABLES AND RETENSIONED SAME CABLES IAW 27-11-00. 2L72 4F RTA21EA 20051110000202005111000020NM 2005 11 10 EIA2005189 120051011A5315 FLOORBEAM BOEING747 747212B 1384886NM BS 400 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 U/D BS 400 FLOORBEAM UPPER CHORD HORIZONTAL FWD FLANGE LBL 23" FLOOR PANEL ATT HOLE CRACKED RUNNING FWD APPROX .060 AND AFT APPROX .060" LONG. REPAIRED PER SB747-53A2452 FIG 9. 2L74 4F A20WE 20051110000412005111000041EA 2005 11 10 SWIA200515817 120051106A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY FALSE ACTIVATIONA SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07941SW 7750 RECEIVED "SMOKE CARGO" MSG WHILE PARKED AT THE GATE. VISUALLY CHECKED CARGO AREA AND FOUND NOTHING ABNORMAL. REPLACED NR 1 CARGO SMOKE DETECTOR. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051110000442005111000044EA 2005 11 10 SWIA200515820 120051101A2751601R590141 DETECTOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07954SW 7815 FLAPS DEGRADED STATUS MSG. REPLACED SKEW DET UNIT IAW 27-51-15. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051110000452005111000045EA 2005 11 10 SWIA200515821 120051024A2760C13045BA04 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA SPOILERS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07713SK121 121 10174 SPLR/STAB FAULT STATUS MESSAGE. REPLACED SSCU 1. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051110000532005111000053EU 2005 11 10 20051181 120051107A2750 FLAP SYSTEM EMB ERJ170ERJ170100 EU GE CF34 CF34* NE TE FLAPS UNKNOWN A UHLAB EMER. DESCENT J WARNING INDICATION DEDESCENT 1 GL17979RP 17000088 WHILE ON DECENT, THE CREW RECEIVED A NO FLAP/FLAP LO RATE WARNING. THE CREW MADE AN EMERGENCY DECENT AND LANDED WITHOUT INCIDENT. 2L74 4F4 FRTA56NM E15NE 20051110000722005111000072SO 2005 11 10 RAIA00511008 120051107A3350 LIGHT EMB 145 EMB145ER 3260211SO CABIN DISCONNECTED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03808HK 145157 EMERGENCY LIGHT ON CEILING AT EXIT ROW INOPERATIVE.. MAINTENANCE RECONNECTED LIGHT CONNECTOR PLUG. 2L72 4F RTT00011AT 20051110000842005111000084NM 2005 11 10 SWAA053533 120051108A53116546549 FRAME BOEING737 7373H4 1384600NM BS 767 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 8L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051110000892005111000089NM 2005 11 10 AALA20050721 120051103A3350P4010049 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21175AN 32394 SJU - EMERGENCY LIGHTS FROM ROWS 16 TO 27 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FROM ROWS 16 TO 27. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20051110000922005111000092NM 2005 11 10 AALA20050720 120051102A3350D71702001 BATTERY PACK BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21784AN 29588 ORD - FOUND OVERHEAD EMERGENCY EXIT AISLE LIGHT IN LEFT HAND FIRST CLASS FORWARD AREA INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY EXIT AISLE LIGHT IN LEFT HAND FIRST CLASS FORWARD AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20051110000932005111000093EU 2005 11 10 AALA20050713 120051029A3350BR9664103 LIGHT AIRBUS300 A300B4605R 3930308EU CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2114056 463 JFK - FORWARD BULKHEAD RIGHT HAND FLOOR EMERGENCY LIGHT INOPERATIVE. REPLACED FORWARD BULKHEAD RIGHT HAND FLOOR EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20051110001012005111000101WP 2005 11 10 IXXA05SMN196S 120050922A7830 FRAME DOUG DC8 DC871F 302199DWP THRUST REVERSER CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING ROUTINE C CHECK INSPECTION, NR 2 ENGINE, T/R LT INTERNAL PART FRAME CRACKED 2 AT 10 O’CLOCK POSITION, YN 208.000. REMOVED DEFLECTION FAIRING SEAL, PERFORMED STOP HOLE OF 0.06 IAW CFM 56-2 MM 78-31-41 REP. 016 PAGE 2. FAB`D STIFFENER (STEEL SHEET 0.080 AMS 5504) IAW CFM 56-2 MM 78-31-41 REP. 016 PAGE 2. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW STIFFENER WITH BLIND BOLTS AND REINSTALLED DEFLECTION FAIRING SEAL IAW CFM 56-2 MM 78-31-41 REP 016 PAGE 2. 2L74 4F RT4A25 20051114000072005111400007NM 2005 11 14 05FDEA03697 120051107A5313 STRINGER BOEING727 727200 138407ENM BS 720F-740 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 MAPPED EXISTING REPAIR ON STRINGER, BS 720 F-740, STR 26R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. STRINGER REPAIR AT BS 720F-740 STR 26 RT ORIGINAL THICKNESS IS 0.080 HAT SECTION IS 0.090 IT HAS 7 EACH FASTENERS IN ROW -A- 3/16" LOCK FASTENERS AND 5 EACH IN ROW -B- 3/16" LOCK FASTENERS REPAIR IS PER SRM 53-10-3 FIG 1 BASED ON A VISUAL EVALUATION WITH THE REPAIR INSTALLED AND GMM 6-2-100 CRITERIA IS A MAJOR REPAIR. 2L73 4F RTA3WE 20051114000112005111400011NM 2005 11 14 SWAA053548 120051109A335007912 COVER BOEING737 7377H4 1384404NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29443WN 29838 EEPLS TRACK COVER LOOSE AT FWD END. SECURED COVER PER MM. 2L72 4F RTA16WE 20051114000132005111400013NM 2005 11 14 SWAA053550 120051109A53106552271 CREASE BEAM BOEING737 7373H4 1384600NM BS 500A-500B CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED D-CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 500A TO BS 500B, WL 208. REPAIRED CREASE BEAM WEB PER SRM. 2L72 4F RTA16WE 20051114000592005111400059WP 2005 11 14 IXXA05SMN256S 120051013A5330 REPAIR DOUG DC8 DC871F 302199DWP FS 1250.00 IMPROPER B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING ROUTINE C CHECK INSPECTION, LT FUSELAGE AFT CENTER SECTION WINDOW BELT EVALUATE CONFORMITY PER SRM AT STA FS 1250.00 L-15.5 LT. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-0 FIG 22A, TR # 53-170, EO SEMAN # 20051302 DATED 09-28-05. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21. FAB`D REPAIR DOUBLER (7073) (AL7075T6 0.190) IAW DC8 SRM 53-2-0 FIG 22A (SHEET 1, 3, 14) DC8 SRM 53-4-1 FIG 19 ITEM A. CLEANED, TREATED, PRIMED AREA + REPAIR DOUBLER IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED REPAIR DOUBLER IAW DC8 SRM 53-2-0 FIG 22A (SHEET 3, 12, 13, 14), DC8 SRM 51-1-21, DC8 SRM 51-1-20D, DC8 SRM 51-3-1. 2L74 4F RT4A25 20051114000612005111400061WP 2005 11 14 IXXA05SMN265S 120051024A5740 FITTING DOUG DC8 DC873F 302199FWP XW 410.000 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING ROUTINE C CHECK INSPECTION, RT FLAP SUPPORT FITTING CRACKED AT STA. XW 410.000. REMOVED AND REPLACED RT FLAP LINK SUPPORT AT STA XW 410.000 IAW DC8 MM 27-51-12 PAGES 201-204. REFER TO N/R FOR OPS CHECK. 2L74 4F RT4A25 20051114000622005111400062WP 2005 11 14 IXXA05SMN266S 120051026A5522 SKIN DOUG DC8 DC871F 302199DWP XE 200.2379 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING C CHECK INSPECT, LT HORIZ STAB ELEVATOR UPPER SKIN CRACKED ½, XE 200.2379. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3. REMOVED FASTENERS IAW DC8 SRM 51-1-21. REMOVED DAMAGED SECTION IAW SEMAN DWG # ED-4085. NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D EXTERNAL REPAIR DOUBLER (AL2024T3 0.040), FILLER (AL2024T3 0.016) IAW SEMAN DWG # ED-4085. CLEANED, TREATED, PRIMED AREA + FILLER + INNER SIDE OF EXTERNAL REPAIR DOUBLER IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACE IAW DC8 SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW SEMAN DWG # ED-4085, DC8 SRM 51-1-21. PERFORMED LT ELEVATOR BALANCING IAW DC8 SRM 51-4-1 PG 1. FOUND WITHIN TOLER2L74 4F RT4A25 20051114000642005111400064NM 2005 11 14 AWXA200501361 120051028A532065C333701 INTERCOSTAL BOEING737 7373S3 1384711NM BS 960 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 DURING C13 CHECK DISCOVERED CORROSION AROUND NUTPLATE ON FLOOR ATTACHMENT INTERCOSTAL AT BS 960, WL 208.1 AND BL 20L. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-51-1A1 FIG 101. REMOVED AND INSTALLED NEW INTERCOSTAL AT BS 960, WL 208.1 AND BL 20L IAW BOEING 737-300 SRM 51-40-02-0G AND 51-40-05-0G. 2L72 4F RTA16WE 20051114000662005111400066NM 2005 11 14 AWXA200501363 120051027A5320654589533 CHANNEL BOEING737 7373S3 1384711NM BS 907 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 DURING C13 CHECK DISCOVERED LEVEL 2 CORROSION ON THE AFT PIT STRINGER CHANNEL AT BS 907 AND STRINGER 27L. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-00-03-1A1. REMOVED AND FABRICATED CHANNEL IAW BOEING 737-300 SRM 51-40-02-0G AND BOEING DWG 65-45895. INSTALLED FABRICATED REPAIR PARTS AT BS 907 AND STR 27L IAW BOEING 737-300S SRM 51-40-02-0G. 2L72 4F RTA16WE 20051114000682005111400068NM 2005 11 14 AWXA200501365 120051017A532065479577 WEB BOEING737 7373S3 1384711NM BS 860 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 DURING C18 CHECK DISCOVERED CORROSION AROUND FASTENER HOLES IN WEB AT BS 860, WL 158 AND BL 18R. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-15-1A1. REMOVED AND INSTALLED NEW WEB AT BS 860, WL 158 AND BL 18R IAW BOEING 737-300 SRM 51-40-02-0G FIG 12. 2L72 4F RTA16WE 20051114000702005111400070NM 2005 11 14 AWXA200501367 120051007A531265163007 BULKHEAD BOEING737 7373S3 1384711NM BS 178 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 DURING C18 CHECK DISCOVERED 178 BULKHEAD WEB CRACKED, 1.0 INCHES, AT BS 178, WL 207 AND BL 1.5R. MAINTENANCE CUTOUT DAMAGE ON WEB IAW BOEING 737-300 SRM 53-10-08-2R11 FIG 201. FABRICATED DOUBLER IAW BOEING 737-300 SRM 53-10-08-2R11 FIG 201. INSTALLED FABRICATED REPAIR PARTS AT BS 178, WL 207 AND BL 1.5R IAW BOEING 737-300 SRM 53-10-08-2R11. 2L72 4F RTA16WE 20051114000722005111400072NM 2005 11 14 AWXA200501369 120051010A5330654577677 SKIN PANEL BOEING737 7373S3 1384711NM BS 727E CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 DURING C18 CHECK DISCOVERED FUSELAGE SKIN CRACKED, 3.0 INCHES IN LENGTH, AT BS 727E+5 AND STR 25R. MAINTENANCE CUT OUT DAMAGED SKIN AT BS 727E+5 AND STR 25R IAW BOEING 737-300 SRM 53-00-01-2R31 FIG 201. FABRICATED DOUBLER, TRIPLER, AND FILLERS IAW BOEING 737-300 SRM 53-00-01-2R31. INSTALLED FABRICATED REPAIR PARTS AT BS 727E+5 AND STR 25R IAW BOEING 737-300 SRM 53-00-01-2R31. 2L72 4F RTA16WE 20051114000742005111400074NM 2005 11 14 AWXA200501371 120051010A532065176856 STRAP BOEING737 7373S3 1384711NM BS 348-252 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 DURING C18 CHECK DISCOVERED STRAP CRACKED, .38 INCHES IN LENGTH BETWEEN BS 348 AND BS 252, STRINGER 16L. MAINTENANCE REMOVED AND INSTALLED NEW STRAP BETWEEN BS 348 AND BS 252, STRINGER 16L IAW BOEING 737-30 SRM 51-40-02-0G. 2L72 4F RTA16WE 20051114000762005111400076NM 2005 11 14 AWXA200501373 120051005A5754 SKIN BOEING757 7572S7 1384962NM NR 3 SLAT DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28904AW A10065 23566 DURING C10 CHECK DISCOVERED SMALL AREA OF DELAMINATION ON THE LOWER SURFACE OF THE NO. 3 SLAT TRAILING EDGE WEDGE AT WS 460L. MAINTENANCE REMOVED DELAMINATION AREA ON THE NR 3 SLAT IAW BOEING 757-200 SRM 51-70-10-2R. FABRICATED DOUBLER AND FILLER IAW BOEING 757-300 SRM 51-40-10-2R. BONDED REPAIR PARTS TO THE NR 3 SLAT TRAILING EDGE WEDGE AT WS 460L IAW BOEING 757-200 SRM 51-70-10-2R. 2L72 4F RTA2NM 20051114000782005111400078EU 2005 11 14 AWXA200501344 120051105A3020326975 VALVE AIRBUS320 A320232 3930326EU ANTI ICE SYS UNKNOWN A AWXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP28656AW244784068 1079 DURING FLT, EN ROUTE CREW REPORTED NR 1 ENGINE ANTI-ICE VALVE CLOSED WOULD NOT OPEN. WAS CHARTER FLIGHT, CREW DIVERTED INTO LAS AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE INTAKE ANTI-ICE VALVE IAW AIRBUS 319/320 AMM 30-21-51 AND AMERICA WEST AIRLINES TASK CARD F1B30301. OPERATIONAL CHECKS WERE NORMAL. DID NOT CONFIRM FAILURE. UNIT WAS INSPECTED, OVERHAULED AND TESTED IAW CMM 30-28-52 REV 1. 2L72 4F RTA28NM 20051114000802005111400080NM 2005 11 14 AWXA200501357 120051010A53306545774 SKIN BOEING737 7373S3 1384711NM BS 727D CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 DURING C18 CHECK DISCOVERED FUSELAGE SKIN CRACKED, 1.5 INCHES, AT BS 727D+3 AND STR 23L. MAINTENANCE TRIMMED OUT CRACK IAW BOEING 737-300 SRM 51-10-02-0G. FABRICATED REPAIR DOUBLER, TRIPLER AND TEAR STRAP IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5361-05301-ES2. INSTALLED FABRICATED REPAIR PARTS AT BS 727D+3 AND STR 23L IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5361-05301-ES2. 2L72 4F RTA16WE 20051114000822005111400082WP 2005 11 14 05FDEA03722 120051108A5347 SEAT TRACK DOUG DC10 DC1030 3023501WP ZONE 100 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25310FE 48299 MAIN CABIN STA 938 RBL 47.5 SEAT TRACK WORN, BLENDED AREA IAW DC10 SRM 53-70-00 VOL1 AREA HAS 50 PERCENT MAT'L LOSS AREA IS OUT OF LIMITS. MAT'L ID FOR NEW SEAT TRACK SECTION 54929150-1200 PO NR 502938.1 IAW DC10 SRM 53-42-01 VOL II. FABRICATED SEAT TRACK SECTION IAW DC10 SRM 53-70-00 FIG 1 VOL1 ALODINED AND PRIMED IAW DC10 SRM 51-21-01 VOL I. INSTALLED NEW SEAT TRACK SECTION IAW DC10 SRM 51-31-01 VOL II. REMOVED AND REINSTALLED FLOORBOARDS IAW DC10-30 AMM 53-21-01-2 N/R N00446 WORK ORDER 00030375. 2L73 4F A22WE 20051114000842005111400084EU 2005 11 14 05FDEA03724 120051109A2550 ROLLER TRAY AIRBUS310 A310203 3930313EU CARGO BAY CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 LT SIDE ROLLER TRAY 1 OB OF CENTER HAS 3 EA SPOTS OF CORROSION 2 AT FS 34 TO FS 35 AND 1AT FS 36 REF N00469. REMOVED AND REPLACED ROLLER TRAY IAW SRM 51-72-10. 2L72 4F RTA35EU 20051114000862005111400086EU 2005 11 14 05FDEA03727 120051109A5347 SEAT TRACK AIRBUS310 A310203 3930313EU FR 61-67 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 FOUND MAIN DECK CARGO NR 1 SEAT TRACK BETWEEN FRAMES 61 AND 67 HAS 10 AREAS WORN REF N00439. REPAIRED SEAT TRACK IAW SRM 53-10-16. 2L72 4F RTA35EU 20051114000882005111400088WP 2005 11 14 05FDEA03729 120051109A5754 SKIN DOUG DC10 DC1030 3023501WP RT WING LE FLAP DENTED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25310FE 48299 RT WING O/B FLAP LOWER O/B SURFACES HAS DENTS. FOUND DENTS AT X0F 775-781 TO BE WITHIN ALLOWABLE LIMITS IAW DC10 SRM 57-10-00 FIG 48 VOL 1. FOUND DENT AT X0F 783-787 TO BE OUT OF LIMITS IAW DC10 SRM 57-10-00 FIG 48 VOL1. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER AND FILLER, MAT'L ID 2024-T3 .050 PO#505741.2 AND SHIMMED IAW DC10 SRM 57-10-00 FIG 85 VOL1. ALODINED AND PRIMED IAW DC10 SRM 51-21-01 VOL 11 AND DC10 SRM 51-41-01 VOL.2. 2L73 4F A22WE 20051114000902005111400090NM 2005 11 14 05FDEA03649 120051107A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 BARREL NUT LT NR 7 BORE CORROSION EXCEED LIMIT. COMPLIED WITH FEDEX EA 1-5510-94568 2L73 4F RTA22WE 20051114000922005111400092NM 2005 11 14 SWAA053544 120051108A5754 SKIN BOEING737 7373Q8 1384670NM RT WING SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29317WN 24068 DURING SCHEDULED C2 CHECK, FOUND NR 6 L/E SLAT LOWER SKIN CRACKED. REPAIRED SLAT PER SRM. 2L72 4F RTA16WE 20051114001272005111400127NM 2005 11 14 05FDEA03721 120051108A5320 FLOOR SUPPORT BOEING727 727225 1384077NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 FOUND SEAT TRACK SUPPORT CORRODED BS 760-848 LBL45. REMOVED AND REPLACED UPPER CHORD SUPPORT BEAM AND SEAT TRACK IAW BAC DWG 65-16279 AND FX B727 SRM 53-10-5 FIG 2. ALODINED AND PRIMED IAW FX B727 SRM 51-10-2. 2L73 4F A3WE 20051114001282005111400128EA 2005 11 14 COMA0560585 120051103A2410820465 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA ADG MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01982CA1903813728 7168 FLIGHT 5828 - ADG DEPLOYED AFTER T/O. REPLACED THE ADG CONTROL PANEL. 2L72 4F RTA21EA 20051114001302005111400130EA 2005 11 14 COMA0560595 120051110A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01735CA 7267 FLIGHT 5518 - FLAPS FAILED AT ZERO DEGREES ON APPROACH TO JFK. FLIGHT LANDED SAFELY. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE FIRST EVENT MAINTENANCE ACTION PARAGRAPH (B) 1, 2, 3 (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2L72 4F RTA21EA 20051114001312005111400131EU 2005 11 14 05FDEA03732 120051109A5347 SEAT TRACK AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 FOUND MAIN CABIN LEFT SIDE BETWEEN FS 15 AND 19 SEAT TRACK 1L HAS EXFOLIATION CORROSION IN 3 EA AREAS REF N00669. REMOVED AND REPLACED SEAT TRACK BTW FS 15 AND 19 NR 1L IAW SRM 51-72-10. 2L72 4F RTA35EU 20051114001322005111400132NM 2005 11 14 05FDEA03734 120051109A5753 FLAP TRACK BOEING727 727225 1384077NM NR 6 FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 NR 6 FLAP TRACK, AFT MOUNTING SURFACE IS CORRODED. RECEIVED NR 6 FLAP TRACK INSTALLED ON FED EX WC 27X5708-03. 2L73 4F A3WE 20051114001332005111400133NM 2005 11 14 05FDEA03733 120051109A5753 FLAP TRACK BOEING727 727225 1384077NM NR 6 FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 NR 6 FLAP TRACK, FWD MOUNT BUSHINGS ARE CORRODED. NR 6 FLAP TRACK REPLACED ON FED EX WC 27X5708-03. 2L73 4F A3WE 20051114001352005111400135EU 2005 11 14 05FDEA03736 120051109A5347 SEAT TRACK AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 FOUND MAIN DECK RIGHT SIDE FS 15 THRU FS 19 SEAT TRACK 2R HAS SEVERAL AREAS OF CORROSION AND PITTING CORROSION, REF N00664. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-72-10. 2L72 4F RTA35EU 20051114001372005111400137EU 2005 11 14 05FDEA03738 120051109A5347 SEAT TRACK AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 FOUND MAIN DECK FLOOR LEVEL FS 35 AT SEAT TRACK 6R SEAT TRACK HAS 1 SQ INCH OF CORROSION, REF N00606. REPAIRED SEAT TRACK IAW SRM 53-10-16 FIG 208. 2L72 4F RTA35EU 20051114001392005111400139 2005 11 14 CALA0500397 420051109A2397 CIRCUIT CARD BOEING767 767424ER 1385270NM SEAT 1 AB BURNED A CALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2776055 29450 AN ODOR OF SMOKE WAS NOTICED IN THE CABIN AND COCKPIT WHILE EN ROUTE TO AMS. THE POWER TO ROWS 1-7 WAS SHUTOFF AND THE ODOR LESSENED. THE FLIGHT WAS CONTINUED TO AMS WHERE IT LANDED WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND THE SEAT ELECTRONICS BOX (IVASEB) AT SEAT 1AB AT FAULT. THE CIRCUIT CARD INSIDE WAS BURNED AND THE PLASTIC COVER WAS DEFORMED. THE IVASEB WAS REMOVED AND REPLACED. THE WIRING AND AREA WERE INSPECTED WITH NO OTHER DAMAGE FOUND. OPERATIONAL CHECKS WERE GOOD. THE RECIRCULATION FAN FILTERS WERE REMOVED AND REPLACED PER MM 21-25-02. 2L72 4F RTA1NM 20051114001402005111400140NM 2005 11 14 CALA0500398 120051007A53156546568148 FLOORBEAM BOEING737 7373T0 1384582NM BS 1016 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769333 23571 INSPECTION FOUND THE RT SIDE OF UPPER CHORD OF FLOORBEAM CORRODED AT STA 1016, RBL 16 TO RBL 35. THE FLOORBEAM WAS REPAIRED BY SPLICING IN A NEW SECTION OF UPPER CHORD IAW ECRA 5321-01299. 2L72 4F RTA16WE 20051114001412005111400141EA 2005 11 14 COMA0560592 120051109A2751601R930561 DETECTOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01467CA 7637 FLIGHT 5352 - FLAPS FAIL CAUTION. REPLACED THE RIGHT FLAP SKEW DETECTOR. 2L72 4F RTA21EA 20051114001422005111400142EA 2005 11 14 COMA0560584 120051102A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01910EV 7727 FLIGHT 5208 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2L72 4F RTA21EA 20051114001442005111400144NM 2005 11 14 UPS05445731 120051108A541065B903604 LINK BOEING747 747123 1384873NM NR 3 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 NR 3 NACELLE REAR ENGINE MOUNT THRUST LINK, CRACK INDICATION REVEALED AT AFT END LUG LOWER EXIT LIMIT. NR 3 ENG REAR MOUNT THRUST LINK REPLACED PER EO B747-7120-22596-A WORK CARRIED OUT ON TASK CARD APPENDIX-H. NR 3 ENG REMOVED AND INSTALLED (FOR ACCESS) AS PER UPS TASK CARD TC 5000. 2L74 4F A20WE 20051114001462005111400146NM 2005 11 14 UPS05545735 120051103A5420 WEB BOEING757 75724APF 1384969NM NR 1 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01404UP 23726 NR 1 PYLON SKIN CRACKED AT ACCESS PANEL 433AL CUTOUT NEAR 11:00 POSITION. REPAIRED CRACK ON NR 1 PYLON SKIN IAW GOODRICH ER NR 05-4594 AND IAW UPS EO B757-5430-23199-A 2L72 4F RTA2NM 20051115000012005111500001NM 2005 11 15 CALA0500395 120051023A3350 FUSE BOEING737 737824 13844BZNM CFMINTCFM56 CFM567B26US NE BATTERY PACK OPEN A CALAK NONE O OTHER ININSP/MAINT 1 SW2726226 28935 INSPECTION FOUND THE EMERGENCY LIGHT INOPERATIVE AT OVERWING ESACPE HATCH, ROWS 11-14. TROUBLESHOOTING ISW WDM 33-51-13 FOUND AN OPEN FUSE ON BATTERY PACK M1694. THE FUSE WAS REMOVED AND REPLACED IAW STANDARD WIRING PRACTICES MANUAL 20-00-00. OPS CHECK WAS GOOD. 2L72 4F4 FRTA16WE E00055EN 20051115000022005111500002NM 2005 11 15 CALA0500396 120051109A21216455072 FAN BOEING757 757324 1384930NM E/E BAY BURNED OUT A CALAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SW2774856 32815 THE LEFT RECIRCULATION FAN EICAS MESSAGE CAME ON WITH INOPERATIVE LIGHT ON LEFT RECIRCULATION FAN SWITCH DURING DESCENT INTO CLE. THERE WAS SOME SMOKE SMELL IN THE CABIN. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LEFT RECIRCULATION FAN BURNED OUT WITH THE CIRCUIT BREAKER TRIPPED. THE FAN WAS REMOVED AND REPLACED IAW MM 21-25-01. OPERATIONAL CHECKS WERE GOOD IAW MM 21-25-00. 2L72 4F RTA2NM 20051115000042005111500004NM 2005 11 15 CALA0500399 120051111A531565C339501 FLOORBEAM BOEING737 737524 1384721NM BS 986.5 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717620 27333 INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, LBL 7 TO LBL 26. THE CORRODED SECTIONS WERE TRIMMED OUT AND FILLER AND REPAIR DOUBLERS WERE INSTALLED IAW SRM 53-60-51, FIGURE 201. 2L72 4F RTA16WE 20051115000082005111500008NM 2005 11 15 CALA0500403 120051113A5313BAC1498117 STRINGER BOEING737 7373T0 1384582NM STA 344-360 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2759338 23576 INSPECTION FOUND STRINGER 25L CORRODED BETWEEN STA 344 AND 360 AT FORWARD O/B SUPPORT FOR E-2 AVIONICS RACK. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 53-00-03. 2L72 4F RTA16WE 20051115000092005111500009NM 2005 11 15 CALA0500404 120051113A5315146N51361 FLOORBEAM BOEING757 757224 1384958NM STA 1640 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713113 27555 INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT STA 1640, RBL 57. THE CORROSION WAS BLENDED OUT AND REPAIRED IAW ECRA 5321-01316. 2L72 4F RTA2NM 20051115000102005111500010NM 2005 11 15 CALA0500405 120051113A335020121 CHARGER BOEING737 737524 1384721NM ROWS 1-6 ABC INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2714668 28928 THE EMERGENCY LIGHTS AT ROWS 1-6ABC WERE FOUND INOPERATIVE. THE M1674 EMERGENCY BATTERY CHARGER WAS REMOVED AND REPLACED IAW MM 33-51-51. 2L72 4F RTA16WE 20051115000112005111500011SO 2005 11 15 C2XA05IA116 120051018A339778241 INVERTER EMB 145 EMB145EP 3260221SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714943 145040 IAH - FLIGHT 2418, DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE LOWER AFT LEFT EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT INVERTER. OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20051115000122005111500012NM 2005 11 15 NOCA2105 120051028A5210 DOOR BOEING767 767300 1385204NM L2 MALFUNCTIONED G NOCAO OTHER O OTHER TXTAXI/GRND HDL 1 EA15760NA 26257 BEFORE DEPARTURE DOOR L2 UNABLE TO CLOSE PROPERLY. CLOSED BY FLIGHT MECHANIC. NO FURTHER PROBLEMS. 2L72 4F RTA1NM 20051115000142005111500014NM 2005 11 15 QXEA200501512 120051108A3297471515 WIRE HARNESS BOMBDRDHC8 DHC8402 1390042NM ZONE 700 INOPERATIVE A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09409QX520 520 4051 BOI-ON FLIGHT 2389, AFTER DEPARTING BOI, THE GEAR WAS SELECTED UP, THE 3 YELLOW GEAR DOOR LIGHTS CAME ON AND THE 3 GREEN LIGHTS STAYED ON AND NO RED LIGHTS. AFTER ABOUT 1 MINUTE THE GEAR DID RETRACT. THE LEFT MAIN GEAR DOOR LIGHT AND NOSE GEAR DOOR LIGHT STAYED ON FOR ANOTHER 15 SECONDS. MAINTENACE REMOVED AND REPLACED NLG WOW NR 2 HARNESS. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051115000152005111500015NM 2005 11 15 QXEA200501511 120051108A293082410610007 CONTROL PANEL BOMBDRDHC8 DHC8402 1390042NM ZONE 700 INOPERATIVE A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09416QX 4083 SEA - ON FLIGHT 2376, HYDRAULIC NR 3 ISOL VALVE SWITCH DOES NOT STAY IN WHEN PRESSED. MAINTENANCE REPLACED HYDRAULIC CONTROL PANEL. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051115000172005111500017NM 2005 11 15 NOCA1405 120050924A3397 CONNECTOR BOEING757 75728A 1384976NM EMERGENCY LIGHT LOOSE G NOCAK NONE L NO TEST ININSP/MAINT 1 EA15750NA 26277 FOUND EMERGENCY PATH LIGHTING ROWS 31, 32 AND 36 INOP. SECURED CONNECTIONS AT ROWS 31, 32 AND 36 SYSTEM OPERATES NORMALLY. 2L72 4F RTA2NM 20051115000182005111500018EA 2005 11 15 QXEA200501513 220051109A7200 ENGINE BOMBDRDHC8 DHC8402 1390042NM PWC 150 PW150A EA NR 1 MALFUNCTIONED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09407QX 4049 MSO FLIGHT NR 2348 - DURING ENGINE START, FOLLOWING BRINGING PROPS OUT OF FEATHER, NR 1 ENGINE RETURNED TO FEATHER MODE WITH POWERPLANT MESSAGE AND NR 1 PEC CAUTION ILLUMINATED. MAINTENANCE INTERROGATED CDS. FOUND FAULT CODE 130. CLEARED FAULT CODE IAW Q400 FIM 61-20-03-810-815. GROUND RAN ENGINES. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E00062EN 20051115000192005111500019NM 2005 11 15 NOCA2205 120051031A3350 BULB BOEING767 767324 1385203NM EMERGENCY LIGHT INOPERATIVE G NOCAK NONE L NO TEST ININSP/MAINT 1 EA15767NA 27569 EMERGENCY AISLE LIGHTS AT SEATS 12B, 12H, 14B, 15B, 23H AND 34B HALF LIT. RELAMPED EMERGENCY AISLE LIGHTS AT SEATS 12B, 12H, 14B, 15B, 23H AND 34B OPS CHECK NORMAL. 2L72 4F RTA1NM 20051115000202005111500020NM 2005 11 15 NOCA1305 120050925A3350BPS73 BATTERY PACK BOEING767 767300 1385204NM L2 DOOR INOPERATIVE G NOCAK NONE L NO TEST ININSP/MAINT 1 EA15760NA 26257 DURING DAILY CHECK, FOUND EMERGENCY PATH LIGHTING FROM L1 TO L2 DOORS INOP. REPLACED EMERGENCY PATH LIGHTING BATTERY PACK, SYSTEM OPERATES NORMALLY. 2L72 4F RTA1NM 20051115000212005111500021NM 2005 11 15 NOCA1805 120051020A3350767 BULB BOEING757 75728A 1384976NM EMERGENCY LIGHT INOPERATIVE G NOCAK NONE L NO TEST ININSP/MAINT 1 EA15756NA 32448 DURING ROUTINE MAINTENANCE, FOUND EMERGENCY EXTERIOR LIGHT FROM L1 DOOR INOPERATIVE. REPLACED BULB, SYSTEM OPERATES NORMALLY. 2L72 4F RTA2NM 20051115000232005111500023EA 2005 11 15 COMA0560583 120051102A3241 ANTI-SKID SYS CNDAIRCL600 CL6002B19 1900309EA MLG BRAKES WARNING LIGHT A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01812CA 7381 FLIGHT 5904 - PARKING BRAKE SOV AND ANTI/SKID CAUTION. RESET SYSTEM. NO DEFECTS NOTED. 2L72 4F RTA21EA 20051115000242005111500024EA 2005 11 15 COMA0560586 120051104A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS UNRELIABLE A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01915CA251459581 7013 FLIGHT 5725 - FLAPS FAIL CAUTION. REPLACED THE LT BPSU. 2L72 4F RTA21EA 20051115000252005111500025EA 2005 11 15 COMA0560590 120051108A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01975CA 7150 FLIGHT 5384 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2L72 4F RTA21EA 20051115000262005111500026EA 2005 11 15 COMA0560591 120051109A2440820464 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA ADG MALFUNCTIONED A COMAA UNSCHED LANDING O OTHER CLCLIMB 1 SO01971CA23469 7145 FLIGHT 5822 - ADG DEPLOYED AFTER TAKEOFF. RESTOWED ADG AND REPLACED ADG CONTROLLER. 2L72 4F RTA21EA 20051115000282005111500028NM 2005 11 15 QXEA200501514 120051027A5330 SKIN BOMBDRDHC8 DHC8402 1390042NM BS 116 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX: DENT IN FUSELAGE OUTER SKIN LOWER LEFT SIDE .79 INCH FWD OF STA 116.00 AND .85 INCH ABOVE CENTER LINE OF STR 29L. DENT IS APPROX 1.7 INCH WIDE BY .90 HIGH BY .015 INCH DEEP. MAINTENANCE REPAIRED IAW NDTM PART 6 51-00-02 AND QX EA 6-53-359 AND RD 8/4-53-666. 2H72 4T RTA13NM 20051115000292005111500029EA 2005 11 15 SWIA200515824 120050612A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 621 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07967SW 7872 FOUND FLOORBEAM ANGLE AT FS 621.00 RT IS CRACKED, ITEM FOUND AT C CHECK INSPECTION. REPAIRED CRACKED FLOOR SUPPORT ANGLE IAW CRJ REO 601R-53-61-117 REV "B". 2L72 4F RTA21EA 20051115000312005111500031NM 2005 11 15 UPS05545736 120051015A5347BAC15202472 SEAT TRACK BOEING757 75724APF 1384969NM BS 440 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01404UP 23726 FOUND MAIN DECK CARGO SEAT TRACK O/B FLANGE HAS CORROSION BS 440, LBL26, WL208. REPAIRED PER SRM 53-00-52-2R AND GOODRICH ER NR 05-4696. 2L72 4F RTA2NM 20051115000342005111500034NM 2005 11 15 UPS05545739 120051015A5347BAC15202472 SEAT TRACK BOEING757 75724APF 1384969NM BS 1318 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01404UP 23726 FOUND BS 1318, WL 208, RBL 45, SEAT TRACK UPPER SURFACE ON INBOARD FLANGE HAS 1EA AREA OF CORROSION. REPAIRED PER SRM 53-00-52-2R AND GOODRICH ER#05-4696. 2L72 4F RTA2NM 20051115000362005111500036NM 2005 11 15 UPS05545741 120051108A5315 FLOORBEAM BOEING757 75724APF 1384969NM BS 1101 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01404UP 23726 FOUND UPPER LOBE FLOORBEAM UPPER CHORD CORROSION, 2 NUTPLATE HOLES STA 1101 LBL33.5 AND LBL40.5. REPAIRED PER EO 05-4661. 2L72 4F RTA2NM 20051115000372005111500037NM 2005 11 15 UPS05545742 120051031A5320 FLOOR SUPPORT BOEING757 75724APF 1384969NM BS 1040-1072 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01404UP 23726 FOUND UPPER LOBE LONGITUDINAL BEAM I/B FLANGE CORROSION AT NUT PLATE HOLES STA 1040-STA 1072 LBL 44, UPPER AND LOWER SURFACES. REMOVED AND REPLACED PER SRM 51-40-02. 2L72 4F RTA2NM 20051115000382005111500038NM 2005 11 15 UPS05545743 120051015A5347144N50245 SEAT TRACK BOEING757 75724APF 1384969NM BS 1084-1153 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01404UP 23726 FOUND UPPER LOBE SEAT TRACK IB FLANGE CORROSION, AT NUT PLATE HOLES STA 1084 TO STA 1153 LBL44. REMOVED AND REPLACED SEAT TRACK WITH NEW PER SRM 51-40-02. 2L72 4F RTA2NM 20051115000412005111500041WP 2005 11 15 AALA20050734 120051110A25302510000405 OVEN DOUG DC9 DC982 3022082WP CABIN FIRE A AALAA UNSCHED LANDING A FLAME/FIRE CLCLIMB 1 SW217535A 49989 FIRE INSIDE FIRST CLASS OVEN. USED TWO FIRE EXTINGUISHERS AND PULLED CIRCUIT BREAKERS. AIR INTERRUPTED TO ATL. REPLACED OVEN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051115000422005111500042NM 2005 11 15 AALA20050733 120051110A253046700017 COFFEEMAKER BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW2139364 24045 NUMBER TWO COFFEE MAKER SPARKS. ITEM DEFERRED AS PDL 2599J AUGH 119168CC. PULLED CIRCUIT BREAKER AND COLLARED. 2L72 4F RTA1NM 20051115000432005111500043WP 2005 11 15 AALA20050735 120051111A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21219AA 49171 LGA - FOUND CEILING EMERGENCY EXIT LIGHTS ABOVE AFT STAIRS INOPERATIVE. FOUND AND REPAIRED BROKEN WIRE AT S3156. REPLACED BATTERY PACK AS PRECAUTION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051115000442005111500044NM 2005 11 15 AALA20050736 120051031A3350D71702100 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21916AN 29517 TUL - EMERGENCY LIGHT BATTERY PACK IN MID CABIN INOPERATIVE. REPLACED BATTERY PACK IN MID COACH SECTION AT STATION FOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20051115000462005111500046NM 2005 11 15 AALA20050729 120051027A3350 WIRE HARNESS BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21386AA 27060 DFW - EMERGENCY LIGHT AT ROW 39H INOPERATIVE. FOUND LOOSE CONNECTION. RESECURED LOOSE CONNECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20051115000492005111500049WP 2005 11 15 AALA20050732 120051109A3397 WIRE HARNESS DOUG DC9 DC982 3022082WP EMERGENCY LIGHT BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW21286AA 49298 LGA - FOUND EMERGENCY LIGHT ACROSS FROM FORWARD LAVATORY INOPERATIVE. REPAIRED BROKEN WIRE AT LIGHT ASSEMBLY FOR EMERGENCY LIGHT ACROSS FROM FORWARD LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051115000532005111500053EA 2005 11 15 SWIA200515827 120050626A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07446SW 7666 FOUND FS 280 RT FLOORBEAM INBD AND OB ANGLES RBL 9.0 CRACKED, ITEM FOUND AT C CHECK INSPECTION. REPLACED ANGLES IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, 51-21-11. 2L72 4F RTA21EA 20051115000542005111500054EA 2005 11 15 SWIA200515828 120050626A5313 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA BS 625 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07446SW 7666 FOUND FS 625 LT INTERCOSTAL ANGLE CRACKED STR 14L, ITEM FOUND AT C CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06, AND 51-42-21. 2L72 4F RTA21EA 20051115000552005111500055EA 2005 11 15 SWIA200515829 120050626A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA CRACKED CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07446SW 7666 CARGO COMPARTMENT FS 621 LHS FLOOR SUPPORT ANGLE CRACKED, ITEM FOUND AT C CHECK INSPECTION. REPAIRED ANGLE IAW CRJ REO 601R53-61-117 REV "C". 2L72 4F RTA21EA 20051115000562005111500056EA 2005 11 15 SWIA200515830 120051108A2750860D10018 FCU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 NM07926SW9405 9405 7687 ON APPROACH; FLAP LEVER WAS POSITION TO 8 DEG AND RECIEVED A FLAPS FAIL CAUTION MESSAGE. REPLACED FECU IAW CRJ 200 MM 27-51-05 AND REPLACED SKEW DETECTOR UNIT IAW CRJ 200 MM 27-51-15. OPERATIONAL CHECK GOOD, PN 601R59014-1 SN 2 OFF A711. 2L72 4F RTA21EA 20051115000582005111500058EA 2005 11 15 SWIA200515832 120051106A2751855D1009 SENSOR CNDAIRCL600 CL6002B19 1900309EA FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07440SW1076610766 7589 WHEN SELECTED FLAPS FROM 0 DEGREES TO 8 DEGREES, RECEIVED "FLAPS FAIL" CAUTION MESSAGE. REPLACED SAME BRAKE POSITION SENSOR. OPERATIONAL CHECK GOOD IAW MM27-51-00. 2L72 4F RTA21EA 20051115000602005111500060NM 2005 11 15 UPS05545745 120051108A5320 WEB BOEING757 75724APF 1384969NM BS 324-334 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01404UP 23726 FOUND UPPER LOBE LAV FLOOR WEB CORROSION STA 324- STA 334 RBL45-RBL 59, WL208. REPAIRED PER ER 05-4675. 2L72 4F RTA2NM 20051115000612005111500061WP 2005 11 15 UPS05845733 120051005A5312 BULKHEAD DOUG DC8 DC873F 302199FWP BS 1766 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 FOUND CRACK ON AFT PRESS BULKHEAD LBL 26, 65 INCHES FROM FLOOR CUT OUT DAMAGED AREA AT FS 1766 LBL26 IAW SRM 53-2-5 FIG 14, NDT AREA IAW SPM 06-10-01-001, NO CRACKS NOTED AT CUT OUT AREA. FABRICATED -15, -17 DOUBLERS AND -9, -11, -13 AND -19 FILLERS IAW SRM 53-2-5-1A FIG 1A AND INSTALLED REPAIR PARTS IAW SRM 53-2-5 FIG 1A PG 3. 2L74 4F RT4A25 20051115000632005111500063WP 2005 11 15 UPS05845751 120051017A53403779659U501 FITTING DOUG DC8 DC873F 302199FWP BS 860 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 FOUND MAIN CARGO COMPARTMENT L2R FITTING CRACKED STA 860. REMOVED AND REPLACED FITTING IAW SRM 51-1-21,51-3-0 AND 51-1-20D. 2L74 4F RT4A25 20051115000712005111500071SO 2005 11 15 RAIA00511009 120051107A3350RPS1B POWER SUPPLY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03818HK 145059 MX - STL - FOUND COCKPIT EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED EMERGENCY BATTERY POWER SUPPLY. 2L72 4T RTT00011AT 20051115000722005111500072SO 2005 11 15 RAIA00511010 120051107A3397 CONNECTOR EMB 145 EMB145EP 3260221SO BATTERY PACK LOOSE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03826HK 145016 MX - STL - FOUND AFT EMERGENCY LIGHTS INOP. MAINTENANCE TIGHTENED CONNECTOR TO BATTERY PACK. 2L72 4F RTT00011AT 20051115000732005111500073EU 2005 11 15 RAIA00511011 120051108A2497 WIRE JETAIRJETSTMJETSTM4101 1500501EU STARTER GEN BROKEN A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03562HK 41078 FLT - 3611 - BWI - FOUND LEFT GENERATOR FAILED. MAINTENANCE RE-SECURED BROKEN WIRE AT NR 1 STARTER GENERATOR. 2L72 4T RTA41NM 20051115000742005111500074EU 2005 11 15 RAIA00511014 120051110A2997 PIN JETAIRJETSTMJETSTM4101 1500501EU HYD CONTROL UNITDAMAGED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03561HK 41077 FLT - 5443 - STL - FLAPS WOULD NOT COME UP AFTER TAKEOFF. MAINTENANCE RESET FLAP BYPASS PIN ON HYDRAULIC CONTROL UNIT. 2L72 4T RTA41NM 20051115000752005111500075SO 2005 11 15 RAIA00511013 120051109A3350 BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03818HK 145059 MX - STL - FOUND EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES. 2L72 4T RTT00011AT 20051115000762005111500076NE 2005 11 15 RAIA00511012 220051109A7297 TERMINAL JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114GR 01514NE EGT WIRE HARNESSBROKEN A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03562HK 41078 75103 FLT - 3601 - RIC - FOUND LEFT IEC FAIL. MAINTENANCE REMOVED AND REPLACED EGT HARNESS TERMINAL END. 2L72 4T4 TRTA41NM E18NE 20051115000772005111500077 2005 11 15 RAIA00511015 420051110A34257003360943 COMPUTER JETAIRJETSTMJETSTM4101 1500501EU AHRS INOPERATIVE A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03566HK18830770 41084 FLT 5429 - STL - NR 1 AHRS FAILED. MAINTENANCE REMOVED AND REPLACED AHRS COMPUTER. 2L72 4T RTA41NM 20051115000792005111500079NM 2005 11 15 NOCA2305 120051102A3397 CONNECTOR BOEING767 767300 1385204NM EMERGENCY LIGHT INOPERATIVE G NOCAK NONE L NO TEST ININSP/MAINT 1 EA15768NA 29898 EMERGENCY FLOOR PATH LIGHTING INOPERATIVE IN FRONT OF 2L LAVATORY. RESEATED CONNECTOR AT 2L LAVATORY OPS CHECK NORMAL. EMERGENCY EXIT MARKER AT 2L DOOR INOPERATIVE. REPLACED CONTACT AND QUICK DISCONNECT AT 2L DOOR EMERGENCY EXIT MARKER OPS CHECKED NORMAL. 2L72 4F RTA1NM 20051115000802005111500080NM 2005 11 15 AWXA200501374 120051025A5315141N5111 FLOORBEAM BOEING757 7572S7 1384962NM BS 345 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28904AW 23566 GYR - DURING C10 CHECK, DISCOVERED FLOORBEAM AT BS 345, WL 208.10 AND BL 60R CORRODED. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. CUT OUT AND REMOVED FLOORBEAM AT STA 345, WL 208.10 AND BL 60R IAW BOEING 757-200 SRM 53-00-51. FABRICATED CHORD, ANGLES AND STRAPS IAW BOEING 757-200 SRM 53-00-51 FIG 201. INSTALLED FABRICATED REPAIR PARTS AT BS 345, WL 208.1 AND BL 60R IAW BOEING 757-200 SRM 53-00-51 FIG 201. 2L72 4F RTA2NM 20051115000832005111500083NM 2005 11 15 NOCA0705 120050627A2997 CONNECTOR BOEING767 767300 1385204NM AIR DRIVEN PUMP LOOSE G NOCAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA15767NA 27569 JFK - UPON GEAR RETRACTION CENTER HYDRAULIC PRESSURE LIGHTS AND EICAS MESSAGES ILLUMINATED. CREW DECLARED AND EMERGENCY AND REQUESTED TO LAND. AIRCRAFT RETURNED TO JFK WITH AN UNEVENTFUL LANDING. CAUSE OF PROBLEM WAS DETERMINED TO BE A LOOSE CONNECTOR ON THE AIR DRIVEN PUMP (ADP). THE CONNECTOR WAS SECURED WITH NO OTHER ITEMS. 2L72 4F RTA1NM 20051115000852005111500085NM 2005 11 15 NOCA0205 120050313A521080330035 RESERVOIR BOEING757 75728A 1384976NM L1 DOOR ASSIST DISCHARGED G NOCAK NONE O OTHER ININSP/MAINT 1 EA15752NA 28174 FOUND L1 DOOR ASSIST BOTTLE PRESSURE LOW. REMOVED AND REPLACED L1 DOOR ASSIST BOTTLE IN ACCORDANCE WITH AIRCRAFT MAINTENANCE MANUAL. 2L72 4F RTA2NM 20051115000892005111500089EA 2005 11 15 COMA0560594 120051110A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS WARNING LIGHT A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01967CA 7134 FLIGHT 5116 - DURING APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE AT 28 DEGREES. FLIGHT LANDED SAFELY. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE FIRST EVENT MAINTENANCE ACTION PARAGRAPH (B) 1, 2, 3 (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2L72 4F RTA21EA 20051115000912005111500091NM 2005 11 15 NOCA0605 120050526A490038002981 APU BOEING757 75728A 1384976NM APU BAY SHUTDOWN G NOCAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 EA15750NA 26277 APU SHUTDOWN WHEN LEFT PACK WAS TURNED OFF PERFORMED BITE PER FIM 49-11-00. RESET APU STARTED AGAIN OPS CHECKED NORMAL. 2L72 4F RTA2NM 20051115000952005111500095SO 2005 11 15 C2XA05BT075 120051029A33503025103 LIGHT EMB 145 EMB145LR 3260212SO RT OVERWING FAULTY A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713908 145465 BTV - DURING SERVICE AND ROUTINE CHECK, MAINTENANCE FOUND THE RIGHT OVERWING EMERGENCY LIGHT TO BE NOT WORKING. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY IAW EMB145 AMM #33-50-07, OPS CHECKED GOOD. 2L72 4T RTT00011AT 20051115001022005111500102GL 2005 11 15 DXTA200501057 220051103A7310 LINE CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL FUEL SYS UNDERTORQUED E DXTAD RETURN TO BLOCK RW PARTIAL RPM/PWR LOSS INADEQUATE Q C TXTAXI/GRND HDL 1 GL07918QS 7500223 DURING THE T/R CHECK, WHILE TAXIING THE RIGHT ENGINE FAILED. CHECKED CABLE FOR SHIM, NONE FOUND. CHECKED ALL BLEED CONTROL LINES FOR PROPER TORQUE. REPLACED A+B FADECS IAW RR AE3007C M/M 76-12-00. REPLACED FPMU IAW AE3007C M/M 73-21-00. FOUND TWO FUEL NOZZLE SUPPLY LINES LEAKING, RETORQUED AND LEAK CHECK GOOD. 2L72 4J4 FRTT00007WITE6CH 20051115001032005111500103NE 2005 11 15 DXTA200501064 220051106A7320 WARNING LIGHT CESSNA560 560XL 2076702CE PWA 545 PW545A NE LT EEC ILLUMINATED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07604QS 5605204 DURING TAKEOFF ROLL, LEFT EEC LIGHT ILLUMINATED PRIOR TO 70 KTS. DEFERRED IAW NJA CE560XL MEL. MEL 73-3. ITEM IS UNDER INVESTIGATION. 2L72 4F4 FRTA22CE E00059EN 20051115001042005111500104CE 2005 11 15 DXTA200501051 120051013A2130BAS169A4400035 DUCT RAYTHNDH125 HAWKER800XP 7150012CE CABIN PRESSURE BLEW OUT E DXTAB EMER. DESCENT S AFFECT SYSTEMS CRCRUISE 1 GL07816QS 258416 WHILE CRUISING AT FL360, HEARD A LOUD POP FROM REAR OF AIRCRAFT. CABIN CLIMB INDICATOR WAS PEGGED AT MAXIMUM READING. PRESSURIZATION WAS LOST. INSPECTED J-DUCT DISCOVERED WATER SEPARATOR SLEEVE BUCK BLOWN, REMOVED J-DUCT AND INSPECTED SLEEVE, FOUND SLEEVE CUT, REPLACED SLEEVE AND INSTALLED J-DUCT. LEAK CHECK J-DUCT AND WATER SEPARATOR CHECK GOOD, ALL WORK DONE IAW HAEKER 800XP AMM 21-10-95. 2L72 4F RTA3EU 20051115001052005111500105 2005 11 15 DXTA200501063 420051105A34601835501010101 MODULE CESSNA500 560CESSNA 2076750CE BURNED E DXTAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL07372QS2553 5600372 POWERED UP AIRCRAFT FOR PREFLIGHT. FMS SCREEN STAYS BLACK AND SMOKE WAS COMING OUT FROM UNDER FMS. FOUND FMS GNS-XL. CONTACTED EMPIRE. REMOVED AND REPLACED GNS-XL IAW CE560 MM 34-61-03. OPS CHECK IAW GNS-XL FLIGHT MANAGEMENT SYSTEM OPERATOR'S MANUAL. 2L72 4F RTA22CE 20051109002822005110900282NM 2005 11 9 05FDEA03659 120051107A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 CRACK INDICATION AT END OF STRINGER -11 (UPPER STRINGER) WAS FOUND DURING HFEC INSPECTION AT RIGHT WING TANK. REPAIRED AS PER SRM 57-20-00. 2L73 4F RTA22WE 20051109002842005110900284WP 2005 11 9 05FDEA03681 120051107A5510 DOUBLER DOUG DC10 DC1010 3022110WP HORIZONTAL STAB UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 FOUND EXTERNAL DOUBLER REPAIR AT LEFT HAND HORIZONTAL STABILIZER ON SKIN, TRAILING EDGE OF STAB BETWEEN STA XE48 AND XE60. PERFORMED A GVI OF EXISTING DOUBLER IAW EO8-5100-7-5001 CRITERIA REQUEST FOUND DOUBLER IN COMPLIANCE WITH DOUGLAS AIRCRAFT COMPANY SERVICE BULLETIN 55-16 FIG 10. 2L73 4F A22WE 20051109002862005110900286WP 2005 11 9 05FDEA03673 120051107A5510 DOUBLER DOUG DC10 DC1010 3022110WP HORIZONTAL STAB UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 FOUND EXTERNAL DOUBLER REPAIR AT RT HORIZONTAL STABILIZER L/E ON FRONT SPAR INBOARD SECTION OF STAB STA XE35. PERFORMED A GVI OF EXISTING DOUBLER IAW EO8-5100-7-5001 CRITERIA REQUEST FOUND DOUBLER IN COMPLIANCE WITH SRM 55-20-00 FIG 9 SHT 1 VOL 1. 2L73 4F A22WE 20051109002882005110900288WP 2005 11 9 05FDEA03675 120051107A5510 DOUBLER DOUG DC10 DC1010 3022110WP HORIZONTAL STAB UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 LOWER SURFACE OF HORIZONTAL STABILIZER CONSTANT SECTION AT FRONT SPAR LEFT SIDE BY REF PLANE YCH 137.6092, FOUND AN EXTERNAL DOUBLER REPAIR. PERFORMED A GVI OF EXISTING DOUBLER IAW EO8-5100-7-5001 CRITERIA REQUEST FOUND DOUBLER IN COMPLIANCE WITH SERVICE BULLETIN 55-16 FIG 13. 2L73 4F A22WE 20051109002902005110900290WP 2005 11 9 05FDEA03677 120051107A5510 DOUBLER DOUG DC10 DC1010 3022110WP HORIZONTAL STAB UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 RT HORIZONTAL STABILIZER UPPER SURFACE FOUND EXTERNAL DOUBLER REPAIR ON SKIN BETWEEN STA XE58 AND XE70. PERFORMED A GVI OF EXISTING DOUBLER IAW EO8-5100-7-5001 CRITERIA REQUEST FOUND DOUBLER IN COMPLIANCE WITH SERVICE BULLETIN 55-16 FIG 18. 2L73 4F A22WE 20051109002922005110900292WP 2005 11 9 05FDEA03679 120051107A5510 DOUBLER DOUG DC10 DC1010 3022110WP HORIZONTAL STAB UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 LEFT L/E AT FRONT SPAR INBOARD AREA OF HORIZONTAL STABILIZER ON SKIN FOUND AN EXTERNAL DOUBLER REPAIR AT STAB STA XE35. PERFORMED A GVI OF EXISTING REPAIR IAW SRM 55-20-00 PG 45 FIG 9 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO8-5100-7-5001. 2L73 4F A22WE 20051110000112005111000011EA 2005 11 10 SWIA200515807 120051103A2750 TRANSMITTER CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07954SW 7815 FLAPS DEGRADED MSGS. REPLACED FLAP POSITION TRANSMITTER. OPERATIONAL CHECK GOOD IAW 27-50-00. 2L72 4F RTA21EA 20051110000182005111000018EA 2005 11 10 SWIA200515814 120051102A27604916406 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07437SW4760 4760 7564 UNCOMMANDED INBOARD GROUND SPOILERS DEPLYED DURING TAXI. REPLACED NR 2 SECU IAW MM 27-61-04, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051110000292005111000029NM 2005 11 10 EIA2005198 120051009A5320 STIFFENER BOEING747 747212B 1384886NM BS 1830 CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 BS 1830 STR 25R FOUND STIFFENER CRACKED. REPLACED DEFECTIVE STIFFENER PER SRM 51-10-01, PG 9. 2L74 4F A20WE 20051110000512005111000051WP 2005 11 10 ABXA050269 120051023A531039536261 STOP FITTING DOUG DC9 DC941 302207NWP MLG DOOR FRAME CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23952AX 47615 AFT P DOME DOOR JAMB UPPER RIGHT DOOR STOP FITTING CRACKED. REMOVED AND REPLACED AFT P DOME DOOR JAMB UPPER RIGHT DOOR STOP FITTING IAW DC-9 SRM 51-30-1, 51-30-2 AND 51-30-5. 2L72 4F A6WE 20051110000592005111000059SO 2005 11 10 146311072005 120051107A56101159SCB51023 WINDSHIELD GULSTMG1159 GIV 3980115SO RROYCETAY TAY6118 EU COCKPIT CRACKED E N93AO OTHER O OTHER NRNOT REPORTED 1 SO13465QS3216 1463 WINDSHIELD CRACKED. 2L72 4F4 FRTA12EA E25NE 20051110000942005111000094WP 2005 11 10 IXXA05SMN260S 120051013A5330 DOUBLER DOUG DC8 DC871F 302199DWP BS 880.000 CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING ROUTINE C CHECK INSPECTION, MAIN CARGO CMPT MLG W/W PRESSURE PANEL DOUBLER CORRODED, STA 880.000 RBL 2’. REMOVED CORROSION FROM DOUBLER IAW DC8 SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0 PG 2P. REMOVED CORRODED DOUBLER IAW DC8 SRM 51-1-21. FABRICATED NEW DOUBLER (AL7075T6 0.050”) IAW DC8 SRM 53-2-0 PG 1. CLEANED, TREATED AND PRIMED AREA + DOUBLER IAW DC8 SRM 51-1-8B. INSTALLED DOUBLER IAW DC8 SRM 51-1-21. 2L74 4F RT4A25 20051110000952005111000095WP 2005 11 10 IXXA05SMN258S 120051013A5330 FASTENER DOUG DC8 DC871F 302199DWP BS 180.000 IMPROPER B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING C CHECK INSPECT, EXTERNAL FS REPAIR FASTENERS IMPROPER AND RIVETS EXCEED ALLOWABLE LIMITS, STA 180.000 L-19R. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-1 FIG 7, EO SEMAN 20051309 DATED 09-29-05. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D. REMOVED DAMAGED SECTION IAW DC8 SRM 53-2-1 FIG 7 (SHEET 1, 3). NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D REPAIR DOUBLER (AL7075T6 0.071) + (04EA) INTERNAL FINGER DOUBLERS (AL7075T6 0.040”) IAW DC8 SRM 53-2-1 FIG 7 (SHEET 1, 3), DC8 SRM 53-4-1 FIG 6 ITEM “A”, DC8 SRM 51-9-0 FIG 68A, DC8 SRM 51-1-4 PG 1 (FORMING). CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS IAW DC8 SRM 51-1-82L74 4F RT4A25 20051110001022005111000102WP 2005 11 10 IXXA05SMN244S 120051013A5753 VANE DOUG DC8 DC871F 302199DWP TE FLAP DAMAGED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING C CHECK INSPECT, RT WING INNER L/E SLOT VANE HAS ELONGATED HOLES AT STA XOLDO 67.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05463. REMOVED NON STANDARD REPAIR IAW DC8 SRM 51-1-21, DC8 SRM 51-3-0. NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D REPAIR DOUBLER, INTERNAL DOUBLER AND FILLER IAW SEMAN DWG # ED-4082. CLEANED, TREATED, PRIMED AREA, FILLER, INTERNAL DOUBLER, INNER SIDE OF EXTERNAL REPAIR DOUBLER IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW SEMAN DWG # ED-4082, DC8 SRM 51-1-21, DC8 SRM 51-3-0, DC8 SRM 51-1-20D, DC8 SRM 51-3-1. 2L74 4F RT4A25 20051114000062005111400006NM 2005 11 14 05FDEA03696 120051107A5313 STRINGER BOEING727 727200 138407ENM BS 643-674 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 EXISTING STRINGER REPAIR IN FWD CARGO BAY AT BS 643-674 S28R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIRED STRINGER AT BS 643-674, STR 28R PER SRM 53-10-3. 2L73 4F RTA3WE 20051114000102005111400010NM 2005 11 14 05FDEA03695 120051107A5330 REPAIR BOEING727 727225 1384077NM BS 1120-1133 IMPROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 FOUND EXISTING EXTERNAL REPAIR ON FUSELAGE BS 1120-1133 STR 18-20R. REPAIR REQURIES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPLACED REPAIR AT BS 1120-1133 STR 18R-20R PER SRM 53-30-3 FIG 3. 2L73 4F A3WE 20051114000122005111400012NM 2005 11 14 SWAA053549 120051109A3350BR2013 LIGHT BOEING737 7375H4 138449DNM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29527SW 26569 EEPLS STRIP LOOSE BETWEEN ROW 6 TO ROW 7. SECURED STRIP PER MM. 2L72 4F RTA16WE 20051114000142005111400014NM 2005 11 14 SWAA053551 120051109A3297FCA41063 RELAY BOEING737 7373Y0 1384671NM NLG WW FAULTY A SWAAO OTHER N FALSE WARNING APAPPROACH 1 SW29664WN 23495 NLG RED LIGHT ILLUMINATED WITH GEAR HANDLE IN DOWN POSITION. RECYCLED GEAR HANDLE, RED LIGHT EXTINGUISHED. REMOVED AND REPLACED R375 NLG LATCHING RELAY PER MM. 2L72 4F RTA16WE 20051114000152005111400015WP 2005 11 14 05FDEA03708 120051108A5330 SKIN DOUG DC10 DC1010 3022110WP BS 1601-1621 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 FOUND MAIN CABIN BETWEEN FUSELAGE STA 1601 AND 1621, STRINGERS 8 AND 9 RT SIDE FOUND A FLUSH REPAIR. PERFORMED A GVI OF EXISTING REPAIR IAW SRM 53-20-00 FIG 13 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001. 2L73 4F A22WE 20051114000192005111400019EU 2005 11 14 05FDEA03713 120051108A5347 SEAT TRACK AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 MAIN DECK RIGHT SIDE FRAME 16 TO 19 SEAT TRACK 3R HAS SEVERAL AREAS OF EXFOLIATION REF N00663. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-21. 2L72 4F RTA35EU 20051114000212005111400021NM 2005 11 14 AWXA200501346 120051011A5340693535214 CLIP BOEING737 7373G7 1384595NM BS 578 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 DURING C16 CHECK DISCOVERED CLIP CRACKED, .25 INCHES, IN CABIN INTERIOR AT BS 578 AND STR 8L. MAINTENANCE REMOVED CLIP AT BS 578 AND STR 8L IAW BOEING 737-300 SRM 51-40-02-0G FIG 8. RECEIVED NEW CLIP AND INSTALLED AT BS 578 AND STR 8L IAW BOEING 737-300 SRM 51-40-02-0G FIG 3 AND 4. 2L72 4F RTA16WE 20051114000232005111400023NM 2005 11 14 AWXA200501348 120051011A534066235744 CLIP BOEING737 7373G7 1384595NM BS 706 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 DURING C16 CHECK DISCOVERED STRINGER CLIP CRACKED, .5 INCHES, AT BS 706 AND STR 11R. MAINTENANCE REMOVED CLIP AT BS 706 AND STR 11R IAW BOEING 737-300 SRM 51-40-02-0G FIG 8. RECEIVED NEW CLIP AND INSTALLED AT BS 706 AND STR 11R IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 3 AND 8, SRM 51-40-05-0G FIGURES 2 AND 3. 2L72 4F RTA16WE 20051114000252005111400025NM 2005 11 14 AWXA200501350 120051011A534065917001156 INTERCOSTAL BOEING737 7373G7 1384595NM BS 616 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 DURING C16 CHECK DISCOVERED INTERCOSTAL CRACKED, 1.1 INCHES, AT BS 616 AND STR 15R. MAINTENANCE REMOVED INTERCOSTAL AT BS 616 AND STR 15R IAW BOEING 737-300 SRM 51-40-2-0G FIG 8. RECEIVED NEW INTERCOSTAL AND INSTALLED AT BS 616 AND STR 15R IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 3, 8 AND 12. 2L72 4F RTA16WE 20051114000272005111400027NM 2005 11 14 AWXA200501352 120051013A5311651630159 FRAME BOEING737 7373G7 1384595NM BS 188 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 DURING C16 CHECK DISCOVERED FRAME 188 CHORD CRACKED, .875 INCHES, AT BS 188, WL 207 AND BL 31R. MAINTENANCE CUT OUT AND REMOVED DAMAGED SECTION OF OUTBOARD CHORD FLANGE IAW BOEING 737-300 SRM 53-00-07-2R11 FIG 201. FABRICATED FILLERS, TAPERED FILLER, AND REPAIR ANGLE IAW BOEING 737-300 SRM 53-00-07-2R11 FIG 201. INSTALLED FABRICATED REPAIR PARTS AT BS 188, WL 207 AND BL 31R IAW BOEING 737-300 SRM 53-00-07-2R11 FIG 201. 2L72 4F RTA16WE 20051114000292005111400029NM 2005 11 14 AWXA200501354 120051009A5320651758243 BEAM BOEING737 7373S3 1384711NM BS 178 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 DURING C18 CHECK DISCOVERED VERTICAL BEAM WEB CRACKED, 1.3 INCHES, AT BS 178, WL 229 AND BL 121R. MAINTENANCE REMOVED DAMAGED PART OF WEB IAW BOEING 737-300 SRM 53-10-08-2R FIG 201. FABRICATED REPAIR WEB AND TAPERED SHIMS IAW BOEING 737-300 SRM 53-10-08-2R FIG 201. INSTALLED FABRICATED REPAIR PARTS AT BS 178, WL 229 AND BL 121R IAW BOEING 773-300 SRM 53-10-08-2R FIG 201. 2L72 4F RTA16WE 20051114000312005111400031NM 2005 11 14 AWXA200501356 120051009A53206545834260 STIFFENER BOEING737 7373S3 1384711NM BS 324 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 DURING C18 CHECK DISCOVERED CORROSION ON THE FLOOR SUPPORT STIFFENER AT BS 324, WL 208 AND BL 11L. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-10-51-1A1 FIG 101. MAINTENANCE REPLACED STIFFENER WITH NEW PART AT BS 324, WL 208 AND BL 11L IAW BOEING 737-300 SRM 51-40-05-0G FIG 2. 2L72 4F RTA16WE 20051114000342005111400034NM 2005 11 14 05FDEA03741 120051109A5330 SKIN BOEING727 7272S2F 1384O81NM BS 1105 UNDAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25213FE 22935 FOUND REPAIR AFT, CARGO COMPARTMENT STA 1105, RBL 5. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT STA 1105, RBL 5 WAS DETERMINED TO BE IAW SRM 53-10-5 FIG 4 BASED ON AN EXTERNAL VISUAL EVALUATION WITH REPAIR INSTALLED. 2L73 4F A3WE 20051114000362005111400036NM 2005 11 14 05FDEA03744 120051109A5313 STRINGER BOEING727 7272S2F 1384O81NM BS 1030 UNDAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25213FE 22935 FOUND REPAIR AT STA 1030, RT SIDE OF FUSELAGE AT CUSP. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT FS STA 1030 RT S 17R WAS DETERMINED TO BE IAW SRM 53-30-3 BASED ON AN EXTERNAL VISUAL EVALUATION WITH REPAIR INSTALLED. 2L73 4F A3WE 20051114000382005111400038NM 2005 11 14 05FDEA03746 120051109A5310 REPAIR BOEING727 7272S2F 1384O81NM BS 1010 UNDAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25213FE 22935 FOUND REPAIR AFT CARGO COMPARTMENT STA 1010 RBL 8, REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT STA 1010, RBL 8 WAS DETERMINED TO BE IAW SRM 51-40-4-FIG 1, BASED ON EXTERNAL VISUAL EVALUATION WITH REPAIR INSTALLED. 2L73 4F A3WE 20051114000402005111400040NM 2005 11 14 05FDEA03748 120051110A5311 FRAME DOUG MD11 MD11 3023602NM BS 1256 CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25576FE 48501 DURING PASSENGER TO FREIGHT CONVERSION: FOUND CRACK 1.2" LONG ON FRAME STA 1256 LT SIDE BETWEEN L11 TO L12. TRIMOUT TIME CRACK WITH 0.5" RADIUS AND 2 REMAINING FASTENERS. PERFORMED INSPECTION FOR CRACK, INSTALLED FILLER MT 7075T6 , INSTALLED REPAIR STRAP MAT 7075T6 WITW THK .126" USING FASTENER HLT436-6. 2L73 4F RTA22WE 20051114000422005111400042NM 2005 11 14 AWXA200501359 120051009A532065163312 ANGLE BOEING737 7373S3 1384711NM BS 294 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 DURING C18 CHECK DISCOVERED ANGLE CRACKED, .4 INCHES, AT FORWARD SIDE OF FRAME 294.5 AT STR 13L. MAINTENANCE REMOVED AND REPLACED WITH NEW ANGLE AT FORWARD SIDE OF FRAME 294.5 IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5310-05303-SS2. 2L72 4F RTA16WE 20051114000442005111400044NM 2005 11 14 05FDEA03698 120051107A5754 DOUBLER DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 RIGHT FIXED LEADING EDGE INTERIOR BEADED DOUBLER FOUND CRACKED AT XORS663. REPAIRED AS PER FEDEX EA 1-5730-90044 2L73 4F RTA22WE 20051114000462005111400046WP 2005 11 14 05FDEA03700 120051108A5347 REPAIR DOUG DC10 DC1010 3022110WP BS 839 UNDAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 FOUND SEAT TRACK SPLICE REPAIR AT STATION 839 X47.500 MAIN CABIN. PERFORMED A GVI OF EXISTING SPLICE IAW EO 8-5100-7-5001 CRITERIA, FOUND SPLICE IN COMPLIANCE WITH SRM 53-70-00 PAGE 3 FIG 1. 2L73 4F A22WE 20051114000482005111400048WP 2005 11 14 05FDEA03702 120051108A5330 REPAIR DOUG DC10 DC1010 3022110WP BS 1997-2013 UNDAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 FOUND EXTERNAL DOUBLER REPAIR BETWEEN STA 1997 AND 2013 LONGERONS 45 AND 41 LT SIDE AT THE AFT PRESSURE BULKHEAD FRAME AREA. PERFORMED A GVI OF EXISTING REPAIR IAW EO 8-5100-7-5001 CRITERIA FOUND IN COMPLIANCE WITH SRM 53-20-00 PAG 61. 2L73 4F A22WE 20051114000502005111400050WP 2005 11 14 05FDEA03704 120051108A5310 REPAIR DOUG DC10 DC1010 3022110WP FUSELAGE UNDAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 FOUND EXTERNAL TRIPLE DOUBLER BETWEEN STA 1853 AND 1887 LONGERONS 36 AND 38 LT SIDE JUST AFT OF BULKHEAD CARGO DOOR. PERFORMED A GVI OF EXISTING REPAIR IAW EO 8-5100-7-5001 CRITERIA FOUND DOUBLER IN COMPLIANCE WITH SRM 53-20-00 FIG 6. 2L73 4F A22WE 20051114000522005111400052WP 2005 11 14 05FDEA03706 120051108A5310 REPAIR DOUG DC10 DC1010 3022110WP BS 2131 UNDAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 AFT FUSELAGE ABOVE HORIZONTAL STABILIZER LT SIDE STA Y2131 FOUND AN EXTERNAL DOUBLER REPAIR. PERFORMED A GVI OF EXISTING REPAIR IAW EO 8-5100-7-5001 CRITERIA FOUND DOUBLER IN COMPLIANCE WITH SRM 53-00-01 FIG 4. 2L73 4F A22WE 20051114000542005111400054WP 2005 11 14 IXXA05SMN254S 120051013A5330 REPAIR DOUG DC8 DC871F 302199DWP BS 1550.00 IMPROPER B IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW11829BX896722998 45994 DURING C CHECK INSPECT, RT FUSELAGE AFT CENTER SECTION FWD OF R-2 DOOR OPENING EVALUATE CONFORMITY PER SRM AT STA FS 1550.00 L-15.5 RT. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-0 FIG 22A, EO SEMAN NR 20051300 DATED 09-28-05. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21. FABRICATED REPAIR DOUBLER ( -7073) (AL7075T6 0.190”) IAW DC8 SRM 53-2-0 FIG 22A (SHEET 1, 3, 14), DC8 SRM 53-4-1 FIG 19 ITEM “B”. CLEANED, TREATED, PRIMED AREA + REPAIR DOUBLER IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED REPAIR DOUBLER IAW DC8 SRM 53-2-0 FIG2A (SHEET 3, 12, 13, 14), DC8 SRM 51-1-21, DC8 SRM 51-1-20D, DC8 SRM 51-3-1 (TORQUE). 2L74 4F RT4A25 20051114000562005111400056WP 2005 11 14 IXXA05RNG070S 120050907A5512 SKIN DOUG DC8 DC872 302199BWP STA XE 235 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK, FOUND CORROSION ON LH HORIZONTAL STABILIZER LOWER SURFACE SKIN, STATION XE 235. BLEND OUT IN CORRODED AREA WAS PERFORMED AND REPAIR DOUBLER WAS INSTALLED IAW EO ATI-091305 AND EWO ATI 55-007. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR. 2L74 4F RT4A25 20051114000582005111400058WP 2005 11 14 IXXA05SMN255S 120051013A5330 REPAIR DOUG DC8 DC871F 302199DWP FS 245.00 IMPROPER B IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW11829BX896722998 45994 DURING C CHECK INSPECTION, LT FUSELAGE FWD CENTER SECTION WINDOW BELT EVALUATE CONFORMITY PER SRM AT STA FS 245.00 L-15.5 LT. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-0 FIG 22A, TR # 53-170, EO SEMAN # 20051301 DATED 09-28-05. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-20D. FAB`D REPAIR DOUBLER (AL7075T6 0.100) IAW DC8 SRM 53-2-0 FIG 22A (SHEET 1, 10, 15) TR # 53-170, DC8 SRM 53-4-1 FIG 6 ITEM B, DC8 SRM 51-9-0 PAG 68A. CLEANED, TREATED, PRIMED AREA + EXT. REPAIR DOUBLER IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED EXT REPAIR DOUBLER IAW DC8 SRM 53-2-0 FIG 22A (SHEET 1, 10, 12, 13, 15), DC8 SRM 51-1-21, DC8 SRM 51-1-20D, DC8 SRM 51-3-1 (TORQUE). 2L74 4F RT4A25 20051114000602005111400060WP 2005 11 14 IXXA05SMN257S 120051013A5330 DOUBLER DOUG DC8 DC871F 302199DWP FS 1356.00 UNKNOWN B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING C CHECK INSPECT, LT FUS AFT CTR SECTION LWR PLATING DOUBLER UPGRADE THICKNESS AT STA FS 1356.00 L-29 RT. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-1 FIG 7, EO SEMAN NR 20051303 DATED 09-29-05. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21. REMOVED DAMAGED SECTION IAW DC8 SRM 53-2-1 FIG 7 (SHEET 1, 4). NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D REPAIR DOUBLER (AL7075T6 0.090) + (02EA) INTERNAL FINGER DOUBLERS (AL7075T6 0.050) + FILLER (AL7075T6 0.080) IAW DC8 SRM 53-2-1 FIG 7 (SHEET 1, 4), DC8 SRM 53-4-1 FIG 16 (SHEET 2) ITEM “C”, DC8 SRM 51-9-0 FIG 68A, DC8 SRM 51-1-4 PG 1 (FORMING). CLEANED, TREATED, PRIMED AREA, REPAIR PARTS IAW DC2L74 4F RT4A25 20051114000772005111400077EU 2005 11 14 AWXA200501343 120051106A5230 HANDLE AIRBUS320 A320231 3930325EU CARGO DOOR UNSECURE A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28627AW 66 FLT 287 - CREW REPORTED AFT CARGO DOOR OPEN ON T/O ROLL PRIOR TO 60 KNOTS. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND HANDLE NOT COMPLETELY CLOSED. CLOSED HANDLE OPS NORMAL. 2L72 4F RTA28NM 20051114000812005111400081NM 2005 11 14 05FDEA02675 120050826A5330 REPAIR DOUG MD11 MD11 3023602NM BS 392-401 UNDAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 EXISTING REPAIR DOUBLER FOUND AT STA 392 TO STA 401 L26 LT. EXISTING REPAIR AT STA 392 TO STA 401 L26 LT EVALUATED AND FOUND CARRIED OUT AS PER SRM 53-40-00 FIG 5 VOL I EO 1-5100-7-5001, TITLE, STRUCTURES, REPAIR CATALOG MD-11 REPAIR CLASSIFICATION AND TRACKING REQUIREMENTS 14CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20051114000872005111400087WP 2005 11 14 05FDEA03728 120051109A5753 SKIN DOUG DC10 DC1030 3023501WP ZONE 500 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25310FE 48299 LEFT WING OUTBOARD FLAP HAS DENTS 4 PLACES. DENTS AT XOF657, 639, AND 611 FOUND TO BE WITHIN LIMITS IAW DC10 SRM 57-10-00 FIG 48 VOL I. REPAIRED DENT AT XOF 516 IAW DC10 SRM 57-10-00 FIG 85 VOL I. SEE FEDEX NONROUTINE NR N00229 OF WORK ORDER 0030375. 2L73 4F A22WE 20051114000892005111400089WP 2005 11 14 05FDEA03709 120051108A5330 REPAIR DOUG DC10 DC1010 3022110WP BS 1139 UNDAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 FOUND EXTERNAL TRIPLE DOUBLER REPAIR AT STA 1139 BETWEEN LONGERON 47 AND 48 RT SIDE. PERFORMED A GVI OF EXISTING REPAIR IAW EO 8-5100-7-5001 CRITERIA FOUND DOUBLER IN COMPLIANCE WITH SRM 53-20-00 FIG 6. 2L73 4F A22WE 20051114000912005111400091NM 2005 11 14 AALA20050716 120051030A3350D71702001 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21778AN 29587 JFK - EGRESS EMERGENCY LIGHTS IN AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EGRESS EMERGENCY LIGHTS IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20051114000932005111400093 2005 11 14 SWAA053545 420051108A25656949956 CABLE BOEING737 7373Q8 1384670NM L2 DOOR SLIDE MISROUTED A SWAAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW29317WN 24068 DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE LATCH CABLE ASSY MISROUTED. REROUTED CABLE ASSY PER MM. 2L72 4F RTA16WE 20051114000952005111400095NM 2005 11 14 SWAA053547 120051109A53306545774 SKIN BOEING737 7373H4 1384600NM BS 740D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29344SW 24152 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 740D, STR 19R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051114000962005111400096EU 2005 11 14 05FDEA03731 120051109A5315 FLOORBEAM AIRBUS310 A310203 3930313EU FUSELAGE DAMAGED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25423FE 281 RT SIDE ROLLER TRAY 1 OB OF CENTER AT FS 38 OB LEG HAS 1 EA DOUBLE DRILLED HOLE REF N00468. REPAIRED FLOORBEAM IAW SRM 53-10-15 FIG 207 AND REPLACED ROLLER TRAY IAW SRM 51-75-10. 2L72 4F RTA35EU 20051114000972005111400097NM 2005 11 14 SWAA053553 120051109A5754 SKIN BOEING737 7373H4 1384600NM LT WING SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED C3 CHECK, FOUND NR 2 L/E SLAT OUTBOARD LOWER SKIN CRACKED. REPAIRED SLAT PER SWA EA. 2L72 4F RTA16WE 20051114000992005111400099NM 2005 11 14 SWAA053555 120051110A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 827 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 827, STR 11L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051114001012005111400101NM 2005 11 14 SWAA053557 120051110A53116546526 FRAME BOEING737 7373H4 1384600NM BS 400 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051114001032005111400103NM 2005 11 14 SWAA053559 120051110A53116546536 SHEAR TIE BOEING737 7373H4 1384600NM BS 597 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 597, BETWEEN STR 13R TO STR 14R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051114001052005111400105NM 2005 11 14 SWAA053561 120051110A335010107451 SIGN BOEING737 7373H4 1384600NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29341SW 24091 R1 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM. 2L72 4F RTA16WE 20051114001072005111400107NM 2005 11 14 SWAA053563 120051109A53306545774 SKIN BOEING737 7373H4 1384600NM BS 727E CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29354SW 25219 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 18L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051114001092005111400109NM 2005 11 14 SWAA053565 120051109A53306545776 SKIN BOEING737 7375H4 138449DNM BS 927 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29508SW 24185 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 25R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051114001112005111400111NM 2005 11 14 SWAA053567 120051110A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 727B CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727B, STR 16L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051114001132005111400113 2005 11 14 SWAA053569 420051104A2565416A2100 CASE BOEING737 7377H4 1384404NM R1 DOOR SLIDE LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29766SW 29806 R1 DOOR EMERGENCY EVAC SLIDE CONTAINER LOOSE. SECURED SLIDE CONTAINER PER MM. 2L72 4F RTA16WE 20051114001192005111400119NM 2005 11 14 05FDEA03749 120051110A5311 FRAME DOUG MD11 MD11 3023602NM BS 1305 CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25576FE 48501 DURING PASSENGER TO FREIGHT COVERSION FOUND CRACK 1.20" LONG ON FRAME STA1305 BETWEEN LT 11 LT 12. DURING PASSENGER TO FREIGHT CONVERSION: FOUND CRACK 1.2" LONG ON FRAME STA 1305 RT SIDE BETWEEN L11 TO L12. TRIMOUT TIME CRACK WITH 0.5" RADIUS AND 2 REMAINING FASTENERS. PERFORMED INSPECTION FOR CRACK, INSTALLED FILLER MT 7075T6, INSTALLED REPAIR STRAP MAT 7075T6 WITW THK .126" USING FASTENER HLT436-6 (APPROVAL BOEING). PROTECT PER SRM 51-21-01. 2L73 4F RTA22WE 20051114001212005111400121EU 2005 11 14 05FDEA03751 120051110A5315 FLOORBEAM AIRBUSA300 A300F4622R 3930360EU BS 10 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25721FD 477 AVIONICS COMPT FLOORBEAM FS 10 RBL 40 ANGLE IS CRACKED. 2L72 4F RTA35EU 20051114001232005111400123NM 2005 11 14 CALA0500393 120051109A5320147A5660Y2 INTERCOSTAL BOEING737 737724 13844BYNM GE CFM56 CFM56* 13802NE STA 947.5-986.5 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2723708 28769 INSPECTION FOUND R-2 DOOR INTERCOSTAL CORRODED AT DRAIN HOLE, STA 947.5 TO 986.5, RBL 38. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F4 FRTA16WE E2GL 20051114001262005111400126EA 2005 11 14 DJFA2005159 120051019A531260032014105 BULKHEAD CNDAIRCL601 CL6012A12 1900303EA GE CF34 CF341A NE FS 409.00 CRACKED E DJFAK NONE O OTHER ININSP/MAINT 1 EA23627CW 3027 DURING A ROUTINE MAINTENANCE VISIT, A CRACK WAS DISCOVERED IN THE PRESSURE BULKHEAD WEB AT FUSELAGE STATION 409.00 WHILE PERFORMING AD 97-24-02. THE CRACK WAS REPAIRED IAW EO NR 601-53-10-266, AND IN CONJUNCTION WITH DRAWING K600-31904. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA21AE E15NE 20051114001292005111400129EA 2005 11 14 COMA0560587 120051105A2750852D10019 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS UNRELIABLE A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01915CA6274 7013 FLIGHT 5290 - FLAPS FAIL CAUTION. REPLACED THE RIGHT INBOARD FLAP ACTUATORS. 2L72 4F RTA21EA 20051114001342005111400134EU 2005 11 14 05FDEA03735 120051109A5347 SEAT TRACK AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 FOUND MAIN CABIN BETWEEN FS 15 AND 16 FLOOR LEVEL LBL 2 SEAT TRACK HAS PITTING CORROSION LEFT SIDE REF N00668. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-72-10. 2L72 4F RTA35EU 20051114001362005111400136EU 2005 11 14 05FDEA03737 120051109A5347 SEAT TRACK AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 FOUND MAIN CABIN FS 17 TO FS 19 RIGHT SIDE SEAT TRACK 4R HAS 2 AREAS OF EXFOLIATED CORROSION, REF N00662. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-75-10. 2L72 4F RTA35EU 20051115000062005111500006NM 2005 11 15 CALA0500401 120051112A523065469231528CAL1 SKIN BOEING737 7373T0 1384582NM CARGO DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2759338 23576 INSPECTION FOUND A 1/2" CRACK AT HOLE CUTOUT IN C-1 INNER DOOR SKIN, STA 440-480, S19R TO S24R. REPAIRED IAW ECRA 5232-01067. 2L72 4F RTA16WE 20051115000162005111500016NM 2005 11 15 NOCA1605 120051006A3350767 BULB BOEING757 75728A 1384976NM EMERGENCY LIGHT INOPERATIVE G NOCAK NONE L NO TEST ININSP/MAINT 1 EA15750NA 26277 JFK - ROUTINE MAINTENANCE FOUND 1L EMERGENCY EXIT EXTERIOR LIGHT INOP. RELAMPED 1L EMERGENCY EXIT LIGHT, OPS CHECK OK. 2L72 4F RTA2NM 20051115000272005111500027EA 2005 11 15 SWIA200515823 120050612A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA CRACKED CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07967SW 7872 FOUND FS 280 AT RBL 9 O/B FLOORBEAM ATTACH ANGLE IS CRACKED, ITEM FOUND AT C CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, 51-21-11, 51-25-01. 2L72 4F RTA21EA 20051115000352005111500035NM 2005 11 15 UPS05545740 120051015A5347BAC15202472 SEAT TRACK BOEING757 75724APF 1384969NM BS 1321 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01404UP 23726 FOUND BS 1321, WL 208, LBL 26, SEAT TRACK OUTBOARD FLANGE HAS AREA OF CORROSION. REPAIRED PER 53-00-52-2R AND GOODRICH ER NR 05-4696. 2L72 4F RTA2NM 20051115000502005111500050NM 2005 11 15 AALA20050737 120051007A3350D71702100 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21788AN 30011 AFW - EMERGENCY LIGHTS IN COACH INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN COACH. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20051115000512005111500051EA 2005 11 15 SWIA200515825 120050612A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 621 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07967SW FOUND FLOOR SUPPORT ANGLE AT FS 621.00 LEFT IS CRACKED, ITEM FOUND AT C CHECK INSPECTION. REPAIR CRACKED SUPPORT ANGLE IAW CRJ REO 601R-53-61-117 REV "B". 2L72 4F RTA21EA 20051115000622005111500062WP 2005 11 15 UPS05845749 120051017A5740 FITTING DOUG DC8 DC873F 302199FWP BS 219 CHAFED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 FOUND CANOE FITTING CHAFFED IB AND OB AT STA 219 LT OB FLAP. BLENDED OUT CHAFED AREA, SHOT PEENED IAW SRM 51-1-8, DPS 4.999-2 AND SAA SK 813-822426. 2L74 4F RT4A25 20051115000652005111500065 2005 11 15 UPS05M45752 420051026A34604059050921 FMC DOUG MD11 MD11F 3023600NM NR 2 INOPERATIVE A IPXAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 SO01256UP 48405 ATB - FMC NR 2 FAILURE, NR 2 FMC REPLACED PER AMM 34-63-01. CROSS LOAD FMC NDB/AMI SOFTWARE PER AMM 34-63-05. RETERMINATED WIRE B903-1073-20BL AT S3-21 POS 35BA PER STD WIRE PRACTICE MNL. 2L73 4F RTA22WE 20051115000812005111500081NM 2005 11 15 AWXA200501375 120051111A3350BR964411 LIGHT BOEING757 7572G7 1384963NM CABIN INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28910AW 24523 SEA - EEL - DURING OVERNIGHT INSPECTION, DISCOVERED EMERGENCY PATHWAY LIGHT AT ROW 23, LEFT, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AT ROW 23L. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA2NM 20051115000842005111500084NM 2005 11 15 NOCA0905 120050808A33501317 LAMP BOEING767 767324 1385203NM EMERGENCY LIGHT INOPERATIVE G NOCAK NONE L NO TEST ININSP/MAINT 1 EA15767NA 27569 BOTH LIGHTS IN EMERGENCY LIGHT FIXTURE OVER RT SIDE FLAP ARE INOP. REPLACED BOTH LAMPS IN EMERGENCY LIGHT FIXTURE OVER RT WING FLAP. ONE LIGHT IN EMERGENCY LIGHT FIXTURE OVER RT WING BEHIND R3 DOOR IS OUT. REPLACE LAMP IN EMERGENCY LIGHT FIXTURE OVER RT WING BEHIND R3 DOOR IAW MM 33-51-06. 2L72 4F RTA1NM 20051115000862005111500086EU 2005 11 15 UPS05145730 120051107A5754A5724228405100 ACCESS PANEL AIRBUSA300 A300F4622R 3930360EU RIGHT KRUEGER CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01120UP 0805 ACCESS PANEL REMOVED IN RIGHT KRUEGER FLAP BOX AREA. INSTALLED ACCESS PANEL IN RIGHT KRUEGER FLAP BOX AREA PER 57000. 2L72 4F RTA35EU 20051115000902005111500090EA 2005 11 15 COMA0560596 120051110A80128989308 START VALVE CNDAIRCL600 CL6002B19 1900309EA RT ENGINE FAULTY A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01868CA13959 7427 FLIGHT 5768 - UPON TAKEOFF ROLL RECEIVED A RIGHT ENGINE START LIGHT AND STATUS MESSAGE, ABORTED TAKEOFF. DURING SECOND TAKEOFF ATTEMPT RECEIVED SAME MESSAGE ALONG WITH NO STARTER CUTOUT CAUTION MESSAGE. AIRCRAFT RETURNED TO GATE. 2L72 4F RTA21EA 20051115000932005111500093NM 2005 11 15 NOCA2405 120051031A5210 DOOR BOEING767 767300 1385204NM L2 DOOR STIFF G NOCAK NONE O OTHER TXTAXI/GRND HDL 1 EA15760NA 26257 DOOR L AT HARD TO ARM. ESCAPE SYSTEM EXAMINED AND EXERCISED FOR DOOR L AT IN ACCORDANCE WITH 25-66-01 206-001. OPERATION CHECKED NORMAL. 2L72 4F RTA1NM 20051115000962005111500096SO 2005 11 15 C2XA05IA125 120051029A335078241 INVERTER EMB 145 EMB145 3260210SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714959 145091 STL - DURING MAINTENANCE INSPECTION, AN EMERGENCY EXIT SIGN WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FIVE EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND APPROVED THE AIRCRAFT FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20051115000982005111500098 2005 11 15 DXTA200501050 420051006A34207023460801 DISPLAY CESSNA680 680CE 2076811CE COCKPIT BURNED E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL07301QS312 6800010 RIGHT PFD / DU NR 4, ATTITUDE FAIL, HEADING FAIL, EVENTUALLY DU BLACKED OUT. FUMES IN THE COCKPIT. DU CAME BACK ON BEFORE LANDING. TROUBLESHOT TO BAD DU NR 4. REPLACED DU NR 4 AND DOWNLOADED FILES TO DU NR 4 IAW CE680 M/M 34-23-00. OP'S CHECK GOOD. 2L72 4F RCT00012WI 20051115001002005111500100CE 2005 11 15 DXTA200501052 120051015A3240GPP125073 PRESSURE SWITCH CESSNA560 560XL 2076702CE MLG BRAKE SYS FAILED E DXTAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07631QS2473 5605131 WHILE ON THE TAXIWAY WITH THE PARKING BRAKE SET THE MASTER CAUTION ILLUMINATED WITH THE LOW BRAKE PRESS AND ANTI-SKID INOP ANNUNCIATORS ILLUMINATED. THE BRAKES FAILED, USED THE EMERGENCY PNEUMATIC BRAKE TO STOP ROLLING. ACCOMPLISHED SEVERAL OPERATIONAL CHECKS OF BRAKE SYSTEM. FOUND BRAKE PACK TO OPERATE AT 1200 PSI AND TURN OFF AT 1500 PSI. REPLACED PRESSURE SWITCH S/N 011 AS A PRECAUTION. REMOVED SWITCH. INSTALLED A REPAIRED SWITCH. LEAK AND OPS CHECK WAS FOUND TO BE SATISFACTORY. ACCOMPLISHED IAW CE560XL MM 32-42-06. ACCOMPLISHED BLEEDING OF ANTI-SKID BRAKE SYSTEM IAW CE560XL MM 32-40-00. SERVICED EMERGENCY GEAR AND PNEUMATIC BRAKE BOTTLE IAW CE560XL MM 12-13-01. 2L72 4F RTA22CE 20051115001072005111500107CE 2005 11 15 DXTA200501060 120051104A323355275043 ACTUATOR CESSNA560 560XL 2076702CE MLG FAILED E DXTAO OTHER J WARNING INDICATION APAPPROACH 1 GL07601QS2979 5605301 NOSE GEAR FAILED TO EXTEND OR LOCK WHEN GEAR SELECTED DOWN. RED UNSAFE LIGHT ON AND NOTICABLE VIBRATION. RECYCLED AND ALL 3 GEAR POSITION LIGHTS CAME ON. LANDED WITHOUT INCIDENT. REMOVED AND INSTALLED A NEW NOSE GEAR UPLOCK ACTUATOR. OPS AND LEAK CHECKS GOOD AT THIS TIME. ALL WORK DONE IAW CESSNA 560XL MM CHAPTER 32-30-05. 2L72 4F RTA22CE 20051115001082005111500108CE 2005 11 15 DXTA200501055 120051103A2821 FILTER BEECH MU300 400A 1155402CE FUEL SYSTEM BYPASSING E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07106QS RK381 ABORTED TAKEOFF AT 50 KTS DUE TO RIGHT FUEL BYPASS LIGHT ILLUMINATED AND STAYED ON UNTIL THROTTLES WERE BACK AT IDLE. REMOVED AND REPLACED BOTH FUSELAGE FUEL BOWL FILTERS, LEAK CHECK GOOD REF 400XP MM 28-20-00. 2H72 4F RTA16SW 20051115001092005111500109CE 2005 11 15 DXTA200501056 120051103A4920 APU RAYTHNDH125 HAWKER800XP 7150012CE SMOKE E DXTAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL07824QS 258523 STARTED THE APU ON THE GROUND UPON OPENING THE BLEED AIR VALVE THE AIRCRAFT FILLED W/SMOKE. DEFERRED IAW NJA HAWKER 800XP MEL 49-00-1 RAN BOTH ENGINES WITH AIR VALVES OPEN NO SMOKE OR ODOR NOTICED. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA3EU 20051115001122005111500112NM 2005 11 15 NOCA0505 120050506A3397 CONNECTOR BOEING767 767324 1385203NM EMERGENCY LIGHT LOOSE G NOCAK NONE H ELECT. POWER LOSS-50 PC ININSP/MAINT 1 EA15767NA 27569 JFK - DOOR OVERHEAD EXIT SIGN LIGHT INOP. SECURED LOOSE CONNECTOR OPS NORMAL. EMERGENCY LIGHT BEHIND SEAT 36AB FOUND LOOSE CONNECTION. R4 EMERGENCY LIGHT INOP CLEANED CONTACT OPS CHECKED NORMAL. 2L72 4F RTA1NM 20051115001132005111500113NM 2005 11 15 NOCA1205 120050920A2450 IDG BOEING767 767324 1385203NM LEFT ENGINE DISENGAGED G NOCAD RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 EA15767NA 27569 AT START OF TAKEOFF ROLL, LEFT GENERATOR DROPPED OFF LINE, "L IDG" EICAS MESSAGE. IDG SERVICED, ENGINE HIGH POWER RUN, ALL INDICATIONS NORMAL. 2L72 4F RTA1NM 20051115001142005111500114NM 2005 11 15 QXEA200501510 120051109A33506104781 BATTERY PACK DHAV DHC8 DHC8202 2809007NM EMERGENCY LIGHT MALFUNCTIONED A QXEAO OTHER O OTHER TXTAXI/GRND HDL 1 NM09362PH* 49 518 PSC - FLOOR TRACK LIGHTING ROW 2-6 INOP. MAINTENANCE REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051115001172005111500117NM 2005 11 15 05FDEA03754 120051110A5753 REPAIR BOEING727 7272S2F 1384O81NM FORE FLAP DAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25213FE 22935 FOUND REPAIR LT I/B FORE FLAP, L/E REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT LT I/B, FORE FLAP WAS DETERMINED TO BE IAW SRM 57-50-4 FIG 1. BASED ON AN EXTERNAL VISUAL EVALUATION WITH REPAIR INSTALLED. REPAIR CLASSIFIED AS MAJOR. BASED ON GMM 6-2-100 CRITERIA. 2L73 4F A3WE 20051115001182005111500118WP 2005 11 15 05FDEA03742 120051109A5730 REPAIR DOUG MD10 MD1010F 3022112WP RT WING UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25372FE 46610 "WINGS BASIC EXTISTING EXTERNAL DOUBLER ON RT WING UPPER SKIN. COMPLIED WITH EA8-5710-92352 WINGS BASIC EXISTING EXTERNAL DOUBLER ON RT WING UPPER SKIN. 2L73 4F RTA22WE 20051115001192005111500119 2005 11 15 BB05097 420051112A256520121 POWER SUPPLY BOEING767 7672B7 1385107NM SLIDE DEFECTIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19656US 26847 PHL - DURING SQUIB TEST, THE RIGHT EMERGENCY ESCAPE SPOILER SQUIB WILL NOT TEST AT SQUIB PANEL. MAINTENANCE FOUND THE RIGHT OFF-WING ESCAPE SYSTEM POWER SUPPLY M962 AND BATTERY DEFECTIVE. REPLACED BOTH POWER SUPPLY AND BATTERY. OPERATIONAL GOOD. 2L72 4F RTA1NM 20051115001202005111500120EU 2005 11 15 EMB05016 120051109A29135116402 PUMP EMB ERJ170ERJ170100 EU NR 2 HYD SYSTEM LEAKING A USAAH DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 EA19807MD222 79 000020 BNA FLT 1647, EN ROUTE DCA TO BNA - ABOUT 50 MILES FROM BNA, THE NR 2 HYDRAULIC SYSTEM QUANTITY DROPPED TO ZERO. THE FLIGHT CREW FOLLOWED THE QRH PROCEDURES, WHICH INCLUDED AN ALTERNATE GEAR EXTENSION. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 ENGINE HYDRAULIC PUMP. OPERATIONALLY CHECKS OK. 2L74 4F RTA56NM 20051115001212005111500121NM 2005 11 15 USAA200511005 120051111A5330 SKIN BOEING737 7373B7 1384580NM BS 727E CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19433US 24555 FOUND 3 INCH CRACK IN FUSELAGE SKIN AT STATION 727E AT STRINGER 23R. 2L72 4F RTA16WE 20051115001232005111500123NM 2005 11 15 SB05146 120051115A335020131A BATTERY PACK BOEING737 737401 1384701NM EMERGENCY LIGHT DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19409US 23879 PIT - MAINTENANCE REPORTED THE AFT GALLEY EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20051115001242005111500124NM 2005 11 15 05FDEA03755 120051110A5710 REPAIR BOEING727 7272S2F 1384O81NM KRUGER FLAP UNDAMAGED A FDEAK NONE O OTHER UKUNKNOWN 1 SO25213FE 22935 FOUND REPAIR AT NR 4 L/E KRUGER FLAP, RT WING TOP SIDE. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT NR 4 L/E KRUGER FLAP, RT WING TOP SIDE WAS DETERMINED TO BE IAW SRM 57-50-3 FIG 3. BASED ON AN EXTERNAL VISUAL EVALUATION WITH REPAIR INSTALLED. REPAIR IS CLASSIFIED AS A MAJOR REPAIR BASED ON GMM 6-2-100 CRITERIA. 2L73 4F A3WE 20051115001252005111500125NM 2005 11 15 05FDEA03763 120051111A5330 SKIN DOUG MD11 MD11 3023602NM ZONE 100 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 FOUND LOWER FUSELAGE, CENTER CARGO DOOR CUTOUT FORWARD LOWER AREA FOUND WITH DENTS. TRIMMED OUT AS PER SRM 53-50-00 FIGURE 16 VOLUME I. HFEC INSPECTION CARRIED OUT AS PER NDTSPM PART 06-10-01-001 REV 12 ON THE PERIPHERY OF TRIMMED EDGE AND FOUND NO CRACK EVIDENT. FILLER AND REPAIR DOUBLER FABRICATED AS PER SRM 53-50-00 FIGURE 16 VOLUME I AND INSTALLED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051115001262005111500126NM 2005 11 15 05FDEA03762 120051110A5753 HINGE FITTING DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 FOUND RIGHT WING OUTBOARD FLAP INBOARD HINGE FITTING OUTBOARD NR 3 BOLT HOLE FOUND CORROSION. CORROSION REMOVED & REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-90057. 2L73 4F RTA22WE 20051115001282005111500128NM 2005 11 15 05FDEA03765 120051111A5330 REPAIR BOEING727 727233 138408ANM FUSELAGE UNDAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25266FE 21672 FOUND REPAIR AT STA 1050 STR 29L. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT STA 1050 STR 29L WAS DETERMINED TO BE IAW SRM 53-30-3 FIG 1 BASED ON GMM 6-2-100 CRITERIA. 2L73 4F RTA3WE 20051115001292005111500129NM 2005 11 15 05FDEA03766 120051111A5330 REPAIR BOEING727 727233 138408ANM FUSELAGE UNDAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25266FE 21672 FOUND REPAIR AT STA 1223 STR 19R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT STA 1223 STR 19R WAS DETERMINED TO BE IAW SRM 53-30-3 FIG 28 BASED ON AN EXTERNAL VISUAL EVALUATION WITH REPAIR INSTALLED. REPAIR IS CLASSIFIED AS MAJOR BASED ON GMM 6-2-100 CRITERIA. 2L73 4F RTA3WE 20051115001302005111500130NM 2005 11 15 05FDEA03756 120051110A5753 REPAIR BOEING727 7272S2F 1384O81NM FORE FLAP UNDAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25213FE 22935 FOUND REPAIR RT INBD FORE FLAP. LEADING EDGE REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION, AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA, PREVIOUSLY INSTALLED REPAIR AT RT INBD FORE FLAP WAS DETERMINED TO BE IAW SRM 57-50-4 FIG 1. BASED ON AN EXTERNAL VISUAL EVALUATION WITH REPAIR INSTALLED. 2L73 4F A3WE 20051115001312005111500131NM 2005 11 15 05FDEA03757 120051110A5330 REPAIR BOEING727 7272S2F 1384O81NM FUSELAGE UNDAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25213FE 22935 FOUND REPAIR STA 500-520 LT BOTTOM FUSELAGE SKIN, BELOW MAIN CARGO DOOR. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT FS 500-FS520 S24L-S25L WAS DETERMINED TO BE IAW SRM 53-30-3 FIG 3. BASED ON AN EXTERNAL VISUAL EVALUATION WITH REPAIR INSTALLED. REPAIR IS CLASSIFIED AS MAJOR BASED ON GMM 6-2-100 CRITERIA. 2L73 4F A3WE 20051115001322005111500132NM 2005 11 15 05FDEA03758 120051110A5754 REPAIR BOEING727 7272S2F 1384O81NM KRUGER FLAP UNDAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25213FE 22935 FOUND REPAIR TOP SIDE NR 3 L/E KRUGER FLAP LT WING. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT NR 3 L/E KRUGER FLAP, TOP SIDE ON LT WING WAS DETERMINED TO BE IAW SRM 57-50-3 FIG 3. BASED ON AN EXTERNAL VISUAL EVALUATION WITH REPAIR INSTALLED. 2L73 4F A3WE 20051115001332005111500133NM 2005 11 15 05FDEA03759 120051110A5753 HINGE FITTING DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 FOUND LEFT WING OUTBOARD FLAP INBOARD HINGE FITTING MOST AFT BOLT HOLE FOUND CORROSION. CORROSION REMOVED & REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-90059. 2L73 4F RTA22WE 20051115001352005111500135NM 2005 11 15 05FDEA03761 120051110A5753 HINGE FITTING DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 FOUND RIGHT WING OUTBOARD FLAP INBOARD HINGE FITTING MOST AFT BOLT HOLE FOUND CORROSION. CORROSION REMOVED & REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-90058. 2L73 4F RTA22WE 20051115001372005111500137WP 2005 11 15 ABXA050274 120051027A531199582387 FRAME DOUG DC9 DC941 302207NWP BS 1152 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23974AX 47623 FOUND CRACK ON FRAME AT FASTENER FS 1152 AT LONGERON 15 RIGHT. REPAIRED AREA IAW DC-9 SRM 53-03. 2L72 4F A6WE 20051115001402005111500140WP 2005 11 15 ABXA050276 120051028A522059131951 DOOR DOUG DC9 DC941 302207NWP EMERGENCY EXIT CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23974AX 47623 RIGHT FORWARD OVERWING EXIT DOOR HAD CRACKS AROUND 2 EACH STOPS ON LOWER AFT CORNER DOOR PAN. REPAIRED LOWER AFT CORNER IAW DC-9 SSRM DWG K07390. RE-INSTALLED DOOR STOPS IAW DC-9 SRM 51-30-1 AND 51-30-2. HEAT TREATED IAW DC-9 SRM 51-10-2A. 2L72 4F A6WE 20051115001412005111500141WP 2005 11 15 ABXA050277 120051028A522059131951 PAN DOUG DC9 DC941 302207NWP EMERGENCY DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23974AX 47623 AFT LEFT OVERWING EXIT DOOR HAD CRACK AT LOWER AFT STOP ON DOOR PAN. REMOVED AND REPLACED DOOR ON JC 9542005. 2L72 4F A6WE 20051115001422005111500142WP 2005 11 15 ABXA050278 120051028A53203924028501 FITTING DOUG DC9 DC941 302207NWP BS 642 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23974AX 47623 FOUND LONGERON END CRACKED KEEL AREA 29 RIGHT AT FS 642. REMOVED AND REPLACED LONGERON END FITTING IAW DC-9 SRM. 2L72 4F A6WE 20051115001432005111500143WP 2005 11 15 ABXA050279 120051031A53119912243105 FRAME DOUG DC9 DC941 302207NWP BS 1041 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23974AX 47623 FOUND FRAME EXFOLIATED AT FS 1041 AT LONGERON 29 LEFT. SPLICED IN NEW FRAME IAW DC-9 SRM. 2L72 4F A6WE 20051115001452005111500145EA 2005 11 15 SWIA200515835 120051106A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY MALFUNCTIONED A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07941SW 7750 CARGO SMOKE TEST NR 2 "SMOKE CARGO" MSG REMAINS. REPLACED NR 2 CARGO SMOKE DETECTOR PER CRJ 200 MM 26-15-01, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051115001472005111500147NE 2005 11 15 SWIA200515837 220051109A7261 CARBON SEAL CNDAIRCL600 CL6002B19 1900309EA PWA 545 PW545A NE ENGINE FAILED A SWIAE ENGINE SHUTDOWN O OTHER DEDESCENT 1 NM07441SW 7602 RIGHT ENGINE OIL PRESS LOW, RAN QRH MID THRUST KEPT OIL PRESS IN GREEN, THEN PRESS WENT BELOW 25 PSI (RED). RAN SINGLE ENG ABNORMAL QRH. SECURED RIGHT ENG. REPLACED NR 7 CARBON SEAL IAW GEEM SPECIAL PROCEDURES 36A. 2L72 4F4 FRTA21EA E00059EN 20051116000012005111600001NM 2005 11 16 05FDEA03779 120051111A5753 REPAIR BOEING727 727233 138408ANM FORE FLAP UNDAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25266FE 21672 FOUND REPAIR ON LT OUTBD FORE FLAP INBD LEADING EDGE. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION, AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT LT OUTBD FORE FLAP I/B L/E WAS DETERMINED TO BE IAW SRM 57-50-4 FIG 1, BASED ON EXTERNAL VISUAL EVALUATION WITH REPAIR INSTALLED. REPAIR CLASSIFIED AS MAJOR BASED ON GMM 6-2-100 CRITERIA. 2L73 4F RTA3WE 20051116000022005111600002NM 2005 11 16 05FDEA03791 120051113A5320 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 FOUND CENTER CARGO, STA 1641 TO 1661 LONGERON 44R SPLICE CRACKED. REMOVED AND INSTALLED WITH NEW LONGERON SPLICE AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2L73 4F RTA22WE 20051116000042005111600004NM 2005 11 16 05FDEA03793 120051113A5313 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 FOUND CENTER CARGO STA 1806 TO 1821 LONGERON 46R CORROSION. REPAIR CARRIED OUT AT CENTER CARGO - STA 1806 TO 1821 LONGERON 46R AS PER SRM 53-10-00 FIG. 1 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051116000052005111600005NM 2005 11 16 05FDEA03794 120051113A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 FOUND CORROSION, LEFT NR 35 BORE. FOUND CORROSION EXCEEDED LIMITS. REPAIR CARRIED OUT IAW FEDEX EA 1-5510-94568. 2L73 4F RTA22WE 20051116000062005111600006WP 2005 11 16 05FDEA03796 120051114A5310 DOOR FRAME DOUG DC10 DC1010F 3022111WP BS 1256 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 MAIN CABIN, FOUND 1 CRACK .25" LONG ON WEB JAMB DOOR NR 3 FWD AT STA 1256 LONG 15 RT. REPAIRED DOOR JAMB IAW SRM 53-50-00 FIG 19 SHT 1 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER F163496/N00496 AND IAW SRM 53-50-00 FIG 19 VOL 1. 2L73 4F A22WE 20051116000082005111600008WP 2005 11 16 05FDEA03798 120051114A5310 REPAIR DOUG DC10 DC1010F 3022111WP BS 505 UNDAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 BARON REPAIR, DOUBLER INSTALLED AT APPROX STA 505 RT SIDE BETWEEN LONG 39 AND 40. PERFORMED A GVI OF BARON DOUBLER IAW FEDEX EA NR 8-5320-38573B AND FEDEX EA NR 8-5320-35995A AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001. 2L73 4F A22WE 20051116000092005111600009WP 2005 11 16 05FDEA03800 120051114A5330 REPAIR DOUG DC10 DC1030F 3023504WP FUSELAGE UNDAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 PERFORMED INSPECTION IAW EO NR 8-5100-7-5001 1D P1 FOUND 3EA DOUBLER REPAIR DIMENSION 9'' BY 8'' ON INTERNAL FUSELAGE SKIN AT STA 275 TO 300 LONG 36 LT. PERFORMED INSPECTION ON REPAIR FRAME AND SKIN IAW EA NR 8-5310-46689 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 E3 P1. 2L73 4F RTA22WE 20051116000102005111600010NM 2005 11 16 05FDEA03775 120051111A5310 REPAIR BOEING727 727225 1384077NM BS 643-660 IMPROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 FOUND EXISTING STRINGER REPAIR IN FWD CARGO BAY BS 643 - BS 660 S27L. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED PREVIOUS REPAIR, FABRICATED AND INSTALLED REPAIR BS 646 TO 660 STR 27L PER SRM 53-10-3 FIG 1 THIS IS A MAJOR REPAIR. 2L73 4F A3WE 20051116000132005111600013NM 2005 11 16 05FDEA03195 120051004A5310 REPAIR DOUG MD11 MD11 3023602NM FUSELAGE UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 MID CABIN- CENTER AUX TANK UPPER SURFACE AT STA 1199 TO 1219 Z=-31 FOUND EXISTING PATCH REPAIR. CENTER AUX TANK UPPER SURFACE AT STA 1199 TO 1219 Z=-31 EXISTING PATCH. REPAIR EVALUATED AND CARRIED OUT AS PER EA NR 1-5720-93203 TITLE: WINGS, PLATES AND SKINS, CENTER WING/AUX TANK UPPER SKIN PANEL ASSEMBLY EXISTING REPAIR. PREVIOUSLY REPAIRED AREA CLASSIFIED AS MAJOR REPAIR PER GMM 6-2-100. 2L73 4F RTA22WE 20051116000142005111600014NM 2005 11 16 05FDEA03752 120051110A5330 REPAIR BOEING727 727225 1384077NM DOOR DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 EXISTING EXTERNAL REPAIR ON AFT CARGO DOOR BS 950E STR 26R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED AND REPLACED REPAIR ON AFT CARGO DOOR PER SRM 52-00-3. 2L73 4F A3WE 20051116000152005111600015NM 2005 11 16 05FDEA03769 120051111A5313 REPAIR BOEING727 727225 1384077NM STRINGER DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 EXISTING STRINGER REPAIR IN FWD CARGO BAY AT BS 710 - BS 720 18", S27R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED EXISTING STR REPAIR AND FABRICATED AND INSTALLED REPAIR PER SRM 53-10-3 AND SRM 51-30-2. 2L73 4F A3WE 20051116000162005111600016NM 2005 11 16 05FDEA03770 120051111A5510 REPAIR BOEING727 727225 1384077NM HORIZONTAL STAB DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 EXISTING REPAIR ON LEFT HORIZONTAL STAB LEADING EDGE WITH SOLID FASTENERS AT L/E STA 61.0 10" WIDE BY 10" LONG. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED NEW REPAIR AT LEFT HORIZ STAB LE STA 61.0 IAW SRM 55-10-3 AND SRM 51-30-5 AND SRM 51-30-2. 2L73 4F A3WE 20051116000202005111600020NE 2005 11 16 AALA20050738 220051112A7510 DUCT DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE ENG ANTI ICE FAILED A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21450AA 49476 DFW INFLIGHT T1680/12 NOV - NUMBER ONE ENGINE LOOP B FIRE WARNING INDICATION. LIGHT WENT OUT AFTER LOWERING THROTTLE ON ENGINE. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED BLOWN LEFT AFT ENGINE ANTI ICE DUCT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 F A6WE E9NE 20051116000222005111600022NM 2005 11 16 AALA20050750 120051114A3350 SOCKET BOEING757 757231 1384950NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21717TW 28485 DFW - EXTERIOR EMERGENCY LIGHT AT DOOR L4 INOPERATIVE. CLEANED LIGHT BULB BASE FOR EXTERIOR EMERGENCY LIGHT AT DOOR L4. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20051116000242005111600024NM 2005 11 16 AALA20050743 120051112A3350P4010049 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21690AA 25696 LAX - FIRST CLASS EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FIRST CLASS EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20051116000262005111600026NM 2005 11 16 AALA20050744 120051113A3350BPS73 BATTERY PACK BOEING767 767223 1385123NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21321AA 22322 LAX - EMERGENCY OVERWING EXIT SIGNS ABOVE HATCH ON RIGHT AND LEFT HAND SIDES INOPERATIVE. REPLACED BATTERY PACK M1209 FOR EMERGENCY OVERWING EXIT SIGNS ABOVE HATCH ON RIGHT AND LEFT HAND SIDES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20051116000272005111600027WP 2005 11 16 AALA20050740 120051111A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217537A 49991 LGA - EMERGENCY LIGHTS AT RIGHT OVERWING AFT EXIT INOPERATIVE. REPLACED BATTERY PACK B2505 FOR EMERGENCY LIGHTS AT RIGHT OVERWING AFT EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051116000282005111600028NM 2005 11 16 AALA20050741 120051112A3350BPS73 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21192AN 32386 LAX - LEFT NUMBER FOUR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR LEFT NUMBER FOUR EXTERIOR EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20051116000292005111600029NM 2005 11 16 AALA20050746 120051111A3350 LIGHT BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21618AA 24526 DFW - AFT EMERGENCY AISLE LIGHT ASSEMBLY DAMAGED. REPLACED AFT EMERGENCY AISLE LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20051116000302005111600030NM 2005 11 16 AALA20050747 120051111A3397 CONNECTOR BOEING777 777223 1385213NM EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21799AN 30258 JFK - EMERGENCY LIGHTS FROM ROW 34 AFT LEFT AND RIGHT HAND SIDES INOPERATIVE. FOUND CANNON PLUG AT ROW 34 DISCONNECTED. RESECURED CONNECTOR FOR EMERGENCY LIGHTS FROM ROW 34 AFT ON LEFT AND RIGHT SIDES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20051116000322005111600032NM 2005 11 16 AALA20050749 120051114A3350BPS73 BATTERY PACK BOEING757 757231 1384950NM EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21717TW 28485 DFW - EMERGENCY FLOOR TRACK LIGHTING FROM ROW 18 AFT INOPERATIVE. REPLACED BATTERY PACK AND CHARGER AT NUMBER 3 LEFT DOOR FOR EMERGENCY FLOOR TRACK LIGHTING FROM ROW 18 AFT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20051116000342005111600034NM 2005 11 16 05FDEA03813 120051114A5310 REPAIR BOEING727 727233 138408ANM BS 420 DAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25266FE 21672 FOUND REPAIR AT STA 420 STR 20L, NOT ACCOMPLISHED USING FAA APPROVED DATA. FEDEX GMM 6-2-100, DETERMINED TO BE A MAJOR REPAIR(REF:00665). REMOVED EXISTING DOUBLER AND FILLER IAW SRM 51-30-2, FABRICATED NEW REPAIR DOUBLER IAW SRM 53-30-3 FIG 1. INSTALLED NEW DOUBLER IAW SRM 53-30-3 FIG 1. 2L73 4F RTA3WE 20051116000372005111600037NM 2005 11 16 05FDEA03815 120051114A5310 REPAIR BOEING727 727233 138408ANM BS 303 PROPER A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25266FE 21672 FOUND REPAIR AT STA 303.9 STR12L, REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT STA 303.9 STR 12L WAS DETERMINED TO BE IAW EO NR 7-5330-7-2345 PT.2 BASED ON AN EXTERNAL VISUAL EVALUATION WITH REPAIR INSTALLED. REPAIR IS CLASSIFIED AS MAJOR BASED GMM 6-2-100. 2L73 4F RTA3WE 20051116000412005111600041NM 2005 11 16 SWAA053572 120051111A5311 FRAME BOEING737 7373H4 1384600NM BS 303 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME ANGLE CRACKED AT BS 303, STR 4L. REMOVED AND REPLACED ANGLE PER SRM. 2L72 4F RTA16WE 20051116000422005111600042NM 2005 11 16 SWAA053573 120051110A53306545775 SKIN BOEING737 7373H4 1384600NM BS 814-815 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29324SW 23414 DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 814 TO BS 815.125, STR 18L. REPAIRED SKIN PER SWA EA AND SRM. 2L72 4F RTA16WE 20051116000452005111600045NM 2005 11 16 SWAA053576 120051113A53146545866 KEELBEAM BOEING737 7373H4 1384600NM BS 710-726 DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29336SW 23940 DURING SCHEDULED 1/4D CHECK, FOUND LT KEEL BEAM DAMAGED BETWEEN BS 710 TO BS 726. REPAIRED KEEL BEAM PER SWA EA. 2L72 4F RTA16WE 20051110000562005111000056CE 2005 11 10 DJFA2005158 120051106A2120 ODOR CESSNA525 525 2076601CE WILINTFJ44 FJ44 66000GL CABIN UNKNOWN E DJFAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA23288CW 5250218 AFTER TAKEOFF THE CREW NOTICED A BURNING ODOR COMING FROM THE CABIN AREA. WHEN THE HEATER TEMPERATURE CONTROL WAS SELECTED TO MANUAL AND TOGGLED TO FULL COLD THE ODOR BEGAN TO DISSIPATE. THE AIRCRAFT WAS RETURNED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED A GROUND ENGINE RUN WITH AIR SOURCE HEAT SELECTED. OPERATIONAL CHECKS WERE NORMAL WITH NO NOTED DEFECTS. 1L72 4F4 FRTA1WI E3GL 20051110000672005111000067WP 2005 11 10 AALA20050714 120051029A3350 CONTACT DOUG DC9 DC982 3022082WP BATTERY PACK DIRTY A AALAK NONE K FLUID LOSS ININSP/MAINT 1 SW21442AA 49468 SFO WHITE EMERGENCY EXIT LIGHTS OVER RT AND LT SIDE OVERWING EXIT DOOR INOPERATIVE. CLEANED BATTERY CONTACTS FOR WHITE EMERGENCY EXIT LIGHTS OVER RT AND LT SIDE OVERWING EXIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F A6WE 20051110000682005111000068NM 2005 11 10 AALA20050712 120051026A3350D71702100 BATTERY PACK BOEING737 737823 13844BZNM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21955AN 29540 BATTERY PACK AT STA NR 328 AT FWD GALLEY DOOR FAILED FUNCTIONAL CHECK. REPLACED BATTERY PACK AT STA NR 328 AT FWD GALLEY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA16WE 20051110000852005111000085NM 2005 11 10 SWAA053534 120051108A53116520722 FRAME BOEING737 7373H4 1384600NM BS 440 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051110000862005111000086NM 2005 11 10 SWAA053535 120051108A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 277 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 11R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051110000902005111000090NM 2005 11 10 AALA20050726 120051107A3397 WIRE HARNESS BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21397AN 29604 LAX - SEAT MOUNTED EMERGENCY LIGHTS ON SEATS 31AB TO 37AB INOPERATIVE. FOND LOOSE CONNECTION AT SEAT WIRING. RESECURED CONNECTION FOR SEAT MOUNTED EMERGENCY LIGHTS ON SEATS 31AB TO 37AB. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20051110000992005111000099WP 2005 11 10 IXXA05SMN261S 120051013A5730 DOUBLER DOUG DC8 DC871F 302199DWP XFS 847.500 CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX 45994 DURING ROUTINE C CHECK INSPECTION, LT OUTER WING, OTBD L/E ACCESS DOOR INTERNAL DOUBLER CORRODED, XFS 847.500. REMOVED CORROSION IAW DC8 SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW DC8 SRM 57-2-0 PG 16. REMOVED CORRODED INTERNAL DOUBLER IAW DC8 SRM 51-1-21. FAB`D NEW DOUBLER (AL7075T6 0.160) IAW DC8 SRM 57-3-1 FIG 7 ITEM Q. CLEANED, TREATED AND PRIMED IAW DC8 SRM 51-1-8B. INSTALLED INTERNAL DOUBLER IAW DC8 SRM 51-1-21. 2L74 4F RT4A25 20051114000082005111400008NM 2005 11 14 05FDEA03715 120051108A5322 SHEAR TIE BOEING727 727200 138407ENM BS 680 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 EXISTING FRAME SHEAR TIE REPAIR AT BS 680 STR 26L-27L. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS ACCOMPLISHED PER SRM 53-10-4. 2L73 4F RTA3WE 20051114000162005111400016WP 2005 11 14 05FDEA03710 120051108A5310 DOOR FRAME DOUG DC10 DC1010 3022110WP BS 1259 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 FOUND MAIN CABIN L-3 DOOR FWD DOOR JAMB STA 1259 FOUND DOUBLER REPAIR BETWEEN STRINGER 24 AND 27. PERFORMED A GVI OF EXISTING REPAIR IAW EO 8-5100-7-5001 CRITERIA FOUND DOUBLER IN COMPLIANCE WITH SRM 53-50-00 FIG 19. 2L73 4F A22WE 20051114000182005111400018NM 2005 11 14 05FDEA03712 120051108A5313 STRINGER BOEING727 727225 1384077NM BS 705-720 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 FOUND EXISTING STRINGER REPAIR IN FWD CARGO BAY AT BS 705 - BS 720 15", S26R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIRED STRINGER IAW SRM 53-10-3. DETERMINED TO BE A MAJOR REPAIR. 2L73 4F A3WE 20051114000202005111400020NM 2005 11 14 AWXA200501345 120051011A5340693535214 CLIP BOEING737 7373G7 1384595NM BS 597 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 DURING C16 CHECK DISCOVERED CLIP CRACKED, .6 INCHES, IN CABIN INTERIOR AT BS 597 AND STR 8L. MAINTENANCE REMOVED CLIP AT BS 597 AND STR 8L IAW BOEING 737-300 SRM 51-40-02-0G FIG 8. RECEIVED NEW CLIP AND INSTALLED AT BS 597 AND STR 8L IAW BOEING 737-300 SRM 51-40-02-0G FIG 3 AND 4. 2L72 4F RTA16WE 20051114000222005111400022NM 2005 11 14 AWXA200501347 120051011A5340693535214 CLIP BOEING737 7373G7 1384595NM BS 616 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 DURING C16 CHECK DISCOVERED CLIP CRACKED, .375 INCHES, IN CABIN INTERIOR AT BS 616 AND STR 4R. MAINTENANCE REMOVED CLIP AT BS 616 AND STR 4R IAW BOEING 737-300 SRM 51-40-02-0G FIG 8. RECEIVED NEW CLIP AND INSTALLED AT BS 616 AND STR 4R IAW BOEING 737-300 SRM 51-40-02-0G FIG 3 AND 4. 2L72 4F RTA16WE 20051114000242005111400024NM 2005 11 14 AWXA200501349 120051011A534066235743 CLIP BOEING737 7373G7 1384595NM BS 685 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 DURING C16 CHECK DISCOVERED STRINGER CLIP CRACKED, .3 INCHES, AT BS 685 AND STR 11L. MAINTENANCE REMOVED CLIP AT BS 685 AND STR 11L IAW BOEING 737-300 SRM 51-40-02-0G FIG 8. RECEIVED NEW CLIP AND INSTALLED AT BS 685 AND STR 11L IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 3 AND 8. 2L72 4F RTA16WE 20051114000632005111400063WP 2005 11 14 IXXA05SMN224S 120051013A5330 RIVET DOUG DC8 DC871F 302199DWP FS 222 IMPROPER B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING C CHECK INSPECT, FWD LWR FUSELAGE BELLY, STA FS 222 L-34.75R. UPGRADE REPAIR DOUBLER TO INCORPORATE A MIN OF 3 ROWS OF RIVETS. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-1 FIG 7, EO SEMAN NR 20051194 DATED 09-20-05. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D. REMOVED DAMAGED SECTION IAW DC8 SRM 53-2-1 FIG 7 (SHEET 1, 3). NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D REPAIR DOUBLER (AL7075T6 0.080) + (02 EA) INTERNAL FINGER DOUBLERS (AL7075T6 0.050) IAW DC8 SRM 53-2-1 FIG 7 (SHEET 1, 3), DC8 SRM 53-4-1 FIG 1 ITEM “B”, DC8 SRM 51-9-0 FIG 68A, DC8 SRM 51-1-4 (FORMING). CLEANED, TREATED, PRIMED AREA + REPAIR PARTS IAW D2L74 4F RT4A25 20051114000652005111400065NM 2005 11 14 AWXA200501362 120051028A5320654585512 SUPPORT BOEING737 7373S3 1384711NM BS 967-980 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 DURING C13 CHECK DISCOVERED CORROSION ON 4 ZEE SUPPORTS FOR THE R2 DOOR SCUFF PLATE FROM BS 967 TO 980, WL 208.1 AND BL 62R. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-15-1A FIG 101. REMOVED AND FABRICATED 4 ZEE SUPPORTS IAW BOEING 737-300 SRM 51-40-02-0G AND BOEING DWG 65-45855. INSTALLED FABRICATED REPAIR PARTS FROM BS 967 TO BS 980, WL 208.1 AND BL 62R IAW BOEING 737-300 SRM 51-40-02G. 2L72 4F RTA16WE 20051114000672005111400067NM 2005 11 14 AWXA200501364 120051007A5340654583347 CLIP BOEING737 7373S3 1384711NM BS 178 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 DURING C18 CHECK DISCOVERED INTERCOSTAL ATTACH CLIP CRACKED, .5 INCHES, AT BS 178, WL 207 AND BL 26L. MAINTENANCE REMOVED AND INSTALLED NEW INTERCOSTAL ATTACH CLIP AT BS 178, WL 207 AND BL 26L IAW BOEING 737-300 SRM 51-40-05-06 FIGS 2 AND 4. 2L72 4F RTA16WE 20051114000692005111400069NM 2005 11 14 AWXA200501366 120051017A5320655486216 WEB BOEING737 7373S3 1384711NM BS 1020 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 DURING C18 CHECK DISCOVERED WEB CRACKED, 2.2 INCHES, AT BS 1020, WL 208 AND FROM BL 38R TO BL 39R. MAINTENANCE REMOVED AND INSTALLED NEW WEB AT BS 1020, WL 208 AND FROM BL 38R TO BL 39R IAW BOEING 737-300 SRM 51-40-02-0G FIG 12. 2L72 4F RTA16WE 20051114000712005111400071NM 2005 11 14 AWXA200501368 120051010A53206545834280 CHANNEL BOEING737 7373S3 1384711NM BS 271-279 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 DURING C18 CHECK DISCOVERED CORROSION ON THE FORWARD LAV, INBOARD, WALL LOWER ATTACH CHANNEL FROM BS 271 TO BS 279, BL 12L AND WL 209. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-10-51-1A1 FIG 101. FABRICATED NEW WALL SUPPORT CHANNEL IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5310-05295-ES3. INSTALLED FABRICATED REPAIR PARTS FROM BS 271 TO BS 279, BL 12L AND AWL 209 IAW AWA ER NR 03-5310-05295-ES3. 2L72 4F RTA16WE 20051114000732005111400073NM 2005 11 14 AWXA200501370 120051009A5315654581292 FLOORBEAM BOEING737 7373S3 1384711NM BS 328 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 DURING C18 CHECK DISCOVERED CORROSION ON CHORD LOCATED AT BS 328, WL 208 AND FROM BL 27R TO BL 56R. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-10-51-1A1 FIG 101. REMOVED DAMAGED SECTION OF CHORD IAW BOEING 737-300 SRM 53-10-51 REPAIR 5, FIG 201. FABRICATED CHORD IAW AMERICA WEST AIRLINES ENGINEERING REQUEST NR 03-5310-05295-ES2. INSTALLED FABRICATED REPAIR PARTS AT BS 328, WL 208 AND FROM BL 27R TO BL 56R IAW BOEING 737-300 SRM 53-10-51 REPAIR 5 FIG 201 AND AWA ER NR 03-5310-05295-ES2. 2L72 4F RTA16WE 20051114000752005111400075NM 2005 11 14 AWXA200501372 120051005A53136546877143 STRINGER BOEING737 7373S3 1384711NM BS 726 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 DURING C18 CHECK DISCOVERED STRINGER 18A CRACKED, 1.5 INCHES, AT BS 726. MAINTENANCE TRIMMED OUT CRACK IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NUMBER 03-5361-05307-ES1. FABRICATED FILLER, GUSSET AND RADIUS FILLER IAW AWA ER NO. 03-5361-05307-ES1. INSTALLED FABRICATED REPAIR PARTS IAW AWA ER NR 03-5361-05307-ES1. 2L72 4F RTA16WE 20051114000792005111400079NM 2005 11 14 05FDEA02883 120050914A5511ALC81212 SPAR DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25574FE 48499 HORIZ STAB RT NR 1 BARREL NUT BORE AREAS CORRODED. HORIZ STAB BARREL NUT BORE NR 1 RT REPAIRED IAW STABILIZERS, HORIZONTAL STABILIZER, BARREL NUT BORE REWORK/REPAIR AD 2003-22-08 - EA NR 1-5510-87628 ATTACHMENT 11. CLASSIFIED AS MAJOR REPAIR IAW FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20051114000832005111400083EU 2005 11 14 05FDEA03725 120051109A5347 SEAT TRACK AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 RT SEAT TRACK AT FS 53 NR 5 RT HAS CORROSION IN SCALLOPS REF N00613. REPAIRED SEAT TRACK SECTION IAW SRM 53-10-16 FIG 205. 2L72 4F RTA35EU 20051114000852005111400085EU 2005 11 14 05FDEA03726 120051109A5330 SKIN AIRBUS310 A310203 3930313EU BS 972 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 FOUND DENT IN FUSELAGE SKIN AT STA 972 FS 10 AT 12 O`CLOCK POSITION, REF N00688. COMPLIED WITH EA 6-5310-94491. 2L72 4F RTA35EU 20051114000942005111400094NM 2005 11 14 SWAA053546 120051109A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29336SW 23940 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT, LOWER CORNER. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051114001382005111400138EA 2005 11 14 COMA0560582 120051102A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT LOOSE A COMAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01796CA 7338 FLIGHT 4942 - EMERGENCY FLOOR PATH LIGHTS ARE INOP FROM ROW 8 AFT. SECURED LOOSE WIRE CONNECTOR. 2L72 4F RTA21EA 20051114001432005111400143EA 2005 11 14 COMA0560589 120051106A3397 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSDIRTY A COMAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01796CA 7338 FLIGHT 5594 - EMERGENCY FLOOR LIGHTS, ROW 8 AFT, ARE INOPERABLE. CLEANED WIRE CONNECTION. OPERATION NORMAL. 2L72 4F RTA21EA 20051114001452005111400145NM 2005 11 14 UPS05445732 120051108A541065B903604 LINK BOEING747 747123 1384873NM NR 4 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 NR 4 NACELLE REAR ENGINE MOUNT THRUST LINK, CRACK INDICATION REVEALED AT FWD END LUG UPPER EXIT LIMIT. NR 4 ENG REAR MOUNT THRUST LINK REPLACED PER EO B747-7120-22596-A WORK CARRIED OUT ON TASK CARD APPENDIX-I NR 4 ENG REMOVED AND INSTALLED (FOR ACCESS) AS PER UPS TASK CARD TC 5000. 2L74 4F A20WE 20051115000032005111500003NM 2005 11 15 NOCA1905 120051025A2930S271T4513 TRANSMITTER BOEING767 767300 1385204NM HYD SYSTEM INOPERATIVE G NOCAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA15760NA 26257 C- HYDRAULIC PRESSURE EICAS MESSAGE AND BOTH CENTER HYDRAULIC LOW PRESSURE LIGHTS ILLUMINATED, AFTER ACCOMPLISHMENT OF QRH NO HELP, CREW DECIDED TO RETURN BACK TO SNN. UNEVENTFUL LANDING WAS ACCOMPLISHED. TROUBLESHOOT SYSTEM AND FOUND CENTER HYDRAULIC AIR PUMP AUTO FUNCTION INOPERATIVE. ITEM DEFERRED PER MEL 29-11-4-1. CENTER HYDRAULIC SYSTEM TRANSMITTER REPLACED OPERATES NORMALLY. 2L72 4F RTA1NM 20051115000052005111500005NM 2005 11 15 CALA0500400 120051111A57540632024T3 SKIN BOEING737 737524 1384721NM NR 6 SLAT CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717620 27333 INSPECTION FOUND A 1" CRACK AROUND FASTENER HOLE IN RT WING NR 6 SLAT SKIN AT LOWER SURFACE 23 INCHES FROM O/B END. THE SLAT WAS REPAIRED IAW SRM 57-43-01. 2L72 4F RTA16WE 20051115000072005111500007NM 2005 11 15 CALA0500402 120051113A52306547952524B SKIN BOEING737 7373T0 1384582NM CARGO DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2759338 23576 INSPECTION FOUND A 1/2" CRACK IN AFT CARGO DOOR INNER SKIN AT LIGHTENING HOLE ABOVE DOOR HANDLE, STA 807-847. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5232-01068. 2L72 4F RTA16WE 20051115000132005111500013NM 2005 11 15 NOCA1505 120051001A2560ACREM1A MEGAPHONE BOEING767 767300 1385204NM FWD CABIN INOPERATIVE G NOCAK NONE O OTHER ININSP/MAINT 1 EA15768NA 29898 DURING CABIN CHECK, FWD GALLEY MEGAPHONE FOUND NOT WORKING. REPLACED BATTERIES FOR MEGAPHONE IN ACCORDANCE WITH AMM-25-63-02. MEGAPHONE OPERATES NORMALLY. 2L72 4F RTA1NM 20051115000392005111500039NM 2005 11 15 UPS05545744 120051015A5347BAC15202472 SEAT TRACK BOEING757 75724APF 1384969NM BS 1144 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01404UP 23726 FOUND UPPER LOBE SEAT TRACK I/B FLANGE CORROSION AT NUT PLATE HOLE STA 1144 RBL 23. REPAIRED PER SRM 53-00-52-2R FIG 201 AND GOODRICH ER NR 05-4696. 2L72 4F RTA2NM 20051115000482005111500048WP 2005 11 15 AALA20050730 120051105A324142807 CONTROL BOX DOUG DC9 DC982 3022082WP ANTI SKID SYS INOPERATIVE A AALAO OTHER J WARNING INDICATION DEDESCENT 1 SW21956U 49701 ORD - AFTER LANDING GEAR WAS EXTENDED THREE OUT OF FOUR ANTI-SKID LIGHTS ILLUMINATED. LEFT INBOARD LIGHT REMAINED OUT. CYCLED THE SYSTEM AND TESTED. NO CHANGE OF LIGHTS. LANDED ORD WITHOUT INCIDENT. FOUND ANTI-SKID CONTROL BOX INOPERATIVE. REPLACED ANTI-SKID CONTROL BOX. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051115000572005111500057SO 2005 11 15 SWIA200515831 120051109A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO EMERGENCY LIGHTSDISCHARGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07232SW9829 9829 120306 FOUND CENTER EMERGENCY LIGHTS INOP. REPLACED ELBP IAW AMM 33-50-02, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20051115000642005111500064WP 2005 11 15 UPS05845753 120051110A5230 SKIN DOUG DC8 DC873F 302199FWP CARGO DOOR DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 FOUND PIT 31 DOOR HAS "CREASE" AT 2 O'CLOCK POSITION. COMPLIED WITH HFEC INSP OF AREA. NO CRACKS DETECTED DEFERRED PER EO DC8-5230-23256-A (D313697). COLD WORKED SKIN IAW DC8 SRM 51-01-04. VERIFIED NO CRACKS EXIST INTERNALLY AND EXTERNALLY. DAMAGE NO FALLS WITHIN LIMITS IAW DC8 SRM 52-01-00 & 51-06-00. ALODINED AND PAINTED AREA IAW DC8 SRM 51-01-08B THIS CLEARS THIS DEFERRAL. 2L74 4F RT4A25 20051115000662005111500066 2005 11 15 NOCA2505 420051110A2565387 BULB BOEING757 75728A 1384976NM R1 DOOR INOPERATIVE G NOCAO OTHER L NO TEST TXTAXI/GRND HDL 1 EA15756NA 32448 R1 DOOR ARM SLIDE INDICATOR INOPERATIVE. RELAMPED R1 DOOR SLIDE ARM LIGHT SYSTEM OPERATES NORMALLY. 2L72 4F RTA2NM 20051115000682005111500068SO 2005 11 15 C2XA05CL088 120051019A3350276005 FUSE EMB 145 EMB145LR 3260212SO BATTERY PACK BLOWN A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2717560 145605 DURING ROUTINE MAINTENANCE, BOTH LEFT AND RIGHT EXTERNAL OVERWING EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE INSPECTED AND REPLACED THE FUSE IN THE NR 4 EMERGENCY BATTERY PACK. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20051115000822005111500082NE 2005 11 15 AWXA200501376 220051112A7250 BLADES AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE NR 2 ENGINE FAILED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28621AW 053 0075 CREW REPORTED ON CLIMB-OUT ECAM MSG ENG 2 STALL. PILOTS RAN QRH PROCEDURE & RAN ENGINE AT IDLE. STALL RETURNED WHEN THEY ADVANCED THRUST LEVER ABOVE IDLE. RETURNED & LANDED WITHOUT FURTHER EVENT. NR 2 ENGINE BOROSCOPED. HPC NR 6, BLADES BENT & OUT OF LIMITS IAW AMM 72-00-00-200-016. MX R & R NR 2 ENGINE IAW AWA TC R5M71302 & F5M71301. OPS & LEAK CHECKS GOOD. CONFIRMED FAULT. COMPRESSOR STALL OF THE NR 2 ENGINE CAUSED BY A BROKEN STAGE 6 BLADE. ENGINE INSPECTED TESTED & REPAIRED IAW EM 71/72-00-00/CD-EM E-V2500-1IA/A5 REV. 61. ENGINE SATISFACTORILY TEST IAW EM 71-00-00 TEST 10. 2L72 4F4 FRTA28NM E311NE 20051115000942005111500094SO 2005 11 15 C2XA05IA122 120051026A335020131A BATTERY EMB 145 EMB145EP 3260221SO EMERGENCY LIGHTSDISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW27159481102025 145056 IAH - DURING MAINTENANCE INSPECTION, SEVERAL EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20051115001012005111500101CE 2005 11 15 DXTA200501058 120051104A3260327 BULB CESSNA500 560CESSNA 2076750CE MLG INDICATOR BURNED E DXTAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL07300QS 5600322 LEFT MAIN LANDING GEAR LIGHT INOP. LIGHT FAILS DURING ROTARY TEST. DURING THE FLIGHT DID NOT GET THE GEAR HORN. CIRCUIT BREAKER DID NOT POP. TS SYSTEM TO BAD LIGHT BULB. REMOVED AND REPLACED BAD BULB. OPS CHECKED ROTARY TEST. SYSTEM OPS CHECKS SATISFACTORY AT THIS TIME. ALL WORK DONE IAW CE560MM 32-60-00. 2L72 4F RTA22CE 20051115001162005111500116NM 2005 11 15 SB05145 120051114A3350110049 CHARGER BOEING737 7373B7 1384580NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19395US 23317 PIT - MAINTENANCE REPORTED THE AFT CABIN EMERGENCY LIGHTS FROM SEAT ROWS 17 THROUGH 22 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY SUPPLY AND CHARGER IN THE AFT CABIN. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20051115001362005111500136WP 2005 11 15 ABXA050273 120051027A5330592032979 SKIN DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23974AX 47623 TWO 1/4" CRACKS IN FUSELAGE SKIN COMING OUT OF FASTENER HOLE AT FORWARD LOWER CARGO DOOR CUT-OUT UPPER FORWARD CORNER. REPAIRED AREA IAW SR 09530117. 2L72 4F A6WE 20051115001382005111500138WP 2005 11 15 ABXA050280 120051101A531599581871 FLOORBEAM DOUG DC9 DC941 302207NWP BS 1013 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23974AX 47623 FOUND FLOORBEAM AT STA 1013, RIGHT BUTT LINE 15 AT DOOR UPLATCH BRACKET CORRODED ON LOWER FLANGE. REPAIRED DAMAGED FLOORBEAM IAW DC-9 SSRM DWG K07411. 2L72 4F A6WE 20051115001442005111500144EA 2005 11 15 SWIA200515834 120051110A27604916405 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07962SW9133 9125 7859 RECEIVED IB GROUND SPL CAUTION MSG. REPLACED NR 2 SECU IAW MM 27-61-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051116000122005111600012NM 2005 11 16 05FDEA03778 120051111A5753 REPAIR BOEING727 727233 138408ANM FORE FLAP UNDAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25266FE 21672 FOUND REPAIR ON LT INBD FORE FLAP LEADING EDGE, 36 INCHES FROM OUTBD END. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT LT I/B FORE FLAP WAS DETERMINED TO BE IWA SRM 57-40-4 FIG 1, BASED ON AN EXTERNAL VISUAL EVALUATION WITH THE REPAIR INSTALLED. REPAIR CLASSIFIED AS MAJOR BASED ON GMM 6-2-100 CRITERIA. 2L73 4F RTA3WE 20051116000212005111600021NM 2005 11 16 AALA20050742 120051112A3350P2010031302 SIGN BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21690AA 25696 LAX - EMERGENCY EXIT SIGN AFT ROW ON RIGHT SIDE INOPERATIVE. REPLACED EMERGENCY EXIT ARROW SIGN AT AFT ROW ON RIGHT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20051116000332005111600033EU 2005 11 16 05FDEA03812 120051114A5410 RIB AIRBUS300 A300B4622R 3930312EU NR 1 PYLON CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25721FD 477 NR 1 PYLON FAIRING 475CL INNER BODY NR 5 AND NR 6 RIBS ARE CRACKED. 2L72 4F RTA35EU 20051116000352005111600035NM 2005 11 16 QXEA200501518 120051113A2730 WARNING LIGHT BOMBDRDHC8 DHC8402 1390042NM PITCH TRIM ILLUMINATED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09411QX 4055 SEA FLIGHT NR 2346 - PITCH TRIM CAUTION. MAINTENANCE C/W Q400 FIM TASK 27-30-00-810-803. PITCH TRIM LIGHT DOES NOT ILLUMINATE. C/W CLOSE OUT AFTER STEP 4A. CHECKS GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051116000442005111600044NM 2005 11 16 SWAA053575 120051113A575265C26485 TAB BOEING737 7373H4 1384600NM LT WING AILERON DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29336SW 23940 DURING SCHEDULED 1/4D CHECK, FOUND LT WING AILERON TAB DELAMINATED. REMOVED AND REPLACED AILERON TAB PER MM. 2L72 4F RTA16WE 20051116000462005111600046NM 2005 11 16 SWAA053577 120051113A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29336SW 23940 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, LBL 17. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051116000492005111600049NM 2005 11 16 SWAA053580 120051113A53206582671 WEB BOEING737 7373H4 1384600NM BS 665 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29336SW 23940 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE BEADED WEB CRACKED AT BS 665, RBL 39. REPAIRED BEADED WEB PER SRM. 2L72 4F RTA16WE 20051116000512005111600051NM 2005 11 16 SWAA053582 120051113A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29433LV 33716 EEPLS TRACK INOP AT FWD END. REMOVED AND REPLACED EEPLS SECTION PER MM. 2L72 4F RTA16WE 20051116000522005111600052NM 2005 11 16 SWAA053583 120051111A335007912 COVER BOEING737 7377H4 1384404NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29451WN 32495 EEPLS TRACK COVER BROKEN AT ROW 11. REMOVED AND REPLACED COVER PER MM. 2L72 4F RTA16WE 20051116000532005111600053NM 2005 11 16 AWXA200501377 120051010A53116516301 FRAME BOEING737 7373S3 1384711NM BS 188 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 DURING C18 CHECK DISCOVERED FRAME AT BS 188, WL 207A ND BL 33L CRACKED, 3.75 INCHES IN LENGTH. MAINTENANCE TRIMMED OUT CRACK AT BS 188 FRAME, WL 207 AND BL 33L IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5300-05309-DF1. MAINTENANCE FABRICATED ANGLE, FLOOR SUPPORT, FILLERS, STRAP, AND SHIMS IAW AWA ER NR 03-5300-05309-DF1. INSTALLED FABRICATED REPAIR PARTS AT BS 188, WL 207 AND BL 33L IAW AWA ER NR 03-5300-05309-DF1. 2L72 4F RTA16WE 20051116000542005111600054NM 2005 11 16 AWXA200501378 120051106A5347D53371110010 SEAT TRACK AIRBUSA319 A319132 3930340NM FR 45 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28813AW 1223 DURING C CHECK INSPECTION, DISCOVERED CORROSION ON SEAT TRACK AT FR 45+5" AND BL -Y765. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW AIRBUS 319 SRM 53-31-15 FIG 101. SEAT TRACK WAS REMOVED FROM FS 41 TO FS 47 AND -Y765 IAW AIRBUS 319 SRM 53-31-15. NEW SEAT TRACK INSTALLED FROM FS 41 TO 47 AND -Y765 IAW AIRBUS 319 SRM 53-31-15. 2L72 4F RTA28NM 20051116000552005111600055NM 2005 11 16 AWXA200501379 120051028A5322654583312 SHEAR TIE BOEING737 7373S3 1384711NM BS 188-196 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 DURING C13 CHECK, DISCOVERED SHEAR TIE CRACKED AT BS 188 THROUGH 196, BL 31R AND WL 207. MAINTENANCE REMOVED AND INSTALLED NEW SHEAR TIE AT BS 188 THROUGH 196, BL 31R AND WL 207 IAW BOEING 737-300 SRM 53-10-51-2R8 FIG 201. 2L72 4F RTA16WE 20051116000562005111600056NM 2005 11 16 AWXA200501380 120051028A5322654583311 SHEAR TIE BOEING737 7373S3 1384711NM BS 188-196 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 DURING C13 CHECK, DISCOVERED SHEAR TIE CRACKED AT BS 188 THROUGH 196, BL 31L AND WL 207. MAINTENANCE REMOVED AND INSTALLED NEW SHEAR TIE AT BS 188 THROUGH 196, BL 31L AND WL 207 IAW BOEING 737-300 SRM 53-10-51-2R8 FIG 201. 2L72 4F RTA16WE 20051116000582005111600058NM 2005 11 16 AWXA200501382 120051106A5347D5337112005 SEAT TRACK AIRBUSA319 A319132 3930340NM FR 45 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28813AW 1223 DURING C CHECK INSPECTION FOUND CORROSION ON SEAT TRACK AT FR 45 + 16" AND BL -Y1292. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW AIRBUS 319 SRM 53-31-15 FIG 101. REMOVED SEAT TRACK AND INSTALLED NEW SEAT TRACK FROM FS 41 TO FS 47 AND BL -Y1292 IAW AIRBUS 319 SRM 51-72-11. 2L72 4F RTA28NM 20051116000592005111600059NM 2005 11 16 AWXA200501383 120051108A5320D53112827201 DUMMY RAIL AIRBUSA319 A319132 3930340NM FR 15 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28813AW 1223 SAL - DURING C CHECK INSPECTION DISCOVERED CORROSION ON DUMMY RAIL LOCATED AT FS 15 + 8" AND Y503.2. NO ALLOWABLE DAMAGE LIMITS FOUND IN THE AIRBUS 319 SRM. MAINTENANCE REMOVED AND INSTALLED NEW DUMMY RAIL FROM FS 12 TO FS 16 AND Y503.2 IAW AIRBUS 319 SRM 51-72-11. 2L72 4F RTA28NM 20051116000612005111600061 2005 11 16 SWAA053584 420051113A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29453WN 29847 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051116000622005111600062 2005 11 16 SWAA053585 420051110A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29475WN 32474 DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051116000642005111600064NM 2005 11 16 SWAA053587 120051113A53116546550 FRAME BOEING737 7375H4 138449DNM AFT CARGO CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29502SW 24179 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT AFT CARGO DOOR CUTOUT, FWD FRAME AT NR 5 STOP FITTING. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20051116000652005111600065NM 2005 11 16 SWAA053588 120051111A53306545768 SKIN BOEING737 7375H4 138449DNM BS 304 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29503SW 24180 DURING WALKAROUND INSP, FOUND FUSELAGE SKIN CRACKED AT BS 304, STR 19R. REPAIRED SKIN PER SWA EA AND SRM. 2L72 4F RTA16WE 20051116000662005111600066 2005 11 16 SWAA053589 420051113A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29607SW 27927 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20051116000682005111600068NM 2005 11 16 SWAA053591 120051111A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 359 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 359, STR 8L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051116000692005111600069NM 2005 11 16 SWAA053592 120051111A5315BAC15171489 FLOORBEAM BOEING737 7373H4 1384600NM COCKPIT FLOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED D CHECK, FOUND COCKPIT FLOOR Z-CHORD CORRODED AT BS 270, BETWEEN LBL 6 TO RBL 11. REMOVED AND REPLACED Z-CHORD PER SRM. 2L72 4F RTA16WE 20051116000762005111600076WP 2005 11 16 UPS05845754 120051024A5340SAA38903881 FITTING DOUG DC8 DC873F 302199FWP FS 1570 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 FOUND SEVERE CORROSION ON SPLICE FITTING AND AROUND FASTENERS AT BS 1570, RBL 20 AS MARKED. REMOVED AND REPLACED FITTING IAW SRM 51-3-0 AND 51-3-2. 2L74 4F RT4A25 20051116000802005111600080NM 2005 11 16 SWAA053598 120051113A2560416A1531 STRAP BOEING737 7377H4 1384404NM EMERGENCY EXIT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29792SW 27887 DURING SCHEDULED 5Y CHECK, FOUND RT OVERWING EMERGENCY EXIT ESCAPE STRAP RETAINING STRAP MISSING. INSTALLED STRAP PER MM. 2L72 4F RTA16WE 20051116000812005111600081NM 2005 11 16 SWAA053599 120051113A53306518420 SKIN BOEING737 7377H4 1384404NM LWR FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29792SW 27887 DURING SCHEDULED 5Y CHECK, FOUND FUSELAGE SKIN CORRODED UNDER FWD AIRPHONE ANTENNA. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051116000832005111600083EU 2005 11 16 MALA050819 120051106A3020 CONTROL UNIT SAAB SF340 340B 7860101EU ANTI ICE SYS MALFUNCTIONED A MALAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL15362PX 340B258 LEFT INTAKE LIGHT ILLUMINATED IN FLIGHT. RECYCLED SWITCH PWE QRH. LIGHT WENT OUT AND REILLUMINATED AFTER APPROX 2 MINS. TROUBLESHOOTING FOUND ANTI-ICE CONTROL UNIT. REMOVED AND REPLACED ANTI-ICE CONTROL UNIT, SN ON 361, SN OFF 113. GROUND RAN A/C. ALL CHECKS GOOD. MX CONTROL NOTIFIED. 2L72 4T RTA52EU 20051116000842005111600084NE 2005 11 16 MALA050816 220051105A7261 WARNING LIGHT SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE ENG CHIP DETECT ILLUMINATED A MALAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL15421XJ 340B421 ON DEPT FROM DTW, THE CAPTAIN NOTICED A RT ENGINE CHIP DETECTOR LIGHT ON. FOLLOWED QRH, LIGHT WENT OUT, THEN CAME BACK 4 TIMES. RETURNED TO DTW. NO FURTHER INFORMATION AT THIS TIME. 2L72 4T4 TRTA52EU E8NE 20051116000862005111600086EU 2005 11 16 MALA050818 120051105A3020 VALVE BAC 146 AVRO146RJ85A1500097EU ANTI ICE SYS FAILED A MALAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL15502XJ E2307 INTAKE NR 4 LOW PRESSURE ILLUMINATED AFTER TAKEOFF AND WOULD NOT GO OUT AFTER RUNNING NON-NORMAL CHECKLIST. REMOVED AND REPLACED NR 4 INTAKE A-ICE VALVE. OPS CHECK GOOD. 2H74 4F RTA49EU 20051116000892005111600089EU 2005 11 16 MALA050821 120051108A2432 BATTERY BAC 146 AVRO146RJ85A1500097EU MASTER FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15532XJ E2366 BATTERY FAILED CAP CHECK. 2H74 4F RTA49EU 20051116000912005111600091NE 2005 11 16 MALA050823 220051108A7261 WARNING LIGHT SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE CHIP DETECTOR ACTIVATED A MALAO OTHER O OTHER UKUNKNOWN 1 GL15421XJ 340B421 ENGINE CHIP DETECTOR INDICATION. NO FURTHER INFORMATION AT THIS TIME. 2L72 4T4 TRTA52EU E8NE 20051116000932005111600093 2005 11 16 AWXA200501385 420051111A256560592101 BOTTLE AIRBUS320 A320232 3930326EU OVERWING SLIDE OUT OF LIMITS A AWXAK NONE O OTHER ININSP/MAINT 1 WP28603AW1641910839 661 DURING OVERNIGHT INSPECTION DISCOVERED RT OVERWING SLIDE INFLATION BOTTLE PRESSURE IS OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED THE RT OVERWING SLIDE BOTTLE IAW AIRBUS 320 MM 25-62-46-04. UNIT WAS OVERHAULED IAW CMM 25-65-17 REV. 11. VENDOR DID NOT CONFIRM FAILURE OF THE UNIT IN THE TEARDOWN REPORT. 2L72 4F RTA28NM 20051116000952005111600095NM 2005 11 16 AWXA200501387 120051113A27512061141 INDICATOR BOEING737 7373G7 1384595NM TE FLAPS FAILED A AWXAO OTHER P NO WARNING INDICATION APAPPROACH 1 WP28309AW2070 2070 24711 PHX - FLIGHT CONTROL - CREW REPORTED ASYMMETRIC TRAILING EDGE FLAPS DURING APPROACH. ONE FLAP WAS AT APPROXIMATELY 25 DEGREES AND OTHER FLAP AT APPROXIMATELY 30 DEGREES. THERE WAS NO ROLL MOTION. MAINTENANCE REMOVED AND REPLACED THE FLAP POSITION INDICATOR IAW AMERICA WEST AIRLINES TASK CARD R1B27 001. OPERATIONAL CHECKS WERE GOOD. VENDOR TEAR DOWN REPORT CONFIRMS FAILURE. FOUND THE LEFT POINTER STICKING AND FAILED TEST NO. 5. REMOVED AND REPLACED THE DIAL ASSY AND INCORPORATED MOD B PER SB 2016-27-4. OPERATIONAL TESTS AND RECERTIFICATION DONE IAW CMM 27-50-03 REV 2. 2L72 4F RTA16WE 20051116000962005111600096NM 2005 11 16 QXEA200501517 120051112A6123 CONNECTOR DHAV DHC8 DHC8202 2809007NM AUTOFEATHER SYS DIRTY A QXEAD RETURN TO BLOCK L NO TEST TXTAXI/GRND HDL 1 NM09366PH 510 PDX FLIGHT NR 2149, ON TAXI OUT FOR TAKEOFF, NR 1 AUTOFEATHER TEST FAILED TO TEST. MAINTENANCE CHECKED FOR 28 VOLTS AT NR 1 FEATHER VALVE, NO DEFECTS NOTED. REMOVED, CLEANED AND RESEATED CONNECTORS AT NR 1 ENGINE TSCU. COMPLIED WITH NR 1 AUTO FEATHER TEST IAW DHC-8 200 MM 71-00-00-868-027. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051116000992005111600099NM 2005 11 16 05FDEA03772 120051111A5310 REPAIR BOEING727 727225 1384077NM BS 720-720B IMPROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 FOUND EXISTING STRINGER REPAIR IN FWD CARGO BAY AT BS 720 10" - BS 720B 15", S27R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EVALUATED EXISTING REPAIR STR 27R BS 720B 15 AND DETERMINED THAT THIS EXISTING REPAIR DOUBLERS HAD THE CORRECT NUMBER OF FASTENERS PER ROW HOWEVER THIS INCORRECT FASTENERS WERE INSTALLED PER SRM 53-10-3 FIG 1 SHT 1-4. REMOVED EXISTING FASTENERS IN REPAIR AND INSTALLED CORRECT FASTENERS IN EXISTING REPAIR IAW SRM 51-30-2 AND SRM 53-10-3 FIG 1 MAJOR REPAIR 2L73 4F A3WE 20051116001022005111600102WP 2005 11 16 05FDEA03799 120051114A5312 REPAIR DOUG DC10 DC1010 3022110WP BS 275 PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 FOUND FWD PRESSURE BULKHEAD STA 275 LT HAND SIDE FOUND REPAIR DOUBLER BETWEEN X 13, X28 AND Z-14, Z-27.7 BEAMS. PERFORMED A GVI OF DOUBLER IAW CONTINENTAL AIRLINES EC/RA #253C037 AND FEDEX EA#8-5310-79443B AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO#8-5100-7-5001. 2L73 4F A22WE 20051116001042005111600104NM 2005 11 16 05FDEA03781 120051111A5510 REPAIR BOEING727 727233 138408ANM HORIZONTAL STAB PROPER A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25266FE 21672 FOUND REPAIR ON LT HORIZONTAL STAB LEADING EDGE 40" FROM THE INBD END. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR ON LT HORIZONTAL STAB LEADING EDGE 40" FROM INBD END, WAS DETERMINED TO BE IAW SRM 55-10-3 FIG 2. REPAIR CLASSIFIED AS MAJOR BASED ON GMM 6-2-100 CRITERIA. 2L73 4F RTA3WE 20051116001052005111600105NM 2005 11 16 05FDEA03782 120051111A5330 REPAIR BOEING727 727233 138408ANM BS 740 PROPER A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25266FE 21672 FOUND REPAIR AT STA 740 STR 3R, REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT STA 740 STR 3 WAS DETERMINED TO BE IAW SRM 53-30-3 FIG 5 BASED ON AN EXTERNAL VISUAL EVALUATION WITH REPAIR INSTALLED. REPAIR IS CLASSIFIED AS MAJOR BASED ON GMM 6-2-100 CRITERIA. 2L73 4F RTA3WE 20051116001062005111600106NM 2005 11 16 05FDEA03783 120051111A5330 REPAIR BOEING727 727233 138408ANM BS 700 IMPROPER A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25266FE 21672 REPAIR AT STA 700 STR 29R-STR 29L. NOT ACCOMPLISHED USING FAA DATA FEDEX GMM 6-2-100 MAJOR REPAIR.(REF:N00637). REMOVED EXISTING REPAIR IAW SRM 51-30-2 SH1. DRILLED NEW HOLES IAW SRM 53-30-3 FIG 1 SH 8, FABRICATED NEW FILLER AND DOUBLER RESPECTIVELY FROM 2024 T3 .050 BATCH NR 999692 AND 2024 T3 .036C BATCH NR 1005831IAW SRM 53-30-3 FIG 1 SH 8. INSTALLED REPAIR PARTS IAW SRM 51-30-2 SH1. REPAIR CLASSIFIED AS MAJOR. 2L73 4F RTA3WE 20051116001072005111600107WP 2005 11 16 05FDEA03784 120051112A5101 BLANKET DOUG DC10 DC1030 3023501WP ZONE 100 BURNED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25319 CAC LT SIDE BLANKET BURNED JUST UNDER NR 1 PNEUMATIC DUCT. 2L73 4F A22WE 20051116001082005111600108EU 2005 11 16 05FDEA03785 120051113A5754 ATTACH ANGLE AIRBUS300 A300B4622R 3930312EU NR 1 SLAT CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25721FD 477 LT WING IB FIXED L/E PNL IB SUPPORT WEB LWR ATTACH ANGLE HAS CRACK AT JUNCTION OF KRUEGER AND NR 1 SLAT. 2L72 4F RTA35EU 20051116001092005111600109NM 2005 11 16 05FDEA03786 120051113A5340 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 FOUND CENTER CARGO, STA 5-113 TO 1541 LONGERON 30 RT SPLICE CRACKED. REMOVED AS PER SRM 51-33-01 VOLUME II. NEW LONGERON SPLICE MACHINED AS PER DRAWING A5A7112 AND INSTALLED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051116001102005111600110NM 2005 11 16 05FDEA03787 120051113A5320 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 FOUND CENTER CARGO STA 5-113 TO 1541 LONGERON 38R SPLICE CRACKED. REMOVED AS PER SRM 51-33-01 VOLUME II. NEW LONGERON SPLICE MACHINED AS PER DRAWING A5A7114 AND INSTALLED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051116001112005111600111NM 2005 11 16 05FDEA03788 120051113A5320 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 FOUND CENTER CARGO, STA 5-113 TO 1541 LONGERON 38L SPLICE CRACKED. CRACKED LONGERON SPLICE AT CENTER CARGO STA 5-113 TO 1541 LONGERON 38L REMOVED AND REPLACED WITH NEW FABRICATED SPLICE AS PER DRAWING A5A7114 AND INSTALLED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2L73 4F RTA22WE 20051116001122005111600112NM 2005 11 16 05FDEA03789 120051113A5320 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 FOUND CENTER CARGO, STA 5-113 TO 1541 LONGERON 44R SPLICE CRACKED. CRACKED SPLICE AT CENTER CARGO STA 5-113 TO 1541 LONGERON 44R REMOVED AND REPLACED WITH NEW LONGERON SPLICE AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2L73 4F RTA22WE 20051116001142005111600114NM 2005 11 16 05FDEA03801 120051114A5330 REPAIR BOEING727 72722 1384002NM BS 480 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 REPAIR AT BS 480 STR 26L TO 27L REQUIRES ENGINEERING DISPOSITION PER EO 7- 5100-7-5000 P3. COMPLIED WITH FED-EX EA 7-5330-95353. FOUND TO BE MAJOR REPAIR 2L73 4F A3WE 20051116001152005111600115WP 2005 11 16 05FDEA03802 120051114A5730 SKIN DOUG DC10 DC1030 3023501WP LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 LT WING L/E FOUND 1 CRACK 1'' LONG ON SKIN AT STA XORS 670. REPAIRED CRACK ON SKIN IAW SRM 57-10-00 FIG 68 SHT 1 AND IAW SRM 51-33-01 PAGE 34-47. 2L73 4F A22WE 20051116001162005111600116WP 2005 11 16 05FDEA03803 120051114A5310 REPAIR DOUG DC10 DC1030 3023501WP BS 1771 PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 MAIN CARGO COMPT AT STA 1771 X-27 Z-15 FOUND TRACK WITH FLUSH REPAIR 3''1/2 BY 2''. PERFORMED INSPECTION ON SEAT TRACK REPAIR IAW SRM 53-70-00 VOL 1 FIG 2A. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 E3 P2. 2L73 4F A22WE 20051116001172005111600117WP 2005 11 16 05FDEA03804 120051114A5310 REPAIR DOUG DC10 DC1030 3023501WP BS 1651 PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 IN MAIN CARGO COMPT AT STA 1651 X-47 Z-19 FOUND TRACK WITH FLUSH REPAIR 3''1/2 BY 2''. PERFORMED INSPECTION ON SEAT TRACK REPAIR IAW SRM 53-70-00 FIG 2A VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 E3 P2. 2L73 4F A22WE 20051116001182005111600118WP 2005 11 16 05FDEA03806 120051114A5310 REPAIR DOUG DC10 DC1030 3023501WP BS 910 PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 IN MAIN CARGO COMPT AT STA 910 X-47 Z-19 FOUND FLUSH REPAIR ON TRACK 3''1/2 BY 2''. PERFORMED INSPECTION ON SEAT TRACK REPAIR IAW SRM 53-70-00 FIG 2A VOL 1 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 E3 P2. 2L73 4F A22WE 20051116001192005111600119WP 2005 11 16 05FDEA03805 120051114A5310 REPAIR DOUG DC10 DC1030 3023501WP BS 1341 PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 IN MAIN CARGO COMPT AT STA 1341 X-47 Z-19 FOUND TRACK WITH FLUSH REPAIR 3''1/2 BY 2''. PERFORMED INSPECTION ON SEAT TRACK REPAIR IAW SRM 53-70-00 FIG 2A VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 E3 P2. 2L73 4F A22WE 20051116001202005111600120WP 2005 11 16 05FDEA03807 120051114A5754 REPAIR DOUG DC10 DC1030F 3023504WP NR 1 SLAT PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 LT WING SLAT NR 1 ON INT SKIN FOUND 1EA FLUSH DOUBLER 22'' BY 22'' AT STA XORS 80. PERFORMED INSPECTION ON SLAT NR 1 REPAIR DOUBLER IAW EA NR 8-5710-90122. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 E3 P2. 2L73 4F RTA22WE 20051116001212005111600121WP 2005 11 16 05FDEA03808 120051114A5210 REPAIR DOUG DC10 DC1030F 3023504WP BS 808 PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 FOUND UPPER FUSELAGE NR 2 LT DOOR FOUND EXTERNAL DOUBLER AT STA 808. PERFORMED INSPECTION ON REPAIR DOUBLER IAW SRM 52-10-00 FIG 12A VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 E3 P2. 2L73 4F RTA22WE 20051116001222005111600122WP 2005 11 16 05FDEA03809 120051114A5310 REPAIR DOUG DC10 DC1030F 3023504WP BS 775 PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 FOUND UPPER FUSELAGE LT SIDE FOUND DOUBLER REPAIR ON EXTERNAL SKIN AT STA 775 FROM LONG 23 TO LONG 24 Z 5. PERFORMED INSPECTION ON REPAIR DOUBLER IAW SRM 53-50-00 FIG 9 VOL 1 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 E3 P1. 2L73 4F RTA22WE 20051116001232005111600123WP 2005 11 16 05FDEA03810 120051114A5510 REPAIR DOUG DC10 DC1030F 3023504WP HORIZONTAL STAB PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 LT HORIZONTAL STABILIZER T/E FOUND NR 1 OLD REPAIR ON UPPER SURFACE AT XE 99.195. THE MEASURE 24'' LONG 5.5'' LARGE. PERFORMED INSPECTION ON SKIN REPAIR DOUBLER IAW EA NR 8-5510-63525, FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 E3 P2. 2L73 4F RTA22WE 20051116001242005111600124WP 2005 11 16 05FDEA03819 120051115A5310 REPAIR DOUG DC10 DC1010 3022110WP BS 1256 IMPROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 FOUND PASSENGERS DOOR 3 LT FOUND 1 EXISTING REPAIR ON FWD JAMB WEB AT STA 1256 BETWEEN LONG 26-27 LT SIDE. REMOVED EXISTING REPAIR, INSPECTED AREA, INSTALLED BUSHING REF EA NR 8-5310-92335. INSTALLED NEW DOUBLER P/N FC148913-3 PER SRM 53-50-00 FIG 19 VOL 1 AND EA NR 8-5310-92335. 2L73 4F A22WE 20051116001252005111600125WP 2005 11 16 05FDEA03820 120051115A5340 ANGLE DOUG DC10 DC1030F 3023504WP BS 1156 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 FOUND CENTER ACCESSORY COMPARTMENT FOUND 1 CRACK 3'' LONG ON T ANGLE, FRAME TO BULKHEAD ATTACH AT STA 1156 Z-29 X-107 RT SIDE. REMOVED FASTENERS FROM AEA0159 FRAME IAW SRM 51-33-01 PAG 34-47. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F160433-3 SPLICE PLATE, F160433-5 FILLER, F160433-11 FILLER, F160433-14 SPLICE ANGLE AND F160433-16 SPLICE ANGLE IAW SRM 53-30-00 FIG 7 VOL 1. REPAIRED FRAME IAW SRM 53-30-00 FIG 7. INSTALLED FASTENERS ON AEA0159 FRAME IAW SRM 51-33-01 PAGE 34-47. 2L73 4F RTA22WE 20051116001262005111600126WP 2005 11 16 05FDEA03821 120051115A5310 REPAIR DOUG DC10 DC1010 3022110WP BS 401-470 PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 FOUND EXTENSIVE DOUBLER REPAIR AROUND L-1 DOOR BETWEEN STA 401 AND 470.25 BOTTOM FWD AND AFT CORNERS ON FUSELAGE SKIN. PERFORMED A GVI OF EXISTING DOUBLER IAW FEDEX EA NR 8-5300-26224 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001. 2L73 4F A22WE 20051116001272005111600127WP 2005 11 16 05FDEA03822 120051115A5310 REPAIR DOUG DC10 DC1010 3022110WP BS 490-535 PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 FOUND FLUSH DOUBLER REPAIR RT SIDE BETWEEN STA 490 AND 535 JUST ABOVE OF FWD NOSE LANDING GEAR ON AN AREA OF ABOUT 43'' BY 21''. PERFORMED A GVI OF REPAIRS IAW CONTINENTAL AIRLINES EC/RA NO 253C042 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO#8-5100-7-5001. 2L73 4F A22WE 20051116001292005111600129NM 2005 11 16 05FDEA03730 120051108A2121 FAN BOEING727 727233 138408ANM CABIN FAILED A FDEAFBA ACTIVATE FIRE EXT. EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO25264FE 21626 STRONG FUMES IN COCKPIT AT FL 320 CRUISE FLT RAN EMERGENCY CHECKLIST AND LANDED AT KSWF. FOUND GASPER FAN C/B POPPED, RESET C/B AND IT POPPED AGAIN. SUSPECT BAD GASPER FAN. REMOVED AND REPLACED GASPER FAN IAW MM 21-23-011-4. 0PS CKS GOOD. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION OFF MFG 21520-1 POS ONL SRL 1834 TAG 8A0725 ON MFG 500702-4620 SRL AA24172 TAG 683835. 2L73 4F RTA3WE 20051116001302005111600130WP 2005 11 16 ABXA050270 120051110A3350L14440 LIGHT DOUG DC9 DC9* WP CABIN INOPERATIVE A ABXAK NONE O OTHER ININSP/MAINT 1 GL23817AX 45928 FOUND MAIN ENTRANCE DOOR EMERGENCY EXIT LIGHT INTERMITTENT. REMOVED AND REPLACED MAIN ENTRY DOOR LIGHT ASSEMBLY AS REQUIRED PER DC-8 MM. 2L72 4F A6WE 20051116001312005111600131WP 2005 11 16 ABXA050271 120051109A335060030451 POWER SUPPLY DOUG DC9 DC931 3022065WP EMERGENCY LIGHT INOPERATIVE A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23938AX 840 47009 EMERGENCY LIGHTS INOP. EMERGENCY BATTERY POWER PACK NEEDED REPLACEMENT, DEFERRED DI NR 46906 DEFERRED PER DC9 AMM 33-53-00-8 AND GMM 07-04. REPLACE POWER PACK ON OR BEFORE 3 FLIGHT DAYS CODE 2 CLEAR DI 46906. REMOVED AND REPLACED EMERGENCY LIGHT PWR SUPPLY IAW DC9 MM 24-30-00-2-0001 PARA "B" SYS, OPS CK GOOD PLACARD REMOVED. 2L72 4F A6WE 20051116001322005111600132WP 2005 11 16 ABXA050272 120051101A3510292617EA1 REGULATOR DOUG DC9 DC931 3022065WP OXYGEN SYS FAILED A ABXAO OTHER O OTHER CRCRUISE 1 GL23946AX 135 47003 DURING CRUISE FLT, F/O USED O2 MASK, THE REGULATOR FOR F/O'S O2 FAILED. WENT TO 100 PERCENT 02 UNDER PRESSURE (EMERG) NOTE: USED 200 LBS OF O2 UNTIL TURNING OFF F/O REGULATOR. REMOVED AND REPLACED F/O'S O2 REGULATOR AND OPS AND LEAK CHECKED GOOD IAW DC9 MM 35-10-01-2-0001. RESERVICED CREW MAIN OXYGEN IAW DC9 MM 12-05-00-3 TO 1800 PSI. 2L72 4F A6WE 20051116001332005111600133EU 2005 11 16 USAA051400 120051115A5320F5331532920000 SUPPORT ANGLE AIRBUS330 A330323 3930335EU FR 40 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19678US 388 FR 40 FROM Y-530 TO Y1065 CORRODED. REPLACED PART AS PER SRM 53-72-11, DEFECT SIZE: .25 INCH AREAS, 50 EA. 2L72 4F RTA46NM 20051116001352005111600135EU 2005 11 16 USAA051402 120051115A5320F53315312202 SUPPORT ANGLE AIRBUS330 A330323 3930335EU FR 39.1 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19678US 388 FR 39.1, Y1065 & Y-1065 CORRODED. REMOVED CORROSION AS PER SRM 51-74-00 PR SRM 51-74-00, 53-35-14 FIG 104, SHEET 3. DEFECT SIZE: .25 INCH AREAS, 20 EA. 2L72 4F RTA46NM 20051116001392005111600139EU 2005 11 16 USAA051399 120051115A5320F5331534420200 SUPPORT ANGLE AIRBUS330 A330323 3930335EU FR 44 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19678US 388 FR 44 Y725 - Y-493 CORRODED. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 53-35-14 FIG 104, 51-72-11. DEFECT SIZE: .063 INCH AT 12 EA AREAS. 2L72 4F RTA46NM 20051116001412005111600141NM 2005 11 16 USAA051389 120051115A5320 STIFFENER BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19518AU 23704 AFT END OF LT PACK BAY AT I/B AFT CORNER CRACKED. FABRICATED NEW ANGLE AND INSTALLED IAW SRM 51-10-02 BOEING DWG 65-45402. DEFECT SIZE: 1 INCH CRACK. 2L72 4F RTA16WE 20051116001432005111600143NM 2005 11 16 USAA051387 120051115A5330 SKIN BOEING737 7373B7 1384580NM BS 727D-727E CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19512AU 23595 STA 727D & 707E AT S-22L CRACKED. INSTALLED DOUBLER REPAIR PER SRM 53-00-01 FIG 201. DEFECT SIZE: TWO CRACKS MEASURING 1.45 INCH. 2L72 4F RTA16WE 20051116001452005111600145CE 2005 11 16 DXTA200501065 120051106A261172111211102 SMOKE DETECTOR CESSNA750 750 2076810CE CARGO BAY DEFECTIVE E DXTAO OTHER N FALSE WARNING DEDESCENT 1 GL07932QS 7500032 BAGGAGE SMOKE MASTER WARNING CAME ON DURING DESENT AT 2500 FT, CLEARED ITSELF AFTER CANCELLING THE MASTER WARNING. FUNCTIONAL TEST OF BAGGAGE SMOKE DETECTION CRACKED BAD. REMOVED AND REPLACED BAGGAGE SMOKE DETECTION WITH REPAIRED UNIT IAW CE750 M/M 26-14-00. OPS CHECK GOOD AT THIS TIME. 2L72 4J RTT00007WI 20051116001462005111600146CE 2005 11 16 DXTA200501066 120051107A21301103P0912 PRESSURE SWITCH CESSNA750 750 2076810CE CABIN PRESSURE FAILED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07966QS880 7500166 HP DUCT O'RESS ILLUMINATED DURING TAKEOFF ROLL. REPLACED BOTH LT & RT PRESSURE SWITCH'S DUE TO POSSIBLE INTERMITTENT OPERATION. OP'S OK IAW CE750 M/M 36-10-00. 2L72 4J RTT00007WI 20051116001482005111600148GL 2005 11 16 DXTA200501071 220051109A7421230626721 IGNITER CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL LT ENGINE INOPERATIVE E DXTAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TXTAXI/GRND HDL 1 GL07947QS776 7500047 CAE330168 DURING ENGINE START, LEFT ENGINE HUNG AT 33 PERCENT AND DID NOT START. FUEL HAD BLOWN OUT THE BACK. COMPLETED STEPS 1 THRU 8 OF TASK 72-00-00-810 IAW RR AE3007C FIM. REMOVED & REPLACED CHANNEL B IGNITER IAW RR AE3007C MM 74-21-10-000-802. 2L72 4J4 FRTT00007WITE6CH 20051116001502005111600150CE 2005 11 16 DXTA200501067 120051107A2810 VENT CESSNA750 750 2076810CE FUEL SYSTEM LEAKING E DXTAH DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL07999QS 7500203 AMBER CAUTION, WING TANK OVER FILL RT, INFLIGHT AND DID NOT EXTINGUISH WHILE VENTING FUEL UNTIL DESENT WAS INITIATED. INSPECTED FLOAT VALVE ON PANEL 642DB, FLAPPER VALVE ON 641DB, FUEL TRANSFER FLOAT VALVE, AND CENTER TANK FLOAT VALVE, CLIMB VENT LINE FLAPPER VALVE, WING FUEL TANK PRESSURE/VACUUM RELIEF VALVE, FUEL FLAPPER CHECK VALVE AND OUTBOARD FUEL TRANSFER FLOAT VALVE. NO DEFECTS NOTED. PERFORMED FUEL TRANSFER SYSTEM FLOW TEST AND FUEL TRANSFER SYSTEM SHUTOFF TEST. BOTH TEST WITHIN LIMITS. 2L72 4J RTT00007WI 20051116001512005111600151CE 2005 11 16 DXTA200501069 120051108A2120 SMOKE BEECH MU300 400A 1155402CE CABIN DETECTED E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07142QS RK432 SMOKE IN THE CABIN DETECTED DURING DESCENT FROM FL320 - FL240, PERSISTED AFTER ISOLATING BLEED AIR AND TURNING ANTI-ICE OFF. NON-ELECTRICAL SMOKE ODOR, BUT UNABLE TO ISOLATE SOURCE. ITEM IS UNDER INVESTIGATION. 2H72 4F RTA16SW 20051116001532005111600153CE 2005 11 16 DXTA200501073 120051110A3297 GROUND STUD CESSNA560 560XL 2076702CE MLG DAMAGED E DXTAO OTHER J WARNING INDICATION LDLANDING 1 GL07622QS 5605286 INFLIGHT UNLOCK LIGHT ILLUMINATED WITH 3 GREEN LIGHTS LEFT, GEAR WAS FLICKERING ON/OFF. ACCOMPLISHED CHECK LIST AND BLEW GEAR DOWN. T/S TO BAD GROUND ON LEFT MAIN GEAR ACTUATOR DOWNLOCK SWITCH GL007. REPAIRED WIRING TO GROUND, JACKED UP AIRCRAFT RESET EMERGENCY N2 GEAR BOTTLE. PERFORMED GEAR FUNCTION, ALL CHECKED GOOD. BLED HYD SYSTEM AND SERVICE HYD & N2 BOTTLE. WORKED DONE IAW 560 XL M/M 32-01-00. 2L72 4F RTA22CE 20051116001562005111600156NE 2005 11 16 DXTA200501077 220051111A720030358005D ENGINE CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE LEFT MALFUNCTIONED E DXTAO OTHER Y ENGINE STOPPAGE TXTAXI/GRND HDL 1 GL07390QS 5600490 PCEJCO453 LEFT ENGINE FAILED AFTER APPROXIMATELY 2-3 MINUTES OF GROUND RUN. PERFORMED ENGINE START UP AND GROUND RAN ACFT FOR 10 MIN. REPEATING PROCEDURE 3 TIMES. DURING RUNS SELECTED VARIOUS MODES OF OPS SUCH AS LT & RT BOOST PUMPS ON/OFF LOW & HIGH GRD IDLE. CABIN PRESS AND BLEED AIR ON/OFF OBSERVED ENG PARAMETER, INDICATORS GAUGES AND ANNUNCIATIONS. NO FAULTS NOTED, NO FAULTS OR ABNORMALITIES FOUND AT THIS TIMEWORK IAW 560 PILOT'S OP MANUAL. 2L72 4F4 FRTA22CE E25EA 20051116001572005111600157CE 2005 11 16 DXTA200501074 120051110A3240 LINE CESSNA500 560CESSNA 2076750CE BRAKES LEAKING E DXTAO OTHER S AFFECT SYSTEMS LDLANDING 1 GL07307QS 5600307 PIC'S BRAKES LOST PRESSURE DURING LANDING ROLLOUT. SIC'S BRAKES WORK NORMALLY. PERFORMED BRAKE BLEED PROCEDURE TO BOTH LT & RT BRAKES. BRAKES OPERATE NORMAL AT THIS TIME. ALL WORK DONE IAW CESSNA 560 MM 32-42-00. 2L72 4F RTA22CE 20051116001582005111600158CE 2005 11 16 DXTA200501076 120051111A3240 LINE CESSNA500 560CESSNA 2076750CE BRAKES LEAKING E DXTAO OTHER S AFFECT SYSTEMS LDLANDING 1 GL07379QS 5600479 BRAKING IS NOT NORMAL, HAVE TO APPLY MORE THAN NORMAL PRESSURE ON BRAKES, ALMOST STANDING ON THEM. BRAKES HAVE PRESSURE BUT FEEL SPONGY. BLED BRAKE SYSTEM. SERVICED RESERVOIR WITH 1 QT OF 500B-4. TAXIED AIRCRAFT. BRAKE OPERATION NORMAL. ALL WORK DONE IAW CITATION 560MM 32-42-00 AND 12-12-02. 2L72 4F RTA22CE 20051116001592005111600159NM 2005 11 16 ASAA0540375 120050803A5753 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU OB FORE FLAP DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02778AS 2086 25110 YXX - LT WING OB FORE FLAP, OB END DAMAGED. REMOVED DAMAGE, INSTALLED LWR FILLER, INSIDE DOUBLER ( FOR LOWER SKIN), CORE AND UPPER DOUBLER. (K) 2L72 4F4 FRTA16WE E21EU 20051116001612005111600161NM 2005 11 16 ASAA0540496 120050921A531165465292 FRAME BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAO OTHER O OTHER NRNOT REPORTED 1 NM02793AS 26880 PAE FRAME CRACKED BIN RAIL SUPPORT BETWEEN STR 8 AND 9 LT AT IB FASTENER. REPAIRED DAMAGED FRAME AT BIN RAIL SUPPORT IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051116001662005111600166EU 2005 11 16 SDR2005074 120051108A2750 COMPUTER AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE TE FLAPS MALFUNCTIONED A TRBAO OTHER J WARNING INDICATION APAPPROACH 1 SO29369AT 369 DURING APPROACH, CREW REPORTED A FLAP UNLOCK INDICATION. EMERGENCY DECLARED. AIRCRAFT LANDED SAFELY. VISUAL INSPECTION AND OPERATIONAL CHECK PERFORMED AND FOUND NO DISCREPANCIES. MULTIFUNCTION COMPUTER RERACKED. FUNCTIONAL CHECK FLIGHT CONDUCTED AND FOUND SATISFACTORY. (K) 2H72 4T4 TRTA53EU E20NE 20051116001762005111600176EU 2005 11 16 SDR2005071 120051029A5610NP1588C13 WINDSHIELD AEROSPATR72 ATR72212A 8680902EU PWA PW120 PW127 NE COCKPIT CRACKED A TRBAO OTHER O OTHER APAPPROACH 1 SO29536AT30 536 ON APPROACH, THE CAPTAIN WINDSHIELD CRACKED. CREW DECLARED EMERGENCY. REPLACED THE WINDSHIELD ASSY. (K) 2H72 4T4 TRTA53EU E20NE 20051116001772005111600177NM 2005 11 16 05FDEA03753 120051110A5310 REPAIR BOEING727 727225 1384077NM BS 385 IMPROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 EXISTING SPLICE REPAIR ON STR 15L BS 385, REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED EXISTING REPAIR AT BS 385 STR 15L. INSTALLED NEW REPAIR BS 385 STR 15L PER SRM 53-10-3 FIG 1 DETAIL II. MAJOR REPAIR. 2L73 4F A3WE 20051116001782005111600178NM 2005 11 16 05FDEA03767 120051111A5330 REPAIR BOEING727 727100 1384036NM BS 620-637 IMPROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 19081 EXISTING EXTERNAL REPAIR ON FUSELAGE BS 620-637 STR 27R-28R. REPAIR REQURIES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED REPAIR DOUBLER, FABBED AND INSTALLED NEW DOUBLER IAW SRM 53-30-3 FIG 1 MAJOR REPAIR 2L73 4F RTA3WE 20051116001792005111600179NM 2005 11 16 USAA051350 120051108A5310 FRAME BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19779AU 24996 FOUND FWD SERV DOOR CUTOUT FWD FRAME AT LOWER O/B CORNER OF FWD UPPER STOP FITTING CRACKED. TRIMMED OUT DAMAGE AREA AND FABRICATED NEW FRAME AND INSTALLED IAW SRM 51-40-02 AND SRM 51-40-03, DEFECT SIZE: 3/16" CRACK. 2L72 4F RTA16WE 20051116001802005111600180NM 2005 11 16 USAA051351 120051108A5320 CHANNEL BOEING737 7373B7 1384580NM BS 360 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND BS 360; S15L CRACKED. REMOVED CRACKED CHANNEL AND INSTALLED NEW CHANNEL IAW SRM 51-10-02, DEFECT SIZE: APPROX 1" CRACK. 2L72 4F RTA16WE 20051116001812005111600181NM 2005 11 16 USAA051352 120051108A5320 ANGLE BOEING737 7373B7 1384580NM BS 350 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND STA 350 AT STRINGER 16L CRACKED. REMOVED, FAB, HEAT TREATED AND INST NEW ANGLE IAW SRM 51-10-02, DWG 69-26555 JOB CARD J020-37-20, DEFECT SIZE: .250" CRACK. 2L72 4F RTA16WE 20051114000982005111400098NM 2005 11 14 SWAA053554 120051109A57556546451 SKI BOEING737 7373H4 1384600NM RT WING SPOILER DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED C3 CHECK, FOUND RT WING NR 6 SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PER MM. 2L72 4F RTA16WE 20051114001002005111400100NM 2005 11 14 SWAA053556 120051110A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 400 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 400, STR 2L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051114001022005111400102NM 2005 11 14 SWAA053558 120051110A531165C25229 FRAME BOEING737 7373H4 1384600NM BS 727E CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727E, STR 8L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051114001042005111400104NM 2005 11 14 SWAA053560 120051110A53116558280 FRAME BOEING737 7373H4 1384600NM BS 360 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, BETWEEN STR 19R TO STR 20R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051114001062005111400106NM 2005 11 14 SWAA053562 120051109A53306545774 SKIN BOEING737 7373H4 1384600NM BS 739D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29343SW 24151 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 739D, STR 19L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051114001082005111400108NM 2005 11 14 SWAA053564 120051110A53116560552 BUTTSTRAP BOEING737 7375H4 138449DNM BS 360 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29502SW 24179 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME BUTT STRAP CRACKED AT BS 360, BETWEEN STR 14R TO STR 15R. REMOVED AND REPLACED BUTT STRAP PER BFG ER. 2L72 4F RTA16WE 20051114001102005111400110NM 2005 11 14 SWAA053566 120051109A575465C26686 SKIN BOEING737 7375H4 138449DNM RT WING SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED C2 CHECK, FOUND NR 4 L/E SLAT LOWER T/E SKIN CRACKED. REPAIRED SLAT PER SRM. 2L72 4F RTA16WE 20051114001122005111400112NM 2005 11 14 SWAA053568 120051110A53106547980 CREASE BEAM BOEING737 7373H4 1384600NM BS 887-907 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED D-CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 887 TO BS 907, WL 208. REPAIRED CREASE BEAM WEB PER SRM. 2L72 4F RTA16WE 20051114001142005111400114NM 2005 11 14 SWAA053570 120051110A335010107451 SIGN BOEING737 7377H4 1384404NM L1 DOOR BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29779SW 27884 DURING SCHEDULED RON CHECK, FOUND L1 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM. 2L72 4F RTA16WE 20051114001152005111400115WP 2005 11 14 05FDEA03717 120051108A5753 SKIN DOUG DC10 DC1030 3023501WP ZONE 500 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25310FE 48299 LEFT WING INBD FLAP LOWER SKIN HAS SMALL DENTS. CHECKED DENT LIMITS IAW DC10 SRM 57-10-00 FIG 48 VOL I. FOUND TWO DENTS OUT OF LIMITS. REPAIRED DENTS AT XIFH 230-231 AND XIFH 278-280 IAW DC10 SRM 57-10-00 FIG 85 VOLI. 2L73 4F A22WE 20051114001162005111400116NM 2005 11 14 05FDEA03719 120051108A5315 FLOORBEAM BOEING727 727225 1384077NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 FOUND CORROSION ON FLOORBEAM STA 344,BL0-LBL30. REMOVED, FABRICATED, ALODINED. PRIMED AND PAINTED FLOORBEAM REPAIR AT STA 344 AT BL0-LBL30 ALL IAW FX SRZ 27-53007 AND B727 SRM'S 51-30-2,53-10-2 FIG 7 AND 51-20-151. 2L73 4F A3WE 20051114001172005111400117NM 2005 11 14 05FDEA03718 120051108A5330 SKIN BOEING727 727233 138408ANM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25265FE 21671 EXTERIOR FUSELAGE, RAM AIR DOORS ACTUATOR ACCESS PANEL HAS CORROSION ON LANDS BETWEEN STRINGER 28-L AND STRINGER 28-R AT STATION BS 720B. REMOVED CORROSION IAW B727 SRM 51-10-6,ORIGINAL MATERIAL AT AREA .090" MATERIAL REMAINING .053" FOUND OUT OF LIMITS IAW B727 SRM 53-30-1 FIGURE 1; REPAIRED AREA IAW FEDEX EA NR 7-5330-92586. "FUSELAGE SKIN-DOOR LAND FOR RAM ACCESS HAS CORROSION-REPAIR". 2L73 4F RTA3WE 20051114001182005111400118WP 2005 11 14 05FDEA03720 120051108A5230 ANGLE DOUG DC10 DC1030 3023501WP ZONE 800 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25310FE 48299 FOUND FWD LOWER CARGO DOOR FRAME AT FWD HINGE POINT ANGLE CRACKED. REMOVED AND REPLACED ANGLE IAW DC-10 SRM 51-33-01 VOL II MATERIAL ID 2024-T3 .040 BOEING DWG ADA 7118, PO 504475.2 FABED IAW DWG ADA 7118 PART MARKED IAW FEDEX GMM 7-0-1000. 2L73 4F A22WE 20051114001202005111400120EU 2005 11 14 05FDEA03750 120051110A5420 BRACKET AIRBUS300 A300B4622R 3930312EU NR 1 PYLON CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25721FD 477 NR 1 PYLON FAIRING 475CL RT FWD BRACKET CRACKED. 2L72 4F RTA35EU 20051114001222005111400122NM 2005 11 14 CALA0500392 120051109A5240147A85408 STRUCTURE BOEING737 737724 13844BYNM GE CFM56 CFM56* 13802NE STA 967-986.5 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2723708 28769 INSPECTION FOUND R-2 DOOR CHORD CORRODED AT STA 967-986.5, RBL 45. THE R-2 DOOR CHORD WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F4 FRTA16WE E2GL 20051114001242005111400124NM 2005 11 14 CALA0500394 120051109A5315BAC15181211 FLOORBEAM BOEING737 737724 13844BYNM GE CFM56 CFM56* 13802NE STA 986.5 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2723708 28769 INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, RBL 24 TO RBL 38. THE FLOORBEAM WAS REPAIRED IAW ECRA 5321-01312. 2L72 4F4 FRTA16WE E2GL 20051114001252005111400125NM 2005 11 14 SWAA053552 120051109A55236959227 BUSHING BOEING737 7373H4 1384600NM ELEVATOR TAB WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED C3 CHECK, LT & RT ELEVATOR TABS FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED LT & RT ELEVATOR TABS NR 1 HINGE BUSHINGS & HARDWARE PER MM. 2L72 4F RTA16WE 20051115000222005111500022EA 2005 11 15 COMA0560588 120051105A5610NP1393216 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A COMAA UNSCHED LANDING O OTHER CRCRUISE 1 SO01868CA139405703 7427 FLIGHT 5031 - COPILOT WINDSHIELD SHATTERED. REPLACED WINDSHIELD. 2L72 4F RTA21EA 20051115000302005111500030NM 2005 11 15 NOCA2005 120051028A3350767 BULB BOEING767 767300 1385204NM 4R DOOR INOPERATIVE G NOCAK NONE L NO TEST ININSP/MAINT 1 EA15760NA 26257 ROUTINE MAINTENANCE FOUND 4R EMERGENCY EXIT EXTERIOR LIGHT INOPERATIVE. RELAMPED 4R EMERGENCY EXIT EXTERIOR LIGHT, OPS CHECK OK. 2L72 4F RTA1NM 20051115000322005111500032NM 2005 11 15 UPS05545737 120051015A5347BAC15202472 SEAT TRACK BOEING757 75724APF 1384969NM BS 585 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01404UP 23726 FOUND MAIN DECK CARGO FLOOR SEAT TRACK HAS CORROSION BS 585, LBL24 WL208. REPAIRED PER SRM 53-00-52-2R. 2L72 4F RTA2NM 20051115000332005111500033NM 2005 11 15 UPS05545738 120051015A5347BAC15202472 SEAT TRACK BOEING757 75724APF 1384969NM FUSLEAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01404UP 23726 FOUND MAIN DECK CARGO TRACK RT FLANGE HAS CORROSION. REPAIRED PER SRM 53-00-52-2R AND GOODRICH ER NR 05-4696. 2L72 4F RTA2NM 20051115000402005111500040NM 2005 11 15 AALA20050728 120051105A25308803010000 OVEN BOEING777 777223 1385213NM GALLEY INOPERATIVE A AALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21787AL 30010 AFT GALLEY NUMBER 9 OVEN BEGAN SMOKING WHILE ON AND WARMING MEALS. FLIGHT ATTENDANTS REPORTED SMOKE SMELL AS ELECTRICAL SMELL. SMOKE AND SMELL STOPPED ONCE OVEN WAS TURNED OFF. REPLACED AFT GALLEY NUMBER 9 OVEN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20051115000452005111500045 2005 11 15 AALA20050727 420051018A2565D31393109 SLIDE BOEING757 757223 1384957NM LT WING DEPLOYED A AALAO OTHER W INADEQUATE Q C CRCRUISE 1 SW21636AM 24594 ON LANDING AT SJU, FOUND LEFT WING SLIDE DEPLOYED AND RAFT MISSING. AIRCRAFT WAS FERRIED TO TUL FOR REPAIRS. REPAIRED SLIDE COMPARTMENT AND DOOR FOR LEFT OVERWING SLIDE. REPLACED DAMAGED SLIDE MECHANISM PARTS AND SLIDE CARRIAGE. REPAIRED LEFT FLAP AND COMPOSITE FUSELAGE PANELS. INSTALLED NEW SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20051115000472005111500047WP 2005 11 15 AALA20050731 120051108A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21588AA 53251 LGA - FOUND TAILCONE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR TAILCONE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20051115000522005111500052EA 2005 11 15 SWIA200515826 120050626A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07446SW 7666 FOUND FS 280 LT FLOORBEAM OB ATTACH ANGLE LBL 9.0 CRACKED, ITEM FOUND AT C CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00. 2L72 4F RTA21EA 20051115000592005111500059EA 2005 11 15 SWIA200515833 120051106A2750766389L CONTROLLER CNDAIRCL600 CL6002C10 1390015EA FLAP/SLATS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07758SK 10222 "SLATS HALF SPEED" ON DPC. REPLACED SFECU 2 (RT SIDE) 27-51-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051115000672005111500067NM 2005 11 15 NOCA1705 120051001A5610141T485235 TRACK BOEING767 767324 1385203NM COCKPIT WINDOW DAMAGED G NOCAA UNSCHED LANDING O OTHER CLCLIMB 1 EA15767NA 27569 CAPTAINS SLIDING WINDOW OPENED ON ROTATION OUT OF JFK. CREW UNABLE TO CLOSE WINDOW IN FLIGHT. DUMPED FUEL AND RETURNED SAFELY TO JFK. REPLACED CAPTAINS SLIDING WINDOW AND LOWER TRACK, WINDOW OPERATES NORMALLY. IT COULD NOT BE DETERMINED IF WINDOW WAS LOCKED PRIOR TO TAKEOFF. 2L72 4F RTA1NM 20051115000692005111500069SO 2005 11 15 C2XA05IA117 120051015A335078241 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY EXIT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714904 145477 BNA - DURING MAINTENANCE INSPECTION, THE RIGHT EMERGENCY EXIT IDENTIFIER WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FIVE EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20051115000702005111500070SO 2005 11 15 C2XA05BT077 120051030A335020131A POWER SUPPLY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT FAULTY A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715973132274656 145159 BNA - CREW REPORTED, ON HEAD START, EXIT ROW OVERHEAD EMERGENCY LIGHTS WILL NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED NR 4 BATTERY POWER SUPPLY IAW EMB145 AMM NR 33-50-04, OPS CHECK GOOD. 2L72 4T RTT00011AT 20051115000782005111500078NM 2005 11 15 NOCA1005 120050627A335020131A BATTERY PACK BOEING767 767324 1385203NM EMERGENCY LIGHT INOPERATIVE G NOCAK NONE L NO TEST ININSP/MAINT 1 EA15767NA 27569 EMERGENCY LIGHTS OUT AT ROWS 18 HG THROUGH 27 HG. TROUBLESHOOT AND REPLACED BATTERY PACK AT SEAT 19HG, OPERATION CHECK NORMAL. EMERGENCY LIGHTS OUT AT L2 EXIT DOOR. TROUBLESHOOT AND REPLACED BATTERY PACK AT L2 JUMP SEAT OPERATION CHECK NORMAL. 2L72 4F RTA1NM 20051115000872005111500087EA 2005 11 15 COMA0560581 120051101A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ILLUMINATED A COMAA UNSCHED LANDING JW WARNING INDICATION INADEQUATE Q C CRCRUISE 1 SO01431CA 7472 FLIGHT 5118 - RT REVERSER UNLOCKED MESSAGE. RT REVERSER WAS PREVIOUSLY DEFERRED, FOUND CONNECTOR STILL CONNECTED. REMOVED AND STOWED CONNECTOR PER MEL. 2L72 4F RTA21EA 20051115000882005111500088EA 2005 11 15 COMA0560593 120051110A329717300233 WIRE HARNESS CNDAIRCL600 CL6002B19 1900309EA NLG FAULTY A COMAL ABORTED APPROACH J WARNING INDICATION DEDESCENT 1 SO01932CA 7038 FLIGHT 5530 - CREW DECLARED AN EMERGENCY ON APPROACH TO ABE DUE TO NOSE WHEEL STEERING FAIL MESSAGE. REPLACED THE STEERING WIRING HARNESS. 2L72 4F RTA21EA 20051115000922005111500092NM 2005 11 15 NOCA1105 120050905A25308201110000 OVEN BOEING757 75728A 1384976NM AFT GALLEY INOPERATIVE G NOCAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA15752NA 28174 SMOKE IN AFT GALLEY. FLIGHT ATTENDANTS AND CREW DETERMINED THAT THE SMOKE WAS ORIGINATING FROM BEHIND THE CONTROL PANEL OF NR 6 OVEN AND NOT FROM CONTENTS BEING COOKED. THE OVEN INSERT WAS REMOVED, CIRCUIT BREAKER FOR NR 6 OVEN PULLED AND POWER TO AFT GALLEY REMOVED. AIRCRAFT DIVERTED TO BOS AND EMERGENCY DECLARED. A NON-EVENTFUL LANDING WAS ACCOMPLISHED. OVEN WAS REMOVED AND INSPECTED OF THE CONNECTORS WAS ACCOMPLISHED OVEN BLOWER MOTOR WAS OVERHEATING. 2L72 4F RTA2NM 20051115000972005111500097CE 2005 11 15 DXTA200501062 120051105A324199122813 CASE CESSNA500 560CESSNA 2076750CE FILTER HOUSING CRACKED E DXTAD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 GL07328QS 5600428 BRAKE PRESS LOW AND ANTI-SKID INOP LIGHTS ON BEFORE LANDING, BRAKES INOP. PEDALS TO FLOOR ON LANDING, USED BOTTLE TO STOP. BRAKE FLUID COMING OUT ALL OVER NOSE WHEEL. REMOVED LEFT NOSE BAGGAGE FLOOR PANELS TO GAIN ACCESS TO ANTI-SKID SYS. FOUND ANTI-SKID SYS FILTER HOUSING CRACKED. CLEANED HYD FLUID AND REPLACED HOUSING. FILTER HOUSING LEAK CHECKED GOOD AND BLED BRAKES. AVIONICS EQUIPMENT REMOVED FOR ACCESS, OPS CHECKED GOOD. TAXI BRAKES CHECKED GOOD. REF 560 MM 32-42-00. 2L72 4F RTA22CE 20051115000992005111500099CE 2005 11 15 DXTA200501053 120051020A323099125374 CYLINDER CESSNA560 560XL 2076702CE RETRACT FAILED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07663QS3361 5605263 LANDING GEAR RETRACTION PROBLEM DURING TAKEOFF, RT MAIN GREEN DOWN LIGHT REMAINED ILLUMINATED (UNLOCK LIGHT NOT ILLUMINATED). PERFORMED LANDING GEAR WILL NOT EXTEND CHECKLIST AND BLEW GEAR DOWN WITH NITROGEN SYSTEM. REMOVED RT MAIN GEAR ACTUATOR DUE TO HIGH RESISTANCE IN DOWNLOCK SWITCH. INSTALLED RENTAL ACTUATOR IAW CE560XL M/M CH 32-30-04, OPS CHECKED GOOD IAW CE560XL M/M CH 32-01-00. DURING GEAR SWING AND BLOW DOWN ACTUATOR (RENTAL) WAS INSPECTED AND RETURNED TO SERVICE. 2L72 4F RTA22CE 20051115001102005111500110NM 2005 11 15 NOCA0105 120050307A3350276005 FUSE BOEING767 767324 1385203NM EMERGENCY LIGHT BLOWN A NOCAK NONE L NO TEST ININSP/MAINT 1 EA15767NA 27569 DURING ROUTINE MAINTENANCE (DAILY CHECK), CABIN EMERGENCY ESCAPE PATH LIGHTING SYSTEMS LOCATIONS 11AB THROUGH 27AB FAILED TO ILLUMINATE DURING TEST. TROUBLESHOT AND FOUND BAD FUSE AT BATTERY POWER SUPPLY. REPLACED FUSE AT POWER SUPPLY. SYSTEM OPERATIONAL CHECK NORMAL. 2L72 4F RTA1NM 20051115001112005111500111NE 2005 11 15 NOCA0405 220050415A73108062550 GOVERNOR BOEING757 75728A 1384976NM RROYCERB211 RB211524* NE RT ENG FUEL FLOWFAULTY G NOCAD RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TXTAXI/GRND HDL 1 EA15750NA 26277 OAK - ON PUSHBACK RT ENGINE SHUTDOWN 30 SECONDS AFTER START AIRCRAFT RETURNED TO GATE. TROUBLESHOT AND REPLACED RT ENGINE FUEL FLOWGOVERNOR. PRECAUTIONARY CHANGE OF RT ENGINE SPAR VALVE ACTUATOR. 2L72 4F4 FRTA2NM E12EU 20051115001152005111500115EU 2005 11 15 05FDEA03714 120051108A5347 SEAT TRACK AIRBUS310 A310203 3930313EU CABIN CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 FOUND MAIN DECK FRAME 45 TO 50 SEAT TRACK 4 LEFT HAS 4 AREAS OF EXFOLIATION, REF N00610. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-72-10. 2L72 4F RTA35EU 20051115001222005111500122EU 2005 11 15 SA05115 120051115A335032145410 EPSU AIRBUS320 A320214 3930316EU EMERGENCY LIGHT FAULTY A USAAK NONE L NO TEST ININSP/MAINT 1 EA19122US16775 1298 PHL - THE EMERGENCY LIGHTS FAILED THE SYSTEM TEST. MAINTENANCE REPLACED THE MIDDLE, RIGHT EMERGENCY POWER SUPPLY UNIT (FIN 12WL). OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20051115001342005111500134NM 2005 11 15 05FDEA03760 120051110A5753 HINGE FITTING DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 FOUND LEFT WING OUTBOARD FLAP INBOARD HINGE FITTING OUTBOARD NR 3 BOLT HOLE FOUND CORROSION. CORROSION REMOVED & REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-90056. 2L73 4F RTA22WE 20051115001482005111500148NM 2005 11 15 SWAA053571 120051111A531165C31240 FRAME BOEING737 7373H4 1384600NM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D CHECK, FOUND AFT CARGO DOOR CUTOUT, FWD FRAME CORRODED BETWEEN STR 24R TO STR 25R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051116000032005111600003NM 2005 11 16 05FDEA03792 120051113A5320 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 FOUND CENTER CARGO, STA 1701 TO 1721 LONGERON 51R SPLICE CRACKED. CRACKED LONGERON SPLICE AT CENTER CARGO STA 1701 TO 1721 LONGERON 51R REMOVED AND REPLACED WITH NEW LONGERON SPLICE AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2L73 4F RTA22WE 20051116000072005111600007NE 2005 11 16 05FDEA03797 220051114A7200 ENGINE DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE NR 3 MALFUNCTIONED A FDEAEA ENGINE SHUTDOWN UNSCHED LANDING ERJVIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 SO25578FE 48458 724032 ABOUT 2-3 MIN AFTER BLEED SHUTDOWN, CREW GOT STICK SHAKER, A/S ALT LOSS WITH NR 3 ENG VIBRATION. BROUGHT NR 3 THROTTLE TO IDLE AND VIBRATION REDUCED BUT STILL NOTICEABLE & NR 3 EVM TURB MONITOR WAS CLIMBING THRU 4 TOWARDS 5. ELECTED TO SHUTDOWN NR 3 ENG & VIBRATION STOPPED. NR 3 EGT ABOUT 50 DEGREES ABOVE NR 1 & 2, REV U/L INDICATOR ILLUMINATED IN EPR GAUGE. COMPLETED BOROSCOPE INSP OF HPT BLADES FOUND 32 BLADES WITH DAMAGE & 8 OF THOSE BLADES MISSING AT LEAST HALF OF BLADE. BLADES THAT ARE DAMAGED ARE FRAGMENTED IN NATURE. ALSO, DURING INSPECTION FOUND AFT COOLING DUCT THAT SURROUNDS HPT BROKEN IN TWO. REMOVED AND REPLACED ENGINE. 2L73 4F4 FRTA22WE E24NE 20051116000362005111600036NM 2005 11 16 05FDEA03814 120051114A5330 REPAIR BOEING727 727233 138408ANM BS 328 IMPROPER A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25266FE 21672 REPAIR AT STA 328 STR 20L, NOT ACCOMPLISHED USING FAA APPROVED DATA, DETERMINED TO BE A MAJOR REPAIR, IAW FEDEX GMM 6-2-100 (REF :N00649). REMOVED NON-CONFORMING DOUBLER, FABRICATED NEW DOUBLER IAW SRM 53-30-3 FIG 1 WITH 2024 T3 .050 BATCH NR 0000999692 AND INSTALLED IAW SRM 51-30-2 DETERMINED TO BE MAJOR REPAIR. 2L73 4F RTA3WE 20051116000382005111600038NM 2005 11 16 05FDEA03816 120051114A5712 RIB DOUG MD11 MD11 3023602NM LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 FOUND LEFT WING FIXED LEADING EDGE NR 16 TRACK INBOARD RIB CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01. 2L73 4F RTA22WE 20051116000402005111600040NM 2005 11 16 05FDEA03818 120051115A5210 SKIN BOEING727 727227 1384078NM PAX DOOR BENT A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 FOUND FORWARD ENTRY DOOR, UPPER AFT CORNER SKIN IS BENT OUTWARDS. REPAIRED FORWARD ENTRY DOOR UPPER AFT CORNER SKIN PER SRM 52-00-3. 2L73 4F A3WE 20051116000482005111600048NM 2005 11 16 SWAA053579 120051113A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM BS 747 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29336SW 23940 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SHEAR TIES CORRODED AT BS 747, RBL 8 AND RBL 14. REPAIRED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20051116000702005111600070 2005 11 16 SWAA053593 420051112A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29655WN 28400 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051116000712005111600071NM 2005 11 16 SWAA053594 120051112A532065458197 WEB BOEING737 7373A4 1384585NM BS 243.7 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED A1 CHECK, FOUND NLG W/W RT FWD SIDE WEB CRACKED AT BS 243.7, WL 168.5. REPAIRED WEB PER SWA EA. 2L72 4F RTA16WE 20051116000732005111600073NM 2005 11 16 SWAA053596 120051112A335065C27093 LIGHT BOEING737 7373Y0 1384671NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20051116000742005111600074EU 2005 11 16 UPS05145760 120051107A5310A53813379 CROSSBEAM AIRBUSA300 A300F4622R 3930360EU FR 50, RBL 20 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01136UP 0819 FOUND MAIN CARGO FS 50 RBL 20 FLOORBOARD BRACE CRACKED. REMOVED, FABRICATED AND REPLACED FLOORBOARD BRACE CROSSBEAM AT FS 50 RBL 20 PER DWG A53813379, SRM 51-40-00, SRM 53-15-15, SRM 51-20-10 AND SRM 51-23-10. 2L72 4F RTA35EU 20051116000792005111600079NM 2005 11 16 SWAA053597 120051111A2560PH22300L GLOWSTRIP BOEING737 7377H4 1384404NM CABIN DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29746SW 29798 DURING SCHEDULED RON CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP DAMAGED. REMOVED AND REPLACED STRIP PER MM. 2L72 4F RTA16WE 20051116000882005111600088EU 2005 11 16 MALA050824 120051109A3260 LIGHT SAAB SF340 340B 7860101EU NLG INOPERATIVE A MALAO OTHER P NO WARNING INDICATION NRNOT REPORTED 1 GL15412XJ 340B412 NOSE GEAR GREEN LIGHT DID NOT ILLUMINATE ON EXTENSION. 2L72 4T RTA52EU 20051116000902005111600090EU 2005 11 16 MALA050822 120051108A2432 BATTERY BAC 146 AVRO146RJ85A1500097EU MASTER FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15524XJ E2349 BATTERY FAILED CAP CHECK. 2H74 4F RTA49EU 20051116000922005111600092EU 2005 11 16 MALA050815 120051104A2910MS21902W6 COUPLING BAC 146 AVRO146RJ85A1500097EU HYD SYSTEM LEAKING A MALAA UNSCHED LANDING KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL15504XJ E2311 F/A REPORTED BURNING ANTI-FREEZE ODOR ROWS 8-9. INSPECT ON CABIN CONFIRMS ODOR BELIEVED TO BE HYD FLUID. INSPECT CABIN , HYD BAY, AIR COND AND EXTERIOR. VERIFIED LEAKAGE FROM RT BRAKE LINE ON RT MLG. REPLACED LINE. NO LEAKAGE NOTED FROM CABIN INTERIOR WITH PARTICULAR ATTENTION TO FS 25/26 AREA. RT AND LT HYD BAY, VERIFIED HYD LEAK AT FS 46 AREA BY NR 2 AC PACK. REPAIRED LEAK BY REPLACING UNION REF IPC 29-10-05-35. NO LEAKS NOTED AFTER UNION REPLACEMENT. RAN GREEN AND YELLOW HYD SYS TO FULL PRESS AND ACTUATED SPOILERS, AIRBRAKE, FLAPS AND BRAKES. ALL SYS OP NORM. OPS AC PACKS, RECIRC FANS AND VERIFIED NO ABNORMAL ODOR EXIST IN CABIN OR COCKPIT. VERIFIED GREEN AND YELLOW HYD SYS SERVICED TO AMM LEVELS.2H74 4F RTA49EU 20051116000942005111600094NM 2005 11 16 AWXA200501386 120051112A5210FE240221001 DIAPHRAGM AIRBUSA319 A319132 3930340NM DOOR ASSIST BOTTLEAKING A AWXAK NONE O OTHER ININSP/MAINT 1 WP28828AW 1552 PHX - EES - DURING OVERNIGHT INSPECTION, DISCOVERED THE L-1 DOOR ASSIST BOTTLE PRESSURE LOW, AT 300 PSI. MAINTENANCE SERVICED THE L1 DOOR ASSIST BOTTLE BUT FAILED LEAK CHECKS. REMOVED AND REPLACED THE L1 DOOR ASSIST BOTTLE DIAPHRAGM IAW AIRBUS 319 AMM 52-10-00-610-001. LEAK CHECKS GOOD. 2L72 4F RTA28NM 20051116001032005111600103NM 2005 11 16 05FDEA03780 120051111A5330 REPAIR BOEING727 727233 138408ANM BS 1020 PROPER A FDEAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO25266FE 21672 FOUND REPAIR AT STA 1020 STR 26L. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT STA 1020 STR 26L WAS DETERMINED TO BE IAW SRM 53-30-3 FIG 5, BASED ON AN EXTERNAL VISUAL EVALUATION WITH REPAIR INSTALLED. REPAIR CLASSIFIED AS MAJOR BASED ON GMM 6-2-100 CRITERIA. 2L73 4F RTA3WE 20051116001342005111600134NM 2005 11 16 USAA051388 120051115A5330 SKIN BOEING767 767201 1385125NM BS 727D CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19645US 23897 LBS 727D & LBS 727E, S-22L AND S-23L CRACKED. INSTALLED DOUBLER IAW BOEING SRM 53-00-01 FIG 201. DEFECT SIZE: 2 EACH CRACKS, 1.45 INCH AND 1 EACH CRACK 1.75 INCH. 2L72 4F RTA1NM 20051116001362005111600136NM 2005 11 16 USAA051403 120051115A53159C53461171 FLOORBEAM BOEING737 737301 1384611NM BS 986 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19592US 23937 MAIN CABIN FLOORBEAM TEE STA 986.5 RBL 20-30 CORRODED. REMOVED & REPLACED TEE PER TYP REP 53-60-01. DEFECT SIZE: 10 INCHES. 2L72 4F RTA16WE 20051116001372005111600137NM 2005 11 16 USAA051404 120051115A5320US5362012990 ANGLE BOEING737 737301 1384611NM CABIN FLOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19592US 23937 MAIN CABIN FLOOR BELOW FLOOR AT BS 616 LEFT SIDE CRACKED. REMOVED & REPLACED ANGLE, INSTALLED FILLER PER SRM 51-40-02 & TYP REP 53-62-01. DEFECT SIZE: .5 INCH. 2L72 4F RTA16WE 20051116001382005111600138NM 2005 11 16 USAA051405 120051115A53306545871114 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19592US 23937 FWD SERVICE DOOR BOTTOM HINGE CUTOUT SKIN CRACKED. FABRICATED DOUBLER & FILLER PER SRM 52-00-01, 52-10-01. DEFECT SIZE: .250 INCH. 2L72 4F RTA16WE 20051116001402005111600140EU 2005 11 16 USAA051391 120051115A5320F53315374200 SUPPORT ANGLE AIRBUS330 A330323 3930335EU BELLY FAIRING CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19678US 388 BELLY FAIRING SUPPORT FLANGE FR 42-44 CORRODED. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-72-11. DEFECT SIZE: .25 INCH AREAS 20 EACH. 2L72 4F RTA46NM 20051116001422005111600142NM 2005 11 16 USAA051406 120051115A575465C267022 SKIN BOEING737 737301 1384611NM RT WING LE FLAP PUNCTURED A USAAK NONE O OTHER ININSP/MAINT 1 EA19592US 23937 RIGHT WING LEADING EDGE ABOVE NR 4 LEADING EDGE FLAP, APPROX L/E STA 205 DENTED. REMOVED EXISTING REPAIR, CUT OUT DAMAGE, INSTALLED FILLER & DOUBLER PER EA 96961. DEFECT SIZE: .6"L X .4"W X .080"D, 2.5"L X 1"W X .100"D DENT & PUNCTURE, .75"L X .3"W. 2L72 4F RTA16WE 20051116001442005111600144CE 2005 11 16 DXTA200501079 120051111A3234 HANDLE CESSNA750 750 2076810CE MLG STUCK E DXTAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 GL07904QS 7500210 LANDING GEAR WOULD NOT RETRACT. HANDLE IS STUCK IN DOWN POSITION. ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20051116001472005111600147CE 2005 11 16 DXTA200501068 120051107A3230 WARNING LIGHT CESSNA750 750 2076810CE MLG ILLUMINATED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07984QS 7500084 GEAR UNLOCK LIGHT ILLUMINATED AFTER T/O AND GEAR SELECTED UP. GEAR WAS RECYCLED WITH SAME RESULT. IT SOUNDED LIKE THE DOORS WERE OPEN. ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20051116001602005111600160NM 2005 11 16 ASAA0540495 120050921A5320655384422 FLOOR SUPPORT BOEING737 737490 1384715NM GE CFM56 CFM56* 13802NE BS 727E CRACKED A ASAAO OTHER O OTHER NRNOT REPORTED 1 NM02793AS 28888 PAE - FLOOR SUPPORT CRACKED AT FRAME FASTENERS. REPAIRED CRACKED FLOOR SUPPORT IAW SRM. (K) 2L72 4F4 FRTA16WE E2GL 20051116001652005111600165SO 2005 11 16 GM05010 120051107A27411159SCC5005 ACTUATOR GULSTMGV GULFSTREAMGV3980116SO RROYCEBR700 BR700710A110 NE STAB TRIM INOPERATIVE E UG8AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL235102 551 CREW REPORTED RECEIVING A (FLAP STAB INOP) MESSAGE DURING CLIMB, AFTER SELECTING FLAPS TO THE UP POSITION. IT WAS DISCOVERED THAT THE HORIZONTAL STABILIZER ACTUATOR NO-BACK MECHANISM HAD TRIPPED CAUSING THE ACTUATOR TO OPERATE IN THE DOWN DIRECTION ONLY. INCORPORATION OF ASC145A, WHICH INTRODUCES AN IMPROVED ACTUATOR, WILL BE ACCOMPLISHED WHEN PARTS BECOME AVAILABLE, AS DEFINED INT HE ASC. CONDITION WAS CORRECTED BY RESETTING AND OPERATIONALLY CHECKING THE NO BACK DEVICE AS INSTRUCTED IN THE MM. FOLLOWING A SUCCESSFUL SERIES OF OPS CHECKS AS INSTRUCTED IN THE MM PROCEDURES. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4F4 FRTA12EA E00057EN 20051116001692005111600169NM 2005 11 16 ASAA0510289 120050909A5315654659212 FLOORBEAM BOEING737 737298C 1384490NM PWA JT8 JT8D17A 52049NE BS 927 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02745AS 20794 BSTA 927.0 RT WL 155 AND RBL 8.0, FLOOR SUPPORT RAIL EXFOLIATION CORROSION UNDER ANCHOR NUT. REPAIRED FLOOR SUPPORT RAIL AT BSTA 927.0 AT WL155 AND RBL 8.0 IAW SRM. (K) 2L72 4F4 FRTA16WE E2EA 20051116001712005111600171NM 2005 11 16 ASAA0510300 120050915A534065353512 STRINGER CLIP BOEING737 737298C 1384490NM PWA JT8 JT8D17 52049NE BS 500 PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02745AS 20794 FWD TIE CLIP AT BSTA 500 STR 19 RT FOUND PUNCTURED. REPLACED TIE CLIP AT BSTA 500, STR 19 RT WITH NEW REPAIR IAW SRM. (K) 2L72 4F4 FRTA16WE E2EA 20051116001882005111600188NM 2005 11 16 USAA051357 120051109A5340 STRINGER CLIP BOEING737 7373B7 1384580NM BS 343 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 CRACK FOUND STATION 343 AT STRINGER 11R. STRINGER TIE CLIP WAS FABRICATED IAW BOEING DRAWING 69-38939-5, DEFECT SIZE: .025. 2L72 4F RTA16WE 20051116001892005111600189NM 2005 11 16 USAA051358 120051109A5315 FLOORBEAM BOEING737 7373B7 1384580NM BS 328 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND CORROSION BS 328 AT RBL 15 AND 12. FABRICATED SPLICE ANGLES AND INSTALLED SPLICE ANGLES AND "T" CAP IAW SRM 53-10-51, DEFECT SIZE: 7" BY.65". 2L72 4F RTA16WE 20051117000012005111700001NM 2005 11 17 USAA051360 120051109A5320 INTERCOSTAL BOEING737 7373B7 1384580NM BS 312 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND CRACK BS312 BL0 CABIN FLOOR SUPPORT STRUCTURE. CUTOUT CRACKED AREA, FABRICATED AND INSTALLED REPAIR IAW SRM 51-70-11, DEFECT SIZE: .25". 2L72 4F RTA16WE 20051117000032005111700003NM 2005 11 17 USAA051385 120051115A53206517688U165 ANGLE BOEING737 7373B7 1384580NM BS 300-353 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 BS 300-353; ZEE ANGLE AT S-17L CORRODED. REPLACED WITH IDENTICAL PART, REMOVED CORRODED ZEE ANGLE WITH NEW IAW SRM 51-10-02 BOEING DWG 65-17688. DEFECT SIZE: APPROX 1 X 43 INCH CORRODED AREA. 2L72 4F RTA16WE 20051117000052005111700005NM 2005 11 17 USAA051383 120051115A53201135095 SUPPORT BOEING737 7373B7 1384580NM BS 294-312 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 STA 294-312, LBL 12 CORRODED. REPLACE INTERCOSTAL MEMBER AND T-FITTING IAW SRM 51-10-02. DEFECT SIZE: INTERCOSTAL HAS A 70 INCH AREA OF CORROSION. 2L72 4F RTA16WE 20051117000062005111700006NM 2005 11 17 USAA051382 120051115A5322 SHEAR TIE BOEING737 7373B7 1384580NM BS 727E CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 STA 727E BETWEEN STRINGER 27L TO 27R CORRODED. INSTALLED REPAIR PARTS PER SRM 53-00-07. DEFECT SIZE: 2 INCH LONG AREA OF CORROSION. 2L72 4F RTA16WE 20051117000072005111700007NM 2005 11 17 USAA051381 120051115A53401122388 ANGLE BOEING737 7373B7 1384580NM BS 787-847 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 RBL 13.80, STA 787-847 CORRODED. CUT OUT DAMAGED SECTION AND SPLICE IN NEW SECTION IAW SRM 53-00-53 FIG 201. DEFECT SIZE: 6 INCH CORROSION. 2L72 4F RTA16WE 20051117000082005111700008NM 2005 11 17 USAA051380 120051115A5310 DOOR FRAME BOEING737 7373B7 1384580NM CARGO DOORWAY CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 AFT CARGO DOOR FRAME AFT WEBBING CRACKED. FABRICATED AND INSTALLED NEW WEBBING IAW SRM 51-70-13. DEFECT SIZE: 1 INCH CRACK. 2L72 4F RTA16WE 20051117000102005111700010NM 2005 11 17 USAA051378 120051115A5320 FLOOR SUPPORT BOEING737 7373B7 1384580NM BS 500D CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 BS 500D BETWEEN 26L AND 26R CORRODED. REMOVED DAMAGED PART AND INSTALLED NEW ANGLE IAW SRM 53-30-53 AND SRM 53-00-53. DEFECT SIZE: CORROSION AREAS APPROXIMATELY 1 INCH IN DIAMETER. 2L72 4F RTA16WE 20051117000112005111700011NM 2005 11 17 USAA051377 120051115A5320 ANGLE BOEING737 7373B7 1384580NM BS 727D-807 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 LEFT TRANSITION ANGLE, STA 727D-807 CORRODED. FABRICATED NEW TRANS ANGLE AND INSTALLED IAW SRM 53-60-53, SRM 51-10-02. DEFECT SIZE: .500 INCH AREA CORROSION AT EACH FASTENER. 2L72 4F RTA16WE 20051117000132005111700013EA 2005 11 17 COMA0560601 120051111A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A COMAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 SO01957CA256094954 7109 FLIGHT 5728 - RIGHT FLIGHT SPOILER DEPLOYED DURING FLIGHT. REPLACED THE RIGHT FLIGHT SPOILER PCU. 2L72 4F RTA21EA 20051117000142005111700014NM 2005 11 17 AT0500042 120051025A2910 LINE BOEING717 717200 1383700NM HYD SYSTEM LEAKING A ZZDAB EMER. DESCENT KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 SO15910AT 55086 ON APPROACH INTO PHF, RIGHT HYD SYS LOW ALERT ON EAD FOLLOWED QRH EMERGENCY DECLARED, NORMAL LANDING OCCURRED WITH GEAR DOORS UP. FOUND RT O/B SPOILER ACTUATOR LINES LEAKING AT ACTUATOR B NUT SLEEVE. REPLACED BOTH LINES REF 20-10, RTS 27-60, SERVICED HYD SYS & LEAK CHECKED GOOD. 2L72 4F TRA6WE 20051117000192005111700019NM 2005 11 17 QXEA200501522 120051111A5420 COWL DOOR BOMBDRDHC8 DHC8402 1390042NM NR 2 ENGINE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX: NR 2 ENGINE NACELLE COWL DOOR 422BL REQUIRES PERMANENT REPAIR OF FWD EDGE CRACKS. MAINTENANCE REPAIRED IAW QX EA 6-71-157, RD 8/4-71-097, QX EA 6-71-222, PSM 1-84-7A, 51-00-06 AND Q400 AMM TASK 51-25-31-370-801. 2H72 4T RTA13NM 20051117000202005111700020WP 2005 11 17 UPS05845768 120051113A2731UNK TAB DOUG DC8 DC871F 302199DWP RT ELELVATOR BINDING A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE:N/A ON TAXI OUT, FOUND BINDING IN ELEV COLUMN MOVEMENT. RT ELEV CNTRL TAB BINDING FOUND PLAY (WEAR) BETWEEN DRIVE TUBE & CRANK-CONTROL TAB. NEED TO ACCOMPLISH A TEST OF THE ELEV & TAB PER MM 27-30-00. WORN BOLT HOLE IN CRANK & TORQ TUBE REPAIRED PER DC8-2730-23267-A. CONNECTED RT ELEV CNTL TAB PUSH ROD AFT BOLT, TIGHTENED & SAFT'D. RT ELEV CNTL TAB CRANK ASSY & O/B DRIVE TORQ TUBE REPAIR REF ABOVE EO&MM 27-30-02-2. GRD CHECKS GOOD. INSTALLED CRANK ASSY TO RT ELEV CNTL TAB O/B DRIVE TUBE REF MM 27-30-02-2&EO. INSTL'D RT ELEV CNTL TAB ACCESS DR. C/W ADJ/TEST ELEV & TAB. OPS GOOD. 2L74 4F RT4A25 20051117000222005111700022WP 2005 11 17 UPS05845770 120051023A523037540252 FITTING DOUG DC8 DC873F 302199FWP DOOR FRAME CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE:C1 A PIT A/C DOOR FRAME AFT SPIDER FITTING IS CRACKED L27R. REMOVED, FABRICATED AND INSTALLED SPIDER FITTING IAW 51-1-20D, 51-3-0, DWG 3754025. 2L74 4F RT4A25 20051117000232005111700023WP 2005 11 17 UPS05845771 120051017A53105772787 DOUBLER DOUG DC8 DC873F 302199FWP FS 260 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE:C1 MAIN CARGO COMP L11L STA 260 CARGO DOOR ANGLE CHAFED MARK. UPON REMOVAL OF REPAIR ANGLE, FOUND DOUBLER CRACKED. REMOVED DOUBLER, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DWG 5772787, SRM 53-2-0 FIG 1F AND 51-1-21. 2L74 4F RT4A25 20051117000242005111700024WP 2005 11 17 UPS05845772 120051023A52303754U25U1 FITTING DOUG DC8 DC873F 302199FWP FS 280 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE:C1 A PIT DOOR FRAME FWD SPIDER IS CRACKED STA 280 L27R. REMOVED AND REPLACED SPIDER FITTING IAW SRM 51-1-20D, 51-1-21. 2L74 4F RT4A25 20051117000262005111700026WP 2005 11 17 UPS05845774 120051005A5310 FINGER DOUBLER DOUG DC8 DC873F 302199FWP BS 920-940 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE:C2 FINGER DOUBLER CRACKED AT STA 920-940 LBL 60. REMOVED FINGER DOUBLER AT STA 920-940 LBL 60 IAW SRM 51-1-20D AND 51-3-0. FABRICATED AND INSTALLED FINGER DOUBLER AT STA 920-940 LBL 60 IAW SRM 53-07-03 FIG 004 AND SRM 51-1-21 SRM 51-1-20D. 2L74 4F RT4A25 20051117000282005111700028NM 2005 11 17 PIDA20050189 120051109A2910211C223296 PRESSURE SWITCH BOEING757 757200 1384950NM HYD SYSTEM MALFUNCTIONED A PIDAK NONE J WARNING INDICATION ININSP/MAINT 1 SO05801DM 26240 STAB TRIM MAINTENANCE MESSAGE ACCOMPANIED BY YAW DAMPER MESSAGE. REPLACED C-HYD SYSTEM PRESSURE SWITCH S10002 PER FIM 22-21-00 AND MM 29-11-19. SYSTEM OPS CHECKS GOOD. 2L72 4F RTA2NM 20051117000302005111700030EA 2005 11 17 COMA0570118 120051106A5730CC670100458 SKIN CNDAIRCL600 CL6002C10 1390015EA LT WING CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01369CA7328 10079 MINOR CORROSION ON WING PLANK AT FUEL PANEL ACCESS CUTOUT FOR PANEL 541AB/BB. ACCOMPLISHED MINOR REPAIR IAW BRAS EO 601R-57-7672. 2L72 4F RTA21EA 20051117000352005111700035SO 2005 11 17 C2XA05IA113 120051013A2120 ODOR EMB 135 EMB135LR 3260305SO COCKPIT DETECTED A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SW2724517 145332 XNA - FLIGHT 3028, THE CREW REPORTED A STRONG ELECTRICAL SMELL IN THE COCKPIT ON APPROACH. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT, AND MAINTENANCE INSPECTED THE AIRCRAFT, WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20051117000362005111700036EA 2005 11 17 COMA0560598 120051110A2752852D10019 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA RT INBD FLAP FAULTY A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01735CA8937 7267 FLIGHT 5244- EN ROUTE JFK-PIT RECEIVED A FLAP FAIL CAUTION MESSAGE AT ZERO DEGREES. FLIGHT LANDED SAFELY. REPLACED THE RIGHT INBOARD FLAP ACTUATOR. 2L72 4F RTA21EA 20051117000392005111700039NM 2005 11 17 AT0500041 120051110A33508039251 POWER SUPPLY BOEING717 717200 1383700NM EMERGENCY LIGHT INOPERATIVE A ZZDAK NONE L NO TEST ININSP/MAINT 1 SO15891AT 55043 ROWS 1 - 10 AND L1 AND R1 EXIT SIGNS INOPERATIVE. SWAPPED BATTERIES, NO HELP. REMOVED AND REPLACED POWER SUPPLY, CORRECTED PROBLEM. ALL LIGHTS WORK PROPERLY. 2L72 4F TRA6WE 20051117000452005111700045NM 2005 11 17 QXEA200501526 120051109A5730 ACCESS PANEL BOMBDRDHC8 DHC8402 1390042NM LT WING CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX: LT WING FUEL ACCESS APERTURE FOR PANEL 522BT HAS PITTING CORROSION ON FWD AND AFT SIDE. MAINTENANCE REPAIRED IAW RD 8/4-57-441, NDTM PART 6, 51-00-02, Q400 SRM 51-21-10, Q400 SRM 51-25-40 AND QX EO 6-57-317. 2H72 4T RTA13NM 20051117000462005111700046EU 2005 11 17 SA05113 120051113A304066642870 COMPUTER AIRBUSA319 A319112 3930323EU AVIONICS BAY FAILED A USAAH DEACTIVATE SYST/CIRCUITS A FLAME/FIRE NRNOT REPORTED 1 EA19711UW19643 1033 PHL FLT 894 EN-ROUTE PIT TO PHL. DURING THE FLIGHT, THE CAPTAIN'S FIXED WINDOW BECAME CRACKED WITH EVIDENCE OF ELECTRICAL ARCING. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 WINDSHIELD HEAT COMPUTER DUE TO A FAULT. ALSO, REPLACED THE CAPTAIN'S FIXED WINDOW DUE TO DAMAGE. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20051117000512005111700051EU 2005 11 17 USAA051395 120051115A5320F5331537320000 SUPPORT ANGLE AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19678US 388 CORROSION ON FLANGE. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 53-35-14 FIG 104, SHT 16, SRM 51-72-11. DEFECT SIZE: .25 INCH AREAS, 10 EA. 2L72 4F RTA46NM 20051117000522005111700052EU 2005 11 17 USAA051396 120051115A5320F533153920000 SUPPORT ANGLE AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19678US 388 CORROSION ON FLANGE AT FR 40 BETWEEN -Y530 TO Y1065. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 53-35-14 FIG 104, SHT 4, SRM 51-72-11. DEFECT SIZE: .25 INCH AREAS, 50 EA. 2L72 4F RTA46NM 20051117000532005111700053EU 2005 11 17 USAA051397 120051115A5320 FLOOR SUPPORT AIRBUS330 A330323 3930335EU FR 73-74 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19678US 388 BETWEEN FR 73-74, YA & YB; CORROSION LEVEL 1; TASK C534159-01. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-72-11. DEFECT SIZE: .125 X .030 INCH DEPTH. 2L72 4F RTA46NM 20051117000562005111700056 2005 11 17 BB05098 420051114A2210285T0015117 MODULE BOEING767 767200 1385120NM AUTOPILOT MALFUNCTIONED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19648US 23900 ON CLIMBOUT DURING FLAP RETRACTION GOT AILERON LOCKOUT EICAS MESSAGE FOLLOWED BY RUDDER RATIO EICAS MESSAGE. COULD NOT GET AUTO PILOT ENGAGED. MAINTENANCE REPLACED THE LEFT SAM MODULE. 2L72 4F RTA1NM 20051117000572005111700057NM 2005 11 17 QXEA200501527 120051109A5730 ACCESS PANEL BOMBDRDHC8 DHC8402 1390042NM LT WING CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX: LT WING FUEL ACCESS APPERTURE FOR PANEL 522AT HAS PITTING CORROSION ON FWD AND AFT SIDE. MAINTENANCE REPAIRED IAW RD 8/4-57-441, NTDM PART 6, 51-00-02, Q400 SRM 51-25-40 AND QX EO 6-57-317. 2H72 4T RTA13NM 20051117000632005111700063EA 2005 11 17 COMA0560600 120051110A2752853D10020 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA RT OUTBD FLAP FAULTY A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01735CA8929 7267 FLIGHT 5244 - EN ROUTE JFK-PIT RECEIVED A FLAP FAIL CAUTION MESSAGE AT ZERO DEGREES. FLIGHT LANDED SAFELY. REPLACED THE RIGHT OUTBOARD FLAP INBOARD ACTUATOR. 2L72 4F RTA21EA 20051117000642005111700064NE 2005 11 17 0501599943 220051106A7200 ENGINE DOUG DC9 DC931 3022065WP PWA JT8 JT8D15 52051NE NR 1 SMOKE A NWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL011308T576221008 47315 700477 AFTER TAKEOFF FLIGHT ATTENDANTS AND PASSENGERS COMPLAINED OF SMOKE IN THE CABIN. FLIGHT CREW RETURNED AIRCRAFT TO DEPARTURE AIRPORT. MAINTENANCE REPLACED ENGINE NR 1. 2L72 4F4 F A6WE E2EA 20051117000652005111700065SO 2005 11 17 C2XA05IA124 120051028A3320 INVERTER EMB 145 EMB145EP 3260221SO CABIN LIGHT FAILED A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW2714940 145033 LFT - FLIGHT 2272, THE CREW REPORTED A STRONG ELECTRICAL SMELL COMING FROM THE TOP OVERHEAD PANEL OF 1A. MAINTENANCE TROUBLESHOT AND PLACED THE LIGHT INVERTER ON MEL 33-20-00/1 CTL NUMBER 061359, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20051117000662005111700066 2005 11 17 QXEA200501516 420051011A2340 HANDSET DHAV DHC8 DHC8202 2809007NM INTERPHONE MALFUNCTIONED A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09361PH 516 PDX FLIGHT 2046 PILOTS CANNOT HEAR FLIGHT ATTENDANT THROUGH INTERPHONE. FLIGHT ATTENDANT CAN HEAR PILOTS JUST FINE. FLIGHT ATTENDANT AND PILOTS ARE ABLE TO MAKE PASSENGER ANNOUNCEMENTS JUST FINE. MAINTENANCE REPLACED HANDSET FOR FLIGHT ATTENDANT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051117000672005111700067 2005 11 17 RAIA00511016 420051111A2210 TRIM SYSTEM JETAIRJETSTMJETSTM4101 1500501EU ELEVATOR MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03568HK 41086 FLT - 3608 - BWI - MANUAL AND ELECTRIC TRIM INOP. MAINTENANCE DEFERRED ELECTRIC ELEVATOR TRIM PER MEL. MANUAL TRIM OPS CHECK OK. 2L72 4T RTA41NM 20051117000712005111700071 2005 11 17 PIDA2005O187 420051105A2210R159723 ACTUATOR BOEING737 7372K5 138448XNM MACH TRIM INTERMITTENT A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05249TR 22598 MACH TRIM INTERMITTENT. PLACED ON MEL 22-5. 11/07/2005: REPLACED MACH TRIM ACTUATOR PER MM 22-21-11. OPS CHECKS GOOD. 2L72 4F RTA16WE 20051117000732005111700073WP 2005 11 17 UPS05845779 120051005A53403755822512N FITTING DOUG DC8 DC873F 302199FWP BS 278 L35R CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE:C2 A-CROSS SLIDE DOOR TORQUE BOX, CORROSION ON LONGERON 35R FS 278. REMOVED BATHTUB FITTING AT STA 279 L35R-L36 IAW SRM 51-1-20D. INSTALLED NEW BATHTUB FITTING AT FS 279 L35R-L35 IAW SRM 53-04-01. 2L74 4F RT4A25 20051117000762005111700076WP 2005 11 17 UPS05845783 120051004A53115644011501 SPAR DOUG DC8 DC873F 302199FWP FS857 RBL26-46 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE:C2 PRESSURE PANEL AT STA 857 RBL 26 TO 46 REAR SPAR TO FUSELAGE ANGLE EXFOLIATED. REMOVED ANGLE CHORD AT STA 857 RBL 26 TO 46 IAW SRM 51-1-20D. LOCATED AND DRILLED RT UPPER AFT SPAR CHORD AND INSTALLED SPAR CHORD IAW SRM 51-1-20D AND SRM 53-2-05-0 FIG 16. 2L74 4F RT4A25 20051117000772005111700077WP 2005 11 17 UPS05845784 120051018A5310 DOOR FRAME DOUG DC8 DC873F 302199FWP CARGO DOOR MISREPAIRED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE:C2 AFTER REMOVAL OF MCD AFT LWR JAMB FOUND ADDITIONAL CUT OUTS NOT PER SRM OR SRO 8530027. FABRICATED AND INSTALLED -1, -3,DOUBLERS AND -5, -7 TRIPPLER AND -11, AND -13 FILLERS IAW UPS EO DC8-5330-23194-A, SAA SK 866-833270, BOEING MESSAGES 1-136046332-5, AND 1-136046332-7, AND FAA FORM 8100-9. 2L74 4F RT4A25 20051117000782005111700078NM 2005 11 17 QXEA200501534 120051115A5230 HANDLE BOMBDRDHC8 DHC8402 1390042NM CARGO DOOR UNSECURE A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09412QX 4059 ON FLIGHT 2362, FUSELAGE DOOR WARNING NEAR 18,00 FEET DURING CLIMB TO 20,000 FEET. SQUEAL FROM DOOR NOTED BY FLIGHT ATTENDANT, DECENDED TO 12,00 FEET AND CONDUCTED EMERGENCY CHECKLISTS. SUDDEN LOSS OF PRESSURIZATION WITH LOUD THUMP NOTED. DIVERTED TO SUN. EXAMINATION OF AFT CARGO DOOR SHOWED THE HANDLE IN THE POPPED RELEASE POSITION. MAINTENANCE INSPECTED AFT CARGO DOOR HANDLE LATCH PIN AND HOOK. NO DEFECTS NOTED. PERFORMED OPERATIONAL CHECKS OF THE AFT CARGO DOOR AND PRESSURIZED AIRCRAFT. NO DEFECTS NOTED. OPERATIONAL CHECKS GOOD. CAUTION AND WARNING DID NOT REOCCUR NOR LOSS OF PRESSURIZATION. PERFORMED GVI OF DOOR AND SURROUNDING STRUCTURE, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS2H72 4T RTA13NM 20051117000792005111700079NM 2005 11 17 QXEA200501521 120051113A6123697072003 GOVERNOR BOMBDRDHC8 DHC8402 1390042NM NR 1 ENGINE INOPERATIVE A QXEAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 NM09413QX3621 3621 4060 BIL - PDX, DIVERTED TO LWS AT FL 240 CRUISE, NR 1 ENGINE OIL PRESSURE BEGAN TO FLUCTUATE AND OIL PRESSURE DROPPED BELOW ALLOWABLE LIMITS AND ENGINE WAS SHUTDOWN. MAINTENANCE DOWNLOADED EMU AND SENT FILE TO TECH SERVICES FOR ANALYSIS. INSPECTED NR 1 ENGINE AND FOUND MAJOR OIL LEAK FROM OVER SPEED GOVERNOR CAUSING OIL PRESSURE LOSS. REMOVED AND REPLACED OVER SPEED GOVERNOR. SERVICED ENGINE WITH OIL. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051117000802005111700080EA 2005 11 17 COMA0560603 120051111A2752853D10020 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA RT TE FLAPS UNRELIABLE A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01735CA8929 5193 7267 FLIGHT 5244 - FLAPS FAIL CAUTION. REPLACED THE RT WING FLAP ACTUATORS. 2L72 4F RTA21EA 20051117000812005111700081EA 2005 11 17 COMA0560602 120051111A2750780513 CONTROL HANDLE CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01967CA111875028 7134 FLIGHT 5028 - FLAPS FAIL CAUTION. REPLACED THE FLAP CONTROL LEVER. 2L72 4F RTA21EA 20051117000822005111700082EA 2005 11 17 COMA0560604 120051111A492038004883 APU CNDAIRCL600 CL6002B19 1900309EA AFT SMOKE A COMAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO01779CA11698756 7306 FLIGHT 5343 - SMOKE IN COCKPIT. REPLACED THE APU. 2L72 4F RTA21EA 20051117000832005111700083EA 2005 11 17 COMA0560605 120051112A5240 DOOR CNDAIRCL600 CL6002B19 1900309EA POWER ACCESS OPEN A COMAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 SO01809CA 7366 FLIGHT 5531 - GROUND POWER ACCESS DOOR OPEN DURING FLIGHT. INSPECTED DOOR, FOUND SERVICEABLE, CLOSED DOOR. 2L72 4F RTA21EA 20051117000862005111700086EA 2005 11 17 QXEA200501533 120051115A5240MS214326FEE9 ROLLER CNDAIRCL600 CL6002C10 1390015EA SERVICE DOOR JAMMED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09609QX 10031 PDX - GALLEY SERVICE DOOR JAMMED. MAINTENANCE INSPECTED AND FOUND THE FORWARD UPPER ROLLER NOT SQUARE IN THE FRAME. UNJAMMED DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2L72 4F RTA21EA 20051117000872005111700087EU 2005 11 17 UPS05145765 120051108A5712A5724199320300 ANGLE AIRBUSA300 A300F4622R 3930360EU RT WING RIB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01136UP 0819 INSPECTION TYPE:1C RT WING KRUEGER BOX AREA CURVED DOUBLER ON 2ND RIB FROM FUSELAGE HAS A CRACK. REMOVED & REPLACED DOUBLER ON 2ND RIB FROM FUSELAGE PER SRM 51-40-21 & 51-40-00. 2L72 4F RTA35EU 20051117000892005111700089NM 2005 11 17 UPS05545775 120051115A5315 FLOORBEAM BOEING757 75724APF 1384969NM MAIN CARGO BAY CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01469UP 25485 INSPECTION TYPE:C CORRISOIN ON MAIN CARGO BAY FLOORBEAM BS 1200, BL-0 TO LBL 60. REPAIRED FLOORBEAM IAW GOODRICH ER 05-4846. 2L72 4F RTA2NM 20051117000912005111700091WP 2005 11 17 UPS05845763 120051017A5330 SKIN DOUG DC8 DC873F 302199FWP R1 DOOR CUTOUT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE:C1 R1 DOOR UPPER FWD CORNER OF CUT OUT IS A .5 INCH CRACK FROM FASTENER TO EDGE OF SKIN. FABRICATED AND INSTALLED DOUBLER, TRIPLER AND FILLER AT FWD UPPER CORNER OF R1 DOOR IAW SRM 53-2-0 FIG 14, 51-1-21 AND 51-3-0. 2L74 4F RT4A25 20051117000952005111700095NM 2005 11 17 ASAA0540446 120050908A575165C26911304 SKIN BOEING737 7374Q8 138447QNM RT AILERON GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND RIGHT AILERON GOUGED AT CUTOUT FOR INBOARD MOUNT. PREPPED DAMAGED AREA, APPLIED LAY-UP REPAIR IAW B737-400 SRM 51-70-03 REPAIR 10. (M) 2L72 4F RTA16WE 20051117000972005111700097NM 2005 11 17 ASAA0540451 120050912A5321654585569 FLOOR PANEL BOEING737 7374Q8 138447QNM FS 983 DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND FLOOR WEB AT RBL 45 BS 983 HAS ELONGATED HOLES. REMOVED DAMAGED PART, FABRCIATED AND INSTALLED REPAIR PIECES IAW 737-400 SRM 51-30-01 AND 51-40-2. (M) 2L72 4F RTA16WE 20051117001082005111700108NM 2005 11 17 ASAA0540475 120050918A552365C25746142A TAB BOEING737 7374Q8 138447QNM RT ELEVATOR GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND RIGHT ELEVATOR DAMAGED AT T/E, OUTBOARD OF TRIM TAB. PREPPED DAMAGED AREA, BONDED REPAIR IAW 737-400 SRM 51-70-04 REPAIR 11. (M) 2L72 4F RTA16WE 20051117001092005111700109NM 2005 11 17 ASAA0540458 120050914A532265465512 SHEAR TIE BOEING737 7374Q8 138447QNM FS 807 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND BS 807 SHEAR TIE CORRODED BETWEEN STRINGER 26-27 LEFT. REMOVED DAMAGED SECTION OF SHEAR TIE, FABRICATED SHEAR TIE AND REPAIR PARTS AND INSTALLED PARTS IAW B737-400 SRM 53-00-07 FIG 101 AND 53-00-07 FIG 201. (M) 2L72 4F RTA16WE 20051117001102005111700110NM 2005 11 17 ASAA0540442 120050908A57536546486456 WEDGE BOEING737 7374Q8 138447QNM TE FLAP GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND RIGHT INBOARD FLAP TRAILING EDGE WEDGE GOUGED IN TWO PLACES. REPLACED RIGHT INBOARD FLAP TRAILING EDGE IAW B737-400 SRM 51-40-5, AND 08. (M) 2L72 4F RTA16WE 20051117001122005111700112NM 2005 11 17 ASAA0540459 120050914A531565C3394111 FLOORBEAM BOEING737 7374Q8 138447QNM FS 312 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND FLOORBEAM AT BS 312 UPPER CHORD IS CORRODED. REMOVED CORRODED SECTION OF UPPER CHORD, FABRICATED AND INSTALLED REPAIR CHORD AND REPAIR PARTS IAW B737-400 SRM 53-10-51 FIGURE 201. (M) 2L72 4F RTA16WE 20051117001132005111700113NM 2005 11 17 ASAA0540444 120050908A532065C335821 SHEAR WEB BOEING737 7374Q8 138447QNM FS 989-992 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND SHEAR WEB CORRODED AT BS 989 LBL 35. REMOVED SHEAR WEB, FABRICATED AND INSTALLED REPLACEMENT PARTS IAW B737-400 SRM 53-60-1 AND 51-40-05. (M) 2L72 4F RTA16WE 20051117001172005111700117NM 2005 11 17 ASAA0540439 120050907A5320654580731 ANGLE BOEING737 7374Q8 138447QNM FS 289 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND ANGLE CRACKED AT BS 289, STRINGER 11R. REMOVED AND REPLACED CRACKED ANGLE WITH NEW PART IAW B737-400 SRM 51-40-2. (M) 2L72 4F RTA16WE 20051117001222005111700122NM 2005 11 17 ASAA0540462 120050915A5310651960337 CREASE BEAM BOEING737 7374Q8 138447QNM FS 360-385 DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND STRINGER 17 CREASE BEAM HAS SHORT EDGE DISTANCE FROM PREVIOUS REPAIR. REMOVED DAMAGED SECTION OF CREASE BEAM AND INSTALLED NEW SECTION OF CREASE BEAM IAW B737-400 SRM 53-00-01 FIG 201 AND SRM 51-40-02. (M) 2L72 4F RTA16WE 20051117001232005111700123NM 2005 11 17 ASAA0540464 120050915A575165C2591129A SKIN BOEING737 7374Q8 138447QNM LT AILERON DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND LEFT AILERON NOSE SKIN DAMAGED AT WS 574. PREPPED DAMAGED AREA, ACCOMPLISHED HOT BOND REPAIR IAW B737-400 SRM 51-70-05. (M) 2L72 4F RTA16WE 20051117001252005111700125EU 2005 11 17 ASAA0540516 220050929A7230 COMPRESSOR BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU ENGINE CONTAMINATED A ASAAC ABORTED TAKEOFF WB INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 NM02772AS 25105 OKC - FOUND TAKEOFF ROLL POWER SET, COCKPIT FILLED WITH SMOKE. TAKEOFF ABORTED LESS THAN 45 KTS. REMOVED SMOKE FUMES FROM CABIN PER B737-400 AMM 21-00-01 AND AMM SUPPLEMENT 72-00-00. PARTIAL WORK ACCOMPLISHED ON MIG-2C 057320. ENGINE COMPRESSOR WASH PERFORMED DURING OVERNIGHT MAINTENANCE. A SLIGHT RESIDUAL DETERGENT ODOR MAY BE EVIDENT DURING THE FIRST TAKEOFF OF THE DAY, BUT IS NOT HARMFUL AND WILL CLEAR FRO THE CABIN QUICKLY. (M) 2L72 4F4 FRTA16WE E21EU 20051117001282005111700128NM 2005 11 17 ASAA0540460 120050920A533065C3235713 SKIN BOEING737 7374Q8 138447QNM FS 385 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND DENT ON PREVIOUS REPAIR DOUBLER ON FUSELAGE SKIN STATION 385 ABOVE STRINGER 16 LEFT. REMOVED PREVIOUS REPAIR, FABRICATED REPAIR DOUBLER AND TRIPLER, INSTALLED REPAIR PIECES IAW B737-400 SRM 53-00-01 FIG 201. (M) 2L72 4F RTA16WE 20051117001312005111700131NM 2005 11 17 ASAA0540514 120050926A531565C339504 FLOORBEAM BOEING737 7374Q8 138447QNM FS 986.5 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND FLOORBEAM STATION 986.5 CORRODED ON UPPER CHORD. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PIECES IAW ASA EA 5310-02498. (M) 2L72 4F RTA16WE 20051117001332005111700133NM 2005 11 17 ASAA0540504 120050926A53206546881127 STRAP BOEING737 7374Q8 138447QNM FS 1152 GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND FUSELAGE SKIN STRAP AT BS 1150 STRINGER 20R GOUGED. REMOVED DAMAGED SECTION OF STRAP, FABRICATED AND INSTALLED REPAIR STRAP AND FILLER IAW ASA EA 5310-02499. (M) 2L72 4F RTA16WE 20051117001352005111700135NM 2005 11 17 ASAA0540508 120050926A57536546434336 SKIN BOEING737 7374Q8 138447QNM TE FLAP BENT A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND RIGHT INBOARD AFT FLAP T/E BENT. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW 737-400 SRM 51-90-10. (M) 2L72 4F RTA16WE 20051115001062005111500106CE 2005 11 15 DXTA200501059 120051104A3243991205017 MASTER CYLINDER CESSNA500 560CESSNA 2076750CE BRAKE ASSY FAILED E DXTAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07312QS1722 5600312 BRAKES ON CO-PILOT SIDE ARE SPONGY, AND WHEN TURNING OFF RUNWAY LEFT PEDAL WENT TO THE FLOOR. REPEAT WRITE-UP. REMOVED PILOT'S AND COPILOT'S LEFT AND RIGHT MASTER CYLINDERS DUE TO CYLINDERS BYPASSING AND INSTALLED OVERHAULED UNITS IN ALL LOCATIONS. BLED SYSTEM. OPS, LEAK, AND TAXI CHECKS GOOD. ALL WORK DONE IAW CHAPTER 32-42-02 OF THE 560 MM. ANTI-SKID CHECKS GOOD IAW 32-42-00 OF 560MM. PILOT'S LT REMOVED P/N: 9912050-17, SN: 0586. 2L72 4F RTA22CE 20051115001272005111500127NM 2005 11 15 05FDEA03764 120051111A5310 REPAIR BOEING727 727233 138408ANM FUSELAGE UNDAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25266FE 21672 FOUND REPAIR AT STA 380 STR 9L. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION, AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT STA 380 STR 9L WAS DETERMINED TO BE IAW SRM 53-30-3 FIG 4 , BASED ON AN EXTERNAL VISUAL INSPECTION WITH REPAIR INSTALLED. REPAIR IS CLASSIFIED AS MAJOR, BASED ON GMM 6-2-100 CRITERIA. 2L73 4F RTA3WE 20051115001392005111500139WP 2005 11 15 ABXA050275 120051028A532299577399 SHEAR TIE DOUG DC9 DC941 302207NWP BS 1021 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23974AX 47623 FOUND CRACK IN SHEAR TIE AT STA 1021 BELOW LONGERON 15 RIGHT. REMOVED AND REPLACED SHEAR TIE AT STA 1021 BELOW LONGERON 15 RIGHT IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20051115001462005111500146EA 2005 11 15 SWIA200515836 120051109A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07445SW 7651 THE 1ST OVERHEAD EMERGENCY LIGHT IN THE CABIN IS INOP. REPLACED CABIN CEILING EMERGENCY LIGHT IAW MM 33-51-16. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051116000112005111600011NM 2005 11 16 05FDEA03776 120051111A5754 REPAIR BOEING727 727233 138408ANM NR 5 SLAT UNDAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25266FE 21672 FOUND REPAIR ON RT NR 5 SLAT UPPER SURFACE. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT NR 5 RT SLAT WAS DETERMINED TO BE IAW SRM 57-50-3 FIG 1 SHT 6 AND 7, BASED ON EXTERNAL VISUAL EVALUATION WITH REPAIR INSTALLED. REPAIR IS CLASSIFIED AS MAJOR BASED ON GMM 6-2-100 CRITERIA. 2L73 4F RTA3WE 20051116000172005111600017NM 2005 11 16 05FDEA03771 120051111A5240 REPAIR BOEING727 727225 1384077NM SERVICE DOOR UNDAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 EXISTING FLUSH REPAIR ON FWD SERVICE DOOR BS 380 STR 9R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR FOUND NOT TO BE WITHIN COMPLIANCE WITH FAA APPROVED DATA, REMOVED FASTENERS FAB REPAIR DOUBLER INSTALLED FILLER WASHERS IN COUNTERSINKS CHEM TREATED AND PRIMED. SEALED, INSTALLED FASTENERS AND PAINTED WHITE REF SRM 52-00-3 FIG 4. BS 380 STR 9R ON FWD SERVICE DOOR THIS IS A MAJOR REPAIR. 2L73 4F A3WE 20051116000182005111600018WP 2005 11 16 05FDEA03811 120051114A5320 ANGLE DOUG DC10 DC1030 3023501WP BS 1781 CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25310FE 48299 CTR CARGO COMPT ANGLE CRACKED AND BENT AT TOP AFT CORNER OF DOOR CUT-OUT FS 1781 LONG 29R. REMOVED ANGLE IAW DC10 SRM 51-35-01 VOL 11. MATERIAL ID FOUND TO BE 2024-T3 IAW ASTME 1476 .050 IAW CALIPER NR E110484B. FAB`D AND PART MARKED IAW FED EX GMM 7-0-1001. INSTALL IAW DC10 SRM 51-35-01 VOL 11. 2L73 4F A22WE 20051116000192005111600019NM 2005 11 16 05FDEA03777 120051111A5330 REPAIR BOEING727 727233 138408ANM BS 480 UNDAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25266FE 21672 FOUND REPAIR LOCATED AT STA 480 STR 23R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT STA 480 STR 23R WAS DETERMINED TO BE IAW SRM 53-30-3 FIG 1. BASED ON EXTERNAL VISUAL EVALUATION WITH REPAIR INSTALLED. REPAIR IS CLASSIFIED AS MAJOR BASED ON GMM 6-2-100 CRITERIA. 2L73 4F RTA3WE 20051116000232005111600023WP 2005 11 16 AALA20050745 120051113A3350P4010049 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21957U 49702 LGA - EMERGENCY LIGHTS FOR FIRST CLASS OVERHEAD INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN FIRST CLASS OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051116000252005111600025NM 2005 11 16 AALA20050739 120051111A21216067721 FAN BOEING757 7572Q8 1384972NM CABIN INOPERATIVE A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21709TW 28168 STL INFLIGHT T1727/11NOV - FLIGHT ATTENDANTS AND PASSENGERS REPORTED STRONG AND DISTINCT ODOR OF BURNING ELECTRICAL OR INSULATION IN THE CABIN. RETURNED TO STL AND LANDED WITHOUT INCIDENT. REPLACED RIGHT HAND RECIRCULATION FAN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20051116000312005111600031WP 2005 11 16 AALA20050748 120051114A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21218AA 49168 BOS - EMERGENCY LIGHTS IN CEILING FROM ROWS 22 TO 26 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN CEILING FROM ROWS 22 TO 26. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051116000392005111600039NM 2005 11 16 05FDEA03817 120051115A5310 REPAIR BOEING727 727233 138408ANM BS 303 PROPER A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25266FE 21672 FOUND REPAIR AT STA 303.9 STR 15L REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT STA 303.9 STR 15L WAS DETERMINED TO BE IAW EO 7-5330-7-2345 PT2, BASED ON EXTERNAL VISUAL EVALUATION WITH REPAIR INSTALLED. 2L73 4F RTA3WE 20051116000432005111600043NM 2005 11 16 SWAA053574 120051113A57206545410 FLOOR SUPPORT BOEING737 7373H4 1384600NM BS 663-665.5 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29336SW 23940 DURING SCHEDULED 1/4D CHECK, FOUND CENTER CABIN LONGITUDINAL FLOORBEAM CRACKED BETWEEN BS 663 TO BS 665.5, BL 0. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20051116000472005111600047NM 2005 11 16 SWAA053578 120051113A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM BS 767 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29336SW 23940 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 767, LBL 17. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051116000502005111600050NM 2005 11 16 SWAA053581 120051112A2612473925 CONTROL PANEL BOEING737 7377H4 1384404NM FIRE DETECTION FAULTY A SWAAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 SW29433LV 33716 DIVERSION/DECLARED EMERGENCY, AFT CARGO FIRE LIGHT AND FIRE DETECTOR FAULT LIGHT ILLUMINATED. CARGO FIRE EXTINGUISHER BOTTLE DISCHARGED. NO EVIDENCE OF FIRE FOUND. REMOVED AND REPLACED CONTROL PANEL FOR AFT CARGO BIN DETECTORS AND ALL SIX AFT CARGO BIN FIRE DETECTORS PER MM. 2L72 4F RTA16WE 20051116000572005111600057NM 2005 11 16 AWXA200501381 120051026A532065566542 REVEAL BOEING737 7373S3 1384711NM BS 794 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 DURING C13 CHECK DISCOVERED REVEAL STRIP CORRODED AT BS 794 AND FROM STR 24R TO STR 25R. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-15-1A1 FIG 101. REMOVED REVEAL STRIP IAW BOEING 737-300 SRM 51-40-02-0G FIG 10. FABRICATED NEW REVEAL STRIP IAW BOEING 737-300 SRM 51-30-01-0G FIG 7 AND DWG 65-56654. INSTALLED FABBED PARTS AT BS 794 AND FROM STR 24R TO STR 25R IAW BOEING 737-300 SRM 51-40-02-0G. 2L72 4F RTA16WE 20051116000632005111600063NM 2005 11 16 SWAA053586 120051113A53116520722 FRAME BOEING737 7375H4 138449DNM FWD CARGO CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29502SW 24179 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, FWD FRAME AT STOP FITTING, STR 24R. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20051116000772005111600077WP 2005 11 16 UPS05845755 120051101A531256122985 PRESSURE PANEL DOUG DC8 DC873F 302199FWP FR 32 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 FOUND LT NOSE TUNNEL, UPPER CEILING PRESSURE PANEL HAS 2 SHEARED RIVETS CRACKS AND BULGING CORROSION AT APPROX STA -32 LBL65. REMOVED EXISTING REPAIR FINGER DOUBLER, FINGER DOUBLER "T" FITTING AND 2 ATTACH FITTINGS. REMOVED CORRODED AREA. FABRICATED AND INSTALLED FILLER, 4 REPAIR DOUBLERS, 1 REPAIR SPLICE IAW SRO 8 530026 AND SRM 51-3-0, 51-1-21 AND 51-1-20D. 2L74 4F RT4A25 20051116000822005111600082NM 2005 11 16 SWAA053600 120051113A53306518420 SKIN BOEING737 7377H4 1384404NM LWR FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29792SW 27887 DURING SCHEDULED 5Y CHECK, FOUND FUSELAGE SKIN CORRODED UNDER AFT AIRPHONE ANTENNA. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051116000852005111600085EU 2005 11 16 MALA050817 120051105A2622 EXTINGUISHER SAAB SF340 340B 7860101EU LAVATORY BROKEN A MALAK NONE O OTHER ININSP/MAINT 1 GL15424XJ 340B424 DURING INSPECTION, FOUND LAV FIRE EXTINGUISHER BROKEN AND DISCHARGED. INSTALLED NEW FIRE EXTINGUISHER IN LAV POSITION IAW SF 340 AMM CH 26 AS REQUIRED. 2L72 4T RTA52EU 20051116000872005111600087EU 2005 11 16 MALA050814 120051102A2612 HANDLE SAAB SF340 340B 7860101EU LT FIRE WILL NOT TEST A MALAO OTHER L NO TEST NRNOT REPORTED 1 GL15411XJ 340B411 LEFT FIRE T-HANDLE WON'T TEST. REPLACED T-HANDLE. 2L72 4T RTA52EU 20051116000972005111600097NM 2005 11 16 QXEA200501515 120051112A243523088002A STARTER GEN DHAV DHC8 DHC8202 2809007NM NR 2 MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09360PH11925756 515 SEA FLIGHT NR 2220, ON CLIMB-OUT NR 2 DC GENERATOR CAUTION LIGHT, RAN CHECKLIST, NR 2 DC GENERATOR CAUTION LIGHT REMAINS ILLUMINATED. MAINTENANCE REPLACED THE STARTER/GENERATOR AND CONTROL UNIT. CONTROL UNIT PART NUMBER 51539-008C, SERIAL NUMBER 3730, TSN 27436, CSN 38720, TSR 10787. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051116001132005111600113NM 2005 11 16 05FDEA03790 120051113A5320 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 FOUND CENTER CARGO STA 5-113 TO 1541 LONGERON 44L SPLICE CRACKED. NEW LONGERON 44L SPLICE FABRICATED AS PER DRAWING A5A7116. CRACKED LONGERON 44L SPLICE ON CENTER CARGO STA 5-113 TO 1541 REMOVED AND REPLACED AS PER SRM 51- 33-01 VOLUME II. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051116001282005111600128NM 2005 11 16 AALA20050695 120051020A3010 HEATER BOEING757 757223 1384957NM WING DE ICING OVERHEATED A AALAA UNSCHED LANDING O OTHER CRCRUISE 1 SW21195AN 32389 AIRCRAFT AIR INTERRUPTED INTO BNA DUE TO HOT SPOT AND DISCOLORIZATION OF SIDEWALL PANEL AT SEAT 17A. FOUND OVERWING DE-ICING HEATER OVERHEATING. PULLED AND COLLARED CIRCUIT BREAKER AND PLACARDED SYSTEM. AIRCRAFT DEPARTED TO BWI. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20051116001552005111600155CE 2005 11 16 DXTA200501078 120051111A261172111211102 SMOKE DETECTOR CESSNA750 750 2076810CE CARGO BAY INOPERATIVE E DXTAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL07926QS 7500026 AT FL 390 RED -BAGGAGE SMOKE- MESSAGE ILLUMINATED FOR 6 TO 7 SECONDS. GAINED ACCESS TO BAGGAGE SMOKE DETECTOR, REMOVED AND REPLACED P/N 72-111211-102 SMOKE DETECTOR. OPS CHECK GOOD IAW 750 MM 26-14-00. CLOSED BAGGAGE ACCESS PANEL. 2L72 4J RTT00007WI 20051116001822005111600182NM 2005 11 16 USAA051353 120051108A5340 ATTACH ANGLE BOEING737 7374B7 1384702NM BS 500C CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19779AU 24996 FOUND STA 500C AT FUSELAGE FRAME AND ATTACH ANGLE CRACKED. REMOVED CRACK, FAB AND INSTALLED REPAIR STRAPS IAW EA 97079, DEFECT SIZE: 1/2" CRACK. 2L72 4F RTA16WE 20051116001842005111600184NM 2005 11 16 USAA051361 120051109A5320 STIFFENER BOEING737 7373B7 1384580NM BS 328 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND STA 328 LBL45 FWD ENTRY FLOOR SUPPORT STRUCTURE CRACKED. REPAIR, FABRICATED NEW L-ANGLE AND INSTALLED IAW SRM 51-10-02 BOEING DWR 65-45812 DEFECT SIZE: .250" 2L72 4F RTA16WE 20051116001862005111600186NM 2005 11 16 USAA051355 120051109A5340 ATTACH ANGLE BOEING737 7373B7 1384580NM BS 380 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND STR 25L AND FRAME AT BS 380 CRACKED. FABRICATED AND INSTALLED NEW ANGLE BOEING DWG 69-38780 AND SRM 53-00-01, DEFECT SIZE: 1". 2L72 4F RTA16WE 20051116001902005111600190NM 2005 11 16 USAA051359 120051109A5315 FLOORBEAM BOEING737 7373B7 1384580NM BS 344 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND STA 344, LBL 42-RBL3, AROUND CLIP NUT HOLES IN FLOORBEAM. REMOVED AND REPLACED T-CAP FROM LBL 1 TO RBL 32 IAW SRM 53-10-51, FIG 201, DEFECT SIZE: 1" BY 1". 2L72 4F RTA16WE 20051117000022005111700002NM 2005 11 17 USAA051386 120051115A5310 ANGLE BOEING737 7373B7 1384580NM BS 727B-727D CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 TRANSITION ANGLE 727B THRU 727D CORRODED. FABRICATED AND INSTALLED REPAIR PART IAW SRM 53-60-53, DEFECT SIZE: 1 INCH CORROSION. 2L72 4F RTA16WE 20051117000122005111700012EU 2005 11 17 USAA051390 120051115A5330 SKIN AIRBUS330 A330323 3930335EU FUSELAGE DENTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19678US 388 L2 DOOR AFT OF FR 33 BETWEEN BEAM 6 AND 7 DENTED. DAMAGE REMOVED (CUT OUT) AND DOUBLER INSTALLED PER EA 97015. DEFECT SIZE: 1.150 X 2.300 INCH. 2L72 4F RTA46NM 20051117000162005111700016NM 2005 11 17 QXEA200501529 120051102A5230 SKIN BOMBDRDHC8 DHC8402 1390042NM CARGO DOOR CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX: AFT CARGO DOOR FWD LOWER SKIN BEHIND FWD LOWER ROLLER BRACKET HAS CHAFING AND CORROSION. MAINTENANCE REPAIRED IAW Q400 NDTM PART 6, 51-00-01-250-301, NDTM PART 6, 51-00-04 AND QX EA 6-52-410. 2H72 4T RTA13NM 20051117000172005111700017NM 2005 11 17 QXEA200501530 120051104A5320 THRESHOLD BOMBDRDHC8 DHC8402 1390042NM SERVICE DOOR CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX: AFT SERVICE DOOR THRESHOLD IS CORRODED BELOW STAINLESS KICKPLATE. MAINTENANCE REPAIRED IAW Q400 SRM 51-14-00, QX EA 6-53-580, RD 8/4-53-1332 AND NDTM PART 6, 51-00-04. 2H72 4T RTA13NM 20051117000182005111700018NM 2005 11 17 QXEA200501519 120051114A2930 HYDRAULIC SYSTEM DHAV DHC8 DHC8202 2809007NM NR 2 MAIN MALFUNCTIONED A QXEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM09351PH 490 MFR FLIGHT 2125 UPON GEAR RETRACTION, RECEIVED NR 2 ENGINE HYDRAULIC PUMP CAUTION LIGHT, NR 2 MAIN PRESSURE DROPPED TO -0-. FLUID LEVEL REMAINED NORMAL. RAN CHECKLIST, CAUTION LIGHT EXTINGUISHED AFTER APPROXIMATELY FIVE MINUTES. MAIN HYDRAULIC PRESSURE RETURNED TO 3000 PSI. MAINTENANCE COMPLIED WITH DHC 8 200 AMM MAIN SYSTEM CYCLING TEST TASK 29-00-00-730-801. NO DEFECTS NOTED. NR 2 SYSTEM HELD PRESSURE DURING TEST. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051117000252005111700025WP 2005 11 17 UPS05845773 120051019A5230 DOOR FRAME DOUG DC8 DC873F 302199FWP CARGO BAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE:C1 C-PIT X-SLIDE DOOR FWD LOWER INTERIOR HAS 3.00 INCH LONG CRACK ON FRAME AS SEEM WITH MIRROR THROUGH 3RD LIGHTENING HOLE AFT. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER IAW SRM 52-2-0, 51-1-21 AND 51-1-20D. 2L74 4F RT4A25 20051117000332005111700033WP 2005 11 17 0501609878 120051107A2120 DUCT DOUG DC9 DC951 3022051WP RT A/C SYSTEM CRACKED A NWAAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 GL01787NC 48149 WHILE IN CRUISE FLIGHT AT FL340, AUTOMATIC TEMPERATURE CONTROL WAS LOST AND THE CABIN STARTED CLIMBING AT 700-800 FPM. AN EMERGENCY DESCENT WAS INITIATED WHEN THE CABIN REACHED 10,000 FT. CABIN ALTITUDE MAXED OUT AT 11,500 FT AND THEN BEGAN TO DESCEND. FLIGHT CONTINUED TO DESTINATION AT 10,000 FT MSL AND LANDED WITHOUT ANY OTHER COMPLICATIONS. MAINTENANCE AT DTW FOUND A DUCT CRACKED & OPENED AND REPLACED IT. ALSO REPLACED TEMPERATURE CONTROLLER. LEAK CHECK WAS GOOD AND THE AIRCRAFT HAS RETURNED TO SERVICE. 2L72 4F RTA6WE 20051117000342005111700034SO 2005 11 17 C2XA05IA127 120051104A335020131A BATTERY EMB 145 EMB145LR 3260212SO CABIN DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW27169187360 5992 145397 IAH - FLIGHT 3470, DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE FORWARD AND GALLEY EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE EMERGENCY LIGHT BATTERY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20051117000422005111700042NM 2005 11 17 CALA0500408 120051116A5220 HANDLE BOEING767 767424ER 1385270NM L-3 DOOR OUT OF ADJUST A CALAK NONE O OTHER ININSP/MAINT 1 SW2767052 29447 THE L-3 EMERGENCY DOOR INTERIOR HANDLE DOES NOT MOVE BACK AGAINST THE DOOR LINING DURING OPERATIONAL CHECK. THIS WOULD HAVE PREVENTED THE EMERGENCY ESCAPE SLIDE FROM DEPLOYING. PERFORMED TORSION SPRING ADJUSTMENT ON THE TORQUE TUBE PER MM 52-22-01, PAGE 511. EMERGENCY DOOR OPERATION CHECKED GOOD. 2L72 4F RTA1NM 20051117000482005111700048EU 2005 11 17 USAA051401 120051115A5315F5347823420100 FLOORBEAM AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19678US 388 FLOOR SUPPORT BEAM AT FR 75, Y-441; CORROSION LEVEL 1; TASK C534159-01. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-72-11. DEFECT SIZE: 1 X 1 INCH AREA. 2L72 4F RTA46NM 20051117000492005111700049EU 2005 11 17 USAA051393 120051115A5347F53311402200 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19678US 388 SEAT TRACK Y450, STA 3850 BETWEEN FR 52-53 CORRODED. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 53-31-15, 51-42-11. DEFECT SIZE: 2.5 X 1.25 AND .75 INCH DIA BOTTOM TRACK. 2L72 4F RTA46NM 20051117000502005111700050EU 2005 11 17 USAA051394 120051115A5320F5331533220000 SUPPORT ANGLE AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19678US 388 FLANGE, FR 42, Y-430 TO Y1065 CORRODED. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER F5331533220000. DEFECT SIZE: .25 INCH AREAS, 50 EA. 2L72 4F RTA46NM 20051117000682005111700068SO 2005 11 17 RAIA00511017 120051113A2770 WARNING LIGHT EMB 145 EMB145LR 3260212SO ELEVATOR ILLUMINATED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03849HK 145002 FLT - 7970 - ORD - ELEVATOR DISCONNECT LIGHT CAME ON. MAINTENANCE DEFERRED ELEVATOR DISCONNECT LIGHT PER MEL AND OPS AND VISUAL CHECK OF GUST LOCK OK. 2L72 4T RTT00011AT 20051117000702005111700070 2005 11 17 PIDA2005O186 420051104A2210 SWITCH BOEING737 7372K5 138448XNM AUTO PILOT MALFUNCTIONED A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05249TR 22598 AUTO PILOT A & B DISENGAGES AT FLAP 1 POSITION. REPLACED FLAP UP SWITCH 25EN55-6 PER MM 27-51-291. SYSTEM OPS CHECKS GOOD. 2L72 4F RTA16WE 20051117000742005111700074WP 2005 11 17 UPS05845780 120051001A5542 SKIN DOUG DC8 DC873F 302199FWP RUDDER DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE:C2 RUDDER RIGHT SIDE HAS 18EA CREASES JUST ABOVE UPS LOGO 2ND HINGE POINT FROM TOP. REMOVED AND REPLACED SKIN ON RUDDER STA ZR53-ZR71 IAW SRM 55-02-00 FIG 6 AND SRM 51-1-21. 2L74 4F RT4A25 20051117000852005111700085NM 2005 11 17 QXEA200501531 120051111A5730 PANEL BOMBDRDHC8 DHC8402 1390042NM LT WING DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX: LT WING AND LADDER PLATE FOR FUEL PANEL 522BT REQUIRES REPAIR. MAINTENANCE REPAIRED IAW QX EA 6-57-394, NDTM PART 6, 51-00-02 AND RD 8/4-57-577. 2H72 4T RTA13NM 20051117000882005111700088NM 2005 11 17 UPS05445782 120051116A541065B903604 LINK BOEING747 747123F NM NR 3 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:AD NR 3 ENGINE REAR MOUNT THRUST LINK CRACK INDICATION REVEALED AT FWD LUG UPPER SURFACE 80 PERCENT FSH & AFT UPPER SURFACE 50 PERCENT FSH BOTH EXCEED LIMIT. NR 3 ENG REAR MOUNT THRUST LINK CHANGED REF MM 71-21-03. 2L74 4F A20WE 20051117000922005111700092WP 2005 11 17 UPS05845764 120051021A531097549241 DOUBLER DOUG DC8 DC873F 302199FWP FS 1240-1260 35LCORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE:C1 WHILE WORKING N/R 822550 FOUND INTERNAL EXFOLIATED BETWEEN STA 1240 AND 1260 L35L. CUT OUT DAMAGED AREA AND REPAIRED IAW SAA SK 813-823058, AND UPS EO DC8-53-20520. 2L74 4F RT4A25 20051117000932005111700093WP 2005 11 17 UPS05845766 120051025A5522723523800013 SKIN DOUG DC8 DC873F 302199FWP RT ELEVATOR CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE:CI 2AE POPPED RIVET HEADS AT I/B LOWER SKIN OF RT ELEVATOR AND OBVIOUS INTERNAL CORROSION. REMOVED AND REPLACED SKIN IAW SRM 55-2-1 PAGE 23 & 24, 51-01-22, 55-2-1 FIG 8, 51-1-21, 51-1-21D AND 51-3-0. 2L74 4F RT4A25 20051117000992005111700099NM 2005 11 17 ASAA0540437 120050831A534069353561 STRINGER CLIP BOEING737 7374Q8 138447QNM FS 807 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND STRINGER TIE CLIP BS 807 STRINGER RT IS CORRODED. REMOVED CLIP, FABRICATED AND INSTALLED NEW CLIP IAW B737-400 SRM 51-30-1, AND 51-40-2. (M) 2L72 4F RTA16WE 20051117001012005111700101NM 2005 11 17 ASAA0540507 120050926A57536546435282 SKIN BOEING737 7374Q8 138447QNM TE FLAP PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND RIGHT OUTBOARD AFT FLAP HAS PUNCTURE APPROX 44 INCH FROM INBOARD END. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW 737-400 SRM 51-70-10. (M) 2L72 4F RTA16WE 20051117001032005111700103NM 2005 11 17 ASAA0540445 120050908A551165C2517317 RIB BOEING737 7374Q8 138447QNM HORIZONTAL STAB CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND LEFT HORIZONTAL L/E HAS CRACKED RIB AT BS 244.72. REMOVED AND REPLACED RIB ON L/E AT BS 244.72 IAW B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20051117001052005111700105NM 2005 11 17 ASAA0540452 120050912A5320 ANGLE BOEING737 7374Q8 138447QNM BS 289 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND ANGLE CRACKED AT BS 289 STRINGER 10 RIGHT. REMOVED CRACKED ANGLE, REPLACED WITH NEW PART IAW 737-400 SRM 51-40-2. (M) 2L72 4F RTA16WE 20051117001072005111700107NM 2005 11 17 ASAA0540397 120050816A531165465488 FRAME BOEING737 7374Q8 138447QNM FS 787 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 PAE - FOUND CRACKED FRAME. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW 737-400 SRM 53-00-07. (M) 2L72 4F RTA16WE 20051117001112005111700111NM 2005 11 17 ASAA0540443 120050908A5320654580730 ANGLE BOEING737 7374Q8 138447QNM FS 289 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND ANGLE CRACKED AT BS 289 STRINGER 12 RT. REMOVED CRACKED ANGLE, REPLACED WITH NEW PART IAW B737-400 SRM 51-40-2. (M) 2L72 4F RTA16WE 20051117001192005111700119NM 2005 11 17 ASAA0540513 120050926A53206545132449 FLOOR SUPPORT BOEING737 7374Q8 138447QNM FS 270 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND FLOOR SUPPORT IN FLIGHT DECK ENTRY WAY IS CORRODED AT STATION 270. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PIECES IAW ASA EA 5310-02501. (M) 2L72 4F RTA16WE 20051117001202005111700120NM 2005 11 17 ASAA0540465 120050915A575165C2591129A FLANGE BOEING737 7374Q8 138447QNM WS 613 DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND LEFT AILERON L/E FLANGE DELAMINATED AT WS 613. PREPPED DAMAGED AREA, ACCOMPLISHED HOT BOND REPAIR AT WS 613 IAW B737-400 SRM 51-70-05. (M) 2L72 4F RTA16WE 20051117001242005111700124NM 2005 11 17 ASAA0540500 120050922A53206546579531 STIFFENER BOEING737 7374Q8 138447QNM FS 1127 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND VERTICAL STIFFENER EXFOLIATED RIGHT SIDE OF TORQUE BOX AT BS 1127. REMOVED STIFFENER, FABRICATED AND INSTALLED REPLACEMENT STIFFENER IAW 737-400 SRM 51-40-5 AND 51-40-3. (M) 2L72 4F RTA16WE 20051117001262005111700126NM 2005 11 17 ASAA0540480 120050918A5310 DOOR FRAME BOEING737 7374Q8 138447QNM BS 259-360 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND INNER CHORD AT BS 259-360 AT RBL 55 IS CORRODED AT R-1 DOOR AREA. REMOVED CORRODED CHORD, REPLACED WITH NEW CHORD IAW 737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20051117001322005111700132NM 2005 11 17 ASAA0540502 120050922A531565C3394116 FLOORBEAM BOEING737 7374Q8 138447QNM FS 312 DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND BS 312 FLOORBEAM UPPER CHORD DAMAGED. REMOVED DAMAGE, FABRICATED AND INSTALLED UPPER CHORD REPAIR PIECES IAW B737-400 SRM 53-10-51 FIG 201. (M) 2L72 4F RTA16WE 20051117001372005111700137NM 2005 11 17 ASAA0540479 120050918A53206552878U102 FLOOR SUPPORT BOEING737 7374Q8 138447QNM FS 942-969 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND INNER CHORD ON FLOOR SUPPORT AT BS 942-989 IS CORRODED. REMOVED CORRODED CHORD, REPLACED WITH NEW CHORD IAW 737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20051117001392005111700139NM 2005 11 17 ASAA0540486 120050920A57536546430130 SKIN BOEING737 7374Q8 138447QNM TE FLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND RIGHT INBOARD FORE FLAP DENTED ON LOWER SURFACE 42 INCHES INBOARD END AND PERCENT FROM L/E. REMOVED DAMAGE, FABRICATED FILLER AND DOUBLER, THE INSTALLED REPAIR FILLER AND DOUBLER IAW 737-400 SRM 51-70-10. (M) 2L72 4F RTA16WE 20051117001402005111700140NM 2005 11 17 ASAA0540477 120050918A5320 FLOOR SUPPORT BOEING737 7374Q8 138447QNM BS 267-350 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND FLOOR SUPPORT ANGLE CHORD IS CORRODED AT BS 267-350 LBL 54. REMOVED CORRODED CHORD, REPLACED CHORD IAW 737-400 SRM 51-40-02. 2L72 4F RTA16WE 20051117001412005111700141NM 2005 11 17 ASAA0540487 120050920A57536546430283 SKIN BOEING737 7374Q8 138447QNM TE FLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND RIGHT OUTBOARD FLAP DISBONDING AT INBOARD TRAILING EDGE. REMOVED DAMAGE, FABRICATED FILLER AND DOUBLER, THEN INSTALLED REPAIR FILLER AND DOUBLER IAW 737-400 SRM 51-70-10. (M) 2L72 4F RTA16WE 20051117001452005111700145NM 2005 11 17 ASAA050447 120050913A5315 FLOORBEAM BOEING737 7374Q8 138447QNM BS 294.5 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND HAT CHANNEL ON FLOORBEAM AT BS 294.5 IS CORRODED. REMOVED CHANNEL, FABRICATED AND INSTALLED REPLACEMENT CHANNEL IAW B737-200 SRM 51-40-02 AND AMM 51-21-21. (M) 2L72 4F RTA16WE 20051117001492005111700149NM 2005 11 17 ASAA0540485 120050920A57536546430130 REPAIR BOEING737 7374Q8 138447QNM TE FLAP DEBONDED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND RIGHT INBOARD FORE FLAP PREVIOUS REPAIR IS DISBONDING. REMOVED DAMAGE, FABRICATED FILLER AND DOUBLER, THEN INSTALLED REPAIR PIECES IAW 737-400 SRM 51-70-10. (M) 2L72 4F RTA16WE 20051117001512005111700151NM 2005 11 17 ASAA0540448 120050913A531565C3394016 FLOORBEAM BOEING737 7374Q8 138447QNM FS 294.5 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND UPPER CHORD OF FLOORBEAM AT BS 294.5 IS CORRODED. REMOVED CORRODED SECTION OF CHORD. FABRICATED REPLACEMENT CHORD AND INSTALLED IAW B737-200 SRM 53-10-51 FIG 201. (M) 2L72 4F RTA16WE 20051117001522005111700152NM 2005 11 17 ASAA0540453 120050913A53156545818100 FLOORBEAM BOEING737 7374Q8 138447QNM FS 360 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND CORROSION ON FLOORBEAM AT BS 360. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PARTS IAW B737-400 SRM 53-00-51 FIG 201. (M) 2L72 4F RTA16WE 20051118000012005111800001NM 2005 11 18 ASAA0510331 120050929A534069353521 STRINGER CLIP BOEING737 737290C 138448VNM FS 639 CRACKED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM02740AS 22578 YXX - FOUND TIE CLIP CRACKED AT STRINGER 2 RT BS 639. REPLACED IAW B737-200 SRM 51-30-02 FIGURE 3. (M) 2L72 4F A16WE 20051118000022005111800002NM 2005 11 18 ASAA0510333 120050929A5315654581252 FLOORBEAM BOEING737 737290C 138448VNM FS 328 CORRODED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM02740AS 22578 YXX - FOUND EXFOLIATING CORROSION FOUND ON UPPER CHORD OF FLOORBEAM. REPLACED WITH REPAIR PARTS IAW B737-200 SRM 53-10-9. (M) 2L72 4F A16WE 20051118000032005111800003NM 2005 11 18 ASAA0510291 120050907A5330654577873 SKIN BOEING737 737290C 138448VNM FS 996 DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02740AS 22578 YXX - FOUND FUSELAGE SKIN DAMAGED AT BS 996 1 INCH BELOW STRINGER 21 LEFT. DAMAGED FUSELAGE SKIN REPAIRED AT BS 996 1 INCH BELOW STRINGER 21 LEFT IAW B737-200 SRM 53-30-3 FIG 48. (M) 2L72 4F A16WE 20051118000072005111800007NM 2005 11 18 ASAA0510296 120050913A531565548951 FLOORBEAM BOEING737 737290C 138448VNM FS 807 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02740AS 22578 YXX - FOUND BEYOND LIMITS CORROSION ON BS 807 FLOORBEAM UPPER CAP AT LBL 24-LBL 45. REPAIRED IAW ERO 4554 AND EA 5310-02425 BY REINFORCEMENT OF CAP WITH STRAP. (M) 2L72 4F A16WE 20051118000082005111800008NM 2005 11 18 ASAA0510297 120050913A53136549886501 STRINGER BOEING737 737290C 138448VNM FS 360 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02740AS 22578 YXX - FOUND CORROSION ON STRINGER 27 RT AT BS 360. REPAIRED BY REPLACEMENT. (M) 2L72 4F A16WE 20051118000092005111800009NM 2005 11 18 ASAA0510328 120050929A53306545777514 SKIN BOEING737 737290C 138448VNM FS 1010 GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02740AS 22578 YXX - FOUND GOUGE IN AIRCRAFT SKIN 2 INCHES ABOVE STRINGER 22 LEFT AT BS 1010. REPAIRED IAW B737-200 SRM 51-10-1 FIGURE 1, 51-30-05 FIGURE 4 AND 51-30-02 FIGURE 4. (M) 2L72 4F A16WE 20051118000102005111800010NM 2005 11 18 ASAA0510329 120050929A5311654576933 DOUBLER BOEING737 737290C 138448VNM FS 360 FRAME DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02740AS 22578 YXX - FOUND FRAME DOUBLER DAMAGED AT BS 360 BETWEEN STRINGER 26 RT PLUS 4 INCHES TO STRINGER 28 RT. REPLACED DOUBLER IAW B737-200 SRM 51-40-3. (M) 2L72 4F A16WE 20051118000122005111800012NM 2005 11 18 ASAA0540398 120050816A5311 FRAME BOEING737 7374Q8 138447QNM BS 400 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 PAE - FOUND CRACKED FRAME AT BIN RAIL STATION 400 BETWEEN STRINGER 8R-9R. REPAIRED CRACKED FRAME AT BIN RAIL STATION 400 BETWEEN STRINGER 8R-9R IAW 737-400 SRM 53-00-07. (M) 2L72 4F RTA16WE 20051118000142005111800014NM 2005 11 18 ASAA0510327 120050929A531165622063 FRAME BOEING737 737290C 138448VNM FS 460 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02740AS 22578 YXX - FOUND FORWARD CARGO PIT FRAME CRACKED AT BS 460 BETWEEN STRINGER 22 AND 23 LEFT. REPLACED FRAME WITH REPAIR PARTS PER B737-200 SRM 53-10-4. (M) 2L72 4F A16WE 20051118000152005111800015NM 2005 11 18 ASAA0510330 120050929A5322 SHEAR TIE BOEING737 737290C 138448VNM BS 360 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02740AS 22578 YXX - FOUND CORROSION ON SKIN TO FRAME AT BS 360 BETWEEN STRINGER 25 RT AND 26 RT. REPLACED IAW B737-200 SRM 53-10-4 FIGURE 8. (M) 2L72 4F A16WE 20051118000172005111800017NM 2005 11 18 ASAA0510334 120050929A5315654581577 FLOORBEAM BOEING737 737290C 138448VNM FS 344 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02740AS 22578 YXX - UPPER CHORD OF BS 344 FLOORBEAM CORRODED FROM RBL 5-10, UNDER FASTENER HEADS AND ON SURFACE. REPLACED WITH REPAIR PARTS IAW B737-200 SRM 53-10-9. (M) 2L72 4F A16WE 20051118000182005111800018NM 2005 11 18 ASAA0510290 120050907A531365627686 STRINGER BOEING737 737290C 138448VNM FS 408 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02740AS 22578 YXX - IN FORWARD CARGO PIT STRINGER 25 LEFT DENTED AT BS 408. REPLACED STRINGER PER B737-200 SRM 53-10-3. (M) 2L72 4F A16WE 20051118000202005111800020NM 2005 11 18 USAA051362 120051110A5311 FRAME BOEING737 7373B7 1384580NM BS 380 DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND HOLE IN FRAME STA 380, S15L. ENLARGED HOLE TO .125 AND INSTALLED RIVET IAW EA 97066, DEFECT SIZE: .100". 2L72 4F RTA16WE 20051118000222005111800022NM 2005 11 18 USAA051365 120051111A53206565C80735105 ANGLE BOEING737 7373B7 1384580NM BS 296 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND CORROSION ON R-1 DOOR THRESHOLD INNER CHORD ANGLE BS 296. REPAIR, DEFECTIVE PART REPLACED WITH IDENTICAL PARTY IAW SRM 51-10-02, DEFECT SIZE: 2" BY 5". 2L72 4F RTA16WE 20051118000242005111800024NM 2005 11 18 USAA051367 120051111A5330 SKIN BOEING737 7374B7 1384702NM BS 727D CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19434US 24556 FOUND CRACK, STATION 727D STRINGER 24R. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER IAW SRM 53-00-01 FIG 201, DEFECT SIZE: 1.375". 2L72 4F RTA16WE 20051118000262005111800026EU 2005 11 18 USAA051368 120051114A5315D5311281820401 FLOORBEAM AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19111US 1114 FOUND CORROSION LT FLOORBEAM (Y254) BETWEEN FS 20-23; CORROSION LEVEL 1; TASK JA-220-53500. REMOVED AND REPLACED DEFECTIVE PART PER SRM 51-72-11, DEFECT SIZE: 1 SQ IN. 2L72 4F RTA28NM 20051118000282005111800028EU 2005 11 18 USAA051370 120051114A5320D5348004320501 SILL AIRBUS320 A320214 3930316EU FR 66 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19111US 1114 FOUND CORROSION FS 66 Y1462 DOOR SILL; CORRODED LEVEL 1; TASK JA-260-53500. INSTALLED FILLER PER SRM 53-41-14, DEFECT SIZE: 1/2" BY 3/4". 2L72 4F RTA28NM 20051118000302005111800030EU 2005 11 18 USAA051372 120051114A5315D5347209001100 FLOORBEAM AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19111US 1114 FOUND CORROSION FLOORBEAM SEGMENT -Y1162, -Y1292 FS 66-68; CORROSION LEVEL 1; TASK JA-260-5350. REPLACED 3 SEGMENTS OF BEAM WITH IDENTICAL PARTS PER DWG D53472780 AND TYP REP 51-40-01, DEFECT SIZE: 1" BY 1", 1/2" BY 1/2", 1/2" BY 3/4". 2L72 4F RTA28NM 20051118000322005111800032EU 2005 11 18 USAA051374 120051114A5315 FLOORBEAM AIRBUS320 A320214 3930316EU FR 17 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19111US 1114 FOUND CORROSION FS 17 AT Y1292; CORROSION LEVEL 1; TASK JA-220-53500. INSTALLED FILLER PER SRM 51-00-14 FIG 204, DEFECT SIZE: 3/4" BY 3/4". 2L72 4F RTA28NM 20051118000392005111800039NM 2005 11 18 QXEA200501532 120051115A2130 CONTROL PANEL DHAV DHC8 DHC8202 2809007NM CABIN PRESSURE MALFUNCTIONED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09364PH 524 PDX FLIGHT NR 2133, CABIN WOULD NOT PRESSURIZE, LOW TO NO FLOW OUT OF CABIN AIR SYSTEM. MAINTENANCE PERFORMED GVI OF ACM, HEAT EXCHANGER AND CONNECTIONS. FOUND NO DEFECTS. PERFORMED GVI OF OP AND LP BLEED AIR DUCTS AND CONNECTIONS ON BOTH NR 1 AND NR 2 ENGINES. FOUND NO DEFECTS. INSPECTED CONNECTOR AND WIRING BEHIND BLEED AIR CONTROL PANEL. FOUND NO DEFECTS. PERFORMED PRESSURIZATION TEST IAW DASH8-200 AMM TASK 21-30-00-780-801. CHECKS GOOD. PERFORMED FUNCTIONAL TEST OF THE BLEED AIR SYSTEM IAW DASH8-202 AMM 21-11-00-720-801. CHECKS GOOD. NO OTHER DEFECTS NOTED. REPLACED BLEED AIR CONTROL PANEL AS A PRECAUTIONARY MEASURE. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051118000402005111800040NM 2005 11 18 QXEA200501535 120051116A2611 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM CARGO BAY MALFUNCTIONED A QXEAO OTHER N FALSE WARNING CRCRUISE 1 NM09352PH 494 YYJ - FLIGHT NR 2076, MASTER WARNING AND SMOKE DETECTOR ILLUMINATED INTERMITTENTLY INFLIGHT. MAINENTNANCE COMPLIED WITH VISUAL INSPECTION OF BAG COMPARTMENT SMOKE DETECTORS, NO DEFECTS NOTED. COMPLIED WITH OPERATIONAL TEST OF BAG COMPARTMENT SMOKE DETECTORS IAW Q200 AMM TASK 26-15-00-71-801. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051118000412005111800041NM 2005 11 18 SWAA053604 120051114A531265C28106 STIFFENER BOEING737 7373H4 1384600NM BS 1016 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29336SW 23940 DURING SCHEDULED 1/4D CHECK, FOUND BS 1016 AFT PRESSURE BLKHD STIFFENER CHANNEL CORRODED AT 6 O'CLOCK POSITION. REPAIRED STIFFENER CHANNEL PER SWA ACO & BAC DRAWING. 2L72 4F RTA16WE 20051118000422005111800042NM 2005 11 18 SWAA053605 120051114A3350MS155721 BULB BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29336SW 23940 DURING SCHEDULED 1/4D CHECK, FOUND EMERGENCY BULLNOSE LIGHT INOP AT ROW 23 DEF. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20051118000432005111800043NM 2005 11 18 SWAA053606 120051114A3350MS155721 BULB BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29336SW 23940 DURING SCHEDULED 1/4D CHECK, FOUND EMERGENCY LIGHT INOP AT ROW 13 ABC. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20051118000442005111800044NM 2005 11 18 SWAA053607 120051114A53306545776 SKIN BOEING737 7373H4 1384600NM BS 944 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29358SW 26595 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 944, STR 24L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051118000452005111800045NM 2005 11 18 SWAA053608 120051113A575465C26686 SKIN BOEING737 7373H4 1384600NM LT WING SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29367SW 26578 DURING SCHEDULED C4 CHECK, FOUND NR 1 L/E SLAT LOWER SKIN CRACKED OTBD OF ACTUATOR. REPAIRED SLAT PER SWA EA. 2L72 4F RTA16WE 20051118000462005111800046 2005 11 18 SWAA053609 420051113A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29367SW 26578 DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051118000472005111800047NM 2005 11 18 SWAA053610 120051114A3350MS155721 BULB BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29371SW 26598 DURING SCHEDULED SERVICE CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20051118000482005111800048NM 2005 11 18 SWAA053611 120051114A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29405WN 27893 DURING SCHEDULED MV2 CHECK, FOUND EEPLS TRACK COVER CRACKED AT ROW 16. REMOVED AND REPLACED COVER PER MM. 2L72 4F RTA16WE 20051118000492005111800049NM 2005 11 18 SWAA053612 120051114A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29457WN 33856 EEPLS TRACK LOOSE AT FWD END. SECURED EEPLS PER MM. 2L72 4F RTA16WE 20051118000502005111800050NM 2005 11 18 SWAA053613 120051114A53116545808 FRAME BOEING737 7373H4 1384600NM BS 294 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 294, STR 18R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051118000512005111800051NM 2005 11 18 SWAA053614 120051113A2560P4010021 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29707SA 27841 DURING SCHEDULED RON CHECK, FOUND FWD GALLEY UPPER FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2L72 4F RTA16WE 20051118000522005111800052NM 2005 11 18 SWAA053615 120051114A335065C34691 LIGHT BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29315SW 23337 DURING SCHEDULED C3 CHECK, FOUND BULLNOSE EMERGENCY LIGHTS INOP AT ROW 19 DEF. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20051118000532005111800053NM 2005 11 18 FX7A200500010 120051103A2750H1010272 SWITCH BOEING727 727224 1384076NM TE FLAPS INOPERATIVE A FX7AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO1979749 22451 ASYMMETRY ON OUTBOARD FLAP, L/R NEEDLES DISAGREE, FLAPS AT 5 DEGREES. DUMPED FUEL AND FOLLOWED THE EMERGENCY PROCEDURES. MAINTENANCE FOUND RT OUTBOARD FLAP FOLLOW UP DRUM IS LOOSE IN THE INSIDE. MAINTENANCE REMOVED AND REPLACED ACTUATOR SWITCH, ALSO REMOVED AND REPLACED THE TRANSMITTER, ALSO PERFORMED THE RIGGING CHECK. 2L73 4F A3WE 20051118000542005111800054NM 2005 11 18 FX7A200500009 120051015A2910BACH8804NN0157 LINE BOEING727 727231 1384079NM HYDRAULIC SYS LEAKING A FX7AA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO1954348 21967 AFTER TAKEOFF, DURING FLAP RETRACTION FROM 15 DEGREES TO 5 DEGREES LOST ALL OF THE SYSTEM A HYDRAULICS. TROUBLESHOT AND FOUND A FLEX LINE AT THE LEFT PCU ELEVATOR LEAKING, REMOVED AND REPLACED HYDRAULIC LINE, IAW MM REF 27-30-81, OP CHECK AND LEAK CHECK NORMAL. 2L73 4F A3WE 20051118000552005111800055NM 2005 11 18 SWAA053616 120051115A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM BS 787 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051118000562005111800056NM 2005 11 18 SWAA053617 120051115A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 578 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 578, STR 11R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051118000572005111800057NM 2005 11 18 SWAA053618 120051115A53106547959 DOOR FRAME BOEING737 7373H4 1384600NM AFT CARGO CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT AFT CARGO DOOR CUTOUT, FWD FRAME NR 5 STOP FITTING. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051118000582005111800058NM 2005 11 18 SWAA053619 120051115A53106520723 DOOR FRAME BOEING737 7373H4 1384600NM FWD CARGO CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29336SW 23940 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, AFT FRAME NR 5 STOP FITTING. REPAIRED FRAME PER SWA EA. 2L72 4F RTA16WE 20051118000592005111800059NM 2005 11 18 SWAA053620 120051115A272065C254105 CONTROL UNIT BOEING737 7373H4 1384600NM RUDDER FAULTY A SWAAO OTHER O OTHER NRNOT REPORTED 1 SW29354SW 25219 RUDDER CONTROLS FEEL EXTREMELY WEAK. REMOVED AND REPLACED RUDDER FEEL AND CENTERING UNIT PER MM. 2L72 4F RTA16WE 20051118000602005111800060NM 2005 11 18 SWAA053621 120051114A53106520722 DOOR FRAME BOEING737 7373H4 1384600NM FWD CARGO CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29358SW 26595 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, FWD FRAME NR 5 STOP FITTING. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20051118000612005111800061NM 2005 11 18 SWAA053622 120051114A52306547953 DOOR BOEING737 7373H4 1384600NM AFT CARGO CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29361SW 26572 DURING SCHEDULED C3 CHECK, FOUND AFT CARGO DOOR SKIN HANDLE CUTOUT CRACKED AT UPPER AFT CORNER. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051118000622005111800062NM 2005 11 18 SWAA053623 120051114A53306545774 SKIN BOEING737 7373H4 1384600NM BS 727E CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29361SW 26572 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 22R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051118000632005111800063 2005 11 18 SWAA053624 420051114A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29433LV 33716 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051118000642005111800064 2005 11 18 SWAA053625 420051114A256563550 SLIDE BOEING737 7377H4 1384404NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29433LV 33716 DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051118000652005111800065 2005 11 18 SWAA053626 420051114A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29433LV 33716 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051118000662005111800066NM 2005 11 18 SWAA053627 120051114A53306545775 SKIN BOEING737 7375H4 138449DNM BS 787 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29522SW 26564 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STR 18L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051118000672005111800067NM 2005 11 18 SWAA053628 120051115A53156546811 FLOORBEAM BOEING737 7373H4 1384600NM BS 986.5 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 DURING SCHEDULED D CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 986.5, BETWEEN RBL 20 TO RBL 41. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20051118000682005111800068NM 2005 11 18 SWAA053629 120051115A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 706 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051118000692005111800069NM 2005 11 18 SWAA053630 120051115A335010107451 SIGN BOEING737 7377H4 1384404NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29796SW 27889 R1 DOOR LOWER EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM. 2L72 4F RTA16WE 20051118000702005111800070NM 2005 11 18 SWAA053601 120051114A3350MS155721 BULB BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED SERVICE CHECK, FOUND OVERWING EMERGENCY LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20051118000712005111800071NM 2005 11 18 SWAA053602 120051114A53116520723 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29336SW 23940 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, FWD LOWER CORNER. REPAIRED FRAME PER SWA EA AND SRM. 2L72 4F RTA16WE 20051118000722005111800072NM 2005 11 18 SWAA053603 120051114A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29336SW 23940 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051118000732005111800073SO 2005 11 18 CHQA20050193 120051108A335066903 LIGHT EMB 135 EMB135LR 3260305SO CABIN BURNED OUT A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11831RP 145663 PROXIMITY LIGHT NOT WORKING. REPLACED PROXIMITY LIGHT IAW EMB 135 MM 33-50-12. 2L72 4F RTT00011AT 20051118000742005111800074EU 2005 11 18 AWXA200501390 120051113A2730 COMPUTER AIRBUS320 A320232 3930326EU NR 1 MALFUNCTIONED A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28662AW 1274 SAN - ABORTED TAKEOFF - FLT 539 - CREW ABORTED TAKEOFF DUE TO FLT CONTROL ELAC 1 FAULT, ABORTED AROUND 80 KNOTS. CREW RESET ELAC 1, OPERATION WAS NORMAL. ATTEMPTED TAKEOFF AGAIN WITHOUT FURTHER INCIDENT. 2L72 4F RTA28NM 20051118000752005111800075NM 2005 11 18 AWXA200501404 120051028A531265175829 BULKHEAD BOEING737 7373S3 1384711NM BS 178 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 MCN - DURING C13 CHECK DISCOVERED WEB CRACKED, .50 INCHES, AT BS 178, WL 185 AND BL 17.1R. MAINTENANCE CUTOUT DAMAGED PORTION OF BULKHEAD WEB IAW BOEING 737-300 SRM 53-10-08-2R12. FABRICATED DOUBLER AND FILLER IAW BOEING 737-300 SRM 53-10-08-2R12. INSTALLED FABRICATED REPAIR PARTS BS 178, WL 185 AND BL 17.1R IAW BOEING 737-300 SRM 53-10-08-2R12. 2L72 4F RTA16WE 20051118000762005111800076NM 2005 11 18 AWXA200501405 120051030A531265175829 BULKHEAD BOEING737 7373S3 1384711NM BS 178 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 MCN - DURING C13 CHECK DISCOVERED WEB CRACKED, 1.1 INCHES, AT BS 178, WL 180 AND BL 5.7R. MAINTENANCE CUTOUT DAMAGED PORTION OF BULKHEAD WEB IAW BOEING 737-300 SRM 53-10-08-2R12. FABRICATED DOUBLER AND FILLER IAW BOEING 737-300 SRM 53-10-08-2R12. INSTALLED FABRICATED REPAIR PARTS AT BS 178, WL 180 AND BL 5.7R IAW BOEING 737-300 SRM 53-10-08-2R12. 2L72 4F RTA16WE 20051118000772005111800077NM 2005 11 18 AWXA200501406 120051029A531265175823 STIFFENER BOEING737 7373S3 1384711NM BS 178 BULKHEAD CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 MCN - DURING C13 CHECK DISCOVERED VERTICAL CHORD CRACKED, .7 INCHES, AT AFT SIDE OF 178 BULKHEAD BL 5.7L AND WL 184. MAINTENANCE CUT OUT DAMAGED AREA OF FORWARD CHORD AT BL 5.7L IAW BOEING 737-300 SRM 53-10-08-2R5. FABRICATED FILLER IAW BOEING 737-300 SRM 53-10-08-2R5. RECEIVED ADDITIONAL REPAIR PARTS AS PART OF REPAIR KIT. INSTALLED REPAIR PARTS AT AFT SIDE OF 178 BULKHEAD BL 5.7L AND WL 184 IAW BOEING 737-300 SRM 53-10-08-2R5. 2L72 4F RTA16WE 20051118000782005111800078NM 2005 11 18 AWXA200501407 120051027A53116546539501 FRAME BOEING737 7373S3 1384711NM BS 616 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 MCN - DURING C13 CHECK DISCOVERED CHORD CRACKED, .3 INCHES, AT BS 616, WL 207 AND BL 60L. MAINTENANCE CUT OUT DAMAGED SECTION OF CHORD AT BS 616 IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5311-01143-DD1. FABRICATED STIFFENING ANGLE AND FILLER IAW AWA ER 03-5311-01143-DD1. INSTALLED FABRICATED REPAIR PARTS AT BS 616, WL 207 AND BL 60L IAW AWA ER 03-5311-01143-DD1. 2L72 4F RTA16WE 20051118000792005111800079NM 2005 11 18 AWXA200501408 120051026A5311651630153 FRAME BOEING737 7373S3 1384711NM BS 188 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 MCN - DURING C13 CHECK DISCOVERED BS 188 FRAME CRACKED, 3.0 INCHES, IN RADIUS OF OUTBOARD CHORD AT BL 31R AND WL 208. MAINTENANCE CUT OUT AND REMOVED DAMAGED SECTION OF CHORD IAW BOEING 737-300 SRM 53-00-07-2R11 FIG 201. FABRICATED ANGLE AND FILLERS IAW BOEING 737-300 SRM 53-00-07-2R11. INSTALLED FABRICATED REPAIR PARTS AT BS 188 FRAME, BL 31R AND WL 208 IAW BOEING 737-300 SRM 53-00-07-2R11 AND AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5312-05315-RC2. 2L72 4F RTA16WE 20051118000802005111800080NM 2005 11 18 AWXA200501409 120051031A5320654581217 STIFFENER BOEING737 7373S3 1384711NM BS 328 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 MCN - DURING C13 CHECK DISCOVERED STIFFENER CRACKED AT AFT SIDE OF BS 328, BL 45L AND WL 206. MAINTENANCE REMOVED STIFFENER IAW BOEING 737-300 SRM 51-40-02-0G. FABRICATED STIFFENER IAW BOEING DRAWING 65-45812. INSTALLED FABRICATED REPAIR PARTS AT BS 328, BL 45L AND WL 206 IAW BOEING 737-300 SRM 51-40-02-0G FIGS 8 AND 12. 2L72 4F RTA16WE 20051118000812005111800081NM 2005 11 18 AALA20050591 120050829A5315 FLOORBEAM BOEING767 767323 1385205NM BS 325 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21389AA 27449 AFW - FLOORBEAM AT STATION 325 HAS CORROSION REMOVED ON UPPER AND LOWER SURFACE BEYOND SRM LIMITS. AREA IS 1.0 INCH BY .021 INCH AT RT BUTTLINE 16, 1.1 BY .040 AT RT BUTTLINE 19.5, 1.2 BY .045 INCH AT RT BUTTLINE 25.5 AND 2.0 BY .021 INCH AT RIGHT BL 54 WITH A DEPTH OF .045. REMOVED AND VERIFIED CORROSION. FABRICATED REPAIR STRAP FROM 301 AND A HALF HARD STAINLESS STEEL .063 THICK. ALODINED ALL BARE ALUMINUM SURFACES. FINISHED BLEND AND REPAIR PARTS WITH TWO COATS OF BMS 10-11 PRIMER. FILLED BLENDS WITH BMS592. INSTALLED REPAIR STRAP WITH BMS595 SEALANT USING BACB30NWG FASTENERS FOR NEW LOCATIONS AND SAME TYPE AS EXISTING FASTENERS AT EXISTING LOCATIONS. INSTALL WITH 4 6D SPACING. 2L72 4F RTA1NM 20051118000822005111800082NM 2005 11 18 CALA0500409 120051116A5320654796012 STRAP BOEING737 7373T0 1384582NM STA 847 FRAME CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2759338 23576 INSPECTION FOUND AFT CARGO STRAP ON FRAME CORRODED AT STA 847 ABOVE S25R. THE STRAP ON FRAME WAS REPAIRED IAW ECRA 5311-01244. 2L72 4F RTA16WE 20051118000832005111800083NM 2005 11 18 CALA0500410 120051116A53206554801512 STRUCTURE BOEING737 7373T0 1384582NM BS 227.8 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2759338 23576 INSPECTION FOUND LOWER O/B CHORD CORRODED AT STA 227.8 FROM LBL 6 TO RBL 8. REPAIRED IAW ECRA 5311-01245. 2L72 4F RTA16WE 20051118000842005111800084SO 2005 11 18 CHQA200500196 120051112A33501317 BULB EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11847RP 145608 LEFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED LEFT OVERWING EMERGENCY EXIT LIGHT IAW EMB MM 33-50-09. OPS CHECK GOOD. 2L72 4F RTT00011AT 20051118000862005111800086SO 2005 11 18 CHQA200500195 120051114A3350100865 BATTERY PACK EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11293SK4260 4260 145500 FOUND AISLE LIGHT 1 EMERGENCY LIGHT INOPERATIVE. REPAIRED SPLICE SP9013 IAW EMB 145 MM 20-21-00. ALSO, REPLACED NR 1 EMERGENCY BATTERY IAW EMB 145 MM 33-50-04. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20051118000882005111800088EA 2005 11 18 COMA0570121 120051115A5347SH670322493 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA FS 280-477 CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01369CA7928 10079 THE LT SEAT TRACK FROM FS 280.00 TO FS 477.00 IS CORRODED. REMOVED THE CORRODED SEAT TRACK AND INSTALLED NEW SERVICEABLE SEAT TRACK IAW CRJ 700 SRM 51-11-02-001-001-A01. 2L72 4F RTA21EA 20051118000902005111800090EA 2005 11 18 COMA0560609 120051115A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01976CA 7151 FLIGHT 5005 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2L72 4F RTA21EA 20051118000912005111800091WP 2005 11 18 IXXA0500116O 120051113A3200 PIN DOUG DC8 DC873F 302199FWP NLG INSTALLED A IXXAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 SW11602AL966662354 45991 AFTER DEPARTURE FROM EDFH, NLG DID NOT RETRACT. FROM NGL INSPECTION WINDOW FOUND GROUND PIN STILL IN GEAR. RETURNED AIRCRAFT TO EDFH AND CREW LANDED WITHOUT INCIDENT. FOUND GROUND HANDLERS NOSE GEAR PIN INSTALLED. THE HANDLERS NOSE GEAR PIN WAS REMOVED, PER ANY APPLICABLE MANUALS AND AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20051118000922005111800092WP 2005 11 18 IXXA05RNG078S 120050910A5512 SKIN DOUG DC8 DC872 302199BWP STA XE173.656 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK, FOUND CORROSION ON RT HORIZONTAL STABILIZER UPPER PLATING AT OUTBOARD CENTER SECTION AROUND STA XE 173.656 BETWEEN AUXILIARY AND AFT UPPER SPAR CAP. CORRODED AREA WAS BLEND OUT AND REPAIR DOUBLER WAS INSTALLED IAW EO ATI 091505 AND EWO ATI 55-009. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR. 2L74 4F RT4A25 20051116000602005111600060NM 2005 11 16 AWXA200501384 120051005A5754 SKIN BOEING757 7572S7 1384962NM NR 4 SLAT GOUGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28904AW A10065 23566 GYR - DURING C10 CHECK, DISCOVERED GROOVES WORN INTO PREVIOUS REPAIR DOUBLER ON THE LOWER SURFACE OF THE T/E WEDGE SKIN, FOR THE NR 4 LEADING EDGE SLAT. DAMAGE WAS CAUSED BY CONTACT WITH FIXED LEADING EDGE DURING EXTENSION AND RETRACTION. MAINTENANCE REMOVED THE EXISTING REPAIR DOUBLER AND FABRICATED REPLACEMENT DOUBLER IAW BOEING 757-200 SRM 51-70-10-2R. INSTALLED FABRICATED REPAIR DOUBLER AT WS 390L, ON THE NR 4 LEADING EDGE SLAT IAW BOEING 757-200 SRM 51-70-10-2R PAR 15, 18, 20 AND 21. 2L72 4F RTA2NM 20051116000672005111600067NM 2005 11 16 SWAA053590 120051111A53116549616 FRAME BOEING737 7373H4 1384600NM BS 947 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME FAILSAFE CHORD CORRODED AT BS 947, RBL 13. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051116000722005111600072NM 2005 11 16 SWAA053595 120051112A53306545774 SKIN BOEING737 7373A4 1384585NM BS 727E CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29678AA 23290 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 20L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051116000752005111600075EU 2005 11 16 UPS05145761 120051107A5712A5724199320200 RIB AIRBUSA300 A300F4622R 3930360EU LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01136UP 0819 FOUND LEFT WING KRUGER FLAP BOX AREA CURVED DOUBLER ON 2ND RIB FROM FUSELAGE CRACKED. REMOVED AND REPLACED DOUBLER PER SRM 51-40-00. 2L72 4F RTA35EU 20051116000782005111600078WP 2005 11 16 UPS05845756 120051022A5322723502200013 SHEAR TIE DOUG DC8 DC873F 302199FWP FS 1240 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 FOUND SHEAR TIE CORRODED AT STA 1240 L35L. REMOVED FAB`D AND INSTALLED REPLACMENT SHEAR TIE IAW SRM 53-04-01-0 FIG 051, 51-01-04-0,53-2-0 AND 51-1-20D. 2L74 4F RT4A25 20051116000982005111600098WP 2005 11 16 05FDEA03768 120051111A5711ARC047242 SPAR DOUG DC10 DC1030F 3023504WP ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25310FE 48299 RT WING, TRAILING EDGE HAS A TWO INCH LONG CRACK IN FITTING AT XORS, 14 INCHES AFT OF INNER REAR SPAR. REMOVED AND REPLACED SUPPORT FITTING ARCO472-42, ( PO# 509448.1) IAW DC10-30 SRM 51-33-01 VOLII. TIMCO MECHANIC 7921, QC INSPECTOR #QC35. 2L73 4F RTA22WE 20051116001002005111600100NM 2005 11 16 05FDEA03773 120051111A5310 REPAIR BOEING727 727225 1384077NM BS 500 IMPROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 EXISTING FRAME REPAIR IN FWD CARGO BAY, BS500, S23L - S25L. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED EXISTING FRAME REPAIR BS 500 STR 23-25L/H FABRICATED ALODINED PRIMED AND INSTALLED NEW REPAIR IAW SRM 51-40-3 FIG 1 THIS IS A MAJOR REPAIR 2L73 4F A3WE 20051116001012005111600101NM 2005 11 16 05FDEA03774 120051111A5310 REPAIR BOEING727 727225 1384077NM BS 675-699 IMPROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 FOUND EXISTING STRINGER REPAIR IN FWD CARGO BAY AT BS 675 - BS 699, S27R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EVALUATED EXISTING REPAIR AT STR 27R BS 675-699 AND FOUND REPAIR DOUBLER BS 687- BS699 TO NOT COMPLY WITH SRM 53-10-3 FIG 1. FABRICATED AND INSTALLED REPAIR DOUBLER BS695-699 STR 27R PER SRM FIG 1 MAJOR REPAIR 2L73 4F A3WE 20051116001492005111600149NE 2005 11 16 DXTA200501072 220051110A7200 ENGINE CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE LEFT SHUTDOWN E DXTAH DEACTIVATE SYST/CIRCUITS RYJPARTIAL RPM/PWR LOSS ENGINE STOPPAGE WARNING INDICATION TXTAXI/GRND HDL 1 GL07372QS 5600372 PCEJCO544 LEFT ENGINE SHUTS DOWN WHEN THROTTLE MOVED FROM CRUISE TO IDLE SETTING. ITEM IS UNDER INVESTIGATION. 2L72 4F4 FRTA22CE E25EA 20051116001522005111600152CE 2005 11 16 DXTA200501070 120051109A3260 WARNING LIGHT CESSNA750 750 2076810CE MLG ILLUMINATED E DXTAO OTHER J WARNING INDICATION DEDESCENT 1 GL07970QS 7500070 DURING DESCENT THROUGH 11,000 WITH PWR AT FLT IDLE THE RED GEAR -UNSAFE- LIGHT CAME ON MOMENTARILY. THE NOSE GEAR PARTIALLY EXTENDED THEN RETRACTED. THIS WAS WHILE GOING INTO HUMID SOUTH FLORIDA AFTER A 4 HR TRIP. ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20051116001542005111600154NE 2005 11 16 DXTA200501075 220051111A72303037092 SENSE LINE CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE COMPRESSOR P3 LEAKING E DXTAD RETURN TO BLOCK XJ ENGINE FLAMEOUT WARNING INDICATION TXTAXI/GRND HDL 1 GL07306QS 5600266 PCE500019 LEFT ENGINE FLAMED OUT (STOPPED RUNNING) APPROXIMATELY 7-10 MINUTES AFTER A NORMAL START. THROTTLE WAS AT IDLE AND HAD NOT BEEN MOVED. ADJUSTED FCU AND FDU LINKAGES PER PRATT & WHITNEY JT15D-5D MM CHAPTER 73-20-01. OPERATIONAL CHECK SATISFACTORY. FOUND COMPRESSOR DELIVERY P3 LINE LEAKING. REMOVED AND REPLACED P3 LINE WITH A MANUFACTURED LINE FROM PRATT & WHITNEY. DOT APPROVAL 4-58 PER PRATT & WHITNEY JT15D-5D MM CHAPTER 73-10-04. LEAK CHECK SATISFACTORY. 2L72 4F4 FRTA22CE E25EA 20051117000092005111700009NM 2005 11 17 USAA051379 120051115A5340 ANGLE BOEING737 7373B7 1384580NM BS 767-787 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 TOP OF TRANSITION ANGLE BETWEEN STA 767 AND 787 CORRODED. REMOVED DAMAGED SECTION, FAB AND REPLACED WITH NEW SECTION IAW SRM 51-10-2 & BOEING DWG 65-47957. DEFECT SIZE: SPOTS OF CORROSION APPROXIMATELY .125 INCH IN DIAMETER. 2L72 4F RTA16WE 20051117000212005111700021WP 2005 11 17 UPS05845769 120051021A5311 SPAR DOUG DC8 DC873F 302199FWP BS 857 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE:C1 MLG WW FWD LWR SPAR CHORD CRACKED BETWEEN FASTENERS ON STA 857 (1.5 INCH LONG) XCW 53.500. REPAIRED SPAR CHORD IAW SRO 8570009. 2L74 4F RT4A25 20051117000292005111700029NM 2005 11 17 PIDA20050190 120051113A531065458076 DOOR FRAME BOEING737 737228 13844AGNM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 CRACK BEHIND R1 DOOR FRAME UPPER FORWARD STOP FITTING. REPLACED FRAME WEB PER DWG 65-45807. 2L72 4F RTA16WE 20051117000312005111700031EU 2005 11 17 AWXA200501388 120051114A5210FE240221001 DIAPHRAGM AIRBUS320 A320232 3930326EU DOOR ASSIST LEAKING A AWXAK NONE O OTHER ININSP/MAINT 1 WP28668AW 1764 LAS - EES - DURING OVERNIGHT INSPECTION DISCOVERED THE L1 DOOR ASSIST BOTTLE LOW, AT ZERO PSI. MAINTENANCE FOUND LEAK AT DIAPHRAGM. REMOVED AND REPLACED DIAPHRAGM AND SEALS ON THE L1 DOOR ASSIST BOTTLE IAW AIRBUS 320 AMM 52-10-00-03. LEAK CHECK WAS GOOD. 2L72 4F RTA28NM 20051117000322005111700032NM 2005 11 17 AWXA200501389 120051114A3350D3186510 SLIDE AIRBUSA319 A319132 3930340NM RT OVERWING WILL NOT TEST A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28804AW133783574 1043 LAS - EEL - DURING OVERNIGHT INSPECTION EMERGENCY SYS LIGHT CHECK FAILED, FAULTED EXTERNAL LIGHT LOAD RIGHT. MAINTENANCE REMOVED AND REPLACED THE RIGHT OVERWING SLIDE IAW AMERICA WEST AIRLINES TASK CARD R1A25301. 2L72 4F RTA28NM 20051117000372005111700037SO 2005 11 17 C2XA05IA123 120051030A3350110049 POWER SUPPLY EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716951 145063 IAH - DURING MAINTENANCE INSPECTION, THE EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE MEL'D THE AFFECTED LIGHTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON FLIGHT 2472, IAH MAINTENANCE REMOVED AND REPLACED THE NUMBER 4 EMERGENCY LIGHT POWER SUPPLY, OPERATIONALLY CHECKED WITH NO DEFECTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20051117000432005111700043NM 2005 11 17 QXEA200501524 120051108A5730 ACCESS PANEL BOMBDRDHC8 DHC8402 1390042NM LT WING CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX: LT WING FUEL ACCESS APERTURE FOR FUEL PANEL 523AT HAS PITTING CORROSION ON FWD AND AFT SIDE. MAINTENANCE REPAIRED IAW RD 8/4-57-441, NDTM PART 6, 51-00-02, Q400 SRM 51-25-40 AND QX EO 6-57-317. 2H72 4T RTA13NM 20051117000442005111700044NM 2005 11 17 QXEA200501525 120051108A5730 ACCESS PANEL BOMBDRDHC8 DHC8402 1390042NM LT WING CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX: LT WING FUEL ACCESS APERTURE FOR PANEL 522CT HAS PITTING CORROSION ON FWD AND AFT SIDE. MAINTENANCE REPAIRED IAW RD 8/4-57-441, NDTM PART 6, 51-00-02, Q400 SRM 51-21-10 AND QX EO 6-57-317. 2H72 4T RTA13NM 20051117000542005111700054EU 2005 11 17 USAA051398 120051115A5320F5347823420000 FLOOR SUPPORT AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19678US 388 FLOOR SUPPORT BEAM AT FR 75, Y441; CORROSION LEVEL 1; TASK C534159-01. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-72-11. DEFECT SIZE: 1 X 1 INCH. 2L72 4F RTA46NM 20051117000552005111700055EU 2005 11 17 USAA051392 120051115A5347F533114002200 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19678US 388 SEAT TRACK Y450, STA 3820 CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 53-31-15, 51-42-11. DEFECT SIZE: 4.25 X 1.25 INCH AREA. 2L72 4F RTA46NM 20051117000602005111700060SO 2005 11 17 C2XA05SD029 120051104A33501317 BATTERY EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT BURNED OUT A C2XAK NONE O OTHER ININSP/MAINT 1 SW2727523 145389 SDF - LT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED LT OVERWING EMERGENCY LIGHT IAW EMB 135 AMM 33-50-10. 2L72 4F RTT00011AT 20051117000612005111700061EA 2005 11 17 COMA0560597 120051110A2752852D10019 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAULTY A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01735CA8937 7267 FLIGHT 5244 - EN ROUTE JFK-PIT RECEIVED A FLAP FAIL CAUTION MESSAGE AT ZERO DEGREES. FLIGHT LANDED SAFELY. REPLACED THE RIGHT INBOARD FLAP OUTBOARD ACTUATOR. 2L72 4F RTA21EA 20051117000622005111700062EA 2005 11 17 COMA0560599 120051110A2752853D10020 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA RT OUTBD FLAP FAULTY A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01735CA8929 7267 FLIGHT 5244 - EN ROUTE JFK-PIT RECEIVED A FLAP FAIL CAUTION MESSAGE AT ZERO DEGREES. FLIGHT LANDED SAFELY. 2L72 4F RTA21EA 20051117000692005111700069NM 2005 11 17 PIDA2005O188 120051108A5330 SKIN BOEING737 7373G7 1384595NM BS 500D-520 CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05390WL 23219 ON WALK AROUND, NOTED SMALL SECTION OF PAINT MISSING ABOVE PAX WINDOW, RIGHT SIDE OF FUSELAGE. CLOSER INSPECTION FOUND CRACK IN FUSELAGE SKIN PARALLEL TO SKIN LAP BETWEEN BS 500D AND BS 520 BETWEEN STR 9 RT AND STR 10 RT. AIRCRAFT FERRIED UNPRESSURIZED FOR REPAIR. NOTE: CRACK IS IN UPPER SKIN PANEL ALONG HORIZONTAL LINE AT TOP EDGE OF LOWER SKIN PANEL LAP JOINT. 11/10/2005: REPAIRED DAMAGE PER SRM 53-00-01. 2L72 4F RTA16WE 20051117000752005111700075WP 2005 11 17 UPS05845781 120051003A5320 CUSP WEB DOUG DC8 DC873F 302199FWP FS220 L21R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE:C2 CUSP CRACKED 3 INCH LONG STA 220 L21R. CUT OUT DAMAGED AREA OF CUSP AT FS 220 L21R IAW SRM 51-1-21D, FABRICATED AND INSTALLED REPAIR -25 ANGLES, CUSP SPLICE AND -21 DOUBLER IAW 53-2-5 FIG 1, 53-2-5 FIG 1 AND SRM 53-02-05 FIG 5. 2L74 4F RT4A25 20051117000842005111700084EA 2005 11 17 COMA0560606 120051113A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO01969CA 7141 FLIGHT 5883 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2L72 4F RTA21EA 20051117001002005111700100NM 2005 11 17 ASA0540506 120050926A5330654577870 SKIN BOEING737 7374Q8 138447QNM FS 986-1016 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND FUSELAGE SKIN DENTED AT BS 1006.5 BETWEEN STRINGER 13-14 RT. REMOVED SKIN, REPLACED WITH NEW SKIN IAW ASA EA 5330-01999 AND 737-400 SRM 51-40-2. (M) 2L72 4F RTA16WE 20051117001042005111700104NM 2005 11 17 ASAA0540449 120050913A53225300072011 SHEAR TIE BOEING737 7374Q8 138447QNM FS 827 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND BS 827 SHEAR TIE BETWEEN 26 LEFT AND 27 LEFT CORRODED OUT OF LIMITS ON ATTACH FLANGE. CORRODED SHEAR TIE REMOVED AND REPLACEMENT SHEAR TIE SPLICED INTO FRAME. (M) 2L72 4F RTA16WE 20051117001142005111700114NM 2005 11 17 ASAA0540457 120050914A552365C2638428A TAB BOEING737 7374Q8 138447QNM RT ELEVATOR PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND RIGHT ELEVATOR TAB IS PUNCTURED. PREPPED DAMAED AREA, APPLIED HOT BOND REPAIR IAW 737-400 SRM 51-70-04 REPAIR 1. (M) 2L72 4F RTA16WE 20051117001152005111700115NM 2005 11 17 ASAA0540461 120050915A532065C3235714 TEAR STRAP BOEING737 7374Q8 138447QNM FS 375 DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND TEAR STRAP DAMAGED BEHIND SKIN REPAIR AT BS 375, STRINGER 16 LEFT. FABRICATED AND INSTALLED DOUBLER FOR TEAR STRAP IAW B737-400 SRM 53-00-01 FIG 201. (M) 2L72 4F RTA16WE 20051117001212005111700121NM 2005 11 17 ASAA0540466 120050915A575165C2591129A FLANGE BOEING737 7374Q8 138447QNM WS 607 DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND LEFT AILERON L/E FLANGE DELAMINATED AT WS 607. PREPPED DAMAGED AREA, ACCOMPLISHED HOT BOND REPAIR AT WS 607 IAW B737-400 SRM 51-70-05. (M) 2L72 4F RTA16WE 20051117001272005111700127NM 2005 11 17 ASAA0540484 120050920A57536546434336 SKIN BOEING737 7374Q8 138447QNM TE FLAP GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND RIGHT INBOARD AFT FLAP T/E DAMAGED THREE PLACES. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR SIN AND DOUBLER IAW 737-400 SRM 51-70-10. (M) 2L72 4F RTA16WE 20051117001292005111700129NM 2005 11 17 ASAA0540476 120050918A5753693880114 FITTING BOEING737 7374Q8 138447QNM TE FLAP CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND RIGHT INBOARD MID FLAP OUTBOARD TORQUE TUBE FITTING CORRODED. REMOVED AND REPLACED TORQUE TUBE FITTING IAW 737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20051117001302005111700130NM 2005 11 17 ASAA0540501 120050922A532065C3394325 SPLICE BOEING737 7374Q8 138447QNM FS 344 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND BS 344 UPPER CHORD SPLICE REPAIR CORRODED. REMOVED CORRODED CHORD REPAIR, FABRICATED AND INSTALLED REPAIR PIECES IAW ASA EA 5310-02494. (M) 2L72 4F RTA16WE 20051117001382005111700138NM 2005 11 17 ASAA0540483 120050918A57536546434336 SKIN BOEING737 7374Q8 138447QNM TE FLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND RIGHT INBOARD AFT FLAP IS DENTED 36 INCHES FROM INBOARD END. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR SKIN AND DOUBLER IAW 737-400 SRM 51-70-10. (M) 2L72 4F RTA16WE 20051117001482005111700148NM 2005 11 17 ASAA0540478 120050918A5210651807351 DOOR BOEING737 7374Q8 138447QNM FS 927-1006 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND CORROSION AROUND FASTENER HOLES ON INNER CHORD AT BS 927-1006, INBOARD OF R-2 DOOR. REMOVED CORRODED CHORD, REPLACED WIT NEW CHORD IAW 737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20051118000052005111800005NM 2005 11 18 ASAA0510332 120050929A532069775361 SPLICE BOEING737 737290C 138448VNM FS 357-369 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02740AS 22578 YXX - FOUND CORROSION ON STRINGER SPLICE AT BS 357-369 STRINGER 28 LEFT. REPAIRED STRINGER SPLICE AT BS 357-369, STRINGER 29 LEFT IAW B737-200 SRM 51-40-3. (M) 2L72 4F A16WE 20051118000062005111800006NM 2005 11 18 ASAA0510295 120050912A5330655496076 SKIN BOEING737 737290C 138448VNM FS 535 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02740AS 22578 YXX - FOUND FUSELAGE SKIN BULGING AT BS 535 LEFT KEELBEAM. REPAIRED BY REPLACEMENT OF LEFT KEEL BEAM SECTION. (M) 2L72 4F A16WE 20051118000112005111800011NM 2005 11 18 ASAA0510292 120050907A533065621096 BEAR STRAP BOEING737 737290C 138448VNM FS 500 SCRATCHED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02740AS 22578 YXX - FOUND SCRATCHES ON BEAR STRAP AT BS 500 FROM STRINGER 3 LEFT TO 17 LEFT. PLT SUBMITTED. BEAR STRAP AT BS 500 FROM STRINGER 3 LEFT TO 17 LEFT WAS REPAIRED IAW ERO 4283 AND EA 5330-01982. (M) 2L72 4F A16WE 20051118000932005111800093WP 2005 11 18 IXXA05RNG085S 120050913A5330 SKIN DOUG DC8 DC872 302199BWP BS 1060 LT CHAFED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK, FOUND CHAFING ON CENTER SECTION AT WHEEL WELL VERTICAL WEB, AROUND STA 1060 LH. CHAFING DAMAGE WAS REMOVED, NEW WEB SEGMENT AND REPAIR DOUBLER STRAP WERE INSTALLED IAW EO ATI-091705 AND EWO ATI-53-029. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR. 2L74 4F RT4A25 20051118000952005111800095WP 2005 11 18 IXXA05RNG092S 120051028A5714 SKIN DOUG DC8 DC872 302199BWP PYLON NR 3 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX 46013 DURING INSPECTION CHECK, CORROSION FOUND ON UPPER SKIN AT OUTBOARD PYLON NR 3 RT. UPPER SKIN AT OUTBOARD PYLON NR 3 WAS REPAIRED IAW SRM 57-2-1 FIG 38 AND EWO ATI-57-057. 2L74 4F RT4A25 20051118000972005111800097WP 2005 11 18 IXXA05RNG069S 120050924A5720 PLATE DOUG DC8 DC872 302199BWP STA XW 91-80 TEMPORARY A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK, FOUND AN INTERIM REPAIR ON INBOARD FLAP UPPER FWD PLATING BETWEEN STA XW91-80, RT. EXISTING DOUBLER WAS REMOVED AND A NEW REINFORCEMENT DOUBLER WAS INSTALLED IAW EO ATI-091105 AND EWO ATI 57-047. 2L74 4F RT4A25 20051118000992005111800099WP 2005 11 18 IXXA05RNG071S 120050914A5330 SKIN DOUG DC8 DC872 302199BWP STA 1440-1460 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK, FOUND A CORROSION ON INNER SKIN STA 1440-1460, LONGERON 22 - RT. CORROSION WAS REMOVED IAW DC8 SRM 51-1-8 PAGE 20, THICKNESS MEASUREMENT WAS PERFORMED IAW ASTM 797-01, AND IT WAS FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0 PAGE 2P. DAMAGE WAS REPAIRED IAW SRM 53-2-1 FIGURE 7 AND EWO ATI 53-023. 2L74 4F RT4A25 20051121000012005112100001WP 2005 11 21 IXXA05RNG083S 120050913A5330 SKIN DOUG DC8 DC872 302199BWP BS 1060 CHAFED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK, FOUND CHAFING ON CENTER SECTION AT WHEEL WELL VERTICAL WEB, AROUND STA 1060 RT. CHAFING DAMAGE WAS TRIMMED OUT, NEW WEB SEGMENT AND REPAIR DOUBLER STRAP WERE INSTALLED IAW EO ATI-091405 AND EWO ATI-53-025. 2L74 4F RT4A25 20051121000022005112100002WP 2005 11 21 IXXA05RNG084S 120050917A5230 SKIN DOUG DC8 DC872 302199BWP BS 1140 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK, FOUND A CORROSION ON AFT LOWER CARGO FWD DOOR SKIN, STA 1140 - RT. CORROSION WAS REMOVED IAW DC8 SRM 51-1-8 PAGE 20, THICKNESS MEASUREMENT WAS PERFORMED IAW ASTME 797-01 AND IT WAS FOUND OUT OF LIMITS IAW DC8 SRM 52-2-0 PAGE 22. DAMAGE WAS REPAIRED IAW EO ATI-091905 AND EWO ATI-52-003. 2L74 4F RT4A25 20051121000032005112100003WP 2005 11 21 IXXA05RNG088S 120051028A5730 SKIN DOUG DC8 DC872 302199BWP WS XOLDI 6.225 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK, FOUND CORROSION ON CENTER EXTENDED LEADING EDGE OUTER LOWER SKIN AROUND STA XOLDI 6.225 - RT. CORROSION WAS REMOVED IAW DC8 SRM 51-1-8 PAGE 20 AND THICKNESS WAS FOUND OUT OF LIMITS IAW SRM 57-2-0 PAGE 16 (MAX: 0.063 IN, MIN: 0.035 IN). DAMAGE WAS REPAIRED IAW EWO ATI 57-053 AND EO ATI-092105. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR. 2L74 4F RT4A25 20051121000052005112100005WP 2005 11 21 IXXA05RNG100S 120051014A5514 PANEL DOUG DC8 DC872 302199BWP ZONE 300 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK, FOUND CORROSION ON HORIZONTAL STABILIZER TRAILING EDGE LOWER AND UPPER PANEL. REPAIR ACCOMPLISHED, REMOVED PANEL AND STIFFENER, FABRICATED AND INSTALLED NEW PANEL AND STIFFENER IN ACCORDANCE WITH DRAWINGS 55-05467-1, 55-05467-2, 55-05467-3, 55-05467-4 AND EWO ATI-55-010. 2L74 4F RT4A25 20051121000082005112100008WP 2005 11 21 IXXA05RNG096S 120051103A5414 SKIN DOUG DC8 DC872 302199BWP ZONE 500 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK, FOUND A CORROSION ON ON UPPER SKIN AT PYLON NR 2 LEADING EDGE UPPER SKIN, LT. CORROSION WAS REMOVED IAW DC8 SRM 51-1-8 PAGE 20, THICKNESS MEASUREMENT WAS PERROMED IAW ASTME 797-01 AND IT WAS FOUND OUT OF LIMITS IAW DC8 SRM 57-2-0 PAGE 16. DAMAGE WAS REPAIRED IAW SRM 57-2-1 AND EWO ATI-57-060. 2L74 4F RT4A25 20051121000102005112100010WP 2005 11 21 IXXA05RNG097S 120051103A5730 SKIN DOUG DC8 DC872 302199BWP WS 257.500 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK, FOUND A CORROSION ON UPPER SKIN AT CENTER EXTENDED LEADING EDGE AROUND STA XW 257.500-LT. CORROSION WAS REMOVED IAW DC8 SRM 51-1-8 PAGE 20, THICKNESS MEASUREMENT WAS PERFORMED IAW ASTME 797-01 AND IT WAS FOUND OUT OF LIMITS IAW DC8 SRM 57-2-0 PAGE 16. DAMAGE WAS REPAIRED IAW SRM 57-2-1 FIGURE 38 AND EWO ATI-57-061. 2L74 4F RT4A25 20051121000112005112100011WP 2005 11 21 IXXA05RNG098S 120051104A5730 SKIN DOUG DC8 DC872 302199BWP WS 360.250 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK WAS FOUND A CORROSION AT RIGHT WING LOWER SKIN OF CENTER EXTENDED LEADING EDGE AROUND WING STATION XFS 360.250, RT. CORROSION WAS REMOVED IAW DC8 SRM 51-1-8 PAGE 20, THICKNESS MEASUREMENT WAS PERFORMED IAW ASTME 797-01 AND IT WAS FOUND OUT OF LIMITS IAW DC8 SRM 57-2-0 PAGE 16. DAMAGE WAS REPAIRED IAW EO ATI-092805 AND EWO ATI-57-062. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR. 2L74 4F RT4A25 20051121000152005112100015NM 2005 11 21 AWXA200501411 120051030A534069353642 STRINGER CLIP BOEING737 7373S3 1384711NM BS 986.5 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 MCN - DURING C13 CHECK DISCOVERED STRINGER TIE CRACKED, .75 INCHES, AT STR 24L AND BS 986.5. MAINTENANCE REMOVED AND INSTALLED FABRICATED STRINGER TIE AT STR 24L AND BS 986.5 IAW BOEING 737-300 SRM 51-40-02 FIGS 8 AND 12. 2L72 4F RTA16WE 20051121000182005112100018NM 2005 11 21 AWXA200501414 120051027A53206545834551 INTERCOSTAL BOEING737 7373S3 1384711NM BS 328 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 MCN - DURING C13 CHECK DISCOVERED INTERCOSTAL CRACKED ON THE AFT SIDE OF BS 328 BEAM AT BL 45L AND WL 208. MAINTENANCE REMOVED AND INSTALLED NEW INTERCOSTAL AT BS 328 BEAM, BL 45L, AND WL 208 IAW BOEING 737-300 SRM 51-40-02-0G. 2L72 4F RTA16WE 20051121000192005112100019NM 2005 11 21 AWXA200501415 120051025A57536546430100 WEDGE BOEING737 7373S3 1384711NM FORE FLAP DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 MCN - DURING C13 CHECK DISCOVERED DISBOND AREA ON THE UPPER SURFACE OF THE RT INBOARD FOREFLAP, 45" FROM INBOARD END. MAINTENANCE REMOVED DISBOND AREA ON THE RT INBOARD FOREFLAP IAW BOEING 737-300 SRM 51-70-10-2R REPAIR 4 FIG 201. FABRICATED FILLER AND DOUBLER IAW BOEING 737-300 SRM 51-70-10-2R REPAIR 4. INSTALLED FABRICATED REPAIR PARTS ON THE UPPER SURFACE OF THE RT INBOARD FOREFLAP, 45" FROM INBOARD END IAW BOEING 737-300 SRM 51-70-10-2R REPAIR 4. 2L72 4F RTA16WE 20051121000232005112100023WP 2005 11 21 05FDEA03834 120051116A5312 BULKHEAD DOUG DC10 DC1010 3022110WP BS 482-489 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 RT AIR CONDITIONING COMPT FOUND 1 CRACK 2 INCHES LONG ON BULKHEAD BETWEEN STA 482 AND STA 489 Z-60 X-24. REPAIRED CRACK IAW SRM 53-30-00 FIG 6 SHT 4 VOL 1, FABRICATED PARTS IAW DETAIL PARTS TRAVELER F164141/N01141 AND IAW SRM 53-30-00 FIG 6 SHT 4 VOL 1. 2L73 4F A22WE 20051121000242005112100024NM 2005 11 21 05FDEA03835 120051116A5511 RIB BOEING727 72722 1384002NM HORIZONTAL STAB DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 DURING INSPECTION OF THE LT HORIZ STAB ELEVATOR RIB AT ELEV STA 136.5, FOUND TO HAVE EXISTING REPAIRS ON THE LOWER IB AND OB FLANGES OF THE RIB AT THE TRAILING EDGE BEAM. RIB REQUIRES REPLACEMENT PER FEDEX EO 7-5510-7-5001 PT 1. REPAIRED PER S.B. 727-55A0091 2L73 4F A3WE 20051121000252005112100025WP 2005 11 21 05FDEA03836 120051116A5320 ANGLE DOUG DC10 DC1010 3022110WP BS 535 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 RIGHT AIR CONDITIONING COMPT FOUND 1 CRACK 1" LONG ON TEE ANGLE AT STA 535 Z-39 X-102. REPAIRED CRACK IAW SRM 53-00-01 FIG 9 SHT 7 VOL 1. 2L73 4F A22WE 20051121000262005112100026WP 2005 11 21 05FDEA03824 120051115A5420 SUPPORT ANGLE DOUG DC10 DC1030 3023501WP NACELLE CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25310FE 48299 NR 1 ENG NOSE COWL AFT SIDE LOWER SUPPORT WEB ANGLE FOR STARTER VALVE WAS CRACKED. REMOVED CRACK SUPPORT ANGLE FROM NR 1 ENGINE AFT SIDE OF AFT BULKHEAD NOSE COWL IAW DC10 SRM 51-31-01 VOL 11. LOCATED AND DRILLED NEW SUPPORT ANGLE IAW DC10 SRM 51-31-01 VOL 11. INSTALLED NEW ANGLE IAW DC10 SRM 51-35-01 VOL11. 2L73 4F A22WE 20051121000282005112100028NM 2005 11 21 05FDEA03826 120051115A5313 STRINGER BOEING727 727227 1384078NM BS 310-317 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 FOUND CORROSION ON STRINGER 21R BS 310-317. FOUND CORROSION ON STR 21R BS 310-317 TO BE OUT OF LIMITS. REMOVED CORRODED PORTION OF STR. REPAIRED STRINGER IAW SRM 53-10-3 FIG 1. 2L73 4F A3WE 20051121000292005112100029NM 2005 11 21 05FDEA03827 120051115A5330 REPAIR BOEING727 727233 138408ANM BS 375 PROPER A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25266FE 21672 FOUND REPAIR AT STA 375 STR 29L TO STR 29R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT STA 375 STR 29L TO 29R WAS DETERMINED TO BE IAW EO NR 7-3450-7-3393 DRW. NR 90282, BASED ON AN EXTERNAL VISUAL EVALUATION WITH REPAIR INSTALLED. REPAIR DETERMINED TO BE A MAJOR BASED ON GMM 6-2-100 CRITERIA. 2L73 4F RTA3WE 20051121000302005112100030NM 2005 11 21 05FDEA03828 120051115A5280 HINGE DOUG MD11 MD11 3023602NM ZONE 500 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 LEFT MAIN LANDING GEAR WHEEL WELL DOOR AFT HINGE FOUND WORN. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL. II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051121000322005112100032NM 2005 11 21 05FDEA03830 120051115A5512 REPAIR DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 PT1 HORIZONTAL STABILIZER RT NR 25 BORE FOUND WITH EXISTING BUSHING REPAIR WITH CORROSION. CORROSION AND EXISTING REPAIR BUSHING ON HORIZONTAL STABILIZER RT NR 25 BORE REMOVED BY REAMING BORE TO 1.067 DIAMETER AND FOUND WITHIN LIMIT AS PER FEDEX EO 1-5510-7-5000 D1 PT1. NEW REPAIR BUSHING FABRICATED AND INSTALLED AS PER FEDEX EO 1-5510-7-5000 D1 PT1 2L73 4F RTA22WE 20051121000332005112100033NM 2005 11 21 05FDEA03831 120051115A2550 CARGO BOEING727 727233 138408ANM CARGO BAY LEAKING A FDEAG O2 MASK DEPLOYED KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 SO25219FE 21102 FUMES IN COCKPIT STRONG ODOR, EMERGENCY EVACUATED ON TAXIWAY. DEPLOYED SLIDE. HAZMAT TEAM DETERMINED THE FUMES AND ODOR WERE COMING FROM THE HAZMAT CAN. HAZMAT TEAM DOWNLOADED HAZMAT CAN AND FOUND ONE DRUM LEAKING UN1993 (TERDODECIL MERCAPTANO). CLEANED UP HAZMAT CAN. NO LEAKS FOUND INSIDE A/C OR CARGO AREA. MX INSPECTED A/C THROUGHOUT CARGO AREA, COCKPIT, E/E COMPARTMENT, FWD AND AFT BELLY CARGO BINS AND AFT AIRSTAIR AREA. NO FURTHER FUMES OR SMELL NOTED IN A/C. FOUND NORMAL. OK FOR SERVICE. 2L73 4F RTA3WE 20051121000342005112100034WP 2005 11 21 05FDEA03832 120051116A5320 SUPPORT DOUG DC10 DC1030 3023501WP ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25310FE 48299 FLOOR PANEL SUPPORTS AT STA 999 AND 1019 RBL 45 ARE CRACKED (2 EA). REMOVED, FABRICATED NEW FLOOR SUPPORT IAW DAC DRAWING NR ACA3763 REV H AND FEDEX GMM 7-0-1000, SEE FEDEX NONROUTINE N00734 OF WORK ORDER NR 0003075. 2L73 4F A22WE 20051121000372005112100037EA 2005 11 21 COMA0560611 120051116A2752852D10019 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA RT TE FLAPS UNRELIABLE A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01969CA8781 7141 FLIGHT 5698 - FLAPS FAIL CAUTION. REPLACED THE RT INBD FLAP ACTUATOR. 2L72 4F RTA21EA 20051121000402005112100040EU 2005 11 21 AWXA200501391 120051114A2560P2070001214 FLASHLIGHT AIRBUS320 A320232 3930326EU INOPERATIVE A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28651AW 866 PHX - EEL - ON GROUND CREW REPORTED AFT EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY FLASHLIGHT. 2L72 4F RTA28NM 20051121000422005112100042NM 2005 11 21 AWXA200501393 120051008A5320651758335 BEAM BOEING737 7373S3 1384711NM BS 178 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 MCN - DURING C18 CHECK DISCOVERED VERTICAL BEAM WEB CRACKED AT AFT SIDE OF 178 BULKHEAD AT BL 5.7L, WL 177 AND BS 178. MAINTENANCE CUT OUT AND REMOVED DAMAGED PART OF WEB IAW BOEING 737-300 SRM 53-10-08-2R12. FABRICATED REPAIR WEB AND SHIMS IAW BOEING 737-300 SRM 53-10-08-2R12. INSTALLED FABRICATED REPAIR PARTS AT AFT SIDE OF 178 BULKHEAD AT BL 5.7L, WL 177 AND BS 178 IAW BOEING 737-300 SRM 53-10-08-2R12. 2L72 4F RTA16WE 20051121000432005112100043NM 2005 11 21 AWXA200501394 120051020A575369388488 CARRIAGE BOEING737 7373S3 1384711NM ZONE 500 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 MCN - DURING C18 CHECK DISCOVERED CORROSION ON THE LT INBOARD MID-FLAP, OUTBOARD CARRIAGE, OUTBOARD FORE FLAP SEQUENCE CARRIAGE TRACK. NO CORROSION REMOVAL LIMITS ARE AVAILABLE. MAINTENANCE REMOVED AND REPLACED THE LT INBOARD MID-FLAP, OUTBOARD CARRIAGE, OUTBOARD FORE FLAP TRACK IAW BOEING SOPM 20-50-01. 2L72 4F RTA16WE 20051121000442005112100044NM 2005 11 21 AWXA200501395 120051020A575369388485 CARRIAGE BOEING737 7373S3 1384711NM TE FLAPS CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 MCN - DURING C18 CHECK DISCOVERED CORROSION ON THE RT INBOARD MID-FLAP, INBOARD CARRIAGE, INBOARD AND OUTBOARD FORE FLAP SEQUENCE CARRIAGE TRACKS. NO CORROSION REMOVAL LIMITS ARE AVAILABLE. MAINTENANCE REMOVED AND REPLACED THE RT INBOARD MID-FLAP, INBOARD CARRIAGE, INBOARD AND OUTBOARD FORE FLAP TRACKS IAW BOEING SOPM 20-50-01. 2L72 4F RTA16WE 20051121000462005112100046NM 2005 11 21 AWXA200501397 120051108A5315D53472172205 FLOORBEAM AIRBUSA319 A319132 3930340NM FR 67 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28813AW 1223 SAL - DURING BC4 CHECK DISCOVERED CORROSION ON FLOOR STRUCTURE AT FR 67+17" AND BL -Y1292. CORROSION WAS REMOVED AND FOUND TO BE OUT OF LIMITS IAW AIRBUS 319 SRM 53-00-14 FIG 102. MAINTENANCE REMOVED AND INSTALLED NEW FLOORBEAM AT FR 67+17" AND BL -Y1292 IAW AIRBUS SRM 51-42-11. 2L72 4F RTA28NM 20051121000492005112100049NM 2005 11 21 AWXA200501400 120051027A53126516300166 BULKHEAD BOEING737 7373S3 1384711NM BS 178 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 MCN - DURING C13 CHECK DISCOVERED WEB CRACKED, 2.0 INCHES, AT BS 178, WL 218 AND BL 12R. MAINTENANCE CUTOUT DAMAGED PORTION OF BULKHEAD WEB IAW BOEING 737-300 SRM 53-10-08-2R9. FABRICATED DOUBLER AND FILLER IAW BOEING 737-300 SRM 53-10-08-2R9. INSTALLED FABRICATED REPAIR PARTS AT BS 178, WL 218 AND BL 12R IAW BOEING 737-300 SRM 53-10-08-2R9. 2L72 4F RTA16WE 20051121000522005112100052WP 2005 11 21 IXXA05SMN242S 120051013A5314 SKIN PANEL DOUG DC8 DC871F 302199DWP WS 960-980.000 IMPROPER B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING C CHECK INSPECT, LT MLG W/W - L-24L HAS NO STANDARD REPAIR BETWEEN BS 960.000 & 980.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-2 FIG 5, TR NR 53-123, EO SEMAN NR 20051282 DATED 09-27-05. REMOVED EXISTING REPAIR IAW DC8 SRM 51-1-20D. STOP DRILLED CRACK END IAW DC8 SRM 53-2-2. NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FABRICATED REPAIR ANGLE, WASHERS IAW DC8 SRM 53-2-2 FIG 5. HEAT TREATED REPAIR ANGLE IAW DC8 SRM 51-1-1 PG 1, 13, 17. CLEANED, TREATED, PRIMED AREA, REPAIR PARTS IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-2 FIG 5, DC8 SRM 51-1-20D, DC8 SRM 51-3-1. 2L74 4F RT4A25 20051121000532005112100053WP 2005 11 21 IXXA05SMN252S 120051013A5330 REPAIR DOUG DC8 DC871F 302199DWP BS 272.000 MISINSTALLED B IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW11829BX896722998 45994 DURING C-CHECK INSPECT, RT FUSE FWD CTR SECTION LWR PLATING FWD OF A PIT DOOR EXISTING DBLR EXCEED MAX RIVETS SPACING AT BS 272.00 L-31R. PERFORMED MAJOR REPAIR IAW FORM 8110-3 NR 05451, SEMAN DWG NR ED-4078, EO SEMAN 20051296. REMOVED REPAIR DOUBLER IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D. REMOVED DAMAGED SECTION IAW SEMAN DWG ED-4078. NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM. NEITHER CRACK NOR CORROSION FOUND. FAB`D REPAIR DOUBLER & REPAIR TRIPLER & FILLER INTERNAL DOUBLER & FILLER IAW SEMAN DWG ED-4078. CLEANED, TREATED, PRIMED AREA & REPAIR PARTS IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM. INSTALLED REPAIR PARTS IAW SEMAN DWG ED-4078, DC8 SRM 51-1-20D, DC8 SRM 51-3-1. 2L74 4F RT4A25 20051121000542005112100054WP 2005 11 21 IXXA05SMN249S 120051013A5330 REPAIR DOUG DC8 DC871F 302199DWP FS 24 L-34LH MISINSTALLED B IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW11829BX896722998 45994 DURING C-CHECK INSPECT, LT NOSE SKIN FWD PAX DOOR JAMB EXISTING DBLR EXCEED OVERAGE RIVETS SPACING AND CHERRY MAX AT STA FS 24 L-36 LT. PERFORMED MAJOR REPAIR IAW FORM 8110-3, SEMAN DWG ED-4077 DATED 10-01-05 AND EO SEMAN 20051295 DATED 10-05-05. REMOVED EXISTING DOUBLER IAW DC8 SRM 51-1-21, DC8 SRM 51-3-0. REMOVED DAMAGED AREA IAW SEMAN DWG NR ED-4097. PERFORMED NDT INSPECTION ON AFFECTED AREA IAW DC8 NDT SPM. NO CORROSION NEITHER CRACK FOUND. FAB`D REPAIR DOUBLER & 02 INTERNAL FINGER DOUBLERS, FILLER IAW SEMAN DWG ED-4077. CLEANED, TREATED, PRIMED AREA, REPAIR PARTS IAW DC8 SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SEMAN DWG NR ED-4077, DC8 SRM 51-1-20D, DC8 SRM 51-1-21, DC8 SRM 51-3-0, DC8 SRM 51-3-1.2L74 4F RT4A25 20051121000572005112100057EA 2005 11 21 VNAA0510019 120051023A5240 ACCESS DOOR CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE FUSELAGE OPEN A VNAAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 GL05720PS 10178 AFTER TAKEOFF THE CREW HEARD A SQUEALING NOISE. THE FLIGHT RETURNED TO IAH WHERE MAINTENANCE FOUND THE SERVICE PANEL ACCESS DOOR OPEN. NO DAMAGE WAS FOUND. THE DOOR WAS PROPERLY SECURED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20051121000582005112100058EA 2005 11 21 VNAA0510020 120051025A5751 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT AILERON LIGHTNING STRIKEA VNAAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL05207PS 7873 DURING AN FAA RAMP CHECK, THE INSPECTOR DISCOVERED EVIDENCE OF LIGHTNING STRIKE DAMAGE ON THE TRAILING EDGE OF THE RT AILERON AND RT OUTBOARD FLAP. MAINTENANCE COMPLIED WITH AN EN ROUTE LIGHTNING STRIKE INSPECTION AND FOUND EVIDENCE OF LIGHTNING DAMAGE ON THE RADOME. THE AIRCRAFT WAS FERRIED TO DAY. MAINTENANCE COMPLIED WITH A DETAILED VISUAL INSPECTION OF THE RT AILERON, RT OUTBOARD FLAP, AND RADOME IAW CRJ200 NDTM 51-20-09. NO LIGHTNING STRIKE DAMAGE WAS FOUND ON ANY OF THE THREE AREAS. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20051121000602005112100060EA 2005 11 21 REXA200500138 120051115A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A REXAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 SO258790A 7790 FLAPS FAIL AT ZERO WHEN SELECTED TO TWENTY. QRH FOLLOWED, ZERO FLAP LANDING PERFORMED. SYSTEM REST AND PLACED ON 72 HOUR WATCH PER AD98-20-01. 2L72 4F RTA21EA 20051121000612005112100061EA 2005 11 21 VNAA0511010 120051114A5100 UNKNOWN CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE UNKNOWN NONE A VNAAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 GL05719PS 10177 THE AIRCRAFT STRUCK A BIRD ON TAKEOFF ROLL. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE PERFORMED A BIRD STRIKE INSPECTION IAW CRJ700 AMM 05-51-25-210-801-A01. NO DAMAGE WAS FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20051121000622005112100062EA 2005 11 21 VNAA0511003 120051106A3000 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE ANTI ICE SYS NONE A VNAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL05216PS 7882 THE ANTI-ICE DUCT WARNING MESSAGE ILLUMINATED WHEN WING ANTI-ICE WAS SELECTED ON. THE CREW FOLLOWED THE QRH AND RETURNED TO PIT. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE WING ANTI-ICE SYSTEM IAW CRJ200 AMM 30-12-00-710-801. THE SYSTEM OPERATIONALLY CHECKED GOOD AND NO DEFECTS WERE FOUND. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20051121000632005112100063EA 2005 11 21 VNAA0511007 120051111A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A VNAAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL05254PS 7935 DURING APPROACH THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED WITH FLAPS AT 8° SELECTED TO 20°. THE CREW FOLLOWED THE QRH, DECLARED AN EMERGENCY, AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE SYSTEM PER THE CRJ FIM. THE FLAP SYSTEM WAS RESET IAW BOMBARDIER SL 00-001. THE FLAPS OPERATIONALLY CHECKED GOOD AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20051121000652005112100065NM 2005 11 21 ASMF200511007 120051110A2150655281057 RELAY BOEING737 73773A 1384606NM A/C PACK FAILED W ASMFA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW23904AM3515 28262 AIRCRAFT RETURNED OF FLIGHT AS A CONSEQUENCE OF DURING CLIMB LEFT PACK TRIP OFF LIGHT TURNED ON. THE OPERATIONAL PROCEDURE WAS PERFORMED, FLYING AT 250 FL. THE CABIN TEMP CONTROLLER BITE TEST WAS PERFORMED IAW FIM 21-52 TASK 834 ALL CORRECT. DURING OVERNIGHT CHECK, THE CABIN TEMP CONTROLLER BITE TEST WAS PERFORMED IAW FIM 21-52 TASK 834, THE RAM AIR DOOR WAS VERIFIED AND THE AIR CONDITIONING RELAY WAS REPLACED IAW 21-52-02 TASK 21-52-02-400-801, TESTED CORRECT. 2L72 4F RTA16WE 20051121000662005112100066EU 2005 11 21 SA05116 120051117A335032145410 EPSU AIRBUS320 A320214 3930316EU EMERGENCY LIGHT FAILED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19109UW19945 1065 DCA - THE MID CABIN RIGHT HAND EMERGENCY POWER SUPPLY UNIT FAILED THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE MID CABIN, RIGHT HAND EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20051121000672005112100067EA 2005 11 21 VNAA0511006 120051109A5210 STRIKER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR SEAL DAMAGED A VNAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL05206PS 7860 THE CREW REPORTED A LOUD SQUEAL FROM THE PASSENGER DOOR DURING CLIMBOUT. THE AIRCRAFT RETURNED TO TYS AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND DAMAGE TO THE PASSENGER DOOR FORWARD AND AFT SEAL STRIKERS. A TEMPORARY REPAIR WAS PERFORMED IAW BOMBARDIER REO 601R-53-22-059. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20051121000682005112100068NM 2005 11 21 USAA051407 120051116A5330146N3300 SKIN BOEING757 757225 1384959NM BS 1194, STR 29 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19602AU 22196 STA 1194, STR 29R CORRODED. BLENDED OUT CORROSION PER SRM 53-00-01 FIG 101 DETAIL II AND REPAIRED IAW EA 97017. DEFECT SIZE: 5.0 L X 2.7 W X .075 D INCH. 2L72 4F RTA2NM 20051121000692005112100069NM 2005 11 21 SWAA053631 120051114A53126545819 PRESSURE PANEL BOEING737 7373H4 1384600NM NLG W/W CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED SERVICE CHECK, FOUND NLG W/W LEFT FWD PRESSURE SIDE WEB CRACKED AT BS 251.625, WL 177. REPAIRED WEB PER SWA EA & SRM. 2L72 4F RTA16WE 20051121000722005112100072NM 2005 11 21 SWAA053633 120051116A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM BS 400 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 400, STR 2L. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20051121000732005112100073NM 2005 11 21 SWAA053634 120051115A3350101114 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29396SW 27690 DURING SCHEDULED C2 CHECK, FOUND CENTER AISLE EMERGENCY EXIT SIGN LENS LOOSE AT ROW 2. SECURED LENS PER MM. 2L72 4F RTA16WE 20051121000742005112100074NM 2005 11 21 SWAA053635 120051116A26975402 WIRE HARNESS BOEING737 7373H4 1384600NM APU BAY FAULTY A SWAAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW29399WN 27693 DECLARED EMERGENCY. APU FIRE HANDLE LIGHT ILLUMINATED & FIRE WARNING BELL SOUNDED. APU FIRE EXTINGUISHER BOTTLE DISCHARGED. REMOVED AND REPLACED APU TAILPIPE FIRE LOOP HARNESS PER MM. 2L72 4F RTA16WE 20051121000752005112100075NM 2005 11 21 SWAA053636 120051116A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29424WN 29828 DURING SCHEDULED HC2 CHECK, FOUND EEPLS TRACK COVERS CRACKED BETWEEN ROW 1 TO ROW 22. REMOVED AND REPLACED COVERS PER MM. 2L72 4F RTA16WE 20051121000762005112100076NM 2005 11 21 SWAA053637 120051116A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29426WN 29830 EEPLS TRACK COVER MISSING AT FWD END. INSTALLED COVER PER MM. 2L72 4F RTA16WE 20051121000792005112100079 2005 11 21 SWAA053640 420051115A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29604SW 27955 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051121000802005112100080NM 2005 11 21 SWAA053641 120051116A53116546548 FRAME BOEING737 7373H4 1384600NM BS 747 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R TO STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051121000812005112100081NM 2005 11 21 SWAA053642 120051116A53116546558 FRAME BOEING737 7373H4 1384600NM BS 907 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R TO STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051121000822005112100082NM 2005 11 21 SWAA053643 120051116A53116546526 FRAME BOEING737 7373H4 1384600NM BS 400 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051121000832005112100083NM 2005 11 21 SWAA053644 120051116A53116546532 FRAME BOEING737 7373H4 1384600NM BS 480 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R TO STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051121000842005112100084NM 2005 11 21 SWAA053645 120051116A532065C27314 CLIP BOEING737 7373H4 1384600NM BS 480 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 480, STR 15L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051121000852005112100085NM 2005 11 21 SWAA053646 120051116A532065C27314 CLIP BOEING737 7373H4 1384600NM BS 480 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 480, STR 16L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051122000022005112200002NM 2005 11 22 05FDEA03837 120051116A7711 INDICATOR BOEING727 727200 138407ENM NR 3 EPR INOPERATIVE A FDEAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO25287FE 21849 CREW REPORTS NR 3 EPR IND INOP/ERRATIC ON TAKEOFF ROLL. REPORTS ALL OTHER INDICATIONS NORMAL. RELEASED FOR SERVICE PER MEL/CDL: 77-01-01. MEL 77-01-01: NR 3 ENGINE EPR INDICATOR INOP. PLACED ON MEL DEFERRAL 77-01-01. EXPIRES 19 NOV 2005. OK FOR SERVICE. REMOVED AND REPLACED NR 3 ENGINE EPR INDICATOR AND TRANSMITTER PER AMM 77-11-011-4. AND OPS CHECKS NORMAL PER AMM 77-11-000-5. 2L73 4F RTA3WE 20051122000032005112200003WP 2005 11 22 05FDEA03839 120051116A7120 MOUNT DOUG MD10 MD1010F 3022112WP ENGINE CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25372FE 46610 COMPLY WITH EA8-7220-92342 ENGINE-FORWARD MOUNT CHAFE REPAIR, NR 3 ENGINE. COMPLIED WITH EA 8-7220-92342. MINOR REPAIR ENGINE FWD MOUNT CHAFE REPAIR. 2L73 4F RTA22WE 20051122000042005112200004NM 2005 11 22 05FDEA03840 120051116A5311 FRAME BOEING727 727200 138407ENM BS 1010 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 AFT CARGO COMPARTMENT, FRAME IS DENTED BS 1010 LBL 27 TO LBL 30 WL 150 TO WL 153. DENT IN FRAME FOUND TO BE OUT OF LIMITS, CUT OUT DAMAGE FABRICATED DOUBLER, ALODIEND & PRIMED, INSTALLED FASTENERS IN REPAIR SRM 51-30-2. 2L73 4F RTA3WE 20051122000112005112200011WP 2005 11 22 05FDEA03848 120051117A5753 REPAIR DOUG DC10 DC1030 3023501WP TE FLAP UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 RIGHT WING OUTBOARD FLAP FOUND FLUSH DOUBLER REPAIR ON UPPER SKIN FROM STA XOF 560 TO STA XOF 599 DIMENSIONS 36.5 X 39 INCHES. REPAIR ACCOMPLISHED WITH EA FEDEX. 2L73 4F A22WE 20051122000122005112200012WP 2005 11 22 05FDEA03882 120051118A5330 REPAIR DOUG DC10 DC1030 3023501WP BS 304-357 PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 TWO EXT DOUBLER ON LEFT NOSE SKIN FROM STA 304 TO STA 357 Z-15. PERFORMED INSPECTION ON REPAIR IAW EA 8-5310-46689 STEP 12 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001-1P E3 AND RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VOL 2 PAR 33. 2L73 4F A22WE 20051122000182005112200018 2005 11 22 SWAA053650 420051114A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29785SW 30602 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20051122000192005112200019WP 2005 11 22 05FDEA03849 120051117A5330 REPAIR DOUG DC10 DC1030 3023501WP BS 755-645 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 RIGHT EXT FUSELAGE FOUND DOUBLER LENGTH 100 INCHES WIDTH 10 INCHES AT STA 755 TO STA 645 LONG 42. EO8-5100-7-5001. 2L73 4F A22WE 20051122000202005112200020WP 2005 11 22 05FDEA03850 120051117A5330 REPAIR DOUG DC10 DC1030 3023501WP BS 645-755 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 LEFT EXT FUSELAGE FOUND DOUBLER LENGTH 100 INCHES WIDTH 10 INCHES AT STA 755 TO STA 645 LONG 42. NO ACTION TAKEN EO8-5100-7-5001. 2L73 4F A22WE 20051122000222005112200022WP 2005 11 22 05FDEA03852 120051117A5330 REPAIR DOUG DC10 DC1030 3023501WP BS 1019-1099 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 RIGHT EXTERNAL FUSELAGE FOUND DOUBLER LENGTH 80 INCH WIDTH 12 INCH AT STA 1019 TO STA 1099 LONG 42. NO ACTION TAKEN EO 8-5100-7-5001-1. 2L73 4F A22WE 20051122000232005112200023WP 2005 11 22 05FDEA03853 120051117A5330 REPAIR DOUG DC10 DC1030 3023501WP BS 999-1099 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 LEFT EXT FUSELAGE FOUND DOUBLER LENGHT 100 INCHES WIDTH 12 INCHES AT STA 999 TO STA 1099 LONG 43. NO ACTION TAKEN EO 8-5100-7-5001-1. 2L73 4F A22WE 20051122000242005112200024WP 2005 11 22 05FDEA03854 120051117A5522 SKIN DOUG DC10 DC1030 3023501WP RT ELEVATOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 IN THE RIGHT DETACHABLE ELEVATOR UPPER SURFACE AT STA XE 75 FOUND 1 EA CRACK 4 INCHES LONG. REMOVED EXISTING DOUBLER NEAR CRACK, CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER IAW SRM 55-10-00 FIG 8 VOL 1. TOUCH UP WHITE TOP COAT ON REPAIR DOUBLER IAW TF110, FABRICATED PART IAW DETAIL PART TRAVELER F160767 IAW SRM 55-10-00. 2L73 4F A22WE 20051122000262005112200026WP 2005 11 22 ASMF200511002 120051104A5240 SEAL DOUG DC9 DC982 3022082WP SERVICE DOOR MISINSTALLED W ASMFBA EMER. DESCENT UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CRCRUISE 1 SW23501AM 49188 ACFT PERFORMED AN UNSCHEDULED LANDING AT CUL DUE TO A PRESSURIZATION FAILURE; EMERGENCY PROCEDURE PERFORMED BEING NOT POSSIBLE TO CONTROL IT, PERFORMING AN EMERGENCY DESCENT TO 14,000 FT. DURING MX REVISION DETECTED A LEAK IN AFT SERVICE DOOR DUE TO SEAL DOOR REAR BOTTOM AREA IMPROPERLY INSTALLED (IN 3 INCHES LONG APPROXIMATELY), 90 PERCENT OF OXYGEN MASKS FOUND DEPLOYED WITH OXYGEN SYS SWITCH IN MANUAL MODE. SEAL DOOR PROPERLY INSTALLED IAW MM 52-42-02, TESTED CORRECT. ACFT FERRIED TO GDL. AT GDL, 79 CHEMICAL OXYGEN GENS REPLACED IAW MM 35-22-01, A/C SYS & PRESSURIZATION TESTS PERFORMED IAW MM 21-32-00, TESTED CORRECT. FDR REMOVED & ANALYZED AND RECORDS DEMONSTRATE THAT AIRCRAFT DID NOT DEPRESSURIZE. 2L72 4F A6WE 20051122000272005112200027WP 2005 11 22 ASMF200511005 120051106A8011447628 COUPLER DOUG DC9 DC987 3022087WP RT ENGINE FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23803ML 49726 DURING RIGHT ENGINE STARTING, THE RIGHT ENGINE DID NOT HAVE TURN IN N1 AND N2 AND START VALVE LIGHT TURNED ON. THE ADAPTER SHAFT STARTER WAS REPLACED IAW MM 80-10-01 PAGE 204, TESTED CORRECT. DURING OVERNIGHT CHECK, OPERATIONAL TEST WAS PERFORMED IAW MM 71-00-01, TESTED CORRECT. 2L72 4F RTA6WE 20051122000282005112200028WP 2005 11 22 ASMF200511001 120051103A2750 WARNING LIGHT DOUG DC9 DC982 3022082WP TE FLAPS ILLUMINATED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23501AM 49188 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING TAXIING FLAPS OUT OF SERVICE MESSAGE WAS SHOWN. TECHNICAL PERSONNEL DEFERRED THE REPORT IAW MEL 27-11, DISPATCHING THE AIRCRAFT. 2L72 4F A6WE 20051122000292005112200029NE 2005 11 22 AALA20050751 220051115A7200 MANIFOLD DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE LT ENGINE INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21248AA 49259 718445 LAX - LEFT ENGINE LOOP-A LIGHT FOLLOWED BY LEFT ENGINE FIRE WARNING DURING CLIMBOUT AT APPROXIMATELY 6000 FEET. THROTTLES TO IDLE AND LIGHTS AND WARNING WENT OUT. LEFT EXHAUST GAS TEMPERATURE AT TAKEOFF IN YELLOW ZONE. RIGHT ENGINE EXHAUST GAS TEMPERATURE NORMAL. CONTINUED OPERATION AT IDLE FOR 20 MINUTES. LANDED LAX WITHOUT INCIDENT. FOUND 13TH STAGE MANIFOLD INNER CASE BLOWN APART. CHANGED LEFT ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 F A6WE E9NE 20051122000332005112200033NE 2005 11 22 ASMF200511003 220051104A731142D395 PRESSURE SWITCH BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE ENGINE FUEL FAILED W ASMFA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW23806AM31390 26273 726735 AIRCRAFT RETURNED OF FLIGHT AS A CONSEQUENCE OF EICAS MESSAGE -L ENG FUEL FILT- WAS SHOWN. THE FUEL PUMP FILTER AND DEFERENTIAL PRESSURE SWITCH WERE REPLACED IAW MM 73-11-02 AND MM 73-34-014 RESPECTIVELY, TESTED CORRECT. 2L72 4F4 FRTA2NM E17NE 20051122000342005112200034WP 2005 11 22 05FDEA03856 120051117A3297 CONDUIT DOUG MD10 MD1010F 3022112WP LT MLG SENSOR UNSECURE A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO2568057 48264 AFTER T/O & GEAR RETRACTION, UNSAFE (RED) ON RT & LT MAINS ON BOTH PRIMARY & CONFIG DISPLAYS. RAN CHECKLIST CYCLED GEAR. GOOD UP INDICATION ON LEFT MAIN BUT STILL UNSAFE ON RIGHT MAIN. RETURNED, LANDED AT KORD. FOUND NO PSEU LAST LEG FAULTS, PERFORMED RT MLG UPLTCH ADJ/TEST, FOUND THE CONDUIT FOR THE UPLATCH SENSORS CLAMPED IMPROPERLY, NOT ALLOWING SENSORS TO MOVE TO THE NEAR STATE. ADJ CONDUIT & RE-CLAMPED. ADJ/TEST OF RIGHT UPLATCH SENSOR GAP GOOD PER AMM. PERFORMED RT & LT MAIN UPLATCH SENSOR INDUCTANCE TEST PER AMM. FOUND THE LT SENSORS CONDUIT IMPROPERLY CLAMPED. RE-ADJUSTED CONDUIT & CHECKED LEFT SENSOR GAP GOOD PER AMM. PERFORMED PSEU RTS GOOD PER AMM. 2L73 4F RTA22WE 20051122000352005112200035EA 2005 11 22 VNAA0510022 120051025A5210 STRIKER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR SEAL DAMAGED A VNAAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL05251PS 7931 DURING AN FAA RAMP CHECK, THE INSPECTOR DISCOVERED DAMAGE TO THE PASSENGER DOOR SEAL STRIKER. THE AIRCRAFT WAS FERRIED TO CAK. MAINTENANCE PERFORMED A TYPE II REPAIR IAW REO 601R-53-22-033. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20051122000372005112200037NM 2005 11 22 05FDEA03857 120051117A5330 SKIN BOEING727 727200 138407ENM BS 1051 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 EXTERNAL FUSELAGE SKIN PILLOWING AROUND FASTENER HEADS AT BS 1051, STR 29 LEFT. SUSPECT CORRODED STRINGER. REMOVED CORROSION FOUND OUT OF LIMITS. REMOVED AREA OF DAMAGE, FABRICATED REPAIR DOUBLER AND FILLER AND ISNTALLED, IAW SRM 53-30-3. 2L73 4F RTA3WE 20051122000382005112200038NM 2005 11 22 05FDEA03858 120051117A3210 FITTING BOEING727 727100 1384036NM TRUNNION CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 LEFT MLG FWD TRUNNION SUPPORT FITTING O/B FLANGE, O/B SURFACE HAS SURFACE CORROSION BETWEEN -THROUGH PIN- AND LWR PORK CHOP FITTING BOLT HOLE LOCATIONS. REPAIRED L/H MLG FWD TRUNNION SUPPORT FITTING PER FED EX EA 7-5710-91408. 2L73 4F RTA3WE 20051122000392005112200039NM 2005 11 22 05FDEA03860 120051117A5330 REPAIR BOEING727 727200 138407ENM BS 370 UNDAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25266FE 21672 FOUND ROUND REPAIR AT STA 370 STR 16L. REPAIR REQUIRES EVALUATION FOR MAJOR / MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT STA 370 STR 16L WAS DETERMINED TO BE IAW FEDEX EO 7-5100-7-2307H - DATE 08/31/93, BASED ON AN EXTERNAL VISUAL EVALUATION WITH THE REPAIR INSTALLED. REPAIR DETERMINED TO BE MAJOR BASED ON FEDEX GMM 6-2-100 CRITERIA. 2L73 4F RTA3WE 20051122000402005112200040WP 2005 11 22 05FDEA03861 120051117A5100S392945221 INSULATION DOUG DC10 DC1010 3022110WP ZONE 100 BURNED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO2568051 47805 IN CENTER ACCESSORY COMPARTMENT RT AND LT SIDE OF FUSELAGE INSULATION BLANKET IS SEVERELY BURNED AROUND 1-2 AND 1-3 SYSTEM PNEUMATIC DUCT. REPLACED INSULATION BLANKETS PER REF: MM 25-28-00. NEED LEAK CHECK 97846. LEAK CHECKED #1 SYSTEM PNEUMATIC DUCT AT CAC, LT SIDE PER MM 36-14-02-1-1 . MX KM-97620 QC 97349 2L73 4F A22WE 20051122000412005112200041WP 2005 11 22 05FDEA03862 120051118A5710 DOUBLER DOUG DC10 DC1030 3023501WP WS 1070 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 LT WING LOWER SURFACE FOUND A DOUBLER 24.5 X 8 INCHES ON SKIN AT STA XORS 1070. REMOVED AND REPLACED FASTENERS IAW SRM 57-10-00 FIG 85 VOL 1. 2L73 4F A22WE 20051122000422005112200042WP 2005 11 22 05FDEA03863 120051118A5754 REPAIR DOUG DC10 DC1030 3023501WP NR 1 SLAT PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 RT WING, SLAT 1 FOUND FLUSH DOUBLER REPAIR ON LOWER SKIN, DIMENS 11.5 X 8.5 INCHES. PERFORMED A GVI OF REPAIR IAW EA 8.5710-90122 AND FOUND IN COMPLIANCE WITH REQUEST BY EO 83500.7.5001. 2L73 4F A22WE 20051122000442005112200044WP 2005 11 22 05FDEA03865 120051118A5330 REPAIR DOUG DC10 DC1030 3023501WP BS 695-675 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 PERFORMED INSPECTION IAW (IAW 8-500-7-5001-1P) FOUND DOUBLER LENGTH 12 INCHES WITH 6 INCHES LT INT FUSE AT STA 695 TO STA 675 LONG 51 TO LONG 52. STRIPPED PAINT IAW SRM 51-21-01 VOL 2 PAR 33. REMOVED RIVET AND INSTALLED FASTENERS PER SRM 52-20-00 FIG 13 VOL 1, TREATED AND PROTECTED AREA IAW SRM 51-21-01 VOL 2. 2L73 4F A22WE 20051122000472005112200047WP 2005 11 22 05FDEA03868 120051118A5755 REPAIR DOUG DC10 DC1030 3023501WP RT WING SPOILER UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 RT WING SPOILER NR 3 FOUND DOUBLER REPAIR ON LOWER SKIN DIMENSION 10 X 6 INCHES. INSPECTED, REMOVED AND INSTALLED SPOILER NR 3 RT WITH NEW HARDWARE IAW MM 27-60-01-4. PERFORMED FUNCTIONAL TEST IAW MM 27-60-01-4. 2L73 4F A22WE 20051122000482005112200048WP 2005 11 22 05FDEA03869 120051118A5730 SKIN DOUG DC10 DC1010 3022110WP LT WING UNSECURE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 ACCESS PANEL LT WING P/N 525 AT FOUND SKIN UNGLUED. REBONDED AND REPAIRED PANEL IAW SRM 57-10-00 FIG 71 VOL 1 AND DWG ARB1111 DPS 1.07- 2 TYPE 2. FABRICATED PART IAW DETAIL PART TRAVELER N02362 AND SRM 57-10-00 FIG 71 VOL 1. 2L73 4F A22WE 20051122000492005112200049NM 2005 11 22 05FDEA03870 120051118A2120 ODOR BOEING727 727100 1384036NM CABIN DETECTED A FDEAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO25198FE 19154 PASSING FL 180 SMELLED FUMES IN THE COCKPIT. RAN SMOKE AND FUME CHECKLIST. RETURNED TO MEMPHIS. SMELLED LIKE BURNING RUBBER OR PLASTIC. FACT REPLACED BOTH CONDENSER BAGS AND FOUND BOTH RT AND LT AIR CYCLE MACHINES OUT OF OIL REPLACED BOTH ACM RAN BOTH PACKS WITH APU AND ENGINE PNEUMATICS NO SIGN OF SMOKE OR SMELL PER JRH 21-51-011. 2L73 4F RTA3WE 20051122000512005112200051NM 2005 11 22 05FDEA03872 120051118A5330 REPAIR BOEING727 727200 138407ENM BS 860-880 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 EXISTING EXTERNAL REPAIR ON FUSELAGE BS 860-880 STR 8R-10R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. ALL WORK WAS ACCOMPLISHED IAW FED EX E.A. 7-5330-91421. REPAIR WAS DETERMINED TO BE A MAJOR REPAIR. 2L73 4F RTA3WE 20051122000532005112200053WP 2005 11 22 05FDEA03874 120051118A5730 REPAIR DOUG DC10 DC1030 3023501WP WS 458 PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 RIGHT WING OUTBOARD FLAP FOUND DOUBLER REPAIR ON UPPER SKIN AT STA XOF 458 DIMENS 4.25 X 35 INCHES. PERFORMED AN INSPECTION ON REPAIR IAW SRM 57-10-00 FIG 9 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001-2P E3. 2L73 4F A22WE 20051122000552005112200055WP 2005 11 22 05FDEA03876 120051118A5751 REPAIR DOUG DC10 DC1030 3023501WP WS 458 RT PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 RIGHT WING OUTBOARD FLAP FOUND DOUBLER REPAIR ON LOWER SKIN AT STA XOF 456 DIMENSION 4.25 X 35 INCHES. PERFORMED AN INSPECTION ON REPAIR IAW SRM 57-10-00 FIG 9 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001-P2 E3. 2L73 4F A22WE 20051122000562005112200056WP 2005 11 22 05FDEA03877 120051118A5730 REPAIR DOUG DC10 DC1030 3023501WP WS 256 PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 RIGHT WING INBOARD VANE FLAP, FOUND DOUBLER ON UPPER SKIN AT STA XIFH 256 DIMENS 4 INCH DIAM. PERFORMED INSPECTION FOUND NO DELAMINATION IAW SRM 51-61-01 VOL 2 TAP TEST. PERFORMED INSPECTION ON REPAIR IAW SRM 51-71-00 VOL 2 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2 E3. 2L73 4F A22WE 20051122000572005112200057WP 2005 11 22 05FDEA03878 120051118A5730 REPAIR DOUG DC10 DC1030 3023501WP RT WING PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 RIGHT WING INBOARD FLAP FOUND FLUSH DOUBLER REPAIR ON UPPER SKIN L/E AT STA XIFH 155 DIMENS. 2.5 X 2 INCHES. PERFORMED A GVI OF REPAIR IAW SRM 57-00-01 FIG 4 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2 E3. 2L73 4F A22WE 20051122000592005112200059WP 2005 11 22 05FDEA03880 120051118A5312 REPAIR DOUG DC10 DC1030 3023501WP BULKHEAD UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 PERFORMED INSPECTION IAW EO 8-5100-7-5001-1P FOUND DOUBLER LENGTH 11 INCHES WIDTH 13.5 INCHES FWD NLG BULKHEAD RT AT STA 490 Z-40. STRIPPED PAINT AREA IAW SRM 51-21-01 PAR 33 VOL 2. REPLACED FASTENERS AS REQUIRED IAW SRM 53-30-00 FIG 6 VOL 1. TREATED AREA IAW SRM 51-21-01 VOL 2. 2L73 4F A22WE 20051122000622005112200062NM 2005 11 22 QXEA200501523 120051109A5730 SKIN BOMBDRDHC8 DHC8402 1390042NM WING OUT OF LIMITS A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX: 7 AREAS OF FWD APERTURE AND 2 AREAS ON AFT APERTURE FOR WING PANEL 522BT ARE BLENDED OUT OF LIMITS. MAINTENANCE REPAIRED IAW NDTM PART 6, 51-00-02, QX EA 6-57-394, RD 8/4-57-577 AND QX EA 6-57-317. 2H72 4T RTA13NM 20051122000642005112200064EA 2005 11 22 VNAA0511005 120051109A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT WINGLET LIGHTNING STRIKEA VNAAO OTHER O OTHER DEDESCENT 1 GL05247JS 7922 THE CREW REPORTED A LIGHTNING STRIKE ON DESCENT INTO YYZ. MAINTENANCE COMPLIED WITH AN EN ROUTE LIGHTNING STRIKE INSPECTION AND FOUND DAMAGE TO THE LEFT WINGLET. THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE COMPLIED WITH DETAILED LIGHTNING STRIKE INSPECTIONS. ALL DAMAGE WAS REPAIRED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20051116001832005111600183NM 2005 11 16 USAA051349 120051108A5311 FRAME BOEING737 7374B7 1384702NM BS 400 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19779AU 24996 FOUND BS 400 AT STRINGER 8R CRACKED. REPAIRED IAW T/R 53-10-20C, DEFECT SIZE: 1/4" CRACK. 2L72 4F RTA16WE 20051116001852005111600185NM 2005 11 16 USAA051354 120051109A5315 FLOORBEAM BOEING737 7373B7 1384580NM BS 344 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND STA 344, LBL42-RBL31; AROUND CLIP NUT HOLES IN FLOOR BEAM CORRODED. REMOVED CORRODED OUT OF LIMITS SECTION OF "T" CAP FROM LBL31 TO RBL31 IAW SRM 53-10-51, FIG 201, DEFECT SIZE: 1" BY 1". 2L72 4F RTA16WE 20051116001872005111600187NM 2005 11 16 USAA051356 120051109A5315 FLOORBEAM BOEING737 7373B7 1384580NM BS 28 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND BS28/LBL27 CRACKED. FABRICATED AND INSTALLED STIFFENER IAW SRM 51-10-02, DEFECT SIZE: 1". 2L72 4F RTA16WE 20051117000042005111700004NM 2005 11 17 USAA051384 120051115A532069374024 ANGLE BOEING737 7373B7 1384580NM BS 294 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 BS 294; S-17R; ATTACHED TO OUTBOARD SIDE OF ZEE ANGLE CRACKED. PART REPLACED WITH IDENTICAL PART IAW SRM 51-10-02. DEFECT SIZE: 1.5 INCH CRACK IN A 4 INCH LONG ANGLE. 2L72 4F RTA16WE 20051117000152005111700015NM 2005 11 17 QXEA200501528 120051104A5753 FLAP TRACK BOMBDRDHC8 DHC8402 1390042NM TE FLAPS DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX: RIGHT INBOARD FLAP INBOARD UPPER FLAP TRACK INNER CHANNEL IS GALLED FROM THE MIDPOINT FWD BY THE AFT FLAP ROLLER SHAFT. MAINTENANCE REPAIRED IAW QX EA 6-57-393, NDTM PART 6, 51-00-02 AND RD 8/4-57-575. 2H72 4T RTA13NM 20051117000272005111700027WP 2005 11 17 UPS05845776 120051003A5310 SHEAR WEB DOUG DC8 DC873F 302199FWP FS 857 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE:C2 HEAVY CORROSION ON RT W/W FWD BULKHEAD STA 857, RBL 26. CUT OUT CORROSION IN SHEAR WEB AT STA 857 RBL 26 AND INSTALLED REPAIR PARTS IAW UPS ENG FILE DC8-53-20517 SAA SK 866-832582, BOEING MESSAGE 1-137210970-2, AND FAA FORM 8100-9. 2L74 4F RT4A25 20051117000382005111700038SO 2005 11 17 C2XA05IA126 120051031A335078241 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716981 145208 LFT - FLIGHT 2551, DURING POST FLIGHT INSPECTION THE CREW REPORTED THE INTERIOR EXIT SIGN AFT OF THE RT EMERGENCY EXIT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FIVE EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20051117000402005111700040NM 2005 11 17 CALA0500406 120051115A524165505734 GATE BOEING737 7373T0 1384582NM R1 DOOR CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2759338 23576 INSPECTION FOUND THE R-1 DOOR LOWER GATE CORRODED AT STOP PINS AND LOWER EDGE, STA 312-328, S18R. A NEW LOWER GATE WAS INSTALLED IAW MM 52-41-61. ADJUSTMENT AND CHECK PERFORMED PER WORK CARD 03-5230-1-8651. 2L72 4F RTA16WE 20051117000412005111700041NM 2005 11 17 CALA0500407 120051115A261389931505 MODULE HONEYWELL BOEING737 737524 1384721NM APU OVERHEAT INOPERATIVE A CALAF ACTIVATE FIRE EXT. N FALSE WARNING CRCRUISE 1 SW271465542572 P100886 28916 CREW RECEIVED APU DET INOP LIGHT ALONG WITH OVHT/DET AND MASTER CAUTION AFTER TAKEOFF WITH APU OFF. WHILE AT CRUISE CREW GOT APU FIRE LIGHT WARNING. QRH PROCEDURES FOLLOWED, APU FIRE BOTTLE WAS DISCHARGED. FIRE WARNING LIGHT EXTINGUISHED, FLT CONTINUED, LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE APU AREA AND FOUND NO EVIDENCE OF FIRE. THE APU LOWER FIRE DETECTOR AND FIRE DETECTION CONTROL MODULE WERE FOUND AT FAULT. THE LOWER FIRE DETECTOR AND FIRE DETECTION MODULE WERE REMOVED AND REPLACED IAW MM 26-15-14 AND 26-10-01. THE APU FIRE BOTTLE WAS ALSO REPLACED IAW MM 26-22-11. AN APU AND ENGINE FIRE DETECTION OPERATIONAL TEST WAS PERFORMED IAW MM 26-11-00 AND 26-15-00 AND ALL OPERATION CHECKED GOOD.2L72 4F RTA16WE 20051117000472005111700047NE 2005 11 17 0501615530 220051001A7321430219 STATOR BOEING757 757251 1384970NM PWA 2037 PW2037 NE ENGINE FAILED A NWAAA UNSCHED LANDING X ENGINE FLAMEOUT CRCRUISE 1 GL01530US1199 1199 23845 716457 DURING CRUISE FLIGHT ENGINE NR 1 OIL PRESSURE DROPPED TO 12 PSI. ENGINE NR 1 FLAMED OUT. FLIGHT CREW DIVERTED AC TO CLT AND PERFORMED AN UNEVENTFUL LANDING. MAINTENANCE REMOVED AND REPLACED THE PMA STATOR AND ROTOR. NOTE: THIS EVENT WAS ORIGINALLY BELIEVED TO BE A COMMANDED ENGINE SHUTDOWN AND REPORTED INTERNALLY ONLY. POST EVENT INVESTIGATION HAS REVEALED THAT THIS EVENT WAS A FLAMEOUT AND IS SDR REPORTABLE. 2L72 4F4 FRTA2NM E17NE 20051117000582005111700058NM 2005 11 17 PCSA11150501 120051115A56105893543129 WINDSHIELD BOEING727 727233 138408ANM COCKPIT CRACKED A PCSAA UNSCHED LANDING O OTHER CLCLIMB 1 SO29495AJ 20937 FLIGHT 8213 DURING CLIMBOUT FROM MIA CREW REPORTED LEFT HAND L1 CAPTAINS WINDSHIELD CRACKED. AIRCRAFT RETURNED BACK TO MIA AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED CAPTAINS L1 WINDSHIELD IAW B727 MM CH 56-11-11 AND REMOVED AND REPLACED THE WINDOW HEAT CONTROLLER IAW B727 MM CH 30-41-02, OPERATIONALY CHECKED NORMAL IAW B727 MM CH 30-41-02. AIRCRAFT WAS RETURNED TO SERVICE. 2L73 4F RTA3WE 20051117000592005111700059 2005 11 17 PCSA11040501 420051104A3421777500505 ADI BOEING727 7272F9 138407DNM COCKPIT SPINNING A PCSAA UNSCHED LANDING O OTHER CRCRUISE 1 SO29199AJ 21426 FLT 8419 AFTER DEPARTURE FROM MIA AND WHILE IN CRUISE THE CREW REPORTED CAPTAINS VG ATTITUDE FLAG IN VIEW CONTINUOUSLY AND RAPID SPINNING OF THE ADI TO THE RIGHT, AUX VG SELECTION AND C/B RESET, NO HELP. AIRCRAFT RETURNED BACK TO MIA AND LANDED WITHOUT ANY FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ADI AND OPERATIONALLY CHECKED GOOD PER B-727 MM CH 31-00-11 AND B-727 MM CH 34-22-02. AIRCRAFT WAS RETURNED TO SERVICE. 2L73 4F RTA3WE 20051117000722005111700072WP 2005 11 17 UPS05845778 120051003A5312 PRESSURE PANEL DOUG DC8 DC873F 302199FWP FS 940 RBL 65 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 INSPECTION TYPE:C2 FUSELAGE FLOORBEAM HEAVY CORROSION STA 940 RBL 65. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS AT STA 940 RBL 65 IAW UPS EO DC8-5330-23084-A, SAA SK 866-832597, BOEING MESSAGE 1-133200277-3 AND FAA FORM 8100-9. 2L74 4F RT4A25 20051117000902005111700090NM 2005 11 17 UPS05545777 120051115A5315 FLOORBEAM BOEING757 75724APF 1384969NM MAIN CARGO BAY CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01469UP 25485 INSPECTION TYPE:C CORROSION ON MAIN CARGO FLOORBEAM BS 1200, BL-0 TO RBL 60. REPAIRED FLOORBEAM IAW GOODRICH ER 05-4846. 2L72 4F RTA2NM 20051117000942005111700094NM 2005 11 17 ASAA0540509 120050926A57536546435282 STRUCTURE BOEING737 7374Q8 138447QNM TE FLAP BENT A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND RIGHT INBOARD AFT FLAP OUTBOARD EDGE BENT, LOWER SIDE. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW 737-400 SRM 51-70-10. (M) 2L72 4F RTA16WE 20051117000962005111700096NM 2005 11 17 ASAA0540450 120050913A5322654655418 SHEAR TIE BOEING737 7374Q8 138447QNM FS 847 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND BS 847 SHEAR TIE BETWEEN STRINGERS 26 LEFT AND 27 LEFT CORRODED. REMOVED DAMAGED SECTION OF SHEAR TIE, FABRICATED AND INSTALLED REPAIR PIECES IAW B737-400 SRM 53-00-07. (M) 2L72 4F RTA16WE 20051117000982005111700098NM 2005 11 17 ASAA0540482 120050918A5320654583442 STRAP BOEING737 7374Q8 138447QNM FS 312-328 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND FLOORBEAM STABILIZER STRAP AT BS 312, RBL 46 IS CRACKED. FABRICATED STRAP AND REPAIR SPLICE, INSTALLED REPAIR PIECE IAW 737-400 SRM 53-10-51 FIG 201. (M) 2L72 4F RTA16WE 20051117001022005111700102NM 2005 11 17 ASAA0540441 120050907A532065C330845 PLATE BOEING737 7374Q8 138447QNM FS 601 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND SPLICE PLATE RIGHT SIDE CRACKED AT BS 601, STRINGER 15 RT. REMOVED CRACKED SPLICE PLATE, FABRICATED AND INSTALLED REPLACEMENT SPLICE PLATED IAW B737-400 SRM 51-30-1 AND 2. (M) 2L72 4F RTA16WE 20051117001062005111700106NM 2005 11 17 ASAA0540396 120050816A531165465488 FRAME BOEING737 7374Q8 138447QNM FS 907 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 PAE - FOUND CRACKED FRAME. REPAIRED CRACKED FRAME IAW 737-400 SRM 53-00-07. (M) 2L72 4F RTA16WE 20051117001162005111700116NM 2005 11 17 ASAA0540463 120050915A575165C2591129A SKIN BOEING737 7374Q8 138447QNM AILERON GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND LEFT AILERON OUTBOARD ATTACH AREA IS GOUGED. PREPPED GOUGED AREA, ACCOMPLISHED HOT BOND REPAIR IAW B737-400 SRM 51-70-05. (M) 2L72 4F RTA16WE 20051117001182005111700118NM 2005 11 17 ASAA0540438 120050907A5322 SHEAR TIE BOEING737 7374Q8 138447QNM BS 986 DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - SHEAR TIE AT BS 986, RBL 49 HAS ELONGATED FASTENER HOLES. REMOVED DAMAGED SHEAR TIE, FABRICATED AND INSTALLED REPLACEMENT SHEAR TIE IAW B737-400 SRM 51-30-1, AND 51-30-3. 2L72 4F RTA16WE 20051117001342005111700134NM 2005 11 17 ASAA0540505 120050926A533065457781 SKIN BOEING737 7374Q8 138447QNM FS 986-1016 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND FUSELAGE SKIN DENTED AT BS 1000 .5 INCH BELOW STRINGER 14R. REMOVED DAMAGED SECTION OF STRAP, FABRICATED AND INSTALLED LAP REPAIR IAW 737-400 SRM 53-00-01 FIGURE 201 AND ASA EA 5330-01999. (M) 2L72 4F RTA16WE 20051117001362005111700136NM 2005 11 17 ASAA0540510 120050926A57536546431285 SKIN BOEING737 7374Q8 138447QNM TE FLAP BENT A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND LEFT OUTBOARD FORE FLAP DENTED, LOWER T/E 21 INCHES FROM INBOARD END. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW 737-400 SRM 51-70-10. (M) 2L72 4F RTA16WE 20051117001422005111700142 2005 11 17 USAASA05104 420050930A2565D30664105 SLIDE AIRBUSA319 A319112 3930323EU PAX CABIN FAULTY A USAAK NONE J WARNING INDICATION ININSP/MAINT 1 EA19733UW 1205 PIT - A FORWARD SERVICE DOOR SLIDE INDICATED UNARMED INTERMITTENTLY ON THE ECAM DOOR/OXY PAGE. MAINTENANCE FOUND THE FORWARD SERVICE DOOR ESCAPE SLIDE PACKED LOOSELY. MAINTENANCE REPLACED THE FORWARD SERVICE DOOR ESCAPE SLIDE. OK FOR SERVICE. (M) 2L72 4F RTA28NM 20051117001442005111700144NM 2005 11 17 ASAA0540499 120050922A531565C3394224 FLOORBEAM BOEING737 7374Q8 138447QNM FS 328 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND FLOORBEAM UPPER CAP CORRODED AT BS 328. REMOVED CHORD, UPPER, FABRICATED AND INSTALLED CHORD AND REPAIR PIECES IAW ASA EA 5310-02489. (M) 2L72 4F RTA16WE 20051117001462005111700146NM 2005 11 17 ASAA0540481 120050918A532065C33986192 SUPPORT BOEING737 7374Q8 138447QNM FS 344-360 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND INTERCOSTAL AT BS 344-360 RBL 50 IS GOUGED AND CORRODED. REMOVED CORRODED T-EXTRUSION, FABRICATED AND INSTALLED REPLACEMENT "T" IAW ASA EA 5310-02490. 2L72 4F RTA16WE 20051118000042005111800004NM 2005 11 18 ASAA0510293 120050912A531169514714 FRAME BOEING737 737290C 138448VNM FS 360 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02740AS 22578 YXX - FOUND CORROSION ON FRAME TO SKIN ATTACH ANGLE AT BS 360 BETWEEN STRINGER 26-27 RT. REMOVED AND REPLACED FRAME TO SKIN ATTACH ANGLE PER SRM 53-10-4. (M) 2L72 4F A16WE 20051118000132005111800013NM 2005 11 18 ASAA0540399 120050816A534765C3148354 SEAT TRACK BOEING737 7374Q8 138447QNM FS 907 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 PAE - FOUND SEAT TRACK CORRODED AT BS 907 RBL 25 WL 208. REMOVED REPLACED SEAT TRACK. (M) 2L72 4F RTA16WE 20051118000872005111800087EA 2005 11 18 COMA0570120 120051115A5347SH670321591 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 280-477 CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01369CA7928 10079 THE RT SEAT TRACK FROM FS 280.00 TO FS 477.00 IS CORRODED. REMOVED THE CORRODED SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW CRJ 700 SRM 51-41-01-001-001-A01. 2L72 4F RTA21EA 20051118000892005111800089EA 2005 11 18 COMA0560607 120051114A5610NP1393215 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A COMAO OTHER O OTHER CRCRUISE 1 SO01735CA167975725 7267 FLIGHT 5010 - PILOT'S WINDSHIELD CRACKED. REPLACED WINDSHIELD. 2L72 4F RTA21EA 20051121000142005112100014NM 2005 11 21 AWXA200501410 120051027A5311651630153 FRAME BOEING737 7373S3 1384711NM BS 188 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 MCN - DURING C13 CHECK DISCOVERED CHORD CRACKED, 2.7 INCHES, AT BS 188, WL 208 AND BL 31L. MAINTENANCE CUT OUT DAMAGED SECTION OF CHORD AT BS 188 IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5300-05314-ES3. FABRICATED REPAIR ANGLE AND FILLERS IAW AWA ER 03-5300-05314-ES3. INSTALLED FABRICATED REPAIR PARTS AT BS 188, WL 208 AND BL 31L IAW AWA ER 03-5300-05314-ES3. 2L72 4F RTA16WE 20051121000352005112100035WP 2005 11 21 05FDEA03833 120051116A5321 FLOOR PANEL DOUG DC10 DC1030 3023501WP ZONE 100 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25310FE 48299 CENTER LOWER CARGO COMPT FLOOR PNL 183ZF HAS BROKE AND CORRODED INSERTS STA 1781 TO 1821 RBL 30 TO37. REMOVED AND REPLACED INSERTS IAW FEDEX DWG SRA 25-005 REV E. 2L73 4F A22WE 20051121000392005112100039WP 2005 11 21 IXXA05SMN225S 120051013A5101 RIVET DOUG DC8 DC871F 302199DWP FS 1254.000 IMPROPER B IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX896722998 45994 DURING C CHECK INSPECT, AFT LWR FUSELAGE BELLY, STA FS 1254.000 L-35.5R, UPGRADE REPAIR DOUBLER TO INCORPORATE A MIN OF 3 ROWS OF RIVETS. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-1 FIG 7, EO SEMAN NR 20051198 DATED 09-20-05. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D. REMOVED DAMAGED SECTION IAW DC8 SRM 53-2-1 FIG 7 (SHEET 1, 3). NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. FAB`D REPAIR DOUBLER (AL7075T6 0.125) + (02 EA) INTERNAL FINGER DOUBLERS (AL7075T6 0.050) IAW DC8 SRM 53-2-1 FIG 7 (SHEET 1, 3), DC8 SRM 53-4-1 FIG 16 (SHEET 1) ITEM “E”, DC8 SRM 51-10-0 FIG 2, DC8 SRM 51-1-4 PG 1 (FORMING). CLEANED, TREATED, PRIMED AREA + 2L74 4F RT4A25 20051121000412005112100041NM 2005 11 21 AWXA200501392 120051009A532065176859 SHEAR WEB BOEING737 7373S3 1384711NM BS 344-346.5 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 MCN - DURING C18 CHECK DISCOVERED SHEAR WEB AT BS 344 TO BS 346.5 AND FROM STR 15L TO STR 17L CRACKED, 1.37 INCHES, AT THE LOWER AFT HOLE. MAINTENANCE REMOVED CRACKED DOUBLER SECTION ON THE SHEAR WEB IAW BOEING 737-300 SRM 51-40-02-0G. FABRICATED NEW DOUBLER SECTION OF SHEAR WEB IAW BOEING DRAWING 65-17685. INSTALLED FABRICATED REPAIR PARTS AT BS 344 TO BS 346.5 AND FROM STR 15L TO STR 17L IAW BOEING 737-300 SRM 51-40-02-0G. 2L72 4F RTA16WE 20051121000702005112100070NM 2005 11 21 SWAA053632 120051116A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM BS 967 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 967, STR 26L. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20051121000712005112100071EA 2005 11 21 REXA200500136 120051106A2611PU90421R3 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA LAVATORY MALFUNCTIONED A REXAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO258495B 7495 LAVATORY SMOKE WARNING ON TAKEOFF. FLIGHT ATTENDANT VERIFIED FALSE WARNING, NO SMOKE FOUND. SYSTEM DEFERRED. DEFER CLEARED BY REMOVING AND REPLACING THE LAVATORY SMOKE DETECTOR. 2L72 4F RTA21EA 20051121000772005112100077NM 2005 11 21 SWAA053638 120051116A5310573149 POST BOEING737 7375H4 138449DNM COCKPIT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29512SW 24189 DURING SCHEDULED 1/2D CHECK, FOUND L1 COCKPIT WINDOW POST CRACKED AT UPPER OUTBOARD CORNER. REPAIRED WINDOW POST PER SRM. 2L72 4F RTA16WE 20051122000082005112200008NM 2005 11 22 05FDEA03844 120051116A5313 STRINGER BOEING727 727200 138407ENM BS 1050 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 CORROSION (C53-111-01) AFT CARGO COMPARTMENT ON STR 29 STA 1050. REPAIRED STR 30 BS 1050 PER SRM 53-10-3. 2L73 4F RTA3WE 20051122000102005112200010EU 2005 11 22 05FDEA03847 120051116A5311 FRAME AIRBUS300 A300B4622R 3930312EU ZONE 100 MISDRILLED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25720FD 417 COMPLY WITH EA 6-5310-92355 FUSELAGE MAIN FRAME EXISTING SHORT PITCH HOLES FR 42, STR 36 RT AND 36 LT. COMLIED WITH EA 6-5310-92355 FUSELAGE MAIN FRAME EXISTING SHORT PITCH HOLES FR 42, STR 36 RT AND 36 LT. 2L72 4F RTA35EU 20051122000152005112200015NM 2005 11 22 CALA0500412 120051117A5320146N36509 PAN BOEING757 757224 1384958NM STA 1340-1620 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713113 27555 INSPECTION FOUND AFT LAV PAN CORRODED AT AFT SIDE, STA 1340-1620, RBL 2 TO RBL 20. THE CORRODED LAV SERVICE PAN DOUBLER WAS REMOVED AND A NEW PAN DOUBLER WAS INSTALLED IAW SRM 51-40-02 AND ENGINEERING DRAWING 146N3650. 2L72 4F RTA2NM 20051122000172005112200017NE 2005 11 22 SWAA053649 220051115A73211853M56P07 HMU BOEING737 7377H4 1384404NM GE CFM56 CFM56* 13802NE RT ENGINE FAULTY A SWAAO OTHER EAJVIBRATION/BUFFET FLAME/FIRE WARNING INDICATION CLCLIMB 1 SW29782SA 29808 LOUD BANG HEARD FROM RT SIDE OF AIRCRAFT. FLAME SEEN FROM NR 2 ENGINE EXHAUST. ENGINE PARAMETERS NORMAL. SUSPECT COMPRESSOR STALL. PERFORMED ENGINE BOROSCOPE. NO DAMAGE FOUND. REMOVED AND REPLACED NR 2 ENGINE HMU PER MM. 2L72 4F4 FRTA16WE E2GL 20051122000602005112200060WP 2005 11 22 05FDEA03881 120051118A5312 REPAIR DOUG DC10 DC1030 3023501WP BULKHEAD UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 PERFORMED INSPECTION IAW EO 8-5100-7-5001-1P FOUND DOUBLER LENGTH 13.5 INCHES WIDTH 11 INCHES FWD NLG BULKHEAD LT STA 490 Z-40. STRIPPED AREA IAW SRM 51-21-01 VOL 2 PAR 33. REPLACED FASTENERS AS REQUIRE IAE SRM 53-30-00 FIG 6 VOL 1 AND TREATED AREA IAW SRM 51-21-01 VOL 2. 2L73 4F A22WE 20051122000612005112200061WP 2005 11 22 05FDEA03823 120051115A5280 REPAIR DOUG DC10 DC1010 3022110WP MLG DOOR PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 JUST ABOVE FWD NOSE LANDING GEAR DOOR BETWEEN STA 490 AND 555 LT SIDE, FOUND FLUSH DOUBLER OF APROX 62 X 25 INCH. PERFORMED A GVI OF REPAIRS IAW CONTINENTAL AIRLINES EC/RA 253C038, 253C039, 253C040, 253C042, 253C044 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001. 2L73 4F A22WE 20051122000692005112200069NM 2005 11 22 FE5F200500003 120051101A5711 SPAR DOUG MD80 MD83 3023681NM WS 188.5-194.5 RCORRODED B FE5FK NONE O OTHER ININSP/MAINT 1 WP03B8023 49952 DURING THE C12 CHECK, PERFORMING THE TASK 0314 AND CPCP CARD 16-57301, AT RT WING REAR SPAR LOWER FOUND 6 X 1 INCH MAX D=0.150 INCH CORROSION AT XRS=188.5 TO 194.5. REQUEST BOEING ASSISTANCE AND IAW BOEING'S RESPONSE REPAIR THE CORROSION AREA. MANUFACTURE ISSUED FAA FORM 8100-9, AND APPROVED REPAIR PROCESS IAW ENGINEER COMMITTED EO-MD80-57-0095 REPAIRED. 2L72 4F RT 20051122000702005112200070NM 2005 11 22 SB05147 120051116A335003600570010 FUSE BOEING737 737301 1384611NM POWER SUPPLY BLOWN A USAAK NONE O OTHER ININSP/MAINT 1 EA19355US 23558 MAINTENANCE REPORTED THE AFT LEFT EXTERIOR EMERGENCY LIGHT AND THE SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 22 AND 23 INOPERATIVE. MAINTENANCE RELAMPED THE EXTERIOR EMERGENCY LIGHT AND REPLACED A BLOWN FUSE ON POWER SUPPLY M1197. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20051122000732005112200073NM 2005 11 22 SWAA053653 120051117A3350207377 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29406WN 27894 EEPLS TRACK LENS MISSING AT FWD END. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20051122000752005112200075NM 2005 11 22 SWAA053655 120051117A53306545768 SKIN BOEING737 7375H4 138449DNM BS 361.5 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29507SW 24184 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 361.5, STR 17L. REPAIRED SKIN PER BFG ER. 2L72 4F RTA16WE 20051122000782005112200078NM 2005 11 22 SWAA053658 120051117A53156545812 FLOORBEAM BOEING737 7375H4 138449DNM BS 328 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29512SW 24189 DURING SCHEDULED 1/2D CHECK, FOUND CABIN FLOORBEAM CORRODED AT BS 328, BL 0. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20051122000792005112200079NM 2005 11 22 SWAA053659 120051117A53156545815 FLOORBEAM BOEING737 7375H4 138449DNM BS 344 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29512SW 24189 DURING SCHEDULED 1/2D CHECK, FOUND CABIN FLOORBEAM CORRODED AT BS 344, BETWEEN BL 0 TO LBL 7.REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20051122000812005112200081NM 2005 11 22 SWAA053661 120051117A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 578 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 578, STR 11R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051122000842005112200084SO 2005 11 22 RAIA00511021 120051116A3097 WIRE EMB 145 EMB145 3260210SO TAT HEATER DAMAGED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03821HK 145068 FLY 5575-STL-TAT 1 AND 2 HEAT INOP. MAINTENANCE REPAIRED WIRING TO RELAY. 2L72 4F RTT00011AT 20051122000862005112200086SO 2005 11 22 RAIA00511026 120051119A3397 CONNECTOR EMB 145 EMB145 3260210SO EMERGENCY LIGHT DIRTY A RAIAK NONE O OTHER ININSP/MAINT 1 CE03802HK 145066 PRE-FLIGHT - PIT - EMERGENCY LIGHT INOP. MAINTENANCE CLEANED CONNECTOR ON EMERGENCY LIGHT ASSEMBLY. 2L72 4F RTT00011AT 20051122000872005112200087SO 2005 11 22 RAIA00511020 120051115A3350 POWER SUPPLY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT MALFUNCTIONED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03812HK 145373 POST - FLIGHT - AUS - EICAS MEESAGE "EMERGENCY LIGHTS NOT ARMED". ALSO UNABLE TO GET EMERGENCY LIGHTS TO COME ON. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY POWER SUPPLY. 2L72 4T RTT00011AT 20051122000882005112200088SO 2005 11 22 RAIA00511023 120051117A3350 LIGHT EMB 145 EMB145LR 3260212SO OVERWING INOPERATIVE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03845HK 14500842 PRE-FLIGHT INSPECTION - IAD - RT OVERWING EMERGENCY LIGHT INOP. MAINTENANCE DEFERRED THE OVERWING EMERGENCY EXIT LIGHT. 2L72 4T RTT00011AT 20051122000902005112200090EU 2005 11 22 RAIA00511025 120051119A3397 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT UNSECURE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03565HK 41082 POST FLIGHT - STL- EMERGENCY LIGHTS AT LEFT HAND EXIT DOOR WON'T TURN ON. MAINTENANCE RESECURED CONNECTOR. 2L72 4T RTA41NM 20051122000912005112200091NM 2005 11 22 AWXA200501423 120051118A2560P4010021 BATTERY BOEING757 7572S7 1384962NM FLASHLIGHT INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28906AW 23568 SEA - EEL - DURING OVERNIGHT CHECK, MAINTENANCE FOUND EMERGENCY FLASHLIGHT AT RT MID CABIN FLIGHT ATTENDANT STATION INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RT MID CABIN FLIGHT ATTENDANT FLASHLIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA2NM 20051122000942005112200094NM 2005 11 22 AWXA200501427 120051028A5343656717217 ATTACH FITTING BOEING737 7373S3 1384711NM LT MLG CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 MCN - DURING C13 CHECK, DISCOVERED CORROSION ON THE LT MAIN LANDING GEAR AFT STABILIZER BEAM ATTACH FITTING. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 57-20-90-1A2 FIG 101. MAINTENANCE REMOVED AND REPLACED THE LT MLG AFT STABILIZER ATTACH FITTING IAW BOEING 737-300 AMM 20-50-11-2 FIG 202. 2L72 4F RTA16WE 20051122000952005112200095NM 2005 11 22 AWXA200501428 120051027A5754 WEDGE BOEING737 7373S3 1384711NM NR 1 SLAT DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 245 24060 MCN - DURING C13 CHECK DISCOVERED DISBOND AREA ON THE UPPER AND LOWER SURFACE OF THE NR 1 SLAT WEDGE, INBOARD END. MAINTENANCE REMOVED THE DISBOND SKIN AND CORE ON THE NR 1 SLATE WEDGE IAW BOEING 737-300 SRM 51-70-10-2R4 REPAIR 4. FABRICATED DOUBLER AND CORE IAW BOEING 737-300 SRM 51-70-10-2R4. BONDED REPAIR PARTS TO THE NR 1 SLAT WEDGE, INBOARD END IAW BOEING 737-300 SRM 51-70-10-2R4. 2L72 4F RTA16WE 20051122000962005112200096NM 2005 11 22 SWAA053664 120051117A53206551698 SPLICE BOEING737 7373H4 1384600NM BS 908 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER SPLICE CRACKED AT BS 908, STR 4L. REPAIRED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20051122000972005112200097NM 2005 11 22 SWAA053665 120051117A55446549837 ANGLE BOEING737 7373H4 1384600NM RUDDER HINGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 DURING SCHEDULED D CHECK, FOUND VERTICAL STAB LT ANGLE CRACKED AT NR 7 RUDDER HINGE. REPAIRED ANGLE PER SRM. 2L72 4F RTA16WE 20051122001012005112200101WP 2005 11 22 UPS05845797 120051022A53205612298341 WEB DOUG DC8 DC873F 302199FWP FS 93 RBL30 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE:C1 COCKPIT SUBFLOOR STA -93 RBL 30 STATIC TUBE CONNECTING POINT PLATE HAS 4 SHEARED HEAD FASTENERS AND POSSIBLE CORROSION UNDER THE PLATE. REPAIRED IAW SAA SK 813-823093 AND UPS EO DC8-5310-23264-A. 2L74 4F RT4A25 20051122001022005112200102WP 2005 11 22 UPS05845798 120051018A53115654671501 FRAME DOUG DC8 DC873F 302199FWP FS 1240 L35L CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE:C1 FRAME HEAVY CORRODED AT STA 1240 L35L. REPAIRED FUSELAGE FRAME IAW SAA SK813-822550 REV A AND UPS EO DC8-53-20516 A. 2L74 4F RT4A25 20051122001032005112200103WP 2005 11 22 UPS05845800 120051019A53205644011501 WEB DOUG DC8 DC873F 302199FWP FS 857 RBL0-23 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE:C1 MAIN CABIN CENTER WING BOX AT STA 857 RBL 5 HAS HEAVY CORROSION ON THE UPPER REAR SPAR CAP. REPAIRED WING REAR SPAR TO FUSELAGE SHEAR WEB ATTACH ANGLE AND WING SKIN SPLICE DOUBLER IAW SAA SK 813-822678 AND UPS EO DC8-57-20145. 2L74 4F RT4A25 20051122001062005112200106NM 2005 11 22 AWXA200501418 120051107A5330146N3430 SKIN BOEING757 7572S7 1384962NM BS 1520-1540 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28904AW 23566 GYR - DURING C10 CHECK DISCOVERED CORROSION UNDER ANTENNA, ON FUSELAGE SKIN, FROM BS 1520 TO BS 1540 AND FROM STR 29L TO STR 30L, JUST AFT OF AFT CARGO PIT DOOR. REMOVED CORROSION FROM FUSELAGE SKIN AND FOUND TO BE OUT OF LIMITS IAW BOEING 757-200 4M 53-00-01-1A. MAINTENANCE CUT OUT DAMAGED SKI IAW BOEING 757-200 SRM 51-00-01-2R FIG 201. FABRICATED DOUBLER IAW BOEING 737-300 SRM 53-00-01-2R3. MAINTENANCE INSTALLED FABRICATED REPAIR PARTS ON FUSELAGE SKIN, FROM BS 1520 TO BS 1540 AND FROM STR 29L TO STR 30L, JUST AFT OF AFT CARGO PIT DOOR IAW BOEING 757-200 SRM 53-00-01-2R. 2L72 4F RTA2NM 20051122001092005112200109NM 2005 11 22 AWXA200501421 120051117A2150 A/C PACK BOEING737 7373U3 13844CCNM RIGHT NOISY A AWXAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 WP28335AW 28740 CREW REPORTED HEARING LOUD HUMMING/GRINDING NOISES DURING TAKEOFF AND CLIMB. CREW DIVERTED INTO PHX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND NOISE COMING FROM THE RT PACK TURBO FAN. THE RT PACK WAS PLACED ON MEL. MEL WAS CLEARED, MAINTENANCE REMOVED AND REPALCED THE R/H PACK, TURBO FAN IAW AMERICA WEST AIRLINES TASK CARD R2C21002. OPERTATIONAL CHECKS WERE GOOD. VENDOR CONFIRMED FAILURE. UNIT HAD IMPELLER, HOSING AND INLET DAMAGE. ALSO SHOWED SIGNS OF RUBBING ON HOUSING AND FOUND DAMAGE DUE TO POSSIBLE BEARING FAILURE. THE UNIT WAS OVERHAULED PER HONEYWELL CMM 21-20-38 REV.4 2L72 4F RTA16WE 20051122001102005112200110NM 2005 11 22 ASAA0540493 120050920A532065C807351 SILL BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU BS 987 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02793AS 28888 CORROSION ON RT MOPSILL AT BS 987+ 10 INCHES, RBL 48. REMOVED AND REPLACED RT MOPSILL AT BS 987 + 10 INCHES, RBL 48 IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051122001122005112200112NM 2005 11 22 05FDEA03916 120051119A5347 SEAT TRACK DOUG MD11 MD11 3023602NM BS 830 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 MAIN DECK CABIN, STA 830 LBL 26 SEAT TRACK FOUND CORRODED. REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-70-00. TRIMMED AS PER SRM 53-70-00. SPLICE FABRICATED AND INSTALLED AS PER SRM 53-70-00. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051122001142005112200114NM 2005 11 22 05FDEA03918 120051119A5347 SEAT TRACK DOUG MD11 MD11 3023602NM BS 6-100-1149 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 FOUND MAIN DECK CABIN, STA 6-100 TO 1149 LBL 8 SEAT TRACK FOUND WITH CORROSION. CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2L73 4F RTA22WE 20051122001152005112200115NM 2005 11 22 05FDEA03919 120051119A5347 SEAT TRACK DOUG MD11 MD11 3023602NM BS 1136 UNDAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 MAIN DECK CABIN, STA 1136 LBL 8 SEAT TRACK FOUND WITH CORROSION. REMOVED AS PER SRM 51-21-01 VOLUME II AND FOUND WITHIN LIMIT AS PER SRM 53-70-00 2L73 4F RTA22WE 20051122001172005112200117NM 2005 11 22 05FDEA03921 120051119A5347 SEAT TRACK DOUG MD11 MD11 3023602NM BS 859-879 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 MAIN DECK CORROSION FOUND ON SEAT TRACK UPPER FLANGE BETWEEN STA 859 TO 879 AT X=8.5. REPAIR CARRIED OUT IAW SRM 53-70-00. 2L73 4F RTA22WE 20051122001202005112200120NM 2005 11 22 05FDEA03859 120051117A5520 RIB BOEING727 72722 1384002NM ELEVATOR HINGE MISLOCATED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25188FE 19081 WHILE WORKING CARD N01365, FOUND RT NR 5 ELEVATOR HINGE RIB MISLOCATED. REMOVED AND REPLACED RT NR 5 ELEVATOR HINGE RIB PER EA 7-5510-91413. 2L73 4F A3WE 20051122001232005112200123NM 2005 11 22 05FDEA03912 120051119A5347 SEAT TRACK DOUG MD11 MD11 3023602NM BS 839 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 MAIN DECK, CORROSION FOUND ON SEAT TRACK CROWN AREA ADJ TO STA 839 AT X=27.5. REPAIR CARRIED OUT AS PER SRM 53-70-00. 2L73 4F RTA22WE 20051122001242005112200124NM 2005 11 22 05FDEA03913 120051119A5347 SEAT TRACK DOUG MD11 MD11 3023602NM BS 899-999 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 MAIN DECK CABIN, STA 899, 939, 959 AND 999 RBL 8 SEAT TRACK FOUND CORROSION. REPAIRED AS PER SRM 53-70-00. 2L73 4F RTA22WE 20051122001252005112200125NM 2005 11 22 05FDEA03914 120051119A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 CABIN, SEAT TRACK BASE ADJ TO STA 1825 APPROX X = -21 FOUND WITH CORROSION. CARRIED OUT REPAIR AS PER SRM 53-70- 00 VOLUME I FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2L73 4F RTA22WE 20051122001262005112200126EU 2005 11 22 UPS05145802 120051116A5220 DIAPHRAGM AIRBUSA300 A300F4622R 3930360EU FWD DOOR MALFUNCTIONED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01134UP 0817 SLIDE ALMOST DEPLOYED. DEFERRED MAIN ENTRY DOOR PER MEL 52-11-01-3. M314029 PLACARD INSTALLED AS MAIN CABIN DOOR SLIDE INOP. REMOVED AND REPLACED FWD DOOR DAMPER PERCUSSION MECHANISM DIAPHRAM PER AMM 52-10-14-3. PLACARD REMOVED. 2L72 4F RTA35EU 20051122001282005112200128WP 2005 11 22 UPS05845786 120051020A53403779659U501 FITTING DOUG DC8 DC873F 302199FWP FS 900 L4L CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE:C1 LONGERON END FITTING POSSIBLE CRACK AT STA 900 L4L. REMOVED AND REPLACED LONGERON END FITTING IAW SRM 51-1-21 AND 51-1-20D. 2L74 4F RT4A25 20051122001312005112200131WP 2005 11 22 UPS05845790 120051019A53126453329 PRESSURE PANEL DOUG DC8 DC873F 302199FWP FS 857 RBL 40 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE:C1 MAIN CABIN SUB FLOOR, FUEL DUMP CHUTE BRACKET UNDER THE PLATE HAS HEAVY CORROSION AT 857 RBL 40. REMOVED DAMAGED AREA AND REPAIRED IAW SAA SK 813-822556 AND UPS EO DC8- 5310-23251-A. 2L74 4F RT4A25 20051122001332005112200133WP 2005 11 22 UPS05845791 120051018A5312 BULKHEAD DOUG DC8 DC873F 302199FWP FS 1766 L11R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE:C1 MAIN CABIN AFT PRESSURE BULKHEAD CRACKED L11R RBL 48. CUT OUT DAMAGED AREA 2 AND FABRICATED AND INSTALLED FINGER DOUBLER, DOUBLER AND 2 FILLER IAW SRM 51-1-20D, 51-3-0, 51-1-21 AND TR- 53-194. 2L74 4F RT4A25 20051122001352005112200135EU 2005 11 22 05FDEA03896 120051118A5340 FITTING AIRBUS300 A300B4622R 3930312EU ZONE 100 INTERFERENCE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25721FD 477 COMPLY WITH EA6-5310-92354, FUSELAGE-SB53-6111- FR46 FITTING/DOUBLER INTERFERENCE. COMPLIED WITH EA 6-5310-92354. 2L72 4F RTA35EU 20051122001372005112200137EA 2005 11 22 SWIA200515855 120050722A5522 SKIN CNDAIRCL600 CL6002B19 1900309EA LT ELEVATOR DAMAGED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07406SW 7030 LT ELEVATOR EXTERNAL LWR SKIN 2 PLACES TRANSVERSE SMOOTH CREASES 6" LENGTH BY 0.011" D - APPROX 28" AND 39" FROM ELEV O/B TIP AND 6" FROM T/E (AREA FLAGGED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ SRM 55-20-00 FIG 203. 2L72 4F RTA21EA 20051122001392005112200139EA 2005 11 22 SWIA200515857 120050719A5712 ANGLE CNDAIRCL600 CL6002B19 1900309EA LT WW CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07412SW 7101 LT WHEEL WELL BAT ANGLE CRACKED, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR PARTS TO LT WHEEL WELL BAT ANGLE IAW CRJ200 SRM 51-42-06 PG 11 AND 51-42-21 PG 17. 2L72 4F RTA21EA 20051122001412005112200141EA 2005 11 22 SWIA200515859 120050811A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07447SW 7677 280 BULKHEAD FLOOR SUPPORT STRUCTURE CLIPS AT LBL 9 AND RBL 9 ARE CRACKED, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW CLIPS IAW CRJ200 SRM 51-42-11. 2L72 4F RTA21EA 20051122001432005112200143EA 2005 11 22 SWIA200515861 120050811A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA BS 484 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07447SW 7677 MAIN CABIN FS484 RT BL 36WL 73.5 CLIP CRACKED, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW 'CLIP' PN 601R-53-41-059-2 AT FS 484 RT BL-36 WL IN MAIN CABIN IAW CRJ200 601R-53-41-059 REV 'A'. 2L72 4F RTA21EA 20051122001452005112200145EA 2005 11 22 SWIA200515863 120050811A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07447SW 7677 MAIN AVIONICS COMPARTMENT STA280 BL 10.5 WL 74.0 CLIP CRACKED, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW ANGLE AND FILLER IAW CRJ200 SRM 51-42-21. 2L72 4F RTA21EA 20051122001472005112200147EA 2005 11 22 SWIA200515865 120051114A2760C13045BA04 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA SPOILERS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07703SK678 678 10139 SPOILER/STAB FAILED. REPLACED NR 2 SSCU IAW CRJ MM ATA CHAPT 27-61-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051122001492005112200149WP 2005 11 22 05FDEA03885 120051118A5753 REPAIR DOUG DC10 DC1030 3023501WP TE FLAPS PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 FOUND LT WING OUTBOARD FLAP LWR SKIN FOUND A DOUBLER 6" BY 4" AT XOF 467. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 57-00-01 FIG 4 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2 E3. 2L73 4F A22WE 20051122001512005112200151NM 2005 11 22 SWAA053678 120051119A53206582671 WEB BOEING737 7373H4 1384600NM BS 665 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE BEADED WEB CRACKED AT BS 665, LBL 30 TO LBL 35. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20051122001522005112200152NM 2005 11 22 SWAA053679 120051119A335020131A BATTERY PACK BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29341SW 24091 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT ROW 16 DEF. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20051122001532005112200153NM 2005 11 22 SWAA053680 120051118A53306545774 SKIN BOEING737 7373H4 1384600NM BS 749.5 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29353SW 24889 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 749.50, STR 18L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051122001542005112200154NM 2005 11 22 SWAA053681 120051118A53306545774 SKIN BOEING737 7373H4 1384600NM BS 514 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29353SW 24889 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 514.750, STR 16R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051122001552005112200155NM 2005 11 22 SWAA053682 120051117A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29452WN 29846 FWD END OF EEPLS TRACK COVER LOOSE. SECURED COVER PER MM. 2L72 4F RTA16WE 20051122001562005112200156NM 2005 11 22 SWAA053683 120051119A53116520723 FRAME BOEING737 7375H4 138449DNM FWD CARGO CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29507SW 24184 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, FWD FRAME LOWER CORNER. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20051122001572005112200157NM 2005 11 22 SWAA053684 120051119A53116547959 FRAME BOEING737 7375H4 138449DNM AFT CARGO CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29507SW 24184 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT AFT CARGO DOOR CUTOUT, FWD FRAME NR 5 STOP FITTING. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051122001582005112200158NM 2005 11 22 SWAA053685 120051119A3397W115055920 WIRE BOEING737 7375H4 138449DNM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29507SW 24184 DURING SCHEDULED SPECIAL VISIT, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REPAIRED WIRE NR W1150-559-20 PER WDM AND MM. 2L72 4F RTA16WE 20051122001592005112200159NM 2005 11 22 SWAA053686 120051116A32106567963 LINK BOEING737 7375H4 138449DNM RT MLG BROKEN A SWAAO OTHER O OTHER LDLANDING 1 SW29510SW 24187 EXTREME VIBRATION FELT AFTER LANDING. FOUND RT MLG UPPER TORSION LINK BROKEN. RT MLG SHIMMY DAMPNER SHAFT BENT. RT MLG LOWER STRUT WARPED. NR 3 AND NR 4 MLG TIRES DAMAGED. NR 1, NR 3, NR 4 AND NR 6 L/E SLATS DAMAGED. REMOVED AND REPLACED RT MLG ASSY, RT MLG UPPER AND LOWER TORSION LINKS, RT MLG SHIMMY DAMPNER, RT MLG LOWER STRUT, NR 3 AND NR 4 MLG TIRE/WHEEL ASSY AND NR 1, NR 3, NR 4 AND NR 6 L/E SLATS PER MM. 2L72 4F RTA16WE 20051122001602005112200160NM 2005 11 22 AWXA200501403 120051028A531265175829 BULKHEAD BOEING737 7373S3 1384711NM BS 178 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 MCN - DURING C13 CHECK DISCOVERED WEB CRACKED, .75 INCHES, AT BS 178, WL 230 AND BL 17.1R. MAINTENANCE CUTOUT DAMAGED PORTION OF BULKHEAD WEB IAW BOEING 737-300 SRM 53-10-08-2R12. FABRICATED DOUBLER AND FILLER IAW BOEING 737-300 SRM 53-10-08-2R12. INSTALLED FABRICATED REPAIR PARTS BS 178, WL 230 AND BL 17.1R IAW BOEING 737-300 SRM 53-10-08-2R12. 2L72 4F RTA16WE 20051122001622005112200162NM 2005 11 22 SWAA053688 120051119A53116520723 FRAME BOEING737 7375H4 138449DNM FWD CARGO CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29512SW 24189 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, AFT FRAME NR 2 STOP FITTING. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051122001642005112200164NM 2005 11 22 SWAA053690 120051118A531165C25229 FRAME BOEING737 7373H4 1384600NM BS 727D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R TO STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051122001662005112200166NM 2005 11 22 SWAA053692 120051118A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 706 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051122001682005112200168 2005 11 22 SWAA053694 420051118A25656557463 BRACKET BOEING737 7373H4 1384600NM GIRT BAR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED D CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT LOWER FLOOR BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER SRM. 2L72 4F RTA16WE 20051122001702005112200170NM 2005 11 22 SWAA053696 120051117A5753 SKIN BOEING737 7373H4 1384600NM LT WING FOREFLAPDELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29648SW 27718 DURING SCHEDULED C4 CHECK, FOUND LT WING T/E INBD FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM. 2L72 4F RTA16WE 20051122001722005112200172 2005 11 22 SWAA053698 420051119A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29763SW 27877 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. SLIDE DID NOT DEPLOY. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20051122001732005112200173NE 2005 11 22 SWAA053699 220051117A7230 COMPRESSOR BOEING737 7377H4 1384404NM GE CFM56 CFM56* 13802NE RT ENGINE STALLED A SWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW29782SA 29808 876598 AIR TURNBACK/DECLARED EMERGENCY, 2 LOUD BANGS HEARD, ALONG WITH MODERATE TO SEVERE VIBRATIONS FELT FROM NR 2 ENGINE. NR 2 ENGINE FUEL FLOW ERRATIC. ALL OTHER INDICATIONS NORMAL. FLAME SEEN FROM NR 2 ENGINE EXHAUST. REMOVED AND REPLACED NR 2 EEC, T12 SENSOR, 5TH STAGE PNEUMATIC BLEED CHECK VALVE AND N2 SENSOR PER MM. DURING TEST FLIGHT FOR COMPRESSOR STALL, NR 2 ENGINE STALLED TWICE DURING CLIMB. REMOVED AND REPLACED NR 2 ENGINE PER MM. 2L72 4F4 FRTA16WE E2GL 20051122001752005112200175WP 2005 11 22 05FDEA03886 120051118A5730 REPAIR DOUG DC10 DC1030 3023501WP LT WING PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 FOUND LT WING L/E EXT SKIN FOUND A FLUSH DOUBLER DIMENSIONS 3" BY 2" AT STA XORS 512. PERFORMED A GVI OF REPAIR IAW SRM 57-10-00 FIG 39 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001-2P. 2L73 4F A22WE 20051122001772005112200177WP 2005 11 22 05FDEA03888 120051118A5310 REPAIR DOUG DC10 DC1030 3023501WP L3 DOOR FRAME PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 MAIN CARGO COMPT L3 JAMB DOOR AT STA 1256 BY 92 AND Z-14 FOUND 1 REPAIR DOUBLER 7" BY 8". PERFORMED A INSPECTION ON REPAIR IAW SRM 53-50-00 FIG 19 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001-2P E3 AND RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VOL 2 PAR 33. 2L73 4F A22WE 20051122001792005112200179WP 2005 11 22 05FDEA03890 120051118A5730 REPAIR DOUG DC10 DC1030 3023501WP LT WING UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 LT WING INBOARD FLAP FOUND A FLUSH DOUBLER 3" BY 5.25" ON LWR SKIN AT STA XIFH 177. PERFORMED A GVI OF REPAIR IAW SRM 57-00-01 FIG 4 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001-2P E3. RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VOL 2 PAR 3. 2L73 4F A22WE 20051122001812005112200181WP 2005 11 22 05FDEA03892 120051118A5730 REPAIR DOUG DC10 DC1030 3023501WP LT WING UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 LT WING INBOARD FLAP FOUND DOUBLER 5" BY 5" ON UPPER SKIN AT STA XIFH 177. PERFORMED AGVI OF REPAIR IAW SRM 57-00-01 FIG 64 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001-2P E3 RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VOL 2 PAR 3. 2L73 4F A22WE 20051122001832005112200183WP 2005 11 22 05FDEA03894 120051118A5751 REPAIR DOUG DC10 DC1030 3023501WP LT WING AILERON PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 LT WING OUTBOARD AILERON UPPER SURFACE FOUND A REPAIR 5" BY 2.75" ON SKIN AT STA XOA 997. PERFORMED A GVI OF REPAIR IAW SRM 57-00-01 FIG 4 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001-2P E3. 2L73 4F A22WE 20051122001852005112200185NM 2005 11 22 SWAA053668 120051118A53156546811 FLOORBEAM BOEING737 7373H4 1384600NM BS 986 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D CHECK, FOUND CABIN FLOORBEAM CORRODED AT BS 986.5, RBL 45. REPAIRED FLOORBEAM PER BFG ER AND SRM. 2L72 4F RTA16WE 20051122001862005112200186NM 2005 11 22 SWAA053669 120051118A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM BS 344 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 344, STR 8R. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2L72 4F RTA16WE 20051122001882005112200188NM 2005 11 22 SWAA053671 120051118A53226546569 SHEAR TIE BOEING737 7373H4 1384600NM BS 967 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 967, STR 4L TO STR 7L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051122001902005112200190NM 2005 11 22 SWAA053673 120051118A53116516301 FRAME BOEING737 7373H4 1384600NM BS 188 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 188, RT SIDE, WL 207. REPAIRED STUB FRAME PER SRM. 2L72 4F RTA16WE 20051122001922005112200192NM 2005 11 22 SWAA053675 120051118A53116516301 FRAME BOEING737 7373H4 1384600NM BS 188 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 188, LT SIDE, WL 208. REMOVED AND REPLACED STUB FRAME PER SRM. 2L72 4F RTA16WE 20051122001952005112200195NM 2005 11 22 ASAA0540455 120050909A531165C323516 FRAME BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU BS 500E DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02793AS 28888 FWD CARGO BAY FRAME IS DENTED. REMOVED DAMAGED SECTION OF FRAME, FABRICATED REPAIR PARTS AND INSTALLED IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051122001982005112200198NM 2005 11 22 ASAA0540427 120050822A57536546430167 WEDGE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU TE FLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02779AS 25111 RT IB MID FLAP T/E WEDGE 7420R HAS SEVERAL DINGS. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLERS IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051122001992005112200199NM 2005 11 22 ASAA0540426 120050822A57536546430167 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU LT TE FLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02779AS 25111 LT IB FORE FLAP DENTED, DELAMINATED ON LOWER SKIN AT CENTER TRACK. REMOVED DAMAGE, FABRICATED AND INSTALLED SKIN SECTION AND DOUBLER IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051122002002005112200200 2005 11 22 CALA0500390 420051107A2330RDAA341305 ELECTRICAL BOX BOEING767 767424ER 1385270NM GE CF6 CF680 30025NE SEAT 19DEF OVERHEATED A CALAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SW2768061 29456 FLIGHT CREW REPORTED SMOKE COMING FROM BELOW SEAT 19E WHILE ENROUTE FROM AMS TO EWR. THE SMOKE LASTED FOR ONLY ABOUT 15 SECONDS. AN EMERGENCY DECLARED AND AIRCRAFT LANDED AT EWR W/O INCIDENT. MECHANIC FOUND THE DSEB (DIGITAL SEAT ELECTRONIC BOX) AT SEAT GROUP 19DEF HAD A BURNED SMELL BUT NO VISUAL EVIDENCE OF FIRE. THE DSEB WAS REMOVED AND REPLACED IAW MM 23-38-55. THE CONNECTORS WERE VISUALLY INSPECTED AND LOOKED GOOD. OPS CHECKS WERE NORMAL. INITIAL EXAMINATION OF THE UNIT REVEALED THAT THE COOLING FANS APPEARED TO BE BLOCKED. THERE WAS DEBRIS (PARTICLES OF FOOD) ON TOP OF AND AROUND THE DSEB. MODIFICATIONS PLAN TO BE INCORPORATED INTO THE UNITS TO HELP PREVENT THIS TYPE OF FAILURE IN THE FUTURE. 2L72 4F4 FRTA1NM E13NE 20051123000012005112300001NM 2005 11 23 ASAA0540494 120050920A531065C335831 SHEAR WEB BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU BS 998 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02793AS 28888 SHEAR WEB CRACKED AT BSTA 998, RBL 41, WL 208. REMOVED AND REPLACED SHEAR WEB AT BSTA 986.5 - 1016, RBL 29-41, WL 208 IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051128000012005112800001NM 2005 11 28 QXEA200501550 120051030A5347 SEAT TRACK BOMBDRDHC8 DHC8402 1390042NM CABIN CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX: RT OUTBOARD SEAT TRACK HAS LIGHT CORROSION AT FWD 2 INCHES OF TRACK. MAINTENANCE REPAIRED IAW RD 8/4-53-884 AND NDTM PART 6, 51-00-02-250-801. 2H72 4T RTA13NM 20051128000042005112800004NM 2005 11 28 SCNA05012 120051121A3350 FUSE BOEING737 7378Q8 13844BXNM BATTERY CHARGER FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15809SY 30683 ON LAYOVER CHECK, MAINTENANCE FOUND EMERGENCY LIGHTS INOP AT SEATS 12, 13, & 14 LEFT SIDE. REPLACED FUSES ON CHARGER AND OPERATION CHECKED NORMAL. 2L72 4F RTA16WE 20051128000052005112800005WP 2005 11 28 ABXA050285 120051105A213021011403 CONTROLLER DOUG DC9 DC941 302207NWP CABIN PRESSURE DEFECTIVE A ABXAO OTHER J WARNING INDICATION DEDESCENT 1 GL23964AX843 47781 CABIN PRESSURIZATION LOSS AT TOP OF DESCENT. CABIN PRESSURE EMERGENCY LIGHT ILLUMINATED, EMERGENCY PROCEDURE COMPLETED. NO FURTHER INCIDENT. PERFORMED BITE TEST PROCEDURES AND THE FOWARD CABIN PRESSURE CONTROLLER FAILED TEST. REPLACED FORWARD CABIN PRESSURE CONTROLLER IAW DC9 AMM 21-32-00-2-0501. 2L72 4F A6WE 20051128000082005112800008NM 2005 11 28 USAA051410 120051122A575465C26601179 SKIN BOEING737 737301 1384611NM LE SLAT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19591US 23936 LWR SURFACE, AFT FASTENER ROW AT OUTBOARD END TO 20.750 INCH INBOARD CRACKED. MAJOR REPAIR, INSTALLED DOUBLER IAW SRM 57-43-01 REPAIR 6. 2L72 4F RTA16WE 20051128000102005112800010NM 2005 11 28 USAA051408 120051122A52306546921225XE SKIN BOEING737 7374B7 1384702NM FWD CARGO DOOR DEFECTIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19779AU 24996 FWD CARGO DOOR, OUTSIDE SKIN, CENTER SECTION AREA DEFECTIVE. REPAIRED SRM 52-00-01, INSTALLED DOUBLER, DEFECT SIZE: 14 INCHES X 20 INCHES. 2L72 4F RTA16WE 20051128000112005112800011EU 2005 11 28 USAA051421 120051122A5321D5367160600000 FLOORBOARD AIRBUSA321 A321211 3930370EU CABIN CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19161UW 1403 AT 41 INCHES FROM END, 64 INCHES FROM OPP END, 4 INCHES FROM EDGE, 15 INCHES FROM OPP EDGE CRACKED. FILLED AND INSTALLED PRECURED DOUBLER IAW SRM 53-02-00 FIG 203. DEFECT SIZE: 5 INCHES. 2L72 4F RTA28NM 20051128000132005112800013EU 2005 11 28 USAA051419 120051122A5310D5347218820200 BEAM AIRBUSA321 A321211 3930370EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19161UW 1403 BEAM Y1292 FROM FRAME 66-68; CORROSION LEVEL 1; TASK JA-260-53500. REMOVED AND REPLACED IAW SRM 51-72-11. DEFECT SIZE: 2 INCHES X 4 INCHES. 2L72 4F4 FRTA28NM E2GL 20051128000142005112800014EU 2005 11 28 USAA051418 120051122A5310D5347209001100 BEAM AIRBUSA321 A321211 3930370EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19161UW 1403 BEAM - Y1292 FROM FRAME 66 THRU FRAME 68; CORROSION LEVEL 1; TASK JA-260-53500. REMOVED AND REPLACED IAW SRM 51-72-11. DEFECT SIZE: 2 INCHES X 6 INCHES. 2L72 4F4 FRTA28NM E2GL 20051128000162005112800016EU 2005 11 28 USAA051416 120051122A5315D5311281820401 FLOORBEAM AIRBUSA321 A321211 3930370EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19161UW 1403 BEAM Y254 FWD CABIN, DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-72-11; CORROSION LEVEL 2; TASK JA-220-53500. DEFECT SIZE: .5 INCH X .5 INCH. 2L72 4F4 FRTA28NM E2GL 20051128000172005112800017NM 2005 11 28 USAA051415 120051122A5330143N361115 SKIN BOEING757 757225 1384959NM RROYCERB211 RB211* 54555NE BS 1300 GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19602AU 22196 STA 1300 STR 29R GOUGED. CUT OUT DAMAGE AND REPAIRED IAW EA 97045. DEFECT SIZE: .15 INCH, L X .10 INCH, W X .031 INCH D. 2L72 4F4 FRTA2NM A12EU 20051128000182005112800018NM 2005 11 28 CALA0500415 120051122A3320BV031120333 SOCKET BOEING757 757224 1384958NM CABIN LIGHTS SHORTED A CALAHA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW2714102 27292 SMOKE BEGAN COMING FROM A CABIN CEILING FLUORESCENT FIXTURE LIGHT AT SEAT 24A (MID LEFT CABIN) WHILE ON CLIMBOUT OF TPA. A TECHNICIAN ON THE FLIGHT REMOVED THE CEILING PANEL, REMOVED THE LIGHT BULB, AND THE SMOKE CEASED. FOUND THE SOCKET WHERE THE BULB PLUGS INTO THE LIGHT ASSEMBLY BURNED. THE AIRCRAFT RETURNED TO TPA WHERE IT LANDED WITHOUT INCIDENT. THE LIGHT SOCKET FOR THE CEILING FLUORESCENT LIGHT AT 24A WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD IAW MM 33-21-00. NO OTHER DEFECTS WERE NOTED. 2L72 4F RTA2NM 20051128000212005112800021NM 2005 11 28 USAA051412 120051122A5754 SKIN BOEING737 737301 1384611NM GE CFM56 CFM56* 13802NE NR 2 SLAT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19591US 23936 LWR SURFACE, AFT ROW OF FASTENERS AT ACTUATOR CRACKED. MAJOR REPAIR, INSTALLED DOUBLER IAW SRM 57-43-01 REPAIR 6. 2L72 4F4 FRTA16WE E2GL 20051128000222005112800022NE 2005 11 28 QXEA200501536 220051117A73145008269H PUMP DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE HP FUEL MALFUNCTIONED A QXEAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 NM09351PH1567610759 490 PCEAG0047 AT 500 FT AGL ON CLIMBOUT, RUNWAY 4 NR 1 ENGINE FAILED WITH AN AUTOFEATHER AND POWER OPTIMUM ON NR 2 ENGINE. COMPLETED ENGINE FAILURE CHECKLIST ON IAC, NH WAS NOT BELOW 60 PERCENT BUT NP WAS BELOW 300 CONTINUED WITH SHUTDOWN OF NR 1 ENGINE. NO DEFECTS OR SPILLS OBSERVED ON POST FLIGHT WALKAROUND. MAINTENANCE PERFORMED SPECIAL INSPECTION PER DHC8-200 MM 05-50-76-210-801 PARAGRAPH B, ON GROUND RUN FOUND NR 1 ENGINE CYCLING IN NH, TQ, NL AND NP. REPLACED MFC AND FUEL PUMP PER MTC 97320-001, ALSO INSPECTED HP ON LP FUEL FILTERS FOR CONTAMINATION, INSPECTED NR 1 ENGINE P3 AND SWAPPED ALL FUEL TANKS. FUEL CONTROL P/N 3117175-03, S/N C31228V, TSN 3601.2 AND CSN 5159. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE2H72 4T4 TRTA13NM E20NE 20051128000232005112800023NM 2005 11 28 CALA0500413 120051121A5310146N559063 CREASE BEAM BOEING757 757224 1384958NM BS 1600 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713113 27555 INSPECTION FOUND CREASE BEAM INNER CHORD CORRODED AT STA 1600, LBL 63. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-70-12 AND ECRA 5310-04501. 2L72 4F RTA2NM 20051128000252005112800025EA 2005 11 28 COMA0560623 120051119A27501217543 DRIVE SHAFT CNDAIRCL600 CL6002B19 1900309EA RT WING WORN A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01735CA6019 7267 FLIGHT 5404 - EN ROUTE PHL-CVG DURING APPROACH RECEIVED A FLAP FAIL CAUTION AT ZERO DEGREE FLAP POSITION. CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE RIGHT WING FLEX DRIVE SHAFT. 2L72 4F RTA21EA 20051128000282005112800028 2005 11 28 SWAA053725 420051121A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051128000292005112800029NM 2005 11 28 SWAA053726 120051121A53306545768 SKIN BOEING737 7373H4 1384600NM BS 373 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 373, STR 17R. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20051117001432005111700143NM 2005 11 17 ASAA0540512 120050926A531565C3394824 FLOORBEAM BOEING737 7374Q8 138447QNM FS 947 PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND FLOORBEAM BS 947 CORRODED AROUND FASTENER HOLES AT LBL 45, RBL 45. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PIECES IAW ASA EO 5310-02500. (M) 2L72 4F RTA16WE 20051117001472005111700147NM 2005 11 17 ASAA0540489 120050920A5313 STRINGER BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND STRINGER "T" CHORD RT SIDE OF APU CUTOUT TORQUE BOX IS EXFOLIATED. REMOVED "T" CHORD, FABRICATED AND INSTALLED REPLACEMENT "T" CHORD IAW 737-400 SRM 51-40-60 AND 51-40-02. (M) 2L72 4F RTA16WE 20051117001502005111700150NM 2005 11 17 ASAA0540511 120050926A57536546435281 SKIN BOEING737 7374Q8 138447QNM TE FLAP PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 OKC - FOUND LEFT OUTBOARD AFT FLAP PUNCTURED. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW 737-400 SRM 51-70-10. (M) 2L72 4F RTA16WE 20051118000162005111800016NM 2005 11 18 ASAA0510294 120050912A5322655496076 SHEAR TIE BOEING737 737290C 138448VNM FS 360 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02740AS 22578 YXX - FOUND SKIN TO FRAME ANGLE CORRODED AT BS 360 BETWEEN STRINGER 25 RT AND 26 RT. REMOVED AND REPLACED FRAME TO SKIN ATTACH ANGLE PER B737-200 SRM 53-10-04 FIGURE 8. (M) 2L72 4F A16WE 20051118000192005111800019NM 2005 11 18 USAA051363 120051110A5320 INTERCOSTAL BOEING737 7373B7 1384580NM BS 344-360 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 STA 344, STA 360, BL0 MAJOR REPAIR, FABRICATED NEW REPAIR PARTS IAW SRM 51-70-11, DEFECT SIZE: .250". 2L72 4F RTA16WE 20051118000212005111800021NM 2005 11 18 USAA051364 120051111A5320 WEB BOEING737 7373B7 1384580NM BS 353 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND CRACK FUSELAGE STATION 353 STRINGER 16 LEFT. REPAIR, CUT WEB TO REMOVE DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 53-10-04, EA 97004 DEFECT SIZE: 2.1". 2L72 4F RTA16WE 20051118000232005111800023NM 2005 11 18 USAA051366 120051111A53206517688U165 ANGLE BOEING737 7373B7 1384580NM BS 300-353 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 FOUND CORROSION BS 300-353 ZEE ANGLE AT S-17L. DEFECTIVE PART REPLACED WITH IDENTICAL PART, REMOVED CORRODED ZEE ANGLE IAW 65-17688, DEFECT SIZE: 1 BY 43 INCHES. 2L72 4F RTA16WE 20051118000252005111800025EU 2005 11 18 USAA051376 120051114A5320D5311282600101 DUMMY RAIL AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19111US 1114 FOUND CORROSION, DUMMY RAIL, Y503.2 FS 12-16; CORROSION LEVEL 1; TASK JA-220-53500. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 53-11-14 AND EA 96240, DEFECT SIZE: 1/2" BY 3". 2L72 4F RTA28NM 20051118000272005111800027EU 2005 11 18 USAA051369 120051114A5320D5348004320401 SILL AIRBUS320 A320214 3930316EU FR 66 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19111US 1114 FOUND CORROSION, FS 66 -Y1462 FLOORBEAM/DOOR SILL; CORROSION LEVEL 1; TASK JA-260-53500. INSTALLED FILLER PER SRM 53-41-14, DEFECT SIZE: 1" BY 1/2". 2L72 4F RTA28NM 20051118000292005111800029EU 2005 11 18 USAA051371 120051114A5320D5347112420000 WEB AIRBUS320 A320214 3930316EU FS 69-70 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19111US 1114 FOUND CORROSION FLOOR WEB BETWEEN FS 69 AND 70 LT SIDE Y1182; CORROSION LEVEL 1; TASK JA-260-535. REPLACED FLOOR WEB WITH IDENTICAL PART PER DWG D53474180, DEFECT SIZE: 1/2" BY 1/2". 2L72 4F RTA28NM 20051118000312005111800031EU 2005 11 18 USAA051373 120051114A5315D5311281400200 FLOORBEAM AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19111US 1114 FOUND CORROSION FLOORBEAM Y-1292 13" AFT OF FS 23; CORROSION LEVEL 1; TASK JA-220-53500. REMOVED AND REPLACED BEAM PER SRM 51-72-11, DEFECT SIZE: 1" BY 1". 2L72 4F RTA28NM 20051118000332005111800033EU 2005 11 18 USAA051375 120051114A5320D5311146100200 FLOOR SUPPORT AIRBUS320 A320214 3930316EU RT FLOOR SUPPORTCORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19111US 1114 FOUND CORROSION RT FLOOR SUPPORT Y-254 AT FRAME 20; CORROSION LEVEL 1; TASK JA-220-53500. DEFECTIVE PART REPLACED WITH IDENT PART PER D5311146100200 DEFECT SIZE: 2 SQ IN. 2L72 4F RTA28NM 20051118000342005111800034 2005 11 18 SA05114 420051114A2565D31517113 SLIDE AIRBUSA319 A319112 3930323EU PASSENGER CABIN READS LOW A USAAK NONE O OTHER ININSP/MAINT 1 EA19762US 1358 THE AFT RIGHT DOOR EMERGENCY ESCAPE SLIDE INDICATED LOW PRESSURE DURING INSPECTION. MAINTENANCE REPLACED THE AFT RIGHT DOOR EMERGENCY ESCAPE SLIDE. OK FOR SERVICE. 2L72 4F RTA28NM 20051118000352005111800035SO 2005 11 18 RAIA00511019 120051114A4990 APU EMB 145 EMB145LR 3260212SO APU BAY LEAKING A RAIAA UNSCHED LANDING KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 CE03814HK 145046 FLT 5565 - STL - SMOKE IN CABIN AND LAVATORY SMOKE WARNING. APU LOW OIL PRESSURE WARNING. MAINTENANCE DEFERRED THE APU DUE TO OIL LEAKING INTO PACKS CAUSING SMOKE WITHIN THE CABIN. 2L72 4T RTT00011AT 20051118000362005111800036SO 2005 11 18 RAIA00511018 120051114A3610M83248 O-RING EMB 145 EMB145LR 3260212SO BLEED AIR SYS LEAKING A RAIAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE03817HK 145058 FLT 5535 - STL - BLEED 2 LEAK WITH ASSOCIATED STRONG ODOR. MAINTENANCE REMOVED AND REPLACED BLEED O-RINGS. 2L72 4T RTT00011AT 20051118000372005111800037EA 2005 11 18 COMA0570119 120051114A2150 ACM CNDAIRCL600 CL6002C10 1390015EA LT AND RT FAILED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01690CA 10182 FLIGHT 4961- FOUND LT AND RT A/C PACK FAULT. CYCLED AIRCRAFT POWER. OPERATIONAL CHECK NORMAL. 2L72 4F RTA21EA 20051118000382005111800038EA 2005 11 18 COMA0560608 120051115A323046193 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA MLG MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01920CA7666 7022 FLIGHT 5036- GEAR DISAGREE WARNING. REPLACED THE MLG PRIORITY VALVE. 2L72 4F RTA21EA 20051118000852005111800085SO 2005 11 18 CHQA200500194 120051113A32608005701 PROXIMITY SENSOR EMB 145 EMB145LR 3260212SO MLG INOPERATIVE A CHQAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL11286SK 145443 AFTER ROTATION WITH A POSITIVE RATE, MLG RAISED & A MASTER WARNING FOR MLG LEVER DISAGREE CAME ON ALONG WITH A MASTER CAUTION FOR INBOARD BRAKE INOP. NOSE AND LT MLG INDS WHITE AND RT MLG IND RED. ASKED FOR VECTORS TO MXE VOR & HOLDING IN ORDER TO ASSESS SITUATION & RUN APPROPRIATE CHECKLISTS. FOLLOWING QRH FOR MLG LVR DISAGREE, CYCLED MLG HANDLE DOWN & ALL 3 GEAR IND WENT TO DOWN & GREEN. CONSIDERING ALL FACTORS, DECIDED TO LEAVE MLG DOWN & RETURN TO PHL AFTER RUNNING ALL NECESSARY CHECK LISTS. DECLARED AN EMERGENCY. LANDED UNEVENTFULLY AND TAXIED BACK TO GATE. MX FOUND 2 BAD PROX SENSORS ON NLG AND ON LT MLG UPLOCK BOX. INSTALLED 2 SERVICEABLE SENSORS IAW EMB 145 MM 32-63-02 AND 32-61-01. 2L72 4T RTT00011AT 20051121000042005112100004WP 2005 11 21 IXXA05RNG091S 120051028A5730 SKIN DOUG DC8 DC872 302199BWP WS 591.25-603.75CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK, FOUND CORROSION ON UPPER SKIN AT OUTBOARD EXTENDED LEADING EDGE AROUND STA XFS 591.250 - 603.750 - RT. CORROSION WAS REMOVED IAW SRM DC8 51-1-8 PAGE 20 AND THICKNESS WAS FOUND OUT OF LIMITS IAW DC8 SRM 57-2-0 PAGE 16 AND ASTME 79701. DAMAGE WAS REPAIRED IAW EWO ATI 57-056 AND SRM 57-2-1 FIG 38. 2L74 4F RT4A25 20051121000162005112100016NM 2005 11 21 AWXA200501412 120051025A575465C267996 SKIN BOEING737 7373S3 1384711NM NR 6 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 MCN - DURING C13 CHECK DISCOVERED 5 CRACKS, 1.0 INCHES IN LENGTH, AROUND RIVETS ON THE RT WING, NR 6 SLAT FROM SS 330R TO SS 341R. MAINTENANCE CUT OUT DAMAGED SKIN ON THE RT WING, NR 6 SLAT IAW BOEING 737-300 SRM 57-43-01-2R6. FABRICATED FILLER AND SPLICE PLATE IAW BOEING 737-300 SRM 57-43-01-2R6. INSTALLED FABRICATED REPAIR PARTS ON THE RT WING, NR 6 SLAT FROM SS 330 R TO SS 341R IAW BOEING 737-300 SRM 57-43-01-2R6. 2L72 4F RTA16WE 20051121000172005112100017NM 2005 11 21 AWXA200501413 120051026A575465C267995 SKIN BOEING737 7373S3 1384711NM NR 1 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 MCN - DURING C13 CHECK DISCOVERED 7 CRACKS, 1.0 INCHES IN LENGTH, ON THE BOTTOM OF THE NR 1 SLAT FROM SS 247L TO SS 263.5L. MAINTENANCE CUT OUT DAMAGED SKIN ON NR 1 SLAT IAW BOEING 737-300 SRM 57-43-01-2R6. FABRICATED FILLER AND SPLICE PLATE IAW BOEING 737-300 SRM 57-43-01-2R6. INSTALLED FABRICATED REPAIR PARTS ON THE BOTTOM OF THE NR 1 SLAT FROM SS 247L TO SS 263.5L IAW BOEING 737-300 SRM 57-43-01-2R6. 2L72 4F RTA16WE 20051121000382005112100038EA 2005 11 21 COMA0560612 120051116A7330 INDICATOR CNDAIRCL600 CL6002B19 1900309EA LT ENGINE FUEL READS LOW A COMAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01975CA 7150 FLIGHT 5464 - LEFT ENGINE FUEL FLOW 400 LBS, 1000 LBS NORMAL. OPERATIONAL CHECK OF FUEL FLOW WAS NORMAL. 2L72 4F RTA21EA 20051121000452005112100045NM 2005 11 21 AWXA200501396 120051104A5315654681236 FLOORBEAM BOEING737 7373G7 1384595NM BS 992 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 MCN - DURING C19 CHECK DISCOVERED CORROSION ON THE FLOORBEAM AT BS 992, BL 14R AND WL 208. CORROSION WAS FOUND TO BE OUT OF LIMIT IAW BOEING 737-300 SRM 53-60-51-1A1 FIG 101. REMOVED FLOORBEAM AT BS 992, BL 14R AND WL 208 IAW BOEING 737-300 SRM 51-40-02-0G. RECEIVED NEW FLOOR SUPPORT AND FABRICATED SHIMS IAW BOEING 37-300 SRM 51-30-01-0G FIG 10. INSTALLED REPAIR PARTS AT BS 992, BL 14R AND WL 208 IAW BOEING 737-300 SRM 53-60-51-1A1 FIG 101. 2L72 4F RTA16WE 20051121000472005112100047NM 2005 11 21 AWXA200501398 120051106A5347D57130147200 SEAT TRACK AIRBUSA319 A319132 3930340NM FR 36-41 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28813AW 1223 SAL - DURING BC4 CHECK DISCOVERED CORROSION ON SEAT TRACK AT LT INBOARD FRAME 37+3 AND Y765. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW AIRBUS 319 SRM 53-31-15 FIG 101. MAINTENANCE REMOVED SEAT TRACK AND INSTALLED NEW SEAT TRACK FROM FRAME 36 TO FRAME 41 AND AT Y765 IAW AIRBUS 319 SRM 51-42-11. 2L72 4F RTA28NM 20051121000482005112100048NM 2005 11 21 AWXA200501399 120051106A5347D53371110008 SEAT TRACK AIRBUSA319 A319132 3930340NM FR 41-47 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28813AW 1223 SAL - DURING BC4 CHECK DISCOVERED CORROSION ON SEAT TRACK AT LT INBOARD FRAME 41 + 7 AND Y765. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW AIRBUS 319 SRM 53-31-15 FIG 101. MAINTENANCE REMOVED SEAT TRACK AND INSTALLED NEW SEAT TRACK FROM FRAME 41 TO FRAME 47 AND AT Y765 IAW AIRBUS 319 SRM 51-42-11. 2L72 4F RTA28NM 20051121000502005112100050NM 2005 11 21 AWXA200501401 120051027A53126516800166 BULKHEAD BOEING737 7373S3 1384711NM BS 178 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 MCN - DURING C13 CHECK DISCOVERED WEB CRACKED, 1.5 INCHES, AT BS 178, WL 218 AND BL 12L. MAINTENANCE CUTOUT DAMAGED PORTION OF BULKHEAD WEB IAW BOEING 737-300 SRM 53-10-08-2R9. FABRICATED DOUBLER AND FILLER IAW BOEING 737-300 SRM 53-10-08-2R9. INSTALLED FABRICATED REPAIR PARTS AT BS 178, WL 218 AND BL 12L IAW BOEING 737-300 SRM 53-10-08-2R9. 2L72 4F RTA16WE 20051121000512005112100051NM 2005 11 21 AWXA200501402 120051027A53126516300166 BULKHEAD BOEING737 7373S3 1384711NM BS 178 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 MCN - DURING C13 CHECK DISCOVERED WEB CRACKED, 1.0 INCHES, AT BS 178, WL 218 AND BL 5.7R. MAINTENANCE CUTOUT DAMAGED PORTION OF BULKHEAD WEB IAW BOEING 737-300 SRM 53-10-08-2R9. FABRICATED DOUBLER AND FILLER IAW BOEING 737-300 SRM 53-10-08-2R9. INSTALLED FABRICATED REPAIR PARTS AT BS 178, WL 218 AND BL 5.7R IAW BOEING 737-300 SRM 53-10-08-2R9. 2L72 4F RTA16WE 20051121000642005112100064EA 2005 11 21 VNAA0511008 120051111A5100 UNKNOWN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE UNKNOWN NONE A VNAAO OTHER E VIBRATION/BUFFET DEDESCENT 1 GL05256PS 7937 THE CREW REPORTED ENCOUNTERING SEVERE TURBULENCE DURING DESCENT BETWEEN FL230 AND FL210. THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE PERFORMED AN EXTREME TURBULENCE / MANEUVER INSPECTION IAW CRJ200 AMM 05-51-03-210-801. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20051121000782005112100078NM 2005 11 21 SWAA053639 120051116A53126582671 PRESSURE PANEL BOEING737 7375H4 138449DNM MLG W/W CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29512SW 24189 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE BEADED WEB CRACKED AT BS 663, LBL 32. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20051121000862005112100086NM 2005 11 21 SWAA053647 120051116A53226546529 SHEAR TIE BOEING737 7373H4 1384600NM BS 500C CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500C, LBL 1. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051122000062005112200006NM 2005 11 22 05FDEA03843 120051116A5314 KEELBEAM BOEING727 727200 138407ENM BS 950C-950F CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 STR 29L KEEL BEAM BS 950C TO 950D WL 148 HAS CORROSION (C53-113-01). 2L73 4F RTA3WE 20051122000072005112200007NM 2005 11 22 05FDEA03842 120051116A5311 FRAME BOEING727 727200 138407ENM BS 990 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 AFT CARGO COMPARTMENT, FRAME IS DENTED BS 990 LBL 29 WL 150. REPAIRED FRAME, BS 990, LBL 29, WL 150 PER SRM 51-40-3. 2L73 4F RTA3WE 20051122000092005112200009NM 2005 11 22 05FDEA03846 120051116A5230 REPAIR BOEING727 727200 138407ENM CARGO DOOR PROPER A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25266FE 21672 FOUND 2 REPAIRS ON LOWER AFT CARGO DOOR. REPAIRS REQUIRE EVALUATION FOR MAJOR / MINOR DETERMINATION AND IF REPAIRS WERE ACCOMPLISHED USING FAA APPROVED DATA. TWO PREVIOUSLY INSTALLED REPAIRS ON LOWER AFT CARGO DOOR NR 3 WERE DETERMINED TO BE IAW SRM 52-00-3 FIG 3, BASED ON AN EXTERNAL VISUAL EVALUATION WITH REPAIRS INSTALLED. REPAIRS DETERMINED TO BE MAJOR BASED ON FEDEX GMM 6-2-100 CRITERIA. 2L73 4F RTA3WE 20051122000162005112200016NM 2005 11 22 SWAA053648 120051113A213171211997101AC CONTROLLER BOEING737 7377H4 1384404NM CABIN PRESSURE FAULTY A SWAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW29749SW 29801 DECLARED EMERGENCY. CABIN ALTITUDE HORN SOUNDED ALONG WITH RAPID DECOMPRESSION & CABIN MASKS DROPPED. CABIN PRESSURE CONTROLLABLE IN ALTERNATE MODE. REMOVED AND REPLACED BOTH CABIN PRESSURE CONTROLLERS, CABIN AFT OUTFLOW VALVE & CABIN PRESSURIZATION CONTROL MODULE PER MM. 2L72 4F RTA16WE 20051122000212005112200021WP 2005 11 22 05FDEA03851 120051117A5330 REPAIR DOUG DC10 DC1030 3023501WP BS 731-791 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 RIGHT EXT FUSELAGE FOUND DOUBLER LENGTH 60 INCHES WIDTH 12 INCHES AT STA 731 TO STA 791 LONG 42 AND 43. NO ACTION TAKEN EO8-5100-7-5001-1. 2L73 4F A22WE 20051122000312005112200031WP 2005 11 22 AALA20050752 120051114A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217525A 49917 DFW - CEILING EMERGENCY LIGHTS AT ROW 14D INOPERATIVE. REPLACED BATTERY PACK AND CHARGER ASSEMBLY FOR CEILING EMERGENCY LIGHTS AT ROW 14D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051122000362005112200036EA 2005 11 22 VNAA0511004 120051106A5512 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE HORIZONTAL STAB LIGHTNING STRIKEA VNAAO OTHER O OTHER DEDESCENT 1 GL05257PS 7939 AFTER LANDING THE CREW REPORTED A POSSIBLE LIGHTNING STRIKE ON THE NOSE OF THE AIRCRAFT. MAINTENANCE PERFORMED AN EN ROUTE LIGHTNING STRIKE INSPECTION AND FOUND EVIDENCE OF LIGHTNING DAMAGE ON THE RT HORIZONTAL STABILIZER TIP FAIRING. THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE PERFORMED A DETAILED LIGHTNING STRIKE INSPECTION. ALL DAMAGE FOUND WAS REPAIRED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20051122000462005112200046WP 2005 11 22 05FDEA03867 120051118A5712 RIB DOUG DC10 DC1030 3023501WP RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 RIGHT WING DROP CRACK ON RIB AND OLD REPAIR. REMOVED AND SCRAP EXISTING REPAIR IAW SRM 51-33-01 PG 34/47 VOL 2. INSTALLED NEW PART P/N F161121-3B IAW SRM 57-00-01 FIG 10 SHT 1 VOL 1 AND SRM 51-33-01 PG 34/47. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F161121/N01121 IAW SRM 57-00-01 FIG 10 SHT 1 VOL 1. 2L73 4F A22WE 20051122000582005112200058WP 2005 11 22 05FDEA03879 120051118A5320 REPAIR DOUG DC10 DC1010 3022110WP BS 2122 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 UPPER AFT FUSELAGE COMPT STA 2122 ON LWR ANGLE OF BULKHEAD FOUND 1 ANGLE REPAIR AT X30. PERFORMED INSPECTION RESTORED HL 64-6 H/L IAW SRM 51-33-01 PG 34/47 VOL 2. 2L73 4F A22WE 20051122000742005112200074NM 2005 11 22 SWAA053654 120051117A3350207377 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29452WN 29846 EEPLS TRACK LENS LOOSE AT ROW 3. SECURED LENS PER MM. 2L72 4F RTA16WE 20051122000822005112200082NM 2005 11 22 SWAA053662 120051117A53116558280 FRAME BOEING737 7373H4 1384600NM BS 360 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051122000832005112200083NM 2005 11 22 SWAA053663 120051117A53116546525 FRAME BOEING737 7373H4 1384600NM BS 380 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051122000982005112200098NM 2005 11 22 SWAA053666 120051117A53306545765 SKIN BOEING737 7373H4 1384600NM BS 516.5 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29352SW 24888 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 516.50, STR 13R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051122000992005112200099WP 2005 11 22 UPS05845795 120051023A5311723504700015 FRAME DOUG DC8 DC873F 302199FWP FS 240 L36 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE:C1 FUSELAGE FRAME IS CRACKED 2" LONG AT F/S 240 L36. CRACK IS IN RADIUS OF UPPER FLANGE. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR SPLICE, ANGLE AND SHEAR TIE CLIP IAW SRM 53-02-00-0, 51-3-2, 51-1-21, 53-4-1 AND 51-1-20D. 2L74 4F RT4A25 20051122001002005112200100WP 2005 11 22 UPS05845796 120051021A53139758507501 LONGERON DOUG DC8 DC873F 302199FWP BS1240-1260 L35LCORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE:C1 WHILE WORKING N/R 822550 FOUND PITTING CORROSION ON STEEL LONGERON 35L I/B SIDE BETWEEN FS 1240-1260. REPAIRED LONGERON 35L IAW SAA SK 813-823057 AND UPS EO DC8-53-20522. 2L74 4F RT4A25 20051122001072005112200107NM 2005 11 22 AWXA200501419 120051027A5330655298875 SKIN BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 MCN - DURING C13 CHECK DISCOVERED, THE L2 DOOR CUTOUT, UPPER HINGE CUTOUT, UPPER CORNER CRACKED, .6 INCHES IN LENGTH. MAINTENANCE CUT OUT CRACKED ARE ON THE L2 DOOR. FABRICATED FILLER AND DOUBLER IAW BOEING 737-300 SRM 53-60-01-2R5. INSTALLED FABRICATED REPAIR PARTS IAW BOEING 737-300 SRM 53-60-01-2R5. 2L72 4F RTA16WE 20051122001112005112200111NM 2005 11 22 05FDEA03915 120051119A5347 SEAT TRACK DOUG MD11 MD11 3023602NM BS 899 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 FOUND MAIN DECK CABIN STA 899 LBL 26 SEAT TRACK CORRODED. REPAIR CARRIED OUT AS PER SRM 53-70-00. 2L73 4F RTA22WE 20051122001162005112200116NM 2005 11 22 05FDEA03920 120051119A5347 SEAT TRACK DOUG MD11 MD11 3023602NM BS 919-979 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 MAIN DECK CORROSION FOUND ON SEAT TRACK FROM STA 919 TO 979 ADJ TO X=-8.5. REPAIRED AS PER SRM 53-70-00. 2L73 4F RTA22WE 20051122001182005112200118EU 2005 11 22 05FDEA03899 120051118A5340 FITTING AIRBUS300 A300B4622R 3930312EU ZONE 100 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25720FD 417 COMPLY WITH EA 6-5310-92351, FUSELAGE SB 53-6111, DISCREPANT BASE FITTING HOLES AT FS 45 RT. COMPLIED WITH EA 6-5310-92351B. 2L72 4F RTA35EU 20051122001212005112200121NM 2005 11 22 05FDEA03910 120051119A5320 FLOOR SUPPORT DOUG MD11 MD11 3023602NM BS 1911 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 CABIN, LATERAL FLOOR SUPPORT ADJ TO STA 1911 FROM X=21 TO X= 75 FOUND WITH CORROSION. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2L73 4F RTA22WE 20051122001362005112200136NM 2005 11 22 05FDEA03898 120051118A5315 FLOORBEAM BOEING727 727227 1384078NM BS 740 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 FOUND DOUBLE HOLE IN FLOORBEAM BS 740 LBL 47 WL 208. REPAIRED PER FED EX EA 7-5810-91429. 2L73 4F A3WE 20051122001382005112200138EA 2005 11 22 SWIA200515856 120050719A5712 ANGLE CNDAIRCL600 CL6002B19 1900309EA RT WW CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07412SW 7101 RT WHEEL WELL BAT ANGLE SUSPECTED CRACKED, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR PARTS TO BAT ANGLE RT WHEEL WELL PER CRJ200 SRM 51-42-06 PG 11. 51-42-21 PG 17. 2L72 4F RTA21EA 20051122001402005112200140EA 2005 11 22 SWIA200515858 120050811A5210 DRAG ANGLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07447SW 7677 PAX DOOR - DRAG ANGLE IS CRACKED (AFT) ADJACENT TO THE ASSIST MOTOR CABLE PULLEY, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED FABRICATED REPAIR PARTS IAW REO 601R-52-11-513. 2L72 4F RTA21EA 20051122001422005112200142EA 2005 11 22 SWIA200515860 120050811A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA BS 484 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07447SW 7677 MAIN CABIN FS484 LT BL AND 28.5 WL 73.5 CLIP CRACKED, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW CLIP MAIN CABIN FS484 LH BL 28.5 WL 73.5 IAW CRJ200 REO 601-53-41-059 REV A. 2L72 4F RTA21EA 20051122001442005112200144EA 2005 11 22 SWIA200515862 120050811A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA BS 484 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07447SW 7677 MAIN CABIN FS 484 RT BL 28.5 WL73.5 CLIP CRACKED, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW 'CLIP' AT FS 484 RT BL 28.5 WL 73.5 IAW CRJ200 RHEO 601R-41-059 REV A. 2L72 4F RTA21EA 20051122001462005112200146EA 2005 11 22 SWIA200515864 120050811A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07447SW 7677 MAIN AVIONICS COMPARTMENT STA 280 BL 10.5 WL 74.0 CLIP CRACKED, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW ANGLE AND FILLER IAW CRJ200 SRM 51-42-21. 2L72 4F RTA21EA 20051122001482005112200148EA 2005 11 22 SWIA200515866 120051112A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07445SW 7651 FLT SPOILERS FAULT STATUS MSG. REPLACED LT OB PCU ON LT FLIGHT SPOILER. OPERATIONAL CHECK GOOD IAW MM 27-61-00. 2L72 4F RTA21EA 20051122001502005112200150NM 2005 11 22 SWAA053677 120051119A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM BS 727E CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 727E, LBL 7 AND LBL 13. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051122001612005112200161NM 2005 11 22 SWAA053687 120051119A534065C27314 STRINGER CLIP BOEING737 7375H4 138449DNM BS 294 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29512SW 24189 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 294.5, STR 11R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051122001632005112200163NM 2005 11 22 SWAA053689 120051119A53156546810 FLOORBEAM BOEING737 7375H4 138449DNM BS 967 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29512SW 24189 DURING SCHEDULED 1/2D CHECK, FOUND CABIN FLOORBEAM CORRODED AT BS 967, RBL 18 TO RBL 42. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20051122001652005112200165NM 2005 11 22 SWAA053691 120051118A531165C25229 FRAME BOEING737 7373H4 1384600NM BS 727D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8L TO STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051122001672005112200167 2005 11 22 SWAA053693 420051118A25656557463 BRACKET BOEING737 7373H4 1384600NM GIRT BAR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED D CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD LOWER FLOOR BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER SRM. 2L72 4F RTA16WE 20051122001692005112200169NM 2005 11 22 SWAA053695 120051117A5754 SKIN BOEING737 7373H4 1384600NM NR 2 SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29648SW 27718 DURING SCHEDULED C4 CHECK, FOUND NR 2 L/E SLAT DELAMINATED. REMOVED AND REPLACED SLAT PER MM. 2L72 4F RTA16WE 20051122001712005112200171 2005 11 22 SWAA053697 420051118A2565D31354 SLIDE BOEING737 7373A4 1384585NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051122001872005112200187NM 2005 11 22 SWAA053670 120051118A53116558280 FRAME BOEING737 7373H4 1384600NM BS 360 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8L TO STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051122001892005112200189NM 2005 11 22 SWAA053672 120051118A53216546833 WEB BOEING737 7373H4 1384600NM COCKPIT FLOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D CHECK, FOUND COCKPIT FLOOR WEB CRACKED BETWEEN BS 188 TO BS 196.5, RBL 29, WL 207. REPAIRED FLOOR WEB PER SRM. 2L72 4F RTA16WE 20051122001912005112200191NM 2005 11 22 SWAA053674 120051118A53116546552 FRAME BOEING737 7373H4 1384600NM BS 827 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 1R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051122001932005112200193NM 2005 11 22 SWAA053676 120051118A53216546833 WEB BOEING737 7373H4 1384600NM COCKPIT FLOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D CHECK, FOUND COCKPIT FLOOR WEB CRACKED BETWEEN BS 188 TO BS 196.5, LBL 29, WL 207. REPAIRED FLOOR WEB PER SRM. 2L72 4F RTA16WE 20051122001942005112200194NM 2005 11 22 05FDEA03897 120051118A5753 SKIN BOEING727 727200 138407ENM TE FLAP MISDRILLED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 LT IB TE MIDFLAP LWR AFT SKIN HAS NUMEROUS FASTENER HOLES DOUBLE DRILLED OR EXCESSIVELY COUNTERSUNK, O/B OF O/B FLAP TRACK. REPAIRED LT IB MIDFLAP LOWER AFT SKIN PER SRM 51-40-2. 2L73 4F RTA3WE 20051122001972005112200197NM 2005 11 22 ASAA0540467 120050914A49106546579 STIFFENER BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU BS 1091 CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02793AS 28888 APU BAY STIFFENER CHAFED ON FWD END. REMOVED AND REPLACED IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051128000022005112800002EA 2005 11 28 COMA0560621 120051119A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01977CA 7157 FLIGHT 5227- EN ROUTE CVG-CID DURING APPROACH RECEIVED A FLAP FAIL CAUTION AT ZERO DEGREE FLAP POSITION. CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3, (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2L72 4F RTA21EA 20051128000062005112800006NM 2005 11 28 BB05099 120051121A2821AC9227F1740 FILTER BOEING767 767200 1385120NM ENGINE FUEL DIRTY A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19655US 25257 ON CLIMBOUT FROM SJU, RECIEVED E/M -RT ENG FUEL FILTER-. RETURNED TO SJU. MAINTENANCE REPLACED THE RIGHT ENGINE FUEL FILTER AND CLEANED THE DIFFERENTIAL PRESSURE SWITCH CONTACTS. NO FURTHER DIFFICULTIES. 2L72 4F RTA1NM 20051128000302005112800030NM 2005 11 28 SWAA053727 120051121A53306545766 SKIN BOEING737 7373H4 1384600NM BS 466 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 466, STR 26L. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20051128000342005112800034 2005 11 28 SWAA053731 420051118A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29394SW 27380 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20051128000362005112800036NM 2005 11 28 SWAA053733 120051121A53306545767 SKIN BOEING737 7375H4 138449DNM BS 405 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 405, STR 16R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051128000382005112800038NM 2005 11 28 SWAA053735 120051122A53156546804 FLOORBEAM BOEING737 7375H4 138449DNM BS 294.5 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29512SW 24189 DURING SCHEDULED 1/2D CHECK, FOUND CABIN FLOORBEAM UPPER CHORD CRACKED AT BS 294.5, LBL 22 TO LBL 27. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20051128000392005112800039NM 2005 11 28 SWAA053736 120051122A534065C27314 STRINGER CLIP BOEING737 7375H4 138449DNM BS 663 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29512SW 24189 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051128000402005112800040NM 2005 11 28 SWAA053737 120051121A5344907822 HINGE FITTING BOEING737 7373H4 1384600NM L1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29613SW 27931 DURING SCHEDULED C3 CHECK, FOUND L1 DOOR LOWER FUSELAGE HINGE BOX FITTING CRACKED. REMOVED AND REPLACED HINGE BOX FITTING PER SRM. 2L72 4F RTA16WE 20051128000432005112800043NM 2005 11 28 SWAA053740 120051122A2560P4010021 BATTERY BOEING737 7373Y0 1384671NM FLASHLIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED RON CHECK, FOUND FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2L72 4F RTA16WE 20051128000452005112800045NM 2005 11 28 SWAA053721 120051121A53306545765 SKIN BOEING737 7373H4 1384600NM BS 500D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 12R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051128000472005112800047NM 2005 11 28 SWAA053723 120051121A53306545765 SKIN BOEING737 7373H4 1384600NM BS 578 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 578, STR 10L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051128000492005112800049NM 2005 11 28 SB05148 120051119A335020131A BATTERY PACK BOEING737 737401 1384701NM EMERGENCY LIGHT DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19409US 23879 ORF - MAINTENANCE REPORTED THE BATTERY PACK FOR THE AFT RIGHT SERVICE DOOR EMERGENCY LIGHTS IS WEAK. MAINTENANCE REMOVED AND REPLACED THE AFT RIGHT BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20051128000512005112800051NM 2005 11 28 SB05149 120051119A33501317 BULB BOEING737 7374B7 1384702NM EMERGENCY LIGHT WEAK A USAAK NONE O OTHER ININSP/MAINT 1 EA19779AU 24996 CLT - PILOT REPORTED THE COCKPIT EMERGENCY EXIT FLOODLIGHT IS VERY DIM ON EMERGENCY BATTERY POWER. MAINTENANCE VERIFIED CORRECT VOLTAGE OF 6.13 VOLTS DC AT EMERGENCY LIGHT SOCKET. INSTALLED NEW BULB FOR EMERGENCY EXIT LIGHT. OPERATIONAL CHECK NORMAL. 2L72 4F RTA16WE 20051128000532005112800053CE 2005 11 28 DJFA2005161 120051116A2910 WARNING LIGHT BEECH MU300 400A 1155402CE HYD SYSTEM ILLUMINATED E DJFAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA23709TA RK180 KRFD - KSDF DURING CRUISE FLIGHT, WHILE ENRANGE TO KLEX, THE CREW NOTED THAT THE HYDRAULIC FLUID PRESSURE WAS INDICATING 2,000 PSI. DUE TO A LONGER RUNWAY LENGTH THE AIRCRAFT WAS DIVERTED TO KSDF AND AN EMERGENCY WAS DECLARED. A MANUAL GEAR EXTENSION WAS PERFORMED AND AN UNEVENTFUL WAS MADE. EMERGENCY BRAKES WERE USED TO STOP THE AIRCRAFT. 2H72 4F RTA16SW 20051128000542005112800054CE 2005 11 28 DJFA2005163 120051110A5711 SPAR CESSNA650 650 2076802CE WING CORRODED E DJFAK NONE O OTHER ININSP/MAINT 1 EA23384CW 6500144 DURING AN UNSCHEDULED MAINTENANCE VISIT, WHILE INVESTIGATING A FUEL LEAK, CORROSION WAS DISCOVERED ON BOTH FORWARD AND BOTH AFT WING SPAR SPLICES ON THE UNDERSIDE OF THE WING DIRECTLY ABOVE THE SKID RAILS. 2L72 4F A9NM 20051128000552005112800055EA 2005 11 28 COMA0560618 120051118A5230 SEAL CNDAIRCL600 CL6002B19 1900309EA CARGO DOOR DAMAGED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01956CA 7105 FLIGHT 9452 - DURING CLIMBOUT OF RDU, CABIN WAS SLOW TO PRESSURIZE. FLIGHT RETURNED TO RDU FOR PRESSURIZATION PROBLEM. FERRIED A/C TO CVG FOR REPLACEMENT OF THE CARGO DOOR SEAL. 2L72 4F RTA21EA 20051128000562005112800056EA 2005 11 28 COMA0560619 120051118A2130 EJECTOR CNDAIRCL600 CL6002B19 1900309EA JET PUMP MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01956CA 7105 FLIGHT 5440 - RECEIVED A CABIN ALTITUDE MESSAGE DURING CRUISE FLIGHT, DIVERTED TO RDU FOR PRESSURIZATION PROBLEM. REMOVED, INSPECTED AND RE-INSTALLED THE JET PUMP EJECTOR IN THE AFT EQUIPMENT BAY. 2L72 4F RTA21EA 20051128000582005112800058NM 2005 11 28 QXEA200501537 120051109A5730 SKIN BOMBDRDHC8 DHC8402 1390042NM WING DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX: ONE AREA ON AFT APERTURE FOR WING PANEL 522AT IS BLENDED OUT OF LIMITS PER RD 8/4-57-441. MAINTENANCE REPAIRED IAW NDTM PART 6, 51-00-02, QX EA 6-57-394 AND RD 8/4-57-577 AND QX EO 6-57-317. 2H72 4T RTA13NM 20051128000622005112800062NM 2005 11 28 QXEA200501539 120051109A5730 SKIN BOMBDRDHC8 DHC8402 1390042NM WING DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX: TWO BLENDED AREAS ON FWD APERTURE AND 2 BLENDED AREAS ON AFT APERTURE FOR WING PANEL 523AT ARE OUT OF LIMITS PER RD 8/4-57-441. MAINTENANCE REPAIRED IAW NDTM PART 6, 51-00-02, QX EA 6-57-394 AND QX EO 6-57-317 AND RD 8/4-57-577. 2H72 4T RTA13NM 20051128000632005112800063EA 2005 11 28 COMA0560613 120051117A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01927CA 7031 FLIGHT 5015 - FLAPS FAIL CAUTION. INSPECTED PER AD 98-20-01 AND LUBRICATED ACTUATORS. 2L72 4F RTA21EA 20051128000652005112800065EU 2005 11 28 SA05117 120051119A3610118511546 PRECOOLER AIRBUS320 A320214 3930316EU NR 1 ENGINE DAMAGED A USAAB EMER. DESCENT G MULTIPLE FAILURE CRCRUISE 1 EA19118US16977 1264 CLT FLT 1130 WHILE EN ROUTE, THE NR 1 ENGINE BLEED SYSTEM INDICATED INOPERATIVE WHEN ECAM MESSAGE -AIR L WING LEAK-, GENERATED. WITH THE NR 2 ENGINE BLEED SYSTEM ON MEL, THE AIRCRAFT DID NOT HAVE SOURCE AIR TO MAINTAIN CABIN PRESSURE, CAUSING BOTH AIR CONDITIONING PACKS TO FAULT. THE FLIGHT DESCENDED TO 10,000 FEET AND RESET THE BLEED SYSTEM. WITH THE SUCCESSFUL RESET, THE FLIGHT CLIMBED BACK TO FL 280 AND CONTINUED TO DESTINATION. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 ENGINE PRECOOLER DUE TO DAMAGED AND MISSING COOLING TUBES. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20051128000662005112800066EU 2005 11 28 SA05118 120051119A3350321431 BATTERY AIRBUSA321 A321211 3930370EU EMERGENCY LIGHTSDISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19172US 1472 TPA - THE MID CABIN, RIGHT SIDE EMERGENCY POWER SUPPLY UNIT FAILED THE OPERATIONAL TEST. MAINTENANCE REPLACED THE BATTERY IN THE MID CABIN, RIGHT SIDE EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20051128000672005112800067CE 2005 11 28 DXTA200501083 120051113A3213 STRUT CESSNA750 750 2076810CE MLG DISCHARGED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07946QS 7500195 GEAR HANDLE COULD NOT BE MOVED TO THE UP POSITION AFTER TAKEOFF. CHECKED NLG STRUT SERVICING. FOUND NO PRESSURE IN LOWER BARREL. SERVICED STRUT, OPERATIONAL CHECK NORMAL. MAINT PERFORMED IAW THE CESSNA 750 M/M CHAPTER 12-10-38. 2L72 4J RTT00007WI 20051128000692005112800069NE 2005 11 28 DXTA200501087 220051116A732031J240401 FUEL FILTER CESSNA560 560XL 2076702CE PWA 545 PW545A NE RT ENGINE BYPASSING E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07615QS 5605360 PCEDB0752 RIGHT ENGINE FUEL FILTER BYPASS LIGHT ILLUMINATED ON TAKEOFF ROLL AT TAKEOFF POWER EXTINGUISHED WHEN POWER REDUCED. OPERATED RT ENGINE AND VERIFIED RT FUEL FILTER BYPASS LIGHT ILLUMINATES NEAR TAKEOFF POWER SETTINGS. REMOVED AND INSPECTED FUEL FILTER. FOUND EVIDENCE OF MINOR CONTAMINATION. CONTACTED PRATT & WHITNEY, PER REQUEST PERFORMED FCU CONTAMINATION CHECK PER P & W 545 M/M 73-20-01 T/R 73-5. NO CONTAMINATION FOUND IN AIRFRAME OR FCU. INSTALLED NEW FUEL FILTER AND O-RINGS. PERFORMED GROUND PENALTY RUN, ALL PARAMETERS NORMAL. INSPECTED FILTER AFTER RUN, NO DEFECTS NOTED. INSTALLED FILTER WITH NEW O-RINGS PER 545 M/M 73-10-05. OPS AND LEAK CHECK GOOD. 2L72 4F4 FRTA22CE E00059EN 20051128000712005112800071NE 2005 11 28 DXTA200501088 220051116A7321 FCU CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE RT ENGINE OUT OF ADJUST E DXTAE ENGINE SHUTDOWN J WARNING INDICATION TXTAXI/GRND HDL 1 GL07339QS 5600339 DURING BRAKE BURN-IN AT 80 KNOTS. THROTTLES REDUCED TO IDLE. A MASTER LIGHT WITH LOW OIL PRESSSURE AND LIGHT AND N2 AT 24 PERCENT ON RT ENGINE ZERO FUEL FLOW. PLACED THROTTLE IN CUTOFF AND TAXIEDTO EJM. PERFORMED IDLE CUTOFF CHECK, LIGHT CHECKS GOOD, RT FAILS. ADJUSTED RT FCU TO FLOW DIVIDER CONNECTING ROD AND SET MIN N2 STOP. SAFTIED ALL AS REQUIRED. ADJUSTED FUEL FLOW INDICATOR SWITCH, RAN RT ENG - FULL FLOW INDICATION OPERATES NORMAL AT THIS TIME. PERFORMED ALL NECESSARY ENG RUNS. ENG OPERATES NORMAL AT THIS TIME IAW P & W M/M 71-00-00/71-01-03 & 560 M/M 73-30-03. 2L72 4F4 FRTA22CE E25EA 20051128000722005112800072NM 2005 11 28 DXTA200501085 120051115A3251 STEERING SYS AMD FALC50FALCON2000 2730170NM NLG MALFUNCTIONED E DXTAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 GL07224QS 124 DURING T/O ROLL, NOSEWHEEL STEERING WOULD NOT ENGAGE UNTIL STEERING WAS TURNED PASSED 45 DEGREES EITHER SIDE. DURING TAXI NWS WORKED INTERMITTENTLY. PERFORMED OPERATIONAL TEST OF STEERING CONTROL SYSTEM WITH NO DEFECTS NOTED PER FALCON 2000 M/M 32-500. 2K73 4F RTA50NM 20051128000772005112800077CE 2005 11 28 DXTA200501092 120051118A2910AS11606K0130 LINE CESSNA750 750 2076810CE HYD SYSTEM RUPTURED E DXTAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL07948QS 7500149 HYD VOLUME LOW A CAS MESSAGE IN FLIGHT. LOST A SYSTEM FLUID. LANDED WITH EMERGENCY BRAKES. STEERING GEAR EXTENDED BEFORE PROBLEM, SO WAS NOT BLOW DOWN. JACKED AIRCRAFT, APPLIED PRESSURE, FOUND NOSE GEAR ACTUATOR EXTEND HOSE RUPTURED. REF SQ 9 THIS WORK ORDER FOR BRAKE BLEED. REPLACED FLEX LINE ASSY LEAK CHECK GOOD IAW 750 MM 32-30-03. BLED HYD SYSTEM IAW 750 MM 12-10-15, NO OTHER LEAKS NOTED. CLEANED BELLY OF AIRCRAFT TO REMOVED OLD SKYDROL. OK TO INSTALL ACCESS PANEL. 2L72 4J RTT00007WI 20051128000812005112800081NM 2005 11 28 UPS05445806 120051118A541065B903604 THRUST LINK BOEING747 747200 1384847NM NR 1 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE:AD CRACK INDICATION REVEALED NR 1 PYLON THRUST LINK AFT LUG LOWER SURFACE BY APPROX 90 PERCENT FSH. NR 1 PYLON THRUST LINK REPLACED AND FWD AND AFT MOUNT BOLTS REPLACED AS PER AMM 71-21-03. 2L74 4F RTA20WE 20051128000832005112800083NM 2005 11 28 UPS05445808 120051118A541065B903604 THRUST LINK BOEING747 747200 1384847NM NR 3 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE:AD CRACK INDICATION REVEALED ON NR 3 PYLON THRUST LINK AFT LUG LOWER SURFACE BY APPROX 90 PERCENT FSH. NR 3 ENG PYLON THRUST LINK REPLACED AND AFT MOUNTING BOLT REPLACED AS PER AMM 71-21-03. 2L74 4F RTA20WE 20051128000842005112800084NM 2005 11 28 UPS05445809 120051119A541065B903604 THRUST LINK BOEING747 747200 1384847NM NR 4 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE:AD NR 4 PYLON REAR ENGINE MOUNT THRUST LINK AFT LUG FOUND CRACK INDICATION AT UPPER AND LOWER SURFACE APPROX 100 PERCENT FSH. NR 4 ENG MOUNT THRUST LINK REPLACED AS PER AMM 71-21-03. 2L74 4F RTA20WE 20051128000872005112800087NM 2005 11 28 UPS05645818 120051119A3244767NS TIRE BOEING767 767300 1385204NM NLG OUT OF ROUND A IPXAL ABORTED APPROACH O OTHER APAPPROACH 1 SO01323UP 27749 INSPECTION TYPE:ETOP ON TAKEOFF ROLL OUT OF CGN AIRCRAFT A SLIGHT ODOR OF RUBBER AND VIBRATION IN THE NOSE WHEEL THAT STARTED SLIGHT AND BECAME MODERATE TO S EVERE. CREW REQUEST EMERGENCY SUPPORT UPON LANDING IN EWR FOR SUSPECTED BLOWN NOSE TIRE. AIRCRAFT LANDED WITHOUT INCIDENT IN EWR. MX FOUND LT AND RT NOSE TIRE PROPERLY INSTALLED AND SERVICED. HOWEVER BOTH TIRES WHERE SEVERLY OUT OF ROUND. REMOVED AND REPLACED BOTH TIRE ASSY. AIRCRAFT DEPARTED AND LANDED IN SDF WITH NO FURTHER REPORT. 2L72 4F RTA1NM 20051128000882005112800088NM 2005 11 28 UPS05M45794 120051117A30203290278 ANTI-ICE VALVE DOUG MD11 MD11F 3023600NM LT WING WARNING LIGHT A IPXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01255UP 48404 INSPECTION TYPE:N/A ATB - ON CLIMBOUT OF CGN TURNED ON WING ANTI ICE GOT WING DISAGREE LIGHT FOLLOWED BY A LEVEL 2 ALERT WING ANTI-ICE K DISAGREE. PERFORMED QRH PROCEDURES. T/S PERFORMED AS PER FIM 30-11-00-1. FOUND LT WING A/I VLV AT FAULT. REMOVED AND REPLACED LT WING A/I VLV AS PER MM 36-11-01-4. L/C OK. ON BOTH PSC R-T-S TEST AS PER MM 36-10-02. NO FAULTS. WING A/I ADJ/TEST PERFORMED AS PER MM 30-11-00-5 FOUND SATISFACTORY. 2L73 4F RTA22WE 20051128000922005112800092WP 2005 11 28 ABXA050284 120051114A53119919619506N FRAME DOUG DC9 DC941 302207NWP BS 775 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23953AX 47608 RIGHT AFT OVER WHEEL WELL FRAME FS 775 FORWARD FLANGE CRACKED AT P & G. REPAIRED FRAME IAW JOB CARD EA 53400320-001-2. 2L72 4F A6WE 20051128000932005112800093NM 2005 11 28 QXEA200501545 120051117A3610 WARNING LIGHT BOMBDRDHC8 DHC8402 1390042NM NR 1 BLEED ILLUMINATED A QXEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM09402QX 4032 PDX FLIGHT 2450: NR 1 BLEED HOT CAUTION LIGHT ILLUMINATED (EXT ONCE NR 1 BLEED SELECTED OFF PER CHECKLIST AFTER ABOUT 45 SPC TO 1 MINUTE). MAINTENANCE COMPLIED WITH OPS TEST OF BLEED AIR SYSTEM PER 36-11-00. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051128000952005112800095NM 2005 11 28 UPS05M45812 120051119A5414 SKIN DOUG MD11 MD11F 3023600NM NR 1 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01277UP 48578 INSPECTION TYPE:N/A NR 1 ENGINE OUTBOARD PYLON HAS 1.5 INCH CRACK THRU A RIVET. REPAIRED PER SRM 54-00-01. 2L73 4F RTA22WE 20051128000992005112800099 2005 11 28 DXTA200501100 420051122A2300 CONTROL PANEL CESSNA650 650 2076802CE CABIN HOT E DXTAO OTHER MB OVER TEMP SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07782QS 6507082 AT FL390 RIGHT REAR PASSENGER AUDIO & LIGHTING PANELS WERE VERY HOT TO THE TOUCH. PANELS COOLED OFF ONCE AIRCRAFT WAS ON THE GROUND. BURNING WIRING ODOR IN A/C REAR, NO SMOKE OBSERVED. ITEM IS UNDER INVESTIGATION. 2L72 4F A9NM 20051128001012005112800101CE 2005 11 28 DXTA200501097 120051121A3010 ANTI-ICE SYSTEM CESSNA560 560XL 2076702CE RT ENGINE MALFUNCTIONED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07602QS 5605518 DURING TAKEOFF ROLL RT ENGINE ANTI-ICE ANNUNCIATOR ILLUMINATED WITH SWITCH IN THE OFF POSITION. TAKEOFF ABORTED. TROUBLESHOT ENGINE ANTI-ICE SYSTEM, PERFORMED ENGINE ANTI-ICE SYSTEM, FUNCTIONAL CHECK PER CESSNA 560XL MAINT MANUAL 30-11-00-710 SYSTEM FUNCTIONS PROPERLY AT THIS TIME. 2L72 4F RTA22CE 20051128001042005112800104CE 2005 11 28 DXTA200501081 120051112A2170 COALESCER BAG CESSNA560 560XL 2076702CE CABIN AIR DIRTY E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL07692QS 5605092 AFTER TAKEOFF A STRONG UNDESCRIBABLE ODOR IN COCKPIT, ODOR WAS NOT PRESENT DURING PREFLIGHT WITH APU RUNNING & BLEED AIR ON (APU WAS ON FOR 30 MIN) DID NOT ODOR LIKE ELECTRICAL, FUEL, OIL OR ENVIRONMENTAL ODOR PROBLEMS. DID NOTICE A FLICKER OF LIGHT ON THE MASTER CAUTION PANEL JUST BEFORE ODOR IN COCKPIT. DO NOT KNOW WHICH LIGHT, BUT IT WAS NEAR THE OIL FILTER BYPASS LIGHT. ODOR PROBLEMS. REMOVED APU OIL LEVEL SWITCH, CLEANED AND REINSTALLED. SERVICED APU OIL LEVEL AND OPS CHECK GOOD. REF 560XL MM 12-11-03, 49-10-00 (RE 100XL MM). REMOVED AND CLEANED COALESCER SOCK. REINSTALLED REF 560XL MM 21-51-00. OPS AND LEAK CHECK GOOD. NO FOUL SMELL NOTED. 2L72 4F RTA22CE 20051128001052005112800105NE 2005 11 28 NACA20050028 220051108A8530404481 CYLINDER DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE NR 8 CRACKED A NACAE ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 AL036174C1611 1611 44075 P33324 NR 1 ENGINE PRECAUTIONARY SHUTDOWN DUE TO BACKFIRING AND RUNNING ROUGH. REPLACED NR 8 CYLINDER DUE TO CRACKED HEAD IAW DC-6MM SECT V, PG 16 & 16A. OP CHECKED GOOD. 2L74 4R4 R 6A3 5E8 20051128001062005112800106NE 2005 11 28 CALA0500414 220051122A7200 ENGINE BOEING737 737824 13844BZNM GE CFM56 CFM56* 13802NE NR 1 FAILED A CALAO OTHER YJ ENGINE STOPPAGE WARNING INDICATION APAPPROACH 1 SW2718243 28806 875965 THE NR 1 ENGINE SHUDDERED AND AUTO SHUTDOWN WHILE ON APPROACH TO IAH. THE CREW DECLARED AN EMERGENCY AND LANDED AT IAH WITHOUT INCIDENT. INITIAL EXAMINATION OF THE ENGINE REVEALED THAT THE NR 1 ENGINE INLET AND EXHAUST WERE CLEAN. THE NR 1 ENGINE WAS REMOVED AND REPLACED. ENGINEERING INVESTIGATION CONFIRMED THE ENGINE FAILURE. BOTH VSV ACTUATORS WERE COMPLETELY OFF DEMAND SCHEDULE. THAT LED TO THE ENGINE STALL AND SUBSEQUENT ROLL TO SUB-IDLE AND ENGINE SHUT DOWN. 2L72 4F4 FRTA16WE E2GL 20051128001082005112800108NM 2005 11 28 QXEA200501546 120051119A6123 AUTOFEATHER SYS BOMBDRDHC8 DHC8402 1390042NM MALFUNCTIONED A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09402QX 4032 PDX FLIGHT 2339: NO AUTOFEATHER SELECT ON ED. MAINTENANCE CYCLED SHIPS POWER, PERFORMED AUTOFEATHER TEST, STARTED BOTH ENGINES AND COULD NOT DUPLICATE. NO FAULTS RECORDED IN CDS. OK FOR CONTINUED SERVICE. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051128001092005112800109EA 2005 11 28 COMA0560616 120051117A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS UNRELIABLE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01912CA156539569 7011 FLIGHT 5094 - FLAPS FAIL CAUTION.REPLACED THE LT BPSU. 2L72 4F RTA21EA 20051128001102005112800110EA 2005 11 28 COMA0560617 120051117A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS WARNING LIGHT A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01910EV 7727 FLIGHT 5901 - FLAPS FAIL CAUTION. RESEST FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2L72 4F RTA21EA 20051128001112005112800111NM 2005 11 28 QXEA200501548 120051120A2750 WARNING LIGHT BOMBDRDHC8 DHC8402 1390042NM TE FLAPS ILLUMINATED A QXEAD RETURN TO BLOCK J WARNING INDICATION NRNOT REPORTED 1 NM09411QX 4055 SEA FLIGHT 2312: FLAP POWER CAUTION LIGHT ILLUMINATED. MAINTENANCE CLEARED FLAP POWER CAUTION IAW DH8-400 SL-27-002A. NO OTHER DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051128001142005112800114NM 2005 11 28 QXEA200501547 120051120A3213 STRUT BOMBDRDHC8 DHC8402 1390042NM NLG OVERSERVICED A QXEAD RETURN TO BLOCK J WARNING INDICATION NRNOT REPORTED 1 NM09401QX 4031 SEA FLIGHT 2316: ALT FAIL MESSAGE BOTH NR 1 AND NR 2 PFD. MAINTENANCE FOUND NLG STRUT OVER-SERVICED CAUSING ASSOCIATED EQUIPMENT MALFUNCTION. SERVICED NLG STRUT IAW AMM 12-10-32. ALT FAIL MESSAGE WENT AWAY AND DID NOT REOCCUR. PERFORMED ADU NR 1 AND NR 2 SELF TEST. NO PROBLEMS NOTED. AIRCRAFT OK FOR CONTINUED SERVICE. AIRCRAFT REMAINS CAT 3 LLM PLACARD REFLECTS SAME. NO PARTS CHANGED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051128001162005112800116NM 2005 11 28 QXEA200501549 120051120A2750 WARNING LIGHT BOMBDRDHC8 DHC8402 1390042NM TE FLAPS FALSE ACTIVATIONA QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09410QX 4053 PDX FLIGHT 2352: FLAP POWER CAUTION AFTER START. MAINTENANCE CLEARED PER DH8-400-SL-27-002A. CYCLED FLAPS, NO CAUTION MESSAGE. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051128001182005112800118EA 2005 11 28 COMA0560620 120051118A4920 APU CNDAIRCL600 CL6002B19 1900309EA APU BAY SMOKE A COMAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO01472CA 7667 FLIGHT 5709 - ON ARRIVAL AT THE GATE IN BOS AND UPON SHUTTING-DOWN THE APU, SMOKE WAS OBSERVED FROM THE APU DUCT. SMOKE HAD FILLED THE AFT EQUIPMENT BAY. DEFERRED THE APU PER MEL 49-10-01-2. 2L72 4F RTA21EA 20051128001202005112800120NE 2005 11 28 72300250 220051122A7311320115 VALVE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUEL HEAT FAILED A K11AEJA ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23723CK 20545 NR 2 ENGINE OIL TEMPERATURE IN HIGH RANGE FOR 15 MINUTES WITH NR 2 FUEL HEAT VALVE ALREADY DEFERRED. ABNORMAL PROCEDURE GUIDELINES IN AOM REQUIRED PRECAUTIONARY ENGINE SHUT DOWN. AIRCRAFT RETURNED TO TUS. 2L73 4F4 FRTA3WE E2EA 20051128001212005112800121 2005 11 28 SCNA05010 420051105A2565 SLIDE BOEING737 7378Q8 13844BXNM R1 DOOR DISLODGED A SCNAO OTHER O OTHER NRNOT REPORTED 1 GL15801SY 30332 PILOT REPORTED R1 DOOR SLIDE FELL OUT OF SLIDE CASE, DOOR WAS DISARMED. MAINTENANCE INSTALLED R1 DOOR ESCAPE SLIDE PACK AND COVER PER TASK 25-66-01-400-801 RII ACCOMPLISHED 2083126. 2L72 4F RTA16WE 20051128001242005112800124NM 2005 11 28 XN0A1278 120051123A2797 WIRE BOEING727 727227 1384078NM WARNING SYS LOOSE A XN0AD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL2373751 21247 SPEED BRAKE/ FLAP WARNING WILL NOT TEST IN TAXI OUT AND T/O WARNING HORN. SECURED LOOSE WIRE ON AURAL WARN CB. CHECKS GOOD ON GROUND. 2L73 4F A3WE 20051128001252005112800125SO 2005 11 28 BSYA200500023 120051123A5210 LATCH PIPER PA31 PA31350 7103110SO CREW DOOR LACK OF LUBE E BSYAA UNSCHED LANDING O OTHER CLCLIMB 1 GL073547C 318052018 ON DEPARTURE OUT OF BUF, PILOTS CREW DOOR POPPED OPEN. AIRCRAFT RETURNED TO BUF. MAINTENANCE FOUND LATCHES STIFF TO OPERATE, LUBED LATCHES, OPS CHECKS GOOD. 1L72 3O A20SO 20051128001262005112800126CE 2005 11 28 BSYA200500021 120051116A3260 SQUAT SWITCH LEAR 35 35A 5170602CE MLG DIRTY E BSYAO OTHER J WARNING INDICATION CLCLIMB 1 GL07813AS 167 GOING OUT OF DSM LANDING GEAR WOULD NOT COME UP, CONTINUED ON TO MDW STILL NO GEAR UP. PILOT LEFT AIRCRAFT IN MDW. MAINTENANCE JACKED AIRCRAFT TO SWING GEAR COULD NOT DUPLICATE PROBLEM. MAINTENANCE THEN CLEANED AND LUBED SQUAT SWITCHES, SWUNG GEAR SEVERAL TIMES, COULD NOT GET IT TO MALFUNCTION. RELEASED FOR SERVICE. 2L72 4F A10CE 20051128001272005112800127 2005 11 28 XN0A1276 420051116A2210 COMPUTER AIRBUS300 A300B4203 3930306EU FLT DIRECTOR MALFUNCTIONED A XN0AD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL23372PC 196 CAPTAIN AND CENTER PANELS C/B TRIPPED, NR 1 FLT DIRECTOR INOPERATIVE. TRANSFERRED C/B DISCREPANCY TO DMI 5894 IAW ENA A300 MEL REF 33-12-01, CAT C, PLACARDS INSTALLED. TRANSFERRED FLT DIRECTOR DISCREPANCY TO DMI 5895 PER ENA A300 MEL REF 22-10-01, CAT C, PLACARDS INSTALLED. R&R CAPTAIN INSTRUMENT PANEL CONTROL SWITCH IAW A300 AMM 33-17-00, OPS CK GOOD. PLACARDS REMOVED. REF DMI 5895 CLEARED BY REPAIRED BROKEN WIRE TO NR 1 FLIGHT DIRECTOR LIGHT CONTROL RHEOSTAT I/A/W 300 AMM 22-10-00. OPS CK GOOD. PLACARDS REMOVED. REF TO DMI 5895 AIRCRAFT CLEARED FOR RVSM OPS.(STATUS: SUPP/CLOSED) 2L72 4F RTA35EU 20051128001292005112800129SO 2005 11 28 Z4TA20050004 220050919A8530537296 HOUSING BEECH 58 58 1152740CE CONT O550 IO550B SO PUSH ROD CRACKED E Z4TAK NONE K FLUID LOSS ININSP/MAINT 1 SO0595KM 1401 1401 TH1315 810485R PILOT REPORTED ABNORMAL OIL LOSS FOR RIGHT ENGINE. ALSO, OIL TRAIL ON LOWER RT WING. UPON INSPECTION, FOUND NR 6 CYLINDER FORWARD PUSH ROD HOUSING CRACKED, ALLOWING OIL TO DRAIN INTO LOWER COWL. REPLACED HOUSING. 1L72 3O3 O 3A16 E3SO 20051128001312005112800131CE 2005 11 28 BSYA200500022 120051122A5210 DOOR BEECH 58 58 1152740CE COCKPIT OPEN E BSYAA UNSCHED LANDING O OTHER CLCLIMB 1 GL073695V TH1183 ON CLIMBOUT OF LCK, COCKPIT DOOR CAME OPEN. RETURNED TO LCK, LANDED, CLOSED DOOR CORRECTLY AND CONTINUED ON WITH FLIGHT. 1L72 3O 3A16 20051128001322005112800132EA 2005 11 28 VTZA200500216 120051113A7931 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA RT ENGINE ILLUMINATED A VTZAE ENGINE SHUTDOWN J WARNING INDICATION DEDESCENT 1 EA27641BR 7349 RIGHT ENGINE LOW OIL PRESSURE WHEN REDUCING POWER BELOW 50 PERCENT. 2L72 4F RTA21EA 20051128001372005112800137NM 2005 11 28 SWAA053700 120051121A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER BFG ER. 2L72 4F RTA16WE 20051128001392005112800139NM 2005 11 28 SWAA053702 120051120A3350604222 BATTERY PACK BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29336SW 23940 DURING SCHEDULED 1/4D CHECK, FOUND L2 DOOR LOWER EMERGENCY EXIT LIGHTS ILLUMINATED WITH EMERGENCY LIGHT SWITCH IN THE OFF POSITION. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20051128001432005112800143NM 2005 11 28 SWAA053706 120051120A52306547952 DOOR FRAME BOEING737 7373H4 1384600NM AFT CARGO CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29369SW 26580 DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR FWD FRAME CRACKED AT LOWER STOP FITTING. REMOVED AND REPLACED CARGO DOOR PER MM. 2L72 4F RTA16WE 20051128001452005112800145NM 2005 11 28 SWAA053708 120051121A53116546529 BELTFRAME BOEING737 7375H4 138449DNM BS 482A CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29512SW 24189 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE BELTFRAME CRACKED AT BS 482A, STR 21L. REPAIRED BELTFRAME PER SWA EA. 2L72 4F RTA16WE 20051128001492005112800149SO 2005 11 28 C2XA05SH130 120051108A5753CRES155PH BUSHING EMB 145 EMB145EP 3260221SO TE FLAP GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714945 145049 SHV - DURING C-CHECK, MAINTENANCE FOUND LT I/B FLAP O/B BUSHING GOUGED (ON FLAP). MAINTENANCE REMOVED AND REPLACED LT I/B FLAP O/B BUSHING (ON FLAP) IAW EMB 145 EC5710-01096. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20051128001512005112800151SO 2005 11 28 C2XA05BT080 120051112A3110 LIGHT EMB 145 EMB145LR 3260212SO INSTRUMENT PANELARCED A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW2715983 145239 EWR---CO2996, CREW REPORTED ON CLIMB-OUT, ARC FLASHING OBSERVED BELOW LEFT CAPTAINS INSTRUMENT PANEL. CAPTAINS INSTRUMENT PANEL LIGHTS OUT AND CIRCUIT BREAKER POPPED. ALSO, INSULATION BURNING ODOR NOTED. EWR, MAINTENANCE INSPECTED AND RELEASED THE AIRCRAFT IAW MEL NR 33-10-00 CATEGORY "C" CONTROL NUMBER 062418, AIRCRAFT RETURNED TO SERVICE. EWR, MAINTENANCE RESET CAPTAINS PILOT LIGHTS CIRCUIT BREAKER AND PERFORMED OPERATIONAL CHECK OF PILOTS INSTRUMENT PANEL LIGHTS IAW EMB145 AMM NR 33-12-00. OPS CHECKED GOOD, NO BURNING SMELL NOTED. MEL CLEARED AND AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20051128001532005112800153SO 2005 11 28 C2XA05SH133 120051115A532014521700007 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713550 145575 SHV - DURING C-CHECK, MAINTENANCE FOUND LT OMEGA BEAM WITH CORROSION BETWEEN FRAMES 21 AND 24. MAINTEANANCE REPAIRED LT OMEGA BEAM BETWEEN FRAMES 21 AND 24 IAW EMB 145 EC5320-01257 REV B. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20051128001562005112800156NM 2005 11 28 ASAA0540436 120050830A5210652999413 GUIDE ARM BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU L-1 DOOR OUT OF RIG A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 CREW PREFLIGHT - L1 DOOR DIFFICULT TO CLOSE. RIGGED L-1 DOOR GUIDE ARM, CONTROL PUSHROD AND STOP PINS. (K) 2L72 4F4 FRTA16WE E21EU 20051128001572005112800157EA 2005 11 28 TIM2005F00007 220050922A7230 GAS GENERATOR BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA RT ENGINE SEIZED E TIMAO OTHER Y ENGINE STOPPAGE TOTAKEOFF 1 NM07194GA29832 UB8 RT ENGINE GAS GENERATOR SECTION SEIZED ON TAKEOFF ROLL, CAUSE OF THE FAILURE IS UNKNOWN AT THIS TIME. (K) 2L72 4T4 TRTA24CE E4EA 20051128001592005112800159NM 2005 11 28 ASAA0540358 120050717A57536546435339 SKIN BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU LT TE FLAP DEBONDED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02706AS 28894 LT OB AFT FLAP PREVIOUSLY INSTALLED REPAIR IS DEBONDING AT IB AFT CORNER. REMOVED DAMAGED AREA. FABRICATED AND INSTALLED FILLER AND DOUBLER AND INSTALLED REPAIR PIECES IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051128001612005112800161NM 2005 11 28 ASAA0540429 120050823A531565C339503 FLOORBEAM BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU BS 986 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 CORROSION ON FLOORBEAM. REMOVED TOP SECTION OF FLOORBEAM, FABRICATED AND INSTALLED REPAIR PARTS AND INSTALLED. (K) 2L72 4F4 FRTA16WE E21EU 20051118000942005111800094WP 2005 11 18 IXXA05RNG086S 120050928A5330 SKIN DOUG DC8 DC872 302199BWP STA 560 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK, FOUND CORROSION ON LOWER CARGO DOOR AFT JAMB STA 560 LONGERON 25 TO 33 RT. CORROSION WAS REMOVED IAW DC8 SRM 51-1-8 PAGE 20, THICKNESS MEASUREMENT WAS PERFORMED IAW ASTM 797-0 AND IT WAS FOUND OUT OF LIMITS IAW SRM 53-2-0 PAGE 2P. DAMAGE WAS REMOVED AND REINFORCEMENT DOUBLER WAS INSTALLED IAW EO ATI-091805 AND EWO ATI-53-031. 2L74 4F RT4A25 20051118000962005111800096WP 2005 11 18 IXXA05RNG095S 120050924A5230 RIVET DOUG DC8 DC872 302199BWP BS 420-440 LOOSE A IXXAO OTHER O OTHER ININSP/MAINT 1 SW11721CX 46013 DURING INSPECTION CHECK, A LOOSE RIVET WAS FOUND ON MAIN CARGO DOOR SKIN BETWEEN STA 420-440-LT. AS TEMPORARY REPAIR BLIND RIVETS WILL BE INSTALLED IAW BOEING MESSAGE 1-136637626 AND EWO ATI 52-004. SOLID RIVETS OR HI-LOCKS MUST BE INSTALLED WITHIN 6000 CYCLES. 2L74 4F RT4A25 20051118000982005111800098WP 2005 11 18 IXXA05RNG066S 120050909A5512 DOUBLER DOUG DC8 DC872 302199BWP STA XFS210-222 IMPROPER A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK, FOUND IMPROPER REPAIR ON RT HORIZONTAL STABILIZER L/E DOUBLER STA XFS 210-222.500. EXISTING DOUBLER WAS REMOVED AND A NEW REINFORCEMENT DOUBLER WAS INSTALLED IAW EO ATI 090805 AND EWO ATI-55-006. 2L74 4F RT4A25 20051121000272005112100027NM 2005 11 21 05FDEA03825 120051115A5330 REPAIR BOEING727 727225 1384077NM BS 376 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 EXISTING EXTERNAL REPAIR ON FUSELAGE BS 376 STR 21R-22R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. ALL WORK ACCOMPLISHED IAW FED EX EA 7-5330-91422. DETERMINED TO BE A MAJOR REPAIR. 2L73 4F A3WE 20051121000312005112100031NM 2005 11 21 05FDEA03829 120051115A5280 HINGE DOUG MD11 MD11 3023602NM ZONE 600 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 RIGHT MAIN LANDING GEAR WHEEL WELL DOOR AFT HINGE FOUND WORN. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL. II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051121000362005112100036EA 2005 11 21 COMA0560610 120051116A339759465 BUSS CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT UNRELIABLE A COMAO OTHER O OTHER NRNOT REPORTED 1 SO01962CA 7123 FLIGHT 5015 - THE AFT SECTION OF THE EMERGENCY FLOOR PATH LIGHTING INOPERABLE. REPLACED POWER STRIP. 2L72 4F RTA21EA 20051121000552005112100055NM 2005 11 21 05FDEA03795 120051114A5270 LIGHT BOEING727 727100 1384036NM AIRSTAIR WARNINGINOPERATIVE A FDEAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 SO25136FE 19855 RTO FOR AFT AIRSTAIR LIGHT IAS 75 KTS. RELEASED FOR SERVICE PER MEL/CDL: 52-06-B CATEGORY: C EXPIRATION: 22NOV05 MEL 52-06-B: AMBER AFT AIRSTAIR DOOR WARNING LIGHT INOP. VERIFIED AFT AIRSTAIR IS CLOSED AND RED LIGHT EXTINGUISHED. COMPLIED WITH TRO HIGH ENERGY STOP INSP IAW MM 05-51-121-6. NO ABNORMALITIES NOTED. OK FOR SERVICE. 2L73 4F RTA3WE 20051121000562005112100056EA 2005 11 21 VNAA0511002 120051106A5280 DOOR CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE NLG DAMAGED A VNAAO OTHER W INADEQUATE Q C TXTAXI/GRND HDL 1 GL05702PS 10135 THE LT NOSE LANDING GEAR DOOR WAS DAMAGED WHEN HIT BY A TOWBAR. THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE INSPECTED AND PERFORMED TEMPORARY REPAIRS IAW REO 670-52-81-015 AND SRM 52-81-02. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20051121000592005112100059EA 2005 11 21 VNAA0511001 120051102A34110856KV10 PITOT HEAD CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE BIRD STRIKE A VNAAO OTHER C F.O.D. APAPPROACH 1 GL05206PS4236 7860 AFTER LANDING THE CREW REPORTED A BIRD STRIKE TO THE RT SIDE OF THE RADOME AND RT PITOT TUBE. MAINTENANCE COMPLIED WITH A BIRD STRIKE INSPECTION. THE RT PITOT TUBE WAS FILLED WITH BIRD DEBRIS. NO OTHER DAMAGE WAS FOUND. THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE REMOVED & REPLACED THE RT PITOT PROBE. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20051122000012005112200001NM 2005 11 22 05FDEA03845 120051116A5230 DEPRESSOR BOEING727 727200 138407ENM CARGO DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 UPON REMOVAL OF AFT CARGO DOOR LOWER SEAL DEPRESSOR, FOUND STUB FRAME CRACKED AT BS 950F, RBL 40, WL 148 SECOND FRAME AFT FROM FWD SIDE OF DOOR. REMOVED AND REPLACED STUB FRAME AT BS 950F, RBL 40 WL 148 IAW SRM 51-30-2 AND SRM 51-30-5. 2L73 4F RTA3WE 20051122000052005112200005NM 2005 11 22 05FDEA03841 120051116A5311 FRAME BOEING727 727200 138407ENM BS 950B DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 AFT CARGO COMPARTMENT, FRAME IS DENTED BS 950B LBL 27 WL 148. REPAIRED FRAME PER SRM 51-40-3. 2L73 4F RTA3WE 20051122000132005112200013WP 2005 11 22 05FDEA03883 120051118A5753 REPAIR DOUG DC10 DC1030 3023501WP TE FLAP PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 RIGHT WING INBOARD FLAP FOUND DOUBLER REPAIR ON LOWER SKIN AT STA XIFH 189 DIMENS.8.5 X 5 INCHES. PERFORMED A GVI OF REPAIR IAW SRM 57-00-01 FIG 4 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001-P2 E3, RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VOL 2 PAR 33. 2L73 4F A22WE 20051122000142005112200014WP 2005 11 22 05FDEA03884 120051118A5730 REPAIR DOUG DC10 DC1030 3023501WP RT WING PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 RIGHT WING TIP WING FOUND DOUBLER REPAIR ON LOWER SKIN DIMENS 10 X 10 INCHES. PERFORMED A GVI OF REPAIR IAW SRM 57-00-01 FIG 4 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001-P2 E3. 2L73 4F A22WE 20051122000252005112200025WP 2005 11 22 05FDEA03855 120051117A5313 LONGERON DOUG DC10 DC1030 3023501WP BS 1523 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 THE CENTER CARGO COMPT BILGE UNDERFLOOR SPACE AT STA 1523 L45 LT SIDE FOUND CORROSION WITH EXFOLIATION ON INTERNAL OF LONGERON AROUND FASTENERS. REMOVED FASTENERS IAW SRM 51-33-01 PG 6/10 VOL 2. REMOVED CORROSION IAW SRM 51-21-01 PAR 34 VOL 2 ORIGINAL MATERIAL THK IS .250 INCH REMAIN MATERIAL THK .170 MATERIAL. REMOVED IS OUT OF LIMITS IAW SRM 53-00-00 FIG 1B. FABRICATED PART IAW DETAIL PART TRAVELER F160212-5 IAW SRM 53-10-00 VOL 2 FIG 2A SHT 1. TREATED REWORKED AREA IAW SRM 51-21-01 PAR 31-24 VOL 2. INSTALLED A REINFORCE/REPAIR ANGLE IAW SRM 53-10-00 VOL 2 FIG 2A SHT 1. INSTALLED FASTENERS IAW SRM 51-33-01 PG 34/47. 2L73 4F A22WE 20051122000302005112200030NM 2005 11 22 AALA20050754 120051116A3350P4010051112 MODULE BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21179AA 32397 IAD - EMERGENCY EXIT LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED POWER SUPPLY MODULE M10978 AND BATTERY PACK FOR EMERGENCY EXIT LIGHTS IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20051122000322005112200032NM 2005 11 22 AALA20050753 120051115A3350 LIGHT BOEING737 737823 13844BZNM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21964AN 30093 MIA - EMERGENCY LIGHT AT SEAT 7D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20051122000432005112200043WP 2005 11 22 05FDEA03864 120051118A5753 REPAIR DOUG DC10 DC1030 3023501WP TE FLAP UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 LT WING OUTBOARD FLAP UPPER SKIN FOUND A FLUSH DOUBLER 39.25 X 36.50 INCHES WITH INSIDE SPLICES BETWEEN XOF 593 AND XOF 557. REMOVED T/E SECTION OF O/B FLAP IN ORDER TO ACCOMPLISH REPAIR IAW DRAW ARC 453. INSTALLED REPAIR IAW FED EX EA 8-5750-88900 AND SRM 57-10-00 FIG 7 VOL 1. REINSTALLED T/E SECTION OF O/B FLAP IAW DRAW ARC 1653. 2L73 4F A22WE 20051122000452005112200045WP 2005 11 22 05FDEA03866 120051118A5311 REPAIR DOUG DC10 DC1030 3023501WP BS 675 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 MAIN CARGO COMPT AT STA 675 L12 RT FOUND FRAME WITH REPAIR DOUBLER 11 X 3 INCHES AND FLUSH REPAIR Z 60 X 92. STRIPPED AREA IAW SRM 51-21-01 PAR 33 VOL 1. REMOVED AND REPLACED FASTENERS AS REQ ON SRM 53-30-00 FIG 4 VOL 1. TREATED AND PROTECTED AREA IAW SRM 51-21-01 VOL 2. 2L73 4F A22WE 20051122000502005112200050NM 2005 11 22 05FDEA03871 120051118A5322 SHEAR TIE BOEING727 727200 138407ENM BS 1090 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 EXERNAL FUSELAGE SKIN PILLOWING AROUND SHEAR TIE FASTENERS AT BS 1090, STR 28 - 29 LEFT. REMOVED SHIM BETWEEN SHEAR TIE & FUSELAGE SKIN AT BS 1090 STR 28-29L FABRICATED NEW SHIM & INSTALLED PER SRM 51-10-2, 51-30-2. 2L73 4F RTA3WE 20051122000522005112200052WP 2005 11 22 05FDEA03873 120051118A5330 REPAIR DOUG DC10 DC1030 3023501WP BS 885 PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 FOUND DOUBLER LENGTH 7 INCHES WIDTH 21 INCHES ON RIGHT EXT FUSELAGE AT STA 885 FROM LONG 39 TO LONG 41. PERFORMED INSPECTION ON REPAIR DOUBLER IAW EA8-5320-40401 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P1 E3. 2L73 4F A22WE 20051122000542005112200054WP 2005 11 22 05FDEA03875 120051118A5751 REPAIR DOUG DC10 DC1030 3023501WP WS 997 LT PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 LEFT WING OUTBOARD AILERON LOWER SURFACE FOUND A FLUSH DOUBLER 27 X 16.5 INCHES ON SKIN AT STA XOA 997. PERFORMED INSPECTION ON REPAIR IAW SRM 57-10-00 FIG 2 VOL 1, FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2 E3. 2L73 4F A22WE 20051122000632005112200063EA 2005 11 22 VNAA0510023 120051028A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A VNAAL ABORTED APPROACH F FLT CONT AFFECTED APAPPROACH 1 GL05209PS 7874 DURING APPROACH THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED WITH FLAPS AT 20 DEGREES SELECTED TO 30 DEGREES. THE CREW ABORTED THE APPROACH, RECONFIGURED THE AIRCRAFT, AND LANDED WITHOUT INCIDENT. MAINTENANCE RECORDED FECU LRU & FAULT LOG CONTENTS PER THE FIM. AN OPERATIONAL TEST OF THE FLAP SYSTEM WAS PERFORMED IAW CRJ200 AMM 27-54-00-710-801. THE FLAP SYSTEM OPS CHECKED GOOD AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20051122000662005112200066EA 2005 11 22 REX200500137 120051115A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A REXAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO25829AY 8029 FLAPS FAIL AT GATE. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD98-20-01. 2L72 4F RTA21EA 20051122000672005112200067EA 2005 11 22 VNAA0510021 120051025A5751 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT AILERON UNDAMAGED A VNAAK NONE O OTHER ININSP/MAINT 1 GL05251PS 7931 DURING AN FAA RAMP CHECK, THE INSPECTOR DISCOVERED EVIDENCE OF LIGHTNING STRIKE DAMAGE ON TOP OF THE LT AILERON. THE AIRCRAFT WAS FERRIED TO CAK. MAINTENANCE COMPLIED WITH A DETAILED LIGHTNING STRIKE INSPECTION AND FOUND NO LIGHTNING DAMAGE TO THE AIRCRAFT. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20051122000682005112200068EA 2005 11 22 VNAA0511009 120051112A2720 PEDAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FOD IN COCKPIT OBSTRUCTED A VNAAC ABORTED TAKEOFF CF F.O.D. FLT CONT AFFECTED TOTAKEOFF 1 GL05220PS 7887 THE TAKEOFF WAS REJECTED DUE TO BINDING IN THE RUDDER PEDALS. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE FOUND A COCKPIT SUN VISOR JAMMING THE RT RUDDER PEDALS. THE SUN VISOR WAS REMOVED AND THE RUDDER SYSTEM OPERATIONALLY CHECKED GOOD IAW CRJ200 AMM 27-21-00-710-801. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20051122000712005112200071NM 2005 11 22 SWAA053651 120051117A3350D71702001 BATTERY PACK BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED SERVICE CHECK, FOUND FWD GALLEY EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20051122000892005112200089SO 2005 11 22 RAIA00511024 120051118A3350 LAMP EMB 145 EMB145 3260210SO EMERGENCY LIGHT INOPERATIVE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03803HK 145077 PRE-FLIGHT - STL - EMERGENCY LIGHT IN GALLEY INOP. MAINTENANCE RELAMPED LIGHT ASSEMBLY AND RESECURED LOOSE CONNECTION AT SERVICE DOOR SHROUD. 2L72 4F RTT00011AT 20051122000922005112200092NM 2005 11 22 AWXA200501425 120051101A534365494427 FITTING BOEING737 7373S3 1384711NM LT MLG ATTACH CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 MCN - DURING C13 CHECK DISCOVERED CORROSION ON THE LT MAIN LANDING GEAR FORWARD STABILIZER BEAM ATTACH FITTING. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 57-20-90-1A2 FIG 101. MAINTENANCE REMOVED AND REPLACED THE LT MLG FORWARD STABILIZER ATTACH FITTING IAW BOEING 737-300 AMM 20-50-11-2 FIG 202. 2L72 4F RTA16WE 20051122000932005112200093NM 2005 11 22 AWXA200501426 120051028A534365494428 ATTACH FITTING BOEING737 7373S3 1384711NM RT MLG CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 MCN - DURING C13 CHECK DISCOVERED CORROSION ON THE RT MAIN LANDING GEAR FORWARD STABILIZER BEAM ATTACH FITTING. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 57-20-90-1A2 FIG 101. MAINTENANCE REMOVED AND REPLACED THE RT MLG FORWARD STABILIZER ATTACH FITTING IAW BOEING 737-300 AMM 20-50-11-2 FIG 202. 2L72 4F RTA16WE 20051122001042005112200104 2005 11 22 AWXA200501416 420051117A3417 ADC BOEING737 7373G7 1384595NM NR 2 MALFUNCTIONED A AWXAA UNSCHED LANDING GJ MULTIPLE FAILURE WARNING INDICATION CLCLIMB 1 WP28154AW 23776 ON CLIMB-OUT, CREW REPORTED AT 80 KNOTS AUTO THROTTLES KICKED OFF AND AROUND 150 KNOTS F/O LOST ALL AIR DATA INSTRUMENTS, ALSO HAD SPEED TRIM FAULT & STALL WARNING. REPORTED THAT ERRORS DECREASED DURING DESCENT. RETURNED & LANDED WITHOUT FURTHER INCIDENT. MX R & R NR 2 ADC IAW MM 34-11-00-501. DURING LEAK CHK, DISCOVERED LEAK IN F/O'S STATIC SYS. REPLACED A CRACKED TEE FITTING. FINAL OPS & LEAK CHECKS GOOD. VENDOR TEAR DOWN REPORT CONFIRMS FAILURE. UNIT FAILED ALTITUDE, AIRSPEED AND POWER INTERRUPT TESTS. FOUND UNIT HIGHLY CONTAMINATED. UNIT WAS OVERHAULED DUE TO EXTENT OF REPAIR REQUIRED. ALL WORK AND OPERATIONAL TESTS WERE PERFORMED IAW ATA 34-11-02. 2L72 4F RTA16WE 20051122001132005112200113NM 2005 11 22 05FDEA03917 120051119A5347 SEAT TRACK DOUG MD11 MD11 3023602NM BS 6-100-1149 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 MAIN DECK CABIN, STA 6-100 TO 1149 RBL 8 SEAT TRACK FOUND CORRODED. REPAIR CARRIED OUT IAW SRM 53-70-00. 2L73 4F RTA22WE 20051122001192005112200119EU 2005 11 22 05FDEA03900 120051118A3240 INDICATOR AIRBUS300 A300F4605R 3930327EU BRAKE SYSTEM MALFUNCTIONED A FDEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO25668FE 772 FL320, THE RT BRAKE PRESS GAUGE INCREASED O TO 2000 PSI. AFTER 12 MIN IT DECREASED TO 1500 PSI. AFT 30 MIN IT DECREASED TO 400 PSI. BRAKE A/S SELECTOR WAS IN THE NORMAL ON POS. ALL WHEEL BRAKES SHOWED REL ON ECAM. PARKING BRAKE WAS VERIFIED OFF. LATER IN THE FLIGHT FROM OAK, THE PROBLEM REPEATED. DURING DESCENT RT BRAKE PRESSURE DECREASED TO ZERO. NORMAL LNDG. PERF OPS TEST OF ALT BRAKING SYS PER MM 32-43-00. OPS CK OK. PERF OPS TEST OF PARKING BRAKE SYS PER MM 32-45-00. OPS CK OK. REMOVED AND REPLACED BRAKE YELLOW PRESS TRIPLE IND MM 32-44-19-4 PRECAUTIONARY. REMOVED AND REPLACED YEL BRAKE SYS PRESS TRANSMITTER 72GG. 2L72 4F RTA35EU 20051122001272005112200127NM 2005 11 22 UPS05545789 120051116A29133508806 PUMP BOEING757 75724APF 1384969NM RROYCERB211 RB211535E4 54555NE NR 1 ENGINE CRACKED A IPXAH DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO01468UP 25484 HYDRAULIC QTY DECREASED TO ZERO AND SYSTEM PRESSURE LIGHT ILLUMINATED. EICAS MESSAGE "L1 HYD SYS PRESS" DISPLAYED. NOTE: PER PILOT EVENT REPORT "DECLARED EMERGENCY". FOUND LT EDP CASE CRACKED AND METAL IN CASE DRAIN AND PRESS FILTER IN MODULE. FLUSHED PUMP PRESS LINES AND CHECKED LT AC PUMP AND MAIN RETURN FILTERS NO CONTAMINATION FOUND. REMOVED AND REPLACED LT EDP IAW 29-11-05-4. OPS CK OK. 2L72 4F4 FRTA2NM E12EU 20051122001302005112200130WP 2005 11 22 UPS05845788 120051020A5512 SKIN DOUG DC8 DC873F 302199FWP HORIZONTAL STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE:C1 INTERGRANULAR CORROSION ON LT HORIZ STAB L/E UPPER SKIN AT SEGMENT JOINT. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER AND 2 EA. FILLERS IAW SRM 55-02-01 FIG 004. 2L74 4F RT4A25 20051128001632005112800163WP 2005 11 28 ASMF200511006 120051108A3241392492 CONTROL VALVE DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE RT MLG ANTI-SKIDFAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23501AM32 49188 AIRCRAFT RETURNED TO PLATFORM, PARKING BREAK CONTROL BREAKER M-36 WAS THROWN OUT CAUSING ALL ANTISKID LIGHTS TO TURN ON. DURING OVERNIGHT CHECK, THE ANTISKID SYSTEM DUAL SERVO VALVE OF THE INNER RT SIDE WAS REPLACED IAW MM 32-43-03, TESTED CORRECT. 2L72 4F4 F A6WE E2EA 20051128001672005112800167CE 2005 11 28 DXTA200501061 120051104A3260327 BULB CESSNA500 560CESSNA 2076750CE PWA 530 PW535A NE BURNED OUT E DXTAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL07807QS 5600617 RT MAIN LANDING GEAR LIGHT WOULD NOT ILLUMINATE. FOLLOWED EMERGENCY CHECKLIST PRIOR TO LANDING. BLEW DOWN W/ EMERGENCY PNEUMATIC AIR. ROTARY TEST VERIFED LIGHT INOPERATIVE. REMOVED AND REPLACED BULB, OPS CHECK GOOD. CYCLED GEAR 10 TIMES AFTER RESETTING BOTTLE. SERVICED BOTTLE AND SAFTIED. GEAR OPS CHECKS GOOD. RESERVOIR AT FULL IAW MM 32-01-00 AND 33-11-01. 2L72 4F4 FRTA22CE E00053EN 20051128001692005112800169SW 2005 11 28 YTRR106612 120051030A6710106310405103 UNIVERSAL JOINT BELL 407 407 1182206SW ALLSN 250C 250C47B GL FUSELAGE TOP WORN B YTRRK NONE E VIBRATION/BUFFET ININSP/MAINT 1 SO01595RL242 53595 UNIVERSAL BEARING ASSEMBLY FOUND WORN. REPLACED PART. 1G71 3U3 UO H2SW E1GL 20051128001702005112800170SW 2005 11 28 YTRR106613 120051012A6710406310405101 UNIVERSAL JOINT BELL 407 407 1182206SW ALLSN 250C 250C47B GL FUSELAGE TOP WORN B YTRRK NONE E VIBRATION/BUFFET ININSP/MAINT 1 SO01407HX370 53092 UNIVERSAL BEARING ASSEMBLY FOUND WORN. REPLACED BEARING ASSY. 1G71 3U3 UO H2SW E1GL 20051128001712005112800171SW 2005 11 28 YTRR106615 120051012A6710406310404101 UNIVERSAL JOINT BELL 407 407 1182206SW ALLSN 250C 250C47B GL FUSELAGE TOP WORN B YTRRK NONE E VIBRATION/BUFFET ININSP/MAINT 1 SO01407HX370 53092 UNIVERSAL BEARING ASSEMBLY FOUND WORN. REPLACED BEARING ASSY. 1G71 3U3 UO H2SW E1GL 20051128001722005112800172SW 2005 11 28 YTRR106618 120050918A6710406310405101 UNIVERSAL JOINT BELL 407 407 1182206SW ALLSN 250C 250C47B GL FUSELAGE TOP WORN B YTRRK NONE E VIBRATION/BUFFET ININSP/MAINT 1 SO01163RL252 53163 UNIVERSAL BEARING ASSEMBLY FOUND WORN. REPLACED BEARING ASSY. 1G71 3U3 UO H2SW E1GL 20051128001792005112800179NM 2005 11 28 QXEA200501552 120051121A2930 WARNING LIGHT DHAV DHC8 DHC8202 2809007NM HYD SYSTEM ILLUMINATED A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09356PH 502 PDX FLIGHT NR 2162, NR 1 STANDBY HYDRAULIC PRESSURE READS ZERO PSI WITH PROPS OUT OF FEATHER AND BOTH SWITCHES AT 1 AND 2. MAINTENANCE FOUND CIRCUIT BREAKER 29218 IN RIGHT WHEEL WELL OPEN, INSPECTED NR 1 STANDBY PUMP FOR OBVIOUS DEFECTS, NONE NOTED. RESET CIRCUIT BREAKER 29218 (REF HORIZON AIR GMM 5-18-0) COMPLIED WITH GROUND RUN AND CYCLED NR 1 HYDRAULIC SYSTEMS USING NR 1 STANDBY PUMP. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051128001802005112800180NM 2005 11 28 QXEA200501541 120051118A6120 TRU DHAV DHC8 DHC8202 2809007NM NR 2 PROPELLER OUT OF ADJUST A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09358PH 506 SEA FLIGHT NR 2154 , DURING AUTOFEATHER TEST OF NR 2 PROP A RIGHT TRU CAUTION CAME ON TESTED SEVEN DIFFERENT TIMES WITH PROP RPM NO GOING BELOW 650. MAINTENANCE COMPLIED WITH ADJUST/TEST OF THE LEFT AND RIGHT TRU'S IAW DHC-8 AMM 24-31-505-508, OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051128001822005112800182NM 2005 11 28 05FDEA03927 120051121A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 HORIZONTAL STABILIZER RIGHT NR 36 BORE FOUND CORROSION EXCEED LIMITS. REPAIR CARRIED OUT IAW FEDEX EA 1-5510-94568. 2L73 4F RTA22WE 20051128001832005112800183WP 2005 11 28 05FDEA03929 120051121A5410 FRAME DOUG DC10 DC1030 3023501WP BULKHEAD CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25310FE 48299 NR 1 ENG NOSE INLET COWL INTERIOR AFT BULKHEAD CHORD ANGLE IS CRACK AT 7 O`CLOCK POSITION CAN BE VIEWED FROM OUTBOARED SIDE. REMOVED AND REPAIRED CRACKED CHORD ANGLE IAW DC10 SRM 54-11-00, FIG 1C VOL 1. N/R # N00405, W/O NR 00030375. 2L73 4F A22WE 20051128001842005112800184NM 2005 11 28 05FDEA03930 120051121A5330 REPAIR BOEING727 727225 1384077NM BS 1217 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 EXISTING EXTERNAL REPAIR WITH BLIND FASTENERS AT BS 1217 S28R 4" BY 4" BY 0.032". REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THIS REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. ALL WORK ACCOMPLISHED IAW FED EX EA 7-5330-91417. REPAIR WAS FOUND TO BE A MAJOR 2L73 4F A3WE 20051128001882005112800188 2005 11 28 MWEA050124 420051118A25652560137 SLIDE DOUG MD88 MD88 3023688NM TAILCONE INOPERATIVE A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 TAIL SLIDE DID NOT DEPLOY WHEN TAILCONE WAS DROPPED. REPLACED LANYARD AND INSTALLED TAILCONE AND SLIDE. 2L72 4F RTA6WE 20051128001892005112800189NM 2005 11 28 MWEA050125 120051118A322059404973 SCHRADER VALVE BOEING717 717200 1383700NM NLG INOPERATIVE A MWEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31924ME 55190 NOSE LANDING DID NOT RETRACT AFTER TAKEOFF. NO SIGNS OF LEAKING, REMOVED AND REPLACED SCHRADER VALVE AND SERVICED STRUTS. 2L72 4F TRA6WE 20051128001902005112800190NM 2005 11 28 MWEA050127 120051122A521059100817 SKIN BOEING717 717200 1383700NM PAX DOOR DEFORMED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31907ME 55171 PASSENGER DOOR LOWER AFT CORNER SKIN EDGE IS DEFORMED. RECONSTRUCTED SKIN AND BLENDED SCRATCHES. 2L72 4F TRA6WE 20051128001922005112800192NE 2005 11 28 COMA0560628 220051119A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE LEFT VIBRATION A COMAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 SO01735CA 7473 807557 FLIGHT 5004 - DURING TAKEOFF, ROLL RECEIVED A LT ENGINE VIBRATION CAUTION, ABORTED TAKEOFF AND RETURNED TO GATE. PERFORMED AN INSPECTION OF THE MASTER CHIP DETECTOR, PERFORMED GROUND RUNS, DISCREPANCY COULD NOT BE DUPLICATED. 2L72 4F4 FRTA21EA E15NE 20051128001952005112800195EA 2005 11 28 COMA0560630 120051121A326046193 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA MLG FAULTY A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01798CA14689 7348 FLIGHT 5573 - DURING CVG APPROACH RECEIVED A GEAR DISAGREE WARNING WHEN LOWERED. CREW DECLARED AN EMERGENCY, ABORTED APPROACH, CYCLED GEAR AGAIN WITH NORMAL INDICATION AND THEN LANDED WITHOUT INCIDENT ON SECOND ATTEMPT. REPLACED THE MLG PRIORITY VALVE. 2L72 4F RTA21EA 20051128001962005112800196EA 2005 11 28 COMA0560625 120051119A27501217542 DRIVE SHAFT CNDAIRCL600 CL6002B19 1900309EA RT WING WORN A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01735CA8360 7267 FLIGHT 5404 - EN ROUTE PHL-CVG, DURING APPROACH RECEIVED A FLAP FAIL CAUTION AT ZERO DEGREE FLAP POSITION. CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE RIGHT WING FLEX DRIVE SHAFT. 2L72 4F RTA21EA 20051128001972005112800197EA 2005 11 28 COMA0560626 120051119A27501217546 DRIVE SHAFT CNDAIRCL600 CL6002B19 1900309EA RT WING WORN A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01765CA8360 7267 FLIGHT 5404 - EN ROUTE PHL-CVG, DURING APPROACH RECEIVED A FLAP FAIL CAUTION AT ZERO DEGREE FLAP POSITION. CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. 2L72 4F RTA21EA 20051128002002005112800200WP 2005 11 28 IXXA05RNG101S 120050908A5730 SKIN DOUG DC8 DC872 302199BWP WS 761.695 UNBONDED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK, FOUND LT WING UPPER SKIN PANEL AT STA XW 761.695 DISBONDED. SKIN WAS REMOVED AND REPLACED ON LT WING UPPER PANEL IAW DOUGLAS DRAWING 5644654, RIVETS WERE INSTALLED IAW DC8 SRM 51-1-21 PAGE 1-7 AND PROTECTIVE TREATMENT WAS APPLIED IAW DC8 SRM 51-1-8 PAGE 13-16. 2L74 4F RT4A25 20051128002012005112800201WP 2005 11 28 IXXA05RNG087S 120050926A5330 SKIN DOUG DC8 DC872 302199BWP BS 1530 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK, FOUND A CORROSION ON FORMER STA 1530 LONGERON 28 - RT. CORROSION WAS REMOVED IAW DC8 SRM 51-1-8 PAGE 20, THICKNESS MEASUREMENT WAS PERFORMED IAW ASTME 797-01 AND IT WAS FOUND OUT OF LIMITS. DAMAGE WAS REPAIRED IAW SRM 53-2-5 FIG 8C-1 AND EWO ATI-53-034. 2L74 4F RT4A25 20051128002072005112800207NM 2005 11 28 AWXA200501430 120051025A57536546486130 SKIN BOEING737 7373S3 1384711NM TE FLAP DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 MCN - DURING C13 CHECK DISCOVERED DISBOND AREA AT THE OUTBOARD END OF THE RT INBOARD MID-FLAP TRAILING EDGE WEDGE. MAINTENANCE CUTOUT DISBOND AREA ON THE UPPER AND LOWER SURFACES IAW BOEING 737-300 SRM 51-70-10-2R4 FIG 203. FABRICATED REPLACEMENT CORE AND DOUBLERS IAW BOEING 737-300 SRM 57-53-02-0I1 FIG 1 AND 51-30-01-0G FIG 2. BONDED REPLACEMENT CORE TO THE REPAIR AREA ON THE RT INBOARD MID-FLAP TRAILING EDGE WEDGE IAW BOEING 737-300 SRM 51-70-10-2R4. 2L72 4F RTA16WE 20051128002112005112800211SO 2005 11 28 CHQA200500198 120051116A3350100865 BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11570RP1342 1342 14500821 EMERGENCY STRIP LIGHT 1 THROUGH 7 INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY. OPS CHECK GOOD AT THE GALLEY AREA IAW EMB 145 MM 33-50-00. 2L72 4T RTT00011AT 20051128002122005112800212WP 2005 11 28 IXXA05RNG102S 120050908A5720 PLATE DOUG DC8 DC872 302199BWP STA XFS 510.222 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK, FOUND A CRACK ON CENTER L/E SLOT DOOR PLATING AROUND STA XFS 510.222-LT. DAMAGE WAS REPAIRED IAW EO ATI-092705 AND EWO ATI 57-052. 2L74 4F RT4A25 20051128002152005112800215WP 2005 11 28 IXXA05RNG105S 120050910A5542 SKIN DOUG DC8 DC872 302199BWP RUDDER CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK, FOUND CORROSION ON LT RUDDER STA´S ZR 335.250, ZR 327 - 319, ZR 310.688, ZR 300 - 290. SKIN WAS REMOVED AND REPLACED IAW DOUGLAS DRAWING 5655077 VIEW A-B&C AND RIVETS WERE INSTALLED IAW DC8 SRM 51-1-21 PAGE 1-7. 2L74 4F RT4A25 20051128002172005112800217WP 2005 11 28 IXXA05RNG108S 120050917A5522 SKIN DOUG DC8 DC872 302199BWP ELEVATOR CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK, FOUND A CORROSION ON RT ELEVATOR UPPER SURFACE, STA XE 246.875-XE 272. SKIN WAS REPLACED IAW DOUGLAS DRAWING 5654970 AND RIVETS WERE INSTALLED IAW DC8 SRM 51-1-21 PAGE 1-7. 2L74 4F RT4A25 20051128002192005112800219NM 2005 11 28 SWAA053710 120051121A53306545769 SKIN BOEING737 7375H4 138449DNM BS 465-471 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29512SW 24189 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE LOWER SKIN CORRODED BETWEEN BS 465 TO BS 471, AT NR 1 DME ANTENNA. REPAIRED SKIN PER SWA EA AND SRM. 2L72 4F RTA16WE 20051128002202005112800220NM 2005 11 28 SWAA053711 120051120A53306545775 SKIN BOEING737 7375H4 138449DNM BS 844 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29513SW 24190 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 844, STR 25L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051128002242005112800224NM 2005 11 28 SWAA053715 120051121A55536547450 FITTING BOEING737 7373H4 1384600NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED D CHECK, FOUND LT AND RT VERTICAL STAB ATTACH FITTING FWD AND AFT PRIMARY CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER. 2L72 4F RTA16WE 20051128002252005112800225 2005 11 28 BSY2005F00002 420051111A341670310N01D01 INDICATOR LEAR 35 35LEAR 5170600CE GARRTTTFE731TFE731* 01518WP ALTITUDE INOPERATIVE E BSYAO OTHER O OTHER NRNOT REPORTED 1 GL071140A 35045 FLIGHT CREW REPORTED THE PILOTS ALTIMETER AND ALTITUDE ALERTER BLANKED OUT DURING CLIMBOUT IN HEAVY RAIN. THE CONNECTOR ON THE PILOTS ALTIMETER INDICATOR WAS REASEATED ANDTHE PILOTS ALTIMETER SYSTEM WAS TESTED AND INSPECTED AND FOUND TO COMPLY AND TO REMAIN RVSM COMPLIANT. THERE HAVE BEEN ON PRIOR REPORTS OF PROBLEMS WITH THIS AIRCRAFT. (NOTE: SEE CONCURRENT REPORT ON THIS AC REGARDING THE AIR DATA COMPUTER). (K) 2L72 4F4 F A10CE E6WE 20051128002262005112800226EA 2005 11 28 A6WA200540325 120051113A5320 SUPPORT ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FS 621 CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31426AW 7669 LT FS621 FLOOR SUPPORT ANGLE IS CRACKED MAINTENANCE PERFORMED REPAIR TO LT FS 621.00 FLOOR SUPPORT ANGLE IAW REO. (K) 2L72 4F4 FRTA21EA E15NE 20051129000022005112900002NM 2005 11 29 CALA0500416 120051123A531565C33950 FLOORBEAM BOEING737 737524 1384721NM BS 986.5 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713624 27528 INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT STA 986.5, RBL 28 TO RBL 45.5 (RIGHT I/B OF R-2 DOOR Z-ANGLE). A REPAIR WAS INSTALLED IAW SRM 53-00-51, FIGURE 201. 2L72 4F RTA16WE 20051129000042005112900004 2005 11 29 QXEA200501567 420051123A3417 ADC BOMBDRDHC8 DHC8402 1390042NM COCKPIT MALFUNCTIONED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09408QX 4050 PDX FLIGHT 2309: FD ADC DATA INVALID MESSAGE ON CAPTAIN'S PFD. MAINTENANCE PERFORMED OPS TEST OF AIR DATA COMPUTER IAW MTC 6341101. RESET C/B ADV1 AND ADV2 (A7 AND A6). ALL CHECKS GOOD. AIRCRAFT PLACARD READS CAT III. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051129000052005112900005NM 2005 11 29 SB05153 120051124A335020121 CHARGER BOEING737 737401 1384701NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19409US 23879 PVD - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT OVER THE L2 DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20051129000062005112900006NE 2005 11 29 EMB05017 220051121A7200426000183 CONTROL QUADRANT EMB ERJ170ERJ170100 EU GE CF34 CF348E5 30015NE THRUST CONTROL UNKNOWN A USAAO OTHER O OTHER TXTAXI/GRND HDL 1 EA19813MA3833 17000031 ENGINE NR 2 WOULD NOT START. AIRFLOW APPEARS NORMAL FOR START CONFIGURATION, NO N2 OR N1 ROTATION. AIRCRAFT RELEASED ON MEL. 11/23/05 - TROUBLESHOT SYSTEM, REMOVED AND REPLACED THRUST CONTROL QUADRANT W/AUTO. OPERATIONAL CHECK IS GOOD ON GROUND RUN UP. 2L74 4F4 FRTA56NM E00063EN 20051129000082005112900008WP 2005 11 29 05FDEA03928 120051121A7160 FRAME DOUG DC10 DC1030F 3023504WP NR 1 INLET COWL CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25310FE 48299 NR 1 ENG NOSE INLET COWL INTERIOR AFT BULKHEAD CHORD ANGLE IS CRACK AT 7 O`CLOCK POSITION CAN BE VIEWED FROM OUTBOARD SIDE. REMOVED AND REPAIRED CRACKED CHORD ANGLE IAW DC10 SRM 54-11-00 FIG 1C VOL 1. N/R N00405, W/O N/R 00030375. 2L73 4F RTA22WE 20051129000102005112900010NM 2005 11 29 05FDEA03947 120051123A5753NRC6753504 SKIN DOUG MD11 MD11 3023602NM TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 SNRM N0596: RH WING OUTBD FLAP AFT INBD HINGE BRACKET FWD OUTBD AFT ATTACH HOLE FOUND WITH CORROSION. CORRECTIVE ACTION: SNRM N0596: RIGHT HAND OUTBOARD FLAP ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND OPERATION TEST CARRIED OUT AS PER AMM 27-50-00-5, SATIS. 2L73 4F RTA22WE 20051129000122005112900012NM 2005 11 29 05FDEA03949 120051123A5753 HINGE BRACKET DOUG MD11 MD11 3023602NM TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 LT WING OUTBD FLAP INBOARD HINGE BRACKET OUTBD CENTER ATTACH HOLE FOUND CORRODED. LT WING OUTBOARD FLAP ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND OPERATION TEST CARRIED OUT AS PER AMM 27-50-00-5, SATIS. 2L73 4F RTA22WE 20051129000142005112900014NM 2005 11 29 05FDEA03951 120051123A5753NRC6753503 FLAP DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 SNRM N0963: LH OUTBD FLAP AFT INBD HINGE BRACKET ATTACH FITTING INBD CENTER BORE FOUND CORRODED. CORRECTIVE ACTION: SNRM N0963: LEFT HAND WING OUTBOARD FLAP ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND OPERATION TEST CARRIED OUT AS PER AMM 27-50-00-5, SATIS. 2L73 4F RTA22WE 20051129000152005112900015WP 2005 11 29 0501629928 120051102A27805919526508 DUCT DOUG DC9 DC931 3022065WP RT WING LE CONTAMINATED A NWAAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL018921E 45836 UPON SLAT EXTENSION FOR LANDING AT SYR, THE AIRCRAFT EXPERIENCED AN UNCOMMANDED ROLLED TO THE RIGHT. NO MENTION OF "SLAT DISAGREEMENT" LIGHT STATUS. COM PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT LANDED UNEVENTFULLY WITHOUT SLATS (FLAPS ONLY). MAINTENANCE FOUND THE T-DUCT HANGING UP AND SPRAYED IT WITH DRY FILM LUBRICANT. OPERATIONAL CHECKS WERE GOOD, THE AIRCRAFT RETURNED TO SERVICE, AND THE CULPRIT T-DUCT WAS REPLACED THE NEXT DAY. 2L72 4F A6WE 20051129000162005112900016CE 2005 11 29 DXTA200501093 120051119A28222C402 PUMP RAYTHNDH125 HAWKER800XP 7150012CE ALIDSGTFE731TFE7313AR WP FUEL BOOST FAILED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07845QS1361 258545 P107257 ON TAKEOFF ROLL THE FUEL 2 LOW PRESS LIGHT CAME ON. ABORTED TAKEOFF AT 60 KNOTS. R & R FAULTY FUEL BOOST PUMP WITH OVERHAULED UNIT IAW HAWKER 800XP MM CHAP 28-20-12. LEAK & OPS CHECK SATISFACTORY. REMOVED LT & RT FUEL FILTERS P/N 897830-1 AND INSTALLED NEW LT & RT FUEL FILTERS PN 897830-1. R & R O-RINGS WITH NEW PN M259881134. REINSTALLED CAP & TORQUED. WORK PERFORMED IAW HONEYWELL LIGHT MM TFE731-5BR CHAP 73-21-02. OPS CHECKED AND LEAK CHECKED USING BOOST PUMPS. 2L72 4F4 FRTA3EU E6WE 20051129000222005112900022NM 2005 11 29 SWAA053751 120051122A53306545765 SKIN BOEING737 7373H4 1384600NM BS 520 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29327SW 23691 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 16R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051129000232005112900023NM 2005 11 29 SWAA053752 120051127A53116545810 FRAME BOEING737 7373H4 1384600NM BS 312 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 312, STR 3L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051129000242005112900024NM 2005 11 29 SWAA053753 120051127A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM BS 300 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 300, STR 3L. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20051129000252005112900025NM 2005 11 29 SWAA053754 120051122A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA AND SRM. 2L72 4F RTA16WE 20051129000262005112900026NM 2005 11 29 SWAA053755 120051121A3213654611646 CYLINDER BOEING737 7373H4 1384600NM LT MLG DAMAGED A SWAAO OTHER O OTHER NRNOT REPORTED 1 SW29360SW 26571 NR 1 MLG WHEEL/TIRE ASSY MISSING. FOUND LT MLG OTBD WHEEL AXLE DAMAGED. REMOVED AND REPLACED NR 1 AND NR 2 MLG WHEEL/TIRE ASSY, LT MLG INNER CYLINDER, TUBE SUPPORT AND METERING PIN. REMOVED AND REPLACED NR 1 AND NR 2 ANTI SKID TRANSDUCERS, NR 1 AND NR 2 BRAKE ASSY'S AND LT INBD T/E AFT FLAP PER MM. 2L72 4F RTA16WE 20051129000272005112900027 2005 11 29 SWAA053756 420051124A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF LIMITS A SWAAK NONE O OTHER ININSP/MAINT 1 SW29367SW 26578 DURING SCHEDULED SERVICE CHECK, R2 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATED OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20051129000282005112900028NM 2005 11 29 SWAA053757 120051125A53306545765 SKIN BOEING737 7373H4 1384600NM BS 520 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29376SW 26584 DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 10R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051129000302005112900030NM 2005 11 29 SWAA053759 120051122A57536546435 SKIN BOEING737 7373H4 1384600NM RT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29392SW 27379 DURING SCHEDULED C3 CHECK, FOUND RT WING OTBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM. 2L72 4F RTA16WE 20051129000362005112900036 2005 11 29 F3LA200500045 420051122A2330 ODOR AIRBUSA319 A319111 3930336NM ENTERTAIN SYS DETECTED A F3LAB EMER. DESCENT BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 NM03942FR 2497 FLIGHT CREW RECEIVED LIVE TV SMOKE INDICATION. FLIGHT ATTENDANT REPORTED AN ELECTRIC ODOR IN AFT GALLEY. DECLARED AM EMERGENCY AND LANDED WITHOUT INCIDENT IN DEN. PERFORMED INSPECTION PER AMM 24-00-00-810-873. VERIFIED LIVE TV EXHAUST COOLING FAN FAILED. PLACARDED LIVE TV SYSTEM INOPERATIVE PER MEL 44-20-01AA, CONTROL NR 1019880. AN ADDENDUM WILL BE SUBMITTED UPON REMOVAL OF PLACARD. REPLACED AFT RACK COOLING FAN ASSY. PER LIVE TV AMM 44-25-00, PAGE 4772. 2L72 4F RTA28NM 20051129000372005112900037SO 2005 11 29 C2XA05SH134 120051115A531014525480003 BEAM EMB 145 EMB145LR 3260212SO CARGO BAY CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713550 145575 SHV-DURING C-CHECK MAINTENANCE FOUND CARGO DOOR CUTOUT LOWER CENTER BEAM WITH CORROSION. MAINTENANCE REMOVED AND REPLACED CARGO DOOR CUTOUT LOWER CENTER BEAM IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20051129000382005112900038NM 2005 11 29 05FDEA03943 120051123A5330 SKIN BOEING727 727227 1384078NM BS 423 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 FOUND BS 423, STR 22-23L, CREASED DENT IN SKIN. REPAIRED SKIN AT BS 423, STR 22-23L PER SRM 53-30-3. 2L73 4F A3WE 20051129000392005112900039NM 2005 11 29 05FDEA03944 120051123A5310 CREASE BEAM BOEING727 727227 1384078NM BS 848-870 MISDRILLED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25485FE 21488 CREASE BEAM IB CHORD HAS DOUBLE HOLES BS 848-870 RBL 63 WL 208. REPAIRED CREASE BEAM I/B CHORD AT BS 848-870 RBL 63, WL 208 PER SRM 51-30-2. 2L73 4F A3WE 20051129000402005112900040NM 2005 11 29 SWAA053763 120051127A53206546804 FLOOR SUPPORT BOEING737 7375H4 138449DNM BS 727B CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29512SW 24189 DURING SCHEDULED 1/2D CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, RBL 24.75. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20051129000412005112900041NM 2005 11 29 SWAA053764 120051127A53156546811 FLOORBEAM BOEING737 7375H4 138449DNM BS 1016 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29512SW 24189 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 1016, RBL 12 TO RBL 36. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20051129000422005112900042NM 2005 11 29 SWAA053765 120051122A53306545776 SKIN BOEING737 7375H4 138449DNM BS 934 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29514SW 25153 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 934, STR 25R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051129000432005112900043NM 2005 11 29 SWAA053766 120051127A5320BAC15171489 CHANNEL BOEING737 7373H4 1384600NM BS 270 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 DURING SCHEDULED D CHECK, FOUND COCKPIT FLOOR Z-CHORD CORRODED AT BS 270, BETWEEN LBL 11 TO RBL 11, WL 208. REMOVED AND REPLACED Z-CHORD PER SRM. 2L72 4F RTA16WE 20051129000442005112900044NM 2005 11 29 SWAA053767 120051127A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM BS 727B CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 727B, RBL 1 TO RBL 2. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051129000452005112900045 2005 11 29 SWAA053768 420051125A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29656SW 28401 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051129000462005112900046NM 2005 11 29 SWAA053769 120051127A335065C27093 LIGHT BOEING737 737317 138447PNM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29661SW 23173 L1 DOOR EMERGENCY EXIT LIGHT BASE CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20051129000472005112900047NM 2005 11 29 SWAA053770 120051123A53306545776 SKIN BOEING737 7373G7 1384595NM BS 923 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29683SW 24008 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 923, STR 23R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051129000482005112900048NM 2005 11 29 SWAA053771 120051122A53306545774 SKIN BOEING737 7373Q8 1384670NM BS 744 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29685SW 23401 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 744, STR 19R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051129000492005112900049NM 2005 11 29 SWAA053772 120051123A53306545765 SKIN BOEING737 7373Q8 1384670NM BS 504C CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 504C, STR 15R. REPAIRED SKIN PER SWA EA AND SRM. 2L72 4F RTA16WE 20051129000502005112900050NM 2005 11 29 SWAA053773 120051123A53306545774 SKIN BOEING737 7373Q8 1384670NM BS 739D-739E CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 739D TO BS 739E, STR 23L. REPAIRED SKIN PER SWA EA AND SRM. 2L72 4F RTA16WE 20051129000512005112900051NM 2005 11 29 05FDEA03945 120051123A5320 WEB BOEING727 727227 1384078NM BS 341 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 FOUND L-1 DOOR CUTOUT UPPER WEB IS GOUGED STA 341, WL 282, LBL 50. REPAIRED L1 DOOR CUTOUT UPPER WEB PER SRM 53-10-1. 2L73 4F A3WE 20051129000522005112900052NM 2005 11 29 AWXA200501432 120051108A5347D53112782202 SEAT TRACK AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28813AW 1223 SAL - DURING BC4 CHECK DISCOVERED EXFOLIATION CORROSION ON SEAT TRACK AT FS 20 AND -Y1292. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 319 SRM 53-31-15 FIG 101. MAINTENANCE REMOVED SEAT TRACK FROM FS 12 TO FS 24, -Y1292 IAW AIRBUS 319 SRM 51-42-11. RECEIVED NEW SEAT TRACK AND INSTALLED FROM FR12 TO FS 24, Y-1292 IAW AIRBUS 319 SRM 51-42-11 AND 51-72-11. 2L72 4F RTA28NM 20051129000532005112900053NM 2005 11 29 AWXA200501433 120051108A5315D53472189204 FLOORBEAM AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28813AW 1223 SAL - DURING BC4 CHECK DISCOVERED EXFOLIATION CORROSION ON FLOORBEAM ON FS 60 AND -Y1292, AFT GALLEY AREA. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 319 SRM 53-00-10. MAINTENANCE REMOVED BEAM FROM FS 68 TO FS 69, -Y1292 IAW AIRBUS 319 SRM 51-42-11. RECEIVED FLOORBEAM AND INSTALLED FROM FS 68 TO FS 69, Y-1292 IAW AIRBUS 319 SRM 51-42-11 AND 51-72-11. 2L72 4F RTA28NM 20051129000542005112900054NM 2005 11 29 AWXA200501434 120051108A5347D53112815202 SEAT TRACK AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28813AW 1223 SAL - DURING BC4 CHECK DISCOVERED EXFOLIATION CORROSION ON FLOORBEAM AT FS 16 AND Y1292. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 319 SRM 53-11-14. MAINTENANCE CUT OUT DAMAGED SECTION OF FLOORBEAM FROM FS 12 TO FS 16 IAW AIRBUS 319 SRM 53-11-14. FABRICATED REPAIR ANGLE AND RECEIVED NEW BEAM SECTION. INSTALLED REPAIR PARTS FROM FS 12 TO FS 16, Y1292 IAW AIRBUS 319 SRM 53-11-14. 2L72 4F RTA28NM 20051129000552005112900055NM 2005 11 29 AWXA200501435 120051108A5315D53472090010 FLOORBEAM AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28813AW 1223 SAL - DURING BC4 CHECK DISCOVERED EXFOLIATION CORROSION ON FLOORBEAM AT FR 66+3 AND Y1292. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 319 SRM 53-00-14. MAINTENANCE REMOVED FLOORBEAM FROM FS 64 TO FS 66 IAW AIRBUS 319 SRM 51-42-11. RECEIVED NEW BEAM SECTION AND INSTALLED FROM FS 64 TO FS 66, Y1292 IAW AIRBUS 319 SRM 51-42-11. 2L72 4F RTA28NM 20051129000562005112900056NM 2005 11 29 AWXA200501436 120051108A5315D5342188204 FLOORBEAM AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28813AW 1223 SAL - DURING BC4 CHECK DISCOVERED EXFOLIATION CORROSION ON FLOORBEAM AT FS 67+18 AND Y1292. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 319 SRM 53-00-14. MX REMOVED BEAM FROM FS 67+18 TO FS 69 IAW AIRBUS 319 SRM 51-42-11. RECEIVED NEW BEAM SECTION AND INSTALLED FROM FS 67+18 TO FS 69, Y1292 IAW AIRBUS 319 SRM 51-42-11. 2L72 4F RTA28NM 20051129000662005112900066EA 2005 11 29 QXEA200501556 120051117A4910 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA APU INLET DOOR FALSE ACTIVATIONA QXEAO OTHER O OTHER TXTAXI/GRND HDL 1 NM09609QX 10031 DEN - FLIGHT 4430 RETURNED TO THE GATE WITH A APU INLET DOOR CAUTION MESSAGE. MAINTENANCE PLACED ON MEL. AIRCRAFT RETURNED TO SERVICE. MEL CLEARED ON 11/19/2005 BY RIGGING THE APU DOOR IAW AMM 49-14-19-820-801-A01. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2L72 4F RTA21EA 20051129000682005112900068EA 2005 11 29 QXEA200501555 120051117A3240 BRAKE ASSY CNDAIRCL600 CL6002C10 1390015EA MLG MALFUNCTIONED A QXEAK NONE O OTHER LDLANDING 1 NM09600QX 10005 PDX - ON LANDING FOR FLIGHT 2481, LEFT BRAKE INEFFECTIVE ABOVE 50 KNOTS. MAINTENANCE BLED THE BRAKE SYSTEM. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2L72 4F RTA21EA 20051129000722005112900072NM 2005 11 29 UPS05245824 120051014A534365216618 SUPPORT BOEING727 72730C 1384009NM RT MLG TRUNNION CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 INSPECTION TYPE:C RT MLG TRUNNION BUTTERFLY FITTING HAS CORROSION. PLS REPLACE. SUPPORT REPLACED IAW DRW 65-19296. 2L73 4F A3WE 20051129000732005112900073NM 2005 11 29 UPS05245826 120051024A5320 INTERCOSTAL BOEING727 72730C 1384009NM BS660 STR 29R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 INSPECTION TYPE:C STA 660, ST 29R REPAIR TO INTERCOSTAL IS CRACKED. PLEASE REPAIR IAW SRM. REPAIR BRACKET FABRICATED IAW SRM 51-20-071 FIG 7. REPAIR BRACKET REPLACED IAW SRM 51-30-02. 2L73 4F A3WE 20051129000742005112900074NM 2005 11 29 UPS05245827 120051013A7120 MOUNT BOEING727 72730C 1384009NM NR 3 ENGINE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 INSPECTION TYPE:C ENGINE NR 3 FWD MOUNT FITTING HAS PITTING CORROSION ON BOTH OUTBOARD HOLES. REPAIR. REPAIRED IAW EO B727-5540-11592-A. 2L73 4F A3WE 20051129000752005112900075NM 2005 11 29 UPS05245828 120051011A5330 SKIN BOEING727 72730C 1384009NM FWD DOOR STR 7L CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 INSPECTION TYPE:C SUSPECT SKIN CRACKS AT UPPER FWD CORNER OF FWD ENTRY DOOR CUT OUT BETWEEN STR 7L AND 8L. PLEASE CARRY OUT NDI AND RECTIFY AS NECESSARY IAW SRM ADDENDUM. HFEC CARRIED OUT IAW NDTM 51-00-00 PT6 FIG 4. TWO CRACKS FOUND. DAMAGE REMOVED IAW EO B727-5330-1460-D. HFEC CARRIED OUT ON ALL EXISTING REMOVED FASTENERS, HOLES AND AROUND CUT OUT IAW NDTM 51-00-00PT6 FIG 4 AND 16. NO DEFECTS FOUND. NEW HOLES PITCH IN DOUBLER IAW EO B727-5330-1460D D. 2L73 4F A3WE 20051129000762005112900076NM 2005 11 29 UPS05245829 120051011A5330 SKIN BOEING727 72730C 1384009NM BS235 STR16L&17LCRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 INSPECTION TYPE:C NDT INDICATES 2 CRACKS EMINATING FROM FASTENERS " BS235.8 STR16L-17L. PLEASE REPAIR IAW SRM 53-30-3 FIG 3. FASTENERS REMOVED FROM AFFECTED AREA IAW SRM 51-80-02. AFFECTED AREA CUTOUT IAW SRM 53-30-3. HFEC CARRIED OUT AROUND CUTOUT AND ON REMOVED FASTENERS IAW NDTM 51-00-00PT6 FIG 4 AND FIG 16. NO DEFECTS FOUND. REPAIR DOUBLER AND FILLER FABRICATED IAW SRM 53-30-3 FIG 1. PRIMED REPAIR DOUBLER AND FILLER AND INSTALLED IAW SRM 53-30-3 FIG 1. 2L73 4F A3WE 20051129000772005112900077NE 2005 11 29 UPS05645819 220051122A7320 HMU BOEING767 76734AF 1385212NM GE CF6 CF680C2B7 NE LT ENGINE MALFUNCTIONED A IPXAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 SO01309UP 27740 ATB - CRUISING AT FL340 MACH .82 LEFT ENG ROLLED BACK TO APPROX 65 PERCENT N1 FF 3.0 SAT WAS -57 OVER THE NEXT 20 MINUTES EXPERIENCED SIX MORE ROLL BACKS WITH REDUCTIONS OF N1 FROM 5% TO 60% ALL OTHER INSTRUMENTS INDICATED ROLL BACKS. REMOVED AND REPLACED HMU RAN A/C AT HIGH PWR APPROX 30 MINS ALL SYSTEMS CKS NORMAL, NO ROLLBACKS NOTED. OK TO CONTINUE. 2L72 4F4 FRTA1NM E13NE 20051129000782005112900078WP 2005 11 29 UPS05845830 120051121A3350 BATTERY PACK DOUG DC8 DC871F 302199DWP EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01702UP 45902 ON PREFLIGHT, FOUND EMERGENCY EXIT LTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER MM 33-50-01-2. OPS CKS GOOD. 2L74 4F RT4A25 20051129000792005112900079NM 2005 11 29 SWAA053774 120051123A53306545775 SKIN BOEING737 7373Q8 1384670NM BS 789 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 789, STR 18L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051129000802005112900080NM 2005 11 29 SWAA053775 120051123A3350BR2013 LIGHT BOEING737 7373Q8 1384670NM CABIN WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED C3 CHECK, FOUND EEPLS STRIP WORN AT ROW 1 DEF. REMOVED AND REPLACED STRIP PER MM. 2L72 4F RTA16WE 20051129000812005112900081NM 2005 11 29 SWAA053743 120051127A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM BS 947 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D CHECK, FOUND FUSELAGE FLOORBEAM CRACKED AT BS 947.5, LBL 55, WL 208. REPAIRED FLOORBEAM PER BFG ER. 2L72 4F RTA16WE 20051129000822005112900082NM 2005 11 29 SWAA053744 120051127A5311BAC1518 FRAME BOEING737 7373H4 1384600NM BS 663 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 2L. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20051129000832005112900083NM 2005 11 29 SWAA053745 120051127A53126516300 BULKHEAD BOEING737 7373H4 1384600NM BS 178 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D CHECK, FOUND FUSELAGE BS 178 BLKHD LT SIDE WEB CRACKED. REPAIRED BS 178 BLKHD WEB PER SRM. 2L72 4F RTA16WE 20051129000842005112900084NM 2005 11 29 SWAA053746 120051127A5315BAC15171489 CHANNEL BOEING737 7373H4 1384600NM COCKPIT FLOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D CHECK, FOUND COCKPIT FLOOR Z-CHORD CORRODED AT BS 270, BETWEEN LBL 54 TO RBL 54, WL 208. REMOVED AND REPLACED Z-CHORD PER SRM. 2L72 4F RTA16WE 20051129000852005112900085NM 2005 11 29 SWAA053747 120051127A53156545805 FLOORBEAM BOEING737 7373H4 1384600NM BS 259 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 259, BETWEEN LBL 11 TO RBL 11, WL 208. REPAIRED FLOORBEAM PER BFG ER. 2L72 4F RTA16WE 20051129000862005112900086NM 2005 11 29 SWAA053748 120051127A53116516301 FRAME BOEING737 7373H4 1384600NM BS 188 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 188, STR 17R. REPAIRED STUB FRAME PER SRM. 2L72 4F RTA16WE 20051129000872005112900087NM 2005 11 29 SWAA053776 120051125A53306545775 SKIN BOEING737 7373Q8 1384670NM BS 883 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 883, STR 23R. REPAIRED SKIN PER SWA EA AND SRM. 2L72 4F RTA16WE 20051129000882005112900088NM 2005 11 29 SWAA053777 120051124A53306545767 SKIN BOEING737 7373Q8 1384670NM BS 435-465 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 435, BS 455 AND BS 465, STR 4R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051129000892005112900089NM 2005 11 29 SWAA053778 120051124A53306545765 SKIN BOEING737 7373Q8 1384670NM BS 472 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 472, STR 4R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051129000902005112900090NM 2005 11 29 SWAA053779 120051124A53306545774 SKIN BOEING737 7373Q8 1384670NM BS 735D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 735D, STR 19R. REPAIRED SKIN PER SWA EA AND SRM. 2L72 4F RTA16WE 20051129000912005112900091NM 2005 11 29 SWAA053780 120051124A53306545774 SKIN BOEING737 7373Q8 1384670NM BS 750 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 19R. REPAIRED SKIN PER SWA EA AND SRM. 2L72 4F RTA16WE 20051129000922005112900092EU 2005 11 29 AWXA200501441 120051125A3397E0052R8B3APNE CONNECTOR AIRBUS320 A320232 3930326EU EMERGENCY LIGHT UNKNOWN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28647AW 762 ATL - EEL - DURING TURN, FOUND EMERGENCY LIGHT INOPERATIVE AT SEAT 15 LEFT. MAINTENANCE FOUND SEAT 15ABC CONNECTOR FROM WALL TO SEAT NOT WORKING PROPERLY. MAINTENANCE REMOVED AND REPLACED CONNECTOR AT ROW 15ABC. OPERATIONAL TESTS WERE GOOD. 2L72 4F RTA28NM 20051129000932005112900093NM 2005 11 29 AWXA200501442 120051127A53306545766 SKIN BOEING737 7373G7 1384595NM BS 500D-520 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 PHX - DURING OVERNIGHT INSPECTION DISCOVERED FUSELAGE SKIN CRACK, 6.0 INCHES IN LENGTH, ON THE RT SIDE OF FUSELAGE AT BS500D+10 TO BS 520, BELOW STR 12R. MAINTENANCE TRIMMED OUT CRACK IAW BOEING 737-300 SRM 53-30-01 REPAIR 31. FABRICATED REPAIR DOUBLER, TRIPLER, STRUCTURAL FILLERS, TEAR STRAP DOUBLERS, AND SHIMS IAW BOEING 737-300 SRM 53-30-01 REPAIR 31. INSTALLED FABRICATED REPAIR PARTS FROM BS 500D+10 TO BS 520 AND BELOW STR 12R IAW BOEING 737-300 SRM 53-30-01 FIG 31. WORK WAS PERFORMED IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NO. 03-5331-05329-DF1. 2L72 4F RTA16WE 20051129000942005112900094EU 2005 11 29 AWXA200501443 120051125A3350321454 BATTERY AIRBUS320 A320232 3930326EU EMERGENCY LIGHT INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28658AW 1110 LAS - EEL - DURING OVERNIGHT INSPECTION, FOUND EMERGENCY ESCAPE PATH LIGHTING IN SEVERAL ROWS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE MID CABIN RT AND LT EMERGENCY PATH LIGHTING BATTERIES. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA28NM 20051129000952005112900095NM 2005 11 29 AWXA200501444 120051106A5754114N300266 SKIN BOEING757 757225 1384959NM NR 6 SLAT DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28907AW2569825698 22691 PHX - DURING A07 CHECK DISCOVERED THE NR 6 SLAT DELAMINATED AT THE INBOARD END AFT WEDGE. MAINTENANCE REMOVED AND REPLACED THE NR 6 SLAT IAW BOEING 757-200 AMM 27-81-01-4. OPERATION AND RIG CHECKS WERE GOOD. 2L72 4F RTA2NM 20051129000972005112900097NM 2005 11 29 AWXA200501446 120051111A5347D5337111000800 SEAT TRACK AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28660AW 1234 SAL - DURING BC4 CHECK DISCOVERED CORROSION ON THE LT INBOARD SEAT TRACK AT FS 46+12 AND Y765. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 103. REMOVED AND REPLACED LT INBOARD SEAT TRACK FROM FS 41 TO FS 47 AND Y765. 2L72 4F RTA28NM 20051129000992005112900099NM 2005 11 29 AWXA200501448 120051113A5320D534172172205 FLOOR SUPPORT AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28660AW 1234 SAL - DURING BC4 CHECK DISCOVERED CORROSION ON LONGITUDINAL BEAM LOCATED AT FS 68-10" AND Y-1162. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-14. REMOVED AND INSTALLED NEW BEAM IAW AIRBUS SRM 51-42-11 FROM FS 66 TO FS 68 AND Y-1162. 2L72 4F RTA28NM 20051129001002005112900100WP 2005 11 29 AALA20050768 120051120A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217549A 53031 SFO - ALL OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK ABOVE ROWS 6, 13, 20, AND 25 FOR ALL OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051129001012005112900101WP 2005 11 29 AALA20050765 120051119A3350 CONNECTOR DOUG DC9 DC983 3022083WP EMERGENCY LIGHT BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW21589AA 53252 SFO - EMERGENCY LIGHT EXIT SIGN AT FORWARD GALLEY DOOR INOPERATIVE. FOUND WIRE BROKEN AT SIGN CONNECTOR. REPINNED CONNECTOR FOR EMERGENCY LIGHT EXIT SIGN AT FORWARD GALLEY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20051129001022005112900102WP 2005 11 29 AALA20050766 120051120A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21226AA 49176 LAX - OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051129001042005112900104NM 2005 11 29 AALA20050767 120051120A3350 BATTERY PACK BOEING757 7572Q8 1384972NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21707TW 27625 DFW - FORWARD ESCAPE PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS FOR FORWARD ESCAPE PATH EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20051129001052005112900105WP 2005 11 29 AALA20050764 120051119A3350P4010049 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21585AA 53248 LGA - EMERGENCY LIGHTS AT FORWARD SEATS INOPERATIVE. REPLACED BATTERY PACK ABOVE FIRST CLASS LAVATORY FOR EMERGENCY LIGHTS AT FORWARD SEATS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051129001072005112900107NM 2005 11 29 PIDA20050191 120051122A5330 LAP JOINT BOEING737 7373G7 1384595NM BS 520 CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05380WL 23218 DURING A-CHECK, FOUND CRACK ABOVE STR 10 RT SKIN LAP JUST FORWARD OF BS 520.REPAIRED PER SRM 53-00-01. 2L72 4F RTA16WE 20051122000652005112200065NM 2005 11 22 CALA0500411 120051116A5220 HANDLE BOEING767 767424ER 1385270NM R-3 DOOR OUT OF ADJUST A CALAK NONE O OTHER ININSP/MAINT 1 SW2767052 29447 THE R-3 EMERGENCY DOOR INTERIOR HANDLE DOES NOT MOVE BACK AGAINST THE DOOR LINING DURING OPERATIONAL CHECK. THIS WOULD HAVE PREVENTED THE EMERGENCY ESCAPE SLIDE FROM DEPLOYING. PERFORMED TORSION SPRING ADJUSTMENT ON THE TORQUE TUBE PER MM 52-22-01, PAGE 511. EMERGENCY DOOR OPERATION CHECKED GOOD. 2L72 4F RTA1NM 20051122000722005112200072NM 2005 11 22 SWAA053652 120051116A53306545769 SKIN BOEING737 7377H4 1384404NM BS 512A CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29404WN 27892 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE LOWER SKIN CORRODED AT BS 512A, UNDER FWD AIRPHONE ANTENNA. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051122000762005112200076NM 2005 11 22 SWAA053656 120051117A53106520723 DOOR FRAME BOEING737 7375H4 138449DNM CARGO BAY CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29507SW 24184 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, AFT FRAME NR 5 STOP FITTING. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20051122000772005112200077NM 2005 11 22 SWAA053657 120051117A53156545810 FLOORBEAM BOEING737 7375H4 138449DNM BS 312 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29512SW 24189 DURING SCHEDULED 1/2D CHECK, FOUND CABIN FLOORBEAM CORRODED AT BS 312, RBL 35. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20051122000802005112200080NM 2005 11 22 SWAA053660 120051117A532065C28106 STIFFENER BOEING737 7375H4 138449DNM BS 1016 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29512SW 24189 DURING SCHEDULED 1/2D CHECK, FOUND BS 1016 AFT PRESSURE BLKHD STIFFENER CHANNEL CORRODED AT 6 O'CLOCK POSITION. REPAIRED STIFFENER CHANNEL PER SWA ACO AND BAC DRAWING. 2L72 4F RTA16WE 20051122000852005112200085SO 2005 11 22 RAIA00511022 120051116A3397 WIRE EMB 145 EMB145 3260210SO EMERGENCY LIGHT BROKEN A RAIAK NONE O OTHER ININSP/MAINT 1 CE03809HK 145187 PRE-FLIGHT INSPECTION -STL - EMERGENCY LIGHT STRIP OUT IN ONE SECTION. MAINTENANCE REPAIRED BROKEN WIRE ON EMERGENCY LIGHT STRIP. 2L72 4F RTT00011AT 20051122001052005112200105NM 2005 11 22 AWXA200501417 120051112A5315141N5112 FLOORBEAM BOEING757 7572S7 1384962NM BS 365 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28904AW 23566 GYR - DURING C10 CHECK DISCOVERED CORROSION LOCATED ON FLOORBEAM TEE CAP AT BS 365, FROM BL 35.5R TO BL 45.0R. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW BOEING 757-200 SRM 53-00-51-1A. MAINTENANCE REMOVED UPPER T CAP IAW BOEING 757-200 SRM 51-40-02. FABRICATED NEW T CAP IAW BOEING G737-300 SRM 53-00-51 FIG 201. INSTALLED FABRICATED REPAIR PARTS IAW BOEING G757-200 SRM 51-00-51. 2L72 4F RTA2NM 20051122001082005112200108NM 2005 11 22 AWXA200501420 120051027A5330655298878 SKIN BOEING737 7373S3 1384711NM BS 960 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 MCN - DURING C13 CHECK DISCOVERED, THE L2 DOOR CUTOUT, AT BS 960 AND STR 17L, LOWER FORWARD CORNER CRACKED, 1.1 INCHES IN LENGTH. MAINTENANCE CUT OUT CRACKED ARE ON THE L2 DOOR. FABRICATED FILLER AND DOUBLER IAW BOEING 737-300 SRM 53-60-01-2R5. INSTALLED FABRICATED REPAIR PARTS AT BS 960 AND STR 17L ON THE L2 DOOR CUTOUT IAW BOEING 737-300 SRM 53-60-01-2R5. 2L72 4F RTA16WE 20051122001222005112200122NM 2005 11 22 05FDEA03911 120051119A5310 FLOOR SUPPORT DOUG MD11 MD11 3023602NM BS 1821-1901 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 CABIN, LONGITUDINAL FLOOR SUPPORT FROM STA 1821 TO 1901 APRROX X=30 UPPER SURFACE FOUND WITH CORROSION. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051122001292005112200129WP 2005 11 22 UPS05845787 120051022A53403755827U501 FITTING DOUG DC8 DC873F 302199FWP FS 270 L33R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE:C1 "A" PTI ZEE FITTING CRACKED AT STA. 270 L33R. REMOVED AND REPLACED ZEE FITTING IAW SRM 51-1-20D. 2L74 4F RT4A25 20051122001322005112200132NM 2005 11 22 05091 120051108A291060B0025435 LINE BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE HYDRAULIC SYS RUPTURED A KCSAO OTHER K FLUID LOSS APAPPROACH 1 GL23 19753 LOST NR 1 HYD ON FINAL, ADP TURN OFF, EDP DEPRESSURIZED. INSPECTED NR 1 HYD SYSTEM. FOUND NR 1 ADP SUPPLY LINE RUPTURED. REMOVED AND REPLACED NR 1 ADP SUPPLY LINE IAW 20-11-18. OPS CHECK NR 1 HYD SYS. LEAK CHECK GOOD. 2L74 4F4 F A20WE E20EA 20051122001342005112200134NM 2005 11 22 AWXA200501422 120051115A32601061226213 CIRCUIT BOARD BOEING737 7373B7 1384580NM MLG FAULTY A AWXAO OTHER J WARNING INDICATION CRCRUISE 1 WP28332AW 23384 PHX - EMERGENCY LANDING - CREW REPORTED RT GREEN GEAR LIGHT REMAINED ON DURING ENTIRE FLIGHT, WITH GEAR UP. GEAR EXTENDED NORMALLY IN PHX. CREW DID MAKE A PRECAUTIONARY FLY BY THE TOWER PRIOR TO LANDING. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT AND TAXIED TO THE GATE. MAINTENANCE REMOVED AND REPLACED THE RT MAIN GEAR DOWN AND LOCKED SWITCH CARD, M981, IAW BOEING 737-300 MM 32-09-20-724-015. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20051122001742005112200174 2005 11 22 SWAA053667 420051118A256565C16820 HOOK BOEING737 7377H4 1384404NM R1 DOOR SLIDE LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29203WN 32483 R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED HOOK PER MM. 2L72 4F RTA16WE 20051122001762005112200176WP 2005 11 22 05FDEA03887 120051118A5751 REPAIR DOUG DC10 DC1030 3023501WP RT AILERON PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 RT WING OUTBOARD AILERON FOUND FLUSH DOUBLER REPAIR ON LOWER SKIN FROM STA XOA 1003 TO STA 1041 DIMENSION 38" BY 26". PERFORMED A GVI OF REPAIR IAW SRM 57-10-00 FIG 2 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001-P2 E3. 2L73 4F A22WE 20051122001782005112200178WP 2005 11 22 05FDEA03889 120051118A5730 REPAIR DOUG DC10 DC1030 3023501WP LT WING PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 LT WING OUTBOARD FLAP LOWER SKIN FOUND A FLUSH DOUBLER 40" BY 34" WITH A EXTERNAL SPLICE BTWN STA XOF 605 AND XOF 639. PERFORMED INSPECTION ON REPAIR DOUBLER IAW SRM 57-10-00 FIG 7 VOL 1 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2 E3. 2L73 4F A22WE 20051122001802005112200180NM 2005 11 22 05FDEA03891 120051118A5310 DOUBLER BOEING727 727233 138408ANM BS 1165 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25220FE 20934 AFT CARGO DOUBLER CORRODED, BETWEEN STR 21L AND 22L STA 1165. COMPLIED WITH FED EX EA 7-5330 91316-FUSELAGE- CORROSION AT AFT LAV SERVICE DOOR CUTOUT-REPAIR . TIMCO MECH #2891 QC227 MAJOR REPAIR 2L73 4F RTA3WE 20051122001822005112200182WP 2005 11 22 05FDEA03893 120051118A5753 REPAIR DOUG DC10 DC1030 3023501WP LT WING FLAP PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 LT WING INBOARD FLAP FOUND A DOUBLER 6" BY 5" ON UPPER SKIN AT STA XIFH 288. PERFORMED A GVI OF REPAIR IAW SRM 57-00-01 FIG 64 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001-2P E3 RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VOL 2 PAR 3. 2L73 4F A22WE 20051122001842005112200184NM 2005 11 22 05FDEA03895 120051118A5315 FLOORBEAM BOEING727 727233 138408ANM BS 620 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25220FE 20934 MAIN CABIN FLOORBEAM TEE CAP CORRODED STA 620 RBL 10 AND RBL15. REMOVED DAMAGED AREA AND INSTALLED FILLER AND 2 (EA.) REPAIR ANGLES IAW B727 SRM 53-10-8 FIG 8. ALODINED AND PRIMED SAME IAW B727 SRM 51-10-2. 2L73 4F RTA3WE 20051122001962005112200196NM 2005 11 22 ASAA0540491 120050919A53136935352 CLIP BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU BS 460 GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02793AS 28888 FWD CARGO BAY STRINGER CLIP GROUGED. REMOVED AND REPLACED STRINGER CLIP IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051128000032005112800003EA 2005 11 28 COMA0560622 120051119A27501217545 DRIVE SHAFT CNDAIRCL600 CL6002B19 1900309EA TE FLAP SYSTEM WORN A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01735CA8360 7267 FLIGHT 5404 - EN ROUTE PHL-CVG DURING APPROACH RECEIVED A FLAP FAIL CAUTION AT ZERO DEGREE FLAP POSITION. CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE RIGHT WING FLEX DRIVE SHAFT. 2L72 4F RTA21EA 20051128000092005112800009NM 2005 11 28 USAA051409 120051122A5711 SPAR BOEING737 7373B7 1384580NM LT WING CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU 23860 LBL 135.5, 12 INCHES FWD FROM REAR SPAR CRACKED. MAJOR REPAIR, REMOVED DAMAGE, INSTALLED REPAIR TEE, FILLERS, AND VERT STIFFENER IAW EA 97047. DEFECT SIZE: 1.5 INCH. 2L72 4F RTA16WE 20051128000122005112800012EU 2005 11 28 USAA051420 120051122A5310D5311278220201 BEAM AIRBUSA321 A321211 3930370EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19161UW 1403 BEAM - Y1292 AT FRAME 16; CORROSION LEVEL 1; TASK JA-220-53500. REMOVED AND REPLACED IAW SRM 51-72-11. DEFECT SIZE: 2 INCHES X 1 INCH. 2L72 4F4 FRTA28NM E2GL 20051128000152005112800015EU 2005 11 28 USAA051417 120051122A5320 SILL AIRBUSA321 A321211 3930370EU GE CFM56 CFM56* 13802NE RT AFT DOOR CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19161UW 1403 RIGHT AFT DOOR SILL FR 66; CORROSION LEVEL 2; TASK JA-260-53500. SPLICE ANGLE REPAIR IAW SRM 53-41-14. DEFECT SIZE: 10 INCHES X .846 INCH. 2L72 4F4 FRTA28NM E2GL 20051128000312005112800031NM 2005 11 28 SWAA053728 120051122A53116545805 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 277, STR 11R. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051128000372005112800037NM 2005 11 28 SWAA053734 120051122A5313BAC1498 STRINGER BOEING737 7375H4 138449DNM BS 520 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29512SW 24189 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 520, STR 10R. REPAIRED STRINGER PER SWA EA. 2L72 4F RTA16WE 20051128000462005112800046NM 2005 11 28 SWAA053722 120051121A53306545767 SKIN BOEING737 7373H4 1384600NM BS 440 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 440, STR 26L. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20051128000482005112800048NM 2005 11 28 SWAA053742 120051121A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29785SW 30602 DURING SCHEDULED HC1 CHECK, FOUND EEPLS TRACK COVER MISSING AT ROW 14 ABC. INSTALLED COVER PER MM. 2L72 4F RTA16WE 20051128000522005112800052WP 2005 11 28 DJFA2005162 220051116A7397 CONNECTOR RAYTHNDH125 HAWKER800XP 7150012CE GARRTTTFE731TFE7315BR WP FUEL FLOW IND LOOSE E DJFAO OTHER N FALSE WARNING DEDESCENT 1 EA23829LX 258466 P107451 CREW REPORTED THAT DURING DESCENT THE LEFT ENGINE BEGAN SURGING UP AND DOWN. THE FUEL FLOW RANGED FROM 400 TO 1,300 LBS / HR. PRIORITY HANDLING WAS REQUESTED AND FIRE RESCUE RESPONSE WAS GIVEN FOLLOWING A NORMAL LANDING IN KMSP. THE ENGINE CONTINUED TO SURGE THROUGH THE LANDING PHASE, AND STOPPED WHEN THE AIRCRAFT BEGAN TAXIING. MX EXAMINED ALL ELECTRICAL CONNECTIONS AND DISCOVERED A LOOSE CONNECTOR ON THE NR 1 ENGINE TORQUE MOTOR. THE CONNECTOR WAS TIGHTENED AND RESAFETIED. P2T2 SENSORS WERE SWAPPED BETWEEN THE LEFT AND RIGHT ENGINES. NO DISCREPANCIES WERE NOTED WHILE PERFORMING GROUND ENGINE RUNS, AND NO ABNORMALITIES WERE NOTED DURING THE TEST FLIGHT. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA3EU E6WE 20051128000572005112800057CE 2005 11 28 DXTA200501080 120051101A2797MS24171D1 RELAY CESSNA750 750 2076810CE TE FLAPS FAILED E DXTAO OTHER J WARNING INDICATION APAPPROACH 1 GL07921QS428 7500241 TRAILING EDGE FLAPS DID NOT DEPLOY FOR LANDING -FLAPS FAIL- WOULD NOT RESET. NO FLAP EMERGENCY LANDING, CHECKLIST USED WITH NO FUTHER EVENTS. REPLACED KZ092 FLAPS POWER RELAY WITH NEW RELAY AND TIGTHENED ALL OTHER TERMINALS IN J-BOX. REINSTALLED FLAP J-BOX AND CYCLED FLAPS MULTIPLE TIMES. OPS CHECK GOOD IAW CITATION 750 M/M CH 27-50-01. 2L72 4J RTT00007WI 20051128000592005112800059NM 2005 11 28 QXEA200501538 120051109A5730 SKIN BOMBDRDHC8 DHC8402 1390042NM WING DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX: 2 AREAS ON FWD APERTURE AND 2 AREAS ON AFT APERTURE FOR WING PANEL 522CT ARE BLENDED OUT OF LIMITS PER RD 8/4-57-441. MAINTENANCE REPAIRED IAW NDTM PART 6, 51-00-02, QX EA 6-57-394 AND RD 8/4-57-577. 2H72 4T RTA13NM 20051128000602005112800060WP 2005 11 28 UPS05845792 120051020A551056545006 SKIN DOUG DC8 DC873F 302199FWP HORIZONTAL STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE:C1 INTERGRANULAR CORROSION ON RT HORIZ STAB L/E UPPER SURFACE AT SEGMENT JOINT. CUT OUT DAMAGED AREA AND FABRICATED AND INSTALLED REPAIR IAW SAA SK 81 3-822948 AND UPS EO DC8-55-20022. 2L74 4F RT4A25 20051128000702005112800070CE 2005 11 28 DXTA200501082 120051113A2910 LINE CESSNA500 560CESSNA 2076750CE HYDRAULIC SYS LEAKING E DXTAD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 GL07332QS 5600523 RIGHT SIDE, RIGHT BRAKE PEDAL FEELS LIKE IT LOSES PRESSURE BUT REGAINS IT WITH MINOR PUMPING. APPLIED BRAKE PRESSURE TO RIGHT BRAKE AND DUPLICATED SQUAWK. INSPECTED BRAKE MASTER CYLINDER AND RIGHT BRAKE FOR DEFECTS, NON NOTED. BLED ANTI-SKID BRAKE SYSTEM. APPLIED BRAKE PRESSURE TO RIGHT/LEFT BRAKES. NO FURTHER DEFECTS NOTED. WORK DONE IAW CITATION MODEL ULTRA MM 32-42-00. 2L72 4F RTA22CE 20051128000742005112800074CE 2005 11 28 DXTA200501089 120051116A2700 WARNING LIGHT CESSNA750 750 2076810CE YAW DAMPER ILLUMINATED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07960QS 7500160 TAKEOFF ABORTED BECAUSE OF 2 AMBER CAS MESSAGES. ONE WENT OUT BEFORE IT WAS IDENTIFIED. THE -LOWER YD OFF STAYED ON- YAW DAMP SYSTEM OPERATIONALLY CHECKS NORMAL IN ACCORDANCE WITH HONEYWELL PRIMUS 2000 MAINTENANCE MANUAL FOR CITATION X. 2L72 4J RTT00007WI 20051128000782005112800078NM 2005 11 28 RA1 120051028A3350900835A BATTERY BOEING727 727191 1384063NM EMERGENCY LIGHT FAILED I R5KBK NONE L NO TEST ININSP/MAINT 1 SO33502MG 497 19391 RIGHT EMERGENCY EXIT SIGN LIGHT INOP. 2L73 4F A3WE 20051128000792005112800079NM 2005 11 28 R5KBRA2 120051028A3350900835A BATTERY BOEING727 727191 1384063NM EMERGENCY LIGHT FAILED I R5KBK NONE L NO TEST ININSP/MAINT 1 SO33502MG 124 19391 LEFT EMERGENCY EXIT SIGN LIGHT INOP. 2L73 4F A3WE 20051128000802005112800080NM 2005 11 28 UPS05445805 120051118A541065B903604 THRUST LINK BOEING747 747200 1384847NM NR 1 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE:AD CRACK INDICATION REVEALED ON NR 1 PYLON THRUST LINK FWD LUG LOWER SURFACE BY APPROX 80 PERCENT FSH. NR 1 PYLON THRUST LINK REPLACED AND FWD AND AFT MOUNT BOLTS REPLACED AS PER AMM 71-21-03. 2L74 4F RTA20WE 20051128000822005112800082NM 2005 11 28 UPS05445807 120051118A541065B903604 THRUST LINK BOEING747 747200 1384847NM NR 3 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE:AD CRACK INDICATION REVEALED ON NR 3 PYLON THRUST LINK FWD LUG LOWER SURFACE BY APPROX 60 PERCENT FSH. NR 3 ENG THRUST LINK REPLACED AND AFT MOUNT BOLT REPLACED AS PER AMM 71-21-03. 2L74 4F RTA20WE 20051128000852005112800085NM 2005 11 28 UPS05445810 120051119A541065B903604 THRUST LINK BOEING747 747200 1384847NM NR 2 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE:AD NR 2 ENG REF TAR FORM S/N: 115643 - UPS REQUEST REPLACEMENT OF THRUST LINK. NR 2 ENG THRUST LINK REPLACED AND BOTH ATTACH BOLTS REPLACED AS PER AMM 71-21-03. 2L74 4F RTA20WE 20051128001072005112800107NM 2005 11 28 UPS05M45815 120051103A5730 SKIN DOUG MD11 MD11F 3023600NM LT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01270UP 48576 INSPECTION TYPE:C2 LEFT WING TIP LWR SURFACE SKIN CRACKED .5 INCH LONG AND HAS HEAVY CORROSION AT XW 998. THE CORRODED AREA WAS TRIMMED OUT AND A FILLER AND DOUBLER WERE INSTALLED IAW SAA SK 270-894256 UPS ENG FILE MD11-57-20035, BOEING MSG 1-139605558-2 BOEING MSG 1-139605558-4, AND FAA FORM 8100-9. 2L73 4F RTA22WE 20051128001122005112800112EA 2005 11 28 COMA0560615 120051117A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01735CA 7267 FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2L72 4F RTA21EA 20051128001352005112800135NM 2005 11 28 SWAA053719 120051121A3350 COVER BOEING737 7373H4 1384600NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29641SW 27714 L1 DOOR LOWER EMERGENCY EXIT LIGHT COVER CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20051128001412005112800141NM 2005 11 28 SWAA053704 120051121A33506104781 BATTERY PACK BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29341SW 24091 DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20051128001422005112800142NM 2005 11 28 SWAA053705 120051121A33506104781 BATTERY PACK BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29341SW 24091 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT BATTERY CHARGER INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20051128001442005112800144NM 2005 11 28 SWAA053707 120051121A53116520723 FRAME BOEING737 7375H4 138449DNM FWD CARGO CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29512SW 24189 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, AFT FRAME LOWER STOP FITTING. REPAIRED FRAME PER SWA EA. 2L72 4F RTA16WE 20051128001472005112800147SO 2005 11 28 C2XA05SH129 120051107A491014526850401 FIREWALL EMB 145 EMB145EP 3260221SO APU BAY CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714945 145049 SHV-DURING C-CHECK MAINTENANCE FOUND AFT LOWER SIDE OF APU FIREWALL RIVET HEAD WITH DAMAGE. MAINTENANCE REPAIRED APU LOWER FIREWALL SKIN DAMAGE I/A/W EC 5330-01521. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20051128001482005112800148SO 2005 11 28 C2XA05CL091 120051106A733077879187 SWITCH EMB 145 EMB145LR 3260212SO NR 2 ENGINE FAULTY A C2XAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW2717560 145605 CLE FLIGHT NR 2844, THE CREW REPORTED A NR 2 ENGINE FUEL IMPENDING BYPASS MESSAGE ON THE EICAS DURING TAKEOFF ROLL. TAKEOFF WAS ABORTED. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE IMPENDING BYPASS SWITCH. THE NR 2 ENGINE FUEL FILTER WAS ALSO REPLACED. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20051128001582005112800158NM 2005 11 28 ASAA0540431 120050823A554265C2584151 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU RUDDER DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 RUDDER SKIN DAMAGED AT 3 LOCATIONS. LWR LT SIDE AT BOTTOM CORNER EDGE 1 INCH, 2 INCH, AND 7 INCH AFT OF L/E. REPAIRED DAMAGE IAW EA. (K) 2L72 4F4 FRTA16WE E21EU 20051128001642005112800164NE 2005 11 28 SDR2005072 220051030A7297 CONNECTOR AEROSPATR72 ATR72 EU PWA PW120 PW127 NE RT ENGINE DIRTY A SIMAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO29550LL 550 DURING CLIMBOUT, THE RT ENGINE HAD A TORQUE FLUCTUATION OF 10-20 PERCENT. CREW PERFORMED A PRECAUTIONARY SHUTDOWN AND RETURNED. CLEANED TORQUE SENSOR CONNECTOR PLUG. OPERATIONAL CHECK FOUND NO MORE FLUCTIONS. (K) 2H72 4T4 TRT E20NE 20051128001772005112800177SO 2005 11 28 CHQA20050191 120051105A335066367 LIGHT EMB 145 EMB145MP 3260216SO ALLSN AE300 AE3007A GL CABIN BROKEN A CHQAK NONE O OTHER ININSP/MAINT 1 GL11976RP 145322 FORWARD FLOOR PROXIMITY LIGHT IS BROKEN. REMOVED AND REPLACED PROXIMITY STRIP IAW MM 33-50-12. 2L72 4F4 FRTT00011ATTE6CH 20051128001852005112800185NM 2005 11 28 05FDEA03931 120051121A5311 FRAME BOEING727 727227 1384078NM BS 500 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 FRAME DENT AT BS 500, ABOVE STR 23L. TRIMED DAMAGE, FABRICATED AND INSTALLED DOUBLER PER SRM 51-40-3. 2L73 4F A3WE 20051128001992005112800199WP 2005 11 28 IXXA05RNG107S 120050916A5720 FAIRING DOUG DC8 DC872 302199BWP WS 149.000 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK, FOUND A CRACK ON LT ELEVATOR LOWER SURFACE, STA XE 149.000. FAIRING WAS FABRICATED AND REPLACED IAW DOUGLAS DRAWING 5655694 VIEW C-C, AND RIVETS WERE INSTALLED IAW DC8 SRM 51-1-21 PAGE 1-7. 2L74 4F RT4A25 20051129000032005112900003NM 2005 11 29 SB05152 120051123A2133106120923 OUTFLOW VALVE BOEING737 7373B7 1384580NM AFT FUSELAGE FAULTY A USAAGBA O2 MASK DEPLOYED EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19512AU64450250 23595 CABIN PRESSURE CLIMBING, AUTO FAIL LIGHT ILLUM, EMERG DESCENT. PRESSURIZATION UNCONTROLLABLE, MASKS DEPLOYED EXCEPT ROW 20. FOUND LT SAFETY RELIEF VALVE FAILED. REPLACED LT & RT VALVE, FWD & AFT OUTFLOW VALVES, DELTA P MODULE, SELECTOR PANEL, PRESSURE CONTROLLER & LT RAM AIR DOOR ACTUATOR. OPS GOOD. REPAIRED LEAKS BOTH CARGO DOORS & AVIONICS COOLING OUTLET VALVE. REPLACED LWR FLAP HINGE MAIN ENTRY DOOR & 12 FUSELAGE BELLY DRAINS. INSPECTED BS 178 FWD PRESSURE B/H UNDER PRESSURE, NO LEAKS. REPLACED CONNECTOR D640 PRESSURE MODULE, REPAIRED PINS 10, 11, 24, 27 & CHAFED WIRES. REPLACED OXYGEN GENERATORS, REPACKED MASKS. FOUND MASK LANYARD CAUGHT AROUND DOOR LATCH ROW 20. REPOSITIONED, OPS GOOD. 2L72 4F RTA16WE 20051129000072005112900007NM 2005 11 29 PCSA11200501 120051120A2750 FLAP SYSTEM BOEING727 727233 138408ANM TE FLAPS DISCONNECTED A PCSAA UNSCHED LANDING O OTHER CLCLIMB 1 SO29495AJ 20937 ON CLIMBOUT, CREW REPORTED OB TRAILING EDGE FLAPS WOULD NOT RETRACT AFTER TAKEOFF. AIRCRAFT RETURNED TO DEPARTURE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT OB FLAP POSITIONING SYSTEM, THE OB FLAP POSITION INDICATOR CONNECTOR WAS SUSPECTED NOT MAKING PROPER CONTACT, PIN CONNECTOR WAS DISCONNECTED AND CLEANED AND RECONNECTED, SYSTEM WAS OPERATIONALLY CHECKED TO BE OPERATING NORMAL IAW MM CH 27-52-21. AIRCRAFT WAS RETURNED TO SERVICE. 2L73 4F RTA3WE 20051129000092005112900009NM 2005 11 29 05FDEA03942 120051122A7932 ENGINE BOEING727 727200 138407ENM NR 3 MALFUNCTIONED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25482FE 21464 AFTER 20 MINUTES AT CRUISE, NR 3 OIL PRESSURE READ 34 PSI. WENT TO QRH, RETARDED THROTTLE AND OIL TEMP ROSE TO 120 C. ALL OTHER INDICATIORS WERE GOOD. SHUT ENGINE DOWN IAW QRH, DIVERTED TO CVG. 2L73 4F RTA3WE 20051129000112005112900011NM 2005 11 29 05FDEA03948 120051123A5753NRC6753504 SKIN DOUG MD11 MD11 3023602NM TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 SNRM N1008: CRACK FOUND AT RH WING OUTBD FLAP LOWER FASTENER HOLE COMMON TO ARC 4009 SUPPORT FITTING LOCATED AT THE #2 HOLE FROM INBD DURING HFEC INSPECTION. CORRECTIVE ACTION: SNRM N1008: RIGH HAND OUTBOARD FLAP ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND OPERATION TEST CARRIED OUT AS PER AMM 27-50-00-5, SATIS. 2L73 4F RTA22WE 20051129001102005112900110EA 2005 11 29 COMA0560632 120051122A3251 ECU CNDAIRCL600 CL6002B19 1900309EA NLG STEERING MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01819CA 7415 FLIGHT 5256 - DURING CRUISE FLIGHT, RECEIVED A STEERING INOPERATIVE MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED AT JFK WITHOUT INCIDENT. PERFORMED A STEERING SYSTEM RESET AND OPERATIONAL CHECK WAS SATISFACTORY. 2L72 4F RTA21EA 20051129001122005112900112NM 2005 11 29 2005UALA01249 120051108A335078941 LAMP BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29786UA 26938 SEAT 1E AFT EMERGENCY LIGHT ASSEMBLY BROKEN. SUPPLEMENTAL DATA UPDATE RELAMPED AFT EMERGENCY LIGHT AT 1E. 2L72 4F4 FRTT0001SE E46NE 20051129001142005112900114 2005 11 29 2005UALA01263 420051113A3417 WARNING LIGHT BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE ADC ILLUMINATED A UALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 WP29799UA 26926 FLIGHT DIVERTED UNDER AMBER ALERT DUE TO MULTIPLE AIR DATA SYSTEM PROBLEMS, OVERWEIGHT LANDING. FOUND DAMAGED QUICK DISCONNECT FOR RIGHT AIR DATA MODULE (ADM) CAUSING INVALID SIGNAL. THE QUICK DISCONNECT WAS REPLACED. THERE WERE 3 ADMS BEING REPLACED AND 2 ADMS WERE FOUND WITH DEFECTIVE A2 TRANSDUCER CARD. THE FINAL FIX WAS REPLACEMENT OF THE LEFT PITOT PROBE. ALL DATA REGARDING THIS OCCURRENCE HAS BEEN SENT TO BOEING FOR FURTHER ANALYSIS. THE FINAL ANALYSIS FROM BOEING WILL BE AVAILABLE ON OR AFTER 2/28/2006, REFERENCE SERVICE REQUEST ID 1-142280425. ALL FINDINGS ARE FROM AMIS AND CIDER. ADMS REMOVED - MR34213-55, -54, -53: PITOT PROBE REMOVED - NO DATA 2L72 4F4 FRTT0001SE E46NE 20051129001162005112900116CE 2005 11 29 DXTA200501110 120051123A2821305262401 FUEL FILTER CESSNA500 560CESSNA 2076750CE LEFT BYPASSING E DXTAC ABORTED TAKEOFF J WARNING INDICATION TXTAXI/GRND HDL 1 GL07844QS 5600629 PRIOR TO 70 KTS DURING TAKEOFF ROLL THE LEFT FUEL FILTER BYPASS ANNUNCIATOR ILLUMINATED & THE TAKEOFF WAS ABORTED. INSPECTED BOTH LEFT AND RIGHT WING TANKS. REMOVED AND REPLACED BOTH ENGINE FUEL FILTERS. PERFORMED LEAK CHECK OF ACCESS PANELS AND ENGINES CHECK GOOD. REF CE560 AFM AND PRATT & WHITNEY MM 73-20-01. 2L72 4F RTA22CE 20051129001172005112900117NM 2005 11 29 2005UALA01265 120051112A5241 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FWD GALLEY DOOR MISDRILLED A UALAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP29328UA 24148 FWD GALLEY DOOR AFT FRAME UPPER HOLE AT STOP FITTING HAS NO ED. SUPPLEMENTAL DATA UPDATE FABRICATED DOUBLER AND FILLER AND INSTALLED REF AAR EO 50267 AND SRM 51-40-02. 2L72 4F4 FRTA16WE E2GL 20051129001182005112900118EU 2005 11 29 2005UALA01266 120051111A3350321430 BATTERY AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE EMERGENCY LIGHTSFAULTY A UALAK NONE L NO TEST ININSP/MAINT 1 WP29489UA 1702 EMERGENCY LIGHT TEST FAULTS "EPSU BATTERY EMER R". SUPPLEMENTAL DATA UPDATE REPLACED EPSU 12WL BATTERY. 2L72 4F4 FRTA28NM E40NE 20051129001192005112900119NM 2005 11 29 2005UALA01272 120051114A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE DOOR 2R CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29315UA 23947 DOOR 2R DOOR CUTOUT HAS POSSIBLE CRACK APPROX 3.5 INCH LOWER FWD CORNER. SUPPLEMENTAL DATA UPDATE ACCOMPLISHED HFEC AND CONFIRMED CRACK THREE AND ONE HALF INCH LONG. MAJOR REPAIR PER SRM 53-00-01 DETAIL IV, DOUBLER-TRIPLER REPAIR SCHEME USED AT FWD LWR CORNER OF DOOR CUTOUT. 2L72 4F4 FRTA16WE E2GL 20051129001202005112900120NM 2005 11 29 WRLA2005147 120051123A2497 WIRE DOUG MD11 MD11F 3023600NM PWA 4460 PW4460 NE ELECTRICAL DAMAGED A WRLAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO11380 48407 TPE/ANC AFTER 5HRS FLIGHT CAC FAN 2 C/B POPPED. AFTER LANDING AND ENGINE SHUTDOWN IN ANC CAC FAN 1 C/B POPPED. AFTER 7HRS 20MIN LEVEL 1 ALERT "AC TIE 1 OFF" APPEARED. CORRETIVE ACTION: UPON INITIAL INSPECTION FOUND AC BUS TIE RELAY OVERHEATED THE BUNDLE AND CAUSED A DIRECT SHORT CIRCUIT THAT TRIPPED THE C.A.C FAN BREAKERS AND BURNED THE WIRE BUNDLE. REMOVED & REPLACED DAMAGED WIRING IAW MM 20-10-01 & MM 24-97-00. REMOVED & REPLACED EPCU, ESC AND NR 1 & 2 CAC FANS OPS CHECK OK. NO AC TIE 1 OFF ALERT DISPLAYED AFTER POWER UP. RTS ALL TESTS PASSED. 2L73 4F4 FRTA22WE E24NE 20051130000012005113000001WP 2005 11 30 05FDEA03963 120051126A5320 PULLEY BRACKET DOUG DC10 DC1030 3023501WP BS 395 CHAFED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25310FE 48299 PILOTS AILERON CONTROL CABLE RUN NR 1 CHAFED INTO PULLEY BRACKET AT FS 395 LBL 30, 8 INCHES FROM BOTTOM FLOOR. PULLEY BRACKET REMOVED AND REPLACED IAW DC10-30 SRM 51-31-01 VOL 11. AILERON RIG PINS P-67 AND P-70 VERIFIED GOOD AND AILERON MECHANICAL TEST GOOD IAW DC10-30 MM 27-10-02-5. 2L73 4F A22WE 20051130000022005113000002NE 2005 11 30 QXEA200501565 320051122A6110 PROPELLER DHAV DHC8 DHC8202 2809007NM HAMSTD14SF 14SF23 NE OUT OF BALANCE A QXEAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 NM09357PH 504 PDX FLT 9851 ON CLIMBOUT WITH PROPS AT 1050 RPM'S HAD A GREAT DEAL OF VIBRATIONS FROM THE PROPS. MAINTENANCE BALANCED BOTH PROPS IAW MTC'S 9610003. OPS CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 6 CP7NE 20051130000042005113000004WP 2005 11 30 ABXA050288 120051114A5313592481661 LONGERON DOUG DC9 DC941 302207NWP BS 642-660 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23953AX 47608 LONGERON 28 RIGHT, STA 642 AND 660, CRACKED AND EXFOLIATED. REMOVED AND REPLACED LONGERON AND FRAME IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 20051130000052005113000005WP 2005 11 30 ABXA050289 120051121A5610 WINDOW DOUG DC8 DC863F 302198FWP COCKPIT LACK OF LUBE A ABXAK NONE O OTHER ININSP/MAINT 1 GL23812AX 46126 CAPTAIN'S CLEARVIEW WINDOW WOULD NOT OPEN. LUBRICATED CAPTAIN'S CLEARVIEW WINDOW ASSEMBLY IAW DC-8 MM 56-00-00. OPS CHECKED GOOD. 2L74 4F 4A25 20051130000062005113000006NM 2005 11 30 QXEA200501568 120051124A2740 SWITCH BOMBDRDHC8 DHC8402 1390042NM PITCH TRIM STICKING A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09400QX 4030 GEG FLIGHT 2351: PITCH TRIM CAUTION LIGHT ILLUMINATES AFTER ENGINE START. MAINTENANCE FOUND F/O PITCH TRIM SWITCH FLAGGED IN CDS. FOUND TO BE STICKING. CLEANED AND LUBED SWITCH. CHECKS GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051130000072005113000007NE 2005 11 30 05FDEA03964 220051126A7210 DUCT DOUG DC10 DC1030F 3023504WP GE CF6 CF650* 30018NE 7TH STAGE CHAFED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25310FE 48299 NR 1 ENG HIGH PRESSURE CONTROL VALVE CHAFING INTO 7TH STAGE AIR PRESSURE TURBINE CONTROL LINE. REMOVED 7TH STAGE COOLING TUBE, PER DC10-30 MM 75-22-00-02. REPAIRED DUCT PER EM 72-09-03. REINSTALLED DUCT AND HIGH PRESSURE VALVE. PERFORMED OPS AND LEAK CHECKS GOOD PER DC10-30 JET RUN HANDBOOK. 2L73 4F4 FRTA22WE E23EA 20051130000092005113000009NM 2005 11 30 05FDEA03966 120051127A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 CORROSION FOUND ON SEAT TRACK CROWN AREA FROM STA 810 TO STA 859 AT X = -75. CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1. REPAIR IS CLASSIFIED MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051130000102005113000010NM 2005 11 30 05FDEA03967 120051127A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 MAIN DECK - CORROSION FOUND ON SEAT TRACK BASE FROM STA 839 TO 859 ADJACENT TO X = 75. CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2L73 4F RTA22WE 20051130000112005113000011NM 2005 11 30 05FDEA03968 120051128A5753 REPAIR DOUG MD11 MD11 3023602NM ZONE 600 MISINSTALLED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25524FE 48480 RIGHT WING - WITH REFERENCE TO EO 1-5100-7-5001 P1, INBOARD FLAP INBOARD SEGMENT UPPER SURFACE AT XIFH 219 TO 225, YIFH 46 TO 52 FOUND WITH EXISTING REPAIR. EVALUATED AND FOUND NOT CARRIED OUT IN ACCORDANCE WITH SRM 57-10-00 FIGURE 34 SHEET 1 VOLUME I. RIGHT HAND WING - INBOARD FLAP INBOARD SEGMENT UPPER SURFACE AT XIFH 219 TO 225, YIFH 46 TO 52 WITH EXISTING REPAIR REMOVED AND REPAIR IS CARRIED OUT AS PER SRM 57-10-00 FIGURE 34 SHEET 1 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051130000152005113000015WP 2005 11 30 05FDEA03972 120051128A5312 FLANGE DOUG DC10 DC1010 3022110WP BULKHEAD CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 CLG WHEEL WELL/SPACE: 1EA CRACK 1 INCH LONG ON DOUBLER FLANGE UPPER SIDE LT VERTICAL BULKHEAD FROM STA 1421 TO 1431 LT SIDE X 31. REMOVED DOUBLER IAW SRM 51-35-01 PG 1/13 VOL 2. CLEANED UP CRACK REPAIRED IAW SRM 53-00-01 FIG 4 SHT 2 VOL 1 WITH FILLER AND REINSTALLED DOUBLER IAW SRM 51-35-01 PG 1/13 VOL 2. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F163443/N00443 AND IAW SRM 53-00-01 FIG 4 SHT 2 VOL 1. 2L73 4F A22WE 20051130000162005113000016WP 2005 11 30 05FDEA03973 120051128A5710 HINGE DOUG DC10 DC1010 3022110WP LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 LT WING LEADING EDGE AT STA XOS 906 FOUND ACCESS PANEL TEE/HINGE CRACK .5 INCH LONG. INSTALLED REPAIR DOUBLER IAW SRM 57-10-00 FIG 49 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F163377/N00377 AND IAW SRM 57-10-00 FIG 49 VOL 1. 2L73 4F A22WE 20051130000182005113000018WP 2005 11 30 05FDEA03975 120051128A5754 REPAIR DOUG DC10 DC1030 3023501WP LT WING SLAT IMPROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 LT WING L/E SLAT FOUND A DOUBLER 20 X 7 INCHES ON LOWER SKIN BETWEEN STA XW 340 AND STA XW 309. REMOVED PART. PERFORMED A GVI OF REPAIR IAW SRM 57-10-00 FIG 55 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001E3. 2L73 4F A22WE 20051130000232005113000023WP 2005 11 30 05FDEA03980 120051128A5520 REPAIR DOUG DC10 DC1030 3023501WP ELEVATOR PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 IN THE UPPER SURFACE OF RT DETACHABLE ELEVATOR AT STA XE82 FOUND 1EA FLUSH REPAIR DOUBLER 6 X 4 INCHES. PERFORMED A GVI OF REPAIR IAW EA 8-5510-90123 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 E3. 2L73 4F A22WE 20051130000252005113000025NM 2005 11 30 DXTA200501106 120051124A2613N160 SENSOR AMD FALC50FALCON2000 2730170NM MLG WW MALFUNCTIONED E DXTAO OTHER N FALSE WARNING CRCRUISE 1 GL07259QS 159 DURING FLIGHT LEFT MAIN LANDING GEAR OVERHEAT LIGHT ILLUMINATED. RESEARCHED TECH DATA. GAINED ACCESS TO WHEEL WELL INSPECTED FOR ANY VISUAL DAMAGE OR DEFECTS, FOUND NONE AT THIS TIME. PERFORMED GEAR WELL OVERHEAT TEST AND TEST PASSED. CONTACTED LMCC FOR HISTORY AND NONE FOUND. PERFORMED OPERATIONAL TEST OF MAIN LANDING GEAR WELL FIRE DETECTOR ON LT SIDE, ANNUNCIATOR GOES OFF AT 340 DEGREES FAHRENHEIT. CONTACTED REP WITH INFO, REP REQUEST, TO INSTALL NEW SENSOR. REMOVED SENSOR P/N B160 AND INSTALLED NEW SENSOR P/N HB160, S/N UK289. PERFORMED OPS CHECK AND FAIL NO INDICATION AT TEMP 420 DEGREES FAHRENHEIT. REMOVED DETECTOR S/N UK289 AND TEMPORARILY INSTALLED ORIGINAL DETECTOR. NEW DETECTOR ON ORDER. R2K73 4F RTA50NM 20051130000262005113000026NM 2005 11 30 DXTA200501107 120051124A5310 STRUCTURE GULSTM200 200 4500308NM FUSELAGE CRACKED E DXTAK NONE O OTHER ININSP/MAINT 1 GL07725QS 105 FORWARD 2 INCHES OF FUEL DIVERTER ON AFT UNDERSIDE OF AIRCRAFT IS SEPARATED FROM FUSELAGE. THERE APPEARS TO BE CRACKS IN FUSELAGE RADIATING FROM BOTH SIDES OF SEPARATED AREA. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA53NM 20051130000282005113000028NM 2005 11 30 DXTA200501102 120051123A213122250R062300 CONTROLLER AMD FALC50FALCON2000 2730170NM CABIN PRESSURE FAILED E DXTAB EMER. DESCENT S AFFECT SYSTEMS CRCRUISE 1 GL07269QS1743 169 AT FL360 AN IMMEDIATE LOSS OF CABIN PRESSURIZATION WAS EXPERIENCED. CABIN PRESSURIZATION IMMEDIATELY WENT ABOVE 10,000 FEET. EMERGENCY DESCENT WAS INITIATED TO 15,000 FEET. AFTER LEVEL OFF AUTOMATIC CABIN PRESSURE CONTROLLER WAS FLASHING A CODE OF AO16. AFTER THE MANUAL MODE OF THE CABIN PRESSURIZATION SYSTEM WAS SELECTED, CABIN PRESSURIZATION BECAME CONTROLLABLE. NO OTHER MALFUNCTIONS OF THE CABIN PRESSURIZATION SYSTEM WERE NOTED. TROUBLESHOT PRESS SYSTEM FOUND PRESS CONTROLLER FAILED. REMOVED & REPLACED AS INSPECTED SERVICEABLE UNIT PER F2000 M/M CH 21-302 AND RAN TO OPS CHECK GOOD. 2K73 4F RTA50NM 20051130000302005113000030CE 2005 11 30 DXTA200501108 120051124A3260 WARNING LIGHT CESSNA750 750 2076810CE MLG FALSE INDICATIONE DXTAO OTHER N FALSE WARNING CLCLIMB 1 GL07978QS 7500187 AFTER GEAR RETRACTION RIGHT MAIN GEAR INDICATOR REMAINED ILLUMINATED. THERE WAS NO RED UNLOCK LIGHT. PUT THE GEAR DOWN AND THEN UP AND THE GREEN LIGHT ILLUMINATED FOR 30 SECONDS AND WENT OUT. PERFORMED LANDING GEAR OPERATIONAL TEST IAW CESSNA 750 MM 32-00-01. NO DEFECTS NOTED. 2L72 4J RTT00007WI 20051130000332005113000033NM 2005 11 30 05FDEA03961 120051125A5310 DOOR FRAME BOEING727 727200 138407ENM ZONE 100 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25266FE 21672 CORROSION ALONG INSIDE OF NR 3 LOWER CARGO DOOR CUTOUT ATF LOWER CORNER. REPAIRED PER E.A 7-5310-92359 FUSELAGE CORROSION ON AFT FRAME OF NR 3 CARGO DOOR OPENING. 2L73 4F RTA3WE 20051130000352005113000035NM 2005 11 30 QXEA200501571 120051124A2750 FLAP SYSTEM BOMBDRDHC8 DHC8402 1390042NM TE FLAPS STUCK A QXEAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM09410QX 4053 GEG FLIGHT 2378: FLAPS STUCK AT 12 DEGREES TAXIING IN. COMPLIED WITH FLAP POWER CAUTION CHECKLIST AND IT RESOLVED ITSELF. MAINTENANCE COMPLIED WITH SERVICE LETTER SL-27-002A. RESET FLAP POWER SYSTEM. OPS CHECK NORMAL. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051130000362005113000036NM 2005 11 30 QXEA200501569 120051123A2430400SG163Q GENERATOR BOMBDRDHC8 DHC8402 1390042NM DC SYSTEM WARNING LIGHT A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09400QX664 4030 BOI FLIGHT 2303: AFTER START NR 2 DC GENERATOR CAUTION LIGHT REMAINS ILLUMINATED. MAINTENANCE REPLACED NR 2 DC GENERATOR IAW MTC 6243101. AIRCRAFT REMAINS CAT III. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051130000372005113000037CE 2005 11 30 DXTA200501109 120051125A2910 LINE CESSNA500 560CESSNA 2076750CE HYDRAULIC SYS LEAKING E DXTAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL07332QS 5600523 DURING TAXI-OUT, CO-PILOTS RIGHT BRAKE PEDAL GOES TO THE FLOOR WITH MINIMAL BRAKE EFFECTIVENESS. AFTER PUMPING BRAKE PEDAL, FULL PRESSURE RETURNS TO BRAKE PEDAL. HOWEVER A SHORT TIME DELAY RETURNS RIGHT BRAKE PEDAL TO SAME CONDITION. BLED BRAKES & ANTI-SKID SYSTEM TO REMOVE ALL AIR IAW CE560 M/M CHAP 32-42-00. BRAKES OPS CHECK & LEAK CHECK GOOD. 2L72 4F RTA22CE 20051130000382005113000038NM 2005 11 30 CALA0500417 120051128A5320146N5447 STRINGER BOEING757 757224 1384958NM BS 1467 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713113 27555 INSPECTION FOUND FLOOR STRINGERS AT CROSS STRAP IN AFT BAG BIN CORRODED AT STA 1467, LBL 26. THE CORROSION WAS REMOVED AND ONE AREA WAS OUT OF LIMITS. A REPAIR WAS INSTALLED IAW SRM 51-70-11, FIGURE 1. THE OTHER AREAS WITHIN LIMITS WERE TREATED AND PRIMED IAW SRM 53-00-53. 2L72 4F RTA2NM 20051130000402005113000040NM 2005 11 30 CALA0500419 120051128A531565C339504 FLOORBEAM BOEING737 737524 1384721NM BS 986.5 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713624 27528 INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, RBL 7 TO LBL 49. REPAIRED IAW ECRA 5310-04494. 2L72 4F RTA16WE 20051130000412005113000041NM 2005 11 30 CALA0500421 120051120A5315141T5107 FLOORBEAM BOEING767 767424ER 1385270NM BS 303 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2767052 29447 INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT STA 303, LBL 23 TO LBL 26. REPAIRED IAW SRM 53-00-51, FIGURE 201, REPAIR 1. 2L72 4F RTA1NM 20051130000432005113000043SO 2005 11 30 RAIA00511032 120051123A3260 DOWNLOCK SWITCH EMB 145 EMB145LR 3260212SO MLG FAILED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03841HK 145382 FLT 8000 - IAD - LANDING GEAR AIR/GROUND FAULT. MAINTENANCE REMOVED AND REPLACED THE DOWNLOCK PROXIMITY SWITCH AND CONNECTOR. 2L72 4T RTT00011AT 20051130000442005113000044SO 2005 11 30 RAIA00511035 120051126A3350 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03810HK 145231 PREFLIGHT - STL - EMERGENCY LIGHT AT EXIT DOOR OUT AT ROW 12. MAINTENANCE REMOVED AND REPLACED THE BULB. 2L72 4T RTT00011AT 20051130000472005113000047SO 2005 11 30 RAIA00511030 120051122A3230355022002 CONTROL UNIT EMB 145 EMB145LR 3260212SO MLG FAILED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03841HK105786857 145382 FLT 8042 - IAD - LANDING GEAR AIR/GROUND FAILURE AFTER TAKEOFF. MAINTENANCE REPLACED THE LANDING GEAR CONTROL UNIT. 2L72 4T RTT00011AT 20051130000492005113000049SO 2005 11 30 RAIA00511036 120051127A3397 CONNECTOR EMB 145 EMB145 3260210SO EMERGENCY LIGHT LOOSE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03802HK 145066 PREFLIGHT - STL - EMERGENCY LIGHT NOT WORKING. MAINTENANCE RESEATED THE CONNECTOR TO THE EXIT SIGN. 2L72 4F RTT00011AT 20051130000502005113000050SO 2005 11 30 RAIA00511037 120051126A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN BURNED OUT A RAIAK NONE O OTHER ININSP/MAINT 1 CE03829HK 145281 PREFLIGHT - IAD - RIGHT OVERWING EMERGENCY EXIT LIGHT BURNED OUT. MAINTENANCE DEFERRED THE OVERWING EMERGENCY LIGHT. 2L72 4T RTT00011AT 20051130000512005113000051EU 2005 11 30 RAIA00511034 120051125A2731 SWITCH JETAIRJETSTMJETSTM4101 1500501EU TRIM MALFUNCTIONED A RAIAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 CE03568HK 41086 FLT 3604 - SYR - ON CLIMBOUT, NOSE DOWN TRIM WOULD NOT WORK USING ELECTRIC TRIM SWITCH. MAINTENANCE DEFERRED THE ELECTRIC ELEVATOR TRIM FUNCTION. 2L72 4T RTA41NM 20051130000532005113000053 2005 11 30 QXEA200501564 420051127A3416 ALTIMETER CNDAIRCL600 CL6002C10 1390015EA COCKPIT ERRATIC A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09607QX 10024 FAT - ON TAXI OUT FOR FLIGHT 2478, CAPTAIN'S RADIO ALTIMETER ERRATIC. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE PLACED THE SYSTEM ON MEL. 2L72 4F RTA21EA 20051130000542005113000054NM 2005 11 30 72000001 120051119A2740 STABILIZER BOEING727 727200 138407ENM JAMMED A K11AJA DUMP FUEL UNSCHED LANDING O OTHER CLCLIMB 1 GL23720CK 21298 AIRCRAFT TOOK OFF FROM KATL TOWARD KYIP. STABILIZER JAMMED IN A VERY NARROW RANGE FROM 2 DEG UP TO 2 DEG DOWN. CREW ELECTED TO RETURN TO KATL. 2L73 4F RTA3WE 20051130000572005113000057NM 2005 11 30 SB05154 120051124A3260189929 DOWNLOCK SENSOR BOEING737 737301 1384611NM NOSE GEAR FAILED A USAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19335US 23232 CLT - FLT266 ON CLIMB OUT FROM CLT, CREW REPORTED THE NOSE LANDING GEAR RED UNSAFE LIGHT ILLUMINMATED AFTER GEAR RETRACTION. CREW EXTENDED LANDING GEAR NORMALLY AND RETURNED TO FIELD. FLIGHT LANDED AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR DOWNLOCK SENSOR S845. OPERATIONAL CHECK GOOD PER MM 32-33. 2L72 4F RTA16WE 20051130000582005113000058NM 2005 11 30 2005UALA01313 120051118A3350 SIGN BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU EMERGENCY EXIT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29348UA 24252 EMERGENCY EXIT SIGN ABOVE FLIGHT DECK DOOR IS INOP. BATTERY PACK REPLACED. 2L72 4F4 FRTA16WE E21EU 20051130000592005113000059NM 2005 11 30 2005UALA01229 120051104A5330 SKIN BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU BS 204 - STR 22 DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29328UA 24148 LOWER FUSELAGE DENT AT STA 204 & STR 22 LEFT. *S/D* REMOVED DAMAGE & ACP NDT FOR CRACKS. NO CRACKS FOUND. FABRICATED AND INSTALLED DOUBLER & FILLER PER SRM 53-10-01 REPAIR NR 11. 2L72 4F4 FRTA16WE E21EU 20051130000602005113000060NM 2005 11 30 2005UALA01230 120051104A5320 ANGLE BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU HORZ STAB CUTOUTCRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29328UA 24148 HORIZONTAL STABILIZER CUTOUT UPPER CHORD ANGLE CRACKED LOCATED BETWEEN STA 1138 & 1156 AT STRINGER 5A. *S/D* REMOVED CRACKED AREA OF CHORD ANGLE. ACP NDT FOR CRACKS. NO CRACKS FOUND. FABRICATED AND INSTALLED NESTED ANGLE REPAIR AND FILLER. PER SRM 51-70-11. 2L72 4F4 FRTA16WE E21EU 20051130000612005113000061NM 2005 11 30 2005UALA01241 120051027A5310 DOOR FRAME BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU CARGO BAY CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29336UA 24240 AFT CARGO DOOR FWD FRAME IS CRACKED AT BOLT HOLE ABOVE THE NR 3 FWD DOOR STOP FITTING. *S/D* REPLACED FORWARD UPPER AND LOWER DOOR FRAMES PER SRM 51-40-02. 2L72 4F4 FRTA16WE E21EU 20051130000632005113000063NM 2005 11 30 2005UALA01302 120051118A2597 WIRE HARNESS AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE SLIDE DEPLOY MISROUTED A UALAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP29830UA 1243 RIGHT FWD MAIN ENTRY DOOR SLIDE DEPLOY CABLE FOUND MISROUTED. CALLOUT LM4118 WAS DONE ON ACFT 4030 R1 SLIDE IN IAD ON 11/11/2004 TO VERIFY CORRECTNESS OF WIRE ROUTING PER AMM 25-62-44. MR25611-149 WAS REPLACED DUE TO TIME WITH MR25611-1162 IN DEC 2005. MR25611-1162 WAS ROBBED AND REPLACED WITH MR25611-1284 IN DEN ON 3/1/2005. MR25611-1284 WAS VERIFIED FOR PROPER INSTALLATION AT ORD ON 3/8/2005. THIS SAME UNIT, WHICH IS THE SUBJECT OF THIS SDR, WAS REPORTED TO HAVE ITS MISROUTED WIRE HARNESS CORRECTED. SINCE THE TIME OF VERIFICATION UNTIL THIS REPORTED FINDINGS, THERE IS NO RECORD TO SHOW HOW THIS HARNESS BECAME MISROUTED. 2L72 4F4 FRTA28NM E40NE 20051130000652005113000065NM 2005 11 30 2005UALA01304 120051120A5330 SKIN BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29374UA 24639 POSSIBLE LONGITUDINAL CRACK BELOW STRINGER AFT OF RIGHT WING BODY FAIRING BELOW EMERGENCY EXIT LIGHT. INSTALLED REPAIR DOUBLER PER UA-EVA-50778. 2L72 4F4 FRTA16WE E21EU 20051130000672005113000067NM 2005 11 30 2005UALA01306 120051120A3350 BATTERY BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29179UA 25158 DOOR 2L BUSTLE EMERGENCY LIGHT DIM. CHARGED BATTERY. 2L74 4F4 FRTA20WE E24NE 20051130000682005113000068NM 2005 11 30 2005UALA01307 120051120A3350 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE GALLEY INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29179UA 25158 RIGHT AISLE OVERHEAD EMERGENCY LIGHT AT ROW 26 AND MID GALLEY CENTER OVERHEAD EMERGENCY LIGHT INOP. REPLACED LAMP. 2L74 4F4 FRTA20WE E24NE 20051130000712005113000071NM 2005 11 30 2005UALA01310 120051120A3397 WIRE BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT BROKEN A UALAK NONE L NO TEST ININSP/MAINT 1 WP29179UA 25158 MID LAVS CENTER AISLE AND RIGHT AISLE EMERGENCY LIGHTS INOP. SPLICED BROKEN FEEDER. 2L74 4F4 FRTA20WE E24NE 20051130000732005113000073NM 2005 11 30 2005UALA01312 120051119A3350 LIGHT BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU CABIN LOOSE A UALAK NONE O OTHER ININSP/MAINT 1 WP29373UA 24638 EMERGENCY EXIT LIGHT STRIP NOT ATTACHED FIRST 6 INCHES. EEL STRIP REINSTALLED. 2L72 4F4 FRTA16WE E21EU 20051130000752005113000075NM 2005 11 30 2005UALA01315 120051121A5300 CREASE BEAM BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU BS 294-336 CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29922UA 26642 FWD GALLEY CREASE BEAM CORRODED FROM STA 294 TO STA 336 AT STR 17, RBL 57 WL 208. REPL'D CREASE BEAM REF SRM51-40-02. 2L72 4F4 FRTA16WE E21EU 20051130000772005113000077 2005 11 30 2005UALA01318 420051120A2565101655305 SLIDE BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE OVERWING UNSERVICEABLE A UALAK NONE O OTHER ININSP/MAINT 1 WP29659UA 27114 DAMAGED BEARINGS. THIS TYPE OF EVENT HAS HAPPENED BEFORE AND BOEING IS WORKING ON IMPROVED FABRICATION MATERIALS TO ADDRESS THIS CONDITION. SLIDE WAS REMOVED FROM THE AIRCRAFT AND SENT TO THE COMPONENT SHOP WHERE BEARINGS WERE REPLACED. 2L72 4F4 FRTA1NM E24NE 20051130000792005113000079NM 2005 11 30 2005UALA01320 120051113A5320 SILL BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU CARGO DOORWAY CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29349UA 24253 AFT PIT HAS DENT IN LOWER SILL. AREA OF DENT IS ON DOOR SILL. REPAIRED SILL AND REINSTALLED. 2L72 4F4 FRTA16WE E21EU 20051130000802005113000080NM 2005 11 30 2005UALA01321 120051122A5311 FRAME BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU BS 440 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29922UA 26642 RIGHT CABIN STA 440 FRAME IS CRACKED BETWEEN STRINGERS 8R & 9R AT PSU SUPPORT BRACKET ATTACH. REPAIRED FRAME REF MM53-10 -84, REPAIR III. 2L72 4F4 FRTA16WE E21EU 20051130000812005113000081NM 2005 11 30 2005UALA01322 120051122A5311 FRAME BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU BS 440 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29922UA 26642 LEFT CABIN STA 440 FRAME IS CRACKED BETWEEN STR 8 & 9 LEFT AT PSU SUPPORT BRACKET ATTACH. MAJOR REPAIR ACP'D PER MM 53-10-84 REPAIR III. 2L72 4F4 FRTA16WE E21EU 20051130000822005113000082NM 2005 11 30 2005UALA01323 120051122A5311 FRAME BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU BS 907 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29922UA 26642 RIGHT AFT CABIN FRAME STA 907 CRACKED BETWEEN STRINGERS 8 & 9 RIGHT AT PSU ATTACH. MAJOR REPAIR ACP'D PER MM 53-10-84 REPAIR III. 2L72 4F4 FRTA16WE E21EU 20051130000832005113000083NM 2005 11 30 2005UALA01324 120051122A5311 FRAME BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU BS 907 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29922UA 26642 LEFT CABIN STA 907 FRAME IS CRACKED BETWEEN STRINGERS 8 - 9 LEFT AT PSU SUPPORT BRACKET ATTACH. MAJOR REPAIR ACP'D PER MM 53-10-84 REPAIR III. 2L72 4F4 FRTA16WE E21EU 20051130000882005113000088NM 2005 11 30 2005UALA01328 120051122A5311 FRAME BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU BS 727D CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29922UA 26642 CABIN FRAME CRACKED STA 727D AT STR 8R AT PSU ATTACH. MAJOR REPAIR ACP'D PER MM 53-10-84 REPAIR III. 2L72 4F4 FRTA16WE E21EU 20051130000892005113000089NM 2005 11 30 2005UALA01329 120051122A5551 ATTACH FITTING BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU HORIZONTAL STAB CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29906UA 25006 LEFT HORIZONTAL STABILIZER FWD SPAR UPPER ATTACH LUG CORRODED. MAJOR REPAIR ACP'D PER AAR EA I050309 FOR LUG REWORK AND BUSHING REPLMTS. 2L72 4F4 FRTA16WE E21EU 20051130000932005113000093 2005 11 30 2005UALA01333 420051122A3414 INDICATOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE AIRSPEED MALFUNCTIONED A UALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP29584UA 26706 RETURNED TO THE FIELD DUE TO AN ERRATIC AIRSPEED INDICATOR. NUMBER 2 MACH AIRSPEED INDICATOR WAS REPLACED. THE AIRSPEED POINTER RETURN SPRING WAS FOUND BROKEN. 2L72 4F4 FRTA2NM E17NE 20051130000942005113000094EA 2005 11 30 SWIA200515879 120051126A5753 FLAP CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ICED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION LDLANDING 1 NM07457SW 7773 FLAPS FAIL CAUTION MSG AFTER LANDING DURING FLAP RETRACTION. REMOVED SNOW AND ICE AS REQUIRED. CYCLE FLAPS SEVERAL TIMES. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051130000952005113000095SO 2005 11 30 SWIA200515880 120051119A3350 SIGN EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07290SW 120317 FLOOR LEVEL EXIT SIGN IS BROKEN AT 9BC. REPLACED EXIT SIGN IAW MM 33-00-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20051130000962005113000096SO 2005 11 30 SWIA200515881 120051120A2750 FLAP SYSTEM EMB 120 EMB120ER 3260203SO TE FLAPS INTERMITTENT A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07290SW 120317 AFTER SELECTING FLAPS TO 15 DEGREES RECEIVED A CONTROL FAULT INDICATION. CLEANED OUTBOARD PAIR FLAP CONNECTOR. OPERATIONAL TEST FLAPS ON GROUND GOOD. 2L72 4T RTA31SO 20051130000972005113000097EA 2005 11 30 SWIA200515882 120051124A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07927SW 7693 FLOOR STRIP EMERGENCY LIGHTS ROWS 2-6 DO NOT ILLUMINATE. REPLACED POWER STRIP FLOOR LIGHTS ROWS 2-6. OPERATIONAL CHECK GOOD IAW CRJ 200 MM 33-50-00. 2L72 4F RTA21EA 20051130000992005113000099EA 2005 11 30 SWIA200515884 120051122A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07592SW 7279 NR 2 CEILING EMERGENCY FLOODLIGHT INOP. RELAMPED NR 2 CEILING EMERGENCY FLOODLIGHT. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051130001052005113000105EA 2005 11 30 SWIA200515890 120051121A2752853D10020 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07944SW1022010220 7764 FLAPS FAILED MESSAGE. REPLACED NR 3 RIGHT WING FLAP ACTUATOR. OPERATIONAL CHECK GOOD IAW MM 27-54-00. 2L72 4F RTA21EA 20051130001082005113000108EA 2005 11 30 SWIA200515893 120051114A276052C52610A1 MANIFOLD CNDAIRCL600 CL6002B19 1900309EA GROUND SPOILER MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07465SW 7845 OUTBOARD GROUND SPOILERON CAUTION MSG ON LANDING. REPLACED GROUND SPOILER MANIFOLD IAW CRJ MM 27-63-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051130001102005113000110EA 2005 11 30 SWIA200515895 120051119A2750 DRIVE SHAFT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS LACK OF LUBE A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07952SW 7805 FLAPS STUCK AT 30 DEG WILL NOT EXTEND OR RETRACT. CLEANED AND RELUBED FLEX DRIVE SHAFT SYSTEM. REMOVED AND REPLACED RIGHT WING NR 1, 2 AND 3 ACTUATORS AND RIGHT WING NR 1, 2, 3 AND 4 ACTUATORS AND RIGHT BPSU. OPERATIONAL CHECK GOOD IAW 27-53-00. 2L72 4F RTA21EA 20051130001112005113000111EA 2005 11 30 SWIA200515896 120051118A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07412SW 7101 OVERHEAD EMERGENCY FLOODLIGHT (THE FORWARD MOST) DOES NOT ILLUMINATE. RELAMPED FORWARD CEILING EMERGENCY LIGHT AS REQUIRED, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051130001142005113000114EA 2005 11 30 SWIA200515899 120051117A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY MALFUNCTIONED A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07460SW 7803 CARGO SMOKE AURAL AND MESSAGE AT THE GATE. REPLACED CARGO COMPARTMENT FORWARD DETECTOR IAW MM 26-15-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051130001202005113000120WP 2005 11 30 AALA20050771 120051121A28223980001 PUMP DOUG DC9 DC982 3022082WP FUEL BOOST INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21427AA 49339 ORD - FORWARD CENTER TANK BOOST PUMP CIRCUIT BREAKER POPPED IN FLIGHT. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED THE CENTER TANK BOOST PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051130001212005113000121WP 2005 11 30 AALA20050772 120051122A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21255AA 49287 SFO - EMERGENCY LIGHT IN TAIL COMPARTMENT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT IN TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051130001222005113000122NE 2005 11 30 AALA20050774 220051123A7230 FAN BLADE BOEING737 737823 13844BZNM GE CFM56 CFM567B24 NE LT ENGINE BIRD INGESTION A AALAA UNSCHED LANDING C F.O.D. CLCLIMB 1 SW21977AN 29550 888712 JFK - ON TAKEOFF FROM LGA TOOK BIRD INTO LEFT ENGINE. DIVERTED TO JFK AND LANDED WITHOUT INCIDENT. PERFORMED BOROSCOPE AND REPLACED COMPLETE SET OF FAN BLADES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA16WE E00055EN 20051130001232005113000123WP 2005 11 30 AALA20050778 120051124A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21251AA 49270 SFO - CEILING EMERGENCY LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051130001242005113000124NM 2005 11 30 UPS05245831 120051014A5330 SKIN BOEING727 72730C 1384009NM BS 852-1011 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 SURFACE CORROSION ON LAP JOINT BETWEEN S-4L AND 5L AT LOCATIONS BETWEEN BS 852 AND 1011. CORROSION REMOVED IAW SRM 51-10-2 (.002") AND FOUND WITHIN LIMITS IAW SRM 51-20-4. 2L73 4F A3WE 20051130001252005113000125NM 2005 11 30 UPS05245832 120051016A5330 SKIN BOEING727 72730C 1384009NM BS360 STR 22L CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 EVIDENCE OF CORROSION AT BS 360 STR 22L AT FWD END OF STR AT AFT FACE OF FRAME. PLEASE INVESTIGATE AND RECTIFY. CORROSION BLENDED OUT IAW SRM 51-10-06. CORROSION FOUND TO BE OUTSIDE LIMITS IAW SRM 51-10-1. REPAIR STRAP FABRICATED IAW SRM 51-20-1 FIG 7. MATERIAL P/N 7055T6 0.063". REPAIR STRAP INSTALLED IAW SRM 51-30-02. 2L73 4F A3WE 20051130001262005113000126NM 2005 11 30 UPS05245833 120051012A5330 SKIN BOEING727 72730C 1384009NM BS 521-515 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 AREA OF SUSPECT CORROSION ON CROWN SKIN BS 521 TO BS 515 BETWEEN STR 2L AND 3L. PLEASE PAINT STRIP AREA, REMOVE FASTENERS IF REQUIRED, REINSPECT AND RECTIFY AS NECESSARY. REPAIRED IAW UPS AUTHORIZATION B727-5330-23323-A 2L73 4F A3WE 20051130001282005113000128NM 2005 11 30 UPS05245835 120051011A5343 TRUNNION BOEING727 72730C 1384009NM LH MLG CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 LT MLG SUPPORT FITTING HAS CRACK INDICATION IN HOLE B & C ON INB FLANGE AND HOLES E IN COUNTERSINKS. REPAIR AND REPLACE FITTING LT MLG TRUNNION REMOVED AND FOUND CRACKED OUTSIDE REPAIRABLE LIMITS IN UPS EO B727-5740-20666C. TRUNNION REPAIRED IAW UPS AUTHORIZATION B727 -5740-23046-B. 2L73 4F A3WE 20051130001292005113000129NM 2005 11 30 UPS05245836 120051015A534365192962 TRUNNION BOEING727 72730C 1384009NM RT MLG CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 RT TRUNNION ATTACH FITTING HAS CRACK AT OB FLANGE HOLE E RUNNING UP APPROX 2.5 INCHES. REMOVE AND REPLACE FITTING. RT TRUNNION FITTING FOUND CRACKED OUTSIDE REPAIRABLE LIMITS IN UPS EO B727-5740-20666C. REPLACED IAW UPS AUTHORIZATION B727-5740-23046-B. 2L73 4F A3WE 20051130001312005113000131CE 2005 11 30 DXTA200501112 120051125A2910 LINE CESSNA500 560CESSNA 2076750CE HYDRAULIC SYS LEAKING E DXTAO OTHER S AFFECT SYSTEMS LDLANDING 1 GL07312QS 5600312 CO-PILOT'S LEFT BRAKE FAILURE UPON LANDING. BRAKE WENT TO FLOOR, REQUIRED PUMPING TO RESTORE PRESSURE. VERIFFIED LT CO-PILOT PEDAL SOFT, REMOVED FWD BAGGAGE PANELS TO GAIN ACCESS INSPECTED LINES IN FWD COMPARTMENT FOR LEAKS CHECKED BRAKE WEAR AND WHEEL WELL LINES FOR LEAKS NO LEAKS FOUND AND BRAKE WEAR IS GOOD BLED BRAKES AS NEEDED IAW CE560 MM 32-42-00. 2L72 4F RTA22CE 20051130001352005113000135CE 2005 11 30 DXTA200501116 120051127A3320 LIGHT CESSNA560 560XL 2076702CE CABIN INOPERATIVE E DXTAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07646QS 5605246 DURING FLIGHT, DISCOVERED LEFT CABIN TABLE AND READING LTS INOP. LEFT FLOOR DROP DOWN LIGHTS INOP, LIQUID HOT PLUS COLD CONTAINERS INOP. ALSO DIVIDER SWITCHES HAD RED FAILURE LIGHTS INDICATED, CABIN PLUS ENTRY DOOR LIGHTS ALSO INOP. AFTER FLIGHT, SMELLED DISTINCT ODOR OF BURNING ELECTRICAL WIRING. NO CIRCUIT BREAKERS POPPED IN COCKPIT/AFT CLOSET OR LIQUOR CABINET. 2L72 4F RTA22CE 20060607001752006060700175SO 2006 6 7 XGN2006F00001 220051011A8530ECI712A CYLINDER BEECH 33 F33A 1151425CE CONT O520 IO520BA 17032SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW051096W1147 CE436 807017 THESE CYLINDERS SHOWED TO BE CRACKED IN THE EXHAUST SIDE OF THE HEAD. THE LEAKS SHOWED UP WHEN DOING THE COMPRESSION CHECK. DUE TO THE NUMBER OF CRACKED CYLINDER HEADS, WE DO A COMPRESSION CHECK EVERY 50 HRS. (K) 1L71 3O3 O 3A15 E5CE 20060612001532006061200153SO 2006 6 12 XGN2006F00047 220050426A8530TISN712ACA CYLINDER BEECH 58 58 1152740CE CONT O520 IO520C 17032SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW05577W 1851 TH375 210755 CYLINDER HEAD CRACKED, FOUND DURING 100 HR INSPECTION. THIS IS AN ON GOING PROBLEM THAT WE ARE FINDING IN OUT FLEET OF AIRCRAFT. (K) 1L72 3O3 O 3A16 E5CE 20051128000072005112800007NM 2005 11 28 USAA200511006 120051115A5330 SKIN BOEING737 7373B7 1384580NM BS 892 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19373US 22952 A 2 INCH CRACK IN FUSELAGE SKIN AT STA 892, 6 INCH BELOW STR 24R. INSTALLED REPAIR DOUBLERS PER SRM 53-00-01 FIG 201. 2L72 4F RTA16WE 20051128000192005112800019NM 2005 11 28 USAA051414 120051122A5330143N361115 SKIN BOEING757 757225 1384959NM RROYCERB211 RB211* 54555NE BS 1337 GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19602AU 22196 STA 1337 STR 30 GOUGED. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 53-00-01 REPAIR 2. DEFECT SIZE: 1.0 INCH, L X .080 INCH, W X .017 INCH D. 2L72 4F4 FRTA2NM A12EU 20051128000202005112800020NM 2005 11 28 USAA051413 120051122A5754 SKIN BOEING737 737301 1384611NM GE CFM56 CFM56* 13802NE NR 2 SLAT DEBONDED A USAAK NONE O OTHER ININSP/MAINT 1 EA19300AU 23228 NR 2 SLAT T/E WEDGE SS 246.4 - 241.9 DEBONDED. INSTALLED DOUBLER IAW EA 97124. DEFECT SIZE: 5 INCH X 4 INCH. 2L72 4F4 FRTA16WE E2GL 20051128000242005112800024NM 2005 11 28 SCNA05011 120051117A3350 LENS BOEING737 737800* NM EMERGENCY EXIT WORN A SCNAK NONE O OTHER ININSP/MAINT 1 GL15PHHZV 30650 DURING CONFORMITY INSPECTION DISCOVERED ROW 15DEF AFT EMERGENCY EXIT LENS ILLEGIBLE. REMOVED AND REPLACED LENS AS REQUIRED, CHECKED GOOD. 2L72 4F RTA16WE 20051128000262005112800026 2005 11 28 UPS05145820 420051123A2565 SLIDE AIRBUSA300 A300F4622R 3930360EU PAX DOOR MALFUNCTIONED A IPXAH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION LDLANDING 1 SO01141UP 0824 MAIN CABIN DOOR WOULD NOT DISARM. PERFORMED DOOR ADJ & TEST PER MM 52-10-30-5 -1.2.3.4. DOOR SEEMS TO OPERATE NORMALLY. 2L72 4F RTA35EU 20051128000272005112800027 2005 11 28 SWAA053724 420051121A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051128000322005112800032NM 2005 11 28 SWAA053729 120051122A531165C22909 FRAME BOEING737 7373H4 1384600NM BS 500C CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 20L. REPAIRED FRAME PER SWA EA. 2L72 4F RTA16WE 20051128000332005112800033NM 2005 11 28 SWAA053730 120051121A2560P4010021 BATTERY BOEING737 7373H4 1384600NM FLASHLIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29362SW 26573 AFT CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2L72 4F RTA16WE 20051128000352005112800035NM 2005 11 28 SWAA053732 120051121A335057771 CAP BOEING737 7377H4 1384404NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29433LV 33716 DURING SCHEDULED MV2 CHECK, FOUND CABIN EEPLS TRACK FWD END CAP BROKEN. REMOVED AND REPLACED END CAP PER MM. 2L72 4F RTA16WE 20051128000412005112800041NM 2005 11 28 SWAA053738 120051122A53116546529 SHEAR TIE BOEING737 7373H4 1384600NM BS 500A CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500A, RBL 1. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051128000422005112800042NM 2005 11 28 SWAA053739 120051122A55516551524 ATTACH FITTING BOEING737 7373H4 1384600NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED D-CHECK, FOUND LT & RT HORIZONTAL STAB ATTACH FITTING LUG FACES CORRODED. REPAIRED LUG FACES PER SRM. 2L72 4F RTA16WE 20051128000442005112800044NE 2005 11 28 SWAA053741 220051121A72401493M73G COMBUST CHAMBER BOEING737 7377H4 1384404NM GE CFM56 CFM56* 13802NE NR 1 ENGINE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29785SW 30602 877637 DURING SCHEDULED HC1 CHECK, FOUND NR 1 ENGINE, NR 8 FUEL NOZZLE BELOW IGNITER HOLE SECONDARY SWIRL NOZZLE VENTURI AREA OF MATERIAL CRACKED AND MISSING. REMOVED AND REPLACED NR 1 ENGINE PER MM. 2L72 4F4 FRTA16WE E2GL 20051128000502005112800050NM 2005 11 28 SB05150 120051120A335020131A BATTERY PACK BOEING737 737301 1384611NM EMERGENCY LIGHT DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19353US 23556 FLL - MAINTENANCE REPORTED THE AFT EMERGENCY LIGHT BATTERY INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY LIGHT BATTERY. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20051128000612005112800061WP 2005 11 28 UPS05845793 120051103A5310 DOOR FRAME DOUG DC8 DC873F 302199FWP BS 1400 L28R CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE:C1 D-PIT TORQUE BOX FRAME AT L28R FS 1400 CRACKED WHERE LATCH MECHANISM ATTACHES. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE DOUBLER IAW SRM 51-3-0, 53-2-0 FIG 1B, 51-1-21 AND 51-1-20D. 2L74 4F RT4A25 20051128000642005112800064NM 2005 11 28 SAA200511006 120051115A5330 SKIN BOEING737 7373B7 1384580NM BS 892 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19373US 22952 A 2 INCH CRACK IN FUSELAGE SKIN AT STA 892, 6 INCHES BELOW STR 24R. INSTALLED REPAIR DOUBLERS PER SRM 53-00-01 FIG 201. 2L72 4F RTA16WE 20051128000682005112800068CE 2005 11 28 DXTA200501084 120051114A7500 ODOR CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE BLEED AIR SYS DETECTED E DXTAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DEDESCENT 1 GL07347QS 5600357 DURING DESCENT, WINDSHIELD HEAT WAS SELECTED TO LOW, AFTER OPENING THE WINDSHIELD BLEED KNOBS. APPROX 1 MINUTE LATER AN ODOR WAS OBSERVED FOLLOWED BY THE -WINDSHIELD AIR OVERHEAT- ANNUNCIATOR. TURNED SYSTEM OFF, SMELL AND LIGHT WENT AWAY. RAN AC, RAN WINDSHIELD HEAT FOR SEVERAL MINUTES, OPERATIONAL CHECK OF WINDSHIELD BLEED AIR ANTI-ICE CHECKED GOOD. COULD NOT DUPLICATE ODOR OR -WINDSHIELD AIR OVERHEAT- ANNUNCIATOR. ALL WORK PERFORMED IAW CESSNA 560 ULTRA MM CH 30-41-00. NO OTHER DISCREPANCIES NOTED. 2L72 4F4 FRTA22CE E25EA 20051128000732005112800073CE 2005 11 28 DXTA200501086 120051116A3246315381 WHEEL CESSNA750 750 2076810CE MLG OUT OF BALANCE E DXTAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 GL07990QS220 7500190 SEVERE NOSE WHEEL SHIMMY STARTED AT APPROXIMATELY 60 KIAS DURING TAKEOFF ROLL. TAKEOFF ABORTED, MAX SPEED APPROXIMATELY 65 KIAS BEFORE ABORT. INSPECTED NOSE GEAR FOR ANY DEFECTS, NONE NOTED. JACKED NOSE, INSPECTED STEERING UNIT AND NO DEFECTS NOTED. FOUND BOTH NOSE TIRES TO BE WORN TO LIMITS. REMOVED AND RAN BOTH TIRES ON WHEEL BALANCER. FOUND BOTH WHEELS TO BE OUT OF BALANCE. INSTALLED TWO OVERHAULED NOSE WHEEL ASSY'S IAW CH 32-41-00 OF THE CE 750 MM. 2L72 4J RTT00007WI 20051128000752005112800075CE 2005 11 28 DXTA200501090 120051117A3241 ACCUMULATOR CESSNA500 560CESSNA 2076750CE BRAKE SYSTEM LOW E DXTAO OTHER SJ AFFECT SYSTEMS WARNING INDICATION LDLANDING 1 GL07808QS 5600619 UPON LANDING, AFTER APPLYING BRAKES, LOW BRAKE PRESS AND ANTI SKID INOP. MASTER CAUTION LAMPS ON FOR 6 SECONDS THEN EXTINGUISHED. ALSO BRAKES GRABBY LT MORE THAN RT. FOUND POWER BRAKE ACCUMULATOR PRECHARGE FLAT SERVICED WITH N2 TO PRECHARGE PRESSURE CHECKED FOR LEAKS. NO LEAKS NOTED CHECKED OPERATION OF POWER BRAKE CHECKS OK IAW CE560 MM 12-13-02 & 32-41. 2L72 4F RTA22CE 20051128000762005112800076CE 2005 11 28 DXTA200501091 120051118A3240215297 BRAKE CESSNA500 560CESSNA 2076750CE MLG STICKING E DXTAO OTHER S AFFECT SYSTEMS LDLANDING 1 GL07312QS125 5600312 UPON LANDING AND TAXIING BRAKES WERE HARD, MORE THAN NORMAL BRAKING PRESSURE WAS REQUIRED. UNEVEN BRAKING AND JERKING DURING TAXI RESULTED. INSPECTED BRAKE SYSTEM, FOUND NO FAULTS ON PANEL. INSPECTED BRAKES AND FOUND RT BRAKE GRABBING WITH NO PRESSURE APPLIED. REMOVED AND REPLACED RT BRAKE ASSY WITH A OVERHAULED UNIT IAW CESSNA 560 MAINTENANCE MANUAL CHAPTER 32-42-01. BLED BRAKE SYSTEM IAW CESSNA 560 MAINTENANCE MANUAL CHAPTER 32-42-00. LEAK AND OPERATIONAL CHECKS SATISFACTORY. 2L72 4F RTA22CE 20051128000862005112800086NM 2005 11 28 UPS05545817 120051119A3150 COMPUTER BOEING757 75724APF 1384969NM LT EICAS FAULTY A IPXABA EMER. DESCENT UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01475UP 28845 MULTIPLE WARNINGS, CAUTION AND ADVISORY EICAS ANNUNCIATIONS ON TAKEOFF ALONG WITH AURAL WARNINGS. RETURNED FOR EMERGENCY LANDING. ALL ANNUNCIATIONS EXCEPT AURALS DISAPPEARED WHEN EICAS COMPUTER SWITCH MOVED FROM AUTO TO RIGHT. REPLACED FAULTY LEFT EICAS COMPUTER PER MM 31-41-02-4. 2L72 4F RTA2NM 20051128000892005112800089WP 2005 11 28 ABXA050281 120051114A574049162701 CLIP DOUG DC9 DC941 302207NWP CENTER WING CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23953AX 47608 FRAME SUPPORT FITTING HAD CRACK INDICATIONS ON INBOARD SIDE. REMOVED AND REPLACED SUPPORT FITTING FS 675, LONGERON 29 LEFT IAW DC9 SRM 51-30-5. 2L72 4F A6WE 20051128000902005112800090WP 2005 11 28 ABXA050282 120051114A532039240261 FITTING DOUG DC9 DC941 302207NWP LONGERON CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23953AX 47608 LONGERON END CRACKED FS 642 AT LONGERON 26 LEFT. REMOVED AND REPLACED LONGERON END FITTING FS 642, LONGERON 26 LEFT IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20051128000912005112800091WP 2005 11 28 ABXA050283 120051114A532049162701 SUPPORT FITTING DOUG DC9 DC941 302207NWP FRAME CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23953AX 47608 FRAME SUPPORT FITTING HAD CRACK INDICATIONS ON INBOARD SIDE FS 675 AT LONGERON 29 LEFT. REMOVED AND REPLACED SUPPORT FITTING FS 675, LONGERON 29 LEFT IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20051128000942005112800094NM 2005 11 28 AT0500043 120051114A3350767 LAMP BOEING737 73776N 13844CHNM EMERGENCY LIGHT INOPERATIVE A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15273AT 32662 EXTERIOR EMERGENCY LIGHT INOP LEFT AFT LOWER. REMOVED AND REPLACED LAMP IAW MM 33-51, OPS CHECKS GOOD. 2L72 4F RTA16WE 20051128000962005112800096NE 2005 11 28 NACA20050029 220051111A8530356994 CYLINDER DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE NR 2 ENGINE CRACKED A NACAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CRCRUISE 1 AL03438721096 1096 533294 CP450668 NR 2 ENGINE SHUT DOWN DUE TO RUNNING ROUGH AND WILL NOT TAKE A LEAN. FOUND NR 2 ENGINE NR 1 CYLINDER WITH CRACKED HEAD. REPLACED NR 1 CYLINDER IAW DC-6MM SECTION V, PG 16 & 16A. OP CHECKED GOOD. 2L74 4R4 R A781 5E8 20051128000972005112800097NE 2005 11 28 NACA20050031 220051122A7421URHB32E SPARK PLUG PWA DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE ENGINE FOULED A NACAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CRCRUISE 1 AL0399330198 198 046212 43576 P33921 NR 3 ENGINE SHUT DOWN DUE TO BACKFIRE AND DOUBLE SHORTED SECONDARY ON NR 15 CYLINDER. REMOVED NR 15 CYLINDER FRONT AND REAR SPARK PLUGS. NO VISUAL DEFECTS NOTED. TESTED PLUGS AND FOUND WOULD NOT FIRE. INSTALLED SERVICEABLE PLUGS. PERFORMED ENGINE OPS CHECK, CHECKED GOOD. REF NAC DC-6MM SEC IV ECO5.1 & ECO1.2. 2L74 4R4 R 6A3 5E8 20051128000982005112800098CE 2005 11 28 DXTA200501099 120051121A5270 POSITION SWITCH CESSNA650 650 2076802CE PAX DOOR OUT OF ADJUST E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07782QS 6507082 CAB DOOR UNLOCK LIGHT WAS FLICKERING ON TAKEOFF ROLL, AFTER THE ABORT THE ANNUNCIATOR EXTINGUISHED. REPEAT WRITE UP. ADJUSTED UPPER FWD DOOR PIN SWITCH, OPERATIONAL CHECKS SATISFACTORY. ALL WORK IAW CE-650 M/M CHPT 52-70-00. 2L72 4F A9NM 20051128001002005112800100CE 2005 11 28 DXTA200501096 120051119A3297 RELAY CESSNA500 560CESSNA 2076750CE ANTI SKID SYS STICKING E DXTAO OTHER S AFFECT SYSTEMS LDLANDING 1 GL07808QS 5600619 UPON LANDING, AFTER APPLYING BRAKES, LOW BRAKE PRESS + ANTI-SKID INOP + MASTER CAUTION LAMPS ON FOR 6 SECONDS THEN EXTINGUISHED. NO BRAKING AVAIL FOR INITIAL 2 SECONDS OF BRAKING. GAINED ACCESS TO BRAKE MOTOR & ANTI-SKID RELAY. TROUBLESHOT SYSTEM TO STICKING ANTI-SKID RELAY, INSTALLED NEW RELAY, CHECK GOOD. INSTALLED REMOVED COMPONENTS, OPS CHECK GOOD. CLOSED NOSE BAGGAGE AS NECESSARY, ALL WORK ACCOMPLISHED IAW MM 32-42-00. 2L72 4F RTA22CE 20051128001022005112800102CE 2005 11 28 DXTA200501098 120051121A2120 ODOR BEECH MU300 400A 1155402CE CABIN DETECTED E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL07142QS RK432 DURING CLIMBOUT THROUGH 15,000 FT AND UP, A PUTRID ODOR WAS COMING FROM AFT CABIN. CABIN HEAT WAS ON ALONG WITH WING HEAT AND ALL ANTI-ICE WAS ON. ODOR DISSIPATED DURING DESCENT. ITEM IS UNDER INVESTIGATION. 2H72 4F RTA16SW 20051128001032005112800103 2005 11 28 DXTA200501095 420051118A3100 POSITION SWITCH CESSNA560 560XL 2076702CE STAB ACTUATOR OUT OF ADJUST E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07645QS 5605145 NO TAKEOFF ANNUNCIATOR ILLUMINATED ON TAKEOFF ROLL, AND WILL NOT GO OUT. VERIFIED DISCREPANCY. NOTED STAB ACTUATOR, NO TAKEOFF, SWITCH OUT OF ADJUSTMENT. ADJUSTED SWITCH INTO LIMITS, OPERATIONAL TEST CHECKS GOOD, MAINTENANCE DONE IAW 560XL MAINTENANCE MANUAL CH 27-40-00. 2L72 4F RTA22CE 20051128001132005112800113NM 2005 11 28 QXEA200501551 120051030A5347 SEAT TRACK BOMBDRDHC8 DHC8402 1390042NM BS 137-200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX: RT OUTBOARD SEAT TRACK IS CORRODED AT STA X137-X140, X154-X157, X169 AND X200. MAINTENANCE REPAIRED IAW RD 8/4-53-844 AND NDTM PART 6, 51-00-02-250-801. 2H72 4T RTA13NM 20051128001152005112800115NM 2005 11 28 QXEA200501540 120051102A5230 SKIN BOMBDRDHC8 DHC8402 1390042NM CARGO DOOR CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX: AFT CARGO DOOR AFT LOWER SKIN BEHIND AFT LOWER ROLLER BRACKET HAS CHAFING AND CORROSION. MAINTENANCE REPAIRED IAW NDTM PART 6, 51-00-01-250-801, NDTM PART 6, 51-00-04 AND QX EA 6-52-410. 2H72 4T RTA13NM 20051128001172005112800117EA 2005 11 28 COMA0560614 120051117A5210 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA PAX DOOR LATCH FALSE ACTIVATIONA COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01587SW 7062 FLIGHT 5743 - CABIN DOOR LATCH CAUTION AND WARNING. INSPECTED LATCH SYSTEM AND PRESSURIZED A/C. NO DEFECTS FOUND. 2L72 4F RTA21EA 20051128001192005112800119GL 2005 11 28 BB05100 220051122A7230 COMPRESSOR BOEING767 767200 1385120NM GE CF6 CF6* 30020GL LT ENGINE STALLED A USAAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 EA19656US 26847 AFTER TAKEOFF, LEFT ENGINE COMPRESSOR STALL. REDUCED LEFT ENGINE THRUST TO IDLE AND RETURNED TO FIELD AMS. MAINTENANCE ACTION PENDING. (OPEN) 2L72 4F4 FRTA1NM E23EA 20051128001222005112800122WP 2005 11 28 NACA20050030 120050927A5713 STRINGER DOUG DC6 DC6A 3021706WP LT WING CRACKED A NACAK NONE O OTHER ININSP/MAINT 1 AL036174C 44075 VISUAL INSPECTION REVEALS 1.5 INCH LONG CRACK ON LEFT WING STRINGER NR 17 AT WING STA 299.5 WHICH WAS DISCOVERED DURING SCHEDULED MAINTENANCE OPERATIONAL CHECK NR 5. MANUFACTURED AND INSTALLED EXTERNAL DOUBLER AND TRIPLER IAW DRAWING NAC2005-25, REV 1R, DATED 22 OCTOBER 2005 PROVIDED BY (STRUCTURES) DER DERT-510232-CE, AND FAA FORM 8110-3, DATED 22 OCTOBER 2005. 2L74 4R 6A3 20051128001232005112800123NM 2005 11 28 BB05101 120051128A3350 SOCKET BOEING767 767200 1385120NM EMERGENCY LIGHT DISCONNECTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19652US 24765 CABIN FLOOR LEVEL EMERGENCY LIGHTS INOPERATIVE ON RIGHT SIDE, ROWS 3-11 AND 28-29. MAINTENANCE RECONNECTED SOCKETS AT TWO LOCATIONS. NO FURTHER FAULTS NOTED. 2L72 4F RTA1NM 20051128001282005112800128SO 2005 11 28 Z4TA20050003 220050919A8530537296 HOUSING BEECH 58 58 1152740CE CONT O550 IO550B SO PUSH ROD CRACKED E Z4TAK NONE K FLUID LOSS ININSP/MAINT 1 SO0595KM 1401 1401 TH1315 810485R PILOT REPORTED ABNORMAL OIL LOSS FOR RIGHT ENGINE. ALSO, OIL TRAIL ON LOWER RT WING. UPON INSPECTION, FOUND NR 6 CYLINDER FORWARD PUSH ROD HOUSING CRACKED, ALLOWING OIL TO DRAIN INTO LOWER COWL. REPLACED HOUSING. 1L72 3O3 O 3A16 E3SO 20051128001302005112800130NM 2005 11 28 SB05151 120051122A21337110033 OUTFLOW VALVE BOEING737 7373B7 1384580NM CABIN PRESSURE FAULTY A USAAGB O2 MASK DEPLOYED EMER. DESCENT O OTHER CRCRUISE 1 EA19512AU4680646806 23595 THE AUTO PRESSURE CONTROL INOPERATIVE PER MEL 21-14A. AIRCRAFT LOST CABIN PRESSURE WITH OXYGEN MASKS DEPLOYING. CABIN WAS UNCONTROLLABLE IN ALL PRESSURIZATION MODES. DESCENDED TO 10,000 FT, CONTINUED TO CLT. LANDED, NO EMERGENCY DECLARED. CREW REPORTED OXYGEN MASKS AT SEAT 1DF, 3DF AND AFT LEFT LAV FLT ATTENDANT STATION DID NOT DEPLOY. REMOVED AND REPLACED AFT OUTFLOW VALVE. OPS CHECK NORMAL. PERFORMED SATISFACTORY PRESSURIZATION CONTROL CHECK. CLEARED MEL 21-14A. DROPPED OXYGEN MASK DOORS, THAT DID NOT DEPLOY. REPLACED ALL AFFECTED OXYGEN GENERATORS, REPACKED OXYGEN MASKS IN PSU'S. OPERATIONALLY CHECKED OXYGEN MASKS AND DOORS PER MM 35-22-00. OPERATIONAL CHECK GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F RTA16WE 20051128001332005112800133EU 2005 11 28 XN0A1277 120051116A2910 LINE AIRBUS300 A300B4203 3930306EU GREEN HYD SYS FAILED A XN0AD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 GL23474AS 219 DURING TAXI GREEN SYSTEM LOST. FOUND LT GEAR AFT OUTBOARD FLEXIBLE BRAKE HYDRAULIC LINE BLOWN. REMOVED AND REPLACED LT GEAR AFT OUTBOARD HYD LINE AS REQUIRED. SERVICED GREEN HYD SYSTEM HYDRAULICS AND ACCUMULATOR, OPS CHECKS GOOD. NO LEAKS NOTED IAW A300 AMM 32-00-00. 2L72 4F RTA35EU 20051128001342005112800134 2005 11 28 SWAA053718 420051121A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29630WN 27705 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051128001362005112800136 2005 11 28 SWAA053720 420051120A256563551 SLIDE BOEING737 7377H4 1384404NM L2 DOOR LOW A SWAAK NONE O OTHER ININSP/MAINT 1 SW29787SA 29812 L2 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATED OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20051128001382005112800138NM 2005 11 28 SWAA053701 120051121A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 277 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051128001402005112800140NM 2005 11 28 SWAA053703 120051121A531165C22908 FRAME BOEING737 7373H4 1384600NM BS 500B CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 20R. REPAIRED FRAME PER SWA EA. 2L72 4F RTA16WE 20051128001462005112800146NM 2005 11 28 SWAA053709 120051121A53116546529 BELTFRAME BOEING737 7375H4 138449DNM BS 482 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29512SW 24189 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE BELTFRAME CRACKED AT BS 482, STR 21L. REPAIRED BELTFRAME PER SWA EA. 2L72 4F RTA16WE 20051128001502005112800150SO 2005 11 28 C2XA05SH131 120051109A523014526324001 SUPPORT EMB 145 EMB145EP 3260221SO CARGO DOOR CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714945 145049 SHV - DURING C-CHECK, MAINTENANCE FOUND FS 68 CARGO DOOR ROD SUPPORT BRACKET(AFT SECTION) CRACKED. MAINTENANCE REPAIRED FS 68 (AFT SECTION) OF CARGO DOOR SUPPORT BRACKET IAW EC 5230-01123. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20051128001522005112800152SO 2005 11 28 C2XA05SH132 120051115A532014521700007 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713550 145575 SHV - DURING C-CHECK MAINTENANCE FOUND RT OMEGA BEAM WITH CORROSION AROUND NUTPLATE HOLE AT FRAME 23. MAINTENANCE REPAIRED RT OMEGA BEAM AT FRAME 23 IAW EMB 145 SRM 53-21-10 PARAGRAPH 6 FIGURE 205. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20051128001542005112800154NM 2005 11 28 QXEA200501544 120051120A242031708001A GENERATOR DHAV DHC8 DHC8202 2809007NM AC SYSTEM MALFUNCTIONED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09349PH137813089 486 BOI FLIGHT NR 2192, NR 1 AC GENERATOR CAUTION ILLUMINATED ON CLIMB. MAINTENANCE REPLACED NR 1 AC GENERATOR AND COMPLIED WITH FUNCTIONAL TEST IAW AMM 24-21-00, PAGES 401-403. OPERATIONAL CHECK AND LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051128001552005112800155NM 2005 11 28 ASAA0540428 120050822A57536546430184 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU TE FLAP PUNCTURED A ASAAK NONE F FLT CONT AFFECTED ININSP/MAINT 1 NM02779AS 25111 RT IB FORE FLAP LWR SKIN PUNCTURED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLERS IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051128001602005112800160NM 2005 11 28 ASAA0540432 120050823A524165535954 SEAL DEPRESSOR BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FWD GALLEY DR CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 FWD GALLEY DOOR CUTOUT FWD UPPER SEAL DEPRESSOR CRACKED. REMOVED AND REPLACED IAW EA. (K) 2L72 4F4 FRTA16WE E21EU 20051128001622005112800162NM 2005 11 28 ASAA0540498 120050922A531365353509 CLIP BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU BS 500C DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02793AS 28880 DAMAGED STRINGER CLIP AT FWD CARGO BAY. REMOVED AND REPLACED STRINGER CLIP IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051128001682005112800168SW 2005 11 28 YTRR106611 120051104A772212444412 INDICATOR BELL 206 206B3 1181506SW ALLSN 250C 250C20B 03013GL COCKPIT OUT OF TOLERANCEB YTRRK NONE O OTHER NRNOT REPORTED 1 SO012043B50 3355 TOT INDICATOR WOULD NOT CHECK OT DURING CALIBRATION CHECK. 1G71 3U3 U H2SW E4CE 20051128001742005112800174NM 2005 11 28 ASMF200510014 120051029A291366087 PUMP BOEING737 737* NM GE CFM56 CFM56* 13802NE LT HYDRAULIC SYSFAILED W ASMFD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SW23851AM5697 29363 CAPTAIN REPORTED LOSS OF HYDRAULIC FLUID IN LT SIDE. DURING REVISION DETECTED A LEAK IN LT MAIN PUMP, SO IT WAS REPLACED IAW MM 29-11-11 AC WAS DISPATCHED. AC RETURNED TO PLATFORM, DURING TAXING PSEU AND LT HYDRAULIC SYS LIGHTS TURNED ON. BREAKERS D1 AND D2 WERE RESEATED TURNING OFF PSEU LT AND HYDRAULIC PUMP WAS REPLACED, SHAFT DAMAGED; ADDITIONALLY THE LT A/C PACKAGE, PNEUMATIC APU WERE DEFERRED DUE TO CONTAMINATION. DURING OVERNIGHT, MAIN PUMP O-RING AND NIPPLE WERE REPLACED IAW MM 20-10-11 AND 20-50-1. THE FIM 21-00 PROCEDURE TASKS 801 TO 804 WERE PERFORMED IAW LT A/C PACKAGE CONTAMINATION. ADDITIONALLY THE APU, LT A/A PACKAGE AND PSEU WERE TESTED IAW MM 49-11-00, 21-00 AND FIM 32-09 TASK 801, ALL CORRECT.2L72 4F4 FRTA16WE E2GL 20051128001782005112800178SO 2005 11 28 CHQA20050192 120051105A335066367 WIRE EMB 145 EMB145LR 3260212SO LIGHT STRIP BROKEN A CHQAK NONE O OTHER ININSP/MAINT 1 GL11280SK 145381 AFT STRIP EMERGENCY FLOOR LIGHTING HAS BROKEN WIRES. REPLACED AFT EMERGENCY LIGHTING STRIP IAW MM 33-26-06. OPS TEST GOOD. 2L72 4T RTT00011AT 20051128001812005112800181NM 2005 11 28 QXEA200501542 120051119A213121178041 CONTROLLER DHAV DHC8 DHC8202 2809007NM CABIN PRESSURE MALFUNCTIONED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09351PH17321 490 PDX FLIGHT NR 2266, AFTER START WHEN BLEED FLOW CONTROL KNOB SELECTED TO 11 O`CLOCK POSITION OR HIGHER CABIN PRESSURIZES/DEPRESSURIZIES AT INCREASING RATES AND SPEEDS (500' UP/DOWN THEN 1000'). WHEN KNOB SELECTED TO MANUAL, AIRCRAFT PRESSURIZED AT 2000 FPM. MAINTENANCE REPLACED CABIN PRESSURE CONTROLLER IAW DASH-8 200 AMM 21-30-06, PAGES 401-404. STEP 4B ON PAGE 404. COMPLIED WITH FUNCTIONAL TEST OF THE PRESSURIZATION CONTROL SYSTEM IAW TASK 21-30-00-720-801. AIRCRAFT RETURNED TO SERVICE 2H72 4T RTA13NM 20051128001862005112800186NM 2005 11 28 05FDEA03932 120051121A5311 FRAME BOEING727 727227 1384078NM BS 560 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 FOUND FRAME DENT AT BS 560 ABOVE STR 24L. REPAIRED FRAME AT BS 560 STR 24L IAW SRM 51-40-3. 2L73 4F A3WE 20051128001912005112800191SO 2005 11 28 CHQA200500199 120051120A2840367934002 FUEL HEATER EMB 145 EMB145LR 3260212SO LT FUEL CELL INOPERATIVE A CHQAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL11262SK1381313813 145168 FLIGHT 3002 - PIT-BWI - WHILE IN CRUISE FLIGHT AT FL230, THE FUEL IMBALANCE LIGHT APPEARED AND THE LEFT FUEL TANK INDICATED 0 POUNDS. COMPLETED QRH CHECKLIST FOR FUEL IMBALANCE, DECLARED AN EMERGENCY WITH ATC. LANDED IN BWI WITHOUT INCIDENT. REMOVED AND REPLACED FUEL CONDITIONING UNIT IAW EMB 145 MM 28-41-01. OPS CHECK GOOD IAW MM 28-41-00. 2L72 4T RTT00011AT 20051128001942005112800194EA 2005 11 28 COMA0560631 120051121A3241 COMPUTER CNDAIRCL600 CL6002B19 1900309EA ANTI SKID SYS MALFUNCTIONED A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01446CA 7546 FLIGHT 5836 - DURING BOS APPROACH RECEIVED AN A/SKID CAUTION MESSAGE AFTER EXTENDING THE LANDING GEAR, APPROACH WAS ABORTED AND MESSAGE CLEARED AFTER 15 SECONDS. SECOND ATTEMPT WAS WITHOUT DIFFICULTY. PERFORMED AN OPERATIONAL TEST OF THE A/SKID SYSTEM, DISCREPANCY COULD NOT BE DUPLICATED. 2L72 4F RTA21EA 20051128002022005112800202WP 2005 11 28 05FDEA03934 120051122A5330 SKIN DOUG DC10 DC1010 3022110WP ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LOWER FUSELAGE ON SKIN PANEL FROM LONG LT TO LONG 48 RT: FOUND PITTING CORROSION BTW STA Y=1941 AND STA Y=1129. REMOVED CORROSION ON BELLY SKIN IAW SRM 51-21-01 PAR 33 PAG 26-27. REMOVED RESIDUAL CORROSION AND BLENDOUT AREA BTW LONG 50 TO LONG 50 IAW SRM 51-21-01 PAR 34. PERFORMED INSPECTION IAW NDI SPM 04. REPAIRED AREA IAW OUT OF LIMITS IAW SRM 53-40-00 FIG 14 VOL 1 AND IAW SRM 53-40-00 FIG 14 AND FIG 20 VOL 1. INSTALLED REPAIR CHANNEL, 13 AND FILLER IAW SRM 53-00-01 VOL1 FIG 7 AND FIG 9. 2L73 4F A22WE 20051128002042005112800204EA 2005 11 28 COMA0560624 120051119A27501217542 DRIVE SHAFT CNDAIRCL600 CL6002B19 1900309EA RT WING WORN A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01735CA8360 7267 FLIGHT 5404 - EN ROUTE PHL-CVG DURING APPROACH RECEIVED A FLAP FAIL CAUTION AT ZERO DEGREE FLAP POSITION. CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE RIGHT WING FLEX DRIVE SHAFT. 2L72 4F RTA21EA 20051128002052005112800205EU 2005 11 28 AWXA200501424 120051120A3350321431 BATTERY AIRBUS320 A320231 3930325EU EMERGENCY LIGHT INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28637AW 099 LAS - EEL - DURING OVERNIGHT INSPECTION DISCOVERED THE EMERGENCY EXIT LIGHT BATTERY, AT ROW 11R, WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT BATTERY AT ROW 11R. OPERATIONAL TESTS WERE GOOD. 2L72 4F RTA28NM 20051128002082005112800208NM 2005 11 28 AWXA200501431 120051027A5320654797380 FLOOR SUPPORT BOEING737 7373S3 1384711NM BS 639 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 MCN - DURING C13 CHECK DISCOVERED CRACK, 2.0 INCHES IN LENGTH, ON THE LT SIDEWALL FLOOR SUPPORT ANGLE AT BS 639, WL 208 AND BL 60L. MAINTENANCE REMOVED FLOOR SUPPORT ANGLE AT BS 639 AND BL 60L IAW BOEING 737-300 51-40-02-0G. FABRICATED SPLICE STRAP AND SPLICE CHANNEL IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5360-05321-ES1. INSTALLED REPAIR PARTS AT BS 639, WL 208 AND BL 60L IAW AWA ER NR 03-5360-05321-ES1. 2L72 4F RTA16WE 20051128002102005112800210SO 2005 11 28 CHQA200500197 120051116A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11570RP 14500821 RIGHT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RIGHT HAND EXTERIOR EMERGENCY LIGHT LOWER. OPS CHECK GOOD IAW EMB 145 MM 33-50-01. 2L72 4T RTT00011AT 20051128002142005112800214WP 2005 11 28 IXXA05RNG104S 120050910A5730 SKIN DOUG DC8 DC872 302199BWP STA XW565 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK, FOUND A CORROSION ON LT WING OUTBOARD AILERON LWD SKIN, STA XW 565 TO XA 638. SKIN IN LT WING OUTBOARD AILERON WAS REMOVED AND REPLACED IAW DRAWING 5763133 AND RIVETS WERE INSTALLED IAW DC8 SRM 51-1-21 PAGE 1-7. 2L74 4F RT4A25 20051128002162005112800216WP 2005 11 28 IXXA05RNG106S 120050913A5730 SKIN DOUG DC8 DC872 302199BWP STA XW31-XW92 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK, FOUND TWO IMPROPER PATCHES AND CORROSION ON RT WING INBOARD FLAP TOP SURFACE, STA XW 31 - XW 92. SKIN ON RT WING INBOARD FLAP WAS REPLACED IAW DOUGLAS DRAWING 5642960 AND RIVETS WERE INSTALLED IAW DC8 SRM 51-1-21 PAGE 1-7. 2L74 4F RT4A25 20051128002212005112800221 2005 11 28 SWAA053712 420051120A25656949956 CABLE BOEING737 7375H4 138449DNM R2 DOOR SLIDE MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29526SW 26568 DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE LATCH CABLE ASSY MISROUTED. REROUTED CABLE ASSY PER MM. 2L72 4F RTA16WE 20051128002222005112800222 2005 11 28 SWAA053713 420051120A25656949956 CABLE BOEING737 7375H4 138449DNM L2 DOOR SLIDE MISROUTED A SWAAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW29526SW 26568 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE LATCH CABLE ASSY MISROUTED. REROUTED CABLE ASSY PER MM. 2L72 4F RTA16WE 20051128002232005112800223NM 2005 11 28 SWAA053714 120051121A53116546539 FRAME BOEING737 7373H4 1384600NM BS 616 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, RBL 65, WL 201. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20051129000172005112900017CE 2005 11 29 DXTA200501094 120051120A2910AE1011923410152 HOSE CESSNA750 750 2076810CE HYD SYSTEM BLOWN E DXTAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL07935QS 7500135 PASSING THRU FL300 AMBER "HYD VOL LOW A" MESSAGE ILLUMINATED, FOLLOWED BY "HYD PUMP FAIL A" AND HYD PTU FAIL' MESSAGES. HYD QTY SHOWED 0%. APPROPRIATE CHECKLIST COMPLETED. AIRCRAFT LANDED. USING EMERGENCY BRAKES. AFTER LANDING LARGE QTY OF CLEAR HYD FLUID NOTED ON BELLY OF AIRCRAFT. - INSTALLED NEW PTU PRESSURE HOSE & REPLACED HYDRAULIC MANIFOLD UPPER PLUG O-RING. BLED / SERVICED 'A' SYSTEM HYDRAULICS IAW CE 750 MM 12-10-15. OPERATIONAL & LEAK CHECKS GOOD. 2L72 4J RTT00007WI 20051129000182005112900018NM 2005 11 29 05FDEA03924 120051120A7932 ENGINE BOEING727 727200 138407ENM NR 3 MALFUNCTIONED A FDEAE ENGINE SHUTDOWN O OTHER CLCLIMB 1 SO25482FE 21464 ON CLIMBOUT NR 3 ENG OIL PRESS WENT TO 30PSI AND OIL T EMP WENT TO 130C. SHUT DOWN ENG NR 3 IAW QRH AND RETURNED TO MEMPHIS. ACCOMP ENG WINDMILLING CK AND R&R OIL FILTER PER M/M 72-00-00, PG 531. RAN ENG AND OPS CKS GOOD AT IDLE. ADJ OIL PRESS RELIEF VALVE PER M/M 79-34-01. TOOK ACFT TO HIGHPOWER AND ALL OPS CK'D GOOD. 2L73 4F RTA3WE 20051129000192005112900019 2005 11 29 QXEA200501543 420051121A34607000700976 DADC DHAV DHC8 DHC8202 2809007NM COCKPIT MALFUNCTIONED A QXEAA UNSCHED LANDING O OTHER APAPPROACH 1 NM09375PH15818151 529 PDX FLIGHT NR 2148, AIII FAILED THREE TIMES, DURING TWO APPROACHES IN SEA AND ONCE PDX 10R. APPROACH WARN FOLLOWED BY NO AIII AND A HEADING FLAG. MAINTENANCE REPLACED NR 1 DADC AND PERFORMED OPERATIONAL TEST IAW MTC 9340014, 53450001, 9344002 AND 934101. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051129000212005112900021NM 2005 11 29 SWAA053750 120051122A53306545766 SKIN BOEING737 7373H4 1384600NM BS 480 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29327SW 23691 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 480, STR 16R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051129000292005112900029NM 2005 11 29 SWAA053758 120051122A55236545166 LINK BOEING737 7373H4 1384600NM LT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29392SW 27379 DURING SCHEDULED C3 CHECK, LT ELEVATOR TAB FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR TAB FWD SUPPORT LINKS AND HARDWARE PER MM. 2L72 4F RTA16WE 20051129000312005112900031NM 2005 11 29 SWAA053760 120051122A3350BR2013 LIGHT BOEING737 7373H4 1384600NM CABIN DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29398SW 27692 DURING SCHEDULED RON CHECK, FOUND FWD END OF EEPLS STRIP DAMAGED. REMOVED AND REPLACED STRIP PER MM. 2L72 4F RTA16WE 20051129000332005112900033NM 2005 11 29 SWAA053762 120051127A532269353656 SHEAR TIE BOEING737 7375H4 138449DNM BS 360 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29512SW 24189 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 360, STR 14R TO STR 15R. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051129000352005112900035 2005 11 29 SWAA053717 420051121A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29625SW 27701 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051129000572005112900057NM 2005 11 29 AWXA200501437 120051108A5315D53472090011 FLOORBEAM AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28813AW 1223 DURING BC4 CHECK DISCOVERED EXFOLIATION CORROSION ON FLOORBEAM AT FS 66-3 AND -Y765. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 319 SRM 53-00-14. MAINTENANCE REMOVED BEAM FROM FS 64 TO FS 66 IAW AIRBUS 319 SRM 51-42-11. RECEIVED NEW BEAM SECTION AND INSTALLED FROM FS 64 TO FS 66, Y1292 IAW AIRBUS 319 SRM 51-42-11. 2L72 4F RTA28NM 20051129000582005112900058NM 2005 11 29 AWXA200501438 120051108A5321D5367228500000 FLOOR PANEL AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28813AW 1223 SAL - DURING BC4 CHECK DISCOVERED GALVANIC CORROSION ON 131CG FORWARD CARGO COMPARTMENT FLOOR PANEL UPPER SURFACE FROM FS 28 TO FS 31 AND FROM Y765 TO -Y765. MAINTENANCE REMOVED AND REPLACED CARGO COMPARTMENT FLOOR PANEL WITH NEW PANEL IAW IRM 9701 REV F. 2L72 4F RTA28NM 20051129000592005112900059NM 2005 11 29 AWXA200501439 120051026A575165C2591118A SKIN BOEING737 7373S3 1384711NM RT AILERONS DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 MCN - DURING C13 CHECK DISCOVERED PLIES SEPARATED ON LOWER SURFACE OF THE RT AILERON AT HINGE ACCESS PANEL. UNABLE TO REPAIR AILERON DUE TO NON-DESTRUCTIVE INSPECTION REQUIREMENTS NOT AVAILABLE AT MCN STATION. MAINTENANCE REMOVED AND REPLACED THE RT AILERON IAW AMERICA WEST AIRLINES TASK CARD R3M27015. 2L72 4F RTA16WE 20051129000602005112900060NM 2005 11 29 AWXA200501440 120051108A5315D53472172204 FLOORBEAM AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28813AW 1223 SAL - DURING BC4 CHECK DISCOVERED EXFOLIATION CORROSION ON FLOORBEAM AT FS 66+7 AND Y1292. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 319 SRM 53-00-14. MAINTENANCE REMOVED BEAM FROM FS 66 TO FS 68 IAW AIRBUS 319 SRM 51-42-11. RECEIVED NEW BEAM SECTION AND INSTALLED FROM FS 66 TO FS 68, Y1292 IAW AIRBUS 319 SRM 51-42-11. 2L72 4F RTA28NM 20051129000612005112900061EU 2005 11 29 10152005A 120051012A3320BA08006281 INVERTER SAAB SF340 340B 7860101EU CABIN LIGHTS FAILED A NSVAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA27239CJ 239 FOUND STRONG ELECTRICAL BURNING SMELL COMING FROM FLIGHT ATTENDANT LIGHTING CONTROL PANEL. REMOVED FLIGHT ATTENDANT PANEL AND FOUND NO EVIDENCE OF BURNING. REINSTALLED AND TURNED ON FOR 5 MIN. COULD NOT DUPLICATE PROBLEM. INSPECTED AND FOUND TO BE SEAT 2A WINDOW LIGHT CAUSING SMOKE AND ODOR IN CABIN. REMOVED LIGHT, DEFERRED IAW MEL 33-20-1 CABIN LIGHT CAT "C" ID NR 15926 PER MX CONTROL. ON 10/13/2005 MECHANICS REMOVED AND REPLACED WINDOW LIGHT INVERTER PN BA 08006-28-1 SN NSN, BUT THE SOCKET NEEDS TO BE REPLACED PART ON ORDER 6500111. MEL REMAINS OPEN. MEL C/W ON 10/18/2005 REPLACED SEAT 2A FWD FITTING PN 6500111, OPS CHECK GOOD. 2L72 4T RTA52EU 20051129000622005112900062EU 2005 11 29 10152005B 120051010A612078249052 PCU SAAB SF340 340B 7860101EU PROPELLER MALFUNCTIONED A NSVAC ABORTED TAKEOFF O OTHER TXTAXI/GRND HDL 1 EA27194CJ 194 LT TQ GAUGE READS ZERO. CREW ABORTED TAKEOFF, LEFT BOTTOM GOVERNOR ENGAGES INTERMITTENTLY. LEFT TQ GAUGE SHOWS NORMAL AS WELL AS NP LEFT AC GEN LIGHT ILLUMINATED TO VERIFY NEG BG ENGAGEMENT. "SUPP-CLOSED" PERFORMED MASTER RIGGING ON LT ENG AND FOUND PCU WOULD NOT COME OUT OF FEATHER. REMOVED AND REPLACED PCU ON LT ENG, PN ON/OFF 782490-52 SN ON 900430, SN OFF 900433. 2L72 4T RTA52EU 20051129000632005112900063CE 2005 11 29 10172005A 120051014A261247790005 FIRE DETECTOR BEECH 1900 1900D 1154162CE RT NACELLE MALFUNCTIONED A NSVAO OTHER O OTHER TXTAXI/GRND HDL 1 EA27124CJ UE24 RT FIRE LOOP STUCK IN TEST MODE. INSPECTED FIRE LOOP NO DEFECTS FOUND, INSPECTED CONTROLLER AND C/B, NO DEFECTS NOTED, DISCONNECTED LOOP AT FIREWALL, FIRE LOOP LIGHT REMAINED ON, RECONNECTED LOOP AT FIREWALL LIGHT REMAINED ON. FOUND FIRE DETECTION CONTROL BOX BAD REPLACED IT WITH NEW ONE PN ON/OFF 477-90005, SN ON 9235-001 SN OFF 8416-011. 2L72 4T RTA24CE 20051129000642005112900064NM 2005 11 29 PIDA20050194 120051122A5330 SKIN BOEING737 7373G7 1384595NM BS 727D-727E CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05380WL 23218 DURING "A" CHECK, FOUND CRACK IN FUSELAGE SKIN JUST BELOW STR 22RT BETWEEN BS 727D AND BS 727E. 2L72 4F RTA16WE 20051129000652005112900065EA 2005 11 29 COMA0560633 120051122A3260750005000 VALVE CNDAIRCL600 CL6002B19 1900309EA MLG FAULTY A COMAO OTHER K FLUID LOSS APAPPROACH 1 SO01982CA21512 7168 FLIGHT 5082- EN ROUTE AZO-CVG, RECEIVED A MLG DISAGREE CAUTION CAUTION WHEN GEAR WAS SELECTED DOWN, CREW DECLARED AN EMERGENCY AND PERFORMED ACTUATION OF THE MANUAL GEAR RELEASE HANDLE. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE MLG SELECTOR. 2L72 4F RTA21EA 20051129000672005112900067EA 2005 11 29 QXEA200501554 120051117A80104120T06P02 STARTER CNDAIRCL600 CL6002C10 1390015EA NR 2 ENGINE INOPERATIVE A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09606QX5159 10023 PDX - ON FLIGHT 2451, RETURNED TO THE GATE WITH NR 2 ENGINE HUNG START. MAINTENANCE REPLACED THE NR 2 STARTER AND VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20051129000702005112900070NM 2005 11 29 UPS05245822 120051012A574065159682A SUPPORT FITTING BOEING727 72730C 1384009NM CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 RT WING FRONT SPAR TO BODY FITTING HAS SUSPECT CRACK ON OUTBD SIDE OF BOTTLE PIN. FITTING REPLACED IAW DWG 65C13724 AND UPS EO B727-5310-7477. 2L73 4F A3WE 20051129001092005112900109NM 2005 11 29 PIDA20050193 120051122A5330 LAP JOINT BOEING737 7373G7 1384595NM BS 440 CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05380WL 23218 DURING "A CHECK, FOUND CRACK ABOVE STR 10 RT SKIN LAP JUST AFT OF BS 440. 2L72 4F RTA16WE 20051129001112005112900111NM 2005 11 29 SWAA053781 120051124A53306545768 SKIN BOEING737 7373Q8 1384670NM BS 328 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 328, STR 17R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051129001132005112900113NM 2005 11 29 2005UALA01250 120051108A335078941 LAMP BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29786UA 26938 EMERGENCY WHITE AISLE LIGHT INOP AT SEAT 35G. SUPPLEMENTAL DATA UPDATE REPLACED LAMP. 2L72 4F4 FRTT0001SE E46NE 20051129001152005112900115NM 2005 11 29 2005UALA01264 120051112A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE AFT GALLEY DOOR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29328UA 24148 AFT GALLEY DOOR LWR HINGE CUTOUT IN FUSELAGE LWR FWD EDGE CRACKED. DATA REMOVED CRACK FABRICATED DOUBLER AND TRIPLER PER SRM 53-60-01. 2L72 4F4 FRTA16WE E2GL 20051130000082005113000008NM 2005 11 30 05FDEA03965 120051127A5754 SKIN DOUG MD11 MD11 3023602NM ZONE 600 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 RIGHT WING - NR 5 SLAT LEADING EDGE FOUND DENTED. TRIMMED OUT AND REPAIRED AS PER SRM 57-10-00. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051130000142005113000014WP 2005 11 30 05FDEA03971 120051128A5320 REPAIR DOUG DC10 DC1010 3022110WP FUSELAGE PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 CENTRAL CARGO COMPT FOUND REPAIR DOUBLER ON JUMB DOOR AT STA 1701 X-102 Z-46 RT SIDE. STRIPPED PAINT FROM DOUBLER IAW SRM 51-21-01, PERFORMED NDI AND GVI. THE REPAIR REWORKED IAW SRM 53-50-00 FIG 12 VOL 1. REPROTECTED AREA IAW SRM 51-21-01 PAR 2 AND THE REPAIR FOUND IN COMPLIANCE WITH SRM 53-50-00 FIG 12 VOL 1. 2L73 4F A22WE 20051130000172005113000017WP 2005 11 30 05FDEA03974 120051128A5730 SKIN DOUG DC10 DC1030 3023501WP RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 RT WING TIP WING CRACKED 1 INCH LONG ON LOWER SKIN. TRIMMED OUT CRACK, INSTALLED FILLER AND DOUBLER IAW SRM 57-00-01 FIG 4 AND SRM 51-35-01 PG 1/13. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F160709/N00709 IAW SRM 57-00-01 FIG 4. 2L73 4F A22WE 20051130000192005113000019WP 2005 11 30 05FDEA03976 120051128A5753 REPAIR DOUG DC10 DC1030 3023501WP LT WING FLAP PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 LT WING OUTBOARD FLAP LOWER SKIN FOUND DOUBLER 35.50 X 4.50 INCHES XOF 462. PERFORMED A GVI OF REPAIR IAW SRM 57-10-00 FIG 9 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 E3. 2L73 4F A22WE 20051130000212005113000021WP 2005 11 30 05FDEA03978 120051128A5330 REPAIR DOUG DC10 DC1030 3023501WP BS 304-357 PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 TWO EXTERNAL DOUBLERS ON LT NOSE SKIN FROM STA 304 TO STA 357 Z-15. PERFORMED AN INSPECTION ON REPAIR IAW SRM 53-00-02 VOL 1 FIG 5 SHT 12 AND 14 WAVINESS CONDITION IS WITHIN LIMITS IAW SRM 53-00-02 VOL 1 PG 4A PAR 5 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001-P1 E3. RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VOL 2 PAR 33. 2L73 4F A22WE 20051130000222005113000022WP 2005 11 30 05FDEA03979 120051128A5730 REPAIR DOUG DC10 DC1030 3023501WP RT WING PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 RIGHT WING LOWER SURFACE FOUND DOUBLER REPAIR ON PANEL 8 X 5 INCHES. PERFORMED INSPECTION TAP TESTING, NO DELAMINATION FOUND IAW SRM 51-61-01 VOL 2 AND PERFORMED INSPECTION ON REPAIR IAW SRM 57-71-00 VOL 2 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001-2P E3. 2L73 4F A22WE 20051130000272005113000027CE 2005 11 30 DXTA200501103 120051123A329766187046 PCB CESSNA560 560XL 2076702CE MLG MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07692QS4853 5605092 AFTER TAKEOFF GEAR UNLOCK LIGHT WOULD NOT EXTINGUISH, ALSO HYD PRESS LIGHT STAYED ON. SHORTLY AFTER STAB MIS COMP LIGHT ALSO CAME ON. GEAR AND FLAPS EXTENDED NORMAL AND WITH GEAR DOWN ALL LIGHTS EXTINGUISHED. INSPECTED, CLEANED AND OHMED WIRES PR034 TO PR002, PLO35 TO JL003, PL000 TO PL0032, JL003 TO PL037. NO FAULTS FOUND, ALL OPS CHECK PASS AT THIS TIME. GAINED ACCESS TO GEAR LOGIC PCB BOARD AND INSPECT, RERACKED WITH NO VISUAL DAMAGE NOTICED AT THIS TIME. CYCLED GEAR SEVERAL TIMES WITH THE FAULT UNLOCK LT ON AND HYD PSI LIGHT ON INTERMITTENTLY. PCB LANDING GEAR P/N 6618704-6 REPLACED. 2L72 4F RTA22CE 20051130000292005113000029CE 2005 11 30 DXTA200501104 120051123A2120 INTAKE DUCT RAYTHNDH125 HAWKER800XP 7150012CE CABIN AIR CONTAMINATED E DXTAGA O2 MASK DEPLOYED UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL07815QS 258705 COCKPIT AND CABIN FILLED WITH SMOKE UPON ROTATION AT TAKEOFF. INSPECTED ACFT TO INCLUDE BOTH ENGS, ALL GEAR WELLS, INSIDE RADOME -HELL HOLE- COCKPIT & CABIN WITH NO DISCREPANCIES. HOWEVER DEICING FLUID WAS FOUND PUDDLED IN THE AIR INLET DUCT FOR THE APU. TROUBLESHOT AND CONCLUDED THAT DEICING FLUID INGESTION THROUGH THE APU AIR INLET LOC LT AFT AIRCRAFT ABOVE NR 1 ENG, WAS THE CAUSE OF THE SMOKE IN THE AIRCRAFT. CLEANED INLET DUCT AND INLET TURBINE THOROUGHLY AND RAN APU FOR APPROXIMATELY 1 HOUR WITH HEAT AND BLEED ON. NO DISCREPANCIES NOTED. PERFORMED ENG RUNS WITH APU ON, BLEEDS ON. NO DISCREPANCIES NOTED. ALL FUNCTIONAL CHECKS GOOD AT THIS TIME. REF H800XP MM 49-11-00. 2L72 4F RTA3EU 20051130000322005113000032NM 2005 11 30 05FDEA03960 120051125A3230 RELIEF VALVE DOUG MD11 MD11 3023602NM TRIM CYLINDER LEAKING A FDEAA UNSCHED LANDING K FLUID LOSS CLCLIMB 1 SO25593FE 48551 AFTER T/O GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. GROUND SENSOR WAS NOT A FACTOR SINCE PRESSURIZATION WAS NORMAL AND A/P ENGAGED. CONSULTED QRH BUT DID NOT USE THE HANDLE RELEASE BUTTON PER MOCC. RETURNED TO DEL. INSPECTION FOUND FLUID DRIPPING FROM TRIM CYLINDER PRESS RELIEF VALVE ON RIGHT L/G. REMOVED AND REPLACED AS PER AMM-32-37-03-4. ADJ/TEST & OPS TEST OF TRUCK BEAM TRIM INTERLOCK CYLINDER C/O SATIS AS PER AMM-32-37-00-5. GEAR HANDLE MOVEMENT CHECKED SATIS VIA USE OF OVERRIDE BUTTON WITH GEAR PINS INSTALLED. SATIS INTERACTION WITH INTERLOCK CYLINDER. HYD SYS NR 3 RESERVICED TO FULL. RETURNED TO SERVICE. 2L73 4F RTA22WE 20051130000342005113000034NM 2005 11 30 05FDEA03962 120051126A5270 SWITCH BOEING727 727200 138407ENM AIRSTAIR DOOR MALFUNCTIONED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25288FE 21850 AMBER AFT AIRSTAIR LIGHT ILLUMINATED DURING CLIMB THROUGH 27,000 MSL. ACCOMPLISHED QRH. LANDED UNEVENTFULLY. OPENED AFT AIRSTAIRS, CLEANED SWITCHES, AND CHECKED DOOR WARNING SYSTEM PER M/M 52-70-001-5. OPS CHECKS NORMAL. OK FOR SERVICE. 2L73 4F RTA3WE 20051130000392005113000039NM 2005 11 30 CALA0500418 120051128A5315146N5089 FLOORBEAM BOEING757 757224 1384958NM BS 1640 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713113 27555 INSPECTION FOUND UPPER AND LOWER SURFACE OF FLOORBEAM CORRODED AT STA 1640, RBL 8. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51. 2L72 4F RTA2NM 20051130000462005113000046SO 2005 11 30 RAIA00511029 120051121A3230 LANDING GEAR EMB 145 EMB145LR 3260212SO MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03810HK 145231 FLT 3553 - LGA - LANDING GEAR FAILS TO RETRACT INFLIGHT. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE LANDING GEAR EXTENSION AND RETRACTION SYSTEM. NO DEFECTS NOTED. 2L72 4T RTT00011AT 20051130000482005113000048SO 2005 11 30 RAIA00511031 120051124A3350 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03822HK 145069 PREFLIGHT - STL - EMERGENCY EXIT OVER SERVICE DOOR INOP. MAINTENANCE REMOVED AND REPLACED THE LIGHT BULB. 2L72 4T RTT00011AT 20051130000552005113000055NM 2005 11 30 72000002 120051123A2740 JACKSCREW BOEING727 727200 138407ENM STABILIZER JAMMED A K11ABLA EMER. DESCENT ABORTED APPROACH UNSCHED LANDING E VIBRATION/BUFFET DEDESCENT 1 GL23720CK 21298 STRONG SHUDDER IN AIRCRAFT, TRIM THEN RAN AWAY. SHUDDER LASTED FOR APPROX 10-15 SECONDS. TRIM THEN JAMMED BUT WAS MANUALLY OPERATIONAL AFTER PROCEDURES. EMERGENCY LANDING, DIVERTED FROM ROC TO SYR DUE TO WEATHER. 2L73 4F RTA3WE 20051130000562005113000056NM 2005 11 30 PCSA11250501 120051125A7312320115 FUEL HEATER BOEING727 727212 138407GNM ZONE 400 FAILED A PCSAEF ENGINE SHUTDOWN ACTIVATE FIRE EXT. MJ OVER TEMP WARNING INDICATION DEDESCENT 1 SO29598AJ 21947 AT TOP OF DESCENT NR 2 ENGINE OIL TEMP BEGAN TO RISE, NR 2 FUEL HEAT VALVE WAS STUCK OPEN. NR 2 ENGINE FUEL HEAT VALVE WAS CYCLED, BUT WOULD NOT CLOSE, OIL TEMP WENT INTO RED 175 DEG, COULD NOT BE DECREASED, OIL PRESSURE NORMAL. DURING NORMAL ATTEMPT TO SHUT NR 2 ENGINE DOWN, INDICATIONS WERE NR 2 ENGINE WAS NOT SHUTTING DOWN. NR 2 ENGINE FIRE HANDLE WAS PULLED. T/S NR 2 ENGINE FUEL HEAT VALVE, VALVE FAILED. REMOVED & REPLACED NR 2 ENGINE FUEL HEAT VALVE, OPS CHECK NORMAL. NR 2 ENGINE MAIN OIL FILTER REMOVED & INSPECTED, NO CONTAMINATION FOUND. ENGINE RUN AND LEAK CHECK WAS ACCOMPLISHED, LEAK CHECK GOOD. ENGINE NR 2 FUEL CUT-OFF LEVER WORKING NORMAL. AIRCRAFT RETURNED TO SERVICE. 2L73 4F A3WE 20051130000622005113000062NE 2005 11 30 2005UALA01301 220051120A7200 ENGINE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 1 SURGES A UALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 WP29407UA 456 V10372 RETURNED TO FIELD AFTER THE NR 1 ENGINE SURGED. ECM SHOWS NO RECORD OF A SURGE/STALL. EEC/FADEC RECORDED NO STALL MESSAGE. FMU WAS REPLACED FOR N1 OVER SPEED AND CHANNEL B FAULT. FMU TEST SHOWS NO FAULT FOUND. CAUSE OF SURGE CAN NOT BE DETERMINED. 2L72 4F4 FRTA28NM E40NE 20051130000642005113000064 2005 11 30 2005UALA01303 420051120A2565 SLIDE AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE DOOR 1L LOW A UALAK NONE O OTHER ININSP/MAINT 1 WP29844UA 1581 DOOR SLIDE PRESSURE LOW AT DOOR 1L. SLIDE PACK ASSY FELL APART IN CONTAINER. MR TIME DATED 20SEP2005 SHOWED THAT ACFT-4044 HAD MR25611-109 INSTALLED ON 1L. MR25611-109 HAD BEEN SCHEDULED TO BE REMOVED DUE TO TIME ON 19NOV2005. MRTIME DATED 28NOV2005 AND 23DEC2005 SHOW THAT 1L DOOR HAS MR25611-1086 INSTALLED. BASED ON MR TIME DATA, THE SLIDE WITH LOW BOTTLE PRESSURE (MR25611-109) IS ALSO DUE FOR REMOVAL DUE TO SERVICE LIFE LIMIT. THE PROBABLE CAUSE FOR SLIDE FALLING APART IS THE BREAKAGE OF THE THIN FRANGIBLE WIRE THAT HOLDS THE PACK TOGETHER. THIS WIRE IS SUPPOSED TO BREAK, BY DESIGN. THIS IS WHY THE AMM HAS PRECAUTIONS TO AVOID ABRUPT MOVEMENT DURING SLIDE HANDLING AND REMOVAL/INSTALLATION. 2L72 4F4 FRTA28NM E40NE 20051130000662005113000066NM 2005 11 30 2005UALA01305 120051120A5730 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE RT WING LE BIRD STRIKE A UALAK NONE O OTHER ININSP/MAINT 1 WP29525UA 24978 BIRD STRIKE TO RIGHT OUTBOARD WING L/E. REPAIRED NR 10 LE SLAT NOSE SKIN PER SRM 57-43-01. 2L72 4F4 FRTA2NM E17NE 20051130000692005113000069NM 2005 11 30 2005UALA01308 120051120A3350 FUSE BOEING747 747422 1384935NM PWA 4056 PW4056 NE POWER SUPPLY FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29179UA 25158 LEFT OVERWNG BODY FAIRING EMERGENCY LIGHTS INOP, 2 AFT ASSY'S. REPLACED FUSE IN PWR SUPPLY. 2L74 4F4 FRTA20WE E24NE 20051130000702005113000070NM 2005 11 30 2005UALA01309 120051121A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE COCKPIT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29179UA 25158 COCKPIT EMERGENCY LIGHT INOP. REPLACED LAMP. 2L74 4F4 FRTA20WE E24NE 20051130000742005113000074NM 2005 11 30 2005UALA01314 120051121A5310 CREASE BEAM BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29922UA 26642 AFT CABIN FLOOR CREASE BEAM CORRODED UNDER SCUFF PLATE & DRAIN GUTTER AT NUT PLATES AT DOOR 2L. INST'D DOUBLER REPAIR FROM STA 967 TO 980 STR 17L, LBL 55" PER SRM 51-70-11 2L72 4F4 FRTA16WE E21EU 20051130000762005113000076NM 2005 11 30 2005UALA01316 120051121A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29552UA 26641 CABIN FLOORBEAM CRACKED UPPER FLANGE FWD SIDE, LBL 26. 2L72 4F4 FRTA2NM E17NE 20051130000782005113000078EU 2005 11 30 2005UALA01319 220051120A7200 ENGINE BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU RIGHT FLAMED OUT A UALAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION NRNOT REPORTED 1 WP29312UA 23673 720431 RIGHT ENGINE FLAMED OUT AFTER STALL. ACCOMPLISHED ENGINE TROUBLESHOOTING PER AMM71-00-02 WITH NO FAULTS FOUND. REPLACED MAIN ENGINE CONTROL (MEC) AND FUEL PUMP AS PRECAUTION. SHOP FINDINGS ON FUEL PUMP AND MEC FUEL PUMP BENCH TEST FOUND NO FAULTS. MEC BENCH TEST FOUND TACHOMETER SHIFTED. THIS CONDITION CAUSES VSV AND TURBINE CLEARANCE TO BE OUT OF LIMITS. THIS CAN HAVE AN EFFECT ON COMPRESSOR PERFORMANCE AND CAN CONTRIBUTE/CAUSED ENGINE SURGE, N2 ROLL BACK AND ENGINE FLAME OUT. 2L72 4F4 FRTA16WE E21EU 20051130000852005113000085NM 2005 11 30 2005UALA01326 120051122A5311 FRAME BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU BS 867 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29922UA 26642 CABIN FRAME CRACKED STA 867 BETWEEN STRINGERS 8 - 9 RIGHT AT PSU ATTACH. MAJOR REPAIR ACP'D PER MM 53-10-84 REPAIR III. 2L72 4F4 FRTA16WE E21EU 20051130000862005113000086EA 2005 11 30 QXEA200501562 120051125A3260521621 TARGET CNDAIRCL600 CL6002C10 1390015EA MLG OUT OF ADJUST A QXEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM09606QX 10023 PDX - ON FLIGHT 2451 LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. PROX SYSTEM 1 FAULT WAS SHOWN. AIRCRAFT RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE ADJUSTED THE NOSE GEAR PROX SENSOR TARGET PX08. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2L72 4F RTA21EA 20051130000872005113000087NM 2005 11 30 2005UALA01327 120051122A5311 FRAME BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU BS 867 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29922UA 26642 CABIN FRAME CRACKED STA 867 BETWEEN STRINGERS 8 - 9 LEFT AT PSU ATTACH. MAJOR REPAIR ACP'D PER MM 53-10-84 REPAIR III. 2L72 4F4 FRTA16WE E21EU 20051130000922005113000092NM 2005 11 30 2005UALA01332 120051122A3230 LANDING GEAR BOEING757 757222 1384956NM PWA 2037 PW2037 NE NOSE MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29589UA 28707 RETURNED TO SFO DUE TO NOSE GEAR RETRACTION PROBLEM. REPLACED NOSE LANDING GEAR LOCK ACTUATOR. OPS CHECK OK. 2L72 4F4 FRTA2NM E17NE 20051130001012005113000101EA 2005 11 30 SWIA200515886 120051122A2730 SENSOR CNDAIRCL600 CL6002C10 1390015EA ELEVATOR OUT OF ADJUST A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07707SK 10003 INTERMITTENT ELEVATOR SPLIT CAUTION MESSAGE. ADJUSTED LT ELEVATOR POSITION SENSOR IAW AMM 27-34-10-400. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051130001042005113000104EA 2005 11 30 SWIA200515889 120051118A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLT SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 NM07962SW 7859 SPOILERON FAULT STATUS MSG ON APPROACH TO SLC. REPLACED LEFT SPOILERON OUTBOARD PCU IAW MM 27-62-01. OPERATIONAL CHECK GOOD. P/N ON 27000-7, OFF 7750. 2L72 4F RTA21EA 20051130001062005113000106EA 2005 11 30 SWIA200515891 120051121A3350 LAMP CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07706SK 10149 EMERGENCY LIGHT PAST EXIT SIGN OUT. RELAMPED LIGHT IAW MM 33-51-09, LIGHT OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051130001092005113000109SO 2005 11 30 SWIA200515894 120051117A2611 SMOKE DETECTOR EMB 120 EMB120ER 3260203SO MALFUNCTIONED A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07291SW 120318 SMOKE DETECTOR INTERMITTENTLY ALARMS WITH NO SMOKE PRESENT. REPLACED SMOKE DETECTOR BATTERY AS REQUIRED. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20051130001122005113000112EA 2005 11 30 SWIA200515897 120051114A274170623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA PITCH TRIM MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION DEDESCENT 1 NM07945SW4217 4217 7770 DURING DESCENT AP PITCH TRIM CAUTION MESSAGE CAME ON FOLLOWED BY STAB CH 1 STATUS MESSAGE. REPLACED HSTA & MOTOR CONTROL UNIT PER MM 27-42-01. OPERATIONAL CHECK GOOD. P/N: 8396-3, S/N OFF: 1036. 2L72 4F RTA21EA 20051130001132005113000113EA 2005 11 30 SWIA200515898 120051118A2751855D10011 SENSOR CNDAIRCL600 CL6002B19 1900309EA BRAKE POSITION MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07447SW 7677 FLAPS FAIL CAUTION MESSAGE APPEARED IN CRUISE. REPLACED RIGHT FLAP BRAKE POSITION SENSOR IAW MM 27-51-10. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051130001152005113000115EA 2005 11 30 SWIA200515900 120051118A5610 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAO OTHER O OTHER CRCRUISE 1 NM07954SW 7815 CAPTAIN SIDE WINDSHIELD CRACKED AT FL360. INSTALLED SERVICEABLE CAPTAIN'S WINDSHIELD ASSY PER CRJ 200 MM 56-00-00, 56-11-01, 56-12-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051130001172005113000117SO 2005 11 30 RAIA00511027 120051122A3350 LAMP EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03838HK 145321 PREFLIGHT - IAD - OVERHEAD EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE AFT OVERHEAD EMERGENCY LIGHT LAMP. 2L72 4T RTT00011AT 20051130001182005113000118SO 2005 11 30 RAIA00511028 120051121A36108166246 VALVE EMB 145 EMB145LR 3260212SO CABIN AIR OVERTEMP A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03839HK1253841 14500829 FLT 7989 - DAY - ON CLIMBOUT, DID 2ND PART OF F/O'S ICE TEST AND RECEIVED AN EICAS MESSAGE OF BLEED 2 OVERTEMP. MAINTENANCE REMOVED AND REPLACED THE FAN AIR VALVE THERMOSTAT. 2L72 4T RTT00011AT 20051130001192005113000119NM 2005 11 30 AALA20050785 120051111A3350 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21952AA 30088 TUL - BATTERY PACK FOR FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT STATION 328 FOR FORWARD CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20051130001302005113000130NM 2005 11 30 UPS05445839 120051126A573065B1704925 PANEL BOEING747 747123F NM LEFT WING DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 LEFT WING LOWER PANEL DELAMINATED OUTBOARD OF NR 3 CANOE. UNDER NR 5 SPOILER ACT, AREA MARKED. COMPLIED WITH EO B747-5720-23353A EXCEPT FOR INSTALLING FASTENERS ON LE OF PANE. REMOVED TEMP REPAIR PANEL SH 1199928 DRILLED UP NEW PANEL. INSTALLED RIVETS AND LOCK FASTENERS FWD EDGE AND SCREWS ON OB EDGE. REF SRM 51-30-12 SH 199928. INSTALLED BULB SEAL ON REAR OF PANEL 1439884. INSTALLED TIE REELS, THIS CLEARS D314807. 2L74 4F A20WE 20051130001322005113000132CE 2005 11 30 DXTA200501115 120051127A2611 WARNING LIGHT CESSNA750 750 2076810CE CARGO SMOKE FALSE ACTIVATIONE DXTAH DEACTIVATE SYST/CIRCUITS N FALSE WARNING CLCLIMB 1 GL07932QS 7500032 "BAGGAGE SMOKE" ILLUMINATED ON EICAS AFTER TAKEOFF. COMPARTMENT WAS ISOLATED AND WE RETURNED FOR LANDING. ONCE ON THE GROUND THERE WAS NO SIGN OF SMOKE OR FIRE IN THE BAGGAGE COMPARTMENT. ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20051130001332005113000133CE 2005 11 30 DXTA200501121 120051128A3240 BRAKE CESSNA500 560CESSNA 2076750CE LT PEDAL MALFUNCTIONED E DXTAO OTHER S AFFECT SYSTEMS LDLANDING 1 GL07312QS 5600312 ON LANDING, LEFT BRAKE PEDAL ON CO-PILOT SIDE WENT TO FLOOR. RIGHT PEDAL WORKED NORMALLY. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20051130001362005113000136CE 2005 11 30 DXTA200501114 120051126A21707464513 COALESCER BAG CESSNA750 750 2076810CE CABIN AIR DIRTY E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL07998QS 7500198 CABIN AND COCKPIT FILLED WITH SMOKE AFTER TAKEOFF. SMOKE DISIPATED WITHIN 2 MINUTES. REMOVED COALESCER SOCK AND REPLACED WITH NEW UNIT IAW CESSNA 750 MM CHAPTER 21-20-40. PERFORMED ENGINE RUN FOR 30 MINUTES AND SYSTEM OPS CHECKED GOOD, NO SMOKE FOUND. 2L72 4J RTT00007WI 20051130001372005113000137CE 2005 11 30 DXTA200501113 120051126A2750 POSITION SWITCH CESSNA560 560XL 2076702CE SPEED BRAKE CONTAMINATED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07616QS 5605345 NO TAKEOFF LIGHT WILL NOT GO OUT IN PROPER T/O CONFIGURATION. LIGHT WENT OUT WITH ENGINES OFF AND CYCLE SPEED BRAKE SWITCH, LIGHT ON WITH ENG/HYD OPERATING. TROUBLESHOT SYSTEM, DISCOVERED LT SPEEDBRAKE RETRACT SWITCH FULL OF WATER AND DEBRIS. CLEANED CONNECTOR CHECKED BOTH LT AND RT RETRACT SWITCH CONTACT. NO DEFECTS NOTED PERFORMED TAKEOFF WARNING SYSTEM OPS CHECK WITH NO DISCREPANCIES. ALL WORK DONE IAW CESSNA 560XL MM 27-40-00. 2L72 4F RTA22CE 20051130001382005113000138CE 2005 11 30 DXTA200501117 120051127A2910 LINE CESSNA500 560CESSNA 2076750CE HYDRAULIC SYS LEAKING E DXTAD RETURN TO BLOCK KS FLUID LOSS AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07332QS 5600523 DURING TAXI-OUT, CO-PILOTS RIGHT BRAKE PEDAL GOES TO THE FLOOR WITH MINIMAL BRAKE EFFECTIVENESS. AFTER PUMPING BRAKE PEDAL , FULL PRESSURE RETURNS TO BRAKE PEDAL. HOWEVER A SHORT TIME DELAY RETURNS RIGHT BRAKE PEDAL TO SAME CONDITION. - BLED BRAKES & ANTI-SKID SYSTEM TO REMOVE ALL AIR IAW CE560 M/M CHAP 32-42-00. BRAKES OPS CHECK AND LEAK CHECK GOOD. 2L72 4F RTA22CE 20051130001392005113000139CE 2005 11 30 DXTA200501118 120051128A3230 UNKNOWN CESSNA750 750 2076810CE UNKNOWN UNKNOWN E DXTAO OTHER E VIBRATION/BUFFET CRCRUISE 1 GL07975QS 7500175 DURING FLIGHT HEARD/FELT "BUMP IN THE NIGHT" THREE TIMES, ONCE DURING CLIMB-OUT, TWICE DURING CRUISE. 2L72 4J RTT00007WI 20051128001872005112800187EU 2005 11 28 05FDEA03933 120051121A7830 REPAIR AIRBUS300 A300B4622R 3930312EU THRUST REVERSER UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25720FD 417 THRUST REVERSER-UPPER TORQUE BOX CAP GOUGE REPAIR. COMPLIED WITH EA 6-7830-92361 THRUST REVERSER UPPER TORQUE BOX GOUGE REPAIR. 2L72 4F RTA35EU 20051128001932005112800193EA 2005 11 28 COMA0560629 120051120A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ILLUMINATED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01914CA 7012 FLIGHT 5132 - DURING TAKEOFF ROLL, RECEIVED A LEFT THRUST REVERSER MESSAGE, ABORTED T/O AND RETURNED TO THE GATE. DEFERRED THE LEFT THRUST REVERSER PER MEL 78-30-01. 2L72 4F RTA21EA 20051128001982005112800198EA 2005 11 28 COMA0560627 120051119A27403094334 SWITCH CNDAIRCL600 CL6002B19 1900309EA PITCH TRIM FAULTY A COMAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 SO01735CA 7420 FLIGHT 5768 - ABORTED TAKEOFF AT IAD, DUE TO STABILIZER TRIM RUN-AWAY, AIRCRAFT RETURNED TO GATE. FERRIED THE AIRCRAFT TO CVG FOR REPLACEMENT OF THE NR 2 PITCH TRIM SWITCH. 2L72 4F RTA21EA 20051128002032005112800203NM 2005 11 28 05FDEA03906 120051119A5320 FLOOR SUPPORT DOUG MD11 MD11 3023602NM ZONE 200 BROKEN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 CABIN, LONGITUDINAL FLOOR SUPPORT '' U '' CHANNEL ADJ TO X=0 STA 1942 FOUND FASTENER ATTACHMENT HOLE BROKEN. REMOVED AND REPLACED AS PER SRM 51-31-01. 2L73 4F RTA22WE 20051128002062005112800206NM 2005 11 28 AWXA200501429 120051027A575465C26602217 SKIN BOEING737 7373S3 1384711NM NR 2 SLAT DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 MCN - DURING C13 CHECK DISCOVERED DISBOND AREA ON THE LOWER SURFACE OF THE LEFT WING, NR 2 SLAT, OUTBOARD END OF SLAT. MAINTENANCE REMOVED DISBOND SKIN AND CORE ON THE NR 2 SLAT IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED REPLACEMENT CORE AND DOUBLER IAW BOEING 737-300 SRM 51-70-10-2R4. BONDED REPLACEMENT PARTS TO THE NR 2 SLAT OUTBOARD END IAW BOEING 737-300 SRM 51-70-10-2R4. 2L72 4F RTA16WE 20051128002092005112800209NM 2005 11 28 05FDEA03838 120051116A7711 INDICATOR BOEING727 7272D4 138407UNM EPR INOPERATIVE A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25287FE 21849 CREW REPORTS NR 3 EPR IND INOP/ERRATIC ON TAKEOFF ROLL. REPORTS ALL OTHER INDICATIONS NORMAL. RELEASED FOR SERVICE PER MEL/CDL: 77-01-01 INFO 16NOV05 18:20 MC1 R. PLEASE WORK IN CONJUNCTION WITH TSI: 77-10 7868. 2L73 4F A3WE 20051128002132005112800213WP 2005 11 28 IXXA05RNG103S 120050907A5730 SKIN DOUG DC8 DC872 302199BWP STA XW736.500 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK, FOUND A CORROSION ON LT WING EXTERIOR LWD SURFACE, REAR SPAR BETWEEN STA XW 736.500 - XW 761.0 AND STA XRS 700.000 - XW 736.000. SKIN WAS REMOVED AND REPLACED IAW DOUGLAS DRAWING 5644654, RIVETS WERE INSTALLED IAW DC8 SRM 51-1-21 PAGE 1-7 AND ANTI-CORROSIVE TREATMENT WAS APPLIED IAW DC8 SRM 51-1-8 PAGE 13-16. 2L74 4F RT4A25 20051128002182005112800218WP 2005 11 28 IXXA05RNG109S 120050921A5753 SKIN DOUG DC8 DC872 302199BWP ZONE 500 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK, FOUND A CORROSION ON LT INBOARD FLAP LWD EXTERIOR SURFACE. SKIN ON LT INBOARD FLAP EXTERIOR SURFACE WAS REPLACED IAW DOUGLAS DRAWING 5642960, AND RIVETS WERE INSTALLED IAW SRM 51-1-21 PAGE 1-7. 2L74 4F RT4A25 20051129000012005112900001EA 2005 11 29 QXEA200501561 120051124A3397M210D4N RELAY CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHTSMALFUNCTIONED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09617QX 10130 OKC - ON FLIGHT 4188 EMERGENCY LIGHTS CYCLE ON AND OFF WITH THE SWITCH IN THE ARM POSITION. AIRCRAFT FERRIED FROM OKC TO DEN FOR REPAIRS. MAINTENANCE IN DEN REPLACED THE AC ESSENTIAL BUS SENSE RELAY (K135) ON PCB5 IN JUNCTION BOX 11. ALSO REPLACED BATTERY PACKS AS PACKS WERE DEPLETED DUE TO THE PROBLEM. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20051129000132005112900013NM 2005 11 29 05FDEA03950 120051123A5753NRC6753503 SUPPORT FITTING DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 CRACK FOUND AT LT WING OUTBD FLAP LOWER FASTENER HOLE COMMON TO ARC 4009 SUPPORT FITTING LOCATED AT THE MOST OUTBD HOLE DURING HFEC INSPECTION. LT WING OUTBOARD FLAP ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND OPERATION TEST CARRIED OUT AS PER AMM 27-50-00-5, SATIS. 2L73 4F RTA22WE 20051129000202005112900020NM 2005 11 29 SWAA053749 120051127A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 827 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 827, RBL 23. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051129000322005112900032NM 2005 11 29 SWAA053761 120051123A3350101073 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29406WN 27894 FWD LOWER EMERGENCY EXIT LIGHT LENS COVER MISSING. INSTALLED LENS COVER PER MM. 2L72 4F RTA16WE 20051129000342005112900034NM 2005 11 29 SWAA053716 120051121A53116520722 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, FWD FRAME NR 5 STOP FITTING. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20051129000692005112900069NM 2005 11 29 UPS05245821 120051016A5330 SKIN BOEING727 72730C 1384009NM BS 441 STR 8L CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 INSPECTION TYPE:C NDT INSPECTION HAS INDICATION OF MATERIAL LOSS AT BS 441 FWD OF CENTER LINE AT STR 8L, INVESTIGATE. CORROSION FOUND BETWEEN SKIN AND DOUBLER. CORROSION REMOVED AND FOUND BE WITHIN LIMITS, AREA REPROTECTED IAW SRM 51-30-02. 2L73 4F A3WE 20051129000712005112900071NM 2005 11 29 UPS05245823 120051101A5313 STRINGER BOEING727 72730C 1384009NM STR 24R BS725 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 INSPECTION TYPE:C STRINGER 24 RT FOUND CORRODED AT BS 725. PLEASE INVESTIGATE DAMAGE FOUND TO BE BEYOND LIMITS IAW SRM 53-10-3. DAMAGED SECTION OF STRINGER 24R CUT OUT AND REMOVED. AREA REPAIRED IAW 53-10-3 FIG 1 DETAIL 1 PAGE 4B. 2L73 4F A3WE 20051129000962005112900096NM 2005 11 29 AWXA200501445 120051113A5320D53472189204 FLOOR SUPPORT AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28660AW 1234 SAL - DURING BC4 CHECK DISCOVERED CORROSION ON LONGITUDINAL BEAM LOCATED AT FS 68 AND Y-1162. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-14. REMOVED AND INSTALLED NEW BEAM IAW AIRBUS SRM 51-42-11 AT FS 68 AND Y-1162. 2L72 4F RTA28NM 20051129000982005112900098NM 2005 11 29 AWXA200501447 120051111A5347D5713014720202 SEAT TRACK AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28660AW 1234 SAL - DURING BC4 CHECK DISCOVERED CORROSION ON THE LT OUTBOARD SEAT TRACK AT FS 36 AND Y1292. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 103. REMOVED AND REPLACED LT OUTBOARD SEAT TRACK FROM FS 36 TO FS 41 AND Y1292. 2L72 4F RTA28NM 20051129001032005112900103NM 2005 11 29 AALA20050763 120051118A3350 LIGHT BOEING767 767223 1385123NM CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21322AA 22323 JFK - RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. SECURED WIRING ON LIGHT ASSEMBLY FOR RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20051129001062005112900106NM 2005 11 29 QXEA200501559 120051122A2910 HYDRAULIC SYSTEM BOMBDRDHC8 DHC8402 1390042NM NR 1 MALFUNCTIONED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09410QX 4053 SEA FLIGHT NR 2309: FLAP POWER CAUTION LIGHT. RESET PER CHECKLIST AND FLAP POWER CAUTION LIGHT CAME ON AGAIN. MAINTENANCE FOUND NR 1 HYD QTY DROPPING APPROX 30 PERCENT WHEN NR 1 ENGINE IS STARTED. BLEED NR 1 HYDRAULIC SYSTEM IAW Q400 AMM 29-10-00, SUBTASK 29-10-00-870-029. PERFORMED OPERATIONAL TEST OF THE FLAPS IAW Q400 AMM 27-50-00. OPS CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051129001082005112900108NM 2005 11 29 PIDA20050192 120051122A5330 LAP JOINT BOEING737 7373G7 1384595NM BS 500B CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05380WL 23218 DURING "A CHECK, FOUND TWO CRACKS ABOVE STR 10 RT SKIN LAP, ONE JUST AFT OF BS 500A AND ONE JUST FORWARD OF BS 500B. 2L72 4F RTA16WE 20051130000032005113000003WP 2005 11 30 ABXA050287 120051114A53203924028501 FITTING DOUG DC9 DC941 302207NWP LONGERON CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23953AX 47608 LONGERON END FITTING CRACKED AT FS 642, LONGERON 29 RIGHT. REMOVED AND REPLACED FITTING IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20051130000122005113000012NM 2005 11 30 05FDEA03969 120051128A5753 REPAIR DOUG MD11 MD11 3023602NM ZONE 600 MISINSTALLED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25524FE 48480 RIGHT WING - WITH REFERENCE TO EO 1-5100-7-5001 P1, INBOARD FLAP INBOARD SEGMENT UPPER SURFACE AT XIFH 165 TO 171, YIFH 54 TO 60 FOUND WITH EXISTING REPAIR. EXISTING REPAIR AT INBOARD FLAP INBOARD SEGMENT UPPER SURFACE AT XIFH 165 TO 171, YIFH 54 TO 60 EVALUATED AND FOUND CARRIED OUT NOT IN ACCORDANCE WITH SRM 57- 10-00 FIGURE 34 SHEET 1 VOLUME I. RIGHT HAND WING - INBOARD FLAP INBOARD SEGMENT UPPER SURFACE AT XIFH 165 TO 171, YIFH 54 TO 60 WITH EXISTING REPAIR REMOVED AND REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 34 SHEET 1 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2- 100. 2L73 4F RTA22WE 20051130000132005113000013NM 2005 11 30 05FDEA03970 120051128A5753 REPAIR DOUG MD11 MD11 3023602NM ZONE 600 MISINSTALLED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25524FE 48480 RIGHT WING - WITH REFERENCE TO EO 1-5100-7-5001 P1, INBOARD FLAP INBOARD SEGMENT UPPER SURFACE AT XIFH 147 TO 153, YIFH 60 TO 63 FOUND WITH EXISTING DENT REPAIR. EVALUATED AND FOUND REPAIR NOT IN ACCORDANCE WITH SRM 57-10-00 FIGURE 34 SHEET 1 VOLUME I. RIGHT HAND WING INBOARD FLAP INBOARD SEGMENT UPPER SURFACE AT XIFH 147 TO 153, YIFH 60 TO 63 WITH EXISTING DENT REMOVED AND REPAIR IS CARRIED OUT AS PER SRM 57-10-00 FIGURE 34 SHEET 1 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2L73 4F RTA22WE 20051130000202005113000020WP 2005 11 30 05FDEA03977 120051128A5753 REPAIR DOUG DC10 DC1030 3023501WP LT WING FLAP PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 LT WING OUTBOARD FLAP UPPER SKIN FOUND A DOUBLER 35 X 4.25 INCHES AT STA XOF 462. PERFORMED A GVI OF REPAIR IAW SRM 57-10-00 FIG 9 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001-2P E3. 2L73 4F A22WE 20051130000242005113000024CE 2005 11 30 DXTA200501105 120051124A3260 WARNING LIGHT CESSNA560 560XL 2076702CE MLG ILLUMINATED E DXTAO OTHER J WARNING INDICATION APAPPROACH 1 GL07623QS 5605299 ON APPROACH SELECTED GEAR DOWN ONLY THE NOSE CAME DOWN WITH A CORRESPONDING NOSE DOWN & LOCKED GREEN LIGHT INDICATION, RED UNSAFE GEAR LIGHT ILLUMINATED & BOTH MAINS WOULD NOT EXTEND. CYCLED GEAR HANDLE ONE TIME GEAR OPERATED NORMALLY ON 2ND TRY. JACKED AIRCRAFT, PERFORMED A VISUAL INSPECTION OF THE LANDING GEAR, NO FAULTS NOTED. PERFORMED THE NOSE AND MAIN LANDING GEAR EXTENSION & RETRACTION PROCEDURE IAW THE CE-560XL MM CH 32-30, ALL CHECKS WERE NORMAL. ACTUATED AND LUBRICATED ALL LANDING GEAR EXTENSION & RETRACTION SWITCHES. REMOVED AIRCRAFT FROM JACKS. 2L72 4F RTA22CE 20051130000312005113000031NM 2005 11 30 QXEA200501570 120051126A30104100S00502 VALVE BOMBDRDHC8 DHC8402 1390042NM WING DEICE SYS MALFUNCTIONED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09411QX3463 4055 BOI FLIGHT 2405: RT OUTBOARD BOOT DOES NOT APPEAR TO INFLATE NORMALLY. DEICE PRESSURE CAUTION LIGHT ILLUMINATES EACH TIME DURING THE CYCLE. MAINTENANCE REMOVED LEADING EDGE 613AR AND REPLACED NR 2 DDV ON RIGHT WING IAW AMM TASK 30-11-16-000-801 AND 30-11-16-400-801. REINSTALLED LEADING EDGE 613AR AND SEALED LEADING EDGE. OPS CHECKS NORMAL IAW TASK 30-11-00-720-801. 2H72 4T RTA13NM 20051130000422005113000042 2005 11 30 CALA0500422 420051129A256565659733 SPRING BOEING737 7373T0 1384582NM L-2 DOOR SLIDE BROKEN A CALAK NONE O OTHER ININSP/MAINT 1 SW2769333 23571 THE R-2 DOOR AND L-2 DOOR ESCAPE SLIDE AFT GIRT BAR FLOOR BRACKETS WERE FOUND WITH SPRINGS BROKEN. NEW GIRT BAR FLOOR BRACKETS WERE INSTALLED AT BOTH AFT DOORS AT AFT POSITIONS IAW MM 25-61-51. 2L72 4F RTA16WE 20051130000452005113000045EU 2005 11 30 RAIA00511033 120051122A2750 CHECK VALVE JETAIRJETSTMJETSTM4101 1500501EU TE FLAPS DIRTY A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03561HK 41077 FLT 5424 - STL - FLAPS WOULD NOT RETRACT. MAINTENANCE CLEANED THE EMERGENCY SYSTEM CHECK VALVE. 2L72 4T RTA41NM 20051130000522005113000052EA 2005 11 30 SWIA200515878 120051126A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT FAILED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07935SW 7725 FIRST STRIP OF FLOOR LEVEL EMERGENCY LIGHTING INOP (5 ROWS). REPLACED CABLE ASSY FOR FIRST SECTION OF EMERGENCY LIGHT STRIP IAW CRJ 200 AMM 33-51-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051130000722005113000072EU 2005 11 30 2005UALA01311 120051120A3350 BATTERY AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE EMERGENCY LIGHT FAULTY A UALAK NONE L NO TEST ININSP/MAINT 1 WP29454UA 1104 CABIN EMERGENCY LIGHTS TEST, EPSU BATTERY EMERGENCY LIGHT FAULT. REPLACED EPSU BATTERY 2L72 4F4 FRTA28NM E40NE 20051130000842005113000084NM 2005 11 30 2005UALA01325 120051122A5311 FRAME BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU BS 827 STR 8L CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29922UA 26642 CABIN FRAME CRACKED AT STA 827 STR 8L AT PSU ATTACH. MAJOR REPAIR ACP'D PER MM 53-10-84 REPAIR III. 2L72 4F4 FRTA16WE E21EU 20051130000902005113000090NM 2005 11 30 2005UALA01330 120051122A5551 ATTACH FITTING BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU HORIZONTAL STAB CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29906UA 25006 LEFT HORIZONTAL STABILIZER FWD SPAR LWR ATTACH FITTING CORRODED. MAJOR REPAIR ACP'D PER AAR EA I050309 FOR LUG REWORK AND BUSHING RPLMT'S. 2L72 4F4 FRTA16WE E21EU 20051130000912005113000091NM 2005 11 30 2005UALA01331 120051122A5610 WINDOW BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU COCKPIT CRACKED A UALAO OTHER O OTHER NRNOT REPORTED 1 WP29327UA 24147 L4 WINDOW CRACKED EN ROUTE. L4 WINDOW MIDDLE PANE SHATTERED, REPLACED WINDOW PER MM 56-11-31. 2L72 4F4 FRTA16WE E21EU 20051130000982005113000098EA 2005 11 30 SWIA200515883 120051124A274184897132 MOTOR CNDAIRCL600 CL6002C10 1390015EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION DEDESCENT 1 NM07760SK491 491 10223 STAB CH 2 INOP STATUS MESSAGE OCCURRED DURING DESCENT. REPLACED HORIZONTAL STAB TRIM ACTUATOR MOTOR IAW AMM 27-42-03. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051130001002005113000100EA 2005 11 30 SWIA200515885 120051123A2751855D10011 SENSOR CNDAIRCL600 CL6002B19 1900309EA BRAKE POSITION MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION LDLANDING 1 NM07447SW4503 4503 7677 FLAPS FAIL INFLIGHT CAUTION MSG. REPLACED BRAKE & POSITION SENSOR UNIT IAW CRJ MM 27-51-10. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051130001022005113000102EA 2005 11 30 SWIA200515887 120051117A2750766389L CONTROLLER CNDAIRCL600 CL6002C10 1390015EA SLAT/FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07762SK 10226 SLATS HALF SPEED STATUS MESSAGE DISPLAYED. REPLACED SFECU 2 IAW AMM 27-51-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051130001032005113000103 2005 11 30 SWIA200515888 420051118A34183995100208 COMPUTER CNDAIRCL600 CL6002B19 1900309EA STALL WARNING MALFUNCTIONED A SWIAO OTHER N FALSE WARNING CRCRUISE 1 NM07948SW4719 4719 7789 STALL FAIL CAUTION ILLUMINATED IN FLIGHT. REPLACED STALL PROTECTION COMPUTER IAW CRJ MM 29-35-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051130001072005113000107EA 2005 11 30 SWIA200515892 120051121A2741 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA COCKPIT INOPERATIVE A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07920SW 7660 CAPTAIN SIDE TRIM SWITCH INOP, WILL NOT TRIM NOSE UP OR DOWN. REPLACED CAPTAIN'S TRIM SWITCH ON YOKE. OPERATIONAL TEST GOOD. 2L72 4F RTA21EA 20051130001162005113000116EA 2005 11 30 SWIA200515901 120051118A5610 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07699BR 7801 CAPTAIN`S WINDOW IS CRACKED (SIDE WINDOW). REPLACED CAPTAIN`S SIDE VIEW WINDOW IAW AMM 56-00-00, 56-11-01, 56-12-01. OPERATIONAL CHECK GOOD. PN/OFF 601R33033-11, SN/OFF 03119H3055. 2L72 4F RTA21EA 20051130001272005113000127NM 2005 11 30 UPS05245834 120051009A5240 SKIN BOEING727 72730C 1384009NM MID GALLEY DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 FOUND SKIN CRACK AT FASTENER HOLE IN MID GALLEY DOOR CUT OUT, UPPER FWD CORNER. PLEASE CONFIRM WITH NDI AND RECTIFY AS NECESSARY HFEC CARRIED OUT ON FASTENER HOLES COMMON TO REPAIR IAW 727NDTM 51-00- 00 PT6 FIG 16. THREE CRACKS FOUND. REPAIR CARRIED OUT IAW UPS EO AUTHORIZATION NUMBER B727-5330-2320-A 2L73 4F A3WE 20051130001342005113000134CE 2005 11 30 DXTA200501111 120051125A3243991205018 MASTER CYLINDER CESSNA500 560CESSNA 2076750CE BRAKES LEAKING E DXTAD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07390QS3969 5600490 ANTI-SKID ANNUNCIATOR ILLUMINATED AND WILL NOT EXTINGUISH AFTER CYCLING THE ANTI-SKID SWITCH AND CIRCUIT BREAKER. BRAKES WORK AT SLOW TAXI SPEEDS BUT ARE NEARLY INOP AT HIGHER SPEEDS. REPLACED CO-PILOT RT BRAKE MASTER CYLINDER, ANTI-SKID SYSTEM FAULT MONITOR AND LT SKID TRANSDUCER CANNON PLUG. OPS CHECKED GOOD IAW CESSNA 560 MM 32-42-00 2L72 4F RTA22CE 20051130001402005113000140CE 2005 11 30 DXTA200501119 120051128A2120 SMOKE CESSNA750 750 2076810CE CABIN DETECTED E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL07998QS 7500198 SMOKE OBSERVED IN CABIN AND COCKPIT SHORTLY AFTER TAKEOFF, SMOKE DISSIPATED AFTER POWER WAS REDUCED TO REMAIN IN PATTERN FOR LANDING. 2L72 4J RTT00007WI 20051130001552005113000155NM 2005 11 30 QXEA200501558 120051122A2740 WARNING LIGHT BOMBDRDHC8 DHC8402 1390042NM PITCH TRIM ILLUMINATED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09414QX 4061 BOI FLIGHT NR 2300: PITCH TRIM CAUTION ILLUMINATED DURING ENGINE START. MAINTENANCE COMPLIED WITH FIM PROCEDURE 27-30-00 PAGES 210-211. ALL FAULTS CLEARED. OK FOR CONTINUED SERVICE. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051130001572005113000157EA 2005 11 30 QXEA200501557 120051118A35101733797 LINE CNDAIRCL600 CL6002C10 1390015EA OXYGEN SYSTEM LEAKING A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09609QX 10031 DEN - LOW OXYGEN PRESSURE CAUTION MESSAGE. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE CAPILLARY LINE AT THE GAUGE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20051130001592005113000159NM 2005 11 30 NOCA2605 120051117A33508100022608 LIGHT BOEING767 767324 1385203NM 1L DOOR INOPERATIVE G NOCAK NONE L NO TEST ININSP/MAINT 1 EA15760NA 26257 ROUTINE MAINTENANCE FOUND 1L EMERGENCY PATH ARROW LIGHT INOP. 2L72 4F RTA1NM 20051130001622005113000162NM 2005 11 30 05FDEA03935 120051122A5753 FLAP TRACK BOEING727 727227 1384078NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 LEFT WING INBOARD FLAP TRACK FORWARD AND AFT MOUNTING FLANGES HAVE CORROSION. MACHINED FWD MOUNT PAD TO .250 REMOVING .020 TO REMOVE CORROSION. AFT PAD TO .260 REMOVING .015 TO REMOVE CORROSION IAW BAC OHM 57-40-01 PAGE 411 FIGURE 402. PERFORMED MAG PARTIAL INSPECTION IAW BAC OHM 57-40-01, NO DEFECTS. ROTO PEENED FORWARD AND AFT PADS IAW OHM 57-40-01 AND BAC SOPM 20-10-03. CAD PLATED MOUNT PADS IAW BAC SOPM 20-42-10 REV IR PRIMED FWD AND AFT PADS IAW SRM 51-10-2. SIGNED BY TIMCO MECH 1560 AND QC280. 2L73 4F A3WE 20051130001642005113000164NM 2005 11 30 05FDEA03937 120051122A5753 FLAP TRACK BOEING727 727227 1384078NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 RIGHT WING O/B FLAR I/B TRACK AFT MOUNT CENTER BOLT HOLE HAS CORROSION. REPAIRED HOLE IAW BOEING OHM 57-40-01. REMOVED CORROSION FROM BORE IAW BOEING OHM 57-40-01. MAG PARTICLE INSPECTION OF BORE IAW BOEING OHM57-40-01. FABRICATED AND INSTALLED BUSHING IAW BOEING OHM 57-40-01 MECH: 7736 INSP:342 REFERENCE FED-EX NON ROUTINE NOO661. 2L73 4F A3WE 20051130001662005113000166NM 2005 11 30 05FDEA03939 120051122A5330 SKIN BOEING727 727233 138408ANM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25220FE 20934 AFT PIT HAS EXFOLIATED SKIN AT STA 1044 TO 1050 STR 29R TO STR 28R. ALL WORK ACCOMPLISHED ON SDR 05-4182. 2L73 4F RTA3WE 20051130001682005113000168NM 2005 11 30 05FDEA03941 120051122A5330 SKIN BOEING727 727227 1384078NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 AFT PIT AT STA BS 1012 AT LBL 29 HAS CORROSION ON SKIN. REMOVED EXISTING REPAIR AND DAMAGED SKIN IAW B727 SRM 53-30-3 FIGURE 3A. FABRICATED NEW REPAIR IAW B727 SRM 53-30-3 FIGURE 3A. ALODINED AND PRIMED IAW B727 SRM 51-10-2; AND INSTALLED NEW REPAIR IAW B727 SRM 53-30-3 FIGURE 3A. THIS IS A MAJOR REPAIR. REFERENCE FEDEX NR N00434, SIGNED BY TIMCO MECH NR 6709 AND QC298. 2L73 4F A3WE 20051130001692005113000169EU 2005 11 30 WRNA20050027 120051115A5610SPSA340141A WINDSHIELD AIRBUS300 A300B4203 3930306EU COCKPIT CRACKED A WRNAA UNSCHED LANDING O OTHER CRCRUISE 1 SO05820SC 8095 154 DURING CRUISE FLIGHT, NOTICE F/O WINDSHIELD HAS A THIN CRACK VISIBLE. THEN WINDSHIELD ARC'D AND CRACKED COMPLETELY, MULTIPLE CRACKS. PERFORMED ABNORMAL CHECKLIST. AIRCRAFT RETURNED TO AIRFIELD. LANDING NORMAL. REMOVED AND REPLACED F/O WINDSHIELD PANEL IAW 56-11-11. SYSTEM TEST PER MM 30-42-00 PG BLOCK 501, OP'S SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA35EU 20051130001702005113000170NM 2005 11 30 SWAA053782 120051125A33506104781 BATTERY PACK BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29742SW 29278 DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING INTERIOR AND EXTERIOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20051130001712005113000171NM 2005 11 30 SWAA053783 120051127A3350101114 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29773SA 27881 R1 DOOR EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED COVER PER MM. 2L72 4F RTA16WE 20051130001732005113000173NM 2005 11 30 2005UALA01268 120051113A3350 WIRE BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT DISCONNECTED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29942UA 26679 EMERGENCY EXIT FLOOR ESCAPE PATH LIGHTS INOP BACK THIRD OF CABIN. RECONNECTED POWER LEADS. 2L72 4F4 FRTA16WE E2GL 20051130001752005113000175 2005 11 30 2005UALA01270 420051112A2565 BATTERY BOEING747 747422 1384935NM PWA 4056 PW4056 NE RIGHT UPPER DECKNO TEST A UALAK NONE L NO TEST ININSP/MAINT 1 WP29173UA 24380 RIGHT UPPER DECK ESCAPE DOOR SLIDE BATTERY OK LIGHT DOES NOT ILLUMINATE WHEN PRESSED TO TEST. 2L74 4F4 FRTA20WE E24NE 20051130001772005113000177NM 2005 11 30 2005UALA01273 120051111A3241 WARNING LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE ANTI SKID SYS INTERMITTENT A UALAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 WP29519UA 24872 AN INTERMITTENT EICAS ANTI-SKID WARNING LIGHT CAUSED A DIVERSION DUE TO CONCERNS WITH A SHORT RUNWAY AT PLANNED DESTINATION. REPLACED ANTISKID-AUTOBRAKE CONTROL UNIT PER MM 32-42-01. OPS CHECK NORMAL. 2L72 4F4 FRTA2NM E17NE 20051201000012005120100001NE 2005 12 1 2005UALA01274 220051115A7200 ENGINE BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 2 POWER LOSS A UALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 WP29546UA 25367 THRUST LOSS OCCURRED MULTIPLE TIMES WITH NR 2 ENGINE. REMOVED AND ROUTED THE EEC, PERFORMED A DATA DUMP, NO FAULTS OR FAILURES FOUND. THE EEC BEING MADE SERVICEABLY AND RETURNED. REMOVED THE N2 TRANSDUCER ALTENATOR STATOR. CONPONENT PASSED ALL ELECTRICAL TEST, CANNON PLUG CONNECTOR DIRTY, THREADS ON SCREW ON BODY. COMPONENT LIKELY CAUSE. NO ISSUE ON ENGINE SINCE REPLACEMENT. 2L72 4F4 FRTA2NM E17NE 20051201000022005120100002NM 2005 12 1 2005UALA01275 120051115A3350 BATTERY AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE EMERGENCY LIGHT FAULTY A UALAK NONE L NO TEST ININSP/MAINT 1 WP29840UA 1522 EPSU BATTERY FWD L DISPLAYED DURING 3SV CABIN EMERGENCY LIGHT CHECK. REPLACED EPSU BATTERY. 2L72 4F4 FRTA28NM E40NE 20051201000042005120100004 2005 12 1 2005UALA01277 420051114A2565 SLIDE BOEING757 757222 1384956NM PWA 2037 PW2037 NE DOOR 1L DISLODGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29577UA 26693 DOOR 1L SLIDE PACK OFF OF DOOR. PER AMIS HISTORY, DURING THE PERIOD OF 1OCT&14NOV 2005, THERE WAS NO REPORTED PREVIOUS ACTIVITY RELATED TO THE 1L DOOR SLIDE THAT COULD HELP IN PINPOINTING A PROBABLE CAUSE WHY THE SLIDE WAS OFF THE DOOR. A PROBABLE CAUSE THAT COULD PERHAPS HAVE ATTRIBUTED TO THIS, COULD BE THAT THE SLIDE WAS SUBJECTED TO SOME IN-SERVICE IMPACT.CORRECTIVE ACTION: SLIDE WAS REINSTALLED PER THE AMM. 2L72 4F4 FRTA2NM E17NE 20051201000082005120100008NM 2005 12 1 AALA20050758 120051115A3350 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21926AN 29527 TUL - VARIOUS BATTERY PACKS FOR EMERGENCY LIGHTS IN CABIN FAILED CHECKS. REPLACED BATTERY PACKS FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20051201000112005120100011NM 2005 12 1 AALA20050760 120051120A2530 OVEN BOEING767 767323 1385205NM GALLEY SMOKE A AALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21346AN 33085 INFLIGHT, OVEN NR 6 IN COACH GALLEY WAS SMOKING FROM BEHIND OVEN. FLIGHT ATTENDANT REPORTED ELECTRICAL SMELL. CLEANED NUMBER SIX OVEN AND RAN NUMBER 6 AND NUMBER 5 OVENS AND AFT GALLEY RIGHT CHILLER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20051201000122005120100012NE 2005 12 1 AALA20050761 220051118A7200 ENGINE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE RIGHT FAILED A AALAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 SW21963TW 53613 728215 INFLIGHT, SHORTLY AFTER LEVEL OFF AT FL320, RIGHT ENGINE FAILED. RIGHT HAND ENGINE OIL QUANTITY AND PRESSURE WERE NORMAL. EXHAUST GAS TEMPERATURE REACHED 800 DEGREES BEFORE SHUTDOWN. NO FIRE INDICATION OCCURRED. LANDED ORD WITHOUT INCIDENT. REPLACED NUMBER TWO ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA6WE E9NE 20051201000142005120100014NM 2005 12 1 2005UALA01278 120051115A3350 LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE DOOR 2R SLIDE NO TEST A UALAK NONE L NO TEST ININSP/MAINT 1 WP29544UA 25322 DOOR 2R SLIDE LIGHT NOT ILLUMINATED WITH DOOR ARMED PER CREW. REPLACED. 2L72 4F4 FRTA2NM E17NE 20051201000162005120100016NM 2005 12 1 2005UALA01279 120051115A3350 LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE DOOR 2L SLIDE BURNED OUT A UALAK NONE L NO TEST ININSP/MAINT 1 WP2987UA 26713 SLIDE LIGHT AT 2L BURNED OUT. REPLACED. 2L72 4F4 FRTA2NM E17NE 20051201000172005120100017NM 2005 12 1 2005UALA01280 120051115A3350PN78941 LAMP BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE EMERGENCY LIGHT FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29798UA 26928 SEAT 1F AFT EMERGENCY LIGHT INOP. REPLACE BULB. 2L72 4F4 FRTT0001SE E46NE 20051201000182005120100018NM 2005 12 1 2005UALA01281 120051115A3397 CONNECTOR BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE SEAT 2A AFT LOOSE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29798UA 26928 SEAT 2F AFT EMERGENCY LIGHT INOP. CONNECTOR LOOSE. 2L72 4F4 FRTT0001SE E46NE 20051201000202005120100020NM 2005 12 1 2005UALA01283 120051115A2120 ODOR BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE CABIN DETECTED A UALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP29226UA 30226 EQUIPMENT COOLING FAULT ON STS PAGE AND BURNING SMELL IN CABIN. EQUIPMENT COOLING FAN ASSEMBLY FAILED. FAN ASSEMBLY REPLACED. 2L72 4F4 FRTT0001SE E46NE 20051201000222005120100022NE 2005 12 1 2005UALA01285 220051116A7200 COMPRESSOR AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE NR 1 ENGINE STALLED A UALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 WP29807UA 798 V10327 NR 1 ENGINE COMPRESSOR STALL. POWER LOSS AT FL360 FOR 8-10 SEC. ENGINE RECOVERED AND FLIGHT DIVERTED INTO DEN. COCKPIT CFDS INDICATED STALL. C3 FINDING DURING BORO MAY OR MAY NOT HAVE CONTRIBUTED TO THE STALL. 2L72 4F4 FRTA28NM E40NE 20051201000232005120100023EU 2005 12 1 2005UALA01286 120051112A3350 POWER SUPPLY AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE EMERGENCY LIGHT NO TEST A UALAK NONE L NO TEST ININSP/MAINT 1 WP29419UA 487 FWD LEFT EMERGENCY POWER SUPPLY UNIT FAILED TEST DURING EMERGENCY LIGHT TEST. PSU REPLACED. 2L72 4F4 FRTA28NM E40NE 20051201000242005120100024 2005 12 1 2005UALA01287 420051117A2565 BOTTLE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE DOOR 1R SLIDE DISCHARGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29422UA 503 DOOR 1R ESCAPE SLIDE BOTTLE INDICATION OUT OF GREEN BAND. THE SLIDE (MR25611-1055) HAD BEEN REMOVED FROM ACFT 4622 WITH A WRITE-UP STATING THAT BOTTLE PRESS NEEDLE WAS IN "RED BAND". HOWEVER, THE SHOP INSPECTION REVEALED THAT THE BOTTLE WAS IN THE "GREEN BAND". TEMP HAD NOT STABILIZED BEFORE READING (AMM 26-62-00, PG-604). PERHAPS MECH DECISION TO REPLACE COULD BE DUE TO NOT ENOUGH GROUND TIME TO LET THE BOTTLE TEMP TO STABILIZE, AS INDICATED ON I & R TAG MECH COMMENT, "LOW PRESS PREVENT DELAY AT DEPARTURE." 2L72 4F4 FRTA28NM E40NE 20051201000262005120100026NM 2005 12 1 2005UALA01289 120051117A3397 WIRE BOEING747 747422 1384935NM PWA 4056 PW4056 NE SEAT 4F DAMAGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29107UA 26900 EEL LTS INOP, SEAT 4F BOTH SEGMENTS. REPAIRED WIRE IN SEAT. 2L74 4F4 FRTA20WE E24NE 20051201000272005120100027NM 2005 12 1 AWXA200501455 120051113A5315D53112782200 FLOORBEAM AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28660AW 1234 SAL - DURING BC4 CHECK DISCOVERED CORROSION SPREAD OUT ON FLOORBEAM BETWEEN FS 16 AND FS 20, Y-1292. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-11-14. REMOVED AND INSTALLED FLOORBEAM IAW AIRBUS SRM 51-42-11 FROM FS 12 TO FS 24 AND Y-1292. 2L72 4F RTA28NM 20051201000322005120100032NM 2005 12 1 2005UALA01294 120051117A3350 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29107UA 26900 EMERGENCY LT INOP AT UPPER DECK DOOR CEILING AFT CENTER AND COCKPIT CEILING. REPLACED LAMP. 2L74 4F4 FRTA20WE E24NE 20051201000342005120100034NM 2005 12 1 2005UALA01296 120051118A3350 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE COCKPIT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29195UA 26899 FLIGHT DECK CEILING EMERGENCY LIGHT INOP. REPLACED LAMP. 2L74 4F4 FRTA20WE E24NE 20051201000362005120100036NM 2005 12 1 2005UALA01299 120051118A3350 CONNECTOR BOEING747 747422 1384935NM PWA 4056 PW4056 NE ROW 18R LOOSE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29195UA 26899 EMERGENCY EEL LIGHT AT UPPER DECK WALL ACROSS ROW 18R INOP. RESECURED EMERGENCY LIGHT CONNECTOR. 2L74 4F4 FRTA20WE E24NE 20051201000372005120100037NM 2005 12 1 2005UALA01300 120051118A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE R1 DOOR INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29195UA 26899 DOOR 1 RIGHT EMERGENCY LIGHT ON BUSTLE INOP. RESECURED EMERGENCY LIGHT. 2L74 4F4 FRTA20WE E24NE 20051201000402005120100040WP 2005 12 1 05FDEA03952 120051124A5312 BULKHEAD DOUG DC10 DC1010 3022110WP BS 575-569 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 RT AIR CONDITIONING COMPT FOUND 1 CRACK 2.50" LONG ON BULKHEAD BETWEEN STA 575 AND STA 569 Z-60 X-24. REPAIRED CRACK IAW SRM 53-30-00 FIG 6 SHT 4 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F164142/N001142 AND IAW SRM 53-30-00 FIG 6 SHT 4 VOL 1. 2L73 4F A22WE 20051201000412005120100041WP 2005 12 1 05FDEA03953 120051124A5310 DOOR FRAME DOUG DC10 DC1010 3022110WP BS 1305 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 MAIN CABIN FOUND 2 CRACKS 1" LONG ALL ON WEB JAMB DOOR NR 3 AFT AT STA 1305 LONG 27 RT SIDE. REPAIRED DOOR JAMB IAW SRM 53-50-00 FIG 19 SHT 2 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER F163497/N00497 AND IAW SRM 53-50-00 FIG 19 SHT 2 VOL 1. 2L73 4F A22WE 20051201000422005120100042WP 2005 12 1 05FDEA03954 120051124A5311 REPAIR DOUG DC10 DC1010 3022110WP BS 475 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 FWD AVIONICS COMPT AT STA 475 FOUND FRAME REPAIR AT X 60. NO ACTION TAKEN FRAME WILL BE REMOVED WITH NRC N00579. 2L73 4F A22WE 20051201000432005120100043CE 2005 12 1 DJFA2005166 120051123A2160 UNKNOWN BEECH MU300 400A 1155402CE COCKPIT FUMES E DJFAGA O2 MASK DEPLOYED UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA23718TA RK195 KAPA - TRIP ID NR 935454, THE CREW REPORTED SMELLING VERY STRONG FUMES IN THE COCKPIT AFTER TAKEOFF. THE FUMES COMING FROM THE "EYEBALL" VENTS WERE REPORTED TO HAVE BURNED THE EYES AND THROATS OF THE CREW. OXYGEN MASKS WERE DONNED, AND A/C WAS RETURNED TO KAPA. AN OVERWEIGHT LANDING WAS MADE IN KAPA W/O FURTHER INCIDENT. MX DISCOVERED THE COCKPIT AND CABIN CONTROL LINES LEADING TO THE TEMPERATURE CONTROL VALVES TO BE SWAPPED. THE LINES AT CONTROL VALVES WERE INSTALLED, AND A FUNCTIONAL CHECK OF CABIN AND COCKPIT TEMPERATURE CONTROL WAS PERFORMED. OPS CHECKS WERE GOOD WITH NO NOTED DEFECTS. AN OVERWEIGHT LANDING WAS PERFORMED WITH NO NOTED DEFECTS. THE A/C WAS RETURNED TO SERVICE. 2H72 4F RTA16SW 20051201000442005120100044WP 2005 12 1 05FDEA03956 120051124A5310 DOOR FRAME DOUG DC10 DC1010 3022110WP BS 1841 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 IN THE AFT CARGO COMPT FOUND EXISTING ANGLE STIFFENER ON JAMB DOOR BETWEEN L37 TO L41 AT STA 1841 LT SIDE. REMOVED GUARD SUPPORT STRIPPED POINT PERFORMED NDI ACCOMPLISHED EA NR 8-5310-93211, REPROTECTED AREA AND REINSTALLED GUARD SUPPORT IAW SRM 51-31-01 PAR 6 VOL 2. 2L73 4F A22WE 20051201000462005120100046WP 2005 12 1 05FDEA03958 120051124A5310 REPAIR DOUG DC10 DC1010 3022110WP BS 879-919 IMPROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 FWD CARGO COMPT FOUND NR 2 SPLICE REPAIR ON LONG NR 51 BETWEEN STA 879-919 RT SIDE. REMOVED SPLICE AND PORTION LONGERON IAW SRM 53-10-00 VOL1 STRIPPED PAINT IAW SRM 51-21-01 VOL 2. PERFORMED NDT INSPECTION RESTORED PAINT IAW SRM 51-21-01 VOL 2. REINSTALLED SPLICE AND PORTION LONGERON IAW SRM 53-10-00 VOL 1. 2L73 4F A22WE 20051201000472005120100047WP 2005 12 1 05FDEA03959 120051124A5310 REPAIR DOUG DC10 DC1010 3022110WP BS 879-939 IMPROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 FWD CARGO COMPT FOUND NR 3 SPLICE REPAIR ON LONG NR 52 BETWEEN STA 879-939. REMOVED SPLICE IAW SRM 53-10-00 VOL 1. STRIPPED PARTS IAW SRM 51-21-01. PERFORMED INSPECTION RESTORED PAINT IAW SRM 51-21-01 VOL 2. REINSTALLED PARTS IAW SRM 53-10-00. 2L73 4F A22WE 20051201000482005120100048NM 2005 12 1 05FDEA03946 120051123A5330 SKIN BOEING727 727227 1384078NM ZONE 100 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 RIGHT FUSELAGE EXTERNAL SKIN HAS A DENT AT STA BS 414 ON STRINGER STR 25-R. CHECKED DENT AND FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-30-1. CUT OUT DAMAGE IAW B727 SRM 53-30-3. FABRICATED DOUBLER AND FILLERS IAW B727 SRM 53-30-3. ALODINED AND PRIMED REPAIR PARTS IAW B727 SRM 51-10-2. INSTALLED REPAIR DOUBLER AND FILLERS IAW B727 SRM 53-30-3. THIS IS A MAJOR REPAIR. SIGNED BY TIMCO MECH NR 110188 AND QC178. 2L73 4F A3WE 20051201000492005120100049CE 2005 12 1 10212005A 120051017A261247790005 FIRE DETECTOR BEECH 1900 1900D 1154162CE RT NACELLE MALFUNCTIONED A NSVAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 EA27124CJ UE24 RT FIRE LOOP ANNUNCIATOR ILLUMINATED DURING RUNUP AND REMAINS ON. INSPECTED FIRE LOOPS, CANNON PLUGS AND A319 NO DEFECTS NOTED. REMOVED AND REPLACED FIRE DETECTION CONTROL UNIT. OPS CHECK GOOD, PN 477-90005, SN 9036-005. 2L72 4T RTA24CE 20051201000532005120100053NE 2005 12 1 11022005B 220051031A74204052T54P02 IGNITION LEAD SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RT ENGINE DAMAGED A NSVAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 EA27203CJ 203 GEE785516 FOUND RT ENGINE FAILED ON TAKEOFF. HEARD POPPING AND THEN PROP AUTO COARSENED. PERFORMED BORESCOPE NO DEFECTS NOTED, FOUND BROKEN IGNITION LEAD. REMOVED AND REPLACED RT ENGINE OUTBOARD IGNITER LEAD, PN 4052T54P02 SN ON UNJM3914, SN OFF UNJC3349. OPS CHECKS GOOD. 2L72 4T4 TRTA52EU E8NE 20051201000542005120100054CE 2005 12 1 11042005A 120051104A3230 CIRCUIT BREAKER BEECH 1900 1900D 1154162CE MLG TRIPPED A NSVAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA2760MJ UE60 GEAR WOULD NOT COME UP AFTER TAKEOFF. RESET LANDING GEAR CONTROL CIRCUIT BREAKER. CYCLED LANDING GEAR FOUR TIMES, OPS CHECK GOOD. 2L72 4T RTA24CE 20051201000572005120100057EU 2005 12 1 11172005B 120051108A7330946432 INDICATOR SAAB SF340 340B 7860101EU FUEL FLOW STUCK A NSVAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA27237MJ 237 LT FUEL FLOW INDICATOR STUCK. REMOVED AND REPLACED FUEL FLOW INDICATOR IAW MM 73-32-05 OPS CHECK GOOD, PN ON/OFF 9-464-32, SN ON 1483, SN OFF 974. 2L72 4T RTA52EU 20051201000602005120100060NM 2005 12 1 05FDEA03901 120051118A2130 CABIN PRESSURE BOEING727 7272S2F 1384O81NM MALFUNCTIONED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25208FE 22930 DEPARTING GTF A/C WOULDN'T PRESSURIZE. AUTO FAIL AND STBY. LIGHTS NOT ILLUMINATED. RAN FAILURE OF PRESS. CONTROL CHECKLIST, MANUALLY CLOSED OUTFLOW VALVE AND RECYCLED PACK SWITCHES TO EVENTUALLY RESTORE PRESSURIZATION. NO DOOR LIGHTS ILLUMINATED BUT LOUD WHISTLING THROUGH COCKPIT WINDOWS. CHECKED PER BMM 21-31-000-5, CHECKS NORMALLY, OK FOR CONTINUED SERVICE. 2L73 4F A3WE 20051201000632005120100063NM 2005 12 1 05FDEA03904 120051119A5313 STRINGER BOEING727 727233 138408ANM BS 1010 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25266FE 21672 AFT CARGO COMPARTMENT BILGE AREA, STR 29L HAS CORROSION STA 1010. REMOVED DAMAGED SEGMENT OF KEEL STA 980-1007 STR 29L. REMOVED PRODUCTION SPLICE CHANNEL. REMOVED SECTION OF SHEAR TIE, FRAME 990 STR 29-28. FABRICATED AND INSTALLED NEW KEEL SEGMENT, PRODUCTIN SPLICE, REPAIR KIT CHANNELS AND STRAPS, SHEAR TIE DOUBLER AND FILLER IAW SB 727-53-0179 SRM 51-10-2, 51-10-4 FIG 12, 51-30-2, AND 51-10-6. REPAIR DETERMINED TO BE MAJOR BASED ON FEDEX GMM 6-2-100 CRITERIA. 2L73 4F RTA3WE 20051201000662005120100066NM 2005 12 1 05FDEA03908 120051119A5320 FLOOR SUPPORT DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 CABIN, LONGITUDINAL FLOOR SUPPORT FROM STA 1911 TO 2007 APPROX X=-21 LAVATORY TIE DOWN UPPER SURFACE FOUND WITH MINOR CORROSION. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2L73 4F RTA22WE 20051201000692005120100069CE 2005 12 1 JBGA20050007 120051118A5270 PIN LEAR 60 60LEAR 5170707CE PAX DOOR OUT OF RIG E JBGAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL07529KF 064 CABIN DOOR LIGHT CAME ON AFTER TAKEOFF. RERIGGED CABIN DOOR PINS SO CABIN DOOR LIGHT STAYS EXTINGUISHED DURING FLIGHT. NEXT FLIGHT HAD NO PROBLEMS. 2L72 4F RTA10CE 20051201000702005120100070SO 2005 12 1 CHQA200500200 120051122A5610163500111 WINDSHIELD EMB 145 EMB145LR 3260212SO COCKPIT CRACKED A CHQAA UNSCHED LANDING O OTHER CLCLIMB 1 GL11283SK1242712427 145424 FLIGHT 3042 BWI-PHL - LEVELING OFF AT 10,000 FEET, THE CREW HEARD A LOUD BANG. CAPTAIN AND FO NOTICED THE LEFT FRONT WINDSHIELD HAD SHATTERED. WITHIN APPROXIMATELY 10 SECONDS THE W/S HEAT 1 FAIL MESSAGE APPEARED ON EICAS. CREW DECLARED AN EMERGENCY AND RETURNED TO BWI. THE APPROACH AND LANDING WERE UNEVENTFUL. MAINTENANCE REMOVED AND REPLACED CAPTAIN'S WINDSHIELD IAW AMM 56-10-01. OPS CHECK GOOD. 2L72 4T RTT00011AT 20051201000712005120100071WP 2005 12 1 IXXA0500117O 120051118A30102563375010 VALVE DOUG DC8 DC862 3021970WP ANTI ICE SYS LEAKING A IXXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW11799AL77263852 45922335 DURING CRUISE, LT MANIFOLD INFLIGHT DECAY CHECK FAILED 30-20 PSI IN ONLY 1.5 SECONDS. CREW RETURNED A/C AND LANDED W/O INCIDENT. ON THE GROUND, DECAY CHECK WAS 5 SECONDS. RT MANIFOLD GROUND DECAY FAILED 30-20-PSI IN ONLY 5 SECONDS. UPON INSPECTION MX FOUND LEAKING DUCT CLAMPS IN CROSS WING MANIFOLD. TIGHTENED AND REPLACED AS NECESSARY. FOUND PRESSURE RELIEF VALVES ON NR 1 AND 3 WOULD NOT CLOSE ON SCHEDULE, ALSO, FOUND LT FLOW CONTROL VALVE LEAKING THROUGH VALVE WHEN CLOSED. FOUND NR 4 WING ANTI-ICE VALVE LEAKING, CENTER SLOTTED EXTEND WING VALVE BLEED AIR DUCT LT SIDE LEAKING AT CLAMP AND A BROKEN DUCT FLANGE. ALL VALVES AND DUCTS WERE REPLACED PER ALL APPLICABLE MANUALS AND A/CT WAS RETURNED TO SERVICE. 2L74 4F 4A25 20051201000722005120100072CE 2005 12 1 DJFA2005164 120051121A2731258CT29115A JACKSCREW RAYTHNDH125 HAWKER800XP 7150012CE TRIM SYS ICED E DJFAO OTHER F FLT CONT AFFECTED CRCRUISE 1 EA23815TA 258534 KAPA - KRSW TRIP ID NR 898928, THE CREW REPORTED THAT THE ELEVATOR TRIM FROZE AT FL 350 WITH AN OUTSIDE AIR TEMPERATURE OF -35 DEGREES AT APPROXIMATELY 90 MINUTES INTO THEIR FLIGHT. NO PRECIPITATION WAS ENCOUNTERED FROM THE GROUND UP TO THIS POINT OF FLIGHT. AFTER DESCENDING TO 12,000 FT THE PROBLEM WAS RESOLVED. MAINTENANCE LUBRICATED THE ELEVATOR TRIM ACTUATOR. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA3EU 20051201000732005120100073EA 2005 12 1 SWIA200515867 120051115A3597 PCB CNDAIRCL600 CL6002C10 1390015EA OXYGEN SYSTEM MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07750SK 10207 WHILE SITTING AT THE GATE, LOADING PAX, ALL THE O2 MASKS DROPPED IN A/C. REPLACED PCB NR 4 IN JB10. OPERATIONAL CHECK GOOD, PN E520004-704, SN OFF E0270. 2L72 4F RTA21EA 20051201000742005120100074EA 2005 12 1 SWIA200515868 120051116A2741 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA COCKPIT INTERMITTENT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07945SW 7770 CAPTAINS TRIM SWITCH IS STICKY. REMOVED AND REPLACED STAB TRIM SWITCH NR 1 CONTROL YOKE. OPERATIONAL CHECK GOOD IAW MM 27-42-00. 2L72 4F RTA21EA 20051201000752005120100075EA 2005 12 1 SWIA200515869 120051116A274170609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 NM07945SW6683 6683 7770 AFTER T/O REC'D WHITE STATUS MSG "STAB TRIM NR 1". REPLACED HSTCU ASSY IAW CRJ MM 27-41-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051201000762005120100076EA 2005 12 1 SWIA200515870 120051115A5610 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAO OTHER O OTHER DEDESCENT 1 NM07962SW 7859 FO'S FRONT WINDSHIELD SHATTERED ON DESCENT. REPLACED FO'S FRONT WINDOW. 2L72 4F RTA21EA 20051201000772005120100077SO 2005 12 1 SWIA200515871 120051110A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT DISCHARGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07292UX2327 2327 120292 FLOOR EMERGENCY LIGHTS, 4 LIGHTS INOP, FIRST 2 RED, FIRST 2 WHITE LIGHTS. REPLACED FWD ELBP. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20051201000782005120100078 2005 12 1 DJFA2005160 420051112A2210 TRIM SYSTEM BEECH MU300 400A 1155402CE MALFUNCTIONED E DJFAH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CLCLIMB 1 EA23478LX RK387 A/C TRIMMED FOR CLIMB AND AUTO PILOT WAS ENGAGED AT 5,000 FT, APPROX 8,000 FT YELLOW BOXED "E" WAS DISPLAYED ON PRIMARY FLT DISPLAY, AND SOON AFTER AUTOPILOT PITCH TRIM FAIL ANNUNCIATOR ILLUMINATED. PITCH TRIM IND POSITION WAS SLIGHTLY NOSE DOWN. WHEN CREW DISENGAGED AUTOPILOT, A/C PITCHED UP AND REQ`D HIGH AMT OF CONTROL YOKE PRESSURE TO STOP THE UPWARD PITCH OF A/C. ALL C/B`SFOUND TO BE IN. WHEN PRIMARY PITCH TRIM WOULD NOT RESPOND, EMERGENCY PITCH TRIM WAS ENGAGED. EMERGENCY PITCH TRIM WAS USED FOR REMAINDER OF FLT, AND A/C WAS LANDED IN KTPA W/O INCIDENT. MX CYCLED PILOTS AND CO-PILOTS TRIM SWITCHES, AND PITCH TRIM EMERG SW. OPS CHECKS OF PITCH TRIM SYS GOOD. A/C RETURNED TO SERVICE. 2H72 4F RTA16SW 20051201000792005120100079NM 2005 12 1 UPS05M45801 120051118A301011501266 SENSOR DOUG MD11 MD11F 3023600NM ANTI ICE SYS INOPERATIVE A IPXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01255UP 48404 ATB - ON CLIMB-OUT TURNED ON WING ANTI-ICE, GOT RED NR 1 MANIFOLD LIGHT. STEM THEN ISOLATED BLEED SYS 1. GOT LEVEL 2 "WING A/I L DISAGREE". ATB DUE TO ICING CONDITIONS. T/S PER FIM 30-11-00-1 AND 36-11 00 FIG 103 BLOCK 13. REMOVED AND REPLACED LEFT A/I DIF SENSOR PER MM 30-11-02-4. NR 1 PSC PERFORMED HI-PWR ENG RUN AT 90 PERCENT N1, A/C IN FLT MODE. A/I SYS CK'D OK. DUCT PRESS 44 PSI. NO FAULTS INDICATED. 2L73 4F RTA22WE 20051201000802005120100080EA 2005 12 1 SWIA200515872 120051118A3350 LIGHT CNDAIRCL600 CL6002C10 1390015EA GALLEY CRACKED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07706SK 10149 GALLEY EMERGENCY LIGHT CRACKED AND LOOSE. REPLACED GALLEY DOOR EMERGENCY LIGHT AS REQUIRED. 2L72 4F RTA21EA 20051201000812005120100081EA 2005 12 1 SWIA200515873 120051116A3350 CHARGER CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07719SK 10188 CABIN EMERGENCY LIGHTS BETWEEN BUSINESS CLASS AND COACH ON BULKHEAD BOTH INOP. INSTALLED NEW FUSE FOR BATTERY PACK 2 CHARGER. OPERATIONAL CHECK GOOD IAW CRJ 700 AMM 33-51-00; 33-51-17. 2L72 4F RTA21EA 20051201000842005120100084EA 2005 12 1 SWIA200515876 120051112A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLT SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07905SW 7437 CREW REPORTS RT OUTBOARD SPOILERON FAULT. REPLACED RT OUTBOARD SPOILERON INBOARD PCU IAW CRJ MM 27-62-01. OPERATIONAL CHECK GOOD, P/N: 27000-7 S/N OFF: MAL3774. 2L72 4F RTA21EA 20051201000852005120100085SO 2005 12 1 SWIA200515877 120051114A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT DISCHARGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07251YV1021910219 120251 FORWARD SECTION OF FLOOR EMERGENCY LIGHT STRIP INOP. REPLACED FORWARD CABIN EMERGENCY LIGHT BATTERY PACK ASSY PER MM 33-50-02, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20051201000882005120100088NM 2005 12 1 05FDEA03923 120051120A5311 FRAME BOEING727 727227 1384078NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25496FE 21670 CORROSION AT FRAME STA BS 480 AT LBL 12, TOP OF FRAME. REMOVED DAMAGED SECTION OF BEAM. FABRICATED "T" CAP REPAIR SECTION, SUPPORT ANGLES, AND REINFORCEMENT STRAPS IAW B727 SRM 53-10-8 FIGURE 3. ALODINED AND PRIMED REPAIR PARTS IAW B727 SRM 51-10-2. INSTALLED REPAIR " T ", SUPPORT ANGLES, AND REINFORCEMENT STRAPS IAW B727 SRM 53-10-3 FIGURE 3. PAINTED REPAIR IAW B727 SRM 51-20-151. 2L73 4F A3WE 20051201000902005120100090NM 2005 12 1 05FDEA03926 120051121A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 MAIN DECK, SEAT TRACK BASE FOUND CORROSION ADJACENT TO STA 430 APPROXIMATELY X = 27.5. REMOVED AS PER SRM 51-21-01 VOLUME II FOUND EXCEEDED LIMIT AS PER SRM 53-00- 01 VOLUME I. DAMAGED SEAT TRACK REMOVED AS PER SRM 51-31-01 VOLUME II. NEW TRACK PART NUMBER ABA7684-509 MACHINED AS PER DRAWING ABA7684 AT STA 430 APPROXIMATELY X = 27.5 AND INSTALLED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2L73 4F RTA22WE 20051201000922005120100092EA 2005 12 1 U5QA05001 120051116A3220 PIN CNDAIRCL600 CL6002B16 1900305EA NLG INSTALLED E U5QAA UNSCHED LANDING WE INADEQUATE Q C VIBRATION/BUFFET CLCLIMB 1 CE05420ST 5027 PILOT REPORTED UNUSUALLY LOUD WIND NOISE AFTER GEAR RETRACTION. NO UNSAFE LIGHT. PILOT DID TOWER FLY-BY AND TOWER CONFIRM LT NOSE DOOR OPEN. LANDED AND MANUALLY RESET GROUND RELEASE LEVER IN NOSE BAY (USED FOR RELEASE OF LT NOSE GEAR DOOR TO INSTALL SAFETY PIN IN NOSE GEAR DURING GROUND HANDLING AND TOWING). CYCLED NOSE DOOR OPEN AND CLOSED USING HYDRAULIC SYSTEM. DOORS FUNCTIONED NORMALLY. 2L72 4F RTA21EA 20051201000932005120100093NM 2005 12 1 DL73S050690 120051107A53306545767103 SKIN BOEING737 737232 1384475NM BS 525 STR 16L CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27309DL 23081 FUSELAGE SKIN CRACKED AT BS 525, JUST ABOVE STR 16L. INSTALLED DOUBLER PER ER/A 451518-14AD, REF AD 2004-18-06, S/B 737-53A1210. 2L72 4F RTA16WE 20051201000942005120100094NM 2005 12 1 DL75K050691 120051109A5330141N323046 SKIN BOEING757 757232 1384965NM BS 412 STR 26L DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27697DL 30318 LIGHTNING STRIKE DAMAGED THE FUSELAGE SKIN AT BS 412 AT STR 26L. FACTORY PLUG WAS DISLODGED DURING REPAIR. INSTALLED DOUBLERS PER ER/A 451519-14. 2L72 4F RTA2NM 20051201000962005120100096NM 2005 12 1 DL76S050694 120051110A2910272T45002362 LINE BOEING767 767332 1382001NM HYD SYSTEM LEAKING A DALAO OTHER K FLUID LOSS CRCRUISE 1 SO27135DL 25145 IN FLIGHT EICAS MESSAGES C-HYD PRESS AND C-HYD QTY SHOWED .07RF, LATER WENT TO ZERO. CENTER ELEC 1 AND 2 PRESS AND CENTER AIR PRESS LIGHTS ILLUMINATED. C/W QRH PROCEDURE. INSPECTED AND FOUND HYD LINE COMING FROM RT BRAKE METERING VALVE TO T FITTING CRACKED. REPLACED LINE. SERVICED CTR HYD TO FULL. PERFORMED LEAK CHECK. LEAK CHECKS GOOD. 2L72 4F RTA1NM 20051201000972005120100097NM 2005 12 1 DL777050695 120051112A3320 BULB BOEING777 777232 1385232NM CABIN LIGHTS BURNED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27866DA 29738 HALOGEN LIGHT IN 2R BUNK AREA IN AFT CREW REST SHORTED OUT. FOUND FLUORESCENT BULB SOCKET IN AFT FLIGHT ATTENDANT CREW REST AFT BUNK RIGHT SIDE BURNED AND PIN ON BULB BURNED. NO FURTHER DAMAGE FOUND. REPLACED BALLAST AND BULB 2L72 4F RTT00001SE 20051201000992005120100099NM 2005 12 1 DLM88050700 120051112A291059369865501 RESERVOIR DOUG MD88 MD88 3023688NM HY SYSTEM UNKNOWN A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27960DL 49979 AT FL350 LEFT HYD PSI=0 AND LEFT HYD PRESS LOW. DID CHECKLIST WITH NO RESOLVE. LEFT SYS STILL PSI=0, QTY 17-19. REPLACED LEFT HYD SYS RESERVOIR AND LEFT ENG PUMP AND FILTERS. PURGED LEFT SYS OF AIR AND BLED RESERVOIR. 2L72 4F RTA6WE 20051201001002005120100100NM 2005 12 1 DLM88050701 120051113A2913623337 PUMP DOUG MD88 MD88 3023688NM HYD SYSTEM UNKNOWN A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27960DL 49979 AT FL350 LEFT HYD PSI=0. DUPLICATE REPORT TO DOCUMENT SECOND COMPONENT REPLACED. REPLACED PUMP. 2L72 4F RTA6WE 20051201001012005120100101NM 2005 12 1 DL76G050702 120051113A5610 WINDOW BOEING767 767324 1385203NM COCKPIT MALFUNCTIONED A DALAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO27394DL 27394 PILOTS WINDOW CAME OPEN ON T/O ROLL AFTER PASSING 80 KTS. PRIOR TO T/O HANDLE WAS VERIFIED IN LOCKED POSITION. ABORTED T/O ROLL AT 100 KTS. MTC VERIFIED OPERATION AND LOCKING MECHANISM WORKS OK. PERFORMED HIGH ENERGY STOP INSPECTION. ALL NORMAL. 2L72 4F RTA1NM 20051201001022005120100102NM 2005 12 1 DL76L050703 120051112A324026124121A BRAKE ASSY BOEING767 767332 1382001NM MLG LEAKING A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 SO27178DN 25143 DURING LANDING ROLLOUT TOWER ALERTED CREW OF SMOKE/VAPOR IN WHEEL WELL AREA. BAA REQUESTED MTC CHECK PRIOR TO TOW ONTO STAND. AFTER INSPECTION, FOUND NR 4 BRAKE UNIT LEAKING AT BRAKE CYLINDER. ISOLATED SYSTEM AND TOWED ONTO STAND. BRAKE REPLACED PER MM AND ALL CHECKS OK. 2L72 4F RTA1NM 20051201001062005120100106NM 2005 12 1 DL73S050710 120051114A53306545767103 SKIN BOEING737 737232 1384475NM BS 540 S-14L CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27326DL 23098 CRACK WAS FOUND IN THE FUSELAGE SKIN AT BS 540 AND JUST BELOW LAP SPLICE AT S-14L. INSTALLED DOUBLER PER ER/A 451595-14AD AND SRM 53-30-3. REF AD 2004-18-06. 2L72 4F RTA16WE 20051201001072005120100107NM 2005 12 1 DL73S050711 120051114A5712654541039 FLOORBEAM BOEING737 737232 1384475NM RBL 24.8 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27326DL 23098 CRACKS WERE FOUND IN THE OVERWING FLOORBEAMS AT RBL 24.8. INSTALLED REPAIR DOUBLERS AND CHANNEL PER ER/A 451614-14AD. REF AD 2001-17-18, AD 93-17-08, AD 90-06-02, SI 03-056673-12AD. 2L72 4F RTA16WE 20051201001082005120100108NM 2005 12 1 DL73S050712 120051114A5315 FLOORBEAM BOEING737 737232 1384475NM BS 678 LBL 24.8 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27326DL 23098 THE OVERWING FLOORBEAM AT LBL 24.8 WAS FOUND CRACKED. INSPECTED PER ER/A 451613-14AD. REF AD 2001-17-18, SI 03-056673-12AD, ER/A 369397-14. 2L72 4F RTA16WE 20051201001092005120100109NM 2005 12 1 DL73S050713 120051116A25305374AD COFFEEMAKER BOEING737 737232 1384475NM GALLEY ARCED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO27309DL 23081 SPARK JUMPED OUT IN FRONT OF AFT GALLEY, NR 2 POSITION COFFEEMAKER. REPLACED SAME. 2L72 4F RTA16WE 20051201001102005120100110NM 2005 12 1 DL75K050715 120051117A4900 ECU BOEING757 757232 1384965NM PWA 2037 PW2037 NE APU INOPERATIVE A DALAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 SO276707A 30395 727266 OFF LT IN GEN CONT SWITCH. ATTEMPTED ONE RESET. GEN OFF LIGHT RE-ILLUMINATED. DURING CLIMBOUT APU LIGHT, ATTEMPTED ONE RESTART APU RPM 103 PERCENT AND APU FAULT THE SECOND TIME. T/S PER FIM. PERFORMED BITE ON ECU AND FOUND OVERSPEED ON APU NOT OPERATING. MINI FLAG SHOWED P2 SENSOR. REMOVED AND REPLACED P2 SENSOR PER AMM. RAN APU, ALL CHECKS NORMAL. 2L72 4F4 FRTA2NM E17NE 20051201001122005120100112EU 2005 12 1 AALA20050776 120051123A3350P4010049 BATTERY PACK AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2111060 470 JFK - EMERGENCY LIGHTS IN AFT LEFT AND RIGHT ZONE INOPERATIVE. REPLACED BATTERY PACKS FOR EMERGENCY LIGHTS IN AFT LEFT AND RIGHT ZONE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20051201001132005120100113WP 2005 12 1 AALA20050779 120051124A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21476AA 49651 SFO - OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 23 AND 27 INOPERATIVE. REPLACED BATTERY PACK AT B5106 FOR OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 23 AND 27. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051201001142005120100114NM 2005 12 1 AALA20050781 120051126A3350 LIGHT BOEING767 767323 1385205NM COCKPIT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21381AN 25450 DFW - EMERGENCY LIGHT OVER COCKPIT DOOR INOPERATIVE. REPLACED EMERGENCY LIGHT OVER COCKPIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20051201001162005120100116WP 2005 12 1 AALA20050773 120051123A3240 LINE DOUG DC9 DC982 3022082WP BRAKE CROSSED A AALAO OTHER O OTHER LDLANDING 1 SW21428AA 49340 LAX - ON LANDING ROLLOUT THE NR 2 MAIN WHEEL BRAKE LOCKED CAUSING THE NR 2 TIRE TO BLOW OUT. FOUND THE FORWARD BRAKE LINES CROSSED ON THE LT MAIN LANDING GEAR. REPOSITIONED THE BRAKE LINES AND ACCOMPLISHED ANTI-SKID TEST. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051201001212005120100121NM 2005 12 1 SWAA053794 120051129A531165C22908 FRAME BOEING737 7373H4 1384600NM BS 500B CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 20L. REPAIRED FRAME PER SWA EA. 2L72 4F RTA16WE 20051201001232005120100123 2005 12 1 SWAA053796 420051129A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29391SW 27378 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051201001262005120100126NM 2005 12 1 SWAA053799 120051129A33509250071 BULB BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29481WN 29853 DURING SCHEDULED RON CHECK, FOUND EEPLS TRACK LIGHT INOP AT ROW 6. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20051201001272005120100127NM 2005 12 1 SWAA053800 120051129A53116545874 FRAME BOEING737 7373H4 1384600NM BS 294-296 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STUB FRAME CRACKED BETWEEN BS 294 TO BS 296, RBL 54.5, WL 209. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20051201001292005120100129NM 2005 12 1 SWAA053802 120051129A55516551524 FITTING BOEING737 7373H4 1384600NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 DURING SCHEDULED D-CHECK, FOUND LT & RT HORIZONTAL STAB ATTACH FITTING LUG FACES CORRODED. REPAIRED LUG FACES PER SRM. 2L72 4F RTA16WE 20051201001302005120100130NM 2005 12 1 SWAA053803 120051128A53306545776 SKIN BOEING737 7373A4 1384585NM BS 982 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29679AA 23291 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 982, STR 21L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051201001332005120100133NM 2005 12 1 05FDEA03983 120051128A5330 REPAIR BOEING727 727227 1384078NM ZONE 100 IMPROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 REPAIR LOCATED AT STA BS 251.6 TO BS 259 STRINGER STR 20-R REQUIRES EVALUATION FOR MAJOR / MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. FABRICATED DOUBLER IAW B727 SRM 53-30-2 FIGURE 1. ALODINED DOUBLER IAW B727 SRM 51-10-2. PRIMED DOUBLER IAW B727 SRM 51-10-2. INSTALLED DOUBLER IAW B727 SRM 53-30-2 FIGURE 1. MAJOR REPAIR. 2L73 4F A3WE 20051201001352005120100135EU 2005 12 1 05FDEA04009 120051129A3260 PROXIMITY SENSOR AIRBUSA300 A300F4622R 3930360EU MLG NO TEST A FDEAA UNSCHED LANDING JG WARNING INDICATION MULTIPLE FAILURE CLCLIMB 1 SO25724FD 530 AFTER T/O GEAR WOULD NOT RETRACT IN EITHER POSITION. PITCH TRIM NR 1 TRIPPED AND WOULD NOT RESET. AUTO THROTTLE LEVERS WERE ON BUT THROTTLES WOULD NOT RESPOND. CAPT ADF/RMI FAILED. RETURNED TO MSY. ON LANDING THRUST REVERSE WOULD NOT DEPLOY CAPT ADC FAILED, AND NOSE WHEEL STEERING WAS INOP. CLEARED THE RUNWAY VIA HIGH SPEED TURNOFF. TOWED TO RAMP. PITOT HEAT OVERHEAT AFTER LANDING. AIRCRAFT PRESSURIZED ON GROUND AND REQUIRED MANUAL DEPRESSURIZATION. GROUND PROXIMITY UNIT FAILED SELF TEST. 2L72 4F RTA35EU 20051201001372005120100137NM 2005 12 1 AALA20050770 120051120A3350P4010049 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21190AA 32384 SFO - EMERGENCY LIGHTS FROM SEAT 16D TO 25D INOPERATIVE. REPLACED BATTERY PACK AT M10953 FOR EMERGENCY LIGHTS FROM SEAT 16D TO 25D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20051201001392005120100139NM 2005 12 1 DL767050678 120051103A2910 LINE BOEING767 767232 1385132NM CENTER ADP FAILED A DALAO OTHER KJ FLUID LOSS WARNING INDICATION LDLANDING 1 SO27101DA 22213 ON TOUCHDOWN LOST CTR HYD SYSTEM. FOUND DISCONNECT ON ADP PRESSURE LINE FAILED. REPLACED SAME. 2L72 4F RTA1NM 20051201001412005120100141 2005 12 1 DL76G050681 420051104A2565BACR13CE2 RELAY BOEING767 767324 1385203NM ESCAPE SLIDE INOPERATIVE A DALAK NONE O OTHER ININSP/MAINT 1 SO27394DL 27394 WHILE PERFORMING ETOPS PRE-DEPARTURE CHECK, NR 1 AND NR 2 LT AND RT OVERWING ESCAPE SLIDE SQUIB TEST LIGHTS WOULD NOT ILLUMINATE. REPLACED K-839 RELAY, SYSTEM TEST CHECKS OK. 2L72 4F RTA1NM 20051201001432005120100143NM 2005 12 1 DL764050683 120051106A3220162T30072 SPRING BOEING767 767432ER 1385134NM NLG MISSING A DALAO OTHER O OTHER TXTAXI/GRND HDL 1 SO27827MH 29698 NOSE GEAR RT DOWNLOCK SPRING MISSING. REPLACED SPRING. 2L72 4F RTA1NM 20051201001512005120100151EU 2005 12 1 05FDEA03994 120051128A5330 SKIN AIRBUS310 A310 EU GE CF6 CF680 30025NE ZONE 200 PUNCTURED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25405FE 237 PUNCTURE AND DENT IN SKIN APPROX FR 44 RT STRINGERS 6-7. DAMAGE APPROX 5.00 IN X 3.2 IN. CUT OUT DAMAGE IAW A310-200 SRM 53-27-00. NDT FOR CRACKS IAW NTM 51-10-08. NO CRACKS NOTED. INSTALLED REPAIR DOUBLER IAW A310-200 SRM 53-10-12 FIG. 228. WORK DOCUMENTED ON NRC N00063. 2L72 4F4 FRTA35EU E13NE 20051130001412005113000141CE 2005 11 30 DXTA200501120 120051128A2822 WARNING LIGHT CESSNA500 560CESSNA 2076750CE BOOST PUMP ILLUMINATED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07801QS 5600601 DURING TAKEOFF POWER UP, LT FUEL BOOST PUMP LIGHT ILLUMINATED. TAKEOFF ROLL WAS STARTED AND ABORTED. 2L72 4F RTA22CE 20051130001422005113000142NM 2005 11 30 AWXA200501449 120051113A5347D53112826001 DUMMY RAIL AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28660AW 1234 SAL - DURING BC4 CHECK DISCOVERED CORROSION ON DUMMY RAIL LOCATED AT FS 16-2" AND Y503.2. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-11-14. REMOVED AND INSTALLED NEW DUMMY RAIL IAW AIRBUS SRM 51-42-11 FROM FS12 TO FS 16 AND Y503.2. 2L72 4F RTA28NM 20051130001432005113000143NM 2005 11 30 AWXA200501450 120051111A5347D5337111200500 SEAT TRACK AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28660AW 1234 SAL - DURING BC4 CHECK DISCOVERED LEVEL 2 CORROSION ON SEAT TRACK AT FS 46+13 AND Y-1292. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 103. REMOVED AND REPLACED SEAT TRACK FROM FS 41 TO FS 47 AND Y-1292. 2L72 4F RTA28NM 20051130001442005113000144NM 2005 11 30 AWXA200501451 120051111A5347D5337111001000 SEAT TRACK AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28660AW 1234 SAL - DURING BC4 CHECK DISCOVERED LEVEL 2 CORROSION ON RT INBOARD SEAT TRACK AT FS 46+14 AND Y-765. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 103. REMOVED AND REPLACED SEAT TRACK FROM FS 41 TO FS 47 AND Y-765. 2L72 4F RTA28NM 20051130001452005113000145NM 2005 11 30 AWXA200501452 120051111A5347D5713014720302 SEAT TRACK AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28660AW 1234 SAL - DURING BC4 CHECK DISCOVERED LEVEL 2 CORROSION ON SEAT TRACK AT FS 38+8 AND Y-1292. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 103. REMOVED AND REPLACED SEAT TRACK FROM FS 36 TO FS 41 AND Y-1292. 2L72 4F RTA28NM 20051130001462005113000146NM 2005 11 30 AWXA200501453 120051111A5347D5713014720000 SEAT TRACK AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28660AW 1234 SAL - DURING BC4 CHECK DISCOVERED LEVEL 2 CORROSION ON SEAT TRACK AT FS 40+14" AND Y765. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 103. REMOVED AND REPLACED SEAT TRACK FROM FS 36 TO FS 41 AND Y765. 2L72 4F RTA28NM 20051130001472005113000147NM 2005 11 30 SWAA053789 120051128A3350101331 COVER BOEING737 7373H4 1384600NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29651SW 27721 DURING SCHEDULED RON CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS COVER BROKEN. REMOVED AND REPLACED COVER PER MM. 2L72 4F RTA16WE 20051130001482005113000148 2005 11 30 SWAA053790 420051128A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29652SW 27722 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051130001492005113000149NM 2005 11 30 SWAA053791 120051128A5610141A4810 WINDOW BOEING737 7377H4 1384404NM COCKPIT ARCED A SWAAO OTHER O OTHER NRNOT REPORTED 1 SW29792SW 27887 R2 COCKPIT WINDOW ARCED. REMOVED AND REPLACED R2 WINDOW AND HEAT CONTROLLER PER MM. 2L72 4F RTA16WE 20051130001502005113000150 2005 11 30 SWAA053784 420051125A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29204WN 29855 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20051130001512005113000151NM 2005 11 30 SWAA053785 120051124A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29416WN 32453 EEPLS TRACK COVER OUT OF POSITION AT FWD END. REPOSITIONED COVER PER MM. 2L72 4F RTA16WE 20051130001522005113000152NM 2005 11 30 SWAA053786 120051128A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29452WN 29846 EEPLS TRACK COVER MISSING AT FWD END. INSTALLED COVER PER MM. 2L72 4F RTA16WE 20051130001532005113000153NM 2005 11 30 SWAA053787 120051128A2170213A10031 COALESCER BAG BOEING737 7377H4 1384404NM A/C BAY ODOR A SWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW29475WN 32474 AIR TURNBACK/DECLARED EMERGENCY. BURNING RUBBER FUMES AND ODOR IN CABIN. PERFORMED VISUAL INSPECTIONS, NO DEFECTS NOTED. REMOVED AND REPLACE LEFT AND RIGHT A/C PACK WATER SEPARATOR BAGS PER MM. 2L72 4F RTA16WE 20051130001542005113000154NM 2005 11 30 SWAA053788 120051128A53156546809 FLOORBEAM BOEING737 7375H4 138449DNM BS 947 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29512SW 24189 DURING SCHEDULED 1/2D CHECK, FOUND CABIN FLOORBEAM CORRODED AT BS 947.5, LBL 16 TO RBL 6. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20051130001562005113000156EA 2005 11 30 COMA0570123 120051123A5310CC670341757 BEAM CNDAIRCL600 CL6002C10 1390015EA FS 280 CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01378CA7622 10097 TRANSVERSE BEAM AT FS 280 FROM LBL 36 TO RBL 36 IS CORRODED ALONG THE UPPER AND LOWER EDGES. REPLACED THE TRANSVERSE BEAM AT FS 280 IAW BRAS REO 670-53-11-047 REV C. 2L72 4F RTA21EA 20051130001582005113000158NM 2005 11 30 QXEA200501560 120051122A3030 WARNING LIGHT BOMBDRDHC8 DHC8402 1390042NM PITOT HEAT ILLUMINATED A QXEAD RETURN TO BLOCK J WARNING INDICATION NRNOT REPORTED 1 NM09406QX 4048 PDX FLIGHT NR 2131: PITOT HEAT STANDBY CAUTION ILLUMINATED. MAINTENANCE CYCLED STANDBY PITOT HEAT CB. OPS CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051130001602005113000160NM 2005 11 30 NOCA2705 120051121A5270 CIRCUIT BREAKER BOEING757 75728A 1384976NM GIRT BAR POPPED G NOCAO OTHER O OTHER TXTAXI/GRND HDL 1 EA15750NA 26277 SNN FLT 123 DOOR GIRT BAR INDICATION CIRCUIT BREAKER POPPED. WILL NOT RESET. DEFERRED CI 25-965 MEL 25-66-5 2L72 4F RTA2NM 20051130001612005113000161EA 2005 11 30 COMA0570122 120051123A532067053110521 WEB CNDAIRCL600 CL6002C10 1390015EA FS 280 CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01378CA7622 10097 FS 280 BULKHEAD LOWER WEBS ARE CORRODED BEYOND LIMITS FROM LBL 36 TO RBL 36. REPLACED THE FS 280 BULKHEAD LOWER WEBS IAW BRAS REO 670-53-11-052 REV A REPAIR NR 2. 2L72 4F RTA21EA 20051130001632005113000163NM 2005 11 30 05FDEA03936 120051122A5753 FLAP TRACK BOEING727 727227 1384078NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 RIGHT WING INBOARD FLAP OUTBOARD TRACK FORWARD MOUNTING BOLT HOLES, BORES HAVE CORROSION. REAMED HOLES 2 EACH TO REMOVE CORROSION WITHIN LIMITS IAW. BAC OHM 57-40-01 NO CORROSION NOTED. FABRICATED AND CAD PLATED AND INSTALLED 2 EACH REPAIR BUSHINGS IAW OHM 57-40-01. REFERENCE FEDEX N/R N00730. SIGNED BY TIMCO MECH 4678 AND QC280. 2L73 4F A3WE 20051130001652005113000165NM 2005 11 30 05FDEA03938 120051122A5330 REPAIR BOEING727 727233 138408ANM ZONE 100 IMPROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25220FE 20934 EXISTING REPAIR AT STA 1148-1166 STR 25L IS NOT PER SRM DATA. INSTALLED EXTERNAL REPAIR DOUBLER IAW B727 SRM 53-30-3 FIG 3. 2L73 4F RTA3WE 20051130001672005113000167NM 2005 11 30 05FDEA03940 120051122A5330 REPAIR BOEING727 727233 138408ANM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25220FE 20934 AFT CARGO, DOUBLER CORRODED, BETWEEN STR 21 AND 22L, STA 1165. ALL WORK ACCOMPLISHED ON FED EX N/R N00243, ENTERED IN ERROR. 2L73 4F RTA3WE 20051130001722005113000172NM 2005 11 30 2005UALA01267 120051112A3350767 LIGHT BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE RT OVERWING INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29937UA 26668 RT OVERWING EMERGENCY LIGHT ON EXTERIOR OF FUSELAGE INOPERATIVE. REPLACED LAMP. 2L72 4F4 FRTA16WE E2GL 20051130001742005113000174NM 2005 11 30 2005UALA01269 120051113A3350 LAMP BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29942UA 26679 AFT EEL LIGHT INOP FRONT OF AFT GALLEY. RECONNECTED LAMP TO POWER CABLE. 2L72 4F4 FRTA16WE E2GL 20051130001762005113000176NM 2005 11 30 2005UALA01271 120051111A3397 CONNECTOR BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29182UA 25279 EMERGENCY LIGHTS INOPERATIVE AT DOOR 3L: SILL, ENTRY CEILING, EXIT SIGN AND SLIDE ILLUMINATED (BUSTLE). RESET CONNECTOR. 2L74 4F4 FRTA20WE E24NE 20051201000032005120100003NM 2005 12 1 2005UALA01276 120051115A3350 LIGHT BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE SEAT MOUNTED BROKEN A UALAK NONE L NO TEST ININSP/MAINT 1 WP29668UA 30024 FOUND SEAT MOUNTED EMERGENCY AISLE LIGHTS BROKEN AT SEATS 28AB AND 29HJ. REPLACED EMERGENCY LIGHT ASSY. 2L72 4F4 FRTA1NM E24NE 20051201000052005120100005WP 2005 12 1 AALA20050759 120051119A3510 OXYGEN BOTTLE DOUG DC9 DC982 3022082WP COCKPIT DISCHARGED A AALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW21237AA 49253 INFLIGHT CREW OXYGEN PRESSURE DROPPED TO ZERO PSI IN CRUISE. REPLACED CREW OXYGEN CYLINDER AND FIRST OFFICER OXYGEN REGULATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051201000062005120100006NM 2005 12 1 AALA20050755 120051117A2760 ACTUATOR BOEING757 757223 1384957NM SPEED BRAKES INOPERATIVE A AALAO OTHER O OTHER LDLANDING 1 SW21658AA 24616 INFLIGHT - AUTO SPEEDBRAKES FAILED TO DEPLOY ON LANDING. REPLACED AUTO SPOILER ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20051201000072005120100007WP 2005 12 1 AALA20050756 120051117A4920 APU DOUG DC9 DC982 3022082WP APU BAY FAILED A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21586AA 53249 INFLIGHT - DURING CLIMB AND HIGH POWER SETTING SMOKE/HAZE IN BOTH CABIN AND COCKPIT. SMOKE/HAZE WOULD ONLY DISSAPATE DURING LOWER POWER SETTINGS. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED APU. SYSTEM GROUND CHECKED NORMAL OPERATIONS. 2L72 4F A6WE 20051201000092005120100009NM 2005 12 1 AALA20050757 120051117A3350 BATTERY PACK BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21359AA 24040 DFW - LEFT AFT EXTERNAL EMERGENCY LIGHT AT SEAT 38G INOPERATIVE. REPLACED BATTERY PACK FOR LEFT AFT EXTERNAL EMERGENCY LIGHT AT 38G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20051201000102005120100010NM 2005 12 1 AALA20050762 120051118A3397 CONNECTOR BOEING767 767323 1385205NM EMERGENCY LIGHT DISCONNECTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21398AN 29605 DFW - EMERGENCY LIGHTS AT SEAT 33D INOPERATIVE. SECURED CONNECTOR UNDER SEAT FOR EMERGENCY LIGHTS AT SEAT 33D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20051201000132005120100013NM 2005 12 1 QXEA200501553 120051121A3040 HEATER BOMBDRDHC8 DHC8402 1390042NM WINDSHIELD MALFUNCTIONED A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09415QX 4081 SEA FLIGHT NR 2350, WHEN SELECTING WINDSHIELD HEAT ON, NR 1 AC GEN KICKS OFF. MAINTENANCE PERFORMED OPS TEST OF THE AC VARIABLE FREQ GENERATION SYSTEM IAW Q400 AMM TASK 24-21-00-710-801. ALSO, PERFORMED OPS TEST OF THE PILOT WINDSHIELD ANTI-ICING SYSTEM IAW Q400 AMM TASK 30-41-00-710-801 AND OPS TEST OF THE CO-PILOT WINDSHIELD AND PILOT SIDE WINDSHIELD IAW Q400 AMM TASK 30-41-00-710-802. ALL CHECKS GOOD AND NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051201000152005120100015NM 2005 12 1 AWXA200501454 120051111A5347D5337111200400 SEAT TRACK AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28660AW 1234 SAL - MAJOR REPAIR - DURING BC4 CHECK DISCOVERED LEVEL 2 CORROSION ON SEAT TRACK AT FR41+3" AND Y1292. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 103. REMOVED AND REPLACED SEAT TRACK FROM FR41 TO FR36 AND Y1292. 2L72 4F RTA28NM 20051201000192005120100019NM 2005 12 1 2005UALA01282 120051115A3350 LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE ROW 15 AFT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29335UA 24230 EMERGENCY EEL STRIP LIGHTING INOP FROM ROW 15 AFT. STRIP REPLACED. 2L72 4F4 FRTA16WE E2GL 20051201000212005120100021EU 2005 12 1 2005UALA01284 120051112A2910 RAM AIR TURB AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE RAT NO TEST A UALAK NONE L NO TEST ININSP/MAINT 1 WP29434UA 592 RAT TEST FAILED AS PER EQ3073. GREEN GOV LIGHT WILL NOT ILLUMINATE DURING TEST. REPLACED RAT GRD CHK MODULE IAW MM, DID NOT HELP. REPLACED RAT PER 29-22-51, NEEDS OPS CHK & LEAK CHK TO BE COMPLETED. INSPECTED INSTALLATION. 2L72 4F4 FRTA28NM E40NE 20051201000252005120100025NM 2005 12 1 2005UALA01288 120051117A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE 5R DOOR INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29107UA 26900 EMERG LT INOP DOOR 5R SLIDE ILLUM. REPLACED LIGHT ASSY. 2L74 4F4 FRTA20WE E24NE 20051201000282005120100028NM 2005 12 1 2005UALA01290 120051117A5310 CREASE BEAM BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE BS 957-1010 CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29921UA 25388 AFT CABIN RT CREASE BEAM CORRODED AT STA 957 TO 1010 RBL 53 AT STRINGER 17R FLOOR AREA. REMOVED & REPLACED CREASE BEAM REF SRM 51-40-02. 2L72 4F4 FRTA16WE E2GL 20051201000292005120100029NM 2005 12 1 2005UALA01291 120051117A5313 CREASE BEAM BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU BS 293-335 CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29921UA 25388 CORROSION FOUND AT CREASE BEAM STA 293 TO 335 RBL 56 AT STRINGER 17L AT WL 207. REMOVED & REPLACED CREASE BEAM REF SRM 51-40-02 2L72 4F4 FRTA16WE E21EU 20051201000302005120100030NM 2005 12 1 2005UALA01292 120051117A5330 SKIN BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE BS 288 STR 2L GOUGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29921UA 25388 EXTERNAL FUSELAGE SKIN AT STA 288 STR 2L AND STR 3L HAS 4 EACH GOUGES. REMOVED DAMAGE, NDT VERIFIED DAMAGE REMOVAL, INSTALLED DOUBLER,TRIPLER AND STRAPS PER SRM 53-00-01 REPAIR NR 31 2L72 4F4 FRTA16WE E2GL 20051201000312005120100031NM 2005 12 1 2005UALA01293 120051117A3350 LAMP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE ROW 17 AFT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29314UA 23675 EEL LIGHTS INOP FROM ROW 17 AFT. REPLACED EEL CABLE AND MOST AFT LAMP. 2L72 4F4 FRTA16WE E2GL 20051201000332005120100033NM 2005 12 1 2005UALA01295 120051118A3350 BULB BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29195UA 26899 RT OVERWING FAIRING EMER LT 2ND FROM AFT HAS ONE BULB INOP. REPLACED LAMP. 2L74 4F4 FRTA20WE E24NE 20051201000352005120100035NM 2005 12 1 2005UALA01297 120051118A3350 CONNECTOR BOEING747 747422 1384935NM PWA 4056 PW4056 NE ROW 56R UNSECURE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29195UA 26899 EMERGENCY EEL LIGHT AT SEAT ROW 56R INOP. RESECURED EEL LIGHT CONNECTOR. 2L74 4F4 FRTA20WE E24NE 20051201000382005120100038WP 2005 12 1 05FDEA03955 120051124A5330 REPAIR DOUG DC10 DC1010F 3022111WP BS 859 PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 FWD OF FWD CARGO DOOR STA 859 BETWEEN STRINGERS 36 AND 37 ON THE RT SIDE THERE IS AN INTERNAL DOUBLER REPAIR. PERFORMED A INSPECTION OF REPAIR IAW EA#8-5330-93229 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO#8-5100-7-5001-P1 E3. 2L73 4F A22WE 20051201000392005120100039CE 2005 12 1 DJFA2005167 120051123A2430 GENERATOR BEECH MU300 400A 1155402CE MALFUNCTIONED E DJFAHA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING HGJELECT. POWER LOSS-50 PC MULTIPLE FAILURE WARNING INDICATION CRCRUISE 1 EA23744TA RK245 KPGD - KSGR TRIP ID NR 935498, APPROXIMATELY 125 NM FROM KSGR BOTH LEFT AND RIGHT GENERATORS WERE CYCLING ON AND OFF ONE AT A TIME. AN EMERGENCY WAS DECLARED AND THE CREW BEGAN A DESCENT TO DIVERT INTO KBPT. RADIOS AND OTHER ELECTRICAL EQUIPMENT WERE TURNING OFF AND ON AS THE GENERATORS CYCLED. THE CREW TURNED THE RIGHT RADIOS OFF PRIOR TO THE START OF THEIR DESCENT AND WITH THE RADIOS TURNED OFF, THE GENERATORS STAYED ON. THE DECLARATION OF AN EMERGENCY WAS CANCELLED BY THE CREW. THE AIRCRAFT WAS THEN DIVERTED TO KHOU AND LANDED WITHOUT FURTHER INCIDENT. 2H72 4F RTA16SW 20051201000452005120100045WP 2005 12 1 05FDEA03957 120051124A5330 REPAIR DOUG DC10 DC1010 3022110WP BS 879 IMPROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LWR FUSELAGE LT SIDE ON SKIN FOUND 1 REPAIR EXISTING AT STA 879 BETWEEN L48 TO L43 . REMOVED PORTION SKIN AT STA 850 TO STA 900 BETWEEN L36 TO L48 LT SIDE IAW SRM 53-20- 00 FIG 17 PER EA NR 8-5330-90128. FABRICATED AND INSTALLED P/N' S F148375/3; -5; -7; -9; -11; - 13, -15; -17 IAW SRM 53-20-00 FIG 17 SHT 1-3-4-5-6-7 EA NR 8-5330-90128. REMOVED DAMAGED SHEAR CLIP AND TEAR CLIP. FABRICATED AND INSTALLED NEW PARTS IAW SRM 53-30-00 FIG 9 AND FIG 18 VOL 1. 2L73 4F A22WE 20051201000502005120100050NE 2005 12 1 10252005A 320051024A614010223N0 INDICATOR SAAB SF340 340B 7860101EU HAMSTD14RF 14RF19 NE PROP RPM MALFUNCTIONED A NSVAO OTHER O OTHER CRCRUISE 1 EA27341CJ 341 LEFT PROP RPM DROPPED 300 RPM IN FLIGHT, UNABLE TO SYNC, AFTER LANDING. LT PROP RPM DROPPED TO 0. REMOVED AND REPLACED PROP RPM GAUGE PN ON/OFF 10223N0, SN ON 237, SN OFF 165 OPS CHECK GOOD. 2L72 4T RTA52EU 6 CP11NE 20051201000512005120100051CE 2005 12 1 11012005A 120051028A61235038912121 AUTOFEATHER SYS BEECH 1900 1900D 1154162CE LT ENGINE MALFUNCTIONED A NSVAO OTHER J WARNING INDICATION CRCRUISE 1 EA27243CJ UE43 IN FLIGHT, LEFT ENGINE AUTOFEATHER LIGHTS LIGHTS EXTINGUISHED WITH POWER AT 3750 TORQUE. REMOVED AND REPLACED LT ENGINE AUTOFEATHER PRESSURE SWITCH PN 50-389121-21, SN ON 10015, SN OFF UNKNOWN. 2L72 4T RTA24CE 20051201000522005120100052CE 2005 12 1 11022005A 120051028A2750SM50D7 RELAY BEECH 1900 1900D 1154162CE TE FLAPS FAILED A NSVAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 EA27152MJ UE52 FLAPS STUCK AT 17 DEGREES. REMOVED AND REPLACED FLAP CONTROL RELAY OPS CHECK NORMAL, P/N SM50D7. 2L72 4T RTA24CE 20051201000552005120100055EU 2005 12 1 11112005A 120051103A28207228306562 TUBE SAAB SF340 340B 7860101EU FUEL SYSTEM LEAKING A NSVAK NONE K FLUID LOSS ININSP/MAINT 1 EA27356CJ 356 DURING LINE CHECK AFTER STRUCTURAL INSPECTION FOUND FUEL LEAKING FROM RIGHT INBOARD DRY BAY DRAIN HOLE. FURTHER INSPECTION REVEALED TO BE A SMALL PIN HOLE IN THE RIGHT STANDBY FUEL PUMP WIRE CONDUIT (TUBE ASSEMBLY). REMOVED AND REPLACED RT STANDBY FUEL PUMP TUBE ASSEMBLY IAW SAAB MM 28-22-1, NO LEAKS NOTED. 2L72 4T RTA52EU 20051201000562005120100056EU 2005 12 1 11172005A 120051114A3150 WARNING SYSTEM SAAB SF340 340B 7860101EU CONFIGURATION FALSE ACTIVATIONA NSVAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 EA27202SR 202 ABORTED TAKEOFF DUE TO CONFIG WARNING DURING TAKEOFF. PERFORMED OPERATIONAL TEST OF TAKEOFF CONFIG WARNING. NO DEFECTS NOTED AT THIS TIME, OPS CHECK GOOD. 2L72 4T RTA52EU 20051201000582005120100058EU 2005 12 1 11182005A 120051117A6120 B-NUT SAAB SF340 340B 7860101EU P3 SWITCH DRAIN LOOSE A NSVAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 EA27321CJ 321 ON TAKEOFF ROLL, AUTOCOARSEN HIGH LIGHT DID NOT ILLUMINATE WITH TORQUE SET TO 80%. REPLACED AUTOCOARSEN COMPUTER FOR TROUBLESHOOTING AND DID NOT CORRECT THE PROBLEM. REINSTALLED ORIGINAL COMPUTER. REPLACED AUTOCOARSEN SWITCHES FOR TROUBLESHOOTING AND DID NOT CORRECT THE PROBLEM EITHER. REINSTALLED ORIGINAL SWITCHES. REMOVED AND REPLACED LEFT AND RIGHT AUTOCOARSEN P3 SENSE SWITCHES, RELAY 44K AND 43K. DID NOT FIX PROBLEM, REINSTALLED ORIGINAL PARTS IN RESPECTIVE PLACES. RESECURED P3 SWITCH DRAIN TUBE B-NUT ON RT ENGINE. PERFORMED AUTOCOARSEN, OPS CHECK IAW 61-22-00, ALL CHECKS GOOD, OK FOR RETURN TO SERVICE. 2L72 4T RTA52EU 20051201000592005120100059WP 2005 12 1 ARWA20051101 120051111A2720 CONTROL CABLE DOUG DC8 DC863F 302198FWP RUDDER SHUTOFF DAMAGED A ARWAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO19661AV 45969 DURING PRE-FLIGHT, FOUND RUDDER POWER LEVER STIFF; "RUDDER CONTROL MANUAL" LIGHT REMAINS ILLUMINATED WITH LEVER IN "ON" POSITION. REMOVED AND REPLACED RUDDER SHUT-OFF VALVE CONTROL CABLE RUN NR 67-C IN ACCORDANCE WITH DC8 M/M 27-22-1; RIGGED AND OPERATIONAL CHECK FOUND NORMAL IN ACCORDANCE WITH DC8 M/M 27-20-00. 2L74 4F 4A25 20051201000612005120100061EU 2005 12 1 05FDEA03902 120051119A78302210727135 ACCESS DOOR AIRBUS300 A300B4622R 3930312EU ZONE 500 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25720FD 417 COMPLY WITH EA 6-7830-92360, THRUST REVERSER NR 1 INBD T/R ACCESS DOOR GOUGE REPAIR. COMPLIED WITH EA 6-7830-92360. 2L72 4F RTA35EU 20051201000622005120100062WP 2005 12 1 05FDEA03903 120051118A3260 INDICATION SYS DOUG DC10 DC1030F 3023504WP MLG MALFUNCTIONED A FDEAO OTHER N FALSE WARNING DEDESCENT 1 SO25312FE 48300 OAK - LEFT MAIN GEAR UNSAFE IN UP POSITION ON BOTH MAIN GEAR INDICATOR AND SYNOPTIC DURING DESCENT. ACCOMPLISHED RED TAB PROCEDURES, BOTH INDICATIONS NML. INTERROGATED CFDS FOUND PSEU LT GEAR UP AND LATCHED A/B SENSOR DISAG INTER. FAULT MSG(317075) FAULT CODE(32-60-07) AS PER MD10 FIM PERFORMED LEFT MLG PROX SENSOR TEST REF:32-61-15-5. JACKED A/C REF AND SWUNG LEFT MAIN GEAR PERFORMED PROX SENSORS INDUCTANCE TEST REF:MD10-30 M.M.32-61-15-5. PSEU SHOWED SENSORS OK AND INDUCTANCE VALUES WERE ALL WITHIN LIMITS. VISUALLY CKD SENSORS AND TARGETS NO DEFECTS NOTED. AS PER ABOVE FIM CHECKED PSEU CURRENT FAULTS AFTER GEAR SWING, NO FAULTS NOTED. REMOVED A/C FROM JACKS AND RESTORED TO NORMAL. 2L73 4F RTA22WE 20051201000642005120100064NM 2005 12 1 05FDEA03905 120051119A5330 REPAIR DOUG MD11 MD11 3023602NM ZONE 100 MISMANUFACTURED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25524FE 48480 LOWER FUSELAGE FWD CARGO DOOR CUTOUT AFT LOWER AREA FOUND WITH EXISTING REPAIR. EXISTING REPAIR ON LOWER FUSELAGE FORWARD CARGO DOOR CUTOUT AFT LOWER AREA EVALUATED AND FOUND NOT IAW SRM 53-50-00, FIGURE 16, VOLUME I. EXISTING REPAIR REMOVED AS PER SRM 51-33-01 VOLUME II, AND NEW REPAIR CARRIED OUT AS PER SRM 53-50-00, FIGURE 16, VOLUME I. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2- 100. 2L73 4F RTA22WE 20051201000652005120100065NM 2005 12 1 05FDEA03907 120051119A5320 FLOOR SUPPORT DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 LONGITUDINAL FLOOR SUPPORT FROM STA 1911 TO 2007 APPROX X=18 FOUND UPPER SURFACE CORROSION AT SEVERAL LOCATION. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051201000672005120100067NM 2005 12 1 05FDEA03909 120051119A5320 FLOOR SUPPORT DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 CABIN LONGITUDINAL FLOOR SUPPORT FROM STA 1911 TO 2007 APPROX AT X= 75 UPPER AND LOWER SURFACE SEVERAL LOCATION FOUND CORROSION. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2L73 4F RTA22WE 20051201000682005120100068CE 2005 12 1 JBJA20050006 120051117A3260 UPLOCK SWITCH LEAR 35 35A 5170602CE MLG LOOSE E JBGAO OTHER N FALSE WARNING CLCLIMB 1 GL07357LJ 357 INBOARD GEAR DOOR LIGHTS WOULD NOT EXTINGUISH AFTER TAKEOFF OUT OF BNA, CYCLED GEAR THEN EVERY THING NORMAL. AFTER GETTING TO HEN GOT A FERRY PERMIT TO GO TO BAL FOR MAINTENANCE TO LOOK AT GEAR OPERATION. INSTALLED NEW RIVETS IN LOOSE LEFT INBOARD DOOR UNLOCK SWITCH MAINTOPS CHECKS GOOD. 2L72 4F A10CE 20051201000822005120100082 2005 12 1 SWIA200515874 420051115A3418C12851BA01 COMPUTER CNDAIRCL600 CL6002B19 1900309EA STALL WARNING NO TEST A SWIAO OTHER L NO TEST NRNOT REPORTED 1 NM07983SW 7961 STALL TEST FAIL, FFOD CHECK. REPLACED STALL COMPUTER IAW 27-35-01, OPERATIONAL CHECK GOOD, PN C12851BA01 SN OFF 521. 2L72 4F RTA21EA 20051201000832005120100083EA 2005 12 1 SWIA200515875 120051117A3350 CHARGER CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07732SK 10194 EMERGENCY EXIT SIGNS WON'T ILLUMINATE ON FORWARD BULKHEAD. REPLACED NR 2 EMERGENCY LIGHT BATTERY CHARGER IAW CRJ 700 AMM 33-51-17. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051201000862005120100086NE 2005 12 1 ARWA20051102 220051117A7230 BLADES DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE NR 4 ENGINE DAMAGED A ARWAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SO19661AV509962626 45969 671240 UPON ENGINE SPOOL UP FOR TAKEOFF, NR 4 ENGINE COMPRESSOR STALLED. PERFORMED BOROSCOPE TO NR 4 ENGINE; FOUND BLADES DAMAGED, SECURED NR 4 ENGINE FOR FERRY FLIGHT IN ACCORDANCE WITH ARROW GMM 6-3-4/5. 2L74 4F4 F 4A25 1E8 20051201000872005120100087NM 2005 12 1 05FDEA03922 120051119A5347 SEAT TRACK DOUG MD11 MD11 3023602NM BS 879-899 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 MAIN DECK, CORROSION FOUND ON SEAT TRACK UPPER FLANGE BETWEEN STA 879 TO 899 AT X=8.5. REPAIR CARRIED OUT IAW SRM 53-70-00. 2L73 4F RTA22WE 20051201000892005120100089NM 2005 12 1 05FDEA03925 120051121A5754 SKIN DOUG MD11 MD11 3023602NM ZONE 600 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 RIGHT WING, NR 3 SLAT LEADING EDGE FOUND DENTED. TRIMMED OUT AND REPAIRED AS PER SRM 57-10-00. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051201000912005120100091NM 2005 12 1 MWEA050126 120051120A3260 SEAL BOEING717 717200 1383700NM PIN LEAKING A MWEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31924ME 55190 NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. PERFORMED BENCH LEAK CHECK OF NOSE LANDING GEAR SHOCK STRUT, FOUND LEAK TO BE AT UPPER METERING PIN SEAL. REMOVED AND REPLACED PIN SEAL. 2L72 4F TRA6WE 20051201000952005120100095NM 2005 12 1 DL76S050692 120050810A5711112T508610 SPAR BOEING767 767332 1382001NM WING CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27116DL 23275 FRONT SPAR AND WING LEADING EDGE RIB HAS CRACK INDICATION. HOLE WAS OVERSIZED TO REMOVE THE CRACK PER ER/A 450059-14AD, REF AD 2004-16-12 AND 01-074906-03AD. 2L72 4F RTA1NM 20051201000982005120100098NM 2005 12 1 DL777050696 120051112A2121 FAN BOEING777 777232 1385232NM CABIN AIR SEIZED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27861DA 29952 RECIRC FAN STATUS MESSAGE, PAX AND FLIGHT ATTENDANTS NOTICED ELEC SMELL IN CABIN. MAINT INFO DISPLAY SHOWED AFT UPPER RECIRC FAN OFF. TURNED UPPER RECIRC FAN OFF AND ODOR CLEARED. SUSPECT UPPER AFT RECIRC FAN FAILED. REPLACED SAME. 2L72 4F RTT00001SE 20051201001032005120100103NM 2005 12 1 DL764050705 120051110A2781851801 SENSOR BOEING767 767432ER 1385134NM SLAT SYSTEM MALFUNCTIONED A DALAO OTHER J WARNING INDICATION APAPPROACH 1 SO27839MH 29712 L/E ASYM MESSAGE DURING DESCENT BEFORE 250 KTS. FOLLOWED QRH PROCEDURES. HIGHEST BRAKE TEMP AT 6.0 NR 6 BRAKE. T/S PER FIM 27-81-00 FIG 107 PSEU FAULTS S295 TARGET FAR FAILURE WITH FAILURE LIGHT ON. REPLACED SENSOR S295 AND CHECKED PER MM. 2L72 4F RTA1NM 20051201001042005120100104NM 2005 12 1 DL75A050706 120051020A5330143N33203 SKIN BOEING757 757212 1384951NM BS 600-630 S17L DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27751AT 23125 THE FUSELAGE SKIN WAS DENTED FORWARD OF THE L2 DOOR BY JETWAY. DENT IS AT BS 610 ABOVE S17L AND IS 1.75 INCH DIA BY 1.1 INCH DEEP. INSTALLED DOUBLER PER ER/A 451214-14 AND INCORPORATED EXISTING REPAIR. 2L72 4F RTA2NM 20051201001052005120100105NM 2005 12 1 DL76K050709 120051113A5512182T32002 SKIN BOEING767 767332 1382001NM HORIZONTAL STAB GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27173DZ 29692 RT HORIZONTAL STABILIZER / UPPER SKIN AT RIB 12, S-5 / REPAIR OF GROUND DAMAGE. GOUGE DUE TO GROUND DAMAGE WAS CUT OUT OF THE RT HORIZONTAL STABILIZER UPPER SKIN AT RIB 12 AND S-5. AN ALUMINUM EXTERNAL DOUBLER IS INSTALLED WITH HI-LOKS TO REPAIR THE DAMAGE. 2L72 4F RTA1NM 20051201001112005120100111WP 2005 12 1 AALA20050769 120051122A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21255AA 49287 SFO - EMERGENCY LIGHTS IN FORWARD CEILING AT ENTRY, SERVICE DOOR AND COCKPIT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN FORWARD CEILING AT ENTRY, SERVICE DOOR AND COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051201001152005120100115WP 2005 12 1 AALA20050782 120051127A33508039001 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW219677W 53627 LGA - EMERGENCY LIGHTS FROM FORWARD TO AFT INOPERATIVE. REPLACED BATTERY PACK IN AFT CARGO FOR EMERGENCY LIGHTS FROM FORWARD POSITION TO AFT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20051201001172005120100117EU 2005 12 1 AALA20050775 120051123A3350P4010049 BATTERY PACK AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2111060 470 EMERGENCY LIGHTS IN FORWARD RT ZONE INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN FORWARD RT ZONE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20051201001182005120100118NM 2005 12 1 SWAA053806 120051129A53126517582 BULKHEAD BOEING737 7373G7 1384595NM BS 178 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29683SW 24008 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE VERTICAL BEAM WEB CRACKED AT BS 178 BULKHEAD, LBL 5.7, WL 179. REMOVED AND REPLACED VERTICAL BEAM WEB PER SRM. 2L72 4F RTA16WE 20051201001192005120100119NM 2005 12 1 SWAA053792 120051128A335007912 COVER BOEING737 7377H4 1384404NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29204WN 29855 DURING SCHEDULED MV2 CHECK, FOUND FWD EEPLS STRIP COVER MISSING. INSTALLED COVER PER MM. 2L72 4F RTA16WE 20051201001202005120100120NM 2005 12 1 SWAA053793 120051128A33509250071 BULB BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29209WN 32484 DURING SCHEDULED RON CHECK, FOUND EGRESS LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20051201001222005120100122NM 2005 12 1 SWAA053795 120051127A57536546435 SKIN BOEING737 7373H4 1384600NM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29354SW 25219 DURING SCHEDULED C3 CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED AT INBOARD AFT EDGE. REPAIRED AFT FLAP PER SRM. 2L72 4F RTA16WE 20051201001242005120100124 2005 12 1 SWAA053797 420051129A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29391SW 27378 DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051201001252005120100125NM 2005 12 1 SWAA053798 120051128A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29409WN 27896 DURING SCHEDULED HC1 CHECK, FOUND EEPLS TRACK COVER CRACKED AT ROW 1 ABC. REMOVED AND REPLACED COVER PER MM. 2L72 4F RTA16WE 20051201001282005120100128NM 2005 12 1 SWAA053801 120051129A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM BS 787 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, LBL 2 TO RBL 7. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051201001312005120100131NM 2005 12 1 SWAA053804 120051129A275118173810 TRANSMITTER BOEING737 7377H4 1384404NM RT WING FLAP FAULTY A SWAAA UNSCHED LANDING O OTHER APAPPROACH 1 SW29742SW 29278 DIVERSION / DECLARED EMERGENCY. T/E FLAPS WOULD NOT EXTEND PAST POSITION 1. REMOVED AND REPLACED RT FLAP POSITION TRANSMITTER PER MM. 2L72 4F RTA16WE 20051201001322005120100132NM 2005 12 1 SWAA053805 120051128A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29763SW 27877 DURING SCHEDULED HC2 CHECK, FOUND EEPLS STRIP WORN AT ROW 13 DEF. REMOVED AND REPLACED STRIP PER MM. 2L72 4F RTA16WE 20051201001342005120100134NM 2005 12 1 05FDEA04008 120051129A5753 FLAP TRACK BOEING727 727227 1384078NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 LEFT WING INBOARD FLAP OUTBOARD TRACK AFT MOUNT BOLT HOLES (BORES) HAVE CORROSION. REMOVED CORROSION BY REAMING FROM BORES G AND F WITH FINAL DIAMETER OF .3765 INCH FOR HOLE F AND .3765 INCH FOR HOLE G. FABRICATED REPAIR BUSHINGS FROM 15-5 PH STEEL PO 453539.1. HEAT TREATED BUSHINGS IAW BAC OVERHAUL MANUAL 57-40-01 AND CAD PLATED BUSHINGS IAW QQP-416 TYPE II CLASS 2 ON PO 510636.1. INSTALLED AND FINAL REAMED BUSHINGS TO .316 INCH ON BORES F AND G IAW BAC OVERHAUL MANUAL 57-40-01. 2L73 4F A3WE 20051201001362005120100136WP 2005 12 1 AALA20050777 120051123A33504TL115 SWITCH DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21431AA 49343 LAX - EMERGENCY LIGHTS IN SEATS INOPERATIVE. REPLACED SWITCH FOR FORWARD FLIGHT ATTENDANT EMERGENCY LIGHT PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051201001382005120100138WP 2005 12 1 AALA20050784 120051128A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21501AA 49738 ORD - CEILING EMERGENCY LIGHTS BETWEEN ROWS 13 AND 19 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS BETWEEN ROWS 13 AND 19. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051201001402005120100140NM 2005 12 1 DL73S050680 120051103A53156545410366 FLOORBEAM BOEING737 737247 138448DNM LBL 0.07 BS 660 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27243WA 23517 CRACKS WERE FOUND IN THE LBL 0.07 FLOORBEAM UPPER CHORD AT THE FLOOR PANEL ATTACH HOLES BETWEEN BS 660-663. CHORD WAS REPAIRED AND MODIFIED PER ER/A 451389-14. REF S/B 737-57-1210 AND 3-062982-03AD. 2L72 4F A16WE 20051201001422005120100142NM 2005 12 1 DL757050682 120051104A335020121 POWER SUPPLY BOEING757 757232 1384965NM L-4 DOOR INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27675DL 25980 LEFT SIDE L3 EMERGENCY LIGHT OUTSIDE ILLUMINATION LIGHT INOP. RELAMPED, NO HELP. REPLACED M737 POWER SUPPLY, CHECKS OK. 2L72 4F RTA2NM 20051201001442005120100144NM 2005 12 1 DL76L050684 120051107A2530 OVEN BOEING767 767332 1382001NM GALLEY CONTAMINATED A DALAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO27197DN 28454 SIGNIFICANT WATER LEAK AFT GALLEY BEHIND OVENS. RTB. REMOVED OVENS LT SIDE OF AFT GALLEY. INSPECTED AREA AROUND OVENS, FOUND SMALL AMOUNT OF WATER IN OVENS BUT NOT OUTSIDE OF OVENS. CLEANED UP AREA. NO LEAKS NOTED. 2L72 4F RTA1NM 20051201001452005120100145NM 2005 12 1 DL76L050685 120051107A3350 BULB BOEING767 767332 1382001NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27185DN 27961 SEAT 4FG EMERGENCY AISLE LIGHTS INOP. RELAMPED, OPS OK. 2L72 4F RTA1NM 20051201001462005120100146NM 2005 12 1 DL757050687 120051019A5330143N3320 SKIN BOEING757 757232 1384965NM STA 600 STR 16L DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27670DN 25331 FUSELAGE SKIN DENTS AND GOUGES BETWEEN STA 585-610 AND STR 15L-18L. THE DAMAGED SKIN IS CUT OUT IN TWO LOCATIONS AND AN EXTERNAL ALUMINUM DOUBLER IS INSTALLED PRIMARILY WITH SOLID ALUMINUM RIVETS. 2L72 4F RTA2NM 20051201001472005120100147 2005 12 1 DLM90050688 420051108A2565105508201 SLIDE DOUG MD90 MD9030 3023690NM TAIL NO TEST A DALAK NONE L NO TEST ININSP/MAINT 1 SO27908DA 53388 PERFORMED OPN 6900 AND SLIDE DID NOT DEPLOY. ADJUSTED AFT STRAPS PER FIG 18 AND SLIDE DEPLOYED AS REQUIRED. 2L72 4F RTA6WE 20051201001482005120100148NM 2005 12 1 DL75K050689 120051103A5330 REPAIR BOEING757 757232 1384965NM STA 1350, STR-1 MISINSTALLED A DALAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO27614DL 22821 FUSELAGE / SKIN / STA 1340-1360, STR 1-2R / SKY RADIO ANTENNA REPAIR. THE ORIGINAL REPAIR INSTALLED BY ER/A 385126-14 WAS REMOVED AND THE CUTOUT IN THE FUSELAGE SKIN WAS ENLARGED TO REMOVE KNIFE EDGED HOLES AND FASTENER HOLES WITH TOO TIGHT SPACING. AN ALUMINUM DOUBLER AND TRIPLER WERE INSTALLED EXTERNALLY OVER THE CUTOUT WITH SOLID ALUMINUM RIVETS. 2L72 4F RTA2NM 20051201001492005120100149WP 2005 12 1 IXXA05RNG110S 120050924A5730 SKIN DOUG DC8 DC872 302199BWP STA XW700 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK WAS FOUND A CORROSION AND BONDED DOUBLER DELAMINATED ON LT WING INTERIOR UPPER SURFACE T/E, STA XW 700 - XW 736.500.SKIN WAS REPLACED IAW MFG DRAWING 5644654, RIVETS WERE INSTALLED IAW SRM 51-1-21 PAGE 1-7 AND ANTI-CORROSIVE TREATMENT WAS APPLIED IAW SRM 51-1-8 PAGE 13-16. 2L74 4F RT4A25 20051201001522005120100152 2005 12 1 BSYA2005019 420051115A2300066106200 TRANSPONDER BEECH 58 58 1152740CE NR 1 BROKEN E BSYAA UNSCHED LANDING O OTHER CLCLIMB 1 GL071859K TH1299 AIRCRAFT TOOK OFF, COULD NOT TRANSMITT FROM EITHER COMM. RADIO. FOUND PILOTS PUSH TO TALK SWITCH BROKEN, CO-PILOTS PUSH TO TALK DID WORK AND THERE WAS A HAND MIC IN GLOVE BOX. AIRCRAFT ALSO HAD A MODE (C) PROBLEM. AIRCRAFT RETURMED TO DEPARTURE, NR 1 TRANSPONDER WAS OK, NR 2 TRANSPONDER INTERMITTENT MODE (C) REMOVED AND REPLACED TRANSPONDER OPS. CHECKS GOOD. 1L72 3O 3A16 20051201001562005120100156WP 2005 12 1 IXXA05RNG111S 120050925A5753 PANEL DOUG DC8 DC872 302199BWP ZONE 600 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK WAS FOUND A CORROSION ON RT WING FLAP IB INTERIOR TRAILING EDGE PANEL PLATING. SKIN WAS REPLACED IAW MFG DRAWING 5652277 AND RIVETS WERE INSTALLED IAW SRM 51-1-21 PAGE 1-7. 2L74 4F RT4A25 20051201001582005120100158WP 2005 12 1 IXXA05RNG113S 120050928A5753 PANEL DOUG DC8 DC872 302199BWP STA XF 415 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK WAS FOUND A CORROSION ON LT OB FLAP T/E PANEL LWD INNER SKIN, STA XF 415. SKIN WAS REPLACED IAW MFG DRAWING 5654758 (STA XW 407-XF415) AND RIVETS WERE INSTALLED IAW SRM 51-1-21 PAGE 1-7. 2L74 4F RT4A25 20051201001602005120100160WP 2005 12 1 IXXA05RNG115S 120050928A5753 SKIN DOUG DC8 DC872 302199BWP STA XW3-91 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK WAS FOUND A CORROSION ON LT IB FLAP T/E PANEL LWD OUTER SKIN, STA XW3 TO XW91.LT IB FLAP T/E PANEL LWD OUTER SKIN WAS REPLACED IAW MFG DRAWING 5652277, AND RIVETS WERE INSTALLED IAW SRM 51-1-21 PAGE 1-7. 2L74 4F RT4A25 20051201001622005120100162EA 2005 12 1 HNAA050098 120051128A6120 BETA LOCKOUT DHAV DHC8 DHC8311 1386006EA PWA PW120 PW123 NE NR 2 ENGINE FAILED A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07337EN 284 ON CLIMB OUT THE NR 2 ENGINE BETA LOCKOUT FAILED ASSOCIATED WITH NR 2 TORQUE FLUCTUATING BETWEEN 70 TO 105 PERCENT. POWER REDUCED TO 900 RPM AND ENGINE STABILIZED. DEACTIVATED BETA LOCKOUT SYSTEM IAW. MEL PROCEDURES. REPLACED MICRO SWITCH 6141-S4. 2H72 4T4 TRTA13NM E20NE 20051201001642005120100164EU 2005 12 1 05FDEA03996 120051128A5330 SKIN AIRBUS310 A310 EU PWA JT9 JT9D* NE ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25450FE 162 2 GOUGES IN UPPER EXTERIOR FUSELAGE SKIN AT FR61 BETWEEN RT STRINGERS 3-4. CUT OUT DAMAGED AREA OF SKIN IAW A310-200 SRM 53-27-00. PERFORMED HFEC IAW NTM 51-10-08. NO CRACKS NOTED. INSTALLED DOUBLER REPAIR IAW A310-200 SRM 53-10-12 FIG. 228. 2L72 4F4 FRTA35EU E20EA 20051201001662005120100166NM 2005 12 1 05FDEA04028 120051129A5240 SKIN DOUG MD11 MD11 3023602NM PWA 4460 PW4460 NE SERVICE DOOR DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 SNRM N2641: CABIN - R4 DOOR EXTERIOR SKIN UPPER EDGE FOUND WITH DENT. CARRIED OUT REPAIR AS PER SRM 52-10-00. 2L73 4F4 FRTA22WE E24NE 20051201001682005120100168NM 2005 12 1 05FDEA04030 120051130A5330 REPAIR DOUG MD11 MD11 3023602NM PWA 4460 PW4460 NE BS 775-795 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 SNRM N1608: REFERENCE TO EO 1-5100-7-5001 PT1 - FORWARD CARGO - STA 775 TO 795 LONGERON 27R FOUND WITH EXISTING REPAIR. FOUND REPAIR PREVIOUSLY ACCOMPLISHED IN ACCORDANCE WITH MD11 SERVICE BULLETIN 53-042 R02. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. THIS IS NOT A REPORTABLE ISSUE, NO MALFUNCTION OR DEFECT. 2L73 4F4 FRTA22WE E24NE 20051201001712005120100171NM 2005 12 1 05FDEA04032 120051130A5347 SEAT TRACK DOUG MD11 MD11 3023602NM PWA 4460 PW4460 NE ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 STA 859 LBL 8 SEAT TRACK FOUND CORROSION. CARRIED OUT REPAIR AS PER SRM 53-70-00. 2L73 4F4 FRTA22WE E24NE 20051201001732005120100173WP 2005 12 1 IXXA05RNG094S 120051031A5730 SKIN DOUG DC8 DC872 302199BWP STA XFS 791.250 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK WAS FOUND A CORROSION ON UPPER SKIN AT OB EXTENDED LEADING EDGE AROUND STA. XFS 791.250 TO 816.000 - LT. DAMAGED AREA WAS CLEANED AND REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-2-1 FIGURE 38 AND EWO ATI-57-059. 2L74 4F RT4A25 20051201001842005120100184NM 2005 12 1 AWXA200501460 120051107A5210 SKIN BOEING737 7373G7 1384595NM GE CFM56 CFM563B1 13802NE DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 920 23779 MAJOR REPAIR - DURING C19 CHECK DISCOVERED THE R1 DOOR EXTERNAL SKIN CRACKED, .2 INCHES IN LENGTH, AT THE UPPER HINGE CUTOUT, UPPER CORNER. MAINTENANCE ROUTED OUT CRACK IAW (ER) NR 03-5211-05314-ES1. FABRICATED REPAIR DOUBLER AND UPPER HINGE COVER IAW ER NR 03-5211-05314-ES1. INSTALLED FABRICATED REPAIR PARTS AT R1 DOOR IAW ER NR 03-5211-05314-ES1. 2L72 4F4 FRTA16WE E2GL 20051201001882005120100188NM 2005 12 1 AWXA200501462 120051119A53406935352U14 STRINGER CLIP BOEING737 7373G7 1384595NM GE CFM56 CFM563B1 13802NE BS 847 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 MCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED STRINGER CLIP CRACKED, .50 INCHES IN LENGTH, AT BS 847 AND STRINGER 4L. MAINTENANCE REMOVED STRINGER CLIP AND INSTALLED NEW CLIP AT BS 847 AND STRINGER 4L IAW BOEING 737-300 SRM 51-40-02-G FIG 3, 8 AND 12. 2L72 4F4 FRTA16WE E2GL 20051201001902005120100190NM 2005 12 1 AWXA200501464 120051119A53406935352U14 STRINGER CLIP BOEING737 7373G7 1384595NM GE CFM56 CFM563B1 13802NE BS 727E CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 MAJOR REPAIR - DURING C19 CHECK DISCOVERED STRINGER CLIP CRACKED, .25 INCHES IN LENGTH, AT BS 727E AND STRINGER 4L. MAINTENANCE REMOVED STRINGER CLIP AND INSTALLED NEW CLIP AT BS 727E AND STRINGER 4L IAW SRM 51-40-02-G FIG 3, 8 AND 12. 2L72 4F4 FRTA16WE E2GL 20051201001922005120100192NM 2005 12 1 AWXA200501466 120051119A532065516989 SPLICE BOEING737 7373G7 1384595NM GE CFM56 CFM563B1 13802NE STRINGER CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 MAJOR REPAIR - DURING C19 CHECK DISCOVERED STRINGER 4L SPLICE CRACKED, .25 INCHES, AT BS 907. MAINTENANCE REMOVED AND INSTALLED NEW STRINGER SPLICE AT STR 4L AND BS 907 IAW SRM 51-40-02-0G FIGURES 3, 8 AND 12. 2L72 4F4 FRTA16WE E2GL 20051201001932005120100193NM 2005 12 1 AWXA200501467 120051104A53136545855101 STRINGER BOEING737 7373G7 1384595NM GE CFM56 CFM563B1 13802NE BS 969-996 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 MAJOR REPAIR - DURING C19 CHECK DISCOVERED CORROSION ON THE R2 INNER CHORD FROM BS 969-996, FROM WL 208-209 AND RBL 50. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-60-15-1A1 FIG 101. REMOVED AND INSTALLED NEW INNER CHORD FROM BS 969 TO BS 996, FROM WL 208 TO WL 209 AND BL 50R IAW SRM 51-40-02-0G FIGS 3, 4, 6, 8, 9 AND 12. 2L72 4F4 FRTA16WE E2GL 20051201001942005120100194NM 2005 12 1 AWXA200501468 120051101A5753 SKIN BOEING737 7373G7 1384595NM GE CFM56 CFM563B1 13802NE TE FLAP DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 MAJOR REPAIR - DURING C19 CHECK DISCOVERED DEBONDED AREA ON THE UPPER AND LOWER SURFACE OF THE LT OB AFT FLAP FROM WBL 230.68L TO WBL 234.68L, IB END. MAINTENANCE REMOVED AREA OF DEBOND IAW SRM 51-70-10-2R4 FIG 203. FABRICATED CORE AND REPAIR DOUBLER IAW SRM 57-53-02-0I FIG 1. BONDED FABRICATED REPAIR PARTS TO THE UPPER AND LOWER SURFACES OF THE LT OB AFT FLAP FROM WBL 230.68L TO WBL 234.68L IAW SRM 51-70-10-2R4 FIG 203. 2L72 4F4 FRTA16WE E2GL 20051201001952005120100195NM 2005 12 1 AWXA200501469 120051101A5753 SKIN BOEING737 7373G7 1384595NM GE CFM56 CFM563B1 13802NE TE FLAP DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 MAJOR REPAIR - DURING C19 CHECK DISCOVERED SKIN SEPARATED AT AFT IB CORNER OF THE RT OB AFT FLAP ASSEMBLY, UPPER AND LOWER SURFACE, FROM WBL 230.28R TO WBL 232.38R. MAINTENANCE REMOVED DISBONDED SKIN FROM UPPER AND LOWER SURFACE IAW SRM 51-70-10-2R4 FIG 203. FABRICATED REPAIR FILLERS AND DOUBLERS IAW SRM 51-70-10-2R4 FIG 203. BONDED REPAIR PARTS TO THE UPPER AND LOWER SURFACE OF THE RT OB AFT FLAP ASSEMBLY FROM WBL 230.28R TO WBL 232.38R IAW SRM 51-70-10-2R4. 2L72 4F4 FRTA16WE E2GL 20051201001962005120100196NM 2005 12 1 AWXA200501470 120051101A5753 SKIN BOEING737 7373G7 1384595NM GE CFM56 CFM563B1 13802NE TE FLAP DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 MAJOR REPAIR - DURING C19 CHECK DISCOVERED DEBOND AREA ON THE UPPER SURFACE OF THE RT OB FORE FLAP FROM WBL 306.61R TO WBL 308.61R. MAINTENANCE REMOVED DEBOND AREA ON THE UPPER SURFACE OF THE RT OB FORE FLAP IAW SRM 51-70-10-2R4. FABRICATED REPAIR DOUBLERS IAW SRM 51-70-10-2R4. BONDED REPAIR PARTS TO THE RT OB FORE FLAP FROM WBL 306.61R TO WBL 308.61R IAW SRM 51-70-10-2R4. 2L72 4F4 FRTA16WE E2GL 20051201001972005120100197NM 2005 12 1 AWXA200501471 120051101A5753 SKIN BOEING737 7373G7 1384595NM GE CFM56 CFM563B1 13802NE TE FLAP DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 MAJOR REPAIR - DURING C19 CHECK DISCOVERED DEBONDED AREA ON THE UPPER SURFACE OF THE LT OB FORE FLAP AT REPAIR DOUBLER, 88 INCHES FROM THE IB END. MAINTENANCE REMOVED DEBONDED AREA AT REPAIR DOUBLER AND DAMAGED HONEYCOMB CORE ON THE LT OB FORE FLAP IAW SRM 51-70-10-2R4. FABRICATED REPLACEMENT CORE AND REPAIR DOUBLER IAW SRM 51-70-10-2R4. BONDED FABRICATED REPAIR PARTS TO THE UPPER SURFACE OF THE LT OB FOREFLAP IAW SRM 51-70-10-2R4. 2L72 4F4 FRTA16WE E2GL 20051201001982005120100198NM 2005 12 1 AWXA200501472 120051118A53226558280511 SHEAR TIE BOEING737 7373G7 1384595NM GE CFM56 CFM563B1 13802NE BS 361 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 MAJOR REPAIR - DURING C19 CHECK DISCOVERED SHEAR TIE CRACKED, .75 INCHES IN LENGTH, AT BS 361, FROM WL 224 TO WL 229 AND FROM STR 14R TO STR 15R. MAINTENANCE CUT OUT DAMAGED SECTION OF SHEAR TIE IAW SRM 53-00-07-2R7. FABRICATED REPAIR DOUBLER AND RECEIVED NEW SHEAR TIE IAW SRM 53-00-07-2R7. INSTALLED FABRICATED REPAIR PARTS IAW SRM 53-00-07-2R7. 2L72 4F4 FRTA16WE E2GL 20051201001992005120100199EU 2005 12 1 USAA051432 120051130A53209Y53465785 SILL AIRBUSA321 A321211 3930370EU AFT SERVICE DOORCORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19164UW 1425 AFT SERVICE DOOR, DEFECTIVE PART REPLACED WITH IDENTICAL PART IAW SRM 51-22-11; LEVEL 1; TASK JA-260-53500 DEFECT SIZE: 4 INCHES X 24 INCHES. 2L72 4F RTA28NM 20051202000062005120200006EU 2005 12 2 USAA051426 120051130A5320D5347217220390 FLOOR SUPPORT AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19112US 1134 FLOOR SUPPORT Y1160 BETWEEN C66-68, DEFECTIVE PART REPLACED WITH IDENTICAL PART IAW SRM 53-11-14, DEFECT SIZE: .5 INCH DIA. SPOT. 2L72 4F4 FRTA28NM E38NE 20051202000102005120200010EU 2005 12 2 USAA051422 120051130A5320D53472172210500 FLOOR SUPPORT AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE Y1160, C66-68 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19112US 1134 FLOOR SUPPORT -Y1160 BETWEEN CROSSBEAMS C66-68, DEFECTIVE PART REPLACED WITH IDENTICAL PART, DEFECT SIZE: .7500 INCH DIA. 2L72 4F4 FRTA28NM E38NE 20051202000112005120200011WP 2005 12 2 IXXA05RNG075S 120050915A5754 DOUBLER DOUG DC8 DC872 302199BWP ZONE 800 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK WAS FOUND A CORROSION ON DOUBLER AT LEADING EDGE OB SLOT UPPER DOOR LT. CORRODED DOUBLER WAS REMOVED AND NEW REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-2-1 FIG 12 AND EWO ATI-57-050. 2L74 4F RT4A25 20051202000132005120200013WP 2005 12 2 IXXA05RNG076S 120050914A5330 SKIN DOUG DC8 DC872 302199BWP STA 208 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK, CORROSION WAS FOUND ON LOWER SKIN STA 208-270 LONGERON 32RH-32 LT. CORROSION WAS REMOVED IAW SRM 51-1-8 PAGE 20, THICKNESS WAS MEASURED IAW ASTME 79701 AND IT WAS FOUND OUT OF LIMITS IAW SRM 53-2-0 PAGE2P. SKIN WAS REPLACED IAW DRAWING 5613862, RIVETS WERE INSTALLED IAW SRM 51-1-21 PAGE 1-7 AND SPLICE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-2-1 FIGURE 4 TR 53-172 AND EWO ATI 53-028. 2L74 4F RT4A25 20051202000142005120200014WP 2005 12 2 IXXA05RNG077S 120050909A5512 PLATE DOUG DC8 DC872 302199BWP STA XE28-RT CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK,CORROSION WAS FOUND ON STABILIZER UPPER TRAILING EDGE PLATING STA XE 28-RH. REPAIR ACCOMPLISHED, REMOVAL PANEL AND STIFFENER, FABRICATION AND INSTALLATION NEW PANEL AND STIFFENER IAW DRAWINGS 55-05467-1, 55-05467-2, 55-05467-3, 55-05467-4 AND EWO ATI-55-010. 2L74 4F RT4A25 20051202000152005120200015WP 2005 12 2 IXXA05RNG082S 120050926A5330 SKIN DOUG DC8 DC872 302199BWP STA 1530-1536 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK, CORROSION WAS FOUND ON LOWER SKIN STA 1530-1536 LONGERON 31RH-31LH.CORROSION WAS REMOVED IAW SRM 51-1-8 PAGE 20, THICKNESS WAS MEASURED IAW ASTME 767-01 AND IT WAS FOUND OUT OF LIMITS. DAMAGE WAS REPAIRED, FABRICATION AND INSTALLATION AN EXTERNAL AND INTERNAL SPLICE, FINGER DOUBLER AND LONGERON STRAP IAW SRM 53-2-1 FIGURE 4 TR 53-172 AND EWO ATI 53-027. SPLICE FITTING PN: 4641326 AT STA FS 1530 WAS FABRICATED AND INSTALLED IAW SRM 51-1-21 PAGE 1-7. 2L74 4F RT4A25 20051202000172005120200017WP 2005 12 2 IXXA05RNG090S 120051028A5730 SKIN DOUG DC8 DC872 302199BWP STA XFS 207.500 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK CORROSION WAS FOUND ON INNER EXTENDED LEADING EDGE OUTER UPPER SKIN AROUND STA XFS 207.500 - RT. DAMAGED AREA WAS BLENDED OUT AND REINFORCEMENT DOUBLER WAS FABRICATED AND INSTALLED IAW EO ATI-092305 AND EWO ATI-57-055. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR. 2L74 4F RT4A25 20051202000192005120200019NM 2005 12 2 PCSA11190501 120051119A213039608831 FLOW VALVE BOEING727 727233 138408ANM PWA JT8 JT8D15 52051NE CABIN PRESSURE DEFECTIVE A PCSAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO29994AJ 20942 ON CLIMBOUT, CREW REPORTED PRESSURIZATION SYSTEM WILL NOT MAINTAIN CABIN ALTITUDE. AIRCRAFT RETURNED BACK TO DEPARTURE AND LANDED WITHOUT ANY FURTHER INCIDENT. MAINTENANCE TROUBLESHOT PRESSURIZATION SYSTEM AND FOUND FLOW CONTROL AND MODULATING VALVE AT FAULT, THE FLOW CONTROL AND MODULATING VALVE WAS REMOVED AND REPLACED IAW MM CH-36-12-61, PRESSURIZATION SYSTEM WAS OPERATIONALLY CHECKED AND FOUND NORMAL IAW W/C 7-29 AND MM CH-5-51-101. AIRCRAFT WAS RETURNED TO SERVICE. 2L73 4F4 FRTA3WE E2EA 20051202000202005120200020NE 2005 12 2 REXA200500141 220051129A7230 COMPRESSOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE ENGINE FAILED A REXAE ENGINE SHUTDOWN BRJSMOKE/FUMES/ODORS/SPARKS PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SO258588D 7588 GEE873446 PASSING THROUGH 2500 FT MSL ON CLIMBOUT FROM, THE FLIGHT CREW HEARD SEVERAL LOUD (BANGS) FROM THE RT ENGINE. THIS WAS FOLLOWED BY ERRATIC ENGINE INDICATIONS AND A REPORT FROM THE FLIGHT ATTENDANT OF A (BURNING SMELL) IN THE CABIN. THE FLIGHT CREW PERFORMED THE QRH CHECKLIST, SHUTDOWN THE ENGINE AND DECLARED AN EMERGENCY. CENTER DIRECTED A RETURN TO DEPARTURE WHERE AN OTHERWISE UNEVENTFUL ILS APPROACH AND LANDING WERE MADE. MAINTENANCE BORESCOPED THE ENGINE AND FOUND DAMAGE TO SEVERAL COMPRESSOR STAGES. ENGINE IS CURRENTLY BEING REMOVED FOR INVESTIGATION OF CAUSE. 2L72 4F4 FRTA21EA E15NE 20051202000212005120200021NM 2005 12 2 SB05155 120051124A21337638101 CONTROLLER BOEING737 7373B7 1384580NM E/E BAY FAULTY A USAAB EMER. DESCENT E VIBRATION/BUFFET CRCRUISE 1 EA19517AU3681436814 23703 FA REPORTED A LOUD SQUEAK AND VIBRATION FROM FIRST CLASS CABIN FLOORBOARDS. AT THAT TIME, THE CABIN PRESSURE BEGAN CLIMBING. CABIN ROSE TO APPROX 11,000 FEET. CREW INITIATED DESCENT TO 10,000 FEET AND PERFORMED QUICK REFERENCE HANDBOOK PROCEDURES. CREW REPORTED OUTFLOW VALVE WAS NEVER OPEN. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINT REMOVED AND REPLACED THE CABIN PRESSURE CONTROLLER IAW MM. OPS CHECK GOOD. REMOVED AND REPLACED CABIN SELECTOR PANEL AND AFT OUTFLOW VALVE. OPS CHECK GOOD. PERFORMED SATISFACTORY HULL LEAK CHECK, PACK CONFIDENCE CHECK. AS FOR THE SQUEAL AND VIBRATION, MAINTENANCE REPLACED THE AUTOMATIC FLOW CONTROL VALVE FOR THE EQUIPMENT COOLING SYS IAW MM. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20051202000222005120200022WP 2005 12 2 IXXA0500119O 120051127A5280510361 LINK ROD DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE MLG DOOR BROKEN A IXXAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 SW11603AL95380572 46003 3 HOURS INTO FLIGHT, A POP WAS HEARD, FOLLOWED BY AIR NOISE AND VIBRATION FROM NOSE GEAR AREA. CREW RETURNED AIRCRAFT TO DEPARTURE AIRPORT AND LANDED WITH OUT INCIDENT. INSPECTION IS ON GOING. WHEN INFORMATION IS AVAILABLE IT WILL BE PROVIDED. UPON INSPECTION FOUND LT AND RT FORWARD DOOR RODS INTERNAL LATCH BROKEN. REMOVED AND REPLACED FORWARD DOOR RODS AND THE OPERATIONAL CHECK WAS GOOD IAW ALL APPLICABLE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F4 FRT4A25 E2GL 20051202000232005120200023NM 2005 12 2 SB05158 120051127A335020131A BATTERY PACK BOEING737 737401 1384701NM CFMINTCFM56 CFM563B2 13802EU AFT CABIN DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19409US 23879 MAINTENANCE REPORTED THE AFT LT EMERGENCY EXIT LIGHT ABOVE THE R2 DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA16WE E21EU 20051202000242005120200024NM 2005 12 2 SB05156 120051124A276165C268643 ACTUATOR BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE RT WING CRACKED A USAAO OTHER KF FLUID LOSS FLT CONT AFFECTED APAPPROACH 1 EA19356US1497714977 23559 ON APPROACH, CREW REPORTED THE LOSS OF SYSTEM A HYDRAULICS SHORTLY AFTER GEAR EXTENSION. CREW REPORTED THE PUMPS WERE OPERATING DRY FOR LESS THAN 2 MINUTES. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE NR 9 SPOILER ACTUATOR CRACKED. REMOVED AND REPLACED THE NR 9 SPOILER ACTUATOR IAW MM 27-62-94. RIGGED AND OPERATIONALLY CHECK GOOD. INSPECTED FILTERS. NO CONTAMINATES FOUND. SERVICED HYDRAULIC SYSTEM. NO LEAKS NOTED. 2L72 4F4 FRTA16WE E2GL 20051202000292005120200029NM 2005 12 2 USAA051411 120051122A575465C26601180 SKIN BOEING737 737301 1384611NM GE CFM56 CFM56* 13802NE NR 6 SLAT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19591US 23936 LWR SURFACE AT AFT ROW OF FASTNERS AT ACTUATOR MAJOR REPAIR, INSTALLED DOUBLER IAW SRM 57-43-01 REPAIR 6. 2L72 4F4 FRTA16WE E2GL 20051202000362005120200036NM 2005 12 2 QXEA200501572 120051122A2430400SG168Q GENERATOR BOMBDRDHC8 DHC8402 1390042NM APU DC FAILED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09416QX232 4083 APU GENERATOR OVERHEAT WITH AUTO SHUTDOWN. SPARKS CAME OUT OF TAIL EXHAUST. SMOKE CAME OUT OF COMPARTMENT VENT AND GENERATOR VENT. MAINTENANCE INSPECTED APU COMPARTMENT FOR SIGNS OF HEAT DAMAGE. NONE NOTED. NO APU FIRE WARNING DETECTED ON FIRE DETECTION PANEL. FOR TROUBLESHOOTING PURPOSE, REMOVED AND REPLACED APU DC GEN IAW AMM TASK 27-33-06-00-801 AND 24-33-01-400-801. C/W OPS TEST OF APU 28U DC GENERATION SYSTEM IAW AMM TASK 24-33-00-710-801. OPS TEST GOOD. NO OTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051202000392005120200039SO 2005 12 2 XGN2005F00009 220051010A8530ECI712A CYLINDER BEECH 36 A36 1151604CE CONT O520 IO520BA 17032SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW05236CH471 E502 280803R FOUND CYLINDER HEAD CRACKED IN THE EXHAUST SIDE OF THE CYLINDER HEAD DURING 50 HR INSPECTION. THIS IS AN ON GOING PROBLEM WITH THE ECI CYLINDERS. (K) 1L71 3O3 O 3A15 E5CE 20051202000412005120200041WP 2005 12 2 IXXA0500118O 120051122A7700 BULB DOUG DC8 DC871F 302199DWP ENGINE INDICATORLOOSE A IXXAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SW11828BX84372876 45993 DURING A TAKEOFF ROLLOUT AT 110KTS, NR 3 ENGINE OIL PRESSURE LIGHT CAME ON. TAKEOFF WAS REJECTED. OIL PRESSURE AND QUANTITY INDICATED NORMAL BUT LIGHT REMAINED ON UNTIL THE ENGINE WAS SHUTDOWN. CREW RETURNED TO BLOCKS. MAINTENANCE DEFERRED THIS IAW MEL 79-6 (CAT B) WITH A NO FLY DATE OF 11/26/05. MAINTENANCE CHECKED NR 3 ENGINE OIL PRESSURE WARNING LIGHT SWITCH AND DIFFERENTIAL SWITCH AND ASSOCIATED WIRING, NO DEFECTS WERE NOTED. FOUND BULB IN LIGHT SOCKET LOOSE. REPLACED BULB AND RAN THE NR 3 ENGINE AND THE OIL PRESSURE LIGHT CHECKS NORMAL WITH NO DEFECTS NOTED IAW ALL APPLICABLE MANUALS. 2L74 4F RT4A25 20051202000442005120200044SW 2005 12 2 ALGA106760 120051103A6220406310405101 PITCH LINK BELL 407 407 1182206SW ALLSN 250C 250C47B GL MAIN ROTOR ROUGH B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03557AL289 53243 RATCHETY AND ROUGH / REPLACED WITH NEW BY FIELD MAINTENANCE. 1G71 3U3 UO H2SW E1GL 20051202000462005120200046NM 2005 12 2 QXEA200501573 120051123A30104100S00502 DUAL VALVE BOMBDRDHC8 DHC8402 1390042NM PWC 150 PW150A EA INOPERATIVE A QXEAO OTHER O OTHER UKUNKNOWN 1 NM09410QX7070 4053 WHEN AIRFRAME DEICE BOOTS ARE SELECTED TO EITHER SLOW, FAST OR MANUAL, THE NR 2 ENGINE INLET BOOT LIGHT FLICKERS ON THEN GOES OUT. THE DEICE PRESSURE CAUTION LIGHT THEN ILLUMINATES. RAN THE CHECKLIST. THE PRESS IS ISO. BOTH SIDES ARE GOOD. MAINTENANCE REMOVED AND REPLACED NR 4 DUAL DISTRIBUTOR VALVE AMM. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E00062EN 20051201001532005120100153WP 2005 12 1 0501649997 120051126A5250 SEAL DOUG DC9 DC931 3022065WP PWA JT8 JT8D7B 52053NE BULKHEAD DOOR LEAKING A NWAAB EMER. DESCENT J WARNING INDICATION DEDESCENT 1 GL018933E 47142 ON DESCENT, WITH ENGINES BROUGHT TO FLIGHT IDLE, THE CABIN WOULD CLIMB. ALTERING ENGINE THRUST WOULD NOT CORRECT CABIN CLIMB. CREW DECLARED AN EMERGENCY AND BEGAN AN IMMEDIATE DESCENT TO 10,000 FEET. NO MENTION OF COM PROCEDURES BUT CABIN PRESSURE CONTROL WAS REGAINED DURING DESCENT. MASKS DID NOT DEPLOY AND ANTI-ICE WAS NOT ON DURING THIS EVENT. A NORMAL SAFE LANDING WAS ACCOMPLISHED. MAINTENANCE FOUND THE AFT PRESSURE BULKHEAD DOOR SEAL LEAKING. REMOVED THE DOOR, CLEANED THE SEAL, AND NO FURTHER PROBLEMS FOUND. THE AIRCRAFT HAS RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 20051201001552005120100155WP 2005 12 1 IXXA05RNG117S 120050926A5730 SKIN DOUG DC8 DC872 302199BWP STA XA621-724 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK WAS FOUND A CORROSION AND BONDED DOUBLERS IN LT OB AILERON UPPER INNER SKIN, STA XA 621 TO XA 724. UPPER SKIN IN LT OB AILERON WAS FABRICATED AND INSTALLED IAW MFG DRAWING 5763133, AND RIVETS WERE INSTALLED IAW SRM 51-1-21 PAGE 1-7. 2L74 4F RT4A25 20051201001572005120100157WP 2005 12 1 IXXA05RNG112S 120050928A5753 SKIN DOUG DC8 DC872 302199BWP STA XF 309.0 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK WAS FOUND A CORROSION AND BONDED DOUBLERS DELAMINATED ON LT OB FLAP T/E UPPER INNER SKIN, STA XF 309.0 TO 333.0. SKIN WAS REPLACED IAW MFG DRAWING 5642970, RIVETS WERE INSTALLED IAW SRM 51-1-21 PAGE 1-7 AND PROTECTIVE TREATMENT WAS APPLIED IAW SRM 51-1-8 PAGE 13-16. 2L74 4F RT4A25 20051201001592005120100159WP 2005 12 1 IXXA05RNG114S 120051027A5730 SKIN DOUG DC8 DC872 302199BWP STA XW 408.343 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK WAS FOUND A CORROSION ON RT WING CENTER LE UPPER EXTERIOR SURFACE, STA XW 408.343. SKIN WAS REPLACED IAW MFG DRAWING 5769857, RIVETS WERE INSTALLED IAW SRM 51-1-21 PAGE 1-7 AND PROTECTIVE TREATMENT WAS APPLIED IAW SRM 51-1-8 PAGE 13-16. 2L74 4F RT4A25 20051201001612005120100161WP 2005 12 1 IXXA05RNG116S 120050928A5753 SKIN DOUG DC8 DC872 302199BWP STA XW2 - XW91 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK WAS FOUND LT OB FLAP T/E PANEL LWD INNER SKIN WITH CORROSION AND BONDED DOUBLER DELAMINANTED, STA XW2-XW91. SKIN ON LT IB FLAP WAS FABRICATED AND INSTALLED IAW MFG DRAWING 5652277, RIVETS WERE INSTALLED IAW SRM 51-1-21 PAGE 1-7. 2L74 4F RT4A25 20051202000092005120200009EU 2005 12 2 USAA051423 120051130A5315D5311281520200 FLOORBEAM AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19112US 1134 LT Y765; CORR. LEVEL 1; TASK J220-53500. DEFECTIVE PART REPLACED WITH IDENTICAL PART IAW SRM 53-11-14, DEFECT SIZE: 1 INCH X 1INCH X 1INCH. 2L72 4F4 FRTA28NM E38NE 20051202000162005120200016WP 2005 12 2 IXXA05RNG089S 120051028A5730 SKIN DOUG DC8 DC872 302199BWP STA XFS 304.00 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK, CORROSION WAS FOUND ON CENTER EXTENDED LEADING EDGE OUTER LOWER SKIN AROUND STA XFS 304.00 - RT. DAMAGED AREA WAS REMOVED AND A REINFORCEMENT DOUBLER WAS FABRICATED AND INSTALLED IAW EO ATI-092205 AND EWO ATI-57-054. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR. 2L74 4F RT4A25 20051202000252005120200025NE 2005 12 2 SA05119 220051123A7321 HMU AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE NR 2 ENGINE FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19113UW160821102 1141 575141 WHILE AT FL 360, THE NR 2 ENGINE GENERATOR FAILED, FOLLOWED BY THE NR 2 ENGINE. THE FLIGHT DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 ENGINE HMU AND ECU FOR TROUBLESHOOTING. ALSO, REPLACED THE NR 2 ENGINE ALTERNATOR ROTOR AND STATOR DUE TO RUB MARKS ON THE STATOR. OPERATIONALLY CHECKS OK. 2L72 4F4 FRTA28NM E38NE 20051202000282005120200028NE 2005 12 2 2005F00109 220051116A7261 COVER BOEING737 737800* NM GE CFM56 CFM56* 13802NE ENGINE OIL MISINSTALLED B E ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO15 ON CLIMB OUT HAD LOW OIL QUANITY INDICATION ON ROLL OUT. QUANITY DROPPED TO ZERO OIL PRESSURE AND TEMPERATURE OKAY. FOUND THE HANDCRANKING DRIVE COVER NOT INSTALLED. RESERVICED ENGINE AND PERFORMED IDLE RUNS FOR 15 MIN. WITH NO DEFFECTS NOTED. 2L72 4F4 FRTA16WE E2GL 20051202000432005120200043SW 2005 12 2 ALGA106759 120051103A6220406310405101 PITCH LINK BELL 407 407 1182206SW ALLSN 250C 250C47B GL MAIN ROTOR RATCHETING B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03557AL209 53243 RATCHETY AND ROUGH / REPLACED WITH NEW BY FIELD MAINTENANCE. 1G71 3U3 UO H2SW E1GL 20051202000472005120200047NM 2005 12 2 ASAA0540424 120050822A53206545855101 SILL BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU BS 947-1000 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 CORROSION ON AFT GALLEY MOP SILL BSTA947-1000, RBL 49, WL 206. REMOVED AND REPLACED AFT GALLEY MOP SILL. (K) 2L72 4F4 FRTA16WE E21EU 20051202000512005120200051SO 2005 12 2 1386111405 120051114A27521159SCC21115 ACTUATOR GULSTMG1159 GIV 3980115SO TE FLAPS INOPERATIVE E N93AA UNSCHED LANDING O OTHER CLCLIMB 1 SO13486QS1243 1386 AFTER TAKEOFF FLAPS WOULD NOT RETRACT PAST 10 DEGREES. 2L72 4F RTA12EA 20051202000622005120200062EU 2005 12 2 XN0A1275 120051111A3242 BRAKE AIRBUS300 A300B4203 3930306EU MLG MALFUNCTIONED A XN0AD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL23473AS 203 GREEN BRAKE INOP ON TAXI. YELLOW SYS PRESSURE SHOW ON BRAKE GAGE. INSPECTED BRAKES THROUGH 8, FOUND NO DEFECTS, PERFORMED OPERATIONAL CHECK OF GREEN AND YELLOW BRAKE SYTEMS. OPS CHECK GOOD. CLEANED AND RESEATED BRAKE, CONTROL BOX AND CONNECTION. ALL SYSTEMS OPS CHECK GOOD AT THIS TIME IAW A300 MM REF 32-42-00. (ORIG/CLOSED) 2L72 4F RTA35EU 20051202000672005120200067SO 2005 12 2 65811122005 120051112A56101159SCB51023 WINDSHIELD GULSTMGV GULFSTREAMGV3980116SO COCKPIT CRACKED E N93AA UNSCHED LANDING O OTHER CRCRUISE 1 SO13516QS3424 658 CO PILOTS WINDSHIELD CRACKED IN FLIGHT. 2L72 4F RTA12EA 20051202000692005120200069NE 2005 12 2 ANCF200400062 220051122A7200 ENGINE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE RIGHT MALFUNCTIONED W ANCFC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO23593AN25448405 53093 P726956D DURING TAKEOFF AND AFTER TAKEOFF THRUST WAS APPLIED, RT ENGINE ACCELERATION WAS VERY SLOW AND STOPPED AT 1.7 EPR. ACCELERATION TO 2 EPR WAS REACHED MOVING RT POWER LEVER MANUALLY. WHEN RT ENGINE REACHED 2 EPR N1 INDICATION STARTED FLASHING AND INDICATION WAS 100.8 PERCENT. RT POWER LEVER WAS 2 KNOBS ADVANCED FROM LT POWER LEVER, IN THIS MOMENT A VERY STRONG CRACKING NOISE WITH VIBRATION CAME FROM RT ENGINE. TAKEOFF WAS DISCONTINUED AND POWER LEVERS ARE MOVING TO IDDLE THRUST. THE DIGITAL FLIGHT DATA RECORDER SHOWS THAT N1 REACHED 108,1 PERCENT SO THE ENGINE WAS REPLACED. 2L72 4F4 FRTA6WE E9NE 20051202000702005120200070NM 2005 12 2 ASMF200511009 120051123A8011784750A3 STARTER BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE LT ENGINE DAMAGED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23805AM6829 26272 727054 DURING LT ENGINE STARTING, THE PNEUMATIC STARTER FAILED. DURING MAINTENANCE REVISION WAS DETECTED THE PNEUMATIC STARTER WITH DAMAGE, SO IT WAS REPLACED IAW MM 80-11-01 AND OPERATIONAL TEST WAS PERFORMED IAW MM 71-00-01, ALL CORRECT. 2L72 4F4 FRTA2NM E17NE 20051202000742005120200074EA 2005 12 2 ASOA05949 120051104A5320 SILL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27838AS 7276 DURING A C-CHECK, THE SERVICE DOOR SILL AREA WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINT REMOVED LIGHT CORROSION IN 2 PLACES OF SERVICE DOOR SILL AREA. CLEANED, TREATED, PRIMED AND PAINTED AREAS IAW SRM. (K) 2L72 4F4 FRTA21EA E15NE 20051202000762005120200076SO 2005 12 2 LR7A05115 120051120A5330 SKIN LKHEED382 382G 526414USO FS 914 DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 143 4698 DURING CARGO OFF-LOADING OPS, LOADER CONTACTED A/C AND DAMAGED SKIN AT FS914 LBL60 WL216 (APROX) THERE IS 1.5 INCH X 2.5 INCH HOLE IN THE OUTER SKIN. AT FS909 LBL60 THERE IS A DENT. AIRCRAFT FERRIED UNPRESSURIZED FOR REPAIR. REPAIRED IAW SMP 583 53-50-22 AND FIG 51-140-12. LP16705 ITEM M2. 2H74 4T A1SO 20051202000832005120200083NM 2005 12 2 HNAA0500101 120051128A2910 LINE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HYD SYSTEM LEAKING A HNAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 EA07935HA 142 LOSS OF NR 2 HYDRAULIC QUANTITY IN FLIGHT WITH ASSOCIATED NR 2 ISO VALVE LIGHT AND OB ROLL SPOILER CAUTION LIGHT. NR 2 HYDRAULIC QUANTITY REMAINED AT 2 QUARTS. FOUND TUBE LEAKING AT NR 2 STAY STRUT ACTUATOR. 2H72 4T4 TRTA13NM E20NE 20051202000922005120200092NM 2005 12 2 HNAA05010 120051128A2910 TUBE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE NR 2 HYD SYSTEM LEAKING A HNAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 EA07935HA 142 LOSS OF NR 2 HYDRAULIC QUANTITY IN FLIGHT WITH ASSOCIATED NR 2 ISO VALVE LIGHT AND OB ROLL SPOILER CAUTION LIGHT. NR 2 HYDRAULIC QUANTITY REMAINED AT 2 QUARTS. FOUND TUBE LEAKING AT NR 2 STAY STRUT ACTUATOR. 2H72 4T4 TRTA13NM E20NE 20051202000932005120200093CE 2005 12 2 BSYA200500024 120051125A5210 DOOR BEECH 58 58 1152740CE CONT O520 IO520C 17032SO COCKPIT OPEN E BSYAA UNSCHED LANDING O OTHER CLCLIMB 1 GL073695V TH1183 ON DEPARTURE, COCKPIT DOOR CAME OPEN. AIRCRAFT THEN RETURNED TO DEPARTURE. MAINTENANCE LUBED AND ADJUSTED UPPER HOOK ASSY, OPS CHECKS GOOD. 1L72 3O3 O 3A16 E5CE 20051202000972005120200097WP 2005 12 2 ASMF200511008 120051116A801138334221 STARTER DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE RT AIRTURB STARTFAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23205AM17826 49405 AIRCRAFT RETURNED TO PLATFORM, RT ENGINE DID NOT START. DURING MAINTENANCE REVISION, IT WAS DETECTED THE RT ENGINE WITHOUT TURN IN N2. THE RT ENGINE STARTER WAS REPLACED IAW MM 80-10-01, TESTED CORRECT. 2L72 4F4 FRTA6WE E9NE 20051202001002005120200100NM 2005 12 2 ANCF200400061 120051115A2782755299D ACTUATOR BOEING757 75728A 1384976NM RROYCERB211 RB211* 54555NE SLATS FAILED W ANCFO OTHER J WARNING INDICATION CLCLIMB 1 SO23506NA 4731 24771 BOTH FLAP POINTERS ARE ON HALF POSITION WITH THE FLAP LEVER UP. L/E SLAT DISAGREE LIGHT ILLUMINATED. L/E SLAT DISAGREE DISPLAY ON EICAS. VOICE RECORDER CB WAS PULL OUT AS SB REQUEST. IAW AMM 27-58-01 PAGE 501 ACCOMPLISHED RIGGING ON TRANSMITTER POSITION SLAT AND PDU TRANSMITTER POSITION. IAW AMM 27-81-01 PAGE 401 REPLACED ROTATOR ACTUATOR NR11. IAW AMM 27-51-01 PAGE 401 REPLACED FSEU 2 AND 3 ACTUATOR SLAT P/N 755299D, S/N A1976; FSEU P/N 285N0011-32, S/N D01503; FSEU P/N 285N0011-40, S/N D00869. 2L72 4F4 FRTA2NM A12EU 20051202001182005120200118EU 2005 12 2 05FDEA03984 120051128A5347 REPAIR AIRBUS310 A310203 3930313EU GE CF6 CF680A3 30025NE FUSELAGE IMPROPER A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25423FE 281 PREVIOUS REPAIRS ON MAIN DECK CARGO SEAT TRACK SPLICE FROM FR 58 TO 61 3RD TRACK LT OF CENTER LINE NEEDS EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA REF N00725. FOUND REPAIR NOT IN CONFORMANCE OF SRM, 53-10-16 FIG 208 R7R REPAIR IAW SRM 53-10-16 FIG 208. MINOR REPAIR IAW GMM 6-2-100. 2L72 4F4 FRTA35EU E13NE 20051202001192005120200119EU 2005 12 2 05FDEA03985 120051128A5522 REPAIR AIRBUS310 A310203 3930313EU GE CF6 CF680A3 30025NE ELEVATOR PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 PREVIOUS REPAIR 2 EA EXT DOUBLERS INSTALLED ON RT ELEVATOR IB UPPER SKIN NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA REF N00719. REPAIR IS IAW EA 6-2730-50500. 2L72 4F4 FRTA35EU E13NE 20051202001202005120200120 2005 12 2 PIDA20050195 420051126A2230734SUE23 COMPUTER BOEING737 737228 13844AGNM PWA JT8 JT8D* NE AUTOTHROTTLE INOPERATIVE A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05252TR 23001 AUTO THROTTLES INOP. REPLACED AUTO THROTTLE COMPUTER IAW MM 22-31-101. OPS CHECKS NORMAL. 2L72 4F4 FRTA16WE E2EA 20051202001212005120200121NM 2005 12 2 ASAA0510318 120050921A5315 FLOORBEAM BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE BS 328 CORRODED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM02740AS 22578 FOUND EXFOLIATION CORROSION FOUND ON UPPER CHORD OF FLOORBEAM AT BS 328, FROM BL 0 -RBL 56. CHORD REPLACED IAW SRM 53-10-9. 2L72 4F4 F A16WE E2EA 20051202001222005120200122NM 2005 12 2 05FDEA03986 120051128A5330 SKIN BOEING727 727227 1384078NM PWA JT8 JT8D9 52048NE ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 CORROSION AT LOWER FUSELAGE STA BS 480 STRINGER STR 29-L. REMOVED CORROSION IAW SRM 51-10-6. SKIN ORIGINAL THICKNESS .090 MATERIAL LOSS .022 MATERIAL REMAINING .068 FOUND OUT OF LIMITS IAW SRM 53-30-1 UT GAGE T8253C. DOUBLER AND FILLER MATERIAL ID 7075-T6 .090 PO 483543.2 IAW SRM 53-30-2 FIGURE 4 AND 53-30-3 FIGURE 2. REMOVED DAMAGE SKIN AREA IAW SRM 53-30-3 FIGURE 2. FABRICATED DOUBLER AND FILLER IAW SRM 53-30-3 FIGURE 2 AND 51-10-2. INSTALLED DOUBLER AND FILLER IAW SRM 53-30-3 FIGURE 2. REMOVED AND REPLACED FASTENERS IAW SRM 51-30-2. 2L73 4F4 F A3WE E2EA 20051202001232005120200123EU 2005 12 2 05FDEA03987 120051128A5330 REPAIR AIRBUS310 A310203 3930313EU GE CF6 CF680 30025NE FUSELAGE IMPROPER A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25423FE 281 PREVIOUS REPAIR EXT DOUBLER INSTALLED ON L1 DOOR AFT UPPER CORNER NEEDS EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA REF N00722. REMOVED AND REPLACED COVER DUE TO NONCONFORMITY IAW SRM 52-10-00 FIG 203. MINOR REPAIR IAW GMM 6-2-100. 2L72 4F4 FRTA35EU E13NE 20051202001242005120200124NM 2005 12 2 05FDEA03988 120051128A5311 FRAME BOEING727 727227 1384078NM PWA JT8 JT8D9 52048NE ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 FORWARD CARGO COMPARTMENT, FRAME AT STA BS 720E BETWEEN STRINGER STR 26-R AND STR 25-R IS CORRODED. REMOVED DAMAGE AREA OF FRAME IAW SRM 53-10-4. FABRICATED INNER AND OUTER REPAIR DOUBLER AND FILLER IAW SRM 51-40-3 FIGURE 1. FABRICATED FRAME SECTION IAW MFG DRAWING 65-17663. ALODINED AND PRIMED REPAIR PARTS AND FRAME SECTION IAW SRM 51-10-2. INSTALLED REPAIR PARTS AND REPAIR FRAME SECTION IAW SRM 51-30-2. 2L73 4F4 F A3WE E2EA 20051202001262005120200126EU 2005 12 2 05FDEA03990 120051128A2916 RESERVOIR AIRBUS310 A310222 3930315EU PWA JT9 JT9D* NE HYDRAULIC SYSTEMLOW A FDEAB EMER. DESCENT KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO25422FE 346 LOST GREEN HYD FLUID IN CRUISE. RESERVOIR LOW PRESSURE. CRANKED GEARS MANUALLY, USED ALTERNATE. ALT-ON-POSITION FOR LANDING (ANTI-SKID). 2L72 4F4 FRTA35EU E20EA 20051202001282005120200128EU 2005 12 2 05FDEA03992 120051128A5330 SKIN AIRBUS310 A310222 3930315EU PWA JT9 JT9D7R4E1 52054NE ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25450FE 162 TWO DENTS AT FR 24 JUST BELOW RT STRINGERS 15 AND 16. CUT OUT DAMAGED SECTION IAW SRM 53-27-00. PERFORMED HFEC IAW NTM 51-10-08. INSTALLED INTERNAL DOUBLER AND FILLER IAW SRM 53-10-12 FIG 229 AND 53-10-14 FIG 201. 2L72 4F4 FRTA35EU E3NE 20051202001302005120200130NM 2005 12 2 05FDEA03999 120051128A5230 SKIN BOEING727 727200 138407ENM PWA JT8 JT8D9 52048NE CARGO DOOR CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 LOWER AFT CARGO DOOR OUTER SKIN IS CHAFED ALONG FAIRING RUB STRIP. REPAIRED LOWER AFT CARGO DOOR OUTER SKIN PER 52-00-3 FIG 4. 2L73 4F4 FRTA3WE E2EA 20051202001332005120200133NM 2005 12 2 05FDEA04001 120051128A5311 FRAME BOEING727 727200 138407ENM PWA JT8 JT8D9A 52048NE BS 950C DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 AFT CARGO COMPARTMENT, DENT IN FRAME BS 950C RBL 36 WL 152. REMOVED DENT DAMAGE AREA, FABRICATED REPAIR PART AND INSTALLED IAW SRM 51-40-3. 2L73 4F4 FRTA3WE E2EA 20051202001352005120200135WP 2005 12 2 05FDEA04003 120051129A5753 SKIN DOUG MD10 MD1010F 3022112WP GE CF6 CF66K 30020NE TE FLAP DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25571FE 47830 LT IB FLAP SKIN UPPER SIDE ACCIDENTALLY DAMAGED DURING STRIPPING ACTIVITIES. REMOVED FLAP SECTION IAW SRM 51-31-01. REFORMED RIB IAW DPS 3.69. PERFORMED INSPECTION, NO CRACK FOUND. PERFORM DOUBLER REPAIR IAW SRM 57-10-00 FIG 85. 2L73 4F4 FRTA22WE E23EA 20051202001372005120200137WP 2005 12 2 05FDEA04005 120051129A5730ARB09831 DOUBLER DOUG MD10 MD1010F 3022112WP GE CF6 CF66K 30020NE RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25571FE 47830 DURING PRE-PAINT INSPECTION FOUND CORROSION WITH EXFOLIATION ON BEVER/TAIL OF RT WING AT STA XORS 284. REPAIRED IAW EA 8-5710-93818. 2L73 4F4 FRTA22WE E23EA 20051202001402005120200140SO 2005 12 2 CHQA200500202 120051125A3350RPS1B BATTERY PACK EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11288SK6276 6276 145461 SEVERAL EMERGENCY EXIT LIGHTS ARE INOP IN THE AFT CABIN. REMOVED AND REPLACED AFT FLOOR EMERGENCY EXIT LIGHT BATTERY PACK IAW 145 AMM 33-50-04. OPS CHECK GOOD. 2L72 4T4 FRTT00011ATTE6CH 20051202001422005120200142SO 2005 12 2 FDK2005F00002 120050919A49304951545 PUMP EMB 145 EMB145LR 3260212SO ALLSN AE3007AE3007C GL APU FUEL LEAKING A FDKAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW07825MJ512 145179 (REF NR F05005)THE CREW NOTED A STRONG ODOR OF FUEL IN THE CABIN (ACTUAL). MAINTENANCE HAS TROUBLESHOT FAULT TO LEAKING PACKINGS AT THE APR ACCELLERATION UNIT. MAINTENANCE REMOVED AND REPLACED APU FUEL PUMP. (K) 2L72 4T4 FRTT00011ATTE6CH 20051202001482005120200148NM 2005 12 2 AMTA200500936 120051024A2610285N002836 CARD BOEING757 75733N 1384931NM GE CF34 CF343B1 NE LEFT UNSERVICEABLE A AMTAK NONE J WARNING INDICATION TXTAXI/GRND HDL 1 GL11552TZ 32586 EICAS MSG (L ENG OH LLP1). REMOVED AND REPLACED LT ENG AUTO FIRE HEAT DET CARD IAW MM. RAN LT ENG, OPS CHECKED OK. (K) 2L72 4F4 FRTA2NM E15NE 20051202001552005120200155WP 2005 12 2 MWEA050131 120051201A531159114481 FRAME DOUG DC9 DC981 3022081WP STA 541 DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31807ME 48033 FOUND LONGERON 19 RIGHT TO LONGERON 22 RIGHT IS DAMAGED. FABRICATED AND INSTALLED SECTION OF FRAME. 2L72 4F A6WE 20051202001572005120200157SO 2005 12 2 LR7A05117 120051017A5312 STIFFENER LKHEED382 382G 526414USO FS1023 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2450 4590 DURING C -6 CHECK PER HC5212, FOUND CARGO DOOR AFT BULKHEAD WEB STIFFENERS CRACKED FS 1023, RBL0. REPLACED WEB STIFFENERS IAW SRM SMP 583 FIGURE 51-70 AND AC43.13-1B PARA 4-57 NR 0106. 2H74 4T A1SO 20051202001592005120200159NM 2005 12 2 SWAA053807 120051129A3350612825 BATTERY PACK BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR UPPER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20051202001622005120200162NM 2005 12 2 SWAA053810 120051127A3350BR2013 LIGHT BOEING737 7377H4 1384404NM EMERGENCY EXIT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29459WN 32497 EEPLS STRIP MISSING AT OVERWING EMERGENCY EXIT. INSTALLED EEPLS PER MM. 2L72 4F RTA16WE 20051202001642005120200164NM 2005 12 2 SWAA053812 120051130A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29479WN 33990 EEPLS STRIP COVER LOOSE AT FWD END. SECURED COVER PER MM. 2L72 4F RTA16WE 20051202001662005120200166NM 2005 12 2 SWAA053814 120051129A5753 SKIN BOEING737 7373H4 1384600NM LT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29649SW 27719 DURING SCHEDULED C4 CHECK, FOUND LT WING T/E OTBD AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2L72 4F RTA16WE 20051202001682005120200168NM 2005 12 2 SWAA053816 120051130A575569359581 ROD END BOEING737 7373A4 1384585NM LT WING SPOILER BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 FOUND LT WING NR 4 GROUND SPOILER OTBD ACTUATOR ROD END BROKEN. REMOVED AND REPLACED GROUND SPOILER OTBD ACTUATOR PER MM. 2L72 4F RTA16WE 20051202001702005120200170NM 2005 12 2 SB05159 120051201A3260189929 SENSOR BOEING737 7373B7 1384580NM RIGHT MLG OUT OF ADJUST A USAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19522AU 23857 BOS - FLT203, AFTER TAKEOFF FROM BOS, CREW COULD NOT RETRACT THE LANDING GEAR. THE GEAR HANDLE WOULD NOT MOVE UP PAST THE OFF POSITION. FLIGHT RETURNED TO THE FIELD AT BOS AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE AIR SAFETY SENSOR OUT OF ADJUSTMENT. ADJUSTED INTERLOCK VALVE TELEFLEX CABLE TO BRING SENSOR WITHIN TOLERANCE. ACCOMPLISHED FUNCTIONAL CHECK OF SPOILER INTERLOCK VALVE AND LANDING GEAR SAFETY SENSORS. OPERATIONAL CHECK OF GEAR RETRACTION GOOD. 2L72 4F RTA16WE 20051202001712005120200171NM 2005 12 2 QXEA200501597 120051129A6120697073002 PITCH CONTROL BOMBDRDHC8 DHC8402 1390042NM PROPELLER MALFUNCTIONED A QXEAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09404QX9618 4046 PDX FLIGHT NR 2311: ON CLIMB-OUT AT AROUND 15K FT, POWERPLANT MESSAGE APPEARED ON THE ED (PUSHED EVENT MARKER). ABOUT 1 MINUTE LATER THE NR 1 PEC CAUTION LIGHT APPEARED AND THE PROP FEATHERED. PER THE CHECKLIST, SHUT THE ENGINE DOWN. MX REMOVED AND REPLACED NR 1 PCU IAW 61-20-11-000-801 AND 61-20-11-400-801. GROUND RAN A/C. OPS TEST GOOD. NO LEAKS NOTED. WHILE POWER LEVER IS AT DETENT, CYCLED CONDITION LEVER FROM MAX TO 900 AND 850 NP REFLECTED CHANGE. NO OTHER DEFECTS NOTED AT THIS TIME. NO NEW FAULT CODES LOGGED. REF FIM TASKS 61-20-04-810-812 FOR CODE 158, TASK 61-20-06-810-818 FOR CODE 260 AND TASK 61-20-05-810-822 FOR CODE 236 FOR TROUBLESHOOTING PROCESS. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051202001732005120200173NM 2005 12 2 QXEA200501600 120051130A3060SFA13S1P0A BLADE DHAV DHC8 DHC8202 2809007NM PROPELLER MALFUNCTIONED A QXEAA UNSCHED LANDING O OTHER CRCRUISE 1 NM09350PH165102231 488 PDX FLIGHT NR 2056, LEFT PROP DE-ICE CREATED CONTINUOUS SPARK RING AROUND NR 1 PROP HUB. MAINTENANCE REPLACED NR 1 BLADE ON NR 1 PROP IAW MTC 9616003. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051202001752005120200175EU 2005 12 2 MALA050831 120051116A3210 CONNECTOR SAAB SF340 340B 7860101EU MLG LOOSE A MALAO OTHER O OTHER APAPPROACH 1 GL15438XJ 340B438 ON FIRST APPROACH INTO BJI GPWS ON SHORT FINAL WENT OFF TOO LOW GEAR. FOUND RT MAIN GEAR DOWN LOCK ACTUATOR CONNECTOR UNSECURED. RESECURED CONNECTOR. 2L72 4T RTA52EU 20051202001772005120200177EU 2005 12 2 MALA050843 120051128A2920 PTU BAC 146 AVRO146RJ85A1500097EU HYD SYSTEM MALFUNCTIONED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15529XJ E2363 FROM CLT TO MSP, GREEN HI TEMP LIGHT ILLUMINATED. REMOVED AND REPLACED POWER TRANSFER UNIT. 2H74 4F RTA49EU 20051205000012005120500001NM 2005 12 5 DHL2005749017 120051102A2782 ROD BOEING727 7272J0 138407ENM ACTUATOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01749DH 22013 NR 3 SLAT WS 515 AT ACT ROD END ATTACH HAS IB FRAMES CRACKED IN AFT RADIUS. REMOVED AND REPLACED DAMAGED IB RIB PN 65-17294-14 PO NR 540053 ON NR 3 SLAT IAW 727 SRM 51-30-2. 2L73 4F RTA3WE 20051205000032005120500003NM 2005 12 5 DHL2005749014 120051102A5320 WEB BOEING727 7272J0 138407ENM BS 950E-950D CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01749DH 22013 FOUND WEB BETWEEN STA 950E AND 950 D ABOVE STR 26 LEFT IS CRACKED M/R. REMOVED WEB FOR FAB NEW AT STA 950E TO 950D STR 26 LT IAW B727 SRM 51-30-2. FAB`D NEW PART MAT USED 7075 T6 .040 PO 900505 DIM 19 1/2" BY 3" IAW B727 SRM 51-20-1 AND 53-10-2 FIG 5. TREATED AND PRIMED PART IAW B727 SRM 51-10-2. INSTALLED REPAIR WEB IAW B727 SRM AND SRM 51-30-2. 2L73 4F RTA3WE 20051205000052005120500005NM 2005 12 5 05FDEA04067 120051201A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 HFEC INSP CARRIED OUT AND CRACK FOUND ON RIGHT WING STRINGER S7. REPAIRED AS PER SRM 57-20-00 FIG. 10 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20051205000062005120500006EU 2005 12 5 MALA050836 120051116A3260 UPLOCK BAC 146 AVRO146RJ85A1500097EU MLG ICED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15504XJ E2311 RIGHT MAIN GEAR UPLOCK UNSAFE LIGHT ON. CYCLED GEAR. AIR RETURN TO DSM, FOUND AND REMOVED ICE FROM MLG DOOR UPLOCK. 2H74 4F RTA49EU 20051205000072005120500007EU 2005 12 5 MALA050837 120051118A3260 WARNING LIGHT SAAB SF340 340B 7860101EU MLG ILLUMINATED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15441XJ 340B441 AFTER TAKEOFF CREW TRIED TO RETRACT THE LANDING GEAR. THE CREW THEN GOT THE GEAR INTRANSIT LIGHT. THE CREW THEN SELECTED GEAR DOWN AND THE LIGHT WENT OUT. AIR RETURNED TO MSP. NO FURTHER INFO AT THIS TIME. 2L72 4T RTA52EU 20051205000082005120500008EU 2005 12 5 MALA050838 120051119A2131 CONTROLLER SAAB SF340 340B 7860101EU CABIN PRESSURE MALFUNCTIONED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15361PX 340B249 AUTO PRESSURE CONTROL INOP. AIR RETURN. REPLACED CONTROLLER. 2L72 4T RTA52EU 20051205000092005120500009 2005 12 5 MALA050841 420051126A3425 COMPUTER SAAB SF340 340B 7860101EU AHRS INOPERATIVE A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15427XJ 340B427 AHRS COMPUTER INOP. AIR TURNBACK 2L72 4T RTA52EU 20051205000102005120500010EU 2005 12 5 MALA050825 120051109A3510 OXYGEN BOTTLE SAAB SF340 340B 7860101EU LEAKING A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15410XJ 340B410 DURING CLIMB, THE OXYGEN CWP LIGHT ILLUMINATED. OXYGEN DROPPED FROM 1400 PSI TO 800 PSI. RETURNED TO MEM. INSPECTED AREA AROUND O2 CYLINDER AND TIGHTENED B-NUTS. CHECKS GOOD 2L72 4T RTA52EU 20051205000132005120500013EU 2005 12 5 MALA050830 120051116A3260 UPLOCK BAC 146 AVRO146RJ85A1500097EU RT MLG WARNING LIGHT A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15504XJ E2311 RIGHT MAIN GEAR UPLOCK UNSAFE LIGHT ON GEAR RETRACTION. CYCLED LANDING GEAR DOWN SAFE TWICE. RETURNED FOR LANDING. FOUND ICE ON MLG DOOR UPLOCK. REMOVED ICE. 2H74 4F RTA49EU 20051205000142005120500014NM 2005 12 5 DHL2005749003 120051030A5755 HINGE BOEING727 7272J0 138407ENM NR 1 SPOILER CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01749DH 22013 FOUND NR 1 SPOILER 2ND HINGE CUTOUT HAS 1" CRACK. STOP DRILLED CRACK IAW 727 SRM 51-10-1. VERIFIED CRACK TERMINATION IN STOP DRILL HOLE IAW B727 NDT PT 6 51-00-00 FIG 23. FABRICATED REPAIR DOUBLER FROM MAT 70-75-T6 071 - PO NR 9002507 DIMS 5 3/4" BY 4 1/4" IAW B727 SRM 57-30-4 FIG 10. TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED REPAIR DOUBLER FROM NR 11 SPOILER 2ND HINGE IAW B727 SRM 51-30-2 AND 57-30-4 FIG 10. 2L73 4F RTA3WE 20051205000162005120500016SO 2005 12 5 LR7A05127 120051017A5312 ANGLE LKHEED382 382G 526414USO FS 1023 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER HC5212, FOUND CARGO DOOR BULKHEAD WEB STIFFENERS CRACKED, FS 1023, RBL37. REPAIRED STIFFENER ANGLES PER SRM 51-140-19, NR 0107. 2H74 4T A1SO 20051205000172005120500017SO 2005 12 5 LR7A05128 120051017A5322 FLANGE LKHEED382 382G 526414USO FS 847 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER HC5315, FOUND CANTED SKIN ATTACH FLANGE CRACKED, FS 847, LBL 65 WL 187. REPAIRED PER LAC MEA 382-53-01-080 (ED01-058-01) NR 0175. 2H74 4T A1SO 20051205000182005120500018SO 2005 12 5 LR7A05129 120051017A5322339007R5 CHANNEL LKHEED382 382G 526414USO FS 1030 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER HC5315, FOUND REAR FUSELAGE RIGHT HAND SIDE CHANNEL CRACKED, FS 1030. REPLACED CHANNEL IAW SRM SMP 583 51-70-00, LEAK CHECKED IAW SMP 581 36-10, NR 0178. 2H74 4T A1SO 20051205000222005120500022SO 2005 12 5 LR7A05133 120051017A5330 SKIN LKHEED382 382G 526414USO FS 757E-777E DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER HC5321, FOUND BELLY SKIN DAMAGED, FS 757E TO FS 777E, BL0. REPAIRED DAMAGED BELLY SKIN PER SRM 51-104-12, NR 0250. 2H74 4T A1SO 20051205000232005120500023SO 2005 12 5 LR7A05134 120051017A53303536128 SKIN LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER HC5211, FOUND RAMP REAR SILL UPPER RIGHT HAND SKIN PANEL SPLIT. REPLACED SKIN PANEL PER DRAWING 353612 AND SRM 51-70, NR 0296. 2H74 4T A1SO 20051205000302005120500030SO 2005 12 5 LR7A05141 120051017A5330 SKIN LKHEED382 382G 526414USO FS 317E DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER HC5321, FOUND STONE DAMAGE, FS 317E.0E, LBL2 WL126. REPAIRED BELLY SKIN PER SRM 51-140-10, NR 0352. 2H74 4T A1SO 20051205000312005120500031SO 2005 12 5 LR7A05142 120051017A5330 SKIN LKHEED382 382G 526414USO BS 764 DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER HC5321, FOUND STONE DAMAGE FS 764.0E, LBL64 WL146. REPAIRED FUSELAGE SKIN PER SRM 51-140-10, NR 0356. 2H74 4T A1SO 20051205000332005120500033SO 2005 12 5 LR7A05144 120051017A5230 DOUBLER LKHEED382 382G 526414USO CARGO DOOR DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER HC5211, FOUND REAR RAMP SHELF DAMAGED RS10 LBL 60-RBL 60. INSTALLED PROTECTIVE PADS IAW DRAWING 105-025-01 PER LAC MEA382-53-05-080, NR 0376. 2H74 4T A1SO 20051205000342005120500034SO 2005 12 5 LR7A05145 120051017A5412 BULKHEAD LKHEED382 382G 526414USO NR 3 NACELLE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER HC5711, FOUND NR 3 NACELLE OUTBOARD BULKHEAD CRACKED. REPAIRED IAW DRAWING R05-025-06 PER LAC MEA382-54-05-078, NR 0387. 2H74 4T A1SO 20051205000362005120500036SO 2005 12 5 LR7A05147 120051017A5753 CAP LKHEED382 382G 526414USO WS 171 R CORRODED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER HC5711, FOUND RIGHT HAND INBOARD FLAP CENTER LOWER SPAR CAP CORROSION, 7-05-074, NR 0407. 2H74 4T A1SO 20051205000392005120500039SO 2005 12 5 LR7A05150 120051017A5311 FRAME LKHEED382 382G 526414USO FS657 MISDRILLED A LR7AK NONE W INADEQUATE Q C ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER HC5313 FOUND FUSELAGE FRAME (LS5408-2) MISDRILLED LINER HOLE LEFT HAND SIDE. FS657, WL158. REPAIRED IAW DRAWING R05-025-08 PER LAC MEA382-53-05-070. NR 0413. 2H74 4T A1SO 20051205000402005120500040SO 2005 12 5 LR7A05151 120051017A5311 FRAME LKHEED382 382G 526414USO FS 667 MISDRILLED A LR7AK NONE W INADEQUATE Q C ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER HC5313, FOUND FUSELAGE FRAME (LS5408-2) MISDRILLED LINER HOLE LEFT HAND SIDE, FS 667, WL158. REPAIRED IAW DRAWING R05-025-08 PER LAC MEA382-53-05-070, NR 0413. 2H74 4T A1SO 20051205000412005120500041SO 2005 12 5 LR7A05152 120051017A5311 FRAME LKHEED382 382G 526414USO FS 697 MISDRILLED A LR7AK NONE W INADEQUATE Q C ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER HC5313, FOUND FUSELAGE FRAME (LS5408-2) MISDRILLED LINER HOLE LEFT HAND SIDE, FS697, WL158. REPAIRED IAW DRAWING R05-025-08 PER LAC MEA382-53-05-070, NR 0413. 2H74 4T A1SO 20051205000422005120500042SO 2005 12 5 LR7A05153 120051017A5311 FRAME LKHEED382 382G 526414USO FS 707 MISDRILLED A LR7AK NONE W INADEQUATE Q C ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER HC5313, FOUND FUSELAGE FRAME (LS5408-2) MISDRILLED LINER HOLE LEFT HAND SIDE, FS707, WL158. REPAIRED IAW DRAWING R05-025-08 PER LAC MEA382-53-05-070, NR 0413. 2H74 4T A1SO 20051205000432005120500043SO 2005 12 5 LR7A05154 120051017A5311 FRAME LKHEED382 382G 526414USO FS 727 MISDRILLED A LR7AK NONE W INADEQUATE Q C ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER HC5313, FOUND FUSELAGE FRAME (LS5408-2) MISDRILLED LINER HOLE LEFT HAND SIDE, FS727, WL158. REPAIRED IAW DRAWING R05-025-08 PER LAC MEA382-53-05-070, NR 0413. 2H74 4T A1SO 20051205000452005120500045SO 2005 12 5 LR7A05156 120051017A5311 FRAME LKHEED382 382G 526414USO FS 626 MISDRILLED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER HC5313, FOUND FUSELAGE FRAME (LS5408-2) MISDRILLED LINER HOLE RIGHT HAND SIDE, FS 626, WL158. REPAIRED IAW DRAWING R05-025-08 PER LAC MEA382-53-05-070, NR 0413. 2H74 4T A1SO 20051205000462005120500046SO 2005 12 5 LR7A05157 120051017A5311 FRAME LKHEED382 382G 526414USO FS 457 MISDRILLED A LR7AK NONE W INADEQUATE Q C ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER HC5313, FOUND FUSELAGE FRAME (LS4010-8) MISDRILLED LINER HOLE LEFT SIDE, FS 457, WL158. REPAIRED IAW DRAWING R05-025-07 PER LAC MEA382-53-05-071, NR 0414. 2H74 4T A1SO 20051205000502005120500050SO 2005 12 5 LR7A05161 120051017A5311 FRAME LKHEED382 382G 526414USO FS 377 MISDRILLED A LR7AK NONE W INADEQUATE Q C ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER HC5313, FOUND FUSELAGE FRAME (LS4010-8) MISDRILLED LINER HOLE RIGHT HAND SIDE, FS 377 WL151. REPAIRED IAW DRAWING R05-025-07 PER LAC MEA382-53-05-071, NR 0414. 2H74 4T A1SO 20051205000552005120500055SO 2005 12 5 LR7A05166 120051017A5320 BRACKET LKHEED382 382G 526414USO FS 1001 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER HC5212, FOUND CARGO DOOR BULKHEAD STIFFENER/TUBE STRUT ATTACH BRACKET CRACKED, FS 1001, RBL20. REPLACED ATTACH BRACKET IAW SRM SMP 583 51-70 AND AC43.13-1B, PARA 4-57 NR 0081. 2H74 4T A1SO 20051205000562005120500056SO 2005 12 5 LR7A05167 120051017A5320 BRACKET LKHEED382 382G 526414USO FS 1001 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2450 4590 ,DURING C-6 CHECK PER HC5212 FOUND CARGO DOOR BULKHEAD STIFFENER/TUBE STRUT ATTACH BRACKET CRACKED, FS 1001, RBL10. REPLACED ATTACH BRACKET IAW SRM SMP 583 51-70 AND AC43.13-1B, PARA 4-57 NR 0081. 2H74 4T A1SO 20051205000572005120500057SO 2005 12 5 LR7A05168 120051017A5320 BRACKET LKHEED382 382G 526414USO FS 1001 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER HC5212, FOUND CARGO DOOR BULKHEAD STIFFENER/TUBE STRUT ATTACH BRACKET CRACKED, FS1001, BL0. REPLACED ATTACH BRACKET IAW SRM SMP 583 51-70 AND AC43.13-1B, PARA 4-57 NR 0081. 2H74 4T A1SO 20051205000582005120500058SO 2005 12 5 LR7A05169 120051017A5320 BRACKET LKHEED382 382G 526414USO FS 1001 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER HC5212, FOUND CARGO DOOR BULKHEAD STIFFENER/TUBE STRUT ATTACH BRACKET CRACKED, FS 1001, LBL20. REPLACED ATTACH BRACKET IAW SRM SMP 583 51-70 AND AC43.13-1B PARA 4-57 NR 0081. 2H74 4T A1SO 20051205000612005120500061NM 2005 12 5 USAA051444 120051201A5320 INTERCOSTAL BOEING737 7374B7 1384702NM BS 307 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19780AU 24997 FOUND CABIN FLOOR INTERCOSTAL AT STA 307, RBL 15.5 CORRODED. REMOVED AND REPLACED, FABRICATED ANGLE PER SRM 51-40-02; CORROSION TASK C53-107-02, DEFECT SIZE: 1" BY 1". 2L72 4F RTA16WE 20051205000622005120500062NM 2005 12 5 USAA051434 120051201A5320 STRINGER CLIP BOEING737 7374B7 1384702NM STA 663.75, S-10CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 FOUND CRACK STA 663.75, S-10R. INSTALLED NEW TIE CLIP IAW 51-10-02, DEFECT SIZE: 1/2" CRACK. 2L72 4F RTA16WE 20051205000642005120500064NM 2005 12 5 USAA051436 120051201A5320UNKNOWN INTERCOSTAL BOEING737 7374B7 1384702NM BS 294 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19780AU 24997 FOUND MAIN CABIN STA 294, STR 16L, DOOR CUTOUT INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL AFT FAB PART, PER SRM 51-70-11 & 53-10-15, DEFECT SIZE: 2". 2L72 4F RTA16WE 20051205000652005120500065NM 2005 12 5 USAA051437 120051201A5320 INTERCOSTAL BOEING737 7374B7 1384702NM BS 294 CORRUPTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19780AU 24997 FOUND CRACK MAIN CABIN FRAME INTERCOSTAL STA 294, STR 11L. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-80-02, DEFECT SIZE: 2.5" 2L72 4F RTA16WE 20051205000672005120500067NM 2005 12 5 USAA051439 120051201A5315 FLOORBEAM BOEING737 7374B7 1384702NM BS 312 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19780AU 24997 FOUND CORROSION MAIN CABIN STA 312 RBL 21 FLOORBEAM UPPER CORD; CORROSION TASK C53-107-02. REMOVED AND REPLACED FLOORBEAM UPPER CORD AND L ANGLES AND INSTALLED SHIMS IAW SRM 53-10-5, DEFECT SIZE: 2L72 4F RTA16WE 20051205000682005120500068NM 2005 12 5 USAA051440 120051201A5320 SHEAR WEB BOEING737 7374B7 1384702NM BS 380-400 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19780AU 24997 FOUND CRACK CABIN FLOOR SHEAR WEB, BET STA 380-400, BL0. INSTALLED FAB SHEAR WEB UPPER CHORD ANGLE PER SRM 51-40-02, DEFECT SIZE: 2.5". 2L72 4F RTA16WE 20051205000692005120500069NM 2005 12 5 USAA051441 120051201A5320 SPLICE BOEING737 7374B7 1384702NM STRINGER CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19780AU 24997 FOUND STRINGER SPLICE BET APPROX STA 903-915, S4R. REMOVED 7, REPLACED FAB STRINGER SPLICE PER SRM 51-40-02, DEFECT SIZE: .25". 2L72 4F RTA16WE 20051205000702005120500070NM 2005 12 5 USAA051433 120051201A53101716930 SUPPORT BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 FOUND SMALL ZEE SUPPORT ON TOP OF AFT SERVICE DOORWAY Z ANGLE. REMOVED CORROSION, TREATED AND PRIMED IAW 53-60-15, DEFECT SIZE: 1" CORROSION TOP AND BOTTOM OF AFT SERVICE DOORWAY Z ANGLE. 2L72 4F RTA16WE 20051205000742005120500074NM 2005 12 5 UPS05245846 120051126A3350 LIGHT BOEING727 72731C 1384011NM EMERGENCY EXIT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 ONE LAMP INOP IN EMERGENCY EXIT LIGHT AT L1 DOOR. RELAMPED OK FOR SERVICE. 2L73 4F A3WE 20051205000782005120500078WP 2005 12 5 UPS05845845 120051129A2612 FIRE WARNING DOUG DC8 DC873F 302199FWP CARGO BAY ILLUMINATED A IPXAO OTHER N FALSE WARNING CRCRUISE 1 SO01808UP 46008 LOWER CARGO FIRE AMBER MX LIGHT CAME ON AFTER 4 HOURS OF FLIGHT (5 AND 11). PERFORMED ADJUSTMENT AND TEST PER DC-8 M/M 26-18-00-5, NO FAULTS FOUND IN MEMORY OR SIGNAL STRENGTH. 2L74 4F RT4A25 20051205000792005120500079 2005 12 5 SWIA200515902 420051122A22166225027001 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA SERVO ELEVATOR MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07412SW1579915799 7101 DURING CRUISE, STARTED TO FEEL A LIGHT FLUTTER IN THE HORIZONTAL AXIS (NOSE UP AND DOWN). SLOWED AIRCRAFT TO .77 AND TURNED OFF TURBULENCE MODE AND FLUTTER STOPPED. REPLACED ELEVATOR SERVO ACTUATOR. REMOVED AND NR 2 AND NR 3 ELEVATOR PCU'S AND REPLACED NR 1 PCU ROD END BOLT AND BUSHING IAW AMM 27-33-01.P/N: 27600-3, S/N OFF: MAL-0664, P/N: 27600-3 S/N OFF: MAL0420, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051205000812005120500081EA 2005 12 5 SWIA200515904 120051123A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07935SW 7725 RT WING FWD EMERGENCY EXIT LIGHT INOP. RELAMPED RT WING FWD EMERGENCY LIGHT BULB REF 33-40-00. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051206000032005120600003EA 2005 12 6 COMA0560652 120051127A2751 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01965CA 7131 FLIGHT 5850 - RECEIVED A FLAP FAIL CAUTION MESSAGE AFTER LANDING WHEN FLAPS WERE SELECTED TO 20 DEGREES. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION PARAGRAPH (B) 1,2,3 (A,B,C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2L72 4F RTA21EA 20051206000042005120600004EA 2005 12 6 COMA0560653 120051127A323046193 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA MLG FAULTY A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01983CA20972 7169 FLAP 5100 - EN ROUTE RSW-CVG, RECEIVED A GEAR DISAGREE WHEN GEAR WAS LOWERED, ABORTED FIRST APPROACH AT CVG, THEN LANDED WITHOUT INCIDENT ON SECOND ATTEMPT. REPLACED THE MLG PRIORITY VALVE. 2L72 4F RTA21EA 20051206000052005120600005NE 2005 12 6 COMA0560643 220051125A72616087T04P06 PUMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT ENGINE MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01510CA7104 7802 FLIGHT 5779 - RT ENGINE LOW OIL PRESSURE WARNING. REPLACED THE ENGINE OIL PUMP. 2L72 4F4 FRTA21EA E15NE 20051206000072005120600007EA 2005 12 6 COMA0560655 120051128A7930CF343A1 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE RIGHT LACK OF LUBE A COMAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SO01804CA16938 7352 807600 FLIGHT 5309 - EN ROUTE RDU-BOS RECEIVED A RIGHT ENGINE OIL PRESSURE WARNING MESSAGE, CREW DECLARED AN EMERGENCY, DIVERTED TO JFK AND PERFORMED IFSD OF THE RIGHT ENGINE. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE RIGHT ENGINE ASSEMBLY. 2L72 4F4 FRTA21EA E15NE 20051206000112005120600011NM 2005 12 6 05FDEA04070 120051202A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 DURING HFEC INSPECTION, FOUND CRACK ON RIGHT WING STRINGER 13. REPAIRED AS PER SRM 57-20-00 FIG. 10 VOL. I. AND CLIP REMOVED & REPLACED AS PER SRM 51-33-01 VOL.II. FABRICATED CLIP AS PER FEDEX EA 1-5720-90713 - WINGS - STRINGER 13 RH REPAIR PER SRM VOL.I 57-20-00 FIGURE 10 - FX ARB0449 CLIP FABRICATION. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20051206000122005120600012NM 2005 12 6 05FDEA04071 120051202A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 DURING HFEC INSPECTION, FOUND CRACK ON RIGHT WING STRINGER 14. REPAIRED AS PER SRM 57-20-00 FIG. 10 VOL. I. AND CLIP REMOVED & REPLACED AS PER SRM 51-33-01 VOL.II. FABRICATED CLIP AS PER FEDEX EA 1-5720-90712 - WINGS - STRINGER 14 RH REPAIR PER SRM VOL.I 57-20-00 FIGURE 10 - FX ARB2689-501 CLIP FABRICATION. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20051206000162005120600016WP 2005 12 6 05FDEA04076 120051202A5315 FLOORBEAM DOUG DC10 DC1030 3023501WP FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 DISCREPANCY IN THE AFT WASTE TANK AREA BULKHEAD STA 2007 FOUND NEW SECTION OF FLOOR T-CAP ANGLE Z-19 LENGTH 35" FROM X75 TO X 40 AND JUNCTION SPLICE. PERFORMED A GVI OF REPAIR IAW SRM 53-40-00 FIG 16 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001-2P E3, PERFORMED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VOL 2 PAR 33. 2L73 4F A22WE 20051206000172005120600017WP 2005 12 6 05FDEA04077 120051202A5320 REPAIR DOUG DC10 DC1030 3023501WP FUSELAGE UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 FOUND CENTER CARGO COMPT FOUND A NEW SECTION OF BEAM AT STA 1701 X-60 TO X-22 Z-100, DIMENSION 40" LENGTH WITH A SPLICE 8" LONG AND 5" HEIGHT. PERFORMED A GVI OF REPAIR IAW SRM 53-60-01 FIG 3 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001-2D E3 RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VOL 2 PAR 33. 2L73 4F A22WE 20051206000182005120600018NM 2005 12 6 05FDEA04055 120051201A5230 SKIN BOEING727 727233 138408ANM ZONE 100 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25220FE 20934 RESKIN C-3 DOOR DUE TO, TOO MANY REPAIRS ON OUTER SKIN. REMOVED AND REPLACED SKIN P/N 65-56927-2 IAW B727 SRM 51-10-2,51-30-2 AND 51-30-5. MINOR REPAIR SIGNED BY NR 1560 QC334. 2L73 4F RTA3WE 20051206000192005120600019EU 2005 12 6 05FDEA04056 120051201A5512 REPAIR AIRBUS310 A310203 3930313EU HORIZONTAL STAB UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 REPAIR ASSESSMENT. HORIZONTAL STAB LE PANEL 331AB. EXISTING REPAIR BETWEEN RIB 2 - 3 LOWER SURFACE. EXISTING REPAIR NOT IAW A310-200 SRM 55-12-12. REMOVED 2 REPAIR ANGLES IAW A310-200 SRM51-40-21. FABRICATED AND INSTALLED NEW ANGLES IAW A310-200 SRM 55-12-12. MINOR REPAIR PER GMM 6-2-100. WORKED ON NRC N00758. 2L72 4F RTA35EU 20051206000202005120600020EU 2005 12 6 05FDEA04057 120051201A5330 REPAIR AIRBUS310 A310203 3930313EU ZONE 200 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 PREVIOUS REPAIR INSTALLED AT FUSELAGE LT SIDE FLUSH REPAIR AFT OF MAIN DECK CARGO DOOR STA 1923 - 1976 FS 35-36, STR 10-11, NEEDS EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR INSTALLED AS PART OF P-F CONVERSION AND MEETS REQUIREMENTS OF DWG R537B1607. NO FURTHER ACTION REQUIRED. MINOR REPAIR PER GMM 6-2-100. WORKED ON NRC N00697. 2L72 4F RTA35EU 20051206000212005120600021EU 2005 12 6 05FDEA04058 120051201A5320 COVER AIRBUS310 A310203 3930313EU ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 MAIN CARGO COMPARTMENT, FS 75L, ABOVE AFT PAX DOOR CORRODED. REPLACED FILLER, ANGLE AND SHIM IAW A310-200 SRM 53-18-18. MINOR REPAIR PER GMM 6-2-100. WORKED ON NRC N00207. 2L72 4F RTA35EU 20051206000222005120600022NM 2005 12 6 05FDEA04059 120051201A5230 REPAIR BOEING727 727233 138408ANM ZONE 100 IMPROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25220FE 20934 EXISTING REPAIR AT STA 1148-1166 STR 25L IS NOT PER SRM DATA. INSTALLED EXTERNAL REPAIR DOUBLER IAW B727 SRM 53-30-3 FIG 3. 2L73 4F RTA3WE 20051206000232005120600023EU 2005 12 6 05FDEA04060 120051201A5330 REPAIR AIRBUS310 A310203 3930313EU ZONE 100 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 PREVIOUS REPAIR INSTALLED AT FUSELAGE LT SIDE FS 39, LT STR 51 - 54, EXTERNAL DOUBLER FWD OF NR 1 AC PACK INLET FAIRING NEEDS EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR HAS BEEN ACCOMPLISHED IAW A310-200 SRM 53-15-12 FIG 201. NO FURTHER ACTION REQUIRED. MINOR REPAIR PER GMM 6-2-100. WORKED ON NRC N00693. 2L72 4F RTA35EU 20051206000242005120600024EU 2005 12 6 05FDEA04061 120051201A5414 REPAIR AIRBUS310 A310203 3930313EU NR 1PYLON UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 PREVIOUS REPAIR INSTALLED ON NR 1 PYLON LT SIDE OB AFT LWR FAIRING EXTERNAL DOUBLER AT RIB 20, NEEDS EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR FOUND NOT TO BE I/A/W A310-200 SRM 54-54-51 FIG 203. REMOVED EXISTING REPAIR I/A/W A310-200 SRM 51-40-21. FABRICATED AND INSTALLED NEW DOUBLER IAW A310-200 SRM 54-54-51 FIG 203. MINOR REPAIR IAW GMM 6-2-100. WORK PEFORMED ON NRC N00704. 2L72 4F RTA35EU 20051206000252005120600025NM 2005 12 6 05FDEA04062 120051201A5230 REPAIR BOEING727 727233 138408ANM ZONE 100 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25220FE 20934 EXISTING REPAIR DOUBLER ON C-1 CARGO DOOR FORWARD LOWER CORNER IS NOT PER SRM DATA. REMOVED AND REPLACED REPAIR DOUBLER IAW B727 SRM 52-00-3, FIG 3. 2L73 4F RTA3WE 20051206000262005120600026EU 2005 12 6 05FDEA04063 120051201A5343 FITTING AIRBUS310 A310203 3930313EU LT MLG WW CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 LT MAIN GEAR WHEEL WELL LOWER AFT CORNER FITTING HAS 15 SQ" OF CORROSION. FABRICATED NEW SPLICE FITTING IAW 6-5315-94776. REPLACED CORRODED SPLICE FITTING IAW EA 6-5315-94755. MINOR REPAIR IAW GMM 6-2-100. WORK PERFORMED ON NRC N00739. 2L72 4F RTA35EU 20051206000272005120600027EU 2005 12 6 05FDEA04064 120051201A5313 STRINGER AIRBUS310 A310203 3930313EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 AIR COND BAY LT SIDE FS 44-FS 47 LT STRINGER 47 HAS 15 SPOTS OF LT CORROSION AS MARKED. REMOVED FASTENERS IAW A310-200 SRM 51-40-21. REMOVED CORROSION IAW A310-200 SRM 51-74-10. MATERIAL LOSS WITHIN ALLOWABLE LIMITS IAW A310-200 SRM 53-10-00. OVERSIZED HOLE REPAIRED BY INSTALLING 2 BUSHINGS AND REPAIR ANGLE IAW EA 6-5310-94773. MAJOR REPAIR PER GMM 6-2-100. WORK PERFORMED ON NRC N00657. 2L72 4F RTA35EU 20051206000292005120600029NM 2005 12 6 05FDEA04043 120051130A5730 SKIN DOUG MD11 MD11F 3023600NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RIGHT WING FIXED LEADING EDGE FOUND CRACKED AT TELESCOPE DUCT UPPER CUTOUT. REPAIR CARRIED OUT AT RIGHT HAND WING FIXED LEADING EDGE TELESCOPING DUCT UPPER SKIN CUTOUT AS PER FEDEX EA 1-5730-90693, TITLE "WINGS - RT WING LEADING EDGE SKIN CRACKS AT TELESCOPING DUCT CUTOUT". 2L73 4F RTA22WE 20051206000302005120600030EU 2005 12 6 05FDEA04044 120051201A5730 REPAIR AIRBUS310 A310203 3930313EU ZONE 600 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 PREVIOUS REPAIR INSTALLED ON RT IB FLAP UPPER SURFACE RIB 17-19, NEEDS EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. THE REPAIR AS NOTED CONFORMS TO SRM 57-52-12 FIG 204 WITH THE EXCEPTION OF FASTENER PITCH. LOCATED AND DRILLED FASTENER HOLE TO COMPLY WITH FASTENER PITCH PER A310-200 SRM 51-40-45. INSTALLED NEW FASTENERS MS20426 A4D IAW A310-200 SRM 51-40-21. NOW PREVIOUSLY INSTALLED REPAIR IS DETERMINE TO BE IAW A310-200 SRM 57-52-11 FIG 204 BASED ON EVALUATION OF LOCATION, SHAPE, SIZE, FASTENER SPACING/NUMBER, AND MATERIAL TYPE/THICKNESS. WORK DOCUMENTED ON NRC N00713. 2L72 4F RTA35EU 20051206000332005120600033EU 2005 12 6 05FDEA04047 120051201A5330 REPAIR AIRBUS310 A310203 3930313EU FUSLEAGE UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 PREVIOUS REPAIR INSTALLED ON FUSELAGE RT SIDE, EXTERNAL DOUBLER AT FR15 BELOW R1 DOOR SCUFF PLATE, NEEDS EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED IAW A310-200 SRM 53-12-12 PB 201. EXISTING REPAIR INSTALLED ON EA6-5330-46467 AND REQUIRES NO FURTHER ACTION. 2L72 4F RTA35EU 20051206000342005120600034NM 2005 12 6 05FDEA04048 120051201A5330 REPAIR BOEING727 727233 138408ANM ZONE 100 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25220FE 20934 FOUND REPAIR LOCATED AT FUSELAGE, RIGHT SIDE STA 1174-1203 STR 19-20. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. INSTALLED NEW REPAIR IAW FED EX B727 P-F SRM 53-30-3 FIG.1A. 2L73 4F RTA3WE 20051206000352005120600035NM 2005 12 6 05FDEA04049 120051201A5320 STRUCTURE BOEING727 727227 1384078NM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 UPON REMOVAL OF REPAIR ON AFT AIRSTAIR (FEDEX CARD 30956, N01070) FOUND CHORD TO BE DAMAGED. REPAIRED CHORD PER SRM 51-30-2. 2L73 4F A3WE 20051206000362005120600036NM 2005 12 6 05FDEA04050 120051201A5260 REPAIR BOEING727 727227 1384078NM AIRSTAIR DOOR UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 TEMPORARY REPAIR INSTALLED ON AIR STAIR DOOR EXTERNAL ON AIR STAIR DOOR EXTERNAL SKIN LT FWD CORNER. REPAIRED DOOR PER SRM 51-30-2. 2L73 4F A3WE 20051206000382005120600038WP 2005 12 6 ABXA050305 120051107A53205779935 WEB DOUG DC8 DC863F 302198FWP STA. 847 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 PSI WEB FROM STA 847, LEFT BUTT LINE 40 - 60 CORRODED. FABRICATED PSI WEB FROM STA 847, LEFT BUTT LINE 40 - 60 IAW DC8 REA D853-52534. MATERIAL USED .063 2024-T3, P/O NR 1118786. 2L74 4F 4A25 20051206000392005120600039WP 2005 12 6 ABXA050302 120051107A53205644678 SPLICE DOUG DC8 DC863F 302198FWP STA. 857 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 SHIM SPLICE CORRODED AT STA 857, LEFT BUTT LINE 20. FABRICATED SHIM AT STA 857, LEFT BUTT LINE 20 IAW DC8 REA D853-52536. MATERIAL USED .090 P/O NR 1112038. 2L74 4F 4A25 20051206000422005120600042EA 2005 12 6 COMA0560648 120051126A2752852D10019 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA LT WING FLAP FAULTY A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01735CA9022 7267 FLIGHT 5556 - EN ROUTE CVG-PWM, RECEIVED A FLAP FAIL MESSAGE AT ZERO DEGREE FLAP POSITION. CREW DECLARED AN EMERGENCY AND FLIGHT LANDED SAFELY AT PWM. 2L72 4F RTA21EA 20051206000442005120600044EA 2005 12 6 COMA0560658 120051130A7732 VIBRATOR CNDAIRCL600 CL6002B19 1900309EA LT ENGINE UNKNOWN A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01435CA 7473 FLIGHT 5525 - LT ENGINE VIBE CAUTION. FOUND LT ENGINE VIBRATION TO BE WITHIN LIMITS. RETURNED TO SERVICE. 2L72 4F RTA21EA 20051206000462005120600046EA 2005 12 6 COMA0560649 120051126A2750860D10018ABCD FCU CNDAIRCL600 CL6002B19 1900309EA AVIONICS BAY FAULTY A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01735CA6970 7267 FLIGHT 5556 - EN ROUTE CVG-PWM, RECEIVED A FLAP FAIL MESSAGE AT ZERO DEGREE FLAP POSITION. CREW DECLARED AN EMERGENCY AND FLIGHT LANDED SAFELY AT PWM. REPLACED THE FLAP ELECTRONIC CONTROL UNIT. 2L72 4F RTA21EA 20051206000472005120600047WP 2005 12 6 05FDEA04082 120051202A5312 REPAIR DOUG DC10 DC1030 3023501WP BULKHEAD UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 PERFORMED INSPECTION IAW EO NR 8-5100-7-5001-1P, FOUND ANGLE LENGTH 30" ON AFT CARGO BULKHEAD PRESSURE STA 2007 X =0 Z-19. PERFORMED A GVI OF REPAIR IAW SRM 53-40-00 FIG 16 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VOL 2 PAR 33. 2L73 4F A22WE 20051206000482005120600048WP 2005 12 6 05FDEA04078 120051202A5753 REPAIR DOUG DC10 DC1030 3023501WP TE FLAP UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 RT WING INBOARD FLAP FOUND DOUBLER REPAIR ON LOWER SKIN AT STA XIFH 210 DIMENSION 5 INCH BY 3 INCH. PERFORMED A GVI OF REPAIR IAW SRM 57-00-01 FIG 4 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 2P RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VOL 2 PAR 33. 2L73 4F A22WE 20051206000492005120600049WP 2005 12 6 05FDEA04079 120051202A5753 REPAIR DOUG DC10 DC1030 3023501WP TE FLAP UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 FOUND RIGHT WING INBOARD FLAP FOUND DOUBLER REPAIR ON UPPER SKIN AT STA XIFH294 DIMENSION 4.5" BY 8". PERFORMED A GVI OF REPAIR IAW SRM 57-00-01 FIG 4 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001-P2 RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VOL 2 PAR 33. 2L73 4F A22WE 20051201001632005120100163EU 2005 12 1 05FDEA03995 120051128A5330 SKIN AIRBUS310 A310 EU PWA JT9 JT9D* NE ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25450FE 162 PUNCTURE, DENT, AND GOUGES IN SKIN AT FR 46 RT STRINGERS 7-9. DAMAGE AREA APPROX 11.5 INCH X 7 INCH. CUT OUT DAMAGED AREA TO SKING ANS STRINGER IAW A310-200 SRM 53-10-12 AND 53-10-14. PERFORMED HFEC IAW NTM 51-10-08. NO CRACKS NOTED. SPLICED STRINGERS IAW A310-200 SRM 53-10-14. INSTALLED SKIN DOUBLER IAW A310-200 SRM 53-10-12. 2L72 4F4 FRTA35EU E20EA 20051201001652005120100165NM 2005 12 1 05FDEA04027 120051129A5347 SEAT TRACK DOUG MD11 MD11 3023602NM PWA 4460 PW4460 NE ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 FS 5-0 TO 1501 LBL 21 FOUND SEAT TRACK WITH CORROSION. REMOVED AS PER SRM 51-21-01. FOUND EXCEEDED LIMIT AS PER SRM 53-70-00. REMOVED AT EXISTING SPLICE AND TRIMMED AS PER SRM 53-70-00. NEW SEAT TRACK REWORKED AND INSTALLED AS PER SRM 53-70-00 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2L73 4F4 FRTA22WE E24NE 20051201001672005120100167NM 2005 12 1 05FDEA04029 120051130A5330 REPAIR DOUG MD11 MD11 3023602NM PWA 4460 PW4460 NE ZONE 100 NONE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 SNRM N1460: FORWARD CARGO - STA 1079 LONGERON 27R FOUND WITH EXISTING REPAIR. REPAIR PREVIOUSLY ACCOMPLISHED IN ACCORDANCE WITH MD11 SERVICE BULLETIN 53-042 R02. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. THIS IS NOT A REPORTABLE ISSUE. NO DEFECT OR MALFUNCTION. 2L73 4F4 FRTA22WE E24NE 20051201001692005120100169NM 2005 12 1 05FDEA04031 120051130A5330 REPAIR DOUG MD11 MD11 3023602NM PWA 4460 PW4460 NE ZONE 100 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 SNRM N1609: REFERENCE TO E1-5100-7-5001 PT1 - FORWARD CARGO - STA 839 TO 859 LONGERON 27R FOUND WITH EXISTING REPAIR. REPAIR PREVIOUSLY ACCOMPLISHED IN ACCORDANCE WITH MD11 SERVICE BULLETIN 53-042 R02. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. NARI, NO M OR D. 2L73 4F4 FRTA22WE E24NE 20051201001702005120100170SO 2005 12 1 Z4TA20050005 220051110A8500 ENGINE BEECH 58 58 1152740CE CONT O550 IO550C SO RIGHT SEIZED E Z4TAA UNSCHED LANDING RY PARTIAL RPM/PWR LOSS ENGINE STOPPAGE CRCRUISE 1 SO0595KM TH1315 810485 PILOT WAS IN CRUISE FLIGHT. HEARD POP AND NOTICED RT ENGINE WAS WINDMILLING. FEATHERED PROPELLER. ATTEMPTED RESTART BUT WAS UNSUCCESSFUL. LANDED AT ALTERNATE FIELD. ON GROUND, DISCOVERED RT ENGINE PROPELLER WOULD NOT TURN - SEIZED. 1L72 3O3 O 3A16 E3SO 20051201001722005120100172WP 2005 12 1 IXXA05RNG068S 120050906A5730 SKIN DOUG DC8 DC872 302199BWP STA XRS 40.869 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK WAS FOUND A CORROSION ON WING UPPER SKIN STA XRS 40.869 REAR SPAR TO AUX SPAR - LT. REPORTED AREA WAS BLENDED OUT AND REINFORCEMENT DOUBLER WAS FABRICATED AND INSTALLED IAW EO ATI-091005 AND EWO ATI 57-045. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR. 2L74 4F RT4A25 20051201001742005120100174WP 2005 12 1 IXXA05RNG099S 120051028A5730 SKIN DOUG DC8 DC872 302199BWP STA XFS710.50 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK WAS FOUND A CORROSION ON CENTER EXTENDED LEADING EDGE LOWER SKIN AROUND STA XFS 710.50-RT. DAMAGED AREA WAS BLENDED OUT AND A REINFORCEMENT DOUBLER WAS FABRICATED AND INSTALLED IAW EO ATI-092905 AND EWO ATI-57-063. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR. 2L74 4F RT4A25 20051201001752005120100175SO 2005 12 1 LR7A05119 120051017A5320 STIFFENER LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FS 1023 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2450 4590 DURING C -6 CHECK PER HC5212, FOUND CARGO DOOR AFT BULKHEAD WEB STIFFENERS CRACKED, FS 1023, RBL20. REPLACED WEB STIFFENERS IAW SRM SMP 583 FIGURE 51-70 AND AC43.13-1B PARA 4-57, NR 0106. 2H74 4T4 T A1SO E282 20051201001762005120100176SO 2005 12 1 LR7A05120 120051017A5320 STIFFENER LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FS 1023 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2450 4590 DURING C -6 CHECK IAW HC5212, FOUND CARGO DOOR AFT BULKHEAD WEB STIFFENERS CRACKED, FS1023, RBL30. REPLACED WEB STIFFENERS IAW SRM SMP 583 FIGURE 51-70 AND AC43 13-1B PARA 4-57, NR 0106. 2H74 4T4 T A1SO E282 20051201001772005120100177SO 2005 12 1 LR7A05121 120051017A5320 STIFFENER LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FS 1023 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2450 4590 DURING C -6 CHECK IAW HC 5212, FOUND CARGO DOOR AFT BULKHEAD WEB STIFFENERS CRACKED, FS 1023, RBL40. REPLACED WEB STIFFENERS IAW SRM SMP 583 FIGURE 51-70 AND AC43 13-1B PARA 4-57, NR 0106. 2H74 4T4 T A1SO E282 20051201001782005120100178SO 2005 12 1 LR7A05122 120051017A5320 STIFFENER LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FS 1023 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK IAW HC5212, FOUND CARGO DOOR AFT BULKHEAD WEB STIFFENERS CRACKED, FS1023, LBL20. REPLACED WEB STIFFENERS IAW SRM SMP 583 FIGURE 51-70 AND AC43.13-1B PARA 4-57, NR 0106. 2H74 4T4 T A1SO E282 20051201001792005120100179SO 2005 12 1 LR7A05123 120051017A5320 ANGLE LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FS 1023 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK IAW HC5212, FOUND CARGO DOOR BULKHEAD WEB STIFFENERS CRACKED, FS 1023, LBL33. REPAIRED STIFFENER ANGLES IAW SRM 51-140-19, NR 0107. 2H74 4T4 T A1SO E282 20051201001802005120100180SO 2005 12 1 LR7A05124 120051017A5320 ANGLE LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FS 1023 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK IAW HC5212, FOUND CARGO DOOR BULKHEAD WEB STIFFENERS CRACKED, FS 1023, LBL36. REPAIRED STIFFENER ANGLES IAW SRM 51-140-19, NR 0107. 2H74 4T4 T A1SO E282 20051201001812005120100181SO 2005 12 1 LR7A05125 120051017A5320 ANGLE LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FS 1023 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK IAW HC5212, FOUND CARGO DOOR BULKHEAD WEB STIFFENERS CRACKED, FS 1023, RBL25. REPAIRED STIFFENER ANGLES IAW SRM 51-140-19, NR 0107. 2H74 4T4 T A1SO E282 20051201001822005120100182 2005 12 1 BSYA200500020 420051115A342252D1371333 GYRO CESSNA208 208 2073702CE DIRECTIONAL FAILED E BSYAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL079642F 20800110 AFTER TAKEOFF, DIRECTIONAL GYRO QUIT, AIRCRAFT RETURNED TO DEPARTURE. REMOVED AND REPLACED GYRO, CHECKS GOOD. 1H71 3T NTA37CE 20051201001852005120100185SO 2005 12 1 1360112205 120051122A32331159SCL41000145 ACTUATOR GULSTMG1159 GIV 3980115SO RROYCETAY TAY6118 EU MLG LEAKING E N93AA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO13460QS2356 1360 CHECK HYD QTY MSG ILLUMINATED, QTY WENT TO ZERO, PRESSURE REMAINED AT 3000 PSI. UPON GEAR EXTENSION LEVEL WENT ABOVE LOW. 2L72 4F4 FRTA12EA E25NE 20051201001872005120100187NM 2005 12 1 AWXA200501461 120051119A53406935352U14 STRINGER CLIP BOEING737 7373G7 1384595NM GE CFM56 CFM563B1 13802NE BS 727C CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 MAJOR REPAIR - DURING C19 CHECK DISCOVERED STRINGER CLIP CRACKED, .25 INCHES IN LENGTH, AT BS 727C AND STRINGER 4L. MAINTENANCE REMOVED STRINGER CLIP AND INSTALLED NEW CLIP AT BS 727C AND STRINGER 4L IAW SRM 51-40-02-G FIG 3, 8 AND 12. 2L72 4F4 FRTA16WE E2GL 20051201001892005120100189NM 2005 12 1 AWXA200501463 120051119A53406935352U14 STRINGER CLIP BOEING737 7373G7 1384595NM GE CFM56 CFM563B1 13802NE BS 887 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 MAJOR REPAIR - DURING C19 CHECK DISCOVERED STRINGER CLIP CRACKED, .50 INCHES IN LENGTH, AT BS 887 AND STRINGER 4L. MAINTENANCE REMOVED STRINGER CLIP AND INSTALLED NEW CLIP AT BS 887 AND STRINGER 4L IAW SRM 51-40-02-G FIG 3, 8 AND 12. 2L72 4F4 FRTA16WE E2GL 20051201001912005120100191NM 2005 12 1 AWXA200501465 120051103A575465C267995 SKIN BOEING737 7373G7 1384595NM GE CFM56 CFM563B1 13802NE ZONE 500 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 MAJOR REPAIR - DURING C19 CHECK DISCOVERED CRACKS ON THE BOTTOM OF THE NR 1 SLAT SKIN AT 10 FASTENERS BELOW ACTUATOR FROM SLAT STATION (SS) 317L TO SS 327L. MAINTENANCE CUTOUT DAMAGED PART OF SKIN IAW SRM 57-43-01-2R6 FIG 201. FABRICATED FILLER AND SPLICE PLATE IAW SRM 57-43-01-2R6. INSTALLED FABRICATED REPAIR PARTS ON THE BOTTOM OF THE NR 1 SLAT FROM SS 317L TO SS 327L. 2L72 4F4 FRTA16WE E2GL 20051202000012005120200001EU 2005 12 2 USAA051431 120051130A5320D5348004320401 SILL AIRBUSA321 A321211 3930370EU BETWEEN FR 67-68CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19164UW 1425 BETWEEN FR 67-68 Y1160, REPLACED SILL IAW SRM 51-72-11 DWG. 53480505; LEVEL 1; TASK JA-260-53500 DEFECT SIZE: .5 INCH X .5 INCH. 2L72 4F RTA28NM 20051202000022005120200002EU 2005 12 2 USAA051430 120051130A5315D5347209200000 FLOORBEAM AIRBUSA321 A321211 3930370EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19164UW 1425 Y765 BETWEEN FR 67-68 ON PAX COMPARTMENT FLOORBEAM REMOVED AND REPLACED FLOORBEAM IAW SRM 51-72-11; CORR. LEVEL 1; TASK JA-260-53500 DEFECT SIZE: 2 SQ. IN. 2L72 4F RTA28NM 20051202000042005120200004EU 2005 12 2 USAA051428 120051130A5315D5311282600101 FLOORBEAM AIRBUSA321 A321211 3930370EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19164UW 1425 PAX FLOORBEAM AT Y503, FR 14-16, REMOVED AND REPLACED FLOORBEAM IAW SRM 51-72-11; CORR. LEVEL 1; TASK JA-220-53500 DEFECT SIZE: 2 SQ. IN. 2L72 4F RTA28NM 20051202000122005120200012NM 2005 12 2 AWXA200501473 120051102A5755654645163A PANEL BOEING737 7373G7 1384595NM GE CFM56 CFM563B1 13802NE ZONE 500 - LT DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 DURING C19 CHECK DISCOVERED DEBONDED AREA ON THE UPPER AND LOWER SURFACE OF THE NR 3 SPOILER PANEL FROM WBL 229.0L TO WBL 304.5L. MAINTENANCE REMOVED DAMAGED AREA ON THE NR 3 SPOILER PANEL IAW SRM 51-70-10-2R4. FABRICATED REPAIR DOUBLER AND REPAIR CORE IAW SRM 51-70-10-2R4. BONDED FABRICATED REPAIR PARTS TO THE NR 3 SPOILER PANEL FROM WBL 229.0L TO WBL 304.5L IAW SRM 51-70-10-2R4. 2L72 4F4 FRTA16WE E2GL 20051202000262005120200026NM 2005 12 2 UPS05M45838 120051126A3260 SENSOR DOUG MD11 MD11F 3023600NM LANDING GEAR MALFUNCTIONED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP 48575 INSPECTION TYPE:N/A ATB - NOSE STRUT ON GND SENSOR WAS IN GND MODE AIRBORNE CYCLE D L/R GND SENSING BREAKER NO AUTO PILOT, NO AUTO THROTTLES. ACTUATED LT AND RT GROUND SENSING SWITCHES NO DEFECTS NOTED TO AFFECTED SYSTEMS IAW SSM 32-24-0. RESET ACFT POWER AND PERFORMED FCC1 AND 2 RTS CAT III B TEST IAW MM 22-02-00-5. PASSED ALL TEST. OK FOR SERVICE. 2L73 4F RTA22WE 20051202000272005120200027NM 2005 12 2 SB05157 120051125A27511817389 TRANSMITTER BOEING737 7374B7 1384702NM LT WING FAULTY A USAAL ABORTED APPROACH F FLT CONT AFFECTED APAPPROACH 1 EA19440US4079440794 24811 ON APPROACH, THE FLAPS STOPPED AT 2 UNITS WHEN SELECTED TO 5 UNITS. CREW ACCOMPLISHED GO-AROUND. WHILE PERFORMING QUICK REFERENCE HANDBOOK PROCEDURES, FLAPS WENT TO 5 UNITS AND WORKED NORMAL UNTIL SELECTION OF 30 UNITS. LT FLAP INDICATION SHOWED 125 UNITS, WHILE RT SHOWED 30 UNITS. NO ROLL WAS NOTED AS FLIGHT LANDED WITHOUT FURTHER INCIDENT. FLAP INDICATION WENT TO 30 UNITS WHILE UTILIZING ALTERNATE FLAP DRIVE SYSTEM. MAINTENANCE REMOVED AND REPLACED THE LT FLAP POSITION TRANSMITTER. OPERATIONAL CHECK GOOD IAW MM 27-58-12. 2L72 4F RTA16WE 20051202000302005120200030WP 2005 12 2 ABXA050286 120051122A3350 BATTERY DOUG DC9 DC931 3022065WP PWA JT8 JT8D* NE EMERGENCY LIGHTSWEAK A ABXAK NONE O OTHER ININSP/MAINT 1 GL23942AX 47552 EMERGENCY LIGHTS WERE INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERIES. OPS CHECK GOOD, IAW AMM 33-53-00-0-0001. 2L72 4F4 F A6WE E2EA 20051202000342005120200034EU 2005 12 2 AWXA200501456 120051126A335032145410 POWER SUPPLY AIRBUS320 A320231 3930325EU LT AFT FAILED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28644AW2254 2254 317 OVERNIGHT MAINTENANCE DISCOVERED EMERGENCY LIGHT TEST FAILING, FAULT (115 VAC AFT L) PRESENT. MAINTENANCE REMOVED AND REPLACED THE LT AFT POWER SUPPLY IAW MM 33-51-38-04. VENDOR CONFIRMED FAULT. UNIT WAS REPAIRED AND TESTED IAW CMM 33-51-09 REV.2 2L72 4F RTA28NM 20051202000402005120200040CE 2005 12 2 JBGA20050006 120051117A3260 UPLOCK SWITCH LEAR 35 35A 5170602CE MLG DOOR LOOSE E JBGAO OTHER N FALSE WARNING CLCLIMB 1 GL07357LJ 357 IB GEAR DOOR LIGHTS WOULD NOT EXTINGUISH AFTER TAKEOFF, CYCLED GEAR THEN EVERY THING NORMAL. AFTER GETTING TO HPN GOT A FERRY PERMIT TO GO FOR MAINTENANCE TO LOOK AT GEAR OPERATION. INSTALLED NEW RIVETS IN LOOSE LT IB DOOR UPLOCK SWITCH MOUNTOPS CHECKS GOOD. 2L72 4F A10CE 20051202000422005120200042EA 2005 12 2 REXA200500140 120051124A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A REXAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO258733G 7733 FLAPS FAILED ON APPROACH AT 8 DEGREES. QRH FOLLOWED WITH UNEVENTFUL LANDING. REST FLAPS AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. 2L72 4F RTA21EA 20051202000492005120200049SO 2005 12 2 PNSA051105 120051117A711013076 COWLING GRUMAVG21 G21A 3951204SO PWA R985 R985* 52008NE LT ENGINE DEPARTED E PNSAK NONE O OTHER CRCRUISE 1 AL0322932 B139 WHILE IN CRUISE FLIGHT THE LT ENGINE COWLING DEPARTED THE AIRCRAFT. THE COWLING'S WAS NOT RECOVERED, FLIGHT WAS OVER WATER. AN UNEVENTFUL LANDING WAS MADE. SINCE THE FLIGHT WAS OVER WATER IT COULD NOT BE DETERMINED WHY THE COWLINGS DEPARTED THE AIRCRAFT. 1H72 3R3 R TC654 5E1 20051202000542005120200054NE 2005 12 2 TSAA0579054 220051015A726169726881 SWITCH BOEING737 737282C 13844AUNM PWA JT8 JT8D NE NR 1 ENGINE FAILED A TSAAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 WP13826AL 23051 CREW SHUTDOWN NR 1 ENGINE AFTER OIL FILTER BYPASS LIGHT ILLUMINATED. CREW THEN LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE OIL BYPASS SWITCH IAW MM 79-35-11. ALSO REMOVED AND REPLACED MAIN OIL STRAINER IAW MM 72-61-53 AS A PRECAUTION. NO DEFECTS NOTED. OPS AND LEAK CHECKS OK IAW MM 79-35-0 AND MM 72-61-53. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA16WE E2EA 20051202000562005120200056NM 2005 12 2 ASAA0540515 120050928A5322654653112 SHEAR TIE BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU BS 460 BENT A ASAAK NONE O OTHER ININSP/MAINT 1 NM02793AS 28888 FWD CARGO BAY SHEAR TIE BENT. REMOVED BENT SHEAR TIE, FABRICATED AND INSTALLED NEW SHEAR TIE IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051202000602005120200060SO 2005 12 2 GLBA20050593 120051126A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT DISCHARGED A GLBAO OTHER O OTHER TXTAXI/GRND HDL 1 NM03293GL1039 120293 FRONT EMERGENCY LIGHTS INOPERATIVE, REPLACED BATTERY PACK. 2L72 4T RTA31SO 20051202000612005120200061NE 2005 12 2 NACA20050027 220051107A8530356993 CYLINDER CB3 DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE ENGINE CRACKED A NACAE ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TXTAXI/GRND HDL 1 AL032907F322 322 533265 NK510186 PRECAUTIONARY ENGINE FEATHER ON GROUND DUE TO OIL LOSS AND RUNNING ROUGH. FOUND NR 18 CYLINDER CRACKED. REPLACED NR 18 CYLINDER IAW MM SECT V PG. 16 AND 16A. OP CHECKED GOOD. 2L74 4R4 R A781 5E8 20051202000842005120200084SO 2005 12 2 PNSA051103 120051116A291078738805 AXLE PIPER PA32 PA32301 7103207SO LYC O540 IO540K1G5 41532EA RAT BROKEN E PNSAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 AL0381052 328206023 AIRCRAFT WAS DEPARTING WITH QUARTERING CROSSWIND JUST AS THE AIRCRAFT WAS ROTATING PILOT FELT AND HEARD A (THUD) ON THE RT SIDE OF AIRPLANE. AIRCRAFT RETURNED TO ITS MAINTENANCE BASE AND A FLYBY WAS MADE AND IT WAS DISCOVERED THAT THE RAT WHEEL AND AXLE ASSEMBLY WAS MISSING FROM AIRCRAFT. A UNEVENTFUL LANDING WAS MADE AND AIRCRAFT WAS MOVED TO HANGER FOR DAMAGE ASSESSMENT. MAINT DISCOVERED THAT THE AXLE FAILED AT THE INNER BEARING RACE AREA OF AXLE. 1L71 3O3 O A3SO 1E4 20051202000852005120200085NM 2005 12 2 ANCF200400060 120051115A2750 LEVER BOEING757 75728A 1384976NM TE FLAPS MALFUNCTIONED W ANCFO OTHER O OTHER CLCLIMB 1 SO23506NA 24771 BOTH FLAP POINTERS ARE ON HALF WITH THE FLAP LEVER IN UP. L/E SLAT DISAGREE LIGHT ILLUM. L/E SLAT DISAGREE DISPLAY ON EICAS. (VOICE RECORDER CB PULL OUT ACCORDING TO SECURITY BULLETIN) IAW AMM 27-09-00 PAGE 201 FSEU N° 2 AND 3 WERE SWAPPED. NO FAULT NOTED ON GROUND, CHECK SYSTEM IAW AMM 27-02-00 PAGE 601. SYSTEM OPERATIONAL CHECK WAS SATISFACTORY. SENSOR SS5050 WAS CHECKED AND NO PROBLEMS FDOUND. 2L72 4F RTA2NM 20051202000962005120200096NM 2005 12 2 ANCF200400059 120051018A5270 WARNING LIGHT BOEING757 757236 1384971NM CARGO DOOR FALSE ACTIVATIONW ANCFO OTHER N FALSE WARNING CLCLIMB 1 SO23506NA EICAS MSG (AFT CARGO DOOR 2) AFTER CLOSE DOORS IAW AMM 52-71-00 FIG 103 PAGE BLOCK 1 PSEU BITE WAS PERFORMED FIM 32-09-03 FIG 103. 2L72 4F RTA2NM 20051202001012005120200101NM 2005 12 2 2005UALA01317 120051121A3350 LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29569UA 26677 EMERGENCY FLOOR PROX LIGHTS INOPERATIVE FROM ROWS 31 THROUGH ROW 34. REPLACED POWER SUPPLY M10817. 2L72 4F4 FRTA2NM E17NE 20051202001252005120200125EU 2005 12 2 05FDEA03989 120051128A5330 REPAIR AIRBUS310 A310203 3930313EU GE CF6 CF680 30025NE FUSELAGE PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 PREVIOUS REPAIR INSTALLED ON FUSELAGE RT SIDE AFT OF STATIC PORT EXT DOUBLER AT FR 34 BETWEEN STR 39 RT AND 40 RT NEEDS EVALUATION FOR MAJOR/MINOR CLASSIFACATION AND REPAIR DATA REF N00717. REPAIR FOUND TO BE IAW EA 6-5310-7952, MINOR IAW EA 6-5310-7952. 2L72 4F4 FRTA35EU E13NE 20051202001292005120200129EU 2005 12 2 05FDEA03993 120051128A5330 SKIN AIRBUS310 A310222 3930315EU PWA JT9 JT9D7R4E1 52054NE ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25450FE 162 2 DENTS AT FR 24 JUST BELOW RT STRINGERS 15 AND 16. CUT OUT DAMAGED SECTION IAW SRM 53-27-00. PERFORMED HFEC IAW NTM 51-10-08. INSTALLED INTERNAL DOUBLER AND FILLER IAW SRM 53-10-12 FIG 229 AND 53-10-14 FIG 201. 2L72 4F4 FRTA35EU E3NE 20051205000152005120500015NM 2005 12 5 DHL2005749006 120051031A5330 SKIN BOEING727 7272J0 138407ENM BS 1045 DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01749DH 22013 FOUND DENT RT SIDE FUSELAGE SKIN STA 1045 ABOVE STR 20R (MARKED). DAMAGED AREA OUT OF LIMITS IAW 727 SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA DIM .750 FABRICATED DOUBLER 2024T3 .090 PO NR 9002435 DIM 5.250" DIA AND FILLER 2024T3 .080 PO NR 9002727 DIM .750" DIA IAW B727 SRM 53-30-3 FIG 13 REV 98. TREATED AND PRIMED REPAIR PARTS IAW B727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B727 SRM 53-30-3 FIG 13. THIS REPAIR IS CATEGORY "A". 2L73 4F RTA3WE 20051205000212005120500021SO 2005 12 5 LR7A05132 120051017A53303752932L DOUBLER LKHEED382 382G 526414USO FS 847 DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER HC5315, FOUND ELEPHANT EAR DAMAGE, FS847, LBL64 WL185. REPLACED ELEPHANT EAR DOUBLER PER SRM 51-70, NR 0224. 2H74 4T A1SO 20051205000372005120500037SO 2005 12 5 LR7A05148 120051017A5311 FRAME LKHEED382 382G 526414USO FS 626 MISDRILLED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER HC5313, FOUND FUSELAGE FRAME (LS5408-2) MISDRILLED LINER HOLE LEFT SIDE, FS626, WL158. REPAIRED IAW DRAWING R05-025-08 PER LAC MEA382-53-05-070, NR 0413. 2H74 4T A1SO 20051205000382005120500038SO 2005 12 5 LR7A05149 120051017A5311 FRAME LKHEED382 382G 526414USO FS 647 MISDRILLED A LR7AK NONE W INADEQUATE Q C ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER HC5313, FOUND FUSELAGE FRAME (LS5408-2) MISDRILLED LINER HOLE LEFT SIDE, FS 647, WL158. REPAIRED IAW DRAWING R05-025-08 PER LAC MEA382-53-05-070, NR 0413. 2H74 4T A1SO 20051205000472005120500047SO 2005 12 5 LR7A05158 120051017A5311 FRAME LKHEED382 382G 526414USO FS 457 MISDRILLED A LR7AK NONE W INADEQUATE Q C ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER HC5313, FOUND FUSELAGE FRAME (LS4010-8) MISDRILLED LINER HOLE LEFT HAND SIDE, FS457, WL162. REPAIRED IAW DRAWING R05-025-07 PER LAC MEA382-53-05-071, NR 0414. 2H74 4T A1SO 20051205000492005120500049SO 2005 12 5 LR7A05160 120051017A5311 FRAME LKHEED382 382G 526414USO FS 742 MISDRILLED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER HC5313, FOUND FUSELAGE FRAME (LS4010-8) MISDRILLED LINER HOLE LEFT HAND SIDE, FS 742, WL151. REPAIRED IAW DRAWING R05-025-07 PER LAC MEA382-53-05-071, NR 0414. 2H74 4T A1SO 20051205000522005120500052SO 2005 12 5 LR7A05163 120051017A5312 BULKHEAD LKHEED382 382G 526414USO FS 617 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER 02SB-382-5785-2, FOUND PRESSURE BULKHEAD WEB CRACKED. FS617 LBL61, WL240. REPLACED WEB IAW SRM SMP 583 51-60/70 AND AC43.13-1B, NR 0429. 2H74 4T A1SO 20051205000602005120500060NM 2005 12 5 SWAA053818 120051130A534065C27314 STRINGER CLIP BOEING737 7373G7 1384595NM BS 360 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29683SW 24008 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 360, STR 10L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051205000662005120500066NM 2005 12 5 USAA051438 120051201A5320 ANGLE BOEING737 7374B7 1384702NM BS 295 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19780AU 24997 FOUND SERVICE DOOR SILL AREA CORRODED AT STA 295 RBL 53. REMOVED AND REPLACED ZEE ANGLE; IAW SRM 51-40-02; CORROSION LEVEL 1; TASK C53-107-01 DEFECT SIZE: 4.5" BY 2.125". 2L72 4F RTA16WE 20051205000712005120500071NM 2005 12 5 USAA051443 120051201A5320 SHEAR WEB BOEING737 7374B7 1384702NM BS 500-520 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19780AU 24997 FOUND CRACK MAIN CABIN FLOOR, STA 500-520 BL0. REMOVED AND REPLACED UPPER CHORD IAW SRM 51-40-02, DEFECT SIZE: .5, .75, .725, .5, 3.0 CRACKS AT FASTENER HOLES. 2L72 4F RTA16WE 20051205000802005120500080EA 2005 12 5 SWIA200515903 120051127A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07442SW 7609 CEILING LEVEL EMERGENCY FLOOD LIGHT INOP. RELAMPED CEILING EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051206000062005120600006EA 2005 12 6 COMA0560647 120051126A2752852D10019 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA LT WING FLAP FAULTY A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01735CA9022 7267 FLIGHT 5556 - EN ROUTE CVG-PWM, RECEIVED A FLAP FAIL MESSAGE AT ZERO FLAP POSITION. CREW DECLARED AN EMERGENCY AND FLIGHT LANDED SAFELY AT PWM. REPLACED THE LEFT WING INBOARD FLAP INBOARD ACTUATOR. 2L72 4F RTA21EA 20051206000082005120600008EA 2005 12 6 COMA0560656 120051130A3245 SWITCH CNDAIRCL600 CL6002B19 1900309EA PARKING BRAKE OUT OF ADJUST A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01918CA 7018 FLIGHT 5672 - PARKING BRAKE CONFIG WARNING. ADJUSTED THE PARKING BRAKE MICROSWITCH. 2L72 4F RTA21EA 20051206000092005120600009NM 2005 12 6 05FDEA04068 120051202A5330 SKIN DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 MAIN DECK COMPARTMENT R3 DOOR CUTOUT BOTTOM FOUND CORRODED. REMOVED AS PER SRM 51-21-01 VOLUME II. ORIGINAL THICKNESS = 0.270", MATERIAL REMOVED = 0.057", MATERIAL REMAINING = 0.213" AND FOUND WITHIN LIMIT AS PER SRM 53-00-01 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051206000102005120600010NM 2005 12 6 05FDEA04069 120051202A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 DURING HFEC INSPECTION, FOUND CRACK ON RIGHT WING STRINGER 43. REPAIRED AS PER SRM 57-20-00 FIG. 10 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20051206000132005120600013NM 2005 12 6 05FDEA04072 120051202A5230 SKIN BOEING BOEING727 727227 1384078NM ZONE 100 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 824 21489 REWORK OF FEDEX SNRM N00215 DUE TO WRONG MATERIAL USED. "FORWARD LOWER CARGO DOOR EXTERIOR SKIN IS DENTED". REMOVED DAMAGE AND FABRICATED REPAIR DOUBLER IAW SRM 52-00-3 FIGURE 3. ALODINED AND PRIMED REPAIR DOUBLER IAW B727 SRM 51-10-2. INSTALLED REPAIR DOUBLER IAW B727 SRM 51-30-2. REMOVED AND REINSTALLED LIGHT FIXTURE IAW B727 SRM 51-30-2. THIS IS A MAJOR REPAIR SIGNED BY TIMCO MECH NR 110290 AND QC401. REFERENCE FEDEX SNRM N01147 2L73 4F A3WE 20051206000142005120600014NM 2005 12 6 05FDEA04074 120051202A5322 SHEAR TIE BOEING727 727233 138408ANM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25220FE 20934 AFT PIT SHEAR TIE CORRODED AT STA 955.0E STRINGER 28R TO 29R. REMOVED AND INSTALLED DOUBLER, SHEAR TIE AND RAILS 1AW B727 SRM 51-10-2, 51-30-02, 51-10-6 AND 53-10-4. MINOR REPAIR SIGNED BY TIMCO MECH.33 NR 7921 QC 362. 2L73 4F RTA3WE 20051206000452005120600045EA 2005 12 6 COMA0560659 120051130A2750860D10018ABCD CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER O OTHER NRNOT REPORTED 1 SO01455CA1621 7592 FLIGHT 5409 - FLAPS HALFSPEED WARNING. REPLACED THE FECU. 2L72 4F RTA21EA 20051206000502005120600050WP 2005 12 6 05FDEA04080 120051202A5730 REPAIR DOUG DC10 DC1030 3023501WP LT WING UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 LEFT WING UPPER SURFACE FOUND A DOUBLER 30.50" BY 12.50" ON SKIN AT STA XORS 130. PERFORMED A GVI OF REPAIR IAW SRM 57-10-00 FIG 44 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-500, RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VOL 2 PAR 33. 2L73 4F A22WE 20051206000512005120600051WP 2005 12 6 05FDEA04081 120051202A5330 REPAIR DOUG DC10 DC1030 3023501WP FUSLEAGE UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 PERFORMED INSPECTION IAW EO NR 8-5100-7-5001-1P FOUND DOUBLER LENGTH 14" WIDTH 10" RT EXT FUSELAGE AT STA 565 TO STA 575 FROM LONG 14 TO LONG 11. PERFORMED A GVI OF REPAIR IAW SRM 53-20-00 FIG 6 SHT 3,4 REV 93 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001, RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VOL 2 PAR 33. 2L73 4F A22WE 20051206000522005120600052EA 2005 12 6 COMA0560651 120051127A3080 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA ANTI-ICE SYSTEM ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01918CA 7018 FLIGHT 5058 - EN ROUTE CMI-CVG, RECEIVED AN ANTI-ICE DUCT WARNING MESSAGE, FLIGHT DIVERTED TO EVV. PERFORMED SYSTEM CHECK OF THE WING ANTI-ICE SYSTEM, CND. 2L72 4F RTA21EA 20051206000532005120600053WP 2005 12 6 ABXA050298 120051024A53305758878 FINGER DOUBLER DOUG DC8 DC863F 302198FWP STA. 1480-1500 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 AFT LOWER CARGO HAD CORRODED FINGER DOUBLER ON INTERIOR SKIN LOCATED AT STA 1480, LEFT BUTT LINE 32, STRINGER 31 LEFT. REPAIRED FINGER DOUBLERS AT STA 1480 AND 1500, LONGERON 31 LEFT IAW REA D853-52524. 2L74 4F 4A25 20051206000562005120600056EA 2005 12 6 COMA0560646 120051126A2752853D10019 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA LEFT WING FLAP FAULTY A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01735CA9022 7267 FLIGHT 5556 - EN ROUTE CVG-PWM RECEIVED A FLAP FAIL MESSAGE AT ZERO FLAP POSITION. CREW DECLARED AN EMERGENCY AND FLIGHT LANDED SAFELY AT PWM. REPLACED THE LEFT WING OUTBOARD FLAP INBOARD ACTUATOR. 2L72 4F RTA21EA 20051206000592005120600059EU 2005 12 6 AWXA200501457 120051126A493038828354 FUEL DIVIDER AIRBUS320 A320232 3930326EU APU FAILED A AWXAO OTHER BA SMOKE/FUMES/ODORS/SPARKS FLAME/FIRE TXTAXI/GRND HDL 1 WP28659AW2201922019 1166 LAS - SMOKE - ON GROUND CATERER REPORTED EXCESSIVE SMOKE COMING FROM APU AND A GATES AGENT REPORTED FLAMES COMING FROM APU. THE APU WAS SHUT DOWN, NO ECAM MESSAGE. APU WAS DEFERRED. MAINTENANCE REMOVED AND REPLACED THE FUEL DIVERTER IAW AIRBUS 320 AMM 49-32-12. OPERATIONAL CHECKS WERE GOOD. VENDOR CONFIRMED FAILURE. FOUND CHECK VALVE PISTON GROOVED. REPAIRED AND RECERTIFIED IAW CMM 49-32-07 REV.01. 2L72 4F RTA28NM 20051206000602005120600060 2005 12 6 AWXA200501458 420051128A2215 ACTUATOR AIRBUS320 A320232 3930326EU RUDDER TRIM MALFUNCTIONED A AWXAO OTHER F FLT CONT AFFECTED CRCRUISE 1 WP28648AW 770 PHX - FLIGHT CONTROL - FLT 266 - DURING CRUISE, CREW REPORTED THAT THE AIRPLANE FLEW AT 4 DEGREE LEFT BANK WITH THE FLIGHT CONTROL PAGE SHOWING LEFT AILERON UP, SLIGHT AMOUNT OF RIGHT RUDDER, AND RUDDER TRIM INDICATION SHOWING 0.0. CREW DISENGAGED AUTOPILOT, STRAIGHTENED AIRCRAFT THEN RE-ENGAGED AUTOPILOT WITH NO HELP. MAINTENANCE ADJUSTED THE LEFT (BLUE) AILERON SERVO AND ADJUSTED THE RUDDER TRIM ACTUATOR IAW AIRBUS AMM 27-22-51 AND AMERICA WEST AIRLINES TASK CARD F3M27303. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA28NM 20051206000622005120600062NM 2005 12 6 AWXA200501475 120051115A5754D5755103920000 PIN AIRBUSA319 A319132 3930340NM ZONE 600 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28660AW 1234 SAL - DURING BC4 CHECK DISCOVERED CORROSION ON THE HINGE PIN FOR THE OUTBOARD SIDE OF THE NR 4 SPOILER. MAINTENANCE REMOVED AND REPLACED THE HINGE PIN, ON THE NR 4 SPOILER IAW AIRBUS 320 AMM 27-64-44-04. 2L72 4F RTA28NM 20051206000632005120600063NM 2005 12 6 AWXA200501476 120051113A5320D53471124200 PLATE AIRBUSA319 A319132 3930340NM BS 69-70 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28660AW 1234 SAL - DURING BC4 CHECK DISCOVERED CORROSION ON SHEAR PLATE LOCATED BETWEEN FS 69 AND FS 70, Y1162. NO ALLOWABLE DAMAGE LIMITS WERE FOUND. MAINTENANCE REMOVED AND REPLACED THE SHEAR PLATE BETWEEN FS 69 AN FS 70, Y1162 IAW BOEING 737-300 SRM 51-72-11. 2L72 4F RTA28NM 20051206000652005120600065NM 2005 12 6 SWAA053819 120051130A532269353656 SHEAR TIE BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29671SW 23785 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 360, BETWEEN STR 14L TO STR 15L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051206000662005120600066EA 2005 12 6 COMA0560641 120051124A275011045D100501 COUPLING CNDAIRCL600 CL6002B19 1900309EA TE FLAPS UNRELIABLE A COMAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 SO01735CA 7267 FLIGHT 5713 - FLAPS FAIL CAUTION. REPLACED THE NR 5 FLEX SHAFT. 2L72 4F RTA21EA 20051206000672005120600067NM 2005 12 6 DHL2005749007 120051031A5330 SKIN BOEING727 7272J0 138407ENM BS 1095 DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01749DH 22013 FOUND DENT RT SIDE FUSELAGE SKIN STA 1095 ABOVE STR 19R. DENT TO BE OUT OF LIMITS IAW B727 SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA 2" BY 1". FABRICATED REPAIR DOUBLER OUT OF 2024T3 0.063 11 1/4" BY 7 1/2" PO NR 53125 IAW B727 SRM 53-30-2 FIG 2 AND SRM 53-30-3 FIG 3. TREATED AND PRIMED PART AND WORK AREA IAW B727 SRM 51-10-2. INSTALLED REPAIR DOUBLER AT BS 1095, STR 19R IAW B727 SRM 53-30-3 FIG 3. THIS REPAIR IS CATEGORY "A". 2L73 4F RTA3WE 20051206000682005120600068NM 2005 12 6 DHL2005749008 120051031A5330 SKIN BOEING727 7272J0 138407ENM BS 1263 DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01749DH 22013 FOUND DENT RT SIDE FUSELAGE SKIN STA 1263 ABOVE STR 19 R (MARKED). CUT OUT DAMAGED AREA DIM 5" BY 3 1/2 AND FABBED REPAIR DOUBLER FROM MATERIAL USE 2024T3 063 PO NR 9002435 DIM 12 1/2" BY 7 1/2" AND FILLER MAT USE 2024T3 .050 PO NR 53081 DIM 12 1/2" BY 6" IAW B727 SRM 53-30-3 FIG NR 14 PARTS TREATED AND PRIMED IAW B727 SRM 51-10-, PARTS INSTALLED IAW B727 SRM 53-30-3 FIG 14. THIS REPAIR IS A CATEGORY "B". 2L73 4F RTA3WE 20051206000702005120600070EA 2005 12 6 COMA0560642 120051125A5210 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR LACK OF LUBE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01587SW 7062 FLIGHT 5637 - CABIN DOOR LATCH CAUTION. CLEANED AND LUBRICATED DOOR INNER HANDLE TENSION ROLLER. 2L72 4F RTA21EA 20051206000712005120600071EA 2005 12 6 COMA0560636 120051123A2750 FLEX COUPLING CNDAIRCL600 CL6002B19 1900309EA TE FLAPS LACK OF LUBE A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01969CA 7141 FLIGHT 5888 - FLAPS FAIL CAUTION. CLEANED AND LUBRICATED THE FLAP FLEX DRIVE SHAFTS. 2L72 4F RTA21EA 20051206000732005120600073NM 2005 12 6 USAA051445 120051201A5310 STRINGER SPLICE BOEING737 7374B7 1384702NM BS 904-913 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19780AU 24997 FOUND CRACK, STR SPLICE BET STA 904-913, S4L. REMOVED 7, REPLACED FAB STRINGER SPLICE PER SRM 51-40-02, DEFECT SIZE: .25". 2L72 4F RTA16WE 20051206000752005120600075NM 2005 12 6 USAA051446 120051201A532065C8735115 ANGLE BOEING737 7374B7 1384702NM BS 957-986 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19780AU 24997 FOUND CABIN FLOOR, DOOR SILL ANGLE SUPPORT STA 957-986, LBL 55, CORRODED. REMOVED AND REPLACED NEW DOOR SILL CHORD PER SRM 51-40-02; CORROSION TASK C53-107-01, DEFECT SIZE: 2"L BY 3"W BY .03"D. 2L72 4F RTA16WE 20051206000762005120600076NM 2005 12 6 USAA051451 120051201A551065C2584151 REPAIR BOEING737 737301 1384611NM RUDDER UNBONDED A USAAK NONE O OTHER ININSP/MAINT 1 EA19591US 23936 FOUND RUDDER COMPOSITE REPAIR APROX 7.5" DIA, 24" FWD OF T/E AND 41" UP FROM BOTTOM L/E. COMPOSITE REPAIR IAW SRM 55-40-01, DEFECT SIZE: APPROX 7.5" DIA LOCATED 24" FWD OF T/E AND 41" UP FROM BOTTOM L/E. (RT SIDE) 2L72 4F RTA16WE 20051206000792005120600079EA 2005 12 6 SWIA200515907 120051129A2752 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 NM07923SW 7664 ON APPROACH TO SLC SELECTING FLAPS 8, FLAPS FAIL CAUTION MSG ILLUMINATED. REPLACED ALL RT AND LT FLAP ACTUATORS PER CRJ MM 27-53-00. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051206000802005120600080EA 2005 12 6 SWIA200515908 120051126A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07919SW 7657 EMERGENCY LIGHT IN CEILING AT ROW 10 IS INOPERATIVE. REPLACED EMERGENCY LIGHT (CEILING) AT ROW 10. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051206000812005120600081EA 2005 12 6 SWIA200515909 120051125A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA ICED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION LDLANDING 1 NM07453SW 7743 AFTER LANDING, RECEIVED FLAPS FAIL MESSAGE WHILE RETRACTING FLAPS. FOUND ICE BUILD UP AT LEFT AND RIGHT INBOARD FLAP LEADING EDGES. REMOVED ICE. PERFORMED 15 EXTENSION/RETRACTIONS. NO FAULTS NOTED. OPERATIONAL CHECK GOOD IAW 27-54-00. 2L72 4F RTA21EA 20051206000832005120600083EA 2005 12 6 SWIA200515911 120051118A3350 LIGHT CNDAIRCL600 CL6002C10 1390015EA CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07732SK 10194 SERVICE DOOR EMERGENCY FLOOD LIGHT INOPERATIVE. REPLACED SERVICE DOOR EMERGENCY LIGHT AS REQ PER AMM 33-51-11. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051206000842005120600084SO 2005 12 6 SWIA200515912 120051120A3350 LAMP EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07291SW 120318 LWR EXTERIOR OVERWING EMERGENCY LIGHT INOP ON RT SIDE. RELAMPED EMERGENCY LIGHT AS REQUIRED. 2L72 4T RTA31SO 20051206000852005120600085EA 2005 12 6 SWIA200515913 120051127A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07952SW 7805 FLAPS FAIL CAUTION MESSAGE APPEARED WHEN FLAPS SELECTED TO 45 DEGREES. REPLACED FECU IAW CRJ MM 27-51-05 AND REPLACED LT FLAP OUTBOARD ACTUATOR IAW CRJ MM 27-53-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051206000862005120600086EA 2005 12 6 SWIA200515914 120051127A274170608 TRIM SYSTEM CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07907SW1155211552 7511 STAB CHANNEL 1 KEEPS KICKING OFF. REPLACED HSTCU IAW AMM 27-41-01 AND REPLACED FO'S PITCH DISCONNECT SWITCH IAW AMM 27-41-30. OPERATIONAL CHECKED GOOD. 2L72 4F RTA21EA 20051206000872005120600087EA 2005 12 6 SWIA200515915 120051127A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLT SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07862AS 7476 "R SPOILERON" CAUTION MESSAGE. REPLACED RT IB SPOILERON PCU IAW CRJ MM 27-62-01. OPERATIONAL CHECK OK. 2L72 4F RTA21EA 20051206000882005120600088EA 2005 12 6 SWIA200515916 120051126A2752 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07408SW 7055 "FLAP FAIL" CAUTION MESSAGE WHEN MOVING FLAP SELECTOR FROM 0 TO 8. FLAPS FAILED AT 0. REPLACED ALL FLAP ACTUATORS ON LT AND RT WINGS IAW CRJ MM 27-53-01, 27-53-03. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051206000912005120600091SO 2005 12 6 SWIA200515919 120051127A273152991 ACTUATOR EMB 120 EMB120ER 3260203SO ELEVATOR TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07579SW7242 7242 120347 ELEVATOR TRIM WHEEL IS EXTERNALLY DIFFICULT TO MOVE. REPLACED RT ELEVATOR TRIM TAB ACTUATOR IAW EMB 120 MM 27-32-02. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20051206000922005120600092SO 2005 12 6 SWIA200515920 120051110A3350 BATTERY PACK EMB 120 EMB120ER 3260203SO EMEGENCY LIGHT DISCHARGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07220SW 120288 EMERGENCY LIGHTS WILL NOT TEST. REPLACED 3 ELBP'S. OPERATIONAL CHECK GOOD, FWD SN 059 OFF; MID SN 1161 OFF; AFT SN 1035 OFF. 2L72 4T RTA31SO 20051206000952005120600095EA 2005 12 6 SWIA200515923 120051129A3350 LIGHT CNDAIRCL600 CL6002C10 1390015EA SERVICE DOOR BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07727SK 10191 SERVICE DOOR ILLUMINATION LIGHT INOP. REPLACED LIGHTS ON SERVICE DOOR EMERGENCY EXIT LIGHT IAW MM 33-51-15. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051206000962005120600096NM 2005 12 6 05FDEA04033 120051130A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 MAIN DECK, CORROSION FOUND SEAT TRACK UPPER FLANGE BETWEEN STA 899 TO 919 AT X = 8.5. REPAIR CARRIED OUT AS PER SRM 53-70-00. 2L73 4F RTA22WE 20051206000972005120600097NM 2005 12 6 05FDEA04034 120051130A5210 SKIN DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 FOUND CABIN, R4 DOOR EXTERIOR SKIN LOWER EDGE FOUND WITH DENT. CARRIED OUT REPAIR AS PER SRM 52-10-00. 2L73 4F RTA22WE 20051206000992005120600099WP 2005 12 6 05FDEA04036 120051130A5310 REPAIR DOUG DC10 DC1030 3023501WP BS 839 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 FOUND INTERNAL DOUBLER LENGTH 4.5" WIDTH 8" AT STA 839 LONG 35 RT FUSELAGE. PERFORMED INSPECTION ON REPAIR IAW SRM 53-20-00 FIG 13 SHT 4 VOL 1 AND EA NR 8-5330-93234 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001-P1. RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VOL 2 PAR 33 AND 24. 2L73 4F A22WE 20051206001002005120600100WP 2005 12 6 05FDEA04037 120051130A5310 REPAIR DOUG DC10 DC1030 3023501WP FUSELAGE UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 FOUND DOUBLER DIAMETER 3.5 INCH RT INT FUSELAGE AT STA 809 LONG 50. PERFORMED INSPECTION ON REPAIR IAW SRM 53-20-00 FIG 13 SHT 4 VOL 1 AND EA NR 8-5330-93234. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P1. 2L73 4F A22WE 20051206001022005120600102WP 2005 12 6 05FDEA04039 120051130A5320 REPAIR DOUG DC10 DC1030 3023501WP BS 809 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 FOUND DOUBLER DIAMETER 3.5 INCH LT SIDE INT FUSELAGE AT STA 809 LONG 50. PERFORMED INSPECTION ON REPAIR IAW SRM 53-20-00 FIG 13 SHT 4 VOL 1 AND EA NR 8-5330-93234 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P1. 2L73 4F A22WE 20051206001032005120600103WP 2005 12 6 05FDEA04040 120051130A5320 REPAIR DOUG DC10 DC1030 3023501WP FUSELAGE UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 PERFORMED INSPECTION IAW EO NR 8-5100-7-5001 P1, FOUND DOUBLER DIAMETER 3.5" LT SIDE INT FUSELAGE AFT CARGO COMPT STA 1876 LONG 31 AND LONG 32. PERFORMED INSPECTION ON REPAIR IAW SRM 53-20-00 FIG 13 SHT 4 VOL 1 AND EA NR 8-5330-93234 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P1. THIS IS -NOT- AN SDR. 2L73 4F A22WE 20051206001052005120600105 2005 12 6 QXEA200501566 420051125A3420 WARNING LIGHT DHAV DHC8 DHC8202 2809007NM RMI FALSE ACTIVATIONA QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09369PH 513 PDX FLIGHT NR 2030, RED OFF FLAG SHOWING FIRST OFFICERS RMI. MAINTENANCE PERFORMED OPERATIONAL TEST OF ADF SYSTEM ON FIRST OFFICERS RMI. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051206001082005120600108EU 2005 12 6 05FDEA04012 120051129A5330 SKIN AIRBUS310 A310222 3930315EU ZONE 200 SCRATCHED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25450FE 162 FUSELAGE EXTERIOR SKIN AT FS 16 RT STRINGERS 7-8 HAS SCRATCHES APPROX 1.8" LONG. REMOVED DAMAGED SECTION OF SKIN IAW A310-200 SRM 53-12-12 FIG 202. PERFORMED HFEC IAW NTM 51-10-08. NO CRACKS NOTED. INSTALLED FILLER AND DOUBLER IAW A310-200 SRM 53-12-12 FIG. 202. WORK DOCUMENTED ON NRC N00056. 2L72 4F RTA35EU 20051206001092005120600109EU 2005 12 6 05FDEA04013 120051129A7830 STRUCTURE AIRBUS310 A310222 3930315EU THRUST REVERSER DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25450FE 162 NR 2 ENGINE IB TR AT 9:00 POS HAS COMPOSITE DAMAGE APPROX 3.8" LONG. INSTALLED EXTERNAL METAL DOUBLER IAW EA 6-5430-94492. 2L72 4F RTA35EU 20051206001102005120600110NM 2005 12 6 05FDEA04014 120051129A5315 FLOORBEAM BOEING727 727227 1384078NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 MAIN DECK FLOORBEAM CORRODED AT STA BS 720D FROM LBL27 TO LBL44. DAMAGE FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-10-1 FIGURE 5. REMOVED STANCHION AND INTERCOSTAL BETWEEN STA BS 720D AND STA BS 720E TO FOM IAW B727 SRM 51-30-2. FABRICATED UPPER CHORD REPAIR IAW B727 SRM 53-10-8 FIGURE 4. ALODINED AND PRIMED REPAIR PARTS IAW B727 SRM 51-10-2. INSTALLED UPPER CHORD REPAIR IAW B727 SRM 53-10-8 FIGURE 4. REINSTALLED STANCHION AND INTERCOSTAL IAW B727 SRM 51-30-2. THIS IS A MAJOR REPAIR. REFERENCE FEDEX SNRM N00780, SIGNED BY TIMCO MECH NR 110174 AND QC261. 2L73 4F A3WE 20051206001142005120600114NM 2005 12 6 05FDEA04019 120051129A5315 FLOORBEAM BOEING727 727227 1384078NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 CABIN FLOORBEAM UPPER TEE CAP CORRODED AT STA BS 380 BETWEEN LBL24 AND LBL36. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW P-FSRM (ER 01-049) 53-10-1 FIGURE 4A. REMOVED DAMAGED AREA AND OBTAINED MATERIAL ID FOR UPPER CHORD AND REPAIR PARTS IAW B727 SRM 53-10-8 FIGURE 9. FABRICATED REPAIR PARTS IAW B727 SRM 53-10-8 FIGURE 9. ALODINED AND PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED UPPER CHORD AND REPAIR PARTS IAW B727 SRM 51-30-2 FIGURE 11. THIS IS A MAJOR REPAIR. REFERENCE FEDEX SNRM N00624 SIGNED BY TIMCO MECH NR 98629 AND QC261 2L73 4F A3WE 20051206001152005120600115NM 2005 12 6 05FDEA04020 120051129A5315 FLOORBEAM BOEING727 727227 1384078NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 FOUND CABIN FLOORBEAM UPPER TEE CAP CORRODED AT STA BS400 BETWEEN BL 0 AND LBL 12. DAMAGE FOUND TO BE BEYOND LIMITS IAW B727 SRM 53-10-1 FIGURE 5. REMOVED DAMAGED UPPER CHORD IAW B727 SRM 53-10-8 FIGURE 3. FABRICATED REPAIR PARTS IAW B727 SRM 53-10-8 FIGURE 3. ALODINED AND PRIMED REPAIR PARTS IAW B727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B727 SRM 51-30-2. THIS IS A MAJOR REPAIR SIGNED BY TIMCO MECH NR 3476 AND QC261 REFERENCE FEDEX SNRM N00604. 2L73 4F A3WE 20051206001162005120600116NM 2005 12 6 05FDEA04021 120051129A5315 FLOORBEAM BOEING727 727233 138408ANM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25220FE 20934 FOUND MAIN CABIN FLOORBEAM T-CAP CORROSION BS 560 LBL 3 TO LBL 24. COMPLIED WITH FLOORBEAM UPPER CHORD REPAIR AT STA 560 LBL 3 TO LBL 24, IAW B727 SRM 53-10-8 FIG 3, SIGNED BY TIMCO MECH NR 5154 AND QC 321. 2L73 4F RTA3WE 20051206001172005120600117NM 2005 12 6 05FDEA04022 120051129A5753 FLAP TRACK BOEING727 727233 138408ANM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25220FE 20934 LEFT WING OUTBOARD FLAP OUTBOARD TRACK, FORWARD MOUNT HOLE "D" HAS PITTING IN INNER BORE. REMOVED ALL PITTING FROM BORE "D ", FABRICATED AND INSTALL REPAIR BUSHING AND FINAL REAM ID, IAW BOEING OHM 57-40-01 SIGNED BY TIMCO MECH NR 4951 AND QC 280, CARD N00841. 2L73 4F RTA3WE 20051206001182005120600118NM 2005 12 6 05FDEA04023 120051129A5753 FLAP TRACK BOEING727 727200 138407ENM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25220FE 20934 RIGHT WING INB FLAP OUTB TRACK FORWARD MOUNT HOLE "D" HAS PITTING IN INNER BORE. REMOVED PITTING , FABRICATED AND INSTALLED REPAIR BUSHING AND FINAL REAM ID IAW BAC OHM57-40-01. 2L73 4F RTA3WE 20051206001202005120600120NM 2005 12 6 05FDEA04025 120051129A5240 REPAIR DOUG MD11 MD11 3023602NM R4 DOOR UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 CABIN, R4 DOOR EXTERIOR SKIN LOWER EDGE FOUND WITH EXISTING REPAIR TAG NR ERA382372-14. EVALUATED AND FOUND NOT IAW SRM 52-10-00. REPAIR AREA TRIMMED OUT AND REPAIR CARRIED OUT AS PER SRM 52-10-00, FIGURE 10, VOLUME I. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051206001212005120600121NM 2005 12 6 05FDEA04026 120051129A5753 SUPPORT ANGLE DOUG MD11 MD11 3023602NM ZONE 600 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE CENTER SUPPORT ANGLE STRUCTURE FOUND CHAFED. REMOVED AS PER CMM 20-11-02 AND FOUND WITHIN DRAWING ARC2126 DESIGN LIMIT. ORIGINAL THICKNESS = 0.180", REMAINING THICKNESS = 0.175", MATERIAL REMOVED = 0.005". REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2L73 4F RTA22WE 20051206001232005120600123NM 2005 12 6 ASAA0510311 120050920A53206559664501 STRINGER SPLICE BOEING737 737290C 138448VNM FS 350-365 DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02740AS 22578 YXX - FOUND STRINGER SPLICE AT BS 365 TO 350 AT STRINGER 27 LEFT HAS ELONGATED HOLES. REPLACED STRINGER SPLICE IAW B737-200 SRM 51-30-5 FIGURE 3. (M) 2L72 4F A16WE 20051206001242005120600124NM 2005 12 6 ASAA0510312 120050920A5320655966423 STRINGER SPLICE BOEING737 737290C 138448VNM FS 350-365 DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02740AS 22578 YXX - FOUND STRINGER SPLICE AT BS 365-350 AT STRINGER 26 RT HAS ELONGATED HOLES. REPLACED STRINGER SPLICE IAW B737-200 SRM 51-30-5 FIGURE 3. (M) 2L72 4F A16WE 20051206001252005120600125NM 2005 12 6 ASAA0510313 120050920A532165549057 FLOORBOARD BOEING737 737290C 138448VNM FS 420 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02740AS 22578 YXX - IN FORWARD CARGO PIT CORROSION ON LOWER CHORD OF CABIN FLOOR BOARD AT BS 420 LBL 36-44 BETWEEN PREVIOUS REPAIR PARTS. THE LOWER CHORD OF CABIN FLOORBEAM AT BS 420 FROM LBL 36-44 WAS REPAIRED IAW EA 5310-02491. (M) 2L72 4F A16WE 20051206001272005120600127SO 2005 12 6 SIMA200531507 120051101A521014540853403 SKIN EMB 135 EMB135KL 3260302SO PAX DOOR DENTED A SIMAO OTHER O OTHER NRNOT REPORTED 1 SW21822AE 145581 FOUND PASSENGER DOOR SKIN HAS A DENT. REPAIRED DENT IAW EMB SRM 52-10-01 PATE 402 BY INSTALLING AN EXTERNAL DOUBLER. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20051206001282005120600128SO 2005 12 6 SIMA200531511 120051102A5311 DOUBLER EMB 135 EMB135KL 3260302SO FRAME CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21822AE 145581 FOUND DOUBLER AT FRAME 22 ON RIGHT HAT BEAM CORRODED. INSTALLED NEW DOUBLER IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20051206001312005120600131EA 2005 12 6 SIMA200530403 120051028A27008489001 SENSOR CNDAIRCL600 CL6002C10 1390015EA HORIZONTAL STAB INOPERATIVE A SIMAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 SW21514AE 10119 CREW RECEIVED STABILIZER FAULT STATUS MESSAGE IN CRUISE. REPLACED HORIZONTAL STABILIZER ACTUATOR POSITION SENSOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA21EA 20051206001322005120600132SO 2005 12 6 SIMA200531502 120051030A532014521700007 REPAIR EMB 135 EMB135KL 3260302SO FLOOR SUPPORT CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21822AE 145581 FOUND REPAIR DOUBLER AT FRAME 20 ON LEFT OMEGA BEAM CORRODED. REPLACED DOUBLER ON LEFT OMEGA BEAM IAW EMB SRM 53-00-10 FIG 201. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20051206001342005120600134SO 2005 12 6 SIMA200531504 120051101A534714000486013 SEAT TRACK EMB 135 EMB135KL 3260302SO CABIN CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21822AE 145581 FOUND LEFT SECOND FROM FORWARD INBOARD SEAT TRACK CORRODED. REPLACED SEAT TRACK IAW EMB 140 AMM 53-01-00. AIRCRAFT WAS RETURNED O SERVICE. (M) 2L72 4F RTT00011AT 20051206001352005120600135SO 2005 12 6 SIMA200531512 120051109A2432464CC0181 CONTACTOR EMB 135 EMB135KL 3260302SO BATTERY BROKEN A SIMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21847AE 145707 DFW - FLT 3831 - RETURN TO FIELD WITH EICAS MESSAGE `ELECTRICAL EMERGENCY ABNORMAL.` AIRCRAFT STAYED ALOFT TO BURN FUEL. LANDED WITHOUT INCIDENT AND UNDER WEIGHT. REPLACED BATTERY CONTACTOR K0015. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20051206001372005120600137SO 2005 12 6 SIMA200530406 120051122A531012304331001 FRAME EMB 145 EMB145LR 3260212SO COCKPIT WINDOW BIRD STRIKE A SIMAO OTHER O OTHER NRNOT REPORTED 1 SW21908AE 14500897 CREW REPORTED BIRD STRIKE ABOVE THE FIRST OFFICERS WINDOW. AIRCRAFT REPOSITIONED TO ABI FOR REPAIR. PERFORMED A 19.5 INCH CUT OUT OF FRAME 6 TO REMOVE FRAME DAMAGE RECONTOURED DENT ON SKIN AT FRAME 7. PREPARED A 19.5 INCH FRAME FILLER, A 8 INCH LOWER FRAME SPLICE AND AN 8.5 INCH UPPER FRAME. FABRICATED 3 SKIN REINFORCEMENT ANGLES AND 2.5 INCH STRAPS FOR FRAME 6 SPLICE. REPAIR ACCOMPLISHED IAW EMB REPAIR STATEMENT IC2005-145/5730A DATED 10/26/2005 AND IC 2005-145/6219 DATED 10/30/2005. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20051206001382005120600138SO 2005 12 6 SIMA200531105 120051102A3350 LIGHT EMB 135 EMB135LR 3260305SO CABIN INCORRECT A SIMAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SW21701MH 145162 EMERGENCY EXIT FLOOR LIGHT PROXIMITY STRIP IS WRONG COLOR. REPLACED EMERGENCY EXIT PROXIMITY LIGHT STRIP. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20051206001402005120600140EA 2005 12 6 ASOA05956 120051028A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 615 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27838AS 7276 DURING A C-CHECK IN MCN, THE FLOORBEAM AT FS 615, RBL 9, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM AT S 615, RBL 9, IAW CRJ 200 SRM 51-42-06, 51-42-20, AND 51-00. (M) 2L72 4F RTA21EA 20051206001422005120600142EA 2005 12 6 ASOA05939 120051031A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27928EV 8006 DURING A GROUND INSPECTION IN VPS, THE CEILING EMERGENCY LIGHT, AT ROW 10, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN CEILING EMERGENCY LIGHT, AT ROW 10. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051206001432005120600143NM 2005 12 6 ASAA0510310 120050920A5313655491057 STRINGER BOEING737 737290C 138448VNM FS 363-375 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02740AS 22578 YXX - FOUND CORROSION ON STRINGER AT BS 363-375 STRINGER 27 RIGHT. STRINGER 27 RT REPLACED FROM 363 TO 407 IAW B737-200 SRM 53-10-3. (M) 2L72 4F A16WE 20051206001442005120600144SO 2005 12 6 SIMA200531510 120051102A534713500439005 SEAT TRACK EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21822AE 145581 SAW - FOUND LEFT FORWARD OUTBOARD SEAT TRACK CORRODED. REPLACED SEAT TRACK IAW EMB 140 AMM 53-01-06. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20051206001452005120600145NM 2005 12 6 ASAA0510317 120050921A5320654576925 STRINGER SPLICE BOEING737 737290C 138448VNM FS 370-380 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02740AS 22578 YXX - FOUND CORROSION ON STRINGER SPLICE AT BS 370-380 STRINGER 27 RT. STRINGER SPLICE REPLACED PER B737-200 SRM 51-30-2. (M) 2L72 4F A16WE 20051206001462005120600146EA 2005 12 6 ASOA05955 120051105A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 379-969 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27709EV 10068 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT SIDEWALL SEAT TRACKS, AT FS 379 TO FS 969, WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE WILL REPAIR THE LEFT AND RIGHT SEAT TRACKS, AT FS 379 TO FS 969, IAW BOMBARDIER 2L72 4F RTA21EA 20051206001472005120600147EA 2005 12 6 ASOA05958 120051106A5240 LEVER CNDAIRCL600 CL6002C10 1390015EA SERVICE DOOR OUT OF ADJUST A ASOAK NONE O OTHER ININSP/MAINT 1 SO27708EV 10060 DURING A GROUND INSPECTION IN SLC, THE SERVICE DOOR WAS FOUND DIFFICULT TO OPEN AND CLOSE. MAINTENANCE LUBRICATED THE SERVICE DOOR, AND ADJUSTED A TURNBUCKLE AT THE LEVER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051206001492005120600149EA 2005 12 6 ASOA05940 120051031A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA PAX DOOR MALFUNCTIONED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27935EV 8037 DURING A GROUND INSPECTION IN OAK, THE PASSENGER DOOR WOULD NOT CLOSE. MAINTENANCE CYCLED THE PASSENGER DOOR. NO DEFECTS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051206001502005120600150EA 2005 12 6 ASOA05938 120051031A5210601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27852AS 7369 DURING A GROUND INSPECTION IN CVG, THE PASSENGER DOOR BOTTOM STEP WAS FOUND TO BE BROKEN. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051206001512005120600151EA 2005 12 6 ASOA05937 120051031A5610NP1393219 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT FAILED A ASOAO OTHER O OTHER CRCRUISE 1 SO27875AS 7559 FLT 4447 - DURING CRUISE FROM ATL-VPS, AT APPROXIMATELY 30,000 FEET, THERE WAS AN ILLUMINATING GLOW FROM THE ANTI-ICE VEIN, FOLLOWED BY A LOUD SHATTERING OF THE NR 2 WINDSHIELD. THE CREW COMPLIED WITH THE QRH AND DIVERTED INTO MGM, AFTER DECLARING AN EMERGENCY. THE AIRCRAFT LANDED SAFELY IN MGM. MAINTENANCE REMOVED AND REPLACED THE NR 2 WINDSHIELD IAW CRJ AMM 56-11-01. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051206001522005120600152EA 2005 12 6 ASOA05953 120051105A5210601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27932EV 8016 DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR BOTTOM STEP WAS FOUND TO BE CRACKED BEYOND LIMTIS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051206001532005120600153EA 2005 12 6 ASOA05952 120051105A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A ASOAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 SO27823AS 7196 DURING APPROACH FROM ATL-OMA, THE FLAPS WERE SELECTED TO 8 DEGREES. THE CREW RECEIVED A FLAPS FALL CAUTION MESSAGE, INDICATING FLAPS WERE AT 0. THE CREW COMPLIED WITH THE QRH, AND DECLARED AN EMERGENCY. THE EMERGENCY VEHICLES WERE DISPATCHED , WITH THE AIRCRAFT LANDING SAFELY IN OMA. MAINTENANCE RESET THE FLAPS AND PERFORMED OPERATIONAL CHECKS. NO DEFECTS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051206001572005120600157NM 2005 12 6 ASAA0510298 120050915A53136545765522 STRINGER BOEING737 737290C 138448VNM FS 434-446 DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02740AS 22578 YXX - FOUND TOOLING DAMAGE AT BS 440, STRINGER 7 RT. REPAIRED IAW B737-200 SRM 53-10-3 FIG 4. (M) 2L72 4F A16WE 20051206001582005120600158NM 2005 12 6 ASAA0510299 120050915A53136545767519 STRINGER BOEING737 737290C 138448VNM FS 510 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02740AS 22578 YXX - IN FORWARD PIT STRINGER 25 LEFT DENTED AT BS 51. REPLACED WITH FABRICATED REPAIR PART IAW B737-200 SRM 53-10-03. (M) 2L72 4F A16WE 20051206001592005120600159NM 2005 12 6 ASAA0510302 120050920A5310655496050 DOUBLER BOEING737 737290C 138448VNM FS 360 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02740AS 22578 YXX - FOUND DOUBLER DAMAGED AT BS 360 BETWEEN STRINGER 27R TO 28L PLUS 14 INCHES. REPLACED DOUBLER PER B737-200 SRM 57-40-3 FIGURE 1. (M) 2L72 4F A16WE 20051206001602005120600160NM 2005 12 6 ASAA0510308 120050920A531165549607 FAILSAFE BOEING737 737290C 138448VNM FOM CUT A ASAAK NONE O OTHER ININSP/MAINT 1 NM02740AS 22578 YXX - FOUND FAIL/SAFE AT BS 360 TO BE CUT FOR ACCESS AT STRINGER 26 RT. REPAIRED IAW B737-200 SRM 51-40-3 FIGURE 1. (M) 2L72 4F A16WE 20051206001642005120600164SO 2005 12 6 SIMA200531505 120051101A550014524980001 BUSHING EMB 135 EMB135KL 3260302SO HORIZONTAL STAB MIGRATED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21822AE 145581 FOUND HORIZONTAL STABILIZER NR 3 BUSHING HAS EVIDENCE OF MIGRATING. REMOVED AND REPLACED HORIZONTAL STABILIZER NR 3 BUSHING IAW EMB SRM 55-10-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20051208000012005120800001NM 2005 12 8 05FDEA03997 120051128A5330 REPAIR BOEING727 727100 1384036NM FUSELAGE IMPROPER A FDEAO OTHER O OTHER ININSP/MAINT 1 SO25188FE 19081 REPAIR AT BS 694, STR 19R REQUIRES ENGINEERING DISPOSITION IAW EO 7-5100-7- 5000 PT1. ACCOMPLISHED REPAIR AT BS 694 STR 19R PER FED EX E.A. 7-5330-91416. 2L73 4F RTA3WE 20051208000042005120800004EU 2005 12 8 05FDEA04041 120051130A3260 SHEAR PIN AIRBUS310 A310 EU MLG FAILED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25807FD 492 AFTER TAKEOFF FROM KMIA,WHEN THE MLG RETRACTED THE LT MLG DOOR SHOWED UNLOCKED ON FWD PANEL, OVERHEAD PNL,AND ECAM.WHILE GERAR HANDLE WAS IN THE UP POSITION THE AMBER DOOR LIGHT WAS ON AND THE RED GEAR UNLK LIGHT WAS ON.WHEN LDG GEAR HANDLE WAS MOVED TO NEUTRAL, THE MLG GREEN LIGHT ILLUMINATED. FOUND LT MLG SIDE BRACE ACTUATOR MOUNT PIN MISSING, GOUGE IN SIDE BRACE. BLENDED OUT DAMAGED AREA WITHIN LIMITS IAW E.A 6-3210-95470. INSTALLED ATTACH PIN, REPLACED SHEAR PIN, REINSTALLED GEAR DOWNLOCK IND. MECH. IAW A310 M/M32-61-14-4. R&R BRACE STRUT ACTUATOR. 2L72 4F RTA35EU 20051208000052005120800005NM 2005 12 8 05FDEA04052 120051201A5510 PANEL BOEING727 727200 138407ENM HORIZONTAL STAB MISINSTALLED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25466FE 21292 INCORRECT REFERENCE WAS USED TO DETERMINE IF HORZ STAB REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA - PREVIOUS REPAIR ON LEFT HORIZONTAL STABILIZER AT STAB STA 115, 3" WIDE X 3" LONG, 15" AFT OF STAB REAR SPAR. ** SD ** COMING REPLACED PREVIOUS REPAIR ON LEFT HORIZONTAL STABILIZER AT STAB STA 115, IAW EA#7- 5510-91418. THIS REPAIR IS DEEMED MAJOR. 2L73 4F RTA3WE 20051202000052005120200005EU 2005 12 2 USAA051427 120051130A5315D5311281520200 FLOORBEAM AIRBUSA321 A321211 3930370EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19164UW 1425 PAX FLOORBEAM AT Y765, FR 16, LT, REMOVED AND REPLACED FLOORBEAM; DEFECTIVE PART REPLACED WITH IDENTICAL PART IAW SRM 51-72-11; CORR. LEVEL 1, DEFECT SIZE: 1 SQ. IN. 2L72 4F RTA28NM 20051202000072005120200007EU 2005 12 2 USAA051425 120051130A5347D531141420200 DUMMY RAIL AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19112US 1134 BETWEEN C20 AND 24 RT -Y190, REPLACED RAIL IAW SRM 51-72-11; CORR. LEVEL 1; TASK JA-220-53500 DEFECT SIZE: 2 INCHES X 1.5 INCHES AND 2 INCHES X 1INCH. 2L72 4F4 FRTA28NM E38NE 20051202000082005120200008EU 2005 12 2 USAA051424 120051130A5320D5311281820401 FLOOR SUPPORT AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19112US 1134 LOCATION: AT CLIP NUT HOLES - FLOOR SUPPORT Y254, C-16, 18, 21 AND BETWEEN C21-23. DEFECTIVE PART REPLACED WITH IDENTICAL PART IAW SRM 53-11-14; CORR. LEVEL 1; TASK JA-220-53500 DEFECT SIZE: .5 INCH DIA AT 4 AREAS. 2L72 4F4 FRTA28NM E38NE 20051202000182005120200018EU 2005 12 2 YENA200582 120051123A212120092455102 COOLING FAN AIRBUS320 A320232 3930326EU IAE V2500 V2500A1 NE E/E BAY FAILED A YENAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15606JB3349 3349 2384 10 MIN INTO FLT, AFT AVIONICS COMPARTMENT, RACK POWER WARNING , LIGHT IN BUTTON AND HORN . TURNED POWER OFF, NO FURTHER WARNING. LEFT IN OFF POSITION FOR REST OF FLT. REMOVED AND REPLACED COOLING FAN ASSY IAW MM 23-39-00. LTV OPS CK GOOD IAW LTV MM 23-39-00. 2L72 4F4 FRTA28NM E311NE 20051202000352005120200035NM 2005 12 2 AWXA200501459 120051113A5347D5347209001000 SEAT TRACK AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28660AW 1234 DURING BC-4 CHECK DISCOVERED LEVEL 2 GALVANIC CORROSION ON SEAT RAIL BEAM AT FR66 AND Y1292. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-00-14. REMOVED AND INSTALLED SEAT RAIL BEAM IAW SRM 51-42-11 FROM FR64 TO FR66 AND Y1292. 2L72 4F RTA28NM 20051202000382005120200038EU 2005 12 2 SDR2005070 120051025A3210140071 TRANSDUCER AEROSPATR72 ATR72 EU PWA PW120 PW127 NE MLG MALFUNCTIONED A TRBAO OTHER M OVER TEMP LDLANDING 1 SO29426AT 426 AFTER LANDING, THE CONTROL TOWER ADVISED ABOUT SMOKE COMING OUT OF THE LT MAIN GEAR. EMERGENCY DECLARED. REPLACED NR 1 SPEED TRANSDUCER. (K) 2H72 4T4 TRT E20NE 20051202000482005120200048CE 2005 12 2 TIM2005F00008 120051003A29101145802271 LINE BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA HYDRAULIC SYS LEAKING E TIMAK NONE K FLUID LOSS ININSP/MAINT 1 NM07195GA UB65 NOSE GEAR WARNING LIGHT ILLUMINATED WHEN LANDING GEAR EXTENDED. GEAR DEPLOYED AFTER 15 TO 20 SECONDS. PROBLEM WAS A LEAK IN THE HYDRAULIC LINE. THE LINE DEVELOPED A PIN HOLE LEAK BECAUSE OF CORROSION FROM THE INSIDE OF THE LINE. (K) 2L72 4T4 TRTA24CE E4EA 20051202000582005120200058EA 2005 12 2 ASOA05950 120051104A5315 FLOORBEAM CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE BS 280 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27709EV 10068 DURING A C-CHECK, THE FORWARD FS 280 FLOOR ANGLE WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACE THE FORWARD FS 280 FLOOR ANGLE. (K) 2L72 4F4 FRTA21EA EOOO63EN 20051202000712005120200071NM 2005 12 2 ASAA0540492 120050919A5311654656627 FRAME BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU BS 995 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02793AS 28888 CORROSION ON FRAME AT BS 995, RBL 46, WL 209. REPAIRED FRAME AT BSTA 995, RBL 46, WL 209 IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051202000782005120200078WP 2005 12 2 ASMF200511010 120051124A30406171 CONTROLLER DOUG DC9 DC987 3022087WP ANTI FOG FAILED W ASMFD RETURN TO BLOCK BH SMOKE/FUMES/ODORS/SPARKS ELECT. POWER LOSS-50 PC TXTAXI/GRND HDL 1 SW23755RA9382 49727 AIRCRAFT RETURNED TO PLATFORM, SMOKE ODOR WAS DETECTED IN THE CABIN FROM THE SEATS 1 AND 2 GRID. THE FORWARD SIDEWALL OF ELECTRICAL / ELECTRONIC COMPARTMENT FROM STATIONS 110 TO 218 WAS OPENED DETECTING THE CAPTAIN FLOOR BURNED AND STRONG SMOKE ODOR IN 3 TEMPERATURE CONTROLLERS. THE WINDOWS AND WINDSHIELDS ANTI-FOG TEMPERATURE CONTROLLERS WERE REPLACED IAW MM 30-41-01 AND WIRING WAS CHECKED IAW WDM 20-50-01, TESTED CORRECT. 2L72 4F RTA6WE 20051202000802005120200080NE 2005 12 2 C1HA200594011 220051125A7261 CAP BOEING727 727290 138408WNM PWA JT8 JT8D17 52049NE ENGINE OIL LOOSE A C1HAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL15294AS 22146 DURING CLIMB-OUT DFW, NR 1 ENGINE OIL QUANTITY INDICATED CONSTANT DECREASE OIL. LANDED WITH 1.0 GALLONS OIL RETURNED DIRECT, UPON LANDING WITNESSED OIL LEAKING FROM COWLING. FOUND OIL CAP NOT ENGAGED. SERVICED ENGINE INSTALLED NEW OIL CAP REF 12-13-01. 2L73 4F4 F A3WE E2EA 20051202000812005120200081SO 2005 12 2 BSYA200500025 120051129A5230 DOOR PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA NOSE CARGO OPEN E BSYAC ABORTED TAKEOFF WJ INADEQUATE Q C WARNING INDICATION TOTAKEOFF 1 GL0735453 318052006 ON TAKEOFF NOSE BAGGAGE LIGHT CAME ON, PILOT ABORTED TAKEOFF SECURED DOOR AND CONTINUED ON WITH FLIGHT. 1L72 3O3 O A20SO E14EA 20051202000822005120200082NM 2005 12 2 HNAA0500100 120051127A6120 SWITCH DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE BETA SYSTEM LACK OF LUBE A HNAAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 EA07912HA 040 DURING CLIMBOUT AT ABOUT 200 TO 300 FEET NR 2 PROP CYCLED ABOUT 150 TO 200 RPM AND TQ CYCLED 85 TO 115 PERCENT FOR ABOUT 90 SECONDS. LUBED BETA BACK UP POWER LEVER SWITCHES, REINSTATED BETA LOCKOUT SWITCHES AND C/W BETA GROUND LOGIC WORK CARD. 2H72 4T4 TRTA13NM E20NE 20051202000912005120200091NE 2005 12 2 111105N523CS1 220051111A7200 ENGINE CESSNA560 560XL 2076702CE PWA 545 PW545A NE RIGHT ODOR E Z5FAEA ENGINE SHUTDOWN UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 NE03523CS 5605507 DD0012 AIRCRAFT DEPARTED AND DURING INITIAL CLIMB OUT CREW NOTICED A LOSS OF OIL PRESSURE AND A SLIGHT ODOR FROM RT ENGINE. THE ENGINE WAS SHUT DOWN AND AN EMERGENCY WAS DECLARED. AIRCRAFT WAS REROUTED AND LANDED WITH NO FURTHUR PROBLEMS. THE ENGINE IS BEING REMOVED AND SENT TO THEMFG CENTER FOR INVESTIGATION AND REPAIR. WILL ADVISE WHEN CAUSE IS KNOWN. 2L72 4F4 FRTA22CE E00059EN 20051202000992005120200099NM 2005 12 2 ASMF200511004 120051105A4920 APU BOEING737 737* NM GE CFM56 CFM56* 13802NE APU BAY FAILED W ASMFD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SW23851AM 29363 DURING ENGINES STARTING, THE PNEUMATIC AUXILIARY POWER UNIT FAILED. THE ENGINES WERE STARTED WITH EXTERNAL PNEUMATIC PLANT IAW MM 49-11-00, TESTED CORRECT. THE FIM PROCEDURE WAS PERFORMED IAW FIM 49-55 TASK 804, ALL CORRECT. 2L72 4F4 FRTA16WE E2GL 20051202001162005120200116EU 2005 12 2 05FDEA03981 120051128A5320 TRACK AIRBUS310 A310203 3930313EU FR 38.2 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 CENTER ROLLER TRACK AT FR 38.2 HAS EXFOLIATED CORROSION INSIDE TRAY AND ON AND AROUND FASTENER HOLES OB LEG FR 38.2 TO 38.1 REF N00463. REMOVED AND REPLACED ROLLER TRAY IAW SRM 51-40-21. 2L72 4F RTA35EU 20051202001172005120200117EU 2005 12 2 05FDEA03982 120051128A5320 ROLLER TRAY AIRBUS310 A310203 3930313EU GE CF6 CF680A3 30025NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 RT OB MOST ROLLER TRAY AT FR 38.2 HAS CORROSION ON IB LEG FASTENER HOLE REF N 00466. REMOVED AND REPLACED ROLLER TRAY IAW SRM 53-10-15. 2L72 4F4 FRTA35EU E13NE 20051202001272005120200127EU 2005 12 2 05FDEA03991 120051128A5311 FRAME AIRBUS310 A310222 3930315EU PWA JT9 JT9D7R4E1 52054NE ZONE 200, FR44 PUNCTURED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25450FE 162 FRAME 44 BETWEEN RT STRINGERS 6 AND 7 HAS PUNCTURED DAMAGE APPROX 1.00 INCH LENGTH WITH DEEP SCRATCHES. DRILLED 0.75 INCH HOLE TO REMOVE DAMAGE. DEBURRED HOLE. NDT FOR CRACKS. NO CRACKS NOTED. ALODINED AND PRIMED AREA. ALL WORK PERFORMED IAW EA 6-5310-93421 AND DOCUMENTED ON NRC N00109. 2L72 4F4 FRTA35EU E3NE 20051202001312005120200131NM 2005 12 2 05FDEA04000 120051128A5320 STRINGER CLIP BOEING727 727200 138407ENM PWA JT8 JT8D9 52048NE BS 950C DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 MECHANICAL DAMAGE TO STRINGER CLIP BS 950C STRINGER 5 RT. REPAIRED STRINGER CLIP PER SRM 53-10-1, 51-30-2. 2L73 4F4 FRTA3WE E2EA 20051202001392005120200139NM 2005 12 2 05FDEA04007 120051129A5315 FLOORBEAM BOEING727 727227 1384078NM PWA JT8 JT8D9 52048NE ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 CABIN FLOORBEAM, UPPER T-CAP CORRODED AT STA BS 440 BL 0 - RBL 24. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1 FIGURE 5. REMOVED DAMAGED T-CAP FROM RBL-8 TO LBL 8 STA BS 440 IAW SRM 53-10-8 FIGURE 3. REMOVED CORROSION FROM RBL 8 TO RBL 24 IAW SRM 51-10-6 AND FOUND WITHIN LIMITS IAW SRM 53-10-1 FIGURE 5. FABRICATED, LOCATED AND DRILLED THE UPPER CHORD SECTION, SUPPORT ANGLES AND REINFORCEMENT STRAPS IAW SRM 53-10-8 FIGURE 3. ALODINED AND PRIMED IAW SRM 51-10-2. PAINTED IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 51-30-2 AND 53-10-8 FIGURE 3. 2L73 4F4 F A3WE E2EA 20051202001412005120200141SO 2005 12 2 CHQA200500201 120051124A33501317 BULB EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL EMERGNECY LIGHT BURNED OUT A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11381SK 145619 RT OVERHEAD AFT EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED THE RT WING AFT EMERGENCY EXIT LIGHT BULB IAW 140 MM 33-50-09. OPS CHECK GOOD. 2L72 4F4 FRTT00011ATTE6CH 20051202001502005120200150NM 2005 12 2 DHL2005749016 120051102A5754 BRACKET BOEING727 7272J0 138407ENM NR 2 SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01749DH 22013 LT WING NR 2 SLAT ACT MOUNT BRACKET IB SIDE HAS INSIDE PLATE CRACKED. REMOVED FABBED NEW AND INSTALLED NR 2 SLAT ACT I/B MOUNT BRACKET MAT USED BAC 1503-10045 PO 9001801 DIM 9.15" BY 3.25" BY 1.25" IAW S/B 727-57-0130 REV 3 FIG 1. REMOVED ALUMINUM DOUBLERS FABBED NEW AND INSTALLED ON IB AND OB MOUNT BRACKETS MAT USED 301 1/2 HD 100 DIM 8.1" BY 2.95 " AND 7.9" 2.95" IAW S/B727-57-0130 REV 3 FIG 1 DATED APRIL 24 2003. 2L73 4F RTA3WE 20051202001522005120200152WP 2005 12 2 MWEA050128 120051201A5330 SKIN DOUG DC9 DC981 3022081WP STA 522-579 DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31807ME 48033 FOUND RIGHT FUSELAGE SKIN IS DAMAGED AT STATION 522-579, FROM LONGERON 19 RIGHT TO LONGERON 22 RIGHT. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20051202001542005120200154WP 2005 12 2 MWEA050130 120051201A53135920323195 LONGERON DOUG DC9 DC981 3022081WP STA 522-579 DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31807ME 48033 FOUND LONGERON 20 RIGHT IS DAMAGED FROM STATION 522-579. FABRICATED AND INSTALLED NEW LONGERON. 2L72 4F A6WE 20051202001562005120200156SO 2005 12 2 LR7A05116 120051017A5312 BULKHEAD LKHEED382 382G 526414USO FS 1023 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER HC5212, FOUND CARGO DOOR BULKHEAD WEB CRACKED LBL40. REPAIRED IAW SRM SMP 583 FIGURE 51-140-17, NR 0086. 2H74 4T A1SO 20051202001582005120200158SO 2005 12 2 LR7A05118 120051017A5312 STIFFENER LKHEED382 382G 526414USO FS1023 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER HC5212, FOUND CARGO DOOR AFT BULKHEAD WEB STIFFENERS CRACKED FS 1023, RBL10. REPLACED WEB STIFFENERS IAW SRM SMP 583 FIGURE 51-70 AND AC43, 13-1B PARA 4-57 NR 0106. 2H74 4T A1SO 20051202001612005120200161NM 2005 12 2 SWAA053809 120051127A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29418WN 29823 EEPLS STRIP LOOSE AT ROW 1. SECURED EEPLS PER MM. 2L72 4F RTA16WE 20051202001632005120200163NM 2005 12 2 SWAA053811 120051130A3350207377 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29476WN 32475 EEPLS TRACK LENS LOOSE AT FWD END. RESECURED LENS PER MM. 2L72 4F RTA16WE 20051202001652005120200165NM 2005 12 2 SWAA053813 120051129A531465C26493 PANEL BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29649SW 27719 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE KEEL BEAM PANEL CRACKED AT BS 670, STR 28R. REPAIRED KEEL BEAM PANEL PER SRM. 2L72 4F RTA16WE 20051202001672005120200167NM 2005 12 2 SWAA053815 120051130A53306545776 SKIN BOEING737 7373Q8 1384670NM BS 941 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 941, STR 21R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051202001692005120200169NM 2005 12 2 SWAA053817 120051130A534065C27314 STRINGER CLIP BOEING737 7373G7 1384595NM BS 360 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29683SW 24008 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051202001722005120200172NM 2005 12 2 QXEA200501599 120051129A30607749341 TIMER DHAV DHC8 DHC8202 2809007NM DEICE SYS INOPERATIVE A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09346PH 477 SEA FLIGHT NR 2281, PROP DE-ICE WILL NOT TEST ON TAXI WITH PROPS ABOVE 900. REPLACED 3061 K1 AND K5 RELAY, CLEANED AND INSPECTED NR 1 AND NR 2 PROP BRUSH BLOCK AND SLIP RINGS. REPLACED PROP DE-ICE TIME. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE 2H72 4T RTA13NM 20051202001742005120200174SO 2005 12 2 LR7A05126 120051017A5312 ANGLE LKHEED382 382G 526414USO FS 1023 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER HC5212, FOUND CARGO DOOR BULKHEAD WEB STIFFENERS CRACKED, FS 1023, RBL34. REPAIRED STIFFENER ANGLES PER SRM 51-140-19, NR 0107. 2H74 4T A1SO 20051202001762005120200176EU 2005 12 2 MALA050842 120051126A2697 CONNECTOR SAAB SF340 340B 7860101EU TAIL PIPE DIRTY A MALAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL15413XJ 340B413 TAIL PIPE HOT. ABORTED TAKEOFF. CLEANED CANNON PLUGS. 2L72 4T RTA52EU 20051202001782005120200178EU 2005 12 2 MALA050834 120051116A3241 VALVE BAC 146 AVRO146RJ85A1500097EU ANTI SKID SYS FAILED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15522XJ E2347 EN ROUTE ANTI-SKID INOP ILLUMINATED. AIR RETURN TO MSP, CHANGED VALVE. 2H74 4F RTA49EU 20051205000112005120500011EU 2005 12 5 MALA050532 120051110A2620 ODOR BAC 146 AVRO146RJ85A1500097EU CABIN DETECTED A MALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL15532XJ E2366 TAKEOFF WAS ENG NR 4 AIR ONLY. AFTER PERFORMING TAKEOFF CHECK NOTICED ODOR. PERFORMED SMOKE, FIRE, FUMES CHECKLIST. RETURNED TO MSP. SMOKE DISSIPATED AS CHECKLIST PROGRESSED. PERFORMED COMP WASH. 2H74 4F RTA49EU 20051205000122005120500012EU 2005 12 5 MALA050828 120051112A3241 VALVE BAC 146 AVRO146RJ85A1500097EU ANTI-SKID SYS INOPERATIVE A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15522XJ E2347 ANTI-SKID YELLOW SYSTEM NR 4 VALVE INOP. REPLACED VALVE. 2H74 4F RTA49EU 20051205000202005120500020SO 2005 12 5 LR7A05131 120051017A5330 SKIN LKHEED382 382G 526414USO FS 870 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER HC5211, FOUND RAMP REAR SILL UPPER CENTER SKIN PANEL CRACKED, FS 870. REPLACED SKIN PANEL IAW SRM SMP 583 FIGURE 51-70 AND AC43, 13-1B PARA 4-57, NR 0202. 2H74 4T A1SO 20051205000262005120500026SO 2005 12 5 LR7A05137 120051017A5315 FLOORBEAM LKHEED382 382G 526414USO FS 210 CORRODED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER HC5312, FOUND CORROSION DAMAGE IN LOWER FORWARD UNDERDECK FLOOR SUPPORT CHANNEL FS 210, BL 0 WL146. REPLACED FLOOR SUPPORT CHANNEL IAW SRM SMP 583 51-70, NR 0307. 2H74 4T A1SO 20051205000272005120500027SO 2005 12 5 LR7A05138 120051017A5320 FLOOR SUPPORT LKHEED382 382G 526414USO FS 197-225 CORRODED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER HC5312, FOUND CORROSION DAMAGE IN LOWER FORWARD UNDERDECK FLOOR SUPPORT TEE SECTION FS 197 TO FS 225. REPLACED FLOOR SUPPORT TEE SECTION IAW SRM SMP 583 51-70, NR 0307. 2H74 4T A1SO 20051205000292005120500029SO 2005 12 5 LR7A05140 120051017A5330 SKIN LKHEED382 382G 526414USO FS 277 DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER HC5321, FOUND STONE DAMAGE FS 277, LBL30 WL126. REPAIRED BELLY SKIN PER SRM 51-140-12, NR 0351. 2H74 4T A1SO 20051205000322005120500032SO 2005 12 5 LR7A05143 120051017A5343 CAP LKHEED382 382G 526414USO FS597 MISDRILLED A LR7AK NONE W INADEQUATE Q C ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER HC3212, FOUND TWO FASTENER HOLES WERE MISTAKENLY DRILLED DURING RIGHT HAND MLG BEAM CAP REPAIR, FS 597. REPAIRED IAW SRM SMP 583 53-40-3 AND ED05-025-1, NR 0373. 2H74 4T A1SO 20051205000532005120500053SO 2005 12 5 LR7A05164 120051017A5730 PANEL LKHEED382 382G 526414USO FS 597 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER SB 382-57-85, FOUND CRACKS IN NR 3 CENTER WING LOWER SURFACE PANEL, FS 597, LBL 60. REPAIRED IAW LOCKHEED REPAIR TASK 39 UNDER GLD 1720 (SK382-57-296) PER LAC MEA382-57-05-086, NR 0459. 2H74 4T A1SO 20051205000722005120500072NM 2005 12 5 USAA051453 120051201A5310 CREASE BEAM BOEING737 7374B7 1384702NM BS 615-639 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 FOUND CORROSION CREASE BEAM FROM STA 615 TO 639. REMOVED CORROSION, TREATED AND ALODINED AND PRIMED IAW 53-60-13, DEFECT SIZE: 1" CORROSION AREAS. 2L72 4F RTA16WE 20051205000732005120500073NM 2005 12 5 DHL2005749011 120051101A5510 TORQUE BOX BOEING727 7272J0 138407ENM BS 1303 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01749DH 22013 UPPER TORQUE BOX CRACKED ON LWR FWD RT CORNER BS 1303 WEB (ACCESS THRU VERT STAB PANL 9504). STOP DRILLED 1/2" LONG CRACK ON BS 1303 FRAME WEB AT RBL 22.00 FWD LWR CORNER IAW BOEING SB 727-53-0094 REV 3 AND COTNEY AEROSPACE ED NR EA204-4 REV IR HFEC VERIFIED STOP DRILL IAW B727 NDT MAN PT 6 51-00-00 FIG 23 AND COTNEY AEROSPACE ED NR EA204-4 REV IR W/8110-3 DATED 11/09/05. THIS REPAIR IS A CATEGORY "B" WITH REPEAT INSP NOT TO EXCEED 2,400 FLIGHT CYCLES. 2L73 4F RTA3WE 20051205000752005120500075NM 2005 12 5 UPS05445843 120051127A3350 BATTERY BOEING747 747123 1384873NM EMERGENCY LIGHT DISCHARGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 EMERGENCY LIGHT OVER THE FLT DECK STAIRS INOP (LOW BATTERY). REMOVED AND REPLACED EMERGENCY LIGHT ASSY IAW MM 33-51-00, OPS NORMAL. 2L74 4F A20WE 20051205000762005120500076WP 2005 12 5 UPS05845841 120051129A33505708458503 BATTERY PACK DOUG DC8 DC873F 302199FWP EMERGENCY LIGHTSINOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01852UP 46052 EMERGENCY LIGHTS INOP; FAILS TEST BUT BATTERY SEEMS TO BE GOOD. INSTALLED REPAIRED BATTERY PACK IAW 33-50-01-2. 2L74 4F RT4A25 20051205000772005120500077WP 2005 12 5 UPS05845844 120051130A3350 LIGHT DOUG DC8 DC873F 302199FWP EMERGENCY EXIT MALFUNCTIONED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 EMERGENCY EXIT LIGHT REMAINED ON IN FLIGHT, BREAKER POPPED, BREAKER RESET LIGHTS OPERATING NORMAL. OPS CK NORMAL ON GROUND PER MM 33-50-00, OK TO CONTINUE SERVICE. 2L74 4F RT4A25 20051206000022005120600002EA 2005 12 6 COMA0560650 120051126A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01455CA 7592 FLIGHT 5703 - FLAP HALF SPEED CAUTION. PERFORMED SYSTEM RESET, OPERATIONAL CHECK WAS NORMAL. 2L72 4F RTA21EA 20051206000152005120600015WP 2005 12 6 05FDEA04075 120051202A5312 REPAIR DOUG DC10 DC1030 3023501WP FUSELAGE UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 PERFORMED INSPECTION IAW EO NR 8-5100-7-5001-1P, FOUND DOUBLER LENGTH 12" WIDTH 9" ON TOP INTERNAL BULKHEAD NLG AT STA 560 Z-38 X11. NO ACTION TAKEN IAW EO NR 8-5100-7-5001 P1 E3 ATTACHMENT "A" NOTE 3 TREATED AND PRIMED AREA IAW SRM 57-21-01 VOL 1. 2L73 4F A22WE 20051206000322005120600032EU 2005 12 6 05FDEA04046 120051201A5730 REPAIR AIRBUS310 A310203 3930313EU ZONE 500 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 PREVIOUS REPAIR INSTALLED ON LT WING IB L/E IB OF NR 1 SLAT, EXTERNAL DOUBLER WS 139 RIB3, NEEDS EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. PREVIOUS REPAIR WAS NOT AN APPROVED REPAIR. REMOVED SKIN IAW A310-200 SRM 51-72-10. FABBED NEW SKIN IAW DWG A572462402 AND INSTALLED IAW A310-200 SRM 51-72-10. 2L72 4F RTA35EU 20051206000372005120600037EU 2005 12 6 05FDEA04051 120051201A5315 REPAIR AIRBUS310 A310203 3930313EU ZONE 200 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 PREVIOUS REPAIRS INSTALLED ON MAIN CARGO DECK FLOORBEAM AT FS 37 30" LEFT OF CENTER, NEEDS EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. PREVIOUS REPAIRS INSTALLED ON EA 6-5310-48685 AND EA 6-5321-50489. NO FURTHER ACTION REQUIRED. WORKED ON NRC N00723. CLASSIFIED AS MINOR REPAIRS PER GMM 6-2-100. 2L72 4F RTA35EU 20051206000412005120600041NM 2005 12 6 05FDEA04066 120051201A5710 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 HFEC INSPECTED CARRIED OUT AND CRACK FOUND ON LOWER LEFT HAND WING STRINGER S44. REPAIR CARRIED OUT ON CRACK FOUND AT LEFT HAND WING STRINGER 44 AS PER FEDEX EA 1-5720-90707, TITLE: "WINGS - STRINGER 44 LEFT HAND CRACK AT WING STATION XORS=508 - REPAIR". REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051206000432005120600043EA 2005 12 6 COMA0570124 120051126A32309752753 RELIEF VALVE CNDAIRCL600 CL6002C10 1390015EA MLG MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01656CA4733 10143 FLIGHT 5820 - GEAR DISAGREE. REPLACED THE BALANCE RELIEF VALVE. 2L72 4F RTA21EA 20051206000582005120600058EA 2005 12 6 SWIA200515905 120051125A27604916406 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 NM07862AS 7476 "SPOILERONS FAULT" AND "IB GND SPLR FAULT" STATUS MESSAGES DURING APPROACH TO SLC. REPLACED SECU NR 2 IAW MM 27-61-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051206000612005120600061EU 2005 12 6 AWXA200501474 120051130A3230 SELECTOR VALVE AIRBUS320 A320232 3930326EU LANDING GEAR MALFUNCTIONED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28675AW 2405 PHX - AIR TURN BACK - FLT 0081 - DURING CLIMB-OUT OF PHX, CREW REPORTED THAT LANDING GEAR WOULD NOT RETRACT. CREW RETURNED AND LANDED IN PHX WITHOUT FURTHER EVENT. MX CYCLED GEAR NUMEROUS TIMES AND WERE UNABLE TO DUPLICATE DISCREPANCY. PERFORMED MLG HYDRAULIC SAFETY VALVE TEST IAW AMERICA WEST AIRLINES TASK CARD A8M32301, NO FAULTS WERE NOTED. REMOVED AND REPLACED 40GA, LANDING GEAR SELECTOR VALVE, AND 41GA, LANDING GEAR DOOR SELECTOR VALVE, IAW AIRBUS 320 AMM 32-31-12 AND 34. REPLACED FOR PRECAUTIONARY PURPOSES. LEAK CHECKS OF VALVES GOOD. OPERATIONAL TESTS WERE GOOD. 2L72 4F RTA28NM 20051206000642005120600064NM 2005 12 6 AWXA200501477 120051111A5347D53472176200 SEAT TRACK AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28660AW 1234 SAL - DURING BC4 CHECK DISCOVERED LEVEL 2 CORROSION ON SEAT TRACK AT FS 58+13" AND Y1292. MAINTENANCE CUT OUT DAMAGED PORTION OF SEAT TRACK FROM FS 58+8" TO FS 59, Y1292 IAW AIRBUS 320 SRM 53-00-15 FIG 201 PAGE 205. FABRICATED L-PROFILE. INSTALLED NEW SECTION OF SEAT TRACK AND FABRICATED L-PROFILE FROM FS 58+8" TO FS 59 IAW AIRBUS 320 SRM 53-00-15 FIG 201 PAGE 205. 2L72 4F RTA28NM 20051206000892005120600089EA 2005 12 6 SWIA200515917 120051125A27518004301 DETECTOR CNDAIRCL600 CL6002B19 1900309EA FLAP SKEW MALFUNCTIONED A SWIAO OTHER FH FLT CONT AFFECTED ELECT. POWER LOSS-50 PC CRCRUISE 1 NM07923SW996 996 7664 FLAPS DEGRADED STATUS MSG INFLIGHT. REPLACED SKEW DETECTION UNIT IAW AMM 27-51-15, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051206001042005120600104EU 2005 12 6 05FDEA04042 120051130A2611 SMOKE DETECTOR AIRBUS300 A300B4622R 3930312EU AVIONICS MALFUNCTIONED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25719FD 388 AVIONICS SMOKE WARN DURING CLIMB-OUT. COMPLIED WITH CHECKLIST. DID NOT SMELL SMOKE. RETURNED TO KMCO. REPLACED AVIONICS COMPARTMENT SMOKE DETECTOR 13WA. OPERATIONAL TEST WAS NORMAL. REF A300 M/M 26-15-12-4 AND 26-15-00-5. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION OFF MFG CG7G0-11 POS AV3 SRL AB1954 TAG A08167 ON MFG CG7G0-11 SRL 728, TAG 172443. 2L72 4F RTA35EU 20051206001122005120600112EU 2005 12 6 05FDEA04017 120051129A7160 COWLING AIRBUS310 A310222 3930315EU PWA JT9 JT9D7R4E1 52054NE ZONE 400 SCRATCHED A FDEAKKKKNONE NONE NONE NONE OOOOTHER OTHER OTHER ININSP/MAINT 1 SO25450FE 162 707738 NR 2 ENG INLET COWL L/E HAS A 4.8" LONG SCRATCH AT 5:00 POS. REMOVED DAMAGED AREA IAW P&W SRM 54-10-00. PERFORMED HFEC IAW NTM 51-10-08. NO CRACKS NOTED. INSTALLED REPAIR DOUBLER AND FILLER IAW P&W SRM 54-10-00 REPAIR NR 10. 2L72 4F4 FRTA35EU E3NE 20051206001192005120600119NM 2005 12 6 05FDEA04024 120051129A5230 SKIN BOEING727 727227 1384078NM CARGO DOOR DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 GOODRICH RESPONSIBILITY. FOUND WHILE WORKING N00409, DENTED FWD CARGO DOOR SKIN 4.5" AFT FROM FWD EDGE AND 3" UP FROM LOWER EDGE. REPAIRED PER SRM 52-00-3. 2L73 4F A3WE 20051206001262005120600126EA 2005 12 6 SIMA200529002 120051013A26114462534 SMOKE DETECTOR CNDAIRCL600 CL6002C10 1390015EA LAVATORY MALFUNCTIONED A SIMAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SW21501BG 10017 XNA - FLT 4168 - FOUND CREW RECEIVED AFT LAV SMOKE MESSAGE ON EICAS ON TAKEOFF ROLL. REPLACED AFT LAV SMOKE DETECTOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA21EA 20051206001412005120600141EA 2005 12 6 ASOA05941 120051031A33506100928 LAMP CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27719EV 10099 DURING A GROUND INSPECTION IN SLC, THE RIGHT EMERGENCY EXIT SIGN, AT SEAT 14D, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE RIGHT EMERGENCY EXIT SIGN, AT SEAT 14D. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051206001482005120600148EA 2005 12 6 ASOA05954 120051105A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 379-969 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27709EV 10068 DURING A C-CHECK IN MCN, THE FLOOR SEAT TRACKS, AT LBL 9 AND RBL 9, FS 379 TO FS 969, WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACE THE FLOOR SEAT TRACKS, FROM FS 379 TO FS 969, LBL 9 AND RBL 9. (M) 2L72 4F RTA21EA 20051206001662005120600166NM 2005 12 6 ASAA0510315 120050921A5330654576889 SKIN BOEING737 737290C 138448VNM FS 360-380 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02740AS 22578 YXX - FOUND IN FORWARD CARGO BAY CORROSION ON SKIN AT BS 360-380 AT STRINGER 27 RT. SKIN REPAIRED PER B737-200 SRM 53-30-3. (M) 2L72 4F A16WE 20051206001672005120600167NM 2005 12 6 ASAA0510320 120050922A55316549559506 SPAR BOEING737 737290C 138448VNM VERTICAL STAB CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02740AS 22578 YXX - FOUND CORROSION ON VERTICAL STABILIZER AFT SPAR RIGHT PRIMARY AFT CLEVIS FORWARD FACE. CLEVIS REPLACED PER BOEING DWG 65-46572 AND B737-200 SRM 51-30-2. (M) 2L72 4F A16WE 20051208000062005120800006NM 2005 12 8 05FDEA04073 120051202A5315 FLOORBEAM BOEING727 727227 1384078NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 FOUND MAIN DECK FLOORBEAM HAS CORROSION AT STA BS 720A BETWEEN RBL4 AND RBL20. CLEANED AREA IAW B727 SRM 51-10-6, AND FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-10-1. REMOVED DAMAGED UPPER CHORD IAW B727 SRM 53-10-8 FIGURE 4. FABRICATED UPPER CHORD, SUPPORT ANGLES, AND REINFORCEMENT STRAPS IAW B727 SRM 53-10-8 FIGURE 4. ALODINED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED UPPER CHORD REPAIR IAW B727 SRM 53-10-8 FIGURE 4 AND 51-30-2. THIS IS A MAJOR REPAIR SIGNED BY TIMCO MECH NR 110174 AND QC303 REFERENCE FEDEX SNRM N00784. 2L73 4F A3WE 20051208000082005120800008WP 2005 12 8 ARWA20051103 120051124A2741AJH73385 DRIVE ASSY DOUG DC10 DC1030 3023501WP TRIM SYSTEM DAMAGED A ARWAO OTHER J WARNING INDICATION APAPPROACH 1 SO19524MD 46999 DURING APPROACH, AUTO PILOT OUT OF TRIM LIGHT ILLUMINATED; DISCONNECTED STABILIZER JAMMED AT 1 DEGREE NOSE UP. REMOVED AND REPLACED HORIZONTAL STABILIZER CHAIN DRIVE UNIT IN ACCORDANCE WITH DC-10 M/M 27-44-05. PERFORMED OPERATIONAL CHECK IN ACCORDANCE WITH DC-10 M/M 27-40-00 PAGE 501 & 601; OPERATIONAL CHECKED NORMAL. 2L73 4F A22WE 20051208000132005120800013EU 2005 12 8 SA05121 120051129A335032145410 EPSU AIRBUS320 A320214 3930316EU PASSENGER CABIN FAULTY A USAAK NONE L NO TEST ININSP/MAINT 1 EA19102UW11559205 844 THE EMERGENCY LIGHTS WOULD NOT TEST. MAINTENANCE REPLACED THE LEFT HAND, MID CABIN EMERGENCY POWER SUPPLY UNIT AND BATTERY. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20051208000152005120800015EU 2005 12 8 USAA051447 120051201A5315D5347219820200 FLOORBEAM AIRBUSA321 A321211 3930370EU BEAM Y1160 FR 68CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19164UW 1425 LOCATION: BEAM Y1160 FR 68 ACTION: DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-43-00, 53-41-04; CORR TASK 260-53500-002 DEFECT SIZE: 3" X 20" 2L72 4F RTA28NM 20051208000162005120800016EU 2005 12 8 USAA051448 120051201A5322D5347112420000 SHEAR TIE AIRBUSA321 A321211 3930370EU Y-1932 BETWEEN FCORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19164UW 1425 FOUND SHEAR TIE CORRODED Y-1932 BETWEEN FRAME 69-70. DEFECRIVE PART REPLACED WITH IDENT PART PER SRM 51-72-11; CORR TASK, JA-260-53500 DEFECT SIZE: 2" X 10". 2L72 4F RTA28NM 20051208000182005120800018EU 2005 12 8 USAA051450 120051201A5315D5347207500100 FLOORBEAM AIRBUSA321 A321211 3930370EU Y-1732 FROM 65-6CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19164UW 1425 FOUND FLOORBEAM CORRODED, Y-1732 FROM 65-66. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-72-11, DEFECT SIZE: 3" X 20". 2L72 4F RTA28NM 20051208000192005120800019EA 2005 12 8 COMA0560660 120051201A3260 PSEU CNDAIRCL600 CL6002B19 1900309EA DOORS UNKNOWN A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01916CA 7014 FLIGHT 5229 - CABIN, SERVICE AND CARGO DOOR CAUTION. RESET PSEU, PSEU PASSED SELF TEST. 2L72 4F RTA21EA 20051208000212005120800021EA 2005 12 8 COMA0560662 120051201A321016735109 POTENTIOMETER CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01403CA 7428 FLIGHT 5490 - NWS INOP. REPLACED RVDT. 2L72 4F RTA21EA 20051208000232005120800023NM 2005 12 8 DL757050716 120050914A5410313N321035 FAIRING BOEING757 757232 1384965NM NR 2 PYLON MISINSTALLED A DALAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO27646DL 24217 DURING MODIFICATION OF THE NR 2 PYLON FAIRING PER EO 06-075080-03AD THE MOD DOUBLER FOR THE NR 1 PYLON WAS INADVERTENTLY INSTALLED. INCORRECT DOUBLER WAS REPLACED WITH A SIMILAR DOUBLER CONTOURED TO MATCH THE NR 2 PYLON FAIRING. REF AD 2003-18-05. 2L72 4F RTA2NM 20051208000252005120800025NM 2005 12 8 DL73S050718 120051116A5330 SKIN BOEING737 737232 1384475NM BS 932 S-21R CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27326DL 23098 FUSELAGE SKIN WAS FOUND CRACKED AT BS 932, S-21R, CRACK IS 3 INCHES LONG. DOUBLER INSTALLED, REF AD 2004-18-06 & 2005-13-30. 2L72 4F RTA16WE 20051208000272005120800027NM 2005 12 8 DL76L050721 120051117A5420311T31571 ANGLE BOEING767 767332 1382001NM NR 2 PYLON CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27183DN 27110 THE NR 2 PYLON MID SPAR CLOSEOUT ANGLE WAS FOUND CRACKED. MID SPAR FITTING WAS INSPECTED AND CLOSEOUT ANGLE REPLACED PER ER/A 451663-14AD, REF AD 2005-19-23, 01-074944-12AD. 2L72 4F RTA1NM 20051208000292005120800029NM 2005 12 8 DL764050725 120051120A2430 CIRCUIT BREAKER BOEING767 767432ER 1385134NM DC STANDBY UNKNOWN A DALAO OTHER O OTHER CRCRUISE 1 SO27835MH 29708 AT CRUISE LOUD POP DOWN IN E&E COMPARTMENT FOLLOWED BY A DC STBY C/B POPPING AND LOSS OFF STBY POWER. RESET P6 PNL A2 C/B DC STBY INSPECTED E&E COMP FOR ABNORMALITIES CHECKS OK. STBY POWER TRANSFER OPS NORMAL. PERFORMED SHORT TEST PER M/M - NTF. 2L72 4F RTA1NM 20051208000312005120800031NM 2005 12 8 DL76S050727 120050811A5412311T12315 BULKHEAD BOEING767 767332 1382001NM NR 1 PYLON DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27116DL 23275 TOOLING DAMAGE WAS INCURRED ON THE MID SPAR BULKHEAD, HOLE COMMON TO UPPER SPAR FITTING AND UPPER SPAR WEB. HOLE WAS OVERSIZED TO REMOVE DAMAGE PER ER/A 099683-14. REF AD 2004-16-12, EO 01-074906-03AD. 2L72 4F RTA1NM 20051208000332005120800033NM 2005 12 8 DLM88050729 120051121A291659369865501 RESERVOIR DOUG MD88 MD88 3023688NM LEFT LEAKING A DALAO OTHER K FLUID LOSS LDLANDING 1 SO27994DL 53346 LEFT SYSTEM HYDRAULIC PRESSURE WENT TO -0- QUANTITY WAS NORMAL IN FLIGHT. REPLACED LEFT SYSTEM RESERVOIR. 2L72 4F RTA6WE 20051208000352005120800035WP 2005 12 8 AALA20050787 120051130A3350P4010049 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217537A 49991 LGA - FORWARD SECTION SEAT MOUNTED EMERGENCY EGRESS LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD SECTION SEAT MOUNTED EMERGENCY EGRESS LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051208000372005120800037WP 2005 12 8 AALA20050790 120051130A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21269AA 49292 SFO - CEILING EMERGENCY LIGHTS AT ROWS 7D TO 15D INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROWS 7D TO 15D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051208000392005120800039EU 2005 12 8 AALA20050780 120051125A2810 FUEL AIRBUS300 A300B4605R 3930308EU LT ENGINE CONTAMINATED A AALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW2190070 513 JFK - DURING CRUISE, LEFT ENGINE FUEL FILTER CLOG LIGHT ILLUMINATED. RETURNED TO JFK AND LANDED WITHOUT INCIDENT. REPLACED NUMBER 1 AND NUMBER 2 ENGINE FUEL FILTERS. ENTERED EACH FUEL TANK AND INSPECTED IN EACH TANK. FOUND SOME EVIDENCE OF OLD SEALANT. CLEANED TANKS AND ACCOMPLISHED RUN UP AND REPLACED FUEL FILTERS AGAIN. NO CONTAMINATION NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20051208000412005120800041WP 2005 12 8 AALA20050786 120051129A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21499AA 49737 LGA - EMERGENCY LIGHT AT STAIRWELL WALKWAY INOPERATIVE. RESECURED LOOSE BATTERY PACK FOR EMERGENCY LIGHT AT STAIRWELL WALKWAY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051208000432005120800043CE 2005 12 8 DXTA200501127 120051204A3240 PEDAL CESSNA500 560CESSNA 2076750CE BRAKE ASSY LEAKING E DXTAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07343QS 5600444 LEFT BRAKE PEDAL ON LEFT SIDE INTERMITTANTLY LOSES HYDRAULIC PRESSURE. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20051208000442005120800044CE 2005 12 8 DXTA200501128 120051204A3150 WARNING LIGHT CESSNA750 750 2076810CE CAS SYSTEM ILLUMINATED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07983QS 7500083 DURING TAKEOFF AROUND 50 KTS THE FADEC FAULT R A-B CAS MESSAGE CAME ON. TAKEOFF WAS ABORTED. THE FAULT WOULD NOT RESET. ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20051208000452005120800045NE 2005 12 8 DXTA200501124 220051201A7320 HMU BEECH MU300 400A 1155402CE PWA JT15 JT15D5 52112NE RT ENGINE OUT OF ADJUST E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07106QS RK381 PCEJA0545 A RIGHT ENGINE WOULD NOT REACH SCHEDULED TAKEOFF POWER OF 98.2 PERCENT. FULL THROTTLE REACHED 96 PERCENT ONLY (N1). ADJUSTED HMU PRESSURE REGULATING VALVE. OPS CHECKED GOOD. PERFORMED EEC AUTHORITY CHECK. 2H72 4F4 FRTA16SW E25EA 20051208000462005120800046CE 2005 12 8 DXTA200501122 120051114A3240216011 BRAKE ASSY CESSNA560 560XL 2076702CE MLG MALFUNCTIONED E DXTAD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07650QS 5605150 TAXIING OUT FOR DEPARTURE FROM TEB, WHILE MAKING RIGHT TURN AIRCRAFT WOULD NOT RESPOND & SUDDENLY MOVED TO THE LEFT. PRESSING ON THE RIGHT BRAKE WAS A RESISTANCE FEEL IN PEDAL MOVEMENT AND ACFT TURNED SHARPLY LEFT. REMOVED RIGHT BRAKE ASSY AS PER CUSTOMER REQUEST, INSTALLED O/H BRAKE ASSY. TAXI CHECK BY CREW AND OPS CHECK GOOD. BLEED BRAKES AS REQUIRED AND NO LEAKS NOTED. ALL WORK PERFORMED IAW CE-560XL MM CHAPTER 32-42-00. 2L72 4F RTA22CE 20051208000472005120800047CE 2005 12 8 DXTA200501125 120051201A3260 POSITION SWITCH CESSNA500 560CESSNA 2076750CE MLG OUT OF ADJUST E DXTAO OTHER J WARNING INDICATION APAPPROACH 1 GL07344QS 5600344 LEFT MAIN GEAR DOWN AND LOCKED LIGHT DID NOT ILLUMINATE UPON LOWERING THE GEAR. DID CHECKS AND EMER EXTENSION DID FLICKER BRIEFLY BUT WENT OUT. SHOWED NO RED LIGHT HAD 3 GREEN, NO RED AFTER LANDING. INSPECTED AND ADJUSTED LT MAIN GEAR ACTUATOR DOWN AND LOCKED SWITCH IAW CE-560 MM 32-31-04. PERFORMED LANDING GEAR RETRACTION AND EXTENSION TEST IAW 32-30-00. SECURED AND SAFTIED EMERGENCY GEAR NITROGEN BOTTLE IAW 12-13-01. GEAR DOWN AND LOCKED INDICATOR LIGHT, OPS CHECK GOOD. 2L72 4F RTA22CE 20051208000482005120800048NM 2005 12 8 SWAA053868 120051205A5312BAC1514 STIFFENER BOEING737 7373H4 1384600NM BS 1017 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D-CHECK, FOUND AFT PRESSURE BULKHEAD RADIAL STIFFENER CORRODED AT BS 1017, LBL 10. REPAIRED RADIAL STIFFENER PER BFG ER. 2L72 4F RTA16WE 20051208000492005120800049NM 2005 12 8 SWAA053869 120051205A53306545765 SKIN BOEING737 7373H4 1384600NM BS 503C CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503C, STR 14R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051208000502005120800050NM 2005 12 8 SWAA053870 120051205A53116520722 FRAME BOEING737 7373H4 1384600NM FWD CARGO CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, FWD FRAME LOWER STOP FITTING. REPAIRED FRAME PER SWA EA. 2L72 4F RTA16WE 20051208000512005120800051NM 2005 12 8 SWAA053871 120051205A5315141A5170 FLOORBEAM BOEING737 7373H4 1384600NM COCKPIT FLOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 DURING SCHEDULED D-CHECK, FOUND COCKPIT FLOORBEAM CORRODED AT BS 260, LBL 6 TO RBL 11, WL 208. REPAIRED FLOORBEAM PER BFG ER. 2L72 4F RTA16WE 20051208000522005120800052NM 2005 12 8 SWAA053872 120051205A53156545410 FLOORBEAM BOEING737 7373H4 1384600NM CABIN FLOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 744A, RBL 26.5. REPAIRED FLOORBEAM PER BFG ER. 2L72 4F RTA16WE 20051208000532005120800053NM 2005 12 8 SWAA053873 120051204A53116558280 FRAME BOEING737 7373G7 1384595NM BS 360 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29683SW 24008 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 13R TO STR 14R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051208000542005120800054NM 2005 12 8 SWAA053874 120051205A53306545774 SKIN BOEING737 7373T5 1384608NM BS 730E CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29696SW 23064 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 730E, STR 19R. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20051208000552005120800055NM 2005 12 8 DL76G050732 120051122A2430BACC18X25 CIRCUIT BREAKER BOEING767 767332 1382001NM COCKPIT FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO271608 30573 STANDBY BUS EICAS MESSAGE IN FLT. STBY POWER OFF LIGHT ILLUM, DID NOT EXTINGUISH WHEN BATTERY SELECTED MESSAGES INCLUDE L YAW DAMPER, L BLD ISLN VLV UTL BUSSES, L/E SLAT DISAGREE, PROBE HEAT AND AILERON LOCK OUT. REPLACED INTERMITTENT C/B, OPS NOW NORMAL. 2L72 4F RTA1NM 20051208000562005120800056NM 2005 12 8 DL757050733 120051122A5330146N37805 SKIN BOEING757 757232 1384965NM STA 1681, S-20L DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27673DL 25978 FUSELAGE SKIN STA 1681, STR-20L REPAIR OF DENT. THE FUSELAGE SKIN WAS FOUND DENTED DUE TO GROUND DAMAGE ON 09/30/03. SIGNED OFF AS TIME-LIMITED PER SRM. ER/A 097076-14 WAS ISSUED 2/21/05 TO EXTEND THE TIME-LIMIT BEFORE PERMANENT REPAIR. REV A OF THE ER/A COVERS THE PERMANENT REPAIR WHICH IS MAJOR AND OCURRED ON 11/22/05. THE REPAIR CUTS OUT THE DAMAGE AND INSTALLS EXTERNAL ALUMINUM DOUBLER AND FILLER OVER THE CUTOUT WITH SOLID ALUMINUM RIVETS. REF ACTS PP B757-53-22108. 2L72 4F RTA2NM 20051208000572005120800057NM 2005 12 8 DL75K050734 120051121A5330148N32161 SKIN BOEING757 757232 1384965NM BS 1851-1854 S25DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27694DA 29726 A DENT WAS DISCOVERED IN THE FUSELAGE SKIN AT BS 1851-1854, BELOW STR 25. INSTALLED DOUBLER PER ER/A 451829-14. 2L72 4F RTA2NM 20051208000582005120800058NM 2005 12 8 DL777050735 120051112A7830315W501083 INSULATION BOEING777 777232 1385232NM NR 1 & 2 ENGINE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27865DA 29737 THRUST REVERSER INSULATION BLANKETS WERE FOUND DAMAGED. INSPECTED AND REPAIRED PER ER/A 451632-14AD REF AD 2005-07-24. 2L72 4F RTT00001SE 20051208000592005120800059NM 2005 12 8 DL73S050736 120051121A5330654577518 SKIN BOEING737 737247 138448DNM BS 727B-750 S18RCRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27242WA 23516 CRACKS WERE FOUND IN THE FUSELAGE SKIN AT BS 727B-750, STR 18R AT THE CHEM MILL. CRACKS WERE REMOVED AND A DOUBLER INSTALLED PER ER/A 451748-14AD AND THE SRM. REF AD 2004-18-06, 2005-13-30. 2L72 4F A16WE 20051208000602005120800060NM 2005 12 8 DL75A050737 120051123A21312117338813 CONTROLLER BOEING757 757212 1384951NM CABIN PRESSURE FAILED A DALAA UNSCHED LANDING S AFFECT SYSTEMS CRCRUISE 1 SO27757AT 23127 BOTH AUTOPRESSURIZATION CONTROLLERS FAILED AT THE SAME TIME AT FL350 WAS ABLE TO CONTROL OUTFLOW VALVE IN MANUAL. DESCENDED TO 10,000 AND DIVERTED TO MCO. REPLACED NR 2 AUTO CONTROLLER DUE TO A LOSS OF AC POWER LAST FLT FAULT ON BITE. BITE AND VERIFICATION OF NR 1 AND NR 2 AUTO CONTROLLERS CHECK OK. MANUAL OPERATION NORMAL. 2L72 4F RTA2NM 20051208000612005120800061NM 2005 12 8 DL764050740 120051123A2120 ODOR BOEING767 767432ER 1385134NM CABIN DETECTED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27837MH 29710 F/A'S NOTICED ELECTRICAL SMELL BY ROW 40 LEFT SIDE OF CABIN. REPAIRED WIRING ON EMPOWER LAPTOP SYSTEM. 2L72 4F RTA1NM 20051208000622005120800062 2005 12 8 DL76G050741 420051125A34174040800912 ADC BOEING767 767332 1382001NM COCKPIT UNKNOWN A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO271611B 30595 AT 32K FEET, F/O ALTIMETER DISAGREED WITH CAPT AND VSI FLUX. 2L72 4F RTA1NM 20051208000632005120800063NM 2005 12 8 DL76G050742 120051126A5610141T480120 WINDOW BOEING767 767332 1382001NM COCKPIT FAILED A DALAO OTHER O OTHER CRCRUISE 1 SO271610D 30594 APPROX 1 HOUR NORTH OF JFK CREW REPORTED RT FWD WINDSHIELD HEAT INOP FOLLOWED BY OUTER PANE SHATTERED. NO AIR LEAKS, JUST OUTER PANE BROKEN. REPLACED WINDSHIELD AND HEAT CONTROLLER. 2L72 4F RTA1NM 20051208000642005120800064NM 2005 12 8 DL76L050743 120051127A7830 WARNING LIGHT BOEING767 767332 1382001NM NR 1 ENGINE FALSE ACTIVATIONA DALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27178DN32904 25143 A LEFT ENGINE REVERSER LIGHT CAME ON MOMENTARILY. TROUBLESHOT PER FIM, UNABLE TO DUPLICATE. 2L72 4F RTA1NM 20051208000652005120800065 2005 12 8 DL76S050744 420051127A256569B522062 PULLEY BOEING767 767332 1382001NM RT WING SLIDE FRACTURED A DALAK NONE O OTHER ININSP/MAINT 1 SO27126DL 24076 WHILE PERFORMING OPN 7013 RIGHT FWD DOOR OVERWING SLIDE DOOR ACTUATOR CHANGE FOUND THE DOOR CABLE PULLEY BROKEN AND CABLE OFF OF PULLEY IPC REF 25-65-51-01-ITEM 730. REPLACED PULLEY AND REINSTALLED CABLE, C/W OPN 7013 SLIDE DOOR ACTUATOR CHANGE. 2L72 4F RTA1NM 20051208000662005120800066NM 2005 12 8 DL76G050745 120051127A32503790037108 METERING VALVE BOEING767 7673P6 1385105NM NLG STEERING FAILED A DALAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO27152DL 24984 T/O ABORTED AT 30 KNOTS DUE TO INABILITY TO MAINTAIN DIRECTIONAL CONTROL WITH RUDDER PEDAL STEERING, AC DRIFTED RAPIDLY LEFT WITH FULL RIGHT RUDDER APPLIED WITH BOTH ENGINES AT T/O POWER. STEERING CONTROL DURING TAXI APPEARED NORMAL. REPLACED STEERING METERING VALVE. 2L72 4F RTA1NM 20051208000672005120800067NM 2005 12 8 DL76L050747 120051127A5420311T31571 ANGLE BOEING767 767332 1382001NM NR 1 PYLON CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27173DN 24800 NR 1 ENGINE PYLON MID SPAR CLOSE OUT ANGLE WAS FOUND CRACKED. REPLACED CRACKED MID SPAR CLOSE OUT ANGLE AND INSPECTED MID SPAR FITTINGS, REF AD 2005-19-23. 2L72 4F RTA1NM 20051208000682005120800068NM 2005 12 8 DL78K050748 120051122A5312148A22811 BULKHEAD BOEING737 737832 13844CFNM BS 1016 LBL 5 DEFORMED A DALAK NONE O OTHER ININSP/MAINT 1 SO273732J 30380 THE BS 1016 AFT PRESSURE BULKHEAD WEB AT LBL 5 AND WL 290 HAS A 5 INCH X 5.5 INCH X 0.156 INCH DEEP OIL CAN. THE BULKHEAD WEB DAMAGE WAS REMOVED AND REPAIR DOULBER WAS INSTALLED PER ER/A 451749-14. 2L72 4F RTA16WE 20051208000692005120800069NM 2005 12 8 DL764050749 120051128A2910UNK LINE BOEING767 767432ER 1385134NM HYD SYSTEM LEAKING A DALAO OTHER K FLUID LOSS CRCRUISE 1 SO27841MH 29714 AT CRUISE, RT HYD QTY ADVISORY MESSAGE WITH SLOWLY DECREASING HYD QTY RT EDP AND RT DEM, PUMPED TURNED OFF RMD ACCESS PNL FROM FWD SPAR LT SIDE OF HORIZ STAB FOUND LT ELEV PRESS LINE DAMAGED. FABRICATED NEW SECTION AND RINGLOCKED IN PLACE PER M/M 20-10-09. INSTALLED LT HORIZ STAB PANEL AND CLOSED ACCESS DOOR TO STAB. 2L72 4F RTA1NM 20051208000702005120800070NM 2005 12 8 DL764050750 120051128A2450 RECEPTACLE BOEING767 767432ER 1385134NM LAVATORY SHORTED A DALAHK DEACTIVATE SYST/CIRCUITSNONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO27837MH 29710 DURING SERVICING OF F/C FWD LAV WHEN CLOSING MIRROR COMPARTMENT SHAVING OUTLET SPARKED. FOUND PREVIOUS REPAIR FAILED. OUTLET NOT SECURE DEACTIVATED F/C FWD SHAVING OUTLET. 2L72 4F RTA1NM 20051208000712005120800071NM 2005 12 8 UPS05M44683 120050607A3244 TIRE DOUG MD11 MD11F 3023600NM NLG DAMAGED A IPXAO OTHER O OTHER LDLANDING 1 SO01250UP 48745 NOSE GEAR TOUCHDOWN, BLOWN TIRE(S) SUBSEQUENT FIRE. ENTERED WRONG TAIL NUMBER ON ORIGINAL MRR, PLEASE DISREGARD UPS05M44678. AIRCRAFT HARD LANDING INSPECTION, DAMAGE ASSESSMENT AND REPAIRS COMPLETED AND AIRCRAFT IS RETURNED TO SERVICE WITH REFERENCE TO BOEING JAC UPS-596 MAINTENANCE RELEASE AND UPS CONTRACT 6-1171-01391. RECORDS ON FILE WITH BOEING W/B 11-0596-091205, PER LP 506858/3. 2L73 4F RTA22WE 20051208000722005120800072NM 2005 12 8 SWAA053875 120051205A53306545774 SKIN BOEING737 7373T5 1384608NM BS 740D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29696SW 23064 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 740D, STR 19R. REPAIRED SKIN PER SWA EA AND SRM. 2L72 4F RTA16WE 20051208000732005120800073NM 2005 12 8 SWAA053876 120051204A3350612825 BATTERY PACK BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29756SA 27872 DURING SCHEDULED RON CHECK, FOUND EEPLS TRACK LIGHTS INOP BETWEEN ROW 1 ABC TO ROW 4 ABC. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20051208000742005120800074NM 2005 12 8 SWAA053866 120051204A3350101331 LENS BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED C3 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2L72 4F RTA16WE 20051208000752005120800075NM 2005 12 8 SWAA053867 120051204A5753 SKIN BOEING737 7373H4 1384600NM LH WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED C4 CHECK, FOUND LT WING OTBD T/E AFT FLAP DELAMINATED. REPAIRED FLAP PER SWA EA. 2L72 4F RTA16WE 20051208000762005120800076EA 2005 12 8 QXEA200501608 120051031A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA BS 1051 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, FUSELAGE EXTERIOR HAS NICKS AT THE SKIN AFT OF THE BAGGAGE DOOR STATION 1051 BETWEEN STRINGERS 13L AND 16L. MAINTENANCE BLENDED OUT DAMAGE IAW CRJ-700 SRM 51-12-00. WITHIN LIMITS OF EA R-53-397 AND REO 670-53-61-213. RESTORED FINISH. 2L72 4F RTA21EA 20051208000772005120800077EA 2005 12 8 QXEA200501612 120051031A5414 SKIN CNDAIRCL600 CL6002C10 1390015EA RT NACELLE GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC DURING C3 CHECK, RIGHT NACELLE AFT CORE COWL HAS NUMEROUS GOUGES ON INBOARD SIDE (LOWER EXTERNAL). MAINTENANCE REMOVED DAMAGE IAW CRJ-700 SRM 51-12-00-001-001-A01. RESTORED FINISH. 2L72 4F RTA21EA 20051208000782005120800078EA 2005 12 8 QXEA200501614 120051031A5730 SKIN CNDAIRCL600 CL6002C10 1390015EA RT WING DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, RIGHT WING UPPER SKIN TRAILING EDGE OUTBOARD OF MULTIFUNCTION SPOILERS HAS LOOSE FASTENERS. MAINTENANCE REPLACED THE RIVETS AS REQUIRED IAW CRJ SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20051208000792005120800079EA 2005 12 8 QXEA200501615 120051031A5730 SKIN CNDAIRCL600 CL6002C10 1390015EA RT WING CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, RIGHT WING UPPER LEADING EDGE SKIN HAS A CHAFED AREA FROM WS 178. MAINTENANCE BLENDED AREA IAW CRJ-700 SRM 57-41-01-101-001-A01. FINISH RESTORED. 2L72 4F RTA21EA 20051208000802005120800080EA 2005 12 8 QXEA200501616 120051031A5753 SKIN CNDAIRCL600 CL6002C10 1390015EA TE FLAP CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, RIGHT WING INBOARD FLAP VANE UPPER SKIN HAS CHAFED DAMAGE AT TRAILING EDGE. REPAIRED IAW CRJ-700 SRM 51-12-00-001-001-A01. TREATED AND PRIMED AND PAINTED AREA. 2L72 4F RTA21EA 20051208000812005120800081EA 2005 12 8 QXEA200501618 120051031A5310 FASTENER CNDAIRCL600 CL6002C10 1390015EA PAX DOOR FRAME MISINSTALLED A QXEAK NONE W INADEQUATE Q C ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, PASSENGER DOOR FRAME AT DOOR ASSIST CABLE BRACKET, LOCK FASTENER INSTALLED WITH NO COLLAR. MAINTENANCE INSTALLED NEW LOCK FASTENER WITH COLLAR IAW CRJ-700 SRM 51-62-21-001-001-A01. 2L72 4F RTA21EA 20051208000822005120800082EA 2005 12 8 QXEA200501604 120051031A541067037140002 SPAR CNDAIRCL600 CL6002C10 1390015EA PYLON TOOL DAMAGE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, FUSELAGE INTERIOR FORWARD SIDE AT STATION 1088.2 BETWEEN STRINGERS 9R AND 10R. PYLON SPAR PART NUMBER 67037140002 TOP SURFACE HAS SEVERAL DRILL MARKS. MAINTENANCE BELNDED OUT DAMAGE IAW EA R-54-86 AND REO 670-54-51-007. RESTORED SURFACE. 2L72 4F RTA21EA 20051208000832005120800083EA 2005 12 8 QXEA200501605 120051031A5410 SPAR CNDAIRCL600 CL6002C10 1390015EA PYLON TOOL DAMAGE A QXEAK NONE W INADEQUATE Q C ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, FUSELAGE INTERIOR FORWARD SIDE AT STATION 1088.2 BETWEEN STRINGERS 9L AND 10L PYLON SPAR PART NUMBER 670-37140-001 TOP SURFACE HAS A DRILL MARK. MAINTENANCE BLENDED OUT DAMAGE IAW EA R-54-86 AND REO 670-54-51-007. RESTORED SURFACE. 2L72 4F RTA21EA 20051208000842005120800084EA 2005 12 8 QXEA200501607 120051031A5230 SKIN CNDAIRCL600 CL6002C10 1390015EA CARGO DOOR NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, AFT BAGGAGE DOOR OUTER SKIN HAS A NICK. MAINTENANCE REMOVED DAMAGE IAW CRJ-700 SRM 51-12-00-001-001-A01. RESTORED FINISH. 2L72 4F RTA21EA 20051208000852005120800085EA 2005 12 8 QXEA200501625 120051031A5754 SKIN CNDAIRCL600 CL6002C10 1390015EA RT SLAT CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, RIGHT SLAT INTERIOR SKIN HAS FRETTING CORROSION. MAINTENANCE BLENDED OUT CORROSION IAW CRJ-700 SRM 57-42-01-101-D01-A01. TREATED AREA. 2L72 4F RTA21EA 20051208000862005120800086NM 2005 12 8 QXEA200501736 120051202A6120 RELAY DHAV DHC8 DHC8202 2809007NM AUTOFEATHER SYS UNKNOWN A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09353PH 496 SEA - NR 2 PROPELLER WON'T FEATHER DURING THE AUTOFEATHER TEST. MAINTENANCE REPLACED NR 2 AUTOFEATHER TEST CIRCUIT RELAY 6121-K4. TESTED AUTOFEATHER SYSTEM TEST SEQUENCE PER AMM D & O 61-26-00, PAGE 9-11, PARAGRAPH F. TEST CIRCUITS AND AUTOFEATHER SYSTEM FUNCTIONED NORMALY. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051208000872005120800087 2005 12 8 QXEA200501737 420051202A34207003360941 INDICATOR DHAV DHC8 DHC8202 2809007NM AHRU MALFUNCTIONED A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09359PH* 20 514 SEA FLIGHT NR 2038, DURING TAXI NR 1 EADI PITCHED DOWN APPROXIMATELY 8 DEGREES BANKED TURNS SETTING OFF SEVERAL MISMATCH MESSAGES ON THE ADVISORY DISPLAY. MAINTENANCE REPLACED NR 1 AHRU IAW D-8 200 MTX CARD 9340019. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051202000532005120200053NM 2005 12 2 ASAA0540422 120050822A53206552878U102 SILL BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU BS 937-1000 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 CORROSION ON AFT ENTRY MOPSILL, BS 937 TO 1000. REMOVED AND REPLACED AFT ENTRY MOPSILL. (K) 2L72 4F4 FRTA16WE E21EU 20051202000572005120200057EA 2005 12 2 ASOA05944 120051102A2910AE71115204 LINE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE ENG DRIVEN PUMP MALFUNCTIONED A ASOAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27758EV1540 10210 DURING CRUISE, AT APPROX 36,000 FT, THE CREW RECEIVED A LT PACK HIGH TEMPERATURE MESSAGE. CREW COMPLIED WITH QRH TO TURN OFF PACK. ONCE PACK WAS TURNED OFF, A LT HYDRAULIC LOW PRESSURE 1 APPEARED FOLLOWED BY A LOUD NOISE AND HYDRAULIC QUANTITY FLUCTUATION. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED. EMERGENCY VEHICLES WERE DISPATCHED WITH THE AIRCRAFT LANDING SAFELY. MAINT REMOVED AND REPLACED THE NR 1 EDP AND PRESSURE LINE. OPS CHECK GOOD. AC OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA EOOO63EN 20051202000592005120200059EA 2005 12 2 ASOA05894 120051023A5210601R3198055 STEP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR DISCONNECTED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27849AS 7347 DURING A GROUND INSPECTION, THE PASSENGER DOOR BOTTOM STEP TIE ROD WAS FOUND DISCONNECTED FROM THE PASSENGER DOOR BOTTOM STEP. MAINT REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20051202000632005120200063NM 2005 12 2 AMTA200500926 120051023A2612710125 SENSOR BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE NR 1 ENGINE UNSERVICEABLE A AMTAK NONE N FALSE WARNING ININSP/MAINT 1 GL11552TZ 32586 NR 1 ENG STATUS MESSAGE (L ENG FIRE LP 1) DISPLAYED. REMOVED AND REPLACED LOOP TS5035 IAW WDM. L ENG FIRE LOOP 1, OPS CHECK GOOD IAW. (K) 2L72 4F4 FRTA2NM E12EU 20051202000682005120200068EU 2005 12 2 MHIA106721 120051104A5302 FRAME UROCOPEC130 EC130B4 8680989EU TMECA ARRIUSARRIUS2B1 NE TAIL BOOM DAMAGED B MHIAK NONE O OTHER ININSP/MAINT 1 EA25454AE5477 3490 23011 SMALL HOLE FOUND ON BOTTEM OF TAIL BOOM AFT OF 2ND FRAME IN TAIL BOOM. 556MM AFT OF TAIL BOOM FLANGE. REPAIRED IAW MFG REPAIR SCHEME MG110220053 NO REVISION, DATED 11/2/05 AND FAA FORM 8110-03 FILE NR DERY-710242-SW/05/331 DATED 11/2/2005. FAA FORM 337 SUBMITTED 11/4/2005. 1G72 3U3 U H9EU E34NE 20051202000752005120200075WP 2005 12 2 U2RA0809 120051104A331016434 TRANSFORMER DOUG DC8 DC863F 302198FWP COCKPIT LIGHTS BROKEN A U2RAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL23865F 7837878378 46088 PILOTS OVERHEAD PANEL LIGHTS INOP, GLOW FUSE ON FOLLOWED BY SMOKE. 2L74 4F 4A25 20051202000882005120200088NM 2005 12 2 TSAA0532055 120051111A3244247F621 TIRE BOEING737 737282 13844ATNM PWA JT8 JT8D9A 52048NE NOSEWHEEL FAILED A TSAAO OTHER O OTHER TXTAXI/GRND HDL 1 WP13824AL 23045 DURING TAXI AFTER LANDING, CREW HEARD A LOAD POP FOLLOWED BY VIBRATION FROM THE NOSEWHEEL AND STEERING DIFFICULTY. CREW STOPPED AIRCRAFT ON TAXIWAY. MAINTENANCE FOUND HOLE IN LT NOSEWHEEL AND BOTH TIRES FLAT. REMOVED AND REPLACED BOTH NOSEWHEEL TIRES, INSPECTED AND FOUND NO OTHER DEFECTS. RETURNED THE AIRCRAFT TO SERVICE. 2L72 4F4 FRTA16WE E2EA 20051202000902005120200090NM 2005 12 2 HNAA050099 120051118A2840 INDICATOR DHAV DHC8 DHC8102 2809003NM NR 2 FUEL MALFUNCTIONED A HNAAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 EA07938HA 152 NR 2 FUEL GAUGE INDICATES DOUBLE THE FUEL BURN NR 2 FUEL GAUGE, OPS NORMAL DURING FERRY FLT. REFUELED IN LGA. MAGNA STICKED NR 2 TANK AND NR 2 FUEL GAUGE MATCHES MAGNA STICK READING. GAUGE OPS NORMAL AT THIS TIME. 2H72 4T RTA13NM 20051202001322005120200132NE 2005 12 2 05FDEA04010 220051129A7200 ENGINE AIRBUS310 A310203 3930313EU GE CF6 CF680 30025NE NR 1 BIRD INGESTION A FDEAA UNSCHED LANDING C F.O.D. CLCLIMB 1 SO25401FE 191 585209 ON DEPARTURE BIRD STRIKE LT NR 1 ENGINE. ENGINE VIB MAX APPROX 3.7 AT 85 PERCENT. AT IDLE APPROX 1.6; EGT NORMAL, N1 + N2 NORMAL OTHERWISE. REDUCED POWER FOR APPROACH. ENGINE HAS BEEN APPROVED FOR REMOVAL (DAMAGE) NEW ENGINE EXPECTED OMA 12/05/05 (THIS WILL CLOSE THIS SDR) 2L72 4F4 FRTA35EU E13NE 20051202001342005120200134EU 2005 12 2 05FDEA04002 120051126A2120EVT4160A DISTRIBUTOR BLK AIRBUS310 A310203 3930313EU GE CF6 CF680A3 30025NE CABIN AIR MALFUNCTIONED A FDEAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO25414FE3044230442 400 VENT EXTRACT LOW FLOW RESET ONCE OK CAME ON DURING TAKEOFF ROLL. TRIPPED ATS LEVERS WITH HEAVY SMELL OF OVERHEAT. 2L72 4F4 FRTA35EU E13NE 20051202001362005120200136WP 2005 12 2 05FDEA04004 120051129A5753 SKIN DOUG MD10 MD1010F 3022112WP GE CF6 CF66K 30020NE TE FLAP DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25571FE 47830 DURING STRIPPING ACTIVITIES, RR IB FLAP SKIN UPPER SIDE ACCIDENTALLY DAMAGED CAUSING CRACK 3 INCHES LONG. REMOVED FLAP SECTION IAW SRM 51-31-01. PERFORMED INSPECTION, NO CRACK FOUND. PERFORMED DOUBLER REPAIR IAW SRM 57-10-00 FIG 85. 2L73 4F4 FRTA22WE E23EA 20051202001382005120200138WP 2005 12 2 05FDEA04006 120051129A5730ARB09832 DOUBLER DOUG MD10 MD1010F 3022112WP GE CF6 CF66K 30020NE LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25571FE 47830 DURING PRE-PAINT INSPECTION FOUND CORROSION WITH EXFOLIATION ON BEVER/TAIL OF LT WING AT STA XORS 284. REPAIRED IAW EA 8-5710-93818. 2L73 4F4 FRTA22WE E23EA 20051202001472005120200147EA 2005 12 2 A6WA200540321 120051108A5340601R3111357 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FS 280 CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31426AW 7669 OB CLIP AT FS 280, LBL 9.0, IS CRACKED IN RADIUS AT TOP OF CLIP CRACK APPROX .5 INCH LONG. REMOVED AND REPLACED FS 280, LBL 9.0 FLOORBEAM TO BULKHEAD ATTACHMENT ANGLE IAW SRM (OB CLIP). (K) 2L72 4F4 FRTA21EA E15NE 20051202001512005120200151NM 2005 12 2 DHL2005749015 120051102A5311 FRAME BOEING727 7272J0 138407ENM BS 970 DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01749DH 22013 FRAME AT STA 970 ABOVE STR 26 LT IS DENTED M/R. CUT OUT DAMAGED AREA 7/8" BY 2 3/4" AND FABBED REPAIR ANGLE FROM 7075 T6 .063 PO 9002351 DIM 4" BY 10 7/8" IAW B727 SRM 51-40-3 FIG 1 AND 53-10-2. TREATED AND PRIMED IAW B727 SRM 51-10-20. INSTALLED REPAIR ANGLE IAW B727 SRM 51-40-3 FIG 1. 2L73 4F RTA3WE 20051202001532005120200153WP 2005 12 2 MWEA050129 120051201A531359361981 LONGERON DOUG DC9 DC981 3022081WP STA 522-579 DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31807ME 48033 LONGERON 21 RIGHT IS DAMAGED AT STATION 522-579. FABRICATED AND INSTALLED NEW SECTION OF LONGERON. 2L72 4F A6WE 20051202001602005120200160NM 2005 12 2 SWAA053808 120051130A53116520722 FRAME BOEING737 7373H4 1384600NM FWD CARGO CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, FWD FRAME LOWER STOP FITTING. REPAIRED FRAME PER SWA EA. 2L72 4F RTA16WE 20051205000022005120500002NM 2005 12 5 DHL2005749012 120051101A5311 FRAME BOEING727 7272J0 138407ENM BS 500 DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01749DH 22013 FOUND DENT ON FRAME AT BS 500 ABOVE STR 24R. CUT OUT DAMAGED AREA 4 1/8" BY 1 1/8" FROM FRAME ON BS 500 ABOVE STR 24R IAW B727 SRM 51-40-3 FIG 1. FAB REPAIR DOUBLER 12" BY 2 1/8" OF 7075 T6 .063 PO 9002351 IAW B727 SRM 51-10-2 FIG 3 AND 51-40-3 FIG 1. TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED REPAIR PART IAW B727 SRM 51-30-2 AND 51-40-3 FIG 1. 2L73 4F RTA3WE 20051205000042005120500004NM 2005 12 5 DHL2005749005 120051031A5330 SKIN BOEING727 7272J0 138407ENM BS 1001 DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01749DH 22013 FOUND DENT RT SIDE FUSELAGE SKIN STA 1001 BELOW STR 25R. EVALUATED DENT AND FOUND OUT OF LIMITS AND IS LESS THAN 10" FROM A CUTOUT OR SPLICE MINIMUM DISTANCE IS 19" IAW B727 SRM 53-30-1 FIG 1. CUT OUT DENTED SECTION OF FUSELAGE SKIN SIZE 1" BY 2.550" AT STA 1001 AND JUST BELOW STR 25R IAW B727 SRM 53-30-3 FIG 1. HFEC INSPECTED CUT OUT AND HOLES WITH NO CRACKS NOTED IAW B727 SRM NDT MAN PT 6 51-00-00 FIG 23+11. FABRICATED DOUBLER 2024T3 .080 PO NR 9002459 (13"BY 10") AND TRIPLER 2024T3 .080 PO 9002459 (10/2" X 8") IAW B727 SRM 53-30-3 FIG 3 AND RO ASTR CO SRD-1 REV IR. TREATED AND PRIMED AREA AND REPAIR PARTS IAW B727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B727 SRM 53-30-3 FIG 3 REV IR ASTR -004RO-1. 2L73 4F RTA3WE 20051205000192005120500019SO 2005 12 5 LR7A05130 120051017A523034318812RMT GUSSET LKHEED382 382G 526414USO FS 980 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER HC5212, FOUND CARGO DOOR BULKHEAD LOWER ANGLE GUSSET CRACKED FS 980. REPLACED LOWER ANGLE GUSSETT PLATE ASSEMBLY IAW SRM SMP 583 51-70 AND AC43.13-1B PARA 4-52, NR 0193. 2H74 4T A1SO 20051205000242005120500024SO 2005 12 5 LR7A05135 120051017A531533766425 FLOORBEAM LKHEED382 382G 526414USO FS 200 CORRODED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER HC5312, FOUND CORROSION DAMAGE LOWER FORWARD UNDERDECK FLOOR SUPPORT ANGLE, FS 200, LBL9 WL146. REPLACED FLOOR SUPPORT ANGLE IAW SRM SMP 583 51-70 AND ED05-025-02, NR 0307. 2H74 4T A1SO 20051205000252005120500025SO 2005 12 5 LR7A05136 120051017A531533766425 FLOORBEAM LKHEED382 382G 526414USO FS 200 CORRODED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER HC5312, FOUND CORROSION DAMAGE LOWER FORWARD UNDERDECK FLOOR SUPPORT ANGLE, FS 200, RBL9 WL146. REPLACED FLOOR SUPPORT ANGLE IAW SRM SMP 583 51-70 AND ED05-025-02, NR 0307. 2H74 4T A1SO 20051205000282005120500028SO 2005 12 5 LR7A05139 120051017A533033799469 DOUBLER LKHEED382 382G 526414USO FS 197 CORRODED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER HC5312, FOUND CORROSION DAMAGE IN LOWER FORWARD UNDERDECK SKIN FS 197, LBL36 WL139 - WL146. INSTALLED DOUBLER PER SRM SMP 583 51-70, NR 0307. 2H74 4T A1SO 20051205000352005120500035SO 2005 12 5 LR7A05146 120051017A5753 CAP LKHEED382 382G 526414USO WS 163 RT CORRODED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER HC5711, FOUND RIGHT HAND OUTBOARD FLAP CENTER LOWER SPAR CAP CORROSION. REPAIRED IAW DRAWING R05-025-03 PER LAC MEA382-57-05-073. NR 0404. 2H74 4T A1SO 20051205000442005120500044SO 2005 12 5 LR7A05155 120051017A5311 FRAME LKHEED382 382G 526414USO FS 757 MISDRILLED A LR7AK NONE W INADEQUATE Q C ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER HC5313, FOUND FUSELAGE FRAME (LS5408-2) MISDRILLED LINER HOLE LEFT HAND SIDE, FS757, WL151. REPAIRED IAW DRAWING R05-025-08 PER LAC MEA382-53-05-070, NR 0413. 2H74 4T A1SO 20051205000482005120500048SO 2005 12 5 LR7A05159 120051017A5311 FRAME LKHEED382 382G 526414USO FS 732 MISDRILLED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER HC5313, FOUND FUSELAGE FRAME (LS4010-8) MISDRILLED LINER HOLE LEFT HAND SIDE, FS732, WL151. REPAIRED IAW DRAWING R05-025-07 PER LAC MEA382-53-05-071, NR 0414. 2H74 4T A1SO 20051205000512005120500051SO 2005 12 5 LR7A05162 120051017A5730 SKIN PANEL LKHEED382 382G 526414USO CWS 171 CORRODED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER HC5711, FOUND LEFT HAND CENTER WING LOWER PLANK CORROSION CWS171-213. REPAIRED IAW DRAWING R05-025-05 PER LAC MEA382-57-05-077, NR 0416. 2H74 4T A1SO 20051205000542005120500054SO 2005 12 5 LR7A05165 120051017A5320 BRACKET LKHEED382 382G 526414USO FS 1001 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER HC5212, FOUND CARGO DOOR BULKHEAD STIFFENER/TUBE STRUT ATTACH BRACKET CRACKED, FS1001, RBL30. REPLACED ATTACH BRACKET IAW SRM SMP 583 51-70 AND AC43.13-1B, PARA 4-57 NR 0081. 2H74 4T A1SO 20051205000592005120500059SO 2005 12 5 LR7A05170 120051017A5320 BRACKET LKHEED382 382G 526414USO FS 1001 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2450 4590 DURING C-6 CHECK PER HC5212, FOUND CARGO DOOR BULKHEAD STIFFENER/TUBE STRUT ATTACH BRACKET CRACKED, FS 1001, RBL40. REPLACED ATTACH BRACKET IAW SRM SMP 583 51-70 AND AC43.13-1B PARA 4-57, NR 0081. 2H74 4T A1SO 20051205000632005120500063NM 2005 12 5 USAA051435 120051201A5315BAC14902734 FLOORBEAM BOEING737 7374B7 1384702NM BS 344 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19780AU 24997 FOUND CORROSION MAIN DECK STA 344, LBL 0; CORROSION LEVEL 1; TASK C53-107-02. FABRICATED REPAIR PARTS, INSTALLED REPAIR FILLER AND ANGLES PER SRM 53-10-51, 51-40-02, DEFECT SIZE: 2.50"L BY 1.10"W BY .031"D. 2L72 4F RTA16WE 20051206000012005120600001EA 2005 12 6 COMA0560645 120051126A2752854D10019 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA LEFT WING FLAP FAULTY A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01735CA9022 7267 FLIGHT 5556 - EN ROUTE CVG-PWM RECEIVED A FLAP FAIL MESSAGE AT ZERO FLAP POSITION. CREW DECLARED AN EMERGENCY AND FLIGHT LANDED SAFELY AT PWM. REPLACED THE LEFT WING OUTBD FLAP ACTUATOR. 2L72 4F RTA21EA 20051206000282005120600028NM 2005 12 6 05FDEA04065 120051201A5320 ANGLE DOUG MD11 MD11F 3023600NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 FOUND CENTER TANK LEFT LOWER CAP ANGLE AT STA 1298.6 SUSPECT CRACK. CTR TANK LT LOWER CAP ANGLE AT STA 1298.6 AREA REPAIRED AS PER FEDEX EA 1-5310-90694 (FUSELAGE - CAP ANGLE LT UNDERWING BARREL STRUCTURE AT STA 1298.6, XCW 46, CRACK - ANGLE FABRICATION & SPLICE INSTALLATION). REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20051206000312005120600031EU 2005 12 6 05FDEA04045 120051201A5730 REPAIR AIRBUS310 A310203 3930313EU ZONE 600 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 PREVIOUS REPAIR INSTALLED ON RT WING TE PANEL EXTERNAL SKIN AFT OF PYLON, EXTERIOR DOUBLER, STA 482-513 RIB 8-9, NEEDS EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. PREVIOUSLY INSTALLED REPAIR ON RT WING T/E PANEL AFT OF PYLON WAS ACCOMPLISHED ON EA 5710-29479. VISUAL EVALUATION CONSISTED OF CORRECT LOCATION, SHAPE, SIZE, FASTENER SPACING/NUMBER, MATERIAL THICKNESS/TYPE AND GOOD WORKMSNSHIP. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. WORK DOCUMENTED ON NRC N00712. 2L72 4F RTA35EU 20051206000402005120600040EU 2005 12 6 05FDEA04053 120051201A5330 REPAIR AIRBUS310 A310203 3930313EU ZONE 100 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 PREVIOUS REPAIR INSTALLED ON FUSELAGE RT SIDE FS 12A STA1091 - 40" BELOW MAIN DECK FLOOR, FLUSH DOUBLER NEEDS EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR NOT IAW A310-200 SRM 53-12-12 PB201 FIG 202. REMOVED EXISTING REPAIR IAW A310-200 SRM 51-40-21. REPAIRED SKIN IAW A310-200 SRM 53-12-12 PB201 FIG 202. MINOR REPAIR IAW GMM 6-2-100. WORKED ON NRC N00715. 2L72 4F RTA35EU 20051206000552005120600055EA 2005 12 6 COMA0560639 120051124A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS UNRELIABLE A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01927CA10282 7031 FLIGHT 5434 - FLAPS FAIL CAUTION. REPLACED THE LT BPSU. 2L72 4F RTA21EA 20051206000722005120600072EA 2005 12 6 COMA0560637 120051123A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA RT TE FLAPS UNRELIABLE A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01735CA175 7267 FLIGHT 5678 - FLAPS FAIL CAUTION. REPLACED THE RT BPSU. 2L72 4F RTA21EA 20051206000902005120600090 2005 12 6 SWIA200515918 420051115A3418 COMPUTER CNDAIRCL600 CL6002B19 1900309EA STALL WARNING MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07983SW 7961 STALL TEST FAIL, FOD CHECK. REPLACED STALL COMPUTER IAW 27-35-01 AND STICK PUSHER IAW MM 27-35-15-400-801. OPERATIONAL CHECK GOOD, PN C12851BA01 SN OFF 521 PN ON 501-1259-04 OFF 2422. 2L72 4F RTA21EA 20051206000932005120600093EA 2005 12 6 SWIA200515921 120051116A2741 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA ELEVATOR INOPERATIVE A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07946SW 7776 CAPTIAN'S TRIM (ELEV) IS INOP. REPLACED PILOT'S PITCH TRIM SWITCH. OPERATIONAL CHECK GOOD PER MM 27-41-05. 2L72 4F RTA21EA 20051206000942005120600094EA 2005 12 6 SWIA200515922 120051119A2730 TRANSMITTER CNDAIRCL600 CL6002C10 1390015EA ELEVATOR POSITIOMALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION LDLANDING 1 NM07707SK 10003 "ELEVATOR SPLIT" CAUTION MESSAGE IN FLARE JUST BEFORE LANDING AND INTERMITTENTLY ON TAXI IN. REPLACED RT ELEVATOR POSITION TRANSMITTER IAW MM 27-34-10. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051206000982005120600098NM 2005 12 6 05FDEA04035 120051130A5312 NONE DOUG MD11 MD11 3023602NM ZONE 200 NONE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 CONFORMITY INSPECTION RECORD FOR N524FE ITEM 8, 2007 AFT PRESSURE BULKHEAD INTERNAL HAD A SPLICE REPAIR AT 6 O'CLOCK POSITION. REPAIR IS PAINTED GRAY. FOUND REPAIR CARRIED OUT IN ACCORDANCE WITH SRM 53-40-00 FIGURE 6 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. NARI, NO M OR D. 2L73 4F RTA22WE 20051206001012005120600101WP 2005 12 6 05FDEA04038 120051130A5320 REPAIR DOUG DC10 DC1030 3023501WP FUSELAGE UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 PERFORMED INSPECTION IAW EO NR 8-5100-7-5001-1P, FOUND DOUBLER DIA 3.5 INCH INT FUSELAGE RT SIDE AT STA 1879 LONG 41. PERFORMED INSPECTION ON REPAIR IAW SRM 53-20-00 FIG 13 SHT 4 VOL 1 AND EA NR 8-5330-93234. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P1. 2L73 4F A22WE 20051206001132005120600113EU 2005 12 6 05FDEA04018 120051129A5220 SKIN AIRBUS310 A310222 3930315EU EMERGENCY EXIT SCRATCHED A FDEAK K NONE NONE O OTHER ININSP/MAINT 1 SO25450FE 162 RT EMERGENCY EXIT DOOR FWD AND BELOW EXTERNAL HANDLE HAS 1 SCRATCH APPROX 7.7 INCH LONG, 1 DENT/GOUGE APPROX 3.8" LONG, AND 1 DENT/GOUGE APPROX 2.2 BY 3" LONG. BLENDED SCRATCH IAW A310-200 SRM 51-73-10 AND FOUND TO WITHIN LIMITS OF A310-200 SRM 52-20-00. CUTOUT DENT/GOUGED AREAS IAW A310-200 SRM 52-10-00 FIG 206. PERFORMED HFEC IAW NTM 51-10-08. NO CRACKS FOUND. INSTALLED DOUBLER AND FILLER IAW EA 6-5220-94441. WORK DOCUMENTED ON NRC N00067 2L72 4F RTA35EU 20051206001292005120600129SO 2005 12 6 SIMA200531508 120051102A534714000486005 SEAT TRACK EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21822AE 145581 FOUND LEFT OUTBOARD SECOND AFT SEAT TRACK FROM FRONT CORRODED. REPLACED SEAT TRACK IAW EMB 140 AMM 53-01-06. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20051206001362005120600136SO 2005 12 6 SIMA200531102 120051031A532014522178005 SILL EMB 145 EMB145 3260210SO SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21610AE15310 145073 THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED EXISTING SILL AND CLEANED AREA. INSTALLED SERVICEABLE SILL. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 31, CHAPTER 51-40-02. (M) 2L72 4F RTT00011AT 20051206001392005120600139EA 2005 12 6 ASOA05957 120051106A33506100976 LAMP CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27701EV 10020 DURING A GROUND INSPECTION IN BTR, THE AFT INTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE AFT INTERIOR EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051206001552005120600155EA 2005 12 6 ASOA05936 120051031A335059257 INVERTER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27848AS 7339 DURING A GROUND INSPECTION IN VPS, THE EMERGENCY LIGHTS, NEAR THE SERVICE DOOR AND FORWARD PASSENGER DOOR, WERE FOUND IN TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY LIGHTS INVERTER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051206001562005120600156NM 2005 12 6 ASAA0510303 120050920A53136549886501 STRINGER BOEING737 737290C 138448VNM FS 395 DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02740AS 22578 YXX - FOUND STRINGER 27L AT BS 395 CUT FOR ACCESS. REPAIRED PER B737-200 SRM 53-10-3 FIGURE 1. (M) 2L72 4F A16WE 20051208000032005120800003EU 2005 12 8 05FDEA04016 120051129A7932VT0304S1 REGULATOR AIRBUS310 A310 EU PWA JT9 JT9D7R4D 52054NE ENG OIL PRESS MALFUNCTIONED A FDEAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 SO25454FE 278 707709 NR 2 ENGINE INDICATED HIGH OIL PRESSURE, THEN FOLLOWED QRH & MONITORED PARAMETERS. OIL PRESS. WENT TO 20-32 PSI (LOW) FOLLOWED QRH AND SHUTDOWN ENGINE. DECLARED EMERGENCY AND LANDED RWY 32L. HIGH OIL PRESS. WAS 100, LOW OIL PRESS. WAS 22. PRESSURE VARIED ACCORDING TO THROTTLE POSITION. ALL OTHER ENGINE PARAMETERS WERE NORMAL EXCEPT RT OIL TEMP AT 130 DEG LEFT ENGINE OIL TEMP 120 DEG. REPLACED THE OIL PRESSURE REGULATOR AND OIL PRESSURE TRANSMITTER 2L72 4F4 FRTA35EU E3NE 20051208000102005120800010EU 2005 12 8 DHL2005362AA2 120051203A5753A5796005000200 RIB AIRBUS300 A300B4203 3930306EU TE FLAP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01362DH 84 DURING "A" CHECK, LT INBD. FLAP NOSE RIB NR 7 CRACKED, REMOVED NOSE SKIN AND RIB NR 7 FROM LT IB FLAP IAW A-300 S/B A-300-57-0242. INSTALLED NEW RIB AND REINSTALLED NOSE SKIN PER S/B A-300-57-0242 2L72 4F RTA35EU 20051208000172005120800017EU 2005 12 8 USAA051449 120051201A5315D5347217220400 FLOORBEAM AIRBUSA321 A321211 3930370EU BEAM Y1160 FRAMECORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19164UW 1425 LOCATION: BEAM Y1160 FRAME 67-68 ACTION: DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-43-00, 53-41-04; TASK JA-260-53500 DEFECT SIZE: 3" X 16" 2L72 4F RTA28NM 20051208000202005120800020EA 2005 12 8 COMA0560661 120051201A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA LEFT UNRELIABLE A COMAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 SO01806CA8548 7359 FLIGHT 4965 - FLAPS FAIL CAUTION. REPLACED THE LEFT BPSU. 2L72 4F RTA21EA 20051208000222005120800022EA 2005 12 8 COMA0560663 120051201A2150350023000 CHECK VALVE CNDAIRCL600 CL6002B19 1900309EA AC PACK MALFUNCTIONED A COMAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION APAPPROACH 1 SO01797CA16703 7344 FLIGHT 5153 - RIGHT AC PACK HIGH TEMP AND SMOKE TOILET WARNING WITH VISIBLE SMOKE. REPLACED THE FAN BYPASS CHECK VALVE. 2L72 4F RTA21EA 20051208000242005120800024NM 2005 12 8 DL76L050717 120051116A5420311T31571 ANGLE BOEING767 767332 1382001NM NR 2 PYLON CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27177DN 25122 NR 2 PYLON CLOSEOUT ANGLE FOUND CRACKED. MID SPAR FITTING WAS INSPECTED FOR CRACKS AND CLOSEOUT ANGLE WAS REPLACED. REF AD 2005-19-23, 01-074944-12AD. 2L72 4F RTA1NM 20051208000262005120800026NM 2005 12 8 DL76L050720 120051117A5420311T31571 ANGLE BOEING767 767332 1382001NM NR 1 PYLON CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27183DN 27110 THE NR 1 PYLON MID SPAR FITTING CLOSEOUT ANGLES WAS FOUND CRACKED. THE MID SPAR FITTINGS WERE INSPECTED AND THE CLOSEOUT ANGLES WERE REPLACED, REF AD 2005-19-23, 01-074944-12AD. 2L72 4F RTA1NM 20051208000282005120800028NM 2005 12 8 DL73S050722 120051115A5330655298878 SKIN BOEING737 737232 1384475NM L2 DOOR CUTOUT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27324DL 23096 A 3 INCH CRACK WAS FOUND IN THE FUSELAGE SKIN AND BEAR STRAP AT THE L-2 DOOR CUTOUT, LOWER FORWARD CORNER. INSTALLED REPAIR DOUBLERS PER THE SRM AND AUTHORIZED LIMITED BLIND FASTENERS PER ER/A 451664-14. 2L72 4F RTA16WE 20051208000302005120800030NM 2005 12 8 DL76L050726 120051120A21203209951 VALVE BOEING767 767332 1382001NM FWD CARGO COMP FAILED A DALAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO27177DN 25122 BEFORE TAKEOFF EICAS DISPLAYED FWD EQUIP VLV AND VLV LIGHT ON OVERHEAD EQUIP COOLING PANEL. REPLACED RELAY K200. 2L72 4F RTA1NM 20051208000322005120800032NM 2005 12 8 DL73S050728 120051118A5330 SKIN BOEING737 737232 1384475NM BS 747-767 S-18RDEFORMED A DALAK NONE O OTHER ININSP/MAINT 1 SO27326DL 23098 THE FUSELAGE SKIN WAS FOUND WITH AN OIL CAN CONDITION FROM BS 747-767 BELOW S-18R. INSTALLED DOUBLER PER ER/A 451596-14AD. REF AD 2005-13-30 & 2004-18-06. 2L72 4F RTA16WE 20051208000342005120800034 2005 12 8 DL75K050730 420051121A2565 LIGHT BOEING757 757232 1384965NM 4L DOOR SLIDE INOPERATIVE A DALAO OTHER O OTHER LDLANDING 1 SO27698DL 29911 INBOUND WRITE UP OF AFT LEFT DOOR 4L SLIDE INDICATOR LIGHT INOP. RELAMPED LIGHT, NO HELP. FOUND FWD GIRT BAR SLIDE LOCK HAD DETACHED FROM THE GIRT BAR AND WAS NOT LOCKING INTO THE DOOR FRAME TO PROPERLY ATTACH THE SLIDE. REINSTALLED THE GIRT BAR SLIDE LOCK PER THE M/M. SLIDE LOCKS AND INDICATION WERE WORKING AS PER THE M/M. 2L72 4F RTA2NM 20051208000362005120800036WP 2005 12 8 AALA20050788 120051130A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217537A 49991 LGA - COCKPIT OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR COCKPIT OVERHEAD EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051208000382005120800038NM 2005 12 8 AALA20050789 120051130A2530AAP2530 OVEN BOEING757 757223 1384957NM CABIN DIRTY A AALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW21190AA 32384 SNN - REPORT OF SMOKE FROM DOOR SEAL AT NUMBER 3 OVEN IN AFT GALLEY. SMOKE STOPPED WHEN OVEN SWITCHED OFF. CLEANED OVENS IN AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20051208000402005120800040EU 2005 12 8 AALA20050783 120051127A3233 CASE AIRBUS300 A300B4605R 3930308EU ACTUATOR SPLIT A AALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW2119059 469 MIA - LOSS OF GREEN HYDRAULIC SYSTEM AFTER TAKEOFF. FOUND NOSE GEAR RETRACT ACTUATOR CASING SPLIT. REPLACED NOSE GEAR RETRACT ACTUATOR. GREEN HYDRAULIC SYSTEM FULL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20051208000882005120800088NM 2005 12 8 QXEA200501738 120051202A3040SYLZ50970 CONTROLLER DHAV DHC8 DHC8202 2809007NM WINDSHIELD HEAT MALFUNCTIONED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09374PH1578015780 528 SEA FLIGHT NR 2199, "LEFT WINDSHIELD HOT" ILLUMINATED DURING TAXI OUT WITH WINDSHIELD HEAT SELECTED TO NORM. MAINTENANCE MEASURED RESISTANCE OF NORM ON OVERHEAD WINDOW TEMP SENSORS AT WINDSHIELD HEAT CONTROLLER. REPLACED RELAYS 3041-K9 ABD K-. REPLACED CONTROLLER. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051208000892005120800089NM 2005 12 8 QXEA200501739 120051202A3040AYLZ50970 CONTROLLER DHAV DHC8 DHC8202 2809007NM WINDSHIELD HEAT MALFUNCTIONED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09374PH240 528 SEA FLIGHT NR 2027, LEFT WINDSHIELD HOT CAUTION LIGHT ILLUMINATED DURING TAXI. MAINTENANCE REPLACED CAPTAINS WINDSHIELD HEAT CONTROLLER. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051208000902005120800090EA 2005 12 8 QXEA200501606 120051031A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA BS 1010-1045 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, FUSELAGE LOWER EXTERNAL SKIN AT STATION 1010-1045 STRINGERS 27-24 HAS NICKS AND AREAS OF PREVIOUS BLEND OUTS BELOW THE GROUND SERVICE DOOR. MAINTENANCE BLENDED OUT AREA IAW CRJ-700 SRM 51-12-00-001-A01. REPLACED DAMAGED FASTENERS. TREATED AND PRIMED AND PAINTED AREA. 2L72 4F RTA21EA 20051208000912005120800091EA 2005 12 8 QXEA200501610 120051031A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA BS 1015-1047 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, FUSELAGE EXTERIOR HAS NICKS ON SKIN ABOVE AFT BAGGAGE DOOR AT STATION 1015 TO 1047. MAINTENANCE BLENDED OUT DAMAGED AREAS IAW CRJ-700 SRM 51-12-00. WITHIN LIMITS OF EA R-53-397 AND REO 670-53-61-213. RESTORED FINISH. 2L72 4F RTA21EA 20051208000922005120800092EA 2005 12 8 QXEA200501626 120051031A5230670387881 FITTING CNDAIRCL600 CL6002C10 1390015EA CARGO DOOR CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, AFT BAGGAGE DOOR INTERNAL AFT UPPER FITTING IS CRACKED IN THE RADIUS. MAINTENANCE REPLACED THE FITTING IAW CRJ-700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20051208000932005120800093NM 2005 12 8 SWAA053835 120051130A53306545776 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29671SW 23785 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051208000942005120800094NM 2005 12 8 SWAA053836 120051130A5313BAC1498 STRINGER BOEING737 7373G7 1384595NM BS 360 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29671SW 23785 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED STRINGER PER SRM. 2L72 4F RTA16WE 20051208000952005120800095EA 2005 12 8 QXEA200501627 120051031A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA BS 280-310 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, LOWER FUSELAGE EXTERNAL GOUGED AT STATION 280-310 STRINGERS 26L TO 26R. MAINTENANCE REMOVED DAMAGE IAW CRJ-700 SRM 51-12-00-001-001-A01. RESTORED FINSIH. 2L72 4F RTA21EA 20051208000972005120800097NE 2005 12 8 COMA0570125 220051203A7200 ENGINE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE RIGHT OVERHEATED A COMAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO01376CA 10092 FLIGHT 5281- RT MOTOR OVERTEMP DURING T/O, ITT 960 C. INSPECTED ENGINE AND FOUND NO DEFECTS. OPERATIONAL CHECKS WERE NORMAL. 2L72 4F4 FRTA21EA EOOO63EN 20051208000982005120800098EA 2005 12 8 COMA0560667 120051203A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA WARNING LIGHT A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01969CA 7141 FLIGHT 5709 - FLAPS FAIL CAUTION. CHECKED RIGGING OF LT AND RT BPSU. 2L72 4F RTA21EA 20051208000992005120800099EA 2005 12 8 COMA0560664 120051202A2797 WIRE HARNESS CNDAIRCL600 CL6002B19 1900309EA SPOILERS UNKNOWN A COMAO OTHER F FLT CONT AFFECTED CRCRUISE 1 SO01957CA 7109 FLIGHT 4996 - UNCOMMANDED RIGHT ROLL, RT FLIGHT SPOILER DEPLOYED. SPOILER FAULT MESSAGE. NO FAULT CODES IN SECU. REPLACED THE RT OUTBD FLIGHT SPOILER WIRE HARNESS FOR TROUBLESHOOTING. 2L72 4F RTA21EA 20051208001002005120800100EA 2005 12 8 COMA0560665 120051202A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA WARNING LIGHT A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01969CA 7141 FLIGHT 5005- FLAPS FAIL CAUTION. INSPECTED FLAPS IAW AD 98-20-01. NO DEFECTS NOTED. 2L72 4F RTA21EA 20051208001032005120800103SO 2005 12 8 SWIA200515947 120051204A27203081401003 ACTUATOR EMB 120 EMB120ER 3260203SO RUDDER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CLCLIMB 1 NM07190SW1254612546 120050 RT RUDDER JAMMED AFTER TAKEOFF. REPLACED LOWER RUDDER ACTUATOR AND RIGGED IAW MM 27-22-02 AND 27-20-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20051208001042005120800104EA 2005 12 8 SWIA200515948 120051205A2752 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA TE FLAP MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 NM07463SW 7820 ON FINAL SELECTED FLAPS 8 DEGREES. RECEIVED FLAPS FAIL MESSAGE. REPLACED FLAP ACTUATORS ON LT AND RT OUTBOARD FLAPS IAW 27-53-05. REPLACED FLEX SHAFT. REPLACED SKEW DETECTION UNIT IAW MM 27-51-15. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051208001052005120800105EA 2005 12 8 SWIA200515949 120051202A3350 SWITCH CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07595SW 7292 EMERGENCY LIGHT INDICATION PUSH SWITCH INOP. REPLACED EMERGENCY LIGHT INDICATOR PUSH SWITCH AS REQUIRED. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051208001062005120800106 2005 12 8 SWIA200515950 420051202A222070609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07439SW7592 7592 7578 STAB TRIM AND MACH TRIM FAILED WILL NOT RE-ENGAGE. REPLACED THE HSTCU IAW MM 27-41-01, OPERATIONAL CHECK GOOD IAW MM 27-40-00. 2L72 4F RTA21EA 20051208001072005120800107EA 2005 12 8 SWIA200515951 120051202A274170609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07466SW 7856 STAB TRIM CH 1 INOP MSG APPEARED IN FLIGHT. REPLACED HSTCU IAW MM 27-41-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051208001082005120800108EA 2005 12 8 SWIA200515952 120051202A27604916406 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07416SW2935 2935 7089 SPOILERONS FAULT STATUS. REPLACED NR 1 SECU IAW 27-61-05. OPERATIONAL CHECK OK. 2L72 4F RTA21EA 20051208001092005120800109EA 2005 12 8 SWIA200515953 120051204A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLT SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07927SW 7693 SPOILERONS FAULT, STATUS WOULD NOT CLEAR. REPLACED RIGHT SPOILERON NR 2 PCU OPERATIONAL CHECK GOOD, PN ON 27000-7 OFF 5830. 2L72 4F RTA21EA 20051208001102005120800110EA 2005 12 8 SWIA200515954 120051204A2752 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07437SW 7564 FLAPS FAILED INFLIGHT WHEN SELECTING FLAPS 8. REMOVED AND REPLACED RIGHT FLAP ACTUATORS R1, R2, R3, R4. OPERATIONAL CHECK OF FLAPS, CHECKS GOOD. 2L72 4F RTA21EA 20051208001112005120800111SO 2005 12 8 SWIA200515955 120051204A27203211001003 PCU EMB 120 EMB120ER 3260203SO RUDDER LEAKING A SWIAO OTHER KFJFLUID LOSS FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07582SW433 433 120350 BLUE HYD RESERVOIR LOW LEVEL LIGHT CAME ON INFLIGHT. REPLACED RUDDER PCU PER EMB 120 MM 27-22-01, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20051208001122005120800112EA 2005 12 8 SWIA200515956 120051202A27604916405 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07927SW1018310183 7693 SPOILERON FAULT STATUS MSG. REPLACED NR 2 SECU PER 27-61-05, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051208001132005120800113EA 2005 12 8 SWIA200515957 120051129A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLT SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07453SW 7743 ON TAXI OUT "FLIGHT SPOILERS FAULT" STATUS MESSAGE. REPLACED RIGHT OB FLIGHT SPOILER PCU IAW CRJ 200 MM 27-62-01, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051208001142005120800114NM 2005 12 8 QXEA200501601 120051201A30103D147211 TIMER DHAV DHC8 DHC8202 2809007NM NR 2 DEICE BOOT INOPERATIVE A QXEAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 NM09365PH1277812778 526 BOI - ON FLIGHT 2204, A/C OVER FLEW IDA CONTINUED TO PIH, THEN DIVERTED TO BOI, NR 2 DEICE BOOT POSITION (BOTH SIDES) INOPERABLE IN AUTO AND FAST MODE, FAILED TO INFLATE OPERATES NORMALLY IN MANUAL MODE. MAINTENANCE REMOVED AND REPLACED DEICE TIMER. OPERATINAL CHECK OF DE-ICING SYSTEM CHECKS GOOD, NO DEFECTS NOTED. C/W VISUAL INSPECTION OF THE BOOTS DURING INFLATION WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051208001152005120800115EA 2005 12 8 COMA05701256 120051204A2613 WIRE CNDAIRCL600 CL6002C10 1390015EA OVERHEAT WARNINGDAMAGED A COMAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01669CA 10176 FLIGHT 4663- WING OVERHEAT WARNING. REPAIRED DEFECTIVE WIRING CONNECTIONS AT INBD TEMP SENSOR. OPERATIONAL CHECK SATISFACTORY. 2L72 4F RTA21EA 20051208001162005120800116NM 2005 12 8 SWAA053820 120051130A57536546431 SKIN BOEING737 7373H4 1384600NM LT WING FOREFLAPDELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED C1 CHECK, FOUND LT WING OTBD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM. 2L72 4F RTA16WE 20051208001172005120800117NM 2005 12 8 SWAA053821 120051130A3350101073 LENS BOEING737 7373H4 1384600NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM. 2L72 4F RTA16WE 20051208001182005120800118NM 2005 12 8 SWAA053822 120051130A53306545774 SKIN BOEING737 7373H4 1384600NM BS 727E CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29338SW 23960 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 18L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051208001192005120800119NM 2005 12 8 SWAA053823 120051130A53306545774 SKIN BOEING737 7373H4 1384600NM BS 747 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29338SW 23960 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 18L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051208001202005120800120NM 2005 12 8 SWAA053824 120051130A53306545774 SKIN BOEING737 7373H4 1384600NM BS 747 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29338SW 23960 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 19R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051208001212005120800121EA 2005 12 8 QXEA200501619 120051031A5753 SKIN CNDAIRCL600 CL6002C10 1390015EA TE FLAP DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, RIGHT INBOARD FLAP LOWER SURFACE HAS GRAVEL DAMAGE. MAINTENANCE BLENDED DAMAGE AREA IAW CRJ-700 SRM 57-01-101-001-A01, RESTORED FINISH. 2L72 4F RTA21EA 20051208001222005120800122SO 2005 12 8 MASA200500398 120050526A322022250100003 SOLENOID VALVE EMB 145 EMB145LR 3260212SO NLG UNKNOWN A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07852MJ626 626 145567 ASH 2935 DCA TO GSP, THE CREW DIVERTED TO CLT DUE TO A LOUD NOISE COMING FROM THE NLG AREA AFTER TAKEOFF. MAINTENANCE REPLACED THE NLG SOLENOID VALVE AND NLG DOOR PROX SWITCH. 2L72 4T RTT00011AT 20051208001232005120800123SO 2005 12 8 MASA200500561 120050718A27503631001011 FCU EMB 145 EMB145LR 3260212SO TE FLAPS WARNING LIGHT A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07843MJ9378 145478 ASH 2687 CLT, FLAP FAIL MESSAGE IN FLIGHT. R2 FECU. 2L72 4T RTT00011AT 20051208001242005120800124 2005 12 8 MASA200500585 420050723A34180861DT5 SENSOR EMB 145 EMB145LR 3260212SO AOA WARNING LIGHT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07833MJ545 145327 ASH 2971 CLT, SPS1 INOP MESSAGE. MX REPLACED THE NR 1 AOA SENSOR AND THE SYSTEM OPS CHECKED GOOD. 2L72 4T RTT00011AT 20051208001252005120800125SO 2005 12 8 MASA200500597 120050727A3260355022002 SQUAT SWITCH EMB 145 EMB145LR 3260212SO MLG WARNING LIGHT A MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW07826MJ 145214 ASH 2731 CLT, LANDING GEAR GROUND AIR FAIL MESSAGE. MX R2 NLG WOW PROX SWITCH. 2L72 4T RTT00011AT 20051208001262005120800126SO 2005 12 8 MASA200500614 120050805A521012028455001 SEAL EMB 145 EMB145LR 3260212SO PAX DOOR UNKNOWN A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07826MJ 145214 ASH 2939 CLT, PAX DOOR DIFFICULT TO OPERATE. MX REPLACED THE PAX DOOR SEAL. 2L72 4T RTT00011AT 20051208001272005120800127GL 2005 12 8 MASA200500696 220050904A732023076368 METERING UNIT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUEL PUMP UNKNOWN A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW07848MJ12531 145530 ASH 2969 CHO, SMOKE WAS COMING FROM THE NR 2 ENGINE EXHAUST DURING TAXI IN. MX REMOVED AND REPLACED THE FPMAU. 2L72 4T4 FRTT00011ATTE6CH 20051208001292005120800129SO 2005 12 8 MASA200500702 120050728A2120BWT138001 DUCT EMB 145 EMB145LR 3260212SO RT RECIRC FAN TORN A MASAK NONE O OTHER ININSP/MAINT 1 SW07835MJ 145353 DURING OVERNIGHT MAINTENANCE A RT RECIRC FAN DUCT WAS FOUND TORN. MAINTENANCE REPLACED DUCT THROUGH A FLEET CAMPAIGN DIRECTIVE (FCD). 2L72 4T RTT00011AT 20051208001302005120800130SO 2005 12 8 MASA200500703 120050730A2120BWT138001 DUCT EMB 145 EMB145LR 3260212SO NR 2 PACK UNKNOWN A MASAK NONE O OTHER ININSP/MAINT 1 SW07836MJ 145359 DURING OVERNIGHT MAINTENANCE A NR 2 PACK WAS FOUND NOISY. MAINTENANCED REPLACED THE DUCT THROUGH A FLEET CAMPAIGN DIRECTIVE (FCD). 2L72 4T RTT00011AT 20051208001422005120800142NM 2005 12 8 QXEA200501732 120051129A5755NAS6604D25 BOLT BOMBDRDHC8 DHC8402 1390042NM SPOILER DAMAGED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09413QX 4060 DURING HIGH SPEED CLIMB & CRUISE, AUTOPILOT ON 'MISTRIM RT WING DOWN' DISCONNECTED AP. MANUALLY RETRIM A/C TO HALF SCALE RT WING DOWN DURING APPROACH WITH FLAPS 15 DEG NEEDED TO START TAKING OUT THAT TRIM UNTIL FLAPS AT 35. NO RT WING DOWN NEEDED. MX PERFORMED GVI OF AILERON TO FLAP GAP SEALS & CONFIRMED SPOILERS REMAINED RETRACTED WITH HYD POWER APPLIED. NO DEFECTS NOTED. PERFORMED OPS TEST OF PITCH & ROLL ACTUATOR IAW AMM. NO DEFECTS NOTED. REPLACED RT INBD SPOILER ATTACH POINT BOLTS & BUSHINGS & ADJUSTED CABLE TENSIONS BETWEEN AILERON SPLITTER QUADRANT TO AILERON TERMINAL QUADRANT & BETWEEN AILERON QUADRANT TO SPLITTER QUADRANT & ADJUSTED RT AILERON PUSH ROD. OCF PERFORMED. ACFT RETURNED TO SERVICE.2H72 4T RTA13NM 20051208001432005120800143NM 2005 12 8 QXEA200501733 120051130A5101 UNKNOWN BOMBDRDHC8 DHC8402 1390042NM UNKNOWN UNKNOWN A QXEAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 NM09412QX 4059 RDD FLIGHT NR 2310, BOTH CONDITION LEVERS INADVERTANTLY BROUGHT BELOW MINIMUM RESULTING IN NR 1 AND NR 2 PEC CAUTION LIGHTS AND PROP RPM 1060-1070. MAINTENANCE C/W Q400 FIM TASK 61-20-05-810-822. RESET SET FAULT CODES. C/W AUTO FEATHER TEST. NO DEFECTS NOTED. PERFORMED OPS TEST OF OVERSPEED GOVERNOR TEST IAW Q400 AMM TASK 61-20-00-710-801. NO DEFECTS NOTED. OPS TESTED GOOD. COMPLIED WITH FIM TASK 61-20--06-810-818. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051208001452005120800145SO 2005 12 8 LR7A05198 120051129A53123435886L BULKHEAD LKHEED382 382G 526414USO BS 1012 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03406LC 711 4676 DURING B-2 CHECK PER HB5302, FOUND LT AFT FUSELAGE BULKHEAD INNER CAP BROKEN/WEB CRACKED AT FS1012, WL265-275, LBL63. REPLACED INNER CAP AND WEB IAW SMP583 CH 51-60 & 51-70, NR 2056. 2H74 4T A1SO 20051208001472005120800147SO 2005 12 8 LR7A05200 120051129A53123632072R BULKHEAD LKHEED382 382G 526414USO BS 1012 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03406LC 711 4676 DURING B-2 CHECK PER HB5302, FOUND RT AFT FUSELAGE BULKHEAD OUTBOARD CAP AT FS 1012, WL270, RBL63. REPLACED OUTBOARD CAP IAW SMP583 CH 51-60 AND 51-70, NR 2069. 2H74 4T A1SO 20051208001492005120800149SO 2005 12 8 LR7A05202 120051129A523034318826 CAP LKHEED382 382G 526414USO FS 990 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03406LC 711 4676 DURING B-2 CHECK PER HB5302 AND DURING GUSSET REPLACEMENT FOUND CARGO DOOR BULKHEAD LOWER CAP CRACKED AT FS 990, WL236, RBL30-59. REPAIRED CAP IAW ER/A 5250-171-ERA, MEA 382-52-05-102, NR 2072. 2H74 4T A1SO 20051208001512005120800151SO 2005 12 8 LR7A05204 120051129A53123425889 BULKHEAD LKHEED382 382G 526414USO FS 1012 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03406LC 711 4676 DURING B-2 CHECK PER HB5302, FOUND LT SIDE BULKHEAD WEB WITH 1 INCH CRACK AT FS 1012, WL270, LBL63. REPLACED WEB IAW SMP583 CH 51-60 AND 51-70, NR 2082. 2H74 4T A1SO 20051208001542005120800154EU 2005 12 8 RAIA00511040 120051123A3220 RELAY JETAIRJETSTMJETSTM4101 1500501EU NLG STRUTE LOOSE A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03563HK 41079 FLT 9460 - BWI -AFTER TAKEOFF, TAT LIGHT CAME ON AT 200 FEET, AT 500 FEET WHEN FLAPS SELECTED TO ZERO, WARMING STARTED. DID NOT STOP UNTIL POWER WAS REDUCED TO APPROX 50 PERCENT. MAINTENANCE INSPECTED AND FOUND NOSE OLEO STRUT SLAVE RELAY LOOSE. RESECURED RELAY AND PERFORMED TAKEOFF CONFIG TEST. CHECKED GOOD. 2L72 4T RTA41NM 20051208001552005120800155SO 2005 12 8 RAIA00512002 120051204A3350 BATTERY PACK EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSINOPERATIVE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03812HK 145373 PRE FLIGHT - STL - FLOOR EMERGENCY LIGHT STRIP OUT AT ROW 12. MAINTENANCE REPLACED THE BATTERY PACK AT ROW 12A. 2L72 4T RTT00011AT 20051208001562005120800156SO 2005 12 8 RAIA00512003 120051204A3350 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03814HK 145046 PRE FLIGHT - STL - LEFT SIDE EMERGENCY LIGHT FWD OF WING INOP. MAINTENANCE REPLACED THE BULB. 2L72 4T RTT00011AT 20051208001582005120800158EU 2005 12 8 RAIA00512005 120051204A3350 WIRE JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT DAMAGED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03570HK 41089 PRE FLIGHT - STL - EMERGENCY LIGHT ON FLOOR IN FRONT OF 6A INOP. MAINTENANCE REPAIRED WIRING TO FLOOR LIGHT STRIP. 2L72 4T RTA41NM 20051208001592005120800159SO 2005 12 8 RAIA00512006 120051204A3397 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DAMAGED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03819HK 145062 PRE FLIGHT - STL - MID CABIN EMERGENCY EXIT LOCATING SIGN FORWARD SIDE DOES NOT ILLUMINATE. MAINTENANCE REPAIRED CONNECTION TO SUBJECT EXIT SIGN. 2L72 4T RTT00011AT 20051208001602005120800160SO 2005 12 8 RAIA00512001 120051201A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03815HK 145048 PRE FLIGHT - STL - EMERGENCY LIGHT OVER 1A AND EXIT PLACARD AT COCKPIT FLOOR INOP. MAINTENANCE INSPECTED EMERGENCY LIGHT SYSTEM. OPS CHECK GOOD. 2L72 4T RTT00011AT 20051208001612005120800161SO 2005 12 8 RAIA00511038 120051130A2130 CABIN PRESSURE EMB 145 EMB145LR 3260212SO CABIN PRESSURE MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03830HK 145313 FLT 5490 - STL - ON CLIMB-OUT, COULD NOT CONTROL CABIN PRESSURE IN EITHER AUTO OR MANUAL MODE. MAINTENANCE INSPECTED STATIC LINES ON OUTFLOW VALVE AND CONTROLLER FOR SECURITY. ALSO, INSPECTED THE AIR FILTER. NO DEFECTS NOTED. 2L72 4T RTT00011AT 20051208001622005120800162SO 2005 12 8 LR7A05196 120051031A5312 BULKHEAD LKHEED382 382G 526414USO BS 1012 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 639 4698 DURING B-2 CHECK FOUND BULKHEAD CRACKED 2 INCHES SPANWISE ORIGINATING AT STANDOFF ATTTACHMENT AT FS 1012, WL282, LBL5. REPAIRED WEB IAW SMP583 FIG 51-140-17, NR 2004. 2H74 4T A1SO 20051208001632005120800163SO 2005 12 8 MASA200500482 120050623A2710 AILERON EMB 145 EMB145LR 3260212SO UNKNOWN A MASAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 SW07846MJ 145507 ASH 2641 CLT, THE CAPTAIN ABORTED TAKEOFF AND RETURNED TO THE GATE WHEN THE AILERONS FELT LIKE THEY WERE BINDING. INITIAL REPORT FROM MX IS SMOOTH OPERATION. MAINTENANCE PERFORMED A HIGHLY DETAILED INSPECTION OF THE AILERON SYSTEM. NO DEFECTS WERE NOTED. REFER TO MASA200500509. 2L72 4T RTT00011AT 20051208001642005120800164NM 2005 12 8 05FDEA04084 120051202A5753 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 LEFT WING OUTBOARD FLAP INBOARD FORWARD HINGE BRACKET AFT UPPER LINK FOUND CRACKED. COMPLIED WITH FEDEX EA 1-5750-90703 (TITLE: WINGS LEFT HAND WING TRAILING EDGE FLAP, INBOARD HINGE, TENSION STRAP - COMPLIANCE WITH BOEING S/B 57- 10). REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20051208001652005120800165NM 2005 12 8 05FDEA04085 120051203A5753 FLAP TRACK BOEING727 727227 1384078NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 LEFT WING INBOARD FLAP OUTBOARD TRACK FORWARD MOUNT HOLES (BORES) HAVE CORROSION. REMOVED CORROSION BY REAMING BORES C, D AND E. MAGNETIC PAR- TICLE INSPECTION AND FABRICATED BUSHINGS FOR BORES C, D AND E IAW FEDEX EA NR 7-5710-92592. ALSO, HEAT TREATED, CAD PLATED INSTALLED AND REAMED BUSHINGS IAW FEDEX E7-5710-92592. THIS IS A MINOR REPAIR REFERENCE FEDEX SNRM N00727, SIGNED BY TIMCO MECH NR 1281 AND QC300. 2L73 4F A3WE 20051208001662005120800166NM 2005 12 8 AWXA200501483 120051202A3150 WARNING LIGHT BOEING737 7373G7 1384595NM UNKNOWN ILLUMINATED A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28156AW 23778 PHX - ABORTED TAKEOFF - FLT 621 - CREW ABORTED TAKEOFF DUE TO UNSPECIFIED INDICATOR WARNING LIGHT. TAXIED BACK AND DEPARTED NORMALLY SEVERAL MINUTES LATER. RECEIVED VERBAL CONFIRMATION FROM SAFETY REPORTING GROUP THAT SPOKE WITH CAPTAIN. CAPTAIN CONFIRMED THAT THE AIRCRAFT WAS CONFIGURED CORRECTLY WHEN RECEIVED TAKE OFF CONFIG HORN AFTER ADVANCING THROTTLES, HAD NOT HIT TAKE OFF POWER YET. TAXIED OFF THE RUNWAY AND CYCLED THE SPOILERS. CREW ATTEMPTED TAKE OFF AGAIN AND IT WAS SUCCESSFUL. 2L72 4F RTA16WE 20051208001672005120800167SO 2005 12 8 MASA200500767 120051004A2720NAS620413 BOLT EMB 145 EMB145LR 3260212SO ATTACH FITTING LOOSE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07830MJ 145259 BNA - RUDDER MAKES POPPING NOISE DURING BACKLASH CHECKS, FOUND 3 EA ATTACH FITTINGS BOLTS LOOSE AT LOWER RUDDER TO STAB SUPPORT. MAINTENANCE REMOVED AND REPLACED BOLT WASHER NUT. 2L72 4T RTT00011AT 20051208001682005120800168SO 2005 12 8 LR7A05171 120051109A532033050202 CAP LKHEED382 382G 526414USO FS 245E CORRODED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2549 4606 DURING C-7 CHECK PER HC5313, FOUND FWD RT CHINE CAP CORRODED BEYOND LIMITS, FS 245E-345E. REPLACED CHINE CAP IAW DRG 3305020 AND SMP 581 CH 90, NR 0105. 2H74 4T A1SO 20051208001692005120800169SO 2005 12 8 LR7A05172 120051109A5320 CHANNEL LKHEED382 382G 526414USO FS 345E DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2549 4606 DURING C-7 CHECK PER HC5302, FOUND DAMAGED CHANNEL IN RT FLOOR PANEL BETWEEN FS 345E AND FS 417. REPAIRED CHANNEL BY SPLICING IAW DRG R05-28-01, MEA 382-53-05-087, NR 0154. 2H74 4T A1SO 20051208001712005120800171SO 2005 12 8 LR7A05174 120051109A5312 BULKHEAD LKHEED382 382G 526414USO FS 597 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2549 4606 DURING C-7 CHECK PER HSP57170, FOUND RT CW REAR WEB CRACKED TWO PLACES, 4MM AT FASTENER HOLE RT CWS76, WL262, FS597 AND 5MM AT FASTERNER HOLE CWS73, WL259, FS597. REPAIRED WEB IAW ED05-028-4 AND SMP 583 FIG 57-30-22, MEA 382-57-05-085, NR 0260. 2H74 4T A1SO 20051208001732005120800173SO 2005 12 8 LR7A05176 120051109A5343 BEAM LKHEED382 382G 526414USO FS597 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2549 4606 DURING C-7 CHECK PER HC5324, FOUND RT MLG BEAM CRACKED 2 INCHES FROM TOP FASTENER HOLE PROGRESSING INBOARD AND SLIGHTLY UPWARD TO INBOARD EDGE OF BEAM WEB FS 597, WL146, RBL64. REPAIRED IAW ED05-028-3 AND SMP 583 FIG 53-40-31, MEA 382-53-05-084, NR 0287. 2H74 4T A1SO 20051208001752005120800175EU 2005 12 8 05FDEA04113 120051204A5753A5724783000300 BLOCK AIRBUS310 A310203 3930313EU FLAPS ICED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25429FE 364 DURING FLAP RETRACTION RECEIVED ECAM WARNING FLAP 2 FAULT, FLAP VANE JAM, FLAPS RETRACTION LIMITED, THIS ALL OCCURRED WHEN FLAP HANDLE WAS MOVED FROM 15/0 TO 0/0. FLAPS INDICATED UP, WITH NO VIBRATIONS IN FLIGHT CONTROLS. REMOVED AND REPLACED RT INBD FLAP, RT INBD FLAP VANE BUFFER IAW AMM 27-56-15-4. INSPECTED FLAP VANE AND FOUND AN EXCESSIVE AMOUNT OF ICE BUILT UP ON THE VANE FITTINGS. THAWED FLAP AND VANE, OP'S CK GOOD. ALL FAULTS CLEARED. NO BINDING OR JAMMING NOTED ON FLAP VANE. 2L72 4F RTA35EU 20051208001772005120800177NM 2005 12 8 05FDEA04115 120051204A7710 O-RING BOEING727 7272S2F 1384O81NM ENGINE DAMAGED A FDEAC ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 SO25217FE 22938 REJECTED FIRST T/O DUE TO ENG FAIL LIGHT ON, NR 3 ENG ADV UP TO RED LINE N1 BUT EPR WAS STILL VERY LOW TO CONTINUE T/O, PILOT SAID ENG RED LINE NI WAS NOT EXCEEDED, REMOVED NR 3 ENG BULLET, PRESS TESTED THAT SECTION OF PT2 LINE, CHKS GOOD. FOUND THE TWO O-RINGS ON THE PT2 COUPLER IN THE BULLET DRYROTTED, CRACKING, AND OF THE WRONG TYPE. REMOVED AND REPLACED TWO "HIGH TEMP" O-RINGS, AND INSTALLED BULLET, PRESS TESTED PT7, AND THE REM. PT2 LINES FROM THE TRANS TO THE ENG, FOUND PT2 LINE LEAKING AT THE FLYING WING TO FUSE CONN, DISCONN, AND INST THAT CONN, LK CHECKS GOOD. RAN NR 1 AND NR 3 ENG AT HIGH PWR PER 727-200JRH, NR 3 EPR OPS CHKS GOOD, ALL NR 1 AND NR 3 NORM. 2L73 4F A3WE 20051208001792005120800179NM 2005 12 8 05FDEA04117 120051204A5280 DOOR DOUG MD11 MD11 3023602NM ZONE 700 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 FOUND LEFT HAND MAIN LANDING GEAR FLIPPER DOOR FORWARD HINGE FOUND WITH A CRACKED APPROXIMATELY 1.0" IN LENGTH. REPAIR CARRIED OUT AT LEFT HAND MAIN LANDING GEAR FLIPPER DOOR FORWARD HINGE CRACKED AREA AS PER SRM 52-10-00 FIGURE 18 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051208001812005120800181NM 2005 12 8 05FDEA04119 120051204A5320 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 FOUND FORWARD CARGO STATION 1129 L52 FOUND CRACKED. CARRIED OUT REPAIR AT CRACKED LONGERON 52 LOCATED AT FORWARD CARGO STATION 1129 AS PER SRM 53-10-00 FIGURE 1 VOLUME I. 2L73 4F RTA22WE 20051208001832005120800183WP 2005 12 8 05FDEA04121 120051205A5330 REPAIR DOUG DC10 DC1010 3022110WP FUSELAGE UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LWR FUS ON SKIN FOUND REPAIR DOUBLER BTW STA 1219 AND 1289 FROM LONG 51 RT TO LONG 51 LT. REMOVED EXISTING DOUBLER IAW SRM 51-35-01 PAR 1-5 STRIPPED PAINT FROM AREA IAW SRM 51-21-01 VOL 2. INSPECTION AREA IAW NDI INSTALLED CONICAL WASHER AND INSTALL NEW DOUBLER IAW EA 8-5330-93219 AND INSTALLED SHEAR CLIP P/N F14383/9 IAW SRM 53-30-00 FIG 9 VOL 1. 2L73 4F A22WE 20051208001852005120800185NM 2005 12 8 05FDEA04123 120051205A5753 HINGE FITTING DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 FOUND RIGHT WING OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING FOUND CORROSION AT INBOARD NR 2 BOLT HOLE. REFER TO SNRM NR N00830 FOR RIGHT HAND WING OUTBOARD FLAP REPLACEMENT. 2L73 4F RTA22WE 20051208001862005120800186EA 2005 12 8 SWIA200515929 120051130A2797 WIRE CNDAIRCL600 CL6002C10 1390015EA SENSOR BROKEN A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07701SK 10133 SLAT FAULT STATUS MESSAGE. REPAIRED SPLICE MT86 AT LT INBD SKEW SENSOR IAW WDM 20-44-00. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051208001872005120800187EA 2005 12 8 SWIA200515930 120051203A3350 LIGHT CNDAIRCL600 CL6002C10 1390015EA CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07706SK 10149 EMERGENCY LIGHT OVERHEAD NEAR ROW 9 IN PAX CABIN INOP. REPLACED EMERGENCY OVERHEAD LIGHT IAW CRJ MM 33-51-15. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051208001882005120800188EA 2005 12 8 SWIA200515931 120051130A3350 BULB CNDAIRCL600 CL6002C10 1390015EA EMEREGENCY LIGHTINOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07748SK 10203 3 OF THE 5 EMERGENCY EXIT FLOOD LIGHTS ARE INOPERATIVE AT GALLEY SERVICE DOOR. REPLACED FLOOR LEVEL EMERGENCY FLOOR LIGHT ASSEMBLY AND BULBS IAW AMM 33-51-11. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051208001902005120800190SO 2005 12 8 SWIA200515933 120051201A27523431001001 ACTUATOR EMB 120 EMB120ER 3260203SO NACELLE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 NM07295SW1010210042 120322 MULTIPLE CONTROL FAULTS ON APPROACH TO SEA. REPLACED RT NACELLE FLAP ACTUATOR IAW MM 27-50-08. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20051208001922005120800192EA 2005 12 8 QXEA200501596 120051129A2760 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA SPOILERS ILLUMINATED A QXEAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM09603QX 10011 BUR - ON TAXI OUT FOR FLIGHT 2459, A SPOILER STAB MESSAGE ILLUMINATED. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE PURGED MOISTURE FROM THE PITOT STATIC SYSTEM. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2L72 4F RTA21EA 20051206000542005120600054EA 2005 12 6 COMA0560638 120051123A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01526CA 7824 FLIGHT 5701- FLAPS FAIL CAUTION. INSPECTED FLAPS PER AD 98-20-01. NO DEFECTS FOUND. 2L72 4F RTA21EA 20051206000572005120600057EA 2005 12 6 COMA0560654 120051127A32604622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG UNRELIABLE A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01983CA195657999 7169 FLIGHT 5100 - GEAR DISAGREE WARNING. REPLACED THE NLG PRIORITY VALVE. 2L72 4F RTA21EA 20051206000692005120600069NM 2005 12 6 DHL2005749009 120051031A5753 SKIN BOEING727 7272J0 138407ENM TE FLAP DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01749DH 22013 FOUND LT WING I/B AFT FLAP DENTED AT LWR SURFACE. CUT OUT DENTED AREA APPROX 3 INCHES. DIA AT LT INB AFT FLAP LWR SURFACE FABBED FILLER APPROX 3" DIA AND DOUBLER APPROX 6" DIA FROM .016" 2024-T3 PO NR 9002556 BONDED FILLER AND DOUBLER SEALED AND PRIMED IAW B277 SRM 57-50-1 FIG 3 AND 51-40-20 FIG 1. 2L73 4F RTA3WE 20051206000742005120600074NM 2005 12 6 DHL2005749004 120051030A5522 SKIN BOEING727 7272J0 138407ENM LT ELEVATOR DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01749DH 22013 FOUND LEFT ELEVATOR LOWER SURFACE DENTED 40" I/B FROM O/B TIP. REMOVED LT ELEVATOR LOWER SKIN PANEL AT ELEV STA 173.21 IAW B727 SRM 51-30-2 FIG 9 LOCATED AND DRILLED FASTENERS HOLES IN NEW PANEL ASSY P/N 65-25639-75 PO NR 540027 IAW B727 SRM 51-30-2 FIG 1. TREATED AND PRIMED PANEL IAW B727 SRM 51-10-2. INSTALLED NEW PANEL AT LT ELEVATOR LOWER SKIN AREA IAE B727 SRM 51-30-2 FIG 8. 2L73 4F RTA3WE 20051206000772005120600077NM 2005 12 6 USAA051452 120051201A5520 REPAIR BOEING737 737301 1384611NM RT ELEVATOR UNKNOWN A USAAK NONE O OTHER ININSP/MAINT 1 EA19591US 23936 FOUND COMPOSITE REPAIR LOWER SURFACEOF RT ELEVATOR, 26.5" OTBD OF INBD END 3" FWD OF THE T/E. COMPOSITE REPAIR IAW 55-40-01. DEFECT SIZE: COMPOISTE REPAIR AT LOWER SURFACE OF RT ELEVATOR, 26.5" OTBD OF INBD END 3" FWD. 2L72 4F RTA16WE 20051206000782005120600078NM 2005 12 6 USAA051442 120051201A5712 RIB BOEING737 7374B7 1384702NM LT WING AILRON GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19780AU 24997 FOUND AILERON NOSE RIB GOUGED LT WING OUTBD HINGE OUTBD SIDE LWR SURFACE. REPLACED, FABRICATED NOSE RIB IN LT AILERON PER SRM 51-40-02, DEFECT SIZE: .75"L X .375"W. 2L72 4F RTA16WE 20051206000822005120600082EA 2005 12 6 SWIA200515910 120051126A27505912999 SENSOR CNDAIRCL600 CL6002C10 1390015EA BRAKE POSITION MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07703SK4433 4433 10139 "SLATS FAIL" MSG ON POWER-UP. REPLACED RT SENSOR, BRAKE POSITION UNIT IAW CRJ 700 MM 27-52-03. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051206001062005120600106NM 2005 12 6 QXEA200501598 120051129A3040 WARNING LIGHT DHAV DHC8 DHC8202 2809007NM WINDSHIELD FALSE ACTIVATIONA QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09359PH 514 SEA FLIGHT NR 2084 ON TAXI OUT, LEFT WINDSHIELD CAUTION LIGHT ILLUMINATED. RAN CHECKLIST AND LIGHT EXTINGUISHED. ADVISED BY MAINTENANCE CONTROL TO RETURN TO GATE. MAINTENANCE COMPLIED WITH OPERATIONAL CHECK OF PILOTS AND COPILOTS WINDSHIELD HEAT SYSTEM IAW DASH8 200 AMM 30-41-00-710-801. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051206001072005120600107NM 2005 12 6 05FDEA04011 120051129A5315 FLOORBEAM BOEING727 727227 1384078NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 FORWARD CARGO COMPARTMENT STA BS 560, BOTTOM OF FLOORBEAM HAS CORROSION BETWEEN RBL10 AND LBL40. REMOVED DAMAGE, FABRICATED 2 EACH REPAIR ANGLES, AND 1 EACH FILLER, AND 1 EACH LOWER STRAP IAW B727 SRM 53-10-8 FIGURE 2 ALODINED AND PRIMED REPAIR PARTS IAW B727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B727 SRM 51-30-2. 2L73 4F A3WE 20051206001112005120600111NM 2005 12 6 05FDEA04015 120051129A5330 REPAIR BOEING727 727227 1384078NM ZONE 100 IMPROPER A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25486FE 21489 REPAIR LOCATED AT STA 1148 STR 30 REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA ITEM NR 17. ORIGINAL DOUBLER WAS NOT DONE USING THE B727 SRM 53-30-3 FIGURE 1. REMOVED DOUBLER IAW B727 SRM 51-30-2. FABRICATED A NEW DOUBLER IAW B727 SRM 53-30-3 FIGURE 1. ALODINED AND PRIMED DOUBLER IAW B727 SRM 51-10-2. INSTALLED DOUBLER IAW B727 SRM 53-30-3 FIGURE 1. THIS IS A MAJOR REPAIR SIGNED BY TIMCO MECH NR 6180 AND QC261. 2L73 4F A3WE 20051206001222005120600122SO 2005 12 6 SIMA200531506 120051101A5530 BEARING EMB 135 EMB135KL 3260302SO VERTICAL STAB CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21822AE 145581 FOUND VERTICAL STABILIZER SPHERICAL BEARINGS CORRODED. REPLACED BOTH VERTICAL STABILIZER SPHERICAL BEARINGS IAW EMB AMM 55-37-00. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20051206001302005120600130EU 2005 12 6 SIMA200530001 120051024A2120 ODOR SAAB SF340 340B 7860101EU COCKPIT DETECTED A SIMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21301AE 340B301 FOUND CREW REPORTED STRONG SMOKE SMELL IN COCKPIT AND FORWARD CABIN. FOLLOWED CHECKLIST AND COULD NOT DETERMINE SOURCE. INSPECTED AVIONICS RACK AIR DISTRIBUTION SYSTEM. PERFORMED OPERATIONAL CHECK OF THE BLEED AND AIR DISTRIBUTION SYSTEM WITH NO DISCREPANCIES NOTED. A/C RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 20051206001332005120600133SO 2005 12 6 SIMA200531503 120051101A534713500439007 SEAT TRACK EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21822AE 145581 FOUND LEFT FORWARD INBOARD SEAT TRACK CORRODED. REPLACED SEAT TRACK IAW EMB 140 AMM 53-01-06. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20051206001542005120600154NM 2005 12 6 ASAA0510316 120050921A5320656210040 FLOOR SUPPORT BOEING737 737290C 138448VNM FS 312-344 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02740AS 22578 YXX - FOUND CORROSION AT 5 CLIP NUT LOCATIONS ON FLOOR SUPPORT STRUCTURE LOCATED AT LBL 40, WL 207, BS 312-344. FLOOR SUPPORT CHORD REPAIRED BY REPLACEMENT PER B737-200 SRM 51-30-2. (M) 2L72 4F A16WE 20051206001612005120600161NM 2005 12 6 ASAA0510304 120050920A53136545800204 STRINGER BOEING737 737290C 138448VNM FOM CUT A ASAAK NONE O OTHER ININSP/MAINT 1 NM02740AS 22578 YXX - FOUND STRINGER 26L AT BS 334 TO BS 358 CUT. REPAIRED PER B737-200 SRM 53-10-3 FIGURE 1. (M) 2L72 4F A16WE 20051206001622005120600162NM 2005 12 6 ASAA0510309 120050920A531565549057 FLOORBEAM BOEING737 737290C 138448VNM FS 420 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02740AS 22578 YXX - FOUND IN FORWARD CARGO PIT LOWER CHORD OF FLOORBEAM CORRODED AT BS 420 LBL 24. LOWER CHORD OF CABIN FLOORBEAM AT BS 420 LBL 24 WAS REPAIRED IAW ERO 4457 AND EA 53110-02491. REF ASA LOG 3017604 FOR WORK DETAILS. (M) 2L72 4F A16WE 20051206001632005120600163NM 2005 12 6 ASAA0510307 120050920A5322655496076 ATTACH ANGLE BOEING737 737290C 138448VNM FS 360 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02740AS 22578 YXX - FOUND CORROSION ON SKIN TO FRAME ATTACH ANGLE BETWEEN STRINGER 28-27 LEFT AT BS 360. SKIN TO FRAME ATTACH ANGLE AT BS 360 BETWEEN STRINGER 27 LEFT AND 28 LEFT REPAIRED PER B737-200 SRM 53-10-4 FIGURE 8. (M) 2L72 4F A16WE 20051206001652005120600165NM 2005 12 6 ASAA0510314 120050920A5315654581577 FLOORBEAM BOEING737 737290C 138448VNM FS 344 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02740AS 22578 YXX - FOUND UPPER CHORD OF BS 344 FLOORBEAM CORRODED FROM RBL 5-10, UNDER FASTENER HEADS AND ON SURFACE. REMOVED AND REPLACED UPPER CHORD PER B737-200 SRM 53-10-9. (M) 2L72 4F A16WE 20051208000022005120800002NM 2005 12 8 05FDEA03998 120051128A5330 SKIN BOEING727 727200 138407ENM BS 1170 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 N00222 BS 1170 STR. 23-24L DENT IN SKIN ** SD ** COMING DENT ON SKIN WAS FOUND TO BE OUT OF LIMITS, REPAIRED DENT ON SKIN AT BS 1170, STR 23L-24L, IAW SRM 53-30-3. 2L73 4F RTA3WE 20051208000092005120800009EU 2005 12 8 DHL2005362AA1 120051204A5753A579600500200 RIB AIRBUS300 A300B4203 3930306EU TE FLAP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01362DH 84 DURING "A" CHECK ACCOMPLISHED INSPECTION OF RT WING INBD. FLAP NOSE RIB NR 7 ON FLAP ASSY. S/N FD 1074 PER S/B A-300-59-240. REMOVED AND REPLACED RIB RN 7 RT AT RT INB. FLAP IAW S/B A-300-57-0240. 2L72 4F RTA35EU 20051208000422005120800042CE 2005 12 8 DXTA200501126 120051203A2170 COALESCER BAG CESSNA650 650 2076802CE CABIN AIR CONTAMINATED E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL07790QS 6507090 HOT OIL SMELL CAME INTO CABIN DURING CLIMB. INDICATED AIRSPEED 215 KNOTS, CLIMBING 100 FT PER MINUTE THRU 41,700 FT. ALL INDICATIONS NORMAL (OIL, HYDRAULIC AND ELECTRICAL). INSPECTED ENGINE, APU, AND ACM OIL LEVELS. ALL INDICATE FULL. REMOVED PLUMBING FROM ACM TURBINE. NO OIL NOTED. CLEANED PLUMBING AND REINSTALLED. REMOVED COALESCER SOCKS AND FOUND VERY DIRTY. CLEANED SOCKS AND REINSTALLED. OPERATED APU FOR 1 HOUR WITH BLEEDS ON. NO DEFECTS NOTED. OPERATED BOTH ENGINES AT DIFFERENT POWER SETTINGS FOR 30 MINUTES. NO DEFECTS NOTED. WORK ACCOMPLISHED PER CESSNA 650 MM 21-50-02, 21-60-00. OPS CHECK GOOD. 2L72 4F A9NM 20051208001012005120800101EA 2005 12 8 COMA0560668 120051203A2752853D10019 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS UNRELIABLE A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01806CA 7359 FLIGHT 5764- FLAPS FAIL CAUTION. REPLACED THE LT NR 3 ACTUATOR. 2L72 4F RTA21EA 20051208001282005120800128SO 2005 12 8 MASA200500701 120050727A2120BWT138001 DUCT EMB 145 EMB145LR 3260212SO NR 2 PACK SCHEDULED MAINT A MASAK NONE O OTHER ININSP/MAINT 1 SW07834MJ 145340 DURING OVERNIGHT MAINTENANCE, A NR 2 PACK DUCT WAS REPLACED THROUGH A FLEET CAMPAIGN DIRECTIVE (FCD). 2L72 4T RTT00011AT 20051208001312005120800131SO 2005 12 8 MASA200500704 120050804A2120BWT138001 DUCT EMB 145 EMB145LR 3260212SO NR 2 PACK DAMAGED A MASAK NONE O OTHER ININSP/MAINT 1 SW07838MJ 145384 DURING OVERNIGHT MAINTENANCE, THE NR 1 AND NR 2 DUCTS WERE FOUND DAMAGED. MAINTENANCE REPLACED BOTH THROUGH A FLEET CAMPAIGN DIRECTIVE (FCD). 2L72 4T RTT00011AT 20051208001332005120800133SO 2005 12 8 MASA200500706 120050803A2120BWT138001 FLEX DUCT EMB 145 EMB145LR 3260212SO NR 2 PACK UNKNOWN A MASAK NONE O OTHER ININSP/MAINT 1 SW07841MJ 145448 DURING OVERNIGHT MAINTENANCE, A NR 2 PACK DUCT WAS REPLACED THROUGH A FLEET CAMPAIGN DIRECTIVE (FCD). 2L72 4T RTT00011AT 20051208001352005120800135EA 2005 12 8 QXEA200501623 120051031A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA FUSELAGE GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, FUSELAGE SKIN UNDER FAIRING PANEL 195DL IS GOUGED FROM ATTACH SCREW END. MAINTENANCE BLENDED DAMAGED AREA IAW REO 670-53-00-014 .030" REMOVED. REPLACED FASTENER. RESTORED FINISH. 2L72 4F RTA21EA 20051208001362005120800136SO 2005 12 8 MASA200500708 120050810A2120BWT138001 FLEX DUCT EMB 145 EMB145LR 3260212SO UNKNOWN A MASAK NONE O OTHER ININSP/MAINT 1 SW07852MJ 145567 DURING OVERNIGHT MAINTENANCE, BOTH DUCTS WERE REPLACED THROUGH A FLEET CAMPAIGN DIRECTIVE (FCD). 2L72 4T RTT00011AT 20051208001372005120800137SO 2005 12 8 MASA200500709 120050728A2120BWT138001 FLEX DUCT EMB 145 EMB145LR 3260212SO NR 2 PACK TORN A MASAK NONE O OTHER ININSP/MAINT 1 SW07858MJ 145767 DURING OVERNIGHT MAINTENANCE A NR 2 PACK WAS FOUND RIPPED. MAINTENANCE REPLACED THE DUCT THROUGH A FLEET CAMPAIGN DIRECTIVE (FCD). 2L72 4T RTT00011AT 20051208001382005120800138EU 2005 12 8 AWXA200501478 120051130A5230 HANDLE AIRBUS320 A320231 3930325EU CARGO DOOR UNSECURE A AWXAC ABORTED TAKEOFF WJ INADEQUATE Q C WARNING INDICATION TOTAKEOFF 1 WP28629AW 076 FLT 859 - DURING TAKEOFF, CREW RECEIVED AFT CARGO DOOR CLASS 1 MAINTENANCE MESSAGE. ABORTED TAKEOFF AT 60 KNOTS. RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE RE-SECURED AFT CARGO DOOR HANDLE, FOUND HANDLE NOT COMPLETELY IN DETENT. OPERATIONAL CHECKS GOOD. 2L72 4F RTA28NM 20051208001392005120800139EU 2005 12 8 AWXA200501479 120051201A3230 LANDING GEAR AIRBUS320 A320232 3930326EU MLG VIBRATION A AWXAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 WP28663AW 1419 PHX - EMERGENCY LANDING - FLT 529 - AFTER TAKEOFF FROM TPA, CREW REPORTED THAT DURING GEAR RETRACTION FELT A SEVERE VIBRATION WITH THE GEAR BEING SLOW TO RETRACT. VIBRATION STOPPED ONCE GEAR WAS IN WHEEL WELL. MADE EMERGENCY LANDING IN PHX WITHOUT FURTHER INCIDENT, AFTER TOWER FLYBY, AND TAXIED TO THE GATE. MAINTENANCE CYCLED GEAR NUMEROUS TIMES IAW AMERICA WEST AIRLINES TASK CARD F4M32301 WITH NO DEFECTS BEING NOTED. PREFORMED VISUAL INSPECTION ON ALL GEARS IAW AIRBUS 320 TSM 32-31-00-810-855 WITH NO DEFECTS BEING NOTED. LUBRICATED MLG AND NLG IAW AIRBUS 320 MM 12-22-32. OPERATIONAL CHECKS WERE GOOD, RETURNED TO SERVICE. 2L72 4F RTA28NM 20051208001402005120800140NM 2005 12 8 QXEA200501731 120051201A2750C1486742003 CONTROL UNIT BOMBDRDHC8 DHC8402 1390042NM TE FLAPS MALFUNCTIONED A QXEAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 NM09412QX9731 4059 PDX FLIGHT NR 2356, INTERMITTENT FLAP DRIVE CAUTION LIGHT AFTER FLAPS SELECTED TO 15 DEGREES. WIGGLING FLAP SEEMED TO REDUCE THE NUMBER OF TIMES CAUTION LIGHT CAME ON. MAINTENANCE REMOVED AND REPLACED FLAP CONTROL MODULE IAW 27-51-06-000-801 AND 27-51-06-400-801. OPS CHECK GOOD. NO FAULTS PRESENT. RII COMPLIED WITH. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051208001412005120800141EA 2005 12 8 COMA0560669 120051204A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS WARNING LIGHT A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01937CA 7044 FLIGHT 5435- FLAPS FAIL CAUTION. INSPECTED FLAPS IAW AD 98-20-01, NO DEFECTS FOUND. 2L72 4F RTA21EA 20051208001932005120800193NM 2005 12 8 QXEA200501745 120051202A2750C1486561 PDU BOMBDRDHC8 DHC8402 1390042NM TE FLAPS FAILED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09412QX9736 4059 PDX FLIGHT NR 2352: ON APPLICATION OF TAKEOFF, JUST ABOVE THE FLIGHT IDLE GATE, THE "FLAP DRIVE" CAUTION LIGHT BEGAN INTERMITTENTLY FLASHING AND CONTINUED UNTIL CLEARING THE RUNWAY. MAINTENANCE INTERROGATED CDS. NO FAULTS LOGGED. OPERATED FLAP SYSTEM INTERMITTENTLY. DUPLICATED FAULT. REMOVED AND REPLACED THE FLAP POWER UNIT IAW Q400 AMM TASK 27-52-01-000-801 AND 27-52-10-400-801. FUNCTIONAL TEST GOOD. NO LEAKS OR FAULTS NOTED. NO FURTHER DEFECTS NOTED. BLED NR 1 HYD SYSTEM. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051208001982005120800198NM 2005 12 8 SWAA053840 120051202A53306545766 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 465, STR 16R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051208002002005120800200NM 2005 12 8 SWAA053842 120051202A573065C29255 SKIN BOEING737 7373H4 1384600NM LT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED 1/4D CHECK, FOUND LT WING UPPER SKIN CRACKED AT WBL 157.00, REAR SPAR UPPER CHORD. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051208002022005120800202NM 2005 12 8 SWAA053844 120051202A3350MS155721 BULB BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED 1/4D CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20051208002042005120800204NM 2005 12 8 SWAA053846 120051202A575465C26602 SKIN BOEING737 7373H4 1384600NM RT WING SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED 1/4D CHECK, FOUND RT WING NR 5 L/E SLAT DELAMINATED. REMOVED AND REPLACED SLAT PER MM. 2L72 4F RTA16WE 20051208002062005120800206NM 2005 12 8 SWAA053848 120051130A33506042221 LIGHT BOEING737 7377H4 1384404NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29427WN 29831 FWD LOWER EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT PER MM. 2L72 4F RTA16WE 20051208002082005120800208NM 2005 12 8 SWAA053850 120051202A335007912 COVER BOEING737 7377H4 1384404NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29479WN 33990 DURING SCHEDULED HC2 CHECK, FOUND EEPLS TRACK COVER BROKEN AT ROW 13 ABC. REMOVED AND REPLACED COVER PER MM. 2L72 4F RTA16WE 20051208002102005120800210EU 2005 12 8 05FDEA04111 120051204A5320 ANGLE AIRBUS300 A300B4622R 3930312EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25721FD 477 FWD CARGO COMPT BELOW ROLLER TRAY SUPPORT ANGLE EXFOLIATED 1" FWD OF FRAME C33 RBL 56". REMOVED AND REPLACED ANGLE SUPPORT IAW SRM 51-40-2. FABRICATED SUPPORT ANGLES (2 EACH) PER MAE TRAVELER T5/559357 AND T5/560339. FABRICATED WED (SHEAR WALL) T5/560340 LOCATED AND DRILLED IAW SRM 51040-44, PREP'D AND PAINTED AREA IAW SRM 51-75-10. 2L72 4F RTA35EU 20051208002122005120800212EA 2005 12 8 QXEA200501621 120051031A5343 ATTACH FITTING CNDAIRCL600 CL6002C10 1390015EA MLG WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, RIGHT MAIN GEAR SIDE STAY HAS PLAY AT THE LOWER ATTACH POINT TO THE MLG AND AT THE UPPER SIDE STAY TO AIRFRAME ATTACH POINTS. MAINTENANCE FOUND PLAY TO BE WITHIN LIMITS IAW EA R-32-201 AND REO 670-32-11-023. 2L72 4F RTA21EA 20051208002132005120800213SO 2005 12 8 LR7A05179 120051109A5330 SKIN LKHEED382 382G 526414USO FS 707 DENTED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2549 4606 DURING C-7 CHECK PER HC5321, FOUND FUSELAGE LOWER EXT SKIN SURFACE DENTED, FS 707, LBL5, WL126. REPAIRED SKIN SURFACE IAW SMP 583 FIG 51-140-12, NR 0401. 2H74 4T A1SO 20051209000022005120900002NM 2005 12 9 QXEA200501576 120051110A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX - NR 2 SEAT TRACK HAS LIGHT SURFACE CORROSION ON TOP OF LUGS AT X438-440, X471, X501. REPAIRED IAW RD 8-53-1342, DHC-8-202 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20051209000032005120900003NM 2005 12 9 QXEA200501577 120051110A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX - NR 2 SEAT TRACK HAS CORROSION IN BOTTOM OF CHANNEL AT X436. REPAIRED IAW RD 8-53-1342, DHC-8-202 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20051209000062005120900006NM 2005 12 9 UPS05245860 120051013A7120NAS7514019 BUSHING BOEING727 72730C 1384009NM NR 3 AFT MOUNT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 INSPECTION TYPE:C ENGINE NR 3 AFT MOUNT FITTING HAS CORROSION ON INNER SURFACE OF UPPER USHING. REPLACE BUSHING. REPLACED BUSHING IAW OHM 20-50-03. 2L73 4F A3WE 20051209000082005120900008NM 2005 12 9 UPS05245863 120051206A3350 LIGHT BOEING727 72725C 138400HNM OVER PAX DOOR INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01932UP 19856 EMERGENCY EXIT LT OVER FWD ENTRY DOOR DOES NOT ILLUMINATE. REPLACED EMERGENCY EXIT BATTERIES. OPS CK NORMAL PER AMM 33-50-67-2. 2L73 4F A3WE 20051209000092005120900009NM 2005 12 9 UPS05445854 120051206A712065B903604 LINK BOEING747 747283B 1384867NM NR 1 MOUNT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 NR 1 ENGINE REAR MOUNT THRUST LINK FWD END LUG BORE UPPER AND LOWER AREA WITH CRACK INDICATION 60 PERCENT FSH AND 80 PERCENT FSH RESPECTIVELY. WHICH EXCEED LIMIT. NR 1 ENGINE REAR MOUNT THRUST LINK REPLACED PER 747 MM 71-21-03 REF EO NR B747-7120-22596 APPENDIX F. 2L74 4F A20WE 20051209000102005120900010NM 2005 12 9 UPS05445855 120051206A712065B903604 LINK BOEING747 747283B 1384867NM NR 2 MOUNT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 NR 2 ENGINE REAR MOUNT THRUST LINK AFT END LUG BORE LOWER AREA WITH CRACK INDICATION 70 PERCEMT FSH WHICH EXCEED LIMIT. NR 2 ENGINE REAR MOUNT THRUST LINK REPLACED PER 747 MM 71-21-03 REF EO NR B747-7120-22596 APPENDIX G. 2L74 4F A20WE 20051209000112005120900011NM 2005 12 9 UPS05445856 120051206A712065B903604 LINK BOEING747 747283B 1384867NM NR 3 MOUNT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 NR 3 ENGINE REAR MOUNT THRUST LINK FWD END LUG BORE UPPER AREA WITH CRACK INDICATION (90 PERCENT FSH ); AND AFT END LUG BORE UPPER AND LOWER AREA WITH CRACK INDICATION 60 PERCENT FSH AND 110 PERCENT FSH RESPECTIVELY. ALL EXCEED LIMIT. NR 3 ENGINE REAR MOUNT THRUST LINK REPLACED PER 747 MM 71-21-03, REF EO NR B747-7120-22596 APPENDIX H. 2L74 4F A20WE 20051209000122005120900012NM 2005 12 9 UPS05445857 120051206A712065B903604 LINK BOEING747 747283B 1384867NM NR 4 MOUNT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 NR 4 ENGINE REAR MOUNT THRUST LINK FWD END LUG BORE LOWER AREA WITH CRACK INDICATION ( > 126 PERCENT FSH ) WHICH EXCEED LIMIT. NR 4 ENGINE REAR MOUNT THRUST LINK REPLACED PER 747 MM 71-21-03, REF EO NR B747-7120-22596-C APPENDIX I. 2L74 4F A20WE 20051209000132005120900013WP 2005 12 9 UPS05845853 120051206A5610DC871MN WINDOW DOUG DC8 DC873F 302199FWP COCKPIT JAMMED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01852UP 46052 CAPT SLIDING WINDOW W/NOT OPEN. PER IMPACTS A/C STATUS SLIDING WINDOW JAMMED AND OVER CTR MECHANISM IS WORN TO A POINT OF CAUSING JAM PROBLEM. REMOVED AND REPLACED CAPT CLEARVIEW WINDOW ASSY IAW 56-10-03-4. ALTERNATE P/N USED PER EO DC8-5610-23421-A. WINDOW OPENS NOW. 2L74 4F RT4A25 20051209000152005120900015EA 2005 12 9 COMA0560671 120051205A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS WARNING LIGHT A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01959CA 7116 FLIGHT 5586 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01. 2L72 4F RTA21EA 20051209000172005120900017EA 2005 12 9 VTZA200500218 120051205A5310601R5211680 DOOR FRAME CNDAIRCL600 CL6002B19 1900309EA BS 338 CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27630BR 7255 PAX DOOR FRAME TOP RADIUS CRACKED AT 1" IN LENGTH FORWARD OF DATUM 1 AT FS 338.90. 2L72 4F RTA21EA 20051209000182005120900018EA 2005 12 9 VTZA200500219 120051205A5346601R536066 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA RT ENGINE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27630BR 7255 RT ENGINE SUPPORT BEAM IS CRACKED IN LOWER WEB AT .75". 2L72 4F RTA21EA 20051209000192005120900019EA 2005 12 9 VTZA200500217 120051205A5210601R317725 DRAG ANGLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27630BR 7255 PAX DOOR AFT DRAG ANGLE IS CRACKED 1.5". 2L72 4F RTA21EA 20051209000202005120900020EA 2005 12 9 VTZA200500220 120051205A53206013501251 ANGLE CNDAIRCL600 CL6002B19 1900309EA BS 625 CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27630BR 7255 LT OBLIQUE ANGLE AT FS 625 IS CRACKED. 2L72 4F RTA21EA 20051209000222005120900022NM 2005 12 9 SWAA053877 120051206A53306545776 SKIN BOEING737 7373H4 1384600NM BS 931 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29326SW 23690 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 931, STR 22R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051209000272005120900027NM 2005 12 9 SWAA053882 120051206A3350101331 COVER BOEING737 7377H4 1384404NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29423WN 29827 RT OVERWING EMERGENCY EXIT LIGHT COVER LOOSE. SECURED COVER PER MM. 2L72 4F RTA16WE 20051209000282005120900028NM 2005 12 9 SWAA053884 120051206A532269353656 SHEAR TIE BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29683SW 24008 DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 360, STR 14R TO STR 15R. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051209000292005120900029EA 2005 12 9 COMA0560670 120051204A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER HOT START A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01486CA 7707 FLIGHT 5746 - RT T/R UNLOCK WARNING. DEFERRED MAINTENANCE PER MEL. 2L72 4F RTA21EA 20051209000312005120900031NM 2005 12 9 MWEA050133 120051205A3213 STRUT BOEING717 717200 1383700NM NOSE LOW A MWEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31910ME 55174 NOSE LANDING GEAR UNSAFE LIGHT STAYED ON. FOUND STRUT LOW, SERVICED STRUT. 2L72 4F TRA6WE 20051209000322005120900032NM 2005 12 9 MWEA050134 120051204A3213 STRUT BOEING717 717200 1383700NM NOSE LOW A MWEAA UNSCHED LANDING O OTHER CLCLIMB 1 GL31903ME 55167 NOSE GEAR TOOK 20 MINUTES TO RETRACT INTO GEAR WELL. NOSE STRUT LOW, SERVICED STRUT. 2L72 4F TRA6WE 20051209000342005120900034SO 2005 12 9 C2XA05CL095 120051123A2760852701 SENSOR EMB 145 EMB145XR 3260214SO LT SPOILER BROKEN A C2XAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW2712136 145719 IAH FLIGHT NR 3098, THE CREW REPORTED A SPOILER OPEN INDICIATION IN FLIGHT. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LEFT OUTBOARD PROXIMITY SENSOR. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RT 20051209000352005120900035SO 2005 12 9 C2XA05SH135 120051202A532014521713005 FLOOR SUPPORT EMB 135 EMB135ER 3260203SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714505 192 SHV - DURING C-CHECK MAINTENANCE, FOUND CENTER OMEGA BEAM CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED CENTER OMEGA BEAM AT FRAME 20 TO FRAME 23 IAW EMB 135 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20051209000362005120900036SO 2005 12 9 C2XA05CL096 120051204A21508152403 ACM EMB 145 EMB145LR 3260212SO LEFT SEIZED A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW27135508705 145575 CLE FLIGHT NR 2944, THE CREW REPORTED A VERY STRONG BURNING SMELL WHENEVER THE ANTI-ICE SYSTEM IS ACTIVATED. MAINTENANCE INSPECTED AND REPLACED THE LEFT AIR CYCLE MACHINE. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20051209000372005120900037NM 2005 12 9 QXEA200501581 120051122A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX - RIGHT INBOARD SEAT TRACK NR 0 HAS PITTING CORROSION INSIDE CHANNEL AND TOP OF TRACK AT STATION X545. REPAIRED IAW DHC-8 SRM 51-40-11. 2H72 4T RTA13NM 20051209000392005120900039NM 2005 12 9 QXEA200501583 120051110A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX - RIGHT OUTBOARD SEAT TRACK NR 10 HAS SPOTS WITH BARE METAL EXPOSED BETWEEN FUSELAGE STATION X266 AND X541. REPAIRED IAW DHC-8-200 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20051209000402005120900040NM 2005 12 9 QXEA200501574 120051110A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX - NR 1 SEAT TRACK HAS LIGHT SURFACE CORROSION ON TOP OF LUGS AT X266, X296-297, X407, X424. REPAIRED IAW RD 8-53-1342, DHC-8-200 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20051209000422005120900042NM 2005 12 9 QXEA200501579 120051110A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX - RIGHT INBOARD SEAT TRACK NR 8 HAS CHAFE MARKS INSIDE CHANNEL, 10" LONG AREA AT APPROXIMATELY STATION X477. REPAIRED IAW RD 8-53-1339, DHC-8-202 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20051209000432005120900043NM 2005 12 9 QXEA200501580 120051110A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX - RIGHT INBOARD SEAT TRACK NR 8 HAS CHAFE MARKS INSIDE CHANNEL, 10" LONG AREA AT APPROXIMATELY STATION X510. REPAIRED IAW RD 8-53-1337, DHC-8-202 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20051209000442005120900044SO 2005 12 9 C2XA05BT081 120051119A5610163500111 WINDSHIELD EMB 145 EMB145LR 3260212SO COCKPIT BURNED A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW27139898196 8196 145271 CREW REPORTED, "ELECTRICAL SMELL IN COCKPIT". MAINTENANCE FOUND BURNED WIRE TERMINALS AT THE NR 1 WINDSHIELD ASSEMBLY. REMOVED AND REPLACED CAPTAINS WINDSHIELD ASSEMBLY IAW EMB145 AMM NR 6-10-01. OPS AND LEAK CHECK GOOD. NO SMELL NOTED, AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20051209000452005120900045SO 2005 12 9 C2XA05IA138 120051129A21302225ON030301 CONTROLLER EMB 145 EMB145LR 3260212SO COCKPIT DEFECTIVE A C2XAB EMER. DESCENT O OTHER DEDESCENT 1 SW27165591138322 145603 IAH - FLIGHT 2102, DURING DESCENT, THE CREW REPORTED THAT A RAPID AND COMPLETE DECOMPRESSION WITH PASSENGER OXYGEN MASK DEPLOYMENT AT 17000 FEET. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE PNEUMATIC AND ELECTROPNUEMATIC OUTFLOW VALVES, AND DIGITAL CONTROLLER. THE AIRCRAFT PRESSURIZATION SYSTEM WAS OPERATIONALLY CHECKED WITH NO DEFECTS. THE AIRCRAFT WAS SATISFACTORILY TEST FLOWN, AND WAS THEN APPROVED FOR RETURN TO SERVICE. THE REMOVED DIGITAL CONTROLLER WAS TESTED, FOUND TO BE DEFECTIVE, AND REMOVED FROM SERVICE. 2L72 4T RTT00011AT 20051209000462005120900046SO 2005 12 9 C2XA05CL097 120051206A32608005701 PROXIMITY SENSOR EMB 145 EMB145EP 3260221SO NLG FAILED A C2XABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW2714938 145029 CLE FLIGHT NR 2235, THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE PRECEEDED BY E1-2 REVERSER DISAGREE IN FLIGHT. THE CREW DECLARED AN EMERGENCY AND RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NOSE LANDING GEAR WOW PROXIMITY SENSOR. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20051209000472005120900047EA 2005 12 9 QXEA200501632 120051031A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA BS 477 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, LOWER FUSELAGE EXTERNAL SKIN GOUGED BY ROCK CHIPS AT STATION 477 PRODUCTION BUTT JOINT BETWEEN STRINGERS 24L AND 25L. MAINTENANCE REPAIRED THE SKIN IAW EA R-53-393 AND REO 670-53-00-075. FINISH RESTORED. 2L72 4F RTA21EA 20051209000482005120900048EA 2005 12 9 QXEA200501633 120051031A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA BS 469-485 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, LOWER FUSELAGE EXTERNAL SKIN GOUGED BY ROCK CHIPS AT STATION 469-485 STRINGERS 26L AND 26R. MAINTENANCE REPAIRED SKIN IAW EA R-53-393 AND REO 670-53-00-075. FINISH RESTORED. 2L72 4F RTA21EA 20051209000492005120900049EA 2005 12 9 QXEA200501634 120051031A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA BS 485-510 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC- DURING C3 CHECK, LOWER FUSELAGE EXTERNAL SKIN GOUGED BY ROCK CHIPS AT STATION 485-510 STRINGERS 25L-27. MAINTENANCE BLENDED OUT DAMAGE IAW CRJ-700 SRM 51-12-00-001-001-A01. RESTORED FINISH. 2L72 4F RTA21EA 20051209000502005120900050EA 2005 12 9 QXEA200501628 120051031A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA BS 310-333 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC- DURING C3 CHECK, LOWER FUSELAGE EXTERNAL SKIN GOUGED AT STATION 310-333 STRINGERS 25L AND 25R 5 PLACES. MAINTENANCE REMOVED DAMAGE IAW CRJ-700 SRM 51-12-00-001-001-A01. RESTORED FINISH. 2L72 4F RTA21EA 20051209000522005120900052EA 2005 12 9 QXEA200501641 120051031A5210 STRINGER CNDAIRCL600 CL6002C10 1390015EA PAX DOOR CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, PASSENGER DOOR FORWARD SIDE STRINGER CRACKED UP FROM RADIUS BETWEEN RISER AND TREAD UNDER HANDRAIL STOWAGE BRACKET. REMOVED DAMAGED AREA IAW REO 670-52-11-104. 2L72 4F RTA21EA 20051209000532005120900053EA 2005 12 9 QXEA200501644 120051031A5754MS21059L3 ANCHOR CNDAIRCL600 CL6002C10 1390015EA SLAT TRACK BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - RIGHT WING SLAT NR 1 INBOARD OF SLAT TRACK PANEL 622BZ HAS A BROKEN ANCHOR UNIT. MAINTENANCE REPLACED WITH A NEW NUT ASSEMBLY IAW CRJ-700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20051209000542005120900054EA 2005 12 9 QXEA200501635 120051031A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA BS 533-549 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, LOWER FUSELAGE EXTERNAL SKIN GOUGED BY ROCK CHIPS AT STATION 533-549 STRINGER 25L-26L. MAINTENANCE BLENDED OUT DAMAGE IAW CRJ-700 SRM 51-12-00-001-001-A01. RESTORED FINISH. 2L72 4F RTA21EA 20051209000552005120900055EA 2005 12 9 QXEA200501631 120051031A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA BS 437 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC- DURING C3 CHECK, LOWER FUSELAGE EXTERNAL SKIN GOUGED BY ROCK CHIPS AT STATION 437, STRINGERS 27-26R. MAINTENANCE REPAIRED SKIN IAW EA R-53-393 AND REO 670-53-00-393-075. FINISH RESTORED. 2L72 4F RTA21EA 20051209000562005120900056EA 2005 12 9 QXEA200501629 120051031A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA BS 333-364 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, LOWER FUSELAGE EXTERNAL LOWER SKIN GOUGED BY ROCK CHIPS AT STATION 333-364, STRINGERS 25L AND 25R. MAINTENANCE REMOVED DAMAGE IAW CRJ-700 SRM 51-12-00-001-001-A01. RESTORED FINISH. 2L72 4F RTA21EA 20051209000572005120900057EA 2005 12 9 ASOA05959 120051107A5340 ATTACH ANGLE CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27709EV 10068 DURING A C-CHECK IN MCN, THE FLOORBOARD ATTACH ANGLE AT, THE PASSENGER DOOR ENTRANCE, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBOARD ATTACH ANGLE, AT THE PASSENGER DOOR ENTRANCE. (M) 2L72 4F RTA21EA 20051209000582005120900058SO 2005 12 9 LR7A05180 120051109A5330 SKIN LKHEED382 382G 526414USO FS 614 DENTED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2549 4606 DURING C-7 CHECK PER HC5321, FOUND FUSELAGE LOWER EXT SKIN SURFACE DENTED. FS 614, RBL36, WL130. REPAIRED SKIN SURFACE IAW SMP 583 FIG 51-140-12, NR 0402. 2H74 4T A1SO 20051209000592005120900059SO 2005 12 9 LR7A05181 120051109A5330 SKIN LKHEED382 382G 526414USO FS 487 DENTED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2549 4606 DURING C-7 CHECK PER HC5321, FOUND FUSELAGE LOWER EXT SKIN SURFACE DENTED, FS 487, RBL14, WL127. REPAIRED SKIN SURFACE IAW SMP 583 FIG 51-140-12, NR 0403. 2H74 4T A1SO 20051209000602005120900060SO 2005 12 9 LR7A05182 120051109A5330 SKIN LKHEED382 382G 526414USO FS 260 DENTED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2549 4606 DURING C-7 CHECK PER HC5321, FOUND FUSELAGE LOWER EXT SKIN SURFACE DENTED, FS 260, LBL10.5, WL126. REPAIRED SKIN SURFACE IAW SMP 583 FIG 51-140-12, NR 0404. 2H74 4T A1SO 20051209000642005120900064SO 2005 12 9 LR7A05186 120051109A5753 SPAR CAP LKHEED382 382G 526414USO FLAP STA 180 CORRODED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2549 4606 DURING C-7 CHECK PER HC571, FOUND CORROSION ON LOWER LT OB FLAP SPAR CAP BEYOND LIMITS, FLAP STA 180. REPAIRED FLAP SPAR CAP IAW SMP 583 57-70-09, NR 0565. 2H74 4T A1SO 20051209000662005120900066SO 2005 12 9 LR7A05188 120051109A5753 SPAR LKHEED382 382G 526414USO FLAP STA 177 CORRODED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2549 4606 DURING C-7 CHECK PER HC571, FOUND CORROSION ON LWR TH IB FLAP SPAR BEYOND LIMITS, FLAP STA 177-213. REPAIRED FLAP SPAR CAP IAW DRG R05-28-05, MEA 382-27-05-094, NR 0580. 2H74 4T A1SO 20051209000672005120900067SO 2005 12 9 LR7A05189 120051109A5753 SPAR LKHEED382 382G 526414USO FLAP STA 163 CORRODED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2549 4606 DURING C-7 CHECK PER HC5712, FOUND CORROSION ON LWR RT OB FLAP SPAR BEYOND LIMITS, FLAP STA 163-208. REPAIRED FLAP SPAR CAP IAW DRG R05-28-07, MEA 382-27-05-096, NR 0606. 2H74 4T A1SO 20051209000682005120900068SO 2005 12 9 LR7A05190 120051109A5312 PRESSURE PANEL LKHEED382 382G 526414USO BS 616 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2549 4606 DURING C-7 CHECK PER SB 382-57-85, FOUND PRESSURE WEB CRACKED 1/2 INCH FROM AFT FASTENER HOLE RUNNING TO AFT EDGE OF WEB, FS 557-617, WL257, RBL61. REPAIRED IAW SMP 583 57-70 AND 51-140-12, NR 0622. 2H74 4T A1SO 20051209000692005120900069SO 2005 12 9 LR7A05191 120051109A53153376655 FLOORBEAM LKHEED382 382G 526414USO BS 228 CORRODED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2549 4606 DURING C-7 CHECK PER HC5312, FOUND 2 INCH SQUARE AREA OF BEAM CAP CORRODED FS228, WL146, RBL11. REPLACED UPPER T CAP IAW DRG 337665 AND 362653, NR 0628. 2H74 4T A1SO 20051209000722005120900072EA 2005 12 9 QXEA200501609 120051031A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA BS 1060 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - IN C3 CHECK, FUSELAGE EXTERIOR HAS SCRATCH ON FUSELAGE SKIN AT STATION 1060 AT STRINGER 14L. MAINTENANCE BLENDED SCRATCH IAW CRJ-700 SRM 51-12-00-001-001-A01. RESTORED FINISH. 2L72 4F RTA21EA 20051209000762005120900076SO 2005 12 9 LR7A05193 120051109A531537235110 FLOORBEAM LKHEED382 382G 526414USO BS 617 CORRODED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2549 4606 DURING C-7 CHECK PER HC5313, FOUND RT CHINE CAP CORRODED BEYOND LIMITS, FS 617. REPLACED CHINE CAP IAW SMP 581 91-00-04, NR 0674. 2H74 4T A1SO 20051209000772005120900077NM 2005 12 9 05FDEA04124 120051205A5753 SUPPORT FITTING DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RIGHT WING OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING FOUND CORROSION AT OUTBOARD NR 2 BOLT HOLE. REFER TO SNRM NO. N0830 FOR RIGHT HAND WING OUTBOARD FLAP REPLACEMENT. 2L73 4F RTA22WE 20051209000782005120900078EU 2005 12 9 UPS05145852 120051204A5412 BULKHEAD AIRBUSA300 A300F4622R 3930360EU NR 2 NACELLE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01140UP 0823 NR 2 ENG LT INLET COWL AFT BULKHEAD WEB CRACKED AT STATIC LPORT LINE UNION TO EEC. REPAIRED BULKHEAD WEB AS PER EO A300-7110-20525. 2L72 4F RTA35EU 20051209000802005120900080EA 2005 12 9 QXEA200501735 120051204A29109300705 HEAT EXCHANGER CNDAIRCL600 CL6002C10 1390015EA NR 2 HYD SYSTEM LEAKING A QXEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 NM09606QX11305 10023 PDX - ON FLIGHT 2451, 100 MILES OUT OF PDX NR 2 HYDRAULIC SYSTEM FAILED. FLIGHT RETURNED TO PDX AND ACCOMPLISHED A UNEVENTFUL LANDING. SHUTOFF VALVE TO NR 2 SYSTEM WAS CLOSED FOR 25-30 MINUTES. MAINTENANCE FOUND SKYDROL LEAKING AT THE EXIT FOR THE HEAT EXCHANGER. REPLACED THE HEAT EXCHANGER. OPERATIONAL CHECKS GOOD. PERFORMED REQUIRED INSPECTIONS FOR ENGINE DRIVEN PUMPS OPERATING WITHOUT FLUID. CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20051209000832005120900083EA 2005 12 9 QXEA200501646 120051031A5230 ARM CNDAIRCL600 CL6002C10 1390015EA CARGO DOOR GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, FORWARD BAGGAGE BAY DOOR FORWARD COUNTERBALANCE ARM GOUGED. MAINTENANCE REPLACED THE ARM IAW EA R-52-251 AND REO 52-35-098. OPERATIONAL CHECKS GOOD. 2L72 4F RTA21EA 20051209000842005120900084EA 2005 12 9 QXEA200501647 120051031A5730 SKIN CNDAIRCL600 CL6002C10 1390015EA WS 231 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, LEFT WING UPPER SURFACE AT STATION 231.23 HAS 2 RIVET HEADS MISSING. REPLACED RIVETS IAW CRJ-700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20051209000862005120900086EA 2005 12 9 QXEA200501636 120051031A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA BS 565-589 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, LOWER FUSELAGE EXTERNAL SKIN GOUGED BY ROCK CHIPS AT STATION 565-589, STRINGERS 27-25R. BLENDED OUT DAMAGE IAW CRJ-700 SRM 51-12-001-001-A01. RESTORED FINISH. 2L72 4F RTA21EA 20051209000872005120900087EA 2005 12 9 QXEA200501643 120051031A5310670341757 CROSSBEAM CNDAIRCL600 CL6002C10 1390015EA BS 280 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC- DURING C3 CHECK, FUSELAGE INTERIOR AT STATION 280 CROSS BEAM IS CORRODED ALONG THE FLANGE. MAINTENANCE REPLACED THE CROSS BEAM. 2L72 4F RTA21EA 20051209000882005120900088EA 2005 12 9 QXEA200501637 120051031A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA BS 629 TOOL DAMAGE A QXEAK NONE W INADEQUATE Q C ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, LOWER FUSELAGE EXTERNAL SKIN AT STATION 629 STRINGER 19L-20L HAS A DRILL MARK IN THE SKIN. BLENDED OUT DAMAGE IAW CRJ-700 SRM 51-12-00-001-001-A01. RESTORED FINISH. 2L72 4F RTA21EA 20051209000922005120900092EA 2005 12 9 QXEA200501649 120051031A5311 FRAME CNDAIRCL600 CL6002C10 1390015EA BS 939 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC- DURING C3 CHECK, FUSELAGE INTERIOR UPPER FRAME AT STATION 939 STRINGER 3R HAS A GOUGE ON THE AFT SIDE. MAINTENANCE REPAIRED FRAME IAW CRJ-700 SRM 53-51-06-101-001-A01. NO CRACKS FOUND. 2L72 4F RTA21EA 20051209000932005120900093SO 2005 12 9 LR7A05194 120051109A5730 PANEL LKHEED382 382G 526414USO FS597 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2549 4606 DURING C-7 CHECK PER SB 382-57-85, FOUND CRACK AT CENTER WING LOWER SURFACE PANEL NR 3 AT FS 597, LBL60. REPAIRED PANEL IAW TASK 0044, DRG SK382-57-298, MEA 382-57-05-099, NR 0744. 2H74 4T A1SO 20051209000942005120900094SO 2005 12 9 LR7A05195 120051109A5330 PANEL LKHEED382 382G 526414USO FS597 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2549 4606 DURING C-7 CHECK PER SB 382-57-85, FOUND CRACK AT CENTER WING LOWER SURFACE PANEL NR 3 AT F 597, RBL60. REPAIRED PANEL IAW TASK 0044, DRG SK382-57-298, MEA 382-57-05-099, NR 0744. 2H74 4T A1SO 20051209000952005120900095NM 2005 12 9 05FDEA04125 120051205A5753 SUPPORT FITTING DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RIGHT WING OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING FOUND CORROSION AT OUTBOARD NR 3 BOLT HOLE. RT WING OUTBD FLAP REMOVED & REPLACED AS PER AMM 27-50-30-4. VANE ADJUSTMENT CARRIED OUT AS PER AMM 27-50-32-5 FOUND SATIS. OUTBD FLAP OPERATIONAL TEST & ADJUSTMENT CARRIED OUT AS PER AMM 27-50-00-5 FOUND SATIS. 2L73 4F RTA22WE 20051209000962005120900096WP 2005 12 9 05FDEA04126 120051205A5520 REPAIR DOUG DC10 DC1030F 3023504WP LT ELEVATOR PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 LT LOWER INBOARD ELEVATOR FOUND 1 EXTERNAL DOUBLER REPAIR AT XE 243 DIMENS 17" BY 6". PERFORMED INSPECTION ON REPAIR DOUBLER IAW SRM 55-10-00 FIG 8 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2 E3 RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VOL 2 PAR 33 AND 24. 2L73 4F RTA22WE 20051209000972005120900097WP 2005 12 9 05FDEA04127 120051205A5754 REPAIR DOUG DC10 DC1030F 3023504WP TE FLAP PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 LT WING INBOARD FLAP FOUND A DOUBLER 8" BY 1" ON UPPER SKIN AT STA XIFH 147.300. PERFORMED A GVI OF REPAIR IAW SRM 57-20-00 FIG 11 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 E3 RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VOL 2 PAR 33. 2L73 4F RTA22WE 20051209001012005120900101NM 2005 12 9 05FDEA04131 120051205A5730 SKIN BOEING727 727227 1384078NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 MAIN CABIN, CENTER WING BOX UPPER SURFACE, SKIN IS CORRODED AT STA BS 820 LBL10. REPAIR CENTER WING BOX UPPER SURFACE OF SKIN IAW FEDEX EA7 5710-92595. "WINGS UPPER SKIN PANEL, CENTER TANK CORRODED, REPAIR ". ALODINED AND PRIMED BARE METAL IAW B727 SRM 51-10-2. INSTALLED FASTENERS WET IAW B727 SRM 51-30-2. CAP SEALED ALL FASTENERS IAW B727-200 MM 28-11-00-0-8. THIS IS A MAJOR REPAIR SIGNED BY TIMCO MECH NR 4315 AND QC298 REFERENCE FEDEX SNRM N01111. 2L73 4F A3WE 20051209001042005120900104WP 2005 12 9 05FDEA04134 120051205A5520 REPAIR DOUG DC10 DC1030F 3023504WP ELEVATOR PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 UPPER LT DETACHABLE ELEVATOR FOUND 1 EXTERNAL DOUBLER REPAIR AT XE 70 DIMENSION 4" BY 3.5". PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 55-10-00 FIG 8 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2 E3, RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 PAR 33 AND 24 VOL 2. 2L73 4F RTA22WE 20051212000012005121200001WP 2005 12 12 ABXA050333 120051130A57143924028 FITTING DOUG DC9 DC941 302207NWP CENTER WING CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23954AX 47612 FOUND CRACKED END FITTING AFT SIDE OF PRESSURE BULKHEAD AT LONGERON 29 RIGHT. REPLACED END FITTING IAW DC9 SRM. 2L72 4F A6WE 20051212000052005121200005WP 2005 12 12 ABXA050335 120051014A5315 FLOORBEAM DOUG DC8 DC863F 302198FWP FS 1660 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 MAIN DECK AFT ACCESSORY COMPARTMENT, STA 1660, LEFT BUTT LINE 44, LONGERON 22 LEFT, FLOORBEAM HAD CORROSION. CLEANED UP SURFACE CORROSION WITH NEGLIGIBLE MATERIAL LOSS EXCEPT FOR AROUND ONE FASTENER HOLE. REPAIRED CORROSION DAMAGE IAW DC8 SRM 51-1-8, PG 20, 53-2-0, 51-5-0, 53-2-0, FIG 18, LWR200302015-4/15/03, AND DC8 SRM 51-1-8, PG 14. REPAIR MATERIAL ALUMINUM EXTRUSION P/N AND10136-2001 7075-T6 0.063" PO NR 1120529 AND 7075-T6 0.063 PO NR 1118787. 2L74 4F 4A25 20051212000062005121200006WP 2005 12 12 ABXA050336 120051017A5312 PRESSURE PANEL DOUG DC8 DC863F 302198FWP FS 980 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DOUBLER CORRODED TOP OF RIGHT WHEEL WELL PRESSURE DECK IN MAIN CARGO, STA 980, RIGHT BUTT LINE 30. REMOVED, FABRICATED, AND INSTALLED DOUBLER AT TOP OF RIGHT WHEEL WELL PRESSURE DECK IN MAIN CARGO STA 980 RIGHT BUTT LINE 30 IAW DC8 SRM 51-1-21, 51-1-14, 51-9-0 AND DPS 3.695. 2L74 4F 4A25 20051212000072005121200007NE 2005 12 12 ABXA050337 220051017A7313 CASE DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE EXHAUST NOZZLE WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 NR 2 ENGINE EXHAUST NOZZLE 6 O'CLOCK POSITION, CASE WORN. REMOVED DAMAGED EXISTING DOUBLERS IAW DC8 SRM 51-1-21. FABRICATED NEW DOUBLERS IAW SSRM DWG NR 78-841 FROM 0.051 301 1/2HD PO NR 1121624, PRIMED CONTACT SURFACE IAW DC8 51-1-8. INSTALLED NEW DOUBLER IAW SSRM DWG NR 78-841 AND DC8 SRM 51-1-21. 2L74 4F4 F 4A25 1E8 20051212000122005121200012EU 2005 12 12 UPS05145866 120051208A3350 LAMP AIRBUS300 A300B4622R 3930312EU LAVATORY INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01148UP 0831 LAV 1T, SUPERNUMARY AREA EMERGENCY AUX WALL MOUNTED ABOVE MIRROR INOP. RELAMPED WITH SERVICEABLE LAMP LAV 1T IAW A300-600 AMM 33-51-21-4. OPS CK NORMAL. 2L72 4F RTA35EU 20051212000132005121200013NM 2005 12 12 UPS05245867 120051209A3350 LIGHT BOEING727 727180C 138406GNM COCKPIT LOOSE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 COCKPIT EMERGENCY EXIT LIGHT LOOSE OUT OF FITTING ABOVE DOOR. SECURED EMERGENCY EXIT LIGHT ON CASE AND INSTALLED LENS REF MM 33-50-67-2. 2L73 4F A3WE 20051212000152005121200015NM 2005 12 12 AWXA200501488 120051122A5321D5367320300000 FLOOR PANEL AIRBUSA319 A319132 3930340NM CABIN CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28660AW 1234 SAL - DURING BC4 CHECK DISCOVERED LEVEL TWO GALVANIC CORROSION ON 131HF FWD CARGO FLOOR PANEL UPPER SURFACE. CORROSION WAS FOUND OUT OF LIMITS IAW AIRBUS 320 SRM 53-02-00 TABLE 105. REPLACEMENT PANEL FABRICATED IAW IRM 9701 REV F PAR 8. INSTALLED REPAIR PART FROM FS 30 TO FS 34 AND FROM Y692 TO -Y692 IAW IRM 9701 REV F PAR 8, 9 AND 10. 2L72 4F RTA28NM 20051212000162005121200016EU 2005 12 12 AWXA200501489 120051206A5347D5713014720202 SEAT TRACK AIRBUS320 A320232 3930326EU CABIN CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28604AW 1196 SAL - DURING BC4 CHECK DISCOVERED CORROSION ON LT OUTBOARD SEAT TRACK AT FS 40+12". MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 101. REMOVED AND INSTALLED NEW SEAT TRACK FROM FS 36 TO FS 41 AND Y1292 IAW AIRBUS 320 SRM 51-72-11. 2L72 4F RTA28NM 20051212000172005121200017EU 2005 12 12 AWXA200501490 120051206A5347D5337111200400 SEAT TRACK AIRBUS320 A320232 3930326EU CABIN CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28604AW 1196 SAL - DURING BC4 CHECK DISCOVERED LEVEL 2 EXFOLIATION CORROSION ON THE LT OUTBOARD SEAT TRACK AT F 42 AND Y1292. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 101. REMOVED AND INSTALLED NEW SEAT TRACK FROM FR41 TO FR47 AND Y1292 IAW AIRBUS 320 SRM 51-42-11. 2L72 4F RTA28NM 20051212000182005121200018EU 2005 12 12 AWXA200501491 120051207A5347D5337111000800 SEAT TRACK AIRBUS320 A320232 3930326EU CABIN CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28604AW 1196 SAL - DURING BC4 CHECK DISCOVERED LEVEL 2 GALVANIC CORROSION ON THE LT INBOARD SEAT TRACK AT FS 46+15" AND Y765. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 101. REMOVED AND INSTALLED NEW SEAT TRACK FROM FS 41 TO FS 47 AND Y765 IAW AIRBUS 320 SRM 51-42-11. 2L72 4F RTA28NM 20051212000192005121200019EU 2005 12 12 AWXA200501492 120051207A5320D5347112420000 PLATE AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28604AW 1196 SAL - DURING BC4 CHECK DISCOVERED LEVEL 2 GALVANIC CORROSION ON SHEAR PLATE LOCATED BETWEEN FS 69 TO FS 70 AND Y1162. NO ALLOWABLE DAMAGE LIMITS WERE FOUND IN THE AIRBUS 320 SRM. MAINTENANCE REMOVED AND INSTALLED NEW SHEAR PLATE BETWEEN FS 69 AND FS 70, Y1162 IAW AIRBUS 320 SRM 51-72-11 AND 51-42-11. 2L72 4F RTA28NM 20051212000242005121200024EU 2005 12 12 AALA20050804 120051205A2780 JACKSCREW AIRBUS300 A300B4605R 3930308EU NR 1 SLAT OVERTORQUED A AALAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 SW217062A 474 JFK - ON TAKEOFF, SLATS WOULD NOT RETRACT. FOUND RIGHT HAND TORQUE LIMITER AND RIGHT HAND NUMBER 1 SLAT JACK SCREWS OVER TORQUE. INDICATIONS POPPED. REPLACED RIGHT HAND NUMBER 1 SLAT JACK SCREW AND RESET RIGHT HAND TORQUE LIMITER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20051212000252005121200025NM 2005 12 12 AALA20050793 120051203A33508039001 BATTERY PACK DOUG MD80 MD83 3023681NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW219414W 53189 SFO - AFT ACCESSORY EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT TAIL CONE FOR AFT ACCESSORY EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RT 20051212000262005121200026WP 2005 12 12 AALA20050798 120051208A3397 CONNECTOR DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21434AA 49452 SFO - EMERGENCY LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED CONNECTOR UNDER SEAT 3F FOR EMERGENCY LIGHTS IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20051212000282005121200028WP 2005 12 12 AALA20050799 120051203A3350P2010031303 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21560AA 53090 SFO - EMERGENCY LIGHTS AT TAIL COMPARTMENT SIDEWALL INOPERATIVE. REPLACED AFT VETICAL EMERGENCY LIGHT ASSEMBLY FOR EMERGENCY LIGHTS AT TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051212000302005121200030WP 2005 12 12 AALA20050791 120051201A3350 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217539A 49993 LGA - TWO OVERHEAD EMERGENCY LIGHTS IN TAIL CONE INOPERATIVE. SECURED LOOSE BATTERY PACKS FOR TWO OVERHEAD EMERGENCY LIGHTS IN TAIL CONE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051212000312005121200031NM 2005 12 12 AALA20050801 120051207A3350P4010051112 MODULE BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21645AA 24603 SFO - EMERGENCY LIGHTS FROM ROWS 15 TO 2 LEFT DOOR INOPERATIVE. REPLACED MODULE AT LOCATION M10799 FOR EMERGENCY LIGHTS FROM ROWS 15 TO 2 LEFT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20051212000322005121200032WP 2005 12 12 AALA20050797 120051203A3220 PISTON DOUG DC9 DC982 3022082WP NLG INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21455AA 49560 NOSE GEAR WOULD NOT RETRACT. LANDED BNA WITHOUT INCIDENT. FOUND CHROME MISSING FROM PISTON. REPLACED PISTON AND SCHRADER VALVE. SERVICED STRUT WITH OIL AND AIR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051212000342005121200034WP 2005 12 12 AALA20050794 120051206A3234 HANDLE DOUG DC9 DC982 3022082WP MLG INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21457AA 49562 AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. HANDLE WOULD NOT COME UP. FOLLOWED QRH. NOSE WHEEL WAS STEERABLE. LANDED ORD WITHOUT INCIDENT. ACCOMPLISHED WORK CARD 32-96-14. NO DEFECTS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051212000362005121200036WP 2005 12 12 AALA20050800 120051203A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21560AA 53090 SFO - OVERHEAD EMERGENCY LIGHT AT AFT FLIGHT ATTENDANT SEAT AND ROWS 12 TO 16 INOPERATIVE. REPLACED BATTERY PACKS AT B5 27 AND B5 102 FOR OVERHEAD EMERGENCY LIGHT AT AFT FLIGHT ATTENDANT SEAT AND ROWS 12 TO 16. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051212000372005121200037EU 2005 12 12 05FDEA04179 120051208A5320 BEAM AIRBUS310 A310203 3930313EU NLG WW DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 IN NOSE WHEEL WELL FWD VERTICAL BEAM RT HAS 1 EA ELONGATED HOLE ON LOWER FLANGE REF N00811. ACCOMPLISHED BUSHING REPAIR IAW EA 6-5312-95444 AND A310-200 SRM 51-40-51 PAGE 12. 2L72 4F RTA35EU 20051212000412005121200041NM 2005 12 12 05FDEA04148 120051205A5315 FLOORBEAM DOUG MD11 MD11F 3023600NM ZONE 100 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 FOUND CENTER CARGO DOOR WAY CEILING AREA STA 1721, X=-98 MAIN DECK FLOORBEAM LOWER SIDE FOUND CHAFED. REPAIR CARRIED OUT AT CENTER CARGO DOOR WAY CEILING AREA AT STA 1721, X=-98 MAIN DECK FLOOR BEAM LOWER SIDE AS PER FEDEX EA 1-5310-90708, TITLE: "FUSELAGE- FLOOR BEAM CHAFING AT FUSELAGE STATION Y=1721, X=-98 REPAIR". REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051212000422005121200042 2005 12 12 TQ0A0512001 420051121A6113 BULKHEAD HARTZL DHAV DHC2 DHC2* 2800108EA PWA R985 R985AN14B 52008NE HARTZLHCB3R HCB3R302 GL SPINNER CRACKED E TQ0AK NONE O OTHER ININSP/MAINT 1 AL0567667 79 EM83 1309 18416 EM83 SPINNER BULKHEAD CRACKED. 1H71 3R3 R A806 5E1 5 CP28EA 20051212000442005121200044NE 2005 12 12 TQ0A20050001 220050516A7200 ENGINE DHAV DHC2 DHC2MK1 2800102EA PWA R985 R985* 52008NE SEIZED E TQ0AA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 AL0567676 809 MM2327 ENGINE SEIZURE DURING CLIMB-OUT. VISUAL INSPECTION OF ENGINE OIL SCREEN AND SUMPS REVEALED STEEL PARTICLES. 1H71 3R3 R A806 5E1 20051212000452005121200045 2005 12 12 TQ0A0003 420051205A611383632SPR BULKHEAD DHAV DHC2 DHC2* 2800108EA PWA R985 R985AN14B 52008NE HARTZLHCB3R HCB3R302 GL SPINNER CRACKED E TQ0AK NONE O OTHER ININSP/MAINT 1 AL0567667 79 1309 18416 EM83 SPINNER BULKHEAD CRACKED. 1H71 3R3 R A806 5E1 5 CP28EA 20051212000512005121200051SO 2005 12 12 MASA200500964 120051124A7830M835362024M RELAY EMB 145 EMB145LR 3260212SO THRUST REVERSER FAILED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07847MJ 145517 ASH 2989 CLT, NR 2 THRUST REVERSER DISAGREE. MAINTENANCE REPLACED THE AIR TO GROUND RELAY. 2L72 4T RTT00011AT 20051212000522005121200052EA 2005 12 12 REXA200500144 120051205A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A REXAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO258409N 7409 FLAPS FAILED AT 0 DEGREES. SYSTEM REST AND PLACED ON 72 HOUR WATCH PER AD 98-20-01. 2L72 4F RTA21EA 20051208000072005120800007WP 2005 12 8 ABXA050300 120051104A5313 DOUBLER DOUG DC8 DC863F 302198FWP STA 1180 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 CORROSION ON TOP OF LONGERON REINFORCEMENT DOUBLER IN AFT CARGO BILGE AT STA 1180, LONGERON 36 TO 34 RIGHT. REMOVED DOUBLER AT STA 1200 LONGERON 34 RIGHT TO 36. REMOVED CORROSION FROM DOUBLER. FOUND TO BE OUT OF LIMITS. FABRICATED, TREATED, PRIMED AND INSTALLED NEW DOUBLER FROM 7075-T6.125 P/O NR 119160 IAW DC8 SRM 51-1-8, 51-1-20D, LWR 200302015 AND SSRM DWG K0T142. 2L74 4F 4A25 20051208000112005120800011EU 2005 12 8 DHL2005362AA3 120051206A5347 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE LOOSE A DHLAK NONE O OTHER ININSP/MAINT 1 SO01362DH 84 DURING "A" CHECK PALLET STOP RAIL LOOSE AT FRAME 19 LT SIDE NR 2 SEAT TRACK. REMOVED AND INSTALLED SEAT TRACK SECTION AT FR. 19 LT SIDE NR 2 OF MAIN CARGO, AS PER A-300 SRM 53-10-10 PAGE 813 / 816. 2L72 4F RTA35EU 20051208000122005120800012EU 2005 12 8 SA05120 120051126A3350321431 BATTERY AIRBUSA319 A319112 3930323EU PASSENGER CABIN FAULTY A USAAK NONE L NO TEST ININSP/MAINT 1 EA19768US 1389 THE LEFT FORWARD EMERGENCY LIGHT FAILED TEST. MAINTENANCE REPLACED THE FORWARD LEFT EMERGENCY LIGHT BATTERY PACK. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20051208000142005120800014EU 2005 12 8 SA05122 120051205A3350321431 BATTERY PACK AIRBUSA321 A321211 3930370EU GE CFM56 CFM56* 13802NE PASSENGER CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19185UW 1666 THE LT FORWARD EMERGENCY LIGHT BATTERY PACK FAILED TEST. MAINTENANCE REPLACED THE LT FORWARD BATTERY PACK. OPERATIONALLY CHECKS OK. 2L72 4F4 FRTA28NM E2GL 20051208000962005120800096EA 2005 12 8 COMA0560666 120051202A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA RIGHT UNRELIABLE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01988CA1131810095 7204 FLIGHT 5667- FLAPS FAIL CAUTION. REPLACED THE RT BPSU. 2L72 4F RTA21EA 20051208001022005120800102EA 2005 12 8 SWIA200515946 120051115A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA BS 654 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07416SW 7089 INTERCOSTAL CRACKED AT FS 654.50 AT STR 4L, ITEM FOUND AT C-CHECK INSPECTION. INTERCOSTAL REPAIRED IAW CRJ SRM 51-71-12 FIG 4 & 51-31-00, 51-25-06, 51-23-00 & 51-25-16. 2L72 4F RTA21EA 20051208001322005120800132SO 2005 12 8 MASA200500705 120050801A2120BWT138001 FLEX DUCT EMB 145 EMB145LR 3260212SO NR 2 PACK UNKNOWN A MASAK NONE O OTHER ININSP/MAINT 1 SW07840MJ 145429 DURING OVERNIGHT MAINTENANCE A NR 2 PACK WAS FOUND TO BE NOISY. MAINTENANCE REPLACED THE DUCT THROUGH A FLIGHT CAMPAIGN DIRECTIVE (FCD). 2L72 4T RTT00011AT 20051208001342005120800134SO 2005 12 8 MASA200500707 120050808A2120BWT138001 FLEX DUCT EMB 145 EMB145LR 3260212SO UNKNOWN A MASAK NONE O OTHER ININSP/MAINT 1 SW07850MJ 145568 DURING OVERNIGHT MAINTENANCE, A NOISE ATTENTUATOR DUCT WAS REPLACED THROUGH A FLEET CAMPAIGN DIRECTIVE (FCD). 2L72 4T RTT00011AT 20051208001962005120800196EU 2005 12 8 05FDEA04110 120051204A3230 LANDING GEAR AIRBUS310 A310222 3930315EU LEFT MALFUNCTIONED A FDEAO OTHER J WARNING INDICATION CLCLIMB 1 SO25455FE 331 AFTER TAKEOFF THE LEFT MAIN GEAR WAS A GOOD BIT SLOWER TO SHOW UP AND LOCKED AFTER THE GEAR WAS RETRACTED. WHILE THE NOSE GEAR AND RIGHT MAIN SHOWED UP AND LOCKED WITH LIGHTS OUT, THE LEFT MAIN HAD A AMBER DOOR LIGHT AND RED UNLOCK LIGHT ILLUMINATED. THERE WAS ALSO A ECAM WARNING ON THE LEFT ECAM SAYING LEFT MAIN NOT UP AND LOCKED. AFTER ABOUT 5 TO 7 SECONDS THE LIGHTS ON THE FORWARD INDICATOR PANEL WENT OUT AND THE ECAM WARNING WENT AWAY. REMOVED AND REPLACED LEFT AND RIGHT MAIN GEAR SEQUENCE VALVES IN REFERENCE TO A310 M/M 32-31-37-4 OPS CHECKS GOOD IN REFERENCE TO A310 M/M 32-31-00-5. 2L72 4F RTA35EU 20051208001972005120800197NM 2005 12 8 SWAA053839 120051202A3350207377 LENS BOEING737 7377H4 1384404NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29204WN 29855 FWD EEPLS TRACK LENS MISSING. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20051208001992005120800199NM 2005 12 8 SWAA053841 120051203A335020121 BATTERY PACK BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED SERVICE CHECK, FOUND AFT GALLEY EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20051208002012005120800201NM 2005 12 8 SWAA053843 120051202A3350MS155721 BULB BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED 1/4D CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20051208002032005120800203NM 2005 12 8 SWAA053845 120051202A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 18L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051208002052005120800205NM 2005 12 8 SWAA053847 120051202A335007912 COVER BOEING737 7377H4 1384404NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29406WN 27894 EEPLS TRACK COVER LOOSE AT FWD END. SECURED COVER PER MM. 2L72 4F RTA16WE 20051208002072005120800207NM 2005 12 8 SWAA053849 120051130A3350MS155721 BULB BOEING737 7377H4 1384404NM FUSELAGE INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29465WN 33829 DURING SCHEDULED RON CHECK, FOUND RT AFT EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20051208002092005120800209NM 2005 12 8 SWAA053851 120051202A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 727B, LBL 3. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051208002112005120800211EU 2005 12 8 05FDEA04112 120051204A3230 SEQUENCE VALVE AIRBUS310 A310222 3930315EU RT MLG MALFUNCTIONED A FDEAO OTHER J WARNING INDICATION CLCLIMB 1 SO25420FE 339 RIGHT LANDING GEAR TAKES 10 SECONDS LONGER THAN THE LEFT GEAR TO RETRACT. ECAM GEAR NOT YET WARNING FOR ABOUT 2 SECONDS. THEN NORMAL OPS WHEN GEAR EXTENDED. CLEANED RESTRICTOR VALVE. REPLACED MAINGEAR ACTUATIN G ASSEMBLY RH IAW AMM 32-31-46. REPLACED LANDING GEAR SEQUENCE VALVE RT IAW AMM 32-31-37. REPLACED RETURN FILTER GREEN HYD SISTEM IAW AMM 29-11-15. PERFORMED TEST IAW 32-31-00 OK. 2L72 4F RTA35EU 20051209000012005120900001EA 2005 12 9 QXEA200501751 120051206A2797MPE9P1 CONNECTOR CNDAIRCL600 CL6002C10 1390015EA FLAP/SLATS SHORTED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09603QX 10011 PDX - ON TAXI OUT FOR FLT 2481, RECEIVED A FLAP HALFSPEED STATUS MESSAGE. RETURNED TO THE GATE. MX REMOVED NR 1 AND NR 2 SFECU IAW CRJ 700 TASK 27-51-05-000-801-A01, AND RANG OUT WIRES FROM SFECU TO NR 2 BPSU IAW CRJ 700 WDM 27-52-00 AND FOUND PINS 11 AND 13 SHORTED TOGETHER AT CONNECTOR MPE10P1. OPENED CONNECTOR MPE10P1 AND FOUND SEVERAL DAMAGED WIRES. FAB`D NEW CONNECTOR MPE10P1 IAW CRJ 700 WDM 27-52-00 MCN R27163-002. SPLICED IN NEW CONNECTOR MPE9P1 IAW MM 20-33-00 PG 212 THROUGH 216 STEP 8. REINSTALLED NR 1 AND NR 2 SFECU'S IAW CRJ AMM TASK 27-51-05-400-801-A01. PERFORMED OPS TEST OF THE FLAPS AND SLATS IAW CRJ AMM TASK 27-50-00-710-801-A01, OPS CHECK GOOD. A/C RETURNED TO SERVICE. 2L72 4F RTA21EA 20051209000052005120900005NM 2005 12 9 UPS05245859 120051025A5230 SKIN BOEING727 72730C 1384009NM CARGO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 INSPECTION TYPE:C AFT CARGO DOOR CRACK ON INNER SKIN SECOND INSPECTION HOLE FWD EDGE AT BOTTOM. REMOVE FASTENER AND CHECK DEPTH OF CRACK TO DETERMINE REPAIR. HFEC CARRIED OUT AND CRACK FOUND CONTAINED WITHIN FASTENER HOLE. REPAIRED IAW SRM 51-40-02. 2L73 4F A3WE 20051209000142005120900014WP 2005 12 9 UPS05845862 120051206A3350 LIGHT DOUG DC8 DC873F 302199FWP CABIN INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 EMERGENCY LIGHTS DISARM CHECK LIGHT INOP. RELAMPED IAW 33-15-00-2. OPS CK GOOD. 2L74 4F RT4A25 20051209000162005120900016EA 2005 12 9 COMA0560672 120051205A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A COMAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01865AS 7507 FLIGHT 5455 - ROW 1 ORANGE EMERGENCY LIGHT INOPERABLE. DEFERRED MAINTENANCE PER MEL. 2L72 4F RTA21EA 20051209000252005120900025NM 2005 12 9 SWAA053880 120051206A5754 SKIN BOEING737 7373H4 1384600NM RT WING SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29386SW PA784 26601 DURING SCHEDULED C4 CHECK, FOUND NR 5 L/E SLAT DELAMINATED AT OTBD UPPER CORNER. REMOVED AND REPLACED NR 5 SLAT PER MM. 2L72 4F RTA16WE 20051209000302005120900030NM 2005 12 9 MWEA050132 120051202A3620R2192 RELAY DOUG MD88 MD88 3023688NM RIGHT INOPERATIVE A MWEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL31601ME 49762 RIGHT AIR CONDITIONING TEMPERATURE LOW LIGHT FOLLOWED BY THE RIGHT ICE PROTECTION. REMOVED AND REPLACED RELAY. 2L72 4F RTA6WE 20051209000412005120900041NM 2005 12 9 QXEA200501575 120051110A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX - NR 1 SEAT TRACK HAS CORROSION IN BOTTOM OF CHANNEL AT X282, X297 AND X377. REPAIRED IAW RD 8-53-1342, DHC-8-200 SRM 51-20-16 AND 51-20-36 2H72 4T RTA13NM 20051209000622005120900062SO 2005 12 9 LR7A05184 120051109A53403561221R ATTACH FITTING LKHEED382 382G 526414USO FS437 DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2549 4606 DURING C-7 CHECK PER HC5313, FOUND ON REMOVAL OF CHINE CAP ASSY FOR REPLACEMENT, CHINE CAP ATTACH FITTING WITH OVER SIZED HOLE AT FS437, RBL58. REPLACED CHINE CAP ATTACH FITTING IAW DRG 3317816, NR 0510. 2H74 4T A1SO 20051209000652005120900065SO 2005 12 9 LR7A05187 120051109A5753 SPAR CAP LKHEED382 382G 526414USO FLAP STA 177 CORRODED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2549 4606 DURING C-7 CHECK PER HC5712, FOUND CORROSION ON LWR RT IB FLAP SPAR CAP BEYOND LIMITS, FLAP STA 177-213. REPAIRED FLAP SPAR CAP IAW DRG R05-28-06, MEA 382-27-05-095, NR 0566. 2H74 4T A1SO 20051209000702005120900070SO 2005 12 9 LR7A05192 120051109A5315 FLOORBEAM LKHEED382 382G 526414USO BS 588 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2549 4606 DURING C-7 CHECK PER SB 382-57-85, FOUND BEAM CRACKED 2ND HOLE FROM TOP INBOARD, 2 EA, 3/4 INCH RUNNING UPWARD AND FORWARD AND 7/8 INCH RUNNING DOWN AND AFT TO EDGE OF BEAM, FS588, WL250, RBL62. REPAIRED BEAM IAW DRG R05-028-08, MEA 382-53-05-100, NR 0669. 2H74 4T A1SO 20051209000902005120900090EA 2005 12 9 QXEA200501639 120051031A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA BS 350 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, LOWER FUSELAGE EXTERNAL SKIN AT STATION 350 STRINGER 21R-22R HAS CHAFFED SKIN AND GOUGES BY POTABLE WATER SERVICE PANEL. MAINTENANCE REPAIRED IAW EA R-53-398 AND REO 670-53-21-143. FINISH RESTORED. 2L72 4F RTA21EA 20051209001022005120900102WP 2005 12 9 05FDEA04132 120051205A5310 REPAIR DOUG DC10 DC1030F 3023504WP FUSLEAGE PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 DISCREPANCY PERFORMED INSPECTION IAW EO NR 8-5100-7-5001-P1 FOUND DOUBLER DIMENS 14" BY 4" RT, EXTERNAL FUSELAGE STA 959 LONG 40 TO LONG 42. PERFORMED A GVI OF REPAIR IAW SRM 53-50-00 FIG 2 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001-1P E3, RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VOL 2 PAR 33. 2L73 4F RTA22WE 20051209001032005120900103WP 2005 12 9 05FDEA04133 120051205A5520 REPAIR DOUG DC10 DC1030F 3023504WP ELEVATOR PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 UPPER LT DETACHABLE ELEVATOR FOUND 1 EXTERNAL DOUBLER REPAIR AT XE 60 DIMENSION 7" BY 6.5. PERFORMED INSPECTION ON REPAIR DOUBLER IAW SRM 55-10-00 VOL 1 FIG 8 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EONR 8-5100-7-5001 P2 E3, RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VOL 2 PAR 33 AND 24. 2L73 4F RTA22WE 20051212000092005121200009WP 2005 12 12 ABXA050339 120051019A5320 STIFFENER DOUG DC8 DC863F 302198FWP FS 980 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 LOWER AFT CARGO FORWARD BULKHEAD LEFT SIDE FRAME CORRODED AT BOTTOM STA 980, 30 LEFT. REMOVED OLD STIFFENER IAW DC8 SRM 51-3-1 AND 51-1-21 WHICH HAD CORROSION OUT OF LIMITS IAW DC8 SRM 53-2-0 AND REPLACED WITH NEW STIFFENER PO NR 1122166 IAW DC8 SRM 51-1-21 AND 51-3-1. 2L74 4F 4A25 20051212000142005121200014WP 2005 12 12 UPS05845864 120051207A3350 BATTERY PACK DOUG DC8 DC873F 302199FWP EMERGENCY EXIT ACTIVATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 EMERGENCY EXIT LIGHTS DIM. REMOVED AND REPLACED BATTERY PACK IAW MM 33-50-01. 2L74 4F RT4A25 20051212000272005121200027WP 2005 12 12 AALA20050792 120051203A3350P4010051111 MODULE DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21225AA 49175 LGA - EMERGENCY LIGHTS IN AFT CABIN INOPERATIVE. REPLACED LIGHT CONTROL MODULE FOR EMERGENCY LIGHTS IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051212000352005121200035WP 2005 12 12 AALA20050795 120051206A3350 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21482AA 49675 SAT - FORWARD EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK AND CHARGER FOR FORWARD EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051212000502005121200050SO 2005 12 12 MASA200500461 120050612A3040 HEATER EMB 145 EMB145LR 3260212SO WINDSHIELD FIRE A MASAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SW07827MJ363 145217 AIR SHUTTLE 2794 FROM CLT TO CRW, HAD VISIBLE FLAMES COMING FROM THE F/O WINDSHIELD HEAT WIRING AREA ON APPROACH. THE CREW USED THE EXTINGUISHER TO STOP THE FLAMES AND DECLARED AN EMERGENCY ON LANDING AND LANDED SAFELY. CONTRACT MX FOUND EVIDENCE OF EXTREME HEAT TO THE POSITIVE WIRE TO THE F/O WINDSHIELD HEAT WITH ASSOCIATED MELTING OF WIRE INSULATION. AIRCRAFT FERRIED TO CLT AND WINDSHIELD, HEAT CONTROLLER, BURNED WIRING REPLACED. 2L72 4T RTT00011AT 20051212000532005121200053EA 2005 12 12 REXA200500145 120051205A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A REXAO OTHER J WARNING INDICATION APAPPROACH 1 SO258745B 7745 FLAPS FAILED FROM 0 DEGREES. PERFORMED QUICK REFERENCE HANDBOOK (QRH). LANDING UNEVENTFUL. SYSTEM REST AND PLACED ON 72 HOUR WACTH PER AD 98-20-01. 2L72 4F RTA21EA 20051212000592005121200059NM 2005 12 12 QXEA200501586 120051110A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM BS 343 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX - RIGHT OUTBOARD SEAT TRACK NR 10 HAS CORROSION INSIDE CHANNEL AT STATION 343. REPAIRED IAW RD 8-53-1342, DHC-8-200 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20051212000602005121200060NM 2005 12 12 QXEA200501587 120051110A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX - RIGHT OUTBOBARD SEAT TRACK NR 10 HAS CORROSION INSIDE CHANNEL AT LUG HOLE AREA AT STATION X365. REPAIRED IAW RD 8-53-1342, DHC-8-200 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20051212000612005121200061NM 2005 12 12 QXEA200501588 120051110A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM BS 376 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX - RIGHT OUTBOARD SEAT TRACK NR 10 HAS PITTING CORROSION THAT IS APPROXIMATELY .017' DEEP INSIDE CHANNEL AT STATION X376. REPAIRED IAW RD 8-53-1342, DHC-8-200 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20051212000672005121200067NM 2005 12 12 QXEA200501594 120051113A5540 HINGE DHAV DHC8 DHC8202 2809007NM RUDDER CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX - LOWER RUDDER HINGE IS CHAFED APPROXIMATELY .020" DEEP ON TOP SURFACE. REPAIRED IAW DHC-8-200 RD 8-55-019. 2H72 4T RTA13NM 20051212000682005121200068NM 2005 12 12 QXEA200501595 120051112A5310 RIVET DHAV DHC8 DHC8202 2809007NM FUSELAGE IMPROPER A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX - RIVET IS NOT SHOT CORRECTLY AT STRINGER 22 CLEAT, STATION 426. REMOVED AND INSTALL RIVET IAW DHC-8-200 SRM 51-40-00. 2H72 4T RTA13NM 20051212000692005121200069WP 2005 12 12 ABXA050322 120051122A53209910023313 STRUCTURE DOUG DC9 DC941 302207NWP E/E COMP CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23954AX 47612 FOUND CORROSION AND CRACK IN SUBFLOOR, UNDER FIRST OFFICER'S INBOARD SEAT TRACK. CUT OUT CRACK AND CORROSION IN SUBFLOOR, INSTALLED DOUBLER IAW DC9 SRM 53. 2L72 4F A6WE 20051212000702005121200070WP 2005 12 12 ABXA050323 120051123A53105917463503 DOOR FRAME DOUG DC9 DC941 302207NWP CABIN CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23954AX 47612 AFT ENTRY DOOR JAMB CRACKED UNDER SEAL DEPRESSOR JUST BELOW UPPER RIGHT CORNER. REPAIRED AFT ENTRY DOOR JAMB UNDER SEAL DEPRESSOR BELOW UPPER RIGHT CORNER IAW DC9 SRM 53-01. 2L72 4F A6WE 20051212000712005121200071WP 2005 12 12 ABXA050324 120051128A5344591412161 HINGE BRACKET DOUG DC9 DC941 302207NWP PAX DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23954AX 47612 CRACK AT FORWARD BOTTOM EDGE OF FORWARD ENTRY DOOR BELOW BOTTOM HINGE BRACKET. REPAIRED CRACK PAN WITH REPAIR IAW DC9 SRM 52-05. 2L72 4F A6WE 20051212000732005121200073WP 2005 12 12 ABXA050326 120051128A531339240271 LONGERON DOUG DC9 DC941 302207NWP BS 648 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23954AX 47612 FOUND CORROSION LONGERON 30 END CAP AFT OF PRESSURE BULKHEAD TO FS 648 APPROXIMATELY LEFT KEEL AREA. REMOVED AND REPLACED END CAPS IAW DC9 SRM. 2L72 4F A6WE 20051212000742005121200074WP 2005 12 12 ABXA050327 120051128A5312592481679 BULKHEAD DOUG DC9 DC941 302207NWP BS 644 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23954AX 47612 FORWARD LOWER CARGO STA 644 BULKHEAD SKIN WAS BULGED FROM LONGERON 30 TO LONGERON 29 LEFT, NUMEROUS RIVETS SHEARED. REMOVED AND REPLACED FINGER DOUBLER IAW DC9 SRM 51-30-1 AND 51-30-5. 2L72 4F A6WE 20051212000752005121200075WP 2005 12 12 ABXA050328 120051128A532039240261N FITTING DOUG DC9 DC941 302207NWP LONGERON CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23954AX 47612 CORROSION RIGHT KEEL AFT OF PRESSURE BULKHEAD LONGERON 26 RIGHT END CAP. REMOVED AND REPLACED FITTING IAW DC9 SRM 51-30-5. 2L72 4F A6WE 20051212000782005121200078WP 2005 12 12 ABXA050331 120051128A53305911412221 SKIN DOUG DC9 DC941 302207NWP BS 617 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23954AX 47612 BROKEN FASTENER HEADS AND BULGE IN FUSELAGE SKIN FS 617, LONGERON 30 - LONGERON 29 RIGHT. REPAIRED AREA IAW DC9 SRM 53-04. 2L72 4F A6WE 20051212000802005121200080EA 2005 12 12 REXA200500150 120051206A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A REXAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO258894A 7894 FLAPS FAILED AT 8 DEGREES WHEN SELECTED TO 20 DEGREES. LANDING UNEVENTFUL. REMOVED AND REPLACED FLAP ELECTRICAL CONTROL UNIT (FECU) IN ACCORDANCE WITH AIRCRAFT MAINTENANCE MANUAL(AMM). OPERATIONALLY TEST AND CHECK RIGGING OF BRAKE POSITON SENSOR UNIT (BPSU) IAW AMM. AIRCRAFT OKAY FOR SERVICE. 2L72 4F RTA21EA 20051212000812005121200081EA 2005 12 12 REXA200500147 120051206A2750 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS OUT OF RIG A REXAO OTHER J WARNING INDICATION APAPPROACH 1 SO258745B 7745 FLAPS FAILED AT 0 DEGREES WHILE ON APPROACH. PERFORMED QUICK REFERENCE HANDBOOK(QRH). LANDING UNEVENTFUL. FOUND LEFT AND RIGHT BRAKE AND POSITION SENSOR UNIT (BPSU) OUT OF RIG. RIGGED BOTH BPSU IN ACCORDANCE WITH AIRCRAFT MAINTENANCE MANUAL. OPERATIONALLY CHECKS GOOD. 2L72 4F RTA21EA 20051212000822005121200082EA 2005 12 12 REXA200500148 120051206A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A REXAO OTHER J WARNING INDICATION APAPPROACH 1 SO258515F 7515 FLAPS FAILED AT 0 DEGREES ON APPROACH. LANDING UNEVENTFUL. INSPECTED, RESET AND PERFORMED OPERATIONAL CHECK. PLACED ON 72 HOUR WATCH PER AD 98-20-01. 2L72 4F RTA21EA 20051212000842005121200084SO 2005 12 12 MASA200500330 120050504A212014522273401 DUCT EMB 145 EMB145LR 3260212SO NR 2 PACK ODOR A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW07860MJ 145773 ASH 2667 PHF TO CLT, THE CREW HAD THE NR 2 PACK PRODUCING A BURNING SMELL WHILE THE APU WAS SUPPLYING BLEED AIR ON THE GROUND. MAINTENANCE REMOVED AND REPLACED THE HIGH PRESSURE DUCTS AND OVERTEMP SWITCH. THE AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. 2L72 4T RTT00011AT 20051212000852005121200085EA 2005 12 12 REXA200500142 120051202A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A REXAO OTHER J WARNING INDICATION APAPPROACH 1 SO258884E 7884 FLAPS FAIL ON APPROACH WHEN SELECTED DOWN. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD 98-20-01 2L72 4F RTA21EA 20051212000862005121200086EA 2005 12 12 REXA200500146 120051206A2751 DETECTION SYS CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A REXAO OTHER N FALSE WARNING APAPPROACH 1 SO258884E 7884 FLAPS FAIL WHEN FLAPS 45 DEGREES WAS SELECTED. PEFORMED QRH. LANDING UNEVENTFUL. REMOVED AND REPLACED SKEW DETECTION UNIT IN ACCORDANCE WITH AIRCRAFT MAINTENANCE MANUAL. OPERATIONALLY CHECKS GOOD. OKAY FOR SERVICE. 2L72 4F RTA21EA 20051212000872005121200087SO 2005 12 12 GLBA2005603 120051129A2131 CONTROLLER EMB 120 EMB120ER 3260203SO CABIN PRESSURE MALFUNCTIONED A GLBAG O2 MASK DEPLOYED SJ AFFECT SYSTEMS WARNING INDICATION CRCRUISE 1 NM03297UX 120297 25K AT REDUCED POWER FOR CRUISE, CABIN ALTITUDE ROSE RAPIDLY, SWITCHED PACKS TO NORMAL, CABIN ALTITUDE STABILIZED FOR 5 MINUTES THEN LOST CABIN CONTROL, OXYGEN MASKS DEPLOYED, MEL'D SYSTEM CONTROL NR 22377. 2L72 4T RTA31SO 20051212000882005121200088NE 2005 12 12 GLBA20050604 320051128A6111RFC11M1R6A BLADE EMB 120 EMB120ER 3260203SO HAMSTD14RF 14RF9 NE RT PROPELLER DAMAGED A GLBAO OTHER O OTHER TXTAXI/GRND HDL 1 NM03299UX 8263 120299 RIGHT PROPELLER STRUCK TAXIWAY LIGHT, REPLACED RIGHT PROPELLER BLADE IN NR 4 POSITION AND PLACED ENGINE ON SPECIAL CHIP DETECTION INSPECTION FOR 50 HOURS 2L72 4T RTA31SO 6 CP11NE 20051212000892005121200089SO 2005 12 12 GLBA20050605 120051130A2170 A/C PACK EMB 120 EMB120ER 3260203SO ODOR A GLBAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 NM0371GL 120071 SMOKE ANNUNCIATOR ILLUMINATED THEN CLEARED, PAC'S SMELL LIKE THEY ARE ABOUT TO FAIL IN CLIMBS AND DESCENTS, PERFORMED CHECK OF PACK SYSTEM, NO DEFECTS FOUND, RETURNED TO SERVICE. 2L72 4T RTA31SO 20051212000932005121200093NM 2005 12 12 SWAA053894 120051208A57536546435 SKIN BOEING737 7373H4 1384600NM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29655WN 28400 DURING SCHEDULED SERVICE CHECK, FOUND LT WING OTBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM. 2L72 4F RTA16WE 20051212000942005121200094NM 2005 12 12 SWAA053895 120051207A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 18L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051212000952005121200095NM 2005 12 12 SWAA053896 120051207A53306545768 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 357, STR 15L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051212000962005121200096NM 2005 12 12 SWAA053897 120051207A53306545765 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 516, STR 15R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051212000972005121200097NM 2005 12 12 SWAA053898 120051207A335065C27095 BATTERY PACK BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29746SW 29798 DURING SCHEDULED MV2 CHECK, FOUND LT FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20051212000982005121200098CE 2005 12 12 AMWA71073 120050529A77141143800663 INDICATOR BEECH 1900 1900D 1154162CE PROPELLER FAILED A AMWAC ABORTED TAKEOFF O OTHER TXTAXI/GRND HDL 1 CE07133YV9292 9292 UE133 UPON TAXI OFF ROLL, CREW OBSERVED LEFT PROP RPM INDICATOR STUCK AT 1300 RPM. ABORTED TAKEOFF AND RETURNED TO GATE WITH NO FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED PROP TACH INDICATOR. 2L72 4T RTA24CE 20051212000992005121200099EA 2005 12 12 REXA200500152 120051207A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A REXAO OTHER J WARNING INDICATION APAPPROACH 1 SO258721B 7721 FLAPS FAIL AT 20 ON APPROACH, QRH FOLLOWED UNEVENTFUL LANDING. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD 98-20-01 2L72 4F RTA21EA 20051212001002005121200100WP 2005 12 12 IXXA0500127S 120050214A5210 SKIN DOUG DC8 DC871F 302199DWP FS 25.000 L-21R DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11821BX858952998 45811 DURING A ROUTINE C CHECK INSPECTION, RT FUSELAGE FORWARD PASSENGER ENTRANCE DOOR UPPER AFT JAMB PLATING WEAR DAMAGE AT STA FS 25.000, L-21R. MAJOR REPAIR ACCOMPLISHED REMOVAL OF DAMAGE. FABRICATED NEW SKIN, CLEANED, TREATED AND PRIMED AREA + NEW SKIN. APPLIED SEALANT TO FAYING SURFACES. INSTALLED NEW SKIN IAW DC8 SRM 52-1-0 PG 1, 52-3-1 FIG 1, 52-1-11, 51-1-21, 51-1-22. 2L74 4F RT4A25 20051212001012005121200101WP 2005 12 12 ABXA050312 120051016A5311 FRAME DOUG DC8 DC863F 302198FWP FS 120 TOOL DAMAGE A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 FORWARD CARGO BAY DRILL START IN FRAME RADIUS, STA 120, ABOVE LONGERON 31 RIGHT, RIGHT BUTT LINE 33. ORIGINAL MATERIAL 7075-T6 0.090" PER DC8 SRM 53-4-1, PG 125. FABRICATED REPAIR ANGLE FROM 7075-0 FIG 2, HEAT TREATED IAW DC8 SRM 51-1-4, SHIM FROM 7075-T6 0.050" PO NR 1118787, TREATED IAW LWR 200302015, PRIMED IAW 51-1-8, INSTALLED DOUBLER AND SHIM IAW 51-1-20D PG 1 AND 51-1-21. 2L74 4F 4A25 20051212001022005121200102WP 2005 12 12 ABXA050311 120051024A53305758878 FINGER DOUBLER DOUG DC8 DC863F 302198FWP FS 1540-1560 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 CORROSION FOUND ON FINGER DOUBLER AT STA 1540, LONGERON 31 RIGHT, RIGHT BUTT LINE 25. REPAIRS ACCOMPLISHED AT STA 1540 - 1560, LONGERON 31 RIGHT IAW REA D853-52525. 2L74 4F 4A25 20051212001032005121200103WP 2005 12 12 ABXA050313 120051101A53305759321501 DOUBLER DOUG DC8 DC863F 302198FWP FS 683 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DOUBLER CORRODED TOP OF WING CENTER SECTION PRESSURE DECK, STA 683, LONGERON 22 LEFT, LEFT BUTT LINE 10. REMOVED CORROSION, FABRICATED AND INSTALLED DOUBLER IAW DC8 SRM 51-1-8 AND REA D853-52529. 2L74 4F 4A25 20051212001042005121200104WP 2005 12 12 ABXA050314 120051016A5340 ATTACH ANGLE DOUG DC8 DC863F 302198FWP FS 160 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 FORWARD CARGO BAY DENT ON GILLINER ATTACH ANGLE, STA. 160, BETWEEN LONGERON 36 LEFT TO 35 LEFT. REMOVED DENT IN FORWARD CARGO BAY GILLINER ATTACH ANGLE STA 160, LONGERON 36 LEFT - 35 LEFT, FOUND TO BE CRACKED, REPAIRED. REMOVED GILLINER ATTACH ANGLE IAW DC8 SRM 51-1-21, WELDED ATTACH ANGEL IAW ABX PROCESS STDS MANUAL 900-7-2-1, TREATED IAW LWR 200302015-4/15/O3, PRMIED IAW DC8 SRM 51-1-8. REINSTALLED GILLINER ANGLE IAW DC8 SRM 51-1-20D. 2L74 4F 4A25 20051212001052005121200105WP 2005 12 12 ABXA050315 120051017A7110 COWLING DOUG DC8 DC863F 302198FWP NR 1 ENGINE SCORED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 NR 1 ENGINE, OUTBOARD FORWARD COWL HOLD OPEN ROD HAD SCORED INNER SIDE OF COWL. REMOVED PREVIOUS REPAIR, FABRICATED NEW DOUBLER, AND APPLIED COMPOSITIE REPAIR IAW DC8 SRM 51-1-9A, TREATED DOUBLER IAW LWR 200302015 AND PRIMED IAW DC8 SRM 51-1-8. 2L74 4F 4A25 20051212001072005121200107CE 2005 12 12 73619 120051019A3210 BOLT BEECH 1900 1900D 1154162CE MLG UNKNOWN A AMWAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE07127ZV UE127 AFTER TAKEOFF, CREW UNABLE TO RETRACT LANDING GEAR. RETURNED TO FIELD WITH NO FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED BOLT IN RIGHT SQUAT SWITCH. 2L72 4T RTA24CE 20051212001112005121200111 2005 12 12 IXXA0500120O 420051129A3422 HSI DOUG DC8 DC871F 302199DWP COCKPIT INOPERATIVE A IXXAA UNSCHED LANDING O OTHER CLCLIMB 1 SW11829BX8971340 45994387 ON CLIMB-OUT FROM KTOL, FO'S ADI/HSI WAS INOP. CREW RETURNED AIRCRAFT TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET C/B AND GYRO PER ALL APPLICABLE MANUALS AND NO DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20051212001142005121200114EA 2005 12 12 QXEA200501653 120051031A5743 FITTING CNDAIRCL600 CL6002C10 1390015EA MLG TRUNNION DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, RIGHT WING STIFFENING WEB ON THE OUTBOARD SIDE OF MAIN GEAR TRUNNION FITTING WAS INADVERTENTLY CHAMFERED. MAINTENANCE REPAIRED TRUNNION FITTING IAW EA R-57-131 AND REO 670-57-21-021. 2L72 4F RTA21EA 20051212001172005121200117EA 2005 12 12 QXEA200501665 120051031A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 809-830 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, LEFT SIDE SEAT RAIL AT STATION 809-830 HAS AREAS OF CORROSION. MAINTENANCE REPAIRED CORRODED AREAS IAW REO 670-53-00-013. RESTORED FINISH. 2L72 4F RTA21EA 20051212001182005121200118EA 2005 12 12 QXEA200501650 120051031A5311 FRAME CNDAIRCL600 CL6002C10 1390015EA BS 939 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC- DURING C3 CHECK, FUSELAGE INTERIOR UPPER FRAME AT STATION 939 STRINGER 3L HAS A GOUGE ON THE ATTACH ANGLE FOR INTERCOSTAL IN RADIUS. MAINTENANCE REPAIRED IAW CRJ-700 SRM 53-51-06-101-001-A01. 2L72 4F RTA21EA 20051212001192005121200119EA 2005 12 12 QXEA200501663 120051031A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 713-760 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, LEFT SIDE SEAT RAIL AT STATION 713-760 HAS AREAS OF CORROSION. MAINTENANCE REPAIRED AREAS IAW CRJ-700 REO 670-53-00-013. RESTORED FINISH. 2L72 4F RTA21EA 20051212001202005121200120EA 2005 12 12 QXEA200501651 120051031A5743 FITTING CNDAIRCL600 CL6002C10 1390015EA MLG TRUNNION DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK. LEFT WING STIFFENING WEB ON OUTBAORD SIDE OF MAIN GEAR TRUNNION FITTING BETWEEN AUX ACTUATOR AND AUX SPAR WAS INADVERTENTLY CHAMFERED. MAINTENANCE REPAIRED FITTING IAW EA R-57-131 AND REO 670-57-21-021. 2L72 4F RTA21EA 20051212001212005121200121EA 2005 12 12 QXEA200501652 120051031A2520 SEAT CNDAIRCL600 CL6002C10 1390015EA CABIN DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - IN C3 CHECK, PASSENGER SEAT NR 5 LEFT OUTBOARD TRAY TABLE CRACKED. MAINTENANCE REPLACED TRAY IAW CRJ-700 CMM 25-21-69. 2L72 4F RTA21EA 20051212001222005121200122EA 2005 12 12 QXEA200501662 120051031A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 677-712 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, LEFT SIDE SEAT RAIL AT STATION 677-712 HAS CORROSION. MAINTENANCE REPAIRED CORROSION IAW REO 670-53-00-013. RESTORED FINISH. 2L72 4F RTA21EA 20051212001232005121200123EA 2005 12 12 QXEA200501655 120051031A5330 RIVET CNDAIRCL600 CL6002C10 1390015EA SKIN MISINSTALLED A QXEAK NONE W INADEQUATE Q C ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, FUSELAGE INTERIOR AT STATION 581 STRINGER 6R HAS A RIVET UNDER DRIVEN. MAINTENANCE REPLACED THE RIVET IAW CRJ-700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20051212001242005121200124EA 2005 12 12 QXEA200501656 120051031A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 916-920 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC- DURING C3 CHECK, RIGHT SIDE SEAL RAIL STATION 916 TO 920 HAS GOUGES ON RAIL. MAINTENANCE REPAIRED IAW REO 670-53-00-013. RESTORED FINISH. 2L72 4F RTA21EA 20051212001272005121200127EA 2005 12 12 QXEA200501661 120051031A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 677-712 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, RIGHT SIDE SEAT RAIL AT STATION 677-712 HAS CORROSION ON INNER SEAT ATTACH LUG. MAINTENANCE REMOVED CORROSION IAW REO 670-53-00-013. RESTORED FINISH. 2L72 4F RTA21EA 20051212001282005121200128WP 2005 12 12 ABXA050317 120051201A3260 INDICATION SYS DOUG DC9 DC931 3022065WP MLG MALFUNCTIONED A ABXAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 GL23947AX 47004 ON FINAL APPROACH, GEAR DOOR OPEN LIGHT REMAINED ON WITH 3 GREEN INDICATIONS. WENT AROUND ON APPROACH, RECYCLED GEAR, GEAR DOOR OPEN LIGHT EXTINGUISHED. JACKED AIRCRAFT, CYCLED LANDING GEAR SEVERAL TIMES, NO DEFECTS NOTED. OPS CHECKED GOOD, REF AMM 32-60-00. 2L72 4F A6WE 20051212001292005121200129NM 2005 12 12 DHL2005749023 120051107A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01749DH 22013 DISCREPANCY NR113286 AS FOLLOWS; GAIN INTERNAL ACCESS TO 3 REPAIRS ON EMP SKIN AT AIR START DOOR, LT AIRSTAIR CUT OUT AND RT AIRSTAIR CUT OUT. REMOVED AIRSTAIRS CUT OUT TORQUE BOX WEB FOR ACCESS IAW B727 SRM 51-30-2 AND FOUND RT SKIN ATTACH ANGLE CRACKED. REMOVED AND REPLACED FASTENERS IN THE DOUBLERS 3EA IAW B727 SRM 57-30-2. FABBED NEW ANGLE MAT 2024T3 .040 PO5070564 DIM 10" BY 3 1/2" IAW B727 SRM 53-10-2 FIG 5 AND 51-20-1 TREATED AND PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED PARTS IAW B727 SRM 51-30-2. REINSTALLED TORQUE BOX AFT AIRSTAIR WEB B727 SRM 51-30-2. 2L73 4F RTA3WE 20051212001302005121200130NM 2005 12 12 SWAA053853 120051202A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 747, RBL 10. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051212001312005121200131NM 2005 12 12 SWAA053854 120051202A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 767, RBL 9 TO RBL 11. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051212001322005121200132NM 2005 12 12 SWAA053855 120051202A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 807, RBL 1. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051212001332005121200133NM 2005 12 12 SWAA053856 120051202A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 867, RBL 9. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051212001342005121200134NM 2005 12 12 SWAA053857 120051130A57536546435 SKIN BOEING737 7373H4 1384600NM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29637SW 27710 DURING SCHEDULED C3 CHECK, FOUND LT WING OTBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM. 2L72 4F RTA16WE 20051212001372005121200137NM 2005 12 12 SWAA053860 120051204A534065C27314 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29671SW 23785 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 500A, STR 16L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051212001422005121200142NM 2005 12 12 SWAA053865 120051202A56105893543130 WINDOW BOEING737 7377H4 1384404NM COCKPIT ARCED A SWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW29710SW 27844 R1 COCKPIT WINDOW ARCED AND CRACKED. REMOVED AND REPLACED R1 WINDOW AND HEAT CONTROLLER PER MM. 2L72 4F RTA16WE 20051212001442005121200144NM 2005 12 12 QXEA200501747 120051204A2760 SPOILER BOMBDRDHC8 DHC8402 1390042NM LEFT UNKNOWN A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09405QX 4047 SEA FLT NR 2316: DURING, AFTER START, CHECKLIST LT INBD SPOILER SHOWS UP ON PFS. NO OTHER CAUTION LIGHT ON. MX FOUND NO FAULTS IN CDS, EPCU, OR PROX SENSOR BOX. PLACED HYD PRESS ON NR 1 AND NR 2 SYSTEMS. WITH PWR LEVERS AT DISC TO FLT IDLE, DISCREPANCY EXITS. WHEN PLA MOVED GREATER THAN 12 DEG ABOVE FLIGHT IDLE, ALL SPOILER RETRACT. AFTER THIS ACTION, SPOILERS ACTED NORMALLY THROUGHOUT ALL PLA ANGLES AND COMBINATIONS OF FLT/TAXI SWITCH. A/C POWER WAS NEVER RESET. PROBLEM DOES NOT RETURN. C/W OPS TEST OF THE ROLL SPOILER SYSTEM IAW Q400 MM TASK 27-61-00-710-801 AND FUNC TEST OF THE GROUND SPOILERS SYSTEM IAW Q400 MM TASK 27-62-00-720-801. NO FAULTS NOTED. OPS CHECK GOOD. NO PARTS REPLACED. A/C RETUR2H72 4T RTA13NM 20051212001462005121200146WP 2005 12 12 IXXA0500122S 120050303A5730 REPAIR DOUG DC8 DC871F 302199DWP XF 385.00 IMPROPER A IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW11821BX858952998 45811 DURING A ROUTINE C CHECK INSPECTION, LT WING OUTBOARD FLAP LOWER AFT PLATING INTERIM REPAIR AROUND STA XF 385.00. MAJOR REPAIR ACCOMPLISHED BY REMOVING EXISTING REPAIR IAW DC8 SRM 51-1-11 PG1, DC8 SRM 51-3-0 PG1. REMOVED DAMAGED AREA IAW DC8 SRM 57-2-5N FIG 2 SHEET 3,4 PERFORMED NDT INSPECTION IAW NDT SPM PART 06-10-01-001. FABRICATED EXTERNAL REPAIR DOUBLER IAW DC8 SRM 57-2-5 FIG 2 SHEET 3,4. CLEANED, TREATED AND PRIMED AREA IAW DC8 SSRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PAGE 9. INSTALLED DOUBLER IAW DC8 SRM 57-2-5 F1G 2 SHEET 3, 4 DC9 SR, 51-1-9, DC8 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20051212001472005121200147WP 2005 12 12 IXXA0500123S 120050303A5711 SPAR CAP DOUG DC8 DC871F 302199DWP RT WING CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11821BX858952998 45811 DURING A ROUTINE C CHECK INSPECTION, FOUND RT WING UPPER FRONT SPAR CAP STRUCTURE CRACK DAMAGE BETWEEN STA XFS-6 CAP. MAJOR REPAIR ACCOMPLISHED BY REMOVING FASTENERS. REMOVING CORROSION FROM SLANT PANEL UPPER CAP AND FOUND OUT OF LIMITS. CLEANED, TREATED AND PRIMED AREA. INSTALLED DOUBLER, REMOVED UPPER SPAR CAP (DAMAGED). REMOVED STIFFENER AND PERFORMED NDT INSPECTION. APPLIED SEALANT TO FAYING SURFACES AND INSTALLED DOUBLER, ANGLE DOUBLER. INSTALLED KIT, TORQUE AND LEAK CHECKED IAW S/B DC8-57-072 R03 DWG DACO 5892075, CN1, DC8 SRM 51-1-8, 51-1-11, 51-1-15, 51-1-20D, 51-1-26, 51-3-0, 51-3-1, 51-3-2, DPS 1.05-8, 3.67-3, 2.5. 2L74 4F RT4A25 20051212001482005121200148WP 2005 12 12 IXXA0500124S 120050223A5730 REPAIR DOUG DC8 DC871F 302199DWP XW87.00-XW 91. IMPROPER A IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW11821BX8589536255 45811 DURING A ROUTINE C CHECK, INSPECTION FOUND LT WING INBOARD FLAP UPPER FORWARD PLATING INTERIM REPAIRS BETWEEN STA XW 87.000 AND XW 91.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF EXISTING REPAIR, AND REMOVED PLATING SEGMENT. PERFORMED NDT INSPECTION AND FABRICATED NEW PLATING SEGMENT + INTERNAL SPLICE + EXTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND NEW REPAIRED PARTS INTERNAL PART. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS IAW SEMAN DWG ED-3845 AND FAA FORM 8110-3 NR 05019, DC8 SRM CHAPTERS 51-1-11, 51-1-20D, 51-1-21, 51-1-22, 51-1-26, 51-3-1, 51-3-2. 2L74 4F RT4A25 20051212001512005121200151WP 2005 12 12 IXXA0500128S 120050213A5730 REPAIR DOUG DC8 DC871F 302199DWP XW2.00 &XW91.00 DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11821BX858952998 45811 DURING A ROUTINE C CHECK INSPECTION, RT WING INBOARD FLAP AFT UPPER PLATING INTERIM REPAIRS AND DENT DAMAGE BETWEEN STA XW 2.00 CANT AND XW 91.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF DAMAGED PLATING. FABRICATED NEW PLATING. CLEANED, TREATED AND PRIMED AREA AND NEW PLATING INTERNAL PART. APPLIED PRC SEALANT TO FAYING SURFACES. INSTALLED NEW PLATING IAW SEMAN DRAWING E. 2L74 4F RT4A25 20051212001522005121200152NM 2005 12 12 DHL2005749018 120051102A5330 FASTENER BOEING727 727200 138407ENM FUSELAGE UNKNOWN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01749DH 22013 COMPLY WITH AD90-24-11 PARA E PER S/B 727-53A0171 REV 2. REMOVED BLIND FASTENERS IN DOUBLER IAW B727 SRM 51-30-2. FAB REINFORCEMENT STRAP MAT 2024T3 .071 PO9002373 13 1/8" BY 2 1/4" AND 2 EA FILLER, 7075-T6 .063 PO 9001920 DIM 2 1/4"X 2 1/4" IAW S/B 727-53A0171. TREATED AND PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED PARTS AND REPLACED BLIND FASTENERS WITH HI-LOCKS IAW S/B 727-53A0171. COMPLIED WITH AD90-24-11 PARA E PER S/B 727-53A0171 REV 2. INSTALLATION OF DOUBLERS AND INCORPORATING VERTICAL REINFORCING STRAP ALSO SPACERS. 2L73 4F RTA3WE 20051212001532005121200153EA 2005 12 12 QXEA200501659 120051031A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 785-797 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, RIGHT SIDE SEAT RAIL AT STATION 785-797 HAS AREAS OF CORROSION. MAINTENANCE REMOVED CORROSION IAW CRJ-700 REO 670-53-00-013. 2L72 4F RTA21EA 20051212001552005121200155EA 2005 12 12 QXEA200501657 120051031A5350SH670375433 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 930-939 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, RIGHT SIDE OF SEAT RAIL AT STATION 930-939 CORRODED. MAINTENANCE REPAIRED CORROSION IAW REO 670-53-0013. 2L72 4F RTA21EA 20051212001582005121200158NE 2005 12 12 ASOA05915 220051126A7200 ENGINE AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE RIGHT MALFUNCTIONED A ASOAA UNSCHED LANDING J WARNING INDICATION DEDESCENT 1 SO11641AS 387 FLT 4086 - DURING DESCENT INTO ATL FROM AGS, AT APPROX 9,000 FEET THE CREW NOTICED THE RIGHT ENGINE TORQUE AT APPROX 20 PERCENT AND THE NP AT APPROX 35 PERCENT WITH ALL OTHER INDICATIONS SHOWING NORMAL WHICH WAS FOLLOWED BY A LARGE YAW TO THE RIGHT AND VIBRATIONS OCCURRED DURING THE OBSERVATION. THE QRH WAS COMPLIED WITH AND THE CREW SHUTDOWN THE RIGHT ENGINE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO MCN, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE ELECTRONIC ENGINE CONTROL, HYDRO-MECHANICAL UNIT AND THE FUEL PUMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T4 TRTA53EU E20NE 20051212001612005121200161EA 2005 12 12 SWIA200515936 120051117A5310 VERTICAL BEAM CNDAIRCL600 CL6002B19 1900309EA BS 409 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07411SW 7067 FUSELAGE; VERTICAL BEAM; LOWER O/B FLANGE IS CRACKED; FS 409.0 + 128; RBL - 18.0, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED LOWER O/B FLANGE IAW CRJ REO 601R-53-41-056 REV "C". 2L72 4F RTA21EA 20051212001662005121200166EA 2005 12 12 SWIA200515941 120051117A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA BS 625 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07411SW 7067 AFT EQUIPMENT COMP; INTERCOSTAL CLIP CRACKED; FS 625.00 STR 14L, ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIP IAW CRJ REO 601R-53-61-100 REV NC & REO 601R-53-61-422 REV NC. 2L72 4F RTA21EA 20051212001702005121200170EA 2005 12 12 SWIA200515945 120051115A5711 SPAR CNDAIRCL600 CL6002B19 1900309EA WS 148 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07416SW 7089 RT WING; LOWER WING PLANK; REAR SPAR LOWER FLANGE IS CRACKED, WS 148.00, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-57-21-130 REV G & REO 601R-57-21-131 REV NC & RII 57-401. 2L72 4F RTA21EA 20051212001712005121200171EA 2005 12 12 QXEA200501622 120051031A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA FUSELAGE GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, FUSELAGE SKIN EXTERIOR UNDER FAIRING 195DL HAS SKIN GOUGES FROM THE FAIRING SPLICE SUPPORT. MAINTENANCE BLENDED CHAFFED AREA IAW REO 670-53-00-014. RESTORED FINISH. 2L72 4F RTA21EA 20051212001722005121200172EA 2005 12 12 QXEA200501624 120051031A5280 STRUCTURE CNDAIRCL600 CL6002C10 1390015EA MLG DOOR DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, LEFT MAIN GEAR DOOR REBATE ON AFT SIDE OF GEAR WELL IS DAMAGED AND BENT. MAINTENANCE REPLACED THE REBATE ANGLE IAW CRJ-700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20051212001752005121200175NM 2005 12 12 QXEA200501741 120051204A3010 TRANSDUCER DHAV DHC8 DHC8202 2809007NM DEICE SYSTEM MALFUNCTIONED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09345PH 476 PDX - RIGHT DE-ICE PRESSURE GAUGE READS 30 AT ALL TIMES. LEFT SIDE NORMAL 18 PSI. MAINTENANCE BEGAN TROUBLESHOOTING OF DE-ICE PRESSURE. SUSPECT PRESSURE TRANSDUCER. PLACED ON MEL. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051212001772005121200177NM 2005 12 12 QXEA200501740 120051204A3040 WINDSHIELD DHAV DHC8 DHC8202 2809007NM COCKPIT MALFUNCTIONED A QXEAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 NM09374PH 530 IDA FLIGHT NR 2204, LEFT WINDSHIELD HOT CAUTION LIGHT ILLUMINATED. S ELECTOR POSITION WAS IN NORM. MAINTENANCE CONNECTED PILOTS WINDOW TO SPARE SENSOR. REFERENCE DASH8 200 AMM 30-41-00, PAGES 201-203, PARAGRAPH 3A 1 (B) AND PARAGRAPH 4A THROUGHT D. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051212001842005121200184EA 2005 12 12 REXA200500139 120051124A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A REXAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO258515F 7515 FLAP FAILURE ON APPROACH WHEN SELECTED TO 20. ABORTED APPROACH, FOLLOWED QRH WITH UNEVENTFUL LANDING. RESET SYSTEM AND PLACED FLAPS ON 72 HOUR WATCH PER AD 98-20-01. 2L72 4F RTA21EA 20051212001862005121200186CE 2005 12 12 1050921026072 120051020A5311 FRAME BEECH 1900 1900D 1154162CE BS 456 CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07146ZV UE146 FOUND FRAME ANGLE AT FS 456 CRACKED. MAINTENANCE INSPECTED AND NO CRACKS WERE NOTED. THEREFORE NO PARTS WERE USED. 2L72 4T RTA24CE 20051212001892005121200189EA 2005 12 12 SWIA200515958 120051205A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY MALFUNCTIONED A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07948SW 7789 "CARGO SMOKE" WARNING MSG APPEARED AND STAYED ILLUMINATED WHEN CARGO BOTTLE 2 WAS TESTED AT THE GATE. REPLACED AFT CARGO SMOKE DETECTOR. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051212001912005121200191EA 2005 12 12 SWIA200515960 120051203A2752 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 NM07440SW 7589 FLAPS FAIL CAUTION MESSAGE ON APPROACH. REPLACED MULTIPLE FLAP ACTUATORS IAW MM 27-53-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051212001932005121200193EA 2005 12 12 SWIA200515962 120051202A2797 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA STALL WARNING INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07983SW 7961 NO PUSHER DURING STALL TEST STALL FAIL CAUTION. INSTALLED A NEW PIN "K" AT CONNECTOR P66 ON WIRE CG247A20N AND REINSTALLED IN CONNECTOR IAW CRJ 200 M/M 20-10-00. OPERATIONAL CHECK GOOD OF STALL PROTECTION SYSTEM IAW CRJ 200 MM 27-35-00. 2L72 4F RTA21EA 20051212001952005121200195EA 2005 12 12 SWIA200515964 120051201A2750 DRIVE SHAFT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A SWIAO OTHER F FLT CONT AFFECTED APAPPROACH 1 NM07952SW 7805 FLAPS FAILED WHEN EXTENDED ON APPROACH. REPLACED NR 5 FLEX SHAFT IAW AMM 27-53-10. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051212001972005121200197NM 2005 12 12 SB05163 120051205A335020131A BATTERY PACK BOEING737 7374B7 1384702NM FORWARD CABIN DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US 24781 MCO - MAINTENANCE REPORTED THE EMERGENCY LIGHTS IN THE FORWARD CABIN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN THE FORWARD LEFT-HAND CABIN. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20051212001992005121200199WP 2005 12 12 05FDEA04196 120051209A5330 SKIN DOUG DC10 DC1010 3022110WP FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25568FE 47827 DURING AIRPLANE'S P TO F MODIFICATION FOUND STA 1139 STR 46-47 ON EXT SURFACE RIVETS WITH HEAD BROKEN AND SKIN BULGING. SUSPECT CORROSION. CUT OUT DAMAGED SKIN BETWEEN STR 45 AND STR 46 LT SIDE AT STA 1145, AND PERFORMED REPAIR IAW SRM 53-20-00 FIG 12 SH 4 & 5 VOL I. 2L73 4F A22WE 20051212002002005121200200WP 2005 12 12 05FDEA04197 120051209A5330 SKIN DOUG DC10 DC1010 3022110WP BS 1119 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25568FE 47827 DURING AIRPLANE' S P TO F MODIFICATION FOUND: STA 1119 BETWEEN STR 34-37 RT SIDE, EXT SURFACE WITH CORROSION AND SOME RIVETS WITH HEAD BROKEN. CUT SKIN BETWEEN STR 42-43 RT SIDE AT STA 1104, PERFORMED REPAIR IAW SRM 543-20-00 FIG 12 SH 6. 2L73 4F A22WE 20051212002022005121200202NM 2005 12 12 BB05102 120051203A3350 BATTERY BOEING767 7672B7 1385107NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19652US 24765 LEFT FLOOR EMERGENCY EXIT LIGHTS FROM ROW 20 TO AFT CABIN ONLY ILLUMINATE FOR FIVE SECONDS DURING TEST. MAINTENANCE REPLACED BATTERY PACK IN LIGHT CONTROL ASSEMBLY AT ROW 27. 2L72 4F RTA1NM 20051213000012005121300001WP 2005 12 13 05FDEA04199 120051209A5330 SKIN DOUG DC10 DC1010 3022110WP BS 348 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25568FE 47827 DURING AIRPLANE' S P TO F MODIFICATION FOUND: AT STA 348 STR 24-28 LT, BULGING ON SKIN WITH HL NOT INSTALLED CORRECTLY. REMOVED FRAME IAW SRM 51-33-01 AND SRM 51-35-01. PERFORMED SKIN AND DYE CHECK IAW CMM 20-30-02, INSTALLED FINGER DOUBLER IAW SRM 53-20-00 FIG 13 SH 2 VOL I. INSTALLED FRAME. FRAME, P/N ABA7037-9. 2L73 4F A22WE 20051213000022005121300002EU 2005 12 13 05FDEA04200 120051209A5610 WINDSHIELD AIRBUS300 A300F4605R 3930327EU COCKPIT CRACKED A FDEAA UNSCHED LANDING O OTHER CLCLIMB 1 SO25671FE 778 RT WINDSHIELD CRACKED. CREW NOTICED A SMALL CRACK DURING CLIMB, DID NOT HEAR OR FEEL ANYTHING HIT WINDOW. NOTICED WINDOW ARCHING, WINDOW HEAT WAS TURNED OFF, THEN THE WINDSHIELD SPIDER WEBBED. REMOVED AND REPLACED RT WINDSHIELD PANEL PER A300 AMM 56-11-11-4, NEEDS SEALANT CURE CHECK, WINDSHIELD WIPER INSTALLED AND OPS CHECK. REINSTALLED RT WINDSHIELD WIPER ARM. REMOVED AND REPLACED RT WINDSHIELD TEMP REGULATOR REF. 2L72 4F RTA35EU 20051213000042005121300004NM 2005 12 13 05FDEA04186 120051208A5313 STRINGER BOEING727 727200 138407ENM BS 950-1009 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 STR 28L BS 950-1009 HAS SEVERAL AREAS OF CORROSION. REMOVED DAMAGED STRINGER 28L FROM BS 950-1009 AND REPLACED PER SRM 53-10-3 FIG 1 AND SRM 51-30-02 2L73 4F RTA3WE 20051213000062005121300006NM 2005 12 13 05FDEA04188 120051208A5330 SKIN BOEING727 727100 1384036NM BS 480 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 REWORK REQUIRED, FROM NR01182. ACCOMPLISH REPAIR PER FEDEX ENGINEERING, BS 480, STR 26L-27L. *S/D* COMPLIED WITH FED EX EA 7-5330-95353, FOUND TO BE A MAJOR REPAIR. 2L73 4F RTA3WE 20051213000122005121300012NM 2005 12 13 USAA200512005 120051204A5330 SKIN BOEING737 737401 1384701NM BS 880 WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19424US 23991 A 3 INCH LONG WEAR AREA ON SKIN AT STA 880 FUSELAGE SKIN UNDER DORSAL FIN. INSTALLED REPAIR DOUBLER PER EA 97175 AND SRM 53-60-01 REPAIR 9. 2L72 4F RTA16WE 20051213000142005121300014WP 2005 12 13 05FDEA04137 120051205A5730 REPAIR DOUG DC10 DC1030F 3023504WP RT WING UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 RIGHT WING INBOARD FLAP FOUND DOUBLER REPAIR ON LOWER SKIN AT STA XIFH 155 DIMENIONS 3.25 INCH. PERFORMED A GVI OF REPAIR IAW SRM 57-00-01 FIG 4 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001-2P E3. RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 PAR 33 VOL 2. 2L73 4F RTA22WE 20051213000152005121300015WP 2005 12 13 05FDEA04138 120051205A5730 REPAIR DOUG DC10 DC1030F 3023504WP RT WING UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 RIGHT WING INBOARD FLAP FOUND DOUBLER REPAIR ON LOWER SKIN AT STA XIFH 189 DIMENIONS 8.5 X 5 INCH. PERFORMED A GVI OF REPAIR IAW SRM 57-00-01 FIG 4 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001-P2. RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 PAR 33 VOL 2. 2L73 4F RTA22WE 20051213000172005121300017WP 2005 12 13 05FDEA04140 120051205A5520 REPAIR DOUG DC10 DC1030F 3023504WP LT ELEVATOR UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 LEFT OUTBOARD ELEVATOR REPAIR ASSESSEMENT FOUND 1EA EXT DOUBLER ON LOWER SIDE AT XE 345 DIMENIONS 7 X 4.5 INCH. PERFORMED INSPECTION ON REPAIR DOUBLER IAW SRM 55-10-00 FIG 8 VOL 1, FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2 E3. RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 PAR 33 AND 24 VOL 2. 2L73 4F RTA22WE 20051213000182005121300018NM 2005 12 13 05FDEA04141 120051205A5753 SKIN BOEING BOEING727 727227 1384078NM ZONE 500 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE BN47 21489 LEFT OUTBOARD MID FLAP OUTBOARD LEADING EDGE HAS 2 EACH GOUGES. REPAIRED FLAP LEADING EDGE IAW FEDEX EA7-5750-92591. WINGS - LEFT WING OUTBOARD MID FLAP LEADING EDGE SKIN HAS GOUGES. THIS IS A MINOR REPAIR BY TIMCO MECH 7153 AND QC303. 2L73 4F A3WE 20051213000192005121300019NM 2005 12 13 CALA0500423 120051129A5315BAC1580940 FLOORBEAM BOEING737 737524 1384721NM STA 947 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713624 27528 INSPECTION FOUND FLOORBEAM FORWARD FLANGE CORRODED AT STA 947, LBL 10.5. A REPAIR STRAP WAS INSTALLED IAW SRM 53-00-51. 2L72 4F RTA16WE 20051213000202005121300020NM 2005 12 13 CALA0500424 120051129A5315BAC1518940 FLOORBEAM BOEING737 737524 1384721NM STA 947 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713624 27528 INSPECTION FOUND FLOORBEAM FORWARD FLANGE CORRODED AT STA 947, RBL 10.5, S18R. REPAIRED IAW SRM 53-60-51. 2L72 4F RTA16WE 20051213000222005121300022NM 2005 12 13 USAA051467 120051205A5315 FLOORBEAM BOEING737 7374B7 1384702NM STA 986.5 LBL8 TCORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 STA 986.5 LBL 8 TO EXTREME RT END. MAJOR REPAIR, REMOVED DAMAGED T-CAP, INSTALLED NEW REPAIRED PART IAW SRM 53-60-01 REV A. DEFECT SIZE: 1 INCH. 2L72 4F RTA16WE 20051213000232005121300023NM 2005 12 13 USAA051466 120051205A53406535352U14 STRINGER CLIP BOEING737 7374B7 1384702NM STA 727G, S4R CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 STA 727G, S4R CRACKED. MAJOR REPAIR, REPLACED TIE CLIP IAW SRM 51-10-02, DEFECT SIZE: .5. 2L72 4F RTA16WE 20051213000252005121300025NM 2005 12 13 USAA051464 120051205A5340 STRINGER CLIP BOEING737 7374B7 1384702NM S-4L, BS 727C CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 S-4L, BS 727C CRACK. MAJOR REPAIR, REPLACED WITH IDENTICAL PART IAW SRM 51-10-02, DEFECT SIZE: .25 INCH. 2L72 4F RTA16WE 20051213000302005121300030NM 2005 12 13 USAA051459 120051205A5534 SKATE ANGLE BOEING737 7374B7 1384702NM VERTICAL STAB WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 RT SIDE VERTICAL STAB AT FIN WL 0.0 HAS WEAR. MAJOR REPAIR, FABRICATED AND INSTALLED REPAIR PART IAW TR 53-20-05A, DEFECT SIZE: 1 INCH. 2L72 4F RTA16WE 20051213000312005121300031NM 2005 12 13 USAA051458 120051205A5315 FLOORBEAM BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 FLOORBEAM AT STA 344 BL 0 TO LBL 25 CORRODED. MAJOR REPAIR, BLENDED AREA, ALODINED AND PAINTED IAW SRM 53-10-51, DEFECT SIZE: .250 INCH. 2L72 4F RTA16WE 20051213000322005121300032NM 2005 12 13 USAA051457 120051205A5340 STRINGER CLIP BOEING737 7374B7 1384702NM BS727D, S5R CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 BS 727D, S5R CRACKED. MAJOR REPAIR, REMOVED AND REPLACED WITH IDENTICAL PART, IAW SRM 51-10-02, DEFECT SIZE: .18 INCH. 2L72 4F RTA16WE 20051213000342005121300034NM 2005 12 13 USAA051455 120051205A5340 STRINGER CLIP BOEING737 7374B7 1384702NM S-4L, BS 727C CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 S-4L, BS 727C CRACKED. MAJOR REPAIR, REPLACED WITH IDENTICAL PART IAW SRM 51-10-02, DEFECT SIZE: .25. 2L72 4F RTA16WE 20051213000352005121300035NM 2005 12 13 USAA051454 120051205A5315 FLOORBEAM BOEING737 7374B7 1384702NM BS 986 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 UPPER FLANGE STA 986.5 - LBL 30 CORRODED. MAJOR REPAIR, INSTALLED FLOORBEAM UPPER CHORD REPAIR IAW SRM 53-60-51 FIG 201, DEFECT SIZE: .250. 2L72 4F RTA16WE 20051213000362005121300036NM 2005 12 13 USAA051468 120051206A5320 INTERCOSTAL BOEING737 737301 1384611NM BS 967-986 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19591US 23936 BETWEEN STA 967 & STA 986 LBL 18 CORRODED. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-10-02, DEFECT SIZE: .25 INCH SPOT OF CORROSION ON TOP & BOTTOM OF NUT PLATE HOLES ON INTERCOSTAL. 2L72 4F RTA16WE 20051208001442005120800144SO 2005 12 8 LR7A05197 120051129A575334862712 FITTING LKHEED382 382G 526414USO TE FLAPS CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03406LC 711 4676 DURING B-2 CHECK PER HB2703, FOUND FLAP TRACK FITTING CRACKED AT FLAP STA 241, LT OWS231. REPLACED FITTING IAW SMP583 CH 51-60 AND 51-70. NR 2031. 2H74 4T A1SO 20051208001462005120800146SO 2005 12 8 LR7A05199 120051129A53123632072L BULKHEAD LKHEED382 382G 526414USO BS 1012 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03406LC 711 4676 DURING B-2 CHECK PER HB5302, FOUND LT AFT FUSELAGE BULKHEAD OUTBOARD CAP CRACKED AT FS1012, WL270, LBL63. REPLACED OUTBOARD CAP IAW SMP583 CH 51-60 AND 51-70, NR 2068. 2H74 4T A1SO 20051208001482005120800148SO 2005 12 8 LR7A05201 120051129A5230 GUSSET LKHEED382 382G 526414USO FS 990 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03406LC 711 4676 DURING B-2 CHECK PER HB5302, FOUND RT CARGO DOOR BULKHEAD LOWER GUSSET CRACKED AT FS 990, WL240, RBL59. REPLACED GUSSET IAW SMP583 CH 51-60 AND 51-70, NR 2070. 2H74 4T A1SO 20051208001502005120800150SO 2005 12 8 LR7A05203 120051129A53303631461 SKIN LKHEED382 382G 526414USO FS 517 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03406LC 711 4676 DURING B-2 CHECK PER HB5301, FOUND CRACKS ON FWD PRESSURIZED SKIN AT FS 517, WL285, LBL20-RBL20. REPLACED PRESSURIZED SKIN IAW SMP583 CH 51-60 AND 51-70. NR 2076. 2H74 4T A1SO 20051208001522005120800152SO 2005 12 8 LR7A05205 120051129A531134004314 FRAME LKHEED382 382G 526414USO FS 477 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03406LC 711 4676 DURING B-2 CHECK PER HB5301, FOUND FWD ATTACH FRAME CRACKED AFTER REMOVAL OF FWD CENTER PRESSURIZED FAIRING AT FS477, WL286, LBL18 - RBL18. REPLACED FRAME SECTION IAW SMP583 CH 51-60 & 51-70. DRG 5340179-501. MEA 382-53-05-104, NR 2084. 2H74 4T A1SO 20051208001532005120800153SO 2005 12 8 RAIA00511039 120051129A3350 INVERTER EMB 145 EMB145ER 3260211SO EMEGENCY LIGHT MALFUNCTIONED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03808HK 145157 PRE-FLIGHT - RIC - OVERHEAD EMERGENCY LIGHT OUT BY EXIT ROW CENTER AISLE. MAINTENANCE REMOVED AND REPLACED THE NR 6 INVERTER. 2L72 4F RTT00011AT 20051208001702005120800170SO 2005 12 8 LR7A05173 120051109A5344338941R BRACKET LKHEED382 382G 526414USO FS 93 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2549 4606 DURING C-7 CHECK PER HSP32302, FOUND RT FWD MLG DOOR BRACKET CRACKED 1/4 INCH FROM OUTER LOWER CORNER RADIUS, FS 93 WL160 RBL 20. REPLACED DOOR BRACKET IAW SMP583 FIG 51-70, NR 0250. 2H74 4T A1SO 20051208001722005120800172SO 2005 12 8 LR7A05175 120051109A5753 SKIN LKHEED382 382G 526414USO TE FLAP CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2549 4606 DURING C-7 CHECK PER HC5711, FOUND LT OB FLAP LE SKIN CRACKED 0.35 INCH ADJACENT TO FLAP CARRIAGE AT FLAP STA 28.1 AND 173.1. FS 600, WL270. REPAIRED SKIN AT FLAP STA 28.1 IAW DRG R05-028-02, MEA 382-57-05-088 AND SKIN AT FLAP STA 173.1 IAW SMP 583 FIG 51-140-12, NR 0275. 2H74 4T A1SO 20051208001742005120800174SO 2005 12 8 LR7A05177 120051109A5330 SKIN LKHEED382 382G 526414USO FS 196 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2549 4606 DURING C-7 CHECK PER HSP53300, FOUND SKIN BELOW NLG INSPECTION WINDOW WITH 1/8 INCH HORIZONTAL CRACKS FROM TWO RIVET HOLES DOWNWARD AND LEFT, FS 196, WL133, LBL1.0. REPAIRED SKIN IAW DRG R05-028-03, MEA 382-53-05-083, NR 0316. 2H74 4T A1SO 20051208001762005120800176EU 2005 12 8 05FDEA04114 120051204A5320 WEB AIRBUS300 A300B4622R 3930312EU ZONE 100 BENT A FDEAK NONE O OTHER ININSP/MAINT 1 SO25721FD 477 W/O 00030954, NR N00541, HORIZ STAB COMPT 2 WEBS BETWEEN FRAMES C85 AND C87 BENT 12TH STRINGER UP FROM 0 BL STRINGER AND 1 WEB BETWEEN FRAME C86 AND C87 11TH STRINGER UP FROM O BL STRINGER ("FROM BOTTOM STRINGERS"). REMOVED 3 WEBS, INSTALLED 3 WEBS IAW SRM 51-40-21. FABRICATED 3 WEBS ON TRAVELERS T5/560850, T5/560848, AND T5/560849. FABRICATED 3 STIFFENERS ON TRAVELERS T5/560847 AND T5/560846. TREATED AND PRIMED IAW SRM 51-21-10 PAINTED WEBS AND STIFFENERS IAW SRM 51-75-10. 2L72 4F RTA35EU 20051208001782005120800178NM 2005 12 8 05FDEA04116 120051204A5330 SKIN DOUG MD11 MD11 3023602NM ZONE 100 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 CENTER CARGO DOOR CUTOUT STA 1708 L40R TO L41R EXTERIOR SKIN EDGE FOUND CHAFED. REPAIR CARRIED OUT AT CENTER CARGO DOOR CUTOUT STA 1708 L40R TO L41R EXTERIOR SKIN EDGE CHAFFED AREA AS PER SRM 53-50-00 FIGURE 16 VOLUME I AND FEDEX EA # 1-5350- 90710, TITLE: "FUSELAGE - CENTER CARGO DOOR FRAME INSTALLATION / DOOR JAMB - EXISTING BUSHING REPAIR". 2L73 4F RTA22WE 20051208001802005120800180NM 2005 12 8 05FDEA04118 120051204A5320 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 FORWARD CARGO STATION 1119 TO STATION 6-10 L52 SPLICE FOUND CRACKED. FORWARD CARGO STATION 1119 TO STATION 6-10 L52 SPLICE REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2L73 4F RTA22WE 20051208001822005120800182NM 2005 12 8 05FDEA04120 120051205A5280 SKIN DOUG MD11 MD11 3023602NM ZONE 700 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 FOUND LEFT MAIN LANDING GEAR DOOR INTERIOR SKIN ON TOP NEAR THE HINGE AREA FOUND CRACKED. FILLER AND REPAIR DOUBLER FABRICATED AS PER SRM 52-10-00 VOLUME I. NEW FILLER AND REPAIR DOUBLER INSTALLED AS PER SRM 51-35-01 VOLUME II. LEFT HAND MAIN LANDING GEAR DOOR REMOVED AND REINSTALLED AS PER MM 32-14-20-4. CARRIED OUT LEFT HAND MAIN LANDING GEAR DOOR OPERATION TEST AS PER AMM 32-34-00-860-801. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2L73 4F RTA22WE 20051208001842005120800184NM 2005 12 8 05FDEA04122 120051205A5753 HINGE FITTING DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 FOUND LEFT WING OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING FOUND CORROSION AT OUTBOARD NR 3 BOLT HOLE. 2L73 4F RTA22WE 20051208001892005120800189EA 2005 12 8 SWIA200515932 120051130A274170623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TRIM ACTUATOR MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07439SW1078510785 7578 STAB TRIM CHANNEL 2 DISCONNECTS. REPLACED HORIZONTAL STABLILIZER TRIM ACTUATOR AND MOTOR CONTROL UNIT IAW CRJMM 27-42-01 AND 27-42-05. OPERATIONAL CHECK GOOD, PN: 8396-3, SN: OFF 750. 2L72 4F RTA21EA 20051208001912005120800191SO 2005 12 8 MASA200500727 120050914A2710 HANDLE EMB 145 EMB145LR 3260212SO ELEVATOR PULLED A MASAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 SW07845MJ 145502 ASH 2735 CLT - ELEVATORS DISCONNECTED. MAINTENANCE FOUND FLIGHT DECK ELEVATOR, DISCONNECT HANDLE PULLED. RESET HANDLE WITH NO FURTHER INCIDENT. 2L72 4T RTT00011AT 20051209000072005120900007NM 2005 12 9 UPS05245861 120051018A321069471231 LINK BOEING727 72730C 1384009NM RT MLG UPLOCK CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 INSPECTION TYPE:C RT MLG UPLOCK FWD SUPPORT LINKS CRACKED. REPLACE LINKS. RT MLG UPLOCK FWD SUPPORT LINKS REPLACED IAW MM 20-80-01. 2L73 4F A3WE 20051209000242005120900024 2005 12 9 SWAA053879 420051205A25656949956 CABLE BOEING737 7373H4 1384600NM R2 DOOR MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29341SW 24091 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE LATCH CABLE ASSY MISROUTED. REROUTED CABLE ASSY PER MM. 2L72 4F RTA16WE 20051209000262005120900026NM 2005 12 9 SWAA053881 120051206A5230 ANGLE BOEING737 7373H4 1384600NM AFT CARGO DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29386SW 2480386 26601 DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR CRACKED AT LOWER AFT CORNER ANGLE WEB SUPPORT. REMOVED AND REPLACED AFT CARGO DOOR PER MM. 2L72 4F RTA16WE 20051209000382005120900038NM 2005 12 9 QXEA200501582 120051122A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX - RIGHT INBOARD SEAT TRACK (NR 9) HAS CORROSION INSIDE CHANNEL AND TOP OF TRACK ST FUSELAGE STATION X597. REPAIRED IAW DHC-8 SRM 51-40-11. 2H72 4T RTA13NM 20051209000512005120900051EA 2005 12 9 QXEA200501640 120051031A5210 STRINGER CNDAIRCL600 CL6002C10 1390015EA PAX DOOR AFT CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC- DURING C3 CHECK, PASSENGER DOOR AFT ANGLE BETWEEN STAR STRINGER AND DOOR SHELL CRACKED 3/4" AT ASSIST CABLE. MAINTENANCE CUT OUT DAMAGED SECTION IAW REO 670-52-11-070 REVISION A STEPS 1 AND 2. 2L72 4F RTA21EA 20051209000612005120900061SO 2005 12 9 LR7A05183 120051109A53403561221R ATTACH FITTING LKHEED382 382G 526414USO BS 417 DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2549 4606 DURING C-7 CHECK PER HC5313, FOUND ON REMOVAL OF CHINE CAP ASSY FOR REPLACEMENT, CHINE CAP ATTACH FITTING WITH OVER SIZED HOLE AT FS417, RBL58. REPLACED CHINE CAP ATTACH FITTING IAW DRG 3317822, NR 0509. 2H74 4T A1SO 20051209000632005120900063SO 2005 12 9 LR7A05185 120051109A531537002717L FLOORBEAM LKHEED382 382G 526414USO FS 196 CORRODED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2549 4606 DURING C-7 CHECK PER HC5312, FOUND FWD FUSELAGE LT FLOOR SUPPORT ANGLE EXFOLIATED AT IB END, FS 196, WL146. REPLACED BEAM CAP ANGLE IAW DRG SMP 583 51-70 AND AC43.13-1B 4-57, NR 0545. 2H74 4T A1SO 20051209000742005120900074EA 2005 12 9 QXEA200501617 120051031A5753 SKIN CNDAIRCL600 CL6002C10 1390015EA TE FLAP CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, RIGHT WING INBOARD FLAP LOWER SKIN CHAFFED TRACK UNDER HINGE FAIRING 683BB. MAINTENANCE BLENDED DAMAGE IAW CRJ-700 57-52-01-101-001-A01. NO CRACKS FOUND. RESTORED FINISH. 2L72 4F RTA21EA 20051209000792005120900079NM 2005 12 9 UPS05245851 120051016A571165C2156623 SPAR BOEING727 72730C 1384009NM BS 870 BRL 36 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 AREA OF SUSPECT CORROSION ON WING CENTER SECTION REAR SPAR LWR CHORD BS 870 RBL36 DUE TO 2 POPPED FASTENER HEADS. PLEASE INVESTIGATE AND RECTIFY AS NECESSARY. AS PER BOEING INSTRUCTIONS THE LWR CHORD WAS REPLACED. NEW CHORD WAS CUT AT RBL 9.5. REPAIR SPLICE ANGLES AND STRAPS INSTALLED IAW SRM51-30-02 AND DWG 65C21566. WCS REPAIR OF WEB CARRIED OUT IAW BOEING REPAIR AND A AAE EO 2005-093-013. UPS AUTHORIZATION NR B727-5710-23321-A. 2L73 4F A3WE 20051209000822005120900082EA 2005 12 9 QXEA200501642 120051031A5210 STRINGER CNDAIRCL600 CL6002C10 1390015EA PAX DOOR CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, PASSENGER DOOR AFT SIDE STRINGER CRACKED UP FROM RADIUS BETWEEN RISER AND TREAD UNDER HANDRAIL STOWAGE BRACKET. MAINTENANCE REPAIRED CRACK IAW REO 670-52-11-104. 2L72 4F RTA21EA 20051209000852005120900085EA 2005 12 9 QXEA200501648 120051031A5320CC670332929 FLOOR SUPPORT CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC- DURING C3 CHECK, FUSELAGE INTERIOR AT STATION 280 CENTER FLOOR ANGLE CORRODED. MAINTENANCE REPLACED THE CENTER FLOOR ANGLE IAW CRJ-700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20051209000912005120900091EA 2005 12 9 QXEA200501645 120051031A5230670397231 ARM CNDAIRCL600 CL6002C10 1390015EA CARGO DOOR GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, FORWARD BAGGAGE DOOR AFT COUNTERBALANCE ARM GOUGED. MAINTENANCE REPAIRED COUNTERBALANCE ARM IAW REO 670-52-35-098. 2L72 4F RTA21EA 20051209000982005120900098WP 2005 12 9 05FDEA04128 120051205A5320 REPAIR DOUG DC10 DC1030F 3023504WP FUSELAGE PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 DISCREPANCY IN THE AFT FUSELAGE SECTION ZONE 316 AT STA Y 2140 FOUND 1 REPAIR ANGLE ON THE FRAME'S CAP AT X10 SIZE 10" X 2.5". PERFORMED A GVI OF REPAIR IAW SRM 53-30-00 VOL 1 FIG 2 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001-2D E3, RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VOL 2 PAR 33. 2L73 4F RTA22WE 20051209000992005120900099WP 2005 12 9 05FDEA04129 120051205A5753 REPAIR DOUG DC10 DC1030F 3023504WP LT WING FLAP PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 DISCREPANCY LT WING INBOARD FLAP FOUND A FLUSH DOUBLER 7.75" BY 4.75" ON LOWER SKIN AT STA XIFH 133. PERFORMED A GVI OF REPAIR IAW EA NR 8-5710-90133 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 AND TREATED STRIPPED AREA IAW SRM 51-21-01 PAR 33 VOL 2. 2L73 4F RTA22WE 20051212000042005121200004WP 2005 12 12 ABXA050334 120051203A54104916270501 CLIP DOUG DC9 DC941 302207NWP RT PYLON CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23954AX 47612 RIGHT FORWARD PYLON HAD A CRACKED ATTACH BRACKET INBOARD AND AFT SIDE RIGHT BUTT LINE 30 APPROXIMATELY AT FLOOR SURFACE. REMOVED AND REPLACED FITTING IAW DC9 SRM 51-30-5. 2L72 4F A6WE 20051212000212005121200021NM 2005 12 12 AWXA200501494 120051208A3620 DUCT AIRBUSA319 A319132 3930340NM NR 2 ENGINE LEAKING A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28660AW 1234 ECAM MESSAGE "AIR R WING LEAK". UNABLE TO DEFER DUE TO WEATHER. RETURNED & LANDED W/O INCIDENT. MX PERFORMED LEAK CHK & ENG RUNS. R&R RT CLAMP ON CROSS BLEED VALVE IAW MM. R&R SEAL ON RT WING LE, INBD OF BLEED DUCT. FOUND NR 2 PYLON AIR LEAK AT AFT CLAMP OF PRECOOLER. REPLACED PRECOOLER & AFT CLAMP PER MM. LEAK CHK GOOD. TEST FLT & FAILED DURING LANDING ROLL WHEN REVERSE APPLIED, ECAM MESSAGE APPEARED, REPORT SHOWED "R WING LOOP A". MX FOUND SLOW LEAK. REPLACED DUCT & TUBE JUST OTBD OF WING ROOT L/E IAW MM. OPS & LEAK CKS GOOD. FAULT CONFIRMED ON NR 2 BMC THAT REPLACED; FOUND UNIT FAILED PRE-TESTS. FAILED TEMP CHANNEL TEST. UNIT INSPECTED & ALL PARTS NECESSARY FOR REPAIR REPLACED. 2L72 4F RTA28NM 20051212000222005121200022EU 2005 12 12 AWXA200501495 120051208A5220 HANDLE AIRBUS320 A320232 3930326EU EMERGENCY EXIT UNSECURE A AWXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP28619AW 527 ONT - AIR TURN BACK - AFTER DEPARTURE CREW REPORTED THE LT FORWARD OVER WING EMERGENCY EXIT OPEN ON ECAM. NO PRESSURIZATION PROBLEMS WERE REPORTED AND NO EMERGENCY WAS DECLARED. CREW RETURNED TO ONT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND RE-SEATED THE LEFT FORWARD OVERWING EMERGENCY EXIT HANDLE, MESSAGE CLEARED. 2L72 4F RTA28NM 20051212000292005121200029EU 2005 12 12 AALA20050803 120051208A5610NP17252015 WINDOW AIRBUS300 A300B4605R 3930308EU COCKPIT FAILED A AALAA UNSCHED LANDING O OTHER CLCLIMB 1 SW2134078 615 SJU - AIRCRAFT DIVERTED TO SJU DUE TO CAPTAIN WINDOW OUTER PANE SHATTERED. HEATING ELEMENT ARCING LOWER LEFT EDGE. LANDED SJU WITHOUT INCIDENT. REPLACED CAPTAINS WINDSHIELD AND WINDSHIELD TEMPERATURE REGULATORY AND WINDOW HEAT PROTECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20051212000332005121200033NM 2005 12 12 AALA20050796 120051205A3350 BATTERY PACK BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21654A 24612 SFO - EMERGENCY EGRESS LIGHTS AT RIGHT HAND AFT FORWARD TO ROW 26 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EGRESS LIGHTS AT RIGHT HAND AFT FORWARD TO ROW 26. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20051212000382005121200038EU 2005 12 12 05FDEA04180 120051208A5330 REPAIR AIRBUS310 A310203 3930313EU FUSELAGE IMPROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 PREVIOUS REPAIR INSTALLED AT FUSELAGE RT SIDE EXT DOUBLER AFT OF BULK CARGO DOOR STA 3885 FR 72 STR 38 RT TO 39 RT NEEDS EVALUATION FOR MAJOR MINOR CLASSIFICATION AND APPROVED REPAIR DATA REF N00699. REPAIR NOT IAW A310-200 SRM 53-10-12 FIG 225 AND 233. REPAIRED AREA IAW EA 6-5310-95479. 2L72 4F RTA35EU 20051212000402005121200040NM 2005 12 12 05FDEA04182 120051208A5330 SKIN BOEING727 727200 138407ENM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25220FE 20934 AFT PIT HAS EXFOLIATED SKIN AT STA 1044 TO 1050 STR 29R-28R. REMOVED DAMAGE IAW B727 SRM 53-30-3 FIG 3 SHEET 1. FABRICATED AND INSTALLED DOUBLER IAW B727 SRM 53-30-3 FIG 3, 51-10-2 AND 51-30-2, MECH NR 7990 QC 362, MAJOR REPAIR. 2L73 4F RTA3WE 20051212000472005121200047EU 2005 12 12 05FDEA04089 120051203A5101 REPAIR AIRBUS310 A310203 3930313EU FUSELAGE NONE A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25424FE 241 PREVIOUS REPAIR INSTALLED AT FUSELAGE LOWER EDGE OF R1 DOOR AT STA 1202 TO STA 1214, FR14B. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND TO CONFORM SRM 52-10-00 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR. 2L72 4F RTA35EU 20051212000482005121200048EU 2005 12 12 05FDEA04090 120051203A5101 REPAIR AIRBUS310 A310203 3930313EU FUSELAGE NOT AN SDR A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25424FE 241 PREVIOUS REPAIR INSTALLED AT FUSELAGE LOWER EDGE OF R1 DOOR AT STA 1250 TO STA 1262, FS 15B. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND TO CONFORM SRM 52-10-00 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR. 2L72 4F RTA35EU 20051212000492005121200049SO 2005 12 12 MASA200500413 120050528A3297 WIRE EMB 145 EMB145LR 3260212SO PROXIMITY SENSORLOOSE A MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW07842MJ 145457 ASH 2831 ROA, L/G AIR GROUND FAIL EICAS MESSAGE. A/C FERRIED TO TO CLT. MX SECURED LOOSE ELECTRICAL CONNECTOR ON NOSE LANDING GEAR PROXIMITY SENSOR, REPLACED LT MLG WOW PROXIMITY SENSOR, AND SERVICED NOSE STRUT. TEST FLIGHT PERFORMED. NO FURTHER DEFECTS NOTED. 2L72 4T RTT00011AT 20051212000542005121200054NM 2005 12 12 SWAA053883 120051206A575365C35616 FLAP TRACK BOEING737 7373G7 1384595NM LT WING CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29671SW 23785 DURING SCHEDULED 1/4D CHECK, FOUND LT WING T/E FLAP NR 2 TRACK CORRODED AT AFT LOWER OTBD ATTACH FITTING. REMOVED AND REPLACED FLAP TRACK PER MM. 2L72 4F RTA16WE 20051212000552005121200055EA 2005 12 12 REXA200500151 120051207A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A REXAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO258458A 7458 FLAP FAIL MESSAGE DURING DEICING. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD 98-20-01. 2L72 4F RTA21EA 20051212000632005121200063NM 2005 12 12 QXEA200501590 120051110A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM BS 427 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX - RIGHT OUTBOARD SEAT TRACK NR 10 HAS PITTING CORROSION INSIDE CHANNEL MEASURING APPROXIMATELY .012" DEEP AT STATION 427. REPAIRED IAW RD 8-53-1342, DHC-8-200 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20051212000642005121200064NM 2005 12 12 QXEA200501591 120051110A5343 FRAME DHAV DHC8 DHC8202 2809007NM MLG MOUNT CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX - RIGHT MAIN LANDING GEAR FRAME HAS FRETTING ON AFT SIDE WHERE RETRACT ACTUATOR FITTING MOUNTS, NEAR BOLT HOLES. REPAIRED IAW RD 8-54-1178 AND SRM 51-20-16. 2H72 4T RTA13NM 20051212000772005121200077WP 2005 12 12 ABXA050330 120051128A534039146541 FITTING DOUG DC9 DC941 302207NWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23954AX 47612 BROKEN FASTENER HEAD AND BULGE IN FUSELAGE SKIN FS 1072. REMOVED AND REPLACED FITTING AT HING 23H, FS 1072 IAW DC9 SRM. 2L72 4F A6WE 20051212000912005121200091NM 2005 12 12 SWAA053892 120051208A57536546435 SKIN BOEING737 7375H4 138449DNM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29522SW 26564 DURING SCHEDULED SERVICE CHECK, FOUND RT WING OTBD T/E AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER SRM. 2L72 4F RTA16WE 20051212001162005121200116EA 2005 12 12 QXEA200501664 120051031A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 785-797 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, LEFT SIDE SEAT RAIL AT STATION 785-797 HAS AREAS OF CORROSION ON INNER SEAT ATTACH LUG. MAINTENANCE REPAIRED CORRODED AREAS IAW CRJ-700 REO 670-53-00-013. RESTORED FINISH. 2L72 4F RTA21EA 20051212001352005121200135NM 2005 12 12 SWAA053858 120051130A5313BAC1498 STRINGER BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29671SW 23785 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 359, STR 14L. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2L72 4F RTA16WE 20051212001382005121200138NM 2005 12 12 SWAA053861 120051204A53306545765 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29671SW 23785 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 518D, STR 12L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051212001432005121200143SO 2005 12 12 LR7A05206 120051203A5340342593L ATTACH FITTING LKHEED382 382G 526414USO FS 858 CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 239 4698 DURING 'A' CHECK PER HA1200, FOUND RAMP SUPPORT ATTACH FITTING CRACKED AT FS 858, WL191, LBL63. REPLACED FITTING IAW SMP583 CH 51-10 AND 51-70, LP NR 21460 ITEM M4. 2H74 4T A1SO 20051212001452005121200145EA 2005 12 12 QXEA200501734 120051201A3234533443 LEVER CNDAIRCL600 CL6002C10 1390015EA MLG MALFUNCTIONED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09616QX 10128 DEN - AFTER LANDING GEAR EXTENSION PROX SYSTEM CAUTION MESSAGE RECEIVED. ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE INTERROGATED MDC AND FOUND L/G SELECTOR VALVE RETRACT SOLENOID LOAD ON. REMOVED/REPLACED L/G CONTROL PANEL LEVER IAW CRJ AMM 32-31-01-000/400-802-A01. PERFORMED L/G EXTENSION/RETRACTION SYSTEM CHECK IAW CRJ AMM 32-30-00-710-801. C/W QX TASK CARD R071101. ALL OPS CHECKS SATISFACTORY AT THIS TIME. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20051212001562005121200156EA 2005 12 12 QXEA200501658 120051031A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 858 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, RIGHT SIDE OF SEAT RAIL AT STATION 858 HAS A GOUGE. MAINTENANCE REPAIRED DAMAGE IAW REO 670-53-00-013. 2L72 4F RTA21EA 20051212001592005121200159EA 2005 12 12 SWIA200515934 120051117A5312 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA BS 559 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07411SW 7067 RT MLG BAY; REAR PRESSURE BULKHEAD IS CRACKED AT AILERON QUADRANT; FS 559.00; RBL 17.0 + RBL 10.0, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED REAR PRESSURE BULKHEAD AT FS 559.00, RBL 17.0 & RBL 10.0 IAW CRJ REO 601R-53-41-260 REV "A". 2L72 4F RTA21EA 20051212001602005121200160EA 2005 12 12 SWIA200515935 120051117A5210 FRAME CNDAIRCL600 CL6002B19 1900309EA BS 336 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07411SW 7067 SUSPECT CRACK IN FRAME IN PAX DOOR AT APPROX STA 336 AT TOP OF DOOR, ITEM FOUND AT C-CHECK INSPECTION. PAX DOOR SUB-FRAME AT STQ 335.70 REPLACED IAW CRJ SRM 51-40-11, 51-25-06, 51-23-00, 51-21-16, 51-42-06, 51-42-10 FIG 4, 51-42-13, 51-42-21. 2L72 4F RTA21EA 20051212001632005121200163EA 2005 12 12 SWIA200515938 120051117A5310 VERTICAL BEAM CNDAIRCL600 CL6002B19 1900309EA BS 409 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07411SW 7067 FUSELAGE; VERTICAL BEAM; LWR O/B FLANGE IS CRACKED; FS 409.0 + 128; LBL -18, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FUSELAGE, VERTICAL BEAM, LWR O/B FLANGE, FS 409.0 + 128, LBL -18 IAW CRJ REO 601R-53-41-379 REV "NC". 2L72 4F RTA21EA 20051212001672005121200167EA 2005 12 12 SWIA200515942 120051117A5320 WEB CNDAIRCL600 CL6002B19 1900309EA BS 724 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07411SW 7067 WEB CRACKED AT FS 724.0 AT STR 24L, ITEM FOUND AT C-CHECK INSPECTION. EDDY CURRENT INSP COMPLETED ON SUSPECT CRACK AREA IAW CRJ 200 NDTM PT 1 51-20-06. NO CRACK INDICATION NOTED. NO FURTHER ACTION REQUIRED. 2L72 4F RTA21EA 20051212001692005121200169EA 2005 12 12 SWIA200515944 120051117A5320 SUPPORT ANGLE CNDAIRCL600 CL6002B19 1900309EA BS 605 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07411SW 7067 CRACKED SUPPORT ANGLE UNDER CARGO DOOR SILL AT STA 605 LBL 42, ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIP IAW CRJ REO 601R-53-61-100 REV NC & REO 601R-53-61-422 REV NC. 2L72 4F RTA21EA 20051212001732005121200173CE 2005 12 12 1050921026131 120051020A5320 SPLICE PLATE BEECH 1900 1900D 1154162CE BS 434 CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07146ZV UE146 FOUND FS 434 CRACKED SPLICE PLATE SIDEWALL. MAINTENANCE REPAIRED THE SPLICE PLATE SIDEWALL. 2L72 4T RTA24CE 20051213000032005121300003NM 2005 12 13 05FDEA04201 120051209A5753 FLAP TRACK BOEING727 727200 138407ENM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25220FE 20934 LEFT WING I/B FLAP O/B TRACK FWD MOUNT HOLE-D HAS PITTING IN INNER BORE. REMOVED PITTING AND CORROSION IAW BAC OHM 57-40-01. FABRICATED AND INSTALLED IAW BAC OHM 57-40-01 AND FED EX EA 7-5710-91314, LT INBOARD FLAP OUTBOARD TRACK OVERSIZE HOLE-D. MINOR REPAIR, TIMCO MECH 1281 QC280. 2L73 4F RTA3WE 20051213000072005121300007NM 2005 12 13 SB05164 120051205A33501012721 LIGHT BOEING737 7374B7 1384702NM SEAT 11ABC INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19449US 24893 CLT - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT AT SEAT 11ABC INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AT SEAT 11ABC. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20051213000132005121300013NM 2005 12 13 USAA200512004 120051129A5330 SKIN BOEING737 737401 1384701NM BS 860-887 WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19418US 23985 APPROX 9 INCH WEAR AREA AT OUTER FUSELAGE SKIN UNDER DORSAL FIN STA 860-887. FABRICATED DOUBLER AND INSTALLED PER EA 97151. 2L72 4F RTA16WE 20051213000162005121300016WP 2005 12 13 05FDEA04139 120051205A5730 REPAIR DOUG DC10 DC1030F 3023504WP RT WING UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 RIGHT WING INBOARD FLAP FOUND DOUBLER REPAIR ON UPPER SKIN AT STA XIFH 236 DIMENIONS 3.5 X 5 INCH. PERFORMED A GVI OF REPAIR IAW SRM 57-00-01 FIG 4 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001-2P. RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 PAR 33 VOL 2. 2L73 4F RTA22WE 20051213000212005121300021NM 2005 12 13 CALA0500425 120051129A5315BAC1518940 FLOORBEAM BOEING737 737524 1384721NM STA 947 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713624 27528 INSPECTION FOUND THE FLOORBEAM AFT FLANGE CORRODED AT STA 947, RBL 4 TO RBL 12. A STRAP REPAIR WAS INSTALLED IAW SRM 53-00-51. 2L72 4F RTA16WE 20051213000262005121300026NM 2005 12 13 USAA051463 120051205A554265C2584151 SKIN BOEING737 737301 1384611NM RUDDER DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19591US 23936 LEFT RUDDER SKIN 4 FEET FROM THE BOTTOM. MAJOR REPAIR, REMOVED DAMAGED, LAYED UP AND CURED REPAIR PLYS IAW SRM 51-70-17, DEFECT SIZE: 2 X 12 INCHES. 2L72 4F RTA16WE 20051213000282005121300028NM 2005 12 13 USAA051461 120051205A5340 STRINGER CLIP BOEING737 7374B7 1384702NM STA 727E, S4L CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 STA 727E, S4L CRACKED. MAJOR REPAIR, REPLACED TIE CLIP IAW SRM 51-10-02. 2L72 4F RTA16WE 20051213000292005121300029NM 2005 12 13 USAA051460 120051205A5340 STRINGER CLIP BOEING737 7374B7 1384702NM STA 727G S4R CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 STA 727G S4R CRACKED. MAJOR REPAIR, REPLACED TIE CLIP IAW SRM 51-10-02. 2L72 4F RTA16WE 20051213000382005121300038NM 2005 12 13 USAA051470 120051206A5320654587512 SUPPORT ANGLE BOEING737 7374B7 1384702NM FWD SERVICE DOORCORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 FWD SERVICE DOOR SCUFF PLATE SUPPORT ANGLE CORRODED. REPLACED WITH IDENTICAL PART, REMOVED CORRODED ANGLE & REINSTALLED NEW ANGLE IAW SRM 51-10-2. DEFECT SIZE: APPROX .5 X 24 INCH CORRODED AREA. 2L72 4F RTA16WE 20051213000402005121300040NM 2005 12 13 USAA051471 120051207A5320 ANGLE BOEING737 7374B7 1384702NM PAX DOORWAY CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 AFT ENTRY DOORWAY Z-ANGLE CORRODED. MAJOR REPAIR, REPLACED WITH IDENTICAL PART, IAW SRM 51-10-02 STEP 8. DEFECT SIZE: .250 X .250 INCH TO 1 X 2 INCH. 2L72 4F RTA16WE 20051213000422005121300042 2005 12 13 SWAA053885 420051207A25651061323 SLIDE BOEING737 7373H4 1384600NM R2 DOOR LOW PRESSURE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 R2 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATED OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20051213000442005121300044 2005 12 13 SWAA053887 420051206A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29386SW 26601 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051213000462005121300046NM 2005 12 13 SWAA053889 120051207A335007912 COVER BOEING737 7377H4 1384404NM LIGHT STRIP OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29427WN 29831 EEPLS STRIP COVER OUT OF POSITION AT FWD END. REPOSITIONED COVER PER MM. 2L72 4F RTA16WE 20051213000472005121300047NM 2005 12 13 SWAA053890 120051206A3350BR2013 LIGHT BOEING737 7373H4 1384600NM CABIN WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29626SW 27702 DURING SCHEDULED C1 CHECK, FOUND EEPLS STRIP WORN AT ROW 1 DEF. REMOVED AND REPLACED EEPLS PER MM. 2L72 4F RTA16WE 20051213000492005121300049NM 2005 12 13 2005UALA01236 120051107A335080541 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE LAV 117 INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29128UA 30023 LAV 117 OUTSIDE LIGHT INOP. *S/D* REPLACED EMERGENCY LIGHT ASSY. 2L74 4F4 FRTA20WE E24NE 20051213000522005121300052NM 2005 12 13 2005UALA01253 120051109A3397 CONNECTOR BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT UNSECURE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29118UA 28811 EEL INOP AT SEAT 43B. *S/D* RESECURED EEL CONNECTOR. 2L74 4F4 FRTA20WE E24NE 20051213000532005121300053NM 2005 12 13 2005UALA01254 120051109A3350362624 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29118UA 28811 EEL INOP AT SEAT 55RH. *S/D* REPLACED LIGHT ASSY. 2L74 4F4 FRTA20WE E24NE 20051213000542005121300054NM 2005 12 13 2005UALA01258 120051110A3397 CONNECTOR BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT UNSECURE A UALAK NONE O OTHER ININSP/MAINT 1 WP29120UA 29166 EMERGENCY EEL LIGHT AT DOOR 5 LEFT, LEFT WALL CROSS-AISLE INOP. *S/D* SECURED LOOSE CONNECTOR. 2L74 4F4 FRTA20WE E24NE 20051213000552005121300055NM 2005 12 13 2005UALA01334 120051122A2612PPA110100 SMOKE DETECTOR AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE LAVATORY MALFUNCTIONED A UALAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 WP29812UA 850 RECEIVED ECAM MESSAGE OF SMOKE IN LAVATORY & CARGO AREAS. TROUBLESHOOTING PROCEDURES FOLLOWED FOR SYSTEM OPERATION VERIFICATION. LISTED BELOW ARE THE FINDINGS FROM THE ACCOMPLISHMENT OF THOSE PROCEDURES. SMOKE DETECTOR (PPA1101-00) LOCATED IN THE FWD CARGO COMPARTMENT WAS INDICATING A FAULT ON THE POST FLIGHT REPORT. FURTHER INVESTIGATION DISCOVERED THE SMOKE DETECTOR MISALIGNED BEHIND THE ACTUAL PROTECTIVE GRILL. SMOKE DETECTOR (PPA1101-00) WAS REPLACED. SYSTEM OPERATIONAL TEST PERFORMED ON FIRE PROTECTION SYSTEM AND RESULT WAS NORMAL. ENGINEERING WILL CONTINUE TO MONITOR WITH RESPECT TO SMOKE DETECTION INDICATIONS. TO DATE, NO EVIDENCE OF ADDITIONAL ISSUES. 2L72 4F4 FRTA28NM E40NE 20051213000562005121300056 2005 12 13 2005UALA01335 420051127A2565 WARNING LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE DOOR 2L GIRT BARINOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29548UA 25396 ONE BULB OF GIRT BAR WARNING LIGHT WILL NOT ILLUMINATE. REPLACED LIGHT ASSY. 2L72 4F4 FRTA2NM E17NE 20051213000582005121300058EU 2005 12 13 2005UALA01337 120051124A5270 SENSOR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CARGO DOOR DIRTY A UALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP29414UA 472 RETURN TO FIELD DUE TO CARGO DOOR INDICATION. CLEANED SENSOR. OPERATED DOOR SEVERAL TIMES WITH NO FAULTS. 2L72 4F4 FRTA28NM E40NE 20051213000592005121300059NE 2005 12 13 2005UALA01338 220051124A7200 ENGINE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 2 BIRD INGESTION A UALAA UNSCHED LANDING CBJF.O.D. SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 WP29443UA 820 V10060 MULTIPLE BIRD STRIKES ON CLIMBOUT, LITE SMOKE ODOR THROUGHOUT CABIN. AIRFRAME AND NR 2 ENG DAMAGED. AMBER ALERT DECLARED AND RETURNED TO FIELD. BIRD STRIKE CAUSED THE RTF. DAMAGED FAN BLADES WERE REPLACED AND THE LPC AND HPC WERE BORESCOPE INSPECTED AND FOUND TO BE SERVICEABLE. COINCIDENTAL DISCOVERY OF FAN ATTRITION LINER LOOSENESS IS WHAT FORCED THE ENGINE TO BE REMOVED. 2L72 4F4 FRTA28NM E40NE 20051213000602005121300060NM 2005 12 13 2005UALA01339 120051125A5210 SNUBBER BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU L1 DOOR MISINSTALLED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29202UA 24717 FLIGHT DIVERTED DUE TO CABIN PRESSURIZATION PROBLEM. FOUND DOOR 1LT SNUBBER INSTALLED INCORRECTLY AND DOOR PRESSURE SEAL DAMAGED. REINSTALLED SNUBBER PER MM52-11-96 PG 401 AND REPAIRED SEAL. 2L72 4F4 FRTA16WE E21EU 20051213000612005121300061NM 2005 12 13 2005UALA01341 120051126A5311 FRAME BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU STA 400 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29921UA 25388 FUSELAGE FRAME CRACKED AT STATION 400 ORIGINATING FROM INBOARD RIVET HOLE OF PSU HANGER BRACKET JUST BELOW STRINGER 8 LEFT. REMOVED DAMAGE & VERIFIED CRACK CONTAINMENT & INSURANCE CUT BY NDT PER MM53-10-84. FABRICATED AND INSTALLED NESTED REPAIR ANGLES & FILLER PER MM53-10-84. 2L72 4F4 FRTA16WE E21EU 20051213000622005121300062NM 2005 12 13 2005UALA01342 120051126A5311 FRAME BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU STA 440 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29921UA 25388 FUSELAGE FRAME CRACKED AT STATION 440 ORIGINATING FROM INBOARD RIVET HOLE OF PSU HANGER BRACKET JUST BELOW STRINGER 8 LEFT. REMOVED DAMAGE & VERIFIED CRACK CONTAINMENT & INSURANCE CUT BY NDT PER MM53-10-84. FABRICATED AND INSTALLED NESTED REPAIR ANGLES & FILLER PER MM53-10-84. 2L72 4F4 FRTA16WE E21EU 20051213000642005121300064NM 2005 12 13 2005UALA01344 120051126A5311 FRAME BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU BS 787 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29921UA 25388 FUSELAGE FRAME CRACKED AT FASTENER ATTACH POINT COMMON TO AIR CONDITIONING DISTRIBUTION RAIL ATTACH POINT AT STA 787 JUST BELOW STRINGER 8 LEFT. REMOVED DAMAGE & VERIFIED CRACK CONTAINMENT & INSURANCE CUT BY NDT PER MM53-10-84. FABRICATED AND INSTALLED NESTED REPAIR ANGLES & FILLER PER MM53-10-84. 2L72 4F4 FRTA16WE E21EU 20051213000652005121300065NM 2005 12 13 2005UALA01345 120051126A5311 FRAME BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU BS 867 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29921UA 25388 FUSELAGE FRAME CRACKED AT FASTENER ATTACH POINT COMMON TO AIR CONDITIONING DISTRIBUTION RAIL ATTACH POINT AT STA 867 JUST BELOW STRINGER 8 LEFT. REMOVED DAMAGE & VERIFIED CRACK CONTAINMENT & INSURANCE CUT BY NDT PER MM53-10-84. FABRICA TED AND INSTALLED NESTED REPAIR ANGLES & FILLER PER MM53-10-84. 2L72 4F4 FRTA16WE E21EU 20051213000672005121300067NM 2005 12 13 2005UALA01347 120051126A5311 FRAME BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU BS 867 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29921UA 25388 FUSELAGE FRAME CRACKED AT FASTENER ATTACH POINT COMMON TO AIR CONDITIONING DISTRIBUTION RAIL ATTACH POINT AT STA 867 JUST BELOW STRINGER 8 RIGHT. REMOVED DAMAGE & VERIFIED CRACK CONTAINMENT & INSURANCE CUT BY NDT PER MM53-10-84. FABRICATED AND INSTALLED NESTED REPAIR ANGLES & FILLER PER MM53-10-84. 2L72 4F4 FRTA16WE E21EU 20051213000712005121300071NM 2005 12 13 2005UALA01351 120051128A5311 FRAME BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU BS 727B DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29921UA 25388 MISDRILLED HOLE DISCOVERED NEXT TO RIVET AT STA 727B ON FRAME WEB AT RBL 3.5. REMOVED DAMAGE.FABRICATED REPAIR PART PER SRM 53-00-07 FIG 201.HEAT TREATED, ALODINED & PRIMED REPAIR PARTS. INSTALLED NESTED ANGLE REPAIR PER SRM 53-00- 07 FIG 201. 2L72 4F4 FRTA16WE E21EU 20051213000722005121300072 2005 12 13 2005UALA01352 420051127A2561 LIFE VEST BOEING757 757222 1384956NM PWA 2037 PW2037 NE SEAT 25D INCORRECT A UALAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP29598UA 28751 INFANT LIFE VEST INSTALLED AT SEAT 25D. 2L72 4F4 FRTA2NM E17NE 20051213000732005121300073NM 2005 12 13 2005UALA01353 120051126A5610 WINDOW BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU COCKPIT ARCED A UALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP29381UA 24656 CAPTAINS SLIDING WINDOW IS ARCING NEAR THE WINDOW FRAME. REPLACED CAPTS SLIDING WINDOW HEAT PIGTAIL WIRES OP TEST OK OVHT TEST OK. 2L72 4F4 FRTA16WE E21EU 20051213000742005121300074NM 2005 12 13 2005UALA01354 120051123A2597 WIRE HARNESS AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE RT DOOR SLIDE MISROUTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29846UA 1600 NR 1 RT DOOR EVAC SLIDE ELECT HARNESS ROUTED WRONG DIRECTION. 2004, THERE WAS A FLEET CAMPAIGN TO VERIFY THE CORRECTNESS OF SLIDE HARNESS ROUTING. FOR THIS PURPOSE, LM CALLOUT LM4118 WAS ISSUED AND ACCOMPLISHED ON ACFT 4046 R1 SLIDE (MR25611-258) IN PHI ON 11/12/2004. THE FINDINGS WAS OK. BASED ON THE MR25611 MRTIME RECORDS AS OF 10/29/2004 AND 11/28/2005, THE SAME SLIDE ASSY (MR25611-258) HAS REMAINED INSTALLED ON THE AIRCRAFT. THERE IS NO RECORD TO SHOW ANY ACTIVITY ON THE UNIT THAT COULD HAVE RESULTED IN THE HARNESS TO BECOME MISROUTED. THE ROUTING WAS CORRECTED. 2L72 4F4 FRTA28NM E40NE 20051213000752005121300075NM 2005 12 13 2005UALA01355 120051125A3350 LIGHT BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU FROM ROW 15 AFT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29311UA 23672 EEL LIGHTS FROM ROW 15 AFT TO GALLEY INOPERATIVE. REPLACED EEL STRIP AT AFT SEATS. 2L72 4F4 FRTA16WE E21EU 20051213000762005121300076NM 2005 12 13 2005UALA01356 120051128A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE RT OVERWING INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29116UA 26908 TWO OF RIGHT OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED FUSE ON POWER SUPPLY. 2L74 4F4 FRTA20WE E24NE 20051213000782005121300078NM 2005 12 13 2005UALA01358 120051127A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE RT MID LAV WALL INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29117UA 28810 RIGHT MID LAV WALL EMERGENCY LIGHT INOP. RESECURED EMERGENCY LIGHT CONNECTION. 2L74 4F4 FRTA20WE E24NE 20051213000792005121300079NM 2005 12 13 2005UALA01359 120051127A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29117UA 28810 CREW REST EMERGENCY CEILING LIGHT INOPERATIVE. RESECURED LAMP. 2L74 4F4 FRTA20WE E24NE 20051213000802005121300080NM 2005 12 13 2005UALA01360 120051128A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE PAX DOOR INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP2927UA 28813 EMERGENCY LIGHTS INOP AT DOOR 5 RT SILL, ROW 17 CEILING, CKPT CEILING, RT FWD GALLEY CEILING AND SEATS 3J, 2J & 3A. REPLACED LAMP. 2L74 4F4 FRTA20WE E24NE 20051213000822005121300082 2005 12 13 2005UALA01362 420051127A2397 WIRE BOEING747 747422 1384935NM PWA 4056 PW4056 NE SEAT 15GH BURNED A UALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 WP2973UA 24380 ELECTRICAL BURNING ODOR IN UPPER DECK CABIN RT SIDE AROUND ROWS 14 & 15. MTC FOUND ODOR COMING FROM PC POWER SUPPLY AT 15GH. REPLACED PC POWER SUPPLY UNIT. 2L74 4F4 FRTA20WE E24NE 20051213000842005121300084NM 2005 12 13 2005UALA01364 120051129A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE DOOR 4L INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29116UA 26908 EMERGENCY EXIT LIGHTS INOPERATIVE AT DOOR 4 LEFT AFT & SEATS 46 THRU 54 RIGHT. REPLACED POWER SUPPLY. 2L74 4F4 FRTA20WE E24NE 20051213000852005121300085NM 2005 12 13 2005UALA01365 120051129A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE DOOR 4L INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29116UA 26908 EEL INOPERATIVE AT DOOR 4L ON DOOR BUSSLE, DOOR 4L CEILING LIGHT, LEFT EXT OVERWING MOST FWD ASSY, EXT OVERWING AT RIGHT MOST AFT ASSY, FLIGHT DECK CEILING AND DOOR 1L AFT SILL. REPLACED LAMP. 2L74 4F4 FRTA20WE E24NE 20051213000862005121300086NM 2005 12 13 2005UALA01366 120051129A3350 SIGN BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY EXIT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29116UA 26908 DOOR 4 RIGHT FWD EMERGENCY EXIT SIGN INOPERATIVE. REPLACED POWER SUPPLY. 2L74 4F4 FRTA20WE E24NE 20051213000872005121300087NM 2005 12 13 2005UALA01367 120051129A5311 FRAME BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU BS 400 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29922UA 26642 RIGHT CABIN FRAME STA 400 IS CRACKED BETWEEN STRINGERS 8-9 RT AT PSU BRACKET ATTACH. MAJOR REPAIR ACP'D PER MM 53-10-84. 2L72 4F4 FRTA16WE E21EU 20051213000882005121300088NM 2005 12 13 2005UALA01368 120051129A5311 FRAME BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU BS 400 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29922UA 26642 LT CABIN FRAME STA 400 IS CRACKED BETWEEN STR'S 8 - 9 LT AT PSU BRACKET ATTACH. MAJOR REPAIR ACP'D PER MM 53-10-84. 2L72 4F4 FRTA16WE E21EU 20051213000902005121300090NM 2005 12 13 2005UALA01370 120051129A5311 FRAME BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU BS 927 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29922UA 26642 CABIN FRAME CRACKED AT STA 927 BETWEEN STRINGERS 8-9 LT AT PSU SUPPORT BRACKET ATTACH. MAJOR REPAIR ACP'D PER SRM 53-00-07, NESTED J ANGLE DOUBLER REPAIR SCHEME. 2L72 4F4 FRTA16WE E21EU 20051213000912005121300091NM 2005 12 13 2005UALA01371 120051129A5311 FRAME BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU BS 907 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29922UA 26642 AFT CARGO FRAME CRACKED AT SHEAR TIE AT STA 907 BETWEEN STRINGERS 21 & 22 LT. MAJOR REPAIR ACP'D PER SRM 53-00-07, SHEAR TIE REPL'D 2L72 4F4 FRTA16WE E21EU 20051213000922005121300092NM 2005 12 13 2005UALA01372 120051129A5730 SKIN BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU LT WING CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29349UA 24253 LT WING ROOT AREA UPPER SKIN SURFACE CORRODED AT FUSELAGE STA 626 TO 663.7 AT WBL 108 10 112. REMOVED CORROSION DAMAGE PER SRM 57-20-01, ROTO PEENED, ALODINED & RESTORED PAINT PER SRM 51-20-01.THE REPAIR IS APPROVED BY FAA 8100-9 DATED NOV 27TH 2005. 2L72 4F4 FRTA16WE E21EU 20051213000932005121300093NM 2005 12 13 2005UALA01373 120051129A5730 SKIN BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU LT WING ROOT CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29349UA 24253 LT WING ROOT AREA UPPER SKIN SURFACE CORRODED AT FUSELAGE STA 616 TO 626 AT WBL 108 10 112. REMOVED CORROSION DAMAGE PER SRM 57-20-01, ROTO PEENED, ALODINED & RESTO RED PAINT PER SRM 51-20-01.THE REPAIR IS APPROVED BY FAA 8100-9 DATED NOV 27TH 2005. 2L72 4F4 FRTA16WE E21EU 20051213000952005121300095NM 2005 12 13 2005UALA01375 120051125A3350 LIGHT AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE AISLE SEATS 9C DAMAGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29819UA 893 SEATS 9C AND 14C AISLE ARMREST MOUNTED EMERGENCY LIGHTING DAMAGED. REPLACED CABIN EMERG LIGHTING MOUNTED TO AISLE ARMREST AT SEAT 9C. 2L72 4F4 FRTA28NM E40NE 20051213000982005121300098NM 2005 12 13 2005UALA01378 120051127A3397 WIRE HARNESS BOEING777 777222 1385219NM PWA PW4077PW4077 NE EMEGENCY LIGHT INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29778UA 26940 SEAT 1E BOTH EEL LIGHTS INOP. SEAT 2E BOTH EMERGENCY LIGHTS INOP/DAMAGED BY PAX ACTIVITY. FOUND EEL HARNESS GOING TO BOTH LIGHTS DAMAGED. 2L72 4F4 FRTT0001SE E46NE 20051213001012005121300101NM 2005 12 13 2005UALA01381 120051130A3210 LANDING GEAR BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29331UA 24192 LANDING GEAR WOULD NOT RETRACT. RESET CIRCUIT BREAKER FOR "'LANDING GEAR LATCH AND PRESSURE WARNING'" ON P6-3 PANEL. PERFORMED OPERATIONAL CHECK PER 7-11-11, 32-32=00 AND 32-34-00 (SWUNG) . NO FAULT FOUND. 2L72 4F4 FRTA16WE E21EU 20051213001052005121300105EU 2005 12 13 2005UALA01385 120051201A5330 SKIN AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29443UA 820 A 4 X 5 X .25 INCH DENT NOTED ON RT SIDE OF FUSELAGE IN THE AREA OF THE RVSM MARKINGS. DENT STARTS APPROX 2.75 INCHES AFT OF 4TH FRAME RIVET ROW AND STOPS .25 INCH FROM 5TH FRAME RIVET ROW. BOTTOM OF DENT TOUCHES WATER LINE RIVET ROW. REPAIR WAS ACCOMPLISHED PER UA-EVA-50805A. 2L72 4F4 FRTA28NM E40NE 20051213001062005121300106NM 2005 12 13 2005UALA01386 120051202A3397 WIRE BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU EMERGENCY LIGHT DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29305UA 23666 FIRST CLASS FLOOR EEL AND GALLEY STRIP EEL LIGHT IS INOP. REPLACED FEEDER CABLE. 2L72 4F4 FRTA16WE E21EU 20051213001072005121300107EA 2005 12 13 COMA0560683 120051210A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01796CA 7338 FLIGHT 5392- INBOUND CVG RECEIVED A FLAP FAIL MESSAGE AT 30 DEGREES. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2L72 4F RTA21EA 20051213001092005121300109EA 2005 12 13 COMA0560685 120051212A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION LDLANDING 1 SO01949CA 7080 FLIGHT 5130- DURING LANDING AT MSG RECEIVED A FLAP FAIL MESSAGE AT 45 DEGREES. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A ,B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2L72 4F RTA21EA 20051213001102005121300110SO 2005 12 13 CHQA200500208 120051208A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LGIHT BURNED OUT A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11294SK 145497 LEFT HAND EXTERNAL OVERWING AFT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BULB LEFT HAND EXTERNAL OVERWING EMERGENCY LIGHT IAW EMB 145 MM 33-50-09. OPS CHECK GOOD. 2L72 4T RTT00011AT 20051213001122005121300112EA 2005 12 13 COMA0560673 120051207A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01917CA 7017 FLIGHT 5305 - RECEIVED A FLAP FAIL CAUTION MESSAGE DURING CVG APPROACH. CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A,B,C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2L72 4F RTA21EA 20051213001162005121300116EA 2005 12 13 COMA0560679 120051207A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS WARNING LIGHT A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01804CA 7352 FLIGHT 5006 - RECEIVED A FLAP FAIL CAUTION MESSAGE INBOUND TO YUL, FLIGHT LANDED WITHOUT INCIDENT. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A,B,C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2L72 4F RTA21EA 20051213001172005121300117EA 2005 12 13 COMA0560680 120051212A5320601R3117115 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FS 484 CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01721CA18482 7259 INTERCOSTAL CRACKED AT FS 484 BL27.00-36.00 RIGHT SIDE BELOW FLOOR AFT OF EMERGENCY EXIT. REPAIRED CRACK IAW BRAS EO 601R-53-41-059. 2L72 4F RTA21EA 20051213001182005121300118WP 2005 12 13 IXXA0500152S 120050217A5310 DOOR FRAME DOUG DC8 DC871F 302199DWP FS 1440.00 WORN A IXXAK NONE O OTHER ININSP/MAINT 1 SW11821BX858952998 45811 DURING A ROUTINE C CHECK INSPECTION, RT FUSELAGE AFT CENTER SECTION AFT CARGO COMPARTMENT AFT DOOR AFT JAMB WEAR DAMAGE AT STA FS 1440.00, L-30R TO L-31R. MAJOR REPAIR ACCOMPLISHED REMOVAL OF FASTENERS AND DAMAGED AREA. PERFORMED AN NDT INSPECTION, FABRICATED EXTERNAL REPAIR DOUBLER + FILLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED FILLER AND REPAIR DOUBLER IAW ALL APPLICABLE MANUALS, DRAWINGS AND FORMS. 2L74 4F RT4A25 20051213001202005121300120WP 2005 12 13 IXXA0500156S 120050303A5240 ACCESS DOOR DOUG DC8 DC871F 302199DWP FS -12.00L-27R CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11821BX859852998 45811 DURING A ROUTINE C CHECK INSPECTION, FOUND RT FUSELAGE NOSE SECTION ACS MODIFICATION DOUBLER LOWER AFT JAMB CORNER RAM AIR EXHAUST ACCESS DOOR COMPARTMENT CRACK DAMAGE AT STA FS -12.00, L-27R. MAJOR REPAIR ACCOMPLISHED REMOVAL OF EXISTING FILLER AND DAMAGED SECTION. PERFORMED AN NDT INSPECTION. FABRICATED REPAIR DOUBLER AND REPAIR TRIPLER + FILLER. APPLIED SEALANT TO FAYING SURFACES AND INSTALLED REPAIRED PARTS IAW ALL APPLICABLE MANUALS, DRAWINGS AND FORMS. 2L74 4F RT4A25 20051213001212005121300121WP 2005 12 13 IXXA0500153S 120050217A5720 PLATE DOUG DC8 DC871F 302199DWP XF 415.-XW 408.0DENTED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11821BX858952998 45811 DURING A ROUTINE C CHECK INSPECTION, FOUND RT WING OUTBOARD FLAP LOWER AFT PLATING DENTS DAMAGE BETWEEN STA XF 415.000 AND XW 408.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF DAMAGED SKIN. FABRICATED NEW SKIN, CLEANED, TREATED AND PRIMED AREA + NEW SKIN INTERNAL PART. APPLIED SEALANT TO FAYING SEURFACES AND INSTALLED NEW SKIN IAW ALL APPLICABLE MANUALS, DRAWNINGS AND FORMS. 2L74 4F RT4A25 20051213001232005121300123WP 2005 12 13 IXXA0500149S 120050303A5730 PANEL DOUG DC8 DC871F 302199DWP XRS 71.000 S7-S8CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11821BX858952998 45811 DURING A ROUTINE C CHECK INSPECTION, FOUND LT INNER WING AFT TOP PANEL PLATING CRACK DAMAGE AROUND STA XRS 71.000, S-7 TO S-8. MAJOR REPAIR ACCOMPLISHED REMOVAL OF FASTENERS FROM REPAIR AREA AND PERFORMED NDT INSPECTION. FABRICATED REPAIR DOUBLER AND FILLER PLUG. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES AND INSTALLED REPAIRED PARTS IN ACCORDANCE WITH SEMON DRAWING ED-3830 AND FAA FORM 8110-3 NR 05030, DC8 SRM 51-1-11, 51-1-15, 51-1-20D, 51-3-1, 51-3-2. 2L74 4F RT4A25 20051213001242005121300124WP 2005 12 13 IXXA0500151S 120050225A5720 PLATE DOUG DC8 DC871F 302199DWP XW 110.000 DENTED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11821BX858952998 45811 DURING A ROUTINE C CHECK INSPECTION, FOUND RT WING INBOARD FLAP UPPER AFT PLATING DENT DAMAGE AT STA XW 110.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF DAMAGED PLATING. FABRICATED NEW PLATING AND FINGER DOUBLER. CLEANED, TREATED AND PRIMED NEW PLATING INTERNAL PART. BONDED FINGER DOUBLERS AND APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIRED PARTS IAW DC8 SRM 57-1-0 PG 1, 57-7-1 FIG 1 SH 1, 51-1-9A, 51-1-11, 51-1-21, 51-1-3, 51-3-0, 51-3-1. 2L74 4F RT4A25 20051213001252005121300125WP 2005 12 13 IXXA0500154S 120050218A5720 PLATE DOUG DC8 DC871F 302199DWP XFS 710.00 DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11821BX858952998 45811 DURING A ROUTINE C CHECK INSPECTION, FOUND LT OUTER WING INBOARD EXTENDED LEADING EDGE ELONGATED HOLE AROUND STA XFS 710.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF PLATING WITH IMPROPER REPAIR. FABRICATED NEW PLATING, CLEANED, TREATED AND PRIMED AREA AND NEW PLATING INTERNAL PART. APPLIED SEALANT TO ALL FAYING SURFACES AND INSTALLED NEW PLATING IAW ALL APPLICABLE MANUALS, DRAWINGS AND FORMS. 2L74 4F RT4A25 20051213001262005121300126EA 2005 12 13 COMA0560674 120051207A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS WARNING LIGHT A COMAO OTHER J WARNING INDICATION CRCRUISE 1 SO01924CA 7026 FLIGHT 5667 - EN ROUTE CVG-FSD RECEIVED A FLAP FAIL CAUTION MESSAGE, FLIGHT LANDED AT FSD WITHOUT INCIDENT. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A,B,C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2L72 4F RTA21EA 20051213001272005121300127WP 2005 12 13 IXXA0500148S 120050228A5730 FASTENER DOUG DC8 DC871F 302199DWP FS 620 L35R-36 MISSING A IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW11821BX858952998 45811 DURING A ROUTINE C CHECK INSPECTION, FOUND WING TO FUSELAGE LOWER PLATING DRAIN HOLE REPAIR MISSING ONE ROW OF FASTENERS AT STA FS 620.000, L-35R TO L-35R. MAJOR REPAIR ACCOMPLISHED REMOVAL OF EXISTING DOUBLER AND FASTENERS WITHIN REPAIR AREA AND REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION, FABRICATED REPAIR DOUBLER, REPAIR TRIPLER, SKIN FILLER AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR DOUBLER, TRIPLER, SKIN FILLER AND INTERNAL DOUBLER FILLER. APPLIED SEALANT TO FAYING SURFACES. INSTALLED ALL REPAIRED PARTS IAW ALL APPLICABLE MANUALS, DRAWINGS AND FORMS. 2L74 4F RT4A25 20051213001302005121300130EA 2005 12 13 ASOA05983 120051115A25602618 FLASHLIGHT CNDAIRCL600 CL6002B19 1900309EA COCKPIT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27937EV 8042 DURING A GROUND INSPECTION IN ATL, THE CAPTAINS FLASHLIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS FLASHLIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051213001392005121300139WP 2005 12 13 ABXA050350 120051012A5340364004U503 FITTING DOUG DC8 DC863F 302198FWP STA. 879 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 FOUND STA 900, L-24, CORROSION ON FORWARD SECTION AND AFT OF FITTING AT ATTACH POINT TO L-24. REMOVED AND REPLACED FITTING WITH NEW PART IAW DC8 SRM 51-10-1. POSITIONED, DRILLED UP HOLES, REAMED AND INSTALLED FITTING AT STA 879 (900) L-24 IN LEFT WHEEL WELL IAW DC8 SRM 51-1-20. 2L74 4F 4A25 20051213001402005121300140WP 2005 12 13 ABXA050349 120051012A53405750198502 FITTING DOUG DC8 DC863F 302198FWP STA. 880 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 UPPER FORWARD MOST SUPPORT ANGLE WAS CRACKED IN 2 PLACES ON TOP OF L-24 FITTING IN RIGHT WHEEL WELL. REMOVED AND REPLACED CRACKED FITTING TOP OF L-24 RIGHT WHEEL WELL STA 880, P/N: 5750198-502 IAW DC8 SRM 51-1-20D. 2L74 4F 4A25 20051213001412005121300141WP 2005 12 13 ABXA050355 120051025A5322 SHEAR TIE DOUG DC8 DC863F 302198FWP STA 440 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 FOUND SHEAR TIE CRACKED AT STA 440, LONGERON 31 RIGHT (REF. NRC HY-275). REMOVED AREA STRUCTURE FOR ACCESS, REMOVED DAMAGED AREA OF FORMER SECTION/SHEAR TIE, LONGERON 30 RIGHT AND LONGERON 31 RIGHT, STA 440. FABRICATED REPAIR PARTS: 1 FORMER SECTION FROM 0.071" 2024-T3 AND 1 SPLICE DOUBLER FROM 0.071" 2024-T3. BOTH PO NR 1122792. FIT, TREATED, AND PRIMED PARTS. INSTALLED REPAIR PARTS. REINSTALLED STRUCTURE REMOVED FOR ACCESS REF DC8 SRM 53-2-0, FIG 2B. 2L74 4F 4A25 20051213001422005121300142WP 2005 12 13 ABXA050348 120051012A5330 SKIN DOUG DC8 DC863F 302198FWP STA. 440 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 LOWER FUSELAGE SKIN, STA 400, LONGERON 31 RIGHT, FASTENER HEADS SHEARED. REMOVED DAMAGED FASTENERS, NOTED CORROSION ON INTERNAL FINGER DOUBLER AT STA 440 LONGERON 31 RIGHT. REPAIRED FINGER DOUBLER IAW REA D853-52523. ELONGATED AND OVER-SIZED HOLES AT STA 440, BETWEEN LONGERON 30 RIGHT AND 31 RIGHT. REMOVED DAMAGED SKIN AREA. FABRICATED: 1 FILLER 0.071" 7075-T6 PO NR 1084025, 1 EXTERNAL DOUBLER P.080" 7075-T6 PO NR 1113384, 2 INTERNAL DOUBLERS .050" 7075-T6 PO NR 1112267. FIT, TREATED AND PRIMED PARTS. INSTALLED REPAIR PARTS AND FASTENERS REF DC8 SRM 53-2-1, FIG 7, SHEETS 1 AND 4. 2L74 4F 4A25 20051213001442005121300144SO 2005 12 13 CHQA200500203 120051130A3350RPS1B BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11275SK7851 7851 145345 WHEN EMERGENCY SELECT LIGHT SWITCH IS POSITIONED IN ARM POSITION, FORWARD EMERGENCY LIGHTS ILLUMINATE. REMOVED AND REPLACED FORWARD EMERGENCY LIGHTS POWER SUPPLY AND OPS CHECK GOOD IAW EMB MM 33-50-00. OK FOR SERVICE. 2L72 4T RTT00011AT 20051213001452005121300145EA 2005 12 13 SWIA200515973 120051206A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07423SW 7456 2ND OVERHEAD EMERGENCY LIGHT POD WILL NOT ILLUMINATE. RELAMPED 2ND OVERHEAD EMERGENCY LIGHT POD AS REQUIRED. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051213001462005121300146EA 2005 12 13 SWIA200515974 120051206A2721BA670905401 LIMITER CNDAIRCL600 CL6002C10 1390015EA RUDDER TRIM MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07764SK 10229 "RUDDER LIMIT FAULT" STATUS MSG. REPLACED NR 1 RUDDER LIMIT NR 1 RVDT IAW 27-25-05, PN BA670-90540-1, SN OFF A1166. 2L72 4F RTA21EA 20051213001472005121300147EA 2005 12 13 SWIA200515975 120051206A2780 DETECTOR CNDAIRCL600 CL6002C10 1390015EA SLATS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07743SK 10199 RCVD "SLAT FAULT" STATUS MSG EN ROUTE. REPLACED LT OUTBOARD SKEW DETECTOR. OPERATIONAL CHECK GOOD IAW 27-51-00. 2L72 4F RTA21EA 20051213001512005121300151NM 2005 12 13 SWAA053900 120051210A53116520722 FRAME BOEING737 7373H4 1384600NM BS 440 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 24R. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20051214000012005121400001NM 2005 12 14 2005UALA01387 120051202A5230 SKIN BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FWD CARGO DOOR CRACKED A UALAO OTHER O OTHER LDLANDING 1 WP29922UA 26642 FWD CARGO DOOR EXTERNAL SKIN IS CRACKED AT LATCH HOUSING CUTOUT, UPPER AFT CORNER. MAJOR REPAIR ACP'D PER SM 70-52-30-67-AR3, STAINLESS STEEL INTERNAL DOUBLER REPAIR, 2L72 4F4 FRTA16WE E2GL 20051214000022005121400002NM 2005 12 14 SB05161 120051202A27511817389 TRANSMITTER BOEING737 7374B7 1384702NM LEFT WING FAULTY A USAAA UNSCHED LANDING F FLT CONT AFFECTED DEDESCENT 1 EA19443US3025030250 24842 ON DESCENT, AT 3,000 FEET, CREW RECEIVED A FLAP LOCKOUT AT 5 UNITS FLAP SETTING. AIRCRAFT DID NOT EXPERIENCE ANY ROLL AND THE CREW SUSPECTS THE WARNING WAS AN INDICATION PROBLEM. CREW DECLARED AN EMERGENCY AND DIVERTED, DUE TO LONGER RUNWAYS. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LT WING FLAP TRANSMITTER IAW MM 27-58-12. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20051214000052005121400005NM 2005 12 14 2005UALA01389 120051203A5330 SKIN BOEING737 737522 138449FNM DOOR CUTOUT CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29921UA 25388 EXTERNAL FUSELAGE SKIN AT AFT GALLEY DOOR CUTOUT IS CRACKED AT FWD LOWER CORNER. REMOVED DAMAGE & ACP NDT FOR CRACK CONTAINMENT.ZERO TIMED 10 EA FASTENER HOLES. FABRICATED AND INSTALLED DOUBLER, TRIPLER AND FILLER REPAIR PER SRM53-00-01 DETAIL 5. 2L72 4F RTA16WE 20051208001942005120800194NE 2005 12 8 QXEA200501730 220051201A7200 ENGINE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE NR 1 UNKNOWN A QXEAD RETURN TO BLOCK Y ENGINE STOPPAGE TXTAXI/GRND HDL 1 NM09601QX 10009 OKC - ON PUSHBACK FOR FLIGHT 4188 DURING ENGINE START, THE NR 1 AUTO SHUTDOWN DURING START. RETURNED TO THE GATE. MAINTENANCE FOUND THE LEFT FADEC START ABORT MESSAGE IN MEMORY DUE TO SLOW N2 RESPONSE. MAINTENANCE SUSPECTED ICING. PERFORMED GROUND RUN OF ENGINE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2L72 4F4 FRTA21EA EOOO63EN 20051208001952005120800195SO 2005 12 8 LR7A05178 120051109A532037234919 CAP LKHEED382 382G 526414USO FS345E CORRODED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2549 4606 DURING C-7 CHECK PER HC53134, FOUND RT CARGO BAY CHINE CAP EXFOLIATED, FS 345E-517. REPLACED CHINE CAP IAW DRG 372349 AND SMP 581 CH 90, NR 0324. 2H74 4T A1SO 20051209000042005120900004EA 2005 12 9 ASOA05951 120051103A5220H341931 HANDLE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE ESCAPE HATCH CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27709EV 10068 DURING A C-CHECK, THE CREW ESCAPE HATCH OUTER HANDLE WAS FOUND TO BE CORRODED ON THE INSIDE. THIS MRR WILL REMAIN OPEN, PENDING MAINTENANCE DETERMINATION OF APPROPRIATE CORRECTIVE ACTION. (K) MAINTENANCE REMOVED AND REPLACED THE CREW ESCAPE HATCH OUTER HANDLE IAW CRJ 700 AMM 52-22-02. OPS CHECKS GOOD. (M) 2L72 4F4 FRTA21EA EOOO63EN 20051209000212005120900021EA 2005 12 9 VTZA200500221 120051205A53206013501252 ANGLE CNDAIRCL600 CL6002B19 1900309EA BS 625 CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27630BR 7255 RT OBLIQUE ANGLE AT FS 625 IS CRACKED. 2L72 4F RTA21EA 20051209000232005120900023NM 2005 12 9 SWAA053878 120051205A5755 CASTING BOEING737 7373H4 1384600NM RT WING SPOILER CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29341SW MA3241 24091 DURING SCHEDULED C1 CHECK, FOUND RT WING NR 5 SPOILER OTBD HINGE CASTING CRACKED. REMOVED AND REPLACED NR 5 SPOILER PER MM. 2L72 4F RTA16WE 20051209000332005120900033NM 2005 12 9 QXEA200501578 120051110A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM BS 445 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX - RIGHT INBOARD SEAT TRACK NR 8 HAS CHAFE MARKS INSIDE CHANNEL, 10" LONG AREA AT STATION X445. REPAIRED IAW RD 8-53-1339, DHC8-202 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20051209000712005120900071NM 2005 12 9 QXEA200501746 120051202A3411 PITOT TUBE BOMBDRDHC8 DHC8402 1390042NM DIRTY A QXEAA UNSCHED LANDING GJ MULTIPLE FAILURE WARNING INDICATION CLCLIMB 1 NM09406QX 4048 SEA FLIGHT NR 2419: AFTER TAKEOFF, HAD A MOMENTARY IAS MISMATCH, THEN AGAIN ON OUR DESCENT RECEIVED ANOTHER IAS MISMATCH MESSAGE THAT WAS 10 KT DIFFERENT. CAPTAIN SIDE WAS SLOWER THAN FO'S AIRSPEED INDICATOR AND ISI AIRSPEED INDICATOR. THE DIFFERENCE LASTED APPROXIMATELY 30 SECONDS AND THEN CORRECTED ITSELF. THEN WENT AHEAD AND RAN IAS MISMATCH CHECKLIST. MAINTENANCE CLEANED OUT CAPTAIN'S PITOT LINES IAW AMM 34-11-00, PAGE 201. C/W PITOT/STATIC LEAK CHECK IAW MTC NR 6341102. CHECKS GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051209000732005120900073EA 2005 12 9 QXEA200501613 120051031A5730 SKIN CNDAIRCL600 CL6002C10 1390015EA RT WING DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, RIGHT WING UPPER SKIN T/EDGE HAS BROKEN AND LOOSE FASTENERS. REPLACED BROKEN AND LOOSE RIVETS IAW CRJ-700 SRM 51-42-06-001-001-AO1. 2L72 4F RTA21EA 20051209000752005120900075EA 2005 12 9 QXEA200501620 120051031A5230 TRACK CNDAIRCL600 CL6002C10 1390015EA CARGO DOOR GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, AFT CARGO DOOR TRACK, AFT TRACK HAS GOUGE MID WAY UP. MAINTENANCE REPAIRED TRACK IAW EA R-53-380 AND REO 670-53-61-208. 2L72 4F RTA21EA 20051209000812005120900081EA 2005 12 9 QXEA200501630 120051031A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA BS 394-421 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, LOWER FUSELAGE EXTERNAL SKIN GOUGED BY ROCK CHIPS AT STATION 394-421, STRINGERS 25 LEFT AND RIGHT. MAINTENANCE REMOVED DAMAGE IAW CRJ-700 SRM 51-12-00-001-001-A01. RESTORED FINISH. 2L72 4F RTA21EA 20051209000892005120900089EA 2005 12 9 QXEA200501638 120051031A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA BS 349 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, LOWER FUSELAGE EXTERNAL SKIN GOUGED AT STATION 349 STRINGERS 18R-19R. MAINTENANCE REPAIRED DAMAGED AREA IAW EA R-53-396 AND REO 670-53-21-142. RESTORED FINISH. 2L72 4F RTA21EA 20051209001002005120900100WP 2005 12 9 05FDEA04130 120051205A5310 REPAIR DOUG DC10 DC1030F 3023504WP FUSELAGE PROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 DISCREPANCY PERFORMED INSPECTION IAW EO NR 8-5100-7-5001-P2 FOUND DOUBLER DIMENS 12" BY 7.5" EXTERNAL FUSELAGE AT STA 1370 LONG 51 RT TO 51 LT. PERFORMED A GVI OF REPAIR IAW SRM 53-40-00 FIG 20 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001-1P RESTORED PAINT ON STRIPPED AREA IAW SRM 52-21-01 VOL 2 PAR 33. 2L73 4F RTA22WE 20051212000082005121200008NE 2005 12 12 ABXA050338 220051019A7200 AIR DUCT DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE NR 4 ENGINE DENTED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 NR 4 ENGINE L/S TRANSITION AIR DUCT HAD SEVERAL DENTS. 2 DENTS AT 9 AND 11 O'CLOCK POSITIONS OUT OF LIMITS IAW DC8 SRM 51-1-9A. CLEANED UP AREA OF DENTS AT 9 AND 11 O'CLOCK POSITIONS AND REPAIRED IAW DC8 SRM 51-1-9A. 2 MORE DENTS AT 11 O'CLOCK POSITION ARE WITHIN LIMITS AND CLEANED UP AREAS AND REPAIRED IAW DC8 SRM 51-1-9A. TREATED REPAIRS IAW LWR200302015 AND PRIMED IAW DC8 51-1-3. 2L74 4F4 F 4A25 1E8 20051212000202005121200020EU 2005 12 12 AWXA200501493 120051207A5320D53471124201 PLATE AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28604AW 1196 SAL - DURING BC4 CHECK DISCOVERED LEVEL 2 GALVANIC CORROSION ON SHEAR PLATE LOCATED BETWEEN FS 69 TO FS 70 AND Y-1162. NO ALLOWABLE DAMAGE LIMITS WERE FOUND IN THE AIRBUS 320 SRM. MAINTENANCE REMOVED AND INSTALLED NEW SHEAR PLATE BETWEEN FS 69 AND FS 70, Y-1162 IAW AIRBUS 320 SRM 51-72-11 AND 51-42-11. 2L72 4F RTA28NM 20051212000232005121200023WP 2005 12 12 AALA20050802 120051205A2820 O-RING DOUG DC9 DC982 3022082WP ENGINE CUT A AALAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SW21513AA 49890 DFW - REPORTS OF SMOKE AND FUEL STREAMING OUT OF LEFT HAND ENGINE DURING LANDING, REVERSE, AND ROLL OUT. FUEL CONTINUED TO LEAK FOR 20 MINUTES AFTER ALL POWER REMOVED. FOUND LEFT HAND ENGINE FILTER BOWL LEAKING. O-RING CUT. REPLACED O-RING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051212000392005121200039EU 2005 12 12 05FDEA04181 120051208A5330 REPAIR AIRBUS310 A310203 3930313EU FUSELAGE UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 PREVIOUS REPAIR INSTALLED ON FUSELAGE RT SIDE FWD OF FS 17 STA 1315 BETWEEN STR 35R AND 38R FLUSH DOUBLER NEEDS EVALUATION FOR MAJOR MINOR CLASSIFICATION AND APPROVED REPAIR DATA REF N00718. REPAIR IAW EA 6-5312-95504. 2L72 4F RTA35EU 20051212000432005121200043 2005 12 12 TQ0A520050003 420051121A6113 BULKHEAD DHAV DHC2 DHC2* 2800108EA PWA R985 R985AN14B 52008NE HARTZLHCB3R HCB3R302 GL SPINNER CRACKED E TQ0AK NONE O OTHER ININSP/MAINT 1 AL0567667 79 1309 18416 EM83 SPINNER BULKHEAD CRACKED. 1H71 3R3 R A806 5E1 5 CP28EA 20051212000462005121200046EU 2005 12 12 05FDEA04088 120051203A5101 REPAIR AIRBUS310 A310 EU FUSLEAGE NONE A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25424FE 241 PREVIOUS REPAIR INSTALLED AT FUSELAGE RIGHT SIDE, BELOW R1 DOOR AT STA 1187 TO STA 1212, FS 14A TO FS 15. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND TO CONFORM SRM 53-12-12 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR 2L72 4F RTA35EU 20051212000582005121200058NM 2005 12 12 QXEA200501585 120051110A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX - RIGHT OUTBOARD SEAT TRACK NR 10 HAS CORROSION AROUND LUG HOLE AT STATION X280. REPAIRED IAW RD 8-53-1342, DHC-8-200 SRM 51-20-16 AND 51-20-36. 2H72 4T RTA13NM 20051212000662005121200066NM 2005 12 12 QXEA200501593 120051113A5540 HINGE DHAV DHC8 DHC8202 2809007NM RUDDER CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX - SAFETY HINGE AT UPPER RUDDER HINGE FOR FORE RUDDER IS CHAFED AT THE TOP SURFACE APPROXIMATELY .003 TO .005" DEEP. REPAIRED IAW RD 8-55-019. 2H72 4T RTA13NM 20051212000792005121200079WP 2005 12 12 ABXA050332 120051130A5730591214426 SKIN DOUG DC9 DC941 302207NWP RT WING CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23954AX 47612 FOUND SKIN, FORWARD OF PANEL 1601, HAD A CRACK COMPLETELY ACROSS THE SKIN. MANUFACTURED NEW SKIN AND INSTALLED IAW DC9 51-30-5 AND 51-30-1. 2L72 4F A6WE 20051212000922005121200092NM 2005 12 12 SWAA053893 120051208A53116546525 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29622SW 27932 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051212001062005121200106WP 2005 12 12 ABXA050316 120051017A5330 DOUBLER DOUG DC8 DC863F 302198FWP FS 940 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 CORRODED DOUBLER IN MAIN CARGO BELOW FLOOR LEVEL AGAINST ABOVE LEFT WHEEL WELL PRESS DECK, STA 940, LEFT BUTT LINE 67. REMOVED, FABRICATED AND REPLACED DOUBLERS IN MAIN CARGO BELOW FLOOR LEVEL AGAINST ABOVE LEFT PRESS DECK STA 940, LEFT BUTT LINE 67 IAW DC8 SRM 51-1-8, 53-2-0, 51-1-20, 51-9-0, 51-1-20D, 53-3-0, 51-3-1 AND DPS 4.710-2. 2L74 4F 4A25 20051212001082005121200108CE 2005 12 12 1050921026090 120051020A5313 STRINGER BEECH 1900 1900D 1154162CE FUSELAGE CORRODED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07146ZV UE146 CORRSION FOUND ON FASTENERS FS 150-183 AND STRINGER 1-3R. MAINTENANCE REMOVED CORROSION AND TREATED FASTENERS WITH ALODINE. 2L72 4T RTA24CE 20051212001252005121200125WP 2005 12 12 05FDEA04136 120051205A5520 REPAIR DOUG DC10 DC1030F 3023504WP LT ELEVATOR UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 FOUND UPPER INBOARD LT ELEVATOR FOUND 1 EXTERNAL DOUBLER REPAIR BETWEEN XE 240 AND XE 191 DIMENS. 45" BY 8". PERFORMED INSPECTION ON REPAIR DOUBLER IAW SRM 55-10-00 FIG 8 VOL 1 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2, RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 PAR 33 AND 24 VOL 2. 2L73 4F RTA22WE 20051212001392005121200139NM 2005 12 12 SWAA053862 120051204A53306545776 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29671SW 23785 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947.5, STR 24R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051212001572005121200157EU 2005 12 12 ASOA05935 120051030A25601135200051 FLASHLIGHT AEROSPATR72 ATR72212 8680945EU CABIN INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27632AS 338 DURING GROUND INSPECTION IN ATL, THE AFT FLIGHT ATTENDANTS FLASHLIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT FLIGHT ATTENDANTS FLASHLIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20051212001622005121200162EA 2005 12 12 SWIA200515937 120051117A5310 VERTICAL BEAM CNDAIRCL600 CL6002B19 1900309EA BS 409 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07411SW 7067 FUSELAGE; VERTICAL BEAM; LOWER I/B + O/B FLANGES ARE CRACKED; FS 409.0 + 128; RBL 27.0, ITEM FOUND AT C-CHECK INSPECTION. REPAIR LOWER I/B & OB FLANGES, FS 409.0 + 128; RBL 27.0 IAW CRJ REO 601R-53-41-056 REV "C". 2L72 4F RTA21EA 20051212001652005121200165EA 2005 12 12 SWIA200515940 120051117A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA BS 625 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07411SW 7067 AFT EQUIPMENT COMP; INTERCOSTAL CLIP IS CRACKED; FS 625.00 STR 14R, ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIP IAW CRJ REO 601R-53-61-100, REV NC & REO 601R-53-61-422 REV NC. 2L72 4F RTA21EA 20051212001682005121200168EA 2005 12 12 SWIA200515943 120051117A5320 SUPPORT ANGLE CNDAIRCL600 CL6002B19 1900309EA BS 589 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07411SW 7067 CRACKED SUPPORT ANGLE UNDER CARGO DOOR SILL AT STA 589 LBL 42, ITEM FOUND AT C-CHECK INSPECTION. 2L72 4F RTA21EA 20051212001742005121200174NM 2005 12 12 AWXA200501484 120051205A2410 GENERATOR BOEING737 73733A 1384673NM NR 1 ENGINE INOPERATIVE A AWXAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 WP28168AW 23629 PILOTS REPORTED LOSS OF NR 1 ENG A/C GEN SYS FELL OFFLINE AT FL 350 & WOULD NOT RESET. VOLTS & FREQUENCY READING ZERO. NO CSD LOW OIL PRESSURE LIGHT PRESENT. RESIDUAL VOLTS AT 115. ATTEMPT TO START APU UNSUCCESFUL DIVERTED SLC FOR REPAIRS. MX PLACED NR 1 ENGINE DRIVEN GEN SYS ON MEL. MX SERVICED APU OIL LEVEL TO IT'S PROPER LEVEL & STARTED APU SUCCESSFULLY. OPS CHECKS WERE FOUND OK. R & R NR 2 ENG. GEN IAW AMWEST TASK CARD R5M24002. DISCOVERED YELLOW CONDUCTOR WIRE SHORTING. REPAIRED WIRE. OPS CHECKS WERE GOOD. VENDOR CONFIRMED FAILURE, FAILED INCOMING TEST. TEARDOWN FOUND SCREEN ON STATOR ASSEMBLY LOOSE. THE UNIT WAS REPAIRED AND TESTED IAW CMM 24-20-77 REV.20 2L72 4F RTA16WE 20051212001762005121200176NM 2005 12 12 QXEA200501743 120051203A7312 HEATER DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE FUEL SYSTEM MALFUNCTIONED A QXEAO OTHER O OTHER CRCRUISE 1 NM09366PH 510 SEA FLIGHT NR 2256 AT CRUISE, NR 2 FUEL TEMP 45 DEGREES AND SLOWLY RISING. IN DESCENT TEMP REACHED 54 DEGREES. RAN THE EMERGENCY CHECKLIST AND THE AUX PUMP COOLED IT TO 50 DEGREES AND IT THEN CONTINUED TO RISE REACHING THE RED RADIAL AT LANDING. MAINTENANCE REPLACED THE NR 2 FUEL HEATER THERMAL ELEMENT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20051212001782005121200178 2005 12 12 QXEA200501744 420051202A34174066010904 ADC DHAV DHC8 DHC8202 2809007NM NR 1 MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09375PH151609194 529 SEA FLIGHT NR 2290 WITH NAV AND HSI SELECT ON CAPTAINS SIDE, THE ADVISORY DISPLAY SHOWS DAOC DATA INVALID MESSAGE. CAPTAINS AIRSPEED INDICATOR DROPPED TO ZERO FOR ABOUT 8 - 10 SECONDS. CHECKLIST PROCEDURE WAS FOLLOWED WHICH ADVISED TO CHANGE HSI SELECT TO FIRST OFFICERS SIDE. CAPTAINS AIRSPEED THEN RETURNED TO NORMAL. MAINTENANCE REPLACED NR 1 AIR DATA COMPUTER IAW -8200 MTX TASK CARD 9340014. PERFORMED PITOT/STATIC LEAK TEST IAW MTC 9341101, NO LEAKS NOTED. PERFORMED THE TRANSPONDER TEST IAW MTC 9345001. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051212001802005121200180CE 2005 12 12 105092102690 120051020A5313129440000209 STRINGER BEECH 1900 1900D 1154162CE BS 163 CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07146ZV UE146 FOUND STRINGER 3R AT FS 163.9. CRACKED. MAINTENANCE REMOVED CORROSION AND TREATED FASTENERS WITH ALODINE. THEREFORE NO PARTS WERE USED. 2L72 4T RTA24CE 20051212001822005121200182CE 2005 12 12 1050921026120 120051020A53201294400673 ANGLE BEECH 1900 1900D 1154162CE BS 400 CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07146ZV UE146 FOUND LEFT FS 400 1 FT ABOVE FLOOR CRACKED. MAINTENANCE FABRICATED REPAIR ANGLE AND INSTALLED. 2L72 4T RTA24CE 20051212001882005121200188NM 2005 12 12 AWXA200501487 120051118A5347D5713014720000 SEAT TRACK AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28660AW 1234 SAL - DURING BC4 CHECK DISCOVERED CORROSION ON RT INBOARD SEAT TRACK AT FS 38+11". MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 101. REMOVED AND INSTALLED NEW SEAT TRACK FROM FS 36 TO FS 40 IAW AIRBUS 320 SRM 51-42-11. 2L72 4F RTA28NM 20051212001902005121200190EA 2005 12 12 SWIA200515959 120051204A2751 SENSOR CNDAIRCL600 CL6002C10 1390015EA SLATS MALFUNCTIONED A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07701SK 10133 SLAT FAULT STATUS MESSAGE. REPLACED BOTH SLAT DISCONNECT SENSORS IN LEFT WING IAW CRJ 700 27-81-39. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051212001922005121200192EA 2005 12 12 SWIA200515961 120051130A2750 PDU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07916SW 7634 FLAP 1/2 SPEED MSG ILLUMINATED. REPLACED FLAP POWER DRIVE UNIT IAW AMM 27-52-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051212001942005121200194EA 2005 12 12 SWIA200515963 120051205A2750 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 NM07935SW 7725 FLAPS FAIL CAUTION MSG ON FINAL. REPLACED LT BPSU AND FECU IAW CRJ 200 MM 27-51-10. OPERATIONAL CHECK GOOD, PN 860D100-18; SN OFF 1191, PN 855D100-11; SN OFF 1999. 2L72 4F RTA21EA 20051212001962005121200196NM 2005 12 12 SB05162 120051204A335020131A BATTERY PACK BOEING737 737401 1384701NM AFT CABIN DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19409US 23879 CLT - MAINTENANCE REPORTED THAT SOME OF THE EMERGENCY LIGHTS IN THE AFT CABIN WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20051212001982005121200198NM 2005 12 12 05FDEA04195 120051209A5540 RUDDER DOUG MD11 MD11 3023602NM DAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25576FE 48501 DURING AIRPLANE'S CONVERSION FROM P TO F, ACCIDENTAL DAMAGE LOWER AFT RUDDER. DURING BRAKE SYSTEM BLEED PROCURE WITH HYD PRESSURE AND LOCK PINS IMPROPERLY INSTALLED AN ERRONEOUS MANEUVER OF THE RUDDER PEDALS CAUSED SUDDEN MOVEMENT OF THE RUDDER TOUCHED THE WORK STAND PLATFORMS. THE DAMAGE CONSIST OF -2EA CRACK ON LT SIDE APPROX 1.5 X 0.355 INCH, T/E 1, .5 X 0.625 INCH, 1EA DENT OF RT SIDE SKIN 1.8 X 11 INCH. REMOVED RUDDER ACCOMPLISHED DVI HINGE, BRACKETS ROD END, FITTING ECC NOT FOUND DEFECT. REPAIRED SKIN LT, RT SIDE FOR SRM 55-10-01 FIG 2. REPAIRED T/E COVER FOR SRM 55-30-00 FIG 1. INSTALLED LOWER AFT RUDDER IAW MM 27-20-20-4. 2L73 4F RTA22WE 20051212002012005121200201WP 2005 12 12 05FDEA04198 120051209A5330 REPAIR DOUG DC10 DC1010 3022110WP BS 475-480 IMPROPER A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25568FE 47827 DURING AIRPLANE' S P TO F MODIFICATION FOUND: AT STA 475-480, STR 30 RT, 1EA EXT REPAIR DOUBLER. REMOVED AND SCRAPPED EXISTING REPAIR DOUBLER IAW SRM 51-33-01, PERFORMED NEW REPAIR PER SRM 53-20-00 FIG 6 SH 15. 2L73 4F A22WE 20051213000052005121300005NM 2005 12 13 05FDEA04187 120051208A5230 SEAL DEPRESSOR BOEING727 727200 138407ENM CARGO DOOR CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 LOWER FWD CARGO DOOR, LOWER DOOR FRAME IS CHAFED. REMOVED AND REPLACED LWR FWD CARGO DOOR FRAME PER SRM 51-30-2. 2L73 4F RTA3WE 20051213000082005121300008NE 2005 12 13 DXTA200501123 220051117A731031J240401 FUEL FILTER CESSNA560 560XL 2076702CE PWA 545 PW545A NE RT ENGINE CONTAMINATED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07615QS 5605360 RT ENG FUEL FILTER BYPASS LIGHT ILLUM ON T/O ROLL AT T/O PWR EXTINGUISHED WHEN PWR REDUCED. VERIFIED RT FUEL FILTER BYPASS LIGHT ILLUMIN NEAR T/O PWR SETTINGS. INSTALLED NEW FUEL FILTER & NEW O-RINGS. ALL PARAMETERS NORMAL. INSPECTED FILTER AFTER RUN, NO DEFECTS NOTED. 2L72 4F4 FRTA22CE E00059EN 20051213000102005121300010 2005 12 13 CALA0500426 420051204A2330RDAA341305 ELECTRICAL BOX BOEING767 767424ER 1385270NM ROW 26 DEF SHORTED A CALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2778060 29455 THE FLIGHT CREW REPORTED SMOKE IN THE CABIN WHILE EN ROUTE FROM HNL TO GUM. THE SMOKE WAS COMING FROM THE DSEB UNDER ROW 26 DEF. THE IFE FOR THAT ZONE WAS TURNED OFF AND THE SMOKE DISSIPATED. THE FLIGHT WAS CONTINUED TO GUM WHERE IT LANDED WITHOUT FURTHER PROBLEM. MAINTENANCE REMOVED AND REPLACED THE DSEB PER MM 23-32-74. THE WIRE HARNESS WAS INSPECTED AND NO PROBLEMS WERE NOTED WITH THE HARNESS OR PINS. OPERATION OF THE IFE SYSTEM AT ROW 26 DEF CHECKED GOOD. 2L72 4F RTA1NM 20051213000112005121300011NM 2005 12 13 CALA0500427 120051204A2530416100129 COFFEEMAKER BOEING737 737524 1384721NM FWD GALLEY BURNED A CALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2717620 27333 A STRONG ELECTRICAL ODOR THAT APPEARED TO BE COMING FROM THE FORWARD GALLEY WAS NOTED IN THE COCKPIT AND CABIN WHILE EN ROUTE TO IAH. THE OVENS, COFFEEMAKERS, AND GALLEY POWER WAS TURNED OFF. THE ODOR DISSIPATED AND THE FLIGHT WAS CONTINUED TO IAH WHERE IT LANDED WITHOUT FURTHER PROBLEM. MAINTENANCE ISOLATED THE PROBLEM TO THE FORWARD GALLEY INBOARD COFFEEMAKER. BOTH COFFEEMAKERS WERE REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE. THE WIRING AND CONNECTORS WERE INSPECTED WITH NO OTHER PROBLEMS FOUND. BOTH COFFEEMAKERS WERE OPERATED WITH NO DEFECTS NOTED. 2L72 4F RTA16WE 20051213000272005121300027NM 2005 12 13 USAA051462 120051205A5310 CREASE BEAM BOEING737 7374B7 1384702NM STA 615 TO 639 LCORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 STA 615 TO 639 LEFT CORRODED. MAJOR REPAIR, REMOVED CORROSION AND TREATED IAW SRM 53-60-13, DEFECT SIZE: 2 INCHES. 2L72 4F RTA16WE 20051213000392005121300039NM 2005 12 13 USAA051472 120051207A5320 ANGLE BOEING737 7374B7 1384702NM SERVICE DOOR CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 Z-ANGLE AT FWD SERVICE DOOR FROM STA 294 TO 330 CORRODED. MAJOR REPAIR, REMOVED AND REPLACED WITH NEW Z-ANGLE IAW SRM 51-10-02 STEP 8. DEFECT SIZE: .250 X .250 INCH TO 1 X 2 INCH. 2L72 4F RTA16WE 20051213000452005121300045 2005 12 13 SWAA053888 420051206A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29386SW 26601 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051213000482005121300048NM 2005 12 13 SWAA053891 120051207A5313BAC1498 STRINGER BOEING737 7373G7 1384595NM BS 727B CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29683SW 24008 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER CRACKED AT BS 727B, STR 14R. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2L72 4F RTA16WE 20051213000502005121300050NM 2005 12 13 2005UALA01251 120051109A3350362624 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29118UA 28811 EEL INOP AT SEAT 1A, 4E AFT, 5E, 17B. *S/D* REPLACED LAMPS. 2L74 4F4 FRTA20WE E24NE 20051213000682005121300068NM 2005 12 13 2005UALA01348 120051126A5311 FRAME BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU BS 787 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29921UA 25388 FUSELAGE FRAME WEB CRACKED AT STATION 787 STRINGER 9 RIGHT. REMOVED DAMAGE & VERIFIED CRACK CONTAINMENT & INSURANCE CUT BY NDT PER MM 53-10-84. FABRICATED AND INSTALLED NESTED REPAIR ANGLES & FILLER PER MM53-10-84. 2L72 4F4 FRTA16WE E21EU 20051213000702005121300070EU 2005 12 13 2005UALA01350 120051128A5310 BEAM AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29434UA 592 CORROSION OUTBOARD BEAM FWD OF R2 DOOR BETWEEN FR66 & FR65. REPLACED DOOR R2 SILL PER SRM 51-42-00-004. 2L72 4F4 FRTA28NM E40NE 20051213000812005121300081NM 2005 12 13 2005UALA01361 120051128A3397 CONNECTOR BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHTSLOOSE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29127UA 28813 EEL INOP, FWD SECTION MAIN STAIR WALL UPPER LEVEL. RESECURED LOOSE CONNECTOR. 2L74 4F4 FRTA20WE E24NE 20051213000972005121300097NM 2005 12 13 2005UALA01377 120051129A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE GALLERY DOOR MISSING A UALAK NONE O OTHER ININSP/MAINT 1 WP29116UA 26908 DOOR 4 GALLEY FWD LOWER WALL EMERGENCY EEL LIGHT MISSING. REPLACED DOOR 4 GALLEY FWD LOWER WALL EMERGENCY LIGHT. 2L74 4F4 FRTA20WE E24NE 20051213001002005121300100NM 2005 12 13 2005UALA01380 120051130A5313 STRINGER BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU STR 6R AT STA 72CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29921UA 25388 STRINGER 6R CRACKED AT STATION 727B. REMOVED 22.5" SECTION OF STRINGER. ACP NDT VERIFICATION OF CRACK CONTAINMENT. FABRICATED STRINGER SECTION & REPAIR "Z" ANGLES & HEAT TREATED. INSTALLED NESTED "Z" ANGLES REPAIR PER SRM53-00-03 #3, SRM 51-40-01 & SRM 51-40-03. REPLACED ADJACENT STRINGER CLIPS PER SRM 51-40-02. 2L72 4F4 FRTA16WE E21EU 20051213001082005121300108EA 2005 12 13 COMA0560684 120051211A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01927CA 7031 FLIGHT 4958 - EN ROUTE LAN-CVG, RECEIVED A THRUST REVERSER UNLOCK MESSAGE, CREW DECLARED AN EMERGENCY AND DIVERTED TO DAY. FLIGHT LANDED WITHOUT INCIDENT. 2L72 4F RTA21EA 20051213001142005121300114EA 2005 12 13 COMA0560682 120051210A5270 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR WARNING LIGHT A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01971CA 7145 FLIGHT 5115- DURING CLIMB-OUT AT MLB RECEIVED A CABIN DOOR OUTER HANDLE CAUTION MESSAGE, FLIGHT DIVERTED TO MCO. DEFERRED CABIN DOOR INDICATION SYSTEM PER MEL. 2L72 4F RTA21EA 20051213001152005121300115EA 2005 12 13 COMA0560677 120051207A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS WARNING LIGHT A COMAO OTHER J WARNING INDICATION DEDESCENT 1 SO01988CA 7204 FLIGHT 5616 - RECEIVED A FLAP FAIL CAUTION MESSAGE INBOUND TO YYZ, FLIGHT LANDED WITHOUT INCIDENT. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION, PARAGRAPH (B) 1,2,3 (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2L72 4F RTA21EA 20051213001312005121300131WP 2005 12 13 ABXA050342 120051031A5330 SKIN DOUG DC8 DC863F 302198FWP BS 857 MISDRILLED A ABXAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL23826AX 46061 FOUND UPPER CARGO STA 857, LEFT BUTT LINE 60 - RIGHT BUTT LINE 60, 5 FASTENERS MIS-DRILLED IN TOP OF CENTER TANK TO SPAR SKIN. REAMED HOLES TO REMOVE DAMAGE, FABRICATED REPAIR BUSHINGS FOR 11 HOLES. INSTALLED REPAIR BUSHINGS WITH WET SEALANT IN HOLES. CONTOURED LOWER BUSHING SURFACE, IN TANK, TO SPAR ANGLE. REF ENGINEERING AUTHORIZATION, BUSHINGS IAW DC8 SRM 51-1-25. 2L74 4F 4A25 20051213001322005121300132EA 2005 12 13 SWIA200515965 120050809A5320 WEB CNDAIRCL600 CL6002B19 1900309EA E/E BAY CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07448SW 7678 AFT EQUIPMENT BAY; ESB LOWER WEB IS CRACKED; LBL 38.0; EXTENDING FROM ACCESS PANEL CUT-OUT, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-61-366 REV "E". 2L72 4F RTA21EA 20051213001342005121300134EA 2005 12 13 SWIA200515967 120051204A2740 MCU CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07907SW 7511 "STAB CH 1 INOP" STATUS MSG CAME ON EN ROUTE TO ORD AND REMAINED ON AFTER SHUTDOWN. REPLACED HORIZONTAL STABILIZER TRIM ACTUATOR AND MOTOR CONTROL UNIT IAW MM 27-40-00, 27-42-01, 27-42-05 AND CAPT'S HORIZONTAL STAB TRIM SWITCH IAW CRJ MM 27-41-05. OPERATIONAL CHECK GOOD, P/N MOTOR CONTROL UNIT: 7062-3 S/N OFF: 216 P/N HSTA: 8396-3 S/N OFF: 778. 2L72 4F RTA21EA 20051213001362005121300136EA 2005 12 13 SWIA200515970 120051206A2797 WIRE CNDAIRCL600 CL6002B19 1900309EA ELEVATOR TRIM DAMAGED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07431SW 7536 FO TRIM SWITCH (ELEVATOR) INOP. REPAIRED WIRING AT FO'S TRIM SWITCH. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051213001372005121300137 2005 12 13 SWIA200515971 420051206A3497 WIRE CNDAIRCL600 CL6002B19 1900309EA STALL WARNING DAMAGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07983SW 7961 STALL FAIL MSG ON STALL TEST. PUSHER DOES NOT ACTUATE. REPAIRED WIRING AT GROUND STUD N1728 IAW 20-00-00 AND WDM 27-35-00 SHEET 6 OF 11 PAGE 4. OPERATIONAL CHECK GOOD IAW MM 27-35-01. 2L72 4F RTA21EA 20051213001382005121300138WP 2005 12 13 ABXA050345 120051026A5310 DOUBLER DOUG DC8 DC863F 302198FWP STA 1180 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 CORROSION ON TOP OF LONGERON REINFORCEMENT DOUBLER IN AFT CARGO BILGE AT STA 1180, LONGERON 35 RIGHT. REMOVED CORROSION AT STA 1180, LONGERON 35 RIGHT. FOUND TO BE OUT OF LIMITS. FABRICATED, TREATED, PRIMED AND INSTALLED NEW DOUBLER FROM 7075-T6, 0.125", PO NR 111960 IAW DC8 SRM 51-1-8, 51-1-20D, 53-2-0, LWR 200302015 AND SSRM DWG K07142. 2L74 4F 4A25 20051213001502005121300150NM 2005 12 13 SWAA053899 120051210A335090083 CHARGER BOEING737 7373H4 1384600NM EMERGENCY LIGHT FAILED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED A2 CHECK, R2 DOOR EMERGENCY EXIT SIGN FAILED TEST. REMOVED AND REPLACED BATTERY CHARGER PER MM. 2L72 4F RTA16WE 20051213001522005121300152NM 2005 12 13 SWAA053901 120051207A575465C26601 SKIN BOEING737 7373H4 1384600NM NR 6 SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 DURING SCHEDULED C4 CHECK, FOUND NR 6 L/E SLAT T/E WEDGE DELAMINATED. REMOVED AND REPLACED SLAT PER MM. 2L72 4F RTA16WE 20051213001532005121300153NM 2005 12 13 SWAA053902 120051207A57536546435 SKIN BOEING737 7373H4 1384600NM TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 DURING SCHEDULED C4 CHECK, FOUND RT WING OTBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM. 2L72 4F RTA16WE 20051214000062005121400006NM 2005 12 14 05FDEA04173 120051208A5270 SWITCH BOEING727 727200 138407ENM AIRSTAIR DOOR MISINSTALLED A FDEAA UNSCHED LANDING WN INADEQUATE Q C FALSE WARNING CRCRUISE 1 SO25288FE 21850 AFT AIRSTAIR AMBER LT ILLUMINATED PRIOR TO BLOCKOUT- ADJUSTED BY MAINTENANCE WHEN AFT AIRSTAIR AMBER LT ILLUMINATED IN FLIGHT- RAN QRH RED TABS. ENT BY: 353958 MEL 08DEC05 10:15 IND ACN RELEASED FOR SERVICE PER MEL/CDL: 52-06-B CAT: C EXP: 16DEC05 C/0257532. FOUND S395 SW INSTALLED INCORRECTLY. INSTALLED CORRECTLY. ALSO FOUND WRONG SW ACT INSTALLED. INSTALLED PROPER ASSY. 2L73 4F RTA3WE 20051214000072005121400007NM 2005 12 14 05FDEA04190 120051208A5313 LONGERON DOUG MD11 MD11 3023602NM ZONE 800 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 CAC COMPARTMENT RIGHT HAND BILGE AREA LONGERON 48R STATION 1139 FOUND EDGE WITH CORROSION. REPAIR CARRIED OUT AS PER FEDEX EA 1-5310-94573 (TITLE: FUSELAGE- MAINFRAME- BODY STATION Y=1134.000, THROUGH Y=1142.000 / LONGERON 48 (RH) SPLICE CORROSION REWORK & REPAIR). REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20051214000082005121400008NM 2005 12 14 05FDEA04191 120051208A5753 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RIGHT HAND WING OUTBOARD FLAP INBOARD AFT HINGE BRACKET FORWARD FITTING ATTACH HOLE AT INBOARD AFT POSITION FOUND CORRODED. CORROSION REMOVED AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-90701. 2L73 4F RTA22WE 20051214000092005121400009NM 2005 12 14 05FDEA04192 120051208A5753 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RT WING OUTBOARD FLAP INBOARD AFT HINGE BRACKET FORWARD FITTING ATTACH HOLE AT OUTBOARD AFT POSITION FOUND CORRODED. CORROSION REMOVED AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-90700. 2L73 4F RTA22WE 20051214000102005121400010NM 2005 12 14 05FDEA04193 120051208A5753 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RIGHT HAND WING OUTBOARD FLAP INBOARD AFT HINGE BRACKET AFT FITTING FORWARD ATTACH HOLE FOUND CORRODED. CORROSION REMOVED AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-90699. 2L73 4F RTA22WE 20051214000112005121400011NM 2005 12 14 05FDEA04194 120051208A5753 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 LEFT HAND WING OUTBOARD FLAP INBOARD AFT HINGE BRACKET FORWARD FITTING ATTACH HOLE AT OUTBOARD AFT POSITION FOUND CORRODED. CORROSION REMOVED AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-90702. 2L73 4F RTA22WE 20051214000142005121400014NM 2005 12 14 USAA200512002 120051201A5330 SKIN BOEING737 737401 1384701NM BS 887 WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19418US 23985 .013 INCH SKIN WEAR, 12 INCH LONG AT STA 887 AND S2R-L (UNDER DORSAL FIN). INSTALLED DOUBLER IAW SRM AND EA 97151. 2L72 4F RTA16WE 20051214000162005121400016 2005 12 14 PIDA20050196 420051202A22104038891916 COMPUTER BOEING737 737228 13844AGNM AUTOPILOT INOPERATIVE A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05252TR 23001 A CHANNEL AUTOPILOT INOP. PLACED ON MEL 22-1. 12/6/2005: REPLACED "A FLIGHT CONTROL COOMPUTER PER MM 22-11-331. OPS CHECKS GOOD. 2L72 4F RTA16WE 20051214000172005121400017CE 2005 12 14 74424 120051202A52101013810159 SHUTOFF VALVE BEECH 1900 1900D 1154162CE PAX DOOR FAILED A AMWAA UNSCHED LANDING O OTHER CLCLIMB 1 CE0710675 UE229 ON CLIMB OUT, CREW WENT TO PRESSURIZE AIRCRAFT AND THE CABIN DOOR ANNUNCIATOR ILLUMINATED. CREW RETURNED TO FIELD WITH NO FURTHER INCIDENT. THE CORRECTIVE ACTION WAS THAT MAINTENANCE REPLACED THE RIGHT INSTRUMENT AIR SHUT OFF VALVE. MORE INFORMATION WILL BE AVAILABLE AT LATER DATE. 2L72 4T RTA24CE 20051214000182005121400018 2005 12 14 SA05123 420051205A256561639103 BOTTLE AIRBUSA321 A321211 3930370EU MID LT CABIN LOW A USAAK NONE O OTHER ININSP/MAINT 1 EA19186US1309813098 1701 PHL - PILOT REPORTED THE LEFT OVERWING EXIT SLIDE BOTTLE PRESSURE LOW. MAINTENANCE REMOVED AND REPLACED THE SLIDE BOTTLE. CHECKS OK PER TASK 25-62-49-020. 2L72 4F RTA28NM 20051214000192005121400019NM 2005 12 14 QXEA200501766 120051208A2120 ODOR BOMBDRDHC8 DHC8402 1390042NM COCKPIT DETECTED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM09411QX 4055 SEA FLIGHT 2329: EXHAUST SMELL COMING FROM NR 2 BLEED AIR. TURNED NR 2 BLEED AIR OFF AND SMELL WENT AWAY. MAINTENANCE GROUND RAN NR 2 ENGINE WITH BLEED AIR ON FOR EXTENDED TIME. NO EXHAUST SMELL IN CABIN OR COCKPIT. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051214000202005121400020NM 2005 12 14 SWAA053925 120051212A53306516352 BEAR STRAP BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN BEAR STRAP CORRODED AT BS 442, RBL 8, FWD CARGO DOOR CUTOUT. REPAIRED SKIN PER BFG ER & SRM. 2L72 4F RTA16WE 20051214000212005121400021NM 2005 12 14 SWAA053926 120051212A3350MS155721 BULB BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29324SW 23414 DURING SCHEDULED A1 CHECK, FOUND RT MID CABIN EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20051214000232005121400023EA 2005 12 14 COMA0560702 120051209A27501104S5100201 COUPLING CNDAIRCL600 CL6002B19 1900309EA TE FLAP UNRELIABLE A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01446CA 7546 FLIGHT 5106 - FLAPS FAIL CAUTION. REPLACED FLAP FLEX DRIVE SHAFTS. 2L72 4F RTA21EA 20051214000252005121400025EA 2005 12 14 COMA0560697 120051208A326016600101 UPLOCK CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01967CA275412573 7134 FLIGHT 5462 - GEAR DISAGREE WARNING. REPLACED NLG UPLOCK. 2L72 4F RTA21EA 20051215000012005121500001NM 2005 12 15 SWAA053943 120051213A3350101073 LENS BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29322SW 23343 DURING SCHEDULED C3 CHECK, FOUND EMERGENCY LIGHT LENS LOOSE AT ROW 6 ABC. SECURED LENS PER MM. 2L72 4F RTA16WE 20051215000022005121500002NM 2005 12 15 CALA0500428 120051209A541065C2630812 FRAME BOEING737 7373T0 1384582NM NR 2 PYLON CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714308 23359 INSPECTION FOUND A 1 INCH CRACK IN NR 2 PYLON FRAME (HORSE COLLAR FITTING) AROUND LOCK FASTENER COLLAR. THE NR 2 PYLON HORSE COLLAR WAS REMOVED AND REPLACED IAW SRM 51-10-2. 2L72 4F RTA16WE 20051215000032005121500003NM 2005 12 15 CALA0500429 120051210A53226546563 SHEAR TIE BOEING737 7373T0 1384582NM STA 967 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714308 23359 INSPECTION FOUND FRAME/SHEAR TIE CORRODED AT STA 967 BETWEEN STRINGERS 27L-27R. THE CORRODED SECTION OF SHEAR TIE WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-00-07, FIGURE 201, REPAIR 8. 2L72 4F RTA16WE 20051215000042005121500004NM 2005 12 15 CALA0500430 120051208A5315141T5112 FLOORBEAM BOEING767 767224 1385170NM BS 303 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776151 30430 INSPECTION FOUND THE FLOORBEAM CORRODED AT BS 303, LBL 27 TO LBL 31. THE CORRODED SECTION OF FLOORBEAM WAS REPLACED IAW SRM 53-00-51, FIGURE 201, REPAIR 2. 2L72 4F RTA1NM 20051215000062005121500006NM 2005 12 15 CALA0500432 120051209A3397NA WIRE BOEING737 737524 1384721NM EMERGENCY LIGHTSSHORTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717614 27327 INSPECTION FOUND THE EMERGENCY EXIT LIGHTS OUT ON SEAT ROWS 7-14ABC. MAINTENANCE FOUND A POWER WIRE SHORTED TO SEAT TRACK AT SEAT 7ABC. THE WIRE WAS REPAIRED IAW SRM 20-11-00. 2L72 4F RTA16WE 20051215000092005121500009NM 2005 12 15 CALA0500435 120051211A2121731376B FAN BOEING757 75733N 1384931NM EQUIP COOL. SYS INOPERATIVE A CALAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SW2757863 32587 A SMOKY ODOR WAS REPORTED IN THE COCKPIT AND CABIN WHILE ON DESCENT INTO LAS. THE ODOR CLEARED WITHIN 2-3 MINUTES. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED INSPECTIONS IAW MM 05-51-58 AND LOCATED THE SOURCE OF THE ODOR AS COMING FROM A FAILED FORWARD EQUIPMENT COOLING FAN. THE FORWARD EQUIPMENT COOLING FAN WAS REMOVED AND REPLACED. LEAK AND OPERATIONAL CHECKS WERE GOOD IAW MM 21-58-06. 2L72 4F RTA2NM 20051215000102005121500010NM 2005 12 15 CALA0500436 120051211A2612G718505 CONTROL PANEL BOEING737 737524 1384721NM FIRE CONTROL INOPERATIVE A CALAFA ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW271664612355 28907 MASTER CAUTION LIGHT & FWD PANEL OVERHEAT/DET LIGHT ILLUMINATED. A-SYS TEST WAS RUN, CHECKED NORMAL. FIVE MINUTES LATER, RED FIRE LIGHT ON CARGO DETECTION SYS ILLUMINATED AND BELL SOUNDED. QRH FOLLOWED AND LIGHT EXTINGUISHED AFTER SECOND FIRE BOTTLE DISCHARGED. AIRCRAFT RETURNED WITHOUT INCIDENT. MX FOUND NO EVIDENCE OF FIRE. FAULT WAS ISOLATED TO COCKPIT FIRE SUPPRESSION PANEL. THE FIRE SUPRESSION PANEL WAS REMOVED AND REPLACED. BOTH CARGO FIRE BOTTLES, METERING VALVE, DIVERTER VALVE, AND LINE FILTERS WERE ALSO REPLACED IAW MM 26-23-10 AND MM 26-26-10. A TEST WAS PERFORMED ON THE FIRE PANEL IAW MM 26-16-10 AND ALL TESTED GOOD. AN OPERATIONAL CHECK OF THE CARGO FIRE SYSTEM CHECKED GOOD. 2L72 4F RTA16WE 20051215000122005121500012NM 2005 12 15 SWAA053927 120051212A53306545768 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29511SW 24188 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 328, STR 17R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051215000142005121500014NM 2005 12 15 SWAA053929 120051212A53126546568 STIFFENER BOEING737 7375H4 138449DNM BS 1016 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29511SW 24188 DURING SCHEDULED 1/2D CHECK, FOUND BS 1016 AFT PRESSURE BULKHEAD ANGLE STIFFENER CORRODED AT BL 0. REPAIRED ANGLE STIFFENER PER ACO & SRM. 2L72 4F RTA16WE 20051215000172005121500017EA 2005 12 15 COMA0560686 120051206A2750865D1007 PDU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01959CA255871629 7116 FLIGHT 2750 - FLAPS FAIL CAUTION. REPLACED THE FLAP PDU. 2L72 4F RTA21EA 20051215000182005121500018EA 2005 12 15 QXEA200501769 120051210A2121GG670950227 FAN CNDAIRCL600 CL6002C10 1390015EA RECIRCULATION FAULTY A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09604QX9253 8305 10019 OKC - ON PUSHBACK FOR FLIGHT 4188. RECEIVED A RECIRC FAN FAULT MESSAGE. RETURNED TO THE GATE. MAINTENANCE PLACED THE LEFT RECIRC FAN ON MEL 21-22-1A. CIRCUIT BREAKER A5 PULLED AND COLLARED, AIRCRAFT RETURNED TO SERVICE. ON 12/10 IN DEN MAINTENANCE REPLACED THE LEFT RECIRC FAN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. MEL CLEARED. 2L72 4F RTA21EA 20051215000192005121500019EA 2005 12 15 COMA0560687 120051206A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS UNRELIABLE A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01709CA119061683 7238 FLIGHT 5399 - FLAPS FAIL CAUTION. REPLACED THE LT BPSU. 2L72 4F RTA21EA 20051215000222005121500022EA 2005 12 15 COMA0560689 120051206A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS WARNING LIGHT A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01446CA 7546 FLIGHT 5130 - FLAPS FAIL CAUTION. INSPECTED FLAP SYSTEM PER AD 98-20-01, NO DEFECTS FOUND. 2L72 4F RTA21EA 20051215000242005121500024SO 2005 12 15 RAIA00511041 120051105A4930 APU EMB 145 EMB145LR 3260212SO APU FUEL SYS LEAKING A RAIAA UNSCHED LANDING KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 CE03811HK 145256 FLT 5582 BNA - FUEL ODOR IN COCKPIT AFTER TAKEOFF. MAINTENANCE DEFERRED THE APU. 2L72 4T RTT00011AT 20051215000272005121500027EU 2005 12 15 RAIA00512010 120051205A3350 POWER SUPPLY JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT INOPERATIVE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03565HK 41082 PREFLIGHT EMERGENCY LIGHT OVERHEAD AT SEAT 9A NOT ILLUMINATING. MAINTENANCE REMOVED AND REPLACED THE NR 3 POWER SUPPLY. 2L72 4T RTA41NM 20051215000282005121500028SO 2005 12 15 RAIA00512008 120051205A3397 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCONNECTED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03840HK 145341 PREFLIGHT EMERGENCY LIGHT EXIT SIGN ON BULKHEAD NOT ILLUMINATED. MAINTENANCE RECONNECTED CONNECTOR TO POWER SUPPLY ABOVE GALLEY SERVICE DOOR. 2L72 4T RTT00011AT 20051215000292005121500029SO 2005 12 15 RAIA00512011 120051206A3397 WIRE EMB 145 EMB145 3260210SO EMERGENCY LIGHT BROKEN A RAIAK NONE O OTHER ININSP/MAINT 1 CE03806HK 145112 PREFLIGHT EMERGENCY LIGHT ON MAIN DOOR HANDRAIL OUT. MAINTENANCE RECONNECTED BROKEN WIRE AT LIGHT ASSY. 2L72 4F RTT00011AT 20051215000302005121500030SO 2005 12 15 RAIA00512012 120051206A3350 LIGHT EMB 145 EMB145 3260210SO ROWS 7-9 INOPERATIVE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03804HK 145082 PREFLIGHT EMERGENCY LIGHTS FLOOR STRIP OUT AT ROWS 7-9. MAINTENANCE DEFERRED THIS SECTION OF FLOOR LIGHTS. 2L72 4F RTT00011AT 20051215000362005121500036EA 2005 12 15 QXEA200501691 120051031A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 490-569 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, RIGHT OUTBOARD SEAT RAIL HAS SCRATCHES GOUGES AND NICKS AT STATION 490-569. REPAIRED IAW REO 670-53-00-013. 2L72 4F RTA21EA 20051215000382005121500038EA 2005 12 15 QXEA200501694 120051031A5730 DOUBLER CNDAIRCL600 CL6002C10 1390015EA LT WING LE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, LEFT WING LOWER SURFACE AT STATION 38, LOWER WING PLANK DOUBLER LEADING EDGE HAS SURFACE RUST. REMOVED RUST IAW CRJ-700 SRM 51-21-06-001-001-A01. RESTORED FINISH. 2L72 4F RTA21EA 20051215000422005121500042EA 2005 12 15 QXEA200501678 120051031A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 696 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, RIGHT SEAT RAIL HAS GOUGES ON TOP SURFACE AT STATION 696. REMOVED DAMAGE IAW REO 670-53-00-013. 2L72 4F RTA21EA 20051215000432005121500043EA 2005 12 15 QXEA200501688 120051031A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 457-475 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, LEFT OUTBOARD SEAT RAIL AT STATION 457-475 HAS SCRATCHES AND CORROSION. REPAIRED IAW 670-53-00-013. 2L72 4F RTA21EA 20051215000452005121500045EA 2005 12 15 QXEA200501671 120051031A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 485-581 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, LEFT INBOARD SEAT RAIL AT STATION 485-581 HAS CORROSION. MAINTENANCE REMOVED AND REPAIRED DAMAGE IAW CRJ-700 REO 670-53-00-013. 2L72 4F RTA21EA 20051215000462005121500046NM 2005 12 15 QXEA200501771 120051209A2731 WARNING LIGHT BOMBDRDHC8 DHC8402 1390042NM PITCH TRIM ILLUMINATED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09417QX 4086 PDX FLIGHT 2308 - AFTER START, THE PITCH TRIM CAUTION REMAINED ILLUMINATED. AFTER ENGINE SHUTDOWN, CAUTION LIGHT WENT OUT. MAINTENANCE REINITIALIZED POWER TO FCS ECU NR 1 AND 2. FAULT LIGHT DID NOT RE-ILLUMINATED. CYCLED TRIM-ELEVATOR NOSE UP AND NOSE DOWN, CHECKS OK. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051215000472005121500047EA 2005 12 15 COMA0560692 120051207A3620 OXYGEN MASKS CNDAIRCL600 CL6002B19 1900309EA CABIN DEPLOYED A COMAG O2 MASK DEPLOYED O OTHER CRCRUISE 1 SO01954CA 7100 FLIGHT 5850 - O2 MASK DEPLOYED DURING DEPRESS. REMOVED AND REPLACED O2 GENERATORS THAT DEPLOYED. 2L72 4F RTA21EA 20051215000492005121500049EA 2005 12 15 COMA0560694 120051207A275011045D100301 COUPLING CNDAIRCL600 CL6002B19 1900309EA TE FLAPS UNRELIABLE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01735CA 7267 FLIGHT 5461 - FLAPS FAIL CAUTION. REPLACED FLAP FLEX DRIVE SHAFT. 2L72 4F RTA21EA 20051215000502005121500050EA 2005 12 15 COMA0560695 120051207A27507455001 CONTROL SWITCH CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION DEDESCENT 1 SO01446CA8476 6164 7546 FLIGHT 5910 - FLAPS FAIL CAUTION. REPLACED THE FLAP CONTROL LEVER. 2L72 4F RTA21EA 20051215000542005121500054EA 2005 12 15 QXEA200501667 120051031A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 933-953 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, LEFT SIDE SEAT RAIL AT STATION 933-953 CORRODED. MAINTENANCE REPAIRED IAW REO 670-53-00-013. 2L72 4F RTA21EA 20051215000582005121500058EA 2005 12 15 QXEA200501674 120051031A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA BS 280 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC- DURING C3 CHECK, FUSELAGE STATION 280 BULKHEAD RIGHT HAND LOWER WEB HAS SEVERAL OVERSIZE HOLES FROM PREVIOUS REPAIR. REPAIRED LOWER WEB IAW CRJ-700 REO 670-53-11-052. 2L72 4F RTA21EA 20051215000592005121500059EA 2005 12 15 QXEA200501672 120051031A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 485-581 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, RIGHT INBOARD SEAT RAIL AT STATION 485-581 HAS CORROSION AND GOUGES. MAINTENANCE REPAIRED IAW CRJ-700 REO 670-53-00-013. 2L72 4F RTA21EA 20051215000622005121500062EA 2005 12 15 QXEA200501693 120051031A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 396-448 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, RIGHT OUTBOARD SEAT RAIL HAS SCRATCHES NICKS AND GOUGES AT STATION 396-448. REPAIRED IAW REO 670-53-00-013. 2L72 4F RTA21EA 20051215000632005121500063EA 2005 12 15 QXEA200501679 120051031A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA FUSELAGE GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, RIGHT INBOARD SEAT RAIL HAS CORROSION AND GOUGES ON TOP SURFACE. REPAIRED IAW REO 670-53-00-013. 2L72 4F RTA21EA 20051215000642005121500064EA 2005 12 15 QXEA200501680 120051031A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 724-830 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, LEFT INBOARD SEAT RAIL AT STATION 724-830 HAS GOUGES ON TOP SURFACE. REPAIRED IAW REO 670-53-00-013. 2L72 4F RTA21EA 20051215000652005121500065EA 2005 12 15 QXEA200501681 120051031A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 850-923 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, RIGHT INBOARD SEAT RAIL HAS GOUGES ON TOP SURFACE AT STATION 850-923. REPAIRED IAW REO 670-53-00-013. 2L72 4F RTA21EA 20051215000682005121500068NM 2005 12 15 AT00500047 120051206A2612473465 CONTROL UNIT BOEING717 717200 1383700NM APU FIRE DETECT INOPERATIVE A ZZDAO OTHER J WARNING INDICATION CLCLIMB 1 SO15935AT 55069 APU FIRE ALERT FOLLOWED QRH ALERT REMAINED ILLUMINATED UNTIL LDG ROLLOUT APU WAS OFF AT THE TIME. INSPECTED APU COMPARTMENT FOUND NO EVIDENCE OF FIRE OR OVERHEATING CONDITIONS. OPS & LEAK CHECK OF APU GOOD, REF 717 M/M 49-10. REMOVED AND REPLACED APU FIRE DETECTOR CONTROL UNIT RE 26-12, NO FAULTS NOTED AT THIS TIME. 2L72 4F TRA6WE 20051215000692005121500069NM 2005 12 15 AT0500046 120051204A33508039251 BATTERY PACK BOEING717 717200 1383700NM EMERGENCY LIGHT INOPERATIVE A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15997AT 55141 E-PATH LIGHTS ON SEATS 1, 2, 3, AND 10D WILL NOT ILLUMINATE. REMOVED AND REPLACED BATTERY PACK ASSY IAW B717 M/M 33-51, OPS CHECK GOOD. 2L72 4F TRA6WE 20051215000702005121500070EA 2005 12 15 QXEA200501675 120051031A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA BS 280 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, FUSELAGE STATION 280 LOWER WEB OF BULKHEAD HAS SEVERAL OVERSIZE HOLES FROM PREVIOUS REPAIR. REPAIRED IAW REO 670-53-11-052. 2L72 4F RTA21EA 20051215000712005121500071EA 2005 12 15 QXEA200501676 120051031A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 581-683 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, LEFT INBOARD SEAT RAIL AT STATION 581-683 HAS CORROSION ON TOP SURFACE. REPAIRED IAW REO 670-53-00-013. 2L72 4F RTA21EA 20051215000732005121500073EA 2005 12 15 QXEA200501683 120051031A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 662-665 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, LEFT OUTBOARD SEAT RAIL AT STATION 662-665 HAS SURFACE SCRATCHES. REPAIRED IAW REO 670-53-00-013. 2L72 4F RTA21EA 20051215000762005121500076EA 2005 12 15 QXEA200501697 120051031A5320 SILL CNDAIRCL600 CL6002C10 1390015EA BS 1031 WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC- DURING C3 CHECK, AFT BAGGAGE DOOR SURROUND SILL HAS AREA OF WEAR AT STATION 1031. REMOVED DAMAGE IAW CRJ-700 SEM 51-12-00-001-001-A01, NO CRACKS FOUND, .059 INCH REMOVED. SILL PLATE REPAIRED IAW EA R-53-394 AND REO 670-53-61-211. 2L72 4F RTA21EA 20051215000782005121500078NM 2005 12 15 QXEA200501753 120051120A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX - RIGHT HAND OUTBOARD SEAT TRACK NR 7 HAS .055 INCH CORROSION PIT AT APPROXIMATELY STATION X240. REPLACED IAW RD 8-53-1102, 8-53-4473 AND DHC-8-202 SRM 51-40-00. 2H72 4T RTA13NM 20051215000792005121500079NM 2005 12 15 QXEA200501754 120051122A5320 SILL DHAV DHC8 DHC8202 2809007NM PAD DOORWAY CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX - CORROSION ON UNDERSIDE OF PASSENGER DOOR SILL BY NUT PLATES. REPAIRED IAW HORIZON AIR EA 2-53-651. 2H72 4T RTA13NM 20051215000802005121500080NM 2005 12 15 QXEA200501755 120051127A5330 SKIN DHAV DHC8 DHC8202 2809007NM FUSELAGE DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX - THERE ARE TWO PROTRUDING DENTS ON LEFTHAND FUSELAGE EXTERNAL SKIN AT STATION X377.00 AND STRINGER Y31.00. REPAIRED IAW RD 8-53-2797 AND HORIZON AIR EA 2-53-640. 2H72 4T RTA13NM 20051215000812005121500081NM 2005 12 15 QXEA200501762 120051121A5320 BRACKET DHAV DHC8 DHC8202 2809007NM PAX DOOR SILL CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX - MAIN CABIN DOOR SILL BRACKET ON AFT SIDE CRACKED. REPLACED IAW DHC-8-202 SRM 51-40-11. 2H72 4T RTA13NM 20051215000852005121500085NM 2005 12 15 QXEA200501759 120051126A5753 FLAP TRACK DHAV DHC8 DHC8202 2809007NM LT WING CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX - LEFT HAND NR 4 FLAP TRACK HAS PITTING CORROSION ON INBOARD CENTER OF TRACK. REPAIRED IAW RD 8-57-988. 2H72 4T RTA13NM 20051215000862005121500086NM 2005 12 15 QXEA200501760 120051125A5753 SKIN DHAV DHC8 DHC8202 2809007NM LT TE FLAP GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX - LEFTHAND OUTBOARD FLAP UPPER INBOARD SKIN IS GOUGED YW173.00. REPAIRED IAW RD 8-57-1022. 2H72 4T RTA13NM 20051215000912005121500091CE 2005 12 15 DEBA401PP2 120051205A5755402EN5068 SWITCH RAYTHN390 390 7150030CE SPEED BRAKES MALFUNCTIONED E DEBAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 CE03401PP190 RB130 ON ACCELERATION FOR TAKEOFF THE CREW RECEIVED A TAKEOFF CONFIGURATION WARNING HORN AT 100KTS, PRIOR TO ROTATION. TAKEOFF WAS ABORTED WITHOUT INCIDENT. THE AIRCRAFT RETURNED TO THE RAMP. WHILE TROUBLESHOOTING THE PROBLEM CORRECTED ITSELF. DETERMINED THAT THE RIGHT SPEED BRAKE INBOARD PANEL STOW SWITCH MUST BE AT FAULT. REMOVED AND REPLACED SWITCH. SIMULATED FAILURE AND IT DUPLICATED THE SYMPTOMS. COMPLETED TESTING AND PERFORMED TEST FLIGHT SATISFACTORILY. 17 2 3F RTA00010WI 20051215000952005121500095NM 2005 12 15 DL73S050751 120051128A5315654541039 FLOORBEAM BOEING737 737247 138448DNM LBL 24.8 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27237WA 23185 CRACKS WERE FOUND IN THE OVERWING FLOORBEAMS AT LBL 24.8. EXISTING FLOORBEAM REPAIR/MODIFICATION WAS REMOVED AND STRUCTURAL REINFORCING WAS ADDED TO THE FLOORBEAM REF AD 2001-17-18, 93-17-08, 90-06-02, 3-056673-03AD. 2L72 4F A16WE 20051215000982005121500098NM 2005 12 15 DL76S050754 120050810A5400BACB30UU12C31D BOLT BOEING767 767332 1382001NM PYLONS INCORRECT A DALAK NONE O OTHER ININSP/MAINT 1 SO27116DL 23275 THE OUTBOARD SIDE LINK BOLT WAS TOO SHORT FOR PROPER INSTALLATION. A THINNER WASHER WAS INSTALLED REF AD 4002-16-12, 1-074906-03AD. 2L72 4F RTA1NM 20051215001052005121500105EA 2005 12 15 COMA0560704 120051206A2750865D1007 PDU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAULTY A COMAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 SO01969CA23983 7141 FLIGHT 5675 - DURING CLIMB-OUT OF CVG RECEIVED A FLAP FAIL CAUTION MESSAGE. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE POWER DRIVE UNIT. 2L72 4F RTA21EA 20051215001082005121500108EA 2005 12 15 COMA0560708 120051209A304016591 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA WINDOW HEAT MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01408CA272022710 7440 FLIGHT 5594 - RT WINDOW HEAT CAUTION. REPLACED THE WINDOW HEAT CONTROLLER. 2L72 4F RTA21EA 20051215001122005121500112NM 2005 12 15 AWXA200501513 120051121A531265163007 BULKHEAD BOEING737 73733A 1384673NM BS 178 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 MCN - DURING C19 CHECK DISCOVERED CRACK UNDER LT ANTENNA ATTACH BRACKET AT BS 178, WL 212 AND BL 5L. MAINTENANCE CUT OUT DAMAGED PART OF WEB IAW BOEING 737-300 SRM 53-10-08-2R11. FABBED DOUBLER AND SHIM IAW BOEING 737-300 SRM 53-10-08-2R11. INSTALLED FABRICATED REPAIR PARTS AT BS 178, WL 212 AND BL 5L IAW BOEING 737-300 SRM 53-10-08-2R11. 2L72 4F RTA16WE 20051215001152005121500115NM 2005 12 15 AWXA200501516 120051117A5315654681138 FLOORBEAM BOEING737 73733A 1384673NM BS 986 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 MCN - DURING C19 CHECK DISCOVERED CORROSION ON THE TOP AND BOTTOM SURFACE ON TRANSVERSE BEAM FROM BL 19L TO BL 19R, WL 208 AND BS 986. CORROSION WAS FOUND TO BE OUT O LIMITS IAW BOEING 737-300 SRM 53-60-51-1A1 FIG 101. MAINTENANCE REPAIRED BEAM FROM BL 19L TO BL 19R, WL 208 AND BS 986 IAW BOEING 737-300 SRM 53-60-51 FIG 201. 2L72 4F RTA16WE 20051212000562005121200056NM 2005 12 12 QXEA200501765 120051207A30107826896 BRUSH BLOCK DHAV DHC8 DHC8202 2809007NM PROPELLER MALFUNCTIONED A QXEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM09362PH1477 399 518 PDX FLIGHT NR 2125, RIGHT ELEVATOR HORN HEAT CAME ON DURING CLIMB, THEN STARTED CYCLING OFF WHILE RIGHT STALL WARNING LIGHT ILLUMINATED. BOTH LIGHTS CYCLED OPPOSITE DURING REMAINDER FO FLIGHT. MAINTENANCE INSPECTED PROP BRUSHBLOCKS NR 1 AND NR 2. FOUND NR 2 BRUSH BLOCK HEAVILY BURNED AND NR 1 WAS DETERIORATED. REPLACED BRUSH BLOCKS IAW DHC-8-200 AMM 61-20-11-000-801, 61-10-11-400-801. CLEANED AREA AND INSTALLED 2 NEW FUSES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051212000572005121200057NM 2005 12 12 QXEA200501584 120051110A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX - RIGHT OUTBOARD SEAT TRACK NR 10 HAS CORROSION AROUND LUG HOLE AT STATION X266. REPAIRED IAW RD 8-53-1342, DHC-8-200 SRM 51-20-16 AND 51-20-36. 2H72 4T RTA13NM 20051212000622005121200062NM 2005 12 12 QXEA200501589 120051110A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM BS 407 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX - RIGHT OUTBOARD SEAT TRACK NR 10 HAS CORROSION INSIDE CHANNEL AND LUG HOLE AREA AT STATION 407. REPAIRED IAW RD 8-53-1342, DHC-8-202 SRM 51-20-16 AND SRN=M 51-20-36. 2H72 4T RTA13NM 20051212000652005121200065NM 2005 12 12 QXEA200501592 120051110A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM BS 545 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 582 PDX - RIGHT OUTBOARD SEAT TRACK NR 12 HAS A CIRCULAR CHAFE MARK INSIDE CHANNEL AT STATION 545. REPAIRED IAW RD 8-53-3644, DHC-8-200 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20051212000722005121200072WP 2005 12 12 ABXA050325 120051128A5312592481659 BULKHEAD DOUG DC9 DC941 302207NWP BS 675 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23954AX 47612 FOUND CORROSION LONGERON 29 LEFT AND ADJACENT LONGERON PRESSURE BULKHEAD TO FS 675 LEFT KEEL AREA. REPAIRED AREA IAW DC9 SRM 53-01. 2L72 4F A6WE 20051212000762005121200076WP 2005 12 12 ABXA050329 120051128A53404916270501 FITTING DOUG DC9 DC941 302207NWP KEELBEAM CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23954AX 47612 RIGHT KEEL FS 675 LONGERON 29 RIGHT CRACKED FITTING. REMOVED AND REPLACED FITTING IAW DC9 SRM. 2L72 4F A6WE 20051212000832005121200083EA 2005 12 12 REXA200500149 120051206A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A REXAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO258894A 7894 FLAPS FAIL CAUTION AT FLAPS 2 DEGREES. LANDING UNEVENTFUL. SYSTEM REST AND PLACED ON 72 HOUR WATCH PER AD 98-20-01. 2L72 4F RTA21EA 20051212001122005121200112WP 2005 12 12 05FDEA04135 120051205A5520 REPAIR DOUG DC10 DC1030F 3023504WP LT ELEVATOR UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 INBOARD LT ELEVATOR UPPER SIDE FOUND 1 EXTERNAL DOUBLER REPAIR DIA 3" AT XE 160. PERFORMED INSPECTION OF REPAIR DOUBLER IAW SRM 55-00-01 VOL 1 FIG 3. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2 E3, RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VOL 2 PAR 33 AND 24. 2L73 4F RTA22WE 20051212001132005121200113EA 2005 12 12 QXEA200501660 120051031A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 713-760 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, RIGHT SIDE SEAT RAIL AT STATION 713-760 HAS AREAS OF CORROSION. MAINTENENCE REMOVED CORROSION IAW CRJ-700 REO 670-53-00-013. RESTORED FINISH. 2L72 4F RTA21EA 20051212001152005121200115EA 2005 12 12 QXEA200501654 120051031A5313 RIVET CNDAIRCL600 CL6002C10 1390015EA STRINGER MISSING A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, FUSELAGE INTERIOR AT STATION 685 STRINGER 6R RIVET MISSING ON STRINGER. MAINTENANCE INSTALLED RIVET IAW CRJ-700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20051212001262005121200126NM 2005 12 12 SWAA053852 120051202A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 727E, LBL 5. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051212001362005121200136NM 2005 12 12 SWAA053859 120051130A534065C27314 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29671SW 23785 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 294.5, STR 11L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051212001402005121200140NM 2005 12 12 SWAA053863 120051204A53156545410 FLOORBEAM BOEING737 7373G7 1384595NM CABIN FLOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29671SW 23785 DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 665, BL 0. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20051212001412005121200141NM 2005 12 12 SWAA053864 120051204A291065C26841 LINE BOEING737 7373Q8 1384670NM A/C BAY LOOSE A SWAAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 SW29672SW 23406 FUMES SMELL IN FWD GALLEY. FOUND HYDRAULIC FLUID LEAK AT LINE FWD OF RT AIR CYCLE MACHINE. TIGHTENED HYDRAULIC LINE PER MM. 2L72 4F RTA16WE 20051212001492005121200149WP 2005 12 12 IXXA0500125S 120050224A5730 REPAIR DOUG DC8 DC871F 302199DWP XW 34.000 IMPROPER A IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW11821BX858952998 45811 DURING A ROUTINE C CHECK INSPECTION, FOUND RT WING INBOARD FLAP AFT LOWER PANEL INTERIM REPARI AT STA XW 34.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF EXISTING REPAIR. REMOVAL OF DAMAGED SECTION. PERFORMED NDT INSPECTION, FABRICATED NEW PLATING SEGMENT, INTERNAL SPLICES, EXTERNAL REPAIR DOUBLER. CLEANED, TREATED AND PRIMED AREA, REPAIR PARTS AND INNER PART OF NEW PLATING SEGMENT. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS + NEW PLATING SEGMENT IAW SEMAN DWG ED-3855 AND FAA FORM 8110-3 NR 0551, DC8 SRM 51-1-11, 51-1-15, 51-1-20D, 51-1-21, 51-1-22, 51-3-0, 51-3-1, 51-1-3 AN EO 2005085 2L74 4F RT4A25 20051212001502005121200150WP 2005 12 12 IXXA0500126S 120050304A5311 FRAME DOUG DC8 DC871F 302199DWP FS55.00 L-24R CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11821BX858952998 45811 DURING A ROUTINE C CHECK INSPECTION, FOUND RT FUSELAGE FORWARD ACCESSORY COMPARTMENT STRUCTURE FRAME CRACK DAMAGE STA FS 55.00 L-24R. MAJOR REPAIR ACCOMPLISHED REMOVAL OF FASTENERS. REMOVAL OF DAMAGED AREA FRAME SEGMENT. PERFORMED NDT INSPECTION, FABRICATED FRAME SEGMENT AND SPLICE DOUBLER. PERFORMED HEAT TREATMENT. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED FRAME SEGMENT AND SPLICES IAW DC8 SRM 53-2-0 FIG 2 SHEET 1, 6 TR NR 53-110, TR NR 53-125, 53-3-1 FIG 3 SH 2, 2A, 51-1-1, 51-1-4, 51-1-11, 51-1-15, 51-1-20D, 51-3-1, 51-3-2,DPS 3.69-4 REV "AM" R-1, 7.00-1 REV "BK" EO 2005220. 2L74 4F RT4A25 20051212001542005121200154EA 2005 12 12 QXEA200501666 120051031A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 856 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, LEFT SIDE SEAT RAIL AT STATION 856 HAS AREAS OF CORROSION. MAINTENANCE REMOVED CORROSION IAW CRJ-700 REO 670-53-00-013. RESTORED FINISH. 2L72 4F RTA21EA 20051212001642005121200164EA 2005 12 12 SWIA200515939 120051117A5310 VERTICAL BEAM CNDAIRCL600 CL6002B19 1900309EA BS 409 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07411SW 7067 FUSELAGE; VERTICAL BEAM; LOWER I/B + O/B FLANGE IS CRACKED; FS 409.0 + 128; LBL 27.0, ITEM FOUND AT C-CHECK INSPECTION. REPAIR IAW CRJ REO 601R-53-41-056 REV "C" . 2L72 4F RTA21EA 20051212001792005121200179NM 2005 12 12 QXEA200501742 120051204A2897 CONNECTOR DHAV DHC8 DHC8202 2809007NM NR 1 ENGINE UNKNOWN A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09364PH 524 EUG FLIGHT NR 2156, NR 1 FUEL FILTER BYPASS, MASTER CAUTION. MAINTENANCE REPLACED NR 1 ENGINE HP AND LOW PRESSURE FUEL FILTERS IAW DHC8-2-- AMM 73-10-00-000-802 AND 73-10-00-400-802, 73-10-00-000-801 AND 73-10-00-400-801. REPLACED CONNECTOR 7700-P1. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051212001812005121200181CE 2005 12 12 1050921026160 120051020A5313 STRINGER BEECH 1900 1900D 1154162CE BS 163 CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07146ZV UE146 FOUND STRINGER 3R AT FS 163.9 CRACKED. MAINTENANCE FABRICATED AND INSTALLED DOUBLER. 2L72 4T RTA24CE 20051212001832005121200183CE 2005 12 12 105092102666 120051020A5311 FRAME BEECH 1900 1900D 1154162CE BS 150 CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07146ZV UE146 FOUND CRACKED INNERSKIN AND FRAME (ASD) STA 150.6. MAINTENANCE REPAIRED THE PROBLEM. 2L72 4T RTA24CE 20051212001852005121200185EA 2005 12 12 ASOA05896 120051024A5210601R3198055 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27847AS 7335 DURING A HANGAR INSPECTIO IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND TO BE BROKEN. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051212001872005121200187CE 2005 12 12 1051101026 120051001A27201295240051 SPRING BEECH 1900 1900D 1154162CE RUDDER BROKEN A AMWAK NONE O OTHER ININSP/MAINT 1 CE07127ZV UE127 FLIGHT CREW REPORTED THAT WHILE ON THE GROUND WHEN THE CONTROL YOKE WAS LET LOOSE IT WOULD FLOP OVER TO THE RIGHT. MAINTENANCE PERSONNEL FOUND THE AFT AILERON/RUDDER INTERCONNECT SPRING HAD BROKEN NEAR THE HOOK END. MAINTENANCE INSTALLED NEW SPRING. INSPECTED FORWARD SPRING AND NO DEFECTS NOTED. 2L72 4T RTA24CE 20051213000092005121300009NM 2005 12 13 05FDEA04083 120051202A5730 SKIN DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 LEFT HAND WING UPPER TRAILING EDGE PANEL FOUND BULGING AT XORS 1036. REMOVED CORROSION AT LEFT HAND WING UPPER TRAILING EDGE PANEL, XORS 1036 AS PER SRM 51-21-011 VOLUME II. ORIGINAL THICKNESS=0.140, MATERIAL REMOVED 0.100, REMAINING THICKNESS=0.040", FOUND EXCEEDED LIMIT AS PER SRM 57-20-00, FIGURE 16 VOLUME I. REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-90697. 2L73 4F RTA22WE 20051213000242005121300024NM 2005 12 13 USAA051465 120051205A5340653532U14 STRINGER CLIP BOEING737 7374B7 1384702NM STA 727E S4L CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 STA 727E S4L. MAJOR REPAIR, REPLACED TIE CLIP IAW SRM 51-10-02, DEFECT SIZE: .6. 2L72 4F RTA16WE 20051213000332005121300033NM 2005 12 13 USAA051456 120051205A5310 CREASE BEAM BOEING737 7374B7 1384702NM STA 578 TO 601 LCORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 STA 578 TO 601 LEFT CORRODED. MAJOR REPAIR, REMOVED CORROSION AND TREATED AREA IAW SRM 53-60-13, DEFECT SIZE: .250 INCH. 2L72 4F RTA16WE 20051213000412005121300041NM 2005 12 13 SB05160 120051202A335020131A BATTERY PACK BOEING737 7374B7 1384702NM AFT CABIN DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19449US 24893 CLT - MAINTENANCE REPORTED THE EMERGENCY EVACUATION AISLE LIGHTS AT ROWS 14R, 16L, 18R AND 23L INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE M1435 BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20051213000512005121300051NM 2005 12 13 2005UALA01252 120051109A3397 WIRE BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT DISCONNECTED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29118UA 28811 EEL INOP AT SEAT 33B. *S/D* RECONNECT EMERGENCY LIGHT. 2L74 4F4 FRTA20WE E24NE 20051213000632005121300063NM 2005 12 13 2005UALA01343 120051126A5311 FRAME BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU BS 827 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29921UA 25388 FUSELAGE FRAME CRACKED AT FASTENER ATTACH POINT COMMON TO AIR CONDITIONING DISTRIBUTION RAIL ATTACH POINT AT STA 827 JUST BELOW STRINGER 8 LEFT. REMOVED DAMAGE & VERIFIED CRACK CONTAINMENT & INSURANCE CUT BY NDT PER MM53-10-84. FABRICATED AND INSTALLED NESTED REPAIR ANGLES & FILLER PER MM 53-10-84. 2L72 4F4 FRTA16WE E21EU 20051213000662005121300066NM 2005 12 13 2005UALA01346 120051126A5311 FRAME BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU BS 907 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29921UA 25388 FUSELAGE FRAME CRACKED AT FASTENER ATTACH POINT COMMON TO AIR CONDITIONING DISTRIBUTION RAIL ATTACH POINT AT STA 907 JUST BELOW STRINGER 8 LEFT. REMOVED DAMAGE & VERIFIED CRACK CONTAINMENT & INSURANCE CUT BY NDT PER MM53-10-84. FABRICA TED AND INSTALLED NESTED REPAIR ANGLES & FILLER PER MM53-10-84. 2L72 4F4 FRTA16WE E21EU 20051213000772005121300077NM 2005 12 13 2005UALA01357 120051127A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE ROWS 2J, 5E & 49INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29117UA 28810 EMERGENCY LIGHTS AT ROWS 2J, 5E & 49HJK ARE INOP. REPLACED EMERGENCY LIGHT. 2L74 4F4 FRTA20WE E24NE 20051213000832005121300083NM 2005 12 13 2005UALA01363 120051129A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE SEATS 4L, 42R, 4INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP2916UA 26908 EEL INOPERATIVE AT SEATS 4L, 42R, 46L & AT ROW 53L CEILING. REPLACED EEL LAMP. 2L74 4F4 FRTA20WE E24NE 20051213000942005121300094NM 2005 12 13 2005UALA01374 120051129A5730 SKIN BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU LT WING ROOT CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29349UA 24253 LT WING ROOT AREA UPPER SKIN SURFACE CORRODED AT FUSELAGE STA 616 TO 617.5 AT WBL 85.0 TO 87.0. REMOVED CORROSION DAMAGE PER SRM 57-20-01, ROTO PEENED, ALODINED & RESTO RED PAINT PER SRM 51-20-01.THE REPAIR IS APPROVED BY FAA 8100-9 DATED NOV 27TH 2005. 2L72 4F4 FRTA16WE E21EU 20051213001032005121300103NM 2005 12 13 2005UALA01383 120051128A3350 LIGHT BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU ROW 15 INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29942UA 26679 AFT CABIN EEL LIGHTS INOP FROM ROW 15 AFT TO AND INCLUDING EEL STRIP IN FRONT AFT GALLEY CART STOWAGE COMPARTMENT. UPDATE REPLACED EEL STRIP IN FRONT OF CART STOWAGE COMPARTMENT. 2L72 4F4 FRTA16WE E21EU 20051213001112005121300111WP 2005 12 13 IXXA0500150S 120050225A5720 PLATE DOUG DC8 DC871F 302199DWP XRS 74.869 S-5 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11821BX858952998 45811 DURING A ROUTINE C CHECK INSPECTION FOUND RT INNER WING AFT TOP PANEL PLATING CRACK DAMAGED AT STA XRS 74.869, S-5. MAJOR REPAIR ACCOMPLISHED REMOVAL OF FASTENERS AND DAMAGED SECTION. PERFORMED NDT INSPECTION AND FABRICATED EXTERNAL DOUBLER + FILLER PLUG. CLEANED, TREATED AND PRIMED AREA + FILLER PLUG + REPAIR DOUBLER SIDE. APPLIED SEALANT TO FAYING SURFACES AND INSTALLED REPAIR PARTS IAW SEMAN DWG ED-3832 AND FAA FORM 8110-3 NR 05020, DC8 SRM 51-1-11, 51-1-15, 51-1-20D, 51-1-22, 51-1-26, 51-3-1, 51-3-2. 2L74 4F RT4A25 20051213001192005121300119WP 2005 12 13 IXXA0500155S 120050228A5720 PLATE DOUG DC8 DC871F 302199DWP XRS 74.869 S-14 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11821BX859852998 45811 DURING ROUTINE C CHECK INSPECTION, FOUND RT INNER WING FWD TOP PANEL PLATING WITH CRACK DAMAGE AT STA XRS 74.869, S-14. MAJOR REPAIR ACCOMPLISHED REMOVAL OF FASTENERS AND DAMAGED AREA. PERFORMED NDT INSPECTION. FABRICATED REPAIR DOUBLER AND FILLER PLUG. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES AND INSTALLED REPAIRED PARTS IAW ALL APPLICABLE MANUALS, DRAWINGS AND FORMS. 2L74 4F RT4A25 20051213001292005121300129EA 2005 12 13 COMA0560676 120051207A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS WARNING LIGHT A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01967CA 7134 FLIGHT 5456 - RECEIVED A FLAP FAIL CAUTION MESSAGE INBOUND TO LGA, FLIGHT LANDED WITHOUT INCIDENT. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2L72 4F RTA21EA 20051213001352005121300135NE 2005 12 13 SWIA200515969 220051206A7200 ENGINE EMB 120 EMB120 3260201SO PWA PW118 PW118B NE LEFT SEIZED A SWIAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 NM07561SW 120335 LT ENG WILL NOT ROTATE. REPLACED LEFT ENG WITH SERVICABLE UNIT IAW MM 71-00-00, P/N: PW118B S/N OFF: 115664. 2L72 4T4 TRTA31SO E20NE 20051215000052005121500005NM 2005 12 15 CALA0500431 120051208A5315141T5113 FLOORBEAM BOEING767 767224 1385170NM BS 325 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776151 30430 INSPECTION FOUND CABIN FLOORBEAM CORRODED AT BS 325, LBL 55. THE CORRODED SECTION OF FLOORBEAM WAS REPLACED IAW SRM 53-00-51 FIGURE 201, REPAIR 2. 2L72 4F RTA1NM 20051215000112005121500011NM 2005 12 15 CALA0500437 120051212A2910271N64431114 LINE BOEING757 757224 1384958NM HYD SYS CRACKED A CALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW2734131 28971 THE LT HYDRAULIC SYSTEM LOST FLUID QUANTITY AND WAS ACCOMPANIED BY ILLUMINATION OF THE HYD SYS LOW QTY LIGHT AND RESERVOIR LIGHTS DURING CLIMBOUT OF EWR. THE AIRCRAFT WAS RETURNED TO EWR. WHEN THE LANDING GEAR WAS EXTENDED NO GREEN LIGHTS APPEARED. A MANUAL GEAR EXTENSION WAS PERFORMED DURING A GO-AROUND. THE AIRCRAFT LANDED WITHOUT PROBLEM. MAINTENANCE FOUND THE LT WHEEL WELL SOAKED WITH HYDRAULIC FLUID. THE HYDRAULIC LINE FROM THE PRESSURE RELIEF VALVE FOR LT SYS TO ACMP CASE DRAIN FILTER MODULE WAS FOUND CRACKED IN HALF. THE LINE WAS REMOVED AND REPLACED. IN ADDITION, THE LT ACMP WAS REMOVED AND REPLACED. LEAK CHECKS WERE GOOD. 2L72 4F RTA2NM 20051215000262005121500026SO 2005 12 15 RAIA00512007 120051204A3397 WIRE EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DAMAGED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03819HK 145062 PREFLIGHT MID CABIN EMERGENCY EXIT LOCATING SIGN FORWARD SIDE DOES NOT ILLUMINATE. MAINTENANCE REPAIRED THE CONNECTION TO EXIT SIGN AT MID CABIN. 2L72 4T RTT00011AT 20051215000342005121500034EA 2005 12 15 QXEA200501698 120051031A5310 DOOR FRAME CNDAIRCL600 CL6002C10 1390015EA CARGO BAY SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, AFT BAGGAGE DOOR SURROUND HAS SCRATCHES ON FORWARD EDGE WL 85 FS 1001. REPAIRED DAMAGED AREA IAW REO 670-53-61-196. RESTORED FINISH AND PERFORMED PRESSURE CHECK. ALL CHECKS GOOD. 2L72 4F RTA21EA 20051215000412005121500041EA 2005 12 15 QXEA200501700 120051031A5310 WINDOW FRAME CNDAIRCL600 CL6002C10 1390015EA COCKPIT DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHCEK, CO-PILOT SIDE WINDSHIELD FRAME POST STRAP SPLICE HAS SCRATCHES ON LOWER OUTER SURFACE. BLENDED DAMAGE IAW EA R-53-391 AND REO 670-56-11-005. 2L72 4F RTA21EA 20051215000442005121500044EA 2005 12 15 QXEA200501689 120051031A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 397-453 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, LEFT OUTBOARD SEAT RAIL HAS SCRATCHES NICKS AND CHAFING AT STATION 397-453. REPAIRED IAW REO 670-53-00-013. 2L72 4F RTA21EA 20051215000562005121500056EA 2005 12 15 QXEA200501670 120051031A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 394-485 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, LEFT ONBOARD SEAT RAIL AT STATION 394-485 HAS CORROSION AND GOUGES. MAINTENANCE BLENDED OUT DAMAGE AND CORROSION IAW REO 670-53-00-013. 2L72 4F RTA21EA 20051215000612005121500061EA 2005 12 15 QXEA200501687 120051031A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 504-568 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, LEFT OUTBOARD SEAT RAIL HAS SCRATCHES AND NICKS AT STATION 504-568. REPAIRED IAW REO 670-53-00-013. 2L72 4F RTA21EA 20051215000752005121500075EA 2005 12 15 QXEA200501685 120051031A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 581-615 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, LEFT OUTBOARD SEAT RAIL HAS CORROSION AT STATION 581-615. REPAIRED IAW REO 670-53-00-013. 2L72 4F RTA21EA 20051215000842005121500084NM 2005 12 15 QXEA200501758 120051125A5753 FLAP TRACK DHAV DHC8 DHC8202 2809007NM LT WING CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX - LEFT HAND NR 5 FLAP TRACK HAS PITTING CORROSION ON OUTBOARD CENTER OF TRACK. REPAIRED IAW RD 8-57-989. 2H72 4T RTA13NM 20051215000872005121500087NM 2005 12 15 QXEA200501761 120051119A5246 STIFFENER DHAV DHC8 DHC8202 2809007NM OIL DOOR CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX - OIL SERVICE DOOR ON PANEL 413AL HAS A CRACKED STIFFENER 10 INCHES FROM TOP AND 3.5 INCHES FROM FRONT EDGE. REPAIRED IAW RD 8-71-213. 2H72 4T RTA13NM 20051215000932005121500093NM 2005 12 15 SCNA05016 120051207A3350D71702001 BATTERY PACK BOEING737 7378Q8 13844BXNM EMERGENCY LIGHT INOPERATIVE A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15809SY3268 30683 DURING ROUTINE MX DISCOVERED EMERGENCY LIGHTS INOP 14DEF THRU 23DEF. TROUBLESHOT AND FOUND FAULTY POWER SUPPLY CHARGER AT SEAT 18DEF. REMOVED AND REPLACED BATTERY CHARGER, OPS CHECKED GOOD. 2L72 4F RTA16WE 20051215000942005121500094NM 2005 12 15 SCNA05015 120051207A3350D71702001 BATTERY PACK BOEING737 7378Q8 13844BXNM EMERGENCY LIGHTSINOPERATIVE A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15809SY3268 30683 DURING ROUTINE MX DISCOVERED SEVERAL EMERGENCY LIGHTS INOP. TROUBLESHOT TO FIND BAD POWER SUPPLY UNIT AT 11A. REMOVED AND REPLACED BATTERY CHARGER PER 31-51-06-960-806. 2L72 4F RTA16WE 20051215000962005121500096NM 2005 12 15 DL73S050752 120051128A5315654541039 FLOORBEAM BOEING737 737247 138448DNM RBL 24.8 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27237WA 23185 CRACKS WERE FOUND IN THE RBL 24.8 FLOORBEAM. REINFORCED CHORD AND WEB WITH ANGLES, CHANNELS, AND DOUBLERS REF AD 2001-17-18, 93-17-08, 90-06-02 AND 03-056673-03AD. 2L72 4F A16WE 20051215000992005121500099NM 2005 12 15 DL73S050755 120051202A212165772 GASPER FAN BOEING737 737232 1384475NM CABIN WORN A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27306DL 23078 CLEANING CREW REPORTS SMOKE IN CBN. UPON INVESTIGATING, FOUND GASPER FAN C/B POPPED RESET TO VERIFY PROBLEM, FAN MAKING NOISE, P/N 214001047 - REPLACED FAN. 2L72 4F RTA16WE 20051215001072005121500107EA 2005 12 15 COMA0560706 120051206A2752852D10019 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA RT TE FLAP FAULTY A COMAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 SO01969CA23983 7141 FLIGHT 5675 - DURING CLIMB-OUT OF CVG RECEIVED A FLAP FAIL CAUTION MESSAGE. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE RIGHT INBD FLAP OUTBD ACTUATOR. 2L72 4F RTA21EA 20051215001142005121500114NM 2005 12 15 AWXA200501515 120051117A53206546812187 FLOOR SUPPORT BOEING737 73733A 1384673NM BS 1011-1015 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 MCN - DURING C19 CHECK DISCOVERED LEVEL 2 GALVANIC CORROSION FOUND ON FLOOR SUPPORT LOCATED FROM BS 1011 TO BS 1015, WL 208, AND BL 7L. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-51-1A-1 FIG 101. MAINTENANCE REMOVED AND INSTALLED NEW FLOOR SUPPORT FROM BS 1011 TO BS 1015, WL 208 AND BL 7L IAW BOEING 737-300 SRM 51-40-02-0G FIG 12. 2L72 4F RTA16WE 20051215001162005121500116NM 2005 12 15 AWXA200501517 120051118A5311654583392 FRAME BOEING737 73733A 1384673NM 178 BULKHEAD CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 MCN - DURING C19 CHECK DISCOVERED ANGLE CRACKED, 1.5 INCHES IN LENGTH, AT BS 178, WL 207 AND BL 29R. MAINTENANCE CUT OUT DAMAGED SECTION OF CHORD AT BS 178, WL 207 AND BL 29R IAW AMERICA WEST AIRLINES (AWA) ENGINEERING REPAIR (ER) NR 03-5300-05341-ES1. FABRICATED CLIP, FILLERS, STRAPS AND WEB IAW AWA ER NO 03-5300-05341-ES1. INSTALLED FABRICATED REPAIR PARTS AT BS 178, WL 207 AND BL 29R IAW AWA ER NO 03-5300-05341-ES1. 2L72 4F RTA16WE 20051215001172005121500117NM 2005 12 15 AWXA200501518 120051116A5311651630153 FRAME BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 MCN - DURING C19 CHECK DISCOVERED FRAME CRACKED, 2.2 INCHES IN LENGTH, AT BS 188, WL 200 AND BL 31R. MAINTENANCE CUT OUT DAMAGED SECTION OF FRAME FLANGE AND CHORD AT BS 188, WL 200 AND BL 31R IAW AMERICA WEST AIRLINES (AWA) ENGINEERING REPAIR (ER) NR 03-5300-05333-HF1. FABRICATED ANGLE AND FILLERS IAW BOEING 737-300 SRM 51-00-07-2R11 AND AWA ER NR 03-5300-05333-HF1. INSTALLED FABRICATED REPAIR PARTS AT BS 188, WL 200 AND BL 31R IAW AWA ER NR 03-5300-05333-HF1. 2L72 4F RTA16WE 20051215001182005121500118SO 2005 12 15 SWIA200515988 120051208A2752 ACTUATOR EMB 120 EMB120ER 3260203SO NACELLE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07299SW 120329 FLAP LIGHT AND ADVANCE STALL WARN LIGHT ON MAP ASYMMETRY, CONTROL FAULT AND DISAGREEMENT LIGHTS CAME ON IN CRUISE. REPLACED FLAP ANNUNCIATOR ASSY AND RIGHT NACELLE FLAP ACTUATOR IAW EMB MM 27-50-05 AND 27-50-03. OPERATIONAL CHECK GOOD, PN OFF 306900-10176; SN OFF 0076 PN 343100-1001; SN OFF 0167. 2L72 4T RTA31SO 20051215001192005121500119EA 2005 12 15 SWIA200515989 120051205A2720 TRANSMITTER CNDAIRCL600 CL6002B19 1900309EA RUDDER POSITION MALFUNCTIONED A SWIAO OTHER FO FLT CONT AFFECTED OTHER NRNOT REPORTED 1 NM07960SW 7853 RUDDER FAILS TO INDICATE FULL TRAVEL TO THE LEFT (INDICATES FULL TRAVEL TO THE RIGHT). REPLACED RUDDER POSITION TRANSMITTER IAW 27-24-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051215001202005121500120EA 2005 12 15 SWIA200515990 120051206A2751601R590141 DETECTOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07980SW 7955 FLAP 1/2 SPEED STATUS MESSAGE. REPLACED SKEW DETECTOR IAW 27-51-15. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051215001212005121500121SO 2005 12 15 SWIA200515991 120051206A3350 LAMP EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07583SW 120351 ONE RED FLOOR LEVEL EMERGENCY EXIT LIGHT INOP. RELAMPED FLOOR LEVEL RED EMERGENCY LIGHT, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20051215001222005121500122SO 2005 12 15 SWIA200515992 120051205A3397 WIRE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT LOOSE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07227SW 120304 FIRST EMERGENCY ROW FLOOR LIGHT INOP. RECONNECTED GROUND WIRE AT 1ST LIGHT ON FLOOR STRIP. OPERATIONAL CHECK OK. 2L72 4T RTA31SO 20051215001262005121500126NM 2005 12 15 2005UALA01407 120051205A5241 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE GALLEY DOOR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29921UA 25388 FWD GALLEY DOOR AFT LOWER FRAME CRACKED OUT OF FASTENER HOLE. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACP'D PER BACO DRAWING 69-69854, FRAME SPLICE REPAIR. 2L72 4F4 FRTA16WE E2GL 20051215001272005121500127NM 2005 12 15 2005UALA01408 120051205A5241 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE GALLEY DOOR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29921UA 25388 FWD GALLEY DOOR FWD LOWER FRAME CRACKED AT FASTENER HOLE. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACP'D PER BACO DRAWING 69-69430, NEW FRAME SECTION SPLICE REPAIR. 2L72 4F4 FRTA16WE E2GL 20051215001332005121500133NM 2005 12 15 2005UALA01414 120051207A5412 FITTING BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE BULKHEAD DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29793UA 26946 NR 1 ENGINE AFT SAILTAIL COMPT LWR BKHD FITTING FAIL CONDUCTIVE TEST. NR 1 ENGINE AFT SAILTAIL COMPT LWR BKHD FITTING FAILED CONDUCTIVE TEST BECAUSE OF HEAT DAMAGE. MAJOR REPAIR WAS ACCOMPLISHED PER EVA UA-EVA-50816B. 2L72 4F4 FRTT0001SE E46NE 20051215001352005121500135EA 2005 12 15 SWIA200515995 120051209A2760 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED DEDESCENT 1 NM07413SW 7102 DURING DESCENT, RIGHT SPOILER WOULD NOT FULLY DISPLAY CAUSING A ROLL TO THE LEFT. REPLACED RT FLIGHT SPOILERON OUTBOARD PCU IAW CRJ MM 27-62-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051215001392005121500139NM 2005 12 15 2005UALA01420 120051208A5311 FRAME BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE BS 654, LBL4 CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29644UA 25094 FRAME TOP CAP CORRODED AT BS 654+121, LBL42, FWD CARGO PIT. MAJOR REPAIR TO FRAME TOP CAP PER SRM AS PERMANENT REPAIR. 2L72 4F4 FRTA1NM E24NE 20051215001422005121500142NM 2005 12 15 2005UALA01423 120051208A5410 BUSHING BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE NR 2 PYLON MIGRATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29644UA 25094 NR 2 PYLON DIAGONAL BRACE FITTING FWD-STRUT ATTACH, INBD SIDE BUSHING IS MIGRATED. NR 2 PYLON DIAGONAL BRACE FITTING FWD-STRUT ATTACH, INBD SIDE BUSHING WAS MIGRATED. BUSHING MIGRATION CAUSE IS UNKNOWN. THE BUSHING WERE REPLACED PER SRM 54-53-90. 2L72 4F4 FRTA1NM E24NE 20051215001432005121500143 2005 12 15 2005UALA01424 420051208A3100 UNKNOWN AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE UNKNOWN UNKNOWN A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29434UA 592 DIVERTED DUE TO NUMEROUS FAULT LIGHTS. SYSTEM TESTS OF FLIGHT WARNING COMPUTERS, RADIO ALTIMETERS AND ENHANCED GROUND PROXIMITY WARNING COMPUTER. RADIO ALTIMETER ANTENNA CHECKED. ENHANCED GROUND PROXIMITY WARNING COMPUTER REPLACED. SYSTEM OPERATION NORMAL TO DATE. THE ENHANCED GROUND PROXIMITY WARNING COMPUTER WAS SHOP TESTED AND HAD TWO VOICE FAILURES. INTERNAL CABLES WERE RESEATED AND UNIT PASSED TEST. 2L72 4F4 FRTA28NM E40NE 20051215001442005121500144NM 2005 12 15 2005UALA01425 120051208A3397 WIRE AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE EMERGENCY EXIT MISINSTALLED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29855UA 1737 RIGHT AFT DOOR OVER THE DOOR EMERGENCY LIGHT INOP, EXIT SIGN WORKS NORMAL. FOUND LIGHT MISWIRED. ADJ WIRE CONNECTION OPS CHECK GOOD. 2L72 4F4 FRTA28NM E40NE 20051215001452005121500145NM 2005 12 15 2005UALA01426 120051203A3350 LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE LT OVERWING INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29521UA 24891 EXTERIOR EEL LIGHT LT OVERWING AFT IS INOP. RELAMPED 2L72 4F4 FRTA2NM E17NE 20051215001472005121500147NM 2005 12 15 2005UALA01428 120051202A5754114N300323 WEDGE BOEING BOEING757 757222 1384956NM PWA 2037 PW2037 NE SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29542UA A20374 25276 T/E WEDGE DELAMINATED NR 5 SLAT. REPAIRED WEDGE IN SHOP 273 AUTOCLAVE PER SRM 50-57-56-01 ON R66 864. 2L72 4F4 FRTA2NM E17NE 20051215001492005121500149NM 2005 12 15 2005UALA01430 120051209A5330 SKIN BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE FUSELAGE GOUGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29666UA 29238 FUSELAGE DENTED AND GOUGED FWD OF AFT CARGO PIT CONTROL PANEL DOOR. FUSELAGE SKIN REPAIRED PER SRM. SUPPLEMENTAL INSPECTIONS REQUIRED BY 37,500 CYCLES ARE MONITORED BY AMIS CF9010. 2L72 4F4 FRTA1NM E24NE 20051215001512005121500151EU 2005 12 15 2005UALA01432 120051210A2120 SMOKE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE COCKPIT DETECTED A UALAA UNSCHED LANDING EB VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP29425UA 508 LOUD VIBRATION HEARD FOLLOWED BY SMOKE SMELL IN THE COCKPIT. BLOWER SWITCH DIDN'T GO INTO OVERRIDE ON AVIONICS VENT. ALSO HAD ECAM AMBER INDICATIONS ON PRESS PAGE FOR INLET AND EXTRACT VALVES. SMOKE REPORTED IN FLIGHT DECK AFTERWARDS. SYSTEM DIDN'T GO INTO PROPER 'SMOKE' CONFIGURATION. 2L72 4F4 FRTA28NM E40NE 20051215001542005121500154NM 2005 12 15 2005UALA01435 120051212A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29120UA 29166 DOOR 5 LEFT EMERGENCY LIGHT AT FED SILL INOP. REPLACED LAMP. 2L74 4F4 FRTA20WE E24NE 20051215001552005121500155NM 2005 12 15 2005UALA01436 120051212A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29120UA 29166 EMERGENCY EEL LIGHT INOP AT SEATS 7GH AND 4A. REPLACED LIGHT ASSY. 2L74 4F4 FRTA20WE E24NE 20051215001562005121500156NM 2005 12 15 2005UALA01437 120051211A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29121UA 29167 SEAT 2J AFT EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY. 2L74 4F4 FRTA20WE E24NE 20051215001572005121500157NM 2005 12 15 2005UALA01438 120051211A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE R1 DOOR INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29121UA 29167 FOUND DOOR 1R EMERGNECY CEILING LIGHT INOP. REPLACED LAMP. 2L74 4F4 FRTA20WE E24NE 20051215001622005121500162NM 2005 12 15 2005UALA01443 120051209A3097 WIRE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE LT PITOT HEAT ARCED A UALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 WP29308UA 23669 CAPT UPPER LT PITOT HEAT CB AT P13-3 C1 INSIDE WIRE ARCED TO GROUND WHEN OPENING PANEL FOR INSPECTION. WIRES BURNT THRU AND SEPERATED AT P18-3 C1 CIRCUIT BREAKER DUE TO WIRE W18-217 BEING ROUTED INCORRECTLY AND CHAFING THRU PROTECTIVE COVER OVER TIME ON THE CIRCUIT BREAKER PANEL FRAME EDGE. WIRE WAS REPAIRED PER GNMM 2-0-21-001 AND AIRCRAFT WAS RETURNED TO SERVICE. DAMAGE WAS STRICTLY DUE TO IMPROPER ROUTING/CHAFE PROTECTION OF WIRE W18-217 TO ADJACENT STRUCTURE. 3 OTHER UAL 737 AIRCRAFT WERE INSPECTED AND FOUND TO HAVE WIRE W18-217 ROUTED CORRECTLY WITH ONE (N925UA) HAVING MINOR CHAFING REQUIRING ANTI-CHAFING SLEEVE INSTALLATION. NOTE THAT LOCATION IS AT P18 PANEL NOT P13 AS SHOWN IN 'DEFECT & CORRECTI2L72 4F4 FRTA16WE E2GL 20051215001632005121500163NM 2005 12 15 SB05165 120051212A335020131A BATTERY PACK BOEING737 7373B7 1384580NM EMERGENCY LIGHTSDISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19522AU 23857 BDL - SEVERAL CABIN EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE LEFT EMERGENCY LIGHT BATTERY PACK. OPERATIONALLY CHECKS OK. 2L72 4F RTA16WE 20051215001662005121500166SO 2005 12 15 SWIA200515976 120050915A5347 SEAT TRACK EMB 120 EMB120ER 3260203SO CABIN CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07579SW 120347 LT AFT SEAT TRACK CORRODED FROM GALLEY TO SEAT 10A, ITEM FOUND AT C-CHECK INSPECTION. REMOVED AND INSTALLED SERVICEABLE LT AFT SEAT TRACK FROM GALLEY TO SEAT 10A. 2L72 4T RTA31SO 20051215001672005121500167SO 2005 12 15 SWIA200515977 120050915A5311 FRAME EMB 120 EMB120ER 3260203SO COCKPIT FLOOR CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07579SW 120347 PILOT'S FLOOR PROP CRACKED AT FRAME 13, ITEM FOUND AT C-CHECK INSPECTION. SPLICED IN REPLACEMENT SECTION OF FRAME NR 13 FLOOR SUPPORT COLUMN (PILOT'S SIDE) PER EMB120 SRM 53-10-10 PG 214-220. 2L72 4T RTA31SO 20051215001702005121500170NM 2005 12 15 USAA051473 120051208A5315 FLOORBEAM BOEING737 737301 1384611NM STA 986.5 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19591US 23936 FOUND CORROSION STA 986.5 BELOW TO BL45. REMOVED DAMAGED FABRICATED NEW T CAP AND INSTALLED ON FLOORBEAM IAW 53-10-05, DEFECT SIZE: .5 INCH AREAS OF CORROSION AROUND CLIP NUT HOLES 38 INCHES IN LENGTH. 2L72 4F RTA16WE 20051215001742005121500174NM 2005 12 15 USAA051478 120051208A53201137215 INTERCOSTAL BOEING737 7374B7 1384702NM BS 312-328 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 FOUND INTERCOSTAL CORRODED AT STA 312-328, RBL 12. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-10-02, DEFECT SIZE: .50" AREAS OF CORROSION AT EACH FASTENER HOLE. 2L72 4F RTA16WE 20051215001762005121500176NM 2005 12 15 USAA051476 120051208A5311 FRAME BOEING737 7374B7 1384702NM BS 727D CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 FOUND FRAME CRACKED BS 727D. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER IAW TR 53-10-20C, DEFECT SIZE: FUSELAGE FRAME CRACKED AT LT PSU RAIL ATTACH BRACKET, CRACK MEASURES .65 INCHES. 2L72 4F RTA16WE 20051215001792005121500179NM 2005 12 15 USAA051485 120051209A53401138858 ATTACH ANGLE BOEING737 7374B7 1384702NM RT PYLON CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 FOUND CRACK RT PYLON UPPER IB AFT AREA, NAC STA 314.24. REMOVED AND REPLACED ATTACH ANGLE IAW SRM 51040-02, DEFECT SIZE: .250" CRACK. 2L72 4F RTA16WE 20051215001802005121500180 2005 12 15 2005UALA01232 420051105A340010604501 RELAY BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FAILED A UALAA UNSCHED LANDING O OTHER NRNOT REPORTED 1 WP29326UA 23958 BOTH IRS ON DC LIGHTS ILLUM JUST AFTER LIFTOFF. SUA IRS POWER FAULT HAS NOT REOCCURRED. 2L72 4F4 FRTA16WE E2GL 20051215001822005121500182NM 2005 12 15 USAA051487 120051209A5311 FRAME BOEING737 7374B7 1384702NM BS 747 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 FOUND FRAME BS 747 BETWEEN S8-S9R AT PSU ATTACH BRACKET. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLERS IAW TR 53-10-2C, DEFECT SIZE: 1" CRACK. 2L72 4F RTA16WE 20051215001832005121500183NM 2005 12 15 USAA051488 120051209A5311 FRAME BOEING737 7374B7 1384702NM STA 787, S 9L CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 FOUND FRAME CRACKED STA 787, S 9L. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLERS IAW TR 53-10-2C, DEFECT SIZE: 1" CRACK. 2L72 4F RTA16WE 20051215001862005121500186NM 2005 12 15 USAA051493 120051212A531365516989 SPLICE BOEING737 7374B7 1384702NM BS908 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 FOUND CRACK BS908 AT STRINGER 4. DEFECTIVE PART REPLACED WITH IDENTICAL PART IAW SRM 51-10-02, DEFECT SIZE: .500". 2L72 4F RTA16WE 20051215001882005121500188NM 2005 12 15 USAA051500 120051212A5311 FRAME BOEING737 7374B7 1384702NM STA 480 S9R CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 FOUND CRACK STA 480 S9R. REMOVED DAMAGE, INSTALLED TWO REPAIR ANGLES IAW 53-10-20C, DEFECT SIZE: 1.000". 2L72 4F RTA16WE 20051215001912005121500191NM 2005 12 15 USAA051507 120051212A575365464301221R WEDGE BOEING737 737301 1384611NM FOREFLAP DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19591US 23936 FOUND DELAMINATION INBOARD FOREFLAP TOP SKIN INBOARD END. REMOVED DAMAGE, FABRICATED AND INSTALLED DOUBLER IAW SRM 51-70-10, DEFECT SIZE: 3.5. 2L72 4F RTA16WE 20051219000012005121900001 2005 12 19 QXEA200501776 420051212A3460 COMPUTER DHAV DHC8 DHC8202 2809007NM AFCS MALFUNCTIONED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM09354PH 498 PDX FLIGHT NR 2227, WHILE BOARDING, POWER DROPPED OFF AIRCRAFT. THEN RESET, NOTICED AN ELECTRICAL SMELL AND THE AUDIO ALERT C/B WAS POPPED AND THE NAV SWITCH AND ANN 1 C/B WAS POPPED. ALT ALERTER DISPLAY IS DARK. MX FOUND TWO COMPONENTS WITH SIGNS OF OVERHEAT AFCS INTERFACE AND ALT ALERTER AURAL WARNING PANEL. INSTALLED SERVICEABLE ALT ALERT AURAL PLANNING PANEL. OPS TEST GOOD IAW DASH 8 200 MM TASK 34-11-41-710-801. INSTALLED NEW AFCS INTERFACE UNIT. PERFORMED OPS TEST OF AFCE UNIT IAW MTC 9340045. PERFORMED OPS TEST OF FLT MANAGEMENT COMPUTERS IAW MTC 9340040. PERFORMED HGS OPS TEST IAW MTC 9340002. ALL OPERATIONAL CHECKS GOOD. A/C RETURNED TO SERVICE. 2H72 4T RTA13NM 20051219000032005121900003NM 2005 12 19 QXEA200501775 120051212A2160 WARNING LIGHT DHAV DHC8 DHC8202 2809007NM ENVIRON CONTROLSILLUMINATED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09367PH 511 SEA FLIGHT NR 2115 - CABIN DUCT HOT AND FLIGHT COMPARTMENT CAUTION LIGHTS ILLUMINATED. PERFORMED APPROPRIATE CHECKLIST. DUCT CAUTION LIGHTS EXTINGUISHED. DUCT TEMP REMAINS AT 40 DEGREES. MAINTENANCE COMPLIED WITH FUNCTIONAL CHECK OF THE TEMP CONTROL SYSTEM IAW DHC-8-200 AMM TASK 21-90-00-720-801. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051219000052005121900005NM 2005 12 19 QXEA200501778 120051212A5230 HANDLE BOMBDRDHC8 DHC8402 1390042NM CARGO DOOR UNSECURE A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09414QX 4061 FCA FLIGHT NR 2396, FUSELAGE DOOR WARNING LIGHT ILLUMINATED DURING CLIMB. RAN CHECKLIST. MFD SHOWED AFT BAGGAGE DOOR OPEN. RETURNED TO FIELD. DID NOT DECLARE EMERGENCY. MAINTENANCE INSPECTED CARGO DOOR HANDLE. FOUND LATCH NOT SECURED. INSPECTED HANDLE LATCH AND NO DISCREPANCIES NOTED. PERFORMED OPERATIONAL TEST IAW AMM TASK 52-31-00-710-801. OPS CHECKED GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051219000072005121900007WP 2005 12 19 ABXA050357 120051213A2170 COALESCER BAG DOUG DC9 DC941 302207NWP A/C PACKS UNKNOWN A ABXAB EMER. DESCENT J WARNING INDICATION DEDESCENT 1 GL23964AX 47781 EN ROUTE RIGHT AC PACK MAINTAINED 13 PSI, AC PRESSURIZATION CONTROLLER WENT TO STBY/LOCKOUT AT TOP OF DESCENT, CABIN PRESSURE CONTROLLER FAILED, PERFORMED EMERGENCY DESCENT. PERFORMED BITE CHECK ON BOTH CABIN PRESSURE CONTROLLERS. NO FAULTS FOUND. SWAPPED NR 1 CONTROLLER WITH NR 2 FOR TROUBLESHOOTING. REPLACED BOTH LEFT AND RIGHT WATER SEPARATOR COALESCER BAGS. PRESSURIZED BOTH PACKS. NO LEAKS NOTED. SYSTEM OPS CHECKED OK IAW DC9 AMM 21.00.00.5. MANUAL OPERATION OF OUTFLOW VALVE CHECKED OK. 2L72 4F A6WE 20051219000082005121900008NM 2005 12 19 05FDEA04202 120051209A5330 REPAIR BOEING727 727233 138408ANM ZONE 100 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25220FE 20934 FOUND REPAIR LOCATED AT FUSELAGE RIGHT SIDE STA 1174-1203 STR19-20. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. COMPLIED WITH FED EX EA 7-5330-92597 PART 1, FUSELAGE SKIN, REWORK OF EXISTING REPAIR. MAJOR REPAIR TIMCO MECH NR 1985 QC 227. 2L73 4F RTA3WE 20051219000122005121900012NM 2005 12 19 05FDEA04225 120051212A5753 HINGE DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 LEFT HAND WING INBOARD TRAILING EDGE FLAP OUTBOARD HINGE (FLAP SIDE) AT PIVOT BORE HOLE OUTBOARD SIDE FOUND CORROSION. CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-94560. 2L73 4F RTA22WE 20051219000152005121900015NM 2005 12 19 05FDEA04228 120051212A5753 MOUNT DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 FOUND LEFT WING, WITH REFERENCE TO EO 1-5750-7-5002, OUTBOARD FLAP INBOARD FORWARD HINGE ACTUATOR INBOARD LUG BORE CORRODED. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-94564. 2L73 4F RTA22WE 20051219000162005121900016NM 2005 12 19 05FDEA04229 120051212A5753 MOUNT DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 FOUND LEFT WING, WITH REFERENCE TO EO 1-5750-7-5002, OUTBOARD FLAP INBOARD FORWARD HINGE ACTUATOR OUTBOARD LUG BORE CORROSION. REMOVED AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-94564. 2L73 4F RTA22WE 20051219000182005121900018NM 2005 12 19 05FDEA04231 120051212A5753 MOUNT DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 FOUND LEFT WING, WITH REFERENCE TO EO 1-5750-7-5002, OUTBOARD FLAP OUTBOARD FORWARD HINGE ACTUATOR INBOARD LUG BORE CORRODED. REMOVED AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-94563. 2L73 4F RTA22WE 20051219000192005121900019NM 2005 12 19 05FDEA04232 120051212A5753 MOUNT DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 FOUND LEFT WING, WITH REFERENCE TO EO 1-5750-7-5002, OUTBOARD FLAP OUTBOARD FORWARD HINGE ACTUATOR OUTBOARD LUG BORE CORRODED. 2L73 4F RTA22WE 20051219000202005121900020NM 2005 12 19 05FDEA04233 120051212A5753 MOUNT DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 RIGHT WING, WITH REFERENCE TO EO 1-5750-7-5002, OUTBOARD FLAP OUTBOARD HINGE ACTUATOR OUTBOARD LUG BORE CORRODED. CORROSION REMOVED AND REPAIR CARRIED OUT AS PER FEDEX EA 15750-94562. 2L73 4F RTA22WE 20051219000222005121900022NM 2005 12 19 05FDEA04235 120051212A5753 BUSHING DOUG MD11 MD11 3023602NM ZONE 600 MIGRATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 RIGHT HAND WING, WITH REFERENCE TO EO 1-5750-7-5002, OUTBOARD FLAP OUTBOARD HINGE UPPER INBOARD MOUNT BUSHING MIGRATED. CORROSION REMOVED AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-94562. 2L73 4F RTA22WE 20051219000232005121900023NM 2005 12 19 05FDEA04236 120051212A5753 BUSHING DOUG MD11 MD11 3023602NM ZONE 600 MIGRATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 FOUND RIGHT WING, WITH REFERENCE TO EO 1-5750-7-5002, OUTBOARD FLAP OUTBOARD HINGE UPPER OUTBOARD MOUNT BUSHING MIGRATED. 2L73 4F RTA22WE 20051219000242005121900024NM 2005 12 19 05FDEA04237 120051212A5753 MOUNT DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 FOUND RIGHT WING, REFWERENCE TO EO 1-5750-7-5002, OUTBOARD FLAP OUTBOARD HINGE SIDE LOAD FITTING ATTACHMENT LOWER MOUNT BORE CORRODED. REPAIRED AS PER FEDEX EA 1-5750-94562. 2L73 4F RTA22WE 20051219000252005121900025WP 2005 12 19 05FDEA04238 120051212A5310 REPAIR DOUG DC10 DC1010 3022110WP DOOR FRAME UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25568FE 47827 DURING AIRPLANE'S P TO F MODIFICATION FOUND AT STA 1305-1316 STR 25-27 LT SIDE, EXISTING REPAIR ON JAMB DOOR. PERFORMED HFEC INSPECTION, REMOVED EXISTING REPAIR DOUBLER AND INSTALLED A NEW ONE IAW SRM 53-50-00 FIG 19, SH 2. 2L73 4F A22WE 20051219000272005121900027WP 2005 12 19 05FDEA04240 120051212A5310 DOOR FRAME DOUG DC10 DC1010 3022110WP FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25568FE 47827 DURING AIRPLANE'S P TO F MODIFICATION FOUND INTERNAL FUSELAGE: CRACK .300" LONG ON WEB OF JAMB DOOR, STA 1256, L16 RT. PERFORMED STOP DRILL CRACK AND NDI. INSTALLED REPAIR DOUBLER IAW SRM 53-50-00 FIG 19, VOL I. 2L73 4F A22WE 20051219000282005121900028NM 2005 12 19 05FDEA04209 120051209A5315 FLOORBEAM BOEING727 727227 1384078NM BS 1130 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 FOUND FLOORBEAM UPPER CHORD CORRODED, BS 1130 , RBL 50, WL 208. REPAIRED FLOORBEAM UPPER CHORD PER FEDEX EA 7-5310-96828A. 2L73 4F A3WE 20051219000302005121900030EA 2005 12 19 SWIA200515979 120051210A335020131A POWER SUPPLY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSINOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07919SW2275 2275 1 CEILING LEVEL EMERGENCY FLOOD LIGHT INOPERATIVE. REPLACED NR 3 ELBP IAW 33-51-04. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051219000332005121900033EA 2005 12 19 SWIA200515982 120051210A2130 PRESSURE SYSTEM CNDAIRCL600 CL6002C10 1390015EA CABIN PRESSURE MALFUNCTIONED A SWIAG O2 MASK DEPLOYED GJ MULTIPLE FAILURE WARNING INDICATION NRNOT REPORTED 1 NM07750SK 10207 AFTER CLOSING MAIN CABIN DOOR CPAM C ALT SPIKED TO 15,000 FEET, MASTER WARNING CABIN PRESS AND AURAL "CABIN PRESSURE" FOLLOWED BY MASTER CAUTION PASS OXY ON AND OXYGEN MASKS DEPLOYED. PERFORMED PAX OXYGEN MASK RE-PACK IN REF W/ AMM 35-20. OPERATIONAL CHECK GOOD OF CPC 1 AND 2 SYS IN REF W/ AMM 35-22. 2L72 4F RTA21EA 20051219000342005121900034EA 2005 12 19 SWIA200515983 120051208A2750860D10018 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07417SW 7400 ON SETTING FLAPS TO 8 DEG, FLAPS HALFSPEED STATUS MSG. INSTALLED A SERVICEABLE FECU IAW MM 27-51-05. OPERATIONAL CHECK GOOD. PN ON 860D100-18ABCD OFF 725 2L72 4F RTA21EA 20051219000352005121900035SO 2005 12 19 SWIA200515984 120051202A5210 RIB EMB 120 EMB120ER 3260203SO PAX DOOR CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07289YV 120289 FWD PAX DOOR ADJUSTER ATTACH RIB IS CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FUSELAGE FORMED FRAME IAW 53-00-04 PG 201-203 AT FRAME 14 FS 4410.5. 2L72 4T RTA31SO 20051219000362005121900036SO 2005 12 19 SWIA200515985 120051202A5210 RIB EMB 120 EMB120ER 3260203SO PAX DOOR CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07289YV 120289 AFT PAX DOOR ACTUATOR ATTACH RIB IS CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FORMED FRAME IAW 5-00-04 PG. 201-203 AT FRAME 15 FS 4825.5. 2L72 4T RTA31SO 20051219000382005121900038SO 2005 12 19 SWIA200515987 120051207A3350 LAMP EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07561SW 120335 FLOOR LEVEL EMERGENCY LIGHT AT SEAT 3A INOP. REPLACED EMERGENCY LIGHT LAMP ASSY AT SEAT 3A. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20051219000392005121900039NM 2005 12 19 SWAA053961 120051214A5311963820 FRAME BOEING737 7373H4 1384600NM BS 178 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29645SW 28330 DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BLKHD SIDE CHORDS CRACKED AT WL 207. REMOVED AND REPLACED SIDE CHORDS PER SRM AND SWA ACO. 2L72 4F RTA16WE 20051219000402005121900040NM 2005 12 19 SWAA053962 120051214A53116547959 FRAME BOEING737 7373H4 1384600NM AFT CARGO CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29645SW 28330 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT AFT CARGO DOOR CUTOUT, FWD FRAME NR 5 STOP FITTING. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20051219000412005121900041NM 2005 12 19 SWAA053963 120051214A53116520722 FRAME BOEING737 7373G7 1384595NM FWD CARGO CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29683SW 24008 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, FWD FRAME NR 5 STOP FITTING. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20051219000422005121900042NM 2005 12 19 SWAA053964 120051214A53306545774 SKIN BOEING737 7373Q8 1384670NM BS 730B-733B CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 730B TO BS 733B, STR 10L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051219000452005121900045NM 2005 12 19 SWAA053967 120051213A335065C34691 LIGHT BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29707SA 27841 DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 19 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20051219000462005121900046NM 2005 12 19 SWAA053968 120051213A3350MS155721 BULB BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29753SW 29848 DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 13 ABC. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20051219000472005121900047NM 2005 12 19 SWAA053969 120051213A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29769SW 30588 EEPLS STRIP COVER LOOSE AT ROW 8 ABC. REMOVED AND REPLACED EEPLS STRIP SECTION PER MM. 2L72 4F RTA16WE 20051219000482005121900048NM 2005 12 19 USAA051505 120051212A5320 ANGLE BOEING737 7374B7 1384702NM BS 967 DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 FOUND GROOVE RIGHT AFT DOOR SILL FUSELAGE STATION 967. REMOVED AND REPLACED ANGLE IAW SRM 51-10-02 DEFECT SIZE: 11" 2L72 4F RTA16WE 20051219000492005121900049NM 2005 12 19 SWAA053903 120051207A53306545765 SKIN BOEING737 7373H4 1384600NM BS 500D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 16R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051219000512005121900051NM 2005 12 19 SWAA053905 120051207A53306545775 SKIN BOEING737 7373H4 1384600NM BS 791 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 791, STR 14R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051219000522005121900052NM 2005 12 19 SWAA053906 120051207A53306545775 SKIN BOEING737 7373H4 1384600NM BS 807 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 807, STR 19L. REPAIRED SKIN PER SWA EA AND SRM. 2L72 4F RTA16WE 20051219000532005121900053NM 2005 12 19 SWAA053907 120051207A53306545774 SKIN BOEING737 7373H4 1384600NM BS 767 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 19L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051219000572005121900057NM 2005 12 19 SWAA053911 120051210A335007912 COVER BOEING737 7377H4 1384404NM ROW 17 BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29430WN 33659 DURING SCHEDULED HC2 CHECK, FOUND EEPLS TRACK COVER BROKEN AT ROW 17. REMOVED AND REPLACED COVER PER MM. 2L72 4F RTA16WE 20051219000682005121900068NM 2005 12 19 SWAA053953 120051214A335007912 COVER BOEING737 7377H4 1384404NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29435WN 32455 EEPLS TRACK COVER BROKEN. REMOVED AND REPLACED COVER PER MM. 2L72 4F RTA16WE 20051219000702005121900070NM 2005 12 19 SWAA053955 120051213A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29449WN 32469 DURING SCHEDULED HC1 CHECK, FOUND EEPLS TRACK COVER CRACKED AT ROW 13. REMOVED AND REPLACED COVER PER MM. 2L72 4F RTA16WE 20051219000712005121900071NM 2005 12 19 SWAA053956 120051214A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29482WN 29852 DURING SCHEDULED HC2 CHECK, FOUND EEPLS TRACK COVER BROKEN AT ROW 1 ABC. REMOVED AND REPLACED COVER PER MM. 2L72 4F RTA16WE 20051219000732005121900073NM 2005 12 19 SWAA053958 120051214A335010107451 SIGN BOEING737 7375H4 138449DNM EMERGENCY EXIT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29526SW 26568 RT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM. 2L72 4F RTA16WE 20051219000742005121900074NM 2005 12 19 SWAA053959 120051213A3350BR2013 COVER BOEING737 7373H4 1384600NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29600WN 27694 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS STRIP MISSING COVER BETWEEN ROWS 6 TO 16 DEF. REMOVED AND REPLACED EEPLS STRIP PER MM. 2L72 4F RTA16WE 20051213000372005121300037NM 2005 12 13 USAA051469 120051206A5320 INTERCOSTAL BOEING737 737301 1384611NM BS 300 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19591US 23936 S16L INTERCOSTAL WEB STA 300 CRACKED. REPLACED WITH IDENTICAL PART, FABRICATED WEB FROM .040 INCH 7075=T6, INSTALLED PER SRM 53-10-15. 2L72 4F RTA16WE 20051213000432005121300043 2005 12 13 SWAA053886 420051206A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29359SW 26596 DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051213000572005121300057NM 2005 12 13 2005UALA01336 120051127A5610 WINDOW BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU COCKPIT ARCED A UALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 WP29370UA 24539 ARCING AND SMOKE FROM CAPTAIN'S SLIDING WINDOW. REPLACED BROKEN LUG ON WIRE W504-404-20W AT T266 AND SECURED WIRING. WINDOW HEAT OPS CHKS OK. 2L72 4F4 FRTA16WE E21EU 20051213000692005121300069NM 2005 12 13 2005UALA01349 120051127A5311 FRAME BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU BS 616 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29921UA 25388 STATION 616 AT WL 201 OVERWING FRAME INNER CHORD CRACKED AT LOWER FASTENER ON RIGHT HAND SIDE. CUT OUT DAMAGE & CONFIRMED CRACK CONTAINMENT PER NDT MAN PART 6 CHAPTER 51. FABRICATED REPAIR ANGLE FROM 15-5PH STAINLESS STEEL & FILLER FROM 7075 T6. HEAT TR EATED, CAD PLATED AND PRIMED REPAIR PARTS & INSTALLED PER MM 53- 11-89. 2L72 4F4 FRTA16WE E21EU 20051213000892005121300089NM 2005 12 13 2005UALA01369 120051129A5310 CREASE BEAM BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU BS 947-996 CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29922UA 26642 CABIN FLOOR CREASE BEAM STR 17R CORRODED FROM STATIONS 947.5 - 996.5, RBL 62.5. MAJOR REPAIR ACP'D PER SRM 51-40-02, CREASE BEAM ASSY REPLMT ACP'D 2L72 4F4 FRTA16WE E21EU 20051213000962005121300096NM 2005 12 13 2005UALA01376 120051128A3350 BATTERY AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE EMERGNECY LIGHT FAULTY A UALAK NONE L NO TEST ININSP/MAINT 1 WP29816UA 871 EMERGENCY LIGHT TEST FAULTS LEFT FWD BATTERY. REPLACED BATTERY. 2L72 4F4 FRTA28NM E40NE 20051213000992005121300099NM 2005 12 13 2005UALA01379 120051126A3350 LIGHT BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE CABIN LOOSE A UALAK NONE O OTHER ININSP/MAINT 1 WP29798UA 26928 EXIT PATH LIGHT AT 2E IS LOOSE. SECURED LOOSE EEL EXIT PATH LIGHTING AT 2E. JARRED LOOSE DURING PASSENGER ENTRY OR EGRESS. 2L72 4F4 FRTT0001SE E46NE 20051213001022005121300102NM 2005 12 13 2005UALA01382 120051130A3350 LIGHT AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE CABIN MALFUNCTIONED A UALAK NONE O OTHER ININSP/MAINT 1 WP29854UA 1731 EMERGENCY EXIT LIGHT SYSTEM LIGHTS WERE FLICKERING, NOW ON FULL TIME OVERHEAD SIGNS AND PATH LIGHTS. RESET CIDS, OPS CHECKS NORMAL. 2L72 4F4 FRTA28NM E40NE 20051213001042005121300104EU 2005 12 13 2005UALA01384 120051201A5320 SILL AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE GALLEY DOOR CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29424UA 506 AFT RT GALLEY DOOR THRESHOLD SILL PLATE WAS FOUND CORRODED THROUGH AT FASTENER HOLE. REPLACED DOOR SILL PLATE REF SRM 51-42-14. 2L72 4F4 FRTA28NM E40NE 20051213001132005121300113EA 2005 12 13 COMA0560681 120051210A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS WARNING LIGHT A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01937CA 7044 FLIGHT 5854 - INBOUND CVG RECEIVED A FLAP FAIL MESSAGE WHEN HANDLE WAS MOVED FROM 30 TO 45 DEGREES. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION, PARAGRAPH (B) 1,2,3 (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2L72 4F RTA21EA 20051213001222005121300122WP 2005 12 13 IXXA0500147S 120050225A5710 REPAIR DOUG DC8 DC871F 302199DWP XW 87.000 IMPROPER A IXXAK NONE O OTHER ININSP/MAINT 1 SW11821BX858952998 45811 DURING A ROUTINE C CHECK INSPECTION, FOUND RT WING INBOARD FLAP FORWARD UPPER PLATING INTERIM REPAIR AT STA XW 87.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF EXISTING REPAIR AND THE DAMAGED AREA. FABRICATED NEW PLATING SEGMENT + INTERNAL SPLICE, EXTERNAL DOUBLERS. CLEANED TREATED AND PRIMED DOUBLERS AND AREA. INSTALLED REPAIR PART IAW SEMAN DWG ED-3841 AND FAA FORM 8110-3 NR 05019, DC8 SRM 51-1-11, 51-1-15, 51-1-20D, 51-1-22, D51-1-26, 51-3-0, 51-3-1, 51-3-2. 2L74 4F RT4A25 20051213001282005121300128EA 2005 12 13 COMA0560675 120051207A2751 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS WARNING LIGHT A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01927CA 7031 FLIGHT 5870 - EN ROUTE BOS YHZ RECEIVED A FLAP FAIL CAUTION MESSAGE. ABORTED FIRST APPROACH AT YHZ, THEN LANDED WITHOUT INCIDENT ON SECOND ATTEMPT. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A, B,C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2L72 4F RTA21EA 20051213001332005121300133EA 2005 12 13 SWIA200515966 120050809A5320 WEB CNDAIRCL600 CL6002B19 1900309EA E/E BAY CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07448SW 7678 AFT EQUIPMENT BAY; ESB LOWER WEB IS CRACKED; RBL - 38.0 EXTENDING FROM ACCESS PANEL CUT-OUT, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED ESB RBL 38 LWR WEB IAW CRJ REO 601R-53-61-366 REV "E". 2L72 4F RTA21EA 20051213001432005121300143EA 2005 12 13 SWIA200515972 120051206A2741 SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB DISCONNECT MALFUNCTIONED A SWIAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 NM07439SW 7578 "STAB TRIM" AND "MACH TRIM" CAUTION MESSAGES ILLUMINATED AFTER TAKE OFF (1500' AGL). REPLACED CO-PILOT STAB DISCONNECT SWITCH IAW MM 27-41-30. OPERATIONAL CHECK GOOD IAW MM 27-40-00. 2L72 4F RTA21EA 20051213001482005121300148SO 2005 12 13 CHQA200500205 120051202A335066367 LIGHT EMB 145 EMB145LR 3260212SO CABIN BURNED OUT A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11268SK 145270 EMERGENCY FLOOR LIGHT STRIP THIRD BACK INOPERATIVE. REMOVED AND REPLACED FLOOR LIGHT STRIP IAW MM 33-60-00. NO FURTHER DEFECTS NOTED. 2L72 4T RTT00011AT 20051213001492005121300149SO 2005 12 13 CHQA200500204 120051202A2120 SMOKE EMB 145 EMB145LR 3260212SO CABIN DETECTED A CHQAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL11268SK 145270 TOOK OFF FROM DCA WITH NO PROBLEMS. AT 1500 FT, BROUGHT FLAPS UP AND WENT TO CLIMB THRUST, NOTICED COCKPIT SEEMED A LITTLE HAZY. F/O OFFICER NOTICED HAZE. HAZE STARTED TO GET THICKER. F/A ATTENDANT SAW SMOKE OR HAZE IN THE CABIN. DIVERTED TO IAD. RAN ALL NORMAL CHECK LISTS. LANDED OVERWEIGHT IN IAD, TAXIED TO GATE. MX INSPECTED AND FOUND COUPLINGS AFT AND FORE OF DUEL TEMP CONTROL VALVE NR 2 TO BE AT FAULT. R/R`D COUPLINGS AND CLAMPS IAW MM 21-60-01 AND OPS CHECK OK IAW MM CH 21. NO DEFECTS NOTED; A/C OK FOR SERVICE. FLT 3120 IAD-IND, WHEN CLIMBING THROUGH 15,000 FEET, TURNED ON MAP LIGHT AND NOTICED HAZE AGAIN. F/A SAW IT, FIRST OFFICER SAW IT. RETURNED TO IAD. TURNED OFF PACK 2 AND SMOKE SEEMED2L72 4T RTT00011AT 20051214000032005121400003EA 2005 12 14 COMA0560696 120051208A2497D18ZZA RELAY CNDAIRCL600 CL6002B19 1900309EA AVIONICS BAY OVERHEATED A COMAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 SO01498CA7485 7792 FLIGHT 5029- ENROUTE CVG-ACY CREW DETECTED AN ELECTRICAL OVERHEAT SMELL FOLLOWED BY AC BUS 1 CAUTION MESSAGE, LEFT AUTO TRANSFER FAIL, GENERATOR 1 OFF CAUTION, STAB TRIM AND MACH TRIM CAUTIONS, EFIS COMP MON WITH IAS YELLOW ON AIRSPEED AND AUTOPILOT NOSE UP TRIM CAUTION. CREW DECLARED AN EMERGENCY AND DIVERTED TO CMH, FLIGHT LANDED WITHOUT INCIDENT. (NO VISIBLE SMOKE IN COCKPIT OR CABIN). FOUND 1K4XD - AC UTILITY BUS #1 RELAY TO BE THE ROOT CAUSE OF ELECTRICAL OVERHEAT SMELL. REPLACED RELAY AND SURROUNDING ELECTRICAL COMPONENTS/WIRING. 2L72 4F RTA21EA 20051214000042005121400004NM 2005 12 14 2005UALA01388 120051203A5312 BULKHEAD BOEING737 737522 138449FNM BS 1016 TOOL DAMAGE A UALAK NONE O OTHER ININSP/MAINT 1 WP29921UA 25388 SEVERAL TOOL MARKS FOUND AROUND LH UPPER WIRE BUNDLE FEED THROUGH ON FWD SIDE OF BLKHD STA 1016. MAJOR REPAIR ACP'D PER AAR EA I050299IR, EXISTING DOUBLER REMOVED, NEW DOUBLER FABRICATED AND INST'D. 2L72 4F RTA16WE 20051214000122005121400012EU 2005 12 14 IXXA0500146O 220051208A73208013212 MEC DOUG DC8 DC871F 302199DWP CFMINTCFM56 CFM563C1 13802EU NR 1 ENGINE INOPERATIVE A IXXAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SW11820BX8719786084 46065 693398 DURING CLIMB FROM KTOL TO KPHL NR 1 THROTTLE HAS TO BE RETARDED APPROX 4 KNOTS WIDTH TO MAINTAIN CLIMB THRUST, AT CRUISE POWER THROTTLE IS JUST ABOVE IDLE. CREW SHUT DOWN ENGINE PRIOR TO LANDING BECAUSE UNABLE TO RETARD POWER, POSITIVE OIL PRESSURE AND QUANTITY NOTED PRIOR TO SHUTDOWN. MAINTENANCE REMOVED AND REPLACED CIT SENSOR AND MEC. PERFORMED FLIGHT IDLE, 75% AND MAXPOWER RUNS. THE NR 1 ENGINE OPS CHECK WAS NORMAL. THE ENGINE RUN WAS ACCOMPLISHED WITHIN 24 HOURS OF ENGINE SHUTDOWN. OPS CHECKS WERE GOOD PER ALL APPLICABLE MANUALS AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F4 FRT4A25 E21EU 20051215000072005121500007 2005 12 15 CALA0500433 420051209A25651268128 ACTUATOR BOEING757 757224 1384958NM SLIDE INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW271313820475 30351 THE SLIDE CARRIAGE FAILED WORK CARD 19-2560-1-7650 STEPS DURING RT OFF WING DEPLOY FUNCTIONAL CHECK. THE RT WING ESCAPE SLIDE ACTUATOR WAS REMOVED AND REPLACED IAW MM 25-65-05. THE DOOR LATCHES WERE ADJUSTED IAW MM 25-65-07. 2L72 4F RTA2NM 20051215000082005121500008 2005 12 15 CALA0500434 420051209A25651268127 ACTUATOR BOEING757 757224 1384958NM SLIDE INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW271313820475 30351 THE LT OFF WING SLIDE DEPLOY CHECK FAILED STEPS OF WORK CARD 19-2560-1-7650. THE LT WING ESCAPE SLIDE DEPLOYMENT ACTUATOR WAS REPLACED IAW MM 25-65-05. 2L72 4F RTA2NM 20051215000152005121500015NM 2005 12 15 SWAA053930 120051212A2560P4010021 BATTERY BOEING737 7373H4 1384600NM FLASHLIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 FWD OUTBOARD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2L72 4F RTA16WE 20051215000162005121500016NM 2005 12 15 SWAA053931 120051212A3350MS155721 BULB BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29714CB 27848 DURING SCHEDULED RON CHECK, FOUND R1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20051215000252005121500025SO 2005 12 15 RAIA00512009 120051205A3350 LIGHT EMB 145 EMB145 3260210SO CABIN BURNED OUT A RAIAK NONE O OTHER ININSP/MAINT 1 CE03820HK 145064 PREFLIGHT CEILING EMERGENCY LIGHT BURNED OUT. MAINTENANCE REPLACED THE EMERGENCY EXIT BULB. 2L72 4F RTT00011AT 20051215000332005121500033EA 2005 12 15 QXEA200501669 120051031A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 349-485 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, FUSELAGE INTERIOR RIGHT INBOARD SEAT RAIL AT STATION 349-485 CORRODED. MAINTENANCE REPAIRED SEAT RAIL IAW REO 670-53-00-013. 2L72 4F RTA21EA 20051215000392005121500039EA 2005 12 15 QXEA200501696 120051031A5320 SILL CNDAIRCL600 CL6002C10 1390015EA CARGO DOORWAY CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, AFT BAGGAGE BAY DOOR SURROUND SILL HAS 6 AREAS OF CORROSION ON INBOARD EDGE. REMOVED MINOR CORROSION IAW CRJ-700 SRM 51-21-06-001-001-A01. NEGLIGIBLE MATERIAL LOSS. RESTORED FINISH. 2L72 4F RTA21EA 20051215000482005121500048EA 2005 12 15 COMA0560693 120051207A2750865D1007 PDU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01995CA1846513781 7229 FLIGHT 5541 - FLAPS FAIL CAUTION. REPLACED THE PDU. 2L72 4F RTA21EA 20051215000552005121500055EA 2005 12 15 QXEA200501668 120051031A5310 RIVET CNDAIRCL600 CL6002C10 1390015EA FUSELAGE UNKNOWN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK. FUSELAGE INTERIOR AT STATION 575 STRINGER 5R HAS A DUMPED RIVET IN THE STRINGER TO SKIN. MAINTENANCE REPLACED THE RIVET IAW CRJ-700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20051215000572005121500057EA 2005 12 15 QXEA200501673 120051031A2810 DRAIN CNDAIRCL600 CL6002C10 1390015EA FUEL BALANCE MISDRILLED A QXEAK NONE W INADEQUATE Q C ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, LEFT WING FUEL BALANCE TUBES DRAIN HOLES DRILLED 180 DEGREES OUT OF POSITION DURING WORK ACCOMPLISHMENT. COMPLIED WITH EA R-57-110. MISDRILLED HOLES PERMISSIBLE IAW EA R-57-110. 2L72 4F RTA21EA 20051215000602005121500060EA 2005 12 15 QXEA200501686 120051031A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 501-570 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, LEFT OUTBOARD SEAT RAIL AT STATION 501-570 HAS SURFACE CORROSION. REPAIRED SEAT RAIL IAW REO 670-53-00-013. 2L72 4F RTA21EA 20051215000672005121500067EA 2005 12 15 QXEA200501695 120051031A5410 SHIELD CNDAIRCL600 CL6002C10 1390015EA RT NACELLE TORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, RIGHT ENGINE RIGHT LOWER MID CORE COWLING FIRE SHIELD LAYER IS TORN AND DISBONDED. REPAIRED IAW EA R-54-84. 2L72 4F RTA21EA 20051215000742005121500074EA 2005 12 15 QXEA200501684 120051031A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 581-661 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, LEFT OUTBOARD SEAT RAIL AT STATION 581-661 HAS SURFACE SCRATCHES. REPAIRED IAW REO 670-53-00-013. 2L72 4F RTA21EA 20051215000822005121500082NM 2005 12 15 QXEA200501756 120051115A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX - NR 3 SEAT TRACK HAS LITE SUFRACE CORROSION ON TOP OF LUGS AT X518-X519. REPAIRED IAW RD 8-53-3644, DHC-8-202 SRM 51-40-00 AND SRM 51-40-11. 2H72 4T RTA13NM 20051215001012005121500101NM 2005 12 15 DL757050757 120051123A5330146N37805 SKIN BOEING757 757232 1384965NM STA 1680 S-20L DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27673DL 25978 FUSELAGE/SKIN/DENT AT STA 1680 BELOW S-20L. THE DENT IS CUT OUT AND AN EXTERNAL ALUMINUM DOUBLER IS INSTALLED WITH SOLID ALUMINUM RIVETS AND HI-LOKS REF ACTS PP B757-53-22108. 2L72 4F RTA2NM 20051215001062005121500106EA 2005 12 15 COMA0560705 120051206A2751601R930303 TRANSMITTER CNDAIRCL600 CL6002B19 1900309EA RT TE FLAP FAULTY A COMAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 SO01969CA23983 7141 FLIGHT 5675 - DURING CLIMB-OUT OF CVG RECEIVED A FLAP FAIL CAUTION MESSAGE. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE FLAP POSITION TRANSMITTER. 2L72 4F RTA21EA 20051215001092005121500109EA 2005 12 15 COMA056707 120051206A2752852D10021 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA RT TE FLAP FAULTY A COMAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 SO01969CA23983 7141 FLIGHT 5675 - DURING CLIMB-OUT OF CVG RECEIVED A FLAP FAIL CAUTION MESSAGE. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE RIGHT INBOARD FLAP INBOARD ACTUATOR. 2L72 4F RTA21EA 20051215001132005121500113NM 2005 12 15 AWXA200501514 120051127A53206546812188 FLOOR SUPPORT BOEING737 73733A 1384673NM BS 101 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 MCN - DURING C19 CHECK DISCOVERED FASTENER HOLE CRACKED, .75 INCHES, ON BEAM AT BS 101, WL 208 AND BL 10L. MAINTENANCE REMOVED AND INSTALLED NEW BEAM AT BS 101, WL 208 AND BL 10L IAW BOEING 737-300 SRM 51-40-02-0G. 2L72 4F RTA16WE 20051215001232005121500123EA 2005 12 15 SWIA200515993 120051209A274170608 TRIM SYSTEM CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED APAPPROACH 1 NM07464SW1120411204 7827 STAB TRIM WENT OFF WHE FLAPS SELECTED ON APPROACH. REPLACED HSTCU. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051215001242005121500124EA 2005 12 15 SWIA200515994 120051202A2750766389L CONTROLLER CNDAIRCL600 CL6002C10 1390015EA FLAP/SLATS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07762SK 10226 FLAPS HALFSPEED MESSAGE. REPLACED SFECU1 IAW MM 27-51-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051215001292005121500129NM 2005 12 15 2005UALA01410 120051206A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29198UA 28716 FOUND 54C EEL INOP. REPLACED EEL LIGHT. 2L74 4F4 FRTA20WE E24NE 20051215001312005121500131EU 2005 12 15 2005UALA01412 120051206A3230664700500A4D CONTROL UNIT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NLG MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 WP29443UA 820 RETURN TO FIELD DUE TO SHOCK ABSORBER FAULT MESSAGE. TROUBLESHOOTING OF NOSE GEAR LOG. JACKED NOSE AND SWUNG GEAR NUMEROUS TIMES, NO FAULTS FOUND. SHOOK OUT WIRING ON NOSE GEAR, NO FAULTS. SEE ITEM FOR SVCING STRUT, PER SFOLM SWANN, REPLACED NR 2 LGCIU PRECAUTIONARY. CONT OF AMIS ITEM 2482006 :REPLACED NR 2 LGCIU, MM 32-31 71 000-001, TEST OK. TROUBLESHOOTING OF NOSE GEAR LOG ITEMS . BY- 13581:JACKED NOSE AND SWUNG GEAR NUMEROUS TIMES, NO FAULTS FOUND. SHOOK OUT WIRING ON NOSE GEAR, NO FAULTS. SEE ITEM FOR SVCING STRUT. PER SFOLM SWANN, REPLACED NR 2 LGCIU PRECAUTIONARY. FOUND NOSE STRUT LOW ON INSPECTION BY-11873, SVC PER 12-14-32 MM. 2L72 4F4 FRTA28NM E40NE 20051215001342005121500134NE 2005 12 15 2005UALA01415 220051207A7200 ENGINE AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE NR 1 UNKNOWN A UALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 WP29812UA 850 V10070 RETURN TO FIELD DUE TO NR 1 ENGINE REDUCED TO IDLE. ENGINE 1 REVERTED FROM EPR MODE TO N1 MODE DUE TO THE APPARENT LOSS OF P2T2 PROBE HEATER. THIS IS PER DESIGN. THIS IS A CHRONIC ISSUE ON THIS ENGINE FIRST RTF EVENT 3 DEC MX REPLACED P2T2 PROBE PER TSM. EPR MODE FAULT REPEATED ON THE 4 DEC MX VERIFIED GOOD INSTALLATION OF P2T2 PROBE CHECK WIRING FOLLOWED BY EEC REPLACEMENT. TSM STEP TO REPLACE RELAY BOX WAS MISSED. SECOND RTF SAMC/ENGINEERING SUGGESTED RELY BOX REPLACEMENT ALONG WITH WIRING AND SOLENOID CHECKS AN FMU REPLACEMENT. ENGINEERING BELIEVES P2T2 RELY BOX WAS THE MOST PROBABLE CAUSE HOWEVER THIS UNIT IS NOT TRACKED AND ON OFF UNIT SN REPORTED SO NO DATA IS NOT AVAILABLE TO CONFIRM TH 2L72 4F4 FRTA28NM E40NE 20051215001482005121500148NM 2005 12 15 2005UALA01429 120051209A5311 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE STA 967 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29922UA 26642 BS 967 INTERNAL FUSELAGE FRAME CRACKED JUST ABOVE DOOR 2 LT. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER PER SRM 53-00-07. 2L72 4F4 FRTA16WE E2GL 20051215001532005121500153NM 2005 12 15 2005UALA01434 120051212A3397 CONNECTOR BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT LOOSE A UALAK NONE O OTHER ININSP/MAINT 1 WP29120UA 29166 AFT GALLEY EMERGENCY WALL EEL LIGHT ON LEFT SIDE INOP. SECURED LOOSE CONNECTOR. 2L74 4F4 FRTA20WE E24NE 20051215001592005121500159NM 2005 12 15 2005UALA01440 120051211A3397 CONNECTOR BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT UNSECURE A UALAK NONE O OTHER ININSP/MAINT 1 WP29121UA 29167 FOUND FROM ROW 35 TO 44 SEAT LT EMERGENCY LIGHT INOP. RESECURED EMERGENCY LIGHT CONNECTOR. 2L74 4F4 FRTA20WE E24NE 20051215001612005121500161NM 2005 12 15 2005UALA01442 120051211A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE LT OVERWING INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29121UA 29167 FOUND OVERWING LT 2ND FROM TOP EMERGENCY LIGHT INOP. REPLACED LAMP. 2L74 4F4 FRTA20WE E24NE 20051215001722005121500172NM 2005 12 15 USAA051480 120051208A53201136993 INTERCOSTAL BOEING737 7374B7 1384702NM STA 312-328 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 FOUND CORROSION STA 312-328, LBL9. REMOVE AND REPLACE INTERCOSTAL IAW SRM 51-10-02, DEFECT SIZE: .5" AREAS OF CORROSION ON THE INTERCOSTAL 16" IN LENGTH. 2L72 4F RTA16WE 20051215001782005121500178NM 2005 12 15 USAA051474 120051208A5340 ATTACH ANGLE BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19591US 23936 FOUND CRACK S15L INTERCOSTAL WEB FWD ATTACH ANGLE AT I/B END IN RADIUS. REMOVED AND REPLACED ANGLE IAW SRM 51-10-02 AND DWG 69-16970, DEFECT SIZE: 1/2" CRACK. 2L72 4F RTA16WE 20051215001852005121500185NM 2005 12 15 USAA051484 120051209A5311 FRAME BOEING737 7374B7 1384702NM STA 727E, S8R-S9CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 FOUND FRAME DAMAGED STA 727E, S8R-S9R. REMOVED DAMAGE INSTALLED ANGLED DOUBLER AND ANGLED TRIPLER IAW TYP REP 53-10-20, DEFECT SIZE: FUSELAGE FRAME CRACKED AT RT PSU RAIL ATTACH BRACKET. 2L72 4F RTA16WE 20051215001872005121500187NM 2005 12 15 USAA051490 120051212A5340 ANGLE BOEING737 7374B7 1384702NM FWD GALLEY AREA CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 FOUND FWD GALLEY AREA CORRODED STA 277-360RBL. MAJOR REPAIR, NEW Z ANGLE PREVIOUSLY INSTALLED IAW BOEING DRWG 65-45834, DEFECT SIZE: .250. 2L72 4F RTA16WE 20051219000062005121900006WP 2005 12 19 ABXA050356 120051213A3260 SWITCH DOUG DC9 DC933F 302207AWP MLG OUT OF POSITION A ABXAO OTHER N FALSE WARNING CLCLIMB 1 GL23932AX 47465 AFTER TAKEOFF WHEN THE GEAR WAS RAISED, GOT THE TAKEOFF WARNING HORN. LOWERED THE GEAR TO EXTINGUISH THE HORN. AFTER THE SLATS AND FLAPS WERE UP, GEAR WAS RAISED WITH NO FURTHER PROBLEMS. TAKEOFF WARNING TESTS OK. GEAR WARNING TEST FAILED AT 5 DEGREES FLAP POSITION. FOUND LANDING GEAR WARNING SWITCH (A2-85) AT FLAP CONTROL DRUM BEING ACTUATED BY CONTROL DRUM CABLE RETAINING SAFETY WIRE. REPOSITIONED SWITCH TO ALIGN WITH CENTER OF ACTUATING CAM. GEAR WARNING TEST OK. REF AMM 27-53-01, DC9-1. 2L72 4F A6WE 20051219000172005121900017NM 2005 12 19 05FDEA04230 120051212A5753 MOUNT DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 FOUND LEFT WING: WITH REFERENCE TO EO 1-5750-7-5002, OUTBOARD FLAP OUTBOARD FORWARD HINGE LOWER INBOARD MOUNT BORE CORRODED. REMOVED AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-94563. 2L73 4F RTA22WE 20051219000212005121900021NM 2005 12 19 05FDEA04234 120051212A5753 MOUNT DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 FOUND RIGHT WING, WITH REFERENCE TO EO 1-5750-7-5002, OUTBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG BORE CORRODED. CORROSION REMOVED AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-94562. 2L73 4F RTA22WE 20051219000312005121900031EA 2005 12 19 SWIA200515980 120051209A274170609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07945SW1485 1485 7770 STAB TRIM INDICATIONS FLUCTUATE IN FLIGHT. REPLACED HSTCU PER CRJ 200 MM 27-40-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051219000502005121900050NM 2005 12 19 SWAA053904 120051207A53306545767 SKIN BOEING737 7373H4 1384600NM BS 404 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 404, STR 26R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051219000552005121900055 2005 12 19 SWAA053909 420051211A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29391SW 27378 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051219000582005121900058EA 2005 12 19 COMA0560709 120051210A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA LEFT MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01937CA11664786 7044 FLIGHT 5557 - FLAPS FAIL CAUTION. REPLACED THE LT BPSU. 2L72 4F RTA21EA 20051219000662005121900066NM 2005 12 19 SWAA053951 120051214A335007912 COVER BOEING737 7377H4 1384404NM ROW 11ABC MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29215WN 32487 EEPLS TRACK COVER MISSING AT ROW 11 ABC. INSTALLED COVER PER MM. 2L72 4F RTA16WE 20051219000672005121900067NM 2005 12 19 SWAA053952 120051214A335065C32046 WIRE BOEING737 7373H4 1384600NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D CHECK, FOUND COCKPIT EMERGENCY EXIT LIGHT INOP. REPAIRED GROUND WIRES L3 & L4 PER WDM. OPS CHECK OK PER MM. 2L72 4F RTA16WE 20051219000762005121900076NM 2005 12 19 USAA051504 120051212A5330 SKIN BOEING737 7373B7 1384580NM BS 860-882 CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19527AU 23862 FOUND STA 860-882 UNDER DORSAL FIN CHAFED. REMOVED DAMAGE, INSTALLED DOUBLER IAW SRM 53-60-01, REPAIR 9 AND EA 97194, DEFECT SIZE:. 2L72 4F RTA16WE 20051219000782005121900078WP 2005 12 19 ABXA050340 120051207A3350 BATTERY PACK DOUG DC8 DC861 3021952WP EMERGENCY LIGHT INOPERATIVE A ABXAO OTHER L NO TEST NRNOT REPORTED 1 GL23842AX 46015 EMERGENCY EXIT LIGHTS (UNDER GLARESHIELD, OVERHEAD AND CLOSET LIGHTS) VERY DIM. OPS CHECKED ALL LIGHTS, ALL OPS CHECKED GOOD AT THIS TIME IAW DC8 MM. 2L74 4F 4A25 20051219000792005121900079NM 2005 12 19 USAA051503 120051212A5330 SKIN BOEING737 737301 1384611NM BS 860-880 CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19353US 23556 FOUND CHAFING STA 860-880 S1L-S1R. INSTALLED DOUBLER IAW EA 97199, DEFECT SIZE: 14" AND 11". 2L72 4F RTA16WE 20051219000802005121900080NM 2005 12 19 USAA051491 120051212A5315 FLOORBEAM BOEING737 737301 1384611NM STA 986.5 LBL6 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19591US 23936 FOUND CORRODED STA 986.5 LBL6 TO LBL43. MAJOR REPAIR REMOVED DAMAGE ON FLOORBEAM AND INSTALLED T CAP IAW TR 53-10-05, DEFECT SIZE: .5"X33". 2L72 4F RTA16WE 20051219000812005121900081NM 2005 12 19 USAA051501 120051212A52106517688U165 ANGLE BOEING737 7374B7 1384702NM FWD ENTRY DOOR CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 FOUND CORROSION FWD ENTRY DOOR Z ANGLE STA 306-346. REMOVED DAMAGED Z ANGLE AND INSTALLED A NEW Z ANGLE IAW 53-10-15 FIG 101, DEFECT SIZE: 38". 2L72 4F RTA16WE 20051219000862005121900086NM 2005 12 19 USAA051496 120051212A575365C2660399A SKIN BOEING737 737301 1384611NM TE FLAP DEBONDED A USAAK NONE O OTHER ININSP/MAINT 1 EA19591US 23936 FOUND TRAILING EDGE WEDGE TOP SKIN DISBONDED INBOARD END NUMBER 3 SLAT. MAJOR REPAIR IAW SRM 51-70-10, DEFECT SIZE: 1". 2L72 4F RTA16WE 20051219000882005121900088NM 2005 12 19 USAA051494 120051212A5311 FRAME BOEING737 7374B7 1384702NM BS 827 S9L CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 FOUND FRAME CRACKED STA 827 S9L. REMOVED DAMAGE, INSTALL ANGLED DOUBLER AND TRIPLER IAW TYP REP 53-10-20C, DEFECT SIZE: .500". 2L72 4F RTA16WE 20051219000892005121900089NM 2005 12 19 USAA051510 120051212A5510 MOUNT BOEING737 7374B7 1384702NM HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 FOUND CORROSION RT HORIZ STAB R1 LUG FWD FACE AND BORE. SPOT FACED FWD FACE OF LUG, INSTALLED NEW BUSHINGS IAW SRM 55-10-10 SRM 52-10-10, DEFECT SIZE: .375". 2L72 4F RTA16WE 20051219000902005121900090NM 2005 12 19 USAA051502 120051212A5311 FRAME BOEING737 7374B7 1384702NM BS 615 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 FOUND CRACK FS 615 RIGHT SIDE ON INNER CORD ANGLE JUST BELOW CABIN FLOOR. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLERS AND DOUBLERS IAW TR 53062-01, DEFECT SIZE: 1.5". 2L72 4F RTA16WE 20051219000972005121900097NM 2005 12 19 SWAA053913 120051208A53126546568 BULKHEAD BOEING737 7375H4 138449DNM BS 1016 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29511SW 24188 DURING SCHEDULED 1/2D CHECK, FOUND BS 1016 AFT PRESSURE BLKHD DOME WEB PANEL NR 6 CRACKED AT 9 O'CLOCK POSITION. REPAIRED DOME WEB PER SWA EA. 2L72 4F RTA16WE 20051219000982005121900098 2005 12 19 SWAA053914 420051211A25656945735 BRACKET BOEING737 7375H4 138449DNM R2 DOOR SLIDE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29524SW 26566 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD ATTACH MOUNT BRACKET CRACKED. REMOVED AND REPLACED MOUNT BRACKET PER MM. 2L72 4F RTA16WE 20051219000992005121900099NM 2005 12 19 SWAA053915 120051209A53116558280 FRAME BOEING737 7373H4 1384600NM BS 360 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29622SW 27932 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051219001002005121900100NM 2005 12 19 SWAA053916 120051209A53116546526 FRAME BOEING737 7373H4 1384600NM BS 400 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29622SW 27932 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051219001012005121900101NM 2005 12 19 SWAA053917 120051209A53206551698 SPLICE BOEING737 7373H4 1384600NM BS 907 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29622SW 27932 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20051219001032005121900103NM 2005 12 19 SWAA053919 120051209A53116546550 FRAME BOEING737 7373H4 1384600NM BS 787 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29622SW 27932 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051219001042005121900104 2005 12 19 SWAA053920 420051209A256565C16820 HOOK BOEING737 7373H4 1384600NM L1 DOOR GIRT BARLOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29637SW 27710 L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINING HOOK LOOSE. SECURED HOOK PER MM. 2L72 4F RTA16WE 20051219001052005121900105NM 2005 12 19 SWAA053921 120051211A575465C26686 SKIN BOEING737 7373H4 1384600NM NR 5 SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29640SW 27713 DURING SCHEDULED SPECIAL VISIT, FOUND NR 5 L/E SLAT LOWER T/E SKIN CRACKED. REPAIRED SLAT PER SRM. 2L72 4F RTA16WE 20051219001072005121900107NM 2005 12 19 SWAA053923 120051209A3350MS155721 BULB BOEING737 7373A4 1384585NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY BULLNOSE LIGHT INOP AT ROW 12 DEF. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20051219001122005121900112EU 2005 12 19 USAA051527 120051213A5315D5347209000500 FLOORBEAM AIRBUSA321 A321211 3930370EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19164UW 1425 FOUND FLOORBEAM CORRODED, -Y1292 FS 66. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-72-11; CORROSION LEVEL 1; TASK JA-260-53500, DEFECT SIZE: 4" X 30". 2L72 4F RTA28NM 20051219001142005121900114EU 2005 12 19 USAA051525 120051213A5347D53456037200 SEAT TRACK AIRBUSA321 A321211 3930370EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19164UW 1425 FOUND CORROSION LEFT OUTBOARD SEAT TRACK AT FS 47. REMOVED AND REPLACED SEAT TRACK PER SRM 53-41-14, 53-41-15; CORROSION LEVEL 1; TASK JA-220-25502, DEFECT SIZE: 1/2" BY 1/4", - 2 AREAS. 2L72 4F RTA28NM 20051219001152005121900115EU 2005 12 19 USAA051524 120051213A5315D531146100200 FLOORBEAM AIRBUSA321 A321211 3930370EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19164UW 1425 FOUND BEAM CORRODED Y-254 AT FS 20R. REMOVED AND REPLACED WITH SAME P/N PER SRM 51-72-11; CORROSION LEVEL 1; TASK JA-220-5350, DEFECT SIZE: 2" X 3" X .047" DEEP. 2L72 4F RTA28NM 20051219001162005121900116NM 2005 12 19 USAA051513 120051213A5510 BUSHING BOEING737 7374B7 1384702NM HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 FOUND CORROSION L6 CLEVIS AFT FACE. REMOVED DAMAGE, FABRICATED AND INSTALLED NEW BUSHING IAW SRM 55-10-10, DEFECT SIZE: .250 DIA SPOTS OF CORROSION. 2L72 4F RTA16WE 20051219001172005121900117NM 2005 12 19 USAA051522 120051213A5510 BUSHING BOEING737 7374B7 1384702NM HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 FOUND CORROSION R8 LUG FWD AND AFT FACES OF BUSHING. REMOVED DAMAGE, FABRICATED AND INSTALLED NEW BUSHING IAW SRM 55-10-10, DEFECT SIZE: .250 DIA SPOTS OF CORROSION. 2L72 4F RTA16WE 20051219001202005121900120NM 2005 12 19 QXEA200501779 120051213A3097 WIRE BOMBDRDHC8 DHC8402 1390042NM PROP HEAT FAILED A QXEAA UNSCHED LANDING J WARNING INDICATION TXTAXI/GRND HDL 1 NM09401QX 4031 SEA FLT NR 2348, DEPARTING SEA, PROP DEICE CAUTION LIGHT ILLUMINATED WHEN NR 2 PROPS WERE HEATED. CAUTION LIGHT WOULD CYCLE OFF AFTER BLADES WERE NO LONGER HEATED AND CAUTION LIGHT WOULD RETURN WITH EACH SUBSEQUENT CYCLE OF PROP HEAT. FLT DIVERTED TO GEG. MX INTERROGATED CDS, FOUND PHASE C OPEN HEATER, NR 2 TMCU. CLEARED NVM. C/W DH8-400-SL-31-001R14. GROUND RAN IAW FUNCTIONAL TEST 30-61-00-720-801. PROP DEICE SYSTEM CHECKED GOOD. PERFORMED GVI OF PROP LEADS (NR 2 PROP) AND R/R`D LEAD ON NR 1 BLADE DUE TO APPEARANCE OF BEING CRIMPED AND INTERMITTENT INDICATION OF AND OPEN WITH VOM. RECHECKED IAW AMM 30-61-00-720-801. NO DEFECTS NOTED. NO FAULT MESSAGES IN CDS. A/C RETURNED TO SERVICE. 2H72 4T RTA13NM 20051219001232005121900123WP 2005 12 19 ABXA050343 120051031A5330 SKIN DOUG DC8 DC863F 302198FWP BS 854 MISDRILLED A ABXAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL23826AX 46061 FOUND UPPER CARGO STA 834, BUTT LINE 0, 4 FASTENERS MIS-DRILLED IN TOP OF CENTER WING SKIN ON TANK. MIS-DRILLED HOLES CLEANED UP, HOLES OPENED UP TO 0.312" AND 0.308", FASTENERS INSTALLED IAW DC8 SRM 51-1-20 ON SPLICE DOUBLER INSTALLATION. 2L74 4F 4A25 20051219001252005121900125WP 2005 12 19 ABXA050347 120051011A5320 SUPPORT FITTING DOUG DC8 DC863F 302198FWP BS 940 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 SUPPORT FITTING WAS CRACKED ON LONGERON 24 RIGHT IN RIGHT MAIN LANDING GEAR WHEEL WELL AT APPROXIMATELY STA 940. REMOVED SUPPORT FITTING BRACKET ON LONGERON 24 STA 940 RIGHT MAIN LANDING GEAR, NEW BRACKET FABRICATED BY OUTSIDE VENDOR, REF REA D853-52521, PO NR 1122790, DRILLED AND TRIMMED FABRICATED PART IAW REA D853-52521, STEP NR 5, INSTALLED SUPPORT FITTING BRACKET ON LONGERON 24, STA 940 RIGHT MAIN LANDING GEAR IAW DC8 SRM 51-1-20D. 2L74 4F 4A25 20051219001262005121900126WP 2005 12 19 ABXA050346 120051102A5315 FLOORBEAM DOUG DC8 DC863F 302198FWP BS 120 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 FOUND MAIN CABIN FLOORBEAM AT STA 120, RIGHT BUTT LINE 51, FORWARD SIDE OF T CAP, CORRODED. REMOVED DAMAGED AREA AND REPLACED WITH ANGLE DOUBLER REPAIR ON FLOORBEAM STA 120, RIGHT BUTT LINE 51 IAW DC8 SRM 51-1-8, 53-2-0, 51-3-0, 53-7-3, 53-0, 51-2-0, 51-1-8, 51-3-1 AND ABX SRM 93-01-14. 2L74 4F 4A25 20051219001272005121900127WP 2005 12 19 ABXA050351 120051020A5315 FLOORBEAM DOUG DC8 DC863F 302198FWP BS 680 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 FOUND MAIN CABIN, STA 680, RIGHT BUTT LINE 26, LOWER SIDE OF FLOORBEAM CORRODED. REMOVED CORROSION IAW DC8 SRM 51-1-8, ORIGINAL MATERIAL THICKNESS 0.178", REMAINING THICKNESS 0.107" AND OUT OF LIMITS IAW DC8 SRM 53-2-0. VERIFIED REPAIR AINGLE AS AND10134-1407 PO NR 1122486. FABRICATED, LOCATED, AND DRILLED REPAIR PARTS IAW ABX DWG K04881. PRECOATED ALL BARE METAL IAW LWR NR 200302015, AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-20D AND ABX DWG K04881. 2L74 4F 4A25 20051219001292005121900129WP 2005 12 19 ABXA050353 120051025A5312 BULKHEAD DOUG DC8 DC863F 302198FWP BS 980 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 FOUND CORROSION ON RIGHT WHEEL WELL, STA 980, LONGERON 24 RIGHT, AFT BULKHEAD UNDER LOWER SIDE OF DIAGONAL FRAME. REMOVED BRACKET AT STA 980 IAW DC8 SRM 51-3-0, 51-1-S0D. REMOVED CORROSION IAW DC8 SRM 53-2-0. ORIGINAL MATERIAL MEASURED .047" AND .046", OUT OF LIMITS 27 PERCENT AND 25 PERCENT IAW DOUGLAS NDT SRM. FABRICATED FILLERS AND DOUBLER 7075-T6 0.063" PO NR 1118787 IAW DC8 SRM 53-2-0, FIG 1D. TREATED AND PRIMED FABRICATED PARTS IAW DC8 SRM 51-1-8, INSTALLED DOUBLER, FILLERS, AND BRACKET AT STA 980 IAW DC8 SRM 53-2-0, FIG. 1D. 2L74 4F 4A25 20051219001312005121900131EA 2005 12 19 ASOA05982 120051115A3350BR9279232 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN DAMAGED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27842AS 7304 DURING A HANGAR INSPECTION IN BTR, THE EMERGENCY LIGHT ON THE FLIGHT ATTENDANTS CABINET WAS FOUND TO BE DAMAGED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY, ON THE FLIGHT ATTENDANTS CABINET. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051219001322005121900132EU 2005 12 19 SA05125 120051209A335032145410 POWER SUPPLY AIRBUS320 A320214 3930316EU EMERGENCY LIGHT FAULTY A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19111US14479 1114 CLT - THE EMERGENCY EXIT LIGHTS IN THE CABIN FLICKER WITH BOTH ENGINE GENERATORS ON. ALSO, THE MID CABIN CEILING LIGHT WAS INOPERATIVE WITH THE LIGHT SWITCH TO ON. MAINTENANCE REPLACED THE FORWARD EMERGENCY POWER SUPPLY UNIT AND BATTERY PACK. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20051219001332005121900133EU 2005 12 19 SA05126 120051209A335032145410 EPSU AIRBUS320 A320214 3930316EU EMERGENCY LIGHT FAULTY A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19111US14479 1114 CLT - THE EMERGENCY EXIT LIGHTS IN THE CABIN FLICKER WITH BOTH ENGINE GENERATORS ON. ALSO, THE MID CABIN CEILING LIGHT WAS INOPERATIVE WITH THE LIGHT SWITCH TO ON. MAINTENANCE REPLACED THE LEFT MID CABIN EMERGENCY POWER SUPPLY UNIT AND BATTERY PACK. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20051219001352005121900135WP 2005 12 19 IXXA0500129S 120050214A5210 SKIN DOUG DC8 DC871F 302199DWP BS1400 30R-31R WORN A IXXAK NONE O OTHER ININSP/MAINT 1 SW11821BX858952998 45811 DURING A ROUTINE C CHECK INSPECTION, RT FUSELAGE AFT CENTER SECTION AFT CARGO COMPARTMENT AFT DOOR FWD JAMB WEAR DAMAGE AT STA FS 1400.00, L-30R TO L-31R. MAJOR REPAIR ACCOMPLISHED REMOVAL OF FASTENERS. REMOVED DAMAGED SECTION. PERFORMED NDT INSPECTION. FABRICATED EXTERNAL REPAIR DOUBLER + FILLER. CLEANED, TREATED AND PRIMED AREA + REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES INSTALLED REPAIR PARTS IAW SEMAN DRAWING ED-3827 AND FAA FORM 8110-3 NR 05055, DC8 SRM 51-1-411, 51-1-21, 51-1-22, 51-1-26, 51-3-1. 2L74 4F RT4A25 20051219001382005121900138NM 2005 12 19 AWXA200501497 120051117A531565C10592156 FLOORBEAM BOEING737 73733A 1384673NM BS 961 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 MCN - DURING C19 CHECK DISCOVERED CORROSION ON THE FLOOR SUPPORT ASSEMBLY AT BS 961, BL 36R TO BL 35R AND WL 208. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-51A1 FIG 101. MAINTENANCE REMOVED AND INSTALLED NEW FLOOR SUPPORT ASSEMBLY AT BS 961, BL 26R TO BL 35R, AND WL 208 IAW BOEING 737-300 SRM 51-40-02-0G FIG 12. 2L72 4F RTA16WE 20051219001432005121900143NM 2005 12 19 AWXA200501502 120051117A531565C10592155 FLOORBEAM BOEING737 73733A 1384673NM BS 957 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 MCN - DURING C19 DISCOVERED CORROSION ON FLOOR SUPPORT AT BS 957, BL 24R AND WL 208. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-51-1A1 FIG 101. MAINTENANCE REMOVED AND INSTALLED NEW FLOOR SUPPORT AT BS 957, BL 24R AND WL 208 IAW BOEING 737-300 SRM 51-40-02-0G FIG 12. 2L72 4F RTA16WE 20051219001442005121900144NM 2005 12 19 AWXA200501503 120051117A531565C10592153 FLOORBEAM BOEING737 73733A 1384673NM BS 961 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 MCN - DURING C19 DISCOVERED CORROSION ON FLOOR SUPPORT AT BS 961, BL 10R TO BL 17R AND WL 208. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-51-1A1 FIG 101. MAINTENANCE REMOVED AND INSTALLED NEW FLOOR SUPPORT AT BS 961, BL 10R TO 17R AND WL 208 IAW BOEING 737-300 SRM 51-40-02-0G FIG 12. 2L72 4F RTA16WE 20051219001452005121900145NM 2005 12 19 AWXA200501504 120051117A53156546568122 FLOORBEAM BOEING737 73733A 1384673NM BS 1016 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 MCN - DURING C19 CHECK DISCOVERED CORROSION ON TOP OF TCAP ON BEAM BS 1016, BL 6R AND WL 208. FOUND CORROSION TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-560-51-1A-1, CUT OUT DAMAGED AREA IAW BOEING 737-300 SRM 51-10-12-06. FABRICATED ANGLES, FILLER, AND EXTRUSION IAW BOEING 737-300 SRM 51-70-12-0G FIG 1. INSTALLED FABRICATED REPAIR PARTS IAW BOEING 737-300 SRM 53-30-51-2R-2 FIG 201. 2L72 4F RTA16WE 20051219001482005121900148NM 2005 12 19 AWXA200501507 120051118A5320654583340 SHEAR WEB BOEING737 73733A 1384673NM BS 188-196 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 MCN - DURING C19 CHECK DISCOVERED WEB CRACKED, 1.1 INCHES, FROM BS 188 TO BS 196, WL 207 AND BL 30R. MAINTENANCE REMOVED SHEAR WEB IAW BOEING 737-300 SRM 53-10-51-2R8. FABRICATED SHEAR WEB IAW BOEING 737-300 SRM 53-10-51-2R8. INSTALLED FABRICATED REPAIR PARTS FROM BS 188 TO BS 196, WL 207 AND BL 30R IAW BOEING 737-300 SRM 53-10-2R8. 2L72 4F RTA16WE 20051219001522005121900152NM 2005 12 19 AWXA200501509 120051118A531265163007 BULKHEAD BOEING737 73733A 1384673NM BS 178 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 MCN - DURING C19 CHECK DISCOVERED WEB CRACKED, .975 INCHES, AT FASTENER AT BS 178, WL 234 AND BL 10R. MAINTENANCE REMOVED SHEAR WEB IAW BOEING 737-300 SRM 53-10-51-2R8. FABRICATED SHEAR WEB IAW BOEING 737-300 SRM 53-10-51-2R8. INSTALLED FABRICATED REPAIR PARTS FROM BS 178, WL 234 AND BL 10R IAW BOEING 737-300 SRM 53-10-2R8. 2L72 4F RTA16WE 20051219001552005121900155NM 2005 12 19 USAA051517 120051213A5510 BUSHING BOEING737 7374B7 1384702NM HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 FOUND CORROSION L3 CLEVIS AFT FACE OF BUSHING. REMOVED DAMAGE, FABRICATED AND INSTALLED NEW BUSHING IAW SRM 55-10-10, DEFECT SIZE: .250 DIA SPOTS OF CORROSION. 2L72 4F RTA16WE 20051219001562005121900156NM 2005 12 19 USAA051516 120051213A5510 BUSHING BOEING737 7374B7 1384702NM HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 FOUND CORROSION L4 CLEVIS FWD FACE OF BUSHING. REMOVED DAMAGE, FABRICATED AND INSTALLED NEW BUSHING IAW 55-10-10. DEFECT SIZE: .250 DIA SPOTS OF CORROSION. 2L72 4F RTA16WE 20051219001572005121900157NM 2005 12 19 USAA051515 120051213A5510 BUSHING BOEING737 7374B7 1384702NM HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 FOUND CORROSION L1 CLEVIS. REMOVED DAMAGE, FABRICATED AND INSTALLED NEW BUSHING IAW SRM 55-10-10, DEFECT SIZE: .250 SPOTS OF CORROSION. 2L72 4F RTA16WE 20051219001592005121900159NM 2005 12 19 USAA051523 120051213A5510 BUSHING BOEING737 7374B7 1384702NM HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 FOUND CORROSION R4 CLEVIS FWD FACE BUSHING. REMOVED DAMAGE, FABRICATED AND INSTALLED NEW BUSHING IAW SRM 55-10-10, DEFECT SIZE: .250 SPOTS OF CORROSION. 2L72 4F RTA16WE 20051219001602005121900160EU 2005 12 19 USAA051539 120051213A5320D5347112420000 SHEAR PLATE AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19113UW 1141 FOUND OVAL CORROSION TOP OF SHEAR WEB, BETWEEN C69 & 70 AT Y1200. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-43-00; CORROSION LEVEL 1; TASK JA-260-53500-12, DEFECT SIZE: 2". 2L72 4F RTA28NM 20051219001632005121900163EU 2005 12 19 USAA051546 120051213A5320D5347112420100 SHEAR WEB AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19113UW 1141 FOUND CORROSION RT SHEAR WEB BETWEEN FS 69 AND 70 - Y1200. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-72-00; CORROSION LEVEL 1; TASK JA-260-53500, DEFECT SIZE: 1" DIA. 2L72 4F RTA28NM 20051219001642005121900164EU 2005 12 19 USAA051545 120051213A5315D5347209000200 FLOORBEAM AIRBUS320 A320214 3930316EU FR 66 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19113UW 1141 FOUND CORROSION FS 66 Y765. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-72-11; CORROSION LEVEL 1; TASK JA-260-53500, DEFECT SIZE: 1-1/2" X 1-1/2". 2L72 4F RTA28NM 20051219001662005121900166NM 2005 12 19 DHL2005765510 120051209A5347 SEAT TRACK BOEING727 727264 138408MNM BS 720-720A CORRODED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15765AT 23014 FOUND CABIN SEAT TRACK, BS 720-720A, RBL 45 CORRODED AT FLOOR PANEL ATTACH UPPER FLANGE AND SIDE OF TRACK. REMOVED AND REPLACED SEAT TRACK FROM STA 690 TO 720D RBL 45 WITH FABRICATED REPAIR SEAT TRACK 110-1/2" FROM BAC1520-792 7178T6 AND INSTALLED IAW B727 SRM 53-10-5 FIG 7. 2L73 4F A3WE 20051219001672005121900167NM 2005 12 19 DHL2005765503 120051212A5320 CHANNEL BOEING727 727264 138408MNM BS 1030-1040 CORRODED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15765AT 23014 AFT CARGO PIT CORROSION ON LOWER SIDE AFT OF FLOOR SUPPORT Z-ANGLE AT BS 1030-1040, RBL 4 CHANNEL CORRODED. REMOVED SECTION OF FLOOR SUPPORT STA 1030 TO 1083 RBL 4. FABRICATED AND INSTALLED CHANNEL 52-5/8" FROM BAC1509-100146, L-ANGLE 12-3/8" BY 7/8" FROM AND 10133-0702, AND L-ANGLE 10-3/4" FROM BAC1490-2583 IAW B727 SRM 53-10-5 FIG 4. 2L73 4F A3WE 20051219001712005121900171NM 2005 12 19 DHL2005765502 120051215A5320 CHANNEL BOEING727 727264 138408MNM BS 950F CORRODED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15765AT 23014 AFT CARGO PIT FLOOR SUPPORT CHANNEL IS CRACKED BEYOND STOP DRILL HOLES (6" FWD OF STA 950F, RBL 4). REMOVED FLOOR SUPPORT IAW B727 SRM 51-30-2. FABRICATED AND INSTALLED FLOOR SUPPORT CHANNEL 5'8" FROM BAC1500-6199 IAW B727 SRM 51-30-2, 51-10-2. 2L73 4F A3WE 20051219001722005121900172NM 2005 12 19 AWXA200501519 120051215A2130756A000005 CONDENSER AIRBUSA319 A319132 3930340NM NR 1 FAILED A AWXAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 WP28827AW2428 2428 1547 CREW REPORTED THAT THE NR 1 PACK WOULD NOT HOLD CABIN PRESSURE WHILE EN ROUTE TO LAS AT FL 270 CABIN CLIMBED TO 9650 FL. CREW PERFORMED EMERGENCY DESCENT TO 10,000 FLT. AT 10,000 FLT CABIN ALT WAS 5500FT. AIRCRAFT LANDED IN LAS WITHOUT FURTHER INCIDENT. MX R & R NR 1 PACK CONDENSER DUE TO FAILURE IAW AIRBUS MM 21-52-32. OPS CHK OK. VENDOR CONFIRMS FAILURE. FOUND A BLOWN PAN ON UNIT. UNIT WAS CLEANED, RECORED AND PASSED ALL TESTS. REPAIRS WERE ACCOMPLISHED IAW OHM/CMM 21-52-10 REV.6. 2L72 4F RTA28NM 20051219001732005121900173EU 2005 12 19 AWXA200501520 120051213A2560P4010021000 BATTERY AIRBUS320 A320231 3930325EU FLASHLIGHT INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28622AW 054 DTW - EEL - DURING INSPECTION DISCOVERED THE FORWARD F/A JUMSEAT INBOARD EMERGENCY FLASHLIGHT BATTERY DEAD. MAINTENANCE REMOVED AND REPLACED THE FORWARD F/A FLASHLIGHT BATTERY PACK IAW AIRBUS 320 MM 25-65-52. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA28NM 20051219001742005121900174NM 2005 12 19 AWXA200501521 120051214A3810288231 COMPRESSOR BOEING757 757225 1384959NM POTABLE WATER ODOR A AWXAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP28913AW10158988 22207 PHX - AIR TURN BACK - FLT 0542 - CREW REPORTED THAT DURING CLIMBING OUT AT 7000 FT, FLIGHT ATTENDANTS REPORTED A BURNING ELECTRICAL SMELL THROUGHOUT CABIN. CREW ACCOMPLISHED ODOR REMOVAL CHECKLIST AND RETURNED TO PHX, LANDING WITHOUT FURTHER EVENT. MAINTENANCE DETERMINED THAT THE POTABLE WATER AIR COMPRESSOR WAS THE CAUSE OF ODOR. REMOVED AND REPLACED THE POTABLE WATER AIR COMPRESSOR IAW BOEING 757-200 MM 38-15-01-F. OPERATIONAL CHECKS WERE GOOD. VENDOR CONFIRMED FAILURE. FAILED PRE-TEST, THERMAL PROTECTOR INOP AND SHROUD DAMAGED. THE UNIT WAS REPAIRED AND TESTED IAW CMM 38-15-11 REV.10 2L72 4F RTA2NM 20051219001752005121900175NM 2005 12 19 AWXA200501522 120051215A3397BR963180 WIRE HARNESS BOEING757 7572G7 1384963NM EMERGENCY LIGHT INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28909AW 24522 PHX - EEL - DURING INSPECTION DISCOVERED ROW 15 ABC EMERGENCY ESCAPE PATH LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE SEAT HARNESS AT ROW 15 ABC. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA2NM 20051219001822005121900182NM 2005 12 19 SWAA053944 120051212A53156546811 FLOORBEAM BOEING737 7375H4 138449DNM BS 987 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29511SW 24188 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 987, BETWEEN RBL 46.5 TO LBL 46.5. REMOVED AND REPLACED FLOORBEAM UPPER CAP PER SRM. 2L72 4F RTA16WE 20051219001842005121900184NM 2005 12 19 SWAA053946 120051212A53306545768 SKIN BOEING737 7375H4 138449DNM BS 320 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29511SW 24188 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 320, R1 DOOR CUTOUT, AFT LOWER CORNER. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051219001862005121900186NM 2005 12 19 SWAA053948 120051212A3350311500 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29735SA 27867 DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY LIGHT LENS LOOSE AT ROW 13 DEF. SECURED LENS PER MM. 2L72 4F RTA16WE 20051219001872005121900187NM 2005 12 19 SWAA053949 120051208A53306545774 SKIN BOEING737 737317 138447PNM BS 734 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29661SW 23173 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 734, STR 27R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051219001892005121900189EA 2005 12 19 VNAA0511017 120051117A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE SCRATCHED A VNAAK NONE O OTHER ININSP/MAINT 1 GL05237PS 7906 AFTER LANDING THE CREW REPORTED A SCRATCH ON THE FUSELAGE BELOW THE CARGO DOOR. MAINTENANCE INSPECTED AND FOUND THE DAMAGE TO BE BEYOND ALLOWABLE LIMITS. THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE PERFORMED A TEMPORARY REPAIR IAW BOMBARDIER REO 601R-53-61-1579. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20051219001902005121900190EA 2005 12 19 VNAA0511021 120051122A5270 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR ILLUMINATED A VNAAO OTHER N FALSE WARNING CRCRUISE 1 GL05251PS 7931 DURING CRUISE THE PASSENGER DOOR WARNING MESSAGE ILLUMINATED. THE CREW FOLLOWED THE QRH AND MADE AN UNEVENTFUL LANDING AT DESTINATION. MAINTENANCE INSPECTED THE PASSENGER DOOR LATCHING AND WARNING SYSTEMS. NO DISCREPANCIES WERE FOUND AND THE PROBLEM COULD NOT BE DUPLICATED. THE SYSTEMS OPERATIONALLY CHECKED GOOD AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20051219001922005121900192EA 2005 12 19 VNAA0511020 120051122A3020GG670800025 SHUTOFF VALVE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE RT ANTI ICE SYS FAILED A VNAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL05703PS3981 10137 THE RIGHT COWL ANTI-ICE CAUTION MESSAGE ILLUMINATED WHEN RIGHT COWL ANTI-ICE WAS SELECTED. THE CREW FOLLOWED THE QRH AND RETURNED TO CLT. MAINTENANCE REMOVED & REPLACED THE RIGHT PRESSURE REGULATING & SHUTOFF VALVE. THE SYSTEM OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20051219001942005121900194EA 2005 12 19 VNAA0511022 120051124A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A VNAAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL05202PS 7858 THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED WITH FLAPS AT 8 DEGREES. THE CREW FOLLOWED THE QRH AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET AND OPERATIONALLY CHECKED THE FLAP SYSTEM. ALL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20051219001972005121900197NM 2005 12 19 SWAA053972 120051214A335007912 COVER BOEING737 7377H4 1384404NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29435WN 32455 EEPLS TRACK COVER BROKEN. REMOVED AND REPLACED COVER PER MM. 2L72 4F RTA16WE 20051219002002005121900200EA 2005 12 19 VNAA0511013 120051114A274170609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE HORIZONTAL STAB FAILED A VNAAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 GL05228PS4074 7897 THE STAB TRIM FAILED IN FLIGHT. THE CREW FOLLOWED THE QRH AND MADE AN UNEVENTFUL LANDING. MAINTENANCE REMOVED & REPLACED THE HORIZONTAL STAB TRIM CONTROL UNIT IAW CRJ200 AMM 24-41-01-000(400)-801. THE STAB TRIM OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20051219002032005121900203EA 2005 12 19 VNAA0511015 120051115A2600601R593201 THERMAL SWITCH CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT WING MALFUNCTIONED A VNAAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL05216PS 7882 THE ANTI-ICE DUCT WARNING MESSAGE ILLUMINATED WITH THE ANTI-ICE SYNOPTIC PAGE INDICATING A LEFT WING FAULT. THE CREW FOLLOWED THE QRH AND MADE AN UNEVENTFUL LANDING. THE AIRCRAFT WAS FERRIED TO DAY. MAINTENANCE TROUBLESHOT THE SYSTEM AND FOUND NO DISCREPANCIES. PER BOMBARDIER TECHNICAL SERVICES RECOMMENDATION MAINTENANCE REMOVED AND REPLACED 21 THERMAL SWITCHES IN THE LEFT WING LEADING EDGE IAW CRJ200 AMM 36-21-07-000(400)-801. THE SYSTEM LEAK AND OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20051219002092005121900209NM 2005 12 19 SWAA053977 120051215A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 867 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29622SW 27932 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 867, STR 4L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051219002112005121900211NM 2005 12 19 SWAA053979 120051215A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM BS 867 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29622SW 27932 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 867, STR 4L. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20051219002122005121900212SO 2005 12 19 CHQA200500209 120051211A2611FDS765A2 SMOKE DETECTOR EMB 145 EMB145LR 3260212SO LAVATORY INOPERATIVE A CHQAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL11570RP 14500821 FLIGHT 6378 CMH-RSW RECEIVED LAV SMOKE EICAS WARNING ABOUT 700 FT AGL AFTER TAKEOFF. DECLARED EMERGENCY, COMPLIED WITH QRH PROCEDURES. FLIGHT ATTENDANT REPORTED AN ODOR IN THE CABIN AND A LITTLE HAZE, BUT NO VISIBLE SMOKE. HAZE CLEARED AFTER 2-3 MINUTES. RETURNED FOR ILS 28L LANDING IN CMH. MAINTENANCE REMOVED AND REPLACED THE LAVATORY SMOKE DETECTOR AND THE SMOKE DETECTOR PANEL. PERFORMED TEST FLIGHT. NO DISCREPANCIES NOTED. 2L72 4T RTT00011AT 20051219002142005121900214SO 2005 12 19 CHQA200500211 120051211A2611 SMOKE DETECTOR EMB 145 EMB145LR 3260212SO LAVATORY MALFUNCTIONED A CHQAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL11570RP 14500821 FLIGHT 6429 TPA-FLL AT 500 FEET, LAVATORY SMOKE EICAS WARNING MESSAGE APPEARED. FLIGHT ATTENDANT REPORTED LAVATORY SMOKE DETECTOR SOUNDING AND ALARM. NO VISIBLE SMOKE. RAN QRH. STILL NO VISIBLE SMOKE NOTED FROM FLIGHT ATTENDANT. RETURNED TO LAND IN TPA. MAINTENANCE UNABLE TO DUPLICATE FAULT. PERFORMED LAVATORY SMOKE DETECTION SYSTEM TEST IAW EMB 145 MM 26-14-00-700-801-A. OPS CHECK GOOD. 2L72 4T RTT00011AT 20051219002152005121900215NM 2005 12 19 SWAA053980 120051214A335065C27095 BATTERY PACK BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29639SW 27712 DURING SCHEDULED RON CHECK, FOUND R2 DOOR EXTERIOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20051219002162005121900216NM 2005 12 19 SWAA053981 120051214A3350BR2013 LIGHT BOEING737 737317 138447PNM ROW 8 ABC LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 EEPLS TRACK LOOSE AT ROW 8 ABC. SECURED EEPLS PER MM. 2L72 4F RTA16WE 20051219002192005121900219NM 2005 12 19 SWAA053984 120051214A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29784SW 29810 DURING SCHEDULED HC2 CHECK, FOUND EEPLS STRIP WORN AT ROW 7 DEF. REMOVED AND REPLACED EEPLS STRIP PER MM. 2L72 4F RTA16WE 20051219002202005121900220NM 2005 12 19 SWAA053970 120051215A575465C26602 SKIN BOEING737 7373H4 1384600NM NR 5 SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED C4 CHECK, FOUND NR 5 L/E SLAT UPPER WEDGE SKIN DELAMINATED AT OUTBOARD END. REPAIRED SLAT PER SRM. 2L72 4F RTA16WE 20051219002212005121900221NM 2005 12 19 SWAA053971 120051214A335007912 COVER BOEING737 7377H4 1384404NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29427WN 29831 EEPLS TRACK COVER LOOSE AT FWD END. SECURED COVER PER MM. 2L72 4F RTA16WE 20051219002222005121900222WP 2005 12 19 05FDEA04321 120051215A5300 REPAIR DOUG DC10 DC1010 3022110WP BS 1511-1520 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568054 47808 EXTERNAL DOUBLER REPAIR FROM STA 1511 TO STA 1520 BETWEEN LONG 52 AND 51 LT. PERFORMED A INSPECTION OF REPAIR IAW SRM 53-40-00 FIG 20 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P1. 2L73 4F A22WE 20051214000132005121400013NM 2005 12 14 USAA200512001 120051201A5330 SKIN BOEING737 737401 1384701NM BS 980-990 WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19418US 23985 SKIN WEAR .036 INCH DEEP, 10 INCH LONG AT STA 980-990 BETWEEN S2R AND S3R (UNDER DORSAL FIN). INSTALLED DOUBLER, TRIPLER AND FILLERS IAW SRM 53-60-01 (REPAIR 9) AND EA 97162. 2L72 4F RTA16WE 20051214000152005121400015NM 2005 12 14 USAA200512003 120051201A5330 SKIN BOEING737 737401 1384701NM BS 980 WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19424US 23991 .015"DEEP WEAR 3" LONG AT STA 980 (ON PREVIOUS REPAIR DOUBLER). REPAIR: INSTALLED DOUBLER AND TRIPLER PER EA 97175 2L72 4F RTA16WE 20051214000222005121400022EA 2005 12 14 COMA0560701 120051209A2752853D10019 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS UNRELIABLE A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01713CA3868 7245 FLIGHT 5653 - FLAPS FAIL CAUTION. REPLACED THE LT FLAP ACTUATOR. 2L72 4F RTA21EA 20051214000242005121400024EA 2005 12 14 COMA0560698 120051208A27501104SD100501 COUPLING CNDAIRCL600 CL6002B19 1900309EA NR 5 FLAP DAMAGED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01709CA 7238 FLIGHT 4989 - FLAPS FAIL CAUTION. REPLACED THE NR 5 FLEX SHAFT. 2L72 4F RTA21EA 20051215000132005121500013NM 2005 12 15 SWAA053928 120051212A531265C28106 STIFFENER BOEING737 7375H4 138449DNM BS 1016 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29511SW 24188 DURING SCHEDULED 1/2D CHECK, FOUND BS 1016 AFT PRESSURE BULKHEAD CHANNEL STIFFENER CORRODED AT BL 0. REPAIRED CHANNEL STIFFENER PER ACO & SRM. 2L72 4F RTA16WE 20051215000202005121500020 2005 12 15 COMA0560688 420051206A34216229336400 COMPUTER CNDAIRCL600 CL6002B19 1900309EA DG MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01809CA275686548 7366 FLIGHT 5005 - PILOT AND CO-PILOT DG WHITE FLAG AND UNRELIABLE. REPLACED THE NR 1 AHC. 2L72 4F RTA21EA 20051215000212005121500021EA 2005 12 15 QXEA200501768 120051211A3320 SWITCH CNDAIRCL600 CL6002C10 1390015EA CABIN LIGHTS SHORTED A QXEAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM09602QX 10010 DEN - ON FLIGHT 4191, SPARKING & SHORT CIRCUIT AT THE LEFT HAND UTILITY CLOSET SWITCH. CIRCUIT BREAKER TRIPPED. MAINTENANCE PLACED SYSTEM ON MEL 33-21-1. COLLARED CIRCUIT BREAKER P4 ON CIRCUIT BREAKER PANEL 1. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20051215000232005121500023EA 2005 12 15 COMA0560690 120051206A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS WARNING LIGHT A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01446CA 7546 FLIGHT 5253 - FLAPS FAIL CAUTION. INSPECTED FLAPS PER AD 98-20-01 AND DEFERRED MAINTENANCE. 2L72 4F RTA21EA 20051215000312005121500031EA 2005 12 15 COMA0560700 120051209A323316520101 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01967CA241274941 7134 FLIGHT 5462 - GEAR DISAGREE WARNING. REPLACED THE NLG RETRACT ACTUATOR. 2L72 4F RTA21EA 20051215000322005121500032EA 2005 12 15 COMA0560703 120051210A3230601R751461 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01967CA2539674 7134 FLIGHT 5116 - GEAR DISAGREE WARNING. REPLACED THE NLG SELECTOR VALVE. 2L72 4F RTA21EA 20051215000352005121500035EA 2005 12 15 QXEA200501690 120051031A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 381-662 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, RIGHT OUTBOARD SEAT RAIL HAS SCRATCHES GOUGES AND CHAFING AT STATION 381-662. REPAIRED IAW REO 670-53-00-013. 2L72 4F RTA21EA 20051215000372005121500037EA 2005 12 15 QXEA200501692 120051031A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 458-481 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, RIGHT OUTBOARD SEAT RAIL HAS SCRATCHES CHAFING AND GOUGES AT STATION 458-481. REPAIRED IAW REO 670-53-00-013. 2L72 4F RTA21EA 20051215000402005121500040EA 2005 12 15 QXEA200501699 120051031A5410CN6242130201 STRIKER CNDAIRCL600 CL6002C10 1390015EA RT NACELLE DOOR WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, RIGHT ENGINE LOWER TRANSITION COWLING LATCH COVER DOOR REBATES AND STRIKER PLATE WORN. LATCH BEARING PADS REPLACED (2 EA) IAW CRJ-700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20051215000512005121500051EA 2005 12 15 COMA0560691 120051207A2130 VALVE CNDAIRCL600 CL6002B19 1900309EA CABIN PRESSURE OBSTRUCTED A COMAA UNSCHED LANDING C F.O.D. CRCRUISE 1 SO01954CA 7100 FLIGHT 5850 - RAPID DEPRESSURIZATION. FOUND INSULATION BLANKET SUCKED INTO OUT FLOW VALVE. SECURED INSULATION AND OPERATIONAL CHECK OF PRESS SYSTEM NORMAL. 2L72 4F RTA21EA 20051215000522005121500052EA 2005 12 15 QXEA200501767 120051210A2420 GENERATOR CNDAIRCL600 CL6002C10 1390015EA NR 1 WARNING LIGHT A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09605QX 10022 DEN - ON PUSHBACK FOR FLIGHT 4327, RECEIVED A NR 1 GENERATOR OFF CAUTION MESSAGE. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE PLACED THE SYSTEM ON MEL 24-11-1B. AIRCRAFT RETURNED TO SERVICE. IN BOI MAINTENANCE REPLACED THE NR 1 IDG WITH NO HELP, ALSO THE NR 1 GCU WITH NO HELP. MEL CONTINUED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20051215000532005121500053NM 2005 12 15 QXEA200501770 120051211A6123 AUTOFEATHER SYS BOMBDRDHC8 DHC8402 1390042NM PROPELLER MALFUNCTIONED A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09411QX 4055 PDX FLIGHT 2308: AUTO FEATHER WOULD NOT ARM ON TAXI. OPS CHECK OK WHILE A/C IS STATIC. MAINTENANCE UPON INSPECTION FOUND NO FAULTS IN CDS. POWER DOWN A/C AND REINITIALIZED A/C. PERFORMED OPS TEST OF AUTO FEATHER SYSTEM IN BOTH MODES WITHOUT ENGINES RUNNING AND WITH ENGINES RUNNING. OPS TESTED GOOD IAW AMM TASK 61-20-00-710-801. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051215000662005121500066EA 2005 12 15 QXEA200501682 120051031A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 850-953 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, LEFT INBOARD SEAT RAIL AT STATION 850-953 HAS CORROSION AND GOUGES. REPAIRED IAW REO 670-53-00-013. 2L72 4F RTA21EA 20051215000722005121500072EA 2005 12 15 QXEA200501677 120051031A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 581-683 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 YYC - DURING C3 CHECK, RIGHT INBOARD SEAT RAIL AT STATION 581-683 HAS CORROSION ON TOP SURFACE. REMOVED CORROSION IAW REO 670-53-00-013. 2L72 4F RTA21EA 20051215000772005121500077NM 2005 12 15 QXEA200501752 120051120A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX - NR 4 SEAT TRACK HAS DEEP CORROSION ON LEFTHAND FLANGE AT X240. REPLACED SEAT TRACK IAW DHC-8-200 SRM 51-40-00 AND RD 8-53-1102, RD 8-53-4473. 2H72 4T RTA13NM 20051215000832005121500083NM 2005 12 15 QXEA200501757 120051128A5753 FLAP TRACK DHAV DHC8 DHC8202 2809007NM RT WING DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX - RIGHTHAND WING NR 2 FLAP TRACK UPPER SURFACE OF LOWER TRACK HAS DIVOT, 8 INCHES FROM FORWARD END. REPAIRED IAW RD 8-57-986. 2H72 4T RTA13NM 20051215000882005121500088NM 2005 12 15 QXEA200501763 120051126A5753 FASTENER DHAV DHC8 DHC8202 2809007NM FLAP TRACK DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX - LEFTHAND WING NR 4 FLAP TRACK INBOARD SIDE OF FLAP TRACK HAS EIGHT FASTENER COLLARS THAT HAVE BEEN BLENDED ON. REPLACED IAW DHC-8-202 SRM 51-40-00 AND RD 8-51-102. 2H72 4T RTA13NM 20051215000892005121500089NM 2005 12 15 QXEA200501764 120051118A7120 SUPPORT TUBE DHAV DHC8 DHC8202 2809007NM NR 2 NACELLE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09374PH 528 PDX - NR 2 ENGINE LOWER OUTBOARD SUPPORT TUBE IS CHAFED IN MULTIPLE SPOTS AT APPROXIMATELY MID POINT. REPAIRED IAW HORIZON AIR EA 2-54-246 AND RD 8-54-2086. 2H72 4T RTA13NM 20051215000902005121500090NM 2005 12 15 SCNA05017 120051209A2620 WARNING LIGHT BOEING737 7378Q8 13844BXNM CARGO DISCHARGE FALSE ACTIVATIONA SCNAO OTHER N FALSE WARNING CLCLIMB 1 GL15801SY 30332 AFTER TAKEOFF TO RSW, CARGO DISCHARGE LIGHT ILLUMINATED FOR 1 HOUR, THEN WENT OUT. MAINTENANCE ACCOMPLISHED FIM TASK 26-23 TASK 802, NO DISCREPANCIES FOUND. SYSTEM CHECKS NORMAL. 2L72 4F RTA16WE 20051215000922005121500092CE 2005 12 15 DEBA401PP1 120051119A5700 UNKNOWN RAYTHN390 390 7150030CE UNKNOWN UNKNOWN E DEBAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 CE03401PP185 RB130 AIRCRAFT WOULD NOT PASS THE BIT CHECK ON PREFLIGHT. CONTACTED NEAREST AUTHORIZED RAYTHEON SERVICE CENTER FOR SERVICE OF THE NITROGEN BOTTLE, BOTTLE WAS JUST AT THE BOTTOM OF THE GREEN. THE THOUGHT WAS THAT IT CAUSED A LOW PRESSURE INDICATION AND MADE THE BIT CHECK FAIL. THE PROBLEM THEN WENT AWAY. AIRCRAFT RETURNED TO SUS WITH NO PROBLEM. 17 2 3F RTA00010WI 20051215000972005121500097NM 2005 12 15 DL757050753 120050722A5330143N3420 SKIN BOEING757 757232 1384965NM FUSELAGE DEFORMED A DALAK NONE O OTHER ININSP/MAINT 1 SO27668DN 25141 THE FUSELAGE SKIN AND BEARSTRAP WERE DENTED AT LOWER AFT CORNER OF THE FORWARD CARGO DOORWAY. INSTALLED REPAIR DOUBLERS. 2L72 4F RTA2NM 20051215001002005121500100NM 2005 12 15 DL73S050756 120051202A3350 FUSE RPS1 BOEING737 737247 138448DNM BATTERY CHARGER BLOWN A DALAO OTHER O OTHER TXTAXI/GRND HDL 1 SO27239WA 0483 23187 APPROX 1/3 OF EMERGENCY LIGHTS ARE INOP. FOUND BATTERY CHARGER FUSES BLOWN AT M9026. T/S FOUND EMERGENCY WIRES IN 3 LOCATION SHORTED TO GROUND. REPAIRED WIRING PER M/M. REPLACED BATTERY CHARGERS M9026 AND M1132, EMERGENCY LIGHTING OPS NORMAL. 2L72 4F A16WE 20051215001022005121500102NM 2005 12 15 DL757050758 120051129A5330146N310014 SKIN BOEING757 757232 1384965NM STA 1350 S-1 TOOL DAMAGE A DALAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO27673DL 25978 FUSELAGE/SKIN/SKY RADIO ANTENNA REMOVAL AND REPAIR OF FASTENER HOLES. THE SKY RADIO ANTENNA INSTALLATION WAS REMOVED FROM THE FUSELAGE SKIN LEAVING NUMEROUS DAMAGED FASTENER HOLES. ALL DAMAGED HOLES WERE CUT OUT AND AN EXTERNAL ALUMINUM DOUBLER INSTALLED WITH SOLID ALUMINUM RIVETS. REF ACTS PP B757-53-22369. 2L72 4F RTA2NM 20051215001032005121500103NM 2005 12 15 DL76G050761 120051204A33500201720001 LIGHT BOEING767 767332 1382001NM SEAT 15 A/B DAMAGED A DALAE ENGINE SHUTDOWN O OTHER TXTAXI/GRND HDL 1 SO271613B 32776 FWD EMERGENCY EXIT LIGHT ASSY 15 A/B DAMAGED. REP FWD EMERGENCY LIGHT ASSY AT SEAT 15 A/B, CK GOOD. 2L72 4F RTA1NM 20051215001042005121500104NM 2005 12 15 DL75K050763 120051204A5610141T480119 WINDOW BOEING757 757232 1384965NM COCKPIT CRACKED A DALAA UNSCHED LANDING O OTHER CLCLIMB 1 SO27613DL 22820 CAPT 1L WINDOW CRACKED AT FL 21000 AT 300 KTS. REPLACED CAPT 1L WINDOW AND WINDOW HEAT CONTROLLER. 2L72 4F RTA2NM 20051215001102005121500110EU 2005 12 15 AWXA200501511 120051212A335032145410 POWER SUPPLY AIRBUS320 A320231 3930325EU AFT CABIN INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28620AW1933318416 052 PHX - EEL - DURING INSPECTION DISCOVERED THE AFT THREE ROWS OF SEATS THE EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LEFT AFT POWER SUPPLY. OPERATIONAL TESTS WERE GOOD. VENDOR CONFIRMED FAULT. REPLACED F2 FUSE. UNIT REPAIRED AND TESTED IAW CMM 33-51-12 REV.2 2L72 4F RTA28NM 20051215001112005121500111NM 2005 12 15 AWXA200501512 120051211A335020131A BATTERY BOEING757 7572S7 1384962NM EMERGENCY LIGHTSINOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28902AW 23322 PHX - EEL - DURING INSPECTION DISCOVERED LEFT AFT BULLNOSE EMERGENCY LIGHTS INOPERATIVE AT ROWS 30 AND 34. MAINTENANCE REMOVED AND REPLACED THE AFT LEFT BATTERY PACK IAW BOEING 757 MM 39-50. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA2NM 20051215001252005121500125NM 2005 12 15 2005UALA01406 120051205A5230 FRAME BOEING737 737522 138449FNM CARGO DOOR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29921UA 25388 FWD CARGO DOOR CRACKED LWR AFT FRAME. SUPPLEMENTAL DATA UPDATE, MAJOR REPAIR ACP'D PER SRM 51-70-13, REPLACED LWR AFT FRAME SECTION OF DOOR PERIMETER, 2L72 4F RTA16WE 20051215001382005121500138NM 2005 12 15 2005UALA01419 120051209A5311 SPAR BOEING747 747422 1384935NM PWA 4056 PW4056 NE BS 1000 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29174UA 24381 FWD PIT STA 1000 SPAR CHORD CRACK, STR 46-47L, 1.42 INCH AND 46-47R, 0.87 IN. STATION 1000 CHORD CRACK FOUND UNDER EXISTING MAINTENANCE PLAN WRITTEN FOR THIS TYPE OF DAMAGE. REPAIRED PER AMM & FAA-APPROVED SERVICE BULLETIN. 2L74 4F4 FRTA20WE E24NE 20051215001402005121500140NM 2005 12 15 2005UALA01421 120051208A5410 BUSHING BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE NR 1 PYLON MIGRATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29644UA 25094 NR 1 PYLON INBD MIDSPAR FITTING, INBD AND OUTBD LUG BUSHINGS MIGRATED. NR 1 PYLON INBD MIDSPAR FITTING, INBD AND OUTBD LUG BUSHINGS WERE MIGRATED. CAUSE OF BUSHING MIGRATIONS IS UNKNOWN. BUSHINGS WERE REPLACED PER MM 54-53-90. 2L72 4F4 FRTA1NM E24NE 20051215001582005121500158NM 2005 12 15 2005UALA01439 120051211A3397 CONNECTOR BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY EXIT UNSECURE A UALAK NONE O OTHER ININSP/MAINT 1 WP29121UA 29167 FOUND DR 3RH EMERGENCY EXIT SIGN INOP. RESECURED EMERGENCY LIGHT CONNECTOR. 2L74 4F4 FRTA20WE E24NE 20051215001642005121500164NM 2005 12 15 SB05166 120051212A335020131A BATTERY PACK BOEING737 7374B7 1384702NM EMERGENCY LIGHTSDISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19432US 24554 CLT - THE EMERGENCY LIGHTS AT ROWS 14, 16, 18 AND 23 ILLUMINATED BRIEFLY. MAINTENANCE REPLACED THE RIGHT BATTERY PACK. OPERATIONALLY CHECKS OK. 2L72 4F RTA16WE 20051215001772005121500177NM 2005 12 15 USAA051475 120051208A5313 SPLICE BOEING737 737301 1384611NM BS 908 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19591US 23936 FOUND SPLICE CRACKED, BS 908 AT STRINGER 5R. REMOVED AND REPLACED STRINGER SPLICE IAW SRM 50-40-02, DEFECT SIZE: 2" CRACK. 2L72 4F RTA16WE 20051215001812005121500181NM 2005 12 15 USAA051486 120051209A5320 INTERCOSTAL BOEING737 737301 1384611NM STA 967-986 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19591US 23936 FOUND INTERCOSTAL CORRODED BETWEEN STA 967 AND STA 986, LBL 18. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-10-02, DEFECT SIZE: 1/4 INCH SPOTS OF CORROSION ON TOP AND BOTTOM OF NUTPLATE HOLES ON INTERCOSTAL 18" LEN. 2L72 4F RTA16WE 20051215001842005121500184NM 2005 12 15 USAA051489 120051209A5340 ATTACH ANGLE BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19591US 23936 FOUND S15L INTERCOSTAL WEB FWD ATTACH ANGLE AT I/B END IN RADIUS. REMOVED AND REPLACED ANGLE IAW SRM 51-10-02 AND DWG NR 69-16970, DEFECT SIZE: 1/2" CRACK. 2L72 4F RTA16WE 20051215001892005121500189NM 2005 12 15 USAA051509 120051212A5510 ATTACH FITTING BOEING737 7374B7 1384702NM HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 FOUND CORROSION RT HORIZ STAB, FWD FACE OF R5 LUG. SPOT FACED LUG AND INSTALLED NEW BUSHINGS IAW SRM 55-10-10 SRM 52-10-10, DEFECT SIZE: .375". 2L72 4F RTA16WE 20051215001902005121500190NM 2005 12 15 USAA051508 120051212A5510 CLEVIS BOEING737 7374B7 1384702NM HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 FOUND HORIZ STAB CENTER SECTION R7 CLEVIS CORRODED. REMOVED BUSHING REAMED BORE SPOT FACED BOTH FACES INSTALLED NEW BUSHINGS AND SHIMS IAW SRM 55-10-10, DEFECT SIZE: .375". 2L72 4F RTA16WE 20051219000022005121900002NM 2005 12 19 QXEA200501774 120051212A33506104789 BATTERY PACK DHAV DHC8 DHC8202 2809007NM EMERGENCY LIGHT MALFUNCTIONED A QXEAO OTHER O OTHER TXTAXI/GRND HDL 1 NM09351PH10699183 490 PDX - TWO RED LIGHTS IN EMERGENCY PATH LIGHTING INOP AT ROW 1. MAINTENANCE REPLACED BATTERY PAC P55. EMERGENCY LIGHTS OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051219000092005121900009NM 2005 12 19 05FDEA04203 120051209A5330 LAP JOINT BOEING727 727227 1384078NM BS 660 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 FOUND DOUBLER HOLE AT MCD LAP SEAM LOWER ROW BS 660 S27L. REPAIRED PER FED EX EA 7-5330-95993A. 2L73 4F A3WE 20051219000102005121900010NM 2005 12 19 05FDEA04205 120051209A5315 FLOORBEAM BOEING727 727227 1384078NM BS 950D CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 FOUND CORROSION C53-111-01 (3) ON FLOORBEAM LOWER FLANGE BS 950D BBL0-LBL44 WL 201. REPAIRED FLOORBEAM LOWER FLANGE BS 950D, BL 0 LBL 44, WL 201 PER SRM 53-10-8, 51-10- 2. 2L73 4F A3WE 20051219000112005121900011NM 2005 12 19 05FDEA04208 120051209A5315 FLOORBEAM BOEING727 727227 1384078NM BS 587 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 FOUND CARGO FLOORBEAM DENTED AT BS 587 LBL 8 WL 156. REMOVED AND FABRICATED CARGO FLOORBEAM AT BS 565-610, LBL 8, W/L 156 USING BAC1517-1507 PER SRM 51-40-3 AND INSTALLED PER SRM 51-30-2. 2L73 4F A3WE 20051219000372005121900037EA 2005 12 19 SWIA200515986 120051208A2752 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07453SW 7743 ON TAXI IN GOT A "FLAPS FAIL" CAUTION MESSAGE WITH FLAPS AT 25 DEGREES. REPLACED ALL EIGHT FLAP ACTUATORS. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051219000542005121900054NM 2005 12 19 SWAA053908 120051209A5210B227102501 MODULE BOEING737 7373H4 1384600NM COCKPIT DOOR BURNED A SWAAA UNSCHED LANDING O OTHER NRNOT REPORTED 1 SW29351SW 24572 BURNING ODOR IN CABIN ALONG WITH SEVERAL MASTER CAUTION LIGHTS ILLUMINATED. FOUND LOCK FAIL LIGHT ASSY BURNT ON COCKPIT DOOR LOCK MODULE ASSY. REMOVED AND REPLACED COCKPIT DOOR LOCK MODULE ASSY PER MM. 2L72 4F RTA16WE 20051219000592005121900059WP 2005 12 19 IXXA0500130O 120051208A2121X7020256D FAN DOUG DC8 DC862F 3021972WP RECIRCULATION BROKEN A IXXAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW1171CX 67734710 45961 DURING CRUISE FROM VTBU, A SLIGHT BURNING SMELL WAS DETECTED DURING CRUISE WHEN USING LEFT RECIRC FAN. FAN WAS TURNED OFF AND SMELL WENT AWAY. MAINTENANCE REMOVED AND REPLACED THE LT RECIRC FAN IAW ALL APPLICABLE MANUALS. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F 4A25 20051219000722005121900072NM 2005 12 19 SWAA053957 120051214A534065C27314 STRINGER CLIP BOEING737 7375H4 138449DNM BS 663 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29511SW 24188 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051219000752005121900075 2005 12 19 SWAA053960 420051213A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29634SW 27937 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051219000822005121900082NM 2005 12 19 USAA051492 120051212A5312 PRESSURE PANEL BOEING737 7374B7 1384702NM BS 664 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 FOUND CRACK FUSELAGE STATION 664 LBL 30. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED A NEW STIFFENER ANGLE AND SHIMS IAW TR 53-60-04, DEFECT SIZE: 2.3" 2L72 4F RTA16WE 20051219000852005121900085NM 2005 12 19 USAA051497 120051212A5510 CLEVIS BOEING737 7374B7 1384702NM HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 FOUND RT HORIZ STAB R12 CLEVIS BOTH FACES. SPOT FACE BOTH FACES, INSTALL NEW BUSHING AND SHIMS IAW SRM 55-10-10, DEFECT SIZE: .325". 2L72 4F RTA16WE 20051219001102005121900110EU 2005 12 19 USAA051529 120051213A5347D53456038202 SEAT TRACK AIRBUSA321 A321211 3930370EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19164UW 1425 FOUND INBOARD SEAT TRACK CORRODED, FS 47 AFT. REMOVED AND REPLACED SECTION OF SEAT TRACK PER SRM 53-41-14; CORROSION LEVEL 2; TASK JA-220-25502, DEFECT SIZE: 1/2" X 1/4" AT THREE PLACES. 2L72 4F RTA28NM 20051219001212005121900121EA 2005 12 19 COMA0560710 120051210A3260162253 TARGET CNDAIRCL600 CL6002B19 1900309EA NLG BENT A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01708CA 7235 FLIGHT 5436 - GEAR DISAGREE WARNING. REPLACED THE NLG CENTERED PROX SENSOR TARGET. 2L72 4F RTA21EA 20051219001242005121900124WP 2005 12 19 ABXA050344 120051025A5340 ATTACH FITTING DOUG DC8 DC863F 302198FWP BS 680 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 FOUND CORNER FITTING OF CENTER WING BOX UPPER SURFACE AT STA 680, RIGHT BUTT LINE 62 WAS CRACKED. REMOVED CRACKED FITTING AT CENTER WING BOX UPPER SURFACE STA 680, RIGHT BUTT LINE 62 IAW DC8 SRM 51-1-20D AND SRM 51-3-1, DRILLED, REAMED AND COUNTERSUNK CORNER FITTING IAW DC8 SRM 51-1-20D AND 51-1-24, INSTALLED CORNER FITTING ON CENTER WING BOX UPPER SURFACE AT STA 680 RIGHT BUTT LINE 62 IAW DC8 SRM 51-1-20D AND SRM 51-3-1 (P/N: 3642974-2 PO NR 1122453). 2L74 4F 4A25 20051219001282005121900128WP 2005 12 19 ABXA050352 120051020A5315 FLOORBEAM DOUG DC8 DC863F 302198FWP BS 920 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 FOUND MAIN CABIN, STA 920, RIGHT BUTT LINE 31, FLOORBEAM CORRODED AT NUTPLATES. REMOVED CORROSION STA 920, RIGHT BUTT LINE 31. MATERIAL LOSS OUT OF LIMITES. FABRICATED REPAIR ANGLES AND INSTALLED IAW DWG K04881 OUT OF 7075 "0", PO NR 1108502 0.063", HEAT TREATED TO T6. 2L74 4F 4A25 20051219001372005121900137NM 2005 12 19 AWXA200501496 120051211A53306545774 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28328AW 23377 PHX - DURING INSPECTION DISCOVERED FUSELAGE SKIN CRACK, 1.0 INCHES LONG, ON THE LT SIDE OF THE AIRCRAFT JUST AFT OF WING TO BODY FAIRING BELOW STRINGER 23L AND 1.5 INCHES AFT OF BS 727D. MAINTENANCE TRIMMED OUT CRACK DAMAGE IAW BOEING 737-300 SRM 53-00-01 REPAIR 31. FABRICATED DOUBLER, TRIPLER AND TEAR STRAP DOUBLER IAW BOEING 737-300 SRM 51-00-00 FIG 16. INSTALLED FABRICATED REPAIR PARTS ON THE LT SIDE OF THE AIRCRAFT JUST AFT OF WING TO BODY FAIRING BELOW STRINGER 23L AND 1.5 INCHES AFT OF BS 727D IAW BOEING 737-300 SRM 51-00-01 REPAIR 31 AND AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5361-05345-RA1. 2L72 4F RTA16WE 20051219001402005121900140NM 2005 12 19 AWXA200501499 120051211A335020131A BATTERY BOEING757 7572S7 1384962NM EMERGENCY LIGHT INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28902AW 23322 PHX - EEL - DURING OVERNIGHT INSPECTION DISCOVERED EXTERIOR EMERGENCY LIGHT AT DOOR 4 LEFT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK, OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA2NM 20051219001462005121900146NM 2005 12 19 AWXA200501505 120051201A5311654653950 FRAME BOEING737 73733A 1384673NM BS 616 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 MCN - DURING C19 CHECK DISCOVERED MAIN CABIN FRAME CRACKED, 1.1 INCHES, AT THE LOWER LEG THROUGH FASTENER AT BS 616, BL 60R AND WL 200. MAINTENANCE CUT OUT DAMAGED AREA IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5311-01143-DD1. FABRICATED FILLER AND REPAIR ANGLE IAW AWA ER 03-5311-01143-DD1. INSTALLED FABRICATED REPAIR PARTS AT BS 616, BL 60R AND WL 200 IAW AWA ER 03-5311-01143-DD1. 2L72 4F RTA16WE 20051219001472005121900147NM 2005 12 19 AWXA200501506 120051202A5311654653949 FRAME BOEING737 73733A 1384673NM BS 816 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 MCN - DURING C19 CHECK DISCOVERED MAIN CABIN FRAME CRACKED, .7 INCHES, ON THE LOWER LEG AT BS 616, BL 60L AND WL 200. MAINTENANCE CUT OUT DAMAGED AREA IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5311-01143-DD1. FABRICATED FILLER AND REPAIR ANGLE IAW AWA ER 03-5311-01143-DD1. INSTALLED FABRICATED REPAIR PARTS AT BS 616, BL 60L AND WL 200 IAW AWA ER 03-5311-01143-DD1. 2L72 4F RTA16WE 20051219001492005121900149NM 2005 12 19 QXEA200501773 120051211A5210 HANDLE BOMBDRDHC8 DHC8402 1390042NM PAX DOOR LOOSE A QXEAO OTHER O OTHER TXTAXI/GRND HDL 1 NM09401QX 4031 SEA FLIGHT NR 2419: F/A REPORTED MCD DIFFICULT TO CLOSE/OPEN. MAINTENANCE RESECURED LOOSE SCREW ON MCD HANDLE CAUSING DOOR TO HANG UP MCD. OPS CHECKS GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051219001512005121900151NM 2005 12 19 AWXA200501508 120051118A5320654583340 SHEAR WEB BOEING737 73733A 1384673NM BS 188-196 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 MCN - DURING C19 CHECK DISCOVERED WEB CRACKED, .75 INCHES, FROM BS 188 TO BS 196, WL 207 AND BL 30L. MAINTENANCE REMOVED SHEAR WEB IAW BOEING 737-300 SRM 53-10-51-2R8. FABRICATED SHEAR WEB IAW BOEING 737-300 SRM 53-10-51-2R8. INSTALLED FABRICATED REPAIR PARTS FROM BS 188 TO BS 196, WL 207 AND BL 30L IAW BOEING 737-300 SRM 53-10-2R8. 2L72 4F RTA16WE 20051219001652005121900165EU 2005 12 19 USAA051544 120051213A5320D5347209001000 FLOOR SUPPORT AIRBUS320 A320214 3930316EU Y1292 C64-66 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19113UW 1141 FOUND CORROSION FLOOR SUPPORT Y1292 C64-66. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-42-11; CORROSION LEVEL 1; TASK JA-260-53500, DEFECT SIZE: 2 SQ IN. 2L72 4F RTA28NM 20051219001692005121900169NM 2005 12 19 DHL2005765505 120051212A5320 FLOOR SUPPORT BOEING727 727264 138408MNM BS 1030-1050 CORRODED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15765AT 23014 AFT CARGO PIT CORROSION ON FLOOR SUPPORT CHANNEL, LWR SIDE, BETWEEN STA 1030 AND 1050 RBL 8. REMOVED SECTION OF FLOOR SUPPORT. FABRICATED AND INSTALLED (3) REPAIR SPLICES 10.50" BY 1" FROM BAC1490-2583, 10.50 BY .085" BY .085" FROM AND10133-0702 AND 29" BY .090" BY 1" BY .050" IAW B727 SRM 53-10-5 FIG 4. 2L73 4F A3WE 20051219001802005121900180NM 2005 12 19 AWXA200501527 120051118A575465C2679920 SKIN BOEING737 73733A 1384673NM NR 6 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 MCN - DURING C19 CHECK DISCOVERED 6 CRACKS ON THE BOTTOM OF THE NR 6 SLAT BELOW ACTUATOR FROM SS 318R TO SS 324R. MAINTENANCE TRIMMED OUT DAMAGED AREA ON THE NR 6 SLAT IAW BOEING 737-300 SRM 57-43-01-2R6. FABRICATED FILLER AND SPLICE PLATE IAW BOEING 737-300 SRM 57-43-01-2R6. INSTALLED FABRICATED REPAIR PARTS ON THE NR 6 SLAT FROM SS 318R TO SS 324R IAW BOEING 737-300 SRM 57-43-01-2R6. 2L72 4F RTA16WE 20051219001882005121900188SO 2005 12 19 CHQA200500212 120051215A33501317 BULB EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT BURNED OUT A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11844RP 145620 EXTERIOR EMERGENCY LIGHT ABOVE LEFT HAND WING INOPERATIVE. REMOVED AND REPLACED OVERWING EMERGENCY LIGHT BULB IAW EMB 145 MM 33-50-10. OPS CHECK GOOD. 2L72 4F RTT00011AT 20051219001912005121900191EA 2005 12 19 VNAA0511019 120051122A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT WING TIP UNKNOWN A VNAAK NONE O OTHER ININSP/MAINT 1 GL05202PS 7858 DURING AN FAA RAMP CHECK, THE INSPECTOR REPORTED EVIDENCE OF LIGHTNING DAMAGE ON THE LT WINGTIP. MAINTENANCE COMPLIED WITH EN ROUTE AND DETAILED LIGHTNING STRIKE INSPECTIONS. NO DAMAGE OR EVIDENCE OF A LIGHTNING STRIKE WAS FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20051219001932005121900193EA 2005 12 19 VNAA0511023 120051126A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT WING GROUND DAMAGE A VNAAO OTHER W INADEQUATE Q C TXTAXI/GRND HDL 1 GL05244PS 7912 THE RIGHT WINGLET SUSTAINED LEADING EDGE DAMAGE AFTER HITTING A BAGGAGE CART WHILE AIRCRAFT WAS BEING MARSHALLED INTO THE GATE. MAINTENANCE REMOVED & REPLACED THE RIGHT WINGLET LEADING EDGE ASSEMBLY. NO FURTHER DAMAGE WAS FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20051219001952005121900195EA 2005 12 19 VNAA0511024 120051130A5210G80082 SEAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TORN A VNAAO OTHER O OTHER DEDESCENT 1 GL05216PS 7882 A LEAK WAS REPORTED AT THE PASSENGER DOOR AND THE AIRCRAFT WOULD NOT MAINTAIN PRESSURIZATION WHEN POWER WAS REDUCED. THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR SEAL. CABIN PRESSURIZATION OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20051219001962005121900196NE 2005 12 19 COMA0560714 220051212A7200CF343A1 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE LEFT FAILED A COMAA UNSCHED LANDING MYJOVER TEMP ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 SO01916CA16448970 7014 807551 FLIGHT 5482 - LEFT ENGINE EXCEEDED ITT LIMITS. IFSD. REPLACED THE LEFT ENGINE. 2L72 4F4 FRTA21EA E15NE 20051219002022005121900202EA 2005 12 19 VNAA0511018 120051119A2750860D10018 FCU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS FAILED A VNAAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL05248PS3520 7925 THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED WHEN FLAPS 45 DEGREE WAS SELECTED. THE CREW FOLLOWED THE QRH, CONTINUED THE APPROACH, AND LANDED. MAINTENANCE REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT. THE FLAPS OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20051219002172005121900217NM 2005 12 19 SWAA053982 120051214A57536546431 SKIN BOEING737 7373T5 1384608NM FOREFLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29696SW 23064 DURING SCHEDULED C2 CHECK, FOUND LT WING OUTBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM. 2L72 4F RTA16WE 20051219002182005121900218NM 2005 12 19 SWAA053983 120051214A33507003661 BALLAST BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29784SW 29810 DURING SCHEDULED HC2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BALLAST PER MM. 2L72 4F RTA16WE 20051219002232005121900223WP 2005 12 19 05FDEA04322 120051215A5300 REPAIR DOUG DC10 DC1010 3022110WP BS 1227 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568054 47808 EXTERNAL DOUBLER REPAIR AT STA 1227 BETWEEN LONG 40 AND 41 RT. PERFORMED A INSPECTION OF REPAIR IAW SRM 53-50-00 FIG 9 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P1. 2L73 4F A22WE 20051219002262005121900226WP 2005 12 19 05FDEA04320 120051215A5245 REPAIR DOUG DC10 DC1010 3022110WP A/C DOOR NONE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25563FE 46948 FOUND AN EXTERNAL DOUBLER REPAIR ON THE UPPER LIP OF THE NR 2 PACK AIR CONDITIONING DOOR LT SIDE OF FUSELAGE DIM 7 X 3 INCHES. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 52-00-01 FIG 4 SHT 2 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2. 2L73 4F A22WE 20051219002292005121900229NM 2005 12 19 05FDEA04315 120051214A5310 UNKNOWN BOEING727 7272S2F 1384O81NM FUSELAGE GROUND DAMAGE A FDEAO OTHER W INADEQUATE Q C TXTAXI/GRND HDL 1 SO25213FE 22935 AIRCRAFT DAMAGED ON PUSHBACK, ON BELLY. REPAIRED AND INSPECTED. 2L73 4F A3WE 20051219002302005121900230NM 2005 12 19 05FDEA04316 120051215A5320 WEB DOUG MD11 MD11 3023602NM ZONE 100 PUNCTURED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 CENTER CARGO LEFT HAND STATION 1841 X= 40 AFT WEB FOUND PUNCTURED. WEB REMOVED AND REPLACED WITH NEW FABRICATED WEB AS PER DRAWING AGA7170 AND INSTALLED AS PER SRM 51-31-01 VOLUME II. 2L73 4F RTA22WE 20051219002312005121900231NM 2005 12 19 05FDEA04317 120051215A5320 FLOOR SUPPORT DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 FS STA 430 LBL 27, FLOOR SUPPORT STRUCTURE FOUND WITH CORROSION. REMOVED AND REPLACED AS PER SRM 51-33-01. 2L73 4F RTA22WE 20051219002332005121900233NM 2005 12 19 ASAA0510306 120050920A5330655496049 DOUBLER BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02740AS 22578 YXX - FOUND CORROSION ON BONDED DOUBLER AT BS 360 BETWEEN STRINGER 26R AND 27R. REPAIRED PER B737-200 SRM 51-40-3. (M) 2L72 4F A16WE 20051219002362005121900236NM 2005 12 19 ASAA0510322 120050922A55316549558506 CLEVIS BOEING737 737290C 138448VNM VERTICAL STAB CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02740AS 22578 YXX - FOUND CORROSION ON VERTICAL STABILIZER AFT SPAR RIGHT PRIMARY FORWARD CLEVIS FORWARD FACE. CLEVIS REPLACED PER BOEING DWG 6546575 AND B737-200 SRM 51-30-2 PARAGRAPH 17. (M) 2L72 4F A16WE 20051219002382005121900238SO 2005 12 19 SIMA200528301 120051005A3350 CONNECTOR EMB 145 EMB145LR 3260212SO BATTERY PACK LOOSE A SIMAK NONE O OTHER CRCRUISE 1 SW21650AE 145417 EMERGENCY LIGHT ARM CIRCUIT BREAKER POPPED. FOUND LOOSE CONNECTOR ON BATTERY PACK. RESECURED CONNECTOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20051219002412005121900241SO 2005 12 19 SIMA200527707 120051003A335020131A POWER SUPPLY EMB 145 EMB145LR 3260212SO CABIN DISCHARGED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21645AE 145212 EMERGENCY LIGHT STRIPS 1-3 WILL NOT REMAIN ON. REPLACED NR 2 POWER SUPPLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20051219002422005121900242SO 2005 12 19 SIMA200529310 120051019A3350201314 POWER SUPPLY EMB 145 EMB145LR 3260212SO CABIN DISCHARGED A SIMAK NONE L NO TEST TXTAXI/GRND HDL 1 SW21636AE 145160 EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY POWER SUPPLY NR 3. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20051219002432005121900243SO 2005 12 19 SIMA200529004 120051013A3350 POWER SUPPLY EMB 145 EMB145LR 3260212SO CABIN DISCHARGED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21922AE 14500906 ORD - FLT 4289 - WHEN THE GPU WAS DISCONNECTED FROM THE AIRCRAFT, THE EMERGENCY LIGHTS CAME ON AND DRAINED THE POWER SUPPLIES. ALL FOUR BATTERY POWER SUPPLIES FOR EMERGENCY CABIN LIGHTING. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20051219002442005121900244SO 2005 12 19 SIMA200530101 120051025A532014522459003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21720AE 145279 SAW - DURING MBV INSPECTION, FOUND RIGHT FLOOR SUPPORT RAMP BETWEEN FRAMES 19 AND 20 IS CORRODED. INSTALLED NEW FLOOR SUPPORT RAMP IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20051219002472005121900247SO 2005 12 19 SIMA200530104 120051025A532014521719003 DOUBLER EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21720AE 145279 DURING MBV INSPECTION, FOUND LEFT OMEGA RIGHT SIDE DOUBLER AT FRAME 20 IS CORRODED. INSTALLED NEW DOUBLER IAW SRM 53-00-10. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20051219002502005121900250SO 2005 12 19 SIMA200529701 120051019A5320 FLOOR SUPPORT EMB 145 EMB145 3260210SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21612AE 145079 THE LEFT OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. PERFORMED A CUTOUT OF THE OMEGA BEAM TO REMOVE THE CORROSION. FABRICATED A FILLER, DOUBLER AND SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB-145/1142 REV 30, CHAPTER 53-00-10, FIG 201. (M) 2L72 4F RTT00011AT 20051219002512005121900251SO 2005 12 19 SIMA200530106 120051019A532014525381003 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21659AE 145762 THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED THE CORROSION BY MAKING A CUT OUT. PREPARED A DOUBLER, FILLER, FABRICATED A PLATE AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 31, CHAPTER 53-00-10. (M) 2L72 4T RTT00011AT 20051219002532005121900253SO 2005 12 19 SIMA200529311 120051020A523014545809405 DOOR EMB 145 EMB145LR 3260212SO CARGO BAY GROUND DAMAGE A SIMAK NONE O OTHER TXTAXI/GRND HDL 1 SW21923AE 14500907 AIRCRAFT WAS STUCK BY GROUND SUPPORT EQUIPMENT WITH DAMAGE TO BAGGAGE DOOR. REPAIRED BAGGAGE DOOR WITH AN EXTERNAL DOUBLER IAW EMB REPAIR STATEMENT IC 2005-145/5995 AND SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20051219002552005121900255SO 2005 12 19 SIMA200529308 120051018A2611FDS765A2 SMOKE DETECTOR EMB 145 EMB145LR 3260212SO LAVATORY MALFUNCTIONED A SIMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW21677AE 14500810 LAVATORY SMOKE WARNING JUST AFTER TAKEOFF. INSPECTED LAVATORY FOUND NO EVIDENCE OF SMOKE OR DAMAGE. REPLACED THE LAVATORY SMOKE DETECTOR SENSOR IAW EMB AMM 26-14-01. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20051219002562005121900256SO 2005 12 19 SIMA200529307 120051017A3240142093 CONTROL UNIT EMB 145 EMB145LR 3260212SO BRAKE SYSTEM MALFUNCTIONED A SIMAO OTHER O OTHER TXTAXI/GRND HDL 1 SW21685AE 14500836 ORD - FLT 4228 - ON LANDING ROLL OUT, BRAKES GRABBED AND THEN HAD POOR BRAKING ABILITY. REPLACED BRAKE CONTROL UNIT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20051219002572005121900257SO 2005 12 19 SIMA200529306 120051014A532014521713005 FLOOR SUPPORT EMB 145 EMB145 3260210SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21612AE 145079 THE GALLEY CENTER BEAM WAS FOUND CORRODED. REMOVED DAMAGED BEAM AND INSTALLED SERVICEABLE BEAM. REPAIR DONE IAW EMB 145 SRM, SRM EMB145/1142 REV 31, CHAPTERS 51-40-02 AND 51-20-03. (M) 2L72 4F RTT00011AT 20051219002582005121900258SO 2005 12 19 SIMA200531509 120051102A532014522178005 PLATE EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21822AE 145581 FOUND SERVICE DOOR CENTER SILL PLATE CORRODED. REPLACED CENTER SILL PLATE IAW EMB SRM 51-40-2. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20051219002612005121900261WP 2005 12 19 AALA20050805 120051205A5280 PAD DOUG DC9 DC983 3022083WP GEAR DOOR INOPERATIVE A AALAO OTHER J WARNING INDICATION APAPPROACH 1 SW219629H 53599 ORD - DURING APPROACH EXTENDED LANDING GEAR AND GEAR DOOR OPEN REMAINED ILLUMINATED. TOWER ADVISED GEAR DOORS MAIN WRE OPEN. WENT AROUND AND ACCOMPLISHED GEAR DOOR OPEN LIGHT QRH, NO HELP. REPLACED BOTH MAIN LANDING GEAR DOOR PADS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20051219002642005121900264CE 2005 12 19 DXTA200501137 120051211A771031J285704 SERVO VALVE CESSNA560 560XL 2076702CE PWA 545 PW545A NE ENGINE INOPERATIVE E DXTAC ABORTED TAKEOFF J WARNING INDICATION TXTAXI/GRND HDL 1 GL07659QS 5605359 PCEDB0739 WHEN TAKEOFF POWER APPLIED, L EEC MAN LIGHT ILLUMINATED. TAKEOFF WAS ABORTED. REMOVED AND REPLACED INOP SERVO VALVE IAW PWA 545A M/M 71-00-00. OPS AND LEAK CHECK GOOD. 2L72 4F4 FRTA22CE E00059EN 20051219002652005121900265CE 2005 12 19 DXTA200501135 120051209A3260 POSITION SWITCH CESSNA750 750 2076810CE MLG OUT OF RIG E DXTAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL07916QS 7500116 RED GEAR UNLOCK LIGHT ON INFLIGHT WITH GEAR IN UP POSITION. RECYCLED GEAR BUT NO CHANGE. JACKED AIRCRAFT. CLEANED AND INSPECTED GEAR UPLOCK SWITCHES. SWUNG GEAR, NO FAULT FOUND. PUT GEAR IN THE UP POSITION AND FROZE SWITCHES, SWUNG GEAR NO FAULT FOUND. AGAIN PUT GEAR UP AND FOUND NOSE SWITCH TO BE OUT OF RIG BY WIGGLING IT. ADJUSTED SWITCH, SWUNG GEAR, WIGGLED SWITCH, AND NO FAULT FOUND AT THIS TIME. DOWN JACKED AIRCRAFT IAW CITATION X MM 32-33-00. 2L72 4J RTT00007WI 20051219002662005121900266CE 2005 12 19 DXTA200501141 120051213A323399121113 ACTUATOR CESSNA500 560CESSNA 2076750CE MLG INOPERATIVE E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07391QS6235 5600493 LEFT MAIN GEAR WOULD NOT RETRACT UPON TAKEOFF GEAR RETRACTION. REMOVED AND REPLACED LT MLG ACTUATOR IAW 560 MM CHAPT 32-31-04, PERFORMED CAMBER AND GEAR DOOR ADJUSTMENTS AS NECESSARY AND SAFETIED IAW 560 MM CHAPT 32-11-01 OPS CHECKED AND LEAK CHECKED ACTUATOR AND FITTINGS, NO LEAKS NOTED. 2L72 4F RTA22CE 20051219002672005121900267NE 2005 12 19 DXTA200501139 220051211A732132448809 FCU CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE FAILED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07325QS1369 5600425 PCEJCO333 DID NOT GET FULL PWR ON RIGHT HAND ENGINE DURING STATIC TAKEOFF, N1 75.9 ITT 450, N2 83 WITH THROTTLES FULL FWD. REMOVED AND REPLACED RIGHT ENGINE FCU AND FUEL PUMP. ENGINE OPERATES NORMAL AT THIS TIME IAW PWA M/M 71-00-00. 2L72 4F4 FRTA22CE E25EA 20051219002692005121900269NM 2005 12 19 DXTA200501140 120051213A2612 FIRE WARNING AMD FALC50FALCON2000 2730170NM NR 2 NACELLE ILLUMINATED E DXTAO OTHER N FALSE WARNING NRNOT REPORTED 1 GL07245QS 145 NR 2 ENGINE FIRE FAULT LIGHT IS ILLUMINATED. ITEM IS UNDER INVESTIGATION. 2K73 4F RTA50NM 20051219002712005121900271NM 2005 12 19 DHL2005749013 120051101A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01749DH 22013 FRAME DENTED BETWEEN STR 23-25L AT BS 680. CUT OUT DAMAGED AREA 1 1/2 INCHES BY 1 INCH, 1 1/4 INCHES BY 1 INCH. FAB REPAIR ANGLE MST IB 7075T6 /063 PO 9002351 22 1/4 INCHES BY 3 7/8 INCHES IAW B727 SRM 53-10-2 FIG 3 AND 51-40-3 FIG 1. TREATED AND PRIMED IAW B727 SRM 51-10-2 . INSTALLED REAPIR PART IAW B727 SRM 51-40-3 FIG 1. 2L73 4F RTA3WE 20051219002732005121900273NM 2005 12 19 SB05170 120051123A3520 OXYGEN MASK BOEING737 7373B7 1384580NM ROW 20 FAILED A USAABG EMER. DESCENT O2 MASK DEPLOYED O OTHER DEDESCENT 1 EA19512AU 23595 BNA FLT 53, EN ROUTE CLT TO MCI. DURING EMERGENCY DESCENT, MASKS DEPLOYED EXCEPT ROW 20. MAINTENANCE, REPLACED OXYGEN GENERATORS, REPACKED MASKS. FOUND MASK LANYARD CAUGHT AROUND DOOR LATCH ROW 20. REPOSITIONED, OPS GOOD. 2L72 4F RTA16WE 20051219002822005121900282NM 2005 12 19 DHL2005749027 120051109A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01749DH 22013 ACCOMPLISH IDENTIFICATION OF EXISTING STRINGER SPLICE REPAIR AT STA 600 STR 28L. EXISTING REPAIR FOUND TO BE NON COMPLIANT IAW 727 SRM 53-10-3 FIG 1 TABLE I. REMOVED EXISTING REPAIR IAW 727 SRM 51-30-2 FABBED AND INSTALLED NEW STR SECTIONS 2EA FROM BAC1498-141 PO 427415 DIM 19"EA AND 3 EA SPLICE SECTIONS FROM BAC1498-132 PO5400126 DIM 13" EA IAW B727 SRM 53-10-3 FIG 1. 2L73 4F RTA3WE 20051219002842005121900284EA 2005 12 19 ASOA05914 120051025A5320 BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27838AS 7276 DURING A C-CHECK IN MCN, THE FS 280 BEAM, OUTBOARD OF RBL 9, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL BE REPAIRING THE FS 280 BEAM, OUTBOARD OF RBL 9, IAW ASA EO`S 600-53-0090 AND 600-53-0091. (M) 2L72 4F RTA21EA 20051219002852005121900285EA 2005 12 19 ASOA05913 120051025A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA EXTERIOR INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27829AS 7232 DURING A GROUND INSPECTION IN CAE, THE RIGHT FORWARD EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE RIGHT FORWARD EXTERIOR EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051219002862005121900286EA 2005 12 19 ASOA05920 120051027A5310 PRESSURE PANEL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27838AS 7275 DURING A C-CHECK IN MCN, THE PRESSURE FLOOR SKIN AT LBL 36 AND RBL 36, FROM FS 409 PLUS 28 TO FS 559, WAS FOUND TO BE CORRODED BEYOND LIMITS. AFTER MAINTENANCE BLENDED, ALODINED, AND PRIMED THE PRESSURE FLOOR SKIN AT LBL 36 AND RBL 36, FROM FS 409 PLUS 28 TO FS 559, IN ACCORDANCE WITH REO 601R-53-41-370. (M) 2L72 4F RTA21EA 20051219002902005121900290EA 2005 12 19 ASOA05929 120051028A2400 ELECTRICAL SYS CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A ASOAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27835AS 7258 FLT 4738 - DURING CRUISE FROM CVG-CLE, THE AC ESS BUS FELL OFFLINE AND WAS RESET IN THE AIR. THE FLIGHT ATTENDANT ALSO REPORTED AN ELECTRICAL BURNING ODOR. THE FLIGHT CONTINUED TO CLE, WHERE IT LANDED SAFELY. MAINTENANCE RESET AC ESS BUS, INSPECTED AND RETORQUED AC ESS BUS RELAY. AIRCRAFT POWERED UP SEVERAL TIMES WITH NO DEFECTS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051219002952005121900295EA 2005 12 19 ASOA05924 120051028A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA BS 610 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27838AS 7276 DURING A C-CHECK IN MCN, THE INTERNAL SKIN AT FS 610, AT STRINGER 22LT, UNDER THE CARGO FLOOR, WAS FOUND TO BE CORRODED. MAINTENANCE REPAIRED THE INTERNAL SKIN AT FS 610, STRINGER 22 LT, UNDER THE CARGO FLOOR IAW BOMBARDIER REO 601R-53-61-1565. (M) 2L72 4F RTA21EA 20051219002972005121900297EU 2005 12 19 ASOA05922 120051028A33507012210 LIGHT AEROSPATR72 ATR72212 8680945EU PAX DOOR INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27633AS 344 DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY LIGHT ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20051219002982005121900298EA 2005 12 19 ASOA05921 120051027A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27838AS 7276 DURING A C-CHECK IN MCN, SKIN CORROSION WAS FOUND AT LBL 36 AND RBL 36, AT FS 409 PLUS 28 THROUGH FS 559. AFTER MAINTENANCE BLENDED, ALODINED, AND PRIMED THE SKIN CORROSION AT LBL 36 AND RBL 36, AT FS 409 PLUS 28 THROUGH FS 559, IAW REO 601R-53-41-370, IT WAS FOUND TO BE WITHIN LIMITS. (M) 2L72 4F RTA21EA 20051219002992005121900299EA 2005 12 19 ASOA05919 120051027A33974871907191 WIRE CNDAIRCL600 CL6002B19 1900309EA CABIN DAMAGED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27838AS 7276 DURING A C-CHECK IN MCN, THE EMERGENCY FLOOR LIGHT WIRING AT THE LAVATORY WAS FOUND TO BE DAMAGED. MAINTENANCE IS REMOVING AND REPLACING THE CONNECTORS TO THE EMERGENCY FLOOR LIGHTS AT THE LAVATORY. (M) 2L72 4F RTA21EA 20051219003072005121900307EA 2005 12 19 ASOA05964 120051110A33506100928 SIGN CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27933EV 8022 DURING A GROUND INSPECTION IN CAE, THE EMERGENCY EXIT SIGN, NEAR THE PASSENGER DOOR, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT SIGN, NEAR THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051219003092005121900309EA 2005 12 19 ASOA05966 120051120A21707536893 COALESCER BAG CNDAIRCL600 CL6002B19 1900309EA A/C BAY DIRTY A ASOAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27920EV 7810 FLT 4400 - DURING CRUISE FROM PIT-CVG, A LIGHT BURNING ODOR WAS NOTED BRIEFLY. THE AIRCRAFT CONTINUED TO CVG, WHERE IT LANDED SAFELY. MAINTENANCE INSPECTED THE AIR CYCLE MACHINE OIL AND REMOVED AND REPLACED THE COALESCER BAGS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051219003102005121900310EA 2005 12 19 ASOA05967 120051110A5260601R319805 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27839AS 7284 DURING A GROUND INSPECTION IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND TO BE BROKEN AT THE ATTACH POINT. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051219003112005121900311EA 2005 12 19 ASOA05968 120051111A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27870AS 7530 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT FS 718 FRAMES, BETWEEN STRINGER 10-12 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REPAIR THE LEFT AND RIGHT FS 718 FRAMES, BETWEEN STRINGER 10-12, IAW ASA EO 600-53-0066. (M) 2L72 4F RTA21EA 20051219003142005121900314EA 2005 12 19 ASOA05971 120051111A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27870AS 7530 DURING A C-CHECK IN MCN, THE RIGHT INBOARD FS 484 CLIP, AT RBL 27, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT INBOARD FS 484 CLIP, AT RBL 27, IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20051219003202005121900320EA 2005 12 19 ASOA05977 120051113A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA EXTERIOR INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27980EV 7759 DURING A GROUND INSPECTION IN CAE, THE FORWARD LEFT EXTERNAL EMERGENCY LIGHT ASSEMBLY WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD LEFT EXTERNAL EMERGENCY LIGHT ASSEMBLY LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051219003252005121900325WP 2005 12 19 IXXA0500132S 120050214A5753 SKIN DOUG DC8 DC871F 302199DWP T/E FLAP DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11821BX858952998 45811 DURING A ROUTINE C CHECK INSPECTION, FOUND RT WING OUTBOARD FLAP UPPER FORWARD PLATING INTERIM REPAIR STA XF 227.00. MAJOR REPAIR ACCOMPLISHED REMOVAL OF DAMAGED PLATING AREA. PERFORMED AN NDT INSPECTION. FABRICATED NEW PLATING SEGMENT, INTERNAL SPLICE AND EXTERNAL DOUBLER CLEANED. TREATED AND PRIMED AREA AND REPAIRED PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIRED PARTS IAW SEMAN DRAWING ED-3848 AND FAA FORM 8110-3 NR 05056, DC8 SRM 51-1-11, 51-1-20D, 51-1-21, 51-1-22, 51-1-26, 51-3-0, 51-3-1, 51-3-2. 2L74 4F RT4A25 20051219003262005121900326WP 2005 12 19 IXXA0500133S 120050304A5311 FRAME DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11821BX858952998 45811 DURING A ROUTINE C CHECK INSPECTION, FOUND RT FUSELAGE FORWARD ACCESSORY COMPARTMENT STRUCTURE FRAME CRACK DAMAGE AT STA FS 55.00,L-24R. MAJOR REPAIR ACCOMPLISHED REMOVAL OF FASTENERS FROM REPAIR AREA. REMOVED DAMAGED FRAME SEGMENT. PERFORMED NDT INSPECTION. FABRICATED FRAME SEGMENT AND SPLICE DOUBLER. PERFORMED HEAT TREATMENT, CLEANED, TREATED AND PRIMED AREA AND REPAIRED PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED FRAME SEGMENT AND SPLICES IAW DC8 SRSM 53-2-0 FGI2 SH 1, 6 TR NR 53-125, 53-3-1 FIG 3 SH 2, 2A, 51-1-1, 51-1-4, 51-1-11, 51-1-15, 51-1-20D, 51-3-1, 51-3-2 DPS 3.69-4 REV "AM" R-1,7.00-1 REFV."BK". 2L74 4F RT4A25 20051219003272005121900327WP 2005 12 19 IXXA0500137S 120050308A5711 SPAR CAP DOUG DC8 DC871F 302199DWP RT WING CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11821BX858952998 45811 DURING A ROUTINE C CHECK INSPECTION, FOUND RT WING UPPER FRONT SPAR CAP STRUCTURE CRACKED BETWEEN STA XFS-6 CAP. MAJOR REPAIR ACCOMPLISHED REMOVAL OF FASTENERS AND CORROSION FROM SLANT PANEL UPPER CAP. FOUND OUT OF LIMITS. CLEANED, TREATED AND PRIMED AREA. INSTALLED DOUBLER AND REMOVED UPPER SPAR CAP. REMOVED STIFFENER PERFORMED NDT INSPECTION. APPLIED SEALANT TO FAYING SURFACES. INSTALLED DOUBLER AND ANGLE DOUBLER IAW S/B DC8-57-072 RO3, DWG DACO 5892075, CN1, DC8 SRM 51-1-8, 51-1-11, 51-1-15, 51-1-20D, 51-1-22, 51-1-26, 51-3-1, 57-2-0, 57-2-1, 57-3-1, 57-3-2 DPS 1.05-8, 3.67-3, 2.50. 2L74 4F RT4A25 20051220000022005122000002NM 2005 12 20 05FDEA04222 120051211A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 RIGHT HAND WING INBOARD TRAILING EDGE FLAP OUTBOARD HINGE (FLAP SIDE) AT PIVOT BORE HOLE INBOARD SIDE FOUND CORROSION. CORROSION REMOVED AS PER FEDEX EA 1-5750-94561. 2L73 4F RTA22WE 20051220000032005122000003NM 2005 12 20 05FDEA04223 120051211A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 RIGHT HAND WING INBOARD TRAILING EDGE FLAP OUTBOARD HINGE (FLAP SIDE) AT PIVOT BORE HOLE OUTBOARD SIDE FOUND CORROSION. CORROSION REMOVED AS PER FEDEX EA 1-5750-94561. 2L73 4F RTA22WE 20051220000042005122000004NM 2005 12 20 05FDEA04224 120051211A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 500 TOOL DAMAGE A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25524FE 48480 LEFT HAND WING INBOARD TRAILING EDGE FLAP OUTBOARD HINGE (FLAP SIDE) AT PIVOT BORE HOLE INBOARD SIDE FOUND TOOL MARK. TOOL MARK REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-94560. 2L73 4F RTA22WE 20051220000052005122000005WP 2005 12 20 05FDEA04324 120051215A5310 REPAIR DOUG DC10 DC1010 3022110WP BS 1801-1821 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568054 47808 EXTERNAL DOUBLER REPAIR ON FUSELAGE FROM STA 1801 TO STA 1821 BETWEEN LONG 36 AND 39 RT SIDE. PERFORMED A INSPECTION OF REPAIR IAW SRM 53-20-00 FIG 6 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P1. 2L73 4F A22WE 20051220000062005122000006WP 2005 12 20 05FDEA04325 120051215A5320 REPAIR DOUG DC10 DC1010 3022110WP BS 680-690 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568054 47808 EXTERNAL DOUBLER REPAIR FROM STA 680 TO STA 690 AT LONG 28 LT Z-30 UPPER CARGO DOOR JAMB LWR SILL. PERFORMED A INSPECTION OF REPAIR IAW SRM 53-50-00 FIG 6 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P1. 2L73 4F A22WE 20051220000082005122000008WP 2005 12 20 05FDEA04327 120051215A5310 REPAIR DOUG DC10 DC1010 3022110WP BS 579-590 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568054 47808 EXTERNAL DOUBLER REPAIR AT FUSELAGE FROM STA 579 TO STA 590 BETWEEN LONG 44 AND 46 LT. PERFORMED AN INSPECTION OF REPAIR IAW SRM 53-20-00 FIG 2 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P1. 2L73 4F A22WE 20051220000092005122000009NM 2005 12 20 05FDEA04328 120051215A5311 FRAME BOEING727 727200 138407ENM BS 500 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 FWD CARGO BAY FRAME I/B FLANGE DENTED AT BS 500, BETWEEN STR 23RT AND 24RT. *S/D* REPAIRED FRAME AT BS 500, STR 23R-24R PER SRM 51-40-3. 2L73 4F RTA3WE 20051220000102005122000010NM 2005 12 20 05FDEA04329 120051215A5322 SHEAR TIE BOEING727 727200 138407ENM BS 1009 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 CORROSION ON AFT CARGO BAY SHEAR TIE BS 1009 WL 136 LBL 4. *S/D* CUT OUT DAMAGED SECTION OF SHEAR TIE AN AREA 1 X 3 INCH IN AFT CARGO BAY BS 1009 WL 136 LBL 4. FABRICATED NEW REPAIR DOUBLER FROM 7075T6 .080 LOT 655633. INSTALLED NEW REPAIR DOUBLER ALL IAW SRM 51-40-3. 2L73 4F RTA3WE 20051220000142005122000014NM 2005 12 20 05FDEA04184 120051208A5315 FLOORBEAM BOEING727 727200 138407ENM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 REWORK OF FEDEX SNRM N00773 DUE TO IMPROPER SRM REPAIR APPLICABILITY MAIN DECK FLOORBEAM CORRODED ON TOP TWO PLACES AT STA BS 312 BETWEEN LBL 4 AND LBL 20. REMOVED IMPROPER REPAIR IAW B727 SRM 51-30-2. FABRICATED REPAIR ANGLES AND TEE CAP SECTION IAW B727 SRM 53-10-8 FIGURE 9. ALODINED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED REPAIR IAW B727 SRM 53-10-8 FIGURE 9. THIS IS A MAJOR REPAIR. 2L73 4F RTA3WE 20051220000152005122000015NM 2005 12 20 05FDEA04185 120051208A5310 REPAIR BOEING727 727200 138407ENM ZONE 100 IMPROPER A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 REPAIR LOCATED AT STA 950F - 970 STRINGER 29-R REQUIRES EVALUATION FOR MAJOR / MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED REPAIR AT STA BS 950F - 970 STRINGER 29R IAW B727 SRM 51-30-2. FABRICATED NEW REPAIR PARTS IAW B727 SRM 51-40-4 FIGURE 1 SHEET 6. ALODINED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B727 SRM 51-40-4 FIGURE 1 SHEET 6 AND 51-30-2. THIS IS A MAJOR REPAIR. 2L73 4F RTA3WE 20051220000162005122000016NM 2005 12 20 05FDEA04333 120051215A5310 REPAIR BOEING727 727200 138407ENM BS 950A UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25274FE 22039 FOUND REPAIR AT STA 950A, STR 29R WAS DETERMINED HAD BEEN ACCOMPLISHED IAW SRM 53-30-3 FIG 3 BASED ON EXTERNAL VISUAL EVALUATION WITH REPAIR INSTALLED, CONSISTED LOCATION, SHAPE, SIZE, FASTENER SPACING, NUMBERS, MATERIAL THICKNESS AND TYPE AND GENERAL WORKMANSHIP OF INSTALLATION, REPAIR CLASSISIFED AS MAJOR REPAIR PER GMM 6-2-100. 2L73 4F RTA3WE 20051220000202005122000020NM 2005 12 20 05FDEA04213 120051209A5343AEA7051501 FITTING DOUG MD11 MD11 3023602NM ZONE 700 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 UPON REMOVAL OF CLG SHOCK STRUT ASSY FOUND LT TRUNNION SUPPORT FITTING FWD MOUNTING HOLE, SHEAR PIN HOLE & AFT MOUNTING HOLE WITH CORROSION. LT TRUNNION SUPPORT FITTING FORWARD MOUNTING HOLE, SHEAR PIN HOLE, AND AFT MOUNTING HOLE CORROSION REMOVED AND REPAIR CARRIED OUT AS PER FEDEX EA1- 5340-9070. TITLE: FUSELAGE - CENTER LANDING GEAR LT SUPPORT FITTING CORROSION REPAIR. 2L73 4F RTA22WE 20051220000212005122000021EU 2005 12 20 05FDEA04215 120051210A5540 STRUCTURE AIRBUS310 A310203 3930313EU RUDDER DAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25424FE 241 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121.370A COMPLY WITH AGING 9-AGING-INSP. RUDDER TRAILING EDGE DAMAGED BETWEEN STA 270 AND STA 330. REPAIRED IAW SRM 55-41-12 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR. 2L72 4F RTA35EU 20051220000232005122000023NM 2005 12 20 05FDEA04335 120051215A5310 REPAIR BOEING727 727200 138407ENM BS 950A UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25274FE 22039 FOUND PREVIOUSLY REPAIR AT STA 950A, STR 29L WAS ACCOMPLISHED IAW SRM 53-30-3, FIG 3 PAGE 13, BASED ON EXTERNAL VISUAL EVALUATION OF LOCATION, SHAPE, SIZE, FASTENER SPACING, NUMBERS AND SPACING, MATERIAL THICKNESS AND GENERAL WORKMANSHIP, REPAIR IS CLASSIFIED AS MAJOR REPAIR. 2L73 4F RTA3WE 20051215001282005121500128NM 2005 12 15 2005UALA01409 120051205A5754114T61241 BRACKET BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE LT WING KRUEGER CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29644UA62879 25094 LT WING KRUEGER FLAP INBD OF NR 1 PYLON, ROTARY ACTUATOR OUTBD SUPPORT BRACKET IS BUCKLED AND CRACKED. BRACKET FAILURE WAS DUE TO FATIGUE. PART WAS REPLACED. 2L72 4F4 FRTA1NM E24NE 20051215001302005121500130NM 2005 12 15 2005UALA01411 120051206A3397 FUSE BOEING747 747422 1384935NM PWA 4056 PW4056 NE LT OVERWING INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29198UA 28716 LEFT OVERWING EMERGENCY LTS INOP, 2 FWD ASSY'S. REPLACED FUSE AT POWER SUPPLY. 2L74 4F4 FRTA20WE E24NE 20051215001322005121500132NM 2005 12 15 2005UALA01413 120051206A5330 BEAR STRAP BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE BS 767-787 CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29921UA 25388 AFT PIT INTERNAL SKIN BEAR STRAP CORRODED BTWN STRINGERS 25R AND 26R BS 767-787. EXTERNAL DOUBLER REPAIRED. 2L72 4F4 FRTA16WE E2GL 20051215001372005121500137NM 2005 12 15 2005UALA01417 120051207A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE PUNCTURED A UALAK NONE O OTHER ININSP/MAINT 1 WP29332UA 24193 PUNCTURE JUST FWD OF RT NOSE GEAR DOOR AND 1 FT FWD OF EXT PWR PANEL DOOR. ACCOMPLISHED INSTALLATION OF REPAIR DOUBLERS AND TRIPLERS PER SRM 53-00-01 REPAIR 31. 2L72 4F4 FRTA16WE E2GL 20051215001412005121500141NM 2005 12 15 2005UALA01422 120051208A5410 BUSHING BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE NR 1 PYLON MIGRATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29644UA 25094 NR 1 PYLON OUTBD MIDSPAR FITTING OUTBD LUG, BUSHING IS MIGRATED. NR 1 PYLON OUTBD MIDSPAR FITTING OUTBD LUG, BUSHING WAS MIGRATED. THE BUSHING MIGRATION IS UNKNOWN. IT WAS REPLACED PER SRM 54-53-90. 2L72 4F4 FRTA1NM E24NE 20051215001462005121500146NM 2005 12 15 2005UALA01427 120051201A3350 LIGHT BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE CABIN INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29938UA 26671 AFT CABIN EEL LIGHTS INOP FROM ROW 15 AFT TO AND INCLUDING EEL STRIP IN FRONT OF AFT GALLEY CART STOWAGE COMPARTMENT. CLEANED TRACK OF MOISTURE, REPLACED LAST EEL LAMP. 2L72 4F4 FRTA16WE E2GL 20051215001502005121500150NM 2005 12 15 2005UALA01431 120051210A5311 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE E&E COMPARTMENT PUNCTURED A UALAK NONE O OTHER ININSP/MAINT 1 WP29922UA 26642 E AND E COMPARTMENT DOOR CUTOUT FWD FRAME HAS A PUNCTURE HOLE IN FRAME WEB AT BS 324 AND RBL 9.5 WL 153.5 APPROX 0.375" IN DIAMETER. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER. 2L72 4F4 FRTA16WE E2GL 20051215001522005121500152EU 2005 12 15 2005UALA01433 120051209A3350 LIGHT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29476UA 1508 EEL LIGHTS AT SEATS 4, 5, 8, 9, 15, 16, 17, 21, 22 AND 23 ARE INOPERATIVE. REPAIRED SHORT UNDER SEAT 8A AND REPLACED 110WL2. 2L72 4F4 FRTA28NM E40NE 20051215001602005121500160NM 2005 12 15 2005UALA01441 120051211A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE GALLEY INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29121UA 29167 AFT GALLEY WALL LT SIDE EMERGENCY LIGHT INOP. REPLACED LAMP. 2L74 4F4 FRTA20WE E24NE 20051215001652005121500165 2005 12 15 SB05167 420051212A2565D31591478 SLIDE BOEING737 737301 1384611NM PASSENGER CABIN READS LOW A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US406823411 23933 PIT - THE FORWARD LEFT SLIDE ASSEMBLY PRESSURE VESSEL WAS FOUND TO BE BELOW LIMITS. MAINTENANCE REPLACED THE LEFT FORWARD SLIDE ASSEMBLY. OK FOR SERVICE. 2L72 4F RTA16WE 20051215001682005121500168NE 2005 12 15 BB05103 220051211A7320FFG022AC GOVERNOR BOEING757 757225 1384959NM GE CFM56 CFM56* 13802NE ZONE 400 FAILED A USAAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 EA19620AU331272583 27199 FLIGHT 491, PHL-MBJ, RIGHT ENGINE WOULD NOT ACCELERATE. THRUST DECAY, LOW EPR, AND ENGINE READINGS CONSISTENT WITH EPR. DIVERTED TO FLL. MAINTENANCE REPLACED THE RIGHT FUEL FLOW GOVERNOR. 2L72 4F4 FRTA2NM E2GL 20051215001692005121500169NM 2005 12 15 USAA051481 120051208A3210 FITTING BOEING737 7374B7 1384702NM R MLG TRUNNION CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 RT MLG FWD TRUNNION TO AFT SPAR FITTING 6:00 POSITION AT HOLE B. INSTALLED TWO NEW FASTENERS IAW TR 57-10-13 REV A DEFECT SIZE: RT MLG BEAM AFT SUPPORT FITTING CRACKED AT 6:00 IN HOLE B, CRACK IS .5" LONG. 2L72 4F RTA16WE 20051215001712005121500171NM 2005 12 15 USAA051482 120051208A53201135423 INTERCOSTAL BOEING737 7374B7 1384702NM STA 947-967 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 FOUND INTERCOSTAL CORRODED STA 947-967, LBL. REMOVED AND REPLACED WITH NEW PART IAW SRM 51-10-02, DEFECT SIZE: .350" AREA OF CORROSION AT FASTENER HOLE, 20 INCHES IN LENGTH. 2L72 4F RTA16WE 20051215001732005121500173NM 2005 12 15 USAA051479 120051208A53201136992 INTERCOSTAL BOEING737 7374B7 1384702NM STA 328-344 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 FOUND CORROSION STA 328-344, LBL9. REMOVED AND REPLACED IAW SRM 51-10-02 DEFECT SIZE: .5 INCH AREAS OF CORROSION ON THE INTERCOSTAL 16 INCHES IN LENGTH. 2L72 4F RTA16WE 20051215001752005121500175NM 2005 12 15 USAA051477 120051208A5315BAC1505100246 FLOORBEAM BOEING737 7374B7 1384702NM BS 328 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 FOUND FLOORBEAM UPPER T CAP CORRODED, BS 328; LBL 60. FAB`D AND INSTALLED NEW T-CAP SECT REPAIR SPLICE IAW 53-10-51, FIG 201, DEFECT SIZE: 1/2" BY 1/2" CORRODED AREAS AROUND CLIP NUT HOLES. 2L72 4F RTA16WE 20051215001922005121500192NM 2005 12 15 USAA051506 120051212A5320 INTERCOSTAL BOEING737 7374B7 1384702NM STA 294.5 S7L CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 FOUND CRACK STA 294.5 S7L. REPLACED DAMAGED PART WITH NEW PART IAW SRM 51-10-02 DWG 65-17684, DEFECT SIZE: .250". 2L72 4F RTA16WE 20051219000132005121900013NM 2005 12 19 05FDEA04226 120051212A5753 MOUNT DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 LEFT HAND WING, WITH REFERENCE TO EO 1-5750-7-5002, OUTBOARD FLAP INBOARD FORWARD HINGE LOWER INBOARD MOUNT BORE CORRODED. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-94564. 2L73 4F RTA22WE 20051219000142005121900014NM 2005 12 19 05FDEA04227 120051212A5753 MOUNT DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 LEFT WING WITH REFERENCE TO EO 1-5750-7-5002, OUTBOARD FLAP INBOARD FORWARD HINGE LOWER MOUNT SURFACE CORRODED. CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-94564. 2L73 4F RTA22WE 20051219000262005121900026WP 2005 12 19 05FDEA04239 120051212A5310 DOOR FRAME DOUG DC10 DC1010 3022110WP FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25568FE 47827 DURING AIRPLANE'S P TO F MODIFICATION FOUND INTERNAL FUSELAGE: CRACK .300" LONG ON WEB OF JAMB DOOR STA 1256 L 16, RT. STOP DRILL CRACK, PERFORMED NDI, INSTALLED REPAIR DOUBLER IAW SRM 53-50-00 FIG 19 VOL I. 2L73 4F A22WE 20051219000292005121900029 2005 12 19 SWIA200515978 420051205A2210 LOGIC CARD CNDAIRCL600 CL6002B19 1900309EA FCC MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07971SW 7947 YD2 INOP, IAPS DEGRADED, FD 2 FAIL STATUS MESSAGES DISPLAYED. REPLACED IOC CARD 2A IAW MM 22-16-06. REPLACED NR 2 FCC CARD IAW MM 22-12-14. OPERATIONAL CHECK GOOD, PN OFF: 622-9815-904 SN OFF: 10BMP PN: 622-9814-008 SN OFF: IGM7N. 2L72 4F RTA21EA 20051219000322005121900032EA 2005 12 19 SWIA200515981 120051129A27515913000 SENSOR CNDAIRCL600 CL6002C10 1390015EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07715SK2631 2631 10179 FLAPS HALFSPEED MSG. REPLACED RT FLAP BPSU. OPERATIONAL CHECK GOOD IAW 27-52-03. 2L72 4F RTA21EA 20051219000432005121900043NM 2005 12 19 SWAA053965 120051214A53306545774 SKIN BOEING737 7373Q8 1384670NM BS 732B-736B CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 732B TO BS 736B, STR 10R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051219000442005121900044NM 2005 12 19 SWAA053966 120051214A53306545775 SKIN BOEING737 7373Q8 1384670NM BS 811-814 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 811 TO BS 814, STR 10R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051219000562005121900056 2005 12 19 SWAA053910 420051208A256565C16820 HOOK BOEING737 7373H4 1384600NM R2 DOOR GIRT BARLOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29398SW 27692 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED HOOK PER MM. 2L72 4F RTA16WE 20051219000692005121900069NM 2005 12 19 SWAA053954 120051213A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29449WN 32469 DURING SCHEDULED HC1 CHECK, FOUND EEPLS TRACK COVERS CRACKED AT ROWS 2, 10 AND 11. REMOVED AND REPLACED COVERS PER MM. 2L72 4F RTA16WE 20051219000832005121900083NM 2005 12 19 USAA051499 120051212A5510 CLEVIS BOEING737 7374B7 1384702NM RT STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 FOUND CORROSION RIGHT STAB CENTER SECTION CLEVIS NR 9 BOTH FACES. SPOT FACE BOTH FAVES, REPLACE BUSHING IAW SRM 55-10-10, DEFECT SIZE: .375". 2L72 4F RTA16WE 20051219001082005121900108NM 2005 12 19 SWAA053924 120051210A53306545776 SKIN BOEING737 7373Q8 1384670NM BS 905 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 905, STR 25R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051219001132005121900113EU 2005 12 19 USAA051526 120051213A5315D5347218920200 FLOORBEAM AIRBUSA321 A321211 3930370EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19164UW 1425 FOUND FLOORBEAM CORRODED, -Y1160 BETWEEN FS 69-FS 70 FLOORBEAM. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-72-11; CORROSION LEVEL 1; TASK JA-260-53500, DEFECT SIZE: 2" X 10". 2L72 4F RTA28NM 20051219001182005121900118NM 2005 12 19 USAA051532 120051213A5310146N852252 STRUCTURE BOEING757 757225 1384959NM BS 1380-1440 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19607AU 22203 FOUND CORROSION STA 1380-1440 AFT CARGO DOOR CUTOUT TORQUE BOX UPPER CAP. PART REPLACED PER SRM 51-40-02. 53-60-15; CORROSION LEVEL 1; TASK NR C53-155-02, DEFECT SIZE: 2.0"L X 1.5"W X .030"D. 2L72 4F RTA2NM 20051219001192005121900119NM 2005 12 19 USAA051520 120051213A5510 BUSHING BOEING737 7374B7 1384702NM HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 FOUND CORROSION R15 CLEVIS FWD AND AFT FACES. REMOVED DAMAGE, FABRICATED AND INSTALLED NEW BUSHING IAW SRM 55-10-1, DEFECT SIZE: .250 DIA SPOTS OF CORROISON. 2L72 4F RTA16WE 20051219001302005121900130WP 2005 12 19 ABXA050354 120051127A5320 STIFFENER DOUG DC8 DC863F 302198FWP BS 940 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING REMOVAL OF LEFT LONGERON, STIFFENER AT STA 940, LONGERON 24 LEFT, LEFT WHEEL WELL, WAS FOUND CRACKED ON BOTTOM OF BASE. FABRICATED NEW STIFFENER FOR STA 940, LONGERON 24 LEFT IAW REA D853-52556, PO NR 1123110. 2L74 4F 4A25 20051219001362005121900136NM 2005 12 19 USAA051519 120051213A5510 BUSHING BOEING737 7374B7 1384702NM HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 FOUND CORROSION, R13 CLEVIS FWD AND AFT FACES OF BUSHING. REMOVED DAMAGE, FABRICATED AND INSTALLED NEW BUSHING IAW SRM 55-10-10, DEFECT SIZE: .250 DIA SPOTS OF CORROSION. 2L72 4F RTA16WE 20051219001412005121900141EU 2005 12 19 AWXA200501500 120051211A3350P4010021000 BATTERY AIRBUS320 A320231 3930325EU AFT GALLEY INOPERATIVE A AWXAO OTHER O OTHER TXTAXI/GRND HDL 1 WP28637AW 099 PHX - EEL - CREW REPORTED THAT THE AFT LEFT GALLEY EMERGENCY FLASHLIGHT WAS LOSING ITS CHARGE. MAINTENANCE REMOVED AND REPLACED THE AFT LEFT EMERGENCY FLASHLIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA28NM 20051219001422005121900142NM 2005 12 19 AWXA200501501 120051116A5311654630153 FRAME BOEING737 73733A 1384673NM BS 188 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 MCN - DURING C19 CHECK DISCOVERED BS 188 FRAME CRACKED, 2.0 INCHES, IN THE OUTBOARD RADIUS AT WL 208 AND BL 31L. MAINTENANCE TRIMMED OUT CRACK IAW BOEING 737-300 SRM 53-00-07 FIG 201. FABRICATED REPAIR ANGLE AND FILLERS IAW BOEING 737-300 SRM 53-00-07 FIG 201. INSTALLED FABRICATED REPAIR PARTS AT WL 208, BS 188 AND WL 208 IAW BOEING 737-300 SRM 53-00-07 FIG 201 AND AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5300-05333-HF2. 2L72 4F RTA16WE 20051219001502005121900150EU 2005 12 19 ASOA05984 120051102A5320 ANGLE AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27643AS 413 DURING A C-CHECK IN YUL, THE ANGLE AT FS 39, BETWEEN STRINGER 21R-21L WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED THE ANGLE AT FS 39, BETWEEN STRINGER 21R-21L, IAW SRM 51-21-42 AND REPLACED THE ANGLE AT FS 39, BETWEEN STRINGER 21R-21 IAW SRM 51-25-04. (M) 2H72 4T RTA53EU 20051219001582005121900158NM 2005 12 19 USAA051514 120051213A5510 BUSHING BOEING737 7374B7 1384702NM HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 FOUND CORROSION R2 DUG AFT BUSHING FWD FACE. REMOVED DAMAGE, FABRICATED AND INSTALLED NEW BUSHING IAW SRM 55-10-10, DEFECT SIZE: .250 DIA SPOTS OF CORROSION. 2L72 4F RTA16WE 20051219001612005121900161EU 2005 12 19 USAA051548 120051213A5320D5311146100200 FLOOR SUPPORT AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19113UW 1141 FOUND CORROSION Y-254 FRAME C-16 TO C-18. FAB'D AND INSTALLED TOP FILLER AND TWO ANGLE DOUBLERS PER SRM 53-00-14; CORROSION LEVEL 1; TASK JA-220-53500 DEFECT SIZE: 4" X 3". 2L72 4F RTA28NM 20051219001622005121900162EU 2005 12 19 USAA051547 120051213A5340 FITTING AIRBUS320 A320214 3930316EU DOOR SILL CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19113UW 1141 FOUND CORROSION AFT SVC DOOR SILL BEAM AT C66 AND Y1400. INSTALLED DOUBLERS PER SRM 53-41-14; CORROSION LEVEL 1; TASK JA-260-53500, DEFECT SIZE: 1/2" X 1-1/2" LONG. 2L72 4F RTA28NM 20051219001702005121900170NM 2005 12 19 DHL2005765518 120051212A5311 FRAME BOEING727 727264 138408MNM BS 1010 CORRODED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15765AT 23014 AFT CARGO COMPT BILGE, BS 1010 FRAME CORRODED AT LOWER FWD SIDE BETWEEN STR 29R - 30. CUT OUT CORRODED AREA. FABRICATED AND INSTALLED REPAIR 5.25" BY 5.25" BY 3.75" BY .75" FROM 7075-T6 .071 IAW B727 SRM 53-10-4 FIG 13. 2L73 4F A3WE 20051219001762005121900176NM 2005 12 19 AWXA200501523 120051130A5320654541041 WEB BOEING737 73733A 1384673NM BS 706 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 MCN - DURING C19 CHECK DISCOVERED VERTICAL WEB CRACKED AT BS 706, BL 25R AND WL 206. REMOVED DAMAGE SECTION ON VERTICAL WEB IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NO. 03-5700-05346-HF2. FABRICATED WEB, STIFFENERS, FILLERS AND REINFORCING DOUBLER IAW AWA ER NO. 03-5700-05346-HF2. INSTALLED FABRICATED REPAIR PARTS ON VERTICAL WEB AT BS 706, BL 25R, AND WL 206 IAW AWA ER NO. 03-5700-05346-HF2. 2L72 4F RTA16WE 20051219001772005121900177NM 2005 12 19 AWXA200501524 120051119A5320654583340 WEB BOEING737 73733A 1384673NM BS 178-188 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 MCN - DURING C19 CHECK DISCOVERED SHEAR WEB CRACKED, 2.2 INCHES, FROM BS 178 TO BS 188 AND FROM BL 24R TO BL 30R, WL 208. MAINTENANCE REMOVED CRACKED SHEAR WEB IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NO. 03-5300-05341-ES1. FABRICATED SHEAR WEB IAW AWA ER 03-5300-05341-ES1. INSTALLED FABRICATED REPAIR PARTS FROM BS 178 TO BS 188, BL 24R TO BL 30R, AND WL 208 IAW AWA ER 03-5300-05341-ES1. 2L72 4F RTA16WE 20051219001782005121900178NM 2005 12 19 AWXA200501525 120051113A575465C26601173 SKIN BOEING737 73733A 1384673NM NR 1 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 A 5.25 INCH CRACK WAS DISCOVERED ON THE NR 1 SLAT LOWER SKIN FROM SS254.75R TO SS 260R. DAMAGE WAS PLACED ON MONITOR TO BE REPAIRED WITHIN 24 MONTHS. MAINTENANCE TRIMMED OUT DAMAGED AREA ON THE NR 1 SLAT LOWER SKIN IAW BOEING 737-300 SRM 57-43-01-2R6. FABRICATED FILLER AND SPLICE PLATE IAW BOEING 737-300 SRM 57-43-01-2R6. INSTALLED FABRICATED REPAIR PARTS ON THE NR 1 SLAT LOWER SKIN FROM SS 254.75R TO SS 260R IAW BOEING 737-300 SRM 57-43-01-2R6. 2L72 4F RTA16WE 20051219001832005121900183NM 2005 12 19 SWAA053945 120051212A53156545410 FLOORBEAM BOEING737 7375H4 138449DNM BS 660 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29511SW 24188 DURING SCHEDULED 1/2D CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 660, BL 0. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20051219001852005121900185NM 2005 12 19 SWAA053947 120051213A53306545769 SKIN BOEING737 7373A4 1384585NM BS 426-446 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 426 TO BS 446, STR 28L TO STR 28R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051219001982005121900198EA 2005 12 19 VNAA0511011 120051114A750020035008067 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE BLEED AIR UNSERVICEABLE A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL05258PS3073 7941 AFTER TAKEOFF THE L 14TH DUCT WARNING MESSAGE ILLUMINATED. THE CREW FOLLOWED THE QRH, RETURNED TO PIT, AND MADE AN UNEVENTFUL OVERWEIGHT LANDING. MAINTENANCE TROUBLESHOT THE SYSTEM AND FOUND NO DISCREPANCIES. THE LT BLEED AIR LEAK CONTROL UNIT WAS REMOVED AND REPLACED IAW CRJ200 AMM 36-21-10-000(400)-801. THE SYSTEM OPERATIONALLY CHECKED GOOD. AN OVERWEIGHT LANDING INSPECTION WAS PERFORMED IAW CRJ200 AMM 05-51-01-210-801. NO DISCREPANCIES WERE FOUND. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20051219001992005121900199EA 2005 12 19 VNAA0511012 120051114A2611 FIRE LOOP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT PYLON OUT OF POSITION A VNAAA UNSCHED LANDING N FALSE WARNING DEDESCENT 1 GL05257PS 7939 THE RT 14TH DUCT WARNING MESSAGE ILLUMINATED. THE CREW FOLLOWED THE QRH, DIVERTED TO ILH, AND MADE AN UNEVENTFUL LANDING. THE AIRCRAFT WAS FERRIED TO CLT WHERE MAINTENANCE TROUBLESHOT THE SYSTEM IAW CRJ200 FIM 36-20-00. THE RT PYLON LOOPS WERE INSPECTED AND REPOSITIONED. EXTENSIVE GROUND RUN-UP AND OPERATIONAL CHECKS WITH ALL PNEUMATIC SYSTEMS ON WERE PERFORMED. NO FAULTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20051219002012005121900201EA 2005 12 19 VNAA0511014 120051115A3260 TARGET CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PROX SENSOR LOOSE A VNAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL05260JS 7957 AFTER TAKEOFF WITH THE GEAR HANDLE SELECTED UP THE GEAR DISAGREE WARNING MESSAGE ILLUMINATED. THE RIGHT MAIN LANDING GEAR DID NOT SHOW LOCKED IN THE UP POSITION. THE CREW FOLLOWED THE QRH, RETURNED TO TYS, AND MADE AN UNEVENTFUL LANDING. THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE FOUND THE RT MLG UPLOCK PROX SENSOR TARGET LOOSE. THE TARGET WAS ADJUSTED AND SECURED IAW CRJ200 AMM 32-61-05. A LANDING GEAR EXTENSION/RETRACTION FUNCTIONAL TEST WAS PERFORMED IAW CRJ 200 AMM 32-30-00-720-801. THE SYSTEM CHECKED GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20051219002042005121900204EA 2005 12 19 VNAA0511016 120051116A3000 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE ANTI ICE TEMP MALFUNCTIONED A VNAAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL05216PS 7882 THE ANTI-ICE DUCT WARNING MESSAGE ILLUMINATED WHEN WING ANTI-ICE WAS SELECTED ON. THE LEFT WING INDICATED OVERHEAT ON THE ANTI-ICE SYNOPTIC PAGE. THE CREW FOLLOWED THE QRH AND MADE AN UNEVENTFUL LANDING AT THEIR DESTINATION. MAINTENANCE REMOVED, INSPECTED, AND REINSTALLED ALL ANTI-ICE PICCOLO TUBES IN THE LEFT WING. NO DISCREPANCIES WERE FOUND. THE ANTI-ICE TEMPERATURE CONTROLLER AND THE LT 14TH STAGE BLEED AIR PRESSURE SWITCH WERE REMOVED AND REPLACED. THE BLEED LEAK DETECTION CONTROL UNITS WERE SWAPPED. THE WING ANTI-ICE SYSTEM LEAK AND OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20051219002062005121900206 2005 12 19 SWAA053974 420051215A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29472WN 33831 R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR WOULD NOT ENGAGE IN FLOOR FITTINGS. REMOVED AND REPLACED SLIDE PER MM. 2L72 4F RTA16WE 20051219002072005121900207NM 2005 12 19 SWAA053975 120051215A53306545776 SKIN BOEING737 7375H4 138449DNM BS 931 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29511SW 24188 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 931, STR 25R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051219002082005121900208NM 2005 12 19 SWAA053976 120051215A534065C27314 STRINGER CLIP BOEING737 7375H4 138449DNM BS 663 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29511SW 24188 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051219002272005121900227NE 2005 12 19 05FDEA04243 220051212A7261AVB731817 FITTING DOUG DC10 DC1030F 3023504WP GE CF6 CF650C2 30018NE NR 2 PYLON FAILED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25303FE 46802 REMOVED NR 2 ENG REF W/C 71T1101 WHILE LOWERING ENGINE AFT LT MOUNT BROKE, TEARING WEB AND CRACKED ANGLES ALSO BOTH T/R HALVES DAMAGED. TURNED OVER TO DAY SHIFT FOR FURTHER EVALUATION. REPLACED WEB AND FITTINGS AS REQUIRED REF DWG AVB7318 AND SRM 51-00-01 RII:271980. 2L73 4F4 FRTA22WE E23EA 20051219002342005121900234NM 2005 12 19 ASAA0510319 120050922A55316549559506 CLEVIS BOEING737 737290C 138448VNM VERTICAL STAB CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02740AS 22578 YXX - FOUND CORROSION ON VERTICAL STABILIZER AFT SPAR RIGHT PRIMARY AFT CLEVIS AFT FACE. CLEVIS REPLACED PER EA 5340-01137. (M) 2L72 4F A16WE 20051219002402005121900240SO 2005 12 19 SIMA200528309 120051007A3320BR900002 BALLAST EMB 145 EMB145LR 3260212SO CABIN BURNED A SIMAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 SW21641AE 145191 BURNING SMELL COMING FROM FRONT VENT OVER FLIGHT ATTENDANT LIGHT CONTROL. REPLACED CEILING LIGHT BALLAST AT SEAT 1A. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20051219002462005121900246SO 2005 12 19 SIMA200530103 120051025A532013500469403 PROFILE EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21720AE 145279 SAW - DURING MBV INSPECTION, FOUND PROFILE Z AT FRAME 22 IS CORRODED. INSTALLED NEW PROFILE Z IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20051219002482005121900248SO 2005 12 19 SIMA200530105 120051025A783014578068002 SKIN EMB 135 EMB135LR 3260305SO THRUST REVERSER PEELING A SIMAK NONE O OTHER ININSP/MAINT 1 SW21720AE 145279 DURING MBV INSPECTION, FOUND RIGHT THRUST REVERSER OUTBOARD MIDDLE SKIN PEELING BACK ON LEADING EDGE. INSTALLED NEW RIGHT THRUST REVERSER OUTBOARD MIDDLE SKIN IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20051219002492005121900249SO 2005 12 19 SIMA200529704 120051019A532014522178005 SILL EMB 145 EMB145 3260210SO FUSLEAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21612AE 145079 ABI - THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED SERVICE DOOR CENTER SILL. INSTALLED SERVICEABLE SILL IAW EMB SRM, SRM 145/1142 REV 31, CHAPTER 51-40-02. (M) 2L72 4F RTT00011AT 20051219002622005121900262WP 2005 12 19 AALA20050808 120051208A2150 ACM DOUG DC9 DC982 3022082WP LT AND RT INOPERATIVE A AALAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SW21582AA 53159 JFK - AIR INTERRUPTED TO JFK DUE TO STRONG ODOR OF OIL AND SMOKE THROUGHOUT CABIN AND COCKPIT. LANDED JFK WITHOUT INCIDENT. PULLED COALESCER BAGS AND FOUND OIL. REPLACED LEFT AND RIGHT HAND PACK AIR CYCLE MACHINE AND COALESCER BAGS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051219002742005121900274GL 2005 12 19 C2XA05CL089 220051023A726123070366 CARBON SEAL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 1 ENGINE FAILED A C2XAO OTHER KBJFLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SW2712569 145630 CAE312203 CLE FLIGHT 2201 - THE CREW REPORTED DURING CLIMB AND DESCENT THERE WAS A OIL ODOR IN THE COCKPIT AND CABIN. MAINTENANCE REPLACED THE NR 1 ENGINE. OPERATIONAL CHECKS WERE GOOD. SUPPLEMENT THE NR 4 CARBON SEAL WAS FOUND TO BE THE CAUSE OF OIL ODOR. 2L72 4T4 FRTT00011ATTE6CH 20051219002812005121900281NM 2005 12 19 DHL2005749026 120051107A5347 SEAT TRACK BOEING727 727200 138407ENM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01749DH 22013 FOUND CORROSION ON SEAT TRACK AT RBL24 BS 770-800. CLEANED CORROSION IAW B727 SRM 51-0-6 AND FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 3. REMOVED SEAT TRACK SECTION AT RBL 24 BS 757-852 IAW B727 SRM 51-30-2 TREAT AT PRIMED AREA IAW B727 SRM 51-10-2. FABRICATED TRACK SECTION FROM BS 757-852 RBL 24 MAT USED BAC1520-841 PO 9002277 DIM 95 IAW B727 SRM 53-10-5 FIG 2. INSTALLED SEAT TRACK SECTION AT BS 757-852 RBL 24 IAW B727 SRM 51-30-2 AND 53-10-5 FIG 2. 2L73 4F RTA3WE 20051219002832005121900283EA 2005 12 19 ASOA05942 120051101A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA PAX DOOR UNKNOWN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27855AS 7395 DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WAS DIFFICULT TO OPEN. MAINTENANCE OPENED AND CLOSED THE PASSENGER DOOR. NO DEFECTS NOTED. OPERATIONAL CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051219002932005121900293EA 2005 12 19 ASOA05926 120051028A5347 CARGO TRACK CNDAIRCL600 CL6002B19 1900309EA CARGO BAY CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27838AS 7276 DURING A C-CHECK IN MCN, THE CARGO COMPARTMENT SEAT TRACKS WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACE THE CARGO COMPARTMENT SEAT TRACKS. (M) 2L72 4F RTA21EA 20051219003012005121900301EA 2005 12 19 ASOA05917 120051027A5320601R3117117 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27838AS 7276 DURING A C-CHECK, THE LT IB CLIP AT FS 484, LBL 27 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LT IB CLIP AT FS 484, LBL 27 IAW EO 600-53-0098. 2L72 4F4 FRTA21EA E15NE 20051219003042005121900304EA 2005 12 19 ASOA05961 120051108A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA EXTERIOR INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27901EV 7618 DURING A GROUND INSPECTION IN MGM, THE EXTERIOR EMERGENCY LIGHT, ABOVE THE RIGHT WING, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EXTERIOR EMERGENCY LIGHT, ABOVE THE RIGHT WING. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051219003052005121900305EA 2005 12 19 ASOA05962 120051109A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27924EV 7830 FLT 4260 - DURING A GROUND INSPECTION IN VPS, THE EMERGENCY LIGHT, ABOVE ROW 2, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY LIGHT, ABOVE ROW 2. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051219003062005121900306EA 2005 12 19 ASOA05963 120051102A5260601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27928EV 8006 DURING A HANGAR INSPECTION IN MCN, THE PASSENGER DOOR BOTTOM STEP, AT THE STAY ROD ATTACH BRACKET, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE PASSENGER DOOR BOTTOM STEP, AT THE STAY ROD ATTACH BRACKET, IAW CRJ SRM 51-73-00. OPS CHEKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051219003122005121900312EA 2005 12 19 ASOA05969 120051111A5210601R380743 ANCHOR FITTING CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27870AS 7500 DURING A C-CHECK IN MCN, THE PASSENGER DOOR FORWARD ANCHOR FITTING WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACE THE PASSENGER DOOR FORWARD ANCHOR FITTING. (M) 2L72 4F RTA21EA 20051219003132005121900313EA 2005 12 19 ASOA05970 120051111A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27870AS 7500 DURING A C-CHECK IN MCN, THE LEFT FS 640 FRAME ANGLE, INSIDE THE LEFT BOX BEAM ACCESS PANEL, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACED THE LEFT FS 640 FRAME ANGLE, INSIDE THE LEFT BOX BEAM ACESS PANEL. (M) 2L72 4F RTA21EA 20051219003152005121900315EA 2005 12 19 ASOA05972 120051111A5210 ANCHOR FITTING CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27900EV 7608 DURING A HANGAR INSPECTION IN MCN, THE PASSENGER DOOR FORWARD ANCHOR FITTING WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR FORWARD ANCHOR FITTING (P/N 601R380742) AND LEVER (P/N 601R319742). OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051219003172005121900317EA 2005 12 19 ASOA05974 120051112A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27870AS 7530 DURING A C-CHECK IN MCN, THE RIGHT INBOARD FS 280 CLIP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT INBOARD FS 280 CLIP IAW CRJ200 SRM 51-42-00. (M) 2L72 4F RTA21EA 20051219003212005121900321EA 2005 12 19 ASOA05978 120051114A5260601R319805 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27837AS 7271 FLT 9970 - DURING A HANGAR INSPECTION IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND TO BE BROKEN. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051219003232005121900323EA 2005 12 19 ASOA05980 120051114A335020131A BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA CABIN DISCHARGED A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27881AS 7496 DURING A HANGAR CHECK IN MCN, THE EMERGENCY LIGHTS AT THE PASSENGER DOOR AND OVERHEAD IN THE CABIN WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051219003282005121900328WP 2005 12 19 IXXA0500138S 120050304A5753 PANEL DOUG DC8 DC871F 302199DWP T/E FLAP DENTED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11821BX858952998 45811 DURING A ROUTINE C CHECK INSPECTION, FOUND RT WING OUTBOARD FLAP AFT PANEL DENT DAMAGE BETWEEN STA XF 304.000-XF 333.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF DAMAGED PLATING. FABRICATED NEW PLATING, CLEANED, TREATED AND PRIMED AREA + INNER FACE ON NEW PLATING. APPLIED SEALANT TO FAYING SURFACES. INSTALLED NEW PLATING IAW DC8 SRSM 57-7-0 PG 1, 57-7-1 FIG 4 TR # 57-94, 51-1-21, 51-3-0, 51-3-1. 2L74 4F RT4A25 20051219003302005121900330EA 2005 12 19 COMA0560678 120051207A2751 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA COCKPIT ACTIVATED A COMAK NONE J WARNING INDICATION APAPPROACH 1 SO01713CA 7245 FLIGHT 5457 - DURING DCA APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE, FLIGHT LANDED WITHOUT INCIDENT. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2L72 4F RTA21EA 20051219003322005121900332EU 2005 12 19 ASOA05987 120051031A5315 FLOORBEAM AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27643AS 413 DURING A C-CHECK IN YUL, FLOORBEAM 41, AT BL 0, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED FLOORBEAM 41, AT BL 0, IAW ASA EO 72-53-0174. (M) 2H72 4T RTA53EU 20051219003342005121900334EU 2005 12 19 ASOA05989 120051028A5311 FRAME AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27643AS 413 DURING A C-CHECK IN YUL, FRAME FRAME 23A, AT STRINGER 21R AND STRINGER 21L, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED THE CORROSION ON FRAME FS 23A, AT STRINGER 21R AND STRINGER 21, IAW SRM 51-21-42. REPAIRED FRAME FS 23A, AT STRINGER 21R AND STRINGER 21L IAW ASA EO 72-53-0199. (M) 2H72 4T RTA53EU 20051219003362005121900336EU 2005 12 19 ASOA05991 120051028A5315 FLOORBEAM AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27643AS 413 DURING A C-CHECK IN YUL, THE FLOORBEAM AT FS 38, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM, AT FS 38, IAW ASA EO 72-53-0171. (M) 2H72 4T RTA53EU 20051219003382005121900338EU 2005 12 19 ASOA05993 120051028A5315 FLOORBEAM AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27643AS 413 DURING A C-CHECK IN YUL, THE FLOORBEAM AT FS 40 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM, AT FS 40, IAW ASA EO 72-53-0173. (M) 2H72 4T RTA53EU 20051220000182005122000018EU 2005 12 20 05FDEA04211 120051209A5610 WINDSHIELD AIRBUS300 A300B4605R 3930308EU COCKPIT CRACKED A FDEAA UNSCHED LANDING O OTHER CRCRUISE 1 SO25671FE 778 RT WINDSHIELD CRACKED. REMOVED AND REPLACED RT WINDSHIELD PANEL PER A300 AMM 56-11-11-4. NEEDS SEALANT CURE CHECK, WINDSHIELD WIPER INSTALLED AND OPS CHECK. 2L72 4F RTA35EU 20051220000192005122000019NM 2005 12 20 05FDEA04212 120051209A5343AEA7051501 FITTING DOUG MD11 MD11 3023602NM ZONE 700 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 UPON REMOVAL OF CLG SHOCK STRUT ASSY FOUND WHEEL WELL SIDE LT TRUNNION FITTING LOWER MATING SURFACE WITH CORROSION. LT TRUNNION FITTING LOWER MATING SURFACE CORROSION REMOVED AND REPAIR CARRIED OUT AS PER FEDEX EA1-5340-90705, TITLE: FUSELAGE CENTER LANDING GEAR LT SUPPORT FITTING CORROSION REPAIR. 2L73 4F RTA22WE 20051220000242005122000024EA 2005 12 20 COMA0560715 120051212A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS WARNING LIGHT A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01927CA 7031 FLIGHT 5151 - DURING JFK APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE AT 20 DEGREES. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE FIRST EVENT, MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2L72 4F RTA21EA 20051220000252005122000025WP 2005 12 20 AALA20050806 120051207A3213 STRUT DOUG DC9 DC983 3022083WP NLG INOPERATIVE A AALAA UNSCHED LANDING O OTHER CLCLIMB 1 SW219622A 53593 ORD - NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF, HAD RED NOSE GEAR LIGHT ON WITH HANDLE UP. GEAR EXTENDED OK. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. AIRCRAFT TAKEN OUT OF SERVICE. FOUND NOSE STRUT NEEDED SERVICE. SERVICED NOSE STRUT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20051220000262005122000026GL 2005 12 20 C2XA05TY055 220051014A720023061402 BEVEL GEAR EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL ENGINE FAILED A C2XAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 SW27125288248 8248 145504 CAE310083 FLT 3251 - AT FL350 ENGINE NR 1 FAILED WITH NO INDICATIONS. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE ASSY, COMPLIED WITH OPERATIONAL CHECKS AND ACFT WAS RELEASED TO SERVICE. *S/D* TEARDOWN REPORT: CAUSE OF THE UNCOMMANDED IN FLIGHT SHUTDOWN WAS A BEVEL GEAR FAILURE. 2L72 4F4 FRTT00011ATTE6CH 20051220000272005122000027EU 2005 12 20 DXTA200501129 120051205A3243 MASTER CYLINDER BRAERO1000 HAWKER1000 7450005EU BRAKES MALFUNCTIONED E DXTAA UNSCHED LANDING S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07552QS 259052 UPON LANDING, CAPTAINS BRAKE PEDALS ARE SPONGY & PEDALS TEND TO GO TO THE FLOOR IN ORDER TO STOP THE AIRCRAFT. BRAKES CHECKED NORMAL ON TAXI OUT PRIOR TO DEPARTURE. BLED (4) BRAKE MASTER CYLINDERS TO THE BRAKE CONTROL VALVE, NJA CREW PERFORMED TAXI CHECK. OPS CHECKED GOOD. WORK PERFORMED IAW HAWKER 1000 M/M CHAP 32-40-00. 2L72 4F RTA3EU 20051220000282005122000028CE 2005 12 20 DXTA200501130 120051205A3310E125R1351 RHEOSTAT CESSNA750 750 2076810CE MAP LIGHT FAILED E DXTAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07975QS 7500175 WHEN PILOT SIDE MAP LIGHT RHEOSTAT IS TURNED TO THE OFF POSITION SMOKE STARTS COMING FROM THE BACK SIDE OF THE ASSEMBLY, WHEN TURNED ON THE SMOKE STOPS. REMOVED AND REPLACED RHEOSTAT, OPS CHECK GOOD, NO SMOKE. WORK DONE IAW C750 MM 33-10-00. 2L72 4J RTT00007WI 20051220000292005122000029CE 2005 12 20 DXTA200501131 120051206A3260602751 POSITION SWITCH CESSNA750 750 2076810CE RT MLG FAULTY E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07978QS 7500187 UPON TAKEOFF RIGHT MAIN GEAR LIGHT WOULD NOT EXTINGUISH (NO UNSAFE LIGHT OR HORN). RECYCLED GEAR SEVERAL TIMES AND LIGHT WOULD STAY ON MIDWAY TO DIVERSIONARY AIRPORT THE LIGHT EXTINGUISHED. REMOVED FAULTY RT DOWNLOCK SWITCH. INSTALLED NEW, OPS CHECK GOOD IAW C750 MM 32-30-04. 2L72 4J RTT00007WI 20051220000312005122000031CE 2005 12 20 DXTA200501132 120051205A275099145104 RESOLVER CESSNA750 750 2076810CE TE FLAPS MALFUNCTIONED E DXTAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL07944QS136 7500144 FLAPS FAIL CAS MESSAGE / SLATS DEPLOYED. FLAPS FAILED APPROX 1 DEGRESS 14,000 FT MSL 230 KIAS. SLOWED TO 180 KIAS STILL FAIL. PERFORMED FLAP SYSTEM OPS CHECK & COULD NOT FIND ANY FAULTS. REMOVED & REPLACED LT & RT FLAP RESOLVERS IAW CE-750 MM CH 27-52-00. PERFORMED FLAP SYSTEM RIGGING & OPS CHECK IAW CE-750 MM CH 27-50-00. OPS CHECKS GOOD. 2L72 4J RTT00007WI 20051220000322005122000032CE 2005 12 20 DXTA200501134 120051208A3240 BRAKE ASSY CESSNA500 560CESSNA 2076750CE MLG MALFUNCTIONED E DXTAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07312QS 5600312 CO-PILOTS BRAKES DURING LANDING ARE SPONGY, GO ALMOST TO FLOOR AND WHEN BRAKES GRAB, THE AIRPLANE TURNS TO THE RIGHT. PERFORMED BRAKE BLEEDING PROCEDURES IAW CE560 MM 32-42-00. PERFORMED SATISFACTORY OPS & LEAK CHECK. 2L72 4F RTA22CE 20051220000332005122000033GL 2005 12 20 C2XA05IA118 220051021A724023073795 TURBINE BLADES EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL RT ENGINE FAILED A C2XAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 SW2716987 145261 CAE312016 IAH - FLIGHT 2010, THE CREW REPORTED AN UNCOMMANDED ENGINE SHUT DOWN IN FLIGHT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20051220000342005122000034WP 2005 12 20 AALA20050807 120051208A4990 OIL SYSTEM DOUG DC9 DC982 3022082WP APU LEAKING A AALAO OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 SW21951U 49245 ORD - COMING IN FOR LANDING AT ABOUT 2000 FEET SMELLED AN UNIDENTIFIED ODOR. AFTER LANDING FLIGHT ATTENDANTS INFORMED CREW OF A LITE HAZY SMOKE IN THE CABIN. SHUT OFF THE WING AND ENGINE ANTI-ICE AND THE SMOKE SUBSIDED. SUSPECT OIL LEAKING INTO APU INLET. REPLACED APU. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051220000352005122000035WP 2005 12 20 AALA20050809 120051209A3244 TIRE DOUG DC9 DC983 3022083WP MLG FAILED A AALAO OTHER O OTHER LDLANDING 1 SW219616G 53563 SFO - NUMBER ONE MAIN TIRE BLOWN ON LANDING. ANTI SKID AND WHEEL NOT TURNING LIGHTS CAME ON. REPLACED NUMBER ONE AND NUMBER TWO WHEEL ASSEMBLY AND TIRES. REPLACED WHEEL SPEED TRANSDUCER. NO OTHER DAMAGE NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20051220000362005122000036EA 2005 12 20 COMA0560711 120051211A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01927CA 7031 FLIGHT 4958 - LT THRUST REVERSER UNLOCKED MESSAGE. DEFERRED MAINTENANCE PER MEL. 2L72 4F RTA21EA 20051220000372005122000037EA 2005 12 20 COMA0560712 120051211A325016900105 ECU CNDAIRCL600 CL6002B19 1900309EA LT ENGINE MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 SO01966CA2519342 7132 FLIGHT 9451 - NOSE WHEEL STEERING INOP CAUTION. REPLACED LT AND RT RVDT'S AND THE ECU. 2L72 4F RTA21EA 20051220000382005122000038EA 2005 12 20 COMA0560716 120051213A5312 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA BS 621 LBL45 DAMAGED A COMAK NONE O OTHER ININSP/MAINT 1 SO01721CA18482 7259 HOLE IN AFT PRESSURE BULKHEAD FS 621 AND LBL 45. INSTALLED RIVET IN FS 621 AND LBL 45 AFT PRESSURE BULKHEAD IAW SRM 51-12-00 PG 21, SMALL HOLE REPAIR. 2L72 4F RTA21EA 20051220000392005122000039EA 2005 12 20 COMA0560713 120051211A27507455001 CONTROL HANDLE CNDAIRCL600 CL6002B19 1900309EA INST PANEL MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01796CA1268 7338 FLIGHT 5076 - FLAPS FAIL CAUTION. REPLACED THE FLAP CONTROL LEVER. 2L72 4F RTA21EA 20051220000402005122000040GL 2005 12 20 C2XA05BT078 220051103A720023070930 HEAT SHIELD EMB 145 EMB145XR 3260214SO ALLSN AE300 AE3007A GL NR 1 ENGINE BROKEN A C2XAK NONE O OTHER ININSP/MAINT 1 SW2718120 145681 CAE312498 DURING ROUTINE CHECK MAINTENANCE FOUND THE NR 1 ENGINE REAR TURBINE BEARING SUPPORT HEAT SHIELD BROKEN, DAMAGED TWO REAR TURBINE BEARING SUPPORT STRUTS/PYLONS (P/N 23077731). THE 11 O`CLOCK POSITION STRUT HAD BEEN CUT 0.25 INCHES THROUGH AND THE 1 O`CLOCK POSITION STRUT WAS CHAFED, BATTERED, AND CUT THROUGH IN VARIOUS PLACES. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE IAW EXPRESSJET TASKCARD 6271001 AND EMB145 XR MM 71-00-00. OPS AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRT TE6CH 20051220000412005122000041SO 2005 12 20 C2XA05BT079 120051105A49204504113 APU EMB 145 EMB145XR 3260214SO TAILCONE FAULTY A C2XAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW27131243892 3892 145689 CREW REPORTED, WHILE TAXIING WITH BOTH ENGINES RUNNING, COCKPIT CREW NOTICED AN ODOR FOLLOWED BY WHITE SMOKE IN COCKPIT. SHORTLY AFTER, FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN. THERE WERE NO INDICATIONS ON THE EICAS. AIRCRAFT RETURNED TO THE GATE. THE AIRCRAFT WAS RELEASED IAW MEL 49-00-00 CATEGORY-C CONTROL NUMBER 061926. AIRCRAFT RETURNED TO SERVICE. APU REMOVED AND REPLACED BY SDF MAINTENANCE, OPS CHECK GOOD. MEL CLEARED, AIRCRAFT RETURNED TO SERVICE. APU P/N INSTALLED 4504113, S/N INSTALLED SP-E0214296. 2L72 4F RT 20051220000422005122000042NM 2005 12 20 SWAA053950 120051213A53306545765 SKIN BOEING737 7373H4 1384600NM BS 454 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 454, STR 16R. REMOVED AND REPLACED SIDE SKIN PANEL BETWEEN BS 360 TO BS 540, STR 14R TO STR 19R PER BFG ER. 2L72 4F RTA16WE 20051220000432005122000043NM 2005 12 20 SWAA053932 120051212A53306545768 SKIN BOEING737 7373H4 1384600NM BS 347 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 347, STR 2L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051220000442005122000044NM 2005 12 20 SWAA053933 120051212A53306545774 SKIN BOEING737 7373H4 1384600NM BS 780 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 780, STR 18L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051220000452005122000045NM 2005 12 20 SWAA053934 120051212A53306545774 SKIN BOEING737 7373H4 1384600NM BS 727D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 20L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051220000462005122000046NM 2005 12 20 SWAA053935 120051212A53306545776 SKIN BOEING737 7373H4 1384600NM BS 927 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 23R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051220000502005122000050SO 2005 12 20 SIMA200530108 120051025A27503635001001 FLAP SYSTEM EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL TE FLAPS STUCK A SIMAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SW21643AE 145200 CREW REPORTED AFTER TAKEOFF DURING FLAP RETRACTION THEY RECEIVED A FLAP FAIL MESSAGE. REPLACED RT FLAP TRANSMISSION BRAKE. OPERATIONAL CHECK GOOD, AC RETURNED TO SERVICE. (K) 2L72 4T4 FRTT00011ATTE6CH 20051220000512005122000051SO 2005 12 20 SIMA200530107 120051021A531114526246003 FLANGE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FRAME 68 CRACKED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21659AE4875 145762 FRAME 68 IB FLANGE WAS FOUND TO BE CRACKED AT THE CARGO DOOR OPEN ROD CUP. CUT OUT THE CRACKED AREA OF THE FRAME. PREPARED A REPAIR SECTION OF NEW FRAME. FABRICATED 2 FRAME SPLICES AND REPAIR ANGLE. REPAIR DONE IAW SRM. (K) 2L72 4T4 FRTT00011ATTE6CH 20051220000592005122000059SO 2005 12 20 SIMA200530402 120051026A531014521713003 BEAM EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL FR 25 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21610AE 145073 DURING INSPECTION OF FUSELAGE CENTER BEAM AT FRAME 25 WAS FOUND TO BE CORRODED. PERFORMED A CUT OUT OF CORRODED AREA. FABRICATED A DOUBLER, FILLER AND 2 SHIM. REPAIR DONE IAW SRM. (K) 2L72 4F4 FRTT00011ATTE6CH 20051220000602005122000060EA 2005 12 20 A6WA200540335 120051128A2710601R9002061 CONTROL CABLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE AILERONS FRAYED A A6WAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 GL31425AW 7663 SPOILERON FAULT, AILERON FEELS ROUGH WHEN TURNED TO THE RIGHT. AC HAS FRAYED AILERON CABLES DUE TO INCORRECT INSTALLATION, REPLACED CABLES. 2L72 4F4 FRTA21EA E15NE 20051220000612005122000061CE 2005 12 20 TIM2005F00010 120051003A29101145802271 LINE BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA LT WING HYD LEAKING E TIMAO OTHER O OTHER NRNOT REPORTED 1 NM07195GA UB65 NOSE GEAR WARNING LIGHT ILLUMINATED WHEN LANDING GEAR EXTENDED. GEAR DEPLOYED AFTER 15 TO 20 SECONDS. PROBLEM WAS A LEAK IN THE HYDRAULIC LINE. THE LINE DEVELOPED A PIN HOLE LEAK BECAUSE OF CORROSION FROM THE INSIDE OF THE LINE. (K) 2L72 4T4 TRTA24CE E4EA 20051220000642005122000064EA 2005 12 20 A6WA200540332 120051121A53206013501251 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE BS 621-625.3 CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31427ZW 7685 LT SIDE FS621 TO 625.30 INTERCOSTAL AT STR 14L IS CRACKED NEAR RADIUS APPROX 1.1 INCH LONG. MAINTENANCE REPLACED INTERCOSTAL IAW SRM. (K) 2L72 4F4 FRTA21EA E15NE 20051220000652005122000065EA 2005 12 20 A6WA200540333 120051127A5510 PIVOT ASSY CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE HORIZONTAL STAB SEIZED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31427ZW 7685 HORIZONTAL STABILIZER RT OUTER PIVOT PIN FOUND TO BE SEIZED IN OUTER BUSHING CAUSING BUSHING TO ROTATE IN LUG. MAINTENANCE REMOVED AND REPLACED HORIZONTAL STABILIZER RT OUTER BUSHING AND REAMED THE LUG TO 2ND OVERSIZE IAW SB. (K) 2L72 4F4 FRTA21EA E15NE 20051220000692005122000069NM 2005 12 20 GAIA05033OP 120051116A527021EN96 SWITCH BOEING727 727224 1384076NM PWA JT8 JT8D9A 52048NE MAIN CARGO DOOR OUT OF ADJUST A GAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW0769735 20664 DURING CLIMB FROM 14,000 FEET THE (MAIN CARGO DOOR NOT CLOSED) LIGHT ILLUMINATED. THE FLIGHT CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. ON DECENT THE LIGHT WENT OFF AT 12,000 FEET. AN UNEVENTFUL LANDING WAS MADE AT DEPARTURE. THE MAIN CARGO DOOR WAS VERIFIED TO BE CLOSED AND LOCKED AND THE MAIN CARGO DOOR INDICATING SYSTEM WAS DEFERRED. INSPECTION REVELED THAT THE MAIN CARGO DOOR LATCH LOCK SWITCH WAS OUT OF ADJUSTMENT. THE SWITCH WAS ADJUSTED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L73 4F4 F A3WE E2EA 20051220000742005122000074EU 2005 12 20 KBM2005F00354 120051125A2432RG222355 BATTERY SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1D NE MASTER WEAK E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1953SH 2 2009 BATTERY WEAK, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051220000752005122000075EU 2005 12 20 KBM2005F00355 120051125A2432RG355 BATTERY SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1D NE MASTER FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1953SH 321 2009 SLOW START, REMOVED AND REPLACED BATTERY. (K) 1G71 3U3 U H9EU E19EU 20051220000762005122000076EU 2005 12 20 KBM2005F00356 120051127A7930704A37642043 TRANSMITTER SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1D NE OIL PRESS TRANSMFAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1953SH 244 2009 ENGINE OIL GAUGE DROPS TO ZERO. REMOVED AND REPLACED OIL PRESSURE TRANSMITTER. (K) 1G71 3U3 U H9EU E19EU 20051220000782005122000078NE 2005 12 20 ALG2005F00090 120051129A2435 SEAL SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL STARTER GEN LEAKING E ALGAO OTHER KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SW03519AL 760058 AFTER LANDING, OIL WAS OBSERVED ON MAIN GEAR AND TAILBOOM. REPLACED GEARBOX SEAL (STARTER/ GENERATOR) AND OIL RING ON STARTER/GENERATOR. ALL WORK C/W ICW C-30 MM. (K) 1G72 3U3 U H1NE E1GL 20051220000792005122000079SO 2005 12 20 SIMA200532908 120051113A532014521700007 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21826AE 145592 DURING INSP, FOUND LT OMEGA BEAM AT FRAME 20 LT, CORRODED. REPAIRED OMEGA BEAM BY INSTALLING A DOUBLER IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4F4 FRTT00011ATTE6CH 20051220000812005122000081EA 2005 12 20 A6WA200540330 120051122A3310 RHEOSTAT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FLOOD LIGHT FAULTY A A6WAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 GL31405AW 7362 WHEN F/O SELECTED FLOOD LIGHTS ON, SMOKE ERUPTED FROM BEHIND SW PANEL FLOOD LABEL DSTLA ON FO`S SIDE PANEL AND CBP3 C1 POPPED AND WAS NOT RESET. INSPECTED AND FOUND FO`S FLOOD LIGHT RHEOSTAT FAULTED. NO OTHER SYS AFFECTED. (K) 2L72 4F4 FRTA21EA E15NE 20051220000822005122000082EU 2005 12 20 KBM2005F00359 120051118A21500500521 MOTOR SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE FWD EVAPORATOR INTERMITTENT E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19966SH233 3787 FWD EVAPORATOR MOTOR ONLY WORKS IN ONE SPEED. (K) 1G71 3U3 U H9EU E19EU 20051220000832005122000083CE 2005 12 20 KC82005F00008 120051114A3250238006668 SERVO LEAR 25 25 5170506CE GE CJ610 CJ6105 30006NE NOSE STEERING DEFECTIVE E KC8AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL2339CK 005 AFTER TAKEOFF, GEAR WAS SELECTED UP, NOSE STEERING SERVO DRIVE NOSE WHEEL 90 DEGREES. NOSE GEAR WOULD NOT RETRACT INTO THE WHEEL WELL. GEAR WAS SELECTED DOWN AND NOSE WHEEL STRAIGHTENED OUT. AIRCRAFT LANDED WITHOUT INCIDENT AND TAXIED BACK TO HANGAR. FOUND DEFECTIVE NOSE STEERING SERVO, SERVO CLUTCH FAILURE HAD OCCURED. REPLACED NOSE STEERING SERVO WITH SERVICEABLE SERVO. PERFORMED STEERING OPERATIONAL CHECKS. PERFORMED LANDING GEAR RETRACTION CHECKS. ALL WORK PERFORMED IAW THE SRM. AIRCRAFT WAS RELEASED FOR SERVICE THIS DATE. (K) 2L72 4J4 J A10CE 1E16 20051220000842005122000084WP 2005 12 20 ASAA0580412 120050805A532199365853 FLOOR PANEL DOUG DC9 DC983 3022083WP FS 465-522 CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02947AS 53020 OKC - DURING C-CHECK, FOUND CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20051220000862005122000086WP 2005 12 20 ASA0580466 120050817A523059101413 SKIN DOUG DC9 DC983 3022083WP FS 643 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02977AS 53453 OKC - DURING C-CHECK, FOUND MID CARGO BAY DOOR SKIN IS DENTED. COLD-FORMED SKIN. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20051220000882005122000088WP 2005 12 20 ASAA0580433 120050807A531359360531 LONGERON DOUG DC9 DC982 3022082WP FS 729-733 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02935AS 49236 OKC - DURING C-CHECK, FOUND LONGERON CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLER STRAP AND SHIM. (M) 2L72 4F A6WE 20051220000892005122000089WP 2005 12 20 ASAA0580434 120050807A5313591140143 LONGERON DOUG DC9 DC982 3022082WP FS 207-218 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02935AS 49236 OKC - DURING C-CHECK INSPECTION, FOUND LONGERON CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR CHANNEL. (M) 2L72 4F A6WE 20051220000922005122000092WP 2005 12 20 ASAA0580416 120050805A5320993061287 CUSP WEB DOUG DC9 DC983 3022083WP FS 1281 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02947AS 53020 OKC - DURING C-CHECK, FOUND RIGHT CUSP WEB CRACKED. STOP DRILLED CRACK. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20051220000952005122000095WP 2005 12 20 ASAA0580454 120050808A53305920323553 SKIN DOUG DC9 DC982 3022082WP FS 503-522 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02935AS 49236 OKC - FOUND FUSELAGE SKIN IS DENTED. RECON TOURED DAMAGED AREA. INSTALLED REPAIR DOUBLER. (M) 2L72 4F A6WE 20051220000992005122000099NE 2005 12 20 AMTA200501070 220051114A7200011524 MODULE LKHEED1011 10113853 5265020WP RROYCERB211 RB211524B4 54555NE NR 1 ENGINE DAMAGED A AMTAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL11161AT 1219 AT FL 330, NR 1 ENGINE HIGH VIB LIGHT CAME ON AND VIB INDICATED 4.5 UNITS ON CHANNEL A/B WHEN NR 1 THROTTLE WAS REDUCED TO IDLE VIB UNITS WERE IND. HIGH VIBRATION WAS INDICATED ON LOW SIDE ONLY. REPLACED FAN ASSEMBLY, THRUST RING, THRUST RING CARRIER AND AIR SEAL. PERFORMED GROUND AVM SURVEY PER M11-71-16 ON NR 1 ENGINE VIB WITHIN LIMITS. (M) 2L73 4F4 F A23WE E12EU 20051220001002005122000100SO 2005 12 20 SIMA200528314 120051009A531112010732001 FRAME EMB 145 EMB145LR 3260212SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21636AE 145160 FOUND FRAME 81 CHAFED THROUGH AT THE 6 O`CLOCK POSITION CAUSED BY APU COWLING BRACKET. REPLACED BOTTOM HALF OF FRAME 81 IAW SRM 51-23-01. INSPECTED APU COWLING BRACKET WITH NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20051220001012005122000101SO 2005 12 20 SIMA200528312 120051009A3350 BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSINOPERATIVE A SIMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW21650AE 145417 EMERGENCY LIGHTS WILL NOT EXTINGUISH. REPLACED NR 1, 2, 3 AND 4 EMERGENCY LIGHT BATTERY POWER SUPPLIES AND NR 2 EMERGENCY LIGHT CHASSIS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. EMERGENCY LIGHT BATTERIES OFF P/N 2-131A. POWER SUPPLY SERIAL NUMBERS OF AS FOLLOWS 1-66089, 2-69701, 3-67880, 4-74123. (M) 2L72 4T RTT00011AT 20051220001022005122000102SO 2005 12 20 SIMA200528308 120051007A2611FDS765A2 SMOKE DETECTOR EMB 145 EMB145LR 3260212SO LAVATORY INOPERATIVE A SIMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW21699AE 14500883 LAV SMOKE INDICATION ON EICAS AFTER TAKEOFF. NO VISIBLE SMOKE WAS NOTED. REPLACED LAVATORY SMOKE DETECTOR PANEL AND LAVATORY SMOKE DETECTOR IAW EMB AMM 26-14-02 AND 26-14-01. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE, P/N FOR PANEL IS FAU-751A-4 S/N IS 043477. (M) 2L72 4T RTT00011AT 20051220001032005122000103WP 2005 12 20 ASAA0580470 120050817A5330595305077 SKIN DOUG DC9 DC983 3022083WP FS 285 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02977AS 53453 OKC - FOUND DURING C-CHECK, FUSELAGE DENTED. REMOVED DAMAGED AREA. INSTALLED INTERNAL AND EXTERNAL DOUBLERS. (M) 2L72 4F RTA6WE 20051220001042005122000104WP 2005 12 20 ASAA0580471 120050817A575359304963 VANE DOUG DC9 DC983 3022083WP TE FLAP CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02977AS 53453 OKC - FOUND LEFT WING OUTBOARD FLAP INBOARD VANE EXTERNAL DOUBLER IS CHAFED. REMOVED DOUBLER. INSTALLED REPLACEMENT DOUBLER. INSTALLED REPLACEMENT DOUBLER. (M) 2L72 4F RTA6WE 20051220001052005122000105WP 2005 12 20 ASAA0580477 120050904A53305920323211 SKIN DOUG DC9 DC982 3022082WP FS 330-338 SCRATCHED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02931AS 49232 OKC - DURING C-CHECK, FOUND FUSELAGE SCRATCHED AND DENTED. REMOVED SCRATCH. COLD FORMED DENTED AREA BACK TO ORIGINAL CONTOUR AND INSTALLED INTERNAL REPAIR DOUBLER. (M) 2L72 4F A6WE 20051219000772005121900077WP 2005 12 19 ABXA050341 120051207A33505708458503 BATTERY PACK DOUG DC8 DC861 3021952WP EMERGENCY LIGHT DISCHARGED A ABXAO OTHER L NO TEST NRNOT REPORTED 1 GL23842AX846 46015 EMERGENCY EXIT LIGHTS STILL DIM AND EMERGENCY HORIZONTAL GYRO LIGHTS DON'T WORK. GYRO FLAGGED WITH BATTERY POWER ONLY. REMOVED AND REPLACED EMERGENCY EXIT LIGHTS BATTERY PACK IAW DC8 MM. EMERGENCY EXIT LIGHTS OPS CHECKED GOOD. REMOVED AND REPLACED STANDBY HORIZON POWER SUPPLY IAW DC8 MM 34-28-00. OPS CHECKED GOOD, P/N: 501-1228-04, S/N: 3998. 2L74 4F 4A25 20051219000842005121900084NM 2005 12 19 USAA051498 120051212A5510 CLEVIS BOEING737 7374B7 1384702NM STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 FOUND FWD AND AFT FACE OF R3 CLEVIS. SPOT FACED BOTH FACES INSTALLED NEW BUSHING IAW SRM 55-10-10, DEFECT SIZE: .375. 2L72 4F RTA16WE 20051219000872005121900087NM 2005 12 19 USAA051495 120051212A575465C26603100A WEDGE BOEING737 737301 1384611NM NR 4 SLAT DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19591US 23936 FOUND NR 4 SLAT INBD LOWER CORNER BOTTOM SKIN WORK THROUGH ON TRAILING EDGE WEDGE. MAJOR REPAIR SRM 51-70-10, DEFECT SIZE: 1". 2L72 4F RTA16WE 20051219000912005121900091NM 2005 12 19 2005UALA01231 120051105A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29379UA 24654 DOOR OPENING AT 2R HAS A CRACK AT THE UPPER HINGE CUT-OUT. VERIFID LENGTH AND LOCATION OF CRACK. CUT OUT DAMAGED AREA AND MFG DOUBLER SKIN REPAIR PER SRM 53-60-01. 2L72 4F4 FRTA16WE E2GL 20051219000922005121900092NM 2005 12 19 2005UALA01233 120051104A2120 ODOR BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN DETECTED A UALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP29304UA 23665 ELEC ODOR DETECTED NEAR ROW 18. SUPPLEMENTAL DATA UPDATE, AIRCRAFT WAS CHECKED WITH NO DISCREPANCIES FOUND, AND NO FURTHER COMPLAINTS OF ELECTRICAL ODOR. AS A PRECAUTION, A CALLOUT HAS BEEN ENTERED TO LOWER THE PSUS BETWEEN ROWS 16 AND 20 TO CHECK FOR DAMAGED WIRING. AS OF 11/28, THERE HAVE BEEN NO REPEAT OCCURRENCES. 2L72 4F4 FRTA16WE E2GL 20051219000942005121900094 2005 12 19 SWAA053912 420051210A256563550 SLIDE BOEING737 7377H4 1384404NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29460WN 32464 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051219001022005121900102NM 2005 12 19 SWAA053918 120051209A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 847 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29622SW 27932 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 847, STR 4L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051219001062005121900106NM 2005 12 19 SWAA053922 120051207A53306545765 SKIN BOEING737 737317 138447PNM BS 518D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29661SW 23173 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 518D, BETWEEN STR 11R AND STR 13R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051219001092005121900109NM 2005 12 19 USAA051521 120051213A5510 BUSHING BOEING737 7374B7 1384702NM HORIZONTAL STAB DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 FOUND R6 CLEVIS FWD FACE OF BUSHING. REMOVED DAMAGE, FABRICATED AND INSTALLED NEW BUSHING IAW SRM 55-10-10, DEFECT SIZE: 2L72 4F RTA16WE 20051219001112005121900111EU 2005 12 19 USAA051528 120051213A5320D5347217220500 FLOOR SUPPORT AIRBUSA321 A321211 3930370EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19164UW 1425 FOUND FLOORBEAM CORRODED, -Y1160 FS 66-67. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-72-11; CORROSION LEVEL 1; TASK JA-260-53500, DEFECT SIZE: 1" X 18". 2L72 4F RTA28NM 20051219001222005121900122NM 2005 12 19 QXEA200501781 120051213A3260 PROXIMITY SENSOR BOMBDRDHC8 DHC8402 1390042NM MLG OUT OF ADJUST A QXEAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM09401QX 4031 SEA FLIGHT NR 9853: AFTER SELECTING GEAR UP, ALL ADVISORY LIGHTS ASSOCIATED WITH LEFT MAIN GEAR AND NOSE GEAR EXTINGUISHED NORMALLY. THE GREEN RIGHT GEAR LIGHT ALSO EXTINGUISHED NORMALLY, BUT ABOUT 10 SECONDS ELAPSED BEFORE THE RED RT GEAR, THEN THE AMBER R DOOR AND FINALLY THE GEAR UNSAFE LIGHT IN THE HANDLE EXTINGUISHED. FLIGHT DIVERTED TO PDX. MX INTERROGATED PSEU. FOUND RT MLG UPLOCK AT HIGH END OF RANGE. RIGGED PROX SENSOR RT MLG UPLOCK TO NORMAL GAP IAW Q400 AMM 32-61-06-830-801. PERFORMED EXTENSION AND RETRACTION OF MAIN LANDING GEAR IAW TASK 32-31-00-710-801. GEAR OPERATED NORMALLY. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051219001342005121900134EU 2005 12 19 ASOA05985 120051031A5310 CREASE BEAM AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27643AS 413 DURING A C-CHECK IN YUL, THE RIGHT SIDE CREASE BEAM, BETWEEN FS 39-40, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT SIDE CREASE BEAM, BETWEEN FS 39-40, IAW ASA EO 72-53-0195. (M) 2H72 4T RTA53EU 20051219001392005121900139EU 2005 12 19 AWXA200501498 120051210A335032145410 POWER SUPPLY AIRBUS320 A320232 3930326EU EMERGENCY LIGHT INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28652AW1768016805 953 LAS - EEL - DURING INSPECTION DISCOVERED, THE AFT EMERGENCY LIGHT POWER SUPPLY INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY LIGHT POWER SUPPLY IAW AMERICA WEST AIRLINES TASK CARD R1C33303. OPERATIONAL CHECKS WERE GOOD. VENDOR DID NOT CONFIRM FAULT. REPLACED S1, KEY SWITCH AND FOIL. REPAIRED AND TESTED IAW CMM 33-51-12 REV. 2. 2L72 4F RTA28NM 20051219001532005121900153NM 2005 12 19 AWXA200501510 120051118A532065479573 SILL BOEING737 73733A 1384673NM BS 795-847 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 MCN - DURING C19 CHECK DISCOVERED CORROSION AROUND SILL WEB NUT PLATES ON TORQUE BOX AT AFT PIT DOOR CUTOUT BETWEEN BS 795 TO BS 847 AND AT STR 25R. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-15-1A1 FIG 101. MAINTENANCE REMOVED AND INSTALLED NEW SILL WEB WITH NEW NUTPLATES ONTO TORQUE BOX AT AFT PIT DOOR CUTOUT IAW BOEING 737-300 SRM 51-40-02-0G FIGS 3, 9, AND 10. 2L72 4F RTA16WE 20051219001542005121900154NM 2005 12 19 USAA051518 120051213A5510 BUSHING BOEING737 7374B7 1384702NM HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 FOUND CORROSION L3 CLEVIS FWD FACE OF BUSHING. REMOVED DAMAGE, FABRICATED AND INSTALLED NEW BUSHING IAW SRM 55-10-10, DEFECT SIZE: .250 DIA SPOTS OF CORROSION. 2L72 4F RTA16WE 20051219001682005121900168NM 2005 12 19 DHL2005765504 120051212A5320 FLOOR SUPPORT BOEING727 727264 138408MNM BS 1035 CORRODED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15765AT 23014 AFT CARGO PIT CORROSION ON LOWER SIDE AFT OF FLOOR SUPPORT CHANNEL, LWR SIDE, STA 1035, ABOVE S-30. REMOVED SECTION OF FLOOR SUPPORT CHANNEL. FABRICATED AND INSTALLED CHANNEL 26-5/8" FROM BAC1509-100146, L-ANGLE 12 BY 1" FROM AND10133-0702, AND L-ANGLE 12" BY 1" FROM BAC1490-2583 IAW B727 SRM 53-10-5 FIG 4. 2L73 4F A3WE 20051219001792005121900179NM 2005 12 19 AWXA200501526 120051116A52105079454 SKIN BOEING737 73733A 1384673NM L1 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 MCN - DURING C19 CHECK DISCOVERED L1 DOOR INNER WEB WITH 2 CRACKS AT LIGHTENING HOLES AND 1 CRACK AT THE TORQUE TUBE ACCESS PANEL CUTOUT FROM BS 312 TO BS 318 AND STRINGER 10L. MAINTENANCE CUT OUT DAMAGED AREA IAW BOEING 737-300 SRM 52-10-01. FABRICATED REPAIR DOUBLERS IAW BOEING 737-300 SRM 51-70-13-0G FIG 1. INSTALLED FABRICATED REPAIR PARTS AT L1 INNER WEB LIGHTENING HOLES AND 1 CRACK AT THE TORQUE TUBE ACCESS PANEL CUTOUT FROM BS 312 TO BS 318 AND STRINGER 10L IAW BOEING 737-300 SRM 51-70-13-0G FIG 1. 2L72 4F RTA16WE 20051219002052005121900205NM 2005 12 19 SWAA053973 120051214A335007912 COVER BOEING737 7377H4 1384404NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29450WN 32470 DURING SCHEDULED HC1 CHECK, FOUND EEPLS TRACK COVERS CRACKED BETWEEN ROW 1 TO ROW 11. REMOVED AND REPLACED COVERS PER MM. 2L72 4F RTA16WE 20051219002102005121900210NM 2005 12 19 SWAA053978 120051215A53156545812 FLOORBEAM BOEING737 7373H4 1384600NM BS 327 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29622SW 27932 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FLOORBEAM STIFFENER CRACKED AT BS 327, RBL 35, WL 201. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20051219002132005121900213SO 2005 12 19 CHQA200500210 120051210A2913PV303211MODA PUMP EMB 145 EMB145LR 3260212SO HYD SYSTEM INOPERATIVE A CHQAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL11288SK1157211572 145461 FLIGHT 3191 PHL-GSO UPON DEPARTURE FROM PHL, RECEIVED HYD 1 LO QTY ON EICAS WHEN THE GEAR WAS RETRACTED. RAN QRH. DURING CRUISE, E1 HYD PUMP FAIL AND EVENTUALLY HYD SYS FAIL APPEARED ON EICAS. RAN QRH AGAIN. COORDINATED WITH DISPATCH AND MAINTENANCE OVER ATLANTA RADIO AND DECLARED AN EMERGENCY. CONTINUED ONTO GSO. LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED ENGINE DRIVEN PUMP IAW EMB 145 MM 29-10-03. OPS CHECK GOOD. LEAK CHECK GOOD. NO LEAKS FOUND AT THIS TIME. 2L72 4T RTT00011AT 20051219002282005121900228EU 2005 12 19 05FDEA04314 120051214A7830 FRAME AIRBUS300 A300B4622R 3930312EU THRUST REVERSER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25720FD 417 EXHAUST THRUST REVERSER TORQUE BOX FWD FRAME CRACKS. COMPLIED WITH EA 6-7830-923658 EXHAUST THRUST REVERSER TORQUE BOX FWD FRAME CRACKS PART 1. 2L72 4F RTA35EU 20051219002352005121900235NM 2005 12 19 ASAA0510321 120050922A55316549558506 CLEVIS BOEING737 737290C 138448VNM VERTICAL STAB CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02740AS 22578 YXX - FOUND CORROSION ON VERTICAL STABILIZER AFT SPAR RIGHT PRIMARY FORWARD CLEVIS AFT FACE. CLEVIS REPLACED PER BOEING DWG 6546575 AND B737-200 SRM 51-30-2 PARAGRAPH 17. (M) 2L72 4F A16WE 20051219002372005121900237NM 2005 12 19 ASAA0510323 120050922A55316549558505 CLEVIS BOEING737 737290C 138448VNM VERTICAL STAB CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02740AS 22578 YXX - FOUND CORROSION ON VERTICAL STABILIZER AFT SPAR LEFT PRIMARY FORWARD CLEVIS FORWARD FACE. FACES MACHINED PER EA 5340-01138. (M) 2L72 4F A16WE 20051219002392005121900239SO 2005 12 19 SIMA200528305 120051005A3350MS33205 RELAY EMB 145 EMB145LR 3260212SO CABIN FAULTY A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21650AE 145417 CVG - FLT 3971 - EMERGENCY LIGHTING CIRCUIT BREAKER POPPED. REPLACED CIRCUIT BREAKER 8500 AND RELAY K0275. OPERATIONAL CHECK OF EMERGENCY LIGHTING SYSTEM GOOD PER EMB AMM 33-50-00. AIRCRAFT RETURNED TO SERVICE. C/B PN IS REBC4105-200003. (M) 2L72 4T RTT00011AT 20051219002452005121900245SO 2005 12 19 SIMA200530102 120051025A532014522459003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21720AE 145279 SAW - DURING MBV INSPECTION, FOUND LEFT FLOOR SUPPORT RAMP BETWEEN FRAMES 19 AND 20 IS CORRODED. INSTALLED NEW FLOOR SUPPORT RAMP IAW EMB SRM 5-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20051219002522005121900252SO 2005 12 19 SIMA200529702 120051018A532014525381003 FLOOR SUPPORT EMB 145 EMB145 3260210SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21612AE 145079 A PREVIOUS REPAIR ON THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. REMOVED THE EXISTING REPAIR AND CLEANED THE AREA. FABRIATED A FILLER, DOUBLER, PLATE AND SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB-145/1142 REV 31, CHAPTER 53-00-10, FIG 201. (M) 2L72 4F RTT00011AT 20051219002542005121900254SO 2005 12 19 SIMA200529309 120051019A361014538590401 DUCT EMB 145 EMB145LR 3260212SO BLEED AIR SYS CRACKED A SIMAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TXTAXI/GRND HDL 1 SW21900AE 14500885 ORD - FLT 4402 - LAVATORY SMOKE WARNING CAME ON DURING TAXI AND WENT OUT. INSPECTED CUSTOMER SERVICE MANIFOLD ON LEFT ENGINE AND FOUND HIGH STAGE BLEED TUBE CRACKED. REPLACED BLEED TUBE. PERFORMED FUNCTIONAL TEST FLIGHT AND PASSED. OPERATIONAL TEST OF SMOKE DETECTOR GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20051219002702005121900270CE 2005 12 19 DXTA200501142 120051214A3260 WARNING LIGHT CESSNA680 680CE 2076811CE NLG FALSE ACTIVATIONE DXTAA UNSCHED LANDING N FALSE WARNING APAPPROACH 1 GL07362QS 6800051 LOWERED LANDING GEAR, NOSE GEAR WAS VERY SLOW COMING OUT AND DOWN. AFTER ABOUT 15 SECS THE NOSE GEAR DROPPED AN NO LIGHT CAME ON, BUT UNLOCK LIGHT REMAINED LIT AND HAD AN ANTISKID FAILED LIGHT. UNLOCK LIGHT WOULD NOT TURN OUT, ITEM IS UNDER INVESTIGATION. 2L72 4F RCT00012WI 20051219002772005121900277NM 2005 12 19 DHL2005749021 120051102A5313 STRINGER BOEING727 7272J0 138407ENM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01749DH 22013 FWD CARGO PIT BILGE AREA STRINGER 27R CORRODED AT BS 720F +14 MARKED. REMOVED BEACON ANTENNA AND CONTROL AIR DUCT AT BS 720F + 14 AND STR 27R IAW B727 SRM 51-30-2 MM 21-20-4 FOR ACCESS. CUT OUT DAMAGED SECTION OF STRINGER 8 1/2 INCHES LONG AT BS 720F + 14 AND STR IAW B727 SRM 53-10-2 FIG1. FABBED STR FROM BAC1498-147 8 1/2 INCHES PO 5096200 SPLICE BAC1498-131 9 INCHES PO9001233 IAW B727 SRM 53-10-3 FIG 1. TREATED AND PRIMED REPAIR PARTS IAW B727 SRM 51-10-2. INSTALLED STR REPAIR IAW B727 SRM 53-10-3 FIG1. REINSTALLED BEACON ANTENNA AND CONTROL AIR DUCT IAW B727 MM 21-20-4 PRESSURIZATION CKS GOOD IAW B727 MM 21-31-0 2L73 4F RTA3WE 20051219002782005121900278NM 2005 12 19 DHL2005749022 120051103A5755 SPOILER BOEING727 727200 138407ENM NR 5 DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01749DH 22013 NR 5 SPOILER UPPER IB FWD CORNER TAPS SOFT. CUT OUT DELAMINATED AREA ON NR 5 SPOILER UPPER IB FWD CORNER APPROX 5 INCHES BY 6 INCHES FABBED FILLER 5 INCHES BY 6 INCHES AND DOUBLER APPROX 6 1/2 INCHES BY 7 12/2 INCHES FROM 7075T6 .020 PO526029 CLEANED PREPPED APPLIED ADHESIVE PRIMER BONDED CLEANED TREATED PRIMED AND SEALED EDGES IAW B727 SRM 57-50-1 FIG 5, 57-50-2 FIG 9 AND 51-40-20 FIG 1. 2L73 4F RTA3WE 20051219002802005121900280NM 2005 12 19 DHL2005749025 120051107A5347 SEAT TRACK BOEING727 727200 138407ENM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01749DH 22013 FOUND CORROSION ON SEAT TRACK AT RBL 45 BS 770-850. REMOVED SEAT TRACK BS 757-852 RBL 45 AND FABBED NEW FROM BAC 1520-841 PO 9002277 DIM 95" IN LENGTH IAW B727 SRM 53-10-2 FIG 7 AND 53-10-5 FIG 2 LWR SURFACED TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED TRACK IAW B727 SRM 51-30-2. 2L73 4F RTA3WE 20051219002882005121900288EA 2005 12 19 ASOA05931 120051029A27501104SC1061 SEAL CNDAIRCL600 CL6002B19 1900309EA T/E FLAP LEAKING A ASOAK NONE F FLT CONT AFFECTED APAPPROACH 1 SO27823AS 7196 DURING APPROACH FROM PHF-ATL, THE FLAPS AT ZERO. THE CREW DECLARED AN EMERGENCY AND THE EMERGENCY VEHICLES WERE DISPATCHED. THE AIRCRAFT LANDED SAFELY WITHOUT FURTHER INCIDENT IN ATL. MX REMOVED AND REPLACED THE FLEX SHAFT SEALS, LUBRICATED THE LEFT FLEX SHAFTS, AND CLEANED THE FLAP ACTUATORS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051219002912005121900291EA 2005 12 19 ASOA05928 120051028A5320 WEB CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27838AS 7276 DURING A C-CHECK IN MCN, THE FLOOR ATTACH WEB , AT FS 559 PLUS 80 TO 621, BL 45 RT, WAS FOUND TO BE CORRODED. AFTER MAINTENANCE BLENDED, ALODINED, AND PRIMED THE FLOOR ATTACH WEB, AT FS 559 PLUS 80 TO 621, BL 45 RT, IAW REO 601R-53-61-1564, IT WAS FOUND TO BW WITHIN LIMITS. (M) 2L72 4F RTA21EA 20051219002922005121900292EA 2005 12 19 ASOA05927 120051028A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27838AS 7276 DURING A C-CHECK IN MCN, THE FLOORBEAM ATTACH POINTS, AT FS 621 TO FS 560, LBL 37L, WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR ATTACH POINTS, AT FS 621 TO 560, LBL 37L IAW CRJ 200 SRM 51-42-06. (M) 2L72 4F RTA21EA 20051219003022005121900302EA 2005 12 19 ASOA05916 120051026A25602618 FLASHLIGHT CNDAIRCL600 CL6002B19 1900309EA COCKPIT DISCHARGED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27903EV 7621 FLT 4500 - DURING A GROUND INSPECTION IN SHV, THE CAPTAINS AND FIRST OFFICERS FLASHLIGHTS WERE FOUND TO BE VERY DIM. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS AND FIRST OFFICERS FLASHLIGHTS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051219003032005121900303EA 2005 12 19 ASOA05960 120051024A2613601R5790011 LOOP CNDAIRCL600 CL6002B19 1900309EA LT PYLON OUT OF POSITION A ASOAJA DUMP FUEL UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO27975EV 7599 FLT 4578 - DURING CRUISE FROM ATL-BTR, AT APPROXIMATELY 26,000 FEET, THE CREW RECEIVED AN INTERMITTENT LEFT 14TH STATE DUCT MASTER WARNING WHICH BECAME CONSTANT. THE QRH WAS COMPLIED WITH AND THE CREW DECLARED AN EMERGENCY . THE AIRCRAFT DIVERTED TO MGM AND LANDED SAFELY. MAINTENANCE FOUND THE 14TH STAGE PYLON LOOP TOUCHING THE FRAME AND THE PYLON LOOP WAS REPOSITIONED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051219003182005121900318EA 2005 12 19 ASA05975 120051112A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27870AS 7500 DURING A C-CHECK IN MCN, THE LEFT OUTBOARD FS 280 CLIP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACED THE LEFT OUTBOARD FS 280 CLIP IAW CRJ 200 SRM 51-42-00. (M) 2L72 4F RTA21EA 20051219003222005121900322EA 2005 12 19 ASOA05979 120051114A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27672BR 7594 FLT 4447 - DURING A GROUND INSPECTION IN VPS, THE EMERGENCY LIGHT, ABOVE ROW 4, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY LIGHT ABOVE ROW 4. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051219003292005121900329EU 2005 12 19 SA05124 120051209A335032145410 LIGHT AIRBUSA319 A319112 3930323EU CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19701UW1755114848 890 TPA - THE RED EMERGENCY SEAT LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE RIGHT SIDE, MID CABIN EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20051219003312005121900331EU 2005 12 19 ASOA05986 120051031A5311 DOUBLER AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27643AS 413 DURING A C-CHECK IN YUL, THE RIGHT SIDE DOUBLER, ON FRAME 39, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT SIDE DOUBLER, ON FRAME 39, IAW ASA EO 72-53-0194. (M) 2H72 4T RTA53EU 20051219003332005121900333EU 2005 12 19 ASOA05988 120051031A5320 FLOOR SUPPORT AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27643AS 413 DURING A C-CHECK IN YUL, THE LEFT AND RIGHT SIDE `Z` FLOOR SUPPORTS, BETWEEN FS 39-40, WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT SIDE `Z` FLOOR SUPPORT, BETWEEN FS 39-40, IAW ASA EO 72-53-0200, AND REMOVED AND REPLACED THE RIGHT SIDE `Z` FLOOR SUPPORT, BETWEEN FS 39-40, IAW ASA EO 72-53-0201. (M) 2H72 4T RTA53EU 20051219003352005121900335EU 2005 12 19 ASOA05990 120051028A5315 FLOORBEAM AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27643AS 413 DURING A C--CHECK IN YUL, THE FLOORBEAM AT FS 36 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM AT FS 36, IAW ASA EO 72-53-0170. (M) 2H72 4T RTA53EU 20051219003372005121900337EU 2005 12 19 ASOA05992 120051028A5315 FLOORBEAM AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27643AS 413 DURING A C-CHECK IN YUL, THE FLOORBEAM, AT FS 39, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED THE FLOORBEAM, AT FS 39, IAW SRM 51-25-01 AND REPLACED THE FLOORBEAM, AT FS 39, IAW ASA EO 72-53-0172. 2H72 4T RTA53EU 20051220000012005122000001NM 2005 12 20 05FDEA04221 120051211A5101 UNKNOWN DOUG MD11 MD11 3023602NM ZONE 300 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25524FE 48480 TO CARRY OUT TRIMMING OF LEFT HAND AFT CHORD TO FACILITATE LEFT HAND NR 35 BORE CLEANING ACCESS. REPAIRED AS PER FEDEX EA 1-5510-94569. 2L73 4F RTA22WE 20051220000072005122000007WP 2005 12 20 05FDEA04326 120051215A5310 REPAIR DOUG DC10 DC1010 3022110WP BS 635-675 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568054 47808 EXTERNAL FUSELAGE DOUBLER REPAIR FROM STA 635 TO STA 675 LONG 28 LT Z-30. PERFORMED AN INSPECTION OF REPAIR IAW SRM 53-50-00 FIG 6 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P1. 2L73 4F A22WE 20051220000112005122000011NM 2005 12 20 05FDEA04330 120051215A5322 SHEAR TIE BOEING727 727200 138407ENM BS 1009 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 CORROSION ON AFT CARGO BAY SHEAR TIE BS 1009 WL 136 RBL 2. 2L73 4F RTA3WE 20051220000132005122000013EU 2005 12 20 05FDEA04332 120051215A5320 FLOOR SUPPORT AIRBUS300 A300F4605R 3930327EU FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25672FE 779 MAIN CABIN BEAM SUPPORT CRACK AT FR 38 .1 RBL 100. REMOVED DAMAGED FLOOR SUPPORT AT FR 38.1 RBL 100 AND REPLACED IAW SRM 51-40-21. 2L72 4F RTA35EU 20051220000172005122000017NM 2005 12 20 05FDEA04210 120051209A5340 STRINGER CLIP BOEING727 727200 138407ENM BS 950F BENT A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 STRINGER CLIP, IN MAIN CABIN, IS BENT AND HAS THREE OPEN HOLES AT STA 950F STR 7R. *S/D* REMOVED AND REPLACED STR CLIP AT BS 950F STR 7R IAW SRM 51-30-2. 2L73 4F RTA3WE 20051220000472005122000047NM 2005 12 20 SWAA053936 120051212A53306545774 SKIN BOEING737 7373H4 1384600NM BS 727E CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 19R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051220000522005122000052EA 2005 12 20 A6WA200540328 120051114A5350 RADOME CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE NONE A A6WAO OTHER O OTHER APAPPROACH 1 GL31408AW 7568 REQUEST BIRD STRIKE INSPECTION. REMOVED AND REPLACED RADOME DUE TO BIRD STRIKE IAW AMM 53-81-01. PERFORMED BIRDSTRIKE AMM 05-51-25. NO FURTHER DAMAGE AND NO ENGINE INGESTION FOUND. (K) 2L72 4F4 FRTA21EA E15NE 20051220000542005122000054EU 2005 12 20 KBM2005F00345 120051127A3210FDT14194 SUPPORT SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE MLG BEARING GOUGED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19250SH1067 3874 LT REAR MAIN GEAR BEARING SUPPORT BAR FWD A DEEP GOUGED BY COMPRESSOR. (K) 1G71 3U3 U H9EU E19EU 20051220000682005122000068SO 2005 12 20 SIMA200532505 120051111A532014525480003 SILL EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21825AE8374 145589 THE BAGGAGE DOOR SILL WAS FOUND CORRODED. REMOVED THE DAMAGED SILL AND INSTALLED SERVICEABLE SILL IAW SRM. (K) 2L72 4F4 FRTT00011ATTE6CH 20051220000702005122000070SO 2005 12 20 SIMA200532903 120051117A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FR 27 LT CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21825AE 145589 THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 27. REMOVED THE CORROSION BY MAKING A CUT OUT. PREPARED A DOUBLER, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (K) 2L72 4F4 FRTT00011ATTE6CH 20051220000802005122000080SO 2005 12 20 SIMA200532511 120051116A2760M83536 RELAY EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL SPOILERS FAILED A SIMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21733KR 145368 AFTER TAKEOFF, RECEIVED EICAS MESSAGE (SPOILER FAIL) ACCOMPAINED BY (OPN) INDICATION IN SPOILERS. REMOVED AND REPLACED LANDING GEAR DOWN LOCK RELAY K0030 AND K0031. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (K) 2L72 4F4 FRTT00011ATTE6CH 20051220000852005122000085WP 2005 12 20 ASAA0580473 120050505A53209936534139 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FS 160-200 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - DUIRNG C-CHECK, PASSENGER CABIN FLOOR TRACK CORRODED. REPLACED DAMAGED TRACK. (M) 2L72 4F RTA6WE 20051220000872005122000087WP 2005 12 20 ASAA0580465 120050817A523059101413 SKIN DOUG DC9 DC983 3022083WP FS 676 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02977AS 53453 OKC - DURING C-CHECK, FOUND MID CARGO BAY DOOR SKIN IS DENTED. COLD FORMED SKIN. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20051220001072005122000107WP 2005 12 20 ASAA0580469 120050817A5320 SUPPORT DOUG DC9 DC983 3022083WP MLG WW CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02977AS 53453 OKC - DURING C-CHECK, FOUND NOSE LANDING GEAR WHEELWELL LEFT SUPPORT FRAME UPPER FASTENER CRACKED. STOP DRILLED CRACK. INSTALLED REPAIR ANGLE, SHIM, AND CLIP 2L72 4F RTA6WE 20051220001082005122000108WP 2005 12 20 ASAA0580443 120050808A53205936597U514 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FS 427 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02935AS 49236 OKC - DURING C-CHECK, FOUND CABIN FLOOR PANEL SUPPORT CORRODED. REPLACED SUPPORT. (M) 2L72 4F A6WE 20051220001102005122000110WP 2005 12 20 ASAA0580459 120050808A575359304741 VANE DOUG DC9 DC982 3022082WP TE FLAP GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02935AS 49236 OKC - DURING C-CHECK, FOUND LEFT INBOARD FLAP VANE GOUGED. REMOVED DAMAGED AREA. INSTALLED REPAIR DOUBLER AND FILLER. (M) 2L72 4F A6WE 20051220001122005122000112WP 2005 12 20 ASAA0580437 120050807A5313591140143 LONGERON DOUG DC9 DC982 3022082WP FS 207-218 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02935AS 49236 OKC - DURING C-CHECK, FOUND LONGERON CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR CHANNEL. (M) 2L72 4F A6WE 20051220001132005122000113WP 2005 12 20 ASAA0580440 120050807A53209958212100 INTERCOSTAL DOUG DC9 DC982 3022082WP FS 1003-1022 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02935AS 49236 OKC - DURING C-CHECK, INTERCOSTAL CORRODED. REPLACED INTERCOSTAL. (M) 2L72 4F A6WE 20051220001142005122000114WP 2005 12 20 ASAA0580442 120050807A5313593643437 LONGERON DOUG DC9 DC982 3022082WP FS 465-495 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02935AS 49236 OKC - DURING C-CHECK, FOUND LONGERON CORRODED. REPLACED DAMAGED SECTION. (M) 2L72 4F A6WE 20051220001162005122000116NM 2005 12 20 ASAA0580485 120050926A532199365859 FLOOR PANEL DOUG MD80 MD83 3023681NM FS 927-1003 DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - DURING HV-CHECK, FOUND PAX CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RT 20051220001172005122000117NM 2005 12 20 ASAA0580486 120050926A532199366403 FLOOR PANEL DOUG MD80 MD83 3023681NM FS 886-927 DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - FOUND HV-CHECK, FOUND PAX CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RT 20051220001192005122000119NM 2005 12 20 ASAA0580487 120050926A532199365847 FLOOR PANEL DOUG MD80 MD83 3023681NM CABIN DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - DURING HV-CHECK, FOUND PAX CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RT 20051220001222005122000122WP 2005 12 20 ASAA0580436 120050807A53209936718U3 INTERCOSTAL DOUG DC9 DC982 3022082WP FS 1309-1320 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02935AS 49236 OKC - DURING C-CHECK, FOUND INTERCOSTAL CORRODED. REPLACED INTERCOSTAL. (M) 2L72 4F A6WE 20051220001232005122000123WP 2005 12 20 ASAA0580438 120050807A5322991960315 SHEAR TIE DOUG DC9 DC982 3022082WP FS 1231 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02935AS 49236 OKC - DURING C-CHECK, FOUND SHEAR TIE CORRODED. REPLACED SHEAR TIE. (M) 2L72 4F A6WE 20051220001252005122000125NM 2005 12 20 USAA051530 120051213A5420EA971481 BRACKET BOEING757 757225 1384959NM NR 2 PYLON IMPROPER A USAAK NONE O OTHER ININSP/MAINT 1 EA19607AU 22203 NR 2 PYLON NAC STA 144 IMPROPER FIT. INSTALLED NEWLY FABRICATED BRACKET PER EA 97148, DEFECT SIZE: 5.7 L X .7 W X .080 H INCH. 2L72 4F RTA2NM 20051220001272005122000127NM 2005 12 20 USAA051531 120051213A5313 STRINGER BOEING757 757225 1384959NM FUSELAGE DEFECTIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19607AU 22203 BS 1401-1450 STR 28R DEFECT. FABRICATED A REPAIR AS SHOWN IN SKETCH ON FIG 3 OF EA 95586B PER SRM 51-40-2 & EA 95586B (TEMP REP). DEFECT SIZE: 40L X 4 INCH. 2L72 4F RTA2NM 20051220001282005122000128EU 2005 12 20 USAA051538 120051213A5320D5347112320200 SUPPORT AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19113UW 1141 OVAL SURFACE, TOP & BOTTOM, BETWEEN C69-70 AT Y1200 CORRODED. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-43-00; CORR LEVEL 1; TASK JA-260-53500-14, DEFECT SIZE: 3 INCH. 2L72 4F RTA28NM 20051220001292005122000129EU 2005 12 20 USAA051537 120051213A5320D5347217220390 FLOOR SUPPORT AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19113UW 1141 FR 64-69 AT -Y1292 CORRODED. REPLACED BEAMS PER SRM 51-72-11; CORR LEVEL 1; TASK JA-260-53500, DEFECT SIZE: 2 X 1, 3 X .5, 2 X 1.5 INCH 2L72 4F RTA28NM 20051220001312005122000131EU 2005 12 20 USAA051535 120051213A5320D5347219220000 FLOOR SUPPORT AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19113UW 1141 Y765 AT CROSSBEAM C-68 CORRODED. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-72-11; CORR LEVEL 1; TASK JA-160-53500. DEFECT SIZE: 1 INCH DIA. 2L72 4F RTA28NM 20051220001332005122000133NM 2005 12 20 USAA051534 120051213A5313146N5417 STRINGER BOEING757 757225 1384959NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19607AU 22203 STA 1364 LBL 15 CORRODED. REMOVED & REINSTALLED NEW STRINGER PER SRM 53-00-53 FIG 101, 53-60-53 FIG 1. DEFECT SIZE: 5.0L X 1.0W X .017D INCH. 2L72 4F RTA2NM 20051220001342005122000134NM 2005 12 20 USAA051533 120051213A5330146N3511 SKIN BOEING757 757225 1384959NM FUSELAGE BULGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19607AU 22203 STA 1432 BL 0 HAS BULGE. CUT OUT DAMAGED SKIN AREA & REPAIRED PER SRM 53-00-01 REP 3. DEFECT SIZE: 3.5L X 5.0W X .071D INCH. 2L72 4F RTA2NM 20051220001372005122000137NM 2005 12 20 DLM88050766 120051130A2750S4913810ES008408CABLE DOUG MD88 MD88 3023688NM T/E FLAP DAMAGED A DALAK NONE F FLT CONT AFFECTED ININSP/MAINT 1 SO27937DL 49810 WHILE PERFORMING OPERATION 5603 ON THE FLAPS, A FLAP BUSSING CABLE WAS FOUND WITH THE NYCOTE COVERING CRACKED/MISSING AND THE CABLE DAMAGED OVER A 4 INCH LENGTH. REPLACED CABLE. 2L72 4F RTA6WE 20051220001382005122000138NM 2005 12 20 SB05168 120051213A278065516023 CONTROL VALVE BOEING737 737400 138449ANM L/E SLAT FAILED A USAAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 EA19432US44124 24554 FLIGHT 432, DCA - TPA: AFTER TAKEOFF AND FLAP RETRACTION, SLATS INDICATED EXTENDED. CONFIRMED VISUALLY BY CREW. AIRCRAFT DIVERTED TO CLT. NO FURTHER DIFFICULTIES. MAINTENANCE REPLACED THE FLAP/SLAT CONTROL VALVE. 2L72 4F RTA16WE 20051220001402005122000140 2005 12 20 C2XA05IA136 420051128A31607014300901 DISPLAY EMB 145 EMB145LR 3260212SO COCKPIT FAILED A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 SW27185578287 8287 145596 MEM - FLIGHT 2462, THE CREW REPORTED A DU4 OVERHEAT MESSAGE FOLLOWED BY THE UNIT GOING BLANK AND AN ACRID ELECTRICAL SMELL. THE AIRCRAFT LANDED AT MEM WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE DU4, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20051220001412005122000141NM 2005 12 20 SWAA053938 120051213A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 741, STR 27L. REPAIRED SKIN PER BFG ER. 2L72 4F RTA16WE 20051220001422005122000142NM 2005 12 20 SWAA053939 120051213A53146545866 KEELBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D-CHECK, FOUND LT KEEL BEAM CORRODED BETWEEN BS 500C TO BS 740. REMOVED AND REPLACED LT KEEL BEAM PER SRM. 2L72 4F RTA16WE 20051220001442005122000144NM 2005 12 20 SWAA053941 120051213A33506545769 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29322SW 23343 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 410, BL 0, NR 2 RADIO ALTIMETER ANTENNA CUTOUT. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051220001592005122000159EA 2005 12 20 A6WA200540320 120051108A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUISELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31426AW 7669 FS 484, LBL 36, IB ANGLE OF INTERCOSTAL IS CRACKED .5 INCH LONG. (K) 2L72 4F4 FRTA21EA E15NE 20051220001602005122000160EA 2005 12 20 A6WA200540319 120051108A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31426AW 7669 FS484, RBL 36 IB ANGLE OF INTERCOSTAL IS CRACKED .5 INCHES LONG. (K) 2L72 4F4 FRTA21EA E15NE 20051220001622005122000162EA 2005 12 20 A6WA200540316 120051101A5610NP13932212 WINDOW CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE COCKPIT CRACKED A A6WAI CABIN DEPRESSURIZATION O OTHER DEDESCENT 1 GL31407AW12492 7424 FO SIDE WINDOW CRACKED DURING DESCENT AT 24,000 FT DIFFERENTIAL PRESSURE NOTED AT 7.2 PRESSURE NORMAL CONTINUED DESCENT IAW QRH FOR UNPRESSURIZED FLIGHT AS PRECAUTION. REMOVED AND REPLACED FO SIDE WINDOW. PRESURIZED CABIN. LEAK CHECK GOOD. WINDOW HEAT OPS CHECK GOOD. (K) 2L72 4F4 FRTA21EA E15NE 20051220001632005122000163NM 2005 12 20 AMTA200501026 120051103A3397 WIRE BOEING757 75723N 1384973NM RROYCERB211 RB211* 54555NE CABIN DISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11522AT 29330 EMERGENCY FLOOR PATH LIGHTING INOPERATIVE AT ROW 28, EXIT MARKER AND 2 LIGHT AT LAV D. RECONNECTED LIGHT ASSY WIRES. OPS CHECK GOOD. (K) 2L72 4F4 FRTA2NM A12EU 20051220001642005122000164NM 2005 12 20 GAIA05029OP 120051102A3350 LIGHT BOEING727 7272J0 138407ENM PWA JT8 JT8D15 52051NE CABIN INOPERATIVE A GAIAK NONE L NO TEST ININSP/MAINT 1 SW07281KH 21105 DURING A-CHECK FOUND L1 EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EXIT LIGHT AT L1 DOOR. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L73 4F4 FRTA3WE E2EA 20051220001662005122000166SO 2005 12 20 GUU2005F00056 120051014A32421661 BRAKE EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE RT MLG WEAK A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO17282AS 724 120226 WHEN APPLYING BRAKES, AIRCRAFT PULLS HARD TO LT SIDE, RT BRAKE EXTREMELY WEAK. REPLACED NR3 AND NR4 BRAKE ASSEMBLIES. (K) 2L72 4T4 TRTA31SO E20NE 20051220001712005122000171EA 2005 12 20 ASOA051001 120051118A5210601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27877AS 7579 DURING A GROUND INSPECTION IN ATL, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051220001722005122000172NM 2005 12 20 ASAA0540377 120050803A57536546430130 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU RT FOREFLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02778AS 25110 YXX - RT IB FORE FLAP DENT FOUND ON UPPER SURFACE AT WBL 107. REPAIRED DENT IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051220001742005122000174EA 2005 12 20 ASOA051006 120051120A335060206 COVER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27882AS 7503 DURING A GROUND INSPECTION IN ATL, THE EMERGENCY EXIT SIGN COVER BY THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT SIGN COVER BY THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051220001762005122000176EA 2005 12 20 ASOA05999 120051118A5210601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27876AS 7576 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND TO BE BROKEN AT THE ATTACH LINK. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENER DOOR. (M) 2L72 4F RTA21EA 20051220001782005122000178NM 2005 12 20 ASAA0580494 120050926A532199365479 FLOOR PANEL DOUG MD80 MD83 3023681NM FS 180-200 DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - DURING HV-CHECK, FOUND PAX CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RT 20051220001792005122000179NM 2005 12 20 ASAA0540381 120050810A552265C25746141 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU LT ELEVATOR DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02778AS 25110 YXX: DURING C-CHECK FOUND LT ELEVATOR UPPER IB SURFACE DAMAGED AT STA 24.00. REPAIRED IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051220001802005122000180WP 2005 12 20 ASAA0580435 120050807A531359360551 LONGERON DOUG DC9 DC982 3022082WP FS 712 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02935AS 49236 OKC - FOUND DURING C-CHECK, LONGERON CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR CHANNEL. (M) 2L72 4F A6WE 20051220001822005122000182EA 2005 12 20 ASOA05998 120051117A5240 DOOR CNDAIRCL600 CL6002B19 1900309EA SERVICE DOOR OUT OF RIG A ASOAK NONE O OTHER ININSP/MAINT 1 SO27875AS 7559 DURING A GROUND INSPECTION IN ATL, THE SERVICE DOOR WAS FOUND DIFFICULT TO OPEN. MAINTENANCE RIGGED THE SERVICE DOOR AND ADJUSTED THE CENTER INTERNAL STABILIZER ROD. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051220001852005122000185NM 2005 12 20 ASAA0540382 120050810A575365C326203 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU LT FOREFLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02778AS 25110 YXX: DURING C-CHECK FOUND LT OB FORE FLAP LOWER SKIN IN LINE WITH NR2 FLAP TRACK HAS 2 DENTS. REPAIRED IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051220001872005122000187NM 2005 12 20 ASAA0580498 120050926A5321993655213 FLOOR PANEL DOUG MD80 MD83 3023681NM FS 200-256 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - DURING HV-CHECK, PAX CABIN FLOOR PANEL HAS CORRODED INSERTS WITH DELAMINATION AROUND INSERTS. REPLACED FLOOR PANEL. (M) 2L72 4F RT 20051220001892005122000189EU 2005 12 20 ASOA051009 120051121A3350 LIGHT AEROSPATR72 ATR72212 8680945EU PAX DOOR INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27633AS 344 DURING A GROUND INSPECTION IN AGS, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE PASSENGER DOOR LIGHT SYSTEM IAW ATR-72 AMM 33-51-11 WITH THE EMERGENCY SWITCHES ON. OPERATIONAL CHECKS WERE GOOD. NO DEFECTS WERE NOTED. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20051220001912005122000191NM 2005 12 20 ASAA0540384 120050810A551265C27494 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU HORIZ STAB DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02778AS 25110 YXX: DURING C-CHECK FOUND LT HORZ STAB AT STA 166 SKIN UPPER SURFACE HAS 2 PARALLEL DENT WITH CREASES. REPAIRED IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051220001932005122000193NM 2005 12 20 ASAA0540386 120050810A575365C2632018 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU RT MIDFLAP CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02778AS 25110 YXX: DURING C-CHECK FOUND RT WING OB MIDFLAP T/E LOWER SIDE AT WBL 262, AHS CHAFFE DAMAGE. REPAIRED IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051220001942005122000194NM 2005 12 20 ASAA0540388 120050810A5320654659320 UNKNOWN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02778AS 25110 YXX: DURING C-CHECK FOUND FWD CARGO BILGE CORRODED ON FLANGE AT BS 500D. REPAIRED IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051220001952005122000195NM 2005 12 20 ASAA0540389 120050810A5311654659320 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02778AS 25110 YXX: DURING C-CHECK, FOUND FWD CARGO BILGE CORRODED ON FRAME AT BS 500D. REPAIRED IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051220001962005122000196NM 2005 12 20 ASAA0540390 120050810A273065617501 TORQUE TUBE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU TAIL CONE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02778AS 25110 YXX: DURING C-CHECK, FOUND TAIL CONE COMPARTMENT ELEVATOR OUTPUT TORQUE TUBE HAS A GOUDGE. REPAIRED IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051220001972005122000197NM 2005 12 20 ASAA0540391 120050810A2120 DUCT BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU A/C SYSTEM CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02778AS 25110 YXX: DURING C-CHECK FOUND RT AC RAM AIR DUCT CRACKED AT ATTACH ANGLE AT FWD SECTION AT BS 540. REPAIRED IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051220001982005122000198EU 2005 12 20 ASOA05994 120051031A5320 FLOOR SUPPORT AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11643AS 413 DURING A C-CHECK IN YUL, THE LEFT SIDE FLOOR SUPPORT, BETWEEN FS 36-38, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED THE LEFT SIDE FLOOR SUPPORT, BETWEEN FS 36-38, IAW SRM 51-25-01, AND REPLACED THE LEFT SIDE FLOOR SUPPORT, BETWEEN FS 36-38, IAW ASA EO 72-53-0187. (M) 2H72 4T RTA53EU 20051220001992005122000199WP 2005 12 20 ASAA0580478 120050904A533059114003 SKIN DOUG DC9 DC982 3022082WP FS 83 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02931AS 49232 OKC - DURING C-CHECK, FUSELAGE DENTED NEAR NLG LEFT DOOR. REMOVED DAMAGED AREA. INSTALLED REPAIR DOUBLER. (M) 2L72 4F A6WE 20051220002012005122000201WP 2005 12 20 ASAA0580411 120050805A532099579185 STIFFENER DOUG DC9 DC983 3022083WP FS 465-541 CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02947AS 53020 OKC - DURING C-CHECK, FOUND CABIN FLOOR PANEL IS CHAFED ON LOWER SURFACE BONDED STIFFENER. REPLACED FLOOR PANEL STIFFENER, HAT CHANNEL. (M) 2L72 4F RTA6WE 20051220002042005122000204EA 2005 12 20 ASOA051002 120051118A27419960013 SWITCH CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A ASOAO OTHER J WARNING INDICATION DEDESCENT 1 SO27840AS 7290 DURING DESCENT FROM CVG-HSV, AT APPROXIMATELY 15,000 FEET THE CREW RECEIVED A STAB TRIM AND MACH TRIM CAUTION MESSAGE. THE QRH WAS COMPLIED WITH BUT THE CREW WAS UNABLE TO RE-ESTABLISH THE PITCH TRIM SYSTEM. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY IN HSV. MAINTENANCE REMOVED AND REPLACED THE TRIM DISCONNECT SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051220002052005122000205EA 2005 12 20 ASOA051005 120051120A5210601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27849AS 7347 DURING HANGAR MAINTENANCE IN BTR, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED NEAR THE ATTACHMENT BRACKET. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR IAW CRJ200 AMM 52-10. OPERATIONAL CHECKS GOOD. (M) 2L72 4F RTA21EA 20051220002062005122000206SO 2005 12 20 SIMA200529009 120051005A532014525381003 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO FS 20 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21661JA 145766 THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED THE CORROSION BY MAKING A CUT OUT. PREPARED A DOUBLER, FILLER, PLATE AND SHIMS. REPAIR DONE IAW EMB SRM, SRM 1435/1142 REV 30, CHAPTER 53-00-10. (M) 2L72 4T RTT00011AT 20051220002072005122000207WP 2005 12 20 ASAA0580480 120050904A5330593602231 SKIN DOUG DC9 DC982 3022082WP FS 1105-1110 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02931AS 49232 OKC - DURING C-CHECK, FOUND INTERNAL SKIN DOUBLER IS CORRODED. REMOVED DAMAGED DOUBLER. INSTALLED REPLACEMENT. (M) 2L72 4F A6WE 20051220002092005122000209WP 2005 12 20 ASAA0580413 120050805A5321993658513 FLOOR PANEL DOUG DC9 DC983 3022083WP FS 541-617 PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02947AS 53020 OKC - DURING C-CHECK, FOUND CABIN FLOOR PANEL IS PUNCTURED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20051220002102005122000210NM 2005 12 20 ASAA0580501 120050926A532099365473 FLOOR SUPPORT DOUG MD80 MD83 3023681NM FS 160-200 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - DURING HV CHECK, FOUND PAX CABIN FLOOR TRACK CORRODED. REPLACED TRACK. (M) 2L72 4F RT 20051220002112005122000211NM 2005 12 20 ASAA0540374 120050803A57536546486131 WEDGE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU LT MIDFLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02778AS 25110 YXX - LT WING IB T/E MID FLAP WEDGE PANEL NR 7220L HAS 2 EACH DENTS ON THE OB EDGE. REMOVED DAMAGED FIBERS - POTTED PUNCTURE FLUSH AND REPAIRED PLIES INSTALLED AND CURED. (K) 2L72 4F4 FRTA16WE E21EU 20051220002122005122000212NM 2005 12 20 ASAA0540419 120050819A532065479573 WEB BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02779AS 25111 AFT PIT DOOR-SILL WEB CORRODED. REMOVED CORRODED WEB, LOCATED AND INSTALLED NEW WEB IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051220002132005122000213NM 2005 12 20 ASAA0540420 120050819A531365C329535 STRINGER BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02779AS 25111 STRINGER 28L IS CORRODED AT BSTA 500G. REMOVED DAMAGED SECTION OF STR 28L, FABRICATED AND INSTALLED REPAIR PIECES IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051220002142005122000214NM 2005 12 20 ASAA0580503 120050926A53209936534177 WEB DOUG MD80 MD83 3023681NM FS 180-200 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - DURING HV CHECK, FOUND PAX CABIN FLOOR WEB CORRODED. REPLACED DAMAGED SECTION. INSTALLED WEB REPAIR AND TWO DOUBLERS. (M) 2L72 4F RT 20051220002152005122000215NM 2005 12 20 ASAA0580496 120050926A532199365463 FLOOR PANEL DOUG MD80 MD83 3023681NM FS 160-180 DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - DURING HV-CHECK, FOUND PAX CABIN FLOOR PANEL HAS CORRODED INSERTS WITH DELAMINATION AROUND INSERTS. REPLACED FLOOR PANEL. (M) 2L72 4F RT 20051220002172005122000217NM 2005 12 20 ASAA0510301 120050915A53206517684672 INTERCOSTAL BOEING737 737298C 1384490NM PWA JT8 JT8D17 52049NE FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02745AS 20794 INTERCOSTAL WEB FOUND CRACKED AT BSTA 295, STR 8 LT. CRACKED INTERCOSTAL WEB AT BSTA 295 AND STR 8 LT REPAIRED, EO. (K) 2L72 4F4 FRTA16WE E2EA 20051220002182005122000218NM 2005 12 20 ASAA0580502 120050926A53209936534139 FLOOR SUPPORT DOUG MD80 MD83 3023681NM FS 160-200 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - DURING HV CHECK, PAX CABIN FLOOR TRACK CORRODED. REPLACED TRACK. (M) 2L72 4F RT 20051220002202005122000220NM 2005 12 20 ASAA0510324 120050922A552165538341 CLEVIS BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE VERTICAL STAB CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02740AS 22578 CORROSION ON VERTICAL STABILIZER AFT SPAR LT FAIL SAFE CLEVIS FACES NOT PARALLEL TO EACH OTHER. FACES MACHINED IAW EA. (K) 2L72 4F4 F A16WE E2EA 20051220002212005122000221EU 2005 12 20 ASOA051000 120051118A3350 LAMP AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27637AS 383 DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY LIGHT ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. (M) 2H72 4T RTA53EU 20051220002232005122000223NM 2005 12 20 ASAA0510325 120050928A534765549711 SEAT TRACK BOEING737 737298C 1384490NM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02745AS 20794 PASSENGER CABIN BSTA 570-540, NR2 FLOOR PANEL FROM LT SIDE, RT SIDE SEAT TRACK BEAM UPPER AND LOWER AREAS HAVE CORROSION. CORRODED SEAT TRACK AND SEAT TRACK BEAM REPAIRED IAW SRM. (K) 2L72 4F4 FRTA16WE E2EA 20051220002242005122000224EA 2005 12 20 ASOA051007 120051120A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27905EV 7632 DURING A GROUND INSPECTION IN VPS, THE EMERGENCY CEILING LIGHT AT ROW 10 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY CEILING LIGHT AT ROW 10. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051220002252005122000225NM 2005 12 20 ASAA0510326 120050929A531165465637 FAILSAFE BOEING737 737298C 1384490NM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02745AS 20794 CORRODED FAIL SAFE ANGLE AT BSTA 967, BETWEEN STRINGER 27 LT AND 27 RT IS CORRODED. BSTA 967 BETWEEN STRINGER 27 RT AND 27 LT FAIL SAFE ANGLE REPAIRED IAW SRM. (K) 2L72 4F4 FRTA16WE E2EA 20051220002262005122000226EA 2005 12 20 ASOA051008 120051120A2612 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA FIRE WARNING SYSILLUMINATED A ASOAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27717EV 10088 DURING CLIMB-OUT FROM LAX-SLC, THE CREW RECEIVED A WHITE FIRE SYSTEM FAULT STATUS MESSAGE WHICH DISAPPEARED AFTER A FEW MINUTES. THE AIRCRAFT LANDED SAFELY IN SLC. MAINTENANCE TESTED THE FIRE SYSTEM AND COULD NOT DUPLICATE THE FAULT ON THE GROUND. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051220002282005122000228WP 2005 12 20 ASAA0580479 120050904A520059114003 DOOR DOUG DC9 DC982 3022082WP FS 95-100 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02931AS 49232 OKC - DURING C-CHECK, FOUND PREVIOUSLY REPAIRED AREA OF FUSELAGE BELOW EXTERNAL POWER DOOR IS DENTED. REMOVED DAMGAED AREA. INSTALLED REPAIR DOUBLER. (M) 2L72 4F A6WE 20051220002292005122000229NM 2005 12 20 ASAA0540354 120050717A57536546486150 SKIN BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU T/E FLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02706AS 28894 RT IB MID FLAP AFT WEDGE HAS NUMEROUS DENTS. REMOVED DENTED AREA OF LOWER SKIN, FABRICATED AND INSTALLED FILLERS AND DOUBLERS IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051219002242005121900224WP 2005 12 19 05FDEA04323 120051215A5300 REPAIR DOUG DC10 DC1010 3022110WP BS 2007-2018 NONE A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568054 47808 EXTERNAL DOUBLER REPAIR FROM STA 2007 TO STA 2018 BETWEEN LONG 41 AND 48 LT. PERFORMED A INSPECTION OF REPAIR IAW SRM 53-20-00 FIG 4 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P1. 2L73 4F A22WE 20051219002252005121900225WP 2005 12 19 05FDEA04319 120051215A5230 REPAIR DOUG DC10 DC1010 3022110WP CARGO DOOR NONE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25563FE 46948 AFT CARGO DOOR AFT PAN HAS AN EXTERNAL DOUBLER AND ANGLE REPAIR DIM 7 X 1.5 INCH. PERFORMED INSPECTION ON DOUBLER AND ANGLE REPAIR IAW SRM 52-10-00 FIG 17 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2. 2L73 4F A22WE 20051219002322005121900232NM 2005 12 19 ASAA0510305 120050920A53136545768144 STRINGER BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02740AS 22578 YXX - FOUND CORROSION ON STRINGER 26R AT BS 500A. REPAIRED PER B737-200 SRM 53-10-3 FIGURE 1. (M) 2L72 4F A16WE 20051219002592005121900259NM 2005 12 19 DHL2005749010 120051031A7110 COWLING BOEING727 7272J0 138407ENM NR 3 ENGINE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01749DH 22013 NR 3 ENG NOSE COWL L/E RING AT 12 O'CLOCK POSITION HAS 2 EA DENTED AREAS. CUT OUT DAMAGED AREA SIZE 5 1/4 INCHES X 5 3/4 INCHES ON NR 3 ENG NOSE COWL L/E RING AT 12 O'CLOCK IAW B727 SRM 54-30-3 FIG 2. FABBED FILLER FROM 2024T3 .071 SIZE 5 1/4 INCHES BY 5 3/4 INCHES PO NR 9002373 AND DOUBLERS FROM 2024 T3 .071 SIZES 8 INCHES BY 1 1/2 INCHES, 7 1/2 INCHES BY 1 1/2 INCHES, 4 INCHES BY 3/4 INCHES AND 4 INCHES BY 3/4 INCHES PO 9002373 IAW B727 SRM 54-30-3 FIG 2. TREATED AND PRIMED PARTS AND AREA IAW B727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B727 SRM 54-30-3 FIG 2. 2L73 4F RTA3WE 20051219002602005121900260EU 2005 12 19 05FDEA04220 120051210A2910 LINE AIRBUS300 A300F4605R 3930327EU NR 1 HYD SYSTEM CHAFED A FDEAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 SO25658FE 752 ABOUT 5 MIN PRIOR TO DESCENT FOR KMEM ARRIVAL HAD ECAM GREEN HYD SYSTEM LOW LEVEL LGT WITH QTY ON OVERHEAD AND ECAM SHOWING AT RED DOT/LOW. RAN ALL CHECKLISTS, DECLARED EMERGENCY, CRANKED GEAR & STOPPED ON CENTER OF RWY AT END OF RWY 36C TOW-IN NO FURTHER PROBLEM. FOUND LINE FROM NUMBER ONE ENGINE HAD TWO HOLES FROM CHAFING AGAINST FITTINGS IN PYLON. REPAIRED LINE IAW AMM 20-23-11-0. LEAKED CHECKED LINES AND SERVICED GREEN SYSTEM HYDS. CYCLED GEAR SEVERAL TIMES, GREEN OPS OK. 2L72 4F RTA35EU 20051219002632005121900263CE 2005 12 19 DXTA200501136 120051210A3240 CONNECTOR CESSNA500 560CESSNA 2076750CE BRAKES LOOSE E DXTAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07358QS 5600455 UPON APPLYING BRAKES FROM A NORMAL TAXI SPEED, THERE IS INITIALLY NO BRAKING RESPONSE, FOLLOWING BY A HARD, GRABING BRAKE, FEELS AS THROUGH THE ANTI SKID IS NOT ALLOWING THE BRAKES TO FUNCTION, THEN GRABS. BLED BRAKE SYSTEM. PERFORMED FUNCTIONAL CHECK OF BRAKE SYSTEM. SYSTEM CHECK NORMAL. FOUND LOOSE CONNECTOR IN LT WHEEL WELL. TIGHTENED CONNECTOR. PERFORMED TRANSDUCER CHECK AND TAXI CHECK. BOTH CHECKS NORMAL. ALL WORK DONE IAW CITATION 560 MM 32-42-00. 2L72 4F RTA22CE 20051219002682005121900268CE 2005 12 19 DXTA200501138 120051211A3213 STRUT CESSNA750 750 2076810CE MLG LEAKING E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07952QS 7500200 AFTER TAKEOFF AND SELECTING THE GEAR UP THE NOSE WHEEL WOULD NOT RETRACT. SELECTED THE GEAR DOWN AND RECEIVED 3 GREEN LIGHTS AND NO RED LIGHT. AFTER EXTENDING THE GEAR THE GEAR SELECT HANDLE WAS LOCKED IN THE DOWN POSITION AND COULD NOT MOVED. JACKED A/C FOUND THAT STRUT WOULD NOT EXTEND ENOUGH TO MAKE SWITCH. STRUT LEAKING EXTERNALLY & INTERNALLY. SERVICED TO MAKE EXTEND IAW 750 M/M 12-10-38, WILL FERRY TO WCSC ON SPECIAL FLIGHT PERMIT FOR STRUT REBUILD. 2L72 4J RTT00007WI 20051219002722005121900272NM 2005 12 19 SB05169 120051122A3520 OXYGEN MASK BOEING737 7373B7 1384580NM SEAT 1DF FAILED A USAABG EMER. DESCENT O2 MASK DEPLOYED O OTHER DEDESCENT 1 EA19512AU 23595 CLT FLT 1058 DURING EMERGENCY DESCENT, CREW REPORTED THE OXYGEN MASKS AT SEAT 1DF, 3DF AND AT THE AFT LEFT LAV FLIGHT ATTENDANT STATION DID NOT DEPLOY. MAINTENANCE, DROPPED OXYGEN MASK DOORS, THAT DID NOT DEPLOY, REPLACED ALL AFFECTED OXYGEN GENERATORS AND REPACKED OXYGEN MASKS IN PSU'S. OPERATIONALLY CHECKED OXYGEN MASKS AND DOORS PER MM 35-22-00. OPERATIONAL CHECK GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F RTA16WE 20051219002752005121900275NM 2005 12 19 DHL2005749019 120051102A5230 DOOR BOEING727 727200 138407ENM CARGO BAY DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01749DH 22013 FWD LWR CARGO DOOR DENTD AT BS 615 BETWEEN STRS 23R AND 24R MARKED. CUT OUT DAMAGED AREA DIM 2 INCHES BY 1 INCH FABBED DOUBLER 2024T3 .063 PO5070593 DIM 9 3/4 INCHES BY 8 INCHES IAW B727 SRM 52-00-30 FIG 3. TREATED AND PRIMED REPAIR EREA AND PART IAW B727 SRM 51-10-2. INSTALLED DOUBLER IAW B727 SRM 52-00-3 FIG 3. 2L73 4F RTA3WE 20051219002762005121900276NM 2005 12 19 DHL2005749020 120051102A5753 SKIN BOEING727 727200 138407ENM LT FOREFLAP DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01749DH 22013 LT WING IB FOREFLAP DELAMINATED AT UPPER SURFACE IB EDGE. REMOVED UPPER SURFACE S/S RUBSTRIP AND DELAMINATED UPPER SKIN APPROX 14" BY 4" CUTOUT DAMAGED CORE APPROX 3 1/4" BY 6" FAB`D SEPTUM APPROX 3 1/4" BY 5 3/4" FROM 2024T3 .012 PO 900534 AND REPAIR CORE APPROX 3 1/4" BY 6" FROM DUR-5052-44-3/16-NE PO 286849 VACUUM BAGGED AND BONDED REPAIR CORE AND SEPTUM FAB`D REPLACEMENT RUBSTRIP APPROX 14" BY 3" FROM 301 1/2 HD .016 PO 9002619 REPAIR SKIN APPROX 14" BY 4" AND EXTERNAL DOUBLER APPROX 14 3/4" BY 5 1/2" FROM 2024T3 .016 PO 9002576 VACUUM BAGGED FOR BONDING. BONDED AND CLEANED TREATED PRIMED AND SEALED REPAIR. BONDED REPLACEMENT RUBSTRIP ALL MX ACTIONS ACCOMP IAW B727 SRM 51-40-20, 51-40-23 FIG 1, 57-50-2 2L73 4F RTA3WE 20051219002792005121900279NM 2005 12 19 DHL2005749024 120050107A5347 SEAT TRACK BOEING727 727200 138407ENM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01749DH 22013 FOUND CORROSION ON SEAT TRACK AT RBL 45 BS 520-580. REMOVED SEAT TRACK RBL 45.5 BS 480-590 IAW B727 SRM 51-30-2 AND 53-10-5 FIG 1. REPLACED SEAT TRACK P/N BAC1520-792 PO 9002389 LOCATED AND DRILLED IAW B727 SRM 53-10-5 FIG1 DIM 110". TREATED AND PRIMED SEAT TRACK IAW B727 SRM 51-10-2. INSTALLED SEAT TRACK RBL 45.5 BS 480-590 IAW B727 SRM 51-30-2 AND 53-10-5 FIG 1. 2L73 4F RTA3WE 20051219002872005121900287EU 2005 12 19 ASOA05932 120051029A2421243230 GENERATOR AEROSPATR72 ATR72212 8680945EU RT ENGINE MALFUNCTIONED A ASOAK NONE BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 SO27636AS 375 DURING CRUISE FROM ATL-PFN, THE CREW REPORTED AN ELECTRICAL ODOR WITH A RIGHT AC WILD GENERATOR FAULT. AIRCRAFT CONTINUED TO PFN WHERE IT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE RIGHT AC WILD GENERATOR. OPERATIONAL CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20051219002892005121900289EA 2005 12 19 ASOA05930 120051029A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA EXTERIOR INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27935EV 8037 DURING A HANGAR INSPECTION IN BTR, THE AFT EMERGENCY LIGHT ON THE LEFT SIDE OF THE FUSELAGE WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE AFT EMERGENCY LIGHT ON THE LEFT SIDE OF THE FUSELAGE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051219002942005121900294EA 2005 12 19 ASOA05925 120051028A5320 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27838AS 7276 DURING A C-CHECK IN MCN, THE FLOOR ATTACH ANGLE, AT BL 45 LT, FS 559 PLUS 112 TO PLUS 80, WAS FOUND TO BE CORRODED. AFTER MAINTENANCE BLENDED, ALODINED, AND PRIMED THE FLOOR ATTACH ANGLE AT BL 45 LT, FS 559 PLUS 112 TO PLUS 80 IAW REO 601R-53-61-1564, IT WAS FOUND TO BE WITHIN LIMITS. (M) 2L72 4F RTA21EA 20051219002962005121900296EA 2005 12 19 ASOA05923 120051028A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA BS 605 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27838AS 7276 DURING A C-CHECK IN MCN, THE FORWARD FS 605, AT STRINGER 26-27, WAS FOUND TO BE CORRODED. AFTER MAINTENANCE BLENDED, ALODINED, AND PRIMED THE FORWARD FS 605, AT STRINGER 26-27, IAW REO 601R-53-61-1565, IT WAS FOUND TO BE WITHIN LIMITS. (M) 2L72 4F RTA21EA 20051219003002005121900300EA 2005 12 19 ASOA05918 120051027A5320601R311719 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27838AS 7276 DURING A C-CHECK IN MCN, THE RIGHT OUTBOARD CLIP AT FS 484, RBL 36 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE RIGHT OUTBOARD CLIP AT FS 484, RBL 36 IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20051219003082005121900308EU 2005 12 19 ASOA05965 120051109A3350LP1670 LIGHT AEROSPATR72 ATR72212 8680945EU CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27630AS 336 FLT 4223 - DURING A GROUND INSPECTION IN MGM, THE EMERGENCY FLOOR TRACK LIGHT, NEAR SEAT 4B, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY FLOOR TRACK LIGHT, NEAR SEAT 4B, AND RECONNECTED THE CANNON PLUG. (M) 2H72 4T RTA53EU 20051219003162005121900316EA 2005 12 19 ASOA05973 120051112A5260601R31707651 STEP CNDAIRCL600 CL6002C10 1390015EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27709EV 10068 DURING A C-CHECK IN MCN, THE PASSENGER DOOR TOP STEP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR TOP STEP AND THE STEP TO FUSELAGE HINGE (P/N CC670-31981-3). (M) 2L72 4F RTA21EA 20051219003192005121900319EA 2005 12 19 ASOA05976 120051107A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA COCKPIT ILLUMINATED A ASOAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27924EV 7830 FLT 4490 - DURING CRUISE FROM XNA-CVG, AT APPROX 25,000 FEET, THE CREW RECEIVED A RIGHT REVERSER UNLOCKED CAUTION MESSAGE. THE CREW COMPLIED WITH THE QRH. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED INTO EVV, WHERE IT LANDED SAFELY. OUTSTATION MAINTENANCE DEACTIVATED THE RIGHT THRUST REVERSER IAW MEL NR 78-30-01. MAINTENANCE REACTIVATED THE RIGHT THRUST REVERSER BY REINSTALLING THE BLEED LINE AND CONNECTORS. OPERATIONAL CHECKS WERE GOOD AND NO DEFECTS WERE NOTED. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051219003242005121900324EA 2005 12 19 ASOA05981 120051115A25602618 FLASHLIGHT CNDAIRCL600 CL6002C10 1390015EA COCKPIT DEFECTIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27744EV 10157 DURING A GROUND INSPECTION IN ATL, THE FIRST OFFICERS FLASHLIGHT ON/OFF SWITCH KEPT MOVING INTO THE ON POSITION. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS FLASHLIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051220000122005122000012NM 2005 12 20 05FDEA04331 120051215A5710 REPAIR BOEING727 727200 138407ENM RT WING ROOT UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25274FE 22039 FOUND REPAIR LOCATED ON RIGHT WING L/E WING ROOT REPAIR REQUIRES EVALUATION FOR COMPLIANCE WITH FAA APPROVED DATA. REPAIR WAS DETERMINED ACCOMPLISHED IAW SRM 57-30-4 FIG 2 BASED ON AN EXTERNAL VISUAL EVALUATION WITH REPAIR INSTALLED, CONSISTED OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBER, MATERIAL THICKNESS AND TYPE AND GENERAL WORKMANSHIP OF PREVIOUS INSTALLATION, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2L73 4F RTA3WE 20051220000222005122000022EU 2005 12 20 05FDEA04334 120051215A5320 FLOOR SUPPORT AIRBUS300 A300B4605R 3930308EU FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25672FE 779 MAIN CABIN BEAM SUPPORT CRACK AT FR 38 RBL 100. REMOVED AND REPLACED DAMAGED FLOOR SUPPORT AT FR 38 RBL 100 IAW SRM 51-40-21 AND DWG 13-A-537-81038. 2L72 4F RTA35EU 20051220000302005122000030CE 2005 12 20 DXTA200501133 120051207A3240 BRAKE ASSY CESSNA500 560CESSNA 2076750CE MLG MALFUNCTIONED E DXTAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07312QS 5600312 CO-PILOTS BRAKES GO TO THE FLOOR AND WHEN BRAKES DID GRAB, THE AIRPLANE TURNED 30 DEGREES HARD TO THE RIGHT. ON ARRIVAL OF ACFT INSPECTED BRAKES FOUND TO APPEAR RELATIVELY NEW. PERFORMED SATISFACTORY BRAKE WEAR CHECK. COMPLETED BRAKE BLEEDING PROCEDURE IAW CE-560 MM 32-42-00. PERFORMED SATISFACTORY OPS AND LEAK CHECK GOOD. 2L72 4F RTA22CE 20051220000582005122000058SO 2005 12 20 ON116HM120505JC 120051205A3234A48617 HANDLE GULSTMG1159 GIV 3980115SO MLG INOPERATIVE E AOQAO OTHER O OTHER NRNOT REPORTED 1 EA11116HM 1024 RT MAIN GEAR DOWN LOCKED GREEN LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. INSPECTED MAIN GEAR SYSTEM AND FOUND GEAR SELECTOR HANDLE WIRE BUNDLE CHAFFING CAUSING FAULT. REPLACED HANDLE ASSY AND ACCOMPLISHED SEVERAL GEAR SWINGS WITH SATISFACTORY RESULTS. (K) 2L72 4F RTA12EA 20051220000632005122000063SO 2005 12 20 SIMA200532902 120051117A531314533888001 STRINGER EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FR 52 CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21825AE8374 145589 STRINGER 19R WAS FOUND TO BE CHAFED AT FRAME 52. BLENDED AND TREATED THE CHAFED AREA WITH EA934. FABRICATED A REPAIR ANGLE AND 2 SHIMS. REPAIR DONE IAW SRM. (K) 2L72 4F4 FRTT00011ATTE6CH 20051220000732005122000073EU 2005 12 20 KBM2005F00351 120051125A243223761 BATTERY SNIAS 350 AS350B 8680801EU TMECA ARRIELARRIEL1B 6OO30NE MASTER INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH2 2957 UNIT STARTS SLOW. REMOVED AND REPLACED BATTERY. (K) 1G71 3U3 U H9EU E19EU 20051220000942005122000094WP 2005 12 20 ASAA0580432 120050807A5313593643437 LONGERON DOUG DC9 DC982 3022082WP FS 294-313 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02935AS 49236 OKC - DURING C-CHECK, FOUND LONGERON CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR CHANNEL. (M) 2L72 4F A6WE 20051220000982005122000098WP 2005 12 20 ASAA0580414 120050805A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP CABIN DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02947AS 53020 OKC - DURING C-CHECK, FOUND CABIN FLOOR PANEL IS CREASED ACROSS TOP. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20051220001112005122000111WP 2005 12 20 ASAA0580439 120050807A5311SR09530057U23 FRAME DOUG DC9 DC982 3022082WP FS 1322 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02935AS 49236 OKC - DURING C-CHECK, FOUND FRAME CORRODED. REPLACED DAMAGED FRAME SECTION. (M) 2L72 4F A6WE 20051220001152005122000115NM 2005 12 20 ASAA0580489 120050926A532199365833 FLOOR PANEL DOUG MD80 MD83 3023681NM FS 826-864 DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - DURING HV C-CHECK, FOUND PAX CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RT 20051220001302005122000130EU 2005 12 20 USAA051536 120051213A5320D5311281820401 FLOOR SUPPORT AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19113UW 1141 Y254, BETWEEN C-16 & C-22 CORRODED. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-72-11; CORR LEVEL 1; TASK JA-220-53500. DEFECT SIZE: 4 X 3 INCH. 2L72 4F RTA28NM 20051220001322005122000132WP 2005 12 20 ASAA0580484 120050904A523059101413 SKIN DOUG DC9 DC982 3022082WP FS 1188-1200 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02931AS 49232 OKC - DURING C-CHECK, FOUND AFT CARGO BAY DOOR SKIN DENTED. REMOVED DAMAGED AREA. INSTALLED EXTERNAL DOUBLER AND TWO INTERNAL STRIP DOUBLERS. (M) 2L72 4F A6WE 20051220001392005122000139SO 2005 12 20 C2XA05TY060 120051209A531514521713003 FLOORBEAM EMB 145 EMB145XR 3260214SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711107 145654 TYS, DURING A SCHEDULED INSPECTION, CORROSION WAS FOUND ON FLOORBEAM AT CARBON FIBER CROSS BEAM AT FRAME 20. MAINTENANCE REMOVED THE ANGLE AND DAMAGED AREA FROM THE LEFT OMEGA BEAM, FABRICATED NEW REPAIR PIECES, ALODINED, PRIMED AND INSTALLED IAW EMB145XR SRM 51-20-03, 53-00-10 AND CPM-51-21-04/05/06. 2L72 4F RT 20051220001672005122000167SO 2005 12 20 GUU2005F00057 120051014A3210 HUB CAP EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE LT MLG LOOSE A GUUAO OTHER O OTHER TXTAXI/GRND HDL 1 SO17282AS 120226 DURING TAXI, RT BRAKE WEAK, LT BRAKE PULLS AIRCRAFT TO THE LT. RESECURED LT WHEEL SPEED TRANSDUCER AND HUB CAP. (K) 2L72 4T4 TRTA31SO E20NE 20051220001682005122000168NM 2005 12 20 ASAA0540471 120050916A53116546525103 FRAME BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02793AS 26880 PAE - FRAME CRACKED AT BIN RAIL STATION. CUTOUT DAMAGE AT FRAME BIN RAIL SUPPORT AND FABRICATED AND INSTALLED REPAIR IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051220001692005122000169EA 2005 12 20 ASOA05995 120051117A3350OL3071BPEGPL LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27847AS 7335 DURING A GROUND INSPECTION IN ATL, THE EMERGENCY LIGHT, NEAR THE TOP OF THE PASSENGER DOOR STEPS, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY LIGHT, NEAR THE TOP O THE PASSENGER DOOR STEPS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051220001702005122000170NM 2005 12 20 ASAA0540376 120050803A5311654659320 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02778AS 25110 YXX - FWD CARGO PIT BILGE, CORROSION ON FRAME LWR FLANGE @ B STA 500B, WBL 95. SHEAR TIE REPAIR ACCOMPLISHED IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051220001732005122000173EA 2005 12 20 ASOA051003 120051117A1100S72451 PLACARD CNDAIRCL600 CL6002C10 1390015EA CABIN WORN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27748EV 10158 DURING A C-CHECK IN MCN, THE EXIT PLACARD ON THE PASSENGER DOOR WAS FOUND WORN. MAINTENANCE REMOVED AND REPLACED THE EXIT PLACARD ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20051220001842005122000184NM 2005 12 20 ASAA0580492 120050926A5321993919511 FLOOR PANEL DOUG MD80 MD83 3023681NM FS 807-826 DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - DURING HV-CHECK, PASSENGER CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RT 20051220001862005122000186WP 2005 12 20 ASAA0580429 120050807A532099579121 INTERCOSTAL DOUG DC9 DC982 3022082WP FS 693-712 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02935AS 49236 OKC - DURING C-CHECK, FOUND INTERCOSTAL CORRODED. REPLACED INTERCOSTAL. (M) 2L72 4F A6WE 20051220001882005122000188EU 2005 12 20 ASOA05997 120051117A33507012210 LAMP AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27631AS 362 DURING A HANGAR INSPECTION IN MCN, THE EMERGENCY LIGHT ASSEMBLY ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. 2H72 4T RTA53EU 20051220002022005122000202WP 2005 12 20 ASAA0580481 120050904A5330591140045 SKIN DOUG DC9 DC982 3022082WP FS 37-53 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02931AS 49232 OKC - DURING C-CHECK, FOUND FUSELAGE SKIN DENTED. REMOVED DAMAGED AREA. INSTALLED FINGER DOUBLER, INTERNAL REPAIR DOUBLER, AND FILLER. (M) 2L72 4F A6WE 20051220002032005122000203WP 2005 12 20 ASAA0580460 120050808A5320SR0952200089 SPACER DOUG DC9 DC982 3022082WP FS 375-427 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02935AS 49236 OKC - DURING C-CHECK, MID CARGO BAY DOOR SILL JAMB BEAM DOUBLER, SPACER, CORRODED. REPLACED SPACER. (M) 2L72 4F A6WE 20051220002162005122000216NM 2005 12 20 ASAA0540421 120050819A5311654653181 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02779AS 25111 FRAME AT BSTA 500, RBL 1, WL 154 CRACKED. REPAIRED FRAME IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051220002192005122000219NM 2005 12 20 ASAA0580505 120050926A5321 FLOOR PANEL DOUG MD80 MD83 3023681NM CABIN DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - FOUND HV-CHECK, PASSENGER CABIN FLOOR PANEL IS DELAMINATED. REPLACED PANEL. (M) 2L72 4F RT 20051220002272005122000227WP 2005 12 20 ASAA0580428 120050805A5313593271725 LONGERON DOUG DC9 DC983 3022083WP FS 756 DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02947AS 53020 OKC - DURING C-CHECK, FREEZE PLUG IN OVERSIZED HOLE IN LONGERON. REMOVED DAMAGED SECTION. SPLICED IN NEW LONGERON SECTION. (M) 2L72 4F RTA6WE 20051220002322005122000232SO 2005 12 20 SIMA200531104 120051103A3150 WARNING SYSTEM EMB 135 EMB135KL 3260302SO COCKPIT FALSE ACTIVATIONA SIMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW21811AE 145529 FLT 4678 - RDU - CREW RECEIVED NUMEROUS WARNING, SPS 1-2 INOP, STICK PUSHER FAIL SPS ADVANCED AND STALL PROTECTION CUT OUT NUMBER 2 BAR ILLUMINATED. RESET STALL PROTECTION SYSTEM AND PERFORMED TEST OF SYSTEM IAW EMB 140 AMM 27-36-00-700-801A. ALL OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20051220002332005122000233NM 2005 12 20 ASAA0540356 120050717A53206547957U11 STRAP BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FLOORBEAM CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02706AS 28894 AFT PIT FLOOR BEAM STRAP HAS CORROSION AS MARKED. REMOVED DAMAGED STRAP, INSTALLED NEW STRAP IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051220002342005122000234NM 2005 12 20 ASAA0580495 120050926A5321 FLOOR PANEL DOUG MD80 MD83 3023681NM CABIN CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - DURING HV CHECK, FOUND PAX CABIN FLOOR PANEL HAS CORRODED INSERTS WITH DELAMINATION AROUND INSERTS. REPLACED FLOOR PANEL. (M) 2L72 4F RT 20051220002352005122000235NM 2005 12 20 ASAA0540357 120050717A52306546921230 SKIN BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU CARGO DOOR SCRATCHED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02706AS 28894 FWD CARGO DOOR SCRATCHED. REMOVED DAMAGE, FABRICATED AND INSTALLED DOUBLER IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051220002362005122000236WP 2005 12 20 ASAA0580423 120050805A53305920323509 SKIN DOUG DC9 DC983 3022083WP FS 471-487 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02947AS 53020 OKC - DUIRNG C-CHECK, FOUND FUSELAGE SKIN DENTED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20051220002372005122000237WP 2005 12 20 ASAA0580418 120050805A5320993053866 CUSP WEB DOUG DC9 DC983 3022083WP FS 237-313 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02947AS 53020 OKC - DURING C-CHECK, FOUND RIGHT UPPER CUSP WEB CORRODED. REMOVED CORRODED SECTION. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20051220002382005122000238WP 2005 12 20 ASAA0580420 120050805A53209930538U12 CUSP WEB DOUG DC9 DC983 3022083WP FS 522-579 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02947AS 53020 OKC - DURING C-CHECK, FOUND RIGHT CUSP WEB CORRODED. REPLACED CUSP WEB. (M) 2L72 4F RTA6WE 20051220002402005122000240NM 2005 12 20 ASAA0540359 120050717A57536546486149 WEDGE BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU LT MIDFLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02706AS 28833 LT IB MID FLAP AFT WEDGE HAS NUMEROUS DENTS. REMOVED DAMAGED AREA. FABRICATED AND INSTALLED FILLERS AND DOUBLERS AND INSTALLED REPAIR PIECES IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051220002422005122000242WP 2005 12 20 ASAA0580424 120050805A53305920323509 SKIN DOUG DC9 DC983 3022083WP FS 569-588 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02947AS 53020 OKC - DURING C-CHECK, FOUND FUSELAGE SKIN DENTED. COLD-WORKED DENTED AREA. INSTALLED INTERNAL REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20051220002432005122000243WP 2005 12 20 ASAA0580419 120050805A53209930538U77 CUSP WEB DOUG DC9 DC983 3022083WP FS 598-712 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02947AS 53020 OKC - DURING C-CHECK, FOUND RIGHT CUSP WEB CORRODED. REPLACED CUSP WEB. (M) 2L72 4F RTA6WE 20051220002462005122000246WP 2005 12 20 ASAA0580425 120051219A5330591140659 SKIN DOUG DC9 DC983 3022083WP FS 222 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02947AS 53020 OKC - DURING C-CHECK, FOUND FUSELAGE SKIN DENTED. COLD-WORKED DENTED AREA. INSTALLED INTERNAL REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20051220002482005122000248WP 2005 12 20 ASAA0580426 120050805A53305932717147 SKIN DOUG DC9 DC983 3022083WP FS 756 DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02947AS 53020 OKC - DURING C-CHECK, FOUND FREEZE PLUG IN FUSELAGE SKIN OVERSIZED HOLE. REMOVED DAMAGED AREA. INSTALLED EXTERNAL REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20051220002502005122000250WP 2005 12 20 ASAA0580500 120050926A532199365513 FLOOR PANEL DOUG DC9 DC983 3022083WP FS 196-256 DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - DURING HV CHECK, PAX CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20051220002512005122000251NM 2005 12 20 ASAA0540363 120050717A533065468822 SKIN BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02797AS 28892 SKIN GOUGED. REPAIRED IAW EA. (K) 2L72 4F4 FRTA16WE E21EU 20051220002522005122000252NM 2005 12 20 ASAA0580504 120050926A532199366393 FLOOR PANEL DOUG MD80 MD83 3023681NM FS 826-886 DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - FOUND HV-CHECK, PAX CABIN FLOOR PANEL IS DELAMINATED. REPLACED PANEL. (M) 2L72 4F RT 20051220002532005122000253WP 2005 12 20 ASAA0580472 120050505A5320993653473 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FS 160-200 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS 53450 OKC - FOUND C-CHECK, PAX CABIN FLOOR TRACK CORRODED. REPLACED DAMAGED TRACK. (M) 2L72 4F RTA6WE 20051220002562005122000256NM 2005 12 20 ASAA0540364 120050717A52426521631 SKIN BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU E/E BAY DOOR BENT A ASAAK NONE O OTHER ININSP/MAINT 1 NM02797AS 28892 EE BAY DOOR EXTERNAL SKIN BENT ON EDGE AT SEVERAL PLACES. REMOVED AND REPLACED EE BAY DOOR SKIN. (K) 2L72 4F4 FRTA16WE E21EU 20051220002572005122000257WP 2005 12 20 ASAA0580462 120050808A57535930476507 SKIN DOUG DC9 DC982 3022082WP TE FLAP DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02935AS 49236 OKC - FOUND DURING C-CHECK, LEFT WING OUTBOARD FLAP T/E OUTER SECTION DAMAGED, DENTED. BOND REPAIRED. (M) 2L72 4F A6WE 20051220002602005122000260NM 2005 12 20 ASAA0540365 120050720A57536546435335 FLAP BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU LEFT SPLIT A ASAAK NONE O OTHER ININSP/MAINT 1 NM02768AS 27082 LT OB AFT FLAP IB END T/E SPLIT. REMOVED AND REPLACED LT OB FLAP IAW AMM. (K) 2L72 4F4 FRTA16WE E21EU 20051220002622005122000262WP 2005 12 20 ASAA0580461 120050808A5340 ATTACH ANGLE DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02935AS 49236 OKC - DURING C-CHECK, FOUND AFT CARGO BAY FRAME ATTACH ANGLE CORRODED. REPLACED ATTACH ANGLE. (M) 2L72 4F A6WE 20051220002632005122000263WP 2005 12 20 ASAA0580463 120050808A5320593038501 SUPPORT BEAM DOUG DC9 DC982 3022082WP FS 1155-1212 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02935AS 49236 OKC - DURING C-CHECK, FOUND AFT CARGO BAY DOOR SUPPORT BEAM CORRODED. REPLACED BEAM. (M) 2L72 4F A6WE 20051220002672005122000267NM 2005 12 20 ASAA0540371 120050803A5534655484222 SKATE ANGLE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU VERTICAL FIN CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 RT AFT SKATE ANGLE FOR VERTICAL FIN CHAFED 18 INCHES FROM AFT END ON OB SIDE. REMOVED AND REPLACED AFT SKATE FOR VERTICAL FIN. (K) 2L72 4F4 FRTA16WE E21EU 20051220002692005122000269NM 2005 12 20 ASAA0580507 120050926A5320993663218 INTERCOSTAL DOUG MD80 MD83 3023681NM FS 522-541 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - DURING HV-CHECK, FOUND INTERCOSTAL CORRODED. REPLACED INTERCOSTAL. (M) 2L72 4F RT 20051220002712005122000271NM 2005 12 20 ASAA0580526 120050928A5523591041449 TAB DOUG MD80 MD83 3023681NM RT ELEVATOR DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - DURING HV-CHECK, FOUND RIGHT ELEVATOR GEARED TAB IS DELAMINATED ON LOWER SURFACE AT TRAILING EDGE. REMOVED DAMAGED SECTION. INSTALLED SKIN REPAIR FILLER AND DOUBLER. (M) 2L72 4F RT 20051220002722005122000272NM 2005 12 20 ASAA0580508 120050926A5320993663217 INTERCOSTAL DOUG MD80 MD83 3023681NM FS 522-541 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - FOUND DURING HV-CHECK, INTERCOSTAL CORRODED. REPLACED INTERCOSTAL. (M) 2L72 4F RT 20051220002732005122000273NM 2005 12 20 ASAA0540373 120050804A531065458752B CREASE BEAM BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 CORROSION ON CREASE BEAM WEB BSTA 336-344, RBL 62, WL 208. REPAIRED CREASE BEAM WEB IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051220002742005122000274NM 2005 12 20 ASAA0580510 120050926A53209910151101 CUSP WEB DOUG MD80 MD83 3023681NM FS 927-946 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - FOUND HV CHECK, CUSP WEB CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RT 20051220002772005122000277NM 2005 12 20 ASAA0580493 120050926A532199365535 FLOOR PANEL DOUG MD80 MD83 3023681NM FS 200-256 DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - FOUND HV-CHECK, PAX CABIN FLOOR PANEL DELAMINATED. REPLAED FLOOR PANEL. (M) 2L72 4F RT 20051220002782005122000278NM 2005 12 20 ASAA0540379 120050804A5534655484226 SKATE ANGLE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU VERTICAL FIN CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 RT FWD SKATE ANGLE FOR VERTICAL FIN CHAFED 3 INCHES FROM FWD END ON IB SIDE. REMOVED AND REPLACED FWD SKATE ANGLE FOR VERTICAL FIN. (K) 2L72 4F4 FRTA16WE E21EU 20051220002812005122000281NM 2005 12 20 ASAA0580509 120050926A532059360715 INTERCOSTAL DOUG MD80 MD83 3023681NM FS 1212-1231 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - DURING HV CHECK, FOUND INTERCOSTAL CORRODED. REPLACED INTERCOSTAL. (M) 2L72 4F RT 20051220002832005122000283NM 2005 12 20 CALA0500441 120051216A5330146N35319 SKIN BOEING757 757224 1384958NM STA 1500-1520 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713138 30351 INSPECTION FOUND CORROSION ON OUTER SKIN SURFACE OF LT GTE AIRPHONE ANTENNA CUTOUT, STA 1500-1520, S28L TO S29L. THE CORRODED AREA WAS CUT OUT AND AN INTERIM REPAIR WAS INSTALLED IAW ECRA 5330-03511. A DIP WAS ISSUED TO ACCOMPLISH A PERMANENT REPAIR WITHIN 12 MONTHS. 2L72 4F RTA2NM 20051220002842005122000284NM 2005 12 20 CALA0500442 120051217A5315147A5506 FLOORBEAM BOEING737 737724 13844BYNM STA 986 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716709 28779 INSPECTION FOUND FLOORBEAM FORWARD FLANGE CORRODED AT SCREW HOLE, STA 986, RBL 30. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, REPAIR 1. 2L72 4F RTA16WE 20051220002862005122000286NM 2005 12 20 CALA0500444 120051217A5315149A5510 FLOORBEAM BOEING737 737724 13844BYNM STA 312 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716709 28779 INSPECTION FOUND FORWARD FLOOR STRUCTURE T-CAP (FLOORBEAM UPPER CHORD) CORRODED AT STA 312, LBL 29 APPROXIMATELY 24 INCHES O/B OF L-1 DOOR THRESHOLD. THE FLOORBEAM UPPER CHORD WAS REPAIRED IAW ECRA 5321-01323. 2L72 4F RTA16WE 20051220002872005122000287NM 2005 12 20 CALA0500445 120051217A5320147A566041 INTERCOSTAL BOEING737 737724 13844BYNM STA 947.5-967 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716709 28779 INSPECTION FOUND INTERCOSTAL AT STA 947.5 TO 967, LBL 46 CORRODED. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-02 AND 51-40-02. 2L72 4F RTA16WE 20051220002902005122000290NM 2005 12 20 ASAA0540393 120050816A5311654652912 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 CRACKED FRAME AT BIN RAIL STA 440. REPAIRED CRACKED FRAME AT BIN RAIL BSTA 440, STR 8L - 9L IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051220002922005122000292NM 2005 12 20 ASAA0540400 120050816A5320654587545 SILL BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 CORROSION ON FWD GALLEY MOPSILL. REMOVED AND REPLACED FWD GALLEY MOPSILL. (K) 2L72 4F4 FRTA16WE E21EU 20051220002972005122000297EU 2005 12 20 USAA051568 120051219A5350F5331533220000 SUPPORT AIRBUS330 A330323 3930335EU FAIRING FLANGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 SEVERAL SPOTS OF CORROSION FOUND ON RECEPTACLES, FS 40.2, CENTER, DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-42-00 AND 51-72-11, DEFECT SIZE: .25" X 1". 2L72 4F RTA46NM 20051220002982005122000298EU 2005 12 20 USAA051562 120051219A5350F5331531220200 SUPPORT AIRBUS330 A330323 3930335EU FAIRING FLANGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 FOUND CORROSION ON RECEPTACLES, FRAME 39.1 CENTER. REPLACED SUPPORT FLANGE PER SRM 51-42-00 AND SRM 51-72-11, DEFECT SIZE: .25" BY 1". 2L72 4F RTA46NM 20051220002992005122000299EU 2005 12 20 USAA051563 120051219A5347F53311325200 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 FOUND CORROSION ON SEAT TRACK -Y450 FS 47. BLEND AREA, SEAT TRACK REPLACED PER SRM 53-31-15, 51-72-11, 51-74-00 CORROSION LEVEL 2; TASK C53-3170-01, DEFECT SIZE: 3" BY 1". 2L72 4F RTA46NM 20051220003002005122000300EU 2005 12 20 USAA051564 120051219A5347F53311325200 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 FOUND CORROSION FS 50.5, Y450. BLEND OUT AND REPLACED PART PER SRM 53-31-15 AND 51-74-00; CORROSION LEVEL 2; TASK C533170-01, DEFECT SIZE: 1.5" BY .5" BY .028". 2L72 4F RTA46NM 20051220003032005122000303EU 2005 12 20 USAA051583 120051219A5321F5367273400000 FLOOR PANEL AIRBUS330 A330323 3930335EU FR 23 DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 FOUND DELAMINATION FS 23. COMPOSITE DOUBLER INSTALLED PER SRM 53-02-00, DEFECT SIZE: 1" BY 4". 2L72 4F RTA46NM 20051220003042005122000304EU 2005 12 20 USAA051582 120051219A5321F5367111201400 FLOOR PANEL AIRBUS330 A330323 3930335EU FR 11 DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 FOUND DELAMINATION FS 11. COMPOSITE DOUBLER INSTALLED PER SRM 53-02-00, DEFECT SIZE: 2" BY 5". 2L72 4F RTA46NM 20051220003102005122000310NM 2005 12 20 ASAA0540413 120050816A53476546813 SEAT TRACK BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 CORROSION ON SEAT TRACK FLANGE, BSTA 344, LBL 45, WL 208. REMOVED AND REPLACED SEAT TRACK IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051220003112005122000311NM 2005 12 20 ASAA0540412 120050816A53206517688126 WEB BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 CORROSION ON WEB UNDER FWD ENTRY DOOR MOPSILL AT BSTA 333-342, LBL 58, WL 208. REPLACED WEB UNDER FWD ENTRY DOOR MOPSILL. (K) 2L72 4F4 FRTA16WE E21EU 20051220003122005122000312NM 2005 12 20 ASAA0540416 120050818A5322654659673 SHEAR TIE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02779AS 25111 SHEAR TIE AT FRAME 727C BL 0 IS CORRODED. REMOVED DAMAGED SECTION OF SHEAR TIE, FABRICATED AND INSTALLED REPAIR PIECES IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051220003132005122000313NM 2005 12 20 ASAA0540408 120050816A532069785402 DOUBLER BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 CORROSION ON FWD ENTRY DOOR MOPSILL WEB DOUBLER. REMOVED AND REPLACED IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051220003152005122000315NM 2005 12 20 ASAA0540415 120050816A53206522072536 INTERCOSTAL BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE MISDRILLED A ASAAK NONE W INADEQUATE Q C ININSP/MAINT 1 NM02771AS 25104 FWD CARGO BAY, BSTA 509, RBL 22, WL 154, INTERCOSTAL HAS A DRILL START. REMOVED, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051220003172005122000317NM 2005 12 20 ASAA0540414 120050816A5311654795965 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 CORROSION ON FRAME WEB BSTA 796, STR 24R. REMOVED CORROSION, OUT OF LIMITS AND REPAIRED IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051220003182005122000318NM 2005 12 20 ASAA0540418 120050818A53226546548110 SHEAR TIE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02779AS 25111 SHEAR TIE AND FRAME AT 747 BL0, RBL 5, IS CORRODED. REMOVED DAMAGED SECTION OF SHEAR TIE AND FRAME, FABRICATED AND INSTALLED REPAIR PIECES IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051220003212005122000321EU 2005 12 20 USAA051579 120051219A5321F5367113100000 FLOOR PANEL AIRBUS330 A330323 3930335EU FR 17 DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 FOUND DELAMINATION FS 17. COMPOSITE DOUBLER INSTALLED PER SRM 53-02-00, DEFECT SIZE: 2" BY 4". 2L72 4F RTA46NM 20051220003222005122000322EU 2005 12 20 USAA051578 120051219A5321F5367273300000 FLOOR PANEL AIRBUS330 A330323 3930335EU FR 7 Y-790 DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 FOUND DELAMINATION FS 7 Y-790. COMPOSITE DOUBLER INSTALLED PER SRM 51-77-1, DEFECT SIZE: 2" BY 5". 2L72 4F RTA46NM 20051220003252005122000325EU 2005 12 20 USAA051576 120051219A53214E33621 FLOOR PANEL AIRBUS330 A330323 3930335EU FR 32 Y1959 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 FOUND CORROSION FS 32 Y1959. MODIFIED PART INSTALED PER TR 53-02-01, DEFECT SIZE: 4" BY 16". 2L72 4F RTA46NM 20051220003262005122000326EU 2005 12 20 USAA051567 120051219A5350F5331532920000 FAIRING AIRBUS330 A330323 3930335EU FRAME 40 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 FOUND CORROSION FRAME 40. REPLACED SUPPORT FLANGE PER SRM 51-42-00, 51-72-11, DEFECT SIZE: .025" BY 1". 2L72 4F RTA46NM 20051220003272005122000327EU 2005 12 20 USAA051574 120051219A53214E33601 FLOOR PANEL AIRBUS330 A330323 3930335EU FR 32 Y-1959 DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 FOUND DELAMINATION FS 32 Y-1959. MODIFIED PART INSTALLED PER TYP REP 53-02-01, DEFECT SIZE: 3" BY 10". 2L72 4F RTA46NM 20051220003312005122000331EU 2005 12 20 USAA051570 120051219A5350F5331537320201 FAIRING AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 FOUND SEVERAL SPOTS OF CORROSION, FS 39.1-40.2 AT Y-430. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-42-00 AND 51-72-11, DEFECT SIZE: .25" BY 1". 2L72 4F RTA46NM 20051220003332005122000333 2005 12 20 UPS05145874 420051215A2565 ARM AIRBUS300 A300B4622R 3930312EU SLIDE INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01145UP 0828 COULD NOT GET SLIDE TO ARM CYCLED SLIDE ARM, OPS CK GOOD ON ECAM. 2L72 4F RTA35EU 20051220003352005122000335WP 2005 12 20 UPS05845876 120051207A3350 LIGHT DOUG DC8 DC871F 302199DWP CABIN INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 FOUND COCKPIT EMERGENCY EXIT LIGHT OVER ENGINEER SEAT INOP. PERFORMED OPS CK OF EMERGENCY LIGHT SYS PER M/M 33-50-02-2, SYS OPS NML. 2L74 4F RT4A25 20051220003362005122000336EU 2005 12 20 USAA051584 120051219A5321F5367272600200 FLOOR PANEL AIRBUS330 A330323 3930335EU FR 22 DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 FOUND DELAMINATION FS 22. COMPOSITE DOUBLER INSTALLED PER SRM 53-02-00, DEFECT SIZE: 1" BY 3". 2L72 4F RTA46NM 20051220003382005122000338EA 2005 12 20 A6WA200540322 120051108A5320601R3111358 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31426AW 7669 IB CLIP AT FS280, RBL 9.0, IS CRACKED IN RADIUS AT TOP OF CLIP, APPROX .5 INCH LONG. REMOVED AND REPLACED FS 280, RBL 9.0 FLOORBEAM TO BULKHEAD IB ATTACHMENT ANGLE IAW SRM. (K) 2L72 4F4 FRTA21EA E15NE 20051220003412005122000341EA 2005 12 20 A6WA200540342 120051108A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31426AW 7669 WO 87925, MWC 214, FS484, LBL 36 IB ANGLE OF INTERCOSTAL IS CRACKED .5 INCH LONG. REPAIRED CRACKED ANGLE AT FS 484, LBL 36 BY REMOVING AND REPAIRING ANGLE WITH FABRICATED ANGLE IAW REO. (K) 2L72 4F4 FRTA21EA E15NE 20051220003442005122000344EA 2005 12 20 A6WA200540336 120051108A5320 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31426AW 7669 OB CUP AT FS280, RBL 9.0 IS CRACKED IN RADIUS AT TOP OF CUP, APPROX .50 INCH LONG. REMOVED AND REPLACED FS280, RBL 9.0 FLOORBEAM TO BULKHEAD ATTACHMENT ANGLE IAW SRM (OB CLIP). (K) 2L72 4F4 FRTA21EA E15NE 20051220003462005122000346EA 2005 12 20 A6WA200540337 120051108A5320 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31426AW 7669 OB CLIP AT FS 280, RBL 9.0 IS CRACKED IN RADIUS AT TOP OF CUP, APPROX .50 INCH LONG. REMOVED AND REPLACED FS 280, RBL 9.0 FLOORBEAM TO BULKHEAD ATTACHMENT ANGLE IAW BRAS SRM (OB CLIP). (K) 2L72 4F4 FRTA21EA E15NE 20051220003512005122000351EA 2005 12 20 A6WA200540329 120051118A2740 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE HORIZ STAB MALFUNCTIONED A A6WAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 GL31420AW 7640 STAB TRIM AND MACH TRIM MESSAGE APPEARED DURING CLIMB. COMPLIED WITH QRH, MESSAGE PERSISTED. REMOVED AND REPLACED HSTCU PN 7060-9, IAW AMM. OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20051220003542005122000354EA 2005 12 20 A6WA200540326 120051113A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31426AW 7669 RT FS 621.00 FLOOR SUPPORT ANGLE IS CRACKED. MAINTENANCE PERFORMED REPAIR TO RT FS 621.00 FLOOR SUPPORT ANGLE IAW REO. (K) 2L72 4F4 FRTA21EA E15NE 20051220003552005122000355NM 2005 12 20 CALA0500448 120051219A5210143N61002005 INTERCOSTAL BOEING757 757224 1384958NM L2 DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713138 30351 INSPECTION FOUND A 1.5 INCH CRACK IN L-2 DOOR INSIDE INTERCOSTAL WEB AT LIGHTENING HOLE JUST FORWARD OF DOOR BOX. THE CRACK WAS TRIMMED OUT AND A DOUBLER WAS INSTALLED IAW ECRA 5210-01874. 2L72 4F RTA2NM 20051220003562005122000356NM 2005 12 20 CALA0500449 120051219A5320141A5504 FLOOR SUPPORT BOEING737 737724 13844BYNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716709 28779 INSPECTION FOUND FORWARD FLOOR STRUCTURE T-CAP (FLOOR SUPPORT) CORRODED AT STA 328, RBL 64. REPAIRED IAW ECRA 5321-01326. 2L72 4F RTA16WE 20051220003582005122000358NM 2005 12 20 SWAA053999 120051217A534065C27314 CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29622SW 27932 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 827, STR 4L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051220003602005122000360NM 2005 12 20 AALA20050829 120051206A3350 BATTERY PACK BOEING737 737823 13844BZNM CABIN FAILED A AALAK NONE O OTHER ININSP/MAINT 1 SW21928AN 29528 TUL - CABIN EMERGENCY LIGHT BATTERY PACKS FAILED DRAIN TEST. REPLACED BATTERY PACKS FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20051220003622005122000362NM 2005 12 20 2005UALA01444 120051213A5230 SKIN BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE CARGO DOOR DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29782UA 26948 DENT WAS FOUND AT SKIN OF BULK CARGO DOOR STA 1916. DAMAGE EXCEEDED LIMIT SO MAJOR REPAIR WAS ACCOMPLISHED. DENT WAS FOUND IN SKIN OF BULK CARGO DOOR STA 1916, WIDTH=1.18" DEPTH=.063". ACP PERM REPAIR PER SRM 52-30-01. REPAIR 12, PARA 4(D). DAMAGED DUE TO IMPACT BY GROUND SUPPORT EQUIPMENT. 2L72 4F4 FRTT0001SE E46NE 20051220003632005122000363NM 2005 12 20 2005UALA01445 120051213A5347 SEAT TRACK BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29174UA 24381 M-D FLOOR STA 1283-1335 SEAT TRACK BEAM TO W-W SKIN ATTACH AREA HAS CORROSION (PRESSURE DECK AND LWR CORD). CORROSION REPAIRED PER OSV ENGINEERING. 2L74 4F4 FRTA20WE E24NE 20051220003652005122000365EU 2005 12 20 2005UALA01447 120051213A5312 BULKHEAD AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE GROUND DAMAGE A UALAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP29491UA 1741 BULKHEAD DAMAGE AT STATION 350 APPROXIMATELY 14 INCHES RIGHT OF FR 1. DAMAGE CAUSED BY IMPACT WITH GROUND EQUIPMENT. HORIZONTAL STIFFENER REPLACE, BULKHEAD WEB DOUBLER INSTALLED, FRAME REPAIR, AND VERTICAL STIFFENER DOUBLER INSTALLED. 2L72 4F4 FRTA28NM E40NE 20051220003672005122000367NM 2005 12 20 2005UALA01449 120051213A5414 BUSHING BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE NR 1 PYLON ROTATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29644UA 25094 NR 1 PYLON DIAGONAL BRACE FITTING AT STRUT ATTACH, FWD INBOARD AND OUTBOARD BUSHINGS HAS EVIDENCE OF ROTATION IN THE BORE. NR 1 PYLON DIAGONAL BRACE FITTING AT STRUT ATTACH, FWD INBD AND OUTBD BUSHINGS HAVE EVIDENCE OF ROTATION IN THE BORE. MIGRATION CAUSE IS UNKNOWN. THEY WERE REPLACED PER SRM 54-53-90. 2L72 4F4 FRTA1NM E24NE 20051220003682005122000368NM 2005 12 20 2005UALA01450 120051213A5414 BUSHING BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE NR 1 PYLON WORN A UALAK NONE O OTHER ININSP/MAINT 1 WP29644UA 25094 NR 1 PYLON UPPER LINK FITTING, INBOARD LUG, OUTBOARD BUSHING LIP FRETTED. NR 1 PYLON UPPER LINK FITTING, INBD LUG, OUTBD BUSHING LIP FRETTED. IT WAS PROBABLY CAUSED BY TOLERANCE BUILD UP. BUSHING WAS REPLACED PER SRM 54-51-93. 2L72 4F4 FRTA1NM E24NE 20051220003702005122000370EU 2005 12 20 2005UALA01452 120051214A3350 LIGHT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE COCKPIT ILLUMINATED A UALAK NONE J WARNING INDICATION ININSP/MAINT 1 WP29454UA 1104 EPSU EMER R DISPLAYED AFTER EMERGENCY LIGHT TEST. REPLACED POWER SUPPLY AND BATTERY AT RH OVER WING EXIT. 2L72 4F4 FRTA28NM E40NE 20051220003712005122000371 2005 12 20 2005UALA01453 420051213A2565 SLIDE AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE DOOR 1R READS LOW A UALAK NONE O OTHER ININSP/MAINT 1 WP29807UA 798 DURING 3 SVC FOUND DOOR 1R SLIDE PACK OUT OF GREEN BAND. DOOR-1R SLIDE BOTTLE WAS FOUND TO HAVE LOW PRESS IN DCA ON 12/12/2005. ACFT WAS FERRIED TO ORD FOR CORRECTIVE ACTION AND SLIDE WAS REPLACED PER AMM-25062-44 WITH A SERVICEABLE ONE ON 12/13/2005. 2L72 4F4 FRTA28NM E40NE 20051220003722005122000372NM 2005 12 20 2005UALA01454 120051213A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29174UA 24381 BULBS FOR EMERGENCY LIGHTS INOPERATIVE AT AISLE EMERGENCY EXIT SIGN ROW 22AB AND 62BD. REPLACED EEL LIGHT. 2L74 4F4 FRTA20WE E24NE 20051220003752005122000375NM 2005 12 20 2005UALA01457 120051213A3397 CONNECTOR BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT LOOSE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29193UA 26890 EMERGENCY AISLE LIGHT UPPER DECK ACROSS ROW 18 INOP. RESECURED EMERGENCY LIGHT CONNECTOR. 2L74 4F4 FRTA20WE E24NE 20051220003782005122000378NM 2005 12 20 2005UALA01460 120051213A2110 WARNING SYSTEM BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU COCKPIT ACTIVATED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29315UA 23947 AT FL330, CABIN ALT WARNING HORN SOUNDED. PRESSURIZATION WAS IN AUTO AND OUTFLOW VALVE INDICATED FULL CLOSED. SWITCHED BOTH PACKS TO HIGH AND STARTED DESCENT. AT FL280, CABIN RATE SLOWED. DURING TROUBLESHOOTING OF CBN PRESSUR IZATION PROBLEM, FOUND RT PACK NOT OPERATING WHEN SWITCHED TO ON . SFOLM BRENDEL. REPLACED ACM AND RPL RT PACK VALVE PER MM 21-51-11..OPS CK GOOD.. 2L72 4F4 FRTA16WE E21EU 20051220003792005122000379NM 2005 12 20 2005UALA01461 120051213A5270 TARGET BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU CARGO DOOR LOOSE A UALAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 WP29375UA 24640 SHORTLY AFTER TAKEOFF AFT CARGO DOOR WARNING LIGHT ILLUMINATED. RETURNED TO DEN WITH AFT CARGO DOOR LIGHT PROBLEM. DOORS CHECKED, FLIGHT DEPARTED WITH 92 PASSENGERS 1:05 LATE. FOUND AFT CARGO DOOR WARNING SWITCH TARGET LOOSE AND OUT OF POSITION. SECURED TARGET AND CHECKED DOOR WARNING OPERATION, REF MM 52-71-32. DOOR WARNING OPS CHECKS NORMAL. 2L72 4F4 FRTA16WE E21EU 20051220003802005122000380NM 2005 12 20 2005UALA01462 120051209A2120 SMOKE BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN DETECTED A UALAO OTHER B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 WP29514UA 24839 DURING TEST FLIGHT CREW EXPERIENCED SMOKE OUT IN CABIN. REPLACED LOWER RECIRC FAN, OPS CHECK OK. 2L72 4F4 FRTA2NM E17NE 20051220003812005122000381NM 2005 12 20 2005UALA01463 120051212A2560 PBE BOEING777 777222 1385219NM PWA PW4077PW4077 NE CABIN UNKNOWN A UALAO OTHER O OTHER UKUNKNOWN 1 WP29771UA 26932 PBE'S PACKAGE DEFECTS AT 1L, 2R, 2L, 3L, 4L, AND 4R. THESE PBES WERE PULLED PREMATURELY AND DID NOT HAVE THE VACUUM SEALS BROKEN. MAINTENANCE CONTROL REVIEWED REMOVAL CRITERIA WITH AMTS INVOLVED AND EMPHASIZED THE USE OF THE SEAL INTEGRITY INDICATOR BUTTON. 2L72 4F4 FRTT0001SE E46NE 20051220003822005122000382NM 2005 12 20 2005UALA01464 120051212A2497 WIRE BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE IDG BURNED A UALAK NONE O OTHER ININSP/MAINT 1 WP2987UA 26939 NR 2 ENG IDG WIRING BURNED. NR 2 ENG IDG FEEDER CABLE TERMINAL LUGS FOUND CORRODED AT ENG DISCONNECT. REPLACED LUGS. ALSO FOUND GENERATOR FEEDER CABLE BURNED & CHAFED AT TERMINAL STRIP. SPLICED IN 3 FT SECTION OF NR 2 CU WIRE. REPLACED FEEDER CABLE SEALS AND SUPPORTS. RE-POTTED WHERE CABLE FEEDS THRU TOP OF J-BOX. CABLE TERMINALS EXPERIENCE THERMAL DISTRESS WHEN CORRODED CONNECTIONS INCREASE CURRENT FLOW. HIGHER TEMPERATURES CAUSE SEALS, POTTING & INSULATION TO OXIDIZE & DETERIORATE. 2L72 4F4 FRTT0001SE E46NE 20051220003832005122000383NM 2005 12 20 2005UALA01465 120051215A5330 SKIN BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29174UA 24381 AFT CARGO DOOR CUTOUT UPPER FWD CORNER HOLE HAS CRACK (IN BODY SKIN). CRACK FOUND BY COA TO ADDRESS CRACKS IN THIS AREA, AS MANDATED BY AD. REPAIRED PER BOEING SERVICE BULLETIN 747-53A2448. 2L74 4F4 FRTA20WE E24NE 20051220003902005122000390EU 2005 12 20 2005UALA01472 120051217A5330 SKIN AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29427UA 512 LEFT AIRPHONE ANTENNA SKIN MATING SURFACE HAS MINOR SURFACE CORROSION. INSTALLED DOUBLER REPAIR PER SRM 53-00-11 FIG 203. 2L72 4F4 FRTA28NM E40NE 20051220003932005122000393NM 2005 12 20 SWAA053985 120051218A3350207377 LENS BOEING737 7377H4 1384404NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29216WR 32488 DURING SCHEDULED 1/2D CHECK, FOUND CABIN EEPLS LENS LOOSE. SECURED LENS PER MM. 2L72 4F RTA16WE 20051220003942005122000394NM 2005 12 20 SWAA053986 120051217A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 368, STR 25L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051220003992005122000399NM 2005 12 20 SWAA053991 120051216A53126516300 BULKHEAD BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29501SW 24178 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE BULKHEAD WEB CRACKED AT BS 178, RBL 5.7, WL 187. REPAIRED BULKHEAD WEB PER SRM. 2L72 4F RTA16WE 20051220000482005122000048NM 2005 12 20 SWAA053937 120051212A5330MS155721 BULB BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED C2 CHECK, FOUND R1 DOOR AFT EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20051220000562005122000056CE 2005 12 20 ON39TW120605JC 120051206A32306600361 CONTROL VALVE LEAR 35 31A 5170531CE GARRTTTFE731TFE731* 01518WP MLG DOOR LEAKING E AOQAO OTHER O OTHER NRNOT REPORTED 1 EA1139TW 4420 047 NOSE GEAR RED UNSAFE LIGHT DID NOT EXTINGUISH ON TAKEOFF, FOLLOWED BY BOTH MAIN GEAR UNSAFE LIGHTS (RED) ILLUMINATING. GEAR WAS EXTENDED AND ALL T3 GEAR INDICATED LOCKED WITH NO UNSAFE CONDITION. AIRCRAFT LANDED UNEVENTFULLY. INSPECTED LANDING GEAR SYS AND TROOUBLESHOT PROBLEM TO THE LANDING GEAR DOOR CONTROL VALVE. FOUND VALVE TO BE LEAKING INTERNALLY INTO THE EMERGENCY AIR SYS SIDE. PURGED FLUID FROM EMERGENCY CIRCUIT. REPLACED LANDING GEAR DOOR CONTROL VALVE. CYCLED GEAR 15 TIMES WITH SATISFACTORY RESULTS. SERVICED HYDRAULIC SYSTEM. (K) 2L72 4F4 FRTA10CE E6WE 20051220000722005122000072NE 2005 12 20 KBM2005F00349 220051129A7321704A34130052 FCU SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE ENGINE FROZEN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV6655 3296 FCU CABLE, UNIT FROZEN, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051220000902005122000090WP 2005 12 20 ASAA0580468 120050817A532059128526 SUPPORT DOUG DC9 DC983 3022083WP FS 38-41 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02977AS 53453 OKC - DURING C-CHECK, FOUND NOSE LANDING GEAR WHEELWELL RIGHT SUPPORT FRAME UPPER FASTENER CRACKED. STOP DRILLED CRACK. INSTALLED REPAIR ANGLE, SHIM, AND CLIP. (M) 2L72 4F RTA6WE 20051220000912005122000091WP 2005 12 20 ASAA0580467 120050817A523059101413 SKIN DOUG DC9 DC983 3022083WP FS 1171-1196 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02977AS 53453 OKC - DURING C-CHECK, FOUND AFT CARGO BAY DOOR SKIN IS DENTED. REMOVED DAMAGED AREA. INSTALLED ONE EXTERNAL DOUBLER, TWO INTERNAL DOUBLERS, AND THREE FILLERS. (M) 2L72 4F RTA6WE 20051220000932005122000093WP 2005 12 20 ASAA0580431 120050807A5313593643437 LONGERON DOUG DC9 DC982 3022082WP FS 322-325 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02935AS 49236 OKC - DURING C-CHECK, FOUND LONGERON CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR CHANNEL. (M) 2L72 4F A6WE 20051220000962005122000096SO 2005 12 20 SIMA200529001 120051012A216014522277403 SWITCH EMB 145 EMB145LR 3260212SO A/C TEMP BROKEN A SIMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21646AE 145213 LRD - FLT 3595 - SMOKE IN CABIN DIVERTED TO LRD. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED AIRCRAFT AIR CONDITIONING SYSTEM. REPLACED OVER TEMPERATURE SWITCH ON NR 2 PACK. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20051220000972005122000097WP 2005 12 20 ASAA0580456 120050808A5330590600731 SKIN DOUG DC9 DC982 3022082WP FS 1295 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02935AS 49236 OKC - FOUND DURING C-CHECK, FUSELAGE SKIN IS DENTED. COLD-WORKED DAMAGED AREA. INSTALLED REPAIR DOUBLER. (M) 2L72 4F A6WE 20051220001062005122000106WP 2005 12 20 ASAA0580415 120050805A5321993281613 STIFFENER DOUG DC9 DC983 3022083WP FS 693-827 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02947AS 53020 OKC - FOUND C-CHECK, CABIN FLOOR PANEL STIFFENER, HAT CHANNEL, DENTED. REPLACED HAT CHANNEL. (M) 2L72 4F RTA6WE 20051220001242005122000124EU 2005 12 20 USAA051542 120051213A5320D5347218820400 FLOOR SUPPORT AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19113UW 1141 CORROSION Y1162 BETWEEN C68-69. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-42-11; CORR LEVEL 1; TASK JA-260-53500, DEFECT SIZE: 1 INCH DIA. 2L72 4F RTA28NM 20051220001262005122000126EU 2005 12 20 USAA051540 120051213A5315D53311281520200 FLOORBEAM AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19113UW 1141 Y129L AT C-18 CORRODED. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-42-11; DEFECT SIZE: .5 X .5 X .070 INCH DEEP. 2L72 4F RTA28NM 20051220001352005122000135EU 2005 12 20 USAA051549 120051213A5311D5311282600101 FRAME AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19113UW 1141 FRAME C-14-C16 Y505 CORRODED. REPLACED BEAM PER SRM 51-72-11; CORR LEVEL 1; TASK JA-220-53500, DEFECT SIZE: 1 X .5 INCH, 1.5 X 1 INCH. 2L72 4F RTA28NM 20051220001432005122000143NM 2005 12 20 SWAA053940 120051213A53306518420 SKIN BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CORRODED/CRACKED BETWEEN BS 259 TO BS 360, STR 19R TO STR 24R. REPAIRED SKIN PER BFG ER. 2L72 4F RTA16WE 20051220001752005122000175NM 2005 12 20 AMTA200501067 120051115A7700 UNKNOWN BOEING757 75723N 1384973NM LT ENGINE UNKNOWN A AMTAO OTHER J WARNING INDICATION CLCLIMB 1 GL11517AT 27973 AT FL390, LT ENGINE COMMAND THRUST LEVEL SHOWED .07 EPR ABOVE ACTUAL EOR AT ALL TIMES ABOVE 35,000 FT. LT THRUST LEVER REQUIRED 1/2 KNOW FORWARD TO ALIGN EPR ALL OTHER ENGINE PARAMETERS MATCHED WITH EPR MATCHED TROUBLESHOT PER FIM 22-32-82-00 MCDP GROUND TEST 02 AND 10 TEST WERE NORMAL. NO FAULTS, WITH EEC`S ON. OPERATIONAL CHECK NORMAL. OK FOR SERVICE. (M) 2L72 4F RTA2NM 20051220001772005122000177EA 2005 12 20 ASOA05996 120051117A5210601R319805 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27827AS 7212 DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR BOTTOM STEP BRACE WAS FOUND TO BE BROKEN. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20051220001902005122000190NM 2005 12 20 ASAA0540383 120050810A5753 FAIRING BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FLAP TRACK CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02778AS 25110 YXX: DURING C-CHECK FOUND LT OB MID FLAP TRACK FAIRING LOWER SURFACE CHAFED. REPAIRED IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051220001922005122000192NM 2005 12 20 ASAA0540385 120050810A5712644544556 RIB BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU RT WING CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02778AS 25110 YXX: DURING C-CHECK FOUND RT WING FUEL TANK RIB LOWER CHORD CRACKED AT WING STA 135.5. REPAIRED IAW EA. (K) 2L72 4F4 FRTA16WE E21EU 20051220002002005122000200WP 2005 12 20 ASAA0580483 120050904A532299364543 SHEAR TIE DOUG DC9 DC982 3022082WP FS 1060 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02931AS 49232 OKC - FOUND DURING C-CHECK, SHEAR TIE CORRODED. REPLACED DAMAGED SECTION OF SHEAR TIE. (M) 2L72 4F A6WE 20051220002222005122000222EA 2005 12 20 ASOA051004 120051119A5210601R3170767 STEP CNDAIRCL600 CL6002C10 1390015EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27738EV 10146 DURING AN A-CHECK IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND CRACKED AT THE ATTACH POINT. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20051220002302005122000230SO 2005 12 20 SIMA200530801 120051101A27503631001011 FCU EMB 145 EMB145LR 3260212SO TE FLAPS FAULTY A SIMAB EMER. DESCENT F FLT CONT AFFECTED APAPPROACH 1 SW21631AE 145139 DURING DESCENT, FLAPS STUCK AT 9 DEGREES EXTENSION. REPLACED FLAP ELECTRONIC CONTROL UNIT. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20051220002472005122000247WP 2005 12 20 ASAA0580422 120050805A5320993061225 CUSP WEB DOUG DC9 DC983 3022083WP FS 1060-1079 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02947AS 53020 OKC - DURING C-CHECK, FOUND RIGHT CUSP WEB CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20051220002492005122000249NM 2005 12 20 ASAA0580499 120050926A532199365443 FLOOR PANEL DOUG MD80 MD83 3023681NM FS 160-200 DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - DURING HV CHECK, FOUND PAX CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RT 20051220002582005122000258WP 2005 12 20 ASAA0580430 120050807A532059360264 INTERCOSTAL DOUG DC9 DC982 3022082WP FS 1164 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02935AS 49236 OKC - DURING C-CHECK, FOUND INTERCOSTAL CORRODED. REPLACED INTERCOSTAL. (M) 2L72 4F A6WE 20051220002592005122000259SO 2005 12 20 SIMA200529010 120051007A532014525381003 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO FS 20 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21658AE 145760 THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED THE CORROSION BY MAKING CUTOUT. FABRICATED A PLATE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 30, CHAPTER 53-00-10 FIG 201 SHEET 1, 51-40-02, 51-20-03, 51-40-06 AND ETN EM-53-087. (M) 2L72 4T RTT00011AT 20051220002642005122000264NM 2005 12 20 ASAA0580506 120050926A5320 CHANNEL DOUG MD80 MD83 3023681NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - FOUND HV-CHECK, PASSENGER CABIN FLOOR PANEL HAS CRACKED HAT CHANNEL. REPLACED DAMAGED CHANNEL. (M) 2L72 4F RT 20051220002662005122000266WP 2005 12 20 ASAA0580410 120050723A5321993654759 FLOOR PANEL DOUG DC9 DC983 3022083WP FS 160-180 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02944AS 53019 OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL HAS CORRODED INSERTS. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20051220002682005122000268WP 2005 12 20 ASAA0580427 120050805A533059360154 SKIN DOUG DC9 DC983 3022083WP FS 1100 DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02947AS 53020 OKC - FOUND DURING C-CHECK, ELONGATED FASTENER HOLE IN FUSELAGE. REMOVED DAMAGED AREA. INSTALLED INTERNAL REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20051220002702005122000270NM 2005 12 20 ASAA0540372 120050803A5534655484226 SKATE ANGLE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU VERTICAL FIN CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 RT FWD SKATE ANGLE FOR VERTICAL FIN CHAFED 3 INCHES FROM FWD END ON IB SIDE. REMOVED AND REPLACED FWD SKATE ANGLE FOR VERTICAL FIN. (K) 2L72 4F4 FRTA16WE E21EU 20051220002792005122000279NM 2005 12 20 ASAA0580511 120050926A5311 FRAME DOUG MD80 MD83 3023681NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - DURING HV-CHECK, FOUND FRAME CORRODED. REMOVED DAMAGED SECTION. INSTALLED TWO REPAIR DOUBLERS, TWO REPAIR PLATES, AND ONE REPAIR FILLER. (M) 2L72 4F RT 20051220002802005122000280NM 2005 12 20 ASAA0540380 120050804A531165465488 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 CRACKED FRAME. REPAIRED CRACK IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051220002822005122000282NM 2005 12 20 CALA0500440 120051216A5330146N35319 SKIN BOEING757 757224 1384958NM STA 1500-1520 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713138 30351 INSPECTION FOUND CORROSION ON OUTER SKIN OF RT GTE AIRPHONE ANTENNA CUTOUT, STA 1500-1520, S28R TO S29R. THE CORRODED AREA WAS CUT OUT AND AN INTERIM REPAIR WAS INSTALLED IAW ECRA 5330-03507. A DIP WAS ISSUED TO ACCOMPLISH A PERMANENT REPAIR WITHIN 12 MONTHS. 2L72 4F RTA2NM 20051220002882005122000288NM 2005 12 20 ASAA0540392 120050816A5322654655159 SHEAR TIE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02779AS 25111 SHEAR TIE AT BSTA 807, BL0, CORRODED. REMOVED CORRODED REPAIR PART, FABRICATED AND NSTALLED REPAIR PIECES IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051220002912005122000291NM 2005 12 20 USAA051559 120051215A5315 FLOORBEAM BOEING737 7374B7 1384702NM BS 887 GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 FOUND GOUGE FWD SIDE OF FLOORBEAM STA 887 BELOW CREASE BEAM A/C RT. FABRICATED AND INSTALLED DOUBLER ISW SRM 51-70-12, DEFECT SIZE: GOUGES IN FWD SIDE OF FLOORBEAM STA 887, BELOW CREASE BEAM, A/C RT. 2L72 4F RTA16WE 20051220003012005122000301EU 2005 12 20 USAA051565 120051219A5347F57110568205 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 FOUND CORROSION SEAT TRACK -Y450 FS 44. BLEND AREA, REPLACED SEAT TRACK PER SRM 57-74-00, 53-31-15, 51-72-11; CORROSION LEVEL 2; TASK C533-170-0, DEFECT SIZE: 3" BY 1" AREA. 2L72 4F RTA46NM 20051220003022005122000302EU 2005 12 20 USAA051575 120051219A53214E33635 FLOOR PANEL AIRBUS330 A330323 3930335EU FR 34 Y1456 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 FOUND CORROSION FS 34 Y1456. MODIFIED PART INSTALLED PER TR 53-002-01, DEFECT SIZE: 5" BY 16". 2L72 4F RTA46NM 20051220003082005122000308NM 2005 12 20 ASAA0540411 120050816A531565465685 FLOORBEAM BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 CORROSION ON FLOORBEAM BSTA 1076, RBL 25-30, WL 208. BLENDED CORROSION, DETERMINED TO BE OUT OF LIMITS, REPAIRED FLOORBEAM IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051220003162005122000316NM 2005 12 20 ASAA0540417 120050818A53226546548110 SHEAR TIE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02779AS 25111 SHEAR TIE AT FRAME 747C, RBL 12 IS CORRODED. REMOVED DAMAGED SECTION OF SHEAR TIE, FABRICATED AND INSTALLED REPAIR PIECES IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051220003192005122000319NM 2005 12 20 ASAA0540423 120050822A572069353013 WEB BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUEL CELL MISDRILLED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 CENTER FUEL CELL, AFT CELL, DRILL START DAMAGE ON UPPER CHORD AND SPANWISE BEAM WEB. REPAIRED DRILL START ON UPPER CHORD AND SPANWISE BEAM. (K) 2L72 4F4 FRTA16WE E21EU 20051220003242005122000324EU 2005 12 20 USAA051566 120051219A5320F53478234200 FLOOR SUPPORT AIRBUS330 A330323 3930335EU Y380.15 FR 78 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 FOUND CORROSION Y380.15 FS 78. BLENDED, INSTALLED NEW SUPPORT FLOOR PER SRM 51-72-11, 51-74-00, 53-00-15; CORROSION LEVEL 2; TASK C534415, DEFECT SIZE: .500 BY .500 BY .065". 2L72 4F RTA46NM 20051220003282005122000328EU 2005 12 20 USAA051573 120051219A53214E33616 FLOOR PANEL AIRBUS330 A330323 3930335EU FR 32 Y1959 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 FOUND CORROSION FS 32 Y1959. MODIFIED PART INSTALLED PER TR 53-02-01, DEFECT SIZE: 3" BY 12". 2L72 4F RTA46NM 20051220003292005122000329EU 2005 12 20 USAA051572 120051219A5321F5367284003400 FLOOR PANEL AIRBUS330 A330323 3930335EU FR 33 DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 FOUND DELAMINATION FS 33. COMPOSITE DOUBLER INSTALLED PER SRM 53-02-00, DEFECT SIZE: 2" BY 4". 2L72 4F RTA46NM 20051220003432005122000343EA 2005 12 20 A6WA200540340 120051121A5712 RIB CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT WING CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31427ZW 7685 AWAC WO 89248, MWC 143. LT BATT RIB ASSY AT WS 53.60 UPPER AFT RADIUS IS CRACKED 2 INCH LONG. INSTALLED REPAIR DOUBLER AND FILLER IAW REO. (K) 2L72 4F4 FRTA21EA E15NE 20051220003472005122000347EA 2005 12 20 A6WA200540338 120051108A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31426AW 7669 OB CLIP AT FS 280, LBL 9.0 IS CRACKED IN RADIUS AT TOP CLIP, CRACK APPROX .50 INCH LONG. REMOVED AND REPLACED FS 280, LBL 9.0 FLOORBEAM TO BULKHEAD ANGLE IAW SRM (OB CLIP). (K) 2L72 4F4 FRTA21EA E15NE 20051220003492005122000349EA 2005 12 20 A6WA200540331 120051121A53206013501252 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31427ZW 7685 RT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STR 14R IS CRACKED NEAR RADIUS APPROX 1.0 INCH LONG. MAINTENANCE REPLACED INTERCOSTAL IAW SRM. (K) 2L72 4F4 FRTA21EA E15NE 20051220003502005122000350EA 2005 12 20 A6WA200540334 120051122A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT WING CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31427ZW 7685 LT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT FOR PANEL 540CB HAS MINOR CORROSION ON OB 5 INCH LONG X .1250 INCH WIDE AND .002 INCH DEEP AND IB 4 INCH LONG X .1250 INCH WIDE AND .002 INCH DEEP. MAINTENANCE PERFORMED A MAJOR REPAIRED TO LT WING LOWER PLANK BY BLENDING MINOR CORROSION AT FUEL TANK ACCESS DOOR CUTOUT FOR PANEL 540CB WS 76. 161. (K) 2L72 4F4 FRTA21EA E15NE 20051220003592005122000359WP 2005 12 20 AALA20050833 120051122A3230 BUSHING DOUG DC9 DC983 3022083WP LT MLG CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21968TW 53618 TUL - LEFT HAND MAIN LANDING GEAR SUPPORT BEAM RETRACT BUSHING AREA INBOARD BUSHING OUTBOARD FACE HAS MINOR CORROSION. AREA IS 2.13 INCHES BY 2.13 INCHES. ORIGINAL THICKNESS .033 AND FINAL MEASUREMENT IS 1.202 REMAINING THICKNESS. LEFT HAND MAIN LANDING GEAR RETRACT BUSHING AREA REWORKED IN ACCORDANCE WITH ESO 80559 DATED NOVEMBER 22 2005. 2L72 4F RTA6WE 20051220003662005122000366NM 2005 12 20 2005UALA01448 120051213A5411 BUSHING BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE NR 2 PYLON LOOSE A UALAK NONE O OTHER ININSP/MAINT 1 WP29644UA 25094 NR 2 PYLON OUTBOARD MIDSPAR FITTING, INBOARD LUG BUSHING MOVES IN BORE. NR 2 PYLON OUTBD MIDSPAR FITTING, INBD LUG BUSHING MOVED IN THE BORE. BUSHING MIGRATION CAUSE IS UNKNOWN. IT WAS REPLACED WITH AN OVERSIZED BUSHING PER SRM 54-53-90 2L72 4F4 FRTA1NM E24NE 20051220003692005122000369NM 2005 12 20 2005UALA01451 120051213A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE GOUGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29589UA 28707 LEFTHAND FUSELAGE, AFT OF DOOR 2L, DENT AND GOUGED SKIN ON FRAME AT STA 760 AND S16. ACCOMPLISHED INTERIM RPR PER SRM53-00-01 RPR#2 PG.201-206. LFEC TO BE ACCOMPLISHED EVERY 3 000 CYCLES. 2L72 4F4 FRTA2NM E17NE 20051220003732005122000373NM 2005 12 20 2005UALA01455 120051213A3397 WIRE BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT LOOSE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29193UA 26890 EMERGENCY LIGHT ALONG STAIRS TO UPPER DECK INOP. SECURED LOOSE CONNECTION. 2L74 4F4 FRTA20WE E24NE 20051220003762005122000376NM 2005 12 20 2005UALA01458 120051213A3397 CONNECTOR BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT LOOSE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29193UA 26890 MID LAV LT FWD WALL EMERGENCY LIGHT INOP. RESECURED EEL CONNECTOR. 2L74 4F4 FRTA20WE E24NE 20051220003842005122000384NM 2005 12 20 2005UALA01466 120051214A335078941 LIGHT BOEING777 777222 1385219NM PWA PW4077PW4077 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29781UA 26945 SEAT 2E BOTH EMERGENCY LIGHTS INOP. RELAMPED BOTH EMERGENCY LIGHTS. OP CHECKS GOOD. 2L72 4F4 FRTT0001SE E46NE 20051220003852005122000385NM 2005 12 20 2005UALA01467 120051215A3397 CONNECTOR BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT LOOSE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29118UA 28811 SEAT 33 ABC EEL LIGHT INOP. SECURED LOOSE CONNECTOR. 2L74 4F4 FRTA20WE E24NE 20051220003862005122000386NM 2005 12 20 2005UALA01468 120051215A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29118UA 28811 UPPER DECK EMERGENCY EXIT CEILING LIGHTS AT ROWS 12, 16, AND 17 INOP. RELAMPED CEILING LAMPS. 2L74 4F4 FRTA20WE E24NE 20051220003892005122000389EU 2005 12 20 2005UALA01471 120051215A5330 SKIN AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE SCRATCHED A UALAK NONE O OTHER ININSP/MAINT 1 WP29410UA 463 LARGE DEEP SCRATCHES APPROXIMATLEY 24-28 INCHES LONG APPROXIMATELY 8 INCHES BEHIND FWD FUSELAGE BULKHEAD JUST AFT OF NOSE RADOME, FROM BELOW WATER LINE TO JUST BELOW RVSM AREA LT SIDE OF FUSELAGE. MAJOR REPAIR REPORTING. BLENDED SCRATCHED AREA PER SRM 53-11-11-101 AND SRM 53-00-11-101 FOR RVSM COMPLIANCE. 2L72 4F4 FRTA28NM E40NE 20051220003972005122000397NM 2005 12 20 SWAA053989 120051216A3350D71702001 BATTERY PACK BOEING737 7373H4 1384600NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29331SW 23695 DURING SCHEDULED SERVICE CHECK, R2 DOOR UPPER EMERGENCY EXIT LIGHT FAILED TEST. REMOVED AND REPLACED BATTERY PACK & CHARGER PER MM. 2L72 4F RTA16WE 20051220003982005122000398 2005 12 20 SWAA053990 420051216A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20051220004042005122000404NM 2005 12 20 SWAA053996 120051218A534065C27314 STRINGER CLIP BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29511SW 24188 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 520, STR 16L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051220004122005122000412EA 2005 12 20 A6WA200540318 120051107A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31426AW 7669 FS 621 TO FS 625 TOP RT INTERCOSTAL ANGLE IS CRACKED 1.5 INCH LONG IN AFT RADIUS. (K) 2L72 4F4 FRTA21EA E15NE 20051220004142005122000414EA 2005 12 20 A6WA200540317 120051107A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31426AW 7669 MWC 22, FS 621 TO FS 625 TOP LT INTERCOSTAL ANGLE CRACKED 1.5 INCH LONG IN AFT RADIUS. C/A IN PROGRESS. (K) 2L72 4F4 FRTA21EA E15NE 20051220004152005122000415EA 2005 12 20 A6WA200540347 120051205A53206013501251 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31470ZW 7927 LT SIDE FS621.00 TO 625.30 INTERCOSTAL AT STR 14L IS CRACKED NEAR RADIUS APPROX 1.1 INCH LONG. REMOVED AND REPLACED INTERCOSTAL, PN 601-35012-51, IAW REO (UNREADABLE). (K) 2L72 4F4 FRTA21EA E15NE 20051220004162005122000416EA 2005 12 20 A6WA200540346 120051113A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31426AW 7669 RT FS 621.00 FLOOR SUPPORT ANGLE IS CRACKED. PERFORMED REPAIR TO RT FS 621.00 FLOOR SUPPORT ANGLE IAW REO. (K) 2L72 4F4 FRTA21EA E15NE 20051220004192005122000419NM 2005 12 20 ASAA0540454 120050909A531565468101 FLOORBEAM BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02793AS 28888 CORROSION ON FLOORBEAM AFT FLANGE. REMOVED CORROSION ON FLOORBEAM, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051220004202005122000420NM 2005 12 20 ASAAS0540469 120050914A53306548L40504 SKIN BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02793AS 28888 RT EMPENNAGE SKIN CHAFED AT RT HORIZONTAL STABILIZER AFT SPAR LOWER CUTOUT. FOUND RT EMPENNAGE SKIN CHAFED AT RT HORIZONTAL STABILIZER AFT SPAR CUTOUT OUT OF LIMITS. REMOVED AND REPLACED SKIN SECTION AND TRACK FILLER. (K) 2L72 4F4 FRTA16WE E21EU 20051220004212005122000421NM 2005 12 20 ASAA0540456 120050909A5320654587653 SILL BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02793AS 28888 CORROSION ON FWD GALLEY MOPSILL. REPLACED MOPSILL. (K) 2L72 4F4 FRTA16WE E21EU 20051220004222005122000422NM 2005 12 20 ASAA0540468 120050914A5320651630019 ANGLE BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE BENT A ASAAK NONE O OTHER ININSP/MAINT 1 NM02793AS 28888 LT L-ANGLE BENT AT BSTA 178, WL 207, LBL 24. REMOVED AND REPLACED BENT ANGLE IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051220004232005122000423NM 2005 12 20 ASAA0540472 120050916A531165465251 FRAME BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02793AS 28888 BSTA 380, FRAME CRACKED AT BIN RAIL STATION. CUTOUT DAMAGE AT FRAME BIN RAIL SUPPORT AND FABRICATED AND INSTALLED REPAIR IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051220004262005122000426NM 2005 12 20 ASAA0540497 120050921A5311654657969 FRAME BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU APU BAY CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02793AS 28888 RT APU CHORD AT FWD HINGE CUTOUT CRACKED. REMOVED AND REPLACED CHORD IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051220004282005122000428NM 2005 12 20 ASAA0540663 120051117A5310654587567 CREASE BEAM BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 RT CREASE BEAM CORRODED. REPLACED IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051220004292005122000429NM 2005 12 20 ASAA0540664 120051117A5320654587545 SILL BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 RT DOOR R1, MOPSILL CORRODED. REPLACED MOPSILL IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051220004302005122000430NM 2005 12 20 ASAA0540470 120050914A531165465301 FRAME BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02793AS 28888 BSTA 480 FRAME IS CRACKED AT BIN RAIL SUPPORT BETWEEN STR 8 LT AND 9 LT AT IB FASTENER. CUTOUT DAMAGE AT BSTA 480 FRAME BIN RAIL SUPPORT AND FABRICATED AND INSTALLED REPAIR. (K) 2L72 4F4 FRTA16WE E21EU 20051220004312005122000431NM 2005 12 20 ASAA0540430 120050823A53206546592 FLOOR SUPPORT BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 WHILE WORKING FOUND FLOOR SUPPORT IN AFT CARGO BAY TO BE DAMAGED AT BSTA 727E+14 INCH, LBL 13. TRIMMED OUT DAMAGED AREA IN FLOOR SUPPORT IN AFT CARGO BAY AT BSTA 727E + 14 INCH LBL 13 AREA, REMOVED .5 INCH X 6 INCH SECTION, THEN FABRICATED AND INSTALLED REPAIR. ALL WORK PERFORMED IAW EA. (K) 2L72 4F4 FRTA16WE E21EU 20051220004332005122000433NM 2005 12 20 ASAA0540394 120050816A5311654652912 FRAME BOEING737 7374Q8 138447QNM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 CRACKED FRAME AT BIN RAIL STA 440. REPAIRED CRACKED FRAME AT BIN RAIL BSTA 440, STR 8L-9L IAW SRM. (K) 2L72 4F4 FRTA16WE E2GL 20051220004342005122000434NM 2005 12 20 ASAA0540433 120050831A53116520722 FRAME BOEING737 7374Q8 138447QNM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 FWD CARGO BAY, BSTA 440, RBL 22, WL 156, FRAME IS DENTED AT FASTENER. TRIMMED OUT DAMAGE AND INSTALLED REPAIR IAW EA. (K) 2L72 4F4 FRTA16WE E2GL 20051220004352005122000435NM 2005 12 20 ASAA0540395 120050816A5311654652612 FRAME BOEING737 7374Q8 138447QNM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 CRACKED FRAME AT BIN RAIL STA 400. REPAIRED CRACKED FRAME AT BIN RAIL BSTA 400, STR 8L- 9L IAW SRM. (K) 2L72 4F4 FRTA16WE E2GL 20051220004372005122000437NM 2005 12 20 USAA051557 120051214A575465C2660309 WEDGE BOEING737 737301 1384611NM WRIGHTR1820 R182060 67020EA L/E SLAT DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19591US 23936 NR 3 LE SLAT ASSY IB TRAILING EDGE WEDGE. REMOVED DAMAGE ON THE WEDGE. DOUBLER REPAIR IAW 51-30-03 AND SRM 51-70-10 DEFECT SIZE: .6 IN X 8 IN. 2L72 4F4 RRTA16WE 5E10 20051221000012005122100001EU 2005 12 21 EMB0518 120051213A2120 SMOKE EMB ERJ170ERJ170100 EU CABIN DETECTED A USAAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 EA19826MD 000046 FLIGHT 1708, DCA TO DFW - ON DESCENT INTO DFW A STRONG SMELL OF SMOKE FILLED THE AFT CABIN FROM ROW 13 BACK. MAINTENANCE INSPECTED A/C AND FOUND IN SAFE CONDITION TO MAINTENANCE FERRY TO PIT. PERFORMED OPERATIONAL CHECK OF CABIN AIR CONDITIONING OFF ENGINE BLEEDS AND CHECKS OF PACKS 1 AND 2. NO SMOKE SMELL PRESENT. A/C RETURNED TO SERVICE. 2L74 4F RTA56NM 20051221000022005122100002EU 2005 12 21 SA05127 120051214A2121EVT3454H FAN AIRBUSA319 A319112 3930323EU AVIONICS BAY OVERHEATED A USAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA19725UW16372 1135 SJU FLT 1037, EN ROUTE PHL TO SJU. DURING THE OPERATION OF THE AIRCRAFT, A BURNING ODOR WAS DETECTED IN THE FLIGHT DECK. AN ECAM WARNING OF BLOWER FAULT WAS GENERATED AROUND THE SAME TIME. THE CREW FOLLOWED PROCEDURES FOR THE WARNING AND COMPLETED THE FLIGHT WITHOUT FURTHER INCIDENT. MAINTENANCE PLACED THE AVIONICS VENT BLOWER SYSTEM ON MEL. MAINTENANCE REPLACED THE EXTRACT FAN AS THE FINAL CORRECTIVE ACTION. 2L72 4F RTA28NM 20051221000062005122100006NM 2005 12 21 SB05171 120051215A532065186215 SILL BOEING737 7373B7 1384580NM GE CFM56 CFM56* 13802NE CARGO DOORWAY DAMAGED A USAABA EMER. DESCENT UNSCHED LANDING O OTHER CRCRUISE 1 EA19517AU 23703 ENROUTE, THE FLIGHT LOST PRESSURIZATION AFTER REACHING CRUISE ALTITUDE. THE FLIGHT DESCENDED TO 10,000 FEET. THE OXYGEN MASKS DID NOT DEPLOY. THE FLIGHT DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FORWARD OUTFLOW VALVE AS A PRECAUTIONARY MEASURE AND THE AFT OUTFLOW VALVE DUE TO AIR LEAKING AROUND WORN DOOR SEALS. ALSO, MAINTENANCE FOUND THE FORWARD CARGO DOOR SEAL AND SILL DAMAGED AND LEAKING AIR. REPLACED THE FORWARD CARGO DOOR SEAL AND SILL. OPERATIONALLY CHECKED AND LEAK CHECKED OK. [CLOSED] 2L72 4F4 FRTA16WE E2GL 20051221000072005122100007NM 2005 12 21 05FDEA04204 120051209A5314 KEELBEAM BOEING727 727227 1384078NM BS 976 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 FOUND CORROSION ON KEELBEAM REPAIR STRAP BS 976 STR29 LT. REPLACED KEEL BEAM REPAIR STRAP PER SR DRAWING 27-53-023A. 2L73 4F A3WE 20051221000082005122100008NM 2005 12 21 05FDEA04206 120051209A5347 SEAT TRACK BOEING727 727227 1384078NM BS 570 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 FOUND CORROSION C53-224-01, STA 570 RBL 1 WL 208 CORROSION ON SEAT TRACK. SEAT TRACK TO BE REPLACED ON CUST ID N00436. 2L73 4F A3WE 20051221000102005122100010NM 2005 12 21 05FDEA04254 120051212A5314 KEELBEAM BOEING727 727227 1384078NM BS 950F-970 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 FOUND CORROSION ON KEELBEAM BS 950F-970 STR 29 LT. REMOVED CORROSION AND RESTORED TO NORMAL ON THE KEEL BEAM BS 950F-970 STR 29 LT IAW DWG #SR27-53-013-REV A. 2L73 4F A3WE 20051221000122005122100012NM 2005 12 21 0501756315 120051217A2120 SMOKE BOEING747 747451 1384940NM CABIN DETECTED A NWAAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NRNOT REPORTED 1 GL01675NW 33001 LAV 2R SMOKE DETECTOR WENT OFF FOR MORE THAN 5 MINUTES. FLIGHT ATTENDANT CREW DEACTIVATED SMOKE DETECTOR. SMOKE WAS ELECTRICAL IN NATURE AND DISSIPATED AFTER ALARM WAS DEACTIVATED. KIX, MAINTENANCE CHECKED LAV 2R, AND TESTED SMOKE DETECTOR FUNCTION NORMAL. OPERATIONAL CHECKED GOOD AND RETURNED TO SERVICE. 2L74 4F RTA20WE 20051221000142005122100014NM 2005 12 21 EIA2005258 120051208A2797 CONNECTOR BOEING747 747212B 1384886NM AILERON SYS DIRTY A EIAAD RETURN TO BLOCK L NO TEST TXTAXI/GRND HDL 1 NM09486EV 20888 BTB DUE TO FAILURE OF LT OTB AILERON TO WORK WITH FLAPS EXTENDED ON PREFLIGHT CHECK. REMOVED AND CLEANED CANNON PLUG ON LT OTB AILERON ELECTRIC LOCKOUT, PER SWPM CH 20-16-0. OP'S CK PER 27-11-16, PG 41, OPS CK OK. 2L74 4F A20WE 20051221000152005122100015NE 2005 12 21 EIA2005259 220051211A7200 ENGINE BOEING747 747212B 1384886NM PWA JT9 JT9D7J 52054NE NR 3 FAILED A EIAAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 NM09485EV 20712 689551 DURING CLIMB-OUT AT 5,000 FT AGL, NR 3 ENG EMITTED A BIG BANG AND STALLED. CAUSE OF DAMAGE UNDETERMINED. REMOVED AND REPLACED ENGINE PER WORK CARD F7201-7204 AND 7207. 2L74 4F4 F A20WE E20EA 20051221000172005122100017WP 2005 12 21 05FDEA04367 120051217A5753 SKIN DOUG MD10 MD1010F 3022112WP ZONE 600 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25359FE 46635 RIGHT WING OUTBOARD FLAP LOWER SKIN, DENT AT XFS 651, 6 INCHES FROM AFT EDGE IS OUT OF LIMITS. REPAIRED IAW DC10 SRM 57-10-00 FIG 85 VOL I MECH. 2668 QC316 SEE FEDEX NON ROUTINE NR N00598 OF WORK ORDER 00031297. 2L73 4F RTA22WE 20051221000192005122100019 2005 12 21 05FDEA04369 220051214A7200 ENGINE AIRBUS300 A300B4605R 3930308EU UNKNOWN UNKNOWN A FDEAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SO25677FE 791 T/O FROM RWY 23R IND WIND 120/09 T/O ROLL SEEMED NORMAL UNTIL ABOUT 110KTS. ACCELERATION SLOWED AT APPROX 125KNTS N1S BOTH ENGS STARTED TO ROLL BACK. TARGET N1 WAS 96.1. ABORTED AT 130KTS WHILE N1 WAS DECELERATING THRU 89%. V1 139, VR 139, V2 143. 2L72 4F RTA35EU 20051221000212005122100021EA 2005 12 21 COMA0560731 120051216A2750855D10011 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS UNRELIABLE A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01507CA100263834 7796 FLIGHT 5803- FLAPS FAIL CAUTION. REPLACED THE RT BPSU. 2L72 4F RTA21EA 20051221000222005122100022NM 2005 12 21 AWXA200501544 120051216A2121EVT3454H FAN AIRBUSA319 A319132 3930340NM CABIN VIBRATION A AWXAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 WP28831AW1594415944 1576 CREW REPORTED THAT DURING CRUISE FLIGHT, AT FL 350, AN UNUSUAL VIBRATION IN THE COCKPIT AND FORWARD GALLEY. THEN REPORTED GETTING SMOKE ODOR IN THE COCKPIT. CREW USED THE O2 MASKS AND DIVERTED TO ABQ. LANDED WITHOUT FURTHER INCIDENT. MX R & R AVIONICS BLOWER FAN, 20HQ, IAW AIRBUS MM 21-26-51. OPERATIONAL CHECKS WERE GOOD. CONFIRMED FAILURE. UPON TEARDOWN VENDOR FOUND FRONT BEARING SHATTERED AND FRONT FLANGE WORN OUT. VENDOR CLEANED UNIT. VENDOR REPLACED BEARINGS, FRONT FLANGE AND CONSUMABLES, BALANCED ROTOR AND MOTOR, AND MODIFIED TO EVT3454HC. VENDOR TESTED UNIT IAW CMM 21-26-42 REV. 7. 2L72 4F RTA28NM 20051221000232005122100023NM 2005 12 21 AWXA200501549 120051127A5330654577349 SKIN BOEING737 7373G7 1384595NM BS 788 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 MCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED SKIN CRACKED, .202 INCHES, AT STRINGER 10L AND BS 788 AT LOWER ROW OF FASTENERS AT LAP SEAM. MAINTENANCE REMOVED DAMAGED AREA IAW BOEING 737-300 SRM 53-00-01-02R30. FABRICATED DOUBLERS, FILLERS AND SPLICE STRAP IAW BOEING 737-300 SRM 53-00-01-02R30. INSTALLED FABRICATED REPAIR PARTS AT STRINGER 10L AND BS 788 IAW BOEING 737-300 SRM 53-00-01-02R30. 2L72 4F RTA16WE 20051221000242005122100024NM 2005 12 21 AWXA200501550 120051122A5330654576655 SKIN PANEL BOEING737 7373G7 1384595NM BS 400 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 MCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED SKIN CRACKED, .246 INCHES, AT STRINGER 10L AND BS 400. MAINTENANCE REMOVED DAMAGED AREA IAW BOEING 737-300 SRM 53-00-01-02R30. FABRICATED DOUBLERS, FILLERS AND SPLICE STRAP IAW BOEING 737-300 SRM 53-00-01-02R30. INSTALLED FABRICATED REPAIR PARTS AT STRINGER 10L AND BS 400 IAW BOEING 737-300 SRM 53-00-01-02R30. 2L72 4F RTA16WE 20051221000262005122100026NM 2005 12 21 AWXA200501552 120051127A5330654577349 SKIN BOEING737 7373G7 1384595NM BS 727B-727C CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 MCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED SKIN CRACKED, .202 INCHES, AT STRINGER 10L AND FROM BS 727B+9 TO 727C+9 AT LOWER ROW OF FASTENERS AT LAP SEAM. MAINTENANCE REMOVED DAMAGED AREA IAW BOEING 737-300 SRM 53-00-01-02R30. FABRICATED DOUBLERS, FILLERS AND SPLICE STRAP IAW BOEING 737-300 SRM 53-00-01-02R30. INSTALLED FABRICATED REPAIR PARTS AT STRINGER 10L AND FROM BS 727B+9 TO BS 727C+9 IAW BOEING 737-300 SRM 53-00-01-02R30. 2L72 4F RTA16WE 20051221000282005122100028NM 2005 12 21 AWXA200501554 120051127A5330654577349 SKIN BOEING737 7373G7 1384595NM BS 756 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 MCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED SKIN CRACKED, .202 INCHES, AT STRINGER 10L AND BS 756 AT LOWER ROW OF FASTENERS AT LAP SEAM. MAINTENANCE REMOVED DAMAGED AREA IAW BOEING 737-300 SRM 53-00-01-02R30. FABRICATED DOUBLERS, FILLERS AND SPLICE STRAP IAW BOEING 737-300 SRM 53-00-01-02R30. INSTALLED FABRICATED REPAIR PARTS AT STRINGER 10L AND BS 756 IAW BOEING 737-300 SRM 53-00-01-02R30. 2L72 4F RTA16WE 20051221000302005122100030NM 2005 12 21 AWXA200501556 120051119A53306545765100 SKIN PANEL BOEING737 7373G7 1384595NM BS 500 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 MCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED SKIN CRACKED, 2.0 INCHES, AT STRINGER 4L AND BS 500+15 AT LOWER ROW OF FASTENERS AT LAP SEAM. MAINTENANCE REMOVED DAMAGED AREA IAW BOEING 737-300 SRM 53-00-01-02R30. FABRICATED DOUBLERS, FILLERS AND SPLICE STRAP IAW BOEING 737-300 SRM 53-00-01-02R30. INSTALLED FABRICATED REPAIR PARTS AT STRINGER 4L AND BS 500+15 IAW BOEING 737-300 SRM 53-00-01-02R30. 2L72 4F RTA16WE 20051221000532005122100053 2005 12 21 0501746623 420051216A22106D34351883 CONTROL PANEL BOEING747 747251B 1384892NM AUTOPILOT ODOR A NWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL01623US 21705 DURING CRUISE, AUTO PILOT FLIGHT CONTROL PANEL EMITTED AN ELECTRICAL ODOR, UPON TURNING LIGHTS OFF SMELL WENT AWAY. MAINTENANCE REMOVED AND REPLACED AUTO PILOT/FLIGHT DIRECTOR MODE SELECTOR PANEL. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2L74 4F A20WE 20051221000562005122100056EA 2005 12 21 COMA0560721 120051213A32971700203 WIRE HARNESS CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A COMAO OTHER N FALSE WARNING CLCLIMB 1 SO01967CA 7134 FLIGHT 5497 - GEAR DISAGREE WARNING. REPLACED THE NLG WOW HARNESS. 2L72 4F RTA21EA 20051221000582005122100058NM 2005 12 21 QXEA200501789 120051216A2120 ODOR BOMBDRDHC8 DHC8402 1390042NM CABIN DETECTED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM09417QX 4086 PDX FLIGHT NR 2422: FA REPORTED BURNING SMELL IN ROWS 11 AND BACK. MAINTENANCE GROUND RAN AIRCRAFT. CYCLED BLEEDS NR 1 AND NR 2 ON AND OFF. COULD NOT DUPLICATE SMELL. FA REPORTED ONLY SMELL, NO SIGN OF SMOKE. NO PARTS REPLACED. AIRCRAFT OK FOR CONTINUED SERVICE. 2H72 4T RTA13NM 20051221000602005122100060WP 2005 12 21 0501659927 120051130A5312 DOOR DOUG DC9 DC931 3022065WP AFT PRESBULKHEADNOT SEATED A NWAAB EMER. DESCENT JS WARNING INDICATION AFFECT SYSTEMS CRCRUISE 1 GL018920E 45835 IN CRUISE FLIGHT AT FL270 AN AIR LEAK AT THE AFT PRESSURE BULKHEAD DOOR WAS REPORTED. THE RED "CABIN PRESS" WARNING LIGHT ILLUMINATED AS THE CABIN ALTITUDE REACHED 10,500 FEET. THE MASKS DID NOT DEPLOY. THE RED BORDER CHECKLIST AND DESCENT TO 11,000 FEET WERE ACCOMPLISHED. CABIN PRESSURE WAS STABILIZED DURING DESCENT. LANDING AT MSP WAS UNEVENTFUL AND MAINTENANCE FOUND THE AFT CABIN PLUG DOOR IMPROPERLY SEATED. AFTER INSPECTION OF THE DOOR SEAL AND FRAME THE CABIN PRESSURE WAS CHECKED. NO LEAKS WERE FOUND SO THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F A6WE 20051221000622005122100062NM 2005 12 21 DHL2005765508 120051212A5520 HINGE FITTING BOEING727 727264 138408MNM NR 1 ELEVATOR CORRODED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15765AT 23014 RT HORIZ STAB T/E NR 1 ELEVATOR ATTACH HINGE LUGS INNER FACES HAS PITTING CORROSION. BLENDED CORROSION ON LUGS IAW TIMCO REO-983 REV IR DATED 12/01/05. FOUND LUGS TO BE WITHIN LIMITS, TREATED AND PRIMED IAW B727 SRM 51-20-1. 2L73 4F A3WE 20051221000642005122100064NM 2005 12 21 DHL2005765506 120051212A5320 FLOOR SUPPORT BOEING727 727264 138408MNM BS 1030-1050 CORRODED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15765AT 23014 AFT BAGGAGE PIT CORROSION ON FLOOR SUPPORT CHANNEL, LWR SIDE, BETWEEN STA 1030 AND 1050 RBL 12. REMOVED SECTION OF FLOOR SUPPORT STA 1030 - 1082. FABRICATED AND INSTALLED (3) REPAIR SPLICES 10.50" BY 1" BY 1" FROM BAC1490-2583, 10.50 BY .085" BY .085" FROM AND10133-0702 AND 36.750" BY .090" BY 1" BY .050" FROM BAC1509-100146 IAW B727 SRM 53-10-5 FIG 4. 2L73 4F A3WE 20051221000662005122100066NM 2005 12 21 DHL2005765507 120051212A5520 HINGE FITTING BOEING727 727264 138408MNM NR 1 ELEVATOR CORRODED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15765AT 23014 FOUND LEFT HORIZ STAB T/E NR 1 ELEVATOR ATTACH HINGE LUGS INNER FACES HAS PITTING CORROSION. BLENDED CORROSION ON LUGS IAW TIMCO REO-983 REV IR DATED 12/01/05. FOUND LUGS TO BE WITHIN LIMITS, TREATED AND PRIMED IAW B727 SRM 51-20-1. 2L73 4F A3WE 20051221000672005122100067EU 2005 12 21 05FDEA04054 120051201A5315 FLOORBEAM AIRBUS310 A310203 3930313EU GE CF6 CF680 30025NE FUSELAGE NONE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 PREVIOUS REPAIRS ON MAIN DECK CARGO FLOORBEAMS AT FS 34, FS 35, AND FS 36, RT OF CENTER, NEEDS EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. EVALUATION DETERMINED REPAIRS TO BE IAW EA 6-5310-29466. NO FURTHER ACTION REQUIRED. MINOR REPAIR IAW GMM 6-2-100. WORKED ON NRC N00727. 2L72 4F4 FRTA35EU E13NE 20051221000682005122100068NM 2005 12 21 05FDEA04144 120051205A5320 INTERCOSTAL BOEING727 727200 138407ENM PWA JT8 JT8D9A 52048NE BS 950B CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 INTERCOSTAL CRACKED BS 950B-2, STR 29R WL 155. REPAIRED IAW SRM 51-40-2. 2L73 4F4 FRTA3WE E2EA 20051221000692005122100069NM 2005 12 21 05FDEA04371 120051219A5101 REPAIR BOEING727 727233 138408ANM NONE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25274FE 22039 FOUND PREVIOUSLY INSTALLED REPAIR AT LT ENTRY DOOR STR 13L WAS ACCOMPLISHED IAW EO 7-5330-7-2345 PT.2, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTED OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL THICKNESS AND TYPE, GENERAL WORKMANSHIP, REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100. 2L73 4F RTA3WE 20051221000722005122100072NM 2005 12 21 05FDEA04373 120051219A5101 REPAIR BOEING727 727233 138408ANM UNDAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25274FE 22039 FOUND PREVIOUSLY INSTALLED REPAIR AT AFT LOWER CORNER OF FWD GALLEY DOOR CUT OUT WAS ACCOMPLISHED IAW SB 727-53-0188, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTED OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL THICKNESS AND TYPE, GENERAL WORKMANSHIP, REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100. 2L73 4F RTA3WE 20051221000742005122100074NM 2005 12 21 05FDEA04375 120051219A5101 REPAIR BOEING727 727233 138408ANM UNDAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25274FE 22039 FOUND PREVIOUSLY INSTALLED REINFORCEMENT DOUBLER AT STA 344 BETWEEN STR 4L AND 5L WAS ACCOMPLISHED IAW RIGID BARRIER MODIFICATION DOCUMENT EA 7-5340-7-5002, PAGE 1 AND VENTURA AEROSPACE DWG 2942, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTED OF LOCATION, SHAPE, SIZE, FASTENERS SPACING AND NUMBERS, MATERIAL THICKNESS AND TYPE, GENERAL WORKMANSHIP, REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100. 2L73 4F RTA3WE 20051221000762005122100076NM 2005 12 21 05FDEA04377 120051219A5330 SKIN BOEING727 727227 1384078NM BS 255 BULGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 BS 255, STR 24-25 L, 2" CREASED BULGE IN THE SKIN. REPAIRED FUSELAGE SKIN AT BS 255 STR 24-25 L/TAS PER FED EX EA 7-5330-91428. 2L73 4F A3WE 20051221000772005122100077EU 2005 12 21 05FDEA04255 120051212A5754 SKIN AIRBUS310 A310222 3930315EU NR 2 SLAT SCRATCHED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25450FE 162 LT WING NR 2 SLAT UPPER SURFACE HAS SCRATCHES AND A PUNCTURE APPROX 2.7 BY 3.2" (NR 39 HURRICANE RITA) REF N00089. REPAIRED NR 2 SLAT IAW EA 6-5750-94524. 2L72 4F RTA35EU 20051221000782005122100078NM 2005 12 21 05FDEA04256 120051212A5330 SKIN BOEING727 727227 1384078NM BS 1184 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 BS 1183 SECTION 48 RIGHT SIDE OUTER SKIN CREASED AT BS 1184 NEXT TO THE TAIL SKID. REMOVED AND REPLACED SKIN PANEL IAW SRM 51-30-2. 2L73 4F A3WE 20051221000792005122100079NM 2005 12 21 05FDEA04257 120051212A5315 FLOORBEAM BOEING727 727227 1384078NM BS 520 TOOL DAMAGE A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25490FE 21493 MECHANICAL DAMAGE (DRILL START) TO FLOORBEAM BS 520 RBL 10.5 WL 208. REPAIRED FLOORBEAM PER SRM 53-10-8. 2L73 4F A3WE 20051221000802005122100080NM 2005 12 21 05FDEA04189 120051208A2780ARB2981115 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 500 CRACKED A FDEAA UNSCHED LANDING FF FLT CONT AFFECTED FLT CONT AFFECTED CLCLIMB 1 SO25593FE 48551 SLAT DISAGREE AFTER T/O PRIOR TO SLAT RETRACT. NO ROLL MOVEMENT. INDICATION STOPPED AT SLAT RETRACTION ON ARRIVAL SFS SLAT DISAGREE AGAIN. FOLLOWED CHECK LIST. NO SLAT LANDING WAS NORMAL. FOUND DAMAGED L/E STRUCTURE WHERE PULLY FOR NR 1 SLAT EXTEND CABLE IS MOUNTED. REF IPC 27-81 -35-01 PULLY MOUNTED NR 2 SLAT TRACK OUTBOARD WALL CAME OFF WITH PULLY. ABOUT 18" BY 18" OF PART OF WALL CAME WITH PULLY. REPAIR C/O ON LHW NR 2 SLAT TRACK O/B WEB AND SUPPORT AS PER FEDEX EA 1-5740-90695. (TITLE: WINGS-LEADING EDGE SLATS - LT NR 2 SLAT TRACK WEB AND SUPPORT REPAIR AT STATION XIS, = 211.719) SLAT OPS TEST AND ADJ AS PER MM 27-80-00 AND MM 27-80-20 AND FOUND SATISFACTORY. 2L73 4F RTA22WE 20051221000822005122100082NM 2005 12 21 05FDEA04259 120051212A5314 KEELBEAM BOEING727 727227 1384078NM BS 950D CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 FOUND CORROSION ON KEELBEAM REPAIR STRAP BS 950D PLUS 5" STR 29 LT. REMOVED AND REPLACED REPAIR STRAP PER DWG SR27-53-023, REV A. 2L73 4F A3WE 20051221000842005122100084NM 2005 12 21 05FDEA04261 120051212A5311 FRAME BOEING727 727227 1384078NM BS 540 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 FWD CARGO BAY FRAME IB FLANGE DENTED AT BS 540, STR 24LT. REPAIRED FRAME AT BS 540 STR 24L PER SRM 51-40-3. 2L73 4F A3WE 20051221000862005122100086NM 2005 12 21 05FDEA04263 120051212A5311 FRAME BOEING727 727227 1384078NM BS 500 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 FWD CARGO BAY FRAME IB FLANGE DENTED AT BS 500, BETWEEN STR 24LT AND STR 25LT. REPAIRED FRAME AT BS 500 STRINGER 24L-25L PER SRM 51-40-3. 2L73 4F A3WE 20051221000882005122100088NM 2005 12 21 DHL2005765513 120051207A5320 FLOOR SUPPORT BOEING727 727264 138408MNM BS 644 CORRODED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15765AT 23014 FOUND FWD PIT FLOOR SUPPORT CORRODED AT STA 644 RBL 2. CUT OUT CRACKED SECTION OF FLOOR SUPPORT STA 644 RBL 2. FABRICATED AND INSTALLED REPAIR SPLICES 21-7/8" BY 1" BY 1-1/4" FROM BAC1520-1485 AND 11-1/4" BY 3/4" BY 1" AND 10-7/8" BY 1-1/4" BY 7/8" FROM BAC1490-2734 IAW B727 SRM 53-10-5 FIG 4. 2L73 4F A3WE 20051221000902005122100090NM 2005 12 21 DHL2005765516 120051207A5347 SEAT TRACK BOEING727 727264 138408MNM BS 1030-1130 CORRODED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15765AT 23014 FOUND UPPER CARGO COMPT TRACK 24R BS 1030 TO 1130 HAS CORROSION. CUT OUT CRACKED SECTION OF TRACK BS 1050 TO 1130. FABRICATED AND INSTALLED REPAIR 40" BY 3.25" FROM 65-23637-53 IAW B727 SRM 53-10-5 FIG 7. 2L73 4F A3WE 20051221000922005122100092EU 2005 12 21 05FDEA04245 120051212A5753 SKIN AIRBUS310 A310222 3930315EU RT WING TE FLAP SCRATCHED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25450FE 162 SCARATCHES TO UPPER SURFACE OF RT WING O/B FLAP BETWEEN NR 3 AND NR 4 CANOES NR 36 HURRICANE RITA REF N00086. REPAIRED 3 EA DENTS ON RT O/B FLAP IAW A310-200 SRM 57-53-12 REPAIR NR 11. 2L72 4F RTA35EU 20051221000932005122100093NE 2005 12 21 ASOA05945 220051102A726030372233 CARBON SEAL AEROSPATR72 ATR72 EU PWA PW120 PW127 NE NR 2 ENGINE WORN A ASOAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27630AS 336 DURING CRUISE, A FUEL SMELL WAS REPORTED AROUND ROWS 2-5, AND REMAINED THE ENTIRE FLIGHT. THE AIRCRAFT LANDED SAFELY. MAINT REMOVED AND REPLACED THE NR 2 ENGINE STARTER GEAR BOX CARBON SEAL. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K) 2H72 4T4 TRT E20NE 20051221000962005122100096NM 2005 12 21 05FDEA04247 120051212A5340 STRINGER CLIP BOEING727 727227 1384078NM BS 620 CUT A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 FOUND FWD CARGO BAY STR CLIP CUT AT BS 620, STR 25LT. REPLACED STRINGER CLIP PER SRM 51-30-2. 2L73 4F A3WE 20051221000992005122100099NM 2005 12 21 AWXA200501529 120051118A575465C26603100SP SKIN BOEING737 73733A 1384673NM ZONE 600 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 MCN - DURING C19 CHECK DISCOVERED 2 CRACKS, .5 AND .75 INCHES IN LENGTH, ON THE BOTTOM OF THE NR 4 SLAT INBOARD OF ACTUATOR FROM SS 50R TO SS 65R. MAINTENANCE TRIMMED OUT DAMAGED AREA ON THE NR 4 SLAT IAW BOEING 737-300 SRM 57-43-01-2R6. FABRICATED FILLER AND SPLICE PLATE IAW BOEING 737-300 SRM 57-43-01-2R6. INSTALLED FABRICATED REPAIR PARTS ON THE NR 4 SLAT FROM SS 50R TO SS 65R IAW BOEING 737-300 SRM 57-43-01-2R6. 2L72 4F RTA16WE 20051221001022005122100102NM 2005 12 21 AWXA200501531 120051116A575465C267945 SKIN BOEING737 73733A 1384673NM NR 2 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 MCN - DURING C19 CHECK DISCOVERED 2 CRACKS, 1.0 INCH, AT FASTENERS LOCATED ON THE NR 2 SLAT BELOW THE INBOARD AUXILIARY TRACK FROM SS 163L TO SS 165L. MAINTENANCE TRIMMED OUT DAMAGED AREA ON THE NR 2 SLAT IAW BOEING 737-300 SRM 57-43-01-2R6. FABRICATED FILLER AND SPLICE PLATE IAW BOEING 737-300 SRM 57-43-01-2R6. INSTALLED FABRICATED REPAIR PARTS ON THE NR 2 SLAT BELOW INBOARD AUXILIARY TRACK FROM SS 163L TO SS 165L IAW BOEING 737-300 SRM 57-43-01-2R6. 2L72 4F RTA16WE 20051221001062005122100106NM 2005 12 21 AWXA200501533 120051117A5340693535214 STRINGER CLIP BOEING737 73733A 1384673NM BS 616 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 MCN - DURING C19 CHECK DISCOVERED STRINGER TIE CLIP CRACKED, .25 INCHES, AT STRINGER 4R AND BS 616. MAINTENANCE REMOVED AND INSTALLED NEW STRINGER CLIP AT 4R AND BS 616 IAW BOEING 737-300 SRM 51-40-02-0G FIG 8 AND FIG 12. 2L72 4F RTA16WE 20051221001082005122100108NM 2005 12 21 AWXA200501535 120051201A532065C3453721 CHANNEL BOEING737 73733A 1384673NM BS 663 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 MCN - DURING C19 CHECK DISCOVERED VERTICAL WEB CHANNEL CRACKED, 1.0 INCH, AT BS 663.75, BL 25R AND WL 206. MAINTENANCE NOTCHED OUT REMAINING MATERIAL ON VERTICAL WEB CHANNEL IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NO. 03-5702-05346-HF1. FABRICATED CHANNEL IAW AWA ER NR 03-5702-05346-HF1. INSTALLED FABRICATED REPAIR PARTS ON VERTICAL WEB AT BS 663.75, BL 25R, AND WL 206 IAW AWA ER NR 03-5702-05346-HF1. 2L72 4F RTA16WE 20051221001092005122100109NM 2005 12 21 AMTA200500944 120051026A2612 TERMINAL BOEING757 75733N 1384931NM GE CF34 CF343B1 NE FIRE LOOP LOOSE A AMTAK NONE N FALSE WARNING CRCRUISE 1 GL11552TZ 32586 LOOP ONE EICAS MSG LT ENG. FOUND TERMINAL LOOSE AT LOOP TS5033. TIGHTENED AS REQUIRED. FIRE LOOP OPS CHECK NORMAL IAW AMM. (K) 2L72 4F4 FRTA2NM E15NE 20051221001112005122100111NM 2005 12 21 AWXA200501537 120051122A5320654795711 STRAP BOEING737 73733A 1384673NM TORQUE BOX CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 MCN - DURING C19 CHECK DISCOVERED CORROSION ON THE AFT PIT DOOR CUTOUT TORQUE BOX STRAP FROM BS 794 TO BS 847, WL 158 AND BL 19R. CORROSION WAS FOUND OUT LIMITS IAW BOEING 737-300 SRM 53-60-15-1A1 FIG 101. MAINTENANCE REMOVED AND INSTALLED NEW STRAP FROM BS 794 TO BS 847, WL 158 AND BL 19R IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 3, 4, 8 AND 12. 2L72 4F RTA16WE 20051221001142005122100114NM 2005 12 21 AWXA200501539 120051116A53206545834107 STRAP BOEING737 73733A 1384673NM FLOORBEAM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 MCN - DURING C19 CHECK DISCOVERED LOWER FLOORBEAM STRAP CRACKED AT BS 344, BL 48L AND WL 200. MAINTENANCE REMOVED DAMAGED SECTION OF STRAP IAW BOEING 737-300 SRM 51-70-13-0G FIG 1. FABRICATED FILLER AND REPAIR PLATES IAW BOEING 737-300 SRM 51-70-13-0G FIG 1. INSTALLED FABRICATED REPAIR PARTS AT BS 344, BL 48L AND WL 200 IAW BOEING 737-300 SRM 51-70-13-0G FIG 1. 2L72 4F RTA16WE 20051221001162005122100116SO 2005 12 21 FDK2005F00000 120050919A2530 ODOR EMB 145 EMB145LR 3260212SO ALLSN AE3007AE3007C GL GALLEY DETECTED A FDKAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW07825MJ 145179 (REF NR F05002) THE CREW REPORTED A SMOKE LIKE SMELL IN GALLEY DURING FLIGHT. MAINTENANCE PERFORMED A GVI TO GALLEY AREA AND WIRING. MAINTENANCE CHANGED TRASH OUT AND CLEANED COFFEE POTS. NO SMOKE SMELL DETECTED. (K) 2L72 4T4 FRTT00011ATTE6CH 20051221001192005122100119NM 2005 12 21 AWXA200501543 120051114A57536546430100 SKIN BOEING737 73733A 1384673NM FOREFLAP DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 MCN - DURING C19 CHECK DISCOVERED DISBOND AREA ON THE UPPER SURFACE OF THE RT INBOARD FORE FLAP 13 INCHES FROM THE INBOARD END FROM WBL 83.74R TO WBL 84.74R. MAINTENANCE CUT OUT DISBOND AREA IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED REPAIR CORE, REPAIR SEPTUM AND REPAIR DOULBER IAW BOEING 737-300 SRM 51-70-10-2R4. BONDED REPAIR PARTS TO THE UPPER SURFACE OF THE RT INBOARD FORE FLAP IAW BOEING 737-300 SRM 51-70-10-2R4. 2L72 4F RTA16WE 20051221001202005122100120SO 2005 12 21 FDK2005F00001 120050919A2560 ESCAPE ROPE EMB 145 EMB145LR 3260212SO ALLSN AE3007AE3007C GL COCKPIT UNSECURE A FDKAK NONE O OTHER ININSP/MAINT 1 SW07825MJ 145179 (REF NR F05004) THE CREW HAD A F/O EMERGENCY ESCAPE ROPE THAT WAS NOT SECURE IN ITS CONTAINER. MAINTENANCE SECURED ESCAPE ROPE. (K) 2L72 4T4 FRTT00011ATTE6CH 20051221001232005122100123EA 2005 12 21 COMA0560726 120051215A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01486CA 7707 FLIGHT 5342 - FOUND RT THRUST REVERSER UNLOCKED MESSAGE. 2L72 4F RTA21EA 20051221001262005122100126 2005 12 21 CALA0500439 420051212A25655A30863 SLIDE BOEING737 737824 13844BZNM L-1 DOOR TWISTED A CALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW2727213193455464 28773 L-1 DOOR SLIDE DID NOT DEPLOY PROPERLY DURING AN EMERGENCY EVACUATION ON RUNWAY AFTER LANDING AT IAH. EVACUATION WAS PERFORMED DUE TO A HYD LEAK THAT CAUSED FORMATION OF HYD MIST AND FUMES IN CABIN ON LANDING AT IAH. SLIDE WAS DESCRIBED AS BEING UNUSEABLE DUE TO FACT THAT WHEN IT DEPLOYED IT BECAME "TWISTED"/WAS IN A COCKED POSITION (ONE SIDE WAS HIGHER THAN THE OTHER). L-I DOOR SLIDE WAS R/R`D IAW MM 25-66-01. ENGINEERING PERFORMED A DEPLOYMENT TEST WITH ANOTHER SLIDE AT L-I DOOR AND SLIDE DEPLOYED AND INFLATED W/O ANY PROBLEMS. SLIDE PACK CONTAINER AT L-1 DOOR WAS ALSO EXAMINED BY ENGINEERING AND NO ANOMALIES WERE FOUND. ANOTHER SLIDE WAS INSTALLED ON L-1 DOOR TO REPLACE TEST SLIDE. INVESTIGATION IS CONT2L72 4F RTA16WE 20051221001282005122100128EU 2005 12 21 RAIA00512014 120051209A3397 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHTSOUT OF ADJUST A RAIAK NONE O OTHER ININSP/MAINT 1 CE03565HK 41082 POST FLIGHT-STL-EMERGENCY LIGHTS ON FLOOR WILL NOT ILLUMINATE. MAINTENANCE ADJUSTED CONNECTION TO EMERGENCY LIGHTS. 2L72 4T RTA41NM 20051221001312005122100131SO 2005 12 21 RAIA00512016 120051212A3397 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSDISCONNECTED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03813HK 145044 PRE-FLIGHT - ST - SECTION OF EMERGENCY LIGHTING NOT WORKING. MAINTENANCE RECONNECTED EMERGENCY EXIT PATHWAY LIGHT STRIP. 2L72 4T RTT00011AT 20051221001332005122100133SO 2005 12 21 RAIA00512019 120051215A2611 FILTER EMB 145 EMB145LR 3260212SO SMOKE DETECTOR DIRTY A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03847HK 14500857 FLT 7976 - IAD - LAVATORY SMOKE MESSAGE ON EICAS IN FLIGHT. MAINTENANCE CLEANED THE SMOKE DETECTOR FILTER. 2L72 4T RTT00011AT 20051221001352005122100135SO 2005 12 21 RAIA00512020 120051215A3350 LIGHT EMB 145 EMB145 3260210SO CABIN MALFUNCTIONED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03805HK 145096 PRE-FLIGHT - RIC - EXIT ROW OVERHEAD EMERGENCY LIGHT OUT FACING FORWARD. MAINTENANCE PERFORMED OPERATIONAL TEST OF EMERGENCY LIGHTING SYSTEM. 2L72 4F RTT00011AT 20051221001362005122100136CE 2005 12 21 O2G2005F00013 120051025A275299146153 PDU CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL T/E FLAP FAILED E O2GAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 NE03610GR1150 7500163 DURING CLIMBOUT OF SDL, WHILE RETRACTING FLAPS THEY FAILED AT 13 PERCENT AND WOULD NOT RESET. REPLACED FLAP PDU AND SOFT START RELAY. (K) 2L72 4J4 FRTT00007WITE6CH 20051221001382005122100138SO 2005 12 21 RAIA00512018 120051214A5210 CONNECTING ROD EMB 145 EMB145LR 3260212SO PAX DOOR OUT OF ADJUST A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03847HK 14500857 FLT 8030 - IAD - MAIN CABIN DOOR EXTREMELY DIFFICULT TO OPEN. MAINTENANCE ADJUSTED MAIN DOOR INTER-CONNECTING RODS. 2L72 4T RTT00011AT 20051220001092005122000109NM 2005 12 20 ASAA0580497 120050926A5321993644511 FLOOR PANEL DOUG MD80 MD83 3023681NM FS 160-200 DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - FOUND HV CHECK, PAX CABIN FLOOR PANEL HAS CORRODED INSERTS WITH DELAMINATION AROUND INSERTS. REPLACED FLOOR PANEL. (M) 2L72 4F RT 20051220001182005122000118WP 2005 12 20 ASAA0580441 120050807A532059366600171 ANGLE DOUG DC9 DC982 3022082WP FS 1115-1211 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02935AS 49236 OKC - FOUND DURING C-CHECK, T-ANGLE CHORD ON SUPPORT BEAM CORRODED. REPLAED T-ANGLE. (M) 2L72 4F A6WE 20051220001202005122000120NM 2005 12 20 ASAA0580490 120050926A532199366889 FLOOR PANEL DOUG MD80 MD83 3023681NM FS 807-826 DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - DURING HV-CHECK, FOUND PAX CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RT 20051220001212005122000121EU 2005 12 20 USAA051543 120051213A5320D5347317220400 FLOOR SUPPORT AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19113UW 1141 CORROSION Y1292-Y1162 BETWEEN FR C66-C68. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-42-11; CORR LEVEL 1; TASK JA-260-53500, DEFECT SIZE: 1 INCH DIA. 2L72 4F RTA28NM 20051220001362005122000136EU 2005 12 20 USAA051541 120051213A5320D5348009 SILL AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19113UW 1141 Y1400 AT C66 CORRODED. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-42-11; CORR LEVEL 1; TASK JA-260-53500. DEFECT SIZE: 1 INCH DIA. 2L72 4F RTA28NM 20051220001452005122000145NM 2005 12 20 SWAA053942 120051213A3350101073 LENS BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29322SW 23343 DURING SCHEDULED C3 CHECK, FOUND EMERGENCY LIGHT LENS LOOSE AT ROW 1 DEF. SECURED LENS PER MM. 2L72 4F RTA16WE 20051220001812005122000181NM 2005 12 20 ASAA0580488 120050926A532199366403 FLOOR PANEL DOUG MD80 MD83 3023681NM FS 886-927 DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - FOUND HV-CHECK, PAX CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RT 20051220001832005122000183NM 2005 12 20 ASAA0580491 120050926A532199366405 FLOOR PANEL DOUG MD80 MD83 3023681NM FS 864-886 DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - DURING HV-CHECK, FOUND PAX CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RT 20051220002082005122000208WP 2005 12 20 ASAA0580482 120050904A532299360737 SHEAR TIE DOUG DC9 DC982 3022082WP FS 636 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02931AS 49232 OKC - DURING C-CHECK, FOUND SHEAR TIE CORRODED. REPLACED SHEAR TIE. (M) 2L72 4F A6WE 20051220002552005122000255WP 2005 12 20 ASAA0580458 120050808A53305936434129 SKIN DOUG DC9 DC982 3022082WP FS 522-541 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02935AS 49236 OKC - DURING C-CHECK, FOUND FUSELAGE SKIN IS DENTED. REMOVED DAMAGED AREA. INSTALLED REPAIR DOUBLER AND STRAPS. (M) 2L72 4F A6WE 20051220002612005122000261WP 2005 12 20 ASAA0580455 120050808A5330593666751 SKIN DOUG DC9 DC982 3022082WP FS 1254 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02935AS 49236 OKC - DURING C-CHECK, FOUND FUSELAGE SKIN IS DENTED. COLD-WORKED DAMAGED AREA. INSTALLED REPAIR DOUBLER. (M) 2L72 4F A6WE 20051220002652005122000265WP 2005 12 20 ASAA0580475 120050828A52005932344501 ACCESS PANEL DOUG DC9 DC982 3022082WP FS 845-946 INTERFERENCE A ASAAK NONE O OTHER ININSP/MAINT 1 NM02934AS 49235 SEA LINE CHECK - WHILE ATTEMPTING TO GAIN ACCESS TO A PANEL ON THE UPPER SURFACE OF THE LEFT WING VIA ONE OF THE OVERWING EMERGENCY EXIT DOORS, IT WAS DETERMINED THAT NOT ONLY WAS THAT DOOR DIFFICULT TO OPEN, BUT THAT ALL OVERWING DOORS WERE DIFFICULT TO OPEN. THE CAUSE WAS INTERFERENCE FROM PROTRUDING DOOR LINING PANEL TRIM. TRIMMED LINING PANELS AS REQUIRED TO ENSURE NO INTERFERENCE DURING DOOR REMOVAL AND INSTALLATION. (M) 2L72 4F A6WE 20051220002752005122000275NM 2005 12 20 ASAA0580512 120050926A5322993607410 SHEAR TIE DOUG MD80 MD83 3023681NM FS 1136-1155 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - DURING HV-CHECK, FOUND SHEAR TIE CORRODED. REPLACED SHEAR TIE. (M) 2L72 4F RT 20051220002762005122000276NM 2005 12 20 ASAA0540378 120050804A5534655484222 SKATE ANGLE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU VERTICAL FIN CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 RT AFT SKATE ANGLE FOR VERTICAL FIN CHAFED 18 INCH FROM AFT END ON OB SIDE. REMOVED AND REPLACED AFT SKATE ANGLE FOR VERTICAL FIN. (K) 2L72 4F4 FRTA16WE E21EU 20051220002852005122000285NM 2005 12 20 CALA0500443 120051217A5315147A5504 FLOORBEAM BOEING737 737724 13844BYNM STA 947.5 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716709 28779 INSPECTION FOUND AFT CABIN LT FLOORBEAM CORRODED AT STA 947.5, LBL 51. A REPAIR WAS INSTALLED IAW ECRA 5321-01325. 2L72 4F RTA16WE 20051220002892005122000289NM 2005 12 20 USAA051558 120051215A53106545871114 DOOR FRAME BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19591US 23936 FOUND LOWER DOOR FRAME LOWER CORNER CRACKED. INSTALLED DOUBLER IAW EA 97192, DEFECT SIZE: FWD SERVICE DOOR HAS A 2 INCH CRACK. 2L72 4F RTA16WE 20051220002962005122000296NM 2005 12 20 ASAA0540402 120050816A5315654581013 FLOORBEAM BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 CORROSION ON FLOORBEAM. REPAIRED IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051220003062005122000306EU 2005 12 20 USAA051580 120051219A5321F5367111801400 FLOOR PANEL AIRBUS330 A330323 3930335EU FR 14 DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 FOUND DELAMINATIONS FS 14. COMPOSITE DOUBLER INSTALLED PER SRM 53-02-00, DEFECT SIZE: 2" BY 5". 2L72 4F RTA46NM 20051220003092005122000309NM 2005 12 20 ASAA0540410 120050816A53206517688U175 SILL BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 CORROSION ON FWD ENTRY DOOR MOPSILL BSTA 300-344, LBL 58, WL 208. REMOVED AND REPLACED IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051220003232005122000323 2005 12 20 QXEA200501782 420051213A3130980470001 RECORDER DHAV DHC8 DHC8202 2809007NM FLIGHT DATA MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09365PH150293026 526 BOI FLT NR 2185 - FLIGHT DATA RECORDER CAUTION LIGHT ILLUMINATED, CONFIRMED CIRCUIT BREAKERS IN PER CHECKLIST. MAINTENANCE REPLACED THE FLIGHT DATA RECORDER. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051220003302005122000330EU 2005 12 20 USAA051571 120051219A5347F53326552203 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 FOUND CORROSION SEAT TRACK -Y2412 AT FS 53.9. BLENDED AREA AS PER 51-74-00, SEAT TRACK REPLACED PER SRM 51-74-00, 53-31-15, DEFECT SIZE: 2" BY 1". 2L72 4F RTA46NM 20051220003372005122000337EU 2005 12 20 USAA051577 120051219A5321F5367270300000 FLOOR PANEL AIRBUS330 A330323 3930335EU FR 25 DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 FOUND DELAMINATION FS 25. COMPOSITE DOUBLER INSTALLED PER SRM 53-02-00, DEFECT SIZE: 1" BY 4". 2L72 4F RTA46NM 20051220003452005122000345EA 2005 12 20 A6WA200540345 120051113A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31426AW 7699 THE FUSELAGE 5 KM BETWEEN VS 55.625 PERCENT AND VS 67.5 PERCENT. SPAR DATUM BETWEEN STRINGER 2R AND 4R HAS A DENT 1.5 INCH LONG X 1.875 INCH WIDE X .109 INCH DEEP. REPAIRED DAMAGE TO FUSELAGE SKIN BETWEEN VS 55.625 AND VS 67.5 SPAR DATUM BETWEEN STRINGERS 2R AND 4R IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20051220003532005122000353EA 2005 12 20 A6WA200540341 120051108A5210 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31426AW 7669 PAX DOOR AFT DRAG ANGLE CRACKED APPROX 1.0 INCH LONG AT DOOR SUPPORT CABLE PULLEY. CUT AWAY DAMAGED SECTION OF DRAG ANGLE AND INSTALLED REPAIR ANGLE AND SPLICES IAW REO. (K) 2L72 4F4 FRTA21EA E15NE 20051220003572005122000357NM 2005 12 20 CALA0500450 120051219A5315141A5505 FLOORBEAM BOEING737 737724 13844BYNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716709 28779 INSPECTION FOUND FORWARD FLOOR STRUCTURE T-CAP (FLOORBEAM) CORRODED AT STA 344. REPAIRED IAW ECRA 5321-01324. 2L72 4F RTA16WE 20051220003612005122000361NM 2005 12 20 AALA20050830 120051201A3350 BATTERY PACK BOEING737 737823 13844BZNM CABIN FAILED A AALAK NONE O OTHER ININSP/MAINT 1 SW21927AN 30077 TUL - CABIN EMERGENCY LIGHT BATTERY PACKS FAILED DRAIN TEST. REPLACED BATTERY PACKS FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20051220003742005122000374NM 2005 12 20 2005UALA01456 120051213A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29193UA 26890 EMERGENCY LIGHT SEAT 42 LT INOP. REPLACED EEL LIGHT. 2L74 4F4 FRTA20WE E24NE 20051220003772005122000377NM 2005 12 20 2005UALA01459 120051213A3350 CHARGER BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29193UA 26890 OVERWING EMERGENCY LIGHT 2ND FROM TOP LT INOP. REPLACED BATTERY CHARGER. 2L74 4F4 FRTA20WE E24NE 20051220003912005122000391EU 2005 12 20 2005UALA01473 120051217A2400 ODOR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE COCKPIT DETECTED A UALAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 WP29436UA 638 STRONG ELECTRICAL SMELL IN THE COCKPIT AND IN THE CABIN. JUST PRIOR TO SMELL, BOTH MCDU'S DUMPED ALL INFO. AFTER DESCENT, RECEIVED PITOT HEAT MSG FOR THE CAPT & F/O SIDE. ACCOMPLISHED HIGH POWER RUN BOTH ENGINES PER JET RUN-UP HANDBOOK. NO SMELLS OR SMOKE WITH PACKS ON AND COCKPIT LIT UP, WINDOW HEAT, PITOT HEAT ON. MCDU'S OPS NORMAL. NO PARTS REPLACED AND NO FURTHER ELECTRICAL SMELL. 2L72 4F4 FRTA28NM E40NE 20051220003922005122000392 2005 12 20 2005UALA01474 420051219A2565 WIRE AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE EVAC SLIDE MISROUTED A UALAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP29806UA 788 LEFT FWD PAX-CREW DOOR SLIDE ASSY EMERGENCY LIGHT WIRING IS MISROUTED. A FLEET CAMPAIGN TO VERIFY THE CORRECTNESS OF SLIDE HARNESS ROUTING. FOR THIS PURPOSE, LM CALLOUT LM4119 WAS ISSUED AND ACCOMPLISHED ON ACFT 4006 L1 SLIDE (MR25611-115) IN LAX ON 11/11/2004. THE FINDINGS WAS OK. BASED ON THE MR25611 MRTIME RECORDS AS OF 10/29/2004 AND 11/28/2005, THE SAME SLIDE ASSY (MR25611-115) HAS REMAINED INSTALLED ON THE AIRCRAFT. THERE IS NO RECORD TO SHOW ANY ACTIVITY ON THE UNIT THAT COULD HAVE RESULTED IN THE HARNESS TO BECOME MISROUTED, WHICH IS THE SUBJECT OF THIS SDR. THE ROUTING WAS CORRECTED ACCORDING TO THE SOURCE AMIS ITEM OF THIS SDR. 2L72 4F4 FRTA28NM E40NE 20051220003962005122000396NM 2005 12 20 SWAA053988 120051217A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 942, STR 24L. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20051220004002005122000400NM 2005 12 20 SWAA053992 120051216A53306516352 BEAR STRAP BOEING737 7375H4 138449DNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29501SW 24178 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN BEAR STRAP CORRODED AT FWD CARGO DOOR CUTOUT UPPER CORNERS. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051220004022005122000402NM 2005 12 20 SWAA053994 120051218A532269353656 SHEAR TIE BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29511SW 24188 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 360, BETWEEN STR 14R TO STR 15R. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051220004062005122000406NM 2005 12 20 SWAA053998 120051217A53116546526 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29622SW 27932 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051220004242005122000424NM 2005 12 20 ASAA0540474 120050916A531165465501 FRAME BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02793AS 28888 BSTA 787 FRAME CRACKED AT BIN RAIL STATION. CUTOUT DAMAGE AT FRAME BIN RAIL SUPPORT AND FABRICATED AND INSTALLED REPAIR IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051220004252005122000425NM 2005 12 20 ASAA0540425 120050822A531565C3394825 FLOORBEAM BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 CORROSION ON FLOORBEAM BSTA 947.5, LBL 16, RBL 16, WL 208. REPAIRED FLOORBEAM IAW SRM AND EA. (K) 2L72 4F4 FRTA16WE E21EU 20051220004272005122000427NM 2005 12 20 ASAA0540503 120050922A575365C2631026 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU RT MIDFLAP BIRD STRIKE A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 DURING COMPLETION OF T/C 48357001 FOUND RT WING IB MIDFLAP LEADING EDGE SKIN DAMAGED BY BIRD STRIKE. SKIN DENTED 8 INCHES LONG X 4 INCHES WIDE AND 1.5 INCHES DEEP. SKIN WAS ALSO RIPPED APPROX 2 INCHES LONG. REPAIRED RT WING IB MIDFLAP LEADING EDGE IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051221000032005122100003EU 2005 12 21 SA05128 120051214A335032145410 EPSU AIRBUS320 A320214 3930316EU PAX CABIN FAULTY A USAAK NONE O OTHER ININSP/MAINT 1 EA19107US19942 1052 DCA - THE REPLACEMENT OF THE RIGHT SIDE MID-CABIN EMERGENCY POWER SUPPLY UNIT WAS REQUIRED. MAINTENANCE REPLACED THE RIGHT SIDE MID-CABIN EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20051221000052005122100005NM 2005 12 21 SB05172 120051216A3297 CIRCUIT BREAKER BOEING737 737400 138449ANM MLG LEVER LATCH PULLED A USAAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 EA19426US 24548 FLIGHT 720, DCA-RSW: AFTER TAKEOFF, CREW HAD TO USE THE LANDING GEAR OVERRIDE TO RETRACT THE LANDING GEAR. FLIGHT DIVERTED TO CLT. MAINTENANCE FOUND THE LANDING GEAR LEVER LATCH CIRCUIT BREAKER PULLED. RESET CIRCUIT BREAKER. PERFORMED OPS TEST PER 32-31-31-4-424. NO FAULTS NOTED. 2L72 4F RTA16WE 20051221000252005122100025NM 2005 12 21 AWXA200501551 120051127A53306545772166 SKIN PANEL BOEING737 7373G7 1384595NM BS 816 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 MCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED SKIN CRACKED, .230 INCHES, AT STRINGER 10L AND BS 816 AT LOWER ROW OF FASTENERS AT LAP SEAM. MAINTENANCE REMOVED DAMAGED AREA IAW BOEING 737-300 SRM 53-00-01-02R30. FABRICATED DOUBLERS, FILLERS AND SPLICE STRAP IAW BOEING 737-300 SRM 53-00-01-02R30. INSTALLED FABRICATED REPAIR PARTS AT STRINGER 10L AND BS 816 IAW BOEING 737-300 SRM 53-00-01-02R30. 2L72 4F RTA16WE 20051221000272005122100027NM 2005 12 21 AWXA200501553 120051126A5330654576656 SKIN PANEL BOEING737 7373G7 1384595NM BS 479 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 MCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED SKIN CRACKED, .234 INCHES, AT STRINGER 10R AND BS 479 AT LOWER ROW OF FASTENERS AT LAP SEAM. MAINTENANCE REMOVED DAMAGED AREA IAW BOEING 737-300 SRM 53-00-01-02R30. FABRICATED DOUBLERS, FILLERS AND SPLICE STRAP IAW BOEING 737-300 SRM 53-00-01-02R30. INSTALLED FABRICATED REPAIR PARTS AT STRINGER 10R AND BS 479 IAW BOEING 737-300 SRM 53-00-01-02R30. 2L72 4F RTA16WE 20051221000292005122100029NM 2005 12 21 AWXA200501555 120051126A53306545772166 SKIN PANEL BOEING737 7373G7 1384595NM BS 867 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 MCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED SKIN CRACKED, .198 INCHES, AT STRINGER 4L AND BS 867 AT LOWER ROW OF FASTENERS AT LAP SEAM. MAINTENANCE REMOVED DAMAGED AREA IAW BOEING 737-300 SRM 53-00-01-02R30. FABRICATED DOUBLERS, FILLERS AND SPLICE STRAP IAW BOEING 737-300 SRM 53-00-01-02R30. INSTALLED FABRICATED REPAIR PARTS AT STRINGER 4L AND BS 867 IAW BOEING 737-300 SRM 53-00-01-02R30. 2L72 4F RTA16WE 20051221000312005122100031NM 2005 12 21 AWXA200501557 120051122A53306545767103 SKIN PANEL BOEING737 7373G7 1384595NM BS 380 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 MCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED 2 SKIN CRACKS, .5 INCHES, AT STRINGER 14L AND BS 380 AT FASTENER HOLES. MAINTENANCE REMOVED DAMAGED AREA IAW BOEING 737-300 SRM 53-00-01-02R30. FABRICATED DOUBLERS, FILLERS AND SPLICE STRAP IAW BOEING 737-300 SRM 53-00-01-02R30. INSTALLED FABRICATED REPAIR PARTS AT STRINGER 14L AND BS 380 IAW BOEING 737-300 SRM 53-00-01-02R30. 2L72 4F RTA16WE 20051221000322005122100032NM 2005 12 21 AWXA200501558 120051126A53306545768313 SKIN PANEL BOEING737 7373G7 1384595NM BS 500 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 MCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED SKIN CRACKED, .25+ INCHES, AT STRINGER 14R AND BS 500 AT LOWER FASTENER HOLE. MAINTENANCE REMOVED DAMAGED AREA IAW BOEING 737-300 SRM 53-00-01-02R30. FABRICATED DOUBLERS, FILLERS AND SPLICE STRAP IAW BOEING 737-300 SRM 53-00-01-02R30. INSTALLED FABRICATED REPAIR PARTS AT STRINGER 14R AND BS 500 IAW BOEING 737-300 SRM 53-00-01-02R30. 2L72 4F RTA16WE 20051221000342005122100034NM 2005 12 21 AWXA200501560 120051119A534069353502 STRINGER CLIP BOEING737 7373G7 1384595NM BS 520 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 MCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED STRINGER TIE CLIP CRACKED, .25 INCHES, AT STR 16L AND BS 520. MAINTENANCE REMOVED STRINGER TIE CLIP AND INSTALLED NEW STRINGER TIE CLIP AT STR 16L AND BS 520 IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 8 AND 12. 2L72 4F RTA16WE 20051221000712005122100071NM 2005 12 21 05FDEA04372 120051219A5101 REPAIR BOEING727 727233 138408ANM UNDAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25274FE 22039 FOUND PREVIOUSLY INSTALLED REPAIR AT STA 680, STR 28 WAS ACCOMPLISHED IAW SRM 51-40-3, FIG 1 PAGE 1, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTED OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL THICKNESS AND TYPE, GENERAL WORKMANSHIP, REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100. 2L73 4F RTA3WE 20051221000732005122100073NM 2005 12 21 05FDEA04374 120051219A5101 REPAIR BOEING727 727233 138408ANM UNDAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25274FE 22039 FOUND PREVIOUSLY INSTALLED REPAIR AT STA 720D, STR 19R WAS ACCOMPLISHED IAW SRM 53-30-3, FIG 6, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTED OF LOCATION, SHAPE, SIZE, FASTENERS SPACING AND NUMBERS, MATERIAL THICKNESS AND TYPE, GENERAL WORKMANSHIP, REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100. 2L73 4F RTA3WE 20051221000752005122100075NM 2005 12 21 05FDEA04376 120051219A5520 REPAIR BOEING727 727233 138408ANM ELEVATOR UNDAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25274FE 22039 FOUND PREVIOUSLY INSTALLED REPAIR ON UPPER SURFACE OF LT ELEVATOR WAS ACCOMPLISHED IAW ENGINEERING REPAIR NR 16-0193, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTED OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL THICKNESS AND TYPE, GENERAL WORKMANSHIP, REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100. 2L73 4F RTA3WE 20051221000812005122100081EU 2005 12 21 05FDEA04258 120051212A5710 TRACK AIRBUS310 A310222 3930315EU RT WING WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25450FE 162 RT WING L/E SECTION OB OF TRACK NR 3 HAS 5 WEAR MARKS IN L/E LARGEST .400 IN DIA AND THE DEEPEST .04. ALL WEAR MARKS ARE CIRCULAR AND ARE WITHIN FOUR IN OF EACH OTHER REF N00136. REPLACED SKIN IAW DRW A57244112 AND EA 6-5741-94835. 2L72 4F RTA35EU 20051221000832005122100083NM 2005 12 21 05FDEA04260 120051212A5311 FRAME BOEING727 727227 1384078NM BS 520 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 FWD CARGO BAY FRAME IB FLANGE DENTED AT BS 520, BETWEEN STR 24LT AND STR 25LT. REPAIRED FRAME PER SRM 51-40-3. 2L73 4F A3WE 20051221000852005122100085NM 2005 12 21 05FDEA04262 120051212A5311 FRAME BOEING727 727227 1384078NM BS 720 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 FOUND FWD CARGO BAY FRAME IB FLANGE DENTED AT BS 720, STR 24RT. REPAIRED FRAME AT B.S. 720 STR 24R PER SRM 51-40-3. 2L73 4F A3WE 20051221000872005122100087NM 2005 12 21 DHL2005765511 120051215A5313 STRINGER BOEING727 727264 138408MNM BS 675 CRACKED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15765AT 23014 FOUND FWD PIT STRINGER CRACKED STA 675 S-29L. CUT OUT CRACKED SECTION OF STRINGER AT STA 675 STR 29L. FABRICATED AND INSTALLED REPAIR STRINGER SECTION 20-5/8" FROM BAC1498-132 AND 5" FROM BAC1498-144 IAW B727 SRM 53-10-3 FIG 1. 2L73 4F A3WE 20051221000892005122100089NM 2005 12 21 DHL2005765514 120051207A5347 SEAT TRACK BOEING727 727264 138408MNM BS 870-950 CORRODED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15765AT 23014 FOUND UPPER CARGO COMPT (CABIN) SEAT TRACK BL 48L BS 870 - 950 + 11 CORRODED. CUT OUT CRACKED SECTION OF SEAT TRACK BL 48L S 870 - 950 + 11. FABRICATED AND INSTALLED SEAT TRACK REPAIR 90.85" BY 3.3" FROM BAC1520-792 IAW B727 SRM 53-10-5 FIG 1 2L73 4F A3WE 20051221000912005122100091NM 2005 12 21 05FDEA04244 120051212A5322 SHEAR TIE BOEING727 727227 1384078NM BS 1010 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 FOUND CORROSION ON SHEAR TIE AT BS 1010 RBL 3 WL 148. REPAIRED SHEAR TIE AT BS 1010 RBL 3 WL 148 IAW SRM 53-10-4 FIG 15. 2L73 4F A3WE 20051221000942005122100094NM 2005 12 21 05FDEA04246 120051212A5340 STRINGER CLIP BOEING727 727227 1384078NM BS 540 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 FWD CARGO BAY STR CLIP GOUGED AT BS 540, STR 24LT. REPLACED STRINGER CLIP PER SRM 51-30-2. 2L73 4F A3WE 20051221000972005122100097NM 2005 12 21 05FDEA04248 120051212A5311 FRAME BOEING727 727227 1384078NM BS 720E DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 FOUND STA 720E STR 7R DOUBLE HOLE IN FRAME WEB. REPAIRED FRAME AT BS 720E, STR 7R PER SRM 51-40-3 FIG 1. 2L73 4F A3WE 20051221001012005122100101NM 2005 12 21 AWXA200501530 120051116A575465C267945 SKIN BOEING737 73733A 1384673NM NR 2 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 MCN - DURING C19 CHECK DISCOVERED 3 CRACKS AT FASTENERS LOCATED ON THE NR 2 SLAT BELOW OUTBOARD AUXILIARY TRACK FROM SS 211L TO SS 214L. MAINTENANCE TRIMMED OUT DAMAGED AREA ON THE NR 2 SLAT IAW BOEING 737-300 SRM 57-43-01-2R6. FABRICATED FILLER AND SPLICE PLATE IAW BOEING 737-300 SRM 57-43-01-2R6. INSTALLED FABRICATED REPAIR PARTS ON THE NR 2 SLAT BELOW OUTBOARD AUXILIARY TRACK FROM SS 211L TO SS 214L IAW BOEING 737-300 SRM 57-43-01-2R6. 2L72 4F RTA16WE 20051221001042005122100104NM 2005 12 21 AWXA200501532 120051117A5340693535214 STRINGER CLIP BOEING737 73733A 1384673NM BS 639 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 MCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED STRINGER TIE CLIP CRACKED, .83 INCHES, AT STRINGER 4L AND BS 639. MAINTENANCE REMOVED AND INSTALLED NEW STRINGER CLIP AT 4L AND BS 639 IAW BOEING 737-300 SRM 51-40-02-0G FIG 8 AND FIG 12. 2L72 4F RTA16WE 20051221001122005122100112NM 2005 12 21 AMTA200500939 120051025A3350 LIGHT BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE CABIN INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11520AT 27976 3 FT SECTION OF FLOOR TRACK EGRESS LIGHTING AT (D) LAV INOPERATIVE. REMOVED AND REPLACED LAMPS AS REQUIRED. IAW MM, OPS CHECK GOOD. (K) 2L72 4F4 FRTA2NM E12EU 20051221001152005122100115NM 2005 12 21 AWXA200501540 120051116A575465C26602217SP WEDGE BOEING737 73733A 1384673NM ZONE 500 DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 MCN - DURING C19 CHECK DISCOVERED DISBOND AREA ON THE UPPER AND LOWER SURFACE OF THE NR 2 SLAT WEDGE, OUTBOARD END FROM SS 250.27L TO SS 254.27L. MAINTENANCE CUT OUT DISBOND AREA IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED DOUBLER AND REPAIR CORE FOR UPPER AND LOWER SURFACE IAW BOEING 737-300 SRM 51-70-10-2R4. BONDED REPAIR PARTS TO NR 2 SLAT WEDGE, UPPER AND LOWER SURFACE, FROM SS 250.27L TO SS 254.27L IAW BOEING 737-300 SRM 51-70-10-2R4. 2L72 4F RTA16WE 20051221001182005122100118NM 2005 12 21 AWXA200501542 120051114A57536546431286 SKIN BOEING737 73733A 1384673NM FOREFLAP DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 MCN - DURING C19 CHECK DISCOVERED DISBOND AREA ON THE LOWER SURFACE OF THE RT OUTBOARD FORE FLAP 13 INCHES FROM THE INBOARD END FROM WS 301R TO WS 307.5R. MAINTENANCE CUT OUT DISBOND AREA IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED REPAIR CORE, REPAIR SEPTUM AND REPAIR DOULBER IAW BOEING 737-300 SRM 51-70-10-2R4. BONDED REPAIR PARTS TO LOWER SURFACE OF THE RT OUTBOARD FORE FLAP IAW BOEING 737-300 SRM 51-70-10-2R4. 2L72 4F RTA16WE 20051221001222005122100122NM 2005 12 21 GAIA05027ST 120051027A5330 SKIN BOEING727 727223 1384074NM PWA JT8 JT8D9A 52048NE FUSELAGE CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07854AA 20995 DURING B-CHECK A 1 INCH CRACK WAS FOUND ON THE FUSELAGE SKIN AT STA 530 STRINGER 26R ON THE LAP SEAM BELOW THE C-1 CARGO DOOR. THE SKIN WAS REPAIRED IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L73 4F4 F A3WE E2EA 20051221001272005122100127NM 2005 12 21 AMTA200500925 120051022A2612 FIRE WARNING BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE COCKPIT FALSE ACTIVATIONA AMTAK NONE N FALSE WARNING ININSP/MAINT 1 GL11552TZ 32586 STATUS MSSG L ENG FIRE LP 1, COMPLETED CONTINUITY CHECKS ON LOOP SYSTEM AND SWAPPED P54 CARDS M681 WITH M682. STATUS MSG CLEAR. ALL CHECKS NORMAL IAW WD. (K) 2L72 4F4 FRTA2NM E12EU 20051221001292005122100129SO 2005 12 21 RAIA00512015 120051209A3350 LAMP EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSINOPERATIVE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03836HK 145695 PRE FLIGHT - ORF - OVERHEAD EMERGENCY LIGHT IN GALLEY INOP. MAINTENANCE RELAMPED GALLEY LIGHT. 2L72 4T RTT00011AT 20051221001322005122100132SO 2005 12 21 RAIA00512017 120051213A3350 POWER SUPPLY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSINOPERATIVE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03847HK 14500857 POST FLIGHT - TYS - COCKPIT OVERHEAD EMERGENCY LIGHT OUT AND COCKPIT STERILE LIGHT OUT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY POWER SUPPLY NR 1. 2L72 4T RTT00011AT 20051221001342005122100134SO 2005 12 21 RAIA00512021 120051215A5210 SEAL EMB 145 EMB145LR 3260212SO PAX DOOR DIRTY A RAIAO OTHER O OTHER TXTAXI/GRND HDL 1 CE03847HK 14500857 FLT 8004 - ORD - MAIN DOOR WOULD NOT OPEN FROM INSIDE. MAINTENANCE CLEANED AND LUBED DOOR SEAL. 2L72 4T RTT00011AT 20051221001372005122100137SO 2005 12 21 RAIA00512013 120051208A5210 MECHANISM EMB 145 EMB145LR 3260212SO PAX DOOR LACK OF LUBE A RAIAK NONE W INADEQUATE Q C ININSP/MAINT 1 CE03847HK 14500857 PRE FLIGHT - IAD - MAIN CABIN DOOR HANDLE WOULD NOT MOVE TO 12 O'CLOCK POSITION IN ORDER TO UNLOCK. MAINTENANCE INSPECTED MAIN DOOR AND LUBED FITTINGS WITH ICE RELEASE. CYCLED DOOR SEVERAL TIMES. 2L72 4T RTT00011AT 20051221001392005122100139NM 2005 12 21 CALA0500446 120051217A5315147A56765 FLOORBEAM BOEING737 737724 13844BYNM STA 951 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716709 28779 INSPECTION FOUND FLOOR SUPPORT CORRODED ON SCREW HOLES AT STA 951, LBL 12 TO LBL 46. ALL LOCATIONS OF CORROSION WERE EITHER REPAIRED OR REPLACED IAW SRM 51-10-02 AND GMM 10-900-01 AND 51-40-02. 2L72 4F RTA16WE 20051221001402005122100140NM 2005 12 21 SB05173 120051220A335020131A BATTERY PACK BOEING737 737401 1384701NM EMERGENCY LIGHTSINOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19406US 23876 FORWARD CABIN RIGHT EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK. NO FURTHER FAULTS. 2L72 4F RTA16WE 20051221001432005122100143NM 2005 12 21 CALA0500447 120051219A5320141A8310U31 STRUCTURE BOEING737 737724 13844BYNM STA 312-328 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716709 28779 INSPECTION FOUND R-1 DOOR CUTOUT AREA CHORD CORRODED ON AFT SIDE BETWEEN STA 312 AND 328, RBL 56. A NEW CHORD ANGLE WAS INSTALLED IAW SRM 51-40-02. 2L72 4F RTA16WE 20051221001472005122100147EA 2005 12 21 DIX2005F00000 220051013A7250310240101 TURBINE BLADES BEECH 100 A100 1152915CE PWA PT6 PT6* 52043EA HARTZLHCB4T HCB4TN3 GL NR 2 ENGINE ACTIVATED E DIXAO OTHER X ENGINE FLAMEOUT NRNOT REPORTED 1 SW05324EC1329 B99 PCE38157 EAA1099M NR 2 ENGINE EXPERIENCED AN INTERNAL HOT SECTION FAILURE RESULTING IN COMPLETE LOSS OF POWER AND FLAMEOUT. ALL ENGINE INDICATIONS WERE NORMAL PRIOR TO THE FAILURE. A ROUTINE HOT SECTION BORESCOPE INSPECTION HAD BEEN PERFORMED. 10.2 HOURS PRIOR TO FAILURE. THIS ENGINE IS 340.6 HOURS FROM SCHEDULED 4000 HOUR OVERHAUL. PRELIMIARY INSPECTION REVEALED COMPRESSOR TURBINES BLADES FAILURE IS PROBABLE GAUGE. (K) 1L72 3T3 T A14CE E2NE 6 CP40EA 20051221001512005122100151CE 2005 12 21 GUU2005F00058 120051011A3240MS28775112 O-RING BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE NR 3 BRAKE WORN A GUUAO OTHER K FLUID LOSS NRNOT REPORTED 1 SO1749543 UE181 NO BRAKES AFTER PRESSING THE RT BRAKE PEDAL. REPLACED NR 3 AND 4 BRAKE ASSEMBLIES. UPON BRAKE REMOVAL, DETERMINED NR 3 BRAKE SWIVEL FITTING O-RING TO BE LEAKING. (K) 2L72 4T4 TRTA24CE E26NE 20051221001532005122100153EA 2005 12 21 COMA0560722 120051213A7830 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER LOOSE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01785CA 7326 FLIGHT 5852 - RT THRUST REVERSER WARNING. SECURED CANNON PLUGS ON THE STOW, DEPLOY AND PDU SWITCHES. OPERATIONAL CHECKS NORMAL. 2L72 4F RTA21EA 20051221001562005122100156SO 2005 12 21 XGN2005F00011 220051011A8530ECI712A CYLINDER BEECH 36 36BEECH 1151602CE CONT O520 IO520BA 17032SO ENGINE CRACKED A XGNAK NONE O OTHER ININSP/MAINT 1 SW051194A844 E159 573460R CRACKS FOUND AT THE 50 HOUR INSPECTION. ON GOING PROBLEM WITH THE ECI CYLINDERS. (K) 1L71 3O3 O 3A15 E5CE 20051221001592005122100159SO 2005 12 21 XGN2005F00012 220051011A8530ECI712A CYLINDER BEECH 36 36BEECH 1151602CE CONT O520 IO520BA 17032SO ENGINE CRACKED A XGNAK NONE O OTHER ININSP/MAINT 1 SW051194A844 E159 573460R CRACKS FOUND AT THE 50 HR INSPECTION. ON GOING PROBLEM WITH THE ECI CYLINDERS. (K) 1L71 3O3 O 3A15 E5CE 20051221001612005122100161SO 2005 12 21 XGN2005F00013 220051011A8530ECI712A CYLINDER BEECH 36 36BEECH 1151602CE CONT O520 IO520BA 17032SO ENGINE CRACKED A XGNAK NONE O OTHER ININSP/MAINT 1 SW051194A898 E159 HEADS FOUND CRACKED AT THE 100 HR INSPECTION. 5 OF THE 6 CYLINDERS HAVE BEEN CHANGED IN THE LAST 400 HOURS OF OPERATION. THIS CONTINUES TO BE AN ON GOING PROBLEM. (K) 1L71 3O3 O 3A15 E5CE 20051221001652005122100165EA 2005 12 21 COMA0560724 120051214A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA RT TE FLAPS UNRELIABLE A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01937CA1552811668 7044 FLIGHT 5492 - FLAPS FAIL CAUTION. REPLACED THE RT BPSU AND ALL LT FLAP ACTUATORS. 2L72 4F RTA21EA 20051221001672005122100167EA 2005 12 21 COMA0560728 120051216A5270 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA PAX DOOR FALSE INDICATIONA COMAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO01918CA 7018 FLIGHT 5001- FOUND CABIN DOOR WARNING. OPERATED CABIN DOOR, NO DEFECTS FOUND. 2L72 4F RTA21EA 20051221001692005122100169EA 2005 12 21 COMA0560729 120051217A2752854D10019 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS UNRELIABLE A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01995CA8205 7229 FLIGHT 5399 - FLAPS FAIL CAUTION. REPLACED THE LT NR 4 FLAP ACTUATOR. 2L72 4F RTA21EA 20051221001702005122100170NM 2005 12 21 USAA200512006 120051215A5330 SKIN BOEING737 7373B7 1384580NM BS 860-887 CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19530AU 24412 FOUND 52 INCH LONG BY .018" DEEP CHAFED AREA AT STA 860-887 S2L - S2R. INSTALLED DOUBLER AND AND RIB STRIPS PER EA 97215. 2L72 4F RTA16WE 20051221001712005122100171SO 2005 12 21 XGN2005F00017 220051011A8530 CYLINDER BEECH 33 F33A 1151425CE CONT O520 IO520BA 17032SO ENGINE CRACKED A XGNAK NONE O OTHER ININSP/MAINT 1 SW051096W CE436 807017 THESE CYLINDERS SHOWED TO BE CRACKED IN THE EXHAUST SIDE OF THE HEAD. THE LEAKS SHOWED UP WHEN DOING THE COMPRESSION CHECK. DUE TO THE NR OF CRACKED CYLINDER HEADS, A COMPRESSION CHECK IS DONE EVERY 50 HOURS. (K) 1L71 3O3 O 3A15 E5CE 20051221001722005122100172EA 2005 12 21 COMA0560730 120051216A3260162255 TARGET CNDAIRCL600 CL6002B19 1900309EA NLG BENT A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01712CA 7244 FLIGHT 5463 - NLG WILL NOT RETRACT. NLG CENTERED, PROX SWITCH TARGET BENT. C/W TEMPORARY REPAIR TO PROX SWITCH TARGET. 2L72 4F RTA21EA 20051221001732005122100173EA 2005 12 21 COMA0560717 120051211A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS WARNING LIGHT A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01937CA 7044 FLIGHT 5009 - FLAPS FAIL CAUTION. INSPECTED FLAP SYSTEM PER AD 98-20-01. NO DEFECTS FOUND. 2L72 4F RTA21EA 20051221001752005122100175NM 2005 12 21 QXEA200501787 120051215A2720 SWITCH BOMBDRDHC8 DHC8402 1390042NM RUDDER OUT OF ADJUST A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09404QX 4046 RNO FLIGHT NR 244, RUD 1 POWERED FLIGHT CONTROL SHUTOFF SWITCH LIGHT ILLUMINATED. NR 1 HYDRAULIC PRESSURE WAS NORMAL. MAINTENANCE FOUND LOWER SERVO SPRING STRUT MOTION DETECTOR MICROSWITCH OUT OF ADJUSTMENT. RIGGED LOWER SERVO SPRING STRUT MOTION DETECTOR MICRO SWITCH IAW AMM 27-21-00-830-816. OPS CHECKS GOOD. RUDDER CONTROL SYSTEM OPS CHECKS GOOD IAW AMM 27-20-00-710-802. RII COMPLIED WITH. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051221001772005122100177NM 2005 12 21 QXEA200501791 120051215A2435400SG163Q STARTER GEN BOMBDRDHC8 DHC8402 1390042NM NR 1 MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09415QX535 4081 PDX FLIGHT NR 2351: NR 1 DC GENERATOR CAUTION LIGHT CAME ON DURING T/O. RESET ATTEMPTED PER CHECKLIST. CAUTION LIGHT CAME BACK ON. DEFERRED IAW MEL REF 24-30-6, PLACARD 347182. MAINTENANCE REMOVED AND REPLACED NR 1 DC STARTER/GENERATOR REF Q400 MTC 6243101. OPS CHECK GOOD. CLEARS RSI 347182. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051221001782005122100178EA 2005 12 21 COMA0560719 120051212A2420755469E IDG CNDAIRCL600 CL6002B19 1900309EA LEFT MALFUNCTIONED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01969CA1789810737 7141 FLIGHT 5817- LEFT IDG CAUTION. REPLACED THE IDG. 2L72 4F RTA21EA 20051221001792005122100179EA 2005 12 21 COMA0560720 120051213A27501104SD100401 FLEX COUPLING CNDAIRCL600 CL6002B19 1900309EA TE FLAPS WORN A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01927CA 7031 FLIGHT 5354 - FLAPS FAIL CAUTION. REPLACED THE LT NR 4 FLEX SHAFT. 2L72 4F RTA21EA 20051221001802005122100180 2005 12 21 COMA0560718 220051212A7261 OIL CAP CNDAIRCL600 CL6002B19 1900309EA RT ENGINE LOOSE A COMAA UNSCHED LANDING WK INADEQUATE Q C FLUID LOSS CLCLIMB 1 SO01588SW 7069 FLIGHT 5690 - RT ENGINE OIL PRESSURE WARNING. FOUND OIL FILTER CAP NOT SEATED. REINSTALLED FILTER AND CAP. NO LEAKS FOUND. 2L72 4F RTA21EA 20051221001822005122100182NM 2005 12 21 QXEA200501772 120051209A5410 STIFFENER BOMBDRDHC8 DHC8402 1390042NM LT NACELLE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09403QX 4037 PDX: LT NACELLE FINGERNAIL SUPPORT DECK UPPER SURFACE OB STIFFENER IS DAMAGED APPROX 40" FWD OF AFT END OF DECK. MAINTENANCE PERFORMED A FRESH BLEND WITH CRACK MAPPED FOR ENGINEERING. COMPLIED WITH STEP 1 OF EA 6-54-379. HFEC BLENDED AREA IAW 1-84-7A, PT-6-51-00-02. NO CRACKS NOTED. FABED REPAIR DOUBLER AND INSTALLED REPAIR DOUBLER IAW EA 6-54-379 STEPS 3 AND 4. 2H72 4T RTA13NM 20051221001832005122100183EA 2005 12 21 COMA0560727 120051215A3220 TORQUE LINK CNDAIRCL600 CL6002B19 1900309EA MLG DISCONNECTED A COMAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 SO01495CA 7774 FLIGHT 5095- GEAR DISAGREE WARNING, WOW CAUTION. AFTER LANDING NLG TORQUE LINKS FOUND DISCONNECTED. 2L72 4F RTA21EA 20051221001842005122100184EA 2005 12 21 SIMA200530109 120051025A4990WE38007703 APU CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF34* NE APU BAY LEAKING A SIMAK NONE KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW21514AE4501 4501 10119 ON TAXI TO THE GATE WITH PACKS AND APU ON SMOKE ENTERED THE CABIN AND CREW RECEIVED LAVATORY SMOKE WARNING. FOUND APU LEAKING OIL INTO THE BLEED SYSTEM REPALCED APU. OPS CHECK GOOD. AC RETURNED TO SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20051221001852005122100185NM 2005 12 21 DL76S050764 120051205A2530 COFFEEMAKER BOEING767 767332 1382001NM FWD GALLEY ARCED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27133DN 24982 1RT GALLEY G1A COFFEEMAKER MAKES ELEC ARCING SOUND WHEN TURNED ON. REPLACED SAME. 2L72 4F RTA1NM 20051221001862005122100186NE 2005 12 21 VGC2005F00002 220050901A7200 ENGINE BOEING727 72725C 138400HNM PWA JT8 JT8D7B 52053NE NR 3 FLAMED OUT A VGCAA UNSCHED LANDING X ENGINE FLAMEOUT CRCRUISE 1 GL23261FL 19359 653417 CREW REPORTED NR3 ENG WHILE IN FLIGHT AT FL320, SUSPECTED FUEL ICING (FUEL ICE LIGHT FLICKERING). PERFORMED PROCEDURES AS REQUIRED. AFTER TURNING FUEL HEAT ON 10 SECONDS LATER, NR3 ENGINE FLAMED OUT. CREW PERFORMED ABNORMAL CHECKLIST, RE-STARTED ENGINE. ALL PARAMETERS WERE NORMAL. CREW RETURNED TO DEPARTURE AS REQUESTED MY MAINT CONTROL AFTER CALLING. AFTER AIRCRAFT RETURNED TO DEPARTURE, FUEL SYSTEM WAS INSPECTED IAW ENG MFG TROUBLESHOOTING GUIDE NR 4. INSP FOUND NO FINDINGS OF FUEL CONTAMINATION OF ENGINE OR AIRCRAFT FUEL SYSTEMS. PERFORMED GROUND RUN IAW GUIDE TO TEST FUEL HEAT SYSTEM, FOUND NO FAULTS. RETURNED AIRCRAFT TO SERVICE IAW GUIDE. (K) 2L73 4F4 F A3WE E2EA 20051221001872005122100187CE 2005 12 21 K5L2005F00002 120051111A37101013810009 SHUTOFF VALVE BEECH 200 A200 1152921CE PWA PT6 PT6A41 52043EA COCKPIT FAILED A K5LAK NONE O OTHER TXTAXI/GRND HDL 1 EA05636B 2170 BC61 AFTER NORMAL ENGINE START, DURING RUN UP NOTICED THAT THE LEFT INSTRUMENT SHUTOFF VALVE PN 101381000-9 WOULD NOT CLOSE WHEN SELECTED OFF. FOUND VALVE SOLENOID TO BE AT FAULT AND INSTALLED OVERHAULED VALVE. RUN UP AND OPS CHECKED NORMAL. (K) 1L72 4T4 T A24CE E4EA 20051221001882005122100188 2005 12 21 BSY2005F00003 420051111A3417702490031304 ADC LEAR 35 35LEAR 5170600CE GARRTTTFE731TFE731* 01518WP E/E BAY MALFUNCTIONED E BSYAO OTHER O OTHER CLCLIMB 1 GL071140A 35045 FLIGHT CREW REPORTED THE PILOTS ALTIMETER AND ALTITUDE ALERTER BLANKED OUT DURING CLIMBOUT IN HEAVY RAIN. THE ADC WAS RESEATED IN THE RACK AND THE NR 1 PITOT/STATIC SYSTEM WAS DRAINED. THE PILOTS ALTIMETER SYSTEM WAS TESTED AND INSPECTED AND FOUND TO COMPLY WITH AND REMAIN RVSM COMPLIANT. THERE HAVE BEEN NO PRIOR REPORTS OF PROBLEMS WITH THIS AIRCRAFT. (NOTE: CONCURRENT REPORT ON THIS AC REGARDING THE PILOTS ALTIMETER INDICATOR). (K) 2L72 4F4 F A10CE E6WE 20051221001892005122100189 2005 12 21 BSY2005F00004 420051115A3417702490031304 ADC LEAR 35 35A 5170602CE GARRTTTFE731TFE731* 01518WP E/E BAY CONTAMINATED E BSYAO OTHER O OTHER NRNOT REPORTED 1 GL07279DM 214 FLIGHT CREW REPORTED PILOTS ALTIMETER AND ALTITUDE ALERTER INTERMITTENTLY SWIN FULL SCALE; MODE (C) ON NR 1 TRANSPONDER WAS INTERMITTENT, OVERSPEED AURAL WARNING WAS INTERMITTENTLY ACTIVATING. THE ADC WAS FOUND TO BE DEFECTIVE DUE TO WATER INTRUSION. THE ADC WAS REPLACED AND THE AREAS FOUND TO BE LEAKING WERE REPAIRED. THE SYSTEM WAS TESTED AND INSPECTED AND FOUND TO COMPLY AND TO REMAIN RVSM COMPLIANT. THERE HAVE BEEN ONO PRIOR REPORTS OF PROBLEMS WITH THIS AIRCRAFT. (K) 2L72 4F4 F A10CE E6WE 20051221001912005122100191NM 2005 12 21 AMTA200501061 120051113A3397 WIRE BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE CABIN DISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11522AT 29330 3 EACH EMERGENCY LIGHTS OUT AT D LAV TO SEAT 28D. FOUND WIRES DISCONNECTED ON EGRESS RECONNECTED WIRES. OPS CHECKED GOOD. (K) 2L72 4F4 FRTA2NM E12EU 20051221001922005122100192NM 2005 12 21 AMTA200501057 120051112A2560SG81911 GLOWSTRIP BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE CABIN MISSING A AMTAK NONE O OTHER ININSP/MAINT 1 GL11517AT 27973 SMALL SECTION OF PHOTOLUMINESCENT ESCAPE PATH LIGHT STRIP MISSING AT APPROX ROW 12. INSTALLED PHOTOLUMINESCENT LIGHT STRIP IAW AMM. (K) 2L72 4F4 FRTA2NM E12EU 20051221001942005122100194WP 2005 12 21 LNX2005F00001 220051108A720031025404 ENGINE FRCHLDSA227 SA227CC 3377522SW GARRTTTPE331TPE33111U 01514WP RIGHT UNKNOWN A LNXAC ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 SO29438MA19981 AC721B P44622C AIRCRAFT WAS ON TAKEOFF ROLL FOR DEPARTURE. THE CREW WAS UNABLE TO ACHIEVE TARGET TORQUE ON THE RT ENGINE AND ABORTED THE ROLL. CAUSE OF LOW TORQUE COULD NOT BE ISOLATED TO AN EXTERNAL CAUSE AND THE ENGINE WAS REMOVED AND SENT TO THE VENDOR FOR EVALUATION. ADDITIONAL DATA WILL BE AVAILABLE AND SUBMITTED FOLLOWING TEARDOWN INSP. (K) 2L72 4T4 TRTA18SW E4WE 20051221001952005122100195 2005 12 21 DIX2005F00001 320051031A6111 PROPELLER BEECH 90 C90 1152913CE DAMAGED E DIXAO OTHER O OTHER TXTAXI/GRND HDL 1 SW05925MM LJ925 REPORTING AN ON-GROUND PROPELLER STRIKE INCIDENT THAT OCCURRED ON AIRCRAFT. THE AIRCRAFT WAS ON THE GROUND PERFORMEING PREFLIGHT CHECKS WHEN THE AIRCRAFT ROLLED OFF THE PAVED RUNUP AREA AND THE LT PROP STRUCK AN OBJECT. UPON PRELLIMINARY INSPECTION OF THE PROPELLER, 2 BLADES WILL REQUIRE REPLACEMENT. THE PROP HAS BEEN REMOVED AND FORWARDED TO A REPAIR FACILITY FOR OVERHAUL. THE ENGINE HAS BEEN INSPECTED IAW MM, AND WAS FOUND TO BE SERVICEABLE FOR CONTINUED OPERATION. (K) 1L72 3T 3A20 20051221002072005122100207NM 2005 12 21 AALA20050828 120051207A3350BPS73 BATTERY PACK BOEING757 757223 1384957NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21642AA 24600 AFW - EMERGENCY LIGHT AT STATION 985 LEFT WING FORWARD INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT STATION 985 LEFT WING FORWARD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20051221002092005122100209NM 2005 12 21 AALA20050822 120051215A3350 LIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21755AN 30263 JFK - EMERGENCY AISLE LIGHTS ON BOTH SIDES OF AFT CABIN INOPERATIVE. REPLACED BURNT FUSE IN CHARGER M33401 AND REPLACED SEAT 31G EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20051221002112005122100211WP 2005 12 21 AALA20050832 120051122A3233 ACTUATOR DOUG DC9 DC983 3022083WP RT MLG CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21968TW 53618 TUL - RIGHT HAND MAIN LANDING GEAR SUPPORT FITTING ASSEMBLY RETRACT ACTUATOR FITTING BORE HAS CORROSION. AREA IS 1.75 INCHES BY 2.2515 INCHES. RIGHT HAND MAIN LANDING GEAR SUPPORT FITTING ASSEMBLY RETRACT ACTUATOR FITTING BORE REWORKED IN ACCORDANCE WITH ESO 80559 DATED NOVEMBER 17 2005. 2L72 4F RTA6WE 20051221002132005122100213EU 2005 12 21 KBM2005F00334 120051118A29131502780 SPLINE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE HYDRAULIC PUMP WORN A KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19115SH8930 3141 HYD PUMP, FOUND HYD SPLINE WORN. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051221002142005122100214EU 2005 12 21 KBM2005F00338 120051107A7334S112021090 SWITCH SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1 60030NE FUEL PRESSURE INTERMITTENT E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19215LA17347 2143 FUEL PRESSURE LIGHT INTERMITTENT, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051221002162005122100216 2005 12 21 KBM2005F00342 420051112A34225050010902 GYRO SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1D NE COCKPIT SPINNING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1953SH 3165 2009 DIRECTIONAL GYRO, UNIT SPINS IN FLIGHT, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051221002172005122100217WP 2005 12 21 ABXA050290 120051125A3350 BATTERY PACK DOUG DC9 DC931 3022065WP PWA PT6 PT6A67D NE CABIN DISCHARGED A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23929AX 45874 EMERGENCY EVACUATION LIGHTS WERE INOP. REPLACED BATTERY PACK IAW DC9 MM 3-53-02. OPS CHECKED GOOD. 2L72 4F4 T A6WE E26NE 20051221002182005122100218NM 2005 12 21 SWAA054002 120051217A532065C27314 CLIP BOEING737 7373H4 1384600NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29622SW 27932 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 767, STR 4L. REMOVED AND REPLACED CLIP IAW SRM. 2L72 4F4 FRTA16WE E2GL 20051222000012005122200001NM 2005 12 22 ASAA0580518 120050926A53305924802133 SKIN DOUG MD80 MD83 3023681NM FS 291-293 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - DURING HV CHECK, FOUND DENT IN FUSELAGE. COLD-FORMED SKIN TO ORIGINAL CONTOUR. INSTALLED INTERNAL REPAIR DOUBLER. (M) 2L72 4F RT 20051222000022005122200002NM 2005 12 22 ASAA0580515 120050926A5322991960385 SHEAR TIE DOUG MD80 MD83 3023681NM FS 1231 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - DURING HV-CHECK, FOUND SHEAR TIE CORRODED. REMOVED DAMGAED SECTION. INSTALLED REPLACEMENT SECTION WITH TWO REPAIR SPLICES. (M) 2L72 4F RT 20051222000052005122200005NM 2005 12 22 ASAA0580521 120050926A5523591041449 TAB DOUG MD80 MD83 3023681NM ELEVATOR DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - FOUND DURING HV-CHECK, RIGHT ELEVATOR GEAR TAB UPPER SURFACE HAS DELAMINATION. REMOVED DAMAGED SECTION. INSTALLED SKIN FILLER AND REPAIR DOUBLER. (M) 2L72 4F RT 20051222000062005122200006NM 2005 12 22 ASAA0580523 120050926A5530591214159 ANGLE DOUG MD80 MD83 3023681NM FS 1479-1480 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - DURING HV CHECK, FOUND VERTICAL STABILIZER TO FUSELAGE LEFT ATTACH ANGLE IS CRACKED. REMOVED DAMAGED SECTION. INSTALLED SKIN FILLER AND REPAIR ANGLE. (M) 2L72 4F RT 20051222000072005122200007NM 2005 12 22 ASAA0540523 120051005A5100 REPAIR BOEING737 7374S3 1384711NM FS 960 TEMPORARY A ASAAK NONE O OTHER ININSP/MAINT 1 NM02786AS 24795 YXX - TEMP REPAIR AT STRINGER 25 LEFT BS 837, AFT CARGO DOOR CUTOUT LOWER CORNER. REMOVED AND REPLACED REPAIR WITH PERM REPAIR PER B737-2000 SRM 53-00-01 FIG 201. (M) 2L72 4F RTA16WE 20051222000082005122200008NM 2005 12 22 ASAA0580520 120050926A5330C23AL230007 DOUBLER DOUG MD80 MD83 3023681NM FS 1212-1231 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - DURING HV-CHECK, FOUND ANTENNA DOUBLER CORRODED IN AFT CARGO BAY. REPLACED DOUBLER. (M) 2L72 4F RT 20051222000102005122200010NM 2005 12 22 ASAA05700071 120050921A5320146A75031 FLOOR SUPPORT BOEING737 737790 13844CNNM FS 773 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02623AS 30166 PAE - DURING SI CHECK, FOUND CORROSION ON FLOOR SUPPORT. REPAIRED IAW EA 5310-02493. (M) 2L72 4F RTA16WE 20051222000112005122200011NM 2005 12 22 ASAA0570099 120051024A5320BAC1496444 SUPPORT BOEING737 737790 13844CNNM FS 500 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02624AS 30778 PAE - DURING SI CHECK, FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT. REPAIRED IAW SRM 53-00-53. (M) 2L72 4F RTA16WE 20051222000132005122200013NM 2005 12 22 ASAA0580517 120050926A53229957739101 SHEAR TIE DOUG MD80 MD83 3023681NM FS 1287 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - DURING HV CHECK, FOUND SHEAR TIE CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPLACEMENT SECTION WITH TWO REPAIR SPLICES. (M) 2L72 4F RT 20051222000172005122200017NM 2005 12 22 ASAA05700070 120050921A5320146A75032 FLOOR SUPPORT BOEING737 737790 13844CNNM FS 773 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02623AS 30166 PAE - DURING SI CHECK, FOUND CORROSION ON FLOOR SUPPORT. REPAIRED IAW EA 5310-02493. (M) 2L72 4F RTA16WE 20051222000182005122200018NM 2005 12 22 ASAA05700063 120050921A5320146A75039 FLOOR SUPPORT BOEING737 737790 13844CNNM FS 773 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02623AS 30166 PAE - DURING CHECK, FOUND CORROSION ON FLOOR SUPPORT. REPAIRED IW EA 5310-02493. (M) 2L72 4F RTA16WE 20051222000202005122200020NM 2005 12 22 ASAA0580525 120050926A575559545811 PANEL DOUG MD80 MD83 3023681NM SPOILER GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - DURING HV-CHECK, LEFT INBOARD SPOILER PANEL GOUGED ON UPPER SURFACE AT TRAILING EDGE. REPLACED DAMAGED PLIES. (M) 2L72 4F RT 20051222000222005122200022NM 2005 12 22 ASAA0570090 120051009A5320143A750180 SUPPORT BOEING737 737790 13844CNNM FS 500C CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02615AS 30344 PAE - DURING C-CHECK, FOUND FORWARD CARGO BAY FLOOR TO SIDEALL SUPPORT CORRODED. REPAIRED IAW SRM 51-40-02 AND 53-00-53. (M) 2L72 4F RTA16WE 20051222000252005122200025NM 2005 12 22 ASAA05700062 120050921A5320146A75035 FLOOR SUPPORT BOEING737 737790 13844CNNM FS 773 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02623AS 30166 PAE - DURING CHECK, FOUND CORROSION ON FLOOR SUPPORT. REPAIRED IAW EA 5310-02493. (M) 2L72 4F RTA16WE 20051222000272005122200027NM 2005 12 22 ASAA0570088 120051009A5320143A7501 SUPPORT BOEING737 737790 13844CNNM BS 500B CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02615AS 30344 PAE - DURING C-CHECK, FOUND FLOOR TO SIDEWALL SUPPORT IS CORRODED AT BS 500B. REPAIRED IAW SRM 51-40-02 AND 53-00-53. (M) 2L72 4F RTA16WE 20051222000282005122200028NM 2005 12 22 ASAA0570097 120051009A5320146A75012 FLOOR SUPPORT BOEING737 737790 13844CNNM FS 758-887 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02615AS 30344 PAE - DURING C-CHECK, FOUND CORROSION ON FLOOR SUPPORT AT BS 758. REPAIRED IAW SRM 53-00-53. (M) 2L72 4F RTA16WE 20051222000302005122200030NM 2005 12 22 ASAA0580514 120050926A5320993053812 CUSP WEB DOUG MD80 MD83 3023681NM FS 522-541 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - DURING HV CHECK, FOUND CUSP WEB CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLER AND DOUBLER. (M) 2L72 4F RT 20051222000312005122200031NM 2005 12 22 ASAA0570091 120051009A5210141A61049 STOP FITTING BOEING737 737790 13844CNNM FS 344 CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02615AS 30344 PAE - DURING C-CHECK, FOUND FORWARD ENTRY DOOR AFT LOWER STOP PIN FITTING IS CHAFED. REPLACED DOOR IAW MM 25-10-00. (M) 2L72 4F RTA16WE 20051220002312005122000231NM 2005 12 20 ASAA0540355 120050717A53206547957U3 WEB BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU AFT CARGO BAY CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02706AS 28894 AFT CARGO DOOR OPENING THRESHOLD WEB IS CORRODED. REMOVED AND REPLACED WEB ASSEMBLY IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051220002392005122000239WP 2005 12 20 ASAA0580417 120050805A5320 CUSP WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02947AS 53020 OKC - DURING C-CHECK, FOUND RIGHT CUSP WEB CORRODED. REMOVED CORRODED SECTION. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20051220002412005122000241WP 2005 12 20 ASAA0580421 120050805A5320993061223 CUSP WEB DOUG DC9 DC983 3022083WP FS 1098-1117 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02947AS 53020 OKC - FOUND DURING C-CHECK, RIGHT CUSP WEB CORRODED. REMOVED DAMAGED SECTION. INTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20051220002442005122000244NM 2005 12 20 ASAA0540360 120050713A532069434562 STRAP BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU CARGO BAY CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02797AS 28892 AFT CARGO SUPPORT STRAP THRESHOLD HAS CORROSION. REMOVED AND REPLACED STRAP. (K) 2L72 4F4 FRTA16WE E21EU 20051220002452005122000245NM 2005 12 20 ASAA0540362 120050713A5320654795731 INTERCOSTAL BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02797AS 28892 CORROSION ON INTERCOSTAL. REMOVED, FABRICATED AND REPLACED INTERCOSTAL. (K) 2L72 4F4 FRTA16WE E21EU 20051220002542005122000254WP 2005 12 20 ASAA0580457 120050808A5330593666751 SKIN DOUG DC9 DC982 3022082WP FS 1271 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02935AS 49236 OKC - FOUND DURING C-CHECK, FUSELAGE SKIN IS DENTED. COLD-WORKED DAMAGED AREA. INSTALLED REPAIR DOUBLER. (M) 2L72 4F A6WE 20051220002932005122000293NM 2005 12 20 USAA051560 120051216A5315 FLOORBEAM BOEING737 737301 1384611NM BS 328 LBL4 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19591US 23936 FOUND CORROSION STATION 328 LBL45. ACCOMPLISHED "T" CAP REPAIR IAW SRM 53-10-2R-5, DEFECT SIZE: 2". 2L72 4F RTA16WE 20051220002942005122000294NM 2005 12 20 ASAA0540401 120050816A5311654653024 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 CRACKED FRAME AT BSTA 480 BIN RAIL, STR 8R-9R. REPAIRED IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051220002952005122000295NM 2005 12 20 USAA051561 120051216A5320 ANGLE BOEING737 737301 1384611NM BS 300-359 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19591US 23936 FOUND CORROSION STATION 300-359 LT "Z" ANGLE. ACCOMPLISHED "T" CAP REPAIR DEFECT SIZE: 2" BY 50". 2L72 4F RTA16WE 20051220003052005122000305EU 2005 12 20 USAA051581 120051219A5321F5367111400000 FLOOR PANEL AIRBUS330 A330323 3930335EU FR 14 DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 FOUND DELAMINATEION FS 14. COMPOSITE DOUBLER INSTALLED PER SRM 51-77-11, 53-02-00, DEFECT SIZE: 1" BY 4". 2L72 4F RTA46NM 20051220003142005122000314NM 2005 12 20 ASAA0540409 120050816A53206531787U5 CHANNEL BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 CORROSION ON U-CHANNEL, BSTA 312 - 344, LBL 59, WL 208. REMOVED AND REPLACED IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051220003202005122000320NM 2005 12 20 ASAA0540473 120050916A531165465331 FRAME BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02793AS 28888 BSTA 480, FRAME CRACKED AT BIN RAIL STATION. CUTOUT DAMAGE AT FRAME BIN RAIL SUPPORT AND FABRICATED AND INSTALLED REPAIR IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051220003322005122000332EU 2005 12 20 USAA051569 120051219A5350F5331537420000 FAIRING AIRBUS330 A330323 3930335EU FR 40.2 - 44 RH CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 FOUND CORROSION FS 40.2 - 44 RT AT Y-430. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-42-00 AND 51-72-11, DEFECT SIZE: .50" BY .250" BY .048". 2L72 4F RTA46NM 20051220003342005122000334WP 2005 12 20 UPS05845875 120051215A33506012235 BATTERY PACK DOUG DC8 DC871F 302199DWP EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 NO EMERGENCY EXIT LIGHT. INSTALLED NEW EMERGENCY LIGHT BATTERY PACK CHECKED OK PER 33-50-02-2. 2L74 4F RT4A25 20051220003392005122000339EA 2005 12 20 A6WA200540327 120051115A2710 AILERON CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT & RT UNKNOWN A A6WAO OTHER F FLT CONT AFFECTED DEDESCENT 1 GL31431AW 7256 REQUEST INSPECTION OF RT AND LT AILERONS. THAWED ICE FROM AILERON, INSPECTED SURFACE MOVEMENT AND SURFACES. NO DEFECTS NOTED. (K) 2L72 4F4 FRTA21EA E15NE 20051220003402005122000340EA 2005 12 20 A6WA200540349 120051207A326016215105 BRACKET CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NLG BENT A A6WAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL31434AW 7322 NOSE DOOR WARNING MESSAGE AND GEAR DISAGREE MESSAGE. INSPECTED AND FOUND NOSE GEAR CENTERING/ EXTENDED PROX SENSOR BRACKET BENT. REMOVED AND REPLACED BRACKET IAW CMM. PERFORMED GEAR SWING IAW AMM. OPS CHECK NORMAL. ALL INDICATIONS ARE NORMAL. (K) 2L72 4F4 FRTA21EA E15NE 20051220003422005122000342EA 2005 12 20 A6WA200540344 120051112A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31426AW 7669 LT FS640 BONDED SKIN CRACKED. REPAIRED LT BONDED DOUBLER AT FS 640 BY FABRICATING ANGLE AND INSTALLING BETWEEN STR6L AND 14L. (K) 2L72 4F4 FRTA21EA E15NE 20051220003482005122000348EU 2005 12 20 A6WA200560020 120051203A36106303125 SEAL BAG BAE146BAE146200A 1500266EU LYC ALF502ALF502R5 41580NE NR 4 PYLON LEAKING A A6WAA UNSCHED LANDING J WARNING INDICATION DEDESCENT 1 GL31290UE E2080 RT ZONE HI TEMP CAPTAIN ILLUMINATED ENROUTE IN ICING CONDITIONS. REPLACED SEALS AT NR 4 PYLON LEADING EDGE AND LEAK CHECKED WING ANTI-ICE. OPS CHECKED GOOD. (K) 2H74 4F4 FRTA49EU E6NE 20051220003522005122000352EA 2005 12 20 A6WA200540339 120051113A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE NICKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31426AW 7669 NUMEROUS NICKS IN PAIR AND/OR SKIN ON AFT FUSELAGE RT SIDE FS 589 TO 605 BETWEEN STRINGERS 21R TO 26R. REPAIRED DAMAGED AREA IAW EO BY CUTTING AWAY DAMAGE AND INSTALLING FILLERS AND EXTERNAL DOUBLERS. (K) 2L72 4F4 FRTA21EA E15NE 20051220003642005122000364NM 2005 12 20 2005UALA01446 120051208A3230 LANDING GEAR BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU NLG MALFUNCTIONED A UALAA UNSCHED LANDING O OTHER NRNOT REPORTED 1 WP29314UA 23675 NO INDICATION OF NOSE GEAR COMING UP. CREW SPOKE WITH SAMC, NO POSITIVE RESULT WITH GEAR. SWITCH S845 "NOSE GR DOWN SENSOR" FAILED. REPLACED SWITCH AND PERFORMED OPERATIONAL CHECK (SWUNG GEAR) OF THE GEAR, CHECKS GOOD. 2L72 4F4 FRTA16WE E21EU 20051220003872005122000387NM 2005 12 20 2005UALA01469 120051215A3397 CONNECTOR BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29118UA 28811 AFT GALLEY LEFT HAND AFT WALL EEL LIGHT INOP. SECURED LOOSE CONNECTOR. 2L74 4F4 FRTA20WE E24NE 20051220003882005122000388NM 2005 12 20 2005UALA01470 120051215A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29118UA 28811 LEFT EXTERIOR OVERWING EMERGENCY LIGHT, 3RD LIGHT ASSY FROM FWD, AFT LAMP INOP. RELAMPED. 2L74 4F4 FRTA20WE E24NE 20051220003952005122000395NM 2005 12 20 SWAA053987 120051217A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STR 21L. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20051220004052005122000405NM 2005 12 20 SWAA053997 120051218A534065C27314 STRINGER CLIP BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29511SW 24188 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 344, STR 10R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051220004132005122000413EA 2005 12 20 A6WA200540315 120051024A2760 ECU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 2 FAULTY A A6WAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 GL31459AW 7863 IN LEVEL FLIGHT AT 240, RECEIVED SPOILERON FAULT, ALSO RECEIVED ROLLING MOVEMENT 5-8 DEGREES TO THE RT. AIRCRAFT RETURNED TO NORMAL FLIGHT CHARACTERISTICS, SPOILERON FAULT EXTINGUISHED ON GROUND. REMOVED AND REPLACED SECU NR 2 IAW AMM, OPS CHECCK GOOD AT THIS TIME. (K) 2L72 4F4 FRTA21EA E15NE 20051220004182005122000418EA 2005 12 20 A6WA200540343 120051108A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31426AW 7669 WO 87925, MWC 213, FS484, RBL36 IB ANGLE OF INTERCOSTAL IS CRACKED .5 INCH LONG. REPAIRED CRACKED ANGLE AT FS 484, RBL36 BY REMOVING AND REPLACING ANGLE WITH FABRICATED ANGLE IAW REO. (K) 2L72 4F4 FRTA21EA E15NE 20051220004322005122000432NM 2005 12 20 ASAA0540490 120050919A53206552878106 SILL BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02793AS 28888 CORROSION ON LT MOPSILL. REMOVED AND REPLACED LT MOPSILL AT BSTA 987+ 10 INCHES, LBL 48. (K) 2L72 4F4 FRTA16WE E21EU 20051220004362005122000436NM 2005 12 20 ASAA0540434 120050830A53126546568520 BULKHEAD BOEING737 7374Q8 138447QNM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 CORROSION ON AFT PRESSURE BULKHEAD C-CHANNEL. REMOVED DAMAGED SECTION OF AFT PRESSURE BULKHEAD AND VERTICAL STIFFENER, FABRICATED REPAIR PARTS AND INSTALLED IAW EA. (K) 2L72 4F4 FRTA16WE E2GL 20051221000092005122100009NM 2005 12 21 05FDEA04207 120051209A5347 SEAT TRACK BOEING727 727227 1384078NM BS 620-640 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 FOUND CORROSION, STA 620 - 640 BL 0 WL 208 CORROSION ON SEAT TRACK. STRINGER TO BE REPLACED ON CUST ID N00436 2L73 4F A3WE 20051221000112005122100011NM 2005 12 21 BB05104A 120051214A3397 CONNECTOR BOEING767 767200 1385120NM EMERGENCY LIGHT LOOSE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19646US 23898 FOUND FLOOR ESCAPE PATH LIGHTING INOPERATIVE ON RIGHT SIDE OF CABIN BETWEEN ROWS SIX AND TWELVE. MAINTENANCE RE-ATTACHED ROW 12 LIGHT CONNECTOR. NO FURTHER FAULTS NOTED. 2L72 4F RTA1NM 20051221000132005122100013NM 2005 12 21 EIA23005257 120051208A5730 SKIN BOEING747 747SR46 1384816NM LT WING CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09477EV 20784 DURING "B" CHECK INSPECTION, FOUND CORROSION ON LT WING LOWER SKIN, LOWER FRONT SPAR CHORD, AND FRONT SPAR WEB BETWEEN FSS 1250 AND 1510. REMOVED DAMAGED CHORD AND REPLACED A REPAIR SECTION OF CHORD FROM FSS 1260 TO THE PRODUCTION SPLICE AT FSS 1446.13. REPAIRED LOWER WING PANEL, AND SPLICED IN NEW SECTION OF FRONT SPAR WEB FROM FSS 1284 TO 1318 REPAIRS ACCOMPLISHED PER SRM 57-30-03, FIG 9, SB 747-57-2158, BAC REPAIR DWG 691U0093, AND ECRA 477-57-108-2. 2L74 4F RTA20WE 20051221000162005122100016NM 2005 12 21 EIA2005260 120051212A2797 CONNECTOR BOEING747 747212B 1384886NM AILERON SYS DIRTY A EIAAD RETURN TO BLOCK L NO TEST TXTAXI/GRND HDL 1 NM09486EV 20888 BTB DUE TO FAILURE OF LT OTB AILERON TO WORK DURING PRE-FLIGHT CONTROL CHECK. CLEANED CONTACTS AND RESEATED CANNNON PLUG ON LOCKOUT ACTUATOR PER SWPM CH 20-16-0. OP'S CHK PER 27-11-16, PG 41 OPS CK OK. 2L74 4F A20WE 20051221000182005122100018WP 2005 12 21 05FDEA04368 120051219A5313 LONGERON DOUG DC10 DC1010 3022110WP BS 1978 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25556FE 46710 LOWER FUSELAGE AFT CARGO STA 1978 LONG 49 RT FOUND 1EA CRACK LONG ABOUT 1" ON UPPER FLANGE OF LONGERON. TRIMMED OUT CRACKED PORTION OF LONGERON INSTALLED 2EA FILLERS AND 1EA ANGLE WITH HI LOCKS AND 2EA BOLTS IAW SRM 53-00-01 FIG 9 SHT 7 VOL 1, BOLTS INSTALLED IAW SRM 51-38-01 PAGE 2A AND PAGE 4. 2L73 4F A22WE 20051221000202005122100020NM 2005 12 21 05FDEA04370 120051219A5101 NONE BOEING727 727233 138408ANM NONE NONE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25274FE 22039 FOUND PREVIOUSLY REPAIR INSTALLED AT STA 660, STR 28R TO 28L WAS ACCOMPLISHED IAW SRM 53-30-3, FIG 2, PAGE 9, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTED OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL THICKNESS AND TYPE, GENERAL WORKMANSHIP, REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100. 2L73 4F RTA3WE 20051221000332005122100033NM 2005 12 21 AWXA200501559 120051126A53306545772188 SKIN BOEING737 7373G7 1384595NM BS 727C CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 MCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED SKIN CRACKED, .380 INCHES, AT STRINGER 4R AND BS 727C+11 AT LOWER ROW OF FASTENERS AT LAP SEAM. MAINTENANCE REMOVED DAMAGED AREA IAW BOEING 737-300 SRM 53-00-01-02R30. FABRICATED DOUBLERS, FILLERS AND SPLICE STRAP IAW BOEING 737-300 SRM 53-00-01-02R30. INSTALLED FABRICATED REPAIR PARTS AT STRINGER 4R AND BS 727C+11 IAW BOEING 737-300 SRM 53-00-01-02R30. 2L72 4F RTA16WE 20051221000352005122100035NM 2005 12 21 AWXA200501561 120051104A5315 FLOORBEAM BOEING737 7373G7 1384595NM BS 986 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 MCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED LEVEL 2 GALVANIC CORROSION ON THE TRANSVERSE BEAM AT BS 986, FROM BL 44R TO BL 44L AND WL 208. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-51-1A1. MAINTENANCE CUT OUT DAMAGED AREA FROM BEAM IAW AMERICA WEST AIRLINES ENGINEERING REQUEST 03--53-15-10. FABRICATED REPLACEMENT BEAM IAW AWA ER NR 03-53-15-10. INSTALLED FABRICATED REPAIR PARTS FROM BL 44R TO BL 44L, WL 208 AND BS 986 IAW AWA ER NR 03-53-15-10. 2L72 4F RTA16WE 20051221000362005122100036EU 2005 12 21 AWXA200501562 120051201A5347D5311278220201 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28603AW 661 SAL - MAJOR REPAIR - DURING C6 CHECK DISCOVERED LEVEL 2 CORROSION ON SEAT TRACK LOCATED AT Y-1292 AND FROM FS 16 TO FS 20. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-11-15 FIG 105. MAINTENANCE REMOVED AND INSTALLED NEW SEAT TRACK AT Y-1292 AND FROM FS 12 TO FS 24 IAW AIRBUS 320 SRM 51-42-11. 2L72 4F RTA28NM 20051221000372005122100037EU 2005 12 21 AWXA200501563 120051130A5520 STRUCTURE AIRBUS320 A320232 3930326EU RT ELEVATOR LE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28603AW 661 SAL - MAJOR REPAIR - DURING C6 CHECK DISCOVERED CRACK, 3 INCHES LONG, ON THE RT ELEVATOR LEADING EDGE, OUTBOARD SIDE BETWEEN RIBS 12 AND 13. MAINTENANCE REMOVED DAMAGED AREA IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 26-5529-05349-SS7. APPLIED A LAYER OF GLASS FABRIC AROUND INNER SKIN OF THE RT ELEVATOR IAW AWA ER NR 26-5521-05347-SS7. FABRICATED DOUBLER AND FILLERS IAW AWA ER NR 26-5521-05347-SS7. INSTALLED FABRICATED REPAIR PARTS ON THE RT ELEVATOR LEADING EDGE, OUTBOARD SIDE BETWEEN RIBS 12 AND 13 IAW AWA ER NR 26-5521-05347-SS7. 2L72 4F RTA28NM 20051221000382005122100038NM 2005 12 21 0501766739 120051217A5101 NONE BOEING747 747251F 1384898NM NONE NONE A NWAAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 GL01639US 23887 ABORTED TAKEOFF BECAUSE PILOT FELT SOMETHING WAS WRONG WITH THE RUDDER, BUT IS WAS JUST A STRONG CROSS WIND. NRT MAINTENANCE CHECKED ALL MAIN WHEEL BRAKES AND FOUND OK. RUDDER OPERATION CHECKED OK. NO TROUBLE FOUND, AIRCRAFT RETURNED TO SERVICE. 2L74 4F A20WE 20051221000392005122100039 2005 12 21 0501705811 420051210A2565520007351 CARTRIDGE BOEING757 757351 1384991NM SLIDE INOPERATIVE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01591NW 32991 NR 1 LEFT OVERWING SLIDE SQUIB LIGHT INOP. FOUND SQUIB BLOWN, REPLACED SQUIB AND RETURNED AIRCRAFT TO SERVICE. 2L72 4F RTA2NM 20051221000412005122100041NM 2005 12 21 SWAA054030 120051219A53306545775 SKIN BOEING737 7373Q8 1384670NM BS 847 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 847, BETWEEN STR 23L TO STR 24L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051221000432005122100043NM 2005 12 21 SWAA054032 120051218A53306518420 SKIN BOEING737 7373Q8 1384670NM BS 261 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 261, STR 9L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051221000452005122100045NM 2005 12 21 SWAA054021 120051219A335010107451 SIGN BOEING737 7373H4 1384600NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 LT CABIN EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED EXIT SIGN PER MM. 2L72 4F RTA16WE 20051221000472005122100047NM 2005 12 21 SWAA054023 120051219A53306545778 SKIN BOEING737 7375H4 138449DNM BS 925-927 CHAFED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29511SW 24188 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CHAFED AT DORSAL FIN BLADE SEAL, BETWEEN BS 925 TO BS 927, LBL 9 & RBL 9. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051221000492005122100049NM 2005 12 21 SWAA054025 120051219A53116520723 FRAME BOEING737 7375H4 138449DNM BS 482A CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29511SW 24188 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482A, STR 20L. REPAIRED FRAME PER SWA EA. 2L72 4F RTA16WE 20051221000512005122100051NM 2005 12 21 SWAA054027 120051219A57126545445 RIB BOEING737 7375H4 138449DNM RT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29511SW 24188 DURING SCHEDULED 1/2D CHECK, FOUND RT WING RIB LOWER CHORD CRACKED AT WBL 135.5, BETWEEN STR 2 AND STR 3. REPAIRED RIB PER SRM AND SWA ACO. 2L72 4F RTA16WE 20051221000542005122100054NM 2005 12 21 QXEA200501788 120051216A2750 FLAP SYSTEM BOMBDRDHC8 DHC8402 1390042NM TE FLAPS MALFUNCTIONED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09404QX 4046 RNO FLIGHT NR 2441, FLAP POWER CAUTION LIGHT ILLUMINATED. PULLED AND RESET FLAP CONT CB AT L7 L-ESSENTIAL AS PER CHECKLIST. FLAP POWER CAUTION LIGHT REILLUMINATED WHEN FLAP SELECTOR MOVED TO NEW POSITION. MAINTENANCE CLEARED NVM, COMPLIED WITH S/L. RESET Q400-SL-005A. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051221000702005122100070EA 2005 12 21 ASOA05943 120051102A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27852AS 7369 DURING AN A-CHECK, THE RT SIDE ENGINE SUPPORT BEAM, AT BL36.20, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REPAIR THE RT SIDE ENGINE SUPPORT BEAM, AT BL 36.20, IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20051221000982005122100098EA 2005 12 21 ASOA05947 120051103A5210 DOOR CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE PAX DOOR MALFUNCTIONED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27720EV 10115 DURING A GROUND INSPECTION, THE PASSENGER DOOR WAS DIFFICULT TO CLOSE AND FELL RAPIDLY AFTER OPENING. MAINTENANCE PERFORMED AN OPERATIONAL CHECK ON THE PASSENGER DOOR. NO DEFECTS NOTED PASSENGER DOOR OPERATED NORMALLY. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA EOOO63EN 20051221001052005122100105EA 2005 12 21 ASOA05893 120051017A25602618 FLASHLIGHT CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27712EV 10074 DURING A C-CHECK, THE FLASHLIGHT AT ROW 19, SEATS A AND B, WAS FOUND TO BE INOPERATIVE. MAINT REMOVED AND REPLACED THE FLASHLIGHT AT ROW 19, SEATS A AND B. (K) 2L72 4F4 FRTA21EA EOOO63EN 20051221001072005122100107NM 2005 12 21 AWXA200501534 120051117A5340693535214 STRINGER CLIP BOEING737 73733A 1384673NM BS 616 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 MCN - DURING C19 CHECK DISCOVERED STRINGER TIE CLIP CRACKED, 1.02 INCHES, AT STRINGER 4L AND BS 616. MAINTENANCE REMOVED AND INSTALLED NEW STRINGER TIE CLIP AT 4L AND BS 616 IAW BOEING 737-300 SRM 51-40-02-0G FIG 8 AND FIG 12. 2L72 4F RTA16WE 20051221001102005122100110NM 2005 12 21 AWXA200501536 120051116A53206545834551 CHANNEL BOEING737 73733A 1384673NM BS 327 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 MCN - DURING C19 CHECK DISCOVERED CHANNEL CRACKED, .97 INCHES, AT BS 327, BL 48L AND WL 208. MAINTENANCE REMOVED AND INSTALLED NEW CHANNEL AT BS 327, BL 48L AND WL 208 IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 4, 8 AND 12. 2L72 4F RTA16WE 20051221001132005122100113NM 2005 12 21 AWXA200501538 120051116A53206545834107 STRAP BOEING737 73733A 1384673NM FLOORBEAM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 MCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED CRACK, .66 INCHES, ON THE LOWER FLOOR BEAM STRAP AT BS 312, WL 200 AND BL 26R. MAINTENANCE REMOVED AND INSTALLED NEW STRAP AT BS 312, WL 200 AND BL 26R IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 3, 4, 8 AND 12. 2L72 4F RTA16WE 20051221001172005122100117NM 2005 12 21 AWXA200501541 120051116A575465C2660399 WEDGE BOEING737 73733A 1384673NM ZONE 500 DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 MCN - DURING C19 CHECK DISCOVERED DISBOND AREA ON THE LOWER SURFACE OF THE NR 3 SLAT WEDGE, FROM SS 102L TO SS 111L. MAINTENANCE CUT OUT DISBOND AREA IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED DOUBLER AND REPAIR CORE IAW BOEING 737-300 SRM 51-70-10-2R4. BONDED REPAIR PARTS TO NO 3 SLAT WEDGE, LOWER SURFACE, FROM SS 102L TO SS 111L IAW BOEING 737-300 SRM 51-70-10-2R4. 2L72 4F RTA16WE 20051221001212005122100121EA 2005 12 21 COMA0560725 120051215A2916601R751113 RESERVOIR CNDAIRCL600 CL6002B19 1900309EA NR 3 HYD SYSTEM MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01809CA15367 7366 FLIGHT 5299 - GEAR DISAGREE WARNING. REPLACED THE NR 3 HYDRAULIC SYSTEM RESERVOIR. 2L72 4F RTA21EA 20051221001242005122100124NM 2005 12 21 CALA0500438 120051213A3350D71702001 CHARGER BOEING767 767424ER 1385270NM BS 522 INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2766057 29452 THE EMERGENCY LIGHT BATTERY FAILED TEST PER W/C 64-3350-1-3800. THE BATTERY PACK AND CHARGER WERE REMOVED AND REPLACED IAW MM 33-51-07. 2L72 4F RTA1NM 20051221001252005122100125NM 2005 12 21 GAIA05028ST 120051027A5711 SPAR BOEING727 727223 1384074NM PWA JT8 JT8D9A 52048NE CENTER WING CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07854AA 20995 DURING B-CHECK A FUEL LEAK WAS FOUND ON THE FUSELAGE AT STA 740. INSPECTION REVEALED A CRACK ON THE WING CENTER SECTION SPAR WEB. THE WING SPAR WEB WAS REPAIRED IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L73 4F4 F A3WE E2EA 20051221001302005122100130NM 2005 12 21 AMTA200500924 120051023A2612 FIRE WARNING BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE COCKPIT FALSE ACTIVATIONA AMTAK NONE N FALSE WARNING CRCRUISE 1 GL11552TZ 32586 L ENG FIRE LP 1 DISPLAYED. PERFORMED FIM TASK AND VISUALLY EXAMINED LT ENG FIRE LOOPS/HARNESSES WITH NO DEFECTS NOTED. AS PRECAUTION REMOVED AND REPLACED FIRE/OVERHEAT CARD M 10224 IAW MM. OPS CHECK GOOD. (K) 2L72 4F4 FRTA2NM E12EU 20051221001412005122100141EA 2005 12 21 TIM2005F00006 220050820A7210310074802 REPAIR BEECH 99 C99 1154006CE PWA PT6 PT6* 52043EA RDUCTION GEARBOXFAILED E TIMAO OTHER K FLUID LOSS NRNOT REPORTED 1 NM07238AL2742491 U238 A REPAIR BY MFG ON A HOLE IN THE REDUCTION GEARBOX REAR HOUSING FAILED. THE FAILURE ALLOWED OIL TO LEAK IN TO THE COMBUSTION SECTION OF THE ENGINE. (K) 1L72 3T3 T A14CE E2NE 20051221001492005122100149EU 2005 12 21 SDR2005069 120051022A275146797648010 INDICATOR AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE COCKPIT FAULTY A TRBAO OTHER N FALSE WARNING LDLANDING 1 SO29355AT 355 ON SHORT FINAL, FLAPS EXTENSION FLAG REMAINED OUT AND FLAPS DID NOT LOCK AT 30 DEGREES. EMERGENCY DECLARED. AIRCRAFT LANDED WITH 15 DEGREES OF FLAPS. REPLACED FLAP INDICATOR. (K) 2H72 4T4 TRTA53EU E20NE 20051221001682005122100168SO 2005 12 21 XGN2005F00016 220051011A8530ECI712A CYLINDER BEECH 33 F33A 1151425CE CONT O520 IO520BA 17032SO ENGINE CRACKED A XGNAK NONE O OTHER ININSP/MAINT 1 SW051096W1147 CE436 807017 THESE CYLINDERS SHOWED TO BE CRACKED IN THE EXHAUST SIDE OF THE HEAD. THE LEAKS SHOWED UP WHEN DOING THE COMPRESSION CHECK. DUE TO THE NR OF CRACKED CYLINDER HEADS. DO A COMPRESSION CHECK EVERY 50 HOURS. (K) 1L71 3O3 O 3A15 E5CE 20051221001962005122100196SW 2005 12 21 BAQ2005F00003 120051118A6220430010100109 YOKE BELL 430 430 1182150SW MAIN ROTOR CRACKED E BAQAK NONE O OTHER ININSP/MAINT 1 GL23431UM 49040 MAIN ROTOR YOKE ASSY FOUND CRACKED WHILE COMPLYING WITH REQUIRED INSP WHENEVER MAIN ROTOR BLADES ARE REMOVED. (K) 1G72 3U RTH9SW 20051221001982005122100198SO 2005 12 21 MK92005F00001 120051101A7330 INDICATION SYS PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2A GL FUELL SYSTEM MALFUNCTIONED E MK9AA UNSCHED LANDING O OTHER CLCLIMB 1 WP133587C 318052118 L67661A DJ8479A SHORTLY AFTER TAKEOFF, PILOT SAW A DROP IN INDICATED FUEL FLOW. EMERGENCY PUMP WAS SELECTED AND PILOT RETURNED TO AIRPORT. MAINTENANCE WAS CONTACTED AND AN INVESTIGATION WAS INITIATED. NO DISCREPANCIES OF MALFUNCTIONS COULD BE FOUND IN ANY COMPONENT OF THE FUEL SYSTEM. AC WAS TEST FLOWN AND RETURNED TO SERVICE. NO MALFUNCTIONS HAVE BEEN REPORTED TO DATE. (K) 1L72 3O3 O A20SO E14EA 5 CP33EA 20051221002012005122100201NE 2005 12 21 AALA20050813 220051211A7230 COMPRESSOR DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE RT ENGINE STALLED A AALAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS CRCRUISE 1 SW21905TW 49157 708581 STL - AT FL280 RIGHT ENGINE COMPRESSOR STALLED. OPERATED ENGINE AT IDLE AND LANDED STL WITHOUT INCIDENT. REPLACED RIGHT HAND ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 F A6WE E9NE 20051221002032005122100203NM 2005 12 21 AALA20050815 120051212A33508039001 BATTERY PACK BOEING757 7572Q8 1384972NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21704X 28163 LGA - EMERGENCY LIGHTS IN AFT TAIL COMPARTMENT INOPERATIVE. REPLACE BATTERY PACK AND REPAIRED BROKEN WIRE FOR EMERGENCY LIGHTS IN AFT TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20051221002052005122100205WP 2005 12 21 AALA20050817 120051213A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW217514A 49891 DTW - OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051221002152005122100215 2005 12 21 KBM2005F00339 420051117A34225050031904 GYRO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE COCKPIT DEFECTIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV4930 3296 UNIT FLAG WILL NOT RETRACT. MEL AIRCRAFT DUE. (K) 1G71 3U3 U H9EU E19EU 20051222000092005122200009NM 2005 12 22 ASAA0580522 120050926A5523593049712 TAB DOUG MD80 MD83 3023681NM ELEVATOR DELAMINATED A ASAAO OTHER O OTHER NRNOT REPORTED 1 NM02982AS 53473 OKC - DURING HV CHECK, FOUND RIGHT ELEVATOR ANTI-FLOAT TAB LOWER SURFACE IS DELAMINATED. REMOVED DAMAGED SECTION. INSTALLED SKIN FILLER AND REPAIR DOUBLER. (M) 2L72 4F RT 20051222000122005122200012NM 2005 12 22 ASAA0510338 120051004A533065737421 SKIN BOEING737 737298C 1384490NM FS 980 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02745AS 20794 YXX - FOUND FUSELAGE SKIN INSIDE SURFACE CORRODED AT BS 980 BETWEEN STRINGER 27 LEFT AND 27 RIGHT. REPAIRED IAW B737-200 SRM 53-30-3 FIGURE 5. (M) 2L72 4F RTA16WE 20051222000162005122200016NM 2005 12 22 ASAA0510337 120051004A53116520722509 FRAME BOEING737 737298C 1384490NM FS 440 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02745AS 20794 YXX - FOUND FORWARD CARGO PIT, MAIN FRAME FOUND CORRODED AT BS 440 AND STRINGER 26 RT. FORWARD CARGO PIT MAIN FRAME AT BS 440 AND 28 RT REPAIRED IAW B737-200 SRM 51-10-01 PARAGRAPH 8. (M) 2L72 4F RTA16WE 20051222000212005122200021NM 2005 12 22 ASAA0570089 120051009A5320146A94014 PLATE BOEING737 737790 13844CNNM FS 267 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02615AS 30344 PAE - DURING C-CHECK, FOUND CORROSION ON FLOOR PANEL SPLICE PLATE. REPAIRED IAW SRM 51-40-02 AND 53-00-53. (M) 2L72 4F RTA16WE 20051222000322005122200032NM 2005 12 22 ASAA0570109 120051026A5330144A3111 REPAIR BOEING737 737790 13844CNNM FS 650 TEMPORARY A ASAAK NONE O OTHER ININSP/MAINT 1 NM02626AS 30793 PAE - DURING DAILY CHECK, FOUND BLIND REPAIR FASTENERS ON TEMP REPAIR AT BS 650 WERE APPROACHING TIME LIMITS AND WOULD EXCEED TIME LIMITS BEFORE PERMANENT REPAIR IS TO BE ACCOMPLISHED AND FUSELAGE SKIN DAMAGED/CRACKED AT STATION 650 IN CROWN AREA AT STRINGER 1 AND STRINGER 2R. REPAIRED IAW SRM 53-00-01 REPAIR NR 3. (M) 2L72 4F RTA16WE 20051222000352005122200035NM 2005 12 22 ASAA0580516 120050926A5322991960443 SHEAR TIE DOUG MD80 MD83 3023681NM FS 1250 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - DURING HV CHECK, FOUND SHEAR TIE CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPLACEMENT SECTION WITH TWO REPAIR SPLICES. (M) 2L72 4F RT 20051222000372005122200037NM 2005 12 22 ASAA0580524 120050926A57535935966506 WEDGE DOUG MD80 MD83 3023681NM TE FLAPS CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - DURING HV-CHECK, FOUND RIGHT INBOARD FLAP INBOARD WEDGE TRAILING EDGE IS CRACKED. REMOVED DAMAGED SECTION. INSTALLED VACUUM CURED SPLICE. (M) 2L72 4F RT 20051222000422005122200042SO 2005 12 22 C2XA05IA144 120051219A32608005701 PROXIMITY SENSOR EMB 145 EMB145XR 3260214SO NLG INOPERATIVE A C2XAO OTHER J WARNING INDICATION CLCLIMB 1 SW27141713392 3392 14500859 DEN - FLIGHT 2187, THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL AFTER TAKEOFF. THE AIRCRAFT DIVERTED TO DEN WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE WEIGHT ON WHEELS PROX SWITCH ON THE NLG, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20051222000432005122200043SO 2005 12 22 C2XA05IA141 120051212A33502013BR BATTERY PACK EMB 145 EMB145 3260210SO EMERGENCY LIGHT DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW27149605687 783 145100 IAH - DURING MAINTENANCE INSPECTION SEVERAL EMERGENCY LIGHT STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE AND FOUR EMERGENCY LIGHT BATTERY PACKS, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20051222000442005122200044SO 2005 12 22 C2XA05CL100 120051215A2910AE71379019 HOSE EMB 145 EMB145LR 3260212SO NR 2 ENG HYD SYSFAILED A C2XAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW2712921 145354 CLE FLIGHT 2974 THE CREW REPORTED A HYDRAULIC SYSTEM 2 FAIL IN FLIGHT. THE FLIGHT DIVERTED INTO SYR AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE HYDRAULIC PUMP HOSE. THE SYSTEM WAS SERVICED AND OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20051222000472005122200047EA 2005 12 22 COMA0560739 120051219A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE TE FLAPS OUT OF SEQUENCE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01783CA 7315 EN ROUTE, DURING CLIMB, RECEIVED A FLAP FAIL CAUTION MESSAGE AT 20 DEGREES. CREW DECLARED AN EMERGENCY AND DIVERTED. FLIGHT LANDED WITHOUT INCIDENT. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE (FIRST EVENT) MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2L72 4F4 FRTA21EA E15NE 20051222000482005122200048 2005 12 22 SWAA054034 420051220A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20051222000492005122200049 2005 12 22 SWAA054035 420051219A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29331SW 23695 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20051222000532005122200053NM 2005 12 22 SWAA054039 120051219A335065C27093 LIGHT BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29392SW 27379 L1 DOOR EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT PER MM. 2L72 4F RTA16WE 20051222000542005122200054 2005 12 22 SWAA054040 420051219A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29394SW 27380 DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051222000552005122200055 2005 12 22 SWAA054041 420051216A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29397SW 27691 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051222000572005122200057NM 2005 12 22 SWAA054043 120051220A532269353656 SHEAR TIE BOEING737 7375H4 138449DNM BS 360 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29501SW 24178 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 360, STR 14R. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051222000582005122200058NM 2005 12 22 SWAA054044 120051219A53306545765 SKIN BOEING737 7375H4 138449DNM BS 498A-500A CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29511SW 24188 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 498A TO BS 500A, STR 12L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051222000602005122200060EA 2005 12 22 COMA0560736 120051218A3010434419883 OVERHEAT SENSOR CNDAIRCL600 CL6002B19 1900309EA LT WING ANTI ICEMALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01409CA 7441 FLIGHT 5021 - WING ANTI-ICE WARNING. REPLACED THE LT WING ANTI-ICE OVERHEAT SWITCH. 2L72 4F RTA21EA 20051222000612005122200061NM 2005 12 22 AALA20050835 120051129A5314 KEELBEAM BOEING757 757223 1384957NM BS 1176 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21663AM 25297 TUL - KEEL BEAM WEB HAS HEAVY CORROSION INSIDE LEFT WHEEL WELL AT STATION 1176. REMOVED DAMAGED AREAS AND FABRICATED DOUBLER, FILLERS, AND SPLICES. REPAIRED PER 757AARD AND ESO 90309 DATED 11-29-2005. 2L72 4F RTA2NM 20051222000622005122200062WP 2005 12 22 AALA20050826 120051219A3213CDK1473501 STRUT DOUG DC9 DC983 3022083WP NLG INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21961TW 53611 ORD - THE NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. REPLACED NOSE LANDING GEAR STRUT SEALS AND SERVICED NOSE LANDING GEAR STRUT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20051222000652005122200065WP 2005 12 22 AALA20050812 120051210A33508029001 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW2133414 49325 SFO - SEAT MOUNTED EMERGENCY LIGHTS FROM 21D TO AFT CABIN INOPERATIVE. REPLACED AFT BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS FROM 21D TO AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051222000662005122200066WP 2005 12 22 AALA20050818 120051213A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21461AA 49566 LGA - CEILING EMERGENCY LIGHTS AT AFT DOOR INOPERATIVE. CLEANED AND ADJUSTED CONTACTS ON BATTERY PACKS FOR CEILING EMERGENCY LIGHTS AT AFT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051222000682005122200068NM 2005 12 22 AALA20050820 120051214A3350 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21697AN 26977 MIA - EMERGENCY LIGHTS FROM SEAT 9D TO 15D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FROM SEAT 9D TO 15D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20051222000692005122200069 2005 12 22 2005UALA01475 420051215A2565D31393110 SLIDE 60493101 BOEING757 757222 1384956NM PWA 2037 PW2037 NE ASPIRATOR UNSERVICEABLE A UALAK NONE O OTHER ININSP/MAINT 1 WP29538UA 0519 25222 ASPIRATOR VALVES LEAKING. SLIDE WAS REMOVED FROM AIRCRAFT AT NORMAL MAINTENANCE INTERVAL. ASPIRATOR FLAPPER VALVE WAS OBSERVED LEAKING DURING SLIDE OVERHAUL AIR RETENTION TEST. SPECIFIC CAUSE OF LEAK WAS NOT DETERMINED. ASPIRATOR WAS REPLACED. 2L72 4F4 FRTA2NM E17NE 20051222000702005122200070SO 2005 12 22 C2XA05SH136 120051209A531214526850401 FIREWALL EMB 145 EMB145EP 3260221SO FUSELAGE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712946 145052 SHV - DURING C-CHECK AFT SURFACE OF FR 81 IS CHAFED IN MUTIPLE LOCATION ON LOWER EDGE. MAINTENANCE REPAIRED AFT SURFACED OF FR 81 ON LOWER EDGE IAW EMB 145 EC5310-01359. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2L72 4F RTT00011AT 20051222000712005122200071SO 2005 12 22 C2XA05SH137 120051209A532014530644403 FLOOR SUPPORT EMB 145 EMB145EP 3260221SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712946 145052 SHV - DURING C-CHECK THE LT OMEGA BEAM AT FR 45 HAS CORROSION. MAINTENANCE REPAIRED LT OMEGA BEAM AT FR 45 IAW EC5320-01276. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2L72 4F RTT00011AT 20051222000732005122200073NM 2005 12 22 2005UALA01262 120051111A33501317 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29182UA 25279 EMERGENCY LIGHT INOP DR2 LT ENTRY CEILING. *S/D* REPLACED LAMP EMERGENCY LIGHT. 2L74 4F4 FRTA20WE E24NE 20051222000742005122200074SO 2005 12 22 C2XA05SH138 120051209A532014530645403 FLOOR SUPPORT EMB 145 EMB145EP 3260221SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712946 145052 SHV - DURING C-CHECK, THE CENTER OMEGA BEAM HAS CORROSION AT FR 45. MAINTENANCE REPAIRED CENTER OMEGA BEAM @ FR 45 IAW EC5320-01276. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2L72 4F RTT00011AT 20051222000762005122200076 2005 12 22 2005UALA01477 420051215A2565D31393110 SLIDE BOEING757 757222 1384956NM PWA 2037 PW2037 NE BOTTOM TUBE UNSERVICEABLE A UALAK NONE O OTHER ININSP/MAINT 1 WP29538UA 25222 BOTTOM INFLATION TUBE HAS A HOLE IN EXCESS OF 1 INCH WHICH WOULD NOT PASS AR TEST. SLIDE WAS REMOVED FROM AIRCRAFT AT NORMAL MAINTENANCE INTERVAL. SLIDE FAILED AIR RETENTION TEST DUE TO HOLE IN INFLATABLE LOWER TUBE. IT WAS OBSERVED THAT SLIDE HAD BEEN PACKED CORRECTLY. EXACT CAUSE OF THE WEAR DAMAGE COULD NOT BE DETERMINED. DAMAGE WAS REPAIRED BY PATCHING PER AIR CRUISERS CMM 25-60-46. 2L72 4F4 FRTA2NM E17NE 20051222000772005122200077NE 2005 12 22 AALA20050825 220051218A7200 ENGINE BOEING757 757223 1384957NM RROYCERB211 RB211535E4 54555NE LEFT STALLED A AALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 SW21645AA 24603 31058 MIA - DURING CLIMBOUT LEFT ENGINE VIBRATION INDICATED 3.4 ON N3. PULLED THROTTLE BACK AND CAUTION INDICATION WENT OUT. AFTER ADVANCING THROTTLE LEFT ENGINE EXPERIENCED A COMPERSSOR STALL. PULLED THROTTLE BACK AND LEFT ENGINE STABILIZED AND OPERATIVE NORMALLY AT THE REDUCED POWER SETTING. REPLACED NUMBER ONE ENGINE AT MIA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA2NM E12EU 20051222000782005122200078WP 2005 12 22 AALA20050831 120051122A5343 BUSHING DOUG DC9 DC983 3022083WP MLG SUPPORT BEAMCORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21968TW 53618 TUL - MAIN LANDING GEAR SUPPORT BEAM RIGHT HAND RETRACT BUSHING INBOARD BUSHING OUTBOARD FACE HAS MINOR CORROSION. AREA IS 2.13 INCHES BY 2.13 INCHES WITH A DEPTH OF .025. ORIGINAL THICKNESS 1.235 INCHES. FINAL THICKNESS 1.210 INCHES. RIGHT HAND MAIN LANDING GEAR RETRACT BUSHING AREA REWORKED IN ACCORDANCE WITH ESO 80559 DATED NOVEMBER 17 2005. 2L72 4F RTA6WE 20051222000792005122200079EU 2005 12 22 USAA051601 120051220A5347F5332655220300 SEAT TRACK AIRBUS330 A330323 3930335EU -Y2462 FR 53.9 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 Y2462 FR 53.9 CORRODED. BLENDED & REPLACED NEW SEAT TRACK PER SRM 51-72-11, 51-74-00, 51-31-15, DEFECT SIZE: .500 X .300 X .070 INCH. 2L72 4F RTA46NM 20051222000822005122200082NM 2005 12 22 USAA051588 120051220A5311 FRAME BOEING737 7374B7 1384702NM BS 601 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 STA 601 LEF TR SIDE ON INNER CORD ANGLE JUST BELOW CABIN FLOOR LEVEL CRACKED. REMOVED DAMAGED METAL, INSTALLED FILLER & REPAIR ANGLE IAW EA 97193, DEFECT SIZE: 1.5 INCH CRACK. 2L72 4F RTA16WE 20051222000852005122200085NM 2005 12 22 USAA051591 120051220A5330202473 SKIN BOEING737 7373B7 1384580NM BS 860-887 CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19530AU 24412 UNDER DORSAL FIN, STA 860-887 S2L-S2R CHAFED. INSTALLED REPAIR DOUBLER, TRIPLER & FILLERS IAW EA 97215, SRM 53-60-01, EO 5304V147, DEFECT SIZE: 52 INCH LINEAR CHAFING, .018 INCH DEPTH MAX. 2L72 4F RTA16WE 20051222000862005122200086NM 2005 12 22 USAA051592 120051220A53201128323 PANEL BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 CORROSION ON WEB PANEL UNDER AFT CARGO DOOR SCUFF PLATE. PART REPLACED WITH IDENTICAL PART REPLACED WEB IAW SRM 53-60-51, DEFECT SIZE: SHEETMETAL 3999 CORROSION ON WEB PANEL UNDER SCUFF PLATE TOP & BOTTOM 2 X 1 INCH. 2L72 4F RTA16WE 20051222000872005122200087NM 2005 12 22 USAA051593 120051220A5343 FITTING BOEING737 737301 1384611NM MLG SUPPORT BEAMCORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19591US 23936 MLG SUPPORT BEAM FITTING ASSY HAS FRETTING ON FWD INBOARD AREA AT STABILIZER. REPAIRED, SMALL BLEND OUT, DEFECT SIZE: SMALL 1 INCH AREA OF CORROSION. 2L72 4F RTA16WE 20051222000882005122200088NM 2005 12 22 USAA051594 120051220A5311 FRAME BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19591US 23936 FWD SERVICE DOOR CUTOUT FWD FRAME CRACKED AT UPPER STOP FITTING LOWER O/B CORNER. REPLACED FRAME SECTION IAW SRM 51-30, DEFECT SIZE: .25 INCH LONG CRACK. 2L72 4F RTA16WE 20051222000892005122200089NM 2005 12 22 USAA051595 120051220A5311 FRAME BOEING737 737301 1384611NM BS 706 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19591US 23936 STA 706 FRAME WEB S9R AT I/B RIVET SECURING A/C PSU SUPPORT CRACKED. INSTALLED DOUBLER IAW TYPICAL REPAIR 53-10-22, DEFECT SIZE: .1875 INCH. 2L72 4F RTA16WE 20051222000912005122200091NM 2005 12 22 USAA051597 120051220A5311 FRAME BOEING737 7374B7 1384702NM BS 600 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19781AU 25020 FUSELAGE STA 600, BETWEEN S17L TO S18L CRACKED. INSTALLED FAB FILLER AND STIFFENER PER TYP REPAIR 53-62-01, SRM 51-40-02, DEFECT SIZE: .5 INCH CRACK. 2L72 4F RTA16WE 20051222000932005122200093EU 2005 12 22 USAA051607 120051220A5347F53311325200 SEAT TRACK AIRBUS330 A330323 3930335EU FR 49.5 Y450 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 FR 49.5 Y450 CORRODED. BLENDED OUT PER 51-74-00, TRACK REPLACED PER 53-31-15, DEFECT SIZE: .5 X .5 X .010 INCH AREA. 2L72 4F RTA46NM 20051222000942005122200094EU 2005 12 22 USAA051614 120051220A5347F57110568205 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 SEAT TRACK - Y450 FR 40 CORRODED. BLEND AREA PER SRM 51-74-00; TRACK REPLACED PER SRM 53-31-15, 51-72-11, DEFECT SIZE: 3 X 1 INCH. 2L72 4F RTA46NM 20051222000952005122200095EU 2005 12 22 USAA051613 120051220A5347F57110568205 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 SEAT TRACK - Y450 FR 42-43 CORRODED. BLEND AREA PER SRM 51-74-00, TRACK REPLACED PER 53-31-15, 51-72-11; CORR LEVEL 1; TASK C53317001, DEFECT SIZE: 3 X 1 INCH. 2L72 4F RTA46NM 20051222001042005122200104EU 2005 12 22 USAA051603 120051220A5330F5331709120100 SKIN AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 FLANGE (LOWER FUSELAGE) ZONE 150 FR 53.2, STR 49-46 RT CORRODED. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-42-11, DEFECT SIZE: .25 INCH AREA 4 PLACES. 2L72 4F RTA46NM 20051222001082005122200108EA 2005 12 22 COMA0560734 120051218A3220 LANDING GEAR CNDAIRCL600 CL6002B19 1900309EA NOSE WARNING LIGHT A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01931CA 7037 FLIGHT 5113 - NWS CAUTION MESSAGE. INSPECTED NLG AND STEERING SYSTEM, OPERATIONAL CHECK SATISFACTORY, NO FAULTS IN COMPUTER. 2L72 4F RTA21EA 20051222001102005122200110NM 2005 12 22 SWAA054046 120051220A53116546558 FRAME BOEING737 7373H4 1384600NM BS 907 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29622SW 27932 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051222001122005122200112NM 2005 12 22 SWAA054048 120051220A53116520722 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29622SW 27932 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, FWD FRAME NR 5 STOP FITTING. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20051222001132005122200113EA 2005 12 22 COMA0560733 120051217A2750855S10011 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS UNRELIABLE A COMAO OTHER J WARNING INDICATION CRCRUISE 1 SO01507CA100203828 7796 FLIGHT 4997 - FLAPS FAIL CAUTION. REPLACED THE RIGHT BPSU. 2L72 4F RTA21EA 20051222001152005122200115EA 2005 12 22 COMA0560732 120051218A2420 IDG CNDAIRCL600 CL6002B19 1900309EA NR 2 GENERATOR WARNING LIGHT A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01806CA 7359 FLIGHT 5411 - GENERATOR 2 AND IDG 2 CAUTION. DEFERRED NR 2 IDG PER MEL. 2L72 4F RTA21EA 20051222001182005122200118SO 2005 12 22 C2XA05IA142 120051215A3350669367 LIGHT EMB 145 EMB145 3260210SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714972 145151 IAH - FLIGHT 2121, DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE FIRST FOUR ROWS OF EMERGENCY LIGHTS WOULD NOT TURN OFF. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE NUMBER THREE AISLE PATH LIGHTING STRIP, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20051227000012005122700001SO 2005 12 27 C2XA05SH140 120051218A531214526850401 FIREWALL EMB 145 EMB145LR 3260212SO AFT FUSELAGE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713553 145585 SHV - DURING C-CHECK MAINTENANCE FOUND APU FIREWALL CRACKED AT THE RIGHT HAND LOWER MOUNT. MAINTENANCE INSTALLED DOUBLER ON THE APU FIREWALL AT THE RIGHT HAND LOWER MOUNT IAW EMB SRM 53-32-13. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20051227000032005122700003SO 2005 12 27 C2XA05TY065 120051217A532014521713005 FLOOR SUPPORT EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712967 145133 TYS - DURING A SCHEDULED INSPECTION, THE LEFT OMEGA BEAM SHOWS SIGNS OF CORROSION ON PREVIOUS REPAIR AT FRAME 20. MAINTENANCE REMOVED PREVIOUS REPAIR PIECES, FABRICATED NEW PIECES, ALODINED, PRIMED AND INSTALLED IAW EMB-145-SRM-51-40-02, 53-00-10, CPM-51-20-04/05. 2L72 4F RTT00011AT 20051227000052005122700005EU 2005 12 27 MALA050880 120051214A2613 WARNING LIGHT SAAB SF340 340B 7860101EU TAIL PIPE ILLUMINATED A MALAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL15412XJ 340B412 LOW ENERGY ABORT DUE TO TAIL PIPE HOT INDICATION. NO FURTHER INFO AT THIS TIME. 2L72 4T RTA52EU 20051227000062005122700006EU 2005 12 27 MALA050886 120051218A5410 COWLING SAAB SF340 340B 7860101EU RT NACELLE OPEN A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15428XJ 340B428 CREW NOTED AFTER TAKEOFF, THE RT IB COWLING WAS UNLATCHED. AIR RETURN TO MEM. POST FLIGHT INSPECTION REVEALED DAMAGE TO COWLING 2L72 4T RTA52EU 20051227000072005122700007EU 2005 12 27 MALA050888 120051221A3260 WARNING LIGHT SAAB SF340 340B 7860101EU MLG MALFUNCTIONED A MALAO OTHER N FALSE WARNING NRNOT REPORTED 1 GL15425XJ 340B425 GEAR INTRANSIT LIGHT REMAINED ON AFTER GEAR EXTENSION. CLEARED SNOW AND ICE OFF GEAR AND CND. 2L72 4T RTA52EU 20051227000082005122700008NM 2005 12 27 MALA050877 120051212A4900 ODOR BOMBDRDHC8 DHC8400 NM APU DETECTED A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL15601XJ APU AUTO SHUT DOWN INFLIGHT HAD A BRIEF STRONG BURNING ODOR IN COCKPIT IT WENT AWAY AS SOON AS APU STOPPED. DEFERRED APU PER MLE 49-10. 2H72 4T RTA13NM 20051227000102005122700010EU 2005 12 27 AWXA200501545 120051217A3397D9299200900000 WIRE HARNESS AIRBUS320 A320232 3930326EU EMERGENCY LIGHTSINOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28656AW 1079 ORD - EEL - DURING INSPECTION DISCOVERED ROW 4L FLOOR PROXIMITY EMERGENCY ESCAPE PATH MARKING SYSTEM INOPERATIVE. MAINTENANCE PLACED ON MEL. MAINTENANCE REMOVED AND REPLACED THE WIRING HARNESS AT ROW 4L. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA28NM 20051227000152005122700015NM 2005 12 27 AWXA200501565 120051219A5330654576654 SKIN PANEL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 MCN - DURING C19 CHECK DISCOVERED TWO FUSELAGE SKIN CRACKS, 1.0 INCHES AND .75 INCHES LONG, JUST ABOVE UPPER ROW OF FASTENERS AT LAP SEAM BETWEEN BS 500 AND BS 520 AND BETWEEN STRINGER 10R AND 12R. MAINTENANCE REMOVED DAMAGE SKIN IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5300-05347-SS3. FABRICATED REPAIR DOUBLER, REPAIR TRIPLER, STRUCTURAL FILLERS, TEAR STRAP INTERNAL DOUBLER AND TAPERED FILLER IAW AWA ER NR 03-5300-05347-SS3. INSTALLED FABRICATED REPAIR PARTS BETWEEN BS 500 AND BS 520 AND BETWEEN STRING 10R AND 12R. 2L72 4F RTA16WE 20051227000162005122700016EU 2005 12 27 AWXA200501566 120051220A335032145410 POWER SUPPLY AIRBUS320 A320232 3930326EU RT OVERWING INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28605AW166819215 543 LAS - EEL - DURING OVERNIGHT INSPECTION DISCOVERED THAT THE RT OVERWING EXIT LIGHT POWER SUPPLY WOULD NOT TEST OR ILLUMINATE LIGHTS. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY IAW AIRBUS 320 MM 33-51-39. OPERATIONAL CHECKS WERE GOOD. VENDOR CONFIRMED FAULT. REPLACED S1 TEST SWITCH, WAS HARD TO ACTIVATE. THE UNIT WAS REPAIRED AND TESTED IAW CMM 33-51-12 REV.2 2L72 4F RTA28NM 20051227000172005122700017NM 2005 12 27 AWXA200501567 120051212A3397D53638 WIRE BOEING737 7373G7 1384595NM EMERGENCY LIGHTSBROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 MCN - EEL - DURING C19 CHECK, DISCOVERED THE EMERGENCY AISLE LIGHTS SEATS AT 5L, 6L, 7L, 8L, 9L, 16L, 21L AND THE AFT LEFT GALLEY EMERGENCY AISLE FLOOR PROXIMITY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE REPAIRED WIRING AT SEATS 5L, 6L, 7L, 8L, 9L, 16L, 21L AND AT THE AFT LEFT GALLEY ISLE FLOOR PROX. LIGHTS IAW BSWPM 20-30-12. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20051227000182005122700018NM 2005 12 27 AWXA200501568 120051220A5101 UNKNOWN BOEING737 7373G7 1384595NM OSCILLATES A AWXAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 WP28158AW 23780 DURING CLIMB, REPORTED AIRFRAME OSCILLATIONS, SIDE TO SIDE ON T/O FROM 1000 TO 5000 FT & CEASED AFTER THROTTLE RETARDED. CREW RETURNED & LANDED WITHOUT EVENT, ACFT OUT OF SERVICE FOR TROUBLESHOOTING. MX R&R NR 1 ENG MEC, NR 1 ENG FUEL PUMP & YAW DAMPER COUPLER. ALSO INSPECTED LT AND RT ENG MOUNTS, PYLONS, PERFORMED RUDDER FREE PLAY CHECKS, INSPECTED VERTICAL SPAR FITTING ATTACH BOLTS & RUDDER SPAR FLANGE. NO DEFECTS NOTED & OPS CHECKS GOOD. REPLACED RUDDER PCU. OPS CHECKS GOOD. 2L72 4F RTA16WE 20051227000192005122700019NM 2005 12 27 AWXA200501569 120051219A3020 VALVE BOEING737 737375 13844BNNM NR 2 NACELLE FAILED A AWXAA UNSCHED LANDING O OTHER CLCLIMB 1 WP28336AW 23707 CREW REPORTED THAT THE NR 2 ENGINE COWL ICE VALVE WOULD NOT OPEN ONCE AIRBORNE BUT WORKED ON GROUND IN SEA. CREW CYCLED SWITCH SEVERAL TIMES PER MX CONTROL AND WAS NO HELP. ICING CONDITIONS WERE EXPECTED EN ROUTE. CREW RETURNED TO SEA AND LANDED WITHOUT FURTHER EVENT. MX PLACED THE NR 2 ENGINE COWL ANTI-ICE VALVE ON MEL. MX R AND R THE NR 2 ENG. ANTI-ICE VALVE, SN 1226. NO HELP. MEL CONTINUED, MAINTENANCE SUSPECTED WIRING. THEN MAINTENANCE REMOVED AND REPLACED THE NO. 2 ENG. ANTI-ICE VALVE AGAIN, SN 0506 AND REPLACED THE ENGINE/WING ANTI-ICE MODULE. OPERATIONAL TESTS WERE GOOD. ANTI-ICE VALVE SN 1226 WAS CONFIRMED FAILURE BY VENDOR, INDUCTION TEST FOUND ECXESSIVE PORT AN 2L72 4F RTA16WE 20051227000202005122700020 2005 12 27 AWXA200501570 420051218A221010618165 FORCE LIMITER BOEING737 7373G7 1384595NM AUTOPILOT MALFUNCTIONED A AWXAA UNSCHED LANDING S AFFECT SYSTEMS CRCRUISE 1 WP28309AW4954425939 24711 MCI - DIVERSION - FLT 621 - DEPARTING FROM MKE EN ROUTE TO PHX, CREW REPORTED DUAL AUTOPILOT FAILURE, WOULD NOT ENGAGE. AIRCRAFT DIVERTED TO MCI TO REFUEL DUE TO INABILITY TO COMPLY WITH RVSM RESTRICTIONS. LANDED WITHOUT FURTHER EVENT IN MCI AND CREW DEFFERED BOTH AUTOPILOTS. IN PHX, MAINTENANCE FOUND THAT THE AILERON FORCE LIMITER WAS POPPING BOTH "A" AND "B" INTERLOCK CIRCUIT BREAKERS. REMOVED AND REPLACED THE AILERON FORCE LIMITER, OPERATIONAL CHECKS WERE GOOD. VENDOR CONFIRMED FAILURE. FAILED PRELIMINARY FUNCTIONAL TEST INTERMITTENT LOGIC SWITCH @17DEGREES. FOUND 2 WORN ACTUATORS, 2 SWITCHES WERE CONTAMINATED AND 2 SWITCHES OUT OF TOLERANCE. REPLACED PARTS, REPAIRED AND TESTED UNIT PER CMM 22-10-02 REV2L72 4F RTA16WE 20051227000222005122700022NM 2005 12 27 DHL2005765529 120051122A5347 SEAT TRACK BOEING727 727264 138408MNM BS 990-1040 CORRODED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15765AT 23014 CORROSION ON UPPER CARGO COMPT TRACK 24L BS 990 TO 1040. REMOVED CORRODED SECTION OF TRACK. FABRICATED AND INSTALLED REPAIR SEAT TRACK 60" BY 3.250" FROM BAC1520-792 AND 59.75" BY 3.30" FROM 65-23637-53 IAW B727 SRM 53-10-4 FIG 7. 2L73 4F A3WE 20051227000232005122700023NM 2005 12 27 DHL2005765530 120051119A5347 SEAT TRACK BOEING727 727264 138408MNM BS 560-640 CORRODED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15765AT 23014 CORROSION ON UPPER CARGO COMPT TRACK 48R BS 560 TO 640. REMOVED CORRODED SECTION OF TRACK. FABRICATED AND INSTALLED REPAIR SEAT TRACK 169.5" FROM BAC1520-792 IAW B727 SRM 53-10-5 FIG 7 AND 51-30-2. 2L73 4F A3WE 20051227000252005122700025WP 2005 12 27 ABXA050362 120051213A532099234847 INTERCOSTAL DOUG DC9 DC941 302207NWP E/E BAY CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23972AX 47631 INTERCOSTAL AT STA 180, LEFT BUTT LINE 18, WAS CRACKED OUT AT LIGHTENING HOLE. REPAIRED INTERCOSTAL IAW DC9 SRM 53-01. 2L72 4F A6WE 20051227000282005122700028NM 2005 12 27 USAA051598 120051220A5754015T1507114 SKIN BOEING767 767201 1385125NM NR 12 SLAT DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19646US 23898 FOUND WS 1045.2 NR 12 SLAT RT WING. FAB'D A 4" ROUND DOUBLER PER SRM 57-43-02, DEFECT SIZE: 1.09"L BY .025"W (REPAIRED AS HOLE). 2L72 4F RTA1NM 20051227000292005122700029 2005 12 27 UPS05145880 420051216A2565 WARNING LIGHT AIRBUS300 A300B4622R 3930312EU DOOR SLIDE INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01124UP 0808 CREW DOOR EVAC SLIDE WARNING LIGHT INOP BUZZER OK. RESET AUTONOMOUS POWER SUPPLY SYSTEM OPS CK OF LIGHT PER MM 52-73-11-4 THIS CLEARS M316289 2L72 4F RTA35EU 20051227000302005122700030NM 2005 12 27 UPS05645882 120051219A2910 LINE BOEING767 76734AF 1385212NM HYD SYSTEM CRACKED A IPXAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SO01331UP 27757 ON APPROACH, LOST LEFT HYDRAULIC PRESSURE RAN HYDRAULIC SYSTEM PRESSURE CHECKLIST. ON T/S FOUND HYD PRESSURE FROM L SYST ACMP TO PRESS/CASE DRAIN MODULE, RIGID LINE WITH CRACK REMOVED AND REPLACED RIGID HYD LINE IAW GMM 5- 9-1. SYSTEM CHK CARRIED OUT IAW AMM 29-11-00-2 AND SERVICE IAW 12-12-0 1-3. 2L72 4F RTA1NM 20051220004012005122000401NM 2005 12 20 SWAA053993 120051218A53126582671 PRESSURE PANEL BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29511SW 24188 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE BEADED WEB CRACKED AT BS 664, LBL 32. REPAIRED BEADED WEB PER SWA EA. 2L72 4F RTA16WE 20051220004032005122000403NM 2005 12 20 SWAA053995 120051218A53116546539 FRAME BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29511SW 24188 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 615, STR 17R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051220004172005122000417EA 2005 12 20 A6WA200540348 120051114A5220H341937 HANDLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE ESCAPE HATCH CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31426AW 7669 MWC 258 CREW ESCAPE HATCH OUTER HANDLE SHAFT HAS PITTING, CORROSION. REMOVED OUTER HANDLE ASSY AND INSTALLED NEW HANDLE ASSY, PN H341937, IAW AMM. (K) 2L72 4F4 FRTA21EA E15NE 20051221000042005122100004NM 2005 12 21 SWAA054009 120051217A53116546548 FRAME BOEING737 7373H4 1384600NM BS 747 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29622SW 27932 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051221000402005122100040NM 2005 12 21 SWAA054029 120051219A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 597 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29622SW 27932 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 597, STR 3R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051221000422005122100042NM 2005 12 21 SWAA054031 120051219A53146545866 KEELBEAM BOEING737 7373Q8 1384670NM BS 727 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED 1/2D CHECK, FOUND LT KEEL BEAM CORRODED AT BS 727. REPAIRED KEEL BEAM PER SRM. 2L72 4F RTA16WE 20051221000442005122100044 2005 12 21 SWAA054033 420051218A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29759GS 30544 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051221000462005122100046NM 2005 12 21 SWAA054022 120051219A5753 SKIN BOEING737 7373H4 1384600NM TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29379SW 26586 DURING SCHEDULED C2 CHECK, FOUND LT WING OUTBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM. 2L72 4F RTA16WE 20051221000482005122100048NM 2005 12 21 SWAA054024 120051219A53306545778 SKIN BOEING737 7375H4 138449DNM BS 889-919 CHAFED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29511SW 24188 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CHAFED AT DORSAL FIN BLADE SEAL, BETWEEN BS 889 TO BS 919, LBL 7. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051221000502005122100050NM 2005 12 21 SWAA054026 120051219A53116520723 FRAME BOEING737 7375H4 138449DNM BS 482 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29511SW 24188 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482, STR 20R. REPAIRED FRAME PER SWA EA. 2L72 4F RTA16WE 20051221000522005122100052NM 2005 12 21 SWAA054028 120051219A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 685 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29622SW 27932 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 685, STR 4L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051221000552005122100055NM 2005 12 21 QXEA200501785 120051215A30607826896 BRUSH BLOCK DHAV DHC8 DHC8202 2809007NM ELEVATOR HEAT MALFUNCTIONED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09356PH3799 250 502 PDX FLIGHT NR 2094, DURING CLIMB-OUT, ELEVATOR HORN HEAT CAUTION LIGHT ILLUMINATED, FOLLOWED BY LEFT STALL WARNING TANK 1 AUXILLARY PUMP LIGHT WENT OUT ALSO. MAINTENANCE INSPECTED AND FOUND NR 1 PROP DEICE BRUSH BLOCK ARCING/OVERHEATED WHICH CAUSED A AND B PHASE CB'S TO TRIP IN NR 1 AC CONTACTOR BOX. REPLACED NR 1 BRUSH BLOCK PER AMM 61-10-11-000-801 AND 61-10-11-400-801. REPLACED TRIPPED FUSES GROUND RAN AIRCRAFT AND OPERATIONAL CHECKED ALL SYSTEMS MENTIONED ABOVE AND PROP HEAT. ALL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051221000572005122100057NM 2005 12 21 0501695506 120051205A33506012113RF BATTERY PACK BOEING757 757251 1384970NM EMERGENCY LIGHT INOPERATIVE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01506US 23195 DURING GEAR CHANGE, FOUND EMERGENCY PATH LIGHTING IN FIRST CLASS INOP. REPLACED BATTERY PACK AND CHECKS NORMAL. 2L72 4F RTA2NM 20051221000592005122100059NM 2005 12 21 AWXA200501528 120051116A575465C267933 SKIN BOEING737 73733A 1384673NM ZONE 500 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 MCN - DURING C19 CHECK DISCOVERED 6 CRACKS ON THE BOTTOM OF THE NR 3 SLAT OUTBOARD OF ACTUATOR FROM SS 51L TO SS 76L. MAINTENANCE TRIMMED OUT DAMAGED AREA ON THE NR 3 SLAT IAW BOEING 737-300 SRM 57-43-01-2R6. FABRICATED FILLER AND SPLICE PLATE IAW BOEING 737-300 SRM 57-43-01-2R6. INSTALLED FABRICATED REPAIR PARTS ON THE NR 3 SLAT FROM SS 51L TO SS 76L IAW BOEING 737-300 SRM 57-43-01-2R6. 2L72 4F RTA16WE 20051221000612005122100061NM 2005 12 21 DHL2005765501 120051207A5753 SKIN BOEING727 727264 138408MNM FOREFLAP GOUGED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15765AT 23014 LEFT OUTBD FORE FLAP L/E SKIN GOUGED 26" INBD OF OUTBD FLAP TRACK. CUT OUT GOUGED AREA, FABRICATED AND INSTALLED REPAIR IAW B727 SRM 57-50-4 FIG 1, MATERIAL 2024-T3 .050" PO NR 801639.2. 2L73 4F A3WE 20051221000632005122100063NM 2005 12 21 DHL2005765515 120051209A5347 SEAT TRACK BOEING727 727264 138408MNM BS 1090-1138 CORRODED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15765AT 23014 UPPER CARGO COMPT TRACK 48L BS 1090 TO 1100 AND 1138 HAVE CORROSION. CUT OUT CRACKED SECTION OF SEAT TRACK BS 1110 TP 1138 LBL 48L. FABRICATED AND INSTALLED REPAIR 19.8" BY 3.25" BY 7.00" BY 1.350" FROM BAC1520-792 IAW B727 SRM 53-10-5 FIG 7. 2L73 4F A3WE 20051221000652005122100065NM 2005 12 21 DHL2005765512 120051207A5320 FLOOR SUPPORT BOEING727 727264 138408MNM BS 644 CORRODED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15765AT 23014 FOUND FWD PIT FLOOR SUPPORT HAS CORROSION AROUND FASTENER HOLES LWR SIDE STA 644 LBL 2. CUT OUT CRACKED SECTION OF FLOOR SUPPORT STA 644 LBL 2. FABRICATED AND INSTALLED REPAIR SPLICES 18-1/2" BY 1" BY 1-1/4" FROM BAC1520-1485 AND 8-1/2" BY 5/8" BY 1" BAC1509-100146 AND 8-1/2" BY 1" BY 1-3/8" FROM BAC1490-2734 IAW B727 SRM 53-10-5 FIG 4. 2L73 4F A3WE 20051221000952005122100095EA 2005 12 21 ASOA05946 120051103A335061000976 LIGHT CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27709EV 10068 DURING A C-CHECK, THE EMERGENCY FLOODLIGHT, NEAR ROW 17, WAS FOUND TO BE INOPERATIVE. MAINT WILL REMOVE AND REPLACE THE LAMP IN THE EMERGENCY FLOODLIGHT ASSY, NEAR ROW 17. (K) 2L72 4F4 FRTA21EA EOOO63EN 20051221001002005122100100EA 2005 12 21 ASOA05948 120051103A25602618 FLASHLIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27889AS 7538 DURING A GROUND INSPECTION, THE CAPTAINS FLASHLIGHT WAS FOUND TO BE INOPERATIVE. MAINT REMOVED AND REPLACED THE CAPT FLASHLIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20051221001032005122100103EA 2005 12 21 ASOA05895 120051023A3350 COVER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27851AS 7360 DURING A GROUND INSPECTION, THE FORWARD RT SIDE EMERGENCY EXIT LIGHT COVER WAS FOUND TO BE BROKEN. MAINT REMOVED AND REPLACED THE FORWARD RT SIDE EMERGENCY EXIT LIGHT COVER. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20051221001542005122100154SO 2005 12 21 XGN2005F00010 220051011A8530ECI712A CYLINDER BEECH 36 36BEECH 1151602CE CONT O520 IO520A 17032SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW051194A741 E159 573460R FOUND CRACK AT THE 100 HR INSPECTION. ON GOING PROBLEM WITH THE ECI CYLINDERS. (K) 1L71 3O3 O 3A15 E5CE 20051221001632005122100163SO 2005 12 21 XGN2005F00014 220051011A8530ECI712A CYLINDER BEECH 58 58 1152740CE CONT O520 IO520C 17032SO ENGINE CRACKED A XGNAK NONE O OTHER ININSP/MAINT 1 SW05577W 645 TH375 FOUND CYLINDER HEAD CRACKED IN THE EXHAUST SIDE DURING A 50 HOUR INSPECTION. THIS IS AN ON GOING PROBLEM WITH THE ECI CYLINDER. (K) 1L72 3O3 O 3A16 E5CE 20051221001662005122100166SO 2005 12 21 XGN2005F00015 220051011A8530ECI712A CYLINDER BEECH 33 F33A 1151425CE CONT O520 IO520BA 17032SO ENGINE CRACKED A XGNAK NONE O OTHER ININSP/MAINT 1 SW051096W1147 CE436 807017 THESE CYLINDERS SHOWED TO BE CRACKED IN THE EXHAUST SIDE OF THE HEAD. THE LEAKS SHOWED UP WHEN DOING THE COMPRESSION CHECK. DUE TO THE NR OF CRACKED CYLINDER HEADS, COMPRESSION CHECK DOEN EVERY 50 HOURS. (K) 1L71 3O3 O 3A15 E5CE 20051221001812005122100181CE 2005 12 21 FRK2005F00000 120051108A2612TA12C59H06CC CLAMP CESSNA500 550 2076604CE PWA JT15 JT15D4 52112NE COWLING FAILED E FRKAO OTHER N FALSE WARNING NRNOT REPORTED 1 NE01245CC 5500212 CLAMP SECURING FIRE DETECTION SENSOR TO SUPPORT STRUCTURE FAILED ALLOWING SENSOR TO CONTACT ENGINE COWLING. THIS CONTACT WITH COWLING CHAFFED INTO SENSOR CAUSING A FALSE ENGINE FIRE WARNING. (K) 1L72 4F4 F A22CE E1NE 20051222000032005122200003NM 2005 12 22 ASAA0570105 120051024A5310141A61503 DOOR FRAME BOEING737 737790 13844CNNM FS 312 CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02624AS 30778 PAE - DURING SI CHECK, FOUND FORWARD ENTRY DOOR FORWARD FRAME CHAFED AT OB RADIUS UPPER END. REPAIRED IAW EA 5210-01181. (M) 2L72 4F RTA16WE 20051222000042005122200004NM 2005 12 22 ASAA0570106 120051024A5210141A610410 STOP FITTING BOEING737 737790 13844CNNM FS 340 CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02624AS 30778 PAE - DURING SI CHECK, FOUND FORWARD ENTRY DOOR AFT LOWER STOP PIN FITTING CHAFED. REPAIRED IAW EA 5210-01183. (M) 2L72 4F RTA16WE 20051222000142005122200014NM 2005 12 22 ASAA0570098 120051024A5321453A161031 FLOOR PANEL BOEING737 737790 13844CNNM FS 500 DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02624AS 30778 PAE - DURING SI CHECK, FOUND FORWARD CARGO BAY AFT FLOOR PANEL FASTENER PULLING THROUGH TEMP REPAIR. REPAIRED IAW SRM 53-00-53/51-40-5. (M) 2L72 4F RTA16WE 20051222000232005122200023NM 2005 12 22 ASAA0570069 120050921A5330141A372212 SKIN BOEING737 737790 13844CNNM FS 233-228 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02623AS 30166 PAE - DURING CHECK, FOUND EXT POWER DOOR CUT OUT CRACKED. REPAIRED IAW EA 5330-01996. (M) 2L72 4F RTA16WE 20051222000262005122200026NM 2005 12 22 ASAA05700061 120050921A5320146A75036 FLOOR SUPPORT BOEING737 737790 13844CNNM FS 773 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02623AS 30166 PAE - DURING C-CHECK, FOUND CORROSION ON FLOOR SUPPORT. REPAIRED IAW EA 5310-02493. (M) 2L72 4F RTA16WE 20051222000292005122200029NM 2005 12 22 ASAA0570103 120051024A5320146A75022 SUPPORT BOEING737 737790 13844CNNM FS 727A-787 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02624AS 30778 PAE - DURING SI CHECK, FOUND CORROSION ON LEFT SIDEWALL SUPPORT PLATE AT BS 727. REPAIRED IAW SRM 53-00-53, 51-40-02. (M) 2L72 4F RTA16WE 20051222000362005122200036NM 2005 12 22 ASAA0580513 120050926A531199115173 FRAME DOUG MD80 MD83 3023681NM FS 180 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - DURING HV-CHECK, FOUND FRAME CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLER, TWO REPAIR ANGLES AND TWO REPAIR PLATES. (M) 2L72 4F RT 20051222000402005122200040SO 2005 12 22 C2XA05CL099 120051213A3230355022002 CONTROL UNIT EMB 145 EMB145LR 3260212SO COCKPIT DEFECTIVE A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW271397914051 145181 CLE FLIGHT 2266, THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR CONTROL MODULE AND THE LANDING GEAR ELECTRONIC UNIT. TEST FLIGHT WAS PERFORMED AND NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE. P/N LANDING GEAR MODULE: 7-45550-3, S/N:0164 CSO:9073, TSO:11880. 2L72 4T RTT00011AT 20051222000452005122200045EA 2005 12 22 COMA0560737 120051219A304016591 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA WINDSHIELD HEAT MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01484CA8929 7702 FLIGHT 5201 - RIGHT WINDSHIELD HEAT CAUTION. REPLACED THE HEAT CONTROLLER. 2L72 4F RTA21EA 20051222000502005122200050NM 2005 12 22 SWAA054036 120051214A53126545819 PRESSURE PANEL BOEING737 7373H4 1384600NM NLG WW CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29351SW 24572 DURING SCHEDULED C3 CHECK, FOUND NLG W/W UPPER CEILING WEB CRACKED AT BS 251.625, RBL 7.75 & LBL 7.75. REPAIRED WEB PER SWA EA. 2L72 4F RTA16WE 20051222000512005122200051 2005 12 22 SWAA054037 420051214A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29351SW 24572 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051222000562005122200056NM 2005 12 22 SWAA054042 120051220A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN DISCONNECTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29488WN 33853 EEPLS TRACK LIGHT INOP. RECONNECTED LIGHT PER MM. 2L72 4F RTA16WE 20051222000672005122200067NM 2005 12 22 AALA20050819 120051213A3350BPS73 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21653A 24611 LAX - EMERGENCY LIGHTS IN AFT CABIN INOPERATIVE. REPLACED BATTERY PACK AT LEFT 737 FOR EMERGENCY LIGHTS IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20051222000832005122200083NM 2005 12 22 USAA051589 120051220A5347BAC1520792 SEAT TRACK BOEING737 7374B7 1384702NM BS 727B, RBL 24.CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 BS 727B, RBL 24.75 RIGHT I/B SEAT TRACK FLOORBEAM CRACKED. CUT OUT DAMAGED SECTION, FAB & INSTALLED NEW SECTION OF TRACK/BEAM & SPLICE PRTS IAW SRM 53-00-52 EA 97204, DEFECT SIZE: .250 INCH CRACK. 2L72 4F RTA16WE 20051222000962005122200096EU 2005 12 22 USAA051612 120051220A5347F57110568205 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 SEAT TRACK - Y450 FR 43 CORRODED. BLEND DAMAGE PER 51-74-00, REPLACED TRACK PER SRM 53-31-15, 51-72-11; CORR LEVEL 2; TASK C53317001, DEFECT SIZE: 3 X 1 INCH. 2L72 4F RTA46NM 20051222001002005122200100EU 2005 12 22 USAA051600 120051220A5320F53479420200 SUPPORT AIRBUS330 A330323 3930335EU STR 26 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 STR 26, 4 BETWEEN FR 77 & 78 CORRODED. MODIFIED PART INSTALLED PER SRM 51-72-11; CORR LEVEL 2; TASK C53415901, DEFECT SIZE: 1 X 1 INCH; LEVEL 2; TASK C534159-01. 2L72 4F RTA46NM 20051222001162005122200116SO 2005 12 22 C2XA05IA139 120051209A3260852701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212SO NLG INOPERATIVE A C2XAK NONE O OTHER ININSP/MAINT 1 SW27139081036310363 145465 IAH - FLIGHT 3471, THE CREW REPORTED EXPERIENCING HEAVY VIBRATION FROM FONT OF AIRCRAFT AFTER BRINGING UP THE GEAR. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. THE AIRCRAFT WAS TEST FLOWN, AND FOUND THAT THE NOSE LANDING GEAR DOORS WERE NOT CLOSING. MAINTENANCE REMOVED AND REPLACED THE NLG PROXIMITY SWITCH, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20051227000042005122700004NM 2005 12 27 MALA050879 120051213A2913 PUMP BOMBDRDHC8 DHC8400 NM HYD SYSTEM INOPERATIVE A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15601XJ CREW REPORTED THAT THEY LOST NR 2 HYDRAULIC QUANTITY INFLIGHT AND DIVERTED TO ABE FOR RUNWAY REQUIREMENTS. REPLACED EDP. 2H72 4T RTA13NM 20051227000092005122700009 2005 12 27 MALA050887 420051219A2210 AUTOPILOT SYS BAC 146 AVRO146RJ85A1500097EU FAULTY A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15533XJ E2367 AUTO PILOT FAULT. AIR RETURN TO MEM. NO FURTHER INFO AT THIS TIME 2H74 4F RTA49EU 20051227000132005122700013 2005 12 27 AWXA200501548 420051218A34426225132120 TRANSCEIVER AIRBUS320 A320232 3930326EU WX RADAR SYS INOPERATIVE A AWXAA UNSCHED LANDING O OTHER CRCRUISE 1 WP28605AW 543 CREW REPORTED THAT EN ROUTE TO SJC, TURNED THE WEATHER RADAR ON AND IT DID NOT WORK. WEATHER IN THE AREA SO CREW RETURNED TO PHX FOR REPAIR. CREW LANDED AIRCRAFT WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE WEATHER RADAR TRANSCEIVER. OPERATIONAL TESTS WERE GOOD. CONFIRMED FAILURE. REPLACED A2AA2U5 AND A2A2VR25 AND ALIGNED A5 TO CORRECT LOW TRANSMITTER POWER. INSTALLED SB 86. TESTED IAW 34-45-21 REV 9. 2L72 4F RTA28NM 20051227000142005122700014NM 2005 12 27 AWXA200501564 120051219A2741 TRIM SYSTEM BOEING737 73733A 1384673NM STABILIZER MALFUNCTIONED A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28173AW 23632 PHX - ABORTED TAKEOFF - FLT 227 - CREW REPORTED THAT THE TAKEOFF WARNING HORN SOUNDED DURING TAKEOFF. ABORTED TAKEOFF AT APPROXIMATELY 45 KNOTS. CAPTAINS TRIM SHOWED 4.8 WHILE THE F/O'S SHOWED 5.2. CREW RESET STAB TRIM AND RECEIVED NO FURTHER WARNINGS. 2L72 4F RTA16WE 20051227000212005122700021EU 2005 12 27 AWXA200501571 120051217A5610NP1653115 WINDSHIELD AIRBUS320 A320231 3930325EU COCKPIT FAILED A AWXAO OTHER O OTHER DEDESCENT 1 WP28626AW2309023090 65 CREW REPORTED THAT AT FL 360, THE CAPT WINDSHIELD OUTER PANE SHATTERED & LT WINDSHIELD ANTI-ICE FAILED. LANDED WITHOUT FURTHER EVENT. MX R & R CAPT WINDSHIELD & NR 1 WINDSHILED HEAT COMPUTER. OPS CHECKS GOOD. PERFORMED FUNCTIONAL TESTS OF CAPT WINDSHIELD HEAT COMPUTER, NO FAULT FOUND. INSPECTED IAW SAGEM CMM 30-42-36 REV ORIG. CAPT WINDOW SCRAPPED AT VENDOR. INITIAL OBSERVATION OF UNIT REVEALED MOISTURE INGRESS. WINDOW WAS HIGH TIME UNIT, 7 YEARS OLD. CONSIDERED NORMAL FAILURE SEQUENCE FOR AGE OF WINDOW. 2L72 4F RTA28NM 20051227000272005122700027WP 2005 12 27 ABXA050360 120051209A5410991550032 RIB DOUG DC9 DC941 302207NWP LT PYLON CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23972AX 47631 AFT UPPER SPAR STRAP ANGLE CRACKED JUST INBOARD OF AFT MOUNT. REMOVED AND REPLACED ANGLE WITH NEW ANGLE IAW DC9 SRM 51-30-05. 2L72 4F A6WE 20051227000312005122700031WP 2005 12 27 UPS05845879 120051218A3350 LIGHT DOUG DC8 DC873F 302199FWP EMERGENCY EXIT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER MM 33-50-01-2. OPS CHECK GOOD. 2L74 4F RT4A25 20051227000342005122700034NM 2005 12 27 USAA051599 120051220A5753 SKIN BOEING757 757225 1384959NM FLAP GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19607AU 22203 FOUND 2.0"L BY 0.80"W BY .055"D AND 1.2"L BY 0.30"W BY .013"D. FAB'D OVERLAY REPAIR AND BONDED TO AREA PER SRM 51-70-17 AND EA 97150, DEFECT SIZE: 2.0"L BY .080"W BY .055"D AND 1.2"L BY .20"W BY .013"D. 2L72 4F RTA2NM 20051227000352005122700035SO 2005 12 27 C2XA05SD033 120051216A33503025103 BULB EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2717115 145666 SDF - NR 2 EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT NR 2 IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD. 2L72 4F RT 20051227000362005122700036SO 2005 12 27 C2XA05RI019 120051220A2910NAS16125 O-RING EMB 145 EMB145LR 3260212SO NR 1 HYD MANFLD DAMAGED A C2XAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW2716919 145393 FLIGHT 2334 EWR TO SDF, CREW REPORTED HYDRAULIC SYSTEM NR 1 FAILED IN FLIGHT. FLIGHT DIVERTED TO RIC. RIC MX FOUND THE CAUSE OF FLUID LOSS TO BE AT THE NR 1 HYD MANIFOLD, EDHP PRESSURE SWITCH. MX REMOVED AND REPLACED THE PRESSURE SWITCH O-RING AND DUE TO THE SYSTEM BEING RUN OUT OF FLUID ALSO REPLACED NR 1 EDHP AND NR 1 EMDP ALONG WITH DECONTAMINATING THE FLUID SYSTEM AND CHANGING NR 1 SYSTEM HYD FLUID FILTERS. 2L72 4T RTT00011AT 20051227000372005122700037NM 2005 12 27 DHL2005765519 120051118A5320 FLOOR SUPPORT BOEING727 727264 138408MNM BS 664 CORRODED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15765AT 23014 FWD PIT FLOOR SUPPORT HAS CORROSION AROUND FASTENERS HOLES LWR SIDE STA. 644 LBL 13. REMOVED CORRODED AREA. FABRICATED AND INSTALLED REPAIRS 8.5" BY .8" BY 1.2" FROM BAC1517-1507 AND 22" BY .75" BY 1.3" BY 1.0" FROM AND10134-1204 IAW B727 SRM 51-40-3 FIG 6, PG 1. 2L73 4F A3WE 20051227000402005122700040NM 2005 12 27 DHL2005765522 120051118A5320 FLOOR SUPPORT BOEING727 727264 138408MNM BS 644 CORRODED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15765AT 23014 FWD PIT FLOOR SUPPORT HAS CORROSION AROUND FASTENERS HOLES LWR SIDE STA 644 RBL 13. REMOVED CORRODED AREA. FABRICATED AND INSTALLED REPAIRS 8.5" BY .8" BY 1.2" FROM AND10134-1204 AND 22" BY 1.3" 1.0" FROM BAC1517-1507 IAW B727 SRM 51-40-3 FIG 1 PG 1. 2L73 4F A3WE 20051227000412005122700041NM 2005 12 27 DHL2005765523 120051118A5330 SKIN BOEING727 727264 138408MNM FUSELAGE LIGHTNING STRIKEB DHLAK NONE O OTHER ININSP/MAINT 1 SO15765AT 23014 LIGHTNING STRIKE FOUND ON AIRCRAFT SKIN RT SIDE BS 205 AND 6" BELOW S-17R. REPAIRED LIGHTNING STRIKE IAW B727 SRM 53-30-3 FIG 20 STEP 2. 2L73 4F A3WE 20051227000432005122700043NM 2005 12 27 DHL2005765524 120051118A5330 SKIN BOEING727 727264 138408MNM FUSELAGE LIGHTNING STRIKEB DHLAK NONE O OTHER ININSP/MAINT 1 SO15765AT 23014 FOUND LIGHTNING STRIKE AIRCRAFT SKIN RT SIDE BS 188 AND 5" BELOW S-17R. REPAIRED LIGHTNING STRIKE ON IAW B727 SRM 53-30-3 FIG 20 STEP 2. 2L73 4F A3WE 20051227000442005122700044NM 2005 12 27 DHL2005765526 120051120A5330 SKIN BOEING727 727264 138408MNM FUSELAGE LIGHTNING STRIKEB DHLAK NONE O OTHER ININSP/MAINT 1 SO15765AT 23014 LIGHTNING STRIKE FOUND ON FUSELAGE RT SIDE SKIN AT BS 243.7 ONE AT FASTENER 8" AND SECOND AT 9" BELOW S-19R. REPAIRED LIGHTNING STRIKE BY INCREASING DIAMETER OF HOLE BY 0.06 IAW B727 SRM 53-30-3 FIG 20. INSTALLED RIVETS IAW B727 SRM 53-30-3 AT STA 243.7, ONE AT 8" AND ONE AT 9" BELOW S-19R IAW B727 SRM 53-30-3 FIG 20. 2L73 4F A3WE 20051227000452005122700045NM 2005 12 27 DHL2005765527 120051120A5330 SKIN BOEING727 727264 138408MNM FUSELAGE LIGHTNING STRIKEB DHLAK NONE O OTHER ININSP/MAINT 1 SO15765AT 23014 LIGHTNING STRIKE FOUND ON FUSELAGE RT SIDE SKIN AT BS 235.8 11" BELOW S-19R. REPAIRED LIGHTNING STRIKE BY INCREASING DIAMETER OF HOLE BY 0.06 IAW B727 SRM 53-30-3 FIG 20. INSTALLED RIVET IAW B727 SRM 53-30-3 AT STA 235.8, 11" BELOW S-19R IAW B727 SRM 53-30-3 FIG 20. 2L73 4F A3WE 20051227000462005122700046 2005 12 27 UPS05245888 420051221A2565 SLIDE BOEING727 72725C 138400HNM CABIN LOOSE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 ESCAPE SLIDE PACK IS VERY LOOSE. SECURED ESCAPE SLIDE AS REQUIRED PER AMM 25-60-15-2. 2L73 4F A3WE 20051227000472005122700047NM 2005 12 27 UPS05445886 120051219A3230 LANDING GEAR BOEING747 747123F NM LEFT INOPERATIVE A IPXAO OTHER J WARNING INDICATION CLCLIMB 1 SO01677UP 20391 ATB - LEFT BODY GEAR WOULD NOT RETRACT. L BODY TILT LIGHTS, BOTH PRIM AND ALT ON. ALSO L/BODY GEAR DOOR LIGHTS BOTH PRIM AND ALT. ON GEAR WA S EXTENDED. NO CHAFED OR PINCHED WIRE REF WDM 32-61-21 PG 2 & 32-6 1-22 PG 1. COMPLIED W/ TECH BOW NO STEERING FAULTS OR LEAK. CYCLED L&R MAIN BODY GEAR 6 TIMES GOING TO OFF POS. & SHAKING WIRES & CARD FILE. NO FAULTS R&R L/H BODY MM32-13-15. AC OK FOR SERVICE. PRI & ALT SYS CK IN ALL SITUATIONS NOTED ABOVE. AC JACKED & LOWERED PER MM 07-11-01. 2L74 4F A20WE 20051227000492005122700049WP 2005 12 27 ABXA050369 120051207A5330591140659 SKIN DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23943AX 47528 FUSELAGE INNER SKIN CRACKED AT MAIN ENTRANCE DOOR OPENING AFT SIDE JUST ABOVE DOOR LOWER CORNER. REPAIRED CRACK IAW DC9 SRM 53-01-1. 2L72 4F A6WE 20051227000512005122700051WP 2005 12 27 ABXA050377 120051210A5313408448519 LONGERON DOUG DC9 DC931 3022065WP BS 718 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23943AX 47528 FOUND LONGERON 7 RIGHT WAS CRACKED AT STA 718. SPLICED LONGERON IAW DC9 SRM 53-02. 2L72 4F A6WE 20051227000552005122700055WP 2005 12 27 ABXA050376 120051210A531327779221 LONGERON DOUG DC9 DC931 3022065WP BS 756 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23943AX 47528 FOUND LONGERON 2 LEFT WAS CRACKED AT STA 756. REMOVED AND REPLACED LONGERON IAW DC9 SRM 53-02. 2L72 4F A6WE 20051227000562005122700056WP 2005 12 27 ABXA050366 120051020A5315 FLOORBEAM DOUG DC8 DC863F 302198FWP BS 70 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 FOUND MAIN CABIN, STA 70, RIGHT BUTT LINE 43-51, LOWER SIDE OF FLOORBEAM CORRODED OUT OF LIMITS. FOUND LOWER SIDE OF FLOORBEAM CORRODED OUT OF LIMITS AT STA 70, RIGHT BUTT LINE 43-51. FABRICATED FILLER AND DOUBLER AND INSTALLED. ALL WORK IAW DC8 SRM 51-1-8, 53-7-3, 51-2-0, 53-2-0, AND LWR 200302015. 2L74 4F 4A25 20051227000612005122700061WP 2005 12 27 ABXA050361 120051209A5330591142642 SKIN DOUG DC9 DC941 302207NWP BS 1041 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23972AX 47631 FOUND CRACK IN FUSELAGE SKIN AT RIVET, STA 1041, LONGERON 17 RIGHT, BELOW LAP SEAM. REPAIRED AREA IAW DC9 SRM 53-04. 2L72 4F A6WE 20051227000622005122700062EU 2005 12 27 USAA051629 120051221A5347F534762142000 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 FOUND CORROSION ON FS 57.4 AND 58 Y450. BLENDED PER SRM 51-74-00, 53-00-15, INSTALLED NEW TRACK PER 51-72-11, DEFECT SIZE: .030" BY 3/4". 2L72 4F RTA46NM 20051227000642005122700064NM 2005 12 27 USAA051618 120051221A52406545871523 SKIN BOEING737 7373B7 1384580NM FWD SERVICE DOORCRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19517AU 23703 FOUUND FWD SERVICE DOOR-OUTER SKIN-UPPER HINGE CUT OUT. INSTALLED DOUBLER IAW TR 52-10-13, DEFECT SIZE: .25". 2L72 4F RTA16WE 20051227000662005122700066EU 2005 12 27 USAA051620 120051221A5321F5367286800100 FLOOR PANEL AIRBUS330 A330323 3930335EU FR 33 Y1456 DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 FOUND FS DELAMINATED 33 Y1456. COMPOSITE DOUBLER INSTALLED PER SRM 53-02-00, DEFECT SIZE: 2" X 6". 2L72 4F RTA46NM 20051227000682005122700068EU 2005 12 27 USAA051622 120051221A5347F5347821720000 SEAT TRACK AIRBUS330 A330323 3930335EU Y450 LT FR 75 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 FOUND CORROSION Y450 LT FS 75. INSTALLED NEW SEAT TRACK PER SRM 51-42-11, 53-00-15, DEFECT SIZE: .050". 2L72 4F RTA46NM 20051227000712005122700071EA 2005 12 27 QXEA200501795 120051124A7830 COWLING CNDAIRCL600 CL6002C10 1390015EA THURST REVERSER WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09604QX 10019 YYC - LOWER LEFT ENGINE TRANS COWL HAS 3 WEAR MARKS ON THE INBOARD THRUST REVERSER SLIDER. BLENDED DAMAGE IAW EA R-78-72 AND REO 670-54-21-496. 2L72 4F RTA21EA 20051227000722005122700072EA 2005 12 27 QXEA200501796 120051124A7830 COWLING CNDAIRCL600 CL6002C10 1390015EA THRUST REVERSER WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09604QX 10019 YYC - LEFT ENGINE UPPER TRANS COWLING HAS 2 WEAR MARKS ON THE FORWARD END OF THE INBOARD THRUST REVERSER SLIDER. BLENDED DAMAGE IAW EA R-78-72 AND REO 670-54-21-496. 2L72 4F RTA21EA 20051227000732005122700073EA 2005 12 27 QXEA200501797 120051124A5310 BEAM CNDAIRCL600 CL6002C10 1390015EA BS 847 TOOL DAMAGE A QXEAK NONE W INADEQUATE Q C ININSP/MAINT 1 NM09604QX 10019 YYC - FUSELAGE BULKHEAD BEAM AT STATION FS 847 RBL 18 HAS TOOLING DAMAGE AT THE FASTENER HOLE ON THE LOWER OUTBOARD FLANGE AND WEB. BLENDED DAMAGE IAW EA R-53-401 AND REO 670-53-41-016. 2L72 4F RTA21EA 20051227000742005122700074EA 2005 12 27 QXEA200501798 120051124A3211 TRUNNION CNDAIRCL600 CL6002C10 1390015EA MLG GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09604QX 10019 YYC - MAIN GEAR TRUNNION HAS A GOUGE ON THE OUTBOARD SIDE. BLENDED OUT AREA IAW CRJ-700 SRM 51-12-00-001-001-A01. MATERIAL LOSS .008", REMAINING THICKNESS .693". RESTORED FINISH. 2L72 4F RTA21EA 20051227000782005122700078EA 2005 12 27 QXEA200501802 120051125A3220 STRUT CNDAIRCL600 CL6002C10 1390015EA NLG CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09604QX 10019 YYC - NOSE GEAR OUTER CYLINDER HAS AREAS OF CORROSION. REPAIRED IAW EA R-32-204 AND REO 670-32-21-080. RESTORED FINISH. 2L72 4F RTA21EA 20051227000792005122700079EA 2005 12 27 QXEA20051803 120051124A5320CC670332929 FLOOR SUPPORT CNDAIRCL600 CL6002C10 1390015EA BS 280 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09604QX 10019 YYC - COCKPIT FLOOR SUPPORT ANGLE AT STATION FS 280 IS CORRODED. REPLACED FLOOR ANGLE IAW CRJ-700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20051227000812005122700081EU 2005 12 27 USAA051623 120051221A5347F5311170420000 SEAT TRACK AIRBUS330 A330323 3930335EU BS 1139 -Y953 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 FOUND CORROSION STA 1139 -Y953. BLENDED PER SRM 53-11-15; REPLACEMENT PER 51-72-11; CORROSION LEVEL 2; TASK C53117201, DEFECT SIZE: .500" X .500" X .028". 2L72 4F RTA46NM 20051227000832005122700083EU 2005 12 27 USAA051625 120051221A5310F53479046004 BEAM AIRBUS330 A330323 3930335EU FR 76, STR 26 LTCORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 FOUND CORROSION FS 76 STR 26 LH Y1447.8. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 53-41-14; CORROSION LEVEL 2; TASK C53415901, DEFECT SIZE: 2" BY 2" BY .010". 2L72 4F RTA46NM 20051227000852005122700085NM 2005 12 27 USAA051616 120051221A5311 FRAME BOEING737 7374B7 1384702NM BS 794.3 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 FOUND CORROSION FRAME 794.3 AND JUST ABOVE S25R. MAJOR REPAIR REMOVED DAMAGED. INSTALL FILLER AND THREE STRAPS IAW SRM 51-70-12, DEFECT SIZE: 3.0". 2L72 4F RTA16WE 20051227000862005122700086EU 2005 12 27 USAA051628 120051221A5320F5347902320400 PROFILE AIRBUS330 A330323 3930335EU BS 77-79 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 FOUND CORROSION AROUND CUP NUTS; STG %26 4A BETWEEN FS 77-79. REPLACED PER SRM 51-72-11; CORROSION LEVEL 2; TASK C53415901, DEFECT SIZE: 1" BY 1". 2L72 4F RTA46NM 20051227000872005122700087NM 2005 12 27 USAA051640 120051221A5315BAC1505100703 FLOORBEAM BOEING737 7374B7 1384702NM BS 986 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19781AU 25020 FOUND CORROSION FLOORBEAM STA 986.5, RBL 4-38. FABRICATED NEW PARTS PER TR 53-60-01 REV A, 53-15-01B; TASK NR C5310702; LEVEL 1, DEFECT SIZE: 46" BY 2.0" BY 0.055". 2L72 4F RTA16WE 20051227000882005122700088EU 2005 12 27 USAA051630 120051221A5320F53479023204 PROFILE AIRBUS330 A330323 3930335EU BS 75-77 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 FOUND CORROSION LEFT GUTTER BETWEEN FS 75-77, AROUND FASTENERS. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-72-11, 51-44-11; 51-42-11; TASK C5341591, DEFECT SIZE: 30 EA 1/4" AREAS. 2L72 4F RTA46NM 20051227000892005122700089EU 2005 12 27 USAA051631 120051221A5320F5347821520000 FLOOR SUPPORT AIRBUS330 A330323 3930335EU Y1447 FR 75 & 76CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 FOUND CORROSION Y1447 FS 75 AND 76. BLENDED PER 51-74-00, INSTALLED NEW TRACK PER SRM 51-72-11, 53-00-15, DEFECT SIZE: .500" BY .400 BY .068". 2L72 4F RTA46NM 20051227000912005122700091NM 2005 12 27 QXEA200501784 120051214A33506138001 BATTERY PACK BOMBDRDHC8 DHC8402 1390042NM EMERGENCY LIGHT INOPERATIVE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX694 694 4055 PDX - ON OPERATIONAL CHECK OF EMERGENCY LIGHT SYSTEM FOUND FORWARD AISLE AND LEFT FORWARD EGRESS LIGHT TO WORK FOR 55 SECONDS. MAINTENANCE REMOVED AND REPLACED NR 1 LEFT HAND BATTERY PACK. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051227000932005122700093NM 2005 12 27 QXEA200501808 120051220A561080260012 WINDSHIELD DHAV DHC8 DHC8202 2809007NM COCKPIT FAILED A QXEAO OTHER O OTHER CRCRUISE 1 NM09355PH30 500 PDX FLIGHT NR 2132 FLIGHT LEVEL 220, FIRST OFFICERS WINDSHIELD SHATTERED. EMERGENCY DECLARED. LANDED WITHOUT INCIDENCE. MAINTENANCE REPLACED CO-PILOTS WINDSHIELD IAW Q200 AMM TASKS 56-10-11-000-801 AND 56-10-11-400-801. OPERATIONAL TEST OF WINDSHIELD HEAT GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051227000942005122700094EU 2005 12 27 USAA051632 120051221A5320F5347823620500 FLOOR SUPPORT AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 FOUND CORROSION -Y 1137 AT FRAME 73. BLENDED PER 51-74-00, REPLACED FLOOR SUPPORT PER 51-72-11, 51-42-11; DEFECT SIZE: .500 BY .400 BY .067". 2L72 4F RTA46NM 20051227000952005122700095EU 2005 12 27 USAA051633 120051221A5320F5331709020100 FLANGE AIRBUS330 A330323 3930335EU BS 53.2 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 FOUND FLANGE (LOWER FUSELAGE) ZONE 150, FS 53.2, STR 55 RT - STR 53-52 LT. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-72-11, DEFECT SIZE: 20 EA. 1/4" AREAS. 2L72 4F RTA46NM 20051227000962005122700096EU 2005 12 27 USAA051634 120051221A5320F5311351520000 FLOOR SUPPORT AIRBUS330 A330323 3930335EU STA 1139 -Y730 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 FOUND CORROSION STA 1139 -Y730. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-74-00, 51-42-11; CORROSION LEVEL 2; TASK C531172, DEFECT SIZE: .500 X .500 X .029". 2L72 4F RTA46NM 20051227001012005122700101NM 2005 12 27 USAA051639 120051221A5320 INTERCOSTAL BOEING737 7374B7 1384702NM BS 294.5-303.9 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19781AU 25020 FOUND CORROSION STA 294.5-303.9 STR 16L. REMOVED AND REPLACED FABRICATED INTERCOSTAL PER SRM 51-40-02, DEFECT SIZE: 1.5". 2L72 4F RTA16WE 20051227001032005122700103NM 2005 12 27 SWAA054072 120051221A534065C27314 STRINGER CLIP BOEING737 7373Q8 1384670NM BS 663 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051227001042005122700104NM 2005 12 27 SWAA054073 120051221A534065C27314 STRINGER CLIP BOEING737 7373Q8 1384670NM BS 663 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051227001052005122700105NM 2005 12 27 SWAA054074 120051220A275056970 MOTOR BOEING737 7373G7 1384595NM TE FLAPS INOPERATIVE A SWAAA UNSCHED LANDING F FLT CONT AFFECTED LDLANDING 1 SW29690SW 23783 DECLARED EMERGENCY, T/E FLAPS WOULD NOT FULLY EXTEND. FOUND HYDRAULIC FLAP DRIVE MOTOR SEIZED. REMOVED AND REPLACED FLAP DRIVE MOTOR PER MM. 2L72 4F RTA16WE 20051227001062005122700106NM 2005 12 27 SWAA054060 120051220A3350BR2013 LIGHT BOEING737 7373H4 1384600NM CABIN DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29357SW 26594 DURING SCHEDULED RON CHECK, FOUND EEPLS STRIP DAMAGED. REMOVED AND REPLACED EEPLS SECTION PER MM. 2L72 4F RTA16WE 20051227001112005122700111NM 2005 12 27 SWAA054065 120051221A53206551698 SPLICE BOEING737 7373H4 1384600NM BS 908 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29623SW 27933 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER SPLICE CRACKED AT BS 908, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20051227001122005122700112NM 2005 12 27 SWAA054066 120051221A53116546558 FRAME BOEING737 7373H4 1384600NM BS 908 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29623SW 27933 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 908, STR 8R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051227001132005122700113NM 2005 12 27 SWAA054067 120051221A53116546526 FRAME BOEING737 7373H4 1384600NM BS 400 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29623SW 27933 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051227001142005122700114 2005 12 27 SWAA054068 420051221A25656557463 GIRT BAR BOEING737 7373Q8 1384670NM L1 DOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED 1/2D CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD BRACKET CORRODED AT BS 312, LBL 56. REMOVED AND REPLACED BRACKET PER SRM. 2L72 4F RTA16WE 20051227001152005122700115NM 2005 12 27 SWAA054069 120051221A53116546540 FRAME BOEING737 7373Q8 1384670NM BS 639 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, STR 17L. REPAIRED FRAME PER SWA EA. 2L72 4F RTA16WE 20051227001182005122700118NM 2005 12 27 PIDA20050198 120051206A3350 LIGHT BOEING737 737228 13844AGNM CABIN INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05252TR 23001 AFT EMERGENCY EXIT LIGHTS AT SEAT 9D AND SEAT 12D ARE INOP. REPLACED LIGHT ASSEMBLY ON SEAT 9D AND 12D. OPS CHECKS GOOD. 2L72 4F RTA16WE 20051227001192005122700119 2005 12 27 PIDA20050200 420051221A22101062038122 CONTROL PANEL BOEING737 7373G7 1384595NM AUTOPILOT MALFUNCTIONED A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05380WL 23218 AUTO PILOT LEVELING OFF 300 FEET ABOVE SELECTED MCP ALTITUDE. REPLACED MODE SELECT PANEL PER MM 22-11-00. OPS CHECKS OK. 2L72 4F RTA16WE 20051227001212005122700121NE 2005 12 27 AWHA5005 220051209A7314025323150 SPLINE CESSNA208 208B 2073701CE PWA PT6 PT6A114 52043NE MCAULY3DF36CB3DF36C526 GL DRIVE ASSY CORRODED E AWHAK NONE O OTHER ININSP/MAINT 1 WP17969FE 2951 208B0092 17219 981511 PRECAUTIONARY INSPECTION OF THE FUEL PUMP DRIVE SPLINE IN ACCORDANCE WITH PRATT AND WHITNEY PT6 MAINTENANCE MANUAL, FUEL PUMP COUPLING IN-SITU INSPECTION 73-10-02 PAGE 210, PARAGRAPH 8D, MAINTENANCE FOUND THE FUEL PUMP DRIVE SPLINE SEVERELY CORRODED AND DAMAGED TO THE POINT OF NEAR FAILURE. THE FUEL PUMP ASSEMBLY WAS REPLACED WITH A FRESH OVERHAULED UNIT AND THE AIRCRAFT RETURNED TO SERVICE. 1H71 3T3 T A37CE E4EA 5 C 20051227001222005122700122NE 2005 12 27 5005120805 220051209A7314025323150 SPLINE SUNDSTRANDEM CESSNA208 208B 2073701CE PWA PT6 PT6A114 52043NE MCAULY3DF36CB3DF36C526 GL DRIVE ASSY CORRODED E AWHAK NONE O OTHER ININSP/MAINT 1 WP17969FE 2951 846 208B0092 17219 981511 PRECAUTIONARY INSPECTION OF THE FUEL PUMP DRIVE SPLINE IN ACCORDANCE WITH PRATT AND WHITNEY PT6 MAINTENANCE MANUAL, FUEL PUMP COUPLING IN-SITU INSPECTION 73-10-02 PAGE 210, PARAGRAPH 8D, MAINTENANCE FOUND THE FUEL PUMP DRIVE SPLINE SEVERELY CORRODED AND DAMAGED TO THE POINT OF NEAR FAILURE. THE FUEL PUMP ASSEMBLY WAS REPLACED WITH A FRESH OVERHAULED UNIT AND THE AIRCRAFT RETURNED TO SERVICE. 1H71 3T3 T A37CE E4EA 5 C 20051227001242005122700124NE 2005 12 27 2005F00115 220051209A7314025323150 SPLINE SUNDSTRANDEM CESSNA208 208B 2073701CE PWA PT6 PT6A114 52043NE MCAULY3DF36CB3DF36C526 GL DRIVE ASSY CORRODED E AWHAK NONE O OTHER ININSP/MAINT 1 WP17969FE 2951 846 208B0092 17219 981511 PRECAUTIONARY INSPECTION OF THE FUEL PUMP DRIVE SPLINE IN ACCORDANCE WITH PRATT AND WHITNEY PT6 MAINTENANCE MANUAL, FUEL PUMP COUPLING IN-SITU INSPECTION 73-10-02 PAGE 210, PARAGRAPH 8D, MAINTENANCE FOUND THE FUEL PUMP DRIVE SPLINE SEVERELY CORRODED AND DAMAGED TO THE POINT OF NEAR FAILURE. THE FUEL PUMP ASSEMBLY WAS REPLACED WITH A FRESH OVERHAULED UNIT AND THE AIRCRAFT RETURNED TO SERVICE. 1H71 3T3 T A37CE E4EA 5 C 20051227001252005122700125NE 2005 12 27 2005F00116 220051209A7314025323150 SPLINE SUNDSTRANDEM CESSNA208 208B 2073701CE PWA PT6 PT6A114 52043NE MCAULY3DF36CB3DF36C526 GL DRIVE ASSY CORRODED E AWHAK NONE O OTHER ININSP/MAINT 1 WP17969FE 2951 846 208B0092 17219 981511 PRECAUTIONARY INSPECTION OF THE FUEL PUMP DRIVE SPLINE IN ACCORDANCE WITH PRATT AND WHITNEY PT6 MAINTENANCE MANUAL, FUEL PUMP COUPLING IN-SITU INSPECTION 73-10-02 PAGE 210, PARAGRAPH 8D, MAINTENANCE FOUND THE FUEL PUMP DRIVE SPLINE SEVERELY CORRODED AND DAMAGED TO THE POINT OF NEAR FAILURE. THE FUEL PUMP ASSEMBLY WAS REPLACED WITH A FRESH OVERHAULED UNIT AND THE AIRCRAFT RETURNED TO SERVICE. 1H71 3T3 T A37CE E4EA 5 C 20051227001282005122700128NM 2005 12 27 P5CA0501415 120051125A7797 WIRE BOEING747 747341 13848AMNM GE CF6 CF650E2 30018NE ENGINE LOOSE A P5CAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 EA15355MC 23395 517824 FLIGHT CREW REPORTED NR 3 ENGINE EGT INOP. FOUND LOOSE WIRE AT HARNESS END (PYLON CONNECTION). SECURED WIRE, ALL OPS AND INDICATIONS NORMAL IAW MM 77-00-00. 2L74 4F4 FRTA20WE E23EA 20051227001292005122700129NM 2005 12 27 SWAA054049 120051220A55116547983 RIB BOEING737 7373H4 1384600NM HORIZONTAL STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29623SW 27933 DURING SCHEDULED D-CHECK, FOUND RT HORIZONTAL STAB L/E RIB CRACKED AT STAB STA 184.7. REMOVED AND REPLACED RIB PER SRM. 2L72 4F RTA16WE 20051227001322005122700132NM 2005 12 27 SWAA054052 120051220A2121215201 FAN BOEING737 7373Q8 1384670NM A/C BAY FAULTY A SWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW29672SW 23406 SMOKE ODOR IN CABIN. REMOVED AND REPLACED GASPER FAN PER MM. 2L72 4F RTA16WE 20051227001362005122700136NM 2005 12 27 SWAA054056 120051219A53126545819 PRESSURE PANEL BOEING737 7373Q8 1384670NM NLG WW CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED 1/2D CHECK, FOUND NLG W/W LEFT FWD SIDE PRESSURE PANEL CRACKED AT BS 240, WL 168.6. REPAIRED WEB PER SWA EA. 2L72 4F RTA16WE 20051227001372005122700137NM 2005 12 27 SWAA054057 120051219A53126545819 PRESSURE PANEL BOEING737 7373Q8 1384670NM NLG W/W CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED 1/2D CHECK, FOUND NLG W/W RIGHT FWD SIDE PRESSURE PANEL CRACKED AT BS 243.7, WL 168.5. REPAIRED WEB PER SWA EA. 2L72 4F RTA16WE 20051227001382005122700138NM 2005 12 27 SWAA054058 120051220A57556546451 SKIN BOEING737 7373Y0 1384671NM LT WING SPOILER DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED A2 CHECK, FOUND LEFT WING NR 2 SPOILER DELAMINATED. REMOVED AND REPLACED NR 2 SPOILER PER MM. 2L72 4F RTA16WE 20051227001392005122700139NM 2005 12 27 SWAA054059 120051220A3350MS155721 BULB BOEING737 7373Y0 1384671NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED A2 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. RELAMPED LIGHTS PER MM. 2L72 4F RTA16WE 20051227001422005122700142NM 2005 12 27 P5CA0501419 120051215A7711ED7472012 TRANSMITTER BOEING747 747283B 1384867NM PWA JT9 JT9D70A 52054NE ENGINE EPR FAILED A P5CAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA15921FT 21575 688856 ON TAKEOFF ROLL, CREW REPORTED NR 3 ENGINE EPR WOULD NOT ADVANCE ABOVE 1.2 EPR, FULL TRAVEL OF THROTTLE HAD NO EFFECT. TAKEOFF ABORTED AT 80 KTS IAS EPR ON NR 3 STAYED AT 1.2 UNTIL ENGINE SHUTDOWN. REPLACED EPR TRANSMITTER, PERFORMED LEAK CHECK AND RAN ENGINE. ALL PARAMETERS NORMAL. 2L74 4F4 F A20WE E3NE 20051227001442005122700144NM 2005 12 27 SWAA054000 120051217A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM GE CFM56 CFM563B1 13802NE BS 807 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29622SW 27932 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 807, STR 4L. REMOVED AND REPLACED CLIP IAW SRM. 2L72 4F4 FRTA16WE E2GL 20051227001452005122700145NM 2005 12 27 SWAA054001 120051217A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM GE CFM56 CFM563B1 13802NE BS 787 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29622SW 27932 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 787, STR 4L. REMOVED AND REPLACED CLIP IAW SRM. 2L72 4F4 FRTA16WE E2GL 20051227001462005122700146NM 2005 12 27 SWAA054003 120051217A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM GE CFM56 CFM563B1 13802NE BS 747 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29622SW 27932 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 747, STR 4L. REMOVED AND REPLACED CLIP IAW SRM. 2L72 4F4 FRTA16WE E2GL 20051227001472005122700147NM 2005 12 27 SWAA054004 120051217A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM GE CFM56 CFM563B1 13802NE BS 727E CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29622SW 27932 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727E, STR 4L. REMOVED AND REPLACED CLIP IAW SRM. 2L72 4F4 FRTA16WE E2GL 20051227001482005122700148NM 2005 12 27 SWAA054005 120051217A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM GE CFM56 CFM563B1 13802NE BS 727D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29622SW 27932 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727D, STR 4L. REMOVED AND REPLACED CLIP IAW SRM. 2L72 4F4 FRTA16WE E2GL 20051227001492005122700149NM 2005 12 27 SWAA054006 120051217A5320BAC15171489 ANGLE BOEING737 7373H4 1384600NM GE CFM56 CFM563B1 13802NE BS 270 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29622SW 27932 DURING SCHEDULED D CHECK, FOUND COCKPIT FLOOR Z-CHORD CORRODED AT BS 270, LBL 10, WL 208. REMOVED AND REPLACED Z-CHORD IAW SRM. 2L72 4F4 FRTA16WE E2GL 20051227001502005122700150NM 2005 12 27 SWAA054007 120051217A53116546555 FRAME BOEING737 7373H4 1384600NM GE CFM56 CFM563B1 13802NE BS 867 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29622SW 27932 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME IAW SRM. 2L72 4F4 FRTA16WE E2GL 20051227001522005122700152 2005 12 27 SWAA054011 420051216A2565D31354 SLIDE BOEING737 7373H4 1384600NM GE CFM56 CFM563B1 13802NE L1 DOOR MISINSTALLED A SWAAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW29647SW 27717 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE IAW MM. 2L72 4F4 FRTA16WE E2GL 20051227001532005122700153NM 2005 12 27 SWAA054012 120051218A53116547959 FRAME BOEING737 7373G7 1384595NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29683SW 24008 DURING SCHEDULED SPECIAL VISIT, FOUND AFT CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 5 STOP FITTING. REMOVED AND REPLACED AFT CARGO DOOR FWD FRAME IAW SRM. 2L72 4F4 FRTA16WE E2GL 20051227001542005122700154NM 2005 12 27 SWAA054013 120051218A53116520723 FRAME BOEING737 7373G7 1384595NM GE CFM56 CFM563B1 13802NE FWD CARGO CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29683SW 24008 DURING SCHEDULED SPECIAL VISIT, FOUND FWD CARGO DOOR CUTOUT AFT FRAME CRACKED AT NR 5 STOP FITTING. REMOVED AND REPLACED FWD CARGO DOOR AFT FRAME IAW SRM. 2L72 4F4 FRTA16WE E2GL 20051227001562005122700156NM 2005 12 27 SWAA054015 120051218A53156546811 FLOORBEAM BOEING737 7373Q8 1384670NM GE CFM56 CFM563B1 13802NE BS 986 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FLOOR BEAM CORRODED AT BS 986.5, RBL 45. REMOVED AND REPLACED FLOORBEAM UPPER T-CHORD IAW SRM. 2L72 4F4 FRTA16WE E2GL 20051227001592005122700159 2005 12 27 SWAA054018 420051216A256563550 SLIDE BOEING737 7377H4 1384404NM CFMINTCFM567CFM567B22 13802NE L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29758SW 27873 DURING SCHEDULED HC 1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE IAW MM. 2L72 4F4 FRTA16WE E00055EN 20051227001602005122700160NM 2005 12 27 SWAA054019 120051216A56105893543130 WINDOW BOEING737 7377H4 1384404NM CFMINTCFM567CFM567B22 13802NE COCKPIT ARCED A SWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW29769SW 30588 R1 COCKPIT WINDOW ARCED. REMOVED AND REPLACED R1 WINDOW AND HEAT CONTROLLER IAW MM. 2L72 4F4 FRTA16WE E00055EN 20051227001642005122700164NM 2005 12 27 SWAA053827 120051201A2121215201 FAN BOEING737 7373H4 1384600NM A/C BAY FAULTY A SWAAK NONE O OTHER ININSP/MAINT 1 SW29378SW 26585 SMOKE SMELL IN AFT CABIN. GASPER FAN CONTROL CIRCUIT BREAKER POPPED. REMOVED AND REPLACED GASPER FAN IAW MM. 2L72 4F RTA16WE 20051227001662005122700166NM 2005 12 27 SWAA053829 120051201A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29418WN 29823 EEPLS STRIP INOP AT FWD END. REMOVED AND REPLACED STRIP IAW MM. 2L72 4F RTA16WE 20051227001672005122700167NM 2005 12 27 SWAA053830 120051201A53116520722 FRAME BOEING737 7373H4 1384600NM BS 440 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 17R. REPAIRED FRAME IAW SRM. 2L72 4F RTA16WE 20051227001712005122700171NM 2005 12 27 SWAA053834 120051130A53306545776 SKIN BOEING737 7373G7 1384595NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29671SW 23785 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR UPPER HINGE CUTOUT, FWD UPPER CORNER. REPAIRED SKIN IAW SRM. 2L72 4F4 FRTA16WE E2GL 20051227001722005122700172NM 2005 12 27 SWAA053837 120051130A53116546549 FRAME BOEING737 7373H4 1384600NM GE CFM56 CFM563B1 13802NE BS 767 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 767, BETWEEN STR 23L TO STR 23R. REMOVED AND REPLACED FRAME SECTION ISW SRM. 2L72 4F4 FRTA16WE E2GL 20051227001732005122700173NM 2005 12 27 SWAA053838 120051130A53116546551 FRAME BOEING737 7373H4 1384600NM GE CFM56 CFM563B1 13802NE BS 807 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 807, BETWEEN LBL 41 TO RBL 19. REMOVED AND REPLACED FRAME SECTION IAW SRM. 2L72 4F4 FRTA16WE E2GL 20051227001742005122700174NM 2005 12 27 ASAA0540403 120050816A53116546548109 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU BS 747, STR 4L CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 CRACKED FRAME AT BIN RAIL BSTA 747, STR 4L AND BL 0. REPAIRED SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051227001752005122700175NM 2005 12 27 ASAA0540404 120050816A53116558280511 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU BS 360 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 CRACKED FRAME AT BIN RAIL BSTA 360, BETWEEN STR 7L AND 8L. REPAIRED IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051227001762005122700176NM 2005 12 27 ASAA0540406 120050816A53206551629U501 SEAL DEPRESSOR BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FWD GALLEY DOOR CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 FWD GALLEY DOOR CUTOUT SEAL DEPRESSOR ABOVE UPPER HINGE CUTOUT IS CRACKED. REMOVED AND REPLACED FWD GALLEY DOOR CUTOUT SEAL DEPRESSOR ABOVE UPPER HINGE CUTOUT. (K) 2L72 4F4 FRTA16WE E21EU 20051227001782005122700178NM 2005 12 27 ASAA0540405 120050816A52416552871U503 SEAL DEPRESSOR BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU AFT GALLEY DOOR CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 AFT GALLEY DOOR CUTOUT SEAL DEPRESSOR CRACKED BELOW LWR HINGE CUTOUT. REMOVED AND REPLACED IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051227001792005122700179SO 2005 12 27 C2XA05SH139 120051218A491014526850401 FIREWALL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL AFT FUSELAGE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713553 145585 DURING C-CHECK MAINTENANCE FOUND APU FIREWALL CRACKED ON THE INSIDE, BETWEEN STRINGERS 9R AND 10R AT THE 3 O'CLOCK POSITION. MAINTENANCE INSTALLED REPAIR DOUBLER ON APU FIREWALL IAW SRM 53-32-13 FIG 204. AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20051227001812005122700181NM 2005 12 27 UPS05M45883 120051219A3510 OXYGEN MASK DOUG MD11 MD11F 3023600NM COCKPIT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01254UP 48406 FO O2 MASK FAILED TEST. SWAPPED F/O 02 MASK WITH 2ND OBSERVERS MASK IAW MM 35-13-10-4. 2L73 4F RTA22WE 20051227001832005122700183WP 2005 12 27 ABXA050371 120051207A57535910041504 VANE DOUG DC9 DC931 3022065WP TE FLAPS CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23943AX 47528 INBOARD FIXED VANE HAD 2 AREAS OF BULGING WITH POPPED RIVET HEADS. LOWER INBOARD AND UPPER OUTBOARD ALSO HAD WATER IN MOUNT ACCESS HOLE. REMOVED RIVETS, CHECKED CORROSION. REMOVED AND REPLACED FIXED VANE IAW DC9 SRM. 2L72 4F A6WE 20051221001422005122100142NM 2005 12 21 QXEA200501790 120051215A3233465509 ACTUATOR BOMBDRDHC8 DHC8402 1390042NM RT MLG MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09401QX9405 4031 BOI FLIGHT NR 2404, UPON GEAR RETRACTION AFTER TO, GEAR RETRACTED BUT RIGHT DOOR LIGHT REMAINED ILLUMINATED AND DOOR WAS VISUALLY CONFIRMED OPEN. AS PER EA CHECKLIST, GEAR WAS CYCLED. DURING THE DOWN CYCLE, GEAR EXTENDED NORMAL AND DOOR CLOSED. DURING CYCLE UP, GEAR RETRACTED NORMAL AND DOOR CLOSED. GEAR EXTENDED NORMAL FOR LANDING IN BOI. AIRCRAFT FERRIED TO PDX. MAINTENANCE REMOVED RT MLG RETRACT ACTUATOR IAW Q400 AMM TASK 32-31-11-000-801. INSTALLED SERVICEABLE MLG ACTUATOR IAW Q400 TASK 32-31-11-400-801. COMPLIED WITH INSTALLATION OF RT MLG ACTUATOR IAW Q400 AMM TASK 32-31-11-400-801. OPS TEST GOOD. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051221001502005122100150EA 2005 12 21 COMA0560723 120051213A3220 SWITCH CNDAIRCL600 CL6002B19 1900309EA HUMAN ERROR NONE A COMAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 SO01420CA 7451 FLIGHT 5581- NLG DOORS MESSAGE AFTER T/O. FOUND MAINTENANCE SWITCH IN THE "OPEN" POSITION. SELECTED SWITCH TO CLOSED. 2L72 4F RTA21EA 20051221001902005122100190NM 2005 12 21 AMTA200501062 120051113A3397 GROUND WIRE BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE CABIN LOOSE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11558TZ 32592 LEFT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. SECURED GROUND STUD 4554 WIRE IAW WDM. LIGHTS OPS CHECK NORMAL. (K) 2L72 4F4 FRTA2NM E12EU 20051221002002005122100200WP 2005 12 21 AALA20050824 120051218A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21242AA 49255 LGA - EMERGENCY LIGHTS THROUGHOUT CABIN INOPERATIVE. REPLACED BATTERY PACKS AT B27, B28, B5104 AND B5107 FOR EMERGENCY LIGHTS THROUGHOUT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051221002022005122100202NM 2005 12 21 AALA20050814 120051212A3350 BATTERY PACK BOEING757 757223 1384957NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21629AA 24587 STL - EMERGENCY ESCAPE PATH LIGHTING AT ROWS 16 TO 24D INOPERATIVE. REPLACED BATTERY PACKS AT MID AND FORWARD CABIN AND BATTERY AND MODULE AT MID AND AFT CABIN FOR EMERGENCY ESCAPE PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20051221002042005122100204NM 2005 12 21 AALA20050816 120051213A3350 LIGHT BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21183AN 29593 LAX - EMERGENCY LIGHTS AT SEAT 36D INOPERATIVE. REPLACED LIGHT ASSEMBLY AT SEAT 36D FOR EMERGENCY LIGHTS AT SEAT 36D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20051221002062005122100206WP 2005 12 21 AALA20050810 120051210A3350 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW2133414 49325 SFO - CEILING EMERGENCY LIGHTS AT ROWS 23 TO 27 INOPERATIVE. REPLACED BATTERY PACK AT ROW 27 FOR CEILING EMERGENCY LIGHTS AT ROWS 23 TO 27. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051221002082005122100208WP 2005 12 21 AALA20050821 120051215A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21460AA 49565 LGA - OVERHEAD AISLE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS IN MID CABIN FOR OVERHEAD AISLE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051221002102005122100210EU 2005 12 21 AALA20050823 120051216A2782 JACKSCREW AIRBUS300 A300B4605R 3930308EU L/E SLAT INOPERATIVE A AALAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SW217076A 610 JFK - SLATS DID NOT EXTEND UPON LANDING. REPLACED LEFT HAND 3 AND 6 AND RIGHT HAND 6 SLAT JACKSCREWS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20051221002122005122100212WP 2005 12 21 AALA20050834 120051123A3233 ACTUATOR DOUG DC9 DC983 3022083WP LT MLG CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21968TW 53618 TUL - LEFT HAND MAIN LANDING GEAR SUPPORT FITTING ASSEMBLY RETRACT ACTUATOR FITTING BORE HAS CORROSION IN LARGE BORE. AREA IS 1.75 INCHES BY 2.2515 INCHES. FINAL MEASUREMENT IS 2.253 INCHES IN 1.75 INCH BUSHING AREA. LOCAL BLEND WHERE BUSHING DOES NOT CONTACT FROM SMALL BORE TO 1.98 INCH FROM FACE. DIMENSION DEPTH 2.270 AND .75 INCH IN DIAMETER. LEFT HAND MAIN LANDING GEAR SUPPORT FITTING ASSEMBLY RETRACT ACTUATOR FITTING BORE AREA REWORKED IN ACCORDANCE WITH ESO 80559 DATED NOVEMBER 22 2005. 2L72 4F RTA6WE 20051222000152005122200015NM 2005 12 22 ASAA0580519 120050926A5330593643673 SKIN DOUG MD80 MD83 3023681NM FS 1237-1238 LIGHTNING STRIKEA ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - DURING HV-CHECK, FOUND FUSELAGE HAS LIGHTNING DAMAGE. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLER AND INTERNAL DOUBLER. (M) 2L72 4F RT 20051222000192005122200019NM 2005 12 22 ASAA0570050 120050729A5321453A161043 FLOOR PANEL BOEING737 737790 13844CNNM FS 440-500 CUT A ASAAK NONE O OTHER ININSP/MAINT 1 NM02645AS 33011 PAE - CUT IN FLOOR REPORT BY GROUND IN CARGO PIT 3, NR 2 FLOORBOARD. REMOVED AND FABRICATED NEW NR 2 FLOOR PANEL THEN INSTALLED IAW SRM 53-30-53. (M) 2L72 4F RTA16WE 20051222000242005122200024NM 2005 12 22 ASAA05700064 120050921A5320146A75011 FLOOR SUPPORT BOEING737 737790 13844CNNM FS 773 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02623AS 30166 PAE - DURING CHECK, FOUND CORROSION ON FLOOR SUPPORT. REPAIRED IAW SRM 53-00-53. (M) 2L72 4F RTA16WE 20051222000332005122200033NM 2005 12 22 ASAA05700060 120050921A5347146A750125 SEAT TRACK BOEING737 737790 13844CNNM FS 773 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02623AS 30166 PAE - DURING C-CHECK, FOUND CORROSION ON FLOOR TRACK AT BS 773. REPAIRED IAW SRM 53-00-53. (M) 2L72 4F RTA16WE 20051222000382005122200038EA 2005 12 22 COMA0560740 120051219A304016591 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA WINDSHIELD HEAT FAULTY A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01484CA8929 7702 FLIGHT 5201 - EN ROUTE LEX-DCA RECEIVED A RIGHT WINDSHIELD HEAT CAUTION MESSAGE. FLIGHT DIVERTED TO CVG. REPLACED THE WINDSHIELD HEAT CONTROLLER. 2L72 4F RTA21EA 20051222000392005122200039SO 2005 12 22 C2XA05IA143 120051213A3350RPS1B POWER SUPPLY EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2717115 145666 IAH - DURING MAINTENANCE INSPECTION THE OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT POWER SUPPLY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20051222000632005122200063WP 2005 12 22 AALA20050827 120051218A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21271AA 49293 LGA - CABIN EMERGENCY CEILING LIGHTS AT ROWS 3DEF, 6DEF, 13DEF, 27DEF AND 11AB AND 27AB INOPERATIVE. REPLACED BATTERY PACK AT B5102, B5104, B5106, AND B5100 FOR CABIN EMERGENCY CEILING LIGHTS AT ROWS 3DEF, 6DEF, 13DEC, 27DEF, 11AB AND 27AB. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20051222000752005122200075 2005 12 22 2005UALA01476 420051215A256562774414 SLIDE 62510101 BOEING777 777222 1385219NM PWA PW4077PW4077 NE FLAPPER VALVES UNSERVICEABLE A UALAK NONE O OTHER ININSP/MAINT 1 WP29777UA 1702 26916 ASPIRATORS, TOP & BOTTM LEAKING FROM THE FLAPPER VALVES. SLIDE/RAFT WAS REMOVED FROM AIRCRAFT AT NORMAL MAINTENANCE INTERVAL. ASPIRATOR FLAPPER VALVES WERE OBSERVED LEAKING DURING SLIDE/RAFT OVERHAUL AIR RETENTION TEST. SPECIFIC CAUSE OF LEAK WAS NOT DETERMINED. ASPIRATORS WERE REPLACED. 2L72 4F4 FRTT0001SE E46NE 20051222000812005122200081NM 2005 12 22 USAA051587 120051220A5311 FRAME BOEING737 7374B7 1384702NM BS 615 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 STA 615 RT SIDE I/B UPPER CORD ANGLE JUST BELOW CABIN FLOOR CRACKED. REMOVED DAMAGE, FAB & INSTALLED FILLERS & DOUBLERS IAW TR 53062-01, DEFECT SIZE: 1.5 INCH CRACK IN THE FRAME. 2L72 4F RTA16WE 20051222000902005122200090NM 2005 12 22 USAA051596 120051220A5311 FRAME BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19591US 23936 FWD SERVICE DOOR CUTOUT FWD FRAME CRACKED AT UPPER STOP FITTING LOWER O/B CORNER. REPLACED FRAME SECTION IAW SRM 51-30, DEFECT SIZE: .25 INCH LONG CRACK. 2L72 4F RTA16WE 20051222000922005122200092NM 2005 12 22 USAA051585 120051220A5310 BEAM BOEING737 737301 1384611NM BS 870 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19591US 23936 BS 870, WL 208, RBL 60 CRACKED. EDDY INSPECTION CONFIRMS SMALL AREA OF DISPLACED METAL ON BEAM EDGE IAW SRM 53-60-13, DEFECT SIZE: .5 INCH CRACK. 2L72 4F RTA16WE 20051222000972005122200097EU 2005 12 22 USAA051611 120051220A5347F53311325200 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 SEAT TRACK - Y450 FR 49 CORRODED. BLEND AREA PER SRM 51-74-00; TRACK REPLACED PER SRM 53-31-15, 51-72-11; CORR LEVEL 2; TASK C53317001, DEFECT SIZE: 3 X 1 INCH. 2L72 4F RTA46NM 20051222000982005122200098EU 2005 12 22 USAA051610 120051220A5347F5331325200 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 FR 47 Y450 CORRODED. BLENDED OUT PER SRM 51-74-00; CORR LEVEL 2; TASK C53317001, DEFECT SIZE: 1 X 1 X .025 INCH. 2L72 4F RTA46NM 20051222001012005122200101EU 2005 12 22 USAA051606 120051220A5347F53311325200 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 SEAT TRACK - Y450 FR 48 CORRODED. BLENDED AND REPLACED TRACK PER SRM 53-31-15, 51-74-00, 51-72-11; CORROSION LEVEL 2; TASK C53317001, DEFECT SIZE: 3 X 1 INCH. 2L72 4F RTA46NM 20051222001032005122200103EU 2005 12 22 USAA051604 120051220A5347F53326552203 SEAT TRACK AIRBUS330 A330323 3930335EU Y246 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 SEAT TRACK - Y2462 CORRODED BETWEEN FR 53.8 & FR. 53.9. BLENDED AREA AS PER 51-74-00, TRACK REPLACED PER 53-31-15, DEFECT SIZE: 2 X 1 INCH AREA. 2L72 4F RTA46NM 20051222001062005122200106EU 2005 12 22 USAA051615 120051220A5347F57110568205 SEAT TRACK AIRBUS330 A330323 3930335EU Y450 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 SEAT TRACK -Y450 FR 40.2 CORRODED. BLEND AREA PER SRM 51-74-00; REPLACED TRACK PER 53-31-15, 51-72-11, DEFECT SIZE: 3 X 1 INCH. 2L72 4F RTA46NM 20051222001072005122200107EU 2005 12 22 USAA051609 120051220A5347F53311325200 SEAT TRACK AIRBUS330 A330323 3930335EU FR 48 Y450 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 FR 48 Y450 CORRODED. BLENDED OUT PER SRM 51-74-00, PART REPLACED PER 53-31-15, DEFECT SIZE: .5 X .5 X .010 INCH. 2L72 4F RTA46NM 20051222001092005122200109NE 2005 12 22 EMB05019 220051219A73204120T00P42 FADEC EMB ERJ170ERJ170100 EU GE CF34 CF34* NE ZONE 200 FAULTY A USAAK NONE O OTHER ININSP/MAINT 1 EA19821MD3595 000042 RMAIE096 PIT - DUE TO HISTORY OF ENGINE 1, NO DISPATCH AND ENGINE 1 FADEC FAULT. REPLACE FADEC 1. MAINTENANCE REMOVED AND REPLACED NR 1 FADEC. NO FAULTS NOTED, OPERATIONAL CHECK IS GOOD. 2L74 4F4 FRTA56NM E15NE 20051222001142005122200114EA 2005 12 22 COMA0560735 120051218A2121 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA COOLING FAN FALSE ACTIVATIONA COMAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO01781CA 7312 FLIGHT 5007 - DISPLAY COOL CAUTION. INSPECTED AND FOUND NO DEFECTS. SYSTEM OPERATION CHECK SATISFACTORY. 2L72 4F RTA21EA 20051222001172005122200117SO 2005 12 22 C2XA05TY063 120051217A532014521713005 FLOOR SUPPORT EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712967 145133 TYS - DURING A SCHEDULED INSPECTION THE AFT DOUBLER ON RIGHT OMEGA BEAM WAS FOUND CORRODED AT FRAME 20. MAINTENANCE REMOVED THE OLD DOUBLER, FABRICATED AND INSTALLED A NEW DOUBLER, ALODINED AND PRIMED IAW EMB-145-SRM-51-40-02/03/06 AND CMP-51-21-04/05/06. 2L72 4F RTT00011AT 20051227000022005122700002SO 2005 12 27 C2XA05TY064 120051217A531114523051401 FRAME EMB 145 EMB145 3260210SO FUSELAGE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712967 145133 TYS - DURING A SCHEDULED INSPECTION CHAFFING WAS FOUND ON FRAME 65 BETWEEN STRINGERS 2L AND 3L. MAINTENANCE REPAIRED FRAME 65 IAW EMB-145-SRM-53-00-04 PAGE 211, FIGURE 206. 2L72 4F RTT00011AT 20051227000112005122700011EU 2005 12 27 AWXA200501546 120051218A4990 OIL SYSTEM AIRBUS320 A320232 3930326EU APU LOW A AWXAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CRCRUISE 1 WP28656AW 1079 CMH - DIVERSION - FLT 683 - DURING FLIGHT, DEPARTED FROM PHX EN ROUTE TO EWR, APU AUTO SHUTDOWN. THE NR 2 GENERATOR WAS ON MEL. CREW DIVERTED TO CMH AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE SERVICED THE APU WITH THREE QUARTS OF OIL. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA28NM 20051227000122005122700012 2005 12 27 AWXA200501547 420051218A3414 INDICATOR BOEING757 7572S7 1384962NM AIRSPEED FAILED A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28902AW 23322 DFW - ABORTED TAKEOFF - FLT 654 - CREW REPORTED THAT ON TAKEOFF ROLL, THE F/O GOT MACH AND AIRSPEED FLAGS ON THE AIRSPEED INDICATOR AT 80 KT. F/0'S AIRSPEED NEEDLE WAS READING ZERO. CREW ABORTED TAKEOFF AT 80 KNOTS AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED OPERATIONAL CHECKS IAW BOEING 757-200 MM 34-13-02-4. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA2NM 20051227000262005122700026WP 2005 12 27 ABXA050365 120051019A53131375211 LONGERON DOUG DC8 DC863F 302198FWP BS 598 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 FORWARD CARGO BAY, CORROSION IN LONGERON 36, STA 598 OUT OF LIMITS. REPAIRED LONGERON 36 IAW DC8 SRM 53-2-2 AND SPLICE WITH NEW SECTION FROM EXTRUSION P/N: S2645716 IAW DC8 SRM 53-2-2-, PG 6. 2L74 4F 4A25 20051227000382005122700038NM 2005 12 27 DHL2005765520 120051118A5320 FLOOR SUPPORT BOEING727 727264 138408MNM BS 644 CORRODED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15765AT 23014 FWD PIT FLOOR SUPPORT HAS CORROSION AROUND FASTENERS HOLES LWR SIDE STA 644 LBL 9. REMOVED CORRODED AREA. FABRICATED AND INSTALLED REPAIRS 8.5" BY .8" BY 1.2" FROM BAC1517-1507 AND 22" BY .75" BY 1.3" BY 1.0" FROM AND10134-1204 IAW B727 SRM 51-40-3 FIG 1, PG 1. 2L73 4F A3WE 20051227000422005122700042NM 2005 12 27 DHL2005765525 120051118A5753 SKIN BOEING727 727264 138408MNM FORE FLAP CHAFED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15765AT 23014 FOUND RT WING O/B T/E FORE FLAP, I/B END AT TOP SKIN HAS 2 CHAFE MARKS. FABRICATED AND INSTALLED REPAIR DOUBLER 7.5" BY 4" FROM 2024-T3 .063 IAW B727 SRM 51-10-2 AND B727 MM 51-20-11 AND SRM 51-30-2. 2L73 4F A3WE 20051227000582005122700058 2005 12 27 AWXA200501572 420051217A23106225272001 TRANSCEIVER BOEING757 7572G7 1384963NM HF SYSTEM INOPERATIVE A AWXAA UNSCHED LANDING O OTHER CRCRUISE 1 WP28908AW681 24233 PHX - AIR TURN BACK - FLT 932 - PRIOR TO ETOPS ENTRY CREW REPORTED, WAS UNABLE TO TRANSMIT ON THE LEFT HF AT ALL STATIONS. AIRCRAFT RETURNED TO PHX AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED THE LT HF RT. OPERATIONAL CHECKS WERE GOOD. VENDOR CONFIRMED FAILURE DUE TO BEING OUT OF CALIBRATION. THE UNIT WAS REPAIRED AND TESTED IAW CMM 23-10-70 REV.6 2L72 4F RTA2NM 20051227000652005122700065EU 2005 12 27 USAA051619 120051221A5347F57110568205 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 FOUND SEAT TRACK -Y450 FS 40.3. BLENDED AREA PER SRM 51-74-00, TRACK REPLACED PER SRM 53-31-15, 51-72-11; CORROSION LEV 2; TASK C5331700, DEFECT SIZE: 3" X 1". 2L72 4F RTA46NM 20051227000672005122700067EU 2005 12 27 USAA051621 120051221A5347F5347821720100 SEAT TRACK AIRBUS330 A330323 3930335EU -Y450 RT FR 73 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 FOUND CORROSION -Y450 RT FR 73. INSTALLED NEW SEAT TRACK PER SRM 51-42-11, 53-00-15, DEFECT SIZE: .500 X .500 X .050". 2L72 4F RTA46NM 20051227000772005122700077EA 2005 12 27 QXEA200501801 120051124A5310CC670341757 CROSSBEAM CNDAIRCL600 CL6002C10 1390015EA BS 280 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09604QX 10019 YYC - FLOOR SUPPORT BEAM AT STATION 280 IS CORRODED ALONG THE TOP FLANGE. REPLACED CROSSBEAM IAW REO 670-53-11-047. 2L72 4F RTA21EA 20051227000902005122700090 2005 12 27 QXEA200501783 420051214A34184100S01806 TIMER BOMBDRDHC8 DHC8402 1390042NM STICK PUSHER INOPERATIVE A QXEAO OTHER N FALSE WARNING CRCRUISE 1 NM09416QX5316 5316 4083 LAX - ON FLIGHT 2445, PUSHER SYSTEM FAILED, ILLUMINATED IN CRUISE. CHECKLIST PROCEDURE COMPLIED WITH. CAUTION LIGHT REMAINED ILLUMINATED. MAINTENANCE INSPECTED 115 VAC PANEL 2 CB'S. OHM'D POWER WIRES FOR AOA PROBES TO TIMER AND MONITOR UNIT AND PROBES. WIRING CHECKED GOOD. RANG OUT CONFIGURATION PLUG 9811-J5003. REMOVED AND REPLACED TIMER AND MONITOR UNIT. PERFORMED FUNCTIONAL TEST OF STALL WARNING STICK PUSHER, ALL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051227000992005122700099NM 2005 12 27 USAA051637 120051221A53206517688U165 SILL BOEING737 7374B7 1384702NM BS 290-360 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19781AU 25020 FOUND CORROSION BET STA 290-360, LBL 48 (CABIN FLOOR). REMOVED AND REPLACED NEW DOOR SILL CHORD PER SRM 51-40-02; CORROSION LEVEL 1; TASK C5310701 DEFECT SIZE: 25"L X 1.5"W X .039"D. 2L72 4F RTA16WE 20051227001022005122700102EU 2005 12 27 USAA051627 120051221A5313F53478211205 LONGERON AIRBUS330 A330323 3930335EU BS 80 -Y450 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 FOUND CORROSION FS 80 -Y450. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-72-11; CORROSION LEVEL 2; TASK C53415901, DEFECT SIZE: 1" X 1". 2L72 4F RTA46NM 20051227001342005122700134NM 2005 12 27 SWAA054054 120051219A53306545774 SKIN BOEING737 7373Q8 1384670NM BS 787 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, BETWEEN STR 20L TO STR 23L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051227001572005122700157NM 2005 12 27 SWAA054016 120051218A53206545410 FLOOR SUPPORT BOEING737 7373Q8 1384670NM GE CFM56 CFM563B1 13802NE BS 662 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED D-CHECK, FOUND NR 3 LONGITUDINAL FLOORBEAM UPPER T-CHORD CRACKED AT BS 662, RBL 24.82. REPAIRED FLOORBEAM IAW EA. 2L72 4F4 FRTA16WE E2GL 20051227001622005122700162NM 2005 12 27 SWAA053825 120051130A53306545774 SKIN BOEING737 7373H4 1384600NM BS 770 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29338SW 23960 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 770, STR 18L. REPAIRED SKIN IAW SRM. 2L72 4F RTA16WE 20051227001852005122700185WP 2005 12 27 ABXA050372 120051207A575399194701 SKIN DOUG DC9 DC931 3022065WP TE FLAPS CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23943AX 47528 UPPER AND LOWER SURFACES HAD CORROSION ON OUTBOARD REMOVEABLE TRAILING EDGE. REMOVED CORROSION, REMOVED AND REPLACED LOWER SKIN IAW DC9 SRM. 2L72 4F A6WE 20051227001882005122700188WP 2005 12 27 ASMF200512009 120051209A2410696233B CSD DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE LEFT FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23754RA516324783 49641 718197 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING LT ENGINE STARTING, THE LT CSD TEMPERATURE INCREASED AND WENT OUT OF RANGE AND LOAD AC WITH 7. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT CHECK, THE LT CSD AND HEAT EXCHANGER AIR/OIL ASSY WERE REPLACED IAW MM 24-10-01, TESTED CORRECT. 2L72 4F4 FRTA6WE E9NE 20051227001892005122700189WP 2005 12 27 ASMF200512010 120051209A2741 WARNING HORN DOUG DC9 DC987 3022087WP PWA JT8 JT8D* NE STAB TRIM ACTIVATED W ASMFK NONE J WARNING INDICATION ININSP/MAINT 1 SW23803ML 49726 DURING GROUND TESTS, THE CAUTION LONG TRIM STABILIZER WAS OUT OF RANGE ACTIVATING THE TAKEOFF ALARM. AIRCRAFT WAS SENT TO THE HANGAR AND THE TRIM STABILIZER WAS TESTED IAW MM 27-40-12 AND DURING OVERNIGHT CHECK, THE TAKEOFF ALARM SYSTEM WAS VERIFIED IAW MM 27-00-00 PAGE 214 STEP B, TESTED CORRECT. 2L72 4F4 FRTA6WE E2EA 20051227001902005122700190EU 2005 12 27 2005UALA01390 120051202A2130 CABIN PRESSURE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE MALFUNCTIONED A UALAA UNSCHED LANDING O OTHER CLCLIMB 1 WP29481UA 1559 CABIN PRESSURE PROBLEM. WHILE ON CLIMB OUT FLIGHT EXPERIENCED VENT SKIN VALVE FAULT, WHICH CAUSED A BLOWER FAULT. BLOWER WOULDN'T GO TO OVERRIDE. 'INLET' WORD ON PRESS PAGE IS AMBER. ACCOMPLISHED TSM 21-26-00-810-801 AND REPLACED AEVC (MR21002, 482-9059) PER MM-21-26-34. 2L72 4F4 FRTA28NM E40NE 20051227001912005122700191NE 2005 12 27 2005UALA01391 220051203A7200 ENGINE AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE NR 1 MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29812UA 850 V10070 NR 1 ENG EPR MODE FAILURE FOLLOWED BY INCREASED FUEL BURN RATIO. ENGINE 1 REVERTED FROM EPR MODE TO N1 MODE DUE TO THE APPARENT LOSS OF THE P2T2 PROBE HEATER. THIS IS PER DESIGN. CREW DECIDED TO DIVERT DUE TO POSSIBLE INCREASED FUEL BURN, SAFETY CONSIDERATION. MAINTENANCE FOLLOWED TSM AND REPLACED THE P2T2 PROBE POST TEST SHOWED A GOOD FIX. HOWEVER, THE PROBE CHANGE DID NOT FIX THIS ISSUE SEE SDR 2005UAL01415. P2T2 PROBE IS NOT A TRACKED PART, OFF UNIT SN NOT REPORTED UNIT LOST. 2L72 4F4 FRTA28NM E40NE 20051227001922005122700192NM 2005 12 27 2005UALA01392 120051201A3397 INVERTER BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29365UA 24534 CREW REPORTS ROW 15 TO AFT CABIN ESCAPE PATH LIGHTING INOPERATIVE. INVERTER REPLACED. 2L72 4F4 FRTA16WE E21EU 20051227001932005122700193EU 2005 12 27 2005UALA01393 120051202A3350 LIGHT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE SEATS 15-17 & 20INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29431UA 571 EMERGENCY LIGHTS AT SEATS 15-17, 20-23 INOPERATIVE. REPLACED EEL POWER SUPPLY. 2L72 4F4 FRTA28NM E40NE 20051227001942005122700194NM 2005 12 27 2005UALA01394 120051205A2913 PUMP AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE HYD SYSTEM MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29849UA 1649 ECAM BLUE ELECTRIC PUMP INDICATION ALONG WITH OTHER ENSUING PROBABLE ELECTRICAL ISSUES LED TO DECISION TO DIVERT FLIGHT. REPLACE B ELEC PUMP LOW PRESSURE DISPLAYED ON UPPER ECAM SCREEN. QTY CHECK OK AND PER SAMC RESELCTED PUMP ON AND SYSTEM APPEARED TO RECOVER. SUSPECT LOW PRESSURE THAT WAS DISPLAYED ON UPPER ECAM WAS ASSOCIATED WITH NR 1 ENG FEEDER CABLE BURNED PIN. REPLACED FEEDER CABLES & OPS CHKS GOOD. 2L72 4F4 FRTA28NM E40NE 20051227001952005122700195EU 2005 12 27 2005UALA01395 120051203A3350 LIGHT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE ROW 9C BROKEN A UALAK NONE L NO TEST ININSP/MAINT 1 WP29432UA 587 EEL LIGHT ASSY BROKEN AT 9C. REPLACED LIGHT ASSY. 2L72 4F4 FRTA28NM E40NE 20051227001962005122700196NM 2005 12 27 2005UALA01396 120051204A3397 WIRE BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU EMERGENCY LIGHT INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29347UA 24251 EEL LIGHT INOP AT AFT GALLEY CART STOWAGE. REPLACED RIBBON CABLE. 2L72 4F4 FRTA16WE E21EU 20051227001972005122700197NM 2005 12 27 2005UALA01397 120051204A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29199UA 28717 AFT GALLEY EMERGENCY CEILING LIGHT INOP. REPLACED LAMP. 2L74 4F4 FRTA20WE E24NE 20051227001982005122700198NM 2005 12 27 2005UALA01398 120051204A3350 POWER SUPPLY BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29199UA 28717 NR 2 LOWER EMERGENCY OVERWING LIGHT RT INOPERTIVE. REPLACED POWER SUPPLY. 2L74 4F4 FRTA20WE E24NE 20051227001992005122700199EA 2005 12 27 COMA0560657 120051130A2760 SPOILER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE RIGHT DEPLOYED A COMAO OTHER F FLT CONT AFFECTED CRCRUISE 1 SO01957CA 7109 UNCOMMANDED ROLL, RT FLIGHT SPOILER DEPLOYED. CND, NO FAULTS FOUND, REPLACED SECU AND SYSTEM 2A PRESSURE SWITCH FOR TROUBLESHOOTING. 2L72 4F4 FRTA21EA E15NE 20051227002112005122700211NM 2005 12 27 2005UALA01400 120051205A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE GALLEY INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29178UA 24385 EEL INOPERATIVE AFT GALLEY CROSS AISLE AT DR 3L AND INOPERATIVE AT RT SIDE AFT GALLEY AT DR 3RT. REPLACED EEL. 2L74 4F4 FRTA20WE E24NE 20051227002122005122700212NM 2005 12 27 2005UALA01401 120051204A3397 CONNECTOR BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT LOOSE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29199UA 28717 EMERGENCY LIGHT ON SEAT 48LT INOPERATIVE. RESECURED EEL CONNECTOR. 2L74 4F4 FRTA20WE E24NE 20051227002132005122700213NM 2005 12 27 2005UALA01402 120051204A2420 GENERATOR BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU NR 1 FAILED A UALAA UNSCHED LANDING GJ MULTIPLE FAILURE WARNING INDICATION CLCLIMB 1 WP29932UA 26658 DIVERTED, DUE TO A FAILED NR 1 GENERATOR AND WEATHER RADAR. MAINTENANCE REPAIRED WIRE W1502-201-18R AT THE NR 1 GENERATOR. THIS WIRE PROVIDES FIELD CURRENT TO THE GENERATOR. TO CORRECT THE RADAR MALFUNCTION, THE TRANSEIVER WAS REPLACED. THE SHOP TESTED THE UNIT AND FOUND NO DEFECTS. 2L72 4F4 FRTA16WE E21EU 20051227002142005122700214NM 2005 12 27 2005UALA01403 120051204A2150 A/C PACK BOEING757 757222 1384956NM PWA 2037 PW2037 NE LEFT SMOKE A UALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP29550UA 25398 AFTER TAKEOFF 1ST OFFICER NOTICED SMOKE FROM VENT SLIT BEHIND REAR WINDOW. COCKPIT NOTICED SMOKE & ODOR RISING FROM SIDE WINDOW VENTS DURING T-O ROLL AND C-O. TURNED OFF LEFT PACK, SMOKE DISSIPATED. NO ODOR WAS DETECTED IN MAIN CABIN. MAINTENANCE VERIFIED NORMAL PACK OPERATION. SMOKE AND ODOR WAS PROBABLY DUE TO GAS PATH WASH PERFORMED ON THE ENGINE. 2L72 4F4 FRTA2NM E17NE 20051227002152005122700215NM 2005 12 27 2005UALA01404 120051203A2120 HAZE BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU CABIN DETECTED A UALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 WP29928UA 26651 BLUE HAZE IN CABIN AFTER DOOR CLOSED FOR PUSHBACK. ODOR ACCOMPANIEDTHE HAZE. LT/RT WATER SEPERATOR COALESCER BAGS FOUND CONTAMINATED. REPLACED BAGS AND PERFORMED PACKS BURNED-OUT. 2L72 4F4 FRTA16WE E21EU 20051227002162005122700216NM 2005 12 27 2005UALA01405 120051201A2420 SPACER BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE APU GEN BURNED A UALAK NONE O OTHER ININSP/MAINT 1 WP29651UA 25389 BURNED SPACER BLOCKS BETWEEN APU GENERATOR 3 CABLES. FAILING SPLICE INSTALLATIONS REVEALED A MISMATCH BETWEEN THE SPLICE AND CRIMPER USED. MANUFACTURERS' SPLICES AND CRIMPER DIES MUST BE USED AS A MATCHED SET; IF NOT, AN INCOMPLETE SWAGE WILL RESULT IN HEAT GENERATION FROM GAPS BETWEEN CABLE AND SPLICE SURFACES. UA DEVELOPING A CHANGE ORDER TO REPLACE OLD AL SPLICES WITH NEWER "COPALUM" VERSION, P/N AMP277161-1 IN THE APU GEN POWER FEEDER CABLES. 2L72 4F4 FRTA1NM E24NE 20051227002172005122700217NM 2005 12 27 05FDEA04386 120051220A5322 SHEAR TIE BOEING727 727200 138407ENM PWA JT8 JT8D9A 52048NE BS 950A CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 N01273 BS 950A S28-29R RBL10-15 SHEAR TIE HAS CORROSION. REMOVED AND REPLACED IAW SRM 51-30-2. 2L73 4F4 FRTA3WE E2EA 20051227002272005122700227NM 2005 12 27 05FDEA04403 120051222A5311 FRAME BOEING727 727100 1384036NM PWA JT8 JT8D7B 52053NE BS 1148 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 AFT CARGO COMPARTMENT, FRAME IS DENTED BETWEEN STR. 26 RT AND 23 RT BS, 1148 IN IB FLANGE. AFT CARGO COMPARTMENT FRAME AT BS 1148 BETWEEN STR 23R, AND 26R WAS FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 51-40-3. 2L73 4F4 FRTA3WE E2EA 20051227002282005122700228NM 2005 12 27 05FDEA04404 120051222A5311 FRAME BOEING727 727100 1384036NM PWA JT8 JT8D7B 52053NE BS 1148 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 N00987 AFT CARGO COMPARTMENT, FRAME IS DENTED BETWEEN STR 26 LT AND 27 LT BS 1148 ON IB FLANGE ** SD ** COMING. 2L73 4F4 FRTA3WE E2EA 20051228000042005122800004SO 2005 12 28 SIMA200532502 120051108A491012060288002 SUPPORT EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL APU MOUNT DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21613AE15292 145081 THE APU COWLING RT LOWER MOUNTING SUPPORT AREA WAS FOUND DAMAGED. FABRICATED A REINFORCEMENT DOUBLER. REPAIR DONE IAW SRM. (K) 2L72 4F4 FRTT00011ATTE6CH 20051228000082005122800008EA 2005 12 28 SWIA200516018 120051217A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07412SW 7101 MID CAB EMERGENCY LIGHTS WON'T COME ON. REPAIRED BROKEN WIRE ON TB 100-2 BY REPLACING PIN IAW RJ WM 20-17-00/10. 2L72 4F RTA21EA 20051228000092005122800009EA 2005 12 28 SWIA200516019 120051217A27507455001 CONTROL LEVER CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07978SW 7953 FLAPS FAIL CAUTION; FLAPS STUCK AT 30 DEGREES. REPLACED FLAP CONTROL LEVER IAW CRJ MM 27-51-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051228000102005122800010EA 2005 12 28 SWIA200516020 120051217A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLT SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07979SW 7954 "SPOILERON FAULT" STATUS MESSAGE. REPLACED RT OUTBOARD SPOILERON PCU IAW AMM 37-62-01. OPERATIONAL CHECK GOOD, PN: 27000-7, SN OFF: MAL-4408. 2L72 4F RTA21EA 20051228000112005122800011EA 2005 12 28 SWIA200516021 120051215A2750860D10018 FCU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION LDLANDING 1 NM07967SW 7872 FLAP FAIL CAUTION MESSAGE ON LANDING. REPLACED FECU PER CRJ 200 MM 27-51-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051228000122005122800012EA 2005 12 28 SWIA200516022 120051216A2781 SENSOR CNDAIRCL600 CL6002C10 1390015EA SLAT SYSTEM MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07742SK 10197 SLAT FAULT STATUS MESSAGE IS DISPLAYED. REPLACED LT IB SLAT DISCONNECT SENSOR PER CRJ MM 27-81-39. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051228000132005122800013EA 2005 12 28 SWIA200516023 120051209A2750766389L CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07762SK1362 1362 10226 "FLAPS HALFSPEED" STATUS MSG. REPLACED NR 1 SFECU IAW MM 27-51-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051228000142005122800014EA 2005 12 28 SWIA200516024 120051219A2751855D10011 SENSOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07935SW4848 4848 7725 FLAPS FAIL ON TAXI WHEN SELECTED FLAPS 20 DEG. REPLACED LEFT BPSU IAW MM 27-51-10. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051228000152005122800015EA 2005 12 28 SWIA200516025 120051219A5610 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT FAILED A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07417SW 7400 ON TAXI OUT, LEFT WINDSHIELD SHATTERED RETURNED TO GATE. REPLACED LEFT WINDSHIELD IAW MM 56-11-01, PN NP-139321-5 SN OFF 01130H7181. 2L72 4F RTA21EA 20051228000172005122800017EA 2005 12 28 SWIA200516027 120051210A2797 WIRE CNDAIRCL600 CL6002C10 1390015EA BPSU CONNECTOR DAMAGED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07715SK 10179 FLAP HALFSPEED MESSAGE. SPLICED AND REPAIRED WIRES AT NR 2 BPSU CONNECTOR P1 IAW 20-44-09. REPLACED SFECU IAW CRJ MM 27-51-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051228000182005122800018EA 2005 12 28 SWIA200516002 120051216A2741 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07592SW 7279 CA STAB TRIM INTERMITTENT, BOTH DIRECTIONS. REPLACED CAPTIANS TRIM SWITCH. IAW 27-41-05. OPERATIONAL CHECK GOOD IAW 27-41-01. 2L72 4F RTA21EA 20051228000212005122800021EA 2005 12 28 SWIA200516005 120051213A2741 SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07979SW 7954 BOTH STAB TRIM 1 AND 2 AND MACH TRIM DISCONNECTED INFLIGHT. REPLACED FO'S DISCONNECT SWITCH, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051228000262005122800026SO 2005 12 28 SIMA200532506 120051114A532014522178005 SILL EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21825AE8374 145589 THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED EXISTING AND INSTALLED SERVICEABLE SILL IAW SRM. (K) 2L72 4F4 FRTT00011ATTE6CH 20051228000272005122800027SO 2005 12 28 SIMA200532904 120051117A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21825AE 145589 THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 27. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED A DOUBLER, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (K) 2L72 4F4 FRTT00011ATTE6CH 20051228000282005122800028SO 2005 12 28 SIMA200530405 120051029A3150 WARNING LIGHT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL LAVATORY FALSE ACTIVATIONA SIMAB EMER. DESCENT N FALSE WARNING CLCLIMB 1 SW21692AE 14500866 LAVATORY SMOKE EICAS MESSAGE ILLUMINATED AFTER TAKEOFF. FOUND BLUE WATER SPILL ON BLEED DUCT IN LAVATORY. CLEANED BLUE WATER SPILL AND PERFORMED OPERATIONAL CHECK OF AIR CONDITIONING SYSTEM. PERFORMED FUNCTIONAL CHECK FLIGHT WITH NO DISCREPANCIES NOTED. AC RETURNED TO SERVICE. (K) 2L72 4T4 FRTT00011ATTE6CH 20051228000292005122800029EU 2005 12 28 KBM2005F00360 120051129A6410355A09103601 BEARING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE TAIL ROTOR OUT OF LIMITS E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19966SH1590 3787 HALF SHELL BEARINGS, UNIT BEYOND LIMITS. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051228000362005122800036CE 2005 12 28 TIM2005F00012 120051104A329711436406819 CIRCUIT BOARD BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA MLG SHORTED E TIMAO OTHER O OTHER NRNOT REPORTED 1 NM07195GA UB65 THE GEAR HANDLE PLACED IN THE DOWN POSITION, GEAR FAILED TO GO DOWN AND THE CIRCUIT BREAKER POPPED. FOLLOW INSPECTION, FOUND A BROKEN WIRE. (K) 2L72 4T4 TRTA24CE E4EA 20051228000492005122800049GL 2005 12 28 ALG2005F00103 220051124A753223073353 BLEED VALVE BELL 206 206L1 1182107SW ALLSN 250C 250C30P 03013GL ENGINE FAILED E ALGAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SW032618 45503 ON TAKEOFF, ENGINE COMPRESSOR STALLED AT 80 PERCNET. LANDED AIRCRAFT AND NOTIFIED MAINTENANCE. PERFORMED MM 179-04. NO DEFECTS NOTED. REMOVED AND REPLACED BLEEDVALVE. (K) 1G71 3U3 U H2SW E1GL 20051228000502005122800050SW 2005 12 28 ALG2005F00104 120051124A5610206540024 WINDSHIELD BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL COCKPIT CRACKED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03362AL 51471 A CRACK WAS NOTICED IN THE UPPER EDGE OF THE PILOTS WINDSCREEN. REPLACED BOTH LT AND RT WINDSHIELD. (K) 1G71 3U3 U H2SW E1GL 20051228000562005122800056GL 2005 12 28 ALG2005F00098 220051201A72614369 CAP BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL ENGINE OIL LEAKING E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW033896W 3197 AFTER OPS CHECK FLIGHT, AN OIL LEAK WAS NOTED. FOUND OIL LEAKING FROM ENGINE RESERVOIR CAP STEM. REPLACED CAP ASSEMBLY. (K) 1G71 3U3 U H2SW E4CE 20051228000572005122800057SW 2005 12 28 ALG2005F00092 120051127A2497 WIRE BELL 206 206L1 1182107SW ALLSN 250C 250C30P 03013GL STARTER GEN BROKEN E ALGAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW0340LP 45233 GENERATOR LIGHT ILLUMINATED IN FLIGHT. PERFORMED EMERGENCY PROCEDURE IAW CHECKLIST. FOUND BROKEN WIRE AT BATTERY CONTROL RELAY. REPLACED TERMINAL END OF WIRE. REPLACED STARTER/GENERATOR BRUSHES DUE TO INTERMITTENT OPERATION DURING OPS, CHECK. (K) 1G71 3U3 U H2SW E1GL 20051228000592005122800059SW 2005 12 28 ALG2005F00116 120051113A6340407375008101 INDICATOR BELL 407 407 1182206SW DUAL TAC UNKNOWN E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03627AL 53284 ON PREFLIGHT, FOUND 5 SEPARATE DEBONDED AREAS AND A CRACK IN THE WINDSHIELD. REMOVED AND REPLACED DUAL TAC GAUGE. (K) 1G71 3U O H2SW 20051228000642005122800064SO 2005 12 28 K2Z2005F00001 220051106A7200AEC534857063S GASKET CESSNA414 414 2075908CE CONT O520 TSIO520* 17040SO MCAULY3AF32C3AF32C* GL ROCKER BOX FAILED E K2ZAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 NM11414AW 4140520 R228062R 970535 PILOT NOTED DROP IN ENGINE OIL PRESSURE IN CRUISE FLIGHT. POSTFLIGHT INSPECTION REVEALED SILICON GASKET (SUCKED) INTO THE ROCKER BOX ALLOWING SUBSTANTIAL OIL LOSS. ENGINE SHUTDOWN, PROP FEATHERED, PRECAUTIONARY LANDING ACCOMPLISHED WITHOUT INCIDENT. (K) 1L72 3O3 ORTA7CE E8CE 5 CP22EA 20051228000732005122800073EA 2005 12 28 A6WA200540352 120051210A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS FAILED A A6WAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL31464AW 7890 FLAPS FAILED AT 20 DEGREES ON APPROACH. NO DEFECTS NOTED. (K) 2L72 4F4 FRTA21EA E15NE 20051228000762005122800076SO 2005 12 28 SIMA200531101 120051103A2560P2070005120 CRADLE EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FLASHLIGHT BROKEN A SIMAK NONE O OTHER ININSP/MAINT 1 SW21703MR 145173 FLIGHT ATTENDANT FLASHLIGHT OVER ROW 13 WILL NOT STAY IN FLASHLIGHT CRADLE. REPLACED FLASHLIGHT CRADLE ASSY IAW SRM. AC RETURNED TO SERVICE. (K) 2L72 4F4 FRTT00011ATTE6CH 20051228000802005122800080SO 2005 12 28 SIMA200532202 120051115A2720 WARNING LIGHT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL RUDDER FALSE ACTIVATIONA SIMAO OTHER N FALSE WARNING LDLANDING 1 SW21633AE 145148 DURING LANDING FLARE EICAS MESSAGE RUDDER SYSTEM ONE AND 2 INOPERATIVE. NO RUDDER CONTROL DURING REMAINDER OF LANDING OR DURING TAXI. PERFORMED OPERATIONAL CHECK OF THE RUDDER SYSTEM WITH NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. (K) 2L72 4T4 FRTT00011ATTE6CH 20051228000822005122800082SO 2005 12 28 SIMA200532201 120051115A5210 STRUCTURE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL PAX DOOR GROUND DAMAGE A SIMAK NONE W INADEQUATE Q C TXTAXI/GRND HDL 1 SW21941LT 14500926 AIRCRAFT WAS STRUCK BY JETBRIDGE CAUSING DAMAGE TO PASSENGER ENTRY DOOR. AIRCRAFT WAS FERRIED TO MAINTENANCE. DOOR REPAIRED WITH AN EXTERNAL DOUBLER AT DAMAGE CORNER IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4T4 FRTT00011ATTE6CH 20051228000842005122800084SO 2005 12 28 SIMA200532501 120051114A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21825AE8374 145589 THE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. CUT OUT SECTION OF BEAM TO REMOVE CORROSION. PREPARED A DOUBLER, FILLER, SHIMS AND A PLATE. REPAIR DONE IAW SRM. (K) 2L72 4F4 FRTT00011ATTE6CH 20051228000852005122800085SO 2005 12 28 SIMA200532905 120051117A531314533888001 STRINGER EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21825AE8374 145589 STRINGER 19L WAS FOUND TO BE CHAFED AT FRAME 52. BLENDED THE CHAFED AREA AND APPLIED EA 934. FRABRICATED A REPAIR ANGLE AND 2 SHIMS. REPAIR DONE IAW SRM. (K) 2L72 4F4 FRTT00011ATTE6CH 20051228000872005122800087SO 2005 12 28 SIMA200532510 120051115A5330AL2024T3 SKIN EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL FR22A/23 PUNCTURED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21610AE15337 145073 SKIN PUNCTURE ON RT FUSELAGE BETWEEN FRAMES 22A/23 AND STRINGER 15R. PERFORMED CUT OUT OF THE SKIN TO REMOVE THE DAMAGE. FABRICATED FILLER AND DOUBLER. REPAIR DONE IAW SRM. (K) 2L72 4F4 FRTT00011ATTE6CH 20051228000882005122800088SO 2005 12 28 FDK2005F00003 120051112A2120 SMOKE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL UNKNOWN DETECTED A FDKAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW07829MJ 145228 (REF: FO5011 - CNTRL NR 100129) THE CREW NOTED SMOKE IN THE CABIN AFTER APU START UP ON THE GROUND DURING PREFLIGHT INSPECTION. MAINTENANCE INSPECTED THE PLANE AND DETERMINED THAT THE APU WAS NOT RUNNING DURING DE-ICING AND INGESTED THE STRAY FLUID CAUSING THE SMOKE AND ODOR. (K) 2L72 4T4 FRTT00011ATTE6CH 20051228001052005122800105GL 2005 12 28 ALG2005F00119 220051101A7200 ENGINE SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL NR 1 FAILED E ALGAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 SW03522AL 760236 CAE890787 IN FLIGHT, NR 1 ENGINE T-5 INCREASED IN TEMPERATURE, AFTER LANDING, NOTIFIED MAINTENANCE. A POWER CHECK REVEALED THAT NR 1 ENGINE WAS A -7. REMOVED AND REPLACED ENGINE WITH A SERVICEABLE ASSEMBLY IAW MM. (K) 1G72 3U3 U H1NE E1GL 20051228001062005122800106 2005 12 28 ALG2005F00096 420051203A3100 INDICATOR SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL COCKPIT FAILED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03518AL 760134 E-DISPLAYED 730 ON MGT GAUGE ENROUTE. NO FLASH OR CHECK LIGHT. NO PLATFORMS LARGE ENOUGH FOR 2 HELICOPTERS IN VICINITY. NO RECORDED ACCUMULATED FAULTS. MGT GAUGE NORMAL. (K) 1G72 3U3 U H1NE E1GL 20051228001072005122800107NE 2005 12 28 ALG2005F00099 120051201A29107665009801105 MODULE SKRSKYS76 S76C 8143008NE HYDRAULIC SYSTEMLEAKING A ALGAK NONE K FLUID LOSS ININSP/MAINT 1 SW03862AL 760531 ON POST FLIGHT INSPECTION FOUND HYDRAULIC FLUID LEAKING FROM NR 1 HYDRAULIC MODULE. REMOVED AND REPLACED NR 1 HYDRAULIC MODULE. GROUND RUN AND LEAK CHECKED. AC RETURNED TO SERVICE. (K) 1G72 3U NCH1NE 20051228001102005122800110NE 2005 12 28 ALG2005F00097 120051201A7797 WIRE SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL INDICATOR BROKEN E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW0331211 760225 T-5 INDICATOR PROBLEM MANIFESTED DURING FLIGHT. INSPECTED SYSTEM AND FOUND BROKEN WIRE AT PIN NR 11 OF NR 2 T-5 INDICATOR CONNECTOR. REPAIRED BROKEN WIRE IAW S-76 MM. PERFORMED SYSTEM TEST USING TESTER. GROUND RUN-UP PERFORMED. NO DEFECTS NOTED. SYSTEM RETURNED TO SERVICE. (K) 1G72 3U3 U H1NE E1GL 20051228001112005122800111NE 2005 12 28 ALG2005F00110 120051118A3297 CIRCUIT BREAKER SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL MLG TRIPPED E ALGAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 SW03717AL 760221 AFTER TAKEOFF, FLIGHT ATTEMPTED TO RAISE THE LANDING GEAR, BUT THE GEAR WOULD NOT RETRACT. RETURNED TO DEPARTURE. FOUND LANDING GEAR CONTROL CIRCUIT BREAKER NOT SET. RESET CIRCUIT BREAKER AND INSPECTED ALL LANDING GEAR COMPONENTS. NO DEFECTS WERE NOTED. JACKED AC AND PERFORMED 5 RETRACTION AND EXTENSION CYCLES WITH NO DEFECTS NOTED. (K) 1G72 3U3 U H1NE E1GL 20051228001122005122800112NE 2005 12 28 ALG2005F00112 120051116A3210 LANDING GEAR SKRSKYS76 S76C 8143008NE RIGHT INOPERATIVE E ALGAO OTHER J WARNING INDICATION APAPPROACH 1 SW03868AL 760580 ON APPROACH TO LANDING, RT LANDING GEAR LIGHT WOULD NOT ILLUMINATE WHEN GEAR WAS DOWN AND LOCKED. PINNED GEAR IAW MEL. (K) 1G72 3U NCH1NE 20051222000342005122200034NM 2005 12 22 ASAA0570107 120051024A5240141A653824 STOP FITTING BOEING737 737790 13844CNNM FS 324 GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02624AS 30778 PAE - DURING SI CHECK, FOUND FORWARD GALLEY DOOR AFT UPPER STOP PIN IS GOUGED. REPAIRED IAW EA 5210-10082. (M) 2L72 4F RTA16WE 20051222000412005122200041SO 2005 12 22 C2XA05IA140 120051212A33502013BR BATTERY PACK EMB 145 EMB145 3260210SO EMERGENCY LIGHT DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW27149603477 783 145100 IAH - DURING MAINTENANCE INSPECTION SEVERAL EMERGENCY LIGHT STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE AND FOUR EMERGENCY LIGHT BATTERY PACKS, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20051222000462005122200046EA 2005 12 22 COMA0560738 120051219A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE TE FLAPS OUT OF SEQUENCE A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01786CA 7333 DURING CVG APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE AT 8 DEGREES, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE (FIRST EVENT) MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2L72 4F4 FRTA21EA E15NE 20051222000522005122200052 2005 12 22 SWAA054038 420051214A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29351SW 24572 DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051222000592005122200059NM 2005 12 22 SWAA054045 120051220A335010107451 LIGHT BOEING737 7373H4 1384600NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29606SW 27926 FWD GALLEY EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20051222000642005122200064WP 2005 12 22 AALA20050811 120051210A3241 VALVE DOUG DC9 DC983 3022083WP ANTI SKID SYS INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW219616G 53563 STL - WHEEL NOT TURNING LIGHT ON AT APPROXIMATELY 130 KNOTS DURING TAKEOFF. EXTINGUISHED AFTER LIFT OFF. NOTED BURNED RUBBER SMELL IN COCKPIT AND CABIN THAT DISSIPATED QUICKLY. ALL BRAKE TEMPS BELOW 50 DEGREES. REPLACED LEFT HAND INBOARD AND OUTBOARD ANTI-SKID VALVES AND INBOARD WHEEL TRANSDUCER. REPLACED ANTI-SKID CONTROL BOX. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20051222000722005122200072SO 2005 12 22 C2XA05SH141 120051218A531214526850401 FIREWALL EMB 145 EMB145LR 3260212SO AFT FUSELAGE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713553 145585 SHV - DURING C-CHECK MAINTENANCE FOUND APU FIREWALL CRACKED AT MID RIGHT HAND SECTION (INSIDE). MAINTENANCE INSTALLED REPAIR DOUBLER ON APU FIREWALL AT MID RIGHT HAND SECTION IAW EMB 145 SRM 53-32-13 FIG 204. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20051222000802005122200080NM 2005 12 22 USAA051586 120051220A5311 FRAME BOEING737 7374B7 1384702NM BS 601 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 STA 601 RIGHT SIDE ON INNER CORD ANGLE JUST BELOW CABIN FLOOR LEVEL CRACKED. REMOVED DAMAGED MATERIAL, INSTALLED FILLER AND STIFFENER ANGLE IAW TR 53-62-01 & EA 97193, DEFECT SIZE: 1.5 INCH CRACK. 2L72 4F RTA16WE 20051222000842005122200084NM 2005 12 22 USAA051590 120051220A5330 SKIN BOEING737 7373B7 1384580NM STA 860-887, S2LCHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19530AU 24412 STA 860-887, S2L-S2R CHAFED. INSTALLED DOUBLER & RUB STRIPS IAW EA 97215, DEFECT SIZE: 52 INCH LONG, .018 INCH DEEP CHAFED AREA. 2L72 4F RTA16WE 20051222000992005122200099EU 2005 12 22 USAA051608 120051220A5347F53311325200 SEAT TRACK AIRBUS330 A330323 3930335EU FR 49 Y450 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 FR 49 Y450 CORRODED. BLENDED OUT PER SRM 51-74-00 & PART REPLACED PER 53-31-15; CORR LEVEL 2; TASK C53317001, DEFECT SIZE: 1 X 1 X .010 INCH. 2L72 4F RTA46NM 20051222001022005122200102EU 2005 12 22 USAA051605 120051220A5347F53311325200 SEAT TRACK AIRBUS330 A330323 3930335EU Y450 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 SEAT TRACK - Y450 BETWEEN FR 50 & 51. BLENDED AREA AS PER SRM 51-74-00, TRACK REPLACED PER 53-31-15, 51-72-11; CORROSION LEVEL 1; TASK C53317001, DEFECT SIZE: 3 X 1 INCH. 2L72 4F RTA46NM 20051222001052005122200105EU 2005 12 22 USAA051602 120051220A5347F5347820720000 SEAT TRACK AIRBUS330 A330323 3930335EU Y794 3 LT FR 74 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 Y794 3 LEFT FR 74 CORRODED. BLENDED, REPLACED NEW SEAT TRACK PER 51-42-11, 51-74-00, 53-00-15, DEFECT SIZE: .500 X .500 X .050 INCH. 2L72 4F RTA46NM 20051222001112005122200111NM 2005 12 22 SWAA054047 120051220A53116546555 FRAME BOEING737 7373H4 1384600NM BS 867 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29622SW 27932 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051227000242005122700024NM 2005 12 27 DHL2005765528 120051122A5322 SHEAR TIE BOEING727 727264 138408MNM BS 950E CORRODED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15765AT 23014 FOUND CORROSION ON BS 950E SHEAR TIES FROM S-27L TO S-29L. FABRICATED AND INSTALLED REPAIR DOUBLER 5-13/16" BY 2-1/4" FROM 7075-T6 .080 IAW B727 SRM 51-30-2, 51-10-1 AND 53-10-4 FIG 11. 2L73 4F A3WE 20051227000322005122700032WP 2005 12 27 UPS05845881 120051212A3350 BATTERY PACK DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 EMERGENCY BATTERY PACK NEEDS REPLACING. REPLACED BAT PACK EMERGENCY LIGHT. OPS NORMAL. OK TO CONTINUE. 2L74 4F RT4A25 20051227000332005122700033WP 2005 12 27 UPS05845884 120051217A2611 BATTERY DOUG DC8 DC873F 302199FWP FIRE DETECTORS MALFUNCTIONED A IPXAO OTHER N FALSE WARNING APAPPROACH 1 SO01809UP 46109 DURING FINAL APPROACH LOW CARGO COMPT FIRE LIGHT CAME ON AS SOON AS PACKS WERE TURNED OFF IT WENT AWAY. PERFORMED LOWER CARGO COMPT SMOKE DETECTION SYS T/S MM 26-18-00-1. REMOVED AND REPLACED BATTERIES ON DETECTORS FA1326, AC3305, AD6652, AD7666 SYS OK LIGHT INDICATED. 2L74 4F RT4A25 20051227000392005122700039NM 2005 12 27 DHL2005765521 120051118A5320 FLOOR SUPPORT BOEING727 727264 138408MNM BS 644 CORRODED B DHLAK NONE O OTHER ININSP/MAINT 1 SO15765AT 23014 FWD PIT FLOOR SUPPORT HAS CORROSION AROUND FASTENERS HOLES LWR SIDE STA 644 RBL 9. REMOVED CORRODED AREA. FABRICATED AND INSTALLED REPAIRS 8.5" BY .8" BY 1.2" FROM AND10134-1204 AND 22" BY 1.3" 1.0" FROM BAC1517-1507 IAW B727 SRM 51-40-3 FIG 1 PG 1. 2L73 4F A3WE 20051227000522005122700052WP 2005 12 27 ABXA050367 120051116A5730 ACCESS PANEL DOUG DC8 DC863F 302198FWP RT WING LEAKING A ABXAK NONE K FLUID LOSS ININSP/MAINT 1 GL23826AX 46061 12 BLIND RIVETS LEAKING UPON PRESSURE CHECKS. RIGHT WING, STRINGER NR 7 NEAR ACCESS PANEL 505F. REMOVED 12 BLIND FASTENERS ON STRINGER NR 7 NEAR ACCESS PANEL 505F OF THE RIGHT WING AND WET INSTALLED NEW FASTENERS IAW DC8 SRM 51-1-21 USING 1422 B1/2 SEALANT. 2L74 4F 4A25 20051227000572005122700057WP 2005 12 27 ABXA050363 120051010A5314 KEELBEAM DOUG DC8 DC863F 302198FWP BS 610-710 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 CORROSION FOUND ON SURFACE OF KEEL BEAM IN MID CARGO BAY BILGE AREA, STA 610 TO 710 APPROXIMATELY BUTT LINE 0. MULTIPLE BLENDED AREAS ON BOTH HORIZONTAL LEGS RANGING FROM 0.010" MIN TO MAX BLEND DEPTH OF 0.141". REMOVED CORROSION ON UPPER SURFACE OF KEEL BEAM IN MID CARGO BAY BILGE AREA STA 640 IAW DC8 SRM 53-2-0, PG 2M AND REA D853-52595. 2L74 4F 4A25 20051227000592005122700059WP 2005 12 27 ABXA050364 120051012A5320 ANGLE DOUG DC8 DC863F 302198FWP BS 857 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 FOUND CORNER ANGLE ON PRESSURE WEB CORRODED ON FORWARD BULKHEAD IN RIGHT WHEEL WELL, STA 857, RIGHT BUTT LINE 48. NEW CORNER ANGLE FABRICATED IAW REA D853-52555. ANGLE INSTALLED IAW DC8 SRM 51-1-20 AT STA 857, RIGHT BUTT LINE 48. 2L74 4F 4A25 20051227000692005122700069NM 2005 12 27 QXEA200501811 120051216A5230 ROLLER BOMBDRDHC8 DHC8402 1390042NM CARGO DOOR FAILED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09414QX 4061 GEG FLIGHT NR 2367, FUSELAGE DOOR WARNING THROUGH CLIMB. FOLLOWED APPROPRIATE CHECKLIST, RETURNED TO GEG. CONFIRMED INFLIGHT WARNING TO BE AFT BAGGAGE DOOR WITH NO LOSS OF CABIN PRESSURE. AIRCRAFT FERRIED TO PDX. MAINTENANCE REPLACED THE LOWER FWD ROLLER IAW AMM TASK 52-31-24-400-801, AND REPAIRED IAW HORIZON AIR EO 6-52-145 AND EO 6-52-397. AFT CARGO DOOR CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051227000702005122700070EA 2005 12 27 QXEA200501794 120051124A7830 COWLING CNDAIRCL600 CL6002C10 1390015EA THRUST REVERSER DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09604QX 10019 YYC - LEFT ENGINE UPPER TRANS COWLING HAS MULTIPLE SCRATCHES ON THE FORWARD END OF THE THRUST REVERSER SLIDER. BLENDED OUT SCRATCHES IAW EA R-78-72 AND REO 670-54-21-496. 2L72 4F RTA21EA 20051227000752005122700075EA 2005 12 27 QXEA200501799 120051124A3211 SUPPORT BEAM CNDAIRCL600 CL6002C10 1390015EA MLG ACTUATOR DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09604QX 10019 YYC - LEFT MAIN GEAR ACTUATOR SUPPORT BEAM HAS A NICK ON THE TOP INSIDE CORNER. BLENDED OUT DAMAGE IAW REO 670-570210023. RESTORED FINISH. 2L72 4F RTA21EA 20051227000802005122700080EA 2005 12 27 QXEA200501804 120051124A5310 BEAM CNDAIRCL600 CL6002C10 1390015EA BS 847 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09604QX 10019 YYC - FUSELAGE BULKHEAD BEAM AT STATION FS 847 HAS A GOUGE ON THE LOWER FLANGE. BLENDED DAMAGE IAW REO 670-70-53-4016 AND R-53-401. RESTORED FINISH. 2L72 4F RTA21EA 20051227000822005122700082EU 2005 12 27 USAA051624 120051221A5320F5347940320200 PLATE AIRBUS330 A330323 3930335EU BS 76-77 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 FOUND CORROSION UNDER CLIP NUTS FS 76 - 77. REPLACED PLATE PER 51-72-11; CORROSION LEVEL 2; TASK C534159, DEFECT SIZE: .750" BY .750". 2L72 4F RTA46NM 20051227000842005122700084EU 2005 12 27 USAA051626 120051221A5320F5347824220300 PROFILE AIRBUS330 A330323 3930335EU -Y450 FR 80 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19675US 370 FOUND CORROSION -Y450 FS 80. REPLACED PER SRM 51-72-11; CORROSION LEVEL 2; TASK C53415901, DEFECT SIZE: 1" BY 1". 2L72 4F RTA46NM 20051227000982005122700098NM 2005 12 27 USAA051636 120051221A532065C3184779 FLOOR SUPPORT BOEING737 7374B7 1384702NM BS 967-986 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19781AU 25020 FOUND CABIN FLOOR SUPPORT BETWEEN STA 967-986.5 LBL 16. REMOVED AND REPLACED NEW SUPPORT ANGLE PER SRM 51-40-02; CORROSION LEVEL 1; TASK C5310702, DEFECT SIZE: 2.125"L BY 2"W BY .069"D. 2L72 4F RTA16WE 20051227001082005122700108NM 2005 12 27 SWAA054062 120051220A3350BR2013 LIGHT BOEING737 7373H4 1384600NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29370SW 26597 DURING SCHEDULED C4 CHECK, FOUND EEPLS STRIP MISSING AT ROW 7 ABC & ROW 16 DEF. INSTALLED EEPLS PER MM. 2L72 4F RTA16WE 20051227001162005122700116NM 2005 12 27 SWAA054070 120051221A53206582671 WEB BOEING737 7373Q8 1384670NM BS 663-665 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED 1/2D CHECK, FOUND BEADED PRESSURE WEB CRACKED BETWEEN BS 663 TO BS 665, LBL 32. REPAIRED WEB PER SWA EA. 2L72 4F RTA16WE 20051227001172005122700117NM 2005 12 27 SWAA054071 120051221A532269353656 SHEAR TIE BOEING737 7373Q8 1384670NM BS 360 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 360, BETWEEN STR 28L TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051227001202005122700120NE 2005 12 27 120805B 220051209A7314025323150 SPLINE CESSNA208 208B 2073701CE PWA PT6 PT6A114 52043NE MCAULY3DF36CB3DF36C526 GL DRIVE ASSY CORRODED E AWHAK NONE O OTHER ININSP/MAINT 1 WP17969FE 2951 208B0092 17219 981511 PRECAUTIONARY INSPECTION OF THE FUEL PUMP DRIVE SPLINE IN ACCORDANCE WITH PRATT AND WHITNEY PT6 MAINTENANCE MANUAL, FUEL PUMP COUPLING IN-SITU INSPECTION 73-10-02 PAGE 210, PARAGRAPH 8D, MAINTENANCE FOUND THE FUEL PUMP DRIVE SPLINE SEVERELY CORRODED AND DAMAGED TO THE POINT OF NEAR FAILURE. THE FUEL PUMP ASSEMBLY WAS REPLACED WITH A FRESH OVERHAULED UNIT AND THE AIRCRAFT RETURNED TO SERVICE. 1H71 3T3 T A37CE E4EA 5 C 20051227001262005122700126NE 2005 12 27 AWHA120805 220051209A7314025323150 SPLINE CESSNA208 208B 2073701CE PWA PT6 PT6A114 52043NE MCAULY3DF36CB3DF36C526 GL DRIVE ASSY CORRODED E AWHAK NONE O OTHER ININSP/MAINT 1 WP17969FE 2951 208B0092 17219 981511 PRECAUTIONARY INSPECTION OF THE FUEL PUMP DRIVE SPLINE IN ACCORDANCE WITH PRATT AND WHITNEY PT6 MAINTENANCE MANUAL, FUEL PUMP COUPLING IN-SITU INSPECTION 73-10-02 PAGE 210, PARAGRAPH 8D, MAINTENANCE FOUND THE FUEL PUMP DRIVE SPLINE SEVERELY CORRODED AND DAMAGED TO THE POINT OF NEAR FAILURE. THE FUEL PUMP ASSEMBLY WAS REPLACED WITH A FRESH OVERHAULED UNIT AND THE AIRCRAFT RETURNED TO SERVICE. 1H71 3T3 T A37CE E4EA 5 C 20051227001272005122700127NM 2005 12 27 CALA0500452 120051220A2560P4010021 BATTERY BOEING767 767424ER 1385270NM FLASHLIGHT INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2776064 29459 THE FLASHLIGHT AT FORWARD F/A SEAT WAS FOUND INOPERATIVE DURING A SERVICE CHECK. THE BATTERY PACK WAS REMOVED AND REPLACED IAW GMM 07-26-01 AND MM 25-64-00. 2L72 4F RTA1NM 20051227001302005122700130NM 2005 12 27 SWAA054050 120051220A53306545765 SKIN BOEING737 7373T5 1384608NM BS 500D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29667SW 23063 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 12L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051227001332005122700133NM 2005 12 27 SWAA054053 120051219A534065C27314 STRINGER CLIP BOEING737 7373Q8 1384670NM BS 294 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 294.5, STR 12L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051227001412005122700141NM 2005 12 27 P5CA0501412 120051110A27801267629 PDU BOEING747 74746NF 13848BTNM LE FLAPS FAILED A P5CAO OTHER J WARNING INDICATION APAPPROACH 1 EA15452PA 30810 ON APPROACH EICAS MSG FLAPS PRIMARY FOLLOWED BY FLAPS DRIVE MSG. TROUBLESHOT THEN REPLACED NR 3 LT L/E PDU IAW MM 27-81-03. 2L74 4F RTA20WE 20051227001552005122700155NM 2005 12 27 SWAA054014 120051218A3397W11604222 WIRE BOEING737 7373G7 1384595NM GE CFM56 CFM563B1 13802NE EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29683SW 24008 DURING SCHEDULED SPECIAL VISIT, COCKPIT EMERGENCY EXIT LIGHT CIRCUIT BREAKER TRIPPED. REPAIRED WIRE NR W1160-42-22 IAW WDM. OPS CHECK OK IAW MM. 2L72 4F4 FRTA16WE E2GL 20051227001612005122700161NM 2005 12 27 SWAA054020 120051218A335010107451 LENS BOEING737 7377H4 1384404NM CONT O520 IO520* 17032SO EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29785SW 30602 R2 DOOR EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED EXIT LIGHT ASSY IAW MM. 2L72 4F3 ORTA16WE E5CE 20051227001682005122700168 2005 12 27 SWAA053831 420051130A2565D31354 SLIDE BOEING737 7373H4 1384600NM GE CFM56 CFM563B1 13802NE L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29637SW 27710 DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE IAW MM. 2L72 4F4 FRTA16WE E2GL 20051227002222005122700222NM 2005 12 27 05FDEA04387 120051220A5322 SHEAR TIE BOEING727 727200 138407ENM PWA JT8 JT8D9A 52048NE BS 950F CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 N01277 BS 950F LBL 12 WL 140 SHEAR TIE CRACKED. REMOVED AND REPLACED SHEAR TIE IAW SRM 53-10-4, AND SRM 51-30-09. 2L73 4F4 FRTA3WE E2EA 20051227002242005122700224NM 2005 12 27 05FDEA04389 120051221A5330 REPAIR BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE BS 1140 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25274FE 22039 FOUND PREVIOUSLY REPAIR INSTALLED AT STA. 1140, STR 20L WAS ACCOMPLISHED IAW SRM 53-30-3 FIG.1, BASED ON AN EXTERNAL EVALUATION CONSISTED OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL THICKNESS AND TYPE, GENERAL WORKMANSHIP OF THE INSTALLATION, REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100. 2L73 4F4 FRTA3WE E2EA 20051228000032005122800003SO 2005 12 28 SIMA200532504 120051109A521014524900403 HANDLE EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL PAX DOOR CRACKED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21613AE15292 145081 A CRACK WAS DISCOVERED ON THE PASSENGER DOOR INNER HANDLE BRACKET. STOP DRILLED THE CRACK ON THE PAX DOOR HANDLE BRACKET. FABRICATED A REINFORCEMENT ANGLE. REPAIR DONE IAW SRM. (K) 2L72 4F4 FRTT00011ATTE6CH 20051228000062005122800006SO 2005 12 28 SWIA200516016 120051217A3350D36604001 BATTERY EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07584SW1091210912 120352 FWD "E" LIGHTS GO OUT DURING OPERATIONAL CHECK AFTER THREE SECONDS. REPLACED FORWARD EMERGENCY LIGHT BATTERY IAW MM 33-50-02. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20051228000192005122800019EA 2005 12 28 SWIA200516003 120051210A2741 SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07945SW 7770 STAB/TRIM MSG'S AND ENGAGEMENT PROBLEMS. REMOVED AND REPLACED BOTH DISCONNECT SWITCHES. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051228000382005122800038CE 2005 12 28 TIM2005F00009 120050729A261230215 FIRE DETECTOR BEECH 99 99A 1154003CE PWA PT6 PT6A27 52043EA RT ENGINE FALSE INDICATIONA TIMAO OTHER N FALSE WARNING APAPPROACH 1 NM07326CA U135 PCE41687 THE RT ENGINE FIRE DETECTION LIGHT CAME ON BRIEFLY ON FINAL APPROACH TO THE AIRPORT. THE RT ENGINE WAS RECENTLY CHANGED AND WAS WASHED TO CHECK FOR POSSIBLE OIL LEAKS. WATER FROM THE WASH CAN ENTER THE ENGINE FIRE DETECTORS AND CAUSE FALSE FIRE WARNINGS. THAT IS THE MOST LIKELY CAUSE FOR THIS FALSE FIRE WARNING. TO PREVENT THIS FROM HAPPENING THE FIRE DETECTORS ARE GENERALLY COVERED TO PREVENT WATER FROM ENTERING THE DETECTORS. (K) 1L72 3T4 T A14CE E4EA 20051228000512005122800051SW 2005 12 28 ALG2005F00102 120051128A2435200SGL32Q STARTER GEN BELL 206 206L4 1182110SW ALLSN 250C 250C30P 03013GL FAILED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03271AL 52287 STARTER/ GENERATOR FAILED ENROUTE TO WC 586, RETURNED TO BASE. REMOVED AND REPLACED STARTER/GENERATOR. (K) 1G71 3U3 UNCH2SW E1GL 20051228000552005122800055SW 2005 12 28 ALG2005F00095 120051130A243523032027 STARTER GEN BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL FAILED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW033912Q 3271 GENERATOR STOPPED CHARGING ON SHORT FINAL. REMOVED AND REPLACED STARTER/ GENERATOR AND BATTERY. (K) 1G71 3U3 U H2SW E4CE 20051228000752005122800075SO 2005 12 28 SIMA200533603 120051125A575114569007409 FITTING EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL LT AILERON WORN A SIMAK NONE O OTHER ININSP/MAINT 1 SW21615AE15242 145087 THE LT AILERON OB HINGE POINT BEARING HOLE WAS FOUND TO BE WORN BEYOND MANUAL LIMITS. REMOVED DAMAGED HINGE FITTING. LOCATED AND DRILLED IN NEW FITTING. APPLIED ALODINE AND PRIMER TO ALL BARE SURFACE. REPAIR DONE IAW SRM. (K) 2L72 4T4 FRTT00011ATTE6CH 20051228000772005122800077SO 2005 12 28 SIMA200532509 120051107A532014525381 FLOOR SUPPORT EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21613AE15292 145081 THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 25. REMOVED THE CORROSION BY MAKING CUTOUT. PREPARED A DOUBLER, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (K) 2L72 4F4 FRTT00011ATTE6CH 20051228000792005122800079SO 2005 12 28 SIMA200530404 120051028A33507287580505 LIGHT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FWD CABIN FAILED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21634AE 145150 EMERGENCY EXIT FLOOR STRIP AT GALLEY WILL NOT ILLUMINATE. REPLACED NR 1 EXIT DOOR EMERGENCY LIGHT, FLOOR PROXIMITY STRIP IAW MM. OPS CHECK GOOD. AC RETURNED TO SERVICE. (K) 2L72 4T4 FRTT00011ATTE6CH 20051228000862005122800086SO 2005 12 28 SIMA200531501 120051108A335020131A BATTERY EMB 135 EMB135KL 3260302SO GARRTTTPE331TPE33112UA 01514WP CABIN DISCHARGED A SIMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW21844AE 145682 CREW FOUND EMERGENCY LIGHTS INTERMITTENT. REPLACED NR 1, NR 2, NR 3, AND NR 4 EMERGENCY LIGHTNING BATTERIES. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. NR 1) PN OFF 2013-1A, SN OFF 60708. NR 2) PN OFF 2013-1A, SN OFF 81147. NR 3) PN OFF 2013-1A, SN OFF 72755. NR4) PN OFF 2013-1A, SN OFF 67824. (K) 2L72 4F4 TRTT00011ATE4WE 20051228000902005122800090SO 2005 12 28 SIMA200530401 120051027A5330AL2024T3 SKIN EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL FR 21, 22 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21610AE15310 145073 DURING INSPECTION OF FUSELAGE SKIN BETWEEN FRAMES 21 AND 22 AND STRINGERS 19R AND 191., WAS FOUND TO BE CORRODED. PERFORMED A CUT OUT OF CORRODED AREA. FABRICATED A FILLER AND DOUBLER. REPAIR DONE IAW SRM. (K) 2L72 4F4 FRTT00011ATTE6CH 20051228000912005122800091WP 2005 12 28 LNX2005F00002 220051115A731031021781 LINE FRCHLD22 22C7A 3370104EA GARRTTTPE331TPE331* 01514WP FUEL SYSTEM LOOSE A LNXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO29438MA AC721B DURING INTIAL DEPARTURE CLIMB THE CREW OBSERVED A FIRE WARNING LIGHT ILLUMINATION ON THE LT ENGINE FIRE WARNING PANEL. EMERGENCY CHECKLIST COMPLETED TO INCLUDE ENGINE SHUTDOWN. RETURNED TO CAP HAITIAN. FOUND THE P3 FUEL CONTROL SENSING LINE LOOSE. TIGHTENED LINE. PERFORMED OPERATIONAL CHECK. (K) 1H71 3I3 T ATC438 E2WE 20051228001042005122800104GL 2005 12 28 ALG2005F00120 220051107A7200 ENGINE SKRSKYS76 S76 8143010NE ALLSN 250C 250C30S 03013GL NR 1 FAILED E ALGAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 SW03705AL 760267 ON PRELANDING CHECK, ENGINE OIL PRESSURE DECREASED AND OIL TEMPERATURE INCREASED ABOVE THE RED LINE. ON LONG FINAL TO THE BASE, SHUTDOWN NR 1 ENGINE. AFTER LANDING, NOTIFIED MAINTENANCE. (K) 1G72 3U3 U H1NE E1GL 20051228001142005122800114EU 2005 12 28 KBM2005F00348 120051119A6720704A34130184 CONTROL CABLE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE TAIL ROTOR BINDING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV1366 3296 CABLE, FOUND UNIT BINDING, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051228001152005122800115EU 2005 12 28 KBM2005F00350 120051125A243223761 BATTERY SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1B 6OO30NE MASTER FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH3 2957 STARTS SLOW, REMOVED AND REPLACED BATTERY. (K) 1G71 3U3 U H9EU E19EU 20051228001162005122800116EU 2005 12 28 KBM2005F00352 120051202A2400410CC01Y140 RELAY SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE GENERATOR FAILED A KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19351WM 2167 GENERATOR LIGHT STAYS ON. REMOVED AND REPLACED RELAY. (K) 1G71 3U3 U H9EU E19EU 20051228001172005122800117EU 2005 12 28 KBM2005F00358 120051122A51009850532210 SWITCH SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE PSI INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19751H 3512 3403 PSI SWITCH INOPERATIVE, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051228001182005122800118EU 2005 12 28 KBM2005F00337 120051115A6520350A33215001 BALL END SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE TAIL ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P1130 2347 BALL END WORN, REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20051228001192005122800119EU 2005 12 28 KBM2005F00341 120051113A80120174078030 DRAIN VALVE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE STARTER LEAKING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19345SH2285 3345 START DRAIN VALVE, UNIT LEAKING, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051228001202005122800120EU 2005 12 28 KBM2005F00336 120051115A6520350A33215300 BEARING SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE TAIL ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P871 2347 LAMINATED BEARINGS ARE WORN, REMOVED AND REMPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20051228001212005122800121NE 2005 12 28 KBM2005F00353 220051124A73210164548530 FCU SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1D NE ENGINE FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1953SH 1645 2009 SUSPECT HIGH SIDE FAILURE NTL GOVERNOR FUEL CONTROL UNIT. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051228001232005122800123 2005 12 28 KBM2005F00344 420051123A2312064105430 TRANSCEIVER SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE VHF COMMS INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19115SH561 3141 UNIT RECEIVES BUT TRANSMITS GARBLED. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051228001252005122800125EU 2005 12 28 KBM2005F00340 120051113A5100926109 HOSE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE UNKNOWN LEAKING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19345SH6505 3345 HOSE- UNIT IS SWOLLEN AND LEAKING, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051228001272005122800127EU 2005 12 28 ALG2005F00091 120051110A77970319767910 WIRE HARNESS UROCOPEC120 EC120B 8680987EU FAILED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03516AL 1157 IN FLIGHT, T4 PORTION OF FLI- INTERMITTENT FLUCTUATION AND T-4 FAILURE. REMOVED HARNESS SN 215B,, INSTALLED HARNESS 279B, OPERATION CHECK GOOD. (K) 1G72 3U NCR0001RD 20051228001282005122800128EU 2005 12 28 ALG2005F00093 120051128A6340G1130043180 PRESSURE SWITCH UROCOPEC120 EC120B 8680987EU GEARBOX INOPERATIVE E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03515AL 1165 INFLIGHT, THE CAUTION WARNING TONE SOUNDED. WHEN LANDING, THE MGB CHIP LIGHT ILLUMINATED. REMOVED AND REPLACED TRANSMISSION PRESSURE SWITCH IAW MM. CHECKED GOOD. (K) 1G72 3U NCR0001RD 20051228001312005122800131 2005 12 28 CALA0500453 420051225A2565D31354418 SLIDE BOEING737 737524 1384721NM L-2 DOOR LOW A CALAK NONE O OTHER ININSP/MAINT 1 SW275860648441 27319 THE L-2 DOOR SLIDE WAS FOUND WITH LOW PRESSURE. THE SLIDE WAS REMOVED AND REPLACED IAW MM 25-61-35. 2L72 4F RTA16WE 20051228001332005122800133NM 2005 12 28 SWAA054075 120051221A53306545767 SKIN BOEING737 7373H4 1384600NM BS 454-456 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 454 TO BS 456, STR 16R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051228001352005122800135NM 2005 12 28 SWAA054077 120051226A53406557463 ATTACH BRACKET BOEING737 7373H4 1384600NM GIRT BAR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR BRACKET LOOSE. SECURED BRACKET PER MM. 2L72 4F RTA16WE 20051228001372005122800137NM 2005 12 28 SWAA054079 120051222A53306545765 SKIN BOEING737 7373H4 1384600NM BS 500 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500, STR 15L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051228001392005122800139NM 2005 12 28 SWAA054081 120051222A335090083 BATTERY PACK BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29339SW 24090 DURING SCHEDULED A1 CHECK, FOUND L1 DOOR INTERIOR & EXTERIOR EMERGENCY EXIT LIGHTS INOP. SECURED BATTERY PACK PER MM. 2L72 4F RTA16WE 20051228001412005122800141NM 2005 12 28 SWAA054083 120051222A53116520722 FRAME BOEING737 7373H4 1384600NM BS 440 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29361SW 26572 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, BS 440, STR 24R. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20051228001432005122800143NM 2005 12 28 SWAA054085 120051223A3350MS155721 BULB BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29394SW 27380 DURING SCHEDULED SERVICE CHECK, FOUND LT FWD CABIN EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20051228001452005122800145NM 2005 12 28 SWAA054087 120051226A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29407WN 29817 FWD LEFT EEPLS STRIP COVER MISSING. INSTALLED COVER PER MM. 2L72 4F RTA16WE 20051228001472005122800147NM 2005 12 28 SWAA054089 120051225A2910F61A0048 VALVE BOEING737 7377H4 1384404NM HYD SYSTEM ODOR A SWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SW29408WN 27895 STRONG ODOR IN CABIN. REMOVED AND REPLACED BOTH HYDRAULIC RESERVOIR CHECK VALVES PER MM. 2L72 4F RTA16WE 20051228001492005122800149 2005 12 28 SWAA054091 420051219A25656949956 CABLE BOEING737 7375H4 138449DNM R2 DOOR SLIDE MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE LATCH CABLE ASSY MISROUTED. REROUTED CABLE ASSY PER MM. 2L72 4F RTA16WE 20051228001522005122800152NM 2005 12 28 SWAA054094 120051222A52306547952 DOOR FRAME BOEING737 7375H4 138449DNM AFT CARGO BAY CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29511SW 24188 DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO DOOR AFT FRAME CRACKED AT NR 5 STOP FITTING. REMOVED AND REPLACED AFT CARGO DOOR PER MM. 2L72 4F RTA16WE 20051228001542005122800154 2005 12 28 SWAA054096 420051223A25656945736 BRACKET BOEING737 7373H4 1384600NM R2 DOOR SLIDE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29623SW 27933 DURING SCHEDULED D-CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD ATTACH MOUNT BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER SRM. 2L72 4F RTA16WE 20051228001562005122800156NM 2005 12 28 SWAA054098 120051223A53116546558 FRAME BOEING737 7373H4 1384600NM BS 908 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29623SW 27933 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 908, STR 8L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051228001582005122800158NM 2005 12 28 SWAA054100 120051223A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 460 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29623SW 27933 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 460, STR 15R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051228001602005122800160NM 2005 12 28 SWAA054102 120051223A53116558280 FRAME BOEING737 7373H4 1384600NM BS 360 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29623SW 27933 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051228001622005122800162NM 2005 12 28 SWAA054104 120051223A53116546548 FRAME BOEING737 7373H4 1384600NM BS 747 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29623SW 27933 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051228001642005122800164NM 2005 12 28 SWAA054106 120051223A53116546548 FRAME BOEING737 7373H4 1384600NM BS 747 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29623SW 27933 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051228001662005122800166NM 2005 12 28 SWAA054108 120051224A291065449913 MODULE BOEING737 7373Y0 1384671NM HYD SYSTEM FAULTY A SWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW29664WN 23495 AIR TURNBACK, LOST A-SYSTEM HYDRAULIC QUANTITY, HYDRAULIC ENGINE & ELECT PUMPS. REMOVED AND REPLACED HYDRAULIC TAIL ISOLATION VALVE MODULE PER MM. 2L72 4F RTA16WE 20051228001682005122800168 2005 12 28 SWAA054110 420051225A2565D31354 SLIDE BOEING737 7373G7 1384595NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29683SW 24008 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20051228001692005122800169EU 2005 12 28 AWXA200501583 120051203A5347D53311281520200 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28604AW 1196 SAL - DURING BC4 CHECK DISCOVERED LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FS 16 AND Y765. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 101, PAGE 102. REMOVED AND INSTALLED NEW SEAT TRACK BETWEEN FR 16 AND FR 24, ALSO AT Y765 IAW AIRBUS 320 SRM 51-72-11. 2L72 4F RTA28NM 20051228001702005122800170NM 2005 12 28 AWXA200501584 120051116A532069434961 WEB BOEING737 7373S3 1384711NM BS 847-896 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 MCN - DURING C20 CHECK DISCOVERED CORROSION ON WEB AT BS 847 TO BS 896 AND BETWEEN BL 20R AND BL 25R. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-53-1A1 FIG 101. MAINTENANCE REMOVED WEB AND INSTALLED NEW WEB AT BS 847 TO BS 867 AND BETWEEN BL 20R AND BL 25R IAW BOEING 737-300 SRM 51-40-02-0G. 2L72 4F RTA16WE 20051228001742005122800174SO 2005 12 28 SWIA200516007 120051104A5347 SEAT TRACK EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07268UE 120207 LT SIDE FWD SHORT SEAT TRACK CORRODED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED LT SIDE FWD SHORT SEAT TRACK IAW EMB120 MM 53-01-05. 2L72 4T RTA31SO 20051228001842005122800184EA 2005 12 28 SWIA200516009 120051208A4920 APU CNDAIRCL600 CL6002B19 1900309EA APU BAY ODOR A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM07983SW 7961 UPON LANDING SMELLED SOMETHING LIKE BURNING ODOR. AFTER PULLING INTO GATE, APU AUTO SHUTDOWN. SMOKE IN THE CABIN AS WELL. REPLACED APU IAW 49-00-00. 2L72 4F RTA21EA 20051228001862005122800186EA 2005 12 28 SWIA200516011 120051215A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07437SW 7564 NR 1 CARGO DETECTOR (SMOKE) INOP. REPLACED NR 1 CARGO SMOKE DETECTOR IAW 26-15-0. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051228001882005122800188 2005 12 28 SWIA200516013 420051214A22166225734002 SERVO EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07584SW1279012790 120352 WITH AUTOPILOT SELECTED TO EITHER SIDE "TRIM FAIL" ON MAP AND THEN TRIM STARTED TO ROLL FORWARD. REPLACED ELEVATOR TRIM SERVO MOTOR IAW MM 22-10-05. 2L72 4T RTA31SO 20051228001902005122800190EA 2005 12 28 SWIA200516015 120051214A2760 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07756SK 10221 SPLR/STAB FAULT STATUS MSG AT GATE. REPLACED NR 1 AND NR 2 SSCU'S, OPERATIONAL CHECK GOOD IAW CRJ 700 MM 27-61-05, PN C13045BA04, SN OFF 1006, PN C13045BA04 SN OFF 1005. 2L72 4F RTA21EA 20051228001962005122800196SO 2005 12 28 SWIA200516032 120051226A27203081401003 ACTUATOR EMB 120 EMB120ER 3260203SO RUDDER MALFUNCTIONED A SWIAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 NM07214SW 120280 RT RUDDER JAMMED AFTER TAKEOFF. REPLACED BOTH RUDDER ACTUATORS IAW MM 27-22-02. OPERATIONAL CHECK GOOD, PN 308140-1003, SN/OFF 0165 SN/OFF 0671. 2L72 4T RTA31SO 20051228001982005122800198SO 2005 12 28 SWIA200516034 120051001A5347 SEAT TRACK EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07217SW 120286 PAX SEAT TRACK CORRODED RT AFT FLOOR, ITEM FOUND AT C-CHECK INSPECTION. REPLACED PAX SEAT TRACK RT AFT FLOOR IAW EMB120 MM 53-01-05. 2L72 4T RTA31SO 20051228002012005122800201SO 2005 12 28 SWIA200516037 120051223A2611 SMOKE DETECTOR EMB 120 EMB120ER 3260203SO LAVATORY FALSE ACTIVATIONA SWIAO OTHER N FALSE WARNING CRCRUISE 1 NM07298SW 120328 LAVATORY SMOKE DETECTOR SOUNDED INFLIGHT THREE TIMES. REPLACED LAVATORY SMOKE DETECTOR. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20060109000012006010900001CE 2006 1 9 DJFA2005177 120051213A275065651201CR CABLE CESSNA500 560CESSNA 2076750CE TE FLAPS FRAYED E DJFAK NONE O OTHER ININSP/MAINT 1 EA23593CW 5600223 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A PHASE 16 INSPECTION, THE FLAP POSITION TRANSMITTER CONTROL CABLE WAS FOUND TO BE FRAYED APART. MAINTENANCE REPLACED THE AFT FLAP POSITION INDICATOR CONTROL CABLES AND RIGGED THE CABLES. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA22CE 20051228002032005122800203CE 2005 12 28 DJFA2005178 120051219A324099121663 BRAKE ASSY CESSNA500 550 2076604CE PWA JT15 JT15D4 52112NE MLG FAILED E DJFAO OTHER J WARNING INDICATION APAPPROACH 1 EA23270CW 5500570 THE CREW REPORTED THAT WHILE THEY WERE ON A VISUAL APPROACH THE ANTI-SKID AND POWER BRAKE PRESSURE LOW LIGHTS ILLUMINATED. THE ANTI-SKID CIRCUIT BREAKER WAS RECYCLED AND THE CREW WERE PREPARING TO USE THE EMERGENCY BRAKING SYSTEM, BUT LATER FOUND THAT THE BRAKES WERE WORKING. WHILE TAXIING, BOTH THE PILOT AND CO-PILOTS BRAKE PEDALS WENT TO THE FLOOR. EMERGENCY BRAKES WERE USED TO STOP THE AIRCRAFT. MAINTENANCE REPLACED THE BRAKE PUMP ASSEMBLY AND MOTOR. OPERATIONAL AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 1L72 4F4 F A22CE E1NE 20051228002052005122800205SW 2005 12 28 EGRR106996 120051116A63202060404122103 PLANETARY GEAR CLARK 1000 1000CLARK 2230102SW TRANSMISSION UNSERVICEABLE B EGRRK NONE O OTHER ININSP/MAINT 1 EA17 344 BKW11338 PREMATURE WEAR OF XMSN PLANETARY SUN GEAR AT LOWER DRIVE SPLINES, WORN HALF THE WAY THRU DRIVE SPLINES .030. 1Q71 3R 2A6 20051228002102005122800210WP 2005 12 28 0501639952 120051124A2915 PRESSURE VALVE DOUG DC9 DC931 3022065WP PWA JT8 JT8D9A 52048NE RT HYD SYSTEM FAILED A NWAADH RETURN TO BLOCK DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 GL01916RW 47144 AS THE AIRCRAFT WAS TAXING OUT FOR DEPARTURE THE RT HYDRAULIC SYSTEM LOST FLUID AND PRESSURE. THE AC RETURNED TO THE GATE WITHOUT ANY FURTHER PROBLEMS. MAINTENANCE FOUND THE RT HYDRAULIC SYSTEM PRESSURE RELIEF VALVE HAD FAILED AND REPLACED IT. ALSO THE RT ELECTRIC HYDRAULIC PUMP WAS REPLACED AS A PRECAUTION. LEAK CHECK AND OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 20051228002122005122800212WP 2005 12 28 ABXA050291 120051129A3350 BATTERY DOUG DC9 DC931 3022065WP PWA JT8 JT8D7B 52053NE EMERGENCY LIGHT WEAK A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23937AX 47074 EMERGENCY COCKPIT LIGHTING WAS INOPERATIVE. REPLACED EMERGENCY COCKPIT LIGHTING BATTERIES IAW AMM 33.53.00.8. OPS CHECKED GOOD. 2L72 4F4 F A6WE E2EA 20051228002142005122800214WP 2005 12 28 IXXA05RNG093S 120051028A5414 SKIN DOUG DC8 DC872 302199BWP ZONE 400 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK WAS FOUND A CORROSION ON THE UPPER SKIN AT OB PYLON NR 4-RT. DAMAGED AREA WAS CLEANED AND REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-2-1 FIG 38 AND EWO ATI 57-058. 2L74 4F RT4A25 20051228002162005122800216NM 2005 12 28 ASMF200512001 120051125A2910S7929462S1014 HOSE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE HYD SYSTEM LEAKING W ASMFK NONE K FLUID LOSS ININSP/MAINT 1 SW23160PL 49763 DURING TRANSIT CHECK, THE LT HYDRAULIC BRAKE ACCUMULATOR HOSE WAS LEAKING. THE HOSE WAS REMOVED AND REPLACED BY FLEXIBLE HOSE IAW MM 32-42-04. THE LT HYDRAULIC BRAKE ACCUMULATOR FLEXIBLE HOSE WAS REPLACED BY ORIGINAL HOSE IAW MM 32-42-04, TESTED CORRECT. 2L72 4F4 FRTA6WE E9NE 20051228002182005122800218WP 2005 12 28 IXXA05RNG080S 120050916A5500 SKIN DOUG DC8 DC872 302199BWP STA XE 279.125 DEFORMED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK WAS FOUND A OIL CAN ON LOWER SURFACE SKIN STA XE 279.125 TO 288.957 - LT. SKIN WAS REPLACED IAW DRAWING 5654970 ZONE 17 TO 21, RIVETS WERE INSTALLED IAW SRM 51-1-21 PAGE 1-7 AND PROTECTIVE TREATMENT WAS APPLIED IAW SRM 51-1-8 PAGE 13-16. 2L74 4F RT4A25 20051228002222005122800222WP 2005 12 28 ABXA050293 120051129A53135750198 LONGERON DOUG DC8 DC863F 302198FWP BS 879 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23812AX 46126 CORROSION FOUND ON LONGERON 24 RIGHT AT STATION 879. REA D853-52752MR PERFORMS AN INTERIM REPAIR TO THE LONGERON. 2L74 4F 4A25 20051228002312005122800231NM 2005 12 28 C8GA20050024 120051202A5210 DOOR BOEING727 727223 1384074NM PWA JT8 JT8D15 52051NE L1 OPEN A C8GAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 SO29708AA57508 22465 DURING CLIMBOUT OPERATION, AIRCRAFT WOULD NOT PRESSURIZE ABOVE 1.5 PSID. AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. ON POST FLIGHT FOUND L1 ENTRY DOOR NOT FULLY CLOSED, OPEN, CYCLED AND RESET DOOR, CONFIRMED FULLY CLOSED AND LOCKED. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 20051230000012005123000001NM 2005 12 30 ZN3R543100 120051212A49209760524 PLENUM HONEYWELL 85129CKB BOEING737 7373TO 138447GNM APU RUPTURED B ZN3RO OTHER T ENGINE CASE PENETRATION NRNOT REPORTED 1 WP0759302 5334 P60474C 23353 TURBINE PLENUM OF APU RUPTURED AT A PREVIOUSLY REPAIRED WELD SEAM. 2L72 4F RTA16WE 20051230000042005123000004NM 2005 12 30 BB05106 120051223A335020121 CHARGER BOEING757 7572B7 1384964NM EMERGENCY LIGHTSFAULTY A USAAK NONE O OTHER ININSP/MAINT 1 EA19613AU 27144 MCO - THE L2 DOOR EXTERIOR EMERGENCY SLIDE LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE L2 DOOR EMERGENCY LIGHTS CHARGER ASSEMBLY. OPERATIONALLY CHECKS OK. 2L72 4F RTA2NM 20051230000062005123000006NM 2005 12 30 CALA0500451 120051216A24976130802 WIRE HARNESS BOEING737 7373T0 1384582NM LT MLG WW BURNED A CALAO OTHER J WARNING INDICATION LDLANDING 1 SW2717329 23459 LT WING BODY OVERHEAT LIGHT, FLAP IND SHOWED RT FLAP RETRACTED, LT FLAP 0700 POSITION. PRESSURIZATION AUTO FAIL LIGHT ILLUM. EMERGENCY DESCENT. M1205 ELEMENT REMOVED & REPLACED FOR OVERHEAT CONDITION, T/E FLAP POSITION IND REPLACED FOR LOCKOUT ISSUE, PRESSURIZATION CONTL TEST PERFORMED, NO FAULTS. LT O/B LANDING LIGHT REPLACED, C/B TRIPPING. FOUND WIRE BUNDLE W0802 WITH WIRES DAMAGED AT CEILING LT MLG WW STA 713, 1 FT O/B OF JUNCTION. W802 WIRING HARNESS REPLACED, AREAS REPAIRED. BURNED WIRES W570-A-R & W570-A-B BTW S72 LMLG UP-LOCK SENSOR & C/P D4840P, WIRES REPLACED. BURNED WIRES W802-004-20 & W802-005-20 FWD OF SPLICE SP4202 & 4204 FOUND, WIRES RESPLICED. FUEL S/O WIRES O/B OF CANOE FAIRING SPLICED.2L72 4F RTA16WE 20051230000092005123000009NM 2005 12 30 2005UALA01073 120051003A5330 SKIN AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE FRAME 5 BIRD STRIKE A UALAK NONE O OTHER ININSP/MAINT 1 WP29851UA 1664 BIRD STRIKE DAMAGE AT FRAME 5 AT TO TOP OF RVSM AREA. *S/D* INST REPAIR DOUBLERS AND FRAME FLANGES PER SRM 53-11-11 AND UA-EVA-50672. 2L72 4F4 FRTA28NM E40NE 20051230000122005123000012NM 2005 12 30 2005UALA01480 120051219A339758781 WIRE BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29315UA 23947 FLOOR EEL LIGHTS ARE INOP FROM ROW 9ABC TO AND INCLUDING THE AFT GALLEY FLOOR LIGHT. REPLACED FEEDER CABLE. 2L72 4F4 FRTA16WE E21EU 20051230000132005123000013NM 2005 12 30 2005UALA01481 120051219A335060243 LIGHT BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU AFT CABIN LOOSE A UALAK NONE O OTHER ININSP/MAINT 1 WP29303UA 23644 FLOOR EMERGENCY LIGHT STRIP LOOSE IN AFT SECTION OF AIRCRAFT. RESECURED LIGHT STRIP. 2L72 4F4 FRTA16WE E21EU 20051230000172005123000017NM 2005 12 30 USAA051643 120051223A5330 SKIN BOEING737 737301 1384611NM BS 500D STR 1 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19591US 23936 BS 500D +2 STR 11 LT CRACKED. INSTALLED DOUBLER IAW EA 97191, DEFECT SIZE: 2.5 INCH. 2L72 4F RTA16WE 20051230000182005123000018NM 2005 12 30 USAA051642 120051223A5311 FRAME BOEING737 7374B7 1384702NM BS 663.75, S 3L CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 STA 663.75, S3L CRACKED. CUT OUT DAMAGE, INSTALLED FILLER, REPAIR ANGLE AND STRAPS IAW SRM 53-00-07-2R9, DEFECT SIZE: .25 INCH. 2L72 4F RTA16WE 20051230000202005123000020NM 2005 12 30 SB05174 120051221A27512061141 INDICATOR BOEING737 737401 1384701NM TE FLAPS FAULTY A USAAL ABORTED APPROACH O OTHER APAPPROACH 1 EA19409US383919528 23879 DCA - FLT 534 EN ROUTE PBI TO DCA DURING APPROACH, THE FLAPS WOULD NOT EXTEND PAST 13 DEGREES. THE CREW PERFORMED A GO-AROUND AND BROUGHT FLAPS BACK UP TO 1 DEGREE. DURING SECOND APPROACH, FLAPS OPERATED NORMALLY. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED FLAPS PER FAULT ISOLATION PROCEDURES (FIP). FLAPS CHECKED GOOD. REPLACED THE FLAP INDICATOR. SYSTEM CHECKS GOOD ON THE GROUND. 2L72 4F RTA16WE 20051230000212005123000021NM 2005 12 30 2005UALA01482 120051216A339758781 WIRE BOEING737 737522 138449FNM CFMINTCFM56 CFM563C 13802EU EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP2941UA 26676 FLOOR LIGHTING EMERGENCY FROM ROW 16 TO AFT GALLEY INOP. REPLACED AFT POWER FEED. 2L72 4F4 FRTA16WE E21EU 20051230000222005123000022NM 2005 12 30 2005UALA01484 120051220A5311 FRAME BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU BS 400 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29923UA 26643 FWD LT CABIN STA 400 FRAME WEB BETWEEN STRINGERS 8L & 9L CRACK AT AIR CONDITIONING DUCT ATTACH BRACKET. MAJOR REPAIR. REMOVED DAMAGE AND NDT FOR CRACK CONTAINMENT. FABRICATED AND INSTALLED NESTED ANGLE REPAIR PER SRM 53-10-84 REPAIR NR 3. 2L72 4F4 FRTA16WE E21EU 20051230000232005123000023NM 2005 12 30 2005UALA01485 120051220A5311 FRAME BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU BS 440 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29923UA 26643 FWD LT CABIN STA 440 FRAME WEB BETWEEN STRINGERS 8L & 9L CRACK AT AIR CONDITIONING DUCT ATTACH BRACKET. MAJOR REPAIR. REMOVED DAMAGE. FABRICATED AND INSTALLED NESTED ANGLE REPAIR PER SRM 53-10-84 REPAIR NR 3. 2L72 4F4 FRTA16WE E21EU 20051230000242005123000024NM 2005 12 30 2005UALA01486 120051220A5311 FRAME BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU BS 747 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29923UA 26643 FWD LT CABIN STA 747 FRAME WEB BETWEEN STRINGERS 8L & 9L CRACK AT AIR CONDITIONING DUCT ATTACH BRACKET. MAJOR REPAIR. REMOVED DAMAGE. FABRICATED AND INSTALLED NESTED ANGLE REPAIR. PER SRM 53-10-84 REPAIR NR 3. 2L72 4F4 FRTA16WE E21EU 20051230000252005123000025NM 2005 12 30 2005UALA01487 120051220A5311 FRAME BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU BS 827 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29923UA 26643 FWD LT CABIN STA 827 FRAME WEB BETWEEN STRINGERS 8L & 9L CRACK AT AIR CONDITIONING DUCT ATTACH BRACKET. MAJOR REPAIR. REMOVED DAMAGE. FABRICATED AND INSTALLED NESTED ANGLE REPAIR PER SRM 53-10-84 REPAIR NR 3. 2L72 4F4 FRTA16WE E21EU 20051230000262005123000026NM 2005 12 30 2005UALA01488 120051220A5311 FRAME BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU BS 867 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29923UA 26643 FWD LT CABIN STA 867 FRAME WEB BETWEEN STRINGERS 8L & 9L CRACK AT AIR CONDITIONING DUCT ATTACH BRACKET. MAJOR REPAIR. REMOVED DAMAGE. FABRICATED AND INSTALLED NESTED ANGLE REPAIR. PER SRM 53-10-84 REPAIR NR 3. 2L72 4F4 FRTA16WE E21EU 20051230000282005123000028NM 2005 12 30 2005UALA01490 120051220A5311 FRAME BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU BS 867 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29923UA 26643 FWD LT CABIN STA 867 FRAME WEB BETWEEN STRINGERS 8R & 9R CRACK AT AIR CONDITIONING DUCT ATTACH BRACKET. MAJOR REPAIR. REMOVED DAMAGE. FABRICATED AND INSTALLED NESTED ANGLE REPAIR. PER SRM 53-10-84 REPAIR NR 3. 2L72 4F4 FRTA16WE E21EU 20051230000292005123000029NM 2005 12 30 2005UALA01491 120051220A5313 STRINGER BOEING737 737522 138449FNM CFMINTCFM56 CFM563C 13802EU STA 907 STR 4 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29923UA 26643 CABIN STATION 907 AT STRINGER 4L STRINGER SPLICE CRACKED. MAJOR REPAIR. REMOVED AND REPLACED DAMAGED STRINGER SPLICE PER SRM 51-40-02. 2L72 4F4 FRTA16WE E21EU 20051230000302005123000030NM 2005 12 30 2005UALA01492 120051220A5322 SHEAR TIE BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU BS 360 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29923UA 26643 RT FWD CABIN STA 360 BETWEEN STRINGERS 13R & 14R SHEAR TIE CRACKED IN RADIUS. MAJOR REPAIR. REMOVED AND REPLACED SHEAR TIE REF SRM 51-40-02. 2L72 4F4 FRTA16WE E21EU 20051230000342005123000034NM 2005 12 30 2005UALA01496 120051219A335058807 LIGHT BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU AFT GALLEY INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29351UA 24319 AFT GALLEY EEL FLOOR LIGHT IS INOP. REPLACED EEL LAMP. 2L72 4F4 FRTA16WE E21EU 20051230000372005123000037 2005 12 30 2005UALA01499 420051220A2565 LANYARD AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE GIRT BAR HANDLE DISCONNECTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29442UA 780 AFT RT DOOR SLIDE GIRT BAR HANDLE RELEASE PIN & LANYARD WERE NOT CONNECTED. DOOR R2 SLIDE ASSY MR25614-1275 WAS INSTALLED IN DEN ON 12/9/2004 TO REPLACE SLIDE ASSY MR25614-158, WHICH HAD TO BE REMOVED DUE TO TIME. PER AMIS, THE SLIDE REPLACEMENT WAS ACCOMPLISHED PER AMM 25-62-44 AND THE REQUIRED INSPECTION WAS ALSO ACCOMPLISHED DURING THAT TIME. FROM THE TIME OF THE SLIDE REPLACEMENT UP UNTIL THE DISCOVERY OF THE DISCREPANCY, THERE WAS NO REPORTED ACTIVITY AT R2 DOOR THAT COULD HAVE ATTRIBUTED TO THE DISCONNECTION OF THE RELEASE PIN AND THE LANYARD. (NOTE: THIS RELEASE PIN IS USED TO DISCONNECT THE SLIDE FROM THE GIRT BAR, DURING SLIDE REMOVAL.) 2L72 4F4 FRTA28NM E40NE 20051230000382005123000038NM 2005 12 30 2005UALA01500 120051119A5210 SEAL BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU L1 DOOR DAMAGED A UALAA UNSCHED LANDING O OTHER CRCRUISE 1 WP29383UA 24658 RT FL DUE TO DOOR 1 LT AIR LEAK. DOOR SEAL DAMAGED. REPLACED DOOR SEAL. 2L72 4F4 FRTA16WE E21EU 20051227000482005122700048WP 2005 12 27 ABXA050368 120051116A5730 ACCESS PANEL DOUG DC8 DC863F 302198FWP RT WING LEAKING A ABXAK NONE K FLUID LOSS ININSP/MAINT 1 GL23826AX 46061 16 BLIND RIVETS LEAKING UPON PRESSURE CHECKS. RIGHT WING, STRINGER NR 5 NEAR ACCESS PANEL 505F. REMOVED 16 BLIND FASTENERS ON STRINGER NR 5 NEAR ACCESS PANEL 505F OF THE RIGHT WING AND WET INSTALLED NEW FASTENERS IAW DC8 SRM 51-1-21 USING 1422 B1/2 SEALANT. 2L74 4F 4A25 20051227000502005122700050WP 2005 12 27 ABXA050370 120051207A53209910078223 INTERCOSTAL DOUG DC9 DC931 3022065WP E/E BAY CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23943AX 47528 THE FORWARD INTERCOSTAL IN THE FORWARD AIR STAIR COMPARTMENT WAS CRACKED. REPAIRED AREA IAW DC9 SRM 53-01. 2L72 4F A6WE 20051227000532005122700053WP 2005 12 27 ABXA050378 120051210A531327779221 LONGERON DOUG DC9 DC931 3022065WP BS 699 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23943AX 47528 LONGERON 5 RIGHT WAS CRACKED AT STA 699. REMOVED CRACKED AREA SPLICED IN LONGERON REPAIR IAW DC9 SRM 53-02. 2L72 4F A6WE 20051227000542005122700054WP 2005 12 27 ABXA050375 120051210A531327779221 LONGERON DOUG DC9 DC931 3022065WP BS 718 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23943AX 47528 FOUND LONGERON 4 LEFT WAS CRACKED AT STA 718. REPAIRED AREA IAW DC9 SRM 53-02. 2L72 4F A6WE 20051227000602005122700060WP 2005 12 27 ABXA050359 120051208A532059107837 PAN DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23972AX 47631 INBOARD DOOR PAN CRACKED AT FORWARD INBOARD CORNER. REPAIRED DOOR IAW DC9 SRM. 2L72 4F A6WE 20051227000632005122700063NM 2005 12 27 USAA051617 120051221A52406545871523 SKIN BOEING737 7373B7 1384580NM FWD SERVICE DOORCRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19517AU 23703 FOUND FWD SERVICE DOOR-OUTER SKIN- LOWER HINGE CUT OUT. INSTALLED DOUBLER IAW TR 52-10-13, DEFECT SIZE: .25". 2L72 4F RTA16WE 20051227000762005122700076EA 2005 12 27 QXEA200501800 120051124A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA BS 280 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09604QX 10019 YYC - BULKHEAD AS FUSELAGE STATION 280 RIGHT LOWER WEB IS CORRODED. REPAIRED WEB IAW REO 670-53-11-052 REVISION A. 2L72 4F RTA21EA 20051227000922005122700092 2005 12 27 DL76G050765 420051205A34604058650930 CDU BOEING767 767324 1385203NM COCKPIT INOPERATIVE A DALAA UNSCHED LANDING O OTHER CRCRUISE 1 SO27394DL 27394 IR - RT CDU WENT BLANK EN ROUTE RESET WITH CB NO FIX. CDU LEFT NO FIX. CDU RT SELECT ON F/O SIDE GOT V TRACK FLAG. FOUND RT CDU COOLING SCREEN CLOGGED CAUSING O/HEAT. REPLACED RT FMS CDU PER MM. CKS OK. 2L72 4F RTA1NM 20051227000972005122700097NM 2005 12 27 USAA051635 120051221A5330 SKIN BOEING737 7374B7 1384702NM BS 403, STR 14R CANNING A USAAK NONE O OTHER ININSP/MAINT 1 EA19781AU 25020 FOUND OIL CANNING STA 403, STR 14R-15R. FAB REPAIR DOUBLER/TRIPLER/FILLERS PER 53-00-01, 53-30-01, DEFECT SIZE: 1.85" X 1.80". 2L72 4F RTA16WE 20051227001002005122700100NM 2005 12 27 USAA051638 120051221A52106555478502 GATE BOEING737 7374B7 1384702NM PAX DOOR CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19781AU 25020 FOUND CORROSION AFT ENTRANCE DOOR, LOWER GATE. REMOVED AND REPLACED PER SRM 52-10-02; 51-40-05; CORROSION LEV 1; TASK C5310701, DEFECT SIZE: 21"L X 0.250"W X 0.154"D. 2L72 4F RTA16WE 20051227001072005122700107NM 2005 12 27 SWAA054061 120051221A5311963820 FRAME BOEING737 7373H4 1384600NM BS 178 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29361SW 26572 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE BS 178 BULKHEAD LEFT SIDE CHORD CRACKED AT WL 207. REMOVED AND REPLACED LEFT SIDE CHORD PER SWA ACO. 2L72 4F RTA16WE 20051227001092005122700109NM 2005 12 27 SWAA054063 120051221A53306545768 SKIN BOEING737 7375H4 138449DNM BS 385-387 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29511SW 24188 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 385 TO BS 387, STR 4R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051227001102005122700110NM 2005 12 27 SWAA054064 120051221A53156546811 FLOORBEAM BOEING737 7375H4 138449DNM BS 1016 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29511SW 24188 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 1016, RBL 30.5. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20051227001232005122700123NE 2005 12 27 2005F00114 220051209A7314025323150 SPLINE SUNDSTRANDEM CESSNA208 208B 2073701CE PWA PT6 PT6A114 52043NE MCAULY3DF36CB3DF36C526 GL DRIVE ASSY CORRODED E AWHAK NONE O OTHER ININSP/MAINT 1 WP17969FE 2951 846 208B0092 17219 981511 PRECAUTIONARY INSPECTION OF THE FUEL PUMP DRIVE SPLINE IN ACCORDANCE WITH PRATT AND WHITNEY PT6 MAINTENANCE MANUAL, FUEL PUMP COUPLING IN-SITU INSPECTION 73-10-02 PAGE 210, PARAGRAPH 8D, MAINTENANCE FOUND THE FUEL PUMP DRIVE SPLINE SEVERELY CORRODED AND DAMAGED TO THE POINT OF NEAR FAILURE. THE FUEL PUMP ASSEMBLY WAS REPLACED WITH A FRESH OVERHAULED UNIT AND THE AIRCRAFT RETURNED TO SERVICE. 1H71 3T3 T A37CE E4EA 5 C 20051227001312005122700131NM 2005 12 27 SWAA054051 120051220A57556546451 SKIN BOEING737 7373T5 1384608NM LT WING SPOILER DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29667SW 23063 DURING SCHEDULED C4 CHECK, FOUND LT WING SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PER MM. 2L72 4F RTA16WE 20051227001352005122700135NM 2005 12 27 SWAA054055 120051219A53306552988 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051227001402005122700140NM 2005 12 27 P5CA0501422 120051215A291310930014 DRIVE ASSY BOEING747 747230B 1384889NM ADP DAMAGED A P5CAO OTHER O OTHER TXTAXI/GRND HDL 1 EA15509MC 21221 ADP CHUGGING, REPORTING NO PRESSURE. OPENED MEL 29-2B 2L74 4F A20WE 20051227001432005122700143NM 2005 12 27 P5CA0501413 120051108A7600 ENGINE BOEING747 74746NF 13848BTNM GE CF6 CF680C2* GL NR 3 MALFUNCTIONED A P5CAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 EA15453PA 30811 70634 NR 3 ENG THRUST LEVER WOULD NOT ADVANCE TO TAKEOFF POWER ON T/O ROLL. LOW SPEED ABORT PERFORMED. A/C RETURNED TO BLOCKS. VISUAL INSPECTION OF THROTTLE & PEDESTAL MECHANISM PERFORMED PER MM 76-11-03. NO DISCREPANCIES FOUND AUTOTHROTTLE. FULL POWER ENGINE GROUND RUN PERFORMED. FLIGHT CREW NOTED, OPS CHECK OF SYSTEM GOOD. 2L74 4F4 FRTA20WE E23EA 20051227001512005122700151NM 2005 12 27 SWAA054008 120051217A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM GE CFM56 CFM563B1 13802NE BS 727C CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29622SW 27932 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727C, STR 4L. REMOVED AND REPLACED CLIP IAW SRM. 2L72 4F4 FRTA16WE E2GL 20051227001582005122700158NM 2005 12 27 SWAA054017 120051218A534065C27314 STRINGER CLIP BOEING737 7373Q8 1384670NM GE CFM56 CFM563B1 13802NE BS 294 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 294.5, STR 13L. REMOVED AND REPLACED CLIP IAW SRM. 2L72 4F4 FRTA16WE E2GL 20051227001632005122700163NM 2005 12 27 SWAA053826 120051130A3350MS155721 BULB BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29339SW 24090 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR LOWER EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT IAW MM. 2L72 4F RTA16WE 20051227001652005122700165NM 2005 12 27 SWAA053828 120051201A33506042221 LIGHT BOEING737 7377H4 1384404NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29409WN 27896 DURING SCHEDULED RON CHECK, FOUND R2 DOOR LOWER EMERGENCY EXIT LIGHT BASE BROKEN. REMOVED AND REPLACED LIGHT ASSY IAW MM. 2L72 4F RTA16WE 20051227001692005122700169 2005 12 27 SWAA053832 420051130A2565D31354 SLIDE BOEING737 7373H4 1384600NM GE CFM56 CFM563B1 13802NE R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29637SW 27710 DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE IAW MM. 2L72 4F4 FRTA16WE E2GL 20051227001702005122700170NM 2005 12 27 SWAA053833 120051130A3350BR2013 LIGHT BOEING737 7373H4 1384600NM GE CFM56 CFM563B1 13802NE CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29637SW 27710 DURING SCHEDULED C3 CHECK, FOUND EEPLS STRIP LOOSE AT ROW 8 DEF. SECURED STRIP IAW MM. 2L72 4F4 FRTA16WE E2GL 20051227001772005122700177NM 2005 12 27 ASAA0540407 120050816A53206517688129 ANGLE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU BS 309 DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 DAMAGED MOPSILL REINFORCEMENT ANGLE. REMOVED AND REPLACED IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20051227001802005122700180NM 2005 12 27 05FDEA04172 120051207A5330 SKIN BOEING727 727200 138407ENM PWA JT8 JT8D9A 52048NE BS206,STR24-24L BULGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 N00204 BS 206, STR 24-24L, 2 INCH CREASED BULGE IN THE SKIN. REPAIRED FUSELAGE SKIN AT BS 206, STR 24L-25L AS PER FED EX EA 7-5310-91431 2L73 4F4 FRTA3WE E2EA 20051227001822005122700182EU 2005 12 27 SA05129 120051217A335032145410 EPSU AIRBUSA319 A319112 3930323EU PAX CABIN FAULTY A USAAK NONE L NO TEST ININSP/MAINT 1 EA19768US1212711845 1389 PIT - THE EMERGENCY LIGHTS FAILED TEST WITH MESSAGE "EPSU INT LOAD EMER R". MAINTENANCE REPLACED THE MID-CABIN, RIGHT SIDE EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20051227001842005122700184WP 2005 12 27 ABXA050373 120051207A5320991555351 INTERCOSTAL DOUG DC9 DC931 3022065WP BS 598-579 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23943AX 47528 FS STA 598-579, LONGERON 27 LEFT AND 28 LEFT, CORRODED. REMOVED AND REPLACED INTERCOSTAL IAW DC9 SRM 51-30. 2L72 4F A6WE 20051227001862005122700186WP 2005 12 27 ABXA050374 120051207A57535910134152 SKIN DOUG DC9 DC931 3022065WP TE FLAPS CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23943AX 47528 SPOT OF CORROSION ON LOWER SIDE OF FLAP LEADING EDGE, AT OUTBOARD END OF INBOARD FIXED VANE. REPAIRED AREA IAW DC9 SRM 57-01. 2L72 4F A6WE 20051227002232005122700223NM 2005 12 27 05FDEA04388 120051221A2780 SWITCH BOEING727 727200 138407ENM PWA JT8 JT8D9A 52048NE SLAT SYS MALFUNCTIONED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25465FE 21289 PASSING FL250 RECEIVED INTERMITTENT LE FLAPS AMBER INDICATOR ON FORWARD PANEL WITH INTERMITTENT NR1 SLAT INDICATOR ON S/O AUX PANEL. RAN RED TABS WITH NORMAL EXTENSION TO FLAPS 30. REPLACED NR 1 SLAT RETRACT SWITCH IAW 27-82-011-4, REPLACED NR1 SLAT ACTUATOR PER 27-81-032-4. INDICATIONS NORMAL. RI 2L73 4F4 FRTA3WE E2EA 20051227002252005122700225NM 2005 12 27 05FDEA04157 120051206A5320 FLOOR SUPPORT BOEING727 727200 138407ENM PWA JT8 JT8D9A 52048NE BS 304 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 N00770 CORROSION (C53-221-01) BS 304, WL 208, LBL 12 TO 50 HOZ FLOOR SUPPORT UPPER FLANGE. REPAIRED FLOOR SUPPORT IAW SRM 51-30-2. 2L73 4F4 FRTA3WE E2EA 20051228000072005122800007SO 2005 12 28 SWIA200516017 120051219A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07576SW725 725 120345 EMERGENCY LIGHTS REAR OF ROW 9 INOP. REPLACED AFT ELBP. OPERATIONAL CHECK GOOD IAW 24-10-05. 2L72 4T RTA31SO 20051228000252005122800025EU 2005 12 28 QML2005F00000 120051130A27529787320308 ACTUATOR PILATSPC12 PC12 7090550EU PWA PT6 PT6* 52043EA TE FLAPS INOPERATIVE D QMLAO OTHER O OTHER NRNOT REPORTED 1 NM03912NM 169 WHEN THE AIRCRAFT IS FLOWN AT VERY LOW TEMPERATURES (BELOW -15 C) FOR MORE THAN 30 MINUTES, AND THE FLAPS ARE SELECTED THE FLAPS FAIL TO MOVE, FLAP WARNING IS GIVEN ON THE CAWS PANEL AND THE FLAPS ARE RENDERED (INOPERATIVE). ONCE THE AIRCRAFT IS ON THE GROUND, AT WARMER TEMPERATURES, THE FLAP RESET IS USED, AND THE FLAPS ARE FUNCTIONAL AGAIN. INSPECTION REVELS THAT THE FLAP ACTUATORS BECOME HARD TO TURN WHEN COLD. THIS IS VERIFIED BY PERFORMING THE CURRENT DRAW TEST IAW THE MFG MM. IT IS RECOMMENDED THAT THE FLAP ACTUATORS BE REDESIGNED TO TOLERATE THE LOWER TEMPERATURES OR A SIMPLER AND EASIER FIX WOULD BE TO INSTALL HEATERS ON EACH FLAP ACTUATOR TO KEEP THEM WARM ENOUGH TO FUNCTION PROPERLY. 1L71 3T3 TRTA78EU E2NE 20051228000392005122800039EA 2005 12 28 TIM2005F00013 220051118A7200PT6A27 ENGINE BEECH 99 99A 1154003CE PWA PT6 PT6A27 52043EA RIGHT FAILED A TIMAO OTHER RYJPARTIAL RPM/PWR LOSS ENGINE STOPPAGE WARNING INDICATION NRNOT REPORTED 1 NM07899CA U104 PCE40522 AIRCRAFT IN FLIGHT AT 13000 FT OIL PRESSURE AND TORQUE STARTS TO FLUCTUATED SLIGHTLY, MOMENTS LATER THE ENGINE FAILED. NO CAUSE FOR FAILURE HAS BEEN FOUND AT THIS TIME. THE ENGINE HAS BEEN TAGGED. THE ENGINE HAS 87.5 HOURS SINCE REPAIRS TO THE ENGINE AT AN ENGINE SHOP. (K) 1L72 3T4 T A14CE E4EA 20051228000462005122800046GL 2005 12 28 ALG2005F00108 220051115A720023004545 ENGINE BELL 206 206L4 1182110SW ALLSN 250C 250C30P 03013GL NOISY E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03176AL 52146 LOUD HOWLING NOISE AT FLIGHT IDLE FROM THE ENGINE TRANSMISSION AREA. REPLACED ENGINE ASSEMBLY. (K) 1G71 3U3 UNCH2SW E1GL 20051228000482005122800048SW 2005 12 28 ALG2005F00117 120051114A2435200SGL111Q STARTER GEN BELL 206 206L4 1182110SW ALLSN 250C 250C30P 03013GL NOISY E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03176AL 52146 PILOT HEARD LOUD NOISE FROM THE ENGINE COMPARTMENT. REMOVED STARTER GEN AND INSTALLED A SERVICEABLE TSO GENERATOR. RAN AC FOR 30 MINUTES AT GROUND IDLE AND 100 PERCENT RPM FOR 10 MINUTES WITH NO NOISE OCCURRING. REMOVED AND INSPECTED ENGINE CHIP PLUGS, CHECKED GOOD. REMOVED FUEL PUMP AND INSTALLED A SERVICEABLE FUEL PUMP. C/W A VIBRATION CHECK. VIBE CHECK GOOD. AC RETURNED TO SERVICE. (K) 1G71 3U3 UNCH2SW E1GL 20051228000522005122800052GL 2005 12 28 KBM2005F00343 220051103A751067A258 ACTUATOR BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL ANTI ICE SYSTEM INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1973DP 889 2513 ACTUATOR, UNIT INOPERATIVE, REMOVED AND REPLACED. (K) 1G71 3U3 U H2SW E4CE 20051228000542005122800054SW 2005 12 28 KBM2005F00357 120051202A7921206061432111 CAGE BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL BLOWER DAMAGED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1973DP 2513 FOUND OIL COOLER IMPELLER DAMAGED. REMOVED AND REPLACED BLOWER CAGE ASSY. (K) 1G71 3U3 U H2SW E4CE 20051228000582005122800058SW 2005 12 28 ALG2005F00111 120051118A6397 CONNECTOR BELL 407 407 1182206SW ALLSN 250C 250C47B GL XMSN PRESSURE DIRTY E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03457AL 53151 IN FLIGHT, TRANSMISSION PRESSURE INDICATOR OSCILLATING BETWEEN 0-120 PSI. CLEANED CONNECTOR PLUG ON TRANSMISSION TRANSMITTER. GROUND OPERATIONAL CHECK GOOD. (K) 1G71 3U3 UO H2SW E1GL 20051228000602005122800060NM 2005 12 28 GAIA05035OP 120051206A3297 CONNECTOR BOEING727 7272J0 138407ENM PWA JT8 JT8D15 52051NE NLG DIRTY A GAIAO OTHER N FALSE WARNING APAPPROACH 1 SW07281KH 21105 DURING APPROACH, INITIAL GEAR EXTENSIO, NOSE GEAR INDICATOR (NOT SAFE), AFTER RECYCLE AND A SHORT DELAY INDICATION NORMAL. LANDING WAS MADE WITHOUT INCIDENT. CLEAN AND RESEATED NOSE GEAR CONNECTOR PLUGS. INSPECTED NOSE GEAR AREA. NO DEFECT NOTED. CHECKED GEAR INDICATION, OPS CHECKED GOOD. (K) 2L73 4F4 FRTA3WE E2EA 20051228000612005122800061EU 2005 12 28 B652005F00000 120050520A2910MS274076 SWITCH BOLKMS105 BO105LSA3 5626020EU ALLSN 250C 250C28 03013GL HYD SYS TEST STUCK E B65AK NONE L NO TEST ININSP/MAINT 1 GL13202LF 2014 WHEN PERFORMING THE FUNCTIONAL TEST OF THE HYDRAULIC SYSTEM, CHAPTER 43-14, PG 24 OF THE MM. UNABLE TO GET THE HYDRAULIC UNIT TO SWITCH OVER TO THE NR 2 POSITION. DURING THE INVESTIGATION, IT WAS OBSERVED THAT THE HYDRAULIC TEST SWITCH WAS STUCK IN THE RESET POSITION. THE RESULT WAS WHEN FAILING THE NR 1 SYSTEM THE HYDRAULIC PAC SHOULD SWITCH OVER TO THE NR 2 SYSTEM, IT WAS TRYING TO RESET TO THE NR 1 POSITION. ADJUSTING THE SWITCH AND THE GUARD YIELDED NO SUCCESS. REPLACING THE SWITCH AND THE SWITCH GUARD YIELDED A POSITIVE RESULT. (K) 1G72 3U3 U H3AU E1GL 20051228000722005122800072EA 2005 12 28 A6WA200540350 120051207A7110 DOOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT NACELLE MISSING A A6WAO OTHER D INFLIGHT SEPARATION CLCLIMB 1 GL31468AW 7916 ON CLIMB OUT, FELT LURCH. UPON INSPECTION, DISCOVERED LT ENGINE DOOR MISSING. REMOVED AND REPLACED LT LOWER COWL DOOR. (PN 228-50081-141). (K) 2L72 4F4 FRTA21EA E15NE 20051228000782005122800078SO 2005 12 28 SIMA200531103 120051102A339778241 INVERTER EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21711PH 145235 THE CENTER FLOOR EMERGENCY LIGHT STRIPS WERE FAILED TO TEST. REPLACED THE DC/AC INVERTER ASSY. OPS CHECK GOOD. AC RETURNED TO SERVICE. (K) 2L72 4F4 FRTT00011ATTE6CH 20051228000812005122800081SO 2005 12 28 SIMA200533602 120051127A532014525381003 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21665AR4628 145778 THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED THE CORROSION BY MAKEING A CUTOUT. PREPARED A DOUBLER, FILLER, PLATE AND 2 SHIMS. REPAIR DONE IAW SRM. (K) 2L72 4T4 FRTT00011ATTE6CH 20051228000832005122800083SO 2005 12 28 SIMA200532907 120051113A532014522178005 SILL EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21826AE 145592 DURING INSPECTION FOUND SERVICE DOOR CENTER SILL CORRODED. REPAIRED SERVICE DOOR SILL BY INSTALLING A DOUBLER IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4F4 FRTT00011ATTE6CH 20051228000892005122800089SO 2005 12 28 SIMA200532507 120051107A532014525381003 FLOOR SUPPORT EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21613AE15292 145081 THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 25. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED A DOUBLER, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (K) 2L72 4F4 FRTT00011ATTE6CH 20051228000932005122800093SO 2005 12 28 TVM2005F00000 120051122A29101159SCH2463 VALVE GULSTMG1159 GIV 3980115SO RROYCETAY TAY6118 EU HYDRAULIC SYS FAILED E TVMAO OTHER K FLUID LOSS NRNOT REPORTED 1 EA25212WZ 1489 LOWER HOUSING RUPTURED, CAUSING FLUID LEAK. (K) 2L72 4F4 FRTA12EA E25NE 20051228000962005122800096EU 2005 12 28 QML2005F00001 120051130A27529787320308 ACTUATOR PILATSPC12 PC12 7090550EU PWA PT6 PT6* 52043EA TE FLAPS INOPERATIVE E QMLAO OTHER O OTHER NRNOT REPORTED 1 NM03912NM3625 169 WHEN THE AIRCRAFT IS FLOWN AT VERY LOW TEMPERATURES (BELOW -15 C) FOR MORE THAN 30 MINUTES, AND THE FLAPS ARE SELECTED THE FLAPS FAIL TO MOVE, FLAP WARNING IS GIVEN ON THE CAWS PANEL AND THE FLAPS ARE RENDERED INOPERATIVE. ONCE THE AIRCRAFT IS ON THE GROUND, AT WARMER TEMPERATURES, THE FLAP RESET IS USED, AND ACTUATORS BECOME HARD TO TURN WHEN COLD. THIS IS VERIFIED BY PERFORMING THE CURRENT DRAW TEST IAW THE MFG MM. IT IS RECOMMENDED THAT THE FLAP ACTUATORS BE REDESIGNED TO TOLERATE THE LOWER TEMPERATURES OR AN SIMPLER AND EASIER FIX WOULD BE TO INSTALL HEATERS ON EACH FLAP ACTUATOR TO KEEP THEM WARM ENOUGH TO FUNCTION PROPERLY. (K) 1L71 3T3 TRTA78EU E2NE 20051228001082005122800108NE 2005 12 28 ALG2005F00100 120051203A6340 CONNECTOR SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL TRANSMISSION DIRTY E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03518AL 760134 FIVE MINUTES AFTER TAKEOFF, TRANSMISSION GAUGE FLUCTUATED AND THEN DROPPED TO ZERO. FOUND TRANSMISSION CONNECTOR PLUG FULL OF OIL AND DIRT. CLEANED CONNECTOR PLUG. GROUND RUN AC WITH NO DEFECTS NOTED. (K) 1G72 3U3 U H1NE E1GL 20051228001292005122800129EU 2005 12 28 ALG2005F00115 120051109A5610350A25902820 WINDSHIELD UROCOPEC120 EC120B 8680987EU COCKPIT CRACKED E ALGAK NONE O OTHER ININSP/MAINT 1 SW03514AL 1266 DURING PREFLIGHT FOUND 5 SEPARATED, DEBONDED AREAS ON WINDOWS AND A CRACK IN THE WINDSHIELD. INSPECTION BY MAINT REVEALED THE NR 8 TAIL ROTOR DRIVE SHAFT HAD FAILED. A WO WAS OPENED FOR REPAIR OF THIS AC. REMOVED AND REPLACED PILOTS WINDSHIELD. (K) 1G72 3U NCR0001RD 20051228001712005122800171NM 2005 12 28 AWXA200501585 120051116A532065479573 WEB BOEING737 7373S3 1384711NM BS 794-847 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 MCN - MAJOR REPAIR - DURING C20 CHECK DISCOVERED CORROSION ON THE AFT CARGO LOWER SILL WEB AT BS 794 TO BS 847 AND BETWEEN BL 20R AND BL 28R. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-15-1A1 FIG 101. MAINTENANCE REMOVED WEB AND INSTALLED NEW WEB AT BS 749 TO BS 847 AND BETWEEN BL 20R AND BL 28R IAW BOEING 737-300 SRM 51-40-02-0G. 2L72 4F RTA16WE 20051228001732005122800173EA 2005 12 28 SWIA200516006 120051217A2760 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 NM07912SW 7595 FLT SPOILERS FAULT STATUS MSG ON APPROACH INTO DEN. REPLACED BOTH NR 1 AND NR 2 SECU'S IAW AMM 27-61-05. OPERATIONAL CHECK GOOD, PN 49-164-05, SN/OFF 01428, PN 49-164-05, SN/OFF 01427. 2L72 4F RTA21EA 20051228001752005122800175SO 2005 12 28 SWIA200516008 120051104A5347 SEAT TRACK EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07268UE 120207 LT SIDE CABIN FLOOR SEAT TRACK FWD END HAS CORROSION, ITEM FOUND AT C-CHECK INSPECTION. REPLACED FORWARD END OF LT SIDE CABIN FLOOR SEAT TRACK IAW EMB120 MM 53-01-05. 2L72 4T RTA31SO 20051228002042005122800204SW 2005 12 28 ALGA106938 120051119A2897407076501107 WIRE HARNESS BELL 407 407 1182206SW ALLSN 250C 250C47B GL FUEL SYSTEM CHAFED B ALGAK NONE O OTHER ININSP/MAINT 1 SW03497AL8670 53172 CHAFING AT AREAS WHERE CABLE COMES THROUGH TRANSFER TUBE. ADDED CHAFING PROTECTION TO CABLE ASSY OR ADELING IN ANOTHER MANNER. 1G71 3U3 UO H2SW E1GL 20051228002062005122800206CE 2005 12 28 DJFA2005169 120051128A2120 UNKNOWN CESSNA525 525 2076601CE WILINTFJ44 FJ441A GL CABIN FUMES E DJFAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA23247CW 5250247 THE CREW REPORTED THAT WHILE IN FLIGHT, BLEED AIR WAS LEAKING INTO THE CABIN AND CREATING NOXIOUS FUMES. MAINTENANCE RAN BOTH ENGINES WITH THE BLEED AIR SOURCE IN ALL POSSIBLE CONFIGURATIONS. NO DEFECTS WERE FOUND. THE VAPOR CYCLE SYSTEM WAS CHECKED FOR OPERATION AND DRAINAGE, AND THE FRESH AIR DUCT AND FAN WERE CHECKED WITH NO NOTED DEFECTS. BOTH ENGINES WERE RAN AGAIN WITH THE COWLING REMOVED, AND NO DEFECTS WERE FOUND. ALL OPERATIONAL CHECKS WERE GOOD, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1L72 4F4 FRTA1WI E3GL 20051228002152005122800215GL 2005 12 28 AMSA102805 120051028A521012545001 STRUT CIRRUSSR SR22 2130001GL PAX DOOR DAMAGED D AMSAO OTHER Z SIGNIFICANT FAILURE REPORT TXTAXI/GRND HDL 1 SW99 0920 PILOT SIDE DOOR PISTON, THAT GOT DISCONNECTED AND JAMMED PILOT'S CONTROL STICK. THERE IS NO WAY, THAT AC COULD BE FLOWN IN THIS CONDITION. IN ORDER TO FREE CONTROLS, DOOR UPHOLSTERY HAD TO BE REMOVED AND PISTON ON DOOR SIDE HAD TO BE DISCONNECTED, DOOR HAD TO BE OPENED AND THEN THE PISTON THAT WAS CAUGHT IN THE CONTROL STICK COULD BE REMOVED. AFTER REMOVAL, FOUND THAT THE PLASTIC ROD END OF THE PISTON HAD BROKEN AND THE PISTON ROD HAD BENT. THE AIRCRAFT OWNER INFORMED IMMEDIATELY THE COPA. THIS IS THE FIRST TIME WE HAVE HAD THIS HAPPEN. AFTER INVESTIGATION, DISCOVERED, THAT THE PISTON PLASTIC ROD END OF BOTH LT AND RT DOORS HAD BEEN DAMAGED AND WERE NOT FULLY LOCKING IN POSITION. 1L71 3O NTA00009CH 20051228002172005122800217WP 2005 12 28 IXXA05RNG079S 120050907A5500 SKIN DOUG DC8 DC872 302199BWP STA XE 104.051 DEFORMED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK WAS FOUND A OIL CAN ON LOWER SURFACE SKIN STA XE 104.051 TO 108.815 - LT. REPAIR SKIN AND REPAIR SPLICE WERE FABRICATED AND INSTALLED IAW SRM 55-2-1 FIG 2A AND EWO ATI 55-011. 2L74 4F RT4A25 20051228002192005122800219WP 2005 12 28 IXXA05RNG081S 120050916A5500 SKIN DOUG DC8 DC872 302199BWP STA XE 89.718 DEFORMED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11721CX81753 46013 DURING INSPECTION CHECK WAS FOUND A OIL CAN ON LOWER SURFACE SKIN STA XE 89.718 TO 108.843-LT. REPAIR DOUBLER WAS INSTALLED IAW EWO ATI 55-013 AND SRM 55-2-1 FIG 2A. 2L74 4F RT4A25 20051228002212005122800221WP 2005 12 28 ABXA050292 120051129A53305779942 SKIN DOUG DC8 DC863F 302198FWP BS 60 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23812AX 46126 CORROSION FOUND ON THE WING TO FUSELAGE SKIN AT STATION 670 AND LONGERON 36. REA D853-52756MR PERFORMS AN INTERIM REPAIR SIMILAR TO SRM 53-2-1, FIG. 7, AS OPERATIONAL SCHEDULING DID NOT ALLOW FOR A PERMANENT REPAIR. 2L74 4F 4A25 20051230000112005123000011EU 2005 12 30 2005UALA01479 120051220A3350321430 BATTERY AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE EMERGENCY LIGHT NO TEST A UALAK NONE L NO TEST ININSP/MAINT 1 WP29415UA 475 DURING 3 SVC EMERGENCY LIGHT TEST RECEIVED FAILURE, BATTERY EMERGENCY RT. REPLACED BATTERY PACK. REPLACED BATTERY PACK. 2L72 4F4 FRTA28NM E40NE 20051230000142005123000014 2005 12 30 EMB05020 420051226A25654A40302 SLIDE EMB ERJ170ERJ170100 EU PAX DOOR DEPLOYED A USAAK NONE O OTHER TXTAXI/GRND HDL 1 EA19820MD2888 17000041 FLIGHT 1702, DCA TO ALB - WHILE CLOSING THE FRONT ENTRY DOOR THE SLIDE WAS ACCIDENTALLY DEPLOYED. UPON DEPLOYMENT THE SLIDE BECAME DETACHED FROM THE AIRCRAFT. MAINTENANCE REMOVED AND REPLACED THE L1 DOOR SLIDE. 2L74 4F RTA56NM 20051230000162005123000016NM 2005 12 30 USAA051644 120051223A5311 FRAME BOEING737 737301 1384611NM BS 727D LBL4 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19591US 23936 FRAME 727D LBL 4 TO RBL 4 CRACKED. REMOVED DAMAGED AREAS, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW EA 97220, DEFECT SIZE: .125. 2L72 4F RTA16WE 20051230000422005123000042EA 2005 12 30 VNAA0512003 120051201A5300 RADOME CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE GROUND DAMAGE A VNAAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL05209PS 7874 WHILE PARKED FOR THE NIGHT THE RADOME WAS STRUCK AND DAMAGED BY A LAV SERVICING TRUCK. AFTER INSPECTING THE AIRCRAFT MAINTENANCE REMOVED AND INSTALLED A SERVICEABLE RADOME. NO OTHER DAMAGE WAS FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20051230000432005123000043EA 2005 12 30 VNAA0512002 120051201A215001649803 SENSOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE COOLING SYSTEM FAILED A VNAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL05258PS3189 7941 THE DISPLAY COOL CAUTION MESSAGE ILLUMINATED DURING CRUISE. THE CREW FOLLOWED THE QRH AND DIVERTED TO CAK. MAINTENANCE REMOVED AND REPLACED THE DISPLAY COOLING SYSTEM LOW FLOW SENSOR. THE SYSTEM OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20051230000492005123000049EA 2005 12 30 VNAA0512009 120051208A3097GG670800161 CONNECTOR CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE ANTI ICE SYS DENTED A VNAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL05708PS3457 10160 DURING CLIMB THE LT AND RT WING ANTI-ICE SYSTEMS CYCLED ON AND OFF. THE CREW FOLLOWED THE QRH AND RETURNED TO CLT. MAINTENANCE TROUBLESHOT THE SYSTEM AND FOUND THE NR 2 - NR 3 SLAT TRACK CONNECTOR FLEX TUBE DENTED CAUSING REDUCED BLEED AIR FLOW TO THE LT OUTBOARD SLAT. THE CONNECTOR WAS REPAIRED IAW BOMBARDIER REO 670-30-11-06. BOTH WING ANTI-ICE SYSTEMS OPERATIONALLY CHECKED GOOD AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20051230000512005123000051NM 2005 12 30 QXEA200501834 120051223A33503017773 SIGN DHAV DHC8 DHC8202 2809007NM EMERGENCY EXIT MALFUNCTIONED A QXEAO OTHER O OTHER TXTAXI/GRND HDL 1 NM09367PH 511 SEA - FORWARD LOWER CABIN EMERGENCY EXIT SIGN ON LEFT HAND SIDE INOP. MAINTENANCE REPLACED EMERGENCY EXIT SIGN AND PERFORMED OPERATIONAL TEST OF EMERGENCY LIGHT SYSTEM IAW DHC-8 200 AMM 33-51-01, PAGES 501-503 WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051230000522005123000052NM 2005 12 30 QXEA200501832 120051222A243023088002B GENERATOR DHAV DHC8 DHC8202 2809007NM DC SYS MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09349PH* 19 486 FLIGHT NR 2093, NR 1 DC GENERATOR ILLUMINATED DURING CLIMB-OUT, RAN CHECKLIST AND RESET GENERATOR, CAUTION LIGHT REMAINED OUT FOR REMAINDER OF FLIGHT. MAINTENANCE REPLACED NR 1 DC STARTER/GENERATOR IAW MTC 98010-001. FUNCTIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051230000532005123000053NM 2005 12 30 QXEA200501833 120051225A61233014403 CONTROL UNIT DHAV DHC8 DHC8202 2809007NM AUTO FEATHER SYSMALFUNCTIONED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09353PH9694 704 496 SEA FLIGHT NR 2230, AFTER PUSHBACK, RAN THE DAILY CHECKS ON THE AUTO FEATHER SYSTEM, THE NR 2 SIDE WOULD NOT FEATHER. UPTRIM LIGHT CAME ON AND ARM LIGHT COMES ON, THEN THERE IS NOT A FEATHER ALTERNATE FEATHER NEVER CAME ON THEN THE AUTO FEATHER ARM LIGHT WENT OUT. MAINTENANCE REPLACED THE TSCU. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051230000542005123000054GL 2005 12 30 RAIA00512022 220051223A753223070418 LINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL BLEED VALVE BROKEN A RAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03825HK 145510 5533 - STL - ENGINE NR 2 ITT EXCEEDED TO YELLOW BRIEFLY HIGHER. MAINTENANCE REMOVED AND REPLACED BROKEN ACCELERATION BLEED VALVE LINE, OPS CK GOOD. 2L72 4T4 FRTT00011ATTE6CH 20051230000562005123000056SO 2005 12 30 RAIA00512026 120051226A3350100865 BATTERY PACK EMB 145 EMB145 3260210SO EMERGENCY LIGHT INOPERATIVE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03802HK 145066 3528 - RIC - EMERGENCY PATH STRIPS INOP BACK HALF OF CABIN. MAINTENANCE REMOVED AND REPLACED NR 3 AND NR 4 EMERGENCY LIGHT BATTERIES. 2L72 4F RTT00011AT 20051230000612005123000061NM 2005 12 30 DL76P050787 120051211A5330146T35313 SKIN BOEING767 767332 1382001NM BS 1375, S29R DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO271402A 25989 FUSELAGE SKIN AT STA 1375, STR 29R WAS FOUND DENTED AND GOUGED BEYOND SRM LIMITS, TOO CLOSE TO DOOR OPENING. INSTALLED REPAIR DOUBLER PER ER/A 452043-14 2L72 4F RTA1NM 20051230000622005123000062NM 2005 12 30 DL75K050790 120051215A2560G1020 BATTERY BOEING757 757232 1384965NM L1 DOOR DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27643DL 23997 FOUND L1 CABIN EMERGENCY FLASHLIGHT CHARGE LOW. REPLACED FLASHLIGHT BATTERY. 2L72 4F RTA2NM 20051230000632005123000063NM 2005 12 30 DL73S050792 120051215A3350RPS1B POWER SUPPLY BOEING737 737247 138448DNM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27239WA 23187 DURING LAYOVER, FOUND EMERGENCY ESCAPE PATH LIGHTING INOP FROM 1C TO 14DEF. REPLACED POWER SUPPLY AT FIRST CLASS CENTER AISLE OVERHEAD. 2L72 4F A16WE 20051230000642005123000064NM 2005 12 30 DL76L050793 120051215A361079275516 CONTROLLER BOEING767 767332 1382001NM LT ENGINE FAILED A DALAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO27181DN 25986 LEFT ENGINE PNEUMATIC SUPPLY PULSES TO 0 PSI ON THROTTLE RETARD THEN CATCHES UP. PRESSURIZATION OK BUT PULSES ALSO. REPLACED LT ENG HP S/O VLV PER MM. REPLACED HP CONTROLLER. NDS CK OUT. NO HELP. REPLACED LT ENG BLEED AIR CARD AND PRV CONTROLLER PER MM. CKS NORMAL. REMOVED MCO/PLAC. 2L72 4F RTA1NM 20051230000652005123000065NE 2005 12 30 DL76S050794 220051216A7261J221P222 PACKING BOEING767 767332 1382001NM GE CF680 CF680A2 NE NR 2 ENGINE LEAKING A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO27137DL 25306 580397 RIGHT ENGINE LOST OIL QTY IN FLIGHT. REPLACED STARTER SHAFT PACKING. 2L72 4F4 FRTA1NM E13NE 20051230000682005123000068NM 2005 12 30 AWXA200501595 120051120A532069434561 FILLER BOEING737 7373S3 1384711NM DOOR SILL CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 MCN - DURING C20 CHECK DISCOVERED CORROSION ON THE AFT CARGO LOWER SILL STRAP FROM BS 796 TO BS 812, WL 158.5 AND BL 19R. NO CORROSION REMOVAL LIMITS WERE AVAILABLE IN THE BOEING 737-300 SRM. MAINTENANCE REMOVED AND INSTALLED NEW AFT CARGO DOOR LOWER SILL STRAP FROM BS 796 TO BS 812, WL 158.5 AND BL 19R IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 3, 4, 6, 7 AND 8. 2L72 4F RTA16WE 20051230000712005123000071NM 2005 12 30 QXEA200501816 120051206A5347 SEAT TRACK BOMBDRDHC8 DHC8402 1390042NM BS 361-469 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09403QX 4037 PDX: LT OUTBOARD SEAT TRACK HAS NICKS, SCRATCHES, AND CORROSION ON TOP RAILS AND IN CHANNEL BETWEEN STA X361 AND X469. MAINTENANCE REPAIRED IAW SRM 51-42-05 ADN 51-40-10. 2H72 4T RTA13NM 20051230000752005123000075NM 2005 12 30 AWXA200501598 120051112A533065184201059 SKIN BOEING737 7373S3 1384711NM BS 215 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 MCN - DURING C20 CHECK DISCOVERED SKIN CRACKED, .320 INCHES, AT THE UPPER AFT CORNER OF THE CAPTAINS WINDSHIELD AT BS 215.8, WL 265 AND BL 26L. MAINTENANCE REMOVED DAMAGE IAW BOEING 737-300 SRM 53-10-01-2R10. FABRICATED FILLER AND DOUBLER IAW BOEING 737-300 SRM 53-10-01-2R10. INSTALLED FABRICATED REPAIR PARTS AT THE UPPER AFT CORNER OF THE CAPTAINS WINDSHIELD AT BS 215.8, WL 265 AND BL 26L IAW BOEING 737-300 SRM 53-10-01-2R10. 2L72 4F RTA16WE 20051230000762005123000076NM 2005 12 30 AWXA200501599 120051122A5522 SKIN BOEING737 7373S3 1384711NM ELEVATOR DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 MCN - DURING C20 CHECK DISCOVERED LT ELEVATOR UPPER SKIN HAD FIBER DAMAGE 46" FROM THE INBOARD EDGE OF THE ELEVATOR. MAINTENANCE REMOVED DAMAGED PLIES IAW BOEING 737-300 SRM 51-70-04-0G R1 FIG 10. BONDED REPAIR PLIES TO REPAIR AREA ON THE LT ELEVATOR UPPER SKIN IAW BOEING 737-300 SRM 51-70-04-0G FIG 10. 2L72 4F RTA16WE 20051230000772005123000077NM 2005 12 30 AWXA200501600 120051126A5542 SKIN BOEING737 7373S3 1384711NM RUDDER DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 MCN - DURING C20 CHECK DISCOVERED FIBER DAMAGE ON THE LT SIDE OF RUDDER 18" FROM THE TRAILING EDGE. MAINTENANCE REMOVED DAMAGED PLIES IAW BOEING 737-300 SRM 51-70-04-0G R1 FIG 10. BONDED REPAIR PLIES TO REPAIR AREA ON THE LT SIDE OF RUDDER IAW BOEING 737-300 SRM 51-70-04-0G FIG 10. 2L72 4F RTA16WE 20051230000782005123000078NM 2005 12 30 AWXA200501601 120051112A5754 SKIN BOEING737 7373S3 1384711NM NR 5 SLAT DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 MCN - DURING C20 CHECK DISCOVERED, THE RT WING, NR 5 SLAT, OUTBOARD TRAILING EDGE LOWER SKIN DELAMINATED. MAINTENANCE REMOVED DISBONDED SKIN IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED REPAIR FILLER AND REPAIR DOUBLER IAW BOEING 737-300 SRM 51-70-10-2R4. BONDED REPAIR PARTS ONTO THE NR 5 SLAT, OUTBOARD, TRAILING EDGE LOWER SKIN IAW BOEING 737-300 SRM 51-70-01-2R4. 2L72 4F RTA16WE 20051230000812005123000081NM 2005 12 30 AWXA200501604 120051116A532065566552 REVEAL BOEING737 7373S3 1384711NM BS 851 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 MCN - DURING C20 CHECK DISCOVERED CORROSION ON THE AFT CARGO DOOR CUTOUT, AFT, FRAME EDGE COVER AT BS 851, FROM WL 158 TO WL 164 AND FROM BL 22R TO BL 25R. NO CORROSION REMOVAL LIMITS WERE FOUND IN THE BOEING 737-300 SRM. MAINTENANCE FABRICATED NEW REVEAL STRIP IAW BOEING 737-300 SRM 51-40-05-0G FIG 3, 51-30-01-0G FIGURE 7 AND BOEING DWG 65-56655. INSTALLED FABRICATED REPAIR PARTS AT BS 851, FROM WL 158 TO WL 164 AND FROM BL 22R TO BL 25R FOR THE AFT CARGO DOOR CUTOUT FRAME EDGE COVER IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 3, 4, 6, 7 AND 8. 2L72 4F RTA16WE 20051230000882005123000088NM 2005 12 30 QXEA200501825 120051205A5347 SEAT TRACK BOMBDRDHC8 DHC8402 1390042NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09403QX 4037 PDX: LT INBOARD SEAT TRACK HAS PITS AND CORROSION IN CENTER CHANNEL BETWEEN STA X377.0 AND X394.5. MAINTENANCE REPAIRED IAW RD 8-53-884, SRM 20-10-01, SRM 51-42-05 AND SRM 51-40-15. 2H72 4T RTA13NM 20051230000912005123000091 2005 12 30 AWXA200501609 420051226A34144039891903 INDICATOR BOEING757 7572S7 1384962NM COCKPIT UNKNOWN A AWXAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 WP28902AW4755947207 23322 CREW REPORTED THAT ON TAKEOFF ROLL THE FO'S AIRSPEED INDICATOR WENT INOPERATIVE AT APPROXIMATELY 80 KTS. AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE MACH AIRSPEED INDICATOR ON THE F/O'S SIDE IAW BOEING 757-200 MM 34-13-02-4. OPS CHK GOOD. COULD NOT CONFIRM FAULT. UNIT INSPECTED AND TESTED IAW CMM 34-13-09 REV 12. 2L72 4F RTA2NM 20051230000932005123000093NM 2005 12 30 AWXA200501611 120051217A57536546486129 WEDGE BOEING737 7373G7 1384595NM TE FLAPS DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 MCN - MAJOR REPAIR - DURING C15 CHECK DISCOVERED DISBOND AREA UPPER SURFACE LT INBOARD MIDFLAP TRAILING WEDGE ASSEMBLY, FROM WBL 87.75 TO WBL 93.75. MAINTENANCE REMOVED DISBONDED AREA ON UPPER SURFACE OF THE LT INBOARD MID FLAP TRAILING EDGE WEDGE IAW BOEING 737-300 SRM 51-70-10-02R4. FABRICATED DOUBLER AND FILLER IAW BOEING 737-300 SRM 51-70-10-02R4. BONDED REPAIR PARTS TO THE UPPER SURFACE OF THE LT INBOARD MIDFLAP TRAILING WEDGE ASSEMBLY, FROM WBL 87.75 TO WBL 93.75 IAW BOEING 737-300 SRM 51-70-10-02R4. 2L72 4F RTA16WE 20051230000942005123000094NM 2005 12 30 AWXA200501612 120051220A5311651758245 FRAME BOEING737 7373G7 1384595NM BS 180 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 MCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED FRAME WEB CRACKED, 1 INCH, AT BS 180, WL 190 AND BL 17.1L. MAINTENANCE REMOVED DAMAGED WEB AND FABRICATED REPLACEMENT WEB IAW BOEING 737-300 SRM 51-40-05-0G FIG B, SHEET 1 AND DRAWING 65-17582 SHEET 9. INSTALLED FABRICATED REPAIR PARTS AT BS 180, WL 190 AND BL 17.1L IAW BOEING 737-300 SRM 51-40-02-0G AND SRM 51-21-99-307-001. 2L72 4F RTA16WE 20051230000952005123000095NM 2005 12 30 AWXA200501613 120051216A57526546455234P TAB BOEING737 7373G7 1384595NM AILERON DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 MCN - MAJOR REPAIR - DURING C15 CHECK DISCOVERED DELAMINATED AREA ON THE OUTBOARD UPPER SKIN OF THE LT AILERON TRIM TAB ASSY, FROM WBL 472.0 TO WBL 474.0. MAINTENANCE REMOVED DISBONDED AREA ON OUTBOARD UPPER SURFACE OF THE LT AILERON TRIM TAB ASSY IAW BOEING 737-300 SRM 51-60-03-0G FIG 1. BONDED REPAIR PLIES TO THE UPPER SURFACE OF THE LT AILERON TRIM TAB FROM WBL 472.0 TO WBL 474.0 IAW BOEING 737-300 SRM 51-60-03-0G FIG 1. AILERON WAS WEIGHED AND FOUND TO BE WITHIN LIMITS IAW BOEING 737-300 SRM 51-00-03-06. 2L72 4F RTA16WE 20051230000962005123000096NE 2005 12 30 AWXA200501614 220051224A75322607MK2 ACTUATOR AIRBUSA319 A319132 3930340NM IAE V2524 V2524A5 NE NR 1 ENGINE MALFUNCTIONED A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28817AW4166 4160 1373 LAX - ABORTED TAKEOFF - FLT 36 - CREW REPORTED THAT DURING TAKEOFF RECEIVED NR 1 COMPRESSOR VANE FAULT, ABORTED TAKEOFF UNDER 70 KNOTS. RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE VSV ACTUATOR. OPERATIONAL TESTS WERE GOOD. 2L72 4F4 FRTA28NM E40NE 20051230000992005123000099EA 2005 12 30 COMA0560744 120051222A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01917CA 7017 FLIGHT 5297 - AFTER LANDING AT NAS RECEIVED A FLAP FAIL CAUTION MESSAGE. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3, (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2L72 4F RTA21EA 20051230001002005123000100NM 2005 12 30 QXEA200501841 120051223A2750 FLAP SYSTEM BOMBDRDHC8 DHC8402 1390042NM TE FLAPS MALFUNCTIONED A QXEAD RETURN TO BLOCK J WARNING INDICATION UKUNKNOWN 1 NM09409QX 4051 RNO FLIGHT NR 2441, FLAP POWER CAUTION LIGHT ILLUMINATED. MAINTENANCE RESET NVW AND C/W Q400 SL-27-002A. CYCLED FLAPS. NO OTHER DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051230001012005123000101EA 2005 12 30 QXEA200501842 220051220A7200312162701 ENGINE BOMBDRDHC8 DHC8402 1390042NM PWC 150 PW150A EA NR 2 MALFUNCTIONED A QXEAEA ENGINE SHUTDOWN UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 NM09403QX8821 4037 PCEFA0124 SMF FLIGHT NR 2307: AT 25,000' SMOKE WARNING LIGHT FOLLOWED IN 1 TO 2 MINUTES BY THE NR 2 ENGINE OIL PRESS WARNING LIGHT. SHUTDOWN THE NR 2 ENGINE. MAINTENACE REMOVED AND REPLACED THE NR 2 ENGINE, NR 2 PROP, (P/N 697070003, S/N DAP0217), NR 2 AC GENERATOR (P/N 28B555-1, S/N 067C0102), AND NR 2 OIL COOLER AND BETA TUBE (P/N D2887-815A, S/N M107329) IAW QX MTC 6710003, 6710004, 6610003, 6610004, 6242101, 6610001, 6610002. OPERATED ECS SYSTEM WITH NR 2 ENGINE BLEED AIR UNTIL NO ODOR WAS NOTED. ALL CHECKS GOOD. NO LEAKS DETECTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E00062EN 20051230001032005123000103NM 2005 12 30 SWAA054129 120051227A53306545768 SKIN BOEING737 7373Q8 1384670NM BS 373 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT E/E COOLING EXHAUST OUTLET INTERNAL DOUBLER, BS 373 AND BS 378, LBL 2.8. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051230001042005123000104NM 2005 12 30 SWAA054130 120051227A53116546540 FRAME BOEING737 7373Q8 1384670NM BS 639 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, STR 17L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051230001052005123000105NM 2005 12 30 SWAA054131 120051227A534065C27314 STRINGER CLIP BOEING737 7373Q8 1384670NM BS 727B CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727B, STR 16R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051230001062005123000106NM 2005 12 30 SWAA054132 120051227A53226546546 SHEAR TIE BOEING737 7373Q8 1384670NM BS 747 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 747, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20051230001072005123000107NM 2005 12 30 SWAA054133 120051222A53306545776 SKIN BOEING737 7373G7 1384595NM BS 930-940 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29691WN 23781 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 930 TO BS 940, STR 23R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20051230001082005123000108NM 2005 12 30 SWAA054134 120051222A53306545776 SKIN BOEING737 7373G7 1384595NM BS 981 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29691WN 23781 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 981, STR 21L. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20051230001102005123000110NM 2005 12 30 SWAA054136 120051224A361032145525 SHUTOFF VALVE BOEING737 7377H4 1384404NM NR 1 ENGINE FAULTY A SWAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW29713SW 27847 DIVERSION/INFLIGHT SHUTDOWN/DECLARED EMERGENCY, LT WING TO BODY OVERHEAT LIGHT ILLUMINATED. LT DUCT PRESSURE DID NOT DROP. SHUTDOWN NR 1 ENGINE. REMOVED AND REPLACED NR 1 ENGINE PRSOV, LOW STAGE REGULATOR AND ENGINE BLEED AIR SOLENOID PER MM. 2L72 4F RTA16WE 20051230001122005123000112NM 2005 12 30 SWAA054138 120051221A3350MS155721 BULB BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29731SA 27863 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20060103000012006010300001EA 2006 1 3 ASOA051076 120051208A5330 DOUBLER CNDAIRCL600 CL6002B19 1900309EA BS 640 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27860AS 7433 DURING A HANGAR INSPECTION IN BTR, THE RIGHT SIDE FS 640, AT STRINGER 10, DOUBLER WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT SIDE FS 640, AT STRINGER 10, DOUBLER IAW CRJ 200 SRM 51-40. (M) 2L72 4F RTA21EA 20060103000022006010300002WP 2006 1 3 05FDEA04420 120051229A5754 SKIN DOUG MD10 MD1010F 3022112WP FLAP LE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25359FE 46635 DENT ON RIGHT HAND INBOARD FLAP LEADING EDGE AT XIFH 174-179. REPAIRED LEADING EDGE SKIN IAW DC10-10 SRM 57-00-01 FIG 4 VOL I. ALODINED AND PRIMERED IAW DC10-10 SRM 51-21-01 VOL. II. SEE FEDEX SNRM NR N00291 OF WORK ORDER NR 00031297. 2L73 4F RTA22WE 20060103000032006010300003NM 2006 1 3 05FDEA04421 120051229A7711 TRANSMITTER BOEING727 727233 138408ANM NR 3 EPR FAILED A FDEAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO25221FE 20932 NUMBER 3 ENG EPR GAUGE FAILED TO REACH TAKEOFF EPR. UPON BLOCK IN NUMBER 3 EPR WAS SPINNING. RELEASED FOR SERVICE PER MEL/CDL: 77-01-01 CAT 'C' EXP: 31DEC05. NR 3 ENGINE EPR INDICATOR, INOP. REMOVED AND REPLACED NR 3 EPR TRANSMITTER PER 727-200 M/M 77-11-011-4. SYSTEM CHECKS NORMAL PER M/M 31-26-000-5. 2L73 4F RTA3WE 20060103000042006010300004NM 2006 1 3 05FDEA04422 120051229A7711 INDICATOR BOEING727 727225 1384077NM NR 2 EPR INOPERATIVE A FDEAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO25463FE 22551 NR 2 EPR WOULD NOT REACH TAKEOFF EPR, NR 2 GAUGE WOULD ONLY REACH APPROXIMATELY 1.55 SETTING. ALL OTHER ENGINE GAUGES READ NORMAL. RELEASED FOR SERVICE PER MEL. NR 2 ENGINE EPR INDICATOR, INOP. RAN NR 2 ENGINE TO TEST EPR INDICATOR AND INDICATOR CHECKS GOOD IAW 727 JRH. REMOVED AND REPLACED NR 2 EPR INDICATOR IAW 727 SMP. 2L73 4F A3WE 20060103000052006010300005NM 2006 1 3 05FDEA04423 120051229A5330 SKIN BOEING727 727233 138408ANM BS 95E GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25274FE 22039 A GOUGE FOUND AT BS 950E, STR 19R DURING PRIMARY INSPECTION, REPAIR ACCOMPLISHED WITH EA 7-5330-92374 ISSUED BY FEDEX ENGINEERING, REPAIR IS CLASSIFIED AS MAJOR PER EA 7-5330-92374. 2L73 4F RTA3WE 20060103000072006010300007EA 2006 1 3 ASOA051064 120051205A323016154103 TORQUE LINK CNDAIRCL600 CL6002B19 1900309EA MLG DISCONNECTED A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27837AS 7271 DURING CLIMB-OUT FROM CAE-ATL, UPON GEAR RETRACTION, THE CREW RECEIVED GEAR DISAGREE AND NOSE DOOR OPEN WARNING MESSAGES ALONG WITH STEERING INOP AND WOW INPUT CAUTION MESSAGES. NOSE GEAR STAYED GREEN AND DOWN. THE CREW COMPLIED WITH THE QRH AND DECLARED AN EMERGENCY. THE AIRCRAFT RETURNED TO CAE, WHERE IT LANDED SAFELY. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NOSE GEAR TORQUE LINKS DISCONNECTED AND RECONNECTED THEM. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060103000082006010300008EU 2006 1 3 ASOA051063 120051205A33507012210 LAMP AEROSPATR72 ATR72 EU EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27643AS 413 DURING A GROUND INSPECTION IN ATL, THE EMERGENCY EXIT LIGHT, NEAR THE REAR SERVICE DOOR WAS, FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT, NEAR THE REAR SERVICE DOOR. OPERATIONAL CHECKS GOOD GOOD. AIRCRAFT OK FOR SERVICE 2H72 4T RT 20060103000092006010300009EA 2006 1 3 ASOA051065 120051205A5270 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA PAX DOOR FALSE INDICATIONA ASOAJA DUMP FUEL UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27836AS 7263 DURING CLIMB-OUT FROM OMA-ATL, AT APPROXIMATELY 8,000 FEET, THE CREW RECEIVED A PASSENGER DOOR LATCH CAUTION MESSAGE. THE CREW COMPLIED WITH THE QRH, WHEN AT APPROXIMATELY 18,500 FEET, A PASSENGER DOOR WARNING MESSAGE WAS RECEIVED. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO MCI, WHERE IT LANDED SAFELY. MAINTENANCE PRESSURIZED THE AIRCRAFT TO 5 DELTA P WITH NO DEFECTS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060103000112006010300011NM 2006 1 3 05FDEA04250 120051212A5330 SKIN BOEING727 727227 1384078NM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 NR 4 JACKSCREW FAIRING FUSELAGE GUIDE HOOK FITTING, FUSELAGE SKIN IS GOUGED 1 INCH BELOW. REPAIRED FUSELAGE SKIN PER SR 27-53-140A. 2L73 4F A3WE 20060103000122006010300012NM 2006 1 3 05FDEA04251 120051212A5347 SEAT TRACK BOEING727 727227 1384078NM BS 640-660 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 FOUND CORROSION C53-224-01, STA 640 - 660 BL 0 WL 208 CORROSION ON SEAT TRACK. REPLACED SEAT TRACK PER SRM 53-10-5. 2L73 4F A3WE 20060103000132006010300013NM 2006 1 3 05FDEA04252 120051212A5314 KEELBEAM BOEING727 727227 1384078NM BS 950C CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 FOUND CORROSION ON KEELBEAM BS 950C PLUS 8" STR29 RT. REMOVED CORROSION AND RESTORED TO NORMAL ON KEELBEAM BS 950C 8" IAW DWG SR 27-53-013-REV A. 2L73 4F A3WE 20060103000142006010300014EU 2006 1 3 05FDEA04253 120051212A5330 SKIN AIRBUS310 A310222 3930315EU BS 67-68 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25450FE 162 FOUND DENT/GOUGE ON SKIN BETWEEN FS 67-68 AND STR 15-16 RT (HURRICANE RITA) REF N00084. REPAIRED AREA IAW A310-200 SRM 53-10-12 AND 53-10-14. 2L72 4F RTA35EU 20060103000152006010300015EA 2006 1 3 ASOA051072 120051207A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27879AS 7600 DURING A HANGAR INSPECTION IN BTR, THE AFT CEILING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT CEILING EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060103000172006010300017EA 2006 1 3 ASOA051066 120051205A5260 HINGE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR STEP CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27882AS 7503 DURING A C-CHECK IN MCN, THE PASSENGER DOOR TOP STEP UPPER HINGE HALF WAS FOUND TO BE CORRODED. (M) 2L72 4F RTA21EA 20060103000182006010300018EA 2006 1 3 ASOA051074 120051208A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27855AS 7395 DURING A GROUND INSPECTION IN GSO, THE FORWARD CABIN OVERHEAD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE FORWARD CABIN OVERHEAD EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060103000192006010300019EA 2006 1 3 ASOA051070 120051123A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA BS 280 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27740EV 10151 DURING A C-CHECK IN TUS, THE LOWER LEFT SIDE FS 280 BULKHEAD WEB WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LOWER LEFT SIDE FS 280 BULKHEAD WEB IAW ASA EC EO700-53-0062, REPAIR NR 2. (M) 2L72 4F RTA21EA 20060103000202006010300020EA 2006 1 3 ASOA051067 120051206A1100S1859 PLACARD CNDAIRCL600 CL6002B19 1900309EA COCKPIT DETERIORATED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27882AS 7503 DURING A C-CHECK IN MCN, FOUR CREW EMERGENCY EXIT PLACARDS WERE FOUND TO BE DETERIORATED. MAINTENANCE WILL REMOVE AND REPLACE THE FOUR CREW EMERGENCY EXIT PLACARDS. (M) 2L72 4F RTA21EA 20060103000212006010300021NM 2006 1 3 SWAA054140 120051226A2913849589 PUMP BOEING737 7377H4 1384404NM NR 2 ENGINE FAULTY A SWAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW29752SW 29804 DECLARED EMERGENCY, NR 2 ENGINE HYDRAULIC PUMP LOW PRESSURE LIGHT ILLUMINATED ALONG WITH "B" SYSTEM HYDRAULIC FAILURE. REMOVED AND REPLACED NR 2 ENGINE HYDRAULIC PUMP PER MM. 2L72 4F RTA16WE 20060103000252006010300025EA 2006 1 3 COMA0560748 120051223A79316087T04P06 PUMP CNDAIRCL600 CL6002B19 1900309EA LT ENGINE MALFUNCTIONED A COMAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01473CA8957 7668 FLIGHT 5667 - LEFT ENGINE OIL PRESSURE WARNING. REPLACED THE ENGINE LUBE AND SCAVENGE PUMP. 2L72 4F RTA21EA 20060103000262006010300026 2006 1 3 COMA0560749 420051225A3444 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA ACTIVATED A COMAO OTHER J WARNING INDICATION CLCLIMB 1 SO01916CA 7014 FLIGHT 5358- AFTER T/O GPWS MESSAGES SOUNDED. DEFERRED SYSTEM PER MEL. 2L72 4F RTA21EA 20060103000272006010300027EA 2006 1 3 COMA0560750 120051226A291673031 RESERVOIR CNDAIRCL600 CL6002B19 1900309EA NR 3 HYD SYS UNRELIABLE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01416CA13754 7450 FLIGHT 5435 - GEAR DISAGREE WARNING. REPLACED THE SYSTEM NR 3 HYDRAULIC RESERVOIR. 2L72 4F RTA21EA 20060103000292006010300029EA 2006 1 3 COMA0560743 120051221A2170P1096 COALESCER BAG CNDAIRCL600 CL6002B19 1900309EA ACM DIRTY A COMAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SO01967CA 7134 FLIGHT 5709 - SMOKE TOILET CAUTION. REPLACED THE ACM COALESCER BAGS. 2L72 4F RTA21EA 20060103000322006010300032NM 2006 1 3 SWAA054111 120051227A335090083 BATTERY PACK BOEING737 7377H4 1384404NM EMERGENCY LIGHTSINOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29222WN 34290 DURING SCHEDULED MV2 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20060103000332006010300033NM 2006 1 3 SWAA054112 120051226A53306545776 SKIN BOEING737 7373H4 1384600NM BS 930 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STR 22R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20060103000382006010300038NM 2006 1 3 QXEA200501831 120051221A2910M610619022 RELAY BOMBDRDHC8 DHC8402 1390042NM HYD SYSTEM FAILED A QXEAD RETURN TO BLOCK K FLUID LOSS TXTAXI/GRND HDL 1 NM09400QX 4030 RNO FLIGHT NR 2445: AFTER PUSHBACK, NR 3 HYD PUMP CAUTION LIGHT REMAINED ILLUMINATED. MAINTENANCE REMOVED AND REPLACED RL4 RELAY IAW Q400 WDM 24-32-00, PG 101, SHT 1. PERFORMED OPS TEST OF THE NR 3 HYD SYSTEM DCMP PER Q400 AMM 29-12-01. OPS CHECK GOOD. NO OTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20060103000402006010300040NM 2006 1 3 SWAA054118 120051227A53116546526 FRAME BOEING737 7373H4 1384600NM BS 400 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29623SW 27933 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20060103000412006010300041NM 2006 1 3 SWAA054119 120051227A531165C25229 FRAME BOEING737 7373H4 1384600NM BS 727D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29623SW 27933 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20060103000422006010300042NM 2006 1 3 SWAA054120 120051227A53106519603 CREASE BEAM BOEING737 7373H4 1384600NM BS 370 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29623SW 27933 DURING SCHEDULED D CHECK, FOUND FUSELAGE CREASE BEAM WEB CORRODED AT BS 370, RBL 68. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20060103000432006010300043NM 2006 1 3 SWAA054121 120051226A57536546435 SKIN BOEING737 7373H4 1384600NM LH WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29643SW 27716 DURING SCHEDULED SERVICE CHECK, FOUND LT WING OUTBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM. 2L72 4F RTA16WE 20060103000442006010300044NM 2006 1 3 SWAA054122 120051226A57536546434 SKIN BOEING737 7373H4 1384600NM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29643SW 27716 DURING SCHEDULED SERVICE CHECK, FOUND LT WING INBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM. 2L72 4F RTA16WE 20060103000472006010300047NM 2006 1 3 SWAA054125 120051226A3350MS155721 BULB BOEING737 7373Q8 1384670NM EMERGENCY LIGHTSINOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29687SW 23388 DURING SCHEDULED C4 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20051227002212005122700221 2005 12 27 PIDA20050199 420051210A22104038890948 CONTROL PANEL BOEING737 737228 13844AGNM PWA JT8 JT8D15 52051NE COCKPIT INOPERATIVE A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05251TR 23792 FIRST OFFICER'S COURSE WINDOW MIDDLE DIGIT SKIPS PAST THE NR 1 ON THE MODE CONTROL PANEL. REPLACED MODE CONTROL PANEL AND OPS NORMAL IAW MM 22-11-341. 2L72 4F4 FRTA16WE E2EA 20051227002262005122700226NM 2005 12 27 05FDEA04402 120051222A5311 FRAME BOEING727 727100 1384036NM PWA JT8 JT8D7B 52053NE BS 990 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 AFT CARGO COMPARTMENT, FRAME IS DENTED BETWEEN STR. 25 LT AND 27 LT BS 990, ON IB FLANGE. REPAIRED FRAME PER SRM 51-40-3. 2L73 4F4 FRTA3WE E2EA 20051228000052005122800005EU 2005 12 28 ALG2005F00105 120051124A2910GHC1004 POWERPACK UROCOPEC120 EC120B 8680987EU HYD SYSTEM MALFUNCTIONED A ALGAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW03523AL 1262 BEFORE TAKEOFF, HYDRAULIC CAUTION LIGHT ILLUMINATED AND THE PILOT FELT FEEDBACK IN THE CYCLIC FORE AND AFT. REMOVED AND REPLACED HYDRAULIC POWER PACK. (K) 1G72 3U NCR0001RD 20051228000162005122800016SO 2005 12 28 SWIA200516026 120051221A2710 LINKAGE EMB 120 EMB120ER 3260203SO LT AILERONS OBSTRUCTED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07560SW 120334 WHEN CHECKING FLIGHT CONTROLS, YOKE HANGS UP HALF WAY TO THE RIGHT. REPLACED LT AILERON RIVET TO QUADRANT LINKAGE IAW MM 31-30-11. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20051228000202005122800020EA 2005 12 28 SWIA200516004 120051214A2750865D1007 PDU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 NM07918SW6524 6524 7645 ON APPROACH "FLAPS HALFSPEED" STATUS MESSAGE CAME ON. REPLACED FLAP PDU PER CRJ MM 27-51-00. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051228000412005122800041CE 2005 12 28 TIM2005F00011 120051108A3297G18A22N GROUND WIRE BEECH 99 99 1154002CE PWA PT6 PT6A27 52043EA MLG CONTROL CORRODED E TIMAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM0724BH U67 LANDING GEAR FAILED TO EXTEND. INSPECTION FOUND A CORRODED GROUND WIRE. THE FAILURE WAS INTERMITTENT THIS CAUSED CONSIDERABLE TROUBLE IN THE TROUBLESHOOTING AND SEVERAL HOURS OF TIME TO REPAIR THE PROBLEM. (K) 1L72 3T4 T A14CE E4EA 20051228000442005122800044CE 2005 12 28 E812005F00001 120051116A3210508102503 BRACE BEECH BEECH 90 C90A 1152911CE PWA PT6 PT6* 52043EA MLG STRUT CORRODED B E81RO OTHER O OTHER NRNOT REPORTED 1 GL03439PW1160 LJ1588 LJ1589 DURING INITIAL 6 YEAR/8000 CYCLE INSPECTION OF MAIN GEAR ASSY, FOUND INTERNAL SURFACE OF UPPER BRACE PITTED AND CORRODED AT AREA IN CONTACT WITH UPPER MAIN GEAR STRUT. CORROSION APPEARS UNUSUAL FOR A CLEAN, NEWER, LOW-TIME AIRCRAFT THAT IS HANGARED IS A NON SALT-AIR TYPE ENVIRONMENT. UPPER BRACE ASSY SHOULD BE ASSEMBLED TO STRUT CYCLINDER. CORROSION PREVENTION COMPOUND AT ASSEMBLY IAW THE COMPONENT MM. SUSPECT CORROSION PREVENTION COMPOUND NOT ADEQUATELY APPLIED AT INITIAL ASSEMBLY. (K) 1L72 3T3 TRT3A20 E2NE 20051228000452005122800045SW 2005 12 28 ALG2005F00113 120051115A5620 WINDOW BELL 407 407 1182206SW ALLSN 250C 250C47B GL PAX CABIN SEPARATED E ALGAO OTHER D INFLIGHT SEPARATION APAPPROACH 1 SW03537AL 53230 ON APPROACH TO LANDING, RT PASSENGER SLIDING WINDOW SEPARATED FROM THE AIRCRAFT. SECOND OCCURRENCE WITH SAME AC WITHIN A WEEK. REPLACED DOOR WITH SERVICEABLE DOOR AND WINDOW. (K) 1G71 3U3 UO H2SW E1GL 20051228000472005122800047SW 2005 12 28 ALG2005F00109 120051120A243523081018 STARTER GEN BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL FAILED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03187AL 51135 DURING FLIGHT, AIRCRAFT GENERATOR FAILED. REPLACED STARTER/GENERATOR. (K) 1G71 3U3 U H2SW E1GL 20051228000532005122800053SW 2005 12 28 ALG2005F00101 120051128A2435 STARTER GEN BELL 206 206L4 1182110SW ALLSN 250C 250C30P 03013GL FAILED A ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03271AL 52287 STARTER/GENERATOR FAILED ENROUTE TO WC 586. RETURNED TO BASE. REMOVED AND REPLACED STARTER/GENERATOR. (K) 1G71 3U3 UNCH2SW E1GL 20051228000632005122800063CE 2005 12 28 LGD2005F00000 120051117A321007410017 LANDING GEAR CESSNA185 A185E 2072818CE LYC O540 IO540K1G5 41532EA HARTZLHCC2Y HCC2YK1 GL LEFT COLLAPSED E LGDAO OTHER O OTHER TXTAXI/GRND HDL 1 AL03771X 9900 1851336 L2026548A CH37015B GEAR BROKE ON LANDING ROLLOUT EST. 700 HOURS ON 3600 FLUIDINE SKIS, EST 7,000 HRS ON WHEEL ADAPTERS WITH 8:50 X 10 TIRES. RECOMMEND INSPECTIONS OR LIFE LIMITED PART, BROKE OFF AT TOP BOLT HOLES. (K) 1H71 3O3 O 3A24 1E4 5 CP920 20051228000702005122800070GL 2005 12 28 ALG2005F00107 220051124A753223073353 BLEED VALVE CESSNASTC STC206C 1182107CE ALLSN 250C 250C30P 03013GL ENGINE FAILED E ALGAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SW032618 45503 ON TAKEOFF, ENGINE COMPRESSOR STALLED AT 80 PERCENT. LANDED AIRCRAFT AND NOTIFIED MAINTENANCE. PERFORMED MM, NO DEFECTS NOTED. REMOVED AND REPLACED BLEEDVALVE. (K) 1H71 3O3 UNTA4CE E1GL 20051228000712005122800071GL 2005 12 28 ALG2005F00118 120051113A6340 INDICATOR CIRRUSSR SR22 2130001GL ALLSN 250C 250C47B GL XMSN OIL PRESS MALFUNCTIONED E ALGAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW03579AL 1057 IN FLIGHT TRANSMISSION PRESSURE DROPPED TO ZERO, RETURNED TO NORMAL AND BACK TO ZERO IN A 15 MINUTE FLIGHT. INSPECTION BY MAINT REVEALED THE NR 8 TAIL ROTOR DRIVE SHAFT HAD FAILED. A WO WAS OPENED FOR REPAIR OF THIS AIRCRAFT. REMOVED AND REPLACED TRANSMISSION OIL GAUGE. (K) 1L71 3O3 UNTA00009CHE1GL 20051228001092005122800109NE 2005 12 28 ALG2005F00094 120051204A6700L109BBM ACTUATOR SKRSKYS76 S76C 8143008NE CYCLIC INOPERATIVE E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03862AL 760531 ON TAKEOFF AND LANDING CYCLIC CONTROL MOVEMENT FEELS LIMITED IN FORE AND AFT TRAVEL. UPON LANDING THE MECHANIC REMOVED PITCH ACTUATOR ARTIFICIAL FEEL SN 10006, AND INSTALLED SERVICEABLE PITCH ACTUATOR SN 71054 AND HE COMPLIED WITH CONTINUITY CHECK OF CONTROLS. THE AC C/W GROUND RUN AND OPS CHECK IAW MM AND NO DEFECTS WERE NOTED. (K) 1G72 3U NCH1NE 20051228001222005122800122EU 2005 12 28 KBM2005F00335 120051118A6410355A09103601 BEARING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE TAIL ROTOR CRACKED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19115SH1436 3141 HALF SHELLS, UNIT CRACKED AND WORN. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051228001242005122800124EU 2005 12 28 KBM2005F00347 120051130A2913POLYV597K4 BELT SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE HYD PUMP CRACKED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19250SH1067 250SH BELT HAS MULTIPLE CRACKS, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051228001262005122800126EU 2005 12 28 KBM2005F00346 120051130A641035509103601 BEARING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE TAIL ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19250SH1067 3874 UNITS WORN BEYOND LIMITS. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20051228001302005122800130NE 2005 12 28 M7K2005F00002 220051208A7261350A54113800 VENT LINE UROCOPEC130 EC130B4 8680989EU TMECA ARRIELARRIEL2B NE ENGINE OIL CRACKED E M7KAO OTHER O OTHER NRNOT REPORTED 1 WP19812MH83 3956 ENGINE OIL VENT TUBE, AIRFRAME PART, MOUNTED ON ENG WITH VENTING ORIFICE PLACED IN EXHAUST PATH HAS ANTI-ROTATION CLAMP WELDED TO STAINLESS TUBE BODY, CRACKS INITIATE IN SPOT WELDS CAUSING CLAMP FLANGE TO CRACK. REPAIR, DRESSING OFF FLANGE REMNANTS, INSTALLING A HIGH TEMP FITTED CLAMP HAS BEEN RECOMMENDED BY AC MFG ENGINEERING DEPART. TUBES NOW HAVE CRACKS DEVELOPING AROUND TUBE CIRCUM EMANATING FROM CLAMP SPOT WELDS. THESE TUBES HAVE BEEN REMOVED AND REPLACED. UNDISCOVERED CRACK AT TUBE SECTION COULD LEAD TO 10 IN LONG, .6250 IN DIA PIECE OF TUBE DEPARTING THE AC, POSSIBLY STRIKING MAIN ROTOR BLADES OR TAIL ROTOR BLADES. RECOMMEND NEW TUBES W/O WELDED CLAMPS, THAT ARE HELD WITH HIGH TEMP CLAMPS. 1G72 3U3 U H9EU E00054EN 20051228001322005122800132NM 2005 12 28 CALA0500454 120051227A25301676 OVEN BOEING737 7373T0 1384582NM FWD GALLEY NONE A CALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2776354 23592 CREW OBSERVED SMOKE ENTERING COCKPIT WHILE IN CRUISE. 1ST CLASS OVENS WERE IN USE. FLT ATTENDANT TURNED OFF 1ST CLASS OVENS & SMOKE CEASED. FLT CONTINUED & LANDED WITHOUT FURTHER PROBLEM. VISUAL INSPECTION PERFORMED BEHIND OVENS, COFFEEMAKER, & P-6 PANELS, NO DEFECTS NOTED. BOTH 1ST CLASS OVENS R & R AS A PRECAUTION IAW MM 25-34-34. OPS CHKS GOOD, NO SMOKE NOTED. PREVIOUS FLT EXPERIENCED SMOKE IN COCKPIT/CABIN & SOURCE DETERMINED TO BE A BURNED LOAF OF BREAD WRAPPED IN A PLASTIC BAG INSIDE FWD GALLEY OVEN. TEARDOWN REPORTS FOUND NO FAULT WITH ONE OVEN. SMOKE A RESULT OF BURNING RESIDUE IN OVERHEATED OVEN. 2L72 4F RTA16WE 20051228001342005122800134 2005 12 28 SWAA054076 420051223A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 R1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20051228001362005122800136NM 2005 12 28 SWAA054078 120051222A53306545774 SKIN BOEING737 7373H4 1384600NM BS 737 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 737, STR 18R. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20051228001382005122800138NM 2005 12 28 SWAA054080 120051222A5511 SPAR BOEING737 7373H4 1384600NM HORIZONTAL STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 DURING SCHEDULED C4 CHECK, FOUND RT HORIZONTAL STAB AFT SPAR CRACKED 5 INCHES FROM ROOT. REPAIRED HORIZONTAL STAB PER SRM. 2L72 4F RTA16WE 20051228001402005122800140 2005 12 28 SWAA054082 420051221A25656949956 CABLE BOEING737 7373H4 1384600NM R2 DOOR SLIDE MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29344SW 24152 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE LATCH CABLE ASSY MISROUTED. REROUTED CABLE ASSY PER MM. 2L72 4F RTA16WE 20051228001422005122800142NM 2005 12 28 SWAA054084 120051221A57536546435 SKIN BOEING737 7373H4 1384600NM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29363SW 26574 DURING SCHEDULED C1 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM. 2L72 4F RTA16WE 20051228001442005122800144NM 2005 12 28 SWAA054086 120051225A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29407WN 29817 EEPLS TRACK LOOSE AT FWD END. SECURED EEPLS PER MM. 2L72 4F RTA16WE 20051228001462005122800146NM 2005 12 28 SWAA054088 120051222A2120 ODOR BOEING737 7377H4 1384404NM CABIN DETECTED A SWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW29408WN 27895 DURING FERRY FLIGHT TO PHX, STRONG FUMES IN COCKPIT CAUSING EYE IRRITATION, O2 MASKS USED IN COCKPIT. REMOVED AND REPLACED HEPA FILTER, MUFFLER, LT & RT COALESCER BAGS & BOTH HYDRAULIC RESERVIOR PRESSURE RESTRICTOR CHECK VALVES PER MM. 2L72 4F RTA16WE 20051228001482005122800148NM 2005 12 28 SWAA054090 120051221A335065C34691 LIGHT BOEING737 7377H4 1384404NM ROW 8 INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29415WN 29836 DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY BULLNOSE LIGHT INOP AT ROW 8. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20051228001502005122800150NM 2005 12 28 SWAA054092 120051225A53306545768 SKIN BOEING737 7375H4 138449DNM BS 312 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29506SW 24183 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 312, STR 18R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20051228001512005122800151NM 2005 12 28 SWAA054093 120051222A53116517684 FRAME BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29511SW 24188 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT L1 DOOR CUTOUT, LOWER FWD CORNER. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051228001532005122800153NM 2005 12 28 SWAA054095 120051222A53106519603 CREASE BEAM BOEING737 7373H4 1384600NM BS 370-410 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29622SW 27932 DURING SCHEDULED D-CHECK, FOUND FUSELAGE CREASE BEAM WEB CORRODED BETWEEN BS 370 TO BS 410, RBL 70. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20051228001552005122800155NM 2005 12 28 SWAA054097 120051223A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 294 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29623SW 27933 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 294, STR 13L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20051228001572005122800157NM 2005 12 28 SWAA054099 120051223A53116546555 FRAME BOEING737 7373H4 1384600NM BS 867 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29623SW 27933 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051228001592005122800159NM 2005 12 28 SWAA054101 120051223A53116546525 FRAME BOEING737 7373H4 1384600NM BS 380 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29623SW 27933 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051228001612005122800161NM 2005 12 28 SWAA054103 120051223A53106546959 CREASE BEAM BOEING737 7373H4 1384600NM BS 500-500A CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29623SW 27933 DURING SCHEDULED D-CHECK, FOUND FUSELAGE CREASE BEAM WEB CORRODED BETWEEN BS 500 TO BS 500A, LBL 69. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20051228001632005122800163NM 2005 12 28 SWAA054105 120051223A53116546550 FRAME BOEING737 7373H4 1384600NM BS 787 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29623SW 27933 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051228001652005122800165NM 2005 12 28 SWAA054107 120051223A53116546555 FRAME BOEING737 7373H4 1384600NM BS 867 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29623SW 27933 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20051228001672005122800167 2005 12 28 SWAA054109 420051225A2565D31354 SLIDE BOEING737 7373G7 1384595NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29683SW 24008 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20051228001772005122800177NM 2005 12 28 AWXA200501588 120051116A5320654797322 WEB BOEING737 7373S3 1384711NM BS 616-639 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 MCN - DURING C20 CHECK DISCOVERED SHEAR WEB CRACKED, 2.5 INCHES, BETWEEN BS 616 AND BS 639, BL 65R AND WL 208. MAINTENANCE REMOVED AND INSTALLED NEW SHEAR WEB BETWEEN BS 616 AND BS 639, BL 65R AND WL 208 IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 8 AND 12. 2L72 4F RTA16WE 20051228001792005122800179NM 2005 12 28 AWXA200501590 120051113A57536546431280 SKIN BOEING737 7373S3 1384711NM ZONE 600 - RIGHTDELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 MCN - DURING C20 CHECK DISCOVERED SEVERAL AREAS OF DELAMINATIONS ON THE RT WING OUTBOARD FORE FLAP FROM WBL 202.69R TO WBL 281.0R. MAINTENANCE REMOVED AND REPLACED THE RT WING OUTBOARD FORE FLAP. 2L72 4F RTA16WE 20051228001812005122800181NM 2005 12 28 AWXA200501592 120051113A57536546486129 SKIN BOEING737 7373S3 1384711NM ZONE 500 - LEFT DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 MCN - DURING C20 CHECK DISCOVERED DISBOND AREA ON THE OUTBOARD END OF THE LT INBOARD MID-FLAP WEDGE PANEL, UPPER SURFACE. MAINTENANCE REMOVED DISBONDED SKIN IAW BOEING 737-300 SRM 51-70-10-2R4 FIG 201. FABRICATED DOUBLER AND FILLER IAW BOEING 737-300 SRM 51-70-10-2R4 FIG 201. BONDED REPAIR PARTS TO THE UPPER SURFACE OF THE INBOARD MIDFLAP WEDGE PANEL IAW BOEING 737-300 SRM 51-70-10-2R4 FIG 201. 2L72 4F RTA16WE 20051228001832005122800183NM 2005 12 28 AWXA200501594 120051120A5320654795711 STRAP BOEING737 7373S3 1384711NM BS 839-851 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 MCN - DURING C20 CHECK DISCOVERED CORROSION ON THE AFT CARGO LOWER SILL STRAP FROM BS 839 TO BS 851, WL 158 AND BL 19R. NO CORROSION REMOVAL LIMITS WERE AVAILABLE IN THE BOEING 737-300 SRM. MAINTENANCE REMOVED AND INSTALLED NEW AFT CARGO DOOR LOWER SILL STRAP FROM BS 839 TO BS 851, WL 158 AND BL 19R IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 3, 4, 6, 7 AND 8. 2L72 4F RTA16WE 20051228001852005122800185EA 2005 12 28 SWIA200516010 120051216A335020131A BATTERY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07405SW 7029 SERVICE DOOR FLOOR EXIT SIGN, MAIN CABIN DOOR FLOOR EXIT SIGN NOT ILLUMINATING. FIRST SECTION OF FLOOR EMERGENCY LIGHTS NOT ILLUMINATED. REPLACED EMERGENCY BATTERY PACK, INDICATORS, AND A WIRE SEGMENT. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051228001892005122800189EA 2005 12 28 SWIA200516014 120051214A2741 SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07418SW 7446 STAB TRIM MACH TRIM DISENGAGED REPEATEDLY ON TAXI OUT RETURNED TO GATE. REPLACED CAPT TRIM DISCONNECT SWITCH IAW CL 600 MM 27-41-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051228001922005122800192EA 2005 12 28 SWIA200516028 120051223A5610 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT FAILED A SWIAO OTHER O OTHER CRCRUISE 1 NM07909SW 7558 RIGHT DV WINDOW SHATTERED INFLIGHT. REPLACED FO SIDE WINDOW IAW CRJ MM 56-12-01. OPERATIONAL CHECK GOOD, PN/OFF NP139322-6, SN/OFF 011-45H8597. 2L72 4F RTA21EA 20051228001942005122800194EA 2005 12 28 SWIA200516030 120051223A274170609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07963SW1030 1030 7865 CAPT'S TRIM SWITCH KICKS OFF MACH TRIM. REPLACED THE HSTCU IAW 27-41-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051228002002005122800200EA 2005 12 28 SWIA200516036 120051221A2760C13045BA04 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07765SK 10231 PITCH FEEL FAULT STATUS MESSAGE WOULD NOT CLEAR AFTER POWER UP. REPLACED SSCU 1 IAW CRJ MM 20-61-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051230000022005123000002NM 2005 12 30 SB05175 120051223A27512061141 INDICATOR BOEING737 737401 1384701NM COCKPIT FAULTY A USAAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 EA19409US3628525 23879 BOS FLT 312 EN-ROUTE, FLL TO BOS. WHILE THE FLIGHT WAS DESCENDING, AND GOING FROM FLAPS 10 TO FLAPS 15, THERE WAS A FLAP DISAGREEMENT. THE FLAPS INDICATED SPLIT BETWEEN 10 AND 15 DEGREES, BUT WITH NO ASSOCIATED ROLL. THE FLIGHT DID A GO-AROUND WHILE RETRACTING THE FLAPS TO 10 DEGREES PER THE CHECKLIST. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE TRAILING EDGE FLAP INDICATOR. OPERATIONALLY CHECKS OK. 2L72 4F RTA16WE 20051230000032005123000003NM 2005 12 30 SB05176 120051225A335020121 CHARGER BOEING737 737301 1384611NM EMERGENCY LIGHT FAULTY A USAAK NONE O OTHER ININSP/MAINT 1 EA19355US 23558 TPA - THE SEAT MOUNTED EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE AFT LEFT BATTERY CHARGER ASSEMBLY. EMERGENCY LIGHTS CHECK OK. 2L72 4F RTA16WE 20051230000052005123000005NE 2005 12 30 BB05107 220051225A7200 ENGINE BOEING767 7672B7 1385107NM GE CF6 CF680 30025NE LEFT BIRD INGESTION A USAAA UNSCHED LANDING C F.O.D. CLCLIMB 1 EA19652US 24765 690194 LGW FLT 15, EN ROUTE MUC TO PHL - A BIRD STRUCK THE LEFT ENGINE AT ROTATION DURING TAKEOFF. THE CREW INITIALLY HEARD AN ABNORMAL SOUND. ALL ENGINE PARAMETERS RETURNED TO NORMAL AFTER AN INITIAL DROP IN ENGINE READINGS. THE CREW DECIDED TO DIVERT TO LGW TO HAVE THE LEFT ENGINE INSPECTED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACTION PENDING. 2L72 4F4 FRTA1NM E13NE 20051230000152005123000015NM 2005 12 30 SB05177 120051228A335020131A BATTERY PACK BOEING737 7373B7 1384580NM EMERGENCY LIGHT DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU 23702 PIT - THE EMERGENCY LIGHTS WERE OUT IN THE FIRST CLASS SECTION AND FORWARD GALLEY. MAINTENANCE REPLACED THE BATTERY CELL ASSEMBLY IN THE FORWARD GALLEY. OPERATIONALLY CHECKS OK. 2L72 4F RTA16WE 20051230000272005123000027NM 2005 12 30 2005UALA01489 120051220A5311 FRAME BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU BS 907 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29923UA 26643 FWD LT CABIN STA 907 FRAME WEB BETWEEN STRINGERS 8R & 9R CRACK AT AIR CONDITIONING DUCT ATTACH BRACKET. MAJOR REPAIR. REMOVED DAMAGE. FABRICATED AND INSTALLED NESTED ANGLE REPAIR. PER SRM 53-10-84 REPAIR NR 3. 2L72 4F4 FRTA16WE E21EU 20051230000312005123000031NM 2005 12 30 2005UALA01493 120051220A5322 SHEAR TIE BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU BS 360 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29923UA 26643 RT FWD CABIN STA 360 BETWEEN STRINGERS 14R & 15R SHEAR TIE CRACKED COMPLETELY THROUGH RADIUS. MAJOR REPAIR. REMOVED AND REPLACED SHEAR TIE. REF SRM 57-40-02. 2L72 4F4 FRTA16WE E21EU 20051230000322005123000032NM 2005 12 30 2005UALA01494 120051220A5414 SKIN BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE NR 1 PYLON CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29644UA 25094 NR 1 PYLON INBOARD FWD STRUT SKIN CRACKED AT PANEL 416BR CUTOUT RADIUS. IT WAS PROBABLY CAUSED BY FATIGUE. THE SKIN WAS REPAIRED PER SRM 54-53-01 WITH -1 AND -2 DOUBLERS. 2L72 4F4 FRTA1NM E24NE 20051230000392005123000039NM 2005 12 30 2005UALA01501 120051222A2797 WIRE BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE SLATS BROKEN A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29665UA 29237 DIVERTED DUE TO LEADING EDGE SLAT ASYMMETRY EICAS. FOUND SLAT SKEW SWITCH WIRING FAILED AT RT WING TIP, STA 1107. CAUSE OF WIRING FAILURE WAS BROKEN 90 DEG CONDUIT ELBOW. 2L72 4F4 FRTA1NM E24NE 20051230000402005123000040EA 2005 12 30 VNAA0512006 120051203A5300 STRUCTURE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE NOSE BIRD STRIKE A VNAAO OTHER O OTHER LDLANDING 1 GL05247JS 7922 THE CREW REPORTED A BIRD STRIKE DURING LANDING APPROACH. MAINTENANCE COMPLIED WITH A BIRD STRIKE INSPECTION AND FOUND A DENT ON THE RT FUSELAGE NOSE SECTION BELOW THE ADG DOOR, THE ADG DOOR WAS CRACKED, AND THE LT WING LEADING EDGE PANEL 530BL WAS DENTED. ALL DAMAGE WAS REPAIRED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20051230000442005123000044EA 2005 12 30 VNAA0512008 120051207A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS ILLUMINATED A VNAAO OTHER O OTHER APAPPROACH 1 GL05209PS 7874 DURING APPROACH WHEN FLAPS WERE SELECTED FROM 20 TO 30 DEGREES THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED. THE CREW FOLLOWED THE QRH AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET AND OPERATIONALLY CHECKED THE FLAP SYSTEM. ALL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20051230000472005123000047EA 2005 12 30 VNAA0512007 120051205A2730DL2428M4 ACTUATOR CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE RT PITCH FEEL FAILED A VNAAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 GL05708PS3438 10160 DURING CLIMB THE PITCH FEEL CAUTION LIGHT ILLUMINATED. THE CREW FOLLOWED THE QRH AND RETURNED TO CLT. MAINTENANCE REMOVED AND REPLACED THE RT PITCH FEEL LINEAR ACTUATOR. THE SYSTEM OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20051230000592005123000059SO 2005 12 30 RAIA00512028 120051226A3350 LIGHT EMB 145 EMB145EP 3260221SO CABIN INOPERATIVE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03826HK 145016 5488 - STL - EMERGENCY ESCAPED PATH LIGHTS SECTION OUT. MAINTENANCE CYCLED AIRCRAFT POWER AND OPS CHK. NO DEFECT FOUND. 2L72 4F RTT00011AT 20051230000662005123000066NM 2005 12 30 QXEA200501835 120051226A2120 HAZE DHAV DHC8 DHC8202 2809007NM CABIN UNKNOWN A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM09345PH 476 PDX FLIGHT 2272, SMOKE HAZE NOTED IN CABIN ON GROUND. MAINTENANCE GROUND RAN AIRCRAFT. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051230000722005123000072NM 2005 12 30 QXEA200501821 120051206A5347 SEAT TRACK BOMBDRDHC8 DHC8402 1390042NM BS 612 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09403QX 4037 PDX: RT OUTBOARD SEAT TRACK NR 19 HAS PITTING CORROSION AT APPROX FS X612. MAINTENANCE REPAIRED IAW NDTM PART 6, 51-00-02 AND RD 8/4-53-884. 2H72 4T RTA13NM 20051230000742005123000074NM 2005 12 30 AWXA200501597 120051116A532065479599 INTERCOSTAL BOEING737 7373S3 1384711NM BS 787-794 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 MCN - DURING C20 CHECK DISCOVERED CORROSION ON THE AFT CARGO FLOOR INTERCOSTAL OUTBOARD SIDE FROM BS 787 TO BS 794, FROM WL 152 TO WL 158 AND BL 20.5R. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-15-0I 1 FIG 101. MAINTENANCE REMOVED AND INSTALLED NEW AFT CARGO FLOOR INTERCOSTAL FROM BS 787 TO BS 794, FROM WL 152 TO WL 158 AND BL 20.5R IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 3, 4, 6, 7 AND 8. 2L72 4F RTA16WE 20051230000792005123000079NM 2005 12 30 AWXA200501602 120051116A5320651630087 FRAME BOEING737 7373S3 1384711NM BS 178 BULKHEAD CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 MCN - DURING C29 CHECK DISCOVERED THAT THE 178 BULKHEAD SIDE CHORD WAS CRACKED, 2.0 INCHES, AT BL 31R AND WL 206. MAINTENANCE REMOVED AND INSTALLED NEW CHORD AT BL 31R AND WL 206 IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 2, 8 AND 12. 2L72 4F RTA16WE 20051230000802005123000080NM 2005 12 30 AWXA200501603 120051112A5320652981818 BRACKET BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 MCN - DURING C20 CHECK DISCOVERED TOP OF BRACKET CRACKED AT BS 323, BL 57L AND WL 207, BETWEEN THE AIRSTAIR CUTOUT UPPER FRAME AND THE L-1 SILL. MAINTENANCE REMOVED AND INSTALLED NEW BRACKET AT BS 323, BL 57L AND WL 207, BETWEEN THE AIRSTAIR CUTOUT UPPER FRAME AND THE L-1 SILL IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 8 AND 12. 2L72 4F RTA16WE 20051230000852005123000085NM 2005 12 30 QXEA200501843 120051225A30104100S00502 VALVE BOMBDRDHC8 DHC8402 1390042NM DEICE SYSTEM MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION DEDESCENT 1 NM09406QX4631 4048 SEA FLIGHT NR 2317, DEICE PRESSURE CAUTION LIGHT CAME ON DURING DESCENT (POWER APPROX 35-40% TRQ). THE LEFT OUTBOARD ADVISORY CAME ON FOR ONLY AN INSTANT, THEN WENT DARK. LEFT DEICE PRESSURE INDICATED NORMAL ON FO'S PRESSURE GAUGE. VISUALLY CONFIRMED BOOT INFLATED OK. RAN DEICE PRESSURE CHECKLIST. PROBLEM NOT SOLVED, (GOT CAUTION LIGHT AGAIN). MAINTENANCE REMOVED LT OUTBOARD DDV IAW Q400 AMM TASK 30-11-16-000-801. INSTALLED NEW DDV IAW Q400 AMM TASK 30-11-16-400-801. REMOVED LEADING EDGE 513AL TO FOM. INSTALLED LEADING EDGE 513AL IAW Q400 AMM TASK 57-23-01-400-801. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051230000892005123000089 2005 12 30 QXEA200501839 420051221A2210 ACTUATOR BOMBDRDHC8 DHC8402 1390042NM YAW DAMPER MALFUNCTIONED A QXEAD RETURN TO BLOCK J WARNING INDICATION UKUNKNOWN 1 NM09417QX4383 292 4086 SEA FLIGHT NR 2340, YAW DAMPER HOT CENTERED MESSAGE APPEARED ON PFD. ATTEMPTED YAW DAMPER RESET BUT IT WOULD NOT RESET. MAINTENANCE REMOVED YAW DAMPER ACTUATOR IAW Q400 AMM TASK 22-11-36-000-801. INSTALLED NEW YAW DAMPER ACTUATOR IAW Q400 AMM TASK 21-11-36-400-801. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051230000982005123000098EA 2005 12 30 COMA0560741 120051220A32304622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG UNRELIABLE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01710CA2349513375 7241 FLIGHT 5274 - GEAR DISAGREE WARNING. REPLACED THE NLG PRIORITY VALVE. 2L72 4F RTA21EA 20060103000062006010300006EU 2006 1 3 05FDEA04424 120051230A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU BS 29.5-30.5 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25672FE 779 MCD FLOOR TRACK CORRODED AT LBL 77 3" AFT OF FS 30. REMOVED AND REPLACED DAMAGED SEAT TRACK SECTION FROM FS 29.5 TO FS 30.5 LBL 77 IAW A300-600 SRM 53-10-16 AND EA NR 6-5310-92607. 2L72 4F RTA35EU 20060103000102006010300010EU 2006 1 3 05FDEA04249 120051212A5330 SKIN AIRBUS310 A310222 3930315EU FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25450FE 162 DEEP DENT AND PUNCTURE TOP OF CROWN SKIN ON BUTT SEAM FS 10 TO 3'" AFT DENT APPROX 14 " LONG AND 10 " WIDE PUNCTURE APPROX 2.60 " LONG DAMAGE AT CROWN C/L (HURRICANE RITA NR 4) REF N00054. REPAIRED AREA IAW EA 6-5330-94744. 2L72 4F RTA35EU 20060103000312006010300031EA 2006 1 3 COMA0560745 120051222A32304622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG FAULTY A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01710CA19127 7241 FLIGHT 9644 - DURING FERRY FLIGHT 9644 CLE-MCO, RECEIVED A GEAR DISAGREE MESSAGE. FLIGHT DIVERTED TO CAK. REPLACED THE NLG PRIORITY VALVE. 2L72 4F RTA21EA 20060103000512006010300051CE 2006 1 3 DXTA200501143 120051215A3297 SPLICE CESSNA500 560CESSNA 2076750CE MLG INDICATOR DISCONNECTED E DXTAO OTHER J WARNING INDICATION APAPPROACH 1 GL07396QS 5600396 UPON GEAR EXTENSION, RIGHT MAIN GEAR LIGHT WOULD NOT ILLUMINATE. BULB CHECKED GOOD ON ROTARY TEST. FOUND DME SPLICE DISCONNECTED IN ACTUATOR HARNESS RECONNECTED AND OPS CHECK GOOD IAW CE560 MM 32-31-04. 2L72 4F RTA22CE 20060103000542006010300054CE 2006 1 3 DXTA200501150 120051217A3240 LINE CESSNA500 560CESSNA 2076750CE BRAKES UNKNOWN E DXTAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07311QS 5600311 R-SIDE R-BRAKE PEDAL GOES FLAT TO THE FLOOR. BLED BRAKES IAW CE560 MM CHP 32-42-00, OPS AND LEAK CHECKED GOOD. 2L72 4F RTA22CE 20060103000572006010300057EA 2006 1 3 ASOA051062 120051205A5210601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27882AS 7503 DURING A C-CHECK IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACE THE PASSENGER DOOR BOTTOM STEP. (M) 2L72 4F RTA21EA 20060103000582006010300058EA 2006 1 3 ASOA051078 120051209A52101170715 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR OUT OF ALIGNMENTA ASOAK NONE O OTHER ININSP/MAINT 1 SO27825AS 7207 DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WOULD NOT OPEN FROM THE OUTSIDE AND THE HANDLE WOULD NOT PROPERLY ALIGN UPON CLOSING. MAINTENANCE ADJUSTED THE PASSENGER DOOR INNER HANDLE STOP AND THE DETENT ON THE PASSENGER DOOR RELEASE HANDLE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060103000592006010300059EA 2006 1 3 ASOA051073 120051207A5220H341931 HANDLE CNDAIRCL600 CL6002C10 1390015EA ESCAPE HATCH CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27716EV 10084 DURING A HANGAR INSPECTION IN MCN, THE CREW ESCAPE HATCH OUTER HANDLE WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CREW ESCAPE HATCH OUTER HANDLE. (M) 2L72 4F RTA21EA 20060103000632006010300063EA 2006 1 3 ASOA051077 120051209A33506100928 LAMP CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHTSBURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27701EV 10020 DURING A HANGAR INSPECTION IN BTR, BOTH CABIN LOWER EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMPS IN BOTH CABIN LOWER EMERGENCY EXIT LIGHT ASSEMBLIES. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060103000652006010300065NM 2006 1 3 QXEA200501836 120051217A52308MK4538001 HANDLE BOMBDRDHC8 DHC8402 1390042NM CARGO DOOR UNSECURE A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09402QX 4032 SEA FLIGHT NR 2332: AFTER TAKEOFF, FUSELAGE DOOR WARNING ILLUMINATED INDICATING AFT BAGGAGE DOOR UNSECURE. UNABLE TO PRESSURIZE, RETURNED TO LAND AT SEA. AIRCRAFT WAS FERRIED TO PDX. MAINTENANCE REMOVED AND REPLACED AFT BAGGAGE DOOR ASSY IAW Q400 AMM TASK 52-31-01-000-802 AND 52-31-01-400-801. OPS TEST GOOD. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20060103000662006010300066EA 2006 1 3 VNAA0512012 120051215A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE LIGHTNING STRIKEA VNAAO OTHER O OTHER CRCRUISE 1 GL05254PS 7935 THE CREW REPORTED A POSSIBLE LIGHTNING STRIKE IN CRUISE AT 15000 FT WITH GEAR AND FLAPS UP. MAINTENANCE PERFORMED EN ROUTE AND DETAILED LIGHTNING STRIKE INSPECTIONS. DAMAGE WAS FOUND ON THE LT HORIZONTAL STABILIZER AND THE LOWER AFT FUSELAGE. ALL DAMAGE WAS REPAIRED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20060103000672006010300067EA 2006 1 3 VNAA0512016 120051220A3411 PITOT SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 2 ADC CONTAMINATED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL05229PS 7898 THE TAKEOFF WAS ABORTED WHEN THE CREW RECEIVED AN IAS MISCOMPARE WARNING. MAINTENANCE INSPECTED THE PITOT STATIC SYSTEMS FOR CONTAMINATION AND FOUND WATER IN THE NR 2 ADC PITOT DRAIN COLLECTOR TUBE. THE P2 LINE WAS PURGED. THE PITOT SYSTEM TESTED & LEAK CHECKED GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20060103000682006010300068EA 2006 1 3 VNAA0512014 120051218A2700 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS UNKNOWN A VNAAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL05250PS 7929 THE FLAPS FAIL MESSAGE ILLUMINATED WHEN FLAPS WERE AT 25 SELECTED TO 30 DEGREES. THE CREW FOLLOWED THE QRH AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET & TESTED THE FLAP SYSTEM IAW BOMBARDIER CRJ200 SL 00-001. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20060103000702006010300070EA 2006 1 3 VNAA0512015 120051218A5246 DOOR CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE REFUELING OPEN A VNAAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 GL05716PS 10171 THE CREW REPORTED A LOUD SQUEALING NOISE FROM THE MAIN LANDING GEAR AREA OF THE FUSELAGE. THE FLIGHT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE REFUEL DOOR OPEN. INSPECTION REVEALED NO DAMAGE. THE DOOR WAS PROPERLY SECURED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20060103000722006010300072EA 2006 1 3 VNAA0512017 120051223A5710 STRUCTURE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT WING LE BIRD STRIKE A VNAAO OTHER O OTHER CLCLIMB 1 GL05262PS 7962 DURING CLIMBOUT FROM BDL THE CREW REPORTED A POSSIBLE BIRD STRIKE. THE FLIGHT CONTINUED TO PIT AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED IMPACT DAMAGE ON THE RT WING INBOARD LEADING EDGE. MAINTENANCE REMOVED AND REPLACED THE RT WING INBOARD LEADING EDGE AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20060103000732006010300073EA 2006 1 3 VNAA0512019 120051223A5270 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR CONTAMINATED A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL05259PS 7945 DURING CLIMBOUT THE FLIGHT ATTENDANT REPORTED A LOUD SQUEAL FROM THE MAIN CABIN DOOR AND THE PASSENGER DOOR WARNING MESSAGE ILLUMINATED INTERMITTENTLY. THE CREW FOLLOWED THE QRH, RETURNED TO FAY, AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED A GOB OF CHEWING GUM FROM THE DOOR SEAL AND PROXI-SENSOR AREA. THE PRESSURIZATION AND DOOR INDICATION SYSTEMS OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20060103000742006010300074EA 2006 1 3 VNAA0512018 120051223A4990MS280343 SENSOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE APU FAILED A VNAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL05216PS 7882 DURING CRUISE THE APU OIL TEMP CAUTION MESSSAGE ILLUMINATED. THE CREW FOLLOWED THE QRH AND, DUE TO A RT IDG MEL AND WEATHER AT BNA, DIVERTED TO TYS. MAINTENANCE REMOVED & REPLACED THE APU HIGH OIL TEMPERATURE SENSOR. THE APU OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20060103000762006010300076NM 2006 1 3 SWAA054150 120051228A53116520723 FRAME BOEING737 7375H4 138449DNM FWD CARGO CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29526SW 26568 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, AFT FRAME NR 5 STOP FITTING. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20060103000772006010300077NM 2006 1 3 SWAA054151 120051228A53116520722 FRAME BOEING737 7375H4 138449DNM FWD CARGO CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29526SW 26568 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, FWD FRAME NR 5 STOP FITTING. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20060103000782006010300078NM 2006 1 3 SWAA054152 120051224A321065447714 DAMPER BOEING737 7373H4 1384600NM RT MLG WW MISSING A SWAAK NONE O OTHER LDLANDING 1 SW29609SW 27929 SEVERE SHIMMY ON LANDING ROLLOUT. ACFT TOWED TO GATE. FOUND RT MLG SHIMMY DAMPER MISSING, RT MLG UPPER & LOWER TORSION LINKS & ATTACHMENT PINS DAMAGED, NR 3 & NR 4 MAIN TIRE/WHEEL ASSY, BRAKES & BRAKE FLEX LINES DAMAGED, RT MLG DAMPER FLEX LINE TORN, RT MLG CLEVIS PIN WORN. REPLACED RT MLG SHIMMY DAMPER AND ASSOCIATED PARTS LISTED PER MM. 2L72 4F RTA16WE 20060103000812006010300081NM 2006 1 3 SWAA054155 120051227A53306545765 SKIN BOEING737 737317 138447PNM BS 514 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 514, STR 16L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20060103000822006010300082NM 2006 1 3 SWAA054156 120051227A53306545776 SKIN BOEING737 737317 138447PNM BS 947.5 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947.5, STR 23R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20060103000892006010300089EA 2006 1 3 VNAA0512013 120051218A492038004883 APU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE APU BAY FAILED A VNAAO OTHER JB WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 GL05241PS4934 7909 DURING DESCENT THE CREW RECEIVED THE APU OVERTEMP AND LAV SMOKE WARNINGS. SMOKE WAS REPORTED IN THE CABIN AND COCKPIT. THE CREW FOLLOWED THE QRH, DECLARED AN EMERGENCY, AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE APU AND FOUND NO LEAKS OR EXTERNAL DAMAGE. THE APU WAS DEFERRED IAW MEL 49-10-01 AND THE AIRCRAFT WAS RELEASED FOR SERVICE. ON 12/21/05 THE APU WAS REMOVED AND REPLACED WITH A SERVICEABLE UNIT. OPERATIONAL AND LEAK CHECKS WERE GOOD. THE MEL WAS CLEARED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20060103000902006010300090NM 2006 1 3 SWAA054147 120051228A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29479WN 33990 EEPLS TRACK LOOSE AT ROW 1 ABC. SECURED EEPLS PER MM. 2L72 4F RTA16WE 20060103000912006010300091NM 2006 1 3 SWAA054148 120051228A53116520722 FRAME BOEING737 7375H4 138449DNM FWD CARGO CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29511SW 24188 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, FWD FRAME LOWER STOP FITTING. REPAIRED FRAME PER SWA EA. 2L72 4F RTA16WE 20060103000922006010300092EA 2006 1 3 VNAA0512011 120051214A3097 WIRE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE ANTI ICE SYS SHORTED A VNAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL05718PS 10175 THE WING ANTI-ICE SENSOR CAUTION MESSAGE ILLUMINATED DURING CLIMB. THE CREW FOLLOWED THE QRH AND RETURNED TO CLT. MAINTENANCE REPAIRED A CHAFED/SHORTED WIRE HARNESS IN THE LEFT WING LEADING EDGE AND REPLACED THE ANTI-ICE & LEAK DETECTION CONTROL UNIT WHICH FAILED DUE TO THE SHORTED WIRES. THE SYSTEM OPERATIONALLY CHECKED GOOD AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20060103000932006010300093EA 2006 1 3 ASOA051032 120051128A5210601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27914EV 7752 DURING A HANGAR INSPECTION IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND TO BE BROKEN AT THE ATTACHMENT ARM. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060103000942006010300094SO 2006 1 3 SIMA200534705 120051202A532014525381003 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO FS 20 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21665BC 145783 THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED THE CORROSION BY MAKING A CUT OUT. PREPARED A DOUBLER, FILLER, PLATE AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 31, CHAPTER 53-00-10. (M) 2L72 4T RTT00011AT 20060103000962006010300096NM 2006 1 3 ASAA0510345 120051108A53116546552506 FRAME BOEING737 737298C 1384490NM FS 827 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02745AS 20794 YXX - FOUND FRAME TO SKIN ATTACHMENT AT BS 827, 5 INCHES BELOW STRINGER 17 LEFT CORRODED. CORROSION REMOVED AND REPAIRED WITH FABRICATED REPAIR SHEAR TIE IAW B737-200 SRM 51-30-05. (M) 2L72 4F RTA16WE 20060103000972006010300097NM 2006 1 3 ASAA0570046 120050725A5321453A26101 FLOOR PANEL BOEING737 737790 13844CNNM FS 767-887 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02645AS 33011 PAE - DURING C-CHECK, FOUND CORROSION ON NR 2 FLOORBOARD AROUND EDGES IN AFT CARGO BAY. REPAIRED IAW SRM 53-60-53. (M) 2L72 4F RTA16WE 20060103000982006010300098NM 2006 1 3 ASAA0570044 120050725A5320146A7502 SUPPORT BOEING737 737790 13844CNNM FS 727-767 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02645AS 33011 PAE - FOUND DURING C-CHECK, CORROSION ON FLOOR SIDEWALL SUPPORT AT BS 727. REPAIRED IAW SRM 51-40-02. (M) 2L72 4F RTA16WE 20060103000992006010300099NM 2006 1 3 ASAA0590082 120050425A5320146A7502 SUPPORT BOEING737 737990 NM FS 767-847 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02309AS 30857 PAE - DURING C-CHECK, FOUND CORROSION IN AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT AT LBL 25. REPAIRED IAW SRM 53-00-53. (M) 2L74 4F RTA16WE 20060103001012006010300101NM 2006 1 3 ASAA0510344 120051108A53306552928597 STRINGER BOEING737 737298C 1384490NM FS 847 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02745AS 20794 YXX - FOUND STRINGER 26 LEFT CORRODED AT BS 847. REMOVED CORROSION, REPLACED PART WITH FABRICATED PART IAW B737-200 SRM 53-10-3. (M) 2L72 4F RTA16WE 20060103001022006010300102NM 2006 1 3 ASAA0570045 120050725A5320146A75021 SUPPORT BOEING737 737790 13844CNNM FS 727-847 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02645AS 33011 PAE - DURING C-CHECK, FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT AT BS 727. REPAIRED IAW SRM 53-60-53. (M) 2L72 4F RTA16WE 20060103001032006010300103NM 2006 1 3 ASAA0590085 120050425A5320146A750217 SUPPORT BOEING737 737990 NM FS 727 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02309AS 30857 PAE - DURING C-CHECK, FOUND CORROSION IN AFT CARGO BAY ON FLOOR SUPPORT AT LBL 20. REPAIRED IAW SRM 53-00-53. (M) 2L74 4F RTA16WE 20060103001042006010300104SO 2006 1 3 SIMA200533902 120051130A3350 CHARGER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSMALFUNCTIONED A SIMAO OTHER O OTHER CLCLIMB 1 SW21650AE 145417 ORD - FLT 4435 - FOUND EMERGENCY LIGHT CIRCUIT BREAKER POPPED. WOULD NOT RESET. EMERGENCY LIGHT NO ARMED EICAS MESSAGE ILLUMINATED. REPLACED NR 3 EMERGENCY BATTERY AND CHARGER IAW EMB 145 MM 33-50-04. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. CHARGER P/N OFF 11-0049 S/N OFF 14855, BATTERY P/N OFF 20131 S/N OFF 67338. (M) 2L72 4T RTT00011AT 20060103001052006010300105NM 2006 1 3 ASAA0510347 120051108A2120655447015 PLENUM BOEING737 7372Q8C 138448SNM NR 2 A/C BAY ODOR A ASAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM02741AS 21959 ANC - FLIGHT DECK FUMES, AFTER LANDING AT SCC ARID SMELL ENTERED FLIGHT DECK, ISOLATED TO LEFT PACK RELEASED PER MEL. FOUND LEFT PACK CHAMBER MIX DUCT BLOWN, DUCT FLANGE PULLED AWAY FROM MIX CHAMBER. REPLACED MIX CHAMBER, REPLACED BOTH COALESCER BAGS. (M) 2L72 4F A16WE 20060103001082006010300108NM 2006 1 3 ASAA0510343 120051108A532069530012 SUPPORT BRACKET BOEING737 737298C 1384490NM FS 616 GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02745AS 20794 YXX - BS 616 STRINGER 17 RIGHT FRAME SUPPORT BRACKET HAS GOUGE ALONG SURFACE AND COMMON FASTENER HOLE. BS 616 STRINGER 17 RIGHT FRAME SUPPORT BRACKET GOUGES REPAIRED IAW B737-200 SRM 51-20-1 FIG 7 AND 51-30-5 FIG 4, FASTENERS INSTALLED IAW B737-200 SRM 51-30-02. (M) 2L72 4F RTA16WE 20060103001112006010300111NM 2006 1 3 ASAA0590087 120050425A5321453A161084 FLOOR PANEL BOEING737 737990 NM CARGO BAY DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02309AS 30857 PAE - DURING C-CHECK, FOUND FORWARD CARGO BAY NR 5 FLOOR PANEL IS DENTED. REPAIRED IAW SRM 51-40-02. (M) 2L74 4F RTA16WE 20060103001132006010300113NM 2006 1 3 ASAA0590089 120050425A5320146A9403 REVEAL BOEING737 737990 NM FS 794 GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02309AS 30857 PAE - DURING C-CHECK, FOUND AFT BAY AFT CARGO DOOR FORWARD FRAME REVEAL IS GOUGED AT BS 794. REPAIRED IAW SRM 51-40-40. (M) 2L74 4F RTA16WE 20060103001152006010300115NM 2006 1 3 ASAA0590088 120050425A5320146A82081 REVEAL BOEING737 737990 NM FS 845 GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02309AS 30857 PAE - DURING C-CHECK, FOUND AFT BAY AFT CARGO DOOR FRAME IS GOUGED AT BS 845. REPAIRED IAW SRM 51-40-05. (M) 2L74 4F RTA16WE 20060103001162006010300116EA 2006 1 3 ASOA051034 120051128A5210600318954 BRACKET CNDAIRCL600 CL6002B19 1900309EA PAX DOOR INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27832AS 7243 DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WOULD NOT CLOSE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR CABLE SUPPORT BRACKET. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060103001172006010300117NM 2006 1 3 ASAA0590095 120050425A5320143A948523 FLOOR SUPPORT BOEING737 737990 NM FS 500L CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02309AS 30857 PAE - DURING C-CHECK, FOUND FLOOR SUPPORT ANGLE CORRODED. REPAIRED IAW SRM 51-40-02. (M) 2L74 4F RTA16WE 20060103001192006010300119NM 2006 1 3 ASAA0590098 120050425A5311146A12511 FRAME BOEING737 737990 NM FS 727 MISDRILLED A ASAAK NONE W INADEQUATE Q C ININSP/MAINT 1 NM02309AS 30857 PAE - DURING C-CHECK, FOUND FRAME HAS DOUBLE DRILLED HOLES AT BS 727. REPAIRED IAW SRM 51-70-11. (M) 2L74 4F RTA16WE 20060103001212006010300121NM 2006 1 3 ASAA0590097 120050425A5320146A750130 FLOOR SUPPORT BOEING737 737990 NM FS 794-847 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02309AS 30857 PAE - DURING C-CHECK, FOUND CORROSION ON FLOOR SUPPORT AT BS 794-847. REPAIRED IAW SRM 53-00-53. (M) 2L74 4F RTA16WE 20060103001232006010300123NM 2006 1 3 ASAA0590100 120050425A5620143A750111 FLOOR SUPPORT BOEING737 737990 NM FS 500A CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02309AS 30857 PAE - DURING C-CHECK, FOUND FLOOR SUPPORT CORRODED AT 500A. REPAIRED IAW SRM 51-40-02. (M) 2L74 4F RTA16WE 20060103001252006010300125EU 2006 1 3 ASOA051033 120051128A33507012210 LAMP AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27634AS 370 DURING A GROUND INSPECTION IN MGM, THE EMERGENCY EXIT SIGN, ABOVE THE FLIGHT ATTENDANTS SEAT, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT SIGN, ABOVE THE FLIGHT ATTENDANTS SEAT. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20060103001262006010300126NM 2006 1 3 ASAA0590092 120050425A5320146A750217 FLOOR SUPPORT BOEING737 737990 NM FS 727 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02309AS 30857 PAE - DURING C-CHECK, FOUND CORROSION IN AFT CARGO BAY ON FLOOR SUPPORT AT LBL 25. REPAIRED IAW SRM. (M) 2L74 4F RTA16WE 20060103001272006010300127NM 2006 1 3 ASAA0590093 120050425A5300143A1221 STRUCTURE BOEING737 737990 NM FS 500A DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02309AS 30857 PAE - DURING C-CHECK, FOUND DAMAGED FASTENER HOLE AT BS 500A. REPAIRED IAW SRM 51-30-01. (M) 2L74 4F RTA16WE 20060103001282006010300128NM 2006 1 3 ASAA0510349 120050425A2612 FIRE LOOP BOEING737 737298C 1384490NM NR 2 NACELLE UNKNOWN A ASAAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 NM02745AS 20794 ANC - DURING CRUISE, NR 2 ENGINE FIRE HANDLE ILLUMINATED. BOTH FIRE BOTTLES FIRE ON TAXI IN PER QRH. REMOVED AND REPLACED LOWER FIRE LOOP. ALSO, REMOVED AND REPLACED FORWARD AND AFT FIRE BOTTLES. (M) 2L72 4F RTA16WE 20060103001292006010300129NM 2006 1 3 ASAA0590107 120050505A5320146A750217 SUPPORT BOEING737 737990 NM FS 727 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02309AS 30857 PAE - FOUND CORROSION IN AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT LBL 20 BS 727 PLUS 4 THRU BS 727D PLUS 4, WL 155. REPLACED SUPPORT. (M) 2L74 4F RTA16WE 20060103001302006010300130NM 2006 1 3 ASAA0590102 120050425A5321453A161081 FLOOR PANEL BOEING737 737990 NM FS 500D DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02309AS 30857 PAE - DURING C-CHECK, FOUND FORWARD CARGO BAY NR 4 FLOOR PANEL DAMAGED. REPAIRED IAW SRM 53-30-53. (M) 2L74 4F RTA16WE 20060103001312006010300131NM 2006 1 3 ASAA0590108 120050505A5321453A261037 FLOOR PANEL BOEING737 737990 NM FS 727 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02309AS 30857 PAE - AFT BAY NR 1 FLOOR PANEL HAS NUMEROUS DENTS. REPLACED FLOOR PANEL. (M) 2L74 4F RTA16WE 20060103001332006010300133NM 2006 1 3 ASAA0540659 120051117A531165C3232516 FRAME BOEING737 7374Q8 138447QNM FS 500E DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND DENT IN FRAME AT BS 500E, STRINGER 24R. REPAIRED DENT PER B737-400 SRM 51-70-11 AND 53-30-53. (M) 2L72 4F RTA16WE 20060103001342006010300134NM 2006 1 3 ASAA0540660 120051117A531165252304 FRAME BOEING737 7374Q8 138447QNM FS 727 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND FRAME CORRODED AT BS 727E, LBL 20. REPAIRED PER B737-400 SRM 53-00-07. (M) 2L72 4F RTA16WE 20060103001352006010300135EA 2006 1 3 ASOA051031 120051113A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA BS 484 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27914EV 7752 DURING A C-CHECK IN TUS, THE FS 484 INTERCOSTAL, LBL 36, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FS 484 INTERCOSTAL, LBL 36, IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20060103001382006010300138NM 2006 1 3 UPS05M45896 120051021A5347 SEAT TRACK DOUG MD11 MD11F 3023600NM BS 1381 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01281UP 48538 INSPECTION TYPE:C CABIN AT STA 1381 RT RBL 107.25 SEAT TRACK CROWN FOUND WITH CORROSION. CORROSION REMOVED PER SRM 51-2101 REV 31 VOL II AT SEAT TRACK & MAT REMOVED 0.038 INCH ORIG THK 0.100 INCH & FOUND EXCEED LIMIT PER SRM 53-70-00 VOL I REV 37 FIG 3. NEW SEAT TRACK EXTRUSION REPAIR SPLICE HATS & SPLICE PLATES BETWEEN STA 1351 TO STA 1411 RBL 107.25 INSTALLED PER SRM 51-31-01 VOL II REV 37 & SRM 53-7 0-00 FIG 1 VOL I REV 37. 2L73 4F RTA22WE 20060103001392006010300139EA 2006 1 3 QXEA200501807 120051220A2150 SENSOR CNDAIRCL600 CL6002C10 1390015EA NR 1 A/C PACK FAILED A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09608QX 10026 DAY- ON TAXI OUT ON FLIGHT 4192 RETURNED TO THE GATE WITH A LEFT AIR CONDITIONING PACK MESSAGE. PLACED ON MEL 21-51-4B. 12/26 REMOVED AND REPLACED NR 1 PACK. DISCHARGE TEMP SENSOR AND NR 1 PACK, DISCHARGE PRESSURE SENSOR IAW CRJ 700 AMM 21-51-22-000-801-A01/21-51-22-400-801-A01, AMM 21-51-24-000-801-A01/21-51-24-400-801-A01. PERFORMED AN OPS AND LEAK CHECK OF SYSTEM, CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20060103001402006010300140EA 2006 1 3 QXEA200501844 120051227A5270840534 SWITCH CNDAIRCL600 CL6002C10 1390015EA PAX DOOR MALFUNCTIONED A QXEAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 NM09611QX 10041 ONT - ON TAXI OUT FOR FLIGHT 2514 RETURNED TO THE GATE WITH A PASSENGER DOOR HANDLE OUT MESSAGE. PLACED ON MEL IAW MEL REF 52-70-1. 12/27 REMOVED AND REPLACED PROX SENSOR PX107 IAW 52-70-04-000-808-A01 AND 52-70-04-400-808-A01. OPERATIONAL CHECKED GOOD, SENSOR UNREASON/OPEN FAULT CLEARED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20060103001412006010300141EA 2006 1 3 QXEA200501810 120051222A5101 UNKNOWN CNDAIRCL600 CL6002C10 1390015EA UNKNOWN UNKNOWN A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09612QX3741 1501 10042 FAT - ON TAXI FOR FLIGHT 2453 SPLR/STAB FAULT & RUD LIMIT FAULT STATUS MSGS KEEP CYCLING ON AND OFF. RETURNED TO THE GATE. REMOVED AND REPLACED ISI PER CRJ700 AMM 34-12-01-000-801-A01 AND 34-12-01-400-801-A01. PERFORMED PITOT LIN P3 CONTAMINATION REMOVAL PER TR 34-0089 34-11-00-100-803-A02. REMOVED STATIC LINE S3 CONTAMINATION PER 34-11-00-100-806-A01, NO CONTAMINATION NOTED ON S3 OR P3. PERFORMED OPS TEST OF ISI PER CRJ-700 AMM 34-12-01-710-801-A01, NO DEFECTS NOTED. PERFORMED MTC R341101 PITOT/STATIC LEAK CHECK, NO LEAKS NOTED. PERFORMED SPOT TESTS SPLR/STAB FAULT CLEARED AND RUD LIMIT FAULT. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20060103001422006010300142EA 2006 1 3 QXEA200501827 120051223A7830 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA THRUST REVERSER ILLUMINATED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09613QX 10045 SJC - RETURNED TO THE GATE FOR A LEFT THRUST REVERSER MESSAGE. PLACED THE SYSTEM ON MEL. AIRCRAFT RETURNED TO SERVICE. MEL CLEARED ON 12/24 IN PDX. COMPLIED WITH FUNCTIONAL CHECK OF LT ENG THRUST REVERSER IAW POWER PLANT GROUND RUN MANUAL 78-30-00-720-801-A01, OPS CHECK GOOD. NO OTHER DEFECTS NOTED. MEL CLOSED AND AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2L72 4F RTA21EA 20060103001432006010300143EA 2006 1 3 QXEA200501806 120051218A2150GG670950191 VALVE CNDAIRCL600 CL6002C10 1390015EA NR 1 A/C PACK INOPERATIVE A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09612QX5272 10042 PDX - ON TAXI FOR FLIGHT 2475 RETURNED TO THE GATE WITH NR 1 AIR CONDITIONING PACK NOT ON-LINE. PLACED ON MEL 21-51-1(A). RETURNED TO SERVICE. ON 12/20 MDC INDICATES LEFT FLOW CONTROL VALVE NO RESPONSE TO COMMAND. REMOVED AND REPLACED LEFT FLOW CONTROL VALVE IAW CRJ AMM TASK 21-53-14-000-801-A01 AND 21-53-14-400-801-A01. OPS CHECK GOOD, NO LEAKS NOTED. PERFORMED SEVERAL ENGINE STARTS. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20060103001442006010300144EA 2006 1 3 QXEA200501828 120051223A2497 CONNECTOR CNDAIRCL600 CL6002C10 1390015EA NR 1 IDG BURNED A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09602QX 10010 GEG - AIRCRAFT RETURNED TO THE GATE ON FLIGHT 4309 FOR THE NR 1 IDG DISCONNECT MESSAGE. NR 1 IDG DISCONNECTED AT 0700 PST 12/23/05. DEFERRED PER MEL REF 24-11-1(A). AIRCRAFT RETURNED TO SERVICE. 12/26 REPLACED J553 CONNECTOR DUE TO BURNED PINS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20060103001452006010300145EA 2006 1 3 QXEA200501829 120051225A7897 CONNECTOR CNDAIRCL600 CL6002C10 1390015EA THRUST REVERSER FAILED A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09613QX 10045 BOI - ON FLIGHT 2463 RETURNED TO THE GATE WITH A LEFT THRUST REVERSER STATUS MESSAGE. AIRCRAFT FERRIED FROM BOI PDX. IN PDX FOUND WIRE FAE 67321-18 SHORTED TO AC GROUND BETWEEN TM155 PIN F TO J505 AT LT STUBWING PIN G. REMOVED AND REPLACED CONNECTOR J505 IAW CRJ WD 20-16-00 PAGE 201-207 AND CRJ 700 WD 78-30-00 SH 1 OF 1 PAGE 01-A01. REPLACED PIN FOR PIN. I NSERTED PIN F OF TM155 AND REINSTALLED TM155. PERFORMED FUNCTIONAL TEST OF THE NR 1 ENG THRUST REVERSER IAW CRJ 700 AMM TASK 78-30-00-720-801-A01. OPS CHECKED GOOD. PRESSURIZED AND DEPRESSURIZED AC FOR LEAK CHECK CP J505 FEED THROUGH IAW CRJ AMM TASK 21-31-00-910-801-A01 AND 21-31-00-910-802-A01. LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20060103001462006010300146EA 2006 1 3 QXEA200501826 120051222A5210 DOOR CNDAIRCL600 CL6002C10 1390015EA MAIN PAX UNKNOWN A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09601QX 10009 TUS - ON FLIGHT 4172 UNABLE TO OPEN MAIN CABIN DOOR. MAINTENANCE OPENED DOOR UPON ARRIVAL FROM INSIDE AND OUTSIDE, DOOR CHECKS NORMAL. COMPLIED WITH CRJ700 AMM TASK 52-11-00-710-802-A02. WHILE COMPLYING WITH TASK 52-11-00-710-801-A01, AFT PSG DOOR OUT HANDLE DISPLAYED ON STEP 20A. PLACED ON MEL 52-70-1. RETURNED TO SERVICE. ON 12/24 PERFORMED OPERATIONAL TEST OF PASSENGER DOOR IAW CRJ 700 AMM TASK 52-11-00-710-801-A02. OPERATIONALLY TESTS SATISFACTORY. ALL DOOR INDICATIONS NORMAL. THIS ACTION CLEARS MEL 52-70-1 AND RSI 347355. PLACARDS REMOVED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2L72 4F RTA21EA 20060103001472006010300147NM 2006 1 3 UPS05M45897 120051017A5347 SEAT TRACK DOUG MD11 MD11F 3023600NM STA1321 LBL27.5 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01281UP 48538 INSPECTION TYPE:C CABIN AT STA 1321 LBL 27.5 SEAT TRACK CROWN FOUND CORRODED. CABIN STA 1321 LBL 27.5 SEAT TRACK CROWN CORROSION REMOVED PER SRM 53-70-00 FIG 3 VOL I REV 37 MAT ORIG THK 0.145: & MAT REMOVED 0.035 FOUND EXCEED LIMIT PER SRM 53-70-00 FIG 3 VOL 3 VOL I REV 37. NEW SEAT TRACK EXTRUSION, REPAIR SPLICE HATS & SPLICE PLATES BETWEEN STA 1209 TO STA 1351 LBL 27.5. INSTALLED PER SRM 51-31-01 VOL II REV 37 & SRM 53-70-00 FIG1 VOL I REV 37. 2L73 4F RTA22WE 20060103001492006010300149NM 2006 1 3 PIDA20050204 120051229A534369378776 FITTING BOEING737 7373G7 1384595NM MLG CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05390WL 23219 RIGHT MAIN LANDING GEAR ACTUATOR OUTBOARD LOWER FORWARD ATTACH FITTING ON WING LOWER SPAR IS CRACKED. REPLACED ATTACH FITTING PER SRM 51-10-2. 2L72 4F RTA16WE 20051228001132005122800113NE 2005 12 28 ALG2005F00114 120051114A3260 INDICATION SYS SKRSKYS76 S76C 8143008NE MLG UNKNOWN E ALGAO OTHER P NO WARNING INDICATION HOHOVERING 1 SW03868AL 760580 UNLOCK LIGHT DID NOT ILLUMINATE DURING GEAR TRANSIT AND GREEN LIGHTS DID NOT ILLUMINATE WHEN GEAR DOWN. RESET CIRCUIT BREAKER, HOVERED AC, CYCLED GEAR 4 TIMES AND LIGHTS WORKED PROPERLY. (K) 1G72 3U NCH1NE 20051228001722005122800172NM 2005 12 28 AWXA200501586 120051120A5312651758243 BULKHEAD BOEING737 7373S3 1384711NM BS 178 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 MCN - DURING C20 CHECK DISCOVERED VERTICAL WEB CRACKED, 1.31 INCHES, FROM WL 226 TO WL 234, BS 178 AND BL 17R. MAINTENANCE REMOVED VERTICAL WEB FROM WL 226 TO WL 234, BS 178 AND BL 17R IAW BOEING 737-300 SRM 53-10-08-2R17 FIG 201. FABRICATED NEW WEB IAW BOEING 737-300 SRM 53-10-08-2R17 AND BOEING DWG 65-17582. INSTALLED FABRICATED REPAIR PARTS AT BS 178, BL 17R AND FROM WL 226 TO WL 234 IAW BOEING 737-300 SRM 53-10-08-2R17 FIG 201. 2L72 4F RTA16WE 20051228001762005122800176NM 2005 12 28 AWXA200501587 120051116A532065479577 WEB BOEING737 7373S3 1384711NM BS 858-863 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 MCN - DURING C20 CHECK DISCOVERED CORROSION ON THE AFT CARGO FLOOR WEB AT BS 858 TO BS 863, BL 19R AND WL 158. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-15-OI 1 FIG 1. MAINTENANCE REMOVED WEB AND INSTALLED NEW WEB AT BS 858 TO BS 863, BL 19R AND WL 158 IAW BOEING 737-300 SRM 51-40-02-0G. 2L72 4F RTA16WE 20051228001782005122800178NM 2005 12 28 AWXA200501589 120051120A532065479576 WEB BOEING737 7373S3 1384711NM BS 794-847 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 MCN - DURING C20 CHECK DISCOVERED CORROSION ON THE AFT CARGO DOOR SILL WEB FROM BS 794 TO BS 847 AND STR 25R. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-15-1A1 FIG 101. MAINTENANCE REMOVED WEB AND INSTALLED NEW WEB FROM BS 794 TO BS 847 AND STR 25R IAW BOEING 737-300 SRM 51-40-02-0G. 2L72 4F RTA16WE 20051228001802005122800180NM 2005 12 28 AWXA200501591 120051113A57536546431279 WEDGE BOEING737 7373S3 1384711NM ZONE 500 - LEFT DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 MCN - DURING C20 CHECK DISCOVERED DISBOND AREA AT THE AFT EDGE OF THE LT OUTBOARD FORE FLAP, APPROXIMATELY 8" FROM THE INBOARD END. MAINTENANCE REMOVED DISBONDED SKIN ON THE LT OTBD FORE FLAP IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED REPAIR FILLER AND DOUBLER IAW BOEING 737-300 SRM 51-70-10-2R4. BONDED REPAIR PARTS TO THE AFT EDGE OF THE LT OUTBOARD FORE FLAP IAW BOEING 737-300 SRM 51-70-10-2R4. 2L72 4F RTA16WE 20051228001822005122800182NM 2005 12 28 AWXA200501593 120051111A5320654581945 GUSSET BOEING737 7373S3 1384711NM BS 259 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 MCN - DURING C20 CHECK DISCOVERED GUSSET AT TOP OF THE NLG CRACKED IN RADIUS AT BS 259, WL 188 AND FROM BL 4L TO BL 4R. MAINTENANCE REMOVED AND REPLACED GUSSET AT THE TOP OF THE NLG IAW BOEING 737-300 SRM 51-40-02-0G FIG 12. 2L72 4F RTA16WE 20051228001872005122800187SO 2005 12 28 SWIA200516012 120051216A2120 SMOKE EMB 120 EMB120ER 3260203SO UNKNOWN DETECTED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM07221SW 120290 ON GROUND SEVERE SMOKE IN COCKPIT SMOKE FROM LEFT PACK BY WING, RIGHT SIDE "AIR COND" FAIL LIGHT ON OVERHEAD PANEL MAP LIGHT ELEC AND DOOR CONTINOUSLY. REPLACED RT WOW HARNESS WITH SERVICEABLE UNIT. TAXIED A/C, OPERATED LT AND RT PACKS. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20051228001912005122800191SO 2005 12 28 SWIA200516039 120051221A3397 WIRE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHTSBROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07565SW 120340 LAST THREE EMERGENCY LIGHTS OUT. REPAIRED BROKEN WIRE UNDER FLOORBOARD AT SEAT 9A, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20051228001932005122800193EA 2005 12 28 SWIA200516029 120051223A2741 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07910SW 7566 STAB TRIM CH 1 WILL NOT STAY ENGAGED. REPLACED STAB TRIM MACH TRIM ENGAGE PANEL. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051228001952005122800195EA 2005 12 28 SWIA200516031 120051219A274170609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07976SW4733 4733 7952 STAB TRIM RUNAWAY. REPLACED HSTCU IAW CRJMM 27-41-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051228001972005122800197SO 2005 12 28 SWIA200516033 120051001A5347 SEAT TRACK EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07217SW 120286 FWD LT FLOOR TRACK CORRODED, GALLEY FLOOR ANCHOR, ITEM FOUND AT C-CHECK INSPECTION. REPLACED FORWARD LT INBOARD SEAT TRACK. 2L72 4T RTA31SO 20051228001992005122800199SO 2005 12 28 SWIA200516035 120051001A5347 SEAT TRACK EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07217SW 120286 PAX SEAT TRACK CORRODED FWD LT SIDEWALL, ITEM FOUND AT C-CHECK INSPECTION. REPLACED PAX SEAT TRACK FWD LT SIDEWALL IAW EMB120 MM 53-01-05. 2L72 4T RTA31SO 20051228002022005122800202EA 2005 12 28 SWIA200516038 120051215A27515913000 SENSOR CNDAIRCL600 CL6002C10 1390015EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07706SK4046 4046 10149 "FLAPS HALFSPEED" STATUS MESSAGE. REPLACED LT FLAP BPSU IAW MM 27-52-03. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20051228002082005122800208EU 2005 12 28 YENA200583 120051125A2611 CONTROL UNIT AIRBUS320 A320232 3930326EU IAE V2500 V2500A1 NE SMOKE DETECTORS MALFUNCTIONED A YENAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 EA15565JB105763589 2031 MOMENTARY CARGO SMOKE WARNING FOLLOWED BY DISCH 1 LIGHT ON CARGO SMOKE PANEL. FOLLOWED BY AGENT 2 DISCH LIGHT. (BOTTLE 2 NOT DISC.) AND ECAM CALLING FOR NR 2 DISCH. REMOVED AND INSTALLED FWD CARGO FIRE ESTINGUISHER IAW 26-23-41. OPS CHECK GOOD. A/C GOOD FOR FURTHER SERVICE. REMOVED AND REPLACED SMOKE SDCU DETECTOR (70WQ) IAW AMM 26-17-34, OPS CHECK GOOD. 2L72 4F4 FRTA28NM E311NE 20051228002092005122800209NM 2005 12 28 AT0500044 120051130A33508039251 BATTERY PACK BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE EMERGENCY LIGHT INOPERATIVE A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15896AT 55048 DURING THE OPERATIONAL TEST OF EMERGENCY EVACUATION LIGHT SYSTEM IAW SERVICE CHECK WORK CARD 604, FOUND SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE FROM ROW 10 FORWARD. REPLACED BATTERY PACK B5-118, SYSTEM OPS CHECKED NORMAL 2L72 4F4 FTRA6WE E00061EN 20051228002112005122800211CE 2005 12 28 113005N133CS1 120051130A2130 CABIN PRESSURE CESSNA525 525 2076601CE WILINTFJ44 FJ44 66000GL MALFUNCTIONED E Z5FAIBG CABIN DEPRESSURIZATION EMER. DESCENT O2 MASK DEPLOYED JS WARNING INDICATION AFFECT SYSTEMS CRCRUISE 1 NE03133CS 5250502 WHILE AT CRUISE, THE CABIN DEPRESSURIZED RAPIDLY. THE 10,000 FOOT CABIN ALTITUDE WARNING LIGHT ILLUMINATED AS THE CABIN WAS CLIMBING AT 3000 FEET/MINUTE, REACHING 16,000 FEET. CREW RECEIVED APPROVAL FROM ATC TO PERFORM EMERGENCY DESCENT TO 10,000 FEET. AT 10,000 FEET THE CREW SET CONTROL TO MANUAL AND WERE ABLE TO STABILIZE CABIN ALTITUDE. AIRCRAFT WAS DIVERTED FOR MAINTENANCE. 1L72 4F4 FRTA1WI E3GL 20051230000072005123000007NM 2005 12 30 BB05105 120051223A5610141T480150 WINDSHIELD BOEING767 767200 1385120NM COCKPIT CRACKED A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19655US27342 25257 FLIGHT 15, MUC-PHL: DURING CLIMBOUT, F/O WINDSHIELD CRACKED. A/C DIVERTED TO AMS FOR WINDSHIELD CHANGE. MAINTENANCE COMPLETED THE WINDSHIELD CHANGE. NO FURTHER DIFFICULTIES. 2L72 4F RTA1NM 20051230000082005123000008NM 2005 12 30 2005UALA00976 120050910A4900 SENSOR BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE APU UNKNOWN A UALAJA DUMP FUEL UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 WP29796UA 26931 P1119 FLIGHT LOST APU. *S/D* LT IDG WAS INOPED 09SEP05. THE RT IDG WAS INOPED, REPLACED. ON 10SEP05 THE APUC GAVE THE MSG COMPLETE LOSS OF APUC BUS ACTIVITY (BOTH LT AND RT 629) FOR 3 SECONDS AFTER THE APU MASTER CONTROL SWITCH HAS BEEN IN THE ON POSITION FOR TEN SECONDS. STATUS MSG-4911110 INACTV ER MODE IAW FIM 49-53 TASK 804 THE APUC CB WAS RESET THE DELTA-P SENSOR WAS CHECKED AND THE APU OPS CHECKED OK. 2L72 4F4 FRTT0001SE E46NE 20051230000102005123000010EU 2005 12 30 2005UALA01478 220051218A7200 ENGINE BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU NR 2 BIRD INGESTION A UALAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 WP29329UA 24149 723258 RETURN TO FIELD DUE TO BIRD STRIKE TO NR 2 ENGINE & ASSOCIATED HIGH VIBRATIONS. AFTER FAN BLADE SET REPLACEMENT HIGH ENGINE VIBRATION CONTINUED AND ENGINE WAS REPLACED. THE ENGINE SHOP VERIFIED CORRECT FAN BLADE SPACER, SHIM, RETAINER AND PROPER FAN BLADE WEIGHT CLASS POSITIONING INSTALLATION (38 FAN BLADES). WHILE VERIFYING FAN BLADE WEIGHT CLASS MATCH TO THEIR ACTUAL MOMENT WEIGHT, ONE FAN BLADE WAS FOUND MISS-MARKED BY VENDOR BY MORE THAN SEVERAL CLASSES. VERIFIED THE MISS-MARKED MOMENT WEIGHT CLASS ON FAN BLADE AS CAUSE FOR ENGINE HIGH FAN VIBRATION. 2L72 4F4 FRTA16WE E21EU 20051230000192005123000019NM 2005 12 30 USAA051641 120051223A5311 FRAME BOEING737 737301 1384611NM BS 706 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19591US 23936 STA 706 FRAME WEB S9L AT I/B RIVET SECURING A/C PSU SUPPORT CRACKED. REMOVED DAMAGE AND INSTALLED, FABRICATED REPAIR PARTS IAW TR 53-10-22, DEFECT SIZE: .187 INCH. 2L72 4F RTA16WE 20051230000332005123000033NM 2005 12 30 2005UALA01495 120051220A5414 BUSHING BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE NR 1 PYLON CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29644UA 25094 NR 1 PYLON UPPER LINK FITTING, OUTBOARD LUG REQUIRES REWORK DUE TO INBOARD LUG REWORKED. BUSHING REPLACEMENT DUE CORRODED BUSHING. BOTH LUGS MUST BE REWORKED AS A PAIR. REWORKED AND BUSHINGS WERE REPLACED DUE TO CORROSION. BUSHINGS WERE REPLACED PER SRM 54-53-90 AND LUGS WERE REWORKED PER MM 54-51-93. 2L72 4F4 FRTA1NM E24NE 20051230000352005123000035NM 2005 12 30 2005UALA01497 120051221A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE SEAT 4F FWD INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29107UA 26900 SEAT 4F FWD EMERGENCY LIGHT INOPERATIVE. SECURED CONNECTOR. 2L74 4F4 FRTA20WE E24NE 20051230000362005123000036NM 2005 12 30 2005UALA01498 120051221A5330 SKIN BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29399UA 24674 A SCRIBE LINE WAS FOUND ON THE FUSELAGE SKIN ALONG THE EDGE OF THE FORWARD SECTION OF THE RT WING TO BODY FAIRING FROM STR 16R TO STR 28R APPROXIMATELY. MAJOR REPAIR. DAMAGE BLENDED. EXTERNAL DOUBLER AND INTERNAL TEARSTRAP INSTALLED. 2L72 4F4 FRTA16WE E21EU 20051230000462005123000046EA 2005 12 30 VNAA0512005 120051203A2100GG670950265 CONTROLLER CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE NR 1 A/C SYSTEM FAILED A VNAAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL05703PS4059 10137 AFTER PUSHBACK THE CREW RECEIVED THE SMOKE AFT LAV WARNING AND SMELLED A BURNING ODOR. THE PASSENGERS WERE EVACUATED THROUGH THE PASSENGER DOOR AND THE AIRCRAFT WAS TOWED BACK ONTO THE GATE. MAINTENANCE REMOVED AND REPLACED THE NR 1 AIR CONDITIONING SYSTEM CONTROLLER. THE SYSTEM OPERATIONALLY CHECKED GOOD AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20051230000502005123000050NM 2005 12 30 BB05108 120051227A3397 WIRE BOEING767 7672B7 1385107NM EMERGENCY LIGHTSBROKEN A USAAK NONE L NO TEST ININSP/MAINT 1 EA19653US 24894 FLOOR LEVEL EMERGENCY LIGHTS AFT CABIN RIGHT SIDE NEAR GALLEY FOUND INOPERATIVE. REPAIRED BROKEN WIRE AT TRACK LIGHT ASSEMBLY. NO FURTHER DIFFICULTIES. 2L72 4F RTA1NM 20051230000672005123000067NM 2005 12 30 QXEA200501812 120051203A5210 SKIN BOMBDRDHC8 DHC8402 1390042NM PAX DOOR GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09403QX 4037 PDX: SCRATCHES AND GOUGES ACROSS OUTBOARD END OF PASSENGER DOOR OUTER SHELL SKIN. MAINTENANCE REPAIRED IAW SRM 52-10-20-992-801, NDTM PART 6 TASK 51-00-01-250-801, SRM 51-25-05 AND SRM 51-20-25. 2H72 4T RTA13NM 20051230000732005123000073NM 2005 12 30 AWXA200501596 120051116A5320654795711 STRAP BOEING737 7373S3 1384711NM BS 774-858 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 MCN - DURING C20 CHECK DISCOVERED CORROSION ON THE AFT CARGO LOWER SILL STRAP FROM BS 774 TO BS 858, WL 158 AND BL 19R. NO CORROSION REMOVAL LIMITS WERE AVAILABLE IN THE BOEING 737-300 SRM. MAINTENANCE REMOVED AND INSTALLED NEW AFT CARGO DOOR LOWER SILL STRAP FROM BS 774 TO BS 858, WL 158 AND BL 19R IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 3, 4, 6, 7 AND 8. 2L72 4F RTA16WE 20051230000832005123000083NM 2005 12 30 QXEA200501823 120051210A5410 STIFFENER BOMBDRDHC8 DHC8402 1390042NM LT NACELLE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09403QX 4037 PDX: LT NACELLE FINGERNAIL SUPPORT DECK, UPPER SURFACE, OUTBOARD STIFFENER IS DAMAGED APPROX 40" FWD OF AFT END OF DECK. FRESH BLEND WITH CRACK. MAINTENANCE REPAIRED IAW HORIZON AIR EA 6-54-379 AND NDTM PART 6, 51-00-02. 2H72 4T RTA13NM 20051230000872005123000087NM 2005 12 30 QXEA200501824 120051205A5347 SEAT TRACK BOMBDRDHC8 DHC8402 1390042NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09403QX 4037 PDX: LT INBOARD SEAT TRACK HAS PITS AND CORROSION IN CENTER CHANNEL BETWEEN STA X177.7 AND X192.95. MAINTENANCE REPAIRED IAW RD 8-53-884, SRM 51-40-10 AND SRM 51-42-05. 2H72 4T RTA13NM 20051230000902005123000090 2005 12 30 RAIA00512024 420051223A3418C850023 STICK SHAKER JETAIRJETSTMJETSTM4101 1500501EU STALL WARNING INOPERATIVE A RAIAD RETURN TO BLOCK L NO TEST TXTAXI/GRND HDL 1 CE03571HK175359474 41090 5467 - SGF - RT STICK SHAKER INOP. MAINTENANCE REMOVED AND REPLACED NR 2 STICK SHAKER. 2L72 4T RTA41NM 20060103000162006010300016EA 2006 1 3 ASOA051071 120051207A1100S1868 PLACARD CNDAIRCL600 CL6002B19 1900309EA PAX DOOR WORN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27970EV 7527 DURING A HANGAR INSPECTION IN MCN, THE PASSENGER DOOR EXIT PLACARD WAS FOUND TO NEEDING REPLACEMENT. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EXIT PLACARD. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060103000282006010300028EA 2006 1 3 COMA0560742 120051221A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01962CA 7123 FLIGHT 5789 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 09-20-01. 2L72 4F RTA21EA 20060103000342006010300034NM 2006 1 3 SWAA054113 120051226A53306545776 SKIN BOEING737 7373H4 1384600NM BS 930 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, BETWEEN STR 24R TO STR 25R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20060103000392006010300039NM 2006 1 3 SWAA054117 120051227A3350101073 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHTSMISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29426WN 29830 EMERGENCY EXIT LIGHT LENS COVER MISSING. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20060103000482006010300048NM 2006 1 3 SWAA054126 120051227A5313BAC1498 STRINGER BOEING737 7373Q8 1384670NM BS 734 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 734, STR 27L. REPAIRED STRINGER PER SWA EA. 2L72 4F RTA16WE 20060103000552006010300055CE 2006 1 3 DXTA200501151 120051218A3230 LINE CESSNA560 560XL 2076702CE MLG UNKNOWN E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07610QS 5605210 AFTER TAKEOFF GEAR WAS SELECTED UP, RED UNLOCK LIGHT REMAINED ON AND HYD PRESS. ANNUNCIATOR WOULD NOT EXTINGUISH. SERVICED HYDRAULIC RESERVOIR TO FULL, JACKED AIRCRAFT TO SWING GEAR. CLEANED INDICATING SWITCH ON THE NOSE GEAR, CHECKED THE WIRING AND CANNON PLUGS ON THE MAIN GEAR AND NOSE GEAR, NO DEFECTS NOTED. CYCLED LANDING GEAR NUMEROUS TIMES WITH THREE GREEN LIGHTS WHEN GEAR WAS DOWN & LOCKED. ALL INDICATING & OPERATION OF THE LANDING GEAR IS NORMAL AT THIS TIME WITH NO DEFECTS NOTED. IAW CE 560XL MM 32-30-00. 2L72 4F RTA22CE 20060103000602006010300060EA 2006 1 3 ASOA051069 120051122A5315 FLOORBEAM CNDAIRCL600 CL6002C10 1390015EA BS 280 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27740EV 10151 DURING A C-CHECK IN TUS, THE FS 280 FLOORBEAM WAS FOUND TO BE CRACKED AND CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FS 280 FLOORBEAM IAW ASA EC EO700-53-0061. (M) 2L72 4F RTA21EA 20060103000612006010300061EA 2006 1 3 ASOA051075 120051208A33974871917190 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSDISCONNECTED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27860AS 7433 DURING A HANGAR INSPECTION IN BTR, THE EMERGENCY FLOOR CENTER STRIP LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE RECONNECTED THE EMERGENCY FLOOR CENTER STRIP LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060103000642006010300064EA 2006 1 3 ASOA051060 120051203A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA BS 280 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27716EV 10084 DURING A C-CHECK IN MCN, THE LEFT SIDE AND RIGHT SIDE FS 280 BULKHEAD WEB WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACED THE LEFT SIDE AND RIGHT SIDE FS 280 BULKHEAD WEB IAW BOMBARDIER REO 670-53-11-052. (M) 2L72 4F RTA21EA 20060103000862006010300086NM 2006 1 3 SWAA054144 120051228A53306545774 SKIN BOEING737 7373K2 13844BANM BS 727E CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29345SA 23786 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 22R. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20060103000872006010300087NM 2006 1 3 SWAA054145 120051228A53306545774 SKIN BOEING737 7373K2 13844BANM BS 744 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29345SA 23786 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 744, STR 25R. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20060103000882006010300088NM 2006 1 3 SWAA054146 120051227A3350207377 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHTSMISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29406WN 27894 DURING SCHEDULED MV2 CHECK, FOUND FWD LT EEPLS TRACK LENS COVER MISSING. INSTALLED LENS COVER PER MM. 2L72 4F RTA16WE 20060103000952006010300095SO 2006 1 3 SIMA200533901 120051130A2150 A/C PACK EMB 145 EMB145LR 3260212SO NR 1 FOD A SIMAO OTHER CB F.O.D. SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SW21625AE 145115 ORD - FLT 4095 - CREW NOTED A STRONG BURNING RUBBER SMELL. SMOKE DETECTOR LIGHT ILLUMINATED WITH NO VISIBLE SMOKE. FOUND FOD INSIDE THE PACK ONE NACA INLET (RUBBER). REMOVED RUBBER AND PERFORMED OPERATIONAL CHECK OF THE ACM WITH NO DISCREPANCIES NOTED. PERFORMED FUNCTIONAL CHECK FLIGHT WITH NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20060103001002006010300100SO 2006 1 3 SIMA200534503 120051209A5230 SKIN EMB 145 EMB145LR 3260212SO CARGO DOOR CRACKED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21620AE 145102 DURING OVERNIGHT MAINTENANCE, CARGO DOOR AFT UPPER CORNER OF SKIN WAS FOUND CRACKED. REPLACED CARGO DOOR ASSEMBLY IAW EMB AMM 52-30-01 AND 52-31-00. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20060103001072006010300107GL 2006 1 3 SIMA200532901 220051120A7261 CARBON SEAL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 2 ENGINE LEAKING A SIMAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SW21909AE 14500899 DFW - FLT 3749 - DURING TAKEOFF, RECEIVED LAVATORY SMOKE MASTER WARNING ON EICAS AND LAVATORY SMOKE DETECTOR ALARM WAS ACTIVATED. FOUND 0 CARBON LEAKING. REPLACED NR 2 ENGINE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T4 FRTT00011ATTE6CH 20060103001122006010300112NM 2006 1 3 ASAA0590091 120050425A5321453A261037 FLOOR PANEL BOEING737 737990 NM FS 727 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02309AS 30857 PAE - DURING C-CHECK, FOUND AFT BAY NR 1 FLOOR PANEL HAS DENTS. REPAIRED IAW SRM 53-60-53. (M) 2L74 4F RTA16WE 20060103001142006010300114NM 2006 1 3 ASAA0590090 120050425A5321453A261057 FLOOR PANEL BOEING737 737990 NM FS 727D DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02309AS 30857 PAE - DURING C-CHECK, FOUND AFT BAY NR 2 FLOOR PANEL HAS DENTS. REPAIRED IAW SRM 51-20-01. (M) 2L74 4F RTA16WE 20060103001222006010300122NM 2006 1 3 ASAA0590099 120050425A5321453A161013 FLOOR PANEL BOEING737 737990 NM FS 400-430 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02309AS 30857 PAE - DURING C-CHECK, FOUND FORWARD CARGO BAY NR 1 FLOOR PANEL EDGE CORROSION AT BS 400. REPAIRED IAW SRM 51-20-01. (M) 2L74 4F RTA16WE 20060103001372006010300137NM 2006 1 3 DL76L050795 120051216A215020224324 ACTUATOR BOEING767 767332 1382001NM LT A/C PACK MALFUNCTIONED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27193DN 28450 LT PACK TEMP LIGHT ILLUMINATED AT FL280. PACK THEN TRIPPED AND WOULD NOT RESET. T/S PER FIM FOUND LT PACK EXH ACT INOP. REPLACED ACTUATOR, OPS CHECKS NORMAL PER AMM. 2L72 4F RTA1NM 20060103001502006010300150EA 2006 1 3 QXEA200501809 120051221A2910 PRESSURE SWITCH CNDAIRCL600 CL6002C10 1390015EA HYD SYSTEM MALFUNCTIONED A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09608QX 10026 DEN - ON TAXI FOR FLIGHT 4325 RECEIVED HYD PUMP 1B CAUTION MSG. RETURNED TO THE GATE. FOUND HYD PUMP 1B LOW PRESSURE SWITCH INTERMITTENT WITH PUMP 1B AND NR 1 ENG DRIVEN PUMP 1A OFF HYD PRESSURE INDICATED 2900 PSI WITH HYD PUMP 1B CAUT MSG CYCLED HYD PUMP 1B SWITCH AND DISCONNECTED AND RECONNECTED LOW PRESSURE SWITCH, WITH NR 1B PUMP SELECTED TO ON EICAS SHOWS GREEN WITH NO CAUTION MSG RESCHEDULED IAW MEL 29-34-1. 12/22 REMOVED AND REPLACED NR 1 PUMP PRESSURE SWITCH IAW CRJ 700 AMM 29-34-01-000-801-A01 AND 29-34-01-400-801-A01, OPS CHECK AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20060103001512006010300151NE 2006 1 3 QXEA200501830 220051226A7310 ACTUATOR CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE NR 2 ENGINE LEAKING A QXEAO OTHER K FLUID LOSS NRNOT REPORTED 1 NM09602QX 10010 DEN - ON FLIGHT 4325 FOUND A FUEL LEAK ON THE RIGHT ENGINE. UPON INSPECTION FOUND FUEL LEAKING FROM NR 2 ENG SLAVE VG ACTUATOR OVERBOARD DRAIN LINE. REMOVED AND REPLACED NR 2 ENG SLAVE VG ACTUATOR IAW AMM TASK 75-30-03-000-801-A01 AND 75-30-03-400-801-A01 LEAK CK'S GOOD, OPS CK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20060103001542006010300154NM 2006 1 3 UPS05245892 120051223A2910 HYDRAULIC SYSTEM BOEING727 72731C 1384011NM HYD LEAKING A IPXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01926UP 19233 INSPECTION TYPE:N/A ATB - HYD QTY AFTER TAKEOFF WENT TO 2.0 GALS AFTER FLAP RETRACTION QTY HELD STEADY AT 2.3 GALS. FOUND ASYS QTY LOW, SERVICED TO PROPER LEVEL PER M/M 12-12-00-2. CHECKED L/E SLAT ACTUATOR AND FLAP POW'S FOR LEAKS, NONE FOUND. NO OTHER LEAKS NOTED ON A/C. RAN ENGS & CYCLED FLAPS AND FLT CONTROLS HYD REMAINED THE SAME. 2L73 4F A3WE 20060103001562006010300156NM 2006 1 3 QXEA200501848 120051228A561080260012 WINDSHIELD DHAV DHC8 DHC8202 2809007NM COCKPIT CRACKED A QXEAO OTHER O OTHER CRCRUISE 1 NM09347PH 480 LMT FLIGHT 2131 CO-PILOT WINDSHIELD CRACKED EN ROUTE. MAINTENANCE REPLACED CO-PILOTS WINDSHIELD WITH NEW FROM STOCK IAW DASH 8 200 MM TASK 56-10-11-000-801 AND 56-10-11-400-801. COMPLIED WITH SERVICE LETTER DH8-SL-51-006. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20060103001582006010300158 2006 1 3 PIDA20050201 420051223A2210 AUTOPILOT SYS BOEING737 7373G7 1384595NM B CHANNEL MALFUNCTIONED A PIDAO OTHER O OTHER DEDESCENT 1 SO05380WL 23218 B-CHANNEL AUTO PILOT CAPTURES PRESELECTED ALTITUDE 300 FEET HIGH ON DESCENT BELOW FLIGHT LEVEL 20,000. A-CHANNEL WORKS FINE. PLACED B-AUTO PILOT ON MEL 22-1. 2L72 4F RTA16WE 20060103001592006010300159NM 2006 1 3 PIDA20050202 120051224A3350900835A BATTERY PACK BOEING737 7372K5 138448XNM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05250TR 22597 OVERHEAD EMERGENCY LIGHT INOP AT ROW 2. REPLACED BATTERY PACK. OPS CHECKS GOOD PER MM 25-60-10. 2L72 4F RTA16WE 20060103001612006010300161NM 2006 1 3 2005UALA01483 120051220A3231 ROD BOEING777 777222 1385219NM PWA PW4077PW4077 NE NLG DOOR DISCONNECTED A UALAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 WP29214UA 30220 DECISION WAS MADE TO RTF AFTER CREW HEARD LOUD VIBRATION COMING FROM THE FRONT OF THE AIRCRAFT AFTER GEAR WAS RETRACTED. ON ARRIVAL FOUND LEFT AFT NOSE LANDING GEAR DOOR STRUT ROD DISCONNECTED FROM DOOR. NOSE LANDING GEAR LEFT AFT DOOR STRUT ASSY PULLED OUT AT ROD END. FINDINGS REFLECTED BROKEN SAFETY WIRE CAUSED BY OVER TWISTING. ISOLATED INCIDENT. 2L72 4F4 FRTT0001SE E46NE 20060103001622006010300162NM 2006 1 3 SWAA054158 120051228A521065C36231 SKIN BOEING737 7373H4 1384600NM L1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED SERVICE CHECK, FOUND L1 DOOR SKIN CRACKED AT LOWER AFT CORNER. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20060103001632006010300163NM 2006 1 3 SWAA054159 120051228A53306545776 SKIN BOEING737 7373H4 1384600NM BS 907 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 907, STR 4L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20060103001672006010300167NM 2006 1 3 SWAA054163 120051229A53116547959 FRAME BOEING737 7373H4 1384600NM AFT CARGO CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29326SW 23690 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT AFT CARGO DOOR CUTOUT, FWD FRAME NR 5 STOP FITTING. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20060103001682006010300168NM 2006 1 3 SWAA054164 120051228A575565C25246 CASTING BOEING737 7373H4 1384600NM RT WING SPOILER CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29331SW 23695 DURING SCHEDULED C2 CHECK, FOUND RT WING NR 5 SPOILER INBOARD ACTUATOR ATTACH POINT SUPPORT CASTING CRACKED. REMOVED AND REPLACED CASTING PER SRM. 2L72 4F RTA16WE 20060103001692006010300169NM 2006 1 3 SWAA054165 120051228A53306545774 SKIN BOEING737 7373H4 1384600NM BS 740 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29331SW 23695 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 740, STR 18R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20060103001702006010300170NM 2006 1 3 SWAA054166 120051228A3350101073 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29331SW 23695 DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY LIGHT LENS LOOSE. SECURED LENS PER MM. 2L72 4F RTA16WE 20060103001752006010300175NM 2006 1 3 SWAA054170 120051229A53206546812 WEB BOEING737 7373H4 1384600NM BS 1015 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29623SW 27933 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR WEB CRACKED AT BS 1015, RBL 39. REPAIRED SHEAR WEB PER SRM. 2L72 4F RTA16WE 20060103001782006010300178SO 2006 1 3 CHQA200500214 120051219A3350RPS1B BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11578RP7860 7860 14500865 EMERGENCY LIGHT CONTROLLED BY NR 3 BATTERY FLICKERS IN ARMED POSITION. REMOVED AND REPLACED EMERGENCY BATTERY POWER SUPPLY NR 3 IAW EMB 145 MM 33-50-04. OPS CHECK GOOD. 2L72 4T RTT00011AT 20060103001802006010300180SO 2006 1 3 CHQA200500216 120051219A3350 SWITCH EMB 145 EMB145LR 3260212SO EMERGENECY LIGHTSTICKING A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11578RP 14500865 EMERGENCY FLOOR LIGHTING BETWEEN ROWS 8-12 PULSATES ON AND OFF WITH COCKPIT SWITCH IN ARMED POSITION. FOUND TEST SWITCH STICKY, CLEANED. OPS CHECK GOOD IAW EMB 145 MM 33-50-00. 2L72 4T RTT00011AT 20060103001812006010300181SO 2006 1 3 CHQA200500217 120051223A33501317 BULB EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT BURNED OUT A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11845RP 145551 LEFT HAND FUSELAGE AFT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LEFT HAND FUSELAGE AFT EMERGENCY LIGHT BULB IAW EMB 135 MM 33-50-10. OPS CHECK GOOD. 2L72 4F RTT00011AT 20060103001822006010300182SO 2006 1 3 CHQA200500219 120051229A26123601133500230C90FIRE LOOP EMB 135 EMB135KL 3260302SO LT ENGINE FAILED A CHQAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL11381SK 145619 FLIGHT 5312 - STL-EWR - E1 FIRE DET FAIL MESSAGE APPEARED WHILE IN CRUISE. DIVERTED TO IND. MAINTENANCE REMOVED AND REPLACED LEFT HAND ENGINE FIRE LOOP IAW EMB 145 MM 26-11-01. FUNCTIONAL CHECK GOOD AT THIS TIME AND DATE. 2L72 4F RTT00011AT 20060103001842006010300184NE 2006 1 3 HAEA200500187 220051209A7200CF7002D2 ENGINE AMD FALCONFALCON20 2730103EU GE CF700 CF7002D2 30010NE LEFT FOD E HAEAA UNSCHED LANDING C F.O.D. TOTAKEOFF 1 SW05699TW103415315 50 245307 CREW PERFORMED A STATIC TO. BOTH ENGINES INDICATED NORMAL. AT 1500 AGL CREW HEARD AN ABNORMAL NOISE FROM THE LT ENGINE ACCOMPANIED BY HIGH EGT INDICATION. CREW REDUCED POWER ANDNOTED THAT THE NOISE ENDED. AN EMERGENCY WAS DECLARED AND THE ACFT RETURNED TO DEPARTURE. AC MADE AN UNEVENTFUL SINGLE ENGINE LANDING. MAINTENANCE FOUND THE ENGINE COMPRESSOR SUFFERED FOD NO DAMAGE TO THE FAN. AIRCRAFT REQURIES ENGINE CHANGE DUE TO FOD. (K) MAINTENANCE FOUND THE ENGINE COMPRESSOR SUFFERED FOD NO DAMAGE TO THE FAN. AIRCRAFT REQUIRES ENGINE CHANGE. [CLOSED] 2L72 4F4 FRTA7EU E7EA 20060103001882006010300188GL 2006 1 3 BAQ2005F00004 220051213A7210355A32070001 PUMP AEROSPAS355 AS355F2 8680812EU ALLSN 250C 250C20 03013GL GEARBOX UNKNOWN E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03942MS 5498 PUMP REMOVED IN COMPLIANCE WITH AD 03-21-09. (K) 1G72 3U3 U H11EU E4CE 20060103001922006010300192NM 2006 1 3 AMTA200501030 120051108A5320 PANEL BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE BS 1440-1560 CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11518AT 27974 AFT PIT RT TRANSITION PANEL CORROSION FS 1440 TO 1560 RBL 18-RBL24. REMOVED CORROSION IAW SRM. OUT OF LIMITS. REMOVED AND REPLACED TRANSITION PANEL RT SIDE FROM 1440-1530 IAW SRM. (K) 2L72 4F4 FRTA2NM E12EU 20060103001942006010300194NM 2006 1 3 ERA2005F00007 120051118A575385750003001 SKIN DHAV DHC8 DHC8103 1386005NM PWA PW121 PW121 52124NE LT FLAP DELAMINATED A ERAAK NONE O OTHER ININSP/MAINT 1 AL03882EA32198 098 FOUND WHILE AIRCRAFT WAS UNDERGOING C1-CHECK. DELAMINATION OF COMPOSITE MATERIAL IN THE LT OB FLAP LOWER SURFACE BETWEEN YW327.40 AND YW404.10. REPAIRED IAW RD. (K) 2H72 4T4 TRTA13NM E20NE 20060103001962006010300196EA 2006 1 3 FFS2005F00007 220051211A7323310047303 WIRE ROPE BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA LT ENGINE GOV STRETCHED G FFSAO OTHER O OTHER NRNOT REPORTED 1 AL01575X 6615 UC149 PCE32425 LT GOVERNOR WOULD NOT GOVERN AFTER TAKE-OFF, SECURED ENGINE, DECLARED EMERGENCY. RETURNED TO DEPARTURE. LANDING UNEVENTFUL. CHANGED BETA VALVE O-RINGS AND CHANGED WIRE ROPE FOR PROPELLER REVERSING LINKAGE. RE-RIGGED BETA VALVE. (K) 2L72 4T4 TRTA24CE E4EA 20060103001992006010300199EU 2006 1 3 COE2005F00004 120051209A2400111CC01A02 BPCU AEROSPATR42 ATR42300 8680920EU PWA 120 PW120 NE INOPERATIVE A COEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM13912FX14962 047 120241 AIR TURNBACK, PILOT REPORTED (CAC SOUNDED, ELEC CAP WARNING ILLUMINATED, ADI (CPL DATA INVALID) ANNUNCIATION ON T/O ROLL. MAINTENANCE REPLACED EMER BATTERY CHARGER RELAY PROTECTION UNIT (BPU). OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2H72 4T4 TRTA53EU E20NE 20060103002002006010300200NE 2006 1 3 ALG2005F00123 120051207A24356854424 SEAL SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL STARTER GEN LEAKING E ALGAK NONE K FLUID LOSS ININSP/MAINT 1 SW03741SW 760070 POST FLIGHT, AFTER LANDING, THE PILOT NOTICED OIL STREAKING DOWN ON THE LT SIDE OF THE AC AND HE ALSO FOUND LARGE AMOUNTS OF OIL INSIDE THE LEFT BAGGAGE COMPARTMENT. THE MECHANIC REMOVED AND REPLACED THE STARTER GENERATOR SEAL AND C/W WITH GROUND RUN AND LEAK CHECK AND AC WAS RETURNED TO SERVICE. (K) 1G72 3U3 U H1NE E1GL 20060103002022006010300202NM 2006 1 3 ERA2005F00004 120051124A531385310028 STRINGER DHAV DHC8 DHC8103 1386005NM PWA 120 PW120 NE LT FUSELAGE CORRODED A ERAAK NONE O OTHER ININSP/MAINT 1 AL03882EA32198 098 FOUND WHILE AIRCRAFT UNDERGOING C1-CHECK. FOUND CORROSION IN LT STRINGER 31P BETWEEN FUSELAGE STA X175.00 AND X182.00. REPAIRED IAW RD. (K) 2H72 4T4 TRTA13NM E20NE 20060103002042006010300204NM 2006 1 3 BJNA051201 120051202A3350 CONNECTOR BOEING737 737282 13844ATNM PWA JT8 JT8D17 52049NE EMERGENCY LIGHT DIRTY A BJNAO OTHER O OTHER DEDESCENT 1 WP11344TM 23044 EMERGENCY EXIT LIGHT ILLUMINATED 2 TIMES ON DESCENT. CLEANED THE CONNECTORS ON THE COCKPIT REMOVABLE EMERGENCY EXIT LIGHT, SYSTEM CHECKS NORMAL. (K) 2L72 4F4 FRTA16WE E2EA 20060103002062006010300206NM 2006 1 3 ERA2005F00005 120051123A531185320282 DOUBLER DHAV DHC8 DHC8103 1386005NM PWA PW121 PW121 52124NE FUSELAGE FRAME GOUGED A ERAAK NONE O OTHER ININSP/MAINT 1 AL03882EA32198 098 FOUND WHILE AIRCRAFT IS UNDERGOING C1-CHECK. FOUND CRACK ON THE BELTFRAME SHEAR TIE AT STA X333.30. GOUGE IN THE WAFFLE DOUBLER AT FUSELAGE STATION X333.30 AND STRINGER 6R (GOUGE CAUSED BY MAINT). REPAIRED IAW RD. (K) 2H72 4T4 TRTA13NM E20NE 20060103002072006010300207NM 2006 1 3 ERA2005F00008 120051117A534385410318101 FRAME DHAV DHC8 DHC8103 1386005NM PWA PW121 PW121 52124NE FUSELAGE CHAFED A ERAAK NONE O OTHER ININSP/MAINT 1 AL03882EA 098 FOUND WHILE AIRCRAFT UNDERGOING C1-CHECK. CHAFE DAMAGE TO LT MLG IB ATTACH FITTING. REPLACED LT IB ATTACH FITTING IAW SRM. (K) 2H72 4T4 TRTA13NM E20NE 20060103002122006010300212NM 2006 1 3 ERA2005F00001 120051026A533085711118 SKIN DHAV DHC8 DHC8103 1386005NM PWA 120 PW120 NE RT WING GOUGED A ERAAK NONE O OTHER ININSP/MAINT 1 AL03881EA31543 233 FOUND WHILE AIRCRAFT UNDERGOING C1 CHECK, AWC 19438, FOUND GOUGE IN RT TOP SKIN AT STRINGER 3R BETWEEN FRAME YW207, STA YW137. REPAIRED IAW RO. (K) 2H72 4T4 TRTA13NM E20NE 20060103002142006010300214NM 2006 1 3 ERA2005F00006 120051119A5720857110069 PLATE DHAV DHC8 DHC8103 1386005NM PWA PW121 PW121 52124NE RT LADDER CRACKED A ERAAO OTHER O OTHER ININSP/MAINT 1 AL03882EA32198 098 FOUND WHILE AIRCRAFT UNDERGOING C1-CHECK IN THE RT LADDER PLATE AT (RT) YW137, FORWARD OF STRIGER 6. REPAIRED IAW RD. (K) 2H72 4T4 TRTA13NM E20NE 20060104000012006010400001NM 2006 1 4 CIHA200579003 120051229A540069169771 ATTACH ANGLE BOEING727 727225 1384077NM NR 1 ENGINE CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15679MG 22557 NR 1 ENGINE ATTACH ANGLE, P/N 69-16977-1, CRACKED AT HOLE-P. EDDY CURRENT INSP VERIFIED. REMOVED & REPLACED NR 1 ENG ATTACH ANGLE P/N:69-16977-1 PER ACD (BACDRW) 65-72772. 2L73 4F A3WE 20060104000052006010400005WP 2006 1 4 DHL2005803512 120051116A27505751153505 DRIVE LINK DOUG DC8 DC873 302199CWP TE FLAPS CRACKED A DHLAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SO01803DH82180 46123 RIGHT OUTBOARD FLAP DRIVE LINK ASSY AT STA XF 219.498 HAS THREE CRACKS: I/B LUG J-POINT 3.500 INCH LENGTH CRACK, O/B LUG J-POINT 0.500 INCH LENGTH CRACK AND REAR LUG J-POINT 3.000 INCH LENGTH CRACK. REMOVED AND REPLACED RT OUTBOARD FLAP DRIVE LINK ASSY AT STA XF 219.498 IAW MM 27-51-4 PG 201-204. REFER TO NR 038928 FOR OPS CHECK. 2L74 4F RT4A25 20060104000062006010400006WP 2006 1 4 DHL2005803513 120051120A534736575041 SEAT TRACK DOUG DC8 DC873 302199CWP CABIN DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 COCKPIT F/E'S AFT SEAT TRACK HAS ELONGATED HOLES. REMOVED AND REPLACED F/E'S AFT SEAT TRACK IAW SRM 51-3-0 PG 1, SRM 51-3-1 PG 2A (TORQUE). REFER TO JC 8-25-40-002 FOR OPS CHECK. 2L74 4F RT4A25 20060104000072006010400007WP 2006 1 4 DHL2005803514 120051117A5753 PANEL DOUG DC8 DC873 302199CWP LT TE FLAP WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 LT INBOARD FLAP UPPER PANEL PLATING WORN 2 INCHES APPROX, STA XW 104.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 1. REMOVED DAMAGED PANEL PLATING IAW SRM 57-1-0, SRM 51-1-21. FABRICATED NEW PLATING (AL 2024T3 0.025) AND BONDED FINGER DOUBLER (AL 2024T3 0.020) IAW SRM 57-7-1 FIG 1 ITEM-A & L. STUCK BOTH PARTS IAW SRM 51-1-9. CLEANED, TREATED AND PRIMED AREA AND INNER SIDE OF NEW PANEL PLATING IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW PANEL PLATING IAW SRM 51-1-21. 2L74 4F RT4A25 20060104000082006010400008WP 2006 1 4 DHL2005803515 120051107A53403779659U501 FITTING DOUG DC8 DC873 302199CWP BS 902-909 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 MAIN CARGO COMPT INTERIOR SPLICE FITTING CRACKED 2 INCHES STA 902.000 - STA 909.000 L-6R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW SPLICE FITTING IAW SRM 51-1-20D (HI-LOK) AND NEW PLI WASHER IAW SRM 51-1-23 PG 1. TORQUED IAW SRM 51-3-1 PG 2A (HI-LOKS). 2L74 4F RT4A25 20060104000132006010400013SO 2006 1 4 1488123005 120051230A5100 INSULATION GULSTMG1159 GIV 3980115SO CARGO BAY MELTED E N93AA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO13490QS2759 1488 DESCENDING THRU 20,000FT AFT BAG SMOKE LIGHT CAME ON FOLLOWED BY AMBER FLOOR OVERHEAT. F/A REPORTED SMELL OF SMOKE AND HEAT. 2L72 4F RTA12EA 20060104000142006010400014NM 2006 1 4 0501816316 120051221A3350 LIGHT BOEING747 747451 1384940NM CABIN LOOSE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01676NW 33002 ROW 9-12 LT EMERGENCY PATHWAY LIGHT OUT. RESECURED LT EMERGENCY PATHWAY LIGHT AT ROW 9. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L74 4F RTA20WE 20060104000152006010400015NM 2006 1 4 0501826314 120051222A3350 LAMP BOEING747 747451 1384940NM EMERGENCY LIGHT INOPERATIVE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01674US 30269 DOOR 5R EMERGENCY LIGHT INOP. RELAMPED LIGHT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L74 4F RTA20WE 20060104000172006010400017NM 2006 1 4 SWAA060014 120051230A53206582671 WEB BOEING737 7375H4 138449DNM CABIN FLOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29511SW 24188 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE BEADED WEB CRACKED AT BS 664, LBL 42. REPAIRED WEB PER SWA EA. 2L72 4F RTA16WE 20060104000182006010400018NM 2006 1 4 SWAA060015 120051230A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM BS 787 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29623SW 27933 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, RBL 8, WL 148. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20060104000222006010400022NM 2006 1 4 SWAA060019 120051230A53116517684 FRAME BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT R1 DOOR CUTOUT, FWD FRAME NR 3 STOP FITTING. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20060104000232006010400023NM 2006 1 4 SWAA060020 120051230A53146545866 KEELBEAM BOEING737 7373Q8 1384670NM BS 542 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED 1/2D CHECK, FOUND RT KEEL BEAM LOWER CHORD CRACKED AT BS 542. REPAIRED KEEL BEAM PER SRM. 2L72 4F RTA16WE 20060104000272006010400027NM 2006 1 4 SWAA060024 120051231A5314144A7155U4 SPLICE BOEING737 7377H4 1384404NM BS 535 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29714CB 27848 DURING SCHEDULED MV2 CHECK, FOUND KEEL BEAM SPLICE PLATES CORRODED AT BS 535. REMOVED AND REPLACED SPLICE PLATES PER SWA EA. 2L72 4F RTA16WE 20060104000282006010400028 2006 1 4 SWAA060025 420051231A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29769SW 30588 R1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20060104000302006010400030EU 2006 1 4 0501773240 120051216A3350NWAD321440 BATTERY PACK AIRBUS320 A320212 3930322EU CABIN INOPERATIVE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01340NW 372 EMERGENCY LIGHT TEST FAILED. REMOVED AND REPLACED BATTERY PACK LOCATED UNDER 12WL PER MM 33-51-38. OPS CHECKED GOOD. 2L72 4F RTA28NM 20060104000332006010400033NM 2006 1 4 SWAA060002 120051228A53306545774 SKIN BOEING737 7373H4 1384600NM BS 767 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29329SW 23693 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 19L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20060104000392006010400039NM 2006 1 4 SWAA060008 120051230A3350207377 LENS BOEING737 7377H4 1384404NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29407WN 29817 DURING SCHEDULED RON CHECK, FOUND EEPLS LENS MISSING AT FWD END. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20060104000452006010400045SO 2006 1 4 507512092005 120051209A5100 INSULATION GULSTMGV GV 3980116SO FUSELAGE ODOR E N93AO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO13518QS 5075 ACRID ODOR FROM LEFT PILLAR BETWEEN LT WINDSHIELD AND SIDE WINDOW. 2L72 4F RTA12EA 20060104000462006010400046SO 2006 1 4 64712072005 120051207A24211159SCAV5003 IDG GULSTMGV GV 3980116SO LEFT FAILED E N93AA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 SO13511QS4341 647 LEFT ENGINE IDG FAILED IN FLIGHT, ATTEMPTED APU START WAS UNSUCESSFUL. 2L72 4F RTA12EA 20060104000472006010400047WP 2006 1 4 0501661243 120050618A2611 SMOKE DETECTOR DOUG DC10 DC1030 3023501WP CARGO BAY MALFUNCTIONED A NWAAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL01243NW 48315 AFT CARGO FIRE WARNING LIGHT BEGAN TO FLICKER EN ROUTE. INTERMITTENT LIGHT OCCURRED WITH INCREASED FREQUENCY. FOLLOWED COM PROCEDURE AND DISCHARGED BOTH BOTTLES. FLIGHT DIVERTED TO THR AND LANDED WITHOUT INCIDENT. NO EVIDENCE OF FIRE FOUND. AFT CARGO COMPT FIRE EXT SYS PLACARD INOP AND FLIGHT CONTINUED TO AMS. REPLACED AFT CARGO COMPT SMOKE DETECTORS AND FIRE BOTTLES. TESTS GOOD. 2L73 4F A22WE 20060104000482006010400048WP 2006 1 4 0501679617 120051121A5311 DOOR FRAME DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01617NW 47235 DURING L-CHECK FOUND CRACK IN AFT LOWER CORNER OF FORWARD SERVICE DOOR FRAME. REPAIRED PER EA 96-204718. 2L72 4F A6WE 20060104000502006010400050WP 2006 1 4 0501849611 120051227A21312075301AB CONTROLLER DOUG DC9 DC932 3022066WP NR 2 FAILED A NWAABA EMER. DESCENT UNSCHED LANDING SJ AFFECT SYSTEMS WARNING INDICATION CRCRUISE 1 GL01611NA 47435 DURING CRUISE FLIGHT AT FL340 THE AIRCRAFT SUDDENLY STARTED TO LOSE CABIN PRESSURIZATION VERY QUICKLY. THE ORANGE -CABIN PRESS AUTO FAIL- LIGHT DID NOT ILLUMINATE AND NO MENTION OF RED -CABIN PRESS- LIGHT STATUS. CREW PERFORMED A RAPID DESCENT TO 10,000 FEET AND SWITCHED TO MANUAL PRESSURE CONTROL. MAXIMUM ALTITUDE THE CABIN REACHED WAS 12,500 FEET AND THE MASKS DID NOT DEPLOY. THE FLIGHT DIVERTED TO SDF AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE NR 2 CABIN PRESSURE CONTROLLER HAD FAILED. REPLACED CONTROLLER. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20060104000512006010400051NM 2006 1 4 C1HA200581019 120051215A541069169771 ATTACH ANGLE BOEING727 7272S7 138407ZNM NR 1 PYLON CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15681CA 22020 WHILE PERFORMING AD 2005-19-24, FOUND NR 1 ENG PYLON FIREWALL ATTACH ANGLE P/N 69-16977-1 CRACKED NEXT TO MOUNT FITTING. REMOVED AND INSTALLED ATTACH ANGLE P/N 69-16977-1 REF BOEING PRINT 65-72772. 2L73 4F A3WE 20060104000522006010400052 2006 1 4 CHQA200500218 420051228A3140701700082430 COMPUTER EMB 135 EMB135KL 3260302SO FAILED A CHQAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL11371SK1034010340 145535 CRUISE ALTITUDE, IC1 FAN FAILURE. IMMEDIATELY, EXPERIENCED A FAILURE OF AUTOPILOT & YAW DAMPER, ASSOCIATED MESSAGES PRESENTED ON EICAS. F/O TOOK MANUAL CONTROL, RAN CHECKLIST FOR AUTOPILOT FAILURE. ALSO, FAILURE OF PITCH TRIM MAIN & BACKUP SYS. EICAS SHOWED BOTH FAILED. RAN QRH PROCEDURES, STARTED DESCENT. CHECKLIST STATES, PULL F11 & C24 CIRCUIT BREAKERS AT SAFE ALTITUDE. AT FL280, PULLED & RESET BREAKERS, THEN RESET PITCH TRIM MAIN & BACKUP SYSTEMS. SYSTEMS SEEMED TO WORK. F/A PREPARED CABIN FOR POSSIBLE DIVERSION. MX ADVISED, NO HISTORY OF OCCURRENCE ON THIS A/C. SYSTEM FAILED AGAIN. DECLARED EMERGENCY, LANDED UNEVENTFULLY. MX FOUND IC600 FAN FAILED. REMOVED & REPLACED IC600, OPS CHECK GOOD. 2L72 4F RTT00011AT 20060104000542006010400054SO 2006 1 4 14361216052 120051216A325051051 SERVO VALVE GULSTMG1159 GIV 3980115SO NLG STEERING FAILED E N93AK NONE O OTHER TXTAXI/GRND HDL 1 SO13436QS4427 1436 NOSE STEERING FAILED ON LANDING. 2L72 4F RTA12EA 20060104000552006010400055NM 2006 1 4 0501726301 120051215A3350 POWER SUPPLY BOEING747 747451 1384940NM EMERGENCY LIGHT MALFUNCTIONED A NWAAO OTHER O OTHER NRNOT REPORTED 1 GL01661US 23719 REPORTED IN DTW, TWO RIGHT AFT LOWER EXTERIOR LIGHTS WERE OUT. DTW MAINTENANCE REMOVED AND REPLACED R3 OVERHEAD POWER SUPPLY. OPS CHECKED GOOD AND RETURNED TO SERVICE. 2L74 4F RTA20WE 20060104000562006010400056SO 2006 1 4 5075120605 120051206A3097 WIRE GULSTMGV GV 3980116SO WINDSHIELD BURNED E N93AO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO13518QS83 5075 CREW SMELLED A SULFER BURNING ODOR AND A PUFF OF SMOKE AT WINDSHIELD. MAINTENANCE FOUND LOOSE CONNECTION AT WINDSHIELD HEAT TERMINAL BLOCK. 2L72 4F RTA12EA 20060104000612006010400061SO 2006 1 4 5075121805 120051218A56101159SCB51021 WINDSHIELD GULSTMGV GV 3980116SO COCKPIT FAILED E N93AA UNSCHED LANDING O OTHER CRCRUISE 1 SO13518QS110 5075 LT WINDSHIELD SMOKED THEN CRACKED. 2L72 4F RTA12EA 20060104000622006010400062NM 2006 1 4 C1HA200593005 120051222A541069169771 ATTACH ANGLE BOEING727 727212 138407GNM NR 1 PYLON CRACKED A C1HAO OTHER O OTHER ININSP/MAINT 1 GL15293AS 21348 WHILE PERFORMING AD 2005-19-24, FOUND NR 1 ENG PYLON CORD ANGLE CRACKED FWD PYLON FIREWALL P/N 69-16977-1. REMOVED CRACKED ATTACH ANGLE AND INSTALLED NEW ATTACH ANGLE 69-16977-1 REF BAC BWG 65-72772. 2L73 4F A3WE 20060104000642006010400064EU 2006 1 4 SA05130 120051225A3350321431 BATTERY PACK AIRBUSA319 A319112 3930323EU EMERGENCY LIGHTSDISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19764US 1369 TPA - FOUND THE MID-CABIN, LEFT EMERGENCY LIGHTS INOPERATIVE DURING INSPECTION. MAINTENANCE REPLACED THE BATTERY PACK IN THE MID-CABIN, LEFT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20060104000662006010400066NM 2006 1 4 05FDEA04408 120051222A5753 FLAP TRACK BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 N0108, CORROSION ON UPPER SURFACE OF NR 6 FLAP TRACK AROUND BOTH AFT MOUNT BOLT HOLES AND CNT OB MOUNT BOLT HOLE. COMING REPLACED NR 6 FLAP TRACK IAW WC27X5708-03 2L73 4F4 FRTA3WE E2EA 20060104000682006010400068CE 2006 1 4 DXTA200501147 120051216A492038635041 SEAL CESSNA560 560XL 2076702CE STARTER GEN LEAKING E DXTAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL07687QS 5605187 WITH APU ON FOR 15 MIN, CAB IN FILLED WITH SMOKE. OIL SMELL TO IT. BLEED AIR ON, TEMPS NORMAL ON APU. CABIN SEEMED TO NOT BE COOLING EFFECTIVELY. - FOUND APU STARTER/GENERATOR GARLOCK SEAL LEAKING OIL INTO ENCLOSURE - REPLACED SEAL IAW HONEYWELL RE100 (XL) MM 49-10-00. ALSO FOUND AREA AROUND FILLER PORT APPEARS TO HAVE OIL SPILLED INTO APU AIR INLET. BOROSCOPE APU NO INTERNAL LEAKS NOTED. REPLACED COALSCER SOCK AND CLEANED ECU & DUCTING TO REMOVE OIL IAW ALIED SIGNAL MM IV SCREW 4-7 OPS/LEAK CHECKS GOOD. 2L72 4F RTA22CE 20060104000692006010400069NM 2006 1 4 DXTA200501148 120051217A4990 OIL SYSTEM GULSTM200 200 4500308NM APU OVERSERVICED E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL07730QS 120 AT ABOUT 300' AFTER DEPARTURE SMOKE STARTED ENTERING COCKPIT & CABIN FROM ENVIRONMENTAL SOURCES. SMOKE HAD OILY ODOR & STRONG OILLY ODOR SENSED AROUND LT ENG. CHECKED LT & RT ENGINES FOR OIL LEAKS, NONE NOTED. CHECKED ENGINE BLEED AIR & ECS DUCTS FOR EXCESSIVE OIL , NO EXCESSIVE OIL. FOUND RT ENGINE OIL RESERVOIR OVERSERVICED & SERVICED IT TO PROPER LEVEL. CONDUCTED ENGINE RUNS AT HIGH PWR SETTINGS WITH ECS ON. NO ABNORMAL INDICATIONS AND NO SMOKE IN CABIN OR COCKPIT MX IAW G200 MM TSK 12-17-00-612-801. 2L72 4F RTA53NM 20060104000702006010400070CE 2006 1 4 DXTA200501149 120051218A3240CV02259 CHECK VALVE CESSNA500 560CESSNA 2076750CE BRAKES MALFUNCTIONED E DXTAO OTHER S AFFECT SYSTEMS LDLANDING 1 GL07392QS 5600429 BRAKES ON FO'S SIDE VERYN MUSHY AND REQUIRE ABNORMAL PRESSURE TO ACTIVATE. BRAKES WILL NOT HOLD PLANE DURING STATIC DEPARTURE. - BLED BRAKES AND INSTALLED A NEW CHECK VALVE IAW CH. 32-42-00 OF THE CE 560 ULTRA M.M. OPS CHECK AND LEAK CHECK GOOD. 2L72 4F RTA22CE 20060104000712006010400071NM 2006 1 4 DXTA200501152 120051218A3230203470060700 CONTROL MODULE AMD FALC50FALCON2000 2730170NM NLG MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07253QS 153 ON GEAR RETRACTION NOSE WHEEL RETRACTED, MAIN GEAR DID NOT RETRACT , MAIN GEAR DOOR LIGHTS REMAINED ON, "AUTO SLATS" LIGHT ILLUMINATED, NOSE WHEEL STEERING MINELCOS DISPLAYED RED AND NOSE WHEEL STEERING WAS INOPERATIVE ON LANDING. - REPLACED R/H NOSE GEAR PROX SWITCH WITH SERVICEABLE UNIT ADJUSTED LEFT NOSE GEAR PROX SWITCH. REPLACED #1 AND #2BSCU WITH REPAIRED UNIT I.A.W F2000 M.M. 32-600, AND MRI. 51-50-05. ACCOMPLISHED OPS CHECK OF NOSE STEERING I.A.W F2000 MM 32-501-37-502 ACCOMPLISHED OPS CHECKS OF BSCU'A IAW F2000 M.M. 32-446 2K73 4F RTA50NM 20060104000722006010400072WP 2006 1 4 UPS05845899 120051219A57115597841501 SPAR DOUG DC8 DC873F 302199FWP LT WING XW736.5 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 INSPECTION TYPE:SV LT WING REAR SPAR UPPER CAP AFT FLANGE IS CRACKED APPROX. 7".(XW736.5). REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW SAA SK 894-928513. 2L74 4F RT4A25 20060104000732006010400073NM 2006 1 4 UPS05M45894 120051013A5347AFA7789542 SEAT TRACK DOUG MD11 MD11F 3023600NM BS 1964, CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01281UP 48538 INSPECTION TYPE:C RT CURVED SEAT TRACK STN 1964, RBL 107.25 EXFOLIATION CORROSION, RT CURVED S/TRACK ST1964 RBL 107.25 EXFOLIATION CORROSION REMOVED PER SRM 53-7 0-00 FIG 3 VOL I REV37 MAT ORIG THK 0.145" AND MAT REMOVED 0.075" FOUND EXCEED LIMIT, NEW S/TRACK REPAIR SPLICE HAT AND SPLICE PLATE BET STA1831-2 007 RBL107.25 INSTALLED PER SRM 51-31-01 VOL II REV37 AND SRM 53-70-00 FIG 1 VOL I REV 37. 2L73 4F RTA22WE 20060104000742006010400074NM 2006 1 4 UPS05M45895 120051013A5347AFA7789547 SEAT TRACK DOUG MD11 MD11F 3023600NM BS 1964 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01281UP 48538 INSPECTION TYPE:C LT CURVED SEAT TRACK ST 1964 LBL 107.25 EXFOLIATION CORROSION. LT CURVED S/TRACK STA1964 LBL107.25 EXFOLIATION CORROSION REMOVED PER SRM53-70 -00 FIG3 VOL I REV 37 MAT ORIG THK 0.145" AND MAT REMOVED 0.070" FOUND EXCEED LIMIT PER SRM 53-70-00 FIG3 VLO I REV37. NEW S/TRACK REPAIR SPLICE HAT AND SPLICE BET ST1831-2007 LBL107.25, INSTALLED PER SRM51-31-01 VOL II REV37 AND SRM53-70-00 FIG 1 VOL I REV 37. 2L73 4F RTA22WE 20060104000752006010400075NM 2006 1 4 DHL05740019 120051022A3260 SWITCH BOEING727 7272Q9 138448MNM MLG DOOR FAILED A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01740DH YELLOW (L GEAR DOOR) LIGHTON S/O PANEL FAILS TO ILLUMINATE ON GEAR RETRACT OR EXTENTION BUT DOES TEST.NO OTHER GEAR INDICATION ARE ABNORMAL. REMOVED AND REPLACED LT LANDING GEAR DOOR WARNING SWITCH IAW B-727 M/M 32-61-11.OPS CHECK GOOD P/N 1EN161-RB1 2L73 4F RTA3WE 20060104000762006010400076EU 2006 1 4 RAIA00512047 120051228A3350 LAMP JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT INOPERATIVE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03573HK 41092 PRE FLIGHT 5435 - STL - EMERGENCY LIGHT OUT AT 2A. MAINTENANCE RELAMPED EMERGENCY LIGHT AT 2A. 2L72 4T RTA41NM 20060104000782006010400078EA 2006 1 4 SWIA200516040 120051220A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07937SW 7735 1 OF 5 LIGHT BULBS INOP ON FLOOR LEVEL EMERGENCY FLOOD LIGHT. REPAIRED WIRING TO SECTION OF INOP LIGHTS. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20060104000792006010400079SO 2006 1 4 SWIA200516041 120051223A3350 SIGN EMB 120 EMB120 3260201SO CABIN MISSING A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07563SW 120338 ILLUMINATE EXIT SIGN (LOWER) AT 6A MISSING. REPLACED LIGHT ASSY. AS REQUIRED. OPERATIONAL CHECKS GOOD. 2L72 4T RTA31SO 20060104001012006010400101GL 2006 1 4 CIEA200500017 320051203A6140503890571 TACH GENERATOR BEECH 200 200BEECH 1152920CE PWA PT6 PT6A41 52043EA HARTZLHCB3T HCB3TN3 GL LT PROPELLER DEFECTIVE E CIEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM035ST 774 BB489 BUA22883 SHORTLY AFTER TAKEOFF, THE PILOT NOTICED THE LT PROP RPM DROPPING. THE OTHER ENGINE INSTRUMENTS DID NOT SEEM TO BE AFFECTED, BUT THE PILOT THOUGHT THE ENGINE WAS LOOSING POWER. THE AIRCRAFT RETURNED AND LANDED AT THE SAME AIRPORT AS THE TAKEOFF. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE ENGINE WAS OPERATED ON THE GROUND FOR TROUBLESHOOTING AND THE PROPELLER WAS INDICATING 9100 RPM AT IDLE. MAINTENANCE TROUBLESHOOTING AND FOUND THE PROP TACH GENERATOR TO BE DEFECTIVE. 1L72 4T4 T A24CE E4EA 6 CP15EA 20051230000412005123000041EA 2005 12 30 VNAA0512001 120051201A5700 STRUCTURE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE LT WING TIP LIGHTNING STRIKEA VNAAK NONE O OTHER ININSP/MAINT 1 GL05710PS 10167 EVIDENCE OF LIGHTNING DAMAGE WAS FOUND ON THE LT WINGLET TIP TRAILING EDGE DURING THE 50 HOUR SERVICE CHECK. MAINTENANCE COMPLIED WITH A LIGHTNING STRIKE INSPECTION. NO FURTHER DAMAGE WAS FOUND. A TEMPORARY REPAIR WAS PERFORMED ON THE LT WINGLET TIP TRAILING EDGE IAW BOMBARDIER REO 670-57-31-002. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20051230000452005123000045EA 2005 12 30 VNAA0512004 120051201A5245 DOOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE A/C DOOR OPEN A VNAAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL05256PS 7937 THE GROUND AIR CONNECTION DOOR WAS FOUND OPEN AFTER THE FLIGHT. MAINTENANCE INSPECTED AND FOUND THE DOOR HINGE CRACKED. THE DOOR WAS REMOVED AND REPLACED WITH A SERVICEABLE UNIT. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20051230000482005123000048EA 2005 12 30 VNAA0512010 120051208A3010GG670800135 SENSOR CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE ANTI ICE SYSTEM FAILED A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL05718PS 10175 DURING CLIMBOUT THE LT WING A/I, RT WING A/I, & WING A/I SNSR CAUTION MESSAGES ILLUMINATED. THE CREW FOLLOWED THE QRH AND RETURNED TO CLT. MAINTENANCE REMOVED & REPLACED THE LEFT WING OUTBOARD ANTI-ICE SENSOR (MT33). THE WING ANTI-ICE SYSTEM OPERATIONALLY CHECK GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20051230000552005123000055SO 2005 12 30 RAIA00512023 120051223A783083990137 SWITCH EMB 145 EMB145LR 3260212SO THRUST REVERSER INTERMITTENT A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03850HK7591 145003 REVERSER NR 1 DISAGREE MESSAGE ON TAKEOFF. MAINTENANCE REMOVED AND REPLACED UPPER OUTBD STOW SWITCH. 2L72 4T RTT00011AT 20051230000572005123000057SO 2005 12 30 RAIA00512027 120051226A3350BA50933901 BATTERY PACK EMB 145 EMB145EP 3260221SO EMERGENCY LIGHT DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03826HK 145016 5497 - STL - CABIN EMERGENCY ESCAPE PATH LIGHTING WILL NOT TEST. MAINTENANCE REPLACED ESCAPE PATH LIGHTING BATTERY PACK. 2L72 4F RTT00011AT 20051230000582005123000058SO 2005 12 30 RAIA00512025 120051223A3397 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT LOOSE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03818HK 145059 MX - STL - FLOOR EMERGENCY EXIT STRIP LIGHT AT OVERWING EMERGENCY EXIT INOP. MAINTENANCE RE-SECURED ELECTRICAL CONNECTOR TO FLOOR STRIP. 2L72 4T RTT00011AT 20051230000602005123000060NM 2005 12 30 QXEA200501837 120051221A21608201003005 ECU BOMBDRDHC8 DHC8402 1390042NM CABIN TEMP MALFUNCTIONED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09405QX1020 4047 PDX FLIGHT NR 2311, FLIGHT COMP PACK HOT CAUTION LIGHT ILLUMINATED ON PUSHBACK. MAINTENANCE PERFORMED FAULT RETRIEVAL IN CDS, FOUND FAULT CODE 3701 (FD COMP OLT TEMP) IN HISTORY (RECENT) C/W Q400 FIM TASK 21-60-00-810-816, STEP 1-4 AND 5A(D). REMOVED AND REPLACED BOTH LT AND RT OUTLET TEMP SENSORS IAW TASK 21-51-91-000-801 AND 21-51-91-400-801. REMOVED AND REPLACED ECS ECU IAW MM TASK 21-61-01-000-801 AND 21-61-01-400-801. OPS CHECK GOOD. C/W OPS TEST OF THE ECS TEMP CONTROL IAW TASK 21-61-00-710-803. OPS CHECK GOOD. NO FURTHER FAULTS OR CAUTION LIGHTS NOTICED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051230000692005123000069NM 2005 12 30 QXEA200501819 120051206A5347 SEAT TRACK BOMBDRDHC8 DHC8402 1390042NM BS 572-591 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09403QX 4037 PDX: LT INBOARD SEAT TRACK HAS PITS AND CORROSION IN CENTER CHANNEL BETWEEN STA X572.25 AND X591.25. MAINTENANCE REPAIRED IAW RD 8-53-884, NDTM PART 6, TASK 51-00-01-250-801 AND RD 8/4-53-884 GENERAL NOTE 6. 2H72 4T RTA13NM 20051230000702005123000070NM 2005 12 30 QXEA200501820 120051206A5347 SEAT TRACK BOMBDRDHC8 DHC8402 1390042NM BS 602-625 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09403QX 4037 PDX: LT INBOARD SEAT TRACK HAS PITS AND CORROSION IN CENTER CHANNEL BETWEEN STA X602.5 AND X625.25. MAINTENANCE REPAIRED IAW NDTM PART 6, TASK 51-00-01-250-801 AND RD 8/4-53-884. 2H72 4T RTA13NM 20051230000822005123000082NM 2005 12 30 QXEA200501822 120051203A3210 YOKE BOMBDRDHC8 DHC8402 1390042NM MLG CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09403QX 4037 PDX: RT MLG YOKE (H MEMBER) INBOARD LOWER LEG IS CHAFING AGAINST THE YOKE TO SHOCK STRUT BONDING STRAP NEAR THE LUBED GREASE FITTING. MAINTENANCE REPAIRED IAW CMM 32-11-04, SRM 51-21-10, SRM 51-25-10 AND SRM 51-25-15. 2H72 4T RTA13NM 20051230000842005123000084NM 2005 12 30 QXEA200501838 120051221A213092146A010401 CONTROLLER BOMBDRDHC8 DHC8402 1390042NM CABIN PRESSURE MALFUNCTIONED A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09405QX7308 4047 PDX FLIGHT NR 2311, UNABLE TO PRESSURIZE CABIN IN AUTO. ATTEMPTED MANUAL ALSO UNABLE TO PRESSURIZE (SEEMED TO START TO WORK BUT NOT VERY WELL). RETURNED TO FIELD. MAINTENANCE REMOVED AND REPLACED CABIN PRESSURE CONTROLLER IAW 21-31-06-000-801 AND 21-31-06-400-801. C/W OPS CHECK OF THE PRESSURIZATION CONTROL IN MANUAL MODE IAW MM TASK 21-31-00-710-803. OPS CHECK GOOD. ALSO C/W FUNCTIONAL TEST OF THE PRESSURIZATION CONTROL IAW 21-31-00-720-801. FUNCTIONAL CHECK GOOD. PRESSURIZED AIRCRAFT 3 TIMES IN MANUAL MODE. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051230000862005123000086NM 2005 12 30 QXEA200501845 120051226A2497 CONNECTOR BOMBDRDHC8 DHC8402 1390042NM BATTERY DIRTY A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09417QX 4086 FCA FLIGHT NR 2396, AFTER START, DURING TAXI, MAIN BATTERY LOAD FLUCTUATED BETWEEN -0.20 AND +0.26, CYCLED BETWEEN THE VALUES EVERY 10-20 SECONDS. MAINTENANCE CLEANED CONNECTIONS TO SHUNT 2431-R4. GROUND RAN AIRCRAFT. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051230000922005123000092NM 2005 12 30 AWXA200501610 120051227A56105893543129 WINDSHIELD BOEING737 73733A 1384673NM COCKPIT CRACKED A AWXAA UNSCHED LANDING O OTHER CRCRUISE 1 WP28174AW19464 23633 DURING CRUISE, DEPARTED FROM DFW EN ROUTE TO LAS, AT FL 340 CREW REPORTED CAPT OUTER WINDSHIELD CRACKED. CREW DIVERTED & LANDED WITHOUT FURTHER INCIDENT. MX R & R CAPT WINDSHIELD. OPS CHECKS GOOD. HIGH TIME WINDOW. WINDOW WAS SCRAPPED AT VENDOR. 2L72 4F RTA16WE 20051230000972005123000097NM 2005 12 30 QXEA200501840 120051223A6123 PROPELLER BOMBDRDHC8 DHC8402 1390042NM FEATHERING SYS MALFUNCTIONED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09403QX 4037 SEA FLIGHT NR 2316: NR 2 ENGINE TAKES 32-34 SECONDS TO TRANSITION FROM FEATHER TO DISC. ALL OTHER INDICATIONS NORMAL. MAINTENANCE C/W THE FUNCTIONAL TEST OF THE PROPELLER TIME TO UNFEATHER ON NR 2 ENGINE PER Q400 AMM TASK 61-20-00-720-801. TIME TO UNFEATHER IS 24 SECONDS, WITHIN LIMITS. NO OTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20051230001022005123000102NM 2005 12 30 SWAA054128 120051227A53206546568 TEE FITTING BOEING737 7373Q8 1384670NM BS 1016 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED 1/2D CHECK, FOUND BS 1016 AFT PRESSURE BLKHD UPPER T-CHORD CORRODED AT RBL 24.75. REMOVED AND REPLACED T-CHORD PER SRM. 2L72 4F RTA16WE 20051230001092005123000109NM 2005 12 30 SWAA054135 120051223A3350PH22300L LIGHT BOEING737 7377H4 1384404NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29709SW 27843 EEPLS STRIP COVER LOOSE BETWEEN ROW 6 DEF TO ROW 8 DEF. REMOVED AND REPLACED EEPLS STRIP PER MM. 2L72 4F RTA16WE 20051230001112005123000111NM 2005 12 30 SWAA054137 120051221A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29718SW 27852 DURING SCHEDULED RON CHECK, FOUND EEPLS STRIP DAMAGED. REMOVED AND REPLACED STRIP PER MM. 2L72 4F RTA16WE 20051230001132005123000113NM 2005 12 30 SWAA054139 120051222A3350MS155721 BULB BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29738CB 27870 DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT LIGHTS INOP AT ROW 8 DEF AND ROW 10 DEF. RELAMPED LIGHTS PER MM. 2L72 4F RTA16WE 20060103000222006010300022NM 2006 1 3 SWAA054141 120051224A3350MS155721 BULB BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29766SW 29806 DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20060103000232006010300023EA 2006 1 3 COMA0560746 120051222A7930601509197 TRANSDUCER CNDAIRCL600 CL6002B19 1900309EA LT ENGINE FAULTY A COMAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SO01473CA10110 7668 FLIGHT 4993 - EN ROUTE LGA-LEX RECEIVED A LEFT ENGINE OIL PRESSURE DROP ASSOCIATED WITH AN OIL PRESSURE WARNING MESSAGE, CREW DECLARED AN EMERGENCY, DIVERTED TO CKB AND PERFORMED IFSD OF THE LEFT ENGINE. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE LEFT ENGINE OIL PRESSURE TRANSDUCER. 2L72 4F RTA21EA 20060103000242006010300024EA 2006 1 3 COMA0560747 120051222A5610NP13932111 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A COMAA UNSCHED LANDING O OTHER CRCRUISE 1 SO01518CA6935 5824 7816 FLIGHT 5701 - PILOT'S WINDSHIELD SHATTERED. REPLACED WINDSHIELD. 2L72 4F RTA21EA 20060103000302006010300030EA 2006 1 3 COMA0570127 120051222A2741C13045BA04 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA AVIONICS BAY FAULTY A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01368CA8273 10075 FLIGHT 4985 - AFTER TAKEOFF FROM ORD WITH A/P ENGAGED, RECEIVED A STAB CHANNEL 2 WARNING. REPLACED THE NR 2 SSCU. 2L72 4F RTA21EA 20060103000352006010300035 2006 1 3 SWAA054114 420051226A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20060103000362006010300036NM 2006 1 3 SWAA054115 120051227A335090083 BATTERY PACK BOEING737 7373H4 1384600NM EMERGENCY LIGHTSINOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED RON CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20060103000372006010300037NM 2006 1 3 SWAA054116 120051226A2560P4010021 BATTERY BOEING737 7373H4 1384600NM FLASHLIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29391SW 27378 DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN INBD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2L72 4F RTA16WE 20060103000452006010300045NM 2006 1 3 SWAA054123 120051226A53306545774 SKIN BOEING737 7373Q8 1384670NM BS 727E CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29687SW 23388 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 24R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20060103000462006010300046NM 2006 1 3 SWAA054124 120051226A57536546430 SKIN BOEING737 7373Q8 1384670NM RT WING FOREFLAPDELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29687SW 23388 DURING SCHEDULED C4 CHECK, FOUND RT WING INBD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM. 2L72 4F RTA16WE 20060103000492006010300049NM 2006 1 3 SWAA054127 120051227A53126516300 BULKHEAD BOEING737 7373Q8 1384670NM BS 178 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED AT BL 0, WL 189. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20060103000502006010300050CE 2006 1 3 DXTA200501146 120051215A323399121114 ACTUATOR CESSNA500 560CESSNA 2076750CE MLG INOPERATIVE E DXTAO OTHER J WARNING INDICATION APAPPROACH 1 GL07327QS8724 5600327 RIGHT GREEN LANDING GEAR LIGHT DID NOT ILLUMINATE WHEN GEAR EXTENDED. GEAR APPEARED DOWN VISUALLY. ALSO ROTARY TEST, GEAR HORN TEST INDICATED FAULTY LIGHT. HOWEVER, AFTER DOING GEAR BLOW DOWN PROCEDURE LIGHT CAME ON. T/S FOUND ACTUATOR BAD. REMOVED AND REPLACED ACTUATOR WITH RECERTIFIED UNIT IAW 560 MM 32-31-04, 32-01-00 AND 32-11-01. OPS CHECK NORMAL. 2L72 4F RTA22CE 20060103000522006010300052CE 2006 1 3 DXTA200501144 120051215A3010 ANTI-ICE SYSTEM CESSNA750 750 2076810CE FAILED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07913QS 7500113 ANTI-ICE ON BEFORE TAKEOFF RECEIVED NO COLD MESSAGES POWER TO TAKEOFF DETENT GOT 'SLAT COLD' MSG AND 'HOT STAB' MSG. ABORTED, SHUT DOWN ANTI-ICING AND ALLOWED TO COOL. RESET ANTI-ICING POWER UP. SAME MESSAGES REPEATED +GOT 'WING ANTI-ICE HOT R' MSG. PERFORMED OPS CK OF ALL ANTI-ICE SYSTEMS IAW CE 750 MM CH 30-00-00. ALL SYSTEMS OPS CK GOOD. ALL ANTI-ICE SENSORS FOUND TO BE WITHIN SERVICEABLE LIMITS IAW CH 30-16-00. 2L72 4J RTT00007WI 20060103000562006010300056EA 2006 1 3 ASOA051061 120051204A5347 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA BS 559 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27882AS 7503 DURING A C-CHECK IN MCN, THE CARGO COMPARTMENT FLOOR TRACKS AT FS 559 PLUS 96, RBL 27 AND RBL 9, WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CARGO COMPARTMENT FLOOR SEAT TRACKS AT FS 559 PLUS 96, RLB 27 AND RBL 9, IAW CRJ 200 SRM 51-40-00. (M) 2L72 4F RTA21EA 20060103000622006010300062EA 2006 1 3 ASOA051068 120051206A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS INOPERATIVE A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27850AS 7355 DURING CLIMB-OUT FROM ATL-ALB, THE CREW ATTEMPTED TO RETURN FLAPS FROM EIGHT DEGREES TO ZERO DEGREES, WHEN AN AMBER FLAPS FAIL CAUTION MESSAGE, WITH THE FLAPS REMAINING AT 8 DEGREES WAS RECEIVED. THE CREW COMPLIED WITH THE QRH AND DECLARED AN EMERGENCY. THE AIRCRAFT RETURNED TO ATL WHERE IT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE RIGHT BPSU. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060103000752006010300075NM 2006 1 3 SWAA054149 120051228A53116547952 FRAME BOEING737 7375H4 138449DNM AFT CARGO CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29526SW 26568 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT AFT CARGO DOOR CUTOUT, AFT FRAME NR 4 STOP FITTING. REPAIRED FRAME PER BFG ER. 2L72 4F RTA16WE 20060103000792006010300079NM 2006 1 3 SWAA054153 120051228A55516551524 FITTING BOEING737 7373H4 1384600NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29622SW 27932 DURING SCHEDULED D-CHECK, FOUND LT & RT HORIZONTAL STAB FITTING LUG FACES CORRODED. REPAIRED LUG FACES PER SRM. 2L72 4F RTA16WE 20060103000832006010300083NM 2006 1 3 SWAA054157 120051227A53306545776 SKIN BOEING737 737317 138447PNM BS 941 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 941, STR 21R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20060103000842006010300084NM 2006 1 3 SWAA054142 120051228A33501010427 COVER BOEING737 7373H4 1384600NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 EMERGENCY EXIT BULLNOSE LIGHT COVER MISSING AT ROW 18. INSTALLED COVER PER MM. 2L72 4F RTA16WE 20060103001242006010300124NM 2006 1 3 ASAA0590101 120050425A5320143A7501162 FLOOR SUPPORT BOEING737 737990 NM FS 500A CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02309AS 30857 PAE - FOUND DURING C-CHECK, FOUND FORWARD CARGO BY FLOOR SUPPORT PLATE CORRODED. REPAIRED IAW SRM 53-00-53. (M) 2L74 4F RTA16WE 20060103001322006010300132NM 2006 1 3 ASAA0540661 120051117A531165C329621 FRAME BOEING737 7374Q8 138447QNM FS 727G CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND CORROSION ON FRAME UPPER CHORD. REPAIRED PER B737-400 SRM 51-70-11. (M) 2L72 4F RTA16WE 20060103001362006010300136EA 2006 1 3 ASOA051030 120051113A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA BS 484 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27914EV 7752 DURING A C-CHECK IN TUS, THE CLIP ON THE INTERCOSTAL AT STA 484, RBL 27, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIP ON THE INTERCOSTAL, AT STATION 484, RBL 27, IAW ASA EC REO 601R-53-41-059. (M) 2L72 4F RTA21EA 20060103001482006010300148NM 2006 1 3 PIDA20050203 120051227A5241 SKIN BOEING737 7373G7 1384595NM L2 DOOR CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05390WL 23219 L2 DOOR SKIN CRACKED IN THE LOWER AFT CORNER OF THE TOP HINGE CUTOUT. REPAIRED DAMAGE AREA PER SRM 52-00-01. 2L72 4F RTA16WE 20060103001532006010300153NM 2006 1 3 DLM88050797 120051217A4900 APU DOUG MD88 MD88 3023688NM PWA JT8 JT8D* NE APU BAY CONTAMINATED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27913DE14332 49956 P80534 AIR TURNBACK, LT AFT LAV SMOKE ALARM WITH FUMES. PERFORMED OPN 5088 AND FOUND APU INLET CONTAMINATED WITH GLYCOL. PERFORMED OPN 5090 - ALT DUCT BURNOUT. ALSO CLEANED A LOT OF GLYCOL FROM 48 SECTION. RAN PACKS, NO SMOKE PRESENT. 2L72 4F4 FRTA6WE E2EA 20060103001652006010300165 2006 1 3 SWAA054161 420051228A25656949956 CABLE BOEING737 7373H4 1384600NM L2 DOOR SLIDE MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29325SW 23689 DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE LATCH CABLE ASSY MISROUTED. REROUTED CABLE ASSY PER MM. 2L72 4F RTA16WE 20060103001662006010300166NM 2006 1 3 SWAA054162 120051228A53306545765 SKIN BOEING737 7373H4 1384600NM BS 520 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29325SW 23689 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 16L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20060103001712006010300171NM 2006 1 3 SWAA054167 120051229A3350D71701100 BATTERY PACK BOEING737 7377H4 1384404NM EMERGENCY LIGHT NO TEST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29416WN 32453 DURING SCHEDULED HC1 CHECK, CABIN EMERGENCY EXIT LIGHTS FAILED TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2L72 4F RTA16WE 20060103001722006010300172NM 2006 1 3 SWAA054168 120051229A53306545774 SKIN BOEING737 7375H4 138449DNM BS 737D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29502SW 24179 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 737D, STR 23L. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20060103001762006010300176NM 2006 1 3 SWAA054171 120051229A53306545774 SKIN BOEING737 7373Y0 1384671NM BS 740D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29664WN 23495 DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 740D, STR 21L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20060103001932006010300193NM 2006 1 3 BJNA051101 120051109A3210 LANDING GEAR BOEING737 737282 13844ATNM PWA JT8 JT8D17 52049NE UNKNOWN A BJNAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP11233TM 23043 AFTER TAKEOFF, RETRACTED LANDING GEAR AND 3 RED LIGHTS REMAINED ILLUMINATED. CYCLED LANDING GEAR DOWN AND UP, 3 GREEN LIGHTS WHEN DOWN, 3 RED LIGHTS WHEN UP. LANDED WITH 3 GREEN LIGHTS. PERFORMED LANDING GEAR ACCY MODULE TEST IAW AMM, COULD NOT DUPLICATE ON GROUND. JACKED AIRCRAFT PERFORMED GEAR REACTION TEST. NO FAULTS FOUND. (K) 2L72 4F4 FRTA16WE E2EA 20060103002052006010300205NM 2006 1 3 ERA2005F00003 120051024A573085711069 PLATE DHAV DHC8 DHC8103 1386005NM PWA 120 PW120 NE LADDER CRACKED A ERAAO OTHER O OTHER ININSP/MAINT 1 AL03881EA31543 233 FOUND WHILE AIRCRAFT UNDERGOING C1-CHECK, AWC 19419. FOUND CRACK IN RT IB LADDER PLATE BETWEEN STRINGER 4 AND 6 AT WING STA YW137. REPAIRED IAW RD. (K) 2H72 4T4 TRTA13NM E20NE 20060103002082006010300208NM 2006 1 3 ERA2005F00009 120051108A534385312779001 PLATE DHAV DHC8 DHC8103 1386005NM PWA PW121 PW121 52124NE TRUNNION CORRODED A ERAAK NONE O OTHER ININSP/MAINT 1 AL03881EA 233 FOUND WHILE AIRCRAFT UNDERGOING C1-CHECK, AWC 19810. CORROSION ON LT NLG TRUNNION PLATE BEYOND MFG LIMITS. REPLACED LT NLG TRUNNION PLATE IAW DWG. (K) 2H72 4T4 TRTA13NM E20NE 20060103002102006010300210NM 2006 1 3 BJNA051202 120051207A33506104791 POWER SUPPLY BOEING737 737282 13844ATNM PWA JT8 JT8D17 52049NE EMERGENCY LIGHT INOPERATIVE A BJNAK NONE L NO TEST ININSP/MAINT 1 WP11789TM 23046 LT OVERWING EXTERIOR EMERGENCY EXIT LIGHT, INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY. (K) 2L72 4F4 FRTA16WE E2EA 20060103002112006010300211CE 2006 1 3 TIM2005F00014 120051110A573011412004873 SKIN BEECH 1900 1900C 1154161CE PWA PT6 PT6A60A 52043NE LT WING DAMAGED E TIMAK NONE O OTHER ININSP/MAINT 1 NM07154GA32854 UB25 THE FASTENERS WERE DISCOVERED TO BE WORKING INTO THE LOWER SKIN WHILE DOING AN INSPECTION OF THE WING. IT APPEARS THAT THIS WAS CAUSED BY NORMAL WING FLEX IN THIS AREA. (K) 2L72 4T4 TRTA24CE E4EA 20060104000022006010400002NM 2006 1 4 0501856303 120051230A2612 CIRCUIT CARD BOEING747 747451 1384940NM CARGO FIRE WARN MALFUNCTIONED A NWAAF ACTIVATE FIRE EXT. N FALSE WARNING APAPPROACH 1 GL01663US 23818 FLIGHT CREW GOT CARGO FIRE WARNING ON APPROACH. WARNING BRIEFLY WENT OFF THEN CAME ON AGAIN. CREW FIRED BOTTLE AND AIRCRAFT LANDED AT DESTINATION WITHOUT INCIDENT. FIRE DEPARTMENT RESPONDED AND USED SENSOR TO DETERMINE NO FIRE WAS PRESENT. REMOVED AND REPLACED CIRCUIT CARD AND SPENT FIRE BOTTLES. AIRCRAFT RETURNED TO SERVICE. 2L74 4F RTA20WE 20060104000032006010400003NM 2006 1 4 C1HA200594012 120051223A3233 ACTUATOR BOEING727 727290 138408WNM LT MLG MALFUNCTIONED A C1HAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15294AS 22146 LEFT MAIN GEAR DID NOT RETRACT ON TAKEOFF, BOTH GREEN LIGHT DOWN AND LOCK LIGHTS AND RED DOOR LIGHTS REMAIN ILLUMINATED, RED DISAGREE LIGHT WAS ALSO ILLUMINATED. REMOVED AND REPLACED LT MLG LOCK MECHANISM PER JOB STATUS MM REF 32-32-51, ALL OPS CHECKS NORMAL. REMOVED AND REPLACED LT MLG LOCK ACTUATOR PER JOB STATUS AND MM 32-32-61. 2L73 4F A3WE 20060104000112006010400011EU 2006 1 4 0501863276 120051229A5210FE240004 CYLINDER AIRBUS320 A320212 3930322EU 2R DOOR LEAKING A NWAAK NONE O OTHER ININSP/MAINT 1 GL01376NW1043110431 01812 DURING LINE CHECK FOUND DOOR 2R ASSIST BOTTLE LEAKING INTERNALLY. DOOR 2R SECURED AND LOCKED FOR FERRY FLIGHT. FERRIED AIRCRAFT FROM DCA TO DTW. REMOVED AND REPLACED DOOR 2R EMERGENCY CYLINDER AND DAMPER PER AMM 52-13-14 PG 401 & 501. 2L72 4F RTA28NM 20060104000212006010400021NM 2006 1 4 SWAA060018 120051229A53306545768 SKIN BOEING737 7373A4 1384585NM BS 356 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29678AA 23290 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 356, STR 18R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20060104000262006010400026NM 2006 1 4 SWAA060023 120051230A3350311500 LENS BOEING737 7373Q8 1384670NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 FWD CABIN BULLNOSE LENS LOOSE. SECURED LENS PER MM. 2L72 4F RTA16WE 20060104000292006010400029NM 2006 1 4 SWAA060026 120051231A7312118411934 HEAT EXCHANGER BOEING737 7377H4 1384404NM NR 1 ENGINE FAULTY A SWAAE ENGINE SHUTDOWN K FLUID LOSS DEDESCENT 1 SW29782SA 29808 DIVERSION/INFLT SHUTDOWN/DECLARED EMERGENCY. NR 1 ENGINE LEAKING FUEL. NR 1 ENGINE SHUTDOWN. REMOVED AND REPLACED NR 1 ENGINE FUEL/OIL HEAT EXCHANGER PER MM. 2L72 4F RTA16WE 20060104000342006010400034NM 2006 1 4 SWAA060003 120051228A53306545774 SKIN BOEING737 7373H4 1384600NM BS 780 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29329SW 23693 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 780, STR 19L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20060104000532006010400053NM 2006 1 4 0501736301 120051216A3350 POWER SUPPLY BOEING747 747451 1384940NM EMERGENCY LIGHT MALFUNCTIONED A NWAAO OTHER O OTHER NRNOT REPORTED 1 GL01661US 23719 REPORTED IN DTW, THE FLOOR TRACK EMERGENCY LIGHTS ON THE UPPER DECK FORWARD HALF SEATS 72K TO 74A GOES ON FOR THREE SECONDS, THEN GOES OUT. DTW MAINTENANCE REMOVED AND REPLACED POWER SUPPLY. OPS CHECKED GOOD AND RETURNED TO SERVICE. 2L74 4F RTA20WE 20060104000572006010400057SO 2006 1 4 CHQA200500213 120051217A3350 GROUND WIRE EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT DIRTY A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11844RP 145620 EMERGENCY LIGHTS WOULD NOT COME ON. PER WD 33-50-50, PERFORMED ELECTRICAL WIRE TEST IAW EMB 135 WD 20-20-03. FOUND GOOD VOLTAGE AND CONTINUITY ON CONNECTORS FOR BATTERIES AND INVERTER. THE GROUNDING WAS POOR. CLEANED GROUND GS0580C. LIGHTING SYSTEM OPS CHECKS GOOD. 2L72 4F RTT00011AT 20060104000582006010400058NM 2006 1 4 0501806313 120051221A3350 WIRE HARNESS BOEING747 747451 1384940NM EMERGENCY LIGHTSBROKEN A NWAAO OTHER L NO TEST NRNOT REPORTED 1 GL01673US 30268 EMERGENCY LIGHTS 31K, 32K FROM 3L TO 3R SECTION OF TRACK LIGHTS OUT. DTW MAINTENANCE FOUND HARNESS BROKEN. REMOVED AND REPLACED HARNESS. OPERATION CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L74 4F RTA20WE 20060104000592006010400059SO 2006 1 4 1436121605 120051216A325051507 MANIFOLD GULSTMG1159 GIV 3980115SO STEER BY WIRE FAILED E N93AK NONE O OTHER TXTAXI/GRND HDL 1 SO13436QS1446 1436 STEER BY WIRE FAILED ON LANDING. 2L72 4F RTA12EA 20060104000632006010400063EU 2006 1 4 0501783228 120051216A3350321454 POWER SUPPLY AIRBUS320 A320211 3930320EU EMERGENCY LIGHT INOPERATIVE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01328NW 298 EMERGENCY EXIT LIGHTS IN REAR GALLEY INOP. REMOVED AND REPLACED POWER SUPPLY 13WL AND BATTERY. OPS CHECKS GOOD. 2L72 4F RTA28NM 20060104000802006010400080SO 2006 1 4 SWIA200516042 120051224A5210 TORQUE TUBE EMB 120 EMB120ER 3260203SO PAX DOOR BINDING A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07566SW 120341 FLIGHT ATTENDANT REPORTS MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE. REPLACED INTERMEDIATE TORQUE TUBE AND BUSHING ON MAIN CABIN DOOR IAW AMM 52-11-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20060104000822006010400082EA 2006 1 4 SWIA200516044 120051224A2751 SENSOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07913SW 7597 "FLAPS DEGRADED" STATUS MESSAGE. REPLACED SKEW DETECTION SENSOR AND OPERATIONAL CHECK GOOD IAW 27-51-15. 2L72 4F RTA21EA 20060104000842006010400084EA 2006 1 4 SWIA200516046 120051226A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07982SW 7956 AFT MOST OVERHEAD EMERGENCY FLOOD LIGHT OUT. RELAMPED AFT MOST OVERHEAD EMERGENCY CABIN FLOODLIGHT. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20060104000862006010400086EA 2006 1 4 SWIA200516048 120051227A2797 PIN CNDAIRCL600 CL6002B19 1900309EA CONNECTOR LOOSE A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TOTAKEOFF 1 NM07592SW 7279 STAB TRIM CH 1 STATUS MESSAGE OCCURRED TWICE, ONCE ON CLIMB-OUT, ONCE ON TAXI IN. REPLACED HSTA AND MCU IAW AMM 27-40-00, 27-42-05 AND RECONNECTED LOOSE PINS AT P268. OPERATIONAL CHECK GOOD, PN: 7062-3, SN OFF: 934, PN: 8396-3 SN OFF: 794. 2L72 4F RTA21EA 20060104000892006010400089SW 2006 1 4 HDCA107099 120051201A6210206015001115 BLADE CLARK 1000 1000CLARK 2230102SW MAIN ROTOR CRACKED B HDCAO OTHER O OTHER NRNOT REPORTED 1 SW03 3116 DURING ROUTINE MAINTENANCE, DISCOVERED CRACK ON MAIN ROTOR BLADE AT BLADE STATION 41.5 EXTENDING CHORDWISE FROM TRAILING EDGE ON BOTH UPPER AND LOWER SKINS ACROSS FINGERS ON TRAILING EDGE EXTENDING 6.3750 INCHES THEN FOLLOWING FINGERS OB, SPANWISE, 5 INCHES. SEPARATION OCCURED AS LIGHT CAN BE SEEN THROUGH CRACK. MAIN ROTOR BLADE SCRAPPED AND REPLACED WITH A NEW PART. 1Q71 3R 2A6 20060104000942006010400094CE 2006 1 4 73127 120050923A30973023141 TERMINAL PWC 1900D BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE GAS GENERATOR CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07127ZV 114065 UE127 114065 DURING A ROUTINE INSPECTION, INSPECTION PERSONNEL FOUND THE RT ENGINE BETA CABLE FRONT PUSH PULL TERMINAL CRACKED AROUND THE ENTIRE CIRCUMFERENCE. IT IS UNKNOWN HOW THIS CONDITION OCCURRED. PARTS HISTORY RESEARCH SHOWED NO RECENT USAGE. MORE INFORMATION WILL BE AVAILABLE AT A LATER DATE. 2L72 4T4 TRTA24CE E26NE 20060104000952006010400095CE 2006 1 4 1050921026071 120051020A5313129440000209 STRINGER BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE BS 456 CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07146ZV UE146 STRINGER 12 AT FS 456 RT CRACKED. MAINTENANCE REPAIRED STRINGER WHILE AIRCRAFT WAS IN STRUCTURAL REPAIR. 2L72 4T4 TRTA24CE E26NE 20060104000962006010400096CE 2006 1 4 74809 120051219A261222412886 FIRE LOOP BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE LT NACELLE FAILED P AMWAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 CE07176YV UE176 WHILE IN ROUTE, THE LT T-HANDLE ILLUMINATED. CREW COMPLIED WITH EMERGENCY CHECKLIST AND DIVERTED DECLARED EMERGENCY AND LANDED SAFELY WITH NO FURTHER INCIDENT. IT WAS THEN FERRIED, MAINTENACE REMOVED AND REPLACED LT FWD FIRE LOOP ASSY. 2L72 4T4 TRTA24CE E26NE 20060104000972006010400097CE 2006 1 4 74784 120051218A3240 BRAKE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE MLG WEAK P AMWAK NONE O OTHER TXTAXI/GRND HDL 1 CE07176YV UE176 WHILE TAXING IN, THE CREW NOTICED THE BRAKES WERE SPONGEY. THE AIRCRAFT WAS THEN FERRIED AND MAINTENANCE BLED THE BRAKES. NO PARTS USED. 2L72 4T4 TRTA24CE E26NE 20060104000992006010400099CE 2006 1 4 74806 120051219A3110 DISPLAY BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA COCKPIT FAILED P AMWAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE07142ZV UE142 CAPT EHSI WENT BLANK AND CREW SMELLED AN ODOR THEY DETERMINED IT TO BE ELECTRICAL RELATED. AIRCRAFT LANDED WITH NO FUTHER INCIDENT. MAINTENANCE REPAIRED WIRES. NO PARTS WERE USED. 2L72 4T3 TRTA24CE E2NE 20060104001002006010400100CE 2006 1 4 73843 120051101A3240 BRAKE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE MLG WEAK A AMWAK NONE O OTHER LDLANDING 1 CE07143YV UE143 UPON LANDING, CAPT'S NOTED BOTH BRAKES WEAK WHEN APPLIED. CREW TAXIED TO THE GATE WITH NO FURTHER INCIDENT. PHONED MAINTENANCE CONTROL, OUTSIDE MAINTENANCE WAS CALLED AND BRAKES WERE BLED. OPS CHECK NORMAL. THEREFORE NO PARTS WERE USED. 2L72 4T4 TRTA24CE E26NE 20060104001052006010400105SW 2006 1 4 ALG2005F00106 120051119A7700 WARNING SYSTEM BELL 206 206L4 1182110SW ALLSN 250C 250C30P 03013GL ENGINE FALSE INDICATIONE ALGAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW03170A1 52063 DURING START TOT PEAKED AT 770 FOR ONE SECOND. MAINTENANCE WAS NOTIFIED. PERFORMED INSPECTION OF TOT INSTRUMENT IAW MM AND FOUND INSTRUMENT SERVICEABLE. PERFORMED HOT END INSPECTION IAW MM AND FOUND NO DEFECTS. REINSTALLED SAME AS REMOVED AND RELEASED AIRCRAFT FOR SERVICE. (K) 1G71 3U3 UNCH2SW E1GL 20060104001092006010400109NE 2006 1 4 2005F00111 220051209A7314025323150 PUMP CESSNA208 208B 2073701CE PWA PT6 PT6A114 52043NE MCAULY3DF36CB3DF36C526 GL FUEL SYS CORRODED E K NONE O OTHER ININSP/MAINT 1 WP17969FE 2951 208B0092 17219 981511 PRECAUTIONARY INSPECTION OF THE FUEL PUMP DRIVE SPLINE IAW MM, FUEL PUMP COUPLING IN-SITU INSPECTION 73-10-02 PAGE 210, PARAGRAPH 8D, MAINTENANCE FOUND THE FUEL PUMP DRIVE SPLINE SEVERELY CORRODED AND DAMAGED TO THE POINT OF NEAR FAILURE. THE FUEL PUMP ASSEMBLY WAS REPLACED WITH A FRESH OVERHAULED UNIT AND THE AIRCRAFT RETURNED TO SERVICE. 1H71 3T3 T A37CE E4EA 5 C 20060104001102006010400110NE 2006 1 4 2005F00112 220051209A7314025323150 PUMP CESSNA208 208B 2073701CE PWA PT6 PT6A114 52043NE MCAULY3DF36CB3DF36C526 GL FUEL PUMP CORRODED E K NONE O OTHER ININSP/MAINT 1 WP17772FE 4666 1637 208B0268 19142 970839 PRECAUTIONARY INSPECTION OF THE FUEL PUMP DRIVE SPLINE IAW MM, FUEL PUMP COUPLING IN-SITU INSPECTION 73-10-02 PAGE 210, PARAGRAPH 8D, MAINTENANCE FOUND THE FUEL PUMP DRIVE SPLINE SEVERELY CORRODED. THE FUEL PUMP ASSEMBLY WAS REPLACED WITH A FRESH OVERHAULED UNIT AND THE AIRCRAFT RETURNED TO SERVICE. 1H71 3T3 T A37CE E4EA 5 C 20060104001112006010400111NE 2006 1 4 2005F00113 220051209A7314025323150 SPLINE CESSNA208 208B 2073701CE PWA PT6 PT6A114 52043NE MCAULY3DF36CB3DF36C526 GL FUEL PUMP CORRODED E K NONE O OTHER ININSP/MAINT 1 WP17772FE 4666 1637 208B0268 19142 970839 PRECAUTIONARY INSPECTION OF THE FUEL PUMP DRIVE SPLINE IAW MM, FUEL PUMP COUPLING IN-SITU INSPECTION 73-10-02 PAGE 210, PARAGRAPH 8D, MAINTENANCE FOUND THE FUEL PUMP DRIVE SPLINE SEVERELY CORRODED. THE FUEL PUMP ASSEMBLY WAS REPLACED WITH A FRESH OVERHAULED UNIT AND THE AIRCRAFT RETURNED TO SERVICE. 1H71 3T3 T A37CE E4EA 5 C 20060104001122006010400112SW 2006 1 4 ALG2005F00121 120051206A2821AC9985F10 FILTER BELL 214 214ST 1182106SW GE CT7TS CT72A 30030NE FUEL SYS FAILED E ALGAA UNSCHED LANDING O OTHER CLCLIMB 1 SW03391AL 28103 ON TAKEOFF, NR 2 ENGINE FUEL FILTER LIGHT CAME ON, AND THE PILOT LANDED THE AC. THE MECHANIC REMOVED AND REPLACED NR 2 ENGINE FUEL FILTER ELEMENT, GROUND RUN AND LEAK CHECKED IAW MM, AC WAS RETURNED TO SERVICE. (K) 2G72 4U4 U H10SW E8NE 20060104001142006010400114NE 2006 1 4 PNSA051106 220051129A7200 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE MISRIGGED A PNSAC ABORTED TAKEOFF JR WARNING INDICATION PARTIAL RPM/PWR LOSS TOTAKEOFF 1 AL03685PA 340B212 WHILE SETTING CTOT TO 80 PERCENT POWER AUTOCOARSEN ARMED LIGHT WENT FROM HIGH TO LOW WITH A POWER FLUCTUATION. FLIGHT CREW REDUCED POWER AND ABORTED TAKEOFF. MAINTENANCE FOUND MANUAL ENGINE RIGGING TO BE INTERFERING WITH AUTOCOARSEN ELECTRICAL SETTINGS. ENGINE MANUAL RIGGING WAS CORRECTED AND AIRCRAFT RETURNED TO SERVICE. 2L72 4T4 TRTA52EU E8NE 20060104001172006010400117GL 2006 1 4 YTRR107130 220051115A73202307031 HMU BELL 407 407 1182206SW ALLSN 250C 250C47B GL ENGINE INOPERATIVE B YTRRO OTHER J WARNING INDICATION CRCRUISE 1 SW03309RL 53092 RESTART FAULT LIGHT ILLUMINATED DURING FLIGHT. UPON LANDING AND SHUT-DOWN, FADEC FAULT LIGHT ALSO ILLUMINATED. REPLACED HMU. 1G71 3U3 UO H2SW E1GL 20060104001222006010400122CE 2006 1 4 4510311242005 120051124A7830 SWITCH LEAR 45 45LEAR 5170805CE GARRTTTFE731TFE7312 01518WP THRUST REVERSER INTERMITTENT E J7SAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SW05412FX 103 LT T/R RED CAS ILLUMINATED ON TAKEOFF ROLL (INDICATES T/R UNLOCK), ON TAXI BACK CAS TURNED YELLOW. MX CHECKED SWITCHES, FOUND S4 TO BE INTERMITTENT. CLEANED SWITCH ACTUATOR, PERFORMED OPERATIONAL CHECK OF SYSTEM , NO FURTHER DEFECTS NOTED. 2L72 4F4 FRTT00008WIE6WE 20060104001252006010400125CE 2006 1 4 BSYA200500031 120051219A5210 DOOR BEECH 58 58 1152740CE CONT O520 IO520* 17032SO CREW OPEN E BSYAA UNSCHED LANDING O OTHER CLCLIMB 1 GL073695V TH1183 ON TAKEOFF OUT, CREW DOOR CAME OPEN AND PILOT RETURNED TO BASE SECURED DOOR THEN TOOK OFF TO CONTINUE FLIGHT. 1L72 3O3 O 3A16 E5CE 20060104001272006010400127CE 2006 1 4 BSYA200500030 120051212A37008250155DP SEAL BEECH 58 58 1152740CE CONT O520 IO520CB 17032SO VACUUM PUMP SLIPPED E BSYAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL07400RP TH319 299491R ON TAKEOFF, PILOT NOTICED SMOKE COMING FROM LT ENGINE, PILOT ELECTED TO RETURN TO DEPARTURE. MAINTENANCE FOUND THAT THE NEWLY INSTALLED VACUUM PUMP SEAL HAD SLIPPED DURING INSTALLATION. REMOVED AND REPLACED SEAL, OPS CHECKS GOOD. 1L72 3O3 O 3A16 E5CE 20060104001292006010400129CE 2006 1 4 JBGA200500008 120051217A773066005042 ACCELEROMETER LEAR 60 60LEAR 5170707CE PWA 305 PW305A 52128NE LT ENGINE FALSE INDICATIONE JBGAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07460AN 127 PCECAO185 ON TAKEOFF, LT ENGINE VIBRATION ANALYZER ACCELEROMETER SHOWED A LIGHT AND PILOT ABORTED TAKE OFF. FALSE INDICATION WAS CAUSED BY A BAD ACCEROMETER, REMOVED AND REPLACED DEFECTIVE ACCEROMETER OPS. CHECKS GOOD. 2L72 4F4 FRTA10CE E35NE 20060104001322006010400132NM 2006 1 4 AT0500049 120051207A78307150021505 THRUST REVERSER BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE RT INOPERATIVE A ZZDAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO15936AT 55058 ENG RH REV FAULT ANNUN IN FLIGHT FOLLOWED BY AMBER RT U/L LIGHT COMPLETED PROCEDURE IAW QRH. REMOVED AND REPLACED RT THRUST REVERSER REF MM 78-30. OPS CK OK FOR SERVICE. 2L72 4F4 FTRA6WE E00061EN 20060104001342006010400134NM 2006 1 4 05FDEA04175 120051208A5315 FLOORBEAM BOEING727 727 UTILSYSNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 FORWARD CARGO COMPARTMENT STA BS 620 BOTTOM SURFACE OF FLOORBEAM UPPER TEE CAP HAS CORROSION AROUND SCREW HOLES LBL50 TO RBL50. REMOVED DAMAGED SECTION OF TEE CAP AT STA BS 620 BETWEEN LBL45 AND RT CUSP. FABRICATED NEW TEE CAP, SPLICES, SHIMS: ALODINED AND PRIMED; AND INSTALLED REPAIR PARTS IAW STANDARD REWORK DRAWING MM. SR27-53-034E SRM 51-10-2. THIS IS A MAJOR REPAIR, MECH NR 6709 AND QC298. REFERENCE N00713. 2L73 4J4 FRTA3WE E2EA 20060104001362006010400136NM 2006 1 4 05FDEA04174 120051208A5315 FLOORBEAM BOEING727 727* NM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 AFT PIT MAIN DECK FLOORBEAM HAS CORROSION AT FASTENER CLIP AT STA, BS 950F, LBL21.0. REMOVED CORROSION IAW SRM 51-10-6 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1 FIGURE 4. REMOVED AND REPLACED FLOORBEAM UPPER TEE CAP SECTION FROM LBL8 TO LBL70 IAW STANDARD REWORK DRAWING SR27-53- 034E. THIS IS A MAJOR REPAIR SIGNED BY MECH NR 1269 AND QC352. REF N00557. 2L73 4F4 FRTA3WE E2EA 20060104001382006010400138NM 2006 1 4 05FDEA04407 120051222A5311 FRAME BOEING727 727100 1384036NM PWA JT8 JT8D7B 52053NE STR25LT, 27LT,BSDENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 AFT CARGO COMPARTMENT, FRAME IS DENTED BETWEEN STR 25 LT AND 27 LT BS 1050 ON IB FLANGE. REPAIRED DENTED FRAME BETWEEN STR 25LT AND 27LT, BS 1050 ON I/B FLANGE IAW SRM 51- 40-3. 2L73 4F4 FRTA3WE E2EA 20060104001402006010400140NM 2006 1 4 05FDEA04405 120051222A5311 FRAME BOEING727 727100 1384036NM PWA JT8 JT8D7B 52053NE BS 1010 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 AFT CARGO COMPARTMENT, FRAME IS DENTED BETWEEN STR 24 LT AND 27 LT BS 1010 ON IB FLANGE. REPAIRED PER 51-40-03 & 53-10-1. 2L73 4F4 FRTA3WE E2EA 20060104001422006010400142NM 2006 1 4 05FDEA04177 120051208A5521 RIB BOEING727 727200 138407ENM PWA JT8 JT8D9A 52048NE ELEVATOR GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 WHILE WORKING CARD NR N00763 FOUND RT NR 5 ELEVATOR HINGE, SUPPORT RIB L/E GOUGED. REPAIRED RIB PER FED EX EA 7-5510-91427. 2L73 4F4 FRTA3WE E2EA 20060104001432006010400143NM 2006 1 4 05FDEA04318 120051215A5101 REPAIR BOEING727 727200 138407ENM PWA JT8 JT8D9A 52048NE ZONE 200 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 REPAIR LOCATED AT STA 303.9 STRINGER 15-L REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. ITEM NR 4, VISUALLY INSPECTED REPAIR AT STA 303.9 STRINGER 15-L. FOUND TO BE IAW SB 727-53A0198 AND EA 7-5330-92599 (FUSELAGE SKIN REPAIR DOUBLER HAS OVRSIZED FASTENERS - AD 98-11-03- R1) WITH RESPECT TO SIZE, SHAPE, SPACING, AND EDGE DISTANCE. THIS REPAIR WAS NOT REMOVED FOR THIS INSPECTION. THIS IS A MINOR REPAIR. 2L73 4F4 FRTA3WE E2EA 20060105000022006010500002NM 2006 1 5 2005UALA01234 120051107A2130720737 RELIEF VALVE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE BS 1016 FAILED A UALABA EMER. DESCENT UNSCHED LANDING O OTHER CRCRUISE 1 WP29340UA50860 24244 EXPERIENCED A RAPID DECOMPRESSION. ACCOMPLISHED SAFETY RELIEF VALVE TEST PER MM 21-32-21 AND TEST FAILED. REPLACED VALVE AND PERFORMED CABIN DEPRESSURIZATION AND ALTITUDE WARNING CHECKS PER MM 05-51-81, SYSTEM OPS GOOD. 2L72 4F4 FRTA16WE E2GL 20060105000042006010500004SO 2006 1 5 CHQA200500222 120051230A2131M835366022M RELAY EMB 135 EMB135LR 3260305SO ANTI ICE SYS STICKING A CHQAB EMER. DESCENT J WARNING INDICATION CLCLIMB 1 GL11844RP 145620 FLT 6387 CVG-MSY - AT APPROX 14,000 FT, EN COUNTERED MODERATE RIME ICING. ICING SYS INITIALLY OPERATED NORMAL. RECEIVED FOLLOWING EICAS MESSAGES: ICE COND A/I INOP, WING A/I FAIL, BLEED 2 VALVE FAIL, PACK 2 FAIL, BLEED VALVE 2 CLSD, PACK 2 VALVE CLSD, & ICE CONDITION. FOLLOWING QRH PROCEDURES, SELECTED MANUAL OVERRIDE KNOB TO ALL. EXITED ICING CONDITIONS AT APPROX 20,000 FT. COMPLETING QRH PROCEDURES, INFORMED ATC THAT UNABLE TO FLY HIGHER THAN 25,000 FT & GOING TO CALL DISPATCH TO GET A NEW FUEL BURN AT LOWER ALT. AT APPROX 23,500 FT, CABIN BEGAN LOSING PRESSURE RAPIDLY. CABIN PRESSURE ROSE QUICKLY TO AROUND 13,500 FT. DECLARED AN EMERGENCY WITH ATC AND STATED PROBLEMS, WE`RE GOING TO DESCEND RAPIDLY T2L72 4F RTT00011AT 20060105000052006010500005GL 2006 1 5 CHQA200500221 220051230A7200AE3007A1P ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 2 SMOKE A CHQAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL11570RP4849 4849 14500821 CAE312622 FLIGHT 6326 - MCO-PFN - AT 400 FEET AGL, RECEIVED "LAV SMOKE" EICAS WARNING ALONG WITH MAIN CABIN SMOKE DETECTOR INDICATION. NO VISIBLE SMOKE WAS SEEN OR SMELLED. MAINTENANCE FOUND NR 2 ENGINE MAKING OIL SMELL IN CABIN/COCKPIT. REMOVED AND REPLACED ENGINE NR 2 IAW RR MM 72-00-00. OPS CHECK GOOD. 2L72 4T4 FRTT00011ATTE6CH 20060105000142006010500014SO 2006 1 5 RAIA00512049 120051231A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN LOOSE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03846HK 14500855 POST FLIGHT 8018 - STL - EMERGENCY LIGHTING UNATTACHED. MAINTENANCE RESECURRED LIGHT STRIP. 2L72 4T RTT00011AT 20060105000152006010500015EA 2006 1 5 SWIA200516049 120051231A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07982SW 7956 EMERGENCY EXIT SIGN IN GALLEY INOP. REPLACED COMPONENT'S LIGHT BULBS IAW 33-51-09. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20060105000162006010500016EA 2006 1 5 SWIA200516050 120051231A27604916420 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07957SW 7829 TAXI OUT GOT "SPOILERON FAULT". REPLACED NR 2 SECU AND OPERATIONAL CHECK GOOD PER AMM 27-61-05. 2L72 4F RTA21EA 20060105000182006010500018EA 2006 1 5 SWIA200516051 120051230A2750855D1009 SENSOR CNDAIRCL600 CL6002B19 1900309EA BRAKE POSITION MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07906SW115959159 7510 FLAP FAIL MSG AT 18000 FT. REPLACED LT BPSU IAW CRJ MM 27-51-10. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20060105000212006010500021EA 2006 1 5 SWIA200516053 120051229A2750860D10018ABCD CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 NM07952SW192 192 7805 ON APPROACH TO LAX AND FLAPS SELECTED AT 20 DEGREES, RECEIVED FLAPS FAIL CAUTION MSG. REPLACED FECU AND OPERATIONAL CHECKS IAW MM 27-51-05. 2L72 4F RTA21EA 20060105000272006010500027EA 2006 1 5 SWIA200516057 120051229A2711 UNKNOWN CNDAIRCL600 CL6002B19 1900309EA FLT CONTROLS UNKNOWN A SWIAO OTHER F FLT CONT AFFECTED CLCLIMB 1 NM07710BR 7852 ON CLIMB-OUT A/C ROLLS TO LEFT AND REQUIRES SIGNIFICANT RT WING DOWN AILERON TRIM. ON APPROACH IT REVERSES. WITH TRIM NEUTRAL A/C ROLLS STRONGLY TO RIGHT. PERFORMED OPERATIONAL TEST OF SKEW DETECTION UNIT, FECU, SECU 1, SECU 2. NO DEFECTS NOTED AT THIS TIME. CHECK RIGGING OF FLAPS AND FREEDOM OF MOVEMENT OF AILERONS. RIGGED WITHIN LIMITS. NO DEFECTS NOTED. ALL IAW CRJ 200 AMM 27-00-00. FLIGHT TEST REQUESTED AND PASSED. 2L72 4F RTA21EA 20060105000322006010500032NM 2006 1 5 2005UALA01506 120051227A339780172424 CABLE BOEING747 747422 1384935NM PWA 4056 PW4056 NE SEAT 4F INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29196UA 28715 PASSENGER SEAT 4F FWD EEL LIGHT INOP. REPLACED Y SPLITTER CABLE. 2L74 4F4 FRTA20WE E24NE 20060105000332006010500033NM 2006 1 5 2005UALA01507 120051227A3350 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29196UA 28715 LAV 110 FRONT AND SIDE WALL EEL LIGHTS INOP, RELAMPED. 2L74 4F4 FRTA20WE E24NE 20060105000342006010500034NM 2006 1 5 2005UALA01508 120051227A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE GALLEY INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29196UA 28715 G2 GALLEY RT SIDE WALL EEL LIGHT INOP. 2L74 4F4 FRTA20WE E24NE 20060105000382006010500038 2006 1 5 2005UALA01511 420051225A3414 INDICATOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE AIRSPEED MALFUNCTIONED A UALAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 WP29588UA 26717 ABORTED TAKEOFF AT 100 KTS AND RETURNED TO THE BLOCKS DUE TO AN AIRSPEED INDICATOR PROBLEM. CAPTAIN'S MACH/AIRSPEED INDICATOR AND LEFT AIR DATA COMPUTER WERE REPLACED IN DEN FOLLOWNG THE EVENT. THE MASI HAD A BROKEN AIRSPEED POINTER RETURN SPRING AND THE DADC HAD BENT & BROKEN PINS ON THE SENSOR CALIBRATION CIRCUIT CARD. 2L72 4F4 FRTA2NM E17NE 20060105000392006010500039SO 2006 1 5 RAIA00512037 120051219A3350 LIGHT EMB 145 EMB145LR 3260212SO OVERWING MALFUNCTIONED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03833HK 145240 PRE FLT 7966 - IAD - OVERWING EMERGENCY LIGHTS ON INSIDE OF AIRCRAFT AS WELL AS OUTSIDE OVERWING EMERGENCY LIGHTS WILL NOT EXTINGUISH WHEN ALL POWER IS REMOVED FROM THE AIRCRAFT AND TOGGLE SWITCH IS IN THE OFF POSITION. MAINTENANCE OPS CHECKED THE SYSTEM WITH NO DEFECTS NOTED. 2L72 4T RTT00011AT 20060105000402006010500040EU 2006 1 5 RAIA00512030 120051217A3350 LIGHT JETAIRJETSTMJETSTM4101 1500501EU CABIN INOPERATIVE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03566HK 41084 POST FLIGHT - STL - EMERGENCY LIGHTS OUT. MAINTENANCE ADJUSTED THE FLOOR PROXIMITY LIGHT STRIP. 2L72 4T RTA41NM 20060105000412006010500041EU 2006 1 5 RAIA00512031 120051217A3350 LIGHT JETAIRJETSTMJETSTM4101 1500501EU CABIN INOPERATIVE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03566HK 41084 POST FLIGHT 5469 - STL - EMERGENCY LIGHTS INOP. MAINTENANCE ADJUSTED THE FLOOR PROXIMITY LIGHTS STRIP. 2L72 4T RTA41NM 20060105000432006010500043EU 2006 1 5 RAIA00512038 120051220A3397 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT DISCONNECTED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03565HK 41082 PRE FLIGHT 5408 - STL - EMERGENCY TRACK LIGHTING INOP. MAINTENANCE INSPECTED AND FOUND CONNECTOR UNPLUGGED. RECONNECTED AND LIGHTS OPS CHECKED NORMAL. 2L72 4T RTA41NM 20060105000462006010500046EU 2006 1 5 RAIA00512041 120051222A2750 PIN JETAIRJETSTMJETSTM4101 1500501EU TE FLAP BYPASS MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03567HK 41085 FLT 5406 - STL -FLAPS WOULD NOT RETRACT FROM 9 DEGREES. NO CAP LIGHTS CAME ON. MAINTENANCE RESET THE FLAP BYPASS PIN. 2L72 4T RTA41NM 20060103000532006010300053CE 2006 1 3 DXTA200501145 120051215A3230691860411 MANIFOLD CESSNA680 680CE 2076811CE MLG INOPERATIVE E DXTAO OTHER J WARNING INDICATION APAPPROACH 1 GL07362QS46 6800051 LOWED LANDING GEAR, NOSE GEAR WAS VERY SLOW COMING OUT AND DOWN. AFTER ABOUT 15 SECS THE NOSE GEAR DROPPED AN NO LIGHT CAME ON BUT UNLOCK LIGHT REMAINED LIT AND WE ALSO HAD AND ANTI-SKID FAILED LIGHT. NOTHING WE ATTEMPTED WOULD TURN OUT THE UNLOCK LIGHT. CYCLED GEAR NUMEROUS TIMES. WHILE EXTENDING GEAR FOUND ALL 3 GREEN GEAR LOCKED LTS ILLUMINATED WITH A RED UNLOCK LIGHT ILLUMINATED. REMOVED AND REPLACED LANDING GEAR CONTROL 2 PCB (NF207). IAW 680 M/M 24-60-10, OP CK GOOD. 2L72 4F RCT00012WI 20060103000692006010300069EA 2006 1 3 VNAA0512020 120051224A5246 PANEL CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE EXTERNAL SERVICEOPEN A VNAAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 GL05716PS 10171 DURING CLIMBOUT THE CREW REPORTED A BANGING SOUND FROM THE RIGHT SIDE OF THE FORWARD FUSELAGE. THE FLIGHT RETURNED TO TLH AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE EXTERNAL SERVICE PANEL DOOR OPEN. THE DOOR WAS INSPECTED AND NO DAMAGE WAS FOUND. THE DOOR WAS PROPERLY SECURED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20060103000712006010300071EA 2006 1 3 VNAA0512021 120051225A5200 ACCESS DOOR CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE ELECTRICAL DOOR OPEN A VNAAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 GL05716PS 10171 DURING CLIMBOUT THE CREW REPORTED AN OPEN ACCESS DOOR. THE FLIGHT RETURNED TO SRQ AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE AC ELECTRICAL GROUND POWER DOOR OPEN. THE DOOR WAS INSPECTED AND NO DAMAGE WAS FOUND. THE DOOR WAS PROPERLY SECURED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20060103000802006010300080NM 2006 1 3 SWAA054154 120051228A534065C27314 STRINGER CLIP BOEING737 7373Q8 1384670NM BS 747 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 747, STR 20R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20060103000852006010300085NM 2006 1 3 SWAA054143 120051228A335065C27095 BATTERY PACK BOEING737 7373H4 1384600NM EMERGENCY LIGHTSINOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29331SW 23695 DURING SCHEDULED RON CHECK, FOUND R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20060103001062006010300106NM 2006 1 3 ASAA0590083 120050425A5320146A7502 SUPPORT BOEING737 737990 NM FS 727B CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02309AS 30857 PAE - DURING C-CHECK, FOUND CORROSION IN AFT CARGO BAY ON FLOOR T TO SIDEWALL SUPPORT AT RBL 20. REPAIRED IAW SRM 51-40-05. (M) 2L74 4F RTA16WE 20060103001092006010300109NM 2006 1 3 ASAA0590084 120050425A5320146A7502 SUPPORT BOEING737 737990 NM FS 727-767 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02309AS 30857 PAE - DURING C-CHECK, FOUND CORROSION IN AFT CARGO BAY SUPPORT AT RBL 25. REPAIRED IAW SRM 51-40-02. (M) 2L74 4F RTA16WE 20060103001102006010300110NM 2006 1 3 ASAA0590086 120050425A5320146A750218 SUPPORT BOEING737 737990 NM FS 727 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02309AS 30857 PAE - DURING C-CHECK, FOUND CORROSION IN AFT CARGO BAY ON FLOOR SUPPORT AT BS 727B PLUS 4. REPAIRED IAW SRM 51-40-02. (M) 2L74 4F RTA16WE 20060103001182006010300118NM 2006 1 3 ASAA0590096 120050425A5320146A81271 WEB BOEING737 737990 NM FS 767-787 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02309AS 30857 PAE - FOUND DURING C-CHECK, CORROSION ON CLOSE OUT WEB AT BS 767-787. REPAIRED IAW SRM 51-40-02. (M) 2L74 4F RTA16WE 20060103001202006010300120NM 2006 1 3 ASAA0590094 120050425A5300143A1260 STRUCTURE BOEING737 737990 NM FS 500J DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02309AS 30857 PAE - DURING C-CHECK, FOUND DAMAGED FASTENER HOLE AT BS 500J. REPAIRED IAW SRM 51-30-01. (M) 2L74 4F RTA16WE 20060103001642006010300164NM 2006 1 3 SWAA054160 120051228A53306545765 SKIN BOEING737 7373H4 1384600NM BS 517D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 517D, STR 13L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20060103001742006010300174NM 2006 1 3 QXEA200501846 120051226A6120MS21027K381 SWITCH BOMBDRDHC8 DHC8402 1390042NM GOVERNOR TEST STICKING A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09410QX 4053 GEG FLIGHT 2303: AS POWER LEVERS WERE ADVANCED TO TAXI, -OSG ABORT- MESSAGE FOLLOWED BY -POWER PLANT- MESSAGE APPEARED ON ED. MAINTENANCE FOUND OVERSIZED GOVERNOR TEST SWITCH STICKING. REMOVED AND REPLACED TEST SWITCH IAW MM 20-30-07. SWITCH OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20060103001792006010300179SO 2006 1 3 CHQA200500215 120051220A3246118145 HUB CAP EMB 145 EMB145LR 3260212SO RT MLG WHEEL MISSING A CHQAA UNSCHED LANDING DJ INFLIGHT SEPARATION WARNING INDICATION CLCLIMB 1 GL11276SK 145348 FLIGHT 900 - LAN-OKC - DURING INITIAL CLIMBOUT, RETRACTED GEAR DURING NORMAL SCHEDULE. RIGHT MAIN SHOWED IN TRANSITION (AMBER BOX) FOR APPROXIMATELY 10 SECONDS, THEN WENT TO RED. RAN QRH, RECYCLED GEAR PER QRH. WHILE PUTTING GEAR IN THE UP POSITION AGAIN, SAME PROBLEM. SELECTED GEAR TO DOWN POSITION, THREE GREEN, RETURNED TO LAN. DECLARED AN EMERGENCY. UPON POST FLIGHT, FOUND INBOARD RIGHT AXLE HUB CAP MISSING, AND WHEEL SPEED TRANSDUCER HANGING OUT OF THE AXLE. MAINTENANCE REMOVED AND REPLACED HUB CAP. OPS CHECK GOOD. 2L72 4T RTT00011AT 20060104000042006010400004SO 2006 1 4 1293122605 120051226A2750 FLAP SYSTEM GULSTMG1159 GIV 3980115SO TE FLAPS FAILED E N93AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO13493QS8860 1293 FLAPS FAILED TO RETRACT PAST 10 DEGREES. OPERATIONAL CHECKS WERE CARRIED OUT, NO DEFECTS NOTED. 2L72 4F RTA12EA 20060104000092006010400009WP 2006 1 4 DHL2005803516 120051121A53203779658U502 FITTING DOUG DC8 DC873 302199CWP BS 902-909 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 MAIN CARGO COMPT L-10L SPLICE FITTING CRACKED 3 INCHES STA 902.000 - 909.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-20D, SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW SPLICE FITTING WITH FASTENERS AND PLI WASHERS IAW SRM 51-1-21, SRM 51-1-23, SRM 51-3-0, SRM 51-1-20D, SRM 51-3-1 PG 2A (TORQUE). 2L74 4F RT4A25 20060104000202006010400020NM 2006 1 4 SWAA060017 120051230A53306545774 SKIN BOEING737 7373A4 1384585NM BS 727C CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING WALK AROUND INSP, FOUND FUSELAGE SKIN CRACKED AT BS 727C, STR 24L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20060104000242006010400024NM 2006 1 4 SWAA060021 120051230A53116517684 FRAME BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT R1 DOOR CUTOUT, FWD FRAME NR 4 STOP FITTING. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20060104000312006010400031NM 2006 1 4 051836316 120051225A3350 WIRE BOEING747 747451 1384940NM EMERGENCY LIGHT PINCHED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01676NW 33002 ROW 9-12 LT EMERGENCY PATHWAY LIGHTS OUT. FOUND WIRE PINCHED, REPOSITIONED WIRE. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L74 4F RTA20WE 20060104000322006010400032NM 2006 1 4 SWAA060001 120051230A53306545767 SKIN BOEING737 7373H4 1384600NM BS 434 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 434, STR 16R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20060104000352006010400035NM 2006 1 4 SWAA060004 120051228A53306545774 SKIN BOEING737 7373H4 1384600NM BS 730-739 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29329SW 23693 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 730 TO BS 739, STR 19L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20060104000412006010400041NM 2006 1 4 SWAA060010 120051230A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29479WN 33990 EEPLS TRACK LOOSE AT FWD END. REMOVED AND REPLACED EEPLS SECTION PER MM. 2L72 4F RTA16WE 20060104000492006010400049SO 2006 1 4 12082005 120051208A3310 ODOR GULSTMGV GV 3980116SO COCKPIT DETECTED E N93AO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO13518QS 5075 BURNING SMELL IN COCKPIT. MAINTENANCE FOUND SPIRAL WRAP TOUCHING PILOTS MAP LIGHT ASSEMBLY AND OVERHEATING. 2L72 4F RTA12EA 20060104000602006010400060SO 2006 1 4 143612282005 120051228A3250421166 WIRE HARNESS GULSTMG1159 GIV 3980115SO STEER BY WIRE FAILED E N93AK NONE O OTHER TXTAXI/GRND HDL 1 SO13436QS4435 1436 STEER BY WIRE FAILURE ON LANDING ROLLOUT. 2L72 4F RTA12EA 20060104000652006010400065EU 2006 1 4 SA05131 120051227A335032145410 EPSU AIRBUS320 A320214 3930316EU EMERGENCY LIGHTSFAULTY A USAAK NONE L NO TEST ININSP/MAINT 1 EA19102UW18417 844 PHL - THE MID-CABIN, RIGHT SIDE EMERGENCY POWER SUPPLY UNIT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE MID-CABIN, RIGHT SIDE EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20060104000672006010400067NM 2006 1 4 QXEA200501786 120051219A5230 DOOR DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE CARGO LOOSE A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09360PH 515 GEG FLIGHT NR 2207 AT FL220 TOTAL PRESSURIZATION FAILURE. DESCENDED TO 80. LANDED WITHOUT INCIDENCE. MAINTENANCE REMOVED AFT BAG DOOR AND PERFORMED BENCH RIGGING. RE-INSTALLED AFT CARGO DOOR IAW AMM TASK 52-30-00-400-801 COMPLIED WITH ADJUSTMENT OF BAGGAGE DOOR ON AIRCRAFT IAW AMM TASK 52-30-00-820-801. OPERATIONAL TEST GOOD. PRESSURIZED AIRCRAFT AND CHECKED DOOR IAW TASK 52-30-00-820-801. NO LEAKS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20060104000812006010400081 2006 1 4 SWIA200516043 420051223A22106229968001 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA YAW DAMPER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07406SW1396212472 7030 NR 2 YD GIVES APPEARANCE OF SLIPPING OR BUMPING UNCOMMANDED. REPLACED NR 2 YD LINEAR ACTUATOR IAW MM 22-22-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20060104000832006010400083 2006 1 4 SWIA200516045 420051222A2210 CIRCUIT CARD CNDAIRCL600 CL6002B19 1900309EA FCC MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07406SW 7030 UNCOMMANDED RUDDER DEFLECTION WHILE AIRBOURNE WITH AUTOPILOT ON AND OFF TO THE RIGHT 1/2 SKID/BACK DEFLECTION. REPLACED NR 1 AND NR 2 FCC CARDS IAW MM 22-12-14. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20060104000852006010400085EA 2006 1 4 SWIA200516047 120051226A5610 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07916SW 7634 LEFT WINDOW DEVELOPED CRACK WHILE AIRCRAFT PARKED AT GATE. REPLACED LT SIDE WINDOW IAW 56-12-00. 2L72 4F RTA21EA 20060104001062006010400106SW 2006 1 4 ALG2005F00122 120051206A7714 ACTUATOR BELL 206 206L4 1182110SW ALLSN 250C 250C30P 03013GL ENGINE OUT OF ADJUST E ALGAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW03175AL 52117 ON TAKEOFF, RPM ROSE TO 104 PERCENT, THE PILOT WAS UNABLE TO BEEP DOWN TO NORMAL RANGE, RETURNED TO DEPARTURE. THE MECHANIC FOUND THE LINEAR ACTUATOR RANGE WAS SET TOO HIGH, HE ADJUSTED THE BEEP RANGE TO WITHIN THE LIMITS AND THE AC WAS RETURNED TO SERVICE. (K) 1G71 3U3 UNCH2SW E1GL 20060105000012006010500001SO 2006 1 5 RAIA00512046 120051228A2913971808 PUMP EMB 145 EMB145LR 3260212SO HYD SYSTEM FAILED A RAIAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 CE03824HK16099159 145498 FLT 5520 - AUS - DURING APPROACH, LOST HYDRAULIC SYSTEM 2 QUANTITY AND THEN E2 ENGINE HYDRAULIC PUMP FAIL MESSAGE. MAINTENANCE REMOVED AND REPLACE THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP. 2L72 4T RTT00011AT 20060105000222006010500022EA 2006 1 5 SWIA200516054 120051226A5210 MECHANISM CNDAIRCL600 CL6002B19 1900309EA PAX DOOR LACK OF LUBE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07453SW 7743 MAIN CABIN DOOR WILL NOT OPEN FROM INSIDE, AND IS HARD TO OPEN FROM THE OUSIDE OF AIRCRAFT. LUBED CABIN DOOR CLOSING MECHANISM. OPERATED DOOR OPEN AND CLOSED 10 TIMES WITH NO DEFECTS NOTED. 2L72 4F RTA21EA 20060105000282006010500028EA 2006 1 5 SWIA200516058 120051227A2740 SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07910SW 7566 CH 1 STAB TRIM WILL NOT ENGAGE. REPLACED FO'S DISCONNECT SWITCH. OPERATIONAL CHECK GOOD PER MM 27-41-30. 2L72 4F RTA21EA 20060105000292006010500029NE 2006 1 5 2005UALA01503 220051224A7200 ENGINE AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE NR 2 FLAMED OUT A UALAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 WP29835UA 1426 V10897 NR 2 ENG FLAMED OUT IN CRUISE. ENG FAIL EICAS MSG. OIL PRESS, QTY GOOD. ATTEMPTED TO RESTART TWICE, NO LIGHT OFF. FMU SHUT OFF TORQUE MOTOR FAILED INTERNALLY. THIS IS A KNOWN ISSUE AND IS BEING ADDRESS ON ATTRITION PER A CATEGORY 6 SERVICE BULLETIN. HOWEVER, THIS IS A NEW FAILURE MODE SO WE WILL INCREASE SB INCORPORATION BY CAMPAIGNING INCLUSION AT ESV. 2L72 4F4 FRTA28NM E40NE 20060105000372006010500037EU 2006 1 5 2005UALA01510 120051223A2710 SERVO VALVE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FLT CONTROLS OSCILLATES A UALAA UNSCHED LANDING EF VIBRATION/BUFFET FLT CONT AFFECTED CLCLIMB 1 WP29440UA 702 RETURNED TO FIELD DUE TO AILERON VIBRATION. RT GREEN AILERON SERVOCONTROL SERVO VALVE WAS FOUND OSCILLATING, THUS CAUSING INFLIGHT AILERON VIBRATION. REPLACEMENT OF THE SERVOVALVE RESOLVED THE PROBLEM. NO FURTHER ANOMALY WAS REPORTED. 2L72 4F4 FRTA28NM E40NE 20060105000502006010500050SO 2006 1 5 RAIA00512036 120051219A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN WEAK A RAIAK NONE O OTHER ININSP/MAINT 1 CE03831HK 145232 PRE FLT 8021 - IAD - EMERGECNY LIGHT ABOVE 2A IS DIM. MAINTENANCE OPS CHECKED THE EMERGENCY LIGHT SYSTEM WITH NO DEFECTS NOTED. 2L72 4T RTT00011AT 20060105000512006010500051NM 2006 1 5 2005UALA01512 120051226A2120 ODOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN DETECTED A UALAB EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP29560UA 26660 MADE DESCENT TO 11,000 FEET DUE TO CABIN PRESSURE PROBLEM AND ODOR IN THE CABIN. REPLACED AUTO PRESSURE CONTROLLER PER MM21-31-02. OPS CHECK OK. 2L72 4F4 FRTA2NM E17NE 20060105000522006010500052NM 2006 1 5 2005UALA01513 120051222A5330 SKIN BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE BS 807 STR 27L BULGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29923UA 26643 LOWER FUSELAGE SKIN IS BULGED AND 2 FASTENER HEADS CRACKED AND PULLING THROUGH STA 807 STR 27L AND 27R WL 148.5 - 148.6. FABRICATED FILLER AND A DOUBLER REFERENCE SRM 53-00-01 AND INSTALLED THE REPAIR PER 53-00-01 DETAIL XI . 2L72 4F4 FRTA16WE E2GL 20060105000532006010500053NM 2006 1 5 2005UALA01514 120051222A3350 LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE GALLEY INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29342UA 24246 EEL LIGHTS INOP FROM ROW 15 AFT. REPLACED EEL STRIP. 2L72 4F4 FRTA16WE E2GL 20060105000542006010500054NM 2006 1 5 2005UALA01515 120051226A2750 WARNING SYSTEM BOEING757 757222 1384956NM PWA 2037 PW2037 NE TE FLAPS ACTIVATED A UALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 WP2987UA 26713 RETURNED TO THE FIELD DUE TO A FLAP ASYMMETRY PROBLEM. THIS EVENT IS CONSIDERED BY ENGINEERING TO BE A ONE-TIME NUISANCE EVENT. THE LE SLAT ASYMMETRY STATUS MESSAGE WAS GENERATED BY THE FLAP/SLAT ELECTRONICS UNIT (FSEU). THE NR 2 FSEU WAS RESET AND ALL OVERLOAD INDICATORS ON THE LE SLAT ACTUATORS WERE CHECKED OK PER AMM 27-81-18. FLAPS WERE OPERATIONALLY CHECKED AND ALL CHECKED NORMAL. THIS IS NO RECENT HISTORY OF LE SLAT ASYMMETRY PROBLEMS LEADING UP TO THIS EVENT AND NO FURTHER OCCURRENCES. 2L72 4F4 FRTA2NM E17NE 20060105000572006010500057NM 2006 1 5 2005UALA01517 120051224A3350 LIGHT BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29919UA 25386 EEL LIGHTS INOP AT MID CABIN. 2L72 4F4 FRTA16WE E2GL 20060105000582006010500058NM 2006 1 5 2005UALA01518 120051226A3350 LIGHT BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29904UA 25004 ESCAPE PATH LIGHTS INOP FROM ROW 14 BACK. 2L72 4F4 FRTA16WE E2GL 20060105000602006010500060NM 2006 1 5 2005UALA01520 120051220A5330 SKIN BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29936UA 26667 RE-EVALUATION OF SKIN AREA FWD OF CARGO DOOR OPENING REVEALS .061 OF APPARENT MATERIAL HAS BEEN REMOVED IN A 1.5 TO 2.0 INCH SCRATCH WHERE BELT LOADER CONTACTED SKIN. SUPPLEMENTAL DATA UPDATE DAMAGE REMOVED AND DOUBLERS INSTALLED PER EVA-50867-A. 2L72 4F4 FRTA16WE E2GL 20060105000692006010500069NM 2006 1 5 2005UALA01523 120051227A2121 FAN BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE EQUIP COOLING MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29942UA 26679 DIVERTED TO ORD DUE TO EQUIPMENT COOLING SUPPLY FAN PROBLEM. INSTRUMENT COOLING SUPPLY FAN FAILED.REPLACED FAN AND RELAY R401. OPS CHECK GOOD. 2L72 4F4 FRTA16WE E2GL 20060105000712006010500071NE 2006 1 5 2005UALA01524 220051227A7200 ENGINE AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE NR 2 FIRE A UALAO OTHER A FLAME/FIRE NRNOT REPORTED 1 WP29803UA 748 V10146 SMOKE AND FLAME COMING FROM NR 2 ENGINE WHILE IN REVERSE. THIS ENGINE HAS ACCUMULATED 20236 TSLSV(SINCE THE NUMBER 5 BEARING COMPARTMENT WAS ACCESSED). THE NUMBER (5) BEARING WAS NOT DPI'D AT THE PRIOR SHOP VISIT SO THERE IS A GOOD CHANCE THE BEARING/CARBON SEAL AREA HAS NEVER BEEN REMOVED(33303 HOURS). WITH THIS AMOUNT OF TIME, EXCESSIVE COKING WAS PRESENT IN THE COMPARTMENT AND WORKED ITS WAY PAST THE NUMBER 5 CARBON SEAL AND INTO THE GASPATH. 2L72 4F4 FRTA28NM E40NE 20060105000722006010500072SO 2006 1 5 RAIA00512044 120051227A3350 BULB EMB 145 EMB145LR 3260212SO EMEGENCY LIGHT INOPERATIVE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03822HK 145069 PRE FLT 5507 - STL - EMERGENCY LIGHT ON MAIN CABIN DOOR INOP. MAINTENANCE RELAMPED THE BULB AT THE MAIN DOOR EMERGENCY LIGHT. 2L72 4T RTT00011AT 20060105000772006010500077EU 2006 1 5 RAIA00512035 120051219A3397 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT LOOSE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03567HK 41085 PRE FLT 5396 - STL - ESCAPE PATH LIGHTING IN FRONT OF CABIN INOP. MAINTENANCE RESECURED LOOSE CONNECTORS. 2L72 4T RTA41NM 20060105000802006010500080NM 2006 1 5 2005UALA01526 120051220A5270 SENSOR BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE R1 DOOR DIRTY A UALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP29669UA 30025 FLIGHT RETURNED TO FIELD DUE TO A DOOR 1-R ARMING INDICATION. FOUND DEBRIS AROUND SENSOR CLEANED AREA AND CYCLED DOOR, NO DEFECTS NOTED. 2L72 4F4 FRTA1NM E24NE 20060105000832006010500083NM 2006 1 5 2005UALA01528 120051225A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE BS 1600 DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29577UA 26693 AFT PIT STA 1600 FRAME HAS A DENT BETWEEN STR 25L AND 26L ON UPPER FLANGE. CUT OUT DAMAGE, INSURANCE CUT, INSTALLED DOUBLER REPAIR PER RE0-G10199, AND EVA-50007. 2L72 4F4 FRTA2NM E17NE 20060105000842006010500084NM 2006 1 5 2005UALA01529 120051225A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE BS 1520 DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29577UA 26693 AFT PIT STA 1520 FRAME HAS A DENT BETWEEN STR 25L AND 26L ON UPPER FLANGE. TRIMMED OUT DAMAGE TO FRAME, INSURANCE CUT, INSTALLED ANGLE REPAIR PER REO G10198 AND EVA 50006. 2L72 4F4 FRTA2NM E17NE 20060105000852006010500085NM 2006 1 5 2005UALA01530 120051225A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE BS 1500 DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29577UA 26693 AFT PIT FRAME STA 1500, STR 25L AND 26L HAS DENT UPPER FLANGE. CUTOUT DAMAGE AND REPAIRED PER REO G10197 AND EVA-50005. 2L72 4F4 FRTA2NM E17NE 20060105000862006010500086NM 2006 1 5 2005UALA01531 120051225A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE BS 1580 DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29577UA 26693 AFT PIT STA 1580 FRAME HAS A DENT BETWEEN STR 25L AND 26L ON UPPER FLANGE. TRIMMED DAMAGE, INSURANCE CUT, INSTALLED ANGLE DOUBLER PER REO G-10195 AND EVA-50003. 2L72 4F4 FRTA2NM E17NE 20060105000932006010500093NM 2006 1 5 2005UALA01537 120051224A3350 LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29520UA 24890 EEL INOP AT AND AROUND DOOR 3L. 2L72 4F4 FRTA2NM E17NE 20060105001012006010500101NM 2006 1 5 USAA051649 120051229A5510 CLEVIS BOEING737 7374B7 1384702NM HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19781AU 25020 FOUND CORROSION CLEVIS R13 ON HORIZ STAB. REMOVED CORROSION, INSTALLED BUSHING PER SRM 55-10-10, DEFECT SIZE: 2". 2L72 4F RTA16WE 20060105001032006010500103NM 2006 1 5 USAA051651 120051229A5320 SPLICE BOEING737 7374B7 1384702NM BS 907 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19781AU 25020 FOUND CRACK FUSELAGE STA 907 LT S4. REMOVED AND REPLACED WITH FABRICATED STRINGER SPLICE PER SRM 51-40-02, DEFECT SIZE: .125". 2L72 4F RTA16WE 20060105001062006010500106NM 2006 1 5 USAA051653 120051229A5330 SKIN BOEING737 7374B7 1384702NM BS 490 DENTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19781AU 25020 FOUND SKIN DENTED FUSELAGE STA 490, LONG 19L-20L . FABRICATED REPAIR AND INSTALLED IAW EA 97190, DEFECT SIZE: 1.250" BY 0.750" BY 0.250"D. 2L72 4F RTA16WE 20060105001112006010500111NM 2006 1 5 USAA051645 120051229A5512 SKIN BOEING737 7374B7 1384702NM HORIZONTAL STAB DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19781AU 25020 FOUND SKIN DAMAGE RT HORIZ STAB LEADING EDGE FASTENER HOLE 3 FT FROM I/B EDGE. REMOVED DAMAGED SKIN, INSTALLED FILLER AND DOUBLER PER EA 97189 DEFECT SIZE: 1/4". 2L72 4F RTA16WE 20060105001142006010500114EU 2006 1 5 USAA051661 120051229A5310D53112830200 BEAM AIRBUSA321 A321211 3930370EU FR 16 & Y-81 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19162UW 1412 FOUND CORROSION FS 16 AND Y-81. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-72-11; CORROSION LEVEL 1; TASK JA-220-53500, DEFECT SIZE: 1" BY 1". 2L72 4F RTA28NM 20060105001162006010500116EA 2006 1 5 ASOA051021 120051126A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27870AS 7530 DURING A GROUND INSPECTION IN MGM, THE LEFT SIDE AFT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LEFT SIDE AFT EMERGENCY LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060105001192006010500119EA 2006 1 5 ASOA051023 120051103A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA BS 280 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11706EV 10054 DURING A C-CHECK IN TUS, THE LEFT FS 280 BULKHEAD WEB WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE LEFT FS 280 BULKHEAD WEB IAW ASA EO 700-53-0062, REPAIR NR 2. (M) 2L72 4F RTA21EA 20060105001212006010500121EA 2006 1 5 ASOA051028 120051127A5344CC670319813 HINGE CNDAIRCL600 CL6002C10 1390015EA PAX DOOR CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27741EV 10155 DURING A C-CHECK IN MCN, THE PASSENGER DOOR TOP STEP HINGE WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR TOP STEP HINGE IAW CRJ 200 AMM 52-10. (M) 2L72 4F RTA21EA 20060105001222006010500122EA 2006 1 5 ASOA051027 120051109A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA BS 621 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27914EV 7752 DURING A C-CHECK IN TUS, THE LEFT AND RIGHT SIDE FLOOR SUPPORT ANGLE, AT FS 621, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LEFT AND RIGHT SIDE FLOOR SUPPORT ANGLE, AT FS 621, IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20060105001232006010500123EA 2006 1 5 ASOA051024 120051103A5310 CROSSBEAM CNDAIRCL600 CL6002C10 1390015EA BS 280 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27706EV 10054 DURING A C-CHECK IN TUS, THE FS 280 CROSSBEAM WAS FOUND TO BE CRACKED AND CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE FS 280 CROSSBEAM IAW ASA EO 700-53-0061. (M) 2L72 4F RTA21EA 20060105001262006010500126EA 2006 1 5 ASOA051022 120051126A33506100928 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27886AS 7531 FLT 4537 - DURING A GROUND INSPECTION IN SHV, THE EMERGENCY EXIT LIGHT, NEAR THE PASSENGER DOOR, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT, NEAR THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060105001342006010500134EA 2006 1 5 A6WA200540360 120051226A5610NP13932112 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE COCKPIT CRACKED A A6WAB EMER. DESCENT O OTHER CRCRUISE 1 GL31457AW5355 7854 FO`S A WINDSHIELD CRACKED AT FLT LEVEL 350. REMOVED AND REPLACED WINDSHIELD IAW AMM, PRESSURE CHECK GOOD. WINDSHIELD HEAT CHECK GOOD. (K) 2L72 4F4 FRTA21EA E15NE 20060105001352006010500135NM 2006 1 5 AMTA200501032 120051106A5310 DOOR FRAME BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE BS 1380-1460 CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11518AT 27974 AFT CARGO DOOR CUTOUT UPPER CAP AT TOP SURFACE HAS CORROSION FROM BS1380-BS1460, WL 146.90, RBL 23. REMOVED UPPER CAP AND FABRICATED NEW FROM 7075-T6 .071 PO NR 786715 IAW SRM. INSTALLED NEW UPPER CAP IAW SRM. DIMENSION OF PART 3.7500 INCH X 65.1250. (K) 2L72 4F4 FRTA2NM E12EU 20060105001362006010500136NM 2006 1 5 AMTA200501038 120051108A532069455787 FITTING BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE AFT CARGO SILL CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11518AT 27974 AFT CARGO DOOR CUTOUT-DOOR SILL SUPPORT 1ST FITTING HAS CORROSION. BS 1380, WL 146.90, RBL 25. CORROSION WAS REMOVED FROM NR 1 DOOR SILL FITTING AND FUND TO BE OUT OF LIMITS AT TIE DOWNS IAW SRM. REPLACED NEW FITTING AND INSTALLED IAW SRM. (K) 2L72 4F4 FRTA2NM E12EU 20060105001392006010500139NM 2006 1 5 AMTA200501103 120051125A3350 FUSE BOEING757 75723N 1384973NM RROYCERB211 RB211535* NE BATTERY CHARGER BLOWN A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11517AT 27973 R4 SLIDE LIGHT INOPERATIVE. TROUBLESHOT, FOUND NO VOLTAGE TO LIGHT ASSY REPLACED FUSE ON BATTERY CHARGER. OPS CHECK GOOD. (K) 2L72 4F4 FRTA2NM E12EU 20060105001412006010500141NE 2006 1 5 I5HA0524006 220050916A7261R2800 ENGINE CVAC 240 240* 2422601WP PWA R2800 R2800* 52026NE LEFT LEAKING A I5HAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL23156PA 1607 324 P2993 DURING CLIMBOUT, THE PILOT OBSERVED A LOSS OF OIL QUANTITY FROM THE LT ENGINE. THE CREW PERFORMED AN EMERGENCY SHUTDOWN OF THE LT ENGINE AND RETURNED TO DEPARTURE. THE CAUSE OF THE OIL LOSS HAS NOT YET BEEN DETERMINED AND THE AIRCRAFT REMAINS AT DEPARTURE. LT ENGINE WAS REMOVED AND REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. SDR WILL REMAIN OPEN UNTIL FINAL RESOLUTION. (K) 2L72 4R4 R A793 5E8 20060105001432006010500143EA 2006 1 5 A6WA200540354 120051211A4910 APU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE APU BAY ODOR A A6WAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 GL31429AW 7711 STRONG SMELL OF JET FUEL AFTER APU START IN FLIGHT APU SHUTDOWN. PERFORMED OPS TEST AND LEAK CHECK OF APU. OPS TEST GOOD AT THIS TIME, IAW AMM. NO LEAKS NOTED. NO FAULT CODES NOTED AFTER INTEROGATION OF ECU, OPS CHECK ACM SYSTEM. NO FUEL SMELL NOTED AT THIS TIME. (K) 2L72 4F4 FRTA21EA E15NE 20060105001442006010500144NM 2006 1 5 AMTA200501042 120051108A5320 SUPPORT BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE L4 DOOR SILL CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11518AT 27974 L-4 DOOR SILL DRAIN SUPPORT CORRODED UNDER DRAIN PLATE. REMOVED CORROSION FOUND TO BE WITHIN LIMITS ALODINED AND PRIMED. (K) 2L72 4F4 FRTA2NM E12EU 20060105001452006010500145NM 2006 1 5 AMTA200501043 120051108A5320 FLOOR SUPPORT BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE BS 1660-1680 CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11518AT 27974 BS 1660-1680, RBL 10, FLOOR SUPPORT CORRODED. REMOVED CORROSION FOUND TO BE WITHIN LIMITS TREATED. (K) 2L72 4F4 FRTA2NM E12EU 20060105001492006010500149EA 2006 1 5 A6WA200540355 120051218A30307858062 COMPUTER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE ZONE 221 FAILED A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31454AW5150 7842 RT AOA HEAT FAIL MESSAGE AFTER TAKEOFF. REMOVED AND REPLACED ADHC NR 2 (AIR DATA HEAT CONTROLLER) IAW AMM. OPS TEST GOOD. (K) 2L72 4F4 FRTA21EA E15NE 20060105001562006010500156EA 2006 1 5 A6WA200540353 120051206A4920 APU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE APU BAY SMOKE A A6WAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 GL31429AW 7711 REQUEST INSPECTION OF APU COMPARTMENT DUE TO EXTREME AMOUNT OF SMOKE AFTER AUTO SHUTDOWN. INSPECTED APU AW CRJ AMM. NO DEFECTS NOTED. (K) 2L72 4F4 FRTA21EA E15NE 20060105001602006010500160WP 2006 1 5 I5HA0258010 120051030A5730CRACKED ACCESS PANEL CVAC 580 580 2422806WP ALLSN 501D 501D13 03004GL RT WING CRACKED A I5HAO OTHER O OTHER NRNOT REPORTED 1 GL23581P 29 DURING A RECENT SCHEDULED INSPECTION, A FUEL LEAK WAS DISCOVERED ON THE LOWER RT WING NEAR THE IB FUEL TANK ACCESS PANEL. A CRACK LOCATED AT WS 8. A NEW ACCESS PANEL DOUBLER WAS INSTALLED IAW DWG. THE AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4T4 TRT E282 20060105001612006010500161EA 2006 1 5 A6WA200540324 120051115A2410755469E IDG CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 1 ENGINE FAULTY A A6WAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL31417AW 7610 ON TAKEOFF ROLL IDG NR 1 FAULT FOLLOWED GEN NR 1 FAULT ABORTED 40 KNOTS BTMS INDICATION 2,2,22 LIGHT BREAKING. SERVICED IDG NR 1 IAW AMM. COMPLIED WITH ENGINE RUN. OPS CHECK GOOD. NOT LEAKS NOTED IAW AMM. NO HIGH ENERGY STOP INSPECTION REQUIRED. (K) 2L72 4F4 FRTA21EA E15NE 20060105001632006010500163NM 2006 1 5 AMTA200501039 120051106A5320146N52421 FLOOR SUPPORT BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE BS 1640-1660 CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11518AT 27974 STA 1640-1660 OBL - FLOOR SUPPORT CORRODED. REMOVED CORROSION FROM FLOOR SUPPORT AND FOUND TO BE OUT OF LIMITS IAW SRM. REMOVED AND REPLACED CHANNEL IAW SRM. AT STA 1640-1660, BL 0. GAGE USED A 2571. (K) 2L72 4F4 FRTA2NM E12EU 20060105001642006010500164NM 2006 1 5 AMTA200501105 120051123A3350 WIRE BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE EMERGENCY LIGHT DISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11522AT 29330 ROWS 28, 29 EMERGENCY FLOOR PROX LIGHTING INOPERATIVE. RECONNECTED WIRES TO LIGHT ASSY AT ROWS 28, 29. OPS OK GOOD. (K) 2L72 4F4 FRTA2NM E12EU 20060105001662006010500166 2006 1 5 KPV2005F00000 420050810A3420 COMPUTER DHAV DHC8 DHC8103 1386005NM PWA PW121 PW121 52124NE AHRU MALFUNCTIONED A KPVAO OTHER O OTHER NRNOT REPORTED 1 WP13810WP 363 DURING TAXI OUT, RECEIVED NR 2 AHRU DATA INVALAD AND NR 2 ADI VOULD NOT STAY, RETURNED TO GATE. MAINTENANCE RE-INITIALIZED POWER AND SYSTEM CHECKED OUT GOOD. NO FURTHER DEFECTS NOTED. (K) 2H72 4T4 TRTA13NM E20NE 20060105001682006010500168NM 2006 1 5 KPV2005F00001 120050805A3250 LINK DHAV DHC8 DHC8103 1386005NM PWA PW121 PW121 52124NE NLG STEERING DAMAGED A KPVAO OTHER O OTHER TXTAXI/GRND HDL 1 WP13809WP 032 DURING TAXI INTO GATE THE NOSE STEERING WAS SLUGGISH. CONTINUED TO GATE. REPLACED NLG STEERING LINK AND BOTH NOSE WHEELS. OPS CHECK GOOD. (K) 2H72 4T4 TRTA13NM E20NE 20060105001712006010500171NM 2006 1 5 KPV2005F00003 120050815A3150 WARNING SYSTEM DHAV DHC8 DHC8103 1386005NM PWA PW121 PW121 52124NE COCKPIT FALSE ACTIVATIONA KPVAO OTHER O OTHER NRNOT REPORTED 1 WP13807WP 023 DURING TAKEOFF, (ROLL SPRL IB GND) AND ROLL SPRL OB GND) CAUTION LIGHTS CAME ON. ABORTED TAKEOFF AND RETURNED TO GATE. CHECKED SYSTEM RIGGING, POWER LEVER MICROSWITCHES AND OPERATIONALLY CHECKED. NO DEFECTS NOTED. (K) 2H72 4T4 TRTA13NM E20NE 20060105001812006010500181EA 2006 1 5 SWIA200515924 120051128A2711AL00102 ACTUATOR CNDAIRCL600 CL6002C10 1390015EA AILERON TRIM MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TOTAKEOFF 1 NM07713SK 10174 PILOT REPORTS (AILERON TRIM MIS CONFIG) AT TAKEOFF. REPLACED AILERON TRIM ACTUATOR. IAW 27-12-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20060105001822006010500182EA 2006 1 5 SWIA200515925 120051201A2750 FLAP CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE LEFT OUT OF RIG A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07762SK 10226 FLAPS HALFSPEED STATUS MESSAGE IN TAXI OUT. RIGGED LT IB SKEW DETECTOR. CLEAR INHIBITS. OPERATIONAL CHECKS GOOD. IAW 27-51-00. 2L72 4F4 FRTA21EA EOOO63EN 20060105001842006010500184SO 2006 1 5 SWIA200515927 120051130A3350 LIGHT EMB 120 EMB120ER 3260203SO CABIN LOOSE A SWIAK NONE L NO TEST ININSP/MAINT 1 NM07221SW 120290 ROW 9 BC EXIT ROW LIGHT INOP. RESECURED BULB AT ROW 9BC. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20060105001872006010500187WP 2006 1 5 ABXA050294 120051102A53205750553 FINGER DOUBLER DOUG DC8 DC863F 302198FWP PWA JT3D JT3D* 52039NE FUSELAGE DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 INSIDE CENTER TANK, STA 857, LT BUTT LINE 20, AFT FINGER TAB OF DOUBLER BROKEN OFF. FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW REA D853-52530. 2L74 4F4 F 4A25 1E8 20060105001882006010500188WP 2006 1 5 ABXA050307 120051109A53205779935 WEB DOUG DC8 DC863F 302198FWP PWA JT3D JT3D* 52039NE FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 CENTERLINE WEB AT STA 800 - 857, BUTT LINE O CORRODED. FABRICATED WEB AT STA 800 - 857, BUTT LINE 0 IAW REA D853-52543. MATERIAL USED .080 7075-T6, P/O NR 1113384. 2L74 4F4 F 4A25 1E8 20060105001892006010500189WP 2006 1 5 ABXA050303 120051107A53205644678 WEB DOUG DC8 DC863F 302198FWP PWA JT3D JT3D* 52039NE FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 WEB CORRODED AT STA 857, RT BUTT LINE 46. FABRICATED WEB AT STA 857, RT BUTT LINE 46 USING .071 7075-T6, P/O NR 1084025 IAW REA D853-52538. 2L74 4F4 F 4A25 1E8 20060105001902006010500190WP 2006 1 5 ABXA050304 120051107A53205644676 ATTACH ANGLE DOUG DC8 DC863F 302198FWP PWA JT3D JT3D* 52039NE FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 RT PRESSURE PANEL AT STA 857, RT BUTT LINE 40 ATTACH ANGLE CORRODED. FABRICATED ATTACH ANGLE RT PRESSURE PANEL AT STA 857, P/N: 5644678 IAW REA D853-52534. 2L74 4F4 F 4A25 1E8 20060105001922006010500192WP 2006 1 5 ABXA050301 120051107A53205644678 WEB DOUG DC8 DC863F 302198FWP PWA JT3D JT3D* 52039NE FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 WEB CORRODED AT STA 857, LT BUTT LINE 46. FABRICATED WEB AT STA 857, LT BUTT LINE 46 USING .063 7075-T6, PO NR 1118787 IAW REA D853-52535. 2L74 4F4 F 4A25 1E8 20060105001932006010500193WP 2006 1 5 ABXA050295 120051025A53145779942 KEELBEAM DOUG DC8 DC863F 302198FWP PWA JT3D JT3D* 52039NE FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 KEEL BEAM CORRODED AT AFT BULKHEAD OF MID ACCESSORY COMPARTMENT, STA 680, BUTT LINE 0, CORROSION APPEARED TO EXTEND UNDER WING CENTER SECTION. REMOVED CORROSION AT KEEL BEAM STA 620 FWD OF BULKHEAD AND UNDER BULKHEAD AS REQUIRED REF SRM 51-1-8, REF REA D853-52595-MR FOR REPAIR PROCEDURE TO REINFORCE KEEL BEAM. TREATED AND PRIMED AS REQUIRED REF, LWR 200302015 AND SRM 51-1-8. 2L74 4F4 F 4A25 1E8 20060105001942006010500194WP 2006 1 5 ABXA050296 120051020A53305779936 SKIN DOUG DC8 DC863F 302198FWP PWA JT3D JT3D* 52039NE FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 FUSELAGE SKIN, STA 1100 TO 1120 AT RT AFT BODY FAIRING, SKIN CORRODED. REMOVED CORROSION AND INSTALLED REPAIRS BETWEEN STA 1100 LONGERON 29 RT TO STA 1120 LONGERON 30 RT IAW REA D853-52518-MR AND SRM 51-1-8, PG 20. 2L74 4F4 F 4A25 1E8 20060105001952006010500195WP 2006 1 5 ABXA050306 120051107A53205644678 ANGLE DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 LOWER CHORD AT STA 857, RT BUTT LINE 23 CORRODED. FABRICATED CHORD AT STA 857, RT BUTT LINE 23 IAW REA D853-52537. MATERIAL USED P/N: AND-10134-1407, P/O NR1122772. 2L74 4F4 F 4A25 1E8 20060105002012006010500201NM 2006 1 5 UPS05245848 120051130A3350 LIGHT BOEING727 72725C 138400HNM RROYCETAY TAY65154 EU CABIN INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01932UP 19856 N/A ENTRY DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSY REF AMM 33-50-00-0. OPS CK NORMAL. 2L73 4F4 F A3WE E25NE 20060105002022006010500202WP 2006 1 5 UPS05845849 120051130A3297 WIRE DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE RT MLG OPEN A IPXAA UNSCHED LANDING N FALSE WARNING LDLANDING 1 SO01851UP 46051 N/A RT MAIN LANDING GEAR LIGHT DID NOT ILLUMINATE DURING LANDING. GEAR WAS DOWN. T/S. FOUND WIRE FROM RT GEAR SWITCH TO TERMINAL BLOCK OPEN. REMOVED AND REPLACED WIRE IAW SWP 20-00-00. OPS CK IAW AMM 32-60-00-2 (E) STEPS 1 TO 6. OPS CK OK ALL 3 GREEN OK. 2L74 4F4 FRT4A25 E2GL 20060105002032006010500203 2006 1 5 UPS05M45850 420051201A2312 CONTROL PANEL DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE COCKPIT DEFECTIVE A IPXAK NONE O OTHER NRNOT REPORTED 1 SO01255UP 48404 N/A DIVERSION - ALL 3 VHF COMMS INOPERATIVE. REMOVED AND REPLACED NR 3 COMM PANEL IAW MM 23-10-01-4 AND TEST IAW 23-11-01-2 AND 23-11-01-2 AND 23-12-01-2 OPS CK NORMAL. 2L73 4F4 FRTA22WE E13NE 20060105002062006010500206NM 2006 1 5 AMTA200501049 120051108A5347 SEAT TRACK BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE BS 377 CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11518AT 27974 SEAT TRACK AT BS 377, WL 197, LBL 50 INSIDE SCALLOPED AREA. REMOVED CORROSION FOUND IN LIMITS TREATED. (K) 2L72 4F4 FRTA2NM E12EU 20060105002132006010500213WP 2006 1 5 ABXA060021 120051202A5311 FRAME DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE BS 1100 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 STA. 1100, LONGERON 18 RT, FRAME CORRODED. REPAIRED FRAME AT STA. 1100, LONGERON 18 RT IAW SRM 53-2-0, FIGURE 2. 2L74 4F4 F 4A25 1E8 20060105002162006010500216WP 2006 1 5 ABXA060018 120051014A5340 FITTING DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE BS 1580 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 AFT CARGO, RT SIDE, STA. 1580 HAD CRACKED FITTING, RBL 58, LONGERON 21 RT. REMOVED AND REPLACED CRACKED FITTING AT STA. 1580, RBL 58 IAW SRM 51-1-21 AND 51-3-1. 2L74 4F4 F 4A25 1E8 20060105002172006010500217WP 2006 1 5 ABXA060017 120051012A53205644011 ANGLE DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE BS 857 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 CORROSION LOWER ANGLE ON PRESSURE WEB ON FWD BULKHEAD STA. 857, FORWARD OF RT. WHEEL WELL, APPROXIMATELY LONGERON 24. WING TO BODY ANGLE AT STA. 857 CORRODED BEYOND LIMITS. ANGLE REMOVED FROM LBL13 - RBL 57.5 AND NEW SECTION INSTALLED IAW SRM 51-1-20. 2L74 4F4 F 4A25 1E8 20060105002182006010500218WP 2006 1 5 ABXA060014 120051223A5322991224644 SHEAR TIE DOUG DC9 DC933F 302207AWP PWA JT8 JT8D7B 52053NE BS 1019 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23932AX 47465 SHEAR TIE DOUBLER CRACKED AT STA. 1019 BETWEEN LONGERON 13-14. REMOVED AND REPLACED DOUBLER IAW ABX DWG K05159. 2L72 4F4 F A6WE E2EA 20060105002192006010500219WP 2006 1 5 ABXA060011 120051220A532099155964 SHELF DOUG DC9 DC933F 302207AWP PWA JT8 JT8D7B 52053NE BS 1038 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23932AX 47465 CRACKED FLANGE ON RT AFT PYLON BULKHEAD GUSSET SHELF AT STA. 1038, LONGERON 15 RT. REMOVED AND REPLACED GUSSETT SHELF IAW SRM 51-30-2. 2L72 4F4 F A6WE E2EA 20060105002212006010500221WP 2006 1 5 ABXA060016 120051011A5315 FLOORBEAM DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE BS 1640 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 CORROSION RUNNING THE ENTIRE FLOORBEAM, FORMER AND FASTENERS AT STA. 1640, LONGERON 22 RT, UNDERSIDE AFT. CORRODED BEYOND LIMITS AT RBL 53-60. REMOVED END CAP AND DOUBLER L/S. REMOVED CORROSION IAW SRM 53-2-0, PG 2P, FIG 1F AND INSTALLED END CAPS AND DOUBLER. CUT OUT CORROSION AT RBL 55. FABRICATED DOUBLER AND FILLER AND INSTALLED. 2L74 4F4 F 4A25 1E8 20060105002222006010500222CE 2006 1 5 DXTA200501171 120051230A2910 LINE CESSNA500 560CESSNA 2076750CE PWA 530 PW535A NE HYDRAULIC SYS FAILED E DXTAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07834QS 5600669 AFTER LANDING POWER BRAKE AND ANTISKID MASTER CAUTION ILLUMINATED AFTER 1 SECONDS. AFTER 10 SECONDS OF ILLUMINATION TOTAL BRAKE FAILURE OCCURRED. EMERGENCY BRAKES WERE USED. PRECHARGE IS OUTSIDE OF SHADED AREA AFTER EVENT, NO OTHER ABNORMAL CONDITIONS WERE PRESENT. RECHARGED EMERGENCY BRAKE BOTTLE IAW MM 12-10-00, BLEED BRAKE SYSTEM AND SERVICED IAW MM 32-42-00 AND PERFOMED OPS CHECK. NO DEFECTS NOTED AFTER CYCLING POWER SEVERAL TIMES. 2L72 4F4 FRTA22CE E00053EN 20060105002252006010500225EA 2006 1 5 COMA0560758 120051230A5347601R3103221 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE BS 399 CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA29272 7031 FLOOR SEAT RAIL CORRODED FROM FS 399.50 TO FS 409+126. REPAIRED LT FLOOR SEAT RAIL FROM FS399.50 TO FS409+126 BY REMOVING AND REPLACING TRACK IAW BRAS EO 601R-53-7965A. 2L72 4F4 FRTA21EA E15NE 20060105002332006010500233NM 2006 1 5 0501876301 120051227A3350 PANEL BOEING747 747451 1384940NM PWA 4056 PW4056 NE BS 830 TRANSPOSED A NWAAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL01661US 23719 UPON INSPECTION, FOUND UPPER DECK EMERGENCY LIGHT OUT ON CENTER CEILING PANEL, STATION 830. MAINTENANCE FOUND CEILING PANELS NR14 AND NR16 SWAPPED. RETURNED TO ORIGINAL POSITION. OPS CHECKED GOOD AND RETURN AIRCRAFT TO SERVICE. 2L74 4F4 FRTA20WE E24NE 20060105002362006010500236WP 2006 1 5 DHL2005803523 120051203A5754 SKIN DOUG DC8 DC873 302199CWP GE CFM56 CFM562C 13802NE LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 NR. 032564: LT WING CTR LE UPPER SKIN HAS 2 CRACKS 0.250 INCH (STA XFS 285.250 - 291.500) (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 11-30-05, DWG AA33-53-R04 REV JR DATE 11-14-05. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D. TRIMMED OUT DAMAGED SECTION AND FABRICATED FILLER (7075T6 AL 0.063 INCH) AND REPAIR DOUBLER (7075T6 AL 0.071 INCH) IAW DWG AA33-53-R04. CLEANED, TREATED AND PRIMED AREA, FILLER AND REPAIR DOUBLER INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG. 9. INSTALLED FILLER AND REPAIR DOUBLER WITH CONICAL WASHERS IAW DWG AA33-53-R04, SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1. 2L74 4F4 FRT4A25 E2GL 20060103001522006010300152SO 2006 1 3 CHQA200500220 120051230A33501317 BULB EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT BURNED OUT A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11833RP 145687 OVERWING EMERGENCY LIGHT INOPERATIVE. RELAMPED EMERGENCY LIGHT IAW EMB 135 MM 33-50-10. OPS CHECK GOOD. 2L72 4F RTT00011AT 20060103001552006010300155NM 2006 1 3 QXEA200501847 120051227A7330HRC44267KS12S3 CONNECTOR BOMBDRDHC8 DHC8402 1390042NM FUEL TEMP DAMAGED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09403QX 4037 PDX - FLIGHT 2309: NR 2 FUEL HEATER TEMP ERRATIC AT FIRST AND THEN WENT TO DASHED LINES. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE FUEL TEMP CANNON PLUG P67 IAW Q400 WD 46-10-00, SHEET 6 OF 7, PG 1. REMOVED AND REPLACED NR 2 FUEL TEMP BULB IAW Q400 AMM 73-31-09-000-801/-400-801. GROUND RAN NR 2 ENGINE. OPS CHECK OF FUEL TEMP GOOD. LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20060103001572006010300157NM 2006 1 3 QXEA200501849 120051228A3350 CONTACT DHAV DHC8 DHC8202 2809007NM BATTERY PACK DIRTY A QXEAK NONE O OTHER TXTAXI/GRND HDL 1 NM09359PH 514 PSC - AFT TWO RED FLOOR TRACK LIGHTS AT ROW 1 INOP. COMPLIED WITH TROUBLESHOOTING, FOUND 2.3 VDC AT 3352-4F20. SWAPPED BATTERY PACK AT PS6 (3352-P52), NO HELP. CLEANED CONTACTS AND POWER SUPPLY P56. OPERATIONAL CHECKS GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20060103001602006010300160NM 2006 1 3 CALA0500455 120051228A5315BAC1505100259 FLOORBEAM BOEING737 737524 1384721NM BS 947.5 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717627 27531 INSPECTION FOUND FLOORBEAM CORRODED AT STA 947.5, BETWEEN LBL 12 AND RBL 18. A NEW FLOORBEAM WAS INSTALLED IAW ECRA 5311-01246. 2L72 4F RTA16WE 20060103001732006010300173NM 2006 1 3 SWAA054169 120051226A57536546430 SKIN BOEING737 7373H4 1384600NM LT WING FOREFLAPDELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29609SW 27929 DURING SCHEDULED RON CHECK, FOUND LT WING INBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM. 2L72 4F RTA16WE 20060103001772006010300177NM 2006 1 3 SWAA054172 120051228A53126516300 STRAP BOEING737 7373Q8 1384670NM BS 178 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE BS 178 BULKHEAD VERTICAL STRAP CRACKED AT BL 0, WL 188. REPAIRED STRAP PER SWA EA. 2L72 4F RTA16WE 20060103001832006010300183NM 2006 1 3 AMTA200501033 120051106A5320 STRAP BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE CARGO DOOR CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11518AT 27974 AFT CARGO DOOR CUTOUT INNER STRAP HAS CORROSION THRU-OUT FROM BS 1380- BS 1460, WL 146.90, RBL 25 IAW SRM. FABRICATED NEW STRAP IAW SRM. INSTALLED FABRICATED STRAP AT BS 1380- 1460, WL 146.90, RBL 25 IAW SRM. (K) 2L72 4F4 FRTA2NM E12EU 20060103001972006010300197EU 2006 1 3 HAEA200500186 120051209A5230SA2490S0 DOOR AMD FALC20FALCONE 2720305EU CARGO OPEN E HAEAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 SO05285TW16801102 285 DEPARTED RWY, CLIMBING TO 9500 FT CARGO DOOR OPENED. CREW DECLARED AN EMERGENCY & RETURNED, LANDING NORMAL. INSPECTION FOUND CARGO DOOR SUSTAINED DAMAGED DURING EVENT ABOVE. ACFT FERRIED TO MX FOR REPAIRS. MX REPAIRED DAMAGE TO DOOR CAP & SURROUNDING SKIN IAW DER INSTRUCTIONS. OPS/RIGGING CHECK OF DOOR LOCK MECHANISHM REVEALED NO DESCREPANCIES. FOUND CHANNEL CRACKED & REPAIRED. AFTER REPAIR PERFORMED GROUND PRESSURIZATION CHK & FOUND SAT. A REVIEW OF EVENTS PRIOR TO DOOR OPENING REVEALED CHANNEL CRACK COULD HAVE BEEN PRE-EXISTING ALLOWING DOOR TO FLEX UNDER CABIN PRESSURE ENOUGH TO DISENGAGE FROM FORWARD LOCK & DISENGAGE ALL LOCKS. ACFT RTS. [CLOSED] 2L72 4F A7EU 20060103002012006010300201NM 2006 1 3 ERA2005F00000 120051101A534785320490133 SEAT TRACK DHAV DHC8 DHC8103 1386005NM PWA 120 PW120 NE CABIN CORRODED A ERAAK NONE O OTHER ININSP/MAINT 1 AL03881EA 233 FOUND WHILE AIRCRAFT WAS UNDERGOING C1 CHECK, AWC 19412, FOUND LT FWD SEAT RAIL CORROSION BEYOND MFG LIMITS. REPAIRED IAW RO. (K) 2H72 4T4 TRTA13NM E20NE 20060103002132006010300213NM 2006 1 3 ERA2005F00002 120051025A533085320300 SKIN DHAV DHC8 DHC8103 1386005NM PWA 120 PW120 NE RT FUSELAGE DENTED A ERAAK NONE O OTHER ININSP/MAINT 1 AL03881EA31543 233 FOUND WHILE AIRCRAFT UNDERGOING C1 CHECK, AWC 19388. FOUND DENT UNDER RT ICE SHIELD BETWEEN FUSELAGE STRINGER 14S AND 15S AT STATION X323.1. REPAIRED IAW MFG RD. 2H72 4T4 TRTA13NM E20NE 20060104000122006010400012SO 2006 1 4 152112282005 120051228A24001159SCAV373805 PDB GULSTMG1159 GIV 3980115SO DC VOLTAGE BURNED E N93AK NONE O OTHER DEDESCENT 1 SO13413QS1429 1521 RIGHT DC VOLTAGE WENT TO ZERO. FOUND PDB TERMINAL BURNED. 2L72 4F RTA12EA 20060104000162006010400016SO 2006 1 4 601122305 120051223A56101159SCB310213 WINDSHIELD GULSTMGV GULFSTREAMGV3980116SO COCKPIT CRACKED E N93AA UNSCHED LANDING O OTHER CRCRUISE 1 SO13502QS4974 601 LT WINDSHIELD CRACKED DURING FLIGHT. 2L72 4F RTA12EA 20060104000382006010400038NM 2006 1 4 SWAA060007 120051230A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29401WN 29813 EEPLS TRACK COVER MISSING AT ROW 1. REMOVED AND REPLACED EEPLS SECTION PER MM. 2L72 4F RTA16WE 20060104000772006010400077SO 2006 1 4 RAIA00512045 120051229A3350 BULB EMB 145 EMB145 3260210SO EMERGENCY LIGHT INOPERATIVE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03805HK 145096 PRE FLIGHT - PIT - EMERGENCY LIGHT IN CEILING INOP. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BULB. 2L72 4F RTT00011AT 20060104001152006010400115CE 2006 1 4 BSYA200500033 120051220A773030707223 MONOPOLE LEAR 35 35LEAR 5170600CE GARRTTTFE731TFE73122B 01518WP ENG COMPUTER FAILED E BSYAD RETURN TO BLOCK J WARNING INDICATION CLCLIMB 1 GL07900JC 178 ON TAKEOFF, RT ENGINE COMPUTER FAILED AND WOULD NOT RESET. RETURNED TO DEPARTURE. FOUND N2 MONOPOLE BAD AND N2 CONNECTOR PLUG BAD. REMOVED AND REPLACED BOTH UNITS OPS CHECKS GOOD. 2L72 4F4 F A10CE E6WE 20060105000082006010500008EU 2006 1 5 RAIA00512048 120051230A3350 LIGHT JETAIRJETSTMJETSTM4101 1500501EU CABIN INOPERATIVE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03571HK 41090 PST FLIGHT 5409 - COU - EMERGENCY FLOOR TRACK LIGHTS OUT AT ROWS 1 THROUGH 3 AND 6 THROUGH 8. MAINTENANCE RESECURRED THE LIGHT CONNECTIONS. 2L72 4T RTA41NM 20060105000192006010500019EA 2006 1 5 SWIA200516052 120051226A2750 SENSOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07923SW 7664 FLAPS DEGRADED MSG. REPLACED LT SENSORS NR 3 AND 4 IAW 27-51-15, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20060105000252006010500025EA 2006 1 5 SWIA200516056 120051227A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07443SW 7638 CEILING "LEVEL" EMERGENCY LIGHT (FLOOD) 1 AT FARTHEST AFT "INOP". RELAMPED LAMP. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20060105000302006010500030NM 2006 1 5 2005UALA01504 120051224A335078941 LAMP BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE SEAT 1E BROKEN A UALAK NONE O OTHER ININSP/MAINT 1 WP29793UA 26946 ARMREST SIDE ONE EMERGENCY PATH MARKING LIGHT BROKEN AT SEAT 1E. REPLACED LAMP ASSY. 2L72 4F4 FRTT0001SE E46NE 20060105000312006010500031NM 2006 1 5 2005UALA01505 120051225A5330141W4320 SKIN BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE BS 345 DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29216UA21611 30549 SKIN DAMAGE BELOW DOOR ONE RIGHT. 2L72 4F4 FRTT0001SE E46NE 20060105000472006010500047SO 2006 1 5 RAIA00512029 120051216A5210 RING EMB 145 EMB145LR 3260212SO PAX DOOR OUT OF POSITION A RAIAO OTHER O OTHER TXTAXI/GRND HDL 1 CE03847HK 14500857 FLT 7978 - IAD - MAIN CABIN DOOR WILL NOT OPEN FROM INSIDE. MAINTENANCE FOUND RETAINER RING OUT OF GROOVE ON INTERMEDIATE TORQUE SHAFT AND RELOCATED IT TO THE CORRECT POSITION. 2L72 4T RTT00011AT 20060105000492006010500049SO 2006 1 5 RAIA00512032 120051217A2520 PSU EMB 145 EMB145LR 3260212SO CABIN DISLODGED A RAIAO OTHER O OTHER DEDESCENT 1 CE03819HK 145062 FLT 5560 - OKC - IN FLIGHT, PASSENGER SERVICE UNIT OVER ROWS 17 AND 18BC SIMPLY FELL DOWN. MAINTENANCE INSPECTED AND SECURED THE PSU PANEL AT ROW 17 AND 18BC. 2L72 4T RTT00011AT 20060105000562006010500056NM 2006 1 5 2005UALA01516 120051222A3350 LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29338UA 24242 EMERGENCY FLOOR LIGHTING INOP AT ROW 17 AFT. 2L72 4F4 FRTA16WE E2GL 20060105000622006010500062NM 2006 1 5 2005UALA01521 120051120A5210 WINDOW BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE COCKPIT UNKNOWN A UALAA UNSCHED LANDING O OTHER CLCLIMB 1 WP29383UA 24658 RETURNED TO THE FIELD DUE TO A FLIGHT DECK WINDOW PROBLEM. 2L72 4F4 FRTA16WE E2GL 20060105000702006010500070EU 2006 1 5 RAIA00512043 120051227A5210 CABLE JETAIRJETSTMJETSTM4101 1500501EU PAX DOOR STUCK A RAIAO OTHER O OTHER TXTAXI/GRND HDL 1 CE03564HK 41081 POST FLIGHT 5414 - PAI - PASSENGER DOOR WON'T OPEN FROM OUTSIDE. MAINTENANCE FREED THE PASSENGER DOOR CABLE FROM THE DOOR HANDLE. 2L72 4T RTA41NM 20060105000792006010500079 2006 1 5 2005UALA01525 420051227A3197 WIRE BOEING757 757222 1384956NM PWA 2037 PW2037 NE INSTRUMENT PANELBURNED A UALAK NONE O OTHER ININSP/MAINT 1 WP29596UA 28749 FOUND BURNED WIRES BEHIND CONNECTOR D40496 UNDER THE P37 PANEL. FIVE WIRES WERE FOUND DAMAGED WITHIN THE P37 PANEL IN THE VICINITY OF CONNECTOR D40496J ON AIRCRAFT 5596. FOUR WIRES WERE BURNT THROUGH AND ONE WIRE HAD INSULATION DAMAGE PRESENT UPON WIRE BUNDLE INSPECTION. 2L72 4F4 FRTA2NM E17NE 20060105000872006010500087NM 2006 1 5 2005UALA01532 120051228A2130 CABIN PRESSURE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29385UA 24660 AUTO PRESSURIZATION FAILURE. TWO TAKEOFFS, TWO OCCURRENCES. FOUND INSULATION HOLDING THE CABIN SAFETY RELIEF VALVE OPEN. IN ADDITION LEAK FROM CLAMP ON LEFT PACK FLOW CONTROL VALVE WHICH WAS REPLACED EARLIER. REPLACED RELIEF VALVE AND CLAMP. PERFORMED OPERATIONAL CHECK OF THE SYSTEM GOOD. NO LEAK FOUND AND NO MORE DISCREPANCIES REPORTED. 2L72 4F4 FRTA16WE E2GL 20060105000922006010500092NM 2006 1 5 2005UALA01536 120051229A335078941 LAMP BOEING777 777222 1385219NM PWA PW4077PW4077 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29777UA 26916 EMERGENCY LIGHT AT SEATS 18C, 20G, 14F FWD WILL NOT LIGHT. 2L72 4F4 FRTT0001SE E46NE 20060105000952006010500095NM 2006 1 5 2005UALA01538 120051224A3350 LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29592UA 28143 EEL INOP AT ROW 34. 2L72 4F4 FRTA2NM E17NE 20060105000972006010500097EU 2006 1 5 USAA051659 120051229A5320D53480043205 SILL AIRBUSA321 A321211 3930370EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19162UW 1412 FOUND CORROSION -Y1732 FS C66. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-42-11; CORROSION LEVEL 1; TASK JA-26053500, DEFECT SIZE: .125 BY .125. 2L72 4F RTA28NM 20060105000992006010500099NM 2006 1 5 USAA051648 120051229A5510 CLEVIS BOEING737 7374B7 1384702NM HORIZONTAL STAB GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19781AU 25020 FOUND CORROSION CLEVIS R4 ON HORIZ STAB. REMOVED CORROSION; BLENDED GOUGES, REPLACED BUSHING PER SRM 55-10-10, DEFECT SIZE: 2" CORROSION; 1/4" GOUGES 3 EA. 2L72 4F RTA16WE 20060105001082006010500108EU 2006 1 5 USAA051656 120051229A5310D53472090010000 FLOOR SUPPORT AIRBUSA321 A321211 3930370EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19162UW 1412 FOUND FLOOR SUPPORT CORRODED, Y1292, FRAME 64 - 70. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 53-00-14, 51-72-11; CORROSION LEVEL 1; TASK JA26053500, DEFECT SIZE: 1" DIA 4 EA. 2L72 4F RTA28NM 20060105001102006010500110EU 2006 1 5 USAA051658 120051229A5310D534720901100 BEAM AIRBUSA321 A321211 3930370EU -Y1292 FR 65 - 6CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19162UW 1412 FOUND BEAM CORRODED -Y1292 FR 65 - 69. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 53-10-15; CORROSION LEVEL 1; TASK JA-260-53500, DEFECT SIZE: 1" BY 52". 2L72 4F RTA28NM 20060105001312006010500131EA 2006 1 5 A6WA200540361 120051227A215078279015 ACM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LEFT SEIZED A A6WAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 GL31403AW17020 7288 ON APPROACH GOT OIL TYPE SMELL FROM LT PACK, AND LT PACK OVERHEATED IN AUTO MODE. WHILE ON GROUND WAS UNABLE TO CONTROL LT PACK IN MANUAL MODE. INSPECTED LT PACK AND FOUND ACM SEIZED AND TO BE THE SOURCE OF THE OIL SMELL. REMOVED AND REPLACED AIR CYCLE MACHINE. (NO FURTHER OCCURRENCES). (K)A6WA200540335 2L72 4F4 FRTA21EA E15NE 20060105001332006010500133EA 2006 1 5 A6WA200540358 120051224A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS FAILED A A6WAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 GL31458AW 7861 FLAPS FAIL AT 8 DEGREES UPON FLAP RETRACTION. COMPLIED WITH SUPPLEMENT 98-18, FLAPS RESET, NO HISTORY IN PAST 72 HOURS. (K) 2L72 4F4 FRTA21EA E15NE 20060105001502006010500150NM 2006 1 5 AMTA200501088 120051120A3350 LIGHT BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE CABIN INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11518AT 27974 EGRESS LIGHTS FROM ROW 30-33, INOPERATIVE. RECONNECTED LIGHT ASSEMBLIES AFFECTED IN FLOOR EGRESS IAW WDM. OPS CHECK GOOD. (K) 2L72 4F4 FRTA2NM E12EU 20060105001532006010500153NM 2006 1 5 AMTA200501048 120051108A5315 FLOORBEAM BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE STA1640, LBL57 CORRODED A AMTAO OTHER O OTHER NRNOT REPORTED 1 GL11518AT 27974 FLOORBEAM STA, 1640, LBL 57 TO RBL 57 CORROSION AROUND CLIP NUT HOLES. REMOVED CORROSION FROM FLOORBEAM STA 1640 AND FOUND AREA WITHIN LIMITS EXCEPT FOR 1 SPOT AT RBL 57 AROUND FASTENER HOLE. TREATED AND PRIMED REPAIR STRAP AREAS AND INSTALLED STRAP IAW REO. (K) 2L72 4F4 FRTA2NM E12EU 20060105001802006010500180 2006 1 5 P5CA0501414 420051102A34232591201901 COUPLER BOEING747 747230B 1384889NM GE CF6 CF650E2 30018NE COMPASS DEFECTIVE A P5CAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA15508MC 21644 FO'S HEADING, FLIGHT DIRECTOR, AND BOTH VOR FLAGS IN RMI CAME INTO VIEW WITH HEADING FLAG IN HSI. REMOVED AND REPLACED NR 2 COMPASS COUPLER IAW AMM 34-21-00. 2L74 4F4 F A20WE E23EA 20060105001912006010500191WP 2006 1 5 ABXA050308 120051111A5315 FLOORBEAM DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 MAIN CABIN, STA 798, BUTT LINE 0 - RT BUTT LINE 48, FLOORBEAM CORRODED. REMOVED NUT PLATES, CLEANED CORROSION ON FLOORBEAM AT STA 798, BUTT LINE 0 - RT BUTT LINE 48, BLENDED AREA, OUT OF LIMITS AT .088 INCH MATERIAL REMAINING FROM ORIGINAL THICKNESS OF .186 INCH. FABRICATED REPAIR ANGLE FROM 7075-T-6511 .125 INCH EXTRUSION P/O NR 1122772, TREATED, PRIMED, AND INSTALLED ANGLE AND NUT PLATES IAW SRM 51-1-8, SSRM DWG K04881, LWR 200302015, SRM 51-1-21A AND 53-2-0, CORROSION CONFINED BETWEEN RT BUTT LINE 33 - 48. 2L74 4F4 F 4A25 1E8 20060105001972006010500197WP 2006 1 5 ABXA050297 120051024A53145750043 KEELBEAM DOUG DC8 DC863F 302198FWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 STA. 680 KEELBEAM INSIDE HEAVY CORROSION ON KEELBEAM TO PRESSURE WEB FOUND DURING ACCOMPLISHMENT OF NR HY-055. REMOVED CORROSION AT KEELBEAM STA. 680, BEHIND BULKHEAD AS REQUIRED REF. SRM 51-1-8 AND REA D853-52595-MR FOR REPAIR PROCEDURE TO REINFORCE KEELBEAM. TREATED AND PRIMED KEELBEAM AS REQUIRED REF. LWR 200302015 AND DC8 SRM 51-1-8. 2L74 4F 4A25 20060105001992006010500199NM 2006 1 5 QXEA200501602 120051201A77973035903CL250 WIRE HARNESS DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE NR 2 ENGINE DEFECTIVE A QXEAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 NM09348PH 484 RETURNED TO GATE. NR 2 ENGINE ITT GAUGE SHOWING 265 DEGREES ON TAXI OUT. OTHER ENGINE PARAMETERS NORMAL. ITT FLUCTUATED BETWEEN 265-450 DEGREES. MAINTENANCE INSPECTED AND FOUND T6 THERMOCOUPLER TRIM HARNESS BAD. REMOVED AND REPLACED HARNESS. GROUND RAN ENGINES WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20060105002002006010500200NM 2006 1 5 QXEA200501603 120051201A3040SYLZ50970 CONTROLLER DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE COCKPIT DEFECTIVE A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09359PH8300 8300 514 RETURNED TO GATE. LT WINDSHIELD HOT CAUTION LIGHT ILLUMINATED ON TAXI, RAN CHECKLIST. CAUTION LIGHT EXTINGUSHED WHEN SELECTED TO WARM UP. MAINTENANCE REMOVED AND REPLACED PILOTS WINDSHIELD HEAT CONTROLLER. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20060105002052006010500205NM 2006 1 5 AMTA200501034 120051108A5320 SILL BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE BS 1400-1460 CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11518AT 27974 AFT CARGO DOOR CUTOUT DOOR SILL CORROSION AROUND NUTPLATES 1400-1460. REMOVED FITTING, CLEANED CORROSION, TREATED, REINSTALLED. (K) 2L72 4F4 FRTA2NM E12EU 20060105002122006010500212WP 2006 1 5 ABXA060015 120051011A5320 CUSP WEB DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE BS 1020-1140 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 CORROSION ON CUSP LINE EXTRUSION, STA. 1020 TO STA. 114O, LONGERON 21 RT. CORRODED BEYOND LIMITS. REMOVED AND REPLACED CUSP EXTRUSION IAW SRM 53-2-5, FIG. 15 AND 15A. 2L74 4F4 F 4A25 1E8 20060105002152006010500215WP 2006 1 5 ABXA060012 120051221A5410591771764 STRAP DOUG DC9 DC933F 302207AWP PWA JT8 JT8D7B 52053NE FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23932AX 47465 PYLON UPPER REAR SPAR STRAP BROKEN APART AT NR 2 PYLON. REMOVED AND REPLACED SPAR STRAP IAW SRM 51-30-1 AND 51-30-5. 2L72 4F4 F A6WE E2EA 20060105002282006010500228NM 2006 1 5 UPS06445906 120051229A712065B903604 THRUST LINK BOEING747 747121 1384871NM PWA JT9 JT9D7A 52054NE NR 4 ENGINE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 AD NR 4 ENGINE REAR ENGINE MOUNT THRUST LINK FOUND CRACKED INDICATION ON FWD END LUG BORE LOWER AREA. NR 4 ENG THRUST LINK REPLACED IAW EO B747-7120-22596 APPENDIX I. 2L74 4F4 F A20WE E20EA 20060105002322006010500232EA 2006 1 5 A6WA200540359 120051226A21707536893 COALESCER BAG CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE AFT FUSELAGE INOPERATIVE A A6WAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 GL31446AW 7806 EXHAUST FUMES IN COCKPIT AND CABIN. WORSE WITH APU ON. INSPECTED APU, FOUND NO LEAKS. REPLACED AC PACKS COALESCER BAGS. OBSERVED CREW RUN UP ENGINES. NO FURTHER FUMES IN COCKPIT OR CABIN. IAW AMM. (K) 2L72 4F4 FRTA21EA E15NE 20060105002372006010500237WP 2006 1 5 DHL2005803543 120051215A7830 FITTING DOUG DC8 DC873 302199CWP GE CFM56 CFM562C 13802NE THRUST REVERSER CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 ITEM REF. NR. 032512: NR3 ENG RT T/R RAIL FITTING CRACKED, STA YN 254.000 AT 12 O'CLOCK POSITION. FABRICATED REINFORCING SPLICE (17-4 PH STAINLESS FLAT BAR) IAW MM 78-31-41 PG.1. APPLIED SILICONE TO AREA AND INSTALLED REINFORCING SPLICE MM 78-31-41 FIG. 902, MM 70-43-33. 2L74 4F4 FRT4A25 E2GL 20060105002392006010500239NM 2006 1 5 DHL2005746005 120051207A3350 LIGHT BOEING727 727224 1384076NM PWA JT8 JT8D15 52051NE CABIN LOOSE A DHLAO OTHER O OTHER CLCLIMB 1 SO01746DH 22252 CABIN DOOR EMERGENCY LIGHT CAME ON AFTER T/O AND STAYED ON. RESECURED AND TESTED EMERGENCY LIGHT IAW MM CHP 33-50-01. OPS CK NORMAL AT THIS TIME. 2L73 4F4 F A3WE E2EA 20060105002422006010500242WP 2006 1 5 ASMF200512002 120051126A272037723745503 SHUTOFF VALVE DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE RUDDER LEAKING W ASMFD RETURN TO BLOCK K FLUID LOSS TXTAXI/GRND HDL 1 SW23205AM1442514425 49405 AIRCRAFT RETURNED TO PLATFORM, DURING TAXING, THE RT PRESSURE AND QUANTITY HYDRAULIC SYSTEM WAS LOST. DURING MAINTENANCE REVISION, THE RUDDER SHUTOFF VALVE WAS LEAKED AND IT WAS REPLACED IAW MM 27-20-08, TESTED CORRECT. 2L72 4F4 FRTA6WE E9NE 20060105002432006010500243NE 2006 1 5 ASMF200512003 220051128A7200 ENGINE BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE LEFT NONE W ASMFD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SW23806AM 26273 AIRCRAFT RETURNED TO PLATFORM, DURING TAXING THE LT ENGINE WAS SHUTOFF WITH 420 OF EGT. DURING MAINTENANCE REVISION, THE LT ENGINE PARAMETERS WAS VERIFIED FINDING WITHIN LIMITS IAW MM 71-00-00. THE LT ENGINE WAS STARTED AND THE OPERATIONAL TEST WAS PERFORMED IAW MM 71-00-00, BEING CORRECT. 2L72 4F4 FRTA2NM E17NE 20060105002452006010500245NM 2006 1 5 ASMF200512005 120051128A8011784750A2 STARTER BOEING757 75729J NM PWA 2037 PW2037 NE RT ENGINE DAMAGED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23703AM119643263 27203 AIRCRAFT RETURNED TO PLATFORM, DURING TAXING THE RT ENGINE WAS REJECTED WITH N1 FALLING AND EGT INCREASING. THE RT STARTER AND VALVE WERE REPLACED IAW MM 80-11-01 AND MM 80-11-02 RESPECTIVELY, TESTED CORRECT. 2L72 4F4 FRTA2NM E17NE 20060105002462006010500246CE 2006 1 5 ACE120105 120051201A561010138402524 WINDSHIELD BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA COCKPIT CRACKED E YADAB EMER. DESCENT O OTHER CRCRUISE 1 AL03113AX7540 UC41 PILOT REPORTED RT FORWARD WINDSHIELD CRACKED. REPLACED CRACKED WINDSHIELD. 2L72 4T4 TRTA24CE E4EA 20060105002482006010500248EA 2006 1 5 COMA0560634 120051117A27507455001 CONTROL LEVER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE COCKPIT FAULTY A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01910EV 7727 FLIGHT 5114- FLAPS FAIL CAUTION. REPLACED THE FLAP CONTROL LEVER. 2L72 4F4 FRTA21EA E15NE 20060105002502006010500250EA 2006 1 5 COMA0560640 120051124A2750 DRIVE SHAFT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE T/E FLAP DIRTY A COMAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 SO01969CA 7141 FLIGHT 5343 - FLAPS FAIL CAUTION. CLEANED AND LUBRICATED FLAP FLEX DRIVE SHAFTS. 2L72 4F4 FRTA21EA E15NE 20060105002512006010500251EA 2006 1 5 COMA0560644 120051126A3234601R751461 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE NLG UNRELIABLE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01967CA23975337 7134 GEAR DISAGREE. REPLACED THE NLG SELECTOR VALVE. 2L72 4F4 FRTA21EA E15NE 20060105002522006010500252NM 2006 1 5 SCNA05013 120051203A2620 WARNING SYSTEM BOEING737 7378Q8 13844BXNM COCKPIT MALFUNCTIONED A SCNAK NONE N FALSE WARNING CLCLIMB 1 GL15801SY 30332 AMBER CARGO FIRE BOTTLE DISCHARGE LIGHT ILLUMINATED ON CLIMBOUT. NO CARGO WARNING WAS RECEIVED. THE CARGO FIRE EXTINGUISHING SYSTEM WAS NEVER ARMED AND THE CARGO FIRE DISCHARGE SWITCH WAS NEVER PUSHED. GREEN EXTINGUISHER TEST LIGHTS INDICATED NORMAL SQUIB CIRCUIT CONTINUITY. CARGO FIRE BOTTLE DISCHARGE LIGHT SUBSEQUENTLY EXTINGUISHED ON ITS OWN AFTER APPROX 15 MINUTES. MAINTENANCE CHECKED AND INSPECTED CONNECTOR PLUGS AND CHECKED SYSTEM IAW AMM 26-16-00-710-801. ALL CHECKED NORMAL. NO DEFECTS NOTED. RELEASED TO SERVICE. 2L72 4F RTA16WE 20060105002532006010500253NM 2006 1 5 EIA2005255 120051123A3350 BATTERY PACK BOEING747 747212B 1384886NM PWA JT9 JT9D* NE CABIN DISCHARGED A EIAAK NONE L NO TEST ININSP/MAINT 1 NM09485EV 20712 CEILING LIGHT ABOVE L5 DOOR / MOST FWD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK BY L5 DOOR. OPS CK NORMAL IAW MM 33-51-00. 2L74 4F4 F A20WE E20EA 20060105002542006010500254NM 2006 1 5 EIA2005256 120051123A3350 BATTERY PACK BOEING747 747212B 1384886NM PWA JT9 JT9D* NE CABIN DISCHARGED A EIAAK NONE L NO TEST ININSP/MAINT 1 NM09485EV 20712 CEILING LIGHT ABOVE R5 DOOR EMERGENCY LIGHT INOPERATIVE.REMOVED AND REPLACED R5 CEILING EMERGENCY LIGHT PACK, OPS CK NORMAL IAW MM 33-51-00 2L74 4F4 F A20WE E20EA 20060105002582006010500258WP 2006 1 5 IXXA0500121O 120051202A3230 UPLOCK DOUG DC8 DC871F 302199DWP GE CFM CFM562 GL NLG LACK OF LUBE A IXXAA UNSCHED LANDING O OTHER CLCLIMB 1 SW11829BX8972957 45994387 DURING CLIMB OUT, UNSATISFACTORY UPLATCH CHECK, NOSE GEAR IS EXTENDING DURING UPLATCH CHECK. CREW RETURNED AIRCRAFT TO DEPARTURE AND LANDED WITH NO INCIDENT. MAINTENANCE LUBED THE UPLATCH MECHANSIM AND CHECKED OPERATION OF UPLATCH BY GEAR RETRACTION. AN UPLATCH CHECK WAS PERFORMED SEVERAL TIMES AS WELL AS NOSE WHEEL EXTENSION/RETRACTION. OPS CHECK WAS GOOD IAW ALL APPLICABLE MANUALS AND AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F4 FRT4A25 E2GL 20060105002592006010500259WP 2006 1 5 ABXA050310 120051026A53135779942 LONGERON DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 CORROSION FOUND ON STR 31 L (LONGERON) FROM STA. 610 - 730 IN MID ACCESSORY COMPARTMENT. REMOVED AND REPLACED LONGERON 31 LT FROM STA. 610-730 REF SRM 51-1-20 AND DPS 3.67-22. 2L74 4F4 F 4A25 1E8 20060105002602006010500260EU 2006 1 5 05FDEA04086 120051203A1100 DATA PLATE AIRBUS310 A310 EU GE CF6 CF680A3 30025NE FUSELAGE MISSING A FDEAK NONE O OTHER ININSP/MAINT 1 SO25424FE 241 DISCREPANCY (N0633 AND N0634): UNABLE TO VALIDATE MFG P/N AND S/N OF INSTALLED AIRFRAME LIFE LIMITED PARTS LT AND RT MLG RETRACT CYLINDERS DUE TO MISSING DATA PLATES. NSTALLED NEW DATA PLATE PER FEDEX DRWG. Z-20-001 REV. A AND AMM 11-22-32 2L72 4F4 FRTA35EU E13NE 20060105002612006010500261EU 2006 1 5 05FDEA04087 120051203A5330 REPAIR AIRBUS310 A310 EU GE CF6 CF680A3 30025NE BS 771-805 MISMANUFACTURED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25424FE 241 2PREVIOUS REPAIR INSTALLED AT LOWER FUSELAGE 6 O'CLOCK POSITION AT STA 771 TO STA 805, FR1 TO FR2. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR NEW REPAIR ACCOMPLISHED PER SRM 53-11-12 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR. 2L72 4F4 FRTA35EU E13NE 20060105002622006010500262EU 2006 1 5 05FDEA04091 120051203A5330 REPAIR AIRBUS310 A310 EU GE CF6 CF680A3 30025NE FUSELAGE MISMANUFACTURED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25424FE 241 PREVIOUS REPAIR INSTALLED AT FUSELAGE LT SIDE BELOW AOA SENSOR AT STA 1364 TO STA 1386, FR18 TO FR19, STR 39LT TO 44LT. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR NEW REPAIR ACCOMPLISHED PER SRM 53-10-12 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR 2L72 4F4 FRTA35EU E13NE 20060105002642006010500264EU 2006 1 5 05FDEA04093 120051203A5101 REPAIR AIRBUS310 A310 EU GE CF6 CF680A3 30025NE FUSELAGE UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25424FE 241 SMIS 424 51-00 0007102 27SEP05 MC1 CLOSE R MOD TYPE Y MOD NO. 9-AGING-INSP REV NO. PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NO. POS PT1 ENT BY: 067708 INFO 30NOV05 21:26 MC1 R DISCREPANCY (N0497): PREVIOUS REPAIR INSTALLED AT FUSELAGE LT SIDE AT STA 2231 TO STA 2251, FR39, STR 35LH. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. **S/D COMING** 2L72 4F4 FRTA35EU E13NE 20060105002652006010500265EU 2006 1 5 05FDEA04094 120051203A5101 REPAIR AIRBUS310 A310 EU GE CF6 CF680A3 30025NE FUSELAGE NONE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25424FE 241 SMIS 424 51-00 0007102 27SEP05 MC1 CLOSE R MOD TYPE Y MOD NO. 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1 ENT BY: 067708 INFO 30NOV05 21:26 MC1 R DISCREPANCY (N0500): PREVIOUS REPAIR INSTALLED BELOW L2 DOOR HANDLE AT STA 3998 TO STA4042, FR74 TO FR75. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 52-10-00 FIG.206 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR 2L72 4F4 FRTA35EU E13NE 20060105002692006010500269NM 2006 1 5 NOCA2805 120051127A2520 PSU BOEING757 75728A 1384976NM RROYCERB211 RB211535E4 54555NE CABIN OPEN G NOCAK NONE O OTHER LDLANDING 1 EA15750NA 26277 FPO AFTER LANDING PSU ROW 34DEF OPENED AND THE OXYGEN MASK WERE EXPOSED. OXYGEN GENERATORS WHERE NOT ACTIVATED. PSU AND SEATS DEFERRED. 2L72 4F4 FRTA2NM E12EU 20060105002712006010500271EA 2006 1 5 QXEA200501749 120051031A532067036541002 FITTING CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE FUSELAGE MISDRILLED A QXEAK NONE W INADEQUATE Q C ININSP/MAINT 1 NM09603QX 10011 DURING C3 CHECK. ON AFT SIDE OF FUSELAGE INTERIOR AT FS 1069.75 BETWEEN STRINGER 9R AND 10R FITTING PN 670-36541-002 HAS SEVERAL DRILL MARKS ON THE TOP SURFACE. MAINTENANCE BLENDED OUT THE DAMAGE IAW EA R-54-86 AND REO 670-54-51-007. RESTORED FINISH. 2L72 4F4 FRTA21EA EOOO63EN 20060105002722006010500272EA 2006 1 5 QXEA200501750 120051031A532067036541001 FITTING CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE FUSELAGE MISDRILLED A QXEAK NONE W INADEQUATE Q C ININSP/MAINT 1 NM09603QX 10011 DURING C3 CHECK. ON FISELAGE INTERIOR AT AFT SIDE OF STATION FS 1069.75 BETWEEN STRINGERS 9L AND 10L, FITTING PN 670-36541-001 HAS A DRILL MARK ON TOP SURFACE. MAINTENANCE REPAIRED FITTING IAW EA R-54-86 AND REO 670-54-51-007. RESTORED FINISH. 2L72 4F4 FRTA21EA EOOO63EN 20060105002732006010500273GL 2006 1 5 CHQA200500207 220051130A7200AE3007A13 ENGINE EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL NR 2 MAKING METAL A CHQAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL11831RP8710 8710 145663 CAE312243 E2 OIL IMPENDING BYPASS MESSAGE DURING CRUISE. OIL QUANTITY DROPPED TO 6 QUARTS, OIL TEMPERATURE WAS OPERATING AROUND 12.5 THEN WENT INTO RED. MOVED LEVERS ACCORDINGLY TO KEEP IN GREEN. LATER IN DESCENT, MOVED TO IDLE AND ENGINE 2 LOW OIL PRESSURE MESSAGE RECEIVED. DECLARED AND EMERGENCY. MAINTENANCE FOUND ALL CHIP DETECTORS FULL OF METAL. REMOVED AND REPLACED NR 2 ENGINE IAW JC CE720001. AIRCRAFT OK TO CONTINUE SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20060105002742006010500274EA 2006 1 5 QXEA200501611 120051031A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE FUSELAGE NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 DURING C3 CHECK. FUSELAGE EXTERIOR HAS NICKS ON THE SKIN AT STATION 1000 STRINGER 15L TO 16L. MAINTENANCE BLENDED OUT DAMAGE IAW CRJ-700 SRM 51-12-00. WITHIN LIMITS OF EA R-53-397 AND REO 670-53-61-213. FINISH RESTORED. 2L72 4F4 FRTA21EA EOOO63EN 20060105002752006010500275EU 2006 1 5 200512041 120051204A29135116402 PUMP EMB ERJ170ERJ170100 EU GE CF34 CF348E5 30015NE NR 2 ENGINE CRACKED A UHLAK NONE K FLUID LOSS CRCRUISE 1 GL17637RW2549 17000051 CREW REPORTED LOSS OF PRESSURE IN NR 2 HYDRAULIC SYSTEM DURING CRUISE FLIGHT. FOUND ENGINE 2 ENGINE DRIVEN PUMP WITH CRACK CAUSING LEAK. REMOVED AND REPLACED PUMP. 2L74 4F4 FRTA56NM E00063EN 20060105002762006010500276NE 2006 1 5 XN0A1280 220051206A7412 EXCITER AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE NR 1 ENGINE FAULTY A XN0AD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL23473AS 203 NO LIGHT UP ON NR1 ENGINE ON (B) IGNITION. FOR T/S TRIED (A) IGNITION BUT NO LIGHT-UP. ABNORMAL PROCEDURES CARRIED OUT IAW QUICK REFERENCE HANDBOOK. REPAIRED (B) SYSTEM IGNITION EXCITER IAW AMM 74-11-01 OPS CK GOOD. PLACED (A) SYSTEM ON DMI LOG NR 5959 IAW ENA MEL REFERENCE 74-00-01 CAT-C. (STATUS:ORIG/CLOSED) 2L72 4F4 FRTA35EU E23EA 20060105002782006010500278 2006 1 5 YENA200585 420051205A2330 ODOR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CABIN DETECTED A YENAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15524JB 1528 F/A'S REPORT ACRID BURNING SMELL ON A/C RT AT ROWS 20 OR 21. LIVE TV TURNED OFF, SMELL WAS INTERMITTENT FROM THEN ON. ACCOMPLISHED WITH TSM 23-39-00-810-801 NO DISCREPANCIES NOTED. REMOVED AND REPLACED SB AT 20 AND 21 DEF AND VDU AT 20 DEF AND 21 DEF AS PRECAUTIONARY. PERFORMED TSM 24-00-00-810-823. NO ODORS OR FAULTS FOUND. 2L72 4F4 FRTA28NM E40NE 20060105002822006010500282EU 2006 1 5 05FDEA04146 120051205A5101 FASTENER AIRBUS310 A310 EU GE CF6 CF680A3 30025NE NR 1 PYLON INCORRECT A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 PREVIOUS REPAIR INSTALLED ON NR 1 PYLON RT SIDE IB AFT LOWER FAIRING EXT DOUBLER STA 1050 RIB 20 NEEDS EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA, REF N00705. REPAIR REVEALED INCORRECT FASTENER INSTALLED REMOVED AND REPLACED REPAIR IAW 54-54-51. 2L72 4F4 FRTA35EU E13NE 20060105002832006010500283NM 2006 1 5 05FDEA04149 120051205A5720 LATCH DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 SNRM N0539: RT WING LEADING EDGE ACCESS PANEL 617CB INTERIOR FRONT, SPAR LOWER CAP, UPPER SURFACE FOUND CORROSION AT LATCH CONTACT AREA.** S/D COMING** 2L73 4F4 FRTA22WE E24NE 20060105002842006010500284WP 2006 1 5 05FDEA04150 120051206A5101 DOUBLER DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL FUSELAGE NONE A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 DISCREPANCY FOUND EXTERNAL DOUBLER BETWEEN STA 735 AND 755 AND LONGERONS 34 AND 35 LT SIDE, WHERE POTABLE WATER SERVICE PANEL USED TO BE LOCATED. PERFORMED INSPECTION ON REPAIR IAW SRM 53-20-00 FIG 6 VOL 1 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P1. 2L73 4F4 F A22WE E23EA 20060105002852006010500285WP 2006 1 5 05FDEA04151 120051206A5311 FRAME DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 CAC LOWER LOBE BILGE FOUND 1EA CRACK, 3 INCHES LONG ON LT FRAME AT STA 1159 CLOSE TO PRESSURE PANEL FWD CENTER WING. REMOVED ATTACH ANGLE IAW SRM 51-33-01 PAR 6-10 VOL 2 REPAIRED FRAME IAW SRM 53-30- 00 FIG 7 VOL 1 REINSTALLED ATTACH ANGLE IAW SRM 51-33-01 PAR 6-10 VOL 2. 2L73 4F4 F A22WE E23EA 20060105002862006010500286NM 2006 1 5 05FDEA04152 120051206A5315 FLOORBEAM BOEING727 727227 1384078NM PWA JT8 JT8D9A 52048NE FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 MAIN DECK TOP SIDE OF FLOORBEAM GOUGED AT STA BS680 LBL47 TO LBL57. REMOVED DAMAGED, FABRICATED REPAIR ANGLES FROM 17-7PH CRES STEEL .063 INCH, FABRICATED FILLER AND INSTALLED REPAIR ANGLES AND FILLER IAW SRM SR27-53-034 REV E. INSTALLED SEAT TRACK AT LBL65 BETWEEN STA BS660 AND STA BS720A IAW B727 SRM 51-30-2. THIS IS A MAJOR REPAIR SIGNED BY MECH NR 110569 AND QC178, REFERENCE N00807. 2L73 4F4 F A3WE E2EA 20060105002872006010500287NM 2006 1 5 05FDEA04153 120051206A551465174282 HINGE FITTING BOEING727 727227 1384078NM PWA JT8 JT8D9A 52048NE HORIZ STAB WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 RT HORIZONTAL STABILIZER IB NR1 ELEVATOR HINGE FITTING ON HORIZONTAL STABILIZER HAS IB FACE OF FITTING WORN. REMOVED BUSHING, SPOTTED FACE, HFEC INSPECTED LUG BORE FABRICATED AND INSTALLED REPAIR WASHER AND NEW BUSHING ALL IAW EA NR 7-5510-91317. THIS IS A MINOR REPAIR SIGNED BY MECH NR 4290 AND QC298 REF N01126. 2L73 4F4 F A3WE E2EA 20060105002902006010500290NM 2006 1 5 05FDEA04156 120051206A5320 FLOOR SUPPORT BOEING727 727227 1384078NM PWA JT8 JT8D15 52051NE BS 297-304 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 CORROSION BS 297-304, WL 208, LBL 12-14. UPPER FLANGE OF FLOOR SUPPORT. REMOVED AND REPLACED FLOOR SUPPORT BS 294-BS312 IAW SRM 51-30-2, SRM 51-10-2. 2L73 4F4 F A3WE E2EA 20060105002912006010500291NM 2006 1 5 05FDEA04158 120051206A5315 FLOORBEAM BOEING727 727227 1384078NM PWA JT8 JT8D15 52051NE FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 CORROSION BS 304, WL 280, LBL 14 GOUGE ON TOP FLANGE, FLOORBEAM. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-30-2 AND SRM 51-10-2. 2L73 4F4 F A3WE E2EA 20060105002942006010500294EU 2006 1 5 AWXA200501482 120051204A273031075440 SERVO AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE ELEVATOR FAILED A AWXAO OTHER E VIBRATION/BUFFET CRCRUISE 1 WP28649AW2929029279 803 ON CLIMB, FELT VIBE IN RUDDER PEDALS. TURNED A/P OFF, INCREASED PITCH OF AC TO SLOW DOWN TO 270 IAS & FL 330, VIBE STOPPED. INSP AC & ELEV SERVO HINGE BRGS FOR CONDITION IAW MM. AC FERRIED BACK FOR REPAIR. DURING FERRY FLT, REPORTED AC CRABBING 2 DEGREES TO RT WITH A 1.3 LT RUDDER TRIM SHOWN ON FLT CTRL PAGE. FOUND ECS PACK INLET DOORS FOR PACKS TO HAVE PLAY. REPLACED ACT BUSHINGS, ATTACH HARDWARE FOR LT PACK INLET DOOR, REPLACED AFT BUSHINGS FOR RT DOOR IAW MM. OPS CK GOOD. FOUND LT IB GREEN, ELEVATOR SERVO FAILED FREE PLAY CHK. R&R LT IB, GREEN, ELEV SERVO IAW MM. OPS & LEAK CHKS GOOD. FOUND PLAIN AND SLEEVE BEARINGS FLATTENED OUT AND WORN. FAILIED INSULATION RESISTANCE TEST. UNIT WAS REPAIRED. 2L72 4F4 FRTA28NM E40NE 20060105002952006010500295EU 2006 1 5 AWXA200501485 120051206A3350E0053R8B3ASNE CONNECTOR AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE CABIN DEFECTIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28628AW 67 EEL-DURING OVERNIGHT INSPECTION DISCOVERED THE EMERGENCY EXIT LIGHT ASSEMBLY AT ROW 24L INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CONNECTOR PLUG FOR THE EMERGENCY LIGHT ASSEMBLY AT ROW 24L IAW MM. OPERATIONAL CHECKS WERE GOOD. 2L72 4F4 FRTA28NM E311NE 20060105002962006010500296EU 2006 1 5 AWXA200501486 120051206A2560P4010021000 BATTERY AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE FLASHLIGHT DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28625AW 064 EEL - CREW REPORTED THAT THE FORWARD FLIGHT ATTENDANT FLASHLIGHT BATTERY IS DEAD. MAINTENANCE REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANT BATTERY. OPERATIONAL CHECKS WERE GOOD. 2L72 4F4 FRTA28NM E311NE 20060105002972006010500297EA 2006 1 5 REXA200500143 120051205A2751 DETECTOR CNDAIRCL600 CL6002B19 1900309EA T/E FLAP MALFUNCTIONED A REXAK NONE N FALSE WARNING APAPPROACH 1 SO258884E 7884 FLAP FAIL AT 42 DEGREES. LANDING UNEVENTFUL.REMOVED AND REPLACED FLAP SKEW DETECTION UNIT IAW AIRCRAFT MM. OPERATIONALLY CHECK GOOD. 2L72 4F RTA21EA 20060105002982006010500298NM 2006 1 5 05FDEA04160 120051206A5311 FRAME BOEING727 727227 1384078NM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 N01022, CORROSION (C53-113-01(2)) ON LOWER CHORD AROUND NUTPLATE HOLE BS 1130 RBL 24 WL 201. REMOVED CORROSION ON LOWER CHORD BS 1130 RBL 24, WL 201, FOUND TO BE OUT OF LIMITS, REPAIRED LOWER CHORD IAW SRM 53-10-8 FIG 10. 2L73 4F4 F A3WE E2EA 20060105003002006010500300EU 2006 1 5 05FDEA04167 120051207A5101 FASTENER AIRBUS310 A310 EU GE CF6 CF680A3 30025NE NR 1 PYLON INCORRECT A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 PREVIOUS REPAIR INSTALLED ON NR 1 PYLON RT SIDE IB AFT LOWER FAIRING EXT DOUBLER STA 1050 RIB 20 NEEDS EVALUATION FOR MAJOR MINOR CLASSIFACATION AND APPROVED REPAIR DATA REF N00705. EVALUATION OF REPAIR REVEALED INCORRECT FASTENERS INSTALLED REPLACED REPAIR IAW SRM 54-54-51, FIG 203, SH 1. 2L72 4F4 FRTA35EU E13NE 20060105003022006010500302EU 2006 1 5 05FDEA04169 120051207A5101 REPAIR AIRBUS310 A310 EU GE CF6 CF680A3 30025NE L/E SLAT NONE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 PREVIOUSLY REPAIR INSTALLED ON L/W NR 1 SLAT IB LEADING EDGE, SKIN BLIND FASTENER FLUSH. REPAIR WS RIB 2 TO RIB 3, NEEDS EVALUATION FOR MAJOR MINOR CLASSIFACATION AND APPROVED REPAIR DATA REF N00708. REPAIR EVALUATED AS GOOD IAW EA 6-5750-95471. 2L72 4F4 FRTA35EU E13NE 20060105003052006010500305EU 2006 1 5 05FDEA04178 120051208A5511 SPAR AIRBUS310 A310 EU GE CF6 CF680A3 30025NE HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 LT HORIZONTAL T/E UPPER IB SPAR ON LOWER SIDE HAS SEVERE EXFOLIATION, REF N00541. REPAIRED LT UPPER IB THS SPAR CORD IAW A310-200 SRM 55-11-21 PARA 7.H PAGES 315TO, 320 FIG 211,213 AND 219 SHEET 2. 2L72 4F4 FRTA35EU E13NE 20060105003072006010500307WP 2006 1 5 ABXA050319 120051128A52204914413 FITTING DOUG DC9 DC941 302207NWP PWA JT8 JT8D15 52051NE EXIT DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23963AX 47780 RT FORWARD OVERWING EXIT DOOR HAD A CRACKED FITTING AT FORWARD LOWER CORNER. REMOVED DAMAGED FITTING AND INSTALLED NEW FITTING IAW SRM 57-30-5 AND 51-30-2. 2L72 4F4 F A6WE E2EA 20060105003082006010500308WP 2006 1 5 ABXA050320 120051201A5610575468827 RETAINER DOUG DC9 DC941 302207NWP PWA JT8 JT8D15 52051NE COCKPIT CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23963AX 47780 CRACKS NOTED ON X-RAY INSPECTION AT CAPTAIN'S OVERHEAD WINDOW RETAINER. REMOVED AND REPLACED CRACKED DOUBLER IAW SRM 51-30-2. 2L72 4F4 F A6WE E2EA 20060105003102006010500310GL 2006 1 5 3002002311405 120051104A2130 PRESSURE SYSTEM BOMBDRBD700 BD7001A10 1390006GL CABIN MALFUNCTIONED E J7SAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SW05514FX 20023 ABORTED TAKEOFF DUE TO AUTO PRESSURIZATION FAILED. MX C/W VISUAL INSPECTION OF THE OUTFLOW VALVE. PERFORMED RINGING OF THE WIRES AND FOUND NO DEFECTS. LOADED THE TEST AND RIGGING FILES. PERFORMED SYSTEM OPS CHECK AND IT PASSED. INSPECTED OUTFLOW VALVE AND CONNECTORS FOR SECURITY, INSPECTED WIRING AND PERFORMED RINGOUTS BETWEEN. IASC NR 1 AND THE OUTFLOW VALVE, OUTLOADED DATA DISK TO MDC, FUNCTIONALLY TESTED, OPS CHECK GOOD AT THIS TIME. COULD NOT DUPLICATE PROBLEM. 2L72 4F RTT00003NY 20060105003142006010500314SO 2006 1 5 GLBA20050614 120051207A32332060500005 ACTUATOR EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE NLG INOPERATIVE A GLBAA UNSCHED LANDING O OTHER CLCLIMB 1 NM03297UX 4540 120297 NOSE LANDING GEAR WOULD NOT RETRACT, REPLACED ACTUATOR. OPS CHECKED SATISFACTORY. 2L72 4T4 TRTA31SO E20NE 20060105003162006010500316 2006 1 5 2005000012 420050728A2330RDAX5321 DECODER DOUG DC10 DC1030 3023501WP GE CF6 CF650C2B 30018NE CABIN FAULTY A CNMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW07810AX 48265 ABOUT 3+15 INTO THE FLIGHT FA'S NOTICED SMOKE COMING FROM LT SIDE OF AIRCRAFT UPPER SIDE WALL ROWS 15-16-17 RAN PROCEDURE 4-8-1-1 CABIN LIGHTING SMOKE, FIRE AND PULLED ALL C/B'S IN MID-GALLEY SERVICE AREA ALL BREAKERS PULLED TO HELP ISOLATE THE SOURCE OF SMOKE. FOUND PROBLEM WAS DECODER FAILURE ISOLATED TO THE FOLLOWING SEATS LT SIDE OB SEATS 12-14-15-16-17 ABC. REPLACED OVERHEAD DECODERS ROWS 12-14-15-16 IAW MM 23-33 P/N RD-AX5321 S/N 104079, 103990, 106855, 100376. INSPECTED WIRING NO DAMAGE NOTED IN OVERHEAD AREA. CHECKED O2 SYSTEM IAW MM 23-33. 2L73 4F4 F A22WE E23EA 20060105003222006010500322EU 2006 1 5 05FDEA04216 120051210A5522 SKIN AIRBUS310 A310 EU GE CF6 CF680 30025NE ELEVATOR DEBONDED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25424FE 241 SMIS 424 51-00 0007102 27SEP05 MC1 CLOSE R MOD TYPE Y MOD NR 9-AGING-INSP REV NO. PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1 ENT BY: 067708 INFO 30NOV05 21:26 MC1 R DISCREPANCY (N618): LT ELEVATOR T/E, DEBONDING AT UPPER AND LOWER SURFACE (FRACTION NR 3) REPAIR CONFORMS TO EXISTING ENGINEERING AUTHORIZATION EA 6-5510-94659. REPAIR EVALUATED IAW GMM 6-2-100 AND CLASSIFIED MAJOR. 2L72 4F4 FRTA35EU E13NE 20060105003242006010500324EU 2006 1 5 05FDEA04217 120051210A5210 STRUCTURE AIRBUS310 A310 EU GE CF6 CF680 30025NE PAX DOOR CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25424FE 241 SMIS 424 51-00 0007102 27SEP05 MC1 CLOSE R MOD TYPE Y MOD NR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NO. POS PT1 ENT BY: 067708 INFO 30NOV05 21:26 MC1 R DISCREPANCY (N369): RT AFT PAX DOORS FWD LWR CORNER, CORROSION FOUND AT DOOR SILL CORNER SEATING. REPAIRED IAW SRM 53-18-12 FIG. 201 REPAIR EVALUATED IAW GMM 6-2-100 AND CLASSIFIED AS (MAJOR). 2L72 4F4 FRTA35EU E13NE 20060105003252006010500325EU 2006 1 5 05FDEA04218 120051210A5320 TRACK AIRBUS310 A310 EU GE CF6 CF680 30025NE FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25424FE 241 SMIS 424 51-00 0007102 27SEP05 MC1 CLOSE R MOD TYPE Y MOD NR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1 ENT BY: 067708 INFO 30NOV05 21:26 MC1 R DISCREPANCY (N585): AFT MDCC FLOOR STRUCTURE, CROSSTRACK AT FR47 BETWEEN Y450 AND Y953 FOUND CRACKED. REPLACED IAW EA 6-5310-94662 AND SRM 51-40-21 AND 51-40-44, 51-72-10. 2L72 4F4 FRTA35EU E13NE 20060105003262006010500326EU 2006 1 5 05FDEA04219 120051210A5730 SKIN AIRBUS310 A310 EU GE CF6 CF680A3 30025NE LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25424FE 241 SMIS 424 51-00 0007102 27SEP05 MC1 CLOSE R MOD TYPE Y MOD NO. 9-AGING-INSP REV NO. PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1 ENT BY: 067708 INFO 30NOV05 21:26 MC1 R DISCREPANCY (N400): LT WING - CRK AT UPPER SKIN SURFACE AT WING NEXT TO (AFT NAVIGATOR LIGHT) REPAIR CONFORMS TO AN EXISTING ENGINEERING AUTHORIZATION 6-5710-93236. REPAIR EVALUATED IAW GMM 6-2-100 AND CLASSIFIED MINOR. 2L72 4F4 FRTA35EU E13NE 20060105003272006010500327CE 2006 1 5 DJFA2005171 120051207A561010138402523 WINDSHIELD BEECH 200 B200 1152922CE PWA PT6 PT6* 52043EA COCKPIT CRACKED E DJFAA UNSCHED LANDING O OTHER CRCRUISE 1 EA23616TA3680 BB1749 TRIP ID NR 934736 WINDSHIELD HEAT WAS TURNED ON AT 10,000 FT WITH AN OUTSIDE AIR TEMPERATURE OF + 2 DEGREES CELSIUS. AFTER REACHING CRUISE ALTITUDE OF FL 250 THE PILOTS SIDE WINDSHIELD SHATTERED. THE CREW DONNED THEIR OXYGEN MASKS AND DECLARED AN EMERGENCY. AN EMERGENCY DESCENT WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO DEPARTURE. A NORMAL APPROACH AND LANDING WAS MADE. MAINTENANCE REPLACED THE LT PILOTS WINDSHIELD. THE AIRCRAFT WAS RETURNED TO SERVICE. 1L72 4T3 T A24CE E2NE 20060105003282006010500328NE 2006 1 5 QXEA200501852 220051229A7200 ENGINE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE NR 1 MALFUNCTIONED A QXEAD RETURN TO BLOCK M OVER TEMP TXTAXI/GRND HDL 1 NM09611QX 10041 DEN - ON TAXI OUT NR 1 ENGINE FLAMED OUT. RETURNED TO THE GATE. MAINTENANCE RESTARTED ENGINE AND IT OPERATED NORMALLY. INTERROGATED MDC ENGINE EXCEEDENCE FOUND R ENG ITT ROSE TO 1102 C DEGREES FOR 4.4 SEC DURING OPERATION. C/W INSPECTION OF ENGINE OPERATED ABOVE ITT LIMITS IAW GE MM SUBTASK TR 22-0025 72-00-00-280-003 FOUND OVER TEMP EXCEEDENCE AT IDLE IN FIGURE 801 SHEET 3 AREA B2 DURING TAXI STALL C/W OP CHECK NR 2 ENG IAW 22-00-00-260-014 GE MM ALL PARAMETERS NORMAL. NO ITT EXCEEDENCE NOTED AFTER FLAMEOUT. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. SCHEDULED BOROSCOPE INSPECTION WITHIN 10 HOURS. 2L72 4F4 FRTA21EA EOOO63EN 20060105003372006010500337EU 2006 1 5 0501893243 120051230A3350 BATTERY AIRBUS320 A320212 3930322EU CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01343NW 387 DURING EMERGENCY LIGHT TEST DISCOVERED EPSU INT LOAD AFT L FAULT INDICATION. REMOVED AND REPLACED BATTERY. OPS CHECKED GOOD. 2L72 4F RTA28NM 20060105003382006010500338NM 2006 1 5 0501922005 120051018A5320 CLIP BOEING747 747251B 1384892NM FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01624US 21706 DURING "M" CHECK, FOUND CRACKS IN INTERCOSTAL ATTACHED SUPPORT CLIP AT BS 340 STR 26L. REPAIRED PER EA 66-205519. 2L74 4F A20WE 20060105003432006010500343NM 2006 1 5 0501966624 120051020A5311 FRAME BOEING747 747251B 1384892NM FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01624US 21706 DURING "M" CHECK, FOUND CRACK ON FRAME AT BS 520 BETWEEN S10 AND S11. REPAIRED PER EA 66-205523. 2L74 4F A20WE 20060105003472006010500347WP 2006 1 5 ABXA060003 120051216A532099236685 STRUCTURE DOUG DC9 DC933F 302207AWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23932AX 47465 FOUND CORROSION ON SUBFLOOR AT FLOORBEAM FS 135, RIGHT BUTT LINE 28 TO 40. REPAIRED CORRODED AREA IAW DC9 SRM 53-01. 2L72 4F A6WE 20060106000012006010600001SO 2006 1 6 C2XA06TY001 120051231A32608005701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL MLG INOPERATIVE A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2713955 145075 PILOT REPORT; LANDING GEAR WOULD NOT RETRACT. AC RETUNED TO FIELD. MAINTENANCE REMOVED AND REPLACED THE NLG UPLOCK PROXIMITY SWITCHES (2 EA). LANDING GEAR EXTENSION AND RETRACTION CHECKS WERE PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20060106000022006010600002SO 2006 1 6 C2XA05SH145 120051231A531014525480003 BEAM EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL CARGO DOORWAY CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2728529 145512 DURING C-CHECK MAINTENANCE FOUND CARGO DOOR CUTOUT BEAM HAS CORROSION. MAINTENANCE REMOVED AND REPLACED CARGO DOOR LOWER CUTOUT BEAM IAW SRM 51-40-02 AND EC 5320-01137. AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20060106000032006010600003SO 2006 1 6 C2XA05SH144 120051231A532014521713605 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO PWA R985 R985* 52008NE FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2728529 145512 DURING C-CHECK, MAINTENANCE FOUND CENTER OMEGA BEAM CORRODED AT RAMP ANGLE FRM 20. MAINTENANCE REMOVED AND REPLACED CENTER OMEGA BEAM FROM FRMS 19-25 IAW SRM 51-40-02. AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2L72 4F3 RRTT00011AT5E1 20060106000052006010600005CE 2006 1 6 DXTA200501173 120051231A3240 BRAKE CESSNA560 560XL 2076702CE PWA 545 PW545A NE MLG VIBRATES E DXTAO OTHER E VIBRATION/BUFFET TXTAXI/GRND HDL 1 GL07648QS 5605574 LT AND RT BRAKES ARE CATCHING AND GRABBING ON BRAKE APPLICATION. LOUD CHATTERING CAN BE HEARD AND THE GRABBING SHAKES THE PLANE. BRAKE WEAR PINS SHOW AMPLE BRAKE WEAR AVAILABLE. BLED LT AND RT BRAKE SYSTEM IAW CE 560XLS MM CHP 32-44-00. TAXI CHECKED GOOD. 2L72 4F4 FRTA22CE E00059EN 20060106000062006010600006CE 2006 1 6 DXTA200501172 120051230A2150 A/C PACK BEECH MU300 400A 1155402CE ODOR E DXTAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07117QS RK391 SMELL OF BURNING RUBBER SMELLED IN THE CABIN WHEN ACFT IS SET TO TAKEOFF POWER. MOST NOTABILY DURING THE FIRST TAKEOFF OF THE DAY. RAN AIRCRAFT WHEN IT FIRST CAME IN (12/30/05) NO SMELL NOTICED. RAN AGAIN FIRST THING THE NEXT DAY (12/31/05) NO SMELL NOTICED IAW MFG CH 21-00-00 AND STANDARD SHOP PRACTICES. 2H72 4F RTA16SW 20060106000082006010600008EA 2006 1 6 COMA0560753 120051230A5347601R3103215 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE BS 363-398 CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA29272 7031 FLOOR SEAT RAIL CORRODED FROM FS363 TO 398. REPAIRED LT FWD SEAT TRACK FROM FS363 TO 398 BY REMOVING AND REPLACING SEAT TRACK IAW CRJ 200 AMM 53-01-11-000-802 AND 53-01-11-400-802. 2L72 4F4 FRTA21EA E15NE 20060106000122006010600012EU 2006 1 6 DHL2005362012 120051220A3260BED2011 PROXIMITY SENSOR AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE LT MLG INOPERATIVE A DHLAO OTHER P NO WARNING INDICATION NRNOT REPORTED 1 SO01362DH 84 FRONT PANEL LANDING GEAR GREEN DOWN AND LOCKED INDICATOR NOT ILLUMINATED (LT MAIN) LIGHT TEST OK NR 2 SYSTEM OK. REMOVED AND REPLACED PROXIMITY DETECTOR UNIT SYS OPS CHECKED SERVICEABLE ON GRD IAW M/M 32-61-12 2L72 4F4 FRTA35EU E23EA 20060104001242006010400124CE 2006 1 4 DJFA2005175 120051204A2750656517547CR CABLE CESSNA500 560CESSNA 2076750CE PWA JT15 JT15* 52060NE TE FLAPS BROKEN E DJFAK NONE O OTHER ININSP/MAINT 1 EA23525CW 5600225 DURING AN UNSCHEDULED MAINTENANCE VISIT WHILE TROUBLESHOOTING A FLAP INDICATION DISCREPANCY, THE FLAP POSITION FOLLOW-UP CABLE WAS FOUND TO BE BROKEN. THE CABLE WAS REPLACED AND ADJUSTED. OPERATIONAL CHECKS OF THE FLAP SYSTEM WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 TRTA22CE E1NE 20060104001262006010400126CE 2006 1 4 BSYR200500028 120051106A273196526013625 ACTUATOR BEECH 58 58 1152740CE CONT O520 IO520C 17032SO TRIM TAB FROZEN E BSYAD RETURN TO BLOCK F FLT CONT AFFECTED TOTAKEOFF 1 GL074098S TH600 ON TAKEOFF, ELEVATOR TRIM FROZE UP, RETURNED. MAINTENANCE CHANGED LT TRIM TAB ACTUATOR OPS CHECKED GOOD. 1L72 3O3 O 3A16 E5CE 20060104001282006010400128CE 2006 1 4 BSYA20050034 120051220A5210 DOOR BEECH 58 58 1152740CE CONT O520 IO520* 17032SO CREW OPEN E BSYAA UNSCHED LANDING O OTHER CLCLIMB 1 GL073695V TH1183 ON DEPARTURE, PILOTS DOOR POPPED OPEN, PILOT RETURNED TO BLOCK REOCCURRED DOOR AND CONTINUED ON WITH FLIGHT. 1L72 3O3 O 3A16 E5CE 20060104001332006010400133NE 2006 1 4 AT0500045 220051201A7200BR700715A130 ENGINE BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE NR 2 INOPERATIVE A ZZDAE ENGINE SHUTDOWN O OTHER CLCLIMB 1 SO15948AT 55011 DURING CLIMB OUT, AT ABOUT 18,500 FT, 2 LOUD BANGS HEARD, RT ENGINE SPOOLED DOWN, EGT ROSE, SEVERE DAMAGE SUSPECTED RAN QRH. REMOVED AND REPLACED NR 2 ENGINE IAW TC 603. ALL OPS NORMAL. A/C OK FOR SVC. 2L72 4F4 FTRA6WE E00061EN 20060104001352006010400135NM 2006 1 4 05FDEA04176 120051208A5315 FLOORBEAM BOEING727 727 UTILSYSNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 MAIN CABIN FLOORBEAM HAS CORROSION AT FASTENER HOLES AT STA BS1130 BETWEEN RBL14 AND RBL40. REPAIRED OUT OF LIMTS SECTION OF STA BS 1130 FLOORBEAM IAW SRM 53-10-8 FIGURE 10. ALODINED AND PRIMED BARE METAL AREAS IAW SRM 51-10-2. INSTALLED REPAIR WITH WET FASTENERS IAW SRM 51-30-2. THIS IS A MAJOR REPAIR SIGNED BY MECH NR 98236 AND QC261. REFERENCE N00970. 2L73 4J4 FRTA3WE E2EA 20060104001372006010400137NM 2006 1 4 05FDEA04147 120051205A5320655612911 STRUCTURE BOEING727 727* NM PWA JT8 JT8D9A 52048NE ZONE 100 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 AFT CARGO DOOR, LOWER CHORD, UPPER TEE CAP AT STA BS 950D TO BS 950E, ABOVE STRINGER 27-R HAS SEVERAL HOLES WITH NO EDGE DISTANCE AND MINIMUM SPACING. REPAIRED DAMAGED CHORD IAW B727 SRM 51-40-4 FIGURE 1. REMOVED AND REINSTALLED 4 EACH CHORD FITTINGS, FILLER STRAPS, CHORD TEE AFTER REPAIR WAS ACCOMPLISHED IAW SRM 51-30-2.ALSO REMOVED AND REINSTALLED STA BS 950D TO BS990 TRANSITION PANEL IAW SRM 51-30-2 AND BAC DWG NR 65-56129. THIS IS A MAJOR REPAIR SIGNED BY MECH NR 7713 AND QC281 REFERENCE SNRM N00890. 2L73 4F4 FRTA3WE E2EA 20060104001392006010400139NM 2006 1 4 05FDEA04406 120051222A5311 FRAME BOEING727 727100 1384036NM PWA JT8 JT8D7B 52053NE BS 1030 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 AFT CARGO COMPARTMENT, FRAME IS DENTED BETWEEN STR. 24 LT AND 27 LT BS 1030 ON IB FLANGE. REPAIRED IAW SRM 51-40-3. 2L73 4F4 FRTA3WE E2EA 20060104001412006010400141NM 2006 1 4 05FDEA04145 120051205A5753 FLAP TRACK BOEING727 727200 138407ENM PWA JT8 JT8D9A 52048NE NR3 FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 N01126 LT WING IB FLAP OB FLAP TRACK CORRODED ON AFT ATTACH POINT. ** SD ** COMING REPLACED FLAP TRACK IAW W/C 27X5705-03 2L73 4F4 FRTA3WE E2EA 20060104001442006010400144NM 2006 1 4 05FDEA04159 120051206A5320 STRAP BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE TENSION STRAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 CORROSION ON TENSION STRAP BS 1070 RBL 45 WL 201. REPAIRED TENSION STRAP IAW SRM 53-10-8 FIG 6. 2L73 4F4 FRTA3WE E2EA 20060105000232006010500023EA 2006 1 5 SWIA200516055 120051229A271010231007 FLUTTER DAMPER CNDAIRCL600 CL6002B19 1900309EA AILERONS LEAKING A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07965SW5396 5396 7871 INTERMITTENT FLUTTER DAMPER STATUS MESSAGE. REPLACED RT AILERON FLUTTER DAMPER IAW MM 27-15-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20060105000362006010500036NM 2006 1 5 2005UALA01509 120051223A2613 WARNING LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 1 ENGINE ILLUMINATED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP2987UA 26713 RETURNED TO MCI, DUE TO NR 1 ENGINE OVERHEAT LIGHT. REPLACED CARD M10224 AND RESEATED M10229 AND M10276. CHECKED ENG DUCTING WITH APU AIR ON AND NO LEAKS FOUND. SHOOK LOOP WHILE WATCHING LIGHT AND OK 2L72 4F4 FRTA2NM E17NE 20060105000442006010500044EU 2006 1 5 RAIA00512039 120051221A3350 CONTACT JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT DIRTY A RAIAK NONE O OTHER ININSP/MAINT 1 CE03574HK 41093 POST FLT 5468 - STL - FORWARD CABIN EXIT EMERGENCY LIGHT. MAINTENANCE REPAIRED CONTACT AT FWD EMERGENCY EXIT LIGHT ASSEMBLY. 2L72 4T RTA41NM 20060105000452006010500045SO 2006 1 5 RAIA00512040 120051221A3350 BULB EMB 145 EMB145 3260210SO EMERGENCY LIGHT INOPERATIVE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03801HK 145053 PRE FLT 3526 - RIC - EMERGENCY LIGHT ABOVE EXIT ROW INOP. MAINTENANCE REPLACED THE BULB. 2L72 4F RTT00011AT 20060105000632006010500063 2006 1 5 2005UALA01522 420051226A2200 FMC BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE COCKPIT WARNING LIGHT A UALAO OTHER J WARNING INDICATION CLCLIMB 1 WP29905UA 25005 FAIL ANNUNCIATOR IS ON, ON FMS CDU'S AND SCREENS DISPLAY 'FMC'. CREW COMMENTS: DUAL FMC FAILURE AT LIFTOFF. AFTER 10 MINS SYSTEM RETURNED. NO CB'S PULLED. THE 737 AIRCRAFT OPERATED BY UNITED AIRLINES HAVE ONLY A SINGLE FMC SYSTEM, THUS THIS WRITEUP IS ERRONEOUS. A SINGLE SYSTEM ERROR WAS SEEN ON BOTH CDUS. THE SYSTEM RETURNED TO NORMAL OPERATION WITHOUT CREW ACTION, AND OPERATIONALLY CHECKED GOOD BY GROUND MAINTENANCE. NO FURTHER MAINTENANCE ACTIONS WERE TAKEN. THE SYSTEM HAD NO HISTORY, AND HAS HAD NO SUBSEQUENT MALFUNCTIONS 2L72 4F4 FRTA16WE E2GL 20060105000752006010500075SO 2006 1 5 RAIA00512034 120051218A3350 BULB EMB 145 EMB145 3260210SO EMERGENCY LIGHT INOPERATIVE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03803HK 145077 PRE-FLT 3546 - RIC - SERVICE DOOR EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE SERVICE DOOR LIGHT BULB. 2L72 4F RTT00011AT 20060105000762006010500076EU 2006 1 5 RAIA00512042 120051222A3397 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT LOOSE A RAIAK NONE O OTHER ININSP/MAINT 1 CE03571HK 41090 PRE FLIGHT 5415 - STL - ESCAPE PATH LIGHTING INOP. MAINTENANCE RESECURED LOOSE CONNECTION AT LIGHT STRIP. 2L72 4T RTA41NM 20060105000812006010500081NM 2006 1 5 2005UALA01527 120051220A2613 WARNING LIGHT BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE BLEED OVERHEAT ILLUMINATED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29666UA 29238 RETURNED TO FIELD DUE TO LEFT BLEED OVERHEAT INDICATION. THE WING DUCT LEAK DETECTORS TS211 & TS212 WERE REPLACED. DURING TROUBLESHOOTING THE SENSOR THAT WAS CAUSING THE FAULT COULD NOT BE DETERMINED SO BOTH WERE REPLACED. THE REMOVED PARTS ARE NON-STOCK, NO FURTHER ANALYSIS. AS OF 09FEB06 THIS WAS THE ONLY ABNORMALITY REPORTED IN AMIS FOR CHAPTER 26. AN 8-IN CRACK WAS FOUND IN THE DUCT CAUSING BLEED AIR LEAKAGE AND "BODY DUCT LEAK" EICAS MESSAGE TO APPEAR. THE DUCT WAS REPLACED. 2L72 4F4 FRTA1NM E24NE 20060105000882006010500088NM 2006 1 5 2005UALA01533 120051229A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29117UA 28810 DRS 1R AND 3R HAVE ONE THRESHOLD EMERGENCY LIGHT OUT. 2L74 4F4 FRTA20WE E24NE 20060105000902006010500090NM 2006 1 5 2005UALA01534 120051229A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29117UA 28810 EMERGENCY LT AT 43 ABC INOP. 2L74 4F4 FRTA20WE E24NE 20060105000982006010500098NM 2006 1 5 USAA051647 120051229A5510 CLEVIS BOEING737 7374B7 1384702NM HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19781AU 25020 FOUND CORROSION CLEVIS R3 ON HORIZ STAB. REMOVED CORROSION; REPLACED BUSHING PER SRM 55-10-10, DEFECT SIZE: 2". 2L72 4F RTA16WE 20060105001182006010500118EA 2006 1 5 ASOA051026 120051113A5300 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA BS 484 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27914EV 7752 DURING A C-CHECK IN TUS, THE FS 484 INTERCOSTAL, AT BL 36, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FS 484 INTERCOSTAL, AT BL 36, IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20060105001202006010500120EA 2006 1 5 ASOA051029 120051127A3350362624 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27852AS 7369 DURING A GROUND INSPECTION IN ATL, THE EMERGENCY FLOOR LIGHT, AT ROW 5, WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT STRIP, AT ROW 5. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060105001272006010500127EA 2006 1 5 A6WA200540357 120051220A3220 LANDING GEAR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NOSE MALFUNCTIONED A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31442AW 7778 AFTER GEAR RETRACTION, NOSE GEAR WOULD NOT RETRACT, GEAR RETRACTION HORN SOUNDED. C/W QRH LANDED IN MSP AT 42000. MEL`D GEAR RET SYS FUNCTION TESTED GEAR SYS. PERFORMED GEAR DISAGREE TEST, FULLY SERVICED NLG STRUT.. PERFORMED LANDING GEAR EXT/RETRACT FUNCTION TEST NUMEROUS TIMES, NO FAULTS NOTED. REMOVED FROM MEL. (K) 2L72 4F4 FRTA21EA E15NE 20060105001302006010500130EA 2006 1 5 A6WA200540362 120051227A2750 DCU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31419AW 7633 AFTER DEPARTURE, UPON FLAP RETRACTION, FLAP FAIL CAUTION MESSAGE APPEARED ON ED1 FLAP POSITION INDICATION ON ED1 READS ZERO DEGREES, FLIGHT CONTROL PAGE ALSO READS ZERO ON ED2. RETURN TO DEPARTURE FOR (FLAP ZERO LANDING). FOUND GROUND PROXIMITY MESSAGE ON MDC CH1 AND CH2. SHOOK WIRING FROM LT BPSU TO FECU - NO DEFECTS. EXCEPT POT NR 6GH7 OUT OF TOLERANCE. ADJ FECU POT 6.7 IAW. REMOVED AND REPLACED DCU NR 1, OK FOR SERVICE. HES INSPECTION NOT REQUIRED IAW MM. (K) 2L72 4F4 FRTA21EA E15NE 20060105001372006010500137NM 2006 1 5 AMTA200501040 120051108A5320 FLOOR SUPPORT BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE BS 1660-1680 CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11518AT 27974 STA 1660-1680, 0 BL - FLOOR SUPPORT CORRODED. REMOVED CORROSION FROM FLOOR SUPPORT AND FOUND TO BE OUT OF LIMITS IAW SRM. REMOVED AND REPLACED NEW CHANNEL IAW SRM AT STA 1660-1680, BL 0. GAGE USE A2571. (K) 2L72 4F4 FRTA2NM E12EU 20060105001382006010500138NM 2006 1 5 AMTA200501094 120051121A3397 PIN BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE EMERGENCY LIGHT DAMAGED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11514AT 27971 ESCAPE PATH LIGHTING SYSTEM DAMAGED AT SEAT 9D. REINSTALLED PIN AT LIGHT ASSY OPS, OK. (K) 2L72 4F4 FRTA2NM E12EU 20060105001472006010500147NM 2006 1 5 AMTA200501047 120051108A5320 SUPPORT BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE R-4 DOOR DRAIN CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11518AT 27974 R-4 DOOR DRAIN SUPPORT STA 1648 TO 1670, RBL 57, CORRODED. REMOVED CORROSION FOUND TO BE WITHIN LIMITS TREATED. (K) 2L72 4F4 FRTA2NM E12EU 20060105001542006010500154NM 2006 1 5 AMTA200501087 120051119A3397 WIRE BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE EMERGENCY LIGHTSDISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11514AT 27971 SEAT ROW 28DEF TO 31DEF EGRESS LIGHTS INOPERATIVE. FOUND DISCONNECTED WIRE RECONNECTED WIRE IAW AMM. OPS CHECK NORMAL. (K) 2L72 4F4 FRTA2NM E12EU 20060105001672006010500167GL 2006 1 5 I5HA058009 220051125A7200501D13 ENGINE CVAC 340 340CVAC 242270AWP ALLSN 501D 501D13 03004GL SHUTDOWN A I5HAO OTHER O OTHER NRNOT REPORTED 1 GL23584E 24 500726 WHILE ENROUTE, THE CREW OBSERVED THE LT OIL QUANTITY GO TO ZERO. THE CREW PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN AND DIVERTED. INSPECTION REVEALED OIL LEAKING FROM THE STRATER O`RING. THE O`RING WAS REMOVED AND REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. (K) 2L72 4R4 T 6A6 E282 20060105001852006010500185EA 2006 1 5 SWIA200515928 120051128A27518004301 DETECTOR CNDAIRCL600 CL6002B19 1900309EA T/E FLAP MALFUNCTIONED A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07408SW 7055 FLAPS DEGRADED MSG. REPLACED SKEW DETECTOR UNIT. OPERATIONAL CHECKS GOOD. IAW 27-51-15. 2L72 4F RTA21EA 20060105001962006010500196WP 2006 1 5 ABXA050309 120051108A53205644678 TRIPLER DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 EXISTING TRIPLER CORRODED AT STA 857, RT BUTT LINE 50. FABRICATED TRIPLER AT STA 857, RT BUTT LINE 50 IAW REA D853-52539. MATERIAL USED .190 7075-T6, P/O NR 1073367. 2L74 4F4 F 4A25 1E8 20060105001982006010500198WP 2006 1 5 ABXA050299 120051101A57145759321501 DOUBLER DOUG DC8 DC863F 302198FWP CENTER WING CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DOUBLER CORRODED TOP OF WING CENTER SECTION PRESSURE DECK, STA. 683, RT BUTT LINE 10. REMOVED CORROSION, FABRICATED AND INSTALLED DOUBLER IAW SRM 51-1-8 AND REA D853-52529. 2L74 4F 4A25 20060105002242006010500224EA 2006 1 5 COMA0560759 120051231A5730601R100463 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE LT WING CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA29272 7031 AFT WING PLANK, FUEL BOOST PUMP SATELLITE HOLE NR 7 HAS CORROSION DAMAGE. INCORPORATED REPAIRS IAW REO 601R-57-21-169 REV B. 2L72 4F4 FRTA21EA E15NE 20060105002262006010500226NM 2006 1 5 UPS06445908 120051230A712065B903604 THRUST LINK BOEING747 747121 1384871NM PWA JT9 JT9D7A 52054NE NR 2 ENGINE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 AD CRACK INDICATIONS FOUND AT NR2 ENG MOUNT THRUST LINK THE INDICATIONS LOCATED AT FWD AND AFT LUG BORE WHICH WERE EXCEEDED THE LIMITS. THRUST LINK REPLACED REF MM 71-21-03. 2L74 4F4 F A20WE E20EA 20060105002352006010500235WP 2006 1 5 DHL2005803524 120051203A5320 CHANNEL DOUG DC8 DC873 302199CWP GE CFM56 CFM562C 13802NE BS 1420-1460 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 NR. 033035: AFT CARGO COMPT. (D) BELLY DOOR JAMB CHANNEL CRACKED 0.250 INCH, STA 1420.000, STA 1460.000. REMOVED CRACKED CHANNEL IAW SRM 51-1-21, SRM 51-3-0. FABRICATED NEW CHANNEL (2024T3 AL 0.050 INCH) IAW SRM 53-2-0. CLEANED, TREATED AND PRIMED AREA AND CHANNEL IAW SRM 51-1-8B. INSTALLED NEW CHANNEL IAW SRM 51-1-21, SRM 51-3-0 2L74 4F4 FRT4A25 E2GL 20060105002402006010500240EU 2006 1 5 DHL2005367005 120051124A3260141FL01D3 DOWNLOCK SWITCH AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE MLG INOPERATIVE A DHLAO OTHER O OTHER APAPPROACH 1 SO01367DH 265 DURING THE APPROACH THE LANDING GEAR WAS EXTENDED AND THE GREEN NOSE GEAR DOWN LIGHT ON THE FWD CENTER PANEL DID NOT ILLUMINATE. THE GREEN NOSE GEAR DOWN LIGHT DID ILLUMINATE ON THE SECOND OFFICERS PANEL. REMOVED AND REPLACED NOSE GEAR DOWN AND LOCKED SWITCH 40GB IAW MM 32-00-00. CHECKED GOOD. (SW. P/N 141FL01D3) 2L72 4F4 FRTA35EU E23EA 20060105002412006010500241NM 2006 1 5 WRNA20050028 120051201A3246 FUSE BOEING747 747200 1384847NM PWA JT9 JT9D7J 52054NE MLG BLOWN A WRNAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO05524UP 21446 TAKEOFF WARNING WENT OFF AT 140 KTS. ABORTED TAKEOFF. NR1,3,5,6, AND 7 MLG WHEEL ASSY'S THERMAL FUSE PLUG DISCHARGED AFTER RETURNING TO GATE. FREIGHT REMOVED FROM AIRCRAFT. PERFORMED TAKEOFF WARNING SYSTEM CHECK IAW 31-26-00 PGS 101 AND 501. SYSTEM OPS NORMAL, NO IRREGULARITIES NOTED. NR1,3,5,6,7 TIRE ASSY'S REMOVED AND REPLACED IAW 32-45-01. NR4, 2, 8 WHEEL ASSY'S REMOVED FOR INSPECTION. AXLE INSP PERFORMED IAW 5-51-10/201, ALL SATISFACTORY. BRAKE ASSY'S WERE REMOVED AND INSPECTION PREFORMED IAW 32-41-15/601. AIRCRAFT RETURNED TO SERVICE. 2L74 4F4 FRTA20WE E20EA 20060105002632006010500263EU 2006 1 5 05FDEA04092 120051203A5101 REPAIR AIRBUS310 A310 EU GE CF6 CF680A3 30025NE FUSELAGE NONE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25424FE 241 PREVIOUS REPAIR INSTALLED AT FUSELAGE LT SIDE AT STA 1923, FR35, STR 22LT. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR CONFORMS TO AN EXISTING FEDEX ENGINEERING AUTHORIZATION 6-5330-94663 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR. 2L72 4F4 FRTA35EU E13NE 20060105002662006010500266SO 2006 1 5 143612042005 120051204A3250 STEERING SYS GULSTMG1159 GIV 3980115SO RROYCETAY TAY6118 EU NLG MALFUNCTIONED E N93AK NONE O OTHER TXTAXI/GRND HDL 1 SO13436QS 1436 STEERING LAGS WHEN TURNED TO LT WITH TILLER OR RUDDER PEDALS. PERFORMED ADJUSTMENT CHECK IAW MM 32-05-00. 2L72 4F4 FRTA12EA E25NE 20060105002672006010500267NM 2006 1 5 MZZA0500015 120051205A2560ACREM1A MEGAPHONE BOEING737 737824 13844BZNM GE CFM56 CFM56* 13802NE CABIN INOPERATIVE A MZZAK NONE O OTHER ININSP/MAINT 1 WP1313227 28788 INSPECTION FOUND FORWARD CABIN MEGAPHONE INOPERATIVE. THE MEGAPHONE WAS REMOVED AND REPLACED IAW MM 25-64-00. 2L72 4F4 FRTA16WE E2GL 20060105002802006010500280SO 2006 1 5 CHQA200500206 120051205A33501317 LIGHT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL EXTERIOR INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11570RP 14500821 EMERGENCY LIGHT ON RT FUSELAGE OUT. RELAMPED EMERGENCY COURTESY LIGHT ON RT WING. OPS CHECK GOOD IAW MM 33-50-09. 2L72 4T4 FRTT00011ATTE6CH 20060105002882006010500288NM 2006 1 5 05FDEA04154 120051206A5320651627910 BEAM BOEING727 727227 1384078NM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 SEAT TRACK ATTACH TEE CAP HAS CORROSION OUT OF LIMITS AT LBL45 FROM STA BS760 TO STA BS850. REMOVED SEAT TRACK FROM BS 740 TO BS850 AT LBL45 IAW SRM 51-30-2. REMOVED, REPLACED AND INSTALLED NEW UPPER CHORD FROM STA BS 760 TO STA BS850 AT LBL45 IAW BAC DRAWING NR 65-16279 AND SRM 51-30-2. REINSTALLED SEAT TRACK SECTION FROM STA BS 740 TO STA BS850 AT LBL45 IAW B727 SRM 51-30-2. THIS IS A MAJOR REPAIR SIGNED BY MECH NR 110487 AND QC303 REF SNRM N01130. 2L73 4F4 F A3WE E2EA 20060105002892006010500289NM 2006 1 5 05FDEA04155 120051206A5315 FLOORBEAM BOEING727 727227 1384078NM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 CABIN FLOORBEAM UPPER TEE CAP CORRODED AT STA BS 344 BETWEEN LBL24 AND RBL24. CUT OUT CORRODED SECTION OF TEE CAP FROM LBL45 TO RBL24 IAW SRM 53-10-8 FIGURE 9. FABRICATED NEW TEE SECTION AND SPLICE ANGLES IAW SRM 53-10-8 FIGURE 9. ALODINED AND PRIMED REPAIR PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 51-30-2. THIS IS A MAJOR REPAIR SIGNED BY MECH NR 98629 AND QC281 REF SNRM N00598. 2L73 4F4 F A3WE E2EA 20060105003012006010500301EU 2006 1 5 05FDEA04168 120051207A5320 PANEL AIRBUS310 A310 EU GE CF6 CF680A3 30025NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 NOSE GEAR WELL, FWD WALL HAS 13 SPOTS OF LIGHT CORRODED AND SEVERAL SMALL SPOTS OF BARE METAL. REF N00747, REPAIRED NOSE LANDING GEAR BAY FORWARD PANEL BY REPLACING IAW REPAIR INSTRUCTION R53611077 AND NLG BAY PANEL REPLACEMENT, DWG R53610532. (K) 2L72 4F4 FRTA35EU E13NE 20060105003192006010500319NE 2006 1 5 ANCF200400063 220051120A7200JT8D219 ENGINE DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE LEFT UNKNOWN W ANCFE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SO23EICEP13268746 53122 P728180D DURING CRUISE FLIGHT AT FL 310, LT OIL PRESS LIGHT CAME (ON) ON EOAP. LT OIL PRESS INDICATION FELL TO 0 WITH (35) AND (40) LIGHTS ON. LT OIL QUANTITY WAS NORMAL INDICATING 16 QTS. LT OIL TEMPERATURE REACHED 131. LT ENGINE WAS SHUTDOWN, FOLLOWING THE CHECKLIST AND REMAINED IN THIS CONDITION FOR 50 MINUTES UNTIL LANDING DURING WINDMILLING. LT OIL PRESS REMAINED IN 0. LOW OIL QUANTITY INDICATING 16 QTS AND LT OIL TEMP REMAINED 96. LT ENGINE WAS REPLACED IAW EWO NR 83-72-6438. ENGINE REMOVAL AND INSTALLATION. TEST SATISFACTORY IAW AMM 71-00-00 PAGE 501. 2L72 4F4 FRT E9NE 20060105003312006010500331EA 2006 1 5 QXEA200501855 120051226A2910 HYDRAULIC LINE CNDAIRCL600 CL6002C10 1390015EA HYDRAULIC SYS CRACKED A QXEAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 NM09290RB 10029 ONT- ON FLIGHT 2515, HYDRAULIC NR 1 LOW PRESS MESSAGE CAME ON INFLIGHT. LOSS OF ALL NR 1 SYSTEM HYDRAULIC FLUID. SYSTEM RAN DRY FOR 25 MINUTES. LANDED WITHOUT INCIDENT. INSPECTED, FOUND HYDRAULIC NR 1 PRESSURE LINE TO GROUND SPOILER SELECTOR VALVE CRACKED AT BEND ABOVE FLAP DRIVE SHAFT 6" OUTBOARD OF FLAP PDV. REPAIRED DAMAGED TUBING BY DEOTECH PERMASWEDGE FITTINGS IAW CRJ-700 TASK 20-30-00-910-802-A01. SERVICED AND BLED IAW 12-12-29-611-801 AND 29-10-00-870-801-A01. GROUND RAN A/C AND OPERATED GROUND SPOILERS, NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20060105003322006010500332EA 2006 1 5 QXEA200501856 120051230A32504480000501 ECU CNDAIRCL600 CL6002C10 1390015EA NLG STEERING MALFUNCTIONED A QXEAK NONE J WARNING INDICATION LDLANDING 1 NM09600QX2895 1216 10005 BUR - FLT 2507 "STEERING INOP" CAUTION MSG DURING CRUISE. LANDED W/O INCIDENT WITH NLGE STEERING INOP. RESET PER CRJ-700/900-SL-32-019 REV B. NO FURTHER FAULTS NOTED. REPEATED THE SAME DAY ON FLT 2504. INTEROGATED MDDC DID NOT FIND ANY CURRENT NOSE WHEEL INOP CAUTION MSG. WENT TO A/C HISTORY PAGE AND FOUND MULTIPLE POSTING OF NOSE WHEEL STEERING LNWS CAT MTOGG STEERING R NWS ACT MT098 LVDT OPEN OR SHORT AND NWS ECU/ NO LA-10C-6BUS INPUT. PERFORMED CRJ 700 FIM TASK 32-51-10-7801-807-A01 FOR T/S, DID CONTINUITY CHECK OF CONNECTORS A164P2 PIN 24 TO A12P5 PIN 51 AND A164 P3 PIN 25 TO A12 P5 P[IN 52 CONTINUITY CHECKS GOOD, REMOVED AND REPLACED ECU (NWS ELEC CONTROL) IAW CRJ 700 AMM TASK 32-51-10-000-801-A01 AND2L72 4F RTA21EA 20060105003362006010500336NM 2006 1 5 0501883116 120051228A335032145410 POWER SUPPLY AIRBUSA319 A319114 3930350NM CABIN DISCHARGED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01316NB 1249 EMERGENCY LIGHT TEST FAILED, FAULT SHOWS EPSU INT LOAD EMER R. RELAMPED CABIN EMERGENCY LIGHTS RIGHT CABIN AND REPLACED EPSU 12WL PER 33-51-39-000-001. OPS CHECKED GOOD. 2L72 4F RTA28NM 20060105003392006010500339NM 2006 1 5 0501936624 120051019A5312 BULKHEAD BOEING747 747251B 1384892NM FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01624US 21706 DURING "M" CHECK FOUND CRACK IN CANTED BULKHEAD WEB AT BS 260 ST 26L. REPAIRED PER EA 66-205518. 2L74 4F A20WE 20060105003412006010500341NM 2006 1 5 0501946624 120051016A5311 FRAME BOEING747 747251B 1384892NM FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01624US 21706 DURING "M" CHECK, FOUND CRACK IN FRAME AT BS 2231 S26L. REPAIRED PER EA 66-205517. 2L74 4F A20WE 20060106000072006010600007EA 2006 1 6 COMA0560754 120051230A5347601R3103215 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE BS 363-398 CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA29272 7031 FLOOR SEAT RAIL CORRODED FROM FS363 TO 398. REPAIRED RT FWD SEAT TRACK FROM FS363 TO 398 BY REMOVING AND REPLACING SEAT TRACK IAW CRJ 200 AMM 53-01-11-000-802 AND 53-01-11-400-802. 2L72 4F4 FRTA21EA E15NE 20060106000132006010600013EU 2006 1 6 DHL2005362013 120051221A3260353251001 INDICATOR AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE LT MLG INOPERATIVE A DHLAO OTHER P NO WARNING INDICATION NRNOT REPORTED 1 SO01362DH 84 LANDING GEAR INDICATOR FORWARD LT MAIN INOP. S/O PANEL INDICATES 3 GREEN. REMOVED AND REPLACED LANDING GEAR IND. UNIT ON CENTER PNL IAW M/M 32-61-14 SYS OPS CHECKED SERVICABLE ON GRD. 2L72 4F4 FRTA35EU E23EA 20060106000182006010600018WP 2006 1 6 DHL2005803529 120051125A5320561610147 CAP DOUG DC8 DC873 302199CWP GE CFM56 CFM562C 13802NE BS -99 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 ITEM REF. NR. 032491: ANTENNA DOPPLER COMPT. CAP 1 INCH CRACK AT STA -99.000. REMOVED CRACKED CAP IAW SRM 51-1-21 PAGE 1, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW CAP IAW SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1 PG. 2. FOR CAP FABRICATION SEE JC EA53100134-001-D (W.O. 600014514) 2L74 4F4 FRT4A25 E2GL 20060106000212006010600021WP 2006 1 6 DHL2005803556 120051216A5730 SKIN DOUG DC8 DC873 302199CWP GE CFM56 CFM562C 13802NE WS 69.5 LT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 PERFORM PREVENTATIVE MODIFICATION IAW SB 57-88 REV. 3 ON LT WING LOWER SKIN CRACK AT STA 69.5 REF. SB AND DRAWING JO 60095-506. PERFORMED PREVENTATIVE MODIFICATION IAW AD80-22-01, SB 57-88 REV. 3 DWG NR JO60095-506. REMOVED FASTENERS AND SKI FITTING IAW DWG JO60095-506, SRM 51-3-0, SRM 51-1-20D. PERFORMED NDT INSPECTION IAW NDT SPM PART 6-10-01-001. NO CRACK FOUND (ENCLOSED SMN FORM 242-2). INSTALLED DOUBLER, TRIPLER AND SKI FITTING (NEW) IAW DWG DACO JO60095-506, DPS 3.67-56, SRM 51-1-22, SRM 51-1-26, SRM 51-1-11 PAGE 9, SRM 51-3-0, SRM 51-1-20D, SRM 51-3-1. FOR FUEL LEAK CHECK SEE NR 39054. 2L74 4F4 FRT4A25 E2GL 20060106000232006010600023WP 2006 1 6 DHL2005803534 120051203A5315 FLOORBEAM DOUG DC8 DC873 302199CWP GE CFM56 CFM562C 13802NE BS 960 MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01803DH82180 46123 WING CTR SECTION FLOORBEAM HOLES (2EA) MISDRILLED STA 960.000 LBL 9.625 INCH, LBL 15.250 INCH(MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 11-30-05 DWG AA33-53-R05 REV JR DATE 11-22-05. DRILLED MISDRILLED HOLES (2EA) TO 0.250 INCH AND 0.290 INCH AND FABRICATED REPAIR STRAP (7075T6 511 0.250 INCH) IAW DWG AA33-53-R05. CLEANED, TREATED AND PRIMED AREA AND REPAIR STRAP IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11. INSTALLED REPAIR STRAP IAW DWG AA33-53-R05, SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1. 2L74 4F4 FRT4A25 E2GL 20060106000242006010600024WP 2006 1 6 DHL2005803528 120051203A5753 PANEL DOUG DC8 DC873 302199CWP GE CFM56 CFM562C 13802NE LT TE FLAP WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 LT IB FLAP UPPER PANEL PLATING WORN 1 INCH APPROX AT STA XW 92.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 12-02-05, DWG AA33-53-R03 REV. JR DATE 11-11-05. REMOVED DAMAGED EXISTING SOLID SEGMENT PLATING IAW SRM 51-1-21. FABRICATED NEW SOLID SEGMENT PLATING (AL2024T3 0.050 INCH) INTERNAL SPLICE (AL2024T3 0.063 INCH) IAW DWG AA33-53-R03. CLEANED, TREATED AND PRIMED AREA INTERNAL SPLICE AND SOLID SEGMENT PLATING INTERNAL PART IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED REPAIR PARTS IAW DWG AA33-53-R03, SRM 51-1-21, SRM 51-3-0, SRM 51-3-1. 2L74 4F4 FRT4A25 E2GL 20060106000262006010600026WP 2006 1 6 DHL2005803545 120051208A534047518201 FITTING DOUG DC8 DC873 302199CWP GE CFM56 CFM562C 13802NE BS 781 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 ITEM REF. NR. 038748: WING CTR. SECTION FITTING CRACKED STA 781.000 (NR5 TRACK). REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D. TORQUED IAW SRM 51-3-1 PG. 2A. FOR FITTING FABRICATION SEE JC EA53100136-001-D (W.O. 600014514). 2L74 4F4 FRT4A25 E2GL 20060106000372006010600037 2006 1 6 200512102 420051210A221017028314403 AUTOPILOT SYS EMB ERJ170ERJ170100 EU MALFUNCTIONED A UHLAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 GL17641RW2381 2381 17000062 LT AILERON HARD TO MOVE AFTER AUTOPILOT DISENGAGED. 2L74 4F RTA56NM 20060106000382006010600038EU 2006 1 6 200512111 120051211A3620 WARNING SYSTEM EMB ERJ170ERJ170100 EU GE CF34 CF348E5 30015NE COCKPIT ACTIVATED A UHLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL17646RW 17000066 ON CLIMB CREW REPORTED ENGINE 11 AND ENGINE 2 BLEED LEAK INDICATION. 2L74 4F4 FRTA56NM E00063EN 20060106000392006010600039EU 2006 1 6 0501683259 120051211A2910 HYDRAULIC LINE AIRBUS320 A320212 3930322EU GREEN SYS LEAKING A NWAAO OTHER K FLUID LOSS CRCRUISE 1 GL01359NW 846 INBOUND, CREW REPORTED A TOTAL LOSS OF THE GREEN HYDRAULIC SYSTEM FLUID. EMERGENCY DECLARED DUE TO LOSS OF NOSE WHEEL STEERING. MAINTENANCE DISCOVERED A HYDRAULIC RIGID PRESSURE LINE IN NR 1 PYLON LEAKING. LOG PAGE INDICATES LEAK CAUSED BY CLAMP. TEMPORARILY REPLACED THE RIGID HYDRAULIC LINE WITH TWO FLEX LINES P/N 00-0550-3-0484 AND 00-0550-3-0481 AND REDUCER P/N MS21916J8-6. LOG DEFERRED TO MONITOR. 2L72 4F RTA28NM 20060106000422006010600042NM 2006 1 6 P5CA0501418 120051109A3244 TIRE BOEING747 7472F6B 1384807NM GE CF6 CF650* 30018NE LANDING GEAR BLOWN A P5CAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 EA15534MC 21832 ON TAKEOFF ROLL, CREW HEARD 2 LOUD BANGS AND LOST NR1 HYDRAULIC SYSTEM. FOUND 8 BLOWN TIRES, REPLACED 12 TIRES AND 3 BRAKES IAW MM 32-45-01 AND 32-45-15, ACCOMPLISHED CONDITIONAL INSPECTIONS IAW MM 05-51-10 AND 05-51-09. 2L74 4F4 F A20WE E23EA 20060106000442006010600044WP 2006 1 6 DHL2005803541 120051130A533057552713N SKIN DOUG DC8 DC873 302199CWP GE CFM56 CFM562C 13802NE BS 160 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 EXTERIOR FUSELAGE SKIN HAS THREE CRACKS OF 0.75 INCH APPROX AT STA 160.000 L-36 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-4-1 FIG. 5C, MFG DWG NR5779934. REMOVED CRACKED PLATING IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED NEW PLATING (AL2014T6 0.050 INCH) IAW SRM 53-4-1 FIG. 5C, ITEM (A), DWG NR 5779934. CLEANED, TREATED AND PRIMED AREA AND NEW PLATING IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG. 9. INSTALLED NEW PLATING FROM STA 70.000 TO 190.000 IAW SRM 51-1-21, SRM 51-1-20D, SRM 51-3-0. TORQUED IAW SRM 51-3-1. 2L74 4F4 FRT4A25 E2GL 20060106000452006010600045EU 2006 1 6 DHL2005367006 120051127A3260 SWITCH AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE NLG DOOR DIRTY A DHLAO OTHER N FALSE WARNING APAPPROACH 1 SO01367DH 265 NOSE GEAR DOOR LIGHT REMAINED ILLUMINATED AFTER GEAR EXTENSION. CLEANED CONNECTOR ON NOSE GEAR DOOR CLOSE SWITCH. OPS CHECKS SERVICEABLE ON GRD IAW M/M 32-22-11 2L72 4F4 FRTA35EU E23EA 20060106000462006010600046WP 2006 1 6 UPS05845872 120051213A3350 BATTERY PACK DOUG DC8 DC871F 302199DWP CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01718UP 46018 EMERG LIGHTS BATTERY INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, OPS GOOD REF MM 33-50-01-2. 2L74 4F RT4A25 20060106000472006010600047NM 2006 1 6 F3LA200500047 120051212A3610 CONTROLLER AIRBUSA319 A319111 3930336NM CFMINTCFM56 CFM565B5 NE BLEED AIR SYS MALFUNCTIONED A F3LAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM03924FR 2030 BLOCK TURNBACK. FLIGHT CREW REPORTED LOW PRESSURE BOTH ENGINES DURING START WITH FUMES INTO CABIN. REPLACED BMC NR1. LOW BLEED PRESSURE OPS CHECKED GOOD IAW AMM 36-11-34, PAGE 401. FOUND DE-ICE FLUID IN APU AIR INTAKE WHICH WAS CAUSING FUMES. CLEANED APU AIR INTAKE. NO FUMES NOTED IAW AMM 49-16-00-100-003. 2L72 4F4 FRTA28NM E37NE 20060106000482006010600048NE 2006 1 6 DHL2005745013 220051123A7200 SWITCH BOEING727 727224 1384076NM PWA JT8 JT8D9A 52048NE NR 2 ENGINE MALFUNCTIONED A DHLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01745DH 20665 DURING TAKEOFF ENG NR 2 WAS NOT MAKING TAKEOFF THRUST. ENG NR1, NR3 WERE NORMAL AT 80 KTS WITH THRUST LEVERS MATCH, NR2 EPR WAS AT 1.6 NOT INCREASING, N1 WAS ABOVE RED LINE. REJECTED T/O AT 80KTS,170,000 LBS 3860 PRESSURE. ENGINE RUNUP PERFORMED IAW JRH. NR2 ENGINE IDLE SPEED 53.1 PERCENT. ACCELERATION TIME TO T/O POWER 6.5 SECONDS. MAX POWER T/O CHECK,POWER SET AT 2.11 EPR N1 94 PERCENT EGT 545. N2 93 PERCENT FF 8000 LBS ALL INDICATIONS WITHIN NORM. 2L73 4F4 F A3WE E2EA 20060106000492006010600049NE 2006 1 6 DHL2005805005 220051215A7200 ENGINE DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C1 13802NE NR 4 SURGES A DHLAD RETURN TO BLOCK RXJPARTIAL RPM/PWR LOSS ENGINE FLAMEOUT WARNING INDICATION TXTAXI/GRND HDL 1 SO01805DH 46125 AFTER ENG START ON NR1 WITH NORMAL INDICATIONS, DURING NR4 ENG STAT NR1 ENG SURGED THEN FAILED. DURING RESTART ATTEMPT NO FUEL FLOW. INSP FUEL FILTER NO CONTAMINATION NOTED. RAN NR1 ENG IAW JRH 11.8 CROSSFEEDING FROM NR2 MAIN TANK OPS NORM. SW BACK TO NR1 MAIN TANK OPS NORM. NASH PUMP OPS NORM IAW MM 73-10-1. 2L74 4F4 FRT4A25 E2GL 20060106000502006010600050NE 2006 1 6 DHL2005753004 220051203A7230 COMPRESSOR BOEING727 727223 1384074NM PWA JT8 JT8D15A 52051NE ENGINE STALLED A DHLAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SO01753DH 22468 CREW REMARKS NOTED COMPRESSOR STALL ON T/O, ENGINE UNKNOWN. OAT +2 C, P.A. 19FT, TOGW 152,900, IAS 0 (GS EST 10 KNTS) B.E. N/A. INSPECTED INLET AND EXHAUST SECTIONS ON ENGINES 1, 2, AND 3 IAW AOPM CH 1.8 PG. 5, NO DEFECTS NOTED AT THIS TIME. 2L73 4F4 F A3WE E2EA 20060106000522006010600052NM 2006 1 6 DHL2005751007 120051213A3350 BATTERY PACK BOEING727 727264 138408MNM PWA JT8 JT8D* NE EMERGENCY LIGHT DISCHARGED A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01751DH 22982 EMERGENCY EXIT LIGHTS INOPERATIVE. ALLOWED PACKS TO RE-CHARGE AND CHECKS SERVICE IAW MM 33-50-01. 2L73 4F4 F A3WE E2EA 20060106000552006010600055NM 2006 1 6 SPAA0500082 120051230A3350900542 BATTERY PACK BOEING737 7372T4 1384492NM PWA JT8 JT8D17 52049NE EMERGENCY LIGHT INTERMITTENT A SPAAK NONE O OTHER ININSP/MAINT 1 WP28703S 22529 CENTER OVERHEAD EMERGENCY EXIT LIGHT STAYS ON ONLY BRIEFLY. REPLACED CENTER OVERHEAD EMERGENCY EXIT LIGHT BATTERY CHARGER IAW MM 33-51-81. GROUND CHECK NORMAL IAW MM 33-51-11. 2L72 4F4 F A16WE E2EA 20060106000592006010600059WP 2006 1 6 DHL2005803522 120051203A5315 FLOORBEAM DOUG DC8 DC873 302199CWP GE CFM56 CFM562C 13802NE BS 940 MISDRILLED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 ITEM REF. NR. 039049: MAIN CARGO COMPT. WING CTR SECTION FLOORBEAM UPPER FLANGE HOLE MISDRILLED STA 940.000 LBL 32.500 INCH (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 11/28/05, DWG AA33-53-R08 REV JR DATE 11/18/05. REMOVED FASTENERS IAW SRM 51-1-21. TRIMMED OUT DAMAGED AREA, FABRICATED REPAIR ANGLE (EXTRUSION 7075T6511 0.190 INCH) FILLER (7075T6 511 0.190 INCH) IAW DWG AA33-53-R08. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG. 9. INSTALLED REPAIR PARTS IAW DWG AA33-53-R08, SRM 51-1-20D, SRM 51-3-1 PG. 2A. 2L74 4F4 FRT4A25 E2GL 20060106000622006010600062WP 2006 1 6 DHL2005803519 120051121A53204772397U1 FITTING DOUG DC8 DC873 302199CWP GE CFM56 CFM562C 13802NE BS 1766 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 ITEM REF. NR. 038721: EMPENNAGE SPLICE FITTING CRACKED 1 INCH STA 1766.000 L-17 RT (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG. 1. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-21, SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW SPLICE FITTING WITH FASTENERS IAW SRM 51-1-21, SRM 51-3-0, SRM 51-3-1 (TORQUE). 2L74 4F4 FRT4A25 E2GL 20060106000632006010600063WP 2006 1 6 DHL2005803518 120051124A53203750257U503 FITTING DOUG DC8 DC873 302199CWP GE CFM56 CFM562C 13802NE BS 1040-1060 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 ITEM REF. NR 033026: AFT CARGO COMPT. SPLICE FITTING CRACKED 2 INCHES STA 1040.000 - STA 1060.000 L-31L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PAGE 1. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-21, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW SPLICE FITTING IAW SRM 51-3-0, SRM 51-1-20D, SRM 51-3-1 2L74 4F4 FRT4A25 E2GL 20060106000642006010600064WP 2006 1 6 DHL2005803517 120051120A5730 REPAIR DOUG DC8 DC873 302199CWP GE CFM56 CFM562C 13802NE WS 485 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 RT WING OB STUB WING LWR EXTERNAL SKIN REPAIR DOUBLER CRACKED 0.500 IN XW 485.000. PERFORMED MAJOR REPAIR IAW SRM 57-2-1A FIG. 1 PG. 3. REMOVED EXTERNAL REPAIR DOUBLER AND INTERNAL REPAIR DOUBLER IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED EXTERNAL REPAIR DOUBLER (AL7075T6 0.080 IN) AND INTERNAL REPAIR DOUBLER (AL7075 (0) 0.063) IAW SRM 57-2-1A FIG. 1 PG. 3. PERFORMED HEAT TREATMENT (7075(0) TO 7075T6) IAW SRM 51-1-1 PG. 1,13,17. CLEANED, TREATED AND PRIMED AREA, INTERNAL REPAIR DOUBLER AND EXTERNAL REPAIR DOUBLER INTERNAL PART IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG. 9. INSTALLED REPAIR PARTS IAW SRM 57-2-1A FIG. 1 PG. 3, SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1 2L74 4F4 FRT4A25 E2GL 20060106000652006010600065NM 2006 1 6 ASMF200512024 120051228A2400914F5654 RELAY DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE ELECTRICAL UNKNOWN W ASMFD RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TXTAXI/GRND HDL 1 SW23169PL3190 53175 AIRCRAFT RETURNED TO PLATFORM, AC CROSS TIE AND APU GENERATOR WERE OUT OF SERVICE. THE BCU, AC CROSS TIE RELAY AND GCU WERE REPLACED IAW MM 24-20-08, MM 24-20-06, MM 24-20-07 RESPECTIVELY, TESTED CORRECT. 2L72 4F4 FRTA6WE E9NE 20060106000662006010600066 2006 1 6 REXA200500155 420051214A25624530152 ELT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FAILED A REXAO OTHER L NO TEST ININSP/MAINT 1 SO258736A7385 2372 7736 ELT FAILS G-SWITCH FUNCTIONAL TEST. REMOVED FROM AIRCRAFT FOR UP TO 90-DAYS FOR REPAIR. 2L72 4F4 FRTA21EA E15NE 20060106000672006010600067WP 2006 1 6 ASMF200512023 120051227A2920405893 PUMP DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE AUX HYD SYS FAILED W ASMFK NONE J WARNING INDICATION ININSP/MAINT 1 SW23204AM15873 49404 DURING TRANSIT CHECK, THE AUXILIARY HYDRAULIC PUMP DID NOT SHUT OFF. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT CHECK, THE RELAY 22-15 AND THE RT AUXILIARY HYDRAULIC PUMP WERE REPLACED IAW MM 29-21-00 AND MM 29-10-06 RESPECTIVELY, TESTED CORRECT. 2L72 4F4 FRTA6WE E9NE 20060106000682006010600068NE 2006 1 6 ASMF200512022 220051227A73143843017 PUMP DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE FUEL SYSTEM DAMAGED W ASMFK NONE K FLUID LOSS ININSP/MAINT 1 SW23881LF4044213674 53051 DURING TRANSIT CHECK WAS DETECTED A FUEL LEAK BETWEEN GEAR BOX PUMP COUPLING AND THE RT ENGINE. AIRCRAFT WAS SENT TO THE HANGAR AND THE RT ENGINE FUEL PUMP WAS REPLACED IAW MM 73-12-01 PAGE 201, TESTED CORRECT. 2L72 4F4 FRT E9NE 20060106000702006010600070EU 2006 1 6 12132005A 120051213A2150M83248 O-RING SAAB SF340 340B 7860101EU UNKNOWN FAILED A NSVAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA27194CJ 194 ODOR OF BURNING RUBBER IN CABIN AND FLIGHT DECK REPORTED INITIALLY AT 12K BY F/A. NO SMOKE OBSERVED AT ANY TIME. RAN A/C ENGINES IAW 71-00-00. ALL SYSTEMS OPS CHECK GOOD. NO UNUSUAL ODORS, NO DEFECTS NOTED. COMPLETED OPS CHECK OF LT AND RT ACM'S WITH NO BURNING ODOR NOTED. OPS CHECK GOOD IAW AMM 21-10-00. CHANGED RT ACM OIL IAW 21-50-02/25 ACM OIL DARK IN COLOR. CHANGED LT ACM SUMP OIL IAW 21-50-02/25 ACM OIL DARK IN COLOR. CLEANED PASSENGER COMPARTMENT RECIRCULATION FILTER IAW 21-22-02. 2L72 4T RTA52EU 20060106000712006010600071CE 2006 1 6 12062005A 120051204A71101299100355 COWLING BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE LEFT LOOSE A NSVAB EMER. DESCENT O OTHER CLCLIMB 1 EA2760MJ UE60 LT TOP FWD ENGINE COWL CAME LOOSE IN FLIGHT. REMOVED AND INSPECTED LT TOP FWD ENGINE COWL, NO DEFECTS NOTED. REINSTALLED COWL AND SECURED LATCHES, NO DEFECTS NOTED. 2L72 4T4 TRTA24CE E26NE 20060106000722006010600072EU 2006 1 6 11302005A 120051125A24326013211 BATTERY SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE EMERGENCY LIGHTSINOPERATIVE A NSVAK NONE L NO TEST ININSP/MAINT 1 EA27239CJ 239 DURING A LINE CHECK 1 INSPECTION 3 FLOOR PROXIMITY LIGHTS AND 2 OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE. EMERGENCY LIGHT POWER SUPPLY 22LN WAS REPLACED AND BOTH THE FLOOR PROXIMITY AND OVERHEAD EMERGENCY LIGHTS WORKED NORMALLY IAW 33-50-01S. 2L72 4T4 TRTA52EU E8NE 20060106000762006010600076CE 2006 1 6 DXTA200501170 120051228A3240 ACCUMULATOR CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE BRAKES OVERSERVICED E DXTAO OTHER WS INADEQUATE Q C AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07332QS 5600523 BRAKES NOT FUNCTIONING PROPERLY, WHILE TAXIING STRAIGHT AHEAD BRAKE PEDALS WERE STIFF AND NON-REACTIVE, THEN WOULD CATCH ONE SIDE AT A TIME CAUSING DIRECTIONAL PROBLEMS. NOTED BRAKE ACCUMULATOR OVERSERVICED AND LT BRAKE SOFT. ADJUSTED ACCUMULATOR PRESSURE AND BLEED LT BRAKE, TAXIED AC. OPS CHECK GOOD. WORK DONE IAW CH 32-42-00 OJF THE 560 ULTRA MM. 2L72 4F4 FRTA22CE E25EA 20060106000782006010600078EA 2006 1 6 SWIA200515996 120051212A3350 INVERTER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CABIN MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07412SW 7101 SECTION OF FLOOR EMERGENCY LIGHTING INOPERATIVE. REPLACED FORWARD FLOOR EMERGENCY LIGHT INVERTER IAW 33-51-00. OPEATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20060106000802006010600080 2006 1 6 SWIA200515998 420051213A3418 WARN PANEL EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE COCKPIT FAULTY A SWIAO OTHER N FALSE WARNING CRCRUISE 1 NM07567SW 120342 DURING CRUISE FLIGHT RECEIVED SEVERAL SPARADIC (STALL WARNING) AURAL WARNINGS. REPLACED STALL WARNING PANEL IAW MM 27-34-08. OPERATIONAL CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20060106000812006010600081 2006 1 6 SWIA200515999 420051211A22106229815904 COMPUTER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE AUTOPILOT SYS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CLCLIMB 1 NM07962SW5414 5414 7859 IN CLIMB, WHILE ON FO SIDE, AUTO PILOT AND YAW DAMP DISENGAGED. REPLACED NR 2 FCC CARD IAW AMM 22-00-00. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20060106000822006010600082EA 2006 1 6 SWIA200516000 120051212A52102R5206B MOTOR CNDAIRCL600 CL6002B19 1900309EA CONT O520 TSIO520* 17040SO PAX DOOR FAILED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07442SW872 872 7609 PAX DOOR WILL NOT OPEN. DOOR ASSIST MOTOR LOCKED UP. REPLACED PAX DOOR ASSIST MOTOR IAW MM 52-11-08, OPERATIONAL CHECK GOOD. 2L72 4F3 ORTA21EA E8CE 20060106000842006010600084NM 2006 1 6 PDCA0501420 120051212A7711ED7472012 TRANSMITTER BOEING747 747283B 1384867NM PWA JT9 JT9D70A 52054NE NR 3 EPR FAILED A P5CAK NONE O OTHER CLCLIMB 1 EA15921FT 21575 688856 ON CLIMB, NR 3 ENGINE EPR STARTED DECREASING AT FL310 EPR IND., ON DESCENT IT READ HIGH (1.24 AT 150 WITH THRUST LEVERS IDLE) (CORRECTIVE ACTION) REPLACED EPR TRANSMITTER IAW MM 77-11-00 AND DEFERRED OPS CHECK IAW DDPG 77-4. 2L74 4F4 F A20WE E3NE 20060106000852006010600085NE 2006 1 6 REXA200500157 220051214A73216078T55P23 FUEL CONTROL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT ENGINE DEFECTIVE A REXABE EMER. DESCENT ENGINE SHUTDOWN O OTHER DEDESCENT 1 SO25824AY11779 8024 GEE872699 ON DESCENT, THE FLIGHT CREW DISCOVERED THAT THE RT ENGINE WAS UNRESPONSIVE TO THRUST LEVER INPUTS. THE FLIGHT CREW PERFORMED THE QRH AND DECLARED AN EMERGENCY. AN OTHERWISE UNEVENTFUL SINGLE ENGINE APPROACH AND LANDING WAS MADE. MAINTENANCE DISCOVERED THE MAIN FUEL CONTROL TO BE DEFECTIVE. FUEL CONTROL WAS REPLACED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20060106000862006010600086NE 2006 1 6 REXA200500156 220051214A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RIGHT DAMAGED A REXAB EMER. DESCENT YJ ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 SO258560F 7560 GEE872874 WHEN LEVEL AT FL300 THE RT ENGINE SHUTDOWN. FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND LANDED WITH NO OTHER PROBLEMS. MAINTENANCE FOUND SEVER DAMAGE TO THE ENGINE'S FAN SECTION. THE ENGINE WAS REPLACED AND THE AIRCRAFT RELEASED FOR SERVICE. DAMAGED ENGINE WILL BE INSPECTED FOR CAUSE DURING THE REPAIR PROCESS. 2L72 4F4 FRTA21EA E15NE 20060106000892006010600089WP 2006 1 6 MWEA050135 120051216A521059100817 SKIN DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE PAX DOOR BENT A MWEAK NONE O OTHER ININSP/MAINT 1 GL13809ME 48071 PASSENGER DOOR OUTER SKIN BENT AT DOOR LOWER FORWARD EDGE FROM JETWAY. COLD FORMED BENT OUTER SKIN. 2L72 4F4 F A6WE E9NE 20060106000922006010600092SO 2006 1 6 SIMA200532508 120051103A532014525381003 FLOOR SUPPORT EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21613AE 145081 A PREVIOUS REPAIR ON THE LT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. REMOVED AHT PREVIOUS REPAIR. PREPARED A FILLER AND DOUBLER. REPAIR DONE IAW SRM. (K) 2L72 4F4 FRTT00011ATTE6CH 20060106000932006010600093SO 2006 1 6 SIMA200532503 120051104A532014525480003 SILL EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21613AE15292 145081 THE CARGO DOOR CUT OUT LOWER SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED LOWER SILL. INSTALLED SERVICEABLE SILL IAW SRM. (K) 2L72 4F4 FRTT00011ATTE6CH 20060106000952006010600095SO 2006 1 6 SIMA200532906 120051117A532014522178005 SILL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21615AE 145087 THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED CENTER SILL AND INSTALLED NEW CENTER SILL IAW SRM AND CPM. (K) 2L72 4T4 FRTT00011ATTE6CH 20060106000982006010600098NM 2006 1 6 USAA051551 120051214A5320 ATTACH ANGLE BOEING737 737301 1384611NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19591US 23936 LOCATION: S12L INTERCOSTAL LWR FWD ATTACH ANGLE AT LB END. MAJOR REPAIR REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-10-02 DEFECT SIZE: .375 IN. 2L72 4F4 FRTA16WE E2GL 20060106000992006010600099NM 2006 1 6 USAA051552 120051214A5330 SKIN BOEING737 737301 1384611NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19591US 23936 RSB 727E RS24, MAJOR REPAIR, CUT OUT CRACK, FABRICATED AND INSTALLED 9.5 IN X 13 IN DOUBLER IAW SRM 53-00-01 FIG 201 DEFECT SIZE: 2T 2L72 4F4 FRTA16WE E21EU 20060106001002006010600100NM 2006 1 6 USAA051553 120051214A5311 FRAME BOEING737 7374B7 1384702NM CFMINTCFM565CFM565B6 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 STA400, S9R, MAJOR REPAIR, REMOVED DAMAGE, INSTALL 2 ANGLED DOUBLERS IAW TR 53-10-20C. DEFECT SIZE: .375 IN. 2L72 4F4 FRTA16WE E37NE 20060106001012006010600101NM 2006 1 6 USAA051554 120051214A5330 SKIN BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE FUSELAGE DENTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19353US 23556 LOCATION: BETWEEN B STA 847 AND 867 ABOVE STRINGER S-20L. FABRICATED AND INSTALLED DOUBLER IAW SRM 53-00-01 REPAIR 31 DETAIL 10, 19, DEFECT SIZE: 1.0 IN. 2L72 4F4 FRTA16WE E2GL 20060109000132006010900013WP 2006 1 9 DHL2005803531 120051203A5311 FRAME DOUG DC8 DC873 302199CWP BS 1580 CRACKED A DHLAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SO01803DH82180 46123 MAIN CARGO COMPT FRAME CRACKED 0.250" STA 1580.000 L-20 - L-21R. PERFORMED MAJOR REPAIR IAW SRM. TRIMMED OUT DAMAGED FRAME SEGMENT, FABRICATED NEW FRAME SEGMENT IAW SRM. TWO ANGLES IAW SRM. HEAT TREATED NEW FRAME SEGMENT AND ANGLES FROM 70750 TO 7075T6 IAW SRM 53-2-0. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11. INSTALLED REPAIR PARTS IAW SRM 53-2-0 FIG 2 SHEET 4-6, SRM 53-2-0 FIG 2 SHEET 5 (TR 53-125). 2L74 4F RT4A25 20060109000142006010900014EA 2006 1 9 COMA0560762 120051229A5730601R100454 SKIN CNDAIRCL600 CL6002B19 1900309EA LT WING CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA29272 7031 RT LOWER WING PLANK HAS FRETTING CORROSION AT FUEL TANK ACCESS CUTOUTS, (610AB NOT IN CRITICAL AREA), (640DB, 640EB, 640FB, 650AB, 650CB, 650DB, 650FB, 650HB IN CRITICAL AREA). REPAIRED LOWER WING PLANK FUEL TANK ACCESS CUTOUTS IAW BOMBARDIER REO 601R-57-21-030. 2L72 4F RTA21EA 20060109000162006010900016WP 2006 1 9 DHL2005803525 120051203A5310 DOUBLER DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 MODIFICATION DOUBLER (ACS) CRACKED 0.500" ON AFT LWR CORNER OF RT PRIMARY HEAT EXCHANGER, STA -12.00. L-27R. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 12-02-05, DWG AA33-53-R01 REV A DATE 12-02-05. REMOVED FASTENERS IAW SRM 51-1-21. TRIMMED OUT DAMAGED SECTION. FABRICATED FILLER (2024T3AL 0.100"), REPAIR DOUBLER (2024T3AL 0.050") TRIPLER DOUBLER (2024T3AL 0.063") IAW DWG AA33-53-R01. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS (CONICAL WASHERS) IAW DWG AA33-53-R01, SRM 51-1-21, SRM 51-1-20D, SRM 51-1-26, SRM 51-3-1 PG 2A. 2L74 4F RT4A25 20060109000182006010900018WP 2006 1 9 DHL2005803549 120051212A53105750092506 DOOR FRAME DOUG DC8 DC873 302199CWP FUSELAGE UNKNOWN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 COMPLY WITH REPAIR MODIFICATION ON "A" BELLY DOOR JAMB CORNER IAW SERV REWORK DRAWING SR 08530019. PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9, AD2005-18-07, SB DC8 53078, SERVICE REWORK DWG SR 08530019, BOEING MESSAGES NR 1-145489684-5, SEMAN DWG ED-4113, 1-145489684-6 DATE 12/08/05. REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-1-21, SRM 51-3-0. FABRICATED EXTERNAL REPAIR DOUBLER, EXTERNAL REPAIR TRIPLER 2 FILLERS IAW SEMAN DWG ED4113, SRM 53-2-0 FIG 22 TR NR 53-189. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACE IAW SRM. INSTALLED REPAIR PARTS IAW SEMAN DWG ED4113, SRM 53-2-0 FIG 22, TR 53-189, SRM 51-3-0, SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1 PG 2A. 2L74 4F RT4A25 20060109000192006010900019WP 2006 1 9 DHL2005803551 120051214A5310 DOOR FRAME DOUG DC8 DC873 302199CWP FUSELAGE UNKNOWN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 COMPLY WITH REPAIR MODIFICATION ON "D" BELLY DOOR AFT LWR JAMB CORNER IAW AD2005-18-07 SB DC8 53-078, SERVICE REWORK DRAWING SR 08530019. PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9, AD2005-18-07, SB DC8 53-078, SERVICE REWORK DWG SR08530019, BOEING MESSAGE NR 1-14237582-5, SEMAN DWG ED4112, 1-145237582-8 DATE 12/08/05. REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-1-20D, SRM 51-3-0. FABRICATED EXTERNAL REPAIR DOUBLER EXTERNAL REPAIR TRIPLER 2 FILLERS SEMAN DWG ED4112, SRM 53-2-0, TR 53-188. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT ON FAYING SURFACES IAW SRM 51-1-11. INSTALLED REPAIR PARTS IAW SEMAN DWG ED 4112, SRM 53-2-0, TR 53-188, SRM 51-3-0, SRM 51-1-21, SRM 51-12L74 4F RT4A25 20060109000212006010900021WP 2006 1 9 DHL2005803546 120051207A5100 DOUBLER DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 NR 2 ACCESS DOOR FRAME INTERNAL DOUBLER 0.75" CRACKED WORN & BROKEN (STA -156.000 TO -165.000). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 12/06/05, DWG AA33-53-R09 REV IR DATE 11/22/05 REMOVED LT/RT NOSE AIR SCOOP IAW SRM 51-3-0. REMOVED EXISTING EXTERNAL REPAIR DOUBLER, EXISTING INTERNAL REINFORCEMENT REPAIR DOUBLER. TRIMMED OUT INTERNAL DOUBLER, FAB`D 4 INTERNAL DOUBLER EXTERNAL DOUBLER INTERNAL DOUBLER. HEAT TREATED FROM 7075-0 TO 7075T6 IAW DWG AA33-53-R09, SRM 51-1-1, DPS 7.00-1. CLEANED, TREATED & PRIMED AREA & REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11. 2L74 4F RT4A25 20060109000222006010900022WP 2006 1 9 DHL2005803552 120051125A5310 DOOR FRAME DOUG DC8 DC873 302199CWP FUSELAGE UNKNOWN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 ACCOMPLISH REPAIR MODIFICATION ON FWD PASSENGER DOOR JAMB CORNERS IAW AD2000-20-08, SB 53-075, SERVICE REWORK DWG SR08530021. DOCUMENT ALL ACTIONS IN THE NR, AIRCRAFT LOG, 337 FORM (MAJOR REPAIR). PERFORMED MAJOR REPAIR ON JAMB CORNERS(4) OF FWD PASSENGER DOOR IAW AD2000-20-08, SB DC8 53-075, DOUGLAS DWG SR08530021, 5750776 (PAPERWORK ENCLOSED TO E.O. SEMAN NR 20051354, 20051350, 20051351, 2005134 DATE 11/04/05) FOR UPPER FWD JAMB CORNER REPAIR SEE NR 39172. 2L74 4F RT4A25 20060109000242006010900024NM 2006 1 9 DHL2005752005 120051220A3350062 BATTERY BOEING727 727223 1384074NM EMERGENCY LIGHT INOPERATIVE A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01752DH 22466 DURING STBY TEST EMERGENCY LIGHTS WILL NOT ILLUMINATE. REMOVED AND REPLACED BATTERYS, OPS CK NORMAL IAW MM 33-50-101, P/N MISC-O62. 2L73 4F A3WE 20060109000282006010900028WP 2006 1 9 DHL2005803550 120051125A5310 DOOR FRAME DOUG DC8 DC873 302199CWP PAX DOOR MISREPAIRED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01803DH82180 46123 FWD PASSENGER DOOR FWD UPPER JAMB CORNER HAS A REPAIR NOT ACCORDING TO DWG NR SR08530021. PERFORMED MAJOR REPAIR IAW AD2000-20-08, S/B DC8 53-075, DOUGLAS DWG SR08530021, DOUGLAS DWG 5750776. REMOVED EXISTING REPAIR IAW SRM 51-1-21, SRM 51-1-20D, SRM 51-1-21A. FAB`D REPAIR DOUBLER (AL7075T6 0.063") AND REPAIR TRIPLER (AL7075T6 0.080") IAW DOUG DW SR08530021. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW DOUG DWG SR08530021, SRM 51-1-21, SRM 51-1-26 (CONICAL WASHERS) SRM 51-3-0, SRM 51-1-20D, SRM 51-3-1 PG 2A. CERT ENCLOSED TO NR 033338. 2L74 4F RT4A25 20060109000292006010900029NM 2006 1 9 DHL2005770009 120051115A2780H1010261 SWITCH BOEING727 7272B7 138407LNM K FLAPS INOPERATIVE A DHLAB EMER. DESCENT F FLT CONT AFFECTED APAPPROACH 1 SO01770AT 21953 DURING FLAP EXTENSION, NR 4 KRUEGER FLAP FAILED TO EXTEND. COMPLETED ABNORMAL PROCEDURE AND LANDED. ON SHORT FINAL NR 4 KRUEGER FLAP EXTENDED. REMOVED AND REPLACED NR 4 L/E FLAP POSITION SWITCH, OPS CK NORMAL IAW B727 M/M 27-82-01 AND 27-82-00. 2L73 4F A3WE 20060109000322006010900032WP 2006 1 9 DHL2005801014 120051012A57305612387 PLATE DOUG DC8 DC873F 302199FWP WING UNKNOWN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH 46033 NR 4 ALT TANK PLATE 505A REMOVED FOR ACCESS. FOUND CRACK FOUND ON VISUAL INSPECTION R/WING WND OF STRINGER 64 APPROX 1" LONG FRONT TO REAR O/B FASTENER AND BY HIGH FREQ EDDY CURRENT. ACP HIGH FREQ EDDY CURRENT INSP. OF LOWER WING SKIN LT SIDE OF LWR WING. OK TO INSTALL, INSTALLED NR 4 ALT TANK PLATE PER M/M 28-10-0 AND 57-30-0 LEAK CK OK. EDDY CURRENT INSP RT WING LWR SURFACE REF LVL III NDT REPORT W.O. 57-100 REV 3 FOR REPAIR SEE LG PG 063738 1W FOR COMPLETE SIGN-OFF AND WORK ACCOMPLISHED. EDDY CURRENT INSP LT WING LWR SURFACE REF LVL III NDT REPORT WO 091005. 2L74 4F RT4A25 20060109000342006010900034NM 2006 1 9 DHL2005782003 120051025A3260 SWITCH BOEING727 727227 1384078NM RT MLG DOOR LACK OF LUBE A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01782DH 21998 AFTER TAKEOFFF WHEN GEAR HANDLE MOVED TO OFF R GEAR DOOR LIGHT ILLUM. ON S/O PANEL AND RED DOOR LIGHT ON FORWARD PANEL. PERFORMED ABNORMAL PROCEDURE. NO HELP. GEAR HANDLE HAD TO REMAIN IN UP TO KEEP LIGHTS OUT. CLEAN AND LUBED RT MLG DOOR SWITCH, OPS CK GOOD IAW 727 MM 32-62-11. 2L73 4F A3WE 20060109000362006010900036WP 2006 1 9 DHL2005806002 120051022A3297 WIRE DOUG DC8 DC873F 302199FWP LT MLG DAMAGED A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01806DH 46002 AFTER TAKEOFF DOORS NOT LATCH LIGHT ILLUMINATED AND REMAINED ON UPLATCH CHECK, GEAR NOT LATCHED LIGHT LIGHT ILLUMINATED AND NOSE WHEELGEAR EXTENDED LEFT MAIN GEAR ALTERNATE LIGHT ILLUMINATED INTERMITTENT. LUBRICATED NOSE GEAR UPLATCH REPAIRED WIRE AT MAIN GEAR (LT) DOOR SWITCH PER WDM 32-10-1 AND OPS CHECKED PER M/M 32-31-6. 2L74 4F RT4A25 20060109000372006010900037NM 2006 1 9 DHL2005751006 120051116A3350S106 BATTERY BOEING727 727264 138408MNM EMERGENCY LIGHT INOPERATIVE A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01751DH 22982 EMERGENCY EXIT LIGHT IN FWD ENTRY INOP. REPLACED BATTERIES IN EMERGENCY EXIT LIGHT ON OUTSIDE ENTRY DOOR. OPS CHECKS GOOD IAW B727 MM 33-50-22, PN OFF AND ON S106. 2L73 4F A3WE 20060105000592006010500059NM 2006 1 5 2005UALA01519 120051226A5340 STRINGER CLIP BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE BS 867 STR 20R CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29923UA 26643 STRINGER CLIP CRACKED STA 867 STR 20R. MAJOR REPAIR ACP'D PER SRM 51-40-02, REPLACED STRINGER CLIP . 2L72 4F4 FRTA16WE E2GL 20060105000742006010500074SO 2006 1 5 RAIA00512033 120051218A3350 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DAMAGED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03819HK 145062 PRE - FLT 5435 - STL - EMERGENCY FLOOR LIGHT OUT AT 9A NOT ILLUMINATING. MAINTENANCE REPAIRED CONNECTION TO EMERGENCY LIGHT STRIP. 2L72 4T RTT00011AT 20060105000912006010500091NM 2006 1 5 2005UALA01535 120051229A2750 WARNING LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE TE FLAPS ILLUMINATED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29519UA 24872 RETURNED TO THE FIELD UNDER AMBER ALERT DUE TO A FLAP ASYMMETRY INDICATION. THE ASYMMETRY INDICATION WAS ILLUMINATED DUE TO A FAILED TE FLAP POSITION TRANSMITTER ON THE LEFT WING. THE SUBJECT LEFT WING POSITION TRANSMITTER WAS REPLACED PER 757 MM 27-58-03. ALL FOLLOWING OPS CHECKS WERE NORMAL. ENGINEERING CONSIDERS THIS TO BE AN ISOLATED INCIDENT. THERE ARE NO RECENT MAINTENANCE OR RELIABILITY TRENDS THAT WOULD DICTATE ANY REVISIONS TO THE EXISTING MAINTENANCE PROGRAM AT THIS TIME. MAINTENANCE PROGRAM FOR SUBJECT TE FLAP TRANSMISSION: ON-CONDITION. 2L72 4F4 FRTA2NM E17NE 20060105000962006010500096NM 2006 1 5 2005UALA01539 120051227A3350 LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29507UA 24743 EXT EMERGENCY LIGHT AT DOOR 4L INOP. 2L72 4F4 FRTA2NM E17NE 20060105001022006010500102NM 2006 1 5 USAA051650 120051229A5551 ATTACH FITTING BOEING737 7374B7 1384702NM HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19781AU 25020 FOUND R2 ON HORIZ STAB. REMOVED CORROSION AND GOUGE, INSTALLED BUSHING PER SRM 55-10-10, DEFECT SIZE: 2". 2L72 4F RTA16WE 20060105001052006010500105NM 2006 1 5 USAA051652 120051229A5320 SPLICE BOEING737 7374B7 1384702NM BS 907 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19781AU 25020 FOUND CRACK RT STA 907, STR 4R. REMOVED AND REPLACED WITH FABRICATED STR SPLICE PER SRM 51-40-02, DEFECT SIZE: .250". 2L72 4F RTA16WE 20060105001072006010500107NM 2006 1 5 USAA051654 120051229A5510 CLEVIS BOEING737 7374B7 1384702NM HORIZOTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19781AU 25020 FOUND CORROSION CLEVIS R7, HORIZ STAB. REMOVED CORROSION, INSTALLED BUSHING PER SRM 55-10-10, DEFECT SIZE: 2". 2L72 4F RTA16WE 20060105001132006010500113EU 2006 1 5 USAA051660 120051229A5347A225408202000 SEAT TRACK AIRBUSA321 A321211 3930370EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19162UW 1412 FOUND CORROSION LT INBD SEAT TRACK BETWEEN FRAMES 47 AND 47.2. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 53-00-15, DEFECT SIZE: 1" BY 30". 2L72 4F RTA28NM 20060105001252006010500125EA 2006 1 5 ASOA051025 120051104A5320 SILL CNDAIRCL600 CL6002C10 1390015EA BS 280 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27706EV 10054 DURING A C-CHECK IN TUS, THE FLOOR SILL AT STATION 280, RBL 36.0 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE FLOOR SILL AT STATION 280, RBL 36, IAW ASA EC REO 670-53-21-144. (M) 2L72 4F RTA21EA 20060105001462006010500146NM 2006 1 5 AMTA200501044 120051108A5347 SEAT TRACK BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE STA 1640, RBL 47CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11518AT 27974 SEAT TRACK STA 1640, RBL47, CORROSION. REMOVED CORROSION FOUND WITHIN LIMITS TREATED. (K) 2L72 4F4 FRTA2NM E12EU 20060105001572006010500157NM 2006 1 5 AMTA200501046 120051108A5320 PLATE BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE THRESHOLD CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11518AT 27974 R-4 THRESHOLD SUPPORT PLATE CROSSION, BS 1678, RBL 56. REMOVED CORROSION, FOUND TO BE WITHIN LIMITS TREATED. (K) 2L72 4F4 FRTA2NM E12EU 20060105001622006010500162NM 2006 1 5 AMTA200501036 120051108A5320 SILL BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE BS 1460 CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11518AT 27974 AFT CARGO DOOR CUTOUT- DOOR SILL SUPPORT 4TH FITTING CORRODED, BS 1460, WL 146.90, WL 146.90, RBL 25. REMOVED CORROSION IN SILL TIE DOWN AND SUPPORT FITTING IAW SRM. FOUND TO BE OUT OF LIMITS IAW SRM. REMOVED AND REPLACED FITTING SUPPORT IAW SRM. (K) 2L72 4F4 FRTA2NM E12EU 20060105001692006010500169NM 2006 1 5 KPV2005F00002 120050808A6120 PCU DHAV DHC8 DHC8103 1386005NM PWA PW121 PW121 52124NE NR 1 FAILED A KPVAO OTHER O OTHER NRNOT REPORTED 1 WP13805WP 353 DURING TAXI OUT NR 1 BETA LIGHT CAME ON WITH THE POWER LEVERS ABOVE FLIGHT IDLE. RETURNED TO GATE. REPLACED NR1 PCU, OPERATIONALLY CHECKS GOOD. (K) 2H72 4T4 TRTA13NM E20NE 20060105001702006010500170NM 2006 1 5 AMTA200501140 120051208A3397 WIRE BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE EMERGENCY LIGHT DAMAGED A AMTAK NONE L NO TEST ININSP/MAINT 1 WP13514AT 27971 SEVERAL FLOOR PATH EMERGENCY LIGHTS OUT AT ROW 12. RELAMPED AND REPAIRED WIRING AT ROW 12 LIGHTS CHECKED GOOD. (K) 2L72 4F4 FRTA2NM E12EU 20060105001832006010500183EA 2006 1 5 SWIA200515926 120051128A2781 SENSOR CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE L/E SLAT MALFUNCTIONED A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07716SK 10180 AFTER POWER UP SLAT FAULT MSG CAME ON. REPLACED RT IB AND OB SLAT DISCONNECT SENSORS. IAW 27-81-39. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA EOOO63EN 20060105002142006010500214WP 2006 1 5 ABXA060020 120051026A5315 FLOORBEAM DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE BS 857 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 MAIN CABIN, STA. 857, LBL 12, FLOORBEAM UPPER CAP CORRODED. REMOVED CORROSION ON FLOORBEAM STA. 857, LBL 12. MATERIAL LOSS OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM DWG K04881. 2L74 4F4 F 4A25 1E8 20060105002202006010500220WP 2006 1 5 ABXA060019 120051101A5315 FLOORBEAM DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE BS 55 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 MAIN CARGO, STA. 55, LBL 20, CORROSION ON UNDERSIDE OF FLOORBEAM CORNER. REMOVED A 3.5 INCH X .7500 INCH SECTION OF UPPER FLANGE FLOORBEAM AT STA. 55, LBL 20 IAW SRM DWG K04881. FABRICATED REPAIR ANGLE, SHIM AND FILLER IAW SRM DWG K04881. 2L74 4F4 F 4A25 1E8 20060105002232006010500223CE 2006 1 5 DXTA200501175 120051231A7700 FADEC CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL COCKPIT INOPERATIVE E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07906QS 7500206 FADEC FAULT CODE CAME ON DURING TAKEOFF, ABORTED TAKEOFF AND RETURNED TO BLOCK. PERFORMED CHECKLIST AND CLEARED FAULT CODE. AIRCRAFT OPS CHECKED GOOD. 2L72 4J4 FRTT00007WITE6CH 20060105002272006010500227NM 2006 1 5 UPS06445907 120051230A712065B403604 THRUST LINK BOEING747 747121 1384871NM PWA JT9 JT9D7A 52054NE NR 4 ENGINE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 AD CRACK INDICATIONS FOUND AT NR 4 ENG MOUNT THRUST LINK THE INDICATIONS LOCATED AT FWD AND AFT LUG BORE WHICH WERE EXCEEDED THE LIMITS. THRUST LINK REPLACED. REF MM 71-21-03. 2L74 4F4 F A20WE E20EA 20060105002292006010500229NM 2006 1 5 UPS06445905 120051229A712065B903604 THRUST LINK BOEING747 747121 1384871NM PWA JT9 JT9D7A 52054NE NR2 ENG CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 AD NR 2 ENGINE REAR ENGINE MOUNT THRUST LINK FOUND CRACKED INDICATION ON AFT END LUG BORE LOWER AREA. NR 2 ENG THRUST LINK REPLACED IAW EO NR B747-7120-22596 APPENDIX G. 2L74 4F4 F A20WE E20EA 20060105002382006010500238WP 2006 1 5 DHL2005803542 120051211A53403779874502N FITTING DOUG DC8 DC873 302199CWP GE CFM56 CFM562C 13802NE BS 834 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 ITEM REF NR. 033356: MAIN CARGO COMPT FITTING CRACKED 1 INCH STA 834.500 L-13R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG. 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-0, SRM 51-3-1 PG. 2A (TORQUE). 2L74 4F4 FRT4A25 E2GL 20060105002492006010500249EA 2006 1 5 COMA0560635 120051122A7931142F1000130D TRANSDUCER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT ENGINE FAULTY A COMAO OTHER N FALSE WARNING CRCRUISE 1 SO01479CA9313 7675 ENROUTE, THE RT ENGINE OIL PRESSURE INDICATION WAS ERRATIC RANGING FROM 8 TO 30 PSI. CREW DECLARED AN EMERGENCY, REDUCED POWER ON THE RT ENGINE TO IDLE AND LANDED WITHOUT INCIDENT. REPLACED THE RT ENGINE OIL PRESSURE TRANSDUCER. 2L72 4F4 FRTA21EA E15NE 20060105002772006010500277 2006 1 5 YENA200584 420051203A3140 COMPUTER AIRBUS320 A320232 3930326EU IAE V2500 V2500A1 NE COCKPIT FAULTY A YENAA UNSCHED LANDING N FALSE WARNING TOTAKEOFF 1 EA15544JB 1835 GEAR FAULT MASTER WARN, COULD NOT CANCEL, RETARD COULD NOT CANCEL, RETURNED 5-8 MIN CONTINUOUS. DEBRIEF FLT CREW FOR FAULT DETAILS, AFTER GEAR UP NLG MASTER WARN ILLUM, NR 1 ENG FIRE TEST ILLUM BRIEFLY. NO AUTO THR OR AP. ON APPR LGB NO RA CALLOUTS. CREW STATED A/C FLEW NML. REVIEWED PFR, FOUND RA1 FAULT (344233) NO ECAM LAST FLT FOUND. OPENED NLG DRS, INSP NLG PROX SENS, HARNESS CON AT J-BOX. NO DEFECTS. PERFORMED CFDS SELF TEST, RAMPDWN ON RA1, RA2-PASSED, LGCIU 1, 2 SELF TEST/GRD SCN, PASSED. FCU 1, 2, SELF TEST PASSED. PFMD CENT WARN SYS GRND SCAN, REPLACED SDAC AS PRECAUTION. REPLACED RA 1, NR 1 FWC, XLD DATABASE FR/ NR2 FWC. REPLACED NR2 FWC. NO FAULTS. PERFORMED CAT 3 LAND TEST. A/C OK FOR CAT 3. 2L72 4F4 FRTA28NM E311NE 20060105002792006010500279NM 2006 1 5 PIDA20050197 120051203A3350 MOUNT BOEING737 737228 13844AGNM PWA JT8 JT8D15A 52051NE CABIN DEFECTIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05252TR 23001 R-2 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED MOUNT PLATE DUE TO NO POWER AT LIGHT RECEPTACLE IN MOUNT PLATE. LIGHT OPS CHECKS OK. 2L72 4F4 FRTA16WE E2EA 20060105002812006010500281WP 2006 1 5 ABXA050318 120051206A335060030451 BATTERY PACK DOUG DC9 DC932F 3022067WP PWA JT8 JT8D7B 52053NE CABIN DISCHARGED A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23909AX 336 47148 DURING PREDEPARTURE CHECK FOUND COCKPIT EMERGENCY LIGHTS WOULD NOT TEST. DEFERRED NR 47327 REMOVED AND REPLACED BATTERIES IN PACK IAW AMM.OPS CHECKED GOOD. DEFERRED IAW GMM. ITEM 2 A12 FOR BATTERY PACK REPLACEMENT WITHIN 3 FLIGHT DAYS. PLACARD INSTALLED, CODE 2 CLEAR, NR 47327 REPLACED EMERGENCY POWER BATTERY PACK ASSY. REF AMM 33-53-00. OPS CHECKED GOOD, PLACARD REMOVED. 2L72 4F4 F A6WE E2EA 20060105002992006010500299EU 2006 1 5 05FDEA04166 120051207A5511 SPAR AIRBUS310 A310 EU GE CF6 CF680A3 30025NE HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 RT HORIZONTAL T/E UPPER IB SPAR ON LOWER SIDE HAS SEVERE EXFOLIATION, REF N00542. REPAIRED RT HORIZONTAL T/E UPPER SPAR CORD IAW SRM 55-11-21 PARA 7.H PAGES 315 TO 324 FIG SHEET 2 AND FIG 213. 2L72 4F4 FRTA35EU E13NE 20060105003032006010500303EU 2006 1 5 05FDEA04170 120051207A5330 SKIN AIRBUS310 A310 EU GE CF6 CF680A3 30025NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 BELLY OF AC RT SIDE FWD OF NR 2 PACK PORTABLE WATER SERVICE HAS CORROSION ON CUTOUT REF N00031. REPAIRED DAMAGE IAW EA 6-5330-94498 AND SRM 51-72-10 AND SRM 53-10-14. 2L72 4F4 FRTA35EU E13NE 20060105003062006010500306 2006 1 5 AT0500048 420051208A256564210103 SLIDE BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE TAIL CONE UNSERVICEABLE A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15929AT 55075 DURING ROUTINE MAINTENANCE SERVICE CHECK FOUND TAIL CONE EMERGENCY ESCAPE SLIDE PRESSURE LOW. REMOVED AND REPLACED TAIL CONE EMERGENCY ESCAPE SLIDE ASSY. 2L72 4F4 FTRA6WE E00061EN 20060105003092006010500309WP 2006 1 5 ABXA050321 120051202A53205912494501 PAN DOUG DC9 DC941 302207NWP PWA JT8 JT8D15 52051NE FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23963AX 47780 FORWARD LOWER CARGO DOOR PAN CRACKED AT AFT HOLD OPEN FITTING. REPAIRED CRACKED DOOR PAN IAW SSRM K05159. 2L72 4F4 F A6WE E2EA 20060105003152006010500315NM 2006 1 5 RYNA200500030 120051206A2611 SMOKE DETECTOR BOEING757 757200 1384950NM RROYCERB211 RB211535E4 54555NE E/E BAY MALFUNCTIONED A RYNAB EMER. DESCENT N FALSE WARNING DEDESCENT 1 CE07151GX 24451 FORWARD EQUIPMENT BAY SMOKE LIGHT CAME ON DURING APPROACH. CLEANED AND RELAMPED FORWARD EQUIPMENT BAY SMOKE DETECTORS. OPERATIONAL CHECKED NORMAL. 2L72 4F4 FRTA2NM E12EU 20060105003172006010500317WP 2006 1 5 2005000013 120050819A36109787344 VALVE DOUG DC10 DC1030 3023501WP GE CF6 CF650C2B 30018NE NR 2 MALFUNCTIONED A CNMAC ABORTED TAKEOFF M OVER TEMP TOTAKEOFF 1 SW07810AX 48265 NR 2 PNEUMATIC TEMP HI LIGHT ILLUMINATED. ASSOCIATED PNEUMATIC TEMP INDICATOR WAS IN THE RED ZONE. REMOVED AND REPLACED NR 2 ENGINE FAN AIR VALVE IAW 36-13. PERFORMED ENGINE RUN, NO DEFECTS NOTED. 2L73 4F4 F A22WE E23EA 20060105003202006010500320NM 2006 1 5 ANCF200400064 120051209A3020 ANTI-ICE VALVE BOEING757 75728A 1384976NM RROYCERB211 RB211535E4 54555NE LT ENGINE MALFUNCTIONED W ANCFC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO23506NA 24771 EICAS MSG L ENG ANTI ICE AND ENG ANTI-ICE VALVE CAME ON DURING TAKEOFF ROLL WITH MAX THRUST SET. IAW AMM 30-21-03 REPLACED ENGINE INLET THERMAL ANTI ICE V/V LTANTI ICE VALVE P/N 7646B000 S/N 040571-5. 2L72 4F4 FRTA2NM E12EU 20060105003302006010500330EA 2006 1 5 QXEA200501854 120051226A2810MS29513020 O-RING CNDAIRCL600 CL6002C10 1390015EA FUEL SUMP DAMAGED A QXEAK NONE K FLUID LOSS UKUNKNOWN 1 NM09612QX 10042 PDX - ON POST FLIGHT 2466, NOTICED FUEL DRIPPING FROM AROUND A FUEL DRAIN UNDER THE RIGHT WING ROOT. REPLACED O-RING ON RT FWD INBD FUEL TANK WATER DRAIN (SUMP). NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20060105003402006010500340NM 2006 1 5 0501956624 120051020A5311 FRAME BOEING747 747251B 1384892NM FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01624US 21706 DURING "M" CHECK, FOUND CRACKS ON FRAME AT BS 520 BETWEEN S9 AND S11. REPAIRED PER EA 66-205522. 2L74 4F A20WE 20060105003422006010500342WP 2006 1 5 0501909753 120051130A5311 FRAME DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01753NW 47117 DURING "H" CHECK, FOUND CRACK IN BULKHEAD FRAME AT BS 37. REPAIRED PER EA 97-204720. 2L72 4F A6WE 20060105003442006010500344NM 2006 1 5 0501916624 120051016A5420 STIFFENER BOEING747 747251B 1384892NM NR 4 PYLON CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01624US 21706 DURING "M" CHECK, FOUND CRACK IN INBOARD STIFFENER OF NR 4 PYLON AT NAC STA 217. REPAIRED PER EA 66-205836. 2L74 4F A20WE 20060106000162006010600016WP 2006 1 6 DHL2005803536 120051128A57515653048U1 BRACKET DOUG DC8 DC873 302199CWP GE CFM56 CFM562C 13802NE LT AILERON BROKEN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 ITEM REF. NR. 033548: LT IB AILERON BRACKET BROKEN (NR 2 HINGE) (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PAGE 1. REMOVED DAMAGED BRACKET IAW SRM 51-1-21, SRM 51-3-0, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW BRACKET IAW SRM 51-1-21, SRM 51-3-0, SRM 51-1-20D. FOR OPS CHECK SEE NR 038928. 2L74 4F4 FRT4A25 E2GL 20060106000222006010600022WP 2006 1 6 DHL2005803535 120051205A5740 FITTING DOUG DC8 DC873 302199CWP GE CFM56 CFM562C 13802NE WS 74 LT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 NR 2 MAIN TANK OB FWD FITTING CRACKED XRS 74.000 S-51 (LWR PART) (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND APPLIED COATING MATERIAL TO AREA IAW SRM 51-1-12 PG. 7. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PAGE 9. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1. FOR LEAK CHECK REFER TO NR 039054. 2L74 4F4 FRT4A25 E2GL 20060106000252006010600025NM 2006 1 6 DHL2005747003 120051216A2780 CONNECTOR BOEING727 727224 1384076NM PWA JT8 JT8D15 52051NE LE FLAPS LOOSE A DHLAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 SO01747DH 22253 AFTER FLAPS WERE RETRACTED TO 0 THE AMBER LE FLAPS LIGHT ILLUMINATED ON FWD PANEL SO PANEL READ NR5 LE FLAP IN TRANSIT ABNORMAL PROCEDURE COMPLETE PROBLEM REMAINED. FOUND CONNECTOR LOOSE FOR SWITCH CLEANED, RESECURED SWITCH CONNECTOR PLUG RAN FLAPS OPS CK NML IAW M/M 27-82-0. DEFERRED IAW MEL 27-6 CAT C CNTRL NR23651 PLACARD INSTALLED. GREEN L/E INTRANSIT LIGHT WILL NOT TEST. REF DMI NR23651. REPLACED LIGHT ASSY, P/N 10-61803-80 IAW M/M 33-10-51, GROUND CHECKS NML.THIS CLEARS DMI NR23651. 2L73 4F4 F A3WE E2EA 20060106000602006010600060WP 2006 1 6 DHL2005803521 120051128A5320 CHANNEL DOUG DC8 DC873 302199CWP GE CFM56 CFM562C 13802NE LT MLG WW CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 ITEM REF. NR. 033296: LT MLG W/W CHANNEL UPPER AFT CORNER CRACKED 0.250 INCH, FS 978.000. REMOVED CRACKED CHANNEL IAW SRM 51-1-21. FABRICATED NEW CHANNEL (AL 7075T6 0.063 INCH) IAW SRM 57-2-0 PG. 1. CLEANED, TREATED AND PRIMED AREA AND CHANNEL IAW SRM 51-1-8B. INSTALLED NEW CHANNEL IAW SRM 51-1-21, SRM 51-1-20D, SRM 51-3-0 TORQUED IAW SRM 51-3-1 PG. 3. 2L74 4F4 FRT4A25 E2GL 20060106000612006010600061WP 2006 1 6 DHL2005803520 120051129A575457695831 STRUCTURE DOUG DC8 DC873 302199CWP GE CFM56 CFM562C 13802NE LT LE SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 ITEM REF. NR. 033485: LT OB SLAT UPPER DOOR CRACKED (CTR DOOR). REMOVED AND REPLACED CTR DOOR ON LT OB SLAT UPPER DOOR IAW MM 27-80-2 PG. 201-203. FOR OPS CHECK SEE NR 038928. 2L74 4F4 FRT4A25 E2GL 20060106000902006010600090WP 2006 1 6 MWEA050136 120051216A521059100817 SKIN DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE PAX DOOR BENT A MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 PASSENGER DOOR OUTER SKIN BENT AT LOWER REAR EDGE FROM JETWAY. COLD FORMED OUTER SKIN. 2L72 4F4 F A6WE E9NE 20060109000352006010900035 2006 1 9 DHL2005785001 420051022A3414 INDICATOR BOEING727 727214 138407RNM COCKPIT INOPERATIVE A DHLAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO01785AT 21691 CAPTAINS AIRSPEED INDICATOR INOP. SWAPPED NR 1/2 ASI FOR T/S, NO HELP. REPOSITIONED TO ORIGINAL. BLEW OUT CAPTS PITOT TUBE, REMOVED DEBRIS. PERF PITOT TEST AND OPS CK GOOD PER B727 MM 34-11-0. 2L73 4F A3WE 20060109000382006010900038WP 2006 1 9 DHL2005802010 120051116A5210 DOOR DOUG DC8 DC873 302199CWP MAIN PAX DAMAGED A DHLAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01802DH 46076 FOUND L1 DOOR DAMAGED BY STAIRS. REMOVED DAMAGED AREA FROM BTM FWD LWR AREA OF DOOR STRUCTURE. FABRICATED DOOR FRAME SEGMENT DOUBLER FROM 2024-T3, .070. INSTALLED REPAIR USING EXSISTING RIVET SPACING AND SECOND ROW SPACING PER SRM. 2L74 4F RT4A25 20060109000392006010900039EU 2006 1 9 DHL2005366007 120051026A2420977J1504 GENERATOR AIRBUS300 A300B4203 3930306EU NR 1 ENGINE FAILED A DHLAB EMER. DESCENT HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 SO01366DH 249 NR 1 ENG DRIVEN GENERATOR FAILED INFLIGHT. ABNORMAL PRODCEDURE COMPLETED NO VOLTS AND NO FREQS INDICATED. REPLACED NR 1 GENERATOR IAW M/M 24-21-11. GROUND RUN OPS CK GOOD. 2L72 4F RTA35EU 20060109000412006010900041NM 2006 1 9 DHL2005762004 120051028A3350MISC062 BATTERY BOEING727 7272B7 138407LNM EMERGENCY LIGHT INOPERATIVE A DHLAK NONE O OTHER ININSP/MAINT 1 SO01762AT 22162 EMERGENCY EXIT LIGHT IN GALLEY WON`T TEST. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERIES IAW M/M 33-50-101, OPS CK NORMAL P/N MISC062. 2L73 4F A3WE 20060109000432006010900043 2006 1 9 DHL2005745011 420051116A34149B810201 INDICATOR BOEING727 727224 1384076NM AIRSPEED INOPERATIVE A DHLAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 SO01745DH 20665 CAPTAINS AIRSPEED INDICATOR INOP. STBY AIRSPEED INDICATOR INDICATIONS NOT NOTED. ABORTED TAKEOFF AT APPROXIMATELY 70 KIAS PRESSURE ALT 26FT. AIRCRAFT WEIGHT 137,100 LB REVERSE THRUST NOT USED. REMOVED AND REPLACED CAPT A/S IND IAW M/M 34-12-21. REMOVED AND REPLACED NR 1 ADC IAW M/M 34-12-03. FLUSHED PITOT SYSTEM ON CAPT SIDE IAW 34-11-00. CHECKED STBY A/S IND. ALL SYSTEM GRD. OPS CKD NORMAL. 2L73 4F A3WE 20060109000502006010900050NM 2006 1 9 QXEA200501859 120051230A242031708001A GENERATOR DHAV DHC8 DHC8202 2809007NM AC SYSTEM MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09346PH132701172 477 RDM FLIGHT NR 2179, GOT NR 1 AC GENERATOR CAUTION LIGHT, WOULD NOT RESET PER EMERGENCY CHECKLIST. MAINTENANCE REPLACED NR 1 AC GENERATOR. AFTER, GROUND RAN BOTH ENGINES AND COMPLIED WITH OPERATIONAL CHECK IAW TASK AMM 24-21-00-000-801, 24-21-00-400-801 AND FUNCTIONAL TEST 24-21-00-720-801. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20060109000522006010900052EA 2006 1 9 COMA0560757 120051230A5730601R3103215 CHANNEL CNDAIRCL600 CL6002B19 1900309EA BS 399-409 CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA29272 7031 FLOOR SEAT RAIL CORRODED. REPAIRED RT FLOOR SEAT RAIL FROM FS 399.5 TO 409+126 BY REMOVING AND REPLACING TRACK IAW BRAS EO 601R-53-7965A. 2L72 4F RTA21EA 20060109000542006010900054NM 2006 1 9 DHL2005785002 120051027A3350 LIGHT BOEING727 727214 138407RNM COCKPIT INOPERATIVE A DHLAK NONE O OTHER ININSP/MAINT 1 SO01785AT 21691 FOUND COCKPIT EMERGENCY EXIT BACKLIT SIGN INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY, OPS CHK'D GOOD IAW MM 33-50-71. 2L73 4F A3WE 20060109000572006010900057NM 2006 1 9 DHL2005788018 120051009A326069141001 BUNGEE CORD BOEING727 727214 138407RNM CARGO DOOR DAMAGED A DHLAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO01788AT 21958 FORWARD GEAR DOOR LIGHT AND S/O NOSE GEAR DOOR LIGHT ON WITH GEAR HANDLE IN OFF POSITION. GOES OUT IN UP POSITION. TRANSFERRED TO DMI LOG ITEM NR 22747 IAW ASTAR MEL 32-1 CAT "C". PLACARDS INSTALLED. REF DMI NR 22747 FWD GEAR DOOR LIGHT AND T/O NOSE GEAR DOOR LIGHT ON WITH GEAR HANDLE IN OFF POSITION. GOES OUT IN UP POSITION. REPLACED LOCK SPRING BUNGEE IAW BMM 32-21-0. RIGGED AND INSPECTED NOSE GEAR RETRACTION SYSTEM IAW BMM 32-35-0. OPS NORMAL, THIS CLEARS DMI 22747 PLACARD REMOVED. 2L73 4F A3WE 20060109000592006010900059EU 2006 1 9 DHL2005367004 120051115A5210 PANEL AIRBUS300 A300B4203 3930306EU PAX DOOR BINDING A DHLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01367DH 265 LEFT MAIN ENTRY DOOR LIGHT ILLUMINATED DURING CLIMB-OUT. BOTH VISUAL INDICATORS INDICATED RED AND 1/2 GREEN. DIFFERENTIAL PRESSURE WAS 2.6 L1 DOOR UPPER COSMETIC PANEL HITTING UPPER DOOR PANEL. CHECKED WIRING AT 43WS INSPECTED LOCK MECH NO DEFECTS NOTED. FOUND COSMETIC DOOR PANEL BINDING AT DOOR FRAME REMOVED PANEL, OPS CKD PER MM 52-71-11. 2L72 4F RTA35EU 20060109000632006010900063EU 2006 1 9 06FDEA0001 120051230A5270 SWITCH AIRBUS300 A300B4622R 3930312EU PAX DOOR LOOSE A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25719FD 388 AVIONICS LIGHT, CHIME CAME ON PASSING 10000 EXECUTED TURNBACK TO KSMP. BURN TO MAX LANDING WEIGHT. FOUND AVIONICS DOOR FLUSH TO FUSELAGE AND DOOR LATCH APPROX 1/8 INCH DOWN. ON INSPECTION FOUND DOOR LOCKED SWITCH WITH BROKEN SAFETY WIRE. RETIGHTENED SWITCH. OPS NORMAL PER A300 MM REF 52-41-14-5 DOOR VERIFIED CLOSED ON DEPARTURE WITH NO LIGHT. 2L72 4F RTA35EU 20060109000842006010900084NM 2006 1 9 AWXA200600002 120051230A3260189929 PROXIMITY SENSOR BOEING737 7373G7 1384595NM MLG MALFUNCTIONED A AWXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP28311AW 24712 LAX - AIR TURNBACK - FLT 277 - AFTER TAKEOFF CREW WAS UNABLE TO RETRACT GEAR. CREW REPORTED 3 GREEN DOWNLOCK LIGHTS AND 3 RED INTRANSIT LIGHTS AFTER FLAPS FULLY RETRACKED, AND RECIEVIED TAKE OFF CONFIGURATION WARNING HORN. CREW RETURNED TO LAX, DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE PERFORMED TROUBLESHOOTING IAW BOEING 737-300 MM 32-31-21. REMOVED AND REPLACED THE AIR SENSING SQUAT SWITCH, M991, IAW BOEING 737-300 MM 32-09-01-5. ALSO REPLACED THE LANDING GEAR CONTROL LEVER LOCK SOLENOID IAW BOEING 737-300 MM 32-31-31-4. OPERATIONAL CHECKS AND GEAR SWINGS WERE GOOD. 2L72 4F RTA16WE 20060109000852006010900085NM 2006 1 9 AWXA200600003 120051231A3097 WIRE BOEING737 7373G7 1384595NM ANTI ICE SYSTEM CHAFED A AWXAA UNSCHED LANDING O OTHER CRCRUISE 1 WP28154AW 23776 LAS - DIVERSION - FLT 0504 - AFTER DEPARTURE CREW REPORTED THE LEFT ENG ANTI-ICE C/B POPPED. CREW ATTEMPTED AN AIR TURN BACK TO PHX BUT WAS UNABLE TO DUE TO WEATHER. DIVERTED TO LAS AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE TROUBLESHOT AND FOUND CHAFED WIRES ABOUT THREE INCHES BACK FROM THE INLET COWL TAI VALVE CONNECTOR. REPAIRED WIRES IAW SWPM 20-10-13. OPERATIONAL CHECKS WERE GOOD IAW BOEING 737-300 MM 30-21-13. 2L72 4F RTA16WE 20060109000862006010900086WP 2006 1 9 05FDEA04280 120051213A5300 REPAIR DOUG DC10 DC1010 3022110WP BS 1205 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25563FE 46948 LOWER FUSELAGE BELLY SKIN FOUND AN EXTERNAL DOUBLER REPAIR AT STA 1205 LONG 52 DIM 4" BY 4". PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 53-40-00 FIG 20 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO# 8-5100-7-5001 P1. 2L73 4F A22WE 20060109000892006010900089WP 2006 1 9 05FDEA04283 120051213A5300 REPAIR DOUG DC10 DC1010 3022110WP BS 1256 UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25563FE 46948 MAIN CABIN R-3 FWD DOOR JAMB HAS AN EXTERNAL DOUBLER REPAIR BOTTOM PART STA 1256 DIM 7" BY 9.75". PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 53-50-00 FIG 19 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2. 2L73 4F A22WE 20060109000912006010900091EA 2006 1 9 COMA0560755 120051230A5347601R3103221 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA BS 399-409 CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA29272 7031 FLOOR SEAT RAIL CORRODED FROM FS399.50 TO FS 409+126. REPAIRED LT FLOOR SEAT RAIL FROM FS 399.50 TO FS 409+126 BY REMOVING AND REPLACING TRACK IAW BRAS EO 601R-53-7965A. 2L72 4F RTA21EA 20060109001002006010900100EA 2006 1 9 COMA0560761 120051229A5730601R100453 SKIN CNDAIRCL600 CL6002B19 1900309EA LT WING CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA29272 7031 LT LOWER WING PLANK HAS FRETTING CORROSION AT FUEL TANK ACCESS CUTOUTS, 540AB, (510AB AND 540BB NOT IN CRITICAL AREA), 540CB, 540EB, 540FB, 550AB, 550CB, 550DB, 550EB, 550FB. REPAIRED LOWER WING PLANK FUEL ACCESS CUTOUTS IAW BOMBARDIER REO 601R-57-21-030. REFER TO TR 2B-2093 FOR REINSPECT INTERVALS FOR THE FOLLOWING:540AB, 540CB, 540EB, 540FB, 550AB, 550CB, 550DB, 550EB, 550FB. 2L72 4F RTA21EA 20060109001022006010900102EU 2006 1 9 AWXA200600001 120051217A5315D53472189200 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28649AW 803 MCN - DURING INSPECTION CORROSION DISCOVERED ON CABIN FLOORBEAM AT FS 68 TO FS 79 AND AT BL Y-1235. MAINTENANCE REMOVED CORROSION AND WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 310 SRM 53-00-14 FIG 102. REMOVED AND INSTALLED NEW FLOORBEAM AT FR 68 TO FR 69 AND Y-1235 IAW AIRBUS 320 SRM 51-42-11. 2L72 4F RTA28NM 20060109001042006010900104EU 2006 1 9 AWXA200600005 120051216A5347D5347219020590 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28649AW 803 DURING INSPECTION DISCOVERED CORROSION ON SEAT TRACK AT FORWARD WALL OF LAVE E OUTBOARD ATTACH POINT FROM FS 65 TO FS 68 AND BL Y-1292. CORROSION ON SEAT RAIL BEAM WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-14 FIG 102. MAINTENANCE REMOVED AND INSTALLED NEW SEAT RAIL BEAM FROM FS 65 TO FS 68 AND BL Y-1292 IAW AIRBUS 320 SRM 51-72-11. 2L72 4F RTA28NM 20060109001062006010900106EU 2006 1 9 AWXA200600007 120051216A5347D5347219020300 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28649AW 803 MCN - DURING INSPECTION DISCOVERED SEAT RAIL BEAM CORRODED AT AFT WALL OF LAVE, INBOARD ATTACH POINT, AT FS 65 TO FS 68 AND BL Y-1225. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-14 FIG 102. REMOVED AND INSTALLED NEW SEAT TRACK RAIL IAW AIRBUS 320 SRM 51-72-11. 2L72 4F RTA28NM 20060109001402006010900140NE 2006 1 9 DHL2005805006 220051220A73104892944226 O-RING DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C1 13802NE BOOST PUMP LEAKING A DHLAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION TXTAXI/GRND HDL 1 SO01805DH 46125 NR 1 ENGINE AT IDLE WHILE STARTING NR 4 ENGINE NR 1 ENGINE FLAMED OUT NORMAL INDICATIONS, REPEAT WRITE UP 12/15. PERFORMED DECAY CHECK ON NR 1 ENG FUEL FEED SUPPLY SYSTEM. NR 1 ENG FEED FAILED CHECK. REMOVED AND REPLACED O-RINGS ON FEED LINE BOOST PUMP TO FRONT SPAR IN NR 1 MAIN TANK. OPS CHECKED GOOD IAW DOUGLAS REPORT MSK91K0578, P/N 4892944-226. 2L74 4F4 FRT4A25 E2GL 20060109001442006010900144NM 2006 1 9 DHL2005743003 120051014A3350 LIGHT BOEING727 727225 1384077NM CABIN DISLODGED A DHLAO OTHER D INFLIGHT SEPARATION NRNOT REPORTED 1 SO01743DH 22438 EMERGENCY EXIT LIGHT ABOVE MAIN ENTRY DOOR HAS FALLEN OFF. RESECURED EMERGENCY EXIT LIGHT ASSY IAW 727 MM 33-50-71, OPS GOOD. 2L73 4F A3WE 20060109001492006010900149WP 2006 1 9 AALA20050841 120051223A26112026TP DUCT DOUG DC9 DC983 3022083WP ANTI ICE RUPTURED A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21567AM 53293 MCO - ON CLIMBOUT AT ABOVE 1700 WITH CLIMB POWER, LEFT B-LOOP CAME ON. SHORTLY AFTER LEFT A-LOOP CAME ON. LEFT FIRE WARNING CAME ON IMMEDIATELY. LEVELED OFF AT 18,000 AND PULLED POWER BACK TO 1.40 ENGINE PRESSURE RATIO AND WARNING WENT OUT. RETURNED TO MCO AND LANDED WITHOUT INCIDENT. NO FURTHER WARNINGS WERE OBSERVED AT ANYTIME. SHUTDOWN ENGINE AFTER LANDING. REPLACED RUPTURED REAR ANTI ICE DUCT ON LEFT ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20060109001512006010900151NM 2006 1 9 AALA20050843 120051227A2932 TRANSFER VALVE BOEING757 757223 1384957NM RT HYD QTY INOPERATIVE A AALAO OTHER J WARNING INDICATION CRCRUISE 1 SW21688AA 25730 ORD - EICAS MESSAGE RIGHT HYDRAULIC QUANTITY WITH RESERVOIR LIGHT ILLUMINATED. FLIGHT CONTROLS WERE NORMAL UNTIL APPROACH WHEN CONTROL PROBLEM STARTED. REINSTATED BOTH RIGHT HAND HYDRAULIC PUMPS. FLIGHT CONTROLS WERE THEN NORMAL FOR LANDING. TIGHTENED LOOSE B-NUT AT BRAKE TRANSFER VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20060109001532006010900153NM 2006 1 9 AALA20050837 120051220A3397 CONNECTOR BOEING777 777223 1385213NM EMERGENCY LIGHT LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21792AN 30253 BOS - EMERGENCY ESCAPE PATH LIGHT AT SEAT 4G INOPERATIVE. FOUND LOOSE CONNECTOR ON SEAT 4G. RESECURED CONNECTOR ON SEAT 4G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20060109001542006010900154 2006 1 9 MWEA050141 420051222A34604087440927 DISPLAY BOEING717 717200 1383700NM COCKPIT FAILED A MWEAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL31910ME 55174 NUMBER TWO DISPLAY UNIT FAILED AND CABIN WAS FILLED WITH SMOKE. REMOVED AND REPLACED NUMBER TWO DISPLAY UNIT. 2L72 4F TRA6WE 20060109001562006010900156WP 2006 1 9 AALA20050838 120051221A3233 ACTUATOR DOUG DC9 DC983 3022083WP MLG INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 SW21590AA 53253 JFK - FLIGHT DIVERTED TO JFK DUE TO THREE RED GEAR WARNING LIGHTS WHEN LANDING GEAR WAS LOWERED. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND LANDING GEAR HANDLE MECHANICALLY BINDING. FREED UP SLIDING ACTION OF HANDLE AND THREE RED LIGHTS EXTINGUISHED. AIRCRAFT FERRIED GEAR DOWN TO LGA FOR FOLLOW UP. REPLACED ROLLER ACTUATOR FOR 5189 SWITCH AT LANDING GEAR HANDLE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20060109001582006010900158WP 2006 1 9 AALA20050840 120051222A3350 CONTACT DOUG DC9 DC982 3022082WP BATTERY PACK INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21479AA 49654 LGA - EMERGENCY LIGHTS AT ROWS 29 TO 32 INOPERATIVE. CLEANED CONTACTS ON ROW 29 BATTERY PACK FOR EMERGENCY LIGHTS AT ROWS 29 TO 32. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20060109001592006010900159NM 2006 1 9 CALA0500456 120051230A5320147A57123 WEB BOEING737 737724 13844BYNM BS 986.5 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2715710 28780 INSPECTION FOUND RT WEB CORRODED AT STA 986.5 RBL 32 TO RBL 33. REPAIRED WEB IAW SRM 51-70-13. 2L72 4F RTA16WE 20060109001612006010900161NM 2006 1 9 CALA0500458 120051228A5315141T5112 FLOORBEAM BOEING767 767224 1385170NM BS 303 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776153 30432 INSPECTION FOUND FLOORBEAM CORRODED AT BS 303, LBL 19 TO LBL 32. REPAIRED IAW SRM 53-00-51, FIGURE 201, REPAIR 1. 2L72 4F RTA1NM 20060109001652006010900165NM 2006 1 9 CALA0500463 120051222A57206545402279 STIFFENER BOEING737 7373T0 1384582NM BS 540 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714358 23943 A 2 INCH CRACK WAS FOUND TO THE WING CENTER SECTION REAR SPAR AT STA 540, RBL 6.15 VERTICAL STIFFENER DURING A WALKAROUND INSPECTION. AN INTERIM REPAIR WAS INSTALLED PER EA 5714-01002, REV C, OP 8 AND ECRA 5714-01011. A DIP WAS ISSUED TO REINSPECT THE STIFFENER EVERY 4500 FLIGHT CYCLES AND TO REPLACE BOTH STIFFENERS (RBL 6.15 AND LBL 6.15) WITHIN 15,000 FLIGHT CYCLES. 2L72 4F RTA16WE 20060109001672006010900167EA 2006 1 9 COMA0560786 120051230A5347601R310327 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA CABIN CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA27272 7031 LEFT FLOOR SEAT RAIL CORRODED FROM FS 559+16 TO FS 559+98. REPAIRED LEFT FLOOR SEAT RAIL FROM FS 559+16 TO FS 559+98 BY BLENDING SEAT RAIL IAW CRJ SRM 53-51-49. 2L72 4F RTA21EA 20060109001712006010900171NM 2006 1 9 UPS06245912 120051221A5754 RIB BOEING727 72722C 138400FNM NR 7 SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE:C RIGHT NR 7 SLAT ACTUATOR RAM FWD ATTACHMENT FITTING INBOARD SUPPORT RIB CRACKED. PLS INVESTIGATE AND RECTIFY. SLAT ACTUATOR RIBS I/B AND O/B DISPLACED IAW SRM 51-30-3. HFEC CARRIED OUT AND FWD ATTACH FITTING INBOARD SUPPORT RIB CRACKS CONFIRMED. CRACKS STOP DRILLED. HFEC CARRIED OUT AND 2 ADDITIONAL CRACKS FOUND. O/B WEB REMOVED AND I/B WEB REMOVED. WEBS FABRICATED IAW BOEING DRAWING 65-17306-3. NR 7 SLAT ACTUATOR I/B AND O/B WEBS INSTALLED IAW BOEING DRAWING 65-17306. 2L73 4F A3WE 20060109001722006010900172EA 2006 1 9 COMA0560774 120051230A5347601R3831231 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA BS 364-409 CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA29272 7031 LT SIDE SEAT RAIL CORRODED FROM FS 364 TO FS 409+18.02. REPAIRED LT SEAT RAIL FROM FS 364 TO FS 409+18.02 BY REMOVING AND REPLACING SEAT RAIL IAW BOMBARDIER EO 601R-53-7965A. 2L72 4F RTA21EA 20060109001782006010900178EA 2006 1 9 COMA0560777 120051230A5347601R3831229 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA CABIN CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA29272 7031 RT SIDE SEAT RAIL CORRODED FROM FS 409+18.02 TO FS 409+111.02. REPAIRED RT SIDE SEAT RAIL FROM FS 409+18.02 TO FS 409+111.02 BY REMOVING AND REPLACING SEAT RAIL IAW BOMBARDIER EO 601R-53-7965A. 2L72 4F RTA21EA 20060110000122006011000012EA 2006 1 10 COMA0560779 120051230A5347601R38312115 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA BS 444-495 CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA29272 7031 RIGHT SIDE SEAT RAIL CORRODED FROM FS 444.02 TO FS 495.98. REPAIRED RIGHT SIDE SEAT RAIL FROM FS 444.02 TO FS 495.98 BY REMOVING AND REPLACING SEAT RAIL IAW BOMBARDIER EO 601R-53-7965A. 2L72 4F RTA21EA 20060110000142006011000014 2006 1 10 UPS05145902 420051229A2565 SLIDE AIRBUSA300 A300F4622R 3930360EU CABIN DEPLOYED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01126UP 0810 INSPECTION TYPE:N/A EMERGENCY SLIDE DEPLOYED. INSTALLED SERVICEABLE ESCAPE SLIDE IAW AMM 25-61-21-4. 2L72 4F RTA35EU 20060110000152006011000015SO 2006 1 10 C2XA05SH146 120051231A491014547494607 FIREWALL EMB 135 EMB135LR 3260305SO APU BAY CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2728529 145512 SHV - DURING C-CHECK MAINTENANCE FOUND APU FIREWALL CRACKED AT MULTIPLE LOCATIONS. MAINTENANCE REMOVED & REPLACED APU FIREWALL IAW EMB 145 EA 5340-01016. AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2L72 4F RTT00011AT 20060110000172006011000017EA 2006 1 10 COMA0560775 120051230A5347601R3831231 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA BS 364-409 CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA29272 7031 RT SIDE SEAT RAIL CORRODED FROM FS 364 TO FS 409+18.02. REPAIRED RT SIDE SEAT RAIL FROM FS 364 TO FS 409+18.02 BY REMOVING AND REPLACING SEAT RAIL IAW BOMBARDIER EO 601R-53-7965A. 2L72 4F RTA21EA 20060110000192006011000019EA 2006 1 10 COMA0560782 120051230A5347601R38312131 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA BS 495-535 CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA29272 7031 LEFT SIDE SEAT RAIL CORRODED FROM FS 495.98 TO FS 535.02. REPAIRED LEFT SIDE SEAT RAIL FROM FS 495.98 TO FS 535.02 BY REMOVING AND REPLACING SIDE SEAT RAIL IAW BOMBARDIER EO 601R-53-7976A. 2L72 4F RTA21EA 20060110000202006011000020EA 2006 1 10 COMA0560783 120051230A5347601R38312131 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA BS 495-535 CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA29272 7031 RIGHT SIDE SEAT RAIL CORRODED FROM FS 495.98 TO FS 535.02. REPAIRED RT SIDE SEAT RAIL FROM FS 495.98 TO FS 535.02 BY REMOVING AND REPLACING SEAT RAIL IAW BOMBARDIER EO 601R-53-7965A. 2L72 4F RTA21EA 20060110000222006011000022EA 2006 1 10 COMA0560785 120051230A5347601R387799 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA BS 559 CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA29272 7031 FLOOR SEAT RAILS CORRODED AT FS 559+96 RBL 9, LBL 9 AND LBL 27. REPAIRED FLOOR SEAT RAILS AT FS 559+96 RBL 9, LBL 9 AND LBL 27 BY REMOVING AND REPLACING SEAT RAIL IAW BOMBARDIER EO 601R-53-7965A. 2L72 4F RTA21EA 20060110000242006011000024CE 2006 1 10 DXTA200501159 120051223A3230 INDICATOR CESSNA750 750 2076810CE MLG MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07975QS 7500175 WHEN SELECTED GEAR UP AFTER TAKEOFF THE RED UNLOCK REMAINED ON AND COULD STILL HEAR THE WIND NOISE FROM ONE OR MORE GEAR STILL NOT UP FULLY. SELECTED GEAR DOWN AND GOT 3 GREEN, NO RED AND LANDED. 2L72 4J RTT00007WI 20060110000262006011000026 2006 1 10 DXTA200501154 420051221A2200 WARNING SYSTEM CESSNA750 750 2076810CE PITCH FEEL ACTIVATED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07937QS 7500137 PITCH FEEL FAIL CAS DURING CLIMBOUT. COMPLIED WITH PITCH FEEL FUNCTIONAL & OPERATIONAL CHECK IAW CE750 M/M 27-30-00. NO FAULTS NOTED. 2L72 4J RTT00007WI 20060110000282006011000028CE 2006 1 10 DXTA200501155 120051222A2821 FUEL FILTER CESSNA560 560XL 2076702CE RIGHT BYPASSING E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07662QS 5605262 RIGHT FUEL FILTER BYPASS LIGHT CAME ON WITH APPLICATION OF T/O POWER DURING TAKEOFF ROLL. REMOVED AND REPLACED RIGHT FUEL FILTER IAW P&W 545 M/M CH 73-10-05, OPS AND LEAK CHECKS SATISFACTORY. 2L72 4F RTA22CE 20060105002442006010500244NE 2006 1 5 P5CA0501416 220051120A73209P6M74G01 METERING TUBE BOEING747 747230B 1384889NM GE CF6 CF650E2 30018NE NR 1 ENGINE LEAKING A P5CAK NONE K FLUID LOSS TXTAXI/GRND HDL 1 WP23508MC 21644 517529 NR1 ENGINE FUEL LEAK AT FUEL METERING UNIT VBV ROD END TUBE. VBV ACTUATOR FUEL TUBE REPLACED AT FUEL CONTROL AND PERFORMED ENGINE RUN AND LEAK CHECK IAW MM 73-21-01. 2L74 4F4 F A20WE E23EA 20060105002702006010500270EA 2006 1 5 QXEA200501748 120051031A3220 TORQUE TUBE CNDAIRCL600 CL6002C10 1390015EA NLG CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 NOSE GEAR OUTER TORQUE TUBE HAS CORROSION. REPAIRED CORROSION IAW EA R-32-199 AND REO 670-32-21-076 AND SCR 0008-04 REVISION 6. 2L72 4F RTA21EA 20060105002922006010500292NM 2006 1 5 AWXA200501480 120051203A3350BR964411 LIGHT BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28328AW 23377 EEL - DURING INSPECTION DISCOVERED EMERGENCY LIGHT AT ROW 5, LT, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. 2L72 4F4 FRTA16WE E21EU 20060105002932006010500293EU 2006 1 5 AWXA200501481 120051204A3150 WARNING SYSTEM AIRBUS320 A320232 3930326EU IAE V2524 V2524A5 NE COCKPIT MALFUNCTIONED A AWXAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 WP28652AW 953 DURING TAKEOFF, CREW REPORTED ECAM MESSAGE (ENG 1 COMPRESSOR VANE). CREW ABORTED TAKEOFF AT ESTIMATED 60 KNOTS AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED TROUBLESHOOTING IAW SRM 75-30-00-810-843 AND TASKCARD FSM 71312, NO FAULTS WERE FOUND. 2L72 4F4 FRTA28NM E40NE 20060105003042006010500304EU 2006 1 5 05FDEA04171 120051207A5101 DOUBLER AIRBUS310 A310 EU GE CF6 CF680A3 30025NE FUSELAGE NONE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25423FE 281 PREVIOUS REPAIR INSTALLED AT FUSELAGE LT EXT DOUBLER ABOVE AND AFT OF CAPT,S SIDE WINDOW, STA. 881 TO 904 FR 7 TO FR 8 NEEDS EVALUATION FOR MAJOR MINOR CLASSIFICATION AND APPROVED REPAIR DATA REF N00696 REPAIR GOOD IAW EA 6-5330-95466. 2L72 4F4 FRTA35EU E13NE 20060105003182006010500318EU 2006 1 5 XN0A1282 120051210A2710 CONNECTOR AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE AILERON DISCONNECTED A XN0AD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL23307FV 235 LT LOW SPEED AILERON WILL NOT CONNECT FOR TAKE-OFF AND THE RT LOW SPEED AILERON IS CONNECTED. CONNECTED THE LT LOW SPEED AILERON CONNECTOR PLUG, SYSTEM OPS CHECKS GOOD IAW AMM 27-11-01.THIS CLEARS DMI NR 5967.(STATUS:ORIG/CLOSED) 2L72 4F4 FRTA35EU E23EA 20060105003212006010500321EU 2006 1 5 05FDEA04214 120051210A5522 SKIN AIRBUS310 A310 EU ELEVATOR DEBONDED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25424FE 241 SMIS 424 51-00 0007102 27SEP05 MC1 CLOSE R MOD TYPE Y MOD NR 9-AGING-INSP REV NO. PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NO. POS PT1 ENT BY: 067708 INFO 30NOV05 21:26 MC1 R DISCREPANCY (N00094) LT HORIZ STAB, ELEVATOR WITH DEBONDING ON TRAILING EDGE UPPER AND LOWER SIDE SKIN SURFACES (FRACTION NR 2) REPAIR CONFORMS TO EXISTING ENGINEERING AUTHORIZATION EA 6-5510-94659. REPAIR EVALUATED IAW GMM 6-2-100 AND CLASSIFIED MAJOR. 2L72 4F RTA35EU 20060105003232006010500323SO 2006 1 5 62512082005 120051208A5101 UNKNOWN GULSTMGV GULFSTREAMGV3980116SO RROYCEBR700 BR700710A110 NE RT MLG UNKNOWN E N93AK NONE O OTHER TXTAXI/GRND HDL 1 SO13507QS 625 WHILE TAXING AIRCRAFT RT MAIN GEAR DEPARTED TAXI WAY. 2L72 4F4 FRTA12EA E00057EN 20060105003292006010500329EA 2006 1 5 QXEA200501853 120051221A801135059532 STARTER CNDAIRCL600 CL6002C10 1390015EA NR 1 FAILED A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09606QX6099 10023 PDX - PUSHBACK FOR FLIGHT 2473, LEFT ENGINE WILL NOT START. ENGINE START STATUS MESSAGE APPEARS BUT THERE IS NO N2 ROTATION. RETURNED TO THE GATE. REPLACED NR 1 STARTER IAW IAM 80-11-01 PGS 401-406, LEAK AND OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20060106000192006010600019WP 2006 1 6 DHL2005803532 120051205A57535751183505 FITTING DOUG DC8 DC873 302199CWP GE CFM56 CFM562C 13802NE LT TE FLAP BROKEN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 LT IB FLAP OB FITTING BROKEN STA 97.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0. REMOVED BROKEN FITTING IAW SRM 51-1-21, SRM 51-1-20D, SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PAGE 9. INSTALLED NEW FITTING IAW SRM 51-1-21, SRM 51-1-20D, SRM 51-3-0, SRM 51-3-1. FOR OPS CHECK SEE NR 038928. 2L74 4F4 FRT4A25 E2GL 20060106000202006010600020WP 2006 1 6 DHL2005803530 120051208A574046143912 CLIP DOUG DC8 DC873 302199CWP GE CFM56 CFM562C 13802NE RT WING BROKEN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 RT WING NR3 MAIN TANK INTERNAL STRUCTURE CLIP BROKEN XRS 22.000 S-63. REMOVED AND REPLACED CLIP ON RT WING NR3 MAIN TANK INTERNAL STRUCTURE XRS 22.000 S-63 IAW SRM 51-1-20D, SRM 51-3-1. FOR LEAK CHECK SEE NR 039053. 2L74 4F4 FRT4A25 E2GL 20060106000292006010600029WP 2006 1 6 DHL2005803544 120051208A534047518202 FITTING DOUG DC8 DC873 302199CWP GE CFM56 CFM562C 13802NE BS 798 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 ITEM REF. NR. 038465: WING CTR SECTION FITTING CRACKED 1 INCH STA 798.000 RBL 22 INCH (MAIN CARGO COMPT). REMOVED CRACKED FITTING AT STA 798.000 RBL 22 INCH IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D. TORQUED IAW SRM 51-3-1. REFER TO JC EA53100137-001-D (W.O. 600014514) FOR FITTING FABRICATION. 2L74 4F4 FRT4A25 E2GL 20060106000302006010600030WP 2006 1 6 DHL2005803557 120051216A5330 SKIN DOUG DC8 DC873 302199CWP GE CFM56 CFM562C 13802NE BS 69.500 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 PERFORM PREVENTATIVE MODIFICATION IAW SB 57-88 REV. 3 ON RT WING LOWER SKIN CRACK AT STA 69.5 REF. SB AND DRAWING J060095-505. PERFORMED PREVENTATIVE MODIFICATION IAW AD80-22-01, SB 57-88 REV. 3 DWG NRJO60095-505. REMOVED FASTENERS AND SKI FITTING IAW DWG JO60095-505, SRM 51-3-0, SRM 51-1-20D. PERFORMED NDT INSPECTION IAW NDT SPM PART 6-10-01-001. NO CRACK FOUND. (ENCLOSED SMN FORM 242-2) INSTALLED DOUBLER, TRIPLET AND SKI FITTING (NEW) IAW DWG JO60095-506, DPS 3.67-56, SRM 51-1-22, SRM 51-1-26, SRM 51-1-11 PAGE 9, SRM 51-3-0, SRM 51-1-20D, SRM 51-3-1. FOR FUEL LEAK CHECK SEE NR 039053. 2L74 4F4 FRT4A25 E2GL 20060106000352006010600035NE 2006 1 6 WRNA20050029 220051210A7200JT9D7Q ENGINE BOEING747 7472U3B 1384846NM PWA JT9 JT9D7Q 52054NE NR 2 MALFUNCTIONED A WRNAEA ENGINE SHUTDOWN UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO05923FT601843218 22769 702370 CLIMBING OUT THRU 16K FT, NR 2 ENGINE SHUTTERED, ACCOMPANIED BY LOUD NOISE. HIGH EGT, EPR AND OIL PRESSURE, TEMP ALL WITHIN LIMITS. SHUT DOWN NR 2 ENGINE. AIRCRAFT RETURNED TO FIELD, LANDING NORMAL. 2L74 4F4 FRTA20WE E3NE 20060106000362006010600036EU 2006 1 6 200512101 120051210A361010012461 BLEED VALVE EMB ERJ170ERJ170100 EU GE CF34 CF348E5 30015NE BLEED AIR SYS FAILED A UHLAO OTHER J WARNING INDICATION TOTAKEOFF 1 GL17651RW54 54 17000072 CREW REPORTED ENGINE 1 AND ENGINE 2 BLEED LEAK MESSAGE. VERIFIED THAT ENGINE BLEED VALVE FAILED OPEN DURING TAKEOFF. 2L74 4F4 FRTA56NM E00063EN 20060106000402006010600040EA 2006 1 6 N6WA00512001 120051210A2730601R05441 TRANSMITTER CNDAIRCL600 CL6002C10 1390015EA ELEVATOR FAULTY A N6WAB EMER. DESCENT N FALSE WARNING CLCLIMB 1 CE03153GJ 10219 ELEVATOR SPLIT MESSAGE DISPLAYED ON EICAS DURING CLIMBOUT. REPLACED ELEVATOR POSITION TRANSMITTER ON THE RT IAW MM 27-34-10. OPS CHECK GOOD. 2L72 4F RTA21EA 20060106000412006010600041EA 2006 1 6 REXA200500154 120051212A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA T/E FLAP MALFUNCTIONED A REXAK NONE J WARNING INDICATION APAPPROACH 1 SO258721B 7721 FLAPS FAIL AT 20 ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAPS AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01 2L72 4F RTA21EA 20060106000562006010600056NM 2006 1 6 PIDA06001 120051229A5230 WEB BOEING737 7373G7 1384595NM CFMINTCFM56 CFM563B2 13802EU FWD CARGO DOOR CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05390WL 23219 INNER WEB OF THE FORWARD CARGO DOOR IS CRACKED. REPAIRED DAMAGE IAW SRM 52-00-01 AND 51-70-13. 2L72 4F4 FRTA16WE E21EU 20060106000832006010600083SO 2006 1 6 SWIA200516001 120051211A275012064207615 LEVER EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE COCKPIT FAILED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07293SW7249 7249 120320 FLAPS WOULD NOT EXTEND TO TAKE OFF POSITION. REPLACED FLAP SELECTOR LEVER. OPERATIONAL CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20060106001022006010600102NM 2006 1 6 USAA051555 120051214A5347 SEAT TRACK BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 LOCATION: BS 727B LBL 45.5 (LT OB SEAT TRACK/FLOORBEAM) ACTION: FABRICATED AND INSTALLED NEW TRACK SECTION IAW SRM 53-00-02 REPAIR 3 DEFECT SIZE: .375 INCH. 2L72 4F RTA16WE 20060106001032006010600103NM 2006 1 6 USAA051556 120051214A5347BAC1520792 SEAT TRACK BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU 25022 LOCATION: BS727B RBL 24.75 (RT IB SEAT TRACK FLOOR BEAM) ACTION: FABRICATED AND INSTALLED NEW SECTION OF TRACK/BEAM IAW SRM 53-00-52 EA 97204 DEFECT SIZE: .250 INCH. 2L72 4F4 FRTA16WE E21EU 20060106001042006010600104NM 2006 1 6 USAA051550 120051214A5414 SKIN BOEING737 737301 1384611NM CFMINTCFM56 CFM563B2 13802EU NR 1 PYLON CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19591US 23936 LOCATION: IB SIDE OF NR 1 ENGINE PYLON. INSTALLED DOUBLER IAW TR 54-50-07, DEFECT SIZE: .250 IN. 2L72 4F4 FRTA16WE E21EU 20060106001062006010600106 2006 1 6 ASMF200512015 420051216A3441HG1050AD05 IRU BOEING757 7572Q8 1384972NM PWA PT6 PT6A67D NE RIGHT FAILED W ASMFK NONE J WARNING INDICATION ININSP/MAINT 1 SW23805AM24925 26272 DURING TRANSIT CHECK, THE LT RDMI SHOWED HDG AND VOR FLAGS. THE SENSORS WERE CHECKED IN FMC SHOWING THAT THE THREE INERTIAL UNITS WERE CORRECT; THE LT AND CENTRAL IRS ALIGN PROCEDURE WAS PERFORMED AND THE RMIS WERE INTERCHANGED, BUT FAILURE CONTINUED. THE RT AND CENTRAL IRS WERE ALIGNED, TESTED CORRECT, SO THE ALTERNATE IRS WAS SELECTED IN FIRST OFFICER PANEL, DISPATCHING THE AIRCRAFT. THE RT INERTIAL UNIT WAS REPLACED IAW MM 34-21-01 AND TESTS WERE PERFORMED IAW MM 24-21-00, BEING CORRECT. 2L72 4F4 TRTA2NM E26NE 20060109000022006010900002WP 2006 1 9 ABXA060009 120051220A534099155589 ATTACH ANGLE DOUG DC9 DC933F 302207AWP CABIN CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23932AX 47465 VENTRAL DOOR UPPER LEFT ATTACH ANGLE CRACKED AROUND RIVET. REMOVED, FABRICATED, AND INSTALLED NEW ANGLE IAW DC9 SRM 51-30-5. 2L72 4F A6WE 20060109000172006010900017WP 2006 1 9 DHL2005803526 120051204A5310 DOUBLER DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 MODIFICATION DOUBLER (ACS) CRACKED 0.500" ON AFT LWR CORNER OF LT PRIMARY HEAT EXCHANGER STA -12.000 L-27L. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 12/02/05, DWG AA33-53-R02 REV TR DATE 11/08/05. REMOVED FASTENERS IAW SRM 51-1-21. TRIMMED OUT DAMAGED SECTION, FABRICATED FILLER (2024T3AL 0.100") REPAIR DOUBLER (2024T3AL 0.050") TRIPLER DOUBLER (2024T3AL 0.063") IAW DWG AA33-53-R02. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS (CONICAL WASHERS) IAW DWG AA33-53-R02, SRM 51-1-21, SRM 51-1-20D, SRM 51-1-21, SRM 51-1-26, SRM 51-3-1 PG 2A. 2L74 4F RT4A25 20060109000202006010900020NM 2006 1 9 DHL2005745014 120051219A3260656021138 ACCESSORY UNIT BOEING727 727224 1384076NM MLG MALFUNCTIONED A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01745DH 20665 WHEN GEAR WAS SELECTED UP RED NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED. ALL DOORS LIGHTS WERE OUT. CYCLED GEAR AS DIRECTED BY MX. NOSE GEAR UNSAFE LIGHT WENT OUT. T/S TO LG ACCESSORY UNIT. REMOVED AND REPLACED LG ACCESSORY UNIT WITH SERVICEABLE UNIT. OPS CHECK GOOD IAW MM 32-09-12 AND 32-61-01. 2L73 4F A3WE 20060109000272006010900027WP 2006 1 9 DHL2005803548 120051207A5753 PLATE DOUG DC8 DC873 302199CWP LT WING FLAP ELONGATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 LT WING OTBD FLAP LWR PLATING RIVETS HOLES ELONGATED BETWEEN XF 210.000 AND XF 247.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 12-06-2005, DWG AA33-53-R10 REV IR DATE 11-22-05. REMOVED DAMAGED EXISTING SOLID PLATING, FABRICATED NEW PLATING (2024T3 0.050") IAW DWG AA33-53-R10, SRM 51-1-22. CLEANED, TREATED AND PRIMED AREA AND NEW PLATING INTERNAL FACE IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACE IAW SRM 51-1-11. INSTALLED NEW PLATING IAW DWG AA33-53-R10, SRM 51-1-21, SRM 51-3-0. 2L74 4F RT4A25 20060109000312006010900031WP 2006 1 9 DHL2005803555 120051212A5743 FITTING DOUG DC8 DC873 302199CWP MLG CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 MLG SUPPORT FITTING (TRAPEZOIDAL) RT HAS 2 CRACKS 0.750" AFTER STOP HOLE OF 0.562" AT STA 863.25 AND 4" CRACK AT STA 870.000. PERFORMED MAJOR REPAIR IAW DOUGLAS DWG 5750127, SRM 53-1-0 PG 1. REMOVED SUPPORT FITTING (TRAPEZOIDAL) AND 2 FITTINGS IAW SRM 53-1-0, SRM 51-1-21, SRM 51-3-0, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW SUPPORT FITTING AND 2 FITTINGS AND BUSHINGS IAW DOUGLAS DWG 5750127, SRM 51-1-21, SRM 51-3-0, SRM 51-1-20D, SRM 51-3-1 (TORQUE). REFER TO JC 8-32-20-007 FOR MLG RETRACTION. 2L74 4F RT4A25 20060109000422006010900042NM 2006 1 9 DHL2005782004 120051117A3260 INDICATION SYS BOEING727 727227 1384078NM MLG MALFUNCTIONED A DHLAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01782DH 21998 AFTER GEAR RETRACTION RED DOOR LIGHT AND LEFT/RIGHT RED DOOR LIGHTS REMAINED ILLUMINATED (AND L GEAR /R GEAR AMBER LIGHTS ILLUMINATED ON S/O PANEL) TAIL SKID AMBER LIGHT ILLUMINATED BUT WENT OUT AFTER A MINUTE COMPLETED ABNORMAL PROCEDURE, LIGHTS SAME AS ABOVE. PERFORMED GEAR SWING TEST IAW B727 M/M 32-32-0, NO DEFECTS NOTED, OPS CHECKS SERVICEABLE. 2L73 4F A3WE 20060109000442006010900044NM 2006 1 9 DHL2005780005 120051122A2420902F2425 PANEL BOEING727 727223 1384074NM NR 3 BUSS PROTECMALFUNCTIONED A DHLAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CLCLIMB 1 SO01780DH 22006 OVER EXCITATION FAULT GEN NR 3. REMOVED AND REPLACED GENENATOR CONTROL PANEL IAW B-MM 24-20-00, OPS CHECK GOOD. REMOVED AND REPLACED BUSS PROTECTION PANEL IAW 24-20-00. 2L73 4F A3WE 20060109000512006010900051NM 2006 1 9 QXEA200501858 120051231A3040NP15790113 WINDSHIELD DHAV DHC8 DHC8202 2809007NM COCKPIT MALFUNCTIONED A QXEAA UNSCHED LANDING J WARNING INDICATION TXTAXI/GRND HDL 1 NM09359PH12378 514 SEA FLIGHT NR 2251, RECEIVED A LEFT WINDSHIELD HOT CAUTION LIGHT AT ROTATION. LIGHT WENT OUT WHEN WINDSHIELD HEAT WAS SELECTED TO WARMUP. MAINTENANCE REPLACED WINDSHIELD AND RELAY 3040-K5. TESTED SYSTEM IAW DHC-8/200 AMM TASK 30-41-00-710-801. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20060109000532006010900053NM 2006 1 9 DHL2005783006 120051027A3260 SWITCH BOEING727 727227 1384078NM MLG DOOR DIRTY A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01783DH 21999 DURING CLIMB-OUT, RT DOOR WARNING LT ILLUMINATED S/O PANEL SHOWED RT GEAR DOOR COMPLIED WITH ABNORMAL PROCEDURE LIGHT OUT WITH GEAR HANDLE UP. CLEANED AND ADJUSTED RT DOOR WARNING SWITCH IAW M/M 32-62-11. OPS CKS GOOD. 2L73 4F A3WE 20060109000612006010900061EU 2006 1 9 05FDEA04426 120051230A5270 SWITCH AIRBUS300 A300B4622R 3930312EU PAX DOOR LOOSE A FDEAE ENGINE SHUTDOWN N FALSE WARNING CLCLIMB 1 SO25719FD 388 AVIONICS LIGHT/CHIME CAME ON PASSING 10000 EXECUTED TURNBACK TO KSMP. BURN TO MAX LNDG WEIGHT. FOUND AVIONICS DOOR FLUSH TO FUSELAGE AND DOOR LATCH APPROX 1/8 INCH DOWN. ON INSPECTION FOUND DOOR LOCKED SWITCH WITH BROKEN SAFETY WIRE. RETIGHTENED SWITCH. OPS NORMAL PER A300 MM REF 52-41-14-5 DOOR VERIFIED CLOSED ON DEPARTURE WITH NO LIGHT. 2L72 4F RTA35EU 20060109000622006010900062NM 2006 1 9 05FDEA04427 120051231A5320AYB71481 ANGLE DOUG MD11 MD11 3023602NM ZONE 100 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 DURING ACCOMPLISHMENT OF LEFT LOWER AUXILIARY TANK CAP ANGLE. REPAIR FOUND 1 FASTENER HOLE ELONGATED. REPAIR CARRIED OUT AT ONE (01) EACH FASTENER WITH ELONGATED HOLE AT LEFT LOWER AUXILIARY TANK CAP ANGLE AS PER FEDEX EA NR 1-5310-90694, TITLE: "FUSELAGE CAP ANGLE LEFT UNDER WING BARREL STRUCTURE AT STATION Y=1298.6, XCW 46, CRACK ANGLE, FABRICATION AND SPLICE INSTALLATION". 2L73 4F RTA22WE 20060109000882006010900088WP 2006 1 9 05FDEA04282 120051213A5312 BULKHEAD DOUG DC10 DC1010 3022110WP BS 584 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 FOUND LT AIR CONDITIONING COMPT FOUND 1 CRACK 4" LONG ON SKIN OF BULKHEAD BETWEEN STA 584 AND STA 580 Z-46 BY 24. TRIMMED OUT CRACK AND INSTALLED FILLER AND 2 REPAIRED DOUBLERS IAW SRM 53-30-00 FIG 6 SHT 2 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F164135/N01135 AND IAW SRM 53-30-00 FIG 6 SHT 2 VOL 1. 2L73 4F A22WE 20060109000902006010900090WP 2006 1 9 05FDEA04284 120051213A5200 REPAIR DOUG DC10 DC1010 3022110WP R3 DOOR UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25563FE 46948 FOUND MAIN CABIN CTR FUSELAGE R-3 DOOR AFT JAMB HAS AN EXTERNAL DOUBLER BOTTOM PART DIM 11" BY 12" STA 1311. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 53-50-00 FIG 19 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2. 2L73 4F A22WE 20060109001012006010900101EA 2006 1 9 COMA0560756 120051230A5347601R310327 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA BS 409-559 CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA29272 7031 FLOOR SEAT RAIL CORRODED FROM FS 409+128 TO 559+10. REPAIRED FLOOR SEAT TRACK FROM FS409+128 TO 559+10 BY REMOVING AND REPLACING SEAT TRACK IAW BRAS EO 601R-53-7965A. 2L72 4F RTA21EA 20060109001372006010900137NM 2006 1 9 DHL2005770008 120051113A2750 FLAP SYSTEM BOEING727 7272B7 138407LNM NR 4 KRUEGER MALFUNCTIONED A DHLAB EMER. DESCENT O OTHER DEDESCENT 1 SO01770AT 21953 DURING FLAP EXTENSION NR 4 KRUEGER FLAP FAILED TO EXTEND. COMPLETED ABNORMAL PROCEDURE AND LANDED. AFTER LANDING NR 4 KRUEGER FLAP SHOWED EXTENDED. PERFORMED OPERATIONAL AND LEAK CHECK ON KRUEGER FLAP SYSTEM, OPS CHECK GOOD. NO LEAKS DETECTED IAW B727 27-81-00. 2L73 4F A3WE 20060109001392006010900139EU 2006 1 9 DHL2005362011 120051217A3260 PROXIMITY SWITCH AIRBUS300 A300B4203 3930306EU LT MLG DIRTY A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01362DH 84 LEFT MAIN LANDING GEAR ON FOWARD PANEL INDICATED A UNSAFE CONDITION. PERFORMED ABNORMAL PROCEDURE. LEFT MAIN GEAR LIGHT ILLUMINATED WHEN ANNUN SWITCH WAS TURNED TO THE TEST POSITION AND LIGHT REMAINED ON. INSPECTED L/G PROXIMITY SWITCHES & SWTICH GAPS. CLEANED PROXIMITY SWITCHES, PERFORMED BYTE CHECK AT PROXIMITY DETECTOR MODULE. SYSTEM CHECK OK. ALL WORK DONE IAW MM 32-61-0 & 32-61-12. 2L72 4F RTA35EU 20060109001412006010900141NM 2006 1 9 DHL2005747002 120051108A2120 SMOKE BOEING727 727224 1384076NM COCKPIT DETECTED A DHLAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO01747DH 22253 COCKPIT FILLED WITH SMOKE, EVACUATED A/C. WITH ENGINE PNEUMATICS RAN BOTH A/C PACKS AND INSPECTED FOR SMOKE SOURCE, NO DEFECTS A/C OK FOR SERVICE IAW MM JRH 6.3. 2L73 4F A3WE 20060109001452006010900145EU 2006 1 9 2005UALA01502 120051223A3230 UPLOCK AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE MLG FAILED A UALAO OTHER J WARNING INDICATION CLCLIMB 1 WP29489UA 1702 GEAR NOT UPLOCKED DISPLAYED ON UPPER ECAM SCREEN. REPLACED LANDING GEAR SEL. VALVE 40GA PER MM32-31-12.OPS CKS GOOD IND. CKS GOOD.ACPD NORMAL GEAR RETRACT-EXTEND 10 TIMES.ACPD ALT. GEAR EXT. ALL CKS GOOD. 2L72 4F4 FRTA28NM E40NE 20060109001462006010900146NM 2006 1 9 MWEA050137 120051217A3260 LANDING GEAR BOEING717 717200 1383700NM NOSE WARNING LIGHT A MWEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31903ME 55167 RED NOSE WHEEL INDICATOR STAYED ON. SERVICED NOSE LANDING GEAR STRUT, ADDED 1.5 PINTS OF STRUT FLUID. RETRACTION OPERATIONS CHECKED OK. 2L72 4F TRA6WE 20060109001482006010900148WP 2006 1 9 MWEA050140 120051219A533059101413 SKIN DOUG DC9 DC981 3022081WP STA 1193 DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31807ME 48033 AFT CARGO DOOR HAS A DENT APPROXIMATELY 6 INCHES IN DIAMETER AND .5 INCH DEEP AT APPROXIMATELY STATION 1193. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20060109001522006010900152 2006 1 9 AALA20050836 420051213A2565 GIRT BAR BOEING767 767323 1385205NM L1 DOOR NOT SEATED A AALAK NONE O OTHER ININSP/MAINT 1 SW21381AN 25450 SFO - THE LEFT ONE DOOR SLIDE GIRT BAR IS NOT INSTALLED IN THE GIRT BAR RECEIVER. INSTALLED GIRT BAR IN THE GIRT BAR RECEIVER FOR LEFT ONE DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20060109001552006010900155NM 2006 1 9 MWEA050142 120051227A4920 APU BOEING717 717200 1383700NM APU BAY ODOR A MWEAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL31916ME 55178 AUXILIARY POWER UNIT FAILED TO START, OIL SMELL IN CABIN. OIL SMELL FOUND TO BE AUXILIARY POWER UNIT EXHAUST BLOWING PAST OPEN GALLEY DOOR, VERIFIED AUXILIARY POWER UNIT OIL AND NO LEAKS. OK FOR SERVICE. 2L72 4F TRA6WE 20060109001632006010900163NM 2006 1 9 CALA0500461 120051228A5315141T5113 FLOORBEAM BOEING767 767224 1385170NM BS 325 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776153 30432 INSPECTION FOUND FLOORBEAM CORRODED AT BS 325, LBL 28 TO LBL 60. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, FIGURE 201, REPAIR 1. 2L72 4F RTA1NM 20060110000062006011000006WP 2006 1 10 UPS06845918 120051229A5712 RIB DOUG DC8 DC871F 302199DWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE:C3, RIGHT O/B LEADING EDGE UPPER RIB CRACKED AT XFS 796. STOP DRILLED CRACK IAW SRM 57-03-01-0, FABRICATED REPAIR ANGLES AND INSTALLED REPAIR ANGLES AT RIGHT O/B LEADING EDGE STA XFS 796 IAW SRM 57-02-00-0, 51-1-8 AND SRM 51-1-20. 2L74 4F RT4A25 20060110000132006011000013EA 2006 1 10 COMA0560781 120051230A5347601R38312119 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA BS 409-444 CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA29272 7031 RIGHT SIDE SEAT RAIL CORRODED FROM FS 409+111.02 TO FS 444.02. REPAIRED RIGHT SIDE SEAT RAIL FROM FS 409+111.02 TO FS 444.02 BY REMOVING AND REPLACING SEAT RAIL IAW BOMBARDIER EO 601R-53-7965A. 2L72 4F RTA21EA 20060110000252006011000025CE 2006 1 10 DXTA200501158 120051223A3297 CONNECTOR CESSNA750 750 2076810CE MLG UPLOCK DIRTY E DXTAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL07946QS 7500195 GEAR UNLOCK LIGHT REMAINED ON AFTER THE GEAR HANDLE WAS SELECTED UP AFTER TAKEOFF. JACKED AIRCRAFT CYCLED GEAR 6 TIMES, OPS CHECKED GOOD. CHECKED RIG AND INSPECTED ALL UPLOCK AND DOWNLOCK SWITCHES. CHECKED GOOD. DISCONNECTED ALL UPLOCK AND DOWNLOCK SWITCHES AND CLEANED CONNECTORS. PERFORMED SEVERAL MORE GEAR SWINGS, CHECKED GOOD. DOWNJACKED AIRCRAFT. WORK DONE IAW CHP 32-10-00 OF THE CE750 MM. 2L72 4J RTT00007WI 20060110000302006011000030WP 2006 1 10 ABXA060005 120051218A53403924028501 FITTING DOUG DC9 DC933F 302207AWP BS 604 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23932AX 47465 END FITTING CRACKED LONGERON 29 RIGHT AT FS 604. REMOVED AND REPLACED END FITTING IAW DC9 SRM 51-30-5. 2L72 4F A6WE 20060110000312006011000031WP 2006 1 10 ABXA060010 120051220A5322991224644 SHEAR TIE DOUG DC9 DC933F 302207AWP BS 1038 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23932AX 47465 RIGHT AFT PYLON BULKHEAD FLANGE CRACKED AT STA 1038, LONGERON 14 RIGHT. REMOVED AND REPLACED PYLON BULKHEAD FLANGE (SHEAR TIE) IAW DC9 SRM. 2L72 4F A6WE 20060110000322006011000032WP 2006 1 10 ABXA060006 120051219A523049157411 HOUSING DOUG DC9 DC933F 302207AWP DOOR HOLD OPEN CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23932AX 47465 HOLD OPEN HOOK SUPPORT STRUCTURE INSIDE SERVICE DOOR WAS CRACKED AT LOWER SHAFT BEARING MOUNT. REPLACED FITTING IAW DC9 SRM. 2L72 4F A6WE 20060110000342006011000034WP 2006 1 10 ABXA060007 120051219A575399575774 SKIN DOUG DC9 DC933F 302207AWP TE FLAP CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23932AX 47465 RIGHT FLAP SECOND FROM OUTBOARD TRAILING EDGE SEGMENT UPPER SURFACE HAD 3 AREAS THAT WERE BULGED. REMOVED SEGMENT, REMOVED AND REPLACED SKIN IAW DC9 SRM 51-30-2. 2L72 4F A6WE 20060110000352006011000035WP 2006 1 10 ABXA060008 120051219A5330591141253 DOUBLER DOUG DC9 DC933F 302207AWP BS 332-351 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23932AX 47465 CORROSION ON ANTENNA PLATE, STA 332 - 351, LONGERON 30 - 29 LEFT. REMOVED AND REPLACED DOUBLER IAW DC9 SRM. 2L72 4F A6WE 20060110000362006011000036WP 2006 1 10 ABXA060013 120051222A57539957577502 PANEL DOUG DC9 DC933F 302207AWP TE FLAP CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23932AX 47465 RIGHT FLAP SEGMENT FROM OUTBOARD EDGE LOWER SURFACE ATTACH POINTS WERE SEPARATING AND CORRODED BETWEEN SKINS. REPLACED SKIN AND DOUBLER IAW DC9 REA C057-52966. 2L72 4F A6WE 20060110000402006011000040WP 2006 1 10 ABXA060001 120051219A533099558402 PANEL DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23973AX 47511 RIGHT TRAPEZOIDAL PANEL UPPER FORWARD OUTBOARD HORIZONTAL FLANGE HAD 6.5 INCH CRACK THROUGH 5 EA FASTENER HOLES. REPAIRED AREA IAW DC9 SRM 57-09. 2L72 4F A6WE 20060110000412006011000041WP 2006 1 10 ABXA050382 120051224A3340 SWITCH DOUG DC9 DC931 3022065WP LIGHT LOOSE A ABXAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 GL23924AX 47403 WHILE EXTENDING LANDING LIGHT FOR ARRIVAL, SPARKS FLEW FROM BEHIND PANEL. TRACED PROBLEM TO LOOSE NOSE LIGHT SWITCH, SECURED SWITCH. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 20060110000702006011000070EA 2006 1 10 SWIA200516077 120051229A5210 PLATE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE PAX DOOR HANDLE BINDING A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07705SK 10145 MAIN CABIN PASSENGER DOOR HARD TO OPEN. RESECURED PAX DOOR OUTER HANDLE FLUSH SPRING LOADED PLATE. OPERATED PAX DOOR FROM INSIDE, OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA EOOO63EN 20060110000712006011000071EA 2006 1 10 SWIA200516076 120051230A2760C13045BA04 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07702SK 10136 FOUND SPLR/STAB FAULT STATUS MESSAGE. REPLACED SSCU NR 2 IAW MM 27-61-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20060110000722006011000072SO 2006 1 10 SWIA200516075 120051230A2611 BATTERY EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE SMOKE DETECTOR DISCHARGED A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07298SW 120328 FOUND LAV SMOKE DETECTOR KEEPS BEEPING ON THE GROUND. REPLACED LAV SMOKE DETECTOR WITH A NEW BATTERY, OPERATIONAL CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20060110000732006011000073 2006 1 10 SWIA200516074 420051229A22166225734002 SERVO EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE ELEVATOR MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07560SW7434 17 120334 A/P FAILED INFLIGHT WHILE SELECTED TO EITHER SIDE. REPLACED A/P ELEVATOR SERVO, OPERATIONAL CHECK GOOD IAW MM 22-10-00. 2L72 4T4 TRTA31SO E20NE 20060110000792006011000079EA 2006 1 10 SWIA200516068 120051230A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE SPOILER MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07459SW 7782 FLIGHT SPOILERS FAULT STATUS MESSAGE DISPLAYED. REPLACED RT NR 2 PCU ON RT FLIGHT SPOILER IAW 27-62-01. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20060110000802006011000080EA 2006 1 10 SWIA200516067 120051226A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY EXIT INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07442SW 7609 FOUND MAIN CABIN DOOR, FWD BULKHEAD, EMERGENCY EXIT SIGN (INOP). REPLACED EMERGENCY LIGHT ASSY. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20060110000842006011000084EA 2006 1 10 SWIA200516063 120051231A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT ENGINE DAMAGED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07446SW 7666 DAMAGE FOUND ON LT LOWER OB ENGINE SUPPORT BEAM WEB (601-35006-147/SB) UNDER FWD IB PANEL NUT PLATE FWD OF FS640.00 AFT OF FS 625.30 AND OB OF LBL36.20, IB OF WL111.09 APPROX 3 INCH LONG, ITEM FOUND AT ROUTINE INSPECTION. C/W REPAIR OF LT LOWER OB ENGINE SUPPORT BEAM IAW REO 601R-53-61-358. 2L72 4F4 FRTA21EA E15NE 20060110001292006011000129SO 2006 1 10 C2XA05SH143 120051231A532014521713605 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2728529 145512 DURING C-CHECK MAINTENANCE FOUND LT OMEGA BEAM AND RAMP ANGLE ATTACH POINT CORRODED AT FRM 20. MAINTENANCE REMOVED AND REPLACED PREVIOUS REPAIR ON LT OMEGA BEAM AT FRM 20 IAW SRM 51-40-02, EC 5320-01137 AND EC 5320-01140. AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2L72 4F RTT00011AT 20060110001302006011000130SO 2006 1 10 C2XA05SH142 120051231A5313PE11001F8 STRINGER EMB 135 EMB135LR 3260305SO FUSELAGE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2728529 145512 DURING C-CHECK MAINTENANCE FOUND STRINGER 1L HAS CHAFE DAMAGE BETWEEN FRAMES 54 AND 55. MAINTENANCE REPAIRED STRINGER 1L BETWEEN FRAMES 54 AND 55 IAW EC 5310-010362. AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2L72 4F RTT00011AT 20060110001362006011000136SO 2006 1 10 1436120405 120051204A3250 STEERING SYS GULSTMG1159 GIV 3980115SO NLG OUT OF ADJUST E N93AK NONE O OTHER TXTAXI/GRND HDL 1 SO13436QS 1436 STEERING LAGS WHEN TURNED TO LT WITH TILLER OR RUDDER PEDALS. PERFORMED ADJUSTMENT CHECK IAW GIV MM 32-05-00. 2L72 4F RTA12EA 20060111000022006011100002NM 2006 1 11 QXEA200501860 120051228A524085311799101 DOOR BOMBDRDHC8 DHC8402 1390042NM INTERPHONE BROKEN A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09416QX 4083 YEG FLIGHT 2319: GROUND SERVICE INTERPHONE COVER DOOR ON NOSE OF AIRCRAFT WAS BROKEN WHEN THE CART WAS DRIVEN AWAY WITH THE CORD STILL PLUGGED IN. MAINTENANCE PLACED ON CDL 52-2, RSI 347487. INSPECTED GROUND INTERPHONE SERVICE DOOR AREA AND DEFECTS/DAMAGE FOUND. INSTALLED NEW COVER DOOR AS REQUIRED. OPS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20060111000032006011100003EA 2006 1 11 ASOA051014 120051124A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27884AS 7513 DURING A CHECK IN MCN, THE FS 280 INTERCOSTAL, AT RBL 9, NEAR THE FLOOR SUPPORT ANGLE, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FS 280 INTERCOSTAL, AT RBL 9, NEAR THE FLOOR SUPPORT ANGLE IAW ASA EO 600-53-0123. (M) 2L72 4F RTA21EA 20060111000042006011100004EU 2006 1 11 ASOA051012 120051123A3350 LIGHT AEROSPATR72 ATR72212 8680945EU CABIN MALFUNCTIONED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27636AS 375 DURING A GROUND INSPECTION IN ATL, THE EMERGENCY LIGHTS CAME ON THREE TIMES. MAINTENANCE PERFORMED OPERATIONAL CHECKS WITH NO DEFECTS NOTED. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20060111000052006011100005NM 2006 1 11 ASAA0540662 120051117A531165C352436 FRAME BOEING737 7374Q8 138447QNM FS 849 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - AFT CARGO BAY ODOR FRAME DOUBLER, BS 849, RBL 28, CORRODED. REPLACED FRAME ASSY PER B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060111000072006011100007EA 2006 1 11 ASOA051020 120051125A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ILLUMINATED A ASOAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27907EV 7648 DURING CRUISE FROM GRR-ATL, THE CREW RECEIVED A RIGHT ENGINE THRUST REVERSER DEPLOY LIGHT. THE QRH WAS COMPLIED WITH AND THE CREW DECLARED AN EMERGENCY. THE AIRCRAFT DIVERTED INTO FWA WHERE IT LANDED SAFELY. MAINTENANCE DEFERRED THE RIGHT THRUST REVERSER IAW MEL NR 78-30-01, CAT C, EXPIRING 12-6-05. (M) 2L72 4F RTA21EA 20060111000092006011100009EA 2006 1 11 ASOA051018 120051125A33508GH00247308 LAMP CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27709EV 10068 DURING A GROUND INSPECTION IN SLC, THE RIGHT AFT EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT AFT EXTERIOR EMERGENCY LIGHT ASSEMBLY LAMP. OPERATIONAL CHECKS TOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060111000112006011100011NM 2006 1 11 ASAA0540369 120050730A26126937307300 CONTROL PANEL BOEING737 737490 1384715NM APU FIRE DETECT UNKNOWN A ASAAO OTHER N FALSE WARNING CRCRUISE 1 NM02703AS 28893 LAX - ENGINE FIRE DETECT `FAULT LIGHT` FLICKERED ON AND OFF IN FLIGHT, DID NOT TURN ON MASTER CAUTION LIGHT. REMOVED AND REPLACED ENGINE AND APU FIRE CONTROL PANEL PER AMM 26-10-02. SYSTEM CHECKED GOOD PER AMM 26-11-00. TESTED NORMAL. (M) 2L72 4F RTA16WE 20060111000132006011100013EU 2006 1 11 ASOA051017 120051124A335011631110129A CONTROL PANEL AEROSPATR72 ATR72212 8680945EU COCKPIT MALFUNCTIONED A ASOAK NONE O OTHER TXTAXI/GRND HDL 1 SO27636AS 375 DURING TAXI TO THE GATE IN MCN, THE EMERGENCY LIGHTS CAME ON WHILE IN THE ARM POSITION. WHEN ON WAS SELECTED THE EMERGENCY LIGHTS TURNED OFF. MAINTENANCE REMOVED AND REPLACED THE ANTI-ICE/MISCELLANEOUS 24VU LIGHT CONTROL PANEL. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20060111000142006011100014EA 2006 1 11 ASOA051015 120051124A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27884AS 7513 DURING A C-CHECK IN MCN, THE RIGHT INBOARD AND OUTBOARD FS 280 CLIPS, AT RBL 9, WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT INBOARD AND OUTBOARD FS 280 CLIPS, AT RBL 9, IAW CRJ SRM 51-42-20. (M) 2L72 4F RTA21EA 20060111000152006011100015NM 2006 1 11 ASAA0570049 120050728A5321453A161032 FLOOR PANEL BOEING737 737790 13844CNNM FS 480-500 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02645AS 33011 PAE - FOUND CORROSION DISCOVERED WHILE WORKING CARD NR 494861. FOUND CORROSION ON NR 3 FLOOR PANEL IN FORWARD CARGO BAY. BLENDED, AND FOUND CORROSION OUT OF LIMITS, FABRICATED NEW NR 3 FLOOR PANEL IAW SRM 53-00-53. (M) 2L72 4F RTA16WE 20060111000162006011100016NM 2006 1 11 ASAA0570048 120050728A5320146A9403114 WEB BOEING737 737790 13844CNNM FS 794 PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02645AS 33011 PAE - FOUND AFT CARGO DOOR CUTOUT FORWARD FRAME CLOSEOUT WEB IS PUNCTURED. REMOVED AND REPLACED WEB PER SRM 51-40-02 AND 53-60-15. (M) 2L72 4F RTA16WE 20060111000182006011100018EA 2006 1 11 ASOA051011 120051123A5210 LATCH CNDAIRCL600 CL6002C10 1390015EA PAX DOOR CONTAMINATED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27738EV 10146 DURING A GROUND INSPECTION IN ATL, THE FORWARD PASSENGER DOOR WOULD NOT CLOSE. MAINTENANCE REMOVED DEBRIS FROM THE PASSENGER DOOR LATCH MECHANISM. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060117000402006011700040NM 2006 1 17 2006UALA00029 120051230A3350 LIGHT BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU EMERGENCY EXIT INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29339UA 24243 EMERGENCY EXIT FLOOR LIGHTING INOP FROM ROW 16 TO AFT END OF AIRCRAFT. 2L72 4F4 FRTA16WE E21EU 20060117000422006011700042NM 2006 1 17 PIDA06002 120051231A276165C268642 ACTUATOR BOEING737 7373G7 1384595NM NR 1 SPOILER BROKEN A PIDAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SO05380WL 23218 LOSS OF -A- SYSTEM HYDRAULIC PRESSURE; QUANTITY ZERO; ISOLATED SYSTEM, PERFORMED MANUAL GEAR EXTENSION & FLAPS 25 LANDING, NO FURTHER INCIDENT. FOUND NR 1 SPOILER ACTUATOR CASTING BROKEN. REPLACED NR 1 SPOILER ACTUATOR PER MM 27-62-94. 2L72 4F RTA16WE 20060117000442006011700044NE 2006 1 17 IXXA0500196O 220051221A7200 ENGINE DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C1 13802NE NR 1 FLAMED OUT A IXXAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 SW11820BX8720786084 46065 693398 DURING FLIGHT FROM KLRD TO KLRD LEVELING AT 17000 FT NR 1 ENGINE FLAMED OUT. ACCOMPLISHED FLAMEOUT CHECK LIST ENGINE STARTED NORMALLY. AFTER WARM UP PERIOD THROTTLE WAS ADVANCED WITH NO RESPONSE FROM ENGINE. THE ENGINE SHUTDOWN. OIL PRESSURE WENT TO 0 AT THAT TIME. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE AND NR 1 ENGINE NOSE COWL. AFTER ENGINE INSTALLATION AN IDLE CHECK AT PARTIAL POWER AND AT MAX POWER WERE PERFORMED AS WELL AS A VISUAL INSPECTION OF FORWARD AND REAR MOUNTS. WORK WAS PERFORMED PER ALL APPLICABLE MANUALS. THERE WERE NO DEFECTS AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F4 FRT4A25 E2GL 20060117000562006011700056NM 2006 1 17 AT0600001 120051229A3397 CONNECTOR BOEING717 717200 1383700NM EMERGENCY LIGHT LOOSE A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15960AT 55022 ROW 12 EMERGENCY AISLE LIGHT IS OUT. REPAIR LOOSE CONNECTOR, OPS CHECK GOOD IAW MM 33-51. 2L72 4F TRA6WE 20060117000582006011700058NM 2006 1 17 SCNA05018 120051218A2620 WARNING LIGHT BOEING737 7378Q8 13844BXNM CARGO FIRE ILLUMINATED A SCNAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL15801SY 30332 WITH SYSTEM NOT ARMED, CARGO FIRE DISCHARGE LIGHT ILLUMINATED. SYSTEM CHECKED NORMAL PER FIM TASK 26-23-00-810-802. OK FOR SERVICE. 2L72 4F RTA16WE 20060117000662006011700066WP 2006 1 17 IXXA0500205S 120050117A5711 SPAR DOUG DC8 DC871F 302199DWP WING CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11820BX860853398 46065 DURING ROUTINE C-CHECK COMPLY WITH AD 2001-06-02, INSPECT LOWER FRONT SPAR CAPS. REMOVED FASTENERS AND PHENOLIC FAIRINGS AS REQUIRED TO FACILITATE INSPECTION OF FRONT LOWER SPAR CAPS. PERFORMED HFEC ON LEFT WING NO CRACKS INDICATED. PERFORMED HFEC ON RIGHT WING, RIGHT WING HOLE NUMBER 3 GOING OUTBOARD HAS CRACK INDICATION. REAMED HOLE TO .500 AND PERFORMED HFEC, NO CRACK INDICATED. STRESS COINED HOLES IN LEFT WING, AND FABRICATED REPAIR BUSHINGS AND PARTS, INSTALLED BUSHINGS, REPAIR PARTS, PHENOLIC FAIRINGS, AND FASTENERS IAW AD2001-06-02, NDT SPM 06-10-01.003, DAC DRAWING J060232, DC8 SERVICE BULLETIN 57-090 DPS 3.67-56, DPS 2.70-2, DC8 SRM 51-1-20D, 51-3-1, 51-1-11, 51-3-0, AND 51-1-16. 2L74 4F RT4A25 20060117000742006011700074WP 2006 1 17 IXXA0500213S 120051008A532057550583 FITTING DOUG DC8 DC871F 302199DWP ZONE 100 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND LONGERON 34 LEFT AT STATION 690 TO 778 CORRODED. REMOVED CORROSION, TREATED AND PRIMED. DURING CORROSION REMOVAL FOUND FITTING CRACKED AT LONGERON 34 LEFT STATION 765 TO 778. FABRICATED NEW FITTING, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED NEW FITTING IAW DC8 SRM 53-20-0, 51-1-8, 53-2-0 AND, 51-1-20. 2L74 4F RT4A25 20060117000912006011700091WP 2006 1 17 IXXA0500238S 120051027A5313 LONGERON DOUG DC8 DC871F 302199DWP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND LONGERON CORRODED AT STATION 1702 LONGERON 28 LEFT. REMOVED DAMAGED, FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED AND INSTALLED REPAIR PARTS IAW COOPESA EO COO-8-53-426-04. 2L74 4F RT4A25 20060117000952006011700095NM 2006 1 17 SCNA05019 120051227A3350 LAMP BOEING737 7378Q8 13844BXNM EMERGENCY LIGHT INOPERATIVE A SCNAK NONE O OTHER ININSP/MAINT 1 GL15801SY 30332 EMERGENCY EXIT LIGHT ASSY ABOVE L2 DOOR HAS ONE LAMP INOP. MAINTENANCE INSTALLED NEW LAMP & OPERATIONALLY CHECKS GOOD. 2L72 4F RTA16WE 20060117001292006011700129NM 2006 1 17 DL76S060033 120051020A5330146T35523 SKIN BOEING767 767332 1382001NM BS 1218 S-36R CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27138DL 25409 THE FUSELAGE SKIN AT BS 1218, S-36R WAS FOUND CORRODED OVER AN APPROXIMATELY 4 INCH BY 8 INCH AREA. THE CORRODED SKIN WAS REMOVED AND A DOULBER INSTALLED. 2L72 4F RTA1NM 20060117001352006011700135NM 2006 1 17 HNAA0500105 120051223A6120 CONTROL UNIT DHAV DHC8 DHC8201 2809001NM NR 2 ENGINE PROPMALFUNCTIONED A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07966HA 452 NR 2 ENGINE UNSCHEDULED PROP FEATHERING IN FLIGHT. REMOVED AND REPLACED NR 2 TSCU. REMOVED AND REPLACED NR 2 EEC. 2H72 4T RTA13NM 20060117001482006011700148NM 2006 1 17 HNAA0500108 120051229A2420 GENERATOR DHAV DHC8 DHC8102 2809003NM LEAKING A HNAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA07828EX 392 RIGHT AC BUSS CAUTION LIGHT ILLUMINATED IN FLIGHT. REMOVED CONNECTOR FROM GENERATOR AND FOUND OIL IN CONNECTOR. REMOVED AND REPLACED AC GENERATOR. 2H72 4T RTA13NM 20060117001542006011700154NM 2006 1 17 SCNA05021 120051230A3520 OXYGEN MASK BOEING737 7378Q8 13844BXNM LAVATORY DEPLOYED A SCNAO OTHER O OTHER NRNOT REPORTED 1 GL15806SY 28215 CREW REPORTED RIGHT AFT LAVATORY OXYGEN MASK DROPPED. MAINTENANCE RESET OXYGEN MASK DOOR LATCH AND OPERATIONALLY CHECKS GOOD. 2L72 4F RTA16WE 20060117001942006011700194NM 2006 1 17 ASAA0510342 120051026A5330654577536 SKIN BOEING737 7372X6C 1384552NM FS 749-752 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 YXX - BS 749 TO 752 AT STRINGER 19 ON RIGHT SIDE, CRACK IN FUSSELAGE SKIN. REPAIRED PER ASA T/C 18150000. (M) 2L72 4F RTA16WE 20060117001962006011700196NM 2006 1 17 ASAA0540559 120051020A5322 SHEAR TIE BOEING737 737490 1384715NM BS 787 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02794AS 28889 PAE - AFT CARGO COMPARTMENT CORRODED SHEAR TIE AT BS 787 BETWEEN STRINGER 26 RIGHT AND 27 RIGHT. REMOVED CORRODED SECTION OF SHEAR TIE, FABRICATED AND INSTALLED IAW 737-400 SRM 53-00-07 FIGURE 201. (M) 2L72 4F RTA16WE 20060117001982006011700198NM 2006 1 17 ASAA0540532 120051012A5311654795978 FRAME BOEING737 737490 1384715NM FS 794 NICKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02793AS 28888 PAE - FOUND AFT CARGO BAY DOORWAY FORWARD FRAME IS NICKED. REPLACED FRAME AND DOUBLER PER B737-200 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060117002462006011700246WP 2006 1 17 ASAA0580453 120050808A5330593666751 SKIN DOUG DC9 DC982 3022082WP FS 1322 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02935AS 49236 OKC - DURING C-CHECK, FOUND FUSELAGE SKIN IS DENTED. COLD-WORKED DAMAGED AREA. INSTALLED REPAIR DOUBLER. (M) 2L72 4F A6WE 20060117002582006011700258WP 2006 1 17 ASAA0580445 120050808A53205936587203 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FS 617-712 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02935AS 49236 OKC - DURING C-CHECK, FOUND CABIN FLOOR PANEL SUPPORT CORRODED. REPLACED SUPPORT. (M) 2L72 4F A6WE 20060117002612006011700261NM 2006 1 17 ASAA0540545 120051014A5320654587512 ANGLE BOEING737 7374Q8 138447QNM FS 300-320 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - FOUND CORROSION ON L-ANGLE AT BS 300-320, RBL 59, WL 208. REPLACED ANGLE PER B737-200 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060117002652006011700265NM 2006 1 17 ASAA0540526 120051009A5322654653170 SHEAR TIE BOEING737 737490 1384715NM FS 500C DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02794AS 28889 OKC - FOUND SHEAR TIE AT BS 500C STRINGER 28 LEFT-28-RT IS CORRODED. REMOVED CORRODED SECTION OF SHEAR TIE, FABRICATED AND INSTALLED REPAIR PIECES IAW B737-400 SRM 53-00-02 FIG 201. (M) 2L72 4F RTA16WE 20060117002722006011700272NM 2006 1 17 DLM90050808 120051220A494027044823 STARTER DOUG MD90 MD9030 3023690NM IAE V2525 V2525D5 NE APU UNSERVICEABLE A DALAD RETURN TO BLOCK BA SMOKE/FUMES/ODORS/SPARKS FLAME/FIRE TXTAXI/GRND HDL 1 SO27904DA12068 53384 P1047 ON APU START, APU FAULT DISPLAYED AND SMOKE COMING FROM TAIL COMPT. ON FURTHER INSP, SAW VISIBLE FLAME COMING FROM APU STARTER. FLAME WENT OUT AND NO EXTINGUISHING AGENT WAS NEEDED. REPLACED STARTER, CLUTCH, AND START RELAY. 2L72 4F4 FRTA6WE A40NE 20060117002742006011700274NM 2006 1 17 USAA051646 120051229A5510 CLEVIS BOEING737 7374B7 1384702NM HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19781AU 25020 FOUND CLEVIS R1 ON HORIZ STAB CORRODED. REMOVED CORROSION, REPLACED BUSHING PER SRM 55-10-10, DEFECT SIZE: 2". 2L72 4F RTA16WE 20060117002762006011700276NE 2006 1 17 DL73S050810 220051220A7261 FILTER BOEING737 737247 138448DNM PWA JT8 JT8D15A 52051NE NR 2 ENGINE BYPASSING A DALAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SO27376DL 23603 717149 NR 2 ENG FILTER BYPASS LIGHT ILLUM IN FLT. ALL ENG PARAMETERS NORMAL. PRESS STAYED GOOD WITH ENG SHUT DOWN. REPLACED FILTER AND DIFF PRESSURE SWITCH. 2L72 4F4 F A16WE E2EA 20060117002882006011700288EU 2006 1 17 USAA051662 120051229A5310D5311141420000 BEAM AIRBUSA321 A321211 3930370EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19162UW 1412 FOUND FWD WET AREA FS 20 - Y200. REMOVED AND REPLACED BEAM PER SRM 51-72-11; CORROSION LEVEL 1; TASK JA-220-53500, DEFECT SIZE: 3' BY 4". 2L72 4F RTA28NM 20060117002902006011700290EU 2006 1 17 USAA051664 120051229A5320D5311281820401 FLOOR SUPPORT AIRBUSA321 A321211 3930370EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19162UW 1412 FOUND FLOOR SUPPORT CORRODED, Y254 AT FR 21. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 53-11-14, 51-42-11; CORROSION LEVEL 1; TASK JA-220-53500 DEFECT SIZE: 3/4" DIA. 2L72 4F RTA28NM 20060117002922006011700292EU 2006 1 17 USAA051666 120051229A5310D53480505 BEAM AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19114UW 1148 FOUND BEAM CORRODED LEFT AFT DOOR BEAM ASSY, UPPER SURFACE AREA. REMOVED AND REPLACED BEAM ASSY PER DWG 53480505 AND SRM 51-43-00; CORROSION LEVEL 1; TASK JA26053500, DEFECT SIZE: 1" BY 1". 2L72 4F RTA28NM 20060117002942006011700294EU 2006 1 17 USAA051668 120051229A5310D534804320501 BEAM AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19114UW 1148 FOUND BEAM CORRODED, -Y1732 FS 66. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-42-00; CORROSION LEVEL 1; TASK JA-260-53500, DEFECT SIZE: 12" X 24". 2L72 4F RTA28NM 20060117002962006011700296NM 2006 1 17 ASAA0540591 120051028A533065C323661 SKIN BOEING737 737490 1384715NM FS 792-824 GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02794AS 28889 OKC - MULTIPLE SKIN GOUGES BELOW AFT PIT DOOR SCUFF PLATE LOWER FORWARD AREA. SKIN REPAIR PER B737-400 SRM 53-00-01 FIG 201 REPAIR IS CATEGORY "B", HOLES HAVE BEEN ZERO TIMED. (M) 2L72 4F RTA16WE 20060117002972006011700297NE 2006 1 17 DLM88050822 220051223A7200JT8D219 ENGINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 OVERSPEED A DALAE ENGINE SHUTDOWN Y ENGINE STOPPAGE CRCRUISE 1 SO27918DE40718 49959 718225 SUSPECT RIGHT COMPRESSOR STALL. EPR PEGGED ABOVE 2, N1 ABOUT 108 PERCENT SHUTDOWN IN FLIGHT. FOLLOWED SEVERE DAMAGE CHECKLIST THERE WAS SOME SMELL OF SMOKE WHICH CLEARED WHEN THE ENGINE WAS SECURED. EDP SHOWED N1 109 PERCENT FOR 30 SEC. PERFORMED BORO NO DEFECTS FOUND. DURING T/S FOUND THROTTLE CONTROL ROD BOLT MISSING CAUSING ENGINE OVERSPEED/STALLS. REPLACED ENGINE ALSO PERFORMED DUCT BURNOUT FOR SMOKE IN CABIN. 2L72 4F4 FRTA6WE E9NE 20060117002982006011700298NE 2006 1 17 DL757050826 220051225A7200PW2037RTC ENGINE BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 1 UNKNOWN A DALAE ENGINE SHUTDOWN N FALSE WARNING CLCLIMB 1 SO27679DA55459 26955 716303 SHORTLY AFTER T/O HAD AN INDICATION OF LEFT ENGINE FIRE WARNING. RAN QRH PROCEDURE. NUMBER 1 ENGINE WAS SHUT DOWN INFLIGHT AND THE FIRE HANDLE WAS PULLED. NO BOTTLES WERE FIRED. FOUND BURN EVIDENCE AT NR 21 FUEL NOZZLE. REPLACED ALL NOZZLES AND MANIFOLDS. 2L72 4F4 FRTA2NM E17NE 20060117002992006011700299NM 2006 1 17 DL78K050827 120051225A2130 CABIN PRESSURE BOEING737 737832 13844CFNM CABIN UNKNOWN A DALAA UNSCHED LANDING O OTHER CLCLIMB 1 SO273732J 30380 ACFT FAILED TO PRESURIZE, UNABLE TO DUPLICATE. 2L72 4F RTA16WE 20060117003012006011700301NM 2006 1 17 DL777050829 120051226A3350D71702030 CHARGER BOEING777 777232 1385232NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27860DA 29951 FOUND ROWS 30 THROUGH 41 SEAT EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY. 2L72 4F RTT00001SE 20060117003032006011700303NE 2006 1 17 DL75K050831 220051227A7200PW2037RTC ENGINE BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 1 SURGES A DALAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SO27652DL51827 24392 716517 AFTER POWER PUSHED UP TO TAKEOFF NR 1 ENG STARTED SURGING FROM 1.08 TO 1.15 EPR. ALL OTHER INDICATIONS ALSO SURGING. SURGED 4 TIMES PULLED POWER BACK AND ABORTED TAKEOFF AT 40KTS. SHUT ENG DOWN. THOROUGHLY INSPECTED AND TESTED ENGINE, UNABLE TO DUPLICATE. 2L72 4F4 FRTA2NM E17NE 20060117003052006011700305 2006 1 17 DLM88050833 420051228A256582700181 COVER DOUG MD88 MD88 3023688NM SLIDE MISINSTALLED A DALAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO27915DL 49546 DURING K-1 LETTER CHECK, FOUND TAILCONE SLIDE COVER AFT MOUNTS NOT INSTALLED. WROTE NR CARD 102 TO REINSTALL COVER. 2L72 4F RTA6WE 20060117003072006011700307NM 2006 1 17 DL777050835 120051228A2760 WARNING LIGHT BOEING777 777232 1385232NM SPOILERS ILLUMINATED A DALAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO27860DA 29951 DURING TAXI OUT SPOILERS ECIAS MSG APPEARED. RAN CHECKLIST, NO HELP. FLT CONTROL STATUS MSG FAULTED NR 7 SPOILER PCA. RAN MAT TEST FAULT CLEARED. ALL FLT CONTROLS OPS NORMAL. OK FOR SERVICE. 2L72 4F RTT00001SE 20060117003092006011700309NM 2006 1 17 DLM88050837 120051229A2530 COFFEEMAKER DOUG MD88 MD88 3023688NM AFT GALLEY BURNED A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27905DL 49536 A/C ARRIVED WITH AN INBOUND STATING 'AFTER LANDING FLIGHT ATTENDANTS REPORTED ACRID SMELL IN AFT CABIN. SMELL DISSIPATED QUICKLY. ALL COCKPIT INDICATIONS APPEARED NORMAL. ANTI ICE WAS ON AND AIRFOIL WAS OFF'. AFTER C/W OPN 5088, MX FOUND COFFEE POTS HOT AND BURNT COFFEE IN BOTTOM OF POTS. A/C APU INTAKE IS CLEAN. AFT CARGO IS CLEAN. 48 SECTION CLEAN AND NO SMOKE DETECTED. 2L72 4F RTA6WE 20060117003102006011700310CE 2006 1 17 4511412212005 120051221A32134532201000V1200 STRUT LEAR 45 45LEAR 5170805CE NOSE GEAR DISCHARGED E J7SAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW05417FX4410 114 ON TAKEOFF, GEAR SELECTED UP NWS FAIL CAS 3 GREEN EXTINGUISHED AND 3 DOOR WHITE UNSAFE LTS REMAINED ILLUMINATED. TOWER FLYBY INDICATED THE NOSE GEAR WAS NOT CENTERED. TOUCHDOWN WAS UNEVENTFUL AND NOSE GEAR SELF-CENTERED ON LANDING. SUSPECT NOSE GEAR IS FLAT (NO PRECHARGE PRESSURE). MAINTENANCE OBSERVED THE UPPER BEARING AT THE END OF THE PISTON HAS BEEN RUBBING ON THE INSIDE OF THE CYLINDER. DAMAGE IS VISIBLE WITH A MIRROR. 2L72 4F RTT00008WI 20060117003112006011700311NM 2006 1 17 DL78K050840 120051231A5270 WARNING LIGHT BOEING737 737832 13844CFNM L1 DOOR FALSE INDICATIONA DALAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO273730B 30538 REJECTED TAKEOFF AT 100 KIAS FOR L1 DOOR INDICATED OPEN ON TAKEOFF. CLEANED DOOR PROX SENSOR. 2L72 4F RTA16WE 20060117003122006011700312NM 2006 1 17 DL777050841 120051231A3397CQCME21W4S CONNECTOR BOEING777 777232 1385232NM 1L DOOR BURNED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27861DA 29952 FOUND CONNECTOR ABOVE L1 DOOR BURNT AND MELTED. REPAIRED SAME. 2L72 4F RTT00001SE 20060118001532006011800153CE 2006 1 18 DXTA200501161 120051225A3260 SQUAT SWITCH CESSNA500 560CESSNA 2076750CE MLG OUT OF ADJUST E DXTAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL07339QS 5600339 AFTER T/O GEAR HANDLE WOULD NOT UNLOCK TO RETRACT GEAR, TOOK 3 ATTEMPTS BEFORE GEAR WOULD COME UP. FOUND LT SQUAT SWITCH INDICATING GROUND, ADJUSTED SWITCH, PERFORMED SEVERAL RIGGING CHECKS, THEN SWUNG GEAR, NO DEFECTS NOTED. JACKED AIRCRAFT AND RIGGED SQUAT SWITCH. TESTED SWITCH WITH GEAR HANDLE INDICATIONS. SWUNG GEAR TO INSURE 3 GREEN. DOWNJACKED AND RAN AIRCRAFT. DISCONNECTED LT SQUAT SWITCH AND COULDN'T GET AIRCRAFT INTO AIR MODE. REJACKED AIRCRAFT ADJUSTED SQUAT SWITCH, PERFORMED SEVERAL OPS CHECKS IN AIR, NO DEFECTS NOTED. SWUNG GEAR, OPS CHECK GOOD. DOWNJACKED AIRCRAFT, PERFORMED, PRESSURIZATION CHECKS, NO DEFECTS NOTED. 2L72 4F RTA22CE 20060119000022006011900002WP 2006 1 19 ABXA060026 120051020A5315 FLOORBEAM DOUG DC8 DC863F 302198FWP BS 120 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 MAIN CABIN, BS 120, RIGHT BUTT LINE 50, FLOORBEAM HAD EXCESSIVE MATERIAL LOSS. REMOVED DAMAGED AREA AND REPLACED WITH ANGLE DOUBLER AND FILLER ON FLOORBEAM BS 120, RIGHT BUTT LINE 50 IAW DC8 SRM 51-1-8, 53-2-0, 51-3-0, 53-7-3, 53-0, 51-2-0, 51-1-8, 51-3-1, 51-1-21 AND ABX SSRM 93-01-14. 2L74 4F 4A25 20060119000162006011900016NM 2006 1 19 AWXA200600056 120051220A5320654583340 WEB BOEING737 7373G7 1384595NM BS 180 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 MCN - DURING C15 CHECK DISCOVERED FLOOR WEB CRACKED, .75 INCHES, AT BS 180, WL 207 AND BL 30R. MAINTENANCE REMOVED CRACKED FLOOR WEB, FABRICATED REPLACEMENT FLOOR WEB AND INSTALLED AT BS 180, WL 207 AND BL 30R IAW BOEING 737-300 SRM 53-10-51, BAC DWG 65-45833 AND BOEING 737-300 SRM 51-40-05-0G. 2L72 4F RTA16WE 20060119000222006011900022NM 2006 1 19 AWXA200600062 120051221A531265163007 BULKHEAD BOEING737 7373G7 1384595NM BS 178 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 MCN - DURING C15 CHECK DISCOVERED 178 BULKHEAD WEB CRACED, 1 INCH, AT WL 212 AND BL 7L. MAINTENANCE REMOVED DAMAGED AREA AND MADE INSURANCE CUT OUT IAW BOEING 737-300 SRM 53-10-08-2R10. FABRICATED DOUBLER AND FILLERS IAW BOEING 737-30 SRM 53-10-08-2R10. INSTALLED FABRICATED REPAIR PARTS AT BS 178, WL 212 AND BL 7L IAW BOEING 737-300 SRM 53-10-08-2R10. 2L72 4F RTA16WE 20060119000232006011900023NM 2006 1 19 AWXA200600063 120051218A534069353524 STRINGER CLIP BOEING737 7373G7 1384595NM BS 947 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 MCN - DURING C15 CHECK DISCOVERED STRINGER CLIP 26R CRACKED AT BS 947. MAINTENANCE REMOVED AND INSTALLED NEW STRINGER CLIP AT STR 26R AND BS 947 IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 8 AND 12. 2L72 4F RTA16WE 20060119000342006011900034NM 2006 1 19 AWXA200600075 120051215A33973402202 PIN BOEING737 7373G7 1384595NM EMERGENCY LIGHT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 MCN - EEL - DURING C15 CHECK DISCOVERED, THE EMERGENCY SEAT PATH FROM BS 328 TO BS 947, HAD DAMAGE TO CONNECTORS. MAINTENANCE REPAIRED THE EMERGENCY LIGHT SEAT PATH ESCAPE HARNESS IAW BOEING SWPM 20-30-12 PAGES 1-2. OPERATIONAL CHECKS WERE GOOD IAW AMERICA WEST AIRLINES TASK CARD A1C33006. 2L72 4F RTA16WE 20060119000432006011900043NM 2006 1 19 AWXA200600084 120051230A5340693535216 STRINGER CLIP BOEING737 7373Y0 1384671NM BS 1006 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - DURING C16 CHECK DISCOVERED STRINGER TIE CRACKED, .75 INCHES, AT STR 5L. AND BS 1006. MAINTENANCE REMOVED AND INSTALLED NEW STRINGER TIE AT STR 5L AND BS 1006 IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 8 AND 12. 2L72 4F RTA16WE 20060119000552006011900055NM 2006 1 19 AWXA200600094 120051209A5311655287477 FRAME BOEING737 7373Y0 1384671NM BS 957 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - DURING C16 CHECK DISCOVERED THE L2 DOOR FRAME CRACKED, .125 INCHES, AT BS 957 JUST BELOW STR 8L. MAINTENANCE REMOVED CRACKED L2 DOOR FRAME FROM BS 957, STRINGER 8L AND INSTALLED A NEW FRAME AT THE L2 DOOR, BS 957 JUST BELOW STR 8L IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 3, 6, 8 AND 12. 2L72 4F RTA16WE 20060119000662006011900066NM 2006 1 19 AWXA200600105 120051220A5320654583311 WEB BOEING737 7373G7 1384595NM BS 194 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 MCN - DURING C15 CHECK DISCOVERED FLOOR WEB CRACKED, 1.1 INCHES, AT BS 194, WL 207 AND BL 30L. MAINTENANCE REMOVED CRACKED WEB AND FABRICATED REPLACEMENT WEB IAW BOEING 737-300 SRM 53-10-51-2R8 FIG 201. INSTALLED FABRICATED REPAIR PARTS AT BS 194, WL 207 AND BL 30L IAW BOEING 737-300 SRM 53-10-51-2R8 FIG 201. 2L72 4F RTA16WE 20060119001132006011900113NM 2006 1 19 AWXA200600121 120051224A53156546568122 FLOORBEAM BOEING737 73733A 1384673NM BS 1016 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - DURING C19 CHECK DISCOVERED CORROSION ON BS 1016 FLOORBEAM FROM BL 17R TO BL 17L, WL 208. MAINTENANCE REMOVED DAMAGED AREA AND FOUND CORROSION TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-15-1A1 FIG 101. FABRICATED REPAIR STRAPS IAW BOEING 737-300 SRM 53-00-51-2R3. INSTALLED FABRICATED REPAIR PARTS ON BS 1016 FLOORBEAM AT BL 17R TO BL 17L AND WL 208 IAW BOEING 737-300 SRM 53-00-51-2R3. 2L72 4F RTA16WE 20060117000172006011700017NM 2006 1 17 DHL2005745012 120051122A3260 SWITCH BOEING727 727224 1384076NM MLG DOOR OUT OF ADJUST A DHLAO OTHER N FALSE WARNING CRCRUISE 1 SO01745DH 20665 RED DOORS LIGHT ON FORWARD PANEL FLICKERS IN FLIGHT AND CORRESPONDING L GEAR DOOR LIGHT ON FLIGHT ENGINEERS PANEL FLICKERS. NO VIBRATION FELT. ADJUSTED LEFT MAIN GEAR DOOR SWITCH IAW B727 M/M 32-62-0, OPS CHECK GOOD. 2L73 4F A3WE 20060117000192006011700019NM 2006 1 17 2006UALA00010 120050103A3350 LIGHT BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU CABIN INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29310UA 23671 EEL FLOOR LIGHTING IN FIRST CLASS IS INOP. 2L72 4F4 FRTA16WE E21EU 20060117000242006011700024NM 2006 1 17 2006UALA00015 120051230A5241 FRAME BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU GALLEY DOOR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29923UA 26643 FWD GALLEY DOOR LOWER FWD FRAME CORNERS CRACKED AT FASTENER HOLES. REPAIR ACP'D PER SRM 51-40-02 AND BACO DRAWING 69-69430, NEW FRAME SPLICE REPAIR SECTION INST'D. 2L72 4F4 FRTA16WE E21EU 20060117000372006011700037NM 2006 1 17 2006UALA00026 120051228A3210 LANDING GEAR AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE UNKNOWN A UALAO OTHER J WARNING INDICATION LDLANDING 1 WP29846UA 1600 LANDING GEAR WAS LOWERED BY FREEFALL METHOD. GEAR SWING ECAM GEAR NOT UP-LOCKED AND GEAR DOOR NOT CLOSED ECAM MSG'S DISPLAYED AFTER GEAR RETRACTION. CREW CYCLED GEAR HANDLE THEN GEAR NOT DOWN AND LOCKED ECAM DISPLAYED WITH ALL GEARS UP AND LOCKED AND GEAR DOORS CLOSED. CYCLED GEAR HANDLE AGAIN ECAMS CLEARED. NECESSARY TO GRAVITY EXTEND GEAR UPON ARRIVAL AT NEXT STATION. REPLACED GEAR DOOR OPEN PROX SENSOR 32GA REF MM 32-31-73, CHECKED NLG TARGET SENSORS REF MM 32-31-73, OP CHECKED GEAR PER MM 32-31-00, OP CHECKED OK ON NR A4219L BY MECH 306692 INSP BY LC46 2L72 4F4 FRTA28NM E40NE 20060117001032006011700103NM 2006 1 17 CALA0600006 120051205A278190004212 SENSOR BOEING737 737724 13844BYNM LE FLAP INOPERATIVE A CALAO OTHER J WARNING INDICATION APAPPROACH 1 SW275471124519 28782 THE TRAILING EDGE FLAPS WENT ASYMMETRICAL WITH SPLIT BETWEEN POS 1 AND 2 WHILE EXTENDING FLAPS FOR LANDING ON APPROACH TO CLE. THE LEADING EDGE FLAPS/SLATS EXTENDED FULLY. AN EMERGENCY WAS DECLARED AND A GO-AROUND WAS PERFORMED. THE AIRCRAFT LANDED SAFELY PER QRH SPEEDS FOR FLAPS AT 1. MAINTENANCE FOUND THE NR 6 I/B FLAP O/B SKEW SENSOR INOPERATIVE. THE SENSOR WAS REMOVED AND REPLACED IAW MM 27-59-01. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20060117001992006011700199NM 2006 1 17 ASAA0540534 120051012A531165465292 FRAME BOEING737 737490 1384715NM FS 940 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02793AS 28888 PAE - FOUND FRAME CRACKED AT BIN RAIL SUPPORT. REPAIRED FRAME CRACK PER B737-200 SRM 53-00-07. (M) 2L72 4F RTA16WE 20060117002012006011700201NM 2006 1 17 ASAA0540517 120051001A532069165004 INTERCOSTAL BOEING737 737490 1384715NM FS 767-787 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02793AS 28888 PAE - WHILE WORKING CARD NUMBER 4953433, FOUND INTERCOSTAL WEB DENTED. REMOVED AND REPLACED INTERCOSTAL WEB IN AFT CARGO BAY PER B737-200 SRM 53-00-04. (M) 2L72 4F RTA16WE 20060117002032006011700203NM 2006 1 17 ASAA0540519 120051001A5347 SEAT TRACK BOEING737 737490 1384715NM BS 536 GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02793AS 28888 PAE - FOUND SEAT TRACK SUPPORT ANGLE GOUGED ON OUTBOARD SIDE. REMOVED AND REPLACED SEAT TRACK SUPPORT ANGLE AT BS 536, RBL 45 WL 206, PER B737-200 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060117002052006011700205NM 2006 1 17 ASAA0540547 120051015A5320651768538 WEB BOEING737 737490 1384715NM FS 344-348 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02794AS 28889 OKC - FOUND WEB AROUND L1 DOOR CUTOUT CORRODED AT BS 344, WL 208.5. REMOVED WEB, FABRICATED AND INSTALLED REPLACEMENT WEB IAW 737-400 SRM 51-30-01 FIGURE 7 AND DWG 6517685. (M) 2L72 4F RTA16WE 20060117002072006011700207NM 2006 1 17 ASAA0540525 120051007A52306547952358 SKIN BOEING737 737490 1384715NM FS 795-846 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02793AS 28888 PAE - FOUND AFT CARGO DOOR OUTER SKIN HAS 4 SMALL DENTS AND CREASE AT BOTTOM AFT CORNER. REMOVED AND REPLACED AFT CARGO DOOR SKIN IAW B737-400 SRM 53-30-01. (M) 2L72 4F RTA16WE 20060117002102006011700210NM 2006 1 17 ASAA0540544 120051013A57536546435340 SKIN BOEING737 737490 1384715NM TE FLAP DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02794AS 28889 OKC - FOUND RIGHT OUTBOARD AFT FLAP IS DAMAGED. REMOVED DAMAGE, FABRICATED AND INSTALLED CORE AND DOUBLER PER B737-200 SRM 51-70-10. (M) 2L72 4F RTA16WE 20060117002122006011700212NM 2006 1 17 ASAA0540560 120051020A53106517688U175 CREASE BEAM BOEING737 737490 1384715NM FS 312-343 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02794AS 28889 PAE - FOUND FORWARD CABIN CREASE BEAM CORRODED AT INNER CHORD, SEVERAL AREAS AT L1 DOOR. REMOVED AND REPLACED CREASE BEAM INNER CHORD IAW B737-400 SRM 51-40-02 PAGE 2. (M) 2L72 4F RTA16WE 20060117002142006011700214NM 2006 1 17 ASAA0540592 120051028A575465C26601 SKIN BOEING737 737490 1384715NM NR 1 SLAT CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02794AS 28889 OKC - NR 1 SLAT T/E LOWER SURFACE IS CHAFED AND CRACKED AT O/B CORNER. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW B737-400 SRM 51-70-10. (M) 2L72 4F RTA16WE 20060117003302006011700330NM 2006 1 17 AT0500050 120051212A33508039251 POWER SUPPLY BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE ROW 23 INOPERATIVE A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15934AT 55070 ROW 23 EPL INOPERATIVE, REMOVED AND REPLACED EPL ASSY AND POWER SUPPLY IAW 33-00 REPAIRED SEAT ROW 23 FLOOR CONNECTOR IAW SWP. 2L72 4F4 FTRA6WE E00061EN 20060118001512006011800151NM 2006 1 18 2005UALA01246 120051106A335020131A BATTERY BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29659UA 27114 EEL OVERHEAD LIGHTS AT SEATS 8B, 6B, 5B, 1B AND FWD OF 1B PLUS FWD LAV EEL LIGHT BAR INOP. *S/D* RESEATED BATTERY ON THE POWER SUPPLY. 2L72 4F4 FRTA1NM E24NE 20060118002132006011800213WP 2006 1 18 GTIA050289 120051216A335060030451 POWERPACK DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE TAIL CMPT OVERHDINOPERATIVE A GTIAK NONE O OTHER UKUNKNOWN 1 GL23830NK 49932 OVERHEAD EMERGENCY LIGHTS IN TAIL COMPARTMENT INOPERATIVE. REMOVED AND REPLACED POWER PACK FOR EMERGENCY LIGHTS IN TAIL COMPARTMENT OVERHEAD. (K) 2L72 4F4 F A6WE E9NE 20060119000132006011900013NM 2006 1 19 AWXA200600052 120051219A531165163019 FRAME BOEING737 7373G7 1384595NM BS 188 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 MCN - DURING C15 CHECK DISCOVERED BS 188 FRAME CHORD WEB CRACKED, .7 INCHES, AT BL 31L AND WL 207. MAINTENANCE CUT OUT DAMAGED PORTION IAW BOEING 737-300 SRM 53-00-07-2R11. FABRICATED FILLERS, TAPERED FILLERS AND REPAIR ANGLES IAW BOEING 737-300 SRM 53-00-07-2R11. INSTALLED FABRICATED REPAIR PARTS AT BS 188, BL 31L AND WL 207 IAW BOEING 737-300 SRM 53-00-07-2R11. 2L72 4F RTA16WE 20060119000262006011900026NM 2006 1 19 AWXA200600066 120051217A532065C320747 INTERCOSTAL BOEING737 7373G7 1384595NM BS 990-996 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 MCN - DURING C15 CHECK DISCOVERED LEVEL 2 GALVANIC CORROSION ON INTERCOSTAL FROM BS 990 TO BS 996, BL 33R AND WL 208. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-51-1A1 FIG 101. MAINTENANCE REMOVED AND INSTALLED NEW INTERCOSTAL FROM BS 990 TO BS 996, BL 33R AND WL 208 IAW BOEING 737-300 SRM 51-40-02-0G FIG 12. 2L72 4F RTA16WE 20060119000332006011900033NM 2006 1 19 AWXA200600074 120051216A5330654577472 SKIN BOEING737 7373G7 1384595NM BS 727E CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 MCN - DURING C15 CHECK DISCOVERED FUSELAGE SKIN CRACKED AT BS 727E+3 AND STR 24L. MAINTENANCE CUTOUT DAMAGED SKIN IAW BOEING 737-300 SRM 53-00-01-2R31. FABRICATED DOUBLER, TRIPLER AND FILLERS IAW BOEING 737-300 SRM 53-00-01-2R31. INSTALLED FABRICATED REPAIR PARTS AT BS 727E+3 AND STR24L IAW BOEING 737-300 SRM 53-00-01-2R31. 2L72 4F RTA16WE 20060119000452006011900045NM 2006 1 19 AWXA200600086 120051206A53226940708501 SHEAR TIE BOEING737 7373Y0 1384671NM BS 727A-727B CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - DURING C16 CHECK DISCOVERED CORROSION ON INTERCOSTAL SHEAR TIE BETWEEN STATIONS 727A AND 727B AT BL 17L IN THE AFT PIT. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-00-04-1A1. REMOVED AND INSTALLED NEW FABRICATED SHEAR TIE BETWEEN STATIONS 727A AND 727B AT BL 17L IN THE AFT PIT IAW BOEING 737-300 SRM 51-40-02-0G FIG 12, 51-30-01-0G, AND BAC DWG 69-40708. 2L72 4F RTA16WE 20060119000462006011900046NM 2006 1 19 AWXA200600087 120051221A5320654583459 ANGLE BOEING737 7373Y0 1384671NM BS 294 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - DURING C16 CHECK DISCOVERED REINFORCEMENT ANGLE CRACKED AT BS 294.5, WL 208 AND FROM BL 40R TO BL 55R. MAINTENANCE REMOVED AND INSTALLED FABRICATED REINFORCEMENT ANGLE IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 12, 13, 14 AND BOEING DWG 65-45808. 2L72 4F RTA16WE 20060119000472006011900047NM 2006 1 19 AWXA200600055 120051219A5311651630110 FRAME BOEING737 7373G7 1384595NM BS 188 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 MCN - DURING C15 CHECK DISCOVERED BS 188 FRAME CHORD WEB CRACKED, .65 INCHES, AT BL 31R AND WL 207. MAINTENANCE CUT OUT DAMAGED PORTION IAW BOEING 737-300 SRM 53-00-07-2R11. FABRICATED FILLERS, TAPERED FILLERS AND REPAIR ANGLES IAW BOEING 737-300 SRM 53-00-07-2R11. INSTALLED FABRICATED REPAIR PARTS AT BS 188, BL 31R AND WL 207 IAW BOEING 737-300 SRM 53-00-07-2R11. 2L72 4F RTA16WE 20060119000502006011900050NM 2006 1 19 AWXA200600089 120051207A5343658276428 SUPPORT BOEING737 7373Y0 1384671NM RT MLG CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - DURING C16 CHECK DISCOVERED CORROSION AROUND 4 FASTENER HOLES ON LOWER SURFACE OF THE RT MLG AFT SUPPORT BEAM. MAINTENANCE REMOVED CORROSION ON LOWER SURFACE OF THE RT MLG AFT SUPPORT BEAM IAW BOEING 737-300 SRM 51-10-02-0G. MATERIAL LOSS WAS BEYOND DESIGN LIMITS IAW BOEING 37-300 SRM 57-51-14-1A1 FIG 101 NOTE A. BEAM WAS REMOVED AND REPLACED ON NR 5844331. 2L72 4F RTA16WE 20060119001122006011900112NM 2006 1 19 AWXA200600120 120051224A532065C1988318 FLOOR SUPPORT BOEING737 73733A 1384673NM BS 994-1004 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - DURING C19 CHECK DISCOVERED CORROSION ON BOTTOM SURFACE OF FLOOR ANGLE AT BS 994 TO BS 1004, BL 42R AND WL 208. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-51-1A1 FIG 101. MAINTENANCE REMOVED AND FABRICATED ANGLE IAW BOEING 737-300 SRM 51-40-02-0G AND BAC DWG BAC1510-335. INSTALLED FABRICATED REPLACEMENT PARTS FROM BS 994 TO BS 1004, BL 42R AND WL 208 IAW BOEING 737-300 SRM 51-40-04-0G FIG. 1 2L72 4F RTA16WE 20060119001292006011900129NM 2006 1 19 AWXA200600109 120051222A5320654583311 WEB BOEING737 73733A 1384673NM BS 197 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - DURING C19 CHECK DISCOVERED WEB CRACKED, .5 INCHES, AT BS 197, WL 207 AND BL 30L. MAINTENANCE REMOVED FLOOR WEB AT BS 197, WL 207 AND BL 30L IAW BOEING 737-300 SRM 53-10-51-2R8 FIG 201. FABRICATED NEW WEB AND INSTALLED AT BS 197, WL 207 AND BL 30L IAW BOEING 737-300 SRM 53-10-51-2R8 FIG 201. 2L72 4F RTA16WE 20060119001312006011900131NM 2006 1 19 AWXA200600111 120051226A5312651758267 BULKHEAD BOEING737 73733A 1384673NM BS 178 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - DURING C19 CHECK DISCOVERED VERTICAL WEB CRACKED, .25 INCHES, AT BS 178, WL 176 AND FROM BL 5L TO BL 7L. MAINTENANCE CUT OUT CRACKED SECTION OF WEB IAW BOEING 737-300 SRM 53-10-08-2R12 FIG 201. FABRICATED REPLACEMENT WEB IAW BOEING 737-300 SRM 53-10-08-2R12 FIG 201. INSTALLED FABRICATED REPLACEMENT PART AT BS 178, WL 183 AND FROM BL 5L TO BL 7L IAW BOEING 737-300 SRM 53-10-08-2R12 FIG 201. 2L72 4F RTA16WE 20060119001482006011900148NM 2006 1 19 AWXA200600113 120051229A5311654655216 FRAME BOEING737 73733A 1384673NM BS 827 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - DURING C19 CHECK DISCOVERED CORROSION ON FRAME ATTACH FLANGE AT BS 827, WL 148, AND FROM BL 3L TO BL 6L. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-00-07-1A1 FIG 101. MAINTENANCE CUT OUT DAMAGED AREA OF FRAME ATTACH FLANGE IAW BOEING 737-300 SRM 53-00-07-2R10 FIG 201. FABRICATED REPAIR FILLER AND RADIUS IAW BOEING 737-300 SRM 53-00-07-2R10. INSTALLED FABRICATED REPAIR PARTS AT BS 827, WL 148 AND FROM BL 3L TO BL 6L IAW BOEING 737-300 SRM 53-00-07-2R10 FIG 201. 2L72 4F RTA16WE 20060119001502006011900150NM 2006 1 19 AWXA200600115 120051222A5311651630110 FRAME BOEING737 73733A 1384673NM BS 188 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - DURING C19 CHECK DISCOVERED BS 188 FRAME CRACKED IN RADIUS AT WL 207 AND BL 30R. MAINTENANCE REMOVED DAMAGED AREA ON BS 188 FRAME IAW BOEING 737-300 SRM 53-00-07-2R11 FIG 201. FABRICATED REPAIR ANGLE AND FILLERS IAW BOEING 737-300 SRM 53-00-07-2R11. INSTALLED FABRICATED REPAIR PARTS ON BS 188 FRAME AT WL 207 AND BL 30R IAW BOEING 737-300 SRM 53-00-07-2R11. 2L72 4F RTA16WE 20060119001512006011900151NM 2006 1 19 AWXA200600116 120051222A534069439341 CLIP BOEING737 73733A 1384673NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - DURING C19 CHECK DISCOVERED CLIP CRACKED, .25 INCHES, AT BS 787 AND BL 19R. MAINTENANCE REMOVED CRACKED CLIP AND FORMED REPLACEMENT CLIP IAW BOEING 737-300 SRM 51-40-02-0G AND B737 DWG 69-43934. INSTALLED REPAIR PARTS AT BS 787 AND BL 19R IAW BOEING 737-300 SRM 51-40-02-0G. 2L72 4F RTA16WE 20060119001532006011900153NM 2006 1 19 AWXA200600118 120051223A53406546812174 ATTACH ANGLE BOEING737 73733A 1384673NM BS 1028 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - DURING C19 CHECK DISCOVERED CORROSION ON SHEAR WEB ATTACH ANGLE AT BS 1028, WL 207 AND BL 17R. NO ALLOWABLE LIMITS IAW BOEING 737-300 SRM 53-60-51-1A FIG 101. MAINTENANCE REMOVED AND FABRICATED ATTACH ANGLE IAW BOEING 737-300 SRM 51-40-05-0G AND BOEING DWG 65-46812. INSTALLED FABRICATED REPLACEMENT PARTS IAW BOEING 737-300 SRM 51-40-02-06-7D FIG 8 AND 12. 2L72 4F RTA16WE 20060120000052006012000005NM 2006 1 20 CALA0600013 120051216A5420311T145028 STIFFENER BOEING767 767224 1385170NM STA 285.45 - 295CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776151 30430 INSPECTION FOUND A 4.5 INCH CRACK IN NR 1 PYLON I/B FRAME CHORD ATTACH SUPPORT -T- (STIFFENER) AT NAC STA 285.45 TO NAC STA 295. THE SUPPORT STIFFENER WAS REPLACED IAW ECRA 5420-01444. 2L72 4F RTA1NM 20060120000252006012000025NM 2006 1 20 CALA0600009 120051216A5420UNK STIFFENER BOEING767 767224 1385170NM BS 285.45-295 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776151 30430 INSPECTION FOUND A 2 INCH CRACK IN NR 2 PYLON I/B FRAME CHORD ATTACH SUPPORT -T- (SUPPORT STIFFENER) DURING FRAME CHORD REMOVAL AT NAC STA 285.45 TO NAC STA 295. THE SUPPORT STIFFENER WAS REPLACED IAW ECRA 5420-01444. 2L72 4F RTA1NM 20060120000262006012000026NM 2006 1 20 CALA0600010 120051216A5411311T235039 FRAME BOEING767 767224 1385170NM NR 2 PYLON CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776151 30430 INSPECTION FOUND A 2 INCH CRACK IN NR 2 PYLON NACELLE STRUT FRAME CHORD AT NAC STA 285.45, I/B AREA. THE FRAME CHORD WAS REPLACED IAW ECRA 5420-01444. 2L72 4F RTA1NM 20060120000272006012000027NM 2006 1 20 CALA0600011 120051216A5410311T21634 CLIP BOEING767 767224 1385170NM NR 1 PYLON CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776151 30430 INSPECTION FOUND A 1.5 INCH CRACK IN NR 1 PYLON LT NACELLE STRUT FRAME CLIP AT NAC STA 285.45. THE FRAME CLIP WAS REPLACED IAW ECRA 5420-01444. 2L72 4F RTA1NM 20060120000282006012000028NM 2006 1 20 CALA0600012 120051216A5410311T235038 FRAME BOEING767 767224 1385170NM NR 1 PYLON CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776151 30430 INSPECTION FOUND A .5 INCH CRACK IN NR 1 PYLON O/B FRAME CHORD DURING ATTACH CLIP REMOVAL AT UPPER CLIP ADJACENT AREA, NAC STA 285.45. THE FRAME CHORD WAS REPLACED IAW ECRA 5420-01444. 2L72 4F RTA1NM 20060120000292006012000029NM 2006 1 20 CALA0600014 120051216A5420311T148027 STIFFENER BOEING767 767224 1385170NM NR 1 PYLON CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776151 30430 INSPECTION FOUND A 1.5 INCH CRACK IN NR 1 PYLON O/B FRAME CHORD ATTACH SUPPORT -T- (STIFFENER) DURING FRAME CHORD REMOVAL AT NAC STA 285.45 TO NAC STA 295. THE STIFFENER WAS REPLACED IAW ECRA 5420-01444. 2L72 4F RTA1NM 20060120000362006012000036CE 2006 1 20 DXTA200501156 120051222A5100 NONE CESSNA500 560CESSNA 2076750CE NONE NONE E DXTAA UNSCHED LANDING O OTHER CRCRUISE 1 GL07324QS 5600423 CLEAR AIR TURBULENCE, NO WARNING, 16000 FT LEVEL FLIGHT, ABOUT 260 KTS, AUTOPILOT DISENGAGED, ATTITUDE REMAINED LEVEL, ALTITUDE +/- ABOUT 100, FORCED VIOLENTLY AGAINST SEAT BELTS, CREW HIT CEILING, TOILET SEAT FLIPPED INTO AISLE, EVENT LASTED LESS THAN 5 SECONDS. DISASSEMBLED AIRCRAFT AND INSPECTED PER CE560 M/M CH 5-50-00 PARA 5, FOUND TO BE SATISFACTORY AT THIS TIME, RE-ASSEMBLED WING & TAIL PANELS. DISASSEMBLED AIRCRAFT AND INSPECTED PER CE560 M/M FOUND TO BE SATISFACTORY, REASSEMBLED TAIL & WING PANELS. 2L72 4F RTA22CE 20060120000372006012000037CE 2006 1 20 DXTA200501157 120051226A2741 WHEEL CESSNA560 560XL 2076702CE TRIM SYSTEM OUT OF POSITION E DXTAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 GL07679QS 5605279 AFTER LIFT OFF EXCESSIVE AMOUNT OF FWD CONTROL PRESSURE REQUIRED FOR NORMAL CLIMB. AIRCRAFT ALMOST WANTED TO ROTATE BY ITSELF. THROUGHOUT FLIGHT, TRIM INDICATOR AT OR ABOVE FWD END OF WHOLE RANGE MARKINGS. UPON INSPECTION OF TRIM WHEEL FOUND TRIM POINTER IN THE WRONG GROVE. LOOSENED TRIM WHEEL REPOSITIONED TRIM WHEEL POINTER IAW 560MM 27-32-01. PERFORMED ELEVATOR TRIM TAB TRAVEL CHECK. CHECK GOOD. CHECKED T/O RANGE TRAVELS, CHECK GOOD. PERFORMED ELECTRIC TRIM TIME CHECK.CHECK GOOD. ADJUSTED TAKEOFF BAND PROX SWITCH, OP'S CHECK GOOD. CLOSED ACCESS PANEL, WORKED IAW 560XL MM CH 27-32-01. 2L72 4F RTA22CE 20060120000382006012000038CE 2006 1 20 DXTA200501153 120051221A2120 ODOR CESSNA750 750 2076810CE COCKPIT DETECTED E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL07956QS 7500156 SMELLED BURNING RUBBER IN THE COCKPIT AT 14,000 FEET. SMELL DIMINISHED WITH POWER REDUCTION. APU WAS RUNNING. NO SMELL ON GROUND WITH APU RUNNING AND ENGINE OFF. INSPECTED ACU OILS & FANS, NO DEFECTS. RAN A/C AT POWER, NO BURNING SMELL NOTED AT THIS TIME. VISUALLY INSPECTED INLET & OUTLET ACM DUCTING. NO CONTAMINANTS NOTED IN DUCT WORK, INSPECTED OIL BOWLS, OIL IS CLEAR WITH NO LOSS INDICATED. REMOVED AND CLEANED FWD & AFT COALESCER SOCKS. REINSTALLED IN A/C. 2L72 4J RTT00007WI 20060117001572006011700157NM 2006 1 17 ASAA0540529 120051012A53306545772 SKIN BOEING737 737490 1384715NM FS 860-887 CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02793AS 28888 PAE - FUSELAGE SKIN IS CHAFED LT AND RT SIDES, BS 860 TO 887 STRINGER 2 LEFT TO STRINGER 2 RT. REPAIRED SKIN PER EA 5360-01043, ER 05-4273. (M) 2L72 4F RTA16WE 20060117001592006011700159NM 2006 1 17 ASAA0540587 120051028A532065529113 REVEAL BOEING737 7374Q8 138447QNM FS 328 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - FOUND FORWARD SERVICE DOOR CUTOUT AFT LOWER SEAL DEPRESSOR IS CRACKED. REMOVED AND REPLACED PER B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060117001612006011700161NM 2006 1 17 ASAA0540581 120051028A534065C161216 FITTING BOEING737 7374Q8 138447QNM FS 313 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - FOUND CORROSION ON FITTING. REMOVED AND REPLACED FITTING PER B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060117001632006011700163NM 2006 1 17 ASAA0540573 120051028A53206517688175 SILL BOEING737 7374Q8 138447QNM FS 320-339 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - FOUND MOPSILL CORRODED. REPLACED MOPSILL PER B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060117001652006011700165NM 2006 1 17 ASAA0540576 120051028A534065C161215 FITTING BOEING737 7374Q8 138447QNM FS 340 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - FOUND FITTING CORRODED. REPLACED CORRODED FITTING PER B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060117001672006011700167NM 2006 1 17 ASAA0540578 120051028A5320654587545 SILL BOEING737 7374Q8 138447QNM FS 294-340 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - FOUND CORROSION ON MOPSILL. REMOVED AND REPLACED MOPSILL PER B737-400 SRM 51-40-52. (M) 2L72 4F RTA16WE 20060117001722006011700172NM 2006 1 17 AWXA200600037 120051221A5340654583347 CLIP BOEING737 73733A 1384673NM BS 178 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - MAJOR REPAIR - DURING C19 DISCOVERED FLOOR WEB ATTACH CLIP CRACKED, .25 INCHES, AT BS 178, WL 208, FROM BL 25L TO BL 29L. MAINTENANCE REMOVED AND INSTALLED NEW FLOOR WEB ATTACH CLIP AT BS 178, WL 208 AND BL 25L TO BL 29L IAW BOEING 737-300 SRM 51-40-02-0G. 2L72 4F RTA16WE 20060117001742006011700174NM 2006 1 17 AWXA200600039 120051221A534069353521 STRINGER CLIP BOEING737 73733A 1384673NM BS 685 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED STRINGER CLIP CRACKED, .5 INCHES, AT BS 685 AND STR 4R. MAINTENANCE REMOVED AND ISNTALLED NEW CLIP AT BS 685 AND STR 4R IAW BOEING 737-300 SRM 51-40-02-0G FIG 8 AND FIG 12. 2L72 4F RTA16WE 20060117001762006011700176NM 2006 1 17 AWXA200600041 120051217A531565498842 FLOORBEAM BOEING737 7373G7 1384595NM BS 967 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 MCN - MAJOR REPAIR - DURING C15 CHECK DISCOVERED CORROSION ON BEAM T-CAP AT BS 967, BL 5L AND BL 41L, WL 208. MAINTENANCE CUT OUT DAMAGED AREA IAW BOEING 737-300 SRM 53-00-52-2R2 FIG 201. FABRICATED SUPPORT ANGLES, STRAPS, EXTRUSION AND REPAIR SECTION IAW BOEING 737-300 SRM 53-00-51-2R2. INSTALLED FABRICATED REPAIR PARTS AT BS 967, WL 208 AND AT BL 5L AND 41L. 2L72 4F RTA16WE 20060117001772006011700177EU 2006 1 17 AWXA200600042 120051230A5220 COVER AIRBUS320 A320232 3930326EU EMERGENCY EXIT MISSING A AWXAO OTHER E VIBRATION/BUFFET CRCRUISE 1 WP28651AW 866 BOS - VIBRATION - CREW REPORTED THAT THE RT EMERGENCY EXIT WINDOWS PRODUCING LOUD SQUEAL AND FLOOR VIBRATION. MAINTENANCE INSPECTION DOORS AND FOUND NO DEFECTS. FOUND MISSING HOIST POINT COVER ON THE FWD DOOR. APPLIED SPED TAPE AND PLACED ON OIL. ON 09JAN06, MAINTENANCE REPLACED THE HOIST POINT COVER. REPORTED FOR PRECAUTIONARY PURPOSES. 2L72 4F RTA28NM 20060117001792006011700179NM 2006 1 17 ASAA0540579 120051028A531165C336411 FRAME BOEING737 7374Q8 138447QNM FS 380 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - FOUND CORROSION ON FRAME. REMOVED DAMAGED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR PARTS PER B737-400 SRM 53-00-07. (M) 2L72 4F RTA16WE 20060117001802006011700180NM 2006 1 17 ASAA0540537 120051012A5347655384421 CARGO TRACK BOEING737 737490 1384715NM FS 945-915 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02793AS 28888 PAE - FOUND CORROSION AT LEFT CARGO TIE DOWN TRACK AT NUT PLATE LOCATIONS. REMOVED CORROSION ON LEFT CARGO TIE DOWN NUT PLATE LOCATIONS, FABRICATED REPAIR PARTS AND INSTALLED PER B737-200 SRM 53-62-53. (M) 2L72 4F RTA16WE 20060117001812006011700181NM 2006 1 17 ASAA0540574 120051028A5320654587514 ANGLE BOEING737 7374Q8 138447QNM FS 317 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - FOUND Z-ANGLE CORRODED. REPLACED CORRODED Z-ANGLE PER B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060117001822006011700182NM 2006 1 17 ASAA0540589 120051028A53136561777505 STRINGER BOEING737 7374Q8 138447QNM FS 359 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND CRACK IN STRINGER 14L AT STRINGER SPLICE. REMOVED DAMAGED SECTION, FABRICATED REPAIR PARTS AND INSTALLED PER B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060117001832006011700183NM 2006 1 17 ASAA0540564 120051025A534069353500503 STRINGER CLIP BOEING737 7374Q8 138447QNM FS 500E CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - FOUND BS 500E STRINGER 12AR AND 12BR STRINGER CLIPS CRACKED. REMOVED AND REPLACED STRINGER 12BR. STRINGER 12AR WAS NDI`D AND FOUND NOT TO BE CRACKED. (M) 2L72 4F RTA16WE 20060117001842006011700184NM 2006 1 17 ASAA0540539 120051012A53476546813109 SEAT TRACK BOEING737 737490 1384715NM FS 320-540 GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02793AS 28888 PAE - FOUND SEAT TRACK AT WL 208, RBL 45 HAS MECHANICAL DAMAGE AT BS 520 AND 540. SEAT TRACK AT WL 208, RBL 45 GOUGED 1 INCH BY 1 INCH BY 40 INCH OUT OF LIMITS. REPAIRED TRACK PER SRM 53-00-52 PAGE 201 FIGURE 21. (M) 2L72 4F RTA16WE 20060117001862006011700186NM 2006 1 17 ASAA0540569 120051026A532065784394 SUPPORT ANGLE BOEING737 7374Q8 138447QNM FS 296 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - FOUND CRACKED SUPPORT ANGLE. REPLACED SUPPORT ANGLE PER B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060117001882006011700188NM 2006 1 17 ASAA0540595 120051102A53116547952355 FRAME BOEING737 7374Q8 138447QNM FS 794 CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - FOUND AFT CARGO DOOR LOWER FORWARD SIDE FRAME HAS MULTIPLE NICKS AND CHAFING FROM LOWER STOP CUTOUT TO LOWER EDGE OF DOOR. REMOVED AND REPLACED FRAME SECTION PER B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060117001902006011700190NM 2006 1 17 ASAA0540583 120051028A5320654587565 WEB BOEING737 7374Q8 138447QNM FS 294-340 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - FOUND CORROSION ON SUBTHRESHOLD WEB COMMON TO MOPSILL. REMOVED DAMAGED WEB, FABRICATED NEW WEB AND INSTALLED PER B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060117001912006011700191NM 2006 1 17 ASAA0540561 120051023A533065C357984 SKIN BOEING737 737490 1384715NM FS 998-999 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02708AS 28895 OKC - FUSELAGE SKIN IS DENTED AT BS 999 BETWEEN STRINGER 13R-14R. A=1.8 INCH, Y=0.067 INCH, A/Y = 26.9. LOWER EDGE OF DENT PERIPHERY IS 1.2 INCH FROM SKIN LAP JOINT UPPER FASTENER ROW. CUTOUT DAMAGED AREA OF SKIN. FABRICATED AND INSTALLED A STRUCTURAL FILLER, EXTERNAL DOUBLER AND EXTERNAL TRIPLER IAW ASA EA 5330-02010. (M) 2L72 4F RTA16WE 20060117001932006011700193NM 2006 1 17 ASAA0540531 120051012A533065C323595 SKIN BOEING737 737490 1384715NM FS 460 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02793AS 28888 PAE - FOUND EXTERNAL SKIN DENT. REMOVED DAMAGED SKIN, FABRICATED REPAIR PARTS AND INSTALLED PER EA 5330-02006. (M) 2L72 4F RTA16WE 20060117001952006011700195NM 2006 1 17 ASAA0540562 120051023A575165C259132 SKIN BOEING737 737490 1384715NM RT AILERON GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02708AS 28895 OKC - RIGHT AILERON TRAILING EDGE LOWER SURFACE GOUGED EDGE ADJACENT TO THE THIRD TAB HINGE FROM THE INBOARD EDGE. REMOVED DAMGAED AREA OF PLIES, PREPARED AND APPLIED REPAIR PLIES IAW B737-400 SRM 57-60-01 FIGURE 201 AND 51-70-05 PARAGRAPH 3. WEIGHT AND BALANCE ACCOMPLISHED ON MIG-5 4911163. (M) 2L72 4F RTA16WE 20060117001972006011700197NM 2006 1 17 ASAA0540520 120051001A5347 SEAT TRACK BOEING737 737490 1384715NM BS 520-540 DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02793AS 28888 PAE - FOUND SEAT TRACK AT WL 208, RBL 45 HAS MECHANICAL DAMAGE AT BS 520 AND 540. SEAT TRACK AT WL 208, RBL 45 GOUGED 1 INCH BY 1 INCH BY .040 OUT OF LIMITS REPAIRED TRACK PER B737-200 SRM 53-00-52 PAGE 201 FIG 20. (M) 2L72 4F RTA16WE 20060117003202006011700320EA 2006 1 17 COMA0560789 120051231A5730601R100414 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE RT WING DENTED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA29272 7031 RT WING SKIN DENTED 1 INCH DIA BY .030 DEEP AT WS 252.8. REPAIRED RT WING SKIN AT WS 252.8 BY BLENDING DAMAGED AREA, PERFORMED EDDY CURRENT ROTO PEN AND TOUCHED UP REWORK AREA IAW REO 601R-57-21-671. 2L72 4F4 FRTA21EA E15NE 20060117003212006011700321WP 2006 1 17 ASA0580449 120050808A53205936442U3 WEB DOUG DC9 DC982 3022082WP FS 1155-1211 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02935AS 49236 OKC - DURING C-CHECK, FOUND AFT CARGO BAY THRESHOLD WEB CORRODED. REPLACED WEB. (M) 2L72 4F A6WE 20060117003252006011700325NM 2006 1 17 PCSA12300501 120051230A2420 CONTROL PANEL BOEING727 727233 138408ANM PWA JT8 JT8D15 52051NE COCKPIT UNSECURE A PCSAA UNSCHED LANDING WG INADEQUATE Q C MULTIPLE FAILURE CRCRUISE 1 SO29994AJ 20942 CLIMBED TO CRUISE, CREW REPORTED NR 3 GEN BREAKER LIGHT CAME ON & WOULD NOT HOLD POWER, NR 2 GEN BREAKER & FIELD LIGHTS CAME ON, NO FAULT NOTED, RESET NR 2 GEN & 20 MIN LATER FAULT RETURNED NO LIGHTS. DID NOT RESET NR 2 BREAKER. DIVERTED ACFT, & LANDED WITHOUT INCIDENT. MX INSP & T/SHOT ACFT GEN SYS, MX FOUND NR 3 GEN CONTROL PANEL NOT SECURED, MX SECURED NR 3 GCU IAW MM & PERFORMED AN OPS CHK IAW MM, OPS CHK ON GROUND FOUND NORMAL. OPS CHK OF NR 2 GEN AC POWER PERFORMED IAW 24-22-00, OPS NORMAL. BUSS PROTECTION PANEL R & R IAW MM; GCU NR 2 SWAPPED TO APU GCU FOR T/SHOOTING. NR 2 AC POWER GEN SYS & APU GEN SYS OPS TESTED & CHKD NORMAL IAW MM. FERRY FLT BACK TO MIA FOR FURTHER INSP. ACFT RETURNED W/OUT INCIDENT.2L73 4F4 FRTA3WE E2EA 20060117003282006011700328NM 2006 1 17 UPS05245890 120051213A5320 FLOOR SUPPORT BOEING727 72722C 138400FNM RROYCETAY TAY65154 EU AFT CARGO BAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE: C AFT CARGO FLOOR SUPPORT BEAM CRACK ON S28 BETWEEN FR 1060 AND 1090 AT SP LICE PLATE FROM RIVET HEAD. CUT OUT DAMAGED SECTION OF FLOOR SUPPORT IAW SRM REF 53-10-5. FABRICATED REPAIR PARTS IAW SRM REF 53-10-5 FIG 4. REPAIR CARRIED OUT IAW SRM REF 53-10-5 FIG4. 2L73 4F4 F A3WE E25NE 20060118002142006011800214NM 2006 1 18 GTIA050288 120051214A3240284703 CONTROL VALVE DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE LT MLG WARPED A GTIAK NONE O OTHER UKUNKNOWN 1 GL23822NK 49392 BRAKES WERE SPONGY AND SLOW TO STOP AC. REMOVED AND REPLACED LT POWER BRAKE CONTROL VALVE ASSY. (K) 2L72 4F4 FRT E9NE 20060119000032006011900003WP 2006 1 19 ABXA060027 120051023A5314 KEELBEAM DOUG DC8 DC863F 302198FWP BS 700-740 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 BS 700 - 740, LEFT BUTT LINE 10, LEFT SIDE OF KEELBEAM, CORROSION ON THE LOWER CENTER WING SPLICE DOUBLER. CLEANED CORROSION, TREATED, AND PRIMED IAW DC8 SRM 51-1-8, 53-2-0, LWR NR 200302015. FABRICATED AND INSTALLED REPAIR DOUBLER IAW REA D853-52564. 2L74 4F 4A25 20060119000212006011900021NM 2006 1 19 AWXA200600061 120051221A53126516300166 BULKHEAD BOEING737 7373G7 1384595NM BS 178 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 MCN - DURING C15 CHECK DISCOVERED BS 178 BULKHEAD WEB CRACKED IN TWO PLACES, .975 INCHES AND 1.1 INCHES, AT WL 213 BL 7R AND WL 218 BL 10R. MAINTENANCE STOP DRILLED BOTH CRACKS IAW BOEING 737-300 SRM 53-10-09-2R10. FABRICATED DOUBLER, STIFFENERS, CLIPS, FILLERS AND STRUCTURAL FILLER IAW BOEING 737-300 SRM 5310-08-2R10. INSTALLED FABRICATED REPAIR PARTS AT BS 178, FROM BL 7R TO BL 10R AND FROM WL 213 TO WL 218. 2L72 4F RTA16WE 20060119000242006011900024NM 2006 1 19 AWXA200600064 120051221A532065C3267712 CHANNEL BOEING737 7373G7 1384595NM BS 986-1006 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 MCN - DURING C15 CHECK DISCOVERED CORROSION ON CHANNEL UNDER WEB FROM BS 986 TO BS 1006, FROM BL 35R TO BL 41R AT WL 208. MAINTENANCE REMOVED AND INSTALLED NEW CHANNEL FROM BS 986 TO BS 1006, FROM BL 35R TO BL 41R AT WL 208 IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 3, 4 AND 12. 2L72 4F RTA16WE 20060119000372006011900037NM 2006 1 19 AWXA200600078 120051206A532065528941 CHANNEL BOEING737 7373Y0 1384671NM BS 540 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - DURING C16 CHECK DISCOVERED CHANNEL CRACKED, .75 INCHES, AT BS 540, WL 206 AND BL 1L. MAINTENANCE REMOVED AND INSTALLED NEW CHANNEL ASSY AT BS 540, WL 206 AND BL 1L IAW BOEING 737-300 SRM 51-40-02-0G FIG 12. 2L72 4F RTA16WE 20060119000382006011900038NM 2006 1 19 AWXA200600079 120051209A532065516989 CHANNEL BOEING737 7373Y0 1384671NM BS 907 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - DURING C16 CHECK DISCOVERED CHANNEL CRACKED, 1.2 INCHES, AT BS 907 AND STR 4L. MAINTENANCE REMOVED AND INSTALLED NEW CHANNEL AT BS 907 AND STR 4L IAW BOEING 737-300 SRM 51-40-02-0G FIG 8 AND 12. 2L72 4F RTA16WE 20060119000412006011900041NM 2006 1 19 AWXA200600082 120051216A5340693535216 STRINGER CLIP BOEING737 7373Y0 1384671NM BS 1006 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - DURING C16 CHECK DISCOVERED STRINGER TIE CRACKED, .25 INCHES, AT STR 7L. AND BS 1006. MAINTENANCE REMOVED AND INSTALLED NEW STRINGER TIE AT STR 7L AND BS 1006 IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 8 AND 12. 2L72 4F RTA16WE 20060119000522006011900052NM 2006 1 19 AWXA200600091 120051203A57536546435278 SKIN BOEING737 7373Y0 1384671NM TE FLAPS DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - DURING C16 CHECK DISCOVERED RT OUTBOARD AFT FLAP DELAMINATED AT THE INBOARD TRAILING EDGE FROM WBL 289R TO WBL 309R. MAINTENANCE REMOVED DISBONDED SKIN AND CORE IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED REPLACEMENT CORE AND DOUBLER IAW BOEING 737-300 SRM 51-70-10-2R4. BONDED REPAIR PARTS TO THE RT OUTBOARD AFT FLAP INBOARD TRAILING EDGE, WBL 289R TO WBL 309R, IAW BOEING 737-300 SRM 51-70-10-2R4. 2L72 4F RTA16WE 20060119000532006011900053NM 2006 1 19 AWXA200600092 120051215A57536546435277SP SKIN BOEING737 7373Y0 1384671NM ZONE 500 DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - DURING C16 CHECK DISCOVERED LT OUTBOARD AFT FLAP DISBONDED 3" FROM THE INBOARD EDGE FROM WS 230.68L TO WS 232.68L. MAINTENANCE REMOVED DISBONDED SKIN IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED FILLER AND DOUBLER IAW BOEING 737-300 SRM 51-70-10-2R4. BONDED REPAIR PARTS TO THE LT OUTBOARD AFT FLAP, WS 230.68L TO WS 232.68L, IAW BOEING 737-300 SRM 51-70-10-2R4. 2L72 4F RTA16WE 20060119000592006011900059NM 2006 1 19 AWXA200600098 120051205A575465C2679311 SKIN BOEING737 7373Y0 1384671NM NR 3 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - DURING C16 CHECK DISCOVERED 2 CRACKS ON THE BOTTOM OF THE NR 3 SLAT SKIN, FROM SS 67L TO SS 69L. MAINTENANCE CUT OUT DAMAGED SKIN IAW BOEING 737-300 SRM 57-43-01-2R6 FIG 201. FABRICATED FILLER AND SPLICE PLATE IAW BOEING 737-300 SRM 57-43-01-2R6 FIG 201. INSTALLED FABRICATED REPAIR PARTS ON THE NR 3 SLAT SKIN FROM SS 67L TO SS 69L IAW BOEING 737-300 SRM 57-43-01-2R6 FIG 201. 2L72 4F RTA16WE 20060119000622006011900062NM 2006 1 19 AWXA200600101 120051218A534069353641 STRINGER CLIP BOEING737 7373G7 1384595NM BS 947 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 MCN - DURING C15 CHECK DISCOVERED STRINGER TIE CLEAT CRACKED, .700 INCHES, AT STR 20L AND BS 947. MAINTENANCE REMOVED AND INSTALLED NEW STRINGER TIE AT STR 20L AND BS 947 IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 3, 8 AND 12. 2L72 4F RTA16WE 20060119000632006011900063NM 2006 1 19 AWXA200600102 120051220A5340654583348 CLIP BOEING737 7373G7 1384595NM BS 178 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 MCN - DURING C15 CHECK DISCOVERED FLOOR WEB CLIP CRACKED, .38 INCHES, AT BS 178, WL 207 AND BL 30R. MAINTENANCE REMOVED CRACKED CLIP AND FABRICATED NEW CLIP IAW BOEING DWG 65-45833. INSTALLED FABRICATED REPAIR PARTS AT BS 178, WL 207 AND BL 30R IAW BOEING 737-300 SRM 51-40-02-0G FIGURE 12. 2L72 4F RTA16WE 20060119001142006011900114NM 2006 1 19 AWXA200600122 120051222A53206546812187 FLOOR SUPPORT BOEING737 73733A 1384673NM BS 1000-1016 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - DURING C19 CHECK DISCOVERED CORROSION ON BS 1000 TO BS 1016 FLOOR SUPPORT FROM BL 5L TO BL 10R, WL 208. MAINTENANCE REMOVED DAMAGED AREA AND FOUND CORROSION TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-15-1A1 FIG 101. REMOVED AND INSTALLED NEW FLOOR SUPPORT AT BS 1000 TO BS 1016 AND FROM BL 5L TO BL 104, WL 208 IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 8 AND 12. 2L72 4F RTA16WE 20060119001492006011900149NM 2006 1 19 AWXA200600114 120051222A5311654655216 FRAME BOEING737 73733A 1384673NM BS 827 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - DURING C19 CHECK DISCOVERED CORROSION ON FUSELAGE FRAME ATTACH ANGLE AT AFT PIT BS 827, BL 13.80R AND WL 148. CORROSION WAS OUT OF LIMITS IAW BOEING 737-300 SRM 53-00-07-1A1 FIG 101. MAINTENANCE REMOVED ANGLE AND FABRICATED REPLACEMENT ANGLE IAW BOEING 737-300 SRM 53-00-07-1A1 FIG 101. INSTALLED FABRICATED REPLACEMENT PARTS AT AFT PIT BS 827, BL 13.80R AND WL 148 IAW BOEING 737-300 SRM 53-00-07-1A1 FIG 101. 2L72 4F RTA16WE 20060119001672006011900167WP 2006 1 19 MWEA050123 120051114A3830 NIPPLE DOUG DC9 DC981 3022081WP LAVATORY FILL BROKEN A MWEAA UNSCHED LANDING O OTHER CLCLIMB 1 GL31807ME 48033 LAVATORY FILL/SERVICE NIPPLE WAS DAMAGED. MAINTENANCE REPLACED FRANGIBLE NIPPLE. 2L72 4F A6WE 20060120000352006012000035CE 2006 1 20 DXTA200501160 120051223A3200 LANDING GEAR CESSNA750 750 2076810CE MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07948QS 7500149 GEAR WOULD NOT RETRACT AFTER TAKEOFF. JACKED AIRCRAFT, OPS CHECK OF LANDING GEAR, LANDING GEAR CYCLED NORMALLY. DISCONNECTED ALL CONNECTORS TO UPLOCKS AND SQUAT SWITCHES. CLEANED ALL CONNECTORS. VERIFIED SQUAT SWITCHES WERE PROPERLY RIGGED. CONNECTED ALL CONNECTORS. PERFORMED LANDING GEAR OPERATIONAL TEST IAW CE MM 32-60-00. ALL CHECKS GOOD. CYCLED GEAR NUMEROUS TIMES WITH NO FAULTS. ALL WORK DONE IAW 750 M/M 32-00-01, 32-60-00 AND 32-60-01. 2L72 4J RTT00007WI 20060120000542006012000054NM 2006 1 20 ASAA0570038 120050718A5700313A240019 SEAL BOEING737 737790 13844CNNM FAIRING CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02613AS 30163 PAE - DURING C-CHECK, FOUND LOWER SKIN CHAFED AT NR 1 ENGINE PYLON AFT FAIRING UPPER BLADE SEAL JUST AFT OF FUEL CELL PANEL 532BB. REPAIRED IAW EA 5720-01272. (M) 2L72 4F RTA16WE 20060120000552006012000055NM 2006 1 20 ASAA0590109 120050606A5230146A610028 SKIN BOEING737 737990 NM CARGO DOOR GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02317AS 30016 PAE - DURING CHECK, FOUND GOUGES AND DENTS ON AFT CARGO DOOR OUTER SKIN. REPAIRED IAW EA 5230-01265. (M) 2L74 4F RTA16WE 20060120000562006012000056NM 2006 1 20 ASAA0570039 120050718A5700313A240019 SEAL BOEING737 737790 13844CNNM FAIRING CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02613AS 30163 PAE - DURING C-CHECK, FOUND RT WING LOWER SKIN CHAFED AT NR 2 ENGINE AFT PYLON FAIRING UPPER BLADE SEAL JUST FORWARD OF FUEL CELL PANEL 632BB. REPAIRED IAW EA 5720-01272. (M) 2L72 4F RTA16WE 20060120000612006012000061NM 2006 1 20 ASAA0570053 120050816A5320146A75022 SUPPORT BOEING737 737790 13844CNNM FS 727-767 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02614AS 30343 PAE - DURING C-CHECK, FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT AT BS 727-767 RT. REPAIRED IAW SRM 51-40-05. (M) 2L72 4F RTA16WE 20060120000632006012000063NM 2006 1 20 ASAA0570035 120050718A5321453A1610 FLOOR PANEL BOEING737 737790 13844CNNM FS 440-500 PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02613AS 30163 PAE - DURING C-CHECK, FOUND FORWARD CARGO BAY NR 2 FLOOR PANEL IS PUNCTURED. REPAIRED IAW SRM 53-00-00. (M) 2L72 4F RTA16WE 20060120000642006012000064NM 2006 1 20 ASAA0590081 120050422A5320141A850533 SUPPORT BOEING737 737990 NM FUSLEAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02323AS 30021 PAE - DURING C-CHECK, FOUND E/E CUTOUT AFT STOP FITTING CHAFED. REPAIRED IAW SRM 51-40-02. (M) 2L74 4F RTA16WE 20060120000662006012000066NM 2006 1 20 ASAA0570028 120050627A53471A2260387 SEAT TRACK BOEING737 737790 13844CNNM FUSELAGE WORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM02629AS 30626 PAE - DURING C-CHECK,FOUND CAPT INBOARD SEAT TRACK WORN BEYOND LIMITS. REPLACED IAW MM 25-11-11. (M) 2L72 4F RTA16WE 20060120000682006012000068NM 2006 1 20 ASAA0590105 120050428A5320143A751022 INTERCOSTAL BOEING737 737990 NM FS 500A DEFORMED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02309AS 30857 PAE - DURING C-CHECK, FOUND INTERCOSTAL AT BS 500A-500B RBL 24 WL 156 DEFORMED. FABRICATED REPLACEMENT INTERCOSTAL IAW SRM 53-30-53. (M) 2L74 4F RTA16WE 20060120000702006012000070NM 2006 1 20 ASAA0590104 120050428A5321453A161013 FLOOR PANEL BOEING737 737990 NM FS 500 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02309AS 30857 PAE - DURING C-CHECK, FOUND FORWARD CARGO BAY NR 3 FLOOR PANEL DAMAGED/DENTED. FABRICATED REPLACEMENT PANEL IAW SRM 51-10-02. (M) 2L74 4F RTA16WE 20060120000722006012000072NM 2006 1 20 ASAA0570040 120050718A5700313A240019 SEAL BOEING737 737790 13844CNNM FAIRING CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02613AS 30163 PAE - DURING C-CHECK, FOUND LEFT WING LOWER SKIN CHAFED AT NR 1 ENGINE PYLON AFT FAIRING UPPER BLADE SEAL JUST FORWARD OF FUEL CELL PANEL 532 BB. REPAIRED IAW EA 5720-01272. (M) 2L72 4F RTA16WE 20060120000742006012000074NM 2006 1 20 ASAA0570043 120050718A5321453A261013 FLOOR PANEL BOEING737 737790 13844CNNM FS 727-774 GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02613AS 30163 PAE - DURING C-CHECK, FOUND AFT CARGO BAY NR 2 FLOOR PANEL GOUGED AND DENTED. REPAIRED IAW SRM 51-40-05. (M) 2L72 4F RTA16WE 20060119000012006011900001WP 2006 1 19 ABXA060031 120051230A5340 FITTING DOUG DC8 DC863F 302198FWP BS 50 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 INTERCOSTAL CORNER FITTING CRACKED FUSELAGE STA 50, RIGHT BUTT LINE 50, FORWARD OF FLOORBEAM. REMOVED CRACKED CORNER FITTING IAW DC8 SRM 51-1-20D. FABRICATED NEW CORNER FITTING IAW REA D853-52924 AND INSTALLED AT STA 50, RIGHT BUTT LINE 50, FORWARD OF FLOORBEAM IAW DC8 SRM 51-1-20D. 2L74 4F 4A25 20060119000042006011900004WP 2006 1 19 ABXA060032 120051214A5315 FLOORBEAM DOUG DC8 DC863F 302198FWP BS 920 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 UPPER HORIZONTAL CAP OF FLOORBEAM CORRODED AT STA 920, LEFT BUTT LINE 10. REMOVED CORROSION. DAMAGE OUT OF LIMITS. FLOORBEAM REPAIRED IAW REA D853-52567. 2L74 4F 4A25 20060119000172006011900017NM 2006 1 19 AWXA200600057 120051220A5320654583340 WEB BOEING737 7373G7 1384595NM BS 180 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 MCN - DURING C15 CHECK DISCOVERED FLOOR WEB CRACKED, .75 INCHES, AT BS 180, WL 207 AND BL 30L. MAINTENANCE REMOVED CRACKED FLOOR WEB, FABRICATED REPLACEMENT FLOOR WEB AND INSTALLED AT BS 180, WL 207 AND BL 30L IAW BOEING 737-300 SRM 53-10-51, BAC DWG 65-45833 AND BOEING 737-300 SRM 51-40-05-0G. 2L72 4F RTA16WE 20060119000292006011900029NM 2006 1 19 AWXA200600069 120051215A57536546486130 WEDGE BOEING737 7373G7 1384595NM TE FLAP DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 MCN - DURING C15 CHECK DISCOVERED THE RT INBOARD MID-FLAP TRAILING EDGE WEDGE HAD DISBOND ON THE UPPER SURFACE, 48.5" FROM THE INBOARD END. MAINTENANCE REMOVED THE DISBONDED SKIN IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED FILLER AND DOUBLER IAW BOEING 737-300 SRM 51-70-10-2R4. BONDED REPAIR PARTS TO THE RT INBOARD MID-FLAP TRAILING EDGE WEDGE UPPER SURFACE, 48.5" FROM INBOARD END IAW BOEING 737-300 SRM 51-70-10-2R4. 2L72 4F RTA16WE 20060119000582006011900058NM 2006 1 19 AWXA200600097 120051207A575465C2679312 SKIN BOEING737 7373Y0 1384671NM NR 6 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - DURING C16 CHECK DISCOVERED 5 CRACKS, .80 INCHES EACH, ON THE BOTTOM OF THE NR 6 SLAT SKIN, FROM SS 320R TO SS 325R. MAINTENANCE CUT OUT DAMAGED SKIN IAW BOEING 737-300 SRM 57-43-01-2R6 FIG 201. FAB`D FILLER AND SPLICE PLATE IAW BOEING 737-300 SRM 57-43-01-2R6 FIG 201. INSTALLED FABRICATED REPAIR PARTS ON THE NR 6 SLAT SKIN FROM SS 320R TO SS 325R IAW BOEING 737-300 SRM 57-43-01-2R6 FIG 201. 2L72 4F RTA16WE 20060119000612006011900061NM 2006 1 19 AWXA200600100 120051218A534069353523 STRINGER CLIP BOEING737 7373G7 1384595NM BS 947 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 MCN - DURING C15 CHECK DISCOVERED STRINGER TIE CRACKED, .700 INCHES, AT STR 26L AND BS 947. MAINTENANCE REMOVED AND INSTALLED NEW STRINGER TIE AT STR 26L AND BS 947 IAW BOIENG 737-300 SRM 51-40-02-0G FIGURES 3, 8 AND 12. 2L72 4F RTA16WE 20060119001282006011900128NM 2006 1 19 AWXA200600108 120051218A5320654587545 STRUCTURE BOEING737 7373Y0 1384671NM BS 288-292 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - DURING C19 CHECK DISCOVERED CORROSION ON RT CHORD FROM BS 288 TO BS 292, WL 208 AND BL 52R. REMOVED CORROSION AND RE-WORK WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-10-15-1A1 FIG 101. MAINTENANCE REMOVED THE RT CHORD FROM BS 288 TO BS 292, WL 208 AND BL 52R AND REPLACED WITH NEW CHORD IAW BOEING 737-300 SRM 51-40-05-0G FIG 8 AND 12. 2L72 4F RTA16WE 20060119001322006011900132NM 2006 1 19 AWXA200600112 120051226A5310655287477 DOOR FRAME BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - DURING C19 CHECK DISCOVERED THE L2 DOORWAY STOP FITTING, LOWER FASTENER HOLE CRACKED .125 INCHES. MAINTENANCE REMOVED THE L2 DOOR FORWARD FRAME IAW BOEING 737-300 SRM 51-40-02-0G FIG 8. INSTALLED NEW L2 DOOR FORWARD FRAME IAW BOEING 737-300 SRM 51-40-02-0G FIG 8. 2L72 4F RTA16WE 20060119001522006011900152NM 2006 1 19 AWXA200600117 120051221A5340693535214 STRINGER CLIP BOEING737 73733A 1384673NM BS 639 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - DURING C19 CHECK DISCOVERED STRINGER TO STRINGER CLIP CRACKED, .25 INCHES, AT BS 639 AND STRINGER 4L. MAINTENANCE REMOVED CRACKED CLIP AND FORMED REPLACEMENT CLIP IAW BOEING 737-300 SRM 51-40-02-0G. INSTALLED NEW REPLACEMENT CLIP AT BS 639 AND STRINGER 4L IAW BOEING 737-300 SRM 51-40-02-0G. 2L72 4F RTA16WE 20060119001542006011900154NM 2006 1 19 AWXA200600119 120051224A5320654585547 ANGLE BOEING737 73733A 1384673NM BS 975-985 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - DURING C19 CHECK DISCOVERED CORROSION ON THE R2 INNER CHORD LOWER ANGLE FROM BS 975 TO BS 985, BL 47R AND WL 207.5. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-15-1A1 FIG 101. MAINTENANCE REMOVED AND FABRICATED REPLACEMENT ANGLE IAW BOEING 737-300 SRM 51-40-02-0G AND BOEING DWG 65-45855. INSTALLED FABRICATED REPAIR PARTS AT BS 975 TO BS 985, BL 47R AND WL 207.5 IAW BOEING 737-300 SRM 51-40-02-0G FIGURE 12. 2L72 4F RTA16WE 20060120000592006012000059NM 2006 1 20 ASAA0570033 120050718A5320146A75022 SUPPORT BOEING737 737790 13844CNNM FS 727-767 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02613AS 30163 PAE - DURING C-CHECK, FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT AT BS 767. REPAIRED IAW SRM 53-00-00. (M) 2L72 4F RTA16WE 20060120000602006012000060NM 2006 1 20 ASAA0570051 120050816A5320146A75022 SUPPORT BOEING737 737790 13844CNNM FS 767 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02614AS 30343 PAE - DURING C-CHECK, FOUND FLOOR TO SIDEWALL SUPPORT CORRODED. REPAIRED IAW SRM 51-40-02. (M) 2L72 4F RTA16WE 20060120000622006012000062NM 2006 1 20 ASAA0590110 120050606A5312143A948535 ANGLE BOEING737 737990 NM BS 500L CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02317AS 30016 PAE - DURING CHECK, FOUND CORROSION ON FORWARD CARGO BAY AFT BULKHEAD LOWER SUPPORT ANGLE. REPAIRED IAW SRM 51-40-02. (M) 2L74 4F RTA16WE 20060120000652006012000065NM 2006 1 20 ASAA0570027 120050627A53471A2260388 SEAT TRACK BOEING737 737790 13844CNNM FUSELAGE WORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM02629AS 30626 PAE - DURING C-CHECK, FOUND F/O INBOARD SEAT TRACK WORN BEYOND LIMITS. REPLACED IAW MM 25-11-11. (M) 2L72 4F RTA16WE 20060120000672006012000067NM 2006 1 20 ASAA0570023 120050524A5321453A261031 FLOOR PANEL BOEING737 737790 13844CNNM FS 727 DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02611AS 29753 PAE - AFT CARGO BAY NR 1 FLOOR PANEL IS DAMAGED. REPAIRED IAW SRM 53-60-53. (M) 2L72 4F RTA16WE 20060120000692006012000069NM 2006 1 20 ASAA0590106 120050428A5321453A261017 FLOOR PANEL BOEING737 737990 NM FS 727J DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02309AS 30857 PAE - DURING C-CHECK, FOUND AFT BAY NR 3 FLOOR PANEL HAS NUMEROUS DENTS. FABRICATED REPLACEMENT. (M) 2L74 4F RTA16WE 20060120000712006012000071NM 2006 1 20 ASAA0570054 120050816A5321453A261058 FLOOR PANEL BOEING737 737790 13844CNNM FS 727-767 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02614AS 30343 PAE - DURING C-CHECK, FOUND AFT CARGO BAY NR 2 FLOOR PANEL DENTED. REPAIRED IAW SRM 53-60-53. (M) 2L72 4F RTA16WE 20060120000732006012000073NM 2006 1 20 ASAA0570042 120050718A5321453A261015 FLOOR PANEL BOEING737 737790 13844CNNM FS 727 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02613AS 30163 PAE - DURING C-CHECK, FOUND AFT CARGO BAY NR 1 FLOOR PANEL GOUGED AND DENTED. REPAIRED IAW SRM 51-40-5. (M) 2L72 4F RTA16WE 20060120000752006012000075NM 2006 1 20 ASAA0570037 120050718A5340141A76502 ATTACH FITTING BOEING737 737790 13844CNNM BS 258 GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02613AS 30163 PAE - DURING C-CHECK, FOUND NLG RETRACT ACTUATOR ATTACH LUG FITTING BEARING BORE DAMAGED. REPAIRED IAW SRM 51-40-02. (M) 2L72 4F RTA16WE 20060120000852006012000085NM 2006 1 20 UPS06445939 120051230A5310 VERTICAL BEAM BOEING747 747212B 1384886NM NLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 INSPECTION TYPE:C NWW RT BS 280 VERTICAL BEAM WEB ONE EA STAND OFF HOLE FOUND CRACK JUST ABOVE WL 170, 3/16" RUNNING O/B 1/16" RUNNING I/B. NWW RT BS 280 VERTICAL BEAM WEB REPAIRED AS PER SRM 51-40-02 FIG 1. 2L74 4F A20WE 20060120000912006012000091NM 2006 1 20 UPS06445949 120051230A531065B100984 STIFFENER BOEING747 747212B 1384886NM KEELBEAM BOX CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 INSPECTION TYPE:C FX- AIR CONDITIONING BAY KEEL BEAM BOX AT BS 983 RBL 9" VERTICAL STIFFENER CRACKED AT LOWER AREA, CRACK LENGTH 1.5". FX- AIR CONDITIONING BAY KEEL BEAM BOX AT BS 983 RBL 9" VERTICAL STIFFENER REPLACED IAW SRM 51-10-01 PG 9. 2L74 4F A20WE 20060120000962006012000096NM 2006 1 20 ASAA0570015 120050121A5311146A9403 FRAME BOEING737 737790 13844CNNM FS 800-787 BENT A ASAAK NONE O OTHER ININSP/MAINT 1 NM02617AS 30542 PAE - DURING MAINTENANCE CHECK, FOUND FORWARD FRAME CLOSURE WEB BENT, AFT CARGO DOOR CUT OUT. REPAIR IAW SRM 51-40-02. (M) 2L72 4F RTA16WE 20060120001032006012000103SO 2006 1 20 UG82006F00000 120051228A27201159B5257253 ATTACH BRACKET GULSTMGV GULFSTREAMGV3980116SO RROYCEBR700 BR700710A110 NE TAIL COMPT FAILED E UG8AO OTHER O OTHER ININSP/MAINT 1 GL235101 4630 2177 550 (REF: GM06-001) NO TONE OR RUDDER LIMIT ANNUNCIATIONS RECEIVED DURING CONTROL CHECK. UPON INSPECTION OF THE RUDDER ACTUATOR IT WAS NOTICED THAT THE FORWARD RUDDER ATTACH FITTING HAD FAILED. SUSPECT INCORRECT HARDWARE STACK UP OR OUT OF PLACE BUSHING TO HAVE CAUSED ATTACH BOLT TO CONTACT THE BRACKET. THIS CONTACT CAUSED WEAR TO OCCUR, OVERTIME, WHICH CAUSED THE ATTACH FITTING TO FAIL. THE ATTACH FITTING WAS REPLACED IAW MM AND THE AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4F4 FRTA12EA E00057EN 20060120001062006012000106NE 2006 1 20 GTIA050285 220051210A7320 UNKNOWN DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE UNKNOWN A GTIAO OTHER R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 GL23832NK 49618 ON RUNWAY CLEARED FOR TAKEOFF THE LT ENGINE WOULD NOT RESPOND TO THROTTLE ADVANCE THE LT ENGINE REMAINED AT IDLE POWER THEN SLOWLY WOUND DOWN TO 44 PERCENT N2, AIRCRAFT TAIL SWAP WITH 803NK. INSPECTED THROTTLE LINKAGE AT FUEL CONTROL. NO DEFECTS NOTED. INSPECTED LT ENGINE INLET. NO DEFECTS NOTED. DRAINED MOSTURE FROM MOISTURE TRAP AND PERFORMED ADJ/TEST OF NR1 ENGINE. NO DEFECTS NOTED. (K) 2L72 4F4 FRTA6WE E9NE 20060120001192006012000119EU 2006 1 20 GTIA050272 120051119A3213 SLEEVE AIRBUS320 A320321 3930325EU IAE V2533 V2533A5 NE MLG CRACKED A GTIAK NONE O OTHER UKUNKNOWN 1 GL23587NK 2476 FOUND NR 4 MAIN TIRE WORN TO LIMITS, WHEN TIRE WAS REMOVED FOUND NR4 MLG AXLE SLEEVE CRACKED. DAMAGED LENGTH MEASUREMENT IS NOT BEYOND .238 INCH, ACCOMPLISHED NDT INSPECTION OF NR4 AXLE SLEEVE, NO CRACK PROPAGATION BEYOND VISIBLE MEASUREMENT OF .238 INCH. (K) 2L72 4F4 FRTA28NM E40NE 20060120001212006012000121NM 2006 1 20 GTIA050265 120051108A3250 ACTUATOR DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE RT MLG LEAKING A GTIAK NONE K FLUID LOSS UKUNKNOWN 1 GL23822NK 49392 RT MLG ACTUATOR SWIVEL GLAND LEAKING, AC TAIL SWAP WITH N815NK. RESEALED RT MLG ACTUATOR SWIVEL GLAND, NO LEAKS NOTED. (K) 2L72 4F4 FRT E9NE 20060120001232006012000123WP 2006 1 20 GTIA050262 120051009A2460 RELAY DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE FUSELAGE MALFUNCTIONED A GTIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL23830NK 49932 DC BUSS (OFF) LIGHT ILLUMINATED DURING TAXI, LOAD METER NORMAL, AIRCRAFT TAIL SWAP 811NK. FOUND DC EMERGENCY POWER TRANSFER RELAY BAD, REMOVED AND REPLACED RELAY. OPS CHECK GOOD. (K) 2L72 4F4 F A6WE E9NE 20060120001272006012000127NM 2006 1 20 GAIA05038OP 120051214A322065348784 PIN BOEING727 727251 138408HNM PWA JT8 JT8D15 52051NE NLG MISSING A GAIAK NONE E VIBRATION/BUFFET LDLANDING 1 SW07279US 21158 EXCESSIVE NOSE WHEEL SHIMMY ON LANDING. THE AIRCRAFT WAS TOWED OFF THE RUNWAY. INSPECTION REVEALED THAT THE NOSE GEAR TORQUE LINK QUICK DISCONNECT WAS MISSING. THE AIRCRAFT WAS INSPECTED FOR DAMAGE AND THE TORQUE LINK PIN WAS REPLACED. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L73 4F4 F A3WE E2EA 20060123000042006012300004NM 2006 1 23 ASAA0510336 120050930A53206517684672 INTERCOSTAL BOEING737 737298C 1384490NM BS 295 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02745AS 20794 YXX - FOUND INTERCOSTAL WEB FOUND CRACKED AT BS 295, STRINGER 8 LEFT. CRACKED INTERCOSTAL WEB AT BS 295 AND STRINGER 8 LEFT REPAIRED IAW ERO 4746 AND EO 5310-02389. (M) 2L72 4F RTA16WE 20060123000052006012300005NM 2006 1 23 ASAA0570056 120050816A5320146A75021 SUPPORT BOEING737 737790 13844CNNM FS 727-747 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02614AS 30343 PAE - DURING C-CHECK, FOUND FLOOR TO SIDEWALL SUPPORT CORRODED. REPAIRED IAW SRM 51-40-02. (M) 2L72 4F RTA16WE 20060123000072006012300007NM 2006 1 23 ASAA05700057 120050831A5310141A372212 DOUBLER BOEING737 737790 13844CNNM FS 235.8 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02622AS 30165 PAE - DURING CHECK, FOUND EXIT POWER DOOR CUTOUT DOUBLER CRACKED. REPAIRED IAW SRM 53-10-1. (M) 2L72 4F RTA16WE 20060123000202006012300020NM 2006 1 23 ASAA0570029 120050630A5321453A261032 FLOOR PANEL BOEING737 737790 13844CNNM FS 727 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02644AS 30795 PAE - DURING CHECK, FOUND CORROSION ON RIGHT AND LEFT SIDES OF NR 2 FLOOR PANEL IN AFT CARGO BAY. REPAIRED IAW SRM 51-40-02. (M) 2L72 4F RTA16WE 20060123000212006012300021NM 2006 1 23 ASAA0510335 120050930A533065621252 SKIN BOEING737 737290C 138448VNM FS 535 BULGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02740AS 22578 YXX - FOUND FUSELAGE SKIN BULGING AT BS 535 AT RT KEEL BEAM. SKIN AT BS 535 AND RT KEEL BEAM WAS REPAIRD IAW ASA EA5360-01040. (M) 2L72 4F A16WE 20060123000232006012300023NM 2006 1 23 ASAA0570017 120050418A5245149A72442 DOUBLER BOEING737 737790 13844CNNM AC BAY DOOR WORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM02607AS 29751 PAE - DURING CHECK, FOUND RIGHT AC BAY DOOR FORWARD INNER DOUBLER WORN. REPAIRED IAW SRM 53-40-71. (M) 2L72 4F RTA16WE 20060123000252006012300025NM 2006 1 23 ASAA0590111 120050616A53472A226390 SEAT TRACK BOEING737 737990 NM COCKPIT WORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM02318AS 30018 PAE - DURING C-CHECK, FOUND F/O`S INBOARD SEAT TRACK WORN. REPAIRED IAW MM 25-11-01. (M) 2L74 4F RTA16WE 20060123000272006012300027NM 2006 1 23 ASAA0570024 120050609A5330141A372212 SKIN BOEING737 737790 13844CNNM FS 219.80-243.80CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02612AS 30162 PAE - DURING C-CHECK, FOUND EXTERNAL POWER DOOR CUTOUT HAS DAMAGE. REPAIRED IAW SRM 51-40-05. (M) 2L72 4F RTA16WE 20060123000282006012300028NM 2006 1 23 ASAA0590113 120050616A5321453A261067 FLOOR PANEL BOEING737 737990 NM CARGO BAY DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02318AS 30018 PAE - DURING C-CHECK, FOUND AFT CARGO BAY NR 3 FLOOR PANEL HAS NUMEROUS DENTS. REPAIRED IAW SRM 53-60-53. (M) 2L74 4F RTA16WE 20060123000302006012300030NM 2006 1 23 ASAA0570036 120050718A5310141A85123 DOOR FRAME BOEING737 737790 13844CNNM FS 323-351 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02613AS 30163 PAE - DURING C-CHECK, FOUND E-BAY DOOR CUTOUT FRAME WEB DENTED ABOVE LATCH FITTING. REPAIRED IAW SRM 51-40-02. (M) 2L72 4F RTA16WE 20060123000372006012300037WP 2006 1 23 ABXA060030 120051222A5311 FRAME DOUG DC8 DC863F 302198FWP BS 1734 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 MAIN CARGO STA 1734 BUTT LINE 0, LONGERON 35 LEFT - 35 RIGHT, SURFACE CORROSION ON FRAME. REMOVED CORROSION FROM FRAME. DAMAGE WAS OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR IAW DC8 SRM 53-2-0 FIG 2, SHT 2. 2L74 4F 4A25 20060123000382006012300038WP 2006 1 23 ABXA060029 120051215A5320 SUPPORT BRACKET DOUG DC8 DC863F 302198FWP BS 1160 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 4606 AFT CARGO COMPARTMENT, TORQUE BOX FORWARD SIDE AT STA 1160, BETWEEN LONGERON 31 RIGHT & 32 RIGHT, ANGLE AND WEB HAD CORROSION. REMOVED CORROSION, TREATED AND PRIMED. FABRICATED NEW SUPPORT BRACKET, FOUND TO BE OUT OF LIMITS. WORK ACCOMPLISHED IAW REA D853-52918. INSTALLED SUPPORT BRACKET AND FASTENERS IAW DC8 SRM 53-2-0, 51-1-8, 51-1-20D AND 51-1-21. 2L74 4F 4A25 20060123000402006012300040WP 2006 1 23 ABXA060034 120051020A5315 FLOORBEAM DOUG DC8 DC863F 302198FWP BS 900 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 MAIN CABIN, STA 900, RIGHT BUTT LINE 54, FLOORBEAM CRACKED ON AFT SIDE UPPER CAP, FROM OUTBOARD END OF BEAM TOWARD INBOARD THROUGH TWO FASTENER HOLES. REPAIRED AREA IAW REA D853-52925 BY TRIMMING OUT CRACKED AREA AND INSTALLING A FILLER. 2L74 4F 4A25 20060123000412006012300041WP 2006 1 23 ABXA060035 120051129A5315 FLOORBEAM DOUG DC8 DC863F 302198FWP BS 880 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 MAIN CABIN, STA 880, RIGHT BUTT LINE 63, FLOORBEAM LOWER CHORD, FORWARD SIDE CORRODED. REPAIRED FLOORBEAM STA 880, RIGHT BUTT LINE 63 IAW REA D853-52566MR. 2L74 4F 4A25 20060123000422006012300042WP 2006 1 23 ABXA060036 120051109A5320 FLOOR SUPPORT DOUG DC8 DC863F 302198FWP BS 25-35 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 FLOOR SUPPORT HAT CHANNEL AT APPROXIMATELY LEFT BUTT LINE 34 BETWEEN STA 25 AND STA 35 WAS CRACKED AND HOLES DAMAGED. REMOVED DAMAGED HAT CHANNEL AND SHIM FROM STA 25 - 35, LEFT BUTT LINE 34. DAMAGE BEYOND REPAIRABLE LIMITS. FABRICATED NEW HAT CHANNEL AND SHIM. ALL PARTS TREATED, PRIMED AND INSTALLED IAW REA D853-52548, DC8 SRM 51-3-1, 51-21-1, 51-1-8, 53-3-1, 51-1-20 AND LWR 200302015. 2L74 4F 4A25 20060123000562006012300056NM 2006 1 23 GAIA05036OP 120051216A33501000677 LIGHT BOEING727 727223 1384074NM PWA JT8 JT8D9 52048NE EMER EXIT LIGHT INOPERATIVE A GAIAK NONE O OTHER ININSP/MAINT 1 SW076827 20180 DURING MAINTENANCE THE CREW ENTRY DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT. OPS CHECK GOOD. AC WAS RETURNED TO SERVICE. (K) 2L73 4F4 F A3WE E2EA 20060123000842006012300084WP 2006 1 23 ARWA20051201 120051208A2130 CABIN PRESSURE DOUG DC10 DC1010 3022110WP UNKNOWN A ARWAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO1968047 47801 AFTER TAKEOFF, UNABLE TO PRESSURIZE; RUN CHECK LIST TWICE, NO RESULT. RETURN TO MPTO. SYSTEM WAS VISUALLY INSPECTED AND PRESSURIZATION CONTROL SYSTEM TEST PERFORMED UNTIL 4 PSI OF DIFFERENTIAL PRESSURE FOUND OK AT THIS TIME IN ACCORDANCE WITH M/M 21-00-00 PAGE 511. 2L73 4F A22WE 20060123001042006012300104NE 2006 1 23 ARWA20050604 220050610A7261SOCN9229M76PO PUMP DOUG DC10 DC1030F 3023504WP GE CF6 CF650C2 30018NE NR 2 ENGINE OIL FAILED A ARWAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION LDLANDING 1 SO19478CT 47819 AFTER LANDING IN KMIA, NR 2 ENGINE OIL PRESSURE DROP DOWN TO 20 PSI; SHUTDOWN ENGINE NR 2. REMOVED AND REPLACED NR 2 ENGINE OIL PRESSURE TRANSMITTER AND REMOVED AND REPLACED OIL PUMP IN ACCORDANCE WITH DC-10 M/M 9-20-04. OPERATIONAL CHECK NORMAL IN ACCORDANCE WITH M/M 71-00. 2L73 4F4 FRTA22WE E23EA 20060119001272006011900127NM 2006 1 19 AWXA200600107 120051224A53106545855538 STRUCTURE BOEING737 73733A 1384673NM BS 947-973 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - DURING C19 CHECK DISCOVERED CORROSION ON THE R2 INNER CHORD FROM BS 947 TO BS 973, WL 208 AND BL 47R. EVIDENCE OF PREVIOUS BLEND OUT PRESENT. REMOVED CORROSION AND RE-WORK WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-15-1A1 FIG 101. MAINTENANCE REMOVED THE R2 INNER CHORD AND REPLACED WITH NEW CHORD IAW BOEING 737-300 SRM 51-40-05-0G FIG 4. 2L72 4F RTA16WE 20060119001302006011900130NM 2006 1 19 AWXA200600110 120051226A5320651758349 VERTICAL BEAM BOEING737 73733A 1384673NM BS 178 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - DURING C19 CHECK DISCOVERED VERTICAL BEAM WEB CRACKED, .5 INCHES, AT BS 178, WL 183 AND BL 5.7R. MAINTENANCE CUT OUT CRACKED SECTION OF WEB IAW BOEING 737-300 SRM 53-10-08-2R12 FIG 201. FABRICATED REPLACEMENT WEB IAW BOEING 737-300 SRM 53-10-08-2R12 FIG 201. INSTALLED FABRICATED REPLACEMENT PART AT BS 178, WL 183 AND BL 5.74 IAW BOEING 737-300 SRM 53-10-08-2R12 FIG 201. 2L72 4F RTA16WE 20060120000582006012000058NM 2006 1 20 ASAA0570026 120050627A5321 REPAIR BOEING737 737790 13844CNNM FS 440-500 TEMPORARY A ASAAK NONE O OTHER ININSP/MAINT 1 NM02629AS 30626 PAE - DURING C-CHECK, FOUND FORWARD CARGO BAY NR 2 FLOOR PANEL HAS A TEMP REPAIR ON AFT END OF PANEL. FABRICATED REPLACEMENT PANEL IAW SRM 51-40-02. (M) 2L72 4F RTA16WE 20060120000902006012000090NM 2006 1 20 UPS06445948 120051230A532065B100983 STIFFENER BOEING747 747212B 1384886NM KEELBEAM BOX CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 INSPECTION TYPE:C FX AIR CONDITIONING BAY KEEL BEAM BOX LT EXTERNAL VERTICAL STIFFENER FOUND CRACKED AT BS 983 LBL 9" LOWER AREA, CRACK LENGTH 2". FX AIR CONDITIONING BAY KEEL BEAM BOX AT BS 983 LBL 9" VERTICAL STIFFENER REPLACED IAW SRM 51-10-01 PG 9. 2L74 4F A20WE 20060120000952006012000095NM 2006 1 20 ASAA0570030 120050630A5321453A261034 FLOOR PANEL BOEING737 737790 13844CNNM FS 727 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02644AS 30795 PAE - DURING CHECK, FOUND CORROSION ON RIGHT AND LEFT SIDES OF NR 1 FLOOR PANEL IN AFT CARGO BAY. REPAIRED IAW SRM 51-40-02. (M) 2L72 4F RTA16WE 20060120001082006012000108 2006 1 20 GTIA050284 420051207A3422 AHRS DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE COCKPIT MALFUNCTIONED A GTIAO OTHER O OTHER UKUNKNOWN 1 GL23835NK 53044 AHARS NR2 CIRCUIT BREAKER POPPED, PFD AND ND OUT. AIRCRAFT TAIL SWAP WITH 808NK. REMOVED AND REPLACED NR2 AHRU. OPS CHECK GOOD. (K) 2L72 4F4 FRTA6WE E9NE 20060120001102006012000110WP 2006 1 20 GTIA050282 120051121A5320 DOUBLER DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FLOOR CORRODED A GTIAK NONE O OTHER UKUNKNOWN 1 GL23802NK 53168 FWD SERVICE DOOR HAS CORROSION ON FLOOR WEB BETWEEN STA 1460 TO 218. REMOVED CORROSION FOUND TO BE OUT OF LIMITS, REMOVED DOUBLER AND FABRICATED NEW ONE, TREATED PRIMED AND INSTALLED REPAIR DOUBLER. (K) 2L72 4F4 FRTA6WE E9NE 20060120001122006012000112WP 2006 1 20 GTIA050280 120051119A5320 FLOOR SUPPORT DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE CORRODED A GTIAK NONE O OTHER UKUNKNOWN 1 GL23802NK 53168 FLOOR SUPPORT LBL 5, STA 195-200 HAS CORROSION ALONG LENGTH. REMOVED CORROSION AND FOUND ADDITIONAL CORROSION ON UNDERSIDE OF FLOOR SUPPORT TO BE OUT OF LIMITS, FABRICATED NEW SUPPORT, TREATED PRIMED AND INSTALLED NEW SUPPORT. (K) 2L72 4F4 FRTA6WE E9NE 20060120001142006012000114WP 2006 1 20 GTIA050279 120051119A5320 FLOOR SUPPORT DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE CORRODED A GTIAK NONE O OTHER UKUNKNOWN 1 GL23802NK 53168 FORE AND AFT FLOOR SUPPORTS AT STA 170-195 ON OB LT SEAT TRACK HAS SPOTS OF CORROSION ALONG LENGTH. REMOVED CORROSION ON SUPPORTS FOUND TO BE OUT OF LIMITS, FABRICATED NEW FLOOR SUPPORT ANGLE, TREATED PRIMED AND INSTALLED SUPPORT. (K) 2L72 4F4 FRTA6WE E9NE 20060120001162006012000116WP 2006 1 20 GTIA050277 120051116A3213 ANGLE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE STA 946 CRACKED A GTIAK NONE O OTHER UKUNKNOWN 1 GL23802NK 53168 ANGLE IS CRCKED IN LT MLG WHEEL WELL FWD DOOR JAMB STRUCTURE STA 946. REMOVED CRACKED ANGLE, FORMED NEW ANGLE, TREATED PRIMED AND INSTALLED REPAIR. (K) 2L72 4F4 FRTA6WE E9NE 20060120001182006012000118WP 2006 1 20 GTIA050274 120051213A5347 SEAT TRACK DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE CORRODED A GTIAK NONE O OTHER UKUNKNOWN 1 GL23802NK 53168 STA 1136, LT IB SEAT TRACK TANG DIMENSION BELOW 0.90. REMOVED DAMAGED AREA DRILLED NEW TRACK, TREATED, PRIMED AND INSTALLED SPLICE. (K) 2L72 4F4 FRTA6WE E9NE 20060120001252006012000125NM 2006 1 20 AMTA200501207 120051222A5320 FLOOR SUPPORT BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE FUSELAGE FLOOR TOOL DAMAGE A AMTAK NONE O OTHER ININSP/MAINT 1 GL11517AT 27973 AFT PIT 3 EA DRILL MARKS, ONE WHICH IS CRACKED THRU FLOOR SUPPORT, STA 1317 TO 1320, RBL 11. REMOVED DAMAGED AFT PIT FLOOR SUPPORT FROM SAT 1342-1309 RBL 11, IAW SRM 51-70-12-00, FIG 1, TREATED AND PRIMED AND INSTALLED REPAIR IAW SRM. (K) 2L72 4F4 FRTA2NM E12EU 20060123000012006012300001NM 2006 1 23 UPS06M45947 120051204A5313 LONGERON DOUG MD11 MD11F 3023600NM BS 2007 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01282UP 48452 INSPECTION TYPE:C AFT CABIN, CORROSION ON LONGERON 27 AT STA 2007 X=27.5 CORROSION ON LONG 27 T-CHORD AT STA 2007 X=27.50. REMOVED PER SRM 51-21- 01V2.R37 AND FOUND OUT OF LIMIT PER SRM 53-40-00V1 FIG7 R.37.ORI THK=0.12 5" MAT REMOVED 0.040".STA 2007 BULKHEAD T-CHORD REMOVED PER SRM 51-31-0 1V.2R.37. T-CHORD FAB PER DWG NJC 6040 USING MAT S2924410. NEW T-CHORD INSTALLED PER SRM 51-31-01 V2R.37, FOUND SATIS. 2L73 4F RTA22WE 20060123000032006012300003NM 2006 1 23 ASAA0570032 120050718A5320146A75021 FLOOR SUPPORT BOEING737 737790 13844CNNM FS 727-847 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02613AS 30163 PAE - DURING C-CHECK, FOUND CORROSION ON LEFT FLOOR TO SIDEWALL SUPPORT AT BS 727-847. REPAIRED IAW SRM 53-00-53. (M) 2L72 4F RTA16WE 20060123000222006012300022NM 2006 1 23 ASAA0570025 120050609A5321141A12010 FLOOR PANEL BOEING737 737790 13844CNNM FS 250 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02612AS 30162 PAE - DURING C-CHECK, FOUND FLOOR DENTED IN COCKPIT. REPAIRED IAW SRM 53-00-01. (M) 2L72 4F RTA16WE 20060123000262006012300026NM 2006 1 23 ASAA0510340 120051019A5340655073432 ATTACH ANGLE BOEING737 737298C 1384490NM FS 685 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02745AS 20794 YXX - EXFOLIATED ANGLE ON LOWER SIDE OF PRESSURE DENT APPROX AT BS 685, RBL 58 INBOARD AND ADJACENT TO FORWARD RIGHT MLG SIDE STRUT SUPPORT FITTING AT RT WHEEL WELL BAY. CORROSION REPAIRED IAW B737-200 SRM 51-20-1 AND 51-30-5. (M) 2L72 4F RTA16WE 20060123000292006012300029NM 2006 1 23 ASAA0570034 120050718A5320146A750501 INTERCOSTAL BOEING737 737790 13844CNNM FS 727A-727B BENT A ASAAK NONE O OTHER ININSP/MAINT 1 NM02613AS 30163 PAE - DURING C-CHECK, FOUND BENT INTERCOSTAL AT BS 727A-727B. REPAIRED IAW SRM 53-00-00. (M) 2L72 4F RTA16WE 20060123000362006012300036WP 2006 1 23 ABXA060028 120051101A5315 FLOORBEAM DOUG DC8 DC863F 302198FWP BS 55 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 MAIN CARGO, STA 55, LEFT BUTT LINE 20, CORROSION ON UPPER FLANGE FLOORBEAM. REMOVED 3.5 X .75 INCH SECTION OF UPPER FLANGE FLOORBEAM. ACCOMPLISHED FLOORBEAM REPAIR IAW SSRM DWG K04881. 2L74 4F 4A25 20060123000392006012300039WP 2006 1 23 ABXA060033 120051229A5330 DOUBLER DOUG DC8 DC863F 302198FWP BS 781-798 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 CORROSION ON BELLY SKIN DOUBLER IN 4 AREAS BETWEEN STA 781 AND STA 798, LEFT BUTT LINE 4 TO LEFT BUTT LINE 10. REMOVED CORROSION ON BELLY SKIN DOUBLER IAW DC8 SRM 51-1-8. THREE AREAS WITHIN LIMITS IAW DC8 SRM 53-02. REMAINING AREA OUT OF LIMITS. ACCOMPLISHED REPAIR IAW REA D853-52923. 2L74 4F 4A25 20060123001062006012300106NE 2006 1 23 ARWA20050304 220050302A7200 COMPRESSOR DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE NR 2 ENGINE STALLED A ARWAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SO19661AV 45969 NR 2 ENGINE COMPRESSOR STALL ON TAKEOFF ABORT AT 30 KNOTS. INSPECTED INLET AND EXHAUST AREA OF ENGINE NR 2; FOUND -PAPER FOD-. REMOVED SMALL RESIDUE IN ACCORDANCE WITH PRATT & WHITNEY 72-00; OPERATIONAL CHECK ON RUN-UP IN ACCORDANCE WITH M/M 71-00. NO COMPRESSOR STALL NOTED, ALL PARAMETERS FOUND NORMAL. 2L74 4F4 F 4A25 1E8 20060123002232006012300223NM 2006 1 23 GAIA05040OP 120051222A7900 OIL FILTER BOEING727 727224 1384076NM PWA JT8 JT8D9A 52048NE NR 3 ENG BYPASSING A GAIAE ENGINE SHUTDOWN EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 SW0769735 20664 DURING CRUISE, DURING FLIGHT VIBRATION AND NOISE FOLLOWED BY OIL FILTER BYPASS LIGHT ON NR 3 ENGINE. NR 3 EINGINE SHUTDOWN AND ENGINE WINDMILLING PROCEDURE FOLLOWED (OIL FILTER BYPASS LIGHT WENT OUT BELOW 25 PERCENT, N2) NOTE: ENGINE WINDMILLED FOR 38 MIN AT 20 PSI. FLIGHT CONTINUED, WHERE LANDING WAS MADE WITHOUT INCIDENT. (K) 2L73 4F4 F A3WE E2EA 20060123002242006012300224NM 2006 1 23 GAIA05039OP 120051222A79007578678 FILTER BOEING727 727224 1384076NM PWA JT8 JT8D9A 52048NE NR 3 ENGINE BYPASSING A GAIAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0769735 20664 DURING CLIMB, OIL FILTER BYPASS LIGHT ILLUMINATED. RETARDING THROTTLE DID NOT EXTINGUISH. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN IAW ABNORMAL PORCEDURES. NOTE: THE ENGINE WAS WINDMILLING FOR ABOUT 15-20 MIN AND OIL PRESSURE WAS ABOUT 20-25 PSI. FLIGHT RETURNED TO MSP WHERE A LANDING WAS MADE WITHOUT INCIDENT. INSPECTED MAIN OIL FILTER ON NR 3 ENGINE, FOUND NO CONTAMINATION. INSTALLED NEW OIL FILTER. RAN ENGINE. RE-INSPECTED OIL FILTER NO CONTAMINATION NOTED. RE-INSTALLED NEW FILTER. RAN ENGINE. NO OIL FILTER BYPASS LIGHT NOTED. OK FOR CONTINUED SERVICE. RAN ENGINE NO LEAKS NOTED. RESERVICED OIL TANK. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L73 4F4 F A3WE E2EA 20060123002312006012300231CE 2006 1 23 KC82006F00000 120051227A3397ALCUAS6845470S WIRE LEAR 35 36A 5170603CE GARRTTTFE731TFE7312 01518WP GLARESHIELD ARCED E KC8AH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL2371CK 035 PILOT REPORTED SMOKE IN THE COCKPIT. HE TURNED OF THE GLARESHIELD LIGHTING AND THE SMOKE STOPPED. FOUND GLARESHIELD FLORESCENT TUBE LEAD WIRES ARCING TO GROUND. REPLACED FLORESCENT TUBE WITH NEW FLORESCENT TUBE AND INSULTED LEAD WIRE ENDS. OPERATIONAL CHECK SATISFACTORY. ALL WORK PERFORMED IAW THE MM. (K) 2L72 4F4 F A10CE E6WE 20060123002362006012300236NM 2006 1 23 AWXA200600014 120051227A5210 DOOR ACTUATOR AIRBUSA319 A319132 3930340NM IAE V2500 V2500A1 NE FUSELAGE OUT OF ADJUST A AWXAK NONE O OTHER ININSP/MAINT 1 WP28814AW 1281 DURING BC4 CHECK DISCOVERED THE R2 DOOR EMERGENCY ASSIST MECH DIMENSION A WAS .4125 INCH, WHICH IS OUT OF LIMITS IAW TASK CARD I1C52307. MAINTENANCE ADJUSTED THE R2 DOOR EMERGENCY ASSIST MECH TO A NEW DIMENSION OF .291 INCHES, WHICH IS IN LIMITS IAW MM 52-13-14. 2L72 4F4 FRTA28NM E311NE 20060120000532006012000053NM 2006 1 20 ASAA0570055 120050816A5340149A761413 FITTING BOEING737 737790 13844CNNM FS 722-729 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02614AS 30343 PAE - DURING C-CHECK, FOUND LEFT WHEEL WELL CUTOUT AFT WEB CORRODED. REPAIRED IAW SRM 51-40-02. (M) 2L72 4F RTA16WE 20060120001042006012000104CE 2006 1 20 6252004N8005Y 120050625A2130 CABIN PRESSURE LEAR 25 25B 5170511CE GE CJ610 CJ6106 30006NE FUSELAGE MALFUNCTIONED E CEDAA UNSCHED LANDING O OTHER CRCRUISE 1 SW058005Y 121 241C287A WHILE ENROUTE, AT FLIGHT LEVEL 410 THE CABIN ALTITUDE EXCEEDED 10000 FT, THE FLIGHT CREW FOLLOWED THE CHECKLIST PROCEDURES AND DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE HAS NOT YET INSPECTED THE AIRCRAFT TO DETERMINE THE SPECIFIC PROBLEM. I WILL NOTIFY YOU OF THE FINDINGS AT A LATER DATE. (K) 2L72 4J4 J A10CE 1E16 20060120001052006012000105NE 2006 1 20 GTIA050286 220051210A7320 BLEED VALVE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE NR1 ENGINE MALFUNCTIONED A GTIAO OTHER R PARTIAL RPM/PWR LOSS UKUNKNOWN 1 GL23834NK 49847 LT ENGINE N2 DROPS BELOW 45 PERCENT WHEN LOAD APPLIED. REPLACED A/C WITH 832NK ON LINE. REMOVED NR1 ENGINE FUEL CONTROL. OPS AND LEAK CHECK GOOD. REMOVED AND REPLACED START BLEED CONTROL VALVE, PERFORMED IDLE CHECK, ENGINE ACCELERATION CHECK. OPS CHECK GOOD. (K) 2L72 4F4 FRTA6WE E9NE 20060120001092006012000109WP 2006 1 20 GTIA050283 120051130A3220 LANDING GEAR DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE NLG VIBRATION A GTIAO OTHER E VIBRATION/BUFFET LDLANDING 1 GL23814NK 49619 AC SHIMMY VERY EXTREME ON LANDING ROLL OUT WHEN BRAKING BETWEEN 60-65 KTS, AC TAIL SWAP WITH 832NK. BLED ALL 4 BRAKES, CHECKED TORQUE VALUES OF ALL 4 MAIN TIRE AXLE NUTS. ALL CHECKED GOOD. NOTE: NR2 BRAKE AFT BLEEDER EMITTING AIR BUBBLES, PURGED AIR FROM SYSTEM. PERFORMED HIGHT DRAG/SIDE LOADS OR UNUSUAL GROUND HANDLING CONDITIONS, NO DEFECTS NOTED. CHECKED NLG TORQUE LINKS UPPER AND LOWER BUSHINGS FOR WEAR-FOUND WITHIN LIMITS. PERFORMED ANTI-SKID SYSTEM MAINT PRACTICES, OPS CHECK GOOD. INSPECTED NLG FOUND FLUID LEVEL LOW AND SCHRADER VALVE DEFECTIVE, SERVICED STRUT AND INSTALLED NEW VALVE, LEAK AND OPS CHECK GOOD. (K) 2L72 4F4 FRTA6WE E9NE 20060120001112006012000111WP 2006 1 20 GTIA050281 120051119A5320 DIAPHRAGM DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE CORRODED A GTIAK NONE O OTHER UKUNKNOWN 1 GL23802NK 53168 FWD GALLEY AFT CORNER IB HAS A 6 INCH HOLE CORRODED THROUGH SUBFLOOR WEB. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED DIAPHRAGM AND FABRICATED NEW DIAPHRAGM, TREATED PRIMED AND INSTALLED. (K) 2L72 4F4 FRTA6WE E9NE 20060120001152006012000115WP 2006 1 20 GTIA050278 120051119A5320 FLOOR SUPPORT DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE CORRODED A GTIAK NONE O OTHER UKUNKNOWN 1 GL23802NK 53168 FLOOR SUPPORT AT STA 198 BETWEEN LT SEAT TRACKS IS CORRODED. REMOVED FLOOR SUPPORT, FABRICATED NEW SUPPORT TREATED AND PRIMED, INSTALLED REPAIR. (K) 2L72 4F4 FRTA6WE E9NE 20060120001172006012000117WP 2006 1 20 GTIA050275 120051121A5347 SEAT TRACK DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE CORRODED A GTIAK NONE O OTHER UKUNKNOWN 1 GL23802NK 53168 RT OB SEAT TRACK FS 493 BOTTOM OF TRACK OUT OF LIMITS, CORROSION. REMOVED CORRODED SEAT TRACK SECTION, DRILLED NEW SEAT TRACK, FABRICATED SPLICE AND PLATE, TREATED, PRIMED AND INSTALLED REPAIR. (K) 2L72 4F4 FRTA6WE E9NE 20060120001202006012000120WP 2006 1 20 GTIA050271 120051115A5610 WINDSHIELD DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE COCKPIT LEAKING A GTIAK NONE O OTHER UKUNKNOWN 1 GL23829NK 49931 FRONT CENTER WINDSHIELD LEAKING WATER, AIRCRAFT TAIL SWAP WITH N808NK. WINDSHIELD SEALANT FOUND DELAPIDATED, RE SEALED WINDSHIELD, LEAK CHECKS GOOD. (K) 2L72 4F4 F A6WE E9NE 20060120001222006012000122WP 2006 1 20 GTIA050264 120051017A5311 FRAME DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE FUSELAGE CRACKED A GTIAK NONE O OTHER UKUNKNOWN 1 GL23804NK 49104 FRAME CANT 1463 AT APPROX LONGERON 19 AND 20 ON AC RT HAS CRACKED WEBBING. INSTALLED PERMANENT REPAIR ON CANTED FRAME FS 1463 BETWEEN R18L AND R25L, IAW EA REV ORIGINAL HAS BEEN ACCOMPLISHED. (K) 2L72 4F4 F A6WE E9NE 20060120001242006012000124WP 2006 1 20 GTIA050227 120050810A5240 LOCK TAB DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE L2 DOOR STOP MISINSTALLED A GTIAK NONE O OTHER UKUNKNOWN 1 GL23832NK 49618 L2 DOOR STOP ADJUSTERS LOOSE ON ENTIRE DOOR. LOCK TABS IMPROPERLY SECURED. REMOVED AND REPLACED ALL LOCK TABS AND ADJUSTED FAIRING IAW MM. OPS AND LEAK CHECKS GOOD. (K) 2L72 4F4 FRTA6WE E9NE 20060120001262006012000126NM 2006 1 20 AMTA200501206 120051221A3397 WIRE BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE FUSELAGE DISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11522AT 29330 EMERGENCY FLOOR TRACK LIGHTING FROM ROW 25 TO RT AFT LAV, INOPERATIVE. RECONNECTED WIRES TO LIGHT ASSY AT ROW 25. OPS CHECK GOOD. (K) 2L72 4F4 FRTA2NM E12EU 20060123000182006012300018WP 2006 1 23 UPS06845962 120051230A5313 LONGERON DOUG DC8 DC871F 302199DWP L24R BS 880 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE:C3 CRACK IN LOWER RADIUS OF L24R, RT W/W STA 880. STOP DRILLED CRACK IAW SRM 53-02-02, FABRICATED AND INSTALLED REPAIR ANGLES -23, AND -24 IAW DPS 7.00-1 SRM 53-02-02,51-3-2 51-1-8, AND SRM 51-1-20D. 2L74 4F RT4A25 20060123000242006012300024NM 2006 1 23 ASAA0570018 120050418A5347 SEAT TRACK BOEING737 737790 13844CNNM FS 240 WORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM02607AS 29751 PAE - DURING CHECK FOUND FLIGHT DECK F/O`S INBOARD AFT SEAT TRACK IS WORN. REPAIRED IAW MM 25-11-11. (M) 2L72 4F RTA16WE 20060123001292006012300129NM 2006 1 23 UPS06445971 120051229A5312141U10878 PRESSURE BLKHD BOEING747 747212B 1384886NM NLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 INSPECTION TYPE:C NOSE W/W BS 400 BULKHEAD PRESSURE PANEL FOUND CRACKED, CRACK LENGTH 1/4". NOSE W/W BS 400 B/H PRESSURE PANEL REPLACED AS PER SRM 51-10-01 PAGE 9 AND INSTALLED AS PER BOEING DWG NR 624U0005 SHT 1 AND SHT 9. 2L74 4F A20WE 20060123002222006012300222NM 2006 1 23 GAIA05037OP 120051215A3260H1010153 DOWNLOCK SWITCH BOEING727 7272J0 138407ENM PWA JT8 JT8D15 52051NE NLG INOPERATIVE A GAIAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 SW07281KH 21105 DURING APPROACH, ON SHORT FINAL, NOSE GEAR LIGHT CHANGED FROM GREEN TO RED, GOT HORN. CYCLED GEAR TWICE TO NO AVAIL. VISUAL INSPECTION THROUGH PORT INDICATED DOWN AND LOCKED. LANDING AND TAXI IN UNEVENTFUL. CLEANED AND RESEATED DOWNLOCK SWITCH AND (DOWNLOCK) SWITCH CONNECTOR. ALL GROUND OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (K) 2L73 4F4 FRTA3WE E2EA 20060123002252006012300225CE 2006 1 23 ROS2006F00000 120051020A529723115036 WIRE LEAR 35 35A 5170602CE GARRTTTFE731TFE73122B 01518WP FS STA 245.9 SHORTED E ROSAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SW07135DE4546 667 FLIGHT CREW REPORTED THE PASSENGER/CREW DOOR LOCK ACTUATOR WAS INOPERATIVE; DOOR ACTUATOR CB WAS OPEN. CB WAS CLOSED, DOOR OPERATION WAS NORMAL. DURING LAST STOP OF TRIP, WHILE CLOSING DOOR CB OPENED AGAIN AND DOOR WARNING ANNUNCIATOR LIGHT ILLUMINATED. MAINT FOUND PLASTIC FLEX TUBE PN 2311503-6 WHICH ENCLOSES LWR DOOR WIRING AT AIRFRAME SIDE HAD BROKEN AT POINT IT SLIPPED OVER PN321503-12 DURING DOOR OPERATION. EVENTUALLY, WIRE INSULATION WORE AWAY AND WIRES SHORTED TO METAL CONDUIT TUBE. WIRES THAT WERE DAMAGED ARE M1B20, M4A20M, AND W58B22. AC IS EQUIPPED WITH OPTION 36 IN DOOR, HOWEVER 24 INCH DOOR INSTALL IS SIMILAR. DAMAGED WIRES WERE LOCATED UNDER THE CABIN FLOOR IN AREA DIFFICULT TO INSPECT. (K)2L72 4F4 F A10CE E6WE 20060124000582006012400058EA 2006 1 24 ASOA051056 120051204A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 349-985 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27716EV 10084 DURING A C-CHECK IN MCN, THE SEAT TRACKS AT FS 349-985, LBL 9, WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS AT FS 349-985, LBL 9, IAW CRJ 700 AMM 53-00-49. (M) 2L72 4F RTA21EA 20060124000592006012400059EA 2006 1 24 ASOA051165 120051231A5210CC67038601965 STRUCTURE CNDAIRCL600 CL6002C10 1390015EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27713EV 10081 DURING A C-CHECK IN MCN, THE AFT SIDE OF THE PASSENGER DOOR, BELOW THE TOP STEP, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE AFT SIDE OF THE PASSENGER DOOR, BELOW THE TOP STEP, IAW BOMBARDIER REO 670-52-11-154. (M) 2L72 4F RTA21EA 20060124000642006012400064EA 2006 1 24 ASOA051053 120051224A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FS 280 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27882AS 7503 DURING A C-CHECK IN MCN, THE INTERCOSTAL AT FS 280, RBL 9, AT THE FLOOR SUPPORT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTAL, AT FS 280, RBL 9 FLOOR SUPPORT IAW BOMBARDIER REO 601R-53-11-171. (M) 2L72 4F RTA21EA 20060124000662006012400066EA 2006 1 24 ASOA051057 120051204A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27716EV 10084 DURING A C-CHECK IN MCN, THE LEFT SIDE WALL SEAT TRACKS, FROM FS 349 TO FS 985, WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED CORROSION FROM THE LEFT SIDE WALL SEAT TRACKS, FROM FS 349 TO 985, IAW BOMBARDIER REO 670-53-00-013. REMOVED AND REPLACED THE LEFT SIDE WALL SEAT TRACKS FROM FS 784 THROUGH FS 861 IAW BOMBARDIER REO 670-53-00-013. (M) 2L72 4F RTA21EA 20060124001052006012400105EA 2006 1 24 ASOA051096 120051215A5320 PLATE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 DURING A C-CHECK IN MCN, THE PASSENGER DOOR AFT ANCHOR FITTING SERRATED PLATE WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACED THE PASSENGER DOOR AFT ANCHOR FITTING SERRATED PLATE. (M) 2L72 4F RTA21EA 20060124001062006012400106EA 2006 1 24 ASOA051098 120051215A5210 STRUCTURE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 DURING A C-CHECK IN MCN, THE PASSENGER DOOR WILL WAS FOUND TO BE CORRODED. (M) 2L72 4F RTA21EA 20060124001072006012400107EA 2006 1 24 ASOA051102 120051216A5310CORRODED BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 DURING A C-CHECK IN MCN, THE LEFT SIDE STATION 349 TRANSVERSE BEAM, UPPER SURFACE AT THE PASSENGER DOOR, WAS FOUND TO BE CORRODED BEYOND LIMITS. (M) 2L72 4F RTA21EA 20060124001082006012400108EA 2006 1 24 ASOA051101 120051215A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA BS 484 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 DURING A C-CHECK IN MCN, THE INBOARD AND OUTBOARD FS 484 CLIPS WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE INBOARD AND OUTBOARD FS 484 CLIPS IAW BOMBARDIER REO 601R-53-41-059. (M) 2L72 4F RTA21EA 20060124001092006012400109EA 2006 1 24 ASOA051104 120051216A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA BS 640 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27849AS 7347 DURING A HANGAR INSPECTION IN BTR, THE RIGHT SIDE FS 640, BETWEEN STRINGER 9 AND 11, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REPAIR THE RIGHT SIDE FS 640, BETWEEN STRINGER 9 AND 11, IAW BOMBARDIER REO 601R-53-61-506. (M) 2L72 4F RTA21EA 20060124001102006012400110EA 2006 1 24 ASOA051103 120051216A5330 DOUBLER CNDAIRCL600 CL6002B19 1900309EA BS 640 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27849AS 7347 DURING A HANGAR INSPECTION IN BTR, THE RIGHT SIDE BONDED SKIN DOUBLER, T STATION 640, BETWEEN STRINGER 9 AND 11, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REPAIR THE RIGHT SIDE BONDED SKIN DOUBER, STATION 640, BETWEEN STRINGER 9 AND 11, IAW BOMBARDIER REO 601R-53-61-506. (M) 2L72 4F RTA21EA 20060124001112006012400111EA 2006 1 24 ASOA051106 120051216A3350OL3071BPEGPL LAMP CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27752EV 10166 DURING A HANGAR INSPECTION IN BTR, THE CEILING EMERGENCY LIGHT, AT ROW 2, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE CEILING EMERGENCY LIGHT, AT ROW 2. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060124001122006012400112EA 2006 1 24 ASOA051105 120051216A3397487190 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCONNECTED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27860AS 7433 DURING A GROUND INSPECTION IN CVG, THE EMERGENCY FLOOR STRIP LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE RECONNECTED THE CONNECTORS TO THE EMERGENCY FLOOR STRIP LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060124001132006012400113EA 2006 1 24 ASOA051099 120051215A5344600314457 HINGE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 DURING A C-CHECK IN MCN, THE PASSENGER DOOR UPPER STEP HINGE WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACED THE PASSENGER DOOR UPPER STEP HINGE. (M) 2L72 4F RTA21EA 20060124001142006012400114EA 2006 1 24 ASOA051100 120051215A5280 STRUCTURE CNDAIRCL600 CL6002B19 1900309EA NLG DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 DURING A C-CHECK IN MCN, THE LEFT SIDE OF THE NOSE LANDING GEAR CUTOUT RADIUS WAS FOUND TO BE CRACKED BEYOND LIMITS. (M) 2L72 4F RTA21EA 20060124001152006012400115EA 2006 1 24 ASOA051107 120051216A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27880AS 7606 DURING A HANGAR INSPECTION IN BTR, THE NR 2 EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE NR 2 EXTERIOR EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060124001162006012400116EA 2006 1 24 ASOA051097 120051215A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FS 718 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 DURING A C-CHECK IN MCN, THE RIGHT SIDE FS 718 FRAME WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REMOVED AND REPLACED THE RIGHT SIDE FS 718 FRAME. (M) 2L72 4F RTA21EA 20060124001212006012400121NM 2006 1 24 AWXA200600015 120051228A3510 REGULATOR BOEING737 7373Y0 1384671NM CFMINTCFM56 CFM563B2 13802EU OXYGEN MASK STUCK A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 06514 23684 EMERGENCY EQUIPMENT, DURING C 16 CHECK DISCOVERED CAPTAIN'S OXYGEN MASK DEMAND REGULATOR STUCK IN EMERGENCY POSITION. MAINTENANCE REMOVED AND REPLACED THE O2 MASK IAW TASK CARD R1B35001. OPERATIONAL CHECKS WERE GOOD. VENDOR TEAR DOWN DOES NOT CONFIRM FAULT. VENDOR REPORTED THAT THE REGULATOR WAS NOT STUCK IN THE EMERGENCY POSITION AND THAT THE ONLY DISCREPANCY WAS THE FACEMASK LENS WAS CLOUDY. LENS WAS CLEANED AND UNIT TESTED GOOD IAW ATP 846114-TP AND ENGINERING SPESPECIFICATIONS 174660-N5 REV. B. 2L72 4F4 FRTA16WE E21EU 20060124001272006012400127EU 2006 1 24 O2G2006F00001 120051215A2131219922 CONTROLLER ISRAELGALAXYGALAXY 4500307EU CABIN PRESSURE FAILED E O2GAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NE0348GX 017 AT FL370 AUTO PRESSURIZATION FAILED IN AUTO MODE. CAPTAIN DEPLOYED MASK AND SWITCHED TO MANUAL MODE AND RECOVERED CABIN ALTITUDE. REMOVED AND REPLACED PRESSURE CONTROLLER. (K) 2L72 4F RTA53NM 20060124001322006012400132CE 2006 1 24 POS2006F00000 120051117A3230672EN51 UPLOCK SWITCH BEECH 100 100BEECH 1152916CE PWA PT6 PT6A60A 52043NE MLG OUT OF ADJUST E POSAO OTHER O OTHER NRNOT REPORTED 1 EA03100KA8425 B11 ON FLIGHT, ON RETRACTING THE LANDING GEAR THE FLIGHT CREW NOTICED THAT THE LANDING GEAR HANDLE STAYED (RED) INDICATING THE LANDING GEAR WAS NOT UP AND STOWED. THE FLIGHT CREW LOWERED THE LANDING GEAR. THE LANDING GEAR WENT DOWN AND GAVE A SAFE DOWN AND LOCKED INDICATION. THE FLIGHT CREW DIVERTED, WHERE THEY LANDED WITHOUT INCIDENT. MAINTENANCE FOUND BY INSP OF THE LANDING GEAR SYSTEM THAT THE CAUSE OF THE GEAR IN TRANSIT LIGHT STAYING ON WAS A SHIFT IN THE UP LIMIT MOTOR SWITCH, NOT ALLOWING FULL TRAVEL IN THE UP POSITION. (K) 1L72 3T4 T A14CE E4EA 20060124001332006012400133GL 2006 1 24 ALG2006F00002 220051218A7200 ENGINE BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL OIL CONSUMPTION E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03198H 3647 DURING FLIGHT IT WAS NOTED THAT THE ENGINE OIL PRESSURE INDICATOR WAS FLUCTUATING. CONTINUED FLIGHT AND OIL PRESSURE AND TEMPERATURE REMAINED WITHIN LIMITS. THE ENGINE WAS REMOVED DO TO OIL CONSUMPTION. (K) 1G71 3U3 U H2SW E4CE 20060124001362006012400136NM 2006 1 24 AMTA200501176 120051218A5310 BEAM BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE FUSELAGE CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11517AT 27973 REMOVED CORROSION FROM BEAM IAW CPM 20-40-00, FOUND TO BE OUT OF LIMITS IAW 757, SRM 53-60-13. REMOVED AND REPLACED BEAM IAW SRM 51-40-02 OVER 50 PERCENT MATERIAL LOSS. (K) 2L72 4F4 FRTA2NM E12EU 20060124001372006012400137NM 2006 1 24 AMTA200501169 120051217A5320 SILL BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE FUSELAGE CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11517AT 27973 FWD C COMPT DOOR CUTOUT SILL AREA NET TIEDOWN FITTING SUPPORT CORRODED AT AFT POSITION. REMOVED CORRODED FITTING INSTALLED NEW FITTING PN 69-45555-9 IAW SRM 51-40-02 AND REINSTALLED FLOOR PANEL. (K) 2L72 4F4 FRTA2NM E12EU 20060124001392006012400139SW 2006 1 24 ALG2006F00003 120051222A6320407040006107 TRANSMISSION BELL 407 407 1182206SW ALLSN 250C 250C47B GL MAIN ROTOR MAKING METAL E ALGAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW03406AL2339 53481 DURING TAKEOFF THE TRANSMISSION CHIP LIGHT ILLUMINATED. FOUND 2 FLAKES ON LOWER CHIP PLUG. TRANSMISSION REMOVED FOR METAL. (K) 1G71 3U3 UO H2SW E1GL 20060124001422006012400142CE 2006 1 24 DXTA200501167 120051221A3297 WIRE CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE RELAY BROKEN E DXTAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07314QS 5600441 WHILE AIRCRAFT WAS STOPPED AND RT SIDE BRAKE PRESSED POWER LO PRESSURE AND ANTI-SKID ANNUNCIATORS ILLUMINATED. INITIALLY HAD SOME BRAKE PRESSURE. TAXIED CLEAR OF ACTIVE TAXIWAY THEN LOST TOTAL PRESSURE BOTH SIDES NORMAL BRAKES PEDALS WENT TO THE FLOOR SOFT. USED EMER. BRAKES FOR 3 SMALL PULLS TO STOP AIRCRAFT. REMOVED AND REPLACED ANTI-SKID MOTOR RELAY. ALSO FOUND A BROKEN WIRE ON NR2 WHEEL SPEED TRANSDUCER. REPAIRED WIRE, BLED ANTI-SKID HYDRAULICS SYSTEM. TAXI CHECKED GOOD. IAW CE 560 MM 32-42-00 AND CE 560 WIRING MANUAL 20-10-06. 2L72 4F4 FRTA22CE E25EA 20060124001442006012400144CE 2006 1 24 DXTA200501168 120051221A3241M83536 RELAY CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE ANTI SKID SYS INOPERATIVE E DXTAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07311QS 5600311 ON TAXI INTO FBO, PARTIAL BRAKE PRESSURE LOST WITH PWR BRAKE LOW PRESSURE AND ANTI SKID INOP ANNUCIATOR LIGHTS ON. TRIED TURNING ANTI-SKID OFF, AND ALL BRAKE PRESSURE LOST. TURNED ANTI-SKID ON RECLAIMED PARTIAL PRESSURE. TROUBLESHOT A/S BRAKE SYS, REPLACED BRAKE CONTROL RELAY, BROKE METER RELAY, BRAKE LOW PRESS SWT FOUND FLUID IN LOWER BRAKE VENT LINE, INSP LT AND RT BRAKE SHUTTLE VLV'S, FOUND FLUID IN BRAKE LINES, RESEALED LT AND RT BRAKE SHUTTLE VLV'S, REINSTALLED, REINSTALLED BRAKE LINES, BLED A/S BRAKE SYSTEM, OPS CHK/LK CHKS GOOD IAW M/M CH'S 12-12-02, 32-42-00, AND CMM CH 32-46-43 CWRRO61D. 2L72 4F4 FRTA22CE E25EA 20060124001462006012400146CE 2006 1 24 DXTA200501166 120051220A2170 COALESCER BAG RAYTHNDH125 HAWKER800XP 7150012CE GARRTTTFE731TFE7315BR WP CABIN AIR ODOR E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL07833QS 258433 REPEAT WRITE UP, SHORTLY AFTER TAKEOFF WE SMELLED SMOKE FUMES AND BAGGAGE FIRE/SMOKE LIGHT CAME ON. ALL BAGGAGE COMPARTMENT LIGHTS WERE VERIFIED OFF PRIOR TO DEPARTURE. REMOVED WATER SEPARATOR SEAL, CHECKED FOR CLEANLINESS. CLEANED AND REINSTALLED SOCK. RAN BOTH ENGINES TO POWER FOR 30 MINS. PRESSURIZED CABIN TO 9 PSID. OPS CHECKED AND LEAK CHECKED WATER SEPARATOR SOCK. ALL OPS CHECK GOOD, NO DEFECTS NOTED. BAGGAGE FLIGHTS NEVER ILLUMINATED. ALL WORK DONE IAW MM CHAPTERS 33-02-00, 21-10-95 AND 71-00-00. 2L72 4F4 FRTA3EU E6WE 20060124001472006012400147NM 2006 1 24 AMTA200501175 120051218A5320 FLOOR SUPPORT BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE BS 1661-1681 CRACKED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11517AT 27973 IN THE AFT GALLEY AT STA 1661 TO 1681, BL 10 INCH, RT AT FLOOR SUPPORT IS CRACKED ON ITS UPPER FLANGE AT 3 FASTENER HOLE. REMOVED FLOOR SUPPORT FAB NEW SUPPORT FROM 2024-T3 .032 PO NR 804693 ALODINED AND PRIMED AND INSTALLED FLOOR SUPPORT IAW SRM. (K) 2L72 4F4 FRTA2NM E12EU 20060124001512006012400151NM 2006 1 24 AMTA200501177 120051218A5320 FLOOR SUPPORT BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE BS 1664-1681 CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11517AT 27973 IN THE AFT GALLEY AREA STA 1664 TO STA 1681.8 BL0 THERE IS CORROSION ON UPPER SURFACE FLOOR SUPPORT BEAM. REMOVED CORROSION FROM FLOOR SUPPORT BEAM AT STA 1664-1681, BL0 SRM 51-10-02 ORIG THICK .050 REMAINING THICK IS .016 OUT OF LIMITS 53-60-51-1A. REMOVED AND REPLACED FLOOR SUPPORT BEAM 51-40-02. (K) 2L72 4F4 FRTA2NM E12EU 20060124001522006012400152NM 2006 1 24 AMTA200501186 120051218A5315 FLOORBEAM BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE BS 365 CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11517AT 27973 CORROSION ON CABIN FLOOR STRUCTURE STA 365, RBL 0 TO RBL 50. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS ORG MTL .125 LOW READING, .079 REPAIRED SECTION OF FLOORBEAM TEE CAP IAW 53-00-51-2 R. (K) 2L72 4F4 FRTA2NM E12EU 20060124001532006012400153NM 2006 1 24 AMTA200501173 120051217A5320 INTERCOSTAL BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE BS 1661-1681 CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11517AT 27973 CORROSION ON UPPER SURFACE OF INTERCOSTAL AROUND FASTENER HOLES AT THE R-4 DOOR SILL STA 1681 TO 1661. REMOVED CORROSION FROM INTERCOSTAL AT R-4 DOOR SILL IAW SRM 51-20-01, ORIG THICKNESS .071 INCH, REMAINING .041 INCHES OUT OF LIMITS IAW SRM; REMOVED AND REPLACED INTERCOSTAL IAW SRM AT STA 1661-1681. (K) 2L72 4F4 FRTA2NM E12EU 20060124001542006012400154NM 2006 1 24 AMTA200501179 120051218A5315 FLOORBEAM BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE BS 1640 CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11517AT 27973 IN THE AFT GALLEY 1640 BL0 TO 60, THERE IS CORROSION AROUND FASTENER HOLES ON THE TOP AND BOTTOM OF THE UPPER TEE CAP OF THE FLOORBEAM. REMOVED CORROSION FROM FLOOR SUPPORT TEE CAP BL0 TO BL56R STA 1640 FOUND AREA WITHIN LIMIT 51-10-02 AND 53-60-51. THE LAST HOLE FOR FLOORBOARD OUT OF LIMIT REO L00986. REPAIR TEE CAP IAW ENG. (K) 2L72 4F4 FRTA2NM E12EU 20060124001552006012400155WP 2006 1 24 ASMF200512019 120051225A278130288DC19 ANNUNCIATOR DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE COCKPIT FAILED W ASMFD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SW23501AM 49188 AIRCRAFT RETURNED TO PLATFORM DURING TAXING THE SLAT DISAGREE LIGHT NOT TURNED ON. DURING MAINTENANCE REVISION, THE SLAT DISAGREE LIGHT WAS FAILING INTERMITTENTLY. THE PSEU BITE WAS PERFORMED, THE SLATS SENSORS A, B, C, D WERE CLEANED, THE COCKPIT DISAGREE LIGHT WAS READJUSTED AND THE FLAP SLAT OPERATIONAL TEST WAS PERFORMED IAW MM 27-80-06, MM 32-60-04 AND MM 27-80-00 RESPECTIVELY, BEING CORRECT. DURING OVERNIGHT CHECK, THE ANNUNCIATOR ASSY L2-641 WAS REPLACED IAW WDM 27-81-00 AND THE SLAT DISAGREE/AUTO SLAT TESTS WERE PERFORMED, BEING CORRECT. 2L72 4F4 F A6WE E9NE 20060124001572006012400157CE 2006 1 24 ON717JB121405JC 120051214A323324170161 ACTUATOR LEAR 60 60LEAR 5170707CE PWA 305 PW305 NE NLG STICKING E AOQAO OTHER O OTHER NRNOT REPORTED 1 EA11717JB3397 093 NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. INSPECTED LANDING GEAR SYSTEM AND FOUND NOSE GEAR FREE FALL ACTUATOR ARM TO BE STICKING IN EXTENDED POSITION. REPLACED NOSE GEAR FREE FALL ACTUATOR. ACCOMPLISHED NOSE GEAR UPLOCK ADJUSTMENT TEST, FREE FALL GEAR BLOW DOWN PLUMBING LEAK CHECK AND SEVERAL GEAR SWINGS WITH SATISFACTORY RESULTS. (K) 2L72 4F4 FRTA10CE E35NE 20060123000022006012300002NM 2006 1 23 ASAA0590112 120050616A5321453A261057 FLOOR PANEL BOEING737 737990 NM CABIN DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02318AS 300 PAE - DURING C-CHECK, FOUND AFT CARGO BAY NR 2 FLOOR PANEL HAS NUMEROUS DENTS. REPAIRED IAW SRM 53-60-53. (M) 2L74 4F RTA16WE 20060123000172006012300017WP 2006 1 23 UPS06845961 120051227A5210 SKIN DOUG DC8 DC871F 302199DWP R-1 DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE:C3 R-1 DOOR FWD UPPER CORNER CRACKED 1/4" LONG. CUT OUT DAMAGED AREA IAW SRM 53-02-00, FABRICATED AND INSTALLED FILLER, DOUBLER AND TRIPLER AT R-1 DOOR UPPER FWD CORNER IAW SRM 53-2-0 FIG 14, 51-1-8, AND SRM 51-1-20D. 2L74 4F RT4A25 20060124000572006012400057EA 2006 1 24 ASOA051164 120051231A5210CC67038601965 STRUCTURE CNDAIRCL600 CL6002C10 1390015EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27713EV 10081 DURING A C-CHECK IN MCN, THE FORWARD SIDE OF THE PASSENGER DOOR, BELOW THE TOP STEP, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FORWARD SIDE OF THE PASSENGER DOOR, BELOW THE TOP STEP, IAW BOMBARDIER REO 670-52-11-154 AND 670-52-11-072. (M) 2L72 4F RTA21EA 20060124000612006012400061EA 2006 1 24 ASOA051168 120051231A5310 CROSSBEAM CNDAIRCL600 CL6002C10 1390015EA BS 280 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27713EV 10081 DURING A C-CHECK IN MCN, THE CROSSBEAM, AT FS 280, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE CROSSBEAM, AT FS 280, IAW ASA EO 700-53-0054A. (M) 2L72 4F RTA21EA 20060124000652006012400065EA 2006 1 24 ASOA051055 120051204A5320 FLOOR SUPPORT CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27716EV 10084 DURING A C-CHECK IN MCN, DURING A C-CHECK IN MCN, THE FLOOR SUPPORT ANGLE, AT THE PASSENGER DOOR, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT ANGLE, AT THE PASSENGER DOOR IAW CRJ SRM 51-41-02. (M) 2L72 4F RTA21EA 20060124001382006012400138NE 2006 1 24 NACA20050032 220051224A7421URHB32E SPARK PLUG PWA DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE NR 13 CYLINDER CRACKED A NACAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CRCRUISE 1 AL0399330239 239 RU1545 43576 36210 NR 4 ENGINE SHUTDOWN DUE TO NR 13 CYLINDER DOUBLE SHORTED SECONDARY. FOUND FRONT PLUG FOULED AND REAR PLUG WITH CRACKED CERAMIC. REPLACED WITH SERVICEABLE PLUGS, REF: NAC MM SEC. IV PG. ECO5.1. OP CHECKED GOOD. 2L74 4R4 R 6A3 5E8 20060124001432006012400143CE 2006 1 24 DXTA200501165 120051219A2730 CONTROL UNIT CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE TRIM SYSTEM OUT OF POSITION E DXTAO OTHER F FLT CONT AFFECTED CLCLIMB 1 GL07333QS 5600333 DURING TAKEOFF-YOKE REQUIRED ALMOST FULL AFT DEFLECTION BEFORE THE AIRCRAFT BECAME AIRBORNE. TAKEOFF TRIM WAS IN NORMAL POSITION AND PARKING BRAKE WAS NOT SET. T/S ELEVATOR TRIM AND ELEVATOR SYSTEM, C/W TRAVEL CHECKS OF ELEV TRIM AND ELEVATOR AND FOUND PITCH TRIM T/O RANGE MARKER TO BE OUT OF POSITION SET T/O TRIM AND REPOSITIONED IAW MM 27-31-08. 2L72 4F4 FRTA22CE E25EA 20060124001452006012400145CE 2006 1 24 DXTA200501169 120051221A3230991420210 ROD CESSNA560 560XL 2076702CE PWA 545 PW545A NE NLG BROKEN E DXTAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL07675QS 5605275 UPON GEAR RETRACTION HEARD A LOUD BANG. NO OTHER INDICATIONS. SHORTLY AFTERWARDS HEARD WHAT SOUNDED LIKE A NOSE GEAR DOOR OPEN. AFTER LANDING LT NOSE GEAR DOOR RETRACTION ROD WAS FOUND BROKEN. INSPECTED NOSE GEAR AND FOUND LT NOSE GEAR DOOR RETRACT ROD BROKEN OFF AND ALSO FOUND THE CENTER HINGE WAS GOUGED. REPLACED THE CENTER AND NOSE GEAR RETRACT ROD WITH NEW. RIGGED NOSE GEAR DOORS. PERFORMED LANDING GEAR EXTENSION AND RETRACTION TO CHECK CLEARANCES AND RIGGING. OPS CHECKS GOOD WORK DONE IAW M/M 32-20-00. 2L72 4F4 FRTA22CE E00059EN 20060124001492006012400149NM 2006 1 24 2006AP01001 120051226A5315 FLOORBEAM BOEING747 747* NM BS 400 CRACKED B K NONE O OTHER ININSP/MAINT 1 SW99 NOSE WHEELWELL, BS 400, RBL 8, RETRACT ARM FAIRING, LWR ANGLE, CRACK LT WING GEAR FWD TRUN BRG HSG SUPT STRUCT IB FITTING MTG BOLT 2ND, UPR SHEARED OFF LT MLG W/W, BS 1241 LBL 1 VERT BEAM W/EXPO, CORROSION/CRACKED. R1 MED INTL STRUCT BET BEAM NR1,2, 14 INCH FWD, VERT FRM CRKD, CABIN ZONE D BS 1285-1300 BBLO PRESS DECK WEB, LONGIT STRAP W/CORROSION BULGES. ENG NR1 RT SIDE T/R BLK DOOR NR3 FROM TAP, FNGR BRKT WITH CRACK ENG NR1 RT SIDE T/R BLKR DOOR FNGR BRKT FROM TOP NR4 WITH CRACK. MN ENTRY DOOR R3, FWD CNR, CRACKS. MN ENTRY DOOR L3 FWD CNR CRACKS AT WELD REPAIR. CABIN ZONE A BS 266, RBL 77 FLOORBEAM UPR CHORD CRKD/BROKEN. CABIN ZONE A BS 266 RBL 77 FLOORBEAM, WEB CRACKED PYLON NR4 STRUT BEAM BRG OB SEIZED. 2L74 4F RTA20WE 20060124001582006012400158NM 2006 1 24 AMTA200501178 120051218A5315 FLOORBEAM BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE BS 1681 CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11517AT 27973 IN THE AFT GALLEY AT STA 1681 B/O THERE IS CORROSION ON THE UPPER SURFACE ON A FLOORBEAM CLIP. REMOVED CORROSION FROM FLOORBEAM THE CLIP AT 1681 BL0 IS LESS THAN 50 OUT OF LIMITS 53-00-01 FAB NEW CLIP 51-40-02. (K) 2L72 4F4 FRTA2NM E12EU 20060124001602006012400160NE 2006 1 24 ALG2006F00000 120051221A5340 BRACKET SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL MLG PROX LOOSE E ALGAA UNSCHED LANDING N FALSE WARNING HOHOVERING 1 SW03917QS 760217 WHEN AIRCRAFT WAS BROUGHT TO A HOVER THE LEFT MAIN GEAR LIGHT WENT OUT AND THE RED UNLOCK LIGHT ILLUMINATED. FOUND BRACKET HOLDING DOWN LOCK PROXIMITY LOOSE TIGHTENED, GROUND CHECK GOOD. (K) 1G72 3U3 U H1NE E1GL 20060124001612006012400161WP 2006 1 24 ASMF200512020 120051225A2410696233B CSD DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE DAMAGED W ASMFD RETURN TO BLOCK MJ OVER TEMP WARNING INDICATION TXTAXI/GRND HDL 1 SW23838AM264199082 49397 728049 AIRCRAFT RETURNED TO PLATFORM, DURING TAXING THE RT CSD REACHED 180 GRADES AND THE CSD SHUT OFF AUTOMATICALLY, THE RT CSD REPORT WAS DEFERRED IAW MEL 24-1. THE RT CSD AND HEAT EXCHANGE AIR OIL ENGINE WERE REPLACED IAW MM 24-10-01/-03, TESTED CORRECT. DEFERRED REPORT WAS CLOSED. 2L72 4F4 FRTA6WE E9NE 20060124001622006012400162NE 2006 1 24 ASMF200512017 220051219A72003400010260 BLADE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE RT ENGINE DAMAGED W ASMFK NONE C F.O.D. ININSP/MAINT 1 SW23160PL 49763 726001 DURING TRANSIT CHECK, A BLADE OF THE RT ENGINE WAS DETECTED WITH DAMAGE AND THE NOISE SUPPRESSOR LINER HAD INCRUSTED A FOD. INSPECTION WAS PERFORMED, DETECTING A DENT OF 0.75 X 0.25 AND .1875 OF LENGTH IAW MM 72-00-00. THE RT ENGINE BLADE WAS REWORKED IAW 72-00-00 FIGURE 201 AND THE NOISE SUPPRESSOR LINER PROVISIONAL REPAIR WAS PERFORMED IAW MM 72-33-66. DURING OVERNIGHT CHECK, THE RT ENGINE BOROSCOPE INSPECTION WAS PERFORMED TO 6TH AND 7TH STAGE COMPRESSOR BLADES, NO DAMAGES WERE FOUND IAW MM 72-00-00 AND THE NOISE SUPPRESSOR LINER DEFINITIVE REPAIR WAS PERFORMED IAW MM 72-33-66, ALL CORRECT. 2L72 4F4 FRTA6WE E9NE 20060124001662006012400166NE 2006 1 24 ASMF200512013 220051214A7200 BLADE DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE LT ENGINE FOD W ASMFK NONE C F.O.D. ININSP/MAINT 1 SW231075T 49724 696395 DURING TRANSIT CHECK, A BLADE OF THE LT ENGINE WAS DETECTED WITH DAMAGE BY FOD. INSPECTION WAS PERFORMED, DETECTING A CRACK OF 0.125 X 0.250 BEING WITHIN LIMITS IAW MM 72-00-00. THE LT ENGINE BLADE WAS REWORKED IAW 72-00-00 PAGE 618, TESTED CORRECT. 2L72 4F4 FRTA6WE E9NE 20060124001672006012400167NM 2006 1 24 ASMF200512014 120051215A2760 WARNING LIGHT DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE SPOILERS ILLUMINATED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23160PL 49763 AIRCRAFT RETURNED TO PLATFORM (SPOILER DEPLOYED) LIGHT TURNED ON. THE REPORT WAS DEFERRED IAW MEL 27-32 CAT B. IN THE NEXT TRANSIT CHECK AT GDL, THE SPOILER SYSTEM WAS CHECKED AND TESTED IAW MM 27-00-00, BEING CORRECT. DEFERRED REPORT WAS CLOSED. 2L72 4F4 FRTA6WE E9NE 20060124001712006012400171EU 2006 1 24 KBM2006F00004 120051214A7500 SWITCH SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE BLEED VALVE STICKING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P3167 2347 717 SOLENOID SWITCH IS STICKING, REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20060124001722006012400172EU 2006 1 24 IJA2006F00000 120051209A65106006F4212M16AMDTBEARING AEROSPAS355 AS355N 8680818EU TMECA ARRIUSARRIUS1A NE T/R DR SHAFT FANFAILED E IJAAO OTHER O OTHER NRNOT REPORTED 1 CE07912EM2615 5560 AC ON NORMAL FLIGHT. AT END OF FIRST LEG OF FLIGHT, PILOT SHUTDOWN THE ENGINES. PILOT THEN NOTICED A NOISE NEAR THE REAR OF AC. MAINT WAS NOTIFIED AND AC WAS GROUNDED UNTIL FURTHER NOTICE. AC WAS MOVED BY TRUCK TO HANGER. DISASSEMBLY WAS CONTINUED AND FOLLOWING PART HAD TO BE REPLACED DUE TO BEARING FAILURE. 2 EA BRGS, SHAFT, FAN, FAN STATOR, FAN. BRG HAD LOCKED UP AND SHAFT WAS TURNING INSIDE BRG. SHAFT WAS HOT ENOUGH TO BURN OFF THE PAINT AND HAD STARTED TO TWIST. SHAFT WOULD HAVE TWISTED OFF AND THE TAIL ROTOR WOULD HAVE STOPPED TURNING WITHIN A FEW MINUTES. (K) 1G72 3U3 URTH11GU E34NE 20060124001732006012400173EA 2006 1 24 A6WA200540364 120051217A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE BS 640-700 DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31433AW 7289 DAMAGE TO FUSELAGE SKIN AT FS640-FS700 STRINGER 18, 19 LT SIDE. MAINTENANCE REMOVED DAMAGE SKIN BETWEEN FS 640- FS 700 AND STRINGER 18 - 19L. FABRICATED DOUBLER AND FILLERS AND INSTALLED IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20060124001742006012400174EU 2006 1 24 632005N217CA 120050603A2750LOTOK47 RHEOSTAT AMD FALC20FALCON 2720302EU GE CF700 CF7002D2 30010NE CONTROL BOX BURNED E CEDAO OTHER O OTHER NRNOT REPORTED 1 SW05217CA 264 75 245G020 ENROUTE, THE CREW OBSERVED SMOKE FROM CENTER CONSOLE, THE CREW REQUESTED AN EMERGENCY DESCENT AND LANDED. MAINTENANCE FOUND THE RHEOSTAT HAD BURNED INSIDE THE FLAP CONTROL BOX. (K) 2L72 4F4 F A7EU E7EA 20060124001752006012400175EU 2006 1 24 KBM2006F00005 120051216A3260645300684 INDICATOR SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE NLG FLUCTUATES E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P 2347 UNIT FLUCTUATES DURING START, REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20060124001772006012400177WP 2006 1 24 AMTA200501220 120051226A33506165741 CHARGER LKHEED1011 10113853 5265020WP RROYCERB211 RB211524B4 54555NE EMERGENCY LIGHTSUNSERVICEABLE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11161AT 1219 EMERGENCY EXIT EXTERIOR LIGHTS FOR R-3 AND L-3 DOOR AND LT P4A AND RT P4A DOOR WORK FOR 12 SECONDS THE N GO OUT. REPLACED AFT RT MOST EMERGENCY POWER PACK FOR R-3 AND RT P4A DOOR IAW MM. OPS CHECK NORMAL. (K) 2L73 4F4 F A23WE E12EU 20060124001782006012400178NM 2006 1 24 AMTA200600014 120051209A5343 BEAM BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE LT MLG CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11514AT 27971 INSPECTED LT MLG TRUCK BEAM PIVOT BORE FOUND PITTED CORROSION THE OUTER RACE AND INSIDE RACE, IB HOLE. BORED LT MLG IB HOLE AND MACHINED FACE IAW REO AND CMM. FABRICATED BUSHING IAW CMM. REPAIR AREA FLAP PEENED AND CHROME PLATED AND BUSHING INSTALLED IAW BSOPM. (K) 2L72 4F4 FRTA2NM E12EU 20060124001792006012400179EU 2006 1 24 KBM2006F00001 120051230A6420350A33215001 BALL END SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE T/R SPIDER WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19250SH1159 3874 T/R SPIDER BALL END CONSISTS OF EXCESSIVE PLAY, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20060124001842006012400184CE 2006 1 24 GUU2006F00004 120051205A551010164001423 HINGE BRACKET BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE VERT STABILIZER CORRODED A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO176954920391 UE194 AT SCHEDULED MAINTENANCE, DETERMINED VERTICAL STABILIZER LOWER HINGE BRACKET TO BE EXFOLIATED. REPLACED VERTICAL STABILIZER LOWER HINGE BRACKET. (K) 2L72 4T4 TRTA24CE E26NE 20060124001852006012400185CE 2006 1 24 GUU2006F00007 120051228A2697 CONNECTOR BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE FIRE DETECTOR LOOSE A GUUAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO1749543 UE181 DURING FLIGHT, RT FIRE EXTINGUISHER DISCHARGE ANNUNCIATOR ILLUMINATED INTERMITTENTLY. RESECURED WIRE CONNECTORS AT RT FIRE EXTINGUISHER ANNUNCIATOR SWITCH. (K) 2L72 4T4 TRTA24CE E26NE 20060207000192006020700019NM 2006 2 7 DL76S060058 120050116A2530828450405 OVEN BOEING767 767332 1382001NM FWD GALLEY ODOR A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27127DL 24077 FWD GALLEY LOWER OVEN HAS AN ODOR OF BURNING RUBBER WHEN ON. REPLACED OVEN, OPS CKECKS OK. 2L72 4F RTA1NM 20060124001882006012400188NE 2006 1 24 KBM2006F00000 220051230A7421CH34745 IGNITER SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE NR 1 ENGINE WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19250SH1676 3874 NR 1 IGNITER TIP WORN, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20060124001892006012400189EU 2006 1 24 KBM2006F00002 120051228A7931642790041 TRANSMITTER SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE OIL PRESSURE LEAKING E KBMAO OTHER K FLUID LOSS NRNOT REPORTED 1 WP19115SH12678 3141 ENGINE OIL PRESSURE SENDER LEAKING FROM END CAP, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20060124001902006012400190EA 2006 1 24 A6WA200640005 120051229A5220 HANDLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE ESCAPE HATCH OUT OF POSITION A A6WAK NONE O OTHER ININSP/MAINT 1 GL31432AW 7257 CREW ESCAPE HATCH OUTER HANDLE STICKS IN THE CLOSED POSITION. CLEANED AND LUBRICATED OUTER HANDLE MECHANISM IAW AMM. (K) 2L72 4F4 FRTA21EA E15NE 20060124001912006012400191CE 2006 1 24 COEA0501753 120051224A5100 UNKNOWN CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE UNKNOWN E COEAO OTHER O OTHER NRNOT REPORTED 1 NM13753FE 208B0248 19121 ON TAKEOFF THE AIRCRAFT WOULD NOT GAIN ALTITUDE. AIRCRAFT CLEARED THE AIRPORT PROPERTY AND IMPACTED THE GROUND JUST AFTER THE FENCE. (K) 1H71 3T3 T A37CE E4EA 20060124002042006012400204WP 2006 1 24 ASMF200512012 120051212A80003927965 SHUTOFF VALVE DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE RT ENGINE MALFUNCTIONED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23216AM6131214544 49586 718083 AIRCRAFT RETURNED TO PLATFORM DURING RT ENGINE STARTING, IT DID NOT HAVE TURN IN N1 AND N2 AND OIL PRESSURE INDICATION. THE RT STARTER AND SHUTOFF VALVE WERE REPLACED IAW MM 80-10-02 AND MM 80-00-00 RESPECTIVELY, TESTED CORRECT. 2L72 4F4 FRTA6WE E9NE 20060124002072006012400207WP 2006 1 24 ASMF200512008 120051208A323059370365001 BUNGEE CYLINDER DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE RT MLG LEAKING W ASMFK NONE K FLUID LOSS ININSP/MAINT 1 SW23583MD175881441 49659 DURING TRANSIT CHECK, TECHNICAL PERSONNEL DETECTED A HYDRAULIC LIQUID LEAK IN THE RT MAIN LANDING GEAR. BUNGEE CYLINDER WAS REPLACED IAW MM 32-32-02, TESTED CORRECT. 2L72 4F4 FRTA6WE E9NE 20060124002092006012400209WP 2006 1 24 ASMF200512007 120051207A3220 PIN DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE NLG TOWING FUSE BROKEN W ASMFK NONE O OTHER ININSP/MAINT 1 SW231003Y 48068 DURING PUSH BACK THE NOSE LANDING GEAR TOWING FUSE PIN WAS BROKEN. IT WAS REPLACED IAW MM 32-21-14 AND THE NOSE LANDING GEAR AND GENERAL INSPECTIONS FOR EXCESSIVE LOAD WERE PERFORMED IAW MM 05-51-03 AND MM 32-20-00 RESPECTIVELY, NO DAMAGES WERE FOUND. 2L72 4F4 F A6WE E9NE 20060125000012006012500001SW 2006 1 25 KBM2006F00007 120051231A6320206030539101 ISOLATION MOUNT BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL M/R GEARBOX INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19188TV1833 2704 AIRCRAFT HAS VERTICAL VIBE DURING OUTOFF GROUND HOVER, ISOLATION MOUNT REMOVED AND REPLACED. (K) 1G71 3U3 U H2SW E4CE 20060125000082006012500008EA 2006 1 25 ASOA051093 120051215A5320 BRACKET CNDAIRCL600 CL6002B19 1900309EA BS 621 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 DURING A C-CHECK IN MCN, THE RIGHT SIDE ANGLE BRACKET, AT FS 621, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REPAIR THE RIGHT SIDE ANGLE BRACKET, AT FS 621, IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20060125000122006012500012EU 2006 1 25 ASOA051092 120051215A33507012210 LAMP AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27633AS 344 DURING A HANGAR INSPECTION IN MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE PASSENGER DOOR EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20060125000192006012500019EA 2006 1 25 ASOA051089 120051214A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA BS 718 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 DURING A C-CHECK IN MCN, THE LEFT SIDE FS 718, STRINGER 10-12, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REPAIR THE LEFT SIDE FS 718, STRINGER 10-12, IAW ASA EO 600-53-0067A. (M) 2L72 4F RTA21EA 20060125000352006012500035SO 2006 1 25 C2XA06IA004 120050109A335072875566958000 LIGHT EMB 145 EMB145XR 3260214SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712122 145684 IAH - FLIGHT 2420, DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT GALLEY EMERGENCY LIGHT STRIP TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20060125000572006012500057WP 2006 1 25 ABXA060046 120051223A5320 STRAP DOUG DC8 DC863 302198AWP BS 902 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 CORROSION ON ANGLE STRAP ON TOP OF MAIN LANDING GEAR WHEEL WELL BOX FORWARD OF FLOORBEAM STA 902, LEFT BUTT LINE 65. REMOVED CORROSION IAW DC8 SRM 51-1-8. DETERMINED TO BE OUT OF ACCEPTABLE LIMITS IAW DC8 SRM 53-2-0. REMOVED AND REPLACED WITH NEW FABRICATED ANGLE IAW DC8 SRM 51-1-21. 2L74 4F 4A25 20060125000622006012500062NM 2006 1 25 2005UALA01237 120051023A5320 FLOOR SUPPORT AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29830UA 1243 AFT GALLEY FLOOR STRUCTURE IS DAMAGED. *S/D* MAJOR REPAIR ACCOMPLISHED ON AFT GALLEY FLOOR STRUCTURE, FRAME 64 RBL 21", F66 BL 0", F66-68 RBL 30", F66-68 RT AFT ENTRY THRESHOLD, F68 BL 0", F68 LBL 6, F68 RBL 12", F68 RBL 15", F68 RBL 25", F68 LBL 24" BY REPLACE AND REPAIR. 2L72 4F4 FRTA28NM E40NE 20060125000632006012500063EU 2006 1 25 2005UALA01255 120051109A5330 SKIN AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29454UA 1104 FUSELAGE WAS DAMAGED BETWEEN FR73 & FR74 AND STR 41R TO 41L DURING AIRCRAFT JACKING, SKIN AND 6 EACH SHEAR TIES WERE BENT. *S/D* REPLACED 6 EA SHEAR TIES BETWEEN STR 41R & 41, 3EA ON FR73 AND FR74 REF SRM 51-42-11. INSTALLED 2EA TRIPLER REPAIRS PER SRM 53-00-11 FIG 204 & 205, AT FR 73 STR 42R & FR73 STR 42R. 2L72 4F4 FRTA28NM E40NE 20060125000642006012500064EU 2006 1 25 2005UALA01259 120051109A5330 SKIN AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29454UA 1104 BIRD STRIKE ON APPROACH LOWER FWD SECTION OF ACFT. *S/D* FABRICATED SKIN REPAIR AND INSTALLED PER SRM 53-00-11. 2L72 4F4 FRTA28NM E40NE 20060125000652006012500065EU 2006 1 25 2005UALA01260 120051108A5330 SKIN AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29455UA 1105 FOUND DENT IN FUSELAGE SKIN ON WALKAROUND 62.5 INCHES FWD OF DOOR 2L. *S/D* INSTALLED DOUBLER REPAIR PER SRM 53-41-11. 2L72 4F4 FRTA28NM E40NE 20060125000662006012500066EU 2006 1 25 2005UALA01261 120051108A5330 SKIN AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29455UA 1105 FOUND DENT IN FUSELAGE AFT OF DOOR 2L, 27 INCHES PAST DOOR & 4.75 INCHES ABOVE DOOR SILL. DENT IS 1.5 INCH WIDE & 1.75 INCH LONG BY .062 DEEP. LOCATED 9 INCHES PAST FR69 & 1 INCH BELOW STR 24. * S/D* ACCOMPLISHED HFEC TO BOTH EXTERNAL AND INTERNAL AREA OF DENT. AREA IS CRACK FREE AND WITHIN LIMITS OF SRM 53-41-11 AND SRM 53-41-11. NO FURTHER ACTION IS REQUIRED. 2L72 4F4 FRTA28NM E40NE 20060125001092006012500109NM 2006 1 25 2006UALA00030 120051230A5523 TAB BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU RT ELEVATOR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29385UA 24660 CRACKS FOUND ON RT ELEVATOR TAB. *S/D* THE RESEARCH FOUND THAT RT ELEVATOR TAB WAS REMOVED FROM AIRCRAFT, ROUTED TO SHOP 273 FOR REPAIR. THE TAB WAS REPAIRED, RETURNED, AND REINSTALLED ON SAME AIRCRAFT. P/N 65C26384-24A, S/N S37182 ELEVATOR TAB WAS REPAIRED FOR A CRACK AT MIDDLE HINGE CUTOUT. 2L72 4F4 FRTA16WE E21EU 20060126000032006012600003NM 2006 1 26 CALA0600029 120051202A5320 INTERCOSTAL BOEING737 737524 1384721NM BS 344-360 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2732626 27530 INSPECTION FOUND CHORD INTERCOSTAL CRACKED AT FASTENER HOLES, STA 344-360, LBL 28. THE CHORD INTERCOSTAL WAS REMOVED AND REPLACED IAW MM 51-40-02. 2L72 4F RTA16WE 20060126000042006012600004EU 2006 1 26 KBM2006F00013 120051227A28203031007710 FUEL LINE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE LEFT LEAKING E KBMAO OTHER K FLUID LOSS NRNOT REPORTED 1 WP19313LV10367 3296 LEFT FUEL LINE LEAKING, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20060126000052006012600005EU 2006 1 26 KBM2006F00012 120051226A6230704A33640021 SPACER SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE SWASHPLATE WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV 3296 SPACERS WORN, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20060126000062006012600006EU 2006 1 26 KBM2006F00015 120051228A62409550176240 TRANSMITTER SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE TORQUE FLUCTUATES E KBMAO OTHER N FALSE WARNING NRNOT REPORTED 1 WP19313LV2 3296 TORQUE TRANSMITTER, UNIT FLUCTUATES, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20060126000112006012600011EA 2006 1 26 ASOA051086 120051213A325016745101 PRESSURE SWITCH CNDAIRCL600 CL6002B19 1900309EA NLG STEERING INOPERATIVE A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27835AS 7258 DURING CLIMB-OUT FROM ATL-TYS, THE CREW RECEIVED A STEERING INOPERATIVE CAUTION MESSAGE. THE QRH WAS COMPLIED WITH AND THE CREW DECLARED AN EMERGENCY. THE EMERGENCY VEHICLES WERE DISPATCHED, AND THE AIRCRAFT RETURNED TO ATL WHERE IT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE NOSE WHEEL STEERING PRESSURE SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060126000122006012600012EU 2006 1 26 KBM2006F00031 120051204A6720 BUSHING SLEEVE SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1D NE PITCH LINK WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1953SH S5020 2009 UNIT HAS WORN BUSHING SLEEVE, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20060126000142006012600014EU 2006 1 26 KBM2006F00022 120051206A6710SC5083 SERVO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE MAIN ROTOR LEAKING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19351WM2445 2167 SAMM SERVO, UNIT HAS BAD LEAK. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20060126000302006012600030EU 2006 1 26 KBM2006F00023 120051208A2435 SHAFT SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE STARTER GEN SHEARED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1937SH 8768 2300 ENGINE WILL NOT START, SHEARED STARTER/GEN SHAFT, REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20060126000312006012600031 2006 1 26 KBM2006F00025 420051229A34225050010902 GYRO SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE MAG, DIRECT INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1937SH 92 2300 MAG IN UNIT WILL NOT RETRACK. AC MEL`D UNIT. (K) 1G71 3U3 UNCH9EU E19EU 20060126000442006012600044EA 2006 1 26 ASOA051085 120051212A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN MALFUNCTIONED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27931EV 8015 DURING A GROUND INSPECTION IN ATW, THE EMERGENCY FLOOR LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY FLOOR LIGHT STRIP WITH NO DEFECTS NOTED. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060126000452006012600045EA 2006 1 26 ASOA051082 120051210A5210601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27874AS 7551 DURING A HANGAR CHECK IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP IAW CRJ 200 SRM 51-41-02. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060126000612006012600061NE 2006 1 26 KBM2006F00011 220051226A7421CH34745 IGNITER SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE ENGINE WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV 3296 9666 IGNITER, UNIT WORN, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20060126000632006012600063EU 2006 1 26 KBM2006F00014 120051227A28200301009720 FUEL LINE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE RIGHT LEAKING E KBMAO OTHER K FLUID LOSS NRNOT REPORTED 1 WP19313LV10367 3296 9666 RT FUEL LINE LEAKING, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20060126000662006012600066EU 2006 1 26 KBM2006F00024 120051226A2435150SG122Q STARTER GEN SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE ENGINE INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1937SH 35 2300 GENERATOR LIGHT ON RESET DID NOT WORK, AFTER 2ND START AND SEVERAL TIMES PUSHING THE (RESET) LIGHT WENT OUT. (K) 1G71 3U3 UNCH9EU E19EU 20060126000682006012600068EA 2006 1 26 ASOA051087 120051214A5210601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27846AS 7328 DURING A HANGAR INSPECTION IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND CRACKED AT THE ATTACH POINT. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060126000702006012600070EU 2006 1 26 KBM2006F00033 120051204A6720350A33214501 SLEEVE SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1D NE TAIL ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1953SH 2009 UNIT HAS WORN HOUSING SLEEVE. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20060126000712006012600071 2006 1 26 KBM2006F00021 420051207A3452 TRANSPONDER SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE ATC INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19351WM346 2167 ATC SAID TRANSPONDER NOT WORKING, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20060126000722006012600072NM 2006 1 26 0501996624 120051025A5330 SKIN BOEING747 747251B 1384892NM FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01624US 21706 DURING M-CHECK FOUND CRACK IN SKIN AND BEAR STRAP AT UPPER AFT CORNER OF NR 3 RT DOOR CUTOUT. REPAIRED PER EA 66-205514. 2L74 4F A20WE 20060202000402006020200040SO 2006 2 2 MASA200500666 120050823A335078241 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSFAILED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07840MJ 145429 ASH 2989 CLT, OVERWING EMERGENCY EXIT CEILING LIGHT INOP. MX REPLACED THE EMERGENCY LIGHT INVERTER. OPS CHECK GOOD. 2L72 4T RTT00011AT 20060126000842006012600084EA 2006 1 26 A6WA200540365 120051218A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT WING CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31433AW 7289 LT WING LOWER PLANK ACCESS HOLE NR2 UNDER PNL 510AB AT WS 12.245 HAS CORROSION ON IB SIDE APPROX 3 INCH L X .1 INCH W X .004 DEEP IN NON CRITICAL AREA. MAINTENANCE REPAIRED WING PLANK ACCESS HOLE AT WS 12.245 IAW REO. (K) 2L72 4F4 FRTA21EA E15NE 20060202000672006020200067SO 2006 2 2 MASA200500797 120051012A3397 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSDIRTY A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07834MJ 145340 ASH 2804 CLT - CABIN EMERGENCY LIGHT E IN ROW 12 INOP. MX CLEANED CONNECTION. 2L72 4T RTT00011AT 20060124000602006012400060EA 2006 1 24 ASOA051163 120051231A5242H34455 HANDLE CNDAIRCL600 CL6002C10 1390015EA E/E BAY DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27713EV 10081 DURING A C-CHECK IN MCN, THE FORWARD AVIONICS BAY DOOR HANDLE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACE THE FORWARD AVIONICS BAY DOOR HANDLE. (M) 2L72 4F RTA21EA 20060124000632006012400063EA 2006 1 24 ASOA051059 120051204A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 349-985 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27716EV 10084 DURING A C-CHECK IN MCN, THE RIGHT SIDEWALL SEAT TRACKS, FROM FS 349 TO FS 985, WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED CORROSION FROM THE RIGHT SIDEWALL SEAT TRACKS, FROM FS 349 TO FS 985, IAW BOMBARDIER REO 670-53-00-013. (M) 2L72 4F RTA21EA 20060124001482006012400148NM 2006 1 24 AMTA200501167 120051216A5315 FLOORBEAM BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE BS 377 CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11517AT 27973 CORROSION ON CABIN FLOOR STRUCTURE STA 377.35, RBL 5 TO LBL20. REMOVED CORROSION 377 LBL 20 WITHIN LIMITS 2 AREAS OUT OF LIMITS LBL 10, LBL18 CUTOUT DAMAGE FAB FOR REPAIR ACH ANGLE 2 FILLER AND STRAP PLATE TREATED AREA SRM. 2L72 4F4 FRTA2NM E12EU 20060124001972006012400197EU 2006 1 24 2006F00000 120051223A3340A463A POWER SUPPLY BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101750B1 41560NE AFT CABIN SMOKE E A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW09330HH 60 7133 ON THE WAY TO PICK UP A PATIENT, IN CRUISE FLIGHT AT NIGHT, THE MEDICAL CREW IN THIS AIR AMBULANCE HELICOPTER DETECTED A BAD SMELL AND THEN SAW SMOKE IN THE AFT CABIN AREA. THE PILOT SHUT DOWN THE ELECTRICAL SYSTEM. AN UNSCHEDULED LANDING WAS MADE INTO A LARGE, WELL LIT, VACANT PARKING LOT AT A LOCAL HIGH SCHOOL. MAINTENANCE DETERMINED SMOKE TO BE FROM STROBE POWER SUPPLY. REPLACED POWER SUPPLY. 1G72 3U3 U H13EU E5NE10 20060124002052006012400205NE 2006 1 24 ASMF200512011 220051209A7200JT8D219 ENGINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE RT SIDE FOD W ASMFK NONE C F.O.D. ININSP/MAINT 1 SW23161PL413244458 49764 708175 DURING TRANSIT CHECK, THE RT ENGINE BLADES FIRST STAGE WERE DETECTED WITH AND THE NOISE SUPPRESSOR HAD INCRUSTED A FOD. INSPECTION WAS PERFORMED, DETECTING 20 COMPRESSOR BLADES OF FIRST STAGE WITH DAMAGE OUT OF LIMITS IAW MM 72-00-00. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT CHECK, THE RT ENGINE WAS REPLACED IAW 71-00-00, TESTED CORRECT. 2L72 4F4 FRTA6WE E9NE 20060125000092006012500009EA 2006 1 25 ASOA051090 120051214A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27924EV 7830 DURING A GROUND INSPECTION IN SHV, THE FORWARD CABIN EMERGENCY LIGHT AND RIGHT WING FORWARD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE WILL REMOVE AND REPLACE THE LAMPS IN THE FORWARD CABIN EMERGENCY LIGHT ASSEMBLY AND THE RIGHT WING FORWARD EMERGENCY LIGHT. (M) 2L72 4F RTA21EA 20060125000452006012500045WP 2006 1 25 ABXA060051 120051229A534039135822AX FITTING DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23968AX 47499 ANGLE CRACKED LOWER INBOARD AREA OF AFT SPAR AT APPROXIMATELY RIGHT BUTT LINE 8. REMOVED AND REPLACED FITTING IAW DC9 SRM 51-30-1 AND 51-30-5. 2L72 4F A6WE 20060125000542006012500054EA 2006 1 25 ASOA051091 120051215A5210601R319805 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 DURING A C-CHECK IN MCN, THE PASSENGER DOOR TOP STEP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACE THE PASSENGER DOOR TOP STEP. (M) 2L72 4F RTA21EA 20060126000152006012600015EA 2006 1 26 ASOA051088 120051214A2497 BUSS CNDAIRCL600 CL6002B19 1900309EA NR 2 FAILED A ASOAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DEDESCENT 1 SO27932EV 8016 DURING DESCENT AT ABOUT 24000 FT, CREW EXPERIENCED AN AC BUSS 2 FAILURE, WITH A BRIEF ELECTRICAL ODOR NOTED & A LOSS OF PRESSURIZATION. CREW RAN AC BUSS 2 MESSAGE CHECKLIST & SUCCESSFULLY RECOVERED NORMAL ELECTRICAL OPS. APPROX 30 SECONDS LATER A MORE SERIOUS ELECTRICAL FAILURE OCCURRED. ADG DEPLOYED & BOTH AC BUSSES 1 & 2 FAILED BUT CAME BACK ONLINE. BOTH AC AUTO TRANSFER FUNCTIONS SHOWED THAT THEY HAD FAILED. UNABLE TO RECOVER ALL OF AC BUSSES EXCEPT FOR AC SERVICE BUSS. AN EMERGENCY DECLARED & ACFT LANDED SAFELY IN ATL. MX R & R A/C TRANSFER CONTRACTOR & ASSOCIATED WIRING IAW ASA EO 600-24-0040. MX ALSO R & R BATTERY PACK FOR PREVENTATIVE MX. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060126000162006012600016EU 2006 1 26 ASOA051084 120051211A3297E00521086SNE CONNECTOR AEROSPATR72 ATR72212 8680945EU MLG BROKEN A ASOAO OTHER J WARNING INDICATION CLCLIMB 1 SO27637AS 383 DURING CLIMB-OUT FROM AGS-ATL, WHILE ATTEMPTING TO RETRACT GEAR, THE CREW RECEIVED A LEFT MAIN GEAR INDICATION. THE QRH WAS COMPLIED WITH AND THE FLIGHT ATTENDANT PERFORMED A VISUAL INSPECTION TO CONFIRM THE GEAR DOOR WAS DOWN. THE GEAR WAS RECYCLED AND THE CREW RECEIVED THREE GREENS ON THE INDICATION PANEL. AN EMERGENCY WAS DECLARED WITH EMERGENCY VEHICLES DISPATCHED. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REPAIRED THE LEFT 11 GAA CONNECTOR PLUG AND REPINNED THE UPLOCK BOX. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20060126000352006012600035EU 2006 1 26 KBM2006F00026 120051229A2820ST11559 FUEL LINE SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE CRACKED E KBMAO OTHER K FLUID LOSS NRNOT REPORTED 1 WP1937SH 2300 FUEL LINE HAS MULTIPLE CRACKS, REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20060126000742006012600074NM 2006 1 26 0502006624 120051028A5330 SKIN BOEING747 747251B 1384892NM FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01624US 21706 DURING M-CHECK FOUND CRACK IN SKIN AND BEAR STRAP AT LOWER FORWARD CORNER OF NR 3 RT ENTRY DOOR CUTOUT AREA. REPAIRED PER EA 66-205513. 2L74 4F A20WE 20060126000832006012600083NE 2006 1 26 592005N209CA 220050509A72005008T301001 BLADE AMD FALC20FALCON 2720302EU GE CF700 CF7002D2 30010NE NR 1 ENGINE BROKEN E CEDAO OTHER O OTHER NRNOT REPORTED 1 SW05209CA 71 304242B WHILE ENROUTE, AIRCRAFT DEVERTED, THE REASON WAS NR1 ENGINE ROLLED BACK. THE CREW USED THE CHECK LIST AND SHUTDOWN THE ENGINE. (K) 2L72 4F4 F A7EU E7EA 20060126000882006012600088CE 2006 1 26 6242004N238CA 120050624A2612 FIRE LOOP LEAR 25 25 5170506CE GE CJ610 CJ6106 30006NE NR 1 ENGINE OUT OF POSITION E CEDAO OTHER O OTHER NRNOT REPORTED 1 SW05238CA 25040 ON DECENT, THE FLIGHT CREW RECEIVED INDICATION OF FIRE IN THE NR1 ENGINE. THE FLIGHT CREW PERFORMED THE CHECKLIST AND COULD NOT CANCEL THE FIRE LIGHT. THE FLIGHT CREW THEN DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE CREW INSPECTED THE AIRCRAFT AND FOUND NO EVIDENCE OF FIRE. MAINTENANCE CREW FOUND THE FIRE DETECTOR LOOP TOUCHING THE ENGINE COWLING CAUSING A FLASE FIRE INDICATION. (K) 2L72 4J4 J A10CE 1E16 20060126000942006012600094NE 2006 1 26 7032005N213CA 220050703A7310CEETS4906 HOSE LEAR 25 25D 5170514CE GE CJ610 CJ6106 30006NE NR 2 ENGINE KINKED E CEDAB EMER. DESCENT YJ ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 SW05213CA 241 ENROUTE, UPON THE AIRCRAFT REACHING ITS ASSIGNED LEVEL OF FL 430 POWER WAS REDUCED FOR CRUISE AND THE NR 2 ENGINE QUIT. AIRCRAFT DESCENDED TO FL 250 AND THE ENGINE WAS RESTARTED. THE AIRCRAFT LANDED WITHOUT FURTHER PROBLEMS. (K) 2L72 4J4 J A10CE 1E16 20060126000952006012600095NE 2006 1 26 GAIA05034OP 220051129A7200JT8D15 ENGINE BOEING727 727251 138408HNM PWA JT8 JT8D15 52051NE NR 1 LEAKING A GAIAC ABORTED TAKEOFF KBJFLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TOTAKEOFF 1 SW07278US 21157 DURING TAKEOFF ROLL THE COCKPIT FILLED WITH SMOKE. TAKEOFF WAS ABORTED AND THE AIRCRAFT TAXIED TO THE RAMP. INVESTIGATION FOUND OIL IN THE NR1 ENGINE BLEED SADDLE DUCTS. ENGINE REMOVED, AIRCRAFT PARKED. (K) 2L73 4F4 F A3WE E2EA 20060126001102006012600110NM 2006 1 26 0509007 120050919A5414 PLATE BOEING737 7372H4 138448CNM NR 2 PYLON WORN A MJYAK NONE O OTHER ININSP/MAINT 1 SW05733TW 22732 ENGINE NR 2 PYLON FWD SECTION WITH PLATE WORN. 2L72 4F A16WE 20060126001122006012600112NM 2006 1 26 0509004 120050919A5754693927221 RIB BOEING737 7372H4 138448CNM NR 4 SLAT CRACKED A MJYAK NONE O OTHER ININSP/MAINT 1 SW05733TW 22732 RT WING, SLAT NR 4 RIB CRACKED AT SLAT STA 0.28. 2L72 4F A16WE 20060126001132006012600113NM 2006 1 26 0509006 120050919A5753 SKIN BOEING737 7372H4 138448CNM RT WING TE FLAP DELAMINATED A MJYAK NONE O OTHER ININSP/MAINT 1 SW05733TW 22732 RT WING INBOARD MID FLAP TRAILING EDGE P/N: 65-71902-42, S/N BN5, DELAMINATED AT WBL 132. 2L72 4F A16WE 20060126001152006012600115WP 2006 1 26 0509009 120050920A5313591141833 LONGERON DOUG DC9 DC915F 3022037WP BS 493-522 CORRODED A MJYAK NONE O OTHER ININSP/MAINT 1 SW05784TW 47014 LOWER FUSELAGE - KEEL AREA - LONGERON 29 RT FROM STA 493 TO STA 522 WITH CORROSION. 2L72 4F A6WE 20060126001162006012600116WP 2006 1 26 0509010 120050920A53404916270501 FITTING DOUG DC9 DC915F 3022037WP BS 523 CRACKED A MJYAK NONE O OTHER ININSP/MAINT 1 SW05784TW 47014 LOWER FUSELAGE - KEEL AREA - LONGERON 29 RT STA 523 OVER LONGERON FITTING CRACKED. 2L72 4F A6WE 20060126001182006012600118WP 2006 1 26 0509012 120050920A575339176601 FITTING DOUG DC9 DC915F 3022037WP TE FLAP CRACKED A MJYAK NONE O OTHER ININSP/MAINT 1 SW05784TW 47014 LT WING FLAP T/E SECTION WITH FITTING CRACKED LOCATED AT STA XFLS 76. 2L72 4F A6WE 20060126001192006012600119WP 2006 1 26 0509013 120050920A5310591235068 SUPPORT DOUG DC9 DC915F 3022037WP WINDSHIELD CORRODED A MJYAK NONE O OTHER ININSP/MAINT 1 SW05784TW 47014 CONTROL CABIN WINDSHIELD WITH SUPPORT CORRODED. 2L72 4F A6WE 20060126001212006012600121WP 2006 1 26 0509015 120050920A534039571741 FITTING DOUG DC9 DC915F 3022037WP FUSELAGE CRACKED A MJYAK NONE O OTHER ININSP/MAINT 1 SW05784TW 47014 RT VENTRAL STAIR CUTOUT WITH FITTING CRACKED LOCATED AT STA Y892. 2L72 4F A6WE 20060127000212006012700021WP 2006 1 27 0509018 120050920A532299220422 SUPPORT FITTING DOUG DC9 DC915F 3022037WP FUSELAGE CRACKED A MJYAK NONE O OTHER ININSP/MAINT 1 SW05784TW 47014 AFT CARGO COMPARTMENT SUPPORT FITTING CRACKED, LOCATED AT STA Y661 BETWEEN LONGERON 22R AND LONGERON 24R. 2L72 4F A6WE 20060127000222006012700022WP 2006 1 27 0509019 120050920A532239573171 SUPPORT FITTING DOUG DC9 DC915F 3022037WP FUSELAGE CRACKED A MJYAK NONE O OTHER ININSP/MAINT 1 SW05784TW 47014 FWD CARGO COMPARTMENT SUPPORT FITTING CRACKED, LOCATED FROM STA Y305 TO STA Y313 BETWEEN LONGERON 29R AND LONGERON 30. 2L72 4F A6WE 20060127000232006012700023WP 2006 1 27 0509020 120050920A573059195721 DOOR DOUG DC9 DC915F 3022037WP LT WING DELAMINATED A MJYAK NONE O OTHER ININSP/MAINT 1 SW05784TW 47014 LT WING, TRAILING EDGE, BUTE DOOR P/N 5919572-1, UPPER SKIN DELAMINATED AT STATION XRS 260 AND SKIN WORN OUT AT STATION XRS 153. 2L72 4F A6WE 20060127000262006012700026 2006 1 27 KBM2006F00039 420051228A3421H321EHM GYRO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE COCKPIT INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19966SH246 3787 UNIT WILL NOT CAGE, FLAG WOULD NOT GO OUT. AC MEL`D. (K) 1G71 3U3 U H9EU E19EU 20060127000292006012700029WP 2006 1 27 CLC2006F00000 120051226A5280NNR6086512 DOOR DOUG DC10 DC1030F 3023504WP GE CF6 CF650* 30018NE RT MLG DAMAGED A CLCAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO2947888 47888 WITH LANDING GEAR RETRACTION OUT. RT MAIN GEAR INDICATES STAYED RED. DIVERTED, INVESTIGATION FOUND SEQUENCE VALVE CABLE BROKEN, CAUSING RT MAIN GEAR DOOR DAMAGE, AND TIRE DAMAGE. (K) 2L73 4F4 FRTA22WE E23EA 20060127000362006012700036 2006 1 27 KBM2006F00037 420051230A34215040017701 GYRO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE ATTITUDE READS HIGH E KBMAO OTHER N FALSE WARNING NRNOT REPORTED 1 WP19884SH821 2884 UNIT READS 12 PERCENT HIGH, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20060127000372006012700037NM 2006 1 27 C7WA200500126 120051230A32301U10851 SEQUENCE VALVE BOEING727 727222 1384073NM PWA JT8 JT8D5 52046NE RT WHEEL WELL INTERMITTENT A C7WAO OTHER J WARNING INDICATION APAPPROACH 1 SO177644U 20038 DURING APPROACH, RT MLG AND NOSE GEAR INDICATION SHOWED UNSAFE. ON SECOND ATTEMPT GEARS CAME DOWN NORMALLY. ON GEAR OPERATIONAL CHECK RT MLG FAILED TO EXTEND, NOSE GEAR OPERATION NORMAL. REMOVED AND REPLACED RT MLG DOOR SEQUENCE VALVE. SYSTEM OPERATIONAL CHECKS GOOD MM. (K) 2L73 4F4 F A3WE E2EA 20060127000382006012700038WP 2006 1 27 05FDEA04271 120051213A5101 REPAIR DOUG DC10 DC1030F 3023504WP CARGO DOOR UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 FWD LOWER CARGO DOOR FOUND EXTERNAL DOUBLER FROM STA 885 TO STA 959 DIM 11 X 12 INCHES. REMOVED AND REPLACED REPAIR IAW SRM 52-10-00 FIG 6 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER F161770-3, DOUBLER IAW SRM 52-10-00 FIG 6 VOL 1. 2L73 4F RTA22WE 20060127000392006012700039EU 2006 1 27 KBM2006F00036 120051226A3300DHS775160 LIGHT SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE UNKNOWN STICKING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH 2884 UNIT STICKING, BODY LIGHT. (K) 1G71 3U3 U H9EU E19EU 20060127000402006012700040EU 2006 1 27 KBM2006F00038 120051208A80129550178290 START VALVE SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE ENGINE LEAKING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1937SH 2300 UNIT LEAKING DURING START UP, REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20060127000422006012700042WP 2006 1 27 05FDEA04274 120051213A5101 REPAIR DOUG DC10 DC1010 3022110WP FUSELAGE NONE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25563FE 46948 LOWER FUSELAGE FWD CARGO COMPT FOUND A SPLICE REPAIR ON FLOORBEAM AT STA 1099 X-46 DIM 10 X 5 INCHES. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 53-60-01 FIG 3 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2. 2L73 4F A22WE 20060127000432006012700043WP 2006 1 27 05FDEA04275 120051213A5101 REPAIR DOUG DC10 DC1010 3022110WP FUSELAGE NONE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25563FE 46948 RAM AIR DUCT CUTOUT HAS AN EXTERNAL TRIPLER DOUBLER ON LOWER FWD CORNER BETWEEN STA 557 TO 572 AND LONG 46 TO 48 LT SIDE DIM 15 X 15 INCHES, 12 X 13 INCHES. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 53-20-00 FIG 2 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P1. 2L73 4F A22WE 20060127000452006012700045WP 2006 1 27 05FDEA04277 120051213A5101 REPAIR DOUG DC10 DC1010 3022110WP FUSELAGE NONE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25563FE 46948 LOWER FUSELAGE FWD CARGO COMPT LOWER FRAME AT STA 879 HAS AN ANGLE REPAIR BETWEEN LONG 49 TO LONG 52 DIM 15 X 2 INCHES. PERFORMED INSPECTION ON ANGLE REPAIR IAW SRM 53-30-00 FIG 8 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2. 2L73 4F A22WE 20060127000462006012700046WP 2006 1 27 05FDEA04279 120051213A5101 REPAIR DOUG DC10 DC1010 3022110WP FUSELAGE NONE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25563FE 46948 LOWER FUSELAGE BELLY SKIN FOUND AN EXTERNAL DOUBLER REPAIR AT STA 1211 LONG 52 DIM 5 X 4.5 INCHES. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 53-40-00 FIG 20 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P1. 2L73 4F A22WE 20060127000482006012700048NM 2006 1 27 C7WA200500125 120051221A275118122993 INDICATOR BOEING727 727232 1384082NM PWA JT8 JT8D9 52048NE COCKPIT INTERMITTENT A C7WAA UNSCHED LANDING O OTHER NRNOT REPORTED 1 WP19511PE 20634 AIR RETURN. IB FLAP STUCK AT 15 DEGREES, AFTER TAKEOFF. REMOVED AND REPLACED FLAP POSITION INDICATOR IAW MM. FLAP SYS OPERATIONAL CHECKS GOOD. (K) 2L73 4F4 F A3WE E2EA 20060127000502006012700050NM 2006 1 27 C7W2006F00000 120051221A27511812993 INDICATOR BOEING727 727232 1384082NM PWA JT8 JT8D9 52048NE TE FLAPS INTERMITTENT A C7WAA UNSCHED LANDING O OTHER NRNOT REPORTED 1 SO29511PE 20634 AIR RETURN. IB FLAP STUCK AT 15 DEGREES AFTER TAKEOFF. REMOVED AND REPLACED FLAP POSITION INDICATOR IAW MM. FLAP SYS OPERATIONAL CHECKS GOOD. 2L73 4F4 F A3WE E2EA 20060127000592006012700059 2006 1 27 KBM2006F00006 420051221A2312064105430 RADIO BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL NR 1 COM VHF MALFUNCTIONED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19188TV 2704 NR 1 COM KNOB WILL NOT TURN POWER OFF, REMOVED AND REPLACED. (K) 1G71 3U3 U H2SW E4CE 20060127000622006012700062WP 2006 1 27 05FDEA04289 120051213A5700 REPAIR DOUG DC10 DC1010 3022110WP RT WING SLAT NONE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25563FE 46948 RIGHT WING SLAT NR 6 STA XOS 860 HEATED AREA HAS AN EXTERNAL DOUBLER REPAIR DIM 10 X 6 INCHES. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 57-10-00 FIG 12 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2. 2L73 4F A22WE 20060127000642006012700064EU 2006 1 27 05FDEA04291 120051213A5330 SKIN AIRBUS310 A310222 3930315EU FUSELAGE PUNCTURED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25450FE 162 PUNCTURE IN SKIN APPROX FR 34 BETWEEN STR 10-12 RT APPROX 8.5 X 4.3 INCHES HURRICANE RITA NR 11 REF N00061. COMPLIED WITH EA 6-5330-93418. 2L72 4F RTA35EU 20060127000662006012700066EU 2006 1 27 05FDEA04293 120051213A5330 SKIN AIRBUS310 A310222 3930315EU FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25450FE 162 SCRATCHES IN SKIN APPROX FR 22-23 RIGHT STR 5-6 APPROX 14 INCHES LONG AREA HURRICANE RITA NR 9 REF N00059. REPAIRED IAW EA 6-5330-94467. 2L72 4F RTA35EU 20060127000862006012700086SO 2006 1 27 MASA200500792 120051011A3350 WIRE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL SIGN LOOSE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07834MJ 145340 ASH 2676 CLT. ROW 12 EXIT SIGN INOPERATIVE. MAINTENANCE RESECURED LOOSE CONNECTION. 2L72 4T4 FRTT00011ATTE6CH 20060127000882006012700088SO 2006 1 27 MASA200500789 120051010A33501317 BULB EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL RT EMER LIGHT BURNED OUT A MASAK NONE O OTHER ININSP/MAINT 1 SW07846MJ 145507 ASH 2738 CLT. RT OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE RELAMPED LIGHT. 2L72 4T4 FRTT00011ATTE6CH 20060127000892006012700089SO 2006 1 27 MASA200500775 120051007A3350BA50933901 CHARGER EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL EXIT SIGNS SYS INOPERATIVE A MASAK NONE O OTHER ININSP/MAINT 1 SW07835MJ4208 4208 145353 ASH 2861 CLT. FLOOR LEVEL EMER LIGHTS INOP AND THE EXIT SIGNS LIGHTS. MX REPLACED THE CHARGER, OPS CHECKED GOOD. 2L72 4T4 FRTT00011ATTE6CH 20060127000902006012700090SO 2006 1 27 MASA200500770 120051005A3350 LIGHT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL EMGR LIGHT SYS INOPERATIVE A MASAK NONE O OTHER ININSP/MAINT 1 SW07835MJ 145353 ASH 2735 CLT. EMERGENCY LIGHT INOPERATIVE. MAINTENANCE RESET THE SYSTEM OP'S GOOD. 2L72 4T4 FRTT00011ATTE6CH 20060127000932006012700093NM 2006 1 27 UPS06446041 120051230A5230 SKIN BOEING747 747200 1384847NM PWA JT9 JT9D7A 52054NE FWD CARGO DR CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 1 INSPECTION TYPE:C FWD CARGO DOOR EXTERNAL SURFACE NR 821FR ACCESS PANEL CUTOUT AREA BILGE UP AT UPPER HALF TOP AREA. CORROSION BLEND OUT 0.070 INCH X 1INCH X 4 INCHES FWD CARGO DOOR NR 821FR ACCESS PANEL CUTOUT INTEGRAL FLANGE TRIMMED OUT AND REPAIRED IAW HX RS NR R52-34-35419 AND UPS EO NR B747-5230-23649-A. 2L74 4F4 FRTA20WE E20EA 20060127000942006012700094NM 2006 1 27 UPS06446040 120051231A575065B08428202 PANEL BOEING747 747200 1384847NM PWA JT9 JT9D7A 52054NE RH WING BLISTERED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 1 INSPECTION TYPE:C RHW - IB MID FLAP LWR FLAP FOUND BULGED UP AT 95 INCHES - 135 INCHES FROM IB SIDE AS MARKED. TIME LIMITED REPAIR ACCOMPLISHED IAW HX RS NR R-57-55-35418 AND UPS EO NR B747-5750-23648-A. 2L74 4F4 FRTA20WE E20EA 20060130000042006013000004EA 2006 1 30 VNAA0512024 120051228A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A VNAAL ABORTED APPROACH FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 GL05209PS 7874 DURING APPROACH WITH FLAPS AT 20 DEGREES THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED. THE CREW ABORTED THE APPROACH AND DECLARED AN EMERGENCY. THE APPROACH WAS RE-ESTABLISHED AND THE AIRCRAFT LANDED FLAPS 20 DEGREES WITH NO FURTHER INCIDENT. MAINTENANCE RESET AND OPERATIONALLY TESTED THE FLAP SYSTEM IAW BOMBARDIER CRJ 200 SL00-001. THE FLAPS OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20060124001592006012400159NM 2006 1 24 AMTA200501187 120051218A5320 SILL BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE FUSELAGE CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11517AT 27973 FWD CARGO COMPT CUTOUT SILL AREA NET TIEDOWN FITTING SUPPORT CORRODED AT AFT POSITION. REMOVED AND REPLACED FITTING. (K) 2L72 4F4 FRTA2NM E12EU 20060124001642006012400164NE 2006 1 24 ASMF200512004 220051128A7200 ENGINE BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE RIGHT FLAMED OUT W ASMFA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 SW23806AM3108713331 26273 726731 AC PERFORMED AN UNSCHEDULED LANDING, FWD AND AFT FUEL PUMP LIGHTS TURNED ON AND RT ENGINE FLAMED OUT ON FLIGHT AND DURING LANDING THE TIRES POSITION 4 AND 8 WAS FLATTED. THE TIRES POSITION 3, 4, 7 AND 8 WERE REPLACED IAW MM 32-45-01 PAGE 401. DURING MAINTENANCE REVISION THE RT TANK BY RULES AND INDICATION WERE DETECTED WITH ZERO FUEL, THE INSTRUMENTS INERTIAL AND FUEL PUMPS WERE DETECTED SHUTDOWN, RT BAR WAS ISOLATED. THE CHIPS DETECTOR AND FILTER WERE CHECKED FINDING WITHOUT EVIDENCE OF MAGNETIC PARTICLES. THE AIRCRAFT WAS REFUELED AND THE OPERATIONAL TESTS WERE PERFORMED WITH OPERATIONAL FEEDING IAW MM 71-00-00, BEING CORRECT. DURING TOWING THE SHEAR PIN WAS BROKE. THE SHEAR PIN WAS REPLACED, ALL CORRECT. 2L72 4F4 FRTA2NM E17NE 20060124001942006012400194 2006 1 24 ASMF200512006 420051205A3441HG1103BA01 IRU DOUG MD88 MD88 3023688NM PWA JT8 JT8D* NE LT SIDE FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23168PL44904 53174 AIRCRAFT RETURNED TO PLATFORM, LT INERTIAL LIGHT TURNED ON. THE INERTIAL UNIT WAS REPLACED IAW MM 34-43-01, TESTED CORRECT. 2L72 4F4 FRTA6WE E2EA 20060125000032006012500003EU 2006 1 25 MDAS094043 120051220A324450079951 TIRE FOKKERF27 F27MK50 EU RT MLG WHEEL CUT W Q0MFK NONE O OTHER ININSP/MAINT 1 WP03 20306 B-12275 RT IB MAIN WHEEL ASSEMBLY LACERATION WAS FOUND DURING TRANSIT CHECK. THIS IS THE 6TH CASE EXPERIENCED. IAW AMM 32-41-00 PERFORMED CHECK THE MAIN TIRE PRESSURE HAS NOT LEAKING, AND REPLACED THE MAIN WHEEL TIRE ASSEMBLY, CHECK NORMAL. 2H72 4T RTA817 20060125000072006012500007EA 2006 1 25 ASOA051095 120051215A5330 DOUBLER CNDAIRCL600 CL6002B19 1900309EA BS 640 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27849AS 7347 DURING A HANGAR INSPECTION IN BTR, THE RIGHT FS 640 DOUBLER, AT STRINGER 10, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACE THE RT FS 640 DOUBLER, AT STRINGER 10, IAW BOMBARDIER REO 601R-53-61-506. (M) 2L72 4F RTA21EA 20060126000732006012600073NM 2006 1 26 0501986624 120051018A5311 FRAME BOEING747 747251B 1384892NM BS 240 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01624US 21706 DURING M-CHECK FOUND CRACK IN FRAME AT BS 240 BETWEEN S13L AND S14L. REPAIRED PER EA 66-205837. 2L74 4F A20WE 20060126001082006012600108WP 2006 1 26 0509017 120050920A575349135671 FITTING DOUG DC9 DC915F 3022037WP RT WING FLAP CRACKED A MJYAK NONE O OTHER ININSP/MAINT 1 SW05784TW 47014 RT WING FLAP REAR SPAR WITH FITTING CRACKED, LOCATED AT STA XFLS 300. 2L72 4F A6WE 20060126001092006012600109NM 2006 1 26 0509005 120050919A57306550818316 PANEL BOEING737 7372H4 138448CNM RT WING DELAMINATED A MJYAK NONE O OTHER ININSP/MAINT 1 SW05733TW 22732 RT WING FIXED PANEL P/N: 65-50818-316, DELAMINATED AT WS 465. 2L72 4F A16WE 20060127000602006012700060EU 2006 1 27 KBM2006F00009 120051205A6720350A33214501 PITCH LINK SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE TAIL ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV420 3296 T/R PITCH LINK, BUSHING IN UNIT WORN, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20060127000762006012700076NM 2006 1 27 NOCA3005 120051220A3231141T699637 ROD END BOEING767 767324 1385203NM GE CF6 CF680C2B7 NE NLG BROKEN G NOCAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 EA15767NA 27569 AIR TURNBACK FOUND NOSE GEAR DOOR LT AFT DOOR SUPPORT ROD BROKEN AT DOOR TO STRUT ATTACH POINT. 2L72 4F4 FRTA1NM E13NE 20060127000852006012700085SO 2006 1 27 MASA200500799 120051012A335078241 INVERTER EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL EMGR LIGHTING INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07835MJ 145353 ASH 2949 CLT. EMERGENCY FLOOR LIGHTING ROWS 7 THROUGH 12 BEING INOPERATIVE. MAINTENANCE REPLACED THE INVERTER. 2L72 4T4 FRTT00011ATTE6CH 20060130000312006013000031SO 2006 1 30 GUU2006F00001 120051209A33501202129901 LIGHT EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE LT FUSELAGE SHORTED A GUUAK NONE O OTHER ININSP/MAINT 1 SO17261AS 120141 AT SCHEDULED MAINTENANCE DETERMINED LT AFT EXTERIOR EMERGENCY LIGHT TO BE INOPERATIVE. REPLACED LT AFT EXTERIOR LIGHT ASSEMBLY. (K) 2L72 4T4 TRTA31SO E20NE 20060130000342006013000034NM 2006 1 30 0501976303 120051228A3350 BATTERY PACK BOEING747 747451 1384940NM EMERGENCY LIGHTSUNKNOWN A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01663US 23818 DURING M-CHECK, SIN MAINTENANCE WAS CHECKING OUT THE UPPER DECK DOOR RIGHT EMERGENCY POWER RESERVOIR FIRING TEST, AND FOUND BATTERY OK LIGHT DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK AND SUPPLY UNIT. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20060130000362006013000036CE 2006 1 30 GUU2006F00005 120051228A554010164001417 HINGE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE VERT STAB CORRODED A GUUAK NONE O OTHER ININSP/MAINT 1 SO176954720838 UE189 AT SCHEDULED INSPECTION, DETERMINED VERTICAL FIN CENTER RUDDER HINGE BRACKET TO BE EXFOLIATED. REPLACED VERTICAL FIN CENTER RUDDER HINGE BRACKET. (K) 2L72 4T4 TRTA24CE E26NE 20060130000372006013000037CE 2006 1 30 GUU2006F00003 120051216A55101016200131 HINGE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE RT HORZ STAB CORRODED A GUUAK NONE O OTHER ININSP/MAINT 1 SO178755718542 UE246 AT SCHEDULED INSPECTION, DETERMINED RT ELEVATOR CENTER HINGE BRACKET TO BE EXFOLIATED. REPLACED RT ELEVATOR CENTER HINGE BRACKET. (K) 2L72 4T4 TRTA24CE E26NE 20060130000392006013000039SW 2006 1 30 KBM2006F00035 120051205A2432RG206 BATTERY BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL DISCHARGED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1973DP 145 2513 BATTERY, REMOVED DUE TO SLOW START. REMOVED AND REPLACED. (K) 1G71 3U3 U H2SW E4CE 20060130000422006013000042NM 2006 1 30 05FDEA04297 120051214A5313AFA77761 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 CENTER CARGO STATION 5-123 TO STATION 1541 LONGERON 48 RIGHT FOUND CORRODED. CTR CARGO COMPARTMENT STATION 5-123 TO STATION 1541 LONGERON 48 RIGHT, REPAIR CARRIED OUT AS PER SRM 53-10-00 FIG 2 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2L73 4F RTA22WE 20060130000562006013000056NM 2006 1 30 05FDEA04380 120051220A5330 REPAIR BOEING727 727200 138407ENM BS 1140 MISINSTALLED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25274FE 22039 FOUND PREVIOUSLY REPAIR AT STA 1140, STR 22L DOES NOT CONFORM TO FAA APPROVED DATA. REMOVED EXISTING REPAIR AND ACCOMPLISHED WITH REPAIR IAW SRM 53-30-3, FIG 1, TABLE 1, REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100. 2L73 4F RTA3WE 20060130000582006013000058EU 2006 1 30 05FDEA04382 120051220A5414 SKIN AIRBUS310 A310222 3930315EU NR 2 PYLON CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25450FE 162 RIGHT WING UPPER SURFACE PANEL LANDINGS ABOVE NR 2 PYLON BENT & CRACKED. REMOVED AND REPLACED CLOSING RIB NR 8 IAW DWG A572-45361 AND A310-200 SRM 51-40-21. REMOVED AND REPLACED 2 ANGLE LANDINGS IAW A310-200-40-21. 2L72 4F RTA35EU 20060130000592006013000059EU 2006 1 30 05FDEA04383 120051220A5330 SKIN AIRBUS310 A310222 3930315EU ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25450FE 162 PUNCTURE AND DENT TOP OF CROWN SKIN CENTERLINE ABOVE COCKPIT BETWEEN FR 7 & 8. PUNCTURE APPROX 2 X 7 INCHES JUST LEFT OF A/C CL. COMPLIED WITH EA 6-5330-94475 BY INSTALLING EXTERNAL DOUBLER. 2L72 4F RTA35EU 20060130000792006013000079NE 2006 1 30 ALG2006F00001 120051221A5320 BRACKET SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL DOWNLOCK SENSOR LOOSE E ALGAO OTHER N FALSE WARNING HOHOVERING 1 SW03917QS 760217 WHEN AIRCRAFT WAS BROUGHT TO A HOVER THE LEFT MAIN GEAR LIGHT WENT OUT AND THE RED UNLOCK LIGHT ILLUMINATED. FOUND BRACKET HOLDING DOWNLOCK PROXIMITY LOOSE TIGHTENED, GROUND CHECK GOOD. (K) 1G72 3U3 U H1NE E1GL 20060130000812006013000081NM 2006 1 30 GTIA050266 120051105A2750 CONTROL UNIT AIRBUSA319 A319132 3930340NM IAE V2524 V2524A5 NE TE FLAPS MALFUNCTIONED A GTIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL23508NK 2567 FLIGHT CONTROL FLAP FAULT FOLLOWED BY FLIGHT CONTROL FLAPS LOCKED, COULD NOT GET FLAPS TO EXTEND AFTER ENGINE START PRIOR TO TAXI, TAIL SWAP WITH AIRCRAFT N802NK. FOUND FAULT ON SFCC NR1, RESET THE WING TIP BRAKE AND SYSTEM OPS CHECK GOOD. (K) 2L72 4F4 FRTA28NM E40NE 20060130000832006013000083WP 2006 1 30 GTIA050270 120051030A5330 SKIN DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE DAMAGED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23835NK 53044 FUSELAGE SKIN DAMAGE AT FORWARD AND AFT LOWER CORNERS OF FORWARD GALLEY SERVICE DOOR CUTOUT. REMOVED DAMAGE AT FORWARD AND AFT LOWER CORNER OF GALLEY SERVICE DOOR CUTOUT IAW SRM, TREATED AND PRIMED AFFECTED AREA. (K) 2L72 4F4 FRTA6WE E9NE 20060130000852006013000085WP 2006 1 30 GTIA050276 120051115A5320 PAN DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE BS 1155 CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23802NK 53168 CORROSION AROUND CEILING PAN WHERE DRAIN GOES THROUGH AFT CARGO ABOVE STRINGER L-18 AT FS 1155. FABRICATED REPAIR FILLER AND DOUBLER, TREATED AND PRIMED FILLER AND DOUBLER, INSTALLED REPAIR AND NEW FLOOR SUPPORT BRACKET. (K) 2L72 4F4 FRTA6WE E9NE 20060130000882006013000088WP 2006 1 30 GTIA050269 120051029A5347 SEAT TRACK DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE BS 465 CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23835NK 53044 RT OB SEAT TRACK SWOLLEN AND CRACKED IN 2 PLACES AT APPROX FS465. CLEANED 2 SPOTS AND REMOVED SUSPECTED CRACK IAW SRM. PERFORMED HFEC OF RT OB SEAT TRACK AT FS 465 NO OTHER DEFECTS NOTED. PERFORMED ULTRASONIC THICKNESS OF SEAT TRACK WITHIN LIMITS, TREATED AND PRIMED. (K) 2L72 4F4 FRTA6WE E9NE 20060130001082006013000108EA 2006 1 30 ASOA051083 120051211A5210601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27909EV 7658 DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060130001442006013000144NM 2006 1 30 SWAA050310 120050203A53116546525 FRAME BOEING737 7373H4 1384600NM BS 380 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29603SW 27954 DURING SPV, FOUND FRAME CRACKED AT BS 380, STRINGER 8R. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20060130001472006013000147NM 2006 1 30 SWAA050361 120050208A53226546546 SHEAR TIE BOEING737 7373Q8 1384670NM BS 727E CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CORRODED BETWEEN BS 727E AND BS 747, FROM LBL 6 TO RBL 6. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20060130001482006013000148NM 2006 1 30 SWAA050377 120050209A53206551698 SPLICE BOEING737 7373Q8 1384670NM BS 908 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STRINGER 4R & STRINGER 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20060130001512006013000151NM 2006 1 30 SWAA050465 120050217A5310 STRUCTURE BOEING737 7373Q8 1384670NM BS 787-847 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND STRUCTURE CRACKED FROM BS 787 TO BS 847, STRINGER 8L. REPAIRED STRUCTURE SECTION PER SRM. 2L72 4F RTA16WE 20060130001552006013000155NM 2006 1 30 SWAA051100 120050414A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 727B CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727B, STR 5L & STR 7L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20060130001612006013000161NM 2006 1 30 SWAA052194 120050726A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 559 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29610WN 27696 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 559, STR 11R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20060130001622006013000162NM 2006 1 30 SWAA052210 120050727A53116546525 FRAME BOEING737 7373H4 1384600NM BS 380 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29610WN 27696 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20060130001642006013000164NM 2006 1 30 SWAA051059 120050412A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 578 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 578, STR 5R TO STR 8R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20060130001652006013000165NM 2006 1 30 SWAA051060 120050412A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 277 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 277, STR 10R & STR 14R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20060130001662006013000166NM 2006 1 30 SWAA051085 120050413A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 685 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 685, STR 4R TO STR 9R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20060130001682006013000168NM 2006 1 30 SWAA051088 120050413A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 727A CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727A, STR 6R & STR 7R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20060130001692006013000169NM 2006 1 30 SWAA051089 120050413A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 727A CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727A, STR 3L & STR 7L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20060130001722006013000172NM 2006 1 30 SWAA051157 120050419A53116546554 FRAME BOEING737 7373H4 1384600NM BS 847 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20060130001732006013000173NM 2006 1 30 SWAA051328 120050504A53116546550 FRAME BOEING737 7373H4 1384600NM BS 787 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20060130001742006013000174NM 2006 1 30 SWAA051318 120050504A53116546548 FRAME BOEING737 7373H4 1384600NM BS 747 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20060130001752006013000175NM 2006 1 30 SWAA051361 120050509A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 663 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29352SW 24888 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 663, STR 10L & STR 10R. REMOVED AND REPLACED CLIPS PER SRM. 2L72 4F RTA16WE 20060125001262006012500126EA 2006 1 25 ASOA01094A 120051215A5312 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 DURING A C-CHECK IN MCN, THE FS 280 BULKHEAD WAS FOUND TO BE CRACKED OUTBOARD OF RBL 9 AND LBL 9, AND THE FLOOR SUPPORT ANGLE WAS FOUND TO BE CRACKED OUTBOARD OF LBL 9 AND CORRODED BETWEEN RBL 9 AND LBL 9. MAINTENANCE WILL REPAIR THE FS 280 BULKHEAD, OUTBOARD OF RBL 9 AND LBL 9, AND THE FLOOR SUPPORT ANGLE OUTBOARD OF RBL AND LBL 9, AND THE FLOOR SUPPORT ANGLE OUTBOARD OF LBL 9, AND BETWEEN RBL 9 AND LBL 9, IAW BOMBARDIER REO 601R-53-11-926. (M) 2L72 4F RTA21EA 20060126000082006012600008EU 2006 1 26 KBM2006F00010 120051224A6410355A09103601 BEARING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE TAIL ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV1768 3296 HALF SHELL BEARINGS, TORN AND WORN, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20060126000622006012600062SW 2006 1 26 KBM2006F00008 120051231A256011010214 SEAT BELT BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL COCKPIT BROKEN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19188TV 2704 SEAT BELT BROKEN, REMOVED AND REPLACED. (K) 1G71 3U3 U H2SW E4CE 20060126001142006012600114WP 2006 1 26 0509008 120050920A532039162171 SUPPORT FITTING DOUG DC9 DC915F 3022037WP BS 576 CORRODED A MJYAK NONE O OTHER ININSP/MAINT 1 SW05784TW 47014 LOWER FUSELAGE - KEEL AREA - STA 576.939 BETWEEN X1.5 AND X8.5 RT SIDE, SUPPORT FITTING CORRODED. 2L72 4F A6WE 20060126001172006012600117WP 2006 1 26 0509011 120050920A53203915130502 FITTING DOUG DC9 DC915F 3022037WP BS 490 CORRODED A MJYAK NONE O OTHER ININSP/MAINT 1 SW05784TW 47014 LOWER FUSELAGE - KEEL AREA - LONGERON 30 STA 490.540 LONGERON END ANGLES (RT AND LT) CORRODED. 2L72 4F A6WE 20060126001202006012600120WP 2006 1 26 0509014 120050920A575349135661 FITTING DOUG DC9 DC915F 3022037WP TE FLAP CRACKED A MJYAK NONE O OTHER ININSP/MAINT 1 SW05784TW 47014 LT WING FLAP REAR SPAR WITH FITTING CRACKED LOCATED AT STA XFLS 300. 2L72 4F A6WE 20060127000412006012700041WP 2006 1 27 05FDEA04273 120051213A5101 REPAIR DOUG DC10 DC1010 3022110WP FUSELAGE NONE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25563FE 46948 LOWER FUSELAGE FWD CARGO COMPT FOUND A SPLICE REPAIR ON FLOORBEAM AT STA 1099 X 46 DIM 10 X 5 INCHES. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 53-60-01 FIG 3 VOL 1 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2. 2L73 4F A22WE 20060127000442006012700044WP 2006 1 27 05FDEA04276 120051213A5101 REPAIR DOUG DC10 DC1010 3022110WP FUSELAGE NONE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25563FE 46948 RAM AIR DUCT CUTOUT ON SKIN HAS AN EXTERNAL TRIPLE DOUBLER REPAIR ON THE UPPER AFT CORNER BETWEEN STA 576-590 LONG 44 TO 46 DIM 14 X 12.5 INCHES, 10 X 11.5 INCHES. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 53-20-00 FIG 2 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P1. 2L73 4F A22WE 20060130000412006013000041EU 2006 1 30 05FDEA04294 120051213A5330 SKIN AIRBUS310 A310222 3930315EU FUSELAGE PUNCTURED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25450FE 162 PUNCTURE IN SKIN FWD OF FR 22 BETWEEN STR 12 & 13 RIGHT SIDE APPROX 4 X 3.2 INCHES HURRICANE RITA NR 7 REF N00057. REPAIRED IAW EA 6-5330-93419. 2L72 4F RTA35EU 20060130000612006013000061NM 2006 1 30 05FDEA04385 120051220A5322 SHEAR TIE BOEING727 727200 138407ENM BS 970 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 BS 970 STR 29L-30 TIE HAS CORROSION. REMOVED SHEAR TIE AT BS 970 STR 29L-30 AND REPLACED WITH NEW SHEAR TIE PER SRM 53-10-4. 2L73 4F RTA3WE 20060130000872006013000087EU 2006 1 30 GTIA050267 120050919A5330 STRUCTURE AIRBUS320 A320321 3930325EU IAE V2533 V2533A5 NE FUSELAGE GROUND DAMAGE A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23583NK 1195 PERFORMED HARD LANDING/ OVERWEIGHT LANDING INSPECTION, FOUND DAMAGE AT LOWER TAIL SECTION BETWEEN FR67-FR68 IAW AMM, NO ADDITIONAL DAMAGE NOTED. INSTALLED INTERM REPAIR IAW EA AND DWG, AIRCRAFT FERRIED FOR REPAIR. PERMANENT REPAIR ACCOMPLISHED, AIRCRAFT OK FOR CONTINUED SERVICE. (K) 2L72 4F4 FRTA28NM E40NE 20060130000912006013000091WP 2006 1 30 AMTA200501232 120051226A3350 BATTERY PACK LKHEED1011 10113853 5265020WP RROYCERB211 RB211524B4 54555NE EMERGENCY LIGHT INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11164AT 1238 C ZONE LT AFT EGRESS STRIP INOPERATIVE. FOUND LT AFT EGRESS POWER STRIP DAMAGED. REPLACED BATTERY PACK, POWER STRIP AND CROSSAISLE LAMP STRIP OPS CHECKED OK IAW. (K) 2L73 4F4 F A23WE E12EU 20060130001392006013000139NM 2006 1 30 SWAA050308 120050203A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 360 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 DURING SPV, FOUND STRINGER CLIP CRACKED BETWEEN BS 360 FROM STRINGER 4L TO STRINGER 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20060130001462006013000146NM 2006 1 30 SWAA050360 120050208A534065C27314 STRINGER CLIP BOEING737 7373Q8 1384670NM BS 727D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, BETWEEN STRINGERS 23L AND 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20060130001492006013000149NM 2006 1 30 SWAA050409 120050211A53226546529 SHEAR TIE BOEING737 7373Q8 1384670NM BS 500 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CORRODED BETWEEN BS 500 AND BS 500D, FROM STRINGER 26L TO STRINGER 27L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20060130001562006013000156NM 2006 1 30 SWAA052288 120050801A55236959227 BUSHING BOEING737 7373H4 1384600NM ELEVATOR TAB FAILED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29604SW 27955 DURING SCHEDULED C4 CHECK, RT ELEVATOR TAB FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB NR 1 HINGE BUSHINGS & HARDWARE PER MM. 2L72 4F RTA16WE 20060130001582006013000158NM 2006 1 30 SWAA052141 120050721A53116546520 FRAME BOEING737 7373H4 1384600NM BS 360 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29609SW 27929 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20060130001632006013000163NM 2006 1 30 SWAA051058 120050412A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 597 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 597, STR 1R TO STR 8R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20060130001702006013000170NM 2006 1 30 SWAA051082 120050413A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 616 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 616, STR 4L & STR 5L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20060130001912006013000191NM 2006 1 30 SWAA051102 120050414A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 727D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727D, BETWEEN STR 3R & STR 5R. REMOVED AND REPLACED CLIPS PER SRM. 2L72 4F RTA16WE 20060130001922006013000192NM 2006 1 30 SWAA051104 120050414A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 500C CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 500C, BETWEEN STR 5L & STR 7L. REMOVED AND REPLACED CLIPS PER SRM. 2L72 4F RTA16WE 20060130001932006013000193NM 2006 1 30 SWAA051105 120050414A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 500D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 500D, BETWEEN STR 6L & STR 8R. REMOVED AND REPLACED CLIPS PER SRM. 2L72 4F RTA16WE 20060130001942006013000194NM 2006 1 30 SWAA051106 120050414A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 520 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 520, BETWEEN STR 6L & STR 8R. REMOVED AND REPLACED CLIPS PER SRM. 2L72 4F RTA16WE 20060130001972006013000197NM 2006 1 30 SWAA051438 120050517A53116546552 FRAME BOEING737 7373H4 1384600NM BS 767 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 8L TO STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20060130002282006013000228NM 2006 1 30 SWAA050446 120050216A53116546550 FRAME BOEING737 7373Q8 1384670NM BS 827 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D CHECK, FOUND FRAME FROM BS 827 TO BS 907, STRINGER 8L, CRACKED. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20060130002292006013000229NM 2006 1 30 SWAA050539 120050222A534065C27314 STRINGER CLIP BOEING737 7373Q8 1384670NM BS 727C CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP AT BS 727C,BETWEEN STR 5L AND 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20060130002302006013000230NM 2006 1 30 SWAA050541 120050222A534065C27314 STRINGER CLIP BOEING737 7373Q8 1384670NM BS 727C CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP AT BS 727C, BETWEEN STR 2R AND 6R CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20060130002312006013000231NM 2006 1 30 SWAA050546 120050222A534065C27314 STRINGER CLIP BOEING737 7373Q8 1384670NM BS 663 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D CHECK, FOUND CRACKED STRINGER CLIP AT BS 663, STR 10L AND 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20060130002322006013000232NM 2006 1 30 SWAA050548 120050222A534065C27314 STRINGER CLIP BOEING737 7373Q8 1384670NM BS 597 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D CHECK, FOUND CRACKED STRINGER CLIP AT BS 597, STR 8L AND 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20060130002342006013000234NM 2006 1 30 SWAA050555 120050223A5753 SKIN BOEING737 737 UTILSYSNM TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29 DURING SHOP VISIT, FOUND LT T/E AFT INBD FLAP UPPER SKIN DELAMINATED. REPAIRED SPARE FLAP PER SWA EA. 2L72 4F RTA16WE 20060130002352006013000235NM 2006 1 30 SWAA050570 120050224A53206551698 SPLICE BOEING737 7373Q8 1384670NM BS 907 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, BETWEEN STR 4L AND STR 4R. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20060130002372006013000237NM 2006 1 30 SWAA050599 120050225A53116546546 FRAME BOEING737 7373Q8 1384670NM BS 827 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 9R. REPAIRED FUSELAGE FRAME PER SRM. 2L72 4F RTA16WE 20060130002382006013000238NM 2006 1 30 SWAA050623 120050228A531365C27314 STRINGER CLIP BOEING737 737317 138447PNM BS 400 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 DURING SCHEDULED SPECIAL VISIT, FOUND CRACKED STRINGER CLIP AT STR 9L, BS 400. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20060130002402006013000240NM 2006 1 30 SWAA050779 120050314A53116546552 FRAME BOEING737 7373H4 1384600NM BS 907 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29605SW 27956 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L TO STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20060130002722006013000272NM 2006 1 30 SWAA051550 120050525A534065C27314 STRINGER CLIP BOEING737 737301 1384611NM BS 616 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 616, BETWEEN STR 1 & STR 8L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20060130002742006013000274NM 2006 1 30 SWAA051570 120050526A534065C27314 STRINGER CLIP BOEING737 737301 1384611NM BS 727A CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 2R. REMOVED AND REPLACED STR CLIP PER SRM. 2L72 4F RTA16WE 20060131000032006013100003NM 2006 1 31 SWAA051427 120050516A534065C27314 STRINGER CLIP BOEING737 737301 1384611NM BS 344 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 344, STR 11R & STR 13R. REMOVED AND REPLACED CLIPS PER SRM. 2L72 4F RTA16WE 20060131000042006013100004NM 2006 1 31 SWAA051571 120050526A53206551698 SPLICE BOEING737 737301 1384611NM BS 908 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4L & STR 4R. REMOVED AND REPLACED STR SPLICE PER SRM. 2L72 4F RTA16WE 20060131000082006013100008NM 2006 1 31 SWAA051741 120050614A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 597 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, BETWEEN STR 8R & STR 9L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20060131000092006013100009NM 2006 1 31 SWAA051738 120050614A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 706 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 2L, STR 9L & STR 10L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20060131000102006013100010NM 2006 1 31 SWAA051739 120050614A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 639 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 2R & STR 4R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20060126001112006012600111NM 2006 1 26 0509003 120050919A5312 BULKHEAD BOEING737 7372H4 138448CNM BS 1016 CRACKED A MJYAK NONE O OTHER ININSP/MAINT 1 SW05733TW 22732 BS 1016 AFT PRESSURE BULKHEAD WEB TO Y-CHORD ATTACHMENT CRACKED. 2L72 4F A16WE 20060126001222006012600122WP 2006 1 26 0509016 120050920A575399577764 FITTING DOUG DC9 DC915F 3022037WP RT WING FLAP CRACKED A MJYAK NONE O OTHER ININSP/MAINT 1 SW05784TW 47014 RT WING FLAP FRONT SPAR WITH FITTING CRACKED, LOCATED AT STA XFLS 288. 2L72 4F A6WE 20060127000632006012700063NM 2006 1 27 05FDEA04290 120051213A5314 KEELBEAM BOEING727 727200 138407ENM BS 980 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 REWORK REQUIRED FROM CARD N00363. REPAIR DOUBLER AT BS 980, STR 29R HAS PILLOWING AND CRACKED FASTENER HEADS. SUSPECT CORROSION ON INTERNAL BEAM. PILLOWING SEALANT STILL EXISTS ALONG INTERNAL BEAM. REPAIRED PER FED EX EA 7-5310-96552. 2L73 4F RTA3WE 20060127000652006012700065EU 2006 1 27 05FDEA04292 120051213A5330 SKIN AIRBUS310 A310222 3930315EU FUSELAGE PUNCTURED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25450FE 162 PUNCTURE & DENT IN SKIN APPROX RT STR 8-10 AT FR 23 PUNCTURE APPROX 11 X 6.5 INCH DENT APPROX 22 X 16 INCH HURRICANE RITA NR 8. REPAIRED IAW EA 6-5330-93417. 2L72 4F RTA35EU 20060127000872006012700087SO 2006 1 27 MASA200500793 120051011A3350 CONNECTOR EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL EXIT SIGN LOOSE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07829MJ 145228 ASH 2773 CLT. ROW 12 EXIT SIGN INOPERATIVE. MAINTENANCE RESECURED LOOSE CONNECTION. 2L72 4T4 FRTT00011ATTE6CH 20060130000012006013000001EA 2006 1 30 VNAA0512022 120051226A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A VNAAO OTHER J WARNING INDICATION APAPPROACH 1 GL05209PS 7874 THE FLAPS FAIL MESSAGE ILLUMINATED ON APPROACH WITH FLAPS AT 20 DEGREES. THE CREW FOLLOWED THE QRH AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET AND TESTED THE FLAP SYSTEM IAW RJ-SL-27-084. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20060130000052006013000005EA 2006 1 30 VNAA0512026 120051216A541422850080802 ACCESS PANEL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT NACELLE MISSING A VNAAO OTHER O OTHER NRNOT REPORTED 1 GL05229PS4167 7898 AFTER FLIGHT THE RT ENGINE NOSE COWL UPPER ACCESS PANEL WAS DISCOVERED MISSING. MAINTENANCE INSTALLED A SERVICEABLE PANEL AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20060130000352006013000035CE 2006 1 30 GUU2006F00002 120051216A55101016200131 HINGE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE LT HORZ STAB CORRODED A GUUAK NONE O OTHER ININSP/MAINT 1 SO1787557 UE246 AT SCHEDULED INSPECTION, DETERMINED LT ELEVATOR CENTER HINGE BRACKET TO BE EXFOLIATED. REPLACED LT ELEVATOR CENTER HINGE BRACKET. (K) 2L72 4T4 TRTA24CE E26NE 20060130000552006013000055NM 2006 1 30 05FDEA04295 120051213A5315 REPAIR BOEING727 727200 138407ENM FLOORBEAM DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 EXISTING FLOORBEAM REPAIR UPPER CHORD AT BS 1130, RBL 5.5 - RBL 15.5 (10 X 2 INCH). REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIRED PER FED EX EA 7-5310-91426. 2L73 4F RTA3WE 20060130000572006013000057NM 2006 1 30 05FDEA04381 120051220A5330 REPAIR BOEING727 727200 138407ENM BS 1183 MISINSTALLED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25274FE 22039 FOUND PREVIOUSLY REPAIR AT STA 1183, STR 27R IS NOT IN CONFORMANCE WITH APPROVED FAA DATA. REMOVED EXISTING REPAIR, ACCOMPLISHED WITH REPAIR IAW SRM 53-30-3, FIG 3 AND SRM 51-30-2. REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100. 2L73 4F RTA3WE 20060130000622006013000062NM 2006 1 30 05FDEA04242 120051212A3260 ROD BOEING727 727100 1384036NM NLG DIRTY A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25188FE 19081 DURING TEST FLIGHT WITH GEAR HANDLE UP NOSE GEAR RED LIGHT AND RED DOORS LIGHT STAYED ON. *S/D* CLEANED DIRT FROM AND LUBRICATED NLG DOOR SWITCH ACTUATOR RODS. JACKED NOSE AND SWUNG GEAR. NLG FUNCTIONALLY TESTED GOOD. SERVICED NLG STRUT. WORK DONE PER MM 32-61-000-15, 07-11-000-2, 12-15-025-2. 2L73 4F RTA3WE 20060130001382006013000138NM 2006 1 30 SWAA050214 120050126A5322 SHEAR TIE BOEING737 7373H4 1384600NM BS 727C CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29602SW 27953 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CORRODED IN AFT CARGO COMPARTMENT, BS 727C, RBL 3. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20060130001452006013000145NM 2006 1 30 SWAA050332 120050206A5310 STRUCTURE BOEING737 7373K2 13844BANM BS 616-639 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29340LV 23738 DURING SCHEDULED 1/2D CHECK, FOUND STRUCTURE BETWEEN BS 616 AND BS 639, STRINGER 18R, CRACKED. REPAIRED STRUCTURE PER T1-153-018. 2L72 4F RTA16WE 20060130001522006013000152NM 2006 1 30 SWAA050444 120050216A53406551698 STRINGER CLIP BOEING737 7373Q8 1384670NM BS 360 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29317WN 24068 DURING SPV, FOUND STRINGER CLIP AT BS 360, STRINGER 4L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20060130001532006013000153NM 2006 1 30 SWAA051083 120050413A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 639 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 639, STR 3R & STR 4R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20060130002362006013000236NM 2006 1 30 SWAA050598 120050225A53116546546 FRAME BOEING737 7373Q8 1384670NM BS 727E CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727E, STR 9L. REPAIRED FUSELAGE FRAME PER SRM. 2L72 4F RTA16WE 20060131000062006013100006NM 2006 1 31 SWAA051617 120050601A53206551698 SPLICE BOEING737 737301 1384611NM BS 360 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, BETWEEN STR 27L & STR 28R. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20060131000112006013100011NM 2006 1 31 SWAA051740 120050614A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 578 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 9R, STR 7R & STR 8L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20060131000142006013100014NM 2006 1 31 SWAA051873 120050627A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 616 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 616, STR 3L, STR 5L & STR 8L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20060131000152006013100015NM 2006 1 31 SWAA051874 120050627A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 597 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 597, STR 7R & STR 8L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20060131000182006013100018NM 2006 1 31 SWAA051943 120050705A53156545410 FLOORBEAM BOEING737 7373H4 1384600NM BS 727B CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, BETWEEN LBL 45 & RBL 45. REPAIRED FLOORBEAM PER BFG ER. 2L72 4F RTA16WE 20060131000192006013100019NM 2006 1 31 SWAA051944 120050705A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 727A CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727A, STR 5L & STR 6L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20060131000202006013100020NM 2006 1 31 SWAA051945 120050705A53116546550 FRAME BOEING737 7373H4 1384600NM BS 727 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BETWEEN BS 727B TO BS 727E, STR 8R TO STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20060131000222006013100022NM 2006 1 31 SWAA051913 120050702A53116546532 FRAME BOEING737 7373H4 1384600NM BS 440 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 440, STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20060131000262006013100026 2006 1 31 SWAA051957 420050705A2565D31354 SLIDE BOEING737 7373Q8 1384670NM L1 & R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20060131000272006013100027NM 2006 1 31 SWAA052112 120050719A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 807 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, BETWEEN STR 17L TO STR 19L. REMOVED AND REPLACED STR CLIP PER SRM. 2L72 4F RTA16WE 20060131000292006013100029NM 2006 1 31 SWAA052251 120050728A53156546805 FLOORBEAM BOEING737 7373H4 1384600NM BS 794 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 794, BETWEEN LBL 8 & LBL 12. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20060131000302006013100030NM 2006 1 31 SWAA052238 120050728A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 787 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29610WN 27696 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CORRODED AT BS 787, STR 26R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20060131000312006013100031NM 2006 1 31 SWAA052240 120050728A53206545410 FLOOR SUPPORT BOEING737 7373G7 1384595NM BS 658-672 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29691WN 23781 DURING SCHEDULED 1/4D CHECK, FOUND CRACK ON NR 2 LONGITUDINAL FLOOR SUPPORT BETWEEN BS 658 TO BS 672. REPAIRED FLOOR SUPPORT PER SWA EA. 2L72 4F RTA16WE 20060131000322006013100032NM 2006 1 31 SWAA052241 120050728A534065C27314 STRINGER CLIP BOEING737 7373G7 1384595NM BS 767 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29691WN 23781 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 767, STR 25L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20060131000332006013100033 2006 1 31 SWAA052229 420050727A256563550 SLIDE BOEING737 7377H4 1384404NM DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29432WN 33715 DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20060131000362006013100036NM 2006 1 31 SWAA052183 120050725A3350A0071701100 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHTSINOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29763SW 27877 DURING SCHEDULED MV2 CHECK, FOUND CABIN EMERGENCY LIGHTS INOP BETWEEN ROW 6 ABC TO ROW 10 ABC. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20060131000382006013100038NM 2006 1 31 SWAA051997 120050708A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 706 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29608SW 27928 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 706, STR 11L & STR 11R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20060131000392006013100039NM 2006 1 31 SWAA052000 120050708A53116546526 FRAME BOEING737 7373H4 1384600NM BS 400 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29608SW 27928 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20060131000412006013100041NM 2006 1 31 SWAA052071 120050715A53116546526 FRAME BOEING737 7373H4 1384600NM BS 380 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29613SW 27931 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380 TO BS 400, STR 8L TO STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20060131000432006013100043NM 2006 1 31 SWAA052099 120050715A53116546550 FRAME BOEING737 7373H4 1384600NM BS 360 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29613SW 27931 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R TO STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20060131000442006013100044NM 2006 1 31 SWAA052100 120050715A53116546552 FRAME BOEING737 7373H4 1384600NM BS 727D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29613SW 27931 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8L TO STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20060131000562006013100056EA 2006 1 31 ASOA051081 120051210A5210601R3807423 ANCHOR CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27874AS 7551 DURING A HANGAR INSPECTION IN MCN, THE FORWARD AND AFT PASSENGER DOOR ANCHORS WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FORWARD AND AFT PASSENGER DOOR ANCHORS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060131000922006013100092NM 2006 1 31 CALA0600033 120050508A52306546921530 SKIN 6546921528 BOEING737 7373T0 1384582NM CARGO DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW277033055784 1054 23460 MAINTENANCE FOUND A CRACK AT LIGHTENING HOLE IN THE LOWER INNER SKIN OF THE FORWARD CARGO DOOR WHILE THE DOOR WAS IN SHOP FOR MAINTENANCE. THE DOOR HAD BEEN REMOVED PREVIOUSLY AT HOU DURING A 4C MAINTENANCE CHECK IN MAY OF 2005. THE DOOR WAS REPAIRED IAW ECRA 5232-01069. 2L72 4F RTA16WE 20060131001282006013100128NM 2006 1 31 AWXA200600136 120051224A5320PL6546598520 CHANNEL BOEING737 73733A 1384673NM BS 1016-1019 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - MAJOR REPAIR - CORROSION FOUND DURING C19 CHECK ON THE RT OUTBOARD SIDE ON THE AFT PRESSURE BULKHEAD FORWARD FACE CENTER CHANNEL ON THE BOTTOM END FROM BS 1016 TO BS 1019, WL 193 TO WL 195 AND FROM BL 2L TO BL 4R. MAINTENANCE REMOVED DAMAGED SECTION OF CHANNEL IAW BOEING 737-300 SRM 51-40-02 AND BAC DRAWING 65C28106. INSTALLED NEW CHANNEL AND SPLICE REPAIR AT RT OUTBOARD SIDE OF AFT PRESSURE BULKHEAD FORWARD FACE FROM BS 1016 TO BS 1019, WL 193 TO WL 195 AND FROM BL 2L TO BL 4R IAW BOEING 737-300 SRM 51-40-02-0G. LEAK CHECK WAS GOOD. 2L72 4F RTA16WE 20060131001292006013100129NM 2006 1 31 AWXA200600137 120051221A5340693535214 STRINGER CLIP BOEING737 73733A 1384673NM BS 616 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED STRINGER CLIP CRACKED, .5 INCHES, AT BS 616 AND STR 4R. MAINTENANCE REMOVED AND INSTALLED NEW STRINGER CLIP AT BS 616 AND STR 4R IAW BOEING 737-300 SRM 51-40-02-0G FIG 3, 8 AND 51-40-02-0G FIG 8 AND 12. 2L72 4F RTA16WE 20060131001312006013100131NM 2006 1 31 AWXA200600139 120051219A57536546431286SP SKIN BOEING737 73733A 1384673NM FOREFLAP CHAFED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED LOWER SKIN CHAFED AT O/B END OF THE RT O/B FORE FLAP, RT WING. MAINTENANCE REPAIRED LOWER SKIN AREA BY REMOVING CHAFED REPAIR DOUBLER AND FILLER IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED REPLACEMENT DOUBLER AND FILLER IAW BOEING 737-300 SRM 57-53-02-0I2 FIG 1 SHEET 5. BONDED FABRICATED REPAIR PARTS TO THE O/B END OF THE RT O/B FORE FLAP, RT WING IAW BOEING 737-300 SRM 51-70-10-2R4 FIG 202. 2L72 4F RTA16WE 20060131001342006013100134NM 2006 1 31 AWXA200600142 120051223A5320 STRAP BOEING737 73733A 1384673NM FLOORBEAM CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED CORROSION ON FLOORBEAM STRAP AT BS 1024 TO BS 1029 AND BL 3R. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-51-1A1. REMOVED AND INSTALLED FABRICATED REPLACEMENT FLOORBEAM STRAP FROM BS 1024 TO BS 1029 AND AT BL 3R IAW BOEING 737-300 SRM 51-40-05-0G FIG 2. 2L72 4F RTA16WE 20060131001372006013100137NM 2006 1 31 UPS06446007 120051228A5512 SKIN BOEING747 747212B 1384886NM EMPENNAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 INSPECTION TYPE:C REF DMI# D305601 - INTERIM REPAIR TO FUSELAGE SKIN PUNCTURE AT FS 2565 (CRACK LENGTH 13"). SKIN AT BS 2553 - 2575 BETWEEN S46R AND S49R PERMANENT REPAIRED AS PER EO# B747-5330-22469-B APPENDIX B AND ZERO, TIME ALL FASTENER HOLES CARRIED OUT IAW SRM 51-10-01 PG 12. 2L74 4F A20WE 20060131001412006013100141NM 2006 1 31 AWXA200600143 120051227A5310654681134 BEAM BOEING737 73733A 1384673NM BS 1006 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - DURING C19 CHECK DISCOVERED CORROSION ON BS 1006 BEAM AT SCREW LOCATED AT BL 10L. CORROSION WAS REMOVED AND FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-51-1A1 FIG 101. MAINTENANCE FABRICATED REPAIR STRAP AND INSTALLED AT BS 1006 BEAM AT BL 10L IAW BOEING 737-300 SRM 53-00-51-2R3. 2L72 4F RTA16WE 20060131001422006013100142NM 2006 1 31 AWXA200600144 120051226A53116546561509 FRAME BOEING737 73733A 1384673NM BS 957 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED AFT GALLEY DOORWAY FRAME CRACKED, .5 INCHES AT BS 957, WL 257 AND BL 58R. MAINTENANCE REMOVED AND INSTALLED NEW REPLACEMENT DOORWAY FRAME AT BS 957, WL 257 AND BL 58R IAW BOEING 737-300 SRM 52-13-31-404-010-800 AND BOEING 737-300 SRM 51-40-02-0G FIG 3, 4, 6, 7 AND 12. 2L72 4F RTA16WE 20060130000292006013000029CE 2006 1 30 GUU2006F00006 120051228A554010164001415 HINGE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE VERTICAL STAB CORRODED A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO176954720838 UE189 AT SCHEDULED INSPECTION, DETERMINED VERTICAL FIN UPPER RUDDER HINGE BRACKET TO BE EXFOLIATED. REPLACED VERTICAL FIN UPPER RUDDER HINGE BRACKET. (K) 2L72 4T4 TRTA24CE E26NE 20060130000332006013000033SO 2006 1 30 GUU2006F00000 120051214A3397 WIRE EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE EMERGENCY LIGHT BROKEN A GUUAK NONE L NO TEST ININSP/MAINT 1 SO17285AS 120265 ON PREFLIGHT, AFT EMERGENCY LIGHTS, LT AND RT, INOPERATIVE. REPAIRED BROKEN WIRES ON RT LIGHT RECEPTACLE. (K) 2L72 4T4 TRTA31SO E20NE 20060130000602006013000060NM 2006 1 30 05FDEA04384 120051220A5322 SHEAR TIE BOEING727 727200 138407ENM BS 970 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 SHEAR TIE REPAIR STRAP BS 970 STR 29 L WL 148 HAS CORROSION. *S/D* REMOVED SHEAR TIE AT BS 970 STR 29L WL 148 AND INSTALLED NEW SHEAR TIE PER SRM 53-10-4. 2L73 4F RTA3WE 20060130000762006013000076WP 2006 1 30 AMTA200501221 120051224A3350516574 CHARGER LKHEED1011 1011385115 5265015WP RROYCERB211 RB211524B4 54555NE EMERGENCY LIGHT UNSERVICEABLE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11194AT 193B1230 R4 DOOR EXTERIOR EMERGENCY EGRESS LIGHT IS INOPERATIVE. REPLACED EMERGENCY LIGHTING POWER PACK IAW MM. OPS CHECK NORMAL. (K) 2L73 4F4 F A23WE E12EU 20060130000822006013000082WP 2006 1 30 GTIA050268 120051106A5312 PRESSURE BLKHD DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE BS 110 DAMAGED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23835NK 53044 TEAR ON AFT PRESSURE BULKHEAD IN NOSE WHEEL WELL, LOWER LT CORNER STA 110. REMOVED DAMAGED AREA, CLEANED SHARP EDGES, FAB FILLER AND DOUBLER FROM 7075-T6, TREATED PRIMED AND INSTALLED REPAIR IAW EA. (K) 2L72 4F4 FRTA6WE E9NE 20060130000842006013000084WP 2006 1 30 GTIA050263 120051021A5240 FRAME DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE L2 DOOR CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23832NK 49618 L-2 DOOR FRAME IS CRACKED JUST BELOW BAYONET. INSTALLED SERVICEABLE DOOR AT L-2 POSITION IAW MM FOR ROG AND LEAK CHECK. (K) 2L72 4F4 FRTA6WE E9NE 20060130000902006013000090WP 2006 1 30 GTIA050273 120051119A5315 SEAT TRACK DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE BS 1136 CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23802NK 53168 STA 1136, SEAT TRACK HAS CORROSION. FABRICATED, TREATED AND INSTALLED SECTION OF SEAT TRACK AT STA 1136. (K) 2L72 4F4 FRTA6WE E9NE 20060130001502006013000150NM 2006 1 30 SWAA050422 120050214A53206551698 SPLICE BOEING737 7373Q8 1384670NM BS 400 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE AT BS 400, STRINGER 14L AND STRINGER 4L, CRACKED. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20060130001542006013000154NM 2006 1 30 SWAA051095 120050413A53156545410 FLOORBEAM BOEING737 7373H4 1384600NM BS 715 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 715, BL 0, WL 204. REPAIRED BEAM PER SRM & EO. 2L72 4F RTA16WE 20060130001572006013000157NM 2006 1 30 SWAA052142 120050721A53116546520 FRAME BOEING737 7373H4 1384600NM BS 380 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29609SW 27929 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20060130001592006013000159NM 2006 1 30 SWAA052198 120050726A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM BS 767 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29610WN 27696 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 767 , LBL 19. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20060130001602006013000160NM 2006 1 30 SWAA052195 120050726A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM BS 747 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29610WN 27696 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 747, RBL 19. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20060130001672006013000167NM 2006 1 30 SWAA051086 120050413A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 706 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 706, STR 8L & STR 9R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20060130001712006013000171NM 2006 1 30 SWAA051156 120050419A53116546548 FRAME BOEING737 7373H4 1384600NM BS 747 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20060130001902006013000190NM 2006 1 30 SWAA051101 120050414A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 727C CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIPS CRACKED AT BS 727C, STR 5L & STR 7L. REMOVED AND REPLACED CLIPS PER SRM. 2L72 4F RTA16WE 20060130001962006013000196NM 2006 1 30 SWAA051437 120050517A53116546554 FRAME BOEING737 7373H4 1384600NM BS 787 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R TO STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20060130002332006013000233NM 2006 1 30 SWAA050554 120050223A534065C27314 STRINGER CLIP BOEING737 7375H4 138449DNM BS 663 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29507SW 24184 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED STRINGER CLIP AT BS 663, STR 10L AND STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20060130002392006013000239NM 2006 1 30 SWAA050624 120050228A534065C27314 STRINGER CLIP BOEING737 737317 138447PNM BS 500A CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CLIP CRACKED AT STR 9L, BS 500A. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20060130002412006013000241NM 2006 1 30 SWAA050806 120050315A534065C27314 STRINGER CLIP BOEING737 7373Q8 1384670NM BS 344 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 11R AND STR 13R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20060130002632006013000263NM 2006 1 30 SWAA051433 120050517A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 727C CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727C, BETWEEN STR 6L & STR 8L. REMOVED AND REPLACED CLIPS PER SRM. 2L72 4F RTA16WE 20060130002642006013000264NM 2006 1 30 SWAA051434 120050517A531165C25228 FRAME BOEING737 7373H4 1384600NM BS 727D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R TO STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20060130002652006013000265NM 2006 1 30 SWAA051506 120050523A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 685 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29353SW 24889 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 11L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20060130002662006013000266NM 2006 1 30 SWAA051536 120050524A53206551698 SPLICE BOEING737 737301 1384611NM BS 536 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 536, STR 10R. REMOVED AND REPLACED SPLICE PER SRM. 2L72 4F RTA16WE 20060130002672006013000267NM 2006 1 30 SWAA051538 120050524A534065C27314 STRINGER CLIP BOEING737 737301 1384611NM BS 500A CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 500A, STR 16R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20060130002682006013000268NM 2006 1 30 SWAA051515 120050524A53206551698 SPLICE BOEING737 7373H4 1384600NM BS 360 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER SPLICE CORRODED AT BS 360 + 5, BETWEEN STR 26L & STR 27L, WL 149. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20060130002692006013000269NM 2006 1 30 SWAA051547 120050525A534065C27314 STRINGER CLIP BOEING737 737301 1384611NM BS 578 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 578, STR 2L & STR 8R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20060130002702006013000270NM 2006 1 30 SWAA051548 120050525A534065C27314 STRINGER CLIP BOEING737 737301 1384611NM BS 597 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 597, BETWEEN STR 2R & STR 9R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20060130002712006013000271NM 2006 1 30 SWAA051549 120050525A534065C27314 STRINGER CLIP BOEING737 737301 1384611NM BS 597 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 597, BETWEEN STR 2L & STR 8L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20060130002732006013000273NM 2006 1 30 SWAA051569 120050526A53116546550 FRAME BOEING737 737301 1384611NM BS 807 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20060130002752006013000275NM 2006 1 30 SWAA051568 120050526A53116546550 FRAME BOEING737 737301 1384611NM BS 727E CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727E, STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20060131000012006013100001NM 2006 1 31 SWAA051411 120050515A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 276 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29352SW 24888 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 276, STR 10R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20060131000052006013100005NM 2006 1 31 SWAA051642 120050602A53156546804 FLOORBEAM BOEING737 7377H4 1384404NM BS 772 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29771SA 27879 DURING SCHEDULED 5Y CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 772, BETWEEN LBL 8 TO LBL 12. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20060131000162006013100016NM 2006 1 31 SWAA051878 120050627A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 706 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 706, STR 10L & STR 11L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20060131000212006013100021NM 2006 1 31 SWAA051994 120050708A53116546550 FRAME BOEING737 7373H4 1384600NM BS 747 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29608SW 27928 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20060131000232006013100023NM 2006 1 31 SWAA051915 120050702A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 294 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 294.5, STR 11L, STR 12L & STR 13L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20060131000242006013100024NM 2006 1 31 SWAA051955 120050705A53226546529 SHEAR TIE BOEING737 7373H4 1384600NM BS 500A CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29608SW 27928 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CORRODED AT BS 500A TO BS 500B, STR 28L TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20060131000342006013100034NM 2006 1 31 SWAA052174 120050725A5315BAC1509100146 FLOORBEAM BOEING737 7373H4 1384600NM BS 767 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE LONGITUDINAL FLOORBEAM CORRODED AT BS 767 + 5, LBL 3 & LBL 12. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20060131001332006013100133NM 2006 1 31 AWXA200600141 120051223A53206545812187 FLOOR SUPPORT BOEING737 73733A 1384673NM BS 1006-1016 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED CORROSION ON FLOOR SUPPORT FROM BS 1006 TO BS 1016, BL 5L TO BL 10L AND WL 208. MAINTENANCE FOUND THE CORROSION TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-51-1A1 FIG 101. REMOVED FLOOR SUPPORT AND INSTALLED NEW FLOOR SUPPORT FROM BS 1006 TO BS 1016, BL 5L TO BL 10L AND WL 208 IAW BOEING 737-300 SRM 51-40-02-0G FIG 12. 2L72 4F RTA16WE 20060131001692006013100169SO 2006 1 31 GNB2006F00000 220051206A741410357586 DISTRIBUTOR GEARCONT CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO MAGNETO STRIPPED E GNBAO OTHER O OTHER NRNOT REPORTED 1 SW014643N2028 402C0006 8233364R ENROUTE, RAN ROUGH, LANDED. RUNUP FOUND RT MAGNETO ROUGH AND EXCESSIVE DROP. (SW01200603304) (K) 1L72 3O3 O A7CE E8CE 20060131001722006013100172SO 2006 1 31 GNB2006F00002 220051207A741410357586 DISTRIBUTOR GEAR CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO MAGNETO STRIPPED E GNBAO OTHER O OTHER NRNOT REPORTED 1 SW0157PB 1862 402C0300 823359R ENROUTE LT ENGINE BEGAN TO RUN ROUGH, LANDED. RUN UP FOUND LT ENGINE MAGNETO ROUGH AND EXCESSIVE DROP. (SW01200603302) (K) 1L72 3O3 O A7CE E8CE 20060131001742006013100174EA 2006 1 31 BGI2006F00000 220051223A7414103571651 COIL ROBSINR44 R44 7640120WP LYC O540 O540F1B5 41532EA MAGNETO FAILED E BGIAO OTHER O OTHER NRNOT REPORTED 1 NM138372H E04BA120R 0387 L2512340A OWNER COMPLAINED OF INTERMITTENT ROUGHNESS AND AT TIMES COMPLETE FAILURE OF RT MAG. UPON INVESTIGATION THE COIL GROUND WIRE WAS FOUND CHAFING ON THE DISTRIBUTOR GEAR TEETH. THE MULTISTRAND WIRES WERE COMPLETELY SEVERED AND ONLY A SMALL AMOUNT OF INSULATION WAS HOLDING THE WIRE STRANDS TOGETHER MAKING INTERMITTENT CONTACT. IMPROPER ROUTING OF GROUND WIRE AT MAG BUILDUP CONTRIBUTED TO FAILURE. CAREFUL ATTENTION TO DETAIL WOULD HAVE PREVENTED THIS OCURRENCE. MAGNETO WAS FACTORY OVERHAULED. THIS IS THE SECOND MAG FAILURE ON THIS AIRCRAFT SINCE BOTH MAGS WERE INSTALLED 137 HRS PREVIOUS. FIRST (LT) MAG FAILURE OCCURRED AT 98 HRS. LT MAG WAS ALSO FACTORY OVERHAULED. (K) 1G71 3O3 O H11NM E295 20060131001802006013100180SO 2006 1 31 SIMA200535510 120051212A532014521713003 FLOOR SUPPORT EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21611AE 145074 DURING CPCP INSPECTION, FOUND CARBON CROSS MEMBER AT FRAME 24-25 CENTER OMEGA BEAM ATTACHMENT IS CORRODED. REPAIRED OMEGA BEAM BY INSTALLING AN EXTERNAL DOUBLER IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4F4 FRTT00011ATTE6CH 20060131001852006013100185SO 2006 1 31 GNB2006F00001 220051205A741410357586 DISTRIBUTOR GEARCONT CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO MAGNETO STRIPPED E GNBAO OTHER O OTHER NRNOT REPORTED 1 SW01747WS2089 402C0080 PRE TAKEOFF RUNUP CHECKED GOOD. PULLED ONTO RUNWAY, APPLIED POWER, RT ENGINE BEGAN TO RUN ROUGH. ABORTED TAKEOFF. MAINTENANCE DISCOVERED 10-15 TEETH STRIPPED ON DISTRIBUTOR GEAR. VERY COLD TEMP, PROBABLE CAUSE. (SW01200603303) (K) 1L72 3O3 O A7CE E8CE 20060131001862006013100186SO 2006 1 31 SIMA200535512 120051213A5320 FLOOR SUPPORT EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21611AE 145074 DURING CPCP INSPECTION FOUND PROFILE ON TOP OF CENTER OMEGA BEAM BETWEEN FRAMES 59-60 HAS SPOTS OF CORROSION. REPAIRED PROFILE IAW IC 2005-145/6986. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4F4 FRTT00011ATTE6CH 20060131001942006013100194EU 2006 1 31 SIMA200600302 120051223A5512725510521 SKIN SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LT HORIZ STAB DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21317AE21509 340B317 HAIL DAMAGE ON THE LT HORIZONTAL STABILIZER TOPSKIN. REMOVED THE EXISTING LT HORIZONTAL STAB TOP SKIN PANEL. POSITIONED NEW LT HORIZONTAL STABILIZER SKIN. MARKED AND DRILLED FASTENER HOLES. REPOSITIONED AND INSTALLED SKIN. REPAIR DONE IAW SRM. (K) 2L72 4T4 TRTA52EU E8NE 20060131001962006013100196EU 2006 1 31 SIMA200600304 120051219A53117252813485 FRAME SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE BS 677 DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21317AE21509 340B317 THE RT SIDEWALL CARGO FRAME AT STA 677 WAS FOUND TO BE DENTED. RECONTOURED THE DENT. PREPARED A REPAIR ANGLE. REPAIR DONE IAW SRM. (K) 2L72 4T4 TRTA52EU E8NE 20060131001972006013100197SO 2006 1 31 SIMA200600306 120051227A532014521725023 SILL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21662EH 145777 DURING CPCP INSPECTION FOUND FORWARD SERVICE DOOR SILL PLATE CORRODED. INSTALLED NEW SILL PLATE IAW EMB SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4T4 FRTT00011ATTE6CH 20060131002002006013100200NE 2006 1 31 ZES2006F00000 220051225A732131J234712 FCU CESSNA500 550 2076604CE PWA 530 PW530A NE LT ENGINE UNSERVICEABLE E ZESAO OTHER O OTHER NRNOT REPORTED 1 EA03630JS47 5501119 PCEDA0654 AFTER DECENDING FROM ALTITUDE, LT ENGINE WOULD NOT ACCELERATE AND REMAINED AT IDLE. PILOTS LANDED THE AIRCRAFT WITHOUT INCIDENT. REMOVED AND REPLACED THE FUEL CONTROL UNIT. OPS CHECKED, OK. (EA03200603629) (K) 1L72 4F4 F A22CE E00053EN 20060206001182006020600118EA 2006 2 6 QXEA200600220 120051207A5310 CROSSBEAM CNDAIRCL600 CL6002C10 1390015EA BS 280 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - CROSS BEAM AT FS 280 HAS SPOTS OF CORROSION AROUND ANCHOR NUT HOLES. CROSS BEAM AT FS 280 CORROSION REMOVED IAW REO 670-53-11-046 REV A REMAINING THICKNESS .037 OVER BLENDED AREAS. AREA TREATED PRIMED AND PAINTED IAW SRM 51-21-16. 2L72 4F RTA21EA 20060131002042006013100204EU 2006 1 31 SIMA200600902 120051228A53117255150522 FRAME SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE BS 236 DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21317AE21509 340B317 FUSELAGE FRAME AT STA 236 WAS FOUND TO BE CRACKED AT THE END OF A PREVIOUS REPAIR. REMOVED THE PREVIOUS REPAIR, EXTENDED THE CUT OUT TO REMOVE THE CRACK. FABRICATED A FILLER AND DOUBLER. REPAIR DONE IAW SRM. (K) 2L72 4T4 TRTA52EU E8NE 20060131002122006013100212EU 2006 1 31 O2G2006F00000 120051215A2131219922 CONTROLLER ISRAELGALAXYGALAXY 4500307EU CABIN PRESSURE FAILED E O2GAO OTHER O OTHER NRNOT REPORTED 1 NE0348GX 017 AT FL370 AUTO PRESSURIZATION FAILED IN AUTO MODE. CAPTAIN DEPLOYED MASK AND SWITCHED TO MANUAL MODE AND RECOVERED CABIN ALTITUDE. COULD NOT CONTROL CABIN ALT PRESSURE IN MANUAL. CHANGED PRESSURE CONTROLLER AND FOUND LOOSE DUCT IN CABIN UNDER FLOOR AREA THAT WAS SEVERED AS WELL. (K) 2L72 4F RTA53NM 20060131002132006013100213NM 2006 1 31 AMTA200501219 120051223A5320 FLOOR SUPPORT BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE BS 1445-4590 CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11517AT 27973 AFT PIT FLOOR SUPPORT HAS SURFACE CORRODED STA 1445 TO STA 1490 LBL 2.5. REMOVED AND REPLACED FLOOR SUPPORT SECTION FROM STA 1445 TO STA 1490 IAW SRM. (K) 2L72 4F4 FRTA2NM E12EU 20060206001192006020600119EA 2006 2 6 QXEA200600213 120051207A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 350-485 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - RT FLOOR SEAT RAIL FS 350.0-485.0 P/N SH670-32159-1 HAS AREAS ON CORROSION BLENDED ALL DAMAGE TO A SMOOTH CONTOUR IAW REO 670-53-00-013 REV A STEP 1. ALODINED REWORKED AREAS PER SRM 51-21-16 IAW REO 670-53-00-01B REV A STEP 3. IDENTIFIED SEAT TRACKS IAW REO 670-53-00-013 REV A STEP 9. COMPLIED WITH STEPS 2 AND STEPS 4 THRU 8 IAW REO 670-53-00-013 REV A. 2L72 4F RTA21EA 20060131002582006013100258NM 2006 1 31 UPS06M46063 120051121A5347AFA7789542 SEAT TRACK DOUG MD11 MD11F 3023600NM BS 1961 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01282UP 48452 INSPECTION TYPE:C AFT CABIN-CORROSION ON SEAT TRACK FLANGE AT STA 1961 X=-107. NR 4 DR RT SILL PLATE REPLACED FOR SEAT TRACK REPAIR REPLACE PER AMM20-50-0 2R.50.SEAT TRACK AT STA 1961 X=-107. REMOVED PER SRM 51-21-01V.2R.37. FOUND OUT OF LIMIT .ORI THK 0.08 INCH AND MAT REMOVED 0.046 INCH. SEAT TRACK REMOVED PER SRM 51-31-01V.2R.37. HEFC INSP AND NDT PER SPM REV 12 C/OUT. FOUND NO CRACK EVIDENT. NEW SEAT/T INSTALLED PER SRM 53-70-00 V.1 REV.38-SATIS. 2L73 4F RTA22WE 20060131002592006013100259NM 2006 1 31 UPS06M46064 120051121A5347AFA7789547 SEAT TRACK DOUG MD11 MD11F 3023600NM BS 1961 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01282UP 48452 INSPECTION TYPE:C AFT CABIN, CORROSION ON SEAT TRACK AT STA 1961 X=107. NR 4 DR LT SILL PLATE REMOVED FOR SEAT REMOVED FOR REPAIR AND REPLACEMENT OF SEAT TRACK PER AMM20-50-02 R.50. CORROSION FOUND OUT OF LIMIT PER SRM 51- 21-01V.2.37. MAT REMOVED 0.043" AND ORI THK 0.145".SEAT TRACK REMOVED PER SRM 51-31-01V2R37. HFEC INSP AND NDT SPM C/OUT FOUND NO EVIDENT OF CRACK. NEW SEAT TRACK INSTALLED PER SRM 53-70-00 F.7.V1.7.R.38, FOUND SATIS. 2L73 4F RTA22WE 20060130001952006013000195NM 2006 1 30 SWAA051131 120050417A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 727E CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727 E, STR 5R & STR 3L. REMOVED AND REPLACED CLIPS PER SRM. 2L72 4F RTA16WE 20060131000022006013100002NM 2006 1 31 SWAA051422 120050516A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 706 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 706, STR 11L & STR 11R. REMOVED AND REPLACED CLIPS PER SRM. 2L72 4F RTA16WE 20060131000072006013100007NM 2006 1 31 SWAA051662 120050605A53156546804 FLOORBEAM BOEING737 7377H4 1384404NM BS 727D CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29771SA 27879 DURING SCHEDULED 5Y CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 727D, BETWEEN LBL 8 TO RBL 8. REPAIRED FLOORBEAM PER SWA EA. 2L72 4F RTA16WE 20060131000172006013100017NM 2006 1 31 SWAA051923 120050704A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 727A CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29332SW 23696 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25R & STR 26L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20060131000282006013100028NM 2006 1 31 SWAA052122 120050720A53116546500 FRAME BOEING737 7373H4 1384600NM BS 727D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29609SW 27929 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, BETWEEN STR 8L & STR 9L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20060131000422006013100042NM 2006 1 31 SWAA052072 120050715A53116546529 FRAME BOEING737 7373H4 1384600NM BS 400 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29613SW 27931 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R TO STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20060131001322006013100132NM 2006 1 31 AWXA200600140 120051223A531165163019 FRAME BOEING737 73733A 1384673NM BS 188 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED BS 188 FRAME CRACKED, .25 INCHES, AT WL 207 AND BL 30L. MAINTENANCE CUT OUT AND REMOVED DAMAGED PORTION OF FLANGE AND CHORD FLANGE FROM BS 188 FRAME IAW BOEING 737-300 SRM 53-00-07-2R11 FIG 201. FABRICATED REPAIR ANGLE AND FILLERS IAW BOEING 737-300 SRM 53-00-07-2R11. INSTALLED FABRICATED REPAIR PARTS AT BS 188 FRAME, WL 207 AND BL 30L IAW BOEING 737-300 SRM 53-00-07-2R11. 2L72 4F RTA16WE 20060131001662006013100166SO 2006 1 31 SIMA200535509 120051212A532014521725401 FLOOR SUPPORT EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21611AE 145074 DURING HMBV INSPECTION FOUND AFT CARGO FLOOR SUPPORT AT FRAME 71 RT HAS CORROSION. INSTALLED NEW FLOOR SUPPORT IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4F4 FRTT00011ATTE6CH 20060131001712006013100171SO 2006 1 31 SIMA200536102 120051220A532014521718005 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21660CL 145764 DURING CPCP INSPECTION FOUND LT OMEGA BEAM AT FRAME 20 CORRODED. REPAIRED OMEGA BEAM BY INSTALLING A DOUBLER IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4T4 FRTT00011ATTE6CH 20060131001792006013100179SO 2006 1 31 SIMA200535511 120051212A534714530659011 SEAT TRACK EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21611AE 145074 DURING CPCP INSPECTION FOUND LT FWD IB SEAT TRACK IS CORRODED. REPLACED SEAT TRACK IAW EMB SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4F4 FRTT00011ATTE6CH 20060131001812006013100181SO 2006 1 31 SIMA200535505 120051214A532014522178005 SILL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21664MS4753 145779 THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. BLENDED THE CORRODED AREA. CLEANED AND TREATED THE BLENDED AREA AND FILLED WITH EPOXY RESIN EA934A. FABRICATED 2 REPAIR DOUBLERS. REPAIR DONE IAW EMB SRM. (K) 2L72 4T4 FRTT00011ATTE6CH 20060131001842006013100184EU 2006 1 31 SIMA200600905 120051219A53117253150522 FRAME SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE BS 258 DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21317AE21509 340B317 THE FUSELAGE FRAME AT STA 258 WAS FOUND TO BE CORRODED. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED A FILLER AND REPAIR ANGLE. REPAIR DONE IAW SRM. (K) 2L72 4T4 TRTA52EU E8NE 20060131001872006013100187SO 2006 1 31 SIMA200535507 120051212A532014521713005 FLOOR SUPPORT EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21611AE 145074 DURING CPCP INSPECTION FOUND CENTER HAT BEAM UPPER PROFILE HAS SPOTS OF CORROSION FROM FRAMES 19 TO 23. REPLACED GUSSET IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4F4 FRTT00011ATTE6CH 20060131001892006013100189SO 2006 1 31 SIMA200600308 120051228A532014521713003 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21662EH 145777 DURING CPCP INSPECTION FOUND OMEGA BEAM AT FRAME 20 IS CORRODED. REPAIRED OMEGA BEAM BY INSTALLING A DOUBLER IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4T4 FRTT00011ATTE6CH 20060131001952006013100195EU 2006 1 31 SIMA200600305 120051228A53117253620187 LONGERON SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LT NACELLE PUNCTURED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21317AE 340B317 PUNCTURE ON THE LT NACELLE OB LWR LONGERON. PERFORMED A CUTOUT TO REMOVE THE DAMAGE. FABRICATED AN ANGLE DOUBLER FOR REPAIR. REPAIR DONE IAW SRM. (K) 2L72 4T4 TRTA52EU E8NE 20060131002172006013100217NE 2006 1 31 7272005N234CA 220050727A7200 ENGINE AMD FALC20FALCON 2720302EU GE CF700 CF7002D2 30010NE NR 1 BIRD INGESTION E CEDAA UNSCHED LANDING CJ F.O.D. WARNING INDICATION CLCLIMB 1 SW05234CA 17 ON TAKEOFF FROM NR 1 ENGINE INGESTED A BIRD. THIS OCCURRED AFTER V1. JUST AFTER ROTATION THE NR1 ENGINE QUIT. IT WAS RESTARTED AND THE AIRCRAFT CLIMBED TO THE ASSIGNED ALTITUDE. THE CREW NOTIFIED THE TOWER AND RETURNED TO DEPARTURE. (K) 2L72 4F4 F A7EU E7EA 20060131002242006013100224WP 2006 1 31 05FDEA04278 120051213A5101 REPAIR DOUG DC10 DC1010 3022110WP FUSELAGE NONE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25563FE 46948 LOWER FUSELAGE FWD PRESSURE BULKHEAD PANEL HAS A WEB REPAIR ON RIGHT SIDE AT STA 1156 BETWEEN 39 TO 42 DIM 12 X 18 INCHES, 20 X 28 INCHES, 20 X 28 INCHES. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 53-40-00 FIG 4A VOL 1 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P1. 2L73 4F A22WE 20060131002392006013100239NM 2006 1 31 05FDEA04336 120051215A5100 NONE BOEING727 727200 138407ENM NONE NONE A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25274FE 22039 FOUND PREVIOUSLY REPAIR AT RT WING NR 6 KRUEGER FLAP WAS ACCOMPLISHED IAW SRM 57-50-3 FIG 2 BASED ON AN EXTERNAL EVALUATION CONSISTED OF LOCATION, SHAPE, SIZE, NUMBERS OF FASTENER AND SPACING, MATERIAL THICKNESS AND GENERAL WORKMANSHIP AND REPAIR IS CLASSIFIED AS MAJOR REPAIR. 2L73 4F RTA3WE 20060201000062006020100006NE 2006 2 1 DL76G060039 220050112A7200CF680C2B6F ENGINE BOEING767 767332 1382001NM GE CF6 CF680C2B6F 30025NE NR 1 MAKING METAL A DALAK NONE J WARNING INDICATION ININSP/MAINT 1 SO271609 2456721873 30574 706114 DURING L/O FOUND METAL IN THE LT ENG MASTER CHIP DETECTOR. REPLACED ENGINE. 2L72 4F4 FRTA1NM E13NE 20060201000222006020100022EA 2006 2 1 SWIA200516155 120051022A5720 ANGLE CNDAIRCL600 CL6002B19 1900309EA LT MLG WW CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07595SW 7292 LEFT WHEEL WELL BAT ANGLE CRACKED, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED ANGLE DOUBLER PER REO 601R-57-51-046 STEP 5-8 REV B. 2L72 4F RTA21EA 20060201000232006020100023EA 2006 2 1 SWIA200516156 120051105A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07597SW 7293 AFT FLOOR ANGLE CRACKED FS 280 LBL 11, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED ANGLE PER REO 601R-53-11-138 AND SRM CRJ200 51-31-06 PG 1 PARA 3 PG 3. 2L72 4F RTA21EA 20060201000732006020100073NM 2006 2 1 P5CA0601428 120050107A3030 ANTI-ICE SYSTEM BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE PITOT PROBE NO TEST A P5CAK NONE L NO TEST ININSP/MAINT 1 EA15858FT 20109 DURING CREW PRE-FLIGHT, FOUND LT UPPER PITOT STATIC PROBE HEAT WOULD NOT TEST. REPLACED PITOT PROBE IAW AMM 34-11-01. 2L74 4F4 F A20WE E20EA 20060201001112006020100111WP 2006 2 1 IXXA05SMN269S 120051215A5210 SKIN DOUG DC8 DC872 302199BWP ZONE 800 DAMAGED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11722CX71621 46130 DURING ROUTINE C-CHECK INSP, LT FWD PASSENGER DOOR DAMAGE. SKIN AT REAR LOWER CORNER HAS BEEN DAMAGED (INCH LONG CUT), NEED TO BE REPAIRED PERFORMED REPAIR IAW AD 2000-20-08, S/B 53-075, DWG NR SR08530021, 5750776, SRM 53-2-0 FIG. 15. TR NR 53-128, 53-196 DATED 01-23-02, 03-26-04. CUT OUT DAMAGED IAW RM 53-2-0 FIG. 15 (SHEET 1) TR NR 53-128. PERFORMED NDT INSP IAW SPM PART 06-10-01-001. FAB REPAIR DOUBLER (ALCLAD 7075 T6 0.063) + REPAIR TRIPLER (ALCLAD 7075 T6 0.080) + FILLER (ALCLAD 7075 T6 0.050) IAW SRM FIG. 185 (SHEET 1), TR NR 53-128, TR NR 53-196. CLEANED, TREATED AND PRIMED AREA + REPAIR PARTS IAW SRM. APPLIED SEALANT TO FAYING SURFACES IAW SRM. INSTALLED REPAIR PARTS IAW SRM. (TORQUE) 2L74 4F RT4A25 20060201001122006020100112WP 2006 2 1 IXXA05SMN273S 120051215A5753 SKIN DOUG DC8 DC872 302199BWP XF 212.000 CRACKED B IXXAO OTHER O OTHER ININSP/MAINT 1 SW11722CX 46130 DURING ROUTINE C-CHECK INSPECTION, LT OB FLAP SKIN CRACKED .5, STA XF 212.000 PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG. 2Q, EO NR 20051445 DATED 12-15-051. REMOVED FASTENERS IAW SRM 51-1-21. REMOVED DAMAGED SECTION IAW SRM 57-2-1 FIG. 2Q. FABRICATED EXTERNAL REPAIR DOUBLER (ALCLAD 2024 T3 0.050) IAW SRM 57-2-1 FIG. 2Q, SRM 57-7-1 FIG. 4, TR NR 57-94 ITEM (C) DATED 18-01-02. CLEANED, TREATED AND PRIMED AREA + EXTERNAL REPAIR DOUBLER IAW SRM 51-1-8B. INSTALLED EXTERNAL REPAIR DOUBLER IAW SRM 57-2-1 FIG. 2Q, SRM 51-1-9 (HYSOL), SRM 51-1-21. 2L74 4F RT4A25 20060201001142006020100114WP 2006 2 1 IXXA05SMN278S 120051216A5210 SKIN DOUG DC8 DC872 302199BWP ZONE 800 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11722CX71621 46130 DURING ROUTINE C-CHECK INSPECTION, FWD PASSENGER DOOR LWR SKIN CRACKED 1 INCH APPROX. PERFORMED MAJOR REPAIR IAW SRM 52-2-0 FIG. 4 (SHEET 3). REMOVED FASTENERS IAW SRM 51-1-21. FABRICATED REPAIR DOUBLER (ALCLAD 7075 T6 0.050”) IAW SRM 52-2-0 FIG. 4 (SHEET 3), SRM 52-3-2 FIG. 1 ITEM L, SRM 51-9-0 FIG. 68A PAGE 10A. CLEANED, TREATED AND PRIMED AREA + REPAIR DOUBLER IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11. INSTALLED REPAIR DOUBLER IAW SRM 52-2-0 FIG. 4 (SHEET 3), SRM 51-1-21. 2L74 4F RT4A25 20060201001272006020100127WP 2006 2 1 IXXA05SMN288S 120051229A5311 FRAME DOUG DC8 DC872 302199BWP BS 255.000 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11722CX71621 46130 DURING ROUTINE C-CHECK INSP, FWD ACCY COMPT INTERNAL PART BETWEEN L-25L AND L-24L, AT STA 255.000 HAS FRAME CRACKED (1.5 INCH). PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG.74 (SHEET 1,3). REMOVED FASTENERS IAW SRM 51-1-21. REMOVED DAMAGED SECTION. FABRICATED EXTERNAL REPAIR DOUBLER (ALCLAD 7075 T6 0.071) AND (02 EA) INTERNAL FINGER DOUBLER (ALCLAD 7075 T6 0.040”) IAW SRM 53-2-1 FIG. 7 (SHEET 1,3), SRM 53-4-1 FIG. 5 ITEM B, SRM 51-9-0 FIG. 68A. CLEANED, TREATED AND PRIMED AREA + REPAIR DOUBLER IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PAGE 9. INSTALLED REPAIR DOUBLER IAW SRM 53-2-1 FIG. 7 (SHEET 1,3), SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2L74 4F RT4A25 20060201001302006020100130WP 2006 2 1 IXXA05SMN297S 120051229A5730 REPAIR DOUG DC8 DC872 302199BWP XW 762.000 MISINSTALLED B IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW11722CX71621 46130 DURING ROUTINE C CHECK INSPECTION, LT WING.- OB L/E HAS NON STANDARD REPAIR, XW 762.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 06006 DATED 01-05-06 REMOVED NON-STANDARD REPAIR IAW SRM 51-1-21, SRM 51-1-20D DC8 SRM 51-3-0 REMOVED DAMAGED SECTION IAW DWG NR ED-4128 PERFORMED NDT INSP IAW NDT SPM PART 06-10-01-001 FABRICATED REPAIR DOUBLER (AL7075T60.063) FILLER (AL7075T60.050) IAW DWG NR ED-4128 CLEANED TREATED; PRIMED AREA, FILLER, REPAIR DOUBLER INNER FACE IAW SRM 51-1-8B APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 INSTALLED REPAIR PARTS IAW DWG NR ED-4128, SRM 51-1-21, SRM 51-1-20D, SRM 51-3-0, SRM 51-3-1 (TORQUE). 2L74 4F RT4A25 20060201001322006020100132WP 2006 2 1 IXXA05SMN308S 120051229A5313 LONGERON DOUG DC8 DC872 302199BWP BS 1617 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11722CX71621 46130 DURING ROUTINE C-CHECK INSPECTION, AFT FUS CRACKED 2, STA FS 1617.000 L.17R. PERFORMED MAJOR REPAIR IAW SRM 53-5-2 FIG. 5. REMOVED CRACKED L-17R IAW SRM 53-1-0, SRM 51-1-20D. FABRICATED NEW LONGERON (EXTRUSION P/N S1616757) IAW SRM 53-5-2 FIG. 5 (SHEET 1) ITEM B, SRM 51-2-0 FIG. 50. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PAGE 9. INSTALLED NEW LONGERON IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2L74 4F RT4A25 20060131000122006013100012NM 2006 1 31 SWAA051756 120050615A53206545410 FLOOR SUPPORT BOEING737 7373H4 1384600NM BS 706-707 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL FLOOR SUPPORT CRACKED AT BS 706 TO BS 707, LBL 25, WL 204. REPAIRED FLOOR SUPPORT PER BFG ER. 2L72 4F RTA16WE 20060131000132006013100013NM 2006 1 31 SWAA051779 120050619A53116546554 FRAME BOEING737 7373H4 1384600NM BS 727E CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727E, STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20060131000252006013100025NM 2006 1 31 SWAA051956 120050705A53116546539 FRAME BOEING737 7373H4 1384600NM BS 616 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29608SW 27928 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CHORD CRACKED AT BS 616, BETWEEN LBL 63 + RBL 63, WL 201. REPAIRED FRAME CHORD PER BFG ER. 2L72 4F RTA16WE 20060131000352006013100035NM 2006 1 31 SWAA052180 120050725A53226546529 SHEAR TIE BOEING737 7373H4 1384600NM BS 500A CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29610WN 27696 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500A, BETWEEN STR 28L & STR 28R. REMOVED AND REPLACED SHEAR TIE PER MM. 2L72 4F RTA16WE 20060131000372006013100037NM 2006 1 31 SWAA051995 120050708A53116546550 FRAME BOEING737 7373H4 1384600NM BS 787 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29608SW 27928 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20060131000402006013100040 2006 1 31 SWAA052023 420050711A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29634SW 27937 DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20060131000682006013100068EA 2006 1 31 ASOA051080 120051210A33979891705501 WIRE HARNESS CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT DISCONNECTED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27710EV 10071 DURING A HANGAR INSPECTION IN MCN, THE EMERGENCY EXIT LIGHT, ON THE FORWARD LEFT WINDSCREEN, WAS FOUND TO BE INOPERATIVE. MAINTENANCE RECONNECTED THE EMERGENCY EXIT LIGHT HARNESS ASSEMBLY. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060131001352006013100135EU 2006 1 31 UPS06146001 120051228A5410A5451506320400 STRUCTURE AIRBUSA300 A300F4622R 3930360EU NR 2 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01137UP 0820 INSPECTION TYPE:5YR NR 2 ENG AFT LWR PYLON MEMBER SECTION IS CRACKED IN 2 EA PLACES RT AND LT AT JOGGLE. REMOVED AND REPLACED MEMBER SECTION IAW SRM 51-40-00. 2L72 4F RTA35EU 20060131001822006013100182SO 2006 1 31 SIMA200535508 120051212A532014521713005 FLOOR SUPPORT EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21611AE 145074 DURING CPCP INSPECTION FOUND OMEGA BEAM DOUBLER AT FRAME 20 IS CORRODED. REPLACED DOUBLER IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4F4 FRTT00011ATTE6CH 20060131001882006013100188SO 2006 1 31 SIMA200600307 120051228A533014564090001 SKIN EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21662EH 145777 DENTS IN LT REAR FUSELAGE LOWER SKIN. REPAIRED DENTS IAW EO EM-53MR-535R2 BY CUTTING OUT DAMAGE AND INSTALLING AN EXTERNAL DOUBLER. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4T4 FRTT00011ATTE6CH 20060131002012006013100201SO 2006 1 31 SIMA200535302 120051216A3242179814 BRAKE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL RT MLG SEIZED A SIMAK NONE O OTHER LDLANDING 1 SW21654AE 145437 DURING LANDING CREW REPORTED BRAKES PULL TO RIGHT. DURING ROLL OUT, REPORTED THUMPING ON RT SIDE OF AIRCRAFT. MAINTENANCE REPORTED THAT BOTH NR 3 AND 4 BRAKES WERE SEIZED. REPLACED BOTH RT MLG WHEEL AND TIRE ASSEMBLIES AND BOTH BRAKES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (K) 2L72 4T4 FRTT00011ATTE6CH 20060131002022006013100202SO 2006 1 31 SIMA200600301 120051221A532014521713005 SILL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21667GB4669 145784 THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. BLENDED THE CORRODED AREAS TO REMOVE THE DAMAGE. APPLIED ALODINE, EPOXY PRIMER AND POLYURETHANE TOP COAT TO THE REWORKED AREAS. FABRICATED 3 REPAIR DOUBLERS. REPAIR DONE IAW SRM. (K) 2L72 4T4 FRTT00011ATTE6CH 20060131002102006013100210EU 2006 1 31 KBM2006F00032 120051204A282355103G SHUTOFF VALVE SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1D NE FUEL SYSTEM INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1953SH 9617 2009 FUEL SHUTOFF VALVE INOPERATIVE, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20060201000212006020100021EA 2006 2 1 SWIA200516154 120051022A5312 ANGLE CNDAIRCL600 CL6002B19 1900309EA BULKHEAD CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07595SW 7292 AFT PRESSURE BULKHEAD AFT SIDE; 2 ANGLES ARE CRACKED; 1 AT LBL40 AND 1 AT 4BL40 WL90 FS 625, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED LEFT HAND AFT PRESSURE BULKHEAD ANGLE PER 601R-35012 AND REO 601R-53-61-422. INSTALLED RIGHT HAND AFT PRESSURE BULKHEAD ANGLE PER 601R-35012 AND REO 601R-53-61-422. 2L72 4F RTA21EA 20060201000242006020100024EA 2006 2 1 SWIA200516157 120051105A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA BS 625 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07597SW 7293 CLIP ON LT SIDE FS625 CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED FS 625 LT CLIP IAW CRJ200 SRM 51-24-16 PG 1-7 51-42-06 PG 1-18. 2L72 4F RTA21EA 20060201000452006020100045EU 2006 2 1 UPS06145999 120051231A5311A5381337900040 FRAME AIRBUSA300 A300F4622R 3930360EU FR 52 LT DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01137UP 0820 INSPECTION TYPE:2C MAIN CARGO COMPARTMENT FLOOR FRAME 52 BTWN FLOOR PNL 242EK AND 242ZJ FRAME DAMAGED PN 99589. REMOVED AND REPLACED FRAME IAW SRM 51-40-00. 2L72 4F RTA35EU 20060201000742006020100074WP 2006 2 1 IXXA05SMN309S 120051229A5313 LONGERON DOUG DC8 DC872 302199BWP BS 1617 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11722CX71621 46130 DURING ROUTINE C CHECK INSPECTION, AFT FUSELAGE.- CRACKED 3, L-17L STA 1617.000. PERFORMED MAJOR REPAIR IAW SRM 53-5-2 FIG. 5. REMOVED CRACKED L-17L IAW SRM 53-1-0, SRM 51-1-20D. FABRICATED NEW LONGERON (EXTRUSION P/N S1616757) IAW SRM 53-5-2 FIG. 5 (SHEET 1) ITEM B, SRM 51-2-0 FIG. 50. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PAGE 9. INSTALLED NEW LONGERON IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2L74 4F RT4A25 20060201001132006020100113WP 2006 2 1 IXXA05SMN277S 120051216A5210 REPAIR DOUG DC8 DC872 302199BWP ZONE 800 MISINSTALLED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11722CX71621 46130 DURING ROUTINE C-CHECK INSPECTION, REPAIR ON EXT SKIN OF FWD PASSENGER DOOR HAS IMPROPER FASTENERS PERFORMED MAJOR REPAIR IAW SRM 52-2-0 FIG. 4 (SHEET 3). REMOVED EXISTING REPAIR IAW SRM 51-1-21. FABRICATED REPAIR DOUBLER (ALCLAD 7075 T6 0.050”) IAW SRM 52-2-0 FIG. 4 (SHEET 3), SRM 52-3-2 FIG. 1 ITEM L, SRM 51-9-0 FIG. 68A. CLEANED, TREATED AND PRIMED AREA AND REPAIR DOUBLER IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11. INSTALLED REPAIR DOUBLER IAW SRM 52-2-0 FIG. 4 (SHEET 3), SRM 51-1-21. 2L74 4F RT4A25 20060201001752006020100175NM 2006 2 1 2005000016 120051213A5220140N2640 GUIDE ARM BOEING757 757200 1384950NM RROYCERB211 RB211535E4 54555NE EMERGENCY DOOR OUT OF ADJUST A CNMAK NONE O OTHER ININSP/MAINT 1 SW07549AX 24528 NR 2 RT ENTRY DOOR FAILED TO FULLY OPEN DURING EVACUATION TEST. PERFORMED COMPLETE DOOR ADJUSTMENT TEST AND ADJUSTED R2 DOOR IAW MM 52-11 PERFORMED OPERATIONAL TEST OF R2 DOOR SLIDE IAW OAI CARD NR 75TC-0890. THE ROOT CAUSE FOR THE FAILURE TO DEPLOY WAS THAT THE DOOR WAS OBSTRUCTED BY THE LOWER SLIDE SKIRT WHEN ATTEMPTING TO DEPLOY SLIDE. ADJUSTMENTS WERE MADE TO THE GUIDE ARM TO ALLOW FOR ADDITIONAL CLEARANCE FOR THE DOOR TO COCK OPEN ENOUGH TO ALLOW CLEARANCE FOR THE LOWER SLIDE SKIRT. NOTE: AIRCRAFT DOOR WAS WITHIN MM LIMITS BOTH BEFORE AND AFTER RIGGING. 2L72 4F4 FRTA2NM E12EU 20060201001852006020100185EU 2006 2 1 UPS06146000 120051228A5410A5451506320300 STRUCTURE AIRBUSA300 A300F4622R 3930360EU PWA 4158 PW4158 NE NR 2 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01137UP 0820 5YR N2 ENG AFT LWR PYLON MEMBER SECTION IS CRACKED IN 2 EA PLACES RT AND LT AT JOGGLE. REMOVED AND REPLACED RT AND LT MEMBER SECTIONS IAW SRM 51-40-00. 2L72 4F4 FRTA35EU E24NE 20060202000212006020200021 2006 2 2 AALA20060062 420051208A25655A33073 SLIDE BOEING737 737823 13844BZNM R2 DOOR INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21902AN 29504 TUL - EMERGENCY RIGHT AFT SERVICE DOOR SLIDE DID NOT DEPLOY AUTOMATICALLY WHEN DOOR WAS OPENED DURING CHECK. DID DEPLOY MANUALLY. REPLACED EMERGENCY RIGHT HAND AFT SERVICE DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20060202000322006020200032SO 2006 2 2 MASA200500803 120051014A335078241 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSINOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07831MJ 145273 ASH 2984 CLT - AFT THREE EMERGENCY FLOOR PROXIMITY LIGHT STRIPS INOP. MX ISOLATED THE PROBLEM TO THE INVERTER. MAINTENANCE REPLACED THE INVERTER. 2L72 4T RTT00011AT 20060202000332006020200033SO 2006 2 2 MASA200500819 120051022A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSINOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07843MJ 145478 DURING THE WALK AROUND IT WAS DISCOVERED THE LT FWD EXTERIOR EMERGENCY LIGHT NOT ILLUMINATING. REPLACED THE LIGHT BULB AFTER TROUBLESHOOTING. OPERATIONAL CHECK GOOD. 2L72 4T RTT00011AT 20060202000342006020200034SO 2006 2 2 MASA200500835 120051026A3397 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSLOOSE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07837MJ 145367 ASH 2739 CLT - THE EMERGENCY EXIT FLOOR PATH LIGHTING INOP. MAINTENANCE FOUND AND RESECURED A LOOSE CONNECTOR ON THE TRACK. 2L72 4T RTT00011AT 20060202000352006020200035SO 2006 2 2 MASA200500855 120051103A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSINOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07854MJ 145490 THE AIRCRAFT WAS ON RON LAST NIGHT AND SCHEDULED FOR A EN ROUTE CHECK INSPECTION. DURING THE WALK AROUND IT WAS DISCOVERED THE RT AFT EXTERIOR EMERGENCY LIGHT NOT ILLUMINATING. REPLACED THE LIGHT BULB AFTER TROUBLESHOOTING. OPERATIONAL CHECK GOOD. 2L72 4T RTT00011AT 20060202000542006020200054SO 2006 2 2 MASA200501091 120051228A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07838MJ 145384 ASH 2848 CLT - 2 EMERGENCY FLOOR PROX LIGHTS INOP FWD CABIN. OPS CHECK GOOD. 2L72 4T RTT00011AT 20060202000702006020200070SO 2006 2 2 MASA200500895 120051116A3397 GROUND WIRE EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSDISCONNECTED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07858MJ 145767 ASH 2896 CLT, EMERGENCY LIGHT INOP RT OVERWING AND SERVICE DOOR. MAINTENANCE RECONNECTED GROUND WIRE. 2L72 4T RTT00011AT 20060202000792006020200079NM 2006 2 2 AALA20060058 120051207A3350BPS73 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21642AA 24600 AFW - LEFT WING FORWARD EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR LEFT WING FORWARD EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20060202001072006020200107CE 2006 2 2 CED2006F00014 120050519A2612872281 ELEMENT LEAR 25 25 5170506CE GE CJ610 CJ6106 30006NE FIRE DETECTOR FALSE INDICATIONE CEDAO OTHER O OTHER NRNOT REPORTED 1 SW05273CA 039 251622A AFTER TAKEOFF AT FLIGHT LEVEL 220, THE CREW OBSERVED A FIRE INDICATION LIGHT ON THE NR 1 ENGINE. THE FLIGHT CREW FOLLOWED STANDARD EMERGENCY PROCEDURES AND RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. ONCE BACK, MAINTENANCE FOUND THE FIRE LOOP ELEMENT TOUCHING THE COWLING GIVING A FALSE FIRE INDICATION. (K) 2L72 4J4 J A10CE 1E16 20060202001092006020200109EU 2006 2 2 CED2006F00001 120050618A3260A23870101 SQUAT SWITCH AMD FALC20FALCON 2720302EU GE CF700 CF7002D2 30010NE RT MLG OUT OF ADJUST E CEDAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SW05209CA 71 304529B AFTER INITIATING TAKEOFF ROLL THE FLIGHT CREW RECEIVED A CABIN PRESSURIZATION WARNING HORN, THE FLIGHT CREW ABORTED TAKEOFF WITHOUT INCIDENT. MAINTENANCE FOUND A LANDING GEAR SQUAT SWITCH OUT OF ADJUSTMENT. (K) 2L72 4F4 F A7EU E7EA 20060202001112006020200111CE 2006 2 2 CED2006F00000 120051101A2720 RUDDER PEDAL LEAR 25 25B 5170511CE GE CJ610 CJ6106 30006NE COCKPIT STIFF E CEDAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SW05233CA 133 251397A THE FLIGHT CREW ABORTED TAKEOFF ROLL. THE FLIGHT CREW NOTICED ON TAKEOFF ROLL THAT THE RUDDER PEDALS FELT STIFF AND HAD VERY LITTLE MOVEMENT. MAINTENANCE INSPECTED AIRCRAFT RUDDER CONTROL CABLE SYSTEM AND FOUND NO DEFECTS. (K) 2L72 4J4 J A10CE 1E16 20060202001122006020200112EU 2006 2 2 CED2006F00002 120051102A2131133007 CONTROLLER AMD FALC20FALCON 2720302EU GE CF700 CF700* 30010NE CABIN PRESSURE DEFECTIVE E CEDAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW05207CA 153 304408B WHEN ENROUTE, THE AIRCRAFT CABIN PRESSURIZATION WARNING LIGHT AND HORN CAME ON. THE FLIGHT CREW RETURNED, WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE PRESSURIZATION SYSTEM AND FOUND THE PRESSURIZATION CONTROLLER TO BE MALFUNCTIONING AND REPLACED THE DEFECTIVE CONTROLLER. (K) 2L72 4F4 F A7EU E7EA 20060202001132006020200113CE 2006 2 2 CED2006F00007 120050614A3244301345870 TIRE LEAR 25 25B 5170511CE GE CJ610 CJ6106 30006NE LT MLG DESTROYED E CEDAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SW05236CA 161 ON TAKEOFF ROLL THE AIRCRAFT BLEW THE LT MAIN GEAR TIRES IN ELP. (K) 2L72 4J4 J A10CE 1E16 20060202001142006020200114EU 2006 2 2 CED2006F00003 120050802A3210 LANDING GEAR AMD FALC20FALCOND 2720304EU GE CF700 CF7002D2 30010NE INOPERATIVE E CEDAO OTHER J WARNING INDICATION DEDESCENT 1 SW05219CA 193 ON DECENT, LANDING GEAR WOULD NOT EXTEND WITH NORMAL PROCEDURES. THE FLIGHT CREW DECLARED AN EMERGENCY AND DEPLOYED THE LANDING GEAR USING PROCEDURE B AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE IS ENROUTE TO THE AIRCRAFT, THE SPECIFIC PROBLEM HAS NOT YET BEEN DETERMINED. WILL ADVISE OF THE PROBLEM AFTER THE AIRCRAFT HAS BEEN INSPECTED BY MAINTENANCE. (K) 2L72 4F4 F A7EU E7EA 20060202001152006020200115CE 2006 2 2 CED2006F00018 120050821A2697208663 INSULATOR LEAR 25 25 5170506CE GE CJ610 CJ6106 30006NE FIRE DECTECTOR DIRTY E CEDAO OTHER O OTHER NRNOT REPORTED 1 SW05273CA 039 WHILE DESCENDING THROUGH FL 220 FOR APPROACH INTO AIRPORT, THE NR2 FIRE LIGHT CAME ON MOMENTARILY. IMMEDIATELY REDUCED THE RT THRUST LEVER TO IDLE. MAINTENANCE INSPECTED AIRCRAFT AND FOUND BAD FIRE LOOP CONNECTION. (K) 2L72 4J4 J A10CE 1E16 20060202001162006020200116CE 2006 2 2 CED2006F00019 120050528A2612 FIRE DETECTOR LEAR 25 25B 5170511CE GE CJ610 CJ6106 30006NE NR 2 ENGINE FALSE ACTIVATIONE CEDAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 SW058005Y 121 WHILE ENROUTE, THE CREW EXPERIENCED INDICATION OF FIRE ON THE NR2 ENGINE. THE CREW THEN FOLLOWED THE EMERGENCY CHECK LIST AND COULD NOT EXTINGUISH THE FIRE LIGHT. THE CREW THEN DECLARED AN EMERGENCY AND LANDED AT THEIR DESTINATION WITHOUT FURTHER INCIDENT. ONCE THE CREW LANDED THEY COULD FIND NO EVIDENCE OF FIRE. MAINTENANCE CREW IS ENROUTE TO THE AIRCRAFT. WILL SUPPLY DETAILS AFTER THEY ARE FOUND. SUSPECT A FALSE FIRE WARNING INDICATION. (K) 2L72 4J4 J A10CE 1E16 20060202001172006020200117EU 2006 2 2 CED2006F00004 120050901A3260A10024239 UPLOCK SWITCH AMD FALC20FALCOND 2720304EU GE CF700 CF7002D2 30010NE NR 1 MLG INOPERATIVE E CEDAO OTHER O OTHER NRNOT REPORTED 1 SW03218CA 218 ON APPROACH, THE LANDING GEAR HAD TO BE LOWERED USING PROCEDURE C (EMERGENCY PROCEDURES). MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NR1 LANDING GEAR UPLOCK SWITCH INOPERATIVE. REMOVED AND REPLACED UPLOCK SWITCH WITH SERVICEABLE PART. OPS CHECK OK. (K) 2L72 4F4 F A7EU E7EA 20060202001192006020200119CE 2006 2 2 CED2006F00008 120050517A78106023T09G02 CASE LEAR 25 25B 5170511CE GE CJ610 CJ6106 30006NE NR2 ENG EXHAUST CRACKED E CEDAO OTHER O OTHER NRNOT REPORTED 1 SW05239CA 25B149 251049 WHILE ENROUTE, AT FLIGHT LEVEL 390, FLIGHT CREW OBSERVED A FIRE INDICATION ON THE NR 2 ENGINE. THE FLIGHT CREW WAS ABLE TO EXTINGUISH THE FIRE INDICATION LIGHT USING STANDARD EMERGENCY PROCEDURES. THE FLIGHT CREW THEN DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE WITH NO FURTHER INCIDENT.(K) 2L72 4J4 J A10CE 1E16 20060202001212006020200121CE 2006 2 2 CED2006F00006 120050521A2810 FUEL TANK LEAR 25 25B 5170511CE GE CJ610 CJ610* 30006NE LT WING LEAKING A CEDAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW05140CA 140 ON TAKEOFF ROLL AND INITIAL CLIMBOUT, FUEL WAS OBSERVED LEAKING FROM THE LT WING TIP. INFORMED THE CREW OF THE LEAK AND INSTRUCTED THEM TO COME AROUND AND LAND. THE CREW LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE LT FUEL VENT AND FOUND NO DISCREPANCIES. THE AIRCRAFT WAS RELEASED FOR TEST FLIGHT, NO DEFECTS WERE NOTED. (SW05200407451) 2L72 4J4 J A10CE 1E16 20060202001252006020200125NE 2006 2 2 CED2006F00010 220050821A7200 ENGINE LEAR 25 25 5170506CE GE CJ610 CJ6106 30006NE NR 2 MALFUNCTIONED E CEDAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SW05238CA 040 HAD TO ABORT THE TAKEOFF WHILE ATTEMPTING TO DEPART. THE REASON FOR THE ABORT WAS THAT THE NR 2 ENGINE WOULD NOT PRODUCE TAKEOFF FOR THE CONDITIONS. MAINTENANCE CHECKED AIRCRAFT AND FOUND IT TO MAKE TAKEOFF EPR ON PERFORMANCE RUN. (K) 2L72 4J4 J A10CE 1E16 20060202001332006020200133EA 2006 2 2 A6WA200540373 120051230A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT WING CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31432AW 7257 LT WING LOWER PLANK HOLE NR4, WS 54.681 HAS CORROSION AT OB SIDE 5 INCH L X .002 INCH D AND AT IB SIDE 5 INCH L X .002 INCH D. NOT IN CRITICAL AREA. MAINTENANCE REPAIRED LT WING LOWER PLANK ACCESS HOLE NR 4 AT WS 54.681 IAW REO. (K) 2L72 4F4 FRTA21EA E15NE 20060202001352006020200135EA 2006 2 2 A6WA200540378 120051230A5210 COVER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31432AW 7257 PASSENGER DOOR UPPER FORWARD CORNER CAP IS CRACKED. MAINTENANCE REPAIRED PASSENGER DOOR UPPER FWD CORNER CAP IAW REPAIR BY INSTALLING NEW COVER PN 6003190278. (K) 2L72 4F4 FRTA21EA E15NE 20060131001782006013100178SO 2006 1 31 SIMA200535506 120051215A532014525381003 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21664MS 145779 THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED THE CORROSION BY MAKING A CUTOUT. PREPARED A DOUBLER, FILLER, 2 SHIMS AND PLATE. REPAIR DONE IAW EMB. (K) 2L72 4T4 FRTT00011ATTE6CH 20060131001832006013100183EU 2006 1 31 SIMA200600303 120051223A55127255150522 SKIN SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RT HORIZ STAB DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21317AE21509 340B317 HAIL DAMAGE ON THE RT HORIZONTAL STABILIZER TOP SKIN PANEL. REMOVED THE EXISTING SKIN PANEL AND MARKED AND DRILLED FASTENER HOLES. REPOSITIONED AND INSTALLED SKIN. REPAIR DONE IAW SRM. (K) 2L72 4T4 TRTA52EU E8NE 20060131002032006013100203SO 2006 1 31 SIMA200600508 120051231A532014525480003 SILL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL CARGO DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21669MB4632 145788 THE CARGO DOOR CUT OUT LOWER SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED LWR SILL. INSTALLED NEW SILL IAW SRM. (K) 2L72 4T4 FRTT00011ATTE6CH 20060131002052006013100205CE 2006 1 31 VLI2006F00001 120051227A574026111444 BRACKET CESSNA CESSNA208 208B 2073701CE PWA PT6 PT6* 52043EA FLAP ACTUATOR CRACKED E VLIAO OTHER O OTHER NRNOT REPORTED 1 SO21741VL651 208B1091 FLAP ACTUATOR BRACKET FAILED DURING NORMAL OPERATION RENDERING FLAP SYSTEM INOPERATIVE. INSTALLED KIT SK208-158. (K) 1H71 3T3 T A37CE E2NE 20060131002622006013100262WP 2006 1 31 UPS06846043 120051229A5330561537271N1 SKIN DOUG DC8 DC871F 302199DWP FS1350-1490 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE:C3 REMOVE AND REPLACE LWR BELLY SKIN FROM STA 1350 TO 1490, L31L TO L31R. REMOVED AND REPLACED LWR BELLY SKIN FROM STA 1350 TO 1490, L31L TO L31R IAW SRM 51-1-21, AND SRM 51-1-20D. 2L74 4F RT4A25 20060201000372006020100037EU 2006 2 1 UPS06145991 120051229A5754A5724199320300 DOUBLER AIRBUSA300 A300F4622R 3930360EU RT K FLAP BOX CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01137UP 0820 INSPECTION TYPE:C2 RT WING KRUEGER FLAP BOX AREA CURVED DOUBLER HAS CRACK APPROX 1". REMOVED AND REPLACED DOUBLER IAW SRM 51-40-00. 2L72 4F RTA35EU 20060202000262006020200026NM 2006 2 2 AALA20060063 120051215A33971703663 SOCKET BOEING767 767323 1385205NM EMERGENCY LIGHTSBROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21384AA 26996 AFW - EMERGENCY LIGHT WIRE BROKEN AT CONNECTOR LOCATED AT KICK PANEL OF SEAT 29H. REPINNED WIRE WITH CONTACT SOCKET FOR EMERGENCY LIGHT WIRE BROKEN AT CONNECTOR AT KICK PANEL OF SEAT 29H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20060202000392006020200039SO 2006 2 2 MASA200500663 120050821A3397 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSLOOSE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07840MJ 145429 ASH 2822 CLT, EMERGENCY LIGHT AT ROW 12 WAS INOP. MX RESECURED THE LIGHT CONNECTOR. 2L72 4T RTT00011AT 20060202000422006020200042SO 2006 2 2 MASA200500738 120050920A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSINOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07834MJ 145340 ASH 2779 GNV - CREW REPORTED EMERGENCY LIGHTS AT ROW 6 INOP. MX REPLACED LIGHT BULBS AND OPS CHECK NORMAL. 2L72 4T RTT00011AT 20060202000442006020200044SO 2006 2 2 MASA200500757 120050927A335078241 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSINOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07853MJ 145464 ASH 2950 CLT - CREW REPORTED THE O/W EMERG LIGHT INOP. MX REPLACED THE INVERTOR. 2L72 4T RTT00011AT 20060202000452006020200045SO 2006 2 2 MASA200500765 120051001A3350 SIGN EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSMALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07831MJ 145273 ASH 2870 CLT, LT EMERGENCY EXIT SIGN WILL NOT ILLUMINATE. MX PERFORMED AN OPERATIONAL TEST OF THE EMERGENCY LIGHT SYSTEM AND COULD NO DUPLICATE THE FAULT. OPS CHECK GOOD 2L72 4T RTT00011AT 20060201000392006020100039EU 2006 2 1 UPS06145993 120051227A5410A5451506300401 STRUCTURE AIRBUSA300 A300F4622R 3930360EU LT PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01137UP 0820 NR 1 ENG AFT LWR PYLON LWR SECTION IS CRACKED FWD, AFT THROUGH PRESS LINE MOUNT HOLE. REMOVED AND REPLACED MEMBER SECTION IAW SRM 51-40-21. 2L72 4F RTA35EU 20060201000402006020100040EU 2006 2 1 UPS06145994 120051227A5410A5451506320400 ANGLE AIRBUSA300 A300F4622R 3930360EU NR 1 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01137UP 0820 NR 1 AFT LWR PYLON MEMBER SECTION IS CRACKED 2 EA PLACES IB AND OB AT JOGGLE. REMOVED AND REPLACED IB AND OB MEMBER SECTION ANGLES IAW SRM 51-40-21 ON NR 882061. 2L72 4F RTA35EU 20060201000412006020100041EU 2006 2 1 UPS06145995 120051227A5410A5451506320300 ANGLE AIRBUSA300 A300F4622R 3930360EU NR 1 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01137UP 0820 NR 1 ENG AFT LWR PYLON MEMBER SECTION IS CRACKED 2 PLACES IB AND OB AT JOGGLE. REMOVED AND REPLACED IB AND OB MEMBER SECTION ANGLES IAW SRM 51-40-21 ON NR 882061. 2L72 4F RTA35EU 20060201000932006020100093EU 2006 2 1 UPS05145893 120051223A2910 HYDRAULIC LINE AIRBUSA300 A300F4622R 3930360EU PWA 4158 PW4158 NE LT AFT PYLON LEAKING A IPXAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO01129UP 0813 NOTED HYDRAULIC FLUID COMING OUT OF LT PYLON, DRY MOTORED ENG TO PIN POINT PROPER PANEL TO REMOVED LT AFT PYLON OB ENG PANEL AFTER REMOVAL FOUND HARD LINE CHAFFED ON BRADED LINK HARDLINE HAS FAILED AND CAUSED LEAK. REPLACED FLEX LINE WITH PERM RIGID HYDRAULIC LINE. NR1 PYLON GREEN SYS ENG HYD CASE LINE. D316960 IS CLOSED. 2L72 4F4 FRTA35EU E24NE 20060201001152006020100115WP 2006 2 1 IXXA05SMN279S 120051216A2120 HEAT EXCHANGER DOUG DC8 DC872 302199BWP ZONE 100 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11722CX71621 46130 DURING ROUTINE C-CHECK INSP, RT AFT HEAT EXCHANGER LT LWR CORNER CRACKED .5 INCH APPROX. PERFORMED MAJOR REPAIR IAW NR 05580 DATE 12-21-05, DWG NR ED 4114 DATE 12-17-05, EO 20051435 DATE 12-21-05. REMOVED FASTENERS IAW SRM 51-1-21. REMOVED DAMAGED SECTION IAW DWG ED-4114. PERFORMED NDT INSPECTION IAW NDT IAW NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER (ALCLAD 2024 T3 0.050”) + REPAIR TRIPLER (ALCLAD 2024 T3 0.063) + FILLER (ALCLAD 2024 T3 0.100) IAW DWG NR ED 4114. CLEANED, TREATED AND PRIMED AREA + REPAIR PARTS IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11. INSTALLED REPAIR PARTS IAW DWG ED 4114, SRM 51-1-21, SRM 51-1-20D AND SRM 51-3-1 (TORQUE) 2L74 4F RT4A25 20060201001282006020100128WP 2006 2 1 IXXA05SMN294S 120051229A5753 SKIN DOUG DC8 DC872 302199BWP XF 224.000 WORN B IXXAK NONE O OTHER ININSP/MAINT 1 SW11722CX71621 46130 DURING ROUTINE C-CHECK INSPECTION, RT OB FLAP UPPER SKIN WORN, STA XF 224.000. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG. 2Q. REMOVED FASTENERS IAW SRM 51-1-21. REMOVED DAMAGED SECTION IAW SRM 57-2-1 FIG. 2Q. FABRICATED EXTERNAL REPAIR DOUBLER (ALCLAD 2024 T3 0.050) IAW SRM 57-2-1 FIG. 2Q, SRM 57-7-1 FIG. 4, TR NR 57-94 ITEM (C) DATED 10-01-02. CLEANED, TREATED AND PRIMED AREA AND EXTERNAL REPAIR DOUBLER IAW SRM 51-1-8B. INSTALLED EXTERNAL REPAIR DOUBLER IAW SRM 57-2-1 FIG. 2Q, SRM 51-1-9 (HYSOL), SRM 51-1-21. 2L74 4F RT4A25 20060201001312006020100131WP 2006 2 1 IXXA05SMN299S 120051229A5730 SKIN DOUG DC8 DC872 302199BWP XFS 566.250 CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11722CX71621 46130 DURING ROUTINE C-CHECK INSP, LT WING OB L/E CORRODED, XFS 566.250 (LWR SURFACE) PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05582 DATE 12-23-05, DWG NR ED 4126 DATE 12-21-05 EO NR 20051457 DATE 12-23-05 REMOVED FASTENERS IAW SRM 51-1-21, DC8 SRM 51-1-20D . REMOVED CORROSION IAW SRM 51-1-8 PAGES 17-18 FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG 2G. REMOVED CORRODED AREA IAW DWG ED 4126 PERFORMED NDT INSPECTION IAW NDT SRM PART 06-10-01-001 FABRICATED REPAIR DOUBLER (AL7075T60.063) FILLER. 2L74 4F RT4A25 20060202000372006020200037SO 2006 2 2 MASA200500861 120051106A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07853MJ 145464 ASH 2873 CLT - EMERGENCY FLOOR LIGHTING INOP AT ROW 3 TO 7. MAINTENANCE REPOSITIONED LIGHTING STRIPS, OPS CHECK NORMAL. 2L72 4T RTT00011AT 20060202000382006020200038SO 2006 2 2 MASA200500864 120051107A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSINOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07834MJ 145340 DURING RON, THE CREW FOUND THE PASSENGER DOOR EMERGENCY LIGHT NOT ILLUMINATING. MX REPLACED THE LIGHT BULB. 2L72 4T RTT00011AT 20060202000412006020200041SO 2006 2 2 MASA200500683 120050829A3397 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSUNSECURE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07840MJ 145429 ASH 2896 CLT - EMERGENCY EXIT CEILING LIGHT ROW 12 INOP. MAINTENANCE RESECURED INVERTER CONNECTOR. AIRCRAFT DEPARTED WITH NO FURTHER PROBLEMS. 2L72 4T RTT00011AT 20060202000432006020200043SO 2006 2 2 MASA200500741 120050922A3350 BALLAST EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSODOR A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW07837MJ 145367 ASH 2870 CHA - STRONG ELECTRICAL ODOR IN CABIN ABOUT ROW 5. MAINTENANCE FOUND SMELL TO BE COMING FROM A LIGHT BALLAST. MX CAPPED AND STOWED CONNECTOR TO ROW 4 AND 5 BALLAST. MX REPLACED LIGHT ASSY. 2L72 4T RTT00011AT 20060202000682006020200068SO 2006 2 2 MASA200500874 120051111A335078241 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSINOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07834MJ 145340 ASH 2736 CAE - EMERGENCY FLOOR PROXIMITTY LIGHTS INOP BEHIND ROW 12. MAINTENANCE REPLACED INVERTER. 2L72 4T RTT00011AT 20060202000712006020200071SO 2006 2 2 MASA200500954 120051125A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07845MJ 145502 ASH 2750 LEX, ONE SEGMENT OF FLOOR PATH LIGHTING INOP. MAINTENANCE COULD NOT DUPLICATE. 2L72 4T RTT00011AT 20060202000722006020200072SO 2006 2 2 MASA200500963 120051127A33501317 LAMP EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSBURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07858MJ 145767 ASH RON CAE, RT FWD OVERWING ESCAPE PATH LIGHTING BULB WAS BURNED OUT. MAINTENANCE REMOVED AND REPLACED LAMP. 2L72 4T RTT00011AT 20060206000102006020600010EA 2006 2 6 QXEA200600230 120051207A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 573-763 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - LT SIDE SEAT RAIL FS 573.0-763.0 HAS AREAS OF GOUGES AND CORROSION. BLENDED ALL DAMAGE TO A SMOOTH CONTOUR IAW REO 670-53-00-00-013 REV A STEP 1. ALODINED REWORKED AREA PER SRM 51-21-16 IAW REO 670-53-00-013 REV A STEP 3. IDENTIFIED SEAT TRACK IAW REO 670-53-00-013 REV STEP 9. COMPLIED WITH STEPS AND STEPS 4 THRU 8 IAW REO 670-53-00-013 REV A. 2L72 4F RTA21EA 20060206000122006020600012EA 2006 2 6 QXEA200600226 120051207A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 357-763 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC- RT SIDE SEAT RAIL FS 357.0-763.0 HAS AREAS OF CORROSION. BLENDED ALL DAMAGE TO A SMOOTH CONTOUR IAW REO 670-53-00-013 REV A STEP 1. ALODINED REWORKED AREAS PER SRM 51-21-16 IAW REO 670-53-00-013 REV A STEP 3. IDENTIFIED SEAT TRACK IAW REO 670-53-00-013 REV A STEP 9. COMPLIED WITH STEPS 2 AND STEPS 4 THR 8 IAW REO 670-53-00-013 REV A. 2L72 4F RTA21EA 20060206000132006020600013EA 2006 2 6 QXEA200600229 120051207A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 861-985 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC- LT SIDE SEAT RAIL FS 861.0-985.0 HAS AREAS OF GOUGES AND CORROSION. BLENDED DAMAGE TO A SMOOTH CONTOUR IAW REO 670-53-00-013 REV A STEP 1. ALODINED REWORKED AREA PER SRM 51-21-16 IAW REO 670-53-00-013 REV A STEP 3. IDENTIFIED SEAT TRACK IAW REO 670-53-00-013 REV A STEP 9. COMPLIED WITH STEP 2 AND STEPS 4 THRU 8 IAW REO 670-53-00-013 REV A. 2L72 4F RTA21EA 20060206000142006020600014EA 2006 2 6 QXEA200600232 120051207A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 379-483 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC- LT SIDE SEAT RAIL FS 379.0 -483.0 HAS AREAS OF GOUGES AND CORROSION. BLENDED ALL DAMAGE TO A SMOOTH CONTOUR IAW REO 670-53-00-013 REV A STEP 1. ALODINED REWORKED AREAS PER SRM 51-21-16 IAW REO 670-53-00-013 REV A STEP 3. IDENTIFIED SEAT TRACK IAW REO 670-53-00-013 REV A STEP 9. COMPLIED WITH STEPS 2 AND STEPS 4 THRU 8 IAW REO 670-53-00-013 REV A. 2L72 4F RTA21EA 20060206000162006020600016EA 2006 2 6 QXEA200600228 120051207A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 379 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - RT SIDE SEAT RAIL FS 379.0-483.0 HAS AREAS OF GOUGES AND CORROSION. REMOVED ALL DAMAGE TO A SMOOTH CONTOUR IAW REO 670-53-00-013 REV A STEP 1. ALODINE REOWRKED AREA PER SRM 51-21-16 IAW REO 670-53-00-213 REV A STEPS 3. COMPLETED WITH STEPS 2 AND STEPS 4 THRU 8 IAW REO 670-53-00-013 REV A. IDENTIFIED SEAT TRACK IAW REO 670-53-00-013 REV A STEP 9. 2L72 4F RTA21EA 20060206000842006020600084EU 2006 2 6 01092006A 120051220A30206124100 DUCT SAAB SF340 340B 7860101EU GE CT7TS CT71 30030NE ANTI-ICE SYSTEM FAULTY A NSVAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27277MJ 277 LT INTAKE LIGHT ILLUMINATED IN FLIGHT. REPLACED INLET LOWER DUCT IAW 30-20-1. 2L72 4T4 URTA52EU E8NE 20060206001002006020600100EU 2006 2 6 01092006B 120051226A6120 UNKNOWN SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE UNKNOWN A NSVACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 EA27311CE 214 AUTOCOARSEN EVENT WHEN PL WERE ADVANCED BEYOND 64 DEGREES PLA- LT ENG. NO ING LIGHT ON SHUTDOWN. PERFORMED AUTOCOARSEN AND CTOT, OPS CHECK GOOD NO DEFECTS NOTED. 2L72 4T4 TRTA52EU E8NE 20060206001012006020600101EA 2006 2 6 QXEA200600208 120051207A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 581-689 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC- INTERNAL FUSELAGE, LT FLOOR SEAT RAIL FS 581.0-689.0 PN SH670-33425-951 HAS AREAS OF CORROSION AND GOUGES. BLENDED ALL DAMAGE TO A SMOOTH CONTOUR IAW REO 670-53-00-013 REV STEP 1. ALODINED REWORKED AREAS PER SRM 51-21-16 IAW ROE 670-53-00-013 REV A STEP 3. COMPLIED WITH STEP 2 AND 4 THRU 8 IAW REO 670-53-00-013 REV A. IDENTIFIED SEAT TRACK IAW REO 670-53-00-013 REV A STEP 9. 2L72 4F RTA21EA 20060206001042006020600104EA 2006 2 6 QXEA200600214 120051207A5340 FITTING CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC- GALLEY NR 1 INB FWD FLOOR FITTING CORRODED P/N 9331091-1. REMOVED CORROSION FROM FITTING IAW CRJ 700 SRM 51-21-06-001-001-A01. NOMINAL THICKNESS OF .110, MIN REMAINING .030. REPAIR C/O IAW EA R-25-286 SECTION 1 AND REO 670-25-31-002. 2L72 4F RTA21EA 20060206001122006020600112EA 2006 2 6 QXEA200600225 120051207A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 784-861 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - RT SIDE SEAT RAIL FS 784.0-861.0 HAS AREAS OF GOUGES AND CORROSION. BLENDED ALL DAMAGE TO A SMOOTH CONTOUR IAW REO 670-53-00-013 REV A STEP 1. ALODINED REWORK AREAS PER SRM 51-21-16 IAW REO 670-53-00-013 REV A STEP 3. IDENTIFIED SEAT TRACK IAW REO 670-53-00-013 REV A STEP 9. COMPLIED WITH STEPS 2 AND STEPS 4 THRU 8 IAW REO 670-53-00-013 REV A. 2L72 4F RTA21EA 20060206001152006020600115EA 2006 2 6 QXEA200600221 120051207A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA BS 280 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - RIGHT FS 280 BULKHEAD LOWER WEB HAS CORROSION ALONG THE FLOOR LINE FUSELAGE INT RT FS 280 BULKHEAD LOWER WEB CORROSION REMOVED IAW REO 670-53-11-052 REV A REPAIR NR 1 REMAIN INT THICKNESS .038 OVER BLENDED AREAS. AREA TREATED PRIMED AND PAINTED IAW SRM 51-21-16. 2L72 4F RTA21EA 20060202000252006020200025NM 2006 2 2 AALA20060064 120051218A3350D71702001 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHTSINOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21761AJ 31478 AFW - CABIN EMERGENCY LIGHT BATTERY PACKS AT STATIONS 2042, 1476, 1522, AND 1600 FAILED FUNCTION TEST. REPLACED CABIN EMERGENCY LIGHT BATTERY PACKS AT STATIONS 2041, 1476, 1522, AND 1600. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20060202000362006020200036SO 2006 2 2 MASA200500859 120051105A33501317 LAMP EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSINOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07859MJ 145769 DURING RON, THE CREW FOUND THE LT AFT EXTERIOR EMERGENCY LIGHT NOT ILLUMINATE. MAINTENANCE REPLACED THE LIGHT BULB. 2L72 4T RTT00011AT 20060202000692006020200069SO 2006 2 2 MASA200500877 120051112A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSINOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07846MJ 145507 DURING RON IN CAE, THE CREW NOTED THAT THE RT FWD EXTERIOR EMERGENCY LIGHT NOT ILLUMINATING. MAINTENANCE REPLACED THE LIGHT BULB. 2L72 4T RTT00011AT 20060202001182006020200118 2006 2 2 CED2006F00005 420050901A3416160027087 ALTIMETER LEAR 25 25B 5170511CE GE CJ610 CJ6106 30006NE COCKPIT FAILED E CEDAO OTHER O OTHER NRNOT REPORTED 1 SW05233CA 133 ON DEPARTURE, THE CAPTAIN`S ALTIMETER FAILED. REMOVED AND REPLACED ALTIMETER. SYSTEM OPS CHECK GOOD. (K) 2L72 4J4 J A10CE 1E16 20060202001202006020200120SO 2006 2 2 SIM2006F00000 120051216A3242179814 BRAKE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL RT MLG SEIZED A SIMAO OTHER O OTHER LDLANDING 1 SW21654AE 145437 DURING LANDING, CREW REPORTED BRAKES PULL TO RIGHT. DURING ROLL OUT, REPORTED THUMPING ON RT SIDE OF AIRCRAFT. MAINTENANCE REPORTED THAT BOTH NR 3 AND NR 4 BRAKES WERE SEIZED. REPLACED BOTH RT MLG WHEEL AND TIRE ASSEMBLIES AND BOTH BRAKES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (K) 2L72 4T4 FRTT00011ATTE6CH 20060202001232006020200123NE 2006 2 2 CED2006F00009 220050726A72615002T26P01 LINE AMD FALCONFALCON20 2730103EU GE CF700 CF7002D2 30010NE NR 2 ENGINE CRACKED E CEDAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW05216CA 11 3004071 ON CLIMBOUT, AT 9000 FT THE NR 2 ENGINE OIL PRESSURE LIGHT BEGAN TO FLICKER. THE FLIGHT CREW FOLLOWED ALL CHECK LIST AND DECIDED TO RETURN TO DEPARTURE. MAINTENANCE INSPECTED THE NR 2 ENGINE AND FOUND A FAN SCAVENGE LINE BROKEN. (K) 2L72 4F4 FRTA7EU E7EA 20060202001242006020200124EU 2006 2 2 CED2006F00011 120050805A7930 WARNING LIGHT AMD FALCONFALCON20 2730103EU GE CF700 CF7002D2 30010NE NR 2 ENGINE ILLUMINATED E CEDAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 SW05216CA 11 304071 WHILE ENROUTE, THE NR2 ENGINE P2 LIGHT (OIL PRESSURE) CAME ON. THE FLIGHT CREW RETURNED TO DEPARTURE ON 1 ENGINE WITHOUT FURTHER INCIDENT. MAINTENANCE HAS NOT YET INSPECTED THE AIRCRAFT, A MAINTENANCE CREW WILL INSPECT THE AIRCRAFT LATER THIS WEEK. WILL NOTIFY OF THEIR FINDINGS AT A LATER DATE. (K) 2L72 4F4 FRTA7EU E7EA 20060202001262006020200126NE 2006 2 2 CED2006F00017 220050506A7532378A3 PLATE GE LEAR 25 25B 5170511CE GE CJ610 CJ6106 30006NE BLEED VALVE MALFUNCTIONED E CEDAO OTHER O OTHER NRNOT REPORTED 1 SW05140CA 77049 140 ON DESCENT, THE NR 1 ENGINE STALLED. THE FLIGHT CREW LT THE ENGINE RUNNING AT IDLE AND LANDED WITHOUT INCIDENT. (K) 2L72 4J4 J A10CE 1E16 20060202001272006020200127EA 2006 2 2 A6WA200540377 120051228A5340 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE BS 625 CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31432AW 7257 LT FS 625 OBLIQUE ANGLE IS CRACKED. MAINTENANCE REMOVED AND REPLACED OBLIQUE ANGLE LT SIDE PH 601R-35012-51 IAW CRJ 200 SRM 51-42-06. (K) 2L72 4F4 FRTA21EA E15NE 20060202001302006020200130CE 2006 2 2 CED2006F00020 120051003A771166001381 INDICATOR LEAR 25 25 5170506CE GE CJ610 CJ6106 30006NE EPR DEFECTIVE E CEDAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SW05238CA 25040 241238A THE AIRCRAFT ABORTED TAKEOFF ROLL, THE NR 2 ENGINE WAS NOT MAKING TAKEOFF EPR. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A DEFECTIVE EPR GAUGE. MAINTENANCE REPLACED THE DEFECTIVE GAUGE. (K) 2L72 4J4 J A10CE 1E16 20060202001312006020200131EU 2006 2 2 CED2006F00022 120051118A5610NP1616012 WINDSCREEN AMD FALC20FALCOND 2720304EU GE CF700 CF7002D2 30010NE COCKPIT CRACKED E CEDAO OTHER O OTHER NRNOT REPORTED 1 SW05219CA 193 304069 DURING TAKEOFF ROLL, BETWEEN 60 AND 80 KNOTS THE CENTER SECTION OF THE WINDSCREEN CRACKED. THE TAKEOFF WAS ABORTED. THE WINDSCREEN HAD A VERTICAL CRACK DOWN THE CENTER. (K) 2L72 4F4 F A7EU E7EA 20060202001322006020200132EU 2006 2 2 CED2006F00024 120050901A3260A10024239 UPLOCK SWITCH AMD FALC20FALCON 2720302EU GE CF700 CF7002D2 30010NE MLG INOPERATIVE E CEDAO OTHER N FALSE WARNING APAPPROACH 1 SW05385AC 144 ON APPROACH THE LANDING GEAR HAD TO BE LOWERED USING PROCEDURE A (EMERGENCY PROCEDURES). MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NR2 LANDING GEAR UPLOCK SWITCH INOPERATIVE. REMOVED AND REPLACED UPLOCK SWITCH WITH SERVICEABLE PART. OPS CHECK GOOD. (K) 2L72 4F4 F A7EU E7EA 20060202001362006020200136NE 2006 2 2 CED2006F00012 220051202A7200 ENGINE AMD FALC20FALCON 2720302EU GE CF700 CF700* 30010NE NR 1 FOD E CEDAA UNSCHED LANDING CRJF.O.D. PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SW05207CA 153 304285 AFTER TAKEOFF, THE NR 1 ENGINE STALLED. THE FLIGHT CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE ENGINE AND FOUND THAT THE NR 1 ENGINE HAD ICE FOD. (K) 2L72 4F4 F A7EU E7EA 20060202001382006020200138EU 2006 2 2 CED2006F00015 120050616A3260GE83 BULB AMD FALC20FALCON 2720302EU GE CF700 CF7002D2 30010NE MLG INDICATOR BURNED OUT E CEDAO OTHER P NO WARNING INDICATION DEDESCENT 1 SW05217CA 75 304244B ON DECENT, THE FLIGHT CREW DID NOT GET INDICATION THAT THE RT MAIN GEAR WAS DOWN AND LOCKED. THE FLIGHT CREW THEN DECLARED AN EMERGENCY AND DIVERTED. THEY HAD THE TOWER CONFIRM THAT THE GEAR WAS DOWN, THEN LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE CREW INSPECTED AIRCRAFT AND FOUND THE LIGHT FOR THE RT MAIN GEAR HAD BURNED OUT. REPLACED THE BULB AND THE SYSTEM OPERATIONAL CHECKED NORMAL. (K) 2L72 4F4 F A7EU E7EA 20060202001402006020200140 2006 2 2 HJB2006F00000 420050907A3417962830A1S8A ADC PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA AIR DATA MALFUNCTIONED B HJBRO OTHER O OTHER NRNOT REPORTED 1 AL05200SJ443 318152054 PILOT REPORTED THAT AIR DATA COMPUTER INSTALLED AS PART OF THE FLIGHT SYSTEMS EFIS-SV SYSTEM WAS REPORTING A 100 FT ERROR. (K) 1L72 3O3 O A20SO E14EA 20060202001412006020200141NE 2006 2 2 CED2006F00021 220051004A7200 ENGINE LEAR 25 25B 5170511CE GE CJ610 CJ6106 30006NE NR 2 SHUTDOWN E CEDAO OTHER YJ ENGINE STOPPAGE WARNING INDICATION NRNOT REPORTED 1 SW05233CA 133 251397A THE NR 2 ENGINE SHUTDOWN. THE FLIGHT CREW FOLLOWED THE EMERGENCY CHECKLIST AND DIVERTED WITHOUT INCEDENT. MAINTENANCE HAS NOT YET INSPECTED THE AIRCRAFT TO DETERMINE THE SPECIFIC PROBLEM. ADDITIONAL INFORMATION WILL BE SUPPLIED AT YOU REQUEST AFTER MAINTENANCE HAS COMPLETED ITS INSPECTION. (K) 2L72 4J4 J A10CE 1E16 20060202001452006020200145EA 2006 2 2 A6WA200540372 120051230A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT WING CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31432AW 7257 LT LOWER WING PLANK HOLE NR 1, WS 54.897 HAS CORROSION AT IB SIDE FORWARD EDGE 2 INCH L .005 INCH D AND AT OB SIDE AFT 4 INCH L X .005 INCH D. NOT IN CRITICAL AREA. MAINT REPAIRED LT LOWER WING PLANK ACCESS HOLE NR 1 IAW REO. (K) 2L72 4F4 FRTA21EA E15NE 20060202001462006020200146NE 2006 2 2 CED2006F00023 220050721A7200 ENGINE LEAR 25 25 5170506CE GE CJ610 CJ6106 30006NE NR 2 MALFUNCTIONED E CEDAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SW05238CA 25040 251690A ON TAKEOFF ROLL, THE NR 2 ENGINE WOULD NEVER PRODUCE TAKEOFF . THE CREW ABORTED TAKEOFF ROLL AND EXITED THE RUNWAY. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND NO DEFECTS. ALL ENGINE PARAMETERS WERE WITHIN NORMAL LIMITATIONS. (K) 2L72 4J4 J A10CE 1E16 20060202001492006020200149EA 2006 2 2 A6WA200540371 120051230A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT WING CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31432AW 7257 LT LWR WING PLANK HOLE NR 2, WS 12.245 HAS CORROSION AT OB SIDE AFT 2 INCH L X .005 INCH D AND AT IB SIDE 8 INCHES L X .005 INCH D. NOT IN CRITICAL AREA. MAINTENANCE REPAIRED LT WING LOWER PLANK ACCESS HOLE NR 2 IAW REO. (K) 2L72 4F4 FRTA21EA E15NE 20060206000112006020600011EA 2006 2 6 QXEA200600234 120051207A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 683-701 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC- RT FLOOR SEAT RAIL FS 683.45-701.45 P/N SH670-33400-961 HAS AREAS OF GOUGES BLENDED ALL DAMAGE TO A SMOOTH CONTOUR IAW REO 670-53-00-013 REV A STEP 1. ALODINED REWORKED AREAS PER SRM 51-21-16. IAW REO 670-53-00-013 REV A STEP 3. IDENTIFIED SEAT TRACK IAW REO 670-53-00-013 REV A STEP 9. COMPLIED WITH STEPS 2 AND STEPS 4 THRU 8 IAW REO 670-53-00-013 REV A. 2L72 4F RTA21EA 20060206000992006020600099EA 2006 2 6 QXEA200600217 120051207A5210 STRINGER CNDAIRCL600 CL6002C10 1390015EA PAX DOOR CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - PAX DOOR AFT STRINGER (STAIR SIDE) CRACKED AT HANDRAIL STOWAGE BRACKET. CUT OUT DAMAGED SIDE PANEL AND FABRICATED REPAIR PARTS IAW REO 670-52-11-104 STEPS 1, 3, 4, 5, 6, 7. HFEC INSPECTION C/O ON CUT-OUT REPAIR AREA OF PAX DOOR STAIR WEB AS REQUIRED IAW NDTM PT 1 51-20-006 NO CRACKS FOUND. REMAINING STEPS 2, AND 8 THROUGH 17 COMPLETED IAW REO 670-52-11-104. 2L72 4F RTA21EA 20060206001022006020600102EA 2006 2 6 QXEA200600209 120051207A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 581-683 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - RT FLOOR SEAT RAIL FS 581.0-683.0 PN SH670-33425-951 HAS AREAS OF GOUGES AND CORROSION. BLENDED ALL DAMAGE TO A SMOOTH CONTOUR IAW REO 670-53-00-013 REV A STEP 1. ALODINED REWORKED AREAS PER SRM 51-21-16 IAW REO 670-53-00-013 REV A STEP 3. IDENTIFIED SEAT TRACK IAW REO 670-53-00-013 REV A STEP 9. COMPLIED WITH STEPS 2 AND STEPS 4 THRU 8 IAW REO 670-53-00-013 REV A. 2L72 4F RTA21EA 20060206001142006020600114EA 2006 2 6 QXEA200600215 120051207A5755 SKIN CNDAIRCL600 CL6002C10 1390015EA SPOILERS CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC- RT WING OUTBD MULTIFUNCTION SPOILER UPPER CENTER HINGE SKIN CRACKED. SPOILER UPPER CENTER HINGE SKIN REPAIRED IAW CRJ 700 EA R-57-136 AND REO 670-57-73-011 REV STEPS 1 AND 2. NDT HFEC CARRIED OUT IAW NDTM PART 1 51-20-006 NO CRACKS NOTED. ROTARY FLAP PEENED REWORK EDGE IAW REO 670-57-73-011. TREATED, PRIMED AND PAINTED IAW CRJ 700 SRM 51-25-16-001-001-A01. 2L72 4F RTA21EA 20060206001162006020600116EA 2006 2 6 QXEA200600222 120051207A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA BS 286 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - LEFT FS 286 BULKHEAD LOWER WEB HAS CORROSION ALONG THE FLOOR LINE. FUSELAGE INT LEFT FS 280 LOWER BULKHEAD CORROSION REMOVED IAW REO 670-53-11-052 REV A REPAIR NR 1 REMAINING WEB THICKNESS .037 IN AFFECTED AREA. AREA TREATED PRIMED AND PAINTED IAW SRM 51-21-163. 2L72 4F RTA21EA 20060206001282006020600128EA 2006 2 6 QXEA200600219 120051207A5310CC670331911 INTERCOSTAL CNDAIRCL600 CL6002C10 1390015EA BS 176 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - FORWARD FUSELAGE AT ADG COMPARTMENT FLOOR INTERCOSTAL RT SIDE STA 176 HAS CRACKED LOWER FLANGE P/N CC670-33191-1 (REF SRM 53-11-43-991-802-50). REPLACED INTERCOSTAL P/N CC670-33191-1 IAW CRJ 700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20060206001292006020600129EA 2006 2 6 SWIA200516194 120050824A5347 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA BS 559 CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07413SW 7102 FUSELAGE; FLOOR SEAT TRACK IS CORRODED; FS 559.00 + 40; RBL - 9.0, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED SEAT TRACK FS 559.00 + 40; RBL - 9.0 IAW CRJ 200 AMM 53-01-11-400-802. 2L72 4F RTA21EA 20060206001302006020600130EA 2006 2 6 SWIA200516195 120050824A5340 ATTACH FITTING CNDAIRCL600 CL6002B19 1900309EA BS 635 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07413SW 7102 AFT EQUIPMENT COMPARTMENT; INTERCOSTAL TO SKIN ATTACH CLIP IS CRACKED; FS 635.0; STR 12R, ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIP IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-25-16, 51-42-21. 2L72 4F RTA21EA 20060206002022006020600202EU 2006 2 6 01092006C 120051228A32465006227 TIRE SAAB SF340 340B 7860101EU NLG FAILED A NSVAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 EA27194CJ 194 ABORTED TO DUE TO SERIOUS NOSE WHEEL SHIMMY AT START OF TO ROLL.REMOVED AND REPLACED NOSE WHEEL TIRE ASSY. IAW 32-41-15-4 LT AND RT PN ON/OFF 5006227. LT SN OFF MAY04-3139, LT SN ON OCT96-2047/MAY94-1676.RT SN OFF MAY04-3136, RT SN ON MAY04-3164. 2L72 4T RTA52EU 20060206002132006020600213EA 2006 2 6 SWIA200516187 120051010A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA BS 625 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07720SW 7297 (2 EA) CRACKED INTERCOSTAL FS 625 WL80 AND WL90 LBL40, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED PER CRJ200 SRM 51-77-00 PG 1 STEPS 1-4; 51-42-06 PG 11; AND 51-42-21 PG 17. 2L72 4F RTA21EA 20060206002142006020600214EA 2006 2 6 SWIA200516188 120051010A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 625 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07720SW 7297 CRACKED ANGLE FS 625 WL80 RBL37 ITEM FOUND AT C-CHECK INSPECTION. INSTALLED ANGLE PER CRJ200 SRM 51-42-21 PG 19 AND CRJ200 51-74-00 AT FS 625 WL 80 RBL 37. 2L72 4F RTA21EA 20060206002152006020600215EA 2006 2 6 SWIA200516189 120051010A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 625 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07720SW 7297 CRACKED ANGLE FS 625 WL80 LBL37, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED ANGLE PER CRJ200 SRM 51-42 PG 17 PART FS 625 WL 80 LBL37. 2L72 4F RTA21EA 20060206002162006020600216EA 2006 2 6 SWIA200516190 120051010A5320 PANEL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07720SW 7297 RIGHT MLG; BAT PNL CRACKED AT BL45.00, ITEM FOUND AT C-CHECK INSPECTION. INSTALLATION OF ANGLE DOUBLER PER REO 601R-57-51-046 REV 'B' SHEET 4 OF 6 RT BAT ANGLE. 2L72 4F RTA21EA 20060202001372006020200137NE 2006 2 2 CED2006F00013 220051109A7200PHC112C31680 HOSE AMD FALC20FALCOND 2720304EU GE CF700 CF7002D2 30010NE NR 1 ENGINE LEAKING E CEDAO OTHER O OTHER NRNOT REPORTED 1 SW05219CA 193 245020 WHILE PASSING THROUGH FL320 ON CLIMB TO FL350, THE NR1 ENGINE ROLLED BACK TO 25 PERCENT. THE CREW REGAINED POWER AND CLIMBED TO FL350 AND LANDED WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED THE ENGINE TO INCLUDE BORESCOPE, AND REPLACED T2 HOSE. ENGINE FLIGHT TESTED GOOD. (K) 2L72 4F4 F A7EU E7EA 20060202001392006020200139EU 2006 2 2 CED2006F00016 120050518A3260A23802105 SQUAT SWITCH AMD FALC20FALCON 2720302EU GE CF700 CF7002D2 30010NE NLG INTERMITTENT E CEDAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW05209CA 71 245U167 ON TAKEOFF, THE GEAR HANDLE SAFETY SWITCH WOULD NOT RELEASE THE GEAR TO COME UP. MAINTENANCE CLEANED NOSE SQUAT SWITCH CONNECTOR. SYSTEM OPS CHECKED GOOD. THE AIRCRAFT WAS RELEASED FOR FLIGHT. ON TAKEOFF, THE SAME PROBLEM REOCCURRED. AIRCRAFT RETURNED TO MAINTENANCE, REPLACED THE SQUAT SWITCH. SYSTEM OPS CHECKED GOOD. (K) 2L72 4F4 F A7EU E7EA 20060202001472006020200147EA 2006 2 2 A6WA200540379 120051228A5712 RIB CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT WING CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31432AW 7257 RT BAH RIB ASSY WS 53.60, FS 523.8 CRACKED 1 INCH IN RADIUS. MAINTENANCE REPAIRED RT BAH RIB ASSY IAW REO. (K) 2L72 4F4 FRTA21EA E15NE 20060206000932006020600093EA 2006 2 6 QXEA200600216 120051207A5210 STRINGER CNDAIRCL600 CL6002C10 1390015EA PAX DOOR CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC- PAX DOOR FWD STRINGER CRACKED AT HANDRAIL STOWAGE BRKT (FWD STAIR SIDE) CUT OUT DAMAGED SIDE PANEL AND FABRICATED REPAIR PARTS IAW REO 670-52-11-104 STEPS 1,3,4,5,6,7. HFEC INSPECTION C/O ON CUT OUT REP AIR AREA OF PAX DOOR STAIR WEB AS REPAIRED IAW NDTM PT 151-20-006 NO CRACKS FOUND REMAINING STEPS 2 AND 8 THROUGH 17 COMPLETED IAW REO 670-52-11-104 2L72 4F RTA21EA 20060207000302006020700030 2006 2 7 0502013265 420051230A450080555154501 PRINTER AIRBUS320 A320212 3930322EU CENTER PEDISTAL SMOKE A NWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL01365NW 0964 PRINTER STARTED SMOKING DURING FLIGHT. PULLED C/B AND LIFTED PRINTER COVER. NO FURTHER PROBLEMS. PRINTER REMOVED AND REPLACED. PRINTER REMOVED (NWA STK 32-3130-9-0006 S/N OFF 02352). 2L72 4F RTA28NM 20060207000452006020700045NM 2006 2 7 DL76L060068 120050119A80107755386 VALVE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 1 ENGINE UNSERVICEABLE A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27184DN 27111 724681 ON CLIMBOUT LT STARTER CUTOUT EICAS PER QRH TURNED OFF LEFT ENG BLEED. ON DESCENT INTO BOM LT STARTER CUTOUT EICAS MESSAGE REAPPEARED WITH BLEED OFF, LANDED BOM. REPAIRED SHORT AT PIN 6 ON C/P AT LT START VALVE AND REPLACED START VALVE. 2L72 4F4 FRTA1NM E24NE 20060207000602006020700060NM 2006 2 7 2005UALA01248 120051109A5340 SUPPORT BRACKET BOEING747 747422 1384935NM PWA 4056 PW4056 NE BS 1831-1860 CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29173UA 24380 MAIN DECK STA 1831-1860, LBL 45 TO RBL 45, SUPPORT BRACKET AND SEAT TRACK ATTACH BEAM HAS AREA OF CORROSION 1 X 3 INCH. *S/D* REPAIR REQUIRED FOR LOCAL AREA, LBL 11.33, WHICH WAS REPAIRED PER SRM 53-00-52, FIGURE 201, REPAIR 5, AS PERMANENT. 2L74 4F4 FRTA20WE E24NE 20060207000772006020700077NM 2006 2 7 2006UALA00101 120050121A5311 FRAME BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU FS 616 STR 17R CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29925UA 26646 CABIN FS 616 BELOW STR 17R FRAME CRACKED. REMOVED DAMAGE, FABRICATED AND INSTALLED ANGLE AND FILLER REPAIR REF MM 53-11-89. 2L72 4F4 FRTA16WE E21EU 20060207001052006020700105NM 2006 2 7 2006UALA00125 120050120A5300 RIVET BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU UNKNOWN CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29338UA 24242 CRACKED RIVETS. REPLACED RIVETS REF SRM 51-40-02 & 53-00-01. 2L72 4F4 FRTA16WE E21EU 20060207001352006020700135WP 2006 2 7 ABXA060076 120051209A53132754438 LONGERON DOUG DC8 DC861 3021952WP BS 250 - 270 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23847AX 46031 FORWARD CARGO, LONGERON 35 LEFT, CRACKED, FS 250 - 270. INSTALLED LONGERON REPAIR AT FORWARD CARGO FS 250 - 270, LONGERON 35 LEFT IAW RFTS 40033 AND PROJECT E-40463. SPLICE REPAIR INSTALLED IAW DC8 SRM 53-2-2 AT LONGERON 35 LEFT. 2L74 4F 4A25 20060206000082006020600008EA 2006 2 6 QXEA200600233 120051207A5320 COLLAR CNDAIRCL600 CL6002C10 1390015EA FASTENER MISSING A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - FUSELAGE INTERIOR HAS (2) MISSING LOCK FASTENER COLLARS AT FS 761, STR 16L, BELOW EXIT DOOR ON FRAME WEB. INSTALLED NEW COLLARS (2) IAW CRJ 700 SRM 51-42-21-001-001-A01 (HST79CKS). 2L72 4F RTA21EA 20060206000092006020600009EA 2006 2 6 QXEA200600231 120051207A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 483-573 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - LT SIDE SEAT RAILS FS 483.0-573.0 HAS AREAS OF GOUGES AND CORROSION. BLENDED ALL DAMAGE TO A SMOOTH CONTOUR IAW REO 670-53-00-013 REV A STEP 1. ALODINED REWORKED AREA PER SRM 51-21-16 IAW REO 670-53-00-013 REV A STEP 3. IDENTIFIED SEAT TRACK IAW REO 670-53-00-013 REV A STEP 9. COMPLIED WITH STEPS 2 AND STEPS 4 THRU 8 IAW REO 670-53-00-013 REV A. 2L72 4F RTA21EA 20060206000152006020600015EA 2006 2 6 QXEA200600227 120051207A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 483-573 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - RT SIDE SEAT RAIL FS 483.0-573.0 HAS AREAS OF CORROSION. REPAIRED IAW REO 670-5-00-013, MAT'L LOSS WITHIN LIMITS OF REO 670-53-00-013 REV A STEP 1. ALODINED REWORKED AREA PER SRM 51-21-16 IAW REO 670-53-00-013 REV A STEP 3. COMPLETED WITH STEPS 2 AND STEPS 4 THRU 8 IAW REO 670-53-00-013 REV A. IDENTIFIED SEAT TRACK IAW REO 670-53-00-013 REV A STEP 9. 2L72 4F RTA21EA 20060206000172006020600017EA 2006 2 6 QXEA200600211 120051207A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 485 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - RT FLOOR SEAT RAIL FS 485.0-581.0 PN670-33426-1 HAS AREAS OF GOUGES AND CORROSION. BLENDED ALL DAMAGE TO A SMOOTH CONTOUR IAW REO 670-53-00-013 REV A STEP 1. ALODINED REWORKED AREAS PER SRM 51-21-16 IAW REO 670-53-00-013 REV A STEP 3. IDENTIFIED SEAT TRACK IAW REO 670-53-00-013 REV A STEP 9. COMPLIED WITH STEPS 2 AND STEPS 4 THRU 8 IAW REO 670-53-00-013 REV A. 2L72 4F RTA21EA 20060206000182006020600018EA 2006 2 6 QXEA200600212 120051207A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 381-485 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - LT FLOOR SEAT RAIL FS 381.45-485.0 P/N SH670-32249-951 HAS AREAS OF GOUGES AND CORROSION. BLENDED OUT ALL DAMAGE TO A SMOOTH CONTOUR IAW REO 670-53-00-013 REV A STEP 1. ALODINED REWORKED AREAS PER SRM 51-21-16 IAW REO 670-53-00-013 REV A STEP 3. COMPLIED WITH STEP 2 AND STEPS 4 THRU 8 IAW REO 670-53-00-013 REV A. IDENTIFIED SEAT TRACK IAW REO 670-53-00-013 REV A STEP 9. 2L72 4F RTA21EA 20060206000722006020600072NM 2006 2 6 05FDEA04337 120051215A5700 REPAIR BOEING727 727200 138407ENM LE FLAP UNKNOWN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25274FE 22039 FOUND PREVIOUSLY REPAIR AT NR 5 KRUEGER FLAP WS 265.0 WAS ACCOMPLISHED IAW SRM 57-50-3 FIG 3, BASED ON EXTERNAL EVALUATION CONSISTED OF LOCATION, SIZE, SHAPE, NUMBER OF FASTENERS AND SPACING, MATERIAL THICKNESS AND GENERAL WORKMANSHIP, REPAIR IS CLASSIFIED AS MAJOR REPAIR PER GMM 6-2-100. 2L73 4F RTA3WE 20060206001032006020600103EA 2006 2 6 QXEA200600210 120051207A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 485 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - LT FLOOR SEAT RAIL FS 485.0-581.0 PN SH670-33426-1 HAS AREAS OF CORROSION AND GOUGES. BLENDED ALL DAMAGE TO A SMOOTH CONTOUR IAW REO 670-53-00-013 REV A STEP 1. ALODINED REWORKED AREAS PER SRM 51-21-16 IAW REO 670-53-00-013 REV STEP 3. IDENTIFIED SEAT TRACK IAW REO 670-53-00-013 REV A STEP 9. COMPLIED WITH STEPS 2 AND 4 THRU 8 IAW REO 670-53-00-013 REV A. 2L72 4F RTA21EA 20060206001132006020600113EA 2006 2 6 QXEA200600224 120051207A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA BS 302 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - FUSELAGE LOWER SKIN AT FS 302 AND STR27 IS CORRODED AROUND THE LOWER TCAS ANTENNA BASE REPAIRED FUSELAGE SKIN IAW EA R-53-405 AND REO 670-53-21-153 REV - .002 MAT'L LOSS. HFEC COMPLETED ON BLENDED AREA IAW CRJ NDTM PT 1 51-20-006. NO CRACKS NOTED. TREATED IAW CRJ 700 SRM 51-21-11-001-001-A01, EA NO R-53-405 AND REO 670-53-21-153. 2L72 4F RTA21EA 20060206001512006020600151NM 2006 2 6 AWXA200600169 120051221A5754 SKIN BOEING737 73733A 1384673NM NR 2 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED 4 CRACKS, RANGING FROM .250 INCHES UP TO .500 INCHES IN LENGTH, ON THE BOTTOM NR 2 SLAT SKIN, BELOW THE OUTBOARD AUXILIARY TRACK. MAINTENANCE REMOVED THE DAMAGE FROM THE NR 2 SLAT SKIN IAW BOEING 737-300 SRM 57-43-01-2R6. FABRICATED FILLER AND SPLICE PLATE IAW BOEING 737-300 SRM 57-43-01-2R6. INSTALLED FABRICATED REPAIR PARTS ON THE BOTTOM NR 2 SLAT SKIN IAW BOEING 737-300 SRM 57-43-01-2R6. 2L72 4F RTA16WE 20060206001842006020600184NM 2006 2 6 QXEA200600040 120051231A5720 ANGLE DHAV DHC8 DHC8202 2809007NM RT WING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09379PH 530 PDX - Z ANGLE CRACKED AT RIGHT WING FRONT SPAR STATION UW560. REPLACED IAW HORIZON AIR EA 2-57-105. 2H72 4T RTA13NM 20060206002002006020600200EA 2006 2 6 SWIA200516192 120051010A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07720SW 7297 FS280 RBL 8 BELOW FLOOR JOINING ANGLE CRACKED BETWEEN BEAM AND SUPPORT. (ITEM FOUND AT C-CHECK INSPECTION.) INSTALLED ANGLE PER REO 601R-53-11-136 AT FS 280 RH. 2L72 4F RTA21EA 20060206002012006020600201EA 2006 2 6 SWIA200516193 120051010A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07720SW 7297 FS 280 LBL8 BELOW FLOOR JOINING ANGLE CRACKED BETWEEN BEAM AND SUPPORT, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED BRACKET CLIP AT 280 LBL 8 PER REO 601R-53-11-136. 2L72 4F RTA21EA 20060207000612006020700061NM 2006 2 7 2005UALA01256 120051109A5320 WEB BOEING747 747422 1384935NM PWA 4056 PW4056 NE BS 900, RBL 40 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29173UA 24380 FWD CARGO STA 900, RBL 40 AREA HAS 6 INCH VERTICAL CRACK IN WEB, 10 INCHES BELOW CARGO FLOOR. *S/D* DAMAGE TRIMMED OUT AND REPAIRED WITH DOUBLER, PER OSV ENGRG, AS PERMANENT REPAIR. 2L74 4F4 FRTA20WE E24NE 20060207001332006020700133WP 2006 2 7 ABXA060074 120051201A5313 LONGERON DOUG DC8 DC861 3021952WP BS 879 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23847AX 46031 RIGHT FS 879.375, LONGERON 24, HAD CRACK AT LOWER AREA. STOP DRILLED AND INSTALLED ANGLE REPAIR IAW DC8 SRM 53-2-2. 2L74 4F 4A25 20060207001342006020700134WP 2006 2 7 ABXA060075 120051206A53133641004U503 LONGERON DOUG DC8 DC861 3021952WP BS 879 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23847AX 46031 LEFT MAIN LANDING GEAR WHEEL WELL LONGERON 24, FS 879 HAD A CRACK AT LOWER FASTENER FORWARD SIDE. REMOVED AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D AND 53-2-0. 2L74 4F 4A25 20060207001622006020700162EA 2006 2 7 QXEA200600263 120051207A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA BS 1690 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC- FORWARD SIDE OF FS 1690 HAS WEAR MARKS ON LT AND RT OUTBOARD AT 3 O'CLOCK AND 9 O'CLOCK POSITIONS. BLENDED OUT DAMAGE IAW CRJ 700 SRM 53-00-00-101-001-A01 AND CRJ 700 SRM 51-12-00-001-001-A01 PARA 7B WITHIN LIMITS LPI C/O ON BLEND REPAIR AREA AS OF BULKHEAD WEB AS REQUIRED IAW NDTM PT 1 51-20-008 NO CRACKS FOUND. TREATED AND PRIMED REWORKED AREA IAW CRJ 700 SRM 51-25-06-001-001-A01. 2L72 4F RTA21EA 20060207001632006020700163EA 2006 2 7 QXEA200600262 120051207A5753 VANE CNDAIRCL600 CL6002C10 1390015EA TE FLAPS DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - RT OUTBD FLAP VANE L/E (LOWER SURFACE) HAS LOOSE FASTENER AT WS 218. REPLACED FASTENER IAW CRJ 700 SRM 51-42-13-001-001-A01. 2L72 4F RTA21EA 20060207001642006020700164EA 2006 2 7 QXEA200600235 120051207A5347SH67033400961 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 683-701 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC- LT FLOOR SEAT RAIL FS 683.45-701.45 P/N SH670-33400-961 HAS AREAS OF GOUGES BLENDED ALL DAMAGE TO A SMOOTH CONTOUR IAW REO 670-53-00-013 REV A STEP 1. ALODINED REWORKED AREAS PER SRM 51-21-16 IAW REO 670-53-00-013. REV A STEP 3. IDENTIFIED SEAT TRACK IAW REO 670-53-00-013. REV A STEP 9. COMPLIED WITH STEPS 2 AND STEPS 4 THRU 8 IAW REO 670-53-00-013 REV A. 2L72 4F RTA21EA 20060207001662006020700166EA 2006 2 7 QXEA200600237 120051207A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 701 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - LT FLOOR SEAT RAIL FS 701.45-836.55 PN SH670-35864-951 HAS AREAS OF GOUGES ALL DAMAGE REMOVED IAW REO 670-53-00-013 REV A STEPS 1 AND 6. REWORKED AREAS ALODINED TO CODE A044 IAW REO 670-53-00-013 REV A STEP 3. IDENTIFIED SEAT TRACK IAW REO 670-53-00-013 REV A STEP 9 AND COMPLIED WITH STEP 2 AND STEPS 4 THRU 8. 2L72 4F RTA21EA 20060207001682006020700168EA 2006 2 7 QXEA200600242 120051207A5730 SKIN CNDAIRCL600 CL6002C10 1390015EA LT WING DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - LT WING, I/B MFS SURROUND SKIN AT WS 170.83 LOOSE FASTNERS. FASTENERS REPLACED IAW CRJ 700 SRM 51-42-06-001-001-A01. TOUCH-UP IAW CRJ 700 SRM 51-25-16-001-001-A01. 2L72 4F RTA21EA 20060207001692006020700169EA 2006 2 7 QXEA200600243 120051207A5730 SKIN CNDAIRCL600 CL6002C10 1390015EA LT WING DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - LT WING, I/B MFS SURROUND AT WS 170.83 LOOSE FASTNERS. FASTENERS REPLACED IAW CRJ 700 SRM 51-42-06-001-001-A01. TOUCH-UP IAW CRJ 700 SRM 51-25-16-001-001-A01. 2L72 4F RTA21EA 20060207001722006020700172EA 2006 2 7 QXEA200600246 120051207A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA BS 1015-1051 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC- FUSELAGE EXTERIOR SKIN ABOVE AFT BAGGAGE DOOR HAS AREAS OF WICK FROM STA1015 TO STA 1051. STR10L TO STR RL BLENDED OUT DAMAGE IAW REO 670-53-61-224, REV STEPS 1 AND 2 PER EA R-53-407. HFEC INSP COMPLETED ON ALL BLENDED AREAS IAW CRJ 700 NDTM PT 01 51-20-006. NO CRACKS NOTED. PREPED PRIMED AND PAINTED REPAIRED AREA IAW CRJ 700 SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20060207001732006020700173EA 2006 2 7 QXEA200600240 120051207A5753 VANE CNDAIRCL600 CL6002C10 1390015EA RT WING FLAP DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - RT WING OUTBD FLAP - FLAP VANE, INBD UPPER L/E HAS BROKEN FASTENERS. REPLACE 6 EA RIVETS (CR3214-4-3) B/N 62151 IAW CRJ 700 SRM 51-42-13-001-001-A01. 2L72 4F RTA21EA 20060207001742006020700174EA 2006 2 7 QXEA200600247 120051207A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA BS 1070-1098 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - FUSELAGE EXTERIOR HAS AREAS OF WICKS ON SKIN FROM STA 1070 TO STA 1098, BETWEEN STR 12L TO 16L. BLENDED OUT DAMAGE IAW REO 670-53-61-224 REV PER EA (STEPS 1 AND 2) R-53-407. HFEC INSP COMPLETED ON ALL BLENDED AREAS IAW CRJ 700 NDTM PT 01 51-20-006. NO CRACKS NOTED. PREPPED PRIMED AND PAINTED REPAIRED AREA IAW CRJ 700 SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20060207001762006020700176EA 2006 2 7 QXEA200600249 120051207A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA BS 1047 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - FUSELAGE EXTERIOR HAS NICK ON SKIN AT STA 1047, STR 19R. BLENDED OUT DAMAGE IAW CRJ 700 SRM 53-61-01-101-004-A01 AND 51-12-00-001-001-A01. NDT - FLP1 CARRIED OUT IAW NDTM PART 1 51-20-008, NO CRACKS NOTED. TRACKED, PRIMED AND PAINTED IAW CRJ SRM 51-25-16-001-001-A01. 2L72 4F RTA21EA 20060207001772006020700177EA 2006 2 7 QXEA200600238 120051207A5347SH67037380951 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 836-850 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - LT FLOOR SEAT RAIL FS 836.55-850.45 PN SH670-37380-951 HAS AREAS OF GOUGES.ALODINED OUT ALL DAMAGE TO A SMOOTH CONTOUR IAW REO 670-53-00-013 REV A STEP 1. ALODINED REWORKED AREAS TO COMP A044 IAW REO 670-53-00-013 REV A STEP 3. IDENTIFIED SEAT TRACK IAW REO 670-53-00-013 REV A STEP 9. COMPLIED WITH STEPS 2, 4, 6, 7 AND 8 OF REO 670-53-00-013 REV A. 2L72 4F RTA21EA 20060207001782006020700178EA 2006 2 7 QXEA200600239 120051207A5730 SKIN CNDAIRCL600 CL6002C10 1390015EA RT WING DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - RT WING UPPER TRAILING EDGE (JUST I/B OF MULTIFUNCTION SPOILERS) HAS LOOSE FASTENER. FASTENERS REPLACED IAW CRJ 700 SRM 51-42-00-001-001-A01 AND 51-42-21-001-001-A01. 2L72 4F RTA21EA 20060207001792006020700179EA 2006 2 7 QXEA200600250 120051207A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA BS 310 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - FUSELAGE EXTERIOR, SKIN AT FWD PAX DOOR CUTOUT, FWD EDGE HAS NICKS ON SKIN, STA 310, BETWEEN STR 13L TO STR 15L. BLEND OUT DAMAGE IAW REO 670-53-21-155 REV A STEPS 1 AND 2 PER EA NR R-53-408. HFEC COMPLETED ON BLENDED AREAS IAW CRJ NDTM PT 01 51-20-006. NO CRACK INDICATIONS NOTED. TOUCHED UP REWORKED AREA PER CRJ 700 SRM 51-21-16-001-001-A01 IAW REO 670-53-21-155 REV A STEP 4. 2L72 4F RTA21EA 20060207001992006020700199NM 2006 2 7 AWXA200600155 120051222A534765538443 CARGO TRACK BOEING737 73733A 1384673NM BS 787 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED CORROSION ON TIE DOWN TRACK LOCATED IN THE AFT PIT AT BS 787, BL 17.2L AND WL 160. MAINTENANCE BLENDED OUT THE CORROSION AND FABRICATED REPAIR STRAP IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5365-06017-SS1. INSTALLED FABRICATED REPAIR PARTS AT BS 787, BL 17.2L AND WL 160 IAW AWA ER NR 03-5365-06017-SS1. 2L72 4F RTA16WE 20060207002002006020700200NM 2006 2 7 AWXA200600156 120051221A575465C267995 SKIN BOEING737 73733A 1384673NM NR 1 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - DURING C19 CHECK DISCOVERED 6 CRACK ON THE BOTTOM OF THE NR 1 SLAT SKIN, BELOW OUTBOARD AUX TRACK. MAINTENANCE REMOVED THE DAMAGED AREA ON THE BOTTOM OF THE NR 1 SLAT SKIN IAW BOEING 737-300 SRM 57-13-01-2R6. FABRICATED FILLER AND SPLICE PLATE IAW BOEING 737-300 SRM 57-13-01-2R6. INSTALLED FABRICATED REPAIR PARTS ON THE NR 1 SLAT SKIN IAW BOEING 737-300 SRM 57-13-01-2R6. 2L72 4F RTA16WE 20060207002012006020700201EU 2006 2 7 AWXA200600157 120051201A5347D53112782202 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28602AW 565 MCN - AT "C" CHECK DISCOVERED CORROSION ON SEAT TRACK Y-765 BETWEEN FRAME 20 AND FRAME 21. NO ALLOWABLE DAMAGE LIMITS WERE FOUND. SEAT TRACK WAS REMOVED AND REPLACED FROM FROM FRAME 12 TO FRAME 24 IAW AIRBUS SRM A320 51-42 -11, PAGE 1-22. CPCP PROTECTION WAS APPLIED PER AIRBUS SRM 51-21-00. 2L72 4F RTA28NM 20060207002032006020700203EU 2006 2 7 AWXA200600159 120050112A5347D53112782202 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28602AW 565 SAL - DURING C-07 CHECK, CORROSION FOUND ON SEAT TRACK Y-1292 BETWEEN FRAME 15 AND FRAME 22 IN 5 PLACES. SEAT TRACK WAS REPLACED IAW A320 51-72-11 PAGE 1-2. 2L72 4F RTA28NM 20060208000102006020800010EA 2006 2 8 QXEA200600254 120051207A5310 DOOR FRAME CNDAIRCL600 CL6002C10 1390015EA FUSELAGE MISREPAIRED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - FUSELAGE AT PAX DOOR AFT FRAME AT TOP HAS OPEN HOLE. INSTALLED RIVET IAW CRJ 700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20060208000112006020800011EA 2006 2 8 QXEA200600255 120051207A5230670396305 SEAL CNDAIRCL600 CL6002C10 1390015EA CARGO DOOR TORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC- FWD BAGGAGE DOOR TOP EXTERNAL SEAL BENT OUT FROM FUSELAGE AND TORN IPC 52-35-00-01-A01-190. DEFLECTOR P/N LE 670-39630-5 REMOVED AND NEW FITTED IAW CRJ 700 LATECORE CMM 52-35-00-300-84-A01. DEFLECTOR P/N LE 670-39630-5 INSTALLED IAW CRJ 700 LATECORE CMM 52-35-00-300-804-A01. 2L72 4F RTA21EA 20060208000122006020800012EA 2006 2 8 QXEA200600256 120051207A5340 FITTING CNDAIRCL600 CL6002C10 1390015EA CARGO DOORWAY WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - FUSELAGE LT FWD BAGGAGE DOOR SURROUND STRUCTURE HAS FWD UPPER FITTING WORN APPROX .010". BLENDED OUT DAMAGE IAW EA R-53-402 AND REO 670-53-31-060 REV. NDT HFEC CARRIED OUT IAW NDTM PART 1 51-20-006. NO CRACKS NOTED. TREATED, PRIMED AND PAINTED IAW CRJ 700 SRM 51-25-16-001-001-A01. 2L72 4F RTA21EA 20060208000132006020800013EA 2006 2 8 QXEA200600257 120051207A5310 DOOR FRAME CNDAIRCL600 CL6002C10 1390015EA BS 1015 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC- AFT BAGGAGE DOOR SURROUND FWD LOWER COMBING HAS AREA OF SCRATCHES AND DENTS. FS 1015. REPAIR CARRIED OUT IAW REO 670-53-61-196 REV- STEPS 1 AND 2. HFEC INSPECTION C/W. BLENDED REPAIR OF LOWER COMBING AS REQUIRED IAW NDTMP 151-20-006 NO CRACKS FOUND TOUCHED UP REWORKED AREA IAW REO 670-53-61-196 REV. AIRCRAFT PRESSURIZED IAW TASK 52-00-00-790-801 LEAK CHECK ELO. NO LEAKS FOUND. REPAIR IAW REO 670-53-61-196 C/W. 2L72 4F RTA21EA 20060208000172006020800017EA 2006 2 8 QXEA200600259 120051207A5753 GUIDE CNDAIRCL600 CL6002C10 1390015EA LT WING TE FLAP WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - LT WING, O/B FLAP AFT GUIDE ROLLER FITTING IS WORN (RECEIVING END). BLENDED OUT DAMAGE ON ROLLER FITTING IAW CRJ700 SRM 57-51-02-201-001-A01. HEFC INSPECTION C/00N BLEND REPAIR AREA OF FITTING AS REQUIRED IAW NDTM PT 151-20-006. NO CRACKS FOUND. ROTARY FLAP PEENED REWORKED AREA IAW CRJ700 SRM TASK 57-51-02-201-011-A01 PARA 2 (2A(4)) TREATED, PRIMED AND PAINTED AREA IAW CRJ700 SRM 51-25-16-001-001-A01. 2L72 4F RTA21EA 20060208000182006020800018EA 2006 2 8 QXEA200600260 120051207A5755 SHROUD CNDAIRCL600 CL6002C10 1390015EA SPOILER BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - RT WING BOTTOM TRAILING EDGE. MULTI FUNCTION SPOILER SHROUD HAS MULTIPLE BROKEN AND LOOSE FASTENERS BETWEEN WS 170.83 TO WS 231.23. FASTENERS REPLACED (MS20426T) IAW CRJ700 SRM 51-02-06-001-001-A01. 2L72 4F RTA21EA 20060208000342006020800034NM 2006 2 8 AWXA200600161 120051222A5320655624577 PAN BOEING737 73733A 1384673NM BS 1006-1016 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - DURING C19 CHECK DISCOVERED LEVEL 2 CORROSION LOCATED ON THE LT AFT LAV FLOOR PAN AT BS 1006 TO BS 1016, WL 208 AND FROM BL 9L TO BL 36L. MAINTENANCE REMOVED AND INSTALLED NEW LAV FLOOR PAN IN THE LT AFT LAV FROM BS 1006 TO BS 1016, WL 208 AND FROM BL 9L TO BL 36L IAW BOEING 737-300 SRM 51-40-02-0G. 2L72 4F RTA16WE 20060208000392006020800039NM 2006 2 8 AWXA200600164 120051223A53306545770 PANEL BOEING737 73733A 1384673NM BS 628 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - DURING C19 CHECK DISCOVERED SKIN CRACK AT FASTENER HOLE AT BS 628 AND STR 4R. MAINTENANCE CUT OUT DAMAGED AREA OF SKIN IAW BOEING 737-300 SRM 53-00-01-2R30. FABRICATED FILLERS AND DOUBLERS IAW BOEING 737-300 SRM 53-00-01-2R30. INSTALLED FABRICATED REPAIR PARTS AT BS 628 AND STR 4R IAW BOEING 737-300 SRM 53-00-01-2R30. 2L72 4F RTA16WE 20060208000402006020800040NM 2006 2 8 AWXA200600166 120051223A5330654577073 PANEL BOEING737 73733A 1384673NM BS 591 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED SKIN CRACK AT FASTENER HOLE AT BS 591 AND STR 4L. MAINTENANCE CUT OUT DAMAGED AREA OF SKIN IAW BOEING 737-300 SRM 53-00-01-2R30. FABRICATED FILLERS AND DOUBLERS IAW BOEING 737-300 SRM 53-00-01-2R31. INSTALLED FABRICATED REPAIR PARTS FROM BS 585 TO BS 591 AND STR 4L IAW BOEING 737-300 SRM 53-00-01-2R30. 2L72 4F RTA16WE 20060206001172006020600117EA 2006 2 6 QXEA200600218 120051207A5210 STRINGER CNDAIRCL600 CL6002C10 1390015EA PAX DOOR CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - PAX DOOR AFT STRINGER (STAIRSIDE) CRACKED AT BASE OF 4TH RISER. DRESSED OUT EDGE CRACK IAW 700/900 SRM FIG 53-00-00-991-804 WITHIN LIMITS. DENT LP C/O ON CUT-OUT REPAIRED AS REQUIRED IAW NDTM PT 1 51-20-008, NO CRACKS FOUND. REPROTECTED IAW CRJ 700/900 SRM 51-25-16. 2L72 4F RTA21EA 20060206001392006020600139EA 2006 2 6 QXEA200600223 120051207A5240CC670382385 HOUSING CNDAIRCL600 CL6002C10 1390015EA GALLEY DOOR CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - GALLEY SERV DOOR MECH HOUSING CRACKED IPC 52-41-03-01-A01 TR 52-0109. HOUSING ASSY REMOVED IAW CRJ 700 AMM 52-41-03-000-801-A01. BUSHINGS FOR INNER LEVER, LATCH CRANK AND VENT CRANK TRANSFERED TO NEW HOUSING P/N CC670-38238-5 IAW CRJ 700 AMM TASK 20-31-00-400-801-A01 PG 404. LATCH CRANK AND VENT CRANK REINSTALLED ACTUATOR SHAFT BRG TRANSFERED OVER. NEW MECH HOUSING P/N CC670-38238-1 HI-LITE INSTALLED IAW CRJ 700 SRM 51-42-21-001-001-A01 P.8 PARA 8C. DETENT ASSY INSTALLED IAW CRJ 700 AMM TASK 52-41-02-400-803-A01, UPLOCK BELL CRANK INSTALLED WITH NEW COLLAR P/N B0206011DV8 AND LATCH AND VENT RODS CONNECTION TO CRACKS, COMPLATE AND ANTENNA HANDLE INSTALLING IAW CRJ 700 AMM TASK 52-41-03-400-801-A01 PG 42L72 4F RTA21EA 20060206001992006020600199EA 2006 2 6 SWIA200516191 120051010A5310 PANEL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07720SW 7297 LEFT MLG; BAT PANEL CRACKED AT BL45.00, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR PARTS IAW REO 601R-57-51-046. 2L72 4F RTA21EA 20060207000282006020700028NM 2006 2 7 ASAA0540370 120050803A523069366791 FITTING BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU STOP PAD CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 CORROSION ON AFT CARGO DOOR FWD LWR STOP PAD FITTING. REMOVED, BLENDED AND FOUND TO BE (OUT OF LIMITS). REPLACED AFT CARGO DOOR FWD LWR STOP PAD FITTING. (K) 2L72 4F4 FRTA16WE E21EU 20060207000552006020700055NM 2006 2 7 DLM88060086 120050128A2150 A/C PACK DOUG MD88 MD88 3023688NM BOTH MALFUNCTIONED A DALAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CRCRUISE 1 SO27963DL 49982 DUE TO COLD CABIN BOTH A/C PACKS RUN FULL HOT MANUAL AT FL 360 CAUSING BOTH PACKS TO OVERHEAT AND TRIP OFF. CABIN PRESSURE WAS LOST AND O2 MASKS AUTOMATICALLY DEPLOYED. CREW INITIATED A RAPID DESCENT TO 10,000 FT. AFTER PACKS COOLED, RESET AND REGAINED PRESSURIZATION. FLIGHT DIVERTED TO AMA FOR MTC. BOTH A/C PACKS PLACARD AT AMA BY MTC AND AIRCRAFT MTC FERRIED TO DFW FOR O2 GEN REPLACEMENTS. 2L72 4F RTA6WE 20060207001152006020700115NM 2006 2 7 2006UALA00135 120050824A5330 SKIN BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU BS 955 DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29376UA 24641 CUTOUT FOR DOOR 2R LOWER HINGE COVER AT STA 955 IS DAMAGED. THE DAMAGE WAS TRIMMED FROM THE -82 SKIN ASSY (-86 SKIN AND -87 DOUBLER) IN ACCORDANCE WITH 737-300 SRM 53-00-01 FIGURE 101, ALLOWABLE DAMAGE NR 1, DETAIL 1 AND 737-300 SRM 51-10-02. 2L72 4F4 FRTA16WE E21EU 20060207001752006020700175EA 2006 2 7 QXEA200600248 120051207A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA BS 1051 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC- FUSELAGE EXTERIOR HAS WICK ON SKIN AT STA 1051, STR 12R. DAMAGE BLENDED OUT IAW CRJ 700 SRM 51-12-00-001-001-A01 BLENDED AREA WITHIN LIMITS IAW CRJ 700 SRM 53-61-01-101-004-A01. NDT FLPI CARRIED OUT IAW NDTM PART 1 51-20-008 NO CRACKS NOTED. TREATED, PRIMED AND PAINTED IAW CRJ 700 SRM 51-25-16-001-001-A01. 2L72 4F RTA21EA 20060207002022006020700202NM 2006 2 7 AWXA200600158 120051223A5330654577073 SKIN BOEING737 73733A 1384673NM BS 690 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - DURING C19 CHECK DISCOVERED SKIN CRACKED AT FASTENER HOLE AT STR 4L, BS 690 ON THE LOWER ROW OF FASTENERS. MAINTENANCE REPAIRED CRACKED SKIN AT FASTENER HOLE, BS 690, S4L IAW BOEING 737-300 SRM 53-00-01-2R31. 2L72 4F RTA16WE 20060208000162006020800016EA 2006 2 8 QXEA200600252 120051207A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA BS 565 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - FUSELAGE EXTERIOR HAS SCRATCH ON SKIN AT STA 565, STR 0. SCRATCH BLENDED OUT IAW CRJ 700/900 SRM TASK 53-31-01-101-001-A01 .003 MAT REMOVED. LPI C/O ON BLEND REPAIRED AREA OF FUSELAGE SKIN AT STA 565 STR AS REQUIRED IAW NDTM PT 1 51-20-008. NO CRACKS FOUND. TREATED, PRIMED AND PAINTED BLENDED AREA IAW CRJ 700 SRM 51-25-16-001-001-A01. 2L72 4F RTA21EA 20060208000352006020800035NM 2006 2 8 AWXA200600165 120051223A5330654577074 SKIN BOEING737 73733A 1384673NM BS 570 DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 DURING C19 CHECK DISCOVERED SKIN CRACK AT FASTENER HOLE AT BS 570 AND STR 4R. MAINTENANCE CUT OUT DAMAGED AREA OF SKIN IAW BOEING 737-300 SRM 53-00-01-2R30. FABRICATED FILLERS, DOUBLERS AND TRIPLER IAW BOEING 737-300 SRM 53-00-01-2R30. INSTALLED FABRICATED REPAIR PARTS AT BS 570 AND STR 4R IAW BOEING 737-300 SRM 53-00-01-2R30. 2L72 4F RTA16WE 20060208000512006020800051NM 2006 2 8 AWXA200600197 120051218A53156545808179 FLOORBEAM BOEING737 7373Y0 1384671NM BS 294 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED LEVEL TWO CORROSION ON FLOORBEAM LOCATED AT BS 294.5, WL 207 AND BL 44R. RE-WORK WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-10-05-1A FIG 101. MAINTENANCE REMOVED DAMAGED SECTION OF FLOORBEAM IAW BOEING 737-300 SRM 53-10-51-2R. FABRICATED REPAIR ANGLES AND FLOORBEAM IAW BOEING 737-300 SRM 53-10-51-2R FIG 201. INSTALLED, FABRICATED REPAIR PARTS AT BS 294.5, WL 207 AND BL 44R. 2L72 4F RTA16WE 20060208000522006020800052NM 2006 2 8 AWXA200600198 120051223A5320 RETAINER BOEING737 73733A 1384673NM BULKHEAD CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED CORROSION ON 1016 BULKHEAD LOWER GASKET RETRAINING STRIP FROM BL 2L TO BL 4R. MAINTENANCE REMOVED CORROSION ON THE -10 STRIP IAW BOEING 737-300 SRM 51-10-02-0G AND WAS WITHIN LIMITS. REMOVED CORROSION ON THE -16 STRIP AND CORROSION WAS OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED THE -16 STRIP IAW BOEING 737-300 SRM 51-40-02-06 FIGURES 9 AND 10 AND BOEING DWG 65-46812. 2L72 4F RTA16WE 20060208001502006020800150WP 2006 2 8 IXXA0500139S 120050304A5712 RIB DOUG DC8 DC871F 302199DWP WS 67.750 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11821BX858952998 45811 DURING A ROUTINE C CHECK INSPECTION, FOUND RT OUTBOARD PYLON STUB WING N 4 RIB EXTENDED LEADING EDGE CRACK DAMAGE AT STA XOLDO 67.750. MAJOR REPAIR ACCOMPLISHED REMOVAL OF DAMAGE. FABRICATED NEW RIB. PERFORMED NDT INSPECTION, CLEANED, TREATED AND PRIMED AREA+ NEW RIB. APPLIED SEALANT TO FAYING SURFACES AND INSTALLED NEW RIB IAW DWG DACO 9753297, REPAIR SPEC NR 2003-05, DC8 SRM 54-1-0 PG 1, 54-3-0 FIG 14B, 51-1-1, 51-1-4, 51-1-20D, 51-3-1, 51-3-2, DPS 3.69-4 REV"AM" R-1, DPS 7.00-REV "BK". 2L74 4F RT4A25 20060208001512006020800151WP 2006 2 8 IXXA0500141S 120050219A5753 REPAIR DOUG DC8 DC871F 302199DWP RT WING TE FLAP UNKNOWN A IXXAK NONE O OTHER ININSP/MAINT 1 SW11821BX858952998 45811 DURING A ROUTINE C CHECK INSPECTION, FOUND RT WING OUTBOARD FLAP UPPER FORWARD PLATING INTERIM REPAIR STA XF 417.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF FASTENERS AND DAMAGE FROM AREA. PERFORMED A NDT INSPECTION TO AREA AND FABRICATED A REPAIR DOUBLER AND FILLER. CLEANED, TREATED AND PRIMED AREA, FILLER AND DOUBLER. APPLIED SEALANT TO FAYING SURFACES AN INSTALLED THE REPAIRED PARTS IAW ALL APPLICABLE MANUALS, DRAWINGS AND REVISIONS. 2L74 4F RT4A25 20060208001522006020800152WP 2006 2 8 IXXA0500142S 120050228A5300 FASTENER DOUG DC8 DC871F 302199DWP BS 1380 MISSING A IXXAK NONE O OTHER ININSP/MAINT 1 SW11821BX858952998 45811 DURING A ROUTINE C CHECK INSPECTION, FOUND AFT CENTER SECTION LOWER PLATING DRAIN HOLE REPAIR ONE ROW FASTENERS MISSING STA 1380.000 L-35 RT L-36. MAJOR REPAIR ACCOMPLISHED REMOVAL OF EXISTING REPAIR. REMOVED DAMAGED SECTION AND PERFORMED NDT INSPECTION. FABRICATED EXTERNAL REPAIR DOUBLER AND INTERNAL FINGER DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES AND INSTALLED REPAIR PARTS IAW ALL APPLICABLE MANUALS, DRAWINGS AND REVISIONS. 2L74 4F RT4A25 20060208001532006020800153WP 2006 2 8 IXXA0500143S 120050224A5330 SKIN DOUG DC8 DC871F 302199DWP FS 1540.00 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11821BX858952998 45811 DURING A ROUTINE C CHECK INSPECTION, FOUND RT FUSELAGE AFT CENTER SECTION LOWER PLATING INTERNAL CORROSION DAMAGE AROUND STA FS 1540.00, L-25R TO L-26R. MAJOR REPAIR ACCOMPLISHED REMOVAL OF CORROSION AND FOUND OUT OF LIMITS. REMOVED FASTENERS FROM REPAIR AREA AND REMOVED THE DAMAGED AREA. PERFORMED AN NDT INSPECTION. FABRICATED EXTERNAL REPAIR DOUBLER, INTERNAL FINGER DOUBLER AND FILLER. CLEANED, TREATED AND PRIMED AREA AND REPAIRED PARTS. APPLIED SEALANT TO FAYING SURFACES AND INSTALLED REPAIRED PARTS IAW ALL APPLICABLE MANUALS, DRAWINGS AND REVISIONS. 2L74 4F RT4A25 20060208001542006020800154WP 2006 2 8 IXXA0500140S 120050303A5330 REPAIR DOUG DC8 DC871F 302199DWP STA 180L-35RH-36MISSING A IXXAK NONE O OTHER ININSP/MAINT 1 SW11821BX858952998 45811 DURING A ROUTINE C CHECK INSPECTION, FOUND FUSELAGE AFT CENTER SECTION LOWER PLATING DRAIN HOLE REPAIR DOUBLER MISSING ONE ROW FASTENERS AT STA 180.000, L-35 RT TO L-36. MAJOR REPAIR ACCOMPLISHED REMOVAL OF EXISTING REPAIR DOUBLER. FABRICATED EXTERNAL REPAIR DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR DOUBLER. APPLIED SEALANT TO FAYING SUFACES. INSTALLED REPAIR DOUBLER IAW ALL APPLICABLE MANUALS AND DRAWINGS. 2L74 4F RT4A25 20060208001552006020800155WP 2006 2 8 IXXA0500145S 120050225A5730 SKIN DOUG DC8 DC871F 302199DWP XRS 144.00 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11821BX858952998 45811 DURING A ROUTINE C CHECK INSPECTION, FOUND RT WING FORWARD TOP PANEL PLATING CRACK DAMAGE AT STA XRS 144.00 FRONT SPAR. MAJOR REPAIR ACCOMPLISHED REMOVAL OF FASTENERS AND DAMAGED AREA. PERFORMED NDT INSPECTION. FABRICATED EXTERNAL DOUBLER AND FILLER PLUG. CLEANED, TREATED AND PRIMED AREA AND REPAIRED PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIRED PARTS IAW SEMAN DWG ED-3833 AND FAA FORM 8110-3 NR 05020, DC8 SRM 51-1-11, 51-1-15, 51-120D, 51-1-22, 51-1-26, 51-3-0, 51-3-1, 51-3-2, 51-6-0. 2L74 4F RT4A25 20060209000032006020900003EA 2006 2 9 ASOA051126S 120051219A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE BS 409-559 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 DURING A C-CHECK, THE FS409+128 TO FS 559.00 AND LBL36 TO FLOOR STR WAS FOUND TO BE CORRODED IN NUMEROUS SPOTS. AFTER MAINTENANCE BLENDED, ALODINED, AND PRIMED THE FS 409+128 TO FS 559.00, AND LBL 36 TO FLOOR STR, IAW REO, IT WAS FOUND TO BE WITHIN LIMITS. (K) 2L72 4F4 FRTA21EA E15NE 20060207001362006020700136WP 2006 2 7 ABXA060073 120051206A5330575499213 SKIN DOUG DC8 DC861 3021952WP BS 620 - 640 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23847AX 46031 FORWARD CARGO FUSELAGE SKIN BULGED, CRACKED, FASTENER SHEARED, EVIDENCE OF EXFOLIATION CORROSION AT PREVIOUS REPAIR, FS 620 - 640, LONGERON 35 LEFT - 36 LEFT. REMOVED CORROSION FORWARD CARGO COMPARTMENT FUSELAGE SKIN IAW DC8 SRM 51-1-8 AT LONGERON 36. INSTALLED DOUBLER AND 2 EACH FINGER DOUBLERS IAW DC8 SRM. 2L74 4F 4A25 20060207001652006020700165EA 2006 2 7 QXEA200600236 120051207A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 701 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC- RT FLOOR SEAT RAIL FS 701.45-836.55 PN SH670-35864-951 HAS AREAS OF GOUGES DAMAGE BLEND OUT WITHIN LIMITS OF REO 670-53-00-013 REV A IAW CRJ 700 SRM 51-12-00 AND 51-21-06 (STEP 1 REO 670-53-00-013 REV A) ALODINED REWORKED AREAS TO A044 IAW REO 670-53-00-013 REV A STEP 3. IDENTIFIED SEAT TRACK IAW REO 670-53-00-013 REV A AND COMPLETE STEPS 1-9. 2L72 4F RTA21EA 20060207001672006020700167EA 2006 2 7 QXEA200600241 120051207A5730 SKIN CNDAIRCL600 CL6002C10 1390015EA LT WING DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - LT WING, O/B MFS SKIN (SURROUND) AT WS 231.23 LOOSE FASTENERS. REPLACED FASTENERS (MS20426T) IAW CRJ 700 SRM 51-42-06-001-001-A01. TOUCHED UP IAW CRJ 700 SRM 51-25-16-001-001-A01. 2L72 4F RTA21EA 20060207001702006020700170EA 2006 2 7 QXEA200600244 120051207A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA BS 939 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - FUSELAGE EXTERIOR HAS NICK ON SKIN AT STA 939, STR 9L. NICK BLENDED OUT IAW CRJ 700/900 SRM TASK 53-51-01-101-002-A01 .004 MAT'R REMOVED. LPI C/O ON BLENDED SKIN REPAIR AREA AS REQUIRED IAW NDTM PT 1 51-20-008 NO CRACKS FOUND. TREATED PRIMED AND PAINTED IAW CRJ 700 SRM 51-25-16-001-001-A01. 2L72 4F RTA21EA 20060208000092006020800009EA 2006 2 8 QXEA200600253 120051207A5330 RIVET CNDAIRCL600 CL6002C10 1390015EA BS 549 LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - FUSELAGE EXTERIOR HAS SMOKING RIVET AT STA 549, STR 0. RIVET REMOVED IAW CRJ 700/900 SRM 51-42-06-001-001-A01 PG 8 PARA 11. RIVET INSTALLED IAW CRJ 700/900 SRM 51-42-06-001-001-A01 PG 4 PARA 2B. 2L72 4F RTA21EA 20060208000142006020800014EA 2006 2 8 QXEA200600258 120051207A5230 SKIN CNDAIRCL600 CL6002C10 1390015EA CARGO DOOR DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - AFT BAGGAGE DOOR HAS AREAS OF SCRATCHES TOP EXTERNAL SURFACE. BLENDED OUT DAMAGE IAW EA R-52-253 AND REO 670-52-31-012 REV- NDT-HFEC CARRIED OUT IAW NDTM PART 1 51-20-006. NO CRACKS NDT ON FASTENERS REPLACED IAW EA R-53-253 AND REO 670-52-31-012 REV. TREATED, PRIMED AND PAINTED IAW CRJ700 SRM 51-25-16-001-001-A01. 2L72 4F RTA21EA 20060208000152006020800015EA 2006 2 8 QXEA200600251 120051207A5310 DOOR FRAME CNDAIRCL600 CL6002C10 1390015EA BS 310 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - FUSELAGE FWD PAX DOOR SURROUND, FWD COMBING HAS GOUGES BETWEEN STR 12L TO STR 16L STA 310. BLENDED GOUGES IAW SRM TASK 53-21-23-101-001-A01 SRM 51-12-00-001-001. PG 9 PARA 7B. LPI C/O BLENDED AREA OF PAX DOOR SURROUND FWD COMBINE AS REPAIRED IAW NDTM PT 51-20-008. NO CRACKS FOUND. TREATED, PRIMED AND PAINTED IAW CRJ 700 SRM 51-25-16-001-001-A01. 2L72 4F RTA21EA 20060208000372006020800037NM 2006 2 8 AWXA200600162 120051222A532065524576 PAN BOEING737 73733A 1384673NM BS 1006-1016 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - DURING C19 CHECK DISCOVERED LEVEL 2 CORROSION LOCATED ON THE RT AFT LAV FLOOR PAN AT BS 1006 TO BS 1016, WL 208 AND FROM BL 9R TO BL 36R. MAINTENANCE REMOVED AND INSTALLED NEW LAV FLOOR PAN IN THE RT AFT LAV FROM BS 1006 TO BS 1016, WL 208 AND FROM BL 9R TO BL 36R IAW BOEING 737-300 SRM 51-40-02-0G. 2L72 4F RTA16WE 20060208000382006020800038EU 2006 2 8 AWXA200600163 120050112A5347D5311281520200 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28602AW 565 SAL - MAJOR REPAIR - DURING C-07 CHECK, CORROSION ON SEAT TRACK WAS FOUND AT Y 1292, BETWEEN FRAMES 15-AND 20 IN THREE PLACES. SEAT TRACK WAS REPLACED IAW AIRBUS SRM 51-72-11. 2L72 4F RTA28NM 20060208000842006020800084NM 2006 2 8 AWXA200600196 120051213A3397BR963507 WIRE HARNESS BOEING737 7373Y0 1384671NM EMERGENCY LIGHTSDAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - EEL - DURING C16 CHECK DISCOVERED EMERGENCY ESCAPE PATH LIGHT HARNESS DAMAGED FROM BS 360 TO BS947, WL 208 AND BL 26L. MAINTENANCE REPAIRED SPLICES AND CONNECTORS ON THE EMERGENCY ESCAPE PATH LIGHT HARNESS IAW BOEING SWPM 20-13-12. REMOVED AND REPLACED CONNECTORS ON HARNESS AT ROWS 2L, 11L, 12L, 13L, 14L 19L, 20L, 5L AND 22L IAW BOEING SWPM 20-42-01. OPERATIONAL CHECKS WERE GOOD IAW AMERICA WEST AIRLINES TASK CARD A1C33005. 2L72 4F RTA16WE 20060208001082006020800108WP 2006 2 8 UPS06846092 120051231A533057503653N SKIN DOUG DC8 DC871F 302199DWP FS 610-779 L36 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE:C3 FWD ACCESSORY COMPT STA 670 BETWEEN L36 TO L35L FUSELAGE SKIN HAS HEAVY CORROSION. REMOVED CORRODED SKIN AT STA 610-779 L31L-L31R IAW SAA EA 008-5320-01-A0019, FABBED AND INSTALLED -1, -2, -3 DOUBLERS, -4. -5, -6, -7, AND -8 STRAPS, AND SKIN IAW UPS ENG FILE NR DC8-53-20527, FAA FORM 8100-9 DATED 01/13/06, BAC MSG NR 1-150178337-2 DATED 01/06-06, SLH-SAT 00009C, AND SAA EA008-5320-01-A0019. 2L74 4F RT4A25 20060208001302006020800130WP 2006 2 8 IXXA0500135S 120050304A5311 FRAME DOUG DC8 DC871F 302199DWP FS 55.00 L-24L CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11821BX858952998 45811 DURING A ROUTINE C CHECK INSPECTION, FOUND LT FUSELAGE FORWARD ACCESSORY COMPARTMENT STRUCTURE FRAME CRACK DAMAGE AT STA FS 55.00, L-24L. MAJOR REPAIR ACCOMPLISHED REMOVAL OF FASTENERS AND CRACKED FRAME SEGMENT. PERFORMED AN NDT INSPECTION. FABRICATED FRAME SEGMENT AND SPLICES. PERFORMED HEAT TREATMENT, CLEANED, TREATED AND PRIMED. APPLIED SEALANT TO FAYING SURFACES. INSTALLED FRAME SEGMENT AND SPLICES IAW DC8 SRM 53-2- FIG 2 SH 1, 6 TR NR 53-125, 53-3-1 FIG 3 SH 2, 2S, 51-1-1, 51-1-4, 51-1-11, 51-1-15, 1-1-20D, 51-3-2, DPS 3.69-7 REV "AM" R-1, 7.00-1 REV "BK". 2L74 4F RT4A25 20060208001312006020800131WP 2006 2 8 IXXA0500136S 120050307A5230 DOUBLER DOUG DC8 DC871F 302199DWP BS335 STR35R-35LCORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11821BX858952998 45811 DURING A ROUTINE C CHECK INSPECTION, FOUND FUSELAGES CENTER SECTION FORWARD CARGO COMPARTMENT FORWARD DOOR AFT JAMB INTERNAL DOUBLER CORROSION DAMAGE STA 335.000 L-35R 35L. MAJOR REPAIR ACCOMPLISHED REMOVAL OF CORROSION AND FOUND OUT OF LIMITS. REMOVED EXISTING DOUBLER AND FASTENERS FROM REPAIR DOUBLER. REMOVED THE DAMAGED AREA. PERFORMED NDT INSPECTION TO AREA, FABRICATED EXTERNAL REPAIR, DOUBLER + FILLER. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS IAW SEMAN DRAWING ED-3879 AND FAA FORM 8110-3 NR 05083, DC8 SRM 51-1-11, 51-1-15, 51-1-20D, 51-1-26, 51-3-1, 51-3-2. 2L74 4F RT4A25 20060209000182006020900018EA 2006 2 9 ASOA051109S 120051217A5321 FLOOR SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE BS 515 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 DURING A C-CHECK, THE RT SIDE PRESSURE FLOOR SKIN, AT FS 515.00, WAS FOUND TO BE CORRODED BEYOND LIMITS. AFTER MAINTENANCE BLENDED, ALODINED, AND PRIMED THE RT SIDE PRESSURE FLOOR SKIN, AT FS 515.00, IAW SRM 51-21-11 AND 51-42-06, IT WAS FOUND TO BE WITHIN LIMITS. (K) 2L72 4F4 FRTA21EA E15NE 20060209000192006020900019EA 2006 2 9 ASOA051114S 120051217A5347 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 DURING C-CHECK, THE FORWARD AND AFT FLOOR TRACKS, AT RBL 27.00, NEAR THE LAVATORY, WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FORWARD AND AFT FLOOR TRACKS, AT RBL 27.00, NEAR THE LAVATORY. (K) 2L72 4F4 FRTA21EA E15NE 20060209000952006020900095WP 2006 2 9 IXXA05SMN271S 120051215A5610 WINDSHIELD DOUG DC8 DC872 302199BWP COCKPIT CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11722CX71621 46130 DURING C-CHECK INSPECTION, COCKPIT LT LATERAL WINDSHIELD CRACKED. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05580. REMOVED FASTENERS IAW DC-8 SRM 51-1-21. REMOVED CORROSION IAW DC-8 RM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW DC-8 SRN 57-2-0 PAGE 16. REMOVED CORRODED AREA IAW SEMAN DWG ED-4119. PERFORMED NDT INSPECTION IAW DC-8 NDT IAW DC-8 NDT SPM PART 06-10-01-001. FAB`D SOLID SEGMENT REPAIR PLATING & INTERNAL SPLICE & (02 EA) REPAIR DOUBLER IAW SEMAN DWG NR ED 4119. CLEANED, TREATED AND PRIMED AREA & REPAIR PARTS INTERNAL PART IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11. INSTALLED REPAIR PARTS IAW SEMAN DWG ED 4119, DC-8 SRM 51-1-2. 2L74 4F RT4A25 20060209001082006020900108EU 2006 2 9 MAC120502 120051228A2612D889N FIRE LOOP FOKKERF27 F27MK500 4990629EU NR 1 ENGINE CHAFED A MTNABEF EMER. DESCENT ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CLCLIMB 1 SO33726FE 10683 AFTER TAKEOFF, THE CREW HAD A FIRE WARNING ON THE NR 1 ENGINE. 2H72 4T A817 20060209001182006020900118NM 2006 2 9 200521 120051231A293154271158010 INDICATOR DHAV DHC8 DHC8103 1386005NM HYD PRESSURE FALSE INDICATIONA KPVAO OTHER O OTHER APAPPROACH 1 WP13811WP 366 (PIREP) NR 1 MAIN HYD PRESSURE INDICATOR READ BELOW 3000 PSI THEN DROPPED TO ZERO APPROX 5 MIN. CAME BACK UP TO 3000 PSI THEN DOWN TO 2000 AND BACK TO 3000 PSI TIL LANDING AND PARK. (MX - OGG) GROUND RUN, OPS CHECK DETERMINED NR 1 HYD INDICATING SYSTEM INTERMITTENT. AIRCRAFT APPROVED FOR FERRY FLIGHT FROM OGG TO HNL ONLY. (MX - HNL) REMOVED AND REPLACED NR 1 MAIN HYD PRESS INDICATOR. SECURED CANNON PLUG AND SECURED SCREW. OPS CHECK GOOD IAW DHC 29-30-00, PG 1 PAR 2. 2H72 4T RTA13NM 20060209001362006020900136NM 2006 2 9 DHL2006752503 120051229A5711 SPAR BOEING727 727223 1384074NM PWA JT8 JT8D15 52051NE RT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01752DH 22466 DISCREPANCY FOUND NR 110621; RT/WING AT WS 170 APPRX L/E CAVITY FRONT SPAR LWR CHORD HAS CORROSION. REMOVED CORR ON RT/WING LWR SPAR AT WS 170 ORIGINAL THICKNESS .413 MAT REMOVED .109 MATL REMAINING IS .304 AND IS OUT OF LIMITS IAW SRM 57-10-1 FIG2 FABBED DOUBLER 301 SS 1/4 HD. PO 445673 .080 16 INCHES X 3 INCHES IAW EMTEQ ENG DRAWING NR 2 - 38255-701 IR DATED 01-06-06 TREATED AND PRIMED AREA AND PART IAW SRM 51-10-2 INSTALLED REPAIR PLATE IAW EMTEQ ENG DRAWING NR 2-38255-701, IR, DATED 01-06-06 WITH FORM 8110 DATED 01-06-06. 2L73 4F4 F A3WE E2EA 20060209001372006020900137WP 2006 2 9 ARWA20051202 120051220A272257553865503 ACTUATOR DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE RUDDER PACK ACTULEAKING A ARWAK NONE K FLUID LOSS ININSP/MAINT 1 SO19441J 536 536 45988 LOG PAGE NR 116558. ON POST FLIGHT FOUND LEAKING BY EMPANAGE LOWER SIDE REAR STRIKE PAD REAR ACCESS PANEL. REMOVED AND REPLACED RUDDER PACK ACTUATOR IAW MM 27-21-6. LEAK CHECK AND OPERATIONAL CHECK IAW MM 27-20-0 FOUND NORMAL, NO LEAKS NOTICE. 2L74 4F4 F 4A25 1E8 20060210000052006021000005SO 2006 2 10 MASA200500552 120050715A33501317 LAMP EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL RT EXT OVERWING INOPERATIVE A MASAK NONE O OTHER NRNOT REPORTED 1 SW07825MJ 145179 THE AIRCRAFT WAS ON R.O.N. LAST NIGHT AND SCHEDULED FOR A ROUTINE CHECK INSPECTION. DURING THE WALK AROUND IT WAS DISCOVERED THE RT EXTERNAL OVERWING EMERGENCY LIGHT NOT ILLUMINATING. REPLACED THE LIGHT BULB. OPERATIONAL CHECK GOOD. 2L72 4T4 FRTT00011ATTE6CH 20060210000062006021000006SO 2006 2 10 MASA200500617 120050806A3350 CONNECTOR EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL EMRG EXIT SIGN INOPERATIVE A MASAK NONE O OTHER NRNOT REPORTED 1 SW07831MJ 145273 ASH 2971 CLT. RT OVERWING EMERGENCY EXIT SIGN INOPERATIVE. MX SECURED THE CONNECTOR AND IT OPS CHECKED GOOD. THE A/C DEPARTED WITHOUT FURTHER INCIDENT. 2L72 4T4 FRTT00011ATTE6CH 20060207001612006020700161EA 2006 2 7 QXEA200600261 120051207A5730 SKIN CNDAIRCL600 CL6002C10 1390015EA LT WING CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC- RT WING OUTBD LEADING EDGE SKIN HAS CHAFED MARK FRO ADJACENT RIVET HEAD AT WS294. CHAFE DAMAGE BLENDED IAW CRJ 700 SRM 57-41-01-101-001-A01 AND 51-12-00-001-001-A01 REMAINING MATERIAL WITHIN LIMITS. LPI COMPLETED ON BLENDED AREA IAW CRJ 700 PT 01 51-20-008. NO CRACKS NOTED. TREATED, PRIMED AND PAINTED IAW CRJ 700 SRM 51-25-16-001-001-A01. 2L72 4F RTA21EA 20060207001712006020700171EA 2006 2 7 QXEA200600245 120051207A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA BS 1000-1047 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - FUSELAGE EXTERIOR, AFT BAGGAGE DOOR CUTOUT HAS EDGE DAMAGE, STA 1000 AND STA 1047, BETWEEN STR14 AND 16L. BLENDED OUT DAMAGE IAW REO 6760-53-61-224 REV-PER EA R-53-407 (STEPS 1 & 2). HFEC INSP COMPLETED ON BLENDED AREA IAW CRJ 700 NDTM PT 01 51-20-006. NO CRACKS NOTED. PREPPED PRIMED AND PAINTED REPAIRED AREA IAW CRJ 700 SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20060208000332006020800033NM 2006 2 8 AWXA200600160 120051224A5312654656841 BULKHEAD BOEING737 73733A 1384673NM BS 1016 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - DURING C19 CHECK DISCOVERED CORROSION ON THE AFT PRESSURE BULKHEAD, LOWER FORWARD FACE SKIN, RT OUTBOARD SIDE OF THE CENTER CHANNEL AT BS 1016, WL 201 AND BL 2R. MAINTENANCE CUT OUT DAMAGED SECTION OF BULKHEAD IAW BOEING DWG 65C28106. RECEIVED AND INSTALLED NEW AFT PRESSURE BULKHEAD SKIN IAW BOEING 737-300 SRM 51-40-02-0G AND DWG 65C28106. LEAK CHECK WAS GOOD IAW BOEING 737-300 AMM 21-00-05-2. 2L72 4F RTA16WE 20060208001682006020800168NM 2006 2 8 DHL2006752501 120051229A5330 SKIN BOEING727 727223 1384074NM PWA JT8 JT8D15 52051NE FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01752DH 22466 DISCREPANCY FOUND NR 110587; DENT LT SIDE FUSELAGE SKIN AT STA 373 STR. 24L (MARKED). DENT IS IN AREA NOT ALLOWED IAW SRM SPECIFICATIONS. CUT OUT DAMAGED AREA DIM 3INCHES X 1INCH FABBED FILLER 2024-T3 .050 PO 9002695 3.1 INCHES X 1.3 INCHES AND DOUBLER 2024-T3 .063 14.5 INCHES X 6.6 INCHES PO 53125 IAW SRM 53-30 3 FIG 3 TREATED AND PRIMED REPAIR IAW SRM 51-10-2 INSTALLED REPAIR PARTS IAW SRM 53-30-3 FIG 3. 2L73 4F4 F A3WE E2EA 20060209000822006020900082EA 2006 2 9 ASOA051118S 120051217A5320 SILL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE BS 559-621 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 DURING C-CHECK, THE RT SIDE SILL, FROM FS 559+64 TO FS 621.00, WAS FOUND TO BE CORRODED BEYOND LIMITS. AFTER MAINTENANCE BLENDED, ALODINED, AND PRIMED THE RT SIDE SILL, FROM FS 559+64 TO FS 621.00, IAW REO, IT WAS FOUND TO BE WITHIN LIMITS. (K) 2L72 4F4 FRTA21EA E15NE 20060209000832006020900083EA 2006 2 9 ASOA051120S 120051218A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE BS 605 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 DURING A C-CHECK, THE FRAME AT FS 605, BETWEEN STR 27 AND STR 26L, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE FRAME AT FS 605, BETWEEN STR 27 AND STR 26L, IAW SRM 51-25-06 AND 51-25-16. (K) 2L72 4F4 FRTA21EA E15NE 20060209000882006020900088EA 2006 2 9 ASOA051116S 120051217A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE BS 559 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 DURING A C-CHECK, THE FLOORBEAM AT FS 559+80, BETWEEN RBL 9.00 AND RBL 27.00, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM AT FS 559+80, BETWEEN RBL 9.0 AND RBL 27.00, IAW SRM. (K) 2L72 4F4 FRTA21EA E15NE 20060209000922006020900092EA 2006 2 9 ASOA051167 120051231A5310 CROSSBEAM CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE BS 280 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27713EV 10081 DURING C-CHECK, THE FS 280, AT LBL 9 AND RBL 9, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FS 280 CROSSBEAM, AT LBL 9 AND RBL 9, IAW EO700-53-0061. (K) 2L72 4F4 FRTA21EA EOOO63EN 20060209000932006020900093EA 2006 2 9 ASOA051117S 120051217A5347 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 DURING C-CHECK, ALL FLOOR TRACKS AT LBL 9 AND RBL 9 HAVE APPARENT CORROSION. MAINTENANCE REMOVED AND REPLACED THE FLOOR TRACKS AT LBL 9 AND RBL 9 IAW SRM. (K) 2L72 4F4 FRTA21EA E15NE 20060210000092006021000009SO 2006 2 10 MASA200500638 120050813A335078241 INVERTER EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL EMRG LIGHT SYS FAILED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07831MJ 145273 ASH 2875 CLT. EMERGENCY AFT FLOOR LIGHTS INOPERATIVE. MAINTENANCE REPLACED INVERTER. AIRCRAFT DEPARTED WITH NO FURTHER PROBLEMS. 2L72 4T4 FRTT00011ATTE6CH 20060214000912006021400091WP 2006 2 14 AMTA200501223 120051214A5410 DRAG STRUT LKHEED1011 10113853 5265020WP NR 1 PYLON CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11163AT 1229 NR 1 PYLON DRAG STRUT AFT INBOARD LUG FOUND WITH CORROSION AS PER W/C 554I5406. CORROSION REMOVED AND FABRICATION OF BUSHING CARRIED OUT AS PER REPAIR CARD R056 AND EER 11664 LOG PAGE 756294 ALSO SEE MACH NR 5410/759, WO NR 288222 NRC 3083. (M) 2L73 4F A23WE 20060214001152006021400115CE 2006 2 14 DJFA2005180 120051216A3297 WIRE RAYTHNDH125 HAWKER800XP 7150012CE NLG INDICT SYS CHAFED E DJFAO OTHER N FALSE WARNING APAPPROACH 1 EA23828CW 258428 ON FINAL APPROACH, CREW ONLY RECEIVED 2 GREEN L/G DOWN AND LOCKED LIGHTS WHEN GEAR WAS EXTENDED. IND FOR N/G WAS NOT RECEIVED. GEAR PIN WAS CHECKED AND IND N/G DOWN. A TEST OF N/G IND BULB WAS GOOD. WHEN FLAPS EXTENDED TO 25 DEGREES GEAR HORN SOUNDED, WHEN A/C WAS SLOWED TO LESS THAN 150 KTS GEAR HORN SOUNDED. CREW ATTEMPTED TO MANUALLY EXTEND GEAR BUT PRESS REQUIRED FOR PUMPING INDICATED L/G WERE EXTENDED. CREW WAS INFORMED GEAR APPEARED TO BE DOWN AFTER MAKING 2 FLY-BYS PAST TOWER. FIRE RESCUE RESPONSE WAS GIVEN FOLLOWING AN UNEVENTFUL LANDING. MX REPAIRED A CHAFED WIRE FOR NLG IND SYS AND ADJUSTED MICRO-SWITCHES. L/G CYCLED SEVERAL TIMES, ALL L/G IND`S WERE OPERATING. A/C WAS RETURNED TO SERVICE. 2L72 4F RTA3EU 20060214001162006021400116SO 2006 2 14 FFKA2005107 220051221A74141068256013 MAGNETO PIPER PA32 PA32R300 7103213SO LYC 0540 IO540K1G5D 41532SO ENGINE INOPERATIVE B FFKAE ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SO058954C1414 32R7680146 L1408148A PILOT REPORTED A DEAD LEFT MAGNETO ON ENGINE GROUND RUN. MAINTENANCE REMOVED MAGNETO AND FOUND NEEDLE BEARINGS FROM THE LEFT HAND SIDE OF MAGNETO DRIVE GEAR IN MAGNETO HOUSING. MAINTENANCE REPLACED MAGNETO AND GROUND RUN WAS NORMAL. 1L71 3O3 O A3SO 1E4 20060209000292006020900029EA 2006 2 9 ASOA051113S 120051217A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE BS 559 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 DURING A C-CHECK, THE FLOORBEAM AT FS 559+80, BETWEEN THE RT SIDE FLOOR SILL AND RBL 27.00, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM AT FS 559+80, BETWEEN THE RT SIDE FLOOR SILL AND RBL 27.00, IAW SRM. (K) 2L72 4F4 FRTA21EA E15NE 20060209000302006020900030EA 2006 2 9 ASOA051166 120051231A5210 PULLEY CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27713EV 10081 DURING A C-CHECK, THE PASSENGER DOOR, ABOVE THE QASSIST CABLE PULLEY, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE PASSENGER DOOR, ABOVE THE ASSIST CABLE PULLEY, IAW REO. (K) 2L72 4F4 FRTA21EA EOOO63EN 20060214001912006021400191CE 2006 2 14 HYI2006F00000 120051202A3230602EN556B UPLOCK SWITCH CESSNA402 402C 207590RCE CONT O520 TSIO520* 17040SO LT WHEELWELL FAILED E HYIAO OTHER J WARNING INDICATION CLCLIMB 1 NE012615G 402C0101 CREW REPORTED GEAR UNSAFE LIGHT REMAINED ON WITH GEAR HANDLE IN UP POSITION, MAINTENANCE REMOVED AND REPLACED THE LT UP LOCK MICROSWITCH, GEAR SWING CHECKS, OK. AIRCRAFT RELEASED FOR SERVICE. (K) 1L72 3O3 O A7CE E8CE 20060209000402006020900040EA 2006 2 9 ASOA051110S 120051217A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE BS 559 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 DURING A C-CHECK, THE FLOOR SUPPORT CAP AT RBL 9, BETWEEN FS 559+64 AND FS 559+80, WAS FOUND TO BE CORRODED BEYOND LIMITS. AFTER MAINTENANCE BLENDED, ALODINED, AND PRIMED THE FLOOR SUPPORT CAP AT RBL 9, BETWEEN FS 559+64 AND FS 559+80, IAW SRM 51-21-06, IT WAS FOUND TO BE WITHIN LIMITS. (K) 2L72 4F4 FRTA21EA E15NE 20060209000632006020900063EA 2006 2 9 ASOA06077 120051231A5210CC67038601965 STRUCTURE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27713EV 10081 DURING A C-CHECK, THE PASSENGER DOOR, BELOW THE TOP STEP ON THE FORWARD SIDE, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE PASSENGER DOOR, BLEOW THE TOP STEP ON THE FORWARD SIDE, IAW REO. (K) 2L72 4F4 FRTA21EA EOOO63EN 20060209000652006020900065EA 2006 2 9 ASOA051111S 120051217A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE BS 574-621 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 DURING A C-CHECK, THE FLOOR SUPPORT CAP AT LBL27, FS 574.00 TO FS621, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT CAP AT LBL 27, FS 574.00 TO FS 621, IAW SRM 51-42-06 AND 51-42-21. (K) 2L72 4F4 FRTA21EA E15NE 20060209000662006020900066EA 2006 2 9 ASOA06080 120051231A5101 UNKNOWN CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE BS 280 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27713EV 10081 DURING A C-CHECK, A SUSPECTED CRACK WAS FOUND AT FS 280, LBL9 AND RBL9. MAINTENANCE REPAIRED THE CRACK AT FS 280, LBL 9 AND RBL 9, IAW REO. (K) 2L72 4F4 FRTA21EA EOOO63EN 20060209000672006020900067EA 2006 2 9 ASOA06078 120051231A5242H34455 HANDLE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE E/E BAY DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27713EV 10081 DURING A C-CHECK, THE FORWARD AVIONICS BAY DOOR HANDLE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FORWARD AVIAONICS BAY DOOR HANDLE IAW SRM 51-42-06. (K) 2L72 4F4 FRTA21EA EOOO63EN 20060209000682006020900068EA 2006 2 9 ASOA06079 120051231A5101 UNKNOWN CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE BS 280 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27713EV 10081 DURING C-CHECK, CORROSION WAS FOUND AT FS 280. MAINTENANCE REPAIRED THE CORRODION AT FS 280 BY INSTALLING NEW WEBS IAW SRM. (K) 2L72 4F4 FRTA21EA EOOO63EN 20060209000702006020900070EA 2006 2 9 ASOA051112S 120051217A5321 FLOOR SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE BS 449-559 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 DURING C-CHECK, THE PRESSURE FLOOR SKIN OB OF LBL 9, BETWEEN FS 449.85 AND FS 559+2, WAS FOUND TO BE CORRODED BEYOND LIMITS. UPON FURTHER INSPECTION OF THE PRESSURE FLOOR SKIN OB OF LBL 9, BETWEEN FS 449.85 AND FS 559+2, MAINTENANCE DETERMINED IT WAS NOT CORROSION. (K) 2L72 4F4 FRTA21EA E15NE 20060209000742006020900074EA 2006 2 9 ASOA051115S 120051217A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE BS 589 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 DURING A C-CHECK, THE FLOOR SUPPORT CAP, AT FS589, LBL 9, WAS FOUND TO BE CORRODED BEYOND LIMITS. UPON FURTHER INSPECTION OF THE FLOOR SUPPORT CAP, AT FS 589, LBL 9, MAINTENANCE DETERMINED THERE TO BE NO CORROSION AFTER CLEANING THE AREA. (K) 2L72 4F4 FRTA21EA E15NE 20060209000752006020900075EA 2006 2 9 ASOA051119S 120051217A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE BS 589-605 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 DURING C-CHECK, THE FLOOR SUPPORT BEAM CAP AT RBL 9.0, BETWEEN FS 589.00 AND 605, WAS FOUND TO BE CORRODED BEYOND LIMITS. UPON FURTHER INSPECTION OF THE FLOOR SUPPORT CAP AT RBL 9.0, BETWEEN FS 589.00 AND 605, MAINTENANCE FOUND NO CORROSION AFTER CLEANING THE AREA. (K) 2L72 4F4 FRTA21EA E15NE 20060209001382006020900138WP 2006 2 9 ARWA20051203 120051221A3231NNB6086511 FITTING DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL RT MLG DOOR BROKEN A ARWAK NONE O OTHER ININSP/MAINT 1 SO1968041 46900 LOG PAGES NR 116686 AND NR 116688. ON SERVICE CHECK FOUND LT MAIN LANDING GEAR DOOR ROLLER ASSEMBLY LOWER SUPPORT FITTING BROKEN. REMOVED AND REPLACED LT MAIN LANDING GEAR DOOR IAW MM 32-14-01. OPERATIONAL CHECK NORMAL IAW MM 32-10-01. 2L73 4F4 F A22WE E23EA 20060210000222006021000022CE 2006 2 10 VLI2006F00000 120051227A534026111444 BRACKET CESSNA CESSNA208 208B 2073701CE PWA PT6 PT6* 52043EA FUSELAGE CRACKED E VLIAK NONE O OTHER ININSP/MAINT 1 SO21742VL651 208B1100 FLAP ACTUATOR BRACKET FAILED DURING NORMAL OPERATION RENDERING FLAP SYSTEM INOPERATIVE. INSTALLED KIT SK208-158. (K) 1H71 3T3 T A37CE E2NE 20060214000782006021400078WP 2006 2 14 AMTA200500972 120051029A5210 SKIN LKHEED1011 1011385115 5265015WP FS 855 CRACKED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11194AT 193B1230 CRACK FOUND AT MED 2R EXTERIOR FUSELAGE SKIN. PAINT STRIPPED AREA AS INDICATED ON R2 DOOR IAW SRM 51-21-02. (M) ACCOMPLISHED REPEATATIVE INSPECTION REQUIREMENTS IAW L10-53AD-0658H PAGE 9. NO FURTHER PROPAGATION NOTED. CRACKS WERE PREVIOUSLY ON DEFERRAL FOR 50 CYCLE RE-INSPECTION. (K) 2L73 4F A23WE 20060214000902006021400090WP 2006 2 14 AMTA200501159 120051214A5343 FITTING LKHEED1011 10113853 5265020WP RT MLG DAMAGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11163AT 1229 RIGHT MLG TRUNNION FORWARD FITTING AND FORWARD LUG INNER CIRCULAR AFT AREA WITH DEEP SCRATCH MARKS AND PITTING CORROSION. REPAIR CARRIED OUT IAW SRM L1011 51-21-02 AND CADMIUM PLATING CARRIED OUT IAW 51-21-01. FABRICATED NEW BUSHINGS AND INSTALLED IAW SRM 57-14-00, REF WO NR 288222. (M) 2L73 4F A23WE 20060214001052006021400105CE 2006 2 14 122505N508CS1 120051225A793199124641 TRANSDUCER CESSNA560 560XL 2076702CE PWA 545 PW545A NE OIL PRESSURE FAILED E Z5FAO OTHER J WARNING INDICATION CLCLIMB 1 NE03508CS3315 5605294 DB0604 AFTER DEPARTING LUK, CREW NOTICED RT ENGINE OIL PRESSURE INDICATOR DROPPED TO ZERO PRESSURE WITH NO OTHER FAILURE INDICATIONS. CREW FOLLOWED CHECKLIST PROCEDURES AND ELECTED TO DECLARE EMERGENCY. THE AIRCRAFT WAS DIVERTED TO CVG WHERE IT HAD AN UNEVENTFUL LANDING. THE PROBLEM WAS TROUBLESHOOT TO A FAILED OIL PRESSURE TRANSDUCER. 2L72 4F4 FRTA22CE E00059EN 20060214002392006021400239SW 2006 2 14 ALG2006F00021 120051230A6710406010432101 BEARING BELL 407 407 1182206SW ALLSN 250C 250C47B GL ANTIDRV LINK BRGWORN E ALGAO OTHER E VIBRATION/BUFFET CRCRUISE 1 SW03436AL 53069 IN CRUISE FLIGHT, FELT BUMP IN AIRFRAME, ALL INSTRUMENTS INDICATED NORMAL. AFTER DESCENDING TO 500 FT, PROBLEM REPEATED. AFTER LANDING, NOTIFIED MAINTENANCE. ANTI-DRIVE LINK BEARINGS WORN. REMOVED AND REPLACED ANTI-DRIVE LINK. (K) 1G71 3U3 UO H2SW E1GL 20060214002422006021400242CE 2006 2 14 S2YA05078 120051125A561010138402524 WINDSHIELD BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE RT WINDSHIELD CRACKED A S2YAO OTHER O OTHER CRCRUISE 1 GL13841SK5728 UE84 DURING FLIGHT, THE RT WINDSHIELD DEVELOPED A CRACK FROM TOP TO BOTTOM. THE CREW LANDED SAFELY AND THE AC WAS FERRIED BACK. MX REPLACED TH RT WINDSHIELD AND RETURNED TO AC TO SERVICE. (K) 2L72 4T4 TRTA24CE E26NE 20060214002432006021400243NM 2006 2 14 S2YA05076 120051113A2421ALT3524 GENERATOR DORNERDO32 DO328300 NM PWA 306 PW306B NE AC GENERATOR INOPERATIVE A S2YAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL13357SK1879 3164 SHORTLY AFTER TAKEOFF, THE CREW REPORTED A LT ALTERNATOR AND LT AC VOLT FAIL CAS MESSAGES. THE CREW PERFORMED AN AIR TURN BACK. MX REPLACED LT ALTERNATOR (AC GENERATOR) AND WITH NO FURTHER DISCREPANCIES RETURNED THE AC TO SERVICE. ON THE SAME FLIGHT, SECOND ATTEMPT THE SAME PROBLEM RETURNED THE CREW PERFORMED A SECOND AIR-TURN-BACK. MX REPLACED THE LT ALTERNATOR CONTROL BOX AND WITH NO FURTHER DISCREPANCIES RETURNED THE AC TO SERVICE. (K) 2H72 4T4 FRTA55NM E35NE 20060215000442006021500044NM 2006 2 15 XN0A1292 120051229A2782 POSITION SWITCH BOEING727 727227 1384078NM LE FLAPS MALFUNCTIONED A XN0AA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 GL2379754 21363 NR 3 LED FLAP NOT ON WITH FLAP HANDLE AT 15 DEGREES, AMBER L/E FLAP LIGHT ON. REMOVED AND REPLACED NR 3 KRUEGER FLAP POSITION SWITCH IAW MM 27-82-1. OPS CHECK GOOD IAW MM 27-82-0. 2L73 4F A3WE 20060210000232006021000023EU 2006 2 10 MDAS094040 120051111A324650079951 WHEEL FOKKERF27 F27MK50 EU RT MLG BROKEN W Q0MFD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 WP03 20312 ON JAN.14 2005, MDA B-12275 (S/N 20306) DURING TAXIING AFTER LANDING, PILOT HEARD A LARGE SOUND FROM RT MLG. MECHANIC FOUND RT MLG IB WHEEL FLANGE BROKEN. ON AUG.23 2005, MDA B-12276 (S/N 20312), FA REPORTED THAT A PASSENGER FOUND THE RT IB MAIN WHEEL TIRE RUPTURED AT BEGINNING OF ROLLING. IMMEDIATELY, CREWS DECIDED ABORT TAKEOFF AND TAXI BACK. ON THE WAY OF TAXIING BACK, AC VIBRATED DUE TO TIRE RUPTURED AT RT OB MAIN WHEEL, CREWS ASK FOR TOW SERVICE. ON NOV.11 2005, MDA B-12276 (S/N 20312) LT MAIN TIRE BROKEN DURING TAXIING. PERFORMED INSP FOUND NR2 WHEEL HUB WAS BROKEN. BREAKAGE OF THE WHEEL HUB WAS MAINLY CAUSED BY FATIGUE CRACKING (HIGH CYCLE) FROM CORROSION SPOTS. 2H72 4T RTA817 20060215001072006021500107EA 2006 2 15 COMA0660120 120050207A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01967CA 7134 FLIGHT 5224 - DURING DTW APPROACH RECEIVED A FLAP FAIL CAUTION MESSAAGE AT 20 DEGREES, CREW DECLARED AN EMERGENCY, ABORTED FIRST APPROACH THEN LANDED WITHOUT INCIDENT ON SECOND ATTEMPT. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3, (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2L72 4F RTA21EA 20060215001082006021500108NM 2006 2 15 F3LA200500046 120051212A532105367180500400 FLOOR PANEL AIRBUSA319 A319111 3930336NM CABIN CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03906FR 5065 1684 DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON FLOOR PANEL 261FF. REMOVED SURFACE CORROSION FROM FLOOR PANEL 261FF. REPAIRED FLOOR PANEL PER SRM 53-02-00 FIG 202. 2L72 4F RTA28NM 20060215001222006021500122EU 2006 2 15 XN0A1281 120051207A3210 UNKNOWN AIRBUS300 A300B4203 3930306EU MLG VIBRATION A XN0AA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL23473AS 203 ON TAKEOFF ROLL AT APPROXIMATELY 135K - SEVERE VIBRATION FELT AND SUSPECT BLOWN TIRE, NORMAL LANDING ACCOMPLISHED. ON POST-FLIGHT INSPECTION FOUND NR 8 TIRE BLOWN. REMOVED AND REPLACED NR 8 AND NR 7 WHEEL AND TIRE ASSY IAW A300 AMM CHAPTER 12-37-32. PERFORMED INSPECTION OF THE AIRCRAFT IAW A300 AMM CHAPTER 05-51-15, NO DEFECTS NOTED. PERFORMED A FUNCTIONAL TEST OF THE ANTISKID SYSTEM IAW A300 AMM CHAPTER 32-42-00, CHECK GOOD. 2L72 4F RTA35EU 20060215002182006021500218EA 2006 2 15 ASOA051126 120051219A5313 STRINGER CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11840AS 7290 DURING A C-CHECK IN MCN, THE FS 409 PLUS 128 TO FS 559, AND BLB 36 TO FLOOR STR WAS FOUND TO BE CORRODED IN NUMEROUS SPOTS. (M) 2L72 4F RTA21EA 20060215002322006021500232EA 2006 2 15 ASOA06121 120051209A3250 STEERING SYS CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A ASOAK NONE J WARNING INDICATION CLCLIMB 1 SO27825AS 7207 DURING CLIMB-OUT FROM AVP-ATL, THE CREW RECEIVED A STEERING INOPERATIVE CAUTION MESSAGE. THE CREW COMPLIED WITH THE QRH, AND THE MESSAGE WENT OUT WITH THE NWS SWITCH IN THE OFF POSITION. AN EMERGENCY WAS DECLARED AND THE EMERGENCY VEHICLES WERE DISPATCHED. THE AIRCRAFT LANDED SAFELY IN ATL, WHERE IT REGAINED NOSE WHEEL STEERING AND TAXIED TO THE GATE UNDER ITS OWN POWER. MAINTENANCE PERFORMED OPERATIONAL CHECKS WITH NO DEFECTS NOTED. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060215002352006021500235EU 2006 2 15 ASOA051123 120051219A33503012000 POWER SUPPLY AEROSPATR72 ATR72212 8680945EU CABIN DEFECTIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27634AS 370 DURING A GROUND INSPECTION IN ATL, THE EMERGENCY EXIT SIGN, ABOVE THE FORWARD CARGO DOOR, WOULD NOT ILLUMINATE BRIGHT. MAINTENANCE REMOVED AND REPLACED THE LEFT 61WL EMERGENCY POWER SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20060215002362006021500236EA 2006 2 15 ASOA051124 120051219A3350OL3071BPEGPL LIGHT CNDAIRCL600 CL6002C10 1390015EA CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27705EV 10051 DURING A GROUND INSPECTION IN SLC, THE EMERGENCY EXIT LIGHT, NEAR THE SERVICE DOOR, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT, NEAR THE SERVICE DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060215002542006021500254NM 2006 2 15 2005UALA01238 120051107A5420311T31571 ANGLE BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE NR 1 PYLON CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29659UA56487 27114 NR 1 PYLON MID SPAR AT STA 233.120 RT SIDE, ANGLE IS CRACKED AT THE 2ND FROM INBOARD ATTACH FASTENER. NR 1 PYLON MID SPAR P/N 311T3157-1 AT STA 233.120 RT SIDE, ANGLE IS CRACKED AT THE 2ND FROM INBOARD ATTACH FASTENER, VERIFIED WITH HFEC. THIS IS THE CLOSE-OUT ANGLE ON THE PYLON INBOARD SIDE, OUTBOARD FASTENER LOOKING INSIDE OF PYLON. THE CRACK IS PROBABLY CAUSED BY FATIGUE AND IT WAS REPAIRED WITH FABRICATED PYLON ANGLE. 2L72 4F4 FRTA1NM E24NE 20060215002552006021500255NM 2006 2 15 2005UALA01244 120051106A2597 WIRE HARNESS BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE FWD CARGO BAY BURNED A UALAK NONE O OTHER ININSP/MAINT 1 WP29668UA 30024 WIRE BUNDLE W1402 HAS BURNT WIRES IN FORWARD PIT AT STA 654 -PDU WIRE BUNDLE. DAMAGED CARGO LOADING SYSTEM WIRES REPAIRED PER SWPM 20-10-13 AND OPS CHECK GOOD PER MM 25-53-01. CAUSE SUSPECTED TO BE METAL SHAVINGS PRODUCING AN ELECTRICAL SHORT AT BURN LOCATION. 2L72 4F4 FRTA1NM E24NE 20060214001642006021400164NE 2006 2 14 JYD2006F00000 120051209A62306595211521101 BEARING SKRSKYS64 CH54B 8142610NE PWA JFTD12JFTD12A5A 52047NE MAIN ROTOR SPALLED B JYDRO OTHER O OTHER NRNOT REPORTED 1 NM09159AC A10105 64084 BEARING OUTER RACE SPALLED AND CRACKED. SPALLING AND CRACK ARE ON NR1 BEARING ROW ONLY. CRACK IS APPROXIMATELY 2.25 INCHES LONG. PROBABLE CAUSE IS UNKNOWN. THE BEARING RACE WILL BE ANALYZED TO DETERMINE THE CAUSE. THERE ARE NO RECOMMENDATIONS TO PREVENT RECURRENCE AT THIS TIME. (K) 2G72 4U4 U H6EA E15EA 20060214001992006021400199EA 2006 2 14 COMA0660125 120050207A335020131A BATTERY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT FAULTY A COMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SO01451CA11363 7562 FLIGHT 5268 - DURING TEST OF THE EMERGENCY LIGHTING, CABIN LIGHTS WOULD NOT ILLUMINATE. REPLACED EMERGENCY BATTERY PACKS. 2L72 4F RTA21EA 20060214002032006021400203CE 2006 2 14 HYI2006F00006 120051202A3230602EN556B UPLOCK SWITCH CESSNA402 402C 207590RCE CONT O520 TSIO520* 17040SO LG SYS FAILED E HYIAO OTHER J WARNING INDICATION CLCLIMB 1 NE01618CA 402C0620 CREW REPORTED GEAR UNSAFE LIGHT REMAINED ON WITH GEAR HANDLE IN UP POSITION, MAINTENANCE ATTEMPTED TO REMOVE AND REPLACE THE RT UPLOCK MICROSWITCH, 2 SWITCHES FAILED (BAD FROM STOCK) BEFORE INSTALLING A SERVICEABLE UNIT, GEAR SWING CHECKS, OK. AIRCRAFT RELEASED FOR SERVICE. (K) 1L72 3O3 O A7CE E8CE 20060215001092006021500109 2006 2 15 XN0A1279 420051202A2211 CONTROL UNIT AIRBUS300 A300B4203 3930306EU YAW DAMPER FAILED A XN0AD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL23473AS 203 NR 2 YAW DAMPER WILL NOT ENGAGE. TRANSFERRED TO DMI LOG 5951 IAW ENA MEL REFERENCE 22-21-01 CAT-A. REMOVED AND REPLACED YAW DAMPER ENGAGE UNIT, OPS CHECK OK IAW A300 AMM 22-11-12. THIS CLEARS DMI 5951. PLACARDS REMOVED. 2L72 4F RTA35EU 20060215001162006021500116NM 2006 2 15 F3LA200500049 120051221A2782830C0000 ACTUATOR AIRBUSA319 A319111 3930336NM SLATS TRIPPED A F3LAO OTHER F FLT CONT AFFECTED APAPPROACH 1 NM03937FR 2948 2400 UPON APPROACH, FLIGHT CREW REPORTED ECAM F/CTL SLATS FAULT. PERFORMED TSM TASK 27-81-00-810-810. FOUND TORQUE LIMITERS POPPED ON SLAT ROTARY ACTUATORS 6079 CM AND 6029 CM. REPLACED SLAT ROTARY ACTUATORS 6079 CM AND 6029 CM PER AMM 27-84-49-000-001 AND 27-84-49-400-001. PERFORMED SLATS OPS TEST PER AMM 27-84-00-710-001. OPS TEST GOOD. 2L72 4F RTA28NM 20060215001302006021500130NM 2006 2 15 XN0A1283 120051213A3220 STRUT BOEING727 727227 1384078NM NLG LOW A XN0AD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL2373751 21247 ON TAXI OUT THE NOSE GEAR SEEMED TO BOTTOM OUT. INSPECTED NOSE STRUT ASSY AND FOUND STRUT LOW ON NITROGEN, SERVICED NLG STRUT WITH NITROGEN IAW B727 MM CHAPTER 32-10-00. 2L73 4F A3WE 20060215002122006021500212EA 2006 2 15 ASOA051079 120051210A2530 ODOR CNDAIRCL600 CL6002B19 1900309EA GALLEY DETECTED A ASOAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO27821AS 7194 THE FLIGHT ATTENDANT REPORTED A POSSIBLE BURNING ODOR ASSOCIATED WITH THE NR 1 GALLEY HEATER. (M) 2L72 4F RTA21EA 20060214002252006021400225CE 2006 2 14 HYI2006F00003 120051202A3230602EN556B UPLOCK SWITCH CESSNA402 402C 207590RCE CONT O520 TSIO520* 17040SO WHEEL WELL FAILED E HYIAO OTHER J WARNING INDICATION CLCLIMB 1 NE012615G4 402C0101 CREW REPORTED LT MAIN GEAR DID NOT FULLY RETRACT WITH HEAR HANDLE IN UP POSITION, MAINTENANCE REMOVED AND REPLACED THE LT UPLOCK MICROSWITCH, GEAR SWING CHECKS, OK. AIRCRAFT RELEASED FOR SERVICE. (K) 1L72 3O3 O A7CE E8CE 20060215001172006021500117NM 2006 2 15 HNAA0500104 120051216A242082455004005 WIRE HARNESS DHAV DHC8 DHC8102 2809003NM NR 1 AC GEN SHORTED A HNAAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 EA07937HA4397143971 148 NR 1 A/C GEN C/L ILLUMINATED IN FLIGHT AND WILL NOT RESET. REPLACED A/C GENERATOR WIRING HARNESS AND CONNECTOR. 2H72 4T RTA13NM 20060215002062006021500206EU 2006 2 15 F3LA200500048 120051220A3220 LUG AIRBUSA318 A318111 3940019EU LANDING GEAR DAMAGED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03805FR 2101 1660 WHILE PERFORMING A BORESCOPE INSPECTION PER EO A0-32EO-20391 (AD 2005-24-06), INSPECTION FOUND DAMAGE TO THE NOSE LANDING GEAR UPPER SUPPORT, THREE ANTI-ROTATIONAL LUGS WERE FOUND TO BE SHEARED AND ONE ANTI-ROTATIONAL LUG WAS FOUND TO BE CRACKED. THE NOSE LANDING GEAR REQUIRES REPLACEMENT. AN ADDENDUM WILL BE SUBMITTED WHEN THE NOSE LANDING GEAR HAS BEEN REPLACED. ADDENDUM: REPLACED THE NOSE LANDING GEAR ASSEMBLY ON 12/27/05. 2L72 4F RT 20060215002212006021500221EA 2006 2 15 ASOA051125 120051219A3350 LIGHT CNDAIRCL600 CL6002C10 1390015EA CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27750EV 10161 DURING A HANGAR INSPECTION IN BTR, THE AFT AND FORWARD CEILING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMPS IN THE AFT AND FORWARD CEILING EMERGENCY LIGHT ASSEMBLIES. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060215002272006021500227EA 2006 2 15 ASOA051134 120051221A2611 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA SMOKE WARNING MALFUNCTIONED A ASOAK NONE N FALSE WARNING TOTAKEOFF 1 SO27873AS 7549 DURING TAKEOFF FROM PIA-ATL, THE CREW RECEIVED A `SMOKE TOILET` CAUTION MESSAGE. THE CREW COMPLIED WITH THE QRH AND DECLARED AND EMERGENCY. THE AIRCRAFT RETURNED TO PIA, WHERE IT LANDED SAFELY. MAINTENANCE INSPECTED THE LAVATORY AND AFT EQUIPMENT BAY WITH NO EVIDENCE OF SMOKE OR FIRE DETECTED. MAINTENANCE THEN CLEANED OIL IN THE AFT EQUIPMENT BAY. NO OTHER DEFECTS WERE NOTED AND MAINTENANCE CLEARED THE DEFERRED LAVATORY SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060216001142006021600114NM 2006 2 16 AWXA200600241 120051219A53306545785U9 SKIN BOEING737 73733A 1384673NM BS 500D CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - DURING C19 CHECK DISCOVERED FUSELAGE SKIN CRACK JUST BELOW STRINGER 12R AND BS 500D+18". MAINTENANCE REMOVED DAMAGED AREA IAW AMERICA WEST AIRLINES (AWA) ENGINEERING REPAIR (ER) NR 03-5331-06013-ES2. FABRICATED DOUBLER, TRIPLER AND FILLER IAW AWA ER NO. 03-5331-06013-ES2. INSTALLED FABRICATED REPAIR PARTS AND NEW WINDOW FRAME AT BS 500D+18 AND STRINGER 12R IAW AWA ER NR 03-5331-06013-ES2. 2L72 4F RTA16WE 20060216001262006021600126NM 2006 2 16 AWXA200600254 120051010A5247 DOOR BOEING737 7373B7 1384580NM APU DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28328AW 23377 PHX - DISCOVERED PREVIOUS BLEND OUT AT STA 1088, ABOVE THE FORWARD RT CORNER OF THE APU DOOR. WAS DETERMINED TO BE CHAFFING DAMAGE ABOUT 6" AFT OF STA 1088 AT STR 20R. DEEP BLENDED OUT AREA WAS NOT COVERED IN THE BOEING 737-300 SRM. MAINTENANCE CLEANED AND INSPECTED THE DAMAGED AREA TO ENSURE NO CRACKS EXISTED, NONE WERE ALLOWED AND NONE WERE FOUND. FABRICATED EXTERNAL DOUBLER FROM 2024-T3 IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NO. 03-5381-05285-HF1. FABRICATED REPAIR PARTS WERE INSTALLED WET AT BS 1088, STR 20R IAW AWA ER NO. 03-5381-05285-HF1. 2L72 4F RTA16WE 20060216001272006021600127EU 2006 2 16 AWXA200600251 120051018A5411 RIB AIRBUS320 A320232 3930326EU LT PYLON DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28658AW 1110 PHX - DURING ROUTINE MAINTENANCE THE LT PYLON NUMBER 5-RIB, LINE ATTACHMENT CLEATS (PN'S D463072820000 & D54610270200) WERE FOUND WORN AND ELONGATED AT SEVERAL LINE ATTACHMENT POINTS. MAINTENANCE REMOVED DISCREPANT PARTS FROM THE LT PYLON. WELDED DISCREPANT LANDING AREAS USING AIRBUS PROCESS SPECIFICATIONS, BUILDING THE LANDINGS BACKUP LARGER THAN DRAWING TOLERANCES. MACHINED THE REPAIR LANDING AREA TO DRAWING D54630728 IAW AWA ER 26-5411-05292-SS1. VISUALLY AND PENETRANT INSPECTED THE REPAIR CLEATS FOR CRACKS AND OTHER DEFECTS. RE-INSTALLED CLEATS WITH SAME TYPE OF FASTENERS AS REMOVED. ALL LINES WERE LEAK CHECKED AND CLEAT CLAMPINGS WERE SECURED PRIOR TO CLOSING UP OF COWLINGS. REPAIRED CLEATS WERE REP2L72 4F RTA28NM 20060215002562006021500256NM 2006 2 15 2005UALA01247 120051108A5711 SPAR BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE LT WING CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29668UA 30024 LEFT WING FRONT SPAR IS CRACKED, PUNCTURED AT NR 1 LEADING EDGE SLAT, INBD AUX TRACK. DETERMINED SLAT SENSOR TARGET WAS PREVIOUSLY INSTALLED 180 DEGREES OUT, CAUSING DAMAGE. LEFT WING FRONT SPAR WAS FOUND CRACKED, PUNCTURED AT THE NR 1 LEADING EDGE SLAT, INBOARD AUX TRACK. DETERMINED THAT THE SLAT SENSOR TARGET WAS PREVIOUSLY INSTALLED 180 DEGREES OUT, THEREBY, CAUSING DAMAGE. THE DAMAGE WAS REPAIRED CUTTING OUT THE DAMAGE PORTION OF THE WEB AND FABRICATING A REPLACEMENT WEB, SPLICE STRAPS PER TIMCO REO (EVA) G11121, REV B. UA-EVA-50770 WAS GENERATED DUE TO FOLLOW SUPPLEMENTAL INSPECTION REQUIREMENT FOR THE REPAIR (REF: EVA EG FU-298). 2L72 4F4 FRTA1NM E24NE 20060216001952006021600195WP 2006 2 16 IXXA05SMN274S 120051215A5751 SKIN DOUG DC8 DC872 302199BWP LT AILERON CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11722CX71621 46130 DURING ROUTINE C-CHECK INSPECTION, DURING ROUTINE C-CHECK INSPECTION, LT IB AIL LWR SKIN CORRODED, STA 593.000. PERFORMED MAJOR REPAIR IAW SRM 52-2-0 FIG. 4 (SHEET 3). REMOVED EXISTING REPAIR IAW SRM 51-1-21. FABRICATED REPAIR DOUBLER (ALCLAD 7075 T6 0.050”) IAW SRM 52-2-0 FIG. 4 (SHEET 3), SRM 52-3-2 FIG. 1. ITEM L, SRM 51-9-0 FIG. 68A. CLEANED, TREATED AND PRIMED AREA REPAIR DOUBLER IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11. INSTALLED REPAIR DOUBLER IAW SRM 52-2-0 FIG. 4 (SHEET 3), SRM 51-1-21. 2L74 4F RT4A25 20060216001962006021600196WP 2006 2 16 IXXA05SMN289S 120051229A5320 FITTING DOUG DC8 DC872 302199BWP FUSELAGE CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11722CX71621 46130 DURING ROUTINE C-CHECK INSPECTION, FWD ACCY COMPT INTERNAL PART FITTING CORRODED AT STA 270.000, L-30 (RT)REMOVED CORROSION FROM FITTING IAW SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PAGE 2A. REMOVED CORRODED FITTING IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2L74 4F RT4A25 20060216002072006021600207NM 2006 2 16 S2YA05079 120051201A2132 WARNING SYSTEM DORNERDO32 DO328300 NM PWA 306 PW306B NE COCKPIT MALFUNCTIONED A S2YAGB O2 MASK DEPLOYED EMER. DESCENT N FALSE WARNING DEDESCENT 1 GL13351SK 3108 DURING FLIGHT, DURING INITIAL DESCENT AFTER PULLING POWER BACK, THE CREW NOTED A LT PACK FAIL/CABIN HIGH CASS MESSAGES AT FL280. THE CREW DEPLOYED THE O2 MASKS AND REQUESTED FL100. THE CREW MADE AN UNEVENTFUL LANDING. MX INSPECTED THE AC AT MULTIPLE POWER AND BLEED CONFIGURATIONS BUT WERE UNABLE TO DUPLICATE PROBLEM. WITH NO FURTHER DISCREPANCIES RETURNED THE AC TO SERVICE. PROBLEM HAS NOT RETURNED. (K) 2H72 4T4 FRTA55NM E35NE 20060216003162006021600316WP 2006 2 16 UPS06846160 120050113A53205753113501N FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01702UP 45902 HEAVY CORROSION ON AFT SIDE OF FITTING BETWEEN LT W/W CIELING AND L24L AT STA 920. REMOVED AND REPLACED FITTING AND REPAIR SPLICE IAW SRM 53-2-0 FIG 008 AND 51-03-01. 2L74 4F RT4A25 20060216003232006021600323NM 2006 2 16 0601055 120051201A5320 FLOOR SUPPORT BOEING737 737230C 1384472NM FUSELAGE CORRODED A MJYAK NONE O OTHER ININSP/MAINT 1 SW05767TW 20258 MAIN CABIN CARGO FLOOR SUPPORT CHANNEL CORRODED. 2L72 4F A16WE 20060216003252006021600325NM 2006 2 16 0601054 120051201A575565799528 SPOILER BOEING737 737230C 1384472NM NR 3 DELAMINATED A MJYAK NONE O OTHER ININSP/MAINT 1 SW05767TW 20258 REPAIRED LEFT WING NR 3 SPOILER DUE TO DELAMINATION. 2L72 4F A16WE 20060216003272006021600327NM 2006 2 16 0601053 120051201A5320656852314A STRAP BOEING737 737230C 1384472NM FUSELAGE CRACKED A MJYAK NONE O OTHER ININSP/MAINT 1 SW05767TW 20258 MAIN CARGO CABIN SUPPORT STRAP CRACKED AT MAIN DOOR LOWER SECTION. 2L72 4F A16WE 20060216001242006021600124NM 2006 2 16 AWXA200600252 120051001A5753 SKIN BOEING757 7572G7 1384963NM TE FLAP DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28910AW 24523 PHX - DISCOVERED THE LT INBOARD FLAP DELAMINATING, 20.5" BY 17.5", ADJACENT TO AND UNDERNEATH THE NR 5 SPOILER PANEL. MAINTENANCE REMOVED DELAMINATED CORE AND INNER SKIN IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 19-5753-05275-HF1. FABRICATED FILLER AND DOUBLER IAW BOEING 757-200 SRM 51-70-10 AND AWA ER 19-5753-05275-HF1. BONDED REPAIR PARTS TO THE LT INBOARD TRAILING EDGE FLAP IAW AWA ER 19-5753-05275-HF1. TAP TEST WAS PERFORMED ON REPAIR AREA TO ENSURE NO DAMAGE EXISTED. THE T/E FLAP PANEL WAS PLACED ON MONITOR TO BE REPLACED NO LATER THAN THE NEXT C CHECK. 2L72 4F RTA2NM 20060216001252006021600125NM 2006 2 16 AWXA200600253 120050927A5753 SKIN AIRBUSA319 A319132 3930340NM RT TE FLAP DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28801AW 889 PHX - DISCOVERED THE RT OUTBOARD FLAP ASSEMBLY, TRAILING EDGE SEPARATING. DAMAGED COMPOSITE HONEYCOMB 7" BY 9". MAINTENANCE REMOVED TOP SKIN AND CORE. ADDITIONAL CORROSION WAS FOUND UNDER UPPER SKIN. REMOVED CORRODED CORE, FINAL DIMENSION OF REMOVED SECTION WAS FROM OUTBOARD EDGE OF FLAP TO 27.5" INBOARD. FABRICATED REPLACEMENT SKIN, CORE AND SPLICE STRAP IAW AMERICA WEST ENGINEERING REPAIR NR 25-5752-05270-RC1. INSTALLED AND BONDED SKIN, CORE AND SPLICE STRAP TO THE RT OUTBOARD FLAP, TRAILING EDGE, IAW AWA ER NR 25-5752-05270-RC1. 2L72 4F RTA28NM 20060216003262006021600326NM 2006 2 16 0601052 120051201A532065621004 FLOOR SUPPORT BOEING737 737230C 1384472NM FUSELAGE CORRODED A MJYAK NONE O OTHER ININSP/MAINT 1 SW05767TW 20258 CARGO CABIN FLOOR SUPPORT CORRODED. 2L72 4F A16WE 20060216003652006021600365NM 2006 2 16 P5CA0601429 120050112A36103206247 RELIEF VALVE BOEING747 747230B 1384889NM NR 1 ENGINE FAILED A P5CAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 EA15509MC 21221 CREW REPORTED NR 1 ENGINE NACELLE TEMP WENT TO TOP END OF SCALE. RETARDED THROTTLES, TEMP DECREASED. RETURNED TO RMS. FOUND NR 1 ENGINE PRESSURE RELIEF VALVE FAILED. REPLACED PER AMM 36-11-03. OPS OK. 2L74 4F A20WE 20060216003852006021600385NM 2006 2 16 P5CA0601424 120051220A2400 ODOR BOEING747 7472F6B 1384807NM COCKPIT DETECTED A P5CAK NONE B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 EA15534MC 21832 DURING DESCENT HAD STRONG ELECTRICAL SMELL IN COCKPIT. PERFORMED INSPECTION OF COCKPIT, UNABLE TO FIND SOURCE OF ELECTRICAL SMELL. 2L74 4F A20WE 20060217000212006021700021CE 2006 2 17 HYI2006F00004 120051202A3260602EN556B UPLOCK SWITCH CESSNA402 402C 207590RCE CONT O520 TSIO520* 17040SO MLG FAILED E HYIAO OTHER O OTHER NRNOT REPORTED 1 NE01618CA 402C0620 CREW REPORTED GEAR UNSAFE LIGHT REMAINED ON WITH GEAR HANDLE IN UP POSITION, MAINTENANCE REMOVED AND REPLACED THE RT UPLOCK SWITCH, GEAR SWING CHECKS OK. AIRCRAFT RELEASED FOR SERVICE. (K) 1L72 3O3 O A7CE E8CE 20060217000272006021700027 2006 2 17 S2YA05070 420051023A3416066306200 ALTIMETER BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE COCKPIT STICKING A S2YAA UNSCHED LANDING O OTHER CLCLIMB 1 GL1381SK 636 UE81 ON CLIMB OUT OF FLIGHT, THE CREW REPORTED THE CAPTAIN`S ALTIMETER FROZE UP (STOPPED CLIMBING) WERE PERFORMEING AN AIR-TURN-BACK. UPON ARRIVAL BACK, THE ALTIMETER BEGAN TO WORK AGAIN. MX REPLACED THE ALTIMETER AND RETURNED THE AC TO SERVICE. (K) 2L72 4T4 TRTA24CE E26NE 20060217000282006021700028NM 2006 2 17 S2YA05063 120051007A291342152 PUMP DORNERDO32 DO328300 NM PWA 306 PW306B NE HYD SYSTEM INOPERATIVE A S2YAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL13351SK6790 2959 3108 SHORTLY AFTER DEPARTURE OF FLIGHT, THE CREW REPORTED A HYDRAULIC A PUMP AMBER CAS MESSAGE. THE CREW PERFORMED AN AIR-TURN-BACK. THE CREW NEED TO MANUALLY EXTEND THE GEAR AND LANDED SAFELY. MX REPLACED THE A SYSTEM AC HYDRAULIC PUMP AND RETURNED THE AC TO SERVICE. (K) 2H72 4T4 FRTA55NM E35NE 20060217000292006021700029CE 2006 2 17 HYI2006F00002 120051202A3260602EN556B UPLOCK SWITCH CESSNA402 402C 207590RCE CONT O520 TSIO520* 17040SO MLG FAILED E HYIAO OTHER O OTHER NRNOT REPORTED 1 NE012615G 402C0101 CREW REPORTED GEAR UNSAFE LIGHT REMAINTED ON WITH GEAR HANDLE IN UP POSITION, MAINTENANCE REMOVED AND REPLACED THE LT UPLOCK MICROSWITCH, GEAR SWING CHECKS, OK. AIRCRAFT RELEASED FOR SERVICE. (K) 1L72 3O3 O A7CE E8CE 20060217000302006021700030NM 2006 2 17 S2YA05068 120051021A75005682C000 SWITCH DORNERDO32 DO328300 NM PWA 306 PW306B NE BLEED AIR SYS INOPERATIVE A S2YAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL13360SK 3136 BEFORE FLIGHT, THE CREW ABORTED THE TAKEOFF BECAUSE OF A LT LOW PRESSURE PRSOV FAILED. MX SWAPPED THE LT AND RT LOW PRESSURE PRSOV FOR TROUBLE SHOOTING AND RETURNED THE AC TO SERVICE. LT LOW PRESSURE PRSOV FAILED AT LOW POWER. MX REPLACED THE 95HB OVERPRESSURE SWITCH AND WITH OPS CHECKS GOOD RETURNED THE AC TO SERVICE. (K) 2H72 4T4 FRTA55NM E35NE 20060217000312006021700031NE 2006 2 17 S2YA05064 220051010A73208228234008 EEC DORNERDO32 DO328300 NM PWA 306 PW306B NE LT ENGINE MALFUNCTIONED A S2YAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL13356SK 3163 DURING FLIGHT, THE CREW REPORTED A LT FADEC MAJOR CAS MESSAGE. THE CREW PERFORMED AN AIR-TURN-BACK. MX COULD NOT DUPLICATE THE DISCREPANCY. MX REPLACED THE LT ELECTRONIC ENGINE CONTROL (EEC) FOR TROUBLESHOOTING AND RETURNED THE AC TO SERVICE. (K) 2H72 4T4 FRTA55NM E35NE 20060217000532006021700053NM 2006 2 17 UPS06M46163 120051206A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01282UP 48452 EMPENNAGE-BARREL NUT HOLE NR 1 LT FOUND WITH SURFACE CORROSION ON SIDE AND BOTTOM AREA. CORROSION REMOVAL C/OUT AFFECTED AREA PER SRM 51-21-01.V2.R38, FOUND BLEND OUT EXCEEDED LIMIT PER MD11-5510-19409-K, REPAIR SLEEVE BUSHING FAB PER MD11-5510-19409-K, APPLIED SEALANT PR1422B 1/2 ON SLEEVE AND BORE AREA. INSTALLED REPAIR SLEEVE BUSHING ON B/N HOLE NR 1 LT BORE. REPAIR ACCOMPLISHED AT B/N HOLE NR 1 LT PER EN 1626-05, FOUND SATIS. 2L73 4F RTA22WE 20060217000542006021700054NM 2006 2 17 UPS06M46164 120051207A5510 BEARING DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01282UP 48452 EMPENNAGE-BARREL NUT HOLE NR 33 LT FOUND BEARING WITH SURFACE CORROSION ON SIDE AND BOTTOM AREA. CORROSION REMOVAL C/OUT AFFECTED AREA PER SRM 51-21-01.V2.R38, FOUND BLEND OUT EXCEEDED LIMIT PER MD11-5510-19409-K, REPAIR SLEEVE BUSHING FAB PER MD11-5510-19409-K, APPLIED SEALANT PR1422B 1/2 ON SLEEVE AND BORE AREA. INSTALLED REPAIR SLEEVE BUSHING ON B/N HOLE NR 33 LT BORE. REPAIR ACCOMPLISHED AT B/N HOLE NR 33 LT PER EN 1040-06, FOUND SATIS. 2L73 4F RTA22WE 20060217000702006021700070NE 2006 2 17 S2YA05074 220051104A7200 EEC DORNERDO32 DO328300 NM PWA 306 PW306B NE LT ENGINE MALFUNCTIONED A S2YAO OTHER J WARNING INDICATION CLCLIMB 1 GL13353SK 3122 SHORTLY AFTER TAKEOFF, THE CREW REPORTED A LT FADEC MAJOR CAS MESSAGE. MX REQUESTED THE PERFORMED AN AIR-TURN-BACK, BECAUSE OF PRIOR HISTORY (LISTED BELOW). MX REPLACED TWO RELAYS AND SCHEDULED A TEST FLIGHT. AFTER THE TEST FLIGHT, HAD NO DISCREPANCIES THE AC WAS RETURNED TO SERVICE. LT FADEC FAULT: MX FOUND FAULT CODE (5A) BUT COULD NOT DUPLICATE THE PROBLEM. WITH MX CONSULT THE MESSAGE CLEARED ON GROUND. MX REPLACED THE LT EEC FOR TROUBLE SHOOTING AND REINITIALIZED. 2H72 4T4 FRTA55NM E35NE 20060217000712006021700071NM 2006 2 17 S2YA05077 120051117A32347178011 HANDLE DORNERDO32 DO328300 NM PWA 306 PW306B NE MLG INOPERATIVE A S2YAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL13354SK13327 3126 SHORTLY AFTER TAKEOFF, THE CREW REPORTED A GROUND SPOILER FAIL CAS MESSAGE AND THEY WERE UNABLE TO RETRACT THE LANDING GEAR. THE CREW PERFORMED AN AIR-TURN-BACK. MX REPLACED LANDING GEAR LEVER AND WITH NO FURTHER DISCREPANCIES RETURNED THE AC TO SERVICE. (K) 2H72 4T4 FRTA55NM E35NE 20060217000732006021700073CE 2006 2 17 S2YA05083 120051223A2100 LINE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE CABIN AIR LOOSE A S2YAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL1387SK UE87 DURING FLIGHT, THE CREW REPORTED RT ENVIRO FAIL AND CABIN ALT HIGH. SINCE THE FLIGHT LEVEL WAS RESTRICTED TO 9500 FT THE CREW PERFORMED AN AIR-TURN-BACK. MX REPLACED THE LT PRSOV BUT THAT DID NOT FIX THE PROBLEM. MX INSPECTED THE SYSTEM AND FOUND A LOOSE TEST LINE AFTER TIGHTENING THE LINE THE SYSTEM OPS CHECKED GOOD AND THE AC WAS RETURNED TO SERVICE. (K) 2L72 4T4 TRTA24CE E26NE 20060217000742006021700074CE 2006 2 17 S2YA05082 120051211A561010138402523 WINDSHIELD BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE COCKPIT CRACKED A S2YAA UNSCHED LANDING O OTHER CRCRUISE 1 GL1379SK 3452 UE79 DURING FLIGHT, THE LT WINDSHIELD CRACKED. THE CREW PERFORMED AN AIR-TURN-BACK. MX REPLACED THE LT WINDSHIELD AND RETURNED THE AC TO SERVICE. (K) 2L72 4T4 TRTA24CE E26NE 20060217000752006021700075NM 2006 2 17 S2YA05081 120051214A2497 WIRE DORNERDO32 DO328300 NM PWA 306 PW306B NE ALTERNATOR CHAFED A S2YAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL13358SK 3188 SHORTLY AFTER TAKEOFF, THE CREW RECEIVED RT LAT FAIL. THE CREW BY REQUEST OF MX PERFORMED AN AIR-TURN-BACK. MX INSPECTED THE RT ALTERNATOR SYSTEM AND FOUND A WIRE HAD CHAFED ON THE COWL DOOR FORWARD ROD BRACKET IAW A SPR MX REPAIRED THE WIRE AND RETURNED THE AC TO SERVICE. (K) 2H72 4T4 FRTA55NM E35NE 20060217000762006021700076NM 2006 2 17 S2YA05076A 120051113A2400243831 CONTROL BOX DORNERDO32 DO328300 NM PWA 306 PW306B NE LT ALTERNATOR INOPERATIVE A S2YAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL13357SK12146 3164 SHORTLY AFTER TAKEOFF OF FLIGHT, THE CREW REPORTED A LT ALTERNATOR AND LT AC VOLT FAIL CAS MESSAGES. THE CREW PERFORMED AN AIR-TURN-BACK. MX REPLACED LT ALTERNATOR (AC GENERATOR) AND WITH NO FURTHER DISCREPANCIES RETURNED THE AC TO SERVICE. ON THE SAME FLIGHT, SECOND ATTEMPT THE SAME PROBLEM RETURNED THE CREW PERFORMED A SECOND AIR-TURN-BACK. MX REPLACED THE LT ALTERNATOR CONTROL BOX AND WITH NO FURTHER DISCREPANCIES RETURNED THE AC TO SERVICE. (K) 2H72 4T4 FRTA55NM E35NE 20060217000792006021700079NM 2006 2 17 S2YA05073 120051104A2421ALT3524 GENERATOR DORNERDO32 DO328300 NM PWA 306 PW306B NE RT AC INOPERATIVE A S2YAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL13358SK1189 3188 SHORTLY AFTER TAKEOFF, THECREW CALLED FOR A MX CONSULT SINCE THE RT ALTERNATOR (AC GENERATOR) FAILED IN FLIGHT. THE CREW AT MX REQUEST PERFORMED AN AIR-TURN-BACK. MX REPLACED THE RT ALTERNATOR AND RETURNED THE AC TO SERVICE. (K) 2H72 4T4 FRTA55NM E35NE 20060217000812006021700081CE 2006 2 17 S2YA05072 120051031A36101143840391 PRESSURE SWITCH BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE BLEED AIR SYS INOPERATIVE A S2YAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL1387SK 22889 UE87 ON TAKEOFF OF FLIGHT, THE CREW REPORTED THE RT ENVIRONMENTAL BLEED AIR SYSTEM FAILED AND ABORTED THE TAKEOFF. THE SYSTEM WAS PUT ON MEL AND THE AC WAS RETURNED TO SERVICE. REPLACED A BAD PRESSURE SWITCH AND WITH NO FURTHER DISCREPANCIES RETURNED THE AC TO SERVICE. (K) 2L72 4T4 TRTA24CE E26NE 20060217000842006021700084CE 2006 2 17 S2YA05067 120051019A284010038901827 PRESSURE SWITCH BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE FUEL SYS INOPERATIVE A S2YAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL13881SK UE88 DURING FLIGHT, THE CREW REPORTED THE RT AUX PUMP AUTO FUNCTION DID NOT STOP THE PUMP, RT NO AUX TRANSFER ILLUMINATED WHEN PUMP WAS IN AUTO FUNCTION. BETWEEN MX AND OPS, IT WAS DECIDED AN AIR-TURN-BACK WAS THE BEST OPTION. MX INSPECTED THE SYSTEM BUT COULD NOT DUPLICATE THE PROBLEM. MX TRANSFERRED 100 POUNDS OF FUEL WITH NO DISCREPANCIES. THE AC WAS RETURNED TO SERVICE. (K) 2L72 4T4 TRTA24CE E26NE 20060217000852006021700085CE 2006 2 17 S2YA05066B 120051013A2750101380002 FLEX DRIVE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE TE FLAPS DAMAGED A S2YAO OTHER J WARNING INDICATION CLCLIMB 1 GL13901SK UE90 SHORTLY AFTER TAKEOFF, THE CREW REPORTED THE FLAPS WERE AT 17 DEGREES AND WILL NOT RETRACT. THE AC CONTINUED WITH THE FLAPS AT 17. THE FLAPS WHERE RAISED USING THE OVER RIDE SWITCH AND THE SYSTEM WAS PUT ON MEL. DISCOVERED THE FLAP MOTOR/GEARBOX STRUGGLING TO MOVE AND THE RT FLEX DRIVE CABLES NEAR THE GEARBOX TWISTED AT THE SPLINE. MX REPLACED THE FLAP MOTOR, GEARBOX AND BOTH RT FLEX DRIVE CABLES. WITH ALL OPS CHECKS WHERE GOOD AND NO FURTHER DEFECTS RETURNED THE AC TO SERVICE. (K) 2L72 4T4 TRTA24CE E26NE 20060217000862006021700086CE 2006 2 17 S2YA05065 120051007A2750100384040 MOTOR BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE TEFLAPS MALFUNCTIONED A S2YAO OTHER J WARNING INDICATION CLCLIMB 1 GL1381SK 2914 UE81 FLAPS FAILED TO EXTEND, SYS WAS MEL`D. MEL WAS CLEARED WHEN MX INSP SYS, OPS CHECKED IT, COULD NOT DUPLICATE DISCREPANCY. TROUBLESHOOTING REPLACED FLAP MOTOR AND FLAP POSITION RELAY (K105). SHORTLY AFTER TAKEOFF CREW REPORTED FLAPS WERE A 17 DEGREES AND WILL NOT RETRACT. AC CONTINUED WITH FLAPS AT 17. FLAPS WERE RAISED USING OVERRIDE SWITCH AND SYSTEM WAS PUT ON MEL. MX INSPECTED WIRING OF BOTH SAFETY SWITCHES AND REPLACED A TERMINAL END ON RT SAFETY SWITCH. ALL OPS CHECKS GOOD,WITH NO FURTHER DEFECTS RETURNED AC TO SERVICE. FLAPS STUCK AGAIN AT 17 DEGREES. MX REPLACED FLAP POSITION RELAY (K105). ALL OPS CHECKS WHERE GOOD, WITH NO FURTHER DEFECTS RETURNED AC TO SERVICE. (K) 2L72 4T4 TRTA24CE E26NE 20060217000872006021700087CE 2006 2 17 S2YA05066A 120051013A27501005210741 GEARBOX BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE TE FLAPS DAMAGED A S2YAO OTHER J WARNING INDICATION CLCLIMB 1 GL13901SK 1522 UE90 SHORTLY AFTER TAKEOFF THE CREW REPORTED THE FLAPS WERE AT 17 DEGREES AND WILL NOT RETRACT. THE AC CONTINUED WITH THE FLAPS AT 17. THE FLAPS WHERE RAISED USING THE OVER RIDE SWITCH AND THE SYSTEM WAS PUT ON MEL. MX DISCOVERED THE FLAP MOTOR/GEAR BOX STRUGGLING TO MOVE AND THE RT FLEX DRIVE CABLES NEAR THE GEARBOX TWISTED AT THE SPLINE. MX REPLACED THE FLAP MOTOR, GEAR BOX AND BOTH RT FLEX DRIVE CABLES. WITH ALL OPS CHECKS WHERE GOOD AND NO FURTHER DEFECTS RETURNED THE AC TO SERVICE. (K) 2L72 4T4 TRTA24CE E26NE 20060217000882006021700088CE 2006 2 17 S2YA05066C 120051013A2750101380006 FLEX DRIVE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE TE FLAPS DAMAGED A S2YAO OTHER J WARNING INDICATION CLCLIMB 1 GL13901SK UE90 SHORTLY AFTER TAKEOFF, THE CREW REPORTED THE FLAPS WERE AT 17 DEGREES AND WILL NOT RETRACT. THE AC CONTINUED WITH THE FLAPS AT 17. THE FLAPS WERE RAISED USING THE OVER RIDE SWITCH AND THE SYSTEM WAS PUT ON MEL. DISCOVERED THE FLAP MOTOR/GEAR BOX STRUGGLING TO MOVE AND THE RT FLEX DRIVE CABLES NEAR THE GEARBOX TWISTED AT THE SPLINE. MX REPLACED THE FLAP MOTOR, GEARBOX AND BOTH RT FLEX DRIVE CABLES. WITH ALL OPS CHECKS WHERE GOOD AND NO FURTHER DEFECTS RETURNED THE AC TO SERVICE. (K) 2L72 4T4 TRTA24CE E26NE 20060217000922006021700092GL 2006 2 17 ALG2006F00020 220051230A7200 ENGINE BELL 206 206L1 1182107SW ALLSN 250C 250C30P 03013GL MAKING METAL A ALGAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SW035759M 45555 ENGINE CHIP LIGHT ILLUMINATED ON START. PILOT FOLLOWED ENGINE CHIP LIGHT PROCEDURE. PILOT FOUND NO METAL ON CHIP PLUG AND REPLACED SAFETY WIRE. COMPLY WITH 30 MINUTE PENALTY RUN. AFTER RETURNING TO BASE NOTIFIED MAINTENANCE. ON POST FLIGHT EXAMINATION OF ENGINE CHIP PLUGS, METAL WAS DISCOVERED ON THE UPPER PLUG. AIRCRAFT WAS GROUNDED FOR ENGINE CHANGE. (K) 1G71 3U3 U H2SW E1GL 20060217000932006021700093CE 2006 2 17 S2YA05065B 120051007A2750SM50D7 RELAY BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE TE FLAPS FAILED A S2YAO OTHER J WARNING INDICATION CLCLIMB 1 GL1381SK UE81 FLAPS FAILED TO EXTEND, SYS WAS MEL`D. MEL WAS CLEARED WHEN MX INS SYS, OPS CHECKED, COULD NOT DUPLICATE DISCREPANCY. TROUBLESHOOTING REPLACED FLAP MOTOR AND FLAP POSITION RELAY (K105). SHORTLY AFTER TAKEOFF CREW REPORTED FLAPS WERE AT 17 DEGREES AND WILL NOT RETRACT. AC CONTINUED WITH FLAPS AT 17. FLAPS WERE RAISED USING OVERRIDE SWITCH AND SYS WAS PUT ON MEL. MX INSPECTED WIRING OF BOTH SAFETY SWITCHES AND REPLACED A TERMINAL END ON RT SAFETY SWITCH. ALL OPS CHECK GOOD WITH NO FURTHER DEFECTS, RETURNED AC TO SERVICE. FLAPS STUCK AGAIN AT 17 DEGREES. MX REPLACED FLAP POSITION RELAY (K105). ALL OPS CHECKS WERE GOOD, NO FURTHER DEFECTS. (K) 2L72 4T4 TRTA24CE E26NE 20060217001022006021700102CE 2006 2 17 S2YA05069 120051021A5270MD3211Q1 BRACKET BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE CARGO DOOR INOPERATIVE A S2YAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL1379SK UE79 DURING FLIGHT, THE CREW REPORTED THE CARGO DOOR ANNUCIATOR ILLUMINATED AND WERE PERFORMING AN AIR-TURN-BACK. THE ANNUCIATOR WAS MEL`D AND THE AC WAS RETURNED TO SERVICE. MX REPLACED THE ACTUATOR BRACKET AND CLEARED THE MEL. (K) 2L72 4T4 TRTA24CE E26NE 20060216001222006021600122NM 2006 2 16 AWXA200600249 120050430A5311 FRAME BOEING757 7572G7 1384963NM BS 720 DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28909AW 24522 PHX - FORWARD CARGO LOADING SYSTEM, AT BL 0, FROM STA 720 THROUGH STA 820, FRAMES DAMAGED BY LOADING JACK SCREW. MAINTENANCE TRIMMED OUT DAMAGE AREA IAW AWA ER 19-5332-05121-RA2. FABRICATED REPAIR ANGLES AND FRAME CLIPS IAW AWA ER NR 19-5332-05121-RA2. INSTALLED FABRICATED REPAIR PARTS FROM STA 720 THROUGH STA 820 IAW AWA ER NR 19-5332-05121-RA2. 2L72 4F RTA2NM 20060216001232006021600123EU 2006 2 16 AWXA200600250 120050913A5522 SKIN AIRBUS320 A320232 3930326EU RT ELEVATOR DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28659AW 1166 PHX - DURING INSPECTION DISCOVERED RT ELEVATOR HAD TRAILING EDGE DAMAGED. MAINTENANCE REMOVED DAMAGED SECTION ON THE TRAILING EDGE OF THE RT ELEVATOR. FABRICATED REPAIR PARTS FROM 2024T3 IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 26-5520-05256-HF1. INSTALLED REPAIR PARTS ONTO RT ELEVATOR TRAILING EDGE IAW AIRBUS 320 SRM 55-22-11 PB 201. 2L72 4F RTA28NM 20060216002012006021600201WP 2006 2 16 IXXA05SMN293S 120051229A5753 SKIN DOUG DC8 DC872 302199BWP T/E FLAP DAMAGED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11722CX71621 46130 DURING ROUTINE C-CHECK INSPECTION, RT OB FLAP HAS A NON STANDARD REPAIR ON UPPER SKIN, STA XF 210.000PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 4, TR NR 57-94, EO SEMAN NR 20051460 DATED 12-16-05. REMOVED DAMAGED PLATING IAW SRM 57-1-0, SRM 51-1-21. FABRICATED NEW PLATING (AL2024T30 0.040”) IAW SRM 57-7-1 FIG 4, TR NR 57-94 ITEM C DATED 10-01-02. CLEANED, TREATED AND PRIMED INNER FACE OF NEW PLATING IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACE IAW SRM 51-1-11 PG 9. INSTALLED NEW PLATING IAW SRM 51-1-21. 2L74 4F RT4A25 20060216002362006021600236CE 2006 2 16 HYI2006F00001 120051202A3260602EN556B UPLOCK SWITCH CESSNA402 402C 207590RCE CONT O520 TSIO520* 17040SO MLG FAILED A HYIAO OTHER O OTHER NRNOT REPORTED 1 NE012615G 402C0101 CREW REPORTED GEAR UNSAFE LIGHT REMAINED ON WITH GEAR HANDLE IN UP POSITION, MAINTENANCE ATTEMPTED TO REMOVE AND REPLACE THE LT HAND UP LOCK MICROSWITCH, 3 SWITCHES FAILED (BAD FROM STOCK) BEFORE INSTALLING A SERVICABLE UNIT, GEAR SWING CHECKS, OK. AIRCRAFT RELEASED FOR SERVICE. (K) 1L72 3O3 O A7CE E8CE 20060216002372006021600237CE 2006 2 16 HYI2006F00007 120051202A3260602EN556B UPLOCK SWITCH CESSNA402 402C 207590RCE CONT O520 TSIO520* 17040SO RT MLG FAILED E HYIAO OTHER O OTHER NRNOT REPORTED 1 NE01618CA 402C0620 CREW REPORTED RT MAIN GEAR DID NOT FULLY RETRACT WITH GEAR HANDLE IN UP POSITION, MAINTENANCE REMOVED AND REPLACED THE RT UPLOCK MICROSWITCH, GEAR SWING CHECKS OK. AIRCRAFT RELEASED FOR SERVICE. (K) 1L72 3O3 O A7CE E8CE 20060216003242006021600324NM 2006 2 16 0601056 120051201A573065508219422 SKIN PANEL BOEING737 737230C 1384472NM RT WING DELAMINATED A MJYAK NONE O OTHER ININSP/MAINT 1 SW05767TW 20258 RIGHT WING TRAILING EDGE LOWER PANEL DELAMINATED 2L72 4F A16WE 20060217000022006021700002EU 2006 2 17 KBM2006F00052 120050830A6410355A09103601 BEARING SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE TAIL ROTOR CRACKED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH1715 2957 HALF SHELL BEARINGS, UNIT CRACKED, REMOVED AND REPLACED WITH NEW. (K) 1G71 3U3 UNCH9EU E19EU 20060217000772006021700077 2006 2 17 S2YA05075 420051108A341606630620000 ALTIMETER BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE COCKPIT MALFUNCTIONED A S2YAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL1387SK 380 UE87 ON CLIMB OUT OF FLIGHT, THE CREW REPORTED THE CAPTAIN`S ALTIMETER FLAGGED SHORTLY AFTER ROTATION AND STAYED FLAGGED. THE CREW PERFORMED AND AIR-TURN-BACK. UPON ARRIVAL BACK, THE ALTIMETER BEGAN TO WORK AGAIN. MX REPLACED THE AITIMETER AND RETURNED THE AC TO SERVICE. (K) 2L72 4T4 TRTA24CE E26NE 20060217000902006021700090CE 2006 2 17 S2YA05065A 120051007A27501005210741 GEARBOX BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE TE FLAPS FAILED A S2YAO OTHER J WARNING INDICATION CLCLIMB 1 GL1381SK 116052914 UE81 FLAPS FIALED TO EXTEND, SYS WAS MEL`D. MEL WAS CLEARED WHEN MX INSP SYS, OPS CHECKED, COULD NOT DUPLICATE DISCREPANCY. TROUBLESHOOTING REPLACED FLAP MOTOR, FLAP POSITION RELAY (K105). SHORTLY AFTER TAKEOFF CRWE REPORTED FLAPS WERE A T 17 DEGREES AND WOULD NOT RETRACT. AC CONTINUED WITH FLAPS AT 17. FLAPS WERE RAISED USING OVERRIDE SWITCH AND SYSTEM WAS PUT ON MEL. MX INSPECTED WIRING OF BOTH SAFETY SWITCHES AND REPLACED TERMINAL END ON RT SAFETY SWITCH. ALL OPS CHECK GOOD, NO FURTHER DEFECTS, RETURNED AC TO SERVICE. FLAPS STUCK AGAIN AT 17 DEGREES. MX REPLACED FLAP POSITION RELAY (K105). ALL OPS CHECKS WERE GOOD, NO FURTHER DEFECTS, RETURNED AC TO SERVICE. (K) 2L72 4T4 TRTA24CE E26NE 20060216002592006021600259EU 2006 2 16 KNK2006F00001 120051228A6700SC5084 SERVO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE LWR PISTON SEAL LEAKING E KNKAO OTHER O OTHER NRNOT REPORTED 1 WP13112AK 3254 9644 SERVO LEAKING FROM LOWER POSTON SEAL. (K) 1G71 3U3 U H9EU E19EU 20060216003702006021600370WP 2006 2 16 DHL2006873001 120050105A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE DAMAGED A DHLAK NONE O OTHER NRNOT REPORTED 1 SO01873SJ 46091 K-LOADER PUNCHED A GAPING HOLE IN THE SIDE OF THE A/C. REPAIRED DAMAGE IAW DOUGLAS SRM 53-2-1 FIG 7 P105-106 FAA FORM 8100-9 & SRM 53-2-2 P47-48, NO DEFECTS NOTED. 2L74 4F RT4A25 20060217000552006021700055NM 2006 2 17 UPS06M46165 120051207A5510 BEARING DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01282UP 48452 INSPECTION TYPE:C EMPENNAGE-BARREL NUT HOLE NR 30 LT FOUND BEARING WITH SURFACE CORROSION ON SIDE AND BOTTOM AREA. CORROSION REMOVAL C/OUT AFFECTED AREA PER SRM51-21-01.V2.R38, FOUND BLEND OUT EXCEEDED LIMIT PER MD11-5510-19409-K, REPAIR SLEEVE BUSHING FAB PER MD11-5510-19409-K, APPLIED SEALANT PR1422B 1/2 ON SLEEVE AND BORE AREA. INSTALLED SLEEVE BUSHING ON B/N HOLE NR 30 LT BORE. REPAIR ACCOMPLISHED AT B/N HOLE NR 30 LT PER EN 1040-06 AND EN 1638-05, FOUND SATIS. 2L73 4F RTA22WE 20060217000782006021700078NM 2006 2 17 S2YA05074A 120051104A7600DOLN1081MSD4NL RELAY DORNERDO32 DO328300 NM PWA 306 PW306B NE MALFUNCTIONED A S2YAO OTHER J WARNING INDICATION CLCLIMB 1 GL13353SK 3122 SHORTLY AFTER TAKEOFF, THE CREW REPORTEDA LT FADEC MAJOR CAS MESSAGE. MX REQUESTED THE PERFORMED AN AIR-TURN-BACK BECAUSE OF PRIOR HISTORY. MX REPLACED 2 RELAYS AND SCHEDULED A TEST FLIGHT. AFTER THE TEST FLIGHT HAD NO DISCREPANCIES THE AC WAS RETURNED TO SERVICE. MX FOUND FAULT CODE 5A BUT COULD NOT DUPLICATE THE PROBLEM. WITH MX CONSULT THE MESSAGE CLEARED ON GROUND. MX REPLACED THE LT EEC FOR TROUBLESHOOTING AND REINITIALIZED. (K) 2H72 4T4 FRTA55NM E35NE 20060217000832006021700083CE 2006 2 17 S2YA05071 120051031A32601003810061 UPLOCK SWITCH BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE NLG INOPERATIVE A S2YAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL1385SK UE85 ON CLIMB OUT OF FLIGHT, THE CREW REPORTED THE RED IN TRANSIT LIGHT STAYED ILLUMINATED AFTER THE GEAR WAS SELECTED UP AND APPARENTLY DID FULLY RETRACT. THE RELEASE WAS AMENDED AND THE AC CONTINUED WITHOUT STOPPING. MX REPLACED THE NOSE GEAR UPLOCK SWITCH AND STRIKE BRACKET. THE SYSTEM WAS RIGGED AND OPS CHECK AND RETURNED THE AC TO SERVICE. (K) 2L72 4T4 TRTA24CE E26NE 20060221001582006022100158EU 2006 2 21 U0GA106525 120051028A28105010997 FUEL CELL UROCOPEC120 EC120B 8680987EU UPPER LEAKING B U0GAA UNSCHED LANDING K FLUID LOSS CRCRUISE 1 SW03116KG 1152 PILOT REPORTED SMELL OF FUEL IN COCKPIT FOR 5 - 10 MINUTES DURING CRUISE FLIGHT. UPON LANDING, MAINENANCE DISCOVERED A LEAK IN IN THE UPPER FUEL CELL AT THE AFT R/H SEAM. 1G72 3U NCR0001RD 20060221001592006022100159EU 2006 2 21 U0GA106526 120051028A6230109013410105 DRIVE LINK AGUSTAA109 A119 0261102EU MAST MISINSTALLED B U0GAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 SW03873MB 14034 UPON PREFLIGHT, PILOT NOTICED THAT ROTATING SCISSORS LINK WAS INCORRECTLY INSTALLED. 1G72 3U H7EU 20060221001712006022100171SW 2006 2 21 ALGA106747 120051008A6410206016201131 BLADE BELL 206 206B3 1181506SW TAIL ROTOR NONE B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03158H 911 2974 C/W AD 2004-24-08 AS PER ASB 206L-04-127 / SENT TO RBI TO C/W AD 2004-24-08 AS PER ASB 206L-04-127 1G71 3U H2SW 20060221001722006022100172SW 2006 2 21 ALGA106748 120051018A6410206016201131 BLADE BELL 206 206B3 1181506SW TAIL ROTOR NONE B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03158H 553 2974 C/W AD 2004-24-08 AS PER ASB 206L-04-127 / SENT TO RBI TO C/W AD 2004-24-08 AS PER ASB 206L-04-127 1G71 3U H2SW 20060221002182006022100218NM 2006 2 21 SB06019 120050220A335020121 CHARGER BOEING737 7374B7 1384702NM ROW 20 DEF FAULTY A USAAO OTHER O OTHER TXTAXI/GRND HDL 1 EA19445US 24863 CLT DURING ELECTRIC POWER INTERRUPTION AT GATE, CREW REPORTED THE EMERGENCY EXIT LIGHTS ILLUMINATED. FLIGHT ATTENDANT NOTICED NUMEROUS FLOOR AND OVERHEAD EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE FOUND THAT WHEN THE EMERGENCY LIGHTS ARE PLACED IN TEST MODE, THE MID TO AFT CABIN EMERGENCY LIGHTS EXTINGUISH AFTER FIVE SECONDS. REMOVED AND REPLACED BATTERY AND CHARGER ASSEMBLY FOR THAT SECTION OF EMERGENCY LIGHTS IN RIGHT-HAND CEILING ABOVE SEAT ROW 20. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20060221002382006022100238NM 2006 2 21 UPS06M46178 120051223A5730 SKIN DOUG MD11 MD11F 3023600NM LT WING CHAFED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01282UP 48452 INSPECTION TYPE:C LHW UPP SURFACE FIXED L/E AREA AT STA XRO 1192 APP (ON TOP LT NR 8 SLAT O/B EDGE AREA) FOUND CHAFF MARK. CHAFF MARK PER A/M DISCREPANCY BLENDED AND PROTECTED PER SRM 51-21-01.V2. R38.ORI THK 0.065,MAT REMOVED 0.031" FOUND EXCEEDED LIMIT. DAMAGED AREA TRIMMED DIA 1 1/2 BY 4 PER EN1042-06. HFEC INSP C/OUT, FOUND SATIS. NO CRACK EVIDENT. REPAIR SKIN FAB AND MAT USE 6061-0-0.063" BARE PER EN1042-06 REPAIR, WELDING AND GRINDING PER EN1042-06, FOUND JOB ACCOMPLISHED, SATIS. 2L73 4F RTA22WE 20060221002422006022100242NM 2006 2 21 UPS06M46167 120051206A2810 FUEL TANK DOUG MD11 MD11F 3023600NM CENTER CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01282UP 48452 INSPECTION TYPE:C CABIN, CORROSION ON UPPER SURFACE OF OF UPPER CTR FUEL TANK AT STA 1239 -1253 X=-107. FASTENERS AT UPPER SURFACE CTR FUEL TANK AT STA 1239-1253X=-107, REMOVED PER SRM 51-31-01 AND 51-33-01 V.2.R.38. CORROSION REMOVAL C/OUT PER SRM 51 -21-01V2.38, FOUND EXCEEDED LIMIT. C/OUT MAGNIFIED V/INSP AND FPI FOUND SATIS. FLAP PEENING C/OUT ON REWORKED AREAS PER CMM20-11-01.R51, IAW EN10 08-06. INSTALL FASTENERS AND REPAIR ACCOMPLISHED PER EN 1008-06, F/SATIS. 2L73 4F RTA22WE 20060221002452006022100245NM 2006 2 21 UPS06M46170 120051121A2810 FUEL TANK DOUG MD11 MD11F 3023600NM CENTER CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01282UP 48452 INSPECTION TYPE:C CABIN, CORROSION ON UPPER SURFACE OF CENTER FUEL TANK BETWEEN STA 1159- 1239 X=-75.0 TO 107.0. FASTENERS AT UPPER SURFACE CTR F/TANK REMOVED FOR ACCESS. CORROSION REMOVAL C/OUT PER SRM 51-33-01 V.2.R38, FOUND EXCEEDED LIMIT. C/OUT MAGNIFIED V/INSP AND FPI FOUND SATIS. FLAP PEENING C/OUT ON REWORKED AREAS PER CMM2 0-11-01.R51, IAW EN1008-06. FAB DOUBLER PER SRM51-31-01.V2.R38. REPAIR AC ACCOMPLISHED AND INSTALLATION COMPLETED PER EN 1008-06 FOUND SATIS. 2L73 4F RTA22WE 20060221002472006022100247CE 2006 2 21 ACE112805 120051128A2435 BEARING LUCAS BEECH 1900 1900C 1154161CE STARTER GEN FAILED E YADAK NONE GHJMULTIPLE FAILURE ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 AL03114AX 1440 97076 UC36 PILOT REPORTED RT GEN OFF LINE AND NO ENGINE STARTER AFTER LANDING - REPLACED STARTER/GENERATOR DUE FRONT BEARING FAILURE 2L72 4T RTA24CE 20060221002482006022100248WP 2006 2 21 DHL2005803500 120051111A5321 FLOOR PANEL DOUG DC8 DC873 302199CWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH8280 46123 ITEM REF. NR. 033352: MAIN CARGO COMPT. FLOOR PANEL CORRODED, STA 0440.000 LBL 56. REMOVED CORROSION FROM FLOOR PANEL STA 1440.000 LBL 56" IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG. 2P. CUT OUT DAMAGED SECTION AND FABRICATED DOUBLER (7075T6 0.080") AND FILLER (7075T6 0.063") IAW SRM 53-2-3 FIG. 10 PG. 39-40. CLEANED, TREATED AND PRIMED AREA, FILLER AND DOUBLER IAW SRM 51-1-8B. INSTALLED FILLER AND DOUBLER IAW SRM 51-1-21. 2L74 4F RT4A25 20060221002492006022100249WP 2006 2 21 DHL2005803501 120051110A5321 FLOOR PANEL DOUG DC8 DC873 302199CWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 ITEM REF NR 033351: MAIN CARGO COMPT. FLOOR PANEL CORRODED, STA 1360.000 LBL 56". REMOVED CORROSION IAW SRM 51-1-8 PG. 17-18 FLOOR PANEL THICKNESS 0.071". BLEND OUT 0.035", REMAINING MATERIAL 0.036". FOUND OUT OF ALLOWABLE LIMITS IAW SRM 53-2-0 PG. 2P. TRIMMED OUT DAMAGED AREA AND FABRICATED FILLER (AL 7075T6 0.071") AND DOUBLER (AL 7075T6 0.080") IAW SRM 53-2-3 PG. 39-40. CLEANED, TREATED AND PRIMED AREA, FILLER AND DOUBLER IAW SRM 51-1-8B. INSTALLED NEW DOUBLER AND FILLER IAW SRM 53-2-3 PG. 39-40, SRM 51-1-21. 2L74 4F RT4A25 20060221002512006022100251WP 2006 2 21 DHL2005803503 120051114A5320475052U1 FITTING DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH82180 46123 ITEM REF. NR. 033307: MAIN CARGO COMPT SPLICE FITTING CRACKED 5.500 INCHES, STA 857.000 L-1 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG. 1. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW SPLICE FITTING IAW SRM 51-1-20D, SRM 51-3-0, SRM 51-3-1 (TORQUE) 2L74 4F RT4A25 20060302000082006030200008EU 2006 3 2 SDR2005081 120051203A2120 ODOR AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE CABIN DETECTED A TRBAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO29440AM 440 WHILE TAXIING, BURNING ODOR NOTICED BY THE FLIGHT CREW. VISUALLY INSPECTED ALL OVERHEAD BINS WIRING BUNDLES AND FOUND NO EVIDENCE OF BURNING. OPERATIONAL CHECK OF ALL SYSTEMS PERFORMED AND FOUND SATISFACTORY. (K) 2H72 4T4 TRTA53EU E20NE 20060302000092006030200009EU 2006 3 2 SDR2005083 120051206A5730 SKIN AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE LT WING CORRODED A TRBAK NONE O OTHER ININSP/MAINT 1 SO29451AT 451 DURING INSPECTION FOUND LT WING LOWER EXTERNAL SKIN WITH CORROSION AT THE T/E (UNDERWING BOX ANGLE END). REMOVED CORROSION AND TREATED IAW SRM. DEFERRED IAW SRAS. AREA BLENDED AS INSTRUCTED. 2H72 4T4 TRTA53EU E20NE 20060302002082006030200208EA 2006 3 2 ASOA051121 120051218A3234533443 LEVER CNDAIRCL600 CL6002C10 1390015EA MLG MALFUNCTIONED A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27712EV 10074 DURING CLIMB-OUT FROM SLC-LAX, THE CREW RECEIVED A MASTER CAUTION `PROX SYSTEM` AND A `PROX SYSTEM 2 FAULT` STATUS MESSAGE. THE CREW COMPLIED WITH THE QRH AND DECLARED AN EMERGENCY. THE AIRCRAFT DIVERTED BACK TO SLC, WHERE IT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR LEVER AND THE LANDING GEAR SELECTOR VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060302002112006030200211EA 2006 3 2 QXEA200600269 120051216A5522 SKIN CNDAIRCL600 CL6002C10 1390015EA RT ELEVATOR WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - RIGHT ELEVATOR TOP LEADING EDGE IS WORN THRU PAINT. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01 AND SRM 51-41-02-001-001-A01. 2L72 4F RTA21EA 20060302002142006030200214EA 2006 3 2 QXEA200600287 120051216A2710 UNKNOWN CNDAIRCL600 CL6002C10 1390015EA AILERON UNKNOWN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - C3 RIGHT AILERON FAILS BACKLASH TEST ON NR 3 HYDRAULIC SYSTEM. REPAIRED IAW CRJ700 SRM 27-11-00-710-001-A01. 2L72 4F RTA21EA 20060302002182006030200218EA 2006 3 2 QXEA200600283 120051212A5340 STRINGER CLIP CNDAIRCL600 CL6002C10 1390015EA BS 611 MISSING A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - C3 FUSELAGE INTERIOR LEFT HAND SIDE, FS611, STRINGER 16L, MISSING ONE TIE CLIP. REPAIRED IAW CRJ700 SRM 53-31-03-991-803 AND SRM 51-42-06-001-A01. 2L72 4F RTA21EA 20060302002192006030200219EA 2006 3 2 QXEA200600274 120051216A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA BS 293 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - C3 EXTERNAL FUSELAGE, SKIN GOUGED AT FS293.0 BETWEEN STRINGER 26R AND 27. REPAIRED IAW REO 670-53-21-153 AND CRJ 700 SRM 51-25-16-001-001-A01. 2L72 4F RTA21EA 20060302002212006030200221EA 2006 3 2 QXEA200600265 120051208A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA BS 975 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - FUSELAGE EXTERIOR, LOWER SKIN AT FS 975, LBL0.75 CHAFED. REPAIRED IAW REO 670-53-00-014, REV AND CRJ700 SRM 51-21-16. 2L72 4F RTA21EA 20060302002282006030200228EA 2006 3 2 ASOA051122 120051219A5210 BUSHING CNDAIRCL600 CL6002B19 1900309EA PAX DOOR UNKNOWN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27825AS 7207 DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WAS FOUND TO BE DIFFICULT TO OPEN. MAINTENANCE REINSTALLED THE BUSHING ON THE LEFT SIDE UPPER ROLLER SUPPORT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060302000102006030200010EU 2006 3 2 SDR2005088 120051215A324014007115 TRANSDUCER AEROSPATR72 ATR72 EU PWA PW120 PW127 NE BRAKES INOPERATIVE A TRBAO OTHER O OTHER LDLANDING 1 SO29426AT 426 SHORT AFTER FINAL LANDING, THE LT OUTER MAIN TIRE WENT FLAT. REPLACED NR 1 SPEED SENSOR TRANSDUCER. (K) 2H72 4T4 TRT E20NE 20060302002072006030200207EA 2006 3 2 ASOA051120 120051218A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA BS 605 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 DURING A C-CHECK IN MCN, THE FRAME AT FS 605, BETWEEN STRINGER 27 AND STRINGER 26L, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO BOMBARDIER FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. (M) 2L72 4F RTA21EA 20060302002152006030200215EA 2006 3 2 QXEA200600289 120051221A5230 STRUCTURE CNDAIRCL600 CL6002C10 1390015EA CARGO DOOR UNKNOWN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - C3 NEW BAG DOOR ASSEMBLY DOES NOT FIT REBATE MUST BE TRIMMED TO FIT. REPAIRED IAW CRJ700 SRM 51-74-16-201-001-A01, HORIZON AIR EA R-52-254 AND REO 670-52-44-007 AND HORIZON AIR EA R-53-409. 2L72 4F RTA21EA 20060302002162006030200216EA 2006 3 2 QXEA200600288 120051217A2710 BUSHING CNDAIRCL600 CL6002C10 1390015EA AILERONS UNKNOWN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - C3 RIGHT AILERON OUTBOARD PCU INBOARD LUG BUSHING FOUND NON CONFORM. REPLACED BUSHING IAW HORIZON AIR EA R-27-218. 2L72 4F RTA21EA 20060302002172006030200217EA 2006 3 2 QXEA200600281 120051213A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 850-985 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - C3 INTERNAL FUSELAGE RIGHT HAND FLOOR SEAT RAIL FS850.45-985.0 HAS AREAS OF GOUGES. REPAIRED IAW REO 670-53-00-013, REV A. 2L72 4F RTA21EA 20060302002202006030200220EA 2006 3 2 QXEA200600275 120051215A5220 SKIN CNDAIRCL600 CL6002C10 1390015EA ESCAPE HATCH DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - C3 EMERGENCY ESCAPE HATCH OUTSIDE SKIN RIGHT HAND SIDE HAS DENT. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01 AND SRM 57-25-16-001-001-A01 2L72 4F RTA21EA 20060303000072006030300007EA 2006 3 3 QXEA200600264 120051215A5753 SKIN CNDAIRCL600 CL6002C10 1390015EA TE FLAPS DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - RIGHT HAND INBOARD FLAP BOTTOM SKIN HAS GRAVEL DAMAGE. REPAIRED IAW CRJ 700 SRM 57-01-101-001-A01. 2L72 4F RTA21EA 20060303000412006030300041EA 2006 3 3 QXEA200600266 120051208A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA BS 981 WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - FUSELAGE EXTERIOR LOWER SKIN AT FS 981, BLO AND LBL1.3 HAS TWO WEAR MARKS. REPAIRED IAW REO 670-53-014 AND CRJ-700 SRM 51-42-21. 2L72 4F RTA21EA 20060303000442006030300044EA 2006 3 3 QXEA200600285 120051212A5311 FASTENER CNDAIRCL600 CL6002C10 1390015EA BS 319 MISSING A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - C3 FUSELAGE INTERIOR RIGHT HAND SIDE FS 319.90, STRINGER 13-14 HAS MISSING LOCK FASTENER COLLAR ON FRAME. REPAIRED IAW CRJ700 SRM 51-42-21-001-001-A01. 2L72 4F RTA21EA 20060303000452006030300045EA 2006 3 3 QXEA200600268 120051210A5320 FASTENER CNDAIRCL600 CL6002C10 1390015EA MLG WW MISINSTALLED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - FUSELAGE LOWER FS822 ON LEFT SIDE OF WHEEL WELL WL500 HAS POORLY INSTALLED RIVET ON INNER GUSSET TO HORIZONTAL SUPPORT. REPAIRED IAW CRJ700 SRM 51-42-21-001-001-A01. 2L72 4F RTA21EA 20060303000462006030300046EA 2006 3 3 QXEA200600273 120051216A5310 DOOR FRAME CNDAIRCL600 CL6002C10 1390015EA BS 349 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - C3 FUSELAGE LEFT FS349, WL89.50 HAS SKIN NICKED AT DOOR FRAME. REPAIRED IAW HORIZON AIR EA R-53-403, REO 670-53-21-151 AND CRJ SRM 51-25-16-001-001-A01. 2L72 4F RTA21EA 20060303000472006030300047EA 2006 3 3 QXEA200600276 120051218A5510 PIN CNDAIRCL600 CL6002C10 1390015EA HORIZONTAL STAB WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - C3 RIGHT HORIZONTAL STAB HINGE PIN ANTI ROTATION STOP LUG IS BEING WORN BY PIN. REPAIRED IAW REO 670-55-11-029 AND HORIZON AIR EA R-55-40. 2L72 4F RTA21EA 20060303000482006030300048EA 2006 3 3 QXEA200600277 120051212A5300 UNKNOWN CNDAIRCL600 CL6002C10 1390015EA BS 597-605 UNKNOWN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - C3 FUSELAGE INTERIOR RIGHT SIDE FS 597-605 AT STRINGER 12R SEVEN RIVETS DUMPED. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20060303000512006030300051EA 2006 3 3 QXEA200600272 120051215A5753 FITTING CNDAIRCL600 CL6002C10 1390015EA ROLLER GUIDE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - C2 RIGHT WING OUTBOARD FLAP ROLLER GUIDE FITTING HAS DAMAGE AT FLS168.98. REPAIRED IAW CRJ700 SRM 57-51-02-201-001-A01 AND SRM 51-25-16-001-001-A01. 2L72 4F RTA21EA 20060303000552006030300055EA 2006 3 3 QXEA200600278 120051210A5320 FASTENER CNDAIRCL600 CL6002C10 1390015EA BS 394 MISSING A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - C3 FUSELAGE INTERIOR RIGHT SIDE FS394 BETWEEN CABIN FLOOR AND RIGHT HAND SIDE RAIL, TWO RIVETS MISSING ON FRAME TO INNER CHORD. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20060303000582006030300058EA 2006 3 3 QXEA200600280 120051213A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 850-977 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - C3 INTERIOR FUSELAGE RIGHT FLOOR SEAT RAIL FS850.45-977.0 HAS AREAS OF GOUGES. REPAIRED IAW REO 670-53-00-013 REV A. 2L72 4F RTA21EA 20060302000122006030200012WP 2006 3 2 IXXA05SMN316S 120051229A5754 VANE DOUG DC8 DC872 302199BWP RT WING LE DAMAGED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11722CX71621 46130 DURING C-CHECK, RT WING - L/E SLOT VANE HOLE ELONGATED, XOLDI 6.225. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 05587 DATED 12-29-05, SEMAN DWG ED-4137 DATED 12-28-05, ED SEMAN 2005 1474 DATED 12-29-05. REMOVED FASTENERS IAW DC8 SRM 51-1-21, DC-8 SRM 51-3-0. REMOVED DAMAGED SECTION IAW SEMAN DWG ED-4137. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01-001, FABRICATED REPAIR DOUBLER (AL 7075 T6 0.071) & FILLER, INTERNAL DOUBLER (ALCLAD 7075 T6 0.063) IAW SEMAN DWG ED-4137. CLEANED, TREATED; PRIMED AREA & INNER SIDE OF REPAIR PARTS IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS. 2L74 4F RT4A25 20060302001962006030200196EA 2006 3 2 ASOA051119 120051217A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA BS 589-605 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 DURING A C-CHECK IN MCN, THE FLOOR SUPPORT BEAM CAP AT RBL 9, BETWEEN FS 589 AND 605, AS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO BOMBARDIER FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. (M) 2L72 4F RTA21EA 20060302002122006030200212EA 2006 3 2 QXEA200600279 120051212A5340 STRINGER CLIP CNDAIRCL600 CL6002C10 1390015EA BS 909 MISINSTALLED A QXEAK NONE W INADEQUATE Q C ININSP/MAINT 1 NM09600QX 10005 YYC - C3 FUSELAGE INTERIOR, STRINGER TIE CLIP AT FS909, STRINGER 6R HAS POORLY INSTALLED RIVET. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20060302002132006030200213EA 2006 3 2 QXEA200600286 120051218A5510 LUG CNDAIRCL600 CL6002C10 1390015EA HORIZONTAL STAB WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - C3 LEFT HAND HORIZONTAL STAB PIVOT PIN ANTI ROTATION LUG WORN. REPAIRED IAW REO 670-55-11-029 AND HORIZON AIR EA R-55-40. 2L72 4F RTA21EA 20060303000422006030300042EA 2006 3 3 QXEA200600267 120051215A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA BS 956 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - FUSELAGE EXTERIOR LOWER SKIN AT FS956 BETWEEN STRINGER 23R AND 24R CHAFED BY LAV SERVICED LATCH. REPAIRED IAW HORIZON AIR EA R-53-404 AND CRJ SRM 57-25-16. 2L72 4F RTA21EA 20060303000432006030300043EA 2006 3 3 QXEA200600284 120051212A5340 STRINGER CLIP CNDAIRCL600 CL6002C10 1390015EA BS 469 MISINSTALLED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - C3 FUSELAGE INTERIOR, STRINGER TIE CLIP HAS TWO POORLY INSTALLED RIVETS AT FS469, STRINGER 7R. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20060303000492006030300049EA 2006 3 3 QXEA200600270 120051216A5522 SKIN CNDAIRCL600 CL6002C10 1390015EA LT ELEVATOR LE WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - LEFT ELEVATOR TOP LEADING EDGE IS WORN THROUGH PAINT. REPAIRED IAW CRJ 700 SRM 51-12-00-001-001-A01 AND SRM 51-41-02-001-001-A01. 2L72 4F RTA21EA 20060303000502006030300050EA 2006 3 3 QXEA200600271 120051210A5242 RETAINER CNDAIRCL600 CL6002C10 1390015EA E/E BAY DOOR CRUSHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - C3 AVIONICS DOOR SEAL RETAINER CRUSHED IN TWO PLACES ON BOTH FRON AND BACK EDGES. REPLACED SEAL IAW CRJ700 SRM 51-42-06-001-001-A01. 2L72 4F RTA21EA 20060303000572006030300057EA 2006 3 3 QXEA200600282 120051213A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA BS 784 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 YYC - C3 INTERNAL FUSELAGE LEFT SIDE SEAT RAIL FS 784.0 - 861.0 HAS AREAS OF GOUGES. REPAIRED IAW REO 670-53-00-013, REV A. AND CRJ 700 SRM 51-21-16. 2L72 4F RTA21EA 20060307000012006030700001WP 2006 3 7 IXXA05SMN270S 120051215A5330 SKIN DOUG DC8 DC872 302199BWP ZONE 100 CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11722CX71621 46130 DURING C CHECK, 2 CORRODED AREAS FOUND ON LOWER FUSELAGE NOSE SECTION AT FOLLOWING LOCATION BS 217 BETWEEN L32 & 31R, BS 223 BETWEEN L32R & 32L, DUE CHANGE. PERFORMED REPAIR IAW DC-8 SRM 53-2-1. REMOVED CORROSION IAW DC8 SRM 51-1-8, FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0. REMOVED CORRODED PLATING SEGMENT. CUT OUT DAMAGED SECTION. FAB`D EXTERNAL SPLICES, INTERNAL FINGER DOUBLER, INTERNAL DOUBLER, TR NR 53-173 DATED 09-20-03. CLEANED, TREATED & PRIMED AREA, REPAIR PART. APPLIED SEALANT TO FAYING SURFACES. INSTALLED NEW PLATING SEGMENT & REPAIR PART. ALL WORK PERFORMED IAW APPLICABLE SRMS. 2L74 4F RT4A25 20060307000022006030700002WP 2006 3 7 IXXA05SMN275S 120051215A5751 SKIN DOUG DC8 DC872 302199BWP LT AILERONS CORRODED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11722CX71621 46130 DURING C CHECK , LT OUTBD AIL LWR SKIN CORRODED, STA XA 722.000. PERFORMED REPAIR IAW FAA FORM 8110-3 NR 05580 DATE 12-21-05, SEMAN DWG NR ED 4119 DATE 12-20-05 & EO SEMAN NR 20051449 DATE 12-21-05. REMOVED FASTENERS. REMOVED CORROSION. FOUND OUT OF LIMITS IAW DC-8 SRM 57-2-0. REMOVED CORRODED AREA. PERFORMED NDT INSPECTION. FAB`D SOLID SEGMENT REPAIR PLATING, INTERNAL SPLICE, REPAIR DOUBLER9. CLEANED, TREATED AND PRIMED AREA, REPAIR PARTS INTERNAL PART. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS. ALL WORK PERFORMED IAW APPLICABLE REFERENCE MATERIALS. 2L74 4F RT4A25 20060307000052006030700005WP 2006 3 7 IXXA05SMN283S 120051216A5410 FITTING DOUG DC8 DC872 302199BWP ZONE 800 CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11722CX71621 46130 DURING ROUTINE C CHECK INSPECTION, NR 2 ENGINE COWL DOOR RAIL FITTING CRACKED 1, AT STA 254.324 (RT SIDE). REMOVED FASTENERS IAW DC8 SRM 51-3-0, DC8 SRM 51-1-21, DC8 SRM 51-1-21A. PERFORMED STOP HOLE, FABRICATED DOUBLER (17-4PH STAINLESS FLAT BAR) IAW ENG SHOP MANUAL CFM 56-2 78-31-41. CLEANED REPAIR AREA AND APPLIED ALODINE 1500 IAW CFM 56 SPM 70-62-13. INSTALLED DOUBLER IAW ENG SHOP MANUAL CFM 56-2 78-31-41, DC8 SRM 51-3-0, DC8 SRM 51-1-21, DC8 SRM 51-3-1 PG 2A (TORQUE). PAINTED IAW CFM 56 SPM 70-64-16 2L74 4F RT4A25 20060307000062006030700006WP 2006 3 7 IXXA05SMN317S 120051229A5754 VANE DOUG DC8 DC872 302199BWP RT WING LE FLAP DAMAGED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11722CX71621 46130 DURING ROUTINE C CHECK INSPECTION, RT WING L/E SLOT VANE HOLE ELONGATED, XILD 42. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 06007 DATED 01-06-06, SEMAN DWG ED-4138 DATED 01-06-06, EO SEMAN NR 20051475 DATED 01-06-06. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-3-0, DC8 SRM 51-1-21. REMOVED DAMAGED SECTION IAW SEMAN DWG ED-4138. PERFORMED NDT INSP IAW NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER (AL 7075T6 0.071), FILLER, INTERNAL DOUBLER (AL7075T6 0.063”) IAW SEMAN DWG ED-4138. CLEANED, TREATED AND PRIMED AREA , REPAIR PARTS IAW DC8 SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SEMAN DWG ED-4138, DC8 SRM 51-1-21, DC8 SRM 51-3-0, DC8 SRM 51-1-20D, DC8 SRM 51-3-1 (TORQUE). 2L74 4F RT4A25 20060307000072006030700007WP 2006 3 7 IXXA05SMN318S 120051229A5754 SKIN DOUG DC8 DC872 302199BWP RT WING LE CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11722CX71621 46130 DURING ROUTINE C CHECK, RT WING OTBD INNER L/E CRACKED .500 XFS 710.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 06007 DATED 01-06-06, SEMAN DWG ED-4139 DATED 01-04-06, EO SEMAN NR 20051476 DATED 01-06-06. REMOVED FASTENERS IAW DC8 SRM 51-1-21, DC8 SRM 51-3-0. REMOVED DAMAGED SECTION IAW SEMAN DWG ED-4139. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01-001. FAB`D REPAIR DOUBLER (AL7075T6 0.063), FILLER (AL7075T6 0.050) IAW SEMAN DWG ED-4139. CLEANED, TREATED AND PRIMED AREA, REPAIR PARTS INNER SIDE IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11. INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-21, SEMAN DWG ED-4139, DC8 SRM 51-3-0, DC8 SRM 51-1-20D, DC8 SRM 51-3-1. 2L74 4F RT4A25 20060307000032006030700003WP 2006 3 7 IXXA05SMN276S 120051216A5751 REPAIR DOUG DC8 DC872 302199BWP LT AILERON MISINSTALLED B IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW11722CX71621 46130 DURING C CHECK, LT INBD AIL LWR SKIN HAS NO STANDARD REPAIR (STA XA 543.000-551.000). PERFORMED MAJOR REPAIR IAW DC8 SRM 57-8-1 FIG 1. REMOVED PANEL PLATING WITH NON STANDARD REPAIR ON IT IAW DC8 SRM 57-1-0, DC8 SRM 51-1-21. FAB`D NEW PLATING (AL2024T30 0.025”), BONDED FINGER DOUBLER (AL2024T3 0.020) IAW DC8 SRM 57-8-1 FIG 1 ITEM “B”, “K”, DOUGLAS DWG # 5705334. BONDED BOTH REPAIR PARTS WITH HYSOL IAW DC8 SRM 51-1-9. CLEANED, TREATED AND PRIMED INNER SIDE OF NEW PANEL PLATING IAW DC8 SRM 51-1-8B. APPLYING SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11. INSTALLED NEW PANEL PLATING IAW DC8 SRM 51-1-21. 2L74 4F RT4A25 20060307000082006030700008WP 2006 3 7 IXXA05SMN322S 120051229A5340 FITTING DOUG DC8 DC872 302199BWP 1530 L24R CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11722CX71621 46130 DURING ROUTINE C CHECK INSPECTION, MAIN CARGO CMPT FITTING CRACKED 3, AT STA 1530.000, L-24R. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW FITTING WITH FASTENERS (HI-LOKS) IAW DC8 SRM 51-1-20D, DC8 SRM 51-3-1. 2L74 4F RT4A25 20060309000642006030900064NM 2006 3 9 UPS06M46384 120051130A5311 FRAME DOUG MD11 MD11F 3023600NM BS 1960 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01282UP 48452 INSPECTION TYPE:C AFT CARGO COMPT AT STA 1960 LONGERON 45 LT FRAME WITH SURFACE CORROSION. CORROSION AT AFT CARGO COMPT REMOVED PER SRM 51-21-01.V.2.R.38. FOUND EXCEEDED LIMIT. FPI C/OUT FOUND NO CRACK EVIDENT. REPAIR DOUBLER FAB PER EN1 036-06, USING MAT 7075-0-0.071"(CLAD ALU SHT) REPAIR DOUBLER PICK UP HOLES & REPAIR BUSHING FAB PER EN1036-06.REPAIR BUSHING & DOUBLER INSTALLED PER EN1036-06, FOUND REPAIR ACCOMPLISHED WITH SATIS. 2L73 4F RTA22WE 20060310000462006031000046NM 2006 3 10 UPS06M46274 120051207A5510 STRUCTURE DOUG MD11 MD11F 3023600NM EMPENNAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01282UP 48452 INSPECTION TYPE:C EMPENNAGE - BARREL NUT HOLE 21 LEFT FOUND BEARING WITH SURFACE CORRODED ON SIDE & BOTTOM AREA. CORROSION REMOVAL C/OUT & FOUND BLENDED OUT BEYOND ALLOWABLE LIMIT. BARREL NUT 21 LEFT & BOTTOM REWORKED PER EN 1637-05. FAB SLEEVE BUSHING PER EO MD11-5510-19409-K,F.5. APPLIED SEALANT PR1422B1/2 BLEND OUT AREA & FAB S/BUSHING PER EO MD11-5510-19409-K. REPAIR ACCOMPLISHED AT BARREL NUT HOLE 21 LEFT PER EO MD11-5510-19409-K & EN1637-05, FOUND SATIS. 2L73 4F RTA22WE 20060310000472006031000047NM 2006 3 10 UPS06M46275 120051221A5510 STRUCTURE DOUG MD11 MD11F 3023600NM EMPENNAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01282UP 48452 INSPECTION TYPE:C EMPENNAGE - BARREL NUT HOLE 26 LEFT FOUND BEARING WITH SURFACE CORROSION ON SIDE & BOTTOM AREA. CORROSION REMOVAL C/OUT & FOUND BLENDED OUT BEYOND ALLOWABLE LIMIT. BARREL NUT BORE & BOTTOM REWORKED PER EN1031-06. FAB SLEEVE BUSHING PER EO MD 11-5510-19409-KF.F.5. APPLIED SEALANT PR1422B1/2 BLEND OUT AREA & S/BUSHING PER EO MD11-5510-19409-K. REPAIR ACCOMPLISHED AT BARREL NUT HOLE 26 LT PER EO MD11-5510-19409-K & EN1031-06, FOUND SATIS. 2L73 4F RTA22WE 20060310000632006031000063NM 2006 3 10 UPS06M46276 120051207A5510 STRUCTURE DOUG MD11 MD11F 3023600NM EMPENNAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01282UP 48452 INSPECTION TYPE:C EMPENNAGE - BARREL NUT HOLE 12 LEFT FOUND BEARING WITH SURFACE CORROSION ON SIDE & BOTTOM AREA. CORROSION REMOVAL C/OUT FOUND BLENDED OUT BEYOND ALLOWABLE LIMIT. BARREL NUT 12 LEFT BORE & BOTTOM REWORKED PER EN1623-05. FAB SLEEVE BUSHING PER EO MD11-5510-19409-K.F-5. APPLIED SEALANT PR1422B1/2 BLEND OUT AREA & S/BUSHING PER EO MD11-5510-19409-K. REPAIR ACCOMPLISHED AT BARREL NUT HOLE 12 LEFT PER EO MD11-5510-19409-K & EN1623-05, FOUND SATIS. 2L73 4F RTA22WE 20060310000652006031000065NM 2006 3 10 UPS06M46277 120051207A5510 STRUCTURE DOUG MD11 MD11F 3023600NM EMPENNAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01282UP 48452 INSPECTION TYPE:C EMPENNAGE - BARREL NUT HOLE 09 LEFT FOUND BEARING WITH SURFACE CORROSION ON SIDE & BOTTOM AREA. CORROSION REMOVAL C/OUT & FOUND BLENDED OUT BEYOND ALLOWABLE LIMIT. BARREL NUT HOLE 09 LEFT BORE & BOTTOM REWORKED PER EN 1622-05. FAB SLEEVE BUSHING PER EO MD11-5510-19409-K,F-5. APPLIED SEALANT PR1422B1/2 BLEND OUT AREA & S/BUSHING PER EO MD11-5510-19409-K. REPAIR ACCOMPLISHED AT BARREL NUT HOLE 09 LEFT PER EO MD11-5510-19409-K & EN1622-05, FOUND SATIS. 2L73 4F RTA22WE 20060307000042006030700004WP 2006 3 7 IXXA05SMN306S 120051229A5340 FITTING DOUG DC8 DC872 302199BWP BS 980 L17-18R CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11722CX71621 46130 DURING C CHECK, MAIN CARGO COMPT FRAME FITTING 3 CRACK, STA 980.000 L-17R TO L-18R. PERFORMED REPAIR IAW DC8 SRM 53-2-0 FIG 7. REMOVED FASTENERS IAW DC8 SRM 51-1-20D. REMOVED FRAME FITTING SEGMENT (CRACKED) IAW DC8 SRM 53-2-0 FIG 7.. FAB`D SPLICE ANGLE, FILLER 5T6 0.160) IAW DC8 SRM 53-2-0 FIG 7 (SHEET 1-2). PERFORMED HEAT TREATMENT TO SPLICE ANGLE IAW DC8 SRM 51-1-1 PAGES 1, 13, 17. PERFORMED NON DESTRUCTIVE INSPECTION REPORT IAW DC8 NDT SPM PART 08-00-02 TO 07. CLEANED, TREATED AND PRIMED AREA, REPAIR PARTS IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11. INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-0 FIG 7, DC8 SRM 51-1-20D, DC8 SRM 51-3-1. 2L74 4F RT4A25 20060309000782006030900078NM 2006 3 9 UPS06M46389 120051123A5755 SKIN DOUG MD11 MD11F 3023600NM SPOILER CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01282UP 48452 INSPECTION TYPE:C RT WING TOP SIDE FIXED T/E PANEL XORS 683.4 FWD OF NR 4 SPOILER FOUND CORROSION UNDERNEATH PNL. CORROSION REMOVAL C/OUT FOUND MAT REMOVED EXCEEDED LIMIT. HFEC C/OUT FOUND NO EVIDENT OF CRACK. FLAP PEENING C/OUT ON REWORK AREA PER EN1039-0 6. REPAIR FILLER FAB USING MAT 7075T6-0.090" PER EN1039-06. UPPER SKIN APP STA XORS 670 TO 697 HI-LOK INSTALLED PER SRM51-33-01,V2.R.38. FIXED T/E UPPER PNL INSTALLED PER SRM 51-33-.01.V2.R.38, FOUND SATIS. 2L73 4F RTA22WE 20060313000972006031300097 2006 3 13 C2XA05BT084 420051128A34207014300901 DISPLAY EMB 145 EMB145LR 3260212SO COCKPIT FAULTY A C2XAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW27185578288 8288 145596 CREW REPORTED, -DU4 OVERHEAT- MESSAGE DISPLAYED FOR ONE SECOND THEN CLEARED. ABOUT 30 MINUTES LATER DU4 WENT BLANK FOLLOWED QUICKLY BY INTENSE, ACRID ELECTRICAL FUMES. DECLARED EMERGENCY AND DIVERTED TO MEM, AIRCRAFT LANDED UNEVENTFULLY. MAINTENANCE REMOVED AND REPLACED THE NR 4 DU-870 IAW EMB145MM 34-22-01. OPS CHECKED GOOD. NO FUMES NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20060313000982006031300098SO 2006 3 13 C2XA05BT088 120051211A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSBURNED OUT A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713997 145298 DURING 1A INSPECTION MAINTENANCE FOUND EMERGENCY CEILING LIGHT NOT WORKING EXIT ROW 12. REMOVED AND REPLACED EMERGENCY CEILING LIGHT BULB IAW EMB145 AMM 33-50-08. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20060313000992006031300099SO 2006 3 13 C2XA05SD032 120051212A335066368 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715983 145239 SDF - AFT EMERGENCY LIGHT STRIP INOP. REMOVED AND REPLACED AFT EMERGENCY LIGHT STRIP IAW EMB 145 AMM 33-50-12, OPS CHECK GOOD. 2L72 4T RTT00011AT 20060313001002006031300100SO 2006 3 13 C2XA05CL098 120051213A3320BR900022 BALLAST EMB 145 EMB145LR 3260212SO GALLEY LIGHT BURNED A C2XAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW2713975 145163 DURING ROUTINE MAINTENANCE THE GALLEY HAD A BURNING ODOR. MAINTENANCE INSPECTED AND FOUND THE GALLEY LIGHT BALLAST BURNED. THE BALLAST WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20060313001372006031300137SO 2006 3 13 C2XA05IA135 120051123A3397 CONNECTOR EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT DISCONNECTED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2711127 145697 IAH - DURING PREFLIGHT INSPECTION THE FORWARD EMERGENCY LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE RESECURED THE ELECTRICAL CONNECTORS, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20060310000712006031000071NM 2006 3 10 UPS06M46283 120051207A5510 STRUCTURE DOUG MD11 MD11F 3023600NM EMPENNAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01282UP 48452 INSPECTION TYPE:C EMPENNAGE - BARREL NUT HOLE 18 LEFT FOUND BEARING WITH SURFACE CORROSION ON SIDE & BOTTOM AREA. CORROSION REMOVAL C/OUT & FOUND BLENDED OUT BEYOND ALLOWABLE LIMIT. BARREL NUT HOLE 18 LEFT BORE & BOTTOM REWORKED PER EN1636-05. FAB SLEEVE BUSHING PER EO MD11-5510-19409-K, FIG-5. APPLIED SEALANT PR1422B1/2 BLEND OUT AREA & S/BUSHING PER EO MD11-5510-19409-K. REPAIR ACCOMPLISHED AT BARREL NUT HOLE 18 LEFT PER EO MD11-5510-19409-K & EN1636-05, FOUND SATIS. 2L73 4F RTA22WE 20060310000722006031000072NM 2006 3 10 UPS06M46284 120051221A5510 STRUCTURE DOUG MD11 MD11F 3023600NM EMPENNAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01282UP 48452 INSPECTION TYPE:C EMPENNAGE - BARREL NUT HOLE NR 17 LEFT FOUND BEARING WITH SURFACE CORROSION ON SIDE & BOTTOM AREA. CORROSION REMOVAL C/OUT & FOUND BLENDED OUT BEYOND ALLOWABLE LIMIT. BARREL NUT HOLE 17 LEFT BORE & BOTTOM REWORKED PER EN1023-06. FAB SLEEVE BUSHING PER EO MD11-5510-19409-K, FIG-5. APPLIED SEALANT PR1422B1/2 BLEND OUT AREA & S/BUSHING PER EO MD11-5510-19409-K. REPAIR ACCOMPLISHED AT BARREL NUT HOLE PER EO MD11-5510-19409-K & EN1023-06, FOUND SATIS. 2L73 4F RTA22WE 20060310000732006031000073NM 2006 3 10 UPS06M46285 120051221A5510 STRUCTURE DOUG MD11 MD11F 3023600NM EMPENNAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01282UP 48452 INSPECTION TYPE:C EMPENNAGE - BARREL NUT HOLE 23 LEFT FOUND BEARING WITH SURFACE CORROSION ON SIDE & BOTTOM AREA. CORROSION REMOVAL C/OUT & FOUND BLENDED OUT BEYOND ALLOWABLE LIMIT. BARREL NUT HOLE 23 LEFT BORE & BOTTOM REWORKED PER EN1025-06. FAB SLEEVE BUSHING PER EO MD11-5510-19409-K, FIG-5. APPLIED SEALANT PR1422B1/2 BLEND OUT AREA & S/BUSHING PER EO MD11-5510-19409-K. REPAIR ACCOMPLISHED AT BARREL NUT HOLE 23 LEFT PER EO MD11-5510-19409-K & EN1025-06, FOUND SATIS. 2L73 4F RTA22WE 20060310000752006031000075NM 2006 3 10 UPS06M46293 120051217A5753S2931361X7075T65ANGLE DOUG MD11 MD11F 3023600NM TE FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01282UP 48452 INSPECTION TYPE:C AFTER I/B FLAP O/B SEGMENT REMOVAL, FOUND FWD O/B SEGMENT MOST O/B AFT END 01/EA ANGLE CRACKED. THE ABOVE MENTIONED CRACKED AREA ANGLE REMOVED PER SRM 51-35-01.V.2R.38. NEW T-FAB & MAT USED S2931361X7075T6511 PER EN1063-06. HFEC C/OUT FOUND NO EVIDENT OF CRACK AT FAB T-ANGLE REWORKED AREA, REPAIR ACCOMPLISHED PER EN1063-06. NEW TEE HOLES TRANSFERRED & NEW TEE INSTALLED PER SRM 51-21-01V.2.R38. 2L73 4F RTA22WE 20060313001062006031300106SO 2006 3 13 C2XA05IA130 120051111A335020131A BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW27149079697 3315 145468 IAH - DURING MAINTENANCE INSPECTION THE NUMBER FOUR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT BATTERY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20060313001072006031300107SO 2006 3 13 C2XA05IA131 120051118A335020131A BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW27169992740 2740 145307 IAH - DURING MAINTENANCE INSPECTION, THE FORWARD SECTION OF AISLE PATH LIGHTING WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE EMERGENCY LIGHT BATTERY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20060313001142006031300114SO 2006 3 13 C2XA05BT076 120051029A335066367 LIGHT EMB 145 EMB145LR 3260212SO CABIN FAULTY A C2XAK NONE O OTHER ININSP/MAINT 1 SW2718982 145223 DURING SERVICE AND ROUTINE CHECK, MAINTENANCE CLEARED MEL CONTROL 061756, CENTER PORTION OF NR 6 FLOOR EMERGENCY PROXIMITY LIGHT STRIP WILL NOT ILLUMINATE. AIRCRAFT RELEASED IAW MEL 33-50-00/2 CATEGORY -C- CONTROL 061756. REMOVED AND REPLACED NR 6 FLOOR PROXIMITY EMERGENCY LIGHT STRIP BETWEEN SEATS 12A AND 15A IAW EMB145 AMM 33-50-12, OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20060313001272006031300127SO 2006 3 13 C2XA05TY059 120051122A335020131A BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2729906 145472 TYS - AIRCRAFT WAS FOUND WITH NR 4 EMERGENCY LIGHT TO HAVE NO OUTPUT. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY IAW EMB 145 AMM 33-50-04 AND THE OPS CHECK WAS GOOD. 2L72 4T RTT00011AT 20060313001282006031300128SO 2006 3 13 C2XA05IA137 120051124A3350110049 CHARGER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713978 145180 MCI - DURING MAINTENANCE INSPECTION, THE RT WING FAIRING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO EMERGENCY LIGHT BATTERY CHARGER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20060313001302006031300130SO 2006 3 13 C2XA05IA132 120051113A335078241 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716981 145208 STL - DURING MAINTENENCE INSPECTION, THE NUMBER FOUR AND FIVE AISLE PATH LIGHT STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FIVE EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20060313001312006031300131SO 2006 3 13 C2XA05IA133 120051113A335078241 INVERTER EMB 145 EMB145 3260210SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714960 145100 STL - DURING MAINTENANCE INSPECTION, THE EMERGENCY LIGHTS AT THE COCKPIT ENTRANCE WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20060313001322006031300132SO 2006 3 13 C2XA05CL094 120051118A3350W102850022 WIRE EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BROKEN A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713978 145180 DURING ROUTINE MAINTENANCE THE EXTERIOR RIGHT OVERWING EMERGENCY LIGHT WOULD NOT ILLUMINATE. MAINTENANCE INSPECTED AND REPAIRED WIRE W102-8500-22. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20060313001332006031300133SO 2006 3 13 C2XA05BT085 120051130A3350110049 CHARGER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT FAULTY A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712563 145612 DURING RON ROUTINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS IN THE COCKPIT CEILING WERE NOT WORKING. MAINTENANCE REMOVED AND REPLACED NR 1 EMERGENCY LIGHT BATTERY CHARGER ASSEMBLY IAW EMB145 AMM 33-50-04, OPS CHECKED GOOD. 2L72 4T RTT00011AT 20060313001342006031300134SO 2006 3 13 C2XA05BT082 120051119A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BLOWN A C2XAK NONE O OTHER ININSP/MAINT 1 SW2719554 145587 DURING SERVICE AND ROUTINE INSPECTION CHECK, MAINTENANCE FOUND THAT THE LEFT OVERWING EMERGENCY LIGHT WAS NOT WORKING. REMOVED AND REPLACED BULB IN LEFT OVERWING EMERGENCY LIGHT ASSEMBLY IAW EMB145 MM 33-50-10, OPS CHECKED GOOD. 2L72 4T RTT00011AT 20060313001352006031300135SO 2006 3 13 C2XA05BT083 120051120A335066367 LIGHT EMB 145 EMB145LR 3260212SO CABIN FAULTY A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714568 145628 DURING ROUTINE CHECK MAINTENANCE FOUND THE NR 2 AND NR 3 EMERGENCY FLOOR STRIP LIGHTS NOT WORKING. REMOVED AND REPLACED NR 3 EMERGENCY FLOOR STRIP LIGHT IAW EMB145 AMM 33-50-12, OPS CHECKED GOOD. 2L72 4T RTT00011AT 20060313001362006031300136SO 2006 3 13 C2XA05IA134 120051121A335082321 SIGN EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2717115 145666 IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THE EXIT ROW EMERGENCY EXIT SIGN TO BE INOPERATIVE. MAINTENANCE RESECURED THE CONNECTOR ON THE AFFECTED LIGHT, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE DISCREPANCY REPEATED ON FLIGHT 2723 IN IAH WHERE MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY EXIT SIGN, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20060313001472006031300147SO 2006 3 13 C2XA05SD030 120051204A335020131A BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2711536 145520 SDF - EMERGENCY LIGHT OVER GALLEY DOOR INOP. REMOVED AND REPLACED NR 1 EMERGENCY LIGHT BATTERY AND BATTERY POWER SUPPLY IAW EMB 145 AMM 33-50-04. OPS CHECK GOOD. 2L72 4T RTT00011AT 20060313001572006031300157SO 2006 3 13 C2XA05IA129 120051111A335020131A BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714907122603315 145468 IAH - FLIGHT 3470, DURING MAINTENANCE INSPECTION THE NR 2 EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO EMERGENCY LIGHT BATTERY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20060313001602006031300160SO 2006 3 13 C2XA05SD031 120051205A2560SG9632 GLOWSTRIP EMB 145 EMB145XR 3260214SO CABIN MISSING A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712157 145787 SDF - PHOTOLUMINESCENT STRIP NEXT TO AFT GALLEY MISSING. INSTALLED MISSING PHOTOLUMINESCENT STRIP NEXT TO AFT GALLEY IAW EMB MM 33-50-12. 2L72 4F RT 20060313001702006031300170SO 2006 3 13 C2XA05CL092 120051107A3350P2070005120 CHARGER EMB 135 EMB135ER 3260203SO EMERGENCY LIGHT BURNED A C2XAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW2719503 145176 CLE - THE CREW REPORTED A ELECTRICAL BURNING SMELL IMMEDIATELY AFTER TAKEOFF. THE AIRCRAFT RETURNED TO CLE WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FORWARD FLIGHT ATTENDANT FLASHLIGHT AND CHARGER ASSEMBLY. ALSO REPLACED THE CEILING LIGHT ABOVE SEAT 1A (P/N 5113WW). 2L72 4F RTT00011AT 20060313001712006031300171SO 2006 3 13 C2XA05RI018 120051107A3397 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DAMAGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715572 145636 RIC - DURING ACFT ROUTINE INSPECTION, MX FOUND EMERGENCY EXIT SIGN (FWD) FAILS TO ILLUMINATE. MX PERFORMED TROUBLESHOOTING AND FOUND BAD CONNECTION ON PLUG P8526. CONNECTION WAS REPAIRED AND SYSTEM WAS OPS CHECKED GOOD. ACFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20060313001722006031300172SO 2006 3 13 C2XA05IA128 120051106A335078241 INVERTER EMB 145 EMB145 3260210SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2727962 145110 STL - FLIGHT 2764, DURING POST FLIGHT INSPECTION THE CREW REPORTED THAT THE NR 6, 7 & 8 AISLE PATH LIGHTING STRIP WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER 6 INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20060313001732006031300173SO 2006 3 13 C2XA05CL093 120051110A33503025103 LIGHT EMB 135 EMB135LR 3260305SO RT OVERWING INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2728529 145512 DURING ROUTINE MAINTENANCE THE RIGHT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE OVERWING LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20060313001782006031300178SO 2006 3 13 C2XA05TY061 120051212A533014520571003 SKIN EMB 145 EMB145XR 3260214SO FUSELAGE DENTED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711106 145650 TYS - A DENT JUST FWD OF SKIN SPLICE BETWEEN FR 23 AND 24 AND STR 18R AND 19R WAS FOUND. MAINTENANCE PERFORMED A REPAIR TO THE DAMAGE SKIN IAW IC2005-145/7374, ALODINED, PRIMED AND PAINTED IAW CPM 51-21-07. LEAK CHECK WAS GOOD. AIRCRAFT WAS RELEASED TO SERVICE. 2L72 4F RT 20060314000902006031400090EU 2006 3 14 06FDEA0926 120051102A2611 SMOKE DETECTOR AIRBUS310 A310203 3930313EU CARGO BAY FALSE ACTIVATIONA FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25407FE 254 CLIMBING THROUGH 12,500 FT RED SMOKE LIGHT ILLUMINATED ON ANNUNCIATOR PANEL (BELOW ENG GAUGES) SIMULTANEOUS ECAM SHOWED AMBER -SMOKE- DIRECTING - DISCH AGENT 2 - NO OTHER INDICATION OF SOURCE OF SMOKE. DISCHARGED AGENT 2 PER ECAM. REMOVED AND INSTALLED THE FWD CARGO SMOKE DETECTORS PER A310-200 26-16-11-4, INSTALLED NR 1 FIRE BOTTLE IAW A310-200 MM 26-23-11-4-01. PERFORMED ADJ/TEST IAW A310-200 MM 26-23-00-5-01. ALL TESTS CHECK GOOD. OK FOR SERVICE. 2L72 4F RTA35EU 20060316001772006031600177WP 2006 3 16 ASAA0580553 120051212A53305924802133 SKIN DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE SKIN DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 C-CHECK, FUSELAGE SKIN DENTED. COLD-WORKED TO ORIGINAL CONTOUR. INSTALLED REPAIR DOUBLER. (K) 2L72 4F4 FRTA6WE E9NE 20060316001842006031600184WP 2006 3 16 ASAA0580548 120051212A532199365443 FLOOR PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 C-CHECK, CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (K) 2L72 4F4 FRTA6WE E9NE 20060316001892006031600189WP 2006 3 16 ASAA0580536 120051220A531359360531 LONGERON DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02934AS 49235 C-CHECK, LONGERON CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPLACEMENT SECTION WITH 2 REPAIR SPLICES. (K) 2L72 4F4 F A6WE E9NE 20060316001922006031600192WP 2006 3 16 ASAA0580537 120051212A256039361901 FITTING DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE GIRT BAR CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 C-CHECK, R-1 DOOR FLOOR MOUNTED GIRT BAR FITTING CORRODED. REPLACED CORRODED FITTING. (K) 2L72 4F4 FRTA6WE E9NE 20060316001932006031600193WP 2006 3 16 ASAA0580534 120051108A5330 SKIN DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 LINE CHECK, FUSELAGE DENTED AFT OF L-1 (FWD PAX) DOOR. REMOVED DAMAGED SECTION SECTION. INSTALLED EXTERNAL DOUBLER WITH BLIND RIVETS IAW EA. (K) 2L72 4F4 FRTA6WE E9NE 20060316001952006031600195WP 2006 3 16 ASAA0580540 120051212A532099365345 WEB DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE FLOOR CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 C-CHECK, CABIN FLOOR WEB CORRODED. REPLACED WEB. (K) 2L72 4F4 FRTA6WE E9NE 20060316001962006031600196WP 2006 3 16 ASAA0580550 120051212A534799336534139 TRACK DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE FLOOR CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 C-CHECK, CABIN FLOOR TRACK CORRODED. REPLACED FLOOR TRACK. (K) 2L72 4F4 FRTA6WE E9NE 20060316001972006031600197WP 2006 3 16 ASAA0580543 120051212A532199365473 FLOOR PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 C-CHECK, CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (K) 2L72 4F4 FRTA6WE E9NE 20060317000192006031700019EA 2006 3 17 ASOA051066S 120051205A52606003152915 HINGE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27882AS 7503 7503 DURING A C-CHECK, THE PASSENGER DOOR TOP STEP UPPER HINGE HALF WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR TOP STEP UPPER HINGE. (K) 2L72 4F4 FRTA21EA E15NE 20060317000382006031700038EU 2006 3 17 SDR2005092 120051227A2612 FIRE LOOP AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE RT ENGINE FALSE ACTIVATIONA TRBAE ENGINE SHUTDOWN N FALSE WARNING TXTAXI/GRND HDL 1 SO29448AM 448 AFTER LANDING, RT ENGINE FIRE WARNING LIGHT FLASHED ON FOR ONE SECOND. CREW SHUTDOWN ENGINE AS PRECAUTIONARY ACTION. DEFERRED RT ENGINE FIRE LOOP (B) SYSTEM IAW MEL. (K) 2H72 4T4 TRTA53EU E20NE 20060317000432006031700043EU 2006 3 17 SDR2005082 120051203A3350 SOCKET AEROSPATR72 ATR72212A 8680902EU PWA PW120 PW127 NE INTERMITTENT A TRBAK NONE O OTHER ININSP/MAINT 1 SO29536AT 536 ON POST FLIGHT INSPECTION FOUND PASSENGER ENTRY EMERGENCY LIGHT INOPERATIVE. REPOSITIONED ENTRY DOOR EMERGENCY LIGHT BULBS. OPERATIONAL CHECK FOUND SATISFACTORY. (K) 2H72 4T4 TRTA53EU E20NE 20060317000452006031700045EU 2006 3 17 SDR2005085 120051208A2800 UNKNOWN AEROSPATR72 ATR72212A 8680902EU PWA PW120 PW127 NE COCKPIT UNKNOWN A TRBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO29536AT 536 AFTER TAKEOFF, MASTER WARNING CAUTION AND FUEL ON CAP PANEL INTERMITTENTLY ON. AIRCRAFT RETURNED TO AIRPORT. INSPECTED FUEL TANK AND FOUND NO EVIDENCE OF DEBRIES. CLEANED FUEL FEEDER TANK. (K) 2H72 4T4 TRTA53EU E20NE 20060317000462006031700046EU 2006 3 17 SDR2005091 120051223A33503012000 POWER SUPPLY AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE CABIN MALFUNCTIONED A TRBAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO29308AE 309 WHILE TAXIING, FA REPORTED EMERGENCY LIGHTS CAME ON AND WOULD NOT EXTINGUISH OR RESET TO OFF. REPLACED EMERGENCY LIGHTS POWER PACK. (K) 2H72 4T4 TRTA53EU E20NE 20060320000042006032000004NE 2006 3 20 AWH2006F00009 220051209A7314 COUPLING CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE MCAULY3AF34C3GFR34C703 GL ENG DRV FUEL PMPCORRODED E AWHAK NONE O OTHER ININSP/MAINT 1 WP17969FE 2951 846 208B0092 17230 961689 PRECAUTIONARY INSPECTION OF THE FUEL PUMP DRIVE SPLINE IAW MM, FUEL PUMP COUPLING IN-SITU INSPECTION. MAINTENANCE FOUND THE FUEL PUMP DRIVE SPLINE SEVERELY CORRODED NEARLY TO THE POINT OF FAILURE. THE FUEL PUMP ASSEMBLY WAS REPLACED WITH A FRESH OVERHAULED UNIT AND THE AIRCRAFT RETURNED TO SERVICE. (K) 1H71 3T3 T A37CE E4EA 5 CP60GL 20060316001742006031600174WP 2006 3 16 ASAA0580538 120051212A5311991224671 FRAME DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 C-CHECK, FUSELAGE FRAME WEB PUNCTURED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER AND FILLER. (K) 2L72 4F4 FRTA6WE E9NE 20060316001752006031600175WP 2006 3 16 ASAA0580539 120051212A5320995576317 INTERCOSTAL DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 C-CHECK, INTERCOSTAL CRACKED AT RADIUS. REPLACED INTERCOSTAL. (K) 2L72 4F4 FRTA6WE E9NE 20060316001762006031600176WP 2006 3 16 ASAA0580552 120051212A532099365335 WEB DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE CABIN FLOOR CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 C-CHECK, CABIN FLOOR WEB CRACKED. REMOVED DAMAGED WEB SECTION. INSTALLED REPAIR DOUBLER. (K) 2L72 4F4 FRTA6WE E9NE 20060316001832006031600183WP 2006 3 16 ASAA0580554 120051212A5330591140659 SKIN DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 C-CHECK, FUSELAGE SKIN DENTED. COLD WORKED TO ORIGINAL CONTOUR. INSTALLED REPAIR DOUBLER. (K) 2L72 4F4 FRTA6WE E9NE 20060316001942006031600194WP 2006 3 16 ASAA0580535 120051108A5330 SKIN DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 SEA LINE CHK, FUSELAGE DAMAGED BY LIGHTNING STRIKE ON LT SIDE. REPAIRED IAW SRM AND EA.(K) 2L72 4F4 FRTA6WE E9NE 20060317000442006031700044EU 2006 3 17 SDR2005086 120051208A3350 BATTERY PACK AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE INOPERATIVE A TRBAK NONE O OTHER ININSP/MAINT 1 SO29440AM 440 DURING PREFLIGHT, THE CREW NOTED THE PAX DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT PACK ASSEMBLY. (K) 2H72 4T4 TRTA53EU E20NE 20060320000812006032000081NE 2006 3 20 AWH2006F00001 220051209A7314 COUPLING CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE MCAULY3AF34C3GFR34C703 GL ENG DRV FUEL PMPCORRODED E AWHAK NONE O OTHER ININSP/MAINT 1 WP17772FE 1637 208B0268 19142 970839 PRECAUTIONARY INSPECTIO OF THE FUEL PUMP DRIVE SPLINE IAW MM. FUEL PUMP COUPLING INSITU INSPECTION. MAINTENANCE FOUND THE FUEL PUMP DRIVE SPLINE SEVERELY CORRODED. TH FUEL PUMP ASSY WAS REPLACED WITH A FRESH OVERHAULED UNIT AND THE AIRCRAFT RETURNED TO SERVICE. (K) 1H71 3T3 T A37CE E4EA 5 CP60GL 20060321000192006032100019NM 2006 3 21 ASAA0510352 120051129A53306545866648 SKIN PANEL BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE BS 618-635 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 CORROSION ON INTERNAL SURFACE OF SKIN PANEL BETWEEN KEEL BEAMS AT BSTA 618 TO 635. REPLACED PANEL WITH FABRICATED REPAIR PART IAW ERO AND EA. (K) 2L72 4F4 FRTA16WE E2EA 20060321001212006032100121NM 2006 3 21 ASAA0510354 120051228A574069406091 ATTACH FITTING BOEING737 7372Q8C 138448SNM PWA JT8 JT8D17 52049NE NR 5 SLAT CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02741AS 21959 DURING L/E LUBE W/C 18412001, FOUND NR 5 L/E SLAT IB SLAT TRACK ATTACH FITTING CRACKED AT MOUNT EAR PN 69-40609-1. REPLACED ATTACH FITTING WITH 69-40609-3 IAW EA TO COMPLY WITH EM 5740-01458 AND AD 2005-20-16. (K) 2L72 4F4 F A16WE E2EA 20060321001222006032100122WP 2006 3 21 2005000014 120050829A2810272002721 CHECK VALVE DOUG DC10 DC1030 3023501WP FUEL SYSTEM MALFUNCTIONED A CNMAA UNSCHED LANDING K FLUID LOSS CLCLIMB 1 SW0759083 47926 AFTER T/O, RECEIVED TANK OVERFILLED LIGHT ON. VISUAL CHECK CONFIRMED FUEL VENTING OUT OF THE LEFT WING VENT. FUEL VENTED FOR APPROX 20 MIN. FUEL LOSS CONFIRMED OUT OF NR 3 MAIN AT 2000 LBS. TRIED TAKING TANKS DOWN TO 3000 LBS BELOW FULL AND REFILLING THEM USING THEIR ASSOC TRANS PUMPS. NO HELP. FUEL FINALLY STOPPED VENTING ON APPROACH. REMOVED AND REPLACED FUEL VENT CHECK VALVE IAW DC 10 M/M 28-12. LEAK CHECK GOOD. 2L73 4F A22WE 20060316001982006031600198WP 2006 3 16 ASAA0580541 120051212A532099100789 WEB DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE L1 DOOR SILL CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 C-CHECK, L-1 DOOR JAMB LOWER SILL WEB CORRODED. REMOVED DAMAGED SECTION OF WEB. INSTALLED REPAIR DOUBLER. (K) 2L72 4F4 FRTA6WE E9NE 20060316001992006031600199WP 2006 3 16 ASAA0580544 120051212A5321993653915 FLOOR PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 C-CHECK, CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (K) 2L72 4F4 FRTA6WE E9NE 20060316002002006031600200WP 2006 3 16 ASAA0850542 120051212A532199365479 FLOOR PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 C-CHECK, CABIN FLOOR PANEL HAS CORRODED INSERTS AND DELAMINATED AROUND INSERTS. REPLACED FLOOR PANEL. (K) 2L72 4F4 FRTA6WE E9NE 20060316002012006031600201WP 2006 3 16 ASAA0580545 120051212A5321993654759 FLOOR PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 C-CHECK, CABIN FLOOR PANEL HAS CORRODED INSERTS AND IS DELAMINATED AROUND INSERTS. REPLACED FLOOR PANEL. (K) 2L72 4F4 FRTA6WE E9NE 20060321002052006032100205WP 2006 3 21 2005000015 120050831A281040F107 VALVE DOUG DC10 DC1030 3023501WP FUEL SYSTEM MALFUNCTIONED A CNMAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW0759083 47926 FUEL VENTING OUT OF THE LEFT WING VENT BOX AREA. RIGHT SIDE OK. NO TANK OVERFILLED LIGHT ON. APPROX 1600 LBS VENTED. AFTER BLOCK IN FUEL LEAKING OUT OF LEFT FUEL VENT BOX DRAIN. REMOVED AND REPLACED CLIMB VENT FLOAT VLV IAW DC10 M/M 28-12. ALSO REMOVED AND REPLACED VENT BOX CK VLV PRECAUTIONARY PER 28-12. 2L73 4F A22WE 20060321002082006032100208NM 2006 3 21 ASAA0580559 120051226A5344 HINGE DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE OXY MASK FAILED A ASAAB EMER. DESCENT C F.O.D. CLCLIMB 1 NM02979AS 53471 CLIMB AT FL260, ENROUTE, FWD FLIGHT ATTENDANT OXYGEN MASK DID NOT DROP DURING CABIN DECOMPRESSION CAUSED BY FUSELAGE SKIN PUNCTURE. DETERMINED THE THE O2 MASK DOOR WAS JAMMED BY A DEBONDED O2 MASK DOOR HINGE. REBONDED O2 MASK DOOR HINGE AND ADJUSTED CLEARANCE. DOOR THEN OP CHECKED OK. (K) 2L72 4F4 FRT E9NE 20060322001722006032200172CE 2006 3 22 GNM2006F00000 120051208A321112116012 FITTING CESSNA206 U206G 2073356CE CONT O520 IO520F 17032SO RT MLG CRACKED E GNMAK NONE O OTHER ININSP/MAINT 1 SW019700M6513 04557 U20604557 DURING AN ANNUAL INSPECTION A CRACK WAS DETECTED ON THE RT OB MLG FITTING. CRACK IS AT FWD, OB UPPER PART OF FITTING NEAR BOLT HOLE WHERE GEAR LEG REST AGAINST FITTING. CAUSE AND DURATION OF CRACK IS UNKNOWN. NO AD`S OR SB APPLY TO GEAR FITTINGS. (K) 1H71 3O3 O A4CE E5CE 20060322002212006032200221SO 2006 3 22 MASA200500956 120051125A3200140197 TRANSDUCER EMB 145 EMB145LR 3260212SO WHEEL SPEED MALFUNCTIONED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07834MJ11862 145340 ASH 2958 CLT. E1 T/R DIAGREE MESSAGE. MAINTENANCE PLACED E1 T/R ON MEL. MX R2 WHEEL SPEED TRANSDUCERS (12/3/2005). 2L72 4T RTT00011AT 20060322002222006032200222GL 2006 3 22 MASA200500979 220051201A7261 CARBON SEAL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL ENGINE LEAKING A MASAE ENGINE SHUTDOWN K FLUID LOSS NRNOT REPORTED 1 SW07847MJ7629 505 145517 ASH 2829 MGM. SHUTDOWN THE ENGINE DUE TO THE LOST OF ENGINE OIL PRESSURE AND THE LOST OF ENGINE OIL. MAINTENANCE REPLACED NR 2 GENERATOR AND NR 2 GENERATOR CARBON SEAL. 2L72 4T4 FRTT00011ATTE6CH 20060322002262006032200226SO 2006 3 22 MASA200501087 120051227A521014525311403 SEAL EMB 145 EMB145LR 3260212SO PAX DOOR LEAKING A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07849MJ 145534 ASH 2904 LIT. PASSENGER DOOR SQUEALS. A/C FERRIED TO CLT TO HAVE THE SEAL REPLACED. MAINTENANCE REMOVED AND REPLACED DOOR SEAL. 2L72 4T RTT00011AT 20060322002292006032200229EU 2006 3 22 SDR2005087 120051211A2761 INDICATION SYS AEROSPATR72 ATR72 EU PWA PW120 PW127 NE SPOILER UNKNOWN A TRBAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 SO29434AT 434 DURING FLIGHT FOUND SPOILER INDICATION INOPERATIVE AND AILERON EXTREMELY HEAVY. AIRCRAFT RETURNED TO AIRPORT. PERFORMED OPERATIONAL CHECK OF SPOILERS AND FOUND WORKING AND INDICATING PROPERLY. PERFORMED A DETAILED VISUAL INSPECTION TO THE AILERON CONTROL MECHANISM AND FOUND SATISFACTORY. FUNCTIONAL CHECK CONDUCTED AND FOUND SATISFACTORY. (K) 2H72 4T4 TRT E20NE 20060321000242006032100024NM 2006 3 21 ASAA0510351 120051128A534065549615 ATTACH ANGLE BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE BS 348.2 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 2 EA CRACKS FOUND AT STOP FITTING FASTENER HOLES AT BS 348.2, S16L. REPLACED INTERCOSTAL ATTACH ANGLE AND WEB FLANGE IAW EA. (K) 2L72 4F4 FRTA16WE E2EA 20060321000252006032100025NE 2006 3 21 ASAA0680257 220050901A7200 ENGINE DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE RIGHT SEIZED A ASAAO OTHER YJ ENGINE STOPPAGE WARNING INDICATION DEDESCENT 1 NM02975AS523797450 53451 P716721D RIGHT ENGINE SEIZED ON FINAL APPROACH. REPLACED ENGINE. TEARDOWN REVEALED INITIAL CAUSE TO BE FAILED COMPRESSOR 8TH STAGE STATOR AT BRAZED WELD REPAIR. CRACK ORIGINATED ON VANE OD T/E AND PROPAGATED INTO HCF. 2L72 4F4 FRTA6WE E2EA 20060322001272006032200127NM 2006 3 22 ASAA0580558 120051226A5330 SKIN DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE FUSELAGE PUNCTURED A ASAAB EMER. DESCENT O OTHER CLCLIMB 1 NM02979AS 53471 CLIMB, ENROUTE, CABIN DECOMPRESSED RAPIDLY AND UNCONTROLLABLE. ALL OXYGEN MASKS, SAME FOR ONE (TO BE REPORTED UNDER SEPARATE SDR), DROPPED PROPERLY. AN EMERGENCY DESCENT WAS MADE AND THE AIRCRAFT LANDED SAFELY BACK AT SEA. INVESTIGATION REVEALED THE CAUSE OF DECOMPRESSION TO BE A PUNCTURE IN THE FUSELAGE SKIN, THOUTHT TO BE THE RESULT OF AN IMPACT BY A RAMP VEHICLE. PUNCTURE REPAIR IS UNDERWAY, AND A FULL INVESTIGATION OF THE EVENT HAS BEEN INITITATED. NOTE: EXACT FUSELAGE LOCATION OF THE DAMAGE WILL BE SPECIFIED ONCE THE REPAIR HAS BEEN COMPLETED. (K) 2L72 4F4 FRT E9NE 20060322002482006032200248EA 2006 3 22 ASOA051128S 120051220A5320 STRUCTURE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 DURING A C-CHECK, THE FS 409+128 TO FS 559.00, AND RBL36 TO FLOOR STR WAS FOUND TO BE CORRODED IN NUMEROUS SPOTS. MAINTENANCE REPAIRED THE FS 409+128 TO FS 559.00, AND RBL 36 TO FLOOR STR IAW REO. (K) 2L72 4F4 FRTA21EA E15NE 20060322002512006032200251EA 2006 3 22 ASOA051102S 120051216A5310 BEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 DURING A C-CHECK, THE LT SIDE STA 349 TRANSVERSE BEAM, UPPER SURFACE AT THE PASSENGER DOOR, WAS FOUND TO BE CORRODED BEYOND LIMITS. AFTER MAINTENANCE ALODINED, PRIMED, AND PAINTED THE LT SIDE STA 349 TRANSVERSE BEAM UPPER SURFACE, AT THE PASSENGER DOOR, IAW SRM, IT WAS FOUND TO BE WITHIN ACCEPTABLE LIMITS. (K) 2L72 4F4 FRTA21EA E15NE 20060322002592006032200259EA 2006 3 22 ASOA051132S 120051220A5260601R3196057 STEP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27914EV 7752 DURING A GROUND INSPECTION, THE PASSENGER DOOR BOTTOM STEP WAS FOUND BROKEN. MAINTENANCE REPAIRED THE PASSENGER DOOR BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20060322002442006032200244WP 2006 3 22 ASAA0680003 120050115A5313593666713 LONGERON DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE BS 1237-1298 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02969AS 53063 C-CHECK, LONGERON CORRODED. REPLACED LONGERON. (K) 2L72 4F4 FRTA6WE E9NE 20060323001352006032300135NM 2006 3 23 DHL2006752524 120051230A5754 ATTACH FITTING BOEING727 727223 1384074NM SLAT ACTUATOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01752DH 22466 FOUND RT WING NR 5 L/E SLAT ACT ROD END ATTACH FITTING, INTERNAL ANGLES INBOARD AND OUTBOARD ARE CRACKED. REMOVED INBOARD AND OUTBOARD RIBS ON RIGHT WING NR 5 SLAT ACT END ATTACH TO FITTING, IAW B727 SRM 51-30-2, FABRICATED 2 EA RIBS FROM 7075-0 .040 SIZE 16" X 6.5" PO 9001602, IAW B727 SRM 57-50-2 FIG 2, HEAT TREATED MATERIAL TO 7075-T6 IAW B727 SRM 51-10-3, TREATED AND PRIMED PARTS IAW B727 SRM 51-10-2, INSTALLED 2 EA RIBS IAW B727 SRM 51-30-2. 2L73 4F A3WE 20060322002462006032200246EA 2006 3 22 ASOA051100S 120051215A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 DURING A C-CHECK, THE LT SIDE OF THE NOSE LANDING GEAR CUTOUT RADIUS WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LT SIDE OF THE NOSE LANDING GEAR CUTOUT RADIUS IAW REO. (K) 2L72 4F4 FRTA21EA E15NE 20060327000752006032700075SO 2006 3 27 MASA200500991 120051204A7830TY204103A CONTROL UNIT EMB 145 EMB145LR 3260212SO THRUST REVERSERSMALFUNCTIONED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07847MJ9753 145517 ASH 2901 CLT. E2 REVERSE DISAGREE. MAINTENANCE REMOVED AND REPLACED ICU. 2L72 4T RTT00011AT 20060327000942006032700094WP 2006 3 27 ASAA0580560 120051229A5210 SKIN DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE PAX DOOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02947AS 53020 GATE-MAIN PAX (L-1) DOOR FORWARD CORNER DENTED BY JETWAY. REPAIRED DENT IAW SRM. (K) 2L72 4F4 FRTA6WE E9NE 20060327001122006032700112 2006 3 27 MASA200500272 420050403A221014534177405 MODULE EMB 145 EMB145LR 3260212SO TRIM CONTROL STICKS A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07838MJ749 145384 ASH 2858 CLT - HAD AN AUTO PILOT FAIL BECAUSE OF AN AILERON MIS-TRIM. MAINTENANCE REPLACED THE TRIM CONTROL MODULE. 2L72 4T RTT00011AT 20060327001132006032700113 2006 3 27 MASA200500296 420050411A22104006719906MOD SERVO EMB 145 EMB145LR 3260212SO RUDDER MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07854MJ4193 145490 ASH FLT 2859 CLT - AIRCRAFT HAD A YAW DAMP FAIL MESSAGE. MAINTENANCE PLACED YAW DAMPER ON MEL AND DOWN GRADED THE AIRCRAFT TO NON RVSM STATUS. MX REPLACED RUDDER SERVO. 2L72 4T RTT00011AT 20060327001152006032700115 2006 3 27 MASA200500350 420050513A23107013270965 RMU EMB 145 EMB145LR 3260212SO COCKPIT FAILED A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW07849MJ8858 8057 145534 ASH 2781 CLT - THE CREW REPORTED SMOKE IN THE COCKPIT. MAINTENANCE IDENTIFIED THE RADIO MANAGEMENT UNIT AS THE SOURCE OF THE FAULT AND REPLACED IT. 2L72 4T RTT00011AT 20060327001162006032700116SO 2006 3 27 MASA200500407 120050523A30100871HT3 DETECTOR EMB 145 EMB145LR 3260212SO ICE FAILED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07828MJ9404 7040 145218 ASH 2972 HSV TO PHL, THE AIRCRAFT DIVERTED TO CLT AFTER THE ANTI-ICE SYSTEM CAME ON IN FLIGHT FOLLOWED BY A REDUCTION IN AIRSPEED, BOTH UNCOMMANDED. MAINTENANCE TROUBLESHOT THE SYSTEM AND REMOVED AND REPLACED THE ICE DETECTORS AND RELAYS. 2L72 4T RTT00011AT 20060327001702006032700170EA 2006 3 27 MASA200500922 120051120A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0737342 7342 ASH 7202 BNA - FORWARD CEILING EMERGENCY FLOOD LIGHT INOPERATIVE. OPS CHECKED GOOD. 2L72 4F RTA21EA 20060327001752006032700175EA 2006 3 27 MASA200500933 120051122A335066903 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0717156 7156 ASH 7181 PHL - FLOOR EMERGENCY EXIT LIGHT INOP. MAINTENANCE REMOVED AND REPLACED STRIP LIGHT. 2L72 4F RTA21EA 20060327001982006032700198 2006 3 27 MASA200500695 420050904A2200 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA AUTOPILOT TRIM FALSE ACTIVATIONA MASAO OTHER O OTHER NRNOT REPORTED 1 SW0777278 7278 ASH 6107 PSP - HAD AN AUTO PILOT TRIM CAUTION MESSAGE WHEN FLAPS WERE SELECTED TO 8 DEGREES. OPS CHECKED GOOD. 2L72 4F RTA21EA 20060328000172006032800017EA 2006 3 28 MASA200500736 120050920A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMEGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07400MJ 7309 ASH 2733 BGM - A CEILING LEVEL EMERGENCY EXIT FLOOD LIGHT THAT WAS INOPERATIVE. MX REPLACED LAMP. 2L72 4F RTA21EA 20060328000192006032800019EA 2006 3 28 MASA200500744 120050923A335066903 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0717275 7275 ASH 6231 PHX - FLOOR EMERGENCY LIGHT IS INOPERATIVE. MX R2 LUMINESCENT STRIP. 2L72 4F RTA21EA 20060328000202006032800020EA 2006 3 28 MASA200500748 120050924A335066903 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0717275 7275 ASH 6224 PHX - THE CREW REPORTED ONE FLOOR PATH LIGHTING STRIP INOP. MAINTENANCE REPLACED THE STRIP. 2L72 4F RTA21EA 20060328000212006032800021EA 2006 3 28 MASA200500751 120050925A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0797325 7325 ASH 6334 PHX - WING EXTERIOR E-EXIT LIGHT INOP. MAINTENANCE REPLACED THE EXIT LIGHT. 2L72 4F RTA21EA 20060328000222006032800022EA 2006 3 28 MASA200500760 120050928A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY SIGN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0717275 7275 ASH 6098 PHX - LEFT EMERGENCY DOOR EXIT SIGN INOP. MAINTENANCE REPLACED THE LIGHT. 2L72 4F RTA21EA 20060328000242006032800024EA 2006 3 28 MASA200500788 120051009A339766903 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT UNKNOWN A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07593ML 7465 ASH 2758 PHL - EMERGENCY EXIT FLOOR PATH LIGHTING INOP. MAINTENANCE RESET THE CONNECTOR. OPS CHECKS GOOD. 2L72 4F RTA21EA 20060327001762006032700176EA 2006 3 27 MASA200500934 120051122A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0717156 7156 ASH 7181 PHL - CEILING EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED. 2L72 4F RTA21EA 20060328000252006032800025EA 2006 3 28 MASA200500791 120051011A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BROKEN A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07591ML 7388 ASH 2762 PHL - ONE FLOOR PATH LIGHTING SEGMENT BROKEN. MAINTENANCE REPLACED THE SEGMENT. 2L72 4F RTA21EA 20060328000262006032800026EA 2006 3 28 MASA200500823 120051023A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0717358 7358 ASH 6089 PHX - FWD FLOOR EMERGENCY FLOODLIGHT INOP. MAINTENANCE RELAMPED THE LIGHT. 2L72 4F RTA21EA 20060328000382006032800038EA 2006 3 28 SWIA200516422 120051223A5320 SILL CNDAIRCL600 CL6002B19 1900309EA PAX DOORWAY CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07407SW 7034 PAX DOOR CUTOUT LWR SILL RISER CORRODED BETWEEN FS 310 & 349, ITEM FOUND AT C CHECK INSPECTION. PAX DOOR CUT OUT LWR SILL RISER REPLACED IAW CRJ SRM 51-40-11, 53-21-23, 51-21-11, 51-23-00, 51-42-06, 51-42-13, 51-25-00. 2L72 4F RTA21EA 20060328000392006032800039EA 2006 3 28 SWIA200516423 120051223A5320 SILL CNDAIRCL600 CL6002B19 1900309EA PAX DOORWAY CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07407SW 7034 PAX DOOR CUT OUT LWR SILL FWD AND AFT BRACKET ASSY FOR AIR STAIR HINGE ARMS CORRODED, ITEM FOUND AT C CHECK INSPECTION. REPLACED BRACKETS IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06. 2L72 4F RTA21EA 20060328000412006032800041EA 2006 3 28 SWIA200516425 120051223A5312 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07407SW 7034 CARGO COMPARTMENT AFT PRESSURE BULKHEAD WEB LBL 27.5, WL 130 CRACKED, ITEM FOUND AT C CHECK INSPECTION. WEB REPAIRED. REF. CRJ REO 601R-53-61-1541 REV "NC". 2L72 4F RTA21EA 20060328000422006032800042EA 2006 3 28 SWIA200516426 120051223A5320 UNKNOWN CNDAIRCL600 CL6002B19 1900309EA BS 630 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07407SW 7034 AFT EQUIPMENT COMP, ESB IS CRACKED ON LOWER WEB AT PANEL CUT-OUT, LT SIDE, FWD I/B CORNER, FS 630.0, LBL 39.0, ITEM FOUND AT C CHECK INSPECTION. REPAIRED REF CRJ REO 601R-53-61-1713, CRJ REO 601R-53-61-366 REV (E), CRJ REO 601R-53-61-1721, 2L72 4F RTA21EA 20060328000432006032800043EA 2006 3 28 SWIA200516427 120051223A5320 UNKNOWN CNDAIRCL600 CL6002B19 1900309EA BS 630 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07407SW 7034 AFT EQUIPMENT COMP, ESB IS CRACKED ON LOWER WEB AT PANEL CUT-OUT, RT SIDE, FWD I/B CORNER, FS 630.0, RBL 39.0, ITEM FOUND AT C CHECK INSPECTION. REPAIRED REF REO 601R-53-61-366 REV E, REO 601R-53-61-1713, REO 601R-53-61-1721. 2L72 4F RTA21EA 20060328000442006032800044EA 2006 3 28 SWIA200516428 120051223A5340 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA BS 621-325 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07407SW 7034 AFT SIDE OF REAR PRESSURE BULKHEAD RT SIDE, STATION 621 TO 625 INTERCOSTAL ATTACH CLIPS CRACKED AT STRINGERS 11R, 15R & 16R, ITEM FOUND AT C CHECK INSPECTION. REPLACED CLIPS IAW CRJ SRM 51-42-06, 51-23-00 AND 51-42-21, 51-42-13, 51-25-00, 51-25-06. 2L72 4F RTA21EA 20060328000452006032800045EA 2006 3 28 SWIA200516429 120051223A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA BS 605 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07407SW 7034 FUSELAGE, UPPER AND LOWER FRAME FLANGES ARE CRACKED, FS 605.00 STR 9L, ITEM FOUND AT C CHECK INSPECTION. REPAIR CARRIED OUT IAW REO 601R-53-61-1717. 2L72 4F RTA21EA 20060328000462006032800046EA 2006 3 28 SWIA200516430 120051223A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 605 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07407SW 7034 CARGO COMPT, FS 605.00 TRANSVERSE BEAM ATTACH ANGLE FOR LANDING PLATE STOP FITTINGS CRACKED, ITEM FOUND AT C CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13, 51-42-21, 51-41-02 AND 51-41-04. 2L72 4F RTA21EA 20060328000482006032800048EA 2006 3 28 SWIA200516432 120051223A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA BS 605 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07407SW 7034 FOUND FS 605.00 BETWEEN STR 18L AND 19L, LOWER FRAME FLANGE CRACKED, ITEM FOUND AT C CHECK INSPECTION. REPAIRED REF REO 601R-53-11-171 REV C. 2L72 4F RTA21EA 20060328000972006032800097EA 2006 3 28 MASA200500989 120051204A2560 COVER CNDAIRCL600 CL6002B19 1900309EA ESCAPE ROPE LOOSE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07592ML 7410 ASH 7245 ORD - RIGHT EMERGENCY ESCAPE ROPE COVER IS LOOSE. MAINTENANCE SECURED THE COVER. 2L72 4F RTA21EA 20060328001062006032800106SO 2006 3 28 MASA200500785 120051008A3350744426 SIGN EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07843MJ 145478 THE AIRCRAFT WAS ON RON LAST NIGHT AND SCHEDULED FOR A 2 DAY EN ROUTE INSPECTION, AND FOUND THE 3RD ROW EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT SIGN. OPERATIONAL CHECKED GOOD. 2L72 4T RTT00011AT 20060328001082006032800108SO 2006 3 28 MASA200500796 120051012A3350 POWER SUPPLY EMB 145 EMB145LR 3260212SO EMEGENCY LIGHT INGESTED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07857MJ7092 145765 DURING RON, INTERIOR CEILING ROW 3 AND 4 EMERGENCY LIGHT WAS FOUND NOT ILLUMINATING. REPLACED THE POWER SUPPLY. 2L72 4T RTT00011AT 20060328001092006032800109SO 2006 3 28 MASA200500833 120051026A2120 SMOKE EMB 145 EMB145LR 3260212SO COCKPIT DETECTED A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW07844MJ 145481 ASH 2824 CLT, CREW WAS PERFORMING THEIR PREFLIGHT INSPECTION, NOTICED A FAINT ELECTRICAL SMOKEY ODOR, IN THE COCKPIT. MAINTENANCE INSPECTED THE AIRCRAFT BUT WERE UNABLE TO DETERMINE THE ORIGIN, AS THE ODOR DISSIPATED. 2L72 4T RTT00011AT 20060328001102006032800110SO 2006 3 28 MASA200500837 120051027A34110856NF PITOT TUBE EMB 145 EMB145LR 3260212SO BURNED A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW07844MJ9922 145481 ASH 2779 GNV - A REPORT OF AN ELECTRICAL BURNING SMELL IN THE FLIGHT DECK. MAINTENANCE REPLACED THE STANDBY PITOT. 2L72 4T RTT00011AT 20060328001112006032800111SO 2006 3 28 MASA200500846 120051030A2560 HOLDER EMB 145 EMB145LR 3260212SO FLASHLIGHT BROKEN A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07849MJ 145534 ASH 2967 DCA - EMERGENCY FLASHLIGHT HOLDER BROKEN. MX REPLACED FLASHLIGHT AND HOLDER. 2L72 4T RTT00011AT 20060328001122006032800112 2006 3 28 MASA200500849 420051031A2562 ELT EMB 145 EMB145LR 3260212SO CABIN MALFUNCTIONED A MASAA UNSCHED LANDING O OTHER NRNOT REPORTED 1 SW07847MJ 145517 ASH 2994 CLT - AIRCRAFT RETURNED TO FIELD DUE TO ELT CAME ON UNCOMMANDED IN FLIGHT. MX RESET ELT. 2L72 4T RTT00011AT 20060328001132006032800113SO 2006 3 28 MASA200500873 120051110A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07853MJ 145464 ASH 2735 CLT - TWO SECTIONS OF FLOOR PATH LIGHTING INOP. MAINTENANCE INSPECTED THE SYSTEM AND FOUND THE LIGHT SEGMENTS TO BE WORKING NORMALLY. 2L72 4T RTT00011AT 20060328001282006032800128EA 2006 3 28 MASA200500978 120051130A3397 PIN CNDAIRCL600 CL6002B19 1900309EA CONNECTOR DAMAGED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0775999 7471 ASH 7220 LAN - FIVE SECTIONS OF EMERGENCY FLOOR PATH LIGHTING INOP. MAINTENANCE RESET PUSHED PIN ON CONNECTOR. 2L72 4F RTA21EA 20060328001302006032800130EA 2006 3 28 MASA200500391 120050524A2497 CIRCUIT BREAKER CNDAIRCL600 CL6002B19 1900309EA TRIPPED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW077305V 7305 ASH 6373 PHX TO YUM - THE CREW RETURNED TO THE GATE FOR NO OIL PRESSURE ON START UP OF THE NR 1 ENGINE. MAINTENANCE FOUND CURCUIT BREAKER POPPED. RESET THE CIRCUIT BREAKER AND PERFORMED AN ENGINE START. OPS CHECKED GOOD AND NO FURTHER DEFECTS WERE NOTED. 2L72 4F RTA21EA 20060929000302006092900030NE 2006 9 29 ASAA0691001 220051030A7320442317P09 HMU BOEING737 737990 NM GE CFM56 CFM56* 13802NE NR 2 ENGINE DAMAGED A ASAAE ENGINE SHUTDOWN BAJSMOKE/FUMES/ODORS/SPARKS FLAME/FIRE WARNING INDICATION TXTAXI/GRND HDL 1 NM02317AS10563 30856 890392 YYC - AFTER START ON NR 2 ENGINE LEVER RAISED TO IDLE MASTER CAUTION ENGINE AND ENGINE CONTROL ON OVERHEAD PANEL ILLUMINATED. GROUND CREW AND OTHER ACFT REPORTED SMOKE AND TORCHING ON NR 2 ENGINE. NR 2 ENGINE LEVER PLACED TO CUT OUT PER TAIL PIPE FIRE CHECK LIST. SMOKE IN CABIN NOTED AND A CABIN EVACUATION WAS INITIATED. WHEN CHECK LIST COMPLETED NO SMOKE IN CABIN OR FROM ENGINE WAS NOTED. FIRE HANDLES PULLED BUT NOT TURNED. WHILE PERFOMING VISUAL INSPECTION NOTED OIL IN THE TAIL PIPE. REPLACED NR 2 ENGINE DUE TO OIL LEAK PER TASK CARD 78471000. 2L74 4F4 FRTA16WE E2GL 20060327001802006032700180EA 2006 3 27 MASA200500945 120051124A335066903 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0777278 7278 ASH 6404 LAS - EMERGENCY FLOOR PATH LIGHTING, 3 SEGMENTS, INOP. MAINTENANCE RELAMPED. 2L72 4F RTA21EA 20060327002152006032700215EA 2006 3 27 ASOA051162 120051231A26128990741 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT ENGINE FALSE ACTIVATIONA ASOAE ENGINE SHUTDOWN N FALSE WARNING DEDESCENT 1 SO11900EV10515 7608 872219 DURING DESCENT FROM ATL-CAK, AT APPROXIMATELY 20,000 FEET, THE FIRE WARNING SYSTEM FOR THE RIGHT ENGINE SOUNDED. THE CREW SHUTDOWN THE RIGHT ENGINE AND FIRED BOTH FIRE BOTTLES. AN EMERGENCY WAS DECLARED, WITH ALL EMERGENCY VEHICLES DISPATCHED. THE AIRCRAFT PERFORMED A SINGLE ENGINE LANDING IN CAK, WHERE IT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED BOTH FIRE BOTTLES. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F4 FRTA21EA E15NE 20060327002232006032700223SO 2006 3 27 MASA200500429 120050601A335066903 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07836MJ 145359 ASH 2873 CLT - MX REPORTED THE NR 3 EMERGENCY FLOOR PATH LIGHT STRIP WAS INOP. MX REPLACED THE LIGHT STRIP WITH A PART ROBBED FROM ANOTHER AIRCRAFT. OPS CHECKS WERE GOOD. 2L72 4T RTT00011AT 20060327002242006032700224SO 2006 3 27 MASA2005460 120050612A5270 SWITCH EMB 145 EMB145LR 3260212SO CARGO DOOR OUT OF ADJUST A MASAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SW07831MJ 145273 AIR SHUTTLE 2792 FROM MOB TO CLT - ABORTED TAKEOFF DUE TO A CARGO DOOR OPEN INDICATION DURING TAKEOFF ROLL. MAINTENANCE LUBED AND ADJUSTED SWITCH, OPS CHECKED GOOD. 2L72 4T RTT00011AT 20060327002252006032700225SO 2006 3 27 MASA200500515 120050703A335066903 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07836MJ 145359 ASH 2731 CLT - THE CAPTAIN REPORTED TWO EMERGENCY EXIT FLOOR LIGHTING STRIPS WERE INOPERATIVE. MAINTENANCE REPLACED NR 2 AND NR 3 FLOOR LIGHTING STRIPS. 2L72 4T RTT00011AT 20060327002272006032700227SO 2006 3 27 MASA200500532 120050710A3350316 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07836MJ 145359 ASH 2647 CLT - CAPTAIN REPORTED AN EMERGENCY EXIT CEILING LIGHT INOPERATIVE. MX REPLACED THE INOPERATIVE BULB. 2L72 4T RTT00011AT 20060327002282006032700228SO 2006 3 27 MASA200500602 120050729A33501317 LAMP EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07833MJ 145327 ASH 2801 CLT, LT OVERWING EMERGENCY EXIT LIGHT INOP. MX REPLAMED THE LIGHT AND IT OPERATED NORMALLY. 2L72 4T RTT00011AT 20060328000272006032800027EA 2006 3 28 MASA200500840 120051029A3397 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT LOOSE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0775994 7367 ASH 7165 IAD - FLOOR EMERGENCY LIGHTS ROW 1 THROUGH 5 INOP. SECURED CONNECTION. 2L72 4F RTA21EA 20060328000282006032800028EA 2006 3 28 MASA200500848 120051031A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0777260 7260 ASH 6098 PHX - RIGHT FORWARD EMERGENCY EXTERIOR LIGHT INOP. MX RELAMPED LIGHT. 2L72 4F RTA21EA 20060328000402006032800040EA 2006 3 28 SWIA200516424 120051223A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 589 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07407SW 7034 CARGO PIT, FS 589.00 TRANSVERSE BEAM ATTACH ANGLE CRACKED AT CARGO DOOR LANDING PLATE, ITEM FOUND AT C CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13, 51-42-21, 51-41-02, 51-41-04. 2L72 4F RTA21EA 20060328001272006032800127EA 2006 3 28 MASA200500995 120051205A335020131A BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0777286294 7286 ASH 6002 PHX - RIGHT EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOP. MAINTENANCE REMOVED AND REPLACED BATTERY. 2L72 4F RTA21EA 20060328001292006032800129EA 2006 3 28 MASA200500982 120051201A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0747202 7202 ASH 7199 ORD - FLAPS FAIL DURING DESCENT. FLAPS FAILED AT 0 DEGREES WHEN SELECTED TO 8 DEGREES. MAINTENANCE C/W PART A. 2L72 4F RTA21EA 20060328001582006032800158SO 2006 3 28 MASA200500692 120050903A2560P2070011100 FLASHLIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07826MJ 145214 ASH 2743 CLT - EMER FLASH LIGHT INOP. MX REMOVED AND REPLACED THE LIGHT. 2L72 4T RTT00011AT 20060328001602006032800160SO 2006 3 28 MASA200500739 120050922A335020131A BATTERY PACK EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A MASAO OTHER L NO TEST NRNOT REPORTED 1 SW07837MJ10236 145367 ASH 2718 CAE - EMERGENCY LIGHTS WILL NOT TEST. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERIES. 2L72 4T RTT00011AT 20060328001612006032800161SO 2006 3 28 MASA200500784 120051008A335066903 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07827MJ 145217 ASH 2999 CLT, CREW REPORTED THE 4TH FROM FWD EMERGENCY FLOOR PATH LIGHT STRIP WAS INOP, R2 LIGHT STRIP. 2L72 4T RTT00011AT 20060328001852006032800185EA 2006 3 28 MASA200500516 120050704A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0777331 7331 ASH 7158 CLE - REAR CEILING LEVEL EMERGENCY FLOOD LIGHT INOP. MX RELAMPED. 2L72 4F RTA21EA 20060328002202006032800220SO 2006 3 28 MASA200501041 120051215A335066903 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07838MJ 145384 ASH 2950 CMH - EMER PATH LIGHTING INOP BETWEEN SEATS 3-7. MX REMOVED AND REPLACED CHARGER AND PATH LIGHT STRIP. OPS CHECK GOOD. 2L72 4T RTT00011AT 20060328002272006032800227EA 2006 3 28 MASA200501029 120051210A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0777302 7302 ASH 6216 PHX - LT WING FORWARD EMERGENCY EXIT LIGHT INOP. MAINTENANCE RELAMPED OPS CHECK GOOD. 2L72 4F RTA21EA 20060328002282006032800228EA 2006 3 28 MASA200501030 120051211A2560111RJ7001 PLACARD CNDAIRCL600 CL6002C10 1390015EA CABIN MISSING A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07503MJ 10058 ASH 7022 ORD - EXIT ROW 12 LT AFT FLOOR PROX EMERG ESCAPE PATH MARKING MISSING. MAINTENANCE REMOVED AND REPLACED MARKER. 2L72 4F RTA21EA 20060328002302006032800230EA 2006 3 28 MASA200501032 120051211A3230 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA MLG ILLUMINATED A MASAO OTHER J WARNING INDICATION LDLANDING 1 SW0747202 7202 ASH 7244 PHL - GEAR DISAGREE ON LANDING. MAINTENANCE RAN THE GEAR THROUGH SEVERAL TIMES AND NO FAILURE. TEST FLIGHT WAS GOOD. 2L72 4F RTA21EA 20060327000762006032700076SO 2006 3 27 MASA200501024 120051210A3260852701 PROXIMITY SENSOR EMB 145 EMB145LR 3260212SO NLG OUT OF POSITION A MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW07834MJ660 145340 ASH 3914 CLT. L/G AIR FAIL MESSAGE AND TR 1 & 2 MESSAGE. MAINTENANCE REPLACED NOSE PROX SENSOR. 2L72 4T RTT00011AT 20060327001112006032700111 2006 3 27 MASA200500200 420050310A2210HG2010AC02 AHRS EMB 145 EMB145LR 3260212SO NR 1 FAILED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07845MJ8388 145502 ASH 2796 CLT - HAD AN AUTO PILOT DISENGAGE DUE TO AN AHRS INOP. MAINTENANCE REPLACED THE AHRS COMPUTER. 2L72 4T RTT00011AT 20060327001142006032700114SO 2006 3 27 MASA200500315 120050425A2711 TRIM SYSTEM EMB 145 EMB145LR 3260212SO MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07833MJ 145327 ASH 2842 CAE TO CLT - THE CREW RETURNED TO THE FIELD DUE TO THE LOSS OF MAIN AND BACKUP PITCH TRIM SYSTEMS. MAINTENANCE RESET THE PITCH TRIM SYSTEM AND IT OPERATED NORMALLY. THE AIRCRAFT DEPARTED WITHOUT INCIDENT. 2L72 4T RTT00011AT 20060327001692006032700169EA 2006 3 27 MASA200500921 120051119A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW077305V 7305 COS - LT CENTER OVERWING EMERGENCY EXIT LIGHT INOP. MAINTENANCE RELAMPED THE EXIT LIGHT, OPS CHECKED GOOD. 2L72 4F RTA21EA 20060327001712006032700171EA 2006 3 27 MASA200500923 120051120A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0737342 7342 ASH 7202 BNA - TWO FORWARD EXTERIOR EMERGENCY FLOOD LIGHTS ONE ON EACH SIDE ARE INOPERATIVE. OPS CHECKED GOOD. 2L72 4F RTA21EA 20060327001722006032700172EA 2006 3 27 MASA200500925 120051120A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0775996 7357 ASH 7122 ORD - AFT CEILING EMERGENCY FLOOD LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LIGHT ASSY. 2L72 4F RTA21EA 20060327001732006032700173SO 2006 3 27 MASA200500926 120051121A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07853MJ 145464 DURING RON, THE CREW FOUND THE AFT INTERNAL EMERGENCY LIGHT NOT ILLUMINATING. AFT INTERNAL EMERGENCY LIGHT NOT ILLUMINATING. 2L72 4T RTT00011AT 20060327001742006032700174EA 2006 3 27 MASA200500927 120051121A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0717358 7358 ASH 6672 COS - RIGHT EXTERIOR OVERWING EMERGENCY LIGHT INOP. MAINTENANCE REPLACED THE LAMP. 2L72 4F RTA21EA 20060327001772006032700177EA 2006 3 27 MASA200500936 120051122A33501317 BULB CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT BURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07503MJ 10058 ASH 7279 CAE - SERVICE DOOR EMERGENCY EXIT LIGHT HAS SEVERAL BULBS BURNED OUT. MAINTENANCE RELAMPED THE SIGN. 2L72 4F RTA21EA 20060327001782006032700178EA 2006 3 27 MASA200500937 120051122A33501317 BULB CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT BURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07503MJ 10058 ASH 7279 CAE - MAIN CABIN DOOR EMERGENCY EXIT LIGHT HAS SEVERAL BULBS BURNED OUT. MAINTENANCE RELAMPED THE SIGN. 2L72 4F RTA21EA 20060327001792006032700179EA 2006 3 27 MASA200500938 120051122A33501317 LAMP CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT BURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07503MJ 10058 ASH 7279 CAE - LEFT OVERWING EMERGENCY EXIT LIGHT HAS SEVERAL BULBS BURNED OUT. MAINTENANCE RELAMPED THE SIGN. 2L72 4F RTA21EA 20060328000232006032800023EA 2006 3 28 MASA200500779 120051008A3397 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCONNECTED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07650ML 7137 ASH 2750 PHL - REAR HALF OF THE EMERGENCY PATH LIGHTING INOPERATIVE. MX CLEANED AND RE CONNECTED CONNECTOR AT BATTERY PACK. 2L72 4F RTA21EA 20060328000372006032800037EA 2006 3 28 SWIA200516421 120051223A5312 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA BS 559 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07407SW 7034 RT MLG BAY, PRESSURE BULKHEAD IS CRACKED BESIDE AILERON QUADRANT ATTACH BOLT, FS 559.0, RBL 17, ITEM FOUND AT C CHECK INSPECTION. RT MLG BAY PRESSURE BULKHEAD REPAIRED. REF. CRJ REO 601R-53-41-260 REV "A". 2L72 4F RTA21EA 20060328001072006032800107SO 2006 3 28 MASA200500795 120051011A335020131A BATTERY PACK EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07835MJ17128687 145353 ASH 2969 CLT, OVERWING EMERGENCY EXIT SIGN WILL NOT ILLUMINATE. MX REPLACED A BATTERY PACK. 2L72 4T RTT00011AT 20060328001592006032800159SO 2006 3 28 MASA200500697 120050905A2560P2070011100 FLASHLIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07845MJ 145502 ASH 2804 CLT - F/A AFT EMERG FLASHLIGHT INOP. MX REPLACED FLASHLIGHT. 2L72 4T RTT00011AT 20060328001652006032800165SO 2006 3 28 RAIA00603025 120050317A3397 WIRE EMB 145 EMB145 3260210SO EMERGENCY LIGHT BROKEN A RAIAK NONE O OTHER ININSP/MAINT 1 CE03803HK 145077 PRE FLIGHT NR 3555 - PIT - FIRST EMERGENCY LIGHT ON THE LEFT SIDE IS INOP. MAINTENANCE REPAIRED A BROKEN WIRE TO THE EMERGENCY LIGHT STRIP. 2L72 4F RTT00011AT 20060328001552006032800155SO 2006 3 28 MASA200500668 120050824A33503025103 LIGHT EMB 145 EMB145LR 3260212SO EXTERNAL INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07842MJ 145457 DURING RON, THE CREW FOUND A LT FWD EXTERNAL EMERGENCY LIGHT INOP. RELAMPED. 2L72 4T RTT00011AT 20060328001562006032800156SO 2006 3 28 MASA200500676 120050827A3350316 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07854MJ 145490 ASH 2633 CLT, THE FWD 2 CEILING EMER LIGHTS INOP. MX REPLACED THE LIGHTS. 2L72 4T RTT00011AT 20060328001572006032800157SO 2006 3 28 MASA200500691 120050902A335066903 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07847MJ 145517 LT FWD FLOOR EMERGENCY STRIP INOP. REPLACED STRIP. 2L72 4T RTT00011AT 20060328002192006032800219SO 2006 3 28 MASA200501040 120051215A243232248001 BATTERY EMB 145 EMB145LR 3260212SO MASTER DISCHARGED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07838MJ9191 145384 ASH 2950 CMH - BOTH MAIN BATTERYS DEAD. MAINTENANCE REMOVED AND REPLACED NR 1 AND NR 2 BATTERY. 2L72 4T RTT00011AT 20060328002292006032800229EA 2006 3 28 MASA200501031 120051211A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0717337 7337 ASH 6491 BIL - CABIN CEILING EMERGENCY FLOOD LIGHT IS INOPERATIVE. MAINTENANCE RELAMPED. 2L72 4F RTA21EA 20060329000922006032900092NM 2006 3 29 2005UALA01243 120051106A3610 SWITCH BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE RT PACK FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29672UA 30027 FLIGHT DIVERTED DUE TO LOST RIGHT PACK. FOUR UNITS WERE REMOVED DUE TO THIS EVENT: HIGH PRESSURE SHUTOFF VALVE AND PRESSURE REGULATING VALVE (HPSOV/PRV, P/N: 790270-4/-14), HIGH PRESSURE CONTROLLER (HPC, P/N: 773289-15) AND PRESSURE REGULATING VALVE CONTROLLER (PRC, P/N: 792755-16). THERE WERE NO FAULTS FOUND ON HPSOV AND PRV. HPC REPAIRED DUE TO BELLOWS FAILURE, WORN BUSHINGS, DAMAGED DIAPHRAGM, BITE PRESSURE SWITCH FAILURES AND DIFFERENTIAL SWITCH FAILURE, WHICH WAS CONSIDERED TO BE THE PRIMARY FAILURE OF THE UNIT. PRC WAS REPAIRED DUE TO SCREW AND ORIFICE DAMAGES. 2L72 4F4 FRTA1NM E24NE 20060425001142006042500114NM 2006 4 25 ASAA0540630 120051108A532065C332685 INTERCOSTAL BOEING737 7374Q8 138447QNM BS 925-987 CRACKED A ASAAO OTHER O OTHER NRNOT REPORTED 1 NM02774AS 25107 PAE - FOUND INTERCOSTAL ANGLE CORRODED AT BS 925-987, FOUND TO BE CRACKED ALSO AT THE FASTENER HOLE. REPLACED INTERCOSTAL IAW B737-400 SRM 53-60-51 AND 51-40-06. (M) 2L72 4F RTA16WE 20060329001202006032900120NM 2006 3 29 ASAA0540700 120051201A57536546435335 STRUCTURE BOEING737 737490 1384715NM T/E FLAP BROKEN A ASAAK NONE O OTHER ININSP/MAINT 1 NM02796AS 28891 OKC - FOUND LEFT OUTBOARD AFT FLAP OUTBOARD CORNER BENT UP AND BROKEN. REPAIRED DAMAGED AREA, IAW B737-400 SRM 51-70-10 PAGES 213, 221, 238, AND 249. (M) 2L72 4F RTA16WE 20060329001212006032900121NM 2006 3 29 ASAA0540622 120051108A532065C332685 INTERCOSTAL BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND INTERCOSTAL ANGLE CORRODED AT BS 925-947, FOUND TO BE CRACKED ALSO AT FASTENER HOLES. REMOVED AND REPLACED INTERCOSTAL IAW B737-400 SRM 51-40-06 AND 53-60-51. (M) 2L72 4F RTA16WE 20060329001222006032900122NM 2006 3 29 ASAA0540623 120051108A53206545855101 SILL BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND AFT SERVICE DOOR CUTOUT MOPSILL IS CORRODED. REMOVED AND REPLACED INTERCOSTAL IAW B737-400 SRM 51-40-02 AND DWG 65-45885. (M) 2L72 4F RTA16WE 20060329001232006032900123NM 2006 3 29 ASAA0540614 120051105A5330 SKIN BOEING737 7374Q8 138447QNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 OKC - DENT IN FUSELAGE SKIN BETWEEN STRINGER 20R-21R, BS 294-296. TEMPORARY REPAIR INSTALLED. REMOVED EXISTING REPAIR, CUTOUT DAMAGED AREA OF SKIN, FABRICATED AND INSTALLED A REPAIR DOUBLER, TRIPLER, FILLERS AND TWO TEAR STRAP INTERNAL DOUBLERS IAW B737-400 SRM 53-00-01, FIG 201, AND REPAIR 31. (M) 2L72 4F RTA16WE 20060329001252006032900125NM 2006 3 29 ASAA0540618 120051103A531565C339503 FLOORBEAM BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02794AS 28889 OKC - FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 986.5. REMOVED UPPER CHORD, FABRICATED AND INSTALLED REPAIR PARTS IAW ASA EA 5310-02512. (M) 2L72 4F RTA16WE 20060329001262006032900126NM 2006 3 29 ASAA0540619 120051108A53206552878102 SILL BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND AFT ENTRY DOOR CUTOUT MOPSILL CORRODED. REMOVED AND REPLACED MOPSILL IAW B737-400 SRM 51-40-02, AND DWG 65-52878. (M) 2L72 4F RTA16WE 20060329001272006032900127NM 2006 3 29 ASAA0540599 120051103A53306545800219 SKIN BOEING737 7374Q8 138447QNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - FOUND DENT IN FUSELAGE SKIN. REPAIRED SKIN PER ASA EA 5330-02014. (M) 2L72 4F RTA16WE 20060329001282006032900128NM 2006 3 29 ASA05400603 120051108A5311 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND BS 380 FRAME MEMBER CRACK AT BIN RAIL ATTACHMENT. REPAIRED PER B737-400 SRM 53-00-07. (M) 2L72 4F RTA16WE 20060329001292006032900129NM 2006 3 29 ASAA0540625 120051108A53476555484 SEAT TRACK BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND CORROSION AT BS 500F-500G, LBL 18.5, WL 156 ON FLOOR TRACK. REMOVED DAMAGED FLOOR TRACK AND REPLACE IAW B737-400 SRM 53-00-53. (M) 2L72 4F RTA16WE 20060329001302006032900130NM 2006 3 29 ASAA0540627 120051108A256065C1612123 FITTING BOEING737 7374Q8 138447QNM GIRT BAR CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND CORROSION ON L1 AFT GIRT BAR FITTING. REPAIRED IAW B737-400 SRM 51-40-02 AND 53-00-07. (M) 2L72 4F RTA16WE 20060329001312006032900131NM 2006 3 29 ASAA0540628 120051108A5311 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND CRACKED FRAME AT BIN RAIL SUPPORT AT BS 360 BETWEEN STRINGER 7-8 LEFT. REPAIRED CRACKED FRAME IAW B737-400 SRM 53-00-07. (M) 2L72 4F RTA16WE 20060329001322006032900132NM 2006 3 29 ASAA0540601 120051103A52306546921169 FRAME BOEING737 7374Q8 138447QNM CARGO DOOR SCRATCHED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - FOUND SCRATCH IN FORWARD CARGO DOOR SIDE FRAME. REPLACED FRAME PER B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060329001332006032900133NM 2006 3 29 ASAA0540631 120051108A53156545808260 FLOORBEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND FLOORBEAM CORRODED. REMOVED, FABRICATED AND INSTALLED FLOORBEAM IAW B737-400 SRM 53-10-51 REPAIR 5. (M) 2L72 4F RTA16WE 20060329001342006032900134NM 2006 3 29 ASAA0540609 120051103A5320 WEB BOEING737 7374Q8 138447QNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - WEB HAS ELONGATED HOLES AT BS 344 TO 360, WL 208, RBL 65. REMOVED DAMAGED SECTION OF WEB, REPAIRED AND INSTALLED NEW SECTION PER B737-400 SRM 51-20-13 FIGURE 1. (M) 2L72 4F RTA16WE 20060329001352006032900135NM 2006 3 29 ASAA0540610 120051108A531069412281011 STOP FITTING BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND AFT ENTRY DOORSILL AREA DOOR STOP PAD FITTINGS CORRODED. REMOVED AND REPLACED PER B737-400 SRM 51-40-02, AND DWG 65-52878. (M) 2L72 4F RTA16WE 20060329001362006032900136NM 2006 3 29 ASAA0540616 120051102A53116545805237 FRAME BOEING737 737490 1384715NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02794AS 28889 OKC - FOUND BS 277 FRAME WEB DAMAGED AT BS 17-18 LEFT DOUBLER REPAIR. REMOVED DAMAGED SECTION OF WEB, FABRICATED AND INSTALLED REPAIR ANGLE IAW ASA EA 5310-02511. (M) 2L72 4F RTA16WE 20060329001372006032900137NM 2006 3 29 ASAA0540602 120051107A5320 STRUCTURE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - FOUND CORROSION AROUND FASTENER AT BS 631, RBL 1, BETWEEN STRINGER 28 RT AND 28 LEFT. PERFORMED BUTT SPLICE STRAP REPAIR PER ASA EA 5310-02516. (M) 2L72 4F RTA16WE 20060329001522006032900152NM 2006 3 29 ASAA0540620 120051108A2560656161219 SUPPORT BOEING737 7374Q8 138447QNM GIRT BAR CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND CORROSION ON L1 DOOR GIRT BAR FITTING SUPPORT. REMOVED AND REPLACED IAW B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060329001532006032900153NM 2006 3 29 ASAA0540615 120051102A533065C338151 REPAIR BOEING737 737490 1384715NM FUSELAGE UNKNOWN A ASAAK NONE O OTHER ININSP/MAINT 1 NM02794AS 28889 OKC - FOUND INTERIM EXTERNAL DOUBLER REPAIR PREVIOUSLY INSTALLED AT BS 279, STRINGER 17-18 LEFT. REMOVED INTERIM REPAIR, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW ASA EA 5310-02513. (M) 2L72 4F RTA16WE 20060329001542006032900154NM 2006 3 29 ASAA0540617 120051102A572065C300361 STIFFENER BOEING737 737490 1384715NM WING DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02794AS 28889 OKC - FOUND DURING ACCOMPLISHMENT OF EO 5710-01108, 1 FASTENER HOLE COMMON TO LBL 6.15 STIFFENER WAS OVERSIZED BEYOND ALLOWABLE DIAMETER TO REMOVED DAMAGE. REAMED HOLE TO .388/.391 DIAMETER, INSTALLED FASTENER IAW ASA EA 5710-01123. (M) 2L72 4F RTA16WE 20060329001552006032900155NM 2006 3 29 ASAA0540608 120051103A5320654587528 WEB BOEING737 7374Q8 138447QNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND WEB HAS ELONGATED HOLES AT BS 332, WL 208, RBL 65. REMOVED DAMAGED SECTION, REPAIRED PER B737-400 SRM 51-70-13. (M) 2L72 4F RTA16WE 20060329001562006032900156NM 2006 3 29 ASAA0540611 120051104A5315654581094 FLOORBEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02775AS 25108 YXX - FOUND CORROSION ON FLOORBEAM AT BS 312, LBL 12-50. DAMAGED SECTION OF FLOORBEAM REPLACED PER B737-400 SRM 53-10-51 FIG 201. (M) 2L72 4F RTA16WE 20060329001572006032900157NM 2006 3 29 ASAA0540613 120051104A533065C329541 SKIN BOEING737 7374Q8 138447QNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 OKC - FOUND FUSELAGE SKIN DENTED OUT OF LIMITS ON EITHER SIDE OF STRINGER 27 LEFT AT BS 853-855. DAMAGE IS ADJACENT TO AN EXISTING REPAIR AT BS 837-850 STRINGER 226 RT-27 RT. REMOVED DAMAGED AREA OF SKIN, REMOVED EXISTING REPAIR DOUBLER. FABRICATED AND INSTALLED A REPAIR DOUBLER, TRIPLER AND FILLER IAW B737-400 SRM 53-00-01, FIG 201, AND REPAIR 31. (M) 2L72 4F RTA16WE 20060329001582006032900158NM 2006 3 29 ASAA0540605 120051105A5311654657959 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND CORROSION AT APU COMPARTMENT LOWER CHORD FOR AIR INLET IS CORRODED AT BS 1118 TO 1125, RBL 20. REMOVED AND REPLACED PER B737-400 SRM 51-40-02 AND DWG 65-46579. (M) 2L72 4F RTA16WE 20060329001592006032900159NM 2006 3 29 ASAA0540713 120051202A5311654653141 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 FOUND FRAME CHAFED AT BS 500E, STRINGER 20 LEFT, WL 188. FOUND OUT OF LIMITS, REPAIRED IAW B737-400 SRM 51-70-11. (M) 2L72 4F RTA16WE 20060425001152006042500115NM 2006 4 25 ASAA0540626 120051108A5320654587547 SHEAR WEB BOEING737 7374Q8 138447QNM BS 294-328 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND CORROSION ON SHEAR WEB. REMOVED AND REPLACED IAW B737-400 SRM 51-40-02 AND DWG 65-45875. 2L72 4F RTA16WE 20060329001602006032900160NM 2006 3 29 ASAA0540698 120051201A5347MFAB53STR016 SEAT TRACK BOEING737 737490 1384715NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02795AS 28890 PAE - MECHANICAL DAMAGE ON MAIN CABIN SEAT TRACK. REMOVED AND REPLACED SEAT TRACK IAW B737-400 SRM 53-00-52. (M) 2L72 4F RTA16WE 20060329001772006032900177NM 2006 3 29 ASAA0540703 120051205A53226546543 SHEAR TIE BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02795AS 28890 PAE - FOUND CORROSION ON FORWARD CARGO FRAME SHEAR TIE. REMOVED DAMAGED SHEAR TIE, FABRICATED AND INSTALLED NEW SHEAR TIE IAW B737-400 SRM 53-00-07. (M) 2L72 4F RTA16WE 20060329001622006032900162EA 2006 3 29 ASOA051149 120051224A7830 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A ASOAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27924EV 7830 DURING CLIMB-OUT FROM ATW-ATL, AT APPROXIMATELY 20,000 FEET, THE CREW RECEIVED A RIGHT REVERSER UNLOCKED CAUTION MESSAGE. THE CREW COMPLIED WITH THE QRH AND DECLARED AN EMERGENCY. THE AIRCRAFT RETURNED TO ATW, WHERE IT LANDED SAFELY. MAINTENANCE PERFORMED OPERATIONAL TESTS OF THRUST REVERSER SYSTEM IAW CRJ-200 AMM 71-00-00-710-806. NO DEFECTS WERE NOTED. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060329001632006032900163EA 2006 3 29 ASOA051147 120051224A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA EXTERIOR INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27832AS 7243 DURING A GROUND INSPECTION IN CAE, THE FORWARD RIGHT SIDE EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE FORWARD RIGHT SIDE EXTERIOR EMERGENCY LIGHT ASSEMBLY. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060329001642006032900164NM 2006 3 29 ASAA0540629 120051108A5320 INTERCOSTAL BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 FOUND INTERCOSTAL ANGLE CORRODED AT BS 925-987, FOUND TO BE CRACKED ALSO AT THE FASTENER HOLE. REPLACED INTERCOSTAL IAW B737-400 SRM 53-60-51 AND 51-40-06. (M) 2L72 4F RTA16WE 20060329001652006032900165NM 2006 3 29 ASAA0540635 120051108A531165C37762 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - FOUND FRAME CRACKED AT FORWARD ENTRY DOOR LOWER STOP PAD FITTING. REMOVED DAMAGED SECTION OF FRAME. FABRICATED AND INSTALLED NEW FRAME, FITTINGS, REPAIR PARTS, AND INSTALLED IAW ASA EA 5310-02518. (M) 2L72 4F RTA16WE 20060329001662006032900166NM 2006 3 29 ASAA0540657 120051114A5311654655935 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND CORROSION AFT CARGO BAY, FRAME LOWER CHORD. CORROSION OUT OF LIMITS, FABRICATED AND INSTALLED NEW SHEAR TIE FRAME PER B737-400 SRM 53-00-07. (M) 2L72 4F RTA16WE 20060329001672006032900167NM 2006 3 29 ASAA0540699 120051201A53306548240504 SKIN BOEING737 737490 1384715NM FUSELAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02795AS 28890 PAE - FOUND RIGHT SKIN CHAFED AT LOWER AFT HORIZONTAL STAB FITTING. REMOVED DAMAGED SKIN, FABRICATED NEW SKIN AND INSTALLED IAW B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060329001682006032900168NM 2006 3 29 ASAA0540701 120051204A53306545800219 SKIN BOEING737 737490 1384715NM FUSELAGE LIGHTNING STRIKEA ASAAK NONE O OTHER ININSP/MAINT 1 NM02788AS 28885 PAE - FOUND LIGHTNING STRIKE AT BS 249 STRINGER 4L. REMOVED BLIND FASTENER AND INSTALLED SOLID FASTENER IAW B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060329001692006032900169NM 2006 3 29 ASAA0540633 120051108A533065458001318 SKIN BOEING737 7374Q8 138447QNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 FOUND FUSELAGE SKIN DENT OUT OF LIMITS AT BS 246, 5 INCHES BELOW AND 5 INCHES AFT OF THE EXTERNAL POWER RECEPTACLE. CUT OUT DAMAGED AREA OF SKIN, FABRICATED AND INSTALLED A REPAIR DOUBLER, TRIPLER AND FILLER IAW B737-400 SRM 53-00-01 FIGURE 201 REPAIR 31 AND ASA EA 5330-02018. (M) 2L72 4F RTA16WE 20060329001702006032900170NM 2006 3 29 ASAA0540634 120051108A533065C3235720 SKIN BOEING737 7374Q8 138447QNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 OKC - FUSELAGE SKIN DENTED IN FIVE LOCATIONS BETWEEN BS 360-368, AT STRINGER 16-18 LEFT. CUT OUT DAMAGED AREA OF SKIN, FABRICATED AND INSTALLED A REPAIR DOUBLER, TRIPLER AND FILLER IAW ASA EA 5330-02022. (M) 2L72 4F RTA16WE 20060329001712006032900171NM 2006 3 29 ASAA0540658 120051114A531565C339501 FLOORBEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND CORROSION AROUND FASTENER HOLES IN FLOORBEAM UPPER CHORD AT BS 986, RLB 24 TO LBL 44, WL 208. REPAIRED PER B737-400 SRM 53-60-51 AND EA 5310-0251. (M) 2L72 4F RTA16WE 20060329001722006032900172EA 2006 3 29 ASOA051153 120051225A5260601R3198055 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27871AS 7537 DURING A GROUND INSPECTION IN MCO, THE PASSENGER DOOR BOTTOM STEP WAS FOUND TO BE BROKEN. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060329001732006032900173EA 2006 3 29 ASOA051144 120051223A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27838AS 7276 DURING A GROUND INSPECTION IN CAE, THE AFT CEILING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE AFT CEILING EMERGENCY LIGHTS. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060329001742006032900174NM 2006 3 29 ASAA0540702 120051205A53206552878125 SILL BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02795AS 28890 PAE - FOUND CORROSION ON AFT ENTRY DOOR MOPSILL. REMOVED AND REPLACED MOPSILL IAW B737-400 SRM 53-60-15. (M) 2L72 4F RTA16WE 20060329001752006032900175NM 2006 3 29 ASAA0540707 120050508A5330 SKIN BOEING727 727200 138407ENM FUSELAGE OUT OF LIMITS A FDEAK NONE O OTHER ININSP/MAINT 1 SO25493FE 21531 N01804 WHILE WORKING N01403. BLENDED EXTERNAL SKIN BTWN BS979 TO BS983 BELOW AND AT STR 25LT. REMAINING MATERIAL FOUND TO BE OUT OF LIMITS. REPARIED SKIN PER SRM 53-30-3 FIG 3. 2L73 4F RTA3WE 20060330001512006033000151EA 2006 3 30 MASA200500636 120050812A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07651ML 7139 DURING PREFLIGHT, CABIN CEILING EMERGENCY FLOOD LIGHTS NR 1 AND NR 3 WERE INOP. MX REPLACED THE BULBS. 2L72 4F RTA21EA 20060330001532006033000153EA 2006 3 30 MASA200500646 120050815A3350316 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0775998 7336 CEILING EMERGENCY FLOOD LIGHT INOP. MAINTENANCE RELAMPED. 2L72 4F RTA21EA 20060330001542006033000154EA 2006 3 30 MASA200500647 120050815A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0717358 7358 REPORTED THAT NUMEROUS FLOOR EXIT LIGHT STRIPS INOP. MAINTENANCE COULD NOT DUPLICATE, OPS CHECKED GOOD. 2L72 4F RTA21EA 20060330002082006033000208EA 2006 3 30 MASA200501036 120051215A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07652ML 7036 ASH 7173 PWM - CEILING EMERGENCY LIGHTS INOP. CONTRACT MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE LIGHTS. OPS CHECKED GOOD. 2L72 4F RTA21EA 20060330002092006033000209EA 2006 3 30 MASA200501037 120051215A32304622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG FAULTY A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07472028492 7202 ASH 7178 CLT - GEAR DISAGREE. NOSE INDICATION SHOWED RED. MX REMOVED AND REPLACED PRIORITY VALVE, PSEU PROX SENSOR, UPLOCK ASSEMBLY AND SERVICED STRUT. 2L72 4F RTA21EA 20060330002102006033000210EA 2006 3 30 MASA200501044 120051216A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN UNSECURE A MASAK NONE L NO TEST NRNOT REPORTED 1 SW0775993 7372 ASH 7160 IAD - PASSENGER DOOR FLOOR LEVEL EMERGENCY FLOOD LIGHT INOP. MAINTENANCE RESECURED LAMP. 2L72 4F RTA21EA 20060330002202006033000220EA 2006 3 30 MASA200500852 120051102A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07652ML 7036 CREW REPORTED EMERGENCY EXIT FLOOD LIGHTS INOP. MX PLACED THIS ITEM ON MEL. MX RELAMPED. 2L72 4F RTA21EA 20060330002212006033000221EA 2006 3 30 MASA200500858 120051105A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0727173 7173 DURING RON IN CAE, THE CREW FOUND THE RT AFT EXTERIOR EMERGENCY LIGHT NOT ILLUMINATING. MAINTENANCE REPLACED THE LIGHT BULB. 2L72 4F RTA21EA 20060330002222006033000222EA 2006 3 30 MASA200500860 120051105A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0727191 7191 EMERGENCY FLOOR TRACK LIGHTING INOP AT ONE ROW. MAINTENANCE REMOVED AND REPLACED LAMP. 2L72 4F RTA21EA 20060330002232006033000223EA 2006 3 30 MASA200500863 120051107A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07651ML 7139 DURING RON, THE CREW FOUND THE RT AFT EXTERIOR EMERGENCY LIGHT NOT ILLUMINATING. MX REPLACED THE LIGHT BULB. 2L72 4F RTA21EA 20060330002242006033000224EA 2006 3 30 MASA200500876 120051112A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0727173 7173 DURING RON IN CLT, THE CREW NOTED THAT THE RT AFT EXTERIOR EMERGENCY LIGHT NOT ILLUMINATING. MAINTENANCE REPLACED THE LIGHT BULB. 2L72 4F RTA21EA 20060330002252006033000225EA 2006 3 30 MASA200500879 120051112A3350 LENS CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT MISSING A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0775998 7336 DURING RON IN BNA, THE CREW NOTED THE FLOOR LEVEL EMERGENCY FLOOD LIGHT LENS MISSING. MAINTENANCE REMOVED AND REPLACED LENS COVER. 2L72 4F RTA21EA 20060330002262006033000226EA 2006 3 30 MASA200500882 120051114A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0775996 7357 OVERHEAD CEILING EMERGENCY LIGHT INOP. MAINTENANCE REPLACED THE LAMP. 2L72 4F RTA21EA 20060329001182006032900118NM 2006 3 29 ASAA0540624 120051108A532265C229106 SHEAR TIE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND CORROSION ON SHEAR TIE. REPAIRED SHEAR TIE IAW B737-400 SRM 53-00-07. (M) 2L72 4F RTA16WE 20060330001552006033000155GL 2006 3 30 MASA200500653 120050817A3350 BATTERY DHAV DH82 DH82 2801000GL EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07445YV 445 THE CREW REPORTED THAT PART OF THE EMERGENCY LIGHTING SYSTEM REMAINING ON WHEN SELECTED OFF. MX RESET THE LOWER EMERGENCY BATTERY AND THE SYSTEM FUNCTIONED NORMALLY. 1Q71 3I EXPA1Q71 20060330001562006033000156EA 2006 3 30 MASA200500677 120050827A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07592ML 7410 THE TWO EXTERIOR EMERGENCY LIGHTS INOP RT SIDE AND LT SIDE. MX PLACED THE LIGHTS ON MEL. MX RELAMPED. 2L72 4F RTA21EA 20060330001572006033000157EA 2006 3 30 MASA200500678 120050827A3350316 LIGHT CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0775996 7357 FWD CABIN OVERHEAD EMERGENCY FLOOD EXIT LIGHT INOP. MX REPLACED THE LIGHT. 2L72 4F RTA21EA 20060330001582006033000158EA 2006 3 30 MASA200500699 120050905A49701495 BULB CNDAIRCL600 CL6002B19 1900309EA APU OIL TEMP MALFUNCTIONED A MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW077291Z 7291 DECLARED AN EMERGENCY IN BOUND TO PHX FOR AN APU HIGH OIL TEMPERATURE CAUTION MESSAGE. MX REMOVED AND REPLACED OIL TEMPERATURE BULB. 2L72 4F RTA21EA 20060330001602006033000160EA 2006 3 30 MASA200500731 120050915A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0775993 7372 REPORTED THE PAX DOOR EXIT LIGHT WAS DIM. MAINTENANCE REPLACED SEVERAL LAMPS IN THE EXIT LIGHT. 2L72 4F RTA21EA 20060330001622006033000162EA 2006 3 30 MASA200500732 120050915A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0775996 7357 EMERGENCY LIGHTS WILL NOT STAY ON WHEN TESTED. MX OPS CHECKED THE LIGHTS AND FOUND NO DEFECTS. 2L72 4F RTA21EA 20060330002532006033000253EA 2006 3 30 MASA200500889 120051115A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0787353 7353 FORWARD OVERHEAD EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED. 2L72 4F RTA21EA 20060330002542006033000254EA 2006 3 30 MASA200500902 120051116A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0777195 7195 LEFT OVERWING EMERGENCY EXIT LIGHT INOP. MAINTENANCE REPLACED THE LAMP. 2L72 4F RTA21EA 20060330002552006033000255EA 2006 3 30 MASA200500918 120051118A3350A1233A2 LENS CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT MISSING A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07514MJ 10116 EMERGENCY EXIT ROW SIGN MISSING RED BULB LENSE COVER. MAINTENANCE INSTALLED COVER. 2L72 4F RTA21EA 20060330002562006033000256EA 2006 3 30 MASA200500919 120051118A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN DISCONNECTED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0787353 7353 FWD EMERGENCY FLOOR ORANGE LIGHTING STRIP INOP. MAINTENANCE RE-CONNECTED THE FLOOR STRIP. 2L72 4F RTA21EA 20060330002582006033000258EA 2006 3 30 MASA200500920 120051119A3350 LENS CNDAIRCL600 CL6002D24 1390016EA EMERGENCY LIGHT MISSING A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07915FJ 15015 OVERHEAD EMERGENCY EXIT SIGN HAS RED AND WHITE LENS MISSING. MAINTENANCE INSTALLED THE LENS. 2L72 4F RTA21EA 20060330002602006033000260 2006 3 30 MASA200500334 420050505A22108220288001 CIRCUIT CARD CNDAIRCL600 CL6002B19 1900309EA MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07759988738 8738 7336 THE AIRCRAFT RETURNED TO THE FIELD DUE TO THE CAPTAINS SIDE PFD BLINKS OFF INTERMITTENTLY, YAW DAMP 1 INOP MESSAGE INTERMITTENT AND CAPTAIN AND F/O'S HDG SPLIT EFIS COMP MON. MAINTENANCE REPLACED THE ENVIRO CONTROL CARD. 2L72 4F RTA21EA 20060330002622006033000262 2006 3 30 MASA200501006 420051207A2210 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA NR 2 DCU LOOSE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0717175 7175 IAPS DEGRADED MSG. MAINTENANCE FOUND THE NR 2 DCU LOOSE AND RE-SECURED IT. 2L72 4F RTA21EA 20060330002672006033000267EA 2006 3 30 MASA200501053 120051219A3350 SIGN CNDAIRCL600 CL6002B19 1900309EA CABIN BROKEN A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0717275 7275 EXIT SIGN NEAR MAIN CABIN DOOR WAS BROKEN. MAINTENANCE REPLACED THE SIGN AND OPS CHECKED THE LIGHTS. OPS CHECK GOOD. 2L72 4F RTA21EA 20060330002682006033000268EA 2006 3 30 MASA200501057 120051219A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0727173 7173 NR 1 CENTER CEILING LEVEL EMERGENCY FLOOD LIGHT INOPERATIVE. MAINTENANCE RELAMPED. 2L72 4F RTA21EA 20060330002692006033000269NM 2006 3 30 MASA200501058 120051219A3350 SIGN DHAV DHC8 DHC8202 2809007NM EMERGENCY EXIT LOOSE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07987HA 425 SEAT 1C EMERGENCY EXIT SIGN HANGING DOWN. MAINTENANCE RE-SECURED THE SIGN. 2H72 4T RTA13NM 20060330002702006033000270NM 2006 3 30 MASA200501059 120051219A3350 SWITCH DHAV DHC8 DHC8202 2809007NM EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07987HA 425 F/A EMERGENCY LIGHT SWITCH INOP. MAINTENANCE TROUBLESHOT AND COULD NOT DUPLICATE, OPS CHECK NORMAL. 2H72 4T RTA13NM 20060330002712006033000271EA 2006 3 30 MASA200501062 120051220A335066903 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0775987 7405 EMERGENCY ESCAPE PATH LIGHTING AND LOWER EMERGENCY EXIT SIGN INOP. MAINTENANCE REMOVED AND REPLACED LIGHTING STRIP. 2L72 4F RTA21EA 20060330002732006033000273EA 2006 3 30 MASA200501063 120051220A3397 WIRE CNDAIRCL600 CL6002D24 1390016EA EMERGENCY LIGHT FIRE A MASAO OTHER A FLAME/FIRE NRNOT REPORTED 1 SW07920FJ 15020 F/O'S SIDE FLOOD LIGHT WIRING FIRE. MAINTENANCE REMOVED AND REPLACED FLOOD LIGHT ASSEMBLY, OPS CHECKED GOOD. 2L72 4F RTA21EA 20060330002742006033000274EA 2006 3 30 MASA200501064 120051220A2800 UNKNOWN CNDAIRCL600 CL6002B19 1900309EA FUEL SYSTEM UNKNOWN A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0717358 7358 FUEL IMBALANCE OF 900 LBS ON T/O ROLL. OPS CHECKED GOOD. 2L72 4F RTA21EA 20060330002762006033000276EA 2006 3 30 MASA200501065 120051221A2560 ESCAPE ROPE CNDAIRCL600 CL6002B19 1900309EA COCKPIT UNSECURE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0775992 7401 EMERGENCY ESCAPE ROPE COVER WON'T STAY STOWED. MAINTENANCE RE-SECURED THE COVER. 2L72 4F RTA21EA 20060330002782006033000278EA 2006 3 30 MASA200501066 120051221A2750860D10018 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A MASAO OTHER O OTHER APAPPROACH 1 SW07273147354 7314 FLAP FAIL AT 8 DEG ON APPROACH. MAINTENANCE REPLACED THE FECU, LUBED FLEX SHAFTS AND C/W PART A AND B. 2L72 4F RTA21EA 20060330002802006033000280EA 2006 3 30 MASA200501067 120051221A3213 STRUT CNDAIRCL600 CL6002B19 1900309EA NLG LEAKING A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07593ML 7465 NOSE GEAR DISAGREE AFTER TAKEOFF UPON GEAR UP SELECTION. AIRCRAFT WAS FERRIED TO CLT. MAINTENANCE REPACKED NOSE STRUT. 2L72 4F RTA21EA 20060330002812006033000281EA 2006 3 30 MASA200501071 120051222A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCONNECTED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0727172 7172 ROW 9 FLOOR EXIT LIGHT INOP. MX RECONNECTED WIRE. 2L72 4F RTA21EA 20060330002832006033000283EA 2006 3 30 MASA200501084 120051226A33508GH00544828 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07650ML 7137 ROW 8 EMERGENCY EXIT LIGHT INOP. MAINTENANCE REPLACED LAMP. 2L72 4F RTA21EA 20060331000142006033100014NM 2006 3 31 ASAA0510055 120050411A532266221211 SHEAR TIE BOEING737 737290C 138448VNM BS 460 DAMAGED A ASAAK NONE W INADEQUATE Q C ININSP/MAINT 1 NM02730AS 22577 SHEAR TIE ANGLE BS 460 BETWEEN STR 20L AND 21L HAS LOW EDGE MARGIN AT FASTENER HOLE. REPAIRED IAW SRM. (K) 2L72 4F A16WE 20060331000152006033100015NM 2006 3 31 ASAA0510031 120050328A5320654659212 CHANNEL BOEING737 737290C 138448VNM BS 847 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 AFT CARGO PIT FLOOR SUPPORT CHANNEL ANCHOR NUT HOLES HAVE CORROSION AT BSTA 847=15, RBL 8. AFT CARGO PIT FLOOR SUPPORT CHANNEL ANCHOR NUT HOLES CORROSION AT BSTA 847=15, RBL 8 REPAIRED IAW SRM. (K) 2L72 4F A16WE 20060331000162006033100016NM 2006 3 31 ASAA0510033 120050329A53136552928595 STRINGER BOEING737 737290C 138448VNM BS 827 S24L CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 AFT CARGO PIT STR 24L HAS CORROSION FWD OF BST 827 FRAME. STRINGER 24L AT BS 827 CORROSION REPAIRED IAW SRM. (K) 2L72 4F A16WE 20060329000912006032900091EU 2006 3 29 U30A200600004 120051129A5210 SKIN AIRBUS320 A320212 3930322EU PAX DOOR DENTED A U30AK NONE O OTHER ININSP/MAINT 1 EA17265AV 427 PERMANENT REPAIR TO THE 1R PAX/CREW DOOR SKIN DENT AT FORWARD LOWER CORNER. REPAIRED UNDER EO 05-52-008, DATED 7 OCT 2005. WHICH INCORPORATES THE PERMANENT REPAIR DEFINITION PER AIRBUS SRM 52-10-00, PARA 5E ,FIG 205. REMOVED DAMAGED SKIN, FABRICATED EXTERNAL DOUBLER & SHIM (2024T3, 0.098 ALUMINUM). APPLIED PROTECTIVE TREATMENT PER SRM 51-23-00. APPLIED SEALANTS PER SRM 51-76-11. FAA FORM 337 HAS BEEN SUBMITTED. 2L72 4F RTA28NM 20060329001382006032900138NM 2006 3 29 ASAA0540704 120051202A53406935352Y1 STRINGER CLIP BOEING737 737490 1384715NM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02795AS 28890 PAE - FOUND AFT CARGO BAY STRINGER CLIP GOUGED. REMOVED AND REPLACED STRINGER CLIP IAW B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060329001392006032900139NM 2006 3 29 ASAA0540598 120051107A531165C3394027 REPAIR BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - PREVIOUS REPAIR CRACKED AT FRAME. REMOVED AND REPLACED REPAIR ANGLES PER ASA EA 5310-02517. (M) 2L72 4F RTA16WE 20060329001402006032900140NM 2006 3 29 ASAA0540600 120051103A53306545800219 SKIN BOEING737 7374Q8 138447QNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - FOUND DENT IN FUSELAGE SKIN. REPLACED SKIN PER ASA EA 5330-02014. (M) 2L72 4F RTA16WE 20060329001412006032900141NM 2006 3 29 ASAA0540604 120051105A53116546579619 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND CORROSION AT APU COMPARTMENT UPPER CHORD FOR AIR INLET IS CORRODED AT BS 1122, RBL 11, WL 214. REMOVED AND REPLACED PER B737-400 SRM 51-40-02 AND DWG 656-46579. (M) 2L72 4F RTA16WE 20060329001422006032900142NM 2006 3 29 ASAA0540710 120051205A256065C161215 MOUNT BOEING737 737490 1384715NM GIRT BAR CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02796AS 28891 OKC - FOUND L1 DOOR GIRT BAR RETAINER MOUNTS CORRODED. REMOVED AND REPLACED MOUNTS IAW B737-400 SRM 51-40-05. (M) 2L72 4F RTA16WE 20060329001432006032900143NM 2006 3 29 ASAA0540715 120051202A53226546593 SHEAR TIE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND CORROSION ON SHEAR TIE. FOUND OUT OF LIMITS, REPAIRED IAW B737-400 SRM 53-00-07 FIG 201. (M) 2L72 4F RTA16WE 20060329001442006032900144NM 2006 3 29 ASAA0540718 120051130A5311654655039 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND CORROSION ON LOWER FRAME CHORD. FOUND OUT OF LIMITS, REPAIRED PER B737-400 SRM 53-00-07, REPAIR 5. (M) 2L72 4F RTA16WE 20060329001452006032900145NM 2006 3 29 ASAA0540719 120051201A533065C32359 SKIN BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND CORROSION ON SKIN UNDER KEEL BEAM. FOUND OUT OF LIMITS, REPAIRED PER ASA EA 5310-01045. (M) 2L72 4F RTA16WE 20060329001462006032900146NM 2006 3 29 ASAA0540712 120051203A5320 STRUCTURE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 FOUND CORROSION AT BS 500G-500G PLUS 8 INCHES, RBL 7, WL 148.5. REPAIRED IAW ASA EA 5360-01047. (M) 2L72 4F RTA16WE 20060329001472006032900147NM 2006 3 29 ASAA0540714 120051202A531165C325523 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND CORROSION ON FRAME. FOUND OUT OF LIMITS, REPAIRED IAW B737-400 SRM 53-00-07. (M) 2L72 4F RTA16WE 20060329001482006032900148NM 2006 3 29 ASAA0540708 120051203A532065C807351 SILL BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02796AS 28891 OKC - FOUND R-2 DOOR MOPSILL CORRODED. REMOVED AND REPLACED MOPSILL IAW B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060329001492006032900149NM 2006 3 29 ASAA0540612 120051104A5330 SKIN BOEING737 7374Q8 138447QNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 OKC - FUSELAGE SKIN EXTERIOR DAMAGE REMOVAL OUT OF LIMITS AT BS 868, 1 INCH BELOW STRINGER 21 RT. CUT OUT DAMAGED AREA OF SKIN, FABRICATED AND INSTALLED A REPAIR DOUBLER, TRIPLER, AND FILLERS PER B737-400 SRM 53-00-01, FIG 201, AND REPAIR 31. (M) 2L72 4F RTA16WE 20060329001502006032900150NM 2006 3 29 ASAA0540606 120051103A5330 DOUBLER BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND CORROSION ON SKIN DOUBLER FOR BODY DRAIN AT BS 500C- 500C PLUS 5 INCHES. REMOVED AND REPLACED DOUBLER PER B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060329001512006032900151NM 2006 3 29 ASAA0540607 120051103A5330 DOUBLER BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND CORROSION ON SKIN DOUBLER FOR BODY DRAIN AT BS 500-500A PLUS 5 INCHES. REMOVED AND REPLACED DOUBLER PER B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060329001612006032900161EA 2006 3 29 ASOA051146 120051223A1100S1868 PLACARD CNDAIRCL600 CL6002B19 1900309EA PAX DOOR FADED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27974EV 7594 DURING A HANGAR INSPECTION IN MCN, THE PASSENGER DOOR EXIT PLACARD WAS FOUND TO NEED REPLACING. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EXIT PLACARD. (M) 2L72 4F RTA21EA 20060331000542006033100054NM 2006 3 31 ASAA0570001 120050113A5100 REPAIR BOEING737 737790 13844CNNM SCHEDULED MAINT A ASAAK NONE O OTHER ININSP/MAINT 1 NM02627AS 30794 DURING MAINTENANCE CHECK FOUND TEMP REPAIR AT BS 394. INSTALLED PERMANENT REPAIR IAW SRM. (K) 2L72 4F RTA16WE 20060331000582006033100058NM 2006 3 31 ASAA0540191 120050319A275069466487 TORQUE TUBE BOEING737 7374Q8 138447QNM FLAP DRIVE WORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 TORQUE TUBE JUST IB OF NR 1 ENGINE PYLON WORN, FLAP DRIVE TORQUE TUBE AT FLOATING SEAL ASSEMBLY WBL 182. REMOVED AND REPLACED TORQUE TUBE JUST IB IF NR 1 ENGINE PYLON PER AMM. (K) 2L72 4F RTA16WE 20060331000602006033100060NM 2006 3 31 ASAA0510054 120050411A532266221611 SHEAR TIE BOEING737 737290C 138448VNM BS 480 S20-21L DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 BSTA 480 BETWEEN STR 20L AND 21L SHEAR TIE ANGLE HAS LOW EDGE MARGIN. REPLACED ANGLE IAW SRM. (K) 2L72 4F A16WE 20060331000762006033100076NM 2006 3 31 AALA20060132 120051222A3397BACC63CB83SN CONNECTOR BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21761AJ 31478 AFW - LEFT HAND NUMBER THREE DOOR (STATION 1522) EMERGENCY ESCAPE LIGHT INOPERATIVE. REPLACED EMERGENCY ESCAPE LIGHT SQUIBB CONNECTOR AT LEFT NUMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20060331000772006033100077EA 2006 3 31 MASA200500999 120051205A3350110049 CHARGER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW077728613271 7286 UPPER AFT CABIN EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED BATTERY CHARGER. 2L72 4F RTA21EA 20060331000812006033100081EA 2006 3 31 MASA200501018 120051209A3397 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT UNSECURE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07591ML 7388 FORWARD FACING EXIT SIGN IN CABIN INOPERATIVE. MAINTENANCE SECURED THE CONNECTION AT THE EMERGENCY LIGHT POWER SUPPLY. 2L72 4F RTA21EA 20060331000822006033100082EA 2006 3 31 MASA200501020 120051210A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0737208 7208 LEFT AFT OVERWING EMERGENCY LIGHT INOP. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. 2L72 4F RTA21EA 20060331000832006033100083EA 2006 3 31 MASA200501025 120051210A2560 GLOWSTRIP CNDAIRCL600 CL6002D24 1390016EA CABIN LOOSE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07911FJ 15011 PHOTO ILLUMINESCENT STRIP AT SERVICE DOOR LOOSE. MAINTENANCE RE-SECURED STRIP. 2L72 4F RTA21EA 20060331000882006033100088NM 2006 3 31 AALA2060133 120051220A5344418W10153412A HINGE BOEING777 777223 1385213NM PSU DOOR INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21761AJ 31478 AFW - PASSENGER SERVICE UNIT OXYGEN BOX AT SEAT ROW 9JH INOPERATIVE. REPLACED OXYGEN DOOR HINGE AT SEAT 9JH. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20060331000932006033100093 2006 3 31 MASA200500504 420050630A3414WL102AMS5 INDICATOR CNDAIRCL600 CL6002B19 1900309EA STNDBY AIRSPEED FAILED A MASAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 SW07759939929 7372 ABORTED TAKEOFF DUE TO A STANDBY AIRSPEED INDICATOR FAILED. MAINTENANCE REPLACED THE INDICATOR. 2L72 4F RTA21EA 20060331000942006033100094 2006 3 31 MASA200500555 420050716A3414WL102AMS5 INDICATOR CNDAIRCL600 CL6002B19 1900309EA STNDBY AIRSPEED INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07759938445 7372 ABORTED TAKEOFF FOR STAND BY AIRSPEED INDICATOR INOP. MX REMOVED AND REPLACED AIRSPEED INDICATOR. 2L72 4F RTA21EA 20060331000952006033100095 2006 3 31 MASA200500609 420050801A3414WL102AMS5 INDICATOR CNDAIRCL600 CL6002B19 1900309EA STNDBY AIRSPEED INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07759997850 7471 STANDBY AIRSPEED INDICATOR READING ZERO AT 80 KTS. MX R2 STANDBY AIRSPEED IND. 2L72 4F RTA21EA 20060331000962006033100096EA 2006 3 31 MASA200500901 120051116A27604916405 ECU CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A MASAO OTHER J WARNING INDICATION APAPPROACH 1 SW07773023845 7302 UNSAFE CAUTION ON LANDING. MAINTENANCE REMOVED AND REPLACED THE NR 2 SFCU. 2L72 4F RTA21EA 20060331000972006033100097 2006 3 31 MASA200500928 420051121A3414WL102AMS5 INDICATOR CNDAIRCL600 CL6002B19 1900309EA STNDBY AIRSPEED INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07773318453 7331 STANDBY AIRSPEED INDICATOR STUCK AT ZERO. MAINTENANCE REPLACED THE INDICATOR. 2L72 4F RTA21EA 20060331001292006033100129 2006 3 31 MASA200501095 420051231A3100 DISPLAY CNDAIRCL600 CL6002B19 1900309EA COCKPIT FAILED A MASAO OTHER O OTHER CRCRUISE 1 SW0797325 7325 CAPTAINS MFD FAILED IN FLIGHT. MAINTENANCE SECURED THE MFD IN POSITION. 2L72 4F RTA21EA 20060331001422006033100142 2006 3 31 MASA200500962 420051126A2340 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA INTERPHONE MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07509MJ 10094 FORE & AFT CABIN EMERGENCY CALL ANNUNCIATOR AURAL MESSAGE/TONE. MAINTENANCE RESET THE INTERPHONE CONTROL UNIT AND THE SYSTEM OPS CHECKED GOOD. 2L72 4F RTA21EA 20060331001512006033100151EA 2006 3 31 MASA200500530 120050708A339764643 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DAMAGED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07591ML 7388 OUT BOUND PILOT FOUND EMERGENCY FLOOR LIGHTS BETWEEN ROW 1 & 5 TO BE INOP. MX REPLACED CABLE ASSY & ACFT CONTINUED OPERATIONS. 2L72 4F RTA21EA 20060331001532006033100153EA 2006 3 31 MASA200500541 120050711A3350 BATTERY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCHARGED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0717275 7275 THE 1ST SECTION OF FLOOR EMERGENCY PROXIMITY LIGHTS INOP. MX CHARGED THE BATTERY AND THE LIGHTS OPERATED NORMALLY. A/C DEPARTED WITHOUT FURTHER INCIDENT. 2L72 4F RTA21EA 20060331001542006033100154EA 2006 3 31 MASA200500579 120050722A3350 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DAMAGED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07650ML 7137 SEVERAL SECTIONS OF FLOOR PATH LIGHTING INOP. REPAIRED WIRE. 2L72 4F RTA21EA 20060331001552006033100155EA 2006 3 31 MASA200500587 120050724A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0775996 7357 CENTER CEILING EMERGENCY FLOOD LIGHT INOP. MAINTENANCE REPLACED LAMP. 2L72 4F RTA21EA 20060331001572006033100157EA 2006 3 31 MASA200500625 120050808A3350 INVERTER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0717275 7275 THE 2ND THROUGH 5TH FLOOR PROXIMITY EMERGENCY LIGHT STRIPS INOP. CONTRACT MX RESET THE INVERTER AND THE LIGHTS OPERATED NORMALLY. A/C DEPARTED WITHOUT FURTHER INCIDENT. 2L72 4F RTA21EA 20060331001652006033100165EA 2006 3 31 MASA200500633 120050812A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07591ML 7388 THE EMERGENCY PATH LIGHTS AFT OF ROW 9 WERE NOT ILLUMINATED. MX REPOSITIONED THE LAST FLOOR STRIP AND OPS WERE NORMAL. 2L72 4F RTA21EA 20060331000492006033100049NM 2006 3 31 ASAA0540198 120050324A575565464524 SKIN BOEING737 7374Q8 138447QNM SPOILER PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02782AS 25113 NR 4 SPOILER HAS A HOLE PIERCED THROUGH. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW SRM. (K) 2L72 4F RTA16WE 20060331000592006033100059NM 2006 3 31 ASAA0510063 120050414A5330654576647 SKIN BOEING737 737290C 138448VNM BS 495 S13R CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 CRACK AT FASTENER, WINDOW 8R BSA 495R - LOWER AFT CORNER. CRACKED FASTENER HOLE AT WINDOW 8R BSTA 495 LOWER AFT CORNER REPAIRED IAW EA. (K) 2L72 4F A16WE 20060331000792006033100079NM 2006 3 31 MASA200501012 120051208A3350 LIGHT DHAV DHC8 DHC8202 2809007NM CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07987HA 425 SEVEN OF THE EMERGENCY FLOOR PATH LIGHTS WERE INOP. CND. OPS CHECK GOOD. 2H72 4T RTA13NM 20060331000922006033100092 2006 3 31 MASA200500501 420050628A3410WL102AMS5 INDICATOR CNDAIRCL600 CL6002B19 1900309EA STNDBY AIRSPEED FAILED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07759939929 7372 ABORTED TAKEOFF DUE TO STANDBY AIRSPEED INDICATOR READING 0. PILOT RETURN TO GATE AND DE-BOARDED. MX REMOVED AND REPLACED STANDBY AIRSPEED. 2L72 4F RTA21EA 20060331001332006033100133EA 2006 3 31 MASA200501098 120051231A33501317 BULB CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07510MJ 10101 MAIN CABIN DOOR EXIT SIGN 3 BULBS INOP. MAINTENANCE REPLACED THE LAMPS. 2L72 4F RTA21EA 20060331001412006033100141 2006 3 31 MASA200500854 420051103A31408221310102 DCU CNDAIRCL600 CL6002D24 1390016EA NR 1 MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07919FJ2157 15019 TAKEOFF CONFIG WARNING FOR AILERON. MAINTENANCE REMOVED AND REPLACED NR 1 DCU. 2L72 4F RTA21EA 20060331001502006033100150EA 2006 3 31 MASA200500475 120050618A335059257 INVERTER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0777331 7331 THE DOOR OPEN NORMAL. OP'S CHECK GOOD. MX REPLACED THE INVERTOR. OP'S CHECK GOOD. 2L72 4F RTA21EA 20060331001812006033100181NM 2006 3 31 ASAA0540669 120051118A5313654657959 STRINGER BOEING737 7374Q8 138447QNM BS 1123 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02775AS 25108 YXX - APU COMPARTMENT RIGHT TORQUE BOX STRINGER AT BS 1126 IS CORRODED. REPLACED STRINGER IAW B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060331001922006033100192NM 2006 3 31 1022200501 120051022A561060B1002818 WINDOW BOEING747 747200B NM COCKPIT CRACKED A OZYAK NONE O OTHER ININSP/MAINT 1 SO29535MC 21833 RIGHT FORWARD NR 1 WINDOW HAS DELAMINATION AND POSSIBLE CRACK. INSPECTED WINDOW, AND FOUND ACCEPTABLE FOR FLIGHT IAW MEL 56-1-1, NR 1 WINDOW OUTER GLASS PLY CRACKED ONLY, AND VISIBILITY THROUGH ASSOCIATED WINDSHIELD IS ACCEPTABLE, AND VISION IS NOT IMPAIRED ON REMAINING WINDSHIELD. AIRPLANE TO BE OPERATED FOR ONE TAKEOFF ONLY TO AN AIRPORT WHERE REPLACEMENT CAN BE MADE. REMOVED AND REPLACED WINDOW, AND RETURNED TO SERVICE. 1L74 4F RTA20WE 20060331002092006033100209NM 2006 3 31 2005UALA01245 120051106A4997D4016P WIRE BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE APU BURNED A UALAK NONE O OTHER ININSP/MAINT 1 WP29659UA56487 27114 EMPENNAGE INSIDE AT BS 1809 RT SIDE BELOW CENTER HORIZONTAL STAB FEEDER WIRE BUNDLES, INSULATION NOT SECURE, LOOSE ON APU FEEDER SPLICES AND FEEDER WIRES FOUND BURNT. *S/D* THE FEEDER WIRE, SPLICE AND CONNECTOR WERE REPLACED. 2L72 4F4 FRTA1NM E24NE 20060403000162006040300016NM 2006 4 3 MASA200500950 120051124A335025137751 LENS DHAV DHC8 DHC8202 2809007NM EMERGENCY LIGHT MISSING A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07988HA 426 LOWER EMERGENCY EXIT SIGN AT ROW 4A MISSING. REPLACED SIGN. 2H72 4T RTA13NM 20060403000282006040300028EA 2006 4 3 MASA200500951 120051125A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07651ML 7139 RIGHT MID-FUSELAGE OVERWING ESCAPE PATH LIGHTING BULB WAS BURNED OUT. MAINTENANCE REMOVED AND REPLACED LAMP. 2L72 4F RTA21EA 20060403000292006040300029EA 2006 4 3 MASA200500953 120051125A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0727172 7172 SECTION OF FLOOR PATH LIGHTING INOP. MAINTENANCE INSPECTED THE SYSTEM AND COULD NOT FIND ANY DEFECTS. 2L72 4F RTA21EA 20060403000302006040300030EA 2006 4 3 MASA200500965 120051124A335066903 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07715SF 7115 FLOOR EMERGENCY ESCAPE PATH LIGHTING RIGHT SIDE OF ACFT IS INOP. MAINTENANCE REPLACED NR 1 FLOOR LIGHT STRIP ON RIGHT SIDE. 2L72 4F RTA21EA 20060403000312006040300031EA 2006 4 3 MASA200500966 120051127A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0777302 7302 SEATS 11F AND 12F EMERGENCY WALL LIGHTS AND ROW 11 CEILING LIGHT INOP. MAINTENANCE RELAMPED AND OPS NORMAL. 2L72 4F RTA21EA 20060403000322006040300032EA 2006 4 3 MASA200500969 120051128A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07400MJ 7309 AFT CEILING LEVEL EMERGENCY FLOODLIGHT INOPERATIVE. MAINTENANCE RELAMPED THE LIGHT ASSEMBLY. 2L72 4F RTA21EA 20060403000332006040300033EA 2006 4 3 MASA200500970 120051128A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0727185 7185 CEILING LEVEL EMERGENCY FLOODLIGHT INOPERATIVE. MAINTENANCE RELAMPED. 2L72 4F RTA21EA 20060404000212006040400021EA 2006 4 4 MASA200500847 120051030A2612 FIRE WARNING CNDAIRCL600 CL6002C10 1390015EA CARGO BAY FALSE ACTIVATIONA MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW07502MJ7501 10050 ASH 7252 DEN - CARGO FIRE INDICATION. FLIGHT CREW DISCHARGED TWO CARGO FIRE EXTINGUSHERS. ACFT DIVERTED TO TUL AND MX FOUND IT TO BE ONLY AN INDICATION PROBLEM. ACFT WAS FERRIED TO CAE DUE TO PARTS AVAILABILITY AND THE FIRE BOTTLES AND SQUIBS WERE REPLACED. 2L72 4F RTA21EA 20060404000222006040400022EA 2006 4 4 MASA200500867 120051109A27515913163 DETECTOR CNDAIRCL600 CL6002C10 1390015EA TE FLAPS MALFUNCTIONED A MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW07501MJ7132 10047 ASH 7238 IAD - AIRSPEED LIMITER STUCK AT 230 KTS WITH FLAPS UP AND FLAP INDICATION REMAINED ON EICAS. MAINTENANCE REMOVED AND REPLACED BOTH RT INBD SKEW SENSORS AND LT BPSU. 2L72 4F RTA21EA 20060404000232006040400023EA 2006 4 4 MASA200500943 120051122A2760C13045BA04 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA SPOILERS MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07508MJ3834 10087 ASH 7133 IAD - OUTBOARD SPOILERON AND FLIGHT SPOILER CAUTION IN FLIGHT. REMOVED AND REPLACED SSCU NR 1. 2L72 4F RTA21EA 20060404000482006040400048EA 2006 4 4 MASA200500894 120051116A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0747202 7202 ASH 7247 ORD - FLAPS FAIL IN FLIGHT AT 4 DEGREES WHEN SELECTED TO 8 DEGREES ON EXTENSION. CONTRACT MAINTENANCE COMPLIED WITH PART A & B. 2L72 4F RTA21EA 20060404000492006040400049EA 2006 4 4 MASA200500914 120051117A5210601R3189325 PUSHROD CNDAIRCL600 CL6002B19 1900309EA PAX DOOR DAMAGED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0727172 7172 ASH 7146 BNA - PAX DOOR THAT WOULD NOT OPEN FROM THE INSIDE. MAINTENANCE REMOVED AND REPLACED PASSENGER DOOR INNER PUSH ROD. 2L72 4F RTA21EA 20060404000602006040400060EA 2006 4 4 MASA200500994 120051205A2621 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA FIRE BOTTLE LOOSE A MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW0777181 7181 ASH 7171 AVP - CARGO FIRE BOTTLE CAUTION MESSAGE IN FLIGHT. MAINTENANCE SECURED LOOSE CONNECTOR. 2L72 4F RTA21EA 20060331000182006033100018NM 2006 3 31 ASAA0540197 120050322A531565C3394311 FLOORBEAM BOEING737 7374Q8 138447QNM BS 344 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02782AS 25113 FLOORBEAM FORWARD UPPER TEE IS CORRODED AT BSTA 344 LBL 15. REMOVED DAMAGED (T) CHORD, FABRICATED AND INSTALLED A REPLACEMENT (T) CHORD IAW SRM. (K) 2L72 4F RTA16WE 20060331000612006033100061NM 2006 3 31 ASAA0510034 120050404A5320654516983 SPLICE BOEING737 737290C 138448VNM BS 907 S26L CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 AFT CARGO PIT BSTA 907, STR 26L SPLICE HAS CORROSION. AFT CARGO PIT BSTA 907 STR 26L SPLICE REPALCED WITH MADE PART IAW SRM. (K) 2L72 4F A16WE 20060331000682006033100068NM 2006 3 31 AALA20060129 120051212A3510 OXYGEN MASK BOEING767 767323 1385205NM COCKPIT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21396AN 29603 AFW - SECOND OBSERVER OXYGEN MASK REGULATOR INOPERATIVE. REPLACED SECOND OBSERVER OXYGEN MASK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20060331000782006033100078EA 2006 3 31 MASA200501003 120051206A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0775995 7361 RIGHT FORWARD EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE RELAMPED THE LIGHT. 2L72 4F RTA21EA 20060331000802006033100080EA 2006 3 31 MASA200501017 120051209A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0727172 7172 NR 3 CEILING EMERGENCY FLOODLIGHT INOPERATIVE. MAINTENANCE PLACED THE LIGHT ON MEL. MX RELAMPED. 2L72 4F RTA21EA 20060331001152006033100115EA 2006 3 31 MASA200500977 120051130A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0737228 7228 OVERHEAD EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED THE LIGHT. 2L72 4F RTA21EA 20060331001322006033100132EA 2006 3 31 MASA200501085 120051226A33508GH00544828 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07650ML 7137 AFT EMERGENCY EXIT LIGHT INOP. MAINTENANCE REPLACED LAMP. 2L72 4F RTA21EA 20060404000502006040400050EA 2006 4 4 MASA200500942 120051123A5210H341437 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR FAILED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07715SF 7115 ASH 2762 CLT - PAX DOOR WILL NOT OPEN. REPLACED LATCH. 2L72 4F RTA21EA 20060404000852006040400085EA 2006 4 4 MASA200500900 120051116A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA MAIN PAX STUCK A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0727172 7172 ASH 7299 ORD - PAX DOOR WILL NOT OPEN FROM INSIDE. CONTRACT MAINTENANCE REMOVED EXCESS GREASE. 2L72 4F RTA21EA 20060404001262006040400126NM 2006 4 4 UPS06246506 120051130A33501000677 LIGHT BOEING727 72725C 138400HNM COCKPIT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01932UP 19856 FLIGHT COMPARTMENT EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT ASSY REF AMM 33-50-00-0. OPS CK NORMAL. DISCOVERED UPON INVESTIGATION OF SELF DISCLOSURE. 2L73 4F A3WE 20060331000512006033100051NM 2006 3 31 ASAA0510065 120050414A531165672063 FRAME BOEING737 737290C 138448VNM BS 480 S22L CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 FWD CARGO FRAME AT BSTA 480 NEAR STR 22L CRACKED. FWD CARGO FRAME AT BSTA 480 NEAR STR 22L CRACKED FRAME REPAIRED IAW SRM. (K) 2L72 4F A16WE 20060331000552006033100055NM 2006 3 31 ASAA0570005 120050113A5320143A948535 ANGLE BOEING737 737790 13844CNNM BS 500D CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02627AS 30794 DURING MAINTENANCE CHECK FOUND CORRODION ON AFT LOWER BULKHEAD SUPPORT ANGLE AT BS 500D. REPAIR IAW SRM. (K) 2L72 4F RTA16WE 20060331000572006033100057NM 2006 3 31 ASAA0570014 120050121A5320146A81271 SUPPORT BOEING737 737790 13844CNNM BS 767-787 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02617AS 30542 DURING MAINTENANCE CHECK, FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT AT BS 767. REPAIR IAW SRM. (K) 2L72 4F RTA16WE 20060331001522006033100152EA 2006 3 31 MASA200500533 120050710A3350600592111 DIODE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0787353 7353 THE CAPTAIN REPORTED AN EMERGENCY EXIT CEILING LIGHT INOPERATIVE. MX REPLACED THE DIODE. 2L72 4F RTA21EA 20060331001562006033100156EA 2006 3 31 MASA200500605 120050730A3350316 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0787353 7353 PASSENGER DOOR EMERGENCY EXIT SIGN WILL NOT ILLUMINATE. MX FOUND LIGHT ASSY FAILED AND WAS REPLACED. NO FURTHER DEFECTS NOTED. 2L72 4F RTA21EA 20060331001582006033100158EA 2006 3 31 MASA200500626 120050809A3350 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT LOOSE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0717358 7358 AISLE EMERGENCY LIGHTS ROWS 2, 3, 4, 5 INOP. MAINTENANCE ADJUSTED THE CONNECTOR. 2L72 4F RTA21EA 20060403000342006040300034EA 2006 4 3 MASA200500972 120051129A33501607591 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DAMAGED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0717156 7156 FLOOR EMERGENCY ESCAPE LIGHT INOP. MAINTENANCE REPLACED CONNECTOR. 2L72 4F RTA21EA 20060404000202006040400020EA 2006 4 4 MASA200500839 120051029A5610NP13932111 WINDSHIELD CNDAIRCL600 CL6002C10 1390015EA COCKPIT FAILED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07515MJ4 10117 ASH 7245 ORD - CAPTAIN'S WINDSHIELD SHATTERED. MAINTENANCE REMOVED AND REPLACED WINDOW. 2L72 4F RTA21EA 20060404000652006040400065EA 2006 4 4 MASA200501039 120051215A5270 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY DOOR MALFUNCTIONED A MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW07571ML 7209 ASH 7201 BOS - L EMERGENCY DOOR CAUTION ILLUMINATED IN FLIGHT. MAINTENANCE ADJUSTED PROX SENSOR SYSTEM. OPS CHECKED GOOD. 2L72 4F RTA21EA 20060404000662006040400066EA 2006 4 4 MASA200501047 120051216A5210 TORQUE TUBE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR OUT OF ADJUST A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0727172 7172 ASH 7223 ORD. PAX DOOR WILL NOT LOCK FROM INSIDE. FERRIED TO YMX. MAINTENANCE HAS COMPLETED A FULL DOOR RIG. MAINTENANCE ADJUSTED THE TORQUE TUBE CAM. 2L72 4F RTA21EA 20060404001392006040400139EA 2006 4 4 MASA200500899 120051116A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW0747202 7202 ASH 7206 FWA - FLAPS FAIL CAUTION IN FLIGHT AT 20 DEGREES. MAINTENANCE COMPLIED WITH PART B. 2L72 4F RTA21EA 20060404001402006040400140EA 2006 4 4 MASA200500946 120051124A52105210838 LATCH CNDAIRCL600 CL6002B19 1900309EA PAX DOOR UNKNOWN A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07715SF 7115 ASH 2749 CLT - MAIN CABIN DOOR WILL NOT OPEN. MAINTENANCE REPLACED LATCH ASSEMBLY. 2L72 4F RTA21EA 20060404001412006040400141EA 2006 4 4 MASA200500948 120051124A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW0747202 7202 ASH 7010 ORD - FLAPS FAIL MASTER CAUTION. COMPLIED WITH PART A EARLIER AND PART B WAS COMPLIED WITH LATER. NO FURTHER DEFECT NOTED. 2L72 4F RTA21EA 20060404002342006040400234 2006 4 4 RTE2006F00001 420051215A611305502283 BULKHEAD CESSNA172 172C 2072408CE CONT O300 O300D 17022SO PROP SPINNER CRACKED E RTEAK NONE O OTHER ININSP/MAINT 1 NM018292X 17248792 24760D1D DURING ROUTINE SCHEDULED INSPECTION, FOUND FWD PROP SPINNER BULKHEAD CRACKED NEAR THE BOLT HOLES. NO APPARENT REASON COULD BE DETERMINED. THE PROP BOLTS WERE CORRECTLY TORQUED. THE PROP WAS CORRECTLY CLOCKED. GROUND AND FLIGHT CHECKS SHOWED NO ABNORMAL VIBRATION. (K) 1H71 3O3 ONT3A12 E253 20060404002352006040400235 2006 4 4 RTE2006F00002 420051215A611305503214 BULKHEAD CESSNA172 172N 2072434CE LYC O320 O320D2G 41508EA NEAR BOLT HOLES CRACKED E RTEAK NONE O OTHER ININSP/MAINT 1 NM01734QQ 17269034 DURING ROUTINE SCHEDULED INSPECTION. FOUND FWD PROP SPINNER BULKHEAD CRACKED NEAR THE BOLT HOLES. NO APPARENT REASON COULD BE DETERMINED. THE PROP BOLTS WERE CORRECTLY TORQUED. THE PROP WAS CORRECTLY CLOCKED. GROUND AND FLIGHT CHECKS SHOWED NO ABNORMAL VIBRATION. (K) 1H71 3O3 ONT3A12 E274 20060403001322006040300132NM 2006 4 3 2006UALA00570 120051202A3211 PIN BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE LT MLG FAILED A UALAK NONE O OTHER ININSP/MAINT 1 WP29673UA 29241 LEFT MAIN GEAR STRUT PIVOT PIN TO BOGIE SNAPPED. 2L72 4F4 FRTA1NM E24NE 20060403001582006040300158NM 2006 4 3 ASAA0510032 120050329A5320654577610 SPLICE BOEING737 737290C 138448VNM BS 907 S27L CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 AFT CARGO PIT STR SPLICE AT BSTA 907 STR 27L HAS CORROSION. AFT CARGO PIT STR SPLICE @ BSTA 907 27L, REPLACED WITH MADE REPAIR PART IAW SRM. (K) 2L72 4F A16WE 20060403001592006040300159SO 2006 4 3 MASA200500611 120050802A3350316 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07826MJ 145214 OVERHEAD EMERGENCY LIGHTS INOP. MX REPLACED THE LIGHT. 2L72 4T RTT00011AT 20060403001602006040300160NM 2006 4 3 ASAA0510060 120050412A2150 DUCT BOEING737 737290C 138448VNM NR2 AC PACK HEATRUPTURED A ASAAO OTHER B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 NM02740AS 22578 BRUNING RUBBER SMELL NOTED IN CABIN AND COCKPIT. SMELL DID NOT DISSIPATE FOR 8-9 MINUTES. FOUND RT PACK HEAT EXCHANGER EXHAUST DUCT BLOWN. REMOVED AND REPLACED DUCT. (K) 2L72 4F A16WE 20060404000612006040400061EA 2006 4 4 MASA200501000 120051205A2752853D10020 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A MASAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 SW07472025755 7202 ASH 7014 BUF - FLAPS FAIL IN FLIGHT. MAINTENANCE REPLACED NR 3 AND NR 4 RT FLAP ACTUATOR. 2L72 4F RTA21EA 20060405000342006040500034NM 2006 4 5 DHL2006752523 120051230A5320 INTERCOSTAL BOEING727 727223 1384074NM BS 1030-1050 BENT A DHLAK NONE O OTHER ININSP/MAINT 1 SO01752DH 22466 FOUND BENT INTERCOSTAL BS 1030-1050, STR 25R. REMOVED INTERCOSTAL AT STA 1030-1050 AT STR 25R IAW B727 SRM 51-30-2. FABRICATED FROM 2024-T3 .050 SIZE 22" BY 5" PO> 503081 IAW B727 SRM 51-40-3 AND SRM 53-10-1. TREATED AND PRIMED PARTS AND AREA IAW B727 SRM 51-10-2. INSTALLED INTERCOSTAL IAW B727 SRM 51-30-2. 2L73 4F A3WE 20060404000672006040400067EA 2006 4 4 MASA200500932 120051121A24103502 TRU CNDAIRCL600 CL6002D24 1390016EA SMOKE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07935LR663 15035 ASH 6443 PHX, SMOKE WAS COMING FROM THE NOSE AREA. MAINTENANCE REPLACED THE TRU. 2L72 4F RTA21EA 20060404000862006040400086EA 2006 4 4 MASA200500904 120051117A5297 WIRE CNDAIRCL600 CL6002B19 1900309EA DOOR SENSOR BROKEN A MASAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW07154SF 7154 ASH 7229 CAE - RETURNED TO THE FIELD DUE TO A PAX DOOR WARNING. MAINTENANCE FOUND AND REPAIRED A BROKEN WIRE ON THE SERVICE DOOR PROX SENSOR. 2L72 4F RTA21EA 20060404002412006040400241 2006 4 4 RTE2006F00000 420051215A611305503214 BULKHEAD CESSNA172 172M 2072418CE LYC O320 O320E2D 41508EA MCAULY1C160 1C160DTM GL PROP SPINNER CRACKED E RTEAK NONE O OTHER ININSP/MAINT 1 NM019379H1501 17266128 L2972927A G1024 DURING ROUTINE SCHEDULED INSPECTION. FOUND FWD PROP SPINNER BULKHEAD CRACKED NEAR THE BOLT HOLES. NO APPARENT REASON COULD BE DETERMINED, THE PROP BOLTS WERE CORRECTLY TORQUED. THE PROP WAS CORRECTLY CLOCKED. GROUND AND FLIGHT CHECKS SHOWED NO ABNORMAL VIBRATION. (K) 1H71 3O3 ONT3A12 E274 5 NP910 20060405000622006040500062EA 2006 4 5 SWIA200516393 120051224A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA BS 484 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07932SW 7714 FUSELAGE, PULLEY INTERCOSTAL HAS A CRACKED O/B ATTACH FLANGE FS 484.00, RBL 36.0. (ITEM FOUND AT C-CHECK INSPECTION.) DAMAGE REPAIRED IAW CRJ REO 601R-53-41-059 REV A. 2L72 4F RTA21EA 20060405000652006040500065EA 2006 4 5 SWIA200516396 120051224A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07932SW FUSELAGE, LOWER FLOORBEAM IS CRACKED, FS 280.0, LBL 11.0, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-11-171 REV C. 2L72 4F RTA21EA 20060405001232006040500123NM 2006 4 5 ASAA0540672 120051121A5311 FRAME BOEING737 7374Q8 138447QNM BS 867 MISDRILLED A ASAAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 NM02774AS 25107 PAE - FOUND MISDRILLED HOLE IN FRAME UPPER FLANGE RADIUS AT BS 867, RBL 22, WL 160. REPAIRED IAW B737-400 SRM 51-70-11. (M) 2L72 4F RTA16WE 20060405001522006040500152NM 2006 4 5 ASAA0540727 120051205A53226546594502 SHEAR TIE BOEING737 7374Q8 138447QNM FS 500B CORRODED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND CORROSION ON UPPER SURFACE OF SHEAR TIE AT FASTENER OUT OF LIMITS. REPAIRED SHEAR TIE PER SRM 53-00-07, AND 51-440-02. (M) 2L72 4F RTA16WE 20060405001562006040500156NM 2006 4 5 ASAA0540728 120051212A531165582801 FRAME BOEING737 737490 1384715NM FS 360 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02795AS 28890 PAE - FOUND CRACKED FRAME AT BIN RAIL SUPPORT BRACKET LEFT SIDE. REPAIRED FRAME AT BIN RAIL SUPPORT BRACKET PER SRM 53-00-07, REPAIR 1. (M) 2L72 4F RTA16WE 20060405001572006040500157NM 2006 4 5 ASAA0540732 120051210A53206552878102 SILL BOEING737 737490 1384715NM FS 915-1006 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02796AS 28891 OKC - FOUND L2 DOOR MOPSILL IS CORRODED. REMOVED AND REPLACED L2 DOOR MOPSILL PER B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060405001712006040500171NM 2006 4 5 ASAA0540678 120051129A532269366534 SHEAR TIE BOEING737 7374Q8 138447QNM FS 460 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND CORROSION ON BS 46, RBL 7 - RBL 10, WL 146 SHEAR TIE. REPAIRED SHEAR TIE IAW B737-400 SRM 53-00-02 REPAIR 4. (M) 2L72 4F RTA16WE 20060405001722006040500172NM 2006 4 5 ASAA0540682 120051129A5311 FRAME BOEING737 7374Q8 138447QNM BS 767 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND CORROSION ON LOWER FRAME CHORD AT BS 767, STRINGER 26R TO 27R. REPAIRED AND REPLACED IAW B737-400 SRM 53-00-07. (M) 2L72 4F RTA16WE 20060405001732006040500173NM 2006 4 5 ASAA0540688 120051122A5315 FLOORBEAM BOEING737 7374Q8 138447QNM BS 986 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02775AS 25108 YXX - FOUND FLOORBEAM AT BS 986.5 CORRODED AT CLIP NUT HOLES ALONG TOP SURFACE. REPAIRED FLOORBEAM IAW ASA EA 5310-02525 AND ERO 4999. (M0 2L72 4F RTA16WE 20060405001742006040500174NM 2006 4 5 ASAA0540691 120051120A53206517688175 SILL BOEING737 7374Q8 138447QNM FS 360 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02775AS 25108 YXX - FOUND L1 DOOR SILL CHORD CORRODED. REPLACED SILL CHORD IAW B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060405002002006040500200NM 2006 4 5 ASAA0540743 120051215A5322654659320 SHEAR TIE BOEING737 737490 1384715NM FS 500B CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02795AS 28890 PAE - FOUND CORROSION ON FORWARD CARGO FRAME SHEAR TIE. REMOVED DAMAGED SHEAR TIE, FABRICATED AND INSTALLED REPAIR TO FRAME SHEAR TIE IAW B737-400 SRM 53-00-07. (M) 2L72 4F RTA16WE 20060405002012006040500201NM 2006 4 5 ASAA0540742 120051216A532265C229099 SHEAR TIE BOEING737 737490 1384715NM FS 500C CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02795AS 28890 PAE - FOUND CORROSION ON FORWARD CARGO FRAME SHEAR TIE. REMOVED DAMAGED SHEAR TIE, FABRICATED AND INSTALLED REPAIR IAW ASA EA 5310-02545. (M) 2L72 4F RTA16WE 20060405002022006040500202NM 2006 4 5 ASAA0540685 120051120A531165582856 FRAME BOEING737 7374Q8 138447QNM FS 360 S8L CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02775AS 25108 YXX - FOUND CRACKED FRAME AT BS 360, STRINGER 8 LEFT. REPAIRED FRAME IAW B737-400 SRM 53-00-07 FIG 201. (M) 2L72 4F RTA16WE 20060405002032006040500203NM 2006 4 5 ASAA0540686 120051122A5712654544556 RIB BOEING737 7374Q8 138447QNM RT WING CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02775AS 25108 YXX - RIGHT WING FUEL TANK RIB AT WBL 135.5 CRACKED AT STRINGER 52. REPAIRED IAW ERO 5013, AND EA 5720-01283. (M) 2L72 4F RTA16WE 20060405002042006040500204NM 2006 4 5 ASAA0540690 120051120A5230654957510 HINGE BOEING737 7374Q8 138447QNM FS 450-480 CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02775AS 25108 YXX - FOUND FORWARD CARGO DOOR WEB ABOVE HINGE ARMS CHAFED. REPAIRED WEB IAW B737-400 SRM 51-70-13. (M) 2L72 4F RTA16WE 20060405002052006040500205NM 2006 4 5 ASAA0540746 120051215A531165465588 FRAME BOEING737 737490 1384715NM FS 907 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02795AS 28890 PAE - REJECTED ITEM FROM CARD 4963163. FRAME CRACKED AT BIN RAIL SUPPORT STATION 907 BETWEEN STRINGER 8R AND 9R. DAMAGE REMOVED EXCEEDS ALLOWABLE LIMITS IN B737-400 SRM 53-00-07 REPAIR 2, DETAIL 1. INSTALLED FRAME REPAIR AT BS 907 FRAME BETWEEN STRINGER 8R AND 9R PER B737-400 SRM 53-00-07 PAGE 201 FIG 2014, REPAIR 1. (M) 2L72 4F RTA16WE 20060405002072006040500207NM 2006 4 5 ASAA0540740 120051215A5322654659320 SHEAR TIE BOEING737 737490 1384715NM FS 440-500A CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02795AS 28890 PAE - FOUND CORROSION ON FORWARD CARGO FRAME SHEAR TIE. FOUND CORROSION OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR TO FRAME SHEAR TIE IAW B737-400 SRM 53-00-07. (M) 2L72 4F RTA16WE 20060405002082006040500208NM 2006 4 5 ASAA0540745 120051216A5322654655545 SHEAR TIE BOEING737 737490 1384715NM FS 867 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02795AS 28890 FOUND CORROSION AFT CARGO BAY SHEAR TIE. REMOVED DAMAGED SHEAR TIE, FABRICATED AND INSTALLED REPAIR PARTS IAW B737-400 SRM 53-00-07. 2L72 4F RTA16WE 20060405002092006040500209NM 2006 4 5 ASAA0540744 120051215A5311654652596 FRAME BOEING737 737490 1384715NM FS 380 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02795AS 28890 PAE - FOUND FRAME CRACKED AT BIN RAIL ATTACH CLIP. REMOVED CRACK IN FRAME, FABRICATED AND INSTALLED REPAIR PARTS IAW B737-400 SRM 53-00-07. (M) 2L72 4F RTA16WE 20060405002102006040500210NM 2006 4 5 ASAA0540741 120051216A5322654659320 SHEAR TIE BOEING737 737490 1384715NM FS 500D CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02795AS 28890 PAE - FOUND CORROSION ON FORWARD CARGO FRAME SHEAR TIE. REMOVED CORROSION, CUT OUT FRAME SHEAR TIE, FABRICATED AND INSTALLED REPAIR IAW B737-400 SRM 53-00-07 FIG 201, REPAIR 3. (M) 2L72 4F RTA16WE 20060405002192006040500219EA 2006 4 5 ASOA051161 120051229A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11860AS 7433 DURING A GROUND INSPECTION IN SHV, THE EMERGENCY FLOOR LIGHT STRIP, FROM ROW 9 TO THE LAVATORY, WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF EMERGENCY FLOOR LIGHT STRIP, FROM ROW 9 TO THE LAVATORY, WITH NO DEFECTS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060512000522006051200052NM 2006 5 12 ASAA0540720 120051201A53206553595501 SEAL DEPRESSOR BOEING737 7374Q8 138447QNM FS 304 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND FORWARD GALLEY DOOR CUTOUT, UPPER FORWARD CORNER, SEAL DEPRESSOR CRACKED. REPLACED SEAL DEPRESSOR PER B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060405000642006040500064EA 2006 4 5 SWIA200516395 120051224A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07932SW 7714 FUSELAGE, LOWER FLOORBEAM IS CRACKED, FS 280.00, RBL 11.0, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-11-171 REV C. 2L72 4F RTA21EA 20060405001932006040500193NM 2006 4 5 ASAA0540696 120051230A532065479573 THRESHOLD BOEING737 737490 1384715NM FS 794-847 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02795AS 28890 FOUND CORROSION AT AFT CARGO BAY DOOR CUTOUT LOWER THRESHOLD. REMOVED AND REPLACED LOWER THRESHOLD IAW B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060405001942006040500194NM 2006 4 5 ASAA0540697 120051201A5347MFAB53STR016 SEAT TRACK BOEING737 737490 1384715NM BS 540-727 GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02795AS 28890 PAE - FOUND MECHANICAL DAMAGE ON MAIN CABIN SEAT TRACK. REMOVED AND REPLACED SEAT TRACK IAW B737-400 SRM 53-00-52. (M) 2L72 4F RTA16WE 20060405001952006040500195NM 2006 4 5 ASAA0540695 120051130A5340 STRINGER CLIP BOEING737 737490 1384715NM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02795AS 28890 AFT CARGO BAY STRINGER CLIP GOUGED. REMOVED AND REPLACED STRINGER CLIP IAW B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060405001972006040500197NM 2006 4 5 ASAA0540747 120051216A533065C45772 SKIN BOEING737 737490 1384715NM FS 907-908 CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02795AS 28890 PAE - FOUND UPPER FUSELAGE SKIN CHAFED. REPAIRED DAMAGED SKIN BY ADDING DOUBLERS AND REPAIR STRAPS PER ASA EA 5330-02033. (M) 2L72 4F RTA16WE 20060405000632006040500063EA 2006 4 5 SWIA200516394 120051224A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA BS 484 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07932SW 7714 FUSELAGE, PULLEY INTERCOSTAL HAS A CRACKED O/B ATTACH FLANGE FS 484.00, LBL 36.0, ITEM FOUND AT C-CHECK INSPECTION. REPAIR CARRIED OUT IAW CRJ REO 601R-53-41-059 REV A, RII 53-401. 2L72 4F RTA21EA 20060405000662006040500066EA 2006 4 5 SWIA200516397 120051224A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07932SW 7714 FUSELAGE, UPPER FLOORBEAM IS CRACKED, FS 280.00, LBL 11.0. (ITEM FOUND AT C-CHECK INSPECTION.) REPAIRED IAW CRJ REO 601R-53-11-138 REV NC. 2L72 4F RTA21EA 20060405000672006040500067EA 2006 4 5 SWIA200516398 120051224A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA BS 625 S14L CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07932SW 7714 AFT EQUIPMENT COMP, INTERCOSTAL CLIP IS CRACKED, FS 625.0 STR 14L, ITEM FOUND AT C-CHECK INSPECTION. CLIP REPLACED IAW CRJ REO 601R-53-61-100 REV NC AND REO 601R-53-61-422 REV NC. 2L72 4F RTA21EA 20060406001862006040600186EA 2006 4 6 ASOA051098S 120051215A5320 SILL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 DURING C-CHECK, THE PASSENGER DOOR SILL WAS FOUND TO BE CORRODED. AFTER MAINTENANCE ALODINED, PRIMED, AND PAINTED THE PASSENGER DOOR SILL IAW SRM, IT WAS FOUND TO BE WITHIN ACCEPTABLE LIMITS. (K) 2L72 4F4 FRTA21EA E15NE 20060406001902006040600190WP 2006 4 6 ASAA0580557 120051212A5753593304943 VANE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE LT WING FLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 C-CHECK, LT WING NR 1 FLAP VANE IS DENTED. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLER AND DOUBLER. (K) 2L72 4F4 FRTA6WE E9NE 20060406002102006040600210WP 2006 4 6 ASAA0580555 120051212A57535930496509 VANE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE TE FLAP VANE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 C-CHECK, LT WING OB FLAP IB VANE IS GOUGED. BLENDED GOUGE. INSTALLED REPAIR DOUBLER. (K) 2L72 4F4 FRTA6WE E9NE 20060406002172006040600217WP 2006 4 6 ASAA0580551 120051212A5347993653473 TRACK DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE CABIN FLOOR CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 C-CHECK, CABIN FLOOR TRACK CORRODED. REPLACED FLOOR TRACK. (K) 2L72 4F4 FRTA6WE E9NE 20060407000462006040700046EA 2006 4 7 ASOA051036 120051129A5210H34149 HANDLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE LACK OF LUBE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27826AS 7207 7210 DURING A GROUND INSPECTION, THE PASSENGER DOOR WAS DIFFICULT TO OPEN. MAINTENANCE LUBRICATED THE PASSENGER DOOR HANDLE ROLLER CAM. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20060407000532006040700053NM 2006 4 7 ASAA0540205 120050330A532065C278121 DOUBLER BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02796AS 28891 CORROSION FOUND ON VHF NR 3 ANT. DOUBLER. REPLACED VHF NR 3 ANT. DOUBLER. (K) 2L72 4F RTA16WE 20060407000592006040700059WP 2006 4 7 AMTA200501158 120051214A3213 LUG LKHEED1011 10113853 5265020WP RROYCERB211 RB211524B4 54555NE LT MLG CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11163AT 1229 LT MAIN LANDING GEAR TRUNION FWD FITTING AFT LUG FWD FACE WITH PITTING CORROSION. REPAIR CARRIED OUT IAW SRM AND CADIUM PLATING CARRIED OUT IAW SRM. TREATED, PRIMED AND PAINTED PARTS AS REQUIRED IAW SRM. (K) 2L73 4F4 F A23WE E12EU 20060407000622006040700062NM 2006 4 7 ASAA0540666 120051118A53206552878U102 SILL BOEING737 7374Q8 138447QNM FS 947-996 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - FOUND CORROSION AT AFT ENTRY DOOR MOPSILL BS 947-996, LBL 52, WL 208 AND CRACKED AT BS 994. REMOVED AND REPLACED AFT ENTRY MOPSILL PER B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060407000632006040700063NM 2006 4 7 ASAA0540667 120051118A531565C3394824 FLOORBEAM BOEING737 7374Q8 138447QNM FS 947 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - FOUND FLOORBEAM CORRODED. REMOVED DAMAGED SECTION OF FLOORBEAM UPPER CHORD, FABRICATED REPAIR PARTS AND INSTALLED PER EA 5310-02515. (M) 2L72 4F RTA16WE 20060407000662006040700066NM 2006 4 7 ASAA0540723 120051205A532265C229097 SHEAR TIE BOEING737 7374Q8 138447QNM FS 500C UNKNOWN A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND FRAME SHEAR TIE PREVIOUS BLEND. REPAIRED OUT OF LIMITS SHEAR TIE PER B737-400 SRM 53-00-07 REPAIR. (M) 2L72 4F RTA16WE 20060407000672006040700067NM 2006 4 7 ASAA0540724 120051205A5310654587567 CREASE BEAM BOEING737 7374Q8 138447QNM FS 328-360 CORRODED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND RIGHT CREASE BEAM CORRODED OUT OF LIMITS. REPLACED CREASE BEAM PER B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060407000682006040700068NM 2006 4 7 ASAA0540665 120051118A5322 SHEAR TIE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - FOUND CORROSION AT AFT CARGO BAY ON SHEAR TIE. REMOVED DAMAGED SECTION OF SHEAR TIE, FABRICATED REPAIR PARTS AND INSTALLED PER B737-400 SRM 53-00-07. (M) 2L72 4F RTA16WE 20060407000942006040700094EA 2006 4 7 ASOA051035 120051129A33501317 LAMP BRUCE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27908EV 7654 DURING A HANGAR INSPECTION, THE AFT CABIN CEILING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE AFT CABIN CEILING EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20060407001052006040700105WP 2006 4 7 AMTA200601160 120051214A5330 SKIN LKHEED1011 10113853 5265020WP RROYCERB211 RB211524B4 54555NE FUSELAGE CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11163AT 1229 BETWEEN FS923/943 AND S-27/28 INNER SKIN FOUND CORRODED. FUSELAGE SKIN BETWEEN FS890 AND FS 983 STGR 26-31 REPAIR CARRIED OUT IAW L1011 SRM AND EER. REPLACED OUTER SKIN, INNER SKIN SLICE, TRIPLER SPLICES AND EXTERNAL AND NTERNAL STRAPS AND FILLERS. (K) 2L73 4F4 F A23WE E12EU 20060405000612006040500061EA 2006 4 5 SWIA200516392 120051224A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 621 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07932SW 7714 CARGO COMPARTMENT FS 621 LT FLOORBEAM CRACKED LBL 42, ITEM FOUND AT C-CHECK INSPECTION. FLOORBEAM REPAIRED IAW CRJ REO 601R-53-61-117 REV "C". 2L72 4F RTA21EA 20060405001502006040500150NM 2006 4 5 ASAA0540673 120051121A531165465492 FRAME BOEING737 7374Q8 138447QNM BS 767 CORRODED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND CORROSION ON LOWER FRAME CHORD AT BS 767, STRINGER 26R TO 27R. REMOVED AND REPLACED CHORD IAW B737-400 SRM 53-00-07. (M) 2L72 4F RTA16WE 20060405001512006040500151NM 2006 4 5 ASAA0540675 120051121A531165C2290911 FRAME BOEING737 7374Q8 138447QNM FS 500F CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND CORROSION ON LOWER FRAME CHORD AT BS S500F, STRINGER 25R TO 26R. REMOVED AND REPLACED SHEAR TIE IAW B737-400 SRM 53-00-07. (M) 2L72 4F RTA16WE 20060406000542006040600054NM 2006 4 6 ASAA0540725 120051205A53116546548 FRAME BOEING737 7374Q8 138447QNM FS 747 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND CORROSION ON LOWER FRAME CHORD OUT OF LIMITS. REPAIRED BY FABRICATING AND INSTALLING REPAIR PER B737-400 SRM 53-00-07. 2L72 4F RTA16WE 20060406002132006040600213WP 2006 4 6 ASAA0580556 120051212A575359304943 VANE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE LT TE FLAP PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 C-CHECK, LT WING NR 1 FLAP VANE IS PUNCTURED. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLER AND DOUBLER. (K) 2L72 4F4 FRTA6WE E9NE 20060407001142006040700114EA 2006 4 7 ASOA051047 120051202A33501317 LAMP BRUCE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27823AS 7196 DURING A GROUND INSPECTION, THE DEILING EMERGENCY LIGHT, AT ROW 9, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE CEILING EMERGENCY LIGHT, AT ROW 9. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20060407001302006040700130EU 2006 4 7 ASOA051052 120051204A33507012210 LAMP AEROSPATR72 ATR72 EU PWA PW120 PW127 NE CABIN BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27643AS 413 DURING A GROUND INSPECTION, THE EMERGENCY LIGHT, NEAR THE FLIGHT ATTENDANTS SEAT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY LIGHT, NEAR THE FLIGHT ATTENDANTS SEAT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2H72 4T4 TRT E20NE 20060407001422006040700142EA 2006 4 7 ASOA051054 120051204A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27882AS 7503 DURING A C-CHECK, THE INTERCOSTAL AT FS 484, RBL 27, WAS FOUND TO BE CRACKED BEYOND LIMITS. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCE DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION. (K) 2L72 4F4 FRTA21EA E15NE 20060407001662006040700166EA 2006 4 7 ASOA051045 120051202A5260 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27672BR 7594 DURING A HANGAR INSPECTION, THE PASSENGER DOOR STEP DRAG ANGLE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE PASSENGER DOOR STEP DRAG ANGLE IAW REO. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20060410000152006041000015NM 2006 4 10 ASAA0540670 120051121A53116546548 FRAME BOEING737 7374Q8 138447QNM FS 747 S25-26L CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND CORROSION LOWER FRAME CHORD AT FS 747 CORRODED FROM STRINGER 25L TO STRINGER 26L. REPAIRED BY FABRICATING AND INSTALLING REPAIR AT BS 747, STRINGER 25L TO STRINGER 26L, IAW B737-400 SRM 53-00-07. (M) 2L72 4F RTA16WE 20060407000702006040700070NM 2006 4 7 ASAA0540668 120051118A532065C361131 WEB BOEING737 7374Q8 138447QNM FS 303.9 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02775AS 25108 YXX - FOUND CRACKED WEB AT BS 303.9, STRINGER 16 LEFT. REPAIRED IAW ERO NR 5039 AND ASA EA 5310-02523. (M) 2L72 4F RTA16WE 20060407000882006040700088NM 2006 4 7 ASAA0540726 120051206A5311654655055 FRAME BOEING737 7374Q8 138447QNM FS 787 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND CORROSION ON LOWER FRAME OUT OF LIMITS. REPAIRED BY FABRICATING AND INSTALLING REPAIR PER ASA EA 5360-01048. (M) 2L72 4F RTA16WE 20060407001552006040700155EA 2006 4 7 ASOA051051 120051203A3350BF50390901 LENS BRUCE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE CABIN CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27716EV 10084 DURING A C-CHECK, THE EMERGENCY EXIT LIGHT LENS, OVER THE SERVICE DOOR, WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE LENS IN THE EMERGENCY EXIT LIGHT, OVER THE SERVICE DOOR. (K) 2L72 4F4 FRTA21EA EOOO63EN 20060407001582006040700158EA 2006 4 7 ASOA051040 120051130A3350487190 CONNECTOR 59465 CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN DISCONNECTED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27981EV 7768 DURING A GROUND INSPECTION, THE CENTER AISLE EMERGENCY LIGHT STRIP WAS FOUND TO BE DISCONNECTED AT THE AFT POSITION. MAINTENANCE RECONNECTED THE CENTER AISLE EMERGENCY LIGHT STRIP AT THE AFT POSITION. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20060407001602006040700160NM 2006 4 7 ASAA0540200 120050328A53206616932000 SUPPORT ANGLE BOEING737 737490 1384715NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02796AS 28891 FLOOR TO AFT BULKHEAD SUPPORT ANGLE DAMAGED. REMOVED FABRICATED AND INSTALLED NEW SUPPORT ANGLE. (K) 2L72 4F RTA16WE 20060410000132006041000013NM 2006 4 10 ASAA0540734 120051212A533065C3579224 SKIN BOEING737 737490 1384715NM FS 860-880 WORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM02796AS 28891 OKC - FOUND WEAR MARKS IN FUSELAGE SKIN. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PIECES IAW ASA EA 5330-02032. (M) 2L72 4F RTA16WE 20060410000612006041000061NM 2006 4 10 ASAA0540676 120051123A53206553594501 REVEAL BOEING737 7374Q8 138447QNM FS 328 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND FORWARD GALLEY DOOR CUTOUT, UPPER CORNER SEAL DEPRESSOR IS CORRODED. REMOVED AND REPLACED REVEAL IAW B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060410001102006041000110NM 2006 4 10 ASAA0540709 120051203A53206517680180 SILL BOEING737 737490 1384715NM FS 277-360 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02796AS 28891 OKC - FOUND L-1 DOOR MOPSILL CORRODED. REMOVED AND REPLACED MOPSILL IAW B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060410001152006041000115EA 2006 4 10 ASOA051050 120051203A33506100928 LAMP BRUCE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE CABIN BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27716EV 10084 DURING A C-CHECK, THE AFT GALLEY FLOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE WILL REMOVE AND REPLACE THE LAMP IN THE AFT GALLEY FLOOR EMERGENCY EXIT LIGHT. (K) 2L72 4F4 FRTA21EA EOOO63EN 20060410001292006041000129NM 2006 4 10 ASAA0540722 120051202A5340693535241 STRINGER CLIP BOEING737 7374Q8 138447QNM FS 663.5 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND STRINGER CLIP CRACKED. REPLACED STRINGER CLIP PER B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060410001382006041000138NM 2006 4 10 ASAA0540199 120050328A53406616932000 SUPPORT ANGLE BOEING737 737490 1384715NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02796AS 28891 FOOR TO AFT BULKHEAD SUPPORT ANGLE DAMAGED. REMOVED FABRICATED AND INSTALLED NEW SUPPORT ANGLE. (K) 2L72 4F RTA16WE 20060406001912006040600191WP 2006 4 6 ASAA0580546 120051212A5321993655213 FLOOR PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 C-CHECK, CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (K) 2L72 4F4 FRTA6WE E9NE 20060406001922006040600192WP 2006 4 6 ASAA0580547 120051212A5321993653737 FLOOR PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 C-CHECK, CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (K) 2L72 4F4 FRTA6WE E9NE 20060406002162006040600216WP 2006 4 6 ASAA0580549 120051212A53479936534139 TRACK DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE CABIN FLOOR CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 C-CHECK, CABIN FLOOR TRACK CORRODED. REPLACED FLOOR TRACK. (K) 2L72 4F4 FRTA6WE E9NE 20060407001252006040700125NM 2006 4 7 ASAA0540204 120050330A531165C229099 FRAME BOEING737 737490 1384715NM FUSE;AGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02796AS 28891 FWD CARGO BAY, CORROSION ON FRAME AT BSTA 500C, WL 148, LBL 5 TO RBL 5. REPAIRED FRAME IAW SRM. (K) 2L72 4F RTA16WE 20060407001412006040700141NM 2006 4 7 ASAA0540201 120050328A53206547690 PLATE BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02796AS 28891 FLOOR TO SIDEWALL SUPPORT PLATE CORRODED. REMOVED AND REPLACED FLOOR-TO-SIDEWALL SUPPORT PLATE. (K) 2L72 4F RTA16WE 20060407001642006040700164EA 2006 4 7 ASOA051043 120051201A33501317 LAMP BRUCE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27978EV 7723 DURING A HANGAR INSPECTION, THE RT CENTER EMERGENCY LIGHT ASSY WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN RT CENTER EMERGENCY LIGHT ASSY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20060410000122006041000012NM 2006 4 10 ASAA0540733 120051211A5320654587570 SILL BOEING737 737490 1384715NM FS 302-379 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02796AS 28891 OKC - FOUND R1 DOOR MOPSILL IS CORRODED. REMOVED AND REPLACED R-1 DOOR MOPSILL PER B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060410000142006041000014NM 2006 4 10 ASAA0540735 120051212A5210 SKIN BOEING737 737490 1384715NM L2 DOOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02796AS 28891 OKC - FOUND L-2 DOOR SKIN DENTED 11.5 INCH FORWARD OF AFT EDGE, 12 INCHES BELOW TAP EDGE, AFT OF HANDLE AND 9 INCHES ABOVE AFT END OF DOOR HANDLE. REMOVED DAMAGED SECTION OF SKIN, FABRICATED AND INSTALLED DOUBLER IAW ASA EA 5230-01291. (M) 2L72 4F RTA16WE 20060410001572006041000157EA 2006 4 10 MASA200500985 120051202A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0747202 7202 ASH 7195 ORD - FLAPS FAIL AT 20 DEGREES. MAINTENANCE C/W PART B. 2L72 4F RTA21EA 20060410001592006041000159EA 2006 4 10 MASA200500997 120051205A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0747202 7202 ASH 7268 ORD - FLAPS FAILED AT 0 DEGREES. MAINTENANCE C/W PART A AND COULD NOT DUPLICATE THE DISCREPANCY 2L72 4F RTA21EA 20060410001602006041000160EA 2006 4 10 MASA200501002 120051206A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA PAX DOOR OUT OF RIG A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0727172 7172 ASH 6106 CLE - PAX DOOR WILL NOT OPEN FROM INSIDE. MAINTENANCE RE-RIGGED THE DOOR. 2L72 4F RTA21EA 20060410001612006041000161EA 2006 4 10 MASA200501005 120051207A2120 SMOKE CNDAIRCL600 CL6002B19 1900309EA CABIN DETECTED A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW07154SF 7154 ASH 2791 TVC - SMOKE IN THE CABIN. RAN PACKS NO SMOKE, OPS CHECKED GOOD. 2L72 4F RTA21EA 20060410001622006041000162EA 2006 4 10 MASA200501026 120051210A5210 ROD END CNDAIRCL600 CL6002B19 1900309EA PAX DOOR DAMAGED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0727172 7172 ASH 7163 CLE - PASSENGER DOOR WOULD NOT OPEN AND WAS DIFFICULT TO CLOSE. FERRY TO IAD WHERE MAINTENANCE REMOVED AND REPLACED ROD ENDS ON THE NR 3 ROD AND THE SPRINGS ON THE PRESSURE RELIEF DOOR. 2L72 4F RTA21EA 20060410001672006041000167NM 2006 4 10 ASAA0540677 120051125A53116553594501 FRAME BOEING737 7374Q8 138447QNM FS 727F S26-27L CORRODED A ASAAO OTHER O OTHER NRNOT REPORTED 1 NM02774AS 25107 PAE - FOUND CORROSION ON LOWER CHORD OF FRAME AT BS 727F AT STRINGER 26L-27L. REPAIRED FRAME IAW B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060410001732006041000173NM 2006 4 10 AWXA200600517 120051211A5754114N4058 PANEL BOEING757 757225 1384959NM WS 425 RT SLAT DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28907AW 22691 GYR - DURING C8 CHECK DISCOVERED DELAMINATION BETWEEN PLIES ON SLAT CLOSURE PANELS ON THE INBOARD AND OUTBOARD ENDS AT WS 425.50R. MAINTENANCE REPAIRED CLOSURE PANELS BY REMOVING DELAMINATED PLIES AND APPLYING REPAIR PLIES AND DOUBLERS USING BMS 9-3 FIBERGLASS AND EY3804 RESIN IAW BOEING 757 SRM 51-70-06. 2L72 4F RTA2NM 20060410001792006041000179NM 2006 4 10 ASAA0540689 120051122A53156546809161 FLOORBEAM BOEING737 7374Q8 138447QNM FS 947 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02775AS 25108 YXX - FOUND FLOORBEAM AT BS 947.5 CORRODED FROM LBL 14 TO RBL 14. REPAIRED FLOORBEAM IAW ASA EA 5310-0257. (M) 2L72 4F RTA16WE 20060410001802006041000180NM 2006 4 10 ASAA0540693 120051121A5512657378352 SKIN BOEING737 737490 1384715NM HORIZONTAL STAB DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02796AS 28891 OKC - FOUND RIGHT HORIZONTAL STAB HAS 2 EACH DENTS 4 FEET OUTBOARD FROM ROOT ON L/E. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND PLATE IAW B737-400 SRM 55-10-01, FIG 201, REPAIR REPAIR 2. (M) 2L72 4F RTA16WE 20060410001812006041000181NM 2006 4 10 ASAA0540694 120051121A5512657378353 SKIN BOEING737 737490 1384715NM HORIZONTAL STAB DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02796AS 28891 OKC - FOUND DENT IN LEFT HORIZONTAL L/E 10 INCH FROM OUTBOARD END. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND PLATE IAW B737-400 SRM 55-10-01, FIGURE 201, REPAIR 2. (M) 2L72 4F RTA16WE 20060410001842006041000184EA 2006 4 10 ASOA051042 120051201A33500L3071BPEGPL LAMP BRUCE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27860AS 7433 DURING A GROUND INSPECTION, THE EMERGENCY LIGHT ASSY, NEAR THE PASSENGER DOOR, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMPS IN THE EMERGENCY LIGHT ASSY, NEAR THE PASSENGER DOOR. (K) 2L72 4F4 FRTA21EA E15NE 20060410001862006041000186EA 2006 4 10 ASOA051037 120051129A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PASSENGER DOOR BINDING A ASOAK NONE O OTHER ININSP/MAINT 1 SO27975EV 7599 DURING A GROUND INSPECTION, THE PASSENGER DOOR WAS BINDING. MAINTENANCE OPERATED THE PASSENGER DOOR WITH NO DEFECTS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20060410001872006041000187EA 2006 4 10 ASOA051041 120051201A33506100928 LAMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27879AS 7600 DURING A GROUND INSPECTION, THE EMERGENCY EXIT LIGHT, AT THE PASSENGER DOOR, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT, AT THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20060410001962006041000196NM 2006 4 10 ASAA0570009 120050115A5320143A750192 SUPPORT BOEING737 737790 13844CNNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02627AS 30794 DURING MAINTENANCE CHECK FOUND CORROSION ON FLOOR SUPPORT AT BS 500A-500D, REPAIR IAW SRM. (K) 2L72 4F RTA16WE 20060410002032006041000203NM 2006 4 10 ASAA0570006 120050113A5320143A75039 INTERCOSTAL BOEING737 737790 13844CNNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02627AS 30794 DURING MAINTENANCE CHECK FOUND CRACKED INTERCOSTAL AT BS 500B, WL156, REPAIR IAW SRM. (K) 2L72 4F RTA16WE 20060410002092006041000209WP 2006 4 10 ASAA0580542 120051212A532199365479 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 C-CHECK, CABIN FLOOR PANEL HAS CORRODED INSTERTS AND IS DELAMINATED AROUND INSTERS. REPLACED FLOOR PANEL. (K) 2L72 4F RTA6WE 20060410002162006041000216NM 2006 4 10 ASAA0570003 120050113A5340146A75024 SUPPORT BOEING737 737790 13844CNNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02627AS 30794 DURING MAINTENANCE CHECK FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT FROM BS 500A-500D AND WL 151, REPAIR IAW SRM. (K) 2L72 4F RTA16WE 20060410002222006041000222NM 2006 4 10 ASAA0570007 120050115A5321140A46202015 SPLICE BOEING737 737790 13844CNNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02627AS 30794 DURING MAINTENANCE CHECK FOUND CORROSION ON FLOOR SPLICE AT BS 871, REPAIR IAW SRM. (K) 2L72 4F RTA16WE 20060410002442006041000244NM 2006 4 10 ASAA0570008 120050115A5321140A4622015 SPLICE BOEING737 737790 13844CNNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02627AS 30794 DURING MAINTENANCE CHECK FOUND CORROSION ON FLOOR SPLICE AT BS 732, REPAIR IAW SRM. (K) 2L72 4F RTA16WE 20060410002582006041000258NM 2006 4 10 ASAA0470049 120050103A5230143A61122 SKIN BOEING737 737790 13844CNNM CARGO DOOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02619AS 30164 DURING IS CHECK FOUND NUMEROUS DENTS AND SCRATCHED/ GOUGES ON FWD CARGO DOOR, REPAIRED IAW EA. (K) 2L72 4F RTA16WE 20060410002682006041000268NM 2006 4 10 ASAA0540522 120051005A5241 SEAL DEPRESSOR BOEING737 7374Q8 138447QNM GALLEY DOOR CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02771AS 25104 AFT GALLEY DOOR CUTOUT SEAL DEPRESSOR CRACKED BELOW LOWER HINGE CUTOUT. REMOVED AND REPLACED IAW SRM. NOTE: REVISION 1 DUE TO MODEL NUMBER, SERIAL NUMBER, AND REFERENCE MATERIAL CORRECTIONS. (K) 2L72 4F RTA16WE 20060410002792006041000279NM 2006 4 10 ASAA0540194 120050321A53156517688704 WEB BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02782AS 25113 MAIN CABIN STA 344 APPROX. LBL 45 AT T-CHORD IS CRACKED. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPLACEMENT DOUBLER, A REPAIR PLATE, AND REPAIR WEB SEGMENT. (K) 2L72 4F RTA16WE 20060410002832006041000283NM 2006 4 10 ASAA0540597 120051106A5314 KEELBEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 KEEL BEAM HAS CORROSION AT LT OB LWR EDGE. BLENDED CORROSION, MAX MATERIAL REMOVED .051, ORIGINAL THICKNESS .140. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR PARTS IAW EA. (K) 2L72 4F RTA16WE 20060410002862006041000286NM 2006 4 10 ASAA0510057 120050411A534065622063 ATTACH FITTING BOEING737 737290C 138448VNM FUSELAGE OUT OF TOLERANCEA ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 BSTA 460 BETWEEN STRINGER 20L AND 21L SKIN TO FRAME ATTACHMENT HAS LOW EDGE MARGIN. REPAIRED IAW SRM. (K) 2L72 4F A16WE 20060410003172006041000317NM 2006 4 10 ASAA0540211 120050411A575365464307 SKIN BOEING737 737490 1384715NM TE FLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02795AS 28890 IB FORE FLAP HAS NUMEROUS DENTS IN LOWER SKIN SURFACE. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM. (K) 2L72 4F RTA16WE 20060407001122006040700112EA 2006 4 7 ASOA051058 120051204A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27716EV 10084 DURING A C-CHECK, THE SEAT TRACKS, FROM FS349 TO FS 985, RBL 9, WERE FOUND TO BE CORRODED BEYOND LIMITS. THIS MRR WILL REMAIN OPEN PENDING MATENANCE DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION. (K) 2L72 4F4 FRTA21EA EOOO63EN 20060407001512006040700151EA 2006 4 7 ASOA051046 120051202A5260601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE DOOR SEPARATED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27879AS 7600 DURING A HANGAR INSPECTION, THE PASSENGER DOOR BOTTOM STEP WAS FOUND TO BE SEPARATED AT THE ATTACHED STAY ROD BRACKET. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20060407001592006040700159EA 2006 4 7 ASOA051039 120051129A5210601R3807413 ANCHOR FITTING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27850AS 7355 DURING A HANGAR INSPECTION, THE PASSENGER DOOR AFT ANCHOR FITTING WAS TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACE THE PASSENGER DOOR AFT ANCHOR FITTING. (K) 2L72 4F4 FRTA21EA E15NE 20060407001652006040700165EA 2006 4 7 ASOA051048 120051202A33508GH00247308 LAMP CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE FUSELAGE BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27708EV 10060 DURING A GROUND INSPECTION, THE AFT RT SIDE OVER WING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE AFT RT SIDE OVER WING EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA EOOO63EN 20060410000872006041000087NM 2006 4 10 AWXA200600604 120051220A5712185N3001 SKIN BOEING757 757225 1384959NM HORIZONTAL STAB DENTED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28907AW 22691 GYR - DURING C 08 CHECK DISCOVERED RIGHT HAND HORIZONTAL STAB UPPER SKIN HAS A PREVIOUSLY BLENDED AREA LOCATED 2 INCHES AFT OF FRONT SPAR AT STA 200 MEASURING APPROX 4 INCHES BY 1.56 INCHES BY 0.032 INCHES DEEP. MAINTENANCE REMOVED DAMAGED SKIN AND CORE IAW BOEING 757-200 SRM 51-70-10-2R. FABRICATED CORE AND REPAIR DOUBLERS IAW BOEING 757-200 SRM 51-70-10-2R. INSTALLED FABRICATED REPAIR PARTS ON THE RT HORIZONTAL STAB IAW BOEING 757-200 SRM 51-70-10-2R. 2L72 4F RTA2NM 20060410001092006041000109NM 2006 4 10 ASAA0540706 120051204A5311 FRAME BOEING737 737490 1384715NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02795AS 28890 PAE - FOUND FRAME CRACKED AT BIN RAIL ATTACH CLIP. REMOVED CRACK IN FRAME, FABRICATED REPAIR PARTS AND INSTALLED IAW B737-400 SRM 53-00-07. (M) 2L72 4F RTA16WE 20060410001162006041000116EA 2006 4 10 ASOA051049 120051203A3350BC50393106 LENS BRUCE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE GALLEY CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27882AS 7503 DURING C-CHECK, THE EMERGENCY EXIT LENS, FORWARD OF THE SERVICE DOOR, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACE THE EMERGENCY EXIT LENS, FORWARD OF THE SERVICE DOOR. (K) 2L72 4F4 FRTA21EA E15NE 20060410001302006041000130NM 2006 4 10 ASAA0540711 120051202A5322 SHEAR TIE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND CORROSION ON SHEAR TIE. REPAIRED IAW B737-400 SRM 53-00-07. (M) 2L72 4F RTA16WE 20060410001992006041000199NM 2006 4 10 ASAA0570002 120050113A5340146A75021 SUPPORT BOEING737 737790 13844CNNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02627AS 30794 DURING MAINTENANCE CHECK FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT FROM BS 727-947 AND WL 152. REPAIR IAW SRM. (K) 2L72 4F RTA16WE 20060410002152006041000215NM 2006 4 10 ASAA0640010 120050107A533065C357984 SKIN BOEING737 737490 1384715NM BS1003-1016 DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02703AS 28893 SKIN HAS 5 EACH DENTES AT BSTA 1003-1016. REMOVED SKIN AT BSTA 986.51016, STRINGER 10-14 RT, FABRICATED AND NSTALLED REPALCEMENT SKIN IAW DWG AND IAW SRM. (K) 2L72 4F RTA16WE 20060410003842006041000384NM 2006 4 10 ASAA0540203 120050330A534565C347882 PLATE BOEING737 737490 1384715NM COCKPIT SCRATCHED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02796AS 28891 UPPER TCAS MOUNTING PLATE IS DAMAGED, REPLACED MOUNTING PLATE. (K) 2L72 4F RTA16WE 20060410003972006041000397NM 2006 4 10 ASAA0540195 120050322A575465C266869 SKIN BOEING737 7374Q8 138447QNM WING DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02782AS 25113 RT NR 5 SLAT IB T/E IS DELAMINATED. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW SRM. (K) 2L72 4F RTA16WE 20060411000202006041100020NM 2006 4 11 ASAA0540716 120051201A531465C32953 KEELBEAM BOEING737 7374Q8 138447QNM BS 500G CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND CORROSION ON KEELBEAM. FOUND OUT OF LIMITS, REPAIRED ASA EA 5360-01045. (M) 2L72 4F RTA16WE 20060410001282006041000128NM 2006 4 10 ASAA0540721 120051203A533065516241 DOUBLER BOEING737 7374Q8 138447QNM FS 967 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND CORROSION ON BONDED SKIN DOUBLER. REPAIRED PER ER 05-4782, AND ASA EA 5360-01046. (M) 2L72 4F RTA16WE 20060410001882006041000188EU 2006 4 10 ASOA051044 120051201A33507012210 LAMP AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE CABIN BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27633AS 344 DURING A HANGAR INSPECTION, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY LIGHT ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2H72 4T4 TRTA53EU E20NE 20060410001972006041000197NM 2006 4 10 ASAA0540521 120051001A533065C2522011 SPLICE BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02793AS 28888 FUSELAGE SKIN BUTT SPLICE HAS CORROSION AT EXISTING REPAIR. REMOVED EXISTING BUTT SPLICE, FABRICATED AND INSTALLED NEW SPLICE IAW SRM. (K) 2L72 4F RTA16WE 20060410002022006041000202NM 2006 4 10 ASAA0570004 120050113A5340146A750217 SUPPORT BOEING737 737790 13844CNNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02627AS 30794 DURING MAINTENANCE CHECK FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT FROM BS767-794 AND WL154, REPAIR IAW SRM. (K) 2L72 4F RTA16WE 20060410002122006041000212NM 2006 4 10 ASAA0540207 120050406A554265C259611 SKIN BOEING737 737490 1384715NM RUDDER PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02795AS 28890 BOTTOM OF RUDDER IS PUNCTURED. COMPLIED WITH A BOND REPAIR IAW SRM. (K) 2L72 4F RTA16WE 20060410002262006041000226NM 2006 4 10 ASAA0540679 120051129A531165465968 FRAME BOEING737 7374Q8 138447QNM FS 727F CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND CORROSION LOWER CHORD OF FRAME AT BS 727F AT STRINGER 26L-27L. REPAIRED FRAME IAW B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060410002272006041000227NM 2006 4 10 ASAA0540680 120051129A531565C3394825 FLOORBEAM BOEING737 7374Q8 138447QNM FS 947 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND CORROSION ON FLOORBEAM. REPAIRED IAW ASA EA 5310-02524. (M) 2L72 4F RTA16WE 20060410002282006041000228SO 2006 4 10 MASA200500610 120050802A3350316 LAMP EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07831MJ 145273 ASH 2743 CLT - THE AFT CABIN OVHD EMERG LIGHT WAS INOP. MX RELAMPED THE LIGHT. 2L72 4T RTT00011AT 20060410002292006041000229NM 2006 4 10 ASAA0540683 120051120A52006545830131 ACCESS DOOR BOEING737 7374Q8 138447QNM FS 328-344 CRACKED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM02775AS 25108 YXX - E/E COMPARTMENT ACCESS DOOR OUTER SURFACE IS DENTED/CRACKED. OUTER SURFACED REPAIRED IAW B737-400 SRM 52-00-01 FIG 201. (M) 2L72 4F RTA16WE 20060410002572006041000257NM 2006 4 10 ASAA0570013 120050119A5340146A75022 SUPPORT BOEING737 737790 13844CNNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02627AS 30794 DURING MAINTENANCE CHECK FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT AT RT BS 727-967, IAW SRM. (K) 2L72 4F RTA16WE 20060410002812006041000281NM 2006 4 10 ASAA0540192 120050320A5315 FLOORBEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02782AS 25113 TOP OF FLOORBEAM CORRODED AT STA 312, LBL 12. REMOVED DAMAGED UPPER CHORD, FABRICATED AND INSTALLED A REPLACEMENT UPPER CHORD IAW SRM. (K) 2L72 4F RTA16WE 20060410003522006041000352NM 2006 4 10 ASAA0540209 120050407A57536546486123 WEDGE BOEING737 737490 1384715NM TE FLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02795AS 28890 LT WING IB MID FLAP WEDGE IS DENTED. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM. (K) 2L72 4F RTA16WE 20060410003892006041000389WP 2006 4 10 AMTA200600199 120050329A52401514281103 FITTING LKHEED1011 10113853 5265020WP RROYCERB211 RB211524B4 54555NE DOOR CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11163AT 1229 R1 DOOR LOWER AFT FITTING FOUND WITH CORROSION. R1 DOOR LOWER AFT FWD FITTING CORRODED WAS REMOVED AND REPLACED WITH NEW IAW SRM. (K) 2L73 4F4 F A23WE E12EU 20060411000012006041100001NM 2006 4 11 ASAA0540729 120051208A53226546593 SHEAR TIE BOEING737 737490 1384715NM FS 500 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02795AS 28890 PAE - FOUND CORROSION ON FORWARD CARGO FRAME SHEAR TIE. CORRODED OUT OF LIMITS FABRICATED AND INSTALLED NEW SHEAR TIE PER SRM 53-00-07. (M) 2L72 4F RTA16WE 20060410001852006041000185EU 2006 4 10 ASOA051038 120051129A33500341519 FUSE AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE CABIN BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27634AS 370 DURING A GROUND INSPECTION, THE EMERGENCY LIGHT, NEAR THE FRONT DOOR, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FUSE IN THE POWER SUPPLY UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2H72 4T4 TRTA53EU E20NE 20060410002082006041000208NM 2006 4 10 ASAA0570011 120050115A5347146A940121 SEAT TRACK BOEING737 737790 13844CNNM FLIGHT DECK WORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM02627AS 30794 DURING MAINTENANCE CHECK FOUND FO IB AFT SEAT TRACK WORN. REPAIR IAW SRM. (K) 2L72 4F RTA16WE 20060410002302006041000230NM 2006 4 10 ASAA0540687 120051122A531565498854 FLOORBEAM BOEING737 7374Q8 138447QNM FS 986.5 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02775AS 25108 YXX - FOUND CORROSION ON FLOORBEAM AT BS 986.5 AT CLIP NUTS. REPAIRED FLOORBEAM IAW ASA EA 5310-02525. (M) 2L72 4F RTA16WE 20060410002312006041000231NM 2006 4 10 ASAA0540692 120051121A5730657378352 SKIN BOEING737 737490 1384715NM RT WING DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02796AS 28891 OKC - FOUND DENT IN RIGHT L/E 15 FEET OUTBOARD FROM WING ROOT. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND PLATE IAW B737-400 SRM 55-10-01, FIG 201, REPAIR 2. (M) 2L72 4F RTA16WE 20060410002372006041000237NM 2006 4 10 ASAA0540681 120051120A5340654580730 ATTACH ANGLE BOEING737 7374Q8 138447QNM FS 291.5 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02775AS 25108 PAE - FOUND FORWARD OF R1 DOOR FRAME AT BS 291.5 ABOVE STRINGER 13 RT SKIN ATTACH ANGLE TO INTERCOSTAL CRACKED. FABRICATED REPAIR PART INSTALLED AT FORWARD OF R-1 DOOR FRAME AT BS 291.5 ABOVE STRINGER 13 RT SKIN ATTACH ANGLE TO INTERCOSTAL. (M) 2L72 4F RTA16WE 20060410002382006041000238NM 2006 4 10 ASAA0540684 120051120A5310654580734 DOOR FRAME BOEING737 7374Q8 138447QNM FS 291.5 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02775AS 25108 YXX - FOUND FORWARD OF R1 DOOR FRAME AT BS 29.1 ABOVE STRINGER 10 RT SKIN ATTACH ANGLE TO INTERCOSTAL IS CRACKED. REPLACED ATTACH ANGLE IAW B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060410002402006041000240NM 2006 4 10 ASAA0540737 120051212A531565C3394325 FLOORBEAM BOEING737 737490 1384715NM FS 344 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02796AS 28891 OKC - FOUND CORROSION ON FLOORBEAM AT BS 344 UPPER FLANGE. REMOVED DAMAGE, CORROSION, FABRICATED AND INSTALLED REPLACEMENT UPPER CHORD IAW ASA EA 5320-01710. (M) 2L72 4F RTA16WE 20060410002412006041000241NM 2006 4 10 ASAA0540671 120051121A5311 FRAME BOEING737 7374Q8 138447QNM BS 727F DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND DENT AT BS 727F, STRINGER 24R-25R IN FRAME. CUTOUT DAMAGE AND INSTALLED REPAIR DOUBLER IAW B737-400 SRM 51-70-11. (M) 2L72 4F RTA16WE 20060410002422006041000242NM 2006 4 10 ASAA0540738 120051212A531565468111 FLOORBEAM BOEING737 737490 1384715NM FS 986.5 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02796AS 28891 OKC - FOUND CORROSION ON BS 986.5 FLOORBEAM UPPER CHORD. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PIECES AND INSTALLED IAW EA 5360-01049. (M) 2L72 4F RTA16WE 20060410002432006041000243NM 2006 4 10 ASAA0540730 120051208A5322654653272 SHEAR TIE BOEING737 737490 1384715NM FS 500C CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02795AS 28890 PAE - FOUND CORROSION ON FORWARD CARGO FRAME SHEAR TIE. FABRICATED AND INSTALLED REPAIR TO FRAME PER SRM 53-00-07. (M) 2L72 4F RTA16WE 20060410002452006041000245NM 2006 4 10 ASAA0540731 120051210A5230 SUPPORT BOEING737 737490 1384715NM CARGO DOOR CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02796AS 28891 OKC - FOUND FORWARD CARGO DOOR CORRODED IN SEVERAL PLACES. REMOVED AND REPLACED SUPPORT AND CHANNEL PER B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060410002502006041000250NM 2006 4 10 ASAA0540210 120050411A53306548240503 SKIN BOEING737 737490 1384715NM FUSELAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02795AS 28890 LT FUSELAGE EXTERNAL SKIN CHAFED AT LT STAB AFT OF BOTTOM LUG CUTOUT STA 1150-1140. REMOVED DAMAGED SKIN, FABRICATED AND INSTALLED REPLACEMENT SKIN IAW SRM. (K) 2L72 4F RTA16WE 20060410002562006041000256NM 2006 4 10 ASAA0540212 120050411A533065184201033 SKIN BOEING737 737490 1384715NM FUSELAGE LIGHTNING STRIKEA ASAAK NONE O OTHER ININSP/MAINT 1 NM02795AS 28890 LIGHTING STRIKE AT FRAME 211.8 ON CREASE BEAM. REMOVED DAMAGED, COMPLIED WITH A HFEC INSPECTION IAW MFG NDT MANUAL, NO DEFECTS NOTED. FABRICATED AND INSTALLED A REPAIR FILLER, DOUBLER, AND TRIPLER IAW SRM. (K) 2L72 4F RTA16WE 20060410002592006041000259NM 2006 4 10 ASAA0570010 120050115A5321146A940121 SPLICE PLATE BOEING737 737790 13844CNNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02627AS 30794 DURING MAINTENACE CHECK FOUND CORROSION ON FLOOR PANEL SPLICE PLATE, REPAIR IAW SRM.. (K) 2L72 4F RTA16WE 20060410003192006041000319NM 2006 4 10 ASAA0540208 120050406A554265C259611 SKIN BOEING737 737490 1384715NM RUDDER DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02795AS 28890 RUDDER IS DAMAGED AT LT SIDE LOWER EDGE. COMPLIED WITH A BOND REPAIR IAW SRM. (K) 2L72 4F RTA16WE 20060410003882006041000388NM 2006 4 10 ASAA0540202 120050330A5340654769024 PLATE BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02796AS 28891 CORROSION ON FLOOR TO SIDEWALL SUPPORT PLATE NUMEROUS AREAS BSTA 727-767, RBL 21. CORROSION BLENDED OUT OF LIMITS, REPAIRED IAW SRM. (K) 2L72 4F RTA16WE 20060411001912006041100191NM 2006 4 11 MASA200500931 120051121A3244314354 TIRE DHAV DHC8 DHC8202 2809007NM MLG FAILED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07437YV1826 437 ASH 6372 PHX, NR 4 TIRE BLEW. MAINTENANCE REPLACED THE NR 3 AND NR 4 MLG TIRES. 2H72 4T RTA13NM 20060411002372006041100237NM 2006 4 11 ASAA0510056 120050411A532266221212 SHEAR TIE BOEING737 737290C 138448VNM FUSELAGE OUT OF TOLERANCEA ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 SHEAR TIE ANGLE BSTA 460 BETWEEN STR 19 AND 20 HAS LOW EDGE MARGIN AT FASTENER HOLE. REPAIRED IAW SRM. (K) 2L72 4F A16WE 20060411002382006041100238NM 2006 4 11 ASAA0510058 120050411A532265465632 SHEAR TIE BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 SHEAR TIE AT BSTA 967 BETWEEN STRINGER 27L THRU 27R HAS CORROSION. SHEAR TIE BETWEEN STRINGER 27L AND 22R REPAIRED IAW SRM. (K) 2L72 4F A16WE 20060411002452006041100245 2006 4 11 KBM2006F00131 420050815A342455508340N5L SWITCH SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1D1 NE COCKPIT STICKING E KBMAK NONE O OTHER ININSP/MAINT 1 WP19350SH 3345 TURN AND BANK POWER SWITCH, STICKING. (K) 1G71 3U3 UNCH9EU E19EU 20060412000432006041200043NM 2006 4 12 ASAA0540752 120051227A531165465588 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02780AS 25112 PAE-FRAME CRACKED AT BIN RAIL. REPAIRED FRAME AT BSTA 907RH BIN RAIL ATTACH POINT. (K) 2L72 4F RTA16WE 20060412000492006041200049NM 2006 4 12 ASAA05400762 120051229A531165465262 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02780AS 25112 PAE- FRAME CRACKED AT BIN RAIL ATTACH POINT. REPAIRED CRACKED FRAME IAW SRM. (K) 2L72 4F RTA16WE 20060412000512006041200051NM 2006 4 12 ASAA0540650 120051114A5320654587547 WEB BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE-CORROSION ON SHEAR WEB. REMOVED AND REPLACED SHEAR WEB IAW SRM. (K) 2L72 4F RTA16WE 20060412000592006041200059NM 2006 4 12 ASAA0540653 120051114A575465C26603201 SKIN BOEING737 7374Q8 138447QNM LE SLAT CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE- NR 3 SLAT LWR T/E SKIN AT OB END CRACKED THROUGH FASTENER HOLE. REPAIRED IAW SRM 57-43-01. (M) 2L72 4F RTA16WE 20060412000622006041200062NM 2006 4 12 ASAA0540636 120051110A531565C33941 FRAME BOEING737 7374Q8 138447QNM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE-MECHANICAL DAMAGE TO FLOOR BEAM AT BSTA 312, LBL 11-54, WL 208. REMOVED AND REPLACED FLOOR BEAM UPPER CHORD AT BSTA 312, WL 208 IAW SRM. (K) 2L72 4F RTA16WE 20060412000632006041200063NM 2006 4 12 ASAA0540648 120051114A53306516303 SKIN BOEING737 737490 1384715NM FUSELAGE TORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM02799AS 29270 ANC - REFUEL TRUCK HIT RT SIDE OF AIRCRAFT. PERFORMED A SRM REPAIR IAW DETAIL 12 AND EA CARGO HOLD. (K) 2L72 4F RTA16WE 20060412000642006041200064NM 2006 4 12 ASAA0540638 120051110A52306546921171 DOOR BOEING737 7374Q8 138447QNM FWD CARGO DOOR SCRATCHED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - FWD CARGO DOOR LWR AFT SIDE FRAME IS SCRATCHED. REMOVED AND REPLACED FRAME IAW SRM. (K) 2L72 4F RTA16WE 20060412000652006041200065NM 2006 4 12 ASAA0540656 120051114A52406551629501 SEAL DEPRESSOR BOEING737 7374Q8 138447QNM DOOR CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE-CORROSION ON FWD SERVICE DOOR CUTOUT SEAL DEPRESSOR. REMOVED AND REPLACED DUE TO FINDING CRACKS WHILE REMOVING CORROSION. (K) 2L72 4F RTA16WE 20060412000662006041200066NM 2006 4 12 ASAA0540637 120051110A5311654654987 FRAME BOEING737 7374Q8 138447QNM FUSELAGE TOOL DAMAGE A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - AFT CARGO BAY DRILL START ON FRAME UPPER FLANGE. REPAIRED FRAME IAW SRM. (K) 2L72 4F RTA16WE 20060412000672006041200067NM 2006 4 12 ASAA0540640 120051110A531565C3394027 FLOORBEAM BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - PREVIOUS REPAIR CRACKED AT FRAME. REMOVED AND REPLACED REPAIR ANGLES IAW EA. (K) 2L72 4F RTA16WE 20060410004022006041000402NM 2006 4 10 ASAA0540206 120050331A532065479573 WEB BOEING737 737490 1384715NM AFT CARGO DOOR CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02796AS 28891 CORROSION ON SUB-THRESHOLD WEB AT AFT CARGO DOOR OPENING. CORROSION REMOVAL BLENDED OUT OF LIMITS, REPLACED SUB-THRESHOLD WEB. (K) 2L72 4F RTA16WE 20060410004042006041000404NM 2006 4 10 ASAA0540193 120050320A5753 WEDGE BOEING737 7374Q8 138447QNM RT WING CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02782AS 25113 RT WING IB T/E MIF FLAP T/E WEDGE IS CHAFFED. REMOVED DAMAGED WEDGE, ORDERED AND REPLACED WITH A NEW WEDGE IAW SRM. (K) 2L72 4F RTA16WE 20060412000422006041200042NM 2006 4 12 ASAA0540763 120051229A532065465262 FLOOR SUPPORT BOEING737 7374Q8 138447QNM CARGO BAY FLOOR CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02780AS 25112 PAE-FWD CARGO BAY FLOOR SUPPORT CORRODED. CUT OUT DAMAGED FLOOR SUPPORT, FABRICATED AND INSTALLED REPAIR IAW SRM. (K) 2L72 4F RTA16WE 20060412000522006041200052NM 2006 4 12 ASAA0540651 120051114A53105079454 BEAM BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE- FWD ENTRY DOOR LWR GATE BEAM CRACKED. REMOVED AND REPLACED IAW SRM. (K) 2L72 4F RTA16WE 20060412000552006041200055NM 2006 4 12 ASAA0540654 120051114A533065C26602311 SKIN BOEING737 7374Q8 138447QNM NR 3 SLAT CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - NR 3 SLAT LWR T/E SKIN AT IB END CRACKED AT FASTENER HOLE. REPAIRED IAW SRM. (K) 2L72 4F RTA16WE 20060412000612006041200061NM 2006 4 12 ASAA0540647 120051110A5320651768564 WEB BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02775AS 25108 YXX-SB, WEB MOD AT BSTA 360, STR 16 LT, TO BE COMPLIED WITH. SB ACCOMPLISHED IAW EO. (K) 2L72 4F RTA16WE 20060412000682006041200068NM 2006 4 12 ASAA0540639 120051110A5311654654965 FRAME BOEING737 7374Q8 138447QNM FUSELAGE TOOL DAMAGE A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE- DRILL START ON FRAME AT BSTA 767, RBL 12, WL 154. REPAIRED FRAME IAW SRM. (K) 2L72 4F RTA16WE 20060412000702006041200070NM 2006 4 12 ASAA0540644 120051109A531565C33940 FLOORBEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02775AS 25108 YXX - CORROSION ON TOP SURFACE OF FLOORBEAM AT BSTA 294.5, LBL 12 TO RBL 12. FLOOR BEAM UPPER CHORD REPAIRED BY SPLICE IAW SRM. (K) 2L72 4F RTA16WE 20060412000712006041200071NM 2006 4 12 ASAA0540641 120051110A53306545800219 SKIN BOEING737 7374Q8 138447QNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - DENT IN FUSELAGE SKIN. REPAIRED SKIN IAW EA. (K) 2L72 4F RTA16WE 20060412000722006041200072NM 2006 4 12 ASAA0540643 120051110A53226546594502 SHEAR TIE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE-CORROSION AT BSTA 500B, RBL 16, WL 149, UPPER SURFACE OF SHEAR TIE AT FASTENER. REPAIRED SHEAR TIE IAW SRM. (K) 2L72 4F RTA16WE 20060412000732006041200073NM 2006 4 12 ASAA0510043 120050411A531365622686 STRINGER BOEING737 737290C 138448VNM FUSEAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 YXX - NDT CRACK INDICATION AT FASTENER HOLE BSTA 470, STR 22L. REPAIRED IAW SRM. (K) 2L72 4F A16WE 20060412000742006041200074NM 2006 4 12 ASAA0540645 120051109A53156545815 FLOORBEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02775AS 25108 YXX - FLOORBEAM AT BSTA 344, BL 0, TO LBL 65 CORRODED AT ANCHOR NUT HOLES. REPAIRED IAW SRM. (K) 2L72 4F RTA16WE 20060412000752006041200075NM 2006 4 12 ASAA0540646 120051109A524065698541 BRACKET BOEING737 7374Q8 138447QNM DOOR CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02775AS 25108 YXX - R-1 DOOR INTERIOR, AT AFT BOTTOM CORNER, PLATE CRACKED THROUGH AT FASTENER HOLES. REPAIRED BY INSTALLING REPAIR PARTS IAW SRM. (K) 2L72 4F RTA16WE 20060412000772006041200077NM 2006 4 12 ASAA0540754 120051222A532265465677 SHEAR TIE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02780AS 25112 PAE-CORROSION ON SHEAR TIE BSTA 1006, STR 27LT TO 27 RT. REMOVED AND REPLACED SHEAR TIE IAW SRM. (K) 2L72 4F RTA16WE 20060412000442006041200044NM 2006 4 12 ASAA0540764 120051229A5322654659320 SHEAR TIE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02795AS 25112 PAE- CORROSION ON FWD CARGO FRAME SHEAR TIE AT BSTA 500B BL 0, STR 28 LT. FOUND CORROSION TO BE OUT OF LIMITS, FABRICATED AND INSTALLED REPAIR TO FRAME SHEAR TIE IAW SRM. (K) 2L72 4F RTA16WE 20060412000482006041200048NM 2006 4 12 ASAA0540765 120051229A5310652072284 DOOR FRAME BOEING737 7374Q8 138447QNM BS 440 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE- FWD CARGO DOOR FWD FRAME CRACKED AT NR5 DOORSTOP FITTING. REMOVED AND REPLACED BSTA 440 FWD CARGO DOOR FRAME IAW SRM. (K) 2L72 4F RTA16WE 20060412000532006041200053NM 2006 4 12 ASAA0540767 120051229A531165465252 FRAME BOEING737 7374Q8 138447QNM BS 380 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE- BSTA 380 FRAME MEMBER CRACKED AT BIN RAIL ATTACH. REPAIRED FLOOR BEAM IAW SRM. (K) 2L72 4F RTA16WE 20060412000562006041200056NM 2006 4 12 ASAA0540655 120051114A5311654658821 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE- CORROSION AFT CARGO BAY FRAME CHROD SHEAR TIE. REPAIRED IAW SRM. (K) 2L72 4F RTA16WE 20060412000572006041200057NM 2006 4 12 ASAA0540768 120051229A531165C32395 FRAME BOEING737 7374Q8 138447QNM BS 727F DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 DENT IN FRAME AT BS 727F BETWEEN STR 22R-24R. REPAIRED FRAME IAW SRM 51-70-11. (K) 2L72 4F RTA16WE 20060412000582006041200058NM 2006 4 12 ASAA0540766 120051229A5315 FLOORBEAM BOEING737 7374Q8 138447QNM FUSELEGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE- CORROSION ON TOP CHORD OF FLOOR BEAM. REPAIRED FLOOR BEAM IAW SRM. (K) 2L72 4F RTA16WE 20060412000602006041200060NM 2006 4 12 ASAA0540751 120051227A531190526911 FRAME BOEING737 7374Q8 138447QNM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02780AS 25112 PAE- FRAME CRACKED AT BIN RAIL ATTACH POINT. INSTALLED FRAME REPAIR DOUBLER ON BSTA 480 FRAME RT AT BIN RAIL LOCATION. (K) 2L72 4F RTA16WE 20060412000692006041200069NM 2006 4 12 ASAA0510042 120050411A53306545774549 SKIN BOEING737 737290C 138448VNM FUSELAGE TOOL DAMAGE A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 YXX - BONDED DOUBLER AND AIRCRAFT SKIN DAMAGED AT BSTA 827 AT STR 21L BY TOOL. BONDED DOUBLER AND AIRCRAFT SKIN AT BSTA 827 AT STR 21L REPAIRED IAW SRM. (K) 2L72 4F A16WE 20060413001512006041300151NM 2006 4 13 2006UALA00609 120051222A2780 SLAT BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29665UA 29237 DIVERTED TO HNL DUE TO LEADING EDGE SLAT ASYMMETRY PROBLEM. FAILURE DUE TO A CRACKED 90 DEGREE CONDUIT. 2L72 4F4 FRTA1NM E24NE 20060413001692006041300169NM 2006 4 13 ASAA0510061 120050414A53406554956504 ATTACH ANGLE BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 YXX- FWD CARGO SKIN-TO-FRAME ATTACH ANGLE AT BSTA 500 AND STR 28 LT CORRODED. REPAIRED WITH MADE REPAIR PART. (K) 2L72 4F A16WE 20060413001702006041300170NM 2006 4 13 ASAA05700059 120050914A53214533A161031 FLOOR PANEL BOEING737 737790 13844CNNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02623AS 30166 PAE: NR 3 FLOOR PANEL OF FWD CARGO PIT HAS NUMEROUS DENTS. REMOVED AND FABRICATED NEW IAW SRM. (K) 2L72 4F RTA16WE 20060413001712006041300171NM 2006 4 13 ASAA05700065 120050921A5340146A101039 STRINGER CLIP BOEING737 737790 13844CNNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02623AS 30166 PAE: DURING C-CHECK FOUND STRINGER CLIP AT BS 847 CRACKED ON OB LEG. REPAIRED IAW SRM. (K) 2L72 4F RTA16WE 20060413001732006041300173NM 2006 4 13 ASAA05700068 120050921A5321453A261017 FLOOR PANEL BOEING737 737790 13844CNNM AFT CARGO BAY GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02623AS 30166 PAE: DURING C-CHECK FOUND AFT CARGO BAY NR 3 FLOOR PANEL GOUGED AND DENTED. REPAIRED IAW SRM. (K) 2L72 4F RTA16WE 20060413001742006041300174NM 2006 4 13 ASAA0570075 120051005A5340143A948530 ANGLE BOEING737 737790 13844CNNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02615AS 30344 PAE: DURING C-CHECK FOUND BULKHEAD LT LOWER L ANGLE CORRODED AT BS 500D. REPAIRED IAW SRM. (K) 2L72 4F RTA16WE 20060413001962006041300196NM 2006 4 13 ASAA05700067 120050921A5321453A261031 FLOOR PANEL BOEING737 737790 13844CNNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02623AS 30166 PAE: DURING C-CHECK FOUND FOUND AFT CARGO BAY FLOOR PANEL NR 2 GOUGED AND CRACKED. REPAIRED IAW SRM. (K) 2L72 4F RTA16WE 20060413001972006041300197NM 2006 4 13 ASAA0570073 120051005A5321453A161032 FLOOR PANEL BOEING737 737790 13844CNNM FUSELAGE PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02615AS 30344 PAE: DURING C-CHECK, FOUND FWD CARGO NR 3 FLOOR PANEL PUNCTURED. REPAIRED IAW SRM. (K) 2L72 4F RTA16WE 20060413001982006041300198NM 2006 4 13 ASAA0570074 120051005A5320143A75011 SUPPORT BOEING737 737790 13844CNNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02615AS 30344 PAE: DURING C-CHECK FOUND FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED AT BS 500C. REPAIRED IAW SRM. (K) 2L72 4F RTA16WE 20060413001992006041300199NM 2006 4 13 ASAA05700066 120050921A5340146A75021 SUPPORT BOEING737 737790 13844CNNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02623AS 30166 PAE: DURING C-CHECK, FOUND FLOOR TO SIDEWALL SUPPORT CORRODED. REPAIRED IAW SRM. (K) 2L72 4F RTA16WE 20060413002002006041300200NM 2006 4 13 ASAA0570078 120051005A5320146A75058 INTERCOSTAL BOEING737 737790 13844CNNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02615AS 30344 PAE: DURING C-CHECK FOUND CORROSION ON INTERCOSTAL AT STA 747-767. REPAIRED IAW SRM. (K) 2L72 4F RTA16WE 20060413002052006041300205NM 2006 4 13 ASAA0570076 120051005A5340143A948535 SUPPORT ANGLE BOEING737 737790 13844CNNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02615AS 30344 PAE: DURING C-CHECK FOUND BULKHEAD LWR CENTER SUPPORT ANGLE IS CORRODED AT BS 500D. REPAIRED IAW SRM. (K) 2L72 4F RTA16WE 20060413002062006041300206NM 2006 4 13 ASAA0510044 120050411A5313 STRINGER BOEING737 737290C 138448VNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 YXX - STRINGER 20L AT BSTA 390 CRACKED THROUGH FASTENER HOLE. REPAIRED IAW SRM. (K) 2L72 4F A16WE 20060413002092006041300209NM 2006 4 13 ASAA0510048 120050411A531165622063 FRAME BOEING737 737290C 138448VNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 YXX - NDT CRACK INDICATION AT FASTENER HOLE ON FRAME TO SKIN ATTACHMENT AT BSTA 480 BETWEEN STRINGER 20L AND STRINGER 21L. REPAIRED FRAME IAW SRM. (K) 2L72 4F A16WE 20060413002102006041300210NM 2006 4 13 ASAA0510046 120050411A531165622063 FRAME BOEING737 737290C 138448VNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 YXX - NDT CRACK INDICATION AT FASTENER HOLE ON FRAME TO SKIN ATTACHMENT AT BSTA 460 BETWEEN STRINGER 20L AND STRINGER 22L. REPAIRE FRAME IAW SRM. (K) 2L72 4F A16WE 20060413002112006041300211NM 2006 4 13 ASAA0510045 120050411A531165622063 FRAME BOEING737 737290C 138448VNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 YXX - NDT CRACK INDICATION AT FASTENER HOLE ON FRAME TO SKIN ATTACHMENT AT BSTA 460 BETWEEN STRINGER 19L STRINGER 20L. REPAIRED FRAME IAW SRM. (K) 2L72 4F A16WE 20060413002122006041300212NM 2006 4 13 ASAA0510052 120050411A531365622684 STRINGER BOEING737 737290C 138448VNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 YXX- NDT CRACK INDICATION AT FASTENER HOLES ON STR 19L, BSTA 460-480. REPAIRED IAW SRM. (K) 2L72 4F A16WE 20060413002152006041300215NM 2006 4 13 ASAA0510037 120050404A531365516983 STRINGER BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 YXX- AFT CARGO PIT BSTA 907, STR 21L SPLICE HAS CORROSION. AFT CARGO PIT BSTA 907, STR 21L REAPIRED IAW SRM. (K) 2L72 4F A16WE 20060413002222006041300222NM 2006 4 13 ASAA0510036 120050401A53136552928517 STRINGER BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 YXX - AFT CARGO PIT BSTA 827-847, STR 27L SPLICE HAS CORROSION. AFT CARGO PIT BSTA 827-847, STR 27L REPAIRED IAW SRM. (K) 2L72 4F A16WE 20060413002302006041300230NM 2006 4 13 ASAA0570079 120051005A5340146A75022 PLATE BOEING737 737790 13844CNNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02615AS 30344 PAE: DURING C-CHECK FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT PLATE AT BS 727. REPAIRED IAW SRM. (K) 2L72 4F RTA16WE 20060413002582006041300258NM 2006 4 13 ASAA0570096 120051009A5320146A75035 FLOOR SUPPORT BOEING737 737790 13844CNNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02615AS 30344 PAE: DURING C-CHECK FOUND CORROSION ON FLOOR SUPPORT AT BS 773. REPAIRED IAW EA. (K) 2L72 4F RTA16WE 20060411002352006041100235NM 2006 4 11 ASAA0540190 120050318A552365C2638416 TAB BOEING737 7374Q8 138447QNM ELEVATOR BROKEN A ASAAK NONE O OTHER ININSP/MAINT 1 NM02764AS 25101 RT ELEVATOR TAB OB FWD LWR CORNER HAS EDGE DAMAGE. REMOVED DAMAGED ELEVATOR TAB, ORDERED AND REPLACED ELEVATOR TAB IAW AMM. (K) 2L72 4F RTA16WE 20060411002362006041100236NM 2006 4 11 ASAA0510064 120050414A5330654576647 SKIN BOEING737 737290C 138448VNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 CRACK AT FASTENER, WINDOW 10R BSTA 500A=15R-LOWER AFT CORNER. CRACKED FASTENER HOLE AT WINDOW 10R BSTA 500A=15R LOWER AFT CORNER REPAIRED IAW EA. (K) 2L72 4F A16WE 20060411002432006041100243EU 2006 4 11 KBM2006F00132 120050815A3310704A46014049 RHEOSTAT SNIAS 350 AS350B2 8680813EU INST LIGHT SYS INOPERATIVE E KBMAO OTHER O OTHER ININSP/MAINT 1 WP19350SH 2957 INSTRUMENT LIGHTS INOPERATIVE IN NR 1 CIRCUIT, REMOVED AND REPLACED DIMMER BOX. (K) 1G71 3U H9EU 20060411002442006041100244 2006 4 11 KBM2006F00133 420051117A34143839949002 INDICATOR SNIAS 350 AS350B2 8680813EU AIRSPEED IND READS HIGH E KBMAO OTHER O OTHER ININSP/MAINT 1 WP19350SH 2957 UNIT READS 10 KNOTS OFF, REMOVED AND REPLACED. (K) 1G71 3U H9EU 20060412000502006041200050NM 2006 4 12 ASAA0540649 120051114A531165465575 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE-CORROSION ON LOWER FRAME CHORD. REMOVED AND REPLACED LOWER FRAME CHORD IAW SRM. (K) 2L72 4F RTA16WE 20060412000542006041200054NM 2006 4 12 ASAA0540652 120051114A531065C26603201 BEAM BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE- NR3 SLAT LWR T/E SKIN AT OB AUX TRACK, 5 EA CRACKS THROUGH FASTENER HOLES. REPAIRED IAW SRM. (K) 2L72 4F RTA16WE 20060412000852006041200085NM 2006 4 12 ASAA0540753 120051221A53206545875U70 SILL BOEING737 7374Q8 138447QNM BS 270-360 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02780AS 25112 PAE-CORROSION AT R-1 DOORWAY MOPSILL FROM BSTA 270-360. REMOVED AND REPLACED R-1 DOOR MOPSILL IAW SRM. (K) 2L72 4F RTA16WE 20060413002032006041300203NM 2006 4 13 ASAA0510047 120050411A531165622063 FRAME BOEING737 737290C 138448VNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 YXX - NDT CRACK INDICATION AT FASTENER HOLE ON FRAME TO SKIN ATTACHMENT AT BSTA 460 BETWEEN STRINGER 21L AND STRINGER 22L. REPAIRED FRAME IAW SRM. (K) 2L72 4F A16WE 20060413002082006041300208NM 2006 4 13 ASAA0510051 120050411A53226546532590 SHEAR TIE BOEING737 737290C 138448VNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 YXX- NDT CRACK INDICATION AT FASTENER HOLE ON SHEAR TIE ANGLE AT BSTA 480 BETWEEN STR 18L AND STR 19L. REPLACED SHEAR TIE ANGLE IAW SRM. (K) 2L72 4F A16WE 20060413002132006041300213NM 2006 4 13 ASAA0540213 120050114A324426098011 TIRE BOEING737 7374Q8 138447QNM MLG TIRE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS4948 988 25107 DURING REPLACEMENT OF NR1 MLG TIRE FOUND NR 1 MLG BRAKE PAD DAMAGE. REMOVED AND REPLACED NR1 MLG TIRE AND BRAKE. PERFORMED CONDITIONAL INSPECTION, AND REPLACED BRAKE GASKET. (K) 2L72 4F RTA16WE 20060413002172006041300217NM 2006 4 13 ASAA0510038 120050404A53136552928594 STRINGER BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 YXX - AFT CARGO PIT BSTA 827, STR 21L SPLICE HAS CORROSION. AFT CARGO PIT BSTA 827, STR 21L REPAIRED IAW SRM. (K) 2L72 4F A16WE 20060414000022006041400002NM 2006 4 14 MASA200500766 120051003A2710LA11A2118 ACTUATOR DHAV DHC8 DHC8202 2809007NM AILERONS MALFUNCTIONED A MASAO OTHER F FLT CONT AFFECTED CRCRUISE 1 SW07447YV8374 8374 447 ASH 7049 DEN, AILERON TRIM MALFUNCTIONED IN FLIGHT. PILOT DECLARED AND EMERGENCY. WORK IS IN PROGRESS. MX R2 AILERON RUDDER TRIM CONTROL PANEL AND AILERON TRIM ACTUATOR. 2H72 4T RTA13NM 20060414000342006041400034EA 2006 4 14 ASOA051152 120051225A3350362624 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27846AS 7328 DURING A HANGAR INSPECTION IN MCN, THE FORWARD AND AFT FLOOR EMERGENCY STRIP LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD AND AFT FLOOR EMERGENCY STRIP LIGHTS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060414000402006041400040EA 2006 4 14 ASOA051151 120051225A3397 WIRE CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT DAMAGED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27738EV 10146 DURING A GROUND INSPECTION IN SLC, THE EMERGENCY EXIT SIGN, DS158, WAS FOUND TO BE INOPERATIVE. MAINTENANCE FOUND AND REPAIRED DAMAGED WIRING AT CANNON PLUG P341. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060414000412006041400041EU 2006 4 14 ASOA051143 120051223A3350 LIGHT AEROSPATR72 ATR72212 8680945EU CABIN MALFUNCTIONED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27633AS 344 DURING A GROUND INSPECTION, THE BACK EMERGENCY LIGHTS STAY ON WHEN ARMED AND DURING TAXI. MAINTENANCE CYCLED THE EMERGENCY LIGHTS TOGGLE SWITCH IN THE ARMED POSITION WITH NO DEFECTS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2H72 4T RTA53EU 20060414000422006041400042EU 2006 4 14 ASOA051142 120051223A33507012210 LAMP AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27636AS 375 DURING A HANGAR INSPECTION, THE EMERGENCY FLOODLIGHT, ON THE PASSENGER DOOR STEPS, WAS FOUND TO BE INOPERATIVE. MAINATENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY FLOOD LIGHT ASSY, ON THE PASSENGER DOOR STEPS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2H72 4T RTA53EU 20060414000432006041400043EU 2006 4 14 ASOA051140 120051222A33503011162 LENS AEROSPATR72 ATR72212 8680945EU EMERGENCY EXIT CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27634AS 370 DURING A HANGAR INSPECTION, THE EMERGENCY EXIT LIGHT LENS COVERS, AT ROWS 17, 10, 8 AND 1, WERE FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LENS COVERS, AT ROWS 17, 10, 6 AND 1. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2H72 4T RTA53EU 20060414000442006041400044EA 2006 4 14 ASOA051136 120051221A3610328955902 CLAMP CNDAIRCL600 CL6002B19 1900309EA ENGINE LOOSE A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27820AS 7188 DURING CLIMB OUT, THE CREW RECEIVED A LT JET OVERHEAT MESSAGE. THE CREW COMPLIED WITH THE QRH WHEN THEY RECEIVED A LT 10TH DUCT WARNING MESSAGE. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED TO DEPARTURE, WHERE IT LANDED SAFELY. MAINTENANCE INSPECTED AIRCRAFT AND FOUND THE ENGINE SIDE OF THE 14TH STAGE SHUTOFF VALVE PIPE CLAMP LOOSE. MAINTENANCE TIGHTENED THE CLAMP AND RAN THE ENGINE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F RTA21EA 20060414000452006041400045EU 2006 4 14 ASOA051141 120051222A3350S3358100500062 LIGHT AEROSPATR72 ATR72212 8680945EU CABIN BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27634AS 370 DURING A HANGAR INSPECTION, THE EMERGENCY FLOODLIGHT, ON THE PASSENGER DOOR STEPS, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOODLIGHT ASSY ON THE PASSENGER DOOR STEPS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2H72 4T RTA53EU 20060414000462006041400046EA 2006 4 14 ASOA051139 120051222A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA MAIN PAX OBSTRUCTED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27900EV 7608 DURING A GROUND INSPECTION, THE PAX DOOR WAS FOUND DIFFICULT TO CLOSE. MAINTENANCE REMOVED AND OBJECT FROM THE BOTTOM OF THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F RTA21EA 20060414000472006041400047EA 2006 4 14 ASOA051137 120051222A3350BA50933901 CHARGER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSINOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27924EV 7830 DURING A GROUND INSPECTION, THE FWD CEILING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY BATTERY CHARGER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F RTA21EA 20060414000482006041400048EA 2006 4 14 ASOA051154 120051226A33508GH00247308 LAMP CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT BURNED OUT A ASOAO OTHER O OTHER NRNOT REPORTED 1 SO27705EV 10051 DURING A HANGAR INSPECTION IN BTR, THE EXTERIOR RIGHT SIDE EMERGENCY LIGHT, JUST AFT OF THE EMERGENCY EXIT DOOR, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EXTERIOR RIGHT SIDE EMERGENCY LIGHT, JUST AFT OF THE EMERGENCY EXIT DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060412000812006041200081NM 2006 4 12 ASAA0650642 120051110A533065458661205 SKIN BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - CORROSION ON SKIN UNDER NR 2 DME ANTENNA. REMOVED AND REPLACED SKIN IAW SRM. (K) 2L72 4F RTA16WE 20060413001952006041300195NM 2006 4 13 ASAA0570080 120051005A5320143A9403188 WEB BOEING737 737790 13844CNNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02615AS 30344 PAE: DURING C-CHECK, FOUND CLOSE OUT WEB CRACKED AT BS 492. REPAIRED IAW SRM. (K) 2L72 4F RTA16WE 20060413002012006041300201NM 2006 4 13 ASAA0570077 120051005A5340143A750116 SUPPORT BOEING737 737790 13844CNNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02615AS 30344 PAE: DURING C-CHECK FOUND FLOOR TO SIDEWALL SUPPORT CORRODED AT BS 500A. REPAIRED IAW SRM. (K) 2L72 4F RTA16WE 20060413002042006041300204NM 2006 4 13 ASAA0510053 120050411A53136545767518 STRINGER BOEING737 737290C 138448VNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 YXX - NDT CRACK INDICATION AT FASTENER HOLES ON STR 20L, BSTA 460-481. REPAIRED IAW SRM. (K) 2L72 4F A16WE 20060413002072006041300207NM 2006 4 13 ASAA0510049 120050411A531165622063 FRAME BOEING737 737290C 138448VNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 YXX- NDT CRACK INDICATION AT FASTENER HOLE ON FRAME TO SKIN ATTACHMENT AT BSTA 480 BETWEEN STRINGER 19L AND STRINGER 20L. REPAIRED FRAME IAW SRM. (K) 2L72 4F A16WE 20060413002142006041300214NM 2006 4 13 ASAA0510035 120050401A53136552928517 STRINGER BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 YXX - AFT CARGO PIT BSTA 807-847, STR 26L SPLICE HAS CORROSION. AFT CARGO PIT BSTA 807-847, STR 26L REPAIRED IAW SRM. (K) 2L72 4F A16WE 20060413002162006041300216NM 2006 4 13 ASAA0510040 120050404A531165622063 FRAME BOEING737 737290C 138448VNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 YXX - FWD CARGO BSTA 480 FRAME CRACKED NEAR STR 22L. FRAME REPAIRED IAW SRM. (K) 2L72 4F A16WE 20060414000632006041400063NM 2006 4 14 ASAA0570111 120051203A5730116A760012 SKIN BOEING737 737790 13844CNNM RT WING TOOL DAMAGE A ASAAK NONE O OTHER ININSP/MAINT 1 NM02611AS 29753 SEA: DURING SCHEDULED MTX FOUND L/E LWR SURFACE DEFORMED AT WBL 658.17. REPAIRED IAW EA. (K) 2L72 4F RTA16WE 20060414000692006041400069NM 2006 4 14 ASAA0540674 120051121A5311654654929 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE: CORROSION ON LOWER FRAME CHORD AT BSTA 767, STR 25R TO 26 R. REMOVED AND REPLACED SHEAR TIE IAW SRM. (K) 2L72 4F RTA16WE 20060414000702006041400070NM 2006 4 14 ASAA0570104 120051024A5320141A5410U12 INTERCOSTAL BOEING737 737790 13844CNNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02624AS 30778 PAE: DURING C-CHECK FOUND CRACKED INTERCOSTAL AT BS 328. REPAIRED IAW SRM. (K) 2L72 4F RTA16WE 20060414000722006041400072NM 2006 4 14 ASAA0540748 120051220A5315654681025 FLOORBEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02780AS 25112 PAE: CORROSION ON FLOORBEAM. BLENDED CORROSION, FABRICATED REPAIR STRAP AND INSTALLED IAW SRM. (K) 2L72 4F RTA16WE 20060414000762006041400076NM 2006 4 14 ASAA0540760 120051227A532065C33495U2 WEB BOEING737 7374Q8 138447QNM FUSELAGE TOOL DAMAGE A ASAAK NONE O OTHER ININSP/MAINT 1 NM02780AS 25112 PAE: RT SHEAR WEB AT BSTA 1016 BL 0, DAMAGED BELOW OVERLAP OF LT SHEAR WEB. FOUND PUNCTURE DAMAGE TO BE OUT OF LIMITS AT BSTA 1016, WL 208, RT SHEAR WEB. REMOVED AND REPLACED RT SHEAR WEB THROUGHOUT BS1016-1026, RBL 0-29 IAW SRM. (K) 2L72 4F RTA16WE 20060414000772006041400077NM 2006 4 14 ASAA0540759 120051228A53206546579Y619 STIFFENER BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02780AS 25112 PAE: CORROSION ON TORQUE BOX STIFFENER. REMOVED AND REPLACED STIFFENER IAW SRM. (K) 2L72 4F RTA16WE 20060414000782006041400078NM 2006 4 14 ASAA0540757 120051228A53206546579531 STIFFENER BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02780AS 25112 PAE: CORROSION ON TORQUE BOX STIFFENER. REMOVED AND REPLACED STIFFENER IAW SRM. (K) 2L72 4F RTA16WE 20060414000822006041400082NM 2006 4 14 ASAA0540739 120051216A5320654652850 SUPPORT BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02795AS 28890 PAE: CORROSION ON FLOOR TO SIDEWALL SUPPORT. REMOVED DAMAGED SUPPORT, FABRICATED AND NEW SUPPORT PIECE AND INSTALLED IAW SRM. (K) 2L72 4F RTA16WE 20060414000832006041400083NM 2006 4 14 ASAA0540755 120051222A5320654795732 INTERCOSTAL BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02780AS 25112 PAE: CORROSION ON INTERCOSTAL AT BSTA 771, RBL 19, WI 156. REMOVED AND REPLACED INTERCOSTAL IAW SRM. (K) 2L72 4F RTA16WE 20060414000842006041400084NM 2006 4 14 ASAA0540756 120051228A531369489503 STRINGER BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02780AS 25112 PAE: CORROSION ON STRINGER END FITTING. REMOVED AND REPLACED FITTING IAW SRM. (K) 2L72 4F RTA16WE 20060414000862006041400086EA 2006 4 14 AOSA051110 120051217A5320 CAP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 DURING A C-CHECK, THE FLOOR SUPPORT CAP AT RBL 9, BETWEEN FS 559+64 AND FS 559+80, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO MFG FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE C/A. (K) 2L72 4F RTA21EA 20060417000262006041700026NE 2006 4 17 MASA200500578 220050720A72616052T16G01 TUBE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE OIL SCAVENGE UNKNOWN A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW0727318 7318 ASH 6414 DRO, IN FLIGHT ENGINE SHUTDOWN OF NR 1 ENGINE DUE TO LOW OIL PRESSURE. MAINTENANCE REPLACED THE TURBINE REAR FRAME C-SUMP SCAVENGE TUBE AND SEALS. 2L72 4F4 FRTA21EA E15NE 20060417000292006041700029EA 2006 4 17 MASA200500307 120050420A3230 LANDING GEAR CNDAIRCL600 CL6002B19 1900309EA NOSE WARNING LIGHT A MASAO OTHER J WARNING INDICATION DEDESCENT 1 SW0727314 7314 ASH 6424 MFR TO PHX, UPON DESCENT INTO PHX, THE NOSE GEAR WAS SLOW TO EXTEND AND A GEAR DISAGREE WARNING WAS DISPLAYED. MAINTENANCE PERFORMED SEVERAL GEAR SWINGS ON EACH HYDRAULIC PUMP WITH NO FAULTS FOUND. 2L72 4F RTA21EA 20060417000552006041700055EA 2006 4 17 MASA200501050 120051218A2760 SPOILER SYS CNDAIRCL600 CL6002B19 1900309EA WARNING LIGHT A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW077291Z 7291 ASH 6089 MRY, CONFIGURATION SPOILERS MESSAGE. MAINTENANCE RESET SYSTEM. OPS CHECK GOOD. 2L72 4F RTA21EA 20060413001112006041300111EU 2006 4 13 SA06022 120050409A5610NP1653116 WINDSHIELD AIRBUSA319 A319112 3930323EU COCKPIT CRACKED A USAAH DEACTIVATE SYST/CIRCUITS A FLAME/FIRE CRCRUISE 1 EA19764US15732 1369 DURING FLIGHT, THE RIGHT SIDE WINDSHIELD ARCED, THEN CRACKED THE OUTER PANE OF THE WINDSHIELD. THE CIRCUIT BREAKER WAS PULLED FOR THE NR 2 WINDSHIELD HEAT COMPUTER. FLIGHT CONTINUED TO DESTINATION AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT SIDE WINDSHIELD. OPERATIONALLY CHECKED THE WINDSHIELD HEAT COMPUTERS AND THE ICE PROBE LIGHT. ALL CHECKS OK. OK FOR SERVICE. 2L72 4F RTA28NM 20060413001722006041300172NM 2006 4 13 ASAA0510062 120050414A5330654576647 SKIN BOEING737 737290C 138448VNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 YXX- CRACK AT FASTENER, WINDOW 6R BSTA 455R - LOWER AFT CORNER. CRACKED FASTENER HOLE AT WINDOW 6R BSTA 455 LOWER AT CORNER REPAIRED IAW EA. (K) 2L72 4F A16WE 20060413001942006041300194NM 2006 4 13 ASAA0570072 120050923A5320141A85123 WEB BOEING737 737790 13844CNNM FUSELAGE PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02647AS 33012 PAE: DURING C-CHECK FOUND E AND E BAY DOOR CUTOUT LT SIDE DOOR LOCK WEB AT FITTING HAS A PUNCTURE. REPAIRED IAW SRM. (K) 2L72 4F RTA16WE 20060413002022006041300202NM 2006 4 13 ASAA0510050 120050411A532065001612 SHEAR TIE BOEING737 737290C 138448VNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 YXX - NDT CRACK INDICATION AT FASTENER HOLE ON SHEAR TIE ANGLE AT BSTA 480 BETWEEN STR 19L AND STR 20L. REPLACED SHEAR TIE ANGLE IAW SRM. (K) 2L72 4F A16WE 20060413002232006041300223NM 2006 4 13 ASAA0510039 120050404A53136552928580 STRINGER BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02730AS 22577 YXX- AFT CARGO PIT BSTA 827, STR 23L SPLICE HAS CORROSION. AFT CARGO PIT BSTA 827, STR 23L REPAIRED IAW SRM. (K) 2L72 4F A16WE 20060413002622006041300262NM 2006 4 13 ASAA0570092 120051009A5320146A75032 FLOOR SUPPORT BOEING737 737790 13844CNNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02615AS 30344 PAE: DURING C-CHECK FOUND CORROSION ON FLOOR SUPPORT AT BS 773. REPAIRED IAW EA. (K) 2L72 4F RTA16WE 20060413002632006041300263NM 2006 4 13 ASAA0570093 120051009A5320146A75036 FLOOR SUPPORT BOEING737 737790 13844CNNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02615AS 30344 PAE: DURING C-CHECK FOUND CORROSION ON FLOOR SUPPORT AT BS 773. REPAIRED IAW EA. (K) 2L72 4F RTA16WE 20060414000582006041400058EA 2006 4 14 ASOA051138 120051222A3350100865 BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHTSMISINSTALLED A ASOAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO27924EV 7830 DURING A GROUND INSPECTION, THE LT AND RT EXTERIOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE EMERGENCY BATTERY PACK AND CHARGER AND FOUND IT INSTALLED INCORRECTLY. REINSTALLED BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20060414000712006041400071NM 2006 4 14 ASAA0540749 120051219A5210507945249 SKIN BOEING737 7374Q8 138447QNM DOOR CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02780AS 25112 PAE: L-1 DOOR INNER SKIN CRACKED ON FWD EDGE. REPAIRED IAW SRM. (K) 2L72 4F RTA16WE 20060414000732006041400073NM 2006 4 14 ASAA0540750 120051220A5311651630440 FRAME BOEING737 7374Q8 138447QNM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02780AS 25112 PAE: RT FRAME WEB GOUGED. INSTALLED REPAIR IAW SRM. (K) 2L72 4F RTA16WE 20060414000752006041400075NM 2006 4 14 ASAA0540758 120051228A5320654657959 STIFFENER BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02780AS 25112 PAE: CORROSION ON TORQUE BOX STIFFENER. REMOVED AND REPLACED STIFFENER IAW SRM. (K) 2L72 4F RTA16WE 20060417001312006041700131EA 2006 4 17 MASA200500634 120050812A5210 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR LACK OF LUBE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0775998 7336 ASH 7158 CLE - MAIN CABIN DOOR HARD TO CLOSE AND LOCK. MX LUBED THE OUTER HANDLE AND OPS WERE NORMAL. 2L72 4F RTA21EA 20060417001362006041700136EA 2006 4 17 MASA200500935 120051122A3010 WARNING MESSAGE CNDAIRCL600 CL6002B19 1900309EA ANTI ICE SYS ILLUMINATED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW0775991 7422 ASH 7197 ORD - ANTI-ICE DUCT WARNING MESSAGE. OPS CHECK GOOD. 2L72 4F RTA21EA 20060417001372006041700137EA 2006 4 17 MASA200500714 120050907A2760 NONE CNDAIRCL600 CL6002B19 1900309EA NONE NONE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0727318 7318 ASH 6098 PHX, SPOILER TAKEOFF CONFIG. MAINTENANCE FOUND THE SPOILER HANDLE TO BE NOT IN A DETENT. MAINTENANCE STOWED THE SPOILER HANDLE CORRECTLY AND WERE UNABLE TO DUPLICATE THE DISCREPANCY. 2L72 4F RTA21EA 20060417001662006041700166EA 2006 4 17 MASA200500649 120050817A261321804100 SENSOR CNDAIRCL600 CL6002B19 1900309EA OVERHEAT LOOP MALFUNCTIONED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW0727318 7318 ASH 6311 OKC, ABORTED TAKEOFF DUE TO THE 14TH STAGE BLEED DUCT WARNING. MAINTENANCE REPLACED THE PYLON OVERHEAT SENSE LOOP. 2L72 4F RTA21EA 20060418000082006041800008EA 2006 4 18 MASA200501055 120051219A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERS WARNING MESSAGE A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW077291Z1916912358 7291 ASH 6098 PHX - CONFIG SPOILER MESSAGE WITH SPOILER AT ZERO DETENT DURING TAKEOFF ROLL. MAINTENANCE REPLACED PCU AND OPS CHECK NORMAL. 2L72 4F RTA21EA 20060418000092006041800009EA 2006 4 18 MASA200501056 120051219A5240 SENSOR CNDAIRCL600 CL6002B19 1900309EA SERVICE DOOR UNSECURE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0727314 7314 ASH 6089 PHX, A/C WOULD NOT PRESSURIZE AND OVERWEIGHT LANDING. MAINTENANCE CORRECTLY COMPLIED WITH MEL PROCEDURE AND COMPLIED WITH OVERWEIGHT INSPECTION. SERVICE DOOR SENSOR RESECURED. 2L72 4F RTA21EA 20060418000122006041800012EA 2006 4 18 MASA200500713 120050907A3260 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA NLG DOOR OUT OF ADJUST A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07591ML ASH 2621 PHL - NOSE GEAR DOOR OPEN MESSAGE IN FLIGHT. MX ADJUSTED PROXIMITY SENSOR, JACKED A/C AND DID GEAR SWINGS. NO FURTHER DEFECTS FOUND. 2L72 4F RTA21EA 20060414000742006041400074NM 2006 4 14 ASAA0540761 120051227A532065C33495U1 WEB BOEING737 7374Q8 138447QNM FUSELAGE TOOL DAMAGE A ASAAK NONE O OTHER ININSP/MAINT 1 NM02780AS 25112 PAE: GOUGE IN WEB AT BSTA 1016, BL0, WL 208. BLENDED OUT GOUGE IN WEB AT BSTA 1016, WL 208, BL0. AREA REMOVED 1.5 INCH X 3.0. 100 INCH MATERIAL REMOVED, FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED WEB AT BSTA 1016, BL 0 WL 208 IAW SRM. (K) 2L72 4F RTA16WE 20060417000102006041700010EA 2006 4 17 MASA200500758 120050927A4990 APU CNDAIRCL600 CL6002B19 1900309EA LACK OF LUBE A MASAO OTHER WMJINADEQUATE Q C OVER TEMP WARNING INDICATION NRNOT REPORTED 1 SW07650ML 7034 ASH 2672 PHL, APU OIL TEMPATURE CAUTION MESSAGE. SVCD APU OIL ADDED 1/2 QT. OPS CHK GOOD. 2L72 4F RTA21EA 20060418000012006041800001EA 2006 4 18 MASA200500650 120050817A2100864807 PSEU CNDAIRCL600 CL6002B19 1900309EA WARNING MESSAGE A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW077305V14175 7305 ASH 6412 PHX. RETURNED TO THE FIELD DUE TO A DISPLAY COOL CAUTION IN ALL MODES IN FLIGHT. R2 PSEU OPS CHECKED GOOD ON GROUND. 2L72 4F RTA21EA 20060418000112006041800011EA 2006 4 18 MASA200500961 120051126A3230848847 PUMP CNDAIRCL600 CL6002B19 1900309EA MLG FAULTED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW077305V13126 7305 ASH 6191 PHX - GEAR DISAGREE WARNING MESSAGE. MAINTENANCE REMOVED AND REPLACED 3A PUMP AND PRIORITY VALVE. 2L72 4F RTA21EA 20060418000272006041800027EA 2006 4 18 MASA200501009 120051208A3610601R5116227 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA BLEED SYSTEM MALFUNCTIONED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW077730218239 7302 ASH 6424 PHX - 10TH STAGE ISOLATION VALVE WOULD NOT CLOSE. MAINTENANCE REMOVED AND REPLACED BLEED CONTROL PANEL. 2L72 4F RTA21EA 20060418000472006041800047EA 2006 4 18 MASA200500417 120050530A2613 CLAMP CNDAIRCL600 CL6002B19 1900309EA OVERHEAT LOOP LOOSE A MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW0777331 7331 ASH 7130 IAD - RT 14TH STAGE DUCT WARNING IN FLIGHT. MAINTENANCE REPLACED LOOP AND SECURED LOOSE CLAMP. 2L72 4F RTA21EA 20060418000542006041800054EA 2006 4 18 MASA200500910 120051117A3150 WARNING MESSAGE CNDAIRCL600 CL6002D24 1390016EA STAB ILLUMINATED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07931LR 15031 ASH 6550 LAS - STAB FAULT STATUS MESSAGE. RESET SYSTEM. OPERATIONAL CHECK NORMAL. 2L72 4F RTA21EA 20060418000932006041800093EA 2006 4 18 MASA200500865 120051107A4990 APU CNDAIRCL600 CL6002D24 1390016EA APU OVERSERVICED A MASAO OTHER WB INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW07921FJ 15021 ASH 6093 PHX, STRONG ODOR IN CABIN WITH PACKS RUNNING. DRAINED AND SERVICED APU OIL TO PROPER LEVEL. PERFORMED SYSTEMS OPERATIONAL CHECKS WITH NO DEFECTS NOTED. 2L72 4F RTA21EA 20060418000942006041800094NE 2006 4 18 MASA200500866 220051109A7200 ENGINE CNDAIRCL600 CL6002D24 1390016EA GE CF34 CF348C1 NE NR 2 FLAMED OUT A MASAD RETURN TO BLOCK XJ ENGINE FLAMEOUT WARNING INDICATION TXTAXI/GRND HDL 1 SW07902FJ 15002 ASH 6183 PHX, NR 2 ENGINE FLAMED OUT ON TAXI OUT PREVIOUSLY DSM. ALL INSPECTIONS CHECKED GOOD PER FIM AND GE. 2L72 4F4 FRTA21EA EOOO63EN 20060418001282006041800128EA 2006 4 18 MASA200500986 120051202A2780771410D SENSOR CNDAIRCL600 CL6002D24 1390016EA SLATS MALFUNCTIONED A MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW07908FJ2272 15008 ASH 6185 SAT - SLAT FAULT STATUS MESSAGE. MX REMOVED AND REPLACED RT INBD DISCONNECT SENSOR. 2L72 4F RTA21EA 20060418001332006041800133EA 2006 4 18 MASA200501045 120051216A2410 IDG CNDAIRCL600 CL6002B19 1900309EA NR 1 UNDERSERVICED A MASAO OTHER WJ INADEQUATE Q C WARNING INDICATION NRNOT REPORTED 1 SW0775994 7367 ASH 7258 MLI - NR 1 IDG CAUTION NR 1 GEN OFF CAUTION ON TAKEOFF ROLL. MAINTENANCE SERVICED NR 1 IDG. OPS CHECK GOOD. 2L72 4F RTA21EA 20060414000622006041400062NM 2006 4 14 ASAA0570110 120051126A5320141A5410012 INTERCOSTAL BOEING737 737790 13844CNNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02625AS 30792 PAE: DURING C-CHECK FOUND INTERCOSTAL CRACKED AT BS 320, WL 208 AND LBL 47. REPAIRED IAW SRM. (K) 2L72 4F RTA16WE 20060414000852006041400085EA 2006 4 14 ASOA051115 120051217A5320 CAP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 DURING A C-CHECK, THE FLOOR SUPPORT CAP, AT FS589, LBL 9, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO MFG FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE C/A. (K) 2L72 4F RTA21EA 20060417000342006041700034EA 2006 4 17 MASA200500892 120051115A2751855D1009 SENSOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07772783135 7278 ASH 6428 PHX, FLAPS FAIL AT ZERO DEGREES IN FLIGHT. MAINTENANCE REPLACED THE RT BPSU. 2L72 4F RTA21EA 20060417000352006041700035EA 2006 4 17 MASA200500476 120050618A5230 SEAL CNDAIRCL600 CL6002B19 1900309EA CARGO DOOR FAILED A MASABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW07650ML3028 7137 ASH 2635 STL, DIVERTED TO CVG DUE TO A CABIN ALT MASTER WARNING IN FLT. THE PLANE WAS CRUISING ABOVE 250 AND NOTICED THE CABIN ALT. CLIMBING ABOVE 120. THE CREW DESCENDED AND WAS ABLE TO STABILIZE THE CABIN ALT. THE PLANE LANDED IN CVG AND CONTRACT MX FOUND A CARGO DOOR SEAL BLOWN OUT, THE PAX DOOR SEAL LEAKING AND THE RT PRSOV PUTTING OUT INSUFFICIENT AIR FLOW. FERRIED TO CKB WHERE MAINTENANCE REMOVED AND REPLACED THE RT PRSOV AND REPAIRED PASSENGER DOOR. 2L72 4F RTA21EA 20060417000412006041700041EA 2006 4 17 MASA200500401 120050505A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA LAVATORY FAULTED A MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW0775991 7422 ASH 7112 MEM TO IAD, SMOKE TOILET CAUTION ON 5 MILE FINAL. FA OBSERVED NO SMOKE IN THE LAV AND THE ALARM CLEARED ITSELF. 2L72 4F RTA21EA 20060417000732006041700073EA 2006 4 17 MASA200500981 120051201A2121 FILTER CNDAIRCL600 CL6002B19 1900309EA CABIN COOLING DIRTY A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW077305V 7305 ASH 6402 LAS, DISPLAY COOL CAUTION MESSAGE WITH FLT FAN, FLT ALT AND STANDBY FAN. MAINTENANCE CLEANED FILTER, OPS CHECKED GOOD. 2L72 4F RTA21EA 20060417001272006041700127EA 2006 4 17 MASA200501083 120051226A2760 WARNING MESSAGE CNDAIRCL600 CL6002B19 1900309EA SPOILERS ILLUMINATED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07592ML 7410 ASH 7262 IAD, AIRCRAFT ABORTED TAKEOFF AND RETURNED TO GATE DUE TO STALL FAIL CAUTION AND CONFIGURE SPOILER CAUTION MESSAGES BELOW 80 KTS. MAINTENANCE RESET AND PERFORMED 5 HIGH SPEED TAXIS WITH NO REOCCURRING FAULTS. 2L72 4F RTA21EA 20060417001302006041700130EA 2006 4 17 MASA200500351 120050513A5210 MOTOR CNDAIRCL600 CL6002B19 1900309EA PAX DOOR ODOR A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW077264V 7264 ASH 6021 SAN TO PHX - DURING THE DOOR CLOSE. THE CREW NOTED THAT THE PASSENGER DOOR ASSIST MOTOR PRODUCED AN ELECTRICAL ODOR. MAINTENANCE CHECKED THE DOOR AND OPS WERE NORMAL. 2L72 4F RTA21EA 20060418000522006041800052EA 2006 4 18 MASA200500908 120051117A2750 WARNING MESSAGE CNDAIRCL600 CL6002D24 1390016EA TE FLAPS ILLUMINATED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07909FJ 15009 ASH 6092 GDL - FLAP FAULT STATUS MESSAGE. MAINTENANCE CLEARED THE INHIBITS AND THE SYSTEM OPERATES NORMALLY. 2L72 4F RTA21EA 20060418000532006041800053EA 2006 4 18 MASA200500909 120051117A3150 WARNING MESSAGE CNDAIRCL600 CL6002D24 1390016EA ILLUMINATED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07909FJ 15009 ASH 6633 LGB - RT INBD MFS PCU JAMMED WITH FLT SPOILER. MAINTENANCE PERFORMED THE SPOST, SYSTEM OPERATES NORMALLY. 2L72 4F RTA21EA 20060418000632006041800063EA 2006 4 18 MASA200501051 120051218A2120 ODOR CNDAIRCL600 CL6002D24 1390016EA CABIN DETECTED A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW07905J 15005 ASH 6437 BOI, BURNING ODOR IN THE CABIN WITH A/C STARTED. CONTRACT MAINTENANCE PERFORMED OPERATIONAL CHECKS OF APU AND ELECTRICAL SYSTEMS. NO DEFECTS NOTED. 2L72 4F RTA21EA 20060418000642006041800064EA 2006 4 18 MASA200501052 120051218A5220 SEAL CNDAIRCL600 CL6002D24 1390016EA EMERGENCY EXIT LEAKING A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07906FJ 15006 ASH 6633 PHX - EMERGENCY EXIT DOOR AT ROW 16A WAS SQUEALING IN FLIGHT. MAINTENANCE CLEANED AND LUBED THE DOOR SEAL. 2L72 4F RTA21EA 20060418001742006041800174EA 2006 4 18 MASA200500684 120050829A2150 WARNING MESSAGE CNDAIRCL600 CL6002B19 1900309EA LT A/C PACK ILLUMINATED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW0727314 7314 ASH 6334 PHX - A/C ABORTED TAKEOFF. LEFT PACK HIGH PRESSURE CAUTION MESSAGE. MX OPS CHECKED IT AND COULD NOT DUPLICATE THE DISCREPANCY. 2L72 4F RTA21EA 20060418001752006041800175NE 2006 4 18 MASA200500645 220050815A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 1 SHUTDOWN A MASAE ENGINE SHUTDOWN J WARNING INDICATION NRNOT REPORTED 1 SW0727318 7318 ASH 6373 DSM - CREW SHUTDOWN THE NR 1 ENG DECLARED AN EMERGENCY AND RTF FOR THE 14TH STAGE DUCT WARNING, WITH THE SYSTEM TURNED OFF. MX OPS CHECK SYSTEM WITH ENGINE RUN UP AND NO FURTHER MSG NOTED. 2L72 4F4 FRTA21EA E15NE 20060418002072006041800207EA 2006 4 18 MASA200500805 120051014A2760 SPOILER CNDAIRCL600 CL6002B19 1900309EA FAULTED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW077291Z 7291 ASH 6374 YUM - CONFIG SPOILER FAULT. MAINTENANCE RESET THE SECU'S AND COULD NOT DUPLICATE THE DISCREPANCY. 2L72 4F RTA21EA 20060418002082006041800208EA 2006 4 18 MASA200501007 120051207A783032725706 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER MALFUNCTIONED A MASAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SW073734215284 7342 ASH 7298 ORD - LT THRUST REVERSER UNLOCK MESSAGE ON TAKEOFF ROLL OUT. MAINTENANCE REMOVED AND REPLACED FLEX LINE AND THE ACTUATOR. 2L72 4F RTA21EA 20060419000102006041900010EA 2006 4 19 MASA200501008 120051208A2750 FLAP SYSTEM CNDAIRCL600 CL6002D24 1390016EA TE FLAPS MALFUNCTIONED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07929LR 15029 ASH 2639 CHS - FLAP CONFIG WARNING. CONTRACT MAINTENANCE RESET THE SYSTEM. NO FURTHER DEFECTS NOTED. 2L72 4F RTA21EA 20060419000122006041900012EA 2006 4 19 MASA200500875 120051111A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW0775992 7401 ASH 2717 ORD - FLAPS FAIL AT 20 DEG DURING TAXI INTO GATE. MAINTENANCE C/W PART "A". 2L72 4F RTA21EA 20060419000132006041900013EA 2006 4 19 MASA200501010 120051208A5297 WIRE HARNESS CNDAIRCL600 CL6002B19 1900309EA PAX DOOR WARN CORRODED A MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW07592ML 7410 ASH 7155 FSD - PAX DOOR WARNING IN FLIGHT. FOUND CORRODED PIN IN DOOR HARNESS. CLEANED PIN, OPS NORM. 2L72 4F RTA21EA 20060419000202006041900020EA 2006 4 19 MASA200500446 120050606A5210601R317631 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07593ML 7465 ASH 2635 STL - PAX DOOR HANDLE BROKEN. THE OUTER HANDLE BROKE OFF WHEN AIRPORT OPERATIONS TRIED TO ENTER ACFT BEFORE FIRST FLIGHT OF THE DAY. THE ACFT WAS FERRIED TO PHL, ACFT CURRENTLY OUT OF SERVICE. MAINTENANCE REMOVED AND REPLACED HANDLE. 2L72 4F RTA21EA 20060419000322006041900032EA 2006 4 19 MASA200500550 120050714A2710 CONTROL CABLE CNDAIRCL600 CL6002B19 1900309EA AILERONS BINDING A MASAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SW0777260 7260 ASH 6332 FSD - ON ARRIVAL TO PHX, CAPT WROTE UP AILERON CONTROL WHEEL BINDS IN LEFT TURN. MAINTENANCE RIGGED AILERON/FUSE AND RT WING CABLES AND PCU. 2L72 4F RTA21EA 20060419000382006041900038NE 2006 4 19 MASA200501038 220051215A7320 FADEC CNDAIRCL600 CL6002D24 1390016EA GE CF34 CF34* NE RIGHT FAULTED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07920FJ 15020 194244 ASH 2638 CLT - RIGHT FADEC FAULT. MAINTENANCE RAN ENGINES NO FAULTS FOUND. OPS CHECK NORMAL 2L72 4F4 FRTA21EA E15NE 20060419000812006041900081EA 2006 4 19 MASA200501046 120051216A499038834491 LINE CNDAIRCL600 CL6002B19 1900309EA APU FUEL SYS ODOR A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0775995 7361 ASH 7186 BNA - ODOR OF FUEL IN THE AFT CABIN. MAINTENANCE REPLACED APU FUEL LINE. 2L72 4F RTA21EA 20060418001492006041800149NM 2006 4 18 ASAA0540632 120051108A5330 SKIN BOEING737 7374Q8 138447QNM FUSELAGE BIRD STRIKE A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 OKC - FOUND FUSELAGE SKIN L/E NEAR RADOME SEAM RIGHT SIDE DAMAGED FROM BIRD STRIKE. TEMPORARY REPAIR INSTALLED, REF EM 5330-02004. REMOVED EXISTING TEMPORARY REPAIR. FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW ASA EA 5310-02519. (M) 2L72 4F RTA16WE 20060419001492006041900149EA 2006 4 19 MASA200500868 120051104A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW0777278 7278 ASH 6019 GJT - FLAP FAIL AT 20 DEG. MAINTENANCE PERFORMED PART "A" OF THE AD AND THE FAULT CLEARED. 2L72 4F RTA21EA 20060419001702006041900170EA 2006 4 19 MASA200500871 120051108A5740CC670170835 HINGE FITTING CNDAIRCL600 CL6002D24 1390016EA WING CRACKED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07917FJ 15017 FOUND FITTING CRACKED. REPAIRED IAW PART E OF SB 670BA-57-010. 2L72 4F RTA21EA 20060418000262006041800026EA 2006 4 18 MASA200500659 120050820A2750855D1009 SENSOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A MASAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 SW07651ML1936 7139 ASH 2623 PHL - DECLARED AN EMERGENCY DUE TO THE FLAPS FAILED AT 8 DEGREES. MX C/W PART A INSP AND RESET FLAPS NO DEFECTS NOTED AT THAT TIME. FLAP INSP PART B C/W WITH BOTH FLAP BPSU(S) FOUND INTERMITTENTLY BAD AND REPLACED 2L72 4F RTA21EA 20060418001142006041800114EA 2006 4 18 MASA200500337 120050506A3150 WARNING MESSAGE CNDAIRCL600 CL6002B19 1900309EA AILERONS ILLUMINATED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW0787358 7358 ASH 6493 PHX - THE CREW REJECTED A TAKEOFF FOR AN AILERON CONFIGURATION MESSAGE ON EICAS. MAINTENANCE PERFORMED HIGH SPEED TAXI TEST TO TRY TO DUPLICATE FAULT BUT COULD NOT. 2L72 4F RTA21EA 20060418001502006041800150NM 2006 4 18 ASAA0540621 120051108A534065C1612123 FITTING BOEING737 7374Q8 138447QNM BS 344 GIRT BAR CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND CORROSION ON L-1 DOOR GIRT BAR FITTING. REMOVED AND REPLACED IAW B737-400 SRM 51-40-02 AND 53-00-07. (M) 2L72 4F RTA16WE 20060418001522006041800152EA 2006 4 18 MASA200501070 120051222A3260 SENSOR CNDAIRCL600 CL6002B19 1900309EA MLG OUT OF ADJUST A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW0775992 7401 GEAR DISAGREE MESSAGE AFTER TAKEOFF. NOSE GEAR DID NOT RETRACT. MAINTENANCE CLEANED STRUT AND ADJUSTED SENSOR AND PERFORMED GEAR SWINGS. OPS CHECK GOOD. 2L72 4F RTA21EA 20060419000312006041900031EA 2006 4 19 MASA200500549 120050714A2760 COMPUTER CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A MASAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SW0777302 7302 ASH 6041 SBP - ABORTED TAKEOFF AND RETURN TO THE GATE DUE TO A CONFIG SPOILER WARNING. MX RE-RACKED COMPUTER AND RESET SYSTEM OPERATIONAL CHECK GOOD, ACFT CONTINUED OPERATIONS. 2L72 4F RTA21EA 20060419000332006041900033EA 2006 4 19 MASA200500551 120050714A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERS UNKNOWN A MASAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SW0777302185 7302 ASH 6678 LAS - ABORTED TAKEOFF AND RETURN TO THE GATE DUE TO A CONFIG SPOILER WARNING. MX REPLACED LT SPOILERON PCU AND PERFORMED HIGH SPEED TAXI RUNS. OPS CHECKED GOOD WITH NO FUTHER FAULT IN MDC. 2L72 4F RTA21EA 20060419000742006041900074NM 2006 4 19 MASA200501054 120051219A2730849557 SPU DHAV DHC8 DHC8202 2809007NM NR 2 MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07989HA2098 427 ASH 6323 GJT, NR 2 SPU CAUTION LIGHT ILLUMINATED. FERRIED TO PHX. MAINTENANCE REMOVED AND REPLACED SPU. OPS CK GOOD. 2H72 4T RTA13NM 20060420000042006042000004NM 2006 4 20 ASAAA0540666 120051118A53206552878U102 SILL BOEING737 7374Q8 138447QNM FS 947-996 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - FOUND CORROSION AT AFT ENTRY DOOR MOPSILL BS 947-996, LBL 52, WL 208 AND CRACKED AT BS 994. REMOVED AND REPLACED AFT ENTRY MOPSILL PER B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060420000052006042000005EA 2006 4 20 MASA200500667 120050823A215078279015 ACM CNDAIRCL600 CL6002B19 1900309EA LEFT SMOKE A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW07273182394 7318 ASH 6499 FAT - SMOKE COMING OUT OF COCKPIT AIR CONDITIONING VENTS AND LEFT PACK WENT TO 107 DEGREES. CONTRACT MX FOUND SMOKE TO BE FROM LEFT PACK, THEY PLACED LEFT PACK ON MEL. ACFT CONTINUED OPERATIONS. MX LATER REMOVED AND REPLACED THE ACM. 2L72 4F RTA21EA 20060420000122006042000012EA 2006 4 20 MASA200500763 120051001A2611 SMOKE WARNING CNDAIRCL600 CL6002B19 1900309EA LAVATORY FALSE ACTIVATIONA MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW0775992 7401 ASH 7150 IAD - SMOKE TOILET MASTER CAUTION LIGHT ILLUMINATED. MX RESET CIRCUIT BREAKERS. 2L72 4F RTA21EA 20060420000232006042000023EA 2006 4 20 MASA200500890 120051115A2760 SPOILER SYS CNDAIRCL600 CL6002D24 1390016EA UNKNOWN A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07903FJ 15003 ASH 6119 PHX - LEFT INBOARD MULTI-FUNCTION SPOILER FAIL ON DEPLOYMENT. CONTRACT MAINTENANCE RESET THE SYSTEM. OPERATIONAL CHECK NORMAL. 2L72 4F RTA21EA 20060420000242006042000024EA 2006 4 20 MASA200500893 120051115A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA UNKNOWN A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0777278 7278 ASH 6021 ICT - FLAPS FAILED AT 8 DEGREES ON TAXI IN. MAINTENANCE RESET AND COMPLIED WITH PART A. 2L72 4F RTA21EA 20060420000302006042000030EA 2006 4 20 MASA200500723 120050912A2750 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS OUT OF RIG A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW077264V 7264 ASH 6237 PHX - RETURNED TO FIELD DUE TO FLAPS FAIL AT ZERO. MAINTENANCE RE-RIGGED BPSU, OPS CHECKED GOOD. 2L72 4F RTA21EA 20060420000382006042000038EA 2006 4 20 MASA200500325 120050430A3230895304 PROXIMITY SENSOR CNDAIRCL600 CL6002D24 1390016EA MLG MALFUNCTIONED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07934FJ17 15034 ASH 6093 PHX TO LGB - THE CREW RETURNED TO THE FIELD DUE TO THE GEAR NOT RETRACTING. MAINTENANCE REMOVED AND REPLACED THE PSEU. 2L72 4F RTA21EA 20060418002002006041800200EA 2006 4 18 MASA200500880 120051021A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW0777278 7278 ASH 6022 FAT - FLAP FAIL IN FLIGHT AT 0 DEGREES. MAINTENANCE RESET THE FLAP SYSTEM AND COMPLIED WITH PART A OF FLAP FAIL INSPECTION. 2L72 4F RTA21EA 20060418002022006041800202EA 2006 4 18 MASA200500594 120050726A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLT SPOILER WARNING MESSAGE A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07651ML3395 7139 ASH 2631 PHL - MASTER WARNING FOR SPOILERS, CONFIG SPOILERS AT TAKEOFF POWER. MX REPLACED A SPOILER PCU. 2L72 4F RTA21EA 20060419000112006041900011EA 2006 4 19 MASA200501011 120051208A5210 TORQUE TUBE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR OUT OF ADJUST A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07592ML 7410 ASH 9001 OKC - PAX DOOR WARNING MESSAGE IN FLIGHT. MAINTENANCE ADJUSTED TORQUE CAM TUBE. 2L72 4F RTA21EA 20060419000392006041900039EA 2006 4 19 MASA200501042 120051215A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0727314 7314 ASH 6499 PHX - FLAPS FAIL AT 20 DEGREES. MAINTENANCE PERFORMED AD PART A. OPS CHECKED GOOD. 2L72 4F RTA21EA 20060419000892006041900089EA 2006 4 19 MASA200500769 120051004A2760 SPOILER CNDAIRCL600 CL6002B19 1900309EA UNWANTED DEPLOY A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07650ML 7137 ASH 2661 PHL - UNCOMMANDED SPOILER DEPLOYMENT. MX RESET AND OPS CHECKED SYSTEM, OPS CHECK GOOD. 2L72 4F RTA21EA 20060419001272006041900127EA 2006 4 19 MASA200500869 120051022A2750 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW077727810905 7278 ASH 6383 DSM - FLAP FAIL AT 8DEG. MAINTENANCE REPLACED THE BPSU. 2L72 4F RTA21EA 20060419002082006041900208EA 2006 4 19 MASA200500974 120051129A2410755469D IDG CNDAIRCL600 CL6002B19 1900309EA NR 2 WARNING MESSAGE A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07715SF2922 7115 ASH 2918 CHA, IDG 2 CAUTION MSG. MAINTENANCE MEL'D IDG. REPOSITIONED TO CLT. MAINTENANCE REMOVED AND REPLACED IDG. 2L72 4F RTA21EA 20060419002102006041900210EA 2006 4 19 MASA200500984 120051202A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07759985918 7336 ASH 7172 GSP, FLAPS FAILED 8 DEGREES. MAINTENANCE REMOVED AND REPLACED RT BPSU. 2L72 4F RTA21EA 20060420000462006042000046NE 2006 4 20 MASA200500421 220050531A7200 NONE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NONE A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW0717358 7358 ASH 6087 PHX - ABORTED TAKEOFF DUE TO THE ENGINE 2 OVERTEMP ON TAKEOFF ROLL. WITHIN LIMITS PER MANUAL 2L72 4F4 FRTA21EA E15NE 20060420000482006042000048EA 2006 4 20 MASA200501074 120051224A2150GG670950095 ACM CNDAIRCL600 CL6002D24 1390016EA LEFT SMOKE A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW07914FJ5521 15014 ASH 6193 PHX - LT AC PACK FAIL, GRINDING NOISE, FUMES AND LIGHT SMOKE. MAINTENANCE INSPECTED AND FOUND PACK FAILED. DEFERRED PACK. MAINTENANCE REMOVED AND REPLACED ACM 2L72 4F RTA21EA 20060420000492006042000049EA 2006 4 20 MASA200501078 120051224A27413094334 SWITCH CNDAIRCL600 CL6002B19 1900309EA PITCH TRIM DIRTY A MASAO OTHER O OTHER NRNOT REPORTED 1 SW077264V 7264 ASH 6168 SBP - FIRST OFFICERS STAB TRIM SWITCH INOPERATIVE. MAINTENANCE REPLACED SWITCH. 2L72 4F RTA21EA 20060420000512006042000051EA 2006 4 20 MASA200501079 120051224A2410 IDG CNDAIRCL600 CL6002B19 1900309EA NR 2 LACK OF LUBE A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW0775992 7401 ASH 7200 IAD - AIRCRAFT ABORTED TAKEOFF FOR IDG NR 2 FAULT WITH GEN 2 OFF MESSAGE. MAINTENANCE SERVICED THE IDG AND OPS CHECK NORMAL. 2L72 4F RTA21EA 20060420000522006042000052EA 2006 4 20 MASA200501076 120051224A2740 UNKNOWN CNDAIRCL600 CL6002B19 1900309EA UNKNOWN A MASAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW07650ML 7137 ASH 7172 ORD - DIVERTED AND DECLARED AN EMERGENCY TO CLT DUE TO THE MACH AND STAB TRIM CAUTION MESSAGES. RESET SYSTEM PERFORMED OPS CHECKED GOOD. 2L72 4F RTA21EA 20060420000812006042000081EA 2006 4 20 MASA200500968 120051127A2150GG670950095 ACM CNDAIRCL600 CL6002D24 1390016EA LEFT OVERHEATED A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW07902FJ4865 15002 ASH 6526 PVR - SMOKE IN THE COCKPIT AND THE LT PACK WENT TO 98° C. MAINTENANCE MEL'D LT AIR CONDITION PACK. MX REMOVED AND REPLACED AIR CYCLE MACHINE. 2L72 4F RTA21EA 20060420000882006042000088NE 2006 4 20 MASA200500467 220050614A7200 NONE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NONE A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW0787353 7353 ASH 6169 LAS - ABORTED TAKEOFF DUE TO THE NR 2 ENGINE OVERTEMP ON TAKEOFF ROLL 904 DEG FOR 4 SECONDS. MX FOUND THE ENGINE TO NOT EXCEED AMM LIMITS. MAINTENANCE PERFORMED A COMP WASH. 2L72 4F4 FRTA21EA E15NE 20060420001022006042000102EA 2006 4 20 MASA200501097 120051231A4990 B-NUT CNDAIRCL600 CL6002B19 1900309EA APU FUEL LINE LEAKING A MASAO OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW07591ML 7388 ASH 7230 ORD - FUEL LEAKING FROM APU SHROUD. RESECURED TWO FUEL LINE B-NUTS. MAINTENANCE PLACED APU ON DEFERRAL SO SHROUD COULD COMPLETELY PURGE OF FUMES. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE COULD NOT DUPLICATE LEAK. 2L72 4F RTA21EA 20060420001232006042000123 2006 4 20 MASA200500776 420051007A3418 STALL WARNING CNDAIRCL600 CL6002B19 1900309EA UNKNOWN A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07591ML 7388 ASH 2699 PHL - ABORTED TAKEOFF DUE TO A STALL FAIL AND A CONFIG SPOILER MESSAGE. MX PERFORMED, OPS CHECK OF STALL SYSTEM. OPS CHECK GOOD. 2L72 4F RTA21EA 20060420001412006042000141EA 2006 4 20 MASA200500896 120051116A3150 WARNING MESSAGE CNDAIRCL600 CL6002D24 1390016EA GE CF34 CF34* NE ACTIVATED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07938LR 15038 194287 ASH 2623 MSP - RT ENG DEGRADED MSG. CREW SHUTDOWN THE ENGINE TO RUN SHUTDOWN BIT. FAULT CHANGED TO A FADEC FAULT STATUS MSG AND MAINTENANCE RESET THE SYSTEM. 2L72 4F4 FRTA21EA E15NE 20060420001432006042000143EA 2006 4 20 MASA200501019 120051209A2797 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA NR 2 SECU UNSECURE A MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW0775991 7422 ASH 7208 ORD - RIGHT SPOILERON FAULT STATUS MESSAGE. MAINTENANCE SECURED THE NR 2 SECU RACK CONNECTION. 2L72 4F RTA21EA 20060420001452006042000145NE 2006 4 20 MASA200500463 220050613A753232895902 BLEED VALVE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 2 ENGINE FAILED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07873536036 6036 7353 872157 ABORTED TAKEOFF DUE TO A NR 2 ENG ITT ACCIDENCE. MAINTENANCE IS IN THE PROCESS OF EVALUATING THE ENGINE AND PERFORMING A HIGH ENERGY RTO INSPECTION. MAINTENANCE IS IN THE PROCESS OF EVALUATING THE ENGINE AND PERFORMING A HIGH ENERGY RTO INSPECTION. MX REPLACED 10TH STAGE VALVE. 2L72 4F4 FRTA21EA E15NE 20060419001712006041900171EA 2006 4 19 MASA200500924 120051120A4900860D10018ABC APU CNDAIRCL600 CL6002D24 1390016EA APU BAY UNKNOWN A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07921FJ6239 15021 ASH 2642 CLT - FIRE/SMOKE IN FWD LAV. MAINTENANCE REMOVED AND REPLACED APU. 2L72 4F RTA21EA 20060419002142006041900214EA 2006 4 19 MASA200500870 120051105A2750 FCU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW0777278 7278 ASH 6414 PHX - FLAP FAIL AT 20DEG. MAINTENANCE REPLACED THE FECU. 2L72 4F RTA21EA 20060420000502006042000050NE 2006 4 20 MASA200500436 220050603A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RIGHT OVERTEMP A MASAC ABORTED TAKEOFF MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 SW071735814731 7358 872628 ASH 6322 PHX - PHX TO GJT ABORTED TAKEOFF DUE TO THE RT ENGINE ITT OVERTEMP. MAINTENANCE REPLACED NR 2 ENGINE. 2L72 4F4 FRTA21EA E15NE 20060420000822006042000082EA 2006 4 20 MASA200500576 120050720A2760 UNKNOWN CNDAIRCL600 CL6002B19 1900309EA UNKNOWN A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0777302 7302 FOUND CONFIG SPOILER FAULT. CONTRACT MAINTENANCE RESET AND OPS CHECKED GOOD. 2L72 4F RTA21EA 20060420001182006042000118WP 2006 4 20 LNX2006F00000 220051108A72308934823 IMPELLER SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE331* 01514WP RT ENGINE CRACKED A LNXAK NONE O OTHER ININSP/MAINT 1 SO29438MA AC721B RT ENGINE WAS UNABLE TO REACH TAKEOFF TARGET TORQUE. ENGINE WAS REMOVED AS A PRECAUTION AND SENT FOR TEARDOWN. ENGINEERING HAS DETERMINED CAUSE TO BE A CRACKED SECOND STAGE IMPELLER RESULTING FROM CYCLIC FATIGUE. THIS IS A FOLLOW UP REPORT AND IS NOW CLOSED. (K) 2L72 4T3 TRTA8SW E2WE 20060420001782006042000178NM 2006 4 20 ASAA0540642 120051110A533065458661205 SKIN BOEING737 7374Q8 138447QNM FS 580 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02773AS 25106 PAE - FOUND CORROSION ON SKIN UNDER NR 2 DME ANTENNA. REMOVED AND REPLACED SKIN PER SRM 51-40-02. (M) 2L72 4F RTA16WE 20060420001922006042000192NM 2006 4 20 ASAA0540762 120051229A534065465262 ATTACH FITTING BOEING737 7374Q8 138447QNM FS 400 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02780AS 25112 PAE - FOUND FRAME CRACKED AT BIN RAIL ATTACH POINT. REPAIRED CRACKED FRAME IAW B737-400 SRM 53-00-07. (M) 2L72 4F RTA16WE 20060420002142006042000214EA 2006 4 20 MASA200500947 120051124A3150 WARNING MESSAGE CNDAIRCL600 CL6002B19 1900309EA ILLUMINATED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0747202 7202 ASH 7026 ORD, FLAP FAIL MESSAGE, FAIL AT 20 DEGREES. MAINTENANCE COMPLIED WITH PART A INSPECTION. 2L72 4F RTA21EA 20060421000102006042100010EA 2006 4 21 MASA200500538 120050711A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA MAIN PAX MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0717337 7337 ASH 6266 PHX - HAD A MAIN PAX DOOR THAT WAS HARD TO OPEN FROM THE INSIDE. MX COULDN'T FIND ANY FAULTS WITH THE DOOR ASSEMBLY. 2L72 4F RTA21EA 20060421000302006042100030EA 2006 4 21 MASA200501022 120051210A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERS FAULTED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07759916501 7422 ASH 7226 ORD - RIGHT SPOILERON FAULT STATUS MESSAGE. MAINTENANCE REMOVED AND REPLACED RIGHT PCU. 2L72 4F RTA21EA 20060421000422006042100042EA 2006 4 21 MASA200500752 120050925A3150 CAUTION MESSAGE CNDAIRCL600 CL6002B19 1900309EA ILLUMINATED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0775983 7481 ASH 7120 ORD - LEFT AND RIGHT PACK HIGH PRESSURE CAUTION MESSAGES AND A/C WOULD NOT PRESSURIZE. OPS CHECK GOOD, NO DEFECTS NOTED. 2L72 4F RTA21EA 20060421000432006042100043EA 2006 4 21 MASA200501090 120051228A2611 SMOKE WARNING CNDAIRCL600 CL6002B19 1900309EA CARGO BAY ILLUMINATED A MASAF ACTIVATE FIRE EXT. N FALSE WARNING CRCRUISE 1 SW0777278 7278 ASH 6412 LAS - CARGO SMOKE WARNING IN FLIGHT, PILOT DISHCARGED BOTH CARGO FIRE EXTINGUISHER BOTTLES. MAINTENANCE REPLACED THE BOTTLES AND OPS CHECK GOOD. 2L72 4F RTA21EA 20060420000222006042000022EA 2006 4 20 MASA200500888 120051115A2120GG690950261 CONTROLLER CNDAIRCL600 CL6002D24 1390016EA ACS UNKNOWN A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW07912FJ3908 15012 ASH 6431 PHX - LT PACK AUTO FAIL CAUTION WITH SMOKE IN CABIN. MAINTENANCE REMOVED AND REPLACED ACS CONTROLLER. 2L72 4F RTA21EA 20060420000532006042000053EA 2006 4 20 MASA200500439 120050604A5210 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA PAX DOOR FALSE ACTIVATIONA MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW0775992 7401 ASH 7103 IAD - PAX DOOR HANDLE THAT WOULD NOT INDICATE STOWED. MX CYCLED DOOR AND COULD NOT DUPLICATE FAULT. 2L72 4F RTA21EA 20060420000842006042000084EA 2006 4 20 MASA200501069 120051222A5270 UNKNOWN CNDAIRCL600 CL6002D24 1390016EA UNKNOWN A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07906FJ 15006 ASH 6094 COS - RT FWD EMER DOOR CAUTION MESSAGE. INDICATION SYSTEM ON MEL. MAINTENANCE COULD NOT DUPLICATE. 2L72 4F RTA21EA 20060420001092006042000109EA 2006 4 20 MASA200500370 120050519A7700 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE UNKNOWN A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW0777302 7302 ASH 6491 PHX TO ICT - THE CREW ABORTED TAKEOFF DUE TO HIGH ITT. MAINTENANCE INSPECTED THE PLANE AND ENGINE BUT COULD NOT DUPLICATE THE PROBLEM. 2L72 4F4 FRTA21EA E15NE 20060420001732006042000173NE 2006 4 20 COE2006F00001 220051027A7314 COUPLING CESSNA208 208B 2073701CE PWA PT6 PT6A114 52043NE ENGINE LOOSE E COEAK NONE O OTHER ININSP/MAINT 1 NM13953FE 870 208B0062 17196 WHEN INSPECTING FUEL PUMP IAW CAB 05-18 AND PWC1645 FOR REDDISH-BROWN STAIN ON COUPLING SHAFT AREA. FOUND NO VISIBLE SIGN. COUPLING WAS LOOSE ON SHAFT WHEN COUPLING WAS REMOVED. FOUND SPLINES WORN ON FUEL PUMP AND COUPLING. THE SB MUST SUPPLY A MEANS TO REMOVE COUPLING AND INSPECT SPLINE ON FUEL PUMP AND WEAR LIMITS SHOULD BE KNOWN FOR PROPER INSPECTION OF FUEL PUMP. (K) 1H71 3T3 T A37CE E4EA 20060420002152006042000215EA 2006 4 20 MASA200501004 120051207A3150 WARNING MESSAGE CNDAIRCL600 CL6002B19 1900309EA ILLUMINATED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0717217 7217 ASH 7140 GSP, FLAP FAIL MESSAGE. MAINTENANCE C/W PART A. 2L72 4F RTA21EA 20060421000022006042100002EA 2006 4 21 MASA200501016 120051209A2750855D1009 SENSOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW07273145834 7314 ASH 6152 DSM - FLAPS FAIL CAUTION MESSAGE. THE AIRCRAFT WAS FERRIED TO PHX FOR REPAIR. MAINTENANCE REMOVED AND REPLACED LT AND RT BPSU'S OPS CK GOOD. 2L72 4F RTA21EA 20060421000182006042100018EA 2006 4 21 MASA200501021 120051210A3150 WARNING MESSAGE CNDAIRCL600 CL6002B19 1900309EA ILLUMINATED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0775991 7422 ASH 7208 SBN - RIGHT SPOILERON STATUS MESSAGE. THE CREW RESET THE SYSTEM WITH MAINTENANCE CONTROL AND IT REQUIRED NO FURTHER ACTION. 2L72 4F RTA21EA 20060421000262006042100026EA 2006 4 21 MASA200501043 120051216A2751771410 SENSOR CNDAIRCL600 CL6002D24 1390016EA SLATS MALFUNCTIONED A MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW07904FJ6928 15004 ASH 2618 CLT - SLAT FAULT STATUS MESSAGE. MAINTENANCE REMOVED AND REPLACED THE INBOARD SLAT DISCONNECT SENSOR. 2L72 4F RTA21EA 20060424000162006042400016EA 2006 4 24 MASA200500883 120051114A2120GG670950093 ACM CNDAIRCL600 CL6002D24 1390016EA LEFT FAILED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07931LR1925 15031 ASH 6439 SAN - SMOKE IN CABIN WITH LT PACK AUTO FAIL. ISOLATED FAULT TO LT PACK. MAINTENANCE REPLACED ACM. 2L72 4F RTA21EA 20060424000212006042400021EA 2006 4 24 MASA200500856 120051103A4990 APU CNDAIRCL600 CL6002D24 1390016EA OVERSERVICED A MASAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 SW07930LR 15030 ASH 6528 PHX - AFT MAIN CABIN HAS FUMES/VAPORS SMELL. MX TROUBLESHOT AND FOUND THE APU OVERSERVICED. MX DRAINED TO PROPER LEVEL AND FOUND NO FURTHER SMELL OR VAPORS. 2L72 4F RTA21EA 20060424000272006042400027EA 2006 4 24 MASA200500872 120051110A32406007300 SENSOR CNDAIRCL600 CL6002D24 1390016EA NR 3 BRAKE MALFUNCTIONED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07927LR2396 15027 ASH 6597 LAS - NR 3 BTMS READS ABNORMAL HIGH TEMP FOLLOWED BY DASHED LINES AT NORMAL TEMPS. MAINTENANCE REMOVED AND REPLACED BTMS SENSOR. 2L72 4F RTA21EA 20060424000452006042400045EA 2006 4 24 MASA200500903 120051116A2760 SPOILER SYS CNDAIRCL600 CL6002B19 1900309EA FAULTED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07591ML 7388 ASH 7212 IAD - INBOARD/OUTBOARD GROUND SPOILER FAULT AFTER TAKEOFF. MAINTENANCE RESET THE SPOILER SYSTEM AND THE OPS CK WAS NORMAL. 2L72 4F RTA21EA 20060424000492006042400049EA 2006 4 24 MASA200500881 120051114A2410 IDG CNDAIRCL600 CL6002B19 1900309EA NR 2 GEN LACK OF LUBE A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW0777195 7195 ASH 7255 FWA - NR 2 GEN OFF ON TAKEOFF ROLL. CONTRACT MAINTENANCE SERVICED IDG. 2L72 4F RTA21EA 20060424000532006042400053EA 2006 4 24 MASA200501014 120051209A7500 ELEMENT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE BLEED AIR SYS LEAKING A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07759996926 7471 ASH 7012 GSP - ANTI-ICE WARNING ON TAKEOFF RIGHT FUSELAGE SHOWS RED. AIRCRAFT FERRIED TO CAE. MAINTENANCE REPLACED THE BLEED TEMP CONTROL UNIT AND SECURED SENSING ELEMENT. 2L72 4F4 FRTA21EA E15NE 20060424000652006042400065EA 2006 4 24 MASA200500500 120050628A2910AE4096G0060000 LINE CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM LEAKING A MASAO OTHER KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SW0717337 7337 ASH 6932 OKC - ACFT WAS REPOSITIONING TO PHX WHEN PILOT OBSERVED HYD SYS 3B WAS SHOWING DASHES ON THE QUANTITY READING. PILOT FOLLOWED THE CFM, MANUALLY DEPLOYED LANDING GEAR AND DECLARED EMERGENCY. ACFT LANDED WITH NO FURTHER INCIDENT. PRELIMINARY INVESTIGATION REVEALED 2 HYD LINES LEAKING NEAR NR 3B ACMP. LINES WERE REPAIRED AND/OR REPLACED. 2L72 4F RTA21EA 20060424000962006042400096EA 2006 4 24 MASA200500466 120050613A2163 SWITCH CNDAIRCL600 CL6002B19 1900309EA DUCT TEMP MALFUNCTIONED A MASAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW0775994 7367 ASH 7180 IAD - THE AIRCRAFT MADE A EMERG LANDING INTO PHL WITH SMOKE IN THE CABIN AND WROTE UP RT PACK DOES NOT RESPOND IN AUTO OR MANUAL. MX REPLACED THE DUCT TEMP SWITCH. 2L72 4F RTA21EA 20060424001022006042400102EA 2006 4 24 MASA200500406 120050508A5270840534 PROXIMITY SWITCH CNDAIRCL600 CL6002B19 1900309EA SERVICE DOOR MALFUNCTIONED A MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW0777260 7260 ASH 6092 LGB TO PHX - THE CAPTAIN REPORTED A SERVICE DOOR CAUTION MESSAGE IN FLIGHT. MAINTENANCE REPLACED THE PROX SWITCH. 2L72 4F RTA21EA 20060424001092006042400109EA 2006 4 24 MASA200500814 120051017A2120 ODOR CNDAIRCL600 CL6002B19 1900309EA COCKPIT DETECTED A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW07400MJ 7309 ASH 2914 BNA - ELECTRICAL SMELL IN COCKPIT. MX COULD NOT DUPLICATE. 2L72 4F RTA21EA 20060424001112006042400111EA 2006 4 24 MASA200501073 120051222A2797601R571151 WIRE HARNESS CNDAIRCL600 CL6002B19 1900309EA TE FLAPS DAMAGED A MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW0727314 7314 FLAP FAIL MESSAGE. PRESS OPS GOOD, REPLACED LT BPSU AND LEFT HARNESS. 2L72 4F RTA21EA 20060424001162006042400116EA 2006 4 24 MASA200501072 120051222A5270 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA PAX DOOR DISLODGED A MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW0727314 7314 OVERBOARD COOL CAUTION. FOUND THE ACTUATOR DISLODGED FROM PAX DOOR SWITCH. MX RECONNECTED. 2L72 4F RTA21EA 20060424001402006042400140EA 2006 4 24 MASA200500485 120050624A2760 CAUTION MESSAGE CNDAIRCL600 CL6002B19 1900309EA SPOILERS FALSE ACTIVATIONA MASAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SW0777302 7302 ASH 6375 PHX - REJECTED TAKEOFF FOR SPOILERS MASTER CAUTION ON TAKEOFF ROLL. MAINTENANCE CHECKED SPOILER SYSTEM OPS WERE NORMAL. 2L72 4F RTA21EA 20060424001432006042400143EA 2006 4 24 MASA200500952 120051125A30307858062 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA ODOR A MASAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW071721711824 7217 ASH 7154 ORD - THE CREW RETURNED TO THE FIELD FOR STRONG ELECTRICAL BURNING SMELL AND SMOKE IN COCKPIT. MAINTENANCE REMOVED AND REPLACED ADSHC. 2L72 4F RTA21EA 20060420000712006042000071SO 2006 4 20 MASA200501068 120051222A783083990168 SWITCH EMB 145 EMB145LR 3260212SO THRUST REVERSER MALFUNCTIONED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07847MJ2455 145517 ABORTED TAKEOFF DUE TO A E-2 THRUST REVERSER DISAGREE. MAINTENANCE REPLACED STOW TRIM SWITCHES. 2L72 4T RTT00011AT 20060420001052006042000105EA 2006 4 20 MASA200501096 120051231A2751 SENSOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW0777331 7331 ASH 7178 CLT - FLAPS FAILED AT ZERO. MAINTENANCE RESET SCREW SENSOR. OPS CHECK GOOD. 2L72 4F RTA21EA 20060420001132006042000113EA 2006 4 20 MASA200500850 120051101A3150 WARNING LIGHT CNDAIRCL600 CL6002D24 1390016EA UNKNOWN A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07919FJ 15019 ASH 6185 MEM - ABORTED T/O AILERON CONFIG WARNING MSG. MX RESET SYSTEM PERFORMED ENG RUNS CND. 2L72 4F RTA21EA 20060420001342006042000134EA 2006 4 20 MASA200500830 120051024A3510 OXYGEN MASK CNDAIRCL600 CL6002B19 1900309EA CABIN UNWANTED DEPLOY A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0775998 7336 ASH 7207 IAD - REAR FLIGHT ATTENDANT OXYGEN MASK POPPED OUT. MX SECURED THE MASK. 2L72 4F RTA21EA 20060420001382006042000138EA 2006 4 20 MASA200500862 120051106A261324403615 OVERHEAT SENSOR CNDAIRCL600 CL6002D24 1390016EA MLG FALSE ACTIVATIONA MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW07919FJ 15019 ASH 6729 PHX - GEAR BAY OVERHEAT WARNING MESSAGE IN FLIGHT. CONTRACT MX MET THE A/C AND INSPECTED THE MAIN GEARS, TIRES AND BRAKES AND FOUND NO FAULTS. MX PLACED THE GEAR OVERHEAT SYSTEM ON MEL AND WAS CLEARED BY REPLACING THE SENSING ELEMENT AT THE NEXT MX STATION 2L72 4F RTA21EA 20060420001422006042000142EA 2006 4 20 MASA200500884 120051114A2750 CONTROL UNIT CNDAIRCL600 CL6002D24 1390016EA UNKNOWN A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07927LR 15027 ASH 6431 PHX - FLAPS 1/2 SPEED MESSAGE ON TAXI. MAINTENANCE RESET SFECU. NO FURTHER DEFECTS NOTED. 2L72 4F RTA21EA 20060420001472006042000147EA 2006 4 20 MASA200501023 120051210A2760 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA UNKNOWN A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0775984 7489 ASH 7198 IAD - LEFT FLIGHT SPOILER CAUTION. SPOILER RETRACTED IN FLIGHT. MAINTENANCE RESET SECU. 2L72 4F RTA21EA 20060420002252006042000225EA 2006 4 20 ZJW2006F00001 220051229A852075077 CRANKSHAFT GULSTM500 500B 0141106SW LYC O540 IO540* 41532EA LT ENGINE BROKEN E ZJWAK NONE Y ENGINE STOPPAGE APAPPROACH 1 CE05667CA 1468166 PILOT REPORTED LT ENGINE QUIT ON SHORT FINAL. ENGINE FEATHERED ITSELF AND LANDED SAFELY. THE CRANKSHAFT AND CRANKCASE HAD BROKEN BETWEEN NR 4 AND NR 5 CYLINDER. THIS REAR PART OF THE ENGINE WAS SEPARATED FROM THE REST OF THE ENGINE. (K) 1H72 3O3 O 6A1 1E4 20060424000052006042400005EA 2006 4 24 MASA200500886 120051114A2720BA670905401 LIMITER CNDAIRCL600 CL6002D24 1390016EA RUDDER WARNING MESSAGE A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07935LR1559 15035 ASH 2611 CLT - RUDDER LIMIT FAULT STATUS MESSAGE. MAINTENANCE REMOVED AND REPLACED RTL RVDT. 2L72 4F RTA21EA 20060424000472006042400047 2006 4 24 MASA200500534 420050710A22106229815704 COMPUTER CNDAIRCL600 CL6002B19 1900309EA MALFUNCTIONED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07759986878 7336 ASH 7033 ORD - THE CAPTAIN REPORTED AN UNCOMMANDED RUDDER MOVEMENT IN FLIGHT. MX REMOVED AND REPLACED FCC CARDS. 2L72 4F RTA21EA 20060424001272006042400127EA 2006 4 24 MASA200500885 120051114A2410755469D IDG CNDAIRCL600 CL6002B19 1900309EA NR 2 FAILED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW077719515942 7195 ASH 7155 FSD - NR 2 IDG CAUTION AND NR 2 GEN CAUTION MESSAGES. MAINTENANCE REMOVED AND REPLACED IDG. 2L72 4F RTA21EA 20060424001872006042400187EA 2006 4 24 MASA200500917 120051118A2750860D10018ABC FCU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07772789573 5110 7278 ASH 6491 PHX - FLAP FAIL CAUTION MESSAGE IN FLIGHT AT 20 DEGREES. MAINTENANCE R2 SFECU, LEFT BPSU, LEFT FLEX SHAFT. 2L72 4F RTA21EA 20060501000852006050100085EA 2006 5 1 A6WA200540369 120051230A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA RT WING CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31432AW 7257 RT WING LWR PLANK HOLE NR 7, WS 116.366 HAS CORROSION AT IB SIDE 2 INCHES L X .005 INCH DEEP AND FWD SIDE .5 INCH L X .005 INCH D, NOT IN CRITICAL AREA. MAINTENANCE REPAIRED RT LWR WING PLANK ACCESS HOLE NR 7 IAW REO. (K) 2L72 4F RTA21EA 20060501000892006050100089EA 2006 5 1 A6WA200540374 120051230A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA KT WING CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31432AW 7257 LT LOWER WING PLANK HOLE NR 7, WS 166.366 HAS CORROSION ON IB SIDE 4 INCH L X .002 INCH D. NOT IN CRITICAL AREA. MAINTENANCE REPAIRED LT WING PLANK ACCESS HOLE NR 7 IAW REO. (K) 2L72 4F RTA21EA 20060502001862006050200186EA 2006 5 2 A6WA200540375 120051230A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31432AW 7257 FS280 FRAME CLIP AT RBL 9 ON OB SIDE IS CRACKED. MAINTENANCE REPLACED CLIP (PN 601R3111358) IAW SRM. (K) 2L72 4F RTA21EA 20060503000762006050300076EA 2006 5 3 A6WA200540376 120051230A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31432AW 7257 FS 280 FRAME CLIP AT LBL 9 OB IS CRACKED. MAINTENANCE REPLACED CLIP (PN 601R3111357) IAW SRM. (K) 2L72 4F RTA21EA 20060503001662006050300166EA 2006 5 3 A6WA200540381 120051230A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED E A6WAK NONE O OTHER ININSP/MAINT 1 GL31432AW 7257 FS 280 FRAME CLIP AT LBL 9 IB IS CRACKED. MAINTENANCE REPLACED CLIP PN 601R3111357 IAW SRM. (K) 2L72 4F RTA21EA 20060503001822006050300182EA 2006 5 3 A6WA200540380 120051228A5712 RIB CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31432AW 7257 LT BATT RIB ASSY AT WS 53.60, FS 523.8 CRACKED 1 INCH RADIUS MAINTENANCE REPAIRED BATT RIB ASSY IAW REO. (K) 2L72 4F RTA21EA 20060505000182006050500018NM 2006 5 5 AWXA200600730 120051219A5320694762616 SUPPORT FITTING BOEING757 757225 1384959NM SILL CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28907AW 22691 DURING C8 CHECK, DISCOVERED CORROSION ON FORWARD CARGO DOOR SILL SUPPORT FITTING, FORWARD ATTACH ANGLE AT BS 600, STR 26R AND WL 156. MAINTENANCE REMOVED AND INSTALLED FABRICATED SUPPORT FITTING AT BS 600, STR 26R AND WL 156 IAW BOEING 757-200 SRM 51-20-01, 51-40-02-0G AND AMM 51-21-10-7. 2L72 4F RTA2NM 20060505000192006050500019NM 2006 5 5 AWXA200600731 120051212A53206945555Y10 SUPPORT FITTING BOEING757 757225 1384959NM DOOR SILL CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28907AW 22691 DURING C8 CHECK DISCOVERED CORROSION ON FORWARD BAG PIT DOOR OPENING THRESHOLD SUPPORT FITTING AT THE AFT END OF DOOR OPENING, BEHIND DOOR SEAL AND RETAINER AT BS 620, STR 25R AND BL 70R. MAINTENANCE REMOVED AND INSTALLED REPLACEMENT THRESHOLD SUPPORT FITTING AT BS 620, STR 25R AND BL 70R IAW BOEING 757-200 SRM 51-40-02-0G. 2L72 4F RTA2NM 20060508001942006050800194WP 2006 5 8 IXXA05SMN303S 120051229A5310 DOOR FRAME DOUG DC8 DC872 302199BWP FUSELAGE CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11722CX71621 46130 DURING ROUTINE C-CHECK INSPECTION, MAIN CARGO DOOR FRAME FORMER CRACKED 2, STA 470.000 L-21L. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-0 FIG 1B (SHEET 3). REMOVED FASTENERS IAW DC8 SRM 51-1-20D. PERFORMED STOP HOLE. FABRICATED ANGLE DOUBLER (7075 O 0.125) IAW DC8 SRM 53-2-0 FIG 1B (SHEET 3), DC8 SRM 51-1-4 (FORMING). HEAT TREATED FROM 7075 O TO 7075 T6 IAW DC8 SRM 51-1-1 PAGES 1, 13, 17. APPLIED SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11. INSTALLED ANGLE DOUBLER IAW DC8 SRM 53-2-0 FIG 1B, DC8 SRM 51-1-21, DC8 SRM 51-3-0, DC-8 SRM 51-1-20D, DC-8 SRM 51-3-1 (TORQUE). 2L74 4F RT4A25 20060508001962006050800196WP 2006 5 8 IXXA05SMN314S 120051229A5730 REPAIR DOUG DC8 DC872 302199BWP RT WING IMPROPER B IXXAK NONE O OTHER ININSP/MAINT 1 SW11722CX71621 46130 DURING ROUTINE C-CHECK INSPECTION, RT WING L/E HAS NON STANDARD REPAIR, XFS 761.695. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, 06014 DATED 01-1-06, SEMAN DWG ED-4135 DATED 01-06-06, ED SEMAN 2005 1472 DATED 01-11-06. REMOVED NON STANDARD REPAIR IAW DC8 SRM 51-1-21. CUT OUT DAMAGED SECTION IAW SEMAN DWG ED-4135. FABRICATED REPAIR DOUBLER (AL 7075 T6 0.063) + (02 EA) FILLERS (AL 7075 T6 0.050) IAW SEMAN DWG ED-4135. CLEANED TREATED; PRIMED AREA + REPAIR PARTS IAW DC8 SRM 51-1-8B, APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11. INSTALLED REPAIR PARTS IAW SEMAN DWG ED-4135, DC8 SRM 51-3-0, DC8 SRM 51-1-21, DC8 SRM 51-3-1 (TORQUE). 2L74 4F RT4A25 20060508001952006050800195WP 2006 5 8 IXXA05SMN307S 120051229A5313 LONGERON DOUG DC8 DC872 302199BWP FUSELAGE CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11722CX71621 46130 DURING ROUTINE C-CHECK INSPECTION, AFT CARGO COMPT L-36 CRACKED 1.5 (STA 1180.000-1190.000). PERFORMED MAJOR REPAIR. REMOVED FASTENERS, REMOVED CRACKED LONGERON SEGMENT IAW DC-8 SRM 53-2-2- FIG 13 (SHEET 3, 4). FABRICATED NEW LONGERON SEGMENT P/N S2753715 EXTRUSION AL 7075 T6 511 IAW DC-8 SRM 53-4-1 FIG 44B ITEM R, DC-8 SRM 51-2-0 FIG 50 (SHEET 2B), DWG DACO 5750322 + SPLICE (AL 7075 T6 51 0.755) + DOUBLER (AL 7075 T6 0.160) IAW DC-8 SRM 53-2-2- FIG 13 (SHEET 3, 4). CLEANED, TREATED AND PRIMED AREA + REPAIR PARTS IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11. INSTALLED REPAIR PARTS IAW DC-8 SRM 53-2-2 FIG 13 (SHEET 3, 4), DC-8 SRM 51-1-20D, DC-8 SRM 51-3-1 (TORQUED). 2L74 4F RT4A25 20060509001082006050900108NM 2006 5 9 AWXA200600634 120051221A5320143N536654 FLOOR SUPPORT BOEING757 757225 1384959NM FUSLAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28907AW 22691 GYR - DURING C08 CHECK DISCOVERED CORROSION, LEVEL 2 EXFOLIATION, ON LOWER SURFACE OF FLOOR SUPPORT CHANNEL FOR FORWARD CARGO DOOR SILL. CORROSION ADJACENT TO ATTACH FASTENER HOLES AT BL 20R, BS 615, WL 160. CORROSION OUT OF SRM LIMITS. MAINTENANCE REMOVED FWD CARGO DOOR SILL FROM BS 560 TO BS 640 IAW BOEING SRM 51-40-02-OG. FABRICATED DOUBLER. INSTALLED FABRICATED DOUBLER IAW BOEING SRM 53-40-02. INSTALLED NEW SIDE PANEL ASSEMBLY AT BL 20R, BS 615, WL 160 IAW BOEING SRM 51-40-02. 2L72 4F RTA2NM 20060510000682006051000068NM 2006 5 10 DL73S060329 120051220A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27326DL 23098 THE FUSELAGE SKIN AT THE AFT ENTRY DOOR UPPER HINGE CUTOUT HAS A .7500 IN. CRACK AT THE UPPER CORNER. THE DAMAGED SKIN WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED. 2L72 4F RTA16WE 20060510002162006051000216NM 2006 5 10 ASAA0570082 120051005A5320141A5410U12 INTERCOSTAL BOEING737 737790 13844CNNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02615AS 30344 PAE: DURING C-CHECK, FOUND INTERCOSTAL CRACKED AT BS 336. REPAIRED IAW SRM. (K) 2L72 4F RTA16WE 20060510002402006051000240EA 2006 5 10 ASOA051131 120051220A33506100976 LAMP CNDAIRCL600 CL6002C10 1390015EA CABIN BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27759EV 10211 DURING A GROUND INSPECTION, THE EMERGENCY LIGHT, ABOVE ROW 4, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY LIGHT ASSY ABOVE ROW 4. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F RTA21EA 20060510002502006051000250EA 2006 5 10 ASOA051114 120051217A5347 TRACK CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 DURING A C-CHECK, THE FORWARD AND AFT FLOOR TRACKS, AT RBL 27.00, NEAR THE LAVATORY, WERE FOUND TO BE CORRODED BEYOND LIMITS. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCE DETERMINATION OF AN APPROPRIATE C/A. (K) 2L72 4F RTA21EA 20060510002572006051000257NM 2006 5 10 ASAA0570095 120051009A5320146A75039 FLOOR SUPPORT BOEING737 737790 13844CNNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02615AS 30344 PAE: DURING C-CHECK FOUND CORROSION ON FLOOR SUPPORT AT BS 773. REPAIRED IAW EA. (K) 2L72 4F RTA16WE 20060510002582006051000258NM 2006 5 10 ASAA0570100 120051024A5321453A261014 FLOOR PANEL BOEING737 737790 13844CNNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02624AS 30778 PAE: DURING IS CHECK FOUND FLOOR PANEL DAMAGED. REPAIRED IAW SRM. (K) 2L72 4F RTA16WE 20060510002562006051000256NM 2006 5 10 ASAA0570101 120051024A5340146A75022 SUPPORT BOEING737 737790 13844CNNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02624AS 30778 PAE: DURING IS CHECK FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT AT BS 727. REPAIRED IAW SRM. (K) 2L72 4F RTA16WE 20060511002482006051100248NM 2006 5 11 ASAA0570102 120051024A5320141A541012 INTERCOSTAL BOEING737 737790 13844CNNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02624AS 30778 PAE: DURING C-CHECK FOUND CRACKED EBAY INTERCOSTAL AT BS 321. REPAIRED IAW SRM. (K) 2L72 4F RTA16WE 20060511002872006051100287NM 2006 5 11 ASAA0570094 120051009A532014575011 FLOOR SUPPORT BOEING737 737790 13844CNNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02615AS 30344 PAE: DURING C-CHECK FOUND CORROSION ON FLOOR SUPPORT AT BS 773. REPAIRED IAW EA. (K) 2L72 4F RTA16WE 20060511002922006051100292EA 2006 5 11 ASOA051128 120051220A5320 STRUCTURE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 DURING A C-CHECK, THE FS 409+128 TO FS 559.00, AND RBL 36 TO FLOOR STR WAS FOUND TO BE CORRODED IN NUMEROUS SPOTS. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCE DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION. (K) 2L72 4F RTA21EA 20060511002952006051100295EA 2006 5 11 ASOA051132 120051220A5260 STEP CNDAIRCL600 CL6002B19 1900309EA DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27914EV 7752 DURING A GROUND INSPECTION, THE PASSENGER DOOR BOTTOM STEP WAS FOUND BROKEN. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCE DETERMINATION OF AN APPROPRIATE C/A. (K) 2L72 4F RTA21EA 20060511002532006051100253EA 2006 5 11 ASOA0511108 120051217A5242H34455 HANDLE CNDAIRCL600 CL6002B19 1900309EA AVIONICSBAY DOORCRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 7290 DURING A C-CHECK, THE FWD AVIONICS BAY DOOR HANDLE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACE THE FORWARD AVIONICS BAY DOOR HANDLE. (K) 2L72 4F RTA21EA 20060511002942006051100294EA 2006 5 11 ASOA051133 120051205A5340601R3111357 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27883AS 7504 DURING C-CHECK, THE LT FS 280 CLIP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LT FS 280 CLIP IAW SRM. (K) 2L72 4F RTA21EA 20060512000322006051200032NM 2006 5 12 ASAA0540717 120051202A53226546593 SHEAR TIE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02774AS 25107 PAE - FOUND CORROSION ON SHEAR TIE. FOUND OUT OF LIMITS, REPAIRED PER B737-400 SRM 53-00-07 FIG 20, REPAIR 3 AND ASA EA 5330-02030. (M) 2L72 4F RTA16WE 20060511002932006051100293EA 2006 5 11 ASOA051135 120051221A21507536893 COALESCER BAG CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE A/C SYS ODOR A ASOAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SO27873AS 200103141 7549 DURING TAKEOFF, THE CREW RECEIVED A (SMOKE TOILET) CAUTION MESSAGE WITH THE LAVATORY SMOKE DETECTOR PREVIOUSLY DEFERRED. THE AIRCRAFT RETURNED TO DEPARTURE, WHERE IT LANDED SAFELY. MAINTENANCE CLEANED OIL FROM BOTH PACKS AND REMOVED AND REPLACED THE COALESCER BAG. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20060515002362006051500236EA 2006 5 15 ASOA051117 120051217A5347 TRACK CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 DURING C-CHECK, ALL FLOOR TRACKS AT LBL 9 AND RBL 9 HAVE APPARENT CORROSION. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCES DETERMINATION OF AN APPROPRIATE C/A. (K) 2L72 4F RTA21EA 20060515002372006051500237EA 2006 5 15 ASOA051111 120051217A5315 CAP CNDAIRCL600 CL6002B19 1900309EA FLOOR BEAM CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 DURING A C-CHECK, THE FLOORBEAM CAP AT LBL 27, FS 574.00 TO FS 621, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO MFG FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE C/A. (K) 2L72 4F RTA21EA 20060515002382006051500238EA 2006 5 15 ASOA051109 120051217A5321 FLOOR SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 DURING A C-CHECK, THE RT SIDE PRESSURE FLOOR SKIN, AT FS 515.00, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO MFG FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE C/A. (K) 2L72 4F RTA21EA 20060512001202006051200120EU 2006 5 12 AWXA200600799 120050514A5711D57252520005 SPAR AIRBUS320 A320232 3930326EU RT WING CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28639AW 471 SAL - DURING C8 CHECK DISCOVERED CRACK IN HOLE NR 54 OF THE RT WING REAR SPAR, ACTUATOR CYLINDER ANCHORAGE. REQUIRES OVER SIZING THE HOLE BEYOND SERVICE BULLETIN LIMITS. MAINTENANCE REAMED HOLE AND INSTALLED OVERSIZED FASTENER AT THE NR 54 HOLE OF THE RT WING REAR SPAR, ACTUATOR CYLINDER ANCHORAGE IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 26-5721-05153-ES1. 2L72 4F RTA28NM 20060512001212006051200121EU 2006 5 12 AWXA200600800 120050519A5711D57252520004 SPAR AIRBUS320 A320232 3930326EU LT WING CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28639AW 471 SAL - DURING C8 CHECK DISCOVERED CRACK IN THE NR 52, 54 AND 55 HOLES OF THE LT WING REAR SPAR, ACTUATOR CYLINDER ANCHORAGE. REQUIRES OVERSIZING THE HOLES BEYOND SERVICE BULLETIN LIMITS. MAINTENANCE REAMED HOLE AND INSTALLED OVERSIZED FASTENER AT THE NR 52, 54 AND 55 HOLES OF THE LT WING REAR SPAR, ACTUATOR CYLINDER ANCHORAGE IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 26-5721-05153-ES1. 2L72 4F RTA28NM 20060516000562006051600056SO 2006 5 16 RAIA00605020 120050509A3350 BULB EMB 145 EMB145 3260210SO EMERGENCY LIGHT UNSECURE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03805HK 145096 MX - EMERGENCY LIGHT INOP. RESECURED BULB. 2L72 4F RTT00011AT 20060516000972006051600097SO 2006 5 16 RAIA00605016 120050508A5270 WARNING LIGHT EMB 145 EMB145 3260210SO SERVICE DOOR FALSE ACTIVATIONA RAIAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 CE03803HK 145077 FLT - 3551 - PIT - SERVICE DOOR OPEN WARNING INDICATION. MAINTENANCE INSPECTED AND CLEANED SERVICE DOOR ACTUATING/LOCKING MECHANISM. 2L72 4F RTT00011AT 20060516001112006051600111EA 2006 5 16 MASA200500503 120050630A2760 WARNING MESSAGE CNDAIRCL600 CL6002B19 1900309EA SPOILERS ILLUMINATED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW0777302 7302 ASH 6078 DSM - ABORTED TAKEOFF AND RETURNED TO THE GATE DUE TO A CONFIG SPOILER FAIL. MAINTENANCE RESET SYSTEM. 2L72 4F RTA21EA 20060516001232006051600123EA 2006 5 16 MASA200500853 120051103A7830TY214810A ISOLATION VALVE CNDAIRCL600 CL6002D24 1390016EA THRUST REVERSER MALFUNCTIONED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07912FJ6415 15012 ASH 6106 PHX - RIGHT THRUST REVERSER UNSAFE CAUTION MESSAGE. MX REPLACED THE RIGHT ISOLATION CONTROL VALVE AND THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20060517000532006051700053WP 2006 5 17 CNMA2005014 120050829A2810272002721 CHECK VALVE DOUG DC10 DC1030 3023501WP FUEL VENT MALFUNCTIONED A CNMAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW0759083 47926 AFTER T/O, GOT THE TANK OVERFILLED LEFT ON. VISUAL CHECK CONFIRMED FUEL VENTING OUT OF THE LEFT WING VENT. FUEL VENTED FOR APPROX 20 MIN. FUEL LOSS CONFIRMED OUT OF NR 3 MAIN AT 2000 LBS. TRIED TAKING TANKS DOWN TO 3000 LBS BELOW FULL AND REFILLING THEM USING ASSOC TRANS PUMPS. NO HELP, FUEL FINALLY STOPPED VENTING ON APPROACH. REMOVED AND REPLACED FUEL VENT CHECK VALVE IAW DC 10 M/M 28-12. LEAK CHECK GOOD. 2L73 4F A22WE 20060517000552006051700055NM 2006 5 17 CNMA200500016 120051213A5210140N2640 GUIDE ARM BOEING757 757200 1384950NM R2 DOOR OUT OF ADJUST A CNMAK NONE O OTHER ININSP/MAINT 1 SW07549AX 24528 NR 2 RT ENTRY DOOR FAILED TO FULLY OPEN DURING EVACUATION TEST. PERFORMED COMPLETE DOOR ADJUSTMENT TEST AND ADJUSTED R2 DOOR IAW B757 M/M 52-11, PERFORMED OPERATIONAL TEST OF R2 DOOR SLIDE IAW OAI CARD 75TC-0890. THE ROOT CAUSE FOR THE FAILURE TO DEPLOY WAS THAT THE DOOR WAS OBSTRUCTED BY THE LOWER SLIDE SKIRT WHEN ATTEMPTING TO DEPLOY SLIDE. ADJUSTMENTS WERE MADE TO THE GUIDE ARM TO ALLOW FOR ADDITIONAL CLEARANCE FOR THE DOOR TO COCK OPEN ENOUGH TO ALLOW CLEARANCE FOR THE LOWER SLIDE SKIRT. NOTE: AIRCRAFT DOOR WAS WITHIN MAINTENANCE MANUAL LIMITS BOTH BEFORE AND AFTER RIGGING. 2L72 4F RTA2NM 20060517000582006051700058WP 2006 5 17 CNMA200500014 120050829A2810272002721 CHECK VALVE DOUG DC10 DC1030 3023501WP FUEL VENT LEAKING A CNMAA UNSCHED LANDING K FLUID LOSS CLCLIMB 1 SW0759083 47926 AFTER T/O, GOT THE TANK OVERFILLED LT ON. VISUAL CHECK CONFIRMED FUEL VENTING OUT OF THE LEFT WING VENT. FUEL VENTED FOR APPROX 20 MIN. FUEL LOSS CONFIRMED OUT OF NR 3 MAIN AT 2000 LBS. TRIED TAKING TANKS DOWN TO 3000 LBS BELOW FULL AND REFILLING THEM USING ASSOC TRANS PUMPS. NO HELP, FUEL FINALLY STOPPED VENTING ON APPROACH. REMOVED AND REPLACED FUEL VENT CHECK VALVE IAW DC 10 M/M 28-12. LEAK CHECK GOOD. 2L73 4F A22WE 20060516001422006051600142EA 2006 5 16 MASA200500728 120050914A2750 FLAP SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A MASAO OTHER O OTHER DEDESCENT 1 SW0777278 7278 ASH 6168 SBP - FLAPS FAIL ON APPROACH. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED PART "A" OF THE FLAP FAIL AD AND COULD NOT FIND A DEFECT. 2L72 4F RTA21EA 20060517000542006051700054WP 2006 5 17 CNMA200500015 120050831A281040F107 CHECK VALVE DOUG DC10 DC1030 3023501WP FUEL VENT LEAKING A CNMAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW0759083 47926 FUEL VENTING OUT OF THE LEFT WING VENT BOX AREA. RIGHT SIDE OK. NO TANK OVERFILLED LT ON. APPROX 1600 LBS VENTED. AFTER BLOCK IN FUEL LEAKING OUT OF LEFT FUEL VENT BOX DRAIN. REMOVED AND REPLACED CLIMB VENT FLOAT VALVE IAW DC10 M/M 28-12. ALSO REMOVED AND REPLACED VENT BOX CHECK VALVE PRECAUTIONARY PER 28-12. 2L73 4F A22WE 20060517002212006051700221EA 2006 5 17 ASOA051113 120051217A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 DURING A C-CHECK, THE FLOORBEAM AT FS 559+80, BETWEEN THE RT SIDE FLOOR SILL AND RBL 27.00, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANC IS SUBMITTING A DAMAGE REPORT TO MFG FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE C/A. (K) 2L72 4F RTA21EA 20060517002202006051700220EA 2006 5 17 ASOA051116 120051217A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 DURING C-CHECK, THE FLOORBEAM AT FS 559+80, BETWEEEN RBL 9.00 AND RBL 27.00, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO MFG FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE C/A. (K) 2L72 4F RTA21EA 20060517002252006051700225EA 2006 5 17 ASOA051130 120051220A5210601R3807423 ANCHOR FITTING CNDAIRCL600 CL6002B19 1900309EA DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27699BR 7803 7801 DURING A HANGAR INSPECTION, THE PASSENGER DOOR FORWARD ANCHOR FITTING WAS FOUND TO BE CRACKED. MAINTENANCE WILL REMOVE AND REPLACE THE PASSENGER DOOR FORWARD ANCHOR FITTING. (K) 2L72 4F RTA21EA 20060517002262006051700226EA 2006 5 17 ASOA051127 120051220A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA FUSELAGE OVERSERVICED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27900EV 7608 DURING A GROUND INSPECTION, THE PASSENGER DOOR WAS FOUND TO BE DIFFICULT TO CLOSE. MAINTENANCE CLEANED THE EXCESS GREASE FROM THE LOCKING LUGS ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K) 2L72 4F RTA21EA 20060517002272006051700227EA 2006 5 17 ASOA051112 120051217A5321 FLOOR SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 DURING C-CHECK, THE PRESSURE FLOOR SKIN OB OF LBL 9, BETWEEN FS 449.85 AND FS 559+2, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO MFG FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE C/A. (K) 2L72 4F RTA21EA 20060517002282006051700228EA 2006 5 17 ASOA051129 120051220A5210601R317047 HANDLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27699BR 7803 7801 DURING A HANGAR INSPECTION, THE PASSENGER DOOR EXTERNAL HANDLE WAS FOUND TO BE CRACKED IN THE LOCK HOLE. MAINTENANCE WILL REMOVE AND REPLACE THE PASSENGER DOOR EXTERNAL HANDLE. (K) 2L72 4F RTA21EA 20060517002292006051700229EA 2006 5 17 ASOA051118 120051217A5320 SILL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 DURING A C-CHECK, THE RT SIDE SILL, FROM FS 559+64 TO FS 621.00, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A DAMAGE REPORT TO MFG FOR ISSUANCE OF AN REO TO DETERMINE THE APPROPRIATE C/A. (K) 2L72 4F RTA21EA 20060519002462006051900246NM 2006 5 19 ASAA0570083 120051005A5340146A75021 PLATE BOEING737 737790 13844CNNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02615AS 30344 DURING C-CHECK FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT PLATE. REPAIRED IAW SRM. (K) 2L72 4F RTA16WE 20060519002482006051900248NM 2006 5 19 ASAA0570086 120051009A5321453A161044 FLOOR PANEL BOEING737 737790 13844CNNM FUSELAGE PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02615AS 30344 DURING C-CHECK, FOUND FWD CARGO PIT NR 2 FLOOR PANEL PUNCTURED. REPAIRED IAW SRM. (K) 2L72 4F RTA16WE 20060519002552006051900255NM 2006 5 19 ASAA0570081 120051005A5320141A5410U12 INTERCOSTAL BOEING737 737790 13844CNNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02615AS 30344 DURING C-CHECK FOUND INTERCOSTAL CRACKED AT BS320. REPAIRED IAW SRM. (K) 2L72 4F RTA16WE 20060519002562006051900256NM 2006 5 19 ASAA0570085 120051009A5321453A231012 FLOOR PANEL BOEING737 737790 13844CNNM FUSELAGE PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02615AS 30344 DURING C-CHECK FOUND AFT CARGO PIT NR 3 FLOOR PANEL PUNCTURED. REPAIRED IAW SRM. (K) 2L72 4F RTA16WE 20060519002572006051900257NM 2006 5 19 ASAA05710087 120051009A5321453A261013 FLOOR PANEL BOEING737 737790 13844CNNM FUSELAGE PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02615AS 30344 DURING C-CHECK FOUND AFT CARGO PIT NR 2 FLOOR PANEL PUNCTURED. REPAIRED IAW SRM. (K) 2L72 4F RTA16WE 20060519002472006051900247NM 2006 5 19 ASAA0570084 120051009A5321453A261015 FLOOR PANEL BOEING737 737790 13844CNNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02615AS 30344 DURING C-CHECK FOUND AFT CARGO PIT NR 1 FLOOR PANEL DENTED AND PUNCTURED. REPAIRED IAW SRM. (K) 2L72 4F RTA16WE 20060523000452006052300045EU 2006 5 23 ASOA051159 120051208A5315 FLOORBEAM AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11640AS 405 DURING A C-CHECK IN YUL, THE FLOORBEAM, AT FS 38 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE FLOORBEAM, AT FS 38, IAW ASA EO 72-53-0205. (M) 2H72 4T RTA53EU 20060523001122006052300112EA 2006 5 23 ASOA051155 120051226A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA FUSELAGE INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27868AS 7474 DURING A GROUND INSPECTION IN MCO, THE PASSENGER DOOR WOULD NOT CLOSE. MAINTENANCE REINSTALLED THE PASSENGER DOOR CABLE ONTO THE PULLEY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060524001662006052400166NM 2006 5 24 MYW2006F00000 120050922A2497 WIRE BOEING727 727212 138407GNM PWA JT8 JT8D17 52049NE FWD GALLEY BURNED A MYWAO OTHER O OTHER ININSP/MAINT 1 SO29727NK 21945 DURING FLIGHT, ALL 8 RT READING STATION CB`S POPPED SIMULTANEOUSLY. PA INOPERATIVE ALL STATIONS. NO SMOKING CB POPPED, PASSENGER AND CREW CALL CB POPPED. ATTEMPTED TO RESET CB`S IAW AOM PROCEDURES. CB`S IMMEDIATELY POPPED. DID NOT ATTEMPT TO RESET, AGAIN. ON POST FLIGHT INSPECTION FOUND 28V DC BATTERY CHARGER CB POPPED. REPLACED APPROXIMATELY 80 BURNED WIRE SEGMENTS BEHIND FWD GALLEY BY DOUBLE SPLICING IAW SWP 20-30-12 AND REPAIRS IAW SWP 20-10-13. ALL SYSTEMS OPS CHECKED GOOD IAW MM. (K) 2L73 4F4 F A3WE E2EA 20060524001692006052400169NM 2006 5 24 MYW2006F00003 120051229A240011519681 CIRCUIT BREAKER BOEING737 7378Q8 13844BXNM CFMINTCFM56 CFM567B26US NE P91 PWR DIST PNLMALFUNCTIONED A MYWAK NONE O OTHER TXTAXI/GRND HDL 1 SO29734MA 30039 ON ARRIVAL, WITH ENGINES RUNNING UNABLE TO PLACE APU ON LINE UNLESS NR 1 GENERATOR BREAKER TRIPPED. TROUBLESHOT IAW FIM TASK 24-21 TASK 301. FOUND GENERATOR CONTROL BREAKER AT FAULT. REMOVED AND REPLACED BREAKER IAW 24-21-41. OPERATIONAL CHECKED GOOD. RETURNED AIRCRAFT TO SERVICE. (K) 2L72 4F4 FRTA16WE E00055EN 20060524001702006052400170NM 2006 5 24 MYW2006F00004 120051231A2450762187F BPCU BOEING737 7378Q8 13844BXNM CFMINTCFM56 CFM567B26US NE E4 RACK FAULTY A MYWAK NONE O OTHER TXTAXI/GRND HDL 1 SO29734MA 30039 ON ARRIVAL, UNABLE TO PLACE APU GENERATOR ON LINE WITH ENGINE GENERATORS ON LINE. FOUND BUS POWER UNIT AT FAULT. REMOVED AND REPLACED BPCU IAW MM. PERFORMED OPS CHECK NORMAL. PERFORMED ELECTRICAL SYSTEM CHECK IAW 24-21-00. OPS CHECK NORMAL. RETURNED AIRCRAFT TO SERVICE. (K) 2L72 4F4 FRTA16WE E00055EN 20060524002132006052400213NM 2006 5 24 MYW2006F00008 120050922A4940 ECU HONEYWELL BOEING737 7378Q8 13844BXNM CFMINTCFM56 CFM567B26US NE APU SYS INOPERATIVE A MYWAK NONE O OTHER TXTAXI/GRND HDL 1 SO29738MA 50F032 32799 ON LANDING, APU DOES NOT START. NO APU INDICATION LIGHTS ON. FRM 492-130-00. TROUBLESHOT SYSTEM, FOUND ECU AT FAULT. REMOVED AND REPLACED APU ECU. APU OPERATION CHECKS GOOD. REMOVED PLACARD AND RETURNED AC TO SERVICE. (K) 2L72 4F4 FRTA16WE E00055EN 20060524002152006052400215WP 2006 5 24 CLC2006F00005 120051102A2760H141012 SWITCH DOUG DC10 DC1030F 3023504WP GE CF6 CF650C2 30018NE FLAP-SLAT SYS MALFUNCTIONED A CLCAK NONE J WARNING INDICATION APAPPROACH 1 SO29612GC 47840 ON APPROACH THE FLAP/SLAT HANDLE ON EXTENSION HAD SLAT DISAGREE LIGHT (ON). WENT TO ABNORMAL CHECK LIST A-5-1, AND A-5-9, AND COMPLIED WITH SAME. EMERGENCY WAS DECLARED. LANDING AT DESTINATION UNEVENTFUL. FINDINGS: RT GROUND SENSING SWITCH BAD. REPLACED RT GROUND SENSING SWITCH IAW AMM, PERFORMED ADJUSTMENT AND TEST IAW AMM. AIRCRAFT RETURNED TO REVENUE SERVICE. (K) 2L73 4F4 FRTA22WE E23EA 20060524002182006052400218NM 2006 5 24 MYW2006F00009 120051208A4990380007021 APU BOEING737 73781Q 13844GENM CFMINTCFM56 CFM567B26US NE FUSELAGE OIL CONSUMPTION A MYWAK NONE O OTHER ININSP/MAINT 1 SO29733MA 30619 APU INOPERATIVE DUE HIGH OIL CONSUMPTION. TRANSFERRED TO DMI LOG SLIP NR 2931 IAW MEL 49-1 CAT (C). PLACARD INSTALLED. REMOVED AND REPLACED APU ON LOG PAGE 200103, 12/18/04. OPERATIONAL AND LEAK CHECKED GOOD IAW. REMOVED PLACARD. AIRCRAFT RETURNED TO SERVICE. (K) 2L72 4F4 FRTA16WE E00055EN 20060523001012006052300101EA 2006 5 23 ASOA051156 120051226A5210601R3198055 STEP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27842AS 7304 DURING A GROUND INSPECTION IN MCO, THE PASSENGER DOOR BOTTOM STEP WAS FOUND TO BE BROKEN. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060523001132006052300113EA 2006 5 23 ASOA051157 120051226A25602618 BATTERY CNDAIRCL600 CL6002B19 1900309EA FLASHLIGHT WEAK A ASOAK NONE O OTHER ININSP/MAINT 1 SO27873EV 7575 DURING A GROUND INSPECTION IN ATL, THE EMERGENCY FLASHLIGHT BATTERIES WERE FOUND TO BE WEAK. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLASH LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060523001142006052300114EA 2006 5 23 ASOA051158 120051226A33974871907191 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA CABIN DISCONNECTED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27861AS 7445 FLT 4578 - DURING A HANGAR INSPECTION IN BTR, THE FORWARD MOST EMERGENCY FLOOR LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE RECONNECTED THE FORWARD MOST EMERGENCY FLOOR LIGHT STRIP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20060523001152006052300115EA 2006 5 23 ASOA051160 120051229A5210601R3807413 ANCHOR FITTING CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 DURING A C-CHECK IN MCN, THE PASSENGER DOOR AFT ANCHOR FITTING WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR AFT ANCHOR FITTING. (M) 2L72 4F RTA21EA 20060524001542006052400154NM 2006 5 24 CALA0600166 120050302A5315UNK FLOORBEAM BOEING737 7373T0 1384582NM BS 294 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714337 23575 INSPECTION FOUND LEFT O/B EDGE OF FLOORBEAM UPPER CHORD CORRODED AT BS 294.5, LBL 20. THE CORRODED SECTION OF UPPER CHORD WAS REMOVED AND A NEW CHORD WAS SPLICED IN IAW ECRA 5310-04463. 2L72 4F RTA16WE 20060524001552006052400155NM 2006 5 24 CALA0600167 120050303A5315UNK FLOORBEAM BOEING737 7373T0 1384582NM BS 277 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714337 23575 INSPECTION FOUND LEFT O/B EDGE OF FLOORBEAM UPPER CHORD CORRODED AT BS 277, LBL 19. THE CORRODED SECTION OF UPPER CHORD WAS REMOVED AND A NEW CHORD WAS SPLICED IN IAW ECRA 5310-04464. 2L72 4F RTA16WE 20060525001432006052500143NM 2006 5 25 ASAA0540705 120051204A532065479573 THRESHOLD BOEING737 737490 1384715NM FS 794-847 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02795AS 28890 PAE - FOUND CORROSION AFT CARGO BAY DOOR CUTOUT LOWER THRESHOLD. REMOVED AND REPLACED LOWER THRESHOLD IAW B737-400 SRM 51-40-02. (M) 2L72 4F RTA16WE 20060525001612006052500161EU 2006 5 25 AWXA200600798 120050521A5711D57252520004 SPAR AIRBUS320 A320232 3930326EU ZONE 500 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28639AW 471 SAL - DURING C8 CHECK DISCOVERED CRACK IN HOLE NR 84 OF THE LT WING REAR SPAR, LT GEAR SUPPORT RIB 5 POSITION THAT REQUIRED OVERSIZE BEYOND SERVICE BULLETIN LIMITS. MAINTENANCE REAMED HOLE AND INSTALLED OVERSIZED FASTENER AT THE NR 84 HOLE OF THE LT WING REAR SPAR, LT GEAR SUPPORT RIB 5 POSITION IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 26-5721-05153-ES1. 2L72 4F RTA28NM 20060526000172006052600017EA 2006 5 26 BSYA200500018 220051110A732225245009 SERVO PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA LT ENGINE MALFUNCTIONED E BSYAA UNSCHED LANDING O OTHER CLCLIMB 1 GL0735584 8052076 DURING CLIMBOUT OF PHL THE LEFT ENGINE STARTED SURGING A COUPLE HUNDRED RPM. PILOT RETURNED TO PHL, NO PROBLEMS. 1L72 3O3 O A20SO E14EA 20060526000222006052600022CE 2006 5 26 BSYA200500032 120051220A3230 LANDING GEAR BEECH 58 58 1152740CE NLG & MLG MALFUNCTIONED E BSYAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL0778RE TH371 ON TAKEOFF OUT OF DTW PILOT SELECTED GEAR UP AND NOTHING HAPPENED. RETURNED TO DTW. 1L72 3O 3A16 20060526000102006052600010WP 2006 5 26 IXXA05SMN305S 120051229A5730 SKIN DOUG DC8 DC872 302199BWP RT WING MISREPAIRED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11722CX71621 46130 DURING ROUTINE C-CHECK INSPECTION, RT WING - T/E LWR SKIN NON STANDARD REPAIR, XW 762.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-0 FIG 2A (SHEET 1), TR 57-84 DATED 08-01-00. REMOVED NON STANDARD REPAIR IAW DC8 SRM 51-1-21. REMOVED DAMAGED SECTION IAW DC-8 SRM 57-2-0 FIG 2A (SHEET 1). FABRICATED NEW EXT REPAIR DOUBLER (AL 2024 T3 0.040) + FILLER (ALCLAD 2024 T3 0.020) IAW DC8 SRM 57-2-0 FIG 2A (SHEET 1), DC-8 SRM 57-3-2 FIG 31. CLEANED, TREATED AND PRIMED AREA INNER SIDE IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACE IAW DC8 SRM 51-1-11. INSTALLED REPAIR PARTS IAW DC8 SRM 57-2-0 FIG 2A (SHEET 1), DC-8 SRM 51-1-21. 2L74 4F RT4A25 20060526000122006052600012WP 2006 5 26 IXXA05SMN321S 120051229A5320 FITTING DOUG DC8 DC872 302199BWP FUSELAGE CRACKED B IXXAK NONE O OTHER ININSP/MAINT 1 SW11722CX71621 46130 DURING ROUTINE C-CHECK INSPECTION, MAIN CARGO COMPT FITTING CRACKED 3, AT STA 1530.000, L-26R. REMOVED CRACKED FITTING IAW DC-8 SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8B. INSTALLED NEW FITTING WITH HI-LOKS IAW DC-8 SRM 51-1-20D, DC-8 SRM 51-3-1 (TORQUE). 2L74 4F RT4A25 20060526000182006052600018SO 2006 5 26 BSYA200500010 120050601A8120LW1246385 BEARING PIPER PA31 PA31P350 7103111SO LYC O540 LTIO540J2BD 41533EA TURBOCHARGER WORN E BSYAC ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 GL073590D1902 8052144 RL199468A ON TAKEOFF OUT OF BUF TOWER NOTICED A LOT OF SMOKE, PILOT ABORTED TAKEOFF AND WAS TOWED BACK. MAINTENANCE FOUND BEARING GONE IN THE TURBO CHARGER AND OIL LEAKING INTO THE EXHAUST. REMOVED AND REPLACED TURBO CHARGER, OPS CHECKS GOOD. 1L72 3O3 ORTA8EA E14EA 20060601000952006060100095NE 2006 6 1 AALA20060319 220050520A7261776623 LINE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE LT ENGINE OIL LEAKING A AALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW21597AA 53287 COS - LEFT ENGINE OIL QUANTITY DECREASED TO ZERO. RAN ENGINE AT IDLE ONE MINUTE. OIL PRESSURE NORMAL THROUGHOUT FLIGHT. LANDED COS WITHOUT INCIDENT. REPLACED NUMBER SIX OIL PUMP TUBE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA6WE E9NE 20060601001052006060100105 2006 6 1 AALA20060311 420050518A3444HG1103BA01 IRU DOUG DC9 DC983 3022083WP INOPERATIVE A AALAA UNSCHED LANDING O OTHER CRCRUISE 1 SW219615W 53562 LAS - LOST BOTH INERTIAL REFERENCE UNITS EN ROUTE TO ORD. LANDED LAS WITHOUT INCIDENT. REPLACED BOTH INERTIAL REFERENCE UNITS AND CONTROL PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20060606001642006060600164NM 2006 6 6 HNAA0600041 120050522A522085210159103 STRUCTURE DHAV DHC8 DHC8102 2809003NM EMERGENCY EXIT CRACKED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07906HA5502255022 09 DURING HEAVY CHECK INSPECTIONS IT WAS NOTED THE DOOR GAS STRUT CHASSIS WAS CRACKED. REPLACED CHASSIS. 2H72 4T RTA13NM 20060607001742006060700174SO 2006 6 7 XGN2006F00003 220051011A8530ECI712A CYLINDER CONT BEECH 36 36BEECH 1151602CE CONT O520 IO520BA 17032SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW051194A884 573460R E159 573460R CRACKS FOUND AT THE 50 HR INSPECTION. ON GOING PROBLEM WITH THE CYLINDERS. (K) 1L71 3O3 O 3A15 E5CE 20060608004092006060800409SO 2006 6 8 XGN2006F00064 220050303A8530ECI712B CYLINDER CONT CESSNA401 401 207590CCE CONT O520 TSIO520E 17040SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW0531DB 774 182351R 4010202 182351R CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K) 1L72 3O3 O A7CE E8CE 20060608004162006060800416SO 2006 6 8 XGN2006F00062 220050506A8530ECI712B CYLINDER CESSNA401 401 207590CCE CONT O520 TSIO520E 17040SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW0531DB 1102 4010202 502537R CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K) 1L72 3O3 O A7CE E8CE 20060608004172006060800417SO 2006 6 8 XGN2006F00063 220050303A8530ECI712B CYLINDER CESSNA401 401 207590CCE CONT O520 TSIO520E 17040SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW0531DB 880 4010202 275320R CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K) 1L72 3O3 O A7CE E8CE 20060608004182006060800418SO 2006 6 8 XGN2006F00028 220050404A8530ECI712BCA CYLINDER CONT CESSNA402 402B 207590PCE CONT O520 TSIO520E 17040SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW054165G1037 502537R 402B1212 502537R CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K) 1L72 3O3 O A7CE E8CE 20060608004192006060800419SO 2006 6 8 XGN2006F00059 220050416A8530ECI712BCA CYLINDER CONT CESSNA401 401 207590CCE CONT O520 TSIO520E 17040SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW053260Q1345 182909R 4010060 182909R CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K) 1L72 3O3 O A7CE E8CE 20060608004302006060800430SO 2006 6 8 XGN2006F00074 220051011A8530ECI712A CYLINDER CONT BEECH 33 F33A 1151425CE CONT O520 IO520BA 17032SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW051096W1147 807017 CE436 807017 THESE CYLINDERS SHOWED TO BE CRACKED IN THE EXHAUST SIDE OF THE HEAD. THE LEAKS SHOWED UP WHEN DOING THE COMPRESSION CHECK. DUE TO THE NUMBER OF CRACKED CYLINDER HEADS. WE DO A COMPRESSION CHECK EVERY 50 HRS. (K) 1L71 3O3 O 3A15 E5CE 20060608004332006060800433SO 2006 6 8 XGN2006F00032 220050302A8530ECI712BCA CYLINDER CONT CESSNA402 402B 207590PCE CONT O520 TSIO520E 17040SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW055421M881 503049R 402B0021 503049R CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K) 1L72 3O3 O A7CE E8CE 20060608004412006060800441SO 2006 6 8 XGN2006F00067 220050508A8530ECI712A CYLINDER CONT BEECH 36 A36 1151604CE CONT O520 IO520BA 17032SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW05236CH1076 280803R E502 280803R CYLINDER HEAD CRACKED IN THE EXHAUST PORT AREA. (K) 1L71 3O3 O 3A15 E5CE 20060609002252006060900225SO 2006 6 9 XGN2006F00033 220050305A8530ECI71BCA CYLINDER CONT CESSNA402 402B 207590PCE CONT O520 TSIO520E 17040SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW055421M943 503049R 402B0021 503049R CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K) 1L72 3O3 O A7CE E8CE 20060609002272006060900227SO 2006 6 9 XGN2006F00034 220050405A8530ECI712BCA CYLINDER CONT CESSNA402 402B 207590PCE CONT O520 TSIO520E 17040SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW055421M943 503049R 402B0021 503049R CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K) 1L72 3O3 O A7CE E8CE 20060612000642006061200064SO 2006 6 12 XGN2006F00004 220051011A8530ECI712A CYLINDER BEECH 36 36BEECH 1151602CE CONT O520 IO520BA 17032SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW051194A898 E159 HEADS FOUND CRACKED AT THE 100 HR INSPECTION. 5 OF THE 6 CYLINDERS HAVE BEEN CHANGED IN THE LAST 400 HRS OF OPERATION. THIS CONTINUES TO BE AN ON GOING PROBLEM. (K) 1L71 3O3 O 3A15 E5CE 20060612000812006061200081SO 2006 6 12 XGN2006F00035 220050604A8530ECI712BCA CYLINDER CONT CESSNA402 402B 207590PCE CONT O520 TSIO520E 17040SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW055421M1094 503049R 402B0021 503049R CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K) 1L72 3O3 O A7CE E8CE 20060612000912006061200091SO 2006 6 12 XGN2006F00036 220050418A8530ECI712BCA CYLINDER CONT CESSNA402 402B 207590PCE CONT O520 TSIO520E 17040SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW055421M1482 503049R 402B0021 503049R CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K) 1L72 3O3 O A7CE E8CE 20060612001052006061200105SO 2006 6 12 XGN2006F00037 220050412A8530ECI712ACA CYLINDER CONT BEECH 55 95C55 1152708CE CONT O520 IO520C 17032SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW055740V 240275R TE103 240275R CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K) 1L72 3O3 O 3A16 E5CE 20060608004202006060800420SO 2006 6 8 XGN2006F00065 220050330A8530ECI712B CYLINDER CESSNA401 401 207590CCE CONT O520 TSIO520E 17040SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW0531DB 4010202 182351R CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K) 1L72 3O3 O A7CE E8CE 20060612001522006061200152SO 2006 6 12 XGN2006F00046 220050426A8530TISN712ACA CYLINDER BEECH 58 58 1152740CE CONT O520 IO520C 17032SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW05577W 400 TH375 561711 CYLINDERS WERE FOUND DURING COMPRESSION CHECK AT THE 100 HR INSPECTION. USING A SOAP SOLUTION TO DETECT CRACKS IN THE EXHAUST SIDE OF THE CYLINDER WHILE DOING A COMPRESSION CHECK. DOING COMPRESSION CHECKS EACH 50 HRS. 3 CRACKED CYLINDERS WERE FOUND ON THE SAME ENGINE AT THIS INSPECTION. (K) 1L72 3O3 O 3A16 E5CE 20060612001542006061200154SO 2006 6 12 XGN2006F00044 220051011A8530ECI712A CYLINDER BEECH 58 58 1152740CE CONT O520 IO520* 17032SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW05577W 694 TH375 FOUND CYLINDER HEAD CRACKED IN THE EXHAUST SIDE DURING A 50 HR INSPECTION. THIS IS AN ON GOING PROBLEM WITH THE CYLINDERS. (K) 1L72 3O3 O 3A16 E5CE 20060612001662006061200166SO 2006 6 12 XGN2006F00048 220051005A8530TISN712ACA CYLINDER BEECH 58 58 1152740CE CONT O520 IO520C 17032SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW05577W 748 TH375 561711R FOUND CRACKED CYLINDER HEAD AT 50 HR INSPECTION. DUE TO THE FREQUENCY OF THE NUMBER OF CYLINDERS WE ARE FINDING CRACKED, WE DO A COMPRESSION CHECK EACH 50 HRS. (K) 1L72 3O3 O 3A16 E5CE 20060612001672006061200167SO 2006 6 12 XGN2006F00072 220051011A8530ECI712A CYLINDER BEECH 36 36BEECH 1151602CE CONT O520 IO520BA 17032SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW051194A844 E159 573460R CRACKS FOUND AT THE 50 HR INSPECTION. ON GOING PROBLEM WITH THE MFG CYLINDERS. (K) 1L71 3O3 O 3A15 E5CE 20060612001692006061200169SO 2006 6 12 XGN2006F00057 220050424A8530ECI712BCA CYLINDER CESSNA402 402B 207590PCE CONT O520 TSIO520E 17040SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW055421M943 402B0021 503049R CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K) 1L72 3O3 O A7CE E8CE 20060612001712006061200171SO 2006 6 12 XGN2006F00060 220050403A8530ECI712BCA CYLINDER CESSNA401 401 207590CCE CONT O520 TSIO520E 17040SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW053260Q1664 4010060 275419R CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K) 1L72 3O3 O A7CE E8CE 20060612001722006061200172SO 2006 6 12 XGN2006F00061 220050506A8530ECI712B CYLINDER CESSNA401 401 207590CCE CONT O520 TSIO520E 17040SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW0531DB 1102 4010202 502537R CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K) 1L72 3O3 O A7CE E8CE 20060612002452006061200245SO 2006 6 12 XGN2006F00066 220050330A8530ECI712B CYLINDER CESSNA401 401 207590CCE CONT O520 TSIO520E 17040SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW0531DB 774 4010202 182351R CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K) 1L72 3O3 O A7CE E8CE 20060612002472006061200247SO 2006 6 12 XGN2006F00068 220050523A8530ECI712A CYLINDER BEECH 36 36BEECH 1151602CE CONT O520 IO520BA 17032SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW051194A521 E159 573460R CYLINDER HEAD CRACKED IN THE EXHAUST PORT AREA. (K) 1L71 3O3 O 3A15 E5CE 20060612002482006061200248SO 2006 6 12 XGN2006F00020 220050523A8530ECI712B CYLINDER CESSNA401 401 207590CCE CONT O520 TSIO520E 17040SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW053217Q858 4010017 812567R CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K) 1L72 3O3 O A7CE E8CE 20060612002492006061200249SO 2006 6 12 XGN2006F00022 220051216A8530ECI712BCA CYLINDER CESSNA401 401 207590CCE CONT O520 TSIO520E 17040SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW053260Q1122 4010060 275430R CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K) 1L72 3O3 O A7CE E8CE 20060612001482006061200148SO 2006 6 12 XGN2006F00045 220050906A8530ECI712A CYLINDER CONT BEECH 58 58 1152740CE CONT O520 IO520C 17032SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW05577W 645 561711R TH375 561711R CYLINDER HEAD CRACKS FOUND AT 50 HR INSPECTION. DUE TO THE FREQUENCY OF THE NR OF CYLINDERS WE ARE FINDING CRACKED, WE DO A COMPRESSION CHECK EACH 50 HOURS. (K) 1L72 3O3 O 3A16 E5CE 20060612001772006061200177SO 2006 6 12 XGN2006F00010 220050924A8530 CYLINDER BEECH 36 A36 1151604CE CONT O520 IO520BA 17032SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW05236CH471 E502 280803R FOUND CYLINDER HEAD CRACKED IN THE EXHAUST SIDE OF THE CYLINDER HEAD DURING 50 HR INSPECTION. THIS IS AN ON GOING PROBLEM WITH THE CYLINDERS. (K) 1L71 3O3 O 3A15 E5CE 20060612001892006061200189SO 2006 6 12 XGN2006F00019 220050520A8530ECI712B CYLINDER CESSNA401 401 207590CCE CONT O520 TSIO520E 17040SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW0531DB 1002 4010202 275320R CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K) 1L72 3O3 O A7CE E8CE 20060612001972006061200197SO 2006 6 12 XGN2006F00016 220050330A8530ECI712B CYLINDER CESSNA401 401 207590CCE CONT O520 TSIO520E 17040SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW0531DB 880 4010202 275320R CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K) 1L72 3O3 O A7CE E8CE 20060612001982006061200198SO 2006 6 12 XGN2006F00021 220050524A8530ECI712BCA CYLINDER CESSNA401 401 207590CCE CONT O520 TSIO520E 17040SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW053260Q1664 4010060 275419R CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K) 1L72 3O3 O A7CE E8CE 20060612002012006061200201SO 2006 6 12 XGN2006F00017 220050506A8530ECI712B CYLINDER CESSNA401 401 207590CCE CONT O520 TSIO520E 17040SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW0531DB 1102 4010202 502537R CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K) 1L72 3O3 O A7CE E8CE 20060612002022006061200202SO 2006 6 12 XGN2006F00018 220050506A8530ECI712B CYLINDER CESSNA401 401 207590CCE CONT O520 TSIO520E 17040SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW0531DB 1102 4010202 502537R CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K) 1L72 3O3 O A7CE E8CE 20060612002202006061200220SO 2006 6 12 XGN2006F00029 220050208A8530ECI712BCA CYLINDER CESSNA402 402B 207590PCE CONT O520 TSIO520E 17040SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW054165G952 402B1212 502537R CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K) 1L72 3O3 O A7CE E8CE 20060612002222006061200222SO 2006 6 12 XGN2006F00070 220050529A8530ECI712A CYLINDER BEECH 36 36BEECH 1151602CE CONT O520 IO520BA 17032SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW051194A741 E159 573460R CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K) 1L71 3O3 O 3A15 E5CE 20060612002232006061200223SO 2006 6 12 XGN2006F00056 220050405A8530ECI712BCA CYLINDER CESSNA402 402B 207590PCE CONT O520 TSIO520E 17040SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW055421M943 402B0021 503049R CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K) 1L72 3O3 O A7CE E8CE 20060612002342006061200234SO 2006 6 12 XGN2006F00071 220051011A8530ECI712A CYLINDER BEECH 36 36BEECH 1151602CE CONT O520 IO520BA 17032SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW051194A898 E159 573460R HEADS FOUND CRACKED AT THE 100 HR INSPECTION. 5 OF THE 6 CYLINDERS HAVE BEEN CHANGED IN THE LAST 400 HR OF OPERATION. THIS CONTINUES TO BE AN ON GOING PROBLEM. (K) 1L71 3O3 O 3A15 E5CE 20060612002382006061200238SO 2006 6 12 XGN2006F00075 220051011A8530ECI712A CYLINDER BEECH 33 F33A 1151425CE CONT O520 IO520BA 17032SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW051096W1147 CE436 807017 THESE CYLINDERS SHOWED TO BE CRACKED IN THE EXHAUST SIDE OF THE HEAD. THE LEAKS SHOWED UP WHEN DOING THE COMPRESSION CHECK. DUE TO THE NUMBER OF CRACKED CYLINDER HEADS, WE DO A COMPRESSION CHECK EVERY 50 HRS. (K) 1L71 3O3 O 3A15 E5CE 20060612000892006061200089SO 2006 6 12 XGN2006F00038 220050412A8530ECI712ACA CYLINDER BEECH 55 95C55 1152708CE CONT O520 IO520C 17032SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW055740V TE103 240275R CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K) 1L72 3O3 O 3A16 E5CE 20060612001312006061200131SO 2006 6 12 XGN2006F00073 220051011A8530ECI7121A CYLINDER CONT BEECH 33 F33A 1151425CE CONT O520 IO520BA 17032SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW051096W 807017 CE436 807017 THESE CYLINDERS SHOWED TO BE CRACKED IN THE EXHAUST SIDE OF THE HEAD. THE LEAKS SHOWED UP WHEN DOING THE COMPRESSION CHECK. DUE TO THE NR OF CRACKED CYLINDER HEADS, COMPRESSION CHECK EVERY 50 HRS. (K) 1L71 3O3 O 3A15 E5CE 20060613002352006061300235NE 2006 6 13 ALGA109060 120050207A63107636109103104 SHAFT SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL ENGINE SHEARED B ALGAK NONE O OTHER NRNOT REPORTED 1 SW03PTYAY 760277 SHAFT SHEARED IN THREAD PORTION, AT BASE OF ATTACHING NUT. REPLACED W/NEW OR SERVICEABLE UNIT BY FIELD MAINT. 1G72 3U3 U H1NE E1GL 20060621001912006062100191NM 2006 6 21 2006UALA01155 120050112A2560 LATCH BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE CABIN FAILED A UALAK NONE O OTHER ININSP/MAINT 1 WP29662UA 27159 LT O/W SLIDE DOOR INTEGRATOR FAILS TORQUE CHECK. REPLACED LATCHES IAW 767 MM 25-65-98. 2L72 4F4 FRTA1NM E24NE 20060621002062006062100206NM 2006 6 21 2006UALA01164 120050412A2560 LATCH BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE CABIN FAILED A UALAK NONE O OTHER ININSP/MAINT 1 WP29658UA 27113 LT OFFWING SLIDE LATCH CHECK FAILS TORQUE CHECK. TORQUE TO OPEN 200 IN/LBS, MAX ALLOWED 175. 2L72 4F4 FRTA1NM E24NE 20060621002072006062100207NM 2006 6 21 2006UALA01165 120050416A2560 LATCH BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE CABIN FAILED A UALAK NONE O OTHER ININSP/MAINT 1 WP29666UA 29238 LT O/W COMPT INTEGRATOR TORQUE CHECK FAILED AND LATCHES MUST BE REPLACED. REMOVE AND REPLACE LATCHES IAW UAL B767 MM-25-65-98. 2L72 4F4 FRTA1NM E24NE 20060621002102006062100210NM 2006 6 21 2006UALA01166 120050425A2560 LATCH BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE CABIN FAILED A UALAK NONE O OTHER ININSP/MAINT 1 WP29672UA 30027 LT O/W DOOR LATCHES FAIL INTEGRATOR TORQUE CHECK. REMOVE AND REPLACE LATCHES IAW UAL B767 MM25-65-98. 2L72 4F4 FRTA1NM E24NE 20060621002122006062100212NM 2006 6 21 2006UALA01168 120050509A2560 LATCH BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE CABIN FAILED A UALAK NONE O OTHER ININSP/MAINT 1 WP29656UA 25394 LT O/W SLIDE COMPT DOOR DISCONNECT HOUSING HAS FAIL CHECK. REMOVE AND REPLACE REF: UALB767 MM 25-65-98. 2L72 4F4 FRTA1NM E24NE 20060621002142006062100214NM 2006 6 21 2006UALA01169 120050516A2560 KEEPER BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE SLIDE DOOR FROZEN A UALAK NONE O OTHER ININSP/MAINT 1 WP29673UA 29241 LT O/W HATCH SLIDE DOOR HAS 1 KEEPER FROZEN. REPLACE KEEPER IAW 767 MM 25-65-98. 2L72 4F4 FRTA1NM E24NE 20060621002162006062100216NM 2006 6 21 2006UALA01170 120050524A2560 LATCH BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE CABIN FAILED A UALAK NONE O OTHER ININSP/MAINT 1 WP29676UA 30028 LT O/W DOOR LATCHES FAILED TORQUE CHECK. REMOVE AND REPLACE LATCHES REF UAL B767 MM-25-65-98. 2L72 4F4 FRTA1NM E24NE 20060621002202006062100220NM 2006 6 21 2006UALA01173 120050830A2560 HOUSING BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE OVERWING EXIT CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29643UA 25093 LT O/W SLIDE COMPARTMENT DISCONNECT HOUSING IS CRACKED. REPLACE HOUSING IAW 767 25-65-98. 2L72 4F4 FRTA1NM E24NE 20060621002272006062100227NM 2006 6 21 2006UALA01177 120051029A2560 LATCH BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE CABIN WORN A UALAK NONE O OTHER ININSP/MAINT 1 WP29659UA 27114 R/W, O/W SLIDE COMPARTMENT, NR 4 AND 3 LATCHES ARE WORN. REMOVE AND REPLACE LATCHES IAW B767 MM25-65-98. 2L72 4F4 FRTA1NM E24NE 20060621001972006062100197NM 2006 6 21 2006UALA01159 120050315A2560 LATCH BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE CABIN WORN A UALAK NONE O OTHER ININSP/MAINT 1 WP29664UA 29236 RT O/W DOOR LATCHES (NR 3 AND NR 4) FAIL EDGE MARGIN CHECK. REPLACE LATCHES IAW MM 25-65-98. 2L72 4F4 FRTA1NM E24NE 20060621002042006062100204NM 2006 6 21 2006UALA01162 120050404A2560 ROD BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE CABIN CHAFED A UALAK NONE O OTHER ININSP/MAINT 1 WP29665UA 29237 LT OVERWING SLIDE CENTER LATCH ROD ASSEMBLY CHAFFED. REPLACE ROD IAW 767, MM-25-65-98. 2L72 4F4 FRTA1NM E24NE 20060621002222006062100222NM 2006 6 21 2006UALA01174 120051027A2560 LATCH BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE CABIN FAILED A UALAK NONE O OTHER ININSP/MAINT 1 WP2968UA 30024 LEFT OFFWING SLIDE DOOR LATCHES FAILED TORQUE CHECK. REMOVE AND REPLACE LATCHES IAW B767 MM 25-65-98. 2L72 4F4 FRTA1NM E24NE 20060621002262006062100226NM 2006 6 21 2006UALA01176 120051027A2560 LATCH BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE CABIN FAILED A UALAK NONE O OTHER ININSP/MAINT 1 WP29668UA 30024 RIGHT OFF-WING SLIDE LATCHES FAILED TORQUE CHECK. REMOVE AND REPLACE LATCHES IAW B767 MM25-65-98. 2L72 4F4 FRTA1NM E24NE 20060621002442006062100244NM 2006 6 21 2006UALA01185 120051227A2560 LATCH BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE CABIN WORN A UALAK NONE O OTHER ININSP/MAINT 1 WP29646UA 25283 NR 3 LATCH EDGE MARGIN BEYOND LIMITS. REPLACED LATCH, IAW B767 MM 25-65-98. 2L72 4F4 FRTA1NM E24NE 20060621001922006062100192NM 2006 6 21 2006UALA01156 120050123A2560 LATCH BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE CABIN FAILED A UALAK NONE O OTHER ININSP/MAINT 1 WP29663UA 27160 LT O/W HATCH FAILS INTEGRATOR TORQUE CHECK. REPLACED LATCHES. 2L72 4F4 FRTA1NM E24NE 20060621002052006062100205NM 2006 6 21 2006UALA01163 120050404A2560 LATCH BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE CABIN FAILED A UALAK NONE O OTHER ININSP/MAINT 1 WP29665UA 29237 RT O/W DOOR LATCH INTEGRATOR FAILS TORQUE CHECK. REPLACE LATCHES IAW 767, MM-25-65-98. 2L72 4F4 FRTA1NM E24NE 20060621002112006062100211NM 2006 6 21 2006UALA01167 120050425A2560 HOUSING BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE OVERWING EXIT CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29672UA 30027 RT O/W DOOR DISCONNECT HOUSING IS CRACKED. REPLACE HOUSING IAW 767 MM-25-65-98. 2L72 4F4 FRTA1NM E24NE 20060621002242006062100224NM 2006 6 21 2006UALA01175 120051030A2560 HOUSING BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE OVERWING EXIT CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29668UA 30024 LT O/W SLIDE DISCONNECT HOUSING IS CRACKED. REPLACE DISCONNECT HOUSING IAW 767MM 25-65-98. 2L72 4F4 FRTA1NM E24NE 20060621002032006062100203NM 2006 6 21 2006UALA01161 120050404A2560 LATCH BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE CABIN FAILED A UALAK NONE O OTHER ININSP/MAINT 1 WP29665UA 29237 LT OVERWING SLIDE NR 3 DOOR LATCH FAILED INSP CHECK. REPLACE LATCH IAW 767 25-65-98. 2L72 4F4 FRTA1NM E24NE 20060621002182006062100218NM 2006 6 21 2006UALA01172 120050614A2560 LATCH BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE CABIN WORN A UALAK NONE O OTHER ININSP/MAINT 1 WP29657UA 27112 LT O/W SLIDE DOOR LATCH FAILS EDGE MARGIN CHECK (NR 3 LATCH). REPLACE LATCH IAW 767, MM 25-65-98. 2L72 4F4 FRTA1NM E24NE 20060712000122006071200012NM 2006 7 12 UPS06547290 120050706A2120 ODOR BOEING757 75724APF 1384969NM COCKPIT DETECTED A IPXAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO01408UP 23730 STRONG OIL ODOR IN FLT. CAPT & F/O EYE'S & THROAT BURNING. OPERATED LT & RT ENG AT HIGH POWER FOR 15 MIN EA SIDE. ISOLATED LT & RT BLEEDS & APU BLEED. RAN LT & RT PACKS SEPARATELY, NO RE-OCCURRENCE OF OIL ODOR OCCURRED. SYS ODORS CLEAN, NO SMOKE. REF MM 71-00-00-2 & FIM 21-00-01. 2L72 4F RTA2NM 20060721001432006072100143NM 2006 7 21 2006F00028 120051224A3320 LIGHT BOEING757 757 UTILUSENM CABIN INOPERATIVE D NWAAO OTHER H ELECT. POWER LOSS-50 PC CRCRUISE 1 GL01 NWA NR 88, 12/24/05, HNL-SEA: SEAT-SPECIFIC CABIN LIGHTING SYSTEM FAILED AT ALL SEATS, SHORTLY AFTER IN-FLIGHT ENTERTAINMENT/VIDEO SYSTEM FAILURE. OCCURRED TWO HOURS INTO THE TRANS-PACIFIC FLIGHT, WELL BEFORE THE MID-WAY POINT. LIGHTS RESTORED AFTER 45 MIN.UPON TOUCHDOWN IN SEA ALL MAIN CABIN LIGHTS FAILED, LEAVING CABIN TOTALLY BLACK. NO EMERGENCY LIGHTS VISIBLE. PASSENGERS USED FLASHLIGHT FOR 5-10 MINS WHILE WAITING TO BE HOOKED UP TO GROUND AUX PWR AT THE GATE. 2L72 4F RTA2NM 20060721001442006072100144NM 2006 7 21 2006F00029 120051224A3350 LIGHT BOEING757 757 UTILUSENM CABIN INOPERATIVE H NWAAO OTHER H ELECT. POWER LOSS-50 PC CRCRUISE 1 NM01 NWA NR 88, 12/24/05, HNL-SEA: SEAT-SPECIFIC CABIN LIGHTING SYSTEM FAILED AT ALL SEATS, SHORTLY AFTER IN-FLIGHT ENTERTAINMENT/VIDEO SYSTEM FAILURE. OCCURRED 2 HOURS INTO THE TRANS-PACIFIC FLIGHT, WELL BEFORE THE MID-WAY POINT. LIGHTS RESTORED AFTER 45 MIN.UPON TOUCHDOWN IN SEA ALL MAIN CABIN LIGHTS FAILED, LEAVING CABIN TOTALLY BLACK. NO EMERGENCY LIGHTS VISIBLE. PASSENGERS USED FLASHLIGHT FOR 5-10 MINS WHILE WAITING TO BE HOOKED UP TO GROUND AUX PWR AT THE GATE. 2L72 4F RTA2NM 20060721001462006072100146NM 2006 7 21 2006F00030 120051224A3320 LIGHT BOEING757 757 UTILUSENM CABIN INOPERATIVE H NWAAO OTHER H ELECT. POWER LOSS-50 PC CRCRUISE 1 NM01 NWA NR88, 12/24/05, HNL-SEA: SEAT-SPECIFIC CABIN LIGHTING SYSTEM FAILED AT ALL SEATS, SHORTLY AFTER IN-FLIGHT ENTERTAINMENT/VIDEO SYSTEM FAILURE. OCCURRED 2 HOURS INTO THE TRANS-PACIFIC FLIGHT, WELL BEFORE THE MID-WAY POINT. LIGHTS RESTORED AFTER 45 MIN. UPON TOUCHDOWN IN SEA ALL MAIN CABIN LIGHTS FAILED, LEAVING CABIN TOTALLY BLACK. NO EMERGENCY LIGHTS VISIBLE. PASSENGERS USED FLASHLIGHT FOR 5-10 MINS WHILE WAITING TO BE HOOKED UP TO GROUND AUX PWR AT THE GATE. 2L72 4F RTA2NM 20060804000042006080400004NE 2006 8 4 HEEA107325 120050827A29109265004900101 HEAT EXCHANGER SKRSKYS92 S92A NE NR 1 HYD SYSTEM RUPTURED E HEEAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW03292PH586 920008 DURING CRUISE FLIGHT, THE NR 1 HYDRAULIC RESERVOIR LOW LIGHT ILLUMINATED, FOLLOWED BY OTHER ASSOCIATED LIGHTS CONFIRMING THE NR 1 HYDRAULIC SYSTEM FAILURE. MAINTENANCE FOUND THE HYDRAULIC SYSTEM HEAT EXCHANGER RUPTURED. 2G72 4U R00024BO 20060804000052006080400005NE 2006 8 4 HEEA107343 120050405A2910SS76D10212SS000 HOSE SKRSKYS92 S92A NE HYD SYSTEM LEAKING B HEEAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW03292PH85 920008 ON FIRST FLIGHT OF DAY, IN CRUISE HYD SERVO ONE LIGHT FOLLOWED BY HYD PUMP ONE LIGHT AND ONE HYD PRESSURE WENT TO ZERO. FOUND PIN HOLE IN HOSE UNDER CLAMP. REPLACED HOSE AND CLAMP. 2G72 4U R00024BO 20060808000192006080800019WP 2006 8 8 05FDEA02208 120050802A5330 DOUBLER DOUG MD10 MD1010F 3022112WP FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25381FE 46615 LOWER FUSELAGE EXTERNAL DOUBLER STA 1210 LONG 52 DAMAGED. REPAIRED IAW SRM 53-40-00 FIGURE 20 VOL 1. 2L73 4F RTA22WE 20060808000472006080800047NE 2006 8 8 HEEA107335 120050821A2910SS76D10175SS000 LINE SKRSKYS92 S92A NE NR 2 HYD SYSTEM RUPTURED B HEEAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW03192PH646 920006 NR 2 HYDRAULIC SYSTEM FAILED IN FLIGHT. MAINTENANCE FOUND NR 2 HYDRAULIC PUMP DISCHARGE HOSE HAD RUPTURED. REPLACED HOSE. 2G72 4U R00024BO 20060808000492006080800049NE 2006 8 8 HEEA107354 120050713A28239230708815101 SELECTOR VALVE SKRSKYS92 S92A NE COCKPIT FAILED E HEEAC ABORTED TAKEOFF XJ ENGINE FLAMEOUT WARNING INDICATION TOTAKEOFF 1 SW03392PH128 920015 DURING TAKEOFF, NR 1 ENGINE FAILED. RETURNED TO DEPARTURE. MAINTENANCE REPLACED FUEL SELECTOR VALVE. 2G72 4U R00024BO 20060818001472006081800147EU 2006 8 18 HCM2006F00004 120050309A6320 GEARBOX UROCOPEC130 EC130B4 8680989EU TMECA ARRIELARRIEL2B NE MAIN ROTOR MAKING METAL E HCMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP1311QM 3751 23022 WHILE ON A SIGHTSEEING FLIGHT ON THE ISLAND OF HAWAII, THE PILOT EXPERIENCED A MAIN ROTOR GEARBOX CHIP INDICATION. A PRECAUTIONARY LANDING WAS MADE AT THE WAIMEA KOHALA AIRPORT AT APPROX 11:30 AM. INVESTIGATION BY THE MECHANIC FOUND SMALL SLIVERS OF METAL. THE METAL WAS REMOVED. THE AC WAS GROUND RUN WITHOUT FURTHER OCCURRENCE. THE AIRCRAFT WAS THEN RETURNED TO BASE. (K) 1G72 3U3 U H9EU E00054EN 20060824000362006082400036EA 2006 8 24 COMA0660502 120050822A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSDAMAGED A COMAK NONE L NO TEST TXTAXI/GRND HDL 1 SO01929CA 7035 FLIGHT 5306 - THE AFT CABIN EMERGENCY FLOOR LEVEL LIGHTING FAILED TEST. REPAIRED WIRING ON AFT EMERGENCY FLOOR LEVEL FLEX STRIP CONNECTOR. 2L72 4F RTA21EA 20060911002802006091100280WP 2006 9 11 I5HA058006 120050801A77006829066 METER CVAC 580 580 2422806WP ALLSN 501D 501D13 03004GL LT ENGINE VIBRATION A I5HAO OTHER O OTHER NRNOT REPORTED 1 GL23588X 52 501545 AUG 1, 2006 DURING THE TAKEOFF ROLL, THE CREW OBSERVED WHAT THEY BELIEVED TO BE A LOSS OF POWER FROM THE LT HAND ENGINE AND FELT A VIBRATION. THE TAKEOFF WAS ABORTED AND THE AIRPLANE RETURNED FOR MAINTENANCE. INSPECTION OF THE LT ENGINE REVEALED DAMAGE TO THE AC GENERATOR AND THE ENGINE DRIVEN HYDRAULIC PUMP CONSISTENT WITH A SEVERE VIBRATION.. ENGINE WAS REMOVED AND INSPECTED. PENDING FURTHER METALLURGICAL ANALYSIS, IT APPEARS THAT COMPRESSOR FAILURE WAS DUE TO THE SEIZURE OF THE TORQUEMETER MIDSHAFT BEARING CAUSING A SEVERE VIBRATION OR WHIP. AS A RESULT, TORQUEMETER TO COMPRESSOR COUPLING WAS BROKEN, CAUSING ENGINE FAILURE. (K) 2L72 4T4 TRT E282 20060913003202006091300320EU 2006 9 13 FQW2006F00000 120050801A5313 LONGERON WSK M18 PZLM18B 9810125EU FUSELAGE BROKEN D FQWGK NONE O OTHER ININSP/MAINT 1 SW1712BS 2287 1Z02718 TOP LT LONGERON BROKE JUST FWD OF HORIZONTAL STABILIZER FORWARD FITTING. (K) 1L71 3R A47EU 20060922000942006092200094SW 2006 9 22 AC2A105034 120050712A7332304466302 PRESSURE SWITCH BELL 427 427 1182207SW PWC PW207 PW207D NE FUEL SYSTEM MALFUNCTIONED E AC2AO OTHER N FALSE WARNING CRCRUISE 1 SO07427GT 56044 PCEBF0099 IMPENDING BYPASS LIGHT CAME ON IN FLIGHT / REPLACED SWITCH. 1G71 3U3 U R00001RCE42NE 20060922000952006092200095SW 2006 9 22 AC2A105018 120050731A7332304466301 PRESSURE SWITCH BELL 427 427 1182207SW PWC PW207 PW207D NE FUEL SYSTEM MALFUNCTIONED E AC2AD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SO07427CK 56043 PCEBF0098 NR 2 FUEL FILTER LIGHT CAME ON/ REPLACED THE TRIPLE SWITCH. 1G71 3U3 U R00001RCE42NE 20060922001142006092200114EU 2006 9 22 O3X06089371 120050923A3250AIR139086 PISTON ROD BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP STEERING JACK CRACKED A O3XAO OTHER O OTHER NRNOT REPORTED 1 SO03937AE 937 AIRCRAFT WAS TAXING FROM THE GATE FOR TAKEOFF. THE NOSE WHEEL STEERING BECAME UNRESPONSIVE. AIRCRAFT RETURNED TO THE GATE AREA INSPECTION REVEALED THAT THE NOSE WHEEL STEERING JACK SHAFT HAD SHEARED AT THE ROD END ATTACH AREA THE JACK WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. AD RELATING TO THIS PART WERE COMPLIED WITH DURING OH. AD, LUB AND SHIMMING OF THE JACK WAS COMPLIED WITH. THE JACK IS LUBRICATED ON ALL ODD (B) CHECK INSPECTIONS. (K) 2L72 4T4 TRTA56EU E4WE 20061010001482006101000148EA 2006 10 10 MASA200602250 120050908A5270 TARGET CNDAIRCL600 CL6002B19 1900309EA EMERGENCY EXIT OUT OF ADJUST A MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW07592ML 7410 ASH 7195 RDU - LT EMERGENCY EXIT CAUTION IN FLIGHT. MX ADJUSTED PROX SENSOR TARGET. 2L72 4F RTA21EA 20061013000972006101300097GL 2006 10 13 C2XABT055 220050808A726123075579 SUMP EMB 145 EMB145XR 3260214SO ALLSN AE300 AE3007A GL NR 1 ENGINE CRACKED G C2XAH DEACTIVATE SYST/CIRCUITS KBJFLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NRNOT REPORTED 1 SW2713123 145688 CAE312329 CREW REPORTED SMOKE IN CABIN. TURNED OFF PACK NR 2 AND SMOKE CLEARED. EWR MAINTENANCE TROUBLESHOT, DETERMINED ENGINE NR 1 CAUSING SMOKE IN CABIN. AIRCRAFT MAINTENANCE FERRIED TO BTV WITH NR 1 BLEED OFF. BTV MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE. OPS CHECKED AND LEAKED CHECKED GOOD. AIRCRAFT RELEASED FOR SERVICE IAW TASKCARD NR 6271001. FRONT SUMP CRACKED, SUMP WAS CRACKED ALLOWING OIL TO SEEP INTO BLEED AIR SYSTEM. 2L72 4F4 FRT TE6CH 20061018000362006101800036NE 2006 10 18 PG9A099168 220050202A75329550164950 BLEED VALVE UROCOPEC130 EC130B4 8680989EU TMECA ARRIELARRIEL2B NE ENGINE FAILED E PG9AO OTHER J WARNING INDICATION NRNOT REPORTED 1 WP19132GC956 3756 23060 AMBER GOV LIGHT ILLUMINATED, VEMD DISPLAYED FAIL CODE 130. REPLACED WITH SERVICABLE PART. 1G72 3U3 U H9EU E00054EN 20061017001182006101700118NM 2006 10 17 MWEA060230 120050512A27014083700903 CONTROL COLUMN BOEING717 717200 1383700NM COCKPIT DISCONNECTED A MWEAK NONE F FLT CONT AFFECTED NRNOT REPORTED 1 GL13910ME 55174 RUDDER LIMIT FAULT ON ENGINE AND ALERT DISPLAY AND CONTROL COLUMN DISCONNECTED. PERFORMED FAULT ISLOATION MANUAL TASK OR RETURNED TO SERVICE WORK, LIGHTNING STRIKE OVERSPEED, CONTROL COLUMN DISCONNECTED, RUDDER LIMITER, ADJUSTED AIR DATA INERTIAL REFERENCE UNIT, ENGINE ELECTRICAL CONTROLLER, VERSATILE INTERGRATED AVIONICS, PITOT STATIC CHECK OF CAPTAIN AND F/O'S ALTERNATE SYSTEM. NTSB REQUIRED REMOVED AND REPLACED AIR DATA INERTIAL REFERENCE NR 1 & NR 2, FLIGHT CONTROL COMPUTER NR 1 & NR 2 AND GROUND PROXIMITY WARNING SYSTEM COMPUTER. RE-SUBMITTED REJECTED SDR ORIGINALY MWEA050043. 2L72 4F TRA6WE 20061117001872006111700187WP 2006 11 17 AALA20061012 120051108A213320219742 ACTUATOR DOUG DC9 DC982 3022082WP CABIN PRESSURE INOPERATIVE A AALAGA O2 MASK DEPLOYED UNSCHED LANDING O OTHER CLCLIMB 1 SW21501AA 49738 ORD INFLIGHT T2301/08NOV, SHORTLY AFTER TAKEOFF AIRCRAFT HAD PRESSURIZATION PROBLEM. CREW DROPPED OXYGEN MASKS AND RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED OUTFLOW VALVE ACTUATORS, SELECTOR, BOTH PRESSURE CONTROLLERS, AND LEFT OXYGEN CANISTER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20071003000492007100300049SO 2007 10 3 EPUA23092005A 220050923A8530SA52000A20P PUSHROD CESSNA207 207A 2073604CE CONT O520 IO520F 17032SO ENGINE BENT E EPUAK NONE O OTHER ININSP/MAINT 1 AL037306798 20700558 293203R ENGINE RUNNING ROUGH REPORTED. MX REMOVED ALL PUSHRODS FOR INSPECTION. NR 5 CYLINDER PUSHRODS (INTAKE AND EXHAUST) BENT. NR 4 CYLINDER PUSHROD (EXHAUST) BENT. NR 2 CYLINDER PUSHROD (EXHAUST) BENT. 1H71 3O3 O A16CE E5CE 20061204000712006120400071NM 2006 12 4 AWXA200601982 120050628A531365617777 STRINGER SPLICE BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 MCN - STRINGER SPLICE CHANNEL CRACKED, BS 359, S15L. REPLACED STRINGER SPLICE CHANNEL, BS 359, S15L IAW AWA ER 03-5301-05193-SS2 . 2L72 4F RTA16WE 20061204000702006120400070NM 2006 12 4 AWXA200601981 120050628A53206517684642 INTERCOSTAL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 MCN - INTERCOSTAL WEB CRACKED, BS 294.5, S7L. REPLACED INTERCOSTAL WEB, BS 294.5, S7L IAW AWA ER 03-5301-05193-SS2. 2L72 4F RTA16WE 20061204000722006120400072NM 2006 12 4 AWXA200601983 120050705A532065165096 FITTING BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 MCN - INTERCOSTAL CLIP CRACKED, BS 350, S16L. REPLACED INTERCOSTAL CLIP, BS 350, S16L IAW AWA ER 03-5301-05193-SS2. 2L72 4F RTA16WE 20061204001132006120400113NM 2006 12 4 AWXA200500842 120050628A53206517684638 INTERCOSTAL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 MCN - INTERCOSTAL WEB CRACKED, BS 294.5, S12L. REPLACED INTERCOSTAL WEB, BS 294.5, S12L IAW AWA ER 03-5301-05193-SS2. REVIEWED AWA ER 03-5301-05193-SS2 AND ALL NON-ROUTINES ASSOCIATED WITH IT AND SUBMITED EACH AREA OF DAMAGE ON SEPARATE SDR'S. IN ADDITION UPDATED PART INFORMATION OF THIS REPORT AND MODIFIED THE PROBLEM DESCRIPTION TO REFLECT ONE ITEM. 2L72 4F RTA16WE 20061211003702006121100370EU 2006 12 11 109040705DG 120050407A6510 DRIVE SHAFT AGUSTAA109 A109 0260109EU ALLSN 250C 250C20B 03013GL TAIL ROTOR DAMAGED B JBZAO OTHER O OTHER NRNOT REPORTED 1 WP2722RX 7155 UPON UNCOWLING FOR A ROUTINE 600 HOUR INSPECTION, THE MAINTENANCE STAFF NOTED THE REMAINS OF A TAIL ROTOR DRIVE SHAFT RUBBER COLLAR (P/N: 109-0425-08-1) LAYING ON THE DECK BELOW ITS RESPECTIVE BEARING HANGAR. THE RUBBER COLLAR APPEARS HEAT DAMAGED AND BRITTLE, THE BEARING APPEARS TO HAVE EXCESSIVE DRAG. THE DRIVE SHAFT SHOWS INDICATIONS OF THE DRIVESHAFT SPINNING INSIDE THE COLLAR AND CAUSING EXCESSIVE WEAR. THIS BEARING ASSEMBLY IS DIFFICULT TO VISUALIZE ON DAILY INSPECTIONS BECAUSE OF ITS LOCATION. 1G72 3U3 U H7EU E4CE 20061228001212006122800121NM 2006 12 28 AALA20061282 120051215A3350 GUARD BOEING757 757223 1384957NM EMERGENCY LIGHT BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21672AA 25337 DFW - EMERGENCY LIGHT SWITCH GUARD AT FLIGHT DECK IS BROKEN. REPLACED THE EMERGENCY LIGHT SWITCH GUARD AT FLIGHT DECK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20070403000482007040300048NM 2007 4 3 AT0700034 120050119A5330 SKIN BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE BS 235 DENTED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15977AT 55036 DENT IN FUSELAGE AT STA 235.5, 4 INCH ABOVE LONG 18L. 3 INCH DIA BY .1 DEEP DENT HAS CREASED AT FRAME 237. INSTALLED REPAIR AT BS 237 TO 252 AND LONG 17 AND 18. IAW SRM 53-00-01 SIZE OF REPAIR 15.2500 INCH X 14.1250 INCH. 2L72 4F4 FTRA6WE E00061EN 20070402001472007040200147NM 2007 4 2 AT0700095 120051130A5330 SKIN BOEING717 717200 1383700NM FUSELAGE DENTED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15972AT 55033 SMOOTH DENT FS 237L ON FRAME .25 INCH ABOVE LONG. 18.4 X 1.5 X .067 INCH. D/X= 22.38 WHICH IS CONDITION 2 PER SRM 53-00-01 REPAIR 2 PAGE 210. REPAIRED DENT AT STA 237 BETWEEN L16L - L18L IAW B717 SRM 53-00-01. 2L72 4F TRA6WE 20070406001122007040600112NM 2007 4 6 AT0700064 120050118A5330 SKIN BOEING717 717200 1383700NM BS 251-256 S17L DENTED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15981AT 55040 FUSELAGE LEFT FWD AREA HAS 4 EA DENTS LOCATED AT APPROX STA 251-256 LONGERON 17. CUT OUT DAMAGED AREA AS PER B-717 MM 53-00-02 REPAIR 6, INSPECT CUT OUT AREA PER B-717 NDT SPM 06-10-01 .001, NO CRACKS FOUND. INSTALLED REPAIR PER B-717 SRM 53-00-01 REPAIR 6. 2L72 4F TRA6WE 20070406001612007040600161NM 2007 4 6 AT0700088 120050426A5320 FITTING BOEING717 717200 1383700NM TAIL CRACKED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15963AT 55024 RIGHT LOUVER ATTACH FITTING ON RIGHT SIDE OF TAIL COMPARTMENT CRACKED. INSTALLED DOUBLER REPAIR AT RIGHT LOUVER IAW AIRTRAN T/C 17-5320-2023. 2L72 4F TRA6WE 20070406001792007040600179NM 2007 4 6 AT0700078 120051024A5330 SKIN BOEING717 717200 1383700NM BS 248 L18L DAMAGED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15951AT 55013 FS 248 AT L18L HAS SMOOTH DENT WITH NO INTERNAL DAMAGE, NO LOOSE OR PULLED FASTENERS. MEASURES 2.5 X 2.5 X .048 INCH. CONDITION 2 WITH D/X 52.08. DENT IS ON L18L, PER RES 05-1279 REQUIRES HFEC OR DYE PENATRENT EVERY 500 HRS. INSTALLED DOUBLER REPAIR AT FS 248 AT L18L IAW B717 SRM 53-00-01 FIG 201. MATERIAL USED DOUBLER 2024T3.025 SIZE 23.75 X 17 INCHES, 2024T3.050 SIZE 18 X 14 INCHES, 2024T3.063 SIZE 25 X 4 INCHES. 2L72 4F TRA6WE 20070412001212007041200121NM 2007 4 12 AT0700017 120050207A5330 SKIN BOEING717 717200 1383700NM BS 237 DENTED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15956AT 55018 FUSELAGE SKIN HAS A DENT ON LEFT SIDE AT BS 237 NEXT TO CUSP LINE. INSTALLED DOUBLER REPAIR ON LEFT FUSELAGE SKIN AT STA 237 BETWEEN L-17L TO 18L AS PER B717 SRM 53-00-01 FIG 204. MATERIAL USED .032" 2024-T3. SIZE OF REPAIR 6.5 X 5.5 INCHES. 2L72 4F TRA6WE 20070412001272007041200127NM 2007 4 12 AT0700041 120050927A5330 SKIN BOEING717 717200 1383700NM BS 242 DENTED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15955AT 55017 DENT ON LEFT SIDE OF FUSELAGE STATION 242 AT L18 REQUIRES HIGH FREQ EDDY CURRENT INSP PER RES 05-1161. INSTALLED FLUSH SKIN PANEL REPAIR AT FS 242 AND L18 LEFT SIDE OF FUSELAGE IAW B717 SRM 53-00-01 FIG 201. 2L72 4F TRA6WE 20070412001282007041200128NM 2007 4 12 AT0700042 120050207A5330 SKIN BOEING717 717200 1383700NM BS 237 DENTED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15956AT 55018 FUSELAGE SKIN HAS A DENT ON LEFT SIDE AT BS 237 NEXT TO CUSP LINE. INSTALLED DOUBLER REPAIR ON LEFT FUSE SKIN AT STA 237 BETWEEN L-17L TO 18L AS PER B717 SRM 53-00-01 FIG 204. MATERIAL USED .032" 2024T3 SIZE OF REPAIR 6.5 X 5.5 INCH. 2L72 4F TRA6WE 20070412001312007041200131NM 2007 4 12 AT0700048 120050813A5330 SKIN BOEING717 717200 1383700NM BS 237 DENTED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15955AT 55139 FOUND DENT LEFT SIDE OF AIRCRAFT AT LONGERON 18 - 3 INCHES BY 1 INCH BY .0625 DEEP AT STATION 237. INSTALLED PERMANENT DOUBLER REPAIR AT STA 229 TO STA 264 BETWEEN L-16L TO 18L IAW B717 SRM 51-00-01 FIG 401. MATERIAL AND SIZE USED. DOUBLER 2024T3-.063 X 36.25 X 14.5 INCH, FILLER .050 X 35 X 14 INCH 2024 T-3, FINGER DOULBER 38.25 X 16.5 X .025, 7075T3. 2L72 4F TRA6WE 20070412001322007041200132NM 2007 4 12 AT0700049 120051001A5330 SKIN BOEING717 717200 1383700NM BS 229 DENTED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15955AT 55139 DENT ON LT SIDE FUSE BETWEEN L17 AND L18 NEAR STA 229. REQUIRES REPAIR WITHIN 4500 FLT HRS AS PER SRM 53-00-01 REPAIR TO COND 3. START TIME 9538:04. INSTALLED PERMANENT DOUBLER REPAIR AT BS 213.5 TO 229 AND BETWEEN L16L AND L18L (15.5 X 14) IAW B717 SRM 53-00-01 FIG 201 REPAIR 6. MATERIAL AND SIZE USED FILLER 2024T-3.050 X 15.5 X 14.0 DOUBLER, T-3 2024 .063 X 15 X14 INCH, FINGER DOUBLER 2024T, .025 X 18 X 17 INCH. 2L72 4F TRA6WE 20070412001652007041200165NM 2007 4 12 AT0700138 120050224A5330 SKIN BOEING717 717200 1383700NM BS 229-244 DENTED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15943AT 55006 FUSELAGE LT SIDE HAS 3EA DENTS AFT OF THE L1 DOOR. ALL THREE DENTS ARE BETWEEN LONGERONS 17L AND 18L. DENT (1) IS 35 INCHES FROM L1 DOOR AND IS 1.25" WIDE X .025" DEEP, DENT (2) IS 38.25 INCHES FROM L1 DOOR AND IS 1.75" WIDE X .025" DEEP WITH A .007" GOUGE, AND DENT (3) IS 40.5 INCHES FROM THE L1 DOOR AND IS 1.375" WIDE X .019" DEEP. THE SKIN IS ALSO CREASED AT STA 237 BY THIS DENT. INSTALLED DOUBLER REPAIR ON FUSELAGE SKIN RT BETWEEN STR 18L AND 16L IAW B717 SRM 53-00-01 FIG 201. SIZE OF INTERNAL DOUBLER 26 X 3.25 INCHES AND FINGER DOUBLER 17 X 6 INCHES. 2L72 4F TRA6WE 20070412001262007041200126NM 2007 4 12 AT0700035 120050616A5330 SKIN BOEING717 717200 1383700NM FS 239 DENTED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15988AT 55068 FUSELAGE DENT AT FS 239L BETWEEN L17 AND L18 MEASURES 6 X 8 X .125 INCH DEEP. INSTALLED PERMANENT REPAIR AT BS 239 BETWEEN LONG 17L AND 18L AS REQUIRED IAW B717 SRM 53-00-01 FIG 201, MATERIAL USED 2024T3.050, 16.25 X 18.5 AND 2024T3.025, 33.5 X 5.75 DOUBLER 2024T3.063, 25 X 4 INCH. 2L72 4F TRA6WE 20070412001222007041200122NM 2007 4 12 AT0700018 120050519A5330 SKIN BOEING717 717200 1383700NM FS 237 DENTED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15953AT 55015 FUSELAGE SKIN HAS DENT AT FUS STA 237 ABOVE LONG 18L. INSTALLED FLUSH REPAIR TO FUSELAGE SKIN AT FS 237 ABOVE LONGERON 18L DUE TO DENT. REPAIR 21 X 14 X 0.050 INCH, 2024 T3 INSTALLED PER B717 SRM 53-00-01 PG 208 FIG 201. 2L72 4F TRA6WE 20070417002892007041700289NM 2007 4 17 AT0700038 120050928A5330 SKIN BOEING717 717200 1383700NM FUSELAGE DENTED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15942AT 55005 FUSELAGE SKIN DENTED AT FS 237 LONGERON 17-18 LEFT. INSTALLED FUSELAGE SKIN REPAIR AT FS 237 BETWEEN LONGERON 17L AND LONGERON 18L IAW SRM 53-00-01 FIG 201, MATERIAL USED 2024 T3 .063, SIZE OF REPAIR 15.5" X 14.125". 2L72 4F TRA6WE 20070417002902007041700290NM 2007 4 17 AT0700039 120050929A5311 FRAME BOEING717 717200 1383700NM FUSELAGE CRACKED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15942AT 55005 AFT ACCESSORY COMPARTMENT CANTED FRAME AT BS 1178 CRACKED IN TWO PLACES LONGERON 16 TO 18 LEFT. INSTALLED FORMED CHANNEL REPAIR AT AFT ACCESSORY COMPARTMENT CANTED FRAME AT BS 1178 BETWEEN LONGERON 16L AND LONGERON 18L IAW B717 SRM 51-70-11 FIG 201. SIZE OF REPAIR 30 INCHES. 2L72 4F TRA6WE 20070417002912007041700291NM 2007 4 17 AT0700040 120050928A5310 DOOR FRAME BOEING717 717200 1383700NM FUSELAGE CORRODED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15942AT 55005 FWD CARGO DOOR LOWER CUTOUT WELL WITH CORROSION. INSTALLED REPAIR AT FWD CARGO LOWER DOOR JAMB IAW DC9/MD80 SRM 531-05 AND RES 05-123 DATED 09/30/05. 2L72 4F TRA6WE 20070417002922007041700292NM 2007 4 17 AT0700043 120051107A5320 STRUCTURE BOEING717 717200 1383700NM FUSELAGE CRACKED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15944AT 55007 RIGHT HAND VENT BOX CRACKED AT UPPER CORNER. INSTALLED ANGLE DOUBLER REPAIR AT RIGHT HAND VENT BOX UPPER CORNER IAW TASK CARD 17-5320-2023 AND B717 SRM 51-41-02. MATERIAL USED 7075 T6 .090 SIZE 6" X 6". 2L72 4F TRA6WE 20070417002862007041700286NM 2007 4 17 AT0700075 120050426A5340 ATTACH FITTING BOEING717 717200 1383700NM FUSELAGE CRACKED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15963AT 55024 RIGHT LOUVER ATTACH FITTING ON RIGHT SIDE OF TAIL COMPARTMENT CRACKED. INSTALLED DOUBLER REPAIR AT RIGHT HAND LOUVER IAW AIRTRAN T/C 17-5320-2023 FIG 1. 2L72 4F TRA6WE 20070426000812007042600081NM 2007 4 26 AT0700036 120050503A5330 SKIN BOEING717 717200 1383700NM FUSELAGE DENTED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15961AT 55023 RT SIDE OF FUSELAGE APPROX 12 INCHES AFT OF THE MIDDLE OF R1 DOOR DAMAGED. DAMAGE IS A DENT 12 INCHES LONG X 7.5 INCHES WIDE AND .150 DEEP. A SCRATCH THAT WAS 9 INCHES LONG X .100 WIDE AND .006 DEEP HAS BEEN BLENDED. INSTALLED FLUSH REPAIR AT STA 218 BETWEEN LONG 17 AND 16 RIGHT HAND IAW B717 SRM 53-00-01 FIG 201. MATERIAL USED 2024T3.063 DOUBLER, .025 2024T3 FINGERS AND .050 2024T3 FILLER. 2L72 4F TRA6WE 20070426000852007042600085NM 2007 4 26 AT0700054 120051202A5210 DOOR BOEING717 717200 1383700NM L1 DOOR BENT A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15994AT 55138 BEND FOUND IN BOTTOM EDGE OF MAIN CABIN DOOR PER RES 05-1513 HFEC AT EVERY C-CHECK. INSTALLED DOUBLER REPAIR AT BOTTOM EDGE OF MAIN CABIN DOOR IAW SRM 52-10-01 PAGE 202 FIG 201. MATERIAL USED 7075.T6.050 35 X 8 INCHES. 2L72 4F TRA6WE 20070613001582007061300158NE 2007 6 13 0089205 320051229A6111 BLADE EMB 120 EMB120 3260201SO HAMSTD14RF 14RF9 NE PROPELLER CRACKED B EY2RO OTHER C F.O.D. ININSP/MAINT 1 GL03 NICKEL SHEATH CRACK 2L72 4T RTA31SO 6 CP11NE 20070613001572007061300157NE 2007 6 13 0088585 320051118A61117826761 UNKNOWN EMB 120 EMB120 3260201SO HAMSTD14RF 14RF9 NE CORRODED B EY2RK NONE O OTHER ININSP/MAINT 1 GL03 CORROSION, BEYOND SPEC. 2L72 4T RTA31SO 6 CP11NE 20071213001812007121300181NM 2007 12 13 2005UALA00542 120050512A5340 STRINGER CLIP BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP2913UA 23674 AFT PIT STA 767 STR 23L & 22L STRINGER CLIPS DAMAGED. REMOVED AND REPLACED STRINGER CLIPS. 2L72 4F4 FRTA16WE E21EU 20071213001882007121300188NM 2007 12 13 2005UALA00543 120050512A5340 STRINGER CLIP BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29313UA 23674 AFT PIT STA 747 STR 23L & STR 22L ARE DAMAGED. REMOVED AND REPLACED STRINGER CLIPS. 2L72 4F4 FRTA16WE E21EU 20080507002372008050700237WP 2008 5 7 RRXA05141 120050126A5311 FRAME DOUG DC8 DC862 3021970WP FS 1220 S21L/R DAMAGED A RRXAK NONE O OTHER ININSP/MAINT 1 WP15994CF 45956 DURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLES IN THE UPPER CARGO COMPT FS 1220 AND L21R TO L21L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED DISCREPANT HOLES, FABRICATED DOUBLERS FROM 7075-T6 AND INSTALLED IAW EO NR 99-236 WITH APPROVED 8110-3 DATED 12-03-99. 2L74 4F 4A25 200805131 200805131 NM 2008 5 13 DL757080675 120050505A2530252010508 CHILLER BOEING757 757232 1384965NM GALLEY FUMES A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27693DL 29725 FUMES LIKE SULPHUR COMING FROM FWD GALLEY FOUND. F/C FREEZER AT FAULT REPLACED. 2L72 4F RTA2NM 20080716 NM 2008 7 16 DHL2008764525 120050525A5523 TAB BOEING727 727264 138408MNM RT ELEVATOR DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01764AT 22984 WHILE AT C CHECK, RT ELEVATOR CONTROL TAB O/B AFT CORNER DELAMINATED. CLEANED AND PREPPED DELAMINATED CORNER ON RT ELEVATOR CONTROL TAB, CUT OUT DELAM AREA APPROX 2 1/2 INCHES BY 2 INCHES, FABRICATED FILLER APPROX 2 1/2 INCHES BY 2 INCHES AND DOUBLER 4 INCHES BY 3 1/2 INCHES FROM .010 2024-T3 PO NR 9003621, BONDED FILLER AND DOUBLER SANDED SMOOTH SEALED AND PRIMED IAW B727 SRM 51-40-20. 2L73 4F A3WE 20090112 CE 2009 1 12 GUUA93353012505A 120050125A5347 SEAT TRACK BEECH 1900 1900D 1154162CE FUSELAGE BROKEN A GUUAK NONE O OTHER ININSP/MAINT 1 SO2981533 UE137 DURING SCHEDULED ROUTINE MX DISCOVERED RT SEAT TRACK FLOOR BOARD ATTACH TAB BROKEN AT FS 238. REPAIRED BROKEN RT SEAT TRACK FLOOR SUPPORT TAB AT FS 238. 2L72 4T RTA24CE 20090112 CE 2009 1 12 GUUA94053021005A 120050210A5347 SEAT TRACK BEECH 1900 1900D 1154162CE FUSELAGE BROKEN A GUUAK NONE O OTHER ININSP/MAINT 1 SO2916540 UE172 DURING SCHEDULED ROUTINE INSP DISCOVERED RT SEAT TRACK FLOORBOARD ATTACH TAB BROKEN AT FS 380. REPAIRED BROKEN RT SEAT TRACK FLOOR SUPPORT TAB AT FS380. 2L72 4T RTA24CE 20090112 CE 2009 1 12 GUUA94253042305A 120050423A5330 SKIN BEECH 1900 1900D 1154162CE FUSELAGE TORN A GUUAK NONE O OTHER ININSP/MAINT 1 SO2947542 UE198 DURING SCHEDULED ROUTINE MX DISCOVERED SKIN TEAR AT FS 475.5 RUNNING FROM THE SKIN EDGE AT THE AFT CARGO DOOR LOWER DOOR SILL EXTENDING DOWN 2.5 INCHES. STOP DRILLED TEAR AND INSTALLED EXTERNAL DOUBLER REPAIR. 2L72 4T RTA24CE 20051129001212005112900121 2005 11 29 YENA200581 120051119A324052615500 PRESSURE SWITCH EMERGENCY BRAKE LEAKING A YENAC ABORTED TAKEOFF KJ FLUID LOSS WARNING INDICATION TOTAKEOFF 1 EA15179JB168 168 REJECTED TAKEOFF AT 60 KTS FW T/O CONFIG WARNING. NO TAKEOFF BRAKES, FOUND NR 1 SYS EMERGENCY BRAKE PRESS BAD. REPLACED PER AMM 32-44-09-000-801-A & 32-44-09-801-A. ADJ & TEST PER AMM 32-44-09-720-801-A, INSP OF FUEL QUANTITY IND HARNESS REQUIRED - A CDCCL ITEM. 20051108001262005110800126 2005 11 8 ASOA05886 120051019A2120 ODOR UNKNOWN DETECTED A ASOAO OTHER O OTHER NRNOT REPORTED 1 SO27843AS FLT 4523 - DURING CLIMB-OUT FROM BWI-ATL, AT APPROXIMATELY 15,000 FEET, THE F/O NOTICED AN ELECTRIC SMOKE ODOR COMING FROM THE FLOOR NEAR THE F/O`S FEET. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED INTO IAD, WHERE IT LANDED SAFELY. MAINTENANCE INSPECTED ALL LIGHT FIXTURES, WIRES, AND COMPONENTS IN THE COCKPIT, AVIONICS BAY, AND THE AFT EQUIPMENT BAY. NO DEFECTS WERE NOTED. BOTH ENGINES AND AIR CONDITION SYSTEMS WERE RAN FOR 45 MINUTES WITH NO DEFECTS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 20050901001432005090100143 2005 9 1 ALG2005F00059 120050725A2560FDC27001692 SEAT BELT COCKPIT FAILED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03 DURING THE MONTH OF JULY, 3 SEAT BELT FAILURES WERE DISCOVERED, ALL THESE SEAT BELTS WERE MFG BY DAFIS AIRCRAFT PRODUCTION WHICH IS ONE OF BELL`S VENDORS. SEAT BELT PN FDC1700-169-2, LOT/BATCH NR 137705-1-2. ALL 3 FAILED SEAT BELTS ARE FROM THE SAME LOT/BATCH NR. THE ABOVE SEAT BELTS CAME FROM BELL AND WENT TO TRINIDAD. (K)